N743FD

Service difficulty reports · 263

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 = 'N743FD' 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 FDEA201306181340O-Ring · damagedGREEN HYD RSVR LOW QTY. COMPLIED WITH ECAM AND QRH PROCEDURES. GRAVITY EXTENDED LANDING GEAR WITH SATISFACTORY RESULTS. AFTER PARKING DID EXTERNAL WALKAROUND FOUND NO EVIDENCE OF ANY HYD LEAKS. AFTER CREW DEBRIEF, QTY CAME BACK UP TO BOTTOM OF TOP HAT AFTER Jun 18, 2013 · N743FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA201306081230Wire Harness · damagedLEFT AFT WINDOW GOT VERY HOT. FLEXIBLE CABLE UNDER CAPTAIN'S SLIDING WINDOW SPARKED, BURNED AND GOT VERY HOT. TURNED OFF LT AND RT WINDOW HEAT. WINDOW COOLED DOWN. POWERED RT WINDOW HEAT. FOUND LT SLIDING WINDOW HARNESS 69DG DAMAGED AT AFT LOWER CORNER OJun 8, 2013 · N743FD · Airbus A300B4622R · Ice/Rain Protection System WiringSDR FDEA201302130339Valve · failedAT FL 260 PACK NR 2 VALVE FAILED. APPROX 10 SECONDS LATER, PACK NR 1 FAILED CABIN PRESSURE WAS 4600' BLEED AIR SUPPLY CONFIRMED GOOD ON ECAM. RESET BOTH PACK VALVES AND BOTH REMAINED FAULTED, CABIN PRESSURE CLIMBED TO 6800' COMPLIED WITH ECAM & QRH AND STAFeb 13, 2013 · N743FD · Airbus A300B4622R · Pneumatic Distribution SystemSDR FDEA201212024226Skin · crackedAFT CARGO DOOR BETWEEN FRAMES 61A TO 62A AND BETWEEN LONGERON 1A TO 2 HAS THREE AREAS OF INTERNAL SKIN FLANGE BENT AND 1 EA CRACKED L-SECTION BETWEEN FRAMES 62 AND FR 62A. R & R CRACKED L-SECTION IAW SRM 51-72-10, PG 1-3 AND SRM 51-40-21 PAR 6. REFORMED 3Dec 2, 2012 · N743FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA201211304223Skin · dentedRIGHT WING AILERON LOWER AFT SURFACE HAS 6 DENTS FROM .5 TO 2 SQUARE INCHES AND FROM .009 TO .015 INCHES APPROX DEEP. REPAIRED 6 EA DENTS AT RT AILERON LWR AFT T/E SECTION IAW SRM 51-77-12, PARA 4C, PG 3-6 AND 51-77-12 4C PG 288-289. NDT SHOWS NO DELAMINATIONov 30, 2012 · N743FD · Airbus A300B4622R · AileronsSDR FDEA201211294207Skin · damagedLIGHTNING DAMAGE FASTENERS WERE TEMPORARILY REPLACED IAW SRM REV 74 53-10-12-101 TABLE 101 PAR 8 & FIG 218, TABLE 1,2,3.Nov 29, 2012 · N743FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201211294206Floor Panel · mismanufacturedDURING INSTALLATION OF BULK CARGO FLOOR PANEL 161 AF FOUND HOLES IN PANEL TO NOT ALIGN WITH HOLES IN STRUCTURE. FABRICATED REPLACEMENT PANEL 161 AF IAW DWG SRZ 25-005, REV J.Nov 29, 2012 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201211294204Skin · damagedLIGHTNING DAMAGE, FASTENERS REPLACED IAW SRM REV 74 53-10-12-101, TABLE 101, PAR 8 & FIG 219 TABLE 1,2,3.Nov 29, 2012 · N743FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201211264181Plate · damagedAFT CARGO DOOR BOTTOM SKIN PROTRUDING .5 SQUARE INCHES. R & R IAW SRM 51-72-10, PGS 1 - 3.Nov 26, 2012 · N743FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA201211254153Web · damagedBULK CARGO BAY FR 69 VERTICAL WEB DEFORMED ABOVE MAIN FLOOR FROM LIGHT TO BULK CARGO DOOR, TOTAL OF SEVEN AREAS AND TOTAL 100 SQUARE INCHES. FOUND TO BE OUT OF LIMITS IAW SRM 53-17-15, FIG 101. R & R IAW SRM 51-72-10, PG. 1-3.Nov 25, 2012 · N743FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201211254152Floorbeam · corrodedCARGO BAY FLOORBEAM AT FRAME 69 BETWEEN ROLLER TRAYS 2L AND 3L HAS ONE SQUARE INCH OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15, FIG 105. R & R FLOORBEAM AT IAW SRM 51-72-10 PG 1-3.Nov 25, 2012 · N743FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA201211214121Floor Panel · delaminatedFLOOR PANEL 151LF HAS APPROX. 30 SQUARE INCHES OF DELAMINATION ON LOWER SURFACE. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005, REV. JNov 21, 2012 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201211214117Floor Support · bentAFT CARGO COMPT FLOOR SUPPORT BETWEEN FR 64-65 ROLLER TRACK 1L BENT APPROX LENGTH 1.5" X WIDTH .75". REMOVED AND REPLACED FLOOR SUPPORTNov 21, 2012 · N743FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201211214114Floor Support · dentedBULK CARGO BAY FLOOR SUPPORT FROM FR 67 TO 68 DEFORMED IN MIDDLE WITH STRAIGHT EDGE PLACED ACROSS. R & R FLOOR CENTER LINE FLOOR SUPPORT IAW SRM 51-72-10, PG 1-3.Nov 21, 2012 · N743FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201211214113Profile · crackedFOUND BULK CARGO COMPARTMENT LONGITUDINAL PROFILE TO HAVE A .75 INCH CRACK ON VERTICAL FLANGE AT FR 65, 19 INCH ALONG Y203. R & R LONGITUDINAL PROFILE Y203 FROM FR65 TO 66 IN BULK CARGO BAY IAW SRM 51-72-10, PG 1-3.Nov 21, 2012 · N743FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201211184071Support · crackedSEAT TRACK SUPPORT CRACKED AT WEB ON THE INBD SIDE. CRACK APPROX .50". R & R SUPPORT IAW SRM 51-40-21.Nov 18, 2012 · N743FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201211164042Floor Support · bentCARGO BAY, 22" INCHES RT OF CENTERLINE FLOOR SUPPORT FROM FR 67 TO FR 68 IS DEFORMED IN THE MIDDLE WITH STRAIGHT EDGE PLACED ACROSS. REMOVED DEFORMED FLOOR PANEL SUPPORT AND REPLACED WITH A SERVICABLE PART IAW A SRM 51-72-10 AND SRM 51-40-21. REPROTECTED ARNov 16, 2012 · N743FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201211154028Roller Track · corrodedAFT CARGO FLOOR ROLLER TRACK 1L LT FLANGE CORRODED AT 8 PLACES BETWEEN FR 57 - FR 58 AROUND THE FASTENER HOLES. AFTER REMOVAL OF LEVEL 1 CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15, FIG 102, SHT 3. R & R ROLLER TRACK WITH FABRICATED REPLACEMENTNov 15, 2012 · N743FD · Airbus A300B4622 · Cargo CompartmentsSDR FDEA201211154024Seat Track · gougedMAIN DECK CARGO SEAT TRACK 2R BETWEEN FR 60 AND FR 61 HAS 2 EACH GOUGES IN SCALLOPS. SMOOTH AND BLENDED AREA BETWEEN SEAT TRACK 2R AT FR 61 PLUS 3" AND FOUND AREA OUT OF LIMITS IAW SRM 53-1016, PG 103, FIG 101. R & R SEAT TRACK SECTION 2R BETWEEN FR 58 AND Nov 15, 2012 · N743FD · Airbus A300B4622 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201211144008Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 241LK IS BROKEN IN HALF. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005, REV. J.Nov 14, 2012 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201211133999Floorboard · delaminatedAFT CARGO BAY FLOORBOARD 151HF HAS A TEN SQUARE INCHES AREA OF DELAMINATION & TWO, TWENTY SQUARE INCHES AREAS OF DELAMINATION. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.Nov 13, 2012 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201211133998Floorboard · crackedFLOORBOARD 231CF TOP SIDE SKIN HAS A CRACK. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.Nov 13, 2012 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201211133997Floor Panel · damagedFWD CARGO FLOOR PANEL 132RF HAS DAMAGED PLIES AND CRUSHED CORE, CORE ALONG ONE SIDE EDGE, ENTIRE LENGTH OF PANEL. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Nov 13, 2012 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201211133996Floor Panel · damagedFWD CARGO FLOOR PANEL 131RF BROKEN. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Nov 13, 2012 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201211133983Floor Support · damagedBULK CARGO PIT FLOOR SUPPORT BETWEEN FR 65 & 66 LOCATED 20 IN RT OF CENTERLINE FOUR FASTENER HOLES MISDRILLED. R & R FLOOR SUPPORT SECTION AT BULK CARGO PIT IAW SRM 51-72-10, PG. 1.Nov 13, 2012 · N743FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201211103934Floor Panel · delaminatedFWD CARGO FLOOR PANEL, 131JG HAS DAMAGED PLIES AND CRUSHED CORE ALONG 1 SIDE THE ENTIRE LENGTH OF PANEL. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ25-005, REV J.Nov 10, 2012 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201211103932Floor Panel · delaminatedFWD CARGO FLOOR PANEL 132QF HAS DAMAGED PLIES AND CRUSHED CORE ALONG BOTH EDGES, ENTIRE LENGTH OF PANEL. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ25-005 REV J.Nov 10, 2012 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201211093917Floor Panel · damagedFWD CARGO FLOOR PANEL 132HG HAS DAMAGED PLIES AND CRUSHED CORE ALONG EDGE, EIGHT PLACES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Nov 9, 2012 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201211093916Floor Panel · damagedFWD CARGO FLOOR PANEL 131YF HAS DAMAGED PLIES AND CRUSHED CORE ALONG BOTH EDGE SIDES, ENTIRE LENGTH OF PANEL. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV. J.Nov 9, 2012 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201211073894Floor Panel · delaminatedFLOOR PANEL 143DF HAS DELAMINATION ON BACKSIDE APPROX 25 PERCENT DUE TO HYD FLUID. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Nov 7, 2012 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201211073893Floor Panel · damagedFLOOR PANEL 147AF HAS COMPOSITE DAMAGE ON FRONT & REAR EDGES AS WELL AS HYD FLUID SOAKED FOAM TAPE & MISSING SECTIONS OF FOAM TAPE. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV. J.Nov 7, 2012 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201211063888Skin · gougedRT EXTERNAL FUSELAGE SKIN GOUGED 5" SQ LOCATED FWD CARGO DOOR FWD CUTOUT FR20 AND 1 FT. ABOVE BOTTOM DOOR CUTOUT. SMOOTHED AND BLENDED GOUGE IAW SRM 51-73-10. CHECKED LIMITS ORIGINAL MATERIAL = 0.236" REMOVED MATERIAL = 0.004" ALLOWABLE REMOVED MATERIAL = 0.Nov 6, 2012 · N743FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201111235009Control Handle · obstructedON DEPARTURE, SLAT HANDLE WOULD NOT RETRACT PAST 15/0 POSITION. SLAT/FLAP HANDLE APPEARS TO BE MECHANICALLY IMPAIRED. ON LANDING, CONFIGURATION HANDLE WOULD NOT GO PAST 15/20 POSITION. DISASSEMBLED SLAT/FLAP HANDLE IN REF TO AMM 27-51-11-04 AND CMM 27-51-11Nov 23, 2011 · N743FD · Airbus A300B4622R · Leading Edge Slat Control SystemSDR FDEA201103050861Floor Panel · delaminatedREWORK WIC "61C5244ZL" BULK CARGO COMPARTMENT FOUND FLOOR PANEL (162HF) SOFTEN. FABRICATED A NEW FLOOR PANEL OF BULK CARGO COMPARTMENT IAW AB6 SRM 53-10-20 AND MCG IRM 9701 FOR REPLACEMENT FLOOR PANEL.Mar 5, 2011 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201103050860Floor Panel · delaminatedREO WORK WIC "61C5244ZL" BULK CARGO COMPT FOUND FLOOR PANEL (161BF) SOFTEN. FABRICATED A NEW FLOOR PANEL OF BULK CARGO COMPARTMENT IAW. AB6 SRM 53-10-20 AND MCG IRM 9701 FOR REPLACEMENT FLOOR PANEL.Mar 5, 2011 · N743FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201103020814Rib · chafedLT WING T/E UPPER FIXED PANEL SUPPORT RIB CHAFING AT NR 5 SPOILER INBD HINGE. REMOVED DAMAGED SUPPORT BRACKET AND MADE REPAIR PART OF BRACKET PER DRAWING NR A57240194 (P/N A57240194200). INSTALLED NEW PART OF BRACKET WITH FASTENERS IAW SRM 57-51-11 AND 51-72Mar 2, 2011 · N743FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA201103020813Structure · delaminatedRIGHT SIDE AND LEFT SIDE WERE FOUND WATER INDICATION REF TO NDT EXPERT INSPECTION REPORT EXP:1102115-1, IAW NTM 55-4 0-07 PB10. 5 POINTS LOCATED AT APPENDIX 2: CUT 5.5 INCH BY 3.5 INCH, APPENDIX 3: CUT 5.5 INCH BY 4.5 INCH, APPENDIX 4: CUT DIZ.4 INCH, APPENDMar 2, 2011 · N743FD · Airbus A300B4622R · Rudder StructureSDR FDEA201103020812Bracket · crackedLT WING T/E CTR AND OTBD FLAP ATTACH AREA FOUND 2 ANGLE GOT BROKEN. REPLACED DAMAGED BRACKET BY NEW BRACKET WITH RIVET REF TO AB6 STM 51-40-21.Mar 2, 2011 · N743FD · Airbus A300B4622R · Wing, Attach FittingsSDR FDEA201103020811Bracket · crackedRT WING OUTER FLAP T/E INBD SIDE 1 SEAL BRACKET BROKEN REPLACED DAMAGED BRACKET BY NEW BRACKET WITH RIVET REF TO SRM 51-40-21.Mar 2, 2011 · N743FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201103020810Bracket · crackedRT WING CENTER FLAP T/E OTBD SIDE 1 SEAL BRACKET BROKEN. REPLACED DAMAGE BRACKET BY NEW BRACKET WITH RIVET REF TO AB6 SRM 51-40-21.Mar 2, 2011 · N743FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201103010803Support Angle · crackedRT WING T/E AREA 1 EA SUPPORT ANGLE CRACKED POSITION UNDER NR 3 SPOILER INBD SIDE. REMOVED DAMAGED ANGLE AND MADE REPAIR PART OF ANGLE IAW DWG A57240073 PN A57240073201. INSTALLED NEW SUPPORT ANGLE WITH FASTENERS IAW SRM 57-51-11 AND 51-72-10.Mar 1, 2011 · N743FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA201103010802Support Angle · crackedLT WING UPPER T/E FIXED PANEL 1EA SUPPORT ANGLE GOT CRACKED AT NR 4 SPOILER OTBD HINGE. REMOVED DAMAGED ANGLE AND MADE REPAIR PART OF ANGLE IAW DWG A57240194 PN A57240194201. INSTALLED NEW PART OF ANGLE WITH FASTENERS IAW AB6 SRM 57-51-11 AND 51-72-10.Mar 1, 2011 · N743FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA201103010801Support Bracket · crackedRT WING T/E AREA 1EA SUPPORT BRACKET CRACKED POSITION UNDER NR 3 SPOILER INBD SIDE. REMOVED DAMAGED BRACKET AND MADE REPAIR PART OF BRACKET IAW DWG A57240071, PN A57240071-201. INSTALLED NEW BRACKET WITH FASTENERS IAW SRM 57-51-11 AND 51-72-10.Mar 1, 2011 · N743FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA201103010800Rib · crackedLT WING INBD FLAP INSP FOUND THE HORIZONTAL UPPER FLANGE OF RIB 25A IN THE UPPER FLANGE OF RIB 25A IN THE UPPER RADII CRACKED. REPLACED DAMAGED RIB BY NEW RIB WITH FASTENER REF TO EO E6-5750-7-5003 PT1 (WINGS- INBD FLAP REINFORCEMENT OF RIB 25A) REPAIR.Mar 1, 2011 · N743FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201102280793Tube · missingPFM 1C CHECK FOUND HOSE TUBE WAS MISSING AT FR38-FR40 OF LEFT WALL OF M/D COMPLIED WITH EA 6-2610-149002 AND CHECK CONDITION IS NORMAL IAW GMM 6-2-100. REPAIR CLASSIFIED AS MINOR.Feb 28, 2011 · N743FD · Airbus A300B4622R · Fuselage Structure (General)SDR FDEA201007082405Landing Gear · malfunctionedGEAR WOULD NOT RETRACT ON T/O. SWITCHED TO SYS 1, NO JOY. COMPLIED WITH QRH. RETURNED FIELD. ALSO PITCH TRIM NR 2, ATS, NR 1 PRESSURE REGULATOR FAULTED AT SAME TIME. PILOT ATTEMPTED TO THROW THE HANDLE, WOULD NOT GO PAST HALFWAY. THEN GOT ECAM INDICATIONJul 8, 2010 · N743FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR FDEA200912234504Warning Light · illuminatedON TAKEOFF, COMPLETED TAKEOFF CONFIGURATION TEST PRIOR TO TAKEOFF (WAS NORMAL) GOT AN UNSAFE CONFIGURATION FOR TAKEOFF ECAM WARNING. REJECTED TAKEOFF FOUND PARKING BRAKE LEVER UP ABOUT 1 INCH. COMPLETED CHECKLISTS- NEXT TAKEOFF NORMAL. OPERATED PARKING BDec 23, 2009 · N743FD · Airbus A300B4622R · Central WarningSDR FDEA200911254172Handle · failedLANDING GEAR WOULD NOT RETRACT IN SYS 1. RETRACTED USING SYS 2, ONLY AFTER SEVERAL SECONDS DELAY. ELECTED TO EXTEND GEAR AND RE-RETRACTED USING SYS 2 TO TEST THE SYS BEFORE CONTINUING TO DESTINATION. GEAR WOULD NOT RETRACT USING EITHER SYS. REMOVED AND REPNov 25, 2009 · N743FD · Airbus A300B4622R · Landing Gear SelectorSDR FDEA200907292830Thrust Reverser · inoperativeON TAKEOFF PWR APPLICATION NR1 REV UNLOCK LIGHT ILLUMINATED. ABORTED TAKEOFF AT 23KTS. "MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) NR 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FWD THRUST POSITION." REMOVED AND REPLACED THE THRUST REVERSER PRJul 29, 2009 · N743FD · Airbus A300B4622R · Engine Thrust ReverserSDR 08FDEA03572Vane · damagedKRUEGER FLAP VANE WAS DAMAGED DURING FUNCTION CHECKS. REPAIR PERFORMED BY REPLACEMENT OF KRUEGER FLAP VANE ASSY IAW AMM 27-87-12/401.Aug 25, 2008 · N743FD · Airbus A300B4622R · Leading Edge Devices
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