# Service difficulty reports: N128FE A list on [N128FE](https://openairdocs.org/aircraft/N128FE.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA202508051370](https://openairdocs.org/sdr/FDEA202508051370.md): Skin · dented · Aug 5, 2025 · N128FE · Boeing 7673S2F · Trailing Edge Flaps > DENT IN LOWER SURFACE AT OTEF STA 232.69 AND 9" OF LEADING EDGE ON LH OUTBOARD FLAP LEADING EDGE ON LH OUTBOARD FLAP WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 REP 1 SHEET 3 REV 92 APR 15.2025 AND SRM 51-70-10-2R REV 92 APR 15.2025 - [SDR FDEA202508041363](https://openairdocs.org/sdr/FDEA202508041363.md): Floor Panel · cracked · Aug 4, 2025 · N128FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL 242TFA AT MDC. FLOOR PANEL 242TFA AT MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIGURE 201 SHEET 2 REV. 92 APR 15, 2025 - [SDR FDEA202508021358](https://openairdocs.org/sdr/FDEA202508021358.md): Skin · dented · Aug 2, 2025 · N128FE · Boeing 7673S2F · Leading Edge Devices > DENT ON EXTERNAL SURFACE OF SLAT NO. 7 AT 3" FROM UPPER EDGE AND 49.5" FROM OUTBOARD EDGE, RIGHT WING RH WING, SLAT NO. 7 AT 3" FROM UPPER EDGE AND 49.5" FROM OUTBOARD EDGE, WAS REPAIRED I.A.W. B767 SRM 57-43-02-02R REP 1 PAG 1-2 AND SRM 51-70-10-2R REPAIR - [SDR FDEA202508011354](https://openairdocs.org/sdr/FDEA202508011354.md): Access Panel · punctured · Aug 1, 2025 · N128FE · Boeing 7673S2F · Fuselage Main, Structure > FLOOR ACCESS PANEL 242 VFF WITH SEVERAL PUNCTURE ON MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 242 VFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR4-B FIG 201 SHEET 2 REV. 92 APR 15,2025 - [SDR FDEA202508011353](https://openairdocs.org/sdr/FDEA202508011353.md): Floor Panel · punctured · Aug 1, 2025 · N128FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL 241AGF AT MDC FLOOR PANEL 241AGF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 92 APR 15,2025 - [SDR FDEA202508011352](https://openairdocs.org/sdr/FDEA202508011352.md): Floor Panel · cracked · Aug 1, 2025 · N128FE · Boeing 7673S2F · Fuselage Floor Panel > CRACKS ON FLOOR PANEL 241WFF FLOOR PANEL 241WFF WAS REPAIRED IAW B767 SRM 53-00-50 2R PAR 4.B FIG 201 SHEET 2 REV.92 APR 15,2025 - [SDR FDEA202508011351](https://openairdocs.org/sdr/FDEA202508011351.md): Floor Panel · punctured · Aug 1, 2025 · N128FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL 242GFF AT MDC FLOOR PANEL 242GFF AT MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIGURE 201 SHEET 2 REV.92 APR 15,2025 - [SDR FDEA202508011350](https://openairdocs.org/sdr/FDEA202508011350.md): Floor Panel · punctured · Aug 1, 2025 · N128FE · Boeing 7673S2F · Fuselage Floor Panel > PUNCTURE ON FLOOR PANEL 251FFF AT MDC FLOOR PANEL 251FFF AT MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR4.B FIGURE 201 SHEET 2 REV. 92 APR 15,2025 - [SDR FDEA202508011348](https://openairdocs.org/sdr/FDEA202508011348.md): Floor Panel · cracked · Aug 1, 2025 · N128FE · Boeing 7673S2F · Fuselage Floor Panel > CRACK ON FLOOR PANEL 251AFF FLOOR PANEL 251AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG.201 (SHEET 2) REV. 92 APR 15,2025 - [SDR FDEA202508011347](https://openairdocs.org/sdr/FDEA202508011347.md): Floor Panel · cracked · Aug 1, 2025 · N128FE · Boeing 7673S2F · Fuselage Floor Panel > CRACKS ON FLOOR PANEL 251QFF FLOOR PANEL 251QFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG.201 (SHEET 2) REV. 92 APR 15,2025 - [SDR FDEA202508011349](https://openairdocs.org/sdr/FDEA202508011349.md): Floor Panel · dented · Aug 1, 2025 · N128FE · Boeing 7673S2F · Fuselage Floor Panel > SEVERAL DENTS ON FLOOR PANEL 251PFF FLOOR PANEL 251PFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG.201 (SHEET 2) REV. 92 APR 15,2025 - [SDR FDEA202312231952](https://openairdocs.org/sdr/FDEA202312231952.md): Brake Assy · making metal · Dec 23, 2023 · N128FE · Boeing 767300 · Landing Gear Brake System > ON WALK AROUND METAL SHAVINGS COMING FROM #5 BRAKE. AMM: 32-11-18-4 COMPLETED INSTALLATION OF LMLG BOGIE BEAM ASSY, IAW AMM 32-11-18-4. PLS SEE W/O 87633, SEQ. 5 FOR ALL WORK ACCOMPLISHED AND PARTS INFORMATION. SERVICABLE MLG BRAKE INSTALLED IN # 5 POSIT - [SDR FDEA202308251492](https://openairdocs.org/sdr/FDEA202308251492.md): Floorbeam · cracked · Aug 25, 2023 · N128FE · Boeing 767300 · Fuselage Main, Floor Beam > 1EA FLOORBEAM ATTACH ANGLE IS CRACKED, INSIDE E&E COMPARTMENT ON LH SIDE AT STA 246, APPROX LBL 44 ON AFT SIDE OF THE FLOORBEAM REMOVED AND REPLACED FLOORBEAM ATTACH ANGLE IAW B767 SRM 51-40-02-0G, BAC DWG 141T5146 REV F, AND BAC DWG 141T5600, SHEET 4, REV - [SDR FDEA202308241490](https://openairdocs.org/sdr/FDEA202308241490.md): Wedge · worn · Aug 24, 2023 · N128FE · Boeing 767300 · Leading Edge Devices > RH WING #8 L/E SLAT, T/E WEDGE, LOWER SURFACE IS WORN JUST OUTBD OF THE INBD AUX TRACK REPAIRED DAMAGE ON THE RH WING #8 SLAT, T/E WEDGE, LOWER SURFACE IAW B767 SRM 57-43- 02-2R AND B767 SRM 51-70-10-2R - [SDR FDEA202308241489](https://openairdocs.org/sdr/FDEA202308241489.md): Wedge · worn · Aug 24, 2023 · N128FE · Boeing 767300 · Leading Edge Devices > RH WING #8 L/E SLAT T/E WEDGE LOWER SURFACE IS WORN JUST OUTBD OF THE OUTBD ROTARY ACTUATOR CONTROL ROD REPAIRED RH WING #8 SLAT, T/E WEDGE IAW B767 SRM 57-43-02-2R AND B767 SRM 51-70-10-2R - [SDR FDEA202308231481](https://openairdocs.org/sdr/FDEA202308231481.md): Slat · worn · Aug 23, 2023 · N128FE · Boeing 767300 · Leading Edge Devices > RH WING #9 L/E SLAT WEDGE LOWER SURFACE IS WORN JUST INBD OF THE INBD ROTARY ACTUATOR TIE ROD. ACCOMPLISHED PERMANENT REPAIR OF RIGHT WING #9 L/E SLAT T/E WEDGE LOWER SURFACE WORN AREA IAW B767 SRM 57-43-02-0I,B767 SRM 51-70-10 AND 57-43-02-2R FIG 201 SHEE - [SDR FDEA202207071694](https://openairdocs.org/sdr/FDEA202207071694.md): Brake · worn · Jul 7, 2022 · N128FE · Boeing 767300 · Landing Gear Brake System > THE INBOARD SURFACE OF THE #4 WHEEL IS TOUCHING OUTBOARD SURFACE OF THE #4 BRAKE ASSEMBLY. EXCESSIVE GAP NOTED BETWEEN #4 BRAKE AND AXLE SLEEVE REMOVED AND REPLACED #4 BRAKE AND TIRE IAW MM REF 32-45-01-4-0, 32-41-08-4-4. - [SDR FDEA202109072235](https://openairdocs.org/sdr/FDEA202109072235.md): Skin · dented · Sep 7, 2021 · N128FE · Boeing 7673S2F · Fuselage Main, Plate/Skin > UPPER FUSELAGE SKIN STA212.5 - STA220.5 S2R-S3R FOUND 1EA DENT. PERFORMED THE REPAIR ON UPPER FUSELAGE SKIN STA212.5 - STA220.5, S2R-S3R PER FEDEX EA #: H-5330-T0363972 P1. TITLE: FUSELAGE - PLATES & SKINS - STA212.5 - STA220.5, RBL15.10 - RBL22.19, DEN - [SDR FDEA2020082642008](https://openairdocs.org/sdr/FDEA2020082642008.md): Attach Angle · cracked · Aug 24, 2020 · N128FE · Boeing 7673S2F · Nacelle/Pylon, Attach Fittings > NR 2 PYLON LT FWD SKIRT BEAM ATTACH ANGLE CRACKED. REMOVED AND REPLACED ATTACH ANGLE PER B767 SRM 51-40-02 AND BAC DWG 313T3310 REV. - [SDR FDEA2020082631996](https://openairdocs.org/sdr/FDEA2020082631996.md): Skin · chafed · Aug 23, 2020 · N128FE · Boeing 7673S2F · Leading Edge Devices > LT WING NR 5 SLAT LOWER TRAILING EDGE WEDGE SKIN CHAFED NUMEROUS SPOTS. REMOVED FINISH AT AREA AS MARKED OF NR 5 SLAT TRAILING EDGE WEDGE. LOWER SKIN, FOUND 1EA AREA OF 4 EA. REQUIRE REPAIR, REPAIRED IAW B767 SRM 57-43-02-1A. REMOVED DAMAGE 1EA AREA AND REPA - [SDR FDEA2020082091936](https://openairdocs.org/sdr/FDEA2020082091936.md): Skin · gouged · Aug 19, 2020 · N128FE · Boeing 7673S2F · Wing Structure > RIGHT WING LE NR 8 SLAT LOWER SURFACE TE HAS GOUGED. REPAIRED THE NR 8 SLAT LOWER SURFACE IAW SRM: 57-42-02-2R, AND 51-70-10-2R, REPAIR 4. MAJOR REPAIR. - [SDR FDEA2020081871909](https://openairdocs.org/sdr/FDEA2020081871909.md): Strap · cracked · Aug 17, 2020 · N128FE · Boeing 7673S2F · Wing Miscellaneous Structure > RIGHT WING L/E CAVITY UPPER SKIN JOINT PLATE CRACKED AT L/E STA. 505. REMOVED AND REPLACED CRACKED SEAL STRAP PER B767 SRM 51-40-02 AND BAC DWG 114T2800 REV. C. - [SDR FDEA202008141881](https://openairdocs.org/sdr/FDEA202008141881.md): Depressor · cracked · Aug 14, 2020 · N128FE · Boeing 7673S2F · Cargo/Baggage Doors > MAIN CARGO DOOR CUTOUT, FWD UPPER SEAL DEPRESSOR DENTED AND GOUGED. AFTER FURTHER EVALUATION FOUND CRACK IN DENT. CHECKED LIMITS FOR DENT AND GOUGE ON SEAL DEPRESSOR AND FOUND CRACK. NO CRACKS ALLOWED PER B767 SRM 53-00-15-1A TABLE A. REMOVED AND REPLACED - [SDR FDEA202001210181](https://openairdocs.org/sdr/FDEA202001210181.md): Warning Light · false activation · Jan 21, 2020 · N128FE · Boeing 7673S2F · Door Warning System > MAIN CARGO DOOR LIGHT ILLUMINATED ON THE EICAS, APPROACHING 370, LIGHT WENT OUT 20-40 MINUTES LATER. - [SDR FDEA201602070487](https://openairdocs.org/sdr/FDEA201602070487.md): Pseu · faulty · Feb 7, 2016 · N128FE · Boeing 7673S2F · Door Warning System > AT FL340, HAS EICAS MSG, MAIN CARGO DOOR. COMPLIED WITH QRH. DESCENT TO 10,000 FT RTB KIND. MAIN DECK CARGO DOOR INDICATION SYS INOPERATIVE. VERIFY & RECORD IN AML & EAML THAT MAIN DECK CARGO DOOR IS CLOSED, LATCHED & LOCKED BEFORE EACH DEPARTURE. ACFT OK - [SDR FDEA201601300403](https://openairdocs.org/sdr/FDEA201601300403.md): Indication Sys · malfunctioned · Jan 30, 2016 · N128FE · Boeing 7673S2F · Door Warning System > EICAS MSG MAIN CARGO DOOR AT FL 340, EXTINGUISHED AT 12000 MSL CABIN ALT OF 9500. RELEASED FOR SERVICE IAW MEL 52-71-01-02 CATEGORY C EXPIRATION 09FEB16. MAIN DECK CARGO DOOR INDICATION SYS INOPERATIVE. VERIFY & RECORD IN AML & EAML THAT MAIN DECK CARGO DO ## 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 = 'N128FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N128FE/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.