N889AS

Service difficulty reports · 162

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 = 'N889AS' 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 SWIA2020050150427Stringer · crackedSTGR 3 CRACKED ON OUTBOARD SIDE AT FS 280.0. (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED SPLICE ANGLE ON OUTBOARD SIDE OF S-3L AT FS280 IAW: CRJ200 SRM. TOPCOAT APPLIED IAW: CRJ200 SRM.Feb 22, 2020 · N889AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2020050150426Fitting · crackedINTERCOASTAL CLIP ON AFT SIDE OF REAR PRESSURE BULKHEAD WEB BETWEEN FS621 AND FS625 LEFT SIDE MID FUSELAGE IS CRACKED. (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED INTERCOASTAL CLIP ON AFT SIDE OF THE REAR PREASSURE BULKHEAD WED BETTWEEN FS621 AND FS625 LEFFeb 22, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020050150425Fitting · crackedINTERCOASTAL CLIP ON AFT SIDE OF REAR PRESSURE BULKHEAD WEB BETWEEN FS621 AND FS625 RIGHT SIDE MID FUSELAGE IS CRACKED. (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED INTERCOASTAL CLIP ON AFT SIDE OF REAR PREASSURE BULKHEAD WEB BETWEEN FS621 AND FS625 RIGHT SFeb 22, 2020 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020050150437Fastener · corrodedLT WING AILERON HINGE FITTING #1, I/B HARDWARE ON THE FWD SPAR CORRODED. (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED LEFT WING AILERON HINGE FITTING #1 INBD HARDWARE IAW CRJ 200 AMM AND CRJ 200 CMM SEE CAMP 20179195Feb 21, 2020 · N889AS · Cndair CL6002B19 · AileronsSDR SWIA2020050150436Fastener · corrodedL/H AILRON RETINING PLATES ATTACHING HARDWARE CORRODED. REF # CAMP 20516992 (C-CHECK) RO 4/30/2020 REMOVED AND REPLACED RETAINING PLATE ATTACH HARDWARE NAS6203 2H AND AN960KDIOL IAW CRJ 200 AMM AND CRJ 200 CMM SEE CAMP 20179195 FOR SIGN OFFFeb 21, 2020 · N889AS · Cndair CL6002B19 · AileronsSDR SWIA2020050150435Fastener · corrodedDAMAGED/ CORRODED HARDWARE ON PANEL 698MT, RT WING T/E. REF. CAMP# 20511101 (C-CHECK) RO 4/30/2020 REPLACED CORRODED/DAMAGED HARDWARE AND REINSTALLED PANEL 698MT IAW CRJ 200 SRM AND AMM.Feb 20, 2020 · N889AS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020050150434Fastener · corrodedDAMAGED/ CORRODED HARDWARE ON PANEL 698LT, RT WING T/E. REF. CAMP# 20511067 (C-CHECK) RO 4/30/2020 REPLACED DAMAGED AND CORRODED HARDWARE AND REINSTALLED PANEL 698LT IAW CRJ 200 SRM AND AMM.Feb 20, 2020 · N889AS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020050150433Fastener · corrodedDAMAGED/ CORRODED HARDWARE ON PANEL 698KT, RT WING T/E. REF. CAMP#20511065 (C-CHECK) RO 4/30/2020 REPLACED DAMAGED/CORRODED HARDWARE AND REINSTALLED PANEL 698KT IAW CRJ 200 SRM AND AMM.Feb 20, 2020 · N889AS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020050150432Fastener · corrodedDAMAGED/ CORRODED HARDWARE ON PANEL 698AB, RT WING T/E. REF. CAMP# 20511061 (C-CHECK) RO 4/30/2020 REPLACED DAMAGED/ CORRODED HARDWARE AND INSTALLED PANEL 698AB IAW CRJ 200 AMMFeb 20, 2020 · N889AS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020050150438Bearing · corrodedREMOVE & REINSTALL LH AILERON TO PERFORM REPLACMENT OF AILERON BEARINGS, BUSHINGS, AND HARDWARE PER AMM. USE NEW BOLTS WHEN REINSTALLING AILERON IAW AMM. COMPLY WITH TASK CARD (C-CHECK) RO 4/30/2020 REMOVED & REINSTALLED LH AILERON TO PERFORM REPLACMENT OFDec 30, 2019 · N889AS · Cndair CL6002B19 · AileronsSDR SWIA2020050150418Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL (J)(2) MODIFYING THE RPB AND Dec 30, 2019 · N889AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2019102246553Electronic Unit · malfunctionedUPON LANDING PROX SYS CHAN CAUTION, STEERING INOP, A/SKID OUTBID A/SKID INBD CAUTION, PARK BRAKE SOV CAUTION. NO STEERING AT THIS TIME EXITED RUNWAY NEED TOW TO GATE FLT# 3840 CLOSEDREMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT (PSEU)IAW AMM. OPS COct 21, 2019 · N889AS · Cndair CL6002B19 · Landing Gear Steering SystemSDR SWIA201844211Structure · crackedPOSSIBLE CRACK FOUND UNDER ACCESS DOOR 211AL AFT LATCH. REMOVED AND REPLACED THE DOOR LANDING SKIN IAW SRM.Jan 19, 2018 · N889AS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201438457Autopilot Sys · malfunctionedUNCOMMANDED STAB TRIM MOVEMENT WITH AUTOPILOT ENGAGED.Jun 29, 2014 · N889AS · Cndair CL6002B19 · Autopilot SystemSDR SWIA201436363Bulkhead · gougedGOUGE ON UPPER FWD FACE OF AFT PRESS BULKHEAD LT OF CTR LINE. C-CHECK REPAIRED GOUGE ON UPPER FWD FACE OF AFT PRESS BULKHEAD LT OF CTR IAW REO.Feb 4, 2014 · N889AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201436357Spar · gougedRT INBD FLAP, GOUGE ON FWD SPAR BETWEEN OTBD & MID VANE ACTUATOR. C-CHECK BLENDED OUT GOUGE ON RT INBD FLAP FWD SPAR IAW SRM.Feb 4, 2014 · N889AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201436356Bulkhead · gougedTHREE GOUGES ON RT SIDE LOWER FWD FACE OF AFT PRESS BULKHEAD JUST ABOVE FLOOR LINE. C-CHECK REPAIRED THREE GOUGES ON RT SIDE LOWER FWD FACE OF AFT PRESS BULKHEAD JUST ABOVE FLOOR LINE WITHIN LIMITS IAW REO.Feb 4, 2014 · N889AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201436355Floor Support · crackedCABIN FLOOR SUPPORT STRUCTURE FS 280.00 BEAM, CLIP CRACKED LBL 9 OTBD SIDE UPPER END. C-CHECK REPLACED CLIP FOR CABIN FLOOR AT FS 280 LBL 9 OTBD SIDE IAW REO.Feb 4, 2014 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201436354Floor Support · crackedCABIN FLOOR SUPPORT STRUCTURE FS 280.00 BEAM, UPPER RADIUS CRACKED LBL 11. C-CHECK REPAIRED CABIN FLOOR SUPPORT STRUCTURE FS 280.00 BEAM, UPPER ANGLE AT LBL 11 IAW REO.Feb 4, 2014 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201436364Skin · gougedLT WING LOWER SKIN IS GOUGED AT WS 385. C-CHECK REPAIRED BLENDED AREA AT LT LOWER WING SKIN, WS 385.00 IAW SRM.Feb 2, 2014 · N889AS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201436362Skin · gougedLT WING LOWER SKIN IS GOUGED AT WS 340, BETWEEN PCU & FLUTTER DAMPER ACCESS PANELS. C-CHECK REPAIRED BLENDED AREA AT LT LOWER WING SKIN, WS 340.00 IAW SRM.Feb 2, 2014 · N889AS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201436361Aileron · chafedRT WING AILERON TOP LE INBD OF CTR HINGE CHAFED. C-CHECK REPAIRED RT WING AILERON TOP LE INBD CTR HINGE CHAFE IAW REO.Feb 2, 2014 · N889AS · Cndair CL6002B19 · AileronsSDR SWIA201436360Aileron · chafedLT WING AILERON TOP LE OTBD OF OTBD HINGE CHAFED. C-CHECK REPAIRED LT WING AILERON TOP LE OTBD OF OTBD HINGE CHAFE IAW REO.Feb 2, 2014 · N889AS · Cndair CL6002B19 · AileronsSDR SWIA201436359Aileron · chafedLT WING AILERON TOP LE INBD OF CTR HINGE CHAFED. C-CHECK BLENDED DAMAGED AREA IAW REO.Feb 2, 2014 · N889AS · Cndair CL6002B19 · AileronsSDR SWIA201436358Aileron · chafedLT WING AILERON TOP LE OTBD OF INBD HINGE CHAFED. C-CHECK BLENDED DAMAGED AREA IAW REO.Feb 2, 2014 · N889AS · Cndair CL6002B19 · AileronsSDR SWIA201335779Secu · failedIN FLIGHT SPOILER SELECTED LT SPOILER DEPLOYED RT FAILED TO DEPLOY CAUSING A ROLL MOMENT. FLT 2915 REPLACED NR 2 SECU IAW AMM. PN ON OFF 49-164-06, SN ON 01697 & SN OFF 01842.Dec 29, 2013 · N889AS · Cndair CL6002B19 · Drag Control SystemSDR SWIA201333793Accumulator · failedHYDRAULIC SYSTEM 3 SHOWED 90% QUANTITY. FLT#2997 REPLACED HYDRAULIC SYSTEM NR 3 ACCUMULATOR IAW AMM. PN ON/OFF 11094-4 SN ON 11094-2859 SN OFF 11094-2701Jun 25, 2013 · N889AS · Cndair CL6002B19 · Hydraulic Power Accumulator, MainSDR SWIA201333771Hydraulic System · contaminatedBOTH BRAKES ARE VERY WEAK, PEDAL TRAVELS ALL THE WAY TO THE STOPS TO GET THE PLANE TO STOP. FLT#2974 INSPECTED BRAKES & FITTINGS. ALL FOUND TO BE NORMAL. BLED AIR OUT OF NR 3 HYDRAULIC SYSTEM. OPERATIONS CHECKED GOOD AT THIS TIME.Jun 19, 2013 · N889AS · Cndair CL6002B19 · Hydraulic System, MainSDR SWIA201333509Light · inoperativeEMERGENCY LIGHT ON STAIRS IS BURNED OUT, RELAMPED.May 19, 2013 · N889AS · Cndair CL6002B19 · Emergency LightingSDR SWIA201332706Light · inoperativeFLT 2971. EMERGENCY LIGHT BY MAIN CABIN DOOR STEPS DOES NOT ILLUMINATE. REPLACED LIGHT.Jan 30, 2013 · N889AS · Cndair CL6002B19 · Emergency LightingSDR SWIA201232277Retractor · obstructedF/O SHOULDER HARNESS INTERNAL REEL STUCK. (FLT 2922) REMOVED DEBRIS FROM F/O'S SHOULDER HARNESS RETRACTOR.Nov 29, 2012 · N889AS · Cndair CL6002B19 · Flight Compartment EquipmentSDR SWIA201231502Reservoir · failedDURING GEAR RETRACTION RECEIVED HYDRAULIC 3 LOW PRESSURE CAUTION, GEAR DISAGREE, AND NOSE DOOR OPEN WARNING. (FLT 2980) REPLACED NR 3 HYDRAULIC SYSTEM RESERVOIR AND SERVICED NR 3 HYDRAULIC SYSTEM TO PROPER LEVEL. P/N: 7303-1 S/N OFF: 471AAug 12, 2012 · N889AS · Cndair CL6002B19 · Hydraulic Reservoir, MainSDR SWIA201231462Mechanism · dirtyMAIN CABIN DOOR WOULD NOT OPEN. (FLT 2986) CLEANED AND LUBED CABIN DOOR LOCK MECHANISM.Aug 8, 2012 · N889AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201231269Uplock · failedGEAR DISAGREE MESSAGE. (FLT 2923) REPLACED RIGHT UPLOCK ASSEMBLY PER AMM 32-32-05 AND BLED HYD SYSTEM NR 3 PER MM. P/N: 17051-101, S/N OFF: NGL/1181/01.Jul 16, 2012 · N889AS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201231057Uplock · failedLEFT MAIN LANDING GEAR DID NOT COME DOWN. (FLT 2950) REPLACED LEFT GEAR UPLOCK ASSEMBLY. P/N: 17051-101, S/N OFF: DCL495-96Jun 19, 2012 · N889AS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201230970Selector Valve · failedRECEIVED A GEAR DOWN DISAGREE. (FLT 2961) REPLACED LANDING GEAR SELECTOR VALVE IN REFERENCE TO MM. P/N ON: 750005000, S/N OFF: 0048T.Jun 7, 2012 · N889AS · Cndair CL6002B19 · Landing Gear SelectorSDR SWIA201230868Light · inoperativeNR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 2996) RELAMPED EMERGENCY LIGHT.May 30, 2012 · N889AS · Cndair CL6002B19 · Emergency LightingSDR SWIA201230590Light · inoperativeNR 2 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 2965) RELAMPED EMERGENCY LIGHTS.May 1, 2012 · N889AS · Cndair CL6002B19 · Emergency LightingSDR SWIA201230194Stop Fitting · out of adjustMAIN CABIN DOOR WOULD NOT OPEN. (FLT 2970) ADJUSTED UPPER FORWARD STOP SHIMS.Mar 27, 2012 · N889AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201230188Light · inoperativeNR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.Mar 24, 2012 · N889AS · Cndair CL6002B19 · Emergency LightingSDR SWIA201229913Skin · dentedDENT ON RIGHT WING LOWER OUTER SKIN 6 INCHES AFT OF LEADING EDGE, BETWEEN WS 330.25 AND WS 343.50. (SERVICE) COMPLIED WITH REO.Mar 1, 2012 · N889AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA201101635Flashlight · inoperativeCAPT FLASHLIGHT WILL NOT STAY ILLUMINATED. R & R CAPT'S FLASHLIGHT IAW AMM 25-61-00.Sep 2, 2011 · N889AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201001828Glowstrip · deterioratedPLASTIC STRIP THAT EMG MARKINGS ON FLOOR IN FRONT OF SEAT 8 C NEEDS REPLACING. REMOVED AND REPLACED PHOTO LUMINESCENT FLOOR MARKING ASSY AT SEAT 8C IAW CRJ 200 AMM 33-51-01.Nov 22, 2010 · N889AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201001513Flashlight · inoperativeF/A REPORTS FLASHLIGHT INOP. REPLACED F/A FLASHLIGHT AT GALLEY AREA OPS CHECKED GOOD IAW AMM 25-61-01. (CLOSED)Oct 7, 2010 · N889AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201001193Isolator · brokenFOUND 4 EA BROKEN ISOLATORS AT 621 BULKHEAD. REMOVED 4EA ISOLATORS 621 BULKHEAD IAW SRM 51-42-13. INSTALLED NEW SERVICEABLE ISOLATORS AT 621 BULKHEAD IAW SRM 51-42-13. (CLOSED)Aug 26, 2010 · N889AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001187Stringer Clip · corrodedFOUND CORRODED CLIP AT FS 319.70 STR 17R. REMOVED CORRODED CLIP AT FS 319.70 IAW SRM 51-42-06. LOCATED AND INSTALLED CLIP IAW SRM 51-42-06, 51-42-13, 51-42-26. PRIOR TO INSTALLATION TREATED, PRIMED & PAINTED IAW SRM 51-25-06 & 51-25-16. BRACKETS PN 601R38Aug 26, 2010 · N889AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201001186Bracket · corrodedSERVICE DOOR CUTOUT LOWER SILL JOINT BRACKET CORRODED AT FS 319.70. REMOVED FLOORBOARD LANDING FWD OF SERVICE DOOR TO ACCESS JOINT BRACKET IAW SRM 51-42-06. REMOVED FWD SERVICE DOOR CUTOUT TRIM PANEL TO ACCESS JOINT BRACKET BY REMOVING 3 EA SCREWS. REMOVED Aug 26, 2010 · N889AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001148Post · crackedFS 409+128 VERT POST RBL 18 OTBD POS AFT RADIUS FAILS NDT WITH AN INDICATION GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED RBL 18 VERTICAL POST AT F.S. 409+128 IAW SRM 51-42-06. INSTALLED FASTENER AND POST AT F.S. 409+128 RBL 18 IAW SRM 51-42-22. INSTALLAug 18, 2010 · N889AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201001147Post · crackedFS 409+128 VERT POST BL 0 LT POS AFT RADIUS FAILS NDT WITH AN INDICATION GREATER THAN 50 PERCENT SCREEN HEIGHT. REMOVED VERT POST AT FS 409+128 BL O IAW SRM 51-42-06. ON FURTHER INVESTGATION RT POST FOUND CRACKED. INDICATION TWO NE POSTS & REF WERE DRILLED Aug 18, 2010 · N889AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201001146Post · crackedREMOVED LBL 18 VERTICAL POST AT FS 409+128 IAW SRM 51-42-06. NEW VERTICAL POST REQUIRES DRILL UP AND INSTALL. DRILLED AND RIVETED NEW POST TO LBL 18 INBD POST IAW SRM 51-42-06. REQUIRE INSTALLATION. INSTALLED VISULOK FASTENERS & RIVETS WITH POST AT FS 409+Aug 18, 2010 · N889AS · Cndair CL6002B19 · Fuselage Main, Structure
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