# Service difficulty reports: N816FD, cancelled Feb 6, 2024

A list on [N816FD, cancelled Feb 6, 2024](https://openairdocs.org/deregistered/N816FD-2024-02-06.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 · 54 reports

- [SDR FDEA201312142981](https://openairdocs.org/sdr/FDEA201312142981.md): Jackscrew · lack of lube · Dec 14, 2013 · N816FD · Airbus A310304 · Trailing Edge Flap Control System
  > ON APPROACH, FLAPS DID NOT EXTEND. FLAPS SYS 1 & SYS 2 FAULT LIGHTS ILLUMINATED UPON MOVING FLAP HANDLE TO ANY EXTENDED POSITION. ALTITUDE 6200 FEET AT KGTF, TEMP -5C. RELIEVED LOAD ON LT FLAPS THEN RESET LT FLAP TO LIMITER. RT LIMITER OK IAW A310-300 AMM
- [SDR FDEA201304100772](https://openairdocs.org/sdr/FDEA201304100772.md): Door · damaged · Apr 10, 2013 · N816FD · Airbus A310304 · Landing Gear Doors
  > EXTENDING LANDING GEAR, RECEIVED ECAM WARNING THAT NLG DOOR WAS NOT CLOSED. BOTH PANELS SHOWED DOOR. FOLLOWED QRH LANDED UNEVENTFULLY. AFTER TAXING IN NOSE GEAR DOOR LIGHT EXTINGUISHED. FOUND AFT HINGE FITTING FOR RT AFT NOSE GEAR DOOR DAMAGED. REMOVED RT
- [SDR FDEA201112155280](https://openairdocs.org/sdr/FDEA201112155280.md): Fuel Cell · leaking · Dec 15, 2011 · N816FD · Airbus A310304 · Fuel Storage
  > RT WING BOTTOM SKIN HAD FUEL SEEPAGE AT SLAT TRACK NR9 CANISTER DRAIN PORT FASTENER. REMOVED AND CLEANED THE DAMAGED SEALANT AREA. RE-APPLIED NEW SEALANT FOR REPAIRING IAW EO 6-5710-7-3304 PT3 AND EA 6-5710-149029 (FOR REPAIR OF FUEL TANK SEALING). THE REPAIR
- [SDR FDEA201112155276](https://openairdocs.org/sdr/FDEA201112155276.md): Fuel Cell · leaking · Dec 15, 2011 · N816FD · Airbus A310304 · Fuel Storage
  > RT WING FRONT SPAR HAD FUEL SEEPAGE AT RIB 18. REMOVED AND CLEANED THE DAMAGED SEALANT AREA. RE-APPLIED NEW SEALANT FOR REPAIRING IAW EO 6-5710-7-3304, PT3 AND EA 6-5710-149029. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
- [SDR FDEA201112155274](https://openairdocs.org/sdr/FDEA201112155274.md): Canister · leaking · Dec 15, 2011 · N816FD · Airbus A310304 · Fuel Storage
  > RT WING SLAT JACKSCREW NR 3 CANISTER DRAIN PORT HAD FUEL SEEPAGE IAW EA 6-5710-149029. REMOVED FUEL PANEL 540BB, 540CB IAW AMM 28-11-22. RE-SEALED SCREWJACK CANISTER IAW EO 6-5710-7-3304C PT1. RE-INSTALLED FUEL PNL 540BB, 540CB IAW AMM 28-11-22. LEAK CH
- [SDR FDEA201112025116](https://openairdocs.org/sdr/FDEA201112025116.md): Skin · dented · Dec 2, 2011 · N816FD · Airbus A310304 · Trailing Edge Flaps
  > RT WING T/E OTBD FLAP UPPER SURFACE DENTED. REPAIRED IAW SRM 57-53-12 FIG 210. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201112025115](https://openairdocs.org/sdr/FDEA201112025115.md): Door · gouged · Dec 2, 2011 · N816FD · Airbus A310304 · Fixed Inner Doors
  > FOUND CREW DOOR GOUGED. REPAIRED IAW EA 6-52-50-149021 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.
- [SDR FDEA201111295067](https://openairdocs.org/sdr/FDEA201111295067.md): Fitting · cracked · Nov 29, 2011 · N816FD · Airbus A310304 · Fuselage Miscellaneous Structure
  > LEFT NOSE SECTION/ FR 12A STIFFENER FITTING WAS FOUND 1 EA CRACK ABOUT.7500" IN LENGTH. ON ZONE B,J AREA IAW NTM 51-10-08, PART 1. REMOVED STIFFENER FITTING AND JUNCTION FITTING. INSTALLED STIFFENER FITTING AND JUNCTION FITTING WITH NEW PART REFER TO EO 6
- [SDR FDEA201111224994](https://openairdocs.org/sdr/FDEA201111224994.md): Floor Panel · damaged · Nov 22, 2011 · N816FD · Airbus A310304 · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOOR PANEL 162AF HAS EDGE IMPACT DAMAGED. FOUND OUT OF LIMITS. REPLACED THE FLOOR PANEL BY FABRICATION OF A NEW PANEL WITH ADHESIVE AND INSERTS IAW SRM 53-10-20 & DWG A53279966. REPAIR MINOR PER GMM 6-2-100.
- [SDR FDEA201110154538](https://openairdocs.org/sdr/FDEA201110154538.md): Power Supply · no test · Oct 15, 2011 · N816FD · Airbus A310304 · Emergency Lighting
  > EMERGENCY LIGHTS WOULD NOT TEST PROPERLY. R & R EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW MM 33-51-14-04-09. OK FOR SERVICE.
- [SDR FDEA200907022465](https://openairdocs.org/sdr/FDEA200907022465.md): Skin · dented · Jul 2, 2009 · N816FD · Airbus A310 · Fuselage Main, Plate/Skin
  > ON WALK AROUND FOUND DENT ON LOWER FUSELAGEAFT OF RADOME BETWEEN FRAME O AND FRAME 1 CUT OUT DAMAGED AREA IAW A310 SRM 53-11-12 FIG. 201. INSTALLED PERMANENT REPAIR IAW A310 SRM 53-11-12 FIG. 201. BETWEEN FRAME 0 AND FRAME 1 AT FUSELAGE LOWER CENTERLINE
- [SDR FDEA200907022464](https://openairdocs.org/sdr/FDEA200907022464.md): Skin · damaged · Jul 2, 2009 · N816FD · Airbus A310304 · Passenger/Crew Doors
  > LOWER AFT CORNER OF L - 1 DOOR HAS 3/16 INCH ARC CUT OUT DAMAGED AREA AND INSTALLED REPAIR OF OUTER SKIN IN CORNER AREA OF L-1 DOOR LOWER AFT CORNER,FR 17, STRINGER 25 LT IAW A310 SRM 52-11-00,FIG 206,PAGE 239/240
- [SDR 08FDEA01298](https://openairdocs.org/sdr/08FDEA01298.md): Outflow Valve · failed · Apr 4, 2008 · N816FD · Airbus A310304 · Pressure Regulator/Outflow Valve
  > UPON CLIMB-OUT CABIN VERTICAL SPEED EXCEEDED 2000FPM, AT 15000 ALT CAB ALT EXCEEDED 10,000. OUTBOARD EXTRACT VALVE FAULTED, UNABLE TO MANUALLY CONTROL CABIN PRESS. REACTIVATED SYSTEM. FAILED OPS CHECKED AS PER AMM 21-23-00-5, VALVE NEVER MOVED. T/S AS PER WD
- [SDR 07FDEA02834](https://openairdocs.org/sdr/07FDEA02834.md): Unknown · odor · Aug 12, 2007 · N816FD · Airbus A310304 · Air Distribution System
  > AFTER LIFT-OFF ACRID SMOKE ODOR AND EYES HAD BURNING SENSATION. LEVEL OFF AT 10,000 FT. NO CLEARING. OPENED RAM AIR ON DESCENT TO CLEAR AIR. SHUT OFF NR 2 PACK AS IT HAD A HIGH TEMP 55 DEG C. NO OTHER WARNINGS. REPLACED CHECK VALVES 291394,293388,291388
- [SDR 07FDEA02911](https://openairdocs.org/sdr/07FDEA02911.md): B-Nut · leaking · Aug 9, 2007 · N816FD · Airbus A310304 · Hydraulic System, Main
  > AFTER ENGINE START CREW REPORTED SMOKE IN THE COCKPIT COMING FROM THE CASPER VENTS. FOUND HYDRAULIC RETURN LINE B NUT LEAKING AT PYLON ON NR 1 ENGINE. SECURED AND OPERATED ENGINE WITH NO LEAKS REMOVED AND REPLACED NR 1 PACK COALESCER BAG PER MM 21-51-16-3.
- [SDR 07FDEA01311](https://openairdocs.org/sdr/07FDEA01311.md): Frame · cracked · Apr 4, 2007 · N816FD · Airbus A310304 · Fuselage Main, Frame
  > DEVIATION TO EO 6-5310-7-5020-SB A310-53-2124- AD 2006-020-06, CRACKS IN FRAME FEET C43, C46 RT REPAIR PERFORMED BY REMOVING THE CRACKS THRU OVERSIZING IAW EA 6-5315-106424 AND RAS 049395/047/2007 ISS. A
- [SDR 07FDEA01310](https://openairdocs.org/sdr/07FDEA01310.md): Frame · cracked · Apr 4, 2007 · N816FD · Airbus A310304 · Fuselage Main, Frame
  > DEVIATION TO EO 6-5310-7-5020, SB A310-53-2124, AD 2006-02-06, CRACKS IN FRAME FEET, C45, C46 LT REPAIR PERFORMED BY CRACK REMOVING THRU OVERSIZING IAW EA 6-5315-106424 AND RAS 049395/047/2007 ISS A.
- [SDR 07FDEA01253](https://openairdocs.org/sdr/07FDEA01253.md): Rib · cracked · Apr 3, 2007 · N816FD · Airbus A310304 · Trailing Edge Flaps
  > FOUND OLD CRACK REPAIR ON INBOARD FLAP RT, RIB 21 (POCKET REPAIR). REPAIR WAS PERFORMED BY REPLACEMENT OF RIB 21 IAW SB A310-57-2055, APPROVED BY EA 6-5752-106443.
- [SDR 07FDEA01159](https://openairdocs.org/sdr/07FDEA01159.md): Fairing · cracked · Mar 28, 2007 · N816FD · Airbus A310304 · Wing Miscellaneous Structure
  > CRACKED SHIM PLATE AT INNER SIDE AFT AREA OF LT NR 3 FLAP TRACK FIXED FAIRING. REPAIR PERFORMED BY WET LAY-UP PER SRM 57-20-35 AND INSERT INSTALLATION, APPROVED BY EA 6-5720-106421 AND RAS/FOK/016/2007 ISS. A
- [SDR 07FDEA01158](https://openairdocs.org/sdr/07FDEA01158.md): Attach Fitting · corroded · Mar 28, 2007 · N816FD · Airbus A310304 · Nacelle/Pylon, Attach Fittings
  > FOUND CORROSION IN AFT PYLON ATTACH FITTING HOLE, PYLON NR 2, RIB 18 REPAIR PERFORMED WITH SB A31-52-2021, APPROVED BY EA 6-5450-106340.
- [SDR 07FDEA01157](https://openairdocs.org/sdr/07FDEA01157.md): Attach Fitting · corroded · Mar 28, 2007 · N816FD · Airbus A310304 · Nacelle/Pylon, Attach Fittings
  > CORROSION IN AFT PYLON ATTACH FITTING HOLE, PYLON NR 2, RIB 18 REPAIR PERFORMED WITH SB A31-52-2021, APPROVED BY EA 6-5450-106340.
- [SDR 07FDEA01129](https://openairdocs.org/sdr/07FDEA01129.md): Fairing · damaged · Mar 26, 2007 · N816FD · Airbus A310304 · Aerodynamic Fairings
  > REPAIR DAMAGE TO FAIRING 577EL REPAIR WAS PERFORMED BY WET LAY-UP REPAIR IAW EA 6-5317-106416 AND RAS/DAHAM/4021689/2007 ISS.A
- [SDR 07FDEA01128](https://openairdocs.org/sdr/07FDEA01128.md): Skin · damaged · Mar 26, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/Skin
  > OLD EXTERNAL DOUBLER REPAIR AT C38/38A, P44 RT REPAIR WAS PERFORMED IAW LHT SDR 0226/007536, APPROVED BY EA 6-5314-106414 AND RAS/DABRE/7005488/2005 ISS.A
- [SDR 07FDEA01111](https://openairdocs.org/sdr/07FDEA01111.md): Frame · cracked · Mar 23, 2007 · N816FD · Airbus A310304 · Fuselage Main, Frame
  > MILLED FRAME CRACKED, C22, P26, RHS REPAIR PERFORMED BY REPLACEMENT OF FITTING IAW EA 6-5313-106374 AND RAS/DABRE/7007381/2007 ISS. A.
- [SDR 07FDEA01110](https://openairdocs.org/sdr/07FDEA01110.md): Bulkhead · gouged · Mar 23, 2007 · N816FD · Airbus A310304 · Fuselage Main, Bulkhead
  > SOME GOUGES FOUND AT BULKHEAD 54, APPROX Y-953 AND Z-957, REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-106419 AND RAS 049380/2007 ISS. A
- [SDR 07FDEA01103](https://openairdocs.org/sdr/07FDEA01103.md): Skin Panel · gouged · Mar 23, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/Skin
  > TWO MISDRILLED HOLES THROUGH THE SKIN PANEL, INTERNAL DOUBLER, C17 FLANGE AND CONNECTING FITTINGS AT P44 LT. REPAIR PERFORMED BY REPLACING CONNECTING FITTINGS P44 BY NEW ONES; INSTALLING STEEL REPAIR BUSHES IN SKIN PANEL, INTERNAL DOUBLER C17 FLANGE AND C17 F
- [SDR 07FDEA01053](https://openairdocs.org/sdr/07FDEA01053.md): Frame · cracked · Mar 21, 2007 · N816FD · Airbus A310304 · Wing Spar
  > DEVIATIONS TO EO 6-5710-7-3322 (CRACKS IN HOLE 23 AND 62 LT). REPAIR PERFORMED BY OVERSIZING HOLE 23 AND 62 LT IAW EA 6-5710-106423 AND RAS/049817/013/2007 ISSUE "A".
- [SDR 07FDEA01052](https://openairdocs.org/sdr/07FDEA01052.md): Mount · chafed · Mar 21, 2007 · N816FD · Airbus A310304 · Nacelle/Pylon, Attach Fittings
  > OLD CHAFING MARK ON PYLON NR 1 FWD PYLON TO ENGINE MOUNT FITTING. REPAIR PERFORMED BY INSTALLATION OF AN PROTECTION ANGLE, APPROVED BY RAS 018876/027/2002 ISSUE "A" AND EA 6-5450-106441.
- [SDR 07FDEA01050](https://openairdocs.org/sdr/07FDEA01050.md): Fitting · damaged · Mar 21, 2007 · N816FD · Airbus A310304 · Fuselage Main, Attach Fittings
  > MISDRILLED HOLES IN C17 AT P44 LT. REPAIR WAS PERFORMED BY BUSHING REPAIR AND NEW FITTING INSTALLATION (P/N A536-10607-206-93, A536- 10607-207-93) IAW EA 6-5312-106418 AND RAS/AS/006/2007 ISSUE "A".
- [SDR 07FDEA01036](https://openairdocs.org/sdr/07FDEA01036.md): Skin · scratched · Mar 21, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/Skin
  > OLD SCRATCH REPAIR ON EXTERNAL SKIN BETWEEN C75/76, P27. REPAIR VERIFICATION, PERFORMED IAW SRM 53-18-12/FIG 102 EA FOR TRACKING: 6-5318-106413.
- [SDR 07FDEA00990](https://openairdocs.org/sdr/07FDEA00990.md): Skin · chafed · Mar 19, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/Skin
  > CHAFE MARKS ON C38.1, P14-15 LT SIDE. REPAIR WAS PERFORMED BY BLEND OUT IAW EA 6-5314-106417 AND RAS/DATLS/0003560/2007 ISS. B
- [SDR 07FDEA00989](https://openairdocs.org/sdr/07FDEA00989.md): Skin · damaged · Mar 19, 2007 · N816FD · Airbus A310304 · Fuselage Main, Plate/Skin
  > DOUBLE HOLE ON FUSELAGE SKIN AT C67, P35 RHS REPAIR WAS PERFORMED BY BUSH REPAIR IAW SRM 51-40-51, APPROVED BY EA 6-53176-106410 AND RAS/DAHAM/4021719/2007 ISS. A
- [SDR 07FDEA00987](https://openairdocs.org/sdr/07FDEA00987.md): Vane · damaged · Mar 19, 2007 · N816FD · Airbus A310304 · Trailing Edge Flaps
  > CHAFE MARK ON INBOARD FLAP VANE. REPAIR WAS PERFORMED.
- [SDR 07FDEA00955](https://openairdocs.org/sdr/07FDEA00955.md): Attach Fitting · damaged · Mar 16, 2007 · N816FD · Airbus A310304 · Vertical Stabilizer
  > V/S TAPERED ATTACH FITTINGS LT REAR, RT REAR AND RT CENTER BRONZE PLATING MISSING. PARTS REPLACED IAW AMM 55-30-11/401, P/N A555-72151-000-00 (1 EA.) AND P/N A555-72201-000- 00 (2 EA.)
- [SDR 07FDEA00954](https://openairdocs.org/sdr/07FDEA00954.md): Floor Support · corroded · Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Miscellaneous Structure
  > CORROSION AT MAIN DECK FLOOR STRUCTURE PARTS C74-75, P26 LT/RT, CONNECTING SECTION P/N A539-80458-200-90, P/N A539-80464-200-51 AND P/N A539-80464-201-00. PARTS REPLACED IAW SRM 51-72-10.
- [SDR 07FDEA00953](https://openairdocs.org/sdr/07FDEA00953.md): Floor Support · corroded · Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Miscellaneous Structure
  > FOUND CORROSION AT MAIN DECK FLOOR STRUCTURE PARTS C74-75, P26 LT/RT (CONNECTING SECTION P/N A539-80458-200-90, P/N A539-80464-200-51 AND P/N A539-80464-201-00). PARTS REPLACED IAW SRM 51-72-10.
- [SDR 07FDEA00952](https://openairdocs.org/sdr/07FDEA00952.md): Crossbeam · corroded · Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, Structure
  > FOUND CORRODED CROSSBEAM AT C67, Y-1070-1115. PART REPLACED IAW SRM 51-72-10.
- [SDR 07FDEA00951](https://openairdocs.org/sdr/07FDEA00951.md): Beam · damaged · Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, Structure
  > TWO LONGITUDINAL BEAMS BETWEEN C64-65, -Y 525 AND Y 805 WITH WRONG EXISTING HOLES. PARTS REPLACED IAW SRM 51-72-10.
- [SDR 07FDEA00948](https://openairdocs.org/sdr/07FDEA00948.md): Stiffener · damaged · Mar 16, 2007 · N816FD · Airbus A310304 · Wing Miscellaneous Structure
  > RT WING, SHROUD BOX F/S SPAR, DAMAGE BY MAIN BARREL PIN. REPAIR WAS RENEWED BY REPLACEMENT OF VERTICAL STIFFENER.
- [SDR 07FDEA00947](https://openairdocs.org/sdr/07FDEA00947.md): Skin · cracked · Mar 16, 2007 · N816FD · Airbus A310304 · Wing, Plate/Skin
  > RT WING BOTTOM SKIN PANEL NR 2, AFT OF REAR SPAR INBOARD OF RIB 11 CRACKED. REPAIR WAS PERFORMED IAW REPAIR DRAWING R572-49152-001 AND SB A310-57-2066 (DOUBLER INSTALLED).
- [SDR 07FDEA00946](https://openairdocs.org/sdr/07FDEA00946.md): Rib · chafed · Mar 16, 2007 · N816FD · Airbus A310304 · Wing, Rib/Bulkhead
  > KRUEGER BOX RT, DAMAGED REPAIR, ABRASION IN AN SUPPORT FLANGE OF RIB 2B. REPAIR WAS PERFORMED BY BLEND OUT.
- [SDR 07FDEA00945](https://openairdocs.org/sdr/07FDEA00945.md): Web · chafed · Mar 16, 2007 · N816FD · Airbus A310304 · Leading Edge Devices
  > CHAFING MARK AT BACK WALL OF KRUEGER FLAP CHAMBER. REPAIR WAS PERFORMED BY BLEND OUT AND REPROTECT.
- [SDR 07FDEA00944](https://openairdocs.org/sdr/07FDEA00944.md): Attach Fitting · chafed · Mar 16, 2007 · N816FD · Airbus A310304 · Wing, Nacelle/Pylon Attach Fittings
  > PYLON NR 2, CHAFING MARKS ON INBOARD SIDE OF PYLON-TO-ENGINE ATTACH FITTING. REPAIR WAS PERFORMED BY BLEND OUT AND RESTORE PROTECTION.
- [SDR 07FDEA00938](https://openairdocs.org/sdr/07FDEA00938.md): Longeron · bent · Mar 16, 2007 · N816FD · Airbus A310304 · APU Cowling/Containment
  > APU ACCESS DOOR LT/RT LOWER LONGERON, OLD BENT REPAIR. REPAIR WAS PERFORMED BY CUT OUT AND INSTALLATION OF NEW LONGERON SECTION.
- [SDR 07FDEA00936](https://openairdocs.org/sdr/07FDEA00936.md): Floorbeam · corroded · Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, Floor Beam
  > AFT CARGO COMP FLOORBEAM AT C63 LT, Y 445 CORRODED. REPAIR WAS PERFORMED IAW SRM 53-10-15/FIG 207 BY LHT SDR.
- [SDR 07FDEA00933](https://openairdocs.org/sdr/07FDEA00933.md): Stringer · chafed · Mar 16, 2007 · N816FD · Airbus A310304 · Fuselage Main, Longeron/Stringer
  > OLD CHAFING MARKS BETWEEN C44-45, P45 LT. REPAIR PERFORMED BY BLEND OUT IAW LHT SDR.
- [SDR 07FDEA00932](https://openairdocs.org/sdr/07FDEA00932.md): Skin · dented · Mar 16, 2007 · N816FD · Airbus A310304 · Cargo/Baggage Doors
  > OLD DENT REPAIR ON BULK CARGO DOOR OUTER SKIN BETWEEN BEAM 1-2 AND BEAM 4-5. REPAIR WAS PERFORMED BY INSTALLING EXTERNAL DOUBLER BETWEEN BEAM 4-5 AND BLEND OUT BETWEEN BEAM 1-2 IAW LHT SDR.
- [SDR 07FDEA00931](https://openairdocs.org/sdr/07FDEA00931.md): Skin · chafed · Mar 16, 2007 · N816FD · Airbus A310304 · Cargo/Baggage Doors
  > TWO OLD NICK/CHAFING MARKS AT THE INTERNAL SKIN OF FWD CARGO DOOR C20A-25A, LONGERON 4-5. REPAIR WAS PERFORMED BY INSTALLING A DOUBLER IAW LHT SDR.
- [SDR 07FDEA00930](https://openairdocs.org/sdr/07FDEA00930.md): Shaft · chafed · Mar 16, 2007 · N816FD · Airbus A310304 · Passenger/Crew Doors
  > OLD CHAFING MARK ON PAX DOOR NR 1 RT AT LOCKING CONTROL SHAFT. REPAIR WAS PERFORMED BY BLEND OUT IAW LHT SDR.
- [SDR 07FDEA00929](https://openairdocs.org/sdr/07FDEA00929.md): Skin · delaminated · Mar 16, 2007 · N816FD · Airbus A310304 · Landing Gear Doors
  > OLD REPAIR ON LT MLG DOOR, DELAMINATED SKIN. REPAIR WAS PERFORMED BY FILL OUT THE DELAMINATED AREA IAW LHT SDR.

Next page: https://openairdocs.org/deregistered/N816FD-2024-02-06/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 = 'N816FD' AND deregistration_id = 'N816FD-2024-02-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N816FD-2024-02-06/reports

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