N854AS

Service difficulty reports · 270

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 = 'N854AS' 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 ASOA2015080913655Housing · crackedG1 EMERGENCY EXIT SIGN, LENS AND HOUSING ARE CRACKED. REMOVED G1 EMERGENCY EXIT SIGN FROM G1 GALLEY IAW AMM 33-51-10-000-801. INSTALLED A NEW FLOOR LEVEL EMERGENCY LIGHT OF T/E G1 PANEL IAW AMM 33-51-10-400-801. OPS TEST OF THE EMERGENCY LIGHTS IAW TASK 33-5Aug 9, 2015 · N854AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015080913593Seat Track · corrodedFLOOR SEAT TRACK CORRODED, BS 394 - 409.0+128, LBL 9.0. BLENDED CORRODED SEAT RAIL AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-79. REMOVED AND REPLACED THE SEAT TRACK IAW AMM-53-01-11-800-802 & AMM 53-01-11-400-802.Aug 9, 2015 · N854AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015080913584Seat Track · corrodedFLOOR SEAT TRACK CORRODED , FS 394-409.0+128, RBL 9.0. BLENDED CORRODED SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-04. FABRICATED NEW SEAT TRACK IAW REO 601T-53-00-485, REV A. INSTALLED SERVICEABLE SEAT TAug 9, 2015 · N854AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015080913583Seat Track · corrodedLT SIDEWALL SEAT TRACK CORRODED FS 409.0+16-FS 409.0+112. BLENDED CORRODED SEAT TRACK 9 FOUND TO BE OUT A LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK FROM LT SIDE WLL AT FS 409 & 16-409 & 112 IAW AMM 53-01-11-000-802. INSTALLED SEAT TRACK IAW AMM 53-01-11-4Aug 9, 2015 · N854AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015080913582Seat Track · corrodedLT SIDEWALL SEAT TRACK CORRODED, FS364 - 409.0+16. BLENDED CORRODED SIDEWALL SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK FROM LT SIDEWALL IAW AMM 53-01-11-00-802. LOCATED AND DRILLED REMAINING FASTENER HOLES IN LT SIDE SEAAug 9, 2015 · N854AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015080913581Seat Track · corrodedRT SIDEWALL SEAT TRACK CORRODED , BS 364-409+16 BLENDED CORRODED SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED CORRODED RT SEAT TRACK AT FS 364-FS 409+16 IAW AMM 53-01-11-000-802 AND LOCATED 16 HOLES ON NEW SEAT TRACK. INSTALLED NEW RT SAug 9, 2015 · N854AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015080913580Seat Track · corrodedRT SIDEWALL SEAT RAIL CORRODED, FS 409.0+16-FS 409.0+112. BLENDED CORRODED SEAT RAIL & FOUND TO BE OUT LIMITS IAW SRM 53-21-49. REMOVED SEAT RAIL IAW AMM 53-01-11-04. PREPARED FASTENER HOLES ON NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11. INSTALLED SEAT TRAug 9, 2015 · N854AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015080913579Coupling · corrodedRT WING L/E SUPPORT COUPLING CORRODED BETWEEN INBD & MID L/E'S MARKED. REMOVED CORRODED RT WING L/E SUPPORT COUPLING AND INSTALLED NEW SERVICABLE RT WING L/E SUPPORT COUPLING IAW SRM 51-42-06-00 AND 51-41-00-00. LOCATED AND DRILLED NEW SERVICABLE RT WING L/EAug 9, 2015 · N854AS · Cndair CL6002B19 · Wing Main, Frame StructureSDR ASOA2015080713578Angle · crackedANGLE CRACKED INSIDE AFT EQUIPMENT BAY AT BS 625.30 AND STR 14L. R & R THE ANGLE IAW SRM 51-42-21.Aug 7, 2015 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015070813284Bulb · burned outLEFT FUSELAGE EXTERNAL AFT EMERGENCY LIGHT IS INOPERATIVE. R & R LT AFT EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECKED GOOD.Jul 4, 2015 · N854AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013122009667Bulb · burned outCABIN CEILING EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-51-16. OPS CHECKED GOOD.Dec 17, 2013 · N854AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013092009053Skin · crackedLT WING CRACKED AT WS 149, LOWER SURFACE, MARKED. REPAIRED IAW GREO 601R-57-21-138, REV A. CLASSIFIED A MAJOR REPAIR IAW GMM 5-3.Sep 18, 2013 · N854AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2013091309001Light · inoperativeCABIN AFT MOST CEILING EMERGENCY LIGHT INOPERATIVE. R & R AFT MOST CEILING EMERGENCY LIGHT IAW 20-10-00.Sep 9, 2013 · N854AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013081608874Latch · lack of lubeSERVICE DOOR EXTERNAL HANDLE INOPERATIVE. CLEANED AND LUBRICATED SERVICE DOOR LATCH MECHANISM, OPS CHECKED GOOD IAW AMM 52-41-03.Aug 14, 2013 · N854AS · Cndair CL6002B19 · Service DoorsSDR ASOA2013081308866Frame · corrodedCORROSION ON TOP PLATE OF BS 349, FRAME BETWEEN 27R AND 42.90R REPAIRED IAW EO CL600-2B19-53I00362.Jul 29, 2013 · N854AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2013080608840Floor Support · corrodedCORROSION AROUND SCREW HOLE ON FLOOR SUPPORT AT BS 409.00 + 10. REPAIRED IAW REO 601R-53-31-797 IAW SRM 51-21-16 AND 51-45-00.Jul 29, 2013 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013073008809Frame · corrodedFRAME AT BS 333 AND BETWEEN RBL 27 TO 42.9 CORRODED. REPAIRED IAW SRM 51-21-06, SRM 53-21-15 SRM TR 53-27, FIG 102. REPAIR CLASSIFIED AS MAJOR.Jul 18, 2013 · N854AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2013072308751Angle · corrodedSERVICE DOOR SILL FWD AT FS 319 AND AFT FS 349 LOWER CORNER ANGLES CORRODED. REPAIR IS CLASSIFIED AS MAJOR. ANGLE REMOVED IAW SRM 51-41-02, 51-42-21. INSTALLED NEW SERVICEABLE ANGLE, IAW SRM 51-41-02 AND 51-42-21.Jul 18, 2013 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013080908853Frame · corrodedCORROSION ON TOP PLATE OF FS 349 FRAME BETWEEN 27R AND 42.90R. REMOVED ANGLE, IAW SRM 51-42-21, 51-42-06 ANGLE CORRODED BEYOND LIMITS. INSTALLED ANGLE THAT WAS FABRICATED IAW IAW EO CL600-2B19-53-I00362A INSTALLATION ACCOMPLISHED IAW SRM 51-42-06 AND 51-42-2Jul 14, 2013 · N854AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2013080908852Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT NR FS 449.85. REPAIRED IAW REO 601R-53-41-666, REV C. REPAIR CLASSIFIED AS MAJOR.Jul 14, 2013 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013080608839Floor Support · corrodedCORROSION AROUND SCREW HOLE ON FLOOR SUPPORT AT FS 409.00 + 10. REPAIRED IAW SRM 51-21-06 & REO 601R-53-31-797. REPAIR CLASSIFIED AS MAJOR.Jul 14, 2013 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013080608838Frame · corrodedCORROSION ON TOP PLATE OF BS 349, FRAME BETWEEN S9-27R. REPAIRED IAW SRM 51-21-06, 51-42-13, 51-42-06, 51-42-15, 51-42-21.Jul 14, 2013 · N854AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2013080608837Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT AT FS 352. REPAIRED IAW SRM 51-21-06, 51-42-16, 51-42-13. REPAIR CLASSIFIED AS MAJOR.Jul 14, 2013 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013073108821Floorboard · corrodedFLOORBOARD 231ALF HAS FIVE SCREW INSERTS AND 1 METAL SQUARE PAD THAT IS CORRODED. R & R WITH NEW SERVICEABLE INSERTS IAW SRM 51-74-06-02. METAL PAD IS COMPLETELY GONE CLEAED UP AREA IAW SRM 51-21-06. REPAIRED POTTED AREA IAW HEXCEL CMM REPAIR METHOD (F) INSJul 14, 2013 · N854AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA2013073008808Sill · corrodedSERVICE DOOR BOTTOM SILL CORRODED. REMOVED ANGLE AT FS 349 FOR SERVICE DOOR SILL IAW SRM 51-42-20-00, AND 51-42-06-00, AND 51-42-13-00. DRILLED NEW SILL IAW SRM 51-40-11 OK TO INSTALL CAP ANGLE AND SILL. INSTALLED SERVICE DOOR CAP ANGLE AND SILL IAW SRM 51Jul 14, 2013 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013072608790Floor Support · corrodedLEFT FLOOR SUPPORT CORRODED BETWEEN FS 349 AND 364. REPAIRED IAW TEMPORARY REV 53-27, AND 51-12-00-00. REPAIR CLASSIFIED AS MAJOR.Jul 14, 2013 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013072408763Frame · corrodedFRAME TOP PLATE CORRODED BETWEEN LBL 27-42.9 AT BS 349. REMOVED CORRODED FASTENERS AND REMOVED TOP PLATE AT FS 349, LBL 27 TO LBL 42.9 IAW SRM 51-42-10. RE-INSTALLED FASTENERS IAW SRM 51-42-13. REMOVED COROSION ON BEAM AT FS349 LBL27 TO LBL42.9 IAW SRM 51Jul 14, 2013 · N854AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2013072408762Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT AT FS 461. REPAIR IS CLASSIFIED AS A MAJOR. REPAIRED IAW REO 601R-53-41-666, REV C.Jul 14, 2013 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013072408761Floor Support · corrodedCORROSION ON LT FLOOR SUPPORT AT FS 439. CLASSIFIED AS A MAJOR REPAIR. REPAIRED IAW REO 601R-53-41-666, REV C.Jul 14, 2013 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013071908738Seat Track · corrodedSEAT TRACK SEGMENT BETWEEN FS 364 TO 394 RBL 9 IS HIGHLY CORRODED. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.Jul 14, 2013 · N854AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2013071808725Light · inoperativePASSENGER DOOR HANDLE BETA LIGHT FAILED FUNCTIONAL TEST. R & R PASSENGER DOOR HANDLE BETA LIGHT IAW AMM 23-57-09-000-801, 33-51-09-400-801. TESTED GOOD.Jul 14, 2013 · N854AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013062808533Lamp · burned outRT NR 1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS RT NR 1 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-12. OPS CHECKED GOOD.Jun 27, 2013 · N854AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2013060703775Handle · lack of lubeSERVICE DOOR WILL NOT OPEN FROM OUTSIDE. CLEANED AND LUBED DOOR OUTER HANDLE IAW AMM 12-20-55 AND OP'S TESTED SERVICE DOOR LATCH MECHANISM IAW AMM 52-41-02, OP'S CHECKED GOOD.Jun 3, 2013 · N854AS · Cndair CL6002B19 · Service DoorsSDR ASOA2012071901933Battery · inoperativeF/A FLASHLIGHT INOPERATIVE. REPLACED BATTERIES IAW AMM 25-61-04. ACFT OK FOR SERVICE.Jul 15, 2012 · N854AS · Cndair CL6002B19 · Emergency EquipmentSDR ASOA2012071901932Handle · lack of lubeSERVICE DOOR OUTER HANDLE WILL NOT POP OUT TO OPEN. LUBRICATED SERVICE DOOR OUTER HANDLE. OPS CHECKED GOOD IAW AMM 52-41-00. SDR CLOSED.Jul 15, 2012 · N854AS · Cndair CL6002B19 · Service DoorsSDR ASOA201201675Handle · lack of lubeSERVICE DOOR CAN NOT BE OPENED FROM OUTSIDE ACFT. TROUBLESHOT SERVICE DOOR, LUBE OUTER HANDLE. DOOR OPS CHECKED OK IAW AMM 52-40-00.May 22, 2012 · N854AS · Cndair CL6002B19 · Service DoorsSDR ASOA201201631Handle · lack of lubeMAIN CABIN DOOR INSIDE TED HANDLE DOES NOT PROPERLY STOW DOOR, DIFFICULT TO CLOSE/OPEN. LUBRICATED PAX DOOR TED HANDLE IAW AMM 12-20-52.May 7, 2012 · N854AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201200709Lever · out of adjustPAX DOOR WILL NOT OPEN FROM CABIN. FOUND OUTER DOOR HANDLE RELEASE LEVER OUT OF ADJUSTMENT. RE-ADJUSTED RELEASE LEVER TO PROPER DIMENSIONS. OPS CHECKED GOOD IAW AMM 52-11-03. ACFT OK FOR SERVICE. (SDR CLOSED)Mar 3, 2012 · N854AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201102316Door · bindingSERVICE DOOR WILL NOT OPEN FROM OUTSIDE. OPS CHECKED SERVICE DOOR IAW AMM 52-41-00. NO DEFECT NOTED.Dec 4, 2011 · N854AS · Cndair CL6002B19 · Service DoorsSDR ASOA201101513Door · out of adjustRT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST - FORCE NECESSARY TO OPERATE HANDLE IS 55 LBF, ALLOWABLE LIMIT IS 30 LB. REMOVED RT EMERGENCY EXIT LINING PANEL 843AZ IAW AMM 52-21-02-000-801, STEP 2B. INSTALLED RT OVERWING EMERGENCY EXIT LINING PANEL 843AZAug 12, 2011 · N854AS · Cndair CL6002B19 · Emergency ExitsSDR ASOA201101502Bulkhead · crackedFS 202.75 FWD PRESS BULKHEAD HAS SEVERAL CRACKS AT PARKING BRAKE CABLE CUTOUT. OPS TEST OF THE PARKING BRAKE SYS DUE IAW AMM TASK 32-45-00-710-801. PERFORMED OPS TEST OF THE PARKING BRAKE SYS IAW AMM 32-45-00-710-801. OPS TEST GOOD. REPAIR REQ'D. REPAIRED Aug 8, 2011 · N854AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201101422Post · crackedFOUND FS 409.0+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FS AFT WL 69.0 AFT FLANGE RADIUS FAILED NDT INSP. REMOVED POST IAW SRM 51-42-06. INSTALLED POST IAW SRM 51-42-06.Aug 1, 2011 · N854AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201101421Post · crackedFOUND FS 409+128 VERTICAL POST LBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS FAILED NDT INSPECTION. EC/TC SIGN OFF STATEMENT REQUIRED. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL REQUIRES OF RAug 1, 2011 · N854AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201101420Seat Track · corrodedCABIN SEAT TRACK ARE CORRODED AT LBL 9 FROM FS 364 TO FS 409+126. REPAIRED IAWREO 601R-53-00-432.Aug 1, 2011 · N854AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101419Bulkhead · crackedFS 202.75 FWD PRESSURE BULKHEAD HAS SEVERAL CRACKS AT PARKING BRAKE CABLE CUT-OUT.Aug 1, 2011 · N854AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201101398Placard · deterioratedFLT DECK EMERGENCY ESCAPE HATCH EXTERIOR PLACARDS ARE WORN. REAPPLIED EXTERIOR PLACARDS ON CREW ESCAPE HATCH EXTERIOR IAW MM 11-10-03-400-801.Jul 27, 2011 · N854AS · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201101391Isolator · brokenFS 621 FWD SIDE HAS 6 BROKEN ISOLATORS. REMOVED AND REPLACED ISOLATORS IAW SRM 51-42-12.Jul 27, 2011 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201101390Seat Track · corrodedCABIN SEAT TRACK CORRODED AT RBL 9 FROM FS 364.00 TO 409.00+126. REMOVED SEAT TRACK IAW AMM 53-01-11. INSTALLED NEW IAW SRM 51-40-11 AND AMM 53-01-11 TASK 53-01-11-400-802, SUBTASK 53-01-11-420-001.Jul 27, 2011 · N854AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101380Bulkhead · crackedREMOVED PARKING BRAKE CABLE FROM FS 202.75 IAW AMM 32-45-01-000-801. INSTALLED PARKING BRAKE CABLE IAW AMM TASK 32-45-01-400-801. ADJUSTMENT CHECK GOOD IAW AMM TASK 32-45-01-820-801. REMOVED NLG SELECTOR VALVE AND ASSOCIATED HYD LINES IAW AMM 32-33-10-000-80Jul 25, 2011 · N854AS · Cndair CL6002B19 · Fuselage Structure (General)SDR ASOA201101382Post · crackedFOUND FS 409.0+128 VERTICAL POST LBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS FAILED NDT INSP. REMOVED POST IAW SRM 51-42-06. LOCATED AND DRILLED NEW PART IAW SRM 51-40-11. INSTALLED POSTIAW EC/TC RJul 25, 2011 · N854AS · Cndair CL6002B19 · Fuselage Main, Structure
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