N499MC
Service difficulty reports · 267
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 = 'N499MC' 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 = 'N499MC' 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 UIEA2011031500190Intercostal · crackedCRACK ON THE INTERCOSTAL OF BULK CARGO COMPARTMENT AT STA 2060, RBL 7.625. (REPAIR IAW EI NR. T2011A53B-685, REV 00.)SDR UIEA2011031500185Intercostal · crackedCRACK ON THE INTERCOSTAL OF BULK CARGO COMPARTMENT AT STATION 2040 RBL 38.525.(REPAIR IAW EI NO. T2011A53B-686 REV. 00.)SDR UIEA2011031400216Rib · crackedCRACK ON 65B23601-5 RIB OF LT HST L/E FAIRING LWR SIDE AT STA 145.01.0. (REPAIR IAW T2011A55B-61.4, REV 00; 01)SDR UIEA2011031400208Structure · crackedCRACK ON THE CHORD OF LT WING FIXED T/E LOWER SUPPORT STRUCTURE AT WS 1185.40. (REPAIR IAW NR T2011A57B-615, REV 00 AND REV 01)SDR UIEA2011031400196Frame · crackedCRACK ON AFT FRAME OF NR 1 ENGINE LT CORE COWL. (REPAIR IAW NR. T2011A71B-675, REV. 00.)SDR UIEA2011031400184Access Panel · worn1 FASTENER HOLE WORN OUT ON NR 3 STRUT. ENG-TO-WING FAIRING ACCESS PANEL 472 EL. (REPAIR IAW E NR T2011A54B-563, REV 00 AND REV. 01.)SDR UIEA2011031000227Rib · crackedCRACK ON 65B23601-7 RIB OF LT HST L/E FAIRING LOWER SIDE AT 151.543. (REPAIR IAW NR T2011A55B-621 REV. 00 AND REV. 01.)SDR UIEA2011031000226Rib · crackedCRACK ON 65B23601-5 RIB OF LT HST L/E FAIRING LOWER SIDE AT STA 145.011. (REPAIR IAW NR T2011A55B-620, REV 00 AND REV. 01.)SDR UIEA2011031000225Rib · crackedCRACK ON 65B23604-25 RIB OF LT HST L/E FARING LWR SIDE AT STA518.646. (REPAIR IAW T2011A55B-617, REV 00; 01).SDR UIEA2011031000224Rib · crackedCRACK ON 65B23604-23 RIB OF LT HST L/E FAIRING UPPER SIDE AT STA 510.103 (REPAIR IAW T2011A55B-616, REV 00; 01)SDR UIEA2011031000223Rib · crackedCRACK ON 65B23604-29 RIB OF LT HST L/E FAIRING UPPER SIDE AT STATION 535.734. (REPAIR IAW T2011A55B-619, REV 00 AND REV 01.)SDR UIEA2011031000222Rib · crackedCRACK ON 65B23604-21, RIB OF RT HST L/E FARING LWR SIDE AT STA 501.359 (REPAIR IAW T2011A55B-614, REV 00; 01)SDR UIEA2011031000220Rib · crackedCRACK ON 65B23604-7, RIB OF LT HST L/E FARING LWR SIDE AT STA 441.753. (REPAIR IAW T2011A55B-613, REV 00; 01)SDR UIEA2011031000219Rib · crackedCRACK ON 65B23601-9 RIB OF LT HST L/E FARING LWR SIDE AT STA 159.109. (REPAIR IAW T2011A55B-612, REV 00; 01)SDR UIEA2011031000217Rib · crackedCRACK ON 65B23601-7 RIB OF LT HST L/E FARING LWR SIDE AT STA 151.543. (REPAIR IAW T2011A55B-611, REV 00; 01)SDR UIEA2011031000186Rib · crackedCRACK ON 65B23604-27 RIB OF LT GST L/E FAIRING UPPER SIDE AT 51A 527.190. (REPAIR - IAW EI T2011A55B-618 REV 00, AMP; REV 01)SDR UIEA2011030900236Skin · dentedFOUND EXTERNAL SKIN HAD DENT AT AFT CARGO DOOR; AFT & AMP; LWR SIDE. STA 1914 TO STA 1918 (REPAIR - IAW EI T2011A52B-565, REV 00 & AMP; REV 01)SDR UIEA2011030900215Rib · crackedCRACK ON 65B23604-26 RIB OF RT HST L/E FARING LWR SIDE AT STA ;527.190 (REPAIR IAW T2011A55B-608, REV 00; 01)SDR UIEA2011030900214Rib · crackedCRACK ON 65B23604-26, RIB OF RT HST L/E FAIRING LWR SIDE AT STA 518.646. (REPAIR IAW T2011A55B-608 REV 00; 01)SDR UIEA2011030900213Rib · crackedCRACK ON 65B23604-24 RIB OF RT HST L/E FAIRING LWR SIDE AT 510.103. (REPAIR IAW T2011A55B607, REV 00; 01)SDR UIEA2011030900212Rib · crackedCRACK - CRACK ON 65B23604-22 RIB OF RT HST L/E FAIRING LWR SIDE AT STA 501.559. (REPAIR IAW T2011A55B-605, REV 00; 01)SDR UIEA2011030900204Rib · crackedCRACK - CRACK ON 65B23604-14 RIB OF RT HST L/E FAIRING LWR SIDE AT STA 467.384. (REPAIR IAW T2011A55B-604, REV 00; 01)SDR UIEA2011030900200Rib · crackedCRACK ON 65B23604-12 RIB OF RT HST L/E FAIRING LWR SIDE AT STA 458.841. (REPAIR IAW T2011A55B-603, REV 00 ; 01)SDR UIEA2011030900198Rib · crackedCRACK ON 65B23604-10 RIB OF RT HST L/E FAIRING LWR SIDE AT STA 450.297. (REPAIR IAW T2011A55B-602, REV 00; 01)SDR UIEA2011030900197Rib · crackedCRACK ON 65B23604-8 RIB OF RT HST 4E FAIRING LWR SIDE AT STA 441.753. (REPAIR - IAW T2011A55B-601, REV 00 ; 01)SDR UIEA2011030900189Skin · dentedFOUND BULK CARGO DOOR OUTER SKIN HAD DENT AT STA 1994 L X W X D = 1" X 0.6" X 0.031" (REPAIR - IAW SRM 52-00-01-2R-9, REV 58.)SDR UIEA2011030900182Skin · crackedCRACK ON THE FOLDING NOSE SKIN OF LT WING NR 10 VC FLAP OTBD EDGE AT ILES 779.50.SDR UIEA2011030900153Skin · dentedDENT - FWD BULK CARGO DOOR OUTER SKIN HAD DENT AT STA 1994 L-1", W-0.6", D-0.031". (IN PROCESS).SDR UIEA2011030900152Skin · dentedDENT- FWD EXTERNAL SKIN HAD A DENT AT AFT AND LOWER SIDE, STA 1917 TO 1918 (IN PROCESS).SDR UIEA2011030800235Skin · dentedFOUND EXTERNAL SKIN HAD DENT AT AFT CARGO DOOR FWD; LWR SIDE, STA 1812 TO STA 1815. (REPAIR - IAW EI T2011A52B-564, REV 00 ; REV 01)SDR UIEA2011030800187Skin · dentedFOUND EXTERNAL SKIN DENTED AT FWD CGO DOOR AFT; LWR STA 670. (REPAIR IAW SRM 52-30-01-2R-2, REV 58).SDR UIEA2011030800147Skin · dentedFWD EXTERNAL SKIN DENTED AT FWD CARGO DOOR AFT AND LOWER SIDE STA 670. REPAIRED FWD CARGO DOOR SKIN IAW SRM 52-30-01 REPAIR 2 FIGURE 201 SHEET 10 REV 58.SDR UIEA2011030800146Skin · dentedDENT FWD EXTERNAL SKIN HAD DENT AT AFT CGO DOOR FWD AND LOWER SIDE. STA 1812 TO STA 1815 (OPEN)SDR UIEA2011030800148Slide · no testDURING U/D SERVICE DOOR SLIDE DEPLOYMENT TEST FOUND SLIDE AUTOMATIC AND MANUAL DEPLOY FUNCITONAL FAIL. (OPEN)SDR UIEA2011030700192Structure · chafedCHAFING DAMAGE ON THE NR 1 ENG NACELLE STRUT INBD AFT SIDE OF FR ACCESS DOOR ASSY. (REPAIR IAW EI T2011A54B-536, REV 00)SDR UIEA2010120500186Winglet · damagedDURING TAXI, ENROUTE FOR TAKEOFF. ACFT CAME IN CONTACT WITH ANOTHER ACFT ON THE TAXI WAY. THE WINGLET WAS DAMAGED. (REMOVED WINGLET AND DISPATCHED IAW CDL 57-28-1).SDR UIEA201000236Skin · damagedDURING WALK-AROUND , MX FOUND DAMAGE TO THE RT WING OTBD FORE AND AFT FLAPS (REF FIG 1-3).DIMENSIONS AND DETAILS: RT OTBD FORE FLAP WBL793 - L/E PUNCTURE - 2.250 IN. X 2.0 IN. (REF FIG 1). RT OTBD FORE FLAP WBL810 - L/E PUNCTURE - 5.0 IN. X 2.5 IN. (REF FIG 2)SDR UIEA201000231Cam · crackedDURING A-CHECK AND INSP IAW EO 4452A068, WEAR WAS FOUND IN THE MAIN DECK SIDE CARGO DOOR MIDSPAN LATCH CAM THAT IS OUTSIDE OF WEAR LIMITS IAW THE AMM 52-32-01-206. FWD MID SPAN LATCH CAM ID= 1.1740 , ALLOWED WEAR LIMITS IAW AMM IS 1.1240 (0.05). AFT MID SPAN SDR UIEA2010092800167Panel · damagedEO 4425A197; DURING MX WALKAROUND, MX FOUND THE MAIN DECK - RT BS1250, WL 248 SIDEWALL PANEL DAMAGED; HOLE 2.5 IN. LONG X 1.5 IN. WIDE. (IAW AMM 25-52-01-308-062, THE DAMAGE/HOLE IS OUT OF LIMITS. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCSDR UIEA2010090100154Skin · damagedEO 4452A084 DURING WALKAROUND INSP, MX FOUND THE CARGO DOOR OUTER SKIN WITH DENT/SCRATCH DAMAGE, MEASURES: 2.0 IN LONG X 1.5 IN WIDE X 0.125 IN DEEP. THE DENT IS OUT OF LIMITS IAW THE SRM 52-30-01, FIG 101, DETAIL XI, ALLOWABLE DAMAGE 1. THE BULK CARGO DOOR OSDR UIEA201000031Tire · separatedON WALKAROUND FOUND NR 4 TIRE RECAP SEPARATED FROM TIRE. PERFORMED AIRCRAFT INSPECTION PER CHAP 5-51-34-201. REPLACED TIRE PER AMM 34-45-01. AIRCRAFT INSPECTION REVEALED SEVERAL DENTS TO LEFT I/B LOWER SURFACES OF FORE, MID AND AFT FLAPS AND TRAILING EDGE PSDR UIEA201000025Support · crackedLT WING LOWER SURFACE ADJACENT TO NR 5 SPOILER OTBD AREA UPPER SURFACE FIXED PANEL SUPPORT STRUCTURE CRACKED. UPPER SURFACE SUPPORT FITTING REPLACED IAW SRM 51-10-02, 51-40-02 AND AMM 57-22-01.SDR UIEA201000024Fitting · crackedLT WING INBD MIS FLAP TRACK CARRIAGE FITTING SAFE LINK ATTACH BOLT BORE HOLE CRACKED. LT WING INBD MID FLAP REPLACED IAW 27-51-01.SDR UIEA201000023Angle · crackedRT OTBD ELEVATOR L/E INBD BALANCE WEIGHT BOX ANGLE CRACKED. ELEVATOR STA 227.65 SUPPORT WEB AND WEB ANGLE REPLACED IAW SRM 51-10-02 AND INSTALLED IAW 51-40-02.SDR UIEA201000022Rib · crackedLT INBD ELEVATOR L/E MOST INBD RIB ANGLE CRACKED. INBD RIB UPPER MOST UPPER RIB ANGLE BRACKET REPLACED IAW SRM 51-00-02 AND 51-40-02.SDR UIEA201000178Conduit · damagedFLEXIBLE ELECTRICAL CONDUIT AT THE LT WING GEAR DAMAGED. "PERFORMED A TIME LIMITED REPAIR IAW THE SWPM 20-10-91".SDR UIEA200900022Support Fitting · failedDENT ON OUTBOARD AFT FLAP NOSE AND MID FLAP DUE TO OUTBOARD FLAP FITTING FAILURE. REPAIRED PER SRM 51-70-17. REPLACED SUPPORT ARM.SDR UIE2008F00011Frame · crackedMAIN DECK CARGO COMPARTMENT RT AFT SIDEWALL CRACKS FOUND ON FRAME INNER FLANGE AT STA 1740 AND 1780. JUST ABOVE FRAME SPLICE AT BETWEEN STRINGER 11R AND 12R. REPAIRED IAW EO 4463A178. (K)SDR UIE2008F00014Wire · chafedDURING CRUISE, EICAS ADVISORY "HYD PRESS ENGINE 1" ON HYD SYNOPTIC. NR EDP AND DEMAND PUMPS RUNNING. THEN NOTED EDP INTERMITTENT AND IAW CHECKLIST EDP SWITCH OFF, BUT PUMP DID NOT SWITCH OFF. (EDP CONTINUED RUNNING INTERMITTENTLY AND DEMAND PUMP RUNNING). LASDR UIEA200800171Duct · damagedAFTER TAKEOFF UNABLE TO PRESSURIZE AIRCRAFT. FOUND CONDITIONED AIR CHECK VALVE CRACKED AND FOUND HOLE ON FORWARD CARGO COMPARTMENT AIR SUPPLY DUCT. REMOVED AND REPLACED CHECK VALVE AND ACCOMPLISHED LEAK CHECK IAW 21-28-08. AIR DUCT REMOVED AND FORWARDED FOR
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