N725FD
Service difficulty reports · 220
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 = 'N725FD' 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 = 'N725FD' 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 FDEA202607080864Warning Buzzer · inoperativeDURING POST-FLIGHT, L1 DOOR SLIDE WARNING BUZZER INOP, WARNING LIGHT OPERATES NORMAL. RELEASED FOR SERVICE PER MEL: 52-73-01-02 CATEGORY C L1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM BUZZERS INOP. MEL: 52-73-01-02. PERFORMED BITE OF ASPSU (70WN). TESTSDR FDEA202605280641Hydraulic Line · leakingCLIMBING THROUGH FL200 COMPLETE LOSS OF GREEN HYDRAULIC SYSTEM. DECLARED AN EMERGENCY AND RETURNED TO MEMPHIS. FOLLOWED QRH PROCEDURES, LANDED UNEVENTFULLY, AND WAS TOWED TO GATE. FOUND FLEX LINE GOING TO LH MANIFOLD-DUAL CONNECTING BLOCK DAMAGED. REMOVED SDR FDEA202602140198Safety Wire · wrong partL1 DOOR SLIDE EJECTOR BAG RELEASE CABLE ATTACHMENT HAS INCORRECT SAFETY WIRE. REQUIRES CAD PLATED COPPER SAFETY WIRE REF FEA 6-2560-F0386375 A P1 STEP 8. FEA: 6-2560-F0386375 A P1 CMM: 25-60-40 RE SAFETIED EJECTOR BAG CABLE ATTACHMENT WITH CAD PLATED COSDR FDEA202506281072Spar · crackedNDT INSP - RT WING FUEL TANK RIB9 REAR SPAR LOWER BOOM OUTBD HOLE W FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0383952 P1 TO REPAIR RH WING REAR SPAR BOTTOM FLANGE HOLE W/558 BETWEEN RIB9 AND 10 CRACKS. THIS EA DEVIATES FROM EO 6-5710-7-5001.THIS IS A CATSDR FDEA202506281071Fitting · damagedCOMPLY WITH EO 6-5230-E0378588 B P5. COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - 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. REPLACED THE MAINSDR FDEA202506100863Stringer · corrodedFWD CARGO FR38.2 - FR39, S44R STRINGER CORRODED. REPAIRED THE CORRODED STRINGER AT FR38.2 - FR39, S44R PER A300-600 SRM53-10-14 & EA:6- 5310-T0383790 P1. TITLE: FUSELAGE - MAINFRAME - STRINGER REPAIR AT STGR44R, FR38.2 - FR39. THIS IS CAT B REPAIR AND MUST SDR FDEA202403280389Control Handle · failedON TAKEOFF FROM MEM, WITH LDG GEAR POSDET ON SYS 1, WITH LNDGGEAR HANDLE UP, LANDING GEAR INDICATED 3 GREEN TRIANGLES, 3 RED UNLOCKED LIGHTS AND NO DOOR LIGHTS ILLUMINATED. AFTER SWITCHING TO POSDET 2 AND RAISING THE HANDLE, AFTER SHORT DELAY, THE GEAR RESDR FDEA202307061183Unknown · unknownAIRCRAFT STRIKE. FUSELAGE DAMAGE AFT OF RADOME. COMPLIED WITH EA # 6-5310-T0375157 PART 1 & 2 FUSELAGE MAINFRAME FRAME 0-FRAME 1/ LOWER FUSELAGE SKIN AT 6 O'CLOCK POSITION STRUCTURALE REPAIR FOR DENT/CREASE TO FRAME AND SKIN.SDR FDEA202303300668Crossbeam · corrodedIN FWD LOWER CGO COMPT EXFOLIATION CORROSION WAS FOUND AT CROSS BEAM AT FR32 JUNCTION TO ROLLER TRACK -Y1500 ABOVE STGR-43R CUT OUT THE CORROSION BEAM AND FABRICATED THE REPAIR PARTS, WET INSTALLED THE REPAIR PARTS WITH FASTENERS. I.A.W A300-600 SRM 53-10-SDR FDEA202303280781Spoiler · wornLH WING ONE ANCHOR NUT ATTACH SKIN ENLARGED AT O/B WEB AREA OF #2 SPOILER FRONT SPAR CAVITY ACCOMPLISHED THE REINFORCEMENT REPAIR, THIS IS CAT.A REPAIR I.A.W FEDEX EA NO:T6-5750- T0373843 P1, SEQ NO:816, TITLE:WING-FLIGHT SURFACES-LH #2 SPOILER-WEAR DAMAGE SDR FDEA202303250707Coupling · crackedMAIN DECK FLOOR STRUCTURE FOUND STRINGER COUPLING CRACK AT FR73A STGR26L BELOW FLOOR AREA FABRICATED NEW SECTION AND INSTALLED WITH SEALANT & FASTENERS I.A.W AIRBUS DRAWING:A53980177(SHEET-1) & GMM 7-0-1001 & A300-600 SRM 51-40-21-001, PARA.7, PAGE.24-50 SDR FDEA202303240769Adapter · wornMAIN DECK - CROSSBEAM FITTED WITH CLS ADAPTER GOT 2EA WORN MARKS AT FR54.1 AND FROM -Y450 TO -Y953 FABRICATED THE ADAPTER PLATE AND WET INSTALLED WITH NEW FASTENERS. I.A.W EA#:T6- 5321-T0373945 P1, TITLE:FUSELAGE-CARGO COMP FLOORS-MAIN DECK CARGO COMPARTMENSDR FDEA202303240766Web · misalignedAFTER REMOVED BUSH INSTALLED ON CWB(CENTER WING BOX) FR44 BEAM RH CUTOUT DOUBLER(Y-212), FOUND HOLE ECCENTRICITY DEVIATION REAMED AND INSTALLED THE BUSH TO THE DAMAGE HOLE, INSTALLED WITH NEW FASTENER I.A.W FEDEX EA NO:T6-5710-T0303307 A PART.3, SEQ NO:808SDR FDEA202303200755Frame · cracked1EA CRACK (1'') WAS FOUND AROUND RIVET HEAD OF LH PAX DOOR FR73A. ACCOMPLISHED THE SPLICE REPAIR WITH NEW FRAME SECTION I.A.W FEDEX EA NO: T6-5310- T0373688 P1, SEQ NO:810, TITLE:FUSELAGE-MAINFRAME-EO 6-5310-E0327267(SB A300-53-6175) INSPECTION -CRACK FOUNDSDR FDEA202303200667Skin · delaminated1EA DISBOND AREA WAS FOUND AT RH #5 SPOILER TOP SKIN.(1.3"X1.4") ACCOMPLISHED THE COMPOSITE REPAIR, THIS IS CAT.A REPAIR I.A.W A300-600 SRM 57-72-11-201, PARA.12, PAGE.211-217, FIG.207 "MAJOR REPAIR"SDR FDEA202303190767Stiffener · corrodedAVIONICS COMP'T BILGE AREA OF STIFFENER CORROSION BETWEEN FR18 AND FR19,S-51L POSITION. REPLACED THE DAMAGE STIFFENER WITH NEW PART I.A.W A300-600 SRM 51-72-10-001.PAGE 2SDR FDEA202303190756Seat Track · corrodedMAIN DECK - SEAT TRACK CROWN AREA GOT CORROSION LOCATION FROM FR14 TO FR15A AND - Y450 REPLACED THE DAMAGE SEAT TRACK WITH NEW I.A.W A300-600 SRM 51-72-10-001.PAGE.2SDR FDEA202303180657Rudder · corrodedRUDDER T/E ANGLE STRIP GOT MINOR CORROSION FROM RIB18-23 ( TOTAL 5 POINT) PFM REPAIR OF APEX STRIP BY NEW STRIP SECTIONS AND CONNECTION PLATES WITH RIVETS, THIS IS CAT.B REPAIR I.A.W A300-600 SRM 55-41-12-201, PARA.16, PAGE.237-239, FIG.208C & SRI:55- 41-12SDR FDEA202303170658Rudder · damaged1EA WATER TRAPPED AREA(50MMX150MM) WAS FOUND AT NO.13 SCREW OF LH RUDDER SIDE PANEL. ACCOMPLISHED THE COMPOSITE STRUCTURE CAT.B REPAIR AT SCREW LINE IN REPAIR ZONE P I.A.W A300-600 SRM 55-41-12-201, PARA.31, PAGE.313-324, FIG.221, & SRI:55-41-12-201, IIR:5SDR FDEA202303150768Doubler · crackedMAIN LANDING GEAR BAY CEILING L/H BONDED DIAPHRAGM U-SHAPE DOUBLER CENTER SECTION A POINT GOT CRACK AT FR49 PLUS 6" AND BEAM4 TO BEAM5 TRIMMED THE DAMAGED AREA AND REINFORCED WITH FILLER & DOUBLER I.A.W FEDEX EA NO:T6-5310-T0373853 P1, SEQ NO:812, TITLE:FUSDR FDEA202303150710Skin · damaged1EA WATER TRAPPED AREA (40MMX60MM)WAS FOUND AT NO.28 FASTENER OF RH ELEVATOR TOP SKIN.(COUNTING FROM I/B TO O/B) REPAIRED THE DAMAGE AREA WITH CORE AND PLIES.THIS IS CAT.B REPAIR. I.A.W A300-600 SRM 55-21-12-201-2, PARA.5J, PAGE.266-270, FIG.212(SHEET-3) SDR FDEA202303150709Skin · damaged1EA WATER TRAPPED AREA (65MMX95MM)WAS FOUND AT NO.30 FASTENER OF LH ELEVATOR TOP SKIN.(COUNTING FROM I/B TO O/B) REPAIRED THE DAMAGE AREA WITH CORE AND PLIES.THIS IS CAT.B REPAIR. I.A.W A300-600 SRM 55-21-12-201-2, PARA.5J, PAGE.266-270, FIG.212(SHEET-3) &SDR FDEA202303150708Skin · damaged1EA WATER TRAPPED AREA (75MMX85MM)WAS FOUND AT NO.18 FASTENER OF LH ELEVATOR TOP SKIN.(COUNTING FROM I/B TO O/B) REPAIRED THE DAMAGE AREA WITH CORE AND PLIES.THIS IS CAT.B REPAIR. I.A.W A300-600 SRM 55-21-12-201-2, PARA.5J, PAGE.266-270, FIG.212(SHEET-3)SDR FDEA202303030656Floorbeam · corrodedBULK CARGO COMPARTMENT FLOOR BEAM EXTERNAL SURFACE GOT CORRODED BETWEEN Y140~-Y810 POSITION,FR66. REMOVED THE DAMAGED FLOOR BEAM AND FABRICATED THE REPAIR PARTS, WET INSTALLED THE REPAIR PARTS I.A.W A300-600 SRM 53-10-15-201, PARA.9, FIG.207, PAGE.237~242,SDR FDEA202211302861Tire · failedNR 3 TIRE FAILED ON LANDING. REMOVED AND REPLACED THE NR 3 TIRE IAW AMM 32-41-11-04-02, PERFORMED GENERAL VISUAL INSPECTION OF ALL ADJACENT COMPONENTS, ADDITIONAL DAMAGE NOTED IN WRI 32-43-7691, PERFORMED BRAKE CHECK IAWSDR FDEA202009282349Skin · dentedFUSELAGE SKIN DENTED, BETWEEN FR 52 AND FR 53, STGR 38R AND STGR 40R. REPAIRED THE FUSELAGE SKIN DENT (OIL CAN) BETWEEN FR 52 AND FR 53, STGR 38R AND STGR 40R, PER A300-600 SRM53-10-12 FIG.223. THIS REPAIR CATEGORY B. THE FIRST INSPECTION THRESHOLD IS 51000SDR FDEA202009252348Skin · crackedUPPER FUSELAGE FR 13 STGR 9R, 1 EA FASTENER HOLE FOUND WITH CRACK SIGNAL (AFT THIRD HOLE FROM LAP JOINT COUNTING FROM BOTTOM). COMPLIED WITH FEDEX EA: 6-5310-T0356680 PT1, EA TITLE: FUSELAGE-MAINFRAME-REPAIR OF CRACKED HOLE IN CIRCUMFERENTIAL JOINT AT FR 13 RSDR FDEA202009252347Skin · crackedUPPER FUSELAGE FR 13 STGR 9R, 1 EA FASTENER HOLE FOUND WITH CRACK SIGNAL (AFT THIRD HOLE FROM LAP JOINT COUNTING FROM BOTTOM). COMPLIED WITH FEDEX EA: 6-5310-T0356680 PT1, EA TITLE: FUSELAGE-MAINFRAME-REPAIR OF CRACKED HOLE IN CIRCUMFERENTIAL JOINT AT FR 13 RSDR FDEA202009182346Frame · crackedLOWER FUSELAGE FR 40, CENTER WING JOINT FOUND LT MIDDLE HOLE WITH CRACK. SIGNAL COMPLIED WITH FEDEX EA: 6-5710-T0356552 PT1, EA TITLE: WINGS-BASIC WING STRUCTURE-CRACK IN THE HOLES AT FR 40 LT AND RT CENTER WING JOINT. REPAIRED LOWER FUSELAGE FR 40, CENTER WSDR FDEA202009182345Frame · crackedLOWER FUSELAGE FR 40, CENTER WING JOINT FOUND LT MIDDLE HOLE WITH CRACK. SIGNAL COMPLIED WITH FEDEX EA: 6-5710-T0356552 PT1, EA TITLE: WINGS-BASIC WING STRUCTURE-CRACK IN THE HOLES AT FR 40 LT AND RT CENTER WING JOINT. REPAIRED LOWER FUSELAGE FR 40, CENTER WSDR FDEA202009182342Frame · crackedLOWER FUSELAGE FR 40, CENTER WING JOINT FOUND LT UPPER HOLE WITH CRACK. SIGNAL COMPLIED WITH FEDEX EA: 6-5710-T0356552 PT1, EA TITLE: WINGS-BASIC WING STRUCTURE-CRACK IN THE HOLES AT FR 40 LT AND RT CENTER WING JOINT. REPAIRED LOWER FUSELAGE FR 40, CENTER WISDR FDEA202009182341Frame · crackedLOWER FUSELAGE FR 40, CENTER WING JOINT FOUND LT UPPER HOLE WITH CRACK. SIGNAL COMPLIED WITH FEDEX EA: 6-5710-T0356552 PT1, EA TITLE: WINGS-BASIC WING STRUCTURE-CRACK IN THE HOLES AT FR 40 LT AND RT CENTER WING JOINT. REPAIRED LOWER FUSELAGE FR 40, CENTER WISDR FDEA202009182340Frame · crackedLOWER FUSELAGE FR40, CENTER WING JOINT FOUND RT UPPER HOLE WITH CRACK. SIGNAL COMPLIED WITH FEDEX EA: 6-5710-T0356552 PT1, EA TITLE: WINGS-BASIC WING STRUCTURE-CRACK IN THE HOLES AT FR 40 LT AND RT CENTER WING JOINT. REPAIRED LOWER FUSELAGE FR 40, CENTER WINSDR FDEA202009152324Beam · crackedNDT INSPECTION FOUND FUSELAGE MAINFRAME RT NR 2 GANTRY OUTBOARD FLANGE WITH CRACK SIGNAL AT FR 51.A. REPAIRED THE FUSELAGE MAINFRAME RT NR 2 GANTRY OUTBOARD FLANGE AT FR 51.A, PER AIRBUS DWG R53810581 ISSUE C. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GSDR FDEA202009152323Beam · crackedNDT INSPECTION FOUND FUSELAGE MAINFRAME LT NR 2 GANTRY OUTBOARD FLANGE WITH CRACK SIGNAL AT FR 51.A. REPAIRED THE FUSELAGE MAINFRAME LT NR 2 GANTRY OUTBOARD FLANGE AT FR 51.A, PER AIRBUS DWG R53810581 ISSUE: C. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX SDR FDEA202009152322Beam · crackedNDT INSPECTION FOUND FUSELAGE MAINFRAME LT NR 2 GANTRY OUTBOARD FLANGE WITH CRACK SIGNAL AT FR 51.A. REPAIRED THE FUSELAGE MAINFRAME LT NR 2 GANTRY OUTBOARD FLANGE AT FR51.A, PER AIRBUS DWG R53810581 ISSUE: C. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GSDR FDEA202009102321Stringer Splice · crackedUPPER FUSELAGE FR 47 S 18L CRACK ON STRINGER CONNECTION SECTION. REPLACED THE CRACKED STRINGER SPLICE AT UPPER FUSELAGE FR 47 STGR 18L AND COMPLETED, PER A300-600 SRM51-40-21. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM6-2-100.SDR FDEA202009102320Stringer Splice · crackedUPPER FUSELAGE FR 47 S18L CRACK ON STRINGER CONNECTION SECTION. REPLACED THE CRACKED STRINGER SPLICE AT UPPER FUSELAGE FR 47 STGR 18L AND COMPLETED, PER A300-600 SRM51-40-21. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM6-2-100.SDR FDEA202009102310Panel · crackedAFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL CRACKED BETWEEN FR 59 AND FR 64. REPLACED AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL BETWEEN FR 59 AND FR 64, PER A300-600 SRM51-40-21. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM 6-2-SDR FDEA202009102309Panel · crackedAFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL CRACKED, BETWEEN FR 59 AND FR 64. REPLACED AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL BETWEEN FR 59 AND FR 64, PER A300-600 SRM51-40-21. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM 6-2SDR FDEA202009102308Panel · crackedAFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL CRACKED, BETWEEN FR 59 AND FR 64. REPLACED AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL BETWEEN FR 59 AND FR 64. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM 6-2-100.SDR FDEA202009102307Panel · crackedAFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL CRACKED, BETWEEN FR 59 AND FR 64. REPLACED AFT CARGO COMPARTMENT DOOR LOWER CUTOUT MILL BOX PANEL BETWEEN FR 59 AND FR 64. THIS REPAIR CATEGORY A MAJOR REPAIR, IAW FEDEX GMM 6-2-100.SDR FDEA202006091165Hydraulic Line · leakingAT FL340, .79 MACH, GRN HYD RSVR LO LEVEL INDICATION RECEIVED. COMPLIED W/ECAM. ZERO FLUID ON OVERHEAD PANEL & ON ECAM GREEN SYSTEM. RAN QRH: HYD RSVR LO LEVEL & HYD SYS LP PR. MANUALLY EXTENDED GR IAW QRH. NO NOSEWHEEL STEERING - TOWED BACK. EMERGENCY SDR FDEA2019022630485Floor Panel · damagedMAIN DECK CARGO COMPARMENT ZONE 230 FLOOR PANEL 231TG HAS BROKEN CORNER FABRICATED NEW FLOOR PANEL PER SRZ-25-005 REV. PSDR FDEA2018092522662Brake · crackedMDIS 725 32-43 2981 22SEP18 DSM FACT U DURING #5 WHEEL CHANGE FOUND #5 BRAKE ASSY TO HAVE SEVERAL CRACKED, BROKEN, AND MISSING DRIVE KEY SEGMENTS AND REINFORCEMENTS. R/I 22SEP18 02:22 DSM U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFFSDR FDEA201809202630Warning System · false activationNR 2 ENGINE LOOP "B" FAULT DURING CRUISE AT FL 300. EXTINGUISHED DURING DESCENT. CREW DEBRIEF INDICATED THAT B LOOP LIGHT NEVER ACTUALLY CAME ON JUST FLICKERED. HAS HISTORY, PERFORMED ENG FIRE TEST REF AMM 26-12-05, TEST GOOD, BITE TEST OF FDCU NO FAULTS. RAN SDR FDEA201804261122Frame · crackedMAIN FRAME, LT SIDE NT 3 GANTRY INBD SIDE LOWER FLANGE WITH CRACK SIGNAL BETWEEN FRAMES 50.A AND 50.B.SDR FDEA201804261121Frame · crackedMAIN FRAME, RT SIDE NR 3 GANTRY INBD SIDE, LOWER FLANGE WITH CRACK SIGNAL BETWEEN FRAMES 50.A AND 50.BSDR FDEA201804100956Door Frame · crackedFWD CARGO COMPARTMENT DOOR ACTUATOR ATTACH FRAME FOUND CRACK AT FR22A.SDR FDEA201804090953Bulkhead Web · crackedMAIN DECK CARGO, HORIZONTAL PRESSURE VERTICAL WEB CRACKED AT FRAME 47, BETWEEN Y0 AND Y-450. REPLACED PRESSURE VERTICAL WEB IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.
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