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 UIEA2017032700413Actuator · failedSTATUS MESSAGE 28649, FOR RIGHT CENTER WING JETTISON TRANSFER VALVE FAILED. REMOVED RIGHT CENTER WING TANK JETTISON TRANSFER VALVE ACTUATOR IAW AMM 28-31-04-004-001, REV 88. INSTALLED A NEW JETTISON TRANSFER VALVE ACTUATOR AT RIGHT CENTER WING TANK IAW ASDR UIEA2017032700414Pdu · failedFUNCTIONAL FAIL OF THE ALTERNATE ELECTRICAL LEADING EDGE SYSTEM. REPLACED WIRE W4747-307-188.18Y.18B AND PERFORMED WIRE CONTINUITY CHECK AND RESULT WAS SATISFACTORY IAW WDM 27-81-32, REV 44. REPLACED THE LT L3 PDU, AND PERFORMED INSTALLATION TEST, THE RESSDR UIEA2016111500841Stringer · damagedSTRINGER 12R AFT END SEVERED AT BS 2658. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-05 FIG 2 AND 53-80-03-01 FIG PG 3.SDR UIEA2016030700119Structure · crackedMAIN DECK L5 BS 2230, BETWEEN STRINGER 22 & 23, FWD CUT OUT FOUND CRACKED. REPAIRED IAW SRM 53-60-152R-3 REPAIR 3.SDR UIEA2016030700120Skin · chafedLEFT BLG INBD STRUT DOOR INNER SKIN FOUND CHAFING MARK. REPAIRED IAW RI 52-80-11263 REV A.SDR UIEA2016030700121Stop Fitting · corrodedMAIN DECK L5 DOOR FWD NR 4 STOP FTG FOUND CORRODED. L5 DOOR FWD NR 4 STOP FTG, PN 65 B08944-9, REPLACED IAW SRM 51-10-02 & FASTENERS INSTALLED IAW SRM 51-40-02.SDR UIEA2016030700122Skin · dentedSTATION 1700 & STRINGER 41L & SKIN DENT. STATION 1690 - 1710, STRINGER 39L - 42L, SKIN DENT AREAS REPAIRED IAW RRI 53 - 61 - 11264 REV A.SDR UIEA2016030700123Fitting · crackedLEFT BS 2598 FWD INNER CHORD, UPPER SPLICE FTG WAS ONE EACH HOLE CRACKED, APPROX 1/16". REPAIRED IAW R1-53-83-11266.SDR UIEA2016030700124Longeron Fitting · crackedLEFT BS 1480, LONGERON EXTENSION FTG FOUND CRACKED APPROX 3/8" IN LENGTH. REPAIRED IAW SB 747-53A-2860 R1 & EO 4453A818 PART 3.SDR UIEA2016030700125Longeron Fitting · crackedRIGHT BS 1480, LONGERON EXTENSION FTG FOUND CRACKED, APPROX 1/2" IN LENGTH. REPAIRED IAW EO 453A818 PART 4 & SB 747-53A 2860 R1.SDR UIEA2016030700126Bulkhead · crackedFS 48, STATION 2658, RBL 34-38, WL313, BULKHEAD WEB CRACKED. REPAIRED IAW R1-53-83-11265 REV A.SDR UIEA2016030700127Stiffener · crackedRIGHT WING ILES 630 SEAL RIB INBD & LE & STIFFENER LOWER FOUND CRACKED. REPAIRED IAW RI-57-24-11273 REV A.SDR UIEA2016030700128Skin · dentedRIGHT WING NR 21, VC FLAP FOLDING NOSE SKIN DENT. REPAIRED IAW NR RI-57-44-11269 REV A.SDR UIEA2015102700595Skin · damagedDURING WALK AROUND, CHECK FOUND PIECE OF SKIN MISSING ON FUSELAGE, STATION 2638 - 2658, BL 310 RT, TEMPORARY REPAIR MADE ON FUSELAGE SKIN IAW EO 4453B153, 4453B154 & 4453B155 ALL PART 1.SDR UIEA2015061400311Fire Warning · false activationCARGO DET 12 MAIN DECK, RESULTED IN FIRE MAIN DECK AFT. EICAS WENT OUT ON DECENT. BACKGROUND COLOR. INSPECTED MAIN DECK CARGO COMPARTMENT LINERS FOR OBVIOUS DAMAGE. IAW AMM TASK 25-59-01, FOUND NO ABNORMALITIES. OK FOR SERVICE. MCC WILL MAKE SDR DUE TO FSDR UIEA2014092200458Fire Loop · failedFIRE MAIN DECK AFT EICAS. FOUND FIRE DET LOOP 12B FAILED IN CMCCFDC UNITS 12B & 13B IAW AMM 26-14-01 PN 2156-756A SN 13473B IN POS 12B SN 12448B INSTALLED AT 13B. CFDC UNITS 12A & 13B PLACED ON DMI IAW 26-14-01-02 MEL MDDR 51415.SDR UIEA2014092200459Warning System · false activationSUPRNMRY OXY ON EICAS. RESET SUPRNMRY SYS IAW AMM 35-00-00 EICAS MSG CLEAR, CHECKED OK.SDR UIEA2014022700086Intercostal · crackedCABIN STATION 1180, LBL 98 - 127 FLOOR INTERCOSTAL WEB FOUND CRACKED. R & R CABIN STATION 1180, LBL 98 - 127 FLOOR INTERCOSTAL WEB IAW R1-53-41-10463.SDR UIEA2014022700087Intercostal · crackedCABIN STATION 1200, RBL 98 - 127 FLOOR INTERCOSTAL WEB FOUND CRACKED. R & R CABIN STATION 1200, RBL 98 - 127 FLOOR INTERCOSTAL WEB IAW R1-53-41-10462.SDR UIEA2013122200612Structure · damagedDAMAGE WAS FOUND NEAR TAIL JACK AREA AT BS 2594, ABOVE STRINGER 42R. DAMAGE WAS FOUND TO BE BEYOND THE LIMITS OF SRM 53-00-01, FIG 101 ALLOWABLE DAMAGE. EO 4453A930, FAA 8110-320 DEC13 & NBSP PART 1 ALLOWS FOR A TIME LIMITED REPAIR & NBSP IAW & NBSP SRM 53-80SDR UIEA2013100800512Oven · smokeOVEN STARTED SMOKING DURING USE. DISCONTINUED AND BREAKERS PULLED.SDR UIEA2012092400442Cam · detachedPOST FLIGHT WALK AROUND INSPECTION, FOUND NR 4 T/E FLAP TRACK FAIRING DAMAGED BY FLAP DRIVE CRANK. FURTHER INSPECTION FOUND THE CAM DRIVE DETACHED FROM MID-FLAP. LT MID-FLAP ASSY AND NR 4 T/E FLAP TRACK FAIRING WAS REPLACED AND RIGGED IAW AMM 27-51-01 AND AMSDR UIEA2012091000395Structure · damagedFOUND LIGHTNING STRIKE DAMAGE TO THE NR 2 ENG LT THRUST REVERSER TRANSLATING COWL. DAMAGE ON THE T/E. A TIME LIMITED REPAIR WAS ACCOMPLISHED AS DESCRIBED IN PART 1 OF EO 4478A233 AND FAA 8110-3.SDR UIEA2012081800365Actuator · failedAFTER GEAR RETRACTION, EICAS MESSAGE, "GEAR DOOR" SYNOPTIC INDICATED LT MAIN GEAR DOOR NOT CLOSED, DUMPED FUEL AND RETURNED TO DEPARTURE. GROUND CHECK LOWER ACTUATOR; FLEX HOSES HAD NO PRESSURE UP. WING GEAR DOOR SEQUENCE VALVE REPLACED; RIGGED IAW MM 32-32SDR UIEA2012070900313Liner · damagedNR 3 ENGINE INTAKE OUTER LINER SEGMENT AT 12 O'CLOCK POS, MINOR DAMAGE SIZE .5 X .5". ACCOMPLISHED EO 4472A095, PART 1 TIME LIMITED REPAIR IAW AMM 20-60-07.SDR UIEA2012070700308Acoustic Liner · puncturedDURING MX WALK AROUND, MAINTENANCE FOUND THE FAN CASE ACOUSTICAL LINER PUNCTURE ON THE NR 3 ENGINE ESN 704925. MX DEFERRED ITEM IAW AMM 72-32-00, TABLE 602 ( OVER-SERVICEABLE-LIMIT EXTENSION), DAMAGE MUST BE REPAIRED WITHIN 10 FLIGHT CYCLES OR 100 FLIGHT HOURSDR UIEA2012062200274Skin · damagedDURING PREFLIGHT INSPECTION FOUND A HOLE IN THE FUSELAGE SKIN ABOVE THE LT BODY GEAR APPROX SIZE 1" X 3". ACCOMPLISHED TIME LIMITED REPAIR IAW E/O 4453A736.SDR UIEA2012042000158Ecu · failedRTO DUE TO TAKE OFF WARNING. "CONFIG GEAR CTR". IAW AMM 32-53-16. STEERING SYS CHECK FOUND LT AND RT BODY GEAR STRNG RT WORK INTERMITTENT BY BITS SHOW IN CMC AND PHYSICAL CHECK ON THE ACTUATORS. THE ECU WAS REPLACED AND TESTED. FOUND MESSAGE 32055, LBG STESDR UIEA2012041800128Actuator · inoperativeBODY GEAR STEERING INOPERATIVE. ACTUATORS ARE VERIFIED LOCKED AND SYSTEM DEACTIVATED. R & R MLG ACTUATOR.SDR UIEA2012042000150Actuator · malfunctionedLOW SPEED RTO BELOW 40 KTS DUE CONFIG WARNING "CONFIG GEAR CTR" BODY GEAR VERIFIED LOCKED IAW DDG REQ. R & R LT MLG ACTUATOR OPS CHECKED OK.SDR UIEA2012041800130Panel · deformedLEFT INBD MID FLAP T/E OF COVE PANEL DEFORMED IN FOUR PLACES. OPENSDR UIEA2012042000151Skin · damagedNR 1 CORE COWL SCRATCH. REPAIRED IAW SRM 54-45-01-2R-1, REPAIR 1.)SDR UIEA2012022300060Skin · crackedCRACK DAMAGE IN SKIN AT BS 983, S 38L IN THE DRAG SPLICE FITTING AREA. CRACK DAMAGE WAS DETECTED DURING C3 CHECK WHILE ACCOMPLISHING INSPECTION IN COMPLIANCE WITH SB 747-53A2444, REV 2, AD 2001-22-04 IAW EO 4453A499. PERMANENET REPAIR DOUBLERS WERE INSTALLEDSDR UIEA2012012400026Gasket · leakingENGINE NR 4 FAIL. NORMAL PARAMETERS DURING TAKEOFF AND INITIAL CLIMB. ROLLED BACK TO IDLE ABOUT 20,000 FT. FAIL DURING DESCENT. AIR TURN BACK. WINDMILLED ABOUT 40 MINUTES. FOUND FUEL LEAK AT FUEL OUT CONNECTION AT FCOC GASKET.SDR UIEA2011121000711Bulb · failedUPON LANDING, CREW REST SOM L/E EICAS MESSAGE DISPLAYED ACCOMPLANIED BY SMOKE ODOR. NO VISIBLE SMOKE, PERFORMED "SMOKE OR FUMES IN CABIN, SOURCE UNKNOWN INSPECTION IAW FIM TASK 21-00 AND FOUND BURNED LIGHT BULB. NO OTHER DEFECTS NOTED. REPLACED LIGHT BULBSDR UIEA2011033000234Skin · gougedR21 WING OTBD AFT FLAP NR 688JT GOUGED AT WBL 689.05. (PENDING)SDR UIEA2011033000173Skin · dentedDURING D2-CHECK, A DENT WAS FOUND ON LT FUSELAGE SKIN AT BS 1700, S-41L. THE DENT WAS BEYOND THE ALLOWABLE LIMIT IAW SRM 53-00-01, FIG 101. HFEC INSPECTED DAMAGED SKIN TO ENSURE FREE OF CRACKS IAW NDT MANUAL PN 6 51-00-00 FIG.23. HFEC INSPECTED THE OPEN HOLSDR UIEA2011032900233Panel · wornNR 3 ENGINE PYLON PANEL NR 472QR BOLT HOSE WORN. (REPAIR IAW EGAT EZ T2P011A54B-688)SDR UIEA2011032900232Panel · wornNR 2 ENGINE PYLON PANEL NR 462QR BOLT HOLES WORN. (REPAIR IAW EGAT E2 NR T2Q11A54B-687)SDR UIEA2011032900229Longeron · crackedRT LONGERON BOX FAIRING CRACK. (REPAIR IAW SRM 51-70-07, REV 58.)SDR UIEA2011032900228Longeron · crackedL/T LONGERON BOX FAIRING CRACK. (REPAIR IAW SRM 51-70-07, REV 58)SDR UIEA2011032900218Skin · dentedDENT ON THE FUSELAGE SKIN AT STA 1700 S-41L. (IAW T2011A53B-592, REV 00, INSP DENT AREA.)SDR UIEA2011032900188Skin · debondedPANEL NR 688IT OF RT OTBD AFT FLAP INNER SKIN DISBOND, WBL 747.678 RT, WBL 799.20 RT (REPAIR IAW NR T2011A57B-624)SDR UIEA2011032500164Skin · debondedDURING D2 CHECK INSP BEING PERFORMED; A DISBOND DAMAGE WAS FOUND TO THE RT WING OTBD T/E AFT FLAP UPPER PANEL INNER SKIN. DELAMINATION AREA WAS BETWEEN WING STATION, WBL 747.678 - 799.20 AND AS SHOWN IN FIGURE 2. (ALL DETAILS OF DAMAGE AND REPAIR DATA WERE RSDR UIEA2011032400162Seat Track · crackedDURING D-CHECK INSP, CRACKS WERE FOUND ON SEAT TRACK AT BS 995. THE DAMAGED SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R-13, FIG 201.SDR UIEA2011031700199Frame · crackedCRACK ON AFT FRAME OF NR 4 ENG LT CORE COWL. (REPAIR IAW T2011A71B-635, REV 00)SDR UIEA2011031700193Frame · crackedCRACK ON AFT FRAME OF NR 3 ENGINE LT CORE COWL. (REPAIR IAW NR T2011A71B-634, REV 00)SDR UIEA2011031600195Seat Track · crackedCRACK - SEAT TRACK UNDER FLOOR OF MAIN CARGO COMPT STA 995 LBL 76. (REPAIR IAW SRM 53-00-52-2R-13, REV 58)SDR UIEA2011031600194Seat Track · crackedCRACK-SEAT TRACK UNDER FLOOR OF MAIN CARGO COMPT, STA 995, RBL 76. (IAW SRM 53-00-52-2R-13, REPAIR 13, FIG 201, REV 58 FOR REPAIR.)SDR UIEA2011031600183Rib · crackedDENT AND CRACK DAMAGE ON THE RIB OF LT WING OTBD T/E AFTER FLAP AT WBL 549.935. (REPAIR IAW EI NR. T2011A57B-597, REV. 00.)
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