# Service difficulty reports: N828AS, cancelled Feb 27, 2015

A list on [N828AS, cancelled Feb 27, 2015](https://openairdocs.org/deregistered/N828AS-2015-02-27.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 3 · 144 reports

- [SDR ASOA2014102311475](https://openairdocs.org/sdr/ASOA2014102311475.md): Skin · damaged · Oct 17, 2014 · N828AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > BURN ON SKIN BETWEEN BS 424 AND 439 BETWEEN STRINGERS 1 AND 2R. BLENDED DAMAGE IAW SRM 51-12-00. FOUND BLEND TO BE OUT BE WITHIN LIMITS IAW REO 601R-53-00-115, REV E.
- [SDR ASOA2014102311474](https://openairdocs.org/sdr/ASOA2014102311474.md): Skin · damaged · Oct 17, 2014 · N828AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > BURN ON SKIN AT BS 409+128 BETWEEN STRINGER 1 - 2R. BLENDED AREA TO REMOVE DAMAGE IAW SRM 51-12-00. FOUND BLEND TO NOT BE WITHIN LIMITS OF REO 601R-53-00-115, REV E.
- [SDR ASOA2012121002627](https://openairdocs.org/sdr/ASOA2012121002627.md): Charger · inoperative · Dec 7, 2012 · N828AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR LEVEL FLOODLIGHT IS INOPERATIVE AT PAX DOOR. R & R TB 105-3 WITH SERVICEABLE DIODE BLOCK IAW ESPM 20-18-10. R & R BATTERY CHARGER PS2LF WITH SERVICEABLE UNIT IAW AMM 33-51-05-00-801 AND 33-51-05-400-8001. SDR CLOSED.
- [SDR ASOA2012120502602](https://openairdocs.org/sdr/ASOA2012120502602.md): Strap · corroded · Nov 19, 2012 · N828AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > NUT PLATE STRAP CORRODED AT RBL 27 TO FLOOR SUPPORT AT FS 559. BLENDED OUT CORROSION IAW REO 601R-53-51-203.
- [SDR ASOA2012112902578](https://openairdocs.org/sdr/ASOA2012112902578.md): Seat Track · corroded · Nov 19, 2012 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 9 AT FS 394 TO 409 + 128 CORRODED. FOUND CORRODED BEYOND LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11. FABRICATED REPLACEMENT SEAT TRACK IAW REO 601R-53-00-485. INSTALLED REPLACEMENT SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2012120502601](https://openairdocs.org/sdr/ASOA2012120502601.md): Frame · corroded · Nov 16, 2012 · N828AS · Cndair CL6002B19 · Fuselage Main, Frame
  > RT FRAME INBD DOUBLER AT FS 473.15 HAS CORROSION LOCATED JUST BELOW LAST ROW OF RIVETS. REMOVED CORROSION IAW SRM 51-21-06. COMPLIED WITH REO 601R-53-41-1641.
- [SDR ASOA2012121002626](https://openairdocs.org/sdr/ASOA2012121002626.md): Attach Angle · corroded · Nov 15, 2012 · N828AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > REMOVED CLIP FOR CORROSION REMOVAL AT FS 348. CORROSION REMOVED FROM CLIP, CLIP FOUND TO BE OUT OF LIMITS IAW SRM 53-21-43. DRILLED UP NEW CLIP IAW SRM 51-40-11-00, MP161880 11/18/12. INSTALLED NEW CLIP ALL WORK DONE IAW SRM 51-42-06. SDR CLOSED.
- [SDR ASOA2012121002625](https://openairdocs.org/sdr/ASOA2012121002625.md): Attach Angle · corroded · Nov 14, 2012 · N828AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > SERVICE DOOR SURROUND STRUCTURE CLIP AT FS 349.00 CORRODED. FABRICATED AND INSTALLED NEW CLIP, IAW SNIEO 601R31148 S01.
- [SDR ASOA2012121002624](https://openairdocs.org/sdr/ASOA2012121002624.md): Attach Angle · corroded · Nov 14, 2012 · N828AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > SERVICE DOOR SURROUND STRUCTURE CLIP AT FS 319.70 CORRODED. REMOVED CLIP AT FS 319.70 IAW SRM 51-42-06. INSTALLED NEW PART ALL WORK DONE IAW SRM 51-42-06 & 51-42-21. FORMED SERVICE DOOR SURROUND STRUCTURE CLIP IAW DWG 601R38303 AND SRM 51-24-21.
- [SDR ASOA2012112902577](https://openairdocs.org/sdr/ASOA2012112902577.md): Channel · corroded · Nov 14, 2012 · N828AS · Cndair CL6002B19 · Passenger/Crew Doors
  > CENTER HINGE CHANNEL FOUND TO BE CORRODED AT HINGE SIDE OF PAX DOOR. REMOVED PAX DOOR CENTER HINGE CHANNEL IAW SRM 51-42-06, 51-42-21. INSTALLED SERVICEABLE PAX DOOR CENTER HINGE CHANNEL IAW SRM 51-42-06, 51-42-21.
- [SDR ASOA2012112902576](https://openairdocs.org/sdr/ASOA2012112902576.md): Support Angle · corroded · Nov 14, 2012 · N828AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT WINDSCREEN SUPPORT ANGLE AT FS 349 CORRODED. BLENDED SUPPORT ANGLE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-43 ALLOWABLE DAMAGE. REMOVED RT SUPPORT ANGLE IAW SRM 51-42-06. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-42-06-00 AND 51-42-13-00 AND 51-42-21-00
- [SDR ASOA2012112902575](https://openairdocs.org/sdr/ASOA2012112902575.md): Angle · corroded · Nov 13, 2012 · N828AS · Cndair CL6002B19 · Passenger/Crew Doors
  > FWD PAX DOOR CORNER ASSY FOUND TO BE CORRODED ON HINGE SIDE. REMOVED FWD PAX DOOR CORNER ASSY IAW SRM 51-42-06. INSTALLED SERVICABLE PAX DOOR FWD CORNER ASSY IAW SRM 51-42-06.
- [SDR ASOA2012112902574](https://openairdocs.org/sdr/ASOA2012112902574.md): Angle · corroded · Nov 13, 2012 · N828AS · Cndair CL6002B19 · Passenger/Crew Doors
  > AFT PAX DOOR CORNER ASSY FOUND TO BE CORRODED ON HINGE SIDE. REMOVED AFT PAX DOOR CORNER ASSY IAW SRM 51-42-06, 51-42-21. INSTALLED SERVICABLE PAX DOOR AFT CORNER ASSY IAW SRM 51-42-06, 51-42-21.
- [SDR ASOA2012112902573](https://openairdocs.org/sdr/ASOA2012112902573.md): Angle · corroded · Nov 13, 2012 · N828AS · Cndair CL6002B19 · Passenger/Crew Doors
  > FIVE HINGE SIDE LT ANGLES FOUND TO BE CORRODED. R & R PAX DOOR ANGLES IAW SRM 51-42-06.
- [SDR ASOA2012121002623](https://openairdocs.org/sdr/ASOA2012121002623.md): Angle · corroded · Nov 9, 2012 · N828AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR SILL PLATE COVER AFT NUTPLATE ANGLE CORRODED. FORMED AND INSTALLED GALLEY SERVICE DOOR SILL PLATE COVER AFT ANGLE IAW DWG 601R38695 AND SRM 51-24-21.
- [SDR ASOA2012121002622](https://openairdocs.org/sdr/ASOA2012121002622.md): Frame · corroded · Nov 9, 2012 · N828AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 349.00 CORRODED AT STRINGER 17 RT. FRAME REPAIRED IAW REO 601R-53-21-2374 REV(P3).
- [SDR ASOA2012120502600](https://openairdocs.org/sdr/ASOA2012120502600.md): Fitting · corroded · Nov 9, 2012 · N828AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LIGHT CORROSION ON FITTING ON CARGO FLOOR AT LT SIDE AFT PRESSURE BULKHEAD. REMOVED FITTING/SPLICE IAW SRM 51-42-06-00 AND 51-42-21-00. INSTALLED NEW SPLICE FITTING IAW SRM 51-42-06. SDR CLOSED.
- [SDR ASOA2012120502599](https://openairdocs.org/sdr/ASOA2012120502599.md): Floor Support · corroded · Nov 9, 2012 · N828AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > NUTPLATE CHANNEL CORRODED BETWEEN LEFT FLOOR SUPPORT AND LBL 27 AT FS 559.00. COMPLIED WITH REO 601R-53-51-203.
- [SDR ASOA2012120402598](https://openairdocs.org/sdr/ASOA2012120402598.md): Channel · corroded · Nov 9, 2012 · N828AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > NUT PLATE CHANNEL CORRODED AT BS 559.00 BETWEEN RBL 9 AND LBL 9. BLENDED NUTPLATE CHANNEL IAW SRM 51-21-06. AREAS BLENDED IN COMPLIANCE WITH REO 601R-53-51-203.
- [SDR ASOA2012120402597](https://openairdocs.org/sdr/ASOA2012120402597.md): Strap · corroded · Nov 9, 2012 · N828AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR FRAME CUTOUT HAS CORROSION ON A STRAP UPPER AFT CORNER. R & R PAX DOOR FRAME UPPER AFT STRAP IAW DWG 600-31153 AND SRM 51-40-11 AND 51-42-20.
- [SDR ASOA2012112902572](https://openairdocs.org/sdr/ASOA2012112902572.md): Fitting · corroded · Nov 9, 2012 · N828AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LIGHT CORROSION ON FITTING ON CARGO FLOOR AT LT SIDE AFT PRESSURE BULKHEAD. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-00 FOUND FITTING/SPLICE TO BE OUT OF TOLERANCE IAW SRM 53-61-23-00. REMOVED FITTING/SPLICE IAW SRM 51-42-06-00 AND 51-42-21-00. INSTALLED
- [SDR ASOA2012112902571](https://openairdocs.org/sdr/ASOA2012112902571.md): Angle · corroded · Nov 9, 2012 · N828AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR UPPER ATTACH RODS, SILL RETAINER ANGLES CORRODED. R & R THRESHOLD ANGLE FS 310 AND 349 IAW SRM 51-42-06 AND 51-42-13.
- [SDR ASOA2012112902570](https://openairdocs.org/sdr/ASOA2012112902570.md): Floor Support · corroded · Nov 9, 2012 · N828AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT CORRODED AT FRAME BS 310. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM TR 53-27. R & R FLOOR SUPPORT IAW SRM 51-42-06-00 AND 51-42-13-00.
- [SDR ASOA2012112902569](https://openairdocs.org/sdr/ASOA2012112902569.md): Seat Track · corroded · Nov 9, 2012 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK CORRODED AT FRAME BS 349. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. FOUND TO BE CORRODED BEYOND LIMITS IAW SRM 51-21-06 AND 53-21-49. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2012112902568](https://openairdocs.org/sdr/ASOA2012112902568.md): Seat Track · corroded · Nov 9, 2012 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK CORRODED AT FRAME BS 349. SEAT TRACK CORRODED BEYOND LIMITS IAW SRM 53-21-49. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2012112902567](https://openairdocs.org/sdr/ASOA2012112902567.md): Angle · cracked · Nov 9, 2012 · N828AS · Cndair CL6002B19 · Fuselage Main, Structure
  > ANGLE CRACKED AT BS 280 CROSSBEAM. FABRICATED NEW ANGLE IAW REO 601R-53-11-171. INSTALLED NEW ANGLE IAW SRM 51-42-06 & 51-42-20.
- [SDR ASOA2012120402596](https://openairdocs.org/sdr/ASOA2012120402596.md): Floor Support · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT PLATE CORRODED BETWEEN FRAMES BS 559+16 AND 559+32. REMOVED CORROSION ON RT FLOOR SUPPORT PLATE IAW SRM 51-21-06.
- [SDR ASOA2012120402595](https://openairdocs.org/sdr/ASOA2012120402595.md): Floor Support · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT CORRODED BETWEEN FRAMES BS 559+48 AND 559+80. REMOVED CORROSION FROM RT FLOOR SUPPORT PLATE IAW SRM 51-21-06.
- [SDR ASOA2012120402594](https://openairdocs.org/sdr/ASOA2012120402594.md): Floor Support · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT CORRODED BETWEEN FRAMES BS 559+80 AND 559+112. REMOVED CORROSION FROM RT FLOOR SUPPORT PLATE IAW SRM 51-21-06.
- [SDR ASOA2012120402593](https://openairdocs.org/sdr/ASOA2012120402593.md): Floor Support · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT FLOOR SUPPORT PLATE CORRODED BETWEEN FS 559+80 AND 559+112. REMOVED CORROSION FROM LT FLOOR SUPPORT PLATE IAW SRM 51-21-06 13 EA LOCATIONS.
- [SDR ASOA2012120402592](https://openairdocs.org/sdr/ASOA2012120402592.md): Floor Support · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT PLATE CORRODED FROM FS 589 TO 559+112. REMOVED CORROSION FROM FLOOR SUPPORT PLATE IAW SRM 51-21-06.
- [SDR ASOA2012112902566](https://openairdocs.org/sdr/ASOA2012112902566.md): Seat Track · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT RBL 9 BETWEEN FS 559+112 AND 574. BLENDED SEAT TRACK IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 51-61-49. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2012112902565](https://openairdocs.org/sdr/ASOA2012112902565.md): Seat Track · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 27 CORRODED BETWEEN FS 559+80 AND 559+96. BLENDED SEAT TRACK IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 51-61-49. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2012112902564](https://openairdocs.org/sdr/ASOA2012112902564.md): Seat Track · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9 CORRODED BETWEEN FS 559+88 AND 559+96. BLENDED SEAT TRACK IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM 51-61-49. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2012112902563](https://openairdocs.org/sdr/ASOA2012112902563.md): Seat Track · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT LBL 9 BETWEEN FS 559+88 AND 559+96. REMOVED CORROSION FROM SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06, 53-51-49 AND 53-21-49. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2012112902562](https://openairdocs.org/sdr/ASOA2012112902562.md): Seat Track · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 27 CORRODED BETWEEN FS 559+80 AND 559+96. REMOVED CORROSION FROM SEAT TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06, 53-51-49 AND 53-21-49. R & R SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2012112902561](https://openairdocs.org/sdr/ASOA2012112902561.md): Cargo Track · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRODED AT LBL 27 BETWEEN FS 559+96 AND 559+112. R & R CARGO TRACK IAW SRM 51-41-02 & 51-41-04.
- [SDR ASOA2012112902560](https://openairdocs.org/sdr/ASOA2012112902560.md): Cargo Track · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRODED AT LBL 27 BETWEEN FS 559+112 AND 574. R & R CARGO TRACK IAW SRM 51-41-02 & 51-41-04.
- [SDR ASOA2012112902559](https://openairdocs.org/sdr/ASOA2012112902559.md): Seat Track · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 9 CORRODED BETWEEN FS 559+112 AND 574. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS MATERIAL LOSS.027 WITH MAXIMUM ALLOWABLE.020 IAW SRM 53-61-49 AND 51-21-06. REMOVED OLD TRACK AND INSTALLED NEW SEAT TRACK IAW SRM 53-61-42.
- [SDR ASOA2012112902558](https://openairdocs.org/sdr/ASOA2012112902558.md): Cargo Track · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRODED AT LBL9 BETWEEN FS874.00 AND 589.00. R & R CARGO TRACK IAW SRM 51-41-02 & 51-41-04.
- [SDR ASOA2012112902557](https://openairdocs.org/sdr/ASOA2012112902557.md): Cargo Track · corroded · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRODED AT LBL9 BETWEEN FS 605 AND FS 589. R & R CARGO TIE DOWN PLATE WITH SCREWS IAW SRM 51-41-02 & 51-41-04.
- [SDR ASOA2012112802556](https://openairdocs.org/sdr/ASOA2012112802556.md): Floor Panel · cracked · Nov 7, 2012 · N828AS · Cndair CL6002B19 · Fuselage Floor Panel
  > FLOOR PANEL CRACKED AT FS 193.00. REPAIRED IAW GREO 601R-53-11-111.
- [SDR ASOA2012112802555](https://openairdocs.org/sdr/ASOA2012112802555.md): Seal · cracked · Nov 5, 2012 · N828AS · Cndair CL6002B19 · Wing Main, Frame Structure
  > RIGHT WING FLIGHT SPOILER CUTOUT CENTER SILL PLATE CRACKED. R & R CRACKED SEAL IAW SRM 51-40-06,51-42-01 & 51-40-2.
- [SDR ASOA2012092802315](https://openairdocs.org/sdr/ASOA2012092802315.md): Pdu · failed · Sep 25, 2012 · N828AS · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT THRUST UNLATCHED MASTER CAUTION IN FLIGHT, COMPLIED WITH QRH. EMERGENCY DECLARED AND ACFT RETURNED TO DEPARTURE. R & R RT ENGINE THRUST REVERSER PDU. RT ENGINE THRUST REVERSER OP CHECKED GOOD IAW AMM 78-32-03. NO FURTHER DEFECTS NOTED.
- [SDR ASOA2012083102160](https://openairdocs.org/sdr/ASOA2012083102160.md): Battery · discharged · Aug 30, 2012 · N828AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT ON F/A PANEL ON POSITION EMERGENCY LIGHT ARE NOT OPERATING. CHARGED BATTERY SUPPLY IAW AMM 33-51-00 AND OPS CHECKED GOOD.
- [SDR ASOA201201309](https://openairdocs.org/sdr/ASOA201201309.md): Door · binding · Apr 19, 2012 · N828AS · Cndair CL6002B19 · Galley Doors
  > GALLEY SERVICE DOOR WILL NOT OPEN OR CLOSE. UNBOUND DOOR AND OPS CHECKED GOOD IAW AMM 52-70-00.
- [SDR ASOA201201283](https://openairdocs.org/sdr/ASOA201201283.md): Nut · missing · Apr 16, 2012 · N828AS · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY SIGN ON GALLEY NEAR SERVICE DOOR INOP. REPLACED MISSING NUT ON GROUND TERMINAL OPS CHECKED GOOD IAW AMM 33-51-10.
- [SDR ASOA201200464](https://openairdocs.org/sdr/ASOA201200464.md): Sensor · intermittent · Feb 11, 2012 · N828AS · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAP FAIL CAUTION MESSAGE AT 0 DEGREES DURING APPROACH. EMERGENCY DECLARED. R & R RT FLAP BRAKE POSITION SENSOR IAW AMM 27-51-10. OP'S CHECKED GOOD.
- [SDR ASOA201200155](https://openairdocs.org/sdr/ASOA201200155.md): Flap System · failed · Jan 14, 2012 · N828AS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ENROUTE, SELECTED FLAPS, 8 FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT ZERO. ACFT DIVERTED, EMERGENCY DECLARED. ACFT OK FOR SERVICE. MCO CLEARED.
- [SDR ASOA201101673](https://openairdocs.org/sdr/ASOA201101673.md): Priority Valve · failed · Sep 8, 2011 · N828AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON TAKEOFF RECEIVED A GEAR DISAGREE, NOSE WHEEL WAS DOWN AND MAINS WERE UP. RAN QRH, DID THE EMERGENCY GEAR EXTENTION. ACFT RETURNED TO DEPARTURE. UPON TOUCHDOWN, HAD NO NOSE WHEEL STEERING. R & R NLG PRIORITY VAVLE IAW AMM 32-33-15, PERFORMED FUNCTIONA

Next page: https://openairdocs.org/deregistered/N828AS-2015-02-27/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 = 'N828AS' AND deregistration_id = 'N828AS-2015-02-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N828AS-2015-02-27/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.