N1424M

PIPER PA-32-260 · 1973 · Fixed-wing single-engine · 1 engine · 6 seats · Valid Registration

Registered owner: FLY HIGH LLC, AL (owner ≠ operator)

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.

4 reports on file, 1997-03-12 – 2003-09-02.

NO TEST · 2003-09-02 Matched by certificate designator
ATA 3350

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ORD - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 13 AND 14. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Source: SDR AALA20030939
NO TEST · 2001-02-07 Unresolved
ATA 3397

Part: WIRE — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD CABIN INOPERATIVE. SPLICED EMERGENCY EXIT LIGHT FLOOR PROXIMITY LIGHT WIRE AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Source: SDR AALA20010225
NO TEST · 1997-11-14 Matched by certificate designator
ATA 3397

Part: WIRE — DEFECTIVE (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, FOUND THE EMERGENCY EXIT PATH MARKING SIGN AT THE RIGHT FORWARD SERVICE DOOR INOPERATIVE. REPAIRED WIRING AT RIGHT FORWARD SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Source: SDR AALA972172
FLT CONT AFFECTED · 1997-03-12 Matched by certificate designator
ATA 2211

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT)

IAD - FLT 1823 - DURING APPROACH TO DCA WHEN NR 1 AUTOPILOT WAS DISCONNECTED, A/C FELT NOSE HEAVY AND STAB TRIM NOTED AT FULL NOSE DOWN. STAB TRIM THEN RAN TO FULL NOSE UP FOLLOWED BY NR 1 AND NR 2 STAB TRIM FAULTING. A/C DIVERTED TO IAD, LANDED W/O INCIDENT. FAULT TEST REVEALED NO FAULTS. PREVIOUS FAULT REVIEW REVEALED AP DISC/INH FMP, TRIM 1 FAIL TRIM SERVO/FAC 1, AP DISC/INH TRIM SERVO/FAC2. AFCS TESTS REVEALED NO SYSTEM FAULTS. PRECAUTIONARY REPLACED FLT AUGMENTATION COMPUTER. SYS GROUND CHECKED NORM OPS. ACCOMP FUNCTIONAL CHECK/MX FERRY FLT IAD/ORD WITH NO DEFECTS FOUND. SYS OPS CHECKED NORM AND A/C RETURNED TO SERV. (M)

Source: SDR AALA970532