# Service difficulty reports: N860AS, cancelled Mar 6, 2023

A list on [N860AS, cancelled Mar 6, 2023](https://openairdocs.org/deregistered/N860AS-2023-03-06.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 · 191 reports

- [SDR ASOA201811081511](https://openairdocs.org/sdr/ASOA201811081511.md): Skin · mechanic error · Oct 31, 2018 · N860AS · Cndair CL6002B19 · Standard Practices/Structures
  > REF BOMBARDIER TUCSON AIR CENTER JOB# 2743351 DURING JACKING OF AIRCRAFT NOSE JACK PAD SLIPPED, DENTING FUSELAGE SKIN AT APPROX. FS 280.00, BL0. C/A REPAIRED PER BOMBARDIER REO 601R-53-11-3320 REV -- DATED 2018-10-29
- [SDR ASOA201810255289](https://openairdocs.org/sdr/ASOA201810255289.md): Skin · gouged · Oct 25, 2018 · N860AS · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBOARD FLAP UPPER SKIN GOUGED. REPAIRED PER REO 601R87-52-2266 REV- DATED 2018-10-23.
- [SDR ASOA201810245286](https://openairdocs.org/sdr/ASOA201810245286.md): Bushing · corroded · Oct 24, 2018 · N860AS · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STABILIZER BUSHING SHOW EVIDENCE OF CORROSION. COMPLIED WITH EC/TC EO600-55-13 C/W AND SB 601R-55-007 REV D DATED 03/25/2011.
- [SDR ASOA2018101925265](https://openairdocs.org/sdr/ASOA2018101925265.md): Doubler · dented · Oct 12, 2018 · N860AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > REF JOB 2743351 FWD EDGE OF PAX DOOR CUT OUT, FS 310.00 IS DENTED. REPAIRED PER REO 601R-53-21-3026 REV - DATED 2018-10-05.
- [SDR ASOA2018100945245](https://openairdocs.org/sdr/ASOA2018100945245.md): Skin · cracked · Oct 4, 2018 · N860AS · Cndair CL6002B19 · Wing, Plate/Skin
  > REF JOB 2743351 LT TRUNNION LOWER WING PLANK HAS 5 CRACKED HOLES. REPAIRED PER REO 601R-57-21-2665 REV -- DATED 2018-09-26.
- [SDR ASOA2018100935244](https://openairdocs.org/sdr/ASOA2018100935244.md): Skin · dented · Oct 3, 2018 · N860AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > REF JOB 2743351 BULDGE ON FUSELAGE SKIN BETWEEN STR 20-21R FWD OF FS 672.20. REPAIRED PER REO 601R-51-00-309 REV A DATED 2017-5-23, AND REO 601R-53-61-6716 REV -- DATED 2018-09-20.
- [SDR ASOA2018100915243](https://openairdocs.org/sdr/ASOA2018100915243.md): Skin · dented · Oct 1, 2018 · N860AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > REF JOB 2743351 DENT ON RT FUSELAGE FS625-640 BETWEEN STR 18-19R. REPAIRED PER EA 30-2018-178 REV --DATED 09/26/2018.
- [SDR ASOA2018100485234](https://openairdocs.org/sdr/ASOA2018100485234.md): Riser · worn · Sep 28, 2018 · N860AS · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > REF JOB 2743351 LT ENGINE AFT PYLON PRODUCTION RISER HAS FRETTING WEAR. C/A REPAIRED IAW REO 601R-71-22-026 AND REO 601R-54-50-036.
- [SDR ASOA201809265285](https://openairdocs.org/sdr/ASOA201809265285.md): Fitting · corroded · Sep 26, 2018 · N860AS · Cndair CL6002B19 · Engine Mount Section
  > RT ENGINE AFT PRODUCTION DUCT FRETTING. REPAIRED PER REO 601R-71-22-026 REV NC DATED 2004-10-05.
- [SDR ASOA2018100465233](https://openairdocs.org/sdr/ASOA2018100465233.md): Door Sill · corroded · Sep 26, 2018 · N860AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REF JOB 2743351 PAX DOOR ENTRY SILL IS CORRODED. C/A REMOVED AND REPLACED SILL IAW AMM 51-42-06.
- [SDR ASOA2018100445232](https://openairdocs.org/sdr/ASOA2018100445232.md): Intercostal · corroded · Sep 24, 2018 · N860AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REF JOB 2743351 INTERCOSTAL CORRODED BETWEEN FS 349.00 AND FS 364.00 STR 26L-27. C/A REMOVED AND REPLACED INTERCOSTAL IAW AMM 51-42-06.
- [SDR ASOA2018100445231](https://openairdocs.org/sdr/ASOA2018100445231.md): Frame · corroded · Sep 24, 2018 · N860AS · Cndair CL6002B19 · Fuselage Main, Frame
  > REF JOB 2743351 OP 138 FRAME CORRODED AT FS 310.00 BETWEEN STR 26L-26R. C/A REMOVED AND REPLACED FRAME IAW AMM 51-42-06,51-42-21.
- [SDR ASOA2016051814903](https://openairdocs.org/sdr/ASOA2016051814903.md): Frame Splice · cracked · May 18, 2016 · N860AS · Cndair CL6002B19 · Fuselage Main, Frame
  > CRACKED FRAME SPLICE AT FRAME BS 409+32 AND STR 6R. RECEIVED AND COMPLIED WITH SNIEO 601R32202 501, REV: B. COMPLIED WITH ECTC SNIEO 601R-32202 501 AND SNIEO 601R32202 501. COMPLIED WITH EC/TC SNIEO 601R32201501 AND SNIEO 601R32201501.
- [SDR ASOA2016051614902](https://openairdocs.org/sdr/ASOA2016051614902.md): Floor Support · corroded · May 16, 2016 · N860AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MULTIPLE SCREW HOLES CORRODED ON FLOORBEAM AT LBL 27 AT CARGO DOOR FS 589-FS 605. DAMAGE IS OUT OF LIMITS IAW GREO 601R-53-00-0005, REV B. FOUND NUMEROUS AREAS ON SECTION OF FLOORBEAM FS 589-605.00 TO BE EXFOILATED AND BEYOND LIMITS IAW REO 601R-53-00-005.
- [SDR ASOA2016051614868](https://openairdocs.org/sdr/ASOA2016051614868.md): Seat Track · corroded · May 16, 2016 · N860AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 9, BS 559 - 559+80 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, & AMM 53-01-11-400-802.
- [SDR ASOA2016051614867](https://openairdocs.org/sdr/ASOA2016051614867.md): Seat Track · corroded · May 16, 2016 · N860AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, RBL 9, BS 559+86 - 559+92 CORRRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11, & AMM 53-01-00-400-02.
- [SDR ASOA2016051614866](https://openairdocs.org/sdr/ASOA2016051614866.md): Cargo Track · corroded · May 16, 2016 · N860AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRODED AT LBL 9. R & R IAW AMM 53-00-49-000-801, & 53-00-49-400-801.
- [SDR ASOA2016051614865](https://openairdocs.org/sdr/ASOA2016051614865.md): Cargo Track · corroded · May 16, 2016 · N860AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRODED AT LBL 9, FWD OF BS 621. R & R THE CARGO TRACK IAW AMM 53-00-49-000-801, & 53-00-49-400-801.
- [SDR ASOA2016051614864](https://openairdocs.org/sdr/ASOA2016051614864.md): Floorbeam · corroded · May 16, 2016 · N860AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > SCREW HOLE CORRODED ON FLOORBEAM RBL 9 AT FS 605.00. COMPLIED WITH ECTC REO 601-53-00-005.
- [SDR ASOA2016051614863](https://openairdocs.org/sdr/ASOA2016051614863.md): Cargo Track · corroded · May 16, 2016 · N860AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > MULTIPLE SCREW HOLES CORRODED ON CARGO TRACK BS 559+80 - 559+112 RBL9. REMOVED CORROSION IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 101. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-01-11.
- [SDR ASOA2016051614862](https://openairdocs.org/sdr/ASOA2016051614862.md): Seat Track · corroded · May 16, 2016 · N860AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRODED RBL 9 BS 559+112 - 574. R & R THE CARGO TRACK IAW AMM 53-00-49-000-801, & 53-00-49-400-801.
- [SDR ASOA2016051614861](https://openairdocs.org/sdr/ASOA2016051614861.md): Cargo Track · corroded · May 16, 2016 · N860AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRODED AT LBL 9, FS 559+80 - 559+96. R & R THE CARGO TRACK IAW AMM 53-00-49-000-801, & 53-00-49-400-801.
- [SDR ASOA2016051614860](https://openairdocs.org/sdr/ASOA2016051614860.md): Cargo Track · corroded · May 16, 2016 · N860AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRODED AT LBL 9, FS 559+112 - 574. R & R THE CARGO TRACK IAW AMM 53-00-49-000-801, & 53-00-49-400-801.
- [SDR ASOA2016051214901](https://openairdocs.org/sdr/ASOA2016051214901.md): Skin · cracked · May 12, 2016 · N860AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT FWD FUSELAGE SKIN CRACKED BELOW AFT TRU DOOR LATCH AT APPROXIMATELY FS 192.00. REMOVED CRACKED DOOR LAND AND INSTALLED NEW SERVICEABLE DOOR LAND ON LT FWD FUSELAGE BELOW TRU DOOR IAW DWG 600-33052 AND SRM 51-42-06-00 AND 51-42-12-00. LOCATED AND DRILLED
- [SDR ASOA2016051114876](https://openairdocs.org/sdr/ASOA2016051114876.md): Skin · dented · May 11, 2016 · N860AS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > LT INBD FLAP LOWER SHIN DENTED AT APPROXIMATELY WS 76.00, 13" T/E OF FLAP. REPAIRED LT INBD FLAP IAW EO EC/TC EO 60057-0483.
- [SDR ASOA2015091913791](https://openairdocs.org/sdr/ASOA2015091913791.md): Light · damaged · Sep 19, 2015 · N860AS · Cndair CL6002B19 · Emergency Lighting
  > FLOOR-LEVEL EMERGENCY FLOODLIGHT AT ENTRANCE AREA DAMAGED. R & R FLOODLIGHT IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2015021312224](https://openairdocs.org/sdr/ASOA2015021312224.md): Lens · missing · Feb 9, 2015 · N860AS · Cndair CL6002B19 · Emergency Lighting
  > EXIT SIGN MISSING AT ROW 7. FOUND EXIT SIGN COVER ON ACFT AND SECURED IAW AMM 33-51-14.
- [SDR ASOA2015021012197](https://openairdocs.org/sdr/ASOA2015021012197.md): Battery Pack · discharged · Feb 6, 2015 · N860AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT LEFT ON TO OUTSIDE FWD FUSELAGE LIGHTS GLOWING FAINTLY, LIGHT WOULD NOT ILLUMINATE WITH SWITCH ON. OPS TEST OF THE EMERGENCY LIGHT IAW AMM 33-51-00, OPS CHECK IS GOOD, ACFT BACK TO SERVICE.
- [SDR ASOA2014062610761](https://openairdocs.org/sdr/ASOA2014062610761.md): Skin · damaged · Jun 22, 2014 · N860AS · Cndair CL6002B19 · Passenger/Crew Doors
  > TWO FASTENERS BACKED OUT OF SKIN ON PAX DOOR. REPAIRED IAW REO 601R-52-11-2236. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3.
- [SDR ASOA2014061810690](https://openairdocs.org/sdr/ASOA2014061810690.md): Skin · dented · Jun 4, 2014 · N860AS · Cndair CL6002B19 · Rudder, Plate/Skin
  > DURING REMOVAL OF RUDDER, FOUND DENT ON LOWER LT SIDE OF RUDDER. FOUND OUT OF LIMITS IAW SRM 55-40-00. MAJOR REPAIR IAW SOP 5702. COMPLIED WITH REO 601R-55-41-105 P1.
- [SDR ASOA2014061810688](https://openairdocs.org/sdr/ASOA2014061810688.md): Skin · corroded · May 22, 2014 · N860AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING LOWER WING PLANK ACCESS HOLE 64B LAND CORRODED. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L. MAJOR REPAIR.
- [SDR ASOA2014061810687](https://openairdocs.org/sdr/ASOA2014061810687.md): Skin · corroded · May 22, 2014 · N860AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING LOWER WING PLANK ACCESS HOLE FUEL PANEL 650EB LAND CORRODED. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L. MAJOR REPAIR.
- [SDR ASOA2014060610654](https://openairdocs.org/sdr/ASOA2014060610654.md): Fitting · corroded · May 22, 2014 · N860AS · Cndair CL6002B19 · Fuselage Main, Structure
  > THE LOWER SERVICE DOOR SEAL FITTING AT FS 329.00 IS CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00-01, FIG 101, SHEET 1 (TR 53-27). LOCATED & DRILLED NEW SERVICE DOOR SEAL FITTING IAW SRM 51-40-11 & DWC 601R38533. INSTALLED NEW SERVICE
- [SDR ASOA2014061810686](https://openairdocs.org/sdr/ASOA2014061810686.md): Fitting · damaged · May 21, 2014 · N860AS · Cndair CL6002B19 · Vertical Stabilizer
  > DAMAGE TO LOWER RT FITTING ON VERTICAL STAB FRONT SPAR. REMOVED DAMAGED LOWER RT FITTING IAW SRM 51-92-21. INSTALLED NEW SERVICEABLE LOWER RT FITTING IAW SRM 51-42-21. MAJOR REPAIR.
- [SDR ASOA2014061810685](https://openairdocs.org/sdr/ASOA2014061810685.md): Fitting · damaged · May 21, 2014 · N860AS · Cndair CL6002B19 · Vertical Stabilizer
  > DAMAGE TO LOWER LT FITTING ON VERTICAL STAB FRONT SPAR. REMOVED DAMAGED LOWER LT FITTING IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE LT LOWER FITTING IAW SRM 51-42-21. MAJOR REPAIR.
- [SDR ASOA2014061810684](https://openairdocs.org/sdr/ASOA2014061810684.md): Bearing · worn · May 21, 2014 · N860AS · Cndair CL6002B19 · Rudder Structure
  > RUDDER CENTER ATTACHMENT UPPER BEARING HAS EXCESSIVE PLAY. COMPLIED WITH EC/TC RIL 0602. MAJOR REPAIR.
- [SDR ASOA2014060610653](https://openairdocs.org/sdr/ASOA2014060610653.md): Support Angle · corroded · May 21, 2014 · N860AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT SIDE WINDSCREEN SUPPORT ANGLE IS CORRODED. R & R RT SIDE WINDSCREEN SUPPORT ANGLE AND CAP IAW SRM 51-42-21 AND 51-42-06.
- [SDR ASOA2014060610652](https://openairdocs.org/sdr/ASOA2014060610652.md): Angle · cracked · May 21, 2014 · N860AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED ON RT SIDE OF REAR PRESSURE BULKHEAD AFT FACE FS 625.00. R & R ANGLE IAW SRM 51-42-20.
- [SDR ASOA2014060610651](https://openairdocs.org/sdr/ASOA2014060610651.md): Angle · cracked · May 21, 2014 · N860AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED ON LT SIDE OF REAR PRESSURE BULKHEAD AFT FACE BS 625. R & R CRACKED ANGLE IAW SRM 51-42-28.
- [SDR ASOA2014061910692](https://openairdocs.org/sdr/ASOA2014061910692.md): Hinge · gouged · May 20, 2014 · N860AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE HALF ON FUSELAGE IS GOUGED. BLENDED GOUGES IAW SRM 51-12-00.
- [SDR ASOA2014061810683](https://openairdocs.org/sdr/ASOA2014061810683.md): Frame · corroded · May 20, 2014 · N860AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 349 FRAME AT SERVICE DOOR CORRODED. BLENDED CORROSION IAW SRM 51-21-06. MAJOR REPAIR.
- [SDR ASOA2014061810682](https://openairdocs.org/sdr/ASOA2014061810682.md): Bulkhead · chafed · May 20, 2014 · N860AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > TWO CHAFE SPOTS ON AFT SIDE OF BS 280 BULKHEAD APPROXIMATELY 24 INCHES ABOVE FLOOR RT SIDE. BLENDED CHAFE SPOTS IAW SRM 51-12-00 AND 53-00-31. MAJOR REPAIR.
- [SDR ASOA2014061810681](https://openairdocs.org/sdr/ASOA2014061810681.md): Skin · chafed · May 20, 2014 · N860AS · Cndair CL6002B19 · Ailerons
  > LT AILERON UPPER L/E CHAFED. BLENDED AREAS IAW SRM 57-60-00. BLENDED AREA OUT OF LIMITS IN PAD UP AREA AT INBD IAW SRM 51-60-00. COMPLIED WITH EC/TC 601R-57-60-013 IAW REO 601R-57-60-013, REV A.
- [SDR ASOA2014061810680](https://openairdocs.org/sdr/ASOA2014061810680.md): Frame · cracked · May 20, 2014 · N860AS · Cndair CL6002B19 · Passenger/Crew Doors
  > FRAME CRACKED IN PAX DOOR AT BS 338.00. COMPLIED WITH ECTC REO 601R-52-11-402 AND GREO 601R-52-11-402. MAJOR REPAIR.
- [SDR ASOA2014061810679](https://openairdocs.org/sdr/ASOA2014061810679.md): Hinge · gouged · May 20, 2014 · N860AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE ON DOOR SIDE GOUGED. BLENDED GOUGES IAW SRM 51-12-00.
- [SDR ASOA2014061710676](https://openairdocs.org/sdr/ASOA2014061710676.md): Floor Support · corroded · May 20, 2014 · N860AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT AFT OF SERVICE DOOR. REPAIRED IAW REO601R-53-21-2539 AND REO 601R-53-21-2544. MAJOR REPAIR.
- [SDR ASOA2014060610650](https://openairdocs.org/sdr/ASOA2014060610650.md): Angle · cracked · May 20, 2014 · N860AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 ANGLE CRACKED AT LBL 9.00. REMOVED CRACKED ANGLE IAW SRM 52-42-20. FABRICATED NEW REPAIR ANGLE IAW REO 601R-53-11-926.
- [SDR ASOA2014060610649](https://openairdocs.org/sdr/ASOA2014060610649.md): Angle · cracked · May 20, 2014 · N860AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280, ANGLE CRACKED AT RBL 9.00. REMOVED CRACKED ANGLE IAW SRM 52-42-20. FABRICATED NEW REPAIR ANGLE IAW REO 601R-53-11-926. COMPLIED WITH EC/TC REO 601R-53-11-926-01 AND COMPLIED WITH EC/TC REO 601R-53-11-926 01.
- [SDR ASOA2014060610648](https://openairdocs.org/sdr/ASOA2014060610648.md): Fairing · damaged · May 20, 2014 · N860AS · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LT WING FLAP CANOE FAIRING 586AB HAS COMPOSITE DAMAGE ON L/E. REPAIRED PANEL 586AB IAW SRM 51-74-00.
- [SDR ASOA2014061810691](https://openairdocs.org/sdr/ASOA2014061810691.md): Cover · missing · May 19, 2014 · N860AS · Cndair CL6002B19 · Rudder Structure
  > LIGHTNING HOLE MISSING COVER ON RUDDER IAW REO 601R-55-41-018. REPAIRED IAW REO 601R-55-41-018. MAJOR REPAIR.

Next page: https://openairdocs.org/deregistered/N860AS-2023-03-06/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 = 'N860AS' AND deregistration_id = 'N860AS-2023-03-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N860AS-2023-03-06/reports

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