N820AS

Service difficulty reports · 161

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 = 'N820AS' 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 ASOA2015012312076Inverter · inoperativeEMERGENCY LIGHT INOPERATIVE NEAR OVERWING EMERGENCY DOOR. R & R THE EMERGENCY LIGHT INVERTER, LT SIDE FWD OF EMERGENCY DOOR IAW AMM 33-51-07. OPS CHECK GOOD.Jan 21, 2015 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014102311477Sign · inoperativeLIGHTED FLOOR-LEVEL EXIT SIGN INOPERATIVE AT LT EMERGENCY EXIT. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.Oct 18, 2014 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014100911397Connector · damagedLIGHTED FLOOR-LEVEL EXIT SIGN AT LEFT EMERGENCY EXIT INOPERATIVE. R & R WIRE SPLICE CONNECTORS IAW SPM 20-17-31. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.Oct 6, 2014 · N820AS · Cndair CL6002B19 · Light System WiringSDR ASOA2014100311371Door · lack of lubeF/A COULD NOT OPEN PASSENGER DOOR FROM THE IN SIDE GROUND CREW HAD TO OPEN DOOR. LUBE THE HARDWARE AND PERFOMED. OPS CHECK IAW AMM 52-11-03, CHECK GOOD ACOK TO SERVICE.Sep 30, 2014 · N820AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2014071110854Door · out of limitsRIGHT TRU DOOR DOES NOT FIT PROPERLY, PARTICULARLY IN RVSM AREA. TRIMMED TO FIT RIGHT TRU DOOR IAW AMM 52-44-11. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.Jul 10, 2014 · N820AS · Cndair CL6002B19 · Service DoorsSDR ASOA2014071110853Door · out of limitsLEFT TRU DOOR DOES NOT FIT PROPERLY, PARTICULARLY IN RVSM AREA. TRIMMED TO FIT LT TRU DOOR IAW AMM 52-44-11. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.Jul 10, 2014 · N820AS · Cndair CL6002B19 · Service DoorsSDR ASOA2014050710467Sign · inoperativeEXIT SIGN INOPERATIVE. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.May 3, 2014 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014041710379Sign · inoperativeLEFT EMERGENCY EXIT LIGHTED FLOOR LEVEL EXIT SIGN INOPERATIVE. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD.Apr 14, 2014 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014041710378Sign · damagedGALLEY LIGHTED FLOOR LEVEL EXIT SIGN DAMAGED. R & R SIGN IAW AMM 33-51-10. SYS OPS CHECKED GOOD. NO FURTHER ACTION.Apr 14, 2014 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014032810206Sign · inoperativeFLOOR LEVEL EXIT SIGN INOPERATIVE AT LT OVERWING. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD.Mar 24, 2014 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014032810205Light · inoperativeFLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. R & R LIGHT ASSY IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD.Mar 24, 2014 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2014011609764O-Ring · failedAFTER TAKEOFF, RECEIVED RT OIL PRESSURE WARNING MESSAGE ACCOMPANIED WITH FLUCTUATIONS OF 25-36 PSI C/W QRH RETURNED TO DEPARTURE. ACFT RETURNED TO DEPARTURE AFTER TAKE OFF, EMERGENCY DECLARED. R & R RT ENGINE OIL PRESSURE SWITCH O-RING IAW AMM-79-31-03, LEAJan 6, 2014 · N820AS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR ASOA2013031303195Sill · corrodedPASSENGER DOOR LOWER SILL FROM FS 295 - 364 AT STRINGER LOCATION 18L IS CORRODED AT MULTIPLE LOCATIONS TO INCLUDE HANDRAIL STOW CUPS. REPAIRED FLOOR SILL FS 215 -364 IAW EO CL600-2B19-53-I00135.Feb 19, 2013 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013031303194Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT BL 0.0 WL 142 APPROX 1.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-4823 AND REO 601R-53-61-1285, REV D, DATED 10/31/2011.Feb 18, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013031303193Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50 WL 130 APPROX .2" IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541 REF D.Feb 18, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2013031303192Angle · crackedAFT SIDE OF REAR PRESSURE BULKHEAD HAS RT FS 621 - 625 OBLIQUE ANGLE CRACKED AT THE RADIUS APPROX .40" LONG. R & R RT FS 625 OBLIQUE ANGLE & SEALED IAW SRM REF 51-42-06, PN 601-35012-52.Feb 18, 2013 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013031303191Frame · corrodedMAIN AVIONIC COMPARTMENT FUSELAGE FRAME BS 333 IS CORRODED AT STR 26R. REMOVED CORRODED FRAME SEGMENT & SERVICEABLE REINFORCING ANGLE IAW SRM 51-42-06 & 51-42-21. INSTALLED NEW FRAME SECTOR AND REINSTALLED SERVICEABLE REINFORCING ANGLE IAW SRM 51-42-06 & 51Feb 15, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2013031303190Frame · corrodedMAIN AVIONIC COMPARTMENT FUSELAGE FRAME 319 IS CORRODED AT STR 26L. REMOVED FRAME SECTOR IAW SRM 51-42-06. LOCATED & DRILLED NEW FRAME SECTOR IAW 51-40-11. INSTALLED NEW FRAME SEGMENT IAW SRM 51-42-06 & 51-42-21.Feb 15, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2013031303189Frame · corrodedMAIN AVIONIC COMPARTMENT FUSELAGE FRAME BS 310 CORRODED AT STR 26R. REMOVED FRAME SECTOR IAW SRM 51-42-06 & 51-42-21. TRIMMED FRAME SECTOR TO FIT AND LOCATED DRILL DEBURR IAW SRM 51-40-11 & 51-42-06 & 51-21-11. INSTALLED FRAME SEGMENT IAW SRM 51-42-06 & 5Feb 15, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2013031303188Intercostal · corrodedMAIN AVIONIC COMPARTMENT DOOR CUTOUT INTERCOSTAL BETWEEN FS 349 AND 364 BETWEEN STR 26-27R IS CORRODED. REMOVED CORRODED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW INTERCOSTAL AND INSTALLED IAW SRM 51-42-06 AND 51-42-21.Feb 15, 2013 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013031303187Angle · crackedRBL 9 ANGLE ON OTBD SIDE AT FS 280 IS CRACKED. REMOVED ANGLE IAW SRM 51-42-21. LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-42-21 & 51-40-11.Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013031303186Attach Angle · crackedCO-PILOTS SIDE WINDOW POST AFT LOWER ATTCHMENT ANGLE IS CRACKED. R & R CO-PILOTS SIDE WINDOW POST AFT LOWER ATTACHMENT ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-21.Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2013031303185Attach Angle · crackedPILOTS SIDE WINDOW POST AFT LOWER ATTACHMENT ANGLE IS CRACKED. R & R PILOT SIDE WINDOW POST AFT LOWER ATTACHMENT ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-21.Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2013031303184Door Frame · corrodedMAIN AVIONICS COMPARTMENT DOOR CUTOUT FRAME AT FS 349 BETWEEN STRINGERS 26L AND 27L ARE CORRODED. REMOVED CORRODED FS 349 LWR FRAME SEGMENT IAW SRM 51-42-06 & 51-42-21. DRILLED & LOCATED NEW FRAME. INSTALLED NEW FS 349 LWR FRAME SEGMENT IAW SRM 51-42-06 & 51Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2013031303183Intercostal · corrodedMAIN AVIONICS COMPARTMENT DOOR CUTOUT INTERCOSTAL BETWEEN FS 349 AND 364 STRINGER 26L - 27L IS CORRODED. REMOVED CORRODED INTERCOSTAL, LOCATED & DRILLED NEW IAW SRM 51-42-06. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013031303182Seat Track · corrodedRT CABIN FLOOR 3RD SECTION OF SEAT TRACK IS CORRODED AT FS 449.85, 473.15, 513 AND 544 RBL 9. R & R RT CABIN FLOOR 3RD SECTION OF SEAT TRACK WITH A NEW SEAT TRACK IAW AMM 51-01-11-000-802 AND 51-01-11-400-802.Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013031303181Seat Track · corrodedRT CABIN FLOOR 2ND SECTION OF SEAT TRACK IS CORRODED AT FS 394, 409+8 AND 409+86 RBL 9. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-020-002, FIG 401.B 1-3. LOCATED & DRILLED NEW SEAT TRACK IAW SRM 51-40-11-00. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-40Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013031303180Seat Track · corrodedRT CABIN FLOOR FWD SEAT TRACK CORRODED AT FS 364 RBL 9. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-020-002, FIG 1B 1-3. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-420-001 FIG 401B 1-8.Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013031303179Seat Track · corrodedLEFT CABIN FLOOR 3RD SECTION OF SEAT TRACK IS CORRODED AT FS 449.85, 473.15, 513 AND 544 LBL 9. REMOVED SEAT TRACK IAW AMM 53-01-11-000-801. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802. FABRICATED SEAT TRACK IAW REO 601R-53-00-485.Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013031303178Seat Track · corrodedLEFT CABIN FLOOR 2ND SECTION OF SEAT TRACK IS CORRODED AT FS 394, 409+8 AND FS 409+16 LBL 9. REMOVED SEAT TRACK IAW AMM 53-01-11-000-801. LOCATED, DRILLED AND COUNTERSUNK NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW AMM 51-01-11-400-802.Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013031303177Seat Track · corrodedLT FWD SEAT TRACK IS CORRODED AT FS 364, LBL 9. R & R LT CABIN FLOOR FWD SEAT TRACK WITH A NEW SERVICEABLE RAIL IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013031303176Structure · crackedCARGO DOOR AFT VERTICAL MEMBER CRACKED INSIDE OF DOOR AT LOWER AFT DOOR STOP FITTING. R & R AFT VERTICAL MEMBER IAW SRM 51-42-06.Feb 13, 2013 · N820AS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR ASOA2013031303175Skin · crackedCARGO DOOR INNER SKIN CRACKED AT THE UPPER FWD STOP BRACKET. CUT AWAY DAMAGE TO CARGO DOOR INNER SKIN & CHANNEL WITH CAP ANGLE AT WL 97.25. NDT PERFORMED FOR CUT LINES, REFER TO FORM NDT-9. FABRICATED REPAIR PARTS, HEAT TREATED PARTS REQUIRED FROM TO CONDITIFeb 13, 2013 · N820AS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR ASOA2013031303174Light · failedSERVICE DOOR INNER HANDLE EXIT SIGN LIGHT FAILED FUNCTIONAL TEST. REMOVED LIGHT IAW AMM 33-51-09-000-802. INSTALLED SERVICEABLE LIGHT IAW AMM 33-51-09-400-802.Feb 12, 2013 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013031303173Bulb · inoperativeCABIN LIGHTING FAILED TESTS. R & R BULBS IAW AMM 33-21-01-000-801. OPS CHECKED GOOD IAW AMM 33-21-07-400-801.Feb 11, 2013 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013031303172Light · failedFLOOR EMERGENCY LIGHTS FAILED. INSTALLED SERVICEABLE LIGHT IAW AMM 33-51-01-400-801.Feb 11, 2013 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2012120402590Handle · lack of lubeON ARRIVAL TO ACFT FOUND MAIN CABIN DOOR OUTER HANDLE JAMMED CLOSED, MISALIGNED WITH RECESSED RECEPTICAL. HAD TO PRY HANDLE OUT TO OPEN DOOR DOES NOT APPEAR TO CLOSE PROPERLY. CLEANED AND LUBED PAX DOOR HANDLE AND PERFORMED OPS CHECKED IAW AMM 52-11-23.Nov 30, 2012 · N820AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012101802379Door · lack of lubePAX DOOR STICKS AND IS REPORTED TO BE DIFFICULT TO OPEN AND CLOSE. LUBRICATED PAX DOOR IAW AMM 52-10-00. OPS CHECKED GOOD, REF 12-20-52.Oct 16, 2012 · N820AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012081002049Valve · failed"GEAR DISAGREE "MASTER WARNING COMPLIED WITH QRH CYCLED GEAR TOOK APPROX 60 SEC FOR GEAR TO COME UP RT MAIN WAS SLOW TO COME DOWN HDY 3 PRESSURE WAS 2700PSI. EMERGENCY DECLARED AS A PRECAUTION. R & R PRIORITY VALVE IAW AMM 32-32-15 IPC REF 32-32-10 ITEM 205 Aug 6, 2012 · N820AS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA201200980Flap System · failedFLAPS FAIL, 20 DEGREES, UPON SELECTING FLAPS 30 DEGREES SPEED 180 KTS. EMERGENCY DECLARED, COMPLIED WITH EC/TC AD 2009-06-12. NO FAULTS. OK FOR SERVICEMar 20, 2012 · N820AS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA201200498Windshield · failedAT FL300 THE CAPTAINS WINDSHIELD BEGAN TO SPARK AND DELAMINATED RESULTING IN A CRACKED WINDSHIELD. FOLLOWED QRH, DIVERTED. R & R LT WINDSHIELD IAW AMM 56-11-01. LEAK AND OPS CHECKED GOOD.Feb 14, 2012 · N820AS · Cndair CL6002B19 · Flight Compartment WindowsSDR ASOA201102385Circuit Breaker · trippedEMERGENCY LIGHTS TURN ON WHEN SWITCH IS TURNED TO ARM. FOUND CIRCUIT BREAKER OPEN, CLOSED CIRCUIT BREAKER, OPS CHECKED GOOD IAW AMM 33-51-00.Dec 19, 2011 · N820AS · Cndair CL6002B19 · Light System WiringSDR ASOA201102090Coalescer Bag · contaminatedODOR IN CABIN ON GROUND AND IN FLIGHT. ODOR LIKE DIRTY SOCKS. OPS CHECK OF THE PACKS RT AND LT. OPS CHECKED GOOD, NO ODOR WITH REF TO AMM 21-51-00.Nov 1, 2011 · N820AS · Cndair CL6002B19 · Humidity Control SystemSDR ASOA201101943Fcu · failedFLAPS FAIL MESSAGE IN FLIGHT GOING FROM 0 TO 8 DEGREES. EMERGENCY DECLARED AS A PRECAUTION. R & R FECU IAW AMM 27-51-05. OPS CHECKED GOOD.Oct 11, 2011 · N820AS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA201100581Intercostal · crackedPAX DOOR LWR FWD INTERCOSTAL IN DRAIN RAMP AREA IS CRACKED. REMOVED UNSERVICABLE LWR FWD INTERCOSTAL AND INSTALLED SERVICABLE INTERCOSTAL IAW SRM 51-42-06 AND SRM 51-42-21. PAX DOOR LWR INNER STRUCTURE. THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY.Mar 16, 2011 · N820AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201100519Attach Angle · corrodedPAX DOOR LWR ATTACH ANGLES (5 EA) ARE CORRODED. REMOVED PAX DOOR LWR ATTACH ANGLES. LOCATED AND INSTALLED NEW ATTACH ANGLES IAW SRM 51-42-06.Mar 16, 2011 · N820AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201100497Floor Support · corrodedCARGO BAY FLOOR CAP STRIP BETWEEN STR9L AND STR27L AND FS 589 IS CORRODED. REMOVED FLOORBEAM CAP AND REPLACED WITH NEW STRIP IAW SRM 51-42-06. MAJOR REPAIR.Mar 16, 2011 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100496Floorbeam · crackedCARGO BAY FLOORBEAM CAP AT LBL9 OTBD FLANGE AT FS 589 IS CRACKED. REPAIRED FLOORBEAM IAW EC/TC REO 601R-53-61-4009 AND REO 601R-53-61-4009. MAJOR REPAIR.Mar 16, 2011 · N820AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201100619Sill · corrodedSERVICE DOOR SILL HAS CORROSION ACROSS SILL FROM FWD TO AFT FRAMES. REMOVED UNSERVICEABLE SERVICE DOOR SILL. INSTALLED SERVICEABLE DOOR SILL IAW SRM 51-42-21. THIS IS A MAJOR REPAIR SILL PLATE FOR THE SERVICE DOOR, FABRICATED AND INSTALLED IAW EO 600-53-0687Mar 13, 2011 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201100580Plate · corrodedCARGO DOOR SEAL PLATE IS CRACKED AT FS 589. R & R CARGO DOOR SEAL PLATE IAW SRM 51-42-06. THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY.Mar 13, 2011 · N820AS · Cndair CL6002B19 · Cargo/Baggage Doors
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