# Service difficulty reports: N127FE

A list on [N127FE](https://openairdocs.org/aircraft/N127FE.md).

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

- [SDR FDEA202506261061](https://openairdocs.org/sdr/FDEA202506261061.md): Web · cracked · Jun 26, 2025 · N127FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > MEC, LT TUNNEL, STA 246 - STA 266 FLOORBEAM WEB CRACKED, LBL APPROX 48 FABRICATED/REPLACED WEB P/N 141T5602-2, REF B767 SRM 51-40-02-0G & BOEING DRW 141T5602.THIS IS A MAJOR REPAIR
- [SDR FDEA202506251048](https://openairdocs.org/sdr/FDEA202506251048.md): Floorboard · damaged · Jun 25, 2025 · N127FE · Boeing 7673S2F · Fuselage Floor Panel
  > NR# 0293: MAIN CARGO DECK, FLOOR PANEL 242JFF HAS DAMAGE. FABRICATED NEW FLOOR PANEL 242JFF, MPN:145T5876-102, RBL 33 - RBL 11, STA. 930 Ï¿½ 984.95 IN REF TO BOEING DWG# 145T5876-102. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION
- [SDR FDEA202506251046](https://openairdocs.org/sdr/FDEA202506251046.md): Floorboard · damaged · Jun 25, 2025 · N127FE · Boeing 7673S2F · Fuselage Floor Panel
  > NR# 0297: MAIN CARGO COMPARTMENT, FLOOR PANEL 242SFF HAS DAMAGE FABRICATED NEW FLOOR PANEL 242SFF, MPN:145T5876-104, RBL 33- RBL 11, STATION 984.95 - 1114.82 IN REF TO BOEING DWG 145T5876-104. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. IN
- [SDR FDEA202506241040](https://openairdocs.org/sdr/FDEA202506241040.md): Floorboard · damaged · Jun 24, 2025 · N127FE · Boeing 7673S2F · Fuselage Floor Panel
  > NR# 0296: MAIN CARGO COMPARTMENT, FLOOR PANEL 241WFF HAS DAMAGE FABRICATED NEW FLOOR PANEL 241WFF, MPN:145T5876-51, RBL 11- LBL 11, STATION 984.95 - 1114.82 IN REF TO BOEING DWG 145T5876-51. SEE JPF FOR ALL THE WORK PERFORMED. THIS IS A MAJOR REPAIR. INS
- [SDR FDEA202506241039](https://openairdocs.org/sdr/FDEA202506241039.md): Floor Panel · damaged · Jun 24, 2025 · N127FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT, FLOOR PANEL 242LFA HAS DAMAGE. FABRICATED MAIN COMPARTMENT, FLOOR PANEL 242LFA (MPN: 145T5876-110) AT STA 930 TO STA 984, RBL 54.75 TO RBL 74.25 IN REF TO BOEING DRAWING 145T5876 ID# 110.THIS IS A MAJOR REPAIR. PLEASE SEE SEQ CARD 1
- [SDR FDEA202506241037](https://openairdocs.org/sdr/FDEA202506241037.md): Floor Panel · dented · Jun 24, 2025 · N127FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT, FLOOR PANEL 242VFF HAS DAMAGE: CORRECTION FLOOR PANEL 242UFF FABRICATED FLOORPANEL 242UFF MPN# 114T5876-112 STA: 980-1114.82 RBL: 54.75- RBL 74.25 IN REF TO BOEING DRAWING 114T5876-112. SEE JPF FOR ALL WORK STEPS ACCOMPLISHED. THIS
- [SDR FDEA202506221025](https://openairdocs.org/sdr/FDEA202506221025.md): Floor Panel · worn · Jun 22, 2025 · N127FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT, FLOOR PANEL 241LFF HAS DAMAGE. FABRICATED NEW FLOOR PANEL 241LFF, MPN:145T5876-19, RBL 11 LBL 11, STATION 930-984.95 IN REF TO BOEING DWG 145T5876-19. SEE JPF FOR ALL WORK PERFORMED. THIS IS A MAJOR REPAIR. INSTALLATION OF THIS PAN
- [SDR FDEA202503050334](https://openairdocs.org/sdr/FDEA202503050334.md): Windshield · cracked · Mar 5, 2025 · N127FE · Boeing 7673S2F · Flight Compartment Windows
  > DURING CRUISE AT FL320, CAPTAIN S WINDSHIELD CRACKED IN A SPIDER WEB DESIGN. L FWD WINDSHIELD HEAT WENT INOP. WINDSHIELD REMOVED. WINDSHIELD HARDWARE IN FLIGHT DECK. J1 / J15 PINS REMOVED. INSTALLATION COMPLIED WITH FROM PARA G (18) IAW AMM 56-11-01-4. SY
- [SDR FDEA202412241829](https://openairdocs.org/sdr/FDEA202412241829.md): Former · cracked · Dec 24, 2024 · N127FE · Boeing 7673S2F · Wing Main, Frame Structure
  > RIGHT WING LEADING EDGE FORMER AT STA 433 CRACKED. REMOVED AND REPLACED RIGHT WING LEADING EDGE FORMER AT STA 433 REF 57-41-01-2R
- [SDR FDEA202410151502](https://openairdocs.org/sdr/FDEA202410151502.md): Control Unit · failed · Oct 15, 2024 · N127FE · Boeing 7673S2F · Door Warning System
  > MAIN CARGO DOOR LIGHT EICAS AND CARGO DOORS DISCREET LIGHT CAME ON DURING FLIGHT. 3 LIGHTS ON MAIN ENTRANCE DOOR PANEL WERE EXTINGUISHED. EXECUTED QRH PROCEDURES. REMOVED & REPLACED THE PSEU PER THE ABOVE AMM REFERENCE, ALL TESTS PASS.
- [SDR FDEA202409011212](https://openairdocs.org/sdr/FDEA202409011212.md): Retainer · cracked · Sep 1, 2024 · N127FE · Boeing 7673S2F · Cargo/Baggage Doors
  > LOWER FORWARD CARGO DOOR SEAL RETAINER DAMAGED AT UPPER FORWARD AREA. LWR FWD CGO DOOR, UPPER SEAL RETAINER REPAIR PERFORMED IAW B767 SRM 52-30-02-2R REPAIR 5. MAJOR REPAIR. SEE JPF.
- [SDR FDEA202306291126](https://openairdocs.org/sdr/FDEA202306291126.md): Slat · damaged · Jun 29, 2023 · N127FE · Boeing 767300 · Wing, Control Surfaces
  > PERFORM MAJOR REPAIR TO SLAT #11 TRAILING EDGE WEDGE IN ACCORDANCE WITH 51-70-10-2R IN THE AREA OF SLAT #11 OSS 933.729. REF B767 SRM51-70-10-2R REPAIR4 & EA:H-5750-T0369144 P3 REPAIR THE #11 SLAT TRAILING EDGE WEDGE AT OSS 933.729. EA TITLE: WINGS - RH
- [SDR FDEA202210222644](https://openairdocs.org/sdr/FDEA202210222644.md): Former · cracked · Oct 22, 2022 · N127FE · Boeing 7673S2F · Wing Main, Frame Structure
  > L/WING FLE OSS 499 HAS A CRACKED FORMER REPLACED FORMER B67-57-002-03 AT L/WING FLE OSS 499 USING EA H-5720-T0371261 AS REFERENCE.
- [SDR FDEA202206231539](https://openairdocs.org/sdr/FDEA202206231539.md): Slat · chafed · Jun 23, 2022 · N127FE · Boeing 767300 · Leading Edge Devices
  > RH WING LEADING EDGE SLAT #11 HAS A WEAR GROOVE ON THE UNDERSIDE(CONCAVE SIDE) SKIN. COMPLIED WITH E.A. H-5750-T0369144 P1.
- [SDR FDEA202009162253](https://openairdocs.org/sdr/FDEA202009162253.md): Floor Panel · delaminated · Sep 16, 2020 · N127FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 242TFA DELAMINATED AND HAS EDGE DAMAGE AT CORNER. REPAIRED AREAS OF DELAMINATION AND EDGE DAMAGE TO CARGO FLOOR PANEL 242TFA, IAW B767 SRM 53-00-50-2R.
- [SDR FDEA202009162226](https://openairdocs.org/sdr/FDEA202009162226.md): Angle · cracked · Sep 16, 2020 · N127FE · Boeing 7673S2F · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON AFT BULKHEAD TO AFT FAIRING INBOARD ATTACH ANGLE CRACKED AT NAC STA 295 LT. REMOVED AND REPLACED ANGLE, PER B767 SRM 551-40-02 AND BOEING DWG 313T3310 REV B.
- [SDR FDEA202009152221](https://openairdocs.org/sdr/FDEA202009152221.md): Housing · cracked · Sep 15, 2020 · N127FE · Boeing 7673S2F · Cargo Compartment Lighting
  > AFT CARGO DOOR UPPER AFT CARGO LIGHT GOUGED AND CRACKED. REPAIRED AFT CARGO DOOR UPPER AFT CARGO LIGHT, IAW B767-AMM 25-00-00-8.
- [SDR FDEA202009152220](https://openairdocs.org/sdr/FDEA202009152220.md): Housing · cracked · Sep 15, 2020 · N127FE · Boeing 7673S2F · Cargo Compartment Lighting
  > AFT CARGO DOOR UPPER FWD CARGO LIGHT GOUGED AND CRACKED. REPAIRED AFT CARGO DOOR UPPER FWD CARGO LIGHT, IAW B767-AMM 25-00-00-8.
- [SDR FDEA2020091432191](https://openairdocs.org/sdr/FDEA2020091432191.md): Skin · chafed · Sep 13, 2020 · N127FE · Boeing 7673S2F · Leading Edge Devices
  > RIGHT WING SLAT NR 11, T/E LOWER SURFACE CHAFE AT O/B TRACK. REPAIRED RT WING NR 11 SLAT T/E LOWER SURFACE CHAFE AT O/B TRACK WITH 250 DEG METAL BOND, IAW B767 SRM 57-43-01-01 FIG 1 DETAIL NR 1, 57-43-02-01 FIG 1 DETAIL NR 4, 57-43-02-2R REPAIR 1 DETAIL NR
- [SDR FDEA2020091422186](https://openairdocs.org/sdr/FDEA2020091422186.md): Beam · gouged · Sep 12, 2020 · N127FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame
  > NR 2 PYLON AFT FAIRING INBOARD LONGITUDINAL BEAM GOUGED AT NUTPLATE LOCATION AT NAC STA 308 LT. REMOVED LATCH BEAM, IAW B767 SRM 51-40-02-0G. REPAIRED LATCH BEAM, IAW B767 SRM 54-52-71-2R AND FED EX EA H5450-T0356442 P1. REINSTALLED LATCH BEAM, IAW B767 SRM
- [SDR FDEA202009112171](https://openairdocs.org/sdr/FDEA202009112171.md): Floor Panel · damaged · Sep 11, 2020 · N127FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242GFF IS DAMAGED. REPAIRED MAIN CABIN FLOOR PANEL 242GFF, IAW B767 SRM 53-00-50-2R.
- [SDR FDEA202009112170](https://openairdocs.org/sdr/FDEA202009112170.md): Floor Panel · damaged · Sep 11, 2020 · N127FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241ZFF IS DAMAGED. REPAIRED MAIN CABIN FLOOR PANEL 241ZFF, IAW B767 SRM 53-00-50-2R.
- [SDR FDEA2020090982147](https://openairdocs.org/sdr/FDEA2020090982147.md): Former · cracked · Sep 8, 2020 · N127FE · Boeing 7673S2F · Wing Main, Frame Structure
  > RT WING LEADING EDGE INTERNAL FORMER CRACKED ON OUTBOARD SIDE OF SLAT NR 8 OUTBOARD ACTUATOR. REMOVED AND REPLACED RT WING RIB FORMER AT W/S 480, PER FEDEX B767 SRM 51-40-02 & BAC DWG 114T2511. LOCATED AND DRILLED PER FEDEX B767-SRM 51-40-05.
- [SDR FDEA2020090972139](https://openairdocs.org/sdr/FDEA2020090972139.md): Bracket · cracked · Sep 7, 2020 · N127FE · Boeing 7673S2F · Wing Main, Frame Structure
  > LT WING, LEADING EDGE CAVITY FWD FORMER BRACKET CRACKED, LEADING EDGE STA 430. REMOVED CRACKED FORMER BRACKET IAW B767 SRM 51-40-02, MATERIAL ID 2024T3.040" IAW BAC DWG 114T2170. FABRICATED RIB FORMER BRACKET, IAW BOEING DWG 114T2170 REV ALODINED, IAW BOEIN
- [SDR FDEA2020090972138](https://openairdocs.org/sdr/FDEA2020090972138.md): Splice Plate · cracked · Sep 7, 2020 · N127FE · Boeing 7673S2F · Wing Main, Frame Structure
  > RT WING LEADING EDGE INTERNAL SPLICE PLATE CRACKED APPROX 1' OUTBOARD OF SLAT #8 OUTBOARD ACTUATOR. REMOVED AND REPLACED SPLICE P/N 114T2800-165, PER BAC DWG 114T2800 REV G.
- [SDR FDEA2020090972137](https://openairdocs.org/sdr/FDEA2020090972137.md): Bracket · cracked · Sep 7, 2020 · N127FE · Boeing 7673S2F · Wing, Attach Fittings
  > LT WING, LEADING EDGE CAVITY FWD FORMER BRACKET CRACKED. LEADING EDGE STA 480 REMOVED AND REPLACED NOSE FORMER, IAW BOEING DWG 114T2511, REV D, B767 SRM 51-40-02 AND B767 SRN 51-40-03.
- [SDR FDEA2020090962134](https://openairdocs.org/sdr/FDEA2020090962134.md): Bracket · cracked · Sep 6, 2020 · N127FE · Boeing 7673S2F · Wing, Attach Fittings
  > LEFT WING PANEL 511KB AREA INBOARD BRACKET CRACKED. REMOVED AND REPLACED BRACKET P/N 256T2425-6, PER BOEING DWG 114T1240 REV D.
- [SDR FDEA2020090942107](https://openairdocs.org/sdr/FDEA2020090942107.md): Bracket · cracked · Sep 4, 2020 · N127FE · Boeing 7673S2F · Wing, Attach Fittings
  > RT WING PANEL 611KB AREA IB BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON RT WING PANEL 611KB AREA, PER FEDEX B767 SRM 51-40-02 AND PER BOEING DWG 114T1240 REV D.
- [SDR FDEA2020090922082](https://openairdocs.org/sdr/FDEA2020090922082.md): Former · cracked · Sep 2, 2020 · N127FE · Boeing 7673S2F · Wing Main, Frame Structure
  > LT WING LEADING EDGE CAVITY FWD FORMER STRAP CRACKED LEADING EDGE STA 505. REMOVED AND REPLACED LT WING LEADING EDGE CAVITY FWD FORMER STRAP LES 505 PN 114T2800-165 SEAL STRIP PO NR 979532.1, IAW BAC DWG 114T2800 REV G, B767 SRM 51-40-02.
- [SDR FDEA202006261369](https://openairdocs.org/sdr/FDEA202006261369.md): Unknown · odor · Jun 26, 2020 · N127FE · Boeing 7673S2F · Air Distribution System
  > ON CLIMBOUT AND DESCENT PACKS SMELL LIKE DIRTY SOCKS. PERFORMED AIR CONDITIONING OIL/FUME CONTAMINATION REMOVAL AS PER MM 21-00-21-2. OIL SMELL WITH PACKS RUNING HAS DISSIPATED, NO SMOKE OR FUMES. PERFORMED BOROSCOPE UNDER WRI 72-00/4125 AND MTSI 72-30/4072
- [SDR FDEA202006261368](https://openairdocs.org/sdr/FDEA202006261368.md): Module · odor · Jun 26, 2020 · N127FE · Boeing 7673S2F · Cabin Cooling System
  > ON CLIMBOUT AND DESCENT PACKS SMELL LIKE DIRTY SOCKS. REMOVED AND REPLACED YSM, PER AMM 27-09-00-2. CHECKS GOOD. UNIT CHANGED, YAW DAMPER/STAB TRIM MODULE.
- [SDR FDEA201909112212](https://openairdocs.org/sdr/FDEA201909112212.md): Pressure Switch · failed · Sep 11, 2019 · N127FE · Boeing 7673S2F · Hydraulic Pressure Sensor
  > UNSCHD STAB TRIM FOR APPROXIMATELY 2 SECONDS ON EICAS, PASSING 8000 FT DURING DESCENT SPEED 210 KTS FLAP 1. REPLD C HYD PRESS SWITCH S29. PRESSURE SWITCH LEAK CKS GOOD. PERFORMED OPS CK OF ADP REF AMM 29-11-03-4-0. T/S UNSCHED STAB TRIM REF FIM 27-09 FAULT TRE
- [SDR FDEA2018110213074](https://openairdocs.org/sdr/FDEA2018110213074.md): Escape Rope · unsecure · Nov 1, 2018 · N127FE · Boeing 7673S2F · Emergency Equipment
  > ON ARRIVAL AT THE ACFT, FOUND AN ESCAPE ROPE DROPPED DOWN AT THE FRONT OF DOOR. RESTORED THE L1 ENTRY DOOR ESCAPE ROPE IAW MM 25-61-04-2-1. AIRCRAFT OK SERVICE.
- [SDR FDEA201802110336](https://openairdocs.org/sdr/FDEA201802110336.md): Transmitter · malfunctioned · Feb 11, 2018 · N127FE · Boeing 7673S2F · Stabilizer Position Indicating
  > RECEIVED RED STABLIZER WARNING ON INITIAL POWER APPLICATION DURING PREFLIGHT STAB TRIM SET TO 6.75. CONFIG T/O CHECK PERFORMED 3 TIMES. AFTER WARNING, STAB INDICATED (AN UNCOMMANDED MOVE) TO 7.1 OR 7.2. CONCLUDED WE HAD UNCOMMANDED MOVEMENT OF APPROX 1/3 UNI
- [SDR FDEA201606152003](https://openairdocs.org/sdr/FDEA201606152003.md): Rotary Actuator · inoperative · Jun 15, 2016 · N127FE · Boeing 7673S2F · Leading Edge Slat Actuator
  > AT 220 KTS RECEIVED L/E SLAT DISAGREE LIGHT. ACCOMPLISHED QRH CHECKLIST 9.1.10, L/E SLAT DISAGREE 0. L/E WOULD NOT DEPLOY BEYOND, BETWEEN UP AND 1, USING ALT FLAPS. QRH LEAD ME TO RUN QRH 9.1.6, L/E SLAT ASYM CHECKLIST. FLAPS DEPLOYED TO 20 USING ALT FLAPS

## 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 = 'N127FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N127FE/reports

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