# Service difficulty reports: N156FE

A list on [N156FE](https://openairdocs.org/aircraft/N156FE.md).

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

- [SDR FDEA202605020532](https://openairdocs.org/sdr/FDEA202605020532.md): Apu · faulted · May 2, 2026 · N156FE · Boeing 7673S2F · Airborne Auxiliary Power Unit (APU) System
  > WHEN I TRIED TO SWITCH FROM EXTERNAL POWER TO APU POWER, THE APU WOULDN T HOLD THE LOAD. EVERYTHING IN THE COCKPIT FLICKERED WITH AUDIBLE CLICKING AND GRINDING SOUNDS AND THERE WAS A STRONG ELECTRICAL BURNING ODOR. SWITCHED BACK TO EXTERNAL POWER AND THE
- [SDR FDEA202510312119](https://openairdocs.org/sdr/FDEA202510312119.md): Skin · delaminated · Oct 31, 2025 · N156FE · Boeing 7673S2F · Trailing Edge Flaps
  > DELAMINATION IN LEADING EDGE 8 INCHES FROM THE RIGHT SIDE FACE, OUTBOARD FLAP, LEFT WING LEFT, WING OUTBOARD FLAP LEADING EDGE, 8 INCHES FROM THE RIGHT SIDE FACE WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIG. 201 SHEET 5 TABLE I AND B767 SRM 51-70-03-
- [SDR FDEA202510312118](https://openairdocs.org/sdr/FDEA202510312118.md): Floor Panel · damaged · Oct 31, 2025 · N156FE · Boeing 7673S2F · Fuselage Floor Panel
  > DEGRADED PREVIOUS REWORK ON MAIN DECK FLOOR ACCESS PANEL 222 AFF. FLOOR PANEL 222 AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV. 93 AUG 15,2025
- [SDR FDEA202510292114](https://openairdocs.org/sdr/FDEA202510292114.md): Floor Panel · dented · Oct 29, 2025 · N156FE · Boeing 7673S2F · Fuselage Floor Panel
  > DENT ON FLOOR PANEL (241 AGF) ON MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 241AGF ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50- 2R PAR 4.B FIG. 201 SHEET 2 REV. 93 AUG 15, 2025
- [SDR FDEA202510292113](https://openairdocs.org/sdr/FDEA202510292113.md): Floor Panel · punctured · Oct 29, 2025 · N156FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL (251 PFF) ON MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 251PFF ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50- 2R PAR 4-B FIG.201 SHEET 2 REV.93 AUG 15,2025
- [SDR FDEA202510292112](https://openairdocs.org/sdr/FDEA202510292112.md): Floor Panel · dented · Oct 29, 2025 · N156FE · Boeing 7673S2F · Fuselage Floor Panel
  > SEVERAL DENTS ON FLOOR PANEL (251UFF) ON MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 251 UFF ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50- 2R PAR 4-B FIG. 201 SHEET 2 REV.93 AUG 15,2025
- [SDR FDEA202510292111](https://openairdocs.org/sdr/FDEA202510292111.md): Floor Panel · punctured · Oct 29, 2025 · N156FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURES ON FLOOR PANEL (241DFF) ON MAIN DECK CARGO COMPARTMENT. FLOOR PANEL 241DFF ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW SRM 53-00-50- 2R PAR.4.B FIG.201 SHEET 2 REV. 93 AUG. 15, 2025
- [SDR FDEA202510272100](https://openairdocs.org/sdr/FDEA202510272100.md): Floor Panel · dented · Oct 27, 2025 · N156FE · Boeing 7673S2F · Fuselage Floor Panel
  > DENT ON FLOOR PANEL (252 JFF)ON MAIN DECK CARGO COMPARTMENT. FLOOR PANEL (252JFF) ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR 4-B FIG.201 SHEET 2 REV 93 AUG, 15,2025.
- [SDR FDEA202510272099](https://openairdocs.org/sdr/FDEA202510272099.md): Floor Panel · punctured · Oct 27, 2025 · N156FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL (252HFF) ON MAIN DECK CARGO COMPARTMENT FLOOR PANEL (252 HFF) ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR4-B FIG 201 SHEET 2 REV 93. AUG 15,2025
- [SDR FDEA202510272098](https://openairdocs.org/sdr/FDEA202510272098.md): Floor Panel · punctured · Oct 27, 2025 · N156FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL (251 SFF) ON MAIN DECK CARGO COMPARTMENT FLOOR PANEL (251 SFF) ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR 4-B FIG 201 SHEET 2 REV.93 AUG 15,2025.
- [SDR FDEA202510272097](https://openairdocs.org/sdr/FDEA202510272097.md): Floor Panel · punctured · Oct 27, 2025 · N156FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL (251QFF) ON MAIN DECK CARGO COMPARTMENT FLOOR PANEL (251 QFF) ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR 4-B FIG.201 SHEET 2 REV.93 AUG 15,2025.
- [SDR FDEA202510272096](https://openairdocs.org/sdr/FDEA202510272096.md): Floor Panel · punctured · Oct 27, 2025 · N156FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL (252SFF) ON MAIN DECK CARGO COMPARTMENT. FLOOR PANEL (252SFF) ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15,2025.
- [SDR FDEA202405220718](https://openairdocs.org/sdr/FDEA202405220718.md): Wedge · dented · May 22, 2024 · N156FE · Boeing 7673S2F · Leading Edge Devices
  > LH WING #3 SLAT TRALING EDGE WEDGE TOP SURFACE HAS A (3.5 INCH) DENT AT WING STATION 750. REPAIRED LH WING L/E # 3 SLAT TRAINLING EDGE WEDGE AT WS OSS 750 IN REF TO 767 SRM 57- 43-02-2R, PG 1-2 DETAIL I & III, FIG.201 SHEETS 1 & 2, AND 767 SRM 51-70-10-2R.
- [SDR FDEA202401310126](https://openairdocs.org/sdr/FDEA202401310126.md): Skin · cracked · Jan 31, 2024 · N156FE · Boeing 7673S2F · Elevator, Plate/Skin
  > LH OUTBOARD ELEVATOR LOWER SKIN WITH HOLE AT 42" FROM ELEVATOR EDGE INTERIOR AND 10" FROM L.E. LH OUTBOARD ELEVATOR LOWER SKIN AT 42" FROM ELEVATOR EDGE INTERIOR AND 10" FROM L.E. WAS REPAIRED IAW E.A. #: H-5520-T0377675 RELEASE DATE: JAN 30,24
- [SDR FDEA202401240108](https://openairdocs.org/sdr/FDEA202401240108.md): Skin · worn · Jan 24, 2024 · N156FE · Boeing 7673S2F · Leading Edge Devices
  > LH WING SLAT 5 TRAILING EDGE WEDGE WITH WEAR MARK OSS 44160 LH WING SLAT 5 TRAILING EDGE WEDGE AT OSS 441.60 WAS REPAIRED IAW B767 SRM 57-43--02-2R FIG 201 SHEET 1-2 AND SRM 51-70-10-2R REP 4 FIG 202 SHEET 8 PAGE 150,163,164. REV 88 DEC 15/2023
- [SDR FDEA202401120072](https://openairdocs.org/sdr/FDEA202401120072.md): Skin · delaminated · Jan 12, 2024 · N156FE · Boeing 7673S2F · Trailing Edge Flaps
  > LH WING OUTBOARD FLAP LEADING EDGE WITH DELAMINATION AT OTEF STA 72 LH WING OUTBOARD FLAP LEADING EDGE AT OTEF STA 72 WAS REPAIRED IAW B767 SRM 57-53-01- 2R REP 1 FIG 201 SHEET 1-3-5-6 PAGE 1-6 AND SRM 51-70-03-0G PAR 5A FIG 5 PAGE 19-36. REV 88 DEC 15/ 202
- [SDR FDEA202301290174](https://openairdocs.org/sdr/FDEA202301290174.md): Valve · malfunctioned · Jan 29, 2023 · N156FE · Boeing 7673S2F · Aircraft Fuel Distribution System
  > POSSIBLE FUEL LEAK ASSOCIATED WITH THE LEFT TANK AND ENGINE, LEFT SIDE DROPPED AN EXTRA 1000 LBS EVERY 10 MINS. AFTER 30 MINS OF FLT, WERE 3500 POUNDS SHORT ON FUEL AT TINGS INTERSECTION. ENGINE FUEL BURNS WERE NORMAL AND EVEN. ACFT ARRIVAL W/ NO VISUAL EXTERN
- [SDR FDEA202208212014](https://openairdocs.org/sdr/FDEA202208212014.md): Former · cracked · Aug 21, 2022 · N156FE · Boeing 7673S2F · Leading Edge Devices
  > FLE FORMER NEAR OSS 441 (UNDER #8 SLAT) APPEARS TO BE CRACKING IN BEND. 0000452710: ROSNER, DANIEL D - 21-AUG-2022 23:25 COMPLIED WITH EA TH-5720-T0370212P1 RIGHT WING FIXED LEADING EDGE OSS 441, REF THIS E.A AND B767 SRM 51-40-02-0G
- [SDR FDEA202201140066](https://openairdocs.org/sdr/FDEA202201140066.md): Skin · none · Jan 14, 2022 · N156FE · Boeing 767300 · Wing Structure
  > LEFT WING #6 SPOILER LOWER SKIN HAS A PUNCTURE REPAIRED LEFT WING #6 SPOILER LOWER SKIN IAW B767 SRM 57-70-01 FIG. 201 SHEET 4 AND 51-70-04-0G
- [SDR FDEA202201130060](https://openairdocs.org/sdr/FDEA202201130060.md): Bracket · cracked · Jan 13, 2022 · N156FE · Boeing 767300 · Nacelle/Pylon, Main Frame
  > #1 PYLON, OUTBD LATCH BEAM ASSY HAS A CRACKED DRAIN LINE SUPPORT BRACKET REMOVED & REPLACED BRACKET IAW BAC DWG 313T2380, SHEET 198, REV - & PL REV A
- [SDR FDEA202201120057](https://openairdocs.org/sdr/FDEA202201120057.md): Former · cracked · Jan 12, 2022 · N156FE · Boeing 767300 · Wing Miscellaneous Structure
  > RIGHT WING LEADING EDGE UPPER SURFACE LES 560 HAS A POPPED RIVET HEAD REMOVED AND REPLACED THE CRACKED R/W L/E NOSE FORMER AT LES 560, OSS 565, IAW BAC DWG 114T2162, REV. -. REMOVED AND REINSTALLED THE NOSE FORMER ATTACH ANGLE IAW FEDEX EA H-5720- T0366360-
- [SDR FDEA202201120058](https://openairdocs.org/sdr/FDEA202201120058.md): Bracket · cracked · Jan 12, 2022 · N156FE · Boeing 767300 · Wing Miscellaneous Structure
  > L/W L/E NOSE FORMER ATTACH BRACKET AT OSS 441.6 IS CRACKED REMOVED AND REPLACED THE R/W L/E NOSE FORMER ATTACH BRACKET AT OSS 441.6 IAW FEDEX EA H-5720- T0366352-P1, DATE: 11JAN2022, TITLE: WINGS - SECONDARY WING STRCT - LH WING, LEADING EDGE, ANGLE, OSS 44
- [SDR FDEA202201120056](https://openairdocs.org/sdr/FDEA202201120056.md): Former · cracked · Jan 12, 2022 · N156FE · Boeing 767300 · Wing Miscellaneous Structure
  > RIGHT WING LEADING EDGE AT LES480 SLAT TRACK CLOSE OUT CURTAIN OUTBOARD FITTING RIVETS PULLED LOOSE FROM LEADING EDGE REMOVED AND REPLACED THE R/W L/E NOSE FORMER FOR THE LES480 SLAT TRACK CLOSE OUT CURTAIN IAW BAC DWG 114T2161, REV. -. REMOVED AND REINSTA
- [SDR FDEA202201120055](https://openairdocs.org/sdr/FDEA202201120055.md): Shear Tie · cracked · Jan 12, 2022 · N156FE · Boeing 767300 · Nacelle/Pylon, Main Frame
  > @1 PYLON, NAC STA 303, INBD SKIRT BEAM ATTACHMENT SHEAR TIE IS CRACKED REMOVED & REPLACED SHEAR TIE IAW BAC DWG 313T2310 SHEET 95, REV -
- [SDR FDEA202201120054](https://openairdocs.org/sdr/FDEA202201120054.md): Bracket · cracked · Jan 12, 2022 · N156FE · Boeing 767300 · Nacelle/Pylon, Main Frame
  > #1 PYLON, OUTBD SIDE, NAC STA 377 FRAME SUPPORT BRACKET IS CRACKED REMOVED & REPLACED BRACKET IAW B767 SRM 51-40-02. ALL PARTS VERIFED PER B767 AIPC 54-53-02
- [SDR FDEA202201120053](https://openairdocs.org/sdr/FDEA202201120053.md): Bracket · cracked · Jan 12, 2022 · N156FE · Boeing 767300 · Nacelle/Pylon, Main Frame
  > #1 PYLON, INBD SIDE, NAC STA 377, FRAME ATTACH BRACKET IS CRACKED REMOVED & REPLACED BRACKET IAW B767 SRM 51-40-02, ALL PARTS VERIFED PER B767 AIPC 54-53-02.
- [SDR FDEA202201110045](https://openairdocs.org/sdr/FDEA202201110045.md): Floor Panel · damaged · Jan 11, 2022 · N156FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 241AGF IS DENTED IN SEVERAL AREAS ON UPPER SURFACE FABRICATED NEW FLOOR PANEL IAW FEDEX DRAWING SRZ-25-005
- [SDR FDEA202201110046](https://openairdocs.org/sdr/FDEA202201110046.md): Floor Panel · damaged · Jan 11, 2022 · N156FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 241ZFF IS DENTED ON UPPER SURFACE REPAIRED DENTED FLOOR PANEL IAW B767 SRM 53-00-50-2R PARAGRAPH 4.D
- [SDR FDEA202109112289](https://openairdocs.org/sdr/FDEA202109112289.md): Packing · leaking · Sep 11, 2021 · N156FE · Boeing 7673S2F · Hydraulic System, Main
  > L HYD QTY ZERO IN FLIGHT. HAD A SLOW LEAK AT CRUISE THAT TOOK ABOUT 50 MINUTES TO REACH ZERO. SUBSEQUENTLY WE GOT L HYD SYS PRESS. COMPLIED WITH QRH AND SHUT DOWN LH SYSTEM. FOUND VERTICLE STAB HYD MANIFOLD TO BE LEAKING FROM UNION ITEM 45 IN A/C IPC 27-21-
- [SDR FDEA202102060297](https://openairdocs.org/sdr/FDEA202102060297.md): Actuator · leaking · Feb 6, 2021 · N156FE · Boeing 7673S2F · Drag Control System
  > MULTIPLE HYD EICAS MSGS. FIRST, C HYD QTY FOLLOWED BY C HYD PRIM 2. THEN HYD SYS PRESS ALTN FLAPS AND GEAR EXTENSION PER QRH. #9 SPOILER ACTUATOR LEAKING. CENTER HYD SYSTEM SHOWS EMPTY. INSTALLED #9 SPOILER PCA REF 767 AMM 27-61-02-4.
- [SDR FDEA2020071311486](https://openairdocs.org/sdr/FDEA2020071311486.md): Smoke Detector · false activation · Jul 11, 2020 · N156FE · Boeing 7673S2F · Smoke Detection
  > LAV SMOKE DETECTION SOUNDED ALARM INFLIGHT. NO VISUAL INDICATION OF SMOKE, VERIFIED BY MX JUMPSEATERS. ALARM SOUNDED FOUR TIMES IN ABOUT TWO MINUTES. PERFORM OPERATIONAL TEST REF AMM 26-13-00-5. OPS TEST GOOD.
- [SDR FDEA2020062541331](https://openairdocs.org/sdr/FDEA2020062541331.md): Tire · failed · Jun 24, 2020 · N156FE · Boeing 7673S2F · Tire
  > AFTER LANDING ALL BRAKE TEMPS ON RT LANDING GEAR AT LEVEL 9. AFTER APPROX 20 MINUTES THERMAL PLUG ON NR 4 TIRE BLEW. PER AMM 05-51-14-2-0 MINIMUM 75 MINUTE BRAKE COOLING AND HIGH ENERGY STOP INSPECTION REQUIRED. REMOVED AND REPLACED NR 4 WHEEL A TIRE ASSY P
- [SDR FDEA2020061641231](https://openairdocs.org/sdr/FDEA2020061641231.md): Squib · disconnected · Jun 14, 2020 · N156FE · Boeing 7673S2F · Fire Bottle, Fixed
  > SQUIB TEST 1 FAILS "1 CARGO". LIGHT DOES NOT COME ON. TEST 2 AND LAMP TEST NORMAL. FOUND SQUIB C/P D1440 ON FWD 1 CARGO FIRE BOTTLE COMPLETELY DISCONNECTED AND ADRIFT. INSPECTED SAME, FOUND SERVICEABLE AND RESECURED REF AMM 26-23-02-4. SQUIB TEST NORMAL.
- [SDR FDEA201909052109](https://openairdocs.org/sdr/FDEA201909052109.md): Warning System · false activation · Sep 5, 2019 · N156FE · Boeing 7673S2F · Leading Edge Slat Position Indicating System
  > INFO ONLY: EXPERIENCED SLAT DISAGREE DURING APPROACH FROM FLAPS 20 TO 25. WENT AROUND DISAGREE DISAPPEARED WHEN FLAPS TRANSITED TO 20. INFO NOTED. CHECKED FSEU FOR FAULTS, NONE FOUND. PERFORMED OPS CHECK OF FLAPS AND SLATS, OPS CHECK GOOD REF AMM 27-51-00-5.

## 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 = 'N156FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N156FE/reports

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