N880AS

Service difficulty reports · 192

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 = 'N880AS' 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 SWIA2018092445090Strut · failedON DEPARTURE NOSE DOOR OPEN WARNING AND GEAR DISAGREE WARNING. COMPLETED QRH. WOW INPUT CAUTION MESSAGE. NO NOSE WHEEL STEERING ON LANDING. (FLT 5014) CLOSED PERFORMED FULL SERVICE ON NOSE LANDING GEAR STRUT IAW AMM. STRUT EXTENSION CHECK GOOD AT THIS TIME. PESep 24, 2018 · N880AS · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR SWIA2018073144944Screw · looseSTRONG INTERMITTENT FUEL SMELL IN THE FLIGHT DECK IN FLIGHT AND ON GROUND. APU RAN ENTIRE FLIGHT. (FLT 5421) CLOSED SECURED LOOSE PANEL SCREWS ON RIGHT WING, NR 5 FUEL PANEL AS REQUIRED. NO LEAKS NOTED. RAN APU AND ENGINES, OPERATED BLEED AIR WITH NO FUEL SMELJul 31, 2018 · N880AS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201844655Proximity Sensor · out of adjustUPON SELECTING GEAR UP ON TAKE OFF, THE NOSE GEAR REMAINED DOWN. CYCLED THE GEAR TWO MORE FULL CYCLES AND ABOUT A MINUTE AFTER THE LAST ATTEMPT THE NOSE GEAR RETRACTED. (FLT 5645) CLOSED ADJUSTED PROX SENSORS S23, S11 AND S03 IAW AMM. OPS CHECK GOOD. PERFORMEMay 11, 2018 · N880AS · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA201743483Sensor · out of adjustGEAR DISAGREE, DECLARED EMERGENCY. PROXIMITY SENSOR WAS OUT OF ADJUSTMENT ON THE LT MAIN LANDING UPLOCK. OPS CHECKED GOOD.Jul 10, 2017 · N880AS · Cndair CL6002B19 · Landing Gear Position and WarningSDR ASOA2016081815280Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE. CHARGED THE BATTERY PACKS AND OPS CHECKED EMERGENCY LIGHTS IAW AMM 33-51-05. OPS CHECKED GOOD.Aug 18, 2016 · N880AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2016052814900Pseu · failedAT 31,000', ENROUTE, RECEIVED AMBER CAUTION PRIX SYSTEM CHANNEL MESSAGE, FOLLWED QRH MANNUALLY EXTENDED GEAR LANDED. ENROUTE, ACFT DIVERTED DUE TO MAINTENANCE EMERGENCY ACTIONS. R & R PSEU IAW AMM 32-61-01, IPC REF32-61-00, ITEM 5, OPS TEST GOOD, IAW THE NATUMay 28, 2016 · N880AS · Cndair CL6002B19 · Landing Gear Position and WarningSDR ASOA2016050914833Bushing · deterioratedRT MLG TRUNNION AFT BUSHING AUX BORE HOLE DIAMETER IS OUT OF LIMITS. REMOVED RT MLG AFT TRUNNION LUG TO TO FIRST OVERSIZE IAW ECTC REO 601R-57-21-003. INSTALLED 1ST OVERSIZE BUSHING IN RT MLG AFT TRUNNION IAW ECTC REC 601R-57-21-003 AND GREO 601R-57-21-003, May 9, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR ASOA2016050714832Bushing · deterioratedRT MLG TRUNNION FWD BUSHING BORE, AFT SPAR, HOLE DIAMETER IS OUT OF LIMITS. REMOVED AND REAMED THE TRUNNION, MLG TRUNNION FWD BUSHING BORE, AFT SPAR, TO 1ST OVERSIZE IAW ECTC REO 601R-57-21-003. INSTALLED 1ST OVERSIZE BUSHING IN THE RT MLG TRUNNION FWD BUSHIMay 7, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR ASOA2016050714831Bushing · deterioratedLT MLG TRUNNION AFT BUSHING BORE AUXILIARY HOLE DIAMETER IS OUT OF LIMITS. REAMED LT MLG AFT TRUNNION LUG TO FIRST OVERSIZE IAW ECTC REO 601R-57-21-003. INSTALLED 1ST OVRSIZE BUSHING INLT MLG AFT TRUNNION IAW ECTC REO 601R-57-21-003.May 7, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR ASOA2016050614830Seat Track · corrodedSEAT TRACK SEGMENT CORRODED AND OUT OF LIMITS ON RBL9 AND BETWEEN FS 559 TO FS 559+86. REMOVED SEAT TRACK SEGEMENTS AT RBL9 BETWEEN FS559-FS559+86 IAW AMM 53-01-11-000-802. INSTALLED SEAT TRACK SEGMENT AT RBL9 BETWEEN FS 559-559+86 IN REF TO AMM 53-01-11-400May 6, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016050614829Intercostal · crackedANGLE CRACKED BETWEEN FS 621 AND FS 625.30 AT STR 15R. REMOVED DISCREPANT INTERCOSTAL AND INSTALLED SERVICABLE INTERCOSTAL AT FS 621-FS625.3, RBL45.6, IAW SRM 51-40-11, 51-42-21, 51-21-16.May 6, 2016 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2016050614828Intercostal · crackedANGLE CRACKED BETWEEN BS 621 AND 625.30 AT STR 15L. REMOVED DISCREPANT INTERCOSTAL AND INSTALLED SERVICABLE INTERCOSTAL AT FS 621-FS 625.3, LBL45.6, IAW SRM 51-40-11, 51-42-21, 51-21-16.May 6, 2016 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2016042914839Floor Support · corrodedCORROSION ON FLOORSILL AT LBL 47 AND BETWEEN FS 349 TO FS 367. BLENDED CORROSION ON FLOOR SILL AT LBL47 BT FS 349 AND FS 367 IAW SRM 51-21-06 AND FOUND TO BE OUT OF LIMITS IAW EC/TC REO 601R-53-00-530. PERFORMED UT THICKNESS INSP IAW BSC NDTM SEC 4.3 MIN REMApr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2016042914827Seat Track · corrodedLBL 9 SEAT TRACK SEGMENT BETWEEN FS 400 TO FS 409+128 CORRODED OUT OF LIMITS. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485, REV A.Apr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016042914825Seat Track · corrodedLBL9 FLOOR SEAT RAIL SEGMENT BETWEEN FS 364 TO FS 400 HAS CORROSION AROUND SEVERAL SCREW HEADS, MARKED. EVALUATED LBL9 FLOOR SEAT RAIL FS 364-400 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED LBL9 FLOOR SEAT RAIL FS 364-FS 400 IAW AMM 53-01-000-802. COApr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016042914824Seat Track · corrodedRBL9 FLOOR SEAT RAIL SEGMENT BETWEEN FS 364 TO FS 400 HAS CORROSION IN A FEW SPOTS. EVALUATED RBL9 FLOORS AT RAIL FS 364-400 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED RBL9 FLOOR SEAT RAIL FS 364-FS 400 IAW AMM 53-01-11-000-802. INSTALLED NEW FABRICApr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016042914823Seat Track · corrodedRBL9, FLOOR SEAT RAIL SEGMENT BETWEEN FS 400 TO FS 409+128 IS CORRODED OUT OF LIMITS. EVALUATED RBL9, FLOOR SEAT RAIL FS 400-FS 409+128 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVE SEAT RAIL. REMOVED RBL9, SEAT RAIL FS 400-FS 409+128 IAW AMM 53-01-11-Apr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016042914822Floorbeam · crackedANGLE CLIP CRACKED AT FS 280 AND RBL9, INBD SIDE. RECEIVED REO 601R-53-11-2904 AND COMPLIED WITH ALL STEPS OF REO 601R-53-11-2904. COMPLIED WITH EC/TC REO 601R-53-11-2904 AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON ROUTINE WORK CARD.Apr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2016042914821Floorbeam · crackedANGLE CLIP CRACKED AT FS 280 AND LBL 9; OTBD SIDE. RECEIVED AND COMPLIED WITH REO 601R-53-11-2904. COMPLIED WITH EC/TC REO 601R-53-11-2904 AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON ROUTINE WORK CARD.Apr 29, 2016 · N880AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2016042614838Skin · crackedLT FWD FUSELAGE SKIN CRACKED BELOW AFT TRU DOOR LATCH AT APPROXIMATELY FS 192.00. REMOVED CRACKED DOOR LAND AT FS 192.00 BELOW TRU DOOR LT IAW SRM 51-42-06 AND 51-42-13-00. LOCATED AND DRILLED NEW SERVICEABLE LT DOOR LAND BELOW AFT TRU DOOR AT APPROXIMATELY Apr 26, 2016 · N880AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2016042614820Door · lack of lubeRIGHT EMERGENCY DOOR FAILED PULL TEST 70 LBS. LUBRICATED RT EMERGENCY EXIT DOOR IAW AMM 12-20-52-640-802. PERFORMED PULL TEST OF RT EMERGENCY EXIT DOOR IAW AMM 52-21-00-720-801, STEPS 4.A, 1, 3. PULL TEST GOOD.Apr 26, 2016 · N880AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA2015110914005Light · damagedFLOOR-LEVEL EMERGENCY FLOOD LIGHT AT MAIN ENTRANCE DOOR DAMAGED. R & R FLOOD LIGHT IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.Nov 9, 2015 · N880AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015072913402Wire · misinstalledREF DMIL A595210 FWD CABIN EMERGENCY CEILING LIGHT INOPERATIVE. TROUBLESHOT FWD EMERGENCY CEILING FLOODLIGHT. FOUND WIRES ON FWD EMERGENCY CEILING FLOODLIGHT INCORECTLY INSTALLED. INSTALLED FWD EMERGENCY CEILING FLOODLIGHT IAW AMM 33-51-16 AND WM 33-51-00. Jul 29, 2015 · N880AS · Cndair CL6002B19 · Light System WiringSDR ASOA2015072713391Wire · misinstalledFWD CABIN EMERGENCY CEILING LIGHT IS INOPERATIVE. TROUBLE SHOT FWD EMERGENCY CEILING FLOODLIGHT. FOUND WIRES ON FWD EMERGENCY CEILING FLOODLIGHT INCORRECTLY INSTALLED. INSTALLED FWD EMERGENCY CEILING FLOODLIGHT IAW AMM 33-51-16 AND WM 33-51-00. OPS CHECK GOJul 27, 2015 · N880AS · Cndair CL6002B19 · Light System WiringSDR ASOA2015031312377Trunnion · damagedRIGHT TOP AFT HOLE ON HORIZONTAL STABILIZER TRUNNION AND ACFT HORIZONTAL STABILIZER OVERSIZED TO .4125, MAX IS .380. REMOVED MOUNTING HARDWARE FROM HORIZONTAL STA IAW AMM 27-42-01-000-801. BOTTOM PINS AND TRUNNIONS TEMP INSTALLED. INSTALLED MOUNTING HARDWAMar 3, 2015 · N880AS · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR ASOA2014111211631Lamp · burned outRIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.Nov 7, 2014 · N880AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014071110849Flashlight · inoperativeF/A FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-61-04. OPS CHECKED GOOD. ACFT OK FOR SERVICE.Jul 9, 2014 · N880AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA2014052710602Bulb · inoperativeGALLEY FLOOR EMERGENCY LIGHT EXIT SIGN HAS FIVE BAD BULBS. REMOVED BULBS FROM THE GALLEY EMERGENCY LIGHT FLOOR EXIT SIGN AND REPLACED WITH SERVICEABLE BULBS IAW 33-51-10-400-801.May 19, 2014 · N880AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014052710601Angle · corrodedTWO ANGLES AT FS 364 LBL AND RBL 18 ARE CORRODED. REMOVED DAMAGED ANGLES IAW SRM 51-42-06. FABRICATED AND INSTALLED NEW ANGLES IAW SNIEO 601R31049-S02.May 16, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014052710600Skin · buckledPAX DOOR FWD AND AFT SKIN ARE BUCKLED, COMPLIED WITH REO:601R-52-11-2227.May 8, 2014 · N880AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2014052710599Skin · damagedDURING VISUAL INSPECTION FOR LIGHTNING STRIKE DAMAGE, FOUND BURNED RIVETS. FOUND TO BE SATISFACTORY.May 7, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2014052710598Skin · crackedLEFT FUEL ACCESS HOLE 550HB HAS MULTIPLE INDICATIONS ON INBD, FWD & AFT SIDE 50 PERCENT FSH, FAILED NDT. C/W ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.May 7, 2014 · N880AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014052710597Beam · corrodedBS 349.00 TRANSVERSE BEAM IS CORRODED OTBD OF RBL 27.00. REO 601R-53-21-2534 REV--HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NRI WORK CARD. RII'S HAVE BEEN ACCOMPLISHED IAW GMM 3-3 PROCEDURES PRIOR TO THE ACFT BEING RETURNEMay 5, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2014052710596Skin · crackedRT BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS ALL AROUND THE VERTICAL & HORIZONTAL LANDING 50 PERCENT FSH FAILED NDT. BLENDED RT WING LOWER SKIN PLANK AT BOOST PUMP LANDING IAW STS EA 26-2014-050.May 5, 2014 · N880AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014052710595Bearing · wornRUDDER UPPER AND LOWER CENTER HINGE BEARINGS HAVE EXCESSIVE PLAY. COMPLIED WITH EC/TC RIL 0602, REPAIR TYPE II: REPLACEMENT OF THE SWAGED BEARING IAW RIL 602, REV E.May 4, 2014 · N880AS · Cndair CL6002B19 · Rudder StructureSDR ASOA2014052710594Bracket · corrodedFOUND MAIN AVIONICS DOOR LATCH PIN RECEIVER SUPPORT BRACKET FS 364.00 FRAME SECTOR AT BL 0 TO BE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 T/R 53-27, FIG 102, SHEET 2. CORROSION IS ON OVERLAPPING ELEMENTS THRU RADIUS. LOCATED, DRILLED UP & INSTMay 3, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014052710593Intercostal · crackedFS 625 CRACKED INTERCOSTAL AT STRINGERS 13 & 14L. REMOVED INTERCOSTAL IAW SRM 51-42-21 AND 51-42-06. LOCATED & DRILLED INTERCOSTAL IAW SRM 51-40-11 AND DWG 601-35012. LOCATED NEW FASTENER HOLES TO NEW SERVICEABLE INTERCOSTAL IAW REO 601R-53-61-5265. MAJORMay 3, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014052710592Striker · dentedPASSENGER DOOR CUT-OUT SEAL STRIKER, UPPER, AT FS 310 IS DAMAGED. C/W BSC REO 601R-53-22-176 REV IAW SRM 51-42-06 AND 51-40-11.May 3, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014052710591Door Sill · corrodedSERVICE DOOR SILL IS CORRODED. REMOVED SERVICE DOOR SILL ANGLE IAW SRM 51-42-21. LOCATED AND DRILLED UP NEW SERVICE DOOR SILL ANGLE, PN 601R38303-253 IAW SRM 51-40-11 AND DWG 601R38303. INSTALLED SILL ANGLE IAW SRM 51-42-06 AND SRM 51-42-11.May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014052710590Door Frame · corrodedSERVICE DOOR SURROUND FWD FITTING AND FLOOR EDGE MEMBER ARE CORRODED AT BS 319. DAMAGE TO FLOOR EDGE MEMBER FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, TR 53-27 AND REQUIRES REPLACEMENT FROM FS 310-319. REMOVED AND LOCATED NEW PART, PN 601R31148-79 IAW SRM 5May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2014052710589Intercostal · corrodedBS 364 INTERCOSTAL BETWEEN 26L & 26R CORRODED. R & R INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014052710588Frame · corrodedFRAME AT BS 364 S23L - 23R IS CORRODED. R & R FRAME SUPPORT ANGLE FROM AFT SIDE OFFS 364.0 IAW SRM 51-42-06. R & R INTERCOSTALS AT LBL/RBL 18.0 BETWEEN FS 349.0-FS 364.0 IAW SRM 51-42-06. R & R FRAME SECTOR AND SPLICE ANGLE FROM FS 364.0 BETWEEN STRINGERS 2May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2014052710587Door Sill · corrodedCARGO BAY DOOR SILL HAS CORROSION AROUND NUTPLATE HOLES. REMOVED CORROSION IAW REO 601R-53-00-526. FOUND TO BE WITHIN LIMITS WITH MAX MATERIAL REMOVED .004, MAX ALLOWABLE .010. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526, REV.May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014052710586Stringer Clip · corrodedFS 280, STRINGER CLIP 3L CRACKED. REMOVED FS 280 STRINGER CLIP IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED, DRILLED AND INSTALLED NEW STRINGER CLIP IAW SRM 51-42-06 AND SRM 51-42-21.May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2014052710585Angle · crackedRT 484, ANGLE AT RBL 27 IS CRACKED .250L. REMOVED CRACKED ANGLE AND LOCATED, DRILLED & INSTALLED NEW ANGLE IAW SRM 51-40-11, 51-42-06 AND 51-42-21.May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014052710584Isolator · brokenBS 621 BULKHEAD FWD FACE HAS A BROKEN ISOLATOR. R & R BROKEN ISOLATOR IAW SRM 51-42-06.May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014052710583Fitting · crackedBS 460, FITTING ON OTBD SIDE OF RBL 9 IS CRACKED .5". REMOVED THE SUPPORT FITTING IAW SRM 51-42-21 AND 51-42-06. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE SUPPORT FITTING IAW SRM 51-40-11, 51-42-06 AND 51-42-21. MAJOR REPAIR.May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014052310582Bearing · wornRIGHT ELEVATOR FAILS BEARING BACKLASH FOR HYD SYS FOUND TO BE OUT OF LIMITS. REPLACED BEARINGS IAW AMM 20-26-00-910-807.May 2, 2014 · N880AS · Cndair CL6002B19 · Elevator StructureSDR ASOA2014052310581Bearing · wornLEFT ELEVATOR FAILS BEARING BACKLASH FOR HYD SYS FOUND TO BE OUT OF LIMITS REPLACED BEARING IAW EC/TC RIL 0183 AND RIL 0183, REV B.May 2, 2014 · N880AS · Cndair CL6002B19 · Elevator StructureSDR ASOA2014051210490Cargo Track · corrodedCARGO TRACK CORRODED LBL 9. R & R CARGO TRACK IAW AMM 20-21-00-910-801 AND SRM 51-40-11.May 2, 2014 · N880AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
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