TM 1-1520-240-CLP-2c. Wiring harness - Fuel quantity sensing —Check connection security of J4.d. PUMP AC circuit breakers, six (6) each —Check in reset position on TANK 1, TANK 2,and TANK 3 (if installed).e. PANEL POWER circuit breaker — Check inreset position.f. PANEL LIGHTING circuit breaker — Checkin reset position.g. PUMP switches — OFF on TANK 1, TANK2, and TANK 3.h. PRESS LOW lights, three (3) each — Pressto test (Aircraft power must be on toilluminate).i. REFUEL VALVE — Check CLOSED.j. Panel illumination switch/rheostat — OFF.k. FUEL QUANTITY switch — Set 1, 2, 3 andTOTAL to check quantity in each tank(aircraft power must be on to illuminate).HYDRAULIC COMPARTMENTS CHECKSAFT COMPARTMENT1. Condition and security of lines and coolers.2. No. 2 flight control system accumulator forproper indication (see chart this section).3. Utility reservoir pressurization accumulator for2500to 3500psi charge.FORWARD COMPARTMENT1. Condition and security of lines and coolers.2. No. 1 flight control system accumulator forproper indication (see chart this section).
Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business
