# Service difficulty reports: N827AS, cancelled Apr 6, 2015 A list on [N827AS, cancelled Apr 6, 2015](https://openairdocs.org/deregistered/N827AS-2015-04-06.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 4 · 183 reports - [SDR ASOA2014020509885](https://openairdocs.org/sdr/ASOA2014020509885.md): Frame · chafed · Jan 24, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Frame > FRAME 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. - [SDR ASOA2014020509884](https://openairdocs.org/sdr/ASOA2014020509884.md): Skin · chafed · Jan 20, 2014 · N827AS · Cndair CL6002B19 · Wing, Plate/Skin > LEFT 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. - [SDR ASOA2014020509883](https://openairdocs.org/sdr/ASOA2014020509883.md): Skin · chafed · Jan 20, 2014 · N827AS · Cndair CL6002B19 · Wing, Plate/Skin > RT 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. - [SDR ASOA2014020509882](https://openairdocs.org/sdr/ASOA2014020509882.md): Skin · cracked · Jan 17, 2014 · N827AS · Cndair CL6002B19 · Wing, Plate/Skin > LOWER 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. - [SDR ASOA2014020509881](https://openairdocs.org/sdr/ASOA2014020509881.md): Skin · cracked · Jan 15, 2014 · N827AS · Cndair CL6002B19 · Wing, Plate/Skin > FUEL 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 ENGINEE - [SDR ASOA2014020509880](https://openairdocs.org/sdr/ASOA2014020509880.md): Skin · cracked · Jan 15, 2014 · N827AS · Cndair CL6002B19 · Wing, Plate/Skin > FUEL 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. - [SDR ASOA2014020509879](https://openairdocs.org/sdr/ASOA2014020509879.md): Floor Support · corroded · Jan 13, 2014 · N827AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > RT 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. - [SDR ASOA2014020509878](https://openairdocs.org/sdr/ASOA2014020509878.md): Strap · corroded · Jan 12, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > STRAP ON FLOORBEAM AT RBL 27-36 CORRODED AT BS 424. INSTALLED NEW STRAP IAW SRM 51-42-06 AND COMPLIED WITH EO 601R3105. - [SDR ASOA2014020509877](https://openairdocs.org/sdr/ASOA2014020509877.md): Support Angle · cracked · Jan 10, 2014 · N827AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > UPON 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 51-42 - [SDR ASOA2014020509876](https://openairdocs.org/sdr/ASOA2014020509876.md): Stiffener · cracked · Jan 9, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > FOUND 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. LOC - [SDR ASOA2014020509875](https://openairdocs.org/sdr/ASOA2014020509875.md): Pressure Deck · cracked · Jan 8, 2014 · N827AS · Cndair CL6002B19 · Fuselage Floor Panel > PRESSURE FLOOR CRACKED ALONG BUMP STOP BEAM AT BS 460 BETWEEN LBL 9-18. REPAIRED IAW REO 601R-53-41-1761. - [SDR ASOA2014020509874](https://openairdocs.org/sdr/ASOA2014020509874.md): Seat Track · corroded · Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CABIN 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. - [SDR ASOA2014020509873](https://openairdocs.org/sdr/ASOA2014020509873.md): Seat Track · corroded · Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CABIN 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. - [SDR ASOA2014020509872](https://openairdocs.org/sdr/ASOA2014020509872.md): Seat Track · corroded · Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RT 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. - [SDR ASOA2014020509871](https://openairdocs.org/sdr/ASOA2014020509871.md): Seat Track · corroded · Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RT 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. - [SDR ASOA2014020509870](https://openairdocs.org/sdr/ASOA2014020509870.md): Seat Track · corroded · Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RT 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. - [SDR ASOA2014020509869](https://openairdocs.org/sdr/ASOA2014020509869.md): Seat Track · corroded · Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LT 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. - [SDR ASOA2014020509868](https://openairdocs.org/sdr/ASOA2014020509868.md): Seat Track · corroded · Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LT 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. - [SDR ASOA2014020509867](https://openairdocs.org/sdr/ASOA2014020509867.md): Seat Track · corroded · Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LT 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. - [SDR ASOA2014020509866](https://openairdocs.org/sdr/ASOA2014020509866.md): Seat Track · corroded · Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT 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. - [SDR ASOA2014020509865](https://openairdocs.org/sdr/ASOA2014020509865.md): Seat Track · corroded · Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK BS 559-559+100 CORRODED. REMOVED AND INSTALLED SEAT TRACK IAW GREO 601R-53-00-485. - [SDR ASOA2014020509864](https://openairdocs.org/sdr/ASOA2014020509864.md): Seat Track · corroded · Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT 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. - [SDR ASOA2014020509863](https://openairdocs.org/sdr/ASOA2014020509863.md): Post · cracked · Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FOUND 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. - [SDR ASOA2014020509862](https://openairdocs.org/sdr/ASOA2014020509862.md): Floor Skin · cracked · Jan 7, 2014 · N827AS · Cndair CL6002B19 · Fuselage Floor Panel > CRACKED PRESSURE FLOOR ALONG BUMP STOP BEAM AT BS 460 BETWEEN RBL 9-16. REPAIRED PRESSURE FLOOR SKIN IAW REO 601R-53-41-1761. - [SDR ASOA2014020509861](https://openairdocs.org/sdr/ASOA2014020509861.md): Anchor Fitting · corroded · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > THREE 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. - [SDR ASOA2014020409860](https://openairdocs.org/sdr/ASOA2014020409860.md): Anchor Fitting · corroded · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > TWO CARGO ANCHOR PLATES CORRODED BETWEEN BS 574 - 605 LBL 9.0. R & R ANCHOR PLATES IAW AMM 20-21-00-910-801. - [SDR ASOA2014020409859](https://openairdocs.org/sdr/ASOA2014020409859.md): Cargo Track · corroded · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CARGO 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. - [SDR ASOA2014020409858](https://openairdocs.org/sdr/ASOA2014020409858.md): Cargo Track · corroded · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CARGO TRACK SEGMENT CORRODED BETWEEN FS 559+95-567, LBL 9.0. FABRICATED AND INSTALLED CARGO TRACK SEGMENT IAW REO 601R-53-00-485 REV. - [SDR ASOA2014020409857](https://openairdocs.org/sdr/ASOA2014020409857.md): Cargo Track · corroded · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CARGO 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. - [SDR ASOA2014020409856](https://openairdocs.org/sdr/ASOA2014020409856.md): Seat Track · corroded · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CARGO 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. - [SDR ASOA2014020409855](https://openairdocs.org/sdr/ASOA2014020409855.md): Seat Track · corroded · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SEAT 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. - [SDR ASOA2014020409854](https://openairdocs.org/sdr/ASOA2014020409854.md): Seat Track · corroded · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SEAT 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- - [SDR ASOA2014020409853](https://openairdocs.org/sdr/ASOA2014020409853.md): Cargo Track · corroded · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CARGO TRACK CORRODED BETWEEN BS 605- 621, LBL 9. R & R DAMAGED CARGO TRACK WITH SERVICEABLE IAW SRM 51-41-02. - [SDR ASOA2014020409852](https://openairdocs.org/sdr/ASOA2014020409852.md): Floor Support · corroded · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > RIGHT 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. - [SDR ASOA2014020409851](https://openairdocs.org/sdr/ASOA2014020409851.md): Floorbeam · corroded · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > RT 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. - [SDR ASOA2014020409850](https://openairdocs.org/sdr/ASOA2014020409850.md): Floorbeam · corroded · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > RT 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. - [SDR ASOA2014020409849](https://openairdocs.org/sdr/ASOA2014020409849.md): Floor Support · corroded · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LEFT 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. - [SDR ASOA2014020409848](https://openairdocs.org/sdr/ASOA2014020409848.md): Floor Panel · cracked · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage Floor Panel > PRESSURE 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. - [SDR ASOA2014020409847](https://openairdocs.org/sdr/ASOA2014020409847.md): Floorbeam · cracked · Jan 6, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > BS 484 FLOORBEAM ANGLES ARE CRACKED AT LBL 27 AND 36. REMOVED AND INSTALLED IAW REO 601R-53-41-059. - [SDR ASOA2014020409846](https://openairdocs.org/sdr/ASOA2014020409846.md): Attach Angle · cracked · Jan 5, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings > ATTACH ANGLE ON FRAME AND FLOOR STRUCTURE AT BS 193 IS CRACKED IN RADIUS. REMOVED AND INSTALL NEW ANGLE IAW SRM 51-42-06. - [SDR ASOA2014020409844](https://openairdocs.org/sdr/ASOA2014020409844.md): Bulkhead · damaged · Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > BS 621 BULKHEAD AT RBL 36.2 DAMAGED. REPAIRED IAW REO 601R-53-61-5137. - [SDR ASOA2014020409843](https://openairdocs.org/sdr/ASOA2014020409843.md): Bulkhead · damaged · Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > FS 621 BULKHEAD AT RBL 27.5 DAMAGED. REPAIRED IAW REO 601R-53-61-5137. - [SDR ASOA2014020409842](https://openairdocs.org/sdr/ASOA2014020409842.md): Bulkhead · damaged · Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > BS 621 BULKHEAD AT RBL 9.5 DAMAGED. REPAIRED IAW REO 601R-53-61-5137. - [SDR ASOA2014020409841](https://openairdocs.org/sdr/ASOA2014020409841.md): Bulkhead · damaged · Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > BS 621, BULKHEAD AT LBL 9.5 DAMAGED. REPAIRED IAW REO 601R-53-61-5137. - [SDR ASOA2014020409840](https://openairdocs.org/sdr/ASOA2014020409840.md): Bulkhead · damaged · Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > BS 621 BULKHEAD AT LBL 18.0 DAMAGED. REPAIRED IAW REO 601R-53-61-5137. - [SDR ASOA2014020409839](https://openairdocs.org/sdr/ASOA2014020409839.md): Bulkhead · cracked · Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > BS 621 BULKHEAD HAS A.6 INCH CRACK IN THE WEB AT RBL 18, WL 131.2. REPAIRED IAW REO 601R-53-61-5137. - [SDR ASOA2014020409838](https://openairdocs.org/sdr/ASOA2014020409838.md): Web · cracked · Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > BS 621 BULKHEAD HAS THREE CRACKS IN THE WEB. REPAIRED IAW REO 601R-53-61-5137. - [SDR ASOA2014020409837](https://openairdocs.org/sdr/ASOA2014020409837.md): Bulkhead · cracked · Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > BS 621 BULKHEAD HAS A.5 INCH CRACK IN THE WEB AT LBL 27.5, WL 97.9. REPAIRED IAW REO 601R-53-61-5137. - [SDR ASOA2014020409836](https://openairdocs.org/sdr/ASOA2014020409836.md): Bulkhead · cracked · Jan 3, 2014 · N827AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > BS 621 BULKHEAD HAS A.5 INCH CRACK IN THE WEB AT LBL 36.2, WL 79.5. REPAIRED IAW REO 601R-53-61-5137. - [SDR ASOA2014020409835](https://openairdocs.org/sdr/ASOA2014020409835.md): Light · no test · Jan 3, 2014 · N827AS · Cndair CL6002B19 · Emergency Lighting > THE ACFT FAILED FUNCTIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM. REPAIRED IAW AMM 33-21-07-000-801 AND AMM 33-21-07-400-801. Next page: https://openairdocs.org/deregistered/N827AS-2015-04-06/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N827AS-2015-04-06/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.