Difference between revisions of "Gipsy major overhaul manual"

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LUBRICATING OIL FOR DE HAVILLAND GIPSY ENGINES
 
 
The Gipsy range of de Havilland piston engines is approved for operation in Arctic and Temperate conditions on lubricants complying with British Ministry of Supply Specification D.Eng.R.D.2472, and in Tropical conditions on lubricants complying with de Havi1land Specification DHE.227.
 
 
The appropriate grade of oil must be used according to the prevailing conditions and the following grades of oil, certified as complying with these requirements, are, until further notice, suitable for use in de Havilland Gipsy engines in appropriate climatic and operating conditions.
 
 
{| class="wikitable"
 
|-
 
|
 
<center>Conditions of</center>
 
 
<center>Operation</center>
 
 
|
 
<center>"Arctic"
 
 
(Below 0 deg. C.)</center>
 
 
|
 
<center>" Temperate "
 
 
(0-30 deg. C.)</center>
 
 
|
 
<center>"Tropical"
 
 
(Above 30 deg. C.)</center>
 
 
|-
 
|
 
<center>Specification</center>
 
 
|
 
<center>D.Eng.R.D.2472.A/O</center>
 
 
|
 
<center>D.Eng.R.D.2472.8/O</center>
 
 
|
 
<center>deHavilland DHE.227</center>
 
 
|-
 
| colspan="4" |
 
<center>The following grades comply with the above specifications.</center>
 
 
|-
 
|
 
<center>Esso Petroleum Co.</center>
 
 
|
 
<center>Esso Aviation Oil 80</center>
 
 
|
 
<center>Esso Aviation Oil 100</center>
 
 
|
 
<center>Esso Aviation Oil 120</center>
 
 
|-
 
|
 
<center>Shell.:.Mex Ltd</center>
 
 
|
 
<center>Aeroshell 80</center>
 
 
|
 
<center>Aeroshell 100</center>
 
 
|
 
<center>Aeroshell 120</center>
 
 
|-
 
|
 
<center>Regent Oil Co.</center>
 
 
|
 
<center>Caltex
 
 
Aircraft Engine Oil 80</center>
 
 
|
 
<center>Caltex
 
 
Aircraft Engine Oil 100</center>
 
 
|
 
<center>Caltex
 
 
Aircraft Engine Oil 120</center>
 
 
|-
 
|
 
<center>Vacuum Oil Co.</center>
 
 
|
 
<center>Mobiloil Aero, grey band</center>
 
 
|
 
<center>Mobiloil Aero, red band</center>
 
 
|
 
<center>Mobiloil Aero, green band</center>
 
 
|-
 
|
 
<center>C. C. Wakefield & Co.</center>
 
 
|
 
<center>Castrolaero " A "</center>
 
 
|
 
<center>Castrolaero<nowiki> " B ''</nowiki></center>
 
 
|
 
<center>Castrolaero " C "</center>
 
 
|}
 
The conditions of operation given above can, of course, act only as a general guide, for, as will be readily appreciated, the wide variations of temperature that may occur in one locality even during a single day would make impossible a literal application of the recom­ mendations. In general, however, if it is expected that the temperatures specified for the use of tropical or arctic grades of oil will be met at ground level during the normal course of opera ion of the aircraft at that particular time, then the appropriate grade of oil should be used.
 
 
 
 
 
  
 
OPERATING LIMITATIONS, PERFORMANCES AND FUEL CONSUMPTION
 
OPERATING LIMITATIONS, PERFORMANCES AND FUEL CONSUMPTION

Revision as of 16:01, 11 July 2020

OPERATION, MAINTENANCE AND OVERHAUL
GIPSY MAJOR SERIES 10

This manual compiles with British Civil Airworthiness Requirements Section A, Chapter A6-2. The technical accuracy of this manual has been verified and is certified as correct.

CONTENTS AND LIST OF CHAPTERS

NOTE : A list of its contents and illustrations appears at the beginning of each chapter.

FRONTISPIECE

FOREWORD

INTRODUCTION

LEADING PARTICULARS

LUBRICATlNG OILS

OPERATING LIMITATIONS

GIPSY MAJOR MK. 8

TORQUE LOADING TABLE

CHAPTER

I.

Description of Engine.

II.

Lubrication.

Ill.

Carburation.

IV.

lgnition.

V.

Installation.

VI.a.

Operating Instructions.

VI.b.

Defect Diagnosis.

VI.c.

Storage and Anti-Corrosion Treatment.

V I.d.

Components containing asbestos.

VII.

Maintenance Schedule and Routine Servicing.

VIII.

Tools and Equipment.

IX.

Dismantling.

Xl.

Rectification and Salvage.

XII.

Reassembling.

XIII.

Testing after Overhaul.

XIV.

Table of Fits and Clearances.

XV.

BTH Magnetos.

XVI.

Rotax Electric Starter.

XVII.

K.L.G. Sparking Plugs.

XVIII.

Lodge Sparking Plugs.

XIX.

Hobson Carburettor.

XX.

Fuel Pump.

Accessory Manufacturers' Addresses.

OPERATING LIMITATIONS, PERFORMANCES AND FUEL CONSUMPTION

For oil pressures and minimum temperature, see Leading Particulars.
Powers subject to a tolerance of minus 4 per cent.

With a fixed-pitch propeller it is not possible to obtain all these conditions but none of the operating limitations may be exceeded.

Gipsy Major 10, Mark 1-1, 1-IA, 1-3, l-3A, 1-7 and 1-7A (Based on Engine Technical Certificate No. SS, issue 6, 25-1-55)

Flying conditions

Time limitation

R.P.M.

Boost pressure in. Hg. cm. Hg.

Cyl. temp, deg. C.

Oil temp, deg. C. Oil grade* D. Eng. R.D.2472 B/O

B.H.P. at Sea Level

Fuel consumption (upper limit)







Galls, per hr.

Litres per hr.

Maximum take-off

Maximum emergency

-- 5 min.

2400

2550

Full Throttle

240

100

136/142

145

11¼

11½

51,11

52,25

Climb

Emergency cruise

60 min. --

--

2400

Full Throttle

230

85

136/142

11¼

51,11

Maximum cruise

--

2300

Minus 1½ Minus 3,8

210

85

138

10

48,9

Maximum cruise, weak

--

2300

Minus 4 Minus 10,2

210

85

120

3750 ft.

1143 m.

38,62

Maximum overspeed

20 sec.

2675

Full Throttle

--

--

--

--

--

Gipsy Major 10, Mark 2 and 2-1. (Based on Engine Technical Certificate No. 89, issue 7, 12-1-56)

Flying conditions

Time limitation

R.P.M.

Boost pressure in. Hg. cm. Hg.

Cyl. temp, deg. C.

Oil temp, deg. C. Oil grade* D. Eng. R.D.2472 B/O

B.H.P. at Sea Level

Fuel consumption (upper limit)







Galls, per hr.

Litres per hr.

Maximum take-off

Normal

Emergency

5 min. 15 min.
2550
Full Throttle
255
100
139/145
11½
52,25

Minimum r.p.m. at

maximum take-off boost pressure

--
2000
--
--
--
--
--
--

Maximum continuous

--
2400
Full Throttle
250
85
136/142
11¼
51,11

Maximum weak mixture

--
2300
Minus 4 Minus 10,2
230
85
120

3750 ft.

1143 m.
9
40,89

Maximum overspeed

20 sec.
2675
Full Throttle
--
--
--
--
--

For information regarding the use of lubricating oils see page vii.

GIPSY MAJOR M K.8

As the original Gipsy Major Mk. 8 engines (pre-mod. 1685) were fitted with Hoyt white­ metal bearings and all the Gipsy Major 10 Mk. 2 engines have the Vandervell main bearings, civil

approval of the Gipsy .M. ajor Mk. 8 was neither sought nor obtained.

With increasing numbers of Royal Air Force Gipsy Major Mk. 8 engines becoming available in the civil market, the Air Registration Board has agreed that this type of engine can be used in civil aircraft subject to the following provisos :-

  1. The military log card or log book must be available.
  2. Before the engine may be used, the operator must comply with the current requirements of Air Registration Board Notice to Licensed Aircraft Engineers No. 16.
  3. On transfer of the engine from the Royal Air Force, a civil type log book must be raised and all relevant entries made in it. The log book may only be raised by the Inspection Department of an organisation approved for the overhaul of de Havilland Gipsy engines, or by a ‘ D’ Licence engineer in this category.
  4. The engine type must be recorded in the log book as “Gipsy Major 10 Mk. 2” and the engine name plate must be altered to accord with this nomenclature.
  5. The log book must be endorsed to the effect that only fixed-pitch propellers may be used on the Gipsy Major Mk. 8, or 10 Mk. 2, engines with Hoyt white-metal main bearings ; modification 1685 introduced Vandervell bearings to Gipsy Major Mk. 8 engines.

The instructions and information given in this handbook for the Gipsy Major 10 Mk. 2 are equally applicable to the Gipsy Major Mk. 8 having regard to· the modification standard of the engine.

When ordering spares for Gipsy Major Mk. 8 engines, operators must inform this Company of the engine number for which the parts are required, so that the correct parts may be supplied.



''''TORQUE LOADING TABLE


To assist overhaul and maintenance operators to ensure that correct loads are applied when tightening certain nuts on Gipsy Major Series 10 engines, the table set out below lists the respective torque loading values. These values are subject to threads being lubricated, and not being stiff to turn during any part of their travel ; they are not the loadings to be applied when the appropriate studs are being inserted. The table will be amended accordingly when appropriate torque loading values are issued for other components of the engine.

Nut Part No.

Descriplion
Torque Loading (lb. in.) and recommended tools

800-CN-1

Nut, Intermediate and Rear Main Bearing

500 to 600

MSW 208, TQ.S0A

800-CN-2

Nut, Front Main Bearing

300 to 400

MSW 207, TQ.S0A

N.372 or

N.376

Nut, Rocker Bracket (pre-mod. 2197)

300
MSW 205. TQ.S0A

N.6542

Nut, Rocker Bracket (mods. 2197 or 2282)*

Tighten to 360, slacken completely and then retighten to 275.

MS W 204, TQ.S0A

1900/3

Nut, Connecting Rod

180 to 270 MSW 204, TQ.50A

801/16B

Nut, Cylinder, Holding Down

350 to 400 mod. 2329 T79017

T79013

T86451

Cylinder Heads (mods. 2197 and 2282)

Modification 2197 introduces a redesigned cylinder head of L.35 (' Y' alloy) which provides for the attachment of the rocker bracket to the cylinder head with three studs and one bolt. The rocker platform provides better support by improved cylinder head webbing ; the valve rocker bracket supports the valve rocker cover thus dispensing with the stirrup bracket ; the cylinder head cooling is improved by additional finning in the vicinity of the exhaust port ; and 14 mm. sparking plug adapters replace the l 2 mm. type. When this modification is embodied, the / 2 mm. sparking "plug end fittings of unscreened, and screened ignition cables are replaced with end fittings suitable for use with the 14 mm. screened type sparking plugs.

As an alternative to the cylinder head mod. 2197, a cylinder head mod. 2282 is introduced incorporating 12 mm. plug adapters to permit the use of 12 mm. sparking plugs.

When assembling the rocker bracket to the cylinder head, it is important that all the rocker bracket attachment nuts are tightened in rotation with small torque increments until the final torque loading value is obtained.