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 FDEA201807031606Floor Panel · damagedMAIN DECK COMPARTMENT FRAME 22-26, FLOOR PANEL 232KG PUNCTURED/DAMAGED. FABRICATED FLOOR PANEL 232KG ON T18/1350933 IAW DWG SRZ-25-005. CLASSIFIED AS CAT "A" MAJOR REPAIR. FLOOR PANEL 232KG INSTALLED ON WORK CARD.SDR FDEA201807031605Floor Panel · crackedMAIN CARGO FLOOR PANEL 231KG HAS CRACK. FABRICATED FLOOR PANEL 231KG ON T18/1350932 IAW DWG SRZ-25-005. CLASSIFIED AS CAT "A" MAJOR REPAIR. FLOOR PANEL 231KG INSTALLED ON WORK CARD.SDR FDEA201803220757Hinge · damagedR1 DOOR WILL NOT FROM OPEN FROM OUTSIDE. PERFORMED A GVI OF DOOR AND HINGES. DOOR NEEDS TO BE LIFTED APPROX 1/4 INCH TO OPEN. REMOVED AND REPLACED DOOR SUSPENSION SUPPORT ARM PINS AND BUSHINGS IAW AMM 52-11-12-04, DOOR OPENS AND CLOSES WITHOUT LIFTING, DOSDR FDEA201802050305Valve · malfunctionedDURING LANDING, THE NR 4 TIRE BLEW. BITE TEST OF BSCU SHOWS NO FAULTS. REMOVED AND REPLACED THE NR 4 BRAKE ASSY IAW MM 32-42-27-4. REMOVED AND REPLACED NR 4 MLG NORMAL BRAKE SERVO VALVE IAW MM 32-42-16-04 REMOVED AND REPLACED THE NR 4 MLG TACHOMETER IAW MSDR FDEA201802050304Tachometer · failedDURING LANDING, THE NR 4 TIRE BLEW. AT APPROX 50KTS STARTING TO BREAK FOR THE HIGH SPEED TURNOFF C TAXIWAY. BITE TEST OF BSCU SHOWS NO FAULTS. DUE TO HISTORY, REMOVED AND REPLACED THE NR 4 BRAKE ASSY IAW MM 32-42-27-4. REMOVED AND REPLACED NR 4 MLG, NORMALSDR FDEA201608232961Selector Valve · unserviceableDURING FINAL, SELECTED GEAR DOWN AND HAD AMBER DOOR LIGHTS AND RED GEAR LIGHT FOR LONGER THAN USUAL FOLLOWED BY ECAM GEAR NOT DOWN AND LOCKED. EXECUTED GO AROUND, RAISED GEAR SUCCESSFULLY. SWITCHED POSITION DETECTOR TO SYSTEM 2 AND LOWERED GEAR HANDLE WITH SDR FDEA201606272155Skin · dentedRT WING NR 3 LEADING SLAT INNER SURFACE FOUND 1EA DENT.SDR FDEA201606172033Floor Support · corrodedBULK CARGO FR 64-FR 65, Y140 FLOOR SUPPORT WITH SLIGHT SURFACE CORROSION. REPLACED THE CORRODED FLOOR SUPPORT ON BULK CARGO FRAME 64-FRAME 65, Y140. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201606172028Fitting · crackedFUSELAGE INTERNAL STRUCTURE AT FRAME 41, STR 24-28 RT FRAME FOOT INBD ROW UPR NR 1 FASTENER HOLE FOUND CRACKED SIGNAL. REPAIRED THE CRACKED HOLE OF FUSELAGE INTERNAL STRUCTURE AT FRAME 41, STR 24-28, RT FRAME FOOT INBD ROW UPPER NR 1 FASTENER IAW EA 6-5315-T0SDR FDEA201606172027Fitting · crackedFUSELAGE INTERNAL STRUCTURE AT FRAME 43, STR 24-28 RT FRAME FOOT INBD ROW LWR NR 2 FASTENER HOLE FOUND CRACKED SIGNAL. REPAIRED THE CRACKED HOLE OF FUSELAGE INTERNAL STRUCTURE AT FRAME 43, STR 24-28, RT FRAME FOOT INBD ROW LOWER NR 2 FASTENER IAW EA 6-5315-T0SDR FDEA201606172026Fitting · crackedFUSELAGE INTERNAL STRUCTURE AT FRAME 42, STGR 24-28 LT FRAME FOOT INBD ROW UPR NR 1 FASTENER HOLE FOUND CRACK SIGNAL. REPAIRED THE CRACKED HOLE OF FUSELAGE INTERNAL STRUCTURE AT FRAME 42, STR 24-28 LT FRAME FOOT INBD ROW UPPER NR 1 FASTENER EA 6-5315-T0326077SDR FDEA201606172025Fitting · crackedFUSELAGE INTERNAL STRUCTURE AT FRAME 46, STGR 24-28LT FRAME FOOT INBD ROW LOWER NR 2 FASTENER HOLE FOUND CRACK SIGNAL.SDR FDEA201606172024Fitting · crackedFUSELAGE INTERNAL STRUCTURE AT FRAME 46, STR 24-28LT FRAME FOOT INBD ROW UPR NR 2 FASTENER HOLE FOUND CRACK SIGNAL. REPAIRED THE CRACKED HOLE OF FUSELAGE INTERNAL STRUCTURE AT FRAME 46, STR 24-28 LT FRAME FOOT INBD ROW UPPER NR 2 FASTENER IAW EA 6-5315-T03260SDR FDEA201606172023Fitting · crackedFUSELAGE INTERNAL STRUCTURE AT FRAME 46, STR 24-STR 28LT FRAME FOOT INBD ROW UPR NR 1, FASTENER HOLE FOUND CRACK SIGNAL. REPAIRED THE CRACKED HOLE OF FUSELAGE INTERNAL STRUCTURE AT FRAME 46 STR 24-28 LT FRAME FOOT INBD ROW UPPER NR 1 FASTENER IAW EA 6-5315-T0SDR FDEA201606141982Angle · crackedRIGHT WING, CENTER SPAR AT RIB 8, STR 12, SEALING ANGLE VERTICAL WEB FOUND CRACKED. REPLACED THE CRACKED ANGLE IAW EO 6-5710-7-5002C, PT2 & REPAIR DWG R57150404. COMPLIED WITH EA 6-5710-T0326233 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201606071859Web · crackedMAIN DECK FRAME 47, Y953 - Y1456, UNDERFLOOR ONE EACH WEB CRACKED. REPAIRED WEB IAW SRM 53-15-15-201, PARA 5A, FIG 201, THE REPAIR WAS CATEGORY B. THE FIRST INSPECTION THRESHOLD WAS 24000FC AFTER REPAIR EMBODIMENT. THE SUBSEQUENT INSPECTION INTERVAL WAS 300SDR FDEA201606021790Web · crackedCENTER TANK, FRAME 40, Y1456, FRONT SPAR INTERNAL WEB SUSPECTED CRACK ACROSS A FASTENER AT THE LOWER END APPROX 2.0 INCHES IN LENGTH. REPAIRED CTR TANK FRAME 40, Y1456, FRONT SPAR INTERNAL WEB IAW SRM 57-10-21, FIG 201 AND DWG R57110271 & R57110273, MAJOR REPSDR FDEA201606021789Web · crackedCENTER TANK, FRAME 40, -Y953, FRONT SPAR INTERNAL WEB SUSPECTED CRACK ACROSS A FASTENER AT THE LOWER END APPROX 2.0 INCHES IN LENGTH. REPAIRED CENTER TANK, FRAME 40, Y953 FRONT SPAR INTERNAL WEB IAW SRM 57-10-21, FIG 201 AND DWG R57110271 & R57110273, MAJOR RSDR FDEA201606021788Web · crackedCENTER TANK, FRAME 40 CL, FRONT SPAR INTERNAL WEB SUSPECTED CRACK ACROSS A FASTENER AT THE LOWER END APPROX 2.0 INCHES IN LENGTH. REPAIRED CENTER TANK, FRAME 40 CL, FRONT SPAR INTERNAL WEB IAW SRM 57-10-21, FIG 201 AND DWG R57110271 & R57110273, MAJOR REPAIR SDR FDEA201606021787Web · crackedCENTER TANK, FRAME 40, Y450, FRONT SPAR INTERNAL WEB SUSPECTED CRACK ACROSS A FASTENER AT THE LOWER END, APPROX 2.0 INCHES IN LENGTH. REPAIRED CENTER TANK, FRAME 40, Y450, FRONT SPAR INTERNAL WEB IAW SRM 57-10-21, FIG 201 AND DWG R57110271 & R57110273, MAJOR SDR FDEA201606021786Web · crackedCENTER TANK, FRAME 40, Y953, FRONT SPAR INTERNAL WEB SUSPECTED CRACK ACROSS A FASTENER AT THE LOWER END, APPROX 2.0 INCHES IN LENGTH. REPAIRED CENTER TANK FRAME 40, Y953, FRONT SPAR INTERNAL WEB IAW SRM 57-10-21, FIG 201 AND DWG, R57110271 & R57110273, MAJOR SDR FDEA201606021785Floor Support · corrodedMAIN DECK FRAMES 11 - 12A, Y730 FLOOR SUPPORT CORRODED.SDR FDEA201606011777Floor Support · crackedMAIN DECK FRAME 14, -Y953, FLOOR SUPPORT CRACKED. REPAIRED THE SUPPORT AT MAIN DECK FRAME 11-FRAME 14, Y953 IAW SRM 53-12-15-201, FIG 207. THE REPAIR WAS CATEGORY B, THE INSPECTION THRESHOLD WAS 51000FC/89000FH AFTER REPAIR EMBODIMENT, THE SUBSEQUENT INSPECTSDR FDEA201606011776Web · crackedMAIN DECK FRAME 47, -Y450 - Y0, UNDER FLOOR ONE EACH WEB CRACKED. THE CRACK LENGTH WAS 0.91", LONGER THAN 0.787", OUT OF REPAIR LIMIT IAW SRM 53-15-15, PARA 5A. REPLACED THE WEB IAW SRM 51-40-21, LOCATION: MAIN DECK FRAME 47-Y450 TO Y0 UNDERFLOOR.SDR FDEA201606011775Web · crackedMAIN DECK FRAME 47, Y0 - Y450, UNDER FLOOR ONE EACH WEB CRACKED. REPAIRED WEB IAW SRM 53-15-15, FIG 201. THIS REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS IAW SRI 53-15-15-2-001-00. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT OF 24000SDR FDEA201606011774Rib · crackedLEFT WING CTR FLAP, RIB 26 FOUND CRACKS AT UPPER STRINGER 2.7 & 2.8 LOCATIONS. REPAIRED THE CRACKED RIB IAW EA 6-5750-T0325833, PT1. THIS REPAIR CATEGORY IS "A" MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201606011773Rib · crackedLEFT WING CTR FLAP, RIB 17 FOUND CRACK AT UPPER STRINGER 2.8 LOCATION. REPAIRED THE CRACKED RIB IAW EA 6-5750-T0325833, PT1. THIS REPAIR CATEGORY IS: A. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201606011772Rib · crackedLEFT WING CTR FLAP, RIB 18 FOUND CRACK AT UPPER STRINGER 2.8. REPAIRED THE CRACKED RIB IAW EA 6-5750-T0325833 PT1. THIS REPAIR CATEGORY IS A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201505211591Bottle · dischargedDOOR BOTTLE BLEW WHILE INSTALLING ESCAPE SLIDE. RELEASED FOR SERVICE IAW MEL 52-XX-XX CATEGORY C, EXPIRATION 31 MAY 15. R1 CREW ENTRY DOOR INOPERATIVE. IF SLIDE TO BE RETAINED ONBOARD THEN PRIOR TO EACH DEPARTURE MX MUST VERIFY SLIDE STOWED ACCORDING TO PRSDR FDEA201408132161Fitting · corrodedLEFT RIB 5 MLG FWD LUG HAS CORROSION IN BORE, FWD FACE & AFT FACE. COMPLIED WITH EA 6-5710-T0310496 P1 WINGS BASIC WING STRUCTURE LT & RT RIB 5 FWD LUG CORROSION.SDR FDEA201408132160Fitting · corrodedRIGHT RIB 5 MLG FITTING FWD LUG BORE, FWD FACE & AFT FACE HAVE CORROSION. COMPLIED WITH EA 6-5710-T0310496 P3 WINGS BASIC WING STRUCTURE LT & RT RIB 5 FWD LUG CORROSION.SDR FDEA201406081359Unknown · unknownWHEN LEVELING AT FL 330, YAW DAMPER 1 & ATS 1 & 2 TRIPPED OFF. COMPLIED WITH ECAM & QRH & SYS WOULD NOT RESET. FLIGHT DIRECTOR 1 ALSO INOPERATIVE, AND IVSI NR 1 AMBER IVS INDICATION. NO TRIFOIL EFIS LAST FLIGHT LEG SHOWED 1 FCC & 1 TCC FAIL. MTP SHOWS ON SDR FDEA201404240800Support Beam · corrodedNLG BAY LT LATERAL PANEL LOWER SUPPORT BEAM INTERNAL SURFACE CORRODED AT AV COMPARTMENT FRAME 11A STRINGER49L, COMPLIED WITH EA 6-5310-T0307525 A. TITLE FUSELAGE, MAINFRAME, CORROSION ON KEEL LATERAL AT FRAME 11 - FRAME 11A, STRINGER 49L. REPAIRED NLG BAY LTSDR FDEA201404230787Frame · crackedCENTER WING JOINT AT FRAME 40 HAD A CRACK SIGNAL. REPAIRED IAW EA 6-5710-127939 B PART 2. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404230786Frame · crackedCENTER WING JOINT AT FRAME 40 HAS A CRACK SIGNAL. REPAIRED IAW EA 6-5710-127939 B PART 2. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404230785Frame · crackedCENTER WING JOINT AT FRAME 40, HAS A CRACK SIGNAL. REPAIRED IAW EA 6-5710-127939 B PART 2. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404210766Sill · crackedRIGHT AFT PAX DOOR LOWER SILL BEAM HAS A CRACK SIGNAL AROUND FASTENER HOLE BETWEEN FRAMES 75 - 75A AT STRINGER 26R. REPAIRED IAW EA 6-5318-T0307544 PART 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404190754Skin · crackedFUSELAGE SKIN AT FRAME 13 CIRCUMFERENTIAL JOINT MID FASTENER HOLE WITH CRACK SIGNAL AT ABOUT STRINGER 23R. REPAIRED IAW EA 6-5330-T0307377 A PART 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404190753Skin · crackedFUSELAGE FRAME 13 CIRCUMFERENTIAL JOINT FWD FASTENER HOLE WITH CRACK SIGNAL AT ABOUT STRINGER 23L. REPAIRED IAW EA 6-5330-T0307377 A PART 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404020621Spar · crackedCENTER WING BOX, INSPECTION OF REAR SPAR & BOTTOM PANEL FOUND WITH A CRACK SIGNAL RT SIDE. REPAIRED IAW 6-5710-T0307446 PART1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404020620Skin · crackedCENTER WING BOX INSPECTION OF REAR SPAR & BOTTOM PANEL FOUND WITH A CRACK SIGNAL LT SIDE. REPAIRED IAW EA 6-5710-T0307446 PART1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404020630Frame · chafedJUNCTION BETWEEN CENTER WING BOX & CRUCIFORM FITTING BETWEEN FRAMES 40 - 44. NDT CHECK FOUND FRAME 43 RT WALL DAMAGED. REPAIRED IAW EA 6-5710-T0307097 A PART 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404020629Frame · crackedJUNCTION BETWEEN CENTER WING BOX & CRUCIFORM FITTING BETWEEN FRAMES 40 - 44. NDT CHECK FOUND FRAME 43 WITH A CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307097 A PART1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404020626Frame · crackedJUNCTION BETWEEN CENTER WING BOX & CRUCIFORM FITTING BETWEEN FRAMES 40 - 44. NDT CHECK FOUND FRAME 42 RT OTBD FASTENER HOLE WITH CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307097 A PART1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404020625Fitting · crackedJUNCTION BETWEEN CENTER WING BOX & CRUCIFORM FITTING BETWEEN FRAME 40 - 44, FRAMES & STIFFENERS NDT CHECK FOUND FRAME 41 RT OTBD FASTENER HOLE WITH CRACKED SIGNAL. REPAIRED IAW 6-5710-T0307097 A PART1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404020624Frame · crackedJUNCTION BETWEEN CENTER WING BOX & CRUCIFORM FITTING BETWEEN FRAME 40 - 44, AT FRAMES & STIFFENERS NDT CHECK, FOUND FRAME 41 WITH A CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0307097 A PART1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201402040255Terminal · brokenIMMEDIATELY AFTER TAKEOFF RECEIVED, FIRST OFFICER`S PROBE HEAT, FAULT ON ECAM WITH CORRESPONDING FIRST OFFICER`S PITOT LIGHT ON PROBE HEAT PANEL. ON LANDING THE PITOT LIGHT WENT OUT. ADDED MPN 180RU01Z01W00A, CPN 2110776 QTY 1. R & R RELAY 154GB & DETECTOR SDR FDEA201401150104Switch · failedFORWARD CARGO DOOR LIGHT CAME ON AT FL320 JUST LEVELED OFF LIGHT REMAINED ON & CABIN PRESS BEGAN RISING AT 500 FT. BEGAN EMERGENCY DESCENT TO FL100. MAX CABIN PRESS REACHED WAS 9500 FT, DECLARED EMERGENCY & DIVERTED TO KPHL. UNEVENTFUL LANDING & TAXI IN. SDR FDEA201312162993Switch · dirtyFL 340, FWD CARGO NOT CLOSED WARNING ON ECAM. CABIN ALT WAS AT 300 FEET PER MINUTE. DESCENDED TO FL 100 & LIGHT EXTINGUISHED AT APPROXIMATELY 15,000'. CABIN ALT THEN STARTED TO DESCEND. INSPECTED FWD CARGO DOOR SEAL, NO DEFECTS NOTED. CLEANED & LUBED FWD SDR FDEA201308161914Pressure Switch · failedDURING CLIMBOUT, GREEN HYD SYS LOW AIR ILLUMINATED. LOW AIR WENT OFF ABOVE 5000 FT. FOLLOWED BY GREEN SYS NR 1 LOW PRESS LIGHT ON ECAM. LOW AIR ILLUMINATED AGAIN DURING DESCENT. SYS PRESSURE REMAINED NORMAL. CREW STATED NR 2 GREEN PUMP SYS PRESSURE WAS
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