N833AS, cancelled Apr 25, 2017

Service difficulty reports · 169

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 = 'N833AS' AND deregistration_id = 'N833AS-2017-04-25'
  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 ASOA2015072813396Battery Pack · inoperativeOVERWING EMERGENCY LIGHTS ON LT AND RT SIDES INOPERATIVE. R & R THE NR 3 BATTERY PACK IAW AMM 33-51-04. REF IPC 33-51-04, ITEM 137. OPS CHECKED GOOD.Jul 28, 2015 · N833AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013121109609Lamp · burned outRT SIDE FWD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.Dec 7, 2013 · N833AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013103009315Smoke Warning · illuminatedSMOKE INDICATION , CARGO SMOKE WARNING, BLEW CARGO BOTTLE, AND DIVERTED.Oct 29, 2013 · N833AS · Cndair CL6002B19 · Smoke DetectionSDR ASOA2013091209000Light · inoperativeTHE EXTERIOR EMERGENCY FLOODLIGHT AFT OF THE RT WING EMERGENCY EXIT IS INOPERATIVE. R & R THE FLOODLIGHT IAW AMM 33-51-21-400-801. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.Sep 8, 2013 · N833AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013091208999Skin · crackedSKIN FAILS NDT INBD SIDE APPROX 8" LT 60 PERCENT SCREEN HEIGHT (X .250). REPAIRED IAW EC/TC EO 600-57-81 AND REO 601R-57-71-030, REV K.Aug 27, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013091208998Skin · crackedSKIN FAILS NDT AROUND ENTIRE HOLE. REPAIRED IAW REO 601R-57-21-1992, ECTC EO 600-57-81 AND REO 601R-57-21-030, REV K.Aug 27, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013091208997Skin · crackedSKIN FAILS NDT MULTIPLE INDICATIONS INBD SIDE OF HOLE 50 PERCENT SCREEN HEIGHT. 1" L X .250. REPAIRED IAW EC/TC EO 600-57-81 AND REO 601R-57-71-030, REV K.Aug 27, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013091208996Skin · crackedSKIN FAILS NDT INBD SIDE 50 PERCENT SCREEN HEIGHT .200 X .200. REPAIRED IAW EC/TC EO 600-57-81 AND REO 601R-57-71-030, REV K.Aug 27, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013091208995Skin · crackedSKIN FAILS NDT WITH INDICATION ON INBD SIDE OF HOLE 2" L X .200 50 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC EO 600-57-81 AND IAW REO 601R-57-71-030, REV K.Aug 27, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013091208994Skin · crackedSKIN FAILS NDT AFT SIDE OF HOLE .200 X .200, 60 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC EO 600-57-81 AND IAW REO 601R-57-71-030, REV K.Aug 26, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013091208993Skin · crackedSKIN FAILS NDT INDICATIONS INBD & OTBD SIDE OF HOLE .500 X .250 70 PERCENT SCREEN HEIGHT. REPAIRED IAW EC/TC EO 600-57-81 AND IAW REO 601R-57-71-030, REV K.Aug 26, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013091208992Angle · crackedLT WING HAS A CRACKED ANGLE JUST FWD & INBD OF MLG. REMOVED 601R10213-11, ANGLE TO REPLACE WITH NEW ANGLE IAW SRM . INSTALLED ANGLE, PN 601R10213-11 IAW SRM 51-42-06, COUNTERSUNK & ALODINED SRM 51-21-00 & 51-40-11.Aug 26, 2013 · N833AS · Cndair CL6002B19 · Wing Miscellaneous StructureSDR ASOA2013091208991Structure · crackedRIGHT BOOST PUMP CUTOUT HOLE FAILS NDT WITH INDICATIONS ON AFT SIDE OF HOLE ON LANDING, GREATER THAN 50 PERCENT SCREEN HEIGHT, APROX 1. ALSO, HAS SMALLER INDICATIONS AROUND ENTIRE HOLE LANDING 10-20 PERCENT SCREEN HEIGHT APROX .1. REPAIRED IAW REO 601R-57-21-Aug 21, 2013 · N833AS · Cndair CL6002B19 · Wing, Attach FittingsSDR ASOA2013091208990Skin · crackedFOUND CARGO DOOR LOWER AFT CORNER FUSELAGE SKIN HAS INDICATION NOTED APRPOX .1" IN LENGTH 90 PERCENT FSH AT THIS LOCATION. IT ALSO, HAS PROTRUDING DENT .2" L X .2 W. FAILED NDT INSPECTION. REPAIRED IAW EO NR: CL 600-2B19-53-I00396 AND REO 601R-53-61-5011, Aug 21, 2013 · N833AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2013083008937Trunnion · crackedINDICATION NOTED IN RT SIDE TURNNION FITTING FASTENER HOLE, 6TH HOLE AFT 9 INDICATION NOTED IN TRUNNION FITTING. 60 PERCENT FULL SCREEN HEIGHT AT OTBD SIDE OF HOLE APPROX .20 IN LENGTH, HOLE FAILS NDT. REPAIRED IAW REO NR 601R-57-21-1988.Aug 19, 2013 · N833AS · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR ASOA2013082808923Post · crackedFS 409.128, RBL 18 VERTICAL POST HAD INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69, REPAIRED IAW REO 601R-53-41-889.Aug 19, 2013 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013091208989Skin · crackedSUSPECT CRACK AT RT WING WS 148.019, EXTENDING OUT FROM A FASTENER. SUSPECTED CRACK IS LOCATED AFT OF THE AFT WING SPAR BESIDE THE PIE PANEL AND DIRECTLY BELOW THE FLAP FLEX SHAFT. ITEM REQUIRES FURTHER INVESTIGATION. REPAIRED IAW SRM 51-42-06, SRM 51-42-2Aug 16, 2013 · N833AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013082808922Post · crackedFS 409+128, RBL 18 VERTICAL POST HAD INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69. REMOVED VERTICAL POST IAW SRM 51-42-06. INSTALLED POST IAW SRM 51-42-06 AND 51-42-22.Aug 15, 2013 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013082208898Post · crackedLBL 18 FS 409+128 OTBD VERT POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROX .250" LONG X 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED OTBD & INBD VERT POST AT FS 409+128 LBL 18 IAW SRM 51-42-06. LOCATED AND DRILLED NEW POSTS AND 601RAug 15, 2013 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013091208988Hinge · gougedPAX DOOR HINGE HALF ON FUSELAGE HAS ONE GOUGED LUG. LUG IS NEXT TO LAST LUG ON AFT END APPROX .025" L X .004" DEEP. REPAIRED IAW REO 601R-53-21-814, TYPE 1. MAJOR REPAIR.Aug 14, 2013 · N833AS · Cndair CL6002B19 · Fuselage, Door HingeSDR ASOA2013091208987Skin · dentedLT WING INBD GROUND SPOILER LOWER INBD SKIN HAS 2 EA DENTS APPROX .100 L X.100 W X .030 D. REPAIRED IAW REO 601R-57-71-382, REV "A".Aug 14, 2013 · N833AS · Cndair CL6002B19 · SpoilersSDR ASOA2013083008936Skin · chafedLEFT AILERON UPPER FIXED L/E IS CHAFED AT THREE LOCATIONS APPROX 6.0 INCHES LONG, .400 INCHES WIDE AND .012 INCHES DEEP. REPAIRED IAW REO 601R-57-60-013.Aug 14, 2013 · N833AS · Cndair CL6002B19 · AileronsSDR ASOA2013082208897Seat Track · corrodedSEAT TRACK FS 409 AND 409+128 CORRODED IN SEVERAL AREAS. REMOVED CABIN SEAT TRACK IAW AMM 53-01-11-00-802. LOCATED & INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802 AND SRM 51-40-11.Aug 14, 2013 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013082208896Seat Track · corrodedSEAT TRACK FS 349 AND FS 409 CORRODED IN SEVERAL AREAS. REMOVED SEAT TRACK IAW 53-01-11-000-802. DRILLED DEBURRED IAW AMM 53-01-11-400-802. INSTALLED NEW SEAT TRACK IAW 53-01-11-400-802. INSTALLED RT SEAT TRACK IAW AMM 53-01-11-400-802.Aug 14, 2013 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013082208895Angle · corrodedFS 280.00 FWD J ANGLE IS CORRODED. REMOVED CORRODED ANGLE IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-11, 51-42-06 AND 51-42-21.Aug 14, 2013 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013082208894Angle · crackedBS 484 ANGLE AT RBL 27 IS CRACKED. R & R CRACKED CLIP WITH NEW IAW SRM 51-42-21 AND 51-40-11.Aug 14, 2013 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013082208893Angle · crackedLT BS 484 ANGLE AT LBL 27 IS CRACKED. R & R CRACKED ANGLE WITH NEW IAW SRM 51-42-21 AND 51-40-11.Aug 14, 2013 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013062103863Flashlight · intermittentPILOT FLASHLIGHT WORKS INTERMITTENTLY. R & R CAPTAIN'S FLASHLIGHT IAW AMM 25-61-04, OPS CHECKED GOOD.Jun 17, 2013 · N833AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA2012091202190Inverter · unserviceableEMERGENCY EXIT DOOR LIGHTED SIGN AT ROW 8A HALF LIGHT. R & R NR 2 INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD.Sep 8, 2012 · N833AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012091202189Lamp · burned outEMERGENCY EXIT DOOR LIGHTED SIGN AT ROW 8D INOPERATIVE. R & R LAMP IAW AMM 33-51-13. OPS CHECKED GOOD.Sep 8, 2012 · N833AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2011121702377Relay · failedEMERGENCY LIGHTS FLICKERING. R & R ACCESS BUSS UNDER VOLTAGE RELAY (K1XD) IAW AMM 24-51-27. OPS CHECKED GOOD. OPS CHECK OF EMERGENCY LIGHT SYS IAW AMM 33-51-01. OPS CHECKED GOOD.Dec 17, 2011 · N833AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201101517Wire · misinstalledLOWER EMERGENCY LIGHT AT LT OVERWING EXIT IS INOPERATIVE. TROUBLESHOOT AND FOUND SPLICES ON WIRES MISSING. INSTALLED 2 NEW QUICK DISCONNECT SPLICES ON THE EMERGENCY LIGHT WIRES IAW ESPM CH 20-11-00 AND 20-16-00. PERFORMED OPS TEST OF LIGHTS IAW AMM 33-51-00Aug 8, 2011 · N833AS · Cndair CL6002B19 · Light System WiringSDR ASOA201101486Crossbeam · corrodedCORROSION FOUND ON FS 349 CROSSBEAM AT SERVICE DOOR. REPAIRED IAW REO 601R-53-61-1541.Aug 8, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201101480Sign · inoperativeRT SERVICE DOOR EXIT SIGN BETA LIGHTS HAS AN LIGHT INTENSITY LESS THAN 100. REMOVED AND REPLACED IAW AMM 33-51-09-400-802. FUNCTIONAL TESTED GOOD IAW AMM TASK 33-51-09-720-801.Aug 5, 2011 · N833AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201101460Pressure Blkhd · crackedREAR PRESSURE BULKHEAD IS CRACKED ABOVE CARGO DOOR, OVER AFT TRACK. PRESSURE BULKHEAD REPAIRED IAW ARM 51-52-06.Aug 5, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201101459Pressure Panel · misrepairedPRESSURE FLOOR DOUBLER CORRODED AFT OF FS 439.00 RBL43. APPEARS TO BE 10F6 UNDOCUMENTED DOUBLERS INSTALLED ON PRESSURE FLOOR. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3, MINIMUM MATERIAL REAug 5, 2011 · N833AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA201101467Seat Track · corroded3 INCH SEAT RAIL FWD OF FS 621.00 AT LBL 9.00 HAS CORROSION ON SURFACE IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAIL IAW AMAug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101466Seat Track · corrodedSHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT RBL 27.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACKAug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101465Seat Track · corrodedSHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT RBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101464Seat Track · corrodedSHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT LBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101463Seat Track · corrodedSHORT SEAT RAIL BETWEEN FS 559.00+80-FS559.00+96 AT LBL 27.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAIL IAW AMM 53-00-11-40Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101462Seat Track · corrodedSHORT SEAT RAIL BETWEEN FS 559.00+112-572.00 AT RBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALL NEW SEAT TRACK RAIL. INSTALLED SEAT TRACK RAILAug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101457Seat Track · corrodedSHORT SEAT RAIL BETWEEN FS 559.00+112-FS572.00 AT LBL 9.00 HAS SURFACE CORROSION IN CARGO COMPARTMENT. REMOVED SEAT TRACK AND TRANSFERRED HOLES TO NEW SEAT TRACK IAW SRM 51-40-11. THIS IS A MINOR REPAIR. INSTALLED SEAT TRACK RAIL IAW AMM 53-00-11-944-001.Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101451Angle · corrodedCORROSION FOUND ANGLE AT FS 349 AT SERVICE DOOR UNDER TEFLON CAP. REMOVED ANGLE & FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 51-21-06. INSTALLED SERVICABLE ANGLE IAW SRM 51-42-06.Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201101450Structure · corrodedCORROSION FOUND AT FS 349 AT PAX DOOR UNDER TEFLON CAP. BLENDED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00.Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201101449Nut Plate · corrodedPASSENGER DOOR SILL PLATE ANGLE CORRODED. UPON FURTHER INSPECTION FOUND 5 NUT CLIPS ONLY TO BE CORRODED. R & R IAW MINOR REPAIR.Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101448Floorbeam · crackedINBD AND OTBD CLIPS CRACKED AT FS280 LBL9. REMOVED CRACKED CLIPS INBD AND OTBD AT FS 280, LBL9 IAW SRM 51-42-00. INSTALLED NEW CLIPS AT FS 280, LBL9, INBD AND OTBD IAW SRM 51-42-00, PN 601R3113-57. THIS IS A MINOR REPAIR. CAMLOCK AT FS 280 CROSS BEAM REQUIAug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201101447Floorbeam · crackedINBD AND OTBD CLIPS CRACKED AT FS 280 RBL 9. REMOVED AND INSTALLED IAW SRM 51-42-00.Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201101446Frame · corrodedFRAME CORRODED AT FS319.70, STR 26R. REMOVED FRAME LOWER SECTION IAW SRM 51-42-06 & 51-42-21. DRILLED NEW SECTION OF FRAME & INSTALLED IAW SRM 51-42-06.Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201101445Frame · corrodedCORROSION AT FRAME FS 333 STR 26 & 27R. REMOVED CORROSION, FRAME FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS SRM 53-00-00.Aug 4, 2011 · N833AS · Cndair CL6002B19 · Fuselage Main, Frame
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