# Service difficulty reports: N806FD, cancelled Mar 2, 2024 A list on [N806FD, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N806FD-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 · 65 reports - [SDR FDEA201401030016](https://openairdocs.org/sdr/FDEA201401030016.md): Sequence Valve · failed · Jan 3, 2014 · N806FD · Airbus A310324 · Landing Gear Retraction/Extension System > RIGHT MLG WOULD NOT GO DOWN. UTILIZED CRANK HANDLE & RT MLG LOWERED. RT MLG SEQUENCE VLV LOCKED UP & WOULD NOT MOVE. R & R RT MLG SEQUENCE VLV IAW AMM A310-300 32-31-37-04. OPERATIONS CHECK & LEAK CHECKED GOOD. - [SDR FDEA201312253039](https://openairdocs.org/sdr/FDEA201312253039.md): Sequence Valve · out of rig · Dec 25, 2013 · N806FD · Airbus A310324 · Landing Gear Retraction/Extension System > GEAR LEVER RAISED, RT MAIN GEAR DID NOT RETRACT. GREEN DOWN INDICATION, GEAR DOOR AMBER. PUT GEAR HANDLE BACK DOWN ALL INDICATIONS BACK TO NORMAL FOR DOWN & LOCKED. JACKED ACFT, SWUNG RT MAIN GEAR, GEAR DID NOT RETRACT. FOUND RT MAIN GEAR SEQUENCE VALVE - [SDR FDEA201206272374](https://openairdocs.org/sdr/FDEA201206272374.md): Actuator · faulted · Jun 27, 2012 · N806FD · Airbus A310324 · Fuel Controlling System > PRIOR TO THRUST SET FOR TAKEOFF, RECEIVED NR 1 ENGINE FADEC CHANNEL A FAULT AND FADEC CHANNEL B FAULT. REJECTED TAKEOFF AT 45-50 KNOTS. FOLLOWED QRH PROCEDURES. SHUTDOWN AND RESTARTED NR 1 ENGINE, ATTEMPTED TAKEOFF AND RECEIVED SAME FAULTS AT SLIGHTLY HI - [SDR FDEA201205041733](https://openairdocs.org/sdr/FDEA201205041733.md): Skin · cracked · May 4, 2012 · N806FD · Airbus A310324 · Nacelle/Pylon, Plate/Skin > NR 1 ENGINE PYLON LT SIDE LOWER SKIN PANEL CRACKED POSITION NEAR AFT ENGINE MOUNT. REPAIRED IAW SRM 51-40-21 AND SRM 54-56-10 C2. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. - [SDR FDEA201205041732](https://openairdocs.org/sdr/FDEA201205041732.md): Skin · cracked · May 4, 2012 · N806FD · Airbus A310324 · Nacelle/Pylon, Plate/Skin > NR 1 ENGINE PYLON RT SIDE LOWER SKIN PANEL CRACKED POSITION NEAR AFT ENGINE MOUNT. REPAIRED IAW SRM 51-40-21 AND SRM 54-56-10 C2. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100. - [SDR FDEA201205011687](https://openairdocs.org/sdr/FDEA201205011687.md): Skin · cracked · May 1, 2012 · N806FD · Airbus A310324 · Wing, Plate/Skin > ONE CRACK FOUND, LENGTH 13MM AT RT WING BOTTOM SKIN LANDING PLATE AREA. REPAIRED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. - [SDR FDEA201204271627](https://openairdocs.org/sdr/FDEA201204271627.md): Floor Support · corroded · Apr 27, 2012 · N806FD · Airbus A310324 · Fuselage Miscellaneous Structure > FWD MAIN DECK COURIER FLOOR AREA FOUND FLOOR SUPPORT CORROSION LOCATION FROM FR 11 TO FR 13A AND Y-724. R & R FLOOR SUPPORT WITH NEW IAW SRM 51-72-10. THE REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR. - [SDR FDEA201204181477](https://openairdocs.org/sdr/FDEA201204181477.md): Floor Panel · damaged · Apr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor Panel > AVIONICS BAY FLOOR PANEL 122PF HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-27- 04. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 12 A53210216. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL IAW AMM 53-10- - [SDR FDEA201204181476](https://openairdocs.org/sdr/FDEA201204181476.md): Floor Panel · damaged · Apr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor Panel > BULK CARGO BAY FLOOR PANEL 162HF HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 17 A53279962. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL IAW AMM 53-10-35 - [SDR FDEA201204181475](https://openairdocs.org/sdr/FDEA201204181475.md): Floor Panel · damaged · Apr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor Panel > BULK CARGO BAY FLOOR PANEL 161JF HAS IMPACT DAMAGED. REMOVED FLOOR PANEL IAW AMM 53-10-35- 04. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20 AND DWG 17 A53279960. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL TO NORMAL CO - [SDR FDEA201204181474](https://openairdocs.org/sdr/FDEA201204181474.md): Floor Panel · damaged · Apr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor Panel > AFT CARGO COMPARTMENT FOUND FLOOR PANEL 151AF HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-33- 04. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 10 A25772831. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL - [SDR FDEA201204181473](https://openairdocs.org/sdr/FDEA201204181473.md): Floor Panel · damaged · Apr 18, 2012 · N806FD · Airbus A310324 · Fuselage Floor Panel > FWD CARGO BAY FLOOR PANEL 132RF HAS IMPACT DAMAGED. REMOVED FLOOR PANEL, FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG A53272792. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR. INSTALLED FLOOR PANEL TO NORMAL CONDITION IAW AMM 53-10-29- - [SDR FDEA201105171851](https://openairdocs.org/sdr/FDEA201105171851.md): Transmitter · leaking · May 17, 2011 · N806FD · Airbus A310324 · Hydraulic Indicating System > LOST YELLOW SYS HYD ENROUTE. COMPLIED WITH ECAM & QRH. HYD FLUID LEAKING FROM YELLOW HYD SYS PRESSURE TRANSMITTER 16WV HSG CAP & CGO DOOR HYD SELECTOR VALVE 10MJ THE CONTROL SHAFT. R & I 16WV & 10MJ ASSY, REPLENISH YELLOW HYD RESERVOIR & LEAK CHECKED OK, - [SDR FDEA201007062366](https://openairdocs.org/sdr/FDEA201007062366.md): Skin · misrepaired · Jul 6, 2010 · N806FD · Airbus A310324 · Fuselage Main, Plate/Skin > AN EXISTING FUSELAGE SKIN REPAIR IS AT FR52-53, BELOW STRINGER 18L. THERE ARE 5 ROWS OF 11 RIVETS ATTACHING THE SKIN (A53870003220) TO THE PLATE (A53870004218). THERE IS NO CUTOUT OR DOUBLER. IAW EA 6-5330-141519, REMOVED RIVETS IAW SRM 51-40-21 AND ROTO-TES - [SDR 08FDEA00830](https://openairdocs.org/sdr/08FDEA00830.md): Seat Track · damaged · Mar 10, 2008 · N806FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO FLOOR SEAT TRACK NR 1 RT SIDE, FR 61 HAS DAMAGE ON LOWER SURFACE,.545 IN ROUND BY.045 IN DEEP. REMOVED DAMAGED SEAT TRACK SECTION FROM FR 60.5 TO FR 61.5 AND REPAIRED IAW A310 SRM 53-10-16,FIG 208 - [SDR 07FDEA04991](https://openairdocs.org/sdr/07FDEA04991.md): Windshield · cracked · Dec 4, 2007 · N806FD · Airbus A310324 · Flight Compartment Windows > A/C HAS DIVERTED INTO CUN DUE F/O WINDSHIELD HAS SHATTERED. REMOVED AND REPLACED F/O WINDSHIELD A310-300 M/M 56-11-11-4, OPN CHECK IS GOOD. OK FOR SVC. REPLACED WINDSHIELD TEMP REGULATOR AS A PRECAUTION AMM 30-42-11-4 REPLACED WINDOW HEAT PROTECTION CON - [SDR 07FDEA04407](https://openairdocs.org/sdr/07FDEA04407.md): Skin Panel · damaged · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/Skin > FOUND DURING P TO F CONVERSION A CUT (10MM) AT SKIN PANEL C 35, P 35 LT REPAIR PERFORMED BY CUT OUT THE SKIN AND INSTALLING A FLUSH REPAIR WITH NEW STRAP AND COUPLING IAW EA 6-5314-82877 AND RAS/DABRE/7005190/2005 ISS A. - [SDR 07FDEA04406](https://openairdocs.org/sdr/07FDEA04406.md): Fitting · chafed · Oct 1, 2007 · N806FD · Airbus A310324 · Nacelle/Pylon, Attach Fittings > FOUND CHAFING MARKS AT PYLON TO WING FITTING RIB 18, PYLON NR 2 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04405](https://openairdocs.org/sdr/07FDEA04405.md): Skin Panel · dented · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/Skin > FOUND NICK ON SKIN PANEL NR 3 C 18-19, P 33 RT REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5313-82859 AND RAS/DABRE/7005143/2005 ISS A. - [SDR 07FDEA04404](https://openairdocs.org/sdr/07FDEA04404.md): Skin · delaminated · Oct 1, 2007 · N806FD · Airbus A310324 · Rudder, Plate/Skin > FOUND AT RUDDER TRAILING EDGE LOWER CORNER DELAMINTION NEAR RIB 0 REPAIR PERFORMED IAW SRM 55-41-12 FIG 208A. - [SDR 07FDEA04403](https://openairdocs.org/sdr/07FDEA04403.md): Fitting · damaged · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Attach Fittings > FOUND MISDRILLED HOLES IN CORNER FITTING C59, P 44 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04402](https://openairdocs.org/sdr/07FDEA04402.md): Doubler · corroded · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/Skin > FOUND CORROSION AT DOUBLER C71-72, P 47-48 LT REPAIR PERFORMED BYREWORK OF CORROSION, NDT FOR CRACK FREE AND FLAP PEENING IAW EA 6-5317-82856 AND RAS/DATLS/0002522/2005 ISS B. - [SDR 07FDEA04401](https://openairdocs.org/sdr/07FDEA04401.md): Stringer · corroded · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND CORROSION AT STRINGER P52 LT, C70-71. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. - [SDR 07FDEA04400](https://openairdocs.org/sdr/07FDEA04400.md): Fitting · cracked · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Attach Fittings > FITTING AT P 48, C78 LT CRACKED (ABOUT 8MM). REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04399](https://openairdocs.org/sdr/07FDEA04399.md): Fitting · corroded · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Attach Fittings > FOUND CORROSION AT FITTING C 63, P44-46 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04398](https://openairdocs.org/sdr/07FDEA04398.md): Spar · damaged · Oct 1, 2007 · N806FD · Airbus A310324 · Wing Spar > SHOULDERED BOLTS FOUND DURING EMBODIMENT OF SB A310-57-2079 AT HOLE NR 21 AND NR 14 RT REAR SPAR AREA OF SPOILER NR 3 RT REPAIR PERFORMED BY REPLACEMENT OF BUSH IAW EA 6-5720-82852 AND RAS /BAE/1000689/2005 ISS A. - [SDR 07FDEA04397](https://openairdocs.org/sdr/07FDEA04397.md): Floorbeam · damaged · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Floor Beam > FOUND OLD MISDRILLED HOLE AT CROSSBEAM C 64 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04396](https://openairdocs.org/sdr/07FDEA04396.md): Stringer · damaged · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND MISDRILLED HOLES AT STRINGER 41 LT, C33-34 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. - [SDR 07FDEA04395](https://openairdocs.org/sdr/07FDEA04395.md): Stringer · corroded · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A. - [SDR 07FDEA04394](https://openairdocs.org/sdr/07FDEA04394.md): Stringer · corroded · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A. - [SDR 07FDEA04393](https://openairdocs.org/sdr/07FDEA04393.md): Stringer · corroded · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A. - [SDR 07FDEA04392](https://openairdocs.org/sdr/07FDEA04392.md): Stringer · corroded · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A. - [SDR 07FDEA04391](https://openairdocs.org/sdr/07FDEA04391.md): Stringer · corroded · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND CORROSION BETWEEN C 39-47 AT STRINGERS BETWEEN P 38-49, LT AND RT. REPAIR PERFORMED BY SMOOTH REWORK OF CORROSION IAW EA 6-5315-82855 AND RAS/AS/0095/2005 ISS A. - [SDR 07FDEA04390](https://openairdocs.org/sdr/07FDEA04390.md): Stringer · corroded · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND CORRODED STRINGER SEGMENT P 57 AT C 72 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04389](https://openairdocs.org/sdr/07FDEA04389.md): Floorbeam · corroded · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Floor Beam > FOUND CROSSBEAM C 63 CORRODED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04388](https://openairdocs.org/sdr/07FDEA04388.md): Flange · corroded · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Miscellaneous Structure > FOUND CORRODED FLANGE AT C61-62, P 56 RT-56 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. - [SDR 07FDEA04387](https://openairdocs.org/sdr/07FDEA04387.md): Stringer · corroded · Oct 1, 2007 · N806FD · Airbus A310324 · Fuselage Main, Longeron/Stringer > FOUND CORRODED STRINGER P 21 LT, BETWEEN 55/58-60 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. - [SDR 07FDEA04386](https://openairdocs.org/sdr/07FDEA04386.md): Panel · cracked · Oct 1, 2007 · N806FD · Airbus A310324 · Nacelle/Pylon, Plate/Skin > FOUND CRACK (ABOUT 6MM) AT PYLON NR 2 RIB 8 OUTBOARD SIDE WALL DOUBLER REPAIR PERFORMED IAW SRM 54-51-31 FIG 201. - [SDR 07FDEA04370](https://openairdocs.org/sdr/07FDEA04370.md): Plate · damaged · Sep 28, 2007 · N806FD · Airbus A310324 · Fuselage Miscellaneous Structure > DAMAGED WEB PLATES BETWEEN FRAME 86-87, STGR. 33 LT REPLACEMENT OF WEB PLATE IAW SRM 51-72-10. - [SDR 07FDEA04369](https://openairdocs.org/sdr/07FDEA04369.md): Plate · damaged · Sep 28, 2007 · N806FD · Airbus A310324 · Fuselage Miscellaneous Structure > DAMAGED WEB PLATES BETWEEN FRAME 86-87, STGR 39 LT AND RT. REPLACEMENT OF WEB PLATES LT AND RT IAW SRM 51-72-10 - [SDR 07FDEA04368](https://openairdocs.org/sdr/07FDEA04368.md): Fitting · corroded · Sep 28, 2007 · N806FD · Airbus A310324 · Fuselage Miscellaneous Structure > CORROSION ON UPPER RUN OUT FITTING BETWEEN FRAME 16A-17, STRG 44 RT, AFTER REWORK NO REMAINING THICKNESS WAS EXISTED. REPLACEMENT OF UPPER RUN OUT FITTING IAW. REPAIR DRW R536-10440 ISSUE C. - [SDR 07FDEA04367](https://openairdocs.org/sdr/07FDEA04367.md): Skin · chafed · Sep 28, 2007 · N806FD · Airbus A310324 · Leading Edge Devices > FOUND SCRATCHES ON NOSE SKIN OF SLAT NR 2 RT WING, RIB 24-27. NOSE SKIN REPAIR PERFORMED IAW SRM 57-43-11/FIG 202/SHEET 11. REFER TO NON ROUTINE DR0399, AT RIB 27 OTHER ASNA0081A FASTENERS ARE INSTALLED ACC TO DRW A578-44242/SHEET 16, IAW AI-STATEMENT 942-03 - [SDR 07FDEA04365](https://openairdocs.org/sdr/07FDEA04365.md): Skin · chafed · Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/Skin > FOUND CHAFING MARKS BETWEEN SLAT TRACK 6 AND JACK 4, LEADING EDGE SKIN, RT WING. REPAIR PERFORMED BY INSTALLATION OF NEW SKIN INSERT IAW SRM 57-41-12/FIG 203, 204. - [SDR 07FDEA04364](https://openairdocs.org/sdr/07FDEA04364.md): Skin · chafed · Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/Skin > FOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 203, 204, CHAFING MARKS BETWEEN SLAT TRACK 5 AND SLAT TRACK 6, LEADING EDGE SKIN, RT WING. NEW REPAIR SKIN INSERT INSTALLED IAW SRM 57-41-12/FIG 203, 204. - [SDR 07FDEA04363](https://openairdocs.org/sdr/07FDEA04363.md): Skin · chafed · Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/Skin > FOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 204, CHAFING MARKS BETWEEN JACK 3 AND SLAT TRACK 5, LEADING EDGE SKIN, RT WING. NEW REPAIR SKIN INSERT INSTALLED IAW SRM 57-41-12/FIG 203, 204. - [SDR 07FDEA04362](https://openairdocs.org/sdr/07FDEA04362.md): Skin · chafed · Sep 28, 2007 · N806FD · Airbus A310324 · Fuselage Main, Plate/Skin > FOUND ON OLD NOSE SKIN REPAIR IAW SRM 57-41-12/FIG 203, 204, CHAFING MARKS BETWEEN SLAT TRACK 1 AND SLAT TRACK 2, LEADING EDGE SKIN, RT WING. NOSE SKIN REPAIR RENEWED, NEW REPAIR SKIN IAW SRM 57-41-12/FIG 203, 204. - [SDR 07FDEA04360](https://openairdocs.org/sdr/07FDEA04360.md): Skin · chafed · Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/Skin > FOUND CHAFING MARKS BETWEEN JACK 3 AND SLAT TRACK 5, LEADING EDGE SKIN, LT WING. NOSE SKIN REPAIR PERFORMED SRM 57-41-12/FIG 203, 204. - [SDR 07FDEA04359](https://openairdocs.org/sdr/07FDEA04359.md): Skin · chafed · Sep 28, 2007 · N806FD · Airbus A310324 · Wing, Plate/Skin > FOUND CHAFING MARKS BETWEEN SLAT TRACK 5 AND SLAT TRACK 6, LEADING EDGE SKIN, LT WING. REPLACEMENT OF CHAFED NOSE SKIN IAW SRM 51-72-10. - [SDR 07FDEA04358](https://openairdocs.org/sdr/07FDEA04358.md): Plate · cracked · Sep 28, 2007 · N806FD · Airbus A310324 · Wing Miscellaneous Structure > FOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 7, FWD OF FRONT SPAR, UPPER SKIN, RT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 7 RT IAW SRM 51-72-10. - [SDR 07FDEA04357](https://openairdocs.org/sdr/07FDEA04357.md): Plate · cracked · Sep 28, 2007 · N806FD · Airbus A310324 · Wing Miscellaneous Structure > FOUND CRACKED REINFORCING PLATE ON SLAT TRACK NR 7, FWD OF FRONT SPAR, UPPER SKIN, LT WING. REPLACEMENT OF REINFORCING PLATE ON TRACK 7 LT IAW SRM 51-72-10. Next page: https://openairdocs.org/deregistered/N806FD-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 = 'N806FD' AND deregistration_id = 'N806FD-2024-03-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N806FD-2024-03-02/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.