# Service difficulty reports: N669FE

A list on [N669FE](https://openairdocs.org/aircraft/N669FE.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 7 · 320 reports

- [SDR FDEA202604200487](https://openairdocs.org/sdr/FDEA202604200487.md): Elevator · not required · Apr 20, 2026 · N669FE · Airbus A300F4605R · Elevator Structure
  > EXISTING REPAIR ON RH ELEVATOR OUTBOARD OF ER2 85MM & IN FRONT OF T/E 810MM UPPER SKIN REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON RH ELEVATOR OUTBOARD OF ER2 85MM & IN FRONT OF T/E 810MM UPPER SKIN WAS EVALUATED AND FOUND IN CONFORMITY WIT
- [SDR FDEA202604190482](https://openairdocs.org/sdr/FDEA202604190482.md): Hinge Arm · delaminated · Apr 19, 2026 · N669FE · Airbus A300F4605R · Spoilers
  > RH WING #4 SPOILER CENTER HINGE ARM INBD ARM OUTBD SURFACE FOUND 2EA DELAMINATION (65MM*50MM*1.42MM,35MM*26MM*1.26MM). COMPLIED WITH EA 6-5750-T0387084 P1 REPAIRED THE DELAMINATION ON RH WING #4 SPOILER CENTER INBD HINGE ARM OUTBD SURFACE. EA TITLE: WING
- [SDR FDEA202604180486](https://openairdocs.org/sdr/FDEA202604180486.md): Fitting · cracked · Apr 18, 2026 · N669FE · Airbus A300F4605R · Fuselage Structure (General)
  > UPPER FUSELAGE - RH "N" HOLD FOUND CRACKED AT FR47 BTW STGR25 AND STGR26. REPAIRED THE CRACKED RH HOLE N IN UPPER FUSELAGE FR47 BTW STGR25 AND STGR26 PER EA 6-5310-T0387082. TITLE: FUSELAGE - MAINFRAME - FR47 RH HOLE N CRACK REPAIR BETWEEN S-24R AND S-26R
- [SDR FDEA202604180485](https://openairdocs.org/sdr/FDEA202604180485.md): Seat Track · no discrepancy · Apr 18, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK FR40-45 -Y1959 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. SEAT TRACK WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG A53832020. NO RECORD FOUND. EO 6-5100-7-5000 D 07 PART 1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATA
- [SDR FDEA202604180481](https://openairdocs.org/sdr/FDEA202604180481.md): Hinge Arm · delaminated · Apr 18, 2026 · N669FE · Airbus A300F4605R · Spoilers
  > LH WING, NR 4 SPOILER CENTER HINGE ARM OUTBD SIDE ARM OTBD SURFACE DELAMINATED 40MM*25MM*1.66MM. COMPLIED WITH EA 6-5750-T0387083 P1 REPAIRED THE DELAMINATION ON LH WING #4 SPOILER CENTER OUTBD HINGE ARM OUTBD SURFACE. EA TITLE: WING - FLIGHT SURFACES - L
- [SDR FDEA202604170458](https://openairdocs.org/sdr/FDEA202604170458.md): Crossbeam · damaged · Apr 17, 2026 · N669FE · Airbus A300F4605R · Fuselage Main, Structure
  > EXISTING REPAIR ON MAIN DECK FR60 -Y1456~-Y1959 CROSSBEAM REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FR60 -Y1456~-Y1959 CROSSBEAM WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH EA6-5310-T0306792 DUE TO A FASTENER HOLE MISS DRILL,
- [SDR FDEA202604170457](https://openairdocs.org/sdr/FDEA202604170457.md): Floor Support · misrepaired · Apr 17, 2026 · N669FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MAIN DECK FR11-FR12A Y0 FLOOR SUPPORT REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON MAIN DECK FR11-FR12A Y0 FLOOR SUPPORT REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK FR11-12A Y0 FLOOR SUPPORT WAS EVALUAT
- [SDR FDEA202604160455](https://openairdocs.org/sdr/FDEA202604160455.md): Seat Track · no discrepancy · Apr 16, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK FR37-39 -Y450 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FR37-39 -Y450 SEAT TRACK WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIG.201, NO RECORD FOUND. EO 6-5100-7
- [SDR FDEA202604160454](https://openairdocs.org/sdr/FDEA202604160454.md): Seat Track · no discrepancy · Apr 16, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK FR40-45 -Y953 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FR40-45 -Y953 SEAT TRACK WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG A53832020 (ISSUE: J00), NO RECORD FOUND. EO 6-5100-7-5000 D
- [SDR FDEA202604160453](https://openairdocs.org/sdr/FDEA202604160453.md): Profile · no discrepancy · Apr 16, 2026 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > EXISTING REPAIR ON BULK CARGO FR66-69 Y0~Y140 LONGITUDINAL PROFILE REQUIRES EVALUATION FOR CONFORMITY. LONGITUDINAL PROFILE WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG A53974262 (ISSUE: D), NO RECORD FOUND. EO 6-5100-7-5000 D 07 PART 1 WAS COMPLETED
- [SDR FDEA202604160451](https://openairdocs.org/sdr/FDEA202604160451.md): Seat Track · no discrepancy · Apr 16, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK FR11-15A Y953 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. FLOOR SUPPORT WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53612519 (ISSUE: B00). NO RECORD FOUND. EO 6-5100-7- 5000 D07 PART 1 WAS COMPLETED. TITLE: STRUCTURES
- [SDR FDEA202604160450](https://openairdocs.org/sdr/FDEA202604160450.md): Seat Track · no discrepancy · Apr 16, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK FR57-57.2 -Y1456 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FR57-57.2 -Y1456 SEAT TRACK WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIG.201, NO RECORD FOUND. EO 6-
- [SDR FDEA202604160449](https://openairdocs.org/sdr/FDEA202604160449.md): Seat Track · no discrepancy · Apr 16, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK FR26-28 Y0 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FR26-28 Y0 SEAT TRACK WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIG.201, NO RECORD FOUND. EO 6-5100-7-5000
- [SDR FDEA202604150452](https://openairdocs.org/sdr/FDEA202604150452.md): Seat Track · no discrepancy · Apr 15, 2026 · N669FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MAIN DECK FR15A-19 Y953 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK FR15A-19 Y953 SEAT TRACK WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG A53612524 (ISSUE: A00), NO RECORD FOUND. EO 6-5100-7-5000 D 07
- [SDR FDEA202604140571](https://openairdocs.org/sdr/FDEA202604140571.md): Skin · cracked · Apr 14, 2026 · N669FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA 6-5750-T0387053 P1 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8. TITLE: WINGS - FLIGHT SURFACE
- [SDR FDEA202604140438](https://openairdocs.org/sdr/FDEA202604140438.md): Rib · cracked · Apr 14, 2026 · N669FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB27 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA 6-5750-T0387053 P1 REPAIRED THE LH WING CENTER FLAP RIB27 UPPER CRACKED FLANGE BETWEEN REAR SPAR AND STGR2.8. CAT A REPAIR. MAJOR REPAIR IAW GMM 6
- [SDR FDEA202604140441](https://openairdocs.org/sdr/FDEA202604140441.md): Crossbeam · cracked · Apr 14, 2026 · N669FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN DECK CARGO COMPARTMENT CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959 CRACKED. REPAIRED THE MAIN DECK CARGO COMPARTMENT CRACKED CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959 PER A300-600F SRM53-10-15-201 FIG.211. THIS IS A CATEGORY A REPAIR. MAJOR REPAIR
- [SDR FDEA202604140437](https://openairdocs.org/sdr/FDEA202604140437.md): Rib · cracked · Apr 14, 2026 · N669FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > LEFT WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8
- [SDR FDEA202604120484](https://openairdocs.org/sdr/FDEA202604120484.md): Seat Track · damaged · Apr 12, 2026 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK FR18-22 Y2462 SEAT TRACK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FR18-22 Y2462 SEAT TRACK WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-10-16 FIG.201A. NO RECORD FOUND. RE-REPAIRED P
- [SDR FDEA202604120440](https://openairdocs.org/sdr/FDEA202604120440.md): Rib · cracked · Apr 12, 2026 · N669FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB26 BETWEEN STGR2.7 AND STGR2.8. REPAIRED RH WING CENTER FLAP RIB UPPER FLANGE CRACK AT RIB26 BETWEEN STGR2.7 AND STGR2.8 PER A300-600F SRM57-50-00-201 PARA.4.A & SRM57-50-00-201 FIG.205 & EA6-575
- [SDR FDEA202604120439](https://openairdocs.org/sdr/FDEA202604120439.md): Rib · cracked · Apr 12, 2026 · N669FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIBS UPPER FLANGE FOUND 3EA CRACK AT RIB11 BETWEEN STGR2.7 AND STGR2.8. REPAIRED RH WING CENTER FLAP RIB UPPER FLANGE CRACK AT RIB11 BETWEEN STGR2.7 AND STGR2.8 PER A300-600F SRM57-50-00-201 PARA.4.A & SRM57-50-00-201 FIG.205 & EA6-5750
- [SDR FDEA202604110583](https://openairdocs.org/sdr/FDEA202604110583.md): Frame Splice · cracked · Apr 11, 2026 · N669FE · Airbus A300F4605R · Fuselage Main, Frame
  > MAIN FRAME, INSPECTION, HOLES IN FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STR 24 & 26, LH /RH, AIRBUS SB A300-53-6123 COMPLIED WITH EO 6-5310-7-5017 P P6. TITLE: FUSELAGE - MAINFRAME - INSPECTION - HOLES IN FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STR 24
- [SDR FDEA202604100429](https://openairdocs.org/sdr/FDEA202604100429.md): Crossbeam · not reported · Apr 10, 2026 · N669FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN DECK CARGO COMPARTMENT CROSSBEAM AT FR67 BETWEEN Y1456 AND Y1959 CRACKED. REPAIRED THE MAIN DECK CARGO COMPARTMENT CRACKED CROSSBEAM AT FR67 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 FIG.211. THIS IS A CATEGORY A REPAIR. MAJOR REPAIR IAW G
- [SDR FDEA202604070574](https://openairdocs.org/sdr/FDEA202604070574.md): Fitting · not reported · Apr 7, 2026 · N669FE · 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 C P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION O
- [SDR FDEA202602180232](https://openairdocs.org/sdr/FDEA202602180232.md): Slide · damaged · Feb 18, 2026 · N669FE · Airbus A300F4605R · Escape Slide
  > WHILE ACCOMPLISHING EA 6-2560-F0386375 REV A PART 1 FOR THE L1 DOOR SLIDE. FOUND THE EJECTOR BAG RELEASE CABLE HAD THE INCORRECT SAFETY WIRE INSTALLED. FACT 18FEB26 21:50 MEM AMM: 25-61-20-05-01 EA: 6-2560-F0386375 REV A PART 1 INSTALLED CAD PLATED
- [SDR FDEA202602060141](https://openairdocs.org/sdr/FDEA202602060141.md): Power Supply · inoperative · Feb 6, 2026 · N669FE · Airbus A300F4605R · Emergency Lighting
  > ON POST FLIGHT FOUND PASSENGER DOOR EMERGENCY EXIT LIGHT TEST INOPERATIVE. IAW AMM 33-51-14-04, REMOVED & INSTALLED THE POWER SUPPLY UNIT. OPS CHECK GOOD. NO DEFECTS NOTED.
- [SDR FDEA202410251581](https://openairdocs.org/sdr/FDEA202410251581.md): Nut · loose · Oct 25, 2024 · N669FE · Airbus A300F4605R · Airborne Auxiliary Power Unit (APU) System
  > ABOUT TO DEPART BFM. TURNED ON APU BLEED. CURRIER AREA FILLED WITH SMOKE. TURNED OFF APU BLEED AND DEPARTED AC. FOUND OIL PUMP NUT LOOSE AT OIL COOLER INLET, TIGHTEN AS REQUIRE IAW A300-600 AMM CH 49-91-16-4 AND SERVICE APU OIL IAW AMM 12-13-49-00. REMO
- [SDR FDEA202403130282](https://openairdocs.org/sdr/FDEA202403130282.md): Adc · failed · Mar 13, 2024 · N669FE · Airbus A300F4605R · Air Data Computer
  > SHORTLY AFTER TAKEOFF, PITCH TRIM 2 & YAW DAMPER 2 CLICKED OFF, FOLLOWED BY A ADC2 INOP MESSAGE. ONCE SLATS RETRACTED, FO FLYING & CONTINUED TIL 17,000 FT. REVIEWED QRH FOR ADC FAULT & NOTED WERE NO LONGER RVSM & FO PLACED AP 1 ON. AFTER 2 MINS, AP1 CLICKED
- [SDR FDEA202310021682](https://openairdocs.org/sdr/FDEA202310021682.md): Flap · corroded · Oct 2, 2023 · N669FE · Airbus A300* · Trailing Edge Flaps
  > LH WING O/B FLAP O/B END T/E SKIN CORRODED AND DISCHARGER FITTING FOUND BROKEN REPAIRED THE CORRODED SKIN AT LH WING O/B FLAP O/B END T/E PER EA:6-5750-T0376427 P1. TITLE: WINGS - FLIGHT SURFACES - LH O/B FLAP, OUTER TRAILING EDGE, UPPER SKIN CORROSION U
- [SDR FDEA202309251644](https://openairdocs.org/sdr/FDEA202309251644.md): Crossbeam · cracked · Sep 25, 2023 · N669FE · Airbus A300* · Fuselage Main, Structure
  > MDCC FLOOR CROSSBEAM FWD STIFFENER CRACKED AT FR31, BTW -Y450 - -Y953 REPAIRED THE CRACK ON THE MDCC FLOOR CROSSBEAM FWD STIFFENER AT FR31, BTW -Y450 - - Y953 PER A300-600F SRM53-10-15-201 PARA.15 & EA:6-5310-T0376313 P1. THE REPAIR IS CAT A REPAIR, MAJOR RE
- [SDR FDEA202309251643](https://openairdocs.org/sdr/FDEA202309251643.md): Seat Track · corroded · Sep 25, 2023 · N669FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > MDCC SEAT TRACK FOUND 2EA CORRODED BETWEEN FR73 - FR78, Y953 REPAIRED THE MDCC CORRODED SEAT TRACK BETWEEN FR73 - FR78, Y953 PER SRMA300-600F SRM53-10-16 FIG.201. THIS REPAIR IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202309251642](https://openairdocs.org/sdr/FDEA202309251642.md): Seat Track · corroded · Sep 25, 2023 · N669FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > MDCC SEAT TRACK FOUND CORROSION AT FR57.3 - FR58 Y-450 REPAIRED THE MDCC SEAT TRACK AT FR57.3 - FR58 Y-450, PER A300-600F SRM53-10-16 FIG.201, THIS REPAIR IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202304130635](https://openairdocs.org/sdr/FDEA202304130635.md): Unknown · unknown · Apr 13, 2023 · N669FE · Airbus A300* · Passenger/Crew Doors
  > DOOR R1 ASSIST BOTTLE BLOWN. RELEASED FOR SERVICE PER MEL: 52-11-01-05 CATEGORY: C EXPIRATION: 23APR23 "MEL 52-11-01-05: CREW ENTRY DOOR R1 - INOP." SLIDE IS NOT BLOWN C/7356956. REMOVED AND REPLACED DIAPHRAGM IN R-1 FWD DOOR DAMPER AND EMERGENCY OPERA
- [SDR FDEA202201050011](https://openairdocs.org/sdr/FDEA202201050011.md): Packing · leaking · Jan 5, 2022 · N669FE · Airbus A300* · Passenger/Crew Doors
  > L1 DOOR DAMPER ASSIST BOTTLE READING. 0. RELEASED FOR SERVICE PER MEL: 52-11-01-05 CAT: C EXP: 15JAN22 "MEL 52-11-01-05: CREW ENTRY DOOR L1 - INOP." RELEASED FOR SERVICE PER MEL: 52-XX-XX-XX CATEGORY: C EXPIRATION: 15JAN22. IDENTIFIED PARTS SEAL
- [SDR FDEA202112133085](https://openairdocs.org/sdr/FDEA202112133085.md): Computer · damaged · Dec 13, 2021 · N669FE · Airbus A300F4605R · Fuel Indicating System
  > SUSPECTED FUEL LEAK DURING CLIMB OUT. PASSING FL200. LEFT INNER TANK WENT FROM 3K TO 200 POUNDS. COMPLIED WITH QRH. IMBALANCE AND FUEL DISCREPANCY STAYED AFTER RESETTING FUEL CHAN SUPPLY BREAKERS. FIRE CHIEF IN BNA SAID NO SIGNS OF A LEAK. LANDING AND TAXI I
- [SDR FDEA202109162318](https://openairdocs.org/sdr/FDEA202109162318.md): Damper · failed · Sep 16, 2021 · N669FE · Airbus A300F4605R · Landing Gear Retraction/Extension System
  > PDIS 669 32-30 3699 15SEP21 MKE OPEN U AFTER TAKE OFF KIND. LANDING GEAR HANDLE WOULD NOT COME UP IN SYS POS 1. POS SYS 2 WAS MEL. BUT TRIED POS SYS 2 AND IT WORKED. USED POS SYS 1 TO LOWER THE GEAR AT MKE. NO ISSUES. "MEL 32-30-01-A: LAND
- [SDR FDEA202103180760](https://openairdocs.org/sdr/FDEA202103180760.md): Adapter · damaged · Mar 18, 2021 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > REPLACE ADAPTER TRACK UNDER LOCK STA1530 LOC. FLOOR STRUCTURE FR58 BTW -Y953 TO -Y450 FOR TERMINATING ACTION ON RUTINE CARD 000832 REPLACED ADAPTER TRACK UNDER LOCK STA1530 LOC. ON FLOOR STRUCTURE FR 58 BTW -Y953 TO -Y450 IAW SRM A300-600 FREIGHTER 51-40-21
- [SDR FDEA202103160841](https://openairdocs.org/sdr/FDEA202103160841.md): Floor Support · corroded · Mar 16, 2021 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > CORROSION FLOOR BEAM Y450 BTW FR 11 TO FR 14 PASSENGER CABIN PERFORMED PERMANENT REPAIR ON FLOOR BEAM Y450 BTW FR11 TO FR 14 PASSENGER CABIN, THIS REPAIR IS CATEGORY B IAW A300-600 FREIGHTER SRM 53-12-15 STEP 5G FIG 207. AND INSPECTION THRESHOLD AT 42500FC
- [SDR FDEA202103130853](https://openairdocs.org/sdr/FDEA202103130853.md): Fitting · cracked · Mar 13, 2021 · N669FE · Airbus A300F4605R · Wing, Attach Fittings
  > CRACK INDICATION ON FRAME 47 RH SIDE ON CWB REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE AT OPEN FASTENER HOLE F (CRACK DIRECTION IS 7 OCLOCK) AT LOWER FUSELAGE (1EA) REPAIRED IAW EA 6-5710-T0360412 (P1) RELEASE DATE 06-APR-21 EA TITTLE: WINGS - BA
- [SDR FDEA202103090759](https://openairdocs.org/sdr/FDEA202103090759.md): Web · cracked · Mar 9, 2021 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > CRACK WEB LOCATED AT LEVEL FR 47 AND Y450 TO Y0 IN PASSENGER CABIN (MAIN DECK) REPLACED WEB AT LEVEL FR47 AND Y450 TO Y0 IN MAIN DECK CABIN AS PER A300-600 SRM 51- 51-72-10 AND DRAWING A53810937 ISSUE B SHEET 01
- [SDR FDEA202103090758](https://openairdocs.org/sdr/FDEA202103090758.md): Web · cracked · Mar 9, 2021 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > CRACK WEB LOCATED AT LEVEL FR 47 AND Y0 TO -Y450 IN PASSENGER CABIN (MAIN DECK) REPLACED WEB LOCATED AT LEVEL FR47 AND Y0 TO -Y450 IN MAIN DECK CABIN AS PER A300- 600 SRM 51-72-10 AND DRAWING A53810937 ISSUE B SHEET 1
- [SDR FDEA202103090741](https://openairdocs.org/sdr/FDEA202103090741.md): Web · cracked · Mar 9, 2021 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > CRACK WEB LOCATED AT LEVEL FR 47 AND Y1456 TO Y953 IN PASSENGER CABIN (MAIN DECK) PERFORMED PERMANENT REPAIR ON WEB LOCATED AT LEVEL FR47 AND Y1456 TO Y953 IN PASSENGER CABIN (MAIN DECK) IAW A300-600 FREIGHTER SRM 53-15-15 PARAGRAPH 5A FIGURE 201 AND DWG#
- [SDR FDEA202103090928](https://openairdocs.org/sdr/FDEA202103090928.md): Support Angle · cracked · Mar 9, 2021 · N669FE · Airbus A300F4605R · Wing Miscellaneous Structure
  > CRACK TRAILING EDGE SUPPORT ANGLE LOCATED AT LEVEL OF RIB 6A REAR SPAR INBOARD SIDE ON RH WING PERFORMED PERMANENT REPAIR ON TRAILING EDGE SUPPORT ANGLE LOCATED AT LEVEL OF OF RIB 6A REAR SPAR INBOARD SIDE ON RH WING IAW EA 6-5710-T0360731 TITTLE: WINGS- BA
- [SDR FDEA202103090739](https://openairdocs.org/sdr/FDEA202103090739.md): Web · cracked · Mar 9, 2021 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > CRACK WEB LOCATED AT LEVEL FR 47 AND -Y1456 TO -Y953 IN PASSENGER CABIN (MAIN DECK) REPAIRED WEB LOCATED AT LEVEL FR47 AND -Y1456 TO -Y953 IN PASSENGER CABIN (MAIN DECK) IAW A300-600 FREIGHTER SRM 53-15-15 PARAGRAPH 5A(2) FIGURE 201 SHEET 1 AND 2 CONFIG. 2
- [SDR FDEA202103080926](https://openairdocs.org/sdr/FDEA202103080926.md): Stringer · corroded · Mar 8, 2021 · N669FE · Airbus A300F4605R · Fuselage Main, Frame
  > CORROSION STRUCTURE INTERNAL STRINGER 37L BETWEEN FR. 46 AND FR. 47 IN AIR CONDITIONING BAY PERFORMED REPAIR ON INTERNAL STRUCTURE STRINGER 37L BTW FR46 AND FR 47 IN AIR CONDITIONING BAY IAW EA# 6-5310-T0360467 P1 TITTLE: FUSELAGE MAINFRAME-CORROSION ON ST
- [SDR FDEA202103070890](https://openairdocs.org/sdr/FDEA202103070890.md): Skin · dented · Mar 7, 2021 · N669FE · Airbus A300F4605R · Ailerons
  > SEVERAL DENTS ON AILERON UPPER AND LOWER SURFACE ON RH WING PERFORMED PERMANENT REPAIR LOC ON LOWER SURFACE BTW RIB 11 TO RIB 12 ON RH AILERON IAW EA 6-5750-T0360611 P1 TITLE WINGS FLIGHT SURFACES RIGHT HAND ALL SPEED AILERON UPPER AND LOWER SKINS MULTIPLE
- [SDR FDEA202103070889](https://openairdocs.org/sdr/FDEA202103070889.md): Skin · dented · Mar 7, 2021 · N669FE · Airbus A300F4605R · Ailerons
  > SEVERAL DENTS ON AILERON LOWER AND UPPER SURFACE ON LH WING PERFORMED PERMANENT REPAIR LOC LOWER SURFACE BTW RIB 9 AND RIB 11 ON LH AILERON IAW EA 6-5750-T0360573 P1 TITLE WINGS FLIGHT SURFACES LEFT HAND ALL SPEED AILERON UPPER AND LOWER SKINS MULTIPLE DEN
- [SDR FDEA202103030648](https://openairdocs.org/sdr/FDEA202103030648.md): Seat Track · corroded · Mar 3, 2021 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK FR56-57.1 -Y1456 SEAT TRACK. REQUIRES EVALUATION PER ATTACHMENT B IAW EO 6-5100-7-5000 P1 THE EXISTING REPAIR ON MAIN DECK FR56-57.1 -Y1456 SEAT TRACK WAS NOT FOUND CONFORMITY WITH A300-600F SRM 53-10-16 FIG 201 AND EVALUATED P
- [SDR FDEA202103030628](https://openairdocs.org/sdr/FDEA202103030628.md): Seat Track · misrepaired · Mar 3, 2021 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON SEAT TRACK Y0 LOCATED BETWEEN FR75 TO FR77 IN MAIN DECK. REQUIRES EVALUATION PER ATTACHMENT B. IAW EO 6-5100-7-5000 P1 THE EXISTING REPAIR ON SEAT TRACK Y0 LOCATED BETWEEN FR75 TO FR77 IN MAIN DECK WAS NOT FOUND CONFORMITY WITH A300-600F
- [SDR FDEA202103030627](https://openairdocs.org/sdr/FDEA202103030627.md): Seat Track · misrepaired · Mar 3, 2021 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR FRAME ON UPPER FUSELAGE (EXISTING REPAIR ON MAIN DECK FR56-FR57.2 - Y953 SEAT TRACK. REQUIRES EVALUATION PER ATTACHMENT B IAW EO 6-5100-7-5000 P1) THE EXISTING REPAIR ON MAIN DECK FR56-FR57.2 -Y953 SEAT TRACK WAS NOT FOUND CONFORMITY WITH A3

Next page: https://openairdocs.org/aircraft/N669FE/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 = 'N669FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N669FE/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.