AIRPLANE SYSTEMS.................................................. 1-67General.................................................................... 1-67Air-Conditioning/Pressurization System ................ 1-67Aural/Visual Warning System................................. 1-68Automatic Flight Control System ........................... 1-70Auxiliary Power Unit .............................................. 1-72Communications ..................................................... 1-73Electrical Power System ......................................... 1-74Emergency Equipment............................................ 1-74Fire Protection System............................................ 1-76Flight Control System............................................. 1-76Flight Instruments ................................................... 1-78Fuel System............................................................. 1-80
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Hydraulic Power System..........................................
1-82
Ice and Rain Protection System ...............................
Center Pedestal................................................
1-131-11
First Officer’s Instrument Panel......................
1-17
Revision 2—June 2004 1-iii
1-12 First Officer’s Side Panel................................ 1-181-13 First Officer’s Side Console............................ 1-191-14 Control Wheel Switches ................................. 1-201-15 Flight Compartment Aft View........................ 1-211-16 Pilot Seats........................................................ 1-221-17 Seat Adjustment .............................................. 1-251-18 Intrusion-Resistant Cockpit
Door Entry System.......................................... 1-261-19 Intrusion-Resistant Cockpit
Door Entry System—Passenger Side.............. 1-271-20 Intrusion-Resistant Cockpit
Door Entry System—Flightdeck Side ............ 1-281-21 Wardrobe Area Equipment ............................. 1-311-22 Passenger Compartment Forward Area .......... 1-321-23 Passenger Compartment Aft Area .................. 1-351-24 Aft Lavatory.................................................... 1-371-25 Aircraft Doors ................................................. 1-381-26 Passenger Door—Operating Controls............. 1-401-27 Passenger Door—Interior Placards................. 1-43
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1-28
Passenger Door—Exterior Controls and Placards .......................
1-441-29
Avionics Bay Door .........................................
This chapter contains brief descriptive information on individualfeatures of the airplane structure and systems. The information con-tained herein does not supersede, nor is it intended to substitute for,any data contained in the manufacturer's system or operating manu-als. For detailed airplane description and operating information,refer to the manufacture’s data.
Revision 1—January 2003 1-1
GENERALThe airplane is a light-alloy, low-wing, twin-engine airplane with aGeneral Electric CF34-3B1 engine on each side of the fuselage anda Garrett auxiliary power unit. The aircraft overall length is 87 feet10 inches (26.77 M), with a wingspan of 69 feet 6 inches (21.21 M)(Figure 1-1).
Aircraft taxiing and turning radii are shown in Figure 1-2.
The airplane requires a minimum flight crew of two. The numberand arrangement of passenger seats may vary.
STRUCTURESGENERAL
The airplane is primarily constructed from aluminum alloy, withcertain structures made from other materials. The primary structuresinclude the fuselage, nacelles, wings, and stabilizers.
FUSELAGEThe semimonocoque fuselage structure has a cover made fromchem-milled skin panels with bonded doublers. The fuselage ispressurized between fuselage stations (FS) 202.75 and FS 621. Allskin-panel joints in this area are pressure and weather sealed. The
MAXIMUM STEERING• SYMMETRICAL THRUST• NO DIFFERENTIAL BRAKING• SLOW CONTINUOUS TURN• AFT CENTER OF GRAVITY• MAX GROSS WEIGHT• DRY RUNWAY
Figure 1-2 Aircraft Taxiing and Turning Radii
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skin panel joints forward of FS 202.75 and aft of FS 621 are weathersealed only. The fuselage has a cylindrical cross section for most ofits length. It becomes D-shaped between FS 409 and FS 559. Thiscreates a space for the wing center section and main landing gearwheel wells. The fuselage comprises the fuselage main structure andaerodynamic fairings. Main fuselage sections include the following:
●
Nose cone
●
Forward fuselage
●
Forward mid fuselage
●
Forward fuselage extension
1-4 Revision 1—January 2003
● Mid fuselage
● Aft fuselage extension
● Aft fuselage
● Fuselage-to-stabilizer section
FLIGHT COMPARTMENT
The flight compartment forward portion (Figure 1-3) has the follow-ing control panel and features:
The flight compartment aft portion (Figure 1-15) includes thefollowing:
● Circuit-breaker panels
● Miscellaneous equipment
● Captain and first officer seats
CIRCUIT
AIRPLANE LEVEL INDICATORS
CIRCUIT
Revision 2—June 2004 1-21
The captain and first officer seats (Figure 1-16) are similar in form,fit, and function. Each seat has a two-stage lever for fore and aftmovement, a seat height lever for vertical movement, and a reclinelever for backrest adjustment. Each seat has an inertia reel control,inertia reel and shoulder straps, lapbelt, crotch belt, and quick-release buckle.
ARMRESTADJUSTMENTKNOBARMREST RETURNSTO RESET POSITION
LUMBAR CONTROL• LEFT HAND KNOB FORUP/DOWN ADJUSTMENT
LAMBS WOOL SEAT COVERS(REMOVEABLE)
CROTCHSTRAP
HARNESS RELEASEBUCKLE
(TO RELEASE, ROTATEKNOB IN EITHER DIRECTION)
LIFE VESTSTOWAGE
POUCH
Revision 1—January 2003 1-23
HEADREST(NON ADJUSTABLE)
STEP BRACKET(TO FACILITATE ACCESSTO ESCAPE HATCH)
SHOULDER HARNESSREEL CONTROL
• DOWN – RELEASED• UP – LOCKED
LUMBAR CONTROL• RIGHT HAND KNOB FORFORWARD/AFT ADJUSTMENT
FORWARD/AFTTRAVEL LEVER• FIRST STAGE - 1 INCH TRACKING STEPS• SECOND STAGE - PRIMARY STOP RELEASE
BACKREST RECLINEHANDLELIFT HANDLEFOR ADJUSTMENT
SEAT UP/DOWNADJUSTMENT(LIFT HANDLEFOR ADJUSTMENT)
THIGH COMFORT LEVER• LH/RH INDEPENDENT
(TWO POSITION LEVERS,LOCATED BELOW THE SEAT)
SERIAL NUMBER 7452 AND SUBSEQUENT
NOTE:CONTROL OF THE COPILOT SEAT IS OPPOSITE OF PILOT SEAT.
Figure 1-16 Pilot Seats (2 of 2)
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Seat Adjustment
Adjust the seat position with the appropriate control levers to obtainthe optimum eye reference position relative to the eye referenceposition datum located on the forward center window post. Use thehandhold on the upper console to assist. Keeping your head in theforward facing position, look toward the ball indicators and adjustthe seat as necessary.
The correct eye reference position is established when the whiteindicator ball appears in the center of the orange ball. The resultingeye level should be approximately in the center of the forward win-dow (Figure 1-17).
1-24 Revision 1—January 2003
NOTEDuring adjustment, the seat must be in the fullupright position.
Correct seat placement (height, fore, and aft):
● All flight controls unrestricted throughout full travel
● Flight instruments and warning lights visible without beingobstructed
FLIGHTDECK SECURITY DOORThe area between the forward galley and the flightdeck contains theFLIGHTDECK SECURITY DOOR (Figure 1-18). This intrusionresistant (reinforced) cockpit door complies with the intrusion andballistic resistance requirements of 14 CFR part 25 Amendment 25-106 and CFR part 121 Amendment 121-288.
1-26 Revision 1—January 2003
FWD
G1 GALLEYREF
WARDROBEASSEMBLY
REF
COCKPIT DOORASSEMBLY
Figure 1-18 Intrusion-Resistant Cockpit Door Entry System
In addition, the intrusion resistant flightdeck door complies with allother applicable regulations including, but not limited to: staticstrength, rapid decompression, smoke evacuation and penetration,required airflow, and emergency ingress and egress.
Components of the intrusion resistant flightdeck door system (Fig-ure 1-19) include the following: cockpit door main latch,mechanical deadbolt, two quick-release hinge pins, view lens,decompression panel, and decompression latch.
FLIGHT DECK DOOR
AUTHORIZED PERSONNEL ONLY
Revision 1—January 2003 1-27
MAINDEADBOLT
LATCH
DEADBOLTASSEMBLY
UPPERDECOMPRESSION
PANEL
COCKPIT DOOR
HINGEASSEMBLY
HINGEASSEMBLY
FWD
CREW ONLY
CREW ONLY
FLIGHTDECK DOORAUTHORIZED PERSONNEL ONLY
Figure 1-19 Intrusion-Resistant Cockpit Door Entry System— Passenger Side
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To secure the flightdeck door during flight, slide the main latch intoposition to lock the door (Figure 1-20).
NOTEThis door will be retrofitted on all Pinnacle CRJs.
DOOR MUST B
AND LOCKE
ANY FLUID SPILLAGE NEAR LATCH
REQUIRES MAINTENANCE ATTENTION
CAUTION - RELEASETHE LOWER HINGE PIN FIRST
CAUTION - RELEASE
THE LOWER HINGE PIN FIRST
1-28 Revision 1—January 2003
FWD
FOR GROUND USE ONLYDEADBOLT POSITIONS
UNLOCKED
LOCKEDKEY OPERABLE
LOCKEDKEY INOPERABLE
FOR GROUND USE ONLY
DEADBOLT POSITIONSUNLOCKED
UNLOCKED
LOCKED
LOCKED
KEY OPERABLE
KEY OPERABLE
LOCKED
LOCKED
KEY INOPERABLE
KEY INOPERABLE
DOOR MUST BE CLOSEDAND LOCKED AT ALL TIMES
COCKPIT DOOR EMERGENCY OPENING
1. UNLOCK AND LIFT LOWER HINGE PIN2. UNLOCK AND PULL DOWN UPPER HINGE PIN3. KICK OUT DOOR AT HINGE SIDE4. ROTATE DOOR CLOCKWISE AND STOW AGAINST THE GALLEY
ANY FLUID SPILLAGE NEAR LATCHREQUIRES MAINTENANCE ATTENTION
E CLOSED
D AT ALL TIMES
COCKPIT DOOR EMERGENCY OPENING
1. UNLOCK AND LIFT LOWER HINGE PIN
2. UNLOCK AND PULL DOWN UPPER HINGE PIN
3. KICK OUT DOOR AT HINGE SIDE
4. ROTATE DOOR CLOCKWISE AND STOW AGAINST
THE GALLEY
Figure 1-20 Intrusion-Resistant Cockpit Door Entry System— Flightdeck Side
The flightdeck door must be kept closed and locked at all times dur-ing flight except to permit access and egress in accordance with theFOM and this FCOM.
Any time the flightdeck door is opened in flight, a challenge andresponse closing and locking verification must be used to verify thatthe door is closed and locked.
Any time one of the required flight crew leaves the flightdeckanother crew member must be present in the flightdeck to ensurethat the required crew member is not locked out of the flightdeck.
Revision 2—June 2004 1-29
Operating Procedures
Normal—To secure the cockpit door for flight, slide the main latchinto position to lock the door. The deadbolt assembly is for grounduse only or as directed by the MEL.
Emergency Procedures
Emergency Egress—Unlock and lift lower hinge pin. Unlock andpull down upper hinge pin. Kick out door at hinge side. Rotate doorclockwise and stow against the galley.
CAUTION
Due to the weight of the door, this proceduremust be started from the lower hinge pin.
Emergency Ingress—In the event that the crew becomes trapped inthe cockpit or becomes incapacitated, rescue personnel can enterthrough the cockpit upper hatch, which is operable from both insideand outside the cockpit.
Decompression Panel—The decompression panel is held on thedoor by the decompression latch. When the pressure differencebetween the passenger cabin and the flightdeck is more than a presetlimit, the latch will release the panel.
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PASSENGER COMPARTMENT
The area just behind the flight compartment bulkhead, on the leftside, is a wardrobe for miscellaneous equipment storage (Figure1-21). The attendant and observer seats are in this area. Whenrequired, the seats pull out on sliding rails from the wardrobe andposition across the center aisle. The seat has a safety harness andprovides a comfortable, safe place for the observer to view the air-plane controls. The seat safety harness is a four-point harness withan adjustable lapbelt and shoulder straps. The harness is completewhen both sides of the lapbelt and the two shoulder straps connectto the quick-release buckle.
Other equipment in the wardrobe area includes the following:
1-30 Revision 1—January 2003
● Attendant’s forward miscellaneous switch panel
● Attendant’s intercom and lighting control panel
● Attendant’s and observer’s life vests
● Observer’s oxygen mask/regulator storage unit
● Music and announcement MP3 player (if installed)
● Cabin log book storage unit
● Portable oxygen, except on some models of the 440LR (SeeCRJ variations page)
The aircraft has the following eight exterior doors (Figure 1-25):● Passenger door● Avionics bay door● Crew escape hatch● Galley service door● Right overwing emergency exit● Aft equipment bay door● Cargo bay door● Left overwing emergency exit
A door warning system provides crew indications about the condi-tion and safety of the following pressurized aircraft doors:
● Passenger door● Galley service door● Avionics bay door● Overwing emergency exits● Cargo bay door
Passenger Door
The passenger door, which is the main entrance/exit for passengersas well as flight crew, is at the forward left-hand side of the fuselage.
Revision 2—June 2004 1-39
The door incorporates integral stairs with a retractable top and bot-tom step and two folding handrails. It opens outwards anddownwards. A gas spring assists with lowering the door, and apower-assist function assists door closing (Figure 1-26).
The door rests upon a support wheel when the door is in the fullyopen position. Stairway lighting is provided in the risers of the stairsand at the threshold area. Stairway lighting is controlled byBOARDING LIGHTS ON/OFF switch/light at the forward atten-dant’s console.
Passenger Door Operation—Inner Handle
The inner door handle rotates downwards to lock and upwards tounlock the passenger door. Operating instructions are placarded onthe door (Table 1-1).
Table 1-1 DOOR OPERATION
TO OPEN TO CLOSE
1. LIFT HANDLE UP 1. PULL DOOR IN
2. PUSH DOOR OUT FIRMLY TO ARMS LENGTH
2. PUSH HANDLE FULLY DOWN
3. CHECK INDICATION MARKS
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INNER HANDLELOCKS AND UNLOCKS LATCHPINS AND UPPER ROTAY
PUSHPLATE
1. MAXIMUM LOAD CAPABILITY- 1000 LG. (454KG)2. MAXIMUM NUMBER OF PASSENGERS ALLOWED ON THE STAIRWAY- 4
NOTICE
DOOR OPERATIONTO OPEN
1. LIFT HANDLE UP2. PUSH DOOR OUT FIRMLY TO ARMS LENGTH
1. PULL DOOR IN2. PUSH HANDLE FULLY DOWN3. CHECK INDICATION MARKS
TO CLOSE
CAUTIONDO NOT OPERATE DOOR ASSIST SYSTEMDURING POWER SWITCHING.(APU GENERATOR TO EXTERNAL POWER)
1-40 Revision 2—June 2004
DOORPULL-INGRIP
LATCHES. OPENS AND CLOSESVENT FLAP AND OUTER HANDLE
2. Maximum number of people permitted onthe stairway is four.
Door Operation (Normal)
Normal door operation is accomplished by executing the followingprocedures. The interior single-lever handle rotates downward tolock and upward to unlock. Total rotation of the handle is approxi-mately 53°.
Revision 2—June 2004 1-41
To open from the interior (Figure 1-27):
● An initial 22° free motion of the handle before unlatchingunlocks the latch mechanism and opens the pressurizationflap in the exterior door surface. Continued rotation of thehandle unlatches the upper two “C” rotary latches and disen-gages the four latch pins.
● As the door is pushed outward, it descends in a controlledgradual movement damped by the motor-actuator. The doorground support wheel deploys from the stowed position.
To open from the exterior (Figure 1-28):
● Grasp the outer handle on its lower edge and rotate upwardand outward. This action unlocks and opens the mechanism,opening the pressurization flap in the exterior door surface.
● Pulling outward on the handle rotates the door downward.The opening sequence then follows that described for theoperation from the interior.
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The handrails are secured in accordance with the handrail placard(Table 1-2).
To close from the interior:
● The door is pulled up using the DOOR ASSIST CLOSEswitch on the forward attendant’s panel (press and hold
Table 1-2 HANDRAIL OPERATION
TO USE TO FOLD
BOTH PINSIN PLACE
THRU POSTS
BOTH PINSIN PLACE
THRU STAIRS
1-42 Revision 2—June 2004
switch until door is fully closed).
NOTEDo not operate door-assist system duringpower switching (APU generator to externalpower).
An interlock on the cam mechanism of thepassenger door prevents the inner handle frommoving to the closed position until the door isfully closed.
● To latch the door, pull and hold the door completely closedby the assist handle provided in the door steps. Simulta-neously push fully down on the interior handle to completethe latching operation.
To close from the exterior, reverse the sequence described for open-ing from the exterior.
1. LIFT HANDLE UP2. PUSH DOOR OUT FIRMLY TO ARMS LENGTH
1. PULL DOOR IN2. PUSH HANDLE FULLY DOWN3. CHECK INDICATION MARKS
TO OPENLIFT HANDLEPUSH DOOR
GREENMARKSMUSTALIGN
GREENMARKSMUSTALIGN
EXIT
Revision 2—June 2004 1-43
OPEN
HANDRAIL OPERATIONTO FOLDTO USE
BOTH PINSIN PLACE
THRU POSTS
BOTH PINSIN PLACE
THRU POSTS
NON-RADIOACTIVELUMINESCENT
MARKER STRIP LOCKED/UNLOCKEDINDICATOR
GREENMARKSMUSTALIGN
CAUTIONDO NOT OPERATEHANDLE IN FLIGHT
EXITPULL
CLOSED
NOTICE1. MAXIMUM LOAD CAPACITY–1000 LB (454kg)2. MAXIMUM NUMBER OF PASSENGERS ALLOWED ON STAIRWAY–4
GREENMARKSMUSTALIGN
NOTE: GREEN LOCKED INDICATOR MUST BE VISIBLE
Figure 1-27 Passenger Door—Interior Placards
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DOOR VENT FLAP • CLOSES WHEN EITHER EXTERIOR OR INTERIOR HANDLE IS STOWED
• OPENS IMMEDIATELY WHEN EITHER EXTERIOR OR INTERIOR HANDLE IS OPERATED
DOOR HANDLE
1-44 Revision 2—June 2004
Operation (Emergency)
The operation of the passenger door as an emergency exit followsexactly the same procedure as described for normal operation. Allapplicable requirements for designation of the passenger door as anemergency exit are contained within the appropriate BombardierAerospace design compliance documentation. Crews should beaware that the required labeling and placarding must be in place forregulatory compliance.
EMERGENCY EXIT
PULL HANDLE UPTO OPEN DOOR
EMERGENCY EXIT
PULL HANDLE UPTO OPEN DOOR
FWD PASSENGER DOOR EXTERIOR
NOTE: STAND CLEAR OF DOOR DURING OPENING
Figure 1-28 Passenger Door—Exterior Controls and Placards
The latched and locked position of the two rotary latches and thelatched position of the four latch pins is visible to the flight crewfrom the interior of the aircraft. There is a visual indication for thelocked condition of the roll latch shaft.
Indications for the rotary latches consist of green-colored identifica-tion strips. One portion of these strips is on the rotary latch, and theother is on the fixed door structure. A register on the upper lock alsoidentifies a locked condition of the roll latch shaft.
The four door side latch pins are similarly marked by green identifi-cation registers incorporated at the end of each bolt attaching the
Revision 2—June 2004 1-45
latch pin to the push rod mechanism. Each identification registerprotrudes through a slot in the inner door surface and is weather-proofed by a transparent cover. The witness marks are underneaththis transparent cover and marked with placards in close proximityto identify the marks at each pin location.
A closed condition of the exterior handle and closed condition of thedoor pressurization flap, as well as a lower lock active position, isverified by a flag indicator. This shows a message indicator betweentwo witness marks and can be viewed through a window centrallylocated in a stair riser. When the lower lock is in the locked position,the flap mechanism directly actuates the red UNLOCK flag to agreen LOCKED flag.
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Flight Deck Indications
Instrument Panel
The passenger door visual and aural indications on the flight deckare controlled by the EICAS data concentrator units and the mastercaution and warning light system.
Door safety is assured by a combination of separate proximityswitch electronic unit output conditions, processed by EICAS inputlogic. If any one of the conditions show a fault, the master cautionand warning lights illuminate and flash appropriately. If a red warn-ing message is displayed on the EDP 1 primary display, a triplechime sounds and the door aural message annunciates. If an amber
1-46 Revision 2—June 2004
caution message is displayed, a single chime sounds. See Table 1-3and Table 1-4 for the light indications, EICAS messages, and corre-sponding door status.
The avionics bay door (Figure 1-29), under the fuselage forwardarea, opens inward and moves forward and aft on tracks. Pressingthe push plate extends the handle for door operation. Turning thehandle 90º, counterclockwise to open and clockwise to close, oper-ates the latch mechanism to engage or disengage two lockpins fromsockets on the fuselage. To set the handle in its recess, push in untilthe trigger plate’s spring-loaded latch engages with the housing.
AFT LATCHPIN
ROLLER
Revision 2—June 2004 1-51
EXTERNALHANDLE
PUSHPLATE
(TRIGGER)KEY
LOCK
FORWARDLATCH FITTINGPROXIMITY SENSOR
TRACK(TYPICAL)
Figure 1-29 Avionics Bay Door
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NOTERestow the avionics bay door handle if it isnecessary to completely open the avionicsdoor for any reason. It is important to remem-ber to un-stow (move the handle to theunlatched position) prior to closing the avion-ics bay door, or damage to the latch pins andsurrounding structure could occur.
Crew Escape Hatch
The crew escape hatch (Figure 1-30) is on the flight compartmentceiling, above the center pedestal. Pressing the push plate on the
1-52 Revision 2—June 2004
outer handle ejects the handle from its recess. Then turning clock-wise to open, counterclockwise to close, the outer handle operatesthe latch mechanism. To retract the handle, align it with the recessand push in until the push plate engages the spring-loaded latch.
Pushing the push plate holding the inner handle allows the innerhandle to turn and operate the latch mechanism. To set the innerhandle in its recess, align it with the recess, then push it in until thetrigger plate engages with the spring-loaded latch.
There is no EICAS caution or warning message for this door. Theonly method for ensuring that the door is secure is for the crew tovisually check the door.
RRNWEA-13C CH01A.fm Page 53 Tuesday, December 14, 2004 2:36 PM
LATCHPINGS
(TYPICAL) RELEASEBUTTON
INNERHANDLE
LOCK PLATE(HATCH CLOSED)
HINGE HOOK(TYPICAL)
EXIT
CLOSE
STAY CLEAR OF HATCH DURING OPENING
TO REMOVE
OPEN HATCHPUSH UP AND AFT
LOCKEDMARKSMUSTALIGN
LOCKEDMARKSMUSTALIGNOPEN
EMERGENCY EXIT
CLOSE
OPEN
“PUSH” RELEASETURN HANDLE TO “OPEN”
PUSH DOOR IN
NOTE TO REMOVE THE CREW ESCAPE HATCH, PUSH THE HATCH UP AND AFT
EXTERIOR HANDLEWITH PUSH PLATE
INTERIOR VIEW
EXTERIOR VIEW
Figure 1-30 Crew Escape Hatch
Revision 2—June 2004 1-53
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RRNWEA-13C CH01A.fm Page 54 Tuesday, December 14, 2004 2:36 PM
Galley Service Door
The plug-type galley service door (Figure 1-31) opens outward,with an initial inward and upward movement. The interior handlerotates clockwise to unlock (OPEN) and counterclockwise to lock(CLOSE) the service door.
Rotating the interior handle to the OPEN position unlatches the doorand raises it for opening. The exterior handle has a push plate andkey lock. With the door unlocked, pressing the push plate extendsthe handle. Moving the exterior handle to the OPEN position oper-ates the door in the same manner as the interior handle. The door isthen opened and stowed against the fuselage in a locked position.
To close the service door, the latch knob is pulled and the doorpushed or pulled into its opening. Rotating the interior or exteriorhandle to the CLOSED position operates the door latches.
From inside the airplane, pulling the exterior handle stow knobretracts the exterior handle. The stow knob is then push back in forstowing. From outside the aircraft, the exterior handle is pushed into complete the door closing sequence.
RRNWEA-13C CH01A.fm Page 55 Tuesday, December 14, 2004 2:36 PM
EMERGENCY EXIT
“PUSH” AND TURN
HANDLE TO “OPEN”
PULL DOOR
OPENCLOSED
FWD
GALLEY SERVICE DOOREXTERIOR
PUSHPLATE
(TRIGGER)
KEY LOCK
EXTERNALHANDLE
EXTERIOR VIEW
ARTICULATEDHINGE
Figure 1-31 Galley Service Door (1 of 2)
Revision 2—June 2004 1-55
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RRNWEA-13C CH01A.fm Page 56 Tuesday, December 14, 2004 2:36 PM
ASSIST HANDLE
EXITLUMINESCENTMARKER STRIP
CAUTIONDO NOT OPERATEHANDLE IN FLIGHT
TO CLOSE1. GRASP ASSIST HANDLE2. UNLOCK LATCH KNOB3. SLIDE DOOR RIGHT4. PULL DOOR IN5. ROTATE HANDLE TO CLOSE POSITION6. STOW EXTERNAL HANDLE7. CHECK INDICATION MARK
TO STOW EXTERNAL HANDLE1. PULL IN KNOB (APPROX 2 INCHES)2. PUSH KNOB FULLY OUT (FLUSH WITH GUARD)
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