N837AS, cancelled Jun 8, 2017

Service difficulty reports · 125

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 = 'N837AS' AND deregistration_id = 'N837AS-2017-06-08'
  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 ASOA2015021312223Isolator · brokenAFT PRESSURE BULKHEAD ISOLATOR ABOVE WL 73.50 ON RBL 9.50 IS BROKEN. REMOVED DEFECTIVE ISOLATOR AND INSTALLED NEW ISOLATOR IAW SRM 51-42-13. REPAIR CLASSIFIED AS MINOR IAW GMM 5-3.Feb 9, 2015 · N837AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015021312222Isolator · brokenAFT PRESSURE BULKHEAD ISOLATOR ABOVE WL 73.50 ON LBL 9.50 IS BROKEN. REMOVED DEFECTIVE ISOLATOR AND INSTALLED NEW ISOLATOR IAW SRM 51-42-13. REPAIR CLASSIFIED AS MINOR IAW GMM 5-3.Feb 9, 2015 · N837AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015020412142Light · intermittentPASSENGER CABIN CEILING EMERGENCY LIGHT INTERMITTENT. R & R THE CEILING EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.Jan 31, 2015 · N837AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014111311637Structure · damagedDAMAGE NOTED ON REPAIR MADE TO UPPER LT WING ROOT. COMPLIED WITH GREO 601R-53-41-341Nov 10, 2014 · N837AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2014091911269Connector · unsecureENTRY LEVEL EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND RESEATED CONNECTOR ON EMERGENCY EXIT LIGHT ASSY AT ENTRY LEVEL AND REINSTALLED LIGHT ASSY IAW AMM 33-51-10, OPS CHECKED GOOD. ACFT OK FOR SERVICE.Sep 16, 2014 · N837AS · Cndair CL6002B19 · Light System WiringSDR ASOA2014021909973Battery · inoperativeNR 3 EMERGENCY BATTERY INOPERATIVE. R & R NR 3 EMERGENCY BATTERY IAW AMM 33-51-04. OPS CHECKED GOOD.Feb 15, 2014 · N837AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013090608966Battery Pack · dischargedF/A FLASHLIGHT INOPERATIVE. REPLACED FA FLASHLIGHT BATTERIES. OPS CHECKED GOOD IAW AMM 25-61-00.Sep 4, 2013 · N837AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA2013051303508Drag Angle · crackedCRACK AT PAX DOOR AFT DRAG ANGLE BY FITTING.May 8, 2013 · N837AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2013031103150Bulb · burned outRT NR 3 EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-51-21. OPS CHECKED GOOD.Mar 7, 2013 · N837AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013030503106Light · crackedEXIT/PULL BETA LIGHT ON PAX DOOR LATCH/LOCK LEVER FOUND TO BE CRACKED. R & R CRACKED BETA EXIT/PULL LIGHT ON PAX DOOR LATCH/LOCK LEVER WITH NEW IAW AMM 20-21-00-901-801.Feb 27, 2013 · N837AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2013030103093Seat Track · corrodedSEAT TRACK ON LBL 9 BETWEEN FS 409+126 TO FS 559+4 HAVE NUMEROUS SPOTS OF CORROSION. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802, SUBTASK 53-01-11-020-002, PART B. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW MM TASK 53Feb 13, 2013 · N837AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013030503105Seat Track · corrodedSEAT TRACK RBL 9.0 FS 559.00 - 559.00+80 HAS NUMEROUS SPOTS OF MINOR CORROSION. R & R DAMAGED SEAT TRACK IAW MM TASK 53-01-11-000-802 AND GREO 601R-53-00-485.Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013030503104Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED APPROX 3.0" IN LENGTH 70 PERCENT FSH AT BL 0.0 WL 108 TO WL 111. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-4813.Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013030503103Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT BL 0.0, WL 136.0 APPROX 1.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH REO 601R-53-61-4813.Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013030103092Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED APPROX 3.0" IN LENGTH 70 PERCENT FSH AT BL 0.0, WL 108 TO WL 111. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1285 REV D, DATED 10/31/2011.Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013030103091Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT BL 0.0, WL 136.0, APPROX 1.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-4813.Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013030103090Angle · corrodedAFTER REMOVAL OF THE DRAINAGE RAMP IN LWR PAX DOOR FOUND BOTH ANGLES AT FS 320.10 AND THE CLIPS AT FS 338.00 ARE CORRODED BEYOND LIMITS. R & R THE ANGLES IAW SRM 51-42-06.Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013030103089Angle · corrodedAFTER REMOVAL OF THE DRAINAGE RAMP IN LWR PAX DOOR, FOUND THE AFT CORNER HAS CORROSION BEYOND LIMITS AND THE FWD CORNER. REMOVED THE PAX DOOR FWD LWR CORNER IAW SRM 51-42-06, SRM 51-42-13 AND SRM 51-42-21. INSTALLED THE NEW PAX DOOR FWD LWR CORNER IAW SRM 51Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013030103088Seat Track · corrodedSEAT TRACK LBL 9.00 FS 364-409+128 IS SEVERELY CORRODED. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013030103087Floorbeam · crackedFLOORBEAM CRACKED AT RBL 9.00 AND LBL 9.00 BETWEEN FS 559.00. REPAIRED IAW SRM 51-42-06.Feb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2013022803085Seat Track · corrodedSEAT TRACK ON RBL 9.00 FROM FS 364.00 TO FRAME STATION 409+128 HAS NUMEROUS SPOTS OF MINOR CORROSION. REMOVED RBL 9.00 FS 364.00-399.50 CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK PN 601R31032-15 IAW AMM 53-01-11-400-802. REMOVEDFeb 12, 2013 · N837AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013030503102Spar · crackedCRACK AT LT WS 148.019 AND THE REAR WING SPAR. AN INDICATION WAS NOTED APPROX .250L .60 PERCENT FULL SCREEN HEIGHT. REPAIRED LT WS 148.019 IAW REO 601R-57-21-130 AND 601R-57-21-131.Feb 8, 2013 · N837AS · Cndair CL6002B19 · Wing SparSDR ASOA2013022803084Seat Track · corrodedLT FLOOR SEAT TRACK, LBL 9 CORRODED THROUGH SIDE OF SEAT TRACK, FS 364.00 - FS 399.50. REMOVED CORRODED FLOOR SEAT TRACK FROM FS 364.00 - FS 399.00, LBL 9 IAW AMM SUBTASK 53-01-11-020-002, FIG 401.B. INSTALLED NEW SEAT TRACK IAW AMM SUBTASK 53-01-11-420-001Feb 8, 2013 · N837AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013022803083Post · crackedFOUND FS 409+128 VERTICAL POST BL0.0 LT SIDE HAS INDICATION NOTED APPROX 3" IN LENGTH, 50 PERCENT FSH AT AFT FLANGE RADIUS WL 69.0. FAILED NDT INSPECTION. REMOVED POST AT STA 409+128 BL 0 IAW SRM 51-42-06. DRILLED UP NEW POST PN 601R32208-159, ASSY AND INSTFeb 8, 2013 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012092702305Light · crackedEMERGENCY LIGHT NEXT TO PASSENGER DOOR HAS A CRACKED FRAME. R & R FLOOD LIGHT, FLOOR LEVEL EMERGENCY LIGHT ASSY IAW AMM 33-51-11. OPS CHECKS GOOD ACFT GOOD FOR SERVICE. SDR CLOSED.Sep 23, 2012 · N837AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201201712Wire · disconnectedWIRES FOUND DISCONNECTED FROM EXIT SIGN, BELOW F/A JUMPSEAT. RECONNECTED AND RESECURED BROKEN WIRE TO FWD ENTRY WAY LIGHTED FLOOR LEVEL EXIT SIGN IAW AMM 33-51-10. OPS CHECKED GOOD.May 31, 2012 · N837AS · Cndair CL6002B19 · Light System WiringSDR ASOA201100264Light · inoperativePAX DOOR AND SERVICE DOOR EMERGENCY LIGHTS INOP. R & R BOTH PAX DOOR AND SERVICE DOOR EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD.Feb 11, 2011 · N837AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201100210Wire · brokenWIRE FOR EMERGENCY LIGHT ON WARDROBE BROKEN. REPLACED SPLICE WITH QUARTER TURN QUICK DISCONNECT. OPS TEST OF EMERGENCY LIGHTS REQUIRED IAW 33-51-00-710-801. PERFORMED OPS TEST OF EMERGENCY LIGHT IAW 33-51-00-710-801. ALL CHECKS GOOD AT THIS TIME.Feb 3, 2011 · N837AS · Cndair CL6002B19 · Light System WiringSDR ASOA201100209Floorbeam · corrodedFLOORBEAM CAP AT RBL 27 FS 621 IS CORRODED. REO 601R-53-61-3968 REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORKCARD. ALL RII'S HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTOR IAW GFeb 3, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201100191Floorbeam · corrodedFLOORBEAM CAP AT LBL 27, FS 621 TO FS 574 IS CORRODED. REPAIRED.Jan 31, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201100190Floorbeam · corrodedCORROSION FOUND ON RT END OF FLOORBEAM, NEAR SERVICE DOOR. REO 601R-53-21-1230 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. RETURNED TO SERVICE.Jan 31, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201100165Isolation Mount · crackedFWD BULKHEAD ISOLATION MOUNT CRACKED. R & R ISOLATOR MOUNTS ON FWD BULKHEAD FS 621 IAW SRM 51-42-06.Jan 25, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201100135Frame · crackedFS 605, LEFT FRAME IS CRACKED AT FASTENERS JUST BELOW WL 73. REMOVED DAMAGED FRAME IAW SRM 51-42-06, PARA 11, PG 18. LOCATED, DRILLED AND INSTALLED NEW FRAME SECTION PN 601R36026-29 IAW SRM 51-42-06, 51-42-21, 51-40-11.Jan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201100134Doubler · corrodedLT PRESSURE FLOOR SKIN DOUBLER OTBD OF LBL 36 JUST FWD OF FS 544 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR SKIN DOUBLER IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PREVIOUS BLENDOUT WAS .010. REMOVED .003 MORE MATERIAL MAKING .013 TOTAL MATERIAL Jan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA201100133Doubler · corrodedRT PRESSURE FLOOR SKIN DOUBLER OTBD OF RBL 36 AT FS 529 IS CORRODED. REMOVED CORROSION ON RT PRESSURE FLOOR SKIN ASSY IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS .010 FROM PREVIOUS BLENDOUT. REMOVED .004 MORE MATERIAL MAJan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA201100132Floor Skin · corrodedLT PRESSURE FLOOR SKIN OTBD OF LBL 36 IS CORRODED AT FS 461. REMOVED CORROSION ON RT PRESSURE FLOOR SKIN ASSY IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS .010 FROM PREVIOUS BLENDOUT. REMOVED .002 MORE MATERIAL MAKING .012Jan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA201100131Doubler · corrodedLT PRESSURE FLOOR SKIN DOUBLER AT FS 461 OTBD OF LBL 36 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR DOUBLER IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS .010 FROM PREVIOUS BLENDOUT DATED 1/21/09. REMOVED .002 MORE MJan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA201100130Doubler · corrodedLT PRESSURE FLOOR SKIN DOUBLER OTBD OF LBL 36 AT FS 424 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR SILL ASSY (SKIN DOUBLER) IAW REO 601R-53-41-666. MATERIAL LOSS IS .003, REMAINING MATERIAL IS .077. MINIMUM ALLOWABLE MATERIAL THICKNESS IS .055. AREJan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA201100129Doubler · corrodedLT PRESSURE FLOOR SKIN DOUBLER OTBD OF LBL 36 AT FS 449+85 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR SILL ASSY (SKIN DOUBLER) IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS .010 FROM PREVIOUS BLENDOUT DATED 1/21/09.Jan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA201100128Doubler · corrodedLT PRESSURE FLOOR SKIN DOUBLER OTBD OF LBL 36 AT FS 544 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR SILL ASSY (SKIN DOUBLER) IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS .010 FROM PREVIOUS BLENDOUT. REMOVED .002 MOJan 19, 2011 · N837AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA201100120Floor Support · crackedFLOOR SUPPORT ANGLE AT FS 621 ON OTBD RT SIDE IS CRACKED IN THE RADIUS. REPLACED EXISTING REPAIR WITH NEW SERVICEABLE PARTS IAW REO 601R-53-61-117, REV C, STEPS 1 THRU 7. REPAIR OF THE DAMAGED PORTIONS OF ANGLE 601R35031-239 IS COMPLETED IAW REO 601R-53-61-1Jan 17, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100109Attach Fitting · crackedFS 280 AND RBL 9, LBL 9 CLIPS ARE CRACKED. R & R CLIPS AT FS 280 LBL 9 INBD AND OTBD AND RBL 9 INBD IAW SRM 51-42-21.Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201100092Angle · corrodedFWD "J" ANGLE AT FS 280 IS CORRODED. FOUND FWD "J" ANGLE CORRODED BEYOND LIMITS. REMOVED FS 280 FWD ANGLE IAW SRM 51-42-06. CLASSIFIED AS A MINOR REPAIR.Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100091Web · crackedFS 280, LOWER WEB AT RBL 11.0 IS CRACKED. REPAIRED IAW REO 601R-53-11-926, REV B.Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100090Floorbeam · corrodedCORROSION FOUND ON RT END OF FLOORBEAM, PN 601R32005-1, NEAR SERVICE DOOR. REPAIRED IAW REO 601R-53-21-1230.Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201100089Floor Support · corrodedRT CARGO FLOOR SUPPORT FROM FS 621 TO FS 559+80 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED FLOOR SUPPORT AND LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SILL IAW REJan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100088Floor Support · corrodedFLOORBEAM CAP AT RBL 27, FS 621 TO 574 IS CORRODED. REMOVED FLOORBEAM CAP RBL 27 FS 574 TO FS 621.00 IAW SRM 51-42-06. LOCATED AND DRILLED UP NEW CAP IAW SRM 51-40-11, SRM 51-42-06 AND SRM 51-42-21. RBL 27, INSTALLED RBL 27, FLOORBEAM CAP IAW REO'S 601R-Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100087Floor Support · corrodedLT CARGO FLOOR SUPPORT SILL FROM FS 621 TO FS 559+80 IS CORRODED. REMOVED AND LOCATED NEW FLOOR SILL IAW SRM 51-42-06 AND 51-42-21.Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100085Floor Support · corrodedFLOORBEAM CAP AT LBL 27, FS 621 TO FS 574 IS CORRODED. REMOVED AND LOCATED AND DRILLED NEW CAP IAW SRM 51-42-06 AND 51-42-21.Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100084Cargo Track · corrodedCARGO TRACKS LBL 27, LBL 9, & RBL 27 ARE CORRODED. REPLACED CARGO TRACKS IAW SRM 51-41-02.Jan 13, 2011 · N837AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
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