N415MC
Service difficulty reports · 147
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 = 'N415MC' 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 = 'N415MC' 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 UIEA2013013100059Lever · damagedRT WING OTBD FORE FLAP TRACK NR 12 ATTACH LEVER ASSY DAMAGED. REMOVED DAMAGED LEVER ASSY LOCATED AND INSTALLED NEW LEVER ASSY IAW COMPONENT MM 57-52-51.SDR UIEA2012122400562Skin · damagedDURING POST FLIGHT WALK-AROUND INSPECTION, PUNCTURE DAMAGE APPROX 4.5" BY 2.5" WAS FOUND ON THE LOWER SURFACE OF THE L/E OF THE RIGHT WING INBD AFT FLAP. PERFORMED A TIME LIMITED REPAIR.SDR UIEA2012111500528Power Supply · inoperativeEMERGENCY LIGHTS ON UPPER DECK INOPERATIVE AT BS 410, 587, 550. R & R EMERGENCY BATTERY POWER SUPPLY M 5170. OPS CHECKED OK IAW AMM 33-51-04.SDR UIEA2012081300357Skin · delaminatedLT WING INBD T/E FWD FLAP DELAMINATED IN FWD EDGE AREA. TIME LIMITED REPAIRED ACCOMPLISHED IAW EO 4457A424 PART 1.SDR UIEA2012081300356Skin · delaminatedRT WING - INBD T/E FWD FLAP FWD EDGE FOUND DELAMINATED, APPROX 60", TIME LIMITED REPAIRED ACCOMPLISHED IAW EO 4457A424, PART 1.SDR UIEA2012070400297Clamp · looseEQUIPMENT COOLING EICAS MESSAGE APPEARED ON CLIMB OUT. WENT AWAY IN OVERRIDE POSITION BUT RETURNED IN BOTH STANDBY AND NORMAL MODES DURING CRUISE. (INSPECTION OF MAIN DECK DISTRIBUTION DUCTS CARRIED OUT. FOUND MAIN DUCT CLAMPS LOOSE AND SEPARATED BETWEEN STASDR UIEA2012051100211Radio · inoperativeINOPERATIVE LEFT VHF AFTER 5 HOURS IN FLIGHT, STRONG ELECTRICAL ODOR COMING FROM RADIO PANEL. LT SIDE RADIO CONTROL PANEL, AUDIO CONTROL PANEL REMOVED FROM RACK, ALL CONNECTORS AND WIRING HARNESS INSPECTED, NO CHAFED WIRING FOUND AND NO WIRE DAMAGE FOUND. LESDR UIEA2012033000111Smoke Detector · faultedFIRE MAIN DECK AFT AT 1:20 FROM AMS, VERIFIED PHYSICALLY THERE WAS NO FIRE. EICAS FOLLOWED STATUS MESSAGES MAIN DECK CARGO 12 LP A, INDICATING A FALSE WARNING. FOUND MAIN DECK CARGO SMOKE DETECTOR 12A AT FAULT, R & R RT SMOKE DETECTOR 12A IAW AMM 26-14-02, TSDR UIEA2012010900006Fairing · damagedLT WING TO BODY FAIRING PANEL DAMAGE AT BS 1550. ACCOMPLISHED PART 1 OF EO 4453A671.SDR UIEA2011122700729Door · damagedDURING MX WALKAROUND FOUND THE NR4 RT ENGINE CORE COWL DOOR SKIRT (MID) FAIRING BENT INWARD, CURLED AND CRACKED IN RADIUS OF BEND. THE LENGTH OF THE DAMAGE EXCEEDS THE SRM LIMITS. REPAIRED DAMAGED.SDR UIEA2011121200713Door · damagedDURING WALKAROUND INSPECTION, MX FOUND THE NR 4 RT ENGINE CORE COWL DOOR SKIRT (MID) FAIRING BENT INWARD, CURLED AND CRACKED IN RADIUS OF BEND. THE LENGTH OF THE DAMAGE EXCEEDS THE SRM LIMITS. PERFORMED A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTSDR UIEA2011111000646Seal · brokenFOUND SECOND DESCENT DEVICE SAFETY SEAL BROKEN. (REPLACED DESCENT DEVICE)SDR UIEA2011111000645Seal · brokenFOUND 6TH DESCENT DEVICE SAFETY SEAL BROKEN. (REPLACED DESCENT DEVICE)SDR UIEA2011111000644Seal · brokenFOUND 5TH EMERGENCY DESCENT DEVICE SAFETY SEAL BROKEN. (REPLACED 5TH DESCENT DEVICE)SDR UIEA2011111000643Seal · brokenFOUND 4TH DESCENT DEVICE SAFETY SEAL BROKEN. (REPLACED DESCENT DEVICE)SDR UIEA2011111000642Seal · brokenFOUND 7TH DESCENT DEVICE SAFETY SEAL BROKEN. (REPLACED DESCENT DEVICE)SDR UIEA2011101300568Handle · damagedDURING WALKAROUND INSPECTION, MX REPORTED DAMAGE FOUND TO MAIN DECK TO FWD E/E COMPARTMENT ACCESS DOOR HANDLE. REPLACED THE DAMAGED DOOR HANDLE.SDR UIEA2011030600144Sleeve · crackedDURING MX WALKAROUND, MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 12 O'CLOCK POSITION ON THE NR 2 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 8" LONG AND IS APPROX 13" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OFSDR UIEA2011021600089Stiffener · damagedDURING LOADING OPERATIONS AT ACC THROUGH THE NOSE CARGO DOOR, LOADER DROPPED CAUSING DAMAGE TO BS260, WL195.8 - CANTED BULKHEAD STIFFENERS (2 EA), CONSISTING IN EDGE CRACKS MEASURING 1.5 INCHES LONG (REF FIG 1). DAMAGE TO THE STIFFENERS EXCEEDS THE SRM 53-10-SDR UIEA2010110900176Sleeve · crackedDURING MX WALKAROUND OF MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, APPROX THE 2 O'CLOCK POSITION ON THE NR2 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 2.25" LONG AND IS NEAR THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OF THE CRACK IS WITHIN LSDR UIEA201000233Skin · puncturedDURING JACKING OF ACFT, MX PUNCTURED AN EXISTING REPAIR DOUBLER THROUGH THE UNDERLYING SKIN, LOCATED AT SECTION 48, BS 2594 ABOVE STRINGER 42R TAIL JACK PAD AREA. PUNCTURE MEASURING 5.0 IN. LENGTH X 1.750 WIDTH. DISPOSITION WAS MADE TO PERFORM PERMANENT REPASDR UIEA2010072400118Compressor · stalledCLIMBING OUT OF APPROX 3500' NR 4 ENG EMITTED 2 LOUD COMPRESSOR STALLS WITH ASSOCIATED SURGES IN N1, N2 AND EGT. SHUTDOWN NR 4 ENG SHUTDOWN ENG AT APPROX 2210Z. DUE TO SIGNIFICANT COMPRESSOR STALL, ELECTED TO COMPLETE THE "SEVERE ENG DAMAGE CHECKLIST", SO FIRESDR UIEA2010072100117Structure · crackedDURING A2 CHECK INSP DAMAGE WAS FOUND, RT WING INBD MID FLAPS CRACKED. PERMANENT REPAIRS ACCOMPLISHED IAW THE SRM 51-70-07 PAR 5A. THE REPAIRS ACCOMPLISHED IAW PART 1 ARE CATEGORY A AND WERE PERFORMED IAW SRM 51-70-07 PARA 5A.SDR UIEA2010052600138Skin · crackedLT WING INBD MID FLAP MOST OTBD T/E FOUND CRACKED. (LT WING INBD MID FLAP MOST OTBD T/E LWR SURFACE COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A. DETAIL REF HX PROCESS CARD SEQ NR EAX 500344-1).SDR UIEA2010052600137Skin · crackedRT WING INBD MID FLAP MOST OTBD T/E FOUND CRACKED (RT WING INBD MID FLAP MOST OTBD T/E LWR SURFACE COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A. DETAIL REF HX PROCESS CARD SEQ NT EAX 500294-1)SDR UIEA2009080500001Door · damagedDURING WALK AROUND INSP BEING PERFORMED; GROUND DAMAGE FOUND ON THE BS 1112.1, BS 1170 AIR CONDITIONING ACCESS DOOR 192 HR. THE DAMAGE PENETRATED THROUGH THE HONEYCOMB MATERIAL (REF FIG 1)(PERFORMED A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONSDR UIEA2010080500137Door · damagedEO 4453A264: GROUND DAMAGE FOUND ON THE BS 1112.1-1170 AIR CONDITIONING ACCESS DOOR 192 HR. THE DAMAGE PENETRATED THROUGH THE HONEYCOMB MATERIAL. (PERFORMED A TIME LIMITED REPAIR AS DESCIBED IN PART 1 WORK INSTRUCTIONS. SCHEDULE PART 2 PRIOR TO THE ACCUMULATISDR UIEA201000181Door · damagedGROUND DAMAGE FOUND ON THE BS 1112.1 - 1170 AIR CONDITIONING ACCESS DOOR 192HR. THE DAMAGE PENETRATED THROUGH THE HONEYCOMB MATERIAL (REF FIG 1.) "TIME LIMITED REPAIR IAW PART 1 WORK INSTRUCTIONS. SCHEDULE PART 2 PRIOR TO THE ACCUMULATION OF 5 CYCLES IN ACC WISDR UIEA200900033Acm · failedAIR TURN BACK, AFTER TAKEOFF UNABLE TO MAINTAIN CABIN PRESSURE DURING CLIMB. NR 1 PACK ON MEL AND NR 3 PACK FAILED DURING CLIMB. NR 2 PACK WAS UNABLE TO MAINTAIN PRESSURE. REPLACED NR 3 ACM, PERFORMED OPS CHECK, ALL NORMAL.SDR UIEA201000122Support · damagedTHE PURPOSE OF THIS EO IS TO RECORD A MAJOR REPAIR. DURING C CHECK INSPECTION BEING PERFORMED AT HKG; DAMAGE WAS FOUND TO THE RIGHT O/B MID FLAP NR 3 TRAILING EDGE PANEL SUPPORT (I/B OF NR 8 CARRIAGE) CONSISTING OF A SCREW HOLE ELONGATED (REFERENCE FIGURE 1).SDR UIEA201000121Support · damagedTHE PURPOSE OF THIS EO IS TO RECORD A MAJOR REPAIR. DURING C CHECK INSPECTION BEING PERFORMED AT HKG; DAMAGE WAS FOUND TO THE LEFT I/B UPPER TRAILING EDGE FIXED PANEL O/B SUPPORT WEB (REFERENCE FIGURE 1). PERMANENT REPAIR PERFORMED IN ACCORDANCE WITH THE 747SDR UIEA200800266Circuit Card · failedMASTER CAUTION/ FIRE WARNING BELL ON GROUND. NO EICAS MESSAGE (NO OTHER LIGHTS OR WARNINGS). REPLACED A15 CARD AT THE M5206 MODULE. OPS CHECKED OK. (S)SDR UIE2008F00000Fire Warning · false activationREF: LOG PAGE 362049; TWICE DURING CRUISE, MOMENTARY ILLUMINATION OF MASTER WARNING LIGHTS WITH ASSOCIATED FIRE WARNING BELL. NO EICAS MESSAGE. ACCOMPLISHED CMC GROUND TEST FIRE PROTECTION SYSTEM. (TEST PASS) NO FAULTS IN CMC FAULT HISTORY, MM26-10-00. (K)SDR UIEA200800035Skin · damagedFOUND LIGHTNING STRIKE AT STATION 166 STRINGER 46R. REPAIRED AS PER SRM 53-00-01 FIGURE 201 REPAIR 1 AND AS PER BOEING MESSAGE 1-764547003-7 AND FAA FORM 8100-9.SDR UIEA200800031Fitting · chafedDURING SCHEDULED MAINTENANCE, FOUND NR 4 PYLON WEAR DAMAGE ON THE LUG FACE OF THE UNDERWING MIDSPAR FITTINGS. THE DAMAGE WAS REMOVED FROM THE LUG SURFACES BY BLENDING SMOOTH. THE FITTINGS WERE CONFIRMED FREE OF CRACKS AND OTHER DAMAGE BY DETAIL VISUAL AND NDSDR UIEA200800030Lug · chafedDURING SCHEDULED MAINTENANCE FOUND NR 1 PYLON WEAR DAMAGE ON THE LUG FACE OF THE UNDERWING MIDSPAR FITTINGS. THE DAMAGE WAS REMOVED FROM THE LUG SURFACES BY BLENDING SMOOTH. THE FITTINGS WERE CONFIRMED FREE OF CRACKS AND OTHER DAMAGE BY DETAIL VISUAL AND NDTSDR UIEA200800034Skin · scratchedFOUND NICK ON FUSELAGE SKIN STATION 2200 STRINGER 22L-23L. REPAIRED AS PER SRM 53-00-01 REPAIR 1 DETAIL 3 FIGURE 201 AND 53-60-01 FIGURE 1 AND SRM 51-40-06 FIGURE 3SDR UIEA200800033Skin · scratchedSCRATCH ON FUSELAGE SKIN AT STATION 1790 BETWEEN STRINGER 38L-39L. INSPECTED AS PER SRM 51-10-02. REPAIRED AS PER SRM 53-00-01 REPAIR 1 FIGURE 201.SDR UIEA200800032Floor Support · crackedMAIN DECK CARGO COMPARTMENT FLOOR PANEL SUPPORT CRACKED AT STATION 531 AND 688 RBL 116. REPAIRED FLOOR PANEL SUPPORT AS PER BOEING DOCUMENT RDR 0691225-1 TO 5.SDR UIEA200700442Skin · crackedDURING LEFT WING LIGHT REPLACEMENT THE PLATFORM SUDDENLY LOWERED AND HIT THE LEADING EDGE SKIN. THE PLATFORM MOVEMENT CAUSED A 15 INCH VERTICAL CRACK. A TIME LIMITED REPAIR WAS ACCOMPLISHED AS PER XEO 57-101007 PART 1 AND SRM 57-41-01 REPAIR 4. PERMANENT REPSDR UIEA200600278Intercostal · crackedA/C M415MC: PERFORMED INTERIM REPAIR TO MAIN DECK SIDE CARGO DOOR INTERCOSTAL CUT-OUT IAW XEO 52-102106, A/C OK FOR CONTINUED OPERATIONS FOR UP TO 6 FLIGHT CYCLES. INTERCOSTAL CUT-OUT WEB REPAIRED IAW SRM 51-70-13 REPAIR FIG 201.SDR UIEA200600224Seat Track · crackedN415MC AT PIK FOR MSG-3, CHECK C-4 & A-4. AS PER N/ROUTINE 163 FWD CARGO SEAT TRACK AT BS 560 LBL 45.5 HAS 6 INCH CRACK AND N/ROUTINE 188 FWD CARGO SEAT TRACK AT BS 560, LBL 25 HAS TWO HOLES. NR 4453A083 WAS GENERATED. FOR N/ROUTINE 163 REPAIR ACCOMPLISHED SDR UIEA200600223Shim · migratedN415MC AT PIK FOR MSG-3 CHECK C-4 & A-4. AS PER N/ROUTINES 168, 169 AND 210, AFT AND FWD CARGO DOORS HINGE SHIMS MIGRATED. XEO 53-082906 WAS GENERATED. REPAIR ACCOMPLISHED TO THE AFT & FWD CARGO DOOR HINGE SHIMS MIGRATION AS PER SRM 51-20-08 AND 50 PERCENT SDR UIEA200600222Fan Blade · lack of lubeN415MC AT PIK FOR MSG-3, C-4&A-4 CHECK. AS PER N/ROUTINE 154, NR 1 ENGINE S/N 704-916 FAN BLADES REMOVED FOR LUBRICATION. IT WAS FOUND, FAN DISKS HAVE NO EVIDENCE OF LUBRICANT. INSPECTION PERFORMED IAW MM 72-31-00, 206 TABLE 601 NR 1 DOVETAILS ON FAN DISK HSDR UIEA200600221Skin · corrodedN415MC AT PIK FOR MSG-3 CHECK C-4 & A-4. AS PER N/ROUTINE 105 LEFT WING UPPER SURFACE WS 752-779 FIVE BLENDED & RESURFACED AREAS ON THE OUTER AREA. FWD MOST DEPTH TO BE CHECKED. FWD BLEND OUT CHECKED BETWEEN WS 752 - WS 779. MAX DEPTH OF BLEND OUT = 0.017 SDR UIEA200600118Lever · brokenSEVERE COMPRESSOR STALL ON ENGINE NR 4 WITH FULL CLIMB POWER AT 6000 FEET ON CLIMBOUT FROM DXB. ENGINE NR 4 ROLLED BACK TO IDLE, OVERTEMP EGT INDICATION. NR 4 ENGINE SHUT DOWN. FUEL JETTISON ACCOMPLISHED. UNEVENTFUL SMOOTH AUTO LAND RWY 30R AT 299.0 TONS. SDR UIEA200300070Skin · bird strikeRIGHT INBOARD FLAP FOREFLAP DAMAGE. BIRD STRIKE ON RIGHT WING L/E FLAPS. PERFORMED INSPECTION PER MM 5-51-14, FOUND RIGHT INBOARD FLAP FOREFLAP DAMAGED OUT OF SRM LIMITS. REMOVED FLAP AND REPAIRED IAW SRM 51-70-07 AND MM 57-52-31. INSTALLED FLAP AS EPR MM
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