# Service difficulty reports: N147FE

A list on [N147FE](https://openairdocs.org/aircraft/N147FE.md).

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

- [SDR FDEA202610151594](https://openairdocs.org/sdr/FDEA202610151594.md): Floor Panel · punctured · Oct 15, 2026 · N147FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 252EFF HAS PUNCTURE DAMAGE. FABRICATED FLOORBOARD 252EFF IAW DWG 146T5869-155, AND DWG SR67-53-009. THIS IS A MAJOR REPAIR.
- [SDR FDEA202610151586](https://openairdocs.org/sdr/FDEA202610151586.md): Floorboard · punctured · Oct 15, 2026 · N147FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 232KFF HAS PUNCTURE DAMAGE. DB04 REPAIRED FLOOR PANEL 232KFF, RBL 11 - RBL 33, BS 654 22 - 680 IAW SRM 53-00-50-2R. SEE JPF FOR WORK ACCOMPLISHED. THIS IS A MAJOR REPAIR.
- [SDR FDEA202610131563](https://openairdocs.org/sdr/FDEA202610131563.md): Floor Panel · dented · Oct 13, 2026 · N147FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 251PFF HAS PUNCTURE DAMAGE. DB03 FABRICATED MAIN DECK FLOORPANEL# 251PFF PN# 146T5869-169 LBL 54.75 - LBL 77.50, STA 1208- 1360 REF BOEING DRAWING 146T5869-169. SEE JPF FOR ALL WORK ACCOMPLISHED. THIS IS A MAJOR REPAIR.
- [SDR FDEA202610131561](https://openairdocs.org/sdr/FDEA202610131561.md): Floor Panel · damaged · Oct 13, 2026 · N147FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 231QFF HAS PUNCTURE DAMAGE. DB01 REPAIRED MAIN DECK CARGO COMPARTMENT FLOORBOARD PANEL 231QFF P/N 143T5876-19 AT STA 654 22 -784, RBL 77.5 - RBL 86.5 PER SRM 53-00-50-2R FIG 201. SEE JPF FOR OTHER WORK ACCOMPLISHED.THIS IS A MAJOR REP
- [SDR FDEA202610131560](https://openairdocs.org/sdr/FDEA202610131560.md): Floor Panel · damaged · Oct 13, 2026 · N147FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 242TFA HAS PUNCTURE DAMAGE. DB08 REPAIRED MAIN DECK CARGO COMPARTMENT FLOOR PANEL 242TFA, P/N 145T5876-96 AT STA 984.95 TO STA 1087, RBL 54.75 TO RBL 74.25 IN REF TO B767 SRM 53-00-50-2R. SEE JPF FOR OTHER WORK ACCOMPLISHED. THIS IS A
- [SDR FDEA202610111556](https://openairdocs.org/sdr/FDEA202610111556.md): Skin · dented · Oct 11, 2026 · N147FE · Boeing 767300 · Leading Edge Devices
  > RIGHT NR 12 SLAT DENTED ON THE UPPER SURFACE OF THE TRAILING EDGE WEDGE 62 FROM THE INBD END. MWT. REPAIRED 2.7" X 2.7" AREA OF DAMAGED TOPSKIN ON UPPER SURFACE OF R/H WING #12 SLAT TE WEDGE PN# 114T4101-68G SERIAL NO# 000331 AT OSS 1045 AND RESTORED TOPC
- [SDR FDEA202610111555](https://openairdocs.org/sdr/FDEA202610111555.md): Floor Panel · punctured · Oct 11, 2026 · N147FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 232NFF HAS PUNCTURE DAMAGE. REPAIRED MAIN DECK CARGO COMPARTMENT FLOORBOARD PANEL 232NFF P/N 143T5876-20 AT STA 731.72-732.72 RBL 79.5 - RBL 80.5 PER SRM 53-00-50-2R FIG 201. SEE JPF FOR OTHER WORK ACCOMPLISHED.THIS IS A MAJOR REPAIR
- [SDR FDEA202610111554](https://openairdocs.org/sdr/FDEA202610111554.md): Floor Panel · punctured · Oct 11, 2026 · N147FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 251KFF HAS PUNCTURE DAMAGE. DB02 FABRICATED FLOOR PANEL 251KFF (MPN: 146T5869-9) AT STA 1197 13- 1210, BETWEEN LBL77.5- LBL88.5 IN REF TO BOEING DRAWING 146T5869-9, AND SR67-53-009. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR R
- [SDR FDEA202610091543](https://openairdocs.org/sdr/FDEA202610091543.md): Floor Panel · punctured · Oct 9, 2026 · N147FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 242HFF HAS PUNCTURE DAMAGE. REPAIRED MAIN DECK CARGO COMPARTMENT FLOORBOARD PANEL #242HFF P/N 145T5876-14 AT STA 885.90-889.90 TO RBL 74.25-76.25 PER B767 SRM 53-00-50-2R,FIG 201,SHEET 1.SEE ON JPF FOR OTHER WORK ACCOMPLISHED.THIS IS
- [SDR FDEA202410041421](https://openairdocs.org/sdr/FDEA202410041421.md): Skin · cracked · Oct 4, 2024 · N147FE · Boeing 7673S2F · Fuselage Main, Plate/Skin
  > ACCIDENTAL DAMAGE BY FOD AT LH FUSELAGE STA 1175, BETWEEN STGR 10-11, REPAIR AS REQUIRED ACCIDENTAL DAMAGE BY FOD AT LH FUSELAGE STA 1175, BETWEEN STGR 10-11 WAS REPAIRED IAW E.A.#: H-5330-T0380846 AND SRM 53-00-01-2R REPAIR 29 FIGURE 201 SHEET 1-12 TABLE
- [SDR FDEA202409281391](https://openairdocs.org/sdr/FDEA202409281391.md): Skin · dented · Sep 28, 2024 · N147FE · Boeing 7673S2F · Trailing Edge Flaps
  > LEFT WING OUTBOARD UPPER FLAP LEADING EDGE WITH A DENT AT 12 IN. OF THE TRAILING EDGE. LEFT WING OUTBOARD UPPER FLAP LEADING EDGE AT 12" OF T/E PANEL 556AT WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 FIG 201 (SHEET 5) TABLE I AND SRM 51-70-17-0G PAR 4.H FI
- [SDR FDEA202409281390](https://openairdocs.org/sdr/FDEA202409281390.md): Skin · dented · Sep 28, 2024 · N147FE · Boeing 7673S2F · Trailing Edge Flaps
  > RH WING, AFT INBOARD FLAP, LOWER SKIN SURFACE, WITH DENT AT IFS 137.25, AND 12'' FROM LEADING EDGE. RH WING, AFT INBOARD FLAP, LOWER SKIN SURFACE AT IFS 137.25, AND 12'' FROM L/E WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 FIG.201 ( SHEET 4) NOTE A AND SR
- [SDR FDEA202409281389](https://openairdocs.org/sdr/FDEA202409281389.md): Floor Panel · dented · Sep 28, 2024 · N147FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO, FLOOR PANEL 231JFF WITH DENTS. MAIN DECK CARGO, FLOOR PANEL 231JFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202409281388](https://openairdocs.org/sdr/FDEA202409281388.md): Skin · dented · Sep 28, 2024 · N147FE · Boeing 7673S2F · Trailing Edge Flaps
  > LEFT WING AFTER INBOARD FLAP UPPER SKIN WITH A DENT AT 3 IN. FORWARD OF THE TRAILING EDGE AND 18 IN. OF THE INBOARD EDGE LEFT WING AFTER INBOARD FLAP UPPER SKIN AT 3 IN FORWARD OF T/E AND 18 IN OF THE INBOARD EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R REP
- [SDR FDEA202409281387](https://openairdocs.org/sdr/FDEA202409281387.md): Floor Panel · delaminated · Sep 28, 2024 · N147FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 242VFF WITH PREVIOUS REPAIR DAMAGE MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 242VFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4.B FIG 201 SHEET 2 REV 90 AUG 15/2024
- [SDR FDEA202308311532](https://openairdocs.org/sdr/FDEA202308311532.md): Floor Panel · gouged · Aug 31, 2023 · N147FE · Boeing 767300 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL DAMAGED AT STA. 1137 AND 3 INCHES LEFT OF CENTER. REF WRI 25-50 5384 AND SEQ 150 OF WORK ORDER 86663. FABRICATED AND INSTALLED NEW FLOOR PANEL. REF SRZ -25-005 REV. R AND B767 AMM 53-01-06-4. ALSO SEE WRI # 25-50/5384 AND SEQ
- [SDR FDEA202208182000](https://openairdocs.org/sdr/FDEA202208182000.md): Former · cracked · Aug 18, 2022 · N147FE · Boeing 767300 · Wing Main, Frame Structure
  > L/E EDGE FORMER CRACKED AT STATION 441 R/H WING MARKED WITH TAPE. REPLACED FORMER AS REQUIRED PER EA H-5720-T0370175.
- [SDR FDEA202208181999](https://openairdocs.org/sdr/FDEA202208181999.md): Former · cracked · Aug 18, 2022 · N147FE · Boeing 767300 · Wing Main, Frame Structure
  > L/E EDGE FORMER CRACKED AT STATION 499 R/H WING MARKED WITH TAPE 0000493008: CRAIL, ROGER L - 19-AUG-2022 01:16 REPLACED FORMER AS REQUIRED. REF E.A TH-5720-T0370175 P1
- [SDR FDEA202107131764](https://openairdocs.org/sdr/FDEA202107131764.md): Sensor · inoperative · Jul 13, 2021 · N147FE · Boeing 7673S2F · Leading Edge Slat Position Indicating System
  > AFTER NORMAL TAKEOFF AND COMPLETING AFTER TAKEOFF CHECKLIST WE WERE CLIMBING THROUGH 11,000' WHEN WE RECEIVED A CAUTION AND LE FLAP DISAGREE EICAS MESSAGE WITH BOTH FLAP INDICATORS SHOWING BETWEEN UP AND 1. A FEW TIMES THEY MOMENTARILY RETURN TO UP BUT THEN
- [SDR FDEA202010192561](https://openairdocs.org/sdr/FDEA202010192561.md): Shear Tie · cracked · Oct 19, 2020 · N147FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame
  > NR 2 PYLON INBOARD WING FITTING CLIP IS CRACKED ON FWD END. REMOVED AND REPLACED SHEAR TIE P/N 313T3310-1156, IAW BAC DWG 313T2310 REV AND B767 SRM 51-40-02.
- [SDR FDEA202010192559](https://openairdocs.org/sdr/FDEA202010192559.md): Stiffener · cracked · Oct 19, 2020 · N147FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR BEAM AT STA 246 HAS 1 EA VERTICAL STIFFENER ANGLE CRACKED AT LBL 50. REMOVED AND REPLACED CRACKED ANGLE P/N 141T5146-16, IAW B767 SRM 51-40-02 AND BAC DWG 141T5600 REV.
- [SDR FDEA202010192555](https://openairdocs.org/sdr/FDEA202010192555.md): Strap · cracked · Oct 19, 2020 · N147FE · Boeing 7673S2F · Wing Miscellaneous Structure
  > RIGHT WING LES 508 LEADING EDGE NOSE STRAP CRACKED. REMOVED AND REPLACED RIGHT WING LES 508 NOSE STRAP, PER B767 SRM 51-40-02 AND BAC DWG 114T2800 REV C.
- [SDR FDEA202010182550](https://openairdocs.org/sdr/FDEA202010182550.md): Former · cracked · Oct 18, 2020 · N147FE · Boeing 7673S2F · Wing Main, Frame Structure
  > RIGHT WING LES 560 LEADING EDGE NOSE FORMER ANGLE CRACKED. REMOVED CRACKED FORMER AND INSTALLED NEW FORMER P/N 114T2512U14, REF BAC DWG 114T2162 REV.
- [SDR FDEA202010182549](https://openairdocs.org/sdr/FDEA202010182549.md): Former · cracked · Oct 18, 2020 · N147FE · Boeing 7673S2F · Wing Main, Frame Structure
  > RIGHT WING LES 490 APPROXIMATELY LEADING EDGE NOSE FORMER CRACKED. REMOVED CRACKED FORMER AND INSTALLED NEW FORMER PN 114T2511U14.
- [SDR FDEA202010092581](https://openairdocs.org/sdr/FDEA202010092581.md): Former · cracked · Oct 9, 2020 · N147FE · Boeing 7673S2F · Wing Main, Frame Structure
  > LEFT WING LEADING EDGE FORMER CRACKED AT NR 5 SLAT AUX TRACK. REMOVED AND REPLACED LEFT WING LEADING EDGE FORMER AND ANGLE, IAW BAC DWG 114T2241, REV. AND EA H AND EA: H-5720-T0357387, P1, RELEASE DATE: OCT 14, 2020, REV DATE: WINGS-SECONDARY WING STRCT SECO
- [SDR FDEA202006051136](https://openairdocs.org/sdr/FDEA202006051136.md): Detector Loop · failed · Jun 5, 2020 · N147FE · Boeing 7673S2F · Overheat Detection
  > 17 MIN INTO FLT RECEIVED LEFT DUCT LEAK LIGHT ON OVERHEAD PANEL., NO EICAS. RAN CHECKLIST AND LIGHT WENT OUT FOR REMAINDER OF FLT. FLT CONDITION LEVEL CRUISE AT FL350. REMOVED AND REPLACED ELEMENT TS407 PER AMM 26-18-01-4-2. LOOP OPS CHECK IS GOOD. INSTA
- [SDR FDEA201905161087](https://openairdocs.org/sdr/FDEA201905161087.md): Light · inoperative · May 16, 2019 · N147FE · Boeing 7673S2F · Landing Gear Position and Warning
  > LEFT MAIN GEAR LIGHT DID NOT ILLUMINATE GREEN NO OTHER INDICATIONS PRESENT TO INDICATE UNSAFE GEAR. RELAMPED LEFT GEAR INDICATOR IAW AMM 33-13-00-2. OPS CHECKED GOOD. A/C OK FOR FLIGHT.

## 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 = 'N147FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N147FE/reports

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