N726FD

Service difficulty reports · 237

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N726FD' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201304090768Panel · missingFOUND LEFT LOWER WING PANEL 512BB MISSING AND ATTACH FITTINGS MISSING. INSTALLED PANEL IAW AMM 57-41-41-04. ACFT OK FOR SERVICE.Apr 9, 2013 · N726FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA201111024730Spar · crackedCOMPLY WITH EA 6-5710-150054 COMPLIED WITH EA 6-5710-150054 - WINGS - CTR WING BOX - AD 2005-23-08. REAR SPAR LOWER FLANGE AT FRAME 47, EXISTING CRACK REPAIR AT HOLES LT SIDE.Nov 2, 2011 · N726FD · Airbus A300B4622R · Wing SparSDR FDEA201110194586Flap Track · gougedRT WING NR3 FLAP TRACK OTBD FACE HAS INDENTATIONS AT FWD AND AFT SECTION. SECTION (EA MEASURING L=1" X W=0.25" X D=0.05") R & R RT NR3 FLAP TRACK BEAM IAW AMM 57-20-24-4. REMOVED ANR RE-INSTALLED NR3 FLAP TRACK CARRIAGES IAW AMM 27-54-27-4 TO FOM. REMOVED ANOct 19, 2011 · N726FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201110174550Skin · gougedLEFT WING CENTER FLAP UPPER SURFACE CHAFED & GOUGED. GOUGES APROXIMATELY .2500" DIA X .040" DEEP. REPAIRED IAW SRM 57-50-00 PB 201 PARA 4F.Oct 17, 2011 · N726FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201110074370Skin · damagedRT WING INBD UPPER FLAP SKIN MISREPAIRED IAW SRM 57-50-00, FIG 205 REPAIRED IAW SRM 57-50-00, FIG 205, PG 219.Oct 7, 2011 · N726FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201110074381Skin · chafedRT WING INBD FLAP, MOST INBD T/E UPPER SURFACE HAS A 2.5 " X .1 " X .002" CHAFE MARK. SMOOTHED & BLENDED CHAFE MARK IAW SRM 51-73-10 ORIGINAL THICKNESS OF .012 AFTER .008 FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00, FIG 101. R & R SKIN ASSY AT RT INBD FLAP T/Oct 7, 2011 · N726FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201110054314Skin · gougedLT WING INBD FLAP UPPER SURFACE GOUGED. LOCATED 24.5 IN. FROME OTBD END AND 22 IN AFT OF LEADING EDGE. GOUGE MEASURES 1.6IN. X .3IN. X .007IN. BLENDED GOUGED SKIN AND REPAIRED IAW EA 6-5750-156025.Oct 5, 2011 · N726FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201110034275Skin · damagedRUDDER TRAILING EDGE TOP SIDE LIGHTING STRIKE RT SIDE STATIC WICK DISCH. ATTACH AREA RUDDER DAMAGE TO T/E STATIC WICK ATTACHMENT WAS REPAIRED IAW SRM 55-41-12, PARA 16B, FIG 208C AND EA 6-5540-145674.Oct 3, 2011 · N726FD · Airbus A300B4622R · Rudder, Plate/SkinSDR FDEA201110034274Skin · damagedRUDDER SKIN LT SIDE GROUP OF 3 EA LIGHTNING STRIKE HOLES AT UPPER SECTION BETWEEN RIB 13-14 REPAIRED 3 EA. LIGHTNING STRIKES HOLES AT UPPER SECTION BETWEEN RIB 13-14 ON LT SKIN OF RUDDER IAW SRM 55-41-12 ( 16 A ) AND FIG 201 PARA 30 A APPLIED SURFACE PROTECTIOOct 3, 2011 · N726FD · Airbus A300B4622R · Rudder, Plate/SkinSDR FDEA201110034273Skin · damagedRUDDER SKIN AT LT SIDE LWR 16IN . FROM BOTTOM AND 26 IN. FROM L/E SPAR HAS A 1.0 L X .75W PUNCTURE. RUDDER SKIN LT SIDE 16 IN FROM LOWER EDGE AND 26 IN FROM FWD SPAR WAS REPAIRED IAW SRM 55-41-12,PARA 30 AS SKIN REPAIR ONLY AS NO DAMAGE WAS FOUND AT THE COROct 3, 2011 · N726FD · Airbus A300B4622R · Rudder, Plate/SkinSDR FDEA201109224070Floor Support · corrodedMAIN DECK FLOOR SUPPORT BETWEEN LONGITUTIONAL BEAM 3L AND 2L HAS 1.5 SQ IN CORROSION R & R "T" CAP ON FLOOR SUPPORT FROM FRAME 11 TO FRAME 12A IAW SRM 51-40-21, PARA 5, 6 & 7 AFTER CORROSION WAS FOUND TO BE OUT OF LIMITS WITH MATERIAL LOSS OF .009 WITH BEFORSep 22, 2011 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201109224069Floor Support · corrodedMAIN DECK LONGITUTIONAL BEAM 3L BETWEEN FRAME 11 AND FRAME 13 CORRODED 4 SQ IN. R & R "T" CAP ON LONGITUTIONAL BEAM FROM FRAME 11 TO FRAME 15 IAW SRM 51-40-21, PAR 6, DUE TO CORROSION BEING OUT OF LIMITS WITH MATERIAL LOSS OF .014, STARTING AT .079 AND ENDINGSep 22, 2011 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201109224065Fitting · damagedUPON REMOVAL AND REPLACEMENT OF FASTENERS AT FRAME 11 JUST AFT OF COCKPIT TO AVIONICS DOOR, FOUND FASTENER HOLE ELONGATED ON WEB. R & R WEB FITTING AT FRAME 11 IAW SRM 51-72-10, PAGES 1 THRU 3.Sep 22, 2011 · N726FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA201109213994Skin · damagedFWD CARGO DOOR CUTOUT DENT AREA SHOWS INDICATIONS OF CRACKS AT 3 LOCATIONS. FABRICATED, LOCATED AND DRILLED REPAIR PARTS IAW SRM 53-13-12, FIG 206. ALODINED AND PRIMED IAW SRM 51-21-10 AND 51-75-10. INSTALLED REPAIR PARTS IAW SRM 53-13-12 AND 51-40-21. APPSep 21, 2011 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201109153897Web · dentedAFT CARGO COMPARTMENT FWD UPPER CORNER SUPPORT WEB DAMAGE/DENT 5" IN LENGTH. REMOVED AND REPLACED PROFILE WEB IAW SRM 51-72-10.Sep 15, 2011 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201109143880Intercostal · corrodedAFT CARGO COMPARTMENT AT FR 63, BETWEEN FLOOR SUPPORT Y1470 AND Y805 INTERCOSTAL CORRODED INBD SIDE OF CUTOUT LINE. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION AND INSTALLED REPLACEMENT SECTION IAW SRM 53-10-15,FIG 207.Sep 14, 2011 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201109143878Floor Support · bentCARGO COMPARTMENT FLOOR SUPPORT S51L BENT FROM FR 65 TO 69. R & R IAW SRM 51-40-21 AND REPROTECTED IAW SRM 51-75-10.Sep 14, 2011 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201109143877Floor Support · bentCARGO COMPARTMENT FLOOR SUPPORT S44L, BENT FR64 TO FR 68. REPAIRED IAW SRM 51-40-21 AND REPROTECTED IAW SRM 51-75-10.Sep 14, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201109143885Access Panel · crackedBOTTOM EXT FUSE EXT ELECTRICAL POWER ACCESS DOOR DOUBLER CRACKED RT SIDE UPPER .1" LENGTH. REMOVED BOTTOM EXT FUSE EXT ELECTRICAL PWR ACCESS DOOR TO FOM DOUBLER IAW SRM 51-40-21. LOCATED AND DRILLED NEW DOUBLER IAW SRM 51-72-10. ALODINED DOUBLER AND HOLES Sep 14, 2011 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201109143879Floorbeam · bentCARGO COMPARTMENT FLOORBEAM FR 67 BENT FROM LBL 46 TO 51 UP SIDE. REMOVED BENT FLOORBEAM IAW SRM 51-40-21, LOCATED AND DRILLED NEW FLOORBEAM IAW SRM 51-72-10, INSTALLED IAW 51-40-21 AND REPROTECTED IAW SRM 51-75-10.Sep 14, 2011 · N726FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA201109093814Angle · crackedLT WING INBD L/E AREA INSIDE KRUEGER FLAP WELL, OTBD SIDE OF FLAP WELL BETWEEN RIB 1 & RIB 2, 1.50" CRACK ON FIXED L/E STRUCTURE. REMOVED 3 EA PROTECTIVE COVERING IAW SRM 51-40-21. REMOVED CRACKED REINFORCING ANGLE IAW SRM 51-40-21. LOCATED AND DRILLED NEW Sep 9, 2011 · N726FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA201109083768Fitting · damagedCENTER WING BOX FWD FACE FR 47 LOWER EDGE FITTING IS DAMAGED CENTER TO 16" RT SIDE. R & R FITTING ON FR 47 IN CTR WING BOX IAW SRM 51-40-21, PARA 5-B.Sep 8, 2011 · N726FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA201109083749Floor Panel · delaminatedFLOOR PANEL 131JG HAS 30 SQ. IN. OF DELAMINATED AND MISSING SKIN IN FWD CARGO. FABRICATED REPLACEMENT PANEL 131JG IAW DWG SRZ 25-005 REV J.Sep 8, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201109063728Skin · misrepairedFLUSH REPAIR ON RT SIDE FUSELAGE SKIN BETWEEN FRAMES 72 & 73 AND BETWEEN STRINGERS 30 & 32 RT, NOT EFFECTIVE IAW SRM 53-10-12, FIG 229. REMOVED AND REPLACED FASTENERS AND NOW IAW SRM 53-10-12,FIG 229.Sep 6, 2011 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201109063727Skin · misrepairedSKIN FLUSH REPAIR LOCATED ON RT SIDE FUSELAGE SKIN BETWEEN FRAMES 76 & 77 AND BETWEEN STRINGERS 28 & 31 RT HAS REPAIR NOT EFFECTIVE IAW SRM 53-10-12, FIG 229. REMOVED AND REPLACED REPAIR IAW SRM 53-10-12,FIG 229.Sep 6, 2011 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201109063720Floor Panel · damagedAFT CARGO FLOOR PANEL 152BF EXPOSE HONEYCOMB REF AMM 53-10-20-06 FABRICATED. REPLACEMENT FLOOR PANEL 152BF IAW DWG SRZ-25-005 REV J. MAJOR REPAIR IAW GMM 6-2-100.Sep 6, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201109033644Rib · crackedNR 2 PYLON OTBD SIDE RIB 3 SPLICE CRACKED. REMOVED DAMAGED SPLICE FROM NR 2 ENGINE OTBD PYLON IAW SRM 51-40-21, LOCATED AND DRILLED NEW SPLICE IAW SRM 51-40-21. LOCATED AND DRILLED NEW SPLICE IAW SRM 51-40-21 P.5-6.Sep 3, 2011 · N726FD · Airbus A300B4622 · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201109033656Skin · misrepairedEXTERNAL REPAIR DOUBLER LOCATED AT LOWER RT SIDE FUSELAGE SKIN BETWEEN FRAMES 30 TO 31 AND BETWEEN STRINGERS 52 RT TO 55 AT TOILET SERVICING ACCESS HAS INCORRECT RIVETS SIZE INSTALLED IN OUTER ROWS.Sep 3, 2011 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201109023642Seat Track · corrodedMAIN DECK SEAT TRACK 2R BET FR 17 AND FR 19 HAS CORROSION .250 INCH LENGTH REF AMM 53-12-00-06. REMOVED CORROSION IN BETWEEN FR17-FR19 SEAT TRACK 2 R IAW SRM 51-74-10. CHECKED LIMITS AND THEY WERE ORIGINAL MAT .028 MAT, LOSS .003, MAT. REMAINING .025 FOUND Sep 2, 2011 · N726FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109013623Floor Support · failedFLOOR SUPPORT MISREPAIRED. REPAIRED IAW SRM 51-72-10, PG 1TO3.Sep 1, 2011 · N726FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201109013619Floor Panel · damagedBULK CARGO FLOOR PANEL 162CF EXPOSE HONEYCOMB REF. AMM 53-10-20-06. FABRICATED FLOOR PANEL IAW DWG SRZ25-005 REV. J MAJOR REPAIR IAW GMM6-2-100Sep 1, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201109013621Seat Track · misrepairedSEAT TRACK MISREPAIRED. R & R SEAT TRACK PER SRM 53-12-16, FIG 201, SH 1&2 PG 202-207. REPAIR IS A MAJOR PER GMM 6-2-100.Sep 1, 2011 · N726FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108313601Floor Panel · corrodedBULK CARGO FLOOR PANEL 161CF BOTTOM OF PANEL CORROSION 50 SQ IN REF AMM 53-10-20. FABRICATED REPLACEMENT PANEL 161CF IAW DWG-25-005 REV J. FABRICATED REPLACEMENT FACE PLATE IAW DWG SRZ-25-011, REV D IDENTIFIED REPLACEMENT PANEL IAW GMM 7-0-1001. MAJOR REPAIAug 31, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201108313599Floor Panel · damagedCENTER AREA FLOOR PANEL 147AF DISBONDED AROUND INSERTS, ALSO LOOSE FASTENERS. REF 25- 50-00-06 FABRICATED REPLACEMENT FLOOR PANEL 147AF IAW DWG SRZ-02-005 REV J. MAJOR REPAIR IAW GMM 6-2-100.Aug 31, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201108293569Floor Panel · crackedFLOOR PANEL 151GF HAS THREE, FIVE INCH CRACKS, FABRICATED FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR IAW GMM 6-2-100.Aug 29, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201108293538Floor Panel · damagedMDCC FLOOR PANEL 231EF IMPACT DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL 231EF IAW DWG. SRZ 25-005 REV. J.Aug 29, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201108283535Floor Panel · crackedFLOOR PNL 132YF HAS 10 SQ. IN OF DELAMINATION, 1EA, 4" CRACK AND 4-1" PUNCTURES. FABBED PANEL 132YF IAW DWG SRZ25-005, REV J.Aug 28, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201108283534Floor Panel · crackedFLOOR PANEL 131ZF HAS 1 EA, 16" CRACK, FABRICATED REPLACEMENT FLOOR PANEL 131ZF IAW DWG SRZ 25-005, REV J.Aug 28, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201108273527Floor Panel · crackedFLOOR PANEL 132ZF HAS ONE 18'' CRACK. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005 REV. J MAJOR REPAIR IAW GMM 6-2-100Aug 27, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201108273526Floor Panel · crackedMAIN DECK FLOORBOARD 261VF CRACKED ACROSS THE MIDDLE FABRICATED REPLACEMENT FLOOR PANEL 261VF IAW DWG SRZ 25-005, REV. JAug 27, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201108273525Floor Panel · crackedMAIN DECK FLOOR PANEL 252ZG CRACKED AT 4EA CLEVIS CUTOUTS FABRICATED REPLACEMENT FLOOR PANEL 252ZG IAW DWG SRZ 25-005, REV J.Aug 27, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201108263521Floorboard · damagedFLOOR PANEL 132RF HAS 50" OF EDGE DAMAGE. FABRICATED FLOOR PANEL 132RF IAW DWG, SRZ25-005 REV J.Aug 26, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201108263520Floor Panel · damagedFLOOR PANEL 131YF HAS 15" OF EDGE DAMAGE, 5" OF DELAMINATION, 20SQ." OF CORROSION FABRICATED REPLACEMENT PANEL IAW GWG SRZ-25-005 REV J IDENTIFIED REPLACEMENT PANEL IAW GMM 7-0-1001.Aug 26, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201108263516Floor Panel · damagedFLOOR PANEL 131HG HAS 10" OF EDGE DAMAGE, 10EA. PUNCTURES, 3EA. CRACKS FABRICATED REPLACEMENT PANEL 313HG IAW DWG SRZ-25-005 REV. J IDENTIFIED REPACEMENT PANEL IAW GMM 7-0-1001.Aug 26, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201108263515Floor Panel · crackedFLOOR PANEL 131RF IS CRACKED ACROSS PANEL. FABRICATED REPLACEMENT PANEL 131RF IAW DWG SRZ 25-005 REV J.Aug 26, 2011 · N726FD · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108253485Floorboard · damagedFLOORBOARD 131QF HAS 22" OF EDGE DAMAGE, 18EA .25 PUNCTURES, FABRICATED REPLACEMENT FLOORBOARD 131QF IAW DWG SRZ-25-005.Aug 25, 2011 · N726FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201107162766Processing Unit · failedAFTER T/O HAD PITOT HEAT LIGHTS TAT LIGHT ON F/O CAP/STBY/F/O THEN ADC1 INOP. ATS 1 & 2 TRIPPED. CAB PRESS REG 2 FAULT. STATUS PAGE PROC: ENG ALTN MODE ATS-ALPHA FLOOR INOPERATIVE, PROBE HEAT PARTIALLY INOPERATIVE, CAB PRESS SYS 2 INOP. FOLLOWED ECAM PROCJul 16, 2011 · N726FD · Airbus A300B4622R · Altimeter, Barometric/EncoderSDR FDEA201012224736Valve · malfunctionedAFTER T/O ECAM INDICATED SLATS SYS 2 FAULT AND OVER-HEAD INDICATED SLATS SYS 2 FAULT LIGHT ILLUMINATED. CREW CYCLED SLATS TWICE - SLATS AND FLAPS WERE NORMAL AFTER SECOND CYCLE - LIGHT REMAINED ILLUMINATED. NR 2 SFCC FAULTED HIGH SPEED VALVE. REPLACED SLAT Dec 22, 2010 · N726FD · Airbus A300B4622R · Leading Edge Slat Control SystemSDR FDEA201011264495Valve · malfunctionedDURING SLAT RETRACTION ECAM IND SLAT SYS 2 FAULT WITH OVERHEAD LIGHT ON. CYCLED HANDLE NO JOY. SPFI INDICATED SLATS UP. ZIPPER AND HOOK WORKED NORMALLY, CONSULTED QRH, DID NOT COVER FAULT WITH SLATS ACTUALLY UP. WITH BOTH VISUAL AND SPFI INDICATING FLAPSNov 26, 2010 · N726FD · Airbus A300B4622R · Leading Edge Slat Control SystemSDR FDEA201011174405Control Handle · inoperativeSELECTED THE LANDING GEAR LEVER DOWN WITH THE POSITION DET IN SYS 1. RECEIVED 3 GREEN DOWN INDICATIONS AND 3 RED UNLK INDICATIONS ON THE FWD PNL INDICATING SYS. THE INDICATING SYSTEMS ON THE OVERHEAD PNL WERE ALL GREEN. RELEASED FOR SERVICE IAW MEL: 32-61-01Nov 17, 2010 · N726FD · Airbus A300B4622R · Landing Gear Selector
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