N5368F

No registry detail on file · not in current registry

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.

11 reports on file, 1996-03-13 – 1996-05-09.

OTHER · 1996-05-09 Matched by certificate designator
ATA 2820

Part: SWITCH — FAILED (FUEL SYS)

FUEL SWITCH INOPERATIVE. VALVE IS STICKING.

Source: SDR HEEA967185
OTHER · 1996-05-06 Matched by certificate designator
ATA 5610

Part: CHIN BUBBLE — MIS MFG (RT FUSELAGE)

R/H CHIN BUBBLE IS TOO SHORT AND WILL NOT REACH CANOPY DOOR POST.

Source: SDR HEEA967111
OTHER · 1996-04-23 Matched by certificate designator
ATA 2312

Part: CONTROL UNIT — FAILED (COCKPIT COMM)

CONTROL UNIT DOES NOT WORK. REPLACED FUSE F1. REPAIRED. FOUND VOLUME TO HAVE DEAD SPOTS WHEN TURNING VOLUME KNOB. REPLACED ON/OFF PONTENTIOMETER R1/S5. REPAIRED. BENCH CHECK GOOD.

Source: SDR HEEA967070
OTHER · 1996-04-18 Matched by certificate designator
ATA 2312

Part: CONTROL UNIT — FUSE BLOWN (COCKPIT COMM)

DOES NOT COME ON. REPLACED FUSE F1. REPAIRED. BENCH CHECK GOOD.

Source: SDR HEEA967061
OTHER · 1996-04-18 Matched by certificate designator
ATA 5320

Part: LONGERON — CORRODED (ENG PAN)

R/H UPPER AFT ENGINE PAN OUTBOARD LONGERON IS CORRODED THROUGH AND CRACKED OUT AT SEVERAL RIVET HOLES IN THE AREA WHERE THE ECU LINE GOES THROUGH THE ENGINE DECK. THE INNER ALUM. DOUBLERS ARE ALSO CORRODED THROUGH IN THIS AREA. REMOVED TRANS DECK AFT A-FRAME SUPPORT. REMOVED ENGINE DECK. REMOVED INNER DOUBLERS. REMOVED UPPER OUTBOARD LONGERON. CUT OUT DAMAGED AREA OF LONGERON AND SPLICED. MFG NEW INNER DOUBLERS. MFG NEW ENGINE DECK. REASSEMBLED AREA AS NEEDED.

Source: SDR HEEA967052
OTHER · 1996-04-18 Matched by certificate designator
ATA 7720

Part: WIRING HARNESS — CORRODED (ENG TEMP)

PART IS CORRODED. (ENG HARNESS CORRODED) REPLACED WITH SERVICEABLE PART.

Source: SDR HEEA967051
OTHER · 1996-04-15 Matched by certificate designator
ATA 7722

Part: INDICATOR — ERROR (EXH TEMP)

EXCESSIVE FRICTION ERROR 20 DEGREES TO 30 DEGREES. S/N 690 & 775

Source: SDR HEEA966999
NO TEST · 1996-04-08 Matched by certificate designator
ATA 7712

Part: TRANSMITTER — WONT TEST (ENG TORQUE)

TORQUE TRANSMITTER WON'TTEST CORRECTLY. CAUSES INDICATOR TO READ LOW.

Source: SDR HEEA966961
NO TEST · 1996-04-08 Matched by certificate designator
ATA 6240

Part: INDICATOR — WONT TEST (MAST MOMENT)

INDICATOR WON'TTEST CORRECTLY. CAUSES INDICATOR TO READ LOW.

Source: SDR HEEA966962
OTHER · 1996-03-13 Matched by certificate designator
ATA 6210

Part: BLADE — CRACKED (M/R)

PART IS CRACKED. (NOSE AND NECK SHELL CRACKED AND SEPARATED THERE ARE SEPARATION ALSO PRESENT ON THE THREE INBOARD LEADING EDGE ABRASION STRIP.

Source: SDR HEEA966855
OTHER · 1996-03-13 Matched by certificate designator
ATA 6210

Part: BLADE — CRACKED (M/R)

PART IS CRACKED. (NOSE AND NECK SHELL CRACKED AND. THE INBOARD STRIP HAS SEPARATION AT JOINT.

Source: SDR HEEA966856