|
New Manual
|
Old Manual
|
A
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| Access panels for aileron bellcranks
|
8-17 |
8-16 |
| Access panels for fuel tank fittings
|
17-1 |
10-24A |
| Access panels in rear fuselage |
24-3 |
NA |
| Aileron quick-connect system |
14-1 |
10-39 |
Aileron initial setting up procedure
|
14-9 |
10-47 |
Bellcranks
|
14-1 |
10-39 |
Fuselage mounted quick-connect bellcranks
|
14-7 |
10-45 |
Mounting belleranks to wing spar
|
14-2 |
10-40 |
Mounting quick-connect bellcrank brackets in cockpit module
|
14-7 |
10-45 |
Push-rods
|
14-3 |
10-41 |
| Ailerons |
8-1 |
8-1 |
Adjustment
|
14-10 |
10-48 |
Attaching the hinges
|
8-7 |
8-6 |
Bellcranks
|
7-3 |
7-2 |
Bellcrank access hole
|
8-17 |
8-16 |
Checking for balance
|
8-16 |
8-15 |
Close-out layups
|
8-4 |
8-4 |
First layup
|
8-2 |
8-1 |
Fitting anchor nuts to hinges
|
8-11 |
8-8 |
Fitting the aileron to the wing
|
8-10 |
8-7 |
Initial setting up procedure
|
14-9 |
10-47 |
Lateral push-rod
|
8-22 |
8-19 |
Leading edge layup
|
8-4 |
8-3 |
Link-rod
|
8-22 |
8-19 |
Mass balance arm and weight attachment
|
8-12 |
8-12 |
Mass balance arm templates
|
8-24 |
8-21 |
Mass balancing
|
8-12 |
8-12 |
Mass balance layup
|
8-15 |
8-14 |
Push-rod installation
|
8-21 |
8-18 |
Root close-out
|
8-5 |
8-4 |
Second layup
|
8-3 |
8-2 |
Setting up procedure
|
14-9 |
10-47 |
Tip close-out
|
8-7 |
8-5 |
Wing cut-out layup for mass balance
|
8-14 |
8-13 |
| Anti-servo trim tab |
5-1 |
5-1 |
Attaching the hinges
|
5-4 |
5-2 |
Flettner strips
|
5-7 |
NA |
Leading edge and root rib layup
|
5-2 |
5-1 |
Preparation for leading edge layup
|
5-1 |
5-1 |
| Antenna for comm radio |
37-2 |
Annex C |
Cable fitting
|
24-1 |
10-73 |
| Avionics - See also Electrical system
|
27-7 |
NA |
|
|
|
B
|
|
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|
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| Battery - See also Electrical system
|
27-5 |
10-129 |
| Brake master cylinder |
12-1 |
10-79 |
Brake bleeding
|
32-4 |
10-121 |
Brake lever
|
12-1 |
10-79 |
Mounting
|
12-2 |
10-80 |
| Brake installation - See also Main landing gear |
32-3 |
10-120 |
| Bungee cord - See also Main landing gear |
32-4 |
10-121 |
|
|
|
C
|
|
|
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|
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| Ceiling panel - See also Fuselage
|
24-3 |
10-76 |
| Choke control |
26-3 |
10-90 |
| Cockpit module |
|
|
Aileron quick connect system - See also Aileron quick connect
|
14-1 |
10-39 |
Bonding into fuselage
|
17-1 |
10-53 |
Access panels for fuel tank fittings
|
17-1 |
10-24A |
Aileron quick-connect bracket reinforcement
|
17-5 |
10-55 |
Bonding cockpit module in place
|
17-4 |
10-54 |
Cockpit seat pans
|
17-5 |
NA |
Control column boots
|
17-5 |
NA |
Preparation for bonding
|
17-4 |
10-54 |
Rudder cable pulleys / seat belt attachment
|
17-3 |
10-53 |
Taping rear bulkhead to fuselage
|
17-5 |
10-55 |
Taping to firewall
|
17-5 |
10-55 |
Fitting flying controls - See also Flying controls
|
13-1 |
10-7 |
Headrest storage area
|
11-5 |
10-8 |
Rear bulkhead access D panel
|
11-3 |
10-2 |
Spar pin reinforcement pads
|
14-10 |
10-48 |
Spar sockets and alignment bushes See also Wing spars
|
14-3 |
10-41 |
Thigh support ribs
|
11-3 |
10-8 |
Wheel well bulkhead
|
34-3 |
NA |
| Comm radio antenna |
37-2 |
Annex C |
Cable fitting
|
24-1 |
10-73 |
| Control stick - See also Flying controls |
13-10 |
10-16 |
|
|
|
D
|
|
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|
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| Door fitting |
36-1 |
10-92 |
Gas struts
|
36-6 |
10-97 |
Glass fitting
|
36-5 |
10-96 |
| Door latches |
35-1 |
10-26 |
Cover plates
|
35-3 |
10-28 |
Cut outs
|
35-4 |
10-29 |
Fitting latch plate covers
|
35-1 |
10-26 |
Shoot bolt guide installation
|
35-8 |
10-33 |
|
|
|
E
|
|
|
|
|
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| Electrical System |
27-1 |
10-128 |
Alternator
|
27-5 |
NA |
Avionics
|
27-7 |
NA |
Battery
|
27-5 |
) NA |
Circuit breakers
|
27-2 |
NA |
Connectors
|
27-4 |
NA |
Load calculations
|
27-10 |
NA |
Master switch / solenoid
|
27-10 |
NA |
Pitch trim
|
27-7 |
NA |
Switches
|
27-1 |
) NA |
Wiring - current rating
|
27-3 |
NA |
Wiring standards
|
27-2 |
NA |
| Elevator push rod - See also Pitch See also Tailplanes |
18-7 |
10-38 |
| Engine cowlings |
25-1 |
10-124 |
|
|
|
F
|
|
|
|
|
|
| Fin |
2-1 |
2-1 |
First layup
|
2-4 |
2-2 |
Foam core preparation
|
2-1 |
2-1 |
Second layup
|
2-6 |
2-4 |
| Fin and rudder attachment |
28-1 |
10-109 |
Bonding the fin to the fuselage
|
28-2 |
10-113 |
Comm radio antenna
|
28-2 |
10-111 |
Drainage holes
|
28-8 |
NA |
Fin trailing edge close-out
|
28-6 |
10-116 |
Push-rod attachment socket
|
28-4 |
10-113 |
Rudder attachment
|
28-3 |
10-112 |
Rudder push-rod
|
28-5 |
10-114 |
| Finishing the flying surfaces |
38-1 |
NA |
Colour
|
38-1 |
NA |
Sanding
|
38-4 |
NA |
Weight build up
|
38-6 |
NA |
| Firewall |
33-1 |
10-132 |
| Flap control system |
31-1 |
10-98 |
Cross tube hinge arms / brackets
|
31-6 |
10-102 |
Flap actuating horn
|
31-10 |
10-106 |
Flap root extension
|
31-12 |
10-108A |
Guide plate rubbing strip
|
31-4 |
10-101 |
Mounting the cross-tube
|
31-5 |
10-102 |
Pins - See also Wing lift/drag pins
|
29-3 |
10-68 |
Push-rod
|
31-9 |
10-105 |
Retraction lever guide plate
|
31-3 |
10-100 |
Retraction lever installation
|
31-1 |
10-98 |
Rubbing strip
|
31-4 |
10-101 |
Safety latch
|
31-5 |
NA |
| Flaps |
9-1 |
9-1 |
Bottom skin lay-up
|
9-2 |
9-2 |
Close-out layups
|
9-7 |
9-5 |
Co-ordinates for incidence template
|
9-12 |
9-9 |
Flap attachment
|
9-11 |
9-8 |
Flap connector plates attachment
|
9-15 |
9-11 |
Hinge plates
|
7-21 |
7-13 |
Installing hinge plates
|
9-5 |
9-4 |
Joining cores together
|
9-1 |
9-1 |
Root close-out lay-up
|
9-8 |
9-6 |
Setting flat angle
|
9-23 |
9-13 |
Setting flap angle
|
31-10 |
10-107 |
Tip close-out lay-up
|
9-9 |
9-7 |
Top skin lay-up
|
9-4 |
9-3 |
| Floor panels - See also Rudder system
|
23-1 |
10-62 |
| Flying controls |
13-1 |
10-7 |
Aileron controls
|
13-1 |
10-9 |
Aileron torque tube
|
13-4 |
10-11 |
Bearing installation
|
13-8 |
10-14 |
Control stick
|
13-10 |
10-16 |
Control stick movement
|
13-10 |
10-16 |
Control system assembly
|
13-1 |
10-9 |
Push-rods
|
13-8 |
10-14 |
Rear bearing
|
13-5 |
10-11 |
| Fuel filler hose and vent lines |
34-2 |
) |
Fuel filler
|
34-1 |
NA |
Fuel selector valve
|
34-2 |
) In |
Fuel sight gauge
|
34-3 |
) Engine |
Fuel system vents
|
34-1 |
) Fitting |
In-line restrictor
|
34-4 |
) Kit |
| Fuel system |
34-1 |
NA |
Wheel well bulkhead
|
34-3 |
NA |
| Fuel tank |
16-1 |
10-49 |
Brackets
|
16-3 |
10-51 |
Fittings
|
16-4 |
10-52 |
Spacers
|
16-5 |
10-52A |
Installation into cockpit module
|
16-1 |
10-49 |
| Fuselage |
10-1 |
10-1 |
Access panels for fuel tank fittings
|
17-1 |
10-24A |
Access panels in rear fuselage
|
24-3 |
NA |
Bottom moulding set-up
|
11-5 |
10-2 |
Fitting the cockpit module - See also Cockpit module
|
17-1 |
10-53 |
Preparing the mouldings
|
11-1 |
10-1 |
Cockpit module rear bulkhead access panel
|
11-3 |
10-2 |
Fuselage bottom moulding set-up
|
11-6 |
10-2 |
Headrest storage area
|
11-5 |
10-8 |
Thigh support ribs
|
11-3 |
10-8 |
Rear bulkhead
|
18-1 |
10-3 |
Top moulding bonding on
|
24-1 |
10-73 |
Access panel in rear fuselage
|
24-3 |
NA |
Bonding and taping
|
24-5 |
10-77 |
Ceiling panel
|
24-3 |
10-76 |
Cockpit frames
|
24-2 |
10-76 |
Pitch control stop upper brackets
|
24-6 |
10-78 |
Trial fit of the top moulding
|
24-4 |
10-75 |
Trim servo wiring and antenna cable
|
24-1 |
10-73 |
Upper pitch control stop
|
24-6 |
10-78 |
|
|
|
H
|
|
|
|
|
|
| Headrest storage area - See also Cockpit module |
11-5 |
10-8 |
|
|
|
I
|
|
|
|
|
|
| Instrument panel module |
26-1 |
10-88 |
Choke control
|
26-3 |
10-90 |
Engine instruments
|
26-3 |
10-89 |
Flight instruments
|
26-4 |
10-91 |
Instrument layout
|
26-2 |
10-89 |
Mounting
|
26-1 |
10-88 |
Pitch trim and indicator
|
26-3 |
10-90 |
|
|
|
L
|
|
|
|
|
|
| Landing gear mounting frame |
22-1 |
10-56 |
Drilling attachment bolt holes
|
22-2 |
10-57 |
Final installation
|
22-4 |
10-59 |
Preparation for installation
|
22-1 |
10-56 |
Retraction arm installation
|
22-3 |
10-58 |
Retraction shaft bush installation
|
22-3 |
10-58 |
| Lift pin socket/root fairings/spar pin latch |
30-1 |
10-82 |
Bonding the sockets
|
30-4 |
10-85 |
Front stiffener
|
30-5 |
10-86 |
Initial wing set-up
|
30-1 |
10-82 |
Rear stiffener
|
30-4 |
10-85 |
Spar pin latches
|
30-8 |
10-87B |
Wing root fairings
|
30-7 |
10-87A |
|
|
|
M
|
|
|
|
|
|
| Main landing gear |
32-1 |
10-118 |
Brake bleeding
|
32-4 |
10-121 |
Bungee cord
|
32-4 |
10-121 |
Main wheel and brake installation
|
32-3 |
10-120 |
Main wheel assembly
|
32-2 |
10-119 |
Shock absorber
|
32-1 |
10-118 |
| Mass balance system - See also Tailplane mass balance |
21-1 |
10-69 |
| Master cylinder - brakes |
12-1 |
10-79 |
|
|
|
O
|
|
|
|
|
|
| Outrigger assembly |
9-21 |
9-12 |
|
|
|
P
|
|
|
|
|
|
| Pip pin recess - See also Tailplanes
|
6-4 |
6-2 |
| Pitch control lower stop - See also Tailplane mass balance |
21-3 |
10-71 |
| Pitch control upper stop - See also Tailplane mass balance |
24-6 |
10-78 |
| Pitch push rod |
18-7 |
10-38 |
| Pitch torque tube |
15-1 |
10-34 |
End caps
|
15-1 |
10-34 |
Installation
|
15-3 |
10-36 |
Support brackets
|
15-2 |
10-35 |
| Pitch trim system |
19-1 |
10-17 |
Bellcrank assembly and mounting
|
19-2 |
10-18 |
Indicator
|
26-3 |
10-90 |
System check
|
19-7 |
10-23 |
Tab link-rod
|
19-6 |
10-20 |
Servo
|
19-5 |
10-20 |
Servo wiring
|
24-1 |
10-73 |
| Pitot system |
7-10 |
NA |
|
|
|
|
|
|
Q
|
|
|
|
|
|
| Quick connect aileron system - See also Aileron quick connect |
14-1 |
10-39 |
|
|
|
R
|
|
|
|
|
|
| Rudder |
3-1 |
3-1 |
Attachment to fuselage - See also Fin & rudder
|
28-1 |
10-109 |
First skin layup
|
3-2 |
3-2 |
Hinge attachment
|
3-8 |
3-6 |
Hinge flange
|
3-6 |
3-4 |
Preparation
|
3-1 |
3-1 |
Second skin layup
|
3-5 |
3-3 |
| Rudder system |
23-1 |
10-62 |
Aft pedals
|
23-6 |
10-65C |
Cable adjustment
|
23-5 |
10-65B |
Cable guides and rubbing blocks
|
23-7 |
10-65C |
Cable pulleys
|
17-3 |
10-53 |
Cables
|
23-4 |
10-65A |
Cables in centre tunnel
|
23-7 |
10-65C |
Floor panels
|
23-1 |
10-62 |
Forward pedals
|
23-6 |
10-65C |
Installing floor panels
|
23-4 |
10-65A |
Pedal installation
|
23-2 |
10-64 |
Pedal lateral alignment
|
23-3 |
10-64 |
Pedal reinforcement
|
23-2 |
10-63 |
Pedal tension springs
|
23-6 |
10-65B |
Pulley installation
|
23-4 |
10-64 |
Push-rod
|
28-5 |
10-114 |
Push rod hole above tailwheel bracket
|
20-2 |
10-61 |
|
|
|
S
|
|
|
|
|
|
| Seat harnesses |
37-1 |
10-126 |
Tunnel attachment point
|
17-3 |
10-53 |
| Shock absorber - See also Main landing gear |
32-1 |
10-118 |
| Spar preparation - See also Wings
|
7-1 |
7-1 |
| Static air system |
24-1 |
10-73 |
| Swinging arm installation - See also Main landing gear |
32-2 |
10-119 |
|
|
|
T
|
|
|
|
|
|
| Tailplane mass balance and control stops |
21-1 |
10-69 |
Lower pitch control stop
|
21-3 |
10-71 |
Mass balance arm installation
|
21-1 |
10-69 |
Pitch control stop / Push-rod containment
|
21-3 |
10-71 |
Push-rod containment bulkhead
|
21-4 |
10-72 |
Upper control stop brackets
|
24-6 |
10-78 |
Upper pitch control stop
|
24-6 |
10-78 |
Weights
|
21-3 |
10-71 |
| Tailplane torque-tube |
18-1 |
10-5 |
Bonding in the tailplane bushes
|
18-6 |
10-5 |
Fitting the torque tube
|
18-5 |
10-5 |
Fuselage rear bulkhead
|
18-1 |
10-3 |
Pitch push-rod
|
18-7 |
10-38 |
Tab drive pins
|
18-3 |
10-21 |
Tailplane torque tube securing
|
18-6 |
10-6 |
| Tailplanes |
4-1 |
4-1 |
Assembly
|
6-1 |
6-1 |
Close-outs
|
4-19 |
4-13 |
Cutting off the anti-servo trim tabs
|
4-16 |
4-11 |
First skin layup (bottom surface)
|
4-11 |
4-8 |
First skin layup (bottom surface) preparation
|
4-10 |
4-7 |
Joining the cores together
|
4-9 |
4-6 |
Laying up the outboard rib
|
4-6 |
4-4 |
Pip pin recess
|
6-4 |
6-2 |
Pressure relief holes
|
4-2 |
4-1 |
Second skin layup (top surface)
|
4-15 |
4-10 |
Second skin layup (top surface) preparation
|
4-13 |
4-9 |
Tab drive pins
|
18-3 |
10-21 |
Tailplane tip
|
4-2 |
4-1 |
The outboard rib
|
4-4 |
4-3 |
| Tailwheel |
20-1 |
10-60 |
Main fitting attachment
|
20-2 |
10-61 |
Rudder push-rod hole
|
20-2 |
10-61 |
| Trim system - See also Pitch trim system |
19-1 |
10-17 |
|
|
|
W
|
|
|
|
|
|
| Wheel assembly - See also Main landing gear |
32-2 |
10-119 |
| Wheel well bulkhead - See also Cockpit module |
34-3 |
NA |
| Windscreen fitting |
36-5 |
10-96 |
| Wing lift/drag pin & flap drive pin installation |
29-1 |
10-66 |
Drilling and tapping
|
29-2 |
10-67 |
Flap pins
|
29-3 |
10-68 |
Pin installation
|
29-3 |
10-68 |
Pin installation preparation
|
29-1 |
10-66 |
| Wings |
7-1 |
7-1 |
Aileron bellcrank housing and link-rod channel
|
7-18 |
7-10 |
Aileron close-out
|
7-27 |
7-16 |
Aileron mass balance cut-out layup
|
8-14 |
8-13 |
Bonding L.E. cores to the spar
|
7-8 |
7-5 |
Bonding T.E. cores to the spar
|
7-23 |
7-13 |
Close-out layups
|
7-27 |
7-17 |
Flap close-out
|
7-26 |
7-16 |
Flap plates
|
7-21 |
7-13 |
Foam Cores
|
7-5 |
7-3 |
Incidence board
|
7-16 |
9-8 |
Jigging for the trailing edge layup
|
7-19 |
7-11 |
Lateral push-rod channel
|
7-18 |
7-11 |
Leading edge ribs layups
|
7-8 |
7-5 |
Leading edge skin layup
|
7-12 |
7-72 |
Pitot system
|
7-10 |
NA |
Root close-out rib
|
7-30 |
7-19 |
Root fairings
|
30-7 |
10-87A |
Spar jigging
|
7-4 |
7-2 |
Spar preparation
|
7-1 |
7-1 |
Spar alignment bush bonding
|
14-6 |
10-44 |
Spar pin latches
|
30-8 |
10-87B |
Spar sockets and alignment bushes
|
14-3 |
10-41 |
Preparation and trial setup
|
14-5 |
10-43 |
Preparation for bonding
|
14-4 |
10-42 |
Tip block attachment
|
9-16 |
8-9 |
Cutting to shape
|
9-17 |
8-9 |
First layup
|
9-18 |
8-10 |
Second layup
|
9-19 |
8-10 |
Trailing edge bottom skin layup
|
7-24 |
7-15 |
Trailing edge close-out
|
7-26 |
7-15 |
Trailing edge cores preparation
|
7-17 |
7-9 |
Trailing edge rib layups
|
7-21 |
7-12 |
Trailing edge top skin layup
|
7-29 |
7-18 |
| Workshop and tools |
1-2 |
1-2 |
