N749FD

Service difficulty reports · 180

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 = 'N749FD' 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 FDEA201612214512Battery Pack · inoperativeDURING CRUISE AT FL 330, R1 DOOR ALARM AND FLASHIG RED WARNING LIGHT. NO ECAM WARNINGS AND NO CABIN PRESSURE CHANGE, RED FLASHING WARNING LIGHT EXTINGUISHED DURING DESCENT BELOW FL 180. IAW AMM: 52-73-18-04 REMOVED AND REPLACED NR 2 AUTONOMOUS STANDBY POWDec 21, 2016 · N749FD · Airbus A300B4622R · Door Warning SystemSDR FDEA201612194495Servo Valve · leakingLOST YELLOW SYS HYD FLUID 20 MINUTE AFTER LEVEL OFF AT ALTITUDE. FOUND HYD FLUID TO BE LEAKING FROM SERVO VALVE ASSY ON NR 5 SPOILER ACTUATOR.Dec 19, 2016 · N749FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA201612074356Warning System · activatedAT CRUISE FL 360, THE R1 SLIDE ARMED WARNING LIGHT ILLUMINATED FLASHING. NO AUDIBLE WARNING. LIGHT WENT OUT SOMETIME DURING DECENT. RELEASED FOR SERVICE PER MEL 52-73-01-01. R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS INOP. OK TO CONTINUE.Dec 7, 2016 · N749FD · Airbus A300B4622R · Door Warning SystemSDR FDEA201611164034Seat Track · wornMDCC FRAMES 57 - 57.2 SEAT TRACK UPPER SECTION WORN. BLENDED AND SMOOTHED THE AREA IAW SRM 51-73-10 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. CUT OUT THE DAMAGED SECTION IAW SRM 53-10-16-201 FIG 208. FABRICATED A REPAIR SECTION IAW SRM 53-10-16-201 FIG Nov 16, 2016 · N749FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201611093908Seat Track · crackedMDCC FRAME 17 SEAT TRACK FOUND CRACKED. REPLACED THE SEAT TRACK IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Nov 9, 2016 · N749FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201611073878Skin · crackedLEFT WING CENTER FLAP UPPER SKIN AT RIB 26 FOUND CRACKED. CUT OUT LOWER SKIN FOR ACCESS IAW SRM 57-50-00 FIG.205 CUT OUT AWAY THE DAMAGE FLANGE OF THE RIB IAW SRM 57-50-00 FIG.201 INSTALLED AREPAIR ANGLE IAW SRM 57-50-00.Nov 7, 2016 · N749FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201611073877Shear Tie · crackedMAIN DECK CARGO FRAME 46 SHEAR TIE HAD A CRACK SIGNAL BETWEEH STRINGERS 24 - 25R. REPAIRED IAW EA 6-5310-T0329498 PT1.Nov 7, 2016 · N749FD · Airbus A300B4622R · Fuselage Internal Mounting StructureSDR FDEA201611073874Support Beam · corrodedMAIN DECK CARGO FRAMES 10 - 13 SUPPORT BEAM CORRODED. REMOVE CORROSION IAW SRM51-74-10. THE SUPPORT BEAM WAS FOUND DELAMINATED AND REPLACED IAW SRM 51-40-21 THIS IS A MAJOR REPAIR IAW GMM 6-2-100.Nov 7, 2016 · N749FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201611073875Rib · crackedCENTER FUEL TANK FRAME 40 BULKHEAD AFT FACE Y450 RIB FOUND CRACKED. CUT OUT THE DAMAGE IAW SRM 57-10-21 FIG 201. FABRICATED A REPAIR IAW SRM 57-10-21 FIG 201, DWG R57110271 & R57110273 . INSTALLED THE REPAIR IAW SRM 57-10-21 FIG 201. MAJOR REPAIR IAW GMMNov 7, 2016 · N749FD · Airbus A300B4622R · Fuselage Main, BulkheadSDR FDEA201611063856Stringer · corrodedAFT CARGO BAY FRAMES 63 - 64, STRINGER 51R CORRODED. REMOVE CORROSION AND FOUND OUT OF LIMITS IAW DWG A53974202. CUT OUT THE DAMAGED AREA IAW SRM53-10-14 FIG 201 SHT.2 FABRICATED A REPAIR IAW SRM 53-10-14 FIG 201 SHT.2. INSTALLED THE REPAIR IAW SRM 53-10-Nov 6, 2016 · N749FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA201611063855Skin · chafedFUSELAGE EXTERNAL SKIN FOUND A SCRATCH BETWEEN FRAMES 41 - 42 STRINGERS 10 - 11R. REPAIRED IAW SRM 53-10-12-201 PARA 6, FIG 225, SHEET 2, SRM 53-10-12-201 PARA 6, FIG 225, SHEET 1, SRM 51-21-10 AND SRM 51-23-00 5, SRM 53-10-12-201 PARA.6 FIG.225 SHEET 6Nov 6, 2016 · N749FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201608182927Hydraulic System · malfunctionedDURING CRUISE AT FL 340, RECEIVED A HYD BLUE SYS LOW PRESSURE ECAM. HYD PAGE OF ECAM SHOWED 2950 PSI IN THE BLUE SYSTEM, NO OTHER INDICATIONS ON OVERHEAD PANEL AND SYSTEM QUANTITY WAS NORMAL. NO OTHER INDICATION ON HYD BLUE SYSTEM, PRESSURE REMAINED CONSTAug 18, 2016 · N749FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA201604131204Frame · crackedFRAME 40 LT SIDE, ALL THREE HOLES FOUND TO BE CRACKED DURING INSPECTION. REAMED FRAME 40 LT, FITTING UPPER HOLE TO .593 IAW SRM 5-40-44. REAMED MIDDLE HOLE TO .577 IAW SRM 51-40-44. REAMED LOWER HOLE TO .515 IAW SRM 51-40-44. THIS REPAIR IS CLASSIFIED AS AApr 13, 2016 · N749FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201510193288Slide · inoperativeRIGHT ENTRY DOOR SLIDE WILL NOT ARM. CREW ENTRY ESCAPE SLIDE INOPERATIVE. IF SLIDE TO BE RETAINED ONBOARD, THEN PRIOR TO EACH DEPARTURE MX MUST VERIFY SLIDE STOWED ACCORDING TO PROCEDURES.Oct 19, 2015 · N749FD · Airbus A300B4622R · Escape SlideSDR FDEA201405030929Stringer · corrodedDURING HIDDEN INTERNAL DAMAGE INSPECTION BETWEEN FR 41 & FR 42 FOUND STRINGER 53R HAS CORROSION AS MARKED, ACCESS THRU ACFT BAY AREA. REPAIRED CORRODED STRINGER AT FR 41& 42 STRINGER 53R IAW TD P1 S1 0309 2014 P4 & EA 6-5310-T0307263A P1.May 3, 2014 · N749FD · Airbus A300F4622R · Fuselage Main, Longeron/StringerSDR FDEA201404300897Frame · corrodedDURING INSPECTION, FOUND FRAME 41 CORRODED BETWEEN STRINGERS 52 & 53R. REPAIRED FRAME IAW TDP1S1103092014.Apr 30, 2014 · N749FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201404150734Skin Panel · corrodedLEFT WING UPPER WING PLANK LOWER SKIN JUST FWD & INBD OF RIB 5 IS CORRODED. REPAIRED LT WING UPPER WING PLANK LOWER SKIN INBD OF RIB 5 IAW EA 6-5730-T0307104 REV NO POS 1 DWG R571-50541 ISSUE B PARA E.Apr 15, 2014 · N749FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA201402270420Rib · corrodedLEFT RIB 5 FWD LUG HAS CORROSION IN BORE & FACES. REPAIRED IAW EA 6-5710-T0306603.Feb 27, 2014 · N749FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA201402270419Rib · corrodedRIGHT RIB 5 FWD LUG HAS CORROSION ON FWD FACE & LUG BORE. REPAIRED IAW EA 6-5710-T0306535.Feb 27, 2014 · N749FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA201212284393Windscreen · crackedCLIMBING OUT OF MEM PASSING APPROX 4500' HEARD A "POP", LOOKED UP AND HAD MANY LARGE CRACKS IN CAPTAINS FRONT WINDSCREEN. R & R WINDSHIELD IAW AMM 56-11-11-04.Dec 28, 2012 · N749FD · Airbus A300B4622R · Flight Compartment WindowsSDR FDEA201203070808Connector · shortedABNORMAL NR 1 THRUST REVERSER UNLOCK ON ECAM. DIVERTED IAW QRH. NO ADVERSE YAW OR ROLL ASSOCIATED WITH THRUST REVERSER UNLOCK. ENGINE WAS NOT SHUTDOWN, KEPT AT IDLE POWER. FOUND PIN J ON CONNECTOR D5003P AT J-BOX SHORTED BETWEEN THE CONNECTOR CHASSIS AND PIMar 7, 2012 · N749FD · Airbus A300B4622R · Engine Exhaust System WiringSDR FDEA201202060501Skin · dentedRIGHT WING CENTER FLAP L/E HAS DENT 2" LONG LOCATED BETWEEN FLAP TRACK NR 3 AND NR 4 RT WING CENTER FLAP L/E DENT 2" LONG LOCATED BETWEEN FLAP TRACK NR 3 AND NR 4 , DENT FOUND TO BE OUT OF LIMITS IAW SRM 57 -50-00, FIG 102, P108, CUTOUT DENT, FABRICATED REPAIRFeb 6, 2012 · N749FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201202060500Skin · gougedLEFT INBD FLAP, LOWER SURFACE OF L/E HAS A 3" LONG X .250 WIDE X .015 DEEP GOUGE BETWEEN THE 4TH AND 5 TH RIB STRIP. REPAIRED LT INBD FLAP L/E IAW SRM 57-50-00, FIG 208 AND TRACKING EA E-6-5750-156096.Feb 6, 2012 · N749FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201201270356Skin · gougedLEFT INBD FLAP LOWER SURFACE OF L/E HAS A 3" LONG X .250" WIDE X .015" DEEP GOUGE BETWEEN THE 4TH AND 5TH RUB STRIP. SMOOTHED AND BLENDED GOUGE ON LT INBD FLAP IAW SRM 51-73-10. CHECKED LIMITS. OUT OF LIMITS IAW SRM 57-50-00 FIG 101. CUT OUT DAMAGE ON LT INJan 27, 2012 · N749FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201201250333Seat Track · wornSEAT TRACK LOBE DAMAGED. REPAIRED SEAT TRACK SECTION IAW SRM 53-10-16 PG 213, 214.Jan 25, 2012 · N749FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201201190254Floor Support · crackedMDCC, FR 48 FLOOR SUPPORT STRUCTURE BELOW SEAT TRACK 4R HAS A CRACK FITTING AT OTBD LWR ATTACHMENT. DEFECT MEASURES 1.75". R & R SUPPORT FR 48 RT SEAT TRACK 4 IAW SRM 51-40-21. REPROTECTED AREA IAW SRM. MATCH DRILLED NEW SUPPORT IAW SRM 51-40-40.Jan 19, 2012 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201201160187Seat Track · gougedMDCC SEAT TRACK 4R FR 75 HAS 2 EA GOUGES AT SCALLOPS. DEFECT MEASURES .75" TOTAL. AFTER REMOVAL OF LEVEL 1 CORROSION, SEAT TRACK WAS FOUND TO BE OUT OF LIMITS. REMOVED GOUGES ON SEAT TRACK SCALLOPS FOUND TO BE OUT OF LIMITS IAW ARM 51-73-10, SRM 53-10-16Jan 16, 2012 · N749FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201201150179Profile · corrodedBULK PIT PROFILE BETWEEN FRAMES 65 AND FR 66 HAS 6 EA NUTPLATES CORRODED AND CORROSION AROUND THE HOLES ON NR 1 PROFILE LT SIDE. REMOVED LEVEL 1 CORROSION IN BULK PIT ON NR 1 PROFILE BETWEEN FR 65 AND FR 66 IAW SRM 51-74-10. FOUND PROFILE TO HAVE EXFOLIATIONJan 15, 2012 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201201140175Adapter · crackedCLEVIS ADAPTER AT FR 57.2 BETWEEN SEAT TRACKS 4L & 5L HAS 1EA CRACK APPROX 1.5" LONG ON OTBD SCALLOP TOP SURFACE THROUGH A FASTENER. REMOVED DAMAGED CLEVIS ADAPTER FROM FR 57.2 BETWEEN SEAT TRACK 4L & 5L AND INSTALL NEW CLEVIS ADAPTER IAW SRM 51-72-10, PARAJan 14, 2012 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201201140174Adapter · damagedMDCC CLEVIS ADAPTER AT FR 57.3 BETWEEN SEAT TRACKS 4L & 5L HAS A BULGE IN THE OTBD SCALLOP UPPER SURFACE MEASURING APPROX 0.5"W X 0.025"H. R & R CLEVIS ADAPTER AT FR 57.3 BETWEEN SEAT TRACK 4L & 5L IAW SRM 51-72-10. REPROTECTED IAW SRM 51-75-10 CPC APPLICATIJan 14, 2012 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201201140173Profile · crackedFWD CARGO COMPARTMENT BETWEEN FR 38.1 AND FR 38.2, RT BOTTOM SIDEWALL PANEL LOWER EDGE LANDING PROFILE CRACKED (3" LONG) FWD CARGO COMPARTMENT BETWEEN FRAME 38.1 AND 38.2. RT BOTTOM SIDEWALL PANEL PROFILE REPAIRED CRACK IAW SRM 51-71-30, NDT VERIFIED CRACK. Jan 14, 2012 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201201140171Seat Track · gougedSEAT TRACK 2L BETWEEN FRAMES 42 AND 43 SCALLOP IS GOUGED. BLENDED OUT GOUGE BETWEEN FR 42 & 43 AT 2L IAW SRM 51-73-10. OUT OF LIMITS IAW 53-10-16, FIG 101 .53W X .76L X .88D. R & R TRACK AT 2L FROM FR 40 TO 45 IAW SRM 51-72-10. PARA 5A & 6A. REPROTECTED IAJan 14, 2012 · N749FD · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201201110099Stringer · corrodedCARGO BAU RT SIDE FR 38.2, 10" STRINGER 45 HAS 3 SQ INCHES OF CORROSION ON OTBD SIDE. REMOVED LEVEL 1 CORROSION ON STRINGER AND WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA OF STRINGER. FABRICATED REPAIR PARTS, PRIMED, INSTALLED AND REPROTECTED IAWJan 11, 2012 · N749FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA201201100077Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT PROFILE BETWEEN FR 64 & FR 65, 20 IN AFT OF L-1 ROLLER TRACK HAS CORROSION IN & AROUND 2 EA FASTENER HOLES.Jan 10, 2012 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201201070039Adapter · crackedCLEVIS ADAPTER AT FR 61 BETWEEN SEAT TRACK 4L AND 5L HAS SCALLOP SECTION BROKEN OFF. R & R CLEVIS ADAPTER AT FR 61 BETWEEN SEAT TRACK 4L AND 5L IAW SRM 51-72-10, PG 1-3 AND SRM 51-40-21, PAR 5.Jan 7, 2012 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201201050025Floor Panel · crackedFLOOR PANEL 152EF HAS A 12" CRACK ON UPPER SURFACE FABRICATED REPLACEMENT FLOOR PANEL 152EF IAW DWG SRZ 25-005, REV J.Jan 5, 2012 · N749FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201201050023Floor Panel · damagedFLOOR PANEL 132 QF HAS 20" OF EDGE DAMAGE AND DELAMINATION. FABRICATED REPLACEMENT FLOOR PANEL 132 QF IAW DWG SRZ 25-005, REV J.Jan 5, 2012 · N749FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201201050022Floorboard · crackedFLOORBOARD 252HH CRACKED 8 IN AT LWR SURFACES FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.Jan 5, 2012 · N749FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201201040015Floorboard · damagedFLOORBOARD 252 YH HAS MISSING BROKEN COMPOSITE MATERIAL NR LWR SECTION DEFECT MEASURES 3.25 INCHES. FABRICATED REPLACEMENT PANEL 252 YH IAW FED-EX DWG SRZ 25-005, REV J.Jan 4, 2012 · N749FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201201030007Floor Panel · delaminated8 EA AREAS ON FLOOR PANEL 131, YF EDGE WHERE SKIN IS DELAMINATED AND TORN. FABRICATED REPLACEMENT FLOOR PANEL 131YF IAW DWG SRZ 25-005, REV J.Jan 3, 2012 · N749FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201201030006Floor Panel · crackedFLOOR PANEL 251ZG HAS 1EA, 11" CRACK. FABRICATED REPLACEMENT FLOOR PANEL 251ZG IAW DWG SRZ 25-005, REV J.Jan 3, 2012 · N749FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201201030005Floor Panel · damagedFLOOR PANEL 251 RG IS BROKEN ACROSS FULL WIDTH OF PANEL APPROX 20" FWD OF AFT EDGE FABRICATED REPLACEMENT PANEL 251 RG IAW DWG SRZ 25-005, REV J.Jan 3, 2012 · N749FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201201010449Adapter · wornMDCC FRAME 54.1, BETWEEN SEAT TRACK 4L AND 5L, CLEVIS ADAPTER HAS WORN SCALLOP (APPROX 1 SQ. IN AREA). REMOVED DAMAGED AREA FROM CLEVIS ADAPTER AT FR 54.1, BETWEEN Y1959 AND Y1456, FOUND CLS ADAPTER TO BE OUT OF LIMITS IAW SRM 53-10-15 FIG 101. R & R CLEVIJan 1, 2012 · N749FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA03385Actuator · failedNR 1 ENG COMPRESSOR STALL BEGINNING DESCENT FROM FL350 ENG WOULD NOT RESTART. WINDMILLING WITHOUT OIL PRESSURE WAS 15 MINUTES. REMOVED AND REPLACED THE STATOR VANE ACTUATOR .Aug 12, 2008 · N749FD · Airbus A300B4622R · Engine Air Intake SystemSDR 08FDEA03191Hose · damagedTOTAL LOSS OF GREEN HYD SYSTEM ON SHORT FINAL GEAR DOWN FLAPS 40 DEGREES DECLARED EMERGENCY LANDED USED DIFF BRAKING STOPPED ON CENTERLINE MAINTENANCE PINNED AND TOWED TO GATE. TURNED PUMPS OFF WHEN DIRECTED BY ECAM BEFORE LANDING. FOUND LT FLEX LINE AT TOJul 30, 2008 · N749FD · Airbus A300B4622R · Hydraulic System, MainSDR 07FDEA04614Skin Panel · corrodedFOUND CORROSION ON TOP SKIN LT WING RIB 25-29 AROUND FASTENER HOLES REPAIR PERFORMED BY BLEND OUT CORROSION, OVERSIZING THE HOLES, FLAP PEENING AND NDT FOR CRACK FREE IAW EA 6-5720-112521 AND RAS/BAE/1005138/2007 ISS A.Oct 17, 2007 · N749FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA04613Skin Panel · corrodedFOUND CORROSION ON LT WING TOP SKIN OVER THE WHOLE WING AREA IN AREA OF FASTENER HOLES REPAIR PERFORMED BLEND OUT THE CORROSION, FLAP PEENING AND NDT FOR CRACK FREE IAW EA 6-5720-112521 AND RAS/BAE/1005138/2007 ISS A.Oct 17, 2007 · N749FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA04607Skin Panel · corrodedFOUND CORROSION ON RT TOP SKIN ON WHOLE AREA AROUND FASTENER HOLES. REPAIR PERORMED BY BLENDOUT CORROSION, OVERSIZING THE HOLES AND FLAP PEENING IAW EA 6-5720-112522 AND RAS/BAE/1005287/2007 ISS A.Oct 16, 2007 · N749FD · Airbus A300B4622R · Trailing Edge FlapsSDR 07FDEA04599Skin Panel · corrodedFOUND CORROSION ON RT WING LEADING EDGE BOTTOM SKIN UPPER SURFACE AND RIB NEAR TRACK NR 7. REPAIR PERFORMED BY BLEND OUT THE CORROSION AND OVERSIZING THE HOLES IAW EA 6-5741-106528 AND RAS BAE/1005113/2007 ISS A.Oct 15, 2007 · N749FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA04598Skin Panel · corrodedFOUND CORROSION ON RT WING LEADING EDGE BOTTOM SKIN UPPER SURFACE AND RIB NEAR TRACK NR 5-7 REPAIR PERFORMED BY BLEND OUT THE CORROSION AND OVERSIZING THE HOLES IAW EA 6-5741-106528 AND RAS BAE/1005113/2007 ISS A.Oct 15, 2007 · N749FD · Airbus A300B4622R · Wing, Plate/Skin
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