# Service difficulty reports: N661FE

A list on [N661FE](https://openairdocs.org/aircraft/N661FE.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 · 318 reports

- [SDR FDEA202609061267](https://openairdocs.org/sdr/FDEA202609061267.md): Frame · cracked · Sep 6, 2026 · N661FE · Airbus A300F4605R · Fuselage Main, Frame
  > INSPECTION OF FRAME 40 LT, LOWER WING JUNCTION, FOUND A CRACK SIGNAL AT FASTENER HOLE NR 1. COMPLIED WITH EA: 6-5710-T0388595 P1. REPAIRED FRAME 40 LT LOWER JUNCTION, CRACKED FASTENER HOLE NR 1. THIS IS CATEGORY B REPAIR. FOLLOW UP INSPECTION IAW EA 6-5710-
- [SDR FDEA202609061266](https://openairdocs.org/sdr/FDEA202609061266.md): Seat Track · corroded · Sep 6, 2026 · N661FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK AT Y1959 BETWEEN FR53 AND FR54 CORRODED. REPAIRED THE CORRODED MAIN DECK SEAT TRACK AT Y1959 BETWEEN FR53 AND FR54 PER SRM53-10-16-201 FIG.201 & EA: 6-5310-T0388627 P1. CATEGORY -A- MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202609011253](https://openairdocs.org/sdr/FDEA202609011253.md): Seat Track · worn · Sep 1, 2026 · N661FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK AT Y1959 BETWEEN FR 62 AND FR 63 FOUND WORN. SEAT TRACK SECTION AT Y1959 BETWEEN FR62 AND FR63 PER A300-600F SRM51-40-21 & SRM53-10-16-201 FIG.201. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202608261228](https://openairdocs.org/sdr/FDEA202608261228.md): Attach Fitting · cracked · Aug 26, 2026 · N661FE · Airbus A300F4605R · Cargo/Baggage Doors
  > FWD CARGO DOOR ACTUATOR ATTACH FITTING FOUND 2EA CRACKS BY HFEC INSPECTION. REPLACED THE CRACKED FWD CARGO DOOR ACTUATOR ATTACH FITTING WITH FABRICATED PART PER SRM51-40-21 & DWG: F52370695(ISSUE. J), A52370501(ISSUE. J) & A52370534(ISSUE. F). RSC TRACKING
- [SDR FDEA202605040543](https://openairdocs.org/sdr/FDEA202605040543.md): Battery · no test · May 4, 2026 · N661FE · Airbus A300F4605R · Emergency Lighting
  > EMERGENCY LIGHT TEST IN COURIER AREA WON'T TEST ON PREFLIGHT. MANUAL OPERATES OK. AMM 33-51-00-05 REMOVED AND REPLACED MAIN DECK EMERGENCY LIGHT BATTERY REF AMM 33-51-00-05. COURIER AREA EMERGENCY LIGHT TEST CKS GOOD.
- [SDR FDEA202602150207](https://openairdocs.org/sdr/FDEA202602150207.md): Safety Wire · wrong part · Feb 15, 2026 · N661FE · Airbus A300F4605R · Escape Slide
  > WHILE PERFORMING F.E.A. 6-2560-F0386375 A P1, FOUND EJECTOR BAG RELEASE CABLE WITH INCORRECT SAFETY WIRE. L1 DOOR SLIDE AMM: 25-61-20-05-01. REMOVED AND REPLACED COPPER WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. OPS CHK GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202602150206](https://openairdocs.org/sdr/FDEA202602150206.md): Slide · damaged · Feb 15, 2026 · N661FE · Airbus A300F4605R · Escape Slide
  > WHILE COMPLING WITH FEA 6-2560-F0386375 A PART 1, FOUND R1 DOOR SLIDE DAMAGED AND WILL RETURN TO STORES. R/I 15FEB26 01:46 MEM REASON CODE: FAILED OPS CK. & REPLACED WITH SERVICABLE UNIT REMOVED & REPLACED R1 DOOR SLIDE. BROKEN SLIDE REMOVED IS P
- [SDR FDEA202512242287](https://openairdocs.org/sdr/FDEA202512242287.md): Valve · failed · Dec 24, 2025 · N661FE · Airbus A300F4605R · Landing Gear Retraction/Extension System
  > DURING APPROACH, LANDING GEAR WOULD NOT EXTEND AFTER MULTIPLE CYCLES AND SWITCHING SYSTEMS 1 & 2. HYDRAULICS GOOD. USED LANDING GEAR GRAVITY EXTENSION QRH PROCEDURE, GEAR EXTENDED. LANDED UNEVENTFULLY, TOWED IN FROM RUNWAY DUE TO NO NOSE WHEEL STEERING.
- [SDR FDEA202508151454](https://openairdocs.org/sdr/FDEA202508151454.md): Monitor · expired · Aug 15, 2025 · N661FE · Airbus A300F4605R · Emergency Equipment
  > CO2 MONITOR (S/N AREJ-2218) CALIBRATION CYCLE EXPIRED. REMOVED AND REPLACED CO2 MONITOR WITH EXPIRED CALIBRATION CYCLE.
- [SDR FDEA202504120591](https://openairdocs.org/sdr/FDEA202504120591.md): Power Supply · no test · Apr 12, 2025 · N661FE · Airbus A300F4605R · Door Warning System
  > L1 AND R1 DOOR SLIDE TEST WARNING LIGHTS DO NOT ILLUMINATE DURING TEST. BUZZERS WORK NORMALLY. L1 AND R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS - INOP. MEL: 52-73-01-01 REPLACED AUTONOMOUS STANDBY POWER SUPPLY UNIT PER A.M.M. 52-73-18- 04.
- [SDR FDEA202407080963](https://openairdocs.org/sdr/FDEA202407080963.md): Csu · failed · Jul 8, 2024 · N661FE · Airbus A300F4605R · Auto Flight System
  > AFTER TAKEOFF ON GEAR RETRACTION THE CAPTAIN RED SPD LIM APPEARED ON PFD. THE NUMBER 2 FAC WAS DEFERRED PER MEL 22-26-34-01 AND THE OP NOTES ABOUT SPEED TREND,VSS, VLS,VMAX,F,S SPEEDS ETC WERE ALSO INDICATED AND MISSING ON CAPT PFD. EMERGENCY DECLARED.
- [SDR FDEA202407060950](https://openairdocs.org/sdr/FDEA202407060950.md): Jackscrew · failed · Jul 6, 2024 · N661FE · Airbus A300F4605R · Trailing Edge Flap Control System
  > ON DEPARTURE 15/0 CONFIGURATION AFTER AT SAFE SPEED WE RETRACTED THE SLATS AND RECEIVED ECAM WARNING OF FLAPS SYS 1 AND 2 FAULT/ FLAPS STUCK. DID NOT CYCLE BECAUSE FLAPS WERE NOT USED AND BOTH FLAPS AND SLATS WERE AT 0. DECLARED AN EMERGENCY AND PROCEED
- [SDR FDEA202406220835](https://openairdocs.org/sdr/FDEA202406220835.md): Controller · malfunctioned · Jun 22, 2024 · N661FE · Airbus A300F4605R · Leading Edge Slat Control System
  > FLAPS STUCK AT 15 ON TAKEOFF. CYCLED NO CHANGE. NO OVERSPEED. AMM 27-51-18-04. T/S PER TSM 27-50-02. RESET TORQUE LIMITERS. OPS SLATS/FLAPS THROUGH ALL DETENTS. NO FAULTS OR ANOMALIES NOTED DURING OPS. TORQUE LIMITERS OPS NORMAL. CHECKED OIL LEVEL OF FLAP
- [SDR FDEA202406010761](https://openairdocs.org/sdr/FDEA202406010761.md): Jackscrew · binding · Jun 1, 2024 · N661FE · Airbus A300F4605R · Leading Edge Slat Control System
  > FLAPS/SLATS STUCK 15/15 ON DEPARTURE. EMERGENCY DECLARED. QRH FOLLOWED. FLAPS OVERSPEED AT 15/15 TO APPROX 225 KTS. ***EMERGENCY DECLARED*** REF TSI 27-80/6666 FOR RH WING #1 SLAT SCREWJACK TORQUE INDICATOR FOUND TRIPPED. ALL SERVICING AND OTHER
- [SDR FDEA202405060601](https://openairdocs.org/sdr/FDEA202405060601.md): Fitting · none · May 6, 2024 · N661FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIRS FOUND ON RHW RIBS OF T/E STRUCTURE AT WI.AX 21.9 NEAR AFT LUG COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQ
- [SDR FDEA202405060600](https://openairdocs.org/sdr/FDEA202405060600.md): Fitting · none · May 6, 2024 · N661FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIRS FOUND ON RHW RIBS OF T/E STRUCTURE AT WI.AX 13.9 NEAR AFT LUG COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQ
- [SDR FDEA202405060599](https://openairdocs.org/sdr/FDEA202405060599.md): Fitting · none · May 6, 2024 · N661FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIRS FOUND ON RHW RIBS OF T/E STRUCTURE AT RIB6A NEAR AFT LUG COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREM
- [SDR FDEA202405050577](https://openairdocs.org/sdr/FDEA202405050577.md): Skin · none · May 5, 2024 · N661FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON LHW CTR FLAP UPR SKIN BTW RIB12~13, T/E-13.8" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT WAS UNDOCUMENTED REPAIR, REMOVED EXISTING REPA
- [SDR FDEA202404260296](https://openairdocs.org/sdr/FDEA202404260296.md): None · none · Apr 26, 2024 · N661FE · Airbus A300* · Standard Practices/Structures
  > EXISTING REPAIR FOUND ON M/D CROSSBEAM AT FR29, BTW Y1456 TO -Y1456 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTI
- [SDR FDEA202404210650](https://openairdocs.org/sdr/FDEA202404210650.md): Skin · cracked · Apr 21, 2024 · N661FE · Airbus A300F4605R · Trailing Edge Flaps
  > PFM EA#: 6-5750-T0378801 P1 FOUND NEW CRACK AT LH WING CTR FLAP RIB26 BTWN STGR 2.7-2.8 ACCOMPLISHED THE CAT.A FLANGE REPAIR AT RIB 26 UPPER FLANGE S-2.7~S-2.8, THE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T0378801 P1, SEQ NO:1119
- [SDR FDEA202404160585](https://openairdocs.org/sdr/FDEA202404160585.md): Dummy Rail · worn · Apr 16, 2024 · N661FE · Airbus A300F4605R · Fuselage Floor Panel
  > FR54/FR54.2 LH NO.5 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. AUTUAL MEASUREMENT:1.14MM REPLACED DAMAGED DUMMY SEAT TRACK WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001,P2 AND 51-40-21-001 PARA7 P24~P50, THE REPAIR CLASSIFIED AS MINOR PER
- [SDR FDEA202404150670](https://openairdocs.org/sdr/FDEA202404150670.md): Fitting · cracked · Apr 15, 2024 · N661FE · Airbus A300F4605R · Cargo/Baggage Doors
  > THE MDC DOOR ACTUATOR AFT SUPPORT FRAME WAS FOUND CRACK ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR24 LONGN1~LONGN3 I.A.W FEDEX EA NO:T6-5230-T0378797 P1, SEQ NO:1121, TITLE:DOORS-CARGO DOOR /HYD SYS-MAIN CARGO ACTUATOR BEARI
- [SDR FDEA202404110576](https://openairdocs.org/sdr/FDEA202404110576.md): Rib · gouged · Apr 11, 2024 · N661FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > R/H SPOILER 3 I/B JACK RIB LWR BORE EDGE DAMAGE. ACCOMPLISHED THE CAT.B HOLE REINFORCEMENT REPAIR AT RH WING NO.3 SPOILER JACK RIB AT ABX 31.675 LOWER HOLE. THE REPAIR CLASSIFIED AS MAJOR REF GMM 6-2-100. I.A.W FEDEX EA:T6-5740-T0378859 P1 SEQ NO:1106, TIT
- [SDR FDEA202404110575](https://openairdocs.org/sdr/FDEA202404110575.md): Rib · gouged · Apr 11, 2024 · N661FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > R/H SPOILER 3 I/B JACK RIB UPR BORE EDGE DAMAGE. ACCOMPLISHED THE CAT.B HOLE REINFORCEMENT REPAIR AT RH WING NO.3 SPOILER JACK RIB AT ABX 31.675 UPPER HOLE. THE REPAIR CLASSIFIED AS MAJOR REF GMM 6-2-100. I.A.W FEDEX EA:T6-5740-T0378859 P1 SEQ NO:1106, TIT
- [SDR FDEA202404110574](https://openairdocs.org/sdr/FDEA202404110574.md): Rib · gouged · Apr 11, 2024 · N661FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > R/H SPOILER 7 I/B JACK RIB UPR BORE EDGE DAMAGE ACCOMPLISHED THE CAT.B HOLE REINFORCEMENT REPAIR AT RH WING NO:7 SPOILER JACK RIB AT SP2X 31.675 UPPER HOLE. THE REPAIR CLASSIFIED AS MAJOR REF GMM 6-2-100. I.A.W FEDEX EA:T6-5740-T0378863 P1, SEQ NO:1109, TI
- [SDR FDEA202404110573](https://openairdocs.org/sdr/FDEA202404110573.md): Rib · corroded · Apr 11, 2024 · N661FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > LH WING NO.5 SPOILER I/B UPPER JACK RIB SCREW HOLE O/B EDGE CORRODED. ACCOMPLISHED THE CAT.B HOLE REINFORCEMENT REPAIR AT LH WING NO.5 SPOILER JACK RIB AT ABX 175.875 UPPER HOLE. THE REPAIR CLASSIFIED AS MAJOR REF GMM 6-2-100. I.A.W FEDEX EA:T6-5740-T03788
- [SDR FDEA202404110572](https://openairdocs.org/sdr/FDEA202404110572.md): Rib · gouged · Apr 11, 2024 · N661FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > LH WING NO.3 SPOILER UPR JACK RIB SCREW HOLE INNER SURFACE SCRATCH. ACCOMPLISHED THE CAT.B HOLE REINFORCEMENT REPAIR AT LH WING NO.3 SPOILER JACK RIB STA ABX 40.425 UPPER HOLE. THE REPAIR CLASSIFIED AS MAJOR REF GMM 6-2-100. I.A.W FEDEX EA:T6-5740-T037886
- [SDR FDEA202404110571](https://openairdocs.org/sdr/FDEA202404110571.md): Rib · gouged · Apr 11, 2024 · N661FE · Airbus A300F4605R · Spoilers
  > LH WING NO.3 SPOILER LWR JACK RIB SCREW HOLE O/B EDGE DAMAGE. ACCOMPLISHED THE CAT.B HOLE REINFORCEMENT REPAIR AT LH WING NO.3 SPOILER JACK RIB AT ABX 40.425 LOWER HOLE. THE REPAIR CLASSIFIED AS MAJOR REF GMM 6-2-100. I.A.W FEDEX EA:T6-5740-T0378860 P1 SEQ
- [SDR FDEA202404110548](https://openairdocs.org/sdr/FDEA202404110548.md): Floor Support · corroded · Apr 11, 2024 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK COMPT - COURIER AREA FOUND 1EA SUPPORT - FLOOR CORRODED LOCATION FROM FR11 TO FR14, Y730 REPLACED THE DAMAGE SUPPORT WITH NEW PARTS, LOCATED IN FR11 TO FR14, Y730 I.A.W A300- 600F SRM 51-72-10-001,P2 REPAIR CLASSIFIED AS MINOR PER GMM6-2-100
- [SDR FDEA202404110538](https://openairdocs.org/sdr/FDEA202404110538.md): Floor Support · corroded · Apr 11, 2024 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK COMPT - COURIER AREA FOUND 1EA SUPPORT - FLOOR CORRODED LOCATION FROM FR11 TO FR15A, Y953 REPLACED THE 1EA SUPPORT WITH NEW AT MAIN DECK COMPT-COURIER AREA LOCATION FROM FR11 TO FR 15A, Y953 I.A.W A300-600F SRM 51-72-10-001, PAGE2 CLASSIFIED AS
- [SDR FDEA202404100616](https://openairdocs.org/sdr/FDEA202404100616.md): Seat Track · gouged · Apr 10, 2024 · N661FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK COMPT FLOOR - SEAT TRACK CROWN AREA GOT GOUGED LOCATION AT FR62 PLUS 2",Y1959 CUT OUT DAMAGE SEAT TRACK,CUT OUT LENGTH=53 INCH AT FR62,Y1959. FABRICATE THE NEW SEAT TRACK AND REPAIR U-SECTION AND INSTALL ALL REPAIR PARTS WET WITH FASTENERS. I.A.
- [SDR FDEA202404100539](https://openairdocs.org/sdr/FDEA202404100539.md): Seat Track · gouged · Apr 10, 2024 · N661FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK COMPT FLOOR - SEAT TRACK CROWN AREA GOT GOUGED LOCATION AT FR62 PLUS 2",Y1959 CUT OUT DAMAGE SEAT TRACK,CUT OUT LENGTH=53 INCH AT FR62,Y1959. FABRICATE THE NEW SEAT TRACK AND REPAIR U-SECTION AND INSTALL ALL REPAIR PARTS WET WITH FASTENERS. I.A.
- [SDR FDEA202404100486](https://openairdocs.org/sdr/FDEA202404100486.md): Elevator · none · Apr 10, 2024 · N661FE · Airbus A300F4605R · Standard Practices/Structures
  > 00087566N00547 AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON R/H ELEVATOR UPR SKIN AT ER10-8", T/E-23.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACK
- [SDR FDEA202404100468](https://openairdocs.org/sdr/FDEA202404100468.md): Elevator · none · Apr 10, 2024 · N661FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER16-16", T/E-10.9" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENT
- [SDR FDEA202404070540](https://openairdocs.org/sdr/FDEA202404070540.md): Support Bracket · cracked · Apr 7, 2024 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > RH AIR CONDITION 144FR FAIRING LOWER SUPPORT BRACKET CRACK AT FR44,S-51R POSITION. REPLACED THE ANGLE BRACKET WITH NEW ONE IAW A300-600F SRM51-72-10-001 PAGE 2 THIS REPAIR CLASSIFIED AS MINOR PER GMM6-2-100 (AT FR44, S-51R FAIRING LOWER SUPPORT BRACKET)
- [SDR FDEA202404070465](https://openairdocs.org/sdr/FDEA202404070465.md): None · none · Apr 7, 2024 · N661FE · Airbus A300F4605R · Standard Practices/Structures
  > 00087566N00415 AIRCRAFT REPAIR ASSESSMENT: EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK BTW FR77 TO FR80/82, Y0 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQU
- [SDR FDEA202404060541](https://openairdocs.org/sdr/FDEA202404060541.md): Support Bracket · cracked · Apr 6, 2024 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > LH AIRCONDITION 143FL FAIRING LOWER SUPPORT ANGLE BRACKET CRACK AT FR44,S-51L POSITION. REPLACED THE ANGLE BRACKET WITH NEW ONE IAW A300-600F SRM 51-72-10-001 PAGE 2 THIS REPAIR CLASSIFIED AS MINOR PER GMM6-2-100 (AT FR44, S-51L FAIRING LOWER SUPPORT BRA
- [SDR FDEA202404050649](https://openairdocs.org/sdr/FDEA202404050649.md): Skin · cracked · Apr 5, 2024 · N661FE · Airbus A300F4605R · Trailing Edge Flaps
  > 2EA CRACKS (MAX:20MM) WERE FOUND AT LH WING CENTER FLAP RIB25 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AT RIB25 UPPER FLANGE S-2.7~REAR SPAR AND EXTERNAL DOUBLERS REPAIR AT RIB26~25 S-2.2~REAR SPAR PLUS 10 INCHES, THE REPAIR CL
- [SDR FDEA202404050648](https://openairdocs.org/sdr/FDEA202404050648.md): Skin · cracked · Apr 5, 2024 · N661FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1EA CRACK (75MM) WAS FOUND AT LH WING CENTER FLAP RIB20 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB 20 BETWEEN UPPER SKIN S-2.8 TO REAR SPAR AND EXTERNAL DOUBLER REPAIR ENCLOSED BY LOWER SKIN RIB 19 TO RIB 20 AND S-2.1 TO REAR
- [SDR FDEA202404050646](https://openairdocs.org/sdr/FDEA202404050646.md): Skin · cracked · Apr 5, 2024 · N661FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1EA CRACK (25MM) WAS FOUND AT LH WING CENTER FLAP RIB13 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB 13 UPPER FLANGE S-2.7~S-2.8, THE REPAIR CLASSIFIED AS CAT.A MAJOR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T0378801 P1, SEQ
- [SDR FDEA202404050638](https://openairdocs.org/sdr/FDEA202404050638.md): Skin · cracked · Apr 5, 2024 · N661FE · Airbus A300F4605R · Trailing Edge Flaps
  > 3EA CRACKS (MAX70MM) WERE FOUND AT LH WING FLAP OF CENTER RIB12 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AT RIB12 UPPER FLANGE S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T03788
- [SDR FDEA202404050637](https://openairdocs.org/sdr/FDEA202404050637.md): Skin · cracked · Apr 5, 2024 · N661FE · Airbus A300F4605R · Trailing Edge Flaps
  > 4EA CRACKS (MAX50MM) WERE FOUND AT LH WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB 11 UPPER FLANGE S-2.7~REAR SPAR AND EXTERNAL DOUBLER REPAIR AT RIB11~RIB13 S-2.2~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.
- [SDR FDEA202404050636](https://openairdocs.org/sdr/FDEA202404050636.md): Skin · cracked · Apr 5, 2024 · N661FE · Airbus A300F4605R · Trailing Edge Flaps
  > 4EA CRACKS (MAX50MM) WERE FOUND AT LH WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB 11 UPPER FLANGE S-2.7~REAR SPAR AND EXTERNAL DOUBLER REPAIR AT RIB11~RIB13 S-2.2~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.
- [SDR FDEA202404050609](https://openairdocs.org/sdr/FDEA202404050609.md): Support Bracket · cracked · Apr 5, 2024 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > LH LANDING GEAR DOOR OPEN ON GROUND PANEL INSIDE FWD SUPPORT BRACKET CRACK AT FR43, S-51L POSITION REPLACED THE DAMAGE SUPPORT WITH NEW AT FR43, S-51L I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.7, PAGE.24-50 REPAIR CLASSIFIED AS MINOR
- [SDR FDEA202404050536](https://openairdocs.org/sdr/FDEA202404050536.md): Support · cracked · Apr 5, 2024 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AFT CGO COMP'T CEILING PANEL SUPPORT CRACK AT ENTRY AREA BTW FR60-FR61 POSITION. REPLACED THE HEADER WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21- 001, PARA6 PAGE7B~PAGE23, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 AND LOCATE
- [SDR FDEA202404020621](https://openairdocs.org/sdr/FDEA202404020621.md): Plate · cracked · Apr 2, 2024 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FWD CGO COMP'T UNDER FLOOR AREA LH SIDE PLATE CRACK AT S-43L~S-44L, FR21 POSITION. REPLACED THE SIDE PLATE WITH NEW PART AT FR21 AND S-43L~44L, I.A.W A300-600F SRM 51-72- 10-001, PAGE 2 & 51-40-21-001, PARA 6~7, PAGE 7B~50. REPAIR CLASSIFIED AS MINOR PER GMM
- [SDR FDEA202404020546](https://openairdocs.org/sdr/FDEA202404020546.md): Seat Track · gouged · Apr 2, 2024 · N661FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR - SEAT TRACK CROWN AREA GOT SOME GOUGES LOCATION FROM FR50 TO FR50 PLUS 3" AND Y0 ACCOMPLISHED THE MAIN DECK SEAT TRACK SPLICE REPAIR AT FR49~FR54 Y0, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA:T6-5310-T03788
- [SDR FDEA202404020545](https://openairdocs.org/sdr/FDEA202404020545.md): Seat Track · gouged · Apr 2, 2024 · N661FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR - SEAT TRACK CROWN AREA GOT SOME GOUGES LOCATION FROM FR50 TO FR50 PLUS 3" AND Y0 ACCOMPLISHED THE MAIN DECK SEAT TRACK SPLICE REPAIR AT FR49~FR54 Y0, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA:T6-5310-T03788
- [SDR FDEA202404020544](https://openairdocs.org/sdr/FDEA202404020544.md): Skin · damaged · Apr 2, 2024 · N661FE · Airbus A300F4605R · Elevator Structure
  > 1EA WATER TRAPPED AREA(70MM X 150MM) WAS FOUND AT R/H ELEVATOR UPPER SKIN PANEL T/E NO.9 SCREW AREA. ACCOMPLISHED THE CAT.A MAJOR COMPOSITE REPAIR AT RH ELEVATOR UPPER SKIN PANEL NO.9 T/E SCREW PER GMM 6-2-100 I.A.W A300-600F SRM 55-21-12-201, PARA 5J, PAGE
- [SDR FDEA202404020543](https://openairdocs.org/sdr/FDEA202404020543.md): Skin · damaged · Apr 2, 2024 · N661FE · Airbus A300F4605R · Elevator Structure
  > 1EA WATER TRAPPED AREA(110MM X 250MM) WAS FOUND AT R/H ELEVATOR UPPER SKIN PANEL T/E NO.25 SCREW AREA. ACCOMPLISHED THE CAT.A MAJOR COMPOSITE REPAIR AT RH ELEVATOR UPPER SKIN PANEL NO.25 T/E SCREW PER GMM 6-2-100 I.A.W A300-600F SRM 55-21-12-201, PARA 5J,

Next page: https://openairdocs.org/aircraft/N661FE/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 = 'N661FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N661FE/reports

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