N496MC
Service difficulty reports · 195
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 = 'N496MC' 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 = 'N496MC' 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 UIEA200900027Fan · failedON "TAXI IN" THERE WAS AN ODOR OF ELECTRICAL BURNING IN THE COCKPIT. ALSO, E/E COOLING FAN STATUS MESSAGE. FOUND E/E FAN FAILED AND DEFERRED FAN PER MEL 21-58-4. ALSO, PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-56. NO FURTHER TROUBLE FOUND. NO PARTS CSDR UIEA201000117Skin · damagedTHE PURPOSE OF THIS EO IS TO RECORD A MAJOR REPAIR. DURING C-CHECK INSP; DAMAGE WAS FOUND TO THE RT INBD AILERON UPPER SURFACE OTBD T/E CORNER MEASURING 0.5 IN. X 1.0 IN. (REF FIG 1). PERMANENT REPAIR PERFORMED IAW THE SRM 51-70-06 FIG 5.1. ACCOMPLISH REPAISDR UIEA201000116Skin · delaminatedACCOMPLISH REPAIR TO THE LT INBD AFT FLAP, LOWER SURFACE INBD FWD AREA OF DELAMINATION IAW SRM 57-53-01 FIG 201,SRM 51-70-07 (REF FIG 1). ACCOMPLISH REPAIR TO THE RT INBD FORE FLAP, INBD T/E LOWER SURFACE DAMAGE IAW SRM 57-53-01, FIG 201, RPR 1 TABLE I AND THESDR UIEA200900006Warning System · false activationCREW REPORTED EQUIPMENT SMOKE STATUS MESSAGE DISPLAYED AFTER LANDING. EXISTING FAULTS REVIEWED , NO RELATED FAULTS NOTED. EQUIPMENT TEST WITH NO FAULTS RESULTS. ACFT WAS RELEASED WITH NO FURTHER MESSAGES.SDR UIE2008F00004Panel · puncturedAFT CARGO COMPARTMENT TORQUE BOX TOP PANEL AT STA 1660 TO 1680 RT SIDE FOUND PUNCTURED AT 2 LOCATIONS. TORQUE BOX TOP PANEL REPAIRED IAW EO. (K)SDR UIEA200700470Support Beam · crackedMAIN DECK CARGO SIDE DOOR AREA, SUPPORT BEAM BETWEEN STA 1820-1840 AND 1840-1860 LBL 102.250, CRACKED AND DENTED. PERMANENT REPAIR ACCOMPLISHED AS PER ATLAS AIR XEO 53-110607, BOEING DRAWING 65B17951 AND FAA FORM 8100-9.SDR UIEA200700469Seat Track · crackedMAIN DECK CARGO SIDE DOOR AREA, SEAT TRACK DAMAGED AND CRACKED AT STA 1850 AND 1920, LBL 99.0. PERMANENT REPAIR ACCOMPLISHED AS PER B747-400 SRM 53-00-52 FIG 201, REPAIR 6. REFERENCE ATLAS AIR XEO NR 53-110607.SDR UIEA200700468Structure · erodedNR 2 ENGINE LT FAN COWL L/E HAS 78.0 INCH AREA OF EROSION AT L/E. PERMANENT REPAIR ACCOMPLISHED AS PER B747-400 SRM 54-21-01, REPAIR 6. REFERENCE ATLAS EO NR 4471A009.SDR UIEA200700392Cowl Fastener · migratedNR 1 ENGINE REVERSER RIGHT SIDE TRANSLATING COWL OUTER SKIN FORWARD SECTION SEVERAL RIVETS MIGRATED. REMOVED AND REPLACED LOOSE AND MIGRATED RIVETS IAW SRM 51-40-02.SDR UIEA200700388Blowout Panel · brokenNR 1 ENGINE REVERSER LEFT SIDE LOWER FORWARD SECTION FORWARD END OF BLOW OUT PANEL SIDE SUPPORT BRACKET SECTION DAMAGED. REMOVED BROKEN RIVETS AND REPLACED WITH NEW RIVETS IAW SRM 51-40-02.SDR UIEA200700387Skin · delaminatedRIGHT WING OUTBOARD FORE FLAP HAS DELAMINATION FROM WBL 804-WBL 817. REPAIRED RIGHT OUTBOARD FOREFLAP LEADING EDGE AT WBL 804 TO WBL 817 IAW SRM 51-70-07 AND ATLAS XEO 57-091507.SDR UIEA200700391Access Panel · damagedNR 1 ENGINE REVERSER RIGHT SIDE LOWER AFT SECTION TENSION LATCH ACCESS PANEL SEVERAL RIVETS MIGRATED. REMOVED AND REPLACED MIGRATED RIVETS IAW SRM 51-40-02.SDR UIEA200700390Skin Panel · dentedNR 1 ENGINE REVERSER RIGHT SIDE THRUST REVERSER FIXED AFT SECTION BEAVER TAIL OUTER SKIN PANEL DENTED. REWORKED DENTED AREA IAW SRM 51-70-01.SDR UIEA200700389Cowl Fastener · damagedNR 1 ENGINE REVERSER LEFT SIDE TRANSLATING COWL FWD SECTION LOWER HALF HAS SEVERAL RIVETS MIGRATED. REMOVED AND REPLACED LOOSE AND MIGRATED RIVETS IAW SRM 51-40-02.SDR UIEA200700215Fan · odorELECTRICAL ODOR IN THE COCKPIT. T/S FOUND E/E COOLING SUPPLY FAN FAILED CAUSING ODOR. DEACTIVATED E/E COOLING SUPPLY FAN IAW DDPG 21-28-06 AS PER MAINTENANCE ACTION PERFORMED.SDR P5CA0701519Unknown · unknownAFTER BLOCK OUT, MAIN TANK NR 2 FWD OVERRIDE/JETTISON PUMP FAIL STATUS MESSAGE DISPLAYED. OPENED MEL 28-31-2C, COMPLIED WITH DDG.SDR P5CA0701518Structure · chafedAFT LWR CARGO DOOR LWR FWD CORNER MINOR CHAFING V-SHAPE .125 INCH. INTERIM REPAIR FROM ENGINEERING PER DER-ISSUED FAA 8110-3.SDR P5CA0701515Unknown · unknownAT PUSHBACK OFF BLOCKS, RECEIVED STATUS MESSAGE FUEL OVRD 2 FWD. DEFER PER MEL 28-31-2.SDR UIEA200700141Seat Track · crackedLOWER AFT CARGO COMPARTMENT SEAT TRACK CRACKED STA 1905-1920, RBL 45. SEAT TRACK REPLACED AS PER SRM 53-00-52.SDR UIEA200700140Seat Track · crackedLOWER AFT CARGO COMPARTMENT SEAT TRACK BETWEEN STA 1905-1920, RBL 25 CRACKED. SEAT TRACK REPLACED AS PER SRM 53-00-52.SDR P5CA0601507Warning Message · illuminatedCREW REPORTED "ANTI-SKID" EICAS MESSAGE DISPLAYED AT ENGINE START. OPENED MEL NR S 32-42-1-1, 32-41-1-A, AND 32-42-4-1A.SDR P5CA0601506Pdu · inoperativeLE SINGLE DRIVE STATUS MSG NR 3 LED INOP PNEUMATICALLY. REPLACED LE PDU.SDR UIEA200600210Shim · migratedC-4 & A-4 CHECK AT PIK., FWD CARGO DOOR FWD ACTUATOR ARM FITTING HAS MIGRATING SHIMS. AFT CARGO DOOR AFT ACTUATOR ARM FITTING HAS MIGRATING SHIMS. ENGG HAS GENERATED XEO 53-081406 PART-1 OF XEO 53-081406 HAS ALREADY ACCOMPLISHED DURING C-CHECK AT PIK ON 15THSDR UIEA200600209Shim · migratedC-4 & A-4 CHECK AT PIK. AFT PIT DOOR HINGE SEGMENTS 1 THRU 12 HAVE MIGRATING SHIMS. AS PER BOEING MESSAGE 1-218612791-2 DATED 11TH AUG 2006, XEO 52-081106 GENERATED. PART-1 ACCOMPLISHED DURING C-CHECK AT PIK. PART-2 WILL BE ACCOMPLISHED (DVI) EVERY 2A CHECSDR UIEA200600206Skin · damagedN496MC AT PIK FOR MSG C-4 & A-4 CHECK. AS PER N/R 39, ON INDUCTION OF A/C FOUND LT I/B T/E FORE FLAP LEADING EDGE DAMAGED, I/B OF NR 3 CANOE. OFF S/N 000532. RECT:LT, I/B T/E FORE FLAP REPLACED AS PER AMM 27-51-02. ON P/N 65B39011-93C & ON S/N 000492.SDR UIEA200600116Seat Track · tornMAIN DECK SEAT TRACK BETWEEN STATION 1430 AND 1442, LBL 99, 12 INCH SECTION OF SEAT TRACK WAS TORN AND DAMAGED. SEAT TRACK WAS PERMANENT REPAIRED PER SRM 53-00-52 FIG 201, REPAIR 6 AND REFERENCE XEO 53-051206.SDR P5CA0501378Fmc · failedCREW REPORTED RT FMC INOP. REPLACED RT FMC- MM 34-61-01. ALL OPS NORMAL.SDR UIEA200500060Connector · contaminatedON TAXI OUT NR2 ENGINE OIL PRESSURE DROPPED BELOW RED LINE-ENGINE SHUTDOWN. T/S IAW MM. CLEANED OIL PRESSURE TRANSMITTER CONNECTOR. ENGINE GROUND RUN PERFORMED ALL WORKING NORMAL. (K)SDR P5CA0401229Connector · dirtyNR 2 ENGINE OIL ITEM INDICATION. CLEANED ELECTRICAL CONNECTOR ON OIL TEMPRATURE SENSOR, NR 2 ENGINE INDICATION OK, IAW AMM 71-00-00.SDR P5CA0401185Transmitter · failedLOSS OF ENGINE NR 1 OIL PSI INDICATION ON LWR EICAS DURING CLIMB, NO EICAS MSG RECD OIL INDICATION HAD BEEN NORMAL THROUGHOUT TAXI. REPLACED NR 1 OIL PRESSURE TRANSMITTER PER MM 79-32-01. OPS CHECK ON RUN OK.SDR P5CA0401129Warning Light · illuminatedAFTER PUSHBACK APU DUCT LEAIL STATUS MESSAGE DISPLAYED. OPENED MEL 49-11-1-1.SDR P5CA0401093Warning Light · illuminatedSTATUS MESSAGE FUEL JET-B. DEFERRED PER MEL 28-31-4-1, PLACARDS INSTALLED.SDR P5CA0401059Hose · looseLOSS OF HYD FLUID, SYSTEM NR 1 ENG PUMP SELECTED OFF. SYSTEM NR 1 PRESS NORMAL TO COMPLETION OF FLIGHT. FOUND PRESS HOSE AT EDP LOOSE. TIGHTENED HOSE/LINE PER MM 29-11-08. NO LEAKS NOTED PER MM 71-00-00.SDR P5CA0401052Actuator · malfunctionedMAIN DECK SIDE DOOR WILL NOT CLOSE IN ELECTRICAL OR MANUAL MODE. REMOVED AND REPLACED LATCH ACTUATOR PER MM 52-32-09.SDR P5CA0401030Actuator · failedON ARRIVAL UNABLE TO OPEN SIDE CARGO DOOR MANUALLY. DOOR LATCH SYS PREVIOUSLY DEFERRED. REPLACED DOOR LATCH ACTUATOR PER MM 52-00-00, OPS CHECK NORMAL. DEFERRAL CLEARED.SDR P5CA0401029Display · failedEXTERNAL POWER FAILED TWICE. WHEN RESTORED, FO'S PFD REMAINED BLANK. SWAPPED LOWER EICAS DISPLAY WITH FO'S PFD AND DEFERRED IAW MEL 31-61-1. DMI AUTH. NR 32082.SDR P5CA0401024Warning Light · false indicationON PUSHBACK ACARS DIDN'T BLOCK OUT. SENSORS INDICATED DOOR OPEN. EICAS INDICATED DOOR CLOSED. ALL DOORS CYCLED AND PHYSICALLY CHECKED CLOSED, EICAS INDICATED ALL DOORS CLOSED.SDR P5CA0301002Pdu · malfunctionedSTATUS MESSAGE L/E MULTIDRIVE. REPLACED NR 3 L/E PDU, OPS CHECK NORMAL PER MM 27-81-00.SDR P5CA0300998Solenoid Valve · malfunctionedRETURNED TO BLOCKS. ENG. NR 3 FAILED TO START DUE TO 0 FUEL FLOW (NO EICAS MESS.) REPLACED NR 3 ENG. HMU FUEL SOLENOID VALVE. OPS CHECK OK IAW MM 73-21-00.SDR P5CA0300985Sense Line · looseSTART FAILURE NR 3 ENGINE - RETURN TO BLOCKS. INSPECTED NR 3 ENGINE, FOUND CDP SENSE LINE AT EEC LOOSE. CLEANED AND PROPERLY SECURED CDP LINE. ENGINE RUN ACCOMPLISHED WITH ALL PARAMETERS NORMAL.SDR P5CA0300974Engine · shutdownNR 3 ENGINE SHUTDOWN DUE TO NO OIL QTY - FL 350 OIL PRESSURE 45. DURATION OF SHUTDOWN - 45 MINUTES. REMOVED AND REPLACED NR 3 ENGINE PER MM 71-00-00 AND ATLAS MX JOB CARD A71710GTI. ENGINE OPS CHECK GOOD PER MM 71-00-00.SDR P5CA0300927Slide · failedRIGHT UPPER DECK SLIDE ASSY FAILED TO DEPLOY DURING MC CHECK. NEW SLIDE INSTALLED.SDR P5CA03000917Warning System · activatedDURING ENG START NR 4 ENG AUTO START EICAS MESSAGE STARTER VLV LIGHT FAILED TO EXTINGUISH WITH SWITCH PUSHED IN. ITEM DEFERRED PER MEL 80-11-01.SDR P5CA0300766Circuit Card · faultyON LANDING ROLL EICAS MSG APPEARED -APU FIRE LOOP A-, -APU FIRE LOOP B- AND APU BOTTLE LOW-. NO INTERIOR OR EXTERIOR INDICATIONS OF FIRE. DE-ACTIVATED APU PER AMM 49-11-00-042-064 AND DEFERRED PER DDPG 49-11-01.SDR UIEA200200024Skin Panel · puncturedFuselage Skin damaged from BS 460 to 480 from between Stringer 38R and 39R by cargo container during loading operation. Stringers 38R and 39R at this location deformed by container. Damaged skin area trimmed out. Damaged area of stringer 38R trimmed out. Strin
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