N910FD
Service difficulty reports · 98
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 = 'N910FD' 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 = 'N910FD' 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 FDEA201507152226Indicator · stiffAFTER BLOCK IN AT GATE, LT MAIN ENTRY DOOR MECHANICAL SLIDE ARMED INDICATOR REMAINED STUCK OUT IN THE ARMED POSITION. AFTER DOOR ARMING HANDLE WAS MOVED TO THE DIS-ARMED POSITION. WHILE SLIDE ANNUNCIATOR LIGHT ABOVE DOOR EXTINGUISHED NORMALLY. MECHANICAL INSDR FDEA201505141508Girt Bar · malfunctionedDURING DISARM OF LT ENTRY DOOR, ARM LEVER BINDS AT MID-POINT, KNUCKLE BUSTER, DID NOT RETRACT. REARMED DOOR & THEN DISARMED AGAIN WITH HEAVY EFFORT. STILL FELT BINDING AT MID-POINT BUT DOOR DISARMED. DURING VISUAL INSPECTION OF THE L-1 ENTRY DOOR FOUND THE SDR FDEA201410012881Skin · dentedRIGHT SIDE OF FUSELAGE SKIN HAS A DENT AT BS 1709 BETWEEN STRINGERS 14 - 16R. REPAIRED IAW EA F-5330-T0311997 PT1.SDR FDEA201409262806Skin · dentedDENT ON FUSELAGE SKIN AT BS 1610 BETWEEN STRINGERS 17 & 18L. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 REPAIR 16.SDR FDEA201306031178Bulb · looseLT ENTRY DOOR EMERGENCY LIGHT DID NOT COME ON DURING TEST. ADJUSTED BULB IN SOCKET. PERFORMED OPS CHECK OF L1 SLIDE LIGHT IAW AMM 33-51-06-2-1. OPS NORMAL. ACFT IS OK FOR SVC.SDR FDEA201210153618Skin · damagedSCRIBE LINE AT S14L BS 1578 TO 1597. ACCOMPLISHED REPAIR IAW EA NR F-3330-123972.SDR FDEA201210103593Skin · damagedSCRIBE LINE AT S20R BS 1675.9 TO 1684.3. ACCOMPLISHED REPAIR OF SCRIBE LINE AT STR 20R, STA 1675.9-1684.3 IAW EA NR F-5330-123972, REV B.SDR FDEA201209263461Seat Track · corrodedSEAT TRACK CORRODED, COURIER AREA BS 345. REMOVED AND REPLACED DAMAGED SEAT TRACK IAW SRM 51-40-05 AND 51-40-02.SDR FDEA201204281666Crank Assy · brokenREMOVED L1 SLIDE AND STARTED TO INSTALL NEW SLIDE IAW AMM 25-66-01-4-0 AND FOUND ARMING LINKAGE FOR GIRT BAR BROKEN . INSTALLED CRANK ASSY. IAW SMP TESTED DOOR MECHANISM IAW AMM 25-11-20-5-0. INSTALLED SLIDE IAW MM REF 25-66-01-4-0. PERFORMED GIRT BAR INSPSDR FDEA201204171459Cover · looseR1 DOOR SLIDE COVER LOOSE. SECURED SLIDE COVER IAW 52-11-02-4-0.SDR FDEA201110104413Battery Pack · dischargedEMERGENCY EXIT LIGHTS WILL NOT TEST. R & R R1 EMERGENCY EXIT BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED NORMAL. PREMATURE REMOVAL/INSTALLATION.SDR FDEA201109244103Transmitter · failedLEFT ENGINE OIL TEMP ROSE TO 200 DEGREES THEN WENT BLANK. CAME BACK ON WITH INDICATIONS NORMAL AND OUT OF LIMITS, FLUCTUATION FOR REST OF FLIGHT. RETURN TO DEPARTURE. INDICATIONS STARTED FL180 IN THE CLIMB. DURING POSTFLT DISCOVERED EICAS DISAGREE STATUS MSDR FDEA201107262945Pressure Switch · inoperativeDURING TAKEOFF, GOT LT OIL FILTER EICAS AT 80 KTS. DURING TAXI BACK, DID NOT HAVE ANY OTHER INDICATIONS. EICAS MESSAGE STAYED ON THROUGH SHUTDOWN. REPEAT. FOUND INOP LT ENG SCAVENGER OIL FILTER DIFFERENTIAL PRESSURE SWITCH, R & R IAW MM 79-35-02-4 AND TESTSDR FDEA201104271648Girt Bar · dirtyR1 DOOR SLIDE ARMED LIGHT WILL NOT ILLUMINATE WHEN DOOR ARMED. CLEANED GIRT BAR POSITION. ARM LIGHT OPERATES NORMALLY IAW AMM 25-66-01-6-0. FINAL CLOSED.SDR FDEA201011234483Skin · dentedC-1 DOOR AFT EDGE OF CUTOUT IS DENTED AT STA 620, STR 22R. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED ALL REPAIR PARTS IAW EA F-5330-123572.SDR FDEA200909303445Windshield · failedCAPTS WINDSHIELD OUTER PANE SHATTERED. REMOVED CAPT'S WINDSHIELD REF AMM 56-11-01-4. INSTALLED WINDSHIELD REF AMM 56-11-01-4 THRU STEP 12B. COMPLETED 1ST TORQUE SEQ AT 1800Z. PREMATURE REMOVAL/INSTALLATION. REMOVED AND REPLACED CAPT'S WINDSHIELD/ F/O'S SLSDR FDEA200906192182Seat Track · misalignedSEVERAL HANDLING SYS, ROLLERS DO NOT SET RIGHT IN THE EXISTING STEELE SEAT TRACKS FROM STA 408.8 TO STA 800, LBL 45 TO RBL 45, CLEANED TRACKS AND VERIFIED DWG TOLERNCES SITTING LEVEL, REMOVED HANDLING SYS. IN AFFECTED AREA IAW SRM 51-40-02 REMOVED FLOOR PANSDR FDEA200904021161Flange · corrodedAFT FUSELAGE CUTOUT FOR APU INTAKE DOOR HOUSING FLANGES ARE CORRODED. REMOVED CORROSION IAW SRM 51-10- 02. OUT OF LIMITS PER SRM 53-80-05, FIG 101, DETAIL 5 AND SRM 53-80-01, FIG 101, DETAIL 3. FABRICATED UPPER FLANGE ON MAE TRAVELER NR T9/782221, LWR FLANSDR FDEA200903261072Skin · dentedFUSELAGE SKIN, BS 1356, BETWEEN S-24L AND S-25L, IS DENTED. CHECKED LIMITS OF DENT AT BS 1356, BETWEEN S-24L AND S-25L, A=.942, Y=.045, A/Y=21. OUT OF LIMITS PER SRM 53-00-01, FIG 201. FABRICATED REPAIR DOUBLER FROM .063"/2024-T3, BATCH NR 158579, IAW SRM 5SDR FDEA200903220997Skin · dentedDENT AT FUSE EXT UPPER SURFACE APPROX STA 1542, S2R. COMPLIED WITH EA 757-5361-16-F1907, REV A AT FUSE STA 1542, S2R. THIS IS A CATEGORY A REPAIR. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR.SDR FDEA200903160932Crease Beam · corrodedMAIN CARGO DECK, BS 685, RT (RBL 58), CREASE BEAM ANGLE IS CORRODED. REMOVED CORROSION IN INBD CREASE BEAM CHORD, RBL 58, IAW SRM 53-30-13, PAGE 102, DETAIL 8. ORIGINAL MATERIAL THICKNESS WAS .080 INCH, AFTER REWORK IS L=4.0 INCH, W=1.0 INCH, D=.050 INCH. SDR FDEA200902270761Frame · corrodedFRAME BS 1701, S-5/6 LT, SPLICE AREA IS CORRODED. REMOVED CORROSION AT FRAME BS 1701, S-5/6 LT, IAW SRM 53-00-07. FOUND CORROSION REWORK TO BE OUT OF LIMITS PER SRM 53-00-07, FIG 101, DETAIL 2 L=3", W=2", D=.010", MATERIAL REMAINING .070". FABRICATED REPLACSDR FDEA200902260739Seat Track · crackedSEAT TRACK 144N5021-2 AT BS 1080-1180, RBL 45.50, CRACKED AT FASTENER HOLE. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK ON MAE TRAVELER NR T9/777784. LOCATED, DRILLED NEW SEAT TRACK IAW SRM 51-40-05. TREATED AND PRIMED NEW SEAT TSDR FDEA200902250719Intercostal · crackedBS 325-345, BL 0, INTERCOSTAL WEB IS CRACKED. REMOVED CRACKED INTERCOSTAL WEB AT BS 325-345, BL 0, PER SRM 51-40-05. RECEIVED NEW WEB ON MAE TRAVELER NR T9/781257, LOCATED, DRILLED PER SRM 51-40-05. INSTALLED REPLACEMENT INTERCOSTAL WEB PER SRM 51-40-05 AT SDR FDEA200902230665Frame · damagedBS 377, S-3R, HAS EXISTING FASTENER HOLES WITH SHORT ED. CUT OUT DAMAGED SECTION OD BS 377 FRAME, S-3R-2L, IAW SRM 53-0-07, FIG 101, REPAIR NR 3. RECEIVED REPAIR FRAME ON MAE TRAVELER NR T9/781551. LOCATED AND DRILLED FRAME, REPAIR SPLICES AND REPAIR ANGLSDR FDEA200902170566Support · corrodedCORRODED SUPPORT WEB ALONG STRINGER S-17L, AT BS 1513, BS 1573 AND BS 1593. REMOVED AND REPLACED TRUSS FITTING AT BS 1500-1520, LBL 65, PER MAE TRAVELER NR T8/776173 AND SRM 51-40-02. CORROSION REMOVAL WAS FOUND TO BE OUT OF LIMITS PER SRM 53-60-13, FIG 101 SDR FDEA200902170565Crease Beam · corrodedCABIN FLOOR SUPPORT AT BS 665-750 HAS SURFACE CORROSION. REMOVED TO BE OUT OF LIMITS AT BS 665-750, LBL 64 PER SRM 51-40-02/51-40-05. CORROSION REWORK DIMENSIONS ARE AS FOLLOWS: L=7 INCH, W=2 INCH, D=.040 INCH. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJORSDR FDEA200902140520Floor Panel · corrodedFLOOR METAL PLATE FROM STA 1681- 1720, HAS CORROSION. REMOVED CORROSION IAW SRM 53-60-51. FABRICATED REPAIR DOUBLERS IAW SRM 53-60-51. INSTALLED REPAIR DOUBLERS IAW SRM 53-60-51, FIG R01, MAJOR REPAIR NR 2 CATEGORY A.SDR FDEA200902140519Skin · corrodedFUSELAGE EXT SKIN CORROSION JUST FWD OF APU DOOR CUT OUT, STA 1885, BL-0. REMOVED AND REPLACED SKIN STRAP IAW SRM 51-40-02. FABRICATED STRAP IAW SRM 51-30-01, CATEGORY A, MAJOR REPAIR.SDR FDEA200902140518Frame · damagedCABIN SECTION 46, FRAME STA 1020, BETWEEN S8R - 9R , 3 MISSED DRILLS. REMOVED DAMAGE IAW SRM 53-00-07. FABRICATED NEW FRAME. INSTALLED REPAIR PARTS IAW SRM 53-00-07, CATEGORY A, MAJOR REPAIR.SDR FDEA200902140517Floorbeam · corrodedSTA 345 FLOORBEAM HAS CORROSION BL 0-24L, ON EXISTING REPAIR. REMOVED AND REPLACED TCAP REPAIR IAW SRM 53-00- 51. FABRICATED ANGLES AND STRAPS IAW SRM 53-00-51.SDR FDEA200902100501Web · corrodedCORREDED LOWER SURFACE OF SUPPORT WEB ALONG RT EMERGENCY EXIT DOOR LOWER SILL AREA. REMOVED CORROSION IAW SRM 51-10-02 ON RT EMER EXIT DOOR LWR SILL, BLENDED AREA L=10.0" X W= 3.0" X D=0.020".ORIG MAT IS 0.063" MAT LOSS 0.048" AREA OUT OF LIMIT IAW SRM 5SDR FDEA200902090494Web · corrodedCORRODED SUPPORT WEB AT STA 1560-STA 1580 ALONG STR 17R, CABIN AREA. REMOVED CORROSION IAW SRM 51-10-02, BLENDED AREA FOUND TO BE OUT OF LIMIT, L=12.0', W=5.0" D=.038" AS PER SRM 53-60-13 FIG 101 DET II. INSTALLED REPAIR WEB STA 1560-1580 IAW SRM 51-40-02. SDR FDEA200902090493Crease Beam · corrodedCABIN FLOOR SUPPORT ANGLE AT STA 790-755 RBL 64 HAS SPOTS OF SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-02, BLENDED AREA L=3" BY W=1.2" D=.O20". ORIGINAL MAT .063 INCH, REMAINING .040 INCH, OUT OF LIMITS AS PER SRM 53-30-13, FIG 101, DET II. REPLACSDR FDEA200902090492Floor Support · corrodedMAIN DECK FLOOR SUPPORT CORRODED AT BS 345-365, LBL 60, L1 DOOR SILL. REMOVED CORROSION ON FLOOR SUPPORT IAW SRM 51-10-02 AT BS 345-365, LBL 60. REMOVED FLOOR SUPPORT IAW SRM 41-40-02. BLENDED AREA IS L=18.0", W=2.0", D=.015", OUT OF LIMITS PER SRM 53-00-51SDR FDEA200902090491Floor Support · corrodedMAIN DECK FLOOR SUPPORT CORRODED AT BS 333.45-345, LBL 64, L1 DOOR SILL. REMOVED CORROSION ON FLOOR SUPPORT IAW SRM 51-10-02, AT BS 333.45-345, LBL 64. REMOVED FLOOR SUPPORT IAW SRM 51-40-02. BLENDED AREA IS L=3.0", W=2.0", D=.012", OUT OF LIMITS PER SRM 53SDR FDEA200902050464Bracket · corrodedCORROSION AT STA 310.5 LBL 25 INTERCOSTAL BRACKET REMOVED CORROSION BY BLEND ON AN AREA IAW SRM 53-00-51. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIGURE 101 DETAIL 3. REMOVED, LOCATED, DRILLED AND INSTALLED NEW REPAIR SUPPORT FROM BATCH NR 0001586153 ATSDR FDEA200902030440Support Angle · corrodedCABIN FLOOR SUPPORT ANGLE, AT BS 700-720, RBL 64 HAVE SPOTS OF CORROSION. REMOVED CORROSION FROM SUPPORT ANGLE PER SRM 51-10-02. OUT OF LIMITS PER SRM 53-00-51, FIG 101, DETAIL 3. REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER SRM 53-00-51, 51-40-02. THIS RSDR FDEA200902030439Floor Support · corrodedMAIN DECK FLOOR INTERCOSTALS, CORRODED ALONG L1 DOOR LOWER SILL, FROM BS 333-377, . REMOVED CORROSION ON FLOOR SUPPORT IAW SRM 51-10-02. FLOOR SUPPORT FOUND OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. FABRICATED FLOOR SUPPORT. LOCATED, DRILLED, TRESDR FDEA200902030438Floorbeam · corrodedSTA 2681 FLOORBEAM TOP AND BOTTOM SURFACE ALONG ANCHOR NUTS AREA HAVE CORROSION. REPAIRED FLOORBEAM AT STA 1681 RBL-31 BOTTOM SURFACE IAW SRM 53-00-51 REPAIR NR 2. THIS IS MAJOR 'A' REPAIR NO FOLLOW-UP INSPECTION REQUIRED.SDR FDEA200901300406Sill · corrodedLT EMERGENCY DOOR, LOWER SILL, AT BS 1340, LOWER SURFACE IS CORRODED, AFT OF FLOORBEAM. REMOVED CORROSION ON LT EMERGENCY DOOR LOWER SILL WEB, BS 1340, LBL 60, PER SRM 51-10-02. CORROSION OUT OF LIMITS PER SRM 53-60-15, FIG 101, DETAIL 4. L=6.0", W=3.0", DSDR FDEA200901290395Crease Beam · corrodedCABIN FLOOR CREASE BEAM WEB SKIN CORRODED AT STA 740. REMOVED AND REPLACED CREASE BEAM WEB IAW SRM 53-30-15 AND 51-40-02. THIS IS A MAJOR 'A' REPAIR NO FOLLOW-UP INSPECTION REQUIRED.SDR FDEA200901290394Crease Beam · corrodedCORRODED TOP SURFACE OF ANGULAR SUPPORT FROM STA 1260-1280 RT SIDE FLOOR LEVEL. REMOVED AND REPLACED CREASE BEAM IAW SRM 51-40-05 FROM FSTA 1180-1290 RT RBL 65. THIS IS A MAJOR 'A' WITH NO FOLLOW-UP REQUIRED.SDR FDEA200901240315Crease Beam · corrodedCABIN FLOOR SUPPORT ANGLE AT BS 755-780 LBL64 CORRODED. CORROSION FOUND TO BE OUT OF LIMIT AS PER SRM 53-30-13 FIG 101 DETAIL VIII. REPLACED CREASE BEAM IAW SRM 51-40-02 AND SRM 53-50-13, CATEGORY "A" MAJOR REPAIR.SDR FDEA200901240314Frame Splice · corrodedFWD CARGO COMPT, RT FRAME SPLICE CORRODED AT FS 720, STR 26R. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS, ORIG MAT .071, REWORK .060, L=3.5, W=1.5, D=.011, OUT OF LIMITS IAW SRM 53--00-07 PAGE 103 FIG 101 DETAIL 2. FABRICATED ON MAE SPLICE PLATE TRAVSDR FDEA200901210297Floorbeam · corrodedSTA 377 FLOORBEAM HAS CORROSION, REMOVED CORROSION IAW SRM 53-00-51. FABRICATED NEW UPPER CHORD AND SPLICE ANGLES ON MAE TRAV NR T9/445482, AND T9/445483. INSTALLED REPAIR PARTS IAW SRM 53-00-51, STA 377, RBL 36- LBL 70, MAJOR REPAIR NR 3. CATEGORY B.SDR FDEA200901210294Doubler · dentedLOWER FUSE AT STA 710 RT HAS A DENT, L= 1.75, W= 1.0, D = 0.047. FABRICATED REPAIR DOUBLER IAW SRM 53-00-013. INSTALLED REPAIR DOUBLER IAW SRM 53-00-013. CATEGORY B MAJOR REPAIR NR 3 REPAIR..SDR FDEA200901210293Frame Splice · corrodedFWD CARGO COMPT, LT FRAME SPLICE CORROSION, STA 740, STR 26L. REMOVED AND REPLACED SPLICE PLATE STA 740, STR 26L IAW SRM 51- 40- 02. SPLICE FABRICATED ON MAE TRAV NR T9/ 777465 IAW SRM 51-40-05. CATEGORY A MAJOR REPAIR.
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