N507MC

Service difficulty reports not matched to an aircraft · 19

They name N507MC, 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 = 'N507MC' 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 UIEA200200062Pressure Panel · crackedDURING CURRENT C-CHECK, FOUND FORWARD PRESSURE DECK SKIN CRACKED TWO PLACES STATION 140 AT RBL 34 AND RBL 43 NEAR WL 215. CRACK LENGTH WAS .025 INCH AT EACH LOCATION FROM EXISTING FASTENER HOLES. CRACKED AREAS TRIMMED AWAY. PERFORMED EC INSPECTION OF CUT OUNov 14, 2002 · N507MC · Boeing 747230B · Fuselage Main, BulkheadSDR UIEA200200030Window · inoperativeL1 WINDSHIELD LOWER AFT ELECTRICAL CONNECTION WAS PRODUCING SMOKE. SYSTEM TURNED OFF. SMOKE EV AC CHECKLIST COMPLETED. C/A: REPLACED L1 WINDOW PER MM 56-11-01 REPLACED LEFT WINDOW HEAT CONTROLLER PER MM. WINDOW HEAT CONTROLLER (PN 657154-5).Aug 13, 2002 · N507MC · Boeing 747230B · Windshield/Door Rain/Ice RemovalSDR UIEA01003Structure · corrodedDURING THE RECENT C-CHECK, THE UPPER CHORD AT BS 1840 WAS FOUND CORRODED BETWEEN LBL 75 AND 98 ON THE HORIZONTAL SURFACE AND EXTENDED DOWN ONTO THE VERTICAL SIDE. CORRODED SECTION WAS REMOVED, REPLACED AND REPAIR ANGLES WERE INSTALLED. REWORKED AREA EXTENDS Jan 25, 2001 · N507MC · Boeing 747230B · Fuselage Miscellaneous StructureSDR UIEA01002Skin · corrodedDURING THE RECENT C-CHECK, THE R/W EXTERNAL SKIN WAS CORRODED AT WS 320 COMMON TO STRINGER 15 AND WBL 179. CORROSION REMOVED, AREA BLENDED, TREATED AND REFINISHED IAW 57-30-01 FIG 2. (M)Jan 25, 2001 · N507MC · Boeing 747230B · Wing, Plate/SkinSDR UIEA01004Spar · corrodedDURING THE RECENT C-CHECK, THE REAR SPAR (OUTSIDE SURFACE) WAS FOUND CORRODED IN THE VICINITY OF THE NR 2 INBOARD FUELING VALVE MOUNT BOLT HOLES AT WS 562.50. FUELING EQUIPMENT AND MOUNT BOLT REMOVED. AREA REWORKED BY SPOT FACING CORRODED AREA, BLENDED, TREAJan 25, 2001 · N507MC · Boeing 747230B · Wing SparSDR UIEA01001Cylinder · corrodedDURING THE RECENT C-CHECK, THE LEFT OUTER CYLINDER SPUD BOSS WAS FOUND CORRODED IN THE AREA OF CHROME LOSS. AREA CLEANED OF CORROSION, TREATED, CHECKED FOR HEAT RELATED DAMAGE. REWORK AREA IS 5MM IN DIAMETER WITH MISSING CHROME AND MATERIAL LOSS OF .4 MM AFTJan 25, 2001 · N507MC · Boeing 747230B · Main Landing Gear Strut/Axle/TruckSDR UIEA99056Frame · dentedFRAME DENTED AT STA 1840 RT TWO PLACES, FIRST BETWEEN STR 12 AND STR 13, SECOND BETWEEN STR 10 AND STR 11. FRAME REPAIRED BETWEEN STR 12/13 PER SRM 53-10-04 FIG 87. FRAME REPAIRED BETWEEN STR 10/11 PER ACC KLM DFX 99-127 REV 2. (X)Jul 16, 1999 · N507MC · Boeing 747230B · Fuselage Main, FrameSDR UIEA99055Structure · crackedBULK CARGO DOOR SKIN, DOUBLER AND TRIPLER CRACKED ON BOTTOM OF CUT-OUT AT BS 1980 RT BETWEEN STR 37 AND STR 38. CRACK IS HORIZONTAL AND MEASURES 0.500 INCHES. CRACK REPAIRED PER ACC KLM DFX 99-120. FORM 8110-3 ISSUED. (X)Jul 16, 1999 · N507MC · Boeing 747230B · Fuselage Main, StructureSDR UIEA99054Frame Web · crackedBS 1265 HFEC INSPECTION PERFORMED ON LT NR 3 MAIN ENTRY DOOR FRAME. UNDER FLOOR, LINE FOUND CRACK INDICATION IN WEB. INTERIM REPAIR ACCOMPLISHED PER ACC KLM DFX 99-119 REV 2. RE-INSPECT AT 2,000 CYCLE INTERVALS. FORM 8110-3 ISSUED. (X)Jul 16, 1999 · N507MC · Boeing 747230B · Fuselage Main, FrameSDR UIEA99053Spar Web · corrodedLEFT WING GEAR WHEEL, SPOT CORROSION FOUND ON CENTER TANK REAR SPAR WEB BEHIND THE BS 1241 LT BULKHEAD FITTING. REF: AD 98-26-23 AND SB 747-57-2263R2. CORROSION REMOVED IAW SB 747-57 2263 REV R2 AND FAX KLM TLS 99-0008H. FORM 8110-3 ISSUED.Jul 16, 1999 · N507MC · Boeing 747230B · Wing SparSDR UIEA99052Frame · crackedBS 520 LT, FOUND CRACK IN FUSELAGE FRAME FLANGE BETWEEN STR 9 AND STR 11. ALSO, SHEAR DOUBLER CRACKED IN CUT-OUT TO NEAREST FASTENER HOLE DURING SECTION 41 INSPECTION. REPAIRED STR 9 PER SRM 53-10-04, FIG 85. REPAIRED FRAME AT STR 10 PER ACC KLM DFX 99-126 Jul 16, 1999 · N507MC · Boeing 747230B · Fuselage Main, FrameSDR UIEA99051Frame · crackedBS 520 RT, FOUND CRACK IN FUSELAGE FRAME AT STR 11 DURING SECTION 41 INSPECTION. CRACK RUNS FROM CUT-OUT TO NEAREST FASTENER HOLE. REPAIRED FRAME PER ACC KLM DFX 99-124 REV 2. FORM 8110-3 ISSUED. (X)Jul 16, 1999 · N507MC · Boeing 747230B · Fuselage Main, FrameSDR UIEA99050Frame · crackedBS 420 LT, FOUND CRACK IN FUSELAGE FRAME AT STR 14E DURING SECT 41 INSPECTION. CRACK RUNS FROM STRINGER CUT-OUT TO INBOARD. REPAIRED FRAME WEB PER ACC KLM DFX 99-134 REV 2, FORM 8110-3. (X)Jul 16, 1999 · N507MC · Boeing 747230B · Fuselage Main, FrameSDR UIEA99049Frame · crackedBS 380 LT, FOUND TWO CRACKS IN FUSELAGE FRAME AT STR 23 DURING SECTION 41 INSPECTION. CRACK RUNS FROM STRINGER CUT-OUT TO NEAREST FASTENER HOLE, THE OTHER TO THE SKIN FLANGE. REPAIRED FRAME WEB, PER KLM DFX 99-132 REV 2, FORM 8110-3 ISSUED. (X)Jul 16, 1999 · N507MC · Boeing 747230B · Fuselage Main, FrameSDR UIEA99048Frame · crackedBS 360 LT, FOUND CRACK IN FUSELAGE (MID) FRAME AT STR 14E DURING SECTION 41 INSPECTION. CRACK RUNS FROM CUT-OUT TO NEAREST FASTENER HOLE BELOW FORMED CHORD. REPAIRED FRAME PER ACC KLM DFX 99-133 REV 1. FORM 8110-3 ISSUED. (X)Jul 16, 1999 · N507MC · Boeing 747230B · Fuselage Main, FrameSDR UIEA9925Rivet · failedFLT NR IB9709 - VCP/EZE - ATB - AT 10,000 FEET DISCOVERED AIRCRAFT UNABLE TO PRESSURIZE. ALL DOOR LIGHTS EXTINGUISHED AND SUFFICIENT AIRFLOW IN THE AIRCRAFT. USE FHB PROCEDURE AND INSPECTED AS MUCH OF AIRCRAFT AS POSSIBLE TO DETERMINE NO HOLES AND PRESSURIZAMay 8, 1999 · N507MC · Boeing 747230B · Cargo/Baggage DoorsSDR UIEA9917Battery Charger · failedFLT 9603 - BTB - DURING TAXI APU BATTERY CHARGER SPARKED TWICE, THEN STARTED, FILLING THE MAIN CABIN WITH SMOKE UNTIL C/B POPPED. AIRCRAFT RETURNED TO GATE. FOUND APU BATTERY CHARGER DEFETIVE. REPLACED APU BATTERY CHARGER, OPERATIONAL CHECK NORMAL. (M)May 8, 1999 · N507MC · Boeing 747230B · Battery/Charger SystemSDR UIEA9611Clamp · looseATB - FLT EX9880 -DXB/DXB - NR 4 ENGINE, BOTH NACELLE TEMP INDICATORS INDICATED 8.4 ON SCALE AT CLIMB POWER CLOSED BLEED VALVE NO CHANGE. REDUCED THROTTLE TO IDLE, INDICATIONS DROPPED TO 2-2.5, SAME AS NR 1, NR 2, NR 3 ENGINE. AT HIGHER POWER INDICATIONS FOLOct 2, 1996 · N507MC · Boeing 747230B · Pneumatic Distribution SystemSDR UIEA9504Shut-Off Valve · failedON LEVEL OFF FROM A CLIMB TO F350, THE NR 4 ENGINE FLAMED OUT FOR NO APPARENT REASON. AIRCRAFT DIVERTED INTO JFK. FOUND NR 4 ENGINE FUEL SHUT OFF VALVE FAILED. REPLACED FUEL SHUT OFF VALVE ACTUATOR PER MM 76-11-04. OPS AND RUN-UP OK. ENGINE INLET, TAIL PIAug 27, 1995 · N507MC · Boeing 747230B · Engine Fuel Distribution
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