# Service difficulty reports: N692FE

A list on [N692FE](https://openairdocs.org/aircraft/N692FE.md).

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

Page 1 of 2 · 65 reports

- [SDR FDEA202602200248](https://openairdocs.org/sdr/FDEA202602200248.md): Safety Wire · wrong part · Feb 20, 2026 · N692FE · Airbus A300F4605R · Emergency Equipment
  > L1 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-
- [SDR FDEA202509121903](https://openairdocs.org/sdr/FDEA202509121903.md): Door · not entered · Sep 12, 2025 · N692FE · Airbus A300F4605R · Cargo/Baggage Doors
  > DOORS - 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 O
- [SDR FDEA202510011865](https://openairdocs.org/sdr/FDEA202510011865.md): Skin · contaminated · Sep 8, 2025 · N692FE · Airbus A300F4605R · Elevator, Plate/Skin
  > RIGHT 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 TITLE
- [SDR FDEA202509081864](https://openairdocs.org/sdr/FDEA202509081864.md): Skin · contaminated · Sep 8, 2025 · N692FE · Airbus A300F4605R · Elevator, Plate/Skin
  > RIGHT 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 TITLE
- [SDR FDEA202509081863](https://openairdocs.org/sdr/FDEA202509081863.md): Skin · contaminated · Sep 8, 2025 · N692FE · Airbus A300F4605R · Elevator, Plate/Skin
  > LEFT 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
- [SDR FDEA202509081862](https://openairdocs.org/sdr/FDEA202509081862.md): Skin · contaminated · Sep 8, 2025 · N692FE · Airbus A300F4605R · Elevator, Plate/Skin
  > LH 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 FLUID
- [SDR FDEA202509081692](https://openairdocs.org/sdr/FDEA202509081692.md): Web · no discrepancy · Sep 8, 2025 · N692FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > EXISTING 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 53-15-15-201
- [SDR FDEA202509081690](https://openairdocs.org/sdr/FDEA202509081690.md): Web · not reported · Sep 8, 2025 · N692FE · Airbus A300F4605R · Fuselage Main, Structure
  > EXISTING 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 53-15-15-20
- [SDR FDEA202509051624](https://openairdocs.org/sdr/FDEA202509051624.md): Skin · misrepaired · Sep 5, 2025 · N692FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > EXISTING 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
- [SDR FDEA202509051623](https://openairdocs.org/sdr/FDEA202509051623.md): Repair · not reported · Sep 5, 2025 · N692FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING 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 53-10-16-201
- [SDR FDEA202409281384](https://openairdocs.org/sdr/FDEA202409281384.md): B-Nut · leaking · Sep 28, 2024 · N692FE · Airbus A300F4605R · Hydraulic System, Main
  > GREEN 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. TI
- [SDR FDEA202306151037](https://openairdocs.org/sdr/FDEA202306151037.md): Fitting · cracked · Jun 15, 2023 · N692FE · Airbus A300F4605R · Fuselage Main, Attach Fittings
  > INSPECTION 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 SID
- [SDR FDEA202306111022](https://openairdocs.org/sdr/FDEA202306111022.md): Spoiler · delaminated · Jun 11, 2023 · N692FE · Airbus A300F4605R · Wing Structure
  > LH 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 WI
- [SDR FDEA202306091010](https://openairdocs.org/sdr/FDEA202306091010.md): Skin · dented · Jun 9, 2023 · N692FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > LWR 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 53-10-12-2
- [SDR FDEA202302180297](https://openairdocs.org/sdr/FDEA202302180297.md): None · none · Feb 18, 2023 · N692FE · Airbus A300F4605R · Fire Detection
  > PDIS 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 VALVE
- [SDR FDEA202203160525](https://openairdocs.org/sdr/FDEA202203160525.md): Valve · failed · Mar 16, 2022 · N692FE · Airbus A300* · Cabin Cooling System
  > PDIS 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
- [SDR FDEA202202230349](https://openairdocs.org/sdr/FDEA202202230349.md): Door · malfunctioned · Feb 23, 2022 · N692FE · Airbus A300F4605R · Door Warning System
  > IN 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 DOO
- [SDR FDEA2020080761782](https://openairdocs.org/sdr/FDEA2020080761782.md): Relay · faulted · Aug 6, 2020 · N692FE · Airbus A300F4605R · Cabin Cooling System
  > AFTER 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 SWI
- [SDR FDEA2020071091484](https://openairdocs.org/sdr/FDEA2020071091484.md): Fire Loop · faulted · Jul 9, 2020 · N692FE · Airbus A300F4605R · Fire Detection
  > NR 1 ENGINE LOOP B FAULT PASSING 5000 FT, DURING INITIAL CLIMB. TURNED OFF IAW QRH
- [SDR FDEA201906051222](https://openairdocs.org/sdr/FDEA201906051222.md): Pseu · unknown · Jun 5, 2019 · N692FE · Airbus A300F4605R · Landing Gear Retraction/Extension System
  > PDIS 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 M
- [SDR FDEA201812013407](https://openairdocs.org/sdr/FDEA201812013407.md): Tire · flat · Dec 1, 2018 · N692FE · Airbus A300F4605R · Tire
  > ON 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.
- [SDR FDEA2018080761929](https://openairdocs.org/sdr/FDEA2018080761929.md): Floor Panel · damaged · Aug 6, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL WAS FOUND DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA2018080321911](https://openairdocs.org/sdr/FDEA2018080321911.md): Floor Panel · damaged · Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL 251NG DAMAGED. FABRICATED 251NG FLOOR PANEL ON T18/1357179 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
- [SDR FDEA2018080321910](https://openairdocs.org/sdr/FDEA2018080321910.md): Floor Panel · damaged · Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL 241KJ HAS DAMAGE. FABRICATED 241KJ FLOOR PANEL ON T18/1357173 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
- [SDR FDEA2018080321909](https://openairdocs.org/sdr/FDEA2018080321909.md): Floor Panel · damaged · Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL 231UG HAS DAMAGE. FABRICATED 231UG FLOOR PANEL ON T18/1357175 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
- [SDR FDEA2018080321908](https://openairdocs.org/sdr/FDEA2018080321908.md): Floor Panel · broken · Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 232VH BROKEN. FABRICATED FLOOR PANEL 232VH FLOOR PANEL ON T18-1357563 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
- [SDR FDEA2018080321907](https://openairdocs.org/sdr/FDEA2018080321907.md): Floor Panel · broken · Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 232CF BROKEN. FABRICATED 232CF FLOOR PANEL ON T18/1357550 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
- [SDR FDEA2018080321906](https://openairdocs.org/sdr/FDEA2018080321906.md): Floor Panel · damaged · Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL 241AJ HAS DAMAGE. FABRICATED 241AJ FLOOR PANEL ON T18/1357201 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
- [SDR FDEA2018080321905](https://openairdocs.org/sdr/FDEA2018080321905.md): Floor Panel · damaged · Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL 231ZG HAS DAMAGE. FABRICATED 231ZG FLOOR PANEL ON T18/1357174 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
- [SDR FDEA2018080321904](https://openairdocs.org/sdr/FDEA2018080321904.md): Floor Panel · damaged · Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL 252GH HAS DAMAGE. FABRICATED 252GH FLOOR PANEL ON T18/1357178 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
- [SDR FDEA2018080321903](https://openairdocs.org/sdr/FDEA2018080321903.md): Floor Panel · damaged · Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
  > MCD 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.
- [SDR FDEA2018080321902](https://openairdocs.org/sdr/FDEA2018080321902.md): Floorboard · damaged · Aug 2, 2018 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
  > MCD 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.
- [SDR FDEA201707051858](https://openairdocs.org/sdr/FDEA201707051858.md): Fork · cracked · Jul 5, 2017 · N692FE · Airbus A300F4605R · Cargo/Baggage Doors
  > ON 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.
- [SDR FDEA201703070813](https://openairdocs.org/sdr/FDEA201703070813.md): Skin · bent · Mar 7, 2017 · N692FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT 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 TI
- [SDR FDEA201602290716](https://openairdocs.org/sdr/FDEA201602290716.md): Frame · deformed · Feb 29, 2016 · N692FE · Airbus A300F4605R · Fuselage Main, Frame
  > MAIN 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 2
- [SDR FDEA201602290715](https://openairdocs.org/sdr/FDEA201602290715.md): Frame · deformed · Feb 29, 2016 · N692FE · Airbus A300F4605R · Fuselage Main, Frame
  > MAIN 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 20
- [SDR FDEA201602230674](https://openairdocs.org/sdr/FDEA201602230674.md): Floor Support · corroded · Feb 23, 2016 · N692FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR FDEA201602180619](https://openairdocs.org/sdr/FDEA201602180619.md): Floor Support · corroded · Feb 18, 2016 · N692FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > BULK 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.
- [SDR FDEA201507142224](https://openairdocs.org/sdr/FDEA201507142224.md): Altimeter · failed · Jul 14, 2015 · N692FE · Airbus A300F4605R · Altimeter, Barometric/Encoder
  > ON 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.
- [SDR FDEA201502040432](https://openairdocs.org/sdr/FDEA201502040432.md): Accumulator · leaking · Feb 4, 2015 · N692FE · Airbus A300F4605R · Hydraulic System, Main
  > IN 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 LEAKI
- [SDR FDEA201501220363](https://openairdocs.org/sdr/FDEA201501220363.md): Lug · corroded · Jan 22, 2015 · N692FE · Airbus A300F4605R · Wing, Landing Gear Attach Fittings
  > LEFT 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.
- [SDR FDEA201501220362](https://openairdocs.org/sdr/FDEA201501220362.md): Lug · corroded · Jan 22, 2015 · N692FE · Airbus A300F4605R · Wing, Landing Gear Attach Fittings
  > RIGHT MLG FWD LUG HAS CORROSION & DAMAGE IN BORE & FWD FACE. COMPLIED WITH DWG R57240425 & EA 6-571-T031050 PT1.
- [SDR FDEA201403050449](https://openairdocs.org/sdr/FDEA201403050449.md): Floorbeam · cracked · Mar 5, 2014 · N692FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN CARGO BAY FLOORBEAM CRACKED AT FRAME 48, BL 0-Y-450. REMOVED AND REPLACED THE FLOORBEAM IAW 51-40-21.
- [SDR FDEA201403050448](https://openairdocs.org/sdr/FDEA201403050448.md): Floorbeam · cracked · Mar 5, 2014 · N692FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN CARGO BAY FLOORBEAM CRACKED FRAME 49, BL 0-Y-450. REMOVE AND REPLACED THE CRACKED FLOORBEAM IAW SRM51-40-21.
- [SDR FDEA201403050447](https://openairdocs.org/sdr/FDEA201403050447.md): Floorbeam · cracked · Mar 5, 2014 · N692FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN CARGO BAY FLOORBEAM CRACKED FRAME 50, BL 0-Y450. REMOVE AND REPLACED THE CRACKED FLOORBEAM IAW SRM 51-40-21.
- [SDR FDEA201210183680](https://openairdocs.org/sdr/FDEA201210183680.md): Warning Message · false activation · Oct 18, 2012 · N692FE · Airbus A300F4605R · Drag Control System
  > ON 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 SPOILERS
- [SDR FDEA201201240316](https://openairdocs.org/sdr/FDEA201201240316.md): Brake · failed · Jan 24, 2012 · N692FE · Airbus A300F4605R · Brake
  > TIRE 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 32-42-27
- [SDR FDEA201112295459](https://openairdocs.org/sdr/FDEA201112295459.md): Warning Message · illuminated · Dec 29, 2011 · N692FE · Airbus A300F4605R · Landing Gear Position and Warning
  > AFTER 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
- [SDR FDEA201110124444](https://openairdocs.org/sdr/FDEA201110124444.md): Floor Panel · dented · Oct 12, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN 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.
- [SDR FDEA201110124443](https://openairdocs.org/sdr/FDEA201110124443.md): Floor Panel · dented · Oct 12, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN 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.

Next page: https://openairdocs.org/aircraft/N692FE/reports.md?page=2

## 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 = 'N692FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N692FE/reports

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