# Service difficulty reports: N807FD, cancelled Mar 2, 2024

A list on [N807FD, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N807FD-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 · 79 reports

- [SDR FDEA2019060311203](https://openairdocs.org/sdr/FDEA2019060311203.md): Sequence Valve · misaligned · May 31, 2019 · N807FD · Airbus A310324 · Landing Gear Retraction/Extension System
  > 6685 ON GEAR EXTENSION RECEIVED UNSAFE INDICATION FOR RT MLG ON SYS 1 SYS 2. COMPLIED WITH QRH PROCEDURES AND LG GRAVITY EXTENSION CHECKLIST. GEAR DOORS REMAINED OPEN, UNEVENTFULL LANDING KLRD. (ON LOW APPROACH, TOWER CONFIRMED RT MLG HUNG UP). TROUB
- [SDR FDEA2018042601120](https://openairdocs.org/sdr/FDEA2018042601120.md): Power Supply · failed · Apr 25, 2018 · N807FD · Airbus A310324 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY 29WLI IAW AMM 33-51-14-04-09. OPS CHECKED GOOD.
- [SDR FDEA201705031343](https://openairdocs.org/sdr/FDEA201705031343.md): Jackscrew · lack of lube · May 3, 2017 · N807FD · Airbus A310324 · Trailing Edge Flap Control System
  > WHEN SELECTING FLAPS TO 15, NOTICE BINDING LEAVING THE SLATS/FLAPS 15/0 GATE AT FLAPS 15 RECEIVED FLAP FAULT SYS 1 AND 2. CYCLED THE FLAP HANDLE, NO CHANGE. QRH PROCDURES COMPLETED. LANDED FLAPS 0. REMOVED AND REPLACED THE FLAP/SLAT HANDLE COMMAND SENS
- [SDR FDEA201612134398](https://openairdocs.org/sdr/FDEA201612134398.md): Floor Support · corroded · Dec 13, 2016 · N807FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > MAIN DECK FRAMES 12A - 14, Y953 FLOOR SUPPORT FOUND CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201612134397](https://openairdocs.org/sdr/FDEA201612134397.md): Skin · dented · Dec 13, 2016 · N807FD · Airbus A310324 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FOUND A DENTED BETWEEN FRAMES 65 - 66, STRINGER 36 - 37R. REPAIRED IAW SRM 53-10-12- 201 PARA 6 FIG225 SHEET 2. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201612094367](https://openairdocs.org/sdr/FDEA201612094367.md): Angle · cracked · Dec 9, 2016 · N807FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > FRAME 47 RT INTERNAL ANGLE\ FOUND CRACKED. REPAIRED THE ANGLE IAW EA 6-5710-T0312253 C P3. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201612094366](https://openairdocs.org/sdr/FDEA201612094366.md): Angle · cracked · Dec 9, 2016 · N807FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > ANGLE AT FRAME 47 LT SIDE FOUND CRACKED. REPAIRED IAW EA 6-5710-T0312253 C P3. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201612094369](https://openairdocs.org/sdr/FDEA201612094369.md): Angle · cracked · Dec 9, 2016 · N807FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > TEE ANGLE AT STIFFENER 8 RT FOUND CRACKED. REPAIRED IAW EA 6-5710-T0330412 P1. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201612094368](https://openairdocs.org/sdr/FDEA201612094368.md): Angle · cracked · Dec 9, 2016 · N807FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > TEE ANGLE AT STIFFENER 8 LT FOUND CRACK. REPAIRED THE TEE ANGLE IAW EA 6-5710-T0330412 P1. MAJOR REPAIR IAW GMM 6-2-100
- [SDR FDEA201612074345](https://openairdocs.org/sdr/FDEA201612074345.md): Attach Fitting · cracked · Dec 7, 2016 · N807FD · Airbus A310324 · Cargo/Baggage Doors
  > AFT CARGO DOOR ACTUATOR ATTACH FITTING FOUND CRACK BY HFEC INSPECTION. REPLACED THE ATTACH FITTING IAW SRM 51-40-21.
- [SDR FDEA201612074344](https://openairdocs.org/sdr/FDEA201612074344.md): Floor Support · corroded · Dec 7, 2016 · N807FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > MAIN DECK FR11-FR14 Y770 FLOOR SUPPORT CORRODED.
- [SDR FDEA201612074343](https://openairdocs.org/sdr/FDEA201612074343.md): Attach Fitting · cracked · Dec 7, 2016 · N807FD · Airbus A310324 · Cargo/Baggage Doors
  > FWD CARGO DOOR ACTUATOR ATTACH FITTING WITH CRACK SIGNAL. REPLACED THE ATTACH FITTING IAW SRM 51-40-21.
- [SDR FDEA201612074342](https://openairdocs.org/sdr/FDEA201612074342.md): Skin · cracked · Dec 7, 2016 · N807FD · Airbus A310324 · Wing, Plate/Skin
  > LEFT WING BOTTOM SKIN FOUND CRACKED AT 581AB CUTOUT. REPAIRED IAW EA 6-5730-T0330205 P1 AND DWG R57249152. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201605021440](https://openairdocs.org/sdr/FDEA201605021440.md): Windshield · cracked · May 2, 2016 · N807FD · Airbus A310324 · Flight Compartment Windows
  > DURING CRUISE FLIGHT AT FL 360, BEGAN TO SEE AN ORANGE GLOW IN LOWER LT CORNER OF CAPTAINS FWD WIND SCREEN. TURNED OUT TO BE WINDSHIELD HEAT ARCING, SO TURNED OFF CAPTAINS WINDSHIELD HEAT. ABOUT THE SAME TIME, CAPTAINS FWD, OUTER WINDSHIELD SHATTERED. REMOV
- [SDR FDEA201601240289](https://openairdocs.org/sdr/FDEA201601240289.md): Windshield · cracked · Jan 24, 2016 · N807FD · Airbus A310324 · Flight Compartment Windows
  > CRACK ON CAPTAINS' OUTER FRONT WINDSHIELD. WINDOW HEAT WAS ON, BUT TURNED OFF ONCE CRACK DEVELOPED. R & R CAPTAINS WINDSHIELD. R & R LT WINDOW TEMP CONTROLLER -19DG. R & R LT WINDOW HEATING PROTECTION UNIT -87DG.
- [SDR FDEA201410123118](https://openairdocs.org/sdr/FDEA201410123118.md): Skin · corroded · Oct 12, 2014 · N807FD · Airbus A310324 · Wing, Plate/Skin
  > LEFT WING UPPER SURFACE SKIN FOUND CORROSION AT THE FRONT OF NR 2 SPOILER. REPAIRED LT WING UPPER SURFACE SKIN IAW EA 6-5730-T0311884 P1. TITLE WING PLATES & SKINS LHS WING TOP SKIN PANEL 2 TE OVERHANG CORROSION REPAIR BETWEEN RIBS 5 - 7. MAJOR REPAIR IAW G
- [SDR FDEA201410113111](https://openairdocs.org/sdr/FDEA201410113111.md): Tee Fitting · cracked · Oct 11, 2014 · N807FD · Airbus A310324 · Wing Miscellaneous Structure
  > CENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTING RT NR 10 FASTENER HOLE WITH CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0312253 TITLE WINGS BASIC WING STRUCTURE SB A310-57-2047 FRAME 47 HOLES CRACKED. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201410062974](https://openairdocs.org/sdr/FDEA201410062974.md): Bracket · cracked · Oct 6, 2014 · N807FD · Airbus A310324 · Ailerons
  > LEFT AILERON OTBD HINGE PANEL BRACKET CRACKED REPAIRED LT AILERON OTBD HINGE PANEL BRACKET IAW EA 6-5750-T0312135. WINGS FLIGHT SURFACES FRONT SPAR LOWER DOUBLER BROKEN AT LT AILERON LOWER SURFACE LE MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201410032930](https://openairdocs.org/sdr/FDEA201410032930.md): Fitting · cracked · Oct 3, 2014 · N807FD · Airbus A310324 · Fuselage Main, Attach Fittings
  > ANGLE & TEE FITTING CRACKED FRAME 47. REPAIRED IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201410032929](https://openairdocs.org/sdr/FDEA201410032929.md): Angle · cracked · Oct 3, 2014 · N807FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > ANGLE & TEE FITTING CRACKED FRAME 47. REPAIRED IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201410032928](https://openairdocs.org/sdr/FDEA201410032928.md): Angle · cracked · Oct 3, 2014 · N807FD · Airbus A310324 · Wing Main, Frame Structure
  > ANGLE & TEE FITTING CRACKED FRAME 47. REPAIRED IAW IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201410032927](https://openairdocs.org/sdr/FDEA201410032927.md): Angle · cracked · Oct 3, 2014 · N807FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > REAR SPAR INTERNAL ANGLE & TEE FITTING RT NR 1 FASTENER HOLE WITH A CRACK SIGNAL. REPAIREDSPAR ANGLE & TEE FITTING IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201409302860](https://openairdocs.org/sdr/FDEA201409302860.md): Floorbeam · corroded · Sep 30, 2014 · N807FD · Airbus A310324 · Fuselage Main, Floor Beam
  > FORWARD CARGO COMPARTMENT FLOORBEAM TEE CORRODED AT FRAME 37, Y140 - Y805. REPAIRED THE FLOORBEAM IAW EA 6-5310-T0311889. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201409272822](https://openairdocs.org/sdr/FDEA201409272822.md): Floorbeam · delaminated · Sep 27, 2014 · N807FD · Airbus A310324 · Fuselage Main, Floor Beam
  > AFT CARGO BAY FLOORBEAM TEE FOUND DELAMINATION AT FRAME 60 Y-805 - Y-1470. CUT THE DELAMINATED BEAM IAW SRM 53-10-15 FIG 207 CHECKED THE CRACKS TO CUTOUT PER NTM 51-10-08 MADE THE REPAIR PARTS IAW SRM 53-10-15 FIG 207 WET INSTALLED THE REPAIR IAW SRM 51-4
- [SDR FDEA201409242751](https://openairdocs.org/sdr/FDEA201409242751.md): Fitting · cracked · Sep 24, 2014 · N807FD · Airbus A310324 · Wing Miscellaneous Structure
  > CENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTING LT NR 10 FASTENER HOLE WITH CRACK SIGNAL. REPAIRED CENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTING LT NR 10 FASTENER HOLE PER EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100
- [SDR FDEA201404010608](https://openairdocs.org/sdr/FDEA201404010608.md): Rib · corroded · Apr 1, 2014 · N807FD · Airbus A310324 · Wing, Rib/Bulkhead
  > RT RIB 5 BORE & AFT FACE HAVE CORROSION. COMPLIED WITH EA 6-5710-T0307063 P 1 WINGS & BASIC WING STRUCTURE, RT RIB 5 LUG CORROSION.
- [SDR FDEA201404010606](https://openairdocs.org/sdr/FDEA201404010606.md): Rib · corroded · Apr 1, 2014 · N807FD · Airbus A310324 · Wing, Rib/Bulkhead
  > LT RIB 5 HAS CORROSION IN BORE & FACE. COMPLIED WITH EA 6-5710-T0307003 WINGS & BASIC STRUCTURE, LT RIB 5 LUG CORROSION.
- [SDR FDEA201402070285](https://openairdocs.org/sdr/FDEA201402070285.md): Fuel · contaminated · Feb 7, 2014 · N807FD · Airbus A310324 · Engine Fuel Distribution
  > EN ROUTE LT OUTER PUMP 1 & PUMP 2 FAILED IN FLIGHT. BOTH PUMPS SHOWED LOW PRESS. FOLLOWED ECAM TO TURNOFF. THAWED LO FUEL PUMPS & TANK WITH 3 COLD BUSTERS FOR 5 HOURS. PERFORMED LO TANK PUMPS OPERATIONAL TESTED IAW AMM IAW 28-21-00-05, BOTH PUMPS CHECKED N
- [SDR FDEA201311302913](https://openairdocs.org/sdr/FDEA201311302913.md): Floor Support · cracked · Nov 30, 2013 · N807FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > MDIS 807 53-00 0008007 30NOV13 BQN CLOSE R FOUND FWD FUSELAGE FLOOR SUPPORT MEMBER BETWEEN C9 & C10, ONE FRAME LT 09 88 WITH SEVERAL CRACKS. A536 11977200 ID WEB IAW SRM 53-11-15 PAGE 4 ITEM 475 PN A53611977200 & ATTACHED FITTING ITEM 185 PN A53610270220.
- [SDR FDEA201204241547](https://openairdocs.org/sdr/FDEA201204241547.md): Fitting · cracked · Apr 24, 2012 · N807FD · Airbus A310324 · Wing Miscellaneous Structure
  > PERFORMED NDT IAW E6-5710-7-3324 A PT2, CRACKS WERE FOUND AT HOLE NR 1 AND HOLE NR 2 OF FRAME 40 RT UPPER CORNER FITTING.
- [SDR FDEA201204241546](https://openairdocs.org/sdr/FDEA201204241546.md): Fitting · cracked · Apr 24, 2012 · N807FD · Airbus A310324 · Wing Miscellaneous Structure
  > PERFORMED NDT IAW E6-5710-7-3324 A PT1, CRACKS WERE FOUND AT HOLE NR 1 AND HOLE NR 2 OF FRAME 40 LT UPPER CORNER FITTING.
- [SDR FDEA201108273530](https://openairdocs.org/sdr/FDEA201108273530.md): Power Supply · failed · Aug 27, 2011 · N807FD · Airbus A310324 · Door Warning System
  > L1 & R1 DOORS ESCAPE SLIDE RELEASE WARNING LIGHTS SYSTEM INOPERATIVE. R & R AUTONOMOUS STANDBY POWER SUPPLY UNIT (70WN). OPS CHECKED GOOD REF MM 52-73-18-04. OK FOR SERVICE.
- [SDR FDEA201104182042](https://openairdocs.org/sdr/FDEA201104182042.md): Battery · failed · Apr 18, 2011 · N807FD · Airbus A310324 · Emergency Lighting
  > ON PREDISPATCH CK, FOUND ON COURIER COMPARTMENT EMERGENCY LT TEST INOP. REMOVED AND REPLACED EMG POWER SUPPLY UNIT AND EMERGENCY SUPPLY BATTERY, REF MM 33-51-14-04-09. OPS CK GOOD. OK FOR SERVICE. (CLOSED)
- [SDR 2011FA0000222](https://openairdocs.org/sdr/2011FA0000222.md): Jackscrew · out of position · Feb 18, 2011 · N807FD · Airbus A310324 · Stabilizer Control System
  > DURING O/H, MX PERFORMED ON THE SCREW JACK ASSY, FE140 SN 125, IDENTIFICATION OF THE WRONG POSITIONING OF THE RATCHET WHEEL (ITEM 3-620 OF CMM 27-44-13), ASSEMBLED ON THE OPPOSITE POSITION COMPARED TO THE SPEC MENTIONED ON THE CMM 27-44-13. LETTER LT-S9-11-10
- [SDR FDEA200910213626](https://openairdocs.org/sdr/FDEA200910213626.md): Skin · damaged · Oct 21, 2009 · N807FD · Airbus A310324 · Rudder, Plate/Skin
  > ACCOMPLISH TERMINATING ACTION REPAIR OF RUDDER. NEW REVISION "C" PART 2 OF EA 6-5540-118407 ACCOMPLISHED TERMINATING ACTION REPAIR OF RUDDER IAW EA NR 6-5540-118407 C PT2 AND RAS/DAHAM/4024327/2008 ISSUE A DATED OCT 20, 2009
- [SDR 07FDEA04039](https://openairdocs.org/sdr/07FDEA04039.md): Skin · misrepaired · Sep 19, 2007 · N807FD · Airbus A310324 · Trailing Edge Flaps
  > OLD EXTERNAL DOUBLER REPAIR ON INBOARD FLAP RT ON LOWER SIDE BETWEEN RIB 10-11, NOT CONFORM TO OLD RECORDS AS PER SRM 57-52-12/FIG 204: EXTERNAL DOUBLER IS ON LOWER SURFACE INSTEAD OF UPPER SURFACE, NO FILLER ON UPPER SURFACE INSTALLED AND NO RIVETS ON TRAILIN
- [SDR 07FDEA04037](https://openairdocs.org/sdr/07FDEA04037.md): Door Frame · damaged · Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Structure
  > DURING LT FWD PAX DOOR FRAMING AFT PANEL REPLACEMENT, A DOUBLE HOLE WAS PERFORMED AT FRAME 18, STRG 26 IN LOWER BEAM WEB AT ITS REAR END AND IN STRG 26 COUPLING. REPAIR PERFORMED BY CUT OUT OF LOWER BEAM WEB IAW EA 6-5312-81117 AND RAS/AS/0017/2005 ISSUE A.
- [SDR 07FDEA04036](https://openairdocs.org/sdr/07FDEA04036.md): Door Frame · damaged · Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Structure
  > DURING LT FWD PAX DOOR FRAMING AFT PANEL REPLACEMENT, A DOUBLE HOLE WAS PERFORMED AT FRAME 18, STRG 26 IN LOWER BEAM WEB AT ITS REAR END AND IN STRG 26 COUPLING. REPLACEMENT OF STRINGER 26 COUPLING BY NEW ONE IAW EA 6-5312-81117 AND RAS/AS/0017/2005 ISSUE A
- [SDR 07FDEA04034](https://openairdocs.org/sdr/07FDEA04034.md): Skin Panel · misrepaired · Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Plate/Skin
  > FOUND OLD DOUBLER REPAIR BETWEEN FRAME 11-11A, STRG 27-28 LT, NOT CONFORM TO REPAIR REFERENCE AS PER SRM 53-12-12/FIG 201. DOUBLER REPAIR RENEWED IAW SRM 53-12-12/FIG 201.
- [SDR 07FDEA04033](https://openairdocs.org/sdr/07FDEA04033.md): Rib · none · Sep 19, 2007 · N807FD · Airbus A310324 · Standard Practices/Structures
  > OLD REPAIR ON RT INBOARD FLAP AT END RIB 21. CUSTOMER DECISION TO FINAL REPAIR PER SB A310-57-2055, REPLACEMENT OF END RIB 21.
- [SDR 07FDEA04032](https://openairdocs.org/sdr/07FDEA04032.md): Rib · none · Sep 19, 2007 · N807FD · Airbus A310324 · Trailing Edge Flaps
  > OLD REPAIR ON LT INBOARD FLAP AT END RIB 21. CUSTOMER DECISION TO FINAL REPAIR PER SB A310-57-2055, REPLACEMENT OF END RIB 21.
- [SDR 07FDEA04029](https://openairdocs.org/sdr/07FDEA04029.md): Stringer · corroded · Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > DURING NON ROUTINE DR0115, FOUND CORROSION ON STRINGER 51 LT, BETWEEN FRAME 54.1-54.2. PARTIAL STRINGER REPLACEMENT WITH SPLICE REPAIR PERFORMED, BETWEEN FRAME 54.1-54.2 IAW SRM 53-10-14/FIG 201 AND 54.2-54.3 (DR0115).
- [SDR 07FDEA04026](https://openairdocs.org/sdr/07FDEA04026.md): Stringer Splice · corroded · Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > CORROSION ON CONNECTING SEGMENT STRG 51 LT, BETWEEN FRAME 54.2-54.3. REPLACEMENT OF CONNECTING SEGMENT IAW SRM 51-72-10.
- [SDR 07FDEA04024](https://openairdocs.org/sdr/07FDEA04024.md): Floorbeam · corroded · Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Floor Beam
  > HEAVY CORROSION ON CROSSBEAM AT FRAME 63 RT, CARGO COMP FLOOR STRUCTURE. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15.
- [SDR 07FDEA04022](https://openairdocs.org/sdr/07FDEA04022.md): Floor Support · corroded · Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > HEAVY CORROSION ON LONGITUDINAL PROFILE (LONGERON) BETWEEN FRAME 66-69 AD, BULK CARGO COMP FLOOR STRUCTURE. REPLACEMENT OF LONGERON IAW SRM 51-72-10.
- [SDR 07FDEA04021](https://openairdocs.org/sdr/07FDEA04021.md): Floorbeam · corroded · Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Floor Beam
  > HEAVY CORROSION ON CROSSBEAM AT FRAME 69 LT, BULK CARGO COMP FLOOR STRUCTURE. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15.
- [SDR 07FDEA04019](https://openairdocs.org/sdr/07FDEA04019.md): Frame · damaged · Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Frame
  > OLD REPAIR ON FRAME 13, STRG 14 LT, FUSELAGE NOSE SECTION. THE REINFORCEMENT REPAIR ANGLE AT FRAME SEGMENT WAS CHAFED AND AFTER REWORK OUT OF LIMIT. REPAIR PERFORMED BY INSTALLING NEW REPAIR ANGLE AT OLD REPAIR AS PER PRINCIPLE IN SRM 53-10-13.
- [SDR 07FDEA04015](https://openairdocs.org/sdr/07FDEA04015.md): Shear Plate · cracked · Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > CRACKED SHEAR PLATE AT STR 26 LT, BETWEEN FRAME 79-80. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10.
- [SDR 07FDEA04014](https://openairdocs.org/sdr/07FDEA04014.md): Stringer · corroded · Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 42 RT, BETWEEN FRAME 72-73. STRINGER SPLICE REPAIR IAW SRM 53-10-14/FIG 201.
- [SDR 07FDEA04013](https://openairdocs.org/sdr/07FDEA04013.md): Stringer · damaged · Sep 19, 2007 · N807FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > OLD DAMAGE ON STRINGER 30 RT, BETWEEN FRAME 54.2-54.3. STRINGER SPLICE REPAIR IAW SRM 53-10-14/FIG 201.

Next page: https://openairdocs.org/deregistered/N807FD-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 = 'N807FD' AND deregistration_id = 'N807FD-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N807FD-2024-03-02/reports

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