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.

SDR UIEA201000157Skin · crackedDURING MX WALKAROUND, MX FOUND 2EA CRACKS ON THE NR2 RT ENGINE CORE COWL OUTER SKIN. 1EA CIRCUMFERENTIAL CRACK IS APPROX 0.5 IN. LONG AND THE OTHER CRACK IS APPROX 2.0 IN. LONG. THE LENGTH AND THE SPACING OF THE CRACKS EXCEED THE SRM LIMITS. DISPOSITION IS TO May 11, 2010 · N412MC · Boeing 74747UF · Nacelle/Pylon, Plate/SkinSDR UIEA201000107Brake Assy · fireON TAXI, GROUND CREW NOTED FIRE COMING FROM NR 2 TIRE/BRAKE ASSY AND SMOKE COMING FROM THE NR 1 TIRE/BRAKE ASSY. R & R NR 1 AND NR 2 TIRE AND BRAKE ASSEMBLIES.Mar 31, 2010 · N412MC · Boeing 74747UF · Landing Gear Brake SystemSDR UIEA201000159Access Panel · crackedCRACKS WERE FOUND IN THE NR 3 PYLON INBD ACCESS PANEL 472FL AS SHOWN IN FIGURE 1. NR 3 PYLON ACCESS PANEL 452FL CRACKED AREA REPAIRED IAW EO 4454A095.Feb 9, 2010 · N412MC · Boeing 74747UF · Nacelle/Pylon, Plate/SkinSDR UIEA200900062Structure · damagedLT WING INBD MID FLAP L/E FOUND DAMAGED AT MOST INBD AREA. PERMANENT REPAIR PERFORMED IN ACFT WITH THE SRM 41-70-07 AND SRM 57-53-01 FIG 201, TABLE 1.Sep 22, 2009 · N412MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA200900048Warning Message · intermittentENROUTE EICAS STARTER CUTOUT ENG 3 ON/OFF INTERMITTENTLY. ACCOMPLISHED PROCEDURES IAW FIM 80-03-11-00. MESSAGE CLEARED. NO LATCHED FAULTS.Aug 12, 2009 · N412MC · Boeing 74747UF · Central WarningSDR UIEA201000179Skin · damagedLT T/E INBD MID FLAP INBD L/E SKIN PANEL WBL 137.55 WITH A GOUGE HOLE/DAMAGE (ONE FACE SKIN AND HONEYCOMB DAMAGE WITHOUT INTERNAL SKIN DAMAGE MEASURING 1.0 IN X 10.0 IN. "TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS OF EO 4457A195. SCHEDULE REPJun 23, 2009 · N412MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA201000162Tray · crackedTRAY CRACKED AT STA 1800 IN AFT CARGO COMPT RT SIDE. "DRILL 0.25 DIA STOP HOLE. MAKE 2 REPAIR PLATES WITH 0.071 7075 = TE CLAD SHEET. INSTALL REPAIR PLATES IAW SRM 53-00-53/206."Jun 23, 2009 · N412MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA201000161Structure · brokenTHE CORNER AT OTBD AFT L/E WING FLAP WAS BROKEN. (0.5" X 0.5"). 1. "REMOVED THE DAMAGE AS SRM 51-70-17. 2. "LAY-UP REPAIRED THE DAMAGE WITH EA9390A/B RESIN BM 59-3 TYH-2. FABRIC AS SRM 51-70-17. CURED UNDER VACUUM. 3. "SANDED SMOOTH THE REPAIR AREA AS SRM 51-Jun 23, 2009 · N412MC · Boeing 74747UF · Leading Edge DevicesSDR UIEA201000160Skin · gougedLT T/E INBD MID FLAP - INBD L/E SKIN PANEL - WBL 137.55 WITH A GOUGE HOLE/DAMAGE. (ONE FACE SKIN AND HONEYCOMB DAMAGE WITHOUT INTERNAL SKIN DAMAGE). MEASURING 1.0 IN X 10.0 IN. "EA4457A195: DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN Jun 23, 2009 · N412MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA200900032Unknown · odorMULTIPLE BLEED OVHT EICAS MESSAGES, COMPLETED QRH PROCEDURES, SMELLED BURNING ODOR. CLOSED LT BLEED SHUTOFF VALVE. STATUS MESSAGE BLEED PRV ENG 2. PERFORMED ENGINE RUN WITH BLEED OFF AND ON. NO BURNING ODOR PRESENT. DISPATCHED THE ACFT WITH HIGH STAGE BLEED May 14, 2009 · N412MC · Boeing 74747UF · Air Distribution SystemSDR UIEA201000180Floorboard · damagedRT MAIN DECK BS 1500 FLOORBOARD DAMAGED. "TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS OF EO 4453A238, INITIATE INSPECTIONS AT EVERY 5 FLIGHT CYCLES. SCHEDULE PERMANENT REPAIR AT THE NEXT A CHECK AFTER PART 1 IN ACC WITH THE SRM 53-00-50 FIG 20Apr 10, 2009 · N412MC · Boeing 74747UF · Fuselage Floor PanelSDR UIEA200800353Skin · gougedBS 1765 STRINGER 34-35R SKIN GOUGED. GOUGE REPAIRED AS PER BOEING MESSAGE 1-1165-0369-47-2 AND EO4453A227.Jan 23, 2009 · N412MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA200800352Structure · dentedNR 1 LEADING EDGE DEVICE BULLNOSE DENTED. REPAIRED AS PER SRM 57-43-02Jan 22, 2009 · N412MC · Boeing 74747UF · Leading Edge DevicesSDR UIEA200800351Skin · dentedNR 10 VC FLAP BULLNOSE HAS DENT. REPAIRED AS PER SRM 57-43-02.Jan 22, 2009 · N412MC · Boeing 74747UF · Leading Edge DevicesSDR UIEA200800355Skin · looseLEFT WING LEADING EDGE FAIRING AT OUTBOARD OF LANDING LIGHT FOUND LOOSE RIVETS. LEADING EDGE REPAIRED AS PER SRM 57-41-01-2R-5 REPAIR 5 FIG 201.Jan 21, 2009 · N412MC · Boeing 74747UF · Leading Edge DevicesSDR UIEA200800354Skin · looseRIGHT WING LEADING EDGE FAIRING AT OUTBOARD OF LANDING LIGHT FOUND LOOSE RIVETS. LEADING EDGE SKIN REPAIRED AS PER SRM 57-41-01-2R-5 REPAIR 5 FIGURE 201.Jan 21, 2009 · N412MC · Boeing 74747UF · Wing, Plate/SkinSDR UIEA200900004Drive Assy · failedAIR TURN BACK, CREW PHONE PATCHED THAT THEY LOST NR 1 WX RADAR SYSTEM. NR 2 WX RADAR SYSTEM WAS ALREADY ON DEFERRAL. CREW RETURNED TO BKK. MAINTENANCE REMOVED AND REPLACED RADAR DRIVE ALL SYSTEMS, OPS CHECKED OK.Dec 29, 2008 · N412MC · Boeing 74747UF · Weather Radar SystemSDR UIEA200800327Radar · failedRIGHT WEATHER RADAR FAILED APPROX 1 HOUR INTO FLIGHT. LEFT RADAR FAILED WHEN SELECTED. PERFORMED AIR TURNBACK. REMOVED DRIED AND REINSTALLED THE WAVE GUIDE DUE TO WATER CONDENSATION. REPLACED RADAR ANTENNA MOUNT AND RADAR CONTROL PANEL. WEATHER RADAR CONTOct 7, 2008 · N412MC · Boeing 74747UF · Weather Radar SystemSDR UIEA200700504Idg · chafedEICAS MESSAGE "ELEC GEN OFF 3" GCB RESET PER QRH, OPERATION NORMAL MOMENTARILY THEN REOCCURRENCE. DIVERTED TO NRT. FOUND CHAFF ON NR 3 IDG T2 HARNESS. PERFORMED REPAIR AS PER SWPM 20-10-13 PAGE 41 PART 2T. THIS ITEM MUST BE REPAIRED WITHIN 500 FLIGHT HOURSDec 17, 2007 · N412MC · Boeing 74747UF · Alternator-Generator DriveSDR UIEA200700318Seat Track · damagedLWR AFT CARGO COMPARTMENT SEAT TRACK CROWN DAMAGED AT STA 1880 RBL 25. DAMAGED SEAT TRACK SECTION REMOVED AND REPLACED PER SRM 53-00-53 REPAIR NR 7 AND 10 AND XEO 53-081107.Aug 14, 2007 · N412MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA200700319Seat Track · damagedMAIN DECK CARGO CTR PALLET LOCK AT STA 1550 UNABLE TO USE LOCK IN POSITION UNTIL FLOOR AND SEAT TRACK REPAIR. SEAT TRACK REPAIRED AT STA 1550 RBL 10 IAW SRM 53-00-52 AND XEO 53-081107-1 AND FLOOR BOARD AT STA 1550 RBL REPAIRED PER SRM 51-70-07.Aug 14, 2007 · N412MC · Boeing 74747UF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA200700268Connector · disconnectedRTO EICAS MSG "CONFIG GEAR STR" WITH HORN AND LIGHTS. SUSPECT WARNING IS DUE TO BODY GEAR STEERING SYS MSG MEL 32-53-2 APPLIES. MAINTENANCE PROCEDURE CARRIED OUT. ELECTRICAL CONNECTORS OF BOTH STEERING ACTUATORS ON RT BODY GEAR DISCONNECTED AND STOWED. ITEJul 15, 2007 · N412MC · Boeing 74747UF · Landing Gear Steering SystemSDR UIEA200700212Rib · crackedRT FIXED T/E PANEL SUPPORT RIB OUTBOARD OF NR 8 SPOILER. HAS 1 CRACK IN RIB WEB APPROX 2" IN LENGTH. REPAIRED IAW XEO- 57-042307-5.Apr 25, 2007 · N412MC · Boeing 74747UF · SpoilersSDR UIEA200700211Structure · damagedRIGHT OUTBOARD AFT FLAP HAS A NICK IN THE TRAILING EDGE AS MARKED 0.25" BY 0.25". REPAIRED IAW XEO- 57-042307-2.Apr 25, 2007 · N412MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA200700209Panel · dentedLT O/B AFT FLAP HAS UPPER ALUMINUM HONEYCOMB PANEL DENTS. REPAIRED IAW XEO- 57-042307-3.Apr 25, 2007 · N412MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA200700207Floor Panel · puncturedDURING A-4 CHECK IN SYD, BULK CARGO FLOOR WAS FOUND PUNCTURED AT TWO PLACES, SIZE 1"BY 1" AND .5" BY .5" WHEN FLOOR WAS REMOVED. REPAIRED IAW XEO- 53-042407.Apr 25, 2007 · N412MC · Boeing 74747UF · Fuselage Floor PanelSDR UIEA200700210Structure · damagedRIGHT INBOARD AILERON OUTBOARD AFT CORNER DAMAGED TO PREVIOUS REPAIR APPROX 3.0" BY 4.0". REPAIRED IAW XEO- 57-042307-1Apr 25, 2007 · N412MC · Boeing 74747UF · AileronsSDR UIEA200700208Door · damagedRT WING LANDING GEAR DOOR ELEPHANT EAR FAIRING IS DAMAGED ON THE LOWER SURFACE AS MARKED. REPAIRED IAW XEO- 52-042307.Apr 25, 2007 · N412MC · Boeing 74747UF · Landing Gear DoorsSDR UIEA200700142Fire Warning · unknownON CLIMB-OUT, FIRE WARNING BELL RANG INTERMITTENT EVERY FEW SECONDS FOR 20 MINUTES OF FLIGHT. NO OTHER INDICATION. MAWEA SYS CYCLED, MAWEA OPERATION CHECK CARRIED OUT AND FOUND NORMAL AS PER AMM 31-51-00, 715-014.Mar 25, 2007 · N412MC · Boeing 74747UF · Fire DetectionSDR UIEA200600280Pressure Switch · damagedRTO, DUE TO - BLEED NR 2 EICAS MSG, LOW SPEED (70 KTS) ABORT. REMOVED AND REPLACED OV PRESSURE SWITCH IAW MM 36-12-03, OPS CHECK OK.Oct 26, 2006 · N412MC · Boeing 74747UF · Pneumatic Indicating SystemSDR UIEA200600134Flap · chafedLEFT HAND OUTBOARD AFT FLAP END WEAR/CHAFE MARK. RANGING IN DEPTH FROM 0.002' TO 0.013'AND FROM 8"X1" IN DIAMETER TO 2"X1".Jun 13, 2006 · N412MC · Boeing 74747UF · Trailing Edge FlapsSDR UIEA200600020Cooling Fan · contaminatedON TRANSIT FLIGHT CREW AND ENGINEERING CREW REPORT BURNING SMELL THROUGHOUT FLIGHT DECK AND NOTICEABLE IN MAIN EQUIPMENT CENTER AND FORWARD CARGO. DEFECT INVESTIGATED, SMELL ISOLATED TO EQUIPMENT COOLING SUPPLY FAN/CENTER RISER FILTER OIL CONTAMINATION. BOTHMar 9, 2006 · N412MC · Boeing 74747UF · Air Distribution FanSDR UIEA200500054Nose Cowl · dentedENGINE 1 NOSE COWL AT 4 O`CLOCK POSITION DENT AT LIP 5.6 INCHES X 4.2 INCHES X 0.224 INCH. DENTED AREA TRIMMED OUT AND SRM WAS PERFORMED. INSTALLED DOUBLER AND FILLER IAW SRM USING BLIND .1562 FASTENERS. (K)Apr 21, 2005 · N412MC · Boeing 74747UF · Nacelle/Pylon, Plate/SkinSDR UIEA200500053Skin · dentedSTA 2660-2680, 2 DENTS FOUND ON EXT SKIN. REPORTED DENT WAS REPAIRED IAW SRM. PERFORMED HFEC INSP, NO CRACKS WERE FOUND. AFTER SECONDARY INSP FOUND DENT, CREASE, AND CHAFING 2.5 INCH X 1.5 INCH X 0.050 INCH. DOUBLER REPAIR PERFORMED IAW SRM. (K)Apr 21, 2005 · N412MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA200500052Skin · dentedSTA 1980-2000, STR 42-44, RT (2 EA) DENT (A) AND (B) WERE FOUND ON THE EXT FUSELAGE. DENT (A) STA 1980-2000, STR 42-43, RT D=0.09, W=1.15 INCH, L=3.8 INCH. DENT (B) STAT 1980-2000, STR 43-44, RT D=0.051, W=1.18, L=1.54. THE DAMAGED AREA TRIMMED OUT. A REPApr 20, 2005 · N412MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR UIEA200400199B-Nut · looseEICAS MESG; ENGINE NR 1 OIL PRESSURE. CONFIRMED OIL PRESSURE BELOW 10 PSI. SHUTDOWN NR 1 ENGINE. CONFIRMED NR 1 ENGINE OIL QTY LOW, AND ON INSPECTION FOUND B-NUT LOOSE FROM OIL TUBE CONNECTED TO FRONT OF MAIN GEAR BOX AT 6 O’CLOCK POSITION. SERVICED ENGINEDec 7, 2004 · N412MC · Boeing 74747UF · Turbine Engine Oil SystemSDR UIEA200400118Gasket · damagedDURING CRUISE ENGINE SHUT DOWN DUE TO FUEL IMBALANCE. POSSIBILITY OF A FUEL LEAK NR 4 ENGINE. FUEL IMBALANCE BETWEEN MAIN NR 1 TANK, AND MAIN NR 4 TANKS. FUEL ENROUTE WAS 1.3 TO 1.4 TOTALIZER 22.6 WHILE CALCULATED 25.6, LEAK COULD BE DOWN STREAM OF FUEL CONJun 28, 2004 · N412MC · Boeing 74747UF · Fuel Controlling SystemSDR UIEA200400117Packing · damagedEICAS MESSAGE 'FUEL IMB' VISUALLY NOTED FUEL LEAK FROM NR 4 ENGINE. ACCOMPLISHED SHUTDOWN PROCEDURES FOR NR 4 ENGINE. TROUBLESHOT FOUND NR 4 ENGINE HMU PERFORMANCE PACKING BADLY DAMAGED. PACKING REPLACED IAW MM 73-21-14. GROUND RUN FOR LEAK CHECK TEST 2, ECJun 25, 2004 · N412MC · Boeing 74747UF · Fuel Controlling SystemSDR UIEA200400003Line · crackedPRECAUTIONARY NR 4 ENGINE SHUTDOWN DUE TO OIL QUANTITY FALLING TO 3 QUARTS AT 1825Z, FL300, MACH .835. FOUND OIL LINE TO LUBE AND SCAVENGE PUMP CRACKED IPC 79-21-03-01 ITEM 303. REPLACED LINE IAW MM 79-21-00, SERVIED ENGINE OIL IAW MM 12-13-03. PERFORMED MPAJan 10, 2004 · N412MC · Boeing 74747UF · Turbine Engine Oil SystemSDR UIEA200400001Manifold · malfunctionedHKB-DXB - NR 4 ENGINE OIL CONSUMPTION HIGH, QUANITY AT ZERO APPROXIMATELY 3 HOURS INTO FLIGHT. OIL PRESSURE LOW APPROXIMATELY 2 HOURS LATER. NR 4 ENGINE SHUTDOWN AT 1758Z, FL330, MACH .813. REPLACED OIL PRESSURE TRANSMITTER MANIFOLD. CARRIED OUT LEAK CHECKJan 8, 2004 · N412MC · Boeing 74747UF · Engine Oil PressureSDR UIEA200300023Blade · damagedREJECTED TAKEOFF, RUNWAY ABORT, ON TAKEOFF 2 LOUD BANGS/SHAKES AT 100 KIAS. EICAS MESSAG 'BRAKE TEMP'. TAKEOFF ABORTED AT APPROXIMATELY 100 KIAS. BRAKE TEMP EXCEEDED 900 DEGREES, PER FIRE DEPARTMENT. EXTINGUISHER AGENT SPRAYED ON LT MLG DUE TO BRAKE FIRE. Jun 15, 2003 · N412MC · Boeing 74747UF · Engine (Turbine/Turboprop)SDR UIEA200200065Compressor Wheel · failedREJECTED TAKEOFF, LOUD BANG HEARD AT 75 KNOTS ON TAKEOFF ROLL. REJECTED TAKEOFF AND RETURNED UNDER TOW. MAX THRUST WAS SET. AIRCRAFT POSITIONED TO HIGH POWER RUN BAY. ENGINE RUN RESULTS FAILED. NR 2 ENGINE BORESCOPE INSPECTION FOUND HPC STAGE 12 AND 13 FADec 2, 2002 · N412MC · Boeing 74747UF · Turbine Engine Compressor SectionSDR UIEA00048Stiffener · crackedAFTER UNLOADING CARGO, FOUND IN AFT CARGO COMPARTMENT, FORWARD BULKHEAD DAMAGE AT STATION 1480, RIGHT BL 50. DAMAGE WAS CONFINED TO THE AFT VERTICAL FLANGE OF THE HORIZONTAL STIFFENER AT WATER LINE 134.97 AND CRACKING ON STIFFENER AT WL 146.71 IN THE RADIUS AOct 20, 2000 · N412MC · Boeing 74747UF · Fuselage Miscellaneous Structure
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