# Service difficulty reports: N157FE

A list on [N157FE](https://openairdocs.org/aircraft/N157FE.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR FDEA202510152011](https://openairdocs.org/sdr/FDEA202510152011.md): Wedge · scratched · Oct 15, 2025 · N157FE · Boeing 7673S2F · Leading Edge Devices
  > RIGHT WING SLAT 8 HAS A DEEP SCRATCH ON UNDERSIDE. REPAIRED THE RT WING NR 8 SLAT UPPER T/E WEDGE BOTTOM SURFACE APPROX OSS 425 IAW SRM 57-43-02-2R, PG 1-2 DETAIL 1 & 2, SRM 51-70-10-2R SEE JPF FOR WORK ACCOMPLISHED. MAJOR REPAIR.
- [SDR FDEA202510131976](https://openairdocs.org/sdr/FDEA202510131976.md): Skin · gouged · Oct 13, 2025 · N157FE · Boeing 7673S2F · Leading Edge Devices
  > LEFT WING, #5 SLAT UPPER T/E BOTTOM SURFACE GOUGED APPROXIMATELY L.E.S. 500. REPAIRED LEFT WING #5 SLAT UPPER T/E WEDGE BOTTOM SURFACE APPROXIMATELY L.E.S. 500 IN REF. TO 767 SRM 57-43-02-2R, PG 1-2 DETAIL 1 & 2, 767 SRM 51-70-10-2R THIS IS A MAJOR REPAIR
- [SDR FDEA202510101949](https://openairdocs.org/sdr/FDEA202510101949.md): Floor Panel · dented · Oct 10, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMP AT STA 412 TO 490 & LBL11 TO RBL11 ABOVE FLOORBOARD 241AFF SURFACE SKIN HAS INDENTATION. FABRICATED FLOOR PANEL 231AFF MPN#143T5875-5, LBL 11- RBL 11, STA 412-490 IN REF TO BOEING DWG 143T5875-5. SEE JPF FOR ALL WORK STEPS ACCOMPLISHED. INS
- [SDR FDEA202510091937](https://openairdocs.org/sdr/FDEA202510091937.md): Floor Panel · dented · Oct 9, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMP AT STA 412 TO 490 & LBL11 TO RBL11 ABOVE FLOORBOARD 241AFF SURFACE SKIN HAS INDENTATION. FABRICATED MAIN DECK FLOOR PANEL 231AFF (MPN: 143T5875-5) AT STA 412- STA 490, LBL 11- RBL 11 IN REF TO BOEING DRAWING 143T5875-5.
- [SDR FDEA202510081921](https://openairdocs.org/sdr/FDEA202510081921.md): Floor Panel · dented · Oct 8, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD 241XFF HAS COMPOSITE FIBER DAMAGE CAUSED BY THE SEAL TAPE REMOVAL AND EDGE FILLER MISSING. FABRICATED FLOORPANEL 241XFF MPN# 145T5876-103 LBL 11 - LBL 33 STA 984.95- 1114.82 IN REF TO BOEING DWG 145T5876-103. JEE JPF FOR ALL WORKSTEPS
- [SDR FDEA202510081919](https://openairdocs.org/sdr/FDEA202510081919.md): Floor Panel · dented · Oct 8, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMP AT STA 285 TO 412 & RBL54.75 TO RBL77.5 ABOVE FLOORBOARD 222CFF SURFACE SKIN HAS INDENTATION. FABRICATED NEW FLOOR PANEL 222CFF, MPN: 141T5856-116, RBL 54.75- RBL 77.50, STA 282-412 IN REF. TO BOEING DWG 141T5856-116. SEE JPF FOR ALL THE WO
- [SDR FDEA202510081917](https://openairdocs.org/sdr/FDEA202510081917.md): Floor Panel · damaged · Oct 8, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD 242UFF IS DAMAGED IN SEVERAL AREAS. FABRICATED NEW FLOOR PANEL 242UF, MPN: 145T5876-112, RBL 54.75- RBL 74.25, STA 980- 1114.82 IN REF. TO BOEING DWG 145T5876-112. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATIO
- [SDR FDEA202510081916](https://openairdocs.org/sdr/FDEA202510081916.md): Floor Panel · damaged · Oct 8, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD 242SFF IS DAMAGED AND HAS EDGE FILLER MISSING. FABRICATED NEW FLOOR PANEL 242SFF, MPN: 145T5876-104, RBL 11- RBL 33, STA 2984.95- 1114.82 IN REF. TO BOEING DWG 145T5876-104. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. I
- [SDR FDEA202510081915](https://openairdocs.org/sdr/FDEA202510081915.md): Floor Panel · damaged · Oct 8, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD 242TFA IS DAMAGED AND IS MISSING EDGE FILLER. FABRICATED NEW FLOOR PANEL 242TFA, MPN: 145T5876-96, RBL 33- RBL 54.75, STA 980-1087 IN REF. TO BOEING DWG 145T5876-96. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLAT
- [SDR FDEA202510081914](https://openairdocs.org/sdr/FDEA202510081914.md): Floor Panel · dented · Oct 8, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD 241WFF HAS NUMEROUS DENTS AND EDGE FILLER MISSING. FABRICATED NEW FLOOR PANEL 241WFF, MPN: 145T5876-51, RBL 11- LBL 11, STA 980-1114.82 IN REF. TO BOEING DWG 145T5876-51. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INST
- [SDR FDEA202510081913](https://openairdocs.org/sdr/FDEA202510081913.md): Floor Panel · dented · Oct 8, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMP AT STA 285 TO 412 & LBL33 TO LBL11 ABOVE FLOORBOARD 221DFF SURFACE SKIN HAS INDENTATION. FABRICATED NEW FLOOR PANEL 221DFF, MPN: 141T5856-117, LBL 11- LBL 33, STA 282-412 IN REF. TO BOEING DWG 141T5856-117. SEE JPF FOR ALL THE WORK PERFORME
- [SDR FDEA202510081912](https://openairdocs.org/sdr/FDEA202510081912.md): Floor Panel · dented · Oct 8, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMP AT STA 285 TO 412 & LBL11 TO RBL11 ABOVE FLOORBOARD 221CFF SURFACE SKIN HAS INDENTATION. FABRICATED NEW FLOOR PANEL 221CFF, MPN: 141T5856-105, LBL 11- RBL 11, STA 282-412 IN REF. TO BOEING DWG 141T5856-105. SEE JPF FOR ALL THE WORK PERFORME
- [SDR FDEA202510081911](https://openairdocs.org/sdr/FDEA202510081911.md): Floor Panel · gouged · Oct 8, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD 242VFF IS PUNCTURED AND MISSING EDGE FILLER. FABRICATED NEW FLOOR PANEL 242VFF, MPN: 145T5876-114, RBL 74.25- RBL 86.25, STA 984.95- 1087 IN REF. TO BOEING DWG 145T5876-114. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. I
- [SDR FDEA202510081910](https://openairdocs.org/sdr/FDEA202510081910.md): Floor Panel · gouged · Oct 8, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD 241AGF IS DAMAGED/PUNCTURED. FABRICATED NEW FLOOR PANEL 241AGF, MPN: 145T5876-113, LBL 77.50- RBL 89.50, STA 984.95-1087 IN REF. TO BOEING DWG 145T5876-113. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF TH
- [SDR FDEA202510081909](https://openairdocs.org/sdr/FDEA202510081909.md): Floor Panel · damaged · Oct 8, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD 241XFF HAS COMPOSITE FIBER DAMAGE CAUSED BY THE SEAL TAPE REMOVAL AND EDGE FILLER MISSING. FABRICATED NEW FLOOR PANEL 241XFF, MPN: 145T5876-103, LBL 33- LBL 54.75, STA 984.95- 1114.82 IN REF. TO BOEING DWG 141T5856-107. SEE JPF FOR ALL
- [SDR FDEA202510081908](https://openairdocs.org/sdr/FDEA202510081908.md): Floor Panel · dented · Oct 8, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMP AT STA 285 TO 412 & RBL33 TO RBL54.75 ABOVE FLOORBOARD 222BFF SURFACE SKIN HAS INDENTATION. FABRICATED NEW FLOOR PANEL 222BFF, MPN: 141T5856-106, RBL 33- RBL 54.75, STA 282-412 IN REF. TO BOEING DWG 141T5856-106. SEE JPF FOR ALL THE WORK PE
- [SDR FDEA202510081907](https://openairdocs.org/sdr/FDEA202510081907.md): Floor Panel · dented · Oct 8, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMP AT STA 285 TO 412 & RBL11 TO RBL33 ABOVE FLOORBOARD 222AFF SURFACE SKIN HAS INDENTATION. FABRICATED NEW FLOOR PANEL 222AFF, MPN: 141T5856-107, RBL 11- RBL 33, STA 282-412 IN REF. TO BOEING DWG 141T5856-107. SEE JPF FOR ALL THE WORK PERFORME
- [SDR FDEA202510061899](https://openairdocs.org/sdr/FDEA202510061899.md): Floor Panel · damaged · Oct 6, 2025 · N157FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO DECK FLOORBOARD 242JFF DAMAGED. FABRICATED NEW FLOOR PANEL 242JFF, MPN: 145T5876-102, RBL 11- RBL 33, STA 930 - 984.95 IN REF. TO BOEING DWG 145T5876-102. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PANEL W
- [SDR FDEA202407231047](https://openairdocs.org/sdr/FDEA202407231047.md): Slat System · asymetric · Jul 23, 2024 · N157FE · Boeing 7673S2F · Leading Edge Slat Control System
  > LE SLAT ASYM WHEN SELECTING F25 FROM F20. EMERGENCY DECLARED. FIM: 27_51_00_815_809 CHECKED FSEU LAST FLIGHT FAULTED LE DISAGREE, TE FLAPS AND MSG 27-81045 AMM: 27-81-00-2 PER MOCC AHM REPORTED SLATS & FLAP HANDLE WAS NOT COMPLETELY IN 25 DETENT. PERFOR
- [SDR FDEA202311101849](https://openairdocs.org/sdr/FDEA202311101849.md): Slat · worn · Nov 10, 2023 · N157FE · Boeing 767300 · Leading Edge Devices
  > LH WING, SLAT NO.5, INTERNAL SURFACE, UPPER SIDE, TRAILING EDGE AREA WITH SEVERAL WEAR (3 PLACES). LH WING, SLAT NO 5 INTERNAL SURFACE, UPPER SIDE TRAILING EDGE AREA WERE REPAIRED IAW B767 S.R.M. 57-43-02-2R FIG 201 SHEET 1-2 AND S.R.M. 51-70-10-2R, REPAIR
- [SDR FDEA202311091845](https://openairdocs.org/sdr/FDEA202311091845.md): Slat · worn · Nov 9, 2023 · N157FE · Boeing 767300 · Leading Edge Devices
  > RH WING, SLAT NO 8 SURFACE INNER SIDE AREA UPPER SKIN (NEAR TELESCOPIC DUCT) WITH WEAR. SLAT # 8 WEDGE SKIN WERE REPAIRED LOWER SKIN WITH FLUSH REPAIR DOUBLER AND UPPER SKIN WITH EXTERNAL REPAIR DOUBLER. IAW B767-300 SRM 57-43-02-2R FIG 201 PAG 1-2; SRM 5
- [SDR FDEA202209182340](https://openairdocs.org/sdr/FDEA202209182340.md): Former · cracked · Sep 18, 2022 · N157FE · Boeing 7673S2F · Wing Main, Frame Structure
  > R/H WING FLE FORMER IS CRACKED AT OSS 499.6. COMPLIED WITH E.A. H-5720-T0370673 P1 ON R/H WING FLE FORMER AT OSS-499.6
- [SDR FDEA202204140962](https://openairdocs.org/sdr/FDEA202204140962.md): Former · cracked · Apr 14, 2022 · N157FE · Boeing 767 · Wing Miscellaneous Structure
  > RH WING FORMER CRACKED AT FLE OSS 441 0000392280: BILLMAN, CRAIG B - 15-APR-2022 02:44 REPLACED FORMER AS REQUIRED PER EA H-5720-TO368022 P1.
- [SDR FDEA202201250131](https://openairdocs.org/sdr/FDEA202201250131.md): Angle · cracked · Jan 25, 2022 · N157FE · Boeing 767300 · Wing, Plate/Skin
  > LH WING FIXED LEADING EDGE NOSE FORMED ANGLE BROKEN AT WS 433. NOSE FORMED ANGLE WAS REPLACED FOR NEW ONE, AT LH WING FIXED LEADING EDGE AT WS 433 IAW EA #: H-5720-T0366557 AND SRM 51-10-02-0G PARAGRAPH 9(A) REV. 82 DEC15, 2021
- [SDR FDEA202201250130](https://openairdocs.org/sdr/FDEA202201250130.md): Angle · cracked · Jan 25, 2022 · N157FE · Boeing 767300 · Wing, Plate/Skin
  > RH WING, FIXED LEADING EDGE WITH (2EA) NOSE FORMER ANGLES CRACKED AT L.E.S. 446.10, L.E.S. 500.10. RH WING, FIXED LEADING EDGE (2EA) NOSE FORMER ANGLES AT L.E.S. 446.10, L.E.S. 500.10 WERE REPLACED IAW E.A. #: H-5720-T0366557 AND SRM 51-10-02-0G PARAGRAPH
- [SDR FDEA202201250129](https://openairdocs.org/sdr/FDEA202201250129.md): Angle · cracked · Jan 25, 2022 · N157FE · Boeing 767300 · Wing, Plate/Skin
  > LH WING FIXED LEADING EDGE NOSE FORMED ANGLE BROKEN AT WS 486. ANGLE WAS REPLACED AT LH WING FIXED LEADING EDGE NOSE AT WS 486 IAW E.A. #: H-5720- T0366557 AND SRM 51-10-02-0G PARAGRAPH 9(A) REV.82 DEC 15, 2021
- [SDR FDEA202201240125](https://openairdocs.org/sdr/FDEA202201240125.md): Slat · cracked · Jan 24, 2022 · N157FE · Boeing 767300 · Wing, Control Surfaces
  > RH WING, SLAT #8, TRAILING EDGE WITH WEAR AND CRACK (2EA) RH WING SLAT #8, TRAILING EDGE WAS REPAIRED IAW B767 SRM 57-43-02-2R PAG. 1-2 FIG.201 (SHEET 1) AND SRM 51-70-10-2R REP. 4 PAG. 149, 162, 163 REV.82 15 DEC 21
- [SDR FDEA202112243150](https://openairdocs.org/sdr/FDEA202112243150.md): Manifold · contaminated · Dec 24, 2021 · N157FE · Boeing 7673S2F · Engine (Turbine/Turboprop)
  > GOT BURNING OIL/RUBBER/STEAM ENGINE/FIRECRACKER SMELL ONE MINUTE AFTER PACKS TURNED ON AND ON DESCENT WITH THROTTLES AT IDLE PASSING FL180. PACKS ARE SUPER LOUD- SUSPECT SOME VALVE ISSUE OR LEAKAGE INTO DUCTS. COMPLETED. T/S SYSTEM REF FIM 21-00-21-2 TAS
- [SDR FDEA202112203108](https://openairdocs.org/sdr/FDEA202112203108.md): Engine · leaking · Dec 20, 2021 · N157FE · Boeing 7673S2F · Engine (Turbine/Turboprop)
  > ON DESCENT, PASSING FL180, STARTED GETTING A STRONG BURNING SMELL. DONNED O2 MASKS AND RAN QRC AND QRH. DECLARED AN EMERGENCY, UNEVENTFUL LANDING. CRASH, FIRE AND RESCUE INSPECTED EXTERIOR FOR EVIDENCE OF A FIRE, NONE NOTED. CFR, ALSO INSPECTED INTERIOR OF
- [SDR FDEA2021122103108](https://openairdocs.org/sdr/FDEA2021122103108.md): Unknown · odor · Dec 20, 2021 · N157FE · Boeing 7673S2F · Air Distribution System
  > ON DESCENT, PASSING FL180, STARTED GETTING A STRONG BURNING SMELL. DONNED O2 MASKS AND RAN QRC AND QRH. DECLARED AN EMERGENCY, UNEVENTFUL LANDING. CRASH, FIRE AND RESCUE INSPECTED EXTERIOR FOR EVIDENCE OF A FIRE, NONE NOTED. CFR, ALSO INSPECTED INTERIOR OF
- [SDR FDEA202111082797](https://openairdocs.org/sdr/FDEA202111082797.md): Skin · cracked · Nov 8, 2021 · N157FE · Boeing 767300 · Fuselage Structure (General)
  > PUNCTURE AND DENT DAMAGE ON SKIN PN:148T3211 BETWEEN STA 1582 AND STA 1629 AND S-33L AND S- 35L. REPAIRED SKIN PN:148T3211 PER E.A.#:H-5330-T0365358 DATED: NOV 13, 2021 "TITLE: FUSELAGE - SECTION 48 FUSELAGE SKIN - PERMANENT REPAIR OF IMPACT DAMAGE BETWEEN
- [SDR FDEA2020020430258](https://openairdocs.org/sdr/FDEA2020020430258.md): Skin · delaminated · Feb 3, 2020 · N157FE · Boeing 7673S2F · Leading Edge Devices
  > LW #5 SLAT TE HAS DELAM SPOT REPAIRED LW #5 SLAT T/E IAW B767 SRM 51-70-10-2R AND 57-43-02-2R.
- [SDR FDEA2020020420257](https://openairdocs.org/sdr/FDEA2020020420257.md): Skin · bent · Feb 2, 2020 · N157FE · Boeing 7673S2F · Leading Edge Devices
  > #10 SLAT EXTERIOR UPPER SURFACE INBD AFT END IS BENT UP. REPAIRED #10 SLAT UPPER I/B SURFACE IAW B767 SRM 57-43-02-2R AND 51-70-10-2R.
- [SDR FDEA202001310251](https://openairdocs.org/sdr/FDEA202001310251.md): Bracket · cracked · Jan 31, 2020 · N157FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame
  > LEFT NACELLE RIB AFT OF PANEL 437BL LH BRACKET CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02, AND DWG 313T3380, REV N.
- [SDR FDEA202001310250](https://openairdocs.org/sdr/FDEA202001310250.md): Attach Angle · cracked · Jan 31, 2020 · N157FE · Boeing 7673S2F · Fuselage Main, Attach Fittings
  > NR 2 ENGINE PYLON AFT END INBD ATTACH ANGLE AT THE AFT FRAME WAS CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02 AND DWG 313T3380, REV N.
- [SDR FDEA201907051488](https://openairdocs.org/sdr/FDEA201907051488.md): O-Ring · ruptured · Jul 5, 2019 · N157FE · Boeing 7673S2F · Elevator Control System
  > GOT A "L HYD QTY" EICAS MESSAGE APROXIMATELY 2.5 HOURS INTO FLIGHT. L HYD QTY WAS.46 ON STATUS PAGE WITH RF MAGENTA. ALSO HAD "QTY" LIGHT ON OVERHEAD. HYD QTY.07 ON SHUTDOWN. FLIGHT CREW VERBALLY RELAYED TO ACMX THAT THE LEFT HYDRAULICS NEVER LOST PRESSURE
- [SDR FDEA201810313070](https://openairdocs.org/sdr/FDEA201810313070.md): Plug · loose · Oct 31, 2018 · N157FE · Boeing 7673S2F · Elevator Control System
  > AT CRUISE FL 340 REC'D L HYD QTY EICAS W/ QTY =.41 IN 5 1/2 MINUTES L HYD QTY WENT TO ZERO. IN ANOTHER 4 MIN L HYD PRESS BEGAN TO DROP. COMPLIED W/ QRH (TURNED "ON" L ELEC HYD PUMP) & PRESSURE RECOVERED. NEXT CAME EICAS L HYD PRIM PUMP. SECURED SAME PER Q
- [SDR FDEA2018082982194](https://openairdocs.org/sdr/FDEA2018082982194.md): Warning Message · false indication · Aug 28, 2018 · N157FE · Boeing 7673S2F · Fuel Indicating System
  > AT ROTATION, RECEIVED AN FMC MESSAGE EICAS ADVISORY AND INSUFFICIENT FUEL ON MCDU. NOTICED TOTALIZER ROLLING BACK FROM 22K DOWN TO 16K PASSING 400FT AGL. DECLARED AN EMERGENCY AND LANDED. INSPECTED, AND FOUND NO EVIDENCE OF FUEL LEAK, STUCK TANK AND RE

## 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 = 'N157FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N157FE/reports

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