REVISION 2: APR 28/2011 TP.70 · QRH-366-00-00-99333-TN3 LEP.70.1 Page Date Page Date ORIGINAL...

QRH-366-00-00-99333-TN3TP.70.0

Title

REVISION 2: APR 28/2011

THIS PAGE INTENTIONALLY LEFT BLANK

QRH-366-00-00-99333-TN3

QRH - 365-00-00-99333-TN3TL.70.1

LETTER OF TRANSMITTAL

(Revision 2: APR 28/2011)

• Insert pages issued in the proper locations according to the List of Effective Pages.

To: Holders of Boeing 737- 300 IAI Special Freighter:

IAI No.

Model Type

Customer Effectivity

Code

Boeing LineNo.

Variable No.

Serial No.

RegistryNo.

RB127 B737-34S GIA 325 2983 PR091 29108 TF-TNM

RB126 B737-34S GIA 326 3001 PR092 29109 OO-TNL

Inquiries regarding this publication should be submitted to:

ISRAEL AEROSPACE INDUSTRIES LTD.

CUSTOMER - SERVICE FAX:

(972)3-9358953

Transmittal

APR 28/2011


QRH - 365-00-00-99333-TN3

Page Date Page Date

List of Effective Pages

ORIGINAL ISSUE: AUG 15/2010REVISION 1: FEB 10/2011REVISION 2 APR 28/2011

Title Page APR 28/2011

LETTER OF TRANSMITTALTL.70.1.....................APR 28/2011

LIST OF EFFECTIVE PAGESLEP.70.1...................APR 28/2011LEP.70.2...................APR 28/2011

TABLE OF CONTENTSTOC.70.1.................AUG 15/2010TOC.70.2..................APR 28/2011

CHAPTER 0PREFACE

PF.70.1 .....................APR 28/2011

CHAPTER NC

NORMAL CHECKLISTSNNC.0.70.1 .............AUG 15/2010NNC.0.70.2 .............AUG 15/2010NNC.0.70.3 .............AUG 15/2010NNC.0.70.4 .............AUG 15/2010

CHAPTER NNC

SECTION 0 MISCELLANEOUS

NNC.0.70.1 .............AUG 15/2010NNC.0.70.2 .............AUG 15/2010NNC.0.70.3 .............AUG 15/2010NNC.0.70.4 .............AUG 15/2010NNC.0.70.5 .............AUG 15/2010

SECTION 1 AIRPLANE GENERAL, EMERGENCY

EQUIPMENT, DOORS, WINDOWSNNC.1.70.1 ............. AUG 15/2010NNC.1.70.2 ............. AUG 15/2010NNC.1.70.3 ............. AUG 15/2010NNC.1.70.4 .............. FEB 10/2011NNC.1.70.5 .............. FEB 10/2011NNC.1.70.6 .............. FEB 10/2011NNC.1.70.7 .............. FEB 10/2011NNC.1.70.8 .............. FEB 10/2011

SECTION 2AIR SYSTEMS

NNC.2.70.1 ............. AUG 15/2010NNC.2.70.2 ............. AUG 15/2010NNC.2.70.3 ............. AUG 15/2010

SECTION 8FIRE PROTECTION

NNC.8.70.1 ..............APR 28/2011NNC.8.70.2 ..............APR 28/2011NNC.8.70.3 ..............APR 28/2011NNC.8.70.4 ..............APR 28/2011NNC.8.70.5 ..............APR 28/2011NNC.8.70.6 ..............APR 28/2011NNC.8.70.7 ..............APR 28/2011NNC.8.70.8 ..............APR 28/2011NNC.8.70.9 ..............APR 28/2011

SECTION 13 HYDRAULICS

NNC.13.70.1 ........... AUG 15/2010NNC.13.70.2 ........... AUG 15/2010NNC.13.70.3 ........... AUG 15/2010NNC.13.70.4 ........... AUG 15/2010NNC.13.70.5 ........... AUG 15/2010NNC.13.70.6 ........... AUG 15/2010

LIST OF EFFECTIVE PAGES

QRH-366-00-00-99333-TN3LEP.70.1APR 28/2011

Page Date Page Date

List of Effective Pages

NNC.13.70.7............AUG 15/2010NNC.13.70.8............AUG 15/2010NNC.13.70.9............AUG 15/2010NNC.13.70.10..........AUG 15/2010NNC.13.70.11..........AUG 15/2010

SECTION 14 LANDING GEAR

NNC.14.70.1............AUG 15/2010NNC.14.70.2............AUG 15/2010NNC.14.70.3............AUG 15/2010NNC.14.70.4............AUG 15/2010NNC.14.70.5............AUG 15/2010NNC.14.70.6............AUG 15/2010NNC.14.70.7............AUG 15/2010NNC.14.70.8............AUG 15/2010NNC.14.70.9............AUG 15/2010NNC.14.70.10..........AUG 15/2010

SECTION 15WARNING SYSTEMS

NNC.15.70.1............AUG 15/2010NNC.15.70.2............AUG 15/2010

EVACUATIONBack Cover.70.1.1 ...AUG 15/2010Back Cover.70.1.2 ...AUG 15/2010

QRH-366-00-00-99333-TN3LEP.70.2 APR 28/2011

Subject Section/Page

Table of Contents

CHAPTER 0PREFACE

MODEL IDENTIFICATION SECTION 1

General ........................................................................................... PF.70.1

CHAPTER NC

NORMAL CHECKLISTS

PREFLIGHT ............................................................................ NNC.0.70.1

BEFORE START .................................................................... NNC.0.70.1

BEFORE TAXI ....................................................................... NNC.0.70.2

BEFORE TAKEOFF ............................................................... NNC.0.70.2

AFTER TAKEOFF ................................................................. NNC.0.70.2

DESCENT ............................................................................... NNC.0.70.3

APPROACH ............................................................................ NNC.0.70.3

LANDING ............................................................................... NNC.0.70.3

SHUTDOWN .......................................................................... NNC.0.70.3

SECURE .................................................................................. NNC.0.70.4

CHAPTER NNC

SECTION 0 MISCELLANEOUS

EMERGENCY DESCENT ............................................................NNC.0.70.1DITCHING < > ..............................................................................NNC.0.70.2

SECTION 1 AIRPLANE GENERAL, EMERGENCY EQUIPMENT, DOORS, WINDOWS

CARGO DOOR .............................................................................NNC.1.70.1ENTRY DOOR ..............................................................................NNC.1.70.4SERVICE DOOR ...........................................................................NNC.1.70.5

TABLE OF CONTENTS

QRH-366-00-00-99333-TN3TOC.70.1AUG 15/2010

Subject Section/Page

Table of Contents

MAIN CARGO DOOR ................................................................. NNC.1.70.6

SECTION 2AIR SYSTEMS

PACK TRIP OFF ........................................................................... NNC.2.70.1

SECTION 8FIRE PROTECTION

SMOKE, FIRE OR FUMES .......................................................... NNC.8.70.1MAIN DECK CARGO - SMOKE, FIRE OR FUMES ................. NNC.8.70.5MAIN DECK CARGO SMOKE DETECTION SYSTEM FAULT .......................................................................... NNC.8.70.7MAIN SMOKE NO FLOW .......................................................... NNC.8.70.8

SECTION 13 HYDRAULICS

HYDRAULIC PUMP LOW PRESSURE ................................... NNC.13.70.1HYDRAULIC PUMP OVERHEAT ........................................... NNC.13.70.1LOSS OF SYSTEM A < > .......................................................... NNC.13.70.2MANUAL REVERSION < > OR LOSS OF SYSTEM A AND SYSTEM B < > ............................................. NNC.13.70.6

SECTION 14 LANDING GEAR

MANUAL GEAR EXTENSION < > .......................................... NNC.14.70.1PARTIAL OR ALL GEAR UP LANDING < > ......................... NNC.14.70.8

SECTION 15WARNING SYSTEMS

WARNING HORN - CABIN ALTITUDE OR CONFIGURATION .............................................................. NNC.15.70.1

EVACUATIONEVACUATION ............................................................BACK COVER.70.1.1

QRH-366-00-00-99333-TN3TOC.70.2 APR 28/2011

QRH-366-00-00-99333-TN3QRH-366-00-00-99333-TN3QRH-366-00-00-99333-TN3

QRH-366-00-00-99333-TN3

CHAPTER 0

PREFACE


QRH-366-00-00-99333-TN3

QRH - 365-00-00-B99333-TN3PF.70.1

General- These B737-300 Flight Crew Operations Manual (FCOM) and Quick

Reference Handbook (QRH) pages are supplementing Operating Manual.

- The data in these supplement with striped-bordered pages reflect all thechanges in the operation of this airplane as a result of the conversion toSpecial Freighter (SF) configuration.

- Supplement Special Freighter text context is identified by (Special Freighter) readout.

- When data changes are made to figures or new figures are added, they areidentified by a symbol ( for minor change or for majorchange).

- The striped-border pages in the Supplement of Special Freighter arenumbered XX.70.XX.

- These B737-300 (FCOM) and (QRH) Supplement pages must be insertedinto the Handbook at the end of each relevant section and may not beremoved without authorization.

- For procedures and information not contained in these Supplement pages,refer to Original Boeing Manual.

Table 1, List of Effective Airplanes for Special Freighter

PREFACE Chapter 0Model Identification Section 1

Special Freighter:

IAI No.

Model Type

Customer Effectivity

Code

Boeing LineNo.

Variable No.

Serial No.

RegistryNo.

RB127 B737-34S GIA 325 2983 PR091 29108 TF-TNM

RB126 B737-34S GIA 326 3001 PR092 29109 OO-TNL

APR 28/2011

Preface


QRH - 365-00-00-B99333-TN3


QRH-366-00-00-99333-TN3

CHAPTER NC

NORMAL CHECKLISTS


QRH-366-00-00-99333-TN3

Normal Checklists

PREFLIGHT

Oxygen . . . . . . . . . . . . . . . . . . . . . . . . . . . Tested, 100%

Instrument transfer switches . . . . . . . . . . . . . . .NORMAL

Window heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON

Pressurization mode selector . . . . . . . . . . . . . . . . AUTO

Flight instruments . . . . . . . . . . . Heading__, Altimeter__

Parking brake. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

Engine start levers . . . . . . . . . . . . . . . . . . . . . . . CUTOFF

MANUAL HYD PUMP HANDLE . . . . . . . . . . . STOWED

SUPERNUMERARY PASSENGERS . . . . . . . BRIEFED

The flight crew should brief supernumeraries passengerson the emergency procedures, cockpit windows, doorsand escape slide operation.

BEFORE STARTFlight deck door . . . . . . . . . . . . . . . . . Closed and lockedFuel . . . . . . . . . . . . . . . . . . . . . . . . . .__KGS, Pumps ON

Supernumerary signs. . . . . . . . . . . . . . . . . . . . . . . . . . __Windows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LockedMCP. . . . . . . . . . . . . . V2__, HEADING__, ALTITUDE__Takeoff speeds. . . . . . . . . . . . . . . . . . V1__, VR__, V2__CDU preflight . . . . . . . . . . . . . . . . . . . . . . . . . .CompletedRudder and aileron trim . . . . . . . . . . . . . . . . . .Free and 0Taxi and takeoff briefing. . . . . . . . . . . . . . . . . .CompletedAnti collision light . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON

Normal Checklists Chapter NC

Special Freighter:

Special Freighter:

QRH-366-00-00-99333-TN3NNC.0.70.1AUG 15/2010

Normal Checklists

BEFORE TAXI

Generators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On

Pitot heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Anti-ice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . __

Isolation valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

Engine start switches . . . . . . . . . . . . . . . . . . . . . . .CONT

Recall . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Checked

Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RTO

Engine start levers . . . . . . . . . . . . . . . . . . . . IDLE detent

Flight controls . . . . . . . . . . . . . . . . . . . . . . . . . . .Checked

Ground equipment . . . . . . . . . . . . . . . . . . . . . . . . . .Clear

BEFORE TAKEOFF

Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . __, Green light

Stabilizer trim . . . . . . . . . . . . . . . . . . . . . . . . . . . __ Units

AFTER TAKEOFF

Engine bleeds. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Packs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO

Landing gear. . . . . . . . . . . . . . . . . . . . . . . . .UP and OFF

Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .UP, No lights

QRH-366-00-00-99333-TN3NNC.0.70.2 AUG 15/2010

Normal Checklists

DESCENT

Pressurization . . . . . . . . . . . . . . . . . . . . . . . LANT ALT__

Recall. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked

Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . __

Landing data . . . . . . . . . . . . . . . VREF __, Minimums __

Approach briefing. . . . . . . . . . . . . . . . . . . . . . .Completed

APPROACH

Altimeters. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . __

LANDING

Engine start switches. . . . . . . . . . . . . . . . . . . . . . . CONT

Speedbrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ARMED

Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Down

Secondary lights . . . . . . . . . . . . . . . . . . . . . . . 2 Green

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . __, Green light

SHUTDOWN

Fuel pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

Pitot heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

Hydraulic panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

ELECTRIC HYDRAULIC PUMP SYS "A" . . . . . . . .ONOR AS REQUIRED

ELECTRIC HYDRAULIC PUMP SYS "B" . . . . . . .OFF

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .UP

Parking brake. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . __

Continued on next page

Special Freighter:

QRH-366-00-00-99333-TN3NNC.0.70.3AUG 15/2010

Normal Checklists

Continued from previous page

Engine start levers . . . . . . . . . . . . . . . . . . . . . . .CUTOFF

Weather radar. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off

SECURE

IRSs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Emergency exit lights . . . . . . . . . . . . . . . . . . . . . . . . OFF

Window heat. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Packs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

QRH-366-00-00-99333-TN3NNC.0.70.4 AUG 15/2010


QRH-366-00-00-99333-TN3

CHAPTER NNC

SECTION 0

MISCELLANEOUS


QRH-366-00-00-99333-TN3

Non-normal ChecklistsMiscellaneous

1. Announce the emergency descent. The pilot flying will advise the supernumerary personnel on the PA system, of impending rapid descent. The first officer will advise ATC and obtain the area altimeter setting.

2. Supernumerary personnel signs . . . . . . . . . . . . . .ON

3. Without delay, descend to the lowest safe altitude or 10,000 feet, whichever is higher.

4. ENGINE START switches (both). . . . . . . . . . . CONT

5. Thrust levers (both). . . . . . . . . . . . . Reduce thrust tominimum or as

needed for anti-ice

6. Speedbrake. . . . . . . . . . . . . . . . . . FLIGHT DETENT

7. Set target speed to Mmo/Vmo.

Emergency Descent

Condition: One or more of these occur:

• Cabin pressure cannot be controlled when the airplane is above 14,000 feet

• A rapid descent is needed.

Special Freighter:

Special Freighter:

If structural integrity is in doubt, limit speed asmuch as possible and avoid high maneuveringloads.


QRH-366-00-00-99333-TN3NNC.0.70.1AUG 15/2010


8. When approaching the level off altitude:

Smoothly lower the SPEED BRAKE lever to the DOWN detent and level off. Add thrust and stabilize on altitude and airspeed.

9. Crew oxygen regulators. . . . . . . . . . . . . . . . . Normal

Flight crew must use oxygen when cabin altitude is above 10,000 feet. To conserve oxygen, move the regulator to Normal.

10. ENGINE START switches (both) . . . . . . . As needed

11. The new course of action is based on weather, oxygen, fuel remaining and available airports. Use of long range cruise may be needed.

1. Send distress signals. Determine position, course, speed, altitude, situation, intention, time and position of intended touchdown and transmit "Mayday". Report type of aircraft and request intercept.

2. Alert the supernumerary personnel to prepare for ditching.

Emergency Descent continued

Ditching < >

Condition: Airplane ditching and evacuation areneeded.

Special Freighter:


QRH-366-00-00-99333-TN3NNC.0.70.2 AUG 15/2010


3. Burn off fuel to reduce touchdown speed and increase buoyancy.

4. Plan to touch down on the windward side and parallel to waves and swells.

5. Plan a flaps 40 landing unless another configuration is needed.

6. Set VREF 40.

7. Do not arm the autobrake.

8. Do not accomplish the normal landing checklist.

9. Checklist Complete Except for Deferred Items.

Descent Checklist

Pressurization . . . . . . . . . . . . . . . . . . . LAND ALT ___

Recall. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked

Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

Landing data . . . . . . . . . . . . . . . . . . . . . . . . . VREF 40

Approach briefing . . . . . . . . . . . . . . . . . . . .Completed

Approach Checklist

Altimeters. . . . . . . . . . . . . .___hpa, ALT crosschecked

Below 5,000 feet

LANDING GEAR AURAL WARNcircuit breaker (P6) . . . . . . . . . . . . . . . . . . . . . . . . Pull

Ditching < > continued

Deferred Items


QRH-366-00-00-99333-TN3NNC.0.70.3AUG 15/2010


This prevents the warning horn with gear retracted and landing flaps selected.

Supernumerary personnel signs . . . . . . . . . . . . . . ON

Engine BLEED air switches (both) . . . . . . . . . . . . OFF

This allows the airplane to be depressurized with the outflow valve closed.

Pressurization mode selector . . . . . . . . . . . . . . . . MAN

Outflow VALVE switch . . . . . . . . . . . . . Hold in CLOSE

until outflow valveindicates fully closed

This prevents water from entering the airplane.

APU switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

GROUND PROXIMITY GEARINHIBIT switch . . . . . . . . . . . . . . . . . . . GEAR INHIBIT

GROUND PROXIMITY TERRINHIBIT switch (as installed) . . . . . . . . TERR INHIBIT

Life vests, shoulder harnesses and seat belts . . . . .On

Confirm that supernumerary personnel preparations are complete.

Transmit all pertinent information regarding final ditching position.


Special Freighter:

Note: The outflow valve takes up to 20 seconds to close.

Special Freighter:


QRH-366-00-00-99333-TN3NNC.0.70.4 AUG 15/2010


After Impact Procedure Review

Set both engine start levers to CUTOFF. This closes fuel shutoff valves to prevent discharge of fuel from ruptured fuel lines.

Start the evacuation.

Proceed to assigned ditching stations, launch rafts and evacuate the airplane as soon as practicable.

The airplane may stay afloat indefinitely if fuel load is minimal and no serious damage was sustained during landing.

Ditching Final

LANDING GEAR lever. . . . . . . . . . . . . . . UP and OFF

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . .___Green light

At 500 feet, advise the cabin crew that ditching is imminent.

At 50 feet, advise the cabin crew to brace for impact.

Maintain airspeed at VREF. Flare the airplane to achieve the minimum rate of descent at touchdown. Maintain 200-300 fpm rate of descent until the start of the flare.

At flare, rotate smoothly to a touchdown attitude of 10-12°. Maintain airspeed and rate of descent with thrust.

At touchdown, reduce thrust to idle.


Not Applicable for Special Freighter:


QRH-366-00-00-99333-TN3NNC.0.70.5AUG 15/2010


QRH-366-00-00-99333-TN3


QRH-366-00-00-99333-TN3

SECTION 1

AIRPLANE GENERAL, EMERGENCY EQUIPMENT,

DOORS, WINDOWS


QRH-366-00-00-99333-TN3

Non-normal ChecklistsAirplane Gen. Emer.

Equip., Doors, Windows

1. Choose one:

♦Pressurization is normal:

Continue normal operation.

♦Pressurization is not normal.

Go to step 2

2. Don oxygen masks.

3. Establish crew communications.

4. Supernumerary personnel signs . . . . . . . . . . . . . .ON

5. Choose one:

♦Airplane has not reached the planned cruise altitude:

Do not continue the climb.

Reset the FLT ALT indicator to the actual airplane altitude

Go to step 6

♦Airplane has reached the planned cruise altitude:

Go to step 6

CARGO DOOR

FWDCARGO

AFTCARGO

Condition: One or more cargo doors are not closed andsecure.

Special Freighter:


QRH-366-00-00-99333-TN3NNC.1.70.1AUG 15/2010

Non-normal ChecklistsAirplane Gen. Emer.Equip., Doors, Windows

6. LAND ALT indicator . . . . . . . . . . . . . . . . . . 9,000 feet

7. Choose one:

♦Minimum safe altitude is at or below 9,000 feet:

Go to step 8

♦Minimum safe altitude is between 9,000 feet and 13,000 feet:

Go to step 10

♦Minimum safe altitude is at or above 13,000 feet:

Go to step 12

8. Descend to 9,000 feet.

9. Maintain a cabin differential pressure of 0 psi by limiting flight altitude to 9,000 feet.

Go to step 15

10. Descend to the minimum safe altitude.

11. LAND ALT indicator . . . . . . . .Select a higher altitude(maximum 13,000 feet) to

maintain a cabin differentialpressure of 0 psi

Go to step 15

12. Descend to the minimum safe altitude.

CARGO DOOR continued

Note: The intermittent cabin altitude/configurationwarning horn will sound and the CABINALTITUDE light (as installed) will illuminateat a cabin altitude of approximately 10,000feet.


QRH-366-00-00-99333-TN3NNC.1.70.2 AUG 15/2010



13. Pressurization mode selector . . . . . . . . . . . . . . MAN

14. Outflow VALVE switch. . . . . . . . . . Adjust to maintaina cabin differential

pressure of 0 psi

15. Plan to land at the nearest suitable airport.

16. When the cabin altitude is at or below 10,000 feet:

Oxygen masks may be removed.

CARGO DOOR continued

Note: The intermittent cabin altitude/configurationwarning horn will sound and the CABINALTITUDE light (as installed) will illuminateat a cabin altitude of approximately 10,000feet.

QRH-366-00-00-99333-TN3NNC.1.70.3AUG 15/2010


1. Choose one:




Plan to land at the nearest suitable airport.

ENTRY DOOR

FWDENTRY

Condition: The entry door light illuminated indicates theentry door is not properly closed, securedand latched.

QRH-366-00-00-99333-TN3NNC.1.70.4 FEB 10/2011



1. Choose one:




Plan to land at the nearest suitable airport.

SERVICE DOOR

FWDSERVICE

Condition: The service door lights illuminated indicatesthe service door is not properly closed,secured and latched.

QRH-366-00-00-99333-TN3NNC.1.70.5FEB 10/2011


MAIN CARGO DOOR

Note: MAIN DECK CARGO DOOR lights arelocated on Captain and First Officer’sinstrument panel.

1. Choose one:

♦If MAIN CARGO door light is illuminated andcabin pressurization is normal:

Continue normal operation

♦If MAIN CARGO door light is illuminated andcabin pressureziation is not normal.

Oxygen masks . . . . . . . . . . . . . . . . . . . . . .On

Crew communications . . . . . . . . . . .Establish

FASTEN BELTS switch . . . . . . . . . . . . . . .On

Descend normally to 9,000 feet or to the minimum safe altitude, whichever is higher.

Pressurization mode selector. . . . . . . . STBY

CAB ALT indicator . . . . . . . . . . . . . 9,000 feet

CABIN RATE selector . . . . . . . . . As desired

MAIN CARGO DOOR

MAIN CARGO DOOR

Special Freighter:

Condition: The main cargo light illuminated indicatesthe main cargo door is not properly closed,secured and latched.


QRH-366-00-00-99333-TN3NNC.1.70.6 FEB 10/2011



If MAIN CARGO door light is illuminated andcabin pressurization is normal: (continued)

If the minimum safe altitude is between 9,000 feet and 13,000 feet.

CAB ALT indicator. . . . . . . . . . . . . . . . . . ___feet

Select a higher altitude (maximum 13,000 feet) to maintain a cabin differential pressure of 0 psi.

Note: The intermittent cabinaltitude/configuration warning hornwill sound and the CABINALTITUDE light (as installed) willilluminate at a cabin altitude ofapproximately 10,000 feet.

If the minimum safe altitude is at or above 13,000 feet.

Pressurization mode selector . . . . . . . . MAN DC

Adjust the outflow valve to maintain a cabin differential pressure of 0 psi.

Note: The intermittent cabinaltitude/configuration warning hornwill sound and the CABINALTITUDE light (as installed) willilluminate at a cabin altitude ofapproximately 10,000 feet.

Pressurization oxygen (as needed) . . . . . . . .ON

Activate passenger oxygen at cabin altitudes in excess of 10,000 feet.

MAIN CARGO DOOR continued


QRH-366-00-00-99333-TN3NNC.1.70.7FEB 10/2011


If MAIN CARGO door light is illuminated andcabin pressurization is normal: (continued)

Oxygen masks may be removed if the cabin altitude is below 10,000 feet.

Plan to land at nearest suitable airport.

MAIN CARGO DOOR continued

QRH-366-00-00-99333-TN3NNC.1.70.8 FEB 10/2011


QRH-366-00-00-99333-TN3

SECTION 2

AIR SYSTEMS


QRH-366-00-00-99333-TN3

Non-normal ChecklistsAir Systems

1. Temperatureselector (affected side) . . . . . . . . . . . . Select warmer

temperature

This reduces the workload on the affected air conditioning pack.

2. TRIP RESET switch. . . . . . . . . . . . . . . . . . . . . . Push

The PACK TRIP OFF light extinguishes if the pack temperature has cooled below limits.

3. Choose one:

♦Both PACK TRIP OFF lights are extinguished:


♦A single PACK TRIP OFF light stays illuminated:


♦Both PACK TRIP OFF lights stay illuminated:

Go to step 4

4. Descend to the lowest safe altitude, or 10,000 feet, whichever is higher. Monitor cabin altitude and rate.

PACKTRIP OFF

PACK TRIP OFF

Condition: A pack overheat occurs.

Note: Both pack valves may have closed resultingin a gradual loss of cabin pressure andeventual CABIN ALTITUDE warning.


QRH-366-00-00-99333-TN3NNC.2.70.1AUG 15/2010


5. When at level off:

Maintain 290 knots minimum. Flight deck and cabin temperatures may increase rapidly at speeds below 290 knots.

6. Choose one:

♦Airplane altitude is at or below 10,000 feet:

Go to step 7

♦Airplane altitude is above 10,000 feet:

Oxygen masks . . . . . . . . . . . . . . . . . . . . ON

Crew communication . . . . . . . . . . .Establish

Passenger oxygen (as installed). . . . . . . ON

Activate passenger oxygen at cabin altitudes in excess of 10,000 feet.

Go to step 7

7. Pressurization mode selector . . . . . . . . . . . . . . MAN

8. Outflow VALVE switch . . . . . . . . . Hold in OPEN untiloutflow VALVE position

indicates fully open

This increases airplane ventilation.

9. If flight deck and cabin temperatures are excessively warm:

Open the flight deck door. This improves flight deck ventilation.

PACK TRIP OFF continued


QRH-366-00-00-99333-TN3NNC.2.70.2 AUG 15/2010


Use flight deck window shades, as needed.

Instruct the cabin crew to:

Dim cabin lighting

Turn off in-flight entertainment systems.

Close cabin window shades.

GALLEY switch . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

PACK TRIP OFF continued



QRH-366-00-00-99333-TN3NNC.2.70.3AUG 15/2010


QRH-366-00-00-99333-TN3


QRH-366-00-00-99333-TN3

SECTION 8

FIRE PROTECTION


QRH-366-00-00-99333-TN3

Non-normal ChecklistsFire Protection

1. Diversion may be needed.

2. Don oxygen masks and set regulators to 100%, as needed.

3. Don smoke goggles, as needed.

4. If smoke or fumes affect vision:

Use the EMERGENCY position on the oxygen regulator to clear the goggles.

5. Establish crew and supernumerary personnel communications.

6. If smoke, fire or fumes source is confirmed to be from main deck cargo compartment, accomplish the MAIN DECK CARGO SMOKE, FIRE or FUMES checklist.

7. BUS TRANSER switch . . . . . . . . . . . . . . . . . . . .OFF

8. GALLEY switch . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

9. RECIRC FAN switches (both) . . . . . . . . . . . . . . .OFF

Smoke, Fire or Fumes

Condition: Smoke, fire or fumes is identified.

Special Freighter:

Special Freighter:




QRH-366-00-00-99333-TN3NNC.8.70.1APR 28/2011


10. Instruct flight attendants to turn off the IFE and PC power switches (as installed).

11. APU BLEED air switch. . . . . . . . . . . . . . . . . . . . OFF

12. Anytime the smoke or fumes become the greatest threat:

Go to the Smoke or Fumes Removal checklist on page 8.14

13. Choose one:

♦Source of the smoke, fire or fumes is obvious and can be extinguished quickly:

Isolate and extinguish the source.

If possible, remove power from the affected equipment by switch or circuit breaker in the flight deck or cabin.

Go to step 14

♦Source of the smoke, fire or fumes is not obvious or cannot be extinguished quickly:

Go to step 15

Smoke, Fire or Fumes continued



QRH-366-00-00-99333-TN3NNC.8.70.2 APR 28/2011


14. Choose one:

♦Source is visually confirmed to be extinguished and the smoke or fumes are decreasing:

Continue the flight at the Captain’s discretion.

Restore unpowered items at the Captain’s discretion.

Go to the Smoke or Fumes Removal checklist on page 8.14, if needed.

♦Source is not visually confirmed to be extinguished or smoke or fumes are not decreasing:

Go to step 15

15. EQUIP COOLING SUPPLYand EXHAUST switches (both) . . . . . . ALTERNATE

16. Instruct the cabin crew to:

Turn on cabin reading lights.

Turn on galley attendants work lights.

Turn off cabin fluorescent light switches.

17. Divert to the nearest suitable airport while continuing the checklist.

18. Consider an immediate landing if the smoke, fire or fumes situation becomes uncontrollable.

19. Do not delay landing in an attempt to complete all of the following steps.




QRH-366-00-00-99333-TN3NNC.8.70.3APR 28/2011


20. ISOLATION VALVE switch. . . . . . . . . . . . . . . CLOSE

21. R PACK switch. . . . . . . . . . . . . . . . . . . . . . . . . . OFF

22. Wait 2 minutes unless the smoke or fumes are increasing. This allows time for the smoke or fumes to clear.

23. Choose one:

♦Smoke or fumes are decreasing:


♦Smoke or fumes continue or are increasing:

R PACK switch . . . . . . . . . . . . . . . . . . . AUTO

L PACK switch . . . . . . . . . . . . . . . . . . . . OFF

Go to step 24

24. Wait 2 minutes unless the smoke or fumes are increasing. This allows time for the smoke or fumes to clear.

25. Choose one:

♦Smoke or fumes are decreasing:


♦Smoke or fumes continue or are increasing:

L PACK switch . . . . . . . . . . . . . . . . . . . AUTO



QRH-366-00-00-99333-TN3NNC.8.70.4 APR 28/2011


Consider an immediate landing.



QRH-366-00-00-99333-TN3NNC.8.70.5APR 28/2011


1. OXYGEN MASKS AND SMOKE GOGGLES(if required) . . . . . . . . . . . . . . . . . . . . . . . .ON, 100%

2. CREW COMMUNICATION(if required) . . . . . . . . . . . . . . . . . . . . . . ESTABLISH

3. COCKPIT DOOR. . . . . . . . . . . . . . . . . . . . . . CLOSE

[Prevents smoke/fumes contamination of/from other compartments.]

4. DEPRESS Switch . . . . PULL GUARD AND PRESS

[Depress light will come on after 7 seconds.]

[Depressurize the airplane and provides restricted heat and ventilation for exclusion of fumes and smoke from the cockpit.]

5. COCKPIT GASPER OUTLETS . . . . . . . . . . . . OPEN

Caution! Do not open any flight deck window.

6. LAND AT NEAREST SUITABLE AIRPORT

7. If immediate landing cannot be made:

AIRPLANE ALTITUDE. . . . 20,000-25,000 FEET

SMOKEMAIN DECK CARGO -

SMOKE, FIRE OR FUMES

Special Freighter

Condition: Smoke, fire or fumes from the main deckcargo, as indicated by the main deck smokedetector system.


QRH-366-00-00-99333-TN3NNC.8.70.6 APR 28/2011


Engine No. 1 and No. 2BLEED AIR Switch . . . . . . . . . . . . . .VERIFY ON

ENGINE THRUST. . MAXIMUM PRACTICAL N1(minimum 45%)

[Provides maximum cabin ventilation.]

Weather Radar Mode Selector(before cabin altitude reach 15,000 feet) . . . . . . . . . . . . . . . . .OFF

Main Deck Smoke/Fumes continued

Note: Do not pressurize airplane, unless fire is outand no structural damage occurred.

QRH-366-00-00-99333-TN3NNC.8.70.7APR 28/2011


1. Main Deck Smoke Detection System . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Test Button. . . . . . . . . . . . . . . PRESS and HOLDuntil aural warning sounds

and the test sequence is complete,then release

2. If On Ground:

Return to gate and contact maintenance personnel.

3. If Inflight:

Continue flight at Captain’s discretion and write up in logbook.

MAIN Main Deck Cargo Smoke Detection System FaultDECK

Special Freighter

Condition: Illumination of the DET FAULT (amber) lightindicates one or more smoke detectors inthe main deck failed.

QRH-366-00-00-99333-TN3NNC.8.70.8 APR 28/2011


Land at the nearest suitable airport.

MAIN SMOKE NO FLOW MAIN SMOKE NO FLOW

Special Freighter

Condition: THE MAIN SMOKE NO FLOW lightilluminated indicates a loss of the smokedetectors ability to identify smoke in themain deck.

Note: The rest of the main cabin smoke detectionsystem remains operative.

QRH-366-00-00-99333-TN3NNC.8.70.9APR 28/2011


QRH-366-00-00-99333-TN3


QRH-366-00-00-99333-TN3

SECTION 13

HYDRAULICS


QRH-366-00-00-99333-TN3

Non-normal ChecklistsHydraulics

1. HYD PUMP switch (affected side) . . . . . . . . . . .OFF

1. ELEC HYD PUMP switch (affected side) . . . . . .OFF

LOWPRESSURE

HYDRAULIC PUMP LOW PRESSURE

Condition: The hydraulic pump pressure is low.

Note: Loss of an engine-driven hydraulic pumpand a high demand on the system mayresult in an intermittent illumination of theLOW PRESSURE light for the remainingelectric motor-driven hydraulic pump.

Special Freighter:

Note: If electrical pump A is switched off, the maincargo door should be operated manually.

OVERHEAT HYDRAULIC PUMP OVERHEAT

Condition: The hydraulic pump temperature is high.

Note: One pump supplies sufficient pressure fornormal system operation.

Special Freighter:

Note: If electrical pump A is switched off, the maincargo door should be operated manually.

QRH-366-00-00-99333-TN3NNC.13.70.1 AUG 15/2010


1. System AFLT CONTROL switch . . . Confirm . . . . STBY RUD

2. System AHYD PUMP switches (both) . . . . . . . . . . . . . . . OFF

Inoperative Items

LOSS OF SYSTEM A < >

FLT CONTROL A HYD PUMPS

A ENG 1 ELEC 2

LOW PRESSURE

LOW PRESSURE

LOW PRESSURE

Condition: Hydraulic system A pressure is low.

Special Freighter:

Note: If electrical hydraulic pump A is switchedoff, the main cargo door should be operatedmanually.

Autopilot A inopAutopilot B is available

Inboard flight spoilers inopRoll rate and speedbrake effectiveness may be reduced in flight.

Main landing gear normal hydraulic system inopManual gear extension is needed.

Ground spoilers inopLanding distance will be increased.


QRH-366-00-00-99333-TN3NNC.13.70.2 AUG 15/2010


Inoperative Items

3. Check the Non-Normal Configuration Landing Distance table in the Advisory Information section of the Performance Inflight chapter.

4. NOSE WHEEL STEERING switch . . . . . . . . . . . ALT

5. Plan for manual gear extension.

6. Checklist Complete Except Deferred Items

LOSS OF SYSTEM A < > continued

Special Freighter:

Main deck cargo door inopManual operation is needed

Alternate brakes inopNormal brakes are available

Engine 1 thrust reverser normal hydraulic pressure inop

Thrust reverser will deploy and retract at a slower rate and some thrust asymmetry can be anticipated during thrust reverser deployment.

Normal nose wheel steering inopAlternate nose wheel steering is available.

Note: When the gear has been lowered manually,it cannot be retracted. The drag penaltywith gear extended may make it impossibleto reach an alternate field.


QRH-366-00-00-99333-TN3NNC.13.70.3 AUG 15/2010


Descent Checklist


Autobrake. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___

Landing data. . . . . . . . . . . . VREF____, Minimums___

Approach briefing . . . . . . . . . . . . . . . . . . . . Completed

Supernumerary Personnel signs . . . . . . . . . . . . . . .On

Approach Checklist

Altimeters . . . . . . . . . . . . . ___hpa, ALT crosschecked

Supernumerary Personnel signs . . . . . . . . . . . . . . .On

Manual Gear Extension

LANDING GEAR lever . . . . . . . . . . . . . . . . . . . . . OFF

Manual gear extension handles . . . . . . . . . . . . . . . Pull

The uplock is released when the handle is pulled to its limit.

The related red landing gear indicator light illuminates, indicating uplock release.

Wait 15 seconds after the last manual gear extension handle is pulled:

LANDING GEAR lever . . . . . . . . . . . . . . . . . . . . DN


Deferred Items

Special Freighter:

Special Freighter:


QRH-366-00-00-99333-TN3NNC.13.70.4 AUG 15/2010


Landing Checklist

Recall. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked

ENGINE START switches . . . . . . . . . . . . . . . . . CONT

Speedbrake . . . . . . . . . . . . . . . . . . . . . . . . . . . ARMED

Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . .Down

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . .___, Green light


QRH-366-00-00-99333-TN3NNC.13.70.5 AUG 15/2010


1. System A and B FLT CONTROLswitches (both) . . . . . . . . . Confirm . . . . STBY RUD

2. System A and BHYD PUMPS switches (all) . . . . . . . . . . . . . . . . OFF

MANUAL REVERSION < >or

LOSS OF SYSTEM A AND SYSTEM B < >

FLT CONTROL HYD PUMPS

A B ENG 1 ELEC 2 ELEC 1 ENG 2

LOW PRESSURE

LOW PRESSURE

LOWPRESSURE

LOW PRESSURE

Condition: Hydraulic system A and B pressures arelow.

Special Freighter:

Note: If electrical hydraulic pump A is switchedoff, the main cargo door should be operatedmanually.


QRH-366-00-00-99333-TN3NNC.13.70.6 AUG 15/2010


Inoperative Items


LOSS OF SYSTEM A AND SYSTEM B < > continued

Autopilots A and B inopAll flight spoilers inop

Roll rate will be reduced and speedbrakes will not be available in flight.

Yaw damper inopTrailing edge flaps normal hydraulic system inop

The trailing edge flaps can be operated with the alternate electrical system. Alternate flap extension time to flaps 15 is approximately 2 minutes.

Leading edge flaps and slats normal hydraulic system inop

The leading edge flaps and slats can be extended with standby hydraulic pressure. Once extended, they can be retracted.

Normal landing gear extension and retraction inopManual gear extension is needed.

Autobrake inopGround spoilers inop

Landing distance will be increased.Normal and alternate brakes inop

Inboard and outboard brakes have accumulator pressure only. On landing, apply steady brake pressure without modulating the brakes.

Both thrust reversers normal pressure inopThrust reversers will deploy and retract at a slower rate.

Nose wheel steering inopDo not attempt to taxi the airplane after stopping.


QRH-366-00-00-99333-TN3NNC.13.70.7 AUG 15/2010


3. Plan to land at the nearest suitable airport.

4. Plan for flaps 15 landing.

5. Set VREF 15.

6. Plan to extend flaps to 15 using alternate flap extension.

7. Plan for manual gear extension.

8. Check the Non-Normal Configuration Landing Distance table in the Advisory Information section of the Performance Inflight chapter.

9. Do not arm the autobrake for landing.

10. Do not arm the speedbrakes for landing.

11. On touchdown, apply steady brake pressure without modulating the brakes.



Note: The drag penalty with the leading edgedevices extended may make it impossibleto reach an alternate field.

Note: When the gear has been lowered manually,it cannot be retracted. The drag penaltywith gear extended may make it impossibleto reach an alternate field.

Note: The crosswind capability of the airplane isgreatly reduced.


QRH-366-00-00-99333-TN3NNC.13.70.8 AUG 15/2010


12. Do not attempt to taxi the airplane after stopping.

13. Checklist Complete Except Deferred Items.

Descent Checklist


Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

Landing data . . . . . . . . . . . . VREF 15, Minimums___


Supernumerary Personnel signs . . . . . . . . . . . . . . . On

Go-Around Procedure Review

Do the normal go-around procedure except:

Advance thrust to go-around smoothly and slowly to avoid excessive pitch-up.

Be prepared to trim.

Limit bank angle to 15° when airspeed is less than 150 knots (or the speed tape minimum maneuver speed).

Approach Checklist




Deferred Items

Special Freighter:


QRH-366-00-00-99333-TN3NNC.13.70.9 AUG 15/2010


Alternate Flap Extension

During flap extension, set the flap lever to the desired flap position.

ALTERNATE FLAPS master switch . . . . . ARM

ALTERNATE FLAPSposition switch . . . . . . . . . . . . . . . Hold DOWN

to extend flapsto 15 on schedule

As flaps are extending, slow to respective maneuvering speed.



230K maximum during alternate flap extension.

Note: The landing gear configuration warningmay sound if the flaps are between 10 and15 and the landing gear are down andlocked.

Note: The amber LE FLAPS TRANSIT light willstay illuminated until the flaps approach theflaps 10 position.

Note: Operation within the lower yellow airspeedband may be needed until the LE FLAPSTRANSIT light extinguishes.

If flap asymmetry occurs, release the switchimmediately. There is no asymmetry protection.


QRH-366-00-00-99333-TN3NNC.13.70.10 AUG 15/2010


Manual Gear Extension

LANDING GEAR lever. . . . . . . . . . . . . . . . . . . . . .OFF

Manual gear extension handles. . . . . . . . . . . . . . . Pull

The uplock is released when the handle is pulled to its limit.

The related red landing gear indicator light illuminates, indicating uplock release.

Wait 15 seconds after the last manual gear extension handle is pulled:

LANDING GEAR lever . . . . . . . . . . . . . . . . . . . . DN

Additional Deferred Item

GROUND PROXIMITY FLAPINHIBIT switch. . . . . . . . . . . . . . . . . . . . FLAP INHIBIT

Landing Checklist

Recall. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked


Speedbrake . . . . . . . . . . . . . . . . . . . . . .DOWN detent


Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . 15, Green light



QRH-366-00-00-99333-TN3NNC.13.70.11 AUG 15/2010


QRH-366-00-00-99333-TN3


QRH-366-00-00-99333-TN3

SECTION 14

LANDING GEAR


QRH-366-00-00-99333-TN3

Non-normal ChecklistsLanding Gear

1. LANDING GEAR lever . . . . . . . . . . OFF (if possible)

2. Manual gearextension handles (affected gear) . . . . . . . . . Pull

The uplock is released when the handle is pulled to its limit. The related red landing gear indicator light illuminates, indicating uplock released.

3. Wait 15 seconds after the last manual gear extension handle is pulled:

LANDING GEAR lever . . . . . . . . DN (if possible)

MANUAL GEAR EXTENSION < >

Condition: One of these occurs:

• Any landing gear is not down and locked when the LANDING GEAR lever is down

• The LANDING GEAR lever is jammed in the OFF position.

Special Freighter:

Note: If a green landing gear indicator light is notilluminated on the center main panel, maingear secondary downlock indication light isgreen, the related landing gear is down andlocked.

270K/.82M maximum.


QRH-366-00-00-99333-TN3NNC.14.70.1AUG 15/2010


4. Check landing gear indicator lights.

5. Choose one:

♦All landing gear indicate down and locked:

Go to step 7

♦No landing gear indicates down and locked:

Go to step 8

♦Only one or two landing gear indicate down and locked:

WHEEL WELL light switch . . . . . . . . . . . . ON

Check gear down lock visual indicator(s) to verify nose landing gear arrow heads are in contact and verify main gears secondary downlock indication lights are green.

Go to step 6

6. Choose one:


Go to step 7

♦Only one or two landing gear are not down and locked:

Go to the Partial or All Gear Up Landing < > checklist on page NNC.14.70.8

Manual Gear Extension < > continued

Note: If the LANDING GEAR lever is in the OFFposition, the red landing gear indicatorlights will also be illuminated.

Special Freighter:


QRH-366-00-00-99333-TN3NNC.14.70.2 AUG 15/2010


7. Choose one:

♦LANDING GEAR lever is in the DN position:

Land normally

♦LANDING GEAR lever is in the OFF position:

GROUND PROXIMITY GEARINHIBIT switch. . . . . . . . . . . . GEAR INHIBIT

Land normally

8. Check total fuel quantity. Manual gear extension may require up to 10 minutes to complete.

Do not accomplish this checklist unless there is sufficient fuel to extend the gear and then complete an approach, with appropriate reserves.

9. Choose one:

♦Sufficient fuel is available:

Go to step 10

♦Sufficient fuel is not available:



Note: Nose wheel steering is not available.


QRH-366-00-00-99333-TN3NNC.14.70.3AUG 15/2010


10. System A must be depressurized in order to extend the landing gear. The following items will be inoperative.

Inoperative Items

11. System AFLT CONTROL switch . . . Confirm . . . . STBY RUD

12. System AHYD PUMP switches (both) . . . . . . . . . . . . . . . OFF


Autopilot A inopAutopilot B is available

Inboard flight spoilers inopRoll rate and speedbrake effectiveness may be reduced in flight.

Main landing gear normal hydraulic system inopManual gear extension after system A is depressurized is needed.

Ground spoilers inopLanding distance will be increased.

Alternate brakes inopNormal brakes are available.

Engine 1 thrust reverser normal hydraulic pressure inop

Thrust reverser will deploy and retract at a slower rate and some thrust asymmetry can be anticipated during thrust reverser deployment.

Nose wheel steering inop


QRH-366-00-00-99333-TN3NNC.14.70.4 AUG 15/2010


Warning! Do not repressurize hydraulic system A inflight or on the ground because thelanding gear may retract.

13. NOSE WHEELSTEERING switch . . . . . . . . . . . . . . . . Verify NORM

Nose wheel steering is not available.

Warning! Do not use alternate nose wheel steeringbecause the landing gear may retract onthe ground.

14. Cycle the SPEED BRAKE lever until system A pressure is below 500 psi.

15. Manual gearextension handles (all). . . . . . . . . . . . . . . . . . Pull

Do not wait for an indication that a landing gear is down and locked before pulling the next handle.


Note: It may take a number of cycles to reducethe system A pressure to below 500 psi.

270K/.82M maximum.

Note: The uplock is released when the handle ispulled to its limit. The related red landinggear indicator light illuminates, indicatinguplock released.


QRH-366-00-00-99333-TN3NNC.14.70.5AUG 15/2010


16. Cycle the SPEED BRAKE lever until all three green landing gear indicator lights are illuminated.

17. Choose one:


Go to step 18

♦Only one or two landing gear are not down and locked:


18. Plan for flaps 15 landing.

19. Set VREF 15 + 10 knots. This provides tail clearance during landing since the flight spoilers powered by hydraulic system A will be unlocked and may float.


Descent Checklist


Autobrake. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___


Note: It may take a number of cycles and up to 4minutes until all three landing gear indicatorlights are illuminated.

With the LANDING GEAR lever in the OFFposition, the red landing gear indicatorlights will stay illuminated.

Deferred Items


QRH-366-00-00-99333-TN3NNC.14.70.6 AUG 15/2010


Landing data . . . . . . . . . . . . . . . VREF 15 + 10 knots, Minimums___



Approach Checklist


Additional Deferred Items

GROUND PROXIMITY FLAPINHIBIT switch. . . . . . . . . . . . . . . . . . . . FLAP INHIBIT

GROUND PROXIMITYGEAR INHIBIT switch . . . . . . . . . . . . . GEAR INHIBIT

Landing Checklist

Recall. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked


Speedbrake . . . . . . . . . . . . . . . . . . . . . . . . . . . ARMED


Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . 15, Green light

Warning! Do not use alternate nose wheel steeringbecause the landing gear may retract onthe ground.


Special Freighter:

Note: Nose wheel steering is not available.

QRH-366-00-00-99333-TN3NNC.14.70.7AUG 15/2010


1. Choose one:

♦Manual gear extension has been attempted or sufficient fuel is not available to complete manual gear extension.

Go to step 2

♦Manual gear extension has not been attempted:

Go to the Manual Gear Extension < > checklist on page NNC.14.70.1

2. Brief the crew and supernumerary personnel on emergency landing and evacuation procedures.

3. Burn off fuel to reduce touchdown speed.

4. Plan a flaps 40 landing.

5. Set VREF 40.

6. LANDING GEARAURAL WARN circuit breaker (P6) . . . . . . . . . . . Pull

This prevents the landing gear warning horn with gear retracted and landing flaps selected.

PARTIAL OR ALL GEAR UP LANDING < >

Condition: All landing gear are not down and lockedafter attempting manual gear extension.

Special Freighter:


QRH-366-00-00-99333-TN3NNC.14.70.8 AUG 15/2010


7. FLIGHT CONTROL AUTO SPEED BRAKEcircuit breaker (P6) . . . . . . . . . . . . . . . . . . . . . . . Pull

This prevents inadvertent deployment of ground spoilers after landing.

8. Do not arm the autobrake for landing. Use manual braking.

9. Do not arm the speedbrakes for landing.


Descent Checklist


Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF

Landing data . . . . . . . . . . . . VREF 40, Minimums___



Approach Checklist


Partial or All Gear Up Landing < > continued

Deferred Items

Special Freighter:


QRH-366-00-00-99333-TN3NNC.14.70.9AUG 15/2010


Landing Procedure Review

Do not extend the speedbrakes unless stopping distance is critical. When stopping distance is critical, extend the speedbrakes after all landing gear, the nose or the engine nacelle have contacted the runway.

Do not use the thrust reversers unless stopping distance is critical.

Turn all fuel pump switches OFF just before the flare.

After stopping, do the Evacuation checklist, if needed.

Additional Deferred Items

STANDBY POWER switch . . . . . . . . . . . . . . . . . . .BAT

APU switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

GROUND PROXIMITYGEAR INHIBIT switch . . . . . . . . . . . . . GEAR INHIBIT

When on approach:

Engine BLEED air switches . . . . . . . . . . . . . . . OFF

This ensures the airplane is depressurized at touchdown.

Landing Checklist

Recall . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked


Speedbrake . . . . . . . . . . . . . . . . . . . . . DOWN detent

Landing gear . . . . . . . . . . . . . . . . . . . . . . . .___ Down

Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . 40, Green light

Partial or All Gear Up Landing < > continued

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QRH-366-00-00-99333-TN3

SECTION 15

WARNING SYSTEMS


QRH-366-00-00-99333-TN3

Non-normal ChecklistsWarning Systems

1. If the intermittent warning horn sounds and the CABIN ALTITUDE light (as installed) illuminates in flight.

Don the oxygen masks and set the regulators to 100%.

Establish crew communications.

Go to the CABIN ALTITUDE WARNING or Rapid Depressurization checklist on page 2.1

Assure MAIN CARGO DOOR light is extinguished.

WARNING HORN - CABIN ALTITUDE OR CONFIGURATION

TAKEOFFCONFIG

CABINALTITUDE

(As installed)

Condition: One of these occurs:

• In flight, an intermittent horn sounds and the CABIN ALTITUDE light (as installed) illuminates, when the cabin altitude is at or above 10,000 feet.

• On the ground, an intermittent horn sounds and the TAKEOFF CONFIG light (as installed) illuminates, when the takeoff configuration is not correct during takeoff.

• In flight, a steady horn sounds when the landing configuration is not correct.

Special Freighter:


QRH-366-00-00-99333-TN3NNC 15.70.1AUG 15/2010


2. If the intermittent warning horn sounds and the TAKEOFF CONFIG light (as installed) illuminates on the ground:

Assure correct airplane takeoff configuration.

Assure MAIN CARGO DOOR light is extinguished.

3. If the steady warning horn sounds in flight:

Assure correct airplane landing configuration.


Special Freighter:

QRH-366-00-00-99333-TN3NNC 15.70.2 AUG 15/2010


QRH-366-00-00-99333-TN3

EVACUATION


QRH-366-00-00-99333-TN3


1. PARKING BRAKE. . . . . . . . . . . . . . . . . . Set C

2. Speedbrake lever . . . . . . . . . . . . . . . DOWN C

3. FLAP lever . . . . . . . . . . . . . . . . . . . . . . . . 40 F/O

4. STANDBY POWER switch . . . . . . . . . . .BAT F/O

5. Pressurization mode selector . . . . . . . . MAN F/O

6. Outflow VALVE switch. . . Hold in OPEN until F/Othe outflow VALVE

position indicates fullyopen

7. If time allows:

Verify that the flaps are 40 before the engine start levers are moved to CUTOFF. C

8. Engine start levers (both) . . . . . . . .CUTOFF C

9. Advise the supernumerary to evacuate and set the EMERG EVAC BELL to ON position,as installed. C

10. Advise the tower. F/O

11. Engine and APUfire switches (all). . . . . . . . Override and pull F/O

Evacuation

Condition: Evacuation is needed.

Special Freighter:


QRH-366-00-00-99333-TN3Back Cover 70.1AUG 15/2010


12. If an engine or APU fire warning occurs:

Illuminated fire switch . . . Rotate to stop F/Oand hold for

1 second

Evacuation continued

QRH-366-00-00-99333-TN3NNC 15.70.2 AUG 15/2010

REVISION 2: APR 28/2011 TP.70 · QRH-366-00-00-99333-TN3 LEP.70.1 Page Date Page Date ORIGINAL...

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Transcript of REVISION 2: APR 28/2011 TP.70 · QRH-366-00-00-99333-TN3 LEP.70.1 Page Date Page Date ORIGINAL...