N924FT
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
21 reports on file, 2003-05-24 – 2004-04-26.
Part: LINE — LEAKING (FUEL SYSTEM) · airframe 67,015 hrs · 18,575 cycles
NR 2 ENGINE FUEL LEAK FROM DRAIN MAST FOUND DURING PREFLIGHT. FOUND PSO LINE AT EVC LEAKING. INSTALLED NEW FERRULE AND RESEATED LINE. PERFORMED IDLE RUN AND LEAK CHECK PER MM 71-00-80. TEST NR 3 NO LEAKS EVIDENT.
Part: START VALVE — FAILED (NR 4 ENGINE) · airframe 67,015 hrs · 18,575 cycles
START VALVE NR 4 ENG ILLUM DURING TAXI. ENGINE SHUTDOWN AND RETURN TO RAMP. R&R STARTER VALVE IAW AMM 80-04-01.
Part: PITOT TUBE — DAMAGED (FUSELAGE) · airframe 66,827 hrs · 18,534 cycles
AT DEPARTURE TIME, CAPT'S MAIN PITOT LIGHT STAYED ON WITH SWITCH IN ON POSITION. R&R CAPT'S PITOT PROBE. OPS AND LEAK CHECK OK PER MM 34-11-01.
Part: SWITCH — FAILED (TE FLAPS) · airframe 66,798 hrs · 18,527 cycles
OUTBOARD AILERONS FAILED TO UNLOCK AFTER FLAPS 20 DEG SELECTED. FOUND FLAP LIMIT SWITCH S216 FAILED. R & R SWITCH, ALL OPS NORMAL.
Part: CONNECTOR — DIRTY (AILERON CONTROL) · airframe 66,715 hrs · 18,512 cycles
ON TAXI OUT FLIGHT CONTROL CHECK, NO O/B AILERON INDICATION. RECONNECTED AND CLEANED CONNECTOR S313 SWITCH. OPS CK NORMAL PER MM 27-10-00.
Part: CONNECTOR — DIRTY (AILERON INDI) · airframe 66,715 hrs · 18,512 cycles
DURING FLIGHT CONTROL CHECK, NO INDICATION OF AILERON MVMT. CLEANED CONNECTOR D3297J AT J-BOX IN RT WHEEL WELL. PERFORMED FLIGHT CONTROL CHECK. ALL OPS AND INDICATIONS NORMAL PER MM 27-11-16.
Part: STOP — OUT OF ADJUST (L-1 DOOR) · airframe 66,474 hrs · 18,465 cycles
L-1 DOOR DIFFICULT TO CLOSE. ADJUSTED ALL STOPS AS REQ'D IAW MM 52-11-01, OPS CHECK NORMAL.
Part: CONNECTOR — LOOSE (AILERON CONTROL) · airframe 66,391 hrs · 18,447 cycles
NO AILERON MOVEMENT DURING FLT CONTROL CHECK. CLEANED AND RESECURED CONNECTOR D3296P AT J42-J-BOX. OPS CK OK, IAW MM 27-11-00.
Part: CONNECTOR — INOPERATIVE (AILERON CONTROL) · airframe 66,391 hrs · 18,447 cycles
NO AILERON MOVEMENT INDICATION DURING FLIGHT CONTROL CHECK. CLEANED CONNECTOR ON AILERON INDICATOR IAW 27-10-00. OPS CK GOOD.
Part: CIRCUIT CARD — LOOSE (AILERON CONTROL) · airframe 66,391 hrs · 18,447 cycles
OB AILERONS LOCKED OUT, CYCLED FLAPS TWICE AND RESET C/B. NO HELP. RESEATED A1 CARD IN FLAP CONTROL CK AND VISUAL, OPS NORMAL IAW MM 27-10-00.
Part: ACTUATOR — FAILED (CARGO DOOR) · airframe 66,065 hrs · 18,382 cycles
MAIN SIDE CARGO DOOR WILL NOT LOCK. MOTOR RUNS BUT ACTUATOR DOES NOT TURN. CORRECTIVE ACTION TAKEN: REMOVED AND REPLACED LATCH ACTUATOR IAW AMM 52-32-09 OPERATION, INDICATION CK OK.
Earlier reports · 2003 · 10 reports
2003
Part: DOWNLOCK SWITCH — SHORTED (NLG) · airframe 65,783 hrs · 18,319 cycles
AFTER PUSHBACK AUTO SPOILER LT CAME ON FOUND PRIM & CONT C/B POPPED. A/C RETURNED TO BLOCKS. TRANSFERRED TO DMI 31904 PER MEL 32-11A FOUND NOSE GEAR PRIMARY DOWNLOCK SWITCH S206 SHORTED.
Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 65,661 hrs · 18,292 cycles
ON ARRIVAL NR 1 ENG HAS HEAVY FUEL LEAK OUT OF DRAIN. REPLACED NR 1 ENGINE FUEL PUMP RUN UP & LEAK OK PER MM 73-11-01 AND 71-00-00.
Part: ACTUATOR — FAILED (FUEL SHUTOFF) · airframe 65,611 hrs · 18,279 cycles
NR 3 ENGINE FAILED TO START. REACHED 40 PERCENT, THEN APPEARED TO FLAME OUT. REPLACED FUEL SOV ACTUATOR.
Part: TIRE — FAILED (MLG) · airframe 65,480 hrs · 18,248 cycles
NR 6 MAIN TIRE WORN TO LIMITS (SHREDDED.) REPLACED NR 6 MAIN TIRE AND ALSO NR 5 MAIN TIRE IAW MM 32-45-01.
Part: AUTOLAND SYS — MALFUNCTIONED (COCKPIT) · airframe 65,283 hrs · 18,205 cycles
LOUD SIDE TONE IN F/O INTERPHONE. RERACKED NR 2 LRRA - TRANSCEIVER IAW MM 34-42-00, OPS CHECK OK. NOISE DISAPPEARED.
Part: INDICATOR — MALFUNCTIONED (OIL PRESSURE) · airframe 65,269 hrs · 18,202 cycles
OIL PRESSURE LIGHT NR 3 ENG FLICKED WITH CORRESPONDING FLUCUATION OIL PRESSURE. CLEANED, INSPECTED CONNECTOR CHECKED OIL FILTER FOR OBSTRUCTIONS AND NO DEFECTS FOUND. ALL INDICATIONS CHECKED NORMAL.
Part: CONTROL PANEL — JAMMED (COCKPIT) · airframe 65,264 hrs · 18,201 cycles
ALTITUDE ALERT CONTROL FROZEN. REMOVED AND REPLACED AUTOPILOT FLT DIRECTOR PANEL.
Part: STARTER — FAILED (NR 4 ENGINE) · airframe 54,864 hrs · 13,836 cycles
ON START UP NR 4 ENG STARTER FAILED. REMOVED AND REPLACED 4 ENG STARTER IAW MM 80-11-01 OPS CK GOOD.
Part: STARTER — FAILED (NR 4 ENGINE) · airframe 75,571 hrs · 18,609 cycles
NR 4 ENG STARTER FAILED ON ENG START. ALL ENG PARAMETERS NORMAL. REMOVED AND REPLACED NR 4 ENG STARTER PER MM 80-11-04. REPLACED STARTER COUPLING AS PRECAUTIONARY STARTER TEST NORMAL PER MM 80-11-04.
Part: CONTROL UNIT — INOPERATIVE (NR 1 ENGINE) · airframe 64,218 hrs · 17,975 cycles
RTB, NR 1 ENG GENERATOR FIELD LT NR 4 ADP INOP. NR 2 GENERATOR ALREADY ON DEFERRAL, 1-2ND RTB NR 3 GEN INOP. SWAPPED NR 1 & NR 2 GCU (NR 2 GEN DEFERRED) OPS NORMAL. CLEANED & RESEATED CONNECTORS FOR NR 4 ADP S/O VALVE, ADP OPS NORMAL 2ND RTB NR 3 ENG GENERATOR OPS CHECKED NORMAL ON ENG RUN. SWAPPED GLU'S FROM NR 2 GENERATOR (ON DEFERRAL) NR 1 GEN OPS NORMAL. NO FURTHER DISCREPENCIES.