N412MC
Service difficulty reports · 193
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 = 'N412MC' 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 = 'N412MC' 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 UIEA2012061900272Blade · damagedDURING BIRD STRIKE INSPECTION IAW AMM 05-51-14, ENGINE 4, FAN BLADE; 8 WAS FOUND TO HAVE DAMAGE. (FAN BLADE 8 WAS INSPECTED IAW AMM 72-31-02 AND THE DAMAGE WAS FOUND TO BE OUT OF ALLOWABLE LIMITS. FAN BLADE 8 WAS REPLACED IAW AMM 72-31-00. VIBRATION SURVEY ASDR UIEA2012041200121Web · crackedWHILE DOING AN "A" CHECK INSPECTION OF THE RT WING FIXED T/E INBD SPOILERS SUPPORT RIBS, A 1.5 INCHES LONG CRACK WAS FOUND ON THE WEB OF THE INBD SUPPORT RIB ASSY AT WBL 255.692. THE DAMAGE EXCEEDED THE LIMITS OF THE SRM 57-51-02, FIGURE 101. CRACK REPAIREDSDR UIEA2012040900120Skin · damagedDURING WALKAROUND INSPECTION, MX REPORTED DAMAGE TO THE LT HORIZ STABILIZER L/E SKIN - SS 250 DENT - REPAIR (REF FIG 1), MEASURING 6.5" X 2.5" X 0.250". DAMAGE IS BEYOND THE SRM LIMITS IAW THE SRM 55-10-01, FIG 101, ALLOWABLE DAMAGE 1. (DISPOSITION WAS MADE TSDR UIEA2012021600052Acoustic Liner · damagedDURING MX WALKAROUND, FOUND DAMAGE TO NR 2 ENGINE THRUST REVERSER ACOUSTIC MESH AND HONEYCOMB. DAMAGE IS LOCATED AT THE 5 O'CLOCK POSITION AND HAS DIMENSIONS 3' LENGTH, .3750" WIDTH AND .2500" DEPTH. REF TO FIG 1 FOR DAMAGE DETAILS. PERFORMED A TIME LIMITEDSDR UIEA2012013000032Beam · damagedDURING TROUBLESHOOTING ON THE AFT CARGO DOOR ACCOMPLISHED, MX FOUND DAMAGE TO THE DOOR INTERNAL BEAM (INNER CHORD OF CLOSEOUT BEAM), NEAR THE FWD HOOK PULL IN RETURN SPRINGS AT BS1810 - BS1820 WITH 2 GOUGES, MEASURING 0.187 IN. AND 0.3875 IN. FROM THE EDGE. (SDR UIEA2012012300022Skin · crackedDURING A-CHECK INSPECTION, MX FOUND DAMAGE TO THE RT WING ILES 750 - UPPER FIXED LEADING PANEL CRACK, MEASURING 43.0" IN LENGTH; THE DAMAGE EXCEEDS THE LIMITS OF THE SRM 57-41-01, FIG 101 IAW SRM 51-70-02. ALLOWABLE DAMAGE GENERAL. PERFORMED A TIME LIMITED RSDR UIEA2011120600702Pdu · failedDURING PROCESS OF UPLOADING ACFT, MDC PDU AT 18L FAILED (SMOKE) PDU REMOVED AND INSTALLED JUMPER AND BLACKING PLATE.SDR UIEA2011111500659Support · brokenFOUND SUPPORT ROD FOR LT WING T/E UPPER FIXED PANEL BROKEN AT WBL 432. REPLACED WITH NEW SUPPORT ASSY IAW AMM 57-22-01. ADJUSTED IAW AMM 57-22-01-825-001.SDR UIEA2011111500658Carriage · damagedFOUND LT INBD FLAP CARRIAGE ON OTBD TRACK CHAFED AND WORN. CARRIAGE REMOVED IAW AMM 27-51-24. INSTALLED NEW CARRIAGE IAW AMM 21-51-24.SDR UIEA2011111500657Carriage · damagedFOUND LT INBD FLAP CARRIAGE DAMAGED. LUG BROKEN AND ROLLER MISSING. CARRIAGE REMOVED IAW AMM 27-51-24. INSTALLED NEW CARRIAGE IAW AMM 27-51-24.SDR UIEA2011111500656Bearing · looseFOUND LT OTBD FORE FLAP INBD FITTING BEARING LOOSE LT OTBD FORE FLAP IAW AMM 27-51-05. REPAIRED.SDR UIEA2011111500655Retainer · brokenFOUND LT LOWER FIXED T/E PANEL WBL129 SEAL RETAINER BROKEN. REPLACE FIXED PANEL AFT SEAL RETAINER IAW AMM 20-51-01.SDR UIEA2011111500654Skin · damagedFOUND LT WING T/E UPPER FIXED PANEL BETWEEN WBL 432 AND WBL 446 DAMAGED. PANEL REMOVED IAW AMM 57-22-01. LT WING T/E UPPER FIXED PANEL REPAIRED IAW EO 4457A383. REINSTALL PANEL IAW AMM 57-22-01.SDR UIEA2011111500653Rib · dentedFOUND LT WING FIXED T/E RIB AT WBL 445.90 DENTED. AILERON REPAIRED IAW EO4457A385 PART III.SDR UIEA2011111500652Skin · damagedFOUND INBD AILERON DAMAGED IN UPPER SURFACE. LT INBD AILERON REMOVED IAW AMM 27-11-01. REPAIRED THE DAMAGED AREA REF TO SRM 51-70-11. INSTALL LT INBD AILERON AFTER REPAIR REF AMM 27-11-01. ADJUSTED AND OPS TESTED IAW AMM 27-11-00, TESTED OK.SDR UIEA2011111500651Structure · damagedDURING AN A CHECK, FOUND LT INBD MID FLAP L/E INBD PART DAMAGED. VISIABLE DAMAGE AREA 1"X4.5" ALSO FOUND 3L TRACK CUTOUT WEB CRACKED. LT INBD MID FLAP REMOVED IAW AMM 27-51-01. INSTALLED NEW LT INBD MIDFLAP IAW AMM 27-51-01. ADJUST IAW AMM 27-51-01, OPS SDR UIEA2011111500650Structure · damagedDURING A CHECK INSPECTION, FOUND LT INBD FORE FLAP DAMAGED. L/E AREA DAMAGED LENGTH 1.25" FRONT SPAR WEB DAMAGE 8" X 4". LT INBD FORE FLAP REMOVED IAW AMM 27-51-02. INSTALLED NEW LT INBD FORE FLAP IAW AMM 27-51-02. ADJUST IAW AMM 27-51-01. OPS CHECKED OK.SDR UIEA2011110600637Support Channel · damagedWING RIB SUPPORT CHANNEL WAS FOUND DAMAGED AS A RESULT OF THE LT INBD T/E FLAP INCIDENT ON 412. THE DAMAGES WHICH ARE APROX 2" LONG X 0.5" DEEP AND 2.5" LONG X 0.3" DEEP ARE LOCATED ON THE OTBD AND INBD FLANGES OF THE CHANNEL. (SINCE A REPLACEMENT PART COULD SDR UIEA2011060700287Fairing · crackedDURING A-CHECK, ON NR2 ENGINE RT T/R TRANSCOWL, AFT FAIRING WAS FOUND WITH A CRACK APPROX 2.45 INCHES IN LENGTH. (DISPOSITION WAS MADE TO PERFORM REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS. PERMANENT REPAIR AS DECRIBED IN PART 2 WILL BE PERFORMED AT 15,0SDR UIEA2011042600252Skin · damagedDURING WALK-AROUND INSP, MX REPORTED DAMAGE WAS FOUND TO THE RT FUSELAGE SKIN BS1937, BELOW S37R (THE DAMAGE IS BEYOND THE SRM 53-00-01, FIGURE 101 ALLOWABLE DAMAGE 1, DETAIL III LIMITS. TIME LIMITED REPAIR ACCOMPLISHED AS DESCRIBED IN PART 1 WORK INSTRUCTIONSDR UIEA2011042600250Skin · dentedDURING WALK-AROUND INSPECTION AT ANC, MX REPORTED DAMAGE WAS FOUND TO THE RT FUSELAGE SKIN BS1928.5, BELOW S38R; 1 INCH DIAMETER. EO 4453A552 (THE DAMAGE IS BEYOND THE SRM 53-00-01, FIGURE 101 ALLOWABLE DAMAGE 1, DETAIL III LIMITS. TIME LIMITED REPAIR ACCOMSDR UIEA2011042600249Skin · damagedTHE PURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR. DURING WALK-AROUND INSP, MX REPORTED LT OTBD MID FLAP - WBL 597 - WBL 730 - T/E - DELAMINATION/DAMAGE (PN: 65B01925-311C / SN: 000551) - T/E MEASURING 11.0 FT. X 7.5 IN. (REF FIGURE 1). (DISPOSITION WAS MASDR UIEA2011022400122Warning Message · illuminatedCONFIGURATION GEAR CENTER, TAKEOFF WARNING AT APPROX 20 KTS. REJECTED TAKEOFF(BODY GEAR STEERING INDICAITON SYSTEM DEACTIVATED AND DEFERRED. BODY GEAR SYSTEM CONFIRMED DEACTIVATED)SDR UIEA2011012500008Support Fitting · damagedDURING D-CHECK INSP OF DATUM ACFT, DAMAGE (WORN HOLE) WAS FOUND ON SUPPORT FITTING OF APU LT SUPPORT LINK FWD SIDE AT STA 2658 (REFER TO FIG 1 FOR DAMAGE LOCATION). (THE REPAIR (FIG 2) WAS PERFORMED IAW EGA-TLS-11-0009 AND WAS APPROVED IAW SR 1-1777633064 ANDSDR UIEA2011012400026Support · chafedCHAFING DAMAGE ON THE SEAL SUPPORT OF LT WING FIXED T/E SPOIL SUPPORT RIB AT WX 863.73. REPAIR IAW EI NR T201157B-154. REV 00.SDR UIEA2011012400022Frame · damagedHEAT DAMAGE ON THE FRAME INNER CHORD AT STA 2638, WL 285 LT SIDE. REPAIRED IAW EI NR T2011 A53B-139 REV EO 00, 01,02 AND 03.SDR UIEA2011012300018Intercostal · crackedCRACK ON BULK CARGO FLOOR INTERCOSTALS AT STA 2020, RBL 0.25 AND STA 2080, RBL 0.25". (REPAIRD IAW EI 2011A53B-122 REV 00 AND 01.)SDR UIEA2011012300016Skin · dentedCREASE AND DENT DAMAGE ON RT FUSELAGE SKIN AT STA 2600 S-42R LWR AFT TAIL JACK PAD AREA. (REPAIRED IAW EI NO T2011 A53B-093REV.00. AND REV 01.)SDR UIEA2011012300012Stiffener · damagedDURING THE D02 PLUS C03, GENERAL DAMAGE WAS DETECTED ON STIFFENER, DEFORMED DAMAGE WAS DETECTED ON 65B04925-47 STIFFENER, AND IMPACT CRACK DAMAGE WAS DETECTED ON THE 65B04925-84 STIFFENERS (2 PLACES).( REPAIR OF GENERAL DAMAGE ON 65B04325-42 STIFFENER AT BS 17SDR UIEA2011012300009Structure · deformedDURING D-CHECK INSP OF DATUM ACFT, DAMAGE (DEFORMATION) WAS FOUND ON AFT CARGO SEAT TRACK AT BS 1826, RBL25. (THE DAMAGE AREA WAS REPAIRED IAW SRM 53-00-52, REPAIR 10.)SDR UIEA2011012200035Web · brokenBROKEN WEB AFT LWR CARGO STRUCTURE AT STA 1760 BETWEEN STRINGER S43R TO S44R (REPAIR DAMAGE AREA IAW SRM 51-70-13, REV 58)SDR UIEA2011012100019Panel · damagedDAMAGE WAS FOUND ON M/D CARGO COMPARTMENT DADO PANEL (P/N 453U7023-33). AT STA 1720(REPAIR IAW EI NO T2011A53B-131 REV 00)SDR UIEA2011012100029Rib · crackedCRACKS ON LT HST L/E RIB AND CLIP AT L/E STA 1318 ( REPLACED CLIP IAW EO NO T2011P55B-188, REV 00. 2. REPAIRED CRACK RIB IAW EI NO T2011A55B-184 REV 00.)SDR UIEA2011012100020Panel · brokenDAMAGE WAS FOUND ON M/D CARGO COMPARTMENT DADO PANEL (P/N 453U7023-33). AT STA 1720(REPAIR IAW EI NO T2011A53B-131 REV 00)SDR UIEA2011012100017Frame · crackedREPAIR NR 4 ENG RT FAN REVERSER TORQUE BOX FWD FRAME CRACK. (REPAIR IAW EI NO T2011 A78B-208 REV 00)SDR UIEA2011012100014Structure · damagedPERFORM AFT CARGO LWR CHORD STRUCTURE AT STA 1640 BETWEEN STRINGER S49R TO S47R. (REPAIR DAMAGE AREA IAW SRM 51-70-13. REV 58)SDR UIEA2011012100013Skin · gougedDURING D02 PLUS C03 CHECK OF DATUM ACFT, GOUGE DAMAGE (1 IN LONG AND 0.003 IN WIDE) WAS FOUND ON THE FUSELAGE SKIN BETWEEN BS 1920-BS 1940 AND S-33L - S-34L.(THE SURFACE FINISH OF THE BLENDED AREA WAS INSPECTED AND VERIFIED TO BE 125 MICROINCHES OR BETTER. THESDR UIEA2011012100010Skin · damagedDURING D02 PLUS C03 CHECK OF DATUM ACFT, CREASE DAMAGE AND A DENT LOCATED ON THE RT FUSELAGE SKIN AT BS 2060 AND S-42R (LOWER AFT SIDE OF TAIL JACK'S LOCATION) WERE SCHEDULED FOR A PERMANENT REPAIR. THE DAMAGED AREAS WERE PREVIOUSLY REPORTED IAW SR 1-18269954SDR UIEA2011012000034Frame · wornWORN NR 4 ENG LT CORE COWL INNER FRAME WORN AT 7:00 POS. (REPAIR IAW 747-400 SRM 54-45-02. REPAIR 1. REV 58)SDR UIEA2011011900033Frame · wornWORN NR 4 ENG LT CORE COWL INNER FRAME WORN AT 7:00 POS. (REPAIR IAW 747-400 SRM 54-45-02. REPAIR 1. REV 58)SDR UIEA2011011900025Skin · dentedREPAIR 2 EA DENTS ON LOWER SIDE WALL FLOW PATH SKIN OF NR1 ENG; RT FAN REVERSER (REPAIR IAW EI NO. T2011A38B-155 REV 00.)SDR UIEA2011011900024Support · crackedREPAIR CRACK ON THE CHORD OF THE LT WING FIXED T/E LWR SUPPORT STRUCTURE AT WS 1293. (REPAIR IAW T2011A57B-157, REV 00.)SDR UIEA2011011900015Cowling · chafedCHAFING FOUND NR 1 ENG LT CORE COWL HAD CHAFING ON INTERIOR FRAME AREA AT ABOUT 3:00. (REPAIR DAMAGE AREA IAW SRM 54-45, FIG 201, REPAIR 1. REV 58.)SDR UIEA2011011400023Shim · migratedSHIM MIGRATION UNDER FIN TO BODY SUPPORT FITITNG AT STA 2517 LBL/RBL 25 (IAW EO T2011A53B-135, REV 00) REPLACE NEW SHIM.SDR UIEA2011011000032Panel · crackedLT LONGERON BOX FAIRING & NBSP; PANEL CRACK (REPAIR IAW SRM 51-70-07, REV 58).SDR UIEA2010111000178Probe · brokenDURING ROUTINE MX "A" CHECK IN PVG, MX WAS ACCOMPLISHING EO 4477A003 AND BROKE OFF AN EGT PROBE ON NR 3, ESN 706125 AT THE 11:30 (PROBE NR 6) POSITION LEAVING THE REMAINDER OF THE PROBE IN THE LPT BOSS INACCESSABLE FOR REMOVAL. AS IAW AMM TASK 77-21-00-216-00SDR UIEA2010083100152Skin · crackedDURING A-CHECK, GOUGES AND A CRACK WERE FOUND IN THE FUSELAGE BELLY SKIN BETWEEN BS 2585 AND 2587 AND S-47L AND -47R. REFER TO FIG 1 FOR DAMAGE LOCATION AND DESCRIPTION. (THE FUSELAGE SKIN AT THE DAMAGE LOCATION IF MADE FROM A 0.050 INCH THICK SKIN WITH A 0.04SDR UIEA2010072200116Seat Track · damagedDURING DAILY CHECK INSP, DAMAGE TO THE LWR AFT CARGO COMPARTMENT - BS 1880, RBL 46.0 SEAT TRACK - CRACKED / DAMAGE WAS FOUND (ACCOMPLISH REPAIR TO THE LOWER AFT CARGO COMPARTMENT. REMOVE/TRIM OUT THE SEAT TRACK DAMAGED SECTION IAW THE SRM 51-10-02. APPLED A SDR UIEA2010071700114Structure · damagedDURING SPECIAL CHECK (TLW); A STORM DRAGGED A MX STAND IMPACTING THE LT WING - OTBD L/E AT OLES1580.95, OLES1606.95 & OLES1625.951. DENT AT OLES 1580.95 (11.0 IN. LONG X 1.750 IN. WIDE X 0.187 IN. DEEP) REFERENCE FIG 1. EXCEEDS THE LIMITS IAW SRM 57-41-01 FIGSDR UIEA2010071100099Outflow Valve · malfunctionedACFT WOULD NOT MAINTAIN CABIN PRESSURE, ALT 310. FLIGHT CREW FOLLOWED QRH PROCEDURES; RETURNED TO STATION. (FUEL REMOVED PRIOR TO LANDING: 62.0. LANDING WT: 302,056) (UPON INSP, MX FOUND RT OUTFLOW VALVE AUTO MODE INOPERATIVE, MANUAL OPS NORMAL. RT OUTFLOW DE
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