N925FD
Service difficulty reports · 119
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 = 'N925FD' 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 = 'N925FD' 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 FDEA201305030904Girt Bar · out of adjustR1 DOOR REQUIRES OPS CHECK OF ARM AND DISARM. ADJUSTED THE R1 DOOR GIRT BAR FLOOR FITTING IAW FIM 52-11 FAULT TREE 813, AMM 52-11-25-5. R1 DOOR SLIDE ARM AND DISARM OPS CHECKS GOOD.SDR FDEA201303230651Switch · malfunctionedEMERGENCY LIGHT SWITCH WILL NOT MOVE THE LEVER TO ARMED POSITION WHEN IT IS CLOSED. SECURED ARMING SWITCH, ACCOMPLISHED OPS TEST AMM 33-51-00-5. OK FOR SERVICE.SDR FDEA201301300224Slide · inoperativeLT FORWARD ENTRY DOOR SLIDE BAR WILL NOT LOCK. SLIDE LIGHT WILL NOT ILLUMINATE. RELEASED FOR SERVICE IAW MEL: 52-11-01-A CATEGORY: B EXPIRATION: 28JAN13 "MEL 52-11-01-A: L1 DOOR SLIDE, INOPERATIVE." INSTALLED NEW L1 DOOR ESCAPE SLIDE IAW AMM 25-66-01-4. PSDR FDEA201301250173Slide · malfunctionedLEFT FORWARD ENTRY DOOR SLIDE BAR WILL NOT LOCK. SLIDE LIGHT WILL NOT ILLUMINATE. INSTALLED NEW L1 DOOR ESCAPE SLIDE PER AMM 25-66-01-4. PERFORMED A FUNCTIONAL TEST OF THE ARMING SYSTEM PER AMM 52-11-25-5. SYSTEM CHECKED NORMAL.SDR FDEA201209063241Lamp · burned outLEFT DOOR SLIDE LIGHT IS INOPERATIVE. FOUND L1 DOOR INTERIOR "SLIDE" ARMED INDICATOR LAMPS TO BE BURNED OUT. REPLACED LAMPS WITH NEW, INDICATOR LIGHT OPS CHECKED NORMAL REF MM 25-66-11-2.SDR FDEA201208122959Girt Bar · bentL1 DOOR DISARM LEVER BINDS. DID NOT ATTEMPT TO OPEN L1 DOOR DUE TO THIS ISSUE. FOUND EMERGENCY POWER RESERVOIR FOR L1 DOOR READING ZERO PRESSURE. FOUND GIRT BAR BENT. REPAIRED.SDR FDEA201207172594Windshield · shortedELECTRICAL ARCING ON CAPTAIN'S WINDOW, LOWER INBD, ABOUT 12" AND INCREASING. COMPLIED WITH QRH PROCEDURES AND TURNED OFF WINDOW HEAT. R & R CAPTAINS WINDSHIELD AND COMPLETED TORQUE IAW AMM 56-11-01-4.SDR FDEA201205312025Tube · crackedDURING CLIMB, PERFORMANCE WAS SUBSTANDARD. RETURNED TO DEPARTURE. INSPECTION FOUND TUBE FROM P1 PROBE TO COWLING BROKEN OFF. ADEL CLAMP THAT SECURES LINE TO THE INSIDE OF THE NOSE COWL WAS BROKEN ALSO.SDR FDEA201112215403Nut · looseNOSE GEAR STEERING HAS 10-15 DEGREES OF TRAVEL BEFORE STEERING RESULTS. TILLER RETAINING NUT LOOSE, RETORQUED IAW MM 32-51-01-4-0. OK FOR SERVICE. FINAL CLOSEDSDR FDEA201109193953Linkage · misalignedDOOR 1L (LT ENTRY) ARM/DISARM LINKAGE NOT RT DISARMED DOOR AND KNUCKLE RAPPER (ARMED PLACARD) STILL OUT. CYCLED DOOR AND WORKED FINE. T/S SLIDE COVER REMOVED. FOUND "KNUCKLE RAPPER" INDICATOR RUBBING ON DOOR LINER. REPOSITIONED CENTER DOOR LINER. OPS NORMASDR FDEA201106232397Pressure Switch · faultyRECEIVED BRAKE SOURCE AND SYS PRESS LIGHT BUT INDICATING GOOD PRESSURE ON STATUS PAGE FOR L-C-R SYSTEMS. T/S BRAKE SOURCE AND RT HYD SYS PRESS LIGHT IAW ASM 32-41-01. FOUND THE ALT BRAKE SELECTOR VALVE PRESS SWITCH S415 TO BE FAULTY. LIGHTLY TAPPED ON SW SSDR FDEA201106102188Tube · crackedON TAKEOFF ALL WAS NORMAL AT 1000 AGL/3800 MSL THE RT EPR GAGE WAS SLIGHTLY HIGHER THAN THE LT EPR. AS WE CLIMBED, THE LT EPR CONTINUED PROGRESSIVELY GET HIGHER (BIGGER SPLIT) N1 EGT N2, N3. FF APPEARED CORRECT. NO QRH PROCEDURES FOR EPR GAGE SO COMPLIED WISDR FDEA201106082152Tube · crackedAPPROX 5 MINS AFTER T/O THE RT ENG EEC AND A/T INOP EICAS MSG'S WERE DISPLAYED W/CORRESPONDING HIGH EPR. COMPLIED W/QRH PROC'S-REF TO MEL FOR POSSIBLE CONSIDERATIONS. THE STBY & NORMAL INSTRUMENTS DISPLAYED THE SAME DATA W/THROTTLE ADJUSTMENTS. WHEN THE RT SDR FDEA201008253137Bracket · misalignedCABLE SHROUD BRACKET AT STA 1640, IF INSTALLED AT THE CORRECT BUTT LINE WILL HAVE SHORT E.D. ON IT'S OTBD EDGE. DUE TO THE DISCREPANCY EFFECTING THE PTF MOD. A REPAIR WAS ACCOMPLISHED AT STA 1640 BETWEEN STR'S 2L-3L. ON W/C 118550391MS1R03 STAM EA 757-2731-SDR FDEA201008203062Skin · dentedDENT AT STA 760 S-16L . EVALUATED DENT FOUND OUT OF LIMITS DUE TO LOCATION IAW SRM 53-00-01 FIG 101 DET III. ACCOMPLISHED EA F-5330-139213, FUSELAGE PLATES AND SKIN BS 760; S-16L SKIN DENT REPAIR. PN 143N3650-1. A=1.9",Y=.033",A/Y=57.5. MAJOR REPAIR.SDR FDEA201008173030Fitting · damagedRT WING INBD SIDE LOAD FITTING OTBD LEG 2EA CODE 'C' FASTERNER HOLES ELONGATED WHILE REMOVING TO COMPLY WITH SIP MOD. REPAIR ACCOMPLISHED ON STAM EA 757-5724-16-F2734. REV- ISSUED 06/29/10. EA F5720-139218 WINGS- ATTACH FITTINGS-(AD2004-12-07) NR2 ENGINE PYLOSDR FDEA201008163010Seat Track · misalignedWATERLINE MISMATCH BETWEEN SEAT TRACK CROWNS AT STA 640 AND 780 RBL 24.75 AND RBL 45.50 THE WATERLINE MISMATCH AT SEAT TRACKS LOCATED AT STA 660 AND 780 RBL 24.75 AND RBL 45.50. REPAIRS ACCOMPLISHED ON STAM EA 757-5335-16-F2656 REV - DATED 04/23/2010; 81SDR FDEA201008102911Skin · damagedL-4 DOOR LOWER SILL FUSELAGE SKIN HAS ONE SCREW HOLE ELONGATED. ACCOMPLISHED EA F 5330-139174. FUSELAGE ELONGATED HOLE IN SKIN NEAR L4 DOOR OPENING. MAJOR REPAIR.SDR FDEA201008102908Stringer · unknownSTA 660 AT S-20L UNABLE TO INSTALL STRINGER SPLICE PN 657N3250-24 DUE TO INCOMING CONDITION (PREVIOUS REPAIR). IN ADDITION TO THIS BETWEEN S-18L AND S-19L THERE ARE 12EA EXISTING FASTENERS COMMON TO PLATE PN 657N3251-2. IT SHOULD HAVE 14 IAW DWG, CALLOUT REPAISDR FDEA201007222645Floorbeam · damagedDURING INSTALLATION OF FLOOR PANELS PN 11861180-1 AND FLOOR PANEL 11861182-15 WAS MISSED DRILLED INTO FLOORBEAM AT STA. 365.25 RBL 13.95 AND LBL 6.80 ON MOD FLOOR PANEL INSTL-SECTION. REMOVED AND REPAIRED FLOORBEAM STA 365.25 RBL 50 TO LBL 15 IAW SRM 53-00-SDR FDEA201007202629Stringer · damagedUPON REMOVAL OF THE OHME FROM THE SURROUND STRUCTURE FOUND A DOUBLE DRILL HOLE CONDITION COMMON TO THE SKIN AND STRINGER AT STA 480 S-8R. REPAIR WAS ACCOMPLISHED ON E.A. 757-5331-16-F2767 REV- DATED 07/12/10. 8130-3.SDR FDEA201007022319Skin · corrodedAFT PIT CARGO DOOR INBD SURFACE CORRODED, REMOVED CORROSION IAW SRM 51-10-02 BLENDED AREA L=15" W=2.0 D=.015 ORIGINAL, MATERIAL .045 REMAINING .030 OUT OF LIMITS IAW SRM 53-30-01 FIG 101, DET. V. REMOVED INNER SKIN IAW SRM 51-40-02. RECEIVED NEW INNER SKIN ONSDR FDEA201006212095Seat Track · misalignedAT STA 660 AND 780, RBL 24.75 AND 45.5 THERE IS A MISSMATCH ON SEAT TRACK CROWN HEIGHT THAT WILL PREVENT THE CARGO HANDLING SYS FROM SITTING LEVEL. FOR TRACKING PURPOSE ONLY COMPLIED WITH EA 757-5335-16-F2656 DUE TO DISCREPANCY EFFECTING THE PTF MOD REPAIR WASDR FDEA201006172044Floor Support · corrodedCABIN FLOOR RT SUPPORT ANGLE HAS CORROSION SPOTS- FS-730-820,STR-17R, UNDER CLIP NUTS. REMOVED CORROSION FROM INBD CREASE BEAM CHORD STA 730-820 RT SIDE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13 FIG 101 DETAIL VIII. ORIG MATERIAL 0.70 AFTESDR FDEA201006111958Plate · corrodedMAIN DECK WEB PLATE CORRODED AT STA 1681 TO 1720, RBL 60 TO LBL60. REMOVED CORROSION ON AFT DECK PLATE STA 1681-1720, RBL60-LBL60 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL III. ORIG MATERIAL .071 AFTER REWORK .051 L=60" W=SDR FDEA201006101940Strap · corrodedLT HORZ STAB LOWER AFT PIVOT FITTING STRAP HAS CORROSION. REMOVED CORROSION FROM FITTING IAW SRM 51-10-02. OUT OF LIMITS IAW SRM 55-10-01 FIG 101 DET II. ACCOMPLISHED EA F-5510-141151, SPLICE PLATE PN 182N1608-5. MAJOR REPAIR.SDR FDEA201006091872Support Angle · corrodedMAIN DECK FLOOR SHEAR WEB SUPPORT ANGLE, RBL 64.5 BETWEEN STA 1180-1290 HAS AREAS OF CORROSION. REMOVED CORROSION FROM RT SIDE IB CREASE BEAM CHORD AT STA 1180-1290 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL II. ORIG MATERISDR FDEA201006021765Stringer · crackedSTR-15R AT STA 580 IS GOUGED AT COVE RADIAS. REPAIRED STRINGER STA 580 STR. 15R IAW SRM 53-00-03 FIG 201 REPAIR NR 2. MAJOR REPAIRSDR FDEA201006021777Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 617.30. REMOVED CORROSION FROM COVE PANEL IAW 51-10-02. BLENDED AREA L= 39", W=1.0", D=.011, MAT .050 REMAINING .039 OUT OF LIMITS IAW SRM 57-43-01, FIG 101, DET VI. FABRICATED COVE PANEL ON TRAVELER NR T10/83SDR FDEA201006021776Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 605.3. REMOVED CORROSION FROM COVE PANEL IAW SRM 51-10-02. BLENDED AREA L=3.5" W=1.0" D=.011, ORIG. MAT .050 REMAINING .039" OUT OF LIMITS IAW 57-43-01 DET VI. FABRICATED COVE PANEL ON TRAVELER NR T10/837838. MINOSDR FDEA201006021775Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 574.80. REMOVED CORROSION FROM COVE PANEL IAW SRM 51-10-02. BLENDED AREA L=24" W= 1.0" D=.010". ORIG. MAT. .050 REMAINING .040 OUT OF LIMITS IAW SRM 57-43-01 FIG 101 DET VII. FABRICATED COVE PANEL ON TRAVELER NR SDR FDEA201006021774Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 677.5. REMOVED CORROSION FROM COVE PANEL IAW SRM 51-10-02. BLENDED AREA L=24.0" W=1.0" D=.009. ORIGINAL MAT. .050 REMAINING .O41 OUT OF LIMITS IAW SRM 57-43-01 FIG. DET VI. FABRICATED COVE PANEL ON TRAVELER NR TSDR FDEA201006021773Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 665.5. REMOVED CORROSION FROM COVE PNL IAW SRM 51-10-02. BLEND OUTDIM=3.0" LX 1,0"W X .010" D, ORIGINAL MAT'L. THICK .050, MAT'L AFTER REWORK .04" FOUND OUT OF LIMITS IAW. SRM 57-43-01 FIG. 101 DET. VI. FABRICSDR FDEA201006021770Angle · corrodedLT WING SLAT NR 2 LOWER EDGE HAS CORROSION UNDER THE SEALANT AND INTERNAL FROM OTBD EDGE TO INBD END. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=130" W=.75" D=.012" ORIG, MAT. .063 REMAINING .051 OUT OF LIMITS IAW SRM 57-43-02 FIG 101 DET II. R & R NSDR FDEA201005291732Shear Web · corrodedMAIN DECK SHEAR WEB HAS CORROSION UNDERNEATH AT STA. 660, LBL 64.5. REMOVED CORROSION ON LT SIDE CREASE BEAM WEB STA 660-680 IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV. ORIG MATERIAL .071 AFTER REWORK .050 L=20 W=1.5. REMOVED ASDR FDEA201005281694Seat Track · crackedMAIN DECK SEAT TRACK CRACK AT STA 680, LBL 45 FABRICATED SEAT TRACK STA 440 TO 680 LBL 45 FROM BAC1520-7927178 T6 511 EXTR BATCH NR 1833789 IAW SRM 53-30-52, TREATED AND PRIMED IAW SRM 51-20-01, LOCATED AND DRILL IAW SRM 51-40-05. MAJOR REPAIRSDR FDEA201005271686Skin · gougedSKIN FOUND GOUGED AT LAP SEAM FWD OF STA 1300 S-20R. GOUGE FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DET IV. ACCOMPLISHED EA F 5330-131194.SDR FDEA201005271685Skin · corrodedNR 7 SLAT NOSE SKIN HAS DEEP PITTED AREAS AND IS CORRODED AT WS 369.50 TO 425.50. BLENDED CORROSION IAW SRM 51-10-02, REWORKED AREA DIMENSIONS = 35.0"L X 1.0"W X .019"D, ORIGINAL MAT'L THICKNESS .063", MAT'L AFTER REWORK .044", FOUND OUT OF LIMITS IAW SRMSDR FDEA201005271684Angle · corrodedRT WING SLAT NR 7 T/E HAS SEALANT CRACKED. REMOVED CRACKED SEALANT & FOUND CORROSION, REMOVED CORROSION, IAW SRM 51-10-02. REWORKED AREA = 12.0"L X 1.0"W X .023"D, ORIGINAL MAT'L .063" MAT'L AFTER REWORK .04", FOUND OUT OF LIMITS IAW SRM 57-43-02, FIG 101SDR FDEA201005261660Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER CAP CORRODED AT STA 324 RBL 30 TO RBL 58. ACCOMPLISHED EA F-5310-139154, PART 2 TO BE ACCOMPLISHED NO LATER THAN 37,500 TFC, PART 3 TO BE ACCOMPLISHED EVERY 12,000 FC AFTER PART 2. MAJOR REPAIR.SDR FDEA201005221616Crease Beam · corrodedMAIN DECK CREASE BEAM HAS CORROSION UNDERNEATH AROUND THE NUTPLATES HOLES, FROM STA 365 TO 418, RBL 60. REMOVED CORROSION FROM RT SIDE IB CREASE BEAM CHORD STA 365-418 RBL 60 IAW SRM 51-10-02. FOUND TO BE WITHIN LIMITS IAW SRM 53-30-15, FIG 101, DETAIL VIII. SDR FDEA201005211603Crease Beam · corrodedL-2 DOOR INBD CREASE BEAM CORRODED AT STA 712, LBL64. REMOVED CORROSION FROM LT SIDE IB CREASE BEAM CHORD STA 605-735. IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15 FIG 101 DETAIL V. ORIG MAT. .080 AFTER REWORK .065. L=30 W=1.0. REMOVED AND SDR FDEA201005201588Shear Web · corrodedMAIN DECK LT SHEAR WEB STA 180-1291 SUPPORT ANGLE AT LBL 64.5 HAS 2 AREAS OF CORROSION AT STA 1280 AND 1186. REMOVED CORROSION FROM LT SIDE INBD CREASE BEAM CHORD STA 1180-1291 IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 FIG 101 DETAIL III.SDR FDEA201005201587Crease Beam · corrodedR-3 DOOR LOWER SILL CREASE BEAM CORRODED AT STA 1320 TO 1360, RBL 60. REMOVED CORROSION ON CREASE BEAM CHORD STA 1320-1360 RLB 60 IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-60-13 FIG 101 DETAIL II. ORIG MATERIAL .071 AFTER REWORK .053 L=.072 W= .053. SDR FDEA201005191580Nut Plate · corrodedAFT UPPER BODY BULKHEAD STA 1787.4 INT/AFT SIDED BETWEEN S-4R TO S-6R HAS SEVERAL NUTPLATES RUSTY. REMOVED CORROSION ON STRAP AT STA 1787.4 S-4R TO S-6R IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-80-01, FIG 101 DETAIL III. ORIG MATERIAL .100 AFTESDR FDEA201005181572Seat Track · corrodedSEAT TRACK FLANGE HAS CORROSION BETWEEN STA 700-740, LBL 45.5. REMOVED CORROSION FROM SEAT TRACK IAW SRM 51-10-02. BLENDED AREA L= 20.0" W=1.0" D=0.035". ORIG. MAT. 0.070 REMAINING 0.045". OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DET I. R & R SEAT TRACK STA 6SDR FDEA201005181567Web · corrodedMAIN DECK RT FLOOR SHEAR WEB BETWEEN STA 1300-1320 HAS CORROSION ON BOTH SURFACES. REMOVED CORROSION IAW SRM 51010-02. BLENDED AREA ORIG MAT .040 MAT LOSS .009 L= 1.112 W=2.105 D= .009 FOUND TO BE OUT OF LIMIT IAW SRM 53-60- 13
FIG 101, DETAIL II. LOCATSDR FDEA201005181565Floorbeam · corrodedNEEDS TO REPLACE STA 1640, FLOORBEAM DUE TO EXISTING REPAIR. R & R 1640 FLOORBEAM IAW SRM 51-40-02, LBL63-RBL63. MAJOR REPAIR.SDR FDEA201005171554Web · corrodedMAIN DECK RT FLOOR SHEAR WEB BETWEEN STA 1360-1380 HAS SURFACE CORROSION. REMOVED CORROSION ON WEB AT STA 1360-1380 RT SIDE CREASE BEAM IAW SRM 51-40-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13 FIG 101, DETAIL II. ORIG MAT .040 AFTER REWORK .021 L=2.07SDR FDEA201005141537Floorbeam · corrodedL-3 DOOR FLOORBEAM AT STA 1320 LBL60 CORRODED. REMOVED CORROSION ON FLOORBEAM AT STA 1320, LBL 60 IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL III. R & R FLOORBEAM AT STA 1320, LBL 34-60 IAW SRM 53-00-51, FIG 201, REPAIR 1. CLASSIF
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