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12) Make sure all the tools and materials are removed and the work area is clean and free from debris.
13) Install the tight inspection doors 513 and 514 [613 and 614] - refer to 52-40-00.
14) Fill up fuel tanks - refer to 12-11-01.
15) Check base (1), molded spacer (13) and the tight inspection doors 513 and 514 [613 and 614] for leaks.
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Validity : S/N 969,1185,1214,1478,1506 - 1508,1513 - 9999 28 40-01(DM) Page 402
SEP 04
16) Close main switch-breaker.
17) Make sure the fuel quantity displayed on the gage indicator is correct. Adjust if if necessary - refer to Page 501.
18) Open main switch-breaker.
19) Make sure all the tools and materials are removed and the work area is clean and free from debris.
20) Install the inspection doors 512, 516 [612, 616] and 519 [619], if installed- refer to 52-40-00.
AFAC
Validity : S/N 969, 1185, 1214, 1478, 1506 - 1508, 1513 - 9999 28-40-01Page 404
pm) SEP 04
14 - Rod
15 - Bolt
16 - Bellcrank
17 - Washer
18 - Nut
19 - Cotter pin
20 - Inspection door
21 - Nut
22 - Cotter pin
23 - Inspection door
24 - Bellcrank
25 - Washer
26 - Bolt
Gages - Removal / Installation
Figure 401 (2/2)
I AFAC
Validity : S/N 969, 1185, 1214, 1478, 1506 - 1508, 1513 - 9999 28-40-01Page 405
pni) SEP 04
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I AFAC
Validity : S/ N 969, 1185, 1214, 1478, 1506 - 1508, 1513 - 9999 28-40-01(D., Page 406
SEP 04
GAGES
ADJUSTMENT / TEST
WARNING : OBEY THE SAFETY PRECAUTIONS DESCRIBED IN 28-00-00. 1. ADJUSTMENT OF CAPACITY GAGES (Figures 501 and 502)
A. Tools and consumable materials
- 1 clinometer
- 1 voltmeter or 1 test bench P/N 8270TB10 00200000
- Ground power unit
- Varnish (TB 07-906)
B. Procedure
WARNING : APPLY THE MAINTENANCE PROCEDURE OF THE FUEL SYSTEM — REFER TO 28-00-00.
NOTE : To adjust the gages, the two following conditions have to be examined :
- dry gage : 12 hours minimum out of fuel
- wet gage : 24 hours minimum in fuel
The condition of the gages leads to differences in output voltage adjustment.
1) Jack up the aircraft - refer to 07-10-00.
2) Level the aircraft - refer to 08-10-00 and, using a clinometer, adjust the longitudinal attitude to - 0° 40' in the nose-down attitude - refer to 20-00-13.
3) Drain the fuel tanks - refer to 12-11-02.
4) Remove the engine monitoring cluster without disconnecting it - refer to 31-10-03.
5) Remove the seat part of the rear seat - refer to 25-12-00.
6) Remove and discard the self-adhesive pads which blank access ports to potentiometers of gaging conditioner (20).
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