N262JM
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
26 reports on file, 2017-12-20 – 2018-06-05.
Part: SKIN — CORRODED (BS 870) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
CORROSION FOUND ON THE FUSLAGE SKIN AROUND BS 870, STRINGERS 46 AND 47L.
Part: GATE — CRACKED (R5 DOOR) · airframe 94,239 hrs · 17,325 cycles
R5 DOOR UPPER GATE CRACKED IN 2 PLACES.
Part: SKIN — CORRODED (BS 1350) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
CORROSION ON INTERIOR SIDE OF FUSELAGE SKIN JUST FWD OF FRAME BS 1350 ABOVE STRINGER 14R.
Part: WEB — CRACKED (BS 160) · airframe 94,239 hrs · 17,325 cycles
CRACKED WEB UNDER MAIN DECK FLOORBOARD OTBD OF DADO PANEL BS 160, RT SIDE.
Part: KEELBEAM — CORRODED (BS 998) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
BS 998 RT SIDE OF KEEL BEAM BOX LOWER ANGLE HAS CORROSION, RBL 8.5
Part: KEELBEAM — CORRODED (BS 985) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
KEEL BEAM HAS CORROSION, BS 985, WL 90, LBL 8.5.
Part: SKIN — CORRODED (BS 1475) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
INTERNAL TO FUSELAGE BS 1475, BETWEEN STRINGERS 16L AND 17L SKIN CORRODED.
Part: SIGN — DAMAGED (CABIN) · airframe 94,239 hrs · 17,325 cycles
CENTER EMERGENCY EXIT SIGN HAS A DAMAGED STUD.
Part: MODULE — FAILED · airframe 94,239 hrs · 17,325 cycles
UPPER DECK DOOR EMERGENCY SYSTEMS "LEFT" FAILS TEST (STEP 1B) BATTERY ANNUNCIATOR.
Part: BATTERY PACK — FAILED · airframe 94,239 hrs · 17,325 cycles
UPPER DECK DOOR EMERGENCY SYSTEMS "RIGHT" FAILS TEST (STEP 1B) BATTERY ANNUNCIATOR.
Part: SHEAR TIE — CORRODED (BS 880) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
CORROSION FOUND ON THE BS 880 SHEAR TIE, BETWEEN STRINGERS 45L 46L.
Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
ABOVE THE NR 2 PYLON, UPPER WING L/E SPAR HAS CORROSION ON SPLICE PLATE.
Part: ACCESS PANEL — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
LEFT INBD MID FLAP ACCESS PANEL 577HT CORRODED.
Part: ACCESS PANEL — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
LEFT INBD MID FLAP ACCESS PANEL 577HT CORRODED.
Part: GATE — CORRODED (R5 DOOR) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
R5 DOOR LOWER GATE HAS EVIDENCE OF CORROSION.
Part: GATE — CRACKED (R5 DOOR) · airframe 94,239 hrs · 17,325 cycles
R5 DOOR LOWER GATE HAS EVIDENCE OF CORROSION.
Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
PILOTS FWD INBOARD SEAT TRACK SHOWS CORROSION.
Part: SIGN — INOPERATIVE (CABIN) · airframe 94,239 hrs · 17,325 cycles
UD EXIT SIGN AT STA 690R INOP.
Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
CO-PILOTS AFT INBOARD SEAT TRACK SHOWS CORROSION.
Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
CO-PILOTS FWD INBOARD SEAT TRACK SHOWS CORROSION.
Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
PILOTS AFT INBOARD SEAT TRACK SHOWS CORROSION.
Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
PILOTS FWD OUTBOARD SEAT TRACK SHOWS CORROSION.
Part: SEAT TRACK — CORRODED (COCKPIT) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
CO-PILOTS FWD OUTBOARD SEAT TRACK SHOWS CORROSION.
Earlier reports · 2017 · 3 reports
2017
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
INTERNAL TO FUSELAGE, STATION 1475 BETWEEN STRINGER 17 L AND 18 L ON FUSELAGE SKIN, EVIDENCE OF CORROSION.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
INTERNAL TO FUSELAGE, STATION 1475 BETWEEN STRINGER 16 L AND 17 L ON FUSELAGE SKIN, EVIDENCE OF CORROSION.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,239 hrs · 17,325 cycles
INTERNAL FUSELAGE SKIN, STATION 1475 BELOW STRINGER 15 RIGHT SIDE, EVIDENCE OF CORROSION.