N142FE
Registered owner: FEDERAL EXPRESS CORP, TN (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.
21 reports on file, 2017-01-25 – 2026-08-19.
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 15,459 hrs · 7,196 cycles
MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251PFF HAS PUNCTURE DAMAGE. JM18 REPAIRED MAINDECK CARGO FLOORPANEL 251PFF MPN: 146T5869-169 LBL 54.75 - LBL 77.50 STA 1208-1370 IN REF TO B767 SRM 53_00_50_2R_0 PAR 4.D. SEE JPF FOR ALL WORK ACCOMPLISHED THIS IS A MAJOR REPAIR.
Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 15,459 hrs · 7,196 cycles
MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 231KFF HAS PUNCTURE DAMAGE. FABRICATED NEW FLOOR PANEL 231KFF, MPN 143T5876-64, LBL 77.5 -LBL 86.5 , STATION 544-654 22 IN REF TO BOEING DWG 143T-5876-64. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANEL WILL BE ACCOMPLISHED ON WO# 92696 NR#0136.
Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 15,459 hrs · 7,196 cycles
MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 231PFF HAS PUNCTURE DAMAGE. FABRICATED FLOORBOARD 231PFF (MPN: 143T5876-129) REF BOEING DWG 143T5876-129 AND FEDEX DWG SR67-53-009. SEE JPF FOR WORK STEPS PERFORMED. THIS IS A MAJOR REPAIR.
Part: FLOORBOARD — PUNCTURED (ZONE 200) · airframe 15,459 hrs · 7,196 cycles
MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251KFF HAS PUNCTURE DAMAGE. FABRICATED FLOORBOARD 251KFF (MPN: 146T5869-9) REF BOEING DWG 146T5869-9 AND FEDEX DWG SR67-53-009. SEE JPF FOR WORK STEPS PERFORMED. THIS IS A MAJOR REPAIR.
Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 15,459 hrs · 7,196 cycles
MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 241KFF HAS PUNCTURE DAMAGE. JM15 FABRICATED FLOORPANEL (MPN: 145T5876-89) AT STA 875.9-933.0, BETWEEN LBL 77.5-LBL 77.5 IN REF TO BOEING DRAWING 145T5876-89 AND SR67-53-009 SEE JPF FOR ALL THE WORK PREFORMED. THIS IS A MAJOR REPAIR.
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 15,459 hrs · 7,196 cycles
MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251HFF HAS PUNCTURE DAMAGE. JM17 REPAIRED MAIN DECK FLOOR PANEL 251HFF, MPN: 146T5869-143 AT STA 1197 22- STA 1250, LBL 33- LBL 54.75 IN REF TO B767 SRM 53-00-50-2R REPAIR 4. D. THIS IS A MAJOR REPAIR. SEE JPF FOR ALL WORK PERFORMED.
Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 15,459 hrs · 7,196 cycles
MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251TFF HAS PUNCTURE DAMAGE. JM010 REPAIRED 2" AREA ON MAIN DECK CARGO FLOOR PANEL 251TFF MPN# 146T5869-147 LBL 33- LBL 54.75 STA 1208-1360 IN REF TO B767 SRM 53_00_50_2R_0 PAR 4.D. SEE JPF FOR ALL WORK STEPS ACCOMPLISHED THIS IS A MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 15,459 hrs · 7,196 cycles
MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 252AFF HAS PUNCTURE DAMAGE. THIS REPAIR WAS ACCOMPLISHED AND DOCUMENTED AS A MINOR REPAIR. PER GMM 6-2-100 THIS IS A MAJOR REPAIR AND NOT DOCUMENTED OR INSPECTED AS SUCH. NO DAMAGE REMOVAL INSPECTED, NO MATERIAL VERIFICATION, NO OK TO BOND AS WELL AS THE SRM REFERENCED FIG.201 SHEET 1 IS REPAIR LIMITS AND NOT A REPAIR SCHEME. THIS IS A REWORK SNRM AND SHOULD BE CODED WITH MALFUNCTION CODE 21.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 15,459 hrs · 7,196 cycles
MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 231CFF HAS PUNCTURE DAMAGE. THIS REPAIR WAS ACCOMPLISHED WITH NO DAMAGE REMOVAL INSPECTED, NO MATERIAL VERIFICATION, NO OK TO BOND/INSTALL, QUESTIONABLE WORKMANSHIP AS WELL AS THE SRM REFERENCED FIG.201 SHEET 1 IS REPAIR LIMITS AND NOT A REPAIR SCHEME. THIS IS A REWORK SNRM AND MALFUNCTION CODE SHOULD BE 21.
Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 15,459 hrs · 7,196 cycles
MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251UFF HAS PUNCTURE DAMAGE. FLOOR PANEL REPAIRED IAW SRM 53-00-50-2R, FIG 201, SHEET 1. MAJOR REPAIR.
Part: FLOOR PANEL — PUNCTURED (ZONE 200) · airframe 15,459 hrs · 7,196 cycles
MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 252EFF HAS PUNCTURE DAMAGE. FLOOR PANEL REPAIRED IAW SRM 53-00-50-2R, FIG 201, SHEET 1. MAJOR REPAIR.
Earlier reports · 2017–2024 · 10 reports
2024
Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 12,979 hrs · 6,018 cycles
HORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN AT EXTERNAL SURFACE, CORROSION AT RBL 27 AND 6" FROM FRONT SPAR. HORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN AT EXTERNAL SURFACE, CORROSION AT RBL 27 AND 6" FRON SPAR WAS REPAIRED IAW H-5510-T0380306 P1
Part: TIRE — LEAKING (NLG) · airframe 12,623 hrs · 5,832 cycles
NLG TIRE RH FOUND WITH RETAINING SEAL LOCK MISSING (EXTERNAL) AND GREASE SPREAD AROUND OF WHEEL. REPLACED NLG WHEEL RH IAW AMM. A/C GOOD FOR SERVICE.
2022
Part: FORMER — CRACKED · airframe 10,009 hrs · 4,573 cycles
RIGHT-HAND WING LEADING EDGE FORMER AT STA OSS-441 P/N 114T2170-6 IS CRACKED REPAIRED IN REF TO SRM B767-300 51-40-02-06, SRM B767-300 51-40-03-06. REF. EA H-5720-T0369070
Part: FORMER — CRACKED (ZONE 500) · airframe 10,009 hrs · 4,573 cycles
LEFT-HAND WING LEADING EDGE AT STA OSS441 FORMER P/N 114T2170-5 IS CRACKED. REPAIRED IN REF TO SRM B767-300 51-40-02-06, SRM B767-300 51-40-03-06. REF. EA H-5720-T0369070
Part: FORMER — CRACKED · airframe 10,009 hrs · 4,573 cycles
RIGHT-HAND WING LEADING EDGE AT STA OSS-499 FORMER P/N 114T2511-14 IS CRACKED REPAIRED IN REF TO SRM B767-300 51-40-02-06, SRM B767-300 51-40-03-06. REF. EA H-5720-T0369070
Part: UNKNOWN — UNKNOWN (N/A) · airframe 9,700 hrs · 4,430 cycles
DURING APPROACH RECEIVED A TRAILING EDGE FLAPS DISAGREE EICAS MESSAGE UPON CONFIGURING TO FLAPS 5. DISCONTINUED THE APPROACH AND COMPLIED WITH QRH. RETURNED TO FOR A UNEVENTFUL FLAPS 20 LANDING. ***EMERGENCY DECLARED*** WHILE CYCLING FLAPS/SLAT`S AS PER B767 M/M 27-51-00-2 AND WHILE MONITERING I/O ON F.S.E.U. AS PER F.I.M. 27-51 F.T. 809 FOUND NO FAULT`S WHEN MOVING FLAP`S FLAP LEVER DETENT AND I/O SHOWED SAME BETWEEN FLAP LEVER AND FLAP`S BUT WHILE MOVING FLAP`S SLIGHTLY OUT OF DETENT I/O SHOWED SPLIT BETWEEN FLAP`S AND FLAP LEVER AND CAUSED FAULT ON F.S.E.U. ALSO M.O.C.C. REPORTED SAME ISSUE, CYCLED FLAP`S SEVERAL TIME`S WHILE IN DETENT WITH NO ISSUE`S AND NO FAULT`S ON F.S.E.U. REINSTALLED REMOVED COVER ON SLAT P.D.U. AND INSTALLED REMOVED RIGHT WING SLAT P.D.U. PANEL AS PER B767 M/M 27-81-10-4, CONFERANCE CALL CONDUCTED WITH M.O.C.C., O.K. FOR SERVICE.
2020
Part: FORMER — CRACKED (RT WING) · airframe 6,730 hrs · 2,992 cycles
R/H WING L/E FORMER FWD OF #8 O/B ROTARY ACTUATOR IS CRACKED. REMOVED AND REPLACED CRACKED FORMER PER B767 SRM 51-40-02 AND BAC DWG 114T2162 REV.-
Part: CHANNEL — CRACKED (BS 492) · airframe 7,018 hrs · 3,031 cycles
MCD CUTOUT FWD EDGE INTERNAL CLOSE OUT TRIM IS CRACKED AND GOUGED. COMPLIED WITH EA H-5320-T0355840 P1 DATED 8-10-20 TITLED " FUSELAGE-AUXILIARY STRUCTURE-MAIN CARGO DOOR-FWD. U CHANNEL, GOUGE DAMAGE -PERMANENT REPAIR"
2019
Part: SEAL — DEFECTIVE (COCKPIT) · airframe 4,907 hrs · 2,122 cycles
UPON CLIMBING THROUGH FL 250 A LOUD SQUEEL STARTED AND CONTINUED THROUGH FL 370. PRESSURIZATION SEEMED NORMAL: DIFF 7.9, CABIN ALT 5900! NOT SURE WHICH SEAL ON WHICH WAS BAD. TOO LOUD TO CONTINUE FLIGHT. UPON DISCENDING THROUGH FL 250 SQUEEL STOPPED. CONTINUED TO LANDING SAFELY.
2017
Part: WARNING LIGHT — FALSE ACTIVATION (TE FLAPS) · airframe 317 hrs · 143 cycles
ON LANDING, GEAR DOWN AND FLAPS 20. WHEN FLAP HANDLE WAS MOVED TO FLAPS 25, RECEIVED A TE FLAPS DISAGREE EICAS AND AMBER TRAILING EDGE DISCREET LIGHT. EXECUTED A GO AROUND, FOLLOWED QRH AND LANDED. WHEN GEAR WAS EXTENDED ON SECOND APPROACH EICAS CLEARED AND FLAPS EXTENDED TO 25. REMOVED AND REPLACED THE NR 1 RVDT ON OUTBOARD SLAT PDU IAW AMM 27-81-11-4, FLAPS AND SLATS CHECKED GOOD IAW AMM 27-51-00-5-0 AND 27-81-00-5-0, OK FOR SERVICE.