N886AS

Service difficulty reports · 165

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 = 'N886AS' 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 ASOA201100982Structure · chafedPAX DOOR, ICE DOOR HAS CHAFE DAMAGE FROM CABLE. BLENDED CHAFED DAMAGE FROM CABLE DAMAGE ON PAX DOOR. ICE DOOR BLENDED AREA DEPTH 15.043 ON STIFFINER MAX ALLOWED IS .100 DAMAGED AREA IS WITHIN SERVICEABLE LIMITS. REPAIR TO THE NICK/ GOUGE DAMAGE ON THE VENT FMay 13, 2011 · N886AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201100975Isolator · brokenPRESSURE BULKHEAD 621 HAS ONE BROKEN ISOLATOR MOUNT ON THE FWD SIDE. R & R ISOLATOR MOUNT ON THE FWD SIDE OF PRESSURE BULKHEAD 621 WITH NEW SERVICEABLE MOUNT IAW SRM 51-42-13.May 13, 2011 · N886AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201100974Skin · corrodedCORROSION AROUND SCREW HOLE ON INNER SKIN OF SERVICE DOOR JUST ABOVE HINGE POINT. BLENDED CORROSION AROUND SCREW HOLE ON INNER SKIN OF SERVICE DOOR JUST ABOVE HINGE POINT, ORIGINAL MAT .063. REMOVED .001 OF MATERIAL REMAINING MATERIAL IS .062 IS WITHIN SERVMay 13, 2011 · N886AS · Cndair CL6002B19 · Service DoorsSDR ASOA201100965Skin · gougedEXTERNAL FUSELAGE BELLY SKIN FS409.0+96 , BL 0.00 IS GOUGED. BLENDED GOUGE ON EXTERNAL FUSELAGE BELLY SKIN FS 409.0+96 BL 0.00 IAW SRM 51-12-00. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-31. THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY.(CLOSED)May 13, 2011 · N886AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201100962Attach Angle · crackedATTACH ANGLE FOR INTERCOSTAL AT FS 484, LBL 37 IS CRACKED. REPAIRED ATTACH ANGLE IAW REO 601R-53-41-059.May 13, 2011 · N886AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201100961Angle · crackedLEFT OBLIQUE ANGLE CRACKED, FS 621 REAR PRESSURE BULKHEAD. REMOVED UNSERVICEABLE ANGLE& INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-21 AND SRM 51-40-11. MAJOR REPAIR.May 13, 2011 · N886AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100958Skin · crackedRIGHT WING LOWER PLANK SKIN CRACKED, AFT EDGE BEHIND REAR SPAR AT APPROX WS 148. REPAIRED IAW EO 600-57-134. MAJOR REPAIR.May 12, 2011 · N886AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA201100953Frame · corrodedRIGHT OTBD END OF FRAME FS 349.0 IS CORRODED. BLENDED FRAME, ORIGINAL MAT'L .063. REMOVED .003. REMAINING MAT'L .060, WITHIN SERVICABLE LIMITS IAW SRM 51-12-00. MAJOR REPAIR.May 12, 2011 · N886AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201100952Frame · crackedFS 280.0 FRAME CRACKED, OTBD OF RBL 9.0. R & R DAMAGED SECTION OF FRAME IAW REO 601R-53-11-136 REV A. MAJOR REPAIR.May 12, 2011 · N886AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201100951Attach Fitting · crackedVERTICAL CLIP, FS 280.0, LBL 9.0 CRACKED. R & R VERTICAL CLIP IAW SRM 51-42-21. MAJOR REPAIR.May 12, 2011 · N886AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201100950Attach Fitting · crackedVERTICAL CLIP FS 280.0, RBL 9.0 CRACKED. R & R VERTICAL CLIP9 IAW SRM 51-42-21. MAJOR REPAIR.May 12, 2011 · N886AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201100949Seat Track · corrodedRIGHT NR 1 SEAT TRACK CORRODED. R & R FLOOR SEAT TRACK WITH NEW SERVICABLE SEAT TRACK IAW AMM 53-01-11.May 12, 2011 · N886AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100948Seat Track · corrodedLEFT NR 1 SEAT TRACK IS CORRODED. R & R SEAT TRACK IAW AMM 53-01-11.May 12, 2011 · N886AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001712Angle · crackedFS 559.0, LBL 18 CRACK INDICATED ON CAP ANGLE. COMPLIED WITH EC/TC REO 601R-53-41-260 AND REO 601R-53-41-260 REV E.Nov 1, 2010 · N886AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001544Light · inoperativeTHE NR 2 OVERHEAD EMERGENCY LIGHT IS INOP. REPLACED THE NR2 OVERHEAD EMERGENCY LIGHT. OPS CHECK GOOD. DONE IAW THE AMM CHAP 33-51-16. (CLOSED)Oct 11, 2010 · N886AS · Cndair CL6002B19 · Emergency LightingSDR ASOA200900778Light · brokenWARDROBE FLOOR EMERGENCY FLOOD LIGHT BASE IS BROKEN.Jul 14, 2009 · N886AS · Cndair CL6002B19 · Emergency LightingSDR ASOA200900775Handle · out of adjustLEFT OVERWING EMERGENCY EXIT FAILS HANDLE PULL TEST, PULL WEIGHT IN EXCESS OF 50LBS.Jul 13, 2009 · N886AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA200900774Handle · out of adjustRIGHT OVERWING EMERGENCY EXIT FAILS HANDLE PULL TEST, PULL WEIGHT IN EXCESS OF 50LBS.Jul 13, 2009 · N886AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA200900762Sign · inoperativeMID CABIN CURVED FWD FACING EMERGENCY EXIT SIGN INOP.Jul 12, 2009 · N886AS · Cndair CL6002B19 · Emergency LightingSDR ASOA200900758Sign · inoperativeFLOOR LEVEL EMERGENCY EXIT SIGN AT LT OVERWING EXIT INOP.Jul 11, 2009 · N886AS · Cndair CL6002B19 · Emergency LightingSDR ASOA200900743Skin · crackedVERTICAL CRACK INDICATION NOTED ON INTERIOR FUSELAGE SKIN AT FS 640 AND STR 10L APPROX 0.125 AFT OF UPPER SKIN CUTOUT AND 1.437 INCH IN LENGTH. FAILED NDT INSPECTION AT 100 FSH.Jul 3, 2009 · N886AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA200900731Sill · corrodedTHE PAX DOOR LOWER SILL ANGLE IS CORRODED. REMOVED SILL AND IAW SRM 51-42-06, 51-42-13, AND 51-42-21. LOCATED AND DRILLED SERVICEABLE ANGLE IAW SRM 51-40-11. INSTALLED IAW SRM 51-42-06, 51-42-13 AND 51-42-21.Jun 25, 2009 · N886AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200900730Frame · damagedTOP FLANGE OF FRAME AT FS 628.0 BOTTOM, 2 INCHES LEFT OF STR 27 IS DENTED AND CRACKED. DENT MEASURES APPROX 1 INCH LONG X .50 INCH WIDE X .020 INCH DEEP, CRACK MEASURES APPROX .30 INCH LONG. REPAIR OF THE CRACK & DENT DAMAGE ON TOP FLANGE IAW REO 601R-53-61-Jun 25, 2009 · N886AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA200900719Frame · corrodedFS 349.00 AT STRINGER 27 HAS CORROSION ON FRAME. REMOVED 6 RIVETS TO ACCESS CORROSION. REMOVED CORROSION IAW SRM 51-21-06. INSTALLED RIVETS WET WITH SEALER IAW SRM 51-42-06 AND SRM 51-23-00. PRIMED AND PAINTED REPAIRED AREA IAW SRM 51-25-01. SLIGHTLY CORJun 25, 2009 · N886AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA200900718Attach Angle · crackedFS 484, RBL 27 OUTBOARD UNDER FLOOR INTERCOSTAL ATTACH ANGLE CRACKED.Jun 25, 2009 · N886AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900717Attach Angle · crackedFS 484, LBL 27 OUTBOARD UNDER FLOOR INTERCOSTAL ATTACH ANGLE CRACKED. REPAIRED FS 484 LBL 27 O/B ATTACH ANGLE IAW REO 601R-53-41-059.Jun 25, 2009 · N886AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900716Seat Track · corrodedFLOOR SEAT TRACK LOCATED IN CARGO BAY AT FS 559.0+80 RBL 27 IS CORRODED. REMOVED FLOOR SEAT TRACK LOCATED IN CARGO BAY AT FS 559.0 + 80 RBL 27. INSTALLED NEW SERVICEABLE SEAT TRACK USING EXISTING HARDWARE AND APPLIED ADHESIVE TO BOTTOM SIDE IAW SRM 51-22-00Jun 25, 2009 · N886AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA200900714Anchor Fitting · crackedTHE AFT PAX DOOR ANCHOR FITTING IS CRACKED. REMOVED PAX DOOR AFT COUNTER BALANCE ANCHOR AS REQUIRED IAW AMM 52-11-17-000-804. INSTALLED NEW PAX DOOR ANCHOR ASSY AS REQUIRED IAW AMM 52-11-17-400-804. PAX DOOR REQUIRES ADJ/TEST. C/W ADJUSTMENT AND OPS CHECK Jun 25, 2009 · N886AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200900713Intercostal · crackedRT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX .70 INCH LONG. REMOVED AND REPLACED RT FS 621.00 TO FS 625.30 STR 14R INTERCOSTAL IAW SRM 51-42-21.Jun 25, 2009 · N886AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200900693Handle · bindingPAX DOOR OUTER HANDLE IS TOO HARD TO OPEN. CLEANED AND LUBRICATED PAX DOOR OUTER HANDLE IAW AMM 12-20-52-640-813. C/W OPS CHECK OF THE PAX DOOR OUTER HANDLE IAW MM 52-11-03-710-802 AND THE PAX DOOR HANDLE CHECKS GOOD AT THIS TIME.Jun 22, 2009 · N886AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200900364Light · inoperativeAFT 2 CEILING EMERGENCY LIGHT ARE INOP.Mar 30, 2009 · N886AS · Cndair CL6002B19 · Emergency LightingSDR ASOA200900073Flap · failedFLAPS FAIL AT 0 WHEN SELECTING 8. FLT 5248, 5668 CX & ON 1/16/09 FLT 5339 CX-C/O.Jan 15, 2009 · N886AS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA200801495Oil System · malfunctionedRT ENG OIL PRESSURE MSG IN FLT. OIL PRESSURE FLUX BETWEEN 40-24 PSI, FOLLOWED QRH EMERGENCY, 1-13 OIL PRESS WENT TO 24 PSI, IN FLT ENG SHUTDOWN PER QRH. EN ROUTE TO ATL A/C DIVERTED TO MCI DUE TO MTC - EMERGENCY DECLARED. REMOVED AND REPLACED NR 2 ENG IDG, Nov 13, 2008 · N886AS · Cndair CL6002B19 · Engine Oil PressureSDR TRAX200800941Light · inoperativeNR 1 INTERIOR CEILING EMERGENCY LIGHT OUT. REMOVED AND REPLACED INTERIOR CEILING EMERGENCY LIGHT LAMP. OPS CHECK GOOD IAW AMM 33-51-16. (S)Jul 28, 2008 · N886AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200800713Step · crackedPAX DOOR UPPER STEP HAS CRACK APPROXIMATELY 4" LONG REMOVED AND REPLACED PAX DOOR TOP STEP IAW AMM 52-11. (B)May 30, 2008 · N886AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200701484Light · malfunctionedEMERGENCY LIGHT ON IN ARMED POSITION.Oct 8, 2007 · N886AS · Cndair CL6002B19 · Emergency LightingSDR TRAX200700867Angle · crackedFS 280 I/B CLIP ON RBL 9 IS CRACKED. REMOVED CRACKED ANGLE. DUPLICATED ANGLE USING PERFORMED ANGLE P/N S6144-3. INSTALLED SERVICEABLE ANGLE IAW CRJ SRM 51-42-21. NEW ANGLE INSTALLED AT FS 280 RBL 9. SUPPLEMENTAL - SDR CLOSED 06/26/07.Jun 18, 2007 · N886AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200700880Skin · crackedPAX DOOR INTERNAL SKIN IS CRACKED AT AFT CORNER OF LOWER STEP. REMOVED LOWER PAX DOOR STEP SUPPORT ANGLE LOWER SECTION OF PAX DOOR AFT DRAG ANGLE TO GAIN ACCESS FOR MEASUREMENT OF DAMAGE AND REPAIR. DH752 MADE ALL DETAILS, DEBURRED ALL, TOUCH UP ALODINE, PRIJun 15, 2007 · N886AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200700879None · nonePAX DOOR INNER SKIN CRACKED UNDER STEP 832ET (FWD SIDE). [06-28-07] UPON FURTHER EVALUATION FOUND TO BE LIMITED TO PAINT ONLY.Jun 15, 2007 · N886AS · Cndair CL6002B19 · Standard Practices/StructuresSDR TRAX200700856Handle · crackedPAX DOOR EXTERNAL HANDLE FLAPPER IS CRACKED. [06-26-07] REPAIRED IAW CRJ SRM 51-42-06, 51-25-06, 51-25-16, AND CRJ MM 11-20-00.Jun 15, 2007 · N886AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200700184Frame · crackedSUSPECT CRACK ON LEFT SIDE FS 640 FRAME.Feb 6, 2007 · N886AS · Cndair CL6002B19 · Fuselage Main, FrameSDR TRAX200600784Step · crackedTOP ASD STEP CRACKED.Sep 23, 2006 · N886AS · Cndair CL6002B19 · Entrance StairsSDR TRAX200600570Support Beam · crackedENG SUPPORT BEAM AT LT FWD (LOWER) PNL CRACKED FROM BOLT TO EDGE OF PNL OPENING.Aug 1, 2006 · N886AS · Cndair CL6002B19 · Fuselage Main, StructureSDR TRAX200600171Step · crackedASD BOTTOM STEP CRACKED AT ATTACH LINK.May 6, 2006 · N886AS · Cndair CL6002B19 · Entrance StairsSDR ASOA06323Handle · crackedDURING A HANGAR INSPECTION, THE PASSENGER DOOR OUTER HANDLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR OUTER HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Mar 16, 2006 · N886AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA06104Threshold · corrodedDURING A C-CHECK, THE SERVICE DOOR THRESHOLD PLATE WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SERVICE DOOR THRESHOLD PLATE IAW SRM 51-40-00. (K)Jan 20, 2006 · N886AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA06100Seat Track · corrodedDURING A C-CHECK, THE CARGO COMPARTMENT SEAT TRACKS, ON LBL 9 AND RBL 9, AFT OF FS 559+80, WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CARGO COMPARTMENT SEAT TRACKS, ON LBL9 AND RBL9, AFT OF FS 559+80, IAW SRM. (K)Jan 19, 2006 · N886AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA06099Clip · crackedDURING A C-CHECK, THE INB AND OB FS 280 CLIPS, LBL9, WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE IB AND OB FS 280 CLIPS, LBL9, IAW SRM 51-42-21. (K)Jan 18, 2006 · N886AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA051022Lamp · burned outFLT 4537 - DURING A GROUND INSPECTION IN SHV, THE EMERGENCY EXIT LIGHT, NEAR THE PASSENGER DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT, NEAR THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT ONov 26, 2005 · N886AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05632SAnchor Fitting · crackedDURING HANGAR MAINTENANCE, THE AFT ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 24, 2005 · N886AS · Cndair CL6002B19 · Entrance Stairs
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