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3) Connect electric connector (8).
4) Install rod (10) and attach it to bellcranks (12) and (20) with bolts (11) and (22), washers (13) and (21)
and nuts (14) and (17). Install new cotter pins (15) and (18).
5) Fill up fuel tanks - refer to 12-11-01.
6) Make sure that there is no leakage between base (7) and gage (5).
7) Close main switch-breaker.
8) Make sure the fuel quantity displayed on the gage indicator is correct.
9) Open main switch-breaker.
10) Make sure all the tools and materials are removed and the work area is clean and free from debris.
11) Install the inspection doors 512 and 516 [612 and 616] and 515 [615], if removed - refer to 52-40-00.
ADAB
Validity : S / N 275 - 968, 970 - 1184, 1186 - 1213,
1215 - 1477, 1479 - 1505, 1509 - 1512 28-40 01Page 402
(DA) SEP 02
1 - Wings spar
2 - Fuselage wing electric connector
3 - Washer
4 - Bolt
5 - Gage
6 - Seal
7 - Base
8 - Electric connector
Gages - Removal / Installation
Figure 401 (1/2)
10 - Rod
11 - Bolt
12 - Bellcrank
13 - Washer
14 - Nut
15 - Cotter pin
16 - Inspection door
17 - Nut
18 - Cotter pin
19 - Inspection door
20 - Bellcrank
21 - Washer
22 - Bolt
Gages - Removal / Installation
Figure 401 (2/2)
ADAB
Validity : S / N 275 - 968, 970 - 1184, 1186 - 1213,
1215 - 1477, 1479 - 1505, 1509 - 1512 28-40-01Page 404
(DA) SEP 02
GAGES
REMOVAL / INSTALLATION
WARNING : OBEY THE SAFETY PRECAUTIONS DESCRIBED IN 28-00-00.
NOTE : This procedure is applicable to L.H. and R.H. installations. Information specific to R.H. installation are given in square brackets.
NOTE : Removal and installation of gages do not affect adjustment. However, if the gage has been replaced or if an adjustment is necessary, refer to Page 501.
NOTE : After applying this procedure, MOD. 194 is applied.
1. REMOVAL OF THE GAGES (Figure 401)
A. Tools and consumable materials
- Isopropyl alcohol (TB 10-002)
- Linttree clean cloth
- Spatula
- Hot air generator
B. Procedure
WARNING : APPLY THE MAINTENANCE PROCEDURE OF THE FUEL TANKS — REFER TO 28-00-00.
1) Drain the fuel tanks - refer to 12-11-02.
2) Remove the inspection doors 512,516 [612, 616] and 519 [619], if installed - refer to 52-40-00.
3) Remove the tight inspection doors 513 and 514 [613 and 614] - refer to 52-40-00.
4) Remove nuts (18) and (21), washers (17) and (25), bolts (15) and (26) and discard cotter pins (19) and (22). Disconnect intermediate aileron control rod (14) from bellcranks (16) and (24).
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