# Service difficulty reports: N142FE A list on [N142FE](https://openairdocs.org/aircraft/N142FE.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA202609011258](https://openairdocs.org/sdr/FDEA202609011258.md): Life Vest · missing · Sep 1, 2026 · N142FE · Boeing 767300 · Life Jacket > F/O SEAT MISSING LIFE VEST. IAW AMM 25-64-00 REPLACED LIFE VEST REF 25-60-00. - [SDR FDEA202608201193](https://openairdocs.org/sdr/FDEA202608201193.md): Floor Panel · punctured · Aug 20, 2026 · N142FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 231DFA HAS PUNCTURE DAMAGE. FABRICATED FLOOR PANEL 231DFA (MPN: 143T5876-63) AT STA 412, BETWEEN LBL54.75-LBL77.5. IN REF TO BOEING DRAWING 143T5876-63, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A - [SDR FDEA202608201191](https://openairdocs.org/sdr/FDEA202608201191.md): Floor Panel · punctured · Aug 20, 2026 · N142FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 241JFF HAS PUNCTURE DAMAGE. JM12 REPAIRED MAIN DECK FLOOR PANEL 251HFF, MPN: 145T5876-107 AT STA 933, LBL 54.75-LBL 77.5 IN REF TO B767 SRM 53-00-50-2R REPAIR 4. D. MAJOR REPAIR. SEE JPF FOR ALL WORK PERFORMED. - [SDR FDEA202608191155](https://openairdocs.org/sdr/FDEA202608191155.md): Floor Panel · dented · Aug 19, 2026 · N142FE · Boeing 767300 · Fuselage Floor Panel > 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 - [SDR FDEA202608191153](https://openairdocs.org/sdr/FDEA202608191153.md): Floor Panel · punctured · Aug 19, 2026 · N142FE · Boeing 767300 · Fuselage Floor Panel > 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 - [SDR FDEA202608191152](https://openairdocs.org/sdr/FDEA202608191152.md): Floorboard · punctured · Aug 19, 2026 · N142FE · Boeing 767300 · Fuselage Floor Panel > 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. - [SDR FDEA202608181151](https://openairdocs.org/sdr/FDEA202608181151.md): Floorboard · punctured · Aug 18, 2026 · N142FE · Boeing 767300 · Fuselage Floor Panel > 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. - [SDR FDEA202608171139](https://openairdocs.org/sdr/FDEA202608171139.md): Floor Panel · punctured · Aug 17, 2026 · N142FE · Boeing 7673S2F · Fuselage Floor Panel > 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 I - [SDR FDEA202608171138](https://openairdocs.org/sdr/FDEA202608171138.md): Floor Panel · dented · Aug 17, 2026 · N142FE · Boeing 7673S2F · Fuselage Floor Panel > 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 - [SDR FDEA202608161136](https://openairdocs.org/sdr/FDEA202608161136.md): Floor Panel · dented · Aug 16, 2026 · N142FE · Boeing 7673S2F · Fuselage Floor Panel > 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 ACCOMPL - [SDR FDEA202608141132](https://openairdocs.org/sdr/FDEA202608141132.md): Floor Panel · damaged · Aug 14, 2026 · N142FE · Boeing 7673S2F · Fuselage Floor Panel > 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, THIS IS A REWORK SNRM AND MALFUNCTION CODE SHOULD BE 21. REPAIRED MAIN DECK - [SDR FDEA202608141131](https://openairdocs.org/sdr/FDEA202608141131.md): Floor Panel · damaged · Aug 14, 2026 · N142FE · Boeing 7673S2F · Fuselage Floor Panel > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 252AFF HAS PUNCTURE DAMAGE REPAIR WAS ACCOMPLISHED AND DOCUMENTED AS A MINOR REPAIR IAW GMM 6-2-100, MAJOR REPAIR AND NOT DOCUMENTED OR INSPECTED AS SUCH. NO DAMAGE REMOVAL INSPECTED, NO MATERIAL VERIFICATION, NO - [SDR FDEA202608111108](https://openairdocs.org/sdr/FDEA202608111108.md): Floor Panel · punctured · Aug 11, 2026 · N142FE · Boeing 7673S2F · Fuselage Floor Panel > 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. - [SDR FDEA202608101107](https://openairdocs.org/sdr/FDEA202608101107.md): Floor Panel · punctured · Aug 10, 2026 · N142FE · Boeing 7673S2F · Fuselage Floor Panel > 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. - [SDR FDEA202408251172](https://openairdocs.org/sdr/FDEA202408251172.md): Skin · corroded · Aug 25, 2024 · N142FE · Boeing 7673S2F · Horizontal Stabilizer, Plate/Skin > 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 - [SDR FDEA202404180471](https://openairdocs.org/sdr/FDEA202404180471.md): Tire · leaking · Apr 18, 2024 · N142FE · Boeing 7673S2F · Tire > 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. - [SDR FDEA202206211495](https://openairdocs.org/sdr/FDEA202206211495.md): Former · cracked · Jun 21, 2022 · N142FE · Boeing 767300 · Wing Miscellaneous Structure > 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 - [SDR FDEA202206211494](https://openairdocs.org/sdr/FDEA202206211494.md): Former · cracked · Jun 21, 2022 · N142FE · Boeing 767300 · Wing Miscellaneous Structure > 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 - [SDR FDEA202206211493](https://openairdocs.org/sdr/FDEA202206211493.md): Former · cracked · Jun 21, 2022 · N142FE · Boeing 767300 · Wing Miscellaneous Structure > 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 - [SDR FDEA202204160975](https://openairdocs.org/sdr/FDEA202204160975.md): Unknown · unknown · Apr 16, 2022 · N142FE · Boeing 767300 · Trailing Edge Flap Control System > 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. - [SDR FDEA202008161908](https://openairdocs.org/sdr/FDEA202008161908.md): Former · cracked · Aug 16, 2020 · N142FE · Boeing 7673S2F · Wing Main, Frame Structure > 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.- - [SDR FDEA2020081831880](https://openairdocs.org/sdr/FDEA2020081831880.md): Channel · cracked · Aug 13, 2020 · N142FE · Boeing 7673S2F · Fuselage Miscellaneous Structure > 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" - [SDR FDEA201907151548](https://openairdocs.org/sdr/FDEA201907151548.md): Seal · defective · Jul 15, 2019 · N142FE · Boeing 7673S2F · Flight Compartment Windows > 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. CONTINUE - [SDR FDEA201701250274](https://openairdocs.org/sdr/FDEA201701250274.md): Warning Light · false activation · Jan 25, 2017 · N142FE · Boeing 7673S2F · Trailing Flap Position Indicating System > 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 AN ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N142FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N142FE/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.