N826AS, cancelled Feb 27, 2015

Service difficulty reports · 127

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 = 'N826AS' AND deregistration_id = 'N826AS-2015-02-27'
  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 ASOA2014062710762Proximity Sensor · out of adjustMAIN GEAR WAS CYCLING UP AND DOWN AFTER TAKEOFF, NOSE GEAR WAS UNKNOWN, RAN THE GEAR DISAGREE CHECKLIST THE QRH AND LANDED WITH THREE GREEN AFTER EMERGENCY GEAR EXTENSION GEAR DISAGREE WARNING MESSAGE. ACFT RETURNED. ADJUSTED BOTH PROXIMITY SENSORS IAW AMM 32Jun 25, 2014 · N826AS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA2014050710468Wire · damagedEMERGENCY FLOODLIGHT INOPERATIVE AT BULKHEAD. REPAIRED WIRE SPLICE CONNECTOR IAW ESPM 20-17-31. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.May 3, 2014 · N826AS · Cndair CL6002B19 · Light System WiringSDR ASOA2013032503250Blades · damagedRT ENGINE FLAMED OUT ON DESCENT AT 4000 & 250 KIAS. ATTEMPTED RELIGHT UNSUCCESSFUL. COMPLIED WITH WITH AREA C BOROSCOPE INSPECTION IAW MANUAL 72-00-00. FOUND DAMAGE BLADES ON STAGE 6 T/E. R & R RT ENGINE IAW AMM 71-00-00. OP'S AND LEAK CHECK GOOD.Mar 19, 2013 · N826AS · Cndair CL6002B19 · Turbine SectionSDR ASOA2012092602304Wire · shortedEMERGENCY LIGHTS COME ON IN ARM POSTION. FOUND WIRE LQ1AZZ SHORTED IAW ESPM 20-12-01. INSTALLED SPLICE ON WIRE LQ1AZZ IAW ESPM 20-16-00. PERFORMED OPS TEST OF SERVICE LIGHTS IAW AMM 33-31-00-710-801. OPS CHECKED GOOD.Sep 23, 2012 · N826AS · Cndair CL6002B19 · Light System WiringSDR ASOA2012092602303Connector · damagedEMERGENCY LIGHTS AT PAX DOOR INOPERATIVE. EMERGENCY LIGHT HAS A CONNECTOR DAMAGED. INSTALLED NEW PIN AND CONNECTOR ONTO WIRE OF EMERGENCY LIGHT IAW ESPM 20-11-00, 20-12-00-20-17-10.Sep 23, 2012 · N826AS · Cndair CL6002B19 · Light System WiringSDR ASOA2012092602301Structure · corrodedPAX DOOR AFT BOTTOM CORNER CORRODED. REMOVED PAX DOOR AFT BOTTOM CORNER (2 PART) IAW SRM 51-42-06. INSTALLED NEW ASD AFT BOTTOM CORNER (2 PART) IAW SRM 51-42-06 DWG NR 600-31998. REPAIR CLASSIFIED AS MAJOR.Sep 11, 2012 · N826AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012092602300Structure · corrodedPAX DOOR FWD BOTTOM CORNER CORRODED. REMOVED FWD BOTTOM CORNER (2 PART) IAW SRM 51-42-06. INSTALLED NEW ASD FWD BOTTOM CORNER IAW SRM 51-42-06, 51-42-21. REPAIR CLASSIFIED AS MAJOR.Sep 11, 2012 · N826AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012092602299Floor Support · corrodedDURING REINSPECTION IAW EO 600-53-216/01 ADDITIONAL CORROSION ON LT FLOOR SUPPORT FROM FS 409 + 128 - FS 559.00 WAS FOUND. REMOVED CORROSION IAW SRM 51-21-06 35. FOUND TO BE OUT OF LIMITS IAW GREO 601R-53-41-666. COMPLIED WITH REO 601R-53-41-666 AND REO 601Sep 6, 2012 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012092602298Floor Support · corrodedDURING REINSPECTION IAW EO 600-53-216/01 FOUND ADDITIONAL CORROSION ON FLOOR SUPPORT FROM FS 409 + 128 TO FS 559.0 ON RT SIDE. REMOVED CORROSION IAW SRM 51-21-06, 33 AREAS. FOUND TO BE OUT OF LIMITS OF GREO 601R-53-41-666. COMPLIED WITH REO 601R-53-41-1624 Sep 6, 2012 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012092602297Isolator · brokenTWO ISOLATORS BROKEN ON AFT BULKHEAD. REMOVED AND REPLACED ISOLATORS IAW SRM 51-42-13.Sep 5, 2012 · N826AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2012092602296Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED AT RIVET. REPAIRED IAW GREO 601R-52-11-513. COMPLIED WITH EC/TC REO 601R-52-11-513.Sep 5, 2012 · N826AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201200946Flap System · unknownFLAPS FAIL AT ZERO WHEN SELECTING FLAPS AT EIGHT. EMERGENCY DECLARED . COMPLIED WITH AD 2009-06-12. PERFORMED TROUBLESHOOTING IAW FIM 27-50-00. FOUND NO FAULTS LOGGED IN FECU AND MDC. PERFORMED OPS TEST OF FLAPS. NO DEFECTS NOTED AND OP'S CHECKED GOOD IAMar 18, 2012 · N826AS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA201200366Warning Message · false activationAT FL 290, RECEIVED A HYD NR 2 HIGH TEMP CAUTION MESSAGE. COMPLIED WITH QRH AN LANDED AT NEAREST SUITABLE AIRPORT. EMERGENCY DECLARED. COULD NOT DUPLICATE COMPLAINT, PERFORMED FUNCTIONAL TEST OF HYD SYS 2 TEMP INDICATION IAW AMM 29-10-00-720-802. NO FURTHEFeb 1, 2012 · N826AS · Cndair CL6002B19 · Hydraulic Indicating SystemSDR ASOA201200347Bpsu · out of adjustFLAP FAIL AT ZERO DEGREES. EMERGENCY DECLARED. RIGGED LT AND RT BPSU, IAW AMM 27-51-01, PERFORMED ADJUSTMENT TEST OF FECU IAW AMM 27-51-05-05. OPS CHECKED GOOD, ACFT OK FOR SERVICE.Jan 29, 2012 · N826AS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA201200049Detector · failedFLAPS FAILED AT 0 DEGREES DURING CRUISE ALT NORMAL LANDING. EMERGENCY DECLARED. R & R SKEW DETECTION UNIT IAW AMM 27-51-15.Jan 4, 2012 · N826AS · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR ASOA201102431Pump · failedCLIMBING OUT OF SAV RECEIVED HYD 2 HI TEMP. FOLLOWED QRH TEMP CONTINUED TO CLIMB ABOVE 135 DEGREES C. DIVERTED, IAW QRH. EMERGENCY DECLARED. R & R NR 2 ENGINE DRIVEN HYD PUMP IAW AMM 29-11-01. OPS AND LEAK CHECKS GOOD.Dec 21, 2011 · N826AS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR ASOA201102258Battery Pack · dischargedEMERGENCY LIGHTS LEFT IN ON POSTION OVERNIGHT AND DISCHARGED THE BATTERIES, EMERGENCY LIGHTS NOW INOP. OPS CHECKED GOOD IAW AMM 33-51-00.Nov 27, 2011 · N826AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201101631Cooling Duct · disconnectedCOOL CAUTION MESSAGE DISPLAYED SHORTLY AFTER T/O, RAN QRH PRECEDURE, MESSAGE PERSISTED, ED T-4 EACH DISLAYED OVERHEAT AND ALL MESSAGE EXTINGUISHED. ( ACFT DIVERTED -- EMERGENCY DECLARED AS A PRECAUTION) CONNECTED THE SUPPLY DUCT TO PLENUM WITH CLAMP IAW AMSep 1, 2011 · N826AS · Cndair CL6002B19 · Air Distribution SystemSDR ASOA201101120Door · bindingPAX DOOR WILL NOT OPEN FROM OUTSIDE. OPS CHECK PAX DOOR SEVERAL TIMES IAW AMM 52-11-00. OPS CHECK GOOD NO FURTHER DEFECTS FOUND.Jun 4, 2011 · N826AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201100527Latch · bindingF/A STATES THAT MAIN CABIN DOOR LATCH WOULD NOT ACTUATE THE FIRST FEW TIMES TRIED TO OPEN THE DOOR UPON ARRIVAL. OPERATED PAX DOOR SEVERAL TIMES NO DEFECTS NOTED, OPS CHECKED GOOD IAW AMM 52-11-00.Mar 19, 2011 · N826AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201100433Door · lack of lubeMAIN DOOR CATCHES WHEN TRYING TO OPEN FROM OUTSIDE. PERFORMED LUBRICATION OF PAX DOOR IAW AMM 12-20-52. OPS CHECK GOOD AT THIS TIME. (CLOSED)Mar 6, 2011 · N826AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201100432Handle · damagedMAIN DOOR WILL NOT OPEN. RESECURED PAX DOOR INSIDE HANDLE STRAP IAW AMM 52-11-02. OPS CHECK GOOD AT THIS TIME. (CLOSED)Mar 6, 2011 · N826AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201100176Handle · out of rigPAX DOOR HANDLE IS VERY HARD TO OPEN AND STOW. APPEARS TO BE IMPROPERLY RIGGED. REMOVED PAX DOOR ACCESS PANELS. REMOVED CLOSING PLATE UNDER BOTTOM FOLDING STOP IAW AMM 52-11-23-820-801, STEP 3.A.2. REMOVED PAX DOOR STAIR PANELS IAW AMM 52-11-04-000-808 AJan 28, 2011 · N826AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201100159Light · brokenFLOOR EMERGENCY FLOOD LIGHT ON WARDROBE IS BROKEN. REPLACED EMERGENCY FLOOR LIGHT ON LOWER WARDROBE ASSY IAW AMM 33-51-19-400-801. OPS CHECKED GOOD IAW AMM 35-51-00-710-801.Jan 24, 2011 · N826AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201100158Skin · corrodedCORROSION ON BELLY SKIN AROUND FASTENERS STA 559+112 TO FS 574 BETWEEN STR 23R-24L.Jan 24, 2011 · N826AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201100127Frame · corrodedFS 333, FRAME IN BELLY IS CORRODED. PRIMED AND PAINTED REPAIR AREA IAW SRM 51-25-01. THIS REPAIR REQUIRES MAJOR/MINOR CLASSIFICATION IAW ASA SOP 5702. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. APPLIED CORROSION INHIBITOR TO BARE AREAS IJan 19, 2011 · N826AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201100141Skin · corrodedCORROSION ON BELLY SKIN AROUND FASTENERS STA 559+112 TO 574 BETWEEN STR 23R-24L. DOUBLER INSTALLED IAW REO 601R-53-61-3943Jan 14, 2011 · N826AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201100077Beam · crackedON THE ECU SUPPORT FRAME THE OTBD FWD BEAM ASSY IS CRACKED, PN 601R95156-66, AND THE INBD BEAM ASSY IS GOUGED. REMOVED INBD BEAM ASSY, PN 601R95155-76, IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE INBD BEAM, PN 601R95155-82 AND ANGLE, 601R95156-63 IAW SRM 51-Jan 10, 2011 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100051Intercostal · corrodedINTERCOSTAL CAP AT FS 559.00+80 BETWEEN RBL 9, 27 & FLOOR SUPPORT IS CORRODED. R & R INTERCOSTAL CAP AT FS 559.00+80 BETWEEN RBL 27 & RBL 9 FLOOR SUPPORT IAW SRM 51-42-06 & SRM 521-42-15. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702. (CLOSED)Jan 10, 2011 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100050Skin · crackedFUSELAGE SKIN IS CRACKED AT FS 235, LT SIDE BL 6.0, RT SIDE HAS BEEN PREVIOUSLY REPAIRED USING REO 601R-53-11-048. REPAIRED IAW REO 601R-53-11-2038.Jan 10, 2011 · N826AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201100076Intercostal · crackedCARGO TIE DOWN PAN AFT LOCATION HAS OTBD, AFT END CRACKED AT FASTENER HOLE ON INTERCOSTAL. R & R INTERCOSTAL, 601R35031-205, IAW SRM 51-42-06. (CLOSED)Jan 7, 2011 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100075Stringer · corrodedSTRINGER 26 RT HEAVILY CORRODED/PITTED AROUND RIVETS APPROX 1/2" 0 0.035" DEEP A FS 336 & 338. INSTALLED NEW STRINGER SEGMENT IAW SRM 53-00-03.Jan 6, 2011 · N826AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA201100042Angle · crackedANGLE UNDER CARGO SUPPORT SILL CRACKED. R & R ANGLE WITH SERVICEABLE ANGLE IAW SRM 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW ASA SOP 5702.Jan 6, 2011 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100036Post · crackedFOUND FS 409+128 VERTICAL POST RBL 18.0 INBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 55 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. REMOVED VERTICAL POST IAW SRM 51-42-06. INSTALLED NEW POST IAW SRM 51-42-06 AND REO 601R-53-41-889. CJan 5, 2011 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100035Skin · corrodedCORROSION ON BELLY SKIN AROUND FASTENERS STA 559+112 TO 574, BETWEEN STR 23R-24L. REMOVED CORROSION FROM BELLY SKIN IAW SRM 51-21-06. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-31 3C.Jan 5, 2011 · N826AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201100034Frame · corrodedFS 333, FRAME IN BELLY IS CORRODED. REMOVED CORRODED FRAME FROM FS 333 IAW SRM 51-42-06 AND 51-742-21. LOCATED AND DRILLED NEW FS 333 FRAME PIN 601R32004-55 AND INSTALLED IAW SRM 51-40-11, 51-42-21 & 51-42-06.Jan 5, 2011 · N826AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201100030Seat Track · corrodedLT AND RT FWD SEAT TRACK SEGMENTS ARE CORRODED. REMOVED 1 EA LT & RT FWD FLOOR SEAT TRACK SEGMENTS DUE TO CORROSION IAW AMM 53-01-11-000-802, STEPS 3B1-3B3. INSTALLED NEW LT & RT FWD FLOOR SEAT TRACK SEGMENTS IAW AMM 53-01-11-420-001, STEPS 3B1-3B8.Jan 4, 2011 · N826AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100029Isolator · crackedFS 621, PRESS BULKHEAD HAS CRACKED ISOLATORS AT RBL 27 (1), LBL 18 (2), LBL 27. REMOVED ISOLATOR MOUNTS. R & R ISOLATOR BRACKETS PN SL2337-3. REINSTALLED ISOLATOR MOUNTS IAW SRM 51-42-06 AND 51-23-00. PRIME TOUCHED UP ISOLATORS ASSY IAW SRM 51-25-06. THISJan 4, 2011 · N826AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201100028Sill · corrodedINTERCOSTAL CAP AT FS 589 BETWEEN RBL 27 AND FLOOR SUPPORT SILL IS CORRODED. REMOVED MINOR CORROSION ON INTERCOSTAL CAP, MAT LOSS .006 IAW SRM 51-21-06, 51-21-11 & 51-25-16. REPAIR CLASSIFIED AS A MINOR.Jan 4, 2011 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100027Floor Support · corrodedRT CARGO FLOOR SUPPORT FROM FS 621 TO 559+112 IS CORRODED. REMOVED MINOR CORROSION FROM RT FLOOR SUPPORT IAW SRM 51-21-06 APPROX .001 - .002. MATERIAL REMOVED WITHIN LIMITS. REPAIR IS CLASSIFIED AS A MINOR.Jan 4, 2011 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100026Seat Track · corrodedCARGO SEAT TRACK AT LBL 9 FS 621, FS 574 AND FS 559+80 IS CORRODED. REMOVED MINOR CORROSION ON INTERCOSTAL CAP, MAT LOSS .006 IAW SRM 51-21-06, 51-21-11 & 51-25-15. REPAIR CLASSIFIED AS A MINOR.Jan 4, 2011 · N826AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100025Seat Track · corrodedCARGO SEAT TRACK AT RBL 27, FS 559+80 IS CORRODED. INSTALLED NEW CARGO TRACK IAW AMM 53-01-11-400-802.Jan 4, 2011 · N826AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100024Seat Track · corrodedCARGO SEAT TRACK AT RBL 9 FS 559+112 AND 559+80 IS CORRODED. R & R SEAT TRACK SEGMENT IAW AMM 20-21-00-910-801.Jan 4, 2011 · N826AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100023Floor Support · corrodedFLOORBEAM CAP AT RBL 9 FS 621 TO FS 574 IS CORRODED. BLENDED CORROSION OF FLOORBEAM CAP IAW REO 601R-53-00-005. FOUND TO BE OUT OF LIMITS. REMOVED FLOORBEAM CAP IAW SRM 51-42-06. LOCATED AND DRILLED NEW FLOORBEAM CAP IAW SRM 51-40-11. INSTALLED NEW SERVIJan 4, 2011 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100022Intercostal · corrodedINTERCOSTAL CAP AT FS 589 BETWEEN RBL 9 AND 27 IS CORRODED. REMOVED MINOR CORROSION ON INTERCOSTAL CAP, MAT LOSS .006 IAW SRM 51-21-06, 51-21-11 & 51-25-16. REPAIR CLASSIFIED AS A MINOR REPAIR.Jan 4, 2011 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100021Intercostal · corrodedINTERCOSTAL CAP AT FS 589 BETWEEN LBL 9 AND 27 IS CORRODED. REMOVED MINOR CORROSION ON INTERCOSTAL CAP AT FS 589 BETWEEN RBL & LBL 9 MAT LOSS .006 IAW SRM 51-21-06, 51-21-11 & 51-25-15. REPAIR CLASSIFIED AS A MINOR.Jan 4, 2011 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100020Intercostal · corrodedINTERCOSTAL CAP AT FS 589 BETWEEN RBL AND LBL 9 IS CORRODED. BLENDED CORROSION ON FLOORBEAM IAW REO 601R-53-60-005, REV A AND FOUND TO BE OUT OF LIMITS REO 601R-53-00-005. REMOVED FLOORBEAM CAP FROM IAW SRM 51-42-06. LOCATED AND DRILLED NEW FLOORBEAM CAP Jan 4, 2011 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100019Floor Support · corrodedFLOORBEAM CAP AT RBL 27, FS 621 TO 574 IS CORRODED. BLENDED CORROSION ON FLOORBEAM CAP LBL 27 IAW REO 601R-53-60-005, REV A AND FOUND TO BE OUT OF LIMITS IAW REO 601R-53-00-005. REMOVED FLOORBEAM CAP IAW SRM 51-42-06. LOCATED AND DRILLED NEW CAP IAW SRM 51Jan 4, 2011 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100018Sill · corrodedCARGO DOOR CUTOUT FLOOR SUPPORT SILL IS CORRODED. REPLACED CARGO DOOR SILL PLATE IAW REO 601R-53-61-1574 & REO 601R-53-61-1574.Jan 4, 2011 · N826AS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201100013Frame · crackedLT AND RT 718 FRAMES ARE CRACKED BEHIND THE ACM'S. REF MWC CO 7210411, JOB 8721046, OPS 17 AND 18.Jan 3, 2011 · N826AS · Cndair CL6002B19 · Fuselage Main, Frame
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