HNA A330 SOPs Rev 3

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OPERATION MANAGEMENT MANUAL

NO.：HU-09-1-G

Hainan Airlines

Standard Flight Operating Manual

SOP

A330-200

Ratifier: Guan Lei

Controlled Status: For Reference only

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Standard Flight Operating Manual

A330

Foreword

The purpose of compiling Flight Standard Operating Procedures Manual is to

strengthen the management of flight techniques of the company and improve unitary

training qualities and technique levels of the flight crew, enabling the operations of

the flight crew to be standardized, normative and follow certain procedures. It alsoaims to strengthen crew cooperation philosophy and raise the level of CRM

management in order to ensure flight safety.

This manual is complied in strict accordance with Aircraft Flight Manual, Flight

Crew Operating Manual, QRH , Operating Criterion and other related manuals issued

by the company.

Flight Standard and Training Department of Hainan Airlines is responsible for the

compilation, modification, printing and management of the manual and appoints some

personnel to make revisions to the manual according to the newest materials of Airbus

and revision proposals of flight department after using the manual. After examined

and approved by Flight Techniques Commission, the manual can be provided for the

overall flight personnel of A330 for their studies and usage. Flight Standard and

Training Department provides manual holders periodically with the newest revision

lists, lists of effective pages and revision pages. In each revision page, revisioncontent, revision time and entry-into-force date will be stated. After receiving revision

interleaves, manual holders should update the manual in an immediate manner to

ensure the latest effectivity of the manual.

The copyright of the manual belongs to Hainan Airlines. Any unit or individual can

not copy the manual without approval The right of final explanation belongs to Flight

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CHH ALL 版本 3

A330 STANDARD OPERATING PROCEDURES 海南航空股份有限公司

HAINAN AIRLINES COMPANY LIMITED 8. ENGINE START P 37

AUTOMATIC ENGINE START- ENG START selec tor .....................................................................................................IGN START

The lower ECAM display shows the ENG page.

- START ENGINE 1......................................................................................................... ANNOUNCE

Engine 1 is usually started first. (It powers the blue hydraulic system, which pressurizes the

parking brake).

- MASTER swi tch 1 ........................................................................................................................ON

Do not turn the MASTER switch ON, until all amber crosses and messages have disappeared on

the engine parameters (upper ECAM display).

ON ECAM UPPER DISPLAY ON ECAM LOWER DISPLAY

N3 increases Corresponding start valve is in line.

Bleed pressure indication is green.

Oil pressure increases.

At 25 % N3 :

- FF increases

30 seconds (maximum) after fuel is on

- EGT increases

- N1 increases

Indication of the active igniter (A or B).

At 50 % N3 Start valve starts closing.

(It is fully closed after about 10 seconds.)

Parameter callouts are not mandatory.

Note : When starting a hot engine (EGT above 100°C, for the first automatic start and above

150°C, for the second automatic start), the EEC controls a dry crank, in order to reduce

engine temperature. The igniters and the fuel are controlled ON, once the EGT is below

100°C (150°C, in case of a second automatic start attempt).

When idle is reached (AVAIL indication i s disp layed) :

- MAIN AND SECONDARY ENG. IDLE PARAMETERS...................................... CHECK NORMAL At ISA sea level : EPR about 1.015

N1 about 22.6 %

N2 about 47 %

N3 about 63 %

EGT about 380° C

FF about 820 kg/h (1800 lb/h)

- START ENGINE 2......................................................................................................... ANNOUNCE

- MASTER swi tch 2 ........................................................................................................................ON

Same procedure as for Engine 1.

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HAINAN AIRLINES COMPANY LIMITED 8. ENGINE START P 38

GROUND RUN UP - DANGER AREAS

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HAINAN AIRLINES COMPANY LIMITED 12. TAKEOFF P 53

At acceleration alt itude :

- FMA..............................................................................................................................ANNOUNCE

Check target speed change from V2 + 10 to the first CLB speed (either preselected or managed).

Note : 1. When THR RED and ACC ALT are equal, the FMA will change from MAN

FLX/SRS/RWY to THR CLB/CLB/NAV (or THR CLB/OP CLB/NAV).

2. If the FCU-selected altitude is equal or close to acceleration altitude, the FMA will

switch from SRS to ALT*. Above acceleration alt itude (or once in CLB phase) :

The following procedure ensures that the aircraft is effectively accelerating toward CLB speed.

At F speed

Note : For takeoff in CONF 1+F, the “F” speed is not displayed.

- FLAPS 1...............................................................................................................................SELECT

At S speed

- FLAPS ZERO.................................................................................................................. SELECT

Note : The CRUISE page replaces the ECAM ENG page, when reaching 1500 feet.

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HAINAN AIRLINES COMPANY LIMITED 12. TAKEOFF P 54

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P 87


P 88

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HAINAN AIRLINES COMPANY LIMITED 19. NON PRECISION APPROACH

CIRCLING APPROACH

For a circling approach, the flight crew should prepare the flight plan as follows :

Primary flight plan : Introduce the instrument approach

Secondary flight plan : - Copy the ACTIVE F-PLN

- Revise the landing runway

The aircraft should circle in CONF 3 at F speed.

Upon reaching MDA/MDH :

- Push the ALT pushbutton.

- Search for visual references.

If the flight crew finds no visual reference :

- AT MAP : Initiate go-around

If the flight crew finds sufficient visual references :

- Select TRK for downwind

- Early on downwind : Activate SEC F-PLN

CAUTION

The PNF should activate the SEC F-PLN.

The PF should maintain visual contact during all the circling.

- Disengage autopilot before reaching the base leg.

- Select both FDs OFF.

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HAINAN AIRLINES COMPANY LIMITED 19. NON PRECISION APPROACH


HAINAN AIRLINES COMPANY LIMITED 20 VISUAL APPROACH

P 89


HAINAN AIRLINES COMPANY LIMITED 20 VISUAL APPROACH

P 90

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HAINAN AIRLINES COMPANY LIMITED 20. VISUAL APPROACH

OBJECTIVE

Perform the approach on a nominal 3 degree glideslope using visual references. Approach to be

stabilized by 500 feet AGL on the correct approach path, in the landing configuration, at VAPP.

Method :

- The autopilot is not used.

- Both FDs are off.

- FPV use is recommended.

- A/THR use is recommended with managed speed.

Bear in mind the possible risk of optical illusions due to hindered night vision.

VISUAL CIRCUITINITIAL/INTERMEDIATE APPROACH

The flight plan selected on the MCDU should include the selection of the landing runway.

The downwind leg might also be part of the Flight plan. This may be a useful indication of the

aircraft position in the circuit on the ND.

However, visual references must be used.

Therefore, at the beginning of the downwind leg :

- Manually ACTIVATE APPR.

- Select FDs to OFF. - Select TRK-FPA to display FPV.

- Check A/THR active in speed mode.

Downwind leg extension 45 seconds (± wind correction)

Turn into base leg with a maximum of 30° bank. Descent with appropriate FPA, in FLAPS 2, at F

speed.

FINAL APPROACH

- The speed trend arrow and FPV help the flight crew make timely and correct thrust settings (if in

manual thrust), and approach path corrections. Avoid descending through the correct approachpath with idle thrust. (Late recognition of this situation without a prompt thrust increase may leadto considerable speed decay and altitude loss).Ensure that the aircraft is stabilized on the final descent path at VAPP (or ground speed mini) inthe landing configuration with the thrust stabilized (usually above idle) at 500 feet above airfieldelevation or as restricted by Operator policy/regulations. If the aircraft is not stabilized, the flightcrew must initiate go-around, unless they think that only small corrections are necessary torectify minor deviations from stabilized conditions due, amongst others, to external perturbations.

- Avoid any tendency to “duck under” in the late stages of the approach.- Avoid destabilizing the approach in the last 100 feet, in order to have the best chance of

performing a good touchdown at the desired position.

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HAINAN AIRLINES COMPANY LIMITED 20. VISUAL APPROACH


HAINAN AIRLINES COMPANY LIMITED 21 LANDING

P 91



P 92

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HAINAN AIRLINES COMPANY LIMITED 21. LANDING

ILS FINAL APPROACH AND LANDING GEOMETRY

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HAINAN AIRLINES COMPANY LIMITED 21. LANDING

MINIMUM VISUAL GROUND SEGMENTS (Flare phase)

Note : This drawing illustrates that, for a CAT III landing (60 meters minimum visual segment),

the minimum RVR is 114 meters at 15 feet.



P 93



P 94

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21. LANDING

GROUND CLEARANCE DIAGRAM

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21. LANDING

LANDING

The cockpit cut-off angle is 20 degrees.

In stabilized approach condit ions, the flare height is approximately 40 feet :

- FLARE ............................................................................................................................. PERFORM

- ATTITUDE ........................................................................................................................ MONITOR

The PNF should monitor the attitude, and call out :

- “PITCH, PITCH”, if the pitch angle reaches 7.5 degrees.

- “BANK, BANK”, if the bank angle reaches 7 degrees.

- THRUST levers .........................................................................................................................IDLE

If autothrust is engaged, it automatically disconnects when the pilot sets both thrust levers to the

IDLE detent.

In manual landing conditions, the “RETARD” callout is triggered at 20 feet Radio Altitude (RA), in

order to remind the pilot to retard the thrust levers.

Note : If one or both thrust levers remain above the IDLE detent, ground spoilers extension is

inhibited.

Ground c learance

- Avoid flaring high.

- A tailstrike occurs, if the pitch attitude exceeds 11 degrees (landing gear compressed), 16

degrees (landing gear extended).

- A wingtip or engine scrape occurs, if the roll angle exceeds 17 degrees.

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HAINAN AIRLINES COMPANY LIMITED 26. STANDARD CALLOUTS P 107



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FLAPS OR GEAR CONFIGURATION

FLAPS' CALLOUTS

FLAPS' CONFIGURATION CALLOUT

1 “FLAPS ONE”

1 + F “FLAPS ONE”

0 “FLAPS ZERO”

The reply will be given when selecting the new flap position.

e.g. :

CALLOUT REMARK

PF "FLAPS ONE"

"SPEED CHECKED" PNF checks the speed :

- Above the S or F speed and accelerating

(Takeoff)

- Below Vfe next and decelerating (Approach)PNF

"FLAPS ONE"

PNF selects the flaps lever position and replies after

checking the blue number on the ECAM flaps

indicator to confirm the correct selection has been

made.

GEAR CALLOUTS

CALLOUT REMARK

PF "GEAR UP (DOWN)"

PNF

"GEAR UP (DOWN)" The PNF selects the gear lever position and replies

after chekcing the red lights on the landing gear

indicator to confirm gear operation.

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FLIGHT PARAMETERS IN APPROACH

PNF will make callouts for the following conditions during final approach. Attitude callouts also to be

made through to landing.

- “SPEED” when speed becomes less than Vapp - 5 or more than speed target + 10.

- “SINK RATE” when V/S is greater than - 1000 ft/min.

- “BANK” when bank angle becomes greater than 7°.

- “PITCH” when pitch attitude becomes lower than 0° or higher than + 10°.

- 'LOC” or “GLIDE” when either localizer or glide slope deviation is :

1/4 dot LOC ; 1 dot GS

- “COURSE” when greater than 1/2 dot or 2.5 degrees (VOR) or 5 degrees (ADF).

- “__ FT HIGH (LOW)” at altitude checks points.

FLIGHT PARAMETERS IN GO-AROUND

During a go-around, the PNF will make a callout for the following conditions :

- ”BANK” : If the bank angle becomes greater than 7°,

- ”PITCH” : If the pitch attitude becomes greater than 20° up or less than 10° up,

- ”SINK RATE” : If there is no climb rate.

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TAXI

EVENT PF PNF

When taxi clearance obtained CLEAR LEFT (RIGHT) SIDECLEAR RIGHT (LEFT) SIDE

Brake transfer check BRAKE CHECK

PRESSURE ZERO

Flight control check in following sequence

(can be done before start of taxi)

FLIGHT CONTROL CHECK

1. Elevators FULL UP, FULL DOWN,

NEUTRAL

2. Ailerons/Spoilers FULL LEFT, FULL RIGHT,

NEUTRAL

3. Rudder * RUDDER FULL LEFT, FULL RIGHT,NEUTRAL

During taxi BEFORE TAKE-OFF C/L

DOWN TO THE LINE BEFORE TAKE-OFF C/L DOWN

TO THE LINE COMPLETE

Lining up on the runway BEFORE TAKEOFF C/L

BELOW THE LINE

BEFORE TAKE-OFF C/L

COMPLETE

Note : * The PNF should follow pedal movement with his/her feet

TAKE-OFFEVENT PF PNF

Setting thrust levers to initial stabilisation

value

TAKE-OFF

Before passing 80 kts THRUST SET

At 100 kts ONE HUNDRED KNOTS

CHECKED

At V1 V1

At VR ROTATE

Gear retraction POSITIVE CLIMB

GEAR UP GEAR UP

If AP is engaged by PNF AP 1(2) ON

Check List AFTER TAKEOFF/CLIMB C/L

DOWN TO THE LINE

AFTER TAKEOFF/CLIMB C/L

DOWN TO THE LINE

COMPLETE

At transition altitude AFTER TAKEOFF/CLIMB C/L

BELOW THE LINE


COMPLETE

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MALFUNCTION BEFORE V1 AT TAKEOFF

EVENT CAPT F/O

If GO decision GO

If RTO decision

. REV green on EWD

. Deceleration

STOP

REVERSE GREEN*

DECEL**

In case of failure or no positive deceleration :

* NO REVERSE ENGINE__or NO REVERSE

** NO DECEL

DECEL callout means that the deceleration is felt by the crew, and confirmed by the speed trend on

the PFD. It can also be confirmed by the DECEL light.

ALTIMETER SETTING CHANGES TO/FROM QNH/QFE-STD

EVENT PF PNF

SET STANDARD

(SET QNH/QFE) STANDARD CROSS-CHECKED

(QNH/QFE)

Barometric setting change and

subsequent altimeter cross-check

CHECKED PASSING FL__(__FT) NOW





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APPROACH AND LANDING

EVENT PF PNF

APPROACH C/L Approach check list

APPROACH C/L COMPLETE

Activation of approach Phase ACTIVATE APPROACH PHASE

APPROACH PHASE ACTIVATED

RA alive

CHECKED

RADIO ALTIMETER ALIVE (see

Note 4 and 5 below)

At “GS*” or below GO altitude for NPA SET GA ALTITUDE __FT

GA ALTITUDE ⎯ SET,

FAF PASSING__(Fix Name),__FT,

CHECKEDLanding check list LANDING C/L

LANDING C/L COMPLETE

1000 feet RA ONE THOUSAND (see Note 5

below)

CHECKED

100 feet above MDA/DH ONE HUNDRED ABOVE

CHECKED

MDA/DH visual reference MINIMUM

CONTINUEMDA/DH no visual reference MINIMUM

GO AROUND-FLAPS

ONE HUNDRED

FIFTY (see Note 5 below)

After touchdown

Ground spoilers extended

REV green on EWD

SPOILERS (see Note 6 below),

REVERSE GREEN, (See note 7

below)

Deceleration DECEL (See Note 8 below)

At 70 knots SEVENTY KNOTS

CHECKED

Note 4 : Crew awareness, crew should now keep RA in scan to landing

Note 5 : PNF monitors pin-programmed auto callout, or announces if inoperative.

Note 6 : If the spoilers are not extended, call NO SPOILER

Note 7 : If reverse deployment is not as expected, call NO REVERSE ENGINE__ or NO REVERSE, as

appropriate.

Note 8 : DECEL Callout means that the deceleration is felt by the crew, and confirmed by the speed trend on

the PFD. It can also be confirmed by the DECEL light. If no positive deceleration, call NO DECEL.

CHH ALL 版本 3

GO AROUND

EVENT PF PNF

GO AROUND decision GO AROUND - FLAPS

Flaps retraction FLAPS ⎯

Gear retraction POSITIVE CLIMB

GEAR UP

GEAR UP

Check list AFTER TAKEOFF/CLIMB C/L

DOWN TO THE LINE


DOWN TO THE LINE

COMPLETE

AFTER TAKEOFF/CLIMB C/LBELOW THE LINE

At transition altitude AFTER TAKEOFF/CLIMB C/L

COMPLETE

AFTER LANDING

EVENT PF PNF

Check list AFTER LANDING C/L

AFTER LANDING C/L

COMPLETE

PARKING

EVENT PF PNF

Check list PARKING C/L

PARKING C/L COMPLETE

SECURING THE AIRCRAFT

EVENT PF PNF

Check list SECURING THE AIRCRAFT

C/L

SECURING THE AIRCRAFT C/L

COMPLETE

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APPENDIX

A330 Special Operation Supplementary SOP

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A330 SPECIAL OPERATION

SUPPLEMENTARY SOP海南航空股份有限公司

HAINAN AIRLINES COMPANY LIMITED

3．RNAV OPERATION

P 120




3．RNAV OPERATION

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RNAV OPERATION SOP

AT DISPATCH OFFICE AND PILOTS ROOM ON GROUND:

Crew and airplane………………………………………………..RNAV operation approved

Company operation………………………………………………RNAV operation approved

Airplane airborne NAV equipment……………compliance with RNAV dispatch requirement

Flight plan……………………………………apply in accordance with RNAV requirement

COCKPIT INSPECTION

Airplane airborne NAV equipment……………compliance with RNAV dispatch requirement

Airborne NAV database………………………………current and cover planned operation area

NAV system……………………………………………………………normal and align

Airplane position………………………………………………………………check correct

RNAV route、DP or STAR……………………………………………………display all input

MCDU flight plan………………………………………………………………check correct

When ATC RNAV clearance obtained

For RNAV1 DP

NAV accuracy……………………...……………………………………check

GPS primary available.

If GPS primary not available：

RNP…………………………………………………………≤1. 0

NAV accuracy periodic check………………………….…………high

Runway and DP……………………………check finally and display correctly

CHH ALL 版本 3

Before takeoff ：

EFIS mode selector……………………………………..…ROSE NAV/ARC

FDs………………………………..………………………………check ON

NAV…………………………………………….. .……………………blue

Airplane position……………………………..………………………check

Map display agrees with airplane and runway，route display agrees with

chart.

After takeoff, at or below 150 meters（500 feet） above airport elevation：

NAV………………………………………………………………check ON

AP…………………………………………………………………check ON

For RNAV2 route

NAV database…………………………………………………check current

If database out of date：

FMGS data and chart data………….………………………compare

If different………………..…….………use non-RNAV procedure

NAV accurary…………………………………………………………check



RNP………………………………………………………… ≤2.0

NAV accuracy periodic check……………………….…………high

ATC cleared RNAV route………………………correctly enter and conform

Map display should agree with text display to confirm the correctness of

the route.




3．RNAV OPERATION

P 122




4．RE-CLEARANCE

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FDs………………………………..………………………………check ON

NAV……………………………………………...…………………check ON

AP…………………………………………………………………check ON

For RNAV1 STAR

NAV database…………………………………………………check current

If database out of date：

FMGS data and chart data………….………………………compare

If different………………..…….………use non-RNAV procedure

NAV accuracy……………………...……………………………………check



RNP………………………………………………………… ≤1.0

NAV accuracy periodic check………………………….………high

Arrival and runway……………………….……check and display correctly


FDs………………………………..………………………………check ON

NAV……………………………………………...…………………check ON

AP…………………………………………………………………check ON

POST FLIGHT

Any event that might affect RNAV operation…………………………………………report

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RE-CLEARANCE SOP

AT DISPATCH OFFICE AND PILOTS ROOM ON GROUND:

Airplane deferred items…………compliance with re-clearance dispatch requirement□

Note: Airborne COM equipment（SATCOM、ACARS、VHF、HF etc.）must ensure

the contact with dispatch enroute.

Re-clearance flight plan……………………………………………obtain; all on board□

Contain Primary flight plan □

Main alternate route flight plan □

Re-clearance decision point（RDP）□

Enroute flight plan from RDP to initial destination airport □

Initial destination airport to other alternates □

Initial destination airport to primary destination airport □

Alternate of initial destination airport to primary destination airport □

Destination and alternate………………………..……weather at or above standard□

Contain Primary destination airport and its alternate

Initial destination airport

Alternate of initial destination airport

（if initial destination or its alternate is enroute alternate or

ETOPS alternate of the route, enroute alternate or ETOPS

alternate requirement must be satisfied）.

Fuel quantity of each flight plan………………………………………list individually□

RDP minimum fuel and total fuel…………………….…determine and reasonable□

Related NOTAMs..……………………………………………………………study□




4．RE-CLEARANCE

P 124




4．RE-CLEARANCE

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Other special operation performed simultaneously

（such as ETOPS） preparation………………………………………………compl ete□

COCKPIT INSPECTION

Airplane deferred items…………compliance with re-clearance dispatch requirement□

HF, SATCAM, ACARS

and SELCAL………………check and compliance with re-clearance dispatch requirement□

Normal FMGES input and check………………………………..……………………complete□

Fuel reserve……………………………………….…………………………enter as required□INFLIGHT:

Fuel on board…………………………………..……check once every 30 minutes and record□

120-70 MINUTES BEFORE RDP

Re-clearance required information…………………………………………downlink dispatch□

Contain following information：

a) flight level；

b) Estimated time to RDP；

c) Estimated fuel remaining at RDP；

d) Estimated time at arrival at final destination.

BEFORE RDP

Re-clearance F-PLN and dispatch sheet…………………………………………………obtain□

The latest live weather at destination and alternate

（the last 1 hour

）and weather forecast

（1 hour before and after the arrival）…………………………………………………obtain□

Currently valid route weather report……………………………………………………obtain□

Currently valid NOTAMs…………………………………………………………obtain□

Captain decision……………………………………………………………downlink dispatch□

Flight surveillance record…………………………………………………………………fill in□

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AFTER DIVERSION/ALTERNATE FLIGHT

Flight surveillance record………………………………………………………………fill in□

Recommended format of free message:

FLXXX

ETO RDP AT XXXX Z

EFOB RDP XX.X TETA DEST AT XXXX Z

REQ ERDISPATCH INFO

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5．RVSM OPERATION

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CHH ALL 版本 3

POST FLIGHT

1.

Report any failure that may affect RVSM operation, fill in Technical Log Book

carefully if necessary.

2. When there was a severe altitude deviation in flight, flight crew should report it

timely through SMS within 24 hours, and fill in RVSM Airspace Severe Altitude

Deviation Report.

Documents

HNA A330 SOPs Rev 3