N118
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.
6 reports on file, 1996-02-07 – 2002-01-17.
Part: LEVER — BROKEN (COCKPIT) · airframe 30,008 hrs · 30,173 cycles
BROKEN CONDITION LEVER. PERFORMED LSC1 AND THEN FERRIED AIRCRAFT TO IND TO FIX CONDITION LEVER.
Part: UPLOCK SWITCH — FAULTY (NLG) · airframe 29,914 hrs · 30,059 cycles
WHEN GEAR GOES UP TCAS AND OAT FAIL AND GET CONFIG WARNING. REMOVED AND REPLACED NLG UPLOCK SWITCH AND RETRACTED GEAR, OAT OPERATED NORMAL, TCAS OPERATED NORMAL, WHEN BRINGING POWER BACK TO FLIGHT IDLE GOT CONFIG WARNING. INSTALLED NLG SWITCH AND THEN OPS CHECK GOOD, NO CONFIG WARNING.
Part: CONNECTOR — LOOSE (LANDING GEAR) · airframe 29,914 hrs · 30,059 cycles
OAT FAIL, TCAS FAIL, AND CONFIG WARNING. RESECURED LOOSE CANNON PLUG ON WOW HARNESS, TEST FLIGHT GOOD.
Part: CHIP DETECTOR — DIRTY (LT ENGINE) · airframe 29,272 hrs · 29,552 cycles
LEFT OIL CHIP DETECTOR LIGHT ON. REMOVED INSPECTED / CLEANED.
Part: WEU — FAULTY (E/E BAY) · airframe 29,913 hrs · 30,054 cycles
WHEN GEAR RETRACTED TCAS AND OAT FAIL AND GOT CONFIG WARNING WHEN POWER REDUCED. REMOVED AND REPLACED WEU, PERFORMED CHECK OF OAT, TCAS ADN CONFIG SYSTEM AND OPS CHECK GOOD.
Part: STIFFENER — CORRODED (BS 870)
CENTER TANK STA 870 BL 0 VERTICAL STIFFENER HAS POPPED FASTENERS AND WEB IS BULDGED. INSTALLED NEW CENTER TANK VERTICAL STIFFENER AND WEB REPAIR PER SRM 51-10-1 AND EA 7-5710-27462.