# Service difficulty reports: N805FD, cancelled Mar 2, 2024

A list on [N805FD, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N805FD-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 · 70 reports

- [SDR FDEA201609133211](https://openairdocs.org/sdr/FDEA201609133211.md): Slat · lack of lube · Sep 13, 2016 · N805FD · Airbus A310324 · Leading Edge Slat Control System
  > DURING APPROACH, SLATS WOULD NOT EXTEND, COMPLIED WITH PHASE 1, ECAM & QRH - SLATS CONFIRMED STUCK. DID NO SLAT/FULL FLAP LANDING IAW QRH. CREW CALLED IN FIRETRUCKS FOR SAFETY PRECAUTION. ACCOMPLISHED SFCC 1 AND 2 BITE TEST IAW AMM TSM 27-80-00 FOUND SFCC
- [SDR FDEA201606131980](https://openairdocs.org/sdr/FDEA201606131980.md): Computer · faulty · Jun 13, 2016 · N805FD · Airbus A310324 · Fuel Indicating System
  > APPROX 60 NM FROM DESTINATION, GOT FUEL ADV ON ECAM. LT OUTER 6K, LT INNER 11.0, CTR WAS 0, TRIM TANK WAS 0, RT INNER STARTED AT 11, THEN 10, THEN 9, THEN 8, ALL THE WAY TO ZERO. RIGHT WAS 4.0 AND DECREASING. DIVERTED. WITH T/O OF 57, FUEL USED COUNTER WAS
- [SDR FDEA201407191860](https://openairdocs.org/sdr/FDEA201407191860.md): Stringer · corroded · Jul 19, 2014 · N805FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER 46R FRAME 63 - 64 STRINGER CORRODED. REPAIRED THE STRINGER PER A310 SRM 53-10-14 PB201 FIG201H
- [SDR FDEA201207262710](https://openairdocs.org/sdr/FDEA201207262710.md): Engine · failed · Jul 26, 2012 · N805FD · Airbus A310324 · Engine (Turbine/Turboprop)
  > UPASSING 3000 ON T/O, FELT ABNORMAL VIBRATION WITH UNUSUAL NOISE. NOTICED N1 VIB AT 1.4 AND N2 VIB AT 2.4 ON ENG 1. WHILE TROUBLESHOOTING RECEIVED ENG 1 EPR MODE FAULT AND ATS LEVER KICKED OFF. NOTICED ENG 1 EGT GAUGE INOP AT "0". ENG 1 N1 BEGAN UNCOM
- [SDR FDEA201204051259](https://openairdocs.org/sdr/FDEA201204051259.md): Fuel Cell · leaking · Apr 5, 2012 · N805FD · Airbus A310324 · Fuel Storage
  > LEFT WING INNER TANK LOWER SURFACE 1 EA BOLT FUEL SEEPING NEAR REAR SPAR RIB 8 POSITION. USED OPTIONAL INSP METHOD WITH HIGH LEVEL FUEL SENSING. TORQUED NUT WITH APPLICABLE VALUE CLEAN UP THE FASTENERS AND RESEALANT ON THE NUT IAW SRM 51-49-00. APPLIED NEW
- [SDR FDEA201204051258](https://openairdocs.org/sdr/FDEA201204051258.md): Fuel Cell · leaking · Apr 5, 2012 · N805FD · Airbus A310324 · Fuel Storage
  > RIGHT OUTER TANK REAR SPAR, FUEL SEEPING AT NR 6 SPOILER BLOCK VALVE SUPPORT FITTING LWR RT FITTING FASTENERS. USED OPTIONAL INSPECTION METHOD WITH HIGH LEVEL FUEL SENSING. TORQUED NUT WITH APPLICABLE VALUE CLEAN UP THE FASTENERS AND SEALANT ON THE NUT IAW SR
- [SDR FDEA201203190997](https://openairdocs.org/sdr/FDEA201203190997.md): Floor Support · corroded · Mar 19, 2012 · N805FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > FWD MAIN DECK, COURIER FLOOR AREA, FOUND FLOOR SUPPORT CORRODED LOCATION FROM FR 11 TO 13A AND Y-724. R & R THE FLOOR SUPPORT IAW SRM 51-72-10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201203160965](https://openairdocs.org/sdr/FDEA201203160965.md): Floor Panel · damaged · Mar 16, 2012 · N805FD · Airbus A310324 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 241NK DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201203130909](https://openairdocs.org/sdr/FDEA201203130909.md): Skin · dented · Mar 13, 2012 · N805FD · Airbus A310324 · Fuselage Main, Plate/Skin
  > NOSE SECTION RT LOWER HALF SKIN PLATE EXTERNAL GOT A DENT JUST BELOW COCKPIT FLOOR LEVEL LOCATION BETWEEN FR 2 AND FR 3 POSITION.
- [SDR FDEA201109264124](https://openairdocs.org/sdr/FDEA201109264124.md): Skin · scratched · Sep 26, 2011 · N805FD · Airbus A310324 · Trailing Edge Flaps
  > LEFT WING OTBD FLAP UPPER SURFACE NEAR FLAP TRACK NR 3, FOUND SURFACE WITH 8" SCRATCH MARK UNDER RUBSTRIP. REPLACED THE O/B FLAP PER AMM 27-50-12-04-0
- [SDR FDEA201106122214](https://openairdocs.org/sdr/FDEA201106122214.md): Thrust Reverser · malfunctioned · Jun 12, 2011 · N805FD · Airbus A310324 · Engine Thrust Reverser
  > AT APPRX 70KTS, NR 2 THRUST REVERSER UNLOCK AMBER LIGHT ON. REJECTED T/O, AFTER STOWING THRUST REVERSER, LIGHT OUT. REVERSER APPEARED TO OPERATE NORMAL. RELEASED FOR SERVICE PER MEL. PERFORMED TROUBLESHOOTING AS PER AMM 78-30-00-02. CARRIED OUT RIGGING
- [SDR FDEA201007082423](https://openairdocs.org/sdr/FDEA201007082423.md): Priority Valve · failed · Jul 8, 2010 · N805FD · Airbus A310324 · Hydraulic System, Main
  > ON START OF T/O ROLL, RECEIVED ECAM FOR BLUE RSVR LO LEVEL, BLUE RSVR INDICATES EMPTY. TURNED OFF BLUE HYD ENG PUMP APPROX, 2 MINUTES AFTER ECAM ALERT. T/S AND FOUND ACTUALLEY BLUE RSVR HYD QTY INDICATED 1.5 G/L AND BLUE HYD MANIFOLD PRIORITY VALVE BROKEN.
- [SDR FDEA201001130093](https://openairdocs.org/sdr/FDEA201001130093.md): Stringer · misrepaired · Jan 13, 2010 · N805FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > PREVIOUS STR REPAIR LOCATED IN AFT CABIN UNDER FLOOR BEHIND BULK CARGO ON STR 51 LT BETWEEN FRAMES 72 TO 74 HAS 2 EACH REPAIR ANGLES AND 1 EACH STR REPAIR SECTION. PREVIOUSLY INSTALLED REPAIR LOCATED IN AFT CABIN UNDER FLOOR BEHIND BULK CARGO ON STR 51 LT BET
- [SDR FDEA201001110078](https://openairdocs.org/sdr/FDEA201001110078.md): Fairing · sheared · Jan 11, 2010 · N805FD · Airbus A310324 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON FAIRING 485AL INBD AFT SECTION MOUNTING RIVETS SHEARED NOT GOING THROUGH REINFORCING STRINGER REMOVED REINFORCING ANGLE. REPAIRED SKIN USING SPLICING METHOD IAW EA 6-5480-137727. REPLACED REINFORCING ANGLE IAW SRM 51-72-10.
- [SDR FDEA200912294540](https://openairdocs.org/sdr/FDEA200912294540.md): Skin · dented · Dec 29, 2009 · N805FD · Airbus A310324 · Fuselage Main, Plate/Skin
  > LT SIDE LWR FUSELAGE SKIN AT FRAME 67 STR 50L DENT MEASURING 12 INCHES X 1 INCH X.188 DEEP. REPAIRED SKIN PN A53974208200 AT FRAME 67 BETWEEN STRINGERS 49L AND 50L USING DOUBLER AND FILLER IAW SRM 53-10-12 FIG. 225 PAGES 357 THROUGH 366.
- [SDR FDEA200912234512](https://openairdocs.org/sdr/FDEA200912234512.md): Stringer · misrepaired · Dec 23, 2009 · N805FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > PREVIOUS STRINGER REPAIR LOCATED IN FWD CARGO ON STRINGER 36 LT BETWEEN FRAMES 20 TO 22 HAS 1 EACH REPAIR SPLICE MEASURING 7.2" LONG AND 1 EACH STRINGER REPAIR SPLICE MEASURING 24.3" LONG. PREVIOUSLY INSTALLED REPAIR LOCATED AT FWD CARGO ON STRINGER 36 LT BETW
- [SDR FDEA200808263598](https://openairdocs.org/sdr/FDEA200808263598.md): Computer · failed · Aug 26, 2008 · N805FD · Airbus A310324 · Leading Edge Slat Control System
  > DURING APPROACH WITH THE LANDING GEAR DOWN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT LIGHTS ON O/H. DISCONTINUED AP AND FOLLOWED QRH. WHEN THE SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGUR
- [SDR FDEA200808263597](https://openairdocs.org/sdr/FDEA200808263597.md): Computer · malfunctioned · Aug 26, 2008 · N805FD · Airbus A310324 · Leading Edge Slat Control System
  > DURING APPROACH WITH THE LDG GEAR DN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT LIGHTS ON O/H. DISCONTINUED AP AND FOLLOWED QRH. WHEN THE SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGURED AGAIN
- [SDR FDEA200808263602](https://openairdocs.org/sdr/FDEA200808263602.md): Limiter · failed · Aug 26, 2008 · N805FD · Airbus A310324 · Leading Edge Slat Control System
  > DURING APPROACH WITH LANDING GEAR DOWN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT O/H. SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGURED AGAIN THE SLATS STUCK AT 15 DEGREES. FOLLOWED QRH FOR
- [SDR 08FDEA03602](https://openairdocs.org/sdr/08FDEA03602.md): Limiter · malfunctioned · Aug 26, 2008 · N805FD · Airbus A310324 · Leading Edge Slat Control System
  > DURING APPROACH WITH LANDING GEAR DOWN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT O/H. SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGURED AGAIN THE SLATS STUCK AT 15 DEGREES. FOLLOWED QRH FOR
- [SDR 08FDEA03598](https://openairdocs.org/sdr/08FDEA03598.md): Slat System · failed · Aug 26, 2008 · N805FD · Airbus A310324 · Leading Edge Slat Control System
  > DURING APPROACH WITH THE LDG GEAR DN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT LIGHTS ON O/H. DISCONTINUED AP AND FOLLOWED QRH. WHEN THE SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGURED AGA
- [SDR 08FDEA03597](https://openairdocs.org/sdr/08FDEA03597.md): Slat System · malfunctioned · Aug 26, 2008 · N805FD · Airbus A310324 · Leading Edge Slat Control System
  > DURING APPROACH WITH THE LDG GEAR DN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT LIGHTS ON O/H. DISCONTINUED AP AND FOLLOWED QRH. WHEN THE SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGURED AGA
- [SDR FDEA200807122844](https://openairdocs.org/sdr/FDEA200807122844.md): Jackscrew · leaking · Jul 12, 2008 · N805FD · Airbus A310324 · Leading Edge Slat Control System
  > SLATS STUCK AT 0 DEG, C/W QRH. EMERGENCY DECLARED, LANDED UNEVENTFULLY AT SYR. REMOVED AND REPLACED RIGHT NR 2 JACKSCREW ASSY PER A310-300MM ATA 27-84-22-4.
- [SDR 08FDEA02844](https://openairdocs.org/sdr/08FDEA02844.md): Jackscrew · stuck · Jul 12, 2008 · N805FD · Airbus A310324 · Leading Edge Slat Control System
  > SLATS STUCK AT O DEG, C/W QRH, EMERGENCY DECLARED, LANDED UNEVENTFULLY AT SYR. REMOVED AND REPLACED RIGHT NR 2 JACKSCREW ASSY PER A310-300MM ATA 27-84-22-4.
- [SDR 07FDEA05026](https://openairdocs.org/sdr/07FDEA05026.md): Stringer · corroded · Dec 11, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > FWD PIT BETWEEN FR 39 AND FR 38.2 STGR 53 LT HAS CORROSION REMOVED CORROSION FOUND TO BE OUT OF LIMIT IAW SRM 53-10-14. FAB`D STRINGER DOUBLER IN T7/711755. REMOVED AND REPLACED STRG DOUBLER AND COUPLING IAW 51-40-44.
- [SDR 07FDEA04854](https://openairdocs.org/sdr/07FDEA04854.md): Stringer · corroded · Nov 19, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BETWEEN FR 38.1 AND FR 38.2 STGR 48 RT HAS CORROSION. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-14. CUT OUT DAMAGE AREA STR 48 RT FR 37-38.1 IAW SRM 53-10-14. REMOVED SHEAR TIE TR 37 STR 47 RT. FAB STRINGER DOUBLER IAW MAE TRAVE
- [SDR 07FDEA04488](https://openairdocs.org/sdr/07FDEA04488.md): Skin · corroded · Oct 4, 2007 · N805FD · Airbus A310324 · Fuselage Main, Plate/Skin
  > FOUND CORROSION AT WEDGE C 70, P56-57 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04485](https://openairdocs.org/sdr/07FDEA04485.md): Stringer · corroded · Oct 4, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION AT STRINGER SEGMENT C 65, P 54 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04483](https://openairdocs.org/sdr/07FDEA04483.md): Stringer · corroded · Oct 4, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION AT STRINGER SEGMENT P48, C 68-69 AND C 70-71. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04451](https://openairdocs.org/sdr/07FDEA04451.md): Skin · dented · Oct 2, 2007 · N805FD · Airbus A310324 · Leading Edge Devices
  > FOUND DENT AT SLAT NR 2 LT OUT OF LIMIT. NOSE SKIN REPAIR PERFORMED IAW SRM 57-43-11 FIG 202.
- [SDR 07FDEA04446](https://openairdocs.org/sdr/07FDEA04446.md): Lug · corroded · Oct 2, 2007 · N805FD · Airbus A310324 · Wing, Attach Fittings
  > FOUND CORROSION ONE BEARING BORE OF RT WING PYLON OUTBOARD MOUNTING LUG REPAIR PERFORMED BY BLEND OUT CORROSION, NDT FOR DAMAGE FREE IAW EA 6-5720- 81124 AND RAS/BAE/1000347/2005 ISS A.
- [SDR 07FDEA04467](https://openairdocs.org/sdr/07FDEA04467.md): Stringer · corroded · Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION AT STRINGER SEGMENT P 56, C55/58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04466](https://openairdocs.org/sdr/07FDEA04466.md): Stringer · corroded · Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION AT STRINGER P 48 LT, C 69-70 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04465](https://openairdocs.org/sdr/07FDEA04465.md): Fitting · corroded · Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT CORNER FITTING P 44 LT, C64 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04464](https://openairdocs.org/sdr/07FDEA04464.md): Frame · damaged · Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Frame
  > FOUND ENLARGED HOLES AT C 26/32 BETWEEN P 13-22 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04463](https://openairdocs.org/sdr/07FDEA04463.md): Fitting · corroded · Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT CORNER FITTING C 33 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04462](https://openairdocs.org/sdr/07FDEA04462.md): Channel · dented · Oct 2, 2007 · N805FD · Airbus A310324 · Passenger/Crew Doors
  > LT AFT CREW DOOR LOWER CHANNEL HAS A NOTCH OUT OF LIMIT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04461](https://openairdocs.org/sdr/07FDEA04461.md): Stringer · corroded · Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION AT STRINGER SEGMENT P 56 LT, C 80 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04460](https://openairdocs.org/sdr/07FDEA04460.md): Skin · misrepaired · Oct 2, 2007 · N805FD · Airbus A310324 · Trailing Edge Flaps
  > FOUND OLD POCKET REPAIRS AT RIB 21 INBOARD FLAP LT NOT CONFORM TO SRM. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SB 57-2055.
- [SDR 07FDEA04459](https://openairdocs.org/sdr/07FDEA04459.md): Stringer · corroded · Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION AT STRINGER SEGMENT C 72, P 48 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04458](https://openairdocs.org/sdr/07FDEA04458.md): Stringer · corroded · Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Longeron/Stringer
  > FOUND CORROSION AT STRINGER SEGMENT C 72, 45 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04457](https://openairdocs.org/sdr/07FDEA04457.md): Flange · corroded · Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Miscellaneous Structure
  > FOUND FLANGE C61-62, AD CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04456](https://openairdocs.org/sdr/07FDEA04456.md): Fitting · corroded · Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Attach Fittings
  > FOUND CORROSION AT RUN OUT FITTING P44 LT/RT, C17 REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R536-10440.
- [SDR 07FDEA04455](https://openairdocs.org/sdr/07FDEA04455.md): Fitting · corroded · Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage Main, Attach Fittings
  > FOUND FITTING AT C13-13A, P26 LT CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04454](https://openairdocs.org/sdr/07FDEA04454.md): Seat Track · corroded · Oct 2, 2007 · N805FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND SEAT TRACK C 15A-19, Y-953 CORRODED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.
- [SDR 07FDEA04453](https://openairdocs.org/sdr/07FDEA04453.md): Skin Panel · corroded · Oct 2, 2007 · N805FD · Airbus A310324 · Wing, Plate/Skin
  > FOUND CORROSION AT CENTER TANK TOP SKIN C 44-48, TRACK 3-5, LT/RT REPAIR PERFORMED BY REMOVAL OF CORROSION AND INSTALLING OF TWO DOUBLERS IAW DRAWING R573-10011 AT BEAM 4 AND 6, C 44-2 AND C 44 LT/RT IAW EA 6-5710-81129 AND RAS/AS/0036/2005 ISS A.
- [SDR 07FDEA04452](https://openairdocs.org/sdr/07FDEA04452.md): Rib · damaged · Oct 2, 2007 · N805FD · Airbus A310324 · Trailing Edge Flaps
  > FOUND OLD REPAIRS ON INBOARD FLAP RIB 21 (POCKET REPAIRS) NOT CONFORM TO SRM REPAIR PERFORMED BY REPLACEMENT OF END RIB 21 IAW SRM 57-2055.
- [SDR 07FDEA04450](https://openairdocs.org/sdr/07FDEA04450.md): Skin · worn · Oct 2, 2007 · N805FD · Airbus A310324 · Wing, Plate/Skin
  > FOUND ON RT WING ON PYLON NR 2 ELONGATED HOLE AT WING TO PYLON BOTTOM SKIN ON AREA OF HYDRAULIC LINES. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-81128 AND RAS/BAE/100457/2005 ISS A.
- [SDR 07FDEA04449](https://openairdocs.org/sdr/07FDEA04449.md): Skin · worn · Oct 2, 2007 · N805FD · Airbus A310324 · Wing, Plate/Skin
  > FOUND ON LT WING ON PYLON NR 1 ELONGATED HOLE AT WING TO PYLON BOTTOM SKIN ON AREA OF HYDRAULIC LINES. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-81128 AND RAS/BAE/100457/2005 ISS A.
- [SDR 07FDEA04448](https://openairdocs.org/sdr/07FDEA04448.md): Skin · damaged · Oct 2, 2007 · N805FD · Airbus A310324 · Trailing Edge Flaps
  > RT INNER FLAP WITH SEVERAL DAMAGES, LIMITED TO 5 FLIGHTS IAW RAS/DABRE/7002673/2003. REPAIR PERFORMED IN WORKSHOP AND RELEASED IAW FAA FORM 8130-3 NR 05/1145.

Next page: https://openairdocs.org/deregistered/N805FD-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 = 'N805FD' AND deregistration_id = 'N805FD-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N805FD-2024-03-02/reports

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