N827AS, cancelled Apr 6, 2015

Service difficulty reports · 183

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 = 'N827AS' AND deregistration_id = 'N827AS-2015-04-06'
  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 ASOA2014020509885Frame · chafedFRAME AT BS 654.5 BETWEEN STRINGERS 13 & 14R HAS A HOLE CHAFED IN IT. .500" X 1.0". REPAIRED FRAME IAW EA 25-2014-028 DATED 1/26/2014.Jan 24, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2014020509884Skin · chafedLEFT LOWER WING PLANK AT LBL 45 IS CHAFED APPROX .7" W X 1.5" L X .038" DEEP ON AFT END. COMPLIED WITH EC/TC REO 601R-57-21-880 IAW REO 601R-57-21-880, REV C DATED 07/18/2011 AS WRITTEN.Jan 20, 2014 · N827AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014020509883Skin · chafedRT LOWER WING PLANK AT RBL 45 IS CHAFED APPROX .7" W X .15" L X .035" DEEP ON AFT END. COMPLIED WITH EC/TC REO 601R-57-21-880 IAW REO 601R-57-21-880, REV C DATED 7/18/2011 AS WRITTEN.Jan 20, 2014 · N827AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014020509882Skin · crackedLOWER WING PLANK RT BOOST PUMP CUTOUT LANDING FOR PANEL 610CB HAS MULTIPLE INDICATIONS NOTED ON HORIZONTAL AND VERTICAL SURFACES GREATER THAN 50 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSP. REMOVED RT BOOST PUMP FOR FOM IAW AMM 28-23-01-000-801. Jan 17, 2014 · N827AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014020509881Skin · crackedFUEL ACCESS HOLE 510AB HAS 2 INDICATIONS, 1 ON INBD SIDE .1 X .1 50 PERCENT FSH AND 1 ON FWD SIDE .1 X .1 50PERCENT FSH. FAILED NDT. MARK ON ACFT. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV K AND FORWARDED ALL REQUIRED FORMS TO ENGINEEJan 15, 2014 · N827AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014020509880Skin · crackedFUEL ACCESS HOLE 640AB HAS AN INDICATION .1 X .1 50 PERCENT FSH ON INBD FWD SIDE MARK ON A/C. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV F.Jan 15, 2014 · N827AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014020509879Floor Support · corrodedRT PRESSURE FLOOR SUPPORT AND ANGLE HAVE SEVERAL AREAS OF CORROSION FROM BS 409+128 - 559. REPAIRED IAW EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666, REV C.Jan 13, 2014 · N827AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014020509878Strap · corrodedSTRAP ON FLOORBEAM AT RBL 27-36 CORRODED AT BS 424. INSTALLED NEW STRAP IAW SRM 51-42-06 AND COMPLIED WITH EO 601R3105.Jan 12, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014020509877Support Angle · crackedUPON REMOVAL OF SUPPORT ANGLE, AT BS 621 AFT SIDE LBL 36 FOR ACCESS FOR FS 621 BULKHEAD REPAIR. IT WAS DISCOVERED ANGLE WAS CRACKED. RECEIVED NEW ANGLE 601R36008-34. LOCATED AND DRILLED ANGLE IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42Jan 10, 2014 · N827AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014020509876Stiffener · crackedFOUND STIFFENER ON AFT SIDE OF BULKHEAD CRACKED APPROX .75" LONG. STIFFENER IS ON OTBD SIDE OF LBL 36 & JUST ABOVE FLOOR LEVEL. REMOVED CRACKED STIFFENER FROM AFT SIDE OF FS 621 BULKHEAD ON OTBD SIDE OF LBL 36 JUST ABOVE FLOOR LEVEL IAW SRM CH 51-42-06. LOCJan 9, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014020509875Pressure Deck · crackedPRESSURE FLOOR CRACKED ALONG BUMP STOP BEAM AT BS 460 BETWEEN LBL 9-18. REPAIRED IAW REO 601R-53-41-1761.Jan 8, 2014 · N827AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA2014020509874Seat Track · corrodedCABIN RT SIDEWALL SEAT TRACK FROM BS 559+16 - 559+48 CORRODED. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. FABRICATED AND INSTALLED SEAT TRACK IAW REO 601R-53-00-485 AND SRM 53-01-11.Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020509873Seat Track · corrodedCABIN RT SIDEWALL SEAT TRACK FROM BS 499 - 559+16 CORRODED. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485L. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020509872Seat Track · corrodedRT SIDEWALL SEAT TRACK BS 449.85 - 499 IS CORRODED. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485. REMOVED IAW AMM 53-01-11-000-802 AND INSTALLED IAW AMM 53-01-11-400-802.Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020509871Seat Track · corrodedRT SIDEWALL SEAT TRACK FROM BS 409+16 - 409+112 IS CORRODED. REMOVED IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-000-802, SRM 51-40-11 AND 51-42-00 AND REO 601R-53-00-485. FABRICATED IAW REO 601R-53-00-485.Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020509870Seat Track · corrodedRT SEAT TRACK AT BS 559 IS CORRODED. REMOVED SEAT TRACK IAW GREO 601R-53-00-485. FABRICATED AND INSTALLED IAW GREO 601R-53-00-485.Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020509869Seat Track · corrodedLT SIDEWALL SEAT TRACK BS 544 -559+80 IS CORRODED. REMOVED SIDE SEAT TRACK IAW AMM 53-01-11-000-802. FABRICATED AND INSTALLED IAW CREO 601R-53-00-485.Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020509868Seat Track · corrodedLT SIDEWALL SEAT TRACK BS 449.85-499 CORRODED. REMOVED SEAT TRACK IAW 53-01-11-000-802 AMM. FABRICATED AND INSTALLED IAW CREO 601R-53-00-485.Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020509867Seat Track · corrodedLT SIDEWALL SEAT TRACK BS 409+112-449.85 CORRODED. REMOVED IAW AMM 53-01-11-000-802. FABRICATED AND INSTALLED IAW CREO 601R-53-00-485.Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020509866Seat Track · corrodedLEFT SIDEWALL SEAT TRACK BS 409+16-409+112 CORRODED. COMPLIED WITH EC/TC REO 601R-53-00-055 AND REO 601R-53-00-055, REV A.Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020509865Seat Track · corrodedSEAT TRACK BS 559-559+100 CORRODED. REMOVED AND INSTALLED SEAT TRACK IAW GREO 601R-53-00-485.Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020509864Seat Track · corrodedLEFT SEAT TRACK FROM BS 409+128-559 IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. COMPLIED WITH REO 601R-53-00-485. FABRICATED AND INSTALLED IAW REO 601R-53-00-485.Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020509863Post · crackedFOUND BS 409+128, FLOOR SUPPORT VERTICAL POST LBL 18 OTBD SIDE HAS A CRACK INDICATION .2" IN LENGTH. FAILED NDT INSPECTION. REMOVED POST IAW SRM 51-42-06 AND 51-42-21. INSTALLED IAW REO 601R-53-41-889.Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014020509862Floor Skin · crackedCRACKED PRESSURE FLOOR ALONG BUMP STOP BEAM AT BS 460 BETWEEN RBL 9-16. REPAIRED PRESSURE FLOOR SKIN IAW REO 601R-53-41-1761.Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA2014020509861Anchor Fitting · corrodedTHREE CARGO ANCHOR PLATES CORRODED BETWEEN BS 559+96-574 LBL 27. REMOVED THREE DAMAGED ANCHOR FITTINGS IAW SRM 51-41-04-00. AND INSTALLED IAW SRM 51-41-04-00.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020409860Anchor Fitting · corrodedTWO CARGO ANCHOR PLATES CORRODED BETWEEN BS 574 - 605 LBL 9.0. R & R ANCHOR PLATES IAW AMM 20-21-00-910-801.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020409859Cargo Track · corrodedCARGO TRACK CORRODED BETWEEN BS 559+95-567, RBL 9.0. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802 AND INSTALLED IAW SRM 53-01-11 AND REO 601R-53-00-485.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020409858Cargo Track · corrodedCARGO TRACK SEGMENT CORRODED BETWEEN FS 559+95-567, LBL 9.0. FABRICATED AND INSTALLED CARGO TRACK SEGMENT IAW REO 601R-53-00-485 REV.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020409857Cargo Track · corrodedCARGO TRACK SEGMENT CORRODED BETWEEN BS 559+80-559+96, RBL 9.0. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802 AND INSTALLED IAW SRM 53-01-11 AND AMM 53-01-11-000-802.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020409856Seat Track · corrodedCARGO TRACK SEGMENT CORRODED BETWEEN BS 559+80-559+96, LBL 9.0. R & R DAMAGED CARGO TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020409855Seat Track · corrodedSEAT TRACK SEGMENT CORRODED BETWEEN BS 559+80-559+96, RBL 27. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SEAT TRACK SEGMENT IAW AMM 53-01-11-400-802.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020409854Seat Track · corrodedSEAT TRACK SEGMENT CORRODED BETWEEN BS 559+80-559+96, LBL 27. REMOVED CORRODED SEAT TRACK IAW IAW AMM 53-01-11-000-802, REV 32-10, APR 12. LOCATED AND DRILLED FASTENER HOLES IN NEW SERVICEABLE SEAT TRACK IAW SRM 51-40-11. INSTALLED SEAT TRACK IAW AMM 53-01-Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020409853Cargo Track · corrodedCARGO TRACK CORRODED BETWEEN BS 605- 621, LBL 9. R & R DAMAGED CARGO TRACK WITH SERVICEABLE IAW SRM 51-41-02.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014020409852Floor Support · corrodedRIGHT CARGO FLOOR SUPPORT HAS CORROSION AROUND NUTPLATES ON BOTTOM BETWEEN BS 589-621, RBL 45. FOUND OUT LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014020409851Floorbeam · corrodedRT CARGO FLOORBEAM CAP HAS CORROSION AROUND FASTENER HOLES AT BS 589 BETWEEN RBL 27-45. DRILLED, LOCATED AND INSTALED NEW CAP IAW SRM 51-42-06, 51-40-11 AND 51-42-15.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014020409850Floorbeam · corrodedRT CARGO FLOORBEAM CAP STRIP HAS CORROSION AROUND FASTENER HOLES AT FS 589 BETWEEN RBL 9-RBL 27. R & R DAMAGED RT CARGO FLOORBEAM CAP STRIPS WITH SERVICEABLE FLOORBEAM CAP STRIPS BETWEEN IAW SRM 51-42-21, & 51-42-06.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014020409849Floor Support · corrodedLEFT FLOOR SUPPORT HAS CORROSION AROUND FASTENER HOLES BETWEEN BS 559+80 AND 559+96 LBL 45. COMPLIED WITH EC/TC REO 601R-53-00-526 AND GREO 601R-53-00-526 REV.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014020409848Floor Panel · crackedPRESSURE FLOOR IS CRACKED AT FS 460 BETWEEN RBL 0.0 AND RBL 9.0. REPAIRED IAW REO 601R-53-41-1761, REV P1 1/14/14.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA2014020409847Floorbeam · crackedBS 484 FLOORBEAM ANGLES ARE CRACKED AT LBL 27 AND 36. REMOVED AND INSTALLED IAW REO 601R-53-41-059.Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014020409846Attach Angle · crackedATTACH ANGLE ON FRAME AND FLOOR STRUCTURE AT BS 193 IS CRACKED IN RADIUS. REMOVED AND INSTALL NEW ANGLE IAW SRM 51-42-06.Jan 5, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2014020409844Bulkhead · damagedBS 621 BULKHEAD AT RBL 36.2 DAMAGED. REPAIRED IAW REO 601R-53-61-5137.Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014020409843Bulkhead · damagedFS 621 BULKHEAD AT RBL 27.5 DAMAGED. REPAIRED IAW REO 601R-53-61-5137.Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014020409842Bulkhead · damagedBS 621 BULKHEAD AT RBL 9.5 DAMAGED. REPAIRED IAW REO 601R-53-61-5137.Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014020409841Bulkhead · damagedBS 621, BULKHEAD AT LBL 9.5 DAMAGED. REPAIRED IAW REO 601R-53-61-5137.Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014020409840Bulkhead · damagedBS 621 BULKHEAD AT LBL 18.0 DAMAGED. REPAIRED IAW REO 601R-53-61-5137.Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014020409839Bulkhead · crackedBS 621 BULKHEAD HAS A .6 INCH CRACK IN THE WEB AT RBL 18, WL 131.2. REPAIRED IAW REO 601R-53-61-5137.Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014020409838Web · crackedBS 621 BULKHEAD HAS THREE CRACKS IN THE WEB . REPAIRED IAW REO 601R-53-61-5137.Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014020409837Bulkhead · crackedBS 621 BULKHEAD HAS A .5 INCH CRACK IN THE WEB AT LBL 27.5, WL 97.9. REPAIRED IAW REO 601R-53-61-5137.Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014020409836Bulkhead · crackedBS 621 BULKHEAD HAS A .5 INCH CRACK IN THE WEB AT LBL 36.2, WL 79.5. REPAIRED IAW REO 601R-53-61-5137.Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014020409835Light · no testTHE ACFT FAILED FUNCTIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM. REPAIRED IAW AMM 33-21-07-000-801 AND AMM 33-21-07-400-801.Jan 3, 2014 · N827AS · Cndair CL6002B19 · Emergency Lighting
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