N122FE

Service difficulty reports · 37

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA202610031487Seat Track · brokenDURING 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, ROct 3, 2026 · N122FE · Boeing 7673S2F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202506180987Warning Light · false activationON 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 Jun 18, 2025 · N122FE · Boeing 7673S2F · Leading Edge Slat Position Indicating SystemSDR FDEA202504200622Stringer Splice · not reportedCOMPLY 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 SApr 20, 2025 · N122FE · Boeing 7673S2F · Fuselage Main, Longeron/StringerSDR FDEA202504200621Stringer Splice · not reportedCOMPLY 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 SApr 20, 2025 · N122FE · Boeing 7673S2F · Fuselage Main, Longeron/StringerSDR FDEA202305300973Door · gouged#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"May 30, 2023 · N122FE · Boeing 767300 · Engine Thrust ReverserSDR FDEA202305260951Frame · cracked#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.May 26, 2023 · N122FE · Boeing 767300 · Nacelle/Pylon, Main FrameSDR FDEA202305260947Angle · crackedMAIN 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 CMay 26, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous StructureSDR FDEA202305260946Angle · crackedMAIN 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 CMay 26, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous StructureSDR FDEA202305260945Angle · crackedMAIN 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 CMay 26, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous StructureSDR FDEA202305260944Angle · crackedMAIN 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 CMay 26, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous StructureSDR FDEA202305240935Angle · crackedMAIN 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 CMay 24, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous StructureSDR FDEA202305240934Angle · crackedMAIN 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 CMay 24, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous StructureSDR FDEA202305240933Angle · crackedMAIN 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 CMay 24, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous StructureSDR FDEA202305240932Angle · crackedMAIN 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 CMay 24, 2023 · N122FE · Boeing 767300 · Fuselage Miscellaneous StructureSDR FDEA202305220914Slat · chafed#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.May 22, 2023 · N122FE · Boeing 767300 · Leading Edge DevicesSDR FDEA202305220913Flap · damagedLW 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.May 22, 2023 · N122FE · Boeing 767300 · Trailing Edge FlapsSDR FDEA202305220912Flap · damagedRH 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.May 22, 2023 · N122FE · Boeing 767300 · Trailing Edge FlapsSDR FDEA202305200911Slat · gougedRIGHT 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.May 20, 2023 · N122FE · Boeing 767300 · Leading Edge DevicesSDR FDEA202305190910Flap · chafedRIGHT 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.May 19, 2023 · N122FE · Boeing 767300 · Trailing Edge FlapsSDR FDEA202305190909Flap · gougedRIGHT 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.May 19, 2023 · N122FE · Boeing 767300 · Trailing Edge FlapsSDR FDEA202305190908Flap · gougedRIGHT 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.May 19, 2023 · N122FE · Boeing 767300 · Trailing Edge FlapsSDR FDEA202305190907Slat · chafed#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.May 19, 2023 · N122FE · Boeing 767300 · Leading Edge DevicesSDR FDEA202305190906Slat · chafed#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.May 19, 2023 · N122FE · Boeing 767300 · Leading Edge DevicesSDR FDEA202209012133None · noneAT 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 DECLAREDSep 1, 2022 · N122FE · Boeing 767300 · Fuel Indicating SystemSDR FDEA202209012134Warning Message · activatedAT 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 DECLAREDSep 1, 2022 · N122FE · Boeing 7673S2F · Fuel Indicating SystemSDR FDEA202207311834Beam · chafed#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.Jul 31, 2022 · N122FE · Boeing 767300 · Nacelle/Pylon, Main FrameSDR FDEA202207301849Beam · chafed#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 PERFORMEDJul 30, 2022 · N122FE · Boeing 767300 · Nacelle/Pylon, Main FrameSDR FDEA202112042990None · noneLIGHTNING 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 LDec 4, 2021 · N122FE · Boeing 767300 · Fuselage Structure (General)SDR FDEA201911012813Fseu · malfunctionedLE 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 Nov 1, 2019 · N122FE · Boeing 7673S2F · Leading Edge Slat Control SystemSDR FDEA2018122433597Lamp · inoperativeL1 DOOR SLIDE EMERGENCY EXIT LIGHT INOP. RE-LAMPED, GRND CKS NORMAL.Dec 23, 2018 · N122FE · Boeing 7673S2F · Emergency LightingSDR FDEA201709262724Floor Panel · delaminatedFLOOR PANEL 141T5856-107 HAS DELAM. FABRICATED NEW FLOOR PANEL 141T5856-107 ON T17/1297035, PER SRZ 25-005, REV M. MAJOR REPAIR.Sep 26, 2017 · N122FE · Boeing 7673S2F · Fuselage Floor PanelSDR FDEA201703170946Switch · stuckDURING 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 Mar 17, 2017 · N122FE · Boeing 7673S2F · Flight Compartment LightingSDR FDEA201608283101Fitting · out of positionFOUND 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 POAug 28, 2016 · N122FE · Boeing 7673S2F · Fire Bottle, PortableSDR FDEA201608263102Fitting · out of positionFOUND 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.Aug 26, 2016 · N122FE · Boeing 7673S2F · Fire Bottle, PortableSDR FDEA201511083518Support Angle · crackedWHILE 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.Nov 8, 2015 · N122FE · Boeing 7673S2F · Cargo/Baggage DoorsSDR FDEA201511033455Probe · damagedABORTED 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 IANov 3, 2015 · N122FE · Boeing 7673S2F · Pitot/Static SystemSDR FDEA201510013035Oxygen Mask · failedDURING 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 SEOct 1, 2015 · N122FE · Boeing 7673S2F · Crew Oxygen System
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