N782TW

MCDONNELL DOUGLAS DC-9-15F · 1967 · Fixed-wing multi-engine · 2 engines · 116 seats · Valid Registration

Registered owner: SIERRA AMERICAN CORP, DE (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.

5 reports on file, 2015-06-17 – 2026-04-03.

WARNING INDICATION · 2026-04-03 Matched by certificate designator
ATA 2130

Part: CONTROL VALVE — STUCK (ZONE 100) · airframe 53,674 hrs · 60,043 cycles

UNABLE TO MAINTAIN CABIN PRESSURE WITH ONE PACK. CABIN LIGHT ILLUMINATED SHORTLY AFTER REACHING FL250. LAFT PACK INOP. RT PACK CURRENTLY ON MEL REF DMI# 7827716C. REMOVED AND REPLACED RT & LT FLOW CONTROL VALVES, LH SHUTOFF DIFFERENTIAL PRESSURE SWITCH PER AMM 21-31-2 AND 21-31-9. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER IAW AMM 21-31-2.

Source: SDR MJYA20260403002
OTHER · 2015-09-17 Matched by certificate designator
ATA 5753

Part: ATTACH FITTING — CORRODED (TE FLAP VANE) · corrosion level 2 · airframe 40,872 hrs · 39,336 cycles

CORROSION WAS FOUND ON THE FLAP FIXED VANE ATTACH FITTING. THIS WAS REPAIRED IAW SRM CHAPTER 51.

Source: SDR MJYA20150811010
OTHER · 2015-06-18 Matched by certificate designator
ATA 5320

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,432 hrs · 57,855 cycles

VERTICAL STIFFENER BETWEEN STATION 58, STRINGER 17 - 21 HAD CORROSION.

Source: SDR MJYA20150618003
OTHER · 2015-06-17 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,432 hrs · 57,855 cycles

LAP SEAM UPPER & LOWER SKIN CORRODED.

Source: SDR MJYA20150617002
OTHER · 2015-06-17 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,432 hrs · 57,855 cycles

LAP SEAM UPPER & LOWER SKIN CORRODED.

Source: SDR MJYA20150617001