N419MC

Service difficulty reports · 287

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 = 'N419MC' 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 UIEA2015050600260Pseu · faultyON FINAL, RT WING GEAR DOOR INDICATED NOT DOWN WITH ALL OTHER INDICATIONS NORMAL. RECYCLED, NORMAL INDICATIONS, STATUS GEAR MONITOR. SENSOR VISUAL CONDITION CHECK OK. PSEU BITE TEST PASSED IAW AMM 32-61-00-501. SENSOR TO TARGET GAP CHECKED OK IAW AMM 32-61-May 5, 2015 · N419MC · Boeing 74748EF · Landing Gear Position and WarningSDR UIEA2015050600259Warning System · false activationGEAR DISAGREE & GEAR DOOR EICAS MSG. EXECUTED A GO AROUND. PERFORMED QRH PROCEDURES. GEAR CAME DOWN NORMAL, NORMAL LANDING. MANUALLY OPENED & CLOSED GEAR DOOR ON THE GND, NO DEFECTS NOTED. INDICATION PSEU TEST PASSED, ALL MSGS ON GND, IAW 32-14-00.May 5, 2015 · N419MC · Boeing 74748EF · Landing Gear Position and WarningSDR UIEA2015050500258Door Seal · defectiveGEAR DISAGREE & GEAR DOOR EICAS WHEN LG WAS FIRST LOWERED. ACCOMPLISHED QRH & GEAR INDICATED DOWN. RT WING MAIN GEAR INDICATED IN TRANSIT. R & R RT BODY OTBD GEAR DOOR SEAL IAW AMM 52-09-00. PSEU GND TEST PASSED IAW AMM 32-09-03/501.May 5, 2015 · N419MC · Boeing 74748EF · Landing Gear DoorsSDR UIEA2015050600261Actuator · faultyEICAS MSGS, GEAR DISAGREE, GEAR DOOR, LP 722506 GEAR MONITOR LP 722511, M19. SUSPECT WING RT LG ACTUATOR FAILURE. REPLACED RT WING GEAR RETRACT ACTUATOR IAW AMM 32-32-01 401 LP 722509. PERFORMED LG SWING TEST, FOUND NORMAL. NO MORE DEFECT NOTED IAW AMM 32-May 5, 2015 · N419MC · Boeing 74748EF · Landing Gear ActuatorSDR UIEA2014113000621Tire · damagedAIRCRAFT RETURNED DUE TO NR 1 HYD & QTY LOW, HYD PRESS ENG 1 & HYD RES PRESS 1 & HYD PRESS DEM 1, GEAR DOOR & GEAR DISAGREE & GEAR MONITOR STATUS MSGS ON TAKEOFF. UPON INVESTIGATION FOUND NR 8 TIRE LOOSED CAPPING WHICH CAUSED DAMAGE TO A NR 1 HYD SYS RETURN LNov 22, 2014 · N419MC · Boeing 74748EF · TireSDR UIEA2014092600466Controller · failedITEM 1 OUT FLOW VLV R EICAS MSG DISPLAYED. MANUAL PRESSURIZATION CONTROL ONLY. ITEM 2 EICAS MSG CABIN ALT AUTO. ITEM 1 CMC BITE SHOWS CPCS OUTFLOW VLV R, ACTUATOR & MOTOR FAIL MSG 21208. PULLED & RESET CABIN PRESS ICU RT CB C3166. REPLACED CHANNEL B CPCS Sep 26, 2014 · N419MC · Boeing 74748EF · Cabin Pressure ControllerSDR UIEA2014090800428Intercostal · crackedMD RT STATION 1200 FLOOR INTERCOSTAL WEB FOUND CRACKED. REPLACED IAW RI 53-41-10674.Sep 9, 2014 · N419MC · Boeing 74748EF · Fuselage Miscellaneous StructureSDR UIEA2014090800429Intercostal · crackedMD RIGHT STATION 1180 FLOOR INTERCOSTAL WEB FOUND CRACKED. REPLACED IAW RI 53-41-10678.Sep 9, 2014 · N419MC · Boeing 74748EF · Fuselage Miscellaneous StructureSDR UIEA2014090800430Skin · crackedNUMBER 1 PYLON OTBD SKIRT FAIRING SKIN FWD AREA FOUND CRACKED. REPAIRED IAW RI-54-50-10676 REV A.Sep 9, 2014 · N419MC · Boeing 74748EF · Nacelle/Pylon, Plate/SkinSDR UIEA2014090800431Skate Angle · damagedNUMBER 3 PYLON INBD SKATE ANGLE OF FAIRING AT NAC 457 TIME LIMITED REPAIR. REPAIRED IAW RI-57-04-10677 REV A.Sep 9, 2014 · N419MC · Boeing 74748EF · Nacelle/Pylon Miscellaneous StructureSDR UIEA2014090800433Skin · crackedFX NOSE GEAR CUT OUT RT REAR CORNER FX SKIN ONE EACH RIVET HOLE CRACK AT STATION 400. REPAIRED IAW RI-53-11-10680 REV A.Sep 9, 2014 · N419MC · Boeing 74748EF · Fuselage Main, Plate/SkinSDR UIEA2014090800434Skin · crackedRIGHT HORIZONTAL STABILIZER UPPER SKIN & UPPER REAR SPAR CHORD ZONE B AREA 8 FASTENER HOLE CRACK FOUND ON 2ND LAYER FROM TOP APPROX 1/16 INCH IN DEPTH. CRACKED BOLT HOLE RT NR 8 REPAIRED IAW RI-55-80-10679 & COMPONENT WORK PROCESS CARD KSJ507950-1.Sep 9, 2014 · N419MC · Boeing 74748EF · Horizontal Stabilizer, Plate/SkinSDR UIEA2014090800435Spar · crackedRIGHT HORIZONTAL STABILIZER UPPER REAR SPAR CHORD HOLE CRACK. FOUND ON 1ST LAYER FROM AFT APPROX 1/16 INCH IN DEPTH RUNNING OTBD CRACKED BOLT HOLE RT 29. REPAIRED IAW RI-55-80-10679 & COMPONENT WORK PROCESS CARD KSJ508198-01.Sep 9, 2014 · N419MC · Boeing 74748EF · Horizontal Stabilizer, Spar/RibSDR UIEA2014090800436Skin · crackedRIGHT HORIZONTAL STABILIZER UPPER SKIN & UPPER REAR SPAR CHORD ZONE B AREA ONE EACH HOLE NR 5 & CRACK FOUND ON 3ND LAYER FROM TOP APPROX 1/16 INCH IN DEPTH. CRACKED BOLT HOLE RT NR 5 REPAIRED IAW RI-55-80-10679 & COMPONENT WORK PROCESS CARD KSJ507638-01.Sep 9, 2014 · N419MC · Boeing 74748EF · Horizontal Stabilizer, Plate/SkinSDR UIEA2014021200056Ecu · malfunctionedEICAS MESSAGE ENG 3 OIL TEMP. ENG SHUT DOWN IAW QRH. INSTALLED NR 3 ENG ECU IAW FIM 7900001 FIG 109 & AMM 73-21-15. PERFORMED GND TEST 11 - 12 ALL PASSED REN ENG IAW AMM 711-00-00. TEST 3 ALL INDICATIONS NORMAL, OIL TEMP NORMAL, OK FOR SERVICE.Feb 12, 2014 · N419MC · Boeing 74748EF · Fuel Control/Turbine EnginesSDR UIEA2013032600155Cargo Track · crackedMX REPORTED DAMAGE TO THE LOWER LOBE. FWD CARGO COMPARTMENT FROM BS 560 -570, LBL 24.75 . SEAT TRACK CRACKED AND DAMAGED. PERFORMED A TIME LIMITED REPAIR .Mar 25, 2013 · N419MC · Boeing 74748EF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2013011500013Clock · inoperativeON DESCENT, A BURNED ELECTRICAL ODOR ASSOCIATED WITH AN IDS DU STATUS MESSAGE WAS NOTICED ON THE FLIGHT DECK. UNABLE TO BRING UP LOWER EICAS DURING THAT TIME, ODOR CEASED WHEN MESSAGE EXTINGUISHED. FOUND CAPTAIN'S DIGITAL CLOCK INOPERATIVE. THE E7/CHR LETTEJan 15, 2013 · N419MC · Boeing 74748EF · Independent InstrumentsSDR UIEA2012121000541Connector · contaminatedON DEPATURE EICAS MESSAGE "FLAPS DRIVE" APPEARED AND THE OTBD T/E FLAPS WOULD NOT RETRACT PAST 1 DEGREE OR EXTEND BEYOND 1 DEGREE. RETURNED TO DEPARTURE. MX FOUND THE LT OTBD FLAP POSITION TRANSMITTER ELECTRIC CONNECTOR WAS CONTAMINATED WITH DEICING FLUID. Dec 10, 2012 · N419MC · Boeing 74748EF · Flight Control System WiringSDR UIEA2012121000542Tire · failedON LANDING, NR 11 TIRE BLEW OUT AS REPORTED BY TOWER. ALSO COCKPIT INDICATION SHOWED BRAKES NR 3 AND NR 4 REGISTERED 5 ON THE BRAKE TEMPERATURE GAUGE. REPLACED NR 11 AND NR 12 WHEEL ASSEMBLIES IAW AMM 32-45-00. ALSO ACCOMPLISHED INSPECTION IAW AMM 05-51-10, 0Dec 10, 2012 · N419MC · Boeing 74748EF · TireSDR UIEA2012102600496Wire · damagedFOUND WIRES DAMAGED FOR LOAD SYS AT STATION CY ON LOWER CARGO PDU'S INOP ELECTRICALLY, MX FOUND DAMAGED WIRE BUNDLE STATION 530 FORWARD CARGO FLOOR AREA. SPLICED WIRES IAW SWPM 20-10-13. OPS CHECKED NORMAL IAW MM 25-53-01.Oct 26, 2012 · N419MC · Boeing 74748EF · Electrical Power System WiringSDR UIEA2012091000405Rib · crackedCRACK ON THE HORIZONTAL STAB L/E RIB. REPAIRED IAW EI T2012A55B-2096, REV 00 AND 01.Sep 3, 2012 · N419MC · Boeing 74748EF · Horizontal Stabilizer, Spar/RibSDR UIEA2012091000409Rib · crackedCRACK ON THE HORIZONTAL STAB L/E RIB. REPAIR IAW EI T2012A55B-2096, REV 00 AND 01.Aug 31, 2012 · N419MC · Boeing 74748EF · Horizontal Stabilizer, Spar/RibSDR UIEA2012091000397Panel · crackedDEFORMED WITH CRACK ON RT FUSE MAIN DECK CARGO DADO PANEL BETWEEN BS 1780 AND 1820. REPAIR IAW EI T2012A25B-1995, REV. 00.Aug 24, 2012 · N419MC · Boeing 74748EF · Fuselage Miscellaneous StructureSDR UIEA2012091000402Pan · crackedCRACK ON NOSE WHEEL WELL PRESSURE PAN AT BS 400 BL 0 WL 140 -150. REPAIR IAW EI T2012A53B-2049, REV 00 AND 01.Aug 10, 2012 · N419MC · Boeing 74748EF · Fuselage Main, BulkheadSDR UIEA2012091000403Strap · corrodedCORROSION ON MAIN DECK SIDE CARGO DOOR LOWER STRAP BETWEEN STA 1902 AND STA 1912. REPAIR IAW EI T2012A52B-2012, REV 00, 01, AND 02.Aug 8, 2012 · N419MC · Boeing 74748EF · Fuselage Miscellaneous StructureSDR UIEA2012091000396Support · crackedCRACK ON THE FRAME SUPPORT OF BS 2898 BULKHEAD AT RBL37, WL320. REPAIR IAW EI T2012A53B-1974, REV. 00.Aug 3, 2012 · N419MC · Boeing 74748EF · Fuselage Miscellaneous StructureSDR UIEA2012091000406Rib · crackedCRACK ON THE HORIZONTAL STAB L/E RIB. REPAIRED IAW EI T2012A55B-2096, REV 00, 01.Aug 3, 2012 · N419MC · Boeing 74748EF · Horizontal Stabilizer, Spar/RibSDR UIEA2012091000407Rib · crackedCRACK ON THE HORIZONTAL STAB L/E RIB. REPAIR IAW EI T2012A55B-2096, REV 00 AND 01.Aug 3, 2012 · N419MC · Boeing 74748EF · Horizontal Stabilizer, Spar/RibSDR UIEA2012091000408Rib · crackedCRACK ON THE HORIZONTAL STAB L/E RIB. REPAIR IAW EI 72012A55B-2096, REV 00 AND 01.Aug 3, 2012 · N419MC · Boeing 74748EF · Horizontal Stabilizer, Spar/RibSDR UIEA2012091000410Rib · crackedCRACK ON THE HORIZONTAL STAB L/E RIB. REPAIR IAW EI T2012A55B-2096, REV 00 AND 01.Aug 3, 2012 · N419MC · Boeing 74748EF · Horizontal Stabilizer, Spar/RibSDR UIEA2012091000411Rib · crackedCRACK ON THE HORIZONTAL STAB L/E RIB. REPAIR IAW EI T2012A55B-2096, REV 00 AND 01.Aug 3, 2012 · N419MC · Boeing 74748EF · Horizontal Stabilizer, Spar/RibSDR UIEA2012091000398Access Panel · crackedCRACK AROUND THE FASTENER HOLES ON ACCESS PANEL 472FL OF NR 3 PYLON LT SIDE. REPAIR IAW EI T2012A54B-1996, REV. 00.Aug 1, 2012 · N419MC · Boeing 74748EF · Nacelle/Pylon, Plate/SkinSDR UIEA2012091000399Access Panel · crackedCRACK ON THE ACCESS PANEL 472GL OF NR 3 PYLON LT SIDE. REPAIR IAW EI NR T2012A54B-1997, REV 00.Aug 1, 2012 · N419MC · Boeing 74748EF · Nacelle/Pylon, Plate/SkinSDR UIEA2012091000400Access Panel · crackedCRACK ON ACCESS PANEL NR 482ER OF NR 4 PYLON RT SIDE. REPAIR IAW EI NR T2012A54B-1973, REV 00.Aug 1, 2012 · N419MC · Boeing 74748EF · Nacelle/Pylon, Plate/SkinSDR UIEA2012091000401Access Panel · crackedCRACK ON THE ACCESS PANEL 452ER OF NR 1 PYLON RT SIDE. REPAIR IAW EI NR T2012A54B-1970, REV 00.Aug 1, 2012 · N419MC · Boeing 74748EF · Nacelle/Pylon, Plate/SkinSDR UIEA2012091000404Skin · damagedLIGHTNING STRIKE ON THE LT WINGLET T/E CASTING UPPER TIP. REPAIR IAW EI T2012A57B-2123, REV 00.Aug 1, 2012 · N419MC · Boeing 74748EF · Wing, Plate/SkinSDR UIEA2012033100113Fairing · delaminatedDURING WALKAROUND INSPECTION, MX FOUND CRACKED AND DELAMINATED RT WING LANDING GEAR DOOR FAIRING AFT EDGE, MEASURING 1.5 IN. X 1.0 IN. REF FIG 1. PERFORMED A TIME LIMITED REPAIR IAW SRM 51-70-17 OR SRM 51-70-07.Mar 30, 2012 · N419MC · Boeing 74748EF · Landing Gear DoorsSDR UIEA2012021000042Structure · puncturedDURING WALKAROUND INSPECTION, MX FOUND RT HORIZONTAL STABILIZER AFT TIP PUNCTURED AND DAMAGED (REF FIG 1), MEASURING 0.5625 IN. X 0.375 IN. X 0.1875 IN DEPTH INTO THE AFT FAIRING CORNER. DAMAGE IS BEYOND LIMITS IAW THE SRM 55-10-01, FIG 101, TABLE I DETAIL V.Feb 10, 2012 · N419MC · Boeing 74748EF · Horizontal Stabilizer StructureSDR UIEA2011121200715Nozzle · dentedDURING MX WALKAROUND OF MX FOUND A DENT ON THE EXHAUST NOZZLE AT THE 8 O'CLOCK POSITION ON THE NR 2 ENGINE. THE DENT IS APPROX 1.0" INCH X 1.250" INCH X 0.168" DEPTH. THE DENT IS APPROX 29.5" FROM THE NOZZLE EDGE. IAW SRM 54-41-30 THE DENT IS OUT OF LIMITS. PDec 12, 2011 · N419MC · Boeing 74748EF · Engine Collector/Tailpipe/NozzleSDR UIEA2011121200712Door · damagedDURING WALKAROUND INSPECTION, MX FOUND THE RT WING LANDING GEAR FIX DOOR L/E WITH 2 EA PULLED RIVETS AND CRACK MEASURING 0.750 INCH LONG. THE DAMAGE EXCEEDS THE LIMITS OF THE SRM 52-80-02, FIGRE 101 IAW SRM 51-70-02. PERFORMED TIME LIMITED REPAIR.Dec 11, 2011 · N419MC · Boeing 74748EF · Landing Gear DoorsSDR UIEA2011111200647Cover · damagedDURING ROUTINE WALK AROUND CHECK OF ACFT. UPPER SIDE WALL ASSY HINGE COVER ON THE NR 2 ENGINE THRUST REVERSER AND THE ADJACENT STRUT FAIRING PANEL WERE FOUND DAMAGED. FABRICATED 2 REPLACEMENT BRACKETS, STRAIGHTEN OUT HINGE COVER, REINSTALLED HINGE COVER WINov 11, 2011 · N419MC · Boeing 74748EF · Engine Thrust ReverserSDR UIEA2011101300569Access Panel · crackedDURING WALK AROUND INSPECTION, MX REPORTED DAMAGE FOUND TO LT WING LOWER L/E PANEL FWD OF INBD FUELING ACCESS DOOR CRACK, MEASURING 3.0" LONG. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS IAW SRM 51-10-02, INOct 13, 2011 · N419MC · Boeing 74748EF · Wing, Plate/SkinSDR UIEA2011072800387Floorbeam · dentedINSPECTION FOUND VISUALLY ON THE BS 560 FWD CARGO COMPARTMENT FLOORBEAM UPPER TEE CHORD FWD FLANGE HAD A DENT AT RBL 18 AND 65B06871-9 INNER CHORD HAD A DENT AT RBL 49 AS NOTED IN FIG 1. NO APPLICABLE SRM REPAIR FOR THIS AREA. FURTHER STUDY OF THE REPAIR AREJul 28, 2011 · N419MC · Boeing 74748EF · Fuselage Main, Floor BeamSDR UIEA2011072800378Tension Tie · damagedDURING INSPECTION, IAW EO 4453A301 REV A, CRACK WAS FOUND AT 1 EA FASTENER HOLE ON AT BS 860 RT SIDE TENSION TIE (STR 9R), AFT CHANNEL. THE SUBJECT DAMAGE WAS DOCUMENTED ON NRC 50599. THE DAMAGED TENSION TIE WAS REPAIRED IAW WORK STEP 11E OF PART 2 OF EO 475Jul 28, 2011 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2011072800379Tension Tie · crackedDURING INSPECTION, IAW EO 4453A301 REV A, CRACK WAS FOUND AT 1 EA FASTENER HOLE ON AT BS 840 LT SIDE TENSION TIE (STR 10L), FWD CHANNEL. (THE DAMAGED TENSION TIE WAS REPAIRED IAW WORK STEP 10E OF PART 2 OF EO 4753B301 REV A IAW WORK STEP 10E OF PART 2 OF EO,Jul 28, 2011 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2011072800380Tension Tie · crackedDURING INSPECTION IAW EO 4453A301, REV A, 1 EA CRACK WAS FOUND ON AT BS 820 RT SIDE TENSION TIE (STR 10R), AFT CHANNEL. (THE DAMAGED TENSION TIE WAS REPAIRED IAW WORK STEP 9E OF PART 2 OF EO 4753B301REV A. IAW WORK STEP 9E OF PART 2 OF EO, THE TENSION TIE CRAJul 28, 2011 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2011072800382Tension Tie · crackedDURING INSPECTION OF DATUM ACFT IAW EO 4453A301 REV A, CRACK WAS FOUND AT 1 EA FASTENER HOLE ON AT BS 840 LT SIDE TENSION TIE (STR 10L), AFT CHANNEL. (THE DAMAGED TENSION TIE WAS REPAIRED IAW WORK STEP 10E OF PART 1 OF EO 4753B301, REV A IAW WORK STEP 10E OF Jul 28, 2011 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2011072800383Tension Tie · crackedDURING INSP OF DATUM ACFT IAW EO 4453A301REV A, CRACKS WERE FOUND AT 2 EA FASTENER HOLES ON AT BS 760 RT SIDE TENSION TIE (STR 10R), AFT CHANNEL. (THE DAMAGED TENSION TIE WAS REPAIRED IAW WORK STEP 6E OF PART 2 OF EO 4753B301, REV A IAW WORK STEP 6E OF PART Jul 28, 2011 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2011072800384Tension Tie · damagedDURING INSPECTION OF DATUM ACFT IAW EO 4453A301 REV A, CRACK WAS FOUND AT 1 EA FASTENER HOLE ON AT BS 760 LT SIDE TENSION TIE (STR 10L), AFT CHANNEL. (THE DAMAGED TENSION TIE WAS REPAIRED IAW WORK STEP 6E OF PART 1 OF EO 4753B301, REV A IAW WORK STEP 6E OF PARJul 28, 2011 · N419MC · Boeing 74748EF · Fuselage Main, StructureSDR UIEA2011072800385Tension Tie · damagedDURING INSPECTION OF DATUM ACFT IAW EO 4453A301REV A, CRACKS WERE FOUND AT 2 EA FASTENER HOLES ON AT BS 740 LT SIDE TENSION TIE (STR 10AL), AFT CHANNEL. (THE DAMAGED TENSION TIE WAS REPAIRED IAW WORK STEP 5E OF PART 1 OF EO 4753B301, REV A, IAW WORK STEP 5E OJul 28, 2011 · N419MC · Boeing 74748EF · Fuselage Main, Structure
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