# Service difficulty reports: N660FE

A list on [N660FE](https://openairdocs.org/aircraft/N660FE.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 5 · 227 reports

- [SDR FDEA202605310657](https://openairdocs.org/sdr/FDEA202605310657.md): Door · cracked · May 31, 2026 · N660FE · Airbus A300F4605R · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR22 AND FR25 FOUND CRACK SIGNAL ON 6EA FASTENER HOLES. REPAIRED THE CRACKED FASTENER HOLES AT MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR22 AND FR25 PER EA 6-5230-T0387491 P1. CRACKED HOLES ON MAIN DECK CAR
- [SDR FDEA202605290658](https://openairdocs.org/sdr/FDEA202605290658.md): Frame · cracked · May 29, 2026 · N660FE · Airbus A300F4605R · Fuselage Main, Frame
  > RH CENTER BOX REAR SPAR FR47 BOTTOM PANEL "D" HOLE FOUND CRACKED SIGNAL. REPAIRED THE "D" HOLE ON RH CENTER WING BOX REAR SPAR FR47 BOTTOM PANEL PER EA 6- 5710-T0387476 P1. EA TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLE D AT FR47 RHS DURING SB57-6086
- [SDR FDEA202605280664](https://openairdocs.org/sdr/FDEA202605280664.md): Skin · cracked · May 28, 2026 · N660FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING INNER FLAP TOP SKIN FOUND CARCKED BTW RIB16 AND RIB17, STGR 2.1 AND STGR 2.2. REPAIRED THE CRACKED SKIN AT RH WING INNER FLAP BTW RIB16 AND RIB17, STGR 2.1 AND STGR 2.2 PER SRM57-50-00-201 PARA.4E FIG.205. RSC TRACKING EA 6-5750-T0387591 WAS RAISE
- [SDR FDEA202605230659](https://openairdocs.org/sdr/FDEA202605230659.md): Floor Support · corroded · May 23, 2026 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK - FWD COURIER AREA FR11-FR14 Y1456 LONGITUDINAL FLOOR SUPPORT CORRODED
- [SDR FDEA202605230649](https://openairdocs.org/sdr/FDEA202605230649.md): Web · cracked · May 23, 2026 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MDC - UNDER FLOOR WEB CRACKED AT FR47 Y-953 - Y-1456. REPAIRED THE CRACKED WEB ON MDC - UNDER FLOOR AT FR47 Y-953 - Y-1456 PER A300-600F SRM53-15-15-201 FIG.201. THIS IS A CATEGORY B REPAIR AND IT MUST BE INSPECTED AT DEFINED INTERVAL PER A300-600F SRI53-1
- [SDR FDEA202605230636](https://openairdocs.org/sdr/FDEA202605230636.md): Web · cracked · May 23, 2026 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MDC - UNDER FLOOR WEB CRACKED AT FR47 Y0 - Y-450. REPAIRED THE CRACKED WEB ON MDC - UNDER FLOOR AT FR47 Y0 - Y-450 PER A300-600F SRM53- 15-15-201 FIG.201. THIS IS A CATEGORY B REPAIR AND IT MUST BE INSPECTED AT DEFINED INTERVAL PER A300-600F SRI53-15-15-2-
- [SDR FDEA202605220635](https://openairdocs.org/sdr/FDEA202605220635.md): Skin · delaminated · May 22, 2026 · N660FE · Airbus A300F4605R · Spoilers
  > RH WING NR 5 SPOILER CENTER HINGE ARM INBD SIDE ARM OUTBD SURFACE DELAMINATED. 38MM*13MM*0.98MM. COMPLIED WITH EA 6-5750-T0387449 P1 REPAIRED THE DELAMINATION ON RT WING NR 5 SPOILER CENTER HINGE ARM INBD SIDE ARM OUTBD SURFACE. EA TITLE: WING - FLIGHT SU
- [SDR FDEA202605210634](https://openairdocs.org/sdr/FDEA202605210634.md): Door Frame · cracked · May 21, 2026 · N660FE · Airbus A300F4605R · Fuselage Main, Structure
  > RH PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKS. REPLACED THE CRACKED SEGMENT ON RH PAX DOOR FRAME AT FR14C PER A300-600F SRM51- 40-21 AND DWG: F52181299(ISSUE: G). RSC TRACKING EA: 6-5210-T0387549 RAISED AND ACCOMPLISHED. TITLE: DOORS - PASSENGER/CREW
- [SDR FDEA202605190780](https://openairdocs.org/sdr/FDEA202605190780.md): Rib · cracked · May 19, 2026 · N660FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB26 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0377102 A P2 PERFORMED HFEC INSPECTION TO CONFIRM THE CRACK IN LH WING CENTER FLAP RIB26 UPR FLANGE BETWEEN STGR2.7 AND STGR2.8 AND REMOVED
- [SDR FDEA202605190633](https://openairdocs.org/sdr/FDEA202605190633.md): Rib · cracked · May 19, 2026 · N660FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB13 BETWEEN STGR2.6 AND STGR2.7 & RIB15 BETWEEN STGR2.7 AND STGR2.8. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB3 BETWEEN REAR SPAR A
- [SDR FDEA202605190632](https://openairdocs.org/sdr/FDEA202605190632.md): Rib · cracked · May 19, 2026 · N660FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB11 BETWEEN REAR SPAR AND STGR2.8 & BETWEEN STGR2.7 AND STGR2.8. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB11 BETWEEN REAR SPAR AND
- [SDR FDEA202605190631](https://openairdocs.org/sdr/FDEA202605190631.md): Rib · cracked · May 19, 2026 · N660FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB13 BETWEEN STGR2.6 AND STGR2.7 & RIB15 BETWEEN STGR2.7 AND STGR2.8. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB13 BETWEEN STGR2.6 AN
- [SDR FDEA202605190630](https://openairdocs.org/sdr/FDEA202605190630.md): Rib · cracked · May 19, 2026 · N660FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB19 & RIB20 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0377102 A P2 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 2EA CRACKS AT RIB19 & RIB20 BETWEEN STGR2.8 AND REAR SPAR. EA TI
- [SDR FDEA202605150792](https://openairdocs.org/sdr/FDEA202605150792.md): Bearing Fitting · damaged · May 15, 2026 · N660FE · Airbus A300F4605R · Cargo/Baggage Doors
  > CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTING 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 OF THE MAI
- [SDR FDEA202605150622](https://openairdocs.org/sdr/FDEA202605150622.md): Stringer · corroded · May 15, 2026 · N660FE · Airbus A300F4605R · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT S44R STRINGER CORRODED AT FR38.2 - FR39. REPAIRED THE CORRODED S44R STRINGER AT FWD CARGO COMPARTMENT FR38.2 - FR39 IAW SRM 53-10-14-201, FIG 208 & EA 6-5310-T0387401, P1. THE FOLLOW UP INSPECTION REQUIREMENT IAW SRI/IIR 53-10-14-2-008-
- [SDR FDEA202602140196](https://openairdocs.org/sdr/FDEA202602140196.md): Safety Wire · wrong part · Feb 14, 2026 · N660FE · Airbus A300F4605R · Escape Slide
  > WHILE PERFORMING F.E.A. 6-2560-F0386375 A P1 FOUND SAFETY WIRE FOR EJECTOR BAG RELEASE CABLE INCORRECT. R1 DOOR AMM: 25-61-20-05-01 REMOVED AND REPLACED SAFETY WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. OPS CHK GOOD. A/C OK FOR SERVICE. INSPECTED
- [SDR FDEA202602140195](https://openairdocs.org/sdr/FDEA202602140195.md): Safety Wire · wrong part · Feb 14, 2026 · N660FE · Airbus A300F4605R · Escape Slide
  > WHILE PERFORMING F.E.A. 6-2560-F0386375 A P1 FOUND SAFETY WIRE FOR PACKBOARD CABLE WIRE INCORRECT. R1 DOOR - AMM: 25-61-20-05-01 REMOVED AND REPLACED SAFETY WIRE FROM PACKBOARD RELEASE CABLE WITH MS20995C15 STAINLESS STEEL WIRE. INSPECTED BY VENDOR. OP
- [SDR FDEA202509251831](https://openairdocs.org/sdr/FDEA202509251831.md): Computer · failed · Sep 25, 2025 · N660FE · Airbus A300F4605R · Fire Detection
  > AFTER DEPARTURE, APPROXIMATELY 1,000 FEET MSL, AVIONICS SMOKE OVERHEAD ALERT, MASTER WARNING BELL AND ECAM ALERT. COMPLIED WITH ECAM AND QRH. EMERGENCY DECLARED. NO REFERENCE REQUIRED PER CREW INPUT NO SMOKE WAS NOTICED IN THE COCKPIT, ONLY THE INDICATI
- [SDR FDEA202507011086](https://openairdocs.org/sdr/FDEA202507011086.md): Seat Track · damaged · Jul 1, 2025 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > WHILE EVALUATING SEAT TRACK DAMAGE UNDER WRI 25-50/8707, FOUND THAT WRONG LOCK WAS IDENTIFIED AND PLACED ON MEL WRI 25-50/8709. DAMAGE TO SEAT TRACK IS UNDER LOCK ID MB0828. LOCK IS STILL LOCATED IN COAT CLOSET. CREATING NEW WRI FOR WRI 25-50/872 OIL. REF
- [SDR FDEA202501240134](https://openairdocs.org/sdr/FDEA202501240134.md): Rib · corroded · Jan 24, 2025 · N660FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > LEFT RIB 5 AFT PINTLE BETWEEN BUSH "D" AND "E" HAS EVIDENCE OF CORROSION. PERFORMED REPAIR ON EA# 6-5710-T0381764 PT1. EA TITLE: WINGS - BASIC WING STRUCTURE - L/H MAIN LANDING GEAR RIB 5, FWD LUG CORROSION. MAJOR REPAIR
- [SDR FDEA202403190314](https://openairdocs.org/sdr/FDEA202403190314.md): Bottle · failed · Mar 19, 2024 · N660FE · Airbus A300F4605R · Emergency Equipment
  > R1 DOOR DAMPER AND EMERGENCY OPERATING CYLINDER PRESSURE BELOW DISPATCH MINIMUMS. SERVICED R1 DOOR DAMPER/EMERGENCY OPERATION CYLINDER REF A300 AMM 52-10-14-03-02 AND PLACARD. ACFT OK TO CONTINUE.
- [SDR FDEA202403110270](https://openairdocs.org/sdr/FDEA202403110270.md): Switch · faulted · Mar 11, 2024 · N660FE · Airbus A300F4605R · Passenger/Crew Doors
  > R1 CABIN DOOR UNSAFE INDICATION ON DEPARTURE. CABIN PRESSURE INDICATIONS WERE NORMAL THROUGHOUT CLIMB. IN CRUISE, PUSHED HANDLE IAW QRH AND UNSAFE INDICATION WENT OUT FOR REMAINDER OF FLIGHT. RELEASED FOR SERVICE PER MEL 52-11-01-05 CATEGORY: C. R &
- [SDR FDEA202311251898](https://openairdocs.org/sdr/FDEA202311251898.md): Elevator · unknown · Nov 25, 2023 · N660FE · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER5-14", T/E-6" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR
- [SDR FDEA202311201956](https://openairdocs.org/sdr/FDEA202311201956.md): Header · cracked · Nov 20, 2023 · N660FE · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT CGO DOOR UPPER L/H SIDE CORNER FOUND PATCH CRACKED. REPLACED THE CRACK PART WITH NEW PART I.A.W A300-600F SRM 51-72-10-001 PAGE 2.
- [SDR FDEA202311201930](https://openairdocs.org/sdr/FDEA202311201930.md): Dummy Rail · damaged · Nov 20, 2023 · N660FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > M/D CARGO COMPARTMENT FOUND NO.1 DUMMY SEAT TRACK (NO.1) CROWN BROKEN AT FR54.1 PLUS 4",RBL0 POS. ACCOMPLISHED THE DUMMY SEAT TRACK REPLACEMENT I.A.W A300-600F SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.7, PAGE.24-50
- [SDR FDEA202311161866](https://openairdocs.org/sdr/FDEA202311161866.md): Skin · unknown · Nov 16, 2023 · N660FE · Airbus A300* · Standard Practices/Structures
  > EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BETWEEN STRINGER 6~8L, FRAME 84~85,EVALUATE TO DETERMINE WHETHER IT IS MAJOR OR MINOR AND WHETHER ACCOMPLISHED PER APPROVED DATA COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAI
- [SDR FDEA202311151966](https://openairdocs.org/sdr/FDEA202311151966.md): Rib · corroded · Nov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > R5 SPLR JACK RIB BOLT BORE CORRODED AT LOACTION NO.1, NO.3 AND NO.4 ACCOMPLISHED THE REINFORCING REPAIR AT RH #5 SPOILER I/B & O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377191 P1,SEQ NO:760,TITLE: WINGS-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIB AT STA ABX
- [SDR FDEA202311151963](https://openairdocs.org/sdr/FDEA202311151963.md): Rib · corroded · Nov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > R7 SPLR JACK RIB BOLT BORE CORRODED AT LOACTION NO.1 ACCOMPLISHED THE REINFORCING REPAIR AT RH #7 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377209 P1,SEQ NO:763,TITLE: WINGS-ATTACH FITTINGS-RH WING #7 SPOILER JACK RIB AT STA SP2X 40.425-BEAM ATTACHM
- [SDR FDEA202311151962](https://openairdocs.org/sdr/FDEA202311151962.md): Rib · corroded · Nov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > R4 SPLR JACK RIB BOLT BORES CORRODED AT LOCATION NO.1 AND NO.2 ACCOMPLISHED THE REINFORCING REPAIR AT RH #4 SPOILER I/B & O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377195 P1,SEQ NO:766,TITLE: WINGS-ATTACH FITTINGS-RH WING #4 SPOILER JACK RIB AT STA ABX 103.
- [SDR FDEA202311151961](https://openairdocs.org/sdr/FDEA202311151961.md): Rib · corroded · Nov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > R3 SPLR JACK RIB BOLT BORES CORRDED AT LOCATION NO.2 AND NO.3 ACCOMPLISHED THE REINFORCING REPAIR AT RH #3 SPOILER I/B & O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377189 P1,SEQ NO:765,TITLE: WINGS-ATTACH FITTINGS-RH WING #3 SPOILER JACK RIB AT STA ABX 31.67
- [SDR FDEA202311151960](https://openairdocs.org/sdr/FDEA202311151960.md): Rib · corroded · Nov 15, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > R6 SPLR JACK RIB BOLT BORE CORRODED AT LOCATION NO.1. ACCOMPLISHED THE REINFORCING REPAIR AT RH #6 SPOILER O/B JACK RIB I.A.W FEDEX EA NO: T6-5740-T0377208 P1, SEQ NO:761, TITLE: WINGS-ATTACH FITTINGS-RH WING #6 SPOILER JACK RIB AT STA SP1X 40.425 - BEAM A
- [SDR FDEA202311141965](https://openairdocs.org/sdr/FDEA202311141965.md): Rib · corroded · Nov 14, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > LH WING SPOILER NO.5 I/B JACK RIB BOLT HOLES CORRODED AT BEAM ATTACHMENT BOLT LOCATION #1 & #3 ACCOMPLISHED THE REINFORCING REPAIR AT LH #5 SPOILER I/B JACK RIB I.A.W FEDEX EA NO:T6- 5740-T0377193 P1,SEQ NO:764,TITLE: WINGS-ATTACH FITTINGS-LH WING #5 SPOILE
- [SDR FDEA202311141964](https://openairdocs.org/sdr/FDEA202311141964.md): Rib · corroded · Nov 14, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > LH WING SPOILER NO.5 O/B JACK RIB BOLT HOLES CORRODED AT BEAM ATTACHMENT BOLT LOCATION #2 & #4 ACCOMPLISHED THE REINFORCING REPAIR AT LH #5 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377193 P1,SEQ NO:764,TITLE: WINGS-ATTACH FITTINGS-LH WING #5 SPOILE
- [SDR FDEA202311141959](https://openairdocs.org/sdr/FDEA202311141959.md): Rib · corroded · Nov 14, 2023 · N660FE · Airbus A300* · Wing, Rib/Bulkhead
  > LH WING SPOILER NO.3 O/B JACK RIB BOLT HOLE CORRODED AT BEAM ATTACHMENT BOLT LOCATION #2 ACCOMPLISHED THE REINFORCING REPAIR AT LH #3 SPOILER O/B JACK RIB I.A.W FEDEX EA NO:T6-5740-T0377187A P1,SEQ NO:762,TITLE: WINGS-ATTACH FITTINGS-LH WING #3 SPOILER JAC
- [SDR FDEA202311131953](https://openairdocs.org/sdr/FDEA202311131953.md): Stringer Splice · corroded · Nov 13, 2023 · N660FE · Airbus A300* · Fuselage Main, Longeron/Stringer
  > AVIONICS COMPT BILGES GOT A STRINGER CORRODED AT FR19-2", STR-52L REPLACED THE SPLICE WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6, PAGE.7B~23
- [SDR FDEA202311131895](https://openairdocs.org/sdr/FDEA202311131895.md): Skin · dented · Nov 13, 2023 · N660FE · Airbus A300* · Fuselage Main, Plate/Skin
  > FUSELAGE TAIL SKIN FOUND 1EA BULGED AT FR93 PLUS 5.3",S-16R PLUS 3.5",POS. CUT OUT DAMAGE AREA,FABRICATED THE REPAIR DOUBLER,WET INSTALLED REPAIR DOUBLER WITH FASTENERS. I.A.W A300-600F SRM 53-19-12-201,PARA.6B,FIG202,PAGE213~PAGE218. "MAJOR REPAIR"
- [SDR FDEA202311131894](https://openairdocs.org/sdr/FDEA202311131894.md): Skin · dented · Nov 13, 2023 · N660FE · Airbus A300* · Fuselage Main, Plate/Skin
  > FUSELAGE TAIL SKIN FOUND 5EA BULGEDS AT FR92 PLUS 4.4", S-16R PLUS 1.8", FR92 PLUS 3", S- 16R PLUS 2.4", FR92 PLUS 5.5", S-17R PLUS 0.9", FR92 PLUS 5.4", S-17R PLUS 2.5", FR92 PLUS 2.8", S-17R PLUS 4.7" POS. CUT OUT DAMAGE AREA, FABEICATED THE REPAIR DOUBL
- [SDR FDEA202311120003](https://openairdocs.org/sdr/FDEA202311120003.md): Retainer · corroded · Nov 12, 2023 · N660FE · Airbus A300* · Fuselage Structure (General)
  > FR40 BULKHEAD T/E LWR SURFACE RETAINER CORRODED. ACCOMPLISHED THE DOUBLER REPAIR TO THE DAMAGE AREA I.A.W FEDEX EA NO:T6-5310- T0377351 P1, SEQ NO:774,TITLE:FUSELAGE - MAINFRAME - PRESSURE FLOOR PANEL REPAIR AT FR40 BETWEEN Y953 AND -Y1456 DUE TO HEAVY EXFO
- [SDR FDEA202311121897](https://openairdocs.org/sdr/FDEA202311121897.md): Slat · gouged · Nov 12, 2023 · N660FE · Airbus A300* · Leading Edge Devices
  > R1 SLAT CHAFING AT RIB20 PLUS 3", T/E -13". ACCOMPLISHED THE BONDED REPAIR WITH SKIN FILLER PIECE AND REPAIR PATCH I.A.W FEDEX EA NO:T6-5750-T0377084 P1, SEQ NO:752, TITLE:WING-FLIGHT SURFACES-RH #1 SLAT-GOUGE DAMAGE FOUND ON TAIL SECTION OUTBOARD LOWER SK
- [SDR FDEA202311100008](https://openairdocs.org/sdr/FDEA202311100008.md): Slat · damaged · Nov 10, 2023 · N660FE · Airbus A300* · Leading Edge Devices
  > LH WING #1 SLAT "D" NOSE SKIN EXTERNAL SURFACE FOUND SLIGHT CREASED AT JACK RIB 1 LOWER SECTION ACCOMPLISHED THE EXTERNAL DOUBLER REPAIR AT JACK RIB 1 I.A.W FEDEX EA NO:T6-5750- T0377059 P1, SEQ NO:775, TITLE:WING - FLIGHT SURFACES - LH #1 SLAT - 02EA CREAS
- [SDR FDEA202311100002](https://openairdocs.org/sdr/FDEA202311100002.md): Slat · damaged · Nov 10, 2023 · N660FE · Airbus A300* · Leading Edge Devices
  > LH WING #1 SLAT "D" NOSE SKIN EXTERNAL SURFACE FOUND SLIGHT CREASED AT JACK RIB 1 LOWER SECTION ACCOMPLISHED THE EXTERNAL DOUBLER REPAIR AT JACK RIB 1 IAW FEDEX EA T6-5750- T0377059 P1, SEQ NO:775, TITLE:WING - FLIGHT SURFACES - LH #1 SLAT - 02EA CREASE LIN
- [SDR FDEA202311100001](https://openairdocs.org/sdr/FDEA202311100001.md): Slat · damaged · Nov 10, 2023 · N660FE · Airbus A300* · Leading Edge Devices
  > LH WING #1 SLAT "D" NOSE SKIN EXTERNAL SURFACE FOUND CREASED AT TRACK RIB 1 LWR SECTION ACCOMPLISHED THE FLUSH REPAIR AT TRACK RIB 1 I.A.W FEDEX EA NO:T6-5750-T0377059 P1, SEQ NO:775, TITLE:WING - FLIGHT SURFACES - LH #1 SLAT - 02EA CREASE LINES FOUND ON
- [SDR FDEA202311101946](https://openairdocs.org/sdr/FDEA202311101946.md): Slat · damaged · Nov 10, 2023 · N660FE · Airbus A300* · Leading Edge Devices
  > R3 SLAT LWR SURFACE PROTUDER AT RIB37-3", T/E-6.5". ACCOMPLISHED THE COLD WORK TO THE PROTUDED LWR SKIN I.A.W FEDEX EA NO:T6-5750- T0377056 P1, SEQ NO:768, TITLE:WING-FLIGHT SURFACES-RH WING-#3 SLAT UPPER SKIN PUNCTURE BETWEEN RIB36 AND 37 "MAJOR REPAIR"
- [SDR FDEA202311101945](https://openairdocs.org/sdr/FDEA202311101945.md): Slat · damaged · Nov 10, 2023 · N660FE · Airbus A300* · Leading Edge Devices
  > R3 SLAT UPPER SURFACE PUNTURED AT RIB37-3", T/E-6.5" CUT OUT THE DAMAGE AREA AND INSTALLED THE EXTERNAL PATCH I.A.W FEDEX EA NO:T6-5750- T0377056 P1, SEQ NO:768, TITLE:WING-FLIGHT SURFACES-RH WING-#3 SLAT UPPER SKIN PUNCTURE BETWEEN RIB36 AND 37 "MAJOR REP
- [SDR FDEA202311101935](https://openairdocs.org/sdr/FDEA202311101935.md): Flap · cracked · Nov 10, 2023 · N660FE · Airbus A300* · Trailing Edge Flaps
  > 8EA CRACKS (MAX 27MM) WERE FOUND AT LH WING CENTER FLAP RIB12 FWD, 15 FWD, 18 AFT, 27 FWD, 27 AFT AND 25 AFT(3EA) AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE RIB FLANGE REPAIRS AND EXTERNAL DOUBLER REPAIRS I.A.W FEDEX EA NO:T6-5750-T0377102 P1, SEQ NO:
- [SDR FDEA202311081879](https://openairdocs.org/sdr/FDEA202311081879.md): Fitting · cracked · Nov 8, 2023 · N660FE · Airbus A300* · Fuselage Main, Structure
  > FLOOR CROSSBEAM 10 PICK-UP FITTING CRACK AT Y-953 POSITION REMOVED CRACK PICK-UP FITTING,THEN INSTALLED NEW ONE WITH FASTENERS I.A.W A300-600F SRM 51-72-10-001,PAGE 2 & 51-40-21-001, PARA.6,PAGE 7B~23
- [SDR FDEA202311081878](https://openairdocs.org/sdr/FDEA202311081878.md): Angle · cracked · Nov 8, 2023 · N660FE · Airbus A300* · Fuselage Miscellaneous Structure
  > FLOOR CROSSBEAM 10 ANGLE FITTING CRACK AT Y-953 POSITION REMOVED CRACK ANGLE FITTING,THEN INSTALLED NEW ONE WITH FASTENERS I.A.W A300-600F SRM 51-72-10-001,PAGE 2 & 51-40-21-001, PARA.6,PAGE 7B~23
- [SDR FDEA202311081877](https://openairdocs.org/sdr/FDEA202311081877.md): Strap · cracked · Nov 8, 2023 · N660FE · Airbus A300* · Fuselage Miscellaneous Structure
  > FUSELAGE INNER S-39R PLATE WEB FOUND STRAP CRACK BETWEEN FR86 & FR87 AREA CRACKED STRAP REPLACED NEW PART,INSTALLED WITH RIVETS I.A.W A300-600F SRM 51-72-10- 001,PAGE 2 AND 51-40-21-001,PARA 6,PAGE 7B-PAGE 23
- [SDR FDEA202311071851](https://openairdocs.org/sdr/FDEA202311071851.md): Flap · unknown · Nov 7, 2023 · N660FE · Airbus A300* · Trailing Edge Flaps
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH O/B FLAP UPR SKIN AT RIB 26A,T/E-2" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 12
- [SDR FDEA202108122008](https://openairdocs.org/sdr/FDEA202108122008.md): Check Valve · dirty · Aug 12, 2021 · N660FE · Airbus A300F4605R · Hydraulic System, Main
  > AFTER BLOCKOUT AT ENGINE START WHEN BLEEDS OPENED WITH BOTH PACKS RUNNING, GOT SMOKE (HYDRALIC FLUID) OUT OF VENTS. ON ENTRY INTO ARCFT, AFTER ENGINE SHUTDOWN, CABIN HAD DISTINCT ODOR OF HYD FLUID. REMOVED AND REPLACED APU PRESSURIZATION LINE ISOLATION CH

Next page: https://openairdocs.org/aircraft/N660FE/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 = 'N660FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N660FE/reports

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