Operating Manual - PSP 601A-6 (Volume 2) - … · steering angle, and the turning radii for the maximum towing angle of ... WIDTH FOR 180 DEGREE TURN MINIMUM TURNING RADII WITH NOSE

OPERATING MANUAL PSP 601A-6

SECTION 1

AIRCRAFT - GENERAL

TABLE OF CONTENTS

MODEL DESIGNATION AND TYPE

OPERATING ROLE AND DESIGN CONCEPT

AIRCRAFT DIMENSIONS

AIRCRAFT TURNING RADII

DANGER AREAS

AIRCRAFT PARKING AND MOORING

SERVICING POINTS

AIRCRAFT ANTENNAS

DOORS

A. Passenger/Crew Door B. Emergency Exit Door C. Baggage Compartment Door D. Rear Equipment Bay Door E. Service Doors F. Door Indication Lights

FLIGHT COMPARTMENT

A. Crew Seats B. Instrument and Control Panels C. Cabin Sign Switches

Page

1

1

1

1

1

2

2

2

2

2 3 3 4 4 4

4

4 4 4

1 - CONTENTS Page 1

Mar 10/95


LIST OF ILLUSTRATIONS

Figure T i t l e Page Number

1 Aircraft Basic Dimensions and Ground Clearances 5

2 Aircraft Turning Radii 6

3 Engine Intake and Exhaust Danger Areas, and APU Exhaust

4

5

6

7

8

9

10

11

12

13

14

15

16

17

18

Danger Area

Aircraft Servicing Points (2 Sheets)

Aircraft Antenna Locations

Passenger/Crew Door

Baggage Compartment Door

Service Doors and Panels

Door Indication Lights and Cabin Signs Switches (2 Sheets)

Crew Seats (2 Sheets)

Flight Compartment Instrument and Control Panel Arrangement

Pi lot 's Instrument Panel

Copilot's Instrument Panel

Centre Instrument Panel (3 Sheets)

Overhead Panel and Glareshield (2 Sheets)

Centre Pedestal (2 Sheets)

Pi lot 's Console, Side and Facia Panels

Copilot's Console, Side and Facia Panels

7/8

9

11

12

13

14

15

16B

18

19

20

20A

22

24

26

27

1 - CONTENTS Page 2

May 01/96


SECTION 1

AIRCRAFT - GENERAL

1. MODEL DESIGNATION AND TYPE

The aircraft, named Challenger, is manufactured by Canadair Limited. The Challenger model covered by this manual is the CL-601, Model 2B16, Variant 601-3A, {Variant 601-3R for airplanes 5135 and subsequent), powered by two General Electric CF34 turbofan engines.

2. OPERATING ROLE AND DESIGN CONCEPT

Primarily, the Challenger is a long-range (transcontinental) business aircraft operated by a crew of two. The aircraft is designed to carry up to 19 passengers in spacious comfort over long distances. The combination of a technologically advanced supercritical wing, quiet and efficient engines, and a wide body enables the Challenger to achieve a high standard of performance, economy and passenger comfort.

3. AIRCRAFT DIMENSIONS (Figure 1)

All basic dimensions, including ground clearances, are given in Figure 1.

4. AIRCRAFT TURNING RADII (Figure 2)

Using the nose gear steering control wheel, the pilot can turn the aircraft, during taxiing, without differential braking. Figure 2 shows the turning radii applicable to the maximum nose wheel steering angle of 55 degrees, the minimum taxi strip width required for a 180-degree turn at the maximum steering angle, and the turning radii for the maximum towing angle of 90 degrees.

5. DANGER AREAS (Figure 3)

I t is essential that persons involved with engine or APU running are aware of the danger areas in front of and to the rear of the engine(s). Before running an engine or the APU, the information illustrated in figure 3 must be used to consider the safety of persons, equipment and buildings in the vicinity of the aircraft.

SECTION 1 Page 1

Apr 10/95

OPERATING MANUAL PS? 6 0 1 A - 6

AIRCRAFT PARKING AND MOORING

When the aircraft i s stationary on the ground, precautions must be taken to ensure safety of personnel and equipment. The extent of safety measures to be observed depends upon the prevailing or expected weather conditions and the expected length of time the aircraft will be stationary. For complete instruct ions on parking and mooring the a ircraf t , refer to Ground Handling and Servic ing Information, PSP 601-13.

SERVICING POINTS (Figure 4)

Location and details for al l aircraft servicing points are shown in Figure 4 .

AIRCRAFT ANTENNAS (Figure 5)

Location and nomenclature of the aircraft antennas are given in Figure 5.

DOORS

The aircraft is provided with a passenger/crew door, a baggage compartment door, a rear equipment bay door, landing gear doors and various small doors which provide access to servicing points. An overwing emergency exit door is provided on the right side of the passenger compartment.

The baggage compartment and emergency exit doors are of the plug type which open inward; all other doors open outward. All doors are flush with the aircraft outer skin when closed*

A. Passenger/Crew Door (Figure 6)

The entrance door is electrically or manually operated and downward opening, with the stairs forming an integral part of the door structure. I t s movement i s controlled .by a counterbalance system of gas springs.

An electrical power assist system provides an optional means of closing the door from inside the aircraft. A control switch, labelled CABIN DOOR, i s located just forward of the entrance door. Holding the switch to the RAISE position activates the system which raises the door from any open position up to the closed position. Once the switch i s released, the door can s t i l l be operated manually. A pull-in handle on the rear handrail can be used to reduce the force required to close the door manually from the inside of the aircraft.

The latching mechanism is operated by an internal single-lever handle, located on the forward side of the steps, a T-handle which i s recessed in a r i s er of a step and an external handle with a keylock.

SECTION 1 Page 2

Apr 02/87

canadair chaliBnqer OPERATING MANUAL

PSP 601A-6

On aircraft 5041 and 5146, a vent flap linked with the external handle locking mechanism is located just above the external handle recess, to ensure that the cabin cannot be fully pressurized unless the door is correctly locked. The vent opens whenever the external handle is moved from the stowed position. A viewing window adjacent to the T-handle displays the legends LOCKED and UNLOCKED to indicate the position of the external handle.

Once closed, the door is latched from the inside by pushing the internal handle downward. The T-handle is then pulled out of its recess to stow the external handle, which clicks audibly when stowed. Verification that the external handle is stowed can be made by ensuring that the internal handle cannot be pulled up. After this check, the T-handle must be stowed in the riser of the step.

From outside the airplane, the door is latched by rotating the external handle fully clockwise to engage the door latches and stow the pull-out handle. Pushing the external handle then places it in the stowed position.

The door is unlocked from the inside when the internal handle is pulled upward, ejecting the external handle from its pocket. The door is then unlatched by continuing to pull the internal handle upward. As the door opens, the handrails unfold upward.

The door unlocks from the outside by the operation of a PUSH trigger in the external handle, which is ejected from its pocket. To unlatch the door, the external handle is then turned 45 degrees counterclockwise. Pull-out and pull-in handles are also provided to assist the operator in opening or closing the door from the outside or inside, respectively. When the door is fully open, a door support leg extends to the ground.

B. Emergency Exit Door

For details of the emergency exit door, refer to Section 8.

C. Baggage Compartment Door (Figure 7)

The baggage compartment door is located on the left side of the aircraft immediately aft of the passenger compartment. The door opens inwards and upwards, and is assisted during opening by balance springs. The door is held closed by two plungers which are operated by an external and an internal handle.

Two proximity switches are installed to provide an indication in the flight compartment when the door is not safely closed.

The external handle stows flush into a pocket in the door outer skin and, in this position, acts as a lock for the latching mechanism. The handle has a keylock which unlocks or locks a PUSH trigger. The PUSH trigger, when pressed, ejects the handle which can then be turned to release the locking plungers and to open the door.

SECTION 1 Page 3

Aug 14/02

canadair chaJienper OPERATING MANUAL

PSP 601A-6

D. Rear Equipment Bay Door (Figure 8)

The rear equipment bay door, located at the bottom of the rear fuselage, provides access to the APU, engine oil replenishment system, air conditioning units, replenishment points for No. 1 and No. 2 hydraulic systems, and the aircraft battery. The door opens downward, has two integral steps, and is secured at the forward edge by two hinges which are equipped with quick-release pins to facilitate easy door removal.

The rear equipment bay door is held closed by two plungers at the rear edge, and is opened and closed by a handle. Handle operation is the same as for the baggage compartment door, with the exception that the rear equipment bay door must be supported during opening because of opening direction.

E. Service Doors (Figure 8)

Quick-release service door sand panels are provided for easy access to the servicing points throughout the aircraft. Location and nomenclature of these doors and panels are given in Figure 8.

F. Door Indication Lights (Figure 9)

For operation of the DOOR INDICATION lights, refer to Figure 9.

FLIGHT COMPARTMENT

Miscellaneous items in the flight compartment include a portable fire extinguisher, located behind the copilot's seat on the bulkhead that separates the flight and passenger compartments, two oxygen masks, two cup holders, and storage boxes and pouches for checklists, etc.

The windshield centre post incorporates a pilot's eye locator to enable seat adjustments for optimum field of vision.

A. Crew Seats (Figure 10)

The pilot's and copilot's seats are identical except that certain controls are installed on opposite sides. On both seats, inertia reel and forward/rearward controls are located inboard, and lumbar support, height and reclining controls are located outboard.

B. Instrument and Controls panels (Figure 11)

The instrument and control panels are arranged as shown in Figure 11, and are presented in Figures 12 to 18.

Circled numbers on the instrument and control panels refer to sections of this manual where information on the item can be found.

c. Cabin 5ign Switches (Figure 9)

For operation of the NO SMOKING and FASTEN SEAT BELT signs in the passenger cabin, refer to Figure 9.

SECTION 1 Page 4

Mar 10/95


t i

8 ft 10 in

] _ Cabin interior dimensions |

[ Length Width {max dia)

28ft 3in I 8ft 2in

Headroom (floor to max height) 6ft 1 in | Volume Floor area Floor width

1150 cu. ft 202.5 sq. ft

7ft 2in

/ \ Measurement at manufacturers empty weight

y£ \ 21 feet elevator up

/ s \ Open passenger door ground clearance 4 inches

EFFECTIYITY

J Ji] A/C5001TO5134

r^ A/C 5135 & SUBS AND ^ POSTSB601-O262 20 ft 8 i r j ^ ^

Aircraft Basic Dimensions and Ground Clearances SECTION 1 Figure 1 p a g e 5

May 01/96

canactatr ctiauencjer


, MAXIMUM TURNING RADII USING NOSE WHEEL STEERING {MAXIMUM STEERING ANGLES I

61 FT MINIMUM TAXI STRIP WIDTH FOR 180 DEGREE TURN

MINIMUM TURNING RADII WITH NOSE WHEEL AT 90° (AIRCRAFT MAXIMUM TOWING ANGLE)

Aircraft Turning Radii SECTION 1 Figure 2 pa g e 6

Apr 02/87

ctiauenQer OPERATING MANUAL

PSP 601A-6

IDLE THRUST MAXIMUM

THRUST

50FT +

100FT +

110 +

120 +

1301

4 SOFT

APU EXHAUST DANGER AREA

+100 FT

+ 150 FT

4-160

J-170

Engine Intake and Exhaust Danger Areas, and APU Exhaust Danger Area

Figure 3

SECTION 1 Page 7/8

Apr 02/87


N0.3HYDRAUUC SYSTEM DC EXTERNAL POWER AC EXTERNAL POWER

PRESSURE REFUEUDEFUEL PANEL AND ADAPTER

Aircraft Servicing Points Figure 4 {Sheet 1)

SECTION 1 Page 9

Apr 10/95


© BRAKE ACCUMULATOR CHARGING POINTS AND INTERPHONE © OXYGEN SYSTEM CHARGING

VALVE AND GAUGE

ACCUMULATOR PRESSURE GAUGE

^ ^ k * RESERVOIR FILL

N0.1 HYDRAULIC SYSTEM AND REAR INTERPHONE

OIL LEVEL CONTROL PANEL

NO.3 HYDRAULIC SYSTBt RESBWOff) FILLS CONNECTION -

© Aircraft Servicing Points

Figure 4 (Sheet 2)

MO J HYDRAULIC SYSTEM ACCUMULATOR CHARGING POtflTAND PRESSURE GAUGE

SECTION 1 Page 10

Apr 10/95

chauenper OPERATING MANUAL

PSP 601A-6

Aircraft Antenna Locations Figure 5

SECTION 1 Page 11

Mar 10/95

canadair challenQsr


EFFECTIVITY

Q] A/C 5041 and 5146 CABIN DOOR SWITCH

o C3 3 O D

EXTERNAL HANDLE

Passenger/Crew Door SECTION 1 Figure 6 Page 12

Aug 14/02


BALANCE SPRING BOXES

PLUNGER

GUIDE TRACKS

HANDLE

HANDLE KEY LOCK

HANDLE HANDLE UNSTOW BUTTON

Baggage Compartment Door Figure 7 SECTION 1

Page 13 Apr 02/87

OXYGEN REFILL


UPPER ELECTRONICS EQUIPMENT BAY

DC GROUND POWER

FLIGHT CONTROL ACCESS

REFUELING CONTROL

7 UPPER ELECTRONICS EQUIPMENT BAY

K

HYORAUUC SYSTEM* SERVICE NO. 3

FLIGHT COMPARTMENT UNDERFLOOR ANO AVIONICS BAY ACCESS

BRAKE AND STEERING HYDRAULIC BAY

\r<8F FUGHT CONTROLS ACCESS

APU CONTROL AND GROUND AIR START

EQUIPMENT BAY DOOR

Service Doors and Panels SECTION 1 Figure 8 Page 14

Apr 02/87

chaJlenQer OPERATING MANUAL

PSP 601A-6

PASSENGER/CREW DOOR UNLOCKED LIGHT

Amber light comes on when the door is unlatched, or when the external handle is not stowed.

PASSENGER/CREW DOOR NOT READY LIGHT Amber light comes on when the T-handle is not correctly stowed.

SEAT BELT SIGN SWITCH

When set to ON, the cabin FASTEN SEAT BELT sign comes on and remains on until set to OFF or AUTO. When set to AUTO, the sign comes on if cabin air pressure is low, or the landing gear is down, or if the flaps are at any angle other than 0 degrees.

CABIN SIGNS

^ \ 0 N ff*<=^\ 0 F F

AUTO

NO/SMKG SEAT BLTS

PASSENGER/CREW DOOR READY LIGHT

Green light comes on when the external and internal handles are stowed.

NO SMOKING SIGN SWITCH

When set to ON, the cabin NO SMOKING sign comes on and remains on until set to OFF or AUTO. When set to AUTO, the sign comes on if cabin air pressure is low or the landing gear is down.

BAGGAGE COMPARTMENT DOOR UNSAFE LIGHT

Amber light comes on when door locking plungers are not safely engaged.

CENTRE PEDESTAL

EFFECTIVITY

A/C 5001 - 5040, 5042-5145, 5147 and subsequent

Door Indicat ion Lights and Cabin Signs Switches S E C T I O N 1 Figure 9 (Sheet 1) pa g e 15

Aug 14/02

dhsjJenqer OPERATING MANUAL

PSP 6 0 1 A - 6

CABIN PASSENGER/CREW DOOR INDICATOR PANEL

Pressing DOOR FAULT switch/light causes either green PASS DOOR LKD or red PASS DOOR UNLOCKED light to come on for the same conditions activating flight compartment indications. Red DOOR FAULT light comes on if microswitch contacts are stuck in lock position when door is unlocked.

PASS DOOR LKD

PASS DOOR UNLKD

DOOR FAULT

ADJACENT TO PASSENGER/CREW DOOR

PASS DR LKD LIGHT

NO SMOKING SIGN SWITCH

When set to ON, the cabin NO SMOKING sign comes on and remains on until set to OFF or AUTO. When set to AUTO, the sign comes on if cabin air pressure is low or the landing gear is down.

Green light comes on to indicate that all door latches and both handles are safely locked.

SEAT BELT SIGN SWITCH

When set to ON, the cabin FASTEN SEAT BELT sign comes on and remains on until set to OFF or AUTO. When set to AUTO, the sign comes on if cabin air pressure is low, or the landing gear is down, or if the flaps are at any angle other than 0 degrees.

CABIN SIGNS ON

OFF

AUTO

NO SMKG SEAT BLTS

PASS DR UNLKD LIGHT

Red light comes on whenever door latches are not in fully latched position or both handles are not safely locked.

BAG DR UNSAFE LIGHT

Amber light comes on if either of the door's two locking plungers are not fully engaged.

C E N T R E P E D E S T A L

EFFECTIV ITY

A/C5041 and 5146

Door Indicat ion Lights and Cabin Signs Switches S E C T I O N 1 Figure 9 (Sheet 2) pa g e 16

Aug 14/02


THIS PAGE INTENTIONALLY LEFT BLANK

SECTION 1 Page 16A

Mar 10/95

canactatr ctiauencjer


QUICK-RELEASE BUCKLE

Front of buckle can be turned to simultaneously release shoulder straps, crotch strap and one pan of lap belt; buckle remains attached to other pari of lap belt. Snap-in attachments are incorporated at strap ends so that safety harness can be easily connected.

SHOULDER STRAPS

LAP BELT,

LUMBAR SUPPORT

ARMREST CONTROL BUTTON

Releases armrest lock to allow angular adjustment of armrests.

RECUNE CONTROL LEVER

Releases seatback lock to allow adjustment from upright to recline. Seatback locks m position when lever is released.

LUMBAR SUPPORT CONTROL VALVE

Releases air from lumbar support to suit contour of pilot's back.

With pilot's back pressed against support, opening valve allows support to match contour of pilot's back. and dosing valve allows support to maintain selected shape. With no pressure on support, opening varve allows support to return to original shape.

HEIGHT CONTROL LEVER

Releases height lock to allow vertical adjustment of seat. Seat locks in selected position when lever is released. NOTE

Pilot's seat shown, copilot's seat identical but opposite.

Crew Seats Figure 10 (Sheet 1)

SECTION 1 Page 16B

Mar 10/95

chaueneter OPERATING MANUAL

PSP 601A-6

INERTIA REEL

INERTIA REEL CONTROL LEVER

When the lever is fully forward The inertia reel allows shoulder strap reei-ou: until strap acceleration exceeds Ig. then the reel locking device operates to prevent reel-out.

When the lever is fully rearward, the inertia reel is locked, thus allowing no reel-out of shoulder straps. and the harness is effectivery fixed.

FORWARD/REARWARD MOVEMENT CONTROL LEVER

Releases seat/ track lock to allow sea: forward/

rearward movement. Releasing control lever allows locking pins to engage when aligned with holes in track.

Track lock positions are approximately one inch apart.

Crew Seats Figure 10 (Sheet 2)

SECTION 1 Page 17

Apr 02/87


AURAL WARNING/JNTERCOM SPEAKBiS

Flight Compartment Instrument and Control Panel Arrangement

Figure 11 SECTION 1

Page 18 Apr 02/87


Pi lo t ' s Instrument Panel Figure 12

SECTION 1 Page 19

Apr 02/87

OPERATING MANUAL PSP601A-6

Copilot's Instrument Panel Figure 13

SECTION 1 Page 20

Apr 02/87


EFFECTMTY: A/C 5136 AM) SUBS

Centre Instrument Panel Figure 14 {Sheet 1)

SECTION 1 Page 20A

Apr 10/95

OPERATING MANUAL PSP 6C1A-6

©

E*GJNE JET WE/FYIOK urt

BFFECTMTY: JVC 8001 TO 6134

Centre Instrument Panel Figure 14 (Sheet 2)

SECTION 1 Page 206

Apr 10/95


EFFECTIVITY: A/C POST SB 601-0262

EFFECT1VITY: A/C 5001,5027 AND SUBS AND A/C POST SB 601-0225

© ©

EFFECTIVITY: A/C POST SB 601-0262

e

Centre Instrument Panel SECTION 1 Figure 14 (Sheet 3) Page 21

Apr 10/95


j Overhead Panel and Glareshield S E C T I O N 1 Figure 15 (Sheet 1) Page 22

May 01/96

chaflsriqer OPERATING MANUAL

PSP 6 0 1 A - 6

HI TEMP HI TEMP HI TEMP

&

A ® MISC LTS ® I ROARDING DOMI COMR SERVICE

ON V S ^ O N W ON V ^ / O W I W / O N

PLS OFF STOV

r— LANDING LTS - i II£FT NOtE RIGHT I

RE COG/ TAXI LT

OFF/ ON*

PLS OFF

STDY OFF

® r EXTERNAL LTS -JOVMDFNL I H A V WING ANT1COLL ' x ^ C X 1KAV WtMO ANTI COU

\OFF / f i \ O F F / f i \ O F F OM 'ON ON

OFF •RT

EFFECTIVITY : A/C POST SB 601-0363

EFFECTIVITY : A/C 5041 AND 5146

o

?» L-MTH STAGE'R

WJBH

ON/ OFF

•LEED OLOSID

DUCT I M I L |

OUCT MOM LOOP A /£=N

BOTH K=?J LOOPB > - ^

| M.CEO I CLOUD

\m\\ OPEN

I I BLEEQ I CLOUD OUCT

11 PAH. I

—PUSH ON/ OFF OFF

FAIL I °" I1

1 '*IL 1

z @ CABIN PRESSURIZATION

EFFECTIVITY : A/C 5135 AND SUBS

e EFFECTIVITY : A/C 5135 AND SUBS

G

Overhead Panel and Glareshield SECTION 1 Figure 15 (Sheet 2) page 23

Aug 14/02

canadair chanenqer


r ©

Centre Pedestal SECTION 1 Figure 16 (Sheet 1) Page 24

Mar 10/95

canadair chanencjer OPERATING MANUAL

PSP 601A-6

I EFFECTIVITY: A/C 5067, 5087 AND SUBS

e

f LASEREF /

I A U O N / ^ > t ^ ATT | ALIGN |

| NAVRDY |

| ON BAH |

FAULT " |

NO AIR |

BATTFAIL J

. 1 1

mm /TEST J

EFFECTIVITY : 5041 and 5146 EFFECTIVITY: A/C POST SB 601-0231

©

Centre Pedestal SECTION 1 Figure 16 (Sheet 2) Page 25

Aug 14/02

canaclair chaUenqer OPERATING MANUAL

PSP 601A-6

Pi lot 's Console, Side and Facia Panels Figure 17

SECTION 1 Page 26

Apr 10/95


Copilot's Console, Side and Facia Panels SECTION 1 Figure 18 P a g e 27

Apr 10/95

Documents

Operating Manual - PSP 601A-6 (Volume 2) - … · steering angle, and the turning radii for the maximum towing angle of ... WIDTH FOR 180 DEGREE TURN MINIMUM TURNING RADII WITH NOSE