# Service difficulty reports: N867AS, cancelled Apr 2, 2020 A list on [N867AS, cancelled Apr 2, 2020](https://openairdocs.org/deregistered/N867AS-2020-04-02.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 · 172 reports - [SDR ASOA201901085011](https://openairdocs.org/sdr/ASOA201901085011.md): Door Sill · damaged · Jan 8, 2019 · N867AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > REF JOB# 2746370 EXISTING UNTREATED BLENDED AREA ON LT PRESSURE FLOOR SILL ANGLE DOUBLER AT FS 422. C/A REPAIRED IN ACCORDANCE WITH REO 601R-53-41-666 REV. C DATED 2012-11-06. - [SDR ASOA201901085010](https://openairdocs.org/sdr/ASOA201901085010.md): Door Sill · damaged · Jan 8, 2019 · N867AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > REF JOB# 2746370 EXISTING UNTREATED BLENDED AREA ON LT PRESSURE FLOOR SILL AT FS 413. C/A REPAIRED IN ACCORDANCE WITH REO 601R-53-41-666 REV. C DATED 2012-11-06. - [SDR ASOA201901085009](https://openairdocs.org/sdr/ASOA201901085009.md): Door Sill · damaged · Jan 8, 2019 · N867AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > REF JOB# 2746370 EXISTING UNTREATED BLENDED AREA ON RT PRESSURE FLOOR SILL AT FS 413. C/A REPAIRED IN ACCORDANCE WITH REO 601R-53-41-666 REV. C DATED 2012-11-06. - [SDR ASOA201901075003](https://openairdocs.org/sdr/ASOA201901075003.md): Door Sill · corroded · Jan 7, 2019 · N867AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > REF JOB 2746370 LT OUTBOARD FLOOR SILL HAS CORROSION AFT OF FRAME 559.00. REPAIRED IN ACCORDANCE WITH SRM REO 601R-53-00-526 REV --DATED 22 MAY 2013 AND EA 32-2018-238 DATED 11/30/2018. - [SDR ASOA201901075002](https://openairdocs.org/sdr/ASOA201901075002.md): Skin · damaged · Jan 7, 2019 · N867AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin > REF JOB 2746370 NICKS AND DENT DAMAGE ON FUSELAGE SKIN BETWEEN FS574.00-605.00 BETWEEN STR 21R-26R. REPAIRED IN ACCORDANCE WITH REO 601R-53-61-6744 REV --DATED 2016-11-02(TEMPORY REPAIR). - [SDR ASOA2018121305336](https://openairdocs.org/sdr/ASOA2018121305336.md): Skin · dented · Nov 20, 2018 · N867AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin > REF BOMBARDIER TUCSON AIR CENTER JOB# 2746375 DENT ON LH FUSELAGE SKIN AFT OF PITOT PROBE. REPAIRED IAW WITH STS EA 30-2018-224 DATED 11/01/2018. - [SDR ASOA201812135335](https://openairdocs.org/sdr/ASOA201812135335.md): Skin · dented · Nov 20, 2018 · N867AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin > REF BOMBARDIER TUCSON AIR CENTER JOB# 2746375 5 DENTS ON LH FUSELAGE SKIN BETWEEN FS 364.00 AND 394.00, 14L-17L. REPAIRED IAW STS EA 48-2018-074 DATED 11/02/2018. - [SDR ASOA201812135334](https://openairdocs.org/sdr/ASOA201812135334.md): Skin · dented · Nov 20, 2018 · N867AS · Cndair CL6002B19 · Spoilers > REF BOMBARDIER TUCSON AIR CENTER JOB# 2746375 DENT ON TOP OUTBOARD SURFACE OF RH FLIGHT SPOILER. REPAIRED IAW EA 32-2018-222 DATED 11/05/2018. - [SDR ASOA2018113025317](https://openairdocs.org/sdr/ASOA2018113025317.md): Skin · damaged · Nov 2, 2018 · N867AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin > FOUND A BLEND OUT AREA ON LH FUSELAGE SKIN FWD OF FS 349.00 BETWEEN STA 18L-19L. REPAIRED PER STS EA 30-2018-227 REV -- DATED 10/25/2018 - [SDR ASOA201706181696](https://openairdocs.org/sdr/ASOA201706181696.md): Flap · damaged · Jun 18, 2017 · N867AS · Cndair CL6002B19 · Trailing Edge Flaps > LEFT WING INBOARD FLAP DAMAGED ON T/E. REPLACED LEFT INBOARD FLAP ASSY IAW AMM 27-54-01-400-801. - [SDR ASOA20161203239](https://openairdocs.org/sdr/ASOA20161203239.md): Door Sill · corroded · Dec 3, 2016 · N867AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CORROSION DAMAGE FOUND ALONG LT FLOOR SILL BETWEEN FS409.00+128-559.00. BLEND DAMAGE LT FLOOR SILL BETWEEN FS409.00+128-559.00 IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF SILL IAW BSC NDTM.43 MIN REMAINING THK OF PANEL/ANGLE PAD-UP IS.012"/.078"/. - [SDR ASOA20161203238](https://openairdocs.org/sdr/ASOA20161203238.md): Door Sill · corroded · Dec 3, 2016 · N867AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CORROSION DAMAGE FOUND ALONG RT FLOOR SILL BETWEEN FS409.00+128-559.00. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION OF SILL IAW BSC NDTM.43 MIN REMAINING THK OF PANEL/ANGLE PAD-UP IS.020"/.043". ORIGINAL IS.055"/.080". REMOVED IS.0 - [SDR ASOA201611281276](https://openairdocs.org/sdr/ASOA201611281276.md): Crossbeam · cracked · Nov 28, 2016 · N867AS · Cndair CL6002B19 · Fuselage Main, Structure > DURING C CHECK, FOUND CROSSBEAM AT BS 484 BETWEEN LBL 27 & THE LT FLOOR SILL HAS TWO CRACKED ANGLES. REMOVED PREVIOUSLY INSTALLED REPAIR ANGLES. FABRICATED NEW REPAIR ANGLES. PERFORMED NDT. NO DEFECTS NOTED AT THIS TIME. DRILLED UP AND INSTALLED NEW ANGLES PER - [SDR ASOA20161119218](https://openairdocs.org/sdr/ASOA20161119218.md): Seat Track · corroded · Nov 19, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT SIDE SEAT TRACK BETWEEN BS 364 TO 409 HAS CORROSION. REMOVED AND INSTALLED A NEW FABRICATED SEAT TRACK IAW REO 601R-53-00-651 REV 0, EC/TC REO 601R-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801. - [SDR ASOA201611181275](https://openairdocs.org/sdr/ASOA201611181275.md): Seat Track · corroded · Nov 18, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > DURING C CHECK, FOUND THE SEAT TRACK AT BS 559+80 TO 559+96, LBL 27 CORRODED. REMOVED, FABRICATED, AND INSTALLED A NEW SEAT TRACK IAW REO 601R-53-00-485, EC/TC REO 601R-53-00-485, AND AMM 53-00-49-000-801/53-00-49-400-801. - [SDR ASOA201611181274](https://openairdocs.org/sdr/ASOA201611181274.md): Seat Track · corroded · Nov 18, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > DURING C CHECK, FOUND THE SEAT TRACK AT BS 559+80 TO 559+96, RBL27 CORRODED. REMOVED, FABRICATED, AND INSTALLED A NEW SEAT TRACK IAW REO 601R-53-00-485, EC/TC REO 601R-53-00-485, AND AMM 53-00-49-000-801/53-00-49-400-801. - [SDR ASOA201611181273](https://openairdocs.org/sdr/ASOA201611181273.md): Seat Track · corroded · Nov 18, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > DURING C CHECK, FOUND THE SEAT TRACK AT BS 559+80 TO 559+96, LBL9 CORRODED. REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK IAW REO 601R-53-00-485, EC/TC REO 601R-53-00-485, & AMM 53-00-49-000-801/53-00-49-400-801. - [SDR ASOA20161118217](https://openairdocs.org/sdr/ASOA20161118217.md): Seat Track · corroded · Nov 18, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT SIDE SEAT TRACK BETWEEN BS 544 TO 559+80 HAS CORROSION. REMOVED AND INSTALLED A NEW FABRICATED SEAT TRACK IAW REO 601R-53-00-651 REV 0, EC/TC REO 601R-53-00-651, AMM 53-01-11-000-802 AND 53-01-11-400-801. - [SDR ASOA20161118216](https://openairdocs.org/sdr/ASOA20161118216.md): Seat Track · corroded · Nov 18, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RT SIDE SEAT TRACK BETWEEN BS 409+112 TO 449.85 HAS CORROSION. REMOVED AND INSTALLED A NEW FABRICATED SEAT TRACK IAW REO 601R-53-00-651 REV 0, EC/TC REO 601R-53-00-651, AMM 53-01-11-000-802 AND 53-01-11-400-801. - [SDR ASOA20161118215](https://openairdocs.org/sdr/ASOA20161118215.md): Seat Track · corroded · Nov 18, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT SIDE SEAT TRACK BETWEEN BS 409+112 TO 449.85 HAS CORROSION. REMOVED AND INSTALLED A NEW FABRICATED SEAT TRACK IAW REO 601R-53-00-651 REV 0, EC/TC REO 601R-53-00-651, AMM 53-01-11-000-802 AND 53-01-11-400-801. - [SDR ASOA20161118214](https://openairdocs.org/sdr/ASOA20161118214.md): Seat Track · corroded · Nov 18, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > SHORT SEAT TRACK BS 559+96 TO 559+112, LBL 9 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485, EC/TC REO 601R-53-00-485, AMM 53-00-49-000-801 AND 53-00-49-400-801. - [SDR ASOA201611151272](https://openairdocs.org/sdr/ASOA201611151272.md): Floorbeam · cracked · Nov 15, 2016 · N867AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > DURING C CHECK, FOUND THE FLOORBEAM BS 461 BETWEEN LBL 9 AND LBL 18 CRACKED. CUT AWAY DAMAGE AND INSTALLED SECONDARY STRUCTURE & DOUBLER IAW EC/TC REO 601R-53-41-2128 REV A. - [SDR ASOA20161114229](https://openairdocs.org/sdr/ASOA20161114229.md): Seat Track · corroded · Nov 14, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 6017-53-00-651 REV 0, EC/TC REO 6017-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801. - [SDR ASOA20161114228](https://openairdocs.org/sdr/ASOA20161114228.md): Seat Track · corroded · Nov 14, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 6017-53-00-651 REV 0, EC/TC REO 6017-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801. - [SDR ASOA20161114227](https://openairdocs.org/sdr/ASOA20161114227.md): Seat Track · corroded · Nov 14, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 6017-53-00-651 REV 0, EC/TC REO 6017-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801. - [SDR ASOA20161114226](https://openairdocs.org/sdr/ASOA20161114226.md): Seat Track · corroded · Nov 14, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 6017-53-00-651 REV 0, EC/TC REO 6017-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801. - [SDR ASOA20161114225A](https://openairdocs.org/sdr/ASOA20161114225A.md): Seat Track · corroded · Nov 14, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT SIDE SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 6017-53-00-651 REV 0, EC/TC REO 6017-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801. - [SDR ASOA20161114224A](https://openairdocs.org/sdr/ASOA20161114224A.md): Seat Track · corroded · Nov 14, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LEFT SIDE SEAT TRACK HAS CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW REO 6017-53-00-651 REV 0, EC/TC REO 6017-53-00-651, AMM 53-01-11-000-802, AND 53-01-11-400-801. - [SDR ASOA20161114213](https://openairdocs.org/sdr/ASOA20161114213.md): Seat Track · corroded · Nov 14, 2016 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RIGHT SIDE SEAT TRACK BETWEEN BS 409 TO 449.96 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-651 REV 0, ECTC REO 601R-53-00-651, AMM 53-01-000-802, AND 53-01-11-400-801. - [SDR ASOA201611131271](https://openairdocs.org/sdr/ASOA201611131271.md): Riser · cracked · Nov 13, 2016 · N867AS · Cndair CL6002B19 · Passenger/Crew Doors > DURING C CHECK, FOUND PAX DOOR AFT GAS STRUT TOP ATTACH STRUCTURE LOOSE AND CRACKED ON STRIP SKIN. TRIMMED ALL DAMAGE FOUND AND INSTALLED SECONDARY STRUCTURE/DOUBLERS PER EC/TC REO 601R52-11-2367 REV 0,EC/TC REO 601R52-11-2366 REV 0, AND EC/TC REO 601R52-11-70 - [SDR ASOA2016072315133](https://openairdocs.org/sdr/ASOA2016072315133.md): Battery Pack · discharged · Jul 23, 2016 · N867AS · Cndair CL6002B19 · Emergency Equipment > FA FLASHLIGHT INOPERATIVE. REPLACED THE BATTERIES AND OPS CHECKED GOOD IAW AMM 25-61-04. ACFT OK FOR SERVICE. - [SDR ASOA2015052912946](https://openairdocs.org/sdr/ASOA2015052912946.md): Lamp · burned out · May 27, 2015 · N867AS · Cndair CL6002B19 · Emergency Lighting > NR 6 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD. - [SDR ASOA2015040712542](https://openairdocs.org/sdr/ASOA2015040712542.md): Lamp · burned out · Apr 3, 2015 · N867AS · Cndair CL6002B19 · Emergency Lighting > EXTERNAL EMERGENCY LIGHT NR 6 INOPERATIVE. RE-LAMPED IAW AMM 33-51-21. SYS OPS CHECKED GOOD. NO FURTHER ACTION. - [SDR ASOA2014103011585](https://openairdocs.org/sdr/ASOA2014103011585.md): Access Panel · corroded · Oct 12, 2014 · N867AS · Cndair CL6002B19 · Wing, Plate/Skin > LT WING LOWER WING PLANK ACCESS HOLE LAND AT FUEL PANEL 540DB CORRODED /PITTED THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED AND COMPLIED WITH GREO 601R-57-21-030. COMPLIED WITH REO 601R-57-21-030 REV L. DATED FEB.5,2014. - [SDR ASOA2014103011584](https://openairdocs.org/sdr/ASOA2014103011584.md): Access Panel · corroded · Oct 12, 2014 · N867AS · Cndair CL6002B19 · Wing, Plate/Skin > LT WING LOWER WING PLANK ACCESS HOLE LAND AT FUEL PANEL 510AB CORRODED /PITTED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED AND COMPLIED WITH GREO 601R-57-21-030. COMPLIED WITH REO 601R-57-21-030, REV C, DATED FEB 5, 2014. - [SDR ASOA2014103011586](https://openairdocs.org/sdr/ASOA2014103011586.md): Floorbeam · corroded · Oct 9, 2014 · N867AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > FS 280, WEB CORRODED AT FLOOR SUPPORT FWD ANGLE BETWEEN LBL9 AND RBL9. COMPLIED WITH ECTC 601R-53-11-926 01 FABRCATED REPAIR PARTS. REMOVED LT AND RT, 4 ATTACH CLIPS AT FS280 -3 WEB FILLER, -5 REPAIR ANGLE, AND -13-5 SHIM, AILERON PULLEY BRACKETS REMOVED WOR - [SDR ASOA2014103011583](https://openairdocs.org/sdr/ASOA2014103011583.md): Angle · corroded · Oct 6, 2014 · N867AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > PAX DOOR LOWER SILL UPPER ANGLE CORRODED AT FS 320.00 AND FS345.00. REPAIRED IAW SRM 51-42-20-00 & DWG 601R-31527. BLENDED CORRODED AREA IAW SRM 51-12-00-00. AFTER FURTHER INVESTIGATION ANGLE REQUIRES REPLACEMENT BECAUSE ITS MORE THAN 30 PERCENT OF LENGTH, - [SDR ASOA2014103011582](https://openairdocs.org/sdr/ASOA2014103011582.md): Bulkhead · gouged · Oct 6, 2014 · N867AS · Cndair CL6002B19 · Fuselage Main, Bulkhead > F/S 621 AFT PRESSURE BULKHEAD HAS 2 NICKS BETWEEN LBL 18 - LBL 27. REMOVED DAMAGE IAW SRM 51-12-00-00. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH REO 601R-53-61-2155, REV A DATED AUG 13,2013. COMPLIED WITH EC/TC REO 601R-53-61- - [SDR ASOA2014103011581](https://openairdocs.org/sdr/ASOA2014103011581.md): Drag Angle · cracked · Oct 6, 2014 · N867AS · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR AFT DRAG ANGLE CRACKED AT MOTOR ASSIST WHEEL PULLEY AREA. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REPAIRED IAW REO 601R-57-11-513, REV A DATED MAR 5, 2009 DWG 601R-31702. COMPLIED WITH EC/TC REO 601R-52-11-513. - [SDR ASOA2014102911570](https://openairdocs.org/sdr/ASOA2014102911570.md): Skin · corroded · Oct 6, 2014 · N867AS · Cndair CL6002B19 · Service Doors > SERVICE DOOR LOWER INNER SKIN HAS CORROSION SEVERAL PLACES. BLENDED CORROSION IAW SRM 51-12-00-00. - [SDR ASOA2014102911569](https://openairdocs.org/sdr/ASOA2014102911569.md): Hinge · gouged · Oct 6, 2014 · N867AS · Cndair CL6002B19 · Fuselage, Door Hinge > PAX DOOR HINGE LUGS ARE GOUGED. REPAIRED IAW REO 601R-52-11-1347. - [SDR ASOA2014103011580](https://openairdocs.org/sdr/ASOA2014103011580.md): Frame · corroded · Oct 4, 2014 · N867AS · Cndair CL6002B19 · Fuselage Main, Frame > CORROSION AT LOWER FRAME SECTION OF BS 319.7 BETWEEN STR26-27L. REMOVED THE CORROSION IAW SRM 51-21-06. REPAIRED IAW EA 32-2014-143. - [SDR ASOA2014103011579](https://openairdocs.org/sdr/ASOA2014103011579.md): Floorbeam · corroded · Oct 4, 2014 · N867AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > AFT FLT DECK SUPPORT ANGLE AT BS 280 IS CORRODED. REMOVED COCKPIT FLOORBEAM ANGLE. INSTALLED NEW COCKPIT FLOORBEAM ANGLE IAW SRM 51-42-06. L - [SDR ASOA2014102911568](https://openairdocs.org/sdr/ASOA2014102911568.md): Seat Track · corroded · Oct 4, 2014 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CORRODED SEAT TRACK BS 394, RBL 9 BEYOND LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW 53-01-11-000-802 AND AMM 53-01-11-400-802. - [SDR ASOA2014102911567](https://openairdocs.org/sdr/ASOA2014102911567.md): Seat Track · corroded · Oct 4, 2014 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CORRODED SEAT TRACK BS 364, RBL 9 BEYOND LIMITS. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802. - [SDR ASOA2014102911566](https://openairdocs.org/sdr/ASOA2014102911566.md): Seat Track · corroded · Oct 4, 2014 · N867AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CORRODED SEAT TRACK BS 394, LBL 9 BEYOND LIMITS. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802. - [SDR ASOA2014103011578](https://openairdocs.org/sdr/ASOA2014103011578.md): Door Sill · corroded · Oct 3, 2014 · N867AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FOUND SERVICE DOOR SILL TO HAVE MULTIPLE CORROSION ALONG SILL. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED CORRODED SERVICE DOOR SILL IAW SRM 51-42-21, INSTALLED NEW SERVICEABLE DOOR SILL, LWR UPPER ANGLE IAW DWG 601R-38303 & SRM 51-42- - [SDR ASOA2014103011577](https://openairdocs.org/sdr/ASOA2014103011577.md): Structure · corroded · Oct 3, 2014 · N867AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CORROSION FOUND ALONG NUTPLATE HOLES OF RT SILL, RBL 42.90, BS 559 - 559+48. R & R RECEPTICLE L/W OTBD FLAP 2ND FROM OTBD PANEL OTBD POSIITON IAW SRM 51-44-11. - [SDR ASOA2014103011576](https://openairdocs.org/sdr/ASOA2014103011576.md): Strap · corroded · Oct 3, 2014 · N867AS · Cndair CL6002B19 · Fuselage Main, Floor Beam > FOUND FLOORBEAM CAP CORRODED SEVERELY AT BS 557 BETWEEN BL 27 AND BL 42.9. REMOVED CORRODED STRAP AND INSTALLED NEW STRAP IAW SRM 51-42-06 AND DWG 601R31025. - [SDR ASOA2014102911565](https://openairdocs.org/sdr/ASOA2014102911565.md): Floor Support · corroded · Oct 3, 2014 · N867AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FLOOR SUPPORT CORRODED BS 574- 621. REPAIRED IAW REO 601R-53-00-526. Next page: https://openairdocs.org/deregistered/N867AS-2020-04-02/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 = 'N867AS' AND deregistration_id = 'N867AS-2020-04-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N867AS-2020-04-02/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.