N1417D
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
13 reports on file, 1996-02-14 – 2002-08-16.
Part: SEPARATOR — CRACKED (ACM BAY)
ON TAKEOFF ROLL ORD, PACK ONE TEMPERATURE WENT TO 145 DEGREES. FLIGHT ATTENDANT AND PASSENGER REPORTED SMOKE IN CABIN. PACK ONE FAULTED ON OVERHEAD. RETURNED ORD AND LANDED WITHOUT INCIDENT. REPLACED LEFT PACK SEPARATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CARGO TRACK — CORRODED (FUSELAGE)
TUL - FOUND CORROSION STATION 20320 UNDER LEFT TIE DOWN TRACK AT BELT FRAME. INSTALLED REPAIR ANGLE PER F100 SRM 53-00-025R07 NR 7.6B FIG 626 ON ESO 51000 4/5/02. (M)
Earlier reports · 1996–2001 · 11 reports
2001
Part: SPLICE — DAMAGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROW 24 INOPERATIVE. REPAIRED SPLICE AT CONNECTOR FOR EMERGENCY EXIT LIGHTS AT ROW 24. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: WIRE — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT DOOR LIGHT INOPERATIVE. TIGHTENED WIRE ON FORWARD EMERGENCY EXIT DOOR LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: DOWNLOCK TARGET — DETACHED (MLG)
DFW - FLT 2257 - DURING LANDING AFTER GEAR EXTENSION, LANIDNG GEAR DOWN LOCK WARNING. ACCOMPLISHED ALTERNATE PROCEDURE GEAR NORMAL INDICATION. LANDED ORD WITHOUT INCIDENT. REPLACED MAIN GEAR BACKUP SENSOR TARGET SCREW. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT ROW 12 FORWARD INOPERATIVE. CONNECTED LOOSE CONNECTOR AT SEAT 12D AND REPLACED CORRODED CONNECTOR AT AT ROW 4. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS AT ROW 12 FORWARD INOPERATIVE. CONNECTED LOOSE CONNECTOR AT SEAT 12 D AND REPLACED CORRODED CONNECTOR AT AT ROW 4. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, RIGHT FORWARD EMERGENCY EXIT LIGHT BROKEN. REPLACED RIGHT FORWARD EMERGENCY EXIT LIGHT.. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: COMPUTER — DEFECTIVE (E/E COMPT)
ORD - FLT 702 - DURING CLIMB-OUT AT 500 FT, STAB TRIM NR 1/2 ILLUMINATED ON MFDU AND WOULD NOT RESET. CREW ACCOMPLISHED JAMMED PROCEDURE CHECKLIST AND RETURNED AND LANDED ORD WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLE SHOT SYSTEM AND FOUND NO FAULTS. A LAND 40 TEST WAS ACCOMPLISHED WITH NO FAULTS DETECTED. UNABLE TO DUPLICATE STAB TRIM 1/2 FAULT AND AS A PRECAUTIONARY. REPLACED FLIGHT AUGMENTATION COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: CONTROL CABLE — BROKEN (MLG)
COS - FLT 0659 - ON APPROACH COS, LANDING GEAR FAILED TO EXTEND. CYCLED GEAR AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO TUL FOR REPAIR. REPLACED TELEFLEX CABLE AND RIGGED. PERFORMED GEAR EXTENSION AND RETRACTION PROCEDURES WITH NO DEFECTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1997
Part: LIGHT — DEFECTIVE (RT WING)
ORD - DURING OVERNIGHT CHECK, FOUND RIGHT WING LOWER FAIRING EMERGENCY LIGHT INOPERATIVE. REPLACED RIGHT WING LOWER FAIRING EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: FRAME — CRACKED (TAIL CONE)
TUL - CRACK AT VERTICAL CUT-OUT AUXILIARY FRAME, LT SIDE. INSTALLED REPAIR CLIP DOUBLER PER SRM 53-00-02 - R71, PAGE 203. TAT: 8,372.3 HRS; CYCLES 6,604. (X)
Part: FRAME — CRACKED (TAIL CONE)
TUL - CRACK AT VERTICAL CUT-OUT AUXILIARY FRAME, RT SIDE. INSTALLED REPAIR CLIP DOUBLER PER 53-00-02-R71, PAGE 203. TST: 8,372.3 HRS. CYCLES, 6,604. (X)