JOINT ADVANCED MULTI-ENGINE T-44A
After aircraft taxis into parking spot, P sets parking brake then directs CP to "Continue the
P ensures brake handle pulled out fully and brakes pumped firm.
CP ensures radar is OFF.
P selects AVIONICS MASTER PWR switch OFF.
P selects #1 Inverter OFF. Ensure #2 inverter picks up the load (both AC bus voltmeters normal). P
selects #2 Inverter OFF.
CP selects vent blower AUTO.
11. CABIN TEMPERATURE MODE
CP selects cabin temperature mode OFF.
P pulls both prop levers into FEATHER and ensures N2 RPM immediately starts to drop. There is
no need to wait for the props to fully feather before continuing the checklist.
13. CONDITION LEVER(S)
"FUEL CUTOFF" (P)
P ensures ITT has been below 650º C for at least 1 minute. P places left hand on left condition lever
and right hand on right condition lever, then simultaneously selects FUEL CUTOFF with both
levers. P notes ITT decrease and monitors engine instruments for a normal shutdown.
14. BOOST PUMPS
P selects both boost pumps OFF.
15. FUEL QUANTITY CURRENT LIMITERS
P notes normal indication on left and right indicators. If either indicator reads zero, a current limiter
may have blown.
Turn all exterior lights OFF except NAV (if used) and BEACON. Turn NAV and BEACON OFF
when props have stopped turning. Return both ANN switches to BRIGHT, turn annunciator lights,
DME, and NCS-31 DIM switches fully bright. Turn all cockpit lights OFF. Turn both utility lights
OFF and return them to their overhead receptacles.
17. GANG BAR
P pulls gang bar aft, securing all electrical power.
18. CONTROL LOCK
"NOT REQUIRED" (P)
P installs control lock. Ensure chain is not tangled, then:
a. Place guard around engine/prop controls, open side facing aft.
b. Pull yoke aft until hole is visible in tube. Push yoke forward approximately 2 inches until hole in
tube and hole in column are lined up. Slide pin into top hole. Route chain around left side of