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.
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
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 FDEA202308021855Trunnion · unknownRIB 5 FWD GEAR TRUNION PINTLE HAS HEAVY PITTINGIN BETWEEN BEARING HALFSAT 2:00 TO 3:00 OCLOCK POSITIONS. REPAIRED PER AIRBUS REPAIR INSTRUCTIONS R57240425SDR FDEA202307051147Frame · crackedFUSELAGE FRAME FR73A FOUND 1EA CRACKED AT S24L - S25L REPAIRED THE CRACK ON THE FUSELAGE FRAME FR73A S24L - S25L PER FEDEX EA: #: 6-5310- T0375001, TITLE: FUSELAGE - MAINFRAME - EO 6-5310-E0327267 (SB A300-53-6175) INSPECTION - CRACK FOUND ON LH&RH DOOR FRASDR FDEA202307051146Frame · crackedFUSELAGE FRAME FR73A FOUND 1EA CRACKED AT S24R - S25R REPAIRED THE CRACK ON THE FUSELAGE FRAME FR73A S24R - S25R PER FEDEX EA:#:6-5310- T0375001, TITLE: FUSELAGE - MAINFRAME - EO 6-5310-E0327267 (SB A300-53-6175) INSPECTION - CRACK FOUND ON LH &RH DOOR FRSDR FDEA202307031142Spoiler · delaminatedRH WING #5 SPOILER OUTBD HINGE ARM OUTBD SURFACE AND OUTBD HINGE ARM LWR SURFACE FOUND DELAMINATION. SIZE: (1): 50MM*20MM, DEPTH: 1.60MM (2): 10MM*15MM DEPTH:2.3MM PERFORMED THE REPAIR ON RH WING #5 SPOILER OUTBD HINGE ARM OUTBD SURFACE AND OUTBD HINGE ARMSDR FDEA202307031141Spoiler · delaminatedRH WING #3 SPOILER INBD HINGE ARM INBD SURFACE FOUND DELAMINATION. SIZE: 40MM*20MM, DEPTH: 1.70MM PERFORMED THE REPAIR ON RH WING #3 SPOILER INBD HINGE ARM INBD SURFACE PER FEDEX EA # 6-5750-T0374955 TITLE: WING - FLIGHT SURFACES - RH 3# SPOILER CENTER HINSDR FDEA202204251049Angle · damaged(6-5710-T0307446 B PT4) R/H REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE / FRAME 47 FASTENER HOLES "A" HAS REJECTABLE INDICATION NOTED AT BOTTOM LAYERS. REPAIRED FASTENER HOLE "A" PER EA 6-5710-T0307446 C PT8 WINGS - BASIC WING STRUCTURE - AD 201SDR FDEA202204251048Angle · cracked(6-5710-T0307446 B PT4) L/H REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE / FRAME 47 FASTENER HOLE "G" HAS CRACK INDICATION NOTED AT 12:0'CLOCK BOTTOM LAYERS. REPAIRED FASTENER HOLE "G" PER EA T-6-5710-T0307446 C PT8 WINGS - BASIC WING STRUCTURE - ASDR FDEA202204221029None · noneENTERED FOR TRAINING PURPOSES ONLY NO ACTION REQUIRED.SDR FDEA202204221028Joint · damagedFWD CARGO FRAME 40 LH HAS FASTENERS WITH DAMAGED INDICATIONS HOLES A, B, AND C. COMPLIED WITH EA 6-5710-127939 PT8: WINGS - BASIC WING STRUCTURE - ALI WORKCARD 5710390-00-11 REPAIRED CRACKED HOLES IN CTR WING JOINT - FR 40 LH / RH. MAJOR REPAIRSDR FDEA202108242081Switch · failedRECEIVED 4 TRANSIENT ECAM GREEN HYD PR LO INDICATION DURING TAXI, WHICH ALSO CAUSED AN AUTO-BRAKE SYSTEM TO FAILURE. ANALOG AND ECAM GREEN HYD PRESSURE AND QUANTITY BOTH SHOWED GOOD WHILE ECAM MESSAGE WAS DISPLAYED. HAD TO ABORT T/O DUE TO SECOND INDICSDR FDEA202101270199Damper · no testDONT PASS OPERATIONAL TEST PASSENGER CREW DOOR 831 DOOR DAMPER AT FWD GALLEY AREA (1 EA). REPLACED PASSENGER CREW DOOR 831 DOOR DAMPER, IAW A300-600 AMM 52-10-14-04-01 AND A300-600 AMM 52-10-14-05-01. PERFORMED FUNCTIONAL TEST, IAW A300-600 AMM 52-10-11-05-0SDR FDEA202101160135Floor Panel · crackedCRACK FLOOR PANEL 131CG IN FWD CARGO COMPARTMENT (1 EA). REPLACED FLOOR PANEL 131CG IN FWD CARGO COMPARTMENT, IAW A300-600 AMM 06-41-53-00-09 AND A300-600 SRM 51-72-10-001 AND 51-40-21.SDR FDEA202101160134Floor Panel · crackedCRACK FLOOR PANEL 131AG IN FWD CARGO COMPARTMENT (1 EA). REPLACED FLOOR PANEL 131AG IN FWD CARGO COMPARTMENT, IAW A300-600 AMM 06-41-53-00-09 AND A300-600 SRM 51-72-10-001 AND 51-40-21.SDR FDEA202101160133Floor Panel · crackedCRACK FLOOR PANEL 131UF IN FWD CARGO COMPARTMENT (1 EA) REPLACED FLOOR PANEL 131UF IN FWD CARGO COMPARTMENT, IAW A300-600 AMM 06-41-53-00-09 AND A300-600 SRM 51-72-10-001 AND 51-40-21.SDR FDEA202101110159Floor Panel · crackedCRACK FLOOR PANEL 232TG IN MAIN DECK CARGO COMPARTMENT IN PASSENGER CABIN. REPAIRED FLOOR PANEL 232TG IN MAIN DECK CARGO COMPARTMENT IN PASSENGER CABIN, AS PER A300-600 SRM 53-10-20 PB201 PARA 9C (3)(B). TOOL USED CALIPER P/N 500-197-30 SN A18135103 DUE DATESDR FDEA202012310308Frame · crackedCRACK INDICATION ON FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION AREA OPEN FASTENER HOLES LOWER POSITION RH SIDE, CRACK DIRECTION IS 6 O CLOCK IN FWD CARGO COMPARTMENT (1EA) PERFORMED REAPIR ON FRAME 40 TO CENTER WING JOINT AT UPSDR FDEA202012310182Frame · crackedCRACK INDICATION ON FRAME 13 OPEN FASTENER HOLE AT LEVEL OF STR 9 RT SIDE, CRACK DIRECTION IS 9 O`CLOCK AT FWD GALLEY AREA (1 EA). REPLACED STRINGER SECTION LOCATED ON FR 13 AT LEVEL STR 9 RT SIDE, IAW A300-600 SRM 51-40-20-001 AND DRAWING #A53610301 ISSUE K SDR FDEA202012300439Pressure Deck · corrodedCORROSION INTERNAL STRUCTURE FWD FACE PRESSURE DECK AT LEVEL FR 39 LOWER AREA IN FWD CARGO COMPARTMENT PERFORMED REPAIR ON PRESSURE BULKHEAD FR39 BTW STR 53LH TO STR 55LH IAW EA# 6- 5314-T0359508 TITLE: FUSELAGE CENTER SECTION-FR39 BULKHEAD BTW S-53LH TO S-SDR FDEA202012300229Seat Track · corrodedCORROSION SEAT TRACK Y953 BETWEEN FR 18 TO FR 19 IN PASSENGER CABIN (MAIN DECK). REPLACED SEAT TRACK Y953 BETWEEN FR 15 TO FR 19 IN PASESENGER CABIN (MAIN DECK), IAW A300-600 SRM 51-40-20 AND DWG NR A53781051 ISSUE A SHEET 3 AND DWG A53612502 ISSUE F SHEET 1.SDR FDEA202012300205Floor Support · corrodedCORROSION FLOOR STRUCTURE LOCATED BETWEEN FR 11 AND FR 15 Y1213 IN PASSENGER CABIN (MAIN DECK). REPLACED FLOOR STRUCTURE LOCATED BETWEEN FR 11 AND FR 15 Y1456 IN PASSENGER CABIN (MAIN DECK), IAW A300-600 DWG 53612310 ISSUE A AND A300-600 SRM 51-72-10.SDR FDEA202012300184Floor Support · corrodedCORROSION FLOOR STRUCTURE LOCATED BETWEEN FR 11 AND FR 15 Y180 IN PASSENGER CABIN (MAIN DECK). REPLACED FLOOR STRUCTURE Y953 LOCATED BETWEEN FR 11 AND FR 15 IN (MAIN DECK), IAW A300-600 SRM 51-72-10 AND DRAWING A53612519 ISSUE AN.SDR FDEA202012300181Frame · crackedCRACK INDICATION ON FRAME 13 OPEN FASTENER HOLE AT LEVEL OF STR 9 LT SIDE, CRACK DIRECTION IS 3 O`CLOCK AT FWD GALLEY AREA (1 EA). REPLACED STRINGER SECTION LOCATED ON FR 13 AT LEVEL STR 9 LT SIDE, IAW A300-600 SRM 51-40-20-001 AND DWG #A53610301 ISSUE K SHEESDR FDEA202012300014Floor Support · corrodedCORROSION FLOOR STRUCTURE LOCATED BETWEEN FR 11 AND FR 13 Y730 IN PASSENGER CABIN (MAIN DECK). REPLACED FLOOR STRUCTURE LOCATED BETWEEN FR 11 AND FR 13 Y730 IN PASSENGER CABIN (MAIN DECK), IAW A300-600 SRM 51-72-10 AND DWG A53612214 SHEET 01 ISSUE M.SDR FDEA202012290324Crossbeam · crackedCRACK FRAME 15A CROSS BEAM AT ATTACHMENT FITTING OF RACK 107VU IN FWD AVIONIC COMPARTMENT PERFORMED REPAIR ON FRAME 15A CROSSBEAM ATTACHMENT FITTING OF RACK 107VU IN FWD AVIONIC COMPARTMENT IAW EA # 6-5310-T0358885 P1 EA TITLE: FUSELAGE-MAINFRAME - AD 20SDR FDEA202012280444Frame · crackedCRACK INDICATION ON FRAME 54 (2 INCH AFT SIDE) AND STGR 44LT (1 INCH UPPER) OPEN HOLE IN AFT CARGO COMPARTMENT (1 EA) (CRACK DIRECTION 12 O CLOCK) PERFORMED REPAIR LOC ON FRAME 54 (2 INCH AFT SIDE) AND STGR 44LT (1 INCH UPPER) OPEN HOLE IN AFT CARGO COMPARTMENSDR FDEA202012280443Frame · crackedCRACK INDICATION ON FRAME 54 STGR 36 LH (1 INCH UPPER) OPEN HOLE IN AFT CARGO COMPARTMENT (1 EA)(CRACK DIRECTION 12 O CLOCK) PERFORMED REPAIR LOC ON FRAME 54, STGR 36LH (1 INCH UPPER) OPEN HOLE IN AFT CARGO COMPARTMENT IAW EA 6-5316-T0359314. TITLE: FUSELASDR FDEA202012280327Door · crackedCRACK ON FORWARD WEB LOC AT FR61A AND BTW LONGERON 1 TO 1A, ON AFT CARGO COMPARTMENT DOOR PERFORMED REPAIR ON FWD WEB LOC AT FR61A AND BTW LONGERON 1 TO 1A ON AFT CARGO COMPARTMENT DOOR IAW EA# 6-5230-T0359408. TITLE: DOORS-CARGO DOOR /HYD SYS-AFT CARGO SDR FDEA202012280447Skin · crackedCRACK INDICATION ON FRAME 54 (2 INCH AFT SIDE) AND STGR 44 LT (2 INCH UPPER) OPEN HOLE IN AFT CARGO COMPARTMENT (1 EA) (CRACK DIRECTION 12 O CLOCK) PERFORMED REPAIR LOC. ON FRAME 54 (2 INCH AFT SIDE) AND STGR 44 LT (2 INCHES UPPER) OPEN HOLE IN AFT CARGO COMPASDR FDEA202012280328Web · crackedCRACK ON AFT WEB LOC AT FR61A AND BTW LONGERON 1 TO 1A, ON AFT CARGO COMPARTMENT DOOR PERFORMED REPAIR ON AFT WEB LOC AT FR61A AND BTW LONGERON 1 TO 1A ON AFT CARGO COMPARTMENT DOOR IAW EA 6-5230-T0359408. TITLE: DOORS-CARGO DOOR/ HYD SYS-AFT CARGO DOOR SDR FDEA202012280137Floor Panel · crackedCRACK FLOOR PANEL 131TF IN FWD CARGO COMPARTMENT (1 EA). REPLACED FLOOR PANEL 131TF ON FWD CARGO COMPARTMENT, IAW A300-600 AMM 06-41-53-00-09 AND A300-600 SRM 51-72-10-001 AND 51-40-21.SDR FDEA202012260278Skin Panel · dentedDENT EXTERNAL SKIN FR 66 TO FR 67 AND STR 52R TO STR 54R AT LOWER FUSELAGE PERFORMED PERMANENT REPAIR ON DENTS LOC EXTERNAL SKIN FR66 TO FR67 AND STR 52R TO STR 54R AT LOWER FUSELAGE. IAW EA 6-5317-103271 A. TITLE: FUSELAGE - FUSELAGE AFT INTERMEDIATE SECTSDR FDEA202012053040None · failedCLIMBING THRU 14000 ON DEPARTURE OUT OF KORF #2 ENGINE SLEZED EPR ROLLED BACK TO 0, NI INDICATED 13.5 % N2 WAS 0 ,EGT SPIKED TO 790 DEG, LOW OIL PRESS LIGHT ILLIMINATED. DIVIERTED TO KRIC AFTER DECLIARING EMERGENCY. #2 ENGINE REPLACEMENT.SDR FDEA202011142842Sensing Element · failedDURNING CLIMBOUT ENGINE NO 1 BLEED LEAK, DIVERTED INTO TPA BECAUSE WE LOST PRESSURIZATION DUE TO DEFERRED NO 2 PACK, DECLARED EMERGENCY. FACT 15NOV20 16:06 TPA. R & R MANIFOLD OVERHEAT SENSING ELEMENT ON LT WING PYLON I/R/T MM 36-22-12-04, REMOVAL P/N 35518-SDR FDEA201901180171Sensor · faultyPDIS 726 28-20 3775 18JAN19 MEM OPEN U LOGPAGES:2958677 OPERATING IN MANUEL FUEL FEED PER THE MEL, CENTER TANK PUMPS OFF, ECAM MEMO PAGE SHOWED CTR TANK FEEDING. ON SCHEMATIC PAGE, CENTER TANK RIGHT PUMP DISPLAY SHOWS ON BUT FAULTED. (OF NOTE, DURING SDR FDEA201812023414Proximity Sensor · failedPER CREW VERBAL, GEAR WOULD NOT RETRACT IN POS DET SYS NR 1, (SYS 2 IS ON MEL). SWITCHED TO POS DET SYS NR 2 AND IT WORKED. COMPLETED INSTALL OF 8GB, AND 12GA BOGIE BEAM SENSOR INCLUDING DIMENSION CHECKS ON RT MAIN GEAR. STILL REQUIRES OPS CHECK. REMOVED AND RSDR FDEA201811233357Proximity Sensor · inoperativeDURING TAKEOFF KMDT LANDING GEAR POSITION DET, SYS2 GEAR HANDLE CAME UP TO NORMAL POSITION, SELECTED SYS 1, WOULD NOT MOVE TO UP WENT BACK TO SYSTEM 2, GEAR HANDLE CAME UP NORMAL. REMOVED REPLACED ELECTRONIC PROXIMITY UNIT IAW MM 32-31-71-04. PERFORMED NORMAL SDR FDEA201811223361Electronic Unit · failedDURING TAKEOFF KMDT LANDING GEAR POSITION DET, SYS 2 GEAR HANDLE CAME UP TO NORMAL POSITION, SELECTED SYS 1, WOULD NOT MOVE TO UP WENT BACK TO SYSTEM 2, GEAR HANDLE CAME UP NORMAL. REMOVED REPLACED ELECTRONIC PROXIMITY UNIT IAW MM 32-31-71-04. PERFORMED NORMSDR FDEA201807181771Duct · contaminatedJ/S REPORTED AN OILY ODOR IN COURIER COMP. WITH VISIBLE OILY SMOKE. THE FIRST OFFICER STATED THAT JUMPSEATERS NOTIFIED THE CREW THAT OILY SMOKE WAS COMING UP THROUGH THE FLOOR VENTS. F/O VERIFIED THAT IT WAS NOT CONDENSATION & WAS OILY SMOKE. NO SMOKE OR ODOSDR FDEA201807161717Rib · crackedRT PYLON RIB 19 HAS CRACK JUST AFT OF AFT PYLON MOUNT. COMPLIED WITH EA 6-5480-T0340823 P1 NACELLES/PYLON FILLETS/FAIRINGS-RW-HW PYLON, AFT FAIRING, RIB 19 CRACKED SRM REPAIR W/MINOR DEVIATIONS, REPAIR IS CLASSIFIED AS CAT A AND MAJOR REPAIR.SDR FDEA2018071641712Skin · damagedRT WING CENTER FLAP APPROX 16" FROM INBD END AND 19" FROM LEADING EDGE, LOWER SURFACE SKIN PREVIOUS REPAIR DEBONDED / CRACKS. REPLACED STRINGER SECTION, REPAIR ANGLE, PACKING PLATE, PACKING STRIPS, AND INSTALLED REPAIR FLAP SKIN DOUBLER IAW SRM 57-50-00-201 FISDR FDEA201807031619Floor Panel · crackedMAIN CARGO FLOOR PANEL 241WH HAS CRACK. FABRICATED FLOOR PANEL 241WH ON T18/1351638 IAW DWG SRZ 25-005. CLASSIFIED AS CAT " A " REPAIR. FLOOR PANEL 241WH INSTALLED ON W/C 240-FL- FIT MAJOR REPAIR.SDR FDEA201807031618Floor Panel · crackedMAIN CARGO FLOOR PANEL 214QH HAS CRACK. FABRICATED FLOOR PANEL 241QH ON T18/1350937 IAW DWG SRZ 25-005. CLASSIFIED AS CAT " A " REPAIR. FLOOR PANEL 241QH INSTALLED ON W/C 240-FL- FIT MAJOR REPAIR.SDR FDEA201807031617Floor Panel · crackedMAIN CARGO FLOOR PANEL 241RJ HAS CRACK. FABRICATED FLOOR PANEL 241RJ ON T18/1350935 IAW DWG SRZ 25-005. CLASSIFIED AS CAT " A " REPAIR. FLOOR PANEL 241RJ INSTALLED ON W/C 240-FL- FIT MAJOR REPAIR.SDR FDEA201807011613Floor Panel · crackedMAIN CARGO FLOOR PANEL 241TH HAS EDGE CRACK. FABRICATED FLOOR PANEL 241TH ON T18/1351637 IAW DWG SRZ 25-005 CLASSIFIED AS A CAT "A" MAJOR REPAIR.SDR FDEA201807031616Floor Panel · crackedMAIN CARGO FLOOR PANEL 251WH HAS CRACK. FABRICATED FLOOR PANEL 251WH ON T18/1351014 IAW DWG SRZ 25-005. CLASSIFIED AS CAT " A " REPAIR. FLOOR PANEL 251WH INSTALLED ON W/C 250-FL- FIT MAJOR REPAIR.SDR FDEA201807031615Floor Panel · crackedMAIN CARGO FLOOR PANEL 251GF HAS CRACK. FABRICATED FLOOR PANEL 251GF ON T18/1350940 IAW DWG SRZ 25-005. CLASSIFIED AS CAT " A " REPAIR. FLOOR PANEL 251GF INSTALLED ON W/C 250-FL- FIT MAJOR REPAIR.SDR FDEA201807031614Floor Panel · crackedMAIN CARGO FLOOR PANEL 251PH HAS CRACK. FABRICATED FLOOR PANEL 251PH ON T18/1351013 IAW DWG SRZ 25-005. CLASSIFIED AS CAT " A " REPAIR. FLOOR PANEL 251PH INSTALLED ON W/C 250-FL- FIT MAJOR REPAIR.SDR FDEA201807031612Floor Panel · crackedMAIN CARGO FLOOR PANEL 242XH HAS CRACK. FABRICATED FLOOR PANEL 242XH ON T18/1350938 IAW DWG SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.SDR FDEA201807031611Floor Panel · puncturedMAIN CARGO FLOOR PANEL 241DF HAS VARIOUS PUNCTURES. FABRICATED FLOOR PANEL 241DF ON T18/1350934 IAW DWG SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.SDR FDEA201807031610Floor Panel · crackedMAIN CARGO FLOOR PANEL 242EF HAS CRACK. FABRICATED FLOOR PANEL 242EF ON T18/1350939 IAW DWG SRZ 25-005. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
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