Lancaster B mk 1 User manual

AP 101B-7200-15

Lancaster B Mk 1

Aircrew Manual

Amendment Information

This electronic publication represents the latest/current at time

version of the publication and includes:

Issue

1 (October 2011)

AIL

1/16 Power Flight Alarm Core (PFLARM) material included

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AP101B-7200-15

Initial Issue

LANCASTER B Mk 1

(PA 474)

AIRCREW MANUAL

THIS DOCUMENT IS THE PROPERTY OF HER BRITANNIC MAJESTY'S GOVERNMENT, and is issued for the

information of such persons only as need to know its contents in the course of their ofcial duties. Any person nding

this document should hand it in to a British Forces unit or to a police station for its safe return to the MINISTRY OF

DEFENCE, D MOD Sy, LONDON SW1A 2HB, with particulars of how and where found.. THE UNAUTHORISED

RETENTION OR DESTRUCTION OF THE DOCUMENT IS AN OFFENCE UNDER THE OFFICIAL SECRETS

ACTS OF 1911-1989. (When released to persons outside Government Service, this document is issued on a

personal basis and the recipient to whom it is entrusted in condence, within the provisions of the Ofcial Secrets

Acts of 1911-1989, is personally responsible for its safe custody and for seeing that the contents are disclosed

only to authorised persons).

Prepared by Handling Squadron

October 2011

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NOTES TO USERS

1. This Aircrew Manual (AM) is complementary to the Lancaster B Mk 1 (PA 474) Flight

Reference Cards (FRCs) (AP101B-7200-14).

2. After the Preliminary Matter, this AM is divided by marker cards as follows:

Part 1 Description and Management of Systems

Part 2 Limitations

Part 3 Handling

Part 4 Emergency Procedures

Part 5 Operating Data

Part 6 Illustrations

3. Where applicable, each part is divided into chapters as listed on the marker card. Each

page is identied by a Part, Chapter and Page reference at the foot of the page. Thus, a

page bearing the reference 1 - 4 Page 3 is Page 3 of Part 1, Chapter 4.

4. The limitations quoted in Part 2 are mandatory and are not to be exceeded except in

an emergency. Instructions containing the words ‘is to’ or ‘are to’ are also mandatory.

5. This AM and its associated FRCs aim to provide the best operating instructions and

advice currently available. Although they provide guidance for most eventualities, they

are not substitutes for sound judgement and good airmanship; moreover, they assume an

adequate knowledge of the pertinent volumes of AP3456 (series) - Flying. Furthermore,

circumstances might require aircrew to depart from or modify the prescribed procedures

and drills. Consequently, the AM and FRCs should not be regarded as documents which

are to be adhered to inexibly at all times other than as explained in para 4.

6. Amendment Lists (ALs) are issued as necessary and each amendment list instruction

sheet includes a list of modications covered by the amendment. New or amended matter

ofimportanceisindicatedby ........forinsertionsand for deletions. Sheets issued

by amendment bear the AL number at the bottom of the odd-numbered page and any

symbols on either page forming a sheet refer to this amendment list. However, when a new

chapter is issued with an AL, or an existing chapter is completely revised, this is indicated

within the heading of the chapter and the symbols do not appear on the pages.

7. The following conventions are observed throughout this Manual:

a. The actual markings on controls are indicated in the text by capital letters.

b. Unless otherwise stated, all airspeeds/altitudes quoted are indicated values.

c. WARNINGS are ‘That which, if not observed, may result in the loss of the aircraft

and/or death or injury’.

d. CAUTIONS are ‘That which, if not observed, may result in damage to the aircraft

or its equipment’.

e. Notes are ‘That which it is essential to emphasize’. Other information which

requires emphasis is printed in italics.

f. Cross references in the text refer to chapters in the same part, unless otherwise stated.

g. Seats are referred to by their normal occupants thus: ‘Pilot’s’ and ‘Co-Pilot’s’ etc.

8. Modication numbers are only referred to in the text when it is necessary to differentiate

between pre- and post-Mod states. A list of modications mentioned in the text is included in the

preliminary pages with a cross reference to the location in the text of the modication details.

IMPORTANT

Proposals for change to this document are to be sent to the Lancaster User Authenticator

(OC Battle of Britain Memorial Flight, RAF Coningsby, Lincoln LN4 4SY) for onward

transmission to the Nimrod Project Team (BBMF Support) and the Publication Organisation

(Ofcer Commanding, Handling Squadron, Boscombe Down, Salisbury, Wilts SP4 0JE)

using a photocopy of Form 765X.

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AP101B-7200-15

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AIRCREW

PUBLICATIONS

AMENDMENT

REQUEST

References

MAP

-01

Chapter

8.2

Originating

Unit

Title/Address

Reference

Date

Air

Publication

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Publication

Document

No.

Amdt

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Comments

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Other

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Send

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to:

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FaxNo:

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Incorporation Details:

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* Delete as appropriate Instructions for Use

1. MOD Form 765X has been introduced to maintain a full audit trail of changes to aircrew publications and documents to ensure

that both the User Authenticator and Handling Sqn are involved at the earliest opportunity after the form has been raised.

2. MOD Form 765X is to be raised by the individual who observed a deficiency, omission or inaccuracy in the Aircrew Manual,

Flight Reference Cards, Operating Data Manual, Mission Operating Procedure cards, Flight Test Schedule or Aircrew Landaway

Flight Servicing Schedule. Apart from typographic errors, a separate MOD F765X is to be raised for each deficiency, omission or

inaccuracy being reported.

3. When an individual raises a MOD Form 765X (by completing the header detail and Part 1) he is to send the form to the

User Authenticator, (RAF: STANEVAL; Army: A Avn Stds, HQAAC; RN: Naval Flying Standards Flight, RNAS

Culdrose or RNAS Yeovilton as appropriate)

4. On receipt the User Authenticator is to complete Part 2, enter a serial number consisting of a 3-letter MOB designator, a 3-digit

number (starting with 001 from1Jan each year) and 2 digits for the year (eg BZN/016/05), comment as appropriate and pass the

form to the Project Team (PT), with a copy to Handling Sqn and a copy to the appropriate Release to Service Authority (RTSA). An

electronic version of the Form is available on the Defence Intranet and the Form can be submitted electronically by the UA in the first

instance but must be followed up by a signed hard copy.

5. The User Authenticator is to keep a register of all MOD Form 765X arisings.

6. The PT is to complete Part 3 of the MOD Form 765X and forward it to Handling Sqn or the Publication Organisation (copy to

Handling Sqn), as appropriate, for action.

7. When the change proposed in the F765X is deemed by the UA or PT to be of an urgent flight safety or operational nature, the

PT can authorize HS by e-mail to proceed with the appropriate amendment action in advance of the completion and signature of Part

3 of the F765X. When issue of an ANA closes a F765X, the Publication Organisation is to raise a Tech Pubs task to ensure that the

change is incorporated at the next routine amendment.

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Preliminaries

Page 1

AP101B-7200-15

Preliminaries

Lancaster B Mk 1

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Preliminaries

Page 2

Intentionally Blank

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Preliminaries

Page 3

AP101B-7200-15

Preliminaries

LIST OF EFFECTIVE PAGES

This list shows all the pages that should be present at the Initial Issue

of this Manual.

Page Issued By Page Issued By

Preliminary Pages

Title Page Initial Issue

Form 765X Initial Issue

Amendment/AIL/ANA

Record Sheet Initial Issue

Prelim Page 1 Initial Issue

Prelim Page 3 Initial Issue

Prelim Page 5 Initial Issue

Prelim Page 7 Initial Issue

Part 1

Marker Card Initial Issue

Part 1 Chapter 1

1 - 1 Page 1 Initial Issue

1 - 1 Page 3 Initial Issue

1 - 1 Page 5 Initial Issue

Part 1 Chapter 2

1 - 2 Page 1 Initial Issue

1 - 2 Page 3 Initial Issue

1 - 2 Page 5 Initial Issue

1 - 2 Page 7 Initial Issue

1 - 2 Page 9 Initial Issue

Part 1 Chapter 3

1 - 3 Page 1 Initial Issue

1 - 3 Page 3 Initial Issue

Part 1 Chapter 4

1 - 4 Page 1 Initial Issue

1 - 4 Page 3 Initial Issue

1 - 4 Page 5 Initial Issue

Part 1 Chapter 5

1 - 5 Page 1 Initial Issue

Part 1 Chapter 6

1 - 6 Page 1 Initial Issue

1 - 6 Page 3 Initial Issue

1 - 6 Page 5 Initial Issue

Part 1 Chapter 7

1 - 7 Page 1 Initial Issue

1 - 7 Page 3 Initial Issue

1 - 7 Page 5 Initial Issue

1 - 7 Page 7 Initial Issue

1 - 7 Page 9 Initial Issue

Part 1 Chapter 8

1 - 8 Page 1 Initial Issue

1 - 8 Page 3 Initial Issue

1 - 8 Page 5 Initial Issue

Part 2

Marker Card Initial Issue

Part 2

Part 2 Page 1 Initial Issue

Part 2 Page 3 Initial Issue

Part 2 Page 5 Initial Issue

Part 2 Page 7 Initial Issue

Part 2 Page 9 Initial Issue

Part 3

Marker Card Initial Issue

Part 3

Part 3 Page 1 Initial Issue

Part 3 Page 3 Initial Issue

Part 3 Page 5 Initial Issue

Part 3 Page 7 Initial Issue

Part 3 Page 9 Initial Issue

Part 4

Marker Card Initial Issue

Part 4

Part 4 Page 1 Initial Issue

Part 4 Page 3 Initial Issue

Part 4 Page 5 Initial Issue

Part 4 Page 7 Initial Issue

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Part 5

Marker Card Initial Issue

Part 5

Part 5 Page 1 Initial Issue

Part 6

Marker Card Initial Issue

Part 6

Part 6 Page 1 Initial Issue

Part 6 Page 3 Initial Issue

Part 6 Page 5 Initial Issue

Part 6 Page 7 Initial Issue

Part 6 Page 9 Initial Issue

Page Issued By Page Issued By

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Preliminaries

Page 5

AP101B-7200-15

Preliminaries

INTRODUCTION

TheLancasterBMk1isaWorldWarIIheavybomberaircraft,witha‘mid

fuselage’straight wing,‘H’tailand conventionalcontrolsurfaces. Itisan

all-metalconstruction(aluminiumalloys)witharetractableundercarriage

andanenclosedcockpit.Itispowered by 4 Merlinsuper-charged‘Vtype

V12’ piston engines, coupled to Hamilton propellers. It is maintained

in service by the RAF for operation by the Battle of Britain Memorial

Flight (BBMF) as a dedicated commemorative and display aircraft, used

solely for ypasts and displays as tasked by the RAF Ceremonial and

Air Events Team, and for training BBMF display pilots for those duties.

No weapons, ares or external stores are carried.

MODIFICATIONS MENTIONED IN THE TEXT

Mod No Title Location in Text

Pt Chap Para

SM/LANC/016 Carriage of Live Data

Transmission

Equipment

2 39

SM/LANC/017 Poppy Drop 2 38

ASSOCIATED PUBLICATIONS

AP101B-7200-5M Flight Test Schedule

AP101B-7200-14 Flight Reference Cards

AP101B-7200-15S Statement of Operating Intent and Usage

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Preliminaries

Page 6

History

PA474 is one of only two Lancasters remaining in airworthy condition

out of the 7377 that were built. She was built in Chester in mid-1945 and

was earmarked for the ‘Tiger Force’ in the Far East. However, the war

with Japan ended before she could take part in any hostilities. She was

therefore assigned to Photographic Reconnaissance duties with No 82

Squadron in the Far East and South Africa. While operating with No 82

Squadron, PA 474 had her turrets removed.

On return to the UK PA474 was loaned to Flight Refuelling at Tarrant

Rushtontobeusedasapilotlessdrone.However,beforetheconversion

started, theAir Ministry decided to use a Lincoln instead and PA474 was

transferred to the Royal College ofAeronautics where she was used for

trials on the Handley Page Laminar Flow wing.

In 1964 she was adopted by the Air Historical Branch (AHB) for future

display in the proposed RAF Museum at Hendon and was own to

Wroughton where she was painted in a camouage paint scheme. During

this period PA474 also took part in 2 lms, ‘Operation Crossbow’ and

the ‘Guns of Navarone’. Later in 1964 she was moved to RAF Henlow

in preparation for display at the RAF Museum.

The rst unit to be equipped with Lancasters was No 44 Squadron and in

1965 the Commanding Ofcer of this unit sought permission from the AHB

for PA474 to be transferred to the care of the Squadron. An inspection

foundthe aircraftwas structurallysound and permission was granted for

PA474 to make a single ight from Henlow to Waddington.

AtWaddingtonarestorationprogrammeonPA474began,thatwouldtake

several years to complete. By 1966 work was progressing well and both

the front and rear turrets were in place. Permission to y PA474 regularly

was granted in 1967. The aircraft eventually joined the Battle of Britain

Memorial Flight in November 1973. A mid-upper turret was discovered

in Argentina and tted in 1975. During 1995/6 PA474 received a brand

new main spar, extending her life for the foreseeable future.

Aftermajorservicingin2006/7,PA474wearsthemarkingsofEE139,the

‘Phantom of the Ruhr’, a ton-up Lancaster that ew her rst 30 ops with

No 100 Squadron and then 91 ops with No 550 Squadron. She sports

the letters HW-R of ‘The Ton’ on her port side and BQ-B of 550 on her

starboard, effectively commemorating the crews of both Squadrons.

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Preliminaries

Page 7

AP101B-7200-15

Preliminaries

ABBREVIATIONS

AGL Above ground level

AMSL Above mean sea level

ARI Airborne Radio Installation

AUW All up weight

BBMF Battle of Britain Memorial Flight

C of G Centre of Gravity

FRCs Flight Reference Cards

ft feet

gal gallon

GPS Global Positioning System

HIRTA High Intensity Radio Transmission Area

IAS Indicated airspeed

IFF Identication Friend or Foe

IMC Instrument Meteorological Conditions

Mod Modication

NE Never Exceed

NO Normal Operating

OAT Outside air temperature

PF Pilot Flying

PNF Pilot Not Flying

PSI Pounds per square inch

SSR Secondary Surveillance Radio

UHF Ultra High Frequency

VHF Very High Frequency

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Preliminaries

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Leading Particulars

Principal Dimensions

Wing Span 102ft 0in

Length Tail up 69ft 6in

Tail down 68ft 10in

Height Tail up 23ft 9in

Tail down 20ft 6in

Track 23ft 9in

Tailplane span 33ft 0in

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AP101B-7200-15

PART 1

DESCRIPTION AND MANAGEMENT

OF SYSTEMS

List of Chapters

Chapter

ELECTRICAL SYSTEM ... ... ... 1

FUEL SYSTEM ... ... ... ... 2

ENGINE SYSTEMS AND CONTROLS ... 3

HYDRAULIC SYSTEM ... ... ... 4

PNEUMATIC SYSTEM ... ... ... 5

AIRFRAME AND CONTROLS ... ... 6

RADIO AND INSTRUMENTS ... ... 7

FIRE PROTECTION SYSTEM

AND EMERGENCY EQUIPMENT... ... 8

PART 1

DESCRIPTION AND

MANAGEMENT

Lanc_Divider_Cards.indd 1 06/10/2011 10:37:09

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1—1

Page 1

AP101B-7200-15

Electrical System

PART 1

CHAPTER 1—ELECTRICAL SYSTEM

Contents Para

DESCRIPTION

Power Supplies - General ... ... ... ... 1

DC Power Supplies... ... ... ... ... ... 2

AC Power Supplies ... ... ... ... ... 10

Distribution... ... ... ... ... ... ... 11

DESCRIPTION

General

1. The aircraft main electrical system is 28 volt DC supplied from four

24 volt batteries and two engine driven DC generators on the inboard

engines. DC Ground Power can be connected for servicing and starting

the engines. Arotary inverter supplies 115 volt AC power.

DC Power Supplies

2. Ground/Flight Switch. AGround/Flight Switch (marked GROUND/

FLIGHT), is on the starboard side of the fuselage just aft of the forward

mainsparandcontrolstheDCtotheaircraft. Whentheswitchisselected

up (marked GROUND) power is supplied from the external supply. In

the down position (marked FLIGHT) power is supplied from the aircraft

batteries and engine driven generators.

3. Ground Power. A 28 volt trolley accumulator can be connected to

the ground power socket in either the port or starboard wheel wells.

Whenever ground power is connected and either of the Ground Power

contactors are closed a Ground Power supply ON light is illuminated at

the Flight Engineer’s station.

4. Batteries. Four24volt40AHleadacidbatteries,givingatotaloutput

of 80AH, are to the rear of the front main spar underneath a wooden

platform. The positive feed from the batteries is connected to the battery

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1—1

Page 2

contactor. The battery contactor, which is below the ground/ight switch

and audible when operated, is closed whenever it is at FLIGHT and the

ground power contactors are open. The negative feed is connected to

earth through the ground/ight switch when it is selected to FLIGHT.

The only electrical services connected permanently to the batteries are

the ground servicing lights controlled by a switch beside the entrance

door.

Note: IfthegroundservicinglightsareleftONthebatterieswillbedrained

irrespective of the position of the ground/ight switch. The ground servicing

lights, which are in parallel, are directly connected to the batteries.

5. DC Generators. Two 1500 watt 24 volt DC generators are provided

and are driven by a quill drive from the main engine wheel case. The

generatorsareconnectedinparalleltoeachotherandtheaircraftbatteries.

Each generator has a cut out, voltage regulator and eld control switches.

The generators output is automatically controlled when the engines are

running.

6. Main Electrical Panel. The main electrical panel (MEP) is on the

starboard side of the fuselage just forward of the front main spar. On

the exterior of the panel are two generator eld switches, two ammeters

(one for each generator) and a system voltmeter. Inside the MEP are

thegeneratorcutouts,carbonpileregulatorsand aircraft services circuit

breakers.

7. Fuse Panels. In addition to the MEP, 3 fuse panels are aft of the

FlightEngineer’spanelandsupplytheremainderoftheaircraftelectrical

services.

8. Voltmeter. The voltmeter indicates the ground power, batteries or

generators voltage across the main busbar within the MEP.

CAUTION: If the voltmeter reads in excess of 29 volts the batteries are

being overcharged.

9. Ammeters. Theammetersshowthetotalloadtakenbythegenerators

whenonline. Theywill only indicatethechargingcurrent of thebatteries

if all electrical services are switched off.

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AP101B-7200-15

Electrical System

AC Power Supplies

10. A G4B compass system requires 115 volt single phase AC power

supplied by a rotary inverter under the Navigator’s table. Power for the

inverter is through a circuit breaker in the MEP. Control of the inverter

is by two buttons on the Navigator’s panel, marked ON and OFF. An

associated doll’s eye indicates when the inverter is running.

Distribution

11. The starter motors, feathering pumps and inverter are supplied through

their associated relays. The main electrical panel CBs are listed in Table 1.

Table 1 - Main Electrical Panel

Number Rating Service System

110 No. 1 FIRE EXT

FIRE

210 No. 2 FIRE EXT

310 No. 3 FIRE EXT

410 No. 4 FIRE EXT

55 No. 1 FIRE WARN

65 No. 2 FIRE WARN

75 No. 3 FIRE WARN

85 No. 4 FIRE WARN

95 No. 1 RAD SHUTTER

ENGINE

FUEL

10 5 No. 2 RAD SHUTTER

11 5 No. 3 RAD SHUTTER

12 5 No. 4 RAD SHUTTER

13 10 No. 1 PROP FEATHER

14 10 No. 2 PROP FEATHER

15 10 No. 3 PROP FEATHER

16 10 No. 4 PROP FEATHER

17 10 No. 1 PORT FUEL PUMP

18 10 No. 2 PORT FUEL PUMP

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Table 1 (continued)

Number Rating Service System

19 10 No. 3 PORT FUEL PUMP

ENGINE

FUEL

20 10 START & BOOST

21 10 No. 1 STBD FUEL PUMP

22 10 No. 2 STBD FUEL PUMP

23 10 No. 3 STBD FUEL PUMP

24 10 SUPERCHARGER

25 25 CRASH SWITCHES

ELECTRICS

NAVIGATION

COMMS

INSTRUMENTS

LIGHTING

26 25 INTERCOM POWER

27 25 INTERCOM POWER

28 10 G4B INVERTER

29 5 G4B INVERTER

30 5 IFF

31 5 NAV 825

32 10 PITOT HEATER

33 5 NAV LIGHTS

34 10 IDENT LIGHTS

35 5 RECOG LIGHTS

36 10 CABIN LIGHTS

37 5 PILLAR LIGHTS

38 5 PILLAR LIGHTS

39 5 SPARE

40 10 ANTI COLL LIGHTS

41 10 FLARE CHUTE

42 20 No. 1 LAND LIGHT

43 20 No. 2 LAND LIGHT

44 20 ENG INST MASTER

45 5 REAR DOOR WARNING

LIGHT

46 5 BOMB DOOR WARNING

LIGHT

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