N523MC, cancelled Feb 14, 2018

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 = 'N523MC' AND deregistration_id = 'N523MC-2018-02-14'
  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 UIEA2011091300511Frame · crackedBS 400, S23R FRAME CRACKED. CRACK AREA STOP DRILLED AND REPAIRED IAW HX RS R53-12-37208, REV A.Sep 13, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011091300508Reveal · crackedBS 2231 S17L REVEAL PANEL CRACK APPRX 0.625" LONG. REVEAL PANEL CRACK REPAIR CARRIED OUT IAW HX RSNO 53-60-37210, REV A. WORK DETAILS REF TO NRC 51169.Sep 13, 2011 · N523MC · Boeing 7472D7B · Fuselage Miscellaneous StructureSDR UIEA2011091300503Frame · crackedBS 2598 BULKHEAD OUTER CHORD AREA WL 274, 1 FASTENER HOLE CRACKED AT FRAME SUPPORT FIG (LT BS 2598, BULKHEAD OUTER CHORD WL 274 CRACKED FASTENER HOLE REPAIRED IAW HX RS 53-13-37213, REV A.)Sep 13, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011091300501Light · inoperativeZONE A RT 1 EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED AND LIGHT TESTED AND FOUND OK, REF AMM 33-51-07.Sep 13, 2011 · N523MC · Boeing 7472D7B · Emergency LightingSDR UIEA2011091300500Frame · crackedBS 1254 FRAME INNER CHORD FASTENER HOLE CRACK 0.040 IN LENGTH. CRACKED SEGMENT CUT OFF AND REPAIRED IAW HX RS R53-42-37204, REV A AND EO 4753B419, PART 1.Sep 13, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011091300499Light · inoperativeL5 DOOR 1EA EMERGENCY LIGHT FOUND INOP. L5 DOOR EMERGENCY LIGHT ASSY REPLACED, HOLD TEST OK MM 33-51-07.Sep 13, 2011 · N523MC · Boeing 7472D7B · Emergency LightingSDR UIEA2011091300498Frame · crackedFRAME BS 2231 BETWEEN S24-25L, 1 EA FASTENER HOLE CRACK APPROX 0.040 LONG AT FRAME STRAP. REPAIRED IAW HX RS R53-62-27215, REV A. REPAIR WORK DETAILS REF TO NRC 51276.Sep 13, 2011 · N523MC · Boeing 7472D7B · Fuselage Structure (General)SDR UIEA2011091300497Reveal · crackedBS 2231, BETWEEN S21-22L FOUND 2 EA FASTENER HOLES CRACK AT REVEAL PANEL. CRACKED AREA STOP HOLE DRILLED AND REPAIR CARRIED OUT IAW HX RS R53-62-37215, REV A.Sep 13, 2011 · N523MC · Boeing 7472D7B · Fuselage Miscellaneous StructureSDR UIEA2011091300496Frame · crackedBS 2231, S26R FRAME AFT INNER CHORD CRACK APPROX 1" LONG ON VERT FLANGE. CRACKED AREA TRIMMED OFF AND REPARIED IAW HX RS R53-62-37218, REV A.Sep 13, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011091300495Frame · crackedBS 2231, S26R, FRAME WEB CRACK APPROX 1" LONG ON FWD INNER CHORD VERT FLANGE. CRACK AREA TRIMMER OFF AND REPAIRED IAW HX RS R53-62=37218, REV A AND WORK DETAILS REF TO NRC NO 50399.Sep 13, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011090900487Skin · crackedINSPECTION DETECTED 2 CRACKS (APPROX 0.030" LONG) ON THE SKIN AT RT BS 980, S38R. REPAIRED IAW SRM 53-30-03, FIG 60.Sep 9, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2011090900486Spar · damagedCRACK DAMAGE WAS DETECTED AND RAN FORWARD TO AFT AND WAS APPROX 4.5 INCHES LONG. WEB WAS CUT AT APPROX NAC STA 286 AND THE SECTION OF THE WEB FROM NAC STA 286.00 TO NAC STA 312.34 WAS REMOVED FROM THE SPAR ASSY. WEB SECTION FABRICATED AND INSTALLED ONTO THSep 9, 2011 · N523MC · Boeing 7472D7B · Nacelle/Pylon, Frame/Spar/RibSDR UIEA2011090900490Channel · crackedDURING INSPECTION IAW EO 4753B328, A FASTENER HOLE CRACK WAS FOUND AT TENSION TIE FWD CHANNEL AT BS 920 LT. CRACK LENGTH WAS 0.125" AND RUNNING OTBD AT 6 O'CLOCK. THE DAMAGED TENSION TIE WAS REPAIRED IAW WORK STEP 29 D OF PART 1 OF EO 4753B328.Sep 1, 2011 · N523MC · Boeing 7472D7B · Fuselage Miscellaneous StructureSDR UIEA2011091300510Frame · crackedLT BS 1265 FRAME WEB CRACKED AT FASTENER HOLE. CRACKED AREA TRIMMED OFF AND REPAIRED IAW HX RS R53-42--37204, REV A AND EO 4753B419, PART 1.Aug 31, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011090900482Rib · damagedDURING THE PRESENT C4 CHECK, NR 2 PYLON LT NAC STA 332 FRAME RIB WAS FOUND WITH A WEAR AROUND MOUNT BOLT HOLE, APPROX 0.035 INCH MATERIAL REMOVED. THE ORIGINAL THICKNESS OF THE RIB WAS REPORTED AT 0.080 INCH.Aug 31, 2011 · N523MC · Boeing 7472D7B · Nacelle/Pylon, Frame/Spar/RibSDR UIEA2011091300504Reveal · crackedREVEAL PANEL BS 2231 BETWEEN S24-25L CRACKED APPROX 0.500: LONG. CRACKED AREA TRIMMED OFF AND REPAIRED IAW HXRS R53-62-37215, REV A.Aug 30, 2011 · N523MC · Boeing 7472D7B · Fuselage Miscellaneous StructureSDR UIEA2011091300509Frame · crackedFRAME BS 2231 BETWEEN S16-17L, FASTENER HOLE CRACK APPROX 0.040 AT FRAME STRAP. CRACKED SEGMENT CUT OFF AND REPAIRED IAW HX RS R53-60-37210, REV A. )Aug 30, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011090200479Fairing · brokenENGINE EXHAUST -NR 2 ENGINE RT UPPER INNER FAIRING REPLACEMENT - DURING THE CURRENT C-CHECK, THE UPPER INNER FAIRING WAS FOUND BROKEN (PARTIAL MISSING) AT FWD SECTION. A REPLACEMENT UPPER INNER FAIRING (PN: 9059M49P002C) HAS BEEN ORDER FOR REPLACEMENT IAW EMAug 30, 2011 · N523MC · Boeing 7472D7B · Engine Thrust ReverserSDR UIEA2011091300507Frame · crackedFRAME BS 2231 BETWEEN S24-25L, 1 FASTENER HOLE CRACK AT FRAME AFT INNER CHORD APPROX 0.040: LONG. CRACK AREA TRIMMED OFF AND REPAIR CARRIED OUT IAW HVRX R53-62-37215, REV A.Aug 29, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011091300506Frame · crackedBS 2231 S26L FRAME AFT INNER CHORD CRACK APPROX .5" LONG AT VENT FLANGE. CRACK AREA TRIMMED OFF AND REPAIRED IAW HXRSNC-R53--62-37206 REV A.Aug 29, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011091300505Frame · crackedBS 2231 FRAME S26R FWD INNER CHORD CRACK APPROX 0.025" LONG ON VENT HANG. CRACK TRIMMED OFF AND REPAIRED IAW HXRS 53-62-47218, REV A.Aug 29, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011090900488Frame · crackedDURING C4 CHECK, DETECTED A CRACK ON THE RT SIDE, BS 360 FRAME THE CRACK IS LOCATED ON THE WEB LAYER ONLY AND IS APPROX 1 INCH LONG RUNNING OTBD AND DOWNWARDS. WHILE PERFORMING REPAIR, ADDITIONAL 2 EA CRACKS WERE DETECTED ON BS 360 FRAME. ONE OF THE CRACKS Aug 26, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011082600468Seat Track · corrodedBS 550-560, RBL 46 SEAT TRACK CORRODED.Aug 26, 2011 · N523MC · Boeing 7472D7B · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2011091300502Skin · damagedEXTERNAL POWER RECEPTACLES ACCESS DOOR CUTOUT FOUND DAMAGED. CRACK TRIMMED OFF AND REPAIRED IAW HX RS R53-11-27121, REV A.Aug 25, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2011082500470Stringer · crackedBS 988, STRINGER 16L CRACKED.Aug 25, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, Longeron/StringerSDR UIEA2011090900480Frame · crackedDISCOVERED A CRACK IN THE FRAME AT BS 360 AND S16R. REPAIR IS CLASSIFIED AS A CATAGORY B PERMANENT REPAIR WITH REPEAT INSPECTION REQUIREMENTS IAW SB 747-53A2265, REV 9.Aug 24, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011082400466Frame · crackedBS 820, S6R FRAME CRACKED, REPAIR ACCOMPLISHED DURING A C4 CHECK ON NRC 505315 IAW SRM 53-10-04, FIGURE 54.Aug 24, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011082400465Frame · crackedBS820, S6L FRAME CRACKED, REPAIR ACCOMPLISHED DURING A C4 CHECK ON NRC 505323 IAW SRM 53-10-04, FIGURE 54.Aug 24, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011090900481Frame · crackedDURING C4 CHECK, WHILE COMPLYING WITH SB 747-53A2265, REV 9, FOUND CRACK DAMAGE TO FRAME. DAMAGE WAS REPAIRED IAW SRM 53-10-04 FIG 11.Aug 22, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011082200462Frame · crackedBS 580, S24L FRAME CRACKED, REPAIRED IAW SRM 53-10-04, FIG 35.Aug 22, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011082200460Frame · crackedFUSELAGE - BS540, S24L-S25L FRAME CRACK - REPAIR (THIS EO DOCUMENTS A REPAIR ACCOMPLISHED DURING A C4 CHECK OF THE DATUM ACFT ON NRC 502668 IAW SRM 53-10-04, FIG 35. THE SRM REPAIR IS CLASSIFIED AS A CATAGORY B, WITH AN INITIAL INSP THRESHOLD OF 20,000 TFC ANAug 22, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011082200459Frame · crackedBS 560, S24-S25L FRAME CRACKED. REPAIRED IAW SRM 53-10-04, FIG 35.Aug 22, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011091300494Channel · crackedRIGHT BS 840 FRAME TO TENSION TIE ATTACHMENT AREA FOUND 1 EA FASTENER HOLE CRACKED AT FWD CHANNEL CRACK APPROX .1250" IN LENGTH. REPAIR CARRIED OUT IAW HX RS NR R53-25-37200, REV 8.Aug 21, 2011 · N523MC · Boeing 7472D7B · Fuselage Miscellaneous StructureSDR UIEA2011090900485Floorbeam · puncturedDURING ROUTINE INSPECTIONS A 1.0 INCH X 0.5 INCH PUNCTURE WAS FOUND IN THE SUBJECT FLOORBEAM WEB AT BS 280, WL 200. THE PUNCTURE WAS REPAIRED BY ACCOMPLISHING A TYPICAL FLOORBEAM WEB REPAIR IAW SRM 53-10-07, FIG 11.Aug 18, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, Floor BeamSDR UIEA2011090900484Frame · crackedDURING C4 CHECK. ACCOMPLISHMENT OF SB 747- 53A2416, REV 2 INSPECTIONS (2) 0.040" CRACKS WERE FOUND IN FRAME . 2 ADDITIONAL 0.50" CRACKS WERE FOUND IN THE WEB. REPAIRED BY TRIMMING OUT THE CRITICAL FASTENER HOLE IAW 624U0060, SHEET 5 AND REPAIRED IAW THE INTAug 17, 2011 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011073100400Fuel Filter · failedDURING CRUISE, NR 2 ENG ROLLED BACK TO IDLE. NO RESPONSE TO THROTTLE MOVEMENTS. APPROX 5 SEC LATER OIL PRESS DROPPED TO ZERO QTY OK. TROUBLESHOT IAW MM FIM 71-00-42 CHECKED CDP TUBES, POWER LEVER CABLE, CHIP DETECTORS, FUEL FILTER- N.T.F PERFORMED VSV-VBV RJul 31, 2011 · N523MC · Boeing 7472D7B · Fuel Controlling SystemSDR UIEA2011073100388Structure · crackedDURING WALK AROUND CHECK, MX FOUND 2EA CRACKS AT 7 O'CLOCK POSITION ON THE AFT CENTER BODY ON THE NR 2 ENGINE. 1EA CRACK MEASURING 1.25 INCHES AND 1EA CRACK MEASURING APPROX 1 INCH REF FIGURE 1. DISPOSITION WAS MADE TO STOP DRILL THE CRACKS USING STANDARD PRJul 31, 2011 · N523MC · Boeing 7472D7B · Engine Exhaust SystemSDR UIEA2011060800288Light · unknown1ST OBSERVER'S SEAT MAP LIGHT. TRANSFERRED & NBSP; TO MDDR 24530. CAT C MEL NR 33-1.Jun 8, 2011 · N523MC · Boeing 7472D7B · Flight Compartment LightingSDR UIEA2011053000268Sleeve · damagedDURING WALK AROUND CHECK, MX FOUND A HOLE 0.5" WIDE ON THE OUTER SLEEVE OF THE LONG FIXED CORE EXHAUST NOZZLE (LFCEN) ON THE NR 2 ENGINE. THE HOLE IS 6.0" FROM THE EXHAUST SLEEVE T/E AT THE 11:00 O' CLOCK POSITION. (DISPOSITION WAS MADE TO REMOVE ANY BURRS UMay 30, 2011 · N523MC · Boeing 7472D7B · Engine Collector/Tailpipe/NozzleSDR UIEA2011041800313Bulb · inoperativeM/D DOOR SILL AFT EMERGENCY LIGHT FOUND INOPERATIVE. BULB REPLACED AND CHECK 'OK' REF AMM 33-51-00.Apr 18, 2011 · N523MC · Boeing 7472D7B · Emergency LightingSDR UIEA2011040800244Door · dentedDURING MX WALKAROUND, MX FOUND DENT ON THE NR 1 ENGINE OIL SERVICE DOOR. MX ACCOMPLISHED PART 2, EO 1971A027, AND INSTALLED A BLANKING PLATE. EO 1971A027 ALLOWS THE BLANKING PLATE TO BE INSTALLED FOR UP TO 10FC. DUE TO LACK OF PART AVAILABILITY, DOOR REPLACEMApr 8, 2011 · N523MC · Boeing 7472D7B · Nacelle/Pylon, Main FrameSDR UIEA2011032800159Unknown · unknownTAKEOFF REJECTED AT 90 KNOTS, WHEN YAW TO THE LT WAS FELT. INSPECTED NR 1 AND NR 2 ENGINES, NO DEFECTS NOTED, PERFORMED HIGH ENERGY STOP INSP, NO DEFECTS NOTED. PERFORMED CHECK OF BRAKES ON LT HAND BODY GEAR, AND LOCKED OUT NR 7 BRAKE DUE TO OVERHEAT CONDITIOMar 28, 2011 · N523MC · Boeing 7472D7B · Landing Gear SystemSDR UIEA2011032200155Accumulator · leakingCREW REPORTED HYD LEAK ON THE NR 4 SYS (FOUND BRAKE ACCUMULATOR LEAKING. R & R ACCUMULATOR, SERVICED SYSTEM, PERFORMED OPERATIONAL AND LEAK CHECKS, ALL; OK.)Mar 22, 2011 · N523MC · Boeing 7472D7B · Hydraulic System, MainSDR UIEA2011020500092Duct · damagedENGINE NR 2 OUTBOARD T/R HALF HI BYPASS "C" DUCT INTERNAL WALL WITH DELAMINATION AND MISSING SKIN MATERIAL(REMOVED SECTION OF DAMAGED SKIN AND PREPARED AREA FABRICATED DOUBLER FROM 2024-T3 0.063 PO 10024219 LOCATED, TRIMMED, DRILLED, PRIMED AND INSTALLED AND SFeb 5, 2011 · N523MC · Boeing 7472D7B · Engine (Turbine/Turboprop)SDR UIEA2011020500046Skin · damagedMAJOR REPAIR. DURING A-CHECK BEING PERFORMED, MX FOUND THE LT WING ILES 718.80; UPPER L/E PANEL - EXTERNAL SKIN WITH CRACK/DELAMINATION DAMAGE , MEASURING 24.0 INCHES LONG, LOCATED 4.5 INCHES FROM THE AFT END OF THE L/E PANEL. REF FIG 1. PERMANENT REPAIR PEFeb 5, 2011 · N523MC · Boeing 7472D7B · Wing, Plate/SkinSDR UIEA2010082600147Mount · damagedTHE PURPOSE OF EO 4725A284 IS TO DOCUMENT A MAJOR REPAIR. DURING WALKAROUND INSP, MX FOUND THE ELECTRICAL CONDUIT AND CONNECTOR MOUNT HSG AT THE NLG DAMAGED. REPAIRED IAW EO 4725A284&NBSP.Aug 26, 2010 · N523MC · Boeing 7472D7B · Fuselage Miscellaneous StructureSDR UIEA2010080900148Actuator · brokenBODY GEAR UNLOCKED LIGHT ILLUMINATED IN BOTH PRIMARY AND ALTERNATE POSITIONS WHEN LINED UP FOR TAKEOFF (FOUND RT BODY GEAR STEERING ACTUATOR BROKEN. R & R BODY GEAR STEERING ACTUATOR IAW MM 32-53-11, OPS CHECK OK)Aug 9, 2010 · N523MC · Boeing 7472D7B · Landing Gear Steering SystemSDR UIEA2010080500132Skin · damagedDURING WALKAROUND INSP, MX FOUND DAMAGE TO THE NR 2 ENG INLET COWL OUTER BARREL SKIN CRACK/DAMAGE (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS; SCHEDULE REPEAT INSPECTIONS AT EVERY 25 FC AND PERMAug 5, 2010 · N523MC · Boeing 7472D7B · Engine Air Intake SystemSDR UIEA2010072700119A/C Pack · inoperativeATB, ELECTRICAL SMOKE SMELL IN COCKPIT. RAN ELECTRICAL SMOKE CHECKLIST, WHEN STEP 6 ACCOMPLISHED, SMOKE DISSIPATED (IAW VERBAL CREW COMMENT, DURING CLIMB, WITH NR 1 PACK ON IS WHEN THE ELECTRICAL SMOKE SMELL WAS NOTICED. UPON INSPECTION OF NR1 ACM, FOUND INOPJul 27, 2010 · N523MC · Boeing 7472D7B · Cabin Cooling SystemSDR UIEA2010070600092Floor Support · crackedDURING C-CHECK, A SUPPORT LOCATED COMMON TO THE AFT CARGO FLOOR FROM BS 1900 TO BS 1920 FROM RBL 17- RBL 23 WAS BENT AND HAD 2 ELONGATED HOLES. (THE DAMAGE WAS TRIMMED OUT AND PERMANENTLY REPAIRED IAW SRM 51-40-02, FIG 2 AS DOCUMENTED ON NRC497. THE SUPPORT IJul 6, 2010 · N523MC · Boeing 7472D7B · Fuselage Miscellaneous Structure
Back to N523MC, cancelled Feb 14, 2018