N536MC

Service difficulty reports not matched to an aircraft · 28

They name N536MC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N536MC' AND registry_match IS NULL
  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 UIEA200600181Skin · crackedPYLON NR 4 ACCESS SKIN CUTOUT AT NAC STA. 273.09, PANEL 483AL, HAS A 0.750 INCH LONG CRACK AT UPPER FORWARD CORNER. ACCOMPLISHED SKIN PERMANENT REPAIR IAW SRM 54-31-03 FIG. 6.ALSO, REFERENCE EO 4754A231.Jul 20, 2006 · N536MC · Boeing 747228F · Nacelle/Pylon, Plate/SkinSDR UIEA200600179Brace · chafedNR 1 PYLON DIAGONAL BRACE HAS A CHAFED AREA ON OB SIDE ZONE 3A. ACCOMPLISHED BLENDOUT REPAIR AND FOUND WITHIN LIMITS IAW SRM 54-41-01 FIG. 3. PERFORMED FPI OF REWORKED AREA, NO DEFECTS FOUND IAW ASTM 1417-05. SHOT PEENED REWORKED AREA IAW SOPM 20-10-03. TREAJul 20, 2006 · N536MC · Boeing 747228F · Nacelle/Pylon Miscellaneous StructureSDR UIEA200600182Skin · delaminatedLT WING UPPER SURFACE LEADING EDGE PANEL AT OLES STA. 1336.0 AND 1495.0 HAS 2 EACH SMALL AREAS OF DELAMINATION. AREAS ARE BOTH 2.0 INCH BY 2.0 INCH. ACCOMPLISHED PREPREG 250 DEGREE PERMANENT HOT BOND REPAIR SRM 51-40-12 AND SRM 51-40-09 FIG. 18. ALSO, REFERENJul 20, 2006 · N536MC · Boeing 747228F · Wing, Plate/SkinSDR UIEA200600180Skin · crackedPYLON NR 4 ACCESS SKIN CUTOUT AT NAC STA 281.34, PANEL 483AL, HAS A 1.0 INCH LONG CRACK AT LOWER AFT CORNER. ACCOMPLISHED SKIN AND INNER DOUBLER PERMANENT REPAIR SRM 54-31-03 FIG. 6.ALSO, REFERENCE EO 4754A231.Jul 20, 2006 · N536MC · Boeing 747228F · Nacelle/Pylon, Plate/SkinSDR UIEA200600183Stiffener · crackedNOSE WHEEL WELL, LT SIDEWALL STIFFENER BETWEEN FUSELAGE STATION 320 LT AND 340 LT, WL 180, WAS FOUND WITH CRACK DURING HFEC INSPECTION. REMOVED AND REPLACED STIFFENER WITH A NEW STIFFENER EXTRUSION P/N BAC1517-1558 IAW SRM 51-40-04 FIG. 2 AND SRM 51-30-02.Jul 20, 2006 · N536MC · Boeing 747228F · Fuselage Miscellaneous StructureSDR UIEA200600119Compressor · stalledON TAKEOFF OUT OF DOV NR 2 ENGINE STALLED ABOUT 5 TIMES WITH REDUCTIONS IN N1, EGT AND N2. NO PARAMETERS WERE EXCEEDED. FLIGHT CONTINUED TO JFK WITHOUT SHUTDOWN. PERFORMED BOROSCOPE OF HPC. 1, 2, 3, 4 AND 7TH STAGES. DEFECTS NOTED, ENGINE TO BE REPLACED. May 23, 2006 · N536MC · Boeing 747228F · Turbine Engine Compressor SectionSDR UIEA200500079Shear Tie · crackedFRAME 440, RT SIDE BETWEEN STRINGERS 10A AND 11 TOP HOLE OF FRAME TO FUSELAGE SKIN ATTACHMENT ANGLE HAS .2500 INCH CRACK GOING UPWARD AND .0625 INCH CRACK GOING DOWNWARD. CUTOUT CRACKED SECTION OF ATTACHMENT ANGLE IAW SRM. ACCOMPLISHED HFEC INSP OF CUTOUT OFMay 24, 2005 · N536MC · Boeing 747271C · Fuselage Internal Mounting StructureSDR UIEA200500070Pan · crackedLT SIDE CANTED BULKHEAD AT BS 1245, LBL 60 CLOSURE PAN FOR AILERON CONTROL CABLE FEED THROUGH TO PRESSURE DECK FOUND WITH (2) CRACKED LINES. CLOSURE PAN REPAIRED IAW MFG MM. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Fuselage Miscellaneous StructureSDR UIEA200500069Skin · crackedNR 1 PYLON LT ACCESS DOOR 452BL CUT OUT LOWER EDGE CRACKED. REPAIRED ACCOMPLISHED IAW MFG MM. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Fuselage Main, Plate/SkinSDR UIEA200500068Frame · crackedNOSE WHEEL WELL STRUCTURE ON INTERIOR OF FUSELAGE CHORD CRACKED AT BS 340, WL 200, LBL 10. REPAIRED IAW MFG MM. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Fuselage Main, FrameSDR UIEA200500067Pressure Panel · corrodedBS 1408, LBL 78 WHEEL WELL PRESSURE DECK CORRODED AT FASTENERS LOCATIONS. PRESSURE DECK REPAIRED IAW MM. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Fuselage Main, BulkheadSDR UIEA200500066Precooler · crackedPYLONS NR1, 2, 3, AND 4, PRECOOLER EXHAUST CUT OUT LOWER EDGE CRACKED. REPAIRS ACCOMPLISHED IAW MM. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Pneumatic SystemSDR UIEA200500065Pylon · crackedLT WING NR 1 PYLON STRUT DOOR 453BL UPPER CORNER CRACKED. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Nacelle/Pylon, Plate/SkinSDR UIEA200500064Pylon · crackedNR 4 PYLON OB SKIN FOUND (2) CRACKS ON ACCESS DOOR 482AR CUTOUT CRACK 1INCH TO 1.5 INCH ON BOTH SKIN AND DOUBLER. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Nacelle/Pylon, Bulkhead/FirewallSDR UIEA200500063Bulkhead · crackedBS 400 BULKHEAD WEB CUT OUT FOR NOSE GEAR RETRACT ACTUATOR PAN FOUND BOTH LOWER CORNERS CRACKED. (K)Apr 26, 2005 · N536MC · Boeing 747228F · Fuselage Main, BulkheadSDR UIEA200400205Fairing · missingON WALK AROUND CHECK, FOUND LT AFT TIP FAIRING OF HORIZONTAL STABILIZER MISSING. EO ISSUED TO ACCOMPLISH TIME-LIMITED REPAIR WORK TO BE DONE PRIOR TO FURTHER FLIGHT. FABRICATED A TIME LIMITED REPLACEMENT FAIRING FROM 0.040 INCH THICK 2024-T3 CLAD SHEET. PERDec 27, 2004 · N536MC · Boeing 747228F · Horizontal Stabilizer, Plate/SkinSDR UIEA200400203Connector · looseNR 4 LEADING EDGE FLAP WOULD NOT RETRACT OR EXTEND NORMALLY OR ELECTRICALLY. JETTISONED 60.0 K FUEL. FOUND FORWARD CONNECTOR LOOSE ON L/E DRIVE UNIT. RESECURED CONNECTOR IAW MM. OPS CHECK OK, NORMAL. (K)Dec 21, 2004 · N536MC · Boeing 747228F · Leading Edge Slat Control SystemSDR UIEA200400150Seal · wornMXP-BOM - WITH NR 1 PACK ONLY ON OPERATION AT FL280 AND 310, CABIN ALTITUDE WILL CONTINUE TO CLIMB AT 10 TO 20 FPM. IN CRUISE WITH BOTH OUTFLOW VALVES FULL CLOSED AND DIFF PRESSURE DECREASING FROM 8.4 PSI WITH NO DROP IN DUCT PRESS, DUCT PRESSURE 42 PSI. AFTAug 24, 2004 · N536MC · Boeing 747228F · Air Distribution SystemSDR UIEA200400143Valve · malfunctionedMXP-ALA - AT 1741Z ON TAKEOFF ROLL AT APPROXIMATELY 120 KNOTS EXPERIENCED THE NR 4 ENGINE FIRE INDICATION. N1 SET AT 106.0. PERFORMED A REJECTED IAW THE FHB. ONCE STOPPED, THE ENGINE FIRE CHECKLIST WAS ACCOMPLISHED. JUST PRIOR TO ROLLING, NR 4 ENGINE FIRE Aug 7, 2004 · N536MC · Boeing 747228F · Engine Bleed Air SystemSDR UIEA200400122Valve · erraticNR 4 ENGINE SHUTDOWN DURING DECENT: NR 4 ENGINE SHUTDOWN RUMBLE AND EGT RISING. AFTER RISING RELIGHT IS STARTED SURGING. SHUTDOWN AGAIN. NR 4 HIGH STAGE VALVE DEACTIVATED, CLOSE AND PERFORMED ENGINE RUN UP, CHECK NORMAL, ENGINE RUN BY FLT CREW AND NR 4 ENGJul 12, 2004 · N536MC · Boeing 747228F · Pneumatic Distribution SystemSDR UIEA200400090Bleed Valve · malfunctionedDURING CLIMB-OUT, NR 2 ENGINE COMPRESSOR STALLED. NR 2 ENGINE SUSTAINED 6 OR MORE HARD COMPRESSOR STALLS WHILE CLIMBING THROUGH 18,000 FT TO 24,000 FT. INSPECTED INTAKE/EXHAUST AREAS, NIL DISCREPANCIES. CHIP DETECTORS CLEAN REMOVED AND REPLACED SAME 8TH STAMay 4, 2004 · N536MC · Boeing 747228F · Compressor Bleed ValveSDR UIEA200400089Engine · malfunctionedPRIOR TO TAKEOFF, DUE TO ANTI-ICE ON, STAT 'C' RUN AT 60 PERCENT. N1 WAS NORMAL. WITH BRAKE RELEASE, TAKEOFF THRUST SET, ROLLING DOWN RUNWAY 13, ASI BELOW 60 KNOTS, NR 3 ENGINE HAD 'BACKFIRED WITH A LOUD NOISE', WITH REDUCTION IN N1 RPM OF ABOUT 10-15 PERCENMay 4, 2004 · N536MC · Boeing 747228F · Engine (Turbine/Turboprop)SDR UIEA200400068Valve · inoperativeAZ9051 PVG/HKG NR 3 ENG BLEED OVERHEAT LIGHT CAME ON DURING TAKEOFF. FOLLOWED CHECKLIST IAW 3.36.5, NR 3 THRUST LEVER BACK TO IDLE LIGHT WILL EXTINGUISH. BUT LIGHT WILL COME BACK ON IF PUSH THRUST LEVER FORWARD MORE THAN 70 PERCENT N1. NR 3 THRUST LEVER USEDApr 22, 2004 · N536MC · Boeing 747228F · Pneumatic Distribution SystemSDR UIEA200400004Clamp · brokenLEFT WING OVERHEATED TWICE ON CLIMB-OUT AND THEN IN CRUISE. COMPLETED CHECKLIST TO ISOLATE LEFT WING WITH ONLY NR 2 ENGINE PYLON VALVES OFF, AND ISOLATION VALVE OPEN. FOLLOWING CLIMB FL320 TO FL350 WITH NR 1 AND NR 2 ENGINES BLEED VALVES CLOSED AND LEFT AND Jan 11, 2004 · N536MC · Boeing 747228F · Pneumatic Distribution SystemSDR UIEA200300072Control Cable · icedNR 3 ENGINE THROTTLE UNABLE TO SELECT IDLE DURING DESCENT. THROTTLE STUCK AT 4 DEGREE THROTTLE ANGLE AND 80 PERCENT N1. ENGINE SHUTDOWN USING ENGINE FAILURE/SHUTDOWN CHECKLIST. PERFORMED INSPECTION IAW 73-21-01 AND 76-11-03 THRUST CONTROL CABLE INSPECTED ALLDec 29, 2003 · N536MC · Boeing 747228F · Power LeverSDR UIEA200300015Clamp · looseNR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED & FIRE BELL ACTIVATED DURING CLIMB THROUGH 3000 FT. NR 1 ENGINE NACELLE TEMP INDICATES 'F' FOR BOTH 'A' AND 'B' LOOPS. ENG FIRE CHECKLIST ACCOMPLISHED. 80,000 KGS OF FUEL DUMPED. AFTER PULLING FIRE HANDLE LIGHT WMar 26, 2003 · N536MC · Boeing 747228F · Pneumatic Distribution SystemSDR UIEA9921Fire Warning · activatedFLT GT020 - FIRE WARNING BELL AND LIGHT SOUNDED ON FORWARD COCKPIT LIGHT FOR CARGO AREA, BUT WENT OUT TOO FAST TO CHECK F/E PANEL. CHECK CARGO AREA FIRE TEST AND INDICATION AND NO ABNORMALITIES NOTED. (M)Apr 14, 1999 · N536MC · Boeing 747228F · Fire DetectionSDR UIEA9916Frame · corrodedINSPECTION OF STA 1319 FRAME REVEALED CORROSION ABOVE THE LEFT HAND LONGERON BEAM. THE AREA WAS REPAIRED IAW ATLAS AIR EO 4753A085. (X)Apr 5, 1999 · N536MC · Boeing 747228F · Fuselage Main, Frame
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