Technical data

13773-001

28-10

Page 730 Nov 2000

Note: If the fuel leak is located at a bondline, joint or seam, mix sealant (MIL-8802

Type 2 Class A and/or Class B) per manufacture’s instructions. (Refer to 20-

10)

If the leak is coming from a small pinhole located away from any bondlines,

joints or seams, mix non-structural resin (Type 2, Class 1) per the manufac-

ture’s instructions.

(l) Fillet, fay or injection seal as required. Brush sealant or resin over repair area making sure

brushed area is larger than the repaired area. (Refer to 20-10)

(m) Allow sealant or resin to fully cure.

(n) Seal and install fuel tank access panel(s). (Refer to 6-00)

(o) Fill the fuel tank. (Refer to 12-10)

(p) Visually inspect tank seams for any signs of leakage or stains. If any leaks are present,

repair tank as needed. (Refer to 28-10)

(q) Connect battery. (Refer to 24-30)

(r) Remove airplane exhaust outlet pipe ground.

B. Collector Tanks

The collector tanks are made out of composite material and are integrated into each side of the wing

and cannot be removed.

(1) Adjustment/Test - Collector Tank

(a) Perform Fuel Tank Pressure Test. (Refer to 28-10)

(2) Inspection/Check - Collector Tank

(a) Drain the corresponding fuel and collector tank bays for the side being serviced. (Refer to

12-10)

(b) Remove the appropriate access panel (LW3 or RW3) from the wing to gain access to the

collector tank bays. (Refer to 6-00)

damage, stains or leaks are present, repair tank.

(d) Seal and secure access panel with screws.

(e) Fill the corresponding fuel tank.

(f) Inspect the fuel and collector tank bays, hoses, and lines for any signs of leakage. Service

as required.