N429MC
Service difficulty reports · 196
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 = 'N429MC' 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 = 'N429MC' 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 UIEA2015123000801Battery Pack · dischargedUPPER RT DOOR EXIT LIGHT DID NOT COME ON. RECHARGED EMER PACK M312 IAW CMM 25-65-02. REINSTALLED BATTERY PACK IAW AMM 33-51-04. OPERATIONS CHECKED GOOD.SDR UIEA2015041700047Door · failedEMERGENCY DOOR OPENING DEVICE FAILED TO DEPLOY DURING CHECK. CARTRIDGE SHOWS FIRED HOWEVER PENETRATOR FAILED TO PIERCE DIAPHRAGM THUS NOT RELEASE THE CHARGE NITROGEN. AFTER INSPECTION, MANIFOLD ASSY. SHOWS PENETRATOR MADE A DENT ON RUPTURE DISC ONLY.SDR UIEA2012122200558Skin · gougedDURING MX WALKAROUND, MX FOUND TWO GOUGES ON THE NR 4 ENGINE LT THRUST REVERSER TRANSLATING COWL OUTER SKIN. PERFORMED A TIME LIMITED REPAIR.SDR UIEA2012101300471Battery · weakCHECK FOUND LT UPPER DOOR BATTERY NO TEST. SWAPPED BATTERY CONFIRMED WEAK. REPLACED BATTERY.SDR UIEA2012042000155Structure · crackedNR 3 NACELLE AFT END CAP CRACKED AT CTR PORTION. REPAIRED IAW EO 4471A090.SDR UIEA2012042000153Tension Tie · crackedBS 1180 RT TENSION TIE AREA FOUND CRACKED AT FRAME. REPAIRED IAW EO 4453A197 AND SB 747-53A2507 FIG 11, OVERSIZE HOLE REPAIR.SDR UIEA2012042000154Channel · crackedM/D STA 1180 RT TENSION TIE FWD CHANNEL CRACKED. REPAIRED IAW SRM 53-40-30-2R-1, REPAIR 1, FIG 201.SDR UIEA2012042000157Fairing · distortedNR 4 ENGINE RT CORE COWL AFT UPPER TITANIUM FAIRING FOUND DISTORTED AND CHAFED. (NR 4 ENG RT CORE COWL AFT UPPER TITANIUM FAIRING DAMAGED AREA REPAIRED IAW SRM 54-41-01, FIG 201, REPAIR 5.)SDR UIEA2012042000152Beam · crackedLT MLG INBD WW DOOR AFT EDGE BEAM CORROSION CRACKED. LT MLG INBD WW DOOR 65B10919-35, REPLACED IAW SRM 51-10-02.SDR UIEA2011122900739Skin · delaminatedDURING MX WALKAROUND MX FOUND DAMAGE TO THE RT INBD AILERON T/E WITH DELAMINATION DAMAGE, MEASURING 2.0" X 4.0". THE DAMAGE EXCEEDS THE LIMITS OF THE SRM 57-60-01, FIG 101 ALLOWABLE DAMAGE 1. (DISPOSITION IS TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PSDR UIEA2011111200649Unknown · unknownDURING AUTO FUELING, RED OVERFILL LIGHT ILLUMINATED AND FUEL SPILLED OUT OF LT WING. (VOLUMETRIC TOPOFF DEFERRED IAW DDPG 28-21-1-2.)SDR UIEA2011110600639Bottle · lowDURING DAILY CHECK, MX FOUND THE RT UPPER DECK DOOR ASSIST BOTTLE LOW (DEFERRED UPPER DECK RT DOOR).SDR UIEA2011101900594Access Door · damagedDURING MX WALKAROUND, REVEALED NR 1 ENGINE THRUST REVERSER ACCESS DOOR WAS FOUND OPEN AND DAMAGED.SDR UIEA2011101900573Skin · crackedDURING MX WALKAROUND, MX FOUND A CRACK WHICH IS APPROX 8" LONG AND 4" WIDE ON THE NR 4 ENGINE CORE COWL SKIN. MX FOUND A 4" SECTION OF THE LT CORE COWL L/E RUB STRIP BROKEN OFF. THIS COINCIDES WITH THE 4" SCRATCH MARKINGS ACROSS THE L/E OF THE DAMAGED AREA SDR UIEA2011100800565Slide · unwanted deployRT EMERGENCY DOOR UPPER DECK WILL NOT ARM SLIDE MANUAL TO AUTOMATIC FUNCTION. INADVERTENT SLIDE DEPLOYMENT. ITEM TRANSFERRED TO (CL1443) IAW DDG 52-23-1-3.SDR UIEA2011091900513Slide · out of positionFOUND U/D RT EMERGENCY DOOR SLIDE MODE SELECTOR LEVER CANNOT BE PUT IN AUTO MODE. SLIDE RE-POSITIONED AND OPS CHECKED OK.SDR UIEA2011041000242Skin · crackedENGINE COWLING - NR 4 RT ENGINE CORE COWL OUTER SKIN - CRACK - REPAIR - DURING MX WALKAROUND, MX FOUND A CRACK ON THE NR 4 RT CORE COWL OUTER SKIN. THE CIRCUMFERENTIAL CRACK IS APPROX 1 IN LONG. THE LENGTH OF THE CRACK EXCEEDS THE SRM LIMITS. (DISPOSITION ISDR UIEA2011030700143Actuator · failedUPON ARRIVAL, THE NR 3 RT THRUST REVERSER, MX FOUND THE T/R NOT STOWED. AFTER INSP MX FOUND THE LOWER BALLSCREW ACTUATOR AT FAULT AND FAILED, NOT ALLOWING THE THRUST REVERSER TO BE MANUALLY STOWED. (DISPOSITION IS TO PERFORM A DETAILED INSPECTION OF THE NR 3SDR UIEA2011020200040Bracket · damagedDURING WALKAROUND INSP, MX REPORTED DAMAGE TO THE LT; WLG DOOR WARNING SENSOR MOUNT BRACKET AT BS1255.750 WITH 2 EA CRACKS REF FIG 1. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS REPAIR DOUBLER (2 EA) MAKE FSDR UIEA2011011400001Pseu · out of adjustAFTER T/O GEAR LEVER WOULD NOT MOVE UP. COMPLIED IAW QRH PROCEDURES. RAISED GEAR (REPLACED PSEU), JACKED ACFT AND TILT SENSOR ADJUSTMENTS ACCOMPLISHED. (FOUND L/B GEAR ALT SWITCH AND R/B GEAR PRIMARY SWITCHES OUT OF ADJUSTMENT). ALL OPERATIONS WERE NORMAL.SDR UIEA2010120600187Skin · delaminatedDURING WALKAROUND INSP, MX FOUND THE RT WING LANDING GEAR DOOR - LOWER EDGE DELAMINATION, MEASURING 2.2 IN. X 0.800 IN. (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, SCHEDULE REPEAT INSPECTIONS ASDR UIEA2010071000098Nose Cowl · dentedDURING WALK AROUND INSP, MX FOUND THE NR 4 ENGINE INLET NOSE COWL L/E DENTED AT APPROX 10 O' CLOCK POSITION MEASURING 10.0 INCHES IN LENGTH AND 0.9 INCH DEEP. AFTER DETAIL VISUAL INSP (10X MAGNIFYING GLASS) IT WAS VERIFIED THAT NO CRACK CONDITION EXISTS. (DISSDR UIEA201000131Failsafe · crackedDURING C-CHECK, IN MARCH 2010, A CRACK WAS FOUND IN THE 65B09631-86 BS 1200, S-9L FRAME FAILSAFE CHORD CRACK COMMON TO THE TENSION TIE. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-70-11, REPAIR 1 AND NRC 503951. THE 65B01753-369 FAILSAFE CHORD IS MADE FROM BAC1490SDR UIEA201000040Tension Tie · crackedLEFT BS 1140 TENSION TIE AREA FOUR FASTENER HOLES CRACKED AT FRAME WEB. BS 1140 FRAME REPAIRED AS PER EO 4453A216 PART 7 POINT 2.SDR UIEA201000039Tension Tie · crackedRIGHT BS 1160 TENSION TIE AREA FOUR FASTENER HOLES CRACKED AT FRAME WEB. BS 1160 TENSION TIE HOLES OVERSIZED REPAIRED AS PER EO4453A197 AND SB 747-53A2507 REV 1.SDR UIEA201000038Tension Tie · crackedRIGHT BS 1160 TENSION TIE AREA ONE FASTENER HOLE CRACKED AT ANGLE CLIP. BS 1160 TENSION TIE ANGLE CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.SDR UIEA201000037Tension Tie · crackedLEFT BS 1180 TENSION TIE AREA 2 FASTENER HOLES CRACKED AT FRAME WEB. BS 1180 FRAME REPAIRED AS PER EO 4453A216 PART 7 POINT 4.SDR UIEA201000036Tension Tie · crackedLEFT BS 1220 TENSION TIE AREA ONE FASTENER HOLE CRACKED AT FRAME. BS 1220 ENTIRE FRAME REPLACED FROM PRODUCTION SPLICE STR 4 TO STR 11.5 PRODUCTION SPLICE PER EO 4453A216 PART 7 POINT 6.SDR UIEA201000035Tension Tie · crackedLEFT BS 1200 TENSION TIE AREA ONE FASTENER HOLE CRACKED AT FAILSAFE CHORD. FAILSAFE CHORD REPAIRED AS PER SRM 51-70-11 FIG 1 AND EO 4453A216.SDR UIEA201000034Tension Tie · crackedRIGHT BS 1140 TENSION TIE AREA ONE FASTENER HOLE CRACKED AT FAILSAFE CHORD. FAILSAFE CHORD REPAIRED AS PER SRM 51-70-12-2R AND EO 4453A216.SDR UIEA201000033Tension Tie · crackedLEFT SIDE BS 1160 TENSION TIE AREA FOUR FASTENER HOLES CRACKED AT FRAME WEB. BS 1160 FRAME REPAIRED AS PER EO 4453A197 PART 5 POINT 6 AND SRM 53-40-07 REPAIR 3.SDR UIEA201000032Structure · crackedLEFT SIDE HORIZONTAL STAB UPPER REAR SPAR AREA ONE HOLE CRACKED AT SPLICE PLATE AREA RUNNING FWD .0625 INCH. REPAIRED AS PER HX RS NUMBER R-55-12-36662 AND EO 4455A035.SDR UIEA201000132Failsafe · crackedDURING C-CHECK, IN MARCH 2010, A CRACK WAS FOUND IN THE 65B01750-806 BS 1140, S-9R FRAME FAIL-SAFE CHORD CRACK COMMON TO THE TENSION TIE. REPAIR ANGLES WERE INSTALLED IAW SRM 51-70-12, REPAIR 1 AND NRC 503241. THE 65B01750-806 FAILSAFE CHORD IS MADE FROM BAC1SDR UIEA201000002Fairing · missingON WALK AROUND, FOUND NR 5 CANOE MISSING. ALSO FOUND DAMAGE TO RT FUSELAGE SKIN AND LONGERON BOX. INSTALLED NR 5 CANOE AND OPERATIONAL CHECK OK. ALSO, ACCOMPLISHED REPAIR REF EO4453A333, FUSELAGE SECTION 44-LONGERON BOX, BS 1442.41 - BS 1480 FUSELAGE SKIN DSDR UIEA201000171Skin · dentedA DENT WAS FOUND IN THE FUSELAGE SKIN AT BS 1993 BETWEEN S-41L AND S-42L. THE DENT MEASURES 3.5 INCHES LONG BY 0.5 INCHES WIDE AND 0.020 INCHES DEEP."THE DENT WAS INSPECTED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III BUT WITHIN LIMITS FSDR UIEA2009120800003Wedge · damagedTHE PURPOSE OF EO 4455A032 IS TO DOCUMENT A MAJOR REPAIR. WHILE PERFORMING A-CHECK INSP, MX REPORTED DAMAGED OF THE RT INBD HORIZ STAB ELEVATOR T/E MEASURING 2.750 IN LONG AND 3.0 IN INTO THE T/E WEDGE. (PERMANENT REPAIR ACCOMPLISHED IAW THE SRM 55-20-01 FIG 2SDR UIEA201000173Skin · delaminatedNR 4 RH T/R COWL WITH DELAMINATION DAMAGE TO THE OUTER SKIN FROM A PREVIOUS REPAIR, LOCATED AT APPROX 2:00 POSITION. DISPOSITION WAS MADE TO PERFORM A REPAIR BY FILLING THE DAMAGED AREA WITH BMS5-28 POTTING COMPOUND OR EQUIVALENT TO CONTOUR AND APPLY (2) LAYERSDR UIEA201000172Strip · missingTHE L/E STRIP ON THE NR 3 RT FAN COWL WAS FOUND WITH APPROX 20" MISSING. "DISPOSITION WAS TO APPLY 1 LAYER OF SPEED TAPE. DVI EVERY FLIGHT CYCLE AND REPLACEMENT OF THE FAN COWL AT THE NEXT "A" CHECK".SDR UIEA200900016Fairing · damagedNR 6 CANOE DAMAGED. PREPARED CLEANED, AND REPAIRED DAMAGE TO CANOE IAW SRM 51-70-07-06-01.SDR UIEA200800337Door · failedLOWER PRESSURE RELIEF DOOR STATUS MESSAGE DISPLAYED WITH PACK 2 MESSAGE. DEACTIVATED LOWER PRESSURE RELIEF DOOR AND PLACED ON MEL 21-32-1SDR UIEA200800330Unknown · odorAIR TURNBACK - LLCCAFR SWITCH IN POSITION "BOTH" TEMP SELECTED FOR 7° LOWER FORWARD , AFT MAIN DECK, FWD AND AFT. THE AIR IN THE COCKPIT WAS UNCONTROLLABLE - HIGH PRESS AIR BLOWING AROUND NAV DISPLAY - SELECTED THE LLCCAFR SWITCH OFF TO CONTROL THE TEMP IN THSDR UIEA200800290Skin · damagedDURING C-CHECK FORWARD CARGO DOOR EXTERNAL SURFACE SPLICE AREA FOUND 1 EA LIGHTNING STRIKE AT UPPER AFT SIDE OF MASTER LOCK HANDLE. REPAIRED AREA AS PER EO 4452A047. (S)SDR UIEA200800291Intercostal · crackedDURING C-CHECK UPPER DECK STATION 360-380 RBL 28 INTERCOSTAL CHANNEL FOUND CRACKED. REPLACED CHANNEL AS PER SRM 51-10-02 AND INTERCOSTAL AS PER SRM 51-40-02. (S)SDR UIEA200800292Skin · crackedDURING C-CHECK AFT CARGO DOOR CUTOUT FORWARD UPPER CORNER FOUND CRACKED AT FASTENER HOLE. REPAIRED AS PER SRM 53-60-01 FIGURE 201. (S)SDR UIEA200800293Skin · damagedDURING C-CHECK FOUND FORWARD CARGO COMPARTMENT STATION 520-540-STR 34-35L SKIN DAMAGED. SKIN REPAIRED AS PER SRM 53-00-01 FIGURE 201. (S)SDR UIEA200800294Skin · scratchedDURING C-CHECK FOUND FUSELAGE SKIN WITH DEEP SCRATCH AT STATION 2080 STR 26-27R. REPAIRED AS PER SRM 53-00-01 FIGURE 201. (S)
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