# Service difficulty reports: N122FE

A list on [N122FE](https://openairdocs.org/aircraft/N122FE.md).

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

- [SDR FDEA202610031487](https://openairdocs.org/sdr/FDEA202610031487.md): Seat Track · broken · Oct 3, 2026 · N122FE · Boeing 7673S2F · Fuselage, Seat/Cargo Attach Fittings
  > DURING UNLOADING, RAMP CREW REPORTED THE MDC LOCK (ID: H503) FLOOR SEAT TRACK IS BROKEN. COMPLIED WITH EA H-5310-T0388991 REPAIRED THE BROKEN MAIN DECK FLOOR CARGO RBL11 SEAT TRACK BETWEEN BS 588 & 654. MAIN DECK FLOOR CARGO TRACK REPAIR IAW SRM 53-00-52, R
- [SDR FDEA202506180987](https://openairdocs.org/sdr/FDEA202506180987.md): Warning Light · false activation · Jun 18, 2025 · N122FE · Boeing 7673S2F · Leading Edge Slat Position Indicating System
  > ON A 10 MILE FINAL WITH THE GEAR DOWN, WE SELECTED FLAPS 25 AND GOT A MASTER CAUTION, LE SLAT DISAGREE LIGHT. WE ELECTED TO DO A GO AROUND AND SELECTED FLAPS 20 AND RAISED THE GEAR AND THE CAUTION LIGHT EXTINGUISHED. WE CAME BACK AROUND AND REATTEMPTED A
- [SDR FDEA202504200622](https://openairdocs.org/sdr/FDEA202504200622.md): Stringer Splice · not reported · Apr 20, 2025 · N122FE · Boeing 7673S2F · Fuselage Main, Longeron/Stringer
  > COMPLY WITH FEDEX EO:H-5310-E0365800 A P2 FOR INSTALL THE SPLICE FITTINGS ON S-20R AT STA 1506, STA 1530, STA 1552. COMPLIED WITH FEDEX EO: H-5310-E0365800 A P2, TITLE: FUSELAGE - MAINFRAME - INSTALLATION OF SPLICE FITTING ON STRINGERS S-20L AND S-20R AT S
- [SDR FDEA202504200621](https://openairdocs.org/sdr/FDEA202504200621.md): Stringer Splice · not reported · Apr 20, 2025 · N122FE · Boeing 7673S2F · Fuselage Main, Longeron/Stringer
  > COMPLY WITH FEDEX EO:H-5310-E0365800 A P1 FOR INSTALL THE SPLICE FITTINGS ON S-20L AT STA 1506, STA 1530, STA 1552. COMPLIED WITH FEDEX EO: H-5310-E0365800 A P1, TITLE: FUSELAGE - MAINFRAME - INSTALLATION OF SPLICE FITTING ON STRINGERS S-20L AND S-20R AT S
- [SDR FDEA202305300973](https://openairdocs.org/sdr/FDEA202305300973.md): Door · gouged · May 30, 2023 · N122FE · Boeing 767300 · Engine Thrust Reverser
  > #1 ENGINE I/B T/R LOWER FWD PANEL INNER SURFACE HAS 2EA GOUGES AS MARKED REPAIRED #1 ENGINE, INBOARD TR, FWD BLOWOUT DOOR IAW FEDEX EA# H-7830-T0374581-P1, TITLED " EXHAUST SYSTEM - THRUST REVERSER GEN - #1 INBD TR, BLOWOUT DOOR, GOUGE"
- [SDR FDEA202305260951](https://openairdocs.org/sdr/FDEA202305260951.md): Frame · cracked · May 26, 2023 · N122FE · Boeing 767300 · Nacelle/Pylon, Main Frame
  > #1 PYLON, HYDRAULIC BAY, OUTBOARD MID SPAR FITTING IS CRACKED REPAIRED #1 PYLON, AFT FAIRING ASSY, NAC STA 329 MID SPAR FRAME IAW B767 SRM 54-52-71- 2R, REPAIR 4.
- [SDR FDEA202305260947](https://openairdocs.org/sdr/FDEA202305260947.md): Angle · cracked · May 26, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, RBL 68 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-8, WO# 85583, NR# N00127. PER BOEING DWG 146T5651, SHT 5, REV C
- [SDR FDEA202305260946](https://openairdocs.org/sdr/FDEA202305260946.md): Angle · cracked · May 26, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, RBL 65 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-6, WO# 85583, NR# N00112. PER BOEING DWG 146T5651, SHT 5, REV C
- [SDR FDEA202305260945](https://openairdocs.org/sdr/FDEA202305260945.md): Angle · cracked · May 26, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, LBL 65 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-5, WO# 85583, NR# N00113. PER BOEING DWG 146T5651, SHT 5, REV C
- [SDR FDEA202305260944](https://openairdocs.org/sdr/FDEA202305260944.md): Angle · cracked · May 26, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, LBL 68 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-7, WO# 85583, NR# N00128. PER BOEING DWG 146T5651, SHT 5, REV C
- [SDR FDEA202305240935](https://openairdocs.org/sdr/FDEA202305240935.md): Angle · cracked · May 24, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, RBL 65 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-6, WO# 85583, NR# N00112. PER BOEING DWG 146T5651, SHT 5, REV C
- [SDR FDEA202305240934](https://openairdocs.org/sdr/FDEA202305240934.md): Angle · cracked · May 24, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, RBL 68 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-8, WO# 85583, NR# N00127. PER BOEING DWG 146T5651, SHT 5, REV C
- [SDR FDEA202305240933](https://openairdocs.org/sdr/FDEA202305240933.md): Angle · cracked · May 24, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, LBL 65 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-5, WO# 85583, NR# N00113. PER BOEING DWG 146T5651, SHT 5, REV C
- [SDR FDEA202305240932](https://openairdocs.org/sdr/FDEA202305240932.md): Angle · cracked · May 24, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR PANEL SUPPORT IS CRACKED AT APPROX. STA 1575, LBL 68 REMOVED CRACKED SUPPORT ANGLE AND INSTALLED FABRICATED SUPPORT ANGLE, 146T5651-7, WO# 85583, NR# N00128. PER BOEING DWG 146T5651, SHT 5, REV C
- [SDR FDEA202305220914](https://openairdocs.org/sdr/FDEA202305220914.md): Slat · chafed · May 22, 2023 · N122FE · Boeing 767300 · Leading Edge Devices
  > #5 SLAT WEDGE LOWER SKIN CHAFFED THROUGH AT AREA OF OBRD MAIN TRACK. REPAIRED #5 SLAT WEDGE LOWER SKIN CHAFFED THROUGH AT AREA OUTBOARD MAIN TRACK WITH PERMANENT REPAIR IAW B767 SRM 57-43-02-2R FIG 201 SHEET 1 AND 51-70-10-2R REPAIR 4.
- [SDR FDEA202305220913](https://openairdocs.org/sdr/FDEA202305220913.md): Flap · damaged · May 22, 2023 · N122FE · Boeing 767300 · Trailing Edge Flaps
  > LW INBOARD MAIN FLAP, UPPER SKIN HAS DAMAGE ON OB EDGE. REPAIRED LW INBOARD MAIN FLAP, UPPER SURFACE SKIN IAW FED EX EA H-5750-T0374477-P1- WING-FLIGHT SURFACES-LH INBD MAIN FLAP, FRANGIBLE STRUCTURE ASSY UPPER SKIN, NICK.
- [SDR FDEA202305220912](https://openairdocs.org/sdr/FDEA202305220912.md): Flap · damaged · May 22, 2023 · N122FE · Boeing 767300 · Trailing Edge Flaps
  > RH WING INBD MAIN FLAP UPPER SURFACE HAS EDGE DAMAGE ON OUTBD END. REPAIRED RH WING INBD MAIN FLAP UPPER SURFACE ON OUTBD END IAW FED EX EA H-5750- T0374487-P1-WING-FLIGHT SURFACES-RH INBD MAIN FLAP, FRANGIBLE STRUCTURE ASSY UPPER SKIN NICK.
- [SDR FDEA202305200911](https://openairdocs.org/sdr/FDEA202305200911.md): Slat · gouged · May 20, 2023 · N122FE · Boeing 767300 · Leading Edge Devices
  > RIGHT WING #8 SLAT TRAILING EDGE LOWER SKIN HAS 2 GOUGES. REPAIRED RIGHT WING #8 SLAT LOWER SKIN IAW B767 SRM 57-43-02-1A AND 51-70-10-2R.
- [SDR FDEA202305190910](https://openairdocs.org/sdr/FDEA202305190910.md): Flap · chafed · May 19, 2023 · N122FE · Boeing 767300 · Trailing Edge Flaps
  > RIGHT WING INBOARD FLAP LOWER SURFACE HAS CHAFFING WEAR MARKS ON EACH SIDE OF #6 FLAP FAIRING REPAIRED RIGHT WING INBOARD FLAP LOWER SKIN IAW B767 SRM 57-53-01-2R AND 51-70-03-0G.
- [SDR FDEA202305190909](https://openairdocs.org/sdr/FDEA202305190909.md): Flap · gouged · May 19, 2023 · N122FE · Boeing 767300 · Trailing Edge Flaps
  > RIGHT WING INBOARD AFT FLAP HAS EDGE DAMAGE ON TRAILING EDGE UPPER SURFACE. REPAIRED RIGHT WING INBOARD AFT FLAP IAW B767 SRM 57-53-01-2R AND 51-70-10-2R.
- [SDR FDEA202305190908](https://openairdocs.org/sdr/FDEA202305190908.md): Flap · gouged · May 19, 2023 · N122FE · Boeing 767300 · Trailing Edge Flaps
  > RIGHT WING INBOARD AFT FLAP HAS EDGE DAMAGE ON TRAILING EDGE UPPER SURFACE. REPAIRED RIGHT WING INBOARD AFT FLAP IAW B767 SRM 57-53-01-2R AND 51-70-10-2R.
- [SDR FDEA202305190907](https://openairdocs.org/sdr/FDEA202305190907.md): Slat · chafed · May 19, 2023 · N122FE · Boeing 767300 · Leading Edge Devices
  > #5 SLAT WEDGE LOWER SKIN CHAFFED THROUGH AT AREA OF INBOARD AUX. TRACK. REPAIRED #5 SLAT WEDGE LOWER SKIN IAW B767 SRM 57-43-02-2R AND 51-70-10-2R.
- [SDR FDEA202305190906](https://openairdocs.org/sdr/FDEA202305190906.md): Slat · chafed · May 19, 2023 · N122FE · Boeing 767300 · Leading Edge Devices
  > #4 SLAT WEDGE LOWER SKIN CHAFFED THROUGH AT AREA OF INBOARD ACTUATOR CONTROL ROD. REPAIRED #4 SLAT WEDGE LOWER SKIN IAW B767 SRM 57-43-02-2R AND 51-70-10-2R.
- [SDR FDEA202209012133](https://openairdocs.org/sdr/FDEA202209012133.md): None · none · Sep 1, 2022 · N122FE · Boeing 767300 · Fuel Indicating System
  > AT CRUISE FL380 RECEIVED FUEL CONFIG EICAS AND FUEL CONFIG AMBER LIGHT ON FUEL PANEL. FUEL LEVEL WAS ABOUT 4K LOWER IN RIGHT MAIN THAN LEFT MAIN, RAN QRH PROCEDURE, RIGHT ENGINE SHUT DOWN PER QRH, DECLARED EMERGENCY DIVERTED TO KBNA. ***EMERGENCY DECLARED
- [SDR FDEA202209012134](https://openairdocs.org/sdr/FDEA202209012134.md): Warning Message · activated · Sep 1, 2022 · N122FE · Boeing 7673S2F · Fuel Indicating System
  > AT CRUISE FL380 RECEIVED FUEL CONFIG EICAS AND FUEL CONFIG AMBER LIGHT ON FUEL PANEL. FUEL LEVEL WAS ABOUT 4K LOWER IN RIGHT MAIN THAN LEFT MAIN, RAN QRH PROCEDURE, RIGHT ENGINE SHUT DOWN PER QRH, DECLARED EMERGENCY DIVERTED TO KBNA. ***EMERGENCY DECLARED
- [SDR FDEA202207311834](https://openairdocs.org/sdr/FDEA202207311834.md): Beam · chafed · Jul 31, 2022 · N122FE · Boeing 767300 · Nacelle/Pylon, Main Frame
  > #1 ENG INBD PANEL 436CR HAS A LOOSE NUTPLATE THAT HAS WORN INTO THE STRUT FAIRING BEAM. REPAIRED #1 ENGINE INBD SKIRT BEAM AT FOWARD END REF 767 SRM 54-52-71-2R FIG 203 REPAIR 3 PAGE 15 AND 767 SRM 51-40-03-0G.
- [SDR FDEA202207301849](https://openairdocs.org/sdr/FDEA202207301849.md): Beam · chafed · Jul 30, 2022 · N122FE · Boeing 767300 · Nacelle/Pylon, Main Frame
  > #1 ENGINE, PYLON PANEL 437BR HAS WORN HINGES. MWT 0000481208: MEYER, LONNY W - 03-AUG-2022 10:53 SKIRT PANEL WAS REMOVED AND BUSHINGS REPLACED REF 767 SRM 51-40-02, SEE JPF FOR MAINTENANCE PERFORMED
- [SDR FDEA202112042990](https://openairdocs.org/sdr/FDEA202112042990.md): None · none · Dec 4, 2021 · N122FE · Boeing 767300 · Fuselage Structure (General)
  > LIGHTNING STRIKE APPROX. STA 532, STR 39L. MWT 0000530614: TURCOTTE, GARRETT S - 05-DEC-2021 15:18 INSTALLED REPAIR DOUBLER REF 767 SRM 53-00-01-2R REPAIR 1 AT SAT 532 STR 39 L
- [SDR FDEA201911012813](https://openairdocs.org/sdr/FDEA201911012813.md): Fseu · malfunctioned · Nov 1, 2019 · N122FE · Boeing 7673S2F · Leading Edge Slat Control System
  > LE SLAT DISAGREE ON FINAL. AFTER GO AROUND AND QRH, EICAS WENT AWAY FOR NORMAL CONFIGURATION AT LANDING. NO STATUS MESSAGE. FSEU SHOWED INTERMITTENT FAULTS WITH DIFFERENT CODES. R & R THE FSEU IAW AMM 27-51-01-4 & BITE CHECKED IAW FIM 27-51, FAULT TREE
- [SDR FDEA2018122433597](https://openairdocs.org/sdr/FDEA2018122433597.md): Lamp · inoperative · Dec 23, 2018 · N122FE · Boeing 7673S2F · Emergency Lighting
  > L1 DOOR SLIDE EMERGENCY EXIT LIGHT INOP. RE-LAMPED, GRND CKS NORMAL.
- [SDR FDEA201709262724](https://openairdocs.org/sdr/FDEA201709262724.md): Floor Panel · delaminated · Sep 26, 2017 · N122FE · Boeing 7673S2F · Fuselage Floor Panel
  > FLOOR PANEL 141T5856-107 HAS DELAM. FABRICATED NEW FLOOR PANEL 141T5856-107 ON T17/1297035, PER SRZ 25-005, REV M. MAJOR REPAIR.
- [SDR FDEA201703170946](https://openairdocs.org/sdr/FDEA201703170946.md): Switch · stuck · Mar 17, 2017 · N122FE · Boeing 7673S2F · Flight Compartment Lighting
  > DURING GEAR DOWN LIGHT CHECK PRESSED LIGHTS TEST SWITCH AND ALL LIGHT STUCK IN THE TEST MODE. UNABLE TO CHANGE RADIO FRQ'S ETC. AFTER LANDING, WE COULD CYCLE THE TEST BUTTON SEVERAL TIMES AND WERE ABLE TO EXTINGUISH THE TEST LIGHTS FUNCTION. ACCOMPLISHED TEST
- [SDR FDEA201608283101](https://openairdocs.org/sdr/FDEA201608283101.md): Fitting · out of position · Aug 28, 2016 · N122FE · Boeing 7673S2F · Fire Bottle, Portable
  > FOUND HAZCAN FIRE EXTINGUISHER FITTINGS IN THE WRONG POSITION IAW DWG B67-26-001, SHEET 4. MOVED HAZCAN FIRE EXTINGUISHER FITTINGS TO THE CORRECT POSITION IAW DWG B67-26-001, SHEET 4. OK FOR SERVICE. MOVED HAZCAN FIRE EXTINGUISHER FITTINGS TO THE CORRECT PO
- [SDR FDEA201608263102](https://openairdocs.org/sdr/FDEA201608263102.md): Fitting · out of position · Aug 26, 2016 · N122FE · Boeing 7673S2F · Fire Bottle, Portable
  > FOUND HAZCAN FIRE EXTINGUISHER FITTINGS IN THE WRONG POSITION IAW DWG B67-26-001, SHEET 4. MOVED HAZCAN FIRE EXTINGUISHER FITTINGS TO THE CORRECT POSITION IAW DWG B67-26-001 SHEET 4. OK FOR SERVICE.
- [SDR FDEA201511083518](https://openairdocs.org/sdr/FDEA201511083518.md): Support Angle · cracked · Nov 8, 2015 · N122FE · Boeing 7673S2F · Cargo/Baggage Doors
  > WHILE REPAIRING LOWER AFT CARGO DOOR UPPER SEAL RETAINER, REF WRI 52-30/0336, FOUND FORM ANGLE CRACK, PICTURES ATTACHED. CUT OUT DAMAGED AREA OF SUPPORT ANGLE & DOOR SEAL RETAINER CHANNEL. IAW SRM 51-70-11-0G FABRICATED NEW SECTION OF SUPPORT ANGLE FILLER.
- [SDR FDEA201511033455](https://openairdocs.org/sdr/FDEA201511033455.md): Probe · damaged · Nov 3, 2015 · N122FE · Boeing 7673S2F · Pitot/Static System
  > ABORTED TAKEOFF ROLL AT 85 KTS. CAPTAINS AIRSPEED INDICATOR REMAINED AT 30 KTS, NEVER INCREASED FROM STATIC. FIRST OFFICERS AIRSPEED INDICATOR READ 85 KTS AT REJECT, QRH REVIEWED. PITOT TUBE COVERS WERE NOT INSTALLED. REMOVED CAPTAINS PITOT STATIC PROBE IA
- [SDR FDEA201510013035](https://openairdocs.org/sdr/FDEA201510013035.md): Oxygen Mask · failed · Oct 1, 2015 · N122FE · Boeing 7673S2F · Crew Oxygen System
  > DURING IN FLIGHT USE OF FIRST OFFICERS O2 MASK, NOTICED THERE WAS RESTRICTION TO AIRFLOW DRAW & A PULSED DELIVERY. CONSTANT EMER FLOW WOULD NOT WORK. SWAPPED WITH JUMP SEAT POSITION MASK & OPERATIONS CHECKED NORMAL. REMOVED INOPERATIVE MASK & INSTALLED A SE

## 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 = 'N122FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N122FE/reports

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