# Service difficulty reports: N663FE

A list on [N663FE](https://openairdocs.org/aircraft/N663FE.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 6 · 264 reports

- [SDR FDEA202604090418](https://openairdocs.org/sdr/FDEA202604090418.md): Handle · faulted · Apr 9, 2026 · N663FE · Airbus A300F4605R · Landing Gear Retraction/Extension System
  > MLG RETRACT INOP, RAISING MLG LEVER AFTER TAKE-OFF. EMERGENCY DECLARED. AFTER BRIEF W/ CREW MLG RETRACT INOP IN SYS 1, CREW DID NOT ATTEMPT TO RETRACT IN SYS 2 DUE TO A MLG WARNING MESSAGE IN SYS 1. ALL DOORS SHOWED UNLOCKED WHEN MLG HANDLE MOVED UP & MLG
- [SDR FDEA202604020396](https://openairdocs.org/sdr/FDEA202604020396.md): Seat Track · damaged · Apr 2, 2026 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > RAMP REPORTED BROKEN LOCK ON MAIN DECK POS 12R. LOCK PN [MT1584]. B/R LOCK REMOVED AND STOWED IN FLIGHT DECK CLOSET. PLND: DATE: 27MAR26 ENT BY: 779762 ON: 27MAR26 17:39 Z AT: IND-HVMX PLNTXT27MAR26 12:39 SEAT TRACK DAMAGE MEL 27MAR26 09:07 IND R
- [SDR FDEA202602140197](https://openairdocs.org/sdr/FDEA202602140197.md): Safety Wire · wrong part · Feb 14, 2026 · N663FE · Airbus A300F4605R · Escape Slide
  > PACKBOARD RELEASE CABLE SAFETY WIRE REQUIRES REPLACEMENT PER FEA 6-2560-F0386375 A P1 L1 DOOR FEA: 6-2560-F0386375 A P1 CMM: 25-60-40 SAFTIED L1 DOOR SLIDE PACKBOARD RELEASE CABLE WITH.015 STAINLESS WIRE.
- [SDR FDEA202407211044](https://openairdocs.org/sdr/FDEA202407211044.md): Skin · gouged · Jul 21, 2024 · N663FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > FOUND GOUGE AT TAIL CONE LOWER SURFACE FR92 PLUS 5.6", S-17R PLUS 3" CUT OUT THE DAMAGE AREA, FABRICATED THE REPAIR DOUBLER WET INSTALLED REPAIR DOUBLER WITH BLIND RIVETS AT TAIL CONE LOWER SURFACE FR92~93, S-17R~18R I.A.W A300- 600F SRM 53-19-12-201, PARA.
- [SDR FDEA202407161033](https://openairdocs.org/sdr/FDEA202407161033.md): Fitting · cracked · Jul 16, 2024 · N663FE · Airbus A300F4605R · Cargo/Baggage Doors
  > PERFORM BEARING FITTING REPLACEMENT AT MAIN DECK CARGO DOOR FR23, LONGN1~3 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR23 LONGN1~LONGN3 I.A.W FEDEX EA NO: T6-5230-T0379479 A P1, SEQ NO:775, TITLE: DOORS-CARGO DOOR/HYD SYS-MAIN
- [SDR FDEA202407111003](https://openairdocs.org/sdr/FDEA202407111003.md): Skin · none · Jul 11, 2024 · N663FE · Airbus A300F4605R · Trailing Edge Flaps
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPPER SKIN BETWEEN RIB16~17, S2.1~S2.2 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIR
- [SDR FDEA202407061002](https://openairdocs.org/sdr/FDEA202407061002.md): Angle · chafed · Jul 6, 2024 · N663FE · Airbus A300F4605R · Fuselage Structure (General)
  > QA SURVEILLANCE ITEM AFT CGO COMP'T RH SIDE PROFILE CORNER GOT SCRATCH AT FR58- FR59A POSITION. REPLACED THE SCRATCHED CORNER PROFILE WITH A NEW ONE. I.A.W A300-600F SRM 51-72-10-001 PAGE 2. AT AFT CARGO COMPARTMENT RH SIDE, FR58~FR59A POSITION. REPAIR IS
- [SDR FDEA202407050995](https://openairdocs.org/sdr/FDEA202407050995.md): Seat Track · worn · Jul 5, 2024 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SEAT TRACK WORN AT FR41~FR41 PLUS 3",Y0 POSITION DAMADED SEAT TRACK REPLACED WITH NEW PART, INSTALLED WITH FASTENERS. I.A.W A300- 600F SRM 51-72-10-001, PAGE 2 AND 51-40-21-001, PARA 7, PAGE 24-50. REPAIR CLASSIFI
- [SDR FDEA202406190986](https://openairdocs.org/sdr/FDEA202406190986.md): Elevator · none · Jun 19, 2024 · N663FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR UPPER SKIN AT ER7 PLUS 10", FRONT SPAR-18.3" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKIN
- [SDR FDEA202406190985](https://openairdocs.org/sdr/FDEA202406190985.md): Support Web · deformed · Jun 19, 2024 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AFT FUSELAGE FOUND 2EA SUPPORT WEB GOT DEFORM AT FR86 S35R AND S38R REPLACED THE NEW SUPPORT WEBS WITH RIVETS. I.A.W A300-600F SRM 51-72-10-001 PAGE.2 AND 51-40-21-001 PARA.6, PAGE.7B~23, THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, AT AFT FUSELAGE FR86
- [SDR FDEA202406190919](https://openairdocs.org/sdr/FDEA202406190919.md): Skin · damaged · Jun 19, 2024 · N663FE · Airbus A300F4605R · Elevator, Plate/Skin
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR UPPER SKIN AT ER7 10", FRONT SPAR-18.3" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQ
- [SDR FDEA202406171040](https://openairdocs.org/sdr/FDEA202406171040.md): Crossbeam · corroded · Jun 17, 2024 · N663FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSS BEAM SURFACE WAS FOUND CORROSION AT FR54.2,-Y70~-Y140 I.A.W A300-600 AMM:20-21-12-00 REPLACED MAIN DECK CARGO COMPATEMENT FLOOR STRUCTURE CROSS BEAM AT FR54.2-Y70-Y140, REPAIR IS CLASSIFIED AS MAJOR PER GMM
- [SDR FDEA202406170994](https://openairdocs.org/sdr/FDEA202406170994.md): Seat Track · corroded · Jun 17, 2024 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SEAT TRACK WAS FOUND CORROSION AT FR53 PLUS 14"~FR54, Y453 ACCOMPLISHED THE SPLICE REPAIR AT MAIN CARGO SEAT TRACK AT Y450 BETWEEN FR52 AND FR53 I.A.W FEDEX EA NO:T6-5310-T0379554 P1, SEQ NO:000771, TITLE:FUSEL
- [SDR FDEA202406170964](https://openairdocs.org/sdr/FDEA202406170964.md): Cargo Track · worn · Jun 17, 2024 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SEAT TRACK WORN AT FR54 PLUS 8"~FR54 PLUS 11", -Y953 INSTALLED THE NEW DUMMY SEAT TRACK AT MAIN DECK FR 54~54.2, -Y953 I.A.W A300-600F SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.7, PAGE.24-50. THE REPAIR CLASS
- [SDR FDEA202406161028](https://openairdocs.org/sdr/FDEA202406161028.md): Rib · cracked · Jun 16, 2024 · N663FE · Airbus A300F4605R · Leading Edge Devices
  > RH WING SLAT 1 SKELETON RIB 24, 1EA WEB LOWER EDGE CRACK AT FOLDING NOSE O/B SIDE ACCOMPLISHED THE ANGLE REPAIR AT RH WING SLAT #1 RIB24 I.A.W FEDEX EA NO:T6-5750- T0379841 P1, SEQ NO:000778, TITLE:WINGS-FLIGHT SURFACES- RH #1 SLAT-RIB24 LEADING EDGE WEB PL
- [SDR FDEA202406150997](https://openairdocs.org/sdr/FDEA202406150997.md): Seat Track · corroded · Jun 15, 2024 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SEAT TRACK WAS FOUND CORROSION AT FR18 PLUS 10"~FR18 PLUS 15",Y953 REPLACED THE CORRODED SEAT TRACK WITH NEW PART AT FR15A~ FR19, Y953 I.A.W A300-600F SRM 51-72-10-001, PAGE 2 AND 51-40-21-001, PARA 6, PAGE 7B~PA
- [SDR FDEA202406150981](https://openairdocs.org/sdr/FDEA202406150981.md): Rib · cracked · Jun 15, 2024 · N663FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1. 1EA CRACK (15MM) WAS FOUND AT R/H WING CENTER FLAP RIB25 AFT AREA OF TOP SURFACE RIB FLANGE. 2. 2EA CRACKS (5MM & 20MM) WERE FOUND AT R/H WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. 3. 1EA CRACK (50MM) WAS FOUND AT R/H WING CENTER FLAP
- [SDR FDEA202406140998](https://openairdocs.org/sdr/FDEA202406140998.md): Floorbeam · cracked · Jun 14, 2024 · N663FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SUPPORT WAS FOUND CRACK AT FR38 PLUS 4",-Y2462 POSITION CRACKED SUPPORT REPLACED NEW PART. INSTALLED WITH FASTENERS I.A.W A300-600F SRM 51- 72-10-001, PAGE.2 AND SRM 51-40-21-001, PARA.7, PAGE.24- PAGE.50. THE REP
- [SDR FDEA202406140996](https://openairdocs.org/sdr/FDEA202406140996.md): Floorbeam · cracked · Jun 14, 2024 · N663FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SUPPORT WAS FOUND CRACK AT FR38 PLUS 4",-Y2462 POSITION CRACKED SUPPORT REPLACED NEW PART. INSTALLED WITH FASTENERS I.A.W A300-600F SRM 51- 72-10-001, PAGE.2 AND SRM 51-40-21-001, PARA.7, PAGE.24- PAGE.50. THE RE
- [SDR FDEA202406140982](https://openairdocs.org/sdr/FDEA202406140982.md): Rib · cracked · Jun 14, 2024 · N663FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1.1EA CRACK (5MM) WAS FOUND AT L/H WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE. 2.1EA CRACK (5MM) WAS FOUND AT L/H WING CENTER FLAP RIB12 AFT AREA OF TOP SURFACE RIB FLANGE. 3.1EA CRACK (25MM) WAS FOUND AT L/H WING CENTER FLAP RIB19 AFT ARE
- [SDR FDEA202406131019](https://openairdocs.org/sdr/FDEA202406131019.md): Seat Track · none · Jun 13, 2024 · N663FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING SLPIECE REPAIR FOUND ON MDCC SEAT TRACK BTW FR58 ~ 61, Y953 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 1
- [SDR FDEA202406131018](https://openairdocs.org/sdr/FDEA202406131018.md): Seat Track · bent · Jun 13, 2024 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING SLPIECE REPAIR FOUND ON MDCC SEAT TRACK BTW FR58 ~ 61, Y953 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 1
- [SDR FDEA202406071031](https://openairdocs.org/sdr/FDEA202406071031.md): Fitting · cracked · Jun 7, 2024 · N663FE · Airbus A300F4605R · Cargo/Baggage Doors
  > THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING WAS FOUND CRACK AT FR24 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR24 LONGN1~LONGN3 I.A.W FEDEX EA NO:T6-5230-T0379479 A P1, SEQ NO:775, TITLE:DOORS-CARGO DOOR/HYD SYS-MAIN CA
- [SDR FDEA202404190474](https://openairdocs.org/sdr/FDEA202404190474.md): Pbe · failed · Apr 19, 2024 · N663FE · Airbus A300F4605R · Emergency Equipment
  > DURING SERVICE CHECK FOUND PBE IN COURIER AREA DUE DATE OF 04/24. INSTALLED ONLY NEW PBE IN COURIER AREA PER AMM 35-31-01-02.
- [SDR FDEA202303160447](https://openairdocs.org/sdr/FDEA202303160447.md): Unknown · unknown · Mar 16, 2023 · N663FE · Airbus A300* · Electrical Power System
  > MDIS 663 24-40 5174 14MAR23 LAX OPEN U AIRCARFT EXTERNAL POWER RECEPTACLE ARCED AT PLUG AND EXTERNAL POWER CONNECTION. SHGN 14MAR23 16:21 LAX U AMM: 24-41-15-04 REF AMM 24-41-15-04 BEGAN EXTERNAL POWER RECEPTACLE REMOVAL BY COMPLETING
- [SDR FDEA202201300161](https://openairdocs.org/sdr/FDEA202201300161.md): Dummy Rail · worn · Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, Structure
  > FR54/FR54.2 LH NO.3 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W SRM 53-15-16-201 PARA 5A PAGE 201-216 FIG.201 PFM REPAIR ACCOMPLISHED.
- [SDR FDEA202201300160](https://openairdocs.org/sdr/FDEA202201300160.md): Dummy Rail · worn · Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, Structure
  > FR54/FR54.2 LH NO.2 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W SRM 53-15-16-201 PARA 5A PAGE 201-216 FIG.201 PFM REPAIR ACCOMPLISHED.
- [SDR FDEA202201300159](https://openairdocs.org/sdr/FDEA202201300159.md): Dummy Rail · worn · Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, Structure
  > FR54/FR54.2 CENTER NO.1 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W SRM 53-15-16-201 PARA 5A PAGE 201-216 FIG.201 PFM REPAIR ACCOMPLISHED.
- [SDR FDEA202201300158](https://openairdocs.org/sdr/FDEA202201300158.md): Dummy Rail · worn · Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, Structure
  > FR54/FR54.2 RH NO.3 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W SRM 53-15-16-201 PARA 5A PAGE 201-216 FIG.201 PFM REPAIR ACCOMPLISHED.
- [SDR FDEA202201300157](https://openairdocs.org/sdr/FDEA202201300157.md): Dummy Rail · worn · Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, Structure
  > FR54/FR54.2 RH NO.2 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W SRM 53-15-16-201 PARA 5A PAGE 201-216 FIG.201 PFM REPAIR ACCOMPLISHED.
- [SDR FDEA202201300156](https://openairdocs.org/sdr/FDEA202201300156.md): Dummy Rail · worn · Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, Structure
  > FR38.2/FR40 LH NO.4 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PFM REPAIR ACCOMPLISHED.
- [SDR FDEA202201300155](https://openairdocs.org/sdr/FDEA202201300155.md): Dummy Rail · worn · Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, Structure
  > FR38.2/FR40 RH NO.5 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PFM REPAIR ACCOMPLISHED.
- [SDR FDEA202201300154](https://openairdocs.org/sdr/FDEA202201300154.md): Dummy Rail · worn · Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, Structure
  > FR38.2/FR40 RH NO.4 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PFM REPAIR ACCOMPLISHED.
- [SDR FDEA202201260230](https://openairdocs.org/sdr/FDEA202201260230.md): Floor Support · corroded · Jan 26, 2022 · N663FE · Airbus A300* · Fuselage Main, Structure
  > MAIN DECK LONGITUDIAL FLOOR STRUCTURE UPR SURFACE WAS FOUND CORROSION AT FR11 ~ FR13A, Y730MM ACCOMPLISHED THE SUPPORT REPLACED I.A.W A300-600F SRM 51-72-10-001 P2
- [SDR FDEA202201230285](https://openairdocs.org/sdr/FDEA202201230285.md): Crossbeam · corroded · Jan 23, 2022 · N663FE · Airbus A300* · Fuselage Floor Panel
  > MDCC FLOOR STRUCTURE CROSSBEAM UPR SURFACE WAS FOUND CORROSION AT FR46,FROM - Y330MM TO -Y370MM REPLACED THE CORROSION CROSSBEAM WITH FABRICATED NEW PART I.A.W AIRBUS DRAWNING NUMBER: A53812936 SHEET.A & A300-600F SRM 51-72-10-001, PAGE2 & 53-15-15-001-2
- [SDR FDEA202201220242](https://openairdocs.org/sdr/FDEA202201220242.md): Floor Support · corroded · Jan 22, 2022 · N663FE · Airbus A300* · Fuselage Main, Structure
  > MAIN DECK LONGITUDIAL FLOOR STRUCTURE UPR SURFACE WAS FOUND CORROSION AT FR12A ~ FR13A, Y1450MM REPAIRED THE DAMAGE AREA WITH TEE SPLICE REPAIR I.A.W. A300-600F SRM 53-12-15-201-2 PARA.5.G P.239-244 FIG.207
- [SDR FDEA202201170275](https://openairdocs.org/sdr/FDEA202201170275.md): Shear Web · cracked · Jan 17, 2022 · N663FE · Airbus A300* · Fuselage Main, Structure
  > N00253 MAIN DECK FLOOR STRUCTURE'S SHEAR WEB CRACKED AT FR79 160MM,-Y1630MM POS. REPLACED THE WEB WITH NEW PART I.A.W A300-600F SRM 51-72-10-001 P.2.
- [SDR FDEA202108071994](https://openairdocs.org/sdr/FDEA202108071994.md): Seat Track · broken · Aug 7, 2021 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT -Y953 AND FR 27 HAS BROKEN LIP. REMOVED AND REPLACED SEAT TRACK -Y953 FR27- FR29 IAW SRM 53-10-16 FIG 201 PARAGRAPH 4. CATEGORY "A" MAJOR REPAIR
- [SDR FDEA202108071993](https://openairdocs.org/sdr/FDEA202108071993.md): Seat Track · sheared · Aug 7, 2021 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT Y0 AND FR 27 HAS BROKEN LIP. EVALUATED DAMAGED SEAT TRACK Y 0 FR 27, FOUND OUT OF LIMITS, IAW SRM 53-10-16, REPAIRED SEAT TRACK IAW SRM 53-10-160 FIGURE 201, FR 26.5 TO FR 27.5. CATEGORY "A" MAJOR REPAIR
- [SDR FDEA202108071992](https://openairdocs.org/sdr/FDEA202108071992.md): Seat Track · sheared · Aug 7, 2021 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT Y450 AND FR 27 HAS BROKEN LIP. EVALUATED DAMAGED SEAT TRACK Y450, FOUND OUT OF LIMITS IAW SRM 53-10-16, REPAIRED SECTION SEAT TRACK Y450 FROM FR 26.5 TO FR 29.5 IAW SRM 53-10-16 FIGURE 201 CATEGORY "A" MAJOR REPAIR
- [SDR FDEA202106201574](https://openairdocs.org/sdr/FDEA202106201574.md): Seat Track · damaged · Jun 20, 2021 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK, ARTICULATING SEAT TRACK IS DAMAGED @ CENTERLINE GUIDE. REPLACED ARTICULATING SEAT TRACK SECTION IAW AIRBUS DWG A53813187000
- [SDR FDEA202103150653](https://openairdocs.org/sdr/FDEA202103150653.md): Cylinder · low pressure · Mar 15, 2021 · N663FE · Airbus A300F4605R · Emergency Equipment
  > AFTER L1 DOOR SLIDE INSTALLATION FOUND L1 DOOR EMERG OP CYL PRESS LOW. SHEAR PIN IN BAD & NIS PDX. ORDERING PART. IDENTIFIED PARTS SHEAR MPN: FE127-100-04 CPN: 5210791 QTY: 1 PART 15MAR21 06:48 PDX U ORDER PART MPN: FE127-100-04 CPN: 5210791 QTY
- [SDR FDEA202103150654](https://openairdocs.org/sdr/FDEA202103150654.md): Bottle · low pressure · Mar 15, 2021 · N663FE · Airbus A300F4605R · Escape Slide
  > UPON SERVICE CHECK FOUND R1 DOOR SLIDE IN RED BAND. RELEASED FOR SERVICE PER MEL: 52-11-01-01. CREW ENTRY DOOR ESCAPE SLIDE R1 INOP. SLIDE REMAINS INSTALLED ON DOOR. PRESSURE NEEDLE IS ALIGNED WITH THE 'MOVABLE GREEN CURSOR'.
- [SDR FDEA202007301718](https://openairdocs.org/sdr/FDEA202007301718.md): Coupling · failed · Jul 30, 2020 · N663FE · Airbus A300F4605R · Pneumatic Distribution System
  > DURING DEPARTURE, ECAM FOR HIGH NAC 250 DEG C, TROUBLSHOT NR 2 ENG IAW QRH. NO CHANGE WITH THROTTLE MOVE OR BLEED VALVE OFF. REACHED TOP OF CLIMB FL290 & TEMP DID NOT REDUCE, LOWEST 215, ONCE THROTTLE FWD 240 DEG AT 290. RETURNED TO DEPART, NR 2 MOTORED, RU
- [SDR FDEA201909112202](https://openairdocs.org/sdr/FDEA201909112202.md): Switch · failed · Sep 11, 2019 · N663FE · Airbus A300F4605R · Landing Gear Position and Warning
  > PDIS 663 32-20 1528 11SEP19 MEM OPEN U LOGPAGES:2636365 AFTER GEAR RETRACTION THE NG DOOR LIGHT REMAINED ILLUMINATED. VIBRATION INDICATED THAT THE DOOR WAS OPEN. PER GOC RETURNED TO BASE AFTER RUNNING QRH SHGN 11SEP19 11:28 MEM U DEBRIEFED C
- [SDR FDEA2019080761800](https://openairdocs.org/sdr/FDEA2019080761800.md): Floorbeam · cracked · Aug 6, 2019 · N663FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MDCC - FR16 -Y1456, FLOOR SUPPORT CRACKED APPROX 1.5 INCH IN LENGTH REPAIRED THE MAIN DECK CRACKED FLOOR SUPPORT AT FR16 -Y1456 PER SRM 53-12-15 FIG 207. THE REPAIR WAS CATEGORY B AND WAS CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201907291734](https://openairdocs.org/sdr/FDEA201907291734.md): None · none · Jul 29, 2019 · N663FE · Airbus A300* · Fuselage Main, Structure
  > EXISTING REPAIR ON MDCC FR29 Y-750 CROSSBEAM REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC FR29 Y-750 CROSSBEAM WAS EVALUATED AND FOUND NO REPAIR DOCUMENT AND NOT CONFORM ANY REPAIR SCHENE IN CURRENT SRM, REPAIRED IT AGAIN PER A300-600F SRM
- [SDR FDEA201907261706](https://openairdocs.org/sdr/FDEA201907261706.md): Door Frame · none · Jul 26, 2019 · N663FE · Airbus A300* · Fuselage Main, Structure
  > EXISTING REPAIR ON FWD CARGO DOOR FWD CUTOUT FR20A BTW S-37R AND S-41R REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FWD CARGO DOOR FWD CUTOUT FR20A BTW S-37R AND S-41R WAS EVALUATED AND FOUND IN CONFORMITY WITH FEDEX DRAWING SR30-53-001 REV.D,FE
- [SDR FDEA201907241675](https://openairdocs.org/sdr/FDEA201907241675.md): Beam · damaged · Jul 24, 2019 · N663FE · Airbus A300* · Fuselage Main, Structure
  > EXISTING REPAIR ON MDCC FR30 Y-750 CROSSBEAM REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC FR30 Y-750 CROSSBEAM WAS EVALUATED AND FOUND NO REPAIR DOCUMENT AND NOT CONFORM ANY REPAIR SCHENE IN CURRENT SRM, REPAIRED IT AGAIN PER FEDEX EA #: 6-
- [SDR FDEA201907241673](https://openairdocs.org/sdr/FDEA201907241673.md): Beam · unknown · Jul 24, 2019 · N663FE · Airbus A300* · Fuselage Main, Structure
  > EXISTING REPAIR ON MDCC FR60 Y-2462 CROSSBEAM REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC FR60 Y-2462 CROSSBEAM WAS EVALUATED AND FOUND IN CONFORMITY WITH FEDEX EA #: 6-2550-53566A, TITLE: FUSELAGE-MAINFRAME-MIAN DECK CARGO COMPARTMENT FL

Next page: https://openairdocs.org/aircraft/N663FE/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 = 'N663FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N663FE/reports

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