# Service difficulty reports: N115FE

A list on [N115FE](https://openairdocs.org/aircraft/N115FE.md).

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

- [SDR FDEA202609141334](https://openairdocs.org/sdr/FDEA202609141334.md): Skin · damaged · Sep 14, 2026 · N115FE · Boeing 7673S2F · Leading Edge Devices
  > NR 10 SLAT HAS MINOR DAMAGE ON LOWER SURFACE APPROXIMATELY 31.5" FROM INBD EDGE. REPAIRED RT WING NR 10 SLAT T/E WEDGE AT OSS 713.5 IAW SRM 57-43-02-2R AND SRM 51-7-10-2R. THIS IS A MAJOR REPAIR.
- [SDR FDEA202601230081](https://openairdocs.org/sdr/FDEA202601230081.md): Window · haze · Jan 23, 2026 · N115FE · Boeing 7673S2F · Flight Compartment Windows
  > L3, R1, R3 WINDOWS DELAMINATING OBSCURING CRITICAL VISIBILITY AREA AND CREATING A FLIGHT SAFETY HAZARD. AMM: 56-11-00-6-0 REF WRI 56-10/1646, R1 (F/O WONDSHIELD) WINDOW IS UNDER OIL FOR DELAMINATION. NO ADDITIONAL DELAMINATION NOTICED. ALL 3 WINDOWS R1,
- [SDR FDEA202512142251](https://openairdocs.org/sdr/FDEA202512142251.md): Skin · dented · Dec 14, 2025 · N115FE · Boeing 7673S2F · Leading Edge Devices
  > LEFT WING NR 5 SLAT HAS A DENT IN UPPER TRAILING WEDGE SKIN 34 INCHES FROM INBD EDGE. REPAIRED LT WING NR 5 SLAT UPPER T/E WEDGE SKIN IAW SRM 57-43-02-0I, PG 1-2, DETAIL 1 & 2, SRM 51-70-10-2R, AND AMM 51-21-10-7. MAJOR REPAIR. SEE JPF FOR OTHER WORK ACCOMPL
- [SDR FDEA202512142250](https://openairdocs.org/sdr/FDEA202512142250.md): Skin · dented · Dec 14, 2025 · N115FE · Boeing 7673S2F · Leading Edge Devices
  > LEFT WING NR 1 SLAT HAS DENT IN UPPER TRAILING WEDGE SKIN 16" FROM I/B EDGE. REPAIRED LEFT WING NR 1 SLAT UPPER T/E WEDGE SKIN SURFACE 16" FROM I/B EDGE IAW SRM 57-43-02-0I, PG 1-2 DETAIL 1 & 2, B767 SRM 51-70-10-2R, AND AMM 51-21-10-7. MAJOR REPAIR. SEE JPF
- [SDR FDEA202511272214](https://openairdocs.org/sdr/FDEA202511272214.md): Idg · failed · Nov 27, 2025 · N115FE · Boeing 7673S2F · AC Generator-Alternator
  > R GEN DRIVE EICAS IN-FLIGHT. ACCOMPANIED BY ILLUMINATED R GEN DRIVE SWITCH LIGHT. COMPLIED WITH QRH. EMERGENCY DECLARED. PERFORMED RT ENG RUN TEST BER AMM 71-00-00-5-3, FOUND RT GEN CONT OFF LIGHT ON. BITE OF BPCU FOUND FAULT RT ENG GEN MPU/WIRING. WIR
- [SDR FDEA202511112158](https://openairdocs.org/sdr/FDEA202511112158.md): Flap System · faulted · Nov 11, 2025 · N115FE · Boeing 7673S2F · Trailing Edge Flap Control System
  > AT APPROX 80 KTS ON TAKEOFF GOT EICAS FLAPS AND CONIF. REJECTED THE TAKEOFF RUNWAY 02R AT BKK AT 303 TOGW AND 31C TEMP. RAN CHECKLISTS, RETURNED TO THE GATE LEAVING FLAPS AT 5. PERFORMED T/S AS PER FIM 31-51 FT 808, NO FAULT FOUND. PERFORMED BITE PROCEDUR
- [SDR FDEA202409051247](https://openairdocs.org/sdr/FDEA202409051247.md): Battery · no test · Sep 5, 2024 · N115FE · Boeing 7673S2F · Emergency Lighting
  > MDIS 115 33-50 0178 05SEP24 02:24 TPE FACT DURING SERVICE CHECK, FOUND EMERGENCY LIGHT DIDN'T ILLUMANATE. FACT 05SEP24 02:30 TPE FIM: 33-51-00-815-802 AMM: 33-51-07-2-0 REF ABOVE REFERENCE PERFORMED T/S AND FOUND THE BATTERY PACK OF THE PO
- [SDR FDEA202403080261](https://openairdocs.org/sdr/FDEA202403080261.md): Sliding Window · cracked · Mar 8, 2024 · N115FE · Boeing 7673S2F · Flight Compartment Windows
  > FO NOTICE IN FLIGHT CRACKING ON PERIMETER OF WINDOWS. RAN CHECKLIST FOR CRACKED WINDOW IN FLIGHT. AS PER CREW DEBRIEF F/O SLIDING WINDOW CRACKED ALONG THE EDGE. NO ARCING AND NO LEAKAGE OR PRESSURISATION ISSUES. CARRIED OUT INSPECTION AND CHECKS FOUND
- [SDR FDEA202203310790](https://openairdocs.org/sdr/FDEA202203310790.md): None · none · Mar 31, 2022 · N115FE · Boeing 767300 · Landing Gear Position and Warning
  > ON APPROACH INTO SKBO (BOG) AT APPROXIMATELY 10700 MSL, AFTER PUTTING THE LANDING GEAR DOWN, WE ONLY GOT GREEN NOSE GEAR AND A GREEN RIGHT MAIN GEAR LIGHTS. WE ACCOMPLISHED A GO AROUND AND BEGAN TO RUN THE QRH. AFTER RUNNING THE QRH, WE HAD THE SAME IND
- [SDR FDEA202203010383](https://openairdocs.org/sdr/FDEA202203010383.md): None · none · Mar 1, 2022 · N115FE · Boeing 767300 · Door Warning System
  > RECEIVED MAIN CARGO DOOR ALERT AT FL 390. QRH WAS FOLLOWED AND DIVERTED TO KJAX. NO PRESSURIZATION ISSUES WERE NOTED AT ANY TIME. ALERT WENT AWAY ON DESCENT PASSING FL 240. REVERSED MEL 52-71-01-02. RE-PERFORMED CARGO DOOR PROX TEST RE
- [SDR FDEA202202110749](https://openairdocs.org/sdr/FDEA202202110749.md): None · none · Feb 11, 2022 · N115FE · Boeing 767300 · Emergency Lighting
  > MDIS 115 33-50 6883 11FEB22 BOG DURING POSFLIGHT CHECK FOUND DOOR EMERGENCY LIGHT TOO DIM. FOUND WRONG LAMP INSTALLED. RELAMPED DOOR EMERGENCY LIGHT IAW AMM33-51-03-2 AND PROPER LAMP PART NUMBER IAW IPC 33-51-50-01.
- [SDR FDEA202201140069](https://openairdocs.org/sdr/FDEA202201140069.md): None · sheared · Jan 14, 2022 · N115FE · Boeing 767300 · Wing Miscellaneous Structure
  > REFER TO HUB STRIKE DAMAGE TO LH SLAT UPON INSPECTION OF UNDERLYING STRUCTURE AFTER REMOVAL OF BONDED PANEL ASSY 521ZB, DISCOVERED HOLE IN LEFT WING FIXED LEADING EDGE PANEL. HOLE IS APPROX. 2.5 X 2.0". COMPLIED WITH EA H-5720-T0366424 PART 1. "WING-SECONDA
- [SDR FDEA202104210962](https://openairdocs.org/sdr/FDEA202104210962.md): Transmitter · out of adjust · Apr 21, 2021 · N115FE · Boeing 767300 · Leading Edge Slat Control System
  > LE SLAT DISAGREE ADJUSTED FLAP HANDLE POS. TRANSMITTERS ON TSI 27-80/6190. PERFORMED FLAP AND SLAT PRIMARY DRIVES AND POSITION INDICATING SYSTEM - TEST REF AMM 27-51-00-5. ALL TEST PASSED.
- [SDR FDEA202102170386](https://openairdocs.org/sdr/FDEA202102170386.md): Floor Panel · damaged · Feb 17, 2021 · N115FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241DFF HAS DAMAGE TO SKIN REPAIRED FLOOR PANEL 241DFF PER B767 SRM 53-00-50-2R PARA 4.E
- [SDR FDEA202102170385](https://openairdocs.org/sdr/FDEA202102170385.md): Skin · cracked · Feb 17, 2021 · N115FE · Boeing 7673S2F · Wing, Plate/Skin
  > LH WING, FIXED LEADING EDGE SKIN IS CRACKED @ FASTENER HOLE @ OSS 665 REPAIRED LEADING EDGE SKIN IAW B767 SRM 57-41-01-2R, FIGURE 201
- [SDR FDEA202102160375](https://openairdocs.org/sdr/FDEA202102160375.md): Shear Tie · cracked · Feb 16, 2021 · N115FE · Boeing 7673S2F · Nacelle/Pylon, Main Frame
  > #2 PYLON @ DOOR 447BL, FWD SKIRT BEAM SHEAR TIE IS CRACKED REMOVED AND REPLACED SHEAR TIE PER BAC DWG 313T2310REV -
- [SDR FDEA202102160374](https://openairdocs.org/sdr/FDEA202102160374.md): Beam · cracked · Feb 16, 2021 · N115FE · Boeing 7673S2F · Wing Main, Frame Structure
  > LEFT WING NOSE BEAM IS CRACKED @ OSS 679 REPAIRED NOSE BEAM WEB IAW B767 SRM 57-41-13-2R, RPEIAR 3
- [SDR FDEA202102120343](https://openairdocs.org/sdr/FDEA202102120343.md): Support Angle · cracked · Feb 12, 2021 · N115FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > AS SEEN FROM BULK PIT AREA, SEAT TRACK SUPPORT ANGLE @ STA 1576, INSIDE R/H SIDEWALL AREA IS CRACKED REMOVED AND REPLACED SEAT TRACK SUPPORT ANGLE PER BAC DWG146T5650 REV C.
- [SDR FDEA202102120342](https://openairdocs.org/sdr/FDEA202102120342.md): Support · cracked · Feb 12, 2021 · N115FE · Boeing 7673S2F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SUPPORT ANGLE @ STA 1576, INSIDE L/H SIDEWALL AREA SEAT TRACK SUPPORT ANGLE IS CRACKED REMOVED AND REPLACED SUPPORT ANGLE PER BAC DWG 146T5650 REV C.
- [SDR FDEA202102120338](https://openairdocs.org/sdr/FDEA202102120338.md): Beam · cracked · Feb 12, 2021 · N115FE · Boeing 7673S2F · Wing Main, Frame Structure
  > R/W L/E LOWER NOSE WEB IS CRACKED.(FWD OF FUEL/DEFUEL PANEL 621QB.) REMOVED DAMAGED WEB SECTION AND REPAIRED IAW B767 SRM 57-41-13-2R. TREATED REPAIR AREA IAW B767 SRM 51-21-01.
- [SDR FDEA202102110336](https://openairdocs.org/sdr/FDEA202102110336.md): Floor Panel · delaminated · Feb 11, 2021 · N115FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241WFF HAS FIBER DAMAGE. FABRICATED FLOOR PANEL 241KFF PER SRZ-25-005 REV R.
- [SDR FDEA202102110335](https://openairdocs.org/sdr/FDEA202102110335.md): Floor Panel · delaminated · Feb 11, 2021 · N115FE · Boeing 7673S2F · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 241KFF HAS FIBER DAMAGE FABRICATED NEW FLOOR PANEL PER SRZ-25-005 REV R.
- [SDR FDEA202102100320](https://openairdocs.org/sdr/FDEA202102100320.md): Seal · cracked · Feb 10, 2021 · N115FE · Boeing 7673S2F · Wing Main, Frame Structure
  > LEFT WING FIXED L/E INNER STRAP CRACKED AT L.E.S 555. REMOVED AND REPLACED STRAP AT L.E.S 555 IAW B767 SRM 51-40-02, 51-40-05 AND BAC DWG 114T2800 REV.C
- [SDR FDEA202102090317](https://openairdocs.org/sdr/FDEA202102090317.md): Floor Support · cracked · Feb 9, 2021 · N115FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT FLOOR SUPPORT STRINGER IS CRACKED AT RBL 36.91 AT STA.1480. REMOVED AND REPLACED FLOOR STRINGER SECTION AT RBL 36.91 IAW B767 SRM 51-40-02 AND BAC DWG 146T3002 146T3002 REV.E.
- [SDR FDEA202102070305](https://openairdocs.org/sdr/FDEA202102070305.md): Attach Angle · cracked · Feb 7, 2021 · N115FE · Boeing 7673S2F · Wing, Attach Fittings
  > R/H WING L/E FORMER ATTACH ANGLE CRACKED @ OSS 441 REMOVED CRACKED FORMER ATTACH ANGLE/INSTALLED NEW L/E FORMER ATTACH ANGLE IAW IAW BAC DWG 114T2241 REV-
- [SDR FDEA202102070301](https://openairdocs.org/sdr/FDEA202102070301.md): Former · cracked · Feb 7, 2021 · N115FE · Boeing 7673S2F · Wing Main, Frame Structure
  > LEFT WING L/E FORMER CRACKED @OSS 441 RRMOVED CRACKED FORMER/INSTALLED NEW FORMERIAW BAC DWG114T2241 REV-
- [SDR FDEA202102070307](https://openairdocs.org/sdr/FDEA202102070307.md): Former · cracked · Feb 7, 2021 · N115FE · Boeing 7673S2F · Wing Main, Frame Structure
  > R/H WING L/E FORMER CRACKED @ OSS499 REMOVED CRACKED R/H L/E FORMER/INSTALLED NEW R/H L/E FORMER @ OSS 499
- [SDR FDEA202102070306](https://openairdocs.org/sdr/FDEA202102070306.md): Former · cracked · Feb 7, 2021 · N115FE · Boeing 7673S2F · Wing Main, Frame Structure
  > R/H WING L/E FORMER CRACKED @ OSS 565 REMOVED CRACKED R/H L/E FORMER/INSTALLED NEW R/H L/E FORMER IAW BAC DWG 114T2512 114T2512 REV D
- [SDR FDEA202102070304](https://openairdocs.org/sdr/FDEA202102070304.md): Former · cracked · Feb 7, 2021 · N115FE · Boeing 7673S2F · Wing Main, Frame Structure
  > R/H WING L/E FORMER CRACKED @ OSS 441 REMOVED CRACKED FORMER/INSTALLED NEW FORMER IAW BAC DWG 114T2241 REV-
- [SDR FDEA202102070303](https://openairdocs.org/sdr/FDEA202102070303.md): Former · cracked · Feb 7, 2021 · N115FE · Boeing 7673S2F · Wing Main, Frame Structure
  > L/H WING L/E FORMER CRACKED @ OSS 565 REMOVED CRACKED FORMER/INSTALLED NEW FORMER IAW BAC DWG 114T2162 REV-
- [SDR FDEA202102070302](https://openairdocs.org/sdr/FDEA202102070302.md): Attach Angle · cracked · Feb 7, 2021 · N115FE · Boeing 7673S2F · Wing, Attach Fittings
  > L/H WING L/E FORMER ATTACH ANGLE CRACKED @ OSS 437 REMOVED CRACKED FORMER ATTACH ANGLE/INSTALLED NEW FORMER ATTACH ANGLE IAW BAC DWG 114T2240 REV-
- [SDR FDEA202102070300](https://openairdocs.org/sdr/FDEA202102070300.md): Attach Angle · cracked · Feb 7, 2021 · N115FE · Boeing 7673S2F · Wing, Attach Fittings
  > L/H WING FORMER ATTACH ANGLE CRACKED @OSS441 REMOVED CRACKED FORMER ATTACH ANGLE/INSTALLED NEW ANGLE IAW BAC DWG114T2241,REV-
- [SDR FDEA202102010262](https://openairdocs.org/sdr/FDEA202102010262.md): Flange · cracked · Feb 1, 2021 · N115FE · Boeing 7673S2F · Fuselage Miscellaneous Structure
  > AFT LOWER CARGO PIT STA. 1087 VERTICAL FLANGE BELOW FLOOR LINE AT LBL25 UPPER END IS CRACKED. REMOVED AND REPLACED AFT LOWER CARGO PIT STA.1087 VERTICAL FLANGE BELOW FLOOR LINE AT LBL25 IAW B767 SRM 51- 40-02 AND BAC DWG 140T0130 REV.G.
- [SDR FDEA2019122313277](https://openairdocs.org/sdr/FDEA2019122313277.md): Ecu · malfunctioned · Dec 21, 2019 · N115FE · Boeing 7673S2F · Fuel Control/Turbine Engines
  > CRUISE FL370 SCANNING OVERHEAD PRIOR TO DESCENT. OBSERVED RT EEC ALTN IN MODE SWITCH. NO ACCOMPANY EICAS. REFERENCED QRH, DECIDED TO PUT BOTH EEC IN SAME MODE "ALTN". ACCOMPLISHED QRH. UPON PUSHING THROTTLES UP N1 AND EGT BEGAN FLUXING. FF AT IDLE WOULD N
- [SDR FDEA2018080311862](https://openairdocs.org/sdr/FDEA2018080311862.md): Light · inoperative · Jul 31, 2018 · N115FE · Boeing 7673S2F · Landing Gear Position and Warning
  > UPON LOWERING GEAR HAD NOSE & LEFT GEAR INDICATION BUT NO RIGHT GEAR INDICATION. RAN CHECKLIST FOR GEAR DISAGREE. JUMPSEATER WAS ABLE TO GET US A BULB TO REPLACE AND GEAR SHOWED ALL GREEN. CREW HAD REPLACED 1 BULB ON GO-AROUND, REPLACED OTHER BULB I/R/T MM 33
- [SDR FDEA201803070639](https://openairdocs.org/sdr/FDEA201803070639.md): Module · malfunctioned · Mar 7, 2018 · N115FE · Boeing 7673S2F · Airspeed/Mach Indicator
  > CAPT ALTIMETER INDICATING 300' LOW DURING CLIMB AFTER 18,000' AT FL340 AND AFTER DESCENT TO FL280. ERROR WENT AWAY AFTER 15-20 MINUTES F/O & STBY ALT INDICATED SAME READING. REMOVED AND REPLACED CAPTAINS AIR DATA MODULE PER AM
- [SDR FDEA201710263047](https://openairdocs.org/sdr/FDEA201710263047.md): Switch · failed · Oct 26, 2017 · N115FE · Boeing 7673S2F · Exterior Lighting
  > AFTER FLYING THIS AIRPLANE FOR A COUPLE DAYS IN A ROW, THE SOURSE OF BURNING RUBBER SMELL IS FROM THE RIGHT "RUNWAY TURNOFF" LIGHT. EACH TIME WE TURNED IT ON, WE GOT THE ODER. IT'S NOT THE RIGHT PACK. (RIGHT) RUNWAY TURNOFF LIGHT INOP. R&R RT SIDE RUNWAY TURN
- [SDR FDEA201708172244](https://openairdocs.org/sdr/FDEA201708172244.md): Indicator · inoperative · Aug 17, 2017 · N115FE · Boeing 7673S2F · Landing Gear Position and Warning
  > ALTERNATE GEAR EXTEND WAS USED DUE TO THE RIGHT MLG GEAR INDICATION INOPERATIVE. COMPLIED WITH CHECK OF NOSE AND MLG LOAD LIMITER CLEARANCES, ALL WITHIN LIMITS IAW 32-35-00-5., OK TO CONTINUE.
- [SDR FDEA201708162241](https://openairdocs.org/sdr/FDEA201708162241.md): Lamp · inoperative · Aug 16, 2017 · N115FE · Boeing 7673S2F · Landing Gear Position and Warning
  > RIGHT MAIN GEAR LIGHTS DID NOT WORK ON GEAR EXTENSION. COMPLIED WITH RED TABS. REPLACED THE LAMPS IN THE RIGHT MAIN GEAR DOWN INDICATION IAW 20-84-18. OK TO CONTINUE. REPLACED THE LAMPS IN THE RIGHT RIGHT MAIN GEAR DOWN INDICATOR.
- [SDR FDEA201507202282](https://openairdocs.org/sdr/FDEA201507202282.md): Light · inoperative · Jul 20, 2015 · N115FE · Boeing 7673S2F · Emergency Lighting
  > EXTERNAL EMER LIGHT IS INOPERATIVE, RIGHT BELOW DOOR. RELAMPED EXTERIOR EMER LIGHT IAW AMM33-51-16-2. OPERATIONS CHECKED GOOD.

## 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 = 'N115FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N115FE/reports

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