N131FL
Registered owner: IFL GROUP INC, MI (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.
19 reports on file, 2004-12-22 – 2015-04-28.
Part: STRUCTURE — CRACKED (NLG WW) · airframe 47,752 hrs · 47,227 cycles
FOUND CRACKS IN NOSE WW AT STATION 26 RT.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 47,752 hrs · 47,227 cycles
FOUND STRINGER TO SKIN CORROSION AT RT FS 210 - 227.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 47,752 hrs · 47,227 cycles
STRINGER 30 CRACKED AT STATION 661.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 47,752 hrs · 47,227 cycles
LEFT SLIDING WINDOW LOWER LONGERON FRAME STATION 64 IS CRACKED.
Part: RIB — CRACKED (LT WING) · airframe 47,752 hrs · 47,227 cycles
LEFT WING DRY BAY RIB 2 CRACKED.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 47,752 hrs · 47,227 cycles
LEFT SLIDING WINDOW LONGERON CRACKED.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 47,752 hrs · 47,227 cycles
CORROSION FOUND AROUND RT PRESS VESSEL ELEC PASS THROUGH.
Part: DOUBLER — CORRODED (CARGO DOOR) · airframe 47,752 hrs · 47,227 cycles
FOUND CORROSION ON AFT CARGO DOOR ACTUATOR DOUBLER.
Part: HINGE — CORRODED (FUSELAGE) · airframe 47,752 hrs · 47,227 cycles
FOUND CORROSION ON CARGO DOOR HINGE. REPLACED DOOR HINGE.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 47,752 hrs · 47,227 cycles
REMOVED PREVIOUS REPAIR BETWEEN STRINGERS 18 - 19 DUE TO CORROSION. CLEANED CORROSION, PRIMED, RESEALED & REINSTALLED.
Part: ANGLE — CRACKED (CARGO DOOR) · airframe 47,752 hrs · 47,227 cycles
REPLACED CRACKED CARGO DOOR ACTUATOR MOUNT ANGLES.
Part: STRINGER — CRACKED (RT WING) · airframe 47,752 hrs · 47,227 cycles
RIGHT WING STRINGER IN DRY BAY BETWEEN RIB 0 - 1 CRACKED.
Part: STRINGER — CRACKED (RT WING) · airframe 47,752 hrs · 47,227 cycles
RIGHT WING STRINGER IN DRY BAY BETWEEN RIB 0 - 1 CRACKED.
Part: SKIN — CORRODED (BS 776) · airframe 47,752 hrs · 47,227 cycles
REMOVED PREVIOUS REPAIR BETWEEN STRINGERS 15 - 16 DUE TO CORROSION. CLEANED CORROSION, PRIMED, RESEALED & REINSTALLED.
Earlier reports · 2004–2013 · 5 reports
2013
Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 47,026 hrs · 46,496 cycles
LEFT HORIZONTAL STABILIZER LWR REAR SPAR CORRODED.
Part: REGULATOR — DAMAGED (ZONE 400) · airframe 47,017 hrs · 46,492 cycles
NR 2 ENGINE RPM FLUCTUATION IN FLIGHT. FOUND REGULATOR DAMAGED.
2009
Part: SPAR — CORRODED (HORIZONTAL STAB)
CORROSION ON LT HORIZONTAL STABILIZER REAR SPAR. (K)
2006
Part: CLAMP — FAILED (EXHAUST) · airframe 44,311 hrs · 43,250 cycles
EXHAUST CLAMP FAILURE.
2004
Part: ELEMENT — CHAFED (RT ENGINE)
AFTER DEPARTING SDF CLIMBING THROUGH 8500 FT, NR 2 ENGINE ZONE 2, FIRE INDICATION LIGHT ILLUMINATED. CREW PERFORMED CHECKLISTS (IE PERFORMED ENGINE SHUTDOWN) AS REQUIRED AND RETURNED TO SDF. CREW REPORTED THAT NO VISUAL INDICATIONS OF FIRE, AND AFTER ENGINE COOLED DOWN, FIRE WARNING TEST STILL FAILED. FALSE FIRE WARNING INDICATION SUSPECTED.