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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA202603230366Skin · damagedRUDDER LEFT SIDE PANEL LEADING EDGE INTERNAL STRUCTURE BETWEEN STA869/BR7 AND UPR EDGE FOUND WATER INGRESS. DAMAGE AT RUDDER LEFT SIDE PANEL LEADING EDGE INTERNAL STRUCTURE BETWEEN STA869/BR7 AND UPR EDGE PER A300-600 SRM55-41-12-201 PARA.30 FIGURE 219.SDR FDEA202603010299Rib · crackedRIGHT WING CENTER FLAP RIBS UPR FLANGE FOUND 3EA CRACKS AT RIB25 BETWEEN STGR2.7 AND REAR SPAR, RIB26 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 3EA CRACKS OF RIB25 AND 26 BETWEEN STGR2SDR FDEA202603010298Rib · crackedRT WING CENTER FLAP RIBS UPR FLANGE FOUND 3EA CRACKS AT RIB18 BETWEEN STGR2.7 AND REAR SPAR, RIB19 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 3EA CRACKS OF RIB18 AND 19 BETWEEN STGR2.7 SDR FDEA202603010297Rib · crackedRT WING CENTER FLAP RIBS UPR FLANGE FOUND 7EA CRACKS AT RIB11 BETWEEN S2.6 AND REAR SPAR, RIB12 BETWEEN STGR2.7 & REAR SPAR, RIB13 BETWEEN S2.6 AND S2.8 COMPLIED WITH EA 6-5750-T0325371 A REPAIRED THE RH WING CENTER FLAP RIB UPR FLANGES 7EA CRACKS OF RIB11SDR FDEA202603010296Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB15 BETWEEN STGR2.5 AND FRONT SPAR COMPLIED WITH EA 6-5750-T0386614 INSPECTED THE LH WING CENTER FLAP RIB UPR FLANGE OF RIB15 BETWEEN STGR2.5 AND FRONT SPAR AND REPAIRED THE BOTTOM SKIN POCKET CUT OUTSDR FDEA202603010295Rib · crackedLH WING CENTER FLAP RIBS UPR FLANGE FOUND 6EA CRACKS AT RIB16 BETWEEN STGR2.7 AND STGR2.8, RIB17 BETWEEN STGR2.8 AND REAR SPAR, RIB18 BETWEEN STGR2.8 AND REAR SPAR, RIB19 BETWEEN STGR2.7 AND REAR SPAR, RIB20 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6SDR FDEA202603010294Rib · crackedLH WING CENTER FLAP RIBS UPR FLANGE FOUND 5EA CRACKS AT RIB25 BETWEEN STGR2.7 AND REAR SPAR, RIB26 BETWEEN STGR2.7 AND REAR SPAR, RIB27 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0386614 REPAIRED THE LH WING CENTER FLAP RIB UPR FLANGES 5EA CRSDR FDEA202603010293Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB11 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0386614 REPAIRED THE LH WING CENTER FLAP RIB UPR FLANGE 1EA CRACK OF RIB11 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - LH SDR FDEA202602250278Skin · chafedRH WING INNER FLAP UPR SKIN FOUND CHAFE MARKS BETWEEN RIB16 AND RIB17. REPAIRED THE DAMAGED UPR SKIN IN RH WING INNER FLAP BETWEEN RIB16 AND RIB17 PER SRM57-50-00-201 PARA.4E. TRACKING EA 6-5750-T0386734 RAISED AND ACCOMPLISHED. REPAIR. MAJOR REPAIR IAW GMMSDR FDEA202602210372Actuator · faultedCARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. COMPLIED WITH EO 6-5230-E0378588 C P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAISDR FDEA202511222198Warning Light · failedINCOMING WALKAROUND INSPECTION FOUND LEFT MAIN ENTRY DOOR ESCAPE SLIDE RELEASE WARNING SYSTEM LIGHTS INOP. ASSOCIATED WARNING BUZZER OPERATES NORMAL. AMM: 52-73-11-04-01 AMM: 52-22-13-04 REMOVED AND REPLACED L1 DOOR EMERGENCY EXIT WARNING LIGHT, WITHSDR FDEA202511202193Light · failedINCOMING WALKAROUND INSPECTION FOUND LT MAIN ENTRY DOOR ESCAPE SLIDE RELEASE WARNING SYSTEM, LIGHTS INOPERATIVE. ASSOCIATED WARNING BUZZER OPERATES NORMALLY. REMOVED AND REPLACED L1 DOOR EMERGENCY EXIT WARNING LIGHT WITH NEW UNIT FROM STOCK. OPS TESTED GOODSDR FDEA202407311070Pitot Head · obstructedREPEAT DISCREPANCY, NO AIRSPEED INDICATION ON FO PFD DURING INITIAL TAKEOFF ROLL. REJECTED THE TAKEOFF. INSPECTED F/O'S PITOT PROBE IAW AMM 34-11-15-06, IT APPEARS TO BE METALLIC DEBRIS IN THE PROBE. PROBE NIS. F/O PITOT PROBE CLOGGED. REMOVED AND REPSDR FDEA202308151427Splice · crackedCOMPLY WITH EO 6-5310-7-5023 A PT1 REPLACED THE CRACKED SPLICE AT THE JUNCTION AT STGR18L FR47, TITLE: FUSELAGE - CENTER SECTION - INSPECTION OF STRINGER 18 LH/RH AT FRAME47, AIRBUS SB A300-53-6157 COMPLIED WITH EO 6-5310-7-5023 A PT1 REPLACED THE CRACKED SDR FDEA202307271315Unknown · unknownLEFT HAND PYLON - FOUND EXISTING REPAIR AT LOWER SPAR BETWEEN RIB 9 AND RIB 10 REQUIRES EVALUATION FOR CONFORMITY TO APPROVED DATA. THE EXISTING REPAIR ON LT PYLON LOWER SPAR BETWEEN RIB 9 & RIB 10 WAS EVALUATED & FOUND IN CONFORMITY WITH DWG: 41R54600029 SDR FDEA202307261304Pressure Deck · corrodedBAY AFT OF FWD CARGO COMPT. FR39-FR40 HORIZONTAL PRESSURE DECK UPPER SURFACE FOUND CORROSION AT Y2462 REPAIRED THE BAY AFT OF FWD CARGO COMPT CORRODED HORIZONTAL PRESSURE DECK UPPER SURFACE FR39-FR40, Y2462 PER A300-600 SRM51-40-21 AND EA:6-5310-T0375709 PSDR FDEA202307261303Pressure Deck · unknownBAY AFT OF FWD CARGO COMPT. FR39-FR40 HORIZONTAL PRESSURE DECK UPPER SURFACE FOUND CORROSION BETWEEN -Y450 AND -Y953 REPAIRED THE BAY AFT OF FWD CARGO COMPT CORRODED HORIZONTAL PRESSURE DECK UPPER SURFACE FR39-FR40, -Y450~-Y953 PER A300-600 SRM51-40-21 ANDSDR FDEA202307261302Fitting · crackedINSPECTION OF FR40 LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33LH FOUND CRACK SIGNAL IN THE UPR SECOND CRACK STOP HOLE REPAIRED THE CRACKED FR40 FWD FRAME FITTING LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33LH PER A300-600 SRM 51-40-21 & EA: 6-5710-161345 SDR FDEA202307261301Fitting · crackedINSPECTION OF FR40 LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33RH FOUND CRACK SIGNAL REPAIRED THE CRACKED FR40 FWD FRAME FITTING LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33RH PER A300-600 SRM51-40-21 & EA:6-5710-T0375488 P1. REPAIR IS CAT A REPAIR.MAJOR RSDR FDEA202307261300Unknown · unknownFWD CARGO DOOR ACTUATOR ATTACH FITTING AT FR22A FOUND CRACKSDR FDEA202307261299Floorbeam · crackedAFT CARGO FLOOR CROSSBEAM FOUND CORROSION AT FR62, -Y140 ~ -Y805. REPAIRED THE AFT CARGO CORRODED FLOOR CROSSBEAM AT FR62 -Y140 ~ -Y805 PER A300-600 SRM 53-10-15 PARA.9. THIS IS CAT.A REPAIR . MAJOR REPAIR IAW FEDEX GMM 6-2-100SDR FDEA202307261298Door · crackedRH FWD PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKS. REPAIRED THE CRACKED FRAME SEGMENT OF RH FWD PAX DOOR AT FR14C PER A300-600 SRM51-40-21 AND AIRBUS DRAWING F52181297 ISSUE: K & F52181299 ISSUE: A. THIS IS CAT A REPAIR. TRACKING EA:6-5210-T0375409 SDR FDEA202307261297Frame · crackedRH AFT PAX DOOR FRAME AT FR73A BETWEEN STGR24RH AND STGR25RH FOUND 1EA CRACK. REPAIRED RH AFT PAX DOOR CRACKED FRAME AT FR73A BETWEEN STGR24RH AND STGR25RH PER SRM51-40-21 & EA 6-5310-T0375247 P1.TITLE:FUSELAGE - MAINFRAME - CRACK FOUND ON RH DOOR FRAME FSDR FDEA202307191278Seat Track · unknownTHE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR74 - FR75, -Y1137.1 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM SUPPLEMENT 53-10-16 FIG.202. EO 6-5100-7-5000 D7 PT1 WAS COMPLETED, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDSDR FDEA202112233122Pump · failedPDIS 746 29-21 2913 23DEC21 IND OPEN U AFTER GEAR RETRACTION AROUND 2500 IN THE INITIAL CLIMB, WE GOT GREEN HYD PUMP #2 LO PR, COMPLIED WITH ECAM AND TURNED OFF. FOLLOWED QRH AND USED ELECTRIC PUMPS FOR APPROACH WITH MANUAL GEAR EXTENSION. SDR FDEA202112223118None · nonePDIS 746 29-21 2911 22DEC21 MEM OPEN U DEPARTING KMEM27 AT APPROX 100 KNTS LOST GREEN SYSTEM HYDRAULIC PUMPS. NO APPARENT LOSS OF FLUID, JUST PSI. COMPLETE LOSS OF GREEN SYSTEM PRESSURE. ABLE TO RECOVER GREEN SYSTEM WITH PTU S. INFO 22DEC21 13:SDR FDEA202103230743Floor Panel · damagedMDCC FLOOR PANEL 251DL FOUND PUNCTURE REPAIRED THE MDCC 251DL PUNCTURED FLOOR PANEL AT FR57 - FR57.1 PER A300-600 SRM 53-10-20-201 PARA.9.A. AND INSTALLED THE MDCC FLOOR PANEL 251DL PER AMM 53-10-25-04- 02. THIS REPAIR CATEGORY AS "A". MAJOR REPAIR IAW FEDESDR FDEA202103200731Stringer · damaged3EA STRINGERS AT STGR50R, 51R, 52R BETWEEN FR67-68 FOUND DOUBLE HOLES AND DEFORMATION REPAIRED DOUBLE HOLES AND DEFORMATION OF 3EA STRINGERS AT STGR50R, 51R, 52R BETWEEN FR67-68 PER EA6-5310-T0360050 P1 & A300-600 SRM 51-40-21 & SRM 53-10-14 FIG.201. THISDR FDEA202103200730Skin · dentedLOWER FUSELAGE SKIN FR67-FR68, STGR49R-STGR50R 1EA DENT REPAIRED THE DENT AT LOWER FUSELAGE SKIN FR67 - FR68, STGR49R - STGR50R PER EA 6- 5310-T0360050 P1 & A300-600 SRM 51-40-21 & SRM 51-40-30. THIS IS A CAT B REPAIR. THE FURTHER INSTPECTION REQUIREMENT PESDR FDEA202103200726Frame · crackedNDT FOUND FUSELAGE - MAINFRAME - LH #4 GANTRY OUTBD FLANGE FR49.1 CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- LH #4 GANTRY OUTBD FLANGE FR49.1 PER AIRBUS DWG: R53810581 ISSUE:C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2-SDR FDEA202103200724Frame · crackedNDT FOUND FUSELAGE - MAINFRAME - RH #4 GANTRY OUTBD FLANGE FR52.A CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- RH #4 GANTRY OUTBD FLANGE FR52.A PER AIRBUS DWG: R53810581 ISSUE: C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2SDR FDEA202103200722Frame · crackedNDT FOUND FUSELAGE - MAINFRAME - LH #2 GANTRY OUTBD FLANGE FR52.A CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- LH #2 GANTRY OUTBD FLANGE FR52.A PER AIRBUS DWG: R53810581 ISSUE: C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2SDR FDEA202103200721Frame · crackedNDT FOUND FUSELAGE - MAINFRAME - LH #2 GANTRY OUTBD FLANGE FR51.A CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- LH #2 GANTRY OUTBD FLANGE FR51.A PER AIRBUS DWG: R53810581 ISSUE: C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2SDR FDEA202103200720Frame · crackedNDT FOUND FUSELAGE - MAINFRAME - RH #3 GANTRY INBD FLANGE FR50.1 CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- RH #3 GANTRY INBD FLANGE FR50.1 PER AIRBUS DWG: R53810581 ISSUE: C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2-1SDR FDEA202103200719Frame · crackedNDT FOUND FUSELAGE - MAINFRAME - RH #3 GANTRY INBD FLANGE FR49.1 CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- RH #3 GANTRY INBD FLANGE FR49.1 PER AIRBUS DWG: R53810581 ISSUE: C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2-1SDR FDEA202103200718Frame · crackedNDT FOUND FUSELAGE - MAINFRAME - RH #3 GANTRY INBD FLANGE FR49 CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- RH #3 GANTRY INBD FLANGE FR49 PER AIRBUS DWG: R53810581 ISSUE: C. THIS REPAIR IS CAT. A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2-100.SDR FDEA202103200717Frame · crackedNDT FOUND FUSELAGE - MAINFRAME - RH #5 GANTRY INBD FLANGE FR51.A CRACK PERFORMED THE REPAIR ON FUSELAGE- MAINFRAME- RH #5 GANTRY INBD FLANGE FR51A PER AIRBUS DWG: R53810583 ISSUE: D. THIS REPAIR IS CAT.A REPAIR AND IT WAS MAJOR REPAIR IAW FEDEX GMM 6-2-100SDR FDEA202103150651Skin · delaminatedLH WING 4# SPOILER CENTER O/B HINGE ARM LOWER SURFACE FOUND DELAMINATION , SIZE : 30MM * 30MM D:1.9MM PERFORMED THE REPAIR ON LH WING 4# SPOILER CENTER O/B HINGE ARM LOWER SURFACE PER EA # :6-5750-T0360096 P1 , TITLE: WING - FLIGHT SURFACE - LH 4# SPOILERSDR FDEA202101190156Proximity Sensor · failedON GEAR RETRACTION, NLG DOOR INDICATOR ILLUMINATED ON BOTH GEAR INDICATOR PANELS. COMPLIED WITH QRH AND RETURNED TO AFW. PROXIMITY BOX SHOWING CODE 32 W/ BOX FAULT LIGHT ON. T/S PER A300 TSM 32-30-00. BITE TEST PROXIMITY DETECTOR PROCESSING UNIT (54GB), PESDR FDEA2019041640793Aileron · stuckON TAXI OUT DURING FLIGHT CONTROL CHECK, LEFT AILERON INDICATOR STUCK IN FULL UP POSITION. SEVERAL MORE MOVEMENTS OF THE AILERON AND THE INDICATOR SHOWS FULL DOWN POSITION WHILE AILERONS CONTROL ARE IN THE NEUTRAL POSITION.SDR FDEA201812063443Adc · malfunctionedPASSING 9000FT SEVERAL FAILURES ADC 2 BOTH PITCH TRIMS BOTH YAW DAMPENERS ALL F/O INDICATIONS OF AIRSPEED ALTITUDE GPS1 ATS. UPDATE A/C BACK AT GATE ENTERED E& E COMPARTMENT STRONG SMELL OF ELECTRICAL ODOR SOMETHING BURNING OR OVERHEATING. CHECKED COMPONENTS OSDR FDEA201811103178Warning System · false activationL1 DOOR RED LIGHT FLASHED DURING FLIGHT, AS REPORTED BY JUMPSEATER. NO PRESSURIZATION O2 COCKPIT INDICATIONS NOTED. PERFORMED OPS CHECK OF DOOR WARNING SYSTEM IAW AMM 52-73-11-04-08. NO FAULTS NOTED. NO 90 HISTORY. ACFT OF FOR SERVICE.SDR FDEA201809182581Floor Panel · delaminatedCOURIER FLOOR PANEL 221RF DELAMINATED. FLOOR PANEL 221RF FABRICATED ON T18/1362586 IAW SRZ 25-005, REPAIR IS CLASSIFED AS CAT "A" AND MAJOR REPAIR.SDR FDEA2018091872561Floor Panel · delaminatedCOURIER FLOOR PANEL 222NF DELAMINATED. FLOOR PANEL 222NF FABRICATED ON T18/1362587, CLASSIFIED AS CAT "A" AND MAJOR REPAIR IAW SRZ 25-005.SDR FDEA2018091432520Adapter · wornWORN SEAT TRACK ADAPTER AT FR 62 BETWEEN -Y953 TO -Y1456. REMOVED WORN SEAT TRACK ADAPTER IAW SRM 51-40-21. LOCATED AND DRILLED NEW SEAT TRACK ADAPTER IAW SRM 51-40-00, INSTALLED NEW SEAT TRACK ADAPTER IAW SRM 51-40-21, REPAIR IS CLASSIFED AS CAT "A" AND MAJORSDR FDEA2018091432487Floor Panel · brokenROLLER TRAY PANEL 131HG FWD PIT IS BROKEN INTO PIECES. FABRICATED FLOOR PANEL 131 HG ON T18/1363243 PER SRZ 25-005 CAT "A" MAJOR REPAIR.SDR FDEA2018091432486Floor Panel · delaminatedFLOOR PANEL 152KF AFT PIT IS DAMAGED. FABRICATED FLOOR PANEL 152KF ON T18/1363818 PER SRZ 25-005 CAT "A" MAJOR REPAIR.SDR FDEA2018091432485Floor Panel · crackedFLOOR PANEL 151EF AFT PIT IS BROKEN IN TWO. FABRICATED FLOOR PANEL 151 EF ON T18/1363152 PER SRZ 25-005 CAT "A" MAJOR REPAIR.SDR FDEA2018091422484Floor Panel · damagedPANEL 152CF AFT PIT IS DAMAGED. FABRICATED FLOOR PANEL 152CF ON T18/1363046 PER SRZ 25-005 CAT "A" MAJOR REPAIR.SDR FDEA2018091422483Floor Panel · delaminatedPANEL 161HF BULK CARGO IS DAMAGED. FABRICATED FLOOR PANEL 161HF ON T18/1365001 PER SRZ 25-005 CAT "A" MAJOR REPAIR.
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