N746FD

Service difficulty reports · 234

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 = 'N746FD' 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 FDEA201401080093Cover · leakingFUEL LEAK INDICATED BY EXCESSIVE DECREASE OF FUEL IN RT INNER TANK. FUEL LEAK FROM NR 2 ENGINE CONFIRMED BY GROUND CREW AFTER LANDING. R & R NR 2 ENGINE FUEL FILTER COVER, DRAIN PLUG & FILTER IAW AMM 73-12-03-04, PERFORMED GROUND IDLE RUN IAW JRH, NO LEAKS Jan 8, 2014 · N746FD · Airbus A300B4622R · Engine Fuel DistributionSDR FDEA201401080072Cover · leakingFUEL LEAK INDICATED BY EXCESSIVE DECREASE OF FUEL IN RT INNER TANK. FUEL LEAK FROM NR 2 ENG CONFIRMED BY GROUND CREW AFTER LANDING. REMOVED AND REPLACED NR 2 ENGINE FUEL FILTER COVER, DRAIN PLUG AND FILTER IAW AMM 73-12-03-04, PERFORMED GROUND IDLE RUN PERJan 8, 2014 · N746FD · Airbus A300B4622R · Engine Fuel DistributionSDR FDEA201111295073Longeron · crackedPANEL 485AL, TOP ATTACH ANGLE ON LT SIDE, 8TH HOLE FWD HAS A CRACK APPROX 3" LONG, JUST BELOW IT. R & R LT LONGERON ANGLE ON PANEL 485AL IAW SRM 54-55-51, FIG 205 AND SRM 51-40-21.Nov 29, 2011 · N746FD · Airbus A300F4605R · Nacelle/Pylon, Longeron/StringerSDR FDEA201111245018Web · deformedINSIDE TAIL COMPARTMENT BETWEEN FR 86 AND 87 AT STR 36R WEB PANEL IS DEFORMED. R & R DEFORMED WEB ON FR 86 AND 87 AT STR 36R IAW SRM 51-40-21.Nov 24, 2011 · N746FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201111245017Web · deformedINSIDE TAIL SECTION BETWEEN FR 86 AND 87 AT STR 33R WEB PANEL IS DEFORMED. R & R DEFORMED WEB SECTION IAW SRM 51-40-21, PG 7 AT FR 86 AND 87 STR 33R.Nov 24, 2011 · N746FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201111225000Channel · crackedAVIIONICS COMPARTMENT RT SIDE AT FR 16 AND FR 17 BATTERY STORAGE RACK HAS CRACK IN HAT CHANNEL. R & R HAT CHANNEL ON BATTERY STORAGE RACK IAW SRM 51-40-21.Nov 22, 2011 · N746FD · Airbus A300B4622R · Battery Box StructureSDR FDEA201111184965Support · crackedNR 2 PYLON UPPER L/E INBD FOLDED SHEET METAL SUPPORT AT RIB J1/STA 422 HAS 2" CRACK. REMOVED METAL SUPPORT AT NR 2 PYLON UPPER L/E INBD AT RIB J1/STA 422 IAW SRM 51-40-21, LOCATED AND DRILLED SHEET METAL NEW SUPPORT IAW SRM 51-40-21 & INSTALLED IAW SRM 51-4Nov 18, 2011 · N746FD · Airbus A300B4622R · Nacelle/Pylon Miscellaneous StructureSDR FDEA201111174945Rib · crackedNR 4 RT SPOILER OTBD HINGE RIB HAS 1EA CRACK APPROX .250 INCHES LONG IN FWD BOTTOM RADIUS. R & R HINGE RIB ON NR 4 RT SPOILER CUTOUT IAW SRM 51-72-10, PARA 5A AND 6A. REPROTECTED FASTENERS IAW SRM 51-75-10, PG 206.Nov 17, 2011 · N746FD · Airbus A300B4622R · SpoilersSDR FDEA201111174944Web · crackedINSIDE TAIL COMPARTMENT ADJACENT TO ACCESS DOOR BETWEEN FR 85 AND 86 AT STR 33R WEB PANEL IS DEFORMED. R & R WEB & STRAP IN TAIL COMPARTMENT BETWEEN FRAME 85 & 86 AT STR 33R IAW SRM 51-40-21, 51-40-44 & 51-42-10, PARA 5A & 6A. REPROTECTED IAW SRM 51-23-10 & Nov 17, 2011 · N746FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201111124887Web · crackedRT WEB ASSY STR 27 HAS A 1.37 INCH CRACK. R & R WEB ASSY IAW SRM 51-72-10 AND SRM 51-40-21.Nov 12, 2011 · N746FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201111124886Floorboard · damagedFLOORBOARD 161GF HAS 3 EA PUNCTURES 1 IN LONG AND 1 EA, 3 IN LONG. FABRICATED REPLACEMENT FLOORBOARD 161GF IAW DWGS SRZ 25-005, REV J.Nov 12, 2011 · N746FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201111104872Floorboard · crackedFLOORBOARD 241SH IS CRACKED ENTIRE WIDTH OF FLOORBOARD ON LOWER SIDE AT FWD CLEVIS ADAPTER 20" WIDE. FLOORBOARD 251SH FABRICATED NEW IAW DWG SRZ25-005 REV J.Nov 10, 2011 · N746FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201111104863Floorboard · crackedFLOORBOARD 241TH IS CRACKED ENTIRE WIDTH ON LOWER SIDE AT FWD. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ25-005, REV J.Nov 10, 2011 · N746FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201111044753Floor Panel · crackedFLOOR PANEL 242WH, COMPOSITE STRUCTURE IS CRACKED 2 PLACES. FABRICATED FLOOR PANEL 242WH IAW DWG SRZ25-005, REV J, MAJOR REPAIR IAW GMM6-2-100.Nov 4, 2011 · N746FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201111034742Floorboard · damagedFLOORBOARD, 241DF HAS 2 EA BROKEN CORNERS AROUND CLEVIS ADAPTER CUT-OUT DEFECT MEASURES 6 INCHES TOTAL FABRICATED REPLACEMENT PANEL 241DF IAW DWG SRZ 25-005, REV J, MAJOR REPAIR IAW GMM 6-2-100.Nov 3, 2011 · N746FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201111034741Floorboard · crackedFLOOR BOARD PNKL231EF HAS CRACK ACROSS PNL FABRICATED REPLACEMENT PANEL 231EF IAW DWG SZ-25-005 REV J MAJOR REPAIR IAW FED- EX GMM 6-2-100Nov 3, 2011 · N746FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201111034739Floorboard · crackedFLOORBOARD 262NF HAS A UNDER CRACK RUNNING THE WIDTH OF BOARD. FLOORBOARD 262NF FABRICATED IAW DWG SRZ 25-005, REV J, MAJOR REPAIR IAW GMM 6-2-100.Nov 3, 2011 · N746FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201111034738Floorboard · crackedMAIN DECK FLOORBOARD 241KJ HAS 5 CRACKS AND 1 CORNER THAT IS BROKEN OFF. FABRICATED REPLACEMENT PANEL 241KJ IAW DWG SR-25-005, REV J, MAJOR REPAIR IAW GMM6-2-100.Nov 3, 2011 · N746FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201111034732Floor Panel · crackedFLOORBOARD 241MF HAS A BROKEN CENTER AT CLEVIS ADAPTER CUT-OUT DEFECT MEASURES 1" LONG. FABRICATED REPLACEMENT FLOOR PANEL 241MF IAW DWG SRZ 25-005, REV J.Nov 3, 2011 · N746FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201111024728Floorboard · damagedFLOORBOARD 242LK COMPOSITE PANEL BROKEN FABBED FLOORBOARD PANEL 242LK IAW DWG SR 25-005, REV J, MAJOR REPAIR IAW GMM 6-2-100.Nov 2, 2011 · N746FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201111024727Floorboard · crackedMAIN DECK FLOORBOARD, 241VG HAS 3 CRACKS AND 1 CORNER BROKEN OFF FABBED FLOORBOARD PANEL 241VG IAW DWG SRZ 25-005, REV J, MAJOR REPAIR IAW GMM6-2-100.Nov 2, 2011 · N746FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201111024726Floorboard · crackedMAINDECK FLOORBOARD 251RG HAS FIVE CRACKS FROM 1'" TO 3.5"LONG FABRICATED REPLACEMENT PANEL 251RG IAW DWG SR 25-005 REV J, MAJOR REPAIR IAW GMM 6-2-100.Nov 2, 2011 · N746FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201111024725Floorboard · crackedMAIN DECK FLOORBOARD 251SH HAS 2 CRACKS, AFT INBD EDGE HAS 1" CRACK, AFT OTBD EDGE HAS 4" CRACK FABRICATED REPLACEMENT PANEL 251SH IAW DWG SR 25-005, REV J MAJOR REPAIR IAW GMM6-2-100.Nov 2, 2011 · N746FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201106242406Bushing · dischargedMLG WOULD NOT COME UP IN POSITION DETENT NR 1 & 2. HANDLE WOULD ONLY RAISE TO THE MIDDLE POSITION AND GEAR SHOWED 3 GREEN WITH3 RED UNLOCK LIGHT. WHEN HANDLE PLACED DOWN, WE SHOWED 3 GREEN WITH THE UNLOCK LIGHT OUT. PROX BOX FAULT CODES ARE 70 "BOX" & BR Jun 24, 2011 · N746FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR FDEA201102010447Selector Valve · failedGEAR FAILED TO RETRACT ON SYS 1. (SYS 2 UNDER MEL) ADJUSTED LT AND RT MLG 62GB, 63GB, 64GB, 65GB SENSOR GAPS REF AMM 32-00-00-4. R & R LANDING GEAR CONTROL HANDLE MODULE (2GA) IAW AMM 32-31-11-04 THROUGH STEP 2.C, STILL REQUIRES TEST (STEP 2.D). R & R LANFeb 1, 2011 · N746FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR FDEA201006081869Clamp · failedSMOKE IN ACFT. APU AUTO SHUTDOWN. APU OIL QTY IS ZERO ON FLT DECK GUAGE & READING ZERO IN THE APU BAY. APU OIL QTY AT BLOCKING READING OVER HALF FULL. DUE TO SMOKE & ODOR OF OIL FROM BOTH PACKS. C/W MM 21-51-00-3 AND R & R BOTH PACK COALESCER BAGS. REFJun 8, 2010 · N746FD · Airbus A300B4622R · APU Oil SystemSDR FDEA200907022457Skin · damagedFOUND ON RH WING LOWER SKIN PANEL RIB 9 AFTER DOUBLER REMOVAL SOME DAMAGES IN FASTENER HOLES IN THIS AREA. REPAIR PERFORMED BY NDT INSPECTION FOR CRACKS, OVERSIZING OF HOLES AND REINSTALLING DOUBLER IAW. RAS/BAE/1009704/2009 ISS.A , APPROVED BY EA 6-5710-13Jul 2, 2009 · N746FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907022456Skin · damagedFOUND ON LH WING LOWER SKIN PANEL RIB 9 AFTER DOUBLER REMOVAL SOME DAMAGES IN FASTENER HOLES IN THIS AREA. REPAIR PERFORMED BY NDT INSPECTION FOR CRACKS , OVERSIZING OF HOLES AND DRILL MISSING HOLE 38 IAW. SB 57-6064 AND REINSTALLING DOUBLER IAW. RAS/BAE/1Jul 2, 2009 · N746FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907022451Fitting · wornFOUND FOUND DAMAGED HOLES AT LOWER JUNCTION FRAME C 47 RT. REPAIR PERFORMED BY REAM UP THE HOLES IAW. RAS 70519233/123/2009 ISSA, APPROVED BY EA 6-5710-131258.Jul 2, 2009 · N746FD · Airbus A300B4622R · Wing, Attach FittingsSDR FDEA200907022450Fitting · wornFOUND FOUND DAMAGED HOLES AT LOWER JUNCTION FRAME C 47 RT REPAIR PERFORMED BY REAM UP THE HOLES IAW. RAS 70519233/123/2009 ISSA, APPROVED BY EA 6-5710-131258.Jul 2, 2009 · N746FD · Airbus A300B4622R · Wing, Attach FittingsSDR FDEA200907022449Fitting · wornFOUND FOUND DAMAGED HOLES AT LOWER JUNCTION FRAME C 47 LT REPAIR PERFORMED BY REAM UP THE HOLES IAW. RAS 70519233/123/2009 ISSA, APPROVED BY EA 6-5710-131258.Jul 2, 2009 · N746FD · Airbus A300B4622R · Wing, Attach FittingsSDR FDEA200907022448Fitting · wornFOUND DAMAGED HOLES AT LOWER JUNCTION FRAME C 47 LT REPAIR PERFORMED BY REAM UP THE HOLES IAW. RAS 70519233/123/2009 ISSA, APPROVED BY EA 6-5710-131258.Jul 2, 2009 · N746FD · Airbus A300B4622R · Wing, Attach FittingsSDR FDEA200907022447Web · misrepairedFOUND OLD SPLICE REPAIR ON FLOOR SUPPORT C 15-15A, Y-1959, NOT PERFORMED IAW. SRM. SPLICE REPAIR RENEWED IAW. SRM 53-12-15 FIG.207.Jul 2, 2009 · N746FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200907022446Fitting · damagedIT WAS NOT POSSIBLE TO FIT THE NEW MLG REACTION ROD ON RT SIDE. REPAIR PERFORMED BY REPLACEMENT OF AFT PICK UP ROD FITTINGS WITH OVERSIZED FASTENERS AND SKIN REAMED UP IAW. RAS/BAE/1009726/2009 ISS. A, APPROVED BY EA 6-5710- 131243.Jul 2, 2009 · N746FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200907022445Fitting · damagedIT WAS NOT POSSIBLE TO FIT THE NEW MLG REACTION ROD ON RT SIDE. REPAIR PERFORMED BY REPLACEMENT OF FWD PICK UP ROD FITTINGS WITH OVERSIZED FASTENERS AND SKIN REAMED UP IAW. RAS/BAE/1009726/2009 ISS. A, APPROVED BY EA 6-5710-131243.Jul 2, 2009 · N746FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200907012434Skin · wornFOUND ELONGATED HOLES ON PYLON SUPPORT BRACKETS AND BOTTOM SKIN LT WING BUSH REPAIR PERFORMED IAW DRAWING R571-50532 AND SB A300-29-6058, APPROVED BY RAS/BAE/101319/2009 ISS A AND EA 6-2900-131225.Jul 1, 2009 · N746FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907012433Skin · wornFOUND ELONGATED HOLES ON PYLON SUPPORT BRACKETS AND BOTTOM SKIN RT WING BUSH REPAIR PERFORMED IAW DRAWING R571-50532 AND SB A300-29-6058, APPROVED BY RAS/BAE/101319/2009 ISS A AND EA 6-2900-131225.Jul 1, 2009 · N746FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907012432Structure · delaminatedFOUND DELAMINATION AROUND ROLLER BLOCKS ON FLAP DEFLECTOR DOORS, INNER AND OUTER SHROUD BOXES, RT WING. REPAIR PERFOREMD BY BONDING REPAIR IAW SRM 51-77-12 AND REINSTALLATION OF ROLLER BLOCKS IAW RAS/BAE/1009227/2009 ISS. A, APPROVED BY EA 6-5750-120223.Jul 1, 2009 · N746FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200907012431Structure · delaminatedFOUND DELAMINATION AROUND ROLLER BLOCKS ON FLAP DEFLECTOR DOORS, INNER AND OUTER SHROUD BOXES, LT WING. REPAIR PERFORMED BY BONDING REPAIR IAW SRM 51-77-12AND REINSTALLATION OF ROLLER BLOCKS IAW RAS/BAE/1009227/2009 ISS A, APPROVED BY EA 6-5750-120223.Jul 1, 2009 · N746FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200907012430Skin · chafedFOUND CHAFING MARKS ON LT CENTER FLAP TOP SKIN BETWEEN RIB 13-15. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARK IAW RAS/FOK/067/2009 ISS. B, APPROVED BY EA 6-5750-129120.Jul 1, 2009 · N746FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200907012429Skin · chafedFOUND CHAFING MARKS ON LT OUTER FLAP TOP SKIN BETWEEN RIB 15-15A. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARK IAW RAS/FOK/074/2009 ISS. C, APPROVED BY EA 6-5750-129184.Jul 1, 2009 · N746FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200907012428Skin · chafedFOUND CHAFING MARKS ON RT OUTER FLAP TOP SKIN BETWEEN RIB 15-15A. REPAIR PERFORMED BY BLENDING OUT THE CHAFING MARK IAW RAS/FOK/075/2009 ISS. C, APPROVED BY EA 6-5750-129183.Jul 1, 2009 · N746FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200906302410Skin · damagedFOUND DAMAGED AND ELONGATED HOLES ON RT INBOARD FLAP RIB 25A AND SB 57-6098 NOT PROPERLY INSTALLED. REPAIR PERFORMED BY REPLACEMENT VARIOUS PARTS ON RIB 25A AND CUT OUT THE SKIN AND INSTALLING A REPAIR PATCH IAW. RAS/FOK/139/2009 ISS. B, APPROVED BY EA 6-5750-Jun 30, 2009 · N746FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200906302409Sill · corrodedFOUND CORRSION IN HOLES OF FWD CARGO DOOR SILL BEAM REPAIR PERFORMED BY BUSH REPAIR IAW. RAS/EFW/9000161/2009 IS. B, APPROVED BY EA 6-5310-129117.Jun 30, 2009 · N746FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200906302399Shroud · corrodedFOUND CORROSION ON RT WING OUTER SHROUD BOX UPPER SKIN. REPAIR PERFORMED BY CUT RIBS TO GAIN ACCESS, REMOVAL OF CORROSION AND NDT FOR CRACK FREE CONDITION IN HOLES AND INSTALLING SKIN AND RIBS IAW. RAS/BAE/1009669/2009 ISS.A , APPROVED BY EA 6-5740-131250Jun 30, 2009 · N746FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200906302398Shroud · corrodedFOUND CORROSION ON LT WING OUTER SHROUD BOX UPPER SKIN. REPAIR PERFORMED BY CUT RIBS TO GAIN ACCESS, REMOVAL OF CORROSION AND NDT FOR CRACK FREE CONDITION IN HOLES AND INSTALLING SKIN AND RIBS IAW. RAS/BAE/1010050/2009 ISS.A , APPROVED BY EA 6-5740-131249.Jun 30, 2009 · N746FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200906302395Skin · corrodedFOUND CORROSION ON SKIN PANELS C 92-95, P 9-14 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 30, 2009 · N746FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200906302392Fitting · corrodedFOUND CORROSION ON PYLON NR 2 SPIGOT FITTING. REPAIR PERFORMED BY REPLACEMENT OF FITING IAW SB 54-6017, APPROVED BY EA 6-5440-120196.Jun 30, 2009 · N746FD · Airbus A300B4622R · Nacelle/Pylon, Main FrameSDR FDEA200906252297Cover · crackedFOUND ON SPOILER NR 4 CRACK IN OTBD HINGE COVER. REPAIR PERFORMED IAW SRM 57-72-11, APPROVED BY RAS/DABRE/7010747/2009 ISS. B, APPROVED BY EA 6-5720-129169.Jun 25, 2009 · N746FD · Airbus A300B4622R · SpoilersSDR FDEA200906252296Cover · crackedFOUND ON SPOILER NR 3 CRACK IN OTBD HINGE COVER. REPAIR PERFORMED IAW SRM 57-72-11, APPROVED BY RAS/DABRE/7010746/2009 ISS. B, APPROVED BY EA 6-5720-129168.Jun 25, 2009 · N746FD · Airbus A300B4622R · Spoilers
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