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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWIA2018040944487Bulkhead · gougedFOUND A GOUGE ON THE AFT SIDE OF THE BS 280 BULKHEAD. REPAIRED THE BULKHEAD IAW REO.SDR 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.SDR SWIA2018040944478Skin · damagedRIGHT LOWER WING PLANK FUEL DRAIN HOLE INBD OF BOOST PUMP FASTENER HOLES ARE ELONGATED. REPAIRED IAW REO. NO LEAKS NOTED.SDR SWIA201844477Skin · dentedDENT WITH CREASE FOUND AT BS 654 TO 672, BETWEEN STRINGER 14L & 15L. REPAIRED THE SKIN IAW REO.SDR SWIA201844494Skin · crackedLEFT TRU LATCH SKIN CRACKED AT AFT LATCH. REMOVED AND REPLACED THE SKIN IAW REO AND SRM.SDR SWIA2018040944492Stringer · crackedSTRINGER 3L IS CRACKED AT BS 379. REPAIRED IAW AMM.SDR SWIA2018040944496Floor Support · corrodedLBL 9 FLOOR SUPPORT IS CORRODED FROM BS 409+128 TO 449.85. REPAIRED IAW REO.SDR SWIA2018040944486Stringer · crackedSTRINGER 3L IS CRACKED JUST AFT OF BS 280. REMOVED AND REPLACED THE STRINGER IAW SRM.SDR SWIA201844483Floor Support · corrodedRIGHT CABIN FLOOR SUPPORT, BS 449.85 CORRODED. REPAIRED IAW REO.SDR SWIA201844481Floorbeam · corrodedFLOORBEAM TEE HAS CORROSION BETWEEN RBL 9 AND LBL 9, BS 589. REPAIRED THE FLOORBEAM IAW REO.SDR SWIA201844475Angle · crackedLEFT INBOARD AND OUTBOARD ANGLES ARE CRACKED AT BS 484. REPLACED ANGLES IAW SRM AND REO.SDR SWIA2018040944474Support Angle · crackedRIGHT INBOARD AND OUTBOARD SUPPORT ANGLES AT BS 484 ARE CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLES IAW REO.SDR SWIA201844493Floor Support · corrodedRIGHT FLOOR SUPPORT IS CORRODED BETWEEN BS 349 TO 367. REPLACED THE FLOOR SUPPORT IAW REO.SDR SWIA201844491Intercostal · corrodedINTERCOSTAL BETWEEN BS 364 TO 349, STRINGER 26L CORRODED. THE INTERCOSTAL WAS REPLACED IAW SRM.SDR SWIA201844490Floor Support · corrodedFLOOR SUPPORT RBL 9 UPPER INBOARD FLANGE IS CORRODED BETWEN BS 409 TO 409+80. REMOVED AND REPLACED IAW SRM AND REO.SDR SWIA2018040944489Floor Support · corrodedFLOOR SUPPORT LBL 9 FLANGE CORRODED BETWEEN BS 409 TO 409+112. REMOVED AND REPLACED IAW REO AND SRM.SDR SWIA2018040944488Frame Angle · corrodedFRAME ANGLE BS 409 IS CORRODED BETWEEN STRINGERS 26L AND 26R. REMOVED CORROSION IAW SRM.SDR SWIA2018040944485Frame · corrodedFRAME, BS.319 IS CORRODED BETWEEN STRINGERS 26R TO 26L. REMOVED AND REPLACED THE FRAME SECTOR IAW SRM.SDR SWIA201844482Angle · corrodedJ ANGLE ATTACHING TO BS 280 FLOORBEAM IS CORRODED BETWEEN LBL 9 AND RBL 9. REMOVED AND REPLACED IAW SRM AND REO.SDR SWIA201844480Floorbeam · corrodedFLOORBEAM UPPER FLANGE HAS SURFACE COROSSION AT BS 349, RBL36. REPAIRED THE FLOOR BEAM FLANGE IAW REO.SDR 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.SDR SWIA2018040944498Skin · dentedRIGHT INBOARD FLAP IS DENTED 6 INCHES FROM THE TRAILING EDGE AND 18 INCHES FROM THE INBOARD EDGE. REPAIRED IAW SRM.SDR SWIA2018040944484Skin · dentedLEFT INBD FLAP LOWER SKIN DENTED. 4 INCHES FROM TRAILING EDGE, AND 8 INCHES FROM INBD EDGE. REPAIRED IAW REO.SDR 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.SDR 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. ASDR ASOA2016022614514Door · bindingMAIN PAX DOOR WOULD NOT OPEN FROM INSIDE CABIN. OPENED AND CLOSED DOOR WITH NO DEFECTS NOTED. ACFT OK FOR SERVICE.SDR ASOA2015120614174Circuit Breaker · trippedEMERGENCY LIGHTS FAILED TO ACTIVATE. OPS CK SYSTEM, OPS CK GOOD, AMM 33-51-01.SDR 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 CSDR 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.SDR 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 60SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 .SDR 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. FSDR 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.SDR 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, REVSDR 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.SDR 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.SDR 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.SDR 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 USDR 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 SDR 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 MEASURSDR 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.SDR 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.SDR 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.
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