# Service difficulty reports: N689FE

A list on [N689FE](https://openairdocs.org/aircraft/N689FE.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 2 · 96 reports

- [SDR FDEA202608181142](https://openairdocs.org/sdr/FDEA202608181142.md): Processor · faulted · Aug 18, 2026 · N689FE · Airbus A300F4605R · Landing Gear Retraction/Extension System
  > TAKEOFF AT IND, MLG WOULD NOT RETRACT. C-W QRH. RETURNED. EMERG DECLARED. AMM 32-31-00-05, NLG RETRACT FULLY, GREEN ON BOTH MLG INDS, BOTH LT & RT MLG STAYED GREEN DOWN ON INDS. PERFORMED MLG EXTEND & RETRACT AT GATE & VERIFIED ALL MLG DOORS EXTEND & RE
- [SDR FDEA202507081309](https://openairdocs.org/sdr/FDEA202507081309.md): Skin · dented · Jul 8, 2025 · N689FE · Airbus A300F4605R · Cargo/Baggage Doors
  > FABRICATE NEW LOWER INNER SKIN PER EA NO:T6-5230-T0382227 AT MDCD FR21~26,LONGN 8 ~ STGR 30L FABRICATED AND INSTALLED NEW LOWER INNER SKIN AT MDCD FR21-26, LONGN 8 - STGR30L POSITION. I.A.W FEDEX EA: T6-5230-T0382227AP2, SEQ NO:966 TITLE:DOORS - MAIN CARG
- [SDR FDEA202507081308](https://openairdocs.org/sdr/FDEA202507081308.md): Fork · damaged · Jul 8, 2025 · N689FE · Airbus A300F4605R · Cargo/Baggage Doors
  > FABRICATE NEW REAR FORK FRAME 21 PER EA NO:T6-5230-T0382227 AT MDCD FR21,LONGN 6~STGR 30L FABRICATED AND INSTALLED NEW REAR FORK FRAME 21 AT MDCD FR21, LONGN 6 - STGR30L POSITION. I.A.W FEDEX EA: T6-5230-T0382227AP2, SEQ NO:966 TITLE:DOORS - MAIN CARGO DO
- [SDR FDEA202507081306](https://openairdocs.org/sdr/FDEA202507081306.md): Skin · dented · Jul 8, 2025 · N689FE · Airbus A300F4605R · Cargo/Baggage Doors
  > PER EA NO:T6-5230-T0382227 PERFORM SPLICE REPAIR ON MDCD INNER SKIN AT FR21,LONGN 4~5 FABRICATED AND INSTALLED NEW REPAIR SPLICE AND CONNECTING CLIP AT MDCD FR21, LONGN 4 - 5 POSITION. I.A.W FEDEX EA: T6-5230-T0382227AP2, SEQ NO:966 MAIN CARGO DOOR - REP
- [SDR FDEA202506301307](https://openairdocs.org/sdr/FDEA202506301307.md): Skin · dented · Jun 30, 2025 · N689FE · Airbus A300F4605R · Cargo/Baggage Doors
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING REPAIR SPLICE FOUND ON MAIN CARGO DOOR INNER SKIN BTW FR20~21, BEAM 3~4 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMEN
- [SDR FDEA202506261053](https://openairdocs.org/sdr/FDEA202506261053.md): Floor Support · cracked · Jun 26, 2025 · N689FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > M/D FLOOR SUPPORT FOUND CRACK AT FR37~FR38, -Y2462. REMOVED CRACK SUPPORT AT M/D FLOOR FR37~38,-Y2462,THEN INSTALLED NEW ONE WITH FASTENERS I.A.W A300-600F SRM 51-72-10-001,PAGE 2 & 51-40-21-001,PARA.7,PAGE 24~25,THE REPAIR IS CLASSIFIED AS MINOR PER GMM
- [SDR FDEA202506191079](https://openairdocs.org/sdr/FDEA202506191079.md): Skin · gouged · Jun 19, 2025 · N689FE · Airbus A300F4605R · Spoilers
  > A GOUGE WAS FOUND ON OUTBD EDGE LOWER SIDE OF L2 SPLR. ACCOMPLISHED DOUBLER REPAIR WITH FASTENERS AT OUTBD EDGE OF L2 SPLR RIB 18 POSITION I.A.W FEDEX EA NO:T6-5750-T0383884P1, SEQ NO: XXX, TITLE: WING - FLIGHT SURFACES - LH #2 SPOILER - WEAR DAMAGE AT OU
- [SDR FDEA202506141122](https://openairdocs.org/sdr/FDEA202506141122.md): Skin · dented · Jun 14, 2025 · N689FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING OUTER FLAP D-NOSE SKIN GOT DENT BETWEEN RIB15~17,S-1.1~1.2 ACCOMPLISHED THE NOSE SKIN FLUSH REPAIR AT RH WING OUTER FLAP RIB15~17, S-1.1~1.2 I.A.W A300-600F SRM 57-50-00-201, PARA.4H, PAGE.231~236, FIG.208 & SRI:57-50-00-201, IIR:57-50- 00-2-002-00
- [SDR FDEA202506131016](https://openairdocs.org/sdr/FDEA202506131016.md): Seat Track · corroded · Jun 13, 2025 · N689FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > M/D SEAT TRACK FOUND CORROSION AT FR80-4", Y0 POS. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK AT FR80~FR78 PLUS 13" Y0 IAW A300-600F SRM 53-10-16-201 PARA.4 FIG201, PAGE203~208. THIS REPAIR CLASSIFIED AS MAJOR CAT A PER GMM6-2-
- [SDR FDEA202506131017](https://openairdocs.org/sdr/FDEA202506131017.md): Seat Track · corroded · Jun 13, 2025 · N689FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > M/D SEAT TRACK FOUND CORROSION AT FR80-5", Y1221.2 POS. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK AT FR80~FR78 PLUS 13" Y1221.2 IAW A300-600F SRM 53-10-16-201 PARA.4 FIG201, PAGE203~208. THIS REPAIR CLASSIFIED AS MAJOR CAT A P
- [SDR FDEA202506121064](https://openairdocs.org/sdr/FDEA202506121064.md): Seat Track · cracked · Jun 12, 2025 · N689FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > M/D FLOOR SUPPORT FOUND CRACK AT FR38.1~FR38.2, -Y2462 POS REMOVED CRACK SUPPORT AT M/D FLOOR FR38.1~38.2,-Y2462,THEN INSTALLED NEW ONE WITH FASTENERS I.A.W A300-600F SRM 51-72-10-001,PAGE 2 & 51-40-21-001,PARA.7,PAGE 24~25,THE REPAIR IS CLASSIFIED AS MIN
- [SDR FDEA202506121052](https://openairdocs.org/sdr/FDEA202506121052.md): Strut · cracked · Jun 12, 2025 · N689FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > M/D FLOOR SUPPORT FOUND CRACK AT FR38.1~FR38.2, Y2462 POS. REPLACED THE CRACK STRUT WITH NEW PART ON M/D FLOOR SUPPORT AT FR38.1 ~FR38.2 Y2462 I.A.W A300-600F SRM 51-72-10-001,PAGE2 AND 51-40-21-001 PARA 7 PAGE24 - PAGE50. THIS REPAIR IS CLASSIFIED AS MINO
- [SDR FDEA202506111081](https://openairdocs.org/sdr/FDEA202506111081.md): Fitting · not reported · Jun 11, 2025 · N689FE · Airbus A300F4605R · Cargo/Baggage Doors
  > REPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER EO NO:E6- 5230-E0378588 B P5 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR23, LONGN1- LONGN3 I.A.W FEDEX EO NO:E6-5230-E0378588 B P5, SEQ NO:949, TITLE: DOORS
- [SDR FDEA202506111005](https://openairdocs.org/sdr/FDEA202506111005.md): Shear Web · cracked · Jun 11, 2025 · N689FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > M/D FLOOR STRUCTURE FOUND A SHEAR WEB CRACK AT FR77-1', S-26R. REPLACED THE CRACK SHEAR WEB WITH NEW PART ON M/D FLOOR STRUCTURE AT FR77-1", S- 26R I.A.W A300-600F SRM 51-72-10-001, PAGE 2 AND 51-40-21-001, PARA 7, PAGE 24~ PAGE 50.THIS REPAIR IS CLASSIFIED
- [SDR FDEA202506091078](https://openairdocs.org/sdr/FDEA202506091078.md): Support · cracked · Jun 9, 2025 · N689FE · Airbus A300F4605R · Wing Miscellaneous Structure
  > LH WING TE CAVITY LOWER FACE OF UPPER FIXED PNL FOUND SUPPORT WEB CRACK NEAR L5 SPLR INBD. TRIMMED OUT AND INSTALLED REPAIR BRACKET REPAIR AT LH WING SKIN SUPPORT ABX144.2 I.A.W FEDEX EA NO: T6-5740-T0383807 P1, SEQ NO: 1013, TITLE: WING-ATTACH FITTINGS
- [SDR FDEA202506031080](https://openairdocs.org/sdr/FDEA202506031080.md): Fitting · cracked · Jun 3, 2025 · N689FE · Airbus A300F4605R · Cargo/Baggage Doors
  > THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING WAS FOUND CRACK AT FRAME 24 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR24, LONGN1- LONGN3 I.A.W FEDEX EO NO:E6-5230-E0378588 B P5, SEQ NO:949, TITLE: DOORS-CARGO DOOR/HYD SYS
- [SDR FDEA202410061431](https://openairdocs.org/sdr/FDEA202410061431.md): Support Fitting · corroded · Oct 6, 2024 · N689FE · Airbus A300F4605R · Wing Main, Frame Structure
  > RH MLG FWD LUG RIB 5 CORROSION IN BORE. REMOVED CORROSION FROM RH MLG FWD LUG RIB 5 PER AIRBUS R57240425 AND EA # 6-5710-T0380814 P1.
- [SDR FDEA202409271380](https://openairdocs.org/sdr/FDEA202409271380.md): Support Fitting · corroded · Sep 27, 2024 · N689FE · Airbus A300F4605R · Wing Main, Frame Structure
  > BUSH E HAS DAMAGE TO CHROME FACE. REMOVED AND REPLACED BUSHING D AND E PER AIRBUS R57240425.
- [SDR FDEA202408271176](https://openairdocs.org/sdr/FDEA202408271176.md): Proximity Sensor · failed · Aug 27, 2024 · N689FE · Airbus A300F4605R · Landing Gear Position and Warning
  > ON DEPARTURE LG WOULD NOT RETRACT ON SYS 2, SWITCHED TO SYS 1 & GEAR WOULD STILL NOT RETRACT. ALL GEAR REMAINED GREEN & DOORS SHOWED UNLOCK UNTIL HANDLE PLACED BACK DOWN. ON ARRIVAL, FOUND FAULT LIGHT ON PROX BOX 54GB. PERFORMED MEMORY RECALL ON 54GB & GOT
- [SDR FDEA202407040936](https://openairdocs.org/sdr/FDEA202407040936.md): Fire Detector · failed · Jul 4, 2024 · N689FE · Airbus A300F4605R · Fire Detection
  > ENG1 LOOP A FAULT DURING CLIMB OUT. APPEARED AND WENT AWAY AFTER A SHORT TIME ON FIRST FLIGHT, OCCURRED AGAIN TWICE DURING 2ND FLIGHT (ALSO DURING CLIMB OUT). RELEASED FOR SERVICE PER MEL: 26-XX-XXC CAT: C EXP: 14JUL24 ENG 1 LOOP A - INOP. FLIGHT CREW M
- [SDR FDEA202305120862](https://openairdocs.org/sdr/FDEA202305120862.md): Controller · failed · May 12, 2023 · N689FE · Airbus A300F4605R · Leading Edge Slat Control System
  > ON FINAL, CONFIGURED SLATS/FLAPS 15/15, WE SELECTED 15\20. AFTER SEVERAL SECONDS WE RECEIVED SLATS/FLAPS FAULT ECAM. IAW ECAM, WE CYCLED FLAP LEVER WITH NO CHANGE. WE THEN DISCONTINUED THE APPROACH AND WENT THROUGH THE QRH PROCEDURE. WE WERE PREPARED FOR
- [SDR FDEA202301280170](https://openairdocs.org/sdr/FDEA202301280170.md): Web · cracked · Jan 28, 2023 · N689FE · Airbus A300* · Fuselage Main, Structure
  > MDCC UNDER FLOOR 1EA WEB CRACKED AT FR47, Y953-Y1456. REPAIRED MDCC UNDER FLOOR CRACKED WEB AT FR47, Y953-Y1456 PER A300-600F SRM53-15-15- 201 FIG.201.THIS IS CAT B REPAIR AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300- 600F SRI53-15-15-2-002-00. INS
- [SDR FDEA202204140959](https://openairdocs.org/sdr/FDEA202204140959.md): Warning Message · false activation · Apr 14, 2022 · N689FE · Airbus A300F4605R · Leading Edge Slat Control System
  > DURING APPROACH AND SLAT EXTENSION, RECEIVED ECAM. SLAT SYS 1 FAULT. & FLAPS SYS 1 & 2 FAULT. CYCLE PER ECAM. FAULT DID NOT CLEAR. ALL 3 FAULTS RETURNED INCLUDING AMBER ECAM KRUGER NOT EXTENDED. COMPLIED WITH QRH DECLARED EMERGENCY & LANDED. LT FLAPS SL
- [SDR FDEA202009012076](https://openairdocs.org/sdr/FDEA202009012076.md): Hinge · delaminated · Sep 1, 2020 · N689FE · Airbus A300F4605R · Spoilers
  > LH WING - 4# SPOILER I/B HINGE LOWER SURFACE DELAMINATED (S=20MM X 15MM,D=2.18MM), I/B HINGE INBD SURFACE DELAMINATED (S=60MM X 60MM,D=1.90MM). LH WING - 4# SPOILER I/B HINGE DELAMINATED.COMPLIED WITH EA: 6-5750-T0356106. TITLE: WING - FLIGHT SURFACES -
- [SDR FDEA202009012075](https://openairdocs.org/sdr/FDEA202009012075.md): Hinge Arm · delaminated · Sep 1, 2020 · N689FE · Airbus A300F4605R · Spoilers
  > RH WING - #3 SPOILER O/B CTR HINGE ARM LWR SURFACE DELAMINATED (S=10MM X 15MM,D=2.0MM), I/B CTR HINGE ARM I/B SURFACE DELAMINATED (S=30MM X 40MM,D=1.5MM). RH WING - #3 SPOILER I/B & O/B CTR HINGE ARM DELAMINATED.COMPLIED WITH EA: 6-5750- T0356102. TITLE:
- [SDR FDEA202008292064](https://openairdocs.org/sdr/FDEA202008292064.md): Hinge Arm · delaminated · Aug 29, 2020 · N689FE · Airbus A300F4605R · Drag Control System
  > RT WING, NR 4 SPOILER I/B CTR HINGE ARM I/B SURFACE DELAMINATED (S=30MM X 40MM,D=1.5MM), O/B CTR HINGE ARM O/B SURFACE DELAMINATED (S=30MM X 25MM,D=1.45MM). RT WING, NR 4 SPOILER I/B & O/B CTR HINGE ARM DELAMINATED. COMPLY WITH EA: 6-5750-T0356104; TITLE
- [SDR FDEA202008292063](https://openairdocs.org/sdr/FDEA202008292063.md): Skin · delaminated · Aug 29, 2020 · N689FE · Airbus A300F4605R · Spoilers
  > RT WING NR 5 SPOILER I/B CTR HINGE ARM I/B SURFACE DELAMINATED (S=30MM X 40MM, D=1.3MM), O/B CTR HINGE ARM O/B SURFACE DELAMINATED (S=30MM X 40MM, D=1.5MM), O/B CTR HINGE ARM LOWER SURFACE DELAMINATED (S=20MM X 20MM, D=2.1MM). RT WING NR 5 SPOILER I/B &
- [SDR FDEA2020083192064](https://openairdocs.org/sdr/FDEA2020083192064.md): Hinge Arm · delaminated · Aug 29, 2020 · N689FE · Airbus A300F4605R · Spoilers
  > RH WING - #4 SPOILER I/B CTR HINGE ARM I/B SURFACE DELAMINATED (S=30MM X 40MM,D=1.5MM), O/B CTR HINGE ARM O/B SURFACE DELAMINATED (S=30MM X 25MM,D=1.45MM).
- [SDR FDEA2020091124201](https://openairdocs.org/sdr/FDEA2020091124201.md): Frame · cracked · Aug 24, 2020 · N689FE · Airbus A300F4605R · Fuselage Main, Frame
  > NDT INSP RT CENTER WING JOINT AT FR40 UPPER HOLE FOUND CRACKED SIGNAL. NDT INSP RT CENTER WING JOINT AT FR40 UPPER HOLE FOUND CRACKED SIGNAL. COMPLIED WITH EA: 6-5710-T0356266 P1. TITLE: WINGS-BASIC WING STRUCTURE-CRACK IN THE UPPER HOLE AT FR40 RHS CENTER W
- [SDR FDEA2020082642001](https://openairdocs.org/sdr/FDEA2020082642001.md): Joint · cracked · Aug 24, 2020 · N689FE · Airbus A300F4605R · Fuselage Main, Structure
  > NDT INSPECTION, RT CENTER WING JOINT AT FR40 UPPER HOLE FOUND CRACKED SIGNAL.
- [SDR FDEA2020052211014](https://openairdocs.org/sdr/FDEA2020052211014.md): Gcu · malfunctioned · May 21, 2020 · N689FE · Airbus A300F4605R · AC Regulator
  > PDIS 689 24-20 1465 20MAY20 GENERATOR #2 FAULT @ CLIMB FROM FL 300 TO FL 330. TRIED RESET GENERATOR #2 WOULD NOT RESET.ATTEMPTED START OF APU @ FL 330 WOULD NOT START.DESCENDED TO FL250 TO ATTEMPT SECOND START OF APU. APU WOULD NOT START. DEC
- [SDR FDEA20180515224](https://openairdocs.org/sdr/FDEA20180515224.md): Skin · dented · May 14, 2018 · N689FE · Airbus A300F4605R · Cargo/Baggage Doors
  > CARGO DOOR EXTERNAL SKIN HAS TWO DENTS. 5 INCHES FROM FWD LOWER CORNER, 1 INCH. AND 4 INCHES FROM FWD EDGE. FOUND TO BE OUT OF LIMITS IAW SRM 52-30-00, CUT OUT DAMAGED AREA, FABRICATED A REPAIR DOUBLER AND INSTALLED IAW SRM 52-34-00. MAJOR REPAIR.
- [SDR FDEA201804301146](https://openairdocs.org/sdr/FDEA201804301146.md): Seat Track · damaged · Apr 30, 2018 · N689FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK -Y1959 DAMAGED BETWEEN FRAMES 63 AND 64. REMOVED DAMAGED SECTION FROM THE SEAT TRACK IAW SRM 51-40-21. FABRICATED A REPAIR IAW SRM 53-10-16, PG 207, FIG 202. INSTALLED THE REPAIR IAW SRM 51-40-21. MAJOR REPAIR.
- [SDR FDEA201710112906](https://openairdocs.org/sdr/FDEA201710112906.md): Solenoid Valve · inoperative · Oct 11, 2017 · N689FE · Airbus A300F4605R · Trailing Edge Flap Control System
  > SLATS & FLAPS SYSTEM 1 AND 2 FAULTED WHEN THE HANDLE WAS SELECTED TO 15/20. FLAPS WOULD RETRACT TO 0 WHEN SELECTED, BUT ONLY EXTEND TO 15/15 WITHOUT A FAULT INDICATION. REPLACED A FAULTY SOLENOID MM 27-54-33-04. OPERATED FLAPS AND SLATS FOR 6 CYCLES WITH B
- [SDR FDEA201705031349](https://openairdocs.org/sdr/FDEA201705031349.md): Valve · cracked · May 3, 2017 · N689FE · Airbus A300F4605R · Hydraulic System, Main
  > AT TOP OF DESCENT, THE GREEN SYS HYD QTY LOW ECAM ILLUMINATED. ECAM AND OVERHEAD BOTH INDICATED QTY LOSS. NO AIR LIGHT WAS ASSOCIATED WITH THIS PROBLEM. MANUALLY EXTENDED GEAR IAW QRH. AFTER LANDING, THE GREEN SYS QTY REAPPEARED BOTH ECAM AND OVERHEAD.
- [SDR FDEA201705021317](https://openairdocs.org/sdr/FDEA201705021317.md): Gauge · leaking · May 2, 2017 · N689FE · Airbus A300F4605R · Passenger/Crew Doors
  > R1 ENTRY DOOR EMERGENCY CYLINDER PRESSURE GAUGE IS MISSING CENTER PLUG IN LENS AND IS LEAKING OIL FROM GAUGE. REMOVED AND REPLACED R1 DOOR DAMPER EMERGENCY OPERATION CYLINDER IAW MM 52-10-14-04-02.
- [SDR FDEA201704291297](https://openairdocs.org/sdr/FDEA201704291297.md): Relief Valve · failed · Apr 29, 2017 · N689FE · Airbus A300F4605R · Hydraulic Indicating System
  > RIGHT AFTER DEPARTING AT FL 340, DURING DESCENT, RECEIVED A GREEN HYD RESERVOIR LOW LEVEL WARNING. CONFIRMED ON OVERHEAD AND ECAM. FOLLOWED ECAM AND QRH PROCEDURES. MANUALLY EXTENDED LANDING GEAR AND SHUT DOWN APPROPRIATE EQUIPMENT. DECLARED EMERGENCY. AC
- [SDR FDEA201704281292](https://openairdocs.org/sdr/FDEA201704281292.md): Valve · stuck · Apr 28, 2017 · N689FE · Airbus A300F4605R · Hydraulic System, Main
  > ON DESCENT TO KMEM, GOT GREEN HYD RESERVOIR LO LEVEL. CONFIRMED ON OVERHEAD & ECAM. FOLLOWED QRH PROCEDURE & MANUAL EXTENDED GEAR AND SHUT DOWN AFFECTED EQUIPMENT. DECLARED EMERGENCY & STOPPED ON RWY. GREEN RSVR AIR CAME ON THEN QUAN FLUCTUATED. NO PUMPS OR
- [SDR FDEA201512214062](https://openairdocs.org/sdr/FDEA201512214062.md): Fluid · low · Dec 21, 2015 · N689FE · Airbus A300F4605R · AC Generator-Alternator
  > ON TAKEOFF ROLL, JUST AFTER SETTING TAKEOFF POWER, ECAM FLASHED LOW OIL PRESS, THEN WENT AWAY, GEN NR 2 FAILED SHORTLY AFTER. REJECTED TAKEOFF PRIOR TO 70 KTS. DURING IDLE RUN NR 2 ENG WAS READING 16 QTS. CHECKED OIL SERVICING ON NR 2 ENG SERVICED WITH 1/2
- [SDR FDEA201511183700](https://openairdocs.org/sdr/FDEA201511183700.md): Floor Panel · delaminated · Nov 18, 2015 · N689FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 251 CH IS DELAMINATED. FABRICATED NEW PANEL ON T15 1172111 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511183698](https://openairdocs.org/sdr/FDEA201511183698.md): Floor Panel · broken · Nov 18, 2015 · N689FE · Airbus A300F4605R · Fuselage Floor Panel
  > MCD FLOOR PANEL 232 ZG HAS BROKEN BOTTOM COMPOSITE LAYER ON RT EDGE CORNER. FABRICATED NEW PANEL ON T15 1172044 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511183697](https://openairdocs.org/sdr/FDEA201511183697.md): Floor Panel · damaged · Nov 18, 2015 · N689FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO COMPARTMENT, FLOOR PANEL 232 VH DAMAGED. FABRICATED NEW PANEL ON T15 1172146 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511183696](https://openairdocs.org/sdr/FDEA201511183696.md): Floor Panel · damaged · Nov 18, 2015 · N689FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC FLOOR PANEL 231 JG PUNCTURED ON SEVERAL PLACES. FABRICATED NEW PANEL ON T15 1172142 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511183699](https://openairdocs.org/sdr/FDEA201511183699.md): Floor Panel · cracked · Nov 18, 2015 · N689FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOORBOARD PANEL 241 LK HAS CRACKED. FABRICATED NEW PANEL ON T15 1172117 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511173678](https://openairdocs.org/sdr/FDEA201511173678.md): Floor Panel · damaged · Nov 17, 2015 · N689FE · Airbus A300F4605R · Fuselage Floor Panel
  > MCD FLOOR PANEL 232 HG LOWER SURFACE DAMAGED AT FASTENER HOLE. FABRICATED NEW PANEL ON T15 1172057 IAW DWG SRZ 25-005 REV L CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511173677](https://openairdocs.org/sdr/FDEA201511173677.md): Floor Panel · delaminated · Nov 17, 2015 · N689FE · Airbus A300F4605R · Fuselage Floor Panel
  > MCD FLOOR PANEL 232 BH HAS DELAMINATED ON RT FWD EDGE CORNER. FABRICATED NEW PANEL ON T15 1172035 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511173676](https://openairdocs.org/sdr/FDEA201511173676.md): Floor Panel · cracked · Nov 17, 2015 · N689FE · Airbus A300F4605R · Fuselage Floor Panel
  > MCD FLOOR PANEL 232 QG HAS CRACK ON MID AFT AREA. FABRICATED NEW PANEL ON T15 1172120 IAW DWG SRZ 25-005 REV L. CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511173674](https://openairdocs.org/sdr/FDEA201511173674.md): Floor Panel · damaged · Nov 17, 2015 · N689FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 231 BH DAMAGED. FABRICATED NEW PANEL ON T15 1172143 IAW DWG SRZ 25-005 REV L CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511173673](https://openairdocs.org/sdr/FDEA201511173673.md): Floor Panel · damaged · Nov 17, 2015 · N689FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 231 UG DAMAGED. FABRICATED NEW PANEL ON T15 1172121 IAW DWG SRZ 25-005 REV L CLASSIFIED AS MAJOR CAT A REPAIR.
- [SDR FDEA201511173672](https://openairdocs.org/sdr/FDEA201511173672.md): Floor Panel · cracked · Nov 17, 2015 · N689FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN DECK FLOOR PANEL 241 KJ HAS CRACKED. FABRICATED NEW PANEL ON T15 1172744 IAW DWG SRZ 25-005 REV L CLASSIFIED AS MAJOR CAT A REPAIR.

Next page: https://openairdocs.org/aircraft/N689FE/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 = 'N689FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N689FE/reports

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