N408MC
Service difficulty reports · 206
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 = 'N408MC' 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 = 'N408MC' 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 UIEA2011110600638Door · damagedDURING WALKAROUND INSP, MX FOUND THE LT WING GEAR DOOR FAIRING - LOWER EDGE CRACKED, MEASURING 7.0 IN. X 2.0 IN. (REF FIG 1) DAMAGE FOUND TO BE BEYOND THE SRM 52-80-02, FIG 101 ALLOWABLE DAMAGE 4 LIMITS IAW SRM 51-70-02, FIG 101 (SHEET 9 OF 41) ALLOWABLE DAMAGSDR UIEA2011082700474Skin · puncturedDURING WALKAROUND, MX FOUND THE NR 4 RT THRUST REVERSER CORE COWL HAS 2 PUNCTURES IN THE SKIN LOCATED ABOVE THE ACCESS PANEL AND BLOWOUT DOOR. DAMAGE TO THE ACCESS PANEL AND BLOWOUT DOOR HINGES, LATCHES AND LANYARDS. REPAIRED.SDR UIEA2011081700455Sleeve · crackedDURING MX WALKAROUND, FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, BETWEEN APPROX THE 9 TO 12 O'CLOCK POSITION ON THE NR 3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 11" LONG AND IS JUST IN FRONT OF NAC STA 349.236. IAW SRM 54-41-30 THE LENGTH OF THE CSDR UIEA2011080700432Skin · damagedDURING MX WALKAROUND, MX FOUND DAMAGE TO THE NR 2 ENG RT THRUST REVERSER TRANSLATING COWL EXTERNAL SKIN OUTER FINISH DAMAGE. THE DAMAGE IS LOCATED IN NEAR THE REVERSER COWL SKIN T/E (REF FIG 1-3): PERFORMED A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK ISDR UIEA2011040100180Skin · dentedDURING LOADING, THE FUSELAGE SKIN AT BS 1935, S-38R WAS DENTED. THE DENT MEASURES 0.75 INCH WIDE BY 1.5 INCH LONG BY 0.0625 INCH DEEP. THERE IS ALSO A GOUGE IN THE DENT 0.003 INCH DEEP. (REMOVE THE GOUGE IN THE DENTED AREA IAW SRM 53-00-01, FIG 101, DETAIL II.SDR UIEA2011011700005Fairing · crackedDURING WALKAROUND INSP, MX REPORTED CRACK DAMAGE FOUND ON THE RT OTBD WBL1241 - L/E FIXED FAIRING. THE CRACK MEASURES 0.375 IN. LONG (REF FIG 1). THE CRACK EXCEEDS THE SRM 57-41-01, FIG 101, ALLOWABLE DAMAGE LIMITS. (DISPOSITION WAS MADE TO PERFORM TIME LIMSDR UIEA2011011500002Solenoid · inoperativeGEAR LEVER WOULD NOT RETRACT. ACCOMPLISHED QRH PROCEDURES. AIR TURN BACK. (TROUBLESHOT TO BAD SOLENOID IN LANDING GEAR CONTROL PANEL. ITEM DEFERRED DDG 32-31-1)SDR UIEA2010123100249Skin · dentedDURING WALKAROUND INSP, MX REPORTED DENT DAMAGE FOUND ON THE LT OTBD FORE FLAP - WBL745 UPPER EXTERNAL SKIN PANEL. MEASURING 5.0 IN LENGTH X 3.125 IN. WIDTH & AMP; 0.625 IN. (REF FIG 1). THE DAMAGED AREA EXCEEDS THE SRM 57-53-01, FIG 101, ALLOWABLE DAMAGE 1 SDR UIEA2010121900195Sleeve · crackedDURING MX WALKAROUND OF N408MC MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 12 O'CLOCK POSITION ON THE NR3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 16" LONG AND IS APPROX 13" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LSDR UIEA2010121100189Skin · damagedDURING WALKAROUND INSP, MX FOUND DAMAGE TO THE OTBD RT WS1585 - L/E NOSE EXTERNAL SKIN MEASURING 2.5 IN. L X 1.5 IN. W AND 0.125 IN. DEPTH (REF. FIG 1). DAMAGED AREA FOUND BEYOND THE SRM 57-41-01, FIG 101, DETAIL III ALLOWABLE DAMAGE (GENERAL) LIMITS. (DISPOSSDR UIEA2010112500183Web · crackedDURING WALK AROUND INSP, DAMAGE TO THE LOWER AFT CARGO COMPARTMENT - BS1850, LBL45.5 FLOOR WEB - CRACK/DAMAGE WAS FOUND MEASURING 2.0 IN. X 4.450 IN. (REF FIGURE 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIOSDR UIEA2010112300180Skin · dentedDURING WALKAROUND INSP, MX FOUND THE LWR LOBE - LWR AFT CARGO DOOR AT BS1817, LWR FWD CORNER AREA WITH A DENT/DAMAGE, MEASURING 12.5 IN. LONG X 0.150 IN. (REF FIG 1). THE DENT EXCEEDS THE SRM 52-30-01, FIG 101, DETAIL XI ALLOWABLE LIMITS. (DISPOSITION WAS MADSDR UIEA201000237Nose Cowl · dentedMX FOUND NR 3 ENGINE INLET NOSE COWL L/E DENTED AT APPROX 2 O' CLOCK POSITION MEASURING 12.0 INCHES IN LENGTH X 5.0 INCHES WIDTH AND 0.5 INCH DEPTH. AFTER DETAIL VISUAL INSP (10X MAGNIFYING GLASS) IT WAS VERIFIED THAT NO SHARP CREASES AND/OR CRACK CONDITION EXSDR UIEA2010083100150Nose Cowl · damagedDURING WALK AROUND INSP, IN MX, FOUND THE NR 3 ENGINE INLET NOSE COWL L/E DENTED (SUSPECTED BIRD-STRIKE) AT APPROX 4 O' CLOCK POSITION MEASURING 5.5 INCHES IN LENGTH, 3.0 INCHES WIDTH AND 0.5 INCH DEPTH. AFTER DETAIL VISUAL INSP (10X MAGNIFYING GLASS) IT WAS VSDR UIEA2010082200142Nozzle · crackedDURING MX WALK AROUND, MX FOUND (1EA) CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 11 O'CLOCK POSITION. THE CIRCUMFERENTIAL CRACK IS APPROX 35.0 IN. LONG. IAW SRM 54-41-30 THE LENGTH OF THE CRACK IS OUT OF LIMITS. DISPOSITION IS TO STOP DRSDR UIEA2010071500100Wheel · delaminatedSUSPECTED DELAMINATION OR DEFLATED NOSE TIRE. GEAR PINS INSTALLED AND ACFT TOWED TO HANGER. (ON INSP, FOUND RT NOSE TIRE, CTR TREAD MISSING. IAW MM 5-51-34-202-001, NO DAMAGE FOUND TO FUSELAGE OR ADJACENT STRUCTURE. FOUND SUPPORT ASSY FOR EXT POWER CABLE MISSSDR UIEA2010062600035Tire · failedDURING WALKAROUND INSP, MX FOUND THE LT MAIN BODY GEAR NR 8 WHEEL SEVERED; DUE TO TIRE DAMAGED/BURST.SDR UIEA2010052400005Fan · failedUPON CLIMB OUT; CREW EXPERIENCED SEVERAL EICAS MESSAGES: EQUIPMENT COOLING LOW FLOW, OXYGEN ON AND CABIN WARNING (DEPRESSURIZATION). (FOUND E/E COOLING FAN BURST, DAMAGING THE ACFT FUSELAGE. R & R EE COOLING SUPPLY FAN, EE COOLING EXHAUST VALVE AND INTERNAL SSDR UIEA2010052400004Stringer · damagedDAMAGE FOUND TO STR 32L AT BS 550 AFTER A BURST EQUIPMENT COOLING EXHAUST VALVE STRUCK S-31L STR & SKIN. REFER TO EO 4453A362 FOR SKIN REPAIR.SDR UIEA2010052400003Stringer · damagedDAMAGE WAS FOUND TO THE 142U0086-198 STRINGER 31L AT BS 550 AFTER A BURST EQUIPMENT COOLING EXHAUST VALVE TRUCK THE S-31L STRINGER AND SKIN. REFER TO EO 4453A362 FOR THE SKIN REPAIR. THE 142U0086-198 STRINGER IS MADE FROM 0.050 INCH THICK 7075-0 SHEET PER QQ-ASDR UIEA2010052400002Skin · damagedDAMAGE WAS FOUND TO THE 65B23701-6 FUSELAGE SKIN AT BS 550 BETWEEN S-31L AND -32L AFTER A BURST EQUIPMENT COOLING EXHAUST VALVE STRUCK THE S-31L STRINGER AND SKIN. REFER TO EO 4453A363 FOR THE STRINGER REPAIR. ACCOMPLISH PART 1 OF THIS EO PRIOR TO FURTHER FLIGSDR UIEA2010052000001Warning Message · false activationAIR TURN BACK DUE RUDDER RATIO MESSAGE DISPLAYED (SRM REPLACED AND SYS CHECKS NORMAL (MX WAS ABLE TO DUPLICATE PROBLEM ON GROUND AND CORRECTED AFTER SRM REPLACED, HOWEVER, AS PREC, REQUESTED PITOT STATIC TEST CHECKOUT OF SYS.)SDR UIEA201000008Rib · crackedCRACKING WAS FOUND IN THE LT/RT HST LEADING EDGE RIBS BETWEEN LE STA 131.946 AND LE STA 527.190. REPAIRED THE 5EA CRACK AREA IAW EI NO T2010A55B-175 REV 00 AND T2010P55B-165 REV 00. CONDITION CHECK NORMAL.SDR UIEA201000007Shim · migratedSHIM MIGRATION WAS FOUND BETWEEN RT LONGERON FITTING AND FUSELAGE SKIN AT STA 1241, RBL 128, WL 175. REPAIR IN IAW EI NR T2010A53B-137 REV 00. CHECK CONDITION NORMAL AND JOB COMPLETED. INITIAL AND REPEAT INSPECTION AT EVERY C-CHECK NOT TO EXCEED 24 MONTHS PSDR UIEA201000006Skin · dentedDENT - SKIN UPPER SURFACE OF FWD CARGO BELOW SKIN STA. 695, S46R-S47R. REPAIRED THE DAMAGED AREA IAW 747-400F SRM 53-00-01 REPAIR 6 REV 53 REPEAT INSPECTION ON THE FOLLOWING METHOD EXTERNAL HFEC INTERVAL 6.000 FLIGHT CYCLES PER EO NR 4453A326. CONDITION CHECSDR UIEA201000005Frame · brokenFOUND FUSELAGE STRUCTURE FRAME BROKEN AT STA 1800 S-10R. REPAIRED THE FRAME BROKEN AREA IAW EI NR T2010A53B-166. FOLLOWED UP INSPECTION PRIOR TO 25,000 TOTAL FLIGHT CYCLES PER EO NR 4453A327.SDR UIEA201000004Skin · wornPART 1-4 FOUND DAMAGE WEAR ON LT AND RT SIDE VERTICAL STAB SEAL INTERFACE SKIN AREA BETWEEN BS 2360-2390 AND BS 2521-2598 AND BS 2280- 2360. BLEND OUT DAMAGE AREA IAW SRM 53-00-01 REV 53 RESIDUAL MATERIAL THICKNESS WITHIN ALLOWABLE DAMAGE, APPLY PROTECTIVE COSDR UIEA201000003Sleeve · dentedA DENT WAS FOUND ON THE NR 4 ENG LT EXHAUST SLEEVE, AT THE 9 O'CLOCK LOCATION NEAR NAC STA 349-236. MANUFACTURER PROVIDED INSPECTION TIMELINE OF REF/D/AND PERFORM FPI INSPECTION PER BAC 5423 TO ENSURE NO CRACKS ARE PRESENT ON NOTED DENT. REPEAT INSPECTION EVSDR UIEA201000158Fairing · damagedTRAILING EDGE I/B MID FLAP LEADING EDGE FAIRING UPPER MID AREA FOUND DAMAGED (DIMENSION 15 X 4.5 INCHES). LT WING - TRAILING EDGE I/B MID FLAP LEADING EDGE FAIRING UPPER MID AREA COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5.0 FIG 6.SDR UIEA200900023Start Valve · malfunctionedDIVERSION: AFTER TAKEOFF EICAS MESSAGE "START CUTOUT 3" DISPLAYED AT APPROX 11,000 FEET, ALSO STATUS MESSAGE "ENG-3 START VALVE". TRANSFERRED TO DMI M09-016 PER MEL 80-11-1. START VALVE TO BE OPERATED MANUALLY UNTIL FINAL REPAIR IS PERFORMED.SDR UIEA200800358Intercostal · crackedBS 1220 LBL 106 BELOW FLOOR WEB CRACKED. FLOORBEAM INTERCOSTAL WEB REPAIRED AS PER 51-70-13 AND EO 4453A229.SDR UIEA200800357Door Frame · crackedL1 DOOR FORWARD UPPER FRAME CRACKED. L1 DOOR UPPER FORWARD FRAME REPAIRED AS PER SRM 51-70-06.SDR UIEA200800356Skin · crackedNR 7 VC FLAP EXTERIOR SURFACE CRACKED. NR 7 VC FLAP REPLACED IAW 27-81-02. RIGGING AND OPS CHECKED IAW 27-81-00.SDR UIEA200800346Structure · damagedWHILE AIRCRAFT WAS TAXING, THE AIRCRAFT STRUCK ANOTHER AIRCRAFT THAT WAS PARKED CAUSING DAMAGE TO RIGHT WINGLET. RIGHT WINGLET REMOVED PER CDL, AREA VISUALLY INSPECTED AND AIRCRAFT RELEASED. ACFT AWAITING PERMANENT REPAIRS. OPENSDR AIEA200800263Fairing · damagedDURING ARRIVAL WALKAROUND INSPECTION FOUND LOWER RT AFT OF BODY GEAR FUSELAGE FAIRING DAMAGED. ACCOMPLISHED TIME LIMITED REPAIR AS PER EO 4453A188 DATED 7/8/08 ENTERED NON MEL DMI N08-037 FOR REPEAT INSPECTION OF PANEL AT EVERY A-CHECK. (A)SDR AIEA200800262Tire · failedDURING ARRIVAL WALK AROUND INSPECTION FOUND NR 11 TIRE SEPARATION. REPLACED NR 11 AND 12 WHEEL ASSEMBLIES. ALSO ACCOMPLISHED TIRE TREAD LOSS CONDITIONAL INSPECTION AS PER 05-51-34-202-001. (A)SDR AIEA200800260Engine · oil consumptionENGINE NR 3 OIL QTY WENT TO 0 (3 HOURS AFTER TAKEOFF). ENGINE SHUT DOWN PRECAUTIONARY. FIM 79-00-00 FOLLOWED. INSPECTED FOR OIL LEAK. NO WETTING FOUND. REPLENISHED 22 QTS OIL AND LEAK AND OPS CHECK PERFORMED. NO LEAK FOUND. IDG AND STARTER DRAIN LINE CASDR UIE2008F00008Skin · delaminatedFOUND DURING A-CHECK. REPAIR THE DAMAGE FOUND ON L/E OF LEFT OB FOREFLAP MEASURING 12 INCHES LONG BY 2 INCHES WIDE IAW SRM 51-70-07. REPAIR CARRIED OUT IAW EO 4457A145. (K)SDR UIEA200800091Access Panel · crackedNR 3 PYLON ACCESS PANEL 472FL BOTH SIDES SKINS ADJACENT TO LATCH AREA HAVE CRACKED. REPAIRED PANEL PER EO 4454A055 AND RE-INSTALLED PER 54-62-02.SDR UIEA200600274Powerpack · wornATB:DUE TO MEDIUM/LIGHT VIBRATION IN RUDDER PEDALS. FLIGHT CONTROL VALVES OFF BY 1. YAW DAMPER OFF NO HELP, A/P OFF NO CHANGES. FOUND UPPER RUDDER HYD RETRACT LINE "B" NUT AND UNION LOOSE BY 2.5 TURN WITH HEAVY LEAK. TIGHTEN BACK IAW MM 27-21-15 OPS AND LEAK CSDR UIEA200600269Fire Loop · malfunctionedIFSD: DUE TO DET FIRE/OHT 2 IN CLIMB REMAINED DISPLAY ENTIRE FLIGHT. STATUS NR 2 ENGINE FIRE LOOP B-RESET. B AND A LOOP CIRCUIT BREAKERS REDUCED, NR 2 THRUST TO IDLE, NO HELP DISPLAYED UNTIL ENGINE SHUTDOWN. ADVISORY, ENG 2 PRECAUTIONARY SHUTDOWN AT 2345, DSDR UIEA200600129Panel · missingON ARR, FOUND ON ENGINE NR 2 INBOARD PYLON PANEL 462RL MISSING. INSP LT FLAPS AND STABILIZER NO DAMAGE FOUND. REPLACED PANEL 462RL ON ENGINE NR 2, OK FOR SERVICE.SDR UIEA200600125Skin · gougedRIGHT TRAILING EDGE AFT FLAP HAS A GOUGE ON THE UPPER SURFACE APPROX ONE INCH LONG, .125 INCH DEEP AND .250 WIDE. LOCATED 3 FEET OUTBOARD OF NR 7 TRACK CANOE. FOUND DURING C-4 CHECK AT PIK, N/ROUTINE NR 148. GOUGE REPAIRED IAW SRM 57-53-01 FIG 101. COVE PASDR UIEA200600124Skin · dentedRT INBOARD AFT FLAP HAS A DENT ON THE UPPER SURFACE APPROX ONE SQUARE INCH AND APPROX .250 DEEP,12 INCHES OUTBOARD OF NR 6 FLAP TRACK CANOE. FOUND DURING C-4 CHECK, N/ROUTINE NR 147. PERMANENT REPAIR CARRIED OUT TO DAMAGE AREA AS PER SRM 51-70-10 FIG 203 ANDSDR UIEA200600123Panel · chippedFLYING PANEL ON THE RIGHT HAND WING INBOARD TRAILING EDGE PREVIOUS REPAIR REQUIRES RE-WORK. AREA MARKED LOCATION IS APPROX WBL 220. NON ROUTINE NR 145. EXISTING REPAIR REMOVED AND A NEW REPAIR INSTALLED IAW SRM 51-70-06.SDR UIEA200600070Engine · damagedNR 1 ENGINE HAD EGT SPIKE TO 943* AT 5,000 MSL POWER REMAINED LOW THROUGHOUT CLIMB AND CRUISE. NR 1 N1- 20% BELOW 2-3-4. N2- 8-10% BELOW 2-3-4, EGT 50*-80* HOTTER THAN 2-3-4. N2 VIB 5.0 2-3-4 WERE 1.1-1.2. JFK NOTIFIED. NR 1 ENGINE SHUT DOWN AS PER JFK INSTSDR UIEA200400185Engine · malfunctionedNR 4 ENGINE NOT MAKING TO THRUST. (RTO) REJECTED TAKE OFF DUE TO NR 4 ENGINE NOT MAKING TAKE OFF THRUST. PERFORMED POWER ASSURANCE CHEDK (TEST 10), ALL WITHIN LIMITS IAW MM 71-00-00.SDR UIEA200400099Actuator · inoperativeTAKEOFF WARNING (CONFIGURATION BODY GEAR) DISPLAYED DURING TAKEOFF. CMC GAVE LT GEAR OB ACTUATOR SWITCH MESSAGE 32055. DEACTIVATED ALL ACTUATORS INDICATION SYS IAW MEL AND TRANSFERRED ITEM TO DMI. (DEACTIVATED RT OB CYLINDER IAW MEL). REMOVED AND REPLACED SDR UIEA200400033Control Unit · malfunctionedEICAS MESSAGE -HEAT WINDOW LT- DISPLAYED AFTER 1 HOUR CRUISE FLT AT FL330 AND SIMULTANEOUSLY L1 WINDOW CRACKED. PRESSURIZATION WAS NORMAL. REPLACED L1 WINDOW HEAT CONTROL UNIT IAW MM 30-41-00 OPERATION CHECK NORMAL. REMOVED AND REPLACED L1 WINDSHIELD IAW MMSDR UIEA200400025Retainer · corrodedCORROSION FOUND IN PORTION OF MISSING SEAL RETAINER. FORM OF CORROSION (FLAKING, PITTING) FOUND. CORROSION CLEANED UP IAW SRM 51-10-02 ALODINE 1200 APPLIED AND REPROTECTED WITH BMS 10-11 TY1.
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