N870AS, cancelled Jul 30, 2023

Service difficulty reports · 146

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 = 'N870AS' AND deregistration_id = 'N870AS-2023-07-30'
  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 SWIA2019102246555Warning Message · false activationN2 VIB MESSAGE CAME UP ON TAKE OFF ROLL. ABORTED TAKE OFF 80 KNOTS. BTMS WITHIN LIMITS FLT # 5946 CLOSED. NO DAMAGE NOTED. PERFORMED HIGH POWER ENGINE RUNS AND DID NOT GET VIBE INDICATION FOR N2. OPS CHECKS GOOD.Oct 21, 2019 · N870AS · Cndair CL6002B19 · Engine Vibration AnalyzerSDR ASOA2019040864012Battery Pack · dischargedIAH - FLIGHT 4306, THE CREW REPORTED EMERGENCY LIGHTS NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE #3 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOT AND THE AIRCRAFT WAS APPROVED FOR RETURN SERVICE.Apr 6, 2019 · N870AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2019040173021Seal · faultyTHE CREW REPORTED AT 35,000 FEET LOST ALL PRESSURIZATION. MAINTENANCE INSPECTED AND REPLACED SERVICE DOOR SEAL. OPERATIONAL CHECK WERE GOOD.Mar 27, 2019 · N870AS · Cndair CL6002B19 · Service DoorsSDR ASOA2016030514551Bulb · missingEMERGENCY RT COVER AND LIGHT BULB MISSING ON NR 1 GALLEY WALL, ENTRANCE LT SIDE. REPLACED EMERGENCY LIGHT ASSY ON IAW AMM 33-5119, GOOD. OK FOR SERVICE.Mar 5, 2016 · N870AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2016012614402Skin · damagedDURING FLIGHT CONTROL TEST AFTER PUSHBACK, THE RT RUDDER PEDDAL WILL NOT REACH FULL DEFLECTION. DAMAGE TO RUDDAR, CAUSING OBSTRUCTION, SHEETMETAL REMOVED IAW REO 601R-55-41-197 PERFORMED OPS TEST OF RUDDAR IAW AMM 27-21-00.Jan 26, 2016 · N870AS · Cndair CL6002B19 · Rudder, Plate/SkinSDR ASOA2015081013475Skin · damagedFUSELAGE SKIN DAMAGE AROUND LOW PRESSURE GROUND CONNECTION DOOR. THE REPAIR HAS BEEN DETERMINED AND CLASSIFIED TO BE MAJOR REAPAIR. RECEIVED AND COMPLIED IAW EA 25-2015-237.Aug 10, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2015042912729Angle · crackedCARGO DOOR CROSSMEMBER ANGLE CRACKED AT FS 621.00 BULKHEAD. R & R ANGLE AT FS 621.00 CARGO DOOR CROSSMEMBER WITH NEW SERVICEABLE PART IAW SRM 51-42-21.Apr 25, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015050412751Skin · crackedFOUND RT LOWER WING PLANK FUEL ACCESS HOLE 640FB HAS MULTIPLE INDICATIONS NOTED ON AFT OTBD SIDE APPROXIMATELY 1.5" LONG, 50 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.Apr 15, 2015 · N870AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015050412750Frame · corrodedCORROSION ON FRAME AT FS 605.00, STR 27. REMOVED CORROSION ON FS 605. FRAME BETWEEN STR 25L AND 25R IAW SRM 51-21-06. FS 605.00 FRAME FOPUND TO BE OUT OF LIMITS IAW SRM 53-00-00, TRR 53-29. REMOVED OLD FS 605.00 FRAME SECTOR, PN:601R36026-27 BETWEEN FACTORY Apr 13, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015050412749Skin · corrodedWING PLANK AT 640BB HAS CORROSION IN SEVERAL AREAS. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.Apr 13, 2015 · N870AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015050412748Skin · corrodedWING PLANK AT 540BB HAS CORROSION AT INBD SIDE IN NON-CRITICAL AREA. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.Apr 13, 2015 · N870AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015050412747Floorbeam · crackedFS 621, LT FLOOR SUPPORT ANGLE CRACKED AT LBL 36. REO:601R-53-61-5473, REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.Apr 13, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015042912728Door Sill · corrodedCORROSION ON CARGO DOOR SILL FROM FS 621.00 TO FS 574.00. 2 AREAS 0.003 IN. OUT OF LIMITS AT FS 589.00+13 AND FS 605.00+6.25 ENGINEERING REQUIREDD. DAMAGE WAS BLENDED OUT TO SMOOTH CONTOUR IAW REO 601R-53-61-5472. COMPLIED WITH REO 601R-53-61-5472.Apr 13, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042912727Floorbeam · corrodedCORROSION ON FLOORBEAM AT FS 589.00 BETWEEN LBL 18 AND LBL 27. FOUND TO BE OUT OF LIMITS IAW TR 53-27, REQUIRES REPLACEMENT. REMOVED CORRODED FLOORBEAM CAP AT FS 589.00 BETWEEN LBL 18 AND LBL 27 IAW SRM 51-42-06, 51-42-21 AND 51-42-15. LOCATED AND INSTALLED Apr 13, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015042912726Seat Track · corrodedRT SIDE SEAT RAILS FROM FS 454 - FS 559+54 HAS SEVERAL AREAS OF CORROSION AROUND THE LOWER EDGE OF THE COIN HOLES; WORST IS AT FS 474, MARKED WITH ORANGE TAPE. REMOVED RT SIDE SEAT RAIL AT FS 449.85 TO FS 495.98 IAW AMM 53-01-11-000-802. INSTALLED RT SIDE SEApr 12, 2015 · N870AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015050412746Retainer · corrodedMAIN AVI BAY DOOR SEAL RETAINER IS CORRODED. REMOVED SEAL RETAINER IAW SRM 51-42-06. REPLACED SEAL RETAINERS IAW SRM 51-42-06. PERFORMED OPS TEST OF THE MAIN AVIONICS COMPARTMENT DOOR SEAL IAW AMM 52-42-07-710-801. OPS TESTED GOOD.Apr 10, 2015 · N870AS · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR ASOA2015050412745Floor Support · corrodedCORROSION ON FLOOR SILL AFT OF PAX DOOR AT FS 349.00. REPAIRED FLOOR SILL BETWEEN FS 280 TO FS 409+128 IAW REO 601R-53-00-530, REV A.Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042912725Floorbeam · corrodedCORROSION FOUND ON AVIONICS BAY FLOORBOARD SUPPORT ANGLE AT FS 333.00. REMOVED FLOORBOARD SUPPORT ANGLE IAW SRM 51-42-06. LOCATED, DRILLED AND INSTALLED FS 333.00 AVIONICS BAY FLOORBOARD SUPPORT BRACKET IAW SRM 51-40-11 AND SRM 51-42-06.Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015042912724Door Sill · corrodedSERVICE DOOR SILL, LOWER, ANGLE HAS CORROSION IN SEVERAL AREAS. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED LOWER SILL IAW SRM 51-42-21 AND 51-42-06. LOCATED AND DRILLED NEW SERVICE DOOR LOWER SILL ANGLE, PN:601R38303-253 IAW SRM 51-40-11. INSTALLED NEW SApr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042912723Door Sill · corrodedCORROSION ON SERVICE DOOR SILL AT FS 319.70 AND FS 349.00. BLENDED AREA REMOVING CORROSION IAW REO 601R-53-00-530. REPAIRED FLOOR SILL BETWEEN FS 280 TO FS 409+128 IAW REO 601R-53-00-530, REV A.Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042912722Floor Support · corrodedCORROSION ON UPPER SURFACE OF FLOOR SUPPORT AROUND 3 FASTENER HOLES BETWEEN FS 310.00 AND FS 349.00 LBL 27. COMPLIED WITH EC/TC REO 601R-53-00-005.Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042912721Floor Support · corrodedCORROSION ON UPPER SURFACE OF RT FLOOR SILL STRUCTURE FROM FS 409.00+128 TO FS 559.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C, DATED 11/06/12 AS WRITTEN.Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015042912720Frame · corrodedCORROSION ON FRAME AT FS 364.00 BETWEEN LBL 24 & RBL 24. COMPLIED WITH EA 32-2015-138.Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015042912719Frame · corrodedCORROSION ON FRAME AT FS 330.00 BETWEEN LBL 24 & RBL 24. FOUND CORROSION TO BE LOCATED ON FRAME SECTOR AT FS 333.00 NOT FS 330.00. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-00. REMOVED CORRODED FRAME IAW SRM 51-42-21 AND 51-42-06. LOCATED AND DRILLED NEWApr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015042912718Frame · corrodedCORROSION ON FRAME AT FS 319.70 BETWEEN LBL 24 & RBL 24. FOUND CORROSION ON FS 319.70 FRAME OUT OF LIMITS IAW SRM 53-00-00. REMOVED FS 319.70 LOWER FRAME SECTOR FOR REPLACEMENT IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW FS 319.70 LOWEApr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015042912717Frame · corrodedCORROSION ON FRAME AT FS 310.00 BETWEEN LBL 24 & RBL 24. FOUND CORROSION ON FRAME TO BE OUT OF LIMITS IAW SRM 53-00-00. COMPLIED WITH REO 601R-53-21-2612 P1.Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015042912716Floorbeam · crackedFS 280.00 FLOORBEAM ANGLE AT RBL 9 OTBD & RBL 27 INBD ARE CRACKED. FABRICATED NEW FS 280, RBL 9 CLIP FROM S6144-13, PERFORMED ANGLE 2024T42 .050" IAW REO 601R-53-11-926, NOTE 20. REMOVED CRACKED CLIP AT FS 280, RBL 9.0, OTBD IAW SRM CH 51-42-21. COMPLIED WIApr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015042912715Floorbeam · crackedFS 280.00 FLOORBEAM ANGLE AT LBL 9 INBD & OTBD ARE CRACKED. FABRICATED NEW FS 280, LBL 9 INBD AND OTBD CLIPS FROM S6144-13, PREFORMED ANGLE 2024T42 .050" IAW REO 601R-53-11-926, NOTE 20. REMOVED CRACKED LBL 9 INBD AND OTBD CLIPS AT FS 280 IAW SRM CH 51-42-21Apr 7, 2015 · N870AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014041010306Lamp · burned outEMERGENCY LIGHT LAMP INOPERATIVE. REPLACED LAMP, OPS CHECKED GOOD, IAW AMM 33-51-00.Apr 6, 2014 · N870AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013121909663Priority Valve · failedGEAR UP DISAGREE WARNING AFTER DEPARTURE. LT AND RT GEAR WERE IN DISAGREEMENT (RED). COMPLIED WITH QRH. MANUAL GEAR HANDLE WAS PULLED IAW QRH. EMERGENCY DECLARED. RETURNED TO DEPARTURE AND LANDED AT 46500 LBS. R & R MLG PRIORITY VALVE IAW AMM 32-32-15.Nov 28, 2013 · N870AS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA2013100109138Lamp · burned outCENTER CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP, OP'S CHECKED GOOD IAW AMM 33-51-16.Sep 27, 2013 · N870AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013053003737Skin · crackedRIGHT LOWER WING SKIN IS CRACKED .25" LONG AT WS 148.09 - REINFORCING ANGLE IN T/E ABOVE SKIN IS CRACKED .75" LONG. C/W ECTC REO 601R-57-21-130 01 AND REO 601R-57-21-130, REV J, DATED 03/08/2011 AS WRITTEN. C/W ECTC REO 601R-57-21-131 AND REO 601R-57-21-131,May 10, 2013 · N870AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013053003736Angle · crackedFS 621, BULKHEAD AFT SIDE FS 621-625 ANGLES CRACKED. REMOVED CRACKED LT & RT FS 621-625 ANGLES AND INSTALLED SERVICEABLE ANGLES IAW SRM 51-40-11 AND SRM 51-42-06.May 8, 2013 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013053003735Attach Bracket · crackedPAX DOOR UPPER SILL ATTACHMENT BRACKET CRACKED AT FS 280. REMOVED CRACKED BRACKET AT FS 280, STR 3 IAW SRM 51-42-06. LOCATED & DRILLED NEW SERVICEABLE ANGLE, PN 600-31057-19 IAW SRM 51-40-11. UPON FURTHER INVESTIGATION ANGLE, PN 600-31057-20, FS 280, STR 3 May 8, 2013 · N870AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2013053003734Bulkhead · crackedFS 621, BULKHEAD FAILS NDT WITH AN INDICATION FSH AT LBL 27.50, WL 130). REPAIRED IAW REO 601R-53-61-1541, REV D.May 7, 2013 · N870AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013053003733Cargo Track · corrodedCARGO TRACKS CORRODED AROUND FASTENER HOLES AT LBL 27 AND LBL 9. R & R CARGO TRACKS IAW AMM 20-21-00-910-801.May 3, 2013 · N870AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013053003732Isolator · crackedPRESSURE BULKHEAD FWD FACE HAS FIVE CRACKED ISOLATORS. R & R ISOLATORS ON FS 621 BULKHEAD IAW SRM 51-42-06.May 3, 2013 · N870AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013053003731Floor Support · corrodedLEFT CABIN FLOOR SUPPORT IS CORRODED AT FOUR NUTPLATE LOCATIONS. DAMAGE IS APPROX BETWEEN FS 409+128 AND FS 559. REPAIRED IAW TASK 51-26-0-110-801, SRM 51-21-11, 51-27-19, 51-21-06, 51-26-00 AND REO 601R-53-41-666.May 3, 2013 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013053003730Skin · crackedLEFT LOWER WING SKIN CRACKED .25" LONG AT WS 148.019. C/W EC/TC REO 601R-57-21-130 AND GENERIC REO 601R-57-21-130, REV J. C/W EC/TC REO 601R-57-21-131 AND REO 601R-57-21-131, REV A. REPAIRED IAW REO 601R-57-51-639, SRM 51-42-06, 51-42-21 & REO 601R-57-21-6Apr 30, 2013 · N870AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013053003729Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED IAW SRM 51-42-06 AND 51-42-10 AND REO 601R-52-11-513, REV A.Apr 30, 2013 · N870AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012100202318Control Lever · failedON SELECTING FLAPS FROM 8 TO 20 DEGREES, FLAPS FAIL CAUTION MESSAGE DISPLAYED. VERIFIED FLAPS STUCK AT 8 DEGREES ON EICAS FLIGHT CONTROL PAGE. COMPLIED WITH QRH. EMERGENCY DECLARED. COMPLIED WITH AD 2009-06-12 TROUBLESHOOTING FOR FLAP FAILURES. R & R FLAP CSep 28, 2012 · N870AS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA2012091702224Motor · malfunctionedPASSENGER DOOR DOES NOT OPEN FULLY. R & R PASSENGER DOOR POWER ASSIST MOTOR IAW AMM 52-11-08. PERFORMED OPS CHECKS OF THE PWR DOOR ASSIST IAW AMM 52-11-08-720-802. NO DEFECTS NOTED DEFER CLEARED PLACARD REMOVED. SDR CLOSED.Sep 13, 2012 · N870AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201201454Detection Sys · malfunctionedDURING FIRE WARNING TEST, DID NOT GET LEFT ENGINE FIRE LOOP-B WARNING MESSAGE AND LEFT FIRE PUSH SWITCH DOES NOT ILLUMINATE. INSPECTED LT ENGINE FIRE LOOPS, NO PROBLEMS NOTED. FOUND LT FIRE PUSH SWITCH LIGHT LOOSE IN ITS SOCKET. RESECURED THE FIRE PUSH SApr 28, 2012 · N870AS · Cndair CL6002B19 · Fire DetectionSDR ASOA201201315Pin · missingSERVICE DOOR RELEASE HANDLE NOT FUNTIONAL. PIN MISSING. REPLACE MISSING PIN ON SERVICE DOOR RELEASE HANDLE. OPS CHECKED GOOD IAW AMM 52-41-02. (SDR CLOSED)Apr 20, 2012 · N870AS · Cndair CL6002B19 · Service DoorsSDR ASOA201100887Isolator · brokenAPPROX RBL 36, WL 92 ON AFT BULKHEAD, ISOLATER BROKEN RT SIDE. R & R RT OTBD ISOLATOR AT WATER LINE 92 ON FS 621 BULKHEAD IAW SRM 51-42-13. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASAMay 4, 2011 · N870AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA201100878Connector · malfunctionedFWD LEFT EMERGENCY LIGHTS ARE INOP ON TEST. FOUND CONNECTORS J11LY AND P10LY SWAPPED WITH CONNECTORS J20LY AND P21LY. INSTALLED TO ORIGINAL CONFIG AND RESEATED CONNECTORS IAW ESPM 20-17-10. PERFORMED OPS CHECK IAW AMM 33-51-00-710-801. SYS CHECKS GOOD. OKMay 4, 2011 · N870AS · Cndair CL6002B19 · Light System WiringSDR ASOA201100783Floorbeam · crackedFS 280 AFT FLOOR ANGLE IS CRACKED OTBD OF RBL9 AND OTBD LBL9, REPAIRED IAW REO 601R-53-11-926 IAW REO 601R-53-11-926, REV B.Apr 15, 2011 · N870AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201100777Post · crackedINDICATION NOTED AT FS 409+128 BL 0.00 WK 69.0 RADIUS OF RT CHANNEL APPROX .10" LENGTH, 55 PERCENT. REMOVED POST ASSY IAW SRM 51-42-06, 51-42-21. INSTALLED NEW SERVICEABLE POST ASSY IAW REO 601R-53-41-889.Apr 15, 2011 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100776Floor Support · corrodedFLOOR SUPPORT CORRODED FS 349 AT SERVICE DOOR SURROUND LOWER AFT FRAME BRACKET. REMOVED CORROSION, FOUND WITHIN LIMITS IAW SRM 53-21-15 AND SRM 53-00-00.Apr 15, 2011 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100775Floor Support · corrodedFS 280, FWD FLOOR SUPPORT ANGLE IS CORRODED. R & R FWD FLOOR SUPPORT ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-06. REPAIR CLASSIFIED AS A MINOR.Apr 15, 2011 · N870AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
Back to N870AS, cancelled Jul 30, 2023