N722FD
Service difficulty reports · 191
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 = 'N722FD' 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 = 'N722FD' 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 FDEA202608271240Adapter · damagedRAMP ONLOAD CREW REPORTS A RESTRAINT SEPERATED FROM THE FLOOR ON THE FORWARD SIDE OF 13C IN MAIN CARGO. BESIDES THE BROKEN FLOOR TRACK LOBES-NO OTHER DAMAGE FOUND ON THE FLOOR TRACK OR ADJACENT FLOOR PANELS. OIL LBB NO RESTRICTION IAW DWG SR30-53-003. SDR FDEA202604120430Bottle · leakingON TAKEOFF OUT OF SNA WHEN WE RETRACTED THE GEAR THERE WAS A LOUD GRINDING SOUND AND EXCESSIVE VIBRATIONS. IN MEM ON FINAL WHEN WE SELECTED GEAR DOWN THERE WERE VIBRATIONS AND THE GEAR DID NOT EXTEND. THE DOORS SHOWED OPEN. ON THE GO AROUND THE GEAR CAME SDR FDEA202602140219Elec Connector · dirtyWHEN R1 SLIDE ARMED NO INDICATION ON ECAM OF SLIDE BEING ARMED. AMM: 52-73-13-05-01 CLEANED CONNECTOR AT ESCAPE SLIDE ARM SWITCH 14WN PER ESPM 20-55-50-0. PERFORMED ADJUSTMENT TEST OF ESCAPE SLIDE IAW AMM 52-73-13-05-01. OPS CHECKS GOOD OK FOR SERVICSDR FDEA202506170977Repair · no discrepancyEXISTING REPAIR ON RH O/B FLAP L/E SKIN BETWEEN RIB1 AND RIB2 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RH O/B FLAP L/E SKIN BETWEEN RIB1 AND RIB2 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM57-50-00-201 FIG.208. EO 6-5100-7-5000SDR FDEA202506141065Skin · crackedLWR FUSELAGE SKIN LAP JOINT AROUND FASTENER AT FR53-54, S44L FOUND CRACK. COMPLIED WITH EA:6-5330-T0383917 P1 REPAIRED LWR FUSELAGE THE CRACKED SKIN LAP JOINT AROUND FASTENER AT FR53-54,S44L. EA TITLE: FUSELAGE - PLATES & SKINS - CRACKED HOLES ON SKIN PANESDR FDEA202506140976Flap · misrepairedEXISTING REPAIR ON LT O/B FLAP L/E SKIN BETWEEN RIB13 AND RIB15 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON LH O/B FLAP L/E SKIN BETWEEN RIB13 AND RIB15 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600 SRM57-50-00-201 FIG.208. RE-REPAIRESDR FDEA202506130997Skin · delaminatedRH WING #4 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: 30MM*10MM, DEPTH: 1.34MM COMPLIED WITH EA 6-5750-T0383788 P1 TO REPAIR RH WING #4 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE SKIN DELAMINATION, EA TITLE: WING - FLIGHTSDR FDEA202506130996Skin · delaminatedRH WING #3 SPOILER CENTER I/B & O/B HINGE ARMS OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: (1)80MM*40MM, DEPTH: 1.3MM (2)80MM*40MM, DEPTH: 1.4MM COMPLIED WITH EA 6-5750-T0383786 P1 TO REPAIR RH WING #3 SPOILER CENTER I/B & O/B HINGE ARMS OUTSIDE SURFACESDR FDEA202506130995Skin · delaminatedLH WING #5 SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: 40MM*20MM, DEPTH: 1.37MM COMPLIED WITH EA 6-5750-T0383770 P1 TO REPAIR LH WING #5 SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE SKIN DELAMINATION, EA TITLE: WING - FLIGHTSDR FDEA202506130994Skin · delaminatedLH WING #3 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: 90MM*10MM, DEPTH: 1.56MM COMPLIED WITH EA 6-5750-T0373146 A P2 TO REPAIR LH WING #3 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE SKIN DELAMINATION, EA TITLE:WING - FLIGHSDR FDEA202506130975Repair · no discrepancyEXISTING REPAIR ON FUSELAGE STRINGER S52R BETWEEN FR67 AND 68 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FUSELAGE STRINGER S52R BETWEEN FR67 AND 68 WAS EVALUATED AND FOUND IN CONFROMITY WITH A300-600 SRM53-10-14-201 FIG.201. EO6-5100-7-5000SDR FDEA202506130974Repair · no discrepancyEXISTING REPAIR ON FUSELAGE STRINGER S51R BETWEEN FR67 AND 68 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER S51R BETWEEN FR67 AND 68 WAS EVALUATED AND FOUND IN CONFROMITY WITH A300-600 SRM53-10-14-201 FIG.201. EO6-5100-7-5000 SDR FDEA202506130973Repair · no discrepancyEXISTING REPAIR ON FUSELAGE STRINGER S50R BETWEEN FR67 AND 68 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER S50R BETWEEN FR67 AND FR68 WAS EVALUATED AND FOUND IN CONFROMITY WITH A300-600 SRM53-10-14-201 FIG.201. EO6-5100-7-500SDR FDEA202506061126Fitting · not reportedDOORS - CARGO 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 B P5. REPLACED THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS. THSDR FDEA202506061128Crossbeam · corrodedAFT CARGO FLOOR BEAM CORRODED, AT FR56,Y805-Y1470. REPAIRED THE CORRODED FLOOR BEAM AT AFT CARGO FR56,Y805-Y1470 PER A300-600 SRM53- 10-15-201 FIGURE 207 & EA 6-5321-T0383821 P1. EA TITLE:FUSELAGE - CARGO COMP FLOOR - AFT CARGO FRAME 56 CROSSBEAM - SRM REPASDR FDEA202412101784Limit Switch · dirtyR1 DOOR WILL NOT ARM. CLEANED THE 14WN LIMIT SWITCH ON THE RH DOOR IAW AMM 52-73-13-05-01. OPS CHECK GOOD AT THIS TIME. ACFT OK FOR SERVICE.SDR FDEA202406030773Power Supply · inoperativeBOTH R1 AND L1 DOOR ESCAPE SLIDE RELEASE WARNING SYSTEM LIGHT TEST FAILED - AUDIBLE BUZZERS WORK ON BOTH DOORS. CHECKING ASPSU TEST SWITCH RESULTED IN NO LIGHTS AT ALL - BOTH BATTERIES APPEAR DISCHARGED. - REMOVED AND REPLACED BOTH BATTERIES IAW AMM 52-SDR FDEA202303080392Aileron · dentedLH WING AILERON TRAILING EDGE WEDGE UPPER SURFACE FOUND SMALL DENTS COMPLIED WITH EA: 6-5750-T0373267 P1. TITLE: WING - FLIGHT SURFACES - LH AILERON TRAILING EDGE WEDGE UPPER SURFACE REPAIR. AND REFER TO A300-600 SRM51-77-12-201 PARA.4.B FIGURE 218 & AMM57SDR FDEA202303030370Spar · crackedRH PYLON LWR SPAR FOUND CRACK BETWEEN RIB6 AND RIB7 AT STIFFENER END BY EDDY CURRENT INSPECTION COMPLID WITH EA: 6-5450-T0373394 P1. TITLE: NACELLES/PYLON - WING PYLON/STRUT - #2 ENGINE PYLON LOWER SPAR CRACK BETWEEN RIB 6&7 - REPAIR. REPAIRED THE RH PYLONSDR FDEA202303030369Fitting · crackedRH WING CENTER SPAR TO RIB 1 SPLICE VERTICAL FLANGE 1EA FASTENER HOLE(TYPE 5) FOUND CRACK SIGNAL BY ULTRASONIC INSPECTION COMPLIED WITH EA: 6-5710-T0373257 P1. TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLE ON FITTING RH WING CWT SPAR TO RIB1. REPAIRED TSDR FDEA202303030368Panel · crackedLH PYLON O/B SIDE PANEL AT RIB8 FOUND 1EA CRACK. REPAIRED THE CRACKED LH PYLON O/B SIDE PANEL AT RIB8 PER EO: 6-5450-7-5003 I PT3 & A300-600 SRM54-51-31-201-2. EO TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB8. AIRBUS SB A300-54-6015 R03 SDR FDEA202303030367Panel · crackedLH PYLON I/B SIDE PANEL AT RIB8 FOUND 1EA CRACK. REPAIRED THE CRACKED LH PYLON I/B SIDE PANEL AT RIB8 PER EO: 6-5450-7-5003 I PT3 & A300-600 SRM54-51-31-201-2. EO TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB8. AIRBUS SB A300-54-6015 R03 SDR FDEA202303030366Frame · crackedFUSELAGE INTERNAL STRUCTURE - FRAME 14 FOUND CRACK SIGNAL AT JUNCTION AREA OF MAIN DECK FLOOR BEAM AND CRUCIFORM FITTING, RH SIDE, BY ULTRASONIC INSPECTION COMPLIED WITH EA: 6-5310-T0373313 P1. TITLE: FUSELAGE - MAINFRAME - CRACK HOLE FOUND ON FRAME 14 STRSDR FDEA202303030365Spoiler · delaminatedLH WING #3 SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 40MM*10MM, DEPTH: 1.7MM COMPLIED WITH EA: 6-5750-T0373146 P1. TITLE: WING - FLIGHT SURFACES - LH 3# SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE LH WISDR FDEA202303030364Door · crackedRH FWD CREW/COURIER DOOR INTERNAL STRUCTURE FRAME SEGMENT AT FR14C FOUND 2EA CRACKS REPLACED RH FWD CREW/COURIER DOOR CRACKED FRAME SEGMENT AT FR14C WITH A FABRICATED PART PER A300-600 SRM51-40-21 AND DWG: A52111406 (ISSUE.C), A52111327(ISSUE.E). TRACKINSDR FDEA202303030363None · noneLH FWD CREW/COURIER DOOR INTERNAL STRUCTURE FRAME SEGMENT AT FR14C FOUND 1EA CRACKSDR FDEA202205121190Selector Valve · unknownMDIS 722 32-44 2658 12MAY22 MEM OPEN U PER FLIGHT CREW: ON TAXI OUT, HOLDING SHORT OF RUNWAY, PARKING BRAKE WAS SET AND INDICATED PARKING BRAKE ON ON ECAM, HOWEVER WHEN BRAKE PEDALS WERE RELEASED A/C MOVED FORWARD. RECYCLED PARKING BRAKE 4 SDR FDEA202203300785None · noneR1 CABIN DOOR DOES NOT INDICATE ARMED ON ECAM. ALL OTHER INDICATIONS ARE NORMAL. REMOVED POWER FROM ASPCU. AFTER PUTTING POWER BACK ON ASPCU, PERFORMED OPERATIONAL TEST OF R1 AND L1 DOORS ARM FUNCTION AND ALL INDICATIONS WORK PROPERLY AT THIS TIME. OSDR FDEA202203080470None · leakingABOUT 5 TO 10 MINUTES IN CRUISE FLIGHT AT FL340 I NOTICED WITH MY OVERHEAD SCAN THAT THE GREEN HYD QUANTITY WAS MID WAY IN THE YELLOW. I THEN LOOKED AT THE GREEN HYDRAULICS ON THE ECAM AT IT SHOWED 440 PSI. FROM THERE IT WAS A FEW MINUTES AND WE GOT THE ECSDR FDEA202012103112Battery Pack · dislodgedDOOR 1R SLIDE HAS BATTERY PACK FALLING OUT OF SLIDE INTERFERING WITH GIRT BAR ENGAGEMENT. REASON CODE: REMOVAL FROM A/C ONLY, NO INSTALLATION OFF MPN: D30546-509FX CPN: 2513882 POS: R1 SRL: A5756 TAG NBR: 00F514. REMOVED ESCAPE SLIDE FROM DOOR 1R, PER SDR FDEA202012083067Battery · detachedCABIN DOOR R-1 NO SLIDE INDICATION ON ECAM WHEN ATTEMPTED TO ARM DOOR FOR PUSHBACK. RELEASED FOR SERVICE PER MEL: 52-XX-XX-XX CAT: C EXP: 14DEC20 "MEL 52-XX-XX-XX: CREW ENTRY DOOR ESCAPE SLIDE R1-INOPERABLE. SLIDE REMAINS INSTALLED ON DOOR. THIS MEL ITEM WSDR FDEA202012053068Unknown · unknownDURING APPROACH WHILE DECELERATING HEARD AND FELT A THUD. SUSPECT POSSIBLE LOAD SHIFT. RAMP REPORTED CAN UNSECURED IN LOWER FORWARD BELLY, ALLOWING CAN TO SHIFT BETWEEN LOCKS, APPROXIMATELY 5 FEET FORWARD AND AFT. PERFORMED INSPECTION ON PALLET LOCKS, NO DESDR FDEA202011022750Floor Panel · crackedFWD CARGO COMPARTMENT METAL FLOOR PANEL 131LG IS CRACKED. FABRICATED FLOOR PANEL 131LG ON VTMAE TRAVELER T20/1516757, IAW DWG A53272573, PART MARKED PANEL PER GMM 07-0-1001. CLASSIFIED AS CAT "A" AND MAJOR REPAIR.SDR FDEA202011022749Floor Panel · crackedFWD CARGO COMPARTMENT METAL FLOOR PANEL 131NG IS CRACKED. FABRICATED FLOOR PANEL 131NG ON VTMAE TRAVELER T20/1516758, IAW DWG A53272579, PART MARKED PANEL, IAW GMM 07-0-1001, CLASSIFIED AS CAT "A" AND MAJOR REPAIR.SDR FDEA202011022748Floorboard · damagedZONE 240 FLOOR BOARD 241XG IS BROKEN. FABRICATED ZONE 240 FLOOR BOARD 241XG ON VTMAE TRAVELER T20/1518620, IAW DWG SRZ-25-005R, MAJOR REPAIR.SDR FDEA202011022746Floorboard · brokenZONE 260 FLOOR BOARD 261NF IS BROKEN. FABRICATED ZONE 260 FLOOR BOARD 261NF ON VTMAE TRAVELER T20/1518281, IAW DWG SRZ-25-005R, MAJOR REPAIR.SDR FDEA202011022745Floorboard · damagedZONE 230 FLOOR BOARD 232TG IS BROKEN. FABRICATED ZONE 230 FLOOR BOARD 232TG ON VTMAE TRAVELER T20/1518299, IAW DWG SRZ-25-005R, MAJOR REPAIR.SDR FDEA202010312737Floorboard · brokenZONE 250 FLOOR BOARD 252BH IS BROKEN. FABRICATED ZONE 250 FLOOR BOARD 252BH ON VTMAE TRAVELER T20/1518269, IAW DWG SRZ-25-005R, MAJOR REPAIR.SDR FDEA202010312736Floorboard · brokenZONE 260 FLOOR BOARD 261RF IS BROKEN. FABRICATED ZONE 260 FLOOR BOARD 261RF ON VTMAE TRAVELER T20/1518266, IAW DWG SRZ-25-005R, MAJOR REPAIR.SDR FDEA202010312735Floorboard · brokenZONE 250 FLOOR BOARD 251RH IS BROKEN. FABRICATED ZONE 250 FLOOR BOARD 251RH ON VTMAE TRAVELER T20/1518289, IAW DWG SRZ-25-005R, MAJOR REPAIR.SDR FDEA202010312734Floorboard · brokenZONE 250 FLOOR BOARD 252VF IS BROKEN. FABRICATED ZONE 250 FLOOR BOARD 252VF ON VTMAE TRAVELER T20/1518802 IAW DWG SRZ- 25-005R, MAJOR REPAIR.SDR FDEA202010272666Floorboard · damagedZONE 230 FLOOR BOARD 231SG IS BROKEN. FABRICATED ZONE 230 FLOOR BOARD 231SG ON TRAVELER T20/1518654, IAW DWG SRZ-25-005R MAJOR REPAIR.SDR FDEA202010272665Floorboard · damagedZONE 250 FLOOR BOARD 252GF IS BROKEN. FABRICATED ZONE 250 FLOOR BOARD 252GF ON TRAVELER T20/1518616, IAW DWG SRZ-25-005R, MAJOR REPAIR.SDR FDEA202010232625Floor Panel · damagedFWD CARGO COMPT FLOOR PANEL 132RF IS BROKEN. FABRICATED FLOOR PANEL 132RF ON VTMAE TRAVELER T20/1517566, IAW DWG SRZ-25-005R. CLASSIFIED AS CAT "A" REPAIR, MAJOR REPAIR.SDR FDEA202010232624Floor Panel · damagedFWD CARGO COMPT FLOOR PANEL 131RF IS BROKEN. FABRICATED FLOOR PANEL 131RF ON VTMAE TRAVELER T20/1517567, IAW DWG SRZ-25-005R. CLASSIFIED AS CAT "A" REPAIR, MAJOR REPAIR.SDR FDEA202010232623Floor Panel · crackedAFT CARGO FLOOR PANEL 152LF HAS CRACK AND EDGE DAMAGE. FABRICATED FLOOR PANEL 152LF ON VTMAE TRAVELER T20/1519074, IAW DWG SRZ-25-005R. CLASSIFIED AND CATAGORY "A" REPAIR, MAJOR REPAIR.SDR FDEA202010232622Floor Panel · damagedPANEL 151KF HAS NUMEROUS AREAS OF DAMAGE TO EDGES AND MISSING CORE. FABRICATED FLOOR PANEL 151KF ON VTMAE TRAVELER T20/1519073 IAW DWG SRZ-25-005R. CLASSIFIED AS CATAGORY "A" REPAIR, MAJOR REPAIR.SDR FDEA202010222600Seat Track · gougedDOT 66-59 MAIN CABIN SEAT TRACK BETWEEN FR 63-64, Y1456 HAVE GOUGED AREAS. REMOVED DAMAGE AT SEAT TRACK Y 1456 ON SCALLOP HOLE UPPER, IAW SRM 51-73-10. MAXIMUM ALLOWABLE MATERIAL REMOVE IS 0.840" AFTER REWORK IS 0.870" FOUND OUT OF LIMITS, IAW SRM 53-10-16 FSDR FDEA202010222599Floor Support · corroded(DOT 38-79) MDC FLOOR SUPPORT Y730 BETWEEN FR 13-FR 14 CORRODED. NO ESTABLISHED LIMITS, FOUND TO BE OUT LIMITS. FABRICATED FLOOR SUPPORT ON VTMAE TRAVELER T20/1518605, P/N FX-A53612213202, IAW SRM 53-12-15, MAT. NSA 343036, BATCH 3272259. LOCATED AND DRILLSDR FDEA202008059477Switch · wornR1 MAIN CABIN ENTRY DOOR SLIDE WILL NOT ARM. IAW TSM 52-70-00, CHECKED FOR GROUND AT R1 DOOR LIMIT SWITCHES. FOUND EXCESSIVE RESISTANCE AT PIN "E" OF LIMIT SWITCH 1 (42WS), AND OPEN FOUND AT PIN "E" OF LIMIT SWITCH 2 (8WS). NO TIME TO FURTHER TROUBLESHOOT DUE
Back to N722FD