# Service difficulty reports: N130FE

A list on [N130FE](https://openairdocs.org/aircraft/N130FE.md).

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

- [SDR FDEA202603060324](https://openairdocs.org/sdr/FDEA202603060324.md): Skin · dented · Mar 6, 2026 · N130FE · Boeing 7673S2F · Trailing Edge Flaps
  > DENT ON LOWER SURFACE OF LT OTBD FLAP, LOCATED AT 39.5" FROM INBOARD EDGE AND 2.5" FROM AFT EDGE. LT OTBD FLAP LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R, REPAIR 1, FIG 201, SHEET 6, & SRM 51-70-17-0G, PAR 4A, FIG 10, SHEET 1, REV 94.
- [SDR FDEA202603010302](https://openairdocs.org/sdr/FDEA202603010302.md): Wedge · worn · Mar 1, 2026 · N130FE · Boeing 7673S2F · Leading Edge Devices
  > WEAR IN WEDGE TRAILING EDGE LOWER SURFACE AT 33.75 INCHES OF INBD END ON SLAT NR 4, LT WING. WEAR IN WEDGE T/E LOWER SURFACE AT 33.75 INCHES OF INBD EDGE WAS REPAIRED IAW SRM 51-70-10-2R, REP 4, FIG 202, REV 94 & SRM 57-43-02-2R, FIG 201, REP 1, SHEET 1, REV
- [SDR FDEA202603010301](https://openairdocs.org/sdr/FDEA202603010301.md): Wedge · worn · Mar 1, 2026 · N130FE · Boeing 7673S2F · Leading Edge Devices
  > WEAR IN WEDGE TRAILING EDGE LOWER SURFACE AT 30" OF INBD END ON SLAT NR 5, LT WING. LT WING, SLAT NR 5 TRAILING EDGE WEDGE LOWER SURFACE AT 30" OF INBD END EDGE WAS REPAIRED IAW SRM 51-70-10-2R, REP 4, FIG 202, SHEET B, REV 94 AND SRM 57-43-02-2R, FIG 201, RE
- [SDR FDEA202602240277](https://openairdocs.org/sdr/FDEA202602240277.md): Floor Panel · punctured · Feb 24, 2026 · N130FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL 231NFF MDC FLOOR PANEL 231NFF MDC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93.
- [SDR FDEA202602240276](https://openairdocs.org/sdr/FDEA202602240276.md): Floor Panel · punctured · Feb 24, 2026 · N130FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL 231QFF MDC FLOOR PANEL 231QFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93.
- [SDR FDEA202602240275](https://openairdocs.org/sdr/FDEA202602240275.md): Floor Panel · punctured · Feb 24, 2026 · N130FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL 251QFF MDC FLOOR PANEL 251QFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV 93.
- [SDR FDEA202602230270](https://openairdocs.org/sdr/FDEA202602230270.md): Floor Panel · punctured · Feb 23, 2026 · N130FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL 241LFF MDC FLOOR PANEL 241LFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15/2025
- [SDR FDEA202602230269](https://openairdocs.org/sdr/FDEA202602230269.md): Floor Panel · punctured · Feb 23, 2026 · N130FE · Boeing 7673S2F · Fuselage Floor Panel
  > PUNCTURE ON FLOOR PANEL 251DFF MDC FLOOR PANEL 251DFF MDC WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 93 AUG 15/2025
- [SDR FDEA202506271070](https://openairdocs.org/sdr/FDEA202506271070.md): Bulb · inoperative · Jun 27, 2025 · N130FE · Boeing 7673S2F · Landing Gear Position and Warning
  > UPON SELECTING GEAR DOWN HAD NO GREEN LIGHT FOR NOSE GEAR. RAN QRH & DETERMINED IT WAS BULB & REPLACED BULBS. NORMAL GEAR EXTENSION THEREAFTER. NORMAL INDICATIONS. CHECKED NOSE GEAR GREEN LIGHTS FOR PROPER INSTALLATION AS PER AMM 33-13-00-2. FOUND SATIS
- [SDR FDEA202406170810](https://openairdocs.org/sdr/FDEA202406170810.md): Bulb · failed · Jun 17, 2024 · N130FE · Boeing 7673S2F · Landing Gear Position and Warning
  > ON APPROACH, AT GEAR EXTENSION, THE RT MLG DID NOT INDICATE SAFE (NO GREEN LIGHTS). THERE WAS NO EICAS OR GEAR DISAGREE LIGHT. BULBS TESTED GOOD. AFTER RETRACTING MLG ON GO AROUND & EXTENDING IT FOR SUBSEQUENT APPROACH, MLG EXTENDED NORMALLY. IAW CREW REPORT,
- [SDR FDEA202403080263](https://openairdocs.org/sdr/FDEA202403080263.md): Support Angle · cracked · Mar 8, 2024 · N130FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > [UPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, LBL 78, "I" BEAM REINFORCE "L" ANGLE ON OUTBOARD SIDE OF "I" BEAM IS CRACKED., 2024-03-08] REMOVED AND REPLACED ANGLE P/
- [SDR FDEA202403050249](https://openairdocs.org/sdr/FDEA202403050249.md): Angle · cracked · Mar 5, 2024 · N130FE · Boeing 7673S2F · Fuselage Main, Structure
  > MAIN CARGO DECK, AT STA. 1582 LBL 78, HAS ANGLE BRACKET (P/N 146T5651-5) CRACKED REMOVED AND REPLACE ANGLE BRACKET P/N 146T5651-5 PER BOEING DWG 146T5651 AND SRM 51-40-02-0G
- [SDR FDEA202402260266](https://openairdocs.org/sdr/FDEA202402260266.md): Support Beam · cracked · Feb 26, 2024 · N130FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > UPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, RBL 78, "I" BEAM REINFORCE "L" ANGLE ON OUTBOARD SIDE OF "I" BEAM IS CRACKED. REMOVED AND REPLACED ANGLE BRACKET REF 767 D
- [SDR FDEA202402260265](https://openairdocs.org/sdr/FDEA202402260265.md): Support Beam · cracked · Feb 26, 2024 · N130FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > UPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, LBL 78, "I" BEAM REINFORCE "L" ANGLE ON OUTBOARD SIDE OF "I" BEAM IS CRACKED. REMOVED AND REPLACED ANGLE P/N 146T5651-7 PER
- [SDR FDEA202402260243](https://openairdocs.org/sdr/FDEA202402260243.md): Support Angle · cracked · Feb 26, 2024 · N130FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > UPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, RBL 78, "I" BEAM REINFORCE "L" ANGLE ON OUTBOARD SIDE OF "I" BEAM IS CRACKED. 0000191391: LINTON, LOREN E - 04-MAR-2024 03
- [SDR FDEA202402250258](https://openairdocs.org/sdr/FDEA202402250258.md): Bracket · cracked · Feb 25, 2024 · N130FE · Boeing 7673S2F · Wing, Attach Fittings
  > LH WING L/E BRACKET CRACKED, VIEWED INSIDE LIGHTNING HOLE AT APPROX WING STATION 510 (BETWEEN #5 SLAT OUTBD SIDE AND #5 SLAT OUTBD AUX TRACK). MARKED WITH ORANGE DOT MK1. BRACKET P/N 114T2800-165. REPAIRED PER EA H-5720-T0378377 B
- [SDR FDEA202402250257](https://openairdocs.org/sdr/FDEA202402250257.md): Bracket · cracked · Feb 25, 2024 · N130FE · Boeing 7673S2F · Wing, Attach Fittings
  > RH WING L/E BRACKET CRACKED, VIEWED INSIDE LIGHTNING HOLE AT APPROX WING STATION 510 (BETWEEN #8 SLAT OUTBD SIDE AND #8 SLAT OUTBD AUX TRACK). MARKED WITH ORANGE DOT MK2. BRACKET P/N 114T2800-165. 0000730634: NGUYEN,QUYNH Q - 07-MAR-2024 19:17 REMOVED AND
- [SDR FDEA202402250241](https://openairdocs.org/sdr/FDEA202402250241.md): Shear Tie · cracked · Feb 25, 2024 · N130FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame
  > #2 PYLON AFT TORQUE BOX BULKHEAD INBOARD SHEAR TIE CRACKED. REMOVE AND REPLACED SHEAR TIE (313T3310-1155) USING 767 SRM REFERENCE 51-40-02-0G AND IPC 54-51-53-13C ALONG WITH BOEING DRW 313T3310-1155 & 313T3310 SH 91.
- [SDR FDEA202402220267](https://openairdocs.org/sdr/FDEA202402220267.md): Support Beam · cracked · Feb 22, 2024 · N130FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > UPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, RBL 78, "I" BEAM REINFORCE "L" ANGLES ON BOTH SIDES ARE CRACKED. REMOVED AND REPLACED "L" ANGLES AT RBL 78 BETWEEN STA 1564
- [SDR FDEA202402220264](https://openairdocs.org/sdr/FDEA202402220264.md): Support Angle · cracked · Feb 22, 2024 · N130FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > UPPER MAIN DECK FLOOR STRUCTURE, AS SEEN FROM BEHIND THE LOWER BULK CARGO, FLOOR PANEL ATTACH STRUCTURE BETWEEN STATION 1564 AND 1582, RBL 78, "I" BEAM REINFORCE "L" ANGLES ON BOTH SIDES ARE CRACKED. 0000239190: BASTIN, WILLIAM D - 08-MAR-2024 20:33 REMOVE
- [SDR FDEA202308111397](https://openairdocs.org/sdr/FDEA202308111397.md): Former · failed · Aug 11, 2023 · N130FE · Boeing 767300 · Wing Main, Frame Structure
  > NOSE FORMER ANGLE AT OSS 499.6 ON THE LEFT WING FIXED LEADING EDGE IS CRACKED. REMOVED THE BROKEN NOSE FORMER ANGLE AT OSS 499.6 ON THE LEFT WING FIXED LEADING EDGE. INSTALLED A 114T251U13 ANGLE. FEDEX DRAWING B67-57-002.
- [SDR FDEA202011132839](https://openairdocs.org/sdr/FDEA202011132839.md): Skin · gouged · Nov 13, 2020 · N130FE · Boeing 7673S2F · Nacelle/Pylon, Plate/Skin
  > NR 2 ENGINE INBOARD CORE COWL INNER SIDE NR 2 FRAME FROM FWD END IS GOUGED. REPAIRED NR 2 ENGINE INBOARD CORE COWL NR 2 FRAME, IAW B767 SRM 54-45-01-2R REPAIR 3.
- [SDR FDEA202011112827](https://openairdocs.org/sdr/FDEA202011112827.md): Beam · damaged · Nov 11, 2020 · N130FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame
  > NR 2 PYLON INBOARD LATCH BEAM MISSING NUTPLATE. REMOVED NR 2 PYLON INBOARD LATCH BEAM, IAW B767 SRM 54-52-71-2R. REPAIRED LATCH BEAM, IAW B767-SRM 54-52-71-2R. REINSTALLED NR 2 PYLON INBOARD LATCH BEAM, IAW B767 SRM 54-52-71-2R.
- [SDR FDEA202011052783](https://openairdocs.org/sdr/FDEA202011052783.md): Bracket · cracked · Nov 5, 2020 · N130FE · Boeing 7673S2F · Wing Miscellaneous Structure
  > RIGHT WING NR 7 SLAT DRIVESHAFT LOOP BRACKET CRACKED, STREAMER ATTACHED. REMOVED AND REPLACED LOOP BRACKET, PER B767 SRM 51-40-02 AND BOEING DWG 114T1240 REV E.
- [SDR FDEA202011052782](https://openairdocs.org/sdr/FDEA202011052782.md): Bracket · cracked · Nov 5, 2020 · N130FE · Boeing 7673S2F · Wing Miscellaneous Structure
  > LEFT WING LES 284 SLAT DRIVESHAFT LOOP BRACKET CRACKED, STREAMER ATTACHED. REMOVED AND REPLACED LOOP BRACKET, PER B767 SRM 51-40-02 AND BOEING DWG 114T1240 REV E.
- [SDR FDEA202007291700](https://openairdocs.org/sdr/FDEA202007291700.md): Flap System · malfunctioned · Jul 29, 2020 · N130FE · Boeing 767300 · Trailing Edge Flap Control System
  > ON APPROACH, SELECTED FLAPS 1 TO FLAPS 5. RECEIVED TE FLAP ASYMMETRY EICAS MSG & TRAILING EDGE LIGHT. COMPLETED THE QRH, TE FLAP ASYMMETRY CHECK LIST & USED ALTERNATE FLAPS, SETTING 20 DEGREES FOR LANDING. 'EMERGENCY DECLARED. ALL SWITCHES BACK TO NORMAL.
- [SDR FDEA2020080329699](https://openairdocs.org/sdr/FDEA2020080329699.md): Warning Message · false activation · Jul 29, 2020 · N130FE · Boeing 7673S2F · Trailing Edge Flap Control System
  > ON APPROACH, AT 7000 FT, 210KTS, SELECTED FLAPS 1 TO FLAPS 5. RECEIVED TE FLAP ASYMMETRY EICAS MESSAGE AND TRAILING EDGE LIGHT. COMPLETED THE QRH TRAILING EDGE FLAP ASYMMETRY CHECK LIST AND USED ALTERNATE FLAPS, SETTING 20 DEGREES FOR LANDING. EMERGENCY
- [SDR FDEA2020073091699](https://openairdocs.org/sdr/FDEA2020073091699.md): Flap System · malfunctioned · Jul 29, 2020 · N130FE · Boeing 7673S2F · Trailing Edge Flap Control System
  > DURING APPROACH, SELECTED FLAPS 1 TO FLAPS 5. RECEIVED TE FLAP ASYMMETRY EICAS MESSAGE AND TRAILING EDGE LIGHT. COMPLETED THE QRH, T/E FLAP ASYMMETRY CHECK LIST AND USED ALTERNATE FLAPS, SETTING 20 DEGREES FOR LANDING. EMERGENCY DECLARED. CREW STATED TE FL
- [SDR FDEA2020060111104](https://openairdocs.org/sdr/FDEA2020060111104.md): Motor · failed · May 31, 2020 · N130FE · Boeing 7673S2F · Cabin Pressure Control System
  > LEVEL AT FL340 GOT A CABIN ALT WARNING. CABIN ALTITUDE WAS JUST ABOVE 10,00 FT. STARTED AN EMERGENCY DESCENT. WHILE IN DESCENT GOT CABIN ALT AUTO 1 INOPERATIVE MESSAGE. SWITCH TO AUTO 2 CONTROLLER AND CABIN ALTITUDE RETURNED TO NORMAL. BITE NR 1 CPC FOUND
- [SDR FDEA2020042730778](https://openairdocs.org/sdr/FDEA2020042730778.md): Warning System · false activation · Apr 23, 2020 · N130FE · Boeing 7673S2F · Trailing Flap Position Indicating System
  > TE FLAP DISAGREE LANDING MOVING FROM 1 TO 5 OPERATED FLAPS IN ALTN, NO FAULTS NO DISAGREE. OPERATED FLAPS NORAMLLY WITH ALL CENTER PUMPS ON (WITH ACMP ON) NO FAULTS NO DISAGREE. CHECKED FLAP POS. MODULES FOR FAULTS NO FAULTS IAW AMM 27-58-01. PERFORMED BIT
- [SDR FDEA201901120103](https://openairdocs.org/sdr/FDEA201901120103.md): Eva System · inoperative · Jan 12, 2019 · N130FE · Boeing 7673S2F · Emergency Equipment
  > WHILE C\W EA H-2560-E0324416 FOUND PILOTS(L\H) EVAS LIGHTS INOP\UNSEEABLE. REMOVED AND REPLACED CAPT EVAS, OPS CHECK GOOD. NOMENCLATURE - EMERGENCY VISION ASSURANCE SYSTEM,
- [SDR FDEA201901110093](https://openairdocs.org/sdr/FDEA201901110093.md): Light · inoperative · Jan 11, 2019 · N130FE · Boeing 7673S2F · Flight Compartment Lighting
  > PDIS 130 33-50 2856 11JAN19 BWI FACT U LOGPAGES:3045527 EMERG LIGHTS DISARM LIGHT ON OVERHEAD PANEL INOP. MEL 11JAN19 13:09 BWI U RELEASED FOR SERVICE PER MEL: 33-51-02 CATEGORY: B EXPIRATION: 14JAN19 "MEL 33-51-02: EXTERIOR EMERGENCY LIGHTS - INOP. 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 = 'N130FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N130FE/reports

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