737-200 Standart Operating Procedures (SOP)

STANDARD OPERATING PROCEDURES

B 737 - 200 PREFACE

Issued : September 2007 Revision : 000 Page : PRE 1 - 1

PREFACE

The B 737 - 200 Standard Operating Procedures (S.O.P) Is a brief standard procedures of

Batavia Air flight crew’s operation.

It is a supplement to the B 737- 200 AOM / AFM, and should be used as legal approved

manual, however should some of the procedures in this manual have a disagreement with

the AOM / AFM, it is because those procedures had been adjusted to suit the company's

needs, thus superseding the procedures written in the AOM / AFM.

For the procedures that had not been covered by this SO.P, please refer to the AOM vol. 1.

The target of this manual is to concur upon a safe and efficient operation, uniformly built to

maintain airmen's self disciplines, therefore this manual is an obligatory.

Any doubt, and, or, questions concerning this manual, may be submitted to the B737 - 200

Pilot Training Manager or Its Chief Pilot.

Criticisms and suggestions will be highly appreciated.

Jakarta, September 2007

Director of Operations Capt. F. C. Tumbelaka

STANDART OPERATING

PROCEDURES B 737 - 200

TABLE OF CONTENT

Issued : September, 2007 Revision : 000 Page : TOC - 1

TABLE OF CONTENT

CHAPTER 1 : Introduction…………………………………………………………….

SOP

1 1

General………………………………………………………………………………………

SOP

1 1 Cockpit Seating………………………………………..…………………………………

SOP

1 2

Crew Coordination…………….…………………………………………………………

SOP

1 3

General………………..……………………………………………………………..

SOP

1 3

General……………………………………………………………………………….

SOP

1 4

Flight Management Computer (FMC)…………………………………….

SOP

1 4

Auto flight System Operation……………………………………………….

SOP

1 5

Manual / CWS Flight Operations…………………………………………

SOP

1 5

Checklist Procedures……………………………………………………………

SOP

1 7

Panel Scan Diagram…………………………………………………………………….

SOP

1 8

PF/Taxiing & PNF/Not Taxiing Areas of Responsibility…………………..

SOP

1 9

Amplified Procedures……………………………………………………………….…….

SOP

2 1

Pre-flight Procedure………………………………………………………………………

SOP

2 1

Initial Cockpit Preparation…………………………………………………………….

SOP

2 2

Exterior Inspection………………………………………………………………………

SOP

2 5

Exterior Inspection – Through Flight…………………………………………….. SOP

2

14

Cockpit Preparation – Captain……………………………………………………...

SOP

2 15

Cockpit Preparation – First Officer…………………………………………………

SOP

2 28

Pushback or Tow out Procedure……………………………………………………

SOP

2 35

Final Cockpit Preparation – Captain and First Officer……………………….

SOP

2 37

Engine Start Procedure………………………………………………………………..

SOP

2 38

After Start…………………………………………………………………………………..

SOP

2 40

Before Take-off……………………………………………………………………………

SOP

2 42

Before Take-off Procedure……………………………………………………………

SOP

2 44

STANDART OPERATING


TABLE OF CONTENT


Take off…………………………………………………………………………………….. SOP 2 46

Take-off Roll………………………………………………………………………..

SOP

2 46

Takeoff Flap Retraction Speed Schedule………………………………………..

SOP

2 53

After Takeoff Procedure……………………………………………………………….

SOP

2 53

Climb and Cruise…………………………………………………………………………

SOP

2 55

Reduce Climb Thrust…………………………………………………………….

SOP

2 57

Climb Speed………………………………………………………………………..

SOP

2 57

Altitude Selection…………………………………………………………………

SOP

2 58

Airplane Trim Technique………………………………………………………

SOP

2 58

Drag Factors Due to Trim Technique………………………………………

SOP

2 59

Turbulent Air Penetration………………………………………………………

SOP

2 59

Moderate to Severe Turbulent with Precipitation……………………..

SOP

2 60

Anti Ice Operation………………………………………………………………..

SOP

2 60

Descent and Approach Procedure………………………………………………….

SOP

2 62

Autoflight Descent………………………………………………………………..

SOP

2 65

Speed Brakes Operation………………………………………………………..

SOP

2 65

Parking Procedure………………………………………………………………..

SOP

2 85

Secured……………………………………………………………………………….

SOP

2 87

Flight Patterns…………………………………………………..................……………

SOP

3 1

Takeoff……………………………………………………………………………….

SOP

3 1

Precision Approach (AFS)……………………………………………………..

SOP

3 2

Non-Precision Approach (AFS)……………………………………………….

SOP

3 3

Circling Approach (AFS)………………………………………………………..

SOP

3 4

Flight Director ILS………………………………………………………………..

SOP

3 5

Visual Traffic Pattern…………………………………………………………….

SOP

3 6

Standard Callouts…………………………………………………………………………..

SOP

4 1

Duties At and After Minimum…………………………………………………

SOP

4 2

STANDART OPERATING


TABLE OF CONTENT


Additional Callouts………………………………………………………………..

SOP

4 3

Auto flight System Callouts……………………………………………………

SOP

4 3

Precautionary Callouts…………………………………………………………..

SOP

4 4

Briefing……………………………………………………………………………………………

SOP

5 1

Takeoff Briefing……………………………………………………………………

SOP

5 1

Approach and Landing Briefing………………………………………………

SOP

5 2

Post Landing………………………………………………………………………..

SOP

5 4

STANDARD OPERATING

PROCEDURES B 737 – 200

LIST OF EFFECTIVE PAGES

LIST OF EFFECTIVE PAGE

Issued : September, 2007 Revision : 000 Page: LOEP 1

CHAPTER PAGE REVISION CHAPTER PAGE REVISION

CONT. PAGE CP 1 000 2 2 000 PREFACE PRE 1 000 2 3 000

TABLE CONT. TC 1 000 2 4 000 TABLE CONT. TC 2 000 2 5 000 TABLE CONT. TC 3 000 2 6 000

LOEP LOEP 1 000 2 7 000 1 1 000 2 8 000 1 2 000 2 9 000 1 3 000 2 10 000 1 4 000 2 11 000 1 5 000 2 12 000 1 6 000 2 13 000 1 7 000 2 14 000 1 8 000 2 15 000 1 9 000 2 16 000 1 10 000 2 17 000 1 11 000 2 18 000 1 12 000 2 19 000 1 13 000 2 20 000 1 14 000 2 21 000 1 15 000 2 22 000 1 16 000 2 23 000 1 17 000 2 24 000 1 18 000 2 25 000 1 19 000 2 26 000 1 20 000 2 27 000 1 21 000 2 28 000 1 22 000 2 29 000 1 23 000 2 30 000 1 24 000 3 1 000 1 25 000 3 2 000 1 26 000 3 3 000 1 27 000 3 4 000 1 28 000 3 5 000 1 29 000 1 30 000 1 31 000 1 32 000 2 1 000


B 737 - 200 CHAPTER 1

INTRODUCTION

Issued : September 2007 Revision : 000 Page : 1 - 1

INTRODUCTION General

The Standard Operating Procedure B 737-200, In order to provide Batavia Aircrew with more detailed instructions on specific company procedures and night techniques, this flight Standard Book has been published. .

The structure of this supplement is based on additions to the standard Boeing Operations Manual. After some general subjects, it follows Normal Procedures, covering a night from start to finish thereafter, several non-normal night procedures are described. These chapters are also meant to support standardization during simulator and flight training.

In case of differences with other documentation, especially on procedural matters, this document will have precedence. However, this document can never overrule AFM restrictions, Boeing Operation Manual Bulletin, tile Dispatch Deviation Procedure, and does not intend to be in conflict with the air laws of any country where Batavia flight arc operated. Whenever FAA and CM rules are mentioned in the Operation Manual and AFM, the FAA rules are to be observed


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Cockpit Seating It is Batavia policy to let the role of. Pilot - flying (PF) and pilot-not-flying (PNF) alternate between Captain and Co-pilot as much as possible. The assignment of cockpit duties (PF and PNF) is subject to Captain's discretion (SCD), and should be done is advance of the actual flight (e.g. during flight preparation). Assignment of PF duties to the Co-pilot should be with the intention that he fulfill these duties for at least a whole sector. When assigning PF and PNF duties for a flight, the Captain shall take the following into account :

- Adverse or marginal conditions (meteorological, performance or other) - Experience level of Co-pilot - Restricted airports - Restrictions for newly assigned Captains

The Captain retains final authority and responsibility at all times, irrespective of duty allocation. Should he wish to take over control, he will clearly state: "I HAVE CONTROL" Should the PF wish to hand over control, he will clearly state: "YOU HAVE CONTROL" In all cases, transfer of control shall be acknowledged.


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Crew Coordination Introduction Good cockpit crew-coordination should contain at least the following elements:

- Mutual supervision ( monitoring & cross-checking ) - Exchange of information ( communication ) - Distribution of workload - Support of follow crew member

Prominent benefits of resulting teamwork are:

- An increase in safety, through detection and correction of individual errors. - An increase in efficiency, through the organized use of all existing resources

Some of the "tools" to ,archive the above are

- Checklist, and their prepare use - Proper Briefings - Standard callouts - Standard pl1raseology - Well defined division of tasks for PF and PNF, for the various phase of flight

These procedural items will be covered in the following chapters

General The main task of the PF is "to control aircraft flight path", with or without the use of the auto flight system. The main ask of the PNF is to monitor the performance of tile PF / aircraft combination and to take care of tile A TC R/T communication. All other duties will be shared between tile two pilots. Tile way in which these tasks are divided depends mainly upon the following variables:

- Automatic or manual flight - Normal or non - normal operation -

However, the following basic rules are always applicable :

- Keep each other "in the loop". Announce all intentions und actions and acknowledge (as applicable). In other words 'COMMUNICATE (verbal and non verbal) Deviation from standard procedures, or errors in judgment, is to be reported at once to other pilot. Standard warning call are: ‘bank” when the maximum maneuvering bank limit is exceeded

- During final stage of approach (inside OM or below 1,000 ft) “ speed high/low” when the speed deviates more than +10/-5 kts from Final approach speed (FAS) “Sink rate” When the rate of descent exceeds 1,000 fpm “…Dots high/low” When deviating 1 dot or more from ILS glide slope


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INTRODUCTION


- Monitor all automated functions for proper operating cross check their performance

by other means on a regular basis. - Checklist reading must always be done aloud, whether it is a "challenge a response"

or "read-and-do" checklist. Configuration changes

- Gear and flap selections shall be made by the PNF, upon command of the PF. Before making any selection, the PNF will satisfy himself that operating limitations and flight procedures allow the configuration change; if not, he will inform the PF.

- After verification of the resulting indication, the following applies:

1. Landing Gear - resulting indication will be announced by the PNF, e.g.: "Gear is

UP" (after take off or go - around) 2. Flaps - PNF will announce "Flaps are UP" after verifying indications.

- The PF will verify every configuration announcement of PNF by checking tile respective indicators silently.

Checklist usage Normal checklists are used by the crew to ensure that airplane condition is acceptable for flight and to operate the airplane and its systems properly during each phase of flight. The following general rules apply:

- During normal operation, procedures and actions may be performed by recall; thereafter he checklist is used to verify completion of all relevant items.

- The Captain shall initiate checklist reading on the ground, the PF in flight. - Reading of normal checklist, in flight, shall be done aloud by the PF and respond to

by the PF, with the following exceptions: . a. AFTER TAKEOFF checklist: no response by PF required. b. DESCENT-APPROACH checklist : response by PF only on items: - ALTIMETERS

- IAS bugs - In case of a disagreement between the reply as given the PF, and the proper

response (according checklist), reading of the checklist shall be discontinued until the discrepancy is resolved.

- Whenever checklist reading has been interrupted, it is the responsibility of the PNF to resume checklist reading at the appropriate time.

- It is the responsibility of both PF and PNF to ensure that checklist items have been accomplished properly. When a checklist response is given by the PF, both pilots will visually check proper control setting or indication. In other words: don't just give the reply, but also look at what you get!

- When an improper indication is noticed, the PF will continue to control or monitor aircraft flight path. The will verify that system controls are properly positioned. Then, if necessary, he will check the related circuit breaker and test related system lights.

- Completion of each checklist will be announced with the statement " …………………CHECK LIST COMPLETE".


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Flight Techniques The use of all available resources, such as autopilot and F/D is encouraged; the following light modes can be distinguished:

- Automatic Flight: Autopilot ON, CWS or any other mode - Manual Flight :" Autopilot not engaged, F/D ON or OFF

Task allocation During automatic flight , the PF normally carries out selections and settings himself. The PNF follows PF settings on his own F/D panel. During manual flight, the PNF will carry out selections on command of the PF. Auto-flight Monitoring Tile APD ( Approach Progress Display ) and position of tile switches on tile flight shield panel are normal references for the actual state of the A/P and F/D and shall be carefully monitored by both pilots. After any selection or setting tile resulting APD and / or changes in switches position of A/P or F/D must be checked for correctness and be called out by tile pilot who made the selection. Tile other pilot confirms with "CHECK". All unwanted, abnormal or uI1expectecl APD, A/P and F/D switches position changes must be called out by either pilot and be confirmed by the other pilot. Crew Coordination - Automatic flight. During automatic flight, the PF normally carries out shield selection and setting himself as follow: PF : - announce the selection or setting (e.g. “VOR / LOC) (this will prompt the PNF to monitor)

- Perform selection of setting - Monitor APD changes

PNF : - Monitor APD changes - Verify resulting APD as correct - Respond “CHECK”

Automatic Mode Change Approach Modes Change-over from ARMED (amber) to ENGAGED (green) mode of VOR/LOC and G/S: PF : - announce “ Localizer Capture” “Glide slope Capture” PNF : - Verify APD indications

- respond “check”


B 737 - 200 CHAPTER 1

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Standard callouts Standard callouts are utilized for the following purposes:

- to indicate awareness of certain flight phase or aircraft position. Examples;

- “V1” - “1000 to go” (1000 ft. prior to level-off, during climb or descent) - “localizer alive” - “100 above”(100 ft. above minimums) - to warn the PF of (impending) deviations or exceedances e.g. speed high/low, bank,

sink rate, etc. Standard callouts are normally accomplished by the PNF, the PF will verify the condition or location from his instruments, and acknowledge. If the PNF omits a required call, the PF shall make it. The main benefits of standard callouts are:

- increased “situational awareness” of both pilots - safeguard against unnoticed pilot incapacitation.

Announcements Most of the “inter-pilot communication (as related to operation of the airplane) will be in the form of brief and to the point announcements, as follows:

- initiation of certain actions (e.g. Captain “Starting Engine No……………..)

- Certain indication or observations (e.g. Co-pilot “ Oil pressure Rising”)

- All change in flight mode, as selected by the PF during automatic flight (e.g. PF: TURBULANCE MODE SET”)

- All change in autopilot usage (e.g. PF: “ Autopilot ON”, or Autopilot Elevator Channel OFF”)

Most announcement will be made by the pilot who task the action, or makes the observation, as applicable; some of them can be made by either pilot. Most announcement will be acknowledged by the other pilot with the word” CHECK”. Proper use of “Standard Callouts “and ”announcements” will promote:

- a structured and brief way of crew communication - the monitoring process by the PNF


B 737 - 200 CHAPTER 1

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Standard Phraseology To minimize confusion and misunderstanding, standard phraseology shall be used during all phase of flight. All wording has been chosen as being exact, concise, easy to say and easy to understand. Avoid jargon. Configuration commands Selection of flaps and gear are made by the PNF, upon the following commands of the PF: FLAPS UP FLAPS TEN FLAPS THIRTY FLAPS ONE FLAPS FIFETEEN FLAPS FORTY FLAPS TWO FLAPS TWENTY-FIVE FLAPS FIVE GEAR DOWN GEAR UP Configuration Announcements After completion of a configuration change, the resulting indication will be announced by the PNF in the following manner “ Gear is up” “ Flaps are up” Thrust settings The following phrenology will be used to command thrust setting: “SET THRUST” “SET CLIMB THRUST” “SET MAXIMUM CONTINUES THRUST” “SET GO-AROUND THRUST”


B 737 - 200 CHAPTER 1

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` PRE-FLIGHT PROCEDURES The appropriate pre-flight procedures will be completed prior to each flight. The required procedures are performed from memory. Checklist are to verify that critical items affecting safety have been accomplished. Any lights that are not illuminated during a system test will be checked by pressing-to-test the affected light. The initial cockpit preparation is to be accomplished:

• By either Captain or Co-pilot. • On the First departure of each day • At each crew change • After a maintenance rectification. • At the discretion of the Captain.

PREPARATION Exterior Safety Inspection The Captain is responsible for ensuring the Exterior Safety Inspection is performed prior to each Flight. Check flight control are unobstructed. Check doors and access panels (not use) properly secure, ports and vents unobstructed and air craft free of damage or fluid leakage. Check wheel chocks in place and ground locking pins removed. Check tire condition and gear struts not fully compressed. See Boeing Manual Vol. 1 for expand check.


B 737 - 200 CHAPTER 1

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The items to be inspected at each section are separately detailed in the following aircraft diagrams and the associated explanations. Nose Section / Gear Area:

A. TOTAL AIR TEMPERATURE PROBE for damage and dust removed. B. STALL WARNING VANE for damage. C. PITOT / STATIC PROBES (Capt on top, Co-Pilot an Bottom) for damage, security,

and dust covers removed. D. RADOME AND CONDUCTOR STRIPS for security. E. WINDSHIELD WIPERS for damage. F. WHEEL WELL LIGHT (2), Switch on and lights and the nose gear inspection light are

operating, NOSE GEAR LOCKING PIN Removed NOSE GEAR VIEWER LENS clean NOSE GEAR SHUBBERS installed NOSE GEAR WHEEL HYDRAULIC COMPONENTS for leaks.

G. SHOCK STRUT not completely compressed and not leaking oil. H. NOSE GEAR TYRES AND WHEELS general condition, inflation.

I. NOSE GEAR DOORS for security and damage.

J. GEAR DOWN INDICATORS for red arrows on locking braces aligned and clean.

K. E & E Compartment closed, latched and flush with surface.


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Right Forward Fuselage :

A. CO-PILOTS SLIDING WINDOW EMERGENCY EXIT HANDLE Flush with surface B. PITOT/STATIC PROBE for damage, security and dust covers removed.

C. CREW AND PASSENGER OXYGEN PRESSURE checked and panel closed

D. OXYGEN Thermal Discharge Disc (green) installed

E. Alternate Static Port (unheated) for condition of static port.

F. Lower Anti-collision Light cover and general condition.

DME and Transponder Antennas for condition.

G. Right Pack Ram Air Deflection and Air Inlet Door for deflector condition. H. Right Wing Illumination Light for Operation and general condition.

I. Inboard Landing and Runway Turn-Off Lights for Operation and condition.


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Right Main Gear Area :

A. Main gear Types for inflation and condition B. Brake wear indicator length remaining, Brake must be set for proper indication, and if

pins are Hub Cap installed. C. Main gear Strut for minimum extension of approx. 4 fingers and check for leaks. D. Landing Gear strut Doors and lower strut door seal for security. E. Gear Down Indicator with the red marks on locking brace aligned and clean.

Main Landing Gear Locking Pin removed.

F. Wheel well Lights (2 floods lights and 2 landing gear inspection lights) for operation System A hydraulic reservoir Indicator on reservoir above refill (FF), and no leaks. System B Hydraulic Reservoir for security and leaks. Standby Hydraulic Reservoir For security and Leaks. Brake Accumulator Gauge for air pressure reading of 1000 psi minimum. For correct indication system B pressure must be zero

G. Main Landing Gear Viewer is Clean.


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Right Wing and Engine :

A. Leading Edge Flaps for condition. B. Engine Cooling for damage. C. Engine Accessory Doors secure. D. Engine Nose Inlet and Inlet Guide Vanes for general condition, inlet guide vanes and

fan blades for damage, vortex dissipater for general condition and for cracks around dissipater attachment to cowling.

E. Engine Dome and Control Sensors (pt2, static pressure, and temperature probes) for security and damages.

F. Engine Outboard cowl latches (for general condition of cowling and latches are secured).

G. Defueling Panel access doors closed and latched. H. Refueling Panel access doors closed and latched. I. Dripsticks (5) agree with alignment mark on lower wing surface cue drip sticks is

located in board of the engine. J. Wing Fuel Tank Surge Vent Opening is Clear K. Wing Navigation Light (green) and position light (white) for operation and damage.

Wing Tip Oscillating Position Light (if fitted) for Operations and damage. L. Upper Anti-Collision Light cover and general condition

VHF antenna for general condition HF antenna (if fitted) connected to forward and aft attachment points

M. Static Discharge Wicks (4) for Security, damage, or missing. N. Right Aileron and tab for security O. Trailing Edge flaps for Security and damage P. ENGINE EXHAUST AREA (EGT,EPR Probe, and turbine blades) for damage or

missing check for any oil or fuel in the exhaust area. Check oil colder for leaks and security. THRUST REVERSER DEFLECTION DOORS are stowed, flush with cowling, and no hydraulic leaks RAM AIR EXHAUST LOUVERS are fully open. Engine APT MOUNT INDICATOR has the tip of the red arrow in the green band.


B 737 - 200 CHAPTER 1

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Aft Fuselage and Trailing area :

A. Main pressure out FLOW VALVE fully open B. APU FIRE EXTINGUISHER PRESSURE GAUGE reads approximately 600 Psi

C. APU FIRE DISCHARGE DISCS for 1 yellow and 1 red

D. APU INLET DOOR Opening is clear.

E. NEGATIVE PRESSURE RELIEF DOOR is flush with surface

F. PRESSURE RELIEF SAFETY VALVE (2) to ensure opening are clear.

APU ACCES DOOR is closed and latched APU GROUND DRAIN MAST for fuel leaks and underside of tail section for APU oil leaks. APU FUEL DRAIN MAST for fuel leaks. If fuel is dripping contact maintenance.

G. VERTICAL STABILESER and RUDDER for damage. STATIC DISCHARGE WICKS ($) for General condition or missing.

H. HORIZONTAL STABILIZER AND ELEVATORS FOR DAMAGE. STATIC DISCHARGE WICKS (3 on each elevator) for general condition or missing.

I. ELEVATOR FEEL PITOT PROBES for general condition.


B 737 - 200 CHAPTER 1

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Left Main Gear Area :

A. MAIN GEAR TYRES for inflation and condition. B. BRAKE WEAR INDICATORS length remaining. Brake must be set for proper

indication, and if pin are flush with brake flange then contact maintenance. RUB CAP installed.

C. MAIN GEAR STRUT for minimum extension of approximately 4 finger and check for leaks.

D. LANDING GEAR DOOR AND SEAL STRUT DOOR and strut door seal for security.

E. GEAR DOWN INDICATORS with the red marks on looking brace aligned and clean.

MAIN LANDING GEAR LOOKING PIN removed.

F. WHEEL WELL AREA for general condition and hydraulic leaks. WHEEL WELL LIGHT (2 floods lights 2 landing gear inspection lights) for inspection. SYSTEM B HYDROLIC RESERVOIR for security and leaks. STANDBY HYDROLIC RESERVOIR for security and leaks. REVERSER ACCUMULATOR PRESSURE (basic aircraft only) minimum of 1000 Psi. BRAKE ACCUMULATOR GAUGE for air pressure reading of 1000 Psi minimum, for correct indication system A pressure must be zero.

G. MAIN LANDING GEAR VIEWER is clean. H. ENGINE FIRE EXTINGISHER BOTTLES (for approximate pressure if 600 Psi)

I. LANDING GEAR ISOLATION VALVE are lock wired with handles Aft.


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Left Wing Engine :

A. TRAILING EDGE FLAPS for security and damage. B. ENGINE EXHAUST ARE (EGT, EPR Probes, and Turbine blades) for damage or

missing, check ………..any oil Fuel in the exhaust are. Check oil cooler for leaks and security. THURST REVERSER DEFLECTION DOORS ARE stowed, flush with cowling, and no hydraulic leaks RAM AIR EXHAUST LOUVERS are fully open. Engine APT MOUNT INDICATOR has the tip the red arrow un the green band.

C. DRIPSTICKS () agree with alignment make on lower wing surface. One drip sticks is located inboard of the engine.

D. RIGHT AILERON AND TAP for security. E. STATIC DISCHARGE WICKS (4) for security, damage, or missing. F. WING FUEL TANK SURGE VENT OPENING is clear. G. WING TIO NAVIGATION LIGHT (green) and position light (white) for operation and

damage. WING TIP OSCILLATING POSITION LIGHTS (if fitted) for Operation and damage. LOGO LIGHT (if fitted) for operation and damage. OUTBOARD LANDING LIGHT for damage and flush with surface.

H. LEADING EDGE SLATS for general condition. I. ENGINE COWLING for damage. J. ENGINE ACCESORY DOORS secure. K. ENGINE NOSE INLET AND INLET GUIDE VANES for general condition inlet guide

vanes and fan blades for damage, vortex dissipater for general condition and for cracks around dissipater attachment to cowling.

L. ENGINE DOME AND CONTROL SENSORS (pt2, static pressure, and temperatures probe) for security and damage.

M. ENGINE OUTBOARD COWL LATCHES for general condition of cowling and that latches are secured.

N. ENGINE COWLING for damage O. LEADING EDGE FLAPS for general condition.


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Left Forward Fuselage :

A. LEFT PACK RAM AIR DEFLECTRO AND AIR INLET DOOR for extended and air inlet open

B. LEFT WING ILLUMINATION LIGHT for operation general condition. C. INBOARD LANDING AND RUN – WAY TURN OFF LIGHTS for operation and

condition. D. ALTERNATE STATIC PORT (unheated) for condition of static port. E. FORWARD OUTFLOW VALVE opening is clear.

Throughout the External Inspection, the security of all doors shown in diagram below to be checked.


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Interior Safety Inspection :

MAINTENACE STATUS............................................................................................Checked The Captain and the First office will verify the maintenance status is acceptable for flight and ensure agreement with authorized dispatch deviation. Battery .................................................................................................................................On Verify battery switch guard down, the DC voltmeter at BATT, at lease 23 V DC and ammeter 0 A. B Hydraulic Pump Switch..................................................................................................Off Verify system A and B electric hydraulic pumps OFF and the hydraulic pump low PRESSURE light are illuminated.


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Landing Gear Lever.......................................................................................................Down

The green landing gear indicator light illuminated. Flap Lever .......................................................................................................................... Set

Position the FLAP lever to agree with the FLAPS position indicator. Radar switches...................................................................................................................Off Ground power (if available) ...............................................................................................On Overheat detection.......................................................................................................Check

- Over heat detection switches – NORM - Test switches – OVERHEAT - Verify that MASTER CAUTION, OVHT / DET annuciator, - APU DET INOP lights are illuminated

Fire / Overheat Warning...............................................................................................Check

Test Switch – HOLD TO FIRE Verify warning bell sound and FIRE WARN, MASTER CAUTION lights and OVHT / DET anunciator illuminate.

FIRE WARN light – PUSH Verify FIRE WARN lights and alarm bell cancel. Verify ENG. 1, APU and ENG. 2 fire switch and ENG. 1 and ENG. 2 OVERHEAT lights illuminate. If AC busses are powered Verify WHEEL WELL lights illuminate.

Extinguisher test switch ...............................................................................................Press

Verify green Extinguisher test light illuminate. APU........................................................................................................... Start & On Busses

Hold start switch momentarily at start, then release to ON. Observe battery voltage drop when the starter is engaged. When the blue GEN OFF BUS light illuminates, place both generator bus switches ON. Verify both BUS OFF light are extinguished

FLAP LEVER.....................................................................................................................SET

Position the flap lever to agree with the flap position indicator EMERGENCY EQUIPMENT..........................................................................................Check


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FIRE AXE.....................................................................................................................CHECK GEAR SAFETY PINS ........................................................................................... ON BOARD

Verify all 3 landing gear pins onboard. CIRCUITS BRAKERS (P-6)....................................................................................CHECKED

Verify circuit breakers are in or collared in compliance with dispatch requirement ELECTRONIC MASTER SWITCHES................................................................................. ON FLIGHT RECORDER..................................................................................................TESTED

Set trip number and date. FLIGHT RECORDER test switch – TEST FLIGHT RECORDER OFF light – extinguished FLIGHT RECORDER test switch – NORMAL Note : IF tape is available, but not moving at the proper speed or broken, light

Illuminates in 15 second MACH AIRSPEED WARNING TEST SWITCH ............................................................PRESS

Verify clacker sounds. STALL WARNING TEST SWITCH..................................................................................TEST

Verify control column vibration when each switches is paused. OXIGEN SYSTEM...................................................................................................CHECKED

Verify crew oxygen valve is OPEN, crew oxygen quantity meets minimum dispatch requirement, passenger oxygen switch is guarded NORMAL and the PASS OXY ON light is extinguished

CAUTION : Switches actuation will cause deployment of passenger oxygen mask.

REVERSER LIGHTS ...................................................................................................CHECK

Verify both reverser light are extinguished. CIRCUIT BREAKERS (P-18)..................................................................................CHECKED RAIN REPELLENT .................................................................................................CHECKED AIRCRAFT DOCUMENTS......................................................................................CHECKED See BATAVIA operation manual for required documentation to be on board NOTE: Drawer must be closed and locked and locked during take, landing, and turbulence.


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COCKPIT PREPARATION – CAPTAIN

The Cockpit Preparation Check is accomplished by both captain and Officer prior to every engine Start. (Refer to panel scan diagram).

Cockpit preparation ............................................................................................... Complete

Verify the interior and exterior inspections have been performed. Escape strap .................................................................................................................Check

Ensure strap is connected to structure. OXYGEN MASK & REGULATOR .................................................................................Check

Mask – Adjust Supply lever – ON Normal / 100% - 100% Verify oxygen available and satisfactory mike operation.

SUN VISOR AND SMOLKE GOGGLES .......................................................................Check

Check they are available and properly stowed. Static Source Selector ............................................................................................... Normal LIGHT TEST .................................................................................................................Check

Master light test and switch – TEST Both Pilots : Use individual test switches or test feature to check appropriate light which do not. Illuminate during light test. Use scan flow to check all lights flashing or illuminating. Position light test switches to BRIGHT – DIM as required.

Flight control Panel......................................................................................................Check

YAW DAMPER switch – ON Switch guards – Down First flight of the day, accomplish stand by rudder check. (Ensure System B pumps are off during check)

Transfer switches....................................................................................................... Normal

Note : On first flight of the day accomplished a TRANSFER CHECK.


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FUEL......................................................................................................... KGS & PUMPS ON Verify FUEL VALVE CLOSED light illuminated dim and FILTER BYPASS lights extinguished. CROSSFEED selector – CLOSED

Verify VALVE OPEN light – Extinguished Note : For the first flight of the day or at a crew change, verify fuel cross feed valve

operation. CROSSFEED selector – OPEN Verify VALVE OPEN light illuminate bright then dim. CROSSFEED selector – CLOSED Verify VALVE OPEN light illuminates bright then extinguished.

Fuel quantity – Check

Verify total fuel quantity meets dispatch requirement. IF required test in accordance with the Supplementary Normal procedures. Note: Do not press QTY TEST if the aircraft is being fuelled.

FUEL PUMP switches (for tank containing fuel ) – ON

LOW PRESSURE lights – Extinguished IF the centre tank contains less than 1000 Kgs of fuel, select centre tank fuel pumps OFF until after takeoff. CUTION L: If a LOW PRESSURE light does not extinguished when the switch is turned ON this may Indicate a locked fuel pump rotor. Place the switch to OFF to prevent possible damage to the pump.

Electrical .......................................................................................................................Check

AC METER selector – APU GEN, Volt / Freq – NORMAL (115 ± VAC/ 400 + 10 Hz) DCMETER selector – BAT, Volt/Amp – normal (26 ± 4 VDC) BATTERY switch – ON (guarded) Galley power switch – ON CSD LOW OIL PRESSURE lights – illuminated. CSD HIGH OIL TEMP lights – Extinguished STANDBY POWER switch – AUTO (guarded) Generator drive DISCONNECT switch – NORMAL (guarded & wire locked) DRIVE TEMP Switch – IN CSD temperature indications – NORMAL Generator ammeter – Zero BUS TRANSFER switch – AUTO (guarded) TRANSFER BUS OFF light – Extinguished BUS OFF lights – extinguished GEN OFF BUS light – illuminated APU GEN OFF BUS light – extinguished (APU operating and selected ON busses 1 and 2)

CIRCUIT BREAKER and PANEL light control.................................................... As desired


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EQUIPMENT COOLING switched........................................................................... NORMAL

OFF lights – Extinguished EMERGENCY EXIT LIGHTS .......................................................................................ARMED

Guard – Down NOT ARMED light – Extinguished

PASSENGER SIGNS.......................................................................................AS REQUIRED

NO SMOKING switch – ON (Non – smoking sectors) FASTEN BELTS switch – ON (if turbulence is anticipated on departure)

WINDOW HEAT.................................................................................................................. ON

ON 10 minutes before takeoff green lights illuminated (select ON prior to Line up) Verify OVERHEAT lights – Extinguished ON lights – Illuminated (except at high ambient temperatures)

PITOT HEAT......................................................................................................................OFF

Select ON Prior to Line up WING and ENGINE ANTI – ICE switches........................................................................OFF

VALVE OPEN lights – Extinguished HYDRAULICS........................................................................................................... NORMAL

Ground interconnect close, system A & B pump ON Cockpit voice recorder ................................................................................................Check

TEST button – Push After a slight delay, observe pointer moves twice into the green band.

Pressurization indicators ............................................................................................Check

Cabin differential pressure – Zero Flt alt – planned cruise level Land alt – destination field elevation Cabin attitude – 200 feet below destination point Cabin rate of climb – Index

Exterior lights ...................................................................................................................SET

Check position lights for day night operation


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ENGINE START Switches ................................................................................................OFF

Note : engine start master valve switch – disarm / differences Flight Director...................................................................................................................SET

Heading selector – R/W heading Pitch control – pull up

AUTO PILOT.........................................................................................................disengaged Marker Beacon Switch........................................................................................ as required Clock................................................................................................................................... Set FLIGHT INSTRUMENTS .............................................................................SET & X- CHECK

Altimeter – Set Adjust barometric indicator. Observe proper altitude and no flags. RMI – Check Position ADF / VOR selectors as required. Observe present hading and no inappropriate flags HIS – check Observe indication zero and OFF flag not in view. ADI – check Observe proper attitude and no warning flags. Airspeed indicators – check Observe proper speed and no flags.

Stand by Horizon............................................................................................................... Set

Pull cage knob to erect horizon. Verify no flag Fuel Quantity Indicators ..........................................................................................Checked

Do not press QTY TEST if the aircraft is being Fuelled. Will stop refuel Fuel flow reset (as installed) ......................................................................................... reset


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Engine Instrument........................................................................................................Check

EPR – 1.0 EPR KNOB – SET (manual or auto) N1 – ZERO EGT – Normal N2 – Zero Fuel Flow – ZERO Oil Pressure – Zero Oil Temperature – NORMAL

Engine oil quantity ........................................................................................................check

Press the engine oil quantity test switch, both indicator move toward zero. Release switch indicator return to original setting.

Antiskid .............................................................................................................................. ON

Guard down. Antiskid INOP extinguished AUTO BRAKE ...................................................................................................................OFF

Verify AUTOBRAKE DISARM Light extinguishes Radio, Radar, Transponder ............................................................................ set & standby Speed Brake lever .............................................................................................Down Detent Reverse Thrust Lever....................................................................................................Down Thrust Levers.................................................................................................................Close START LEVERS........................................................................................................ CUTOFF STABILIZER TRIM CUTOUT switches ................................................................... NORMAL WHELL WELL FIRE WARNING SYSTEM......................................................................TEST


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RADIOS AND NAVIGATION .............................................................................................SET

VHF COMM Radio Frequencies – SET (preset) SET VHF 1 to required ATC frequency, Set VHF 2 ATI, Company frequency, or Emergency Frequency when away from terminal areas as required Audio Control Panel – SET Verify all switch and selector correctly set. VHF NAV Radio Frequency – SET AND IDENTIFY FOR DEPARTURE. AUTO / MAN Switch – Manual ADF Radios – SET Verify ADF’s ON Required frequencies set and identified.

Electronic Panel Light Control............................................................................ As desired RUDDER & AILERON TRIMS ............................................................................... free & zero Seat................................................................................................................................Adjust Rudder Pedals ..............................................................................................................Adjust

Adjust rudder pedals to permit full rudder pedal and brake application. The seat and rudder pedals should be adjusted so that it is possible to apply maximum braking with full rudder deflection. If rudder pedals are to be displaced, hold the nose wheel steering wheel to prevent nose wheel turning. Do not turn adjusting crank rapidly when approaching extremes of travel.


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INTRODUCTION


COCKPIT PREPARATION – CO-PILOT The Cockpit Preparation Check accomplished by both Captain and first Officer prior to every engine Start. (Refer to panel scan Diagram). Cockpit preparation ............................................................................................... Complete

Verify the interior and exterior inspections have been performed. Escape strap .................................................................................................................Check

Ensure strap is connected to structure. OXYGEN MASK & REGULATOR .................................................................................Check

Mask – Adjust Supply lever – ON Normal / 100% - 100% Verify oxygen availability and satisfactory mike operation.

SUN VISOR AND SMOKE GOGGLES .........................................................................Check

Check they are available and properly stowed Static Source Selector ............................................................................................... Normal Air conditioning System.....................................................................One pack, bleeds ON

AIR TEMPERATURE selector – As desired Temperature selector – As desired RAM DOOR FULL OPEN light – illuminated GASPER FAN switch – ON Air Conditioning PACK switches – One ON ISOLATION VALVE switch – AUTO ENGINE BLEED air switches – ON APU BLEED air switch – As required.

PERZUATION CONTROL AND INDICATORS .................................................................SET

Cabin differential pressure – Zero FLT ALT – Planned Cruise level LAND ALT – DESTINATION FIELD ELEVATION CABIN RATE selector – INDEX CAB ALT Indicator – set 200 feet below destination field elevation. FLT.GRD Switch – GRD PRESSURIZATION MODE Selector – AUTO Verify AUTO FAIL Light extinguished.


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INTRODUCTION


FLIGHT INSTRUMENTS .........................................................................SET & X-CHECKED

Altimeter – Set Adjust barometric indicator. Observe proper altitude and no flag. RMI – Check Position ADF / VOR selector as required. Observe present heading and no inappropriate flags HIS – Check Observe present heading and no flags. Vertical speed indicator – Check Observe indication zero and OFF flag not in view. ADI – check Observe proper altitude and no warning flags Airspeed indicators – check Observe proper speed and no flags.

GPWS ..........................................................................................................................CHECK

Pressing test switch for more than 2 seconds test all the GPWS visual and aural Warnings.

Altitude alert set (for departure) .....................................................SET FOR DEPARTURE ADF Radios .......................................................................................SET FOR DEPARTURE

Tune and identify station. Set on ADF


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INTRODUCTION


TAKE OFF BRIEFING After Captain & Co-pilot preparation accomplished PILOT FLYING (PF) must brief PLIOT NON FLYING (Co-pilot briefing in brackets):

- If I (you) reject the take off , I (you) will call aborting, apply maximum braking, close the thrust levers, and select reverse thrust. You (I) will ensure the speed brakes are deployed.

- If the emergency occurs after V1, I will continued the take off (unless relieved) and

you will monitor my actions and the flight path. The following items, as applicable, must also be covered:

1. Take off configuration (e.g. reduced thrust, flaps & packs) 2. Engine inoperative departure details.

3. Radio, radio aids, transponder, and SID

4. Minimum flap retraction altitude.

5. Noise abatement.

6. Safety altitude, transition, and planned / cleared altitudes.

7. addition factor (e.g. notams, inoperative equipment)

For normal line operations it is acceptable to use the abridged take off briefing format. Abridged Take Off Briefing This will be my / Your standard take off…….(then cover items (1) to (7) above) The Captain calls “Before START CHECKLIST DOWN TO LINE” when before start scan completed to rudder aileron trims. The Firs officer reads the checklist and the captain respond and the Firs Officer reports “ BEFORE START CHECKLIST COMPLETED TO THE LINE”


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Takeoff data card.................................................................................................COMPLETE

External ASI bugs should be set at V1, VR and flap retraction speeds. The internal Cursor bugs should be set at V2. The external (outer) bug set at flaps up Maneuvering speed.

After completing paper work the Captain calls “BEFORE START CHECKLIST BELOW THE LINE” when the TAKE OFF DATA are set and Prior to push and start the engine The Co-pilot reads the checklist and the captain responds. The Co-pilot reports “BEFORE START CHECKLIST COMPLETED”

FLAPS – UP MANEUVERING SPEED


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INTRODUCTION


Pushback our Tow Procedure This procedure is required when the airplane is to be pushed back or towed away from the terminal or loading area. Flight interphone contact with Ground Crew ...................................................Established Captain will established communication with Ground Crew and Pilot with the ATC Nose gear steering bypass lockout pin ................................................................. Installed The pin should be install when staring engine while pushing back otherwise when pin not available the engines will be started when pushback accomplished and “A hydraulic Electric pump switched OFF before pushback tow bar connected. Confirm if required “STEERING BYPASS PIN INSTALLED< ALL DOORS AND PANELS CLOSED”’ When cleared for push back or tow out: Parking brake...........................................................................................................Released Captain shall released Parking Brakes when called by Ground Crew. ANTI COLLISION LIGHT.................................................................................................... ON Captain position Anti Collision Light switch to ON, ensure hydraulic “A” pump OFF, Ground Interconnect Closed Note : do not start push back for B 737-200 ICAO PUSHBACK PHRASEOLOGY

PHRASE ACTION BY CAPTAIN

1 2 3 4 5 6 7 8 9 10

Capt : ENG : Capt : ENG : ENG : Capt : ENG : Capt : ENG : Capt :

Ready for pushback Confirm brakes released & System A depressurized. Brakes released, System A depressurized. Commencing pushback. Pushback completed, confirm brake set Brakes set, remove towbar. Towbar removed. Request engine start. You may start engine Start engine No:………

Switch off system A hydraulics pumps, check A pressure ZERO Released parking brake, rests feet on cockpit floor. Set parking brake. Start engine


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Final Cockpit Preparation – Captain and Co – pilot

After pushback/start-up approval has been obtained by the Co – pilot and the Captain call for “Push Back & Start”

........................................CLEAR FOR PUSHBACK & START .............................................. Doors ............................................................................................................................Closed

Verify all doors caution lights extinguished. AIR CONDITIONING PACK ..............................................................................................OFF START PRESSURE............................................................................................................PSI

The minimum start pressure is 30 psi at sea level. Allow 0.5 psi reduction for each 1.000 ft above sea level.

ANTI COLLISION LIGHT.................................................................................................... ON

Captain shall position anti collision light switch to ON to alert the Ground Crew and Tower that the engines will be started and/ or aircraft shall be commencing movement.

The Captain calls “BEFORE START CHECKLIST BELOW THE LINE”.

The Co-pilot reads the checklist and the Captain responds. The Co-pilot reports “BEFORE START CHECKLIST COMPLETED”

THE CAPTAIN WILL ACCOMPLISH THE ENGINE START PROCEDURE Parking brake..................................................................................................................... Set

After aircraft stop parking brake – set Hydraulic System “S” pumps switches .......................................................................... ON

System “A” pressure checked TowBar / Steering Bypass pin – disconnected / Removed


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Checklist Procedures

CHECKLIST INITIATED BY READ BY RESPOND BY Before start down to the line

Captain calls for checklist when before start scan is completed to departure briefing. And to be completed when documents and take off data received.

F/O

CAPT

Before start below the line

Captain call for checklist when all doors are closed & start / pushback clearance is received.

F/O CAPT

After start Captain call for checklist when the After Start scan is completed

F/O CAPT

Before Take-Off Captain call for checklist during taxi and when the situation permits.

F/O CAPT

After Take-Off PF call for checklist when flaps are up / no light & the situation permits and to be completed when passing transition altitude or 10.000 ft AGL whichever is higher.

PNF PNF

Descent Approach PF calls for checklist anytime during descent and to be completed when passing transition level or 10.000 ft AGL Whichever is lower.

PNF PF

Landing PF calls for landing checklist down to flaps, after landing gear is extended and flaps 15 is selected. The Checklist is completed when Landing Flaps is Selected.

PNF PF

After landing Captain calls for after landing Checklist at Taxi speed and when the situation permits

F/O F/O

Shutdown Captain calls for the checklist when the Shutdown scan is completed

F/O CAPT

Scan checks are accomplished from memory prior to executing the checklist. The Checklist in the used to verify the scan checks were correctly accomplished. Safety of the flight and flight conditions permitting are factors to be considered prior to calling for or accomplishing a checklist.


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AMPLIFIED PROCEDURES


Amplified Procedures Pre-flight Procedures The appropriate pre-flight procedures will be complete prior to each flight. The required procedures are performed from memory. Checklist are used to verify that critical items, affecting safety have been accomplished. Any lights that are not illuminate during a system test will be checked by pressing-to-test the affected light. The pre-flight Procedures consist of as applicable, the preparation and the before start checks. The initial Cockpit Preparation is to be accomplished:

• By the First Officer prior to assuming normal crew position. • On the first departure of each day. • At each crew change. • After a 2 hour transit. • After a maintenance rectification. • At the discretion of the Captain.


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Engine Start Procedure

Captain First Officer Announce engine start sequence Normal starting sequence is 2,1

Announce “STARTING ENGINE No---------“ Position ENGINE START switch to GRD. Verify START VALVE OPEN light illuminate Start timing.

Press 30 psi min Monitor Drop In start pressure Verify START VALVE OPEN Light illuminate Star timing

Verify increase in N2 RPM Verify oil pressure rising and respond “CHECK”

Verify increase in oil pressure by max of 30 second and calls “OIL PRESSURE RISING” when observed.

Verify increase in N1 RPM Position engine start lever to IDLE detent and Note time when:

• N1 rotation is observe • N2 RPM reaches 20 %. • At a minimum of 15% N2 (max

monitoring).

Note time

Verify fuel flow (360-450 kph) and EGT indication At 35-40% N2 RPM check ENGINE START switch move to OFF; if not, position start switch to OFF N2 ± 36%

Verify proper duct pressure indication as the Engine Start switch moves to OFF and report “STARTER CUTOUT, PRESSURE RESTORED” After the START VALVE OPEN light extinguished.

Monitor N1, N2, EGT, fuel flow and oil pressure for normal indication as the engine accelerates and stabilizes at idle. Verify START VALVE OPERN light extinguished.

Standard day, sea level, approximate stabilize idle indication for JT8D: - 15 - 17

• EPR - 1.06 - 1.07 • N1 RPM - 33% - 35% • N2 RPM - 56 % - 59% • EGT - 300-400°C - 380 °C • Fuel flow - 1200 pph/550 kph - 1250 pph /567 kph • OIL PRESS - 40-50 psi - 40 – 50 psi


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CAUTION : Normal engine start consideration:

• Advancing engine start lever to idle prematurely can cause s “HOT” start. • Keep hand on engine start lever while observing RPM, EGT, and fuel flow until

stabilized • If fuel is shut off inadvertently (by closing engine start lever) do not reopen engine

start lever in an attempt to restart engine. • Failure of ENGINE START to hold in GRD until starter cut out RPM is reached can

result in a “HOT” start . do not re-engage ENGINE START switch until N2 RPM is zero.

Note: Accomplish the Aborted Engine Start procedure for one or more of the following

condition.

• No N1 rotation after N2 reaches 20% • No oil pressure indication by 30 seconds • No increase in EGT within 20 seconds after the engine start lever rise to idle. • No increase or a very slow increase in N1 or N2 after EGT indication. • EGT rapidly approaching or exceeding the start limit.


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PHASE of FLIGHT or

EVENT

PILOT FLYING

PILOT NOT FLYING

Release the brake and advance thrust lever to approximately 1.40 EPR and calls “CHECK ENGINE STABILIZED”

Observe Engine parameters stabilized and normal Calls “STABILZED” Start Timing Gradually advance Thrust Lever and calls “SET TAKEOFF THRUST”

Hold light forward pressure on the control column. Maintain directional control using rudder pedals

Advance thrust levers to takeoff EPR and calls “TAKEOFF THRUST SET”

Commencing Takeoff roll

Captain guards the thrust levers until V1

Monitor engine parameters. Verify oil pressure in green band.

80 Knot

Verify speed and respond “CHECKED”

Calls “EIGHTY”

V1

Verify V1

Calls “V1”

VR

Commence smooth rotation to Acquire pitch attitude.

Alls “ROTATE”


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PHASE of FLIGHT or EVENT

PILOT FLYING

PILOT NOT FLYING

POSITVE LIFT- OFF With positive rate of climb

Observe positive rate of climb and Respond “GEAR UP”

Verify and calls ”POSITIVE CLIMB” Select gear up – Vs = 500’ up Monitor gear retraction. - altimeter up

Takeoff/ Climb Maintain pitch

Monitor engine instruments and crosscheck flight progress.

Above 400 ft AGL, as Applicable

Respond “CHECK” Calls “FOUR HUNDRED”

At 1000 ft AGL (or any other altitude specified by Authorities or Specific Takeoff Chart)

Respond “SET CLIMB TRUSHT” Reduce attitude to acceleration Pitch (approximately 10° or 1000 FPM up). Verify speed and calls “FLAPS ONE” or” FLAPS FIVE” V2 + 15 Flaps 1 V2 +…../190 Flap up

Calls “ONE THOUSAND” Verify speed V2 + 15 then select flaps 1 or 5

At 170/180 (if Takeoff flaps 10/15)

Verify speed and respond “FLAPS ONE”

Calls ‘ONE SEVENTY” or “ TWO EIGHTY”. Select Flaps 1

At 190/200 Verify speed and respond “FLAPS UP” Gear lever OFF

Calls “ONE SEVENTY” or “ONE EIGHTY” Select flaps UP.

Flaps retraction, Airplane accelerating. At flaps up Minimum Maneuvering Speed and flaps Up No - light

Respond “AFTER TAKEOFF CHECKLIST” Prefer reach 11.000’ A/P engaged (engaged A/P after aircraft at proper trim)

Verify Flaps Up/No light and calls “FLAPS UP-NO LIGHT”. And when situation permit: Accomplished and report “AFTER TAKEOFF CHECKLIST HOLDING AT…………………”

Caution : To avoid the possibility of the shoulder harness buckles snapping back and

inadvertently puling circuit breakers, hold both straps before releasing and then allow the straps to slowly retract to the stowed position.


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Phase of flight OR Event

PILOT FLYING PILOT NOT FLYING

Transition Altitude 11.00

Set altimeter to 1013.2 hPa / 29.92 In Crosscheck altimeter reading. Differences

10.000 ft Set schedule speed

Set external lights as required. Landing lights OFF Passenger sign as required. Cockpit door remain locked

(Set external lights). Verify that the altitude on altimeter and PRESSURIZATION CONTROL PANEL are in agreement. Review optimum altitude and accomplish step climb, if appropriate

(Night Operation) Final Cruise Altitude Once if cruising one hour or less, and every one hour if cruising more than one hour

Review One Engine Out Performance and Depressurization procedures. RVSM comply check (if applicable). MEA/MORA/GRID MORA and nearest suitable Airport.

Check AIRCOND and PRESSURIZATION

Prepare for arrival. Complete Approach briefing

Monitor and record weather at Destination and Alternate Airport. Prepare for arrival


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Phase of Flight Or Event PILOT FLYING PILOT NOT FLYING

Prior to TOD Complete Descent Approach briefing Where possible, set up the Approach Radio Aids Set altimeter bugs to landing minimum Verify landing weight Set VREF Flaps 30/40 and approach speeds on ASI

Descent Clearance Received

Set descent altitude in altitude alert window

Verify descent altitude correctly set

Top of Descent Verify cabin rate of descent. (Set external light for NIGHT operation)

Verify descent altitude correctly set

At transition level or 10.000 ft whichever is higher

Calls to initiate “DESCENT – APPROACH CHECKLIST” Verify and respond checklist

Accomplished Descent – Approach Checklist and report “DESCENT – APPROACH HOLDING AT………..”

Transition LVL Set and crosscheck altimeter reading QNH Transition LVL or 10.000 ft AAL whichever is lower

Verify and respond checklist.

Verify and report “DESCENT – APPROACH CHECKLIST COMPLETED”

10.000 ft AAL Verify Restriction speed Fasten belt ON. INBD Landing its ON. Set external lights for DAY ops.

Prior to INITIAL APPROACH FIX Or 5000 ft AAL Whichever is higher

Verify MINIMUMS. Approach COURSEs, ADF’s. VHF NAV’s and MARKER switches set for approach. Verify cabin Report - Received


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PRECISION APPROACH PROCEDURE

Precision autopilot approach are NOT permitted below MINIMUM. The PF will only execute APPROACH when the HIS localizer depict correct to the intercept course, and the approach clearance is received. The PF shall start configuring flaps 5 or flaps 100 when cleared for approach at initial approach altitude before approaching initial approach fix (or approx. 5 nm to FAP)

PRECISION APPROACH PROCEDURE ( A/P ) Phase of Flight

Or Event Pilot Flying Pilot Not Flying

At approx. 10 knots above the Flaps Up maneuvering speed

Calls “FLAPS 1” Verify Flaps / Status extension

Verify speed, respond “Speed Check” Select Flaps 1. Monitor flaps / stats extension.

Deceleration approx 10 knots above Flaps 1 Maneuvering speed

Call “FLAPS 5” Verify Flaps extension

Verify speed, respond “Speed Check” Select Flaps 5. Monitor flaps extension.

Cleared for approach and on intercept heading for final approach

Select VOR / LOC mode and calls “VOR / LOC ARMED”

Verify mode and respond “CHECKED”

Firs Positive inward movement of localizer bar.

Verify indication and respond “CHECKED”

Calls “LOCALIZER ALIVE”

Localizer capture

Verify indication and respond “CHECKED” Set heading bug to Go- Around Heading Select approach mode and calls “GLIDE SLOPE ARMED”

Calls “LOCARIZER CAPTURE” Verify GO – Around Heading correctly set. Verify mode and respond “CHECKED”

First positive movement or Glide Slope pointer

Verify indication and respond “CHECK”

Calls “GLIDE SLOPE ALIVE”

At one dot up

Verify indication and respond “GEAR DOWN, FLAPS 15, LANDING CHECKLIST” Verify flaps extension.

Calls “ONE DOT” Select Gear Lever down Verify speed, calls “Speed Check” Select Flaps 15 Monitor flaps / slats extension


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Respond Landing Checklist Perform Landing Checklist and Report ”LANDING CHECKLIST HOLDING AT FLAPS”.

PRECISION APPROACH PROCEDURE ( A/ P ) Phase of Flight

Or Event PILOT FLYING PILOT NOT FLYING

Glide Slope capture Verify Indication and respond “SET GO – AROUND ALTITUDE, FLAPS 25 “ Verify flaps extension.

Calls “GLIDE SLOPE CAPTURE”’ Set Go-Around Altitude Correctly. Verify speed, respond “Speed Check” Select Flaps 25. Monitor Flaps extension.

Calls “FLAPS 30/40, COMPLETE LANDING CHECKLIST” Verify flaps extension.

Verify speed, respond “speed check” Select Flaps 30/40 Monitor flaps extension.

Established on Glide Slope but NOT LOWER than 1000 ft AAL.

Respond Landing Checklist Complete Landing Checklist and Report “LDG CHECKLIST COMPLETE”.

At Outer Marker Check altitude and Respond “Marker switch OFF:”.

Calls ”OUTER MARKER” Select Marker Switch OFF

At 1000 ft AAL Respond “CHECK”’ Check Landing Flaps.

Calls “ONE THOUSAND”.

At 500 ft AAL Respond “CLEARED” or “NOT CLEARED”. (ATC clearance). Set Landing Lights.

Calls ‘ FIVE HUNDRED”

At 100 ft above DA/DH

Respond “CHECK”. Look for visual reference and callout

Calls “APPROACHING MINIMUM” Verify visual clues

Calls “MINIMUM”. Not later than DA/DH The PIC Call out “LANDING” or GO-AROUND

After callout Landing

Disconnect A/P. Callout ‘A / P Disconnect”.

Monitor and callout deviation.

At 100’, 50’, 30’, 10’ RA

Callout “ONE HUNDRED, FIVETY, THIRTY, TEN”. (if the aircraft is not equipped)


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Precision Approach Procedure ( MANUAL)

PRECISION APPROACH PROCEDURE ( MANUAL) Phase of Flight


At approx. 10 knots above Flaps Up maneuvering speed.

Calls “FLAPS 1”. Verify Flaps/Slats extension.

Verify speed, respond “Speed Check”. Select Flaps 5. Monitor Flaps extension.

Deceleration approx, 10 knots above Flaps 1 maneuvering speed.

Calls “FLAPS 5”. Verify Flaps extension.

Verify speed, respond “speed Check”. Select Flaps 5. Monitor Flaps extension.

First positive inward movement of localizer bar.

Verify indication and respond “CHECK”.

Calls “LOCALIZER CAPTURE”

Localizer capture.

Verify indication and respond “CHECK”. Set GO-AROUND heading.

Calls” LOCALIZER CAPTURE”. Verify Go-Around heading correctly set

At one up.

Verify indication and respond “GEAR DOWN, FLAPS 15, LANDING CHECKLIST”. Verify Flaps/Slats extension.

Calls “ONE DOT”. Select Gear Lever down. Verify speed, calls “ Speed Check”. Select Flaps 15. Monitor Flaps/Slats extension.

Respond Landing Checklist. Perform LANDING Checklist and Report “LANDING CHECKLIST HOLDING AT FLAPS”.

Glide Slope capture.

Verify indication and respond “SET GO-AROUN ALTITUDE, FLAPS 25”. Verify Go-Around Altitude correctly set. Verify Flaps extension.

Calls “GLIDE SLOPE CAPTURE”. Set GO-AROUND Altitude. Verify speed, respond “Speed Check”. Select Flaps 25. Monitor Flaps extension.


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PRECISION APPROACH PROCEDURE ( MANUAL)

Phase of Flight Or Event Pilot Flying Pilot Not Flying

Calls “FLAPS 30/40, COMPLETE LANDING CHECKLIST”. Verify Flaps extension.

Verify speed, Respond “Speed Check” Select Flaps 30/40 Monitor Flaps extension.

Established on Glide Slope but NOT LOWER than 1000 ft AAL.

Respond Landing Checklist Complete Landing Checklist and Report “LANDING CHECKLIST COMPLETE”.

At Outer Marker Check altitude and Respond “Marker switch OFF”.

Calls “OUTER MARKER”. Select Marker Switch OFF

At 1000 ft AAL Respond “CHECK” Check Landing Flaps.


At 500 ft AAL Respond “CLEARED” or “NOT CLEARED”. (ATC clearance).

Calls “ FIVE HUNDRED”. Set Landing Lights

Respond “CHECK”. Verify visual clues.

Calls “APPROACHING MINIMUM” Look for visual reference and callout.

Calls “MINIMUM”. Not later than DA/DH The PIC callout “LANDING” or “GO-AROUND”. After callout Landing Monitor and callout deviation. At 100’ , 50’, 30’ , 10’ RA Callout “ONE HUNDRED, FIVETY,

THIRTY, TEN”. (if the aircraft is not equipped)


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NON – PRECISION (VOR – DME / LOC – DME /VOR /NDB) APPROACH PROCEDURES

Note: Non – precision autopilot approaches are NOT permitted below MINIMUM. Prior to leaving the final Approach Fix, Set the altitude alert to the next higher 100 ft increment above MDA or Intermediate Altitude, for example MDA 1720, set 1800. Set Go-Around altitude only AFTER ALTitude HOLD is established at MDA For an NDB approach, HIS is set to VOR / ILS. The PF shall configure flaps 5 or flaps 10 when cleared for approach at initial approach altitude before approaching initial approach fix (or approx. 5 nm to FAF) or when parallel to inbound approach course.

Non Precision Approach Procedure ( A/P )

NON - PRECISION APPROACH PROCEDURE (A/P) Phase of Flight or

Event Pilot Flying Pilot Not Flying

At approx, 10 knots Above Flaps Up Maneuvering speed

Calls “FLAPS 1”. Verify flaps/ Slats extension.

Verify speed, respond “speed check”. Select Flaps 1 Monitor Flaps / Slats extension.

Decelerating approx, 10 knots above Flaps 1 maneuvering speed

Calls “FLAPS 1”. Verify flaps extension.

Verify speed, respond “speed check”. Select Flaps 5 Monitor Flaps extension.

On intercept heading and cleared for approach

Select VOR / LOC and calls “VOR / LOC ARMED”.

Verify mode and respond “CHECKED”

First positive inward movement of course


Call “ COURSE ALIVE”.

Course capture Verify indication and respond “CHECKED”. Set heading bug to GO-Around Heading.

Call “Course Capture”. Verify Go-Around Heading Correctly set.


B 737 - 200 CHAPTER 2



VOR / LOC APPROACH (A/P)

Phase of Flight Or Event Pilot Flying Pilot Not Flying

Set INTEMEDIATE APP ALTITUDE or MDA*

Verify Altitude correctly set

Calls “GEAR DOWN, FLAPS 15, LANDING CHECKLIST”. Verify flaps / Slats extension

Select gear lever down. Verify speed calls “Speed Checks”. Select Flaps 15. Monitor flaps/Slats extension.

At 90° onto final course or 2 nm to final Approach Fix and maintaining the final approach altitude.

Respond Landing Checklist Perform Landing Checklist and Report “LANDING CHECKLIST HOLDING AT FLAPS”.

Calls “FLAPS 25”. Verify flaps extension

Verify speed, calls “Speed checks”. Select Flaps 25. Monitor Flaps extension.

Final approach Fix and commencing descent or turning on the final track

( DO NOT SELECT FLAPS 25 FOR CIRLING APPROACH). During approach

Monitor approach progress. Look for landing cues.

Calls “ FLAPS 30/40, COMPLETE LANDING CHECKLIST” Verify flaps extension

Verify speed, respond “ Speed Checks” Select Flaps 30 / 40. Monitor flaps extension.

Established on final approach but NOT LOWER Than 1.000 ft AAL

Respond Landing Checklist Complete Landing Checklist and Report “LDG CHECKLIST COMPLETED”.


Calls “ONE THEOUSAND”

At 500 ft AAL Respond ‘ CLEARED” or “ NOT CLEARED”. (ATC clearance). Set landing lights.

Calls “FIVE HUNDRED”

At 100 ft above MDA Respond “CHECK” Verify visual clues

Calls “APPROACHING MINIMUM”. Look for visual reference and callout.

Respond “CHEK” Calls “MINIMUM” or “MDA” At MDA or Missed Approach Point (MAP) Verify ALT HoLD.

Set GO-Around Altitude. * Verify Go – Around Altitude Correctly set.


B 737 - 200 CHAPTER 2



VOR / LOC APPROACH (A/P)

Phase Of Flight Or Event Pilot Flying Pilot Not Flying

Calls “MINIMUM”. No later than Missed Approach point The PIC callout “LANDING” or “ GO-ARROUND”. After callout Landing Callout “A / P DISCONNECT”. Monitor and callout deviation. At 100’ , 50’, 30’, 10’ RA

Callout “ONE HUNDRED, FIVETY,THIRTY, TEN”. (If the aircraft is not equipped).

• Do not set GO – Around Altitude or MDA until Established at Alt Hold.


B 737 - 200 CHAPTER 2



Non Precision Approach Procedure ( MANUAL)

NON - PRECISION APPROACH PROCEDURE ( MANUAL) Phase of Flight

or Event Pilot Flying Pilot Not Flying

Approx. 10 knots above Flaps Up Maneuvering speed.

Calls” FLAPS 1” Verify flaps / Slats extension.

Verify speed, Respond “speed Check”. Select Flaps 1. Monitor flaps / slats extension.

Decelerating approx. 1 knots above Flaps 1 maneuvering speed.


Verify speed, respond “speed checks” Select Flaps 5 Monitor Flaps extension

First Positive inward movement of Course.


Calls “COURSE ALIVE”

Course capture Verify indication and respond “CHEKED” Set Go-Around heading

Calls “COURSE CAPTURE” VERIFY Go-Around Heading correctly set.

Calls “SET MDA”. Verify Altitude correctly set.

Set INTEMEDIATE APP ALTITUDE or MDA *

Calls “ GEAR DOWN, FLAPS 15, LANDING CHECKLIST” Verify flaps/slats extension.

Select gear down lever down. Verify speed calls “speed check” Select Flaps 15 Monitor flaps/slats extension.

At 90° onto final course or 2 nm to Final Approach Fix and maintain the final approach altitude.

Respond Landing Checklist

Perform Landing Checklist and Report “LANDING CHECKLIST HOLDING FLAPS”.


Verify speed calls “speed check” Select Flaps 25 Monitor Flaps extension

Final approach Fix and commencing descent or turning on the final track

(DO NOT SELECT FLAPS 25 FOR CIRCLING APPROCH) During approach

Monitor approach progress Look for landing cues.


B 737 - 200 CHAPTER 2



VOR / LOC APPROACH (MANUAL)

Phase of Flight


Calls “FLAPS 30 / 40 , COMPLETE LANDING CHECKLIST”. Verify flaps extension.

Verify speed, respond “ Speed check” Select Flaps 30 / 40 Monitor flaps extension.

Established on final approach but NOT LOWER Than 1.000 ft AAL

Respond Landing Checklist Complete Landing Checklist and report “LDG CHECKLIST COMPLETED”.



At 500 ft AAL Respond “CLEARED’ or “NOT CLEARED”. (ATC clearance).

Calls “ FIVR HUNDRED”. Set landing lights.

At 100 ft above MDA Respond “CHECK” Verify visual clues.

Calls “APPROACHING MINIMUM” Look for visual reference and callout.

Calls “MINIMUM” No later than Missed Approach Point The PIC callout “LANDING” or “GO-AROUND”. After callout Landing Monitor and callout deviation. At 100’, 50’, 300’, 10’, RA

Callout “ONE HUNDRED, FIVETY, THIRTY, TEN”. (If the aircraft is not equipped).

• Do not select MDA or Go-Around Altitude until established at ALT HoLD


B 737 - 200 CHAPTER 2



CIRCLING APPROACH

The approach category for circling approach is “D”. Pay special attention to the location of high go around and other obstacles. Briefing should cover determining the correct Go-Around procedure from any part of the circuit. The circling must be execute at or above the MDA and visual contact must be maintained all times. Prior to starting the base leg turn: Select flaps 30 / 40, set speed bug V ref + 5 Turn Flight Directors OFF. Disengage Autopilot and control the airplane MANUALLY. Complete THE LANDING CHECKLIST. The PNF sets the missed-approach heading and missed-approach altitude.

VISUAL APPROACH

The approach may only be execute when full visual reference to the runway and surrounding terrain can be maintained at all times. Use all available NAV aids as backup to visual clues. The description of the approach covers basically the situation where a circuit is required. When circuit is amended he distance to go to touchdown and interception of the visual glide path. PIC may request to make “VISUAL APPROACH” when • The pilot has the airport insight and can maintain visual reference to terrain. • The reported celling is not below the initial approach altitude, or • HE reports at initial approach altitude or at any time during the instrument

approach procedure that the visibility will permit a visual approach and he has reasonable assurance that the landing can be accomplished.

The PIC shall not cancel his IFR flight plan to make a visual approach and separation therefore shall be provide between the aircraft cleared for a visual approach and other arriving and departing aircraft. The visual approach procedure may save some flying time but also introduces the risk of an undershoot or landing at a work airport. Moreover it may create terrain clearance hazards if continues good separation/visibility is not assured. Therefore, if a choice of runway is available, preference should be given to a runway equipped with glide slope guidance, with due regard to other operational factors.


B 737 - 200 CHAPTER 2



Experience has shown that full use of available aids in the most effective means to prevent an undershoot or a landing on the wrong runway or airport. The PIC must be prepared for a go-around from any point of the visual approach.

VISUAL APPROACH

Phase Of Flight Or Event

Pilot Flying Pilot Not Flying

At abeam THR - Starting timing 35 sec ± 1 sec/kts win (normal) 25 sec ± 1 sec/kts win (short) 35 sec ± 1 sec/kts win (lowl)

- start timing

Calls “GEAR DOWN, FLAPS 15, LANDING CHECKLIST Verify flaps / slats extension.

Select gear lever down. Verify speed, calls “speed Check”. Select Flaps 15. Monitor flaps/slats extension.

After abeam THR • 25 sec (normal) • 15 sec (short) • 15 sec (low)

Respond Landing Checklist. Perform Landing Checklist and

Report “LENDING CHECKLIST HOLDING AT FLAPS”.

Time is up Start turning with 20° bank and

Descent 700 FPM (normal) Descent 1000 FPM (short) Level Turn (low)

Calls “FLAPS 25”. Verify flaps/slats extension.

Verify speed, call “speed check”. Select Flaps 25. Monitor flaps/slats extension.

On Base leg Adjust Base leg in order to be on final at 800 AAL on normal glide path (except for Low Level Circuit).

At but not lower than 1000 ft AAL

Disconnect A/P Verify.

At 1000 ft AAL Calls “CHECKED”. Calls “ONE THOUSAND Calls “FLAPS 30/40, COMPLETE LANDING CHECKLIST”. Verify flaps extension.

Verify speed, calls “ Speed checks”. Select Flaps 30/40. Monitor Flaps extension.

Turning final When approaching glide path

Respond Landing Checklist. Complete Landing Checklist and Report “LANDING CHECKLIST COMPLETED”’


B 737 - 200 CHAPTER 2



On Final Check Landing Flaps. Set missed-approach heading. Set missed-approach altitude.

At 500 ft AAL Respond “CLEARED” or “ NOT CLEARED”. (ATC clearance).

Calls “ FIVE HUNDRED”. Set Landing Lights.

The PIC calls “LANDING” or “GROUND”. At 100’ , 50’ , 30’, 10’ RA

Calls “ONE HUNDRED,FIFTY,THIRTY, TEN” ( if the aircraft is not equipped)

DELAYED FLAP APPROACH A delayed-flap approach is allowed only in Visual Meteorological Conditions. Use normal approach technique. At 2.000 ft AGL, select landing gear down and flaps 15. At 1.500 ft AGL, select flaps 25.

At 1.000 ft AGL, select landing flaps and decelerate to Final Approach speed (Vref + 5)


B 737 - 200 CHAPTER 2



DURING ROLL PROCEDURE

The landing roll procedure assumes the auto throttle and auto brakes are selected for landing. Use rudder to maintain airplane on centerline. Displacing the aileron into the wind assist directional controls.

Rudder pedal steering improves with a slight forward pressure on the control column. The aileron and rudder are effective until approximately 60 knots. Thereafter apply manual brakes consistent with the run way length remaining or to facilitate turnoff at a convenient point and speed. Do not use nose steering wheel until reaching taxi speed. After touchdown and during landing roll, the following procedures are accomplished during normal deceleration.

Phase of Flight Or Event

PILOT FLYING PILOT NOT PLAYING

Touch down Verify speed brake deploys and callout “SPEED BRAKE UP”. If NOT UP callout “SPEED BRAKE NOT UP”.

Landing Roll Monitor direction and deceleration. Reverse Thrust Select reverse thrust Verify REVERSERS UNLOCKED

light illuminates. Callout “REVERSERS UNLOCKED”. Monitor engine instruments. Advice PF of any engine limit being Exceeded or other abnormalities.

80 knots Apply brake. (if landing distance is not limited).

Callout “EIGHTY”.

70 knots Gradually reduce thrust to idle reverse

Callout “SEVENTY”.

60 knots Verify thrust near reverse idle Callout “SIXTY”. Turn – off speed Move the reverse thrust

levers to the full forward position.

Verify REVERSERS UNLOCKED Lights extinguished.

On the Captain’s command, First Officer initiates the AFTER LANDING checklist WARNING : Do not select reverse thrust prior to touchdown.

After reverse thrust has been initialed, a full stop landing must be made.


B 737 - 200 CHAPTER 2



REVERSE THRUST APPLICATION

At touchdown, rapidly raise the reverse Thrust Lever UP and move them aft to interlock, then to number 2 detent. Modulate reverse thrust are required and avoid exceeding engine limits. Conditions permitting, limit reverse thrust to 1.40 EPR for passenger comport. Initiate reverse thrust cancellation at 70 knots so as to be at idle reverse by 60 knots and canceling Reverse thrust by turn-off speed. If an engine surges or stalls during reverse thrust operation, quickly shutdown is necessary. It is recommended to operate the engine at or near idle for three minutes prior to shutdown, otherwise the minimum engine idle or near idle shutdown time in one minute. The use of MAXIMUM REVERSE THRUST to a complete stop is only permitted under EMMERGENCY situation. If taxiing with one engine shut down, the crew should be aware of system requirement, i.e., Hydraulic, brakes, and electrical.

MANUAL BRAKING

Upon application of reverse thrust, apply a smooth and steady brake pedal pressure consistent with the remaining runway length available. Do not attempt to modulate the braking by releasing and re-applying the brakes. Do not release break pedal pressure until the airplane has decelerated to a safe taxi speed.


B 737 - 200 CHAPTER 2



GO – AROUND GO – AROUND PROCEDURE A G/A during precision or non-precision approaches must be controlled manually. Retract the gear and flaps on scheduled. The A/P may be re-engaged, when the airplane is in trim, above 1.500 ft AGL

Phase of Flight Or Event

Pilot Flaying Pilot Not Flying

Go - Around The PIC Command “GO-AROUND”. Advance Thrust Lever to Go-Around EPR and calls “SET GO-AROUND THRUST, FLAPS 15”. Rotate toward 15° up pitch attitude Observe positive rate of climb indicated and respond “GEAR UP”.

Set GO-AROUND Thrust. Position PLAF lever to 15 and Monitor flap retraction. Monitor airplane performance Callout “GO-AROUND THRUST SET”. Verify and callout “PSITIVE CLIMB” Select GEAR UP and monitor gear retraction.

Cross-check flight instruments for proper indications. At 400 ft AAL or 400 ft RA

Verify and respond “SET RADIOS” Callout “FOUR HUNDRED”. Tune NAV as briefed and Report “RADIO SET”.

AT 1000 feet AAL Verify altitude and respond “SET CLIMB THRUST”. CALLS FOR FLAPS RETRECTION UPON Achieving speed schedule. Verify airplane acceleration.

Callout “ONE THAUSAND”. Set climb thrust Verify speed and select flaps accordingly. Monitor flaps/slats retraction, airspeed, attitude, and airplane flight progress.

Verify airplane levels off at the selected or go-around altitude and maintains the minimum maneuvering speed appropriate for the flaps selected. Flaps Up/No Light and situation permits

Calls” AFTER TAKEOFF CHECKLIST”.

Performance the Checklist and Reports “AFTER TAKEOFF


B 737 - 200 CHAPTER 2



CHECKLIST COMPLETED”. WAVE – OFF / REJECTED LANDING

The wave-off procedure (rejected landing) is similar to the go-around procedure except that the maneuver begins with the trust levers at least at or near idle and at altitudes below 50 ft. Apply thrust to G/A (G/A EPR) and simultaneously rotate initially to stop the descent. Be prepares for a slow and /or an uneven engine spool – up. Do not rotate to climb attitude until the speed is a minimum of V ref + 15. Ensure a positive rate of climb before retracting flaps to 15. Touching of the main gears on the runway is expected as it may take a few seconds for the engines to spool-up to go-around thrust. Do not call for ”gear up” until the critical phase has passed and a positive climb path is achieved. Note: The speed brake will automatically retract and auto brake will disarm as thrust

levers are advanced after a touchdown.

WARNING: DO NOT ATTEMPT A GO – AROUND AFTER REVERSE THRUST HAS BEEN INITIATED.


B 737 - 200 CHAPTER 2



MANDATORY GO – AROUND During an instrument approach, execute an immediate missed approach:

1. On all ILS / PRECISION approaches, the pilot not flying shall advices the pilot flying to commence and immediate go-around if the aircraft path is outside of the following parameters when the aircraft is at in altitude not less than 200 feet above the aerodrome reference altitude.

Localizer deviation : greater than 1 dot. Glide slope deviation : greater than 1 dot Airspeed deviation : speed less than V ref Greater than V ref + 20 kts Rate of Descent : greater than 1.000 fpm Warnings : any GPWS warning. The call by the PNF shall be: “MANDATORY GO-AROUND”.

2. On all Non – precision and visual approach, the pilot not plying shall advise the pilot flying to commence an immediate go-around if the aircraft path is outside of the following parameters when the aircraft is at an altitude not less than 200 feet above the aerodrome reference altitude. Centerline deviation ; NOT on extended centerline. Glide Path deviation : VASI / PAPI indicate ALL REDS (Too Low) VASI / PAPI indicate ALL WHITES (Too High) Airspeed deviation : speed less than V ref Greater than V ref + 20 kts Rate of descent : greater than 1000 fpm. Warning Any GPWS warning, unless visual and

aircraft confirmed to be in a safe condition.

The call by PNF shall be “ MANDATORY GO-AROUND”. 3. During any type of approach, execute an immediate go around for any of

following conditions: I. If a NAV radio, transmitter or flight instrument failure occurs this will

affect the ability to safety complete the approach. II. When the instruments show significant disagreement and visual contact

has NOT been established. III. If GPWS terrain and pull-up warnings sound and visual contact has NOT

been established during descent.


B 737 - 200 CHAPTER 2



After Landing TAXI-IN PROCEDURE This procedure is accomplished when clear of the active runway and when aircraft is at a save taxi speed. Crew must be diverted from the primary task of safety taxiing the airplane. Avoid all unnecessary activities and duties that can be accomplished at another time. After reaching a save taxi speed, the captain will position the speed brake lever to the DOWN DETENT position MANUALLY. The captain will then command the First Officer to accomplish the AFTER LANDING CHEKLIST when the situation permits. The First Officer starts the chronograph stopwatch and monitors engine operation at or near idle for three minutes prior to engine shutdown. SPEED BRAKE LEVER ...................................................................................DOWN DETENT

Verify Speed Brake Lever is in the down detent. FLAPS .............................................................................................................. UP, NO LIGHTS APU...........................................................................................................STRAT, ON BUSSES AS APPLICABLE:

Select the DC Voltmeter to BATT and AC Voltmeter to APU.

Start the APU by momentarily placing the APU start switch to ON, Note Chronograph.

APU starter engagement is observed on the DC ammeter as a full left deflection.

Select both APU generator switches when APU available light illuminates.

Verify APU GEN OFF BUS light extinguished.

If the APU start in unsuccessful, a restart attempt is initiated after a lapse of 30

seconds from the time the APU start switch is selected OFF.

WINDOW HEAT..................................................................................................AS REQUIRED

PITOT HEAT ........................................................................................................................OFF

AIR COND & PRESSURIZATION.......................................................................SET, GROUND FLT / GRD Switch – ground

Observe OUTFLOW VALVE move towards OPEN

ENGINE START SWITCHES ...............................................................................................OFF


B 737 - 200 CHAPTER 2



EXTERIOR LIGHTS......................................................................................... AS REQUIRED DAY : INBOARD Lights – OFF NOGHT : Lights are Captain’s management Select strobes OFF or STEADY upon vacating the runway (s) FLIGHT DIRECTORS (if applicable) .................................................................................OFF AUTO BRAKE ...................................................................................................................OFF HF’S, RADAR / TRANSPORDER ................................................................ OFF & STANDBY

Both HF’s – OFF Both WX switches on the L/R EFIS Control Panel – OFF Radar Control Panel Mode Selector – TEST Transponder – STBY Altitude Reporting switch will remain ON

Stabilizer Trim .................................................................................. set approximately 5 units SLIDE BARS ......................................................................................................... DISARNED

At the moment just before parking; on the Captains command, the first officer announce “FLIGHT ATTENDENT DISARM SLIDE BARS AND CROSS CHECK”.

The first officer reads and verifies that the after landing checklist was correctly accomplished, when the situation permits.

Note: To avoid the possibility of the shoulder harness buckles snapping back and inadvertently pulling circuit breakers, hold both straps before releasing and the allow the straps to retract slowly to the stowed position.


B 737 - 200 CHAPTER 2



Shutdown Procedure

After the airplane has come to a complete stop, the Captain and First Officer will perform the following actions: Parking brake ........................................................................................................... set

Captain sets the park brake and both verify that the parking Bake Warming Light illuminates.

START LEVERS............................................................................................ CUT OFF The Captain shall position BOTH start levers to the cut off detent position while observing for position indication of decreasing fuel flow and EGT of engines. Note: if possible, operate the engines at the idle for three minutes prior to shutdown

to thermally stabilize the engine hot section. Operating times at or near idle, such as taxiing before shutdown, are applicable to this three-minutes period. If operational requirements dictate, the engine may be shutdown with a one-minutes cooling period. For timing purpose, idle thrust includes momentary break-away thrust.

FUEL PUMPS.........................................................................................ON PUMP ON

Select one fuel pump ON, use centre tank if fuel is sufficient when the APU is running.

Note: whenever the APU is operating and AC electrical power is on the airplane busses, extended service life of the APU fuel control unit can be realized by operating at least one fuel boost pump to supply fuel under pressure to the APU

FASTEN SEAT BELTS ..........................................................................................OFF

Verify slide bar disarmed report by Flight Attendant before switching off.

WINDOW HEAT .....................................................................................................OFF

Verify that windows heat switches are in off position.

ANTI – ICE ............................................................................................................OFF

Verify that WING ANTI–ICE and ENGINE ANTI–ICE SWITCHES are in off position.

ELECTRIC HYDROULIC PUMPS..........................................................................OFF

Switch off electric hydraulic pump a first, followed by electric hydraulic pump B.

AIR CONDITIONING .....................................................................................PACK ON

The first officer sets:

One pack – ON


B 737 - 200 CHAPTER 2



Use the left pack on odd dates and the right pack on even dates.

Isolation valve switch – AUTO

Both engine bleed switches – ON

APU bleed air switch – ON (if APU pneumatic is available).

ANTI – COLLISION light.........................................................................................OFF

The captain selects anti-collision light switch to OFF position when both engine N1 indication reads less than 5 %.

PARKING BRAKE ................................................................................AS REQUIRED

With the chocks confirmed in place, the captain may release the parking brake, exercise caution on slopping parking terminal.

DOORS ..........................................................................................................OPENED

The Captain will command the Flight Attendants to open doors after parking brake is released.

Verify that Cockpit door is unlocked.

Cockpit lights ................................................................................................As desired The Captain calls for the “SHUTDOWN CHEKLIST”. The First Officer reads the checklist and the Captain responds. The First Officer states “SHUTDOWN CHECKLIST IS COMPLTETED”.


B 737 - 200 CHAPTER 2



Secured

These checks are non – routine and are applicable to unscheduled off-line station terminating flights. The Captain calls for the SECURE Checklist. The First Officer READS and the Captain ACTIONS and RESPONDS to the check. GALLEY POWER ...................................................................................................OFF The galley power switch is left ON during through flights, OFF on terminating flights.

EMERGENCY EXIT LIGHTS .................................................................................OFF

AIR CONDITIONING ................................................................................ PACKS OFF

Both packs – OFF APU bleed air switch – OFF

APU/GROUND POWER ......................................................................AS REQUIRED

Note: it is recommended that the APU be operated for one full minute with no pneumatic load prior to shut down

BATTERY ...............................................................................................................OFF

Note: Delay Battery switch to OFF for approximately 20 second after APU shutdown, for the APU door to drive to full close., This assures the APU will start prior to the next flight.

OXIGEN SHUTOFF VALVE ..............................................................................CLOSE

The first officer closes the crew oxygen shutoff valve. On completion the First Officer report “ SECURE CHECKLIST COMPLETED”. Note: For unscheduled terminating flights, ensure external conditions are secure, CHOCKS in place and GEAR PINS installed.


B 737 - 200 CHAPTER 3 BRIEFINGS


BRIEFINGS General The objective of crew briefing are:

• To plan ahead • To clarify perception • To review procedures

The Captain shall ensure a crew briefing is completed prior to every takeoff and landing. The briefing shall be accomplished as soon as practicable so as not to interfere with final takeoff or landing preparations. Departure Briefing

Time permit, departure briefing should be completed before engine start.

For the first flight of the day, the crew should make complete briefing. On a second and subsequent takeoff with the same PF, the term “STANDARD” might be used with review some same items such as SID, speeds, engine Failure Procedure/special procedure, etc. Both crew members shall acknowledge that the operation of flight shall be in accordance with the “COMPANY STANDARD PROCEDURES & CALLOUTS”, and this refers to the operation if the airplane in accordance to the procedures describes in the Operation Manual. Prior to each departure, the pilot flying shall describe:

1. NOTAM, Weather condition (Dep/,En-route, Dest, and alternate). 2. The aircraft serviceability (DMI/MEL/DDPG). 3. Starting procedure (on the gate/while push back/after push back engine

sequence number and using APU / GTC. 4. Runway in use and taxi routing. 5. Takeoff performance ; Flaps setting, FULL/REDUCED thrust, bleeds ON/OFF,

anti ice ON/OFF. 6. During rolling monitor engine instruments, flight instruments and recall panel. 7. Callout speed “EIGHTY, V1 and ROTATE. 8. As depicted below. 9. Follow SID / SPECIAL PROCEDURE, etc 10. The procedure in the event of an IBFLIGHT RETURN (radar vector

/ILS/VOR/visual). 11. The SID, MSA, MORA/MEA, TRANSITION ALTITUDE, INTENDED LEVEL. 12. RADIO/NAV SET-UP. 13. NOISE ABATEMENT or SPECIAL CLIMB OUT PROCEDURE ( if any ) 14. Any ADDITIONAL BRIEFING when considering supplementary normal

operation, environment factors, minimum equipment list dispatch considerations, or any other situation where it is necessary to review or define crew responsibilities.




Additional, for the first sector, the Captain shall ensure the following company takeoff

briefing

8. For Captain Sector

Malfunction BEFORE V1, IDENTIFY. In case of rejected takeoff, I will call STOP and simultaneously;

Close thrust levers. Apply maximum manual braking. Raise speed brake. Maximum reverse thrust. If speed brake not deploy, callout “SPEED BRAKE”. Note the RTO speed for Brake Cooling Schedule. Notify ATC when practicable, and standby for further instructions.

Malfunction At or AFTER V1, continue TAKEOFF, IDENTIFY. No action below 400 ft AGL, except silence bell and select gear up when positive climb. In case of engine failure: The acceleration altitude is 1000 ft AGL (or as stated on ENGINE FAILURE

PROCEDURE). Retract Flaps on schedule If any immediate action, done after 400 ft AGL.

8. For Co-pilot Sector

Malfunction Before V1, IDENTIFY. In case of rejected takeoff, you will call “STOP” and you have control. I will revert to support duty and monitor your actions: If speed brake is not deploy, I will callout “SPEEDBRAKE” Note RTO speed for Brake Cooling Schedule. Notify ATC when practicable, and standby for further Instructions.

Malfunction AT or AFTER V1, continue TAKEOFF, IDENTIFY. No action below 400 ft AGL, except silence bell and select gear up when positive climb. In case of engine failure: The acceleration altitude is 1000 ft AGL (or as stated on ENGINE FAILURE

PROCEDURE). Retract flaps on schedule If any immediate action, done after 400 ft AGL

At the end of briefing, the Captain should stress the following:

Should you have any doubt on the safety of the flight, do not hesitate to bring it to my attention immediately”




Malfunctions affecting the safety of the flight are generally associated with, but not limited to, power plant failures, engine fire, and takeoff configuration warning. Rejecting the takeoff solely for the amber Master Caution Light, once take off thrust has been set and take off roll established is not recommended. Where possible, ATC departure clearance should be copied and reviewed BEFORE the pushback / engine start, or where situation permits during taxi. Taxi duties:

Pilot Flying Pilot Not Flying Ensure safe taxi speed Monitor taxi speed, call if excessive Ensure nose wheel follow correct taxi guidelines/lights; No shortcut especially during turns. Ensure that the aircraft is clear of obstacles.

Monitor taxi path. Ensure that the aircraft is clear of obstacles.

Takeoff

Ensure control column in neutral position by V1

When pilot incapacitation is recognized, PNF shall immediately take over controls. Descent and Approach Briefing

The Pilot Flying briefs the pilot not Flying as to his intention for the approach, landing and missed approach procedures, preferably before starting the descent. The items covered must include but are not limited to the following items:

1. Aircraft status (MEL/Maintenance Report) 2. Aerodrome status (NOTAMs, Airfield lights, runway length available,

peculiarities) 3. Weather conditions (destination)

4. Top of descent calculation 5. STAR (cross check with FMC where applicable)

a. Chart number / data / validity b. Intended track c. Altitude / speed restriction

6. APPROACH ( cross check with FMC where applicable)

a. Chart number / date / validity b. Type of approach




c. Landing Runway d. Airport elevation e. MSA,MEA/MORA/GRID MORA. f. Transition level

g. Holding pattern/entry/minimum holding altitude h. Outbound and procedure turn heading i. Inbound course j. Minimum altitudes during approach k. Minimums : altitude & visibility ( RVR should be used when reported) l. Missed approach point m. Missed approach procedure n. Approach and missed approach navaids setup

7. LANDING DATA

a. Landing weight b. Flap setting c. Vref d. Auto brakes setting

8. TAXI

a. Route to parking bay b. Docking system

9. ALTERNATE DIVERSION

a. Weather b. Fuel requirements

10. Any other items deemed important. At the end of the briefing, the Captain should stress the following:

It is the responsibility of the flight crew to ensure safe conduct of flight. A go-around must be executed if the aircraft is not stabilized and deemed unsafe at any time during the approach. When pilot incapacitation is recognized, PNF shall immediately take over controls.

“ Should you have any doubt on the safety of the flight, do not hesitate to bring it to y attention immediately”

Phase Captain Co – pilot




Post Landing:

Turn – off speed

Ensure reverse Thrust levers in full forward position. Stow speed brakes to DOWN DETENT position MANUALLY after exiting runway.

Verify REVERSE UNLOCKED lights extinguished.

Taxi

Ensure correct safe taxi speed

Monitor taxi speed

Taxi

Ensure nose wheel follows correct taxi guidelines/lights No shortcut especially during turns. Ensure that the aircraft is clear of obstacle.

Monitor taxi path. Ensure that the aircraft is clear of obstacle

Parking

Ensure correct parking bay and docking procedures

Monitor appropriate bay and parking guidance display. Callout if docking speed is excessive.

Documents

737-200 Standart Operating Procedures (SOP)