# Service difficulty reports: N850AS, cancelled Jul 30, 2018

A list on [N850AS, cancelled Jul 30, 2018](https://openairdocs.org/deregistered/N850AS-2018-07-30.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 · 178 reports

- [SDR ASOA2015111714064](https://openairdocs.org/sdr/ASOA2015111714064.md): Lamp · burned out · Nov 17, 2015 · N850AS · Cndair CL6002B19 · Emergency Lighting
  > EXTERNAL EMERGENCY LIGHT, NR 2 INOPERATIVE. RE-LAMPED IAW AMM 33-51-21. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2015092513833](https://openairdocs.org/sdr/ASOA2015092513833.md): Bracket · unserviceable · Sep 25, 2015 · N850AS · Cndair CL6002B19 · Nose/Tail Landing Gear
  > NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. GEAR DISAGREE MSG AND NOSE DOOR MSG DISPLATED GEAR HANDLE PULLED AND STOWED. ACFT RETURNED TO DEPARTURE. R & R NLG LENTER BRACKET IAW CMM 32-20-04, OPS CHECK IAW AMM 32-30-00. OPS CHECK GOOD.
- [SDR ASOA2015073013530](https://openairdocs.org/sdr/ASOA2015073013530.md): Seat Track · corroded · Jul 30, 2015 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK HAS CORROSION AT BS 409+16 TO 409+112. CORROSION EXCEEDS THE LIMITS OF SRM 53-21-49, FIG 101. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.
- [SDR ASOA2015072513528](https://openairdocs.org/sdr/ASOA2015072513528.md): Seat Track · corroded · Jul 25, 2015 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BS 544 - 559+112 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-00. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-40-11, AND AMM 53-01-11-400-802.
- [SDR ASOA2015072513527](https://openairdocs.org/sdr/ASOA2015072513527.md): Seat Track · corroded · Jul 25, 2015 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BS 544 - 559+112 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.
- [SDR ASOA2015072513526](https://openairdocs.org/sdr/ASOA2015072513526.md): Seat Track · corroded · Jul 25, 2015 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BS 450 - 499 CORRODED. CORROSION FOUND OUT OF LIMITS IAW SRM 53-21-49-00, FIG 101. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.
- [SDR ASOA2015072513525](https://openairdocs.org/sdr/ASOA2015072513525.md): Seat Track · corroded · Jul 25, 2015 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BS 409+128 - 559 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-00. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 & GREO 601R 53-00-485 AND GREO 601R-53-00-485, REV A.
- [SDR ASOA2015072513524](https://openairdocs.org/sdr/ASOA2015072513524.md): Seat Track · corroded · Jul 25, 2015 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BS 394 - 409+128 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-40-802.
- [SDR ASOA2015072513523](https://openairdocs.org/sdr/ASOA2015072513523.md): Seat Track · corroded · Jul 25, 2015 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BS 364 - 394 FOUND CORRODED. CORROSION FOUND OUT OF LIMITS OF SRM 53-21-49, FIG 101. R & R THE SEAT TRACK IAW AMM 53-01-11-000-400-802.
- [SDR ASOA2015072513522](https://openairdocs.org/sdr/ASOA2015072513522.md): Seat Track · corroded · Jul 25, 2015 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BS 364-394 LT FOUND CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.
- [SDR ASOA2015072413521](https://openairdocs.org/sdr/ASOA2015072413521.md): Floor Support · corroded · Jul 24, 2015 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND LT SIDE PRESSURE FLOOR SUPPORT AT BS 544. REPAIRED IAW EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2015072413520](https://openairdocs.org/sdr/ASOA2015072413520.md): Floor Support · corroded · Jul 24, 2015 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON LT SIDE PRESSURE FLOOR SUPPORT AT BS 522.4. REPAIRED IAW EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2015072413519](https://openairdocs.org/sdr/ASOA2015072413519.md): Floor Support · corroded · Jul 24, 2015 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND LT SIDE PRESSURE FLOOR SUPPORT AT BS 513. REPAIRED IAW EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2015072413518](https://openairdocs.org/sdr/ASOA2015072413518.md): Floor Support · corroded · Jul 24, 2015 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND RT PRESSURE FLOOR SUPPORT AT BS 513. REPAIRED IAW ECTC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2015072413517](https://openairdocs.org/sdr/ASOA2015072413517.md): Angle · corroded · Jul 24, 2015 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE FOUND CORRODED, RT SIDE BS 449.85 - 473.15. REPAIRED IAW EC/TC REO 601R-53-41-666-01 AND REO 601R-53-41-666, REV C.
- [SDR ASOA2015072313516](https://openairdocs.org/sdr/ASOA2015072313516.md): Floor Support · corroded · Jul 23, 2015 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT BETWEEN BS 310 - 319.7 CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-00. REPLACED THE FLOOR SUPPORT IAW SR 51-42-06-00.
- [SDR ASOA2015072113515](https://openairdocs.org/sdr/ASOA2015072113515.md): Angle · cracked · Jul 21, 2015 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON ANGLE ATTACHED TO AFT PRESSURE BULKHEAD AT BS 625 - 621 ABOVE LOWER TRANSVERSE BEAM STRUCTURE LT SIDE. R & R THE ANGLE IAW SRM 51-42-20.
- [SDR ASOA2015072113514](https://openairdocs.org/sdr/ASOA2015072113514.md): Angle · cracked · Jul 21, 2015 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON ANGLE ATTACHED TO AFT PRESSURE BULKHEAD BS 625 - 621 ABOVE LOWER TRANSVERSE BEAM STRUCTURE RT SIDE. REMOVED CRACKED ANGLE AND INSTALLED IAW SRM 51-42-21-00 AND SRM 51-40-11-00.
- [SDR ASOA2015072113513](https://openairdocs.org/sdr/ASOA2015072113513.md): Skin · dented · Jul 21, 2015 · N850AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT FOUND ON FUSELAGE AT BS 625 - 640 AND STRINGERS 25-26. REPAIRED IAW EA 32-2015-319 SECTION 1.
- [SDR ASOA2015072113512](https://openairdocs.org/sdr/ASOA2015072113512.md): Battery Pack · no test · Jul 21, 2015 · N850AS · Cndair CL6002B19 · Emergency Lighting
  > NR 1 EMERGENCY LIGHT BATTERY PACK FAILED OPS CHECK. R & R THE BATTERY PACK IAW AMM 33-51-04-000-801 & OPS CHECKED GOOD 35-51-04-400-801.
- [SDR ASOA2015072013531](https://openairdocs.org/sdr/ASOA2015072013531.md): Structure · damaged · Jul 20, 2015 · N850AS · Cndair CL6002B19 · Trailing Edge Flaps
  > DURING VISUAL INSPECTION OF RT WING DAMAGE TO RT FLAP OTBD T/E. COMPLIED WITH EC/TC EO 600-57-128 02. REPAIRED DAMAGE IAW SRM 51-42-00, KJ161732 8/9/15 (PB) M/A: 4. REMOVED T/E WEDGE IAW SRM 51-42-06. INSTALLED NEW T/W WEDGE IAW SRM 51-42-06. COMPLIED WIT
- [SDR ASOA2015042212627](https://openairdocs.org/sdr/ASOA2015042212627.md): Sign · inoperative · Apr 18, 2015 · N850AS · Cndair CL6002B19 · Emergency Lighting
  > LIGHTED FLOOR-LEVEL EXIT SIGN AT ENTRANCE BULKHEAD INOPERATIVE. R & R SIGN IAW AMM 33-51-10. SYS OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2015020212137](https://openairdocs.org/sdr/ASOA2015020212137.md): Bulkhead · cracked · Jan 28, 2015 · N850AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED ALONG RBL 27.50 BETWEEN SECOND AND THIRD STAND OFF, FROM FLOOR WL 73.50.
- [SDR ASOA2015020212136](https://openairdocs.org/sdr/ASOA2015020212136.md): Bulkhead · cracked · Jan 28, 2015 · N850AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED ABOVE WL121.93 AND RBL9.50.
- [SDR ASOA2015020212135](https://openairdocs.org/sdr/ASOA2015020212135.md): Bulkhead · cracked · Jan 28, 2015 · N850AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED BELOW WL 120.43 AND LBL 18.00.
- [SDR ASOA2015020212134](https://openairdocs.org/sdr/ASOA2015020212134.md): Angle · cracked · Jan 28, 2015 · N850AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CRACK ANGLE BELOW AFT END OF CARGO DOOR HORIZONTAL SUPPORT AT APPROXIMATELY WL120.43 AND LBL36.2.
- [SDR ASOA2015020212133](https://openairdocs.org/sdr/ASOA2015020212133.md): Bulkhead · cracked · Jan 28, 2015 · N850AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED AT UPPER END OF CARGO DOOR AFT TRACK AND LBL 27.5.
- [SDR ASOA2014110711616](https://openairdocs.org/sdr/ASOA2014110711616.md): Lens · missing · Nov 6, 2014 · N850AS · Cndair CL6002B19 · Emergency Lighting
  > EXIT SIGN LENS IN GALLEY BY SERVICE DOOR MISSING. REPLACED THE EXIT SIGN LENS IAW AMM 33-51-13.
- [SDR ASOA2014091211215](https://openairdocs.org/sdr/ASOA2014091211215.md): Light · inoperative · Sep 10, 2014 · N850AS · Cndair CL6002B19 · Emergency Lighting
  > NR 5 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R NR 5 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2013122009665](https://openairdocs.org/sdr/ASOA2013122009665.md): Lens · detached · Dec 16, 2013 · N850AS · Cndair CL6002B19 · Emergency Lighting
  > LENS DETACHED ON EMERGENCY LIGHT JUST AFT OF SERVICE DOOR. REPLACED LENS IAW CMM 33-51-21.
- [SDR ASOA2013091108985](https://openairdocs.org/sdr/ASOA2013091108985.md): Lens · missing · Sep 7, 2013 · N850AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT NEAR PAX BOARDING DOOR MISSING COVER. REPLACED MISSING EMERGENCY LIGHT COVER IAW AMM 33-51-19. OPS CHECKED GOOD. NO FURHTER DEFECTS NOTED.
- [SDR ASOA2013062103883](https://openairdocs.org/sdr/ASOA2013062103883.md): Connector · broken · Jun 17, 2013 · N850AS · Cndair CL6002B19 · Light System Wiring
  > WIRING FOR GALLEY EMERGENCY EXIT LIGHT ON TRIM PANEL HAS BROKEN CONNECTOR (QUICK DISCONNECT) ON ACFT SIDE. REPLACED EMERGENCY EXIT LIGHT TRIM PANEL CONNECTOR IAW ESPM 20-17-10. NO DISCREPENCIES FOUND AT THIS TIME.
- [SDR ASOA2013062103882](https://openairdocs.org/sdr/ASOA2013062103882.md): Door · corroded · Jun 12, 2013 · N850AS · Cndair CL6002B19 · Service Doors
  > MID CAP DOOR ON SERVICE DOOR CORRODED OUT OF LIMITS. R & R MID CAP ON SERVICE DOOR.
- [SDR ASOA2013062103881](https://openairdocs.org/sdr/ASOA2013062103881.md): Attach Angle · corroded · Jun 10, 2013 · N850AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > ATTACH ANGLE BS 349, RT OTBD CORRODED. R & R ATTACH ANGLE IAW SRM 51-42-06 AND SRM 51-42-21.
- [SDR ASOA2013062103880](https://openairdocs.org/sdr/ASOA2013062103880.md): Floorbeam · corroded · Jun 7, 2013 · N850AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM FS 349 IS CORRODED. REPAIRED FLOORBEAM IAW REO 601R-53-21-2443. NDT PERFORMED. MAJOR REPAIR.
- [SDR ASOA2013062103879](https://openairdocs.org/sdr/ASOA2013062103879.md): Seat Track · corroded · Jun 4, 2013 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK AT BS 559 - 559 + 80 CORRODED. INSTALLED SEAT TRACK IAW AMM 53-01-11, AMM 51-21-11, SRM 51-40-11, SRM 51-41-02, AMM 53-01-11 AND AMM 51-23-00.
- [SDR ASOA2013062103878](https://openairdocs.org/sdr/ASOA2013062103878.md): Seat Track · corroded · Jun 4, 2013 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK AT FS 349 - 409 CORRODED. INSTALLED SEAT TRACK IAW AMM 53-01-11, SRM 51-21-11, SRM 51-41-02, SRM 51-40-11, SRM 51-23-00.
- [SDR ASOA2013062103877](https://openairdocs.org/sdr/ASOA2013062103877.md): Seat Track · corroded · Jun 4, 2013 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK AT FS 349 -409 CORRODED. INSTALLED SEAT TRACK IAW AMM 53-01-11, SRM 51-41-02, SRM 51-40-11, SRM 51-21-11, SRM 51-23-00.
- [SDR ASOA2013062103876](https://openairdocs.org/sdr/ASOA2013062103876.md): Seat Track · corroded · Jun 4, 2013 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK AT FS 409 + 96 - 559 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11, CLEANED AREA IAW SRM 51-26-00.
- [SDR ASOA2013062103875](https://openairdocs.org/sdr/ASOA2013062103875.md): Seat Track · corroded · Jun 4, 2013 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK AT FS 409 + 96 - 559 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11. CLEANED AREA IAW SRM 51-26-00.
- [SDR ASOA2013062103874](https://openairdocs.org/sdr/ASOA2013062103874.md): Seat Track · corroded · Jun 4, 2013 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FLOOR SEAT TRACK AT FS 409 - 409 + 96 CORRODED. BLENDED SEAT TRACK. FOUND OUT OF LIMITS IAW SRM 53-21-49 AND SRM 51-21-06. MATERIAL REMAINING 0.40" MINIMUM MATERIAL 0.50". R & R SEAT TRACK IAW AMM 53-01-11. CLEANED AREA IAW SRM 51-26-00.
- [SDR ASOA2013062103873](https://openairdocs.org/sdr/ASOA2013062103873.md): Seat Track · corroded · Jun 4, 2013 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK AT FS 409 - 409 + 96 CORRODED. R & R SEAT TRACK IAW AMM 53-01-11. CLEANED AREA IAW SRM 51-26-00.
- [SDR ASOA2013062103872](https://openairdocs.org/sdr/ASOA2013062103872.md): Sill · corroded · Jun 3, 2013 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL HAS CORROSION ON FWD AND AFT SIDES. REMOVED FWD AND AFT CLEAT, REMOVED MID BRACKET, REMOVED KICK ANGLE AND MID CAP, DRILLED NEW KICKANGLE AND MID CAP, INSTALLED MID CAP TO NEW KICK ANGLE, INSTALLED ASSEMBLY IAW SRM 51-42-21, 51-42-06,
- [SDR ASOA2013062103871](https://openairdocs.org/sdr/ASOA2013062103871.md): Angle · corroded · Jun 3, 2013 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR THRESHOLD ANGLE CORRODED. R & R THRESHOLD ANGLE IAW SRM 51-42-06, 51-42-26, 51-40-11, 51-42-21, 51-25-16.
- [SDR ASOA2013062103870](https://openairdocs.org/sdr/ASOA2013062103870.md): Seat Track · cracked · May 31, 2013 · N850AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT SIDE SEAT TRACK FWD OF FS 409.0+128 CRACKED. CLEANED DAMAGE AREA, NO DEFECTS NOTED IAW SRM 53-21-49. DIMENSION AFTER REMOVAL OF DAMAGE: 19.31MM SIDE SEAT TRACK FOUND WITHIN LIMITS IAW SRM 53-21-49, 101 LOCATION Q ALODINED AREA IAW SRM 51-21-11.
- [SDR ASOA2013062103869](https://openairdocs.org/sdr/ASOA2013062103869.md): Sill · corroded · May 30, 2013 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT SILL AFT OF SERVICE DOOR HAS CORROSION. R & R RT SILL AFT OF SERVICE DOOR IAW SRM 51-42-06 AND SRM 51-42-10. FOUND OUT OF LIMITS WITH A.010 MAT LOSS IAW SRM TR 53-27-00.
- [SDR ASOA2013062103868](https://openairdocs.org/sdr/ASOA2013062103868.md): Bracket · cracked · May 30, 2013 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 L BRACKET CRACKED RT SIDE. R & R WITH SERVICEABLE PART IAW SRM 51-42-20, SRM 51-42-06, SRM 51-22-00 AND SRM 51-42-20, AMM 51-25-00, AMM 51-25-56.
- [SDR ASOA2013062103867](https://openairdocs.org/sdr/ASOA2013062103867.md): Bracket · cracked · May 30, 2013 · N850AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 280 BRACKET CRACKED LT SIDE. R & R WITH SERVICEABLE PART IAW SRM 51-42-20, SRM 51-42-06, SRM 51-22-00 AND SRM 51-42-20, AMM 51-25-00, AMM 51-25-56.
- [SDR ASOA2013062103866](https://openairdocs.org/sdr/ASOA2013062103866.md): Bulb · burned out · May 23, 2013 · N850AS · Cndair CL6002B19 · Emergency Lighting
  > DURING EMERGENCY LIGHTS OPS TEST, FOUND OVERHEAD EMERGENCY FLOODLIGHT INOPERATIVE AT BS 544. R & R CEILING EMERGENCY LIGHT BULB IAW AMM 33-51-16. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.
- [SDR ASOA2013030503101](https://openairdocs.org/sdr/ASOA2013030503101.md): Isolator · broken · Mar 2, 2013 · N850AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUR ISOLATORS BROKEN ON AFT PRESSURE BULKHEAD. R & R DAMAGED ISOLATORS ON THE AFT PRESSURE BULKHEAD IAW SRM 51-42-13.

Next page: https://openairdocs.org/deregistered/N850AS-2018-07-30/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 = 'N850AS' AND deregistration_id = 'N850AS-2018-07-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N850AS-2018-07-30/reports

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