N692FE

Service difficulty reports · 65

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 = 'N692FE' 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 FDEA202602200248Safety Wire · wrong partL1 SLIDE ASSY. REPLACE PACKBOARD RELEASE CABLE SAFETY WIRE WITH MS20995C15 STAINLESS STEEL WIRE AND EJECTOR BAG RELEASE CABLE WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. SMIS 25-60/7157, AMM: 25-61-21-04 AMM: 25-61-20-05-01 CMM: 25-60-40 FEA: 6-2560-Feb 20, 2026 · N692FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202509121903Door · not enteredDOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24 COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OSep 12, 2025 · N692FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202510011865Skin · contaminatedRIGHT ELEVATOR UPPER SURFACE 1EA POS FOUND FLUID, AS MARKED (#6 AT RIB20(ER16) SIZE:234MM X 60MM) REPAIRED RH ELEVATOR UPPER SURFACE 1EA POS FLUID(#6 AT RIB20(ER16)) PER A300-600F SRM55-21-12-201 PARA.5.J & SRM51-77-12-201 & EA 6-5520-T0385132 P1. EA TITLESep 8, 2025 · N692FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA202509081864Skin · contaminatedRIGHT ELEVATOR UPPER SURFACE 1EA POS FOUND FLUID, AS MARKED (#6 AT RIB20(ER16) SIZE:234MM X 60MM) REPAIRED RH ELEVATOR UPPER SURFACE 1EA POS FLUID(#6 AT RIB20(ER16)) PER A300-600F SRM55-21-12-201 PARA.5.J & SRM51-77-12-201 & EA 6-5520-T0385132 P1. EA TITLESep 8, 2025 · N692FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA202509081863Skin · contaminatedLEFT ELEVATOR LWR SURFACE 1EA POS FOUND FLUID, #5 AT RIB14 ER10 SIZE:85MMX55MM. REPAIRED LH ELEVATOR LWR SURFACE 1EA POS FLUID (#5 AT RIB14 (ER10)) PER SRM55-21-12-201 PARA.5.J & SRM51-77-12-201 & EA 6-5520-T0385133 P1. EA TITLE: STABILIZERS - ELEVATORS Sep 8, 2025 · N692FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA202509081862Skin · contaminatedLH ELEVATOR UPPER SURFACE 4EA POS FOUND FLUID, AS MARKED (#1 AT RIB20(ER16) SIZE:48MMX35MM, #2 AT RIB 16 (ER13) SIZE: 87MMX67MM, #3 AT RIB 15 (ER10-ER13 )SIZE:70MMX62MM, #4 AT RIB 9(ER6-ER7 ) SIZE:95MMX80MM) REPAIRED LH ELEVATOR UPPER SURFACE 4EA POS FLUIDSep 8, 2025 · N692FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA202509081692Web · no discrepancyEXISTING REPAIR ON MAIN DECK CARGO UNDER FLOOR WEB FR47 BETWEEN Y0 AND Y450 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO UNDER FLOOR WEB BETWEEN Y0 AND Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-15-15-201Sep 8, 2025 · N692FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202509081690Web · not reportedEXISTING REPAIR ON MAIN DECK CARGO UNDER FLOOR WEB FR47 BETWEEN Y0 AND -Y450 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO UNDER FLOOR WEB BETWEEN Y0 AND -Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-15-15-20Sep 8, 2025 · N692FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202509051624Skin · misrepairedEXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR19-FR20A STGR37R-STGR39R REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR19-FR20A STGR37R-STGR39R WAS EVALUATED AND FOUND DID NOT CONFORM TO SRM 53-13-12-201 FIG201, RE-REPAIRED Sep 5, 2025 · N692FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202509051623Repair · not reportedEXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y953 BETWEEN FR36 AND FR38.2 REQUIRES EVALUATION FOR CONFORMITY. THE EXISITNG REPAIR ON MAIN DECK SEAT TRACK AT -Y953 BETWEEN FR36 AND FR 38.2 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-10-16-201Sep 5, 2025 · N692FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202409281384B-Nut · leakingGREEN HYDRO QUANTITY ALERT ON ECAM, INDICATING RED DOT. QUANTITY INDICATION INCREASED TO AND REMAINED JUST ABOVE YELLOW ARC AT GEAR EXTENSION, REMAINING SAME AT SHUTDOWN. FOUND L/H ELEVATOR GREEN SYSTEM HYDRAULIC ACTUATOR LEAKING AT PRESSURE LINE B-NUT. TISep 28, 2024 · N692FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA202306151037Fitting · crackedINSPECTION OF FR40 LOWER WING JUNCTION FASTENER HOLES, RH SIDE, FOUND FASTENER HOLE #3 WITH CRACK SIGNAL. COMPLIED WITH EA: 6-5710-T0374876 P1, TITLE: WINGS - BASIC WING STRUCTURE - FR40RH LOWER JUNCTION LOWER HOLE - CRACK REPAIR. REPAIRED THE FR40 RH SIDJun 15, 2023 · N692FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA202306111022Spoiler · delaminatedLH WING #4 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 40MM*15MM, DEPTH: 1.15MM COMPLIED WITH EA: 6-5750-T0374744 P1. TITLE: WING - FLIGHT SURFACES - LH 4# SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE LH WIJun 11, 2023 · N692FE · Airbus A300F4605R · Wing StructureSDR FDEA202306091010Skin · dentedLWR FUSELAGE SKIN FR67-FR69 STGR50-51RH FOUND DENT REPAIRED THE LWR FUSELAGE SKIN DENT BETWEEN FR67-FR69 STGR50-51RH PER A300-600F SRM53-10-12-101 FIGURE 208. THIS IS CATEGORY B REPAIR. IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI 53-10-12-2Jun 9, 2023 · N692FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202302180297None · nonePDIS 692 26-12 4205 17FEB23 MEM OPEN U WHILE TAKING THE RUNWAY FOR TAKE OFF, ECAM SHOWED A MAIN DECK CARGO MID 2 LOOP FAULT AND THEN A MAIN DECK MID 2 SMOKE DETECTION. PACK 2 FAULTED IMMEDIATELY AND MAIN DECK CARGO VALVE, HOT AIR SUPPLY VALVEFeb 18, 2023 · N692FE · Airbus A300F4605R · Fire DetectionSDR FDEA202203160525Valve · failedPDIS 692 21-50 3348 16MAR22 MEM OPEN U DURING REJECT FOR DOOR OPEN ECAM (AS PREVIOUSLY WRITTEN UP); GOT A NEW ECAM FOR PACK 1 FAULT. COMPLIED WITH ECAM AND QRH. FAULT REMAINED. R/I 17MAR22 15:18 GSP Mar 16, 2022 · N692FE · Airbus A300* · Cabin Cooling SystemSDR FDEA202202230349Door · malfunctionedIN FLIGHT ECAM FOR FWD CARGO DOOR NOT CLOSED. ECAM AND QRH COMPLETED. EMERGENCY DECLARED TO THE TO RETURN TO CYEG AND THE REQUIREMENT TO REMAIN MAX ALT 100 MEA/MORA. ACCOMPLISHED FWD CARGO COMP DOOR ADJUSTMENT/TEST, IAW AMM 52-31-11-05-2. CYCLED FWD CARGO DOOFeb 23, 2022 · N692FE · Airbus A300F4605R · Door Warning SystemSDR FDEA2020080761782Relay · faultedAFTER TAKE OFF, ALL AIRFLOW STOPPED. BOTH PACK FLOW CONTROL VALVES SHOWED CLOSED. CABIN SLOWLY CLIMBED AT 300-400 FPM UNTILL 10,000 CABIN ALTITUDE DURING CLIMB, TRIED RUNNING PACKS IN MANUAL, CYCLED PACK VALVES WITH NO LUCK. CYCLED REGULATOR AND SYS SWIAug 6, 2020 · N692FE · Airbus A300F4605R · Cabin Cooling SystemSDR FDEA2020071091484Fire Loop · faultedNR 1 ENGINE LOOP B FAULT PASSING 5000 FT, DURING INITIAL CLIMB. TURNED OFF IAW QRHJul 9, 2020 · N692FE · Airbus A300F4605R · Fire DetectionSDR FDEA201906051222Pseu · unknownPDIS 692 32-30 0495 05JUN19 MKE OPEN U LOGPAGES:3110219 LANDING GEAR FAILED TO RETRACT IN POSITION DET. #2. POSITION DET #1 WAS ALREADY MEL. RETURNED TO MKE. DID NOT DECLARE AN EMERGENCY. MEL 05JUN19 15:59 MKE U RELEASED FOR SERVICE PER MJun 5, 2019 · N692FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201812013407Tire · flatON ARRIVAL LEFT NOSE TIRE FLAT. DEBRIEF OF CREW. CREW STATED NO ABNORMAL ROLLOUT OR TAXI. NO LEFT PULL FROM NOSE UNTIL TURNING LEFT INTO FINAL PARKING AT GATE. REPLACED BOTH LT AND RT NOSE TIRE AND WHEEL ASSY PER MM 32-41-12-04-01.Dec 1, 2018 · N692FE · Airbus A300F4605R · TireSDR FDEA2018080761929Floor Panel · damagedFLOOR PANEL WAS FOUND DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Aug 6, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018080321911Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 251NG DAMAGED. FABRICATED 251NG FLOOR PANEL ON T18/1357179 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018080321910Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 241KJ HAS DAMAGE. FABRICATED 241KJ FLOOR PANEL ON T18/1357173 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018080321909Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 231UG HAS DAMAGE. FABRICATED 231UG FLOOR PANEL ON T18/1357175 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018080321908Floor Panel · brokenMAIN DECK CARGO FLOOR PANEL 232VH BROKEN. FABRICATED FLOOR PANEL 232VH FLOOR PANEL ON T18-1357563 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018080321907Floor Panel · brokenMAIN DECK CARGO FLOOR PANEL 232CF BROKEN. FABRICATED 232CF FLOOR PANEL ON T18/1357550 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018080321906Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 241AJ HAS DAMAGE. FABRICATED 241AJ FLOOR PANEL ON T18/1357201 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018080321905Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 231ZG HAS DAMAGE. FABRICATED 231ZG FLOOR PANEL ON T18/1357174 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018080321904Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 252GH HAS DAMAGE. FABRICATED 252GH FLOOR PANEL ON T18/1357178 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018080321903Floor Panel · damagedMCD FLOOR PANEL 251BH DAMAGED. FABRICATED 251BH FLOOR PANEL ON 18/1357176 IAW DWG SRZ 25-005 REV N. REPAIR IS CLASSIFED AS CAT "A" AND MAJOR REPAIR.Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2018080321902Floorboard · damagedMCD FLOOR PANEL 262YF HAS DAMAGE. FABRICATED 262YF FLOOR PANEL ON T18/1357177 IAW DWG SRZ 25-005 REV N. REPAIR IS CLASSIFIED AS CAT "A" AND MAJOR REPAIR.Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201707051858Fork · crackedON AFT CARGO DOOR LATCH AND DOOR FRAME FORKS INSPECTION. CRACKS NOTED IN HOLE LOCATIONS 5 AND 6 OF FRAME FORK 61. REMOVED AND REPLACED WITH NEW DOOR.Jul 5, 2017 · N692FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201703070813Skin · bentLEFT WING OTBD AFT FLAP TRAILING EDGE HAS BENT SKIN EVALUATED DENT AND FOUND TO BE WITHIN LIMITS IAW A300 SRM 57-50-00 SHEET 4 FIG 103 L=1.2 ,W=1.1, D=.070 MAX DEPTH ALLOWED IS .150 ( TR85723) HFEC AREA IAW A300 NTM 51-10- 08 NO CRACK INDICATION NOTED AT TIMar 7, 2017 · N692FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201602290716Frame · deformedMAIN DECK FRAME 59, STRINGER 12 - 13 LT, FRAME DEFORMED & CHAFED. BLEND OUT THE CHAFED AREA PER SRM51-73-10, THE REMAINING THICKNESS WITHIN THE DESIGN TOLERANCE PER DWG A53970111 , REPAIRED THE DEFORMED FRAME OF MAIN DECK FR59 STG 12-13L PER SRM53-10-13 FIG 2Feb 29, 2016 · N692FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201602290715Frame · deformedMAIN DECK FRAME 58, STRINGER 12 - 14 LT, FRAME DEFORMED & CHAFED. BLEND OUT THE CHAFED AREA PER SRM51-73-10, THE REMAINING THICKNESS WITHIN THE DESIGN TOLERANCE PER DWG A53970111, REPAIRED THE DEFORMED FRAME OF MAIN DECK FR58 STG 12-14L PER SRM53-10-13 FIG 20Feb 29, 2016 · N692FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201602230674Floor Support · corrodedMAIN DECK FRAME 11 - 14, Y730 FLOOR SUPPORT CORRODED. R & R THE FLOOR SUPPORT IAW SRM 51-40-21 AND DWG A53612214000. MAJOR REPAIR IAW GMM 6-2-100.Feb 23, 2016 · N692FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201602180619Floor Support · corrodedBULK CARGO, FRAME 66, Y140, FLOOR SUPPORT WITH INNER GRANULAR CORROSION. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21 & DWG A5397426220600. MAJOR REPAIR IAW GMM 6-2-100.Feb 18, 2016 · N692FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201507142224Altimeter · failedON TAKEOFF FROM SEA LEVEL AIRPORT, CAPTAIN`S ALTIMETER FROZE AT 00 FEET. MOVING ALTIMETER SETTING KNOB HAD NO EFFECT. STAYED FROZEN UNTIL TAXI IN 2 MINUTES FROM BLOCK-IN. R & R CAPTAINS ALTIMETER IAW AMM 34-12-21-04. CHECKED OK.Jul 14, 2015 · N692FE · Airbus A300F4605R · Altimeter, Barometric/EncoderSDR FDEA201502040432Accumulator · leakingIN CRUISE, YELLOW HYD PUMP LO PRESS. FOLLOWED QRH, SECURED PUMP, FLUID LEVEL JUST ABOVE RED DOT FOR RAT SYS. ON APPROACH, ACTIVATED PTU IAW QRH. AFFECTED EQUIPMENT NOT RESTORED, LANDED WITH MULTIPLE COMPONENTS OFF. FOUND YELLOW SYS ACCUMULATOR TO BE LEAKIFeb 4, 2015 · N692FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201501220363Lug · corrodedLEFT MLG FWD LUG HAS CORROSION & DAMAGE IN BORE. COMPLIED WITH REPAIR DWG R57240425 & EA 6-5710-T0315053 PT 1. CLASSIFIED AS A CAT C MAJOR REPAIR.Jan 22, 2015 · N692FE · Airbus A300F4605R · Wing, Landing Gear Attach FittingsSDR FDEA201501220362Lug · corrodedRIGHT MLG FWD LUG HAS CORROSION & DAMAGE IN BORE & FWD FACE. COMPLIED WITH DWG R57240425 & EA 6-571-T031050 PT1.Jan 22, 2015 · N692FE · Airbus A300F4605R · Wing, Landing Gear Attach FittingsSDR FDEA201403050449Floorbeam · crackedMAIN CARGO BAY FLOORBEAM CRACKED AT FRAME 48, BL 0-Y-450. REMOVED AND REPLACED THE FLOORBEAM IAW 51-40-21.Mar 5, 2014 · N692FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201403050448Floorbeam · crackedMAIN CARGO BAY FLOORBEAM CRACKED FRAME 49, BL 0-Y-450. REMOVE AND REPLACED THE CRACKED FLOORBEAM IAW SRM51-40-21.Mar 5, 2014 · N692FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201403050447Floorbeam · crackedMAIN CARGO BAY FLOORBEAM CRACKED FRAME 50, BL 0-Y450. REMOVE AND REPLACED THE CRACKED FLOORBEAM IAW SRM 51-40-21.Mar 5, 2014 · N692FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201210183680Warning Message · false activationON TAKEOFF ROLL, HAD ECAM AMBER ALERT. REJECTION WAS PREFORMED. DURING REJECT, ECAM ALERT RESET. ONLY ITEM NOTICED ON ECAM BEFORE IT RESET WAS THE WORD "SPOILERS". AT BLOCK IN CREW REPORTED NORMAL FLIGHT AFTER REJECT TAKEOFF. CHECKED MOVEMENT OF SPOILERSOct 18, 2012 · N692FE · Airbus A300F4605R · Drag Control SystemSDR FDEA201201240316Brake · failedTIRE BLOWN OUT DURING LANDING. PERFORMED INSPECTION AFTER BRAKE OVERHEAT AS PER AMM 05-51-16-00 STEP C2. REMOVED AND REPLACED WHEELS AND BRAKES IAW AMM 12-37-32 AND AMM 32-42-27Jan 24, 2012 · N692FE · Airbus A300F4605R · BrakeSDR FDEA201112295459Warning Message · illuminatedAFTER TAKEOFF, ECAM WARNING "LANDING GEAR RETRACTION INOP". ECAM DIRECTED "L/G LEVER DOWN, MAX SPEED 270 KTS, AUTOBRAKE DISARM", THEN "PROC FUEL CONSUMPTION INCREASED" ALSO RECEIVED "WINDSHEAR ALERT NOT AVAILABLE" AND "AUTO THROTTLES DISARMED". ALSO "ALPHA Dec 29, 2011 · N692FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA201110124444Floor Panel · dentedMAIN DECK CARGO COMPARTMENT AFT AREA FLOOR PANEL NR 252JF FOUND WITH DENT AT FRAME 57.3, RBL 60. FLOOR PANEL REPAIRED AS PER SRM 53-10-20 REV 21. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 113.Oct 12, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201110124443Floor Panel · dentedMAIN DECK CARGO COMPARTMENT AFT AREA FLOOR PANEL NR 252PG FOUND WITH DENT AT FRAME 57.3, RBL 20. FLOOR PANEL REPAIRED AS PER SRM 53-10-20 REV 21. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 113.Oct 12, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
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