# Service difficulty reports: N662FE

A list on [N662FE](https://openairdocs.org/aircraft/N662FE.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 · 229 reports

- [SDR FDEA202607100896](https://openairdocs.org/sdr/FDEA202607100896.md): Sensor · faulted · Jul 10, 2026 · N662FE · Airbus A300F4605R · Hydraulic Reservoir, Main
  > GREEN SYSTEM OVERHEAT LIGHT FLASHING AND CHIME WARINING.
- [SDR FDEA202605250637](https://openairdocs.org/sdr/FDEA202605250637.md): Actuator · stuck · May 25, 2026 · N662FE · Airbus A300F4605R · Pressure Regulator/Outflow Valve
  > AIR RETURN IN RJAA DUE TO CABIN PRESSURE 1 & 2 FAULT. FORWARD OUTFLOW VALVE STUCK FULL OPEN. NO EMERGENCY OR PRIORITY DECLARED. R & R FWD OUTFLOW VALVE ACTUATOR PER AMM 21-31-12-04.
- [SDR FDEA202604240530](https://openairdocs.org/sdr/FDEA202604240530.md): Frame · cracked · Apr 24, 2026 · N662FE · Airbus A300F4605R · Fuselage Main, Frame
  > INSPECTION OF FR40 LOWER JUNCTION FASTENER HOLE NR 3 RT SIDE FOUND CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0387217 P1 TO REPAIR FR40 RH SIDE LOWER JUNCTION CRACKED FASTENER HOLE #3, MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57107960 FOR WORK DETAILS.
- [SDR FDEA202604230503](https://openairdocs.org/sdr/FDEA202604230503.md): Skin · delaminated · Apr 23, 2026 · N662FE · Airbus A300F4605R · Spoilers
  > LEFT WING NR 5 SPOILER INBD MID HINGE ARM OTBD SURFACE DELAMINATED. SIZE: 60 MM - 23 MM - DEPTH: 1.0 MM. COMPLIED WITH EA:6-5750-T0387139 P1 TO REPAIR LH WING #5 SPOILER I/B MID HINGE ARM O/B SURFACE DELAMINATION, HIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW
- [SDR FDEA202604190507](https://openairdocs.org/sdr/FDEA202604190507.md): Rib · cracked · Apr 19, 2026 · N662FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT CENTER FLAP RIB UPPER FLANGE FOUND ONE CRACK AT RIB 11 BETWEEN STGR 2.7 AND STGR 2.8. COMPLIED WITH EA:6-5750-T0344015 A P2 TO REPAIR LH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB11 BETWEEN STGR2.7 AND STGR2.8, EA TITLE: WINGS - FLIGHT SURFACES - CR
- [SDR FDEA202604190506](https://openairdocs.org/sdr/FDEA202604190506.md): Rib · cracked · Apr 19, 2026 · N662FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT CENTER FLAP RIB UPPER FLANGE FOUND ONE CRACK AT RIB 25 BETWEEN STGR 2.8 AND REAR SPAR. COMPLIED WITH EA:6-5750-T0344015 A P2 TO REPAIR LH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB25 BETWEEN STGR2.8 AND REAR SPAR, EA TITLE: WINGS - FLIGHT SURFACES -
- [SDR FDEA202604190505](https://openairdocs.org/sdr/FDEA202604190505.md): Rib · cracked · Apr 19, 2026 · N662FE · Airbus A300F4605R · Trailing Edge Flaps
  > RIGHT CENTER FLAP RIB UPPER FLANGE FOUND ONE CRACK AT RIB 13 BETWEEN STGR 2.7 AND STGR 2.8. COMPLIED WITH EA:6-5750-T0344016 A P2 TO REPAIR RH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB13 BETWEEN STGR2.7 AND STGR2.8, EA TITLE: WINGS - FLIGHT SURFACES - C
- [SDR FDEA202604190504](https://openairdocs.org/sdr/FDEA202604190504.md): Rib · cracked · Apr 19, 2026 · N662FE · Airbus A300F4605R · Trailing Edge Flaps
  > RIGHT CENTER FLAP RIB UPPER FLANGE FOUND ONE CRACK AT RIB 25 BETWEEN STGR 2.7 AND STGR 2.8. COMPLIED WITH EA:6-5750-T0344016 A P2 TO REPAIR RH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB25&RIB27 BETWEEN STGR2.7 AND STGR2.8, EA TITLE: WINGS - FLIGHT SURFACES
- [SDR FDEA202602220253](https://openairdocs.org/sdr/FDEA202602220253.md): Safety Wire · misinstalled · Feb 22, 2026 · N662FE · Airbus A300F4605R · Emergency Equipment
  > REMOVE AND REPLACE RT SLIDE. (AMM: 25-61-21-04) DURING INSPECTION FOR FEA 6-2560-F0386375 REV NO. A PS P1 FOUND EJECTOR BAG RELEASE HANDLE INCORRECTLY SAFETY WIRED AND BOTTLE EMPTY MAKING UNIT UNSERVICEABLE. REMOVED AND REPLACED RT SLIDE ASSY. OPS CHKD G
- [SDR FDEA202510031877](https://openairdocs.org/sdr/FDEA202510031877.md): Warning Light · illuminated · Oct 3, 2025 · N662FE · Airbus A300F4605R · Landing Gear Position and Warning
  > DURING GEAR RETRACTION OUT OF ORD, GOT AMBER L/G DOORS NOT CLOSED ECAM. BOTH GEAR PANELS SHOWED NOSE GEAR DOOR AMBER DOOR LIGHT ON. COMPLETED ECAM AND QRH. WE FLEW TO IND AT 260 KIAS. AMBER DOOR LIGHT REMAINED ON ENTIRE FLIGHT UNTIL GEAR EXTENSION. JACKE
- [SDR FDEA202508081873](https://openairdocs.org/sdr/FDEA202508081873.md): Battery · no test · Aug 8, 2025 · N662FE · Airbus A300F4605R · Emergency Lighting
  > COURIER AREA EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE DURING TEST. R & R EXIT LIGHT BATTERY AND OPS CHECKS GOOD. OKAY FOR SERVICE.
- [SDR FDEA202409241355](https://openairdocs.org/sdr/FDEA202409241355.md): Hydraulic System · low · Sep 24, 2024 · N662FE · Airbus A300F4605R · Hydraulic Indicating System
  > DURING CRUISE AT FL330, GREEN HYD INDICATOR NEEDLE MOVING LOWER TOWARD YELLOW RANGE. INDICATION CONTINUED MOVING RAPIDLY FROM MIDDLE GREEN RANGE INTO YELLOW RANGE. HYD PRESSURE REMAINED NORMAL. END OF FLIGHT QTY INDICATION WAS SIGNIFICANTLY LESS THAN PREVI
- [SDR FDEA202407201037](https://openairdocs.org/sdr/FDEA202407201037.md): Jackscrew · corroded · Jul 20, 2024 · N662FE · Airbus A300F4605R · Leading Edge Slat Control System
  > SLAT SYS 1 2 FAULT. QRH PROCEDURE COMPLIED WITH. PERFORMED NO SLAT LANDING. HIGHEST BRAKE TEMP ON LANDING 260. AMM: 27-84-00-02 TSM: 27-80-02 AMM: 12-13-27-00 JRH: A300-600 CARRIED OUT THE BITE CHECK ON BOTH SFCC1 AND SFCC2, BOTH SFCCS INDICATED A SL
- [SDR FDEA202310051713](https://openairdocs.org/sdr/FDEA202310051713.md): Aileron · unknown · Oct 5, 2023 · N662FE · Airbus A300* · Ailerons
  > EXISTING DOUBLER REPAIR FOUND ON LH AILERON LOWER SKIN BETWEEN RIB 15~16, TRAILING EDGE-4",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, INSPECTION OF
- [SDR FDEA202309281759](https://openairdocs.org/sdr/FDEA202309281759.md): Floorbeam · corroded · Sep 28, 2023 · N662FE · Airbus A300* · Fuselage Main, Floor Beam
  > MAIN DECK FLOOR CROSS BEAM FOUND CORROSION AT FR47 Y-330 TO Y-400 REPLACED THE CROSS BEAM WITH FASTENERS I.A.W A300-600F SRM 51-72-10-001, PAGE.2 & 51- 40-21-001, PARA.6-7, PAGE.7B~50
- [SDR FDEA202309271783](https://openairdocs.org/sdr/FDEA202309271783.md): Seat Track · corroded · Sep 27, 2023 · N662FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR SEAT TRACK FOUND CORROSION AT FR45 PLUS 3", Y450 INSTALLED NEW SECTION OF SEAT TRACK AND ACCOMPLISHED THE SPLICE REPAIR THIS IS CAT.A REPAIR I.A.W FEDEX EA NO:T6-5310-T0376506 P1, TITLE: FUSELAGE-MAINFRAME-MAIN CARGO SEAT TRACK SPLICE REPAI
- [SDR FDEA202309271724](https://openairdocs.org/sdr/FDEA202309271724.md): Angle · damaged · Sep 27, 2023 · N662FE · Airbus A300* · Fuselage Miscellaneous Structure
  > CHECK FOUND ANGLE BROKEN NEAR 6030VT AT BAY UNDER AFT CGO COMPT. REPLACED THE BROKEN ANGLE WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE.2
- [SDR FDEA202309261814](https://openairdocs.org/sdr/FDEA202309261814.md): Rib · corroded · Sep 26, 2023 · N662FE · Airbus A300* · Spoilers
  > LH WING T/E #5 SPOILER O/B JACK RIB SURROUNDING UPR BORE AREA CORROSION ACCOMPLISHED THE REINFORCING REPAIR, THIS IS CAT.B REPAIR I.A.W FEDEX EA NO:T6-5740- T0376432 P1, SEQ NO:1202, TITLE:WING-ATTACH FITTINGS-LH WING #5 SPOILER JACK RIB AT STA ABX184.625 B
- [SDR FDEA202309261813](https://openairdocs.org/sdr/FDEA202309261813.md): Rib · corroded · Sep 26, 2023 · N662FE · Airbus A300* · Spoilers
  > LH WING T/E #3 SPOILER I/B JACK RIB SURROUNDING LWR BORE AREA CORROSION ACCOMPLISHED THE REINFORCING REPAIR, THIS IS CAT.B REPAIR I.A.W FEDEX EA NO:T6-5740- T0376377 P1, SEQ NO:1201, TITLE:WING-ATTACH FITTINGS-LH WING #3 SPOILER JACK RIB AT STA ABX31.675 BE
- [SDR FDEA202309261727](https://openairdocs.org/sdr/FDEA202309261727.md): Floor Support · corroded · Sep 26, 2023 · N662FE · Airbus A300* · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR FOUND SUPPORT CORROSION BETWEEN FR11 PLUS 10" AND FR11 PLUS 16",Y730 REPLACED THE DAMAGE SUPPORT WITH NEW I.A.W A300-600F SRM 51-72-10-001, PAGE 2
- [SDR FDEA202309261723](https://openairdocs.org/sdr/FDEA202309261723.md): Profile · cracked · Sep 26, 2023 · N662FE · Airbus A300* · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE Z-PROFILE CRACK NEAR FR80/82, -Y1487. REPLACED THE NEW PROFILE-Z. I.A.W A300-600F SRM 51-72-10-001,P2
- [SDR FDEA202309261722](https://openairdocs.org/sdr/FDEA202309261722.md): Spoiler · damaged · Sep 26, 2023 · N662FE · Airbus A300* · Spoilers
  > LH WING #6 SPOILER RH SIDE HINGE ARM PARTIAL DISBONDED. REPAIRED THE HINGE ARM BY HOT BONDING REPAIR, THIS IS CAT.A REPAIR I.A.W A300-600F SRM 57-73-11-201, PARA 13, PAGE 218-221, FIG 208. MAJOR REPAIR
- [SDR FDEA202309261721](https://openairdocs.org/sdr/FDEA202309261721.md): Support · damaged · Sep 26, 2023 · N662FE · Airbus A300* · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR FOUND SUPPORT BROKEN NEAR FR37 PLUS 5", STGR26L REPLACED THE NEW SUPPORT I.A.W A300-600F SRM 51-72-10-001, P.2
- [SDR FDEA202309241790](https://openairdocs.org/sdr/FDEA202309241790.md): Bracket · cracked · Sep 24, 2023 · N662FE · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT CGO COMP'T FWD PRESSURE BULKHEAD SUPPORT BRACKET CRACK AT Y1959,FR54 POSITION. REPLACED DAMAGE PART WITH NEW ONE. I.A.W. A300-600F SRM 51-72-10-001, PAGE2.
- [SDR FDEA202309241785](https://openairdocs.org/sdr/FDEA202309241785.md): Bracket · cracked · Sep 24, 2023 · N662FE · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT CARGO COMP'T FWD PRESSURE BULKHEAD SUPPORT BRACKET CRACK AT -Y1959, FR54 POSITION REPLACED THE CRACK BRACKET WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE.2
- [SDR FDEA202309231786](https://openairdocs.org/sdr/FDEA202309231786.md): Web · cracked · Sep 23, 2023 · N662FE · Airbus A300* · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT WAS FOUND A WEB CRACK AT STGR44LH, FR20 POS REMOVED CRACK WEB AND INSTALLED NEW WEB I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, P.7B-P.23
- [SDR FDEA202309221812](https://openairdocs.org/sdr/FDEA202309221812.md): Flange · gouged · Sep 22, 2023 · N662FE · Airbus A300* · Fuselage, Door Hinge
  > LH M/L/G DOOR CENTER HINGE FWD SUPPORT FLANGE FOUND GOUGE REPLACED WITH NEW FLANGE FITTING I.A.W A300-600F SRM 51-72-10-001, PAGE.2
- [SDR FDEA202309221809](https://openairdocs.org/sdr/FDEA202309221809.md): Flange · gouged · Sep 22, 2023 · N662FE · Airbus A300* · Fuselage, Door Hinge
  > RH M/L/G DOOR CENTER HINGE AFT SUPPORT FLANGE FWD SURFACE FOUND GOUGE REPLACED WITH NEW FLANGE FITTING I.A.W A300-600F SRM 51-72-10-001, PAGE.2
- [SDR FDEA202309221726](https://openairdocs.org/sdr/FDEA202309221726.md): Support Fitting · damaged · Sep 22, 2023 · N662FE · Airbus A300* · Fuselage Miscellaneous Structure
  > RH M/W/W AFT WALL CENTER 1 EA HYD TUBE SUPPORT FITTING BROKEN. REPLACED BROKEN FITTING WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001 PAGE2
- [SDR FDEA202309221725](https://openairdocs.org/sdr/FDEA202309221725.md): Shear Web · cracked · Sep 22, 2023 · N662FE · Airbus A300* · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE SHEAR WEB CRACK NEAR FR79 PLUS 5",-Y1620. REMOVED CRACK SHEAR WEB THEN INSTALLED NEW ONE WITH FASTENERS I.A.W A300-600F SRM 51-72-10-001,PAGE 2 AND 51-40-21-001,PAGE 24-50,PARA.7
- [SDR FDEA202309221718](https://openairdocs.org/sdr/FDEA202309221718.md): Web · cracked · Sep 22, 2023 · N662FE · Airbus A300* · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE SHEAR WEB CRACK NEAR FR77 -Y1887 REPLACED THE WEB WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE.2
- [SDR FDEA202309221689](https://openairdocs.org/sdr/FDEA202309221689.md): Shear Web · cracked · Sep 22, 2023 · N662FE · Airbus A300* · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE SHEAR WEB CRACK NEAR FR79 5" Y1620. REPLACED THE NEW SHEAR WEB. ONE.I.A.W A300-600F SRM 51-72-10-001,P2.
- [SDR FDEA202309221687](https://openairdocs.org/sdr/FDEA202309221687.md): Elevator · damaged · Sep 22, 2023 · N662FE · Airbus A300* · Elevator Structure
  > 1EA WATER STRAPPED AREA (200MM X 70MM) WAS FOUND AT ER7 OF LH ELEVATOR TOP SKIN. REPAIRED THE DAMAGE AREA WITH CORE AND PLIES. THIS IS CAT A REPAIR I.A.W A300-600F SRM 55-21-12-201 PARA 5J, PAGE 268-270. FIG212(SHEET2). MAJOR REPAIR
- [SDR FDEA202309211760](https://openairdocs.org/sdr/FDEA202309211760.md): Seat Track · corroded · Sep 21, 2023 · N662FE · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR FOUND SEAT TRACK CORROSION BETWEEN FR44 PLUS 3" AND FR44 PLUS 10", Y450 REPLACED THE NEW SEAT TRACK (P/N:A5383202020400) I.A.W A300-600F SRM 51-72-10-001, PAGE.2
- [SDR FDEA202309201784](https://openairdocs.org/sdr/FDEA202309201784.md): Door · damaged · Sep 20, 2023 · N662FE · Airbus A300* · Cargo/Baggage Doors
  > BULK CARGO COMP'T DOOR EXTERNAL SURFACE GOT A PUNCH AT FR68 PLUS 2", BEAM5-0.4" POSITION ACCOMPLISHED THE DOUBLER REPAIR, THIS IS CAT.B REPAIR I.A.W A300-600F SRM 52-34-00-201, PARA.7, PAGE.217-223/224, FIG.203(SHEET-2) & SRI:52-34-00-201, IIR:52-34-00-2-0
- [SDR FDEA202309201720](https://openairdocs.org/sdr/FDEA202309201720.md): Strap · bent · Sep 20, 2023 · N662FE · Airbus A300* · Fuselage Miscellaneous Structure
  > REAR FUSELAGE INTERNAL STRUCTURE FOUND S-39R WEB PLATE DEFORM BETWEEN FR86 & FR87 AREA INSTALLED THE NEW STRAP WITH RIVETS I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21- 001, PARA6, PAGE.7B-23
- [SDR FDEA202309191829](https://openairdocs.org/sdr/FDEA202309191829.md): Fitting · cracked · Sep 19, 2023 · N662FE · Airbus A300* · Cargo/Baggage Doors
  > THE MDC DOOR ACTUATOR YOKE FWD SUPPORT FRAME WAS FOUND CRACK FABRICATED NEW SUPPORT FRAMES AND INSTALLED WITH FASTENERS,I.A.W FEDEX EA NO:T6- 5230-T0376261 P1,SEQ NO:1214,TITLE:DOORS-CARGO DOOR/HYD SYS-MAIN CARGO DOOR ACTUATOR BEARING FITTING REPLACEMENT (F
- [SDR FDEA202306141031](https://openairdocs.org/sdr/FDEA202306141031.md): Check Valve · failed · Jun 14, 2023 · N662FE · Airbus A300* · Air Conditioning System
  > ACRID FUMES & HAZE FROM A/C VENTS ON TAKEOFF. SECURED PACKS & BLEEDS & HAZE APPEARED TO CLEAR. LANDED NORMAL & SHUT DOWN ENGINES. TOWED TO GATE. INSTALLED APU PRESSURIZATION CHECK VALVE. PURGED & CLEANED ALL LINES & DUCTING AS NEEDED TO REMOVE RESIDUAL HYD
- [SDR FDEA202301270169](https://openairdocs.org/sdr/FDEA202301270169.md): Connector · chafed · Jan 27, 2023 · N662FE · Airbus A300* · Fire Detection
  > MDIS 662 26-12 4356 27JAN23 RIC OPEN U RAMP CREW REPORTS SMOKE COMING FROM AFT BELLY AREA. MX CALLED OUT AND SHUT OFF A/C POWER, FIRE DEPT NOTIFED AS PRECAUTION. REF AWM 25-52-04, RETERMINATED WIRES 2454-5004, 2454-5006,2451-6604,2451-6605, 2
- [SDR FDEA202111112830](https://openairdocs.org/sdr/FDEA202111112830.md): None · damaged · Nov 11, 2021 · N662FE · Airbus A300* · Wing Main, Frame Structure
  > RH FR47 HOLE 11 HAS THREAD DAMAGE INDICATIONS IN ALL LAYERS. REFER TO EO 6-5710- E0342809 FOR LOCATIONS COMPLIED WITH E.A. 6 - 5710 - T0353473 D P11 "WINGS - BASIC WING STRUCTURE - FR 47 RHS REPAIRED HOLES"
- [SDR FDEA202111112829](https://openairdocs.org/sdr/FDEA202111112829.md): None · damaged · Nov 11, 2021 · N662FE · Airbus A300* · Wing Main, Frame Structure
  > RH FR47 HOLE 13 HAS THREAD DAMAGE INDICATIONS IN ALL LAYERS. REFER TO EO 6-5710- E0342809 FOR LOCATIONS COMPLIED WITH E.A. 6 - 5710 - T0353473 D P11 " WINGS - BASIC WING STRUCTURE - FR 47 RHS REPAIRED HOLES"
- [SDR FDEA202111112828](https://openairdocs.org/sdr/FDEA202111112828.md): None · damaged · Nov 11, 2021 · N662FE · Airbus A300* · Wing Main, Frame Structure
  > RH FR47 HOLE 10 HAS THREAD DAMAGE INDICATIONS IN ALL LAYERS. REFER TO EO 6-5710- E0342809 FOR LOCATIONS COMPLIED WITH E.A. 6-5710-TO353473 D P11 "WINGS - BASIC WING STRUCTURE - FR47 RHS REPAIRED HOLES
- [SDR FDEA202103250764](https://openairdocs.org/sdr/FDEA202103250764.md): Spar · cracked · Mar 25, 2021 · N662FE · Airbus A300F4605R · Wing Spar
  > NDT INSPECTED - RH WING FR47 RH 11# HOLE FOUND CRACKED SINGNAL. REPAIRED THE CRACKED HOLE 11 OF RH WING FR47 REAR SPAR AND INTERNAL CORNER ANGLE PER EA 6-5710-T0353473 B P10 & SRM 51-40-44 & SRM 51-40-21. THIS IS A CAT B REPAIR. THE FURTHER INSPECTION REQ
- [SDR FDEA202103250763](https://openairdocs.org/sdr/FDEA202103250763.md): Fitting · cracked · Mar 25, 2021 · N662FE · Airbus A300F4605R · Wing, Attach Fittings
  > NDT INSP - RH WING FR47 171# HOLE FOUND CRACKED SINGNAL. REPAIRED THE CRACKED HOLE 171 OF RH WING FR47 AFT FITTING PER EA 6-5710-T0353473 B P10 & SRM 51-40-44 & SRM 51-40-21. THIS IS A CAT B REPAIR. THE FURTHER INSPECTION REQUIREMENT PER EA 6-5710-T0353473
- [SDR FDEA202103140640](https://openairdocs.org/sdr/FDEA202103140640.md): Skin · delaminated · Mar 14, 2021 · N662FE · Airbus A300F4605R · Spoilers
  > RH 5# SPOILER LOWER HINGE ARM AND TOP SKIN FOUND DELAMINATED. PERFORMED THE REPAIR ON RH 5# SPOILER LOWER HINGE ARM AND TOP SKIN PER FEDEX EA # 6-5750-T0360394 P1, TITLE: WING - FLIGHT SURFACE - RH 5# SPOILER CENTER HINGE ARMS LOWER AND OUTSIDE SURFACES
- [SDR FDEA202011112813](https://openairdocs.org/sdr/FDEA202011112813.md): Adc · failed · Nov 11, 2020 · N662FE · Airbus A300F4605R · Altimeter, Barometric/Encoder
  > DURING DEPARTURE NAV ADC IAS DISCREPANCY ON CAPT'S SIDE MASTER WARNING FOR OVERSPEED DISCREPANCY. SELECTED "SYS" 2 ON ADC SWITCHING PANEL FOR F/O'S AIRSPEED INFO ON CAPT'S SIDE. MULTIPLE EXTRA ADC ISSUES ON ECAM REPORTED TO MAINTENANCE AFTER LANDING. REMOVE
- [SDR FDEA2019122643300](https://openairdocs.org/sdr/FDEA2019122643300.md): Indicator · inoperative · Dec 24, 2019 · N662FE · Airbus A300F4605R · Emergency Equipment
  > DOOR R1 SLIDE WILL NOT INDICATE ARMED. ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR INOPERATIVE. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE.. ARMED DOOR AFTER ARRIVAL, DOOR OPERATED AND ARMED PROPERLY IAW AM
- [SDR FDEA201905171094](https://openairdocs.org/sdr/FDEA201905171094.md): Limiter · tripped · May 17, 2019 · N662FE · Airbus A300F4605R · Leading Edge Slat Control System
  > PDIS 662 27-80 0819 17MAY19 MEM FACT U LOGPAGES:2913364 ON APPROACH INTO KMEM RECEIVED SLATS SYSTEM 1&2 FAULT. RECYCLED SLATS PER PHASE 1S, NO HELP. COMPLIED WITH ECAM AND QRH PROCEDURES. FLAPS WORKED NORMALLY. LANDED 0/40 SLATS WERE 0 UNEVENTFUL LA
- [SDR FDEA2019042290868](https://openairdocs.org/sdr/FDEA2019042290868.md): Smoke Detector · failed · Apr 19, 2019 · N662FE · Airbus A300F4605R · Smoke Detection
  > AFTER TAKEOFF AT APPROX. 1500 AGL. GOT AN AVIONICS SMOKE LIGHT, IT STAYED ON UNTIL 50FT FROM THE GATE TAXIING IN WE ADHERED TO THE QRH & THE ECAM, NEVER HAD ANY SMOKE INDICATONS FIRE CHIEF CONFIRMED NO SMOKE. ALSO AFTER BLOCKIN, THE AVIONICS SMOKE LIGHT
- [SDR FDEA2019042290866](https://openairdocs.org/sdr/FDEA2019042290866.md): Smoke Detector · false activation · Apr 19, 2019 · N662FE · Airbus A300F4605R · Smoke Detection
  > AFTER TAKEOFF AT APPROX. 1500 AGL. GOT AN AVIONICS SMOKE LIGHT, IT STAYED ON UNTIL 50FT FROM THE GATE TAXIING IN ADHERED TO THE QRH & THE ECAM, NEVER HAD ANY SMOKE INDICATONS FIRE CHIEF CONFIRMED NO SMOKE. ALSO AFTER BLOCKIN, THE AVIONICS SMOKE LIGHT A

Next page: https://openairdocs.org/aircraft/N662FE/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 = 'N662FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N662FE/reports

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