# Service difficulty reports: N817FD, cancelled Mar 2, 2024

A list on [N817FD, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N817FD-2024-03-02.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 · 66 reports

- [SDR FDEA201405211117](https://openairdocs.org/sdr/FDEA201405211117.md): Fitting · damaged · May 21, 2014 · N817FD · Airbus A310304 · Wing Miscellaneous Structure
  > LEFT RIB 5 FWD LUG BORE OUT OF ROUND REPAIRED LT RIB 5 FWD LUG BORE OUT OF ROUND IAW DWG R57249389 & COMPLIED WITH EA 6-5710-T0308275.
- [SDR FDEA201401030015](https://openairdocs.org/sdr/FDEA201401030015.md): Switch · malfunctioned · Jan 3, 2014 · N817FD · Airbus A310304 · Door Warning System
  > LEFT CABIN DOOR SHOWED UNLOCKED AT FL 240. LEVELED OFF, PERFORMED QRH & PUSHED ON THE HANDLE. DOOR SHOWED LOCKED. CONTINUED TO CLIMB & DOOR SHOWED UNLOCKED AT FL 340, FINAL ALTITUDE WAS TO BE FL 400, RETURNED TO DEPARTURE. REMOVED AND REPLACED DOOR WARNIN
- [SDR FDEA201312122966](https://openairdocs.org/sdr/FDEA201312122966.md): Hinge Fitting · nicked · Dec 12, 2013 · N817FD · Airbus A310304 · Fuselage, Door Hinge
  > NOSE LANDING GEAR, RT AFT DOOR HINGE FITTING, BEARING HOLE FOUND TWO NICKS. REPAIRED IAW EA 6-5310-99725B PART 2.
- [SDR FDEA201304240855](https://openairdocs.org/sdr/FDEA201304240855.md): Wire Harness · failed · Apr 24, 2013 · N817FD · Airbus A310304 · Landing Gear System Wiring
  > AFTER TOUCHDOWN, DURING ROLLOUT NR 5 AND NR 6 TIRES BLEW. ACFT REMAINED ON CENTERLINE. REMOVED AND INSTALLED AND ROUTED LT MLG HARNESS LOOM THRU NR 5 AND NR 6 BOGIES IN POSITION IAW MM 32-11-43-04.
- [SDR FDEA201203160978](https://openairdocs.org/sdr/FDEA201203160978.md): Shear Plate · corroded · Mar 16, 2012 · N817FD · Airbus A310304 · Fuselage Miscellaneous Structure
  > FWD END SHEAR PLATE FOUND CORRODED AT SEVERAL LOCATIONS FROM BS 410 TO 440, BL 0 TO LBL 24.75 FWD END SHEAR PLATE REPAIRED IAW EA F-5310-157901.
- [SDR FDEA201202160591](https://openairdocs.org/sdr/FDEA201202160591.md): Computer · malfunctioned · Feb 16, 2012 · N817FD · Airbus A310304 · Fuel Quantity Indicator
  > APPROX 1.5 HRS INTO FLIGHT, RT OTBD FUEL TANK QTY BEGAN TO DECREASE RAPIDLY. TANK WENT TO EMPTY, XX, AND REMAINED UNTIL IN DESCENT AT 16,000 FT, THEN QTY RETURNED TO 6.42. TROUBLESHOOTING VERIFIED FUEL LEVEL IN RT OTBD TANK ON RT NR 2 & NR 3 MAGNETIC LEVEL
- [SDR FDEA201107032558](https://openairdocs.org/sdr/FDEA201107032558.md): Floorbeam · damaged · Jul 3, 2011 · N817FD · Airbus A310304 · Fuselage Main, Floor Beam
  > BULK CARGO COMPARTMENT, FR 63 FLOORBEAM BOTTOM CEILING PANEL ATTACHMENT BETWEEN SEAT TRACK 1 AND 2L HAS A DRILL START. COMPLIED WITH EA 6-5310-145342 PT1.
- [SDR FDEA201107012531](https://openairdocs.org/sdr/FDEA201107012531.md): Stringer · gouged · Jul 1, 2011 · N817FD · Airbus A310304 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT LT SIDE FWD OF FR 54.1, STR 37 HAS GOUGE. REMOVED, REPAIRED AND RE-INSTALLED STRINGER SECTION IAW SRM 53-10-14, PGS 201 THROUGH 231 SRM 51-21-10, PG 2, SRM 51-40-44, PG 1 AND SRM 51-75-10, PG 204.
- [SDR FDEA201107012532](https://openairdocs.org/sdr/FDEA201107012532.md): Seal · cracked · Jul 1, 2011 · N817FD · Airbus A310304 · Fuel Storage
  > METALLIC VAPOR SEAL CRACKED ON LT SIDE AT FR 42-43, R & R METALLIC VAPOR SEAL ON LT SIDE FR 42-43.
- [SDR FDEA201106142246](https://openairdocs.org/sdr/FDEA201106142246.md): Web · damaged · Jun 14, 2011 · N817FD · Airbus A310304 · Fuselage Miscellaneous Structure
  > AFT PIT FR 69 RBL 26 VERTICAL WEB PUNCTURED AT CARGO FLOOR LEVEL REMOVED AND REPLACED VERTICAL WEB AT FR 69 RBL 26 IAW SRM 51-40-21
- [SDR FDEA201106122211](https://openairdocs.org/sdr/FDEA201106122211.md): Seat Track · cracked · Jun 12, 2011 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NR 3 LT CORRODED AT FR 19. REMOVED CORROISON FROM NR 3 SEAT TRACK AT FR 19 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED NR 3 LT SEAT TRACK SECTION AT FR 19 IAW SRM 51-72-10.
- [SDR FDEA201106122212](https://openairdocs.org/sdr/FDEA201106122212.md): Seat Track · corroded · Jun 12, 2011 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC SEAT TRACK, NR 6, RT CORRODED INSIDE TRACK. REMOVED LEVEL 1 CORROSION ON SEAT TRACK NR 6 AT FR 19 AND FOUND TO BE OUT OF LIMITS IAW AIRBUS SRM 53-10-16. REPAIRED NR 6 SEAT TRACK AT FR 19 IAW EA 6-5310-145630.
- [SDR FDEA201106122210](https://openairdocs.org/sdr/FDEA201106122210.md): Seat Track · corroded · Jun 12, 2011 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SEAT TRACK NR6 BETWEEN FRAME 19 & 20 HAS CORRSION 1 SQ INCH. REMOVED LEVEL 1 CORROSION FROM RT NR 6 SEAT TRACK BETWEEN FRAME 19 & 20 AND FOUND BEYOND LIMITS IAW SRM 53-10-16. REPAIRED IAW EA 6-5310-145630.
- [SDR FDEA201106122213](https://openairdocs.org/sdr/FDEA201106122213.md): Floorbeam · corroded · Jun 12, 2011 · N817FD · Airbus A310304 · Fuselage Main, Floor Beam
  > MDC UNDERFLOOR TEE HAS 1 SQ INCH OF CORROSION FWD OF SEAT TRACK NR LT AT FR 12A. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED AND REPLACED TEE FWD OF SEAT TRACK NR 3 AT FR 12A IAW SRM 51-72- 10.
- [SDR FDEA201106102204](https://openairdocs.org/sdr/FDEA201106102204.md): Seat Track · damaged · Jun 10, 2011 · N817FD · Airbus A310304 · Fuselage Main, Frame
  > SEAT TRACK 4L AT FRAME 54.3 HAS DAMAGE TO TACK AND SCALLOPS. BLENDED DAMAGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 4L SECTION AT FR 54.3 IAW SRM 51-72-10.
- [SDR FDEA201106102201](https://openairdocs.org/sdr/FDEA201106102201.md): Seat Track · damaged · Jun 10, 2011 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach Fittings
  > MDC SEAT TRACK 5R HAS 2 GOUGES AT SCALLOPS, 1 AT 54.2 AND 1 7 INCHES AFT OF 54.2. BLENDED DAMAGED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 5R SECTION AT FR 54.2 INCLUDING 17 INCHES AFT OF FR 54.2.
- [SDR FDEA201106102203](https://openairdocs.org/sdr/FDEA201106102203.md): Seat Track · damaged · Jun 10, 2011 · N817FD · Airbus A310304 · Fuselage Main, Frame
  > 2 EA GOUGES ON SEAT TRACK 3R FROM FRAME 54.2 TO FRAME 55/58. BLENDED GOUGED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 3R SECTION AT FR 54.2
- [SDR FDEA201106102202](https://openairdocs.org/sdr/FDEA201106102202.md): Seat Track · damaged · Jun 10, 2011 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK 2R AT FRAME 54.2 HAS GOUGE AT SCALLOP. BLENDED GOUGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 2R SECTION AT AT FR 54.2 IAW SRM 51-72-10.
- [SDR FDEA201106052123](https://openairdocs.org/sdr/FDEA201106052123.md): Fitting · corroded · Jun 5, 2011 · N817FD · Airbus A310304 · Nacelle/Pylon Miscellaneous Structure
  > NR2 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 2 PYLON IAW AMM 54-50-00-4 REMOVED AND REPLACED UPPER AND LOWER SPIGOT FITTING IAW S/B 54-20-20 PAR. B(6) REINSTALLED NR 2 PYLON IAW AMM 54-50-00-4 COMPLIED WITH FEDEX EA 6
- [SDR FDEA201106052121](https://openairdocs.org/sdr/FDEA201106052121.md): Fitting · corroded · Jun 5, 2011 · N817FD · Airbus A310304 · Nacelle/Pylon, Main Frame
  > NR 1 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 1 PYLON IAW AMM 54-50-00-4. REMOVED AND REPLACED UPPER AND LOWER SPIGOT FITTINGS IAW S/B 54-2020 PARA B(6). REINSTALLED NR 1 PYLON IAW AMM 54-50-00-4. COMPLIED WITH EA-5450-
- [SDR FDEA201106012083](https://openairdocs.org/sdr/FDEA201106012083.md): Seat Track · misinstalled · Jun 1, 2011 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK NR 2 LT Y450 BETWEEN FRAMES 47/48 TO 49 HAS AN EXISTING REPAIR WITH INCORRECT FASTENERS INSTALLED ON TOP FLANGE. REMOVED AND REPLACED 20 EACH RIVETS AND INSTALLED 20 EACH LOCK FASTENERS ON TOP FLANGE OF SEATTRACK REPAIR BETWEEN FRAMES
- [SDR FDEA201002090367](https://openairdocs.org/sdr/FDEA201002090367.md): Bellcrank · dirty · Feb 9, 2010 · N817FD · Airbus A310304 · Landing Gear Door Retract Section
  > LT MAIN GEAR DOOR WOULD NOT CLOSE ON T/O. RETURNED TO DEPARTURE. OPS CHECKED LT MLG DOOR IAW MM 32-12-11-5. OPS CHECKS NORMAL. DURING TROUBLESHOOTING, WERE ABLE TO DUPLICATE THIS PROBLEM BY OPERATING DOOR WITH GROUND CONTROL HANDLE, AFTER DISASSEMBLING, CL
- [SDR FDEA200907012422](https://openairdocs.org/sdr/FDEA200907012422.md): Idg · underserviced · Jul 1, 2009 · N817FD · Airbus A310304 · Alternator-Generator Drive
  > ON T/O ROLL AT APPROX 80 KNOTS RECEIVED ECAM ALERT, NR 1 IDG OIL PRESS W/ GEN 1 FAULT. RTO AND RETURNED TO BLOCKS. GEN 1 FAULT CLEARED BUT IDG NR1 FAULT KEPT FLICKERING. SERVICED NR 1 ENG IDG IAW AMM 12-13-24-0. RAN NR 1 ENG IAW JRH CHAP 5. NO LEAKS NOTED,
- [SDR FDEA200812065096](https://openairdocs.org/sdr/FDEA200812065096.md): Bushing · damaged · Dec 6, 2008 · N817FD · Airbus A310304 · Fuselage, Landing Gear Attach Fittings
  > MAIN FRAME RT NOSE LANDING GEAR BEARING FITTING INSPECTION PER EA T6-5310-99725A, REQUIRES REMOVAL OF REPAIR BUSHING FOR INSPECTION. REMOVED REPAIR BUSHING, FABRICATED REPLACEMENT REPAIR BUSHING AND INSTALLED IAW FEDEX EA 6-5310-99725A, RELEASE DATE 07/20/06.
- [SDR 08FDEA04961](https://openairdocs.org/sdr/08FDEA04961.md): Seat Track · damaged · Nov 22, 2008 · N817FD · Airbus A310304 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPT SEAT TRACK NR 2 RT, 12 IN AFT OF FR 43 HAS 2 DAMAGED SCALLOPS. REMOVED DAMAGED SECTION OF SEAT TRACK NR 2 RT. FABRICATED REPLACEMENT SECTION AND INSTALLED BETWEEN FR 40 AND FR 45 IAW A310 SRM 53-10-16 AND SRM 51-40-21.
- [SDR 08FDEA01724](https://openairdocs.org/sdr/08FDEA01724.md): Transmitter · inoperative · May 1, 2008 · N817FD · Airbus A310304 · Hydraulic Indicating System
  > ON FINAL APPROACH, RECEIVED SLAT SYS 1 AND 2 FAULT FOLLOWED UP SHORTLY W/GREEN HYD ECAM COMMAND TO TURN OFF BOTH GREEN HYD PUMPS. FAULTS ON OVERHEAD WERE AS FOLLOWS: GREEN SYS SERVO (GREEN PUMPS OFF), SLAT SYS 1 AND 2, SPOILER NR 5. DID GO AROUND FOUND RT M
- [SDR 08FDEA00192](https://openairdocs.org/sdr/08FDEA00192.md): Hydraulic System · low · Jan 18, 2008 · N817FD · Airbus A310304 · Hydraulic System, Main
  > REJECT T/O DUE TO ECAM: GREEN SYSTEM HYD QTY LOW. VERY COLD OUTSIDE AIR TEMP. PERFORMED VISUAL INSPECTION AND NO LEAKS FOUND. SERVICED GREEN HYD SYS PER SMP AND A310-300 AMM REF 12-12-29, SERVICED TWO QTS. A/C OK FOR SERVICE.
- [SDR 07FDEA00151](https://openairdocs.org/sdr/07FDEA00151.md): Slide · low · Jan 22, 2007 · N817FD · Airbus A310304 · Escape Slide
  > R1 DOOR ESCAPE SLIDE PRESSURE INDICATOR NOT IN GREEN BAND REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE IAW A310-300 AMM 25-61-22-4-01 AND A310 - 300 AMM 52-10-00-3.
- [SDR 06FDEA03588](https://openairdocs.org/sdr/06FDEA03588.md): Fitting · corroded · Oct 4, 2006 · N817FD · Airbus A310304 · Fuselage Main, Attach Fittings
  > COMPLY WITH AGING 9-AGING-INSP, FOUND CORROSION AND WEAR LOCATED IN RT FITTING BETWEEN FS 16A/ FS 17 IN HOLE AT ATTACHMENT FITTING OF AFT DOOR.
- [SDR 06FDEA03400](https://openairdocs.org/sdr/06FDEA03400.md): Skin · damaged · Sep 22, 2006 · N817FD · Airbus A310304 · Landing Gear Doors
  > RT MLG-STRUT DOOR W/SKIN SURFACE DAMAGED AND REPAIR AT LOWER AREA THE STRUT DOOR WAS REPAIRED PER FEDEX EA 6-5280-99721 EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MINOR".
- [SDR 06FDEA03054](https://openairdocs.org/sdr/06FDEA03054.md): Skin · damaged · Aug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge Flaps
  > FOUND REPAIR LOCATED RT OUTBD FLAP AT INNER LOWER SKIN SURFACE AND UPPER SKIN SURFACE OF T/E RIB 11/RIB 12. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO AN
- [SDR 06FDEA03053](https://openairdocs.org/sdr/06FDEA03053.md): Skin · damaged · Aug 22, 2006 · N817FD · Airbus A310304 · Landing Gear Doors
  > FOUND REPAIR LOCATED MLG RT W/W DOOR AT INNER LOWER SKIN SURFACE AT OUTBD LOWER PART. REPAIR REQUIRE EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR W/W DOOR PER SRM 52-81-12. REPAIR EVALUATED PER GMM
- [SDR 06FDEA03052](https://openairdocs.org/sdr/06FDEA03052.md): Skin · damaged · Aug 22, 2006 · N817FD · Airbus A310304 · Elevator, Plate/Skin
  > FOUND REPAIR LOCATED AT RT ELEVATOR AT INNER LOWER SKIN SURFACE STA 833/ER 38 AND STA 791/ ER36. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 55-2
- [SDR 06FDEA03051](https://openairdocs.org/sdr/06FDEA03051.md): Skin · damaged · Aug 22, 2006 · N817FD · Airbus A310304 · Elevator, Plate/Skin
  > FOUND REPAIR LOCATED RT ELEVATOR AT INNER LOWER SKIN STA 604/ER26 AND STA 566/ER 24. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 55-21-12 FIG 204.
- [SDR 06FDEA03050](https://openairdocs.org/sdr/06FDEA03050.md): Skin · damaged · Aug 22, 2006 · N817FD · Airbus A310304 · Leading Edge Devices
  > FOUND REPAIR LOCATED ON LT NR 2 SLAT SKIN SURFACE OF L/E BETWEEN RIB 44/45 (NEXT JACK RIB 4). REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR, DISCREPANCY REPORT 43000001-391
- [SDR 06FDEA03049](https://openairdocs.org/sdr/06FDEA03049.md): Skin · damaged · Aug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge Flaps
  > FOUND REPAIR LOCATED INBD FLAP LT AT LOWER SURFACE AT RIB 8/ RIB 10. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR COVERED BY RAS REF: RAS /DA/BRE/1642/97, REPAIR EVALUATE
- [SDR 06FDEA03048](https://openairdocs.org/sdr/06FDEA03048.md): Skin · damaged · Aug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge Flaps
  > FOUND REPAIR LOCATED LT INB FLAP AT T/E UPPER AND LOWER SKIN SURFACE BETWEEN RIB 5 AND RIB 8. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXIS
- [SDR 06FDEA03047](https://openairdocs.org/sdr/06FDEA03047.md): Skin · damaged · Aug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge Flaps
  > FOUND REPAIR LOCATED RT OUTB FLAP AT INNER LOWER SKIN SURFACE AT T/E OF INDB OF RIB 3. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SR
- [SDR 06FDEA03046](https://openairdocs.org/sdr/06FDEA03046.md): Skin · damaged · Aug 22, 2006 · N817FD · Airbus A310304 · Trailing Edge Flaps
  > FOUND REPAIR LOCATED RT INB FLAP AT INNER LOWER AND UPPER SKIN SURFACE AT T/E OF FLAP RIB 19. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA REPAIR CONFORMS TO EXISTING FEDEX ENGINEERING AUTHORIZ
- [SDR 06FDEA03045](https://openairdocs.org/sdr/06FDEA03045.md): Structure · unknown · Aug 22, 2006 · N817FD · Airbus A310304 · Wing Miscellaneous Structure
  > FOUND REPAIR LOCATED ON RT WING T/E WS 1625, RIB 26-27 BETWEEN OUTB FLAP AND WING TIP. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. THIS REPAIR WAS REMOVED AND REPLACED A NEW TRAILING EDGE P
- [SDR 06FDEA03044](https://openairdocs.org/sdr/06FDEA03044.md): Door · misrepaired · Aug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) Doors
  > FOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 5055/5065 FS 100/100. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA, REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REP
- [SDR 06FDEA03043](https://openairdocs.org/sdr/06FDEA03043.md): Door · misrepaired · Aug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) Doors
  > FOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 4986/5003 FR 98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED
- [SDR 06FDEA03042](https://openairdocs.org/sdr/06FDEA03042.md): Door · misrepaired · Aug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) Doors
  > FOUND REPAIR RT APU DOOR BETWEEN STA 4969/5001 FS 97/98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR AC
- [SDR 06FDEA03041](https://openairdocs.org/sdr/06FDEA03041.md): Door · misrepaired · Aug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) Doors
  > FOUND REPAIR RT APU DOOR BETWEEN STA 4937/4969 FR 96/97 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPL
- [SDR 06FDEA03040](https://openairdocs.org/sdr/06FDEA03040.md): Door · misrepaired · Aug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) Doors
  > FOUND REPAIR LOCATED LT APU DOOR BETWEEN STA 5033/5045 FS 99/99. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR
- [SDR 06FDEA03039](https://openairdocs.org/sdr/06FDEA03039.md): Skin · damaged · Aug 22, 2006 · N817FD · Airbus A310304 · Cargo/Baggage Doors
  > PREVIOUS REPAIR FOUND AT BULK COMP´T DOOR SKIN LOCATED AT BEAM 5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR ACCOMPLISHED USING FAA DATA EXISTING REPAIR COVERED BY RAS REF:RAS/DAHAM/4014519/2001. REPAIR EVALUATED PER GMM 6-2-100
- [SDR 06FDEA3035](https://openairdocs.org/sdr/06FDEA3035.md): None · none · Aug 22, 2006 · N817FD · Airbus A310203 · Standard Practices/Structures
  > NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121.370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT AFT COMP´T DOOR FRAME BETWEEN FS 63/64 AND STRINGER BETWEEN 40/44 RT. REPAIR REQUIRES EVALUATION
- [SDR 06FDEA3036](https://openairdocs.org/sdr/06FDEA3036.md): None · none · Aug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/Structures
  > NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121.370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT FUSELAGE SKIN LOCATED BETWEEN FS 64/67 AND BETWEEN STRG 33/40 RT. REPAIR REQUIRES EVALUATION FOR
- [SDR 06FDEA3037](https://openairdocs.org/sdr/06FDEA3037.md): None · none · Aug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/Structures
  > NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121.370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT FUSELAGE SKIN LOCATED BETWEEN FS 66/68 AND BETWEEN STRG 48/54 RT. REPAIR REQUIRES EVALUATION FOR
- [SDR 06FDEA3038](https://openairdocs.org/sdr/06FDEA3038.md): None · none · Aug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/Structures
  > NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121.370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED LT FS4715/4760, FS 89/90, STRG 33/38 NEXT TO APU INLET. REPAIR REQUIRED EVALUATION FOR MAJOR/ MINOR D

Next page: https://openairdocs.org/deregistered/N817FD-2024-03-02/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 = 'N817FD' AND deregistration_id = 'N817FD-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N817FD-2024-03-02/reports

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