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 SWIA2018040944487Bulkhead · gougedFOUND A GOUGE ON THE AFT SIDE OF THE BS 280 BULKHEAD. REPAIRED THE BULKHEAD IAW REO.Feb 20, 2018 · N854AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2018040944479Skin · corrodedRIGHT LOWER WING PLANK FUEL DRAIN HOLE INBD OF BOOST PUMP HAS CORROSION .5 INCHES AROUND ENTIRE CIRCUMFERENCE OF DRAIN VALVE HOLE. REPAIRED IAW REO.Feb 17, 2018 · N854AS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2018040944478Skin · damagedRIGHT LOWER WING PLANK FUEL DRAIN HOLE INBD OF BOOST PUMP FASTENER HOLES ARE ELONGATED. REPAIRED IAW REO. NO LEAKS NOTED.Feb 17, 2018 · N854AS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201844477Skin · dentedDENT WITH CREASE FOUND AT BS 654 TO 672, BETWEEN STRINGER 14L & 15L. REPAIRED THE SKIN IAW REO.Feb 12, 2018 · N854AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201844494Skin · crackedLEFT TRU LATCH SKIN CRACKED AT AFT LATCH. REMOVED AND REPLACED THE SKIN IAW REO AND SRM.Feb 11, 2018 · N854AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2018040944492Stringer · crackedSTRINGER 3L IS CRACKED AT BS 379. REPAIRED IAW AMM.Feb 10, 2018 · N854AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2018040944496Floor Support · corrodedLBL 9 FLOOR SUPPORT IS CORRODED FROM BS 409+128 TO 449.85. REPAIRED IAW REO.Feb 9, 2018 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018040944486Stringer · crackedSTRINGER 3L IS CRACKED JUST AFT OF BS 280. REMOVED AND REPLACED THE STRINGER IAW SRM.Feb 9, 2018 · N854AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA201844483Floor Support · corrodedRIGHT CABIN FLOOR SUPPORT, BS 449.85 CORRODED. REPAIRED IAW REO.Feb 9, 2018 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201844481Floorbeam · corrodedFLOORBEAM TEE HAS CORROSION BETWEEN RBL 9 AND LBL 9, BS 589. REPAIRED THE FLOORBEAM IAW REO.Feb 9, 2018 · N854AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201844475Angle · crackedLEFT INBOARD AND OUTBOARD ANGLES ARE CRACKED AT BS 484. REPLACED ANGLES IAW SRM AND REO.Feb 9, 2018 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018040944474Support Angle · crackedRIGHT INBOARD AND OUTBOARD SUPPORT ANGLES AT BS 484 ARE CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLES IAW REO.Feb 9, 2018 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201844493Floor Support · corrodedRIGHT FLOOR SUPPORT IS CORRODED BETWEEN BS 349 TO 367. REPLACED THE FLOOR SUPPORT IAW REO.Feb 8, 2018 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201844491Intercostal · corrodedINTERCOSTAL BETWEEN BS 364 TO 349, STRINGER 26L CORRODED. THE INTERCOSTAL WAS REPLACED IAW SRM.Feb 8, 2018 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201844490Floor Support · corrodedFLOOR SUPPORT RBL 9 UPPER INBOARD FLANGE IS CORRODED BETWEN BS 409 TO 409+80. REMOVED AND REPLACED IAW SRM AND REO.Feb 8, 2018 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018040944489Floor Support · corrodedFLOOR SUPPORT LBL 9 FLANGE CORRODED BETWEEN BS 409 TO 409+112. REMOVED AND REPLACED IAW REO AND SRM.Feb 8, 2018 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018040944488Frame Angle · corrodedFRAME ANGLE BS 409 IS CORRODED BETWEEN STRINGERS 26L AND 26R. REMOVED CORROSION IAW SRM.Feb 8, 2018 · N854AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2018040944485Frame · corrodedFRAME, BS.319 IS CORRODED BETWEEN STRINGERS 26R TO 26L. REMOVED AND REPLACED THE FRAME SECTOR IAW SRM.Feb 8, 2018 · N854AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201844482Angle · corrodedJ ANGLE ATTACHING TO BS 280 FLOORBEAM IS CORRODED BETWEEN LBL 9 AND RBL 9. REMOVED AND REPLACED IAW SRM AND REO.Feb 8, 2018 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201844480Floorbeam · corrodedFLOORBEAM UPPER FLANGE HAS SURFACE COROSSION AT BS 349, RBL36. REPAIRED THE FLOOR BEAM FLANGE IAW REO.Feb 8, 2018 · N854AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201844476Post · crackedBS 409 +118 VERTICAL POST AT RBL 18 OUTBOARD POST AFT SIDE IN RADIUS HAS A CRACK INDICATION. REMOVED AND REPLACED THE VERTICAL POST IAW REO.Feb 6, 2018 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018040944498Skin · dentedRIGHT INBOARD FLAP IS DENTED 6 INCHES FROM THE TRAILING EDGE AND 18 INCHES FROM THE INBOARD EDGE. REPAIRED IAW SRM.Feb 4, 2018 · N854AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018040944484Skin · dentedLEFT INBD FLAP LOWER SKIN DENTED. 4 INCHES FROM TRAILING EDGE, AND 8 INCHES FROM INBD EDGE. REPAIRED IAW REO.Feb 4, 2018 · N854AS · Cndair CL6002B19 · Trailing Edge FlapsSDR ASOA201703161333Skin · crackedRT LOWER WING PLANK HAS ONE CRACKED FASTENER HOLE. ENLARGED HOLE TO REMOVE CRACK AND INSTALLED FREEZE PLUGS IAW REO 601R-57-21-2547 AND EC/TC REO 601R-57-21-2547.Mar 16, 2017 · N854AS · Bombdr CL6002D15 · Wing, Plate/SkinSDR ASOA2016030814553Plunger · disconnectedF/A REPORTED MAIN PAX DOOR WOULD NOT OPEN. FOUND PLUNGER DISCONNECTED. R & R SCREW AND PIN TO INNER HANDLE ASSY IAW CMM 52-11-07. REF IPC 52-11-03. ITEMS 107 AND 110. PERFORMED OPS TEST OF THE PASSENGER DOOR HANDLES IAW AMM 52-11-03. NO DEFECTS FOUND. AMar 8, 2016 · N854AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2016022614514Door · bindingMAIN PAX DOOR WOULD NOT OPEN FROM INSIDE CABIN. OPENED AND CLOSED DOOR WITH NO DEFECTS NOTED. ACFT OK FOR SERVICE.Feb 26, 2016 · N854AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2015120614174Circuit Breaker · trippedEMERGENCY LIGHTS FAILED TO ACTIVATE. OPS CK SYSTEM, OPS CK GOOD, AMM 33-51-01.Dec 6, 2015 · N854AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015082813675Connector · disconnectedEMERGENCY EXIT LIGHTS INOPERATIVE ON F/A BS AND GALLEY 1. TROUBLESHOT EMERGENCY EXIT LIGHTS ON F/A BS AND GALLEY FOUND CONNECTORS FOR FLOOR EXIT SIGN AT SERVICE DOOR AND FLOOR LEVEL FLOOD LIGHT SWAPPED AND FLOOR EXIT SIGN WIRE AT SIGN, DAMAGED AT SIGN. PUT CAug 28, 2015 · N854AS · Cndair CL6002B19 · Light System WiringSDR ASOA2015082813674Lens · crackedWARDROBE EMERGENCY EXIT LIGHT LENS CRACKED. R & R WARDROBE LOWER EMERGENCY EXIT LIGHT LENS, REF AMM TASK 33-51-10-000-801 AND 33-51-10-400-801.Aug 28, 2015 · N854AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015081713673Bulkhead · crackedREAR PRESSURE BULKHEAD IS CRACKED ABOVE LINTEL AREA IS MARKED. COMPLIED WITH EC/TC REO 601R-53-61-1230 AND GREO 601R-53-61-1230, REV F DATED: 10/31/2011 AS WRITTEN. MODIFIED DOUBLER ITEM -1 IAW REO 601R-53-61-5546 P1. RECEIVED AND COMPLIED WITH EC/TC REO 60Aug 17, 2015 · N854AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015081513672Access Panel · crackedFUEL ACCESS HOLE 550FB HAS A INDICATION ON THE OTBD SIDE APPROXIMATELY .25 W X 9.0 LONG 50 PERCENT FSH FAILED NDT. COMPLIED WITH ECTC EO 600-57-81, C/W IAW REO 601R-57-21-030, REV L.Aug 15, 2015 · N854AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015081513671Access Panel · crackedFUEL ACCESS HOLE 650GB HAS INDICATION ON THE INBD & OTBD SIDE APPROXIMATELY .25 W X 8.0L FAILED NDT. COMPLIED WITH ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.Aug 15, 2015 · N854AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015081513670Access Panel · crackedFUEL ACCESS HOLE 550GB HAS A INDICATION ON FWD SIDE APPROXIMATELY .25W X 7.0L 65 PERCENT FSH FAILED NDT. COMPLIED WITH ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.Aug 15, 2015 · N854AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015081513669Access Panel · crackedLT FUEL ACCESS HOLE 550CB HAS INDICATION ON INBD SIDE APPROXIMATELY .25W X 9.0L 50 PERCENT FSH FAILED NDT. COMPLIED WITH ECTC EO 600-57-81, C/W IAW REO 601R-57-21-030, REV L.Aug 15, 2015 · N854AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015081513668Access Panel · crackedLT FUEL ACCESS HOLE 550DB HAS 2 INDICATIONS ON THE FWD & AFT SIDE APPROXIMATELY .25W X 4.0L 50 PERCENT FSH FAILED NDT. COMPLIED WITH ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L.Aug 15, 2015 · N854AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015081513667Access Panel · crackedFUEL ACCESS HOLE 640CB HAS A INDICATIONS ON THE INBD SIDE APPROXIMATELY .25 W X 7.0L 60 PERCENT FSH FAILED NDT. COMPLIED WITH ECTC EO 600-57-81, C/W IAW REO 601R-57-21-030, REV L.Aug 15, 2015 · N854AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015081213596Seat Track · corrodedSEAT TRACK SEGMENT CORRODED OUT OF LIMITS AT RBL 9 AND BS 409+128 - 559+32. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.Aug 12, 2015 · N854AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015081213595Seat Track · corrodedSEAT RAIL SEGMENT CORRODED OUT OF LIMITS AT RBL9 AND BETWEEN FS 559+32 AND FS 559+80. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802 .Aug 12, 2015 · N854AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015081213594Seat Track · corrodedCORROSION UNDER FIVE SCREW HEADS LBL 9 SEAT TRACK SEGMENT BETWEEN BS 559+32 AND 559+80. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802. FAug 12, 2015 · N854AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015081113666Skin · corrodedFUSELAGE SKIN UNDER FRAME BS 333 IS CORRODED BETWEEN STRINGERS 26 - 27L. REMOVED CORROSION FROM SKIN AT FS 333 IAW SRM 51-21-06-001-001. RECEIVED AND COMPLIED WITH EA 32-2015-331, REV.Aug 11, 2015 · N854AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2015081113665Frame · corrodedFRAME BS 333 IS CORRODED BETWEEN STRINGERS 26 AND 27L. REMOVED CORROSION DAMAGE FROM FS 333 BETWEEN STR 26L AND 26R FWD AND ADT SIDE IAW SRM 51-21-06. BLENDED AREA ARE OUT OF ALLOWABLE LIMITS IAW SRM 53-21-15. RECEIVED AND COMPLIED WITH EA 32-2015-332, REVAug 11, 2015 · N854AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015081013664Intercostal · crackedRADIUS CRACK FOUND ON END OF INTERCOSTAL AT BS 621 AND BETWEEN WL 82 - 100. REMOVED AND REPLACED THE INTERCOSTA IAW SRM 51-42-06, 51-42-21, AND DWG 601-35012.Aug 10, 2015 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015081013663Hinge · gougedPAX DOOR PIANO HINGE LUGS ON DOOR SIDE, NR 7, 15 AND 22. COMPLIED WITH EC/TC REO 601R-52-11-1347. BLENDED AREAS ARE WITHIN LIMITS IAW REO 601R-52-11-1347.Aug 10, 2015 · N854AS · Cndair CL6002B19 · Fuselage, Door HingeSDR ASOA2015081013662Hinge · gougedPAX DOOR ON PIANO HINGE LUGS 5, 13, AND 24 ON FUSE SIDE ARE GOUGED. COMPLIED WITH EC/TC REO 601R-53-21 REPAIR TYPE I. BLENDED LUGS ARE WITHIN ALLOWABLE LIMIT IAW REO 601R-53-21-814.Aug 10, 2015 · N854AS · Cndair CL6002B19 · Fuselage, Door HingeSDR ASOA2015080913661Frame · corrodedFS 349.0 FRAME CORRODED FWD AND AFT SIDES STR 25L-25R. CORROSION ON FRAME 349 OUT OF LIMITS IAW SRM 53-00-00. REMOVED FR 349 IAW SRM 51-42-06. RECEIVED NEW FRAME SECTOR & DRILLED ALL FASTENER ATTACH HOLES REF SRM 51-40-11 & DWG 601R32005. STIFFENER ANGLE UAug 9, 2015 · N854AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015080913660Intercostal · corrodedMAIN AVIONICS BAY INTERCOSTAL CORRODED FS 349-FS 364, STR 27L. REMOVED CORROSION FROM INTERCOSTAL FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001 AND 53-00-00-001-001. REMOVED INTERCOSTAL IAW SRM 51-42-06. REINSTALLED INTERCOSTAL IAW SRM 51-42-06 AND SRM Aug 9, 2015 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015080913659Intercostal · corrodedMAIN AVIONICS, BAY INTERCOSTAL CORRODED BS 349 - 364, STR 27R. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-0000-001-001. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001. REINSTALLED INTERCOSTAL IAW SRM 51-42-06 AND SRM 51-42-21. MECHANICALLY MEASURAug 9, 2015 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015080913658Door Sill · corrodedCORROSION FOUND ON AFT CARGO DOOR SILL AROUND SCREW HOLES. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526, REV-DATED 05/22/2013 AS WRITTEN.Aug 9, 2015 · N854AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015080913657Bulkhead Web · gougedFS 621.00 BULKHEAD FWD FACE WEB SCREW MARKS AT LB727.50, LBL18.0. RBL18.0, RBL27.50 AND RBL 36.20. COMPLIED WITH EC/TC REO 601R-53-61-2155 AND METAL THE REQUIREMENTS OF REO 601R-53-61-2155, REV A.Aug 9, 2015 · N854AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015080913656Glowstrip · deterioratedPANELS 232BZ, PHOTOLUMINESENT STRIP DISCOLORED AND TORN. R & R PHOTOLUMINESCENT STRIP ON PANEL 232BZ IAW AMM 11-3-00-000-801 AND 11-30-00-400-801.Aug 9, 2015 · N854AS · Cndair CL6002B19 · Emergency Equipment
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