# Service difficulty reports: N829AS, cancelled Feb 20, 2015

A list on [N829AS, cancelled Feb 20, 2015](https://openairdocs.org/deregistered/N829AS-2015-02-20.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 · 134 reports

- [SDR ASOA2014031410127](https://openairdocs.org/sdr/ASOA2014031410127.md): Light · damaged · Mar 10, 2014 · N829AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOODLIGHT DAMAGED. R & R FLOODLIGHT IAW AMM 33-51-19. OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2013092709106](https://openairdocs.org/sdr/ASOA2013092709106.md): Bulb · burned out · Sep 26, 2013 · N829AS · Cndair CL6002B19 · Emergency Lighting
  > LT AFT EXTERNAL EMERGENCY LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2013051003501](https://openairdocs.org/sdr/ASOA2013051003501.md): Intercostal · corroded · Apr 26, 2013 · N829AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AFT OF MAIN AVI DOOR CUTOUT AT FS 394 - 409, S26L HAS MINOR CORROSION ON FWD END OF ATTACH FLANGE. REPAIRED IAW SRM 51-42-06.
- [SDR ASOA2013051003500](https://openairdocs.org/sdr/ASOA2013051003500.md): Skin · corroded · Apr 19, 2013 · N829AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LT SIDE LOWER WING PLANK ACCESS HOLE FOR PANEL 540DB HAS INDICATIONS OF CORROSION ON LANDING APPROX 55 PERCENT, FULL SCREEN HEIGHT. ACCESS HOLE FAILED NDT. REPAIRED IAW EC/TC EO 600-57-81 & REO 601R-57-21-030, REV J.
- [SDR ASOA2013051003499](https://openairdocs.org/sdr/ASOA2013051003499.md): Skin · corroded · Apr 19, 2013 · N829AS · Cndair CL6002B19 · Wing, Plate/Skin
  > ACCESS HOLE FOR PANEL 650GB ON LOWER WING PLANK HAS INDICATIONS OF CORROSION ON LANDING APPROX 58 PERCENT FULL SCREEN HEIGHT. ACCESS HOLE 650GB FAILED NDT. REPAIRED IAW EC/TC EO 600-57-81 & REO 601R-57-21-030, REV J.
- [SDR ASOA2013051003498](https://openairdocs.org/sdr/ASOA2013051003498.md): Skin · corroded · Apr 19, 2013 · N829AS · Cndair CL6002B19 · Wing, Plate/Skin
  > ACCESS HOLE 610AB LOWER WING PLANK ACCESS HOLE HAS INDICATIONS OF CORROSION ON LANDING APPROX 50 PERCENT FULL SCREEN HOLE. ACCESS HOLE FAILED NDT. REPAIRED IAW EC/TC EO 600-57-81 & REO 601R-57-21-030, REV J.
- [SDR ASOA2013051003497](https://openairdocs.org/sdr/ASOA2013051003497.md): Floor Support · corroded · Apr 15, 2013 · N829AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT FS 449.85 HAS CORROSION AROUND 1 FLOORBOARD NUTPLATE HOLE. REPAIRED IAW REO 601R-53-41-1689.
- [SDR ASOA2013051003496](https://openairdocs.org/sdr/ASOA2013051003496.md): Post · cracked · Apr 15, 2013 · N829AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND FS 409+128 VERTICAL POST BL 0.0 RT SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS WL 69 APPROX.2" IN LENGTH 60 PERCENT FSH. FAILED NDT INSPECTION. REMOVED RT POST FORM LT POST AT FS 409.00+182 BL 0.0 IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE RT SID
- [SDR ASOA2013051003495](https://openairdocs.org/sdr/ASOA2013051003495.md): Post · cracked · Apr 15, 2013 · N829AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND FS 409+128 VERTICAL POST RBL 18.0 INBD SIDE HAS INDICATION NOTED AT AFT FLANGE RADIUS WL 69.0 APPROX.2" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED FS 409+128, RBL 18.0 CRACKED POST ASSY DRILLED, LOCATED FASTENER HOLES IAW SRM 51-42-06 AN
- [SDR ASOA2013050903492](https://openairdocs.org/sdr/ASOA2013050903492.md): Bulkhead · cracked · Apr 15, 2013 · N829AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50 WL 130 APPROX.4" IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541.
- [SDR ASOA2013050903491](https://openairdocs.org/sdr/ASOA2013050903491.md): Panel · corroded · Apr 12, 2013 · N829AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING LWR WING PLANK ACCESS HOLE 510AB HAS PITTING/CORROSION AT INBD LOCATION. REPAIRED IAW EO 600-57-81 & REO 601R-57-21-030, REV J.
- [SDR ASOA2013050903490](https://openairdocs.org/sdr/ASOA2013050903490.md): Panel · corroded · Apr 12, 2013 · N829AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LWR WING PLANK ACCESS HOLE 540BB HAS PITTING/CORROSION AT INBD AND OTBD LOCATIONS. REPAIRED IAW EO 600-57-81 & REO 601R-57-21-030, REV J.
- [SDR ASOA2013050903489](https://openairdocs.org/sdr/ASOA2013050903489.md): Skin · corroded · Apr 12, 2013 · N829AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING LOWER WING PLANK ACCESS HOLE 640AB CORRODED AT AFT LOCATION. REPAIRED IAW EO 600-57-81 & REO 601R-57-21-030, REV J.
- [SDR ASOA2013050903488](https://openairdocs.org/sdr/ASOA2013050903488.md): Skin · corroded · Apr 12, 2013 · N829AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING LOWER WING PLANK ACCESS HOLE 640BB HAS CORROSION AT FWD AND AFT LOCATIONS. REPAIRED IAW EO 600-57-81 & REO 601R-57-21-030, REV J.
- [SDR ASOA2013051003494](https://openairdocs.org/sdr/ASOA2013051003494.md): Floor Support · cracked · Apr 11, 2013 · N829AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484 FLOOR SUPPORT ANGLE AT RBL 27 IS CRACKED. REMOVED ANGLE IAW SRM 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE ANGLE IAW SRM 51-40-11. INSTALLED NEW ANGLE IAW SRM 51-42-21.
- [SDR ASOA2013050903487](https://openairdocs.org/sdr/ASOA2013050903487.md): Sill · corroded · Apr 11, 2013 · N829AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR FLOOR SILL IS CORRODED. REMOVED CORRODED SILL PLATE FROM SERVICE DOOR SURROUND STRUCTURE IAW SRM 51-42-21. LOCATED AND DRILLED NEW SILL PLATE IAW SRM 51-40-11. INSTALLED SERVICE DOOR SILL PLATE IAW SRM 51-42-10, 51-42-06 AND 51-42-21.
- [SDR ASOA2013050903486](https://openairdocs.org/sdr/ASOA2013050903486.md): Floor Support · cracked · Apr 11, 2013 · N829AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484, FLOOR SUPPORT ANGLE AT RBL 27 IS CRACKED. REMOVED CLIP PN 601R31171-9 IAW SRM 51-42-21 AT FS 484 RBL 27. LOCATED AND DRILLED NEW SERVICEABLE CLIP PN 601R31171-9 IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE CLIP IAW SRM 51-42-21.
- [SDR ASOA2013050803482](https://openairdocs.org/sdr/ASOA2013050803482.md): Angle · cracked · Apr 11, 2013 · N829AS · Cndair CL6002B19 · Trailing Edge Flaps
  > LT OTBD FLAP MIDDLE HINGE POINT OTBD ATTACH ANGLE FOR 595BB IS CRACKED IN RADIUS 2.5". DRILLED UP NEW SERVICEABLE ATTACH ANGLE IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE ATTACH ANGLE ON LT OTBD FLAP MIDDLE HINGE IAW SRM 51-42-06.
- [SDR ASOA2013050803481](https://openairdocs.org/sdr/ASOA2013050803481.md): Frame · cracked · Apr 9, 2013 · N829AS · Cndair CL6002B19 · Fuselage Main, Frame
  > LT FS 718 FRAME PREVIOUS REPAIR SHOWS VISUAL SIGNS OF A CRACK BETWEEN STRINGERS 10L AND 12L. REPLACED SECTION OF FRAME BS 718 FROM STR 5L-21L IAW SRM 51-42-06 AND 51-41-02 TO ACCOMODATE SB 601R-53-055.
- [SDR ASOA2013050803480](https://openairdocs.org/sdr/ASOA2013050803480.md): Frame · cracked · Apr 9, 2013 · N829AS · Cndair CL6002B19 · Fuselage Main, Frame
  > RT FS 718, FRAME PREVIOUS REPAIR SHOWS VISUAL SIGNS OF A CRACK BETWEEN STRINGERS 10R AND 12R. REMOVED SECTION OF FRAME STATION 718 BETWEEN STR 5R AND 21R IAW SRM 51-42-06 AND 51-41-02. RECEIVED NEW FRAME SECTION PO 600-36030-24, REQ'S LOCATING AND DRILLING.
- [SDR ASOA2012110602429](https://openairdocs.org/sdr/ASOA2012110602429.md): Light · damaged · Nov 2, 2012 · N829AS · Cndair CL6002B19 · Emergency Lighting
  > ROW 1CD EMERGENCY FLOOR STRIP DAMAGED. R & R ROW 1CD EMERGENCY FLOOR TRACK STRIP IAW CRJ 200 33-51-01, NO FURTHER DEFECTS.
- [SDR ASOA201201285](https://openairdocs.org/sdr/ASOA201201285.md): Bulb · burned out · Apr 16, 2012 · N829AS · Cndair CL6002B19 · Emergency Lighting
  > AFT EMERGENCY CEILING LIGHT INOPERATIVE. R & R AFT EMERGENCY CEILING LIGHT BULB. OP'S CHECKED GOOD.
- [SDR ASOA201200159](https://openairdocs.org/sdr/ASOA201200159.md): Flap System · malfunctioned · Jan 13, 2012 · N829AS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED, 22 DEG LT, 20 DEG RT. EMERGENCY DECLARED. TROUBLESHOT FLAP SYSTEM IAW FIM 27-50-00 WITH NO DEFECTS NOTED. PEFORMED OPS TEST OF THE FECU FLAP SYS IAW AMM 27-51-05. OPS CHECKED GOOD.
- [SDR ASOA201102278](https://openairdocs.org/sdr/ASOA201102278.md): Torque Link · disconnected · Nov 26, 2011 · N829AS · Cndair CL6002B19 · Nose/Tail Landing Gear
  > GEAR DISAGREE. NOSE GEAR WOULD NOT COME UP. C/W QRH ALSO WOW INPUT CAUTION MESSAGE. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) COMPLIED WITH RIL 2585 AND RO 11/973 TO RETURN THE NOSE GEAR TO SERVICE. (CREW FOUND NLG TORQUE L
- [SDR ASOA201101267](https://openairdocs.org/sdr/ASOA201101267.md): Door · binding · Jul 4, 2011 · N829AS · Cndair CL6002B19 · Passenger/Crew Doors
  > COULD NOT GET MAIN CABIN DOOR TO OPEN UPON ARRIVAL. OPS CHECK OG MAIN CABIN DOOR IAW AMM 52-10-00, OK FOR SERVICE.
- [SDR ASOA201100534](https://openairdocs.org/sdr/ASOA201100534.md): Seat Track · corroded · Mar 22, 2011 · N829AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO BAY SEAT TRACK CORRODED. LOCATED AND DRILLED SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW SRM 51-41-02. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.
- [SDR ASOA201100614](https://openairdocs.org/sdr/ASOA201100614.md): Channel · corroded · Mar 17, 2011 · N829AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR BOTTOM INSIDE (WITH DOOR IN THE CLOSED POSITION) HAS MINOR CORROSION ON CHANNEL & SEVERAL RIVETS. REMOVED FASTENERS IN AREA & CLEANED AREA OF CHANNEL, FOUND CHANNEL TO BE CORRODED BEYOND REPAIR. REPLACEMENT OF CHANNEL. RII FOUND TO BE SATISFACTORY
- [SDR ASOA201100530](https://openairdocs.org/sdr/ASOA201100530.md): Intercostal · cracked · Mar 17, 2011 · N829AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LOWER FWD INTERCOSTAL ARE CRACKED. REMOVED CRACKED LOWER FWD INTERCOSTAL FROM THE PAX DOOR IAW SRM 51-42-06. DRILLED & INSTALLED NEW SERVICEABLE INTERCOSTAL ON THE PAX DOOR IAW SRM 51-42-06. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.
- [SDR ASOA201100521](https://openairdocs.org/sdr/ASOA201100521.md): Attach Fitting · corroded · Mar 17, 2011 · N829AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PAX DOOR FRAME CLIPS ON BOTTOM END AT FS 320.10, 329.50 AND 338.00 ARE CORRODED. REMOVED 5 CORRODED FRAME CLIPS FROM UPPER (HINGE) SECTION. FIT, DRILLED & INSTALLED 5 NEW FRAME CLIPS ONTO UPPER SECTION OF PAX DOOR IAW SRM 51-42-06. THIS REPAIR IS CLASSIFIED A
- [SDR ASOA201100499](https://openairdocs.org/sdr/ASOA201100499.md): Isolator · broken · Mar 16, 2011 · N829AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621.00 PRESSURE BULKHEAD HAS ISOLATOR CRACKED. R & R ISOLATOR IAW SRM 51-42-06. MINOR REPAIR.
- [SDR ASOA201100498](https://openairdocs.org/sdr/ASOA201100498.md): Frame · corroded · Mar 16, 2011 · N829AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME AT FS 333.00 HAS SEVERAL AREAS OF CORROSION ON FWD SIDE OF FRAME BETWEEN STR 25L AND STR 25R.
- [SDR ASOA201100520](https://openairdocs.org/sdr/ASOA201100520.md): Floor Support · corroded · Mar 11, 2011 · N829AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO FLOOR SUPPORT AT LBL 27 OTBB SIDE HAS MINOR CORROSION AROUND NUTPLATES FROM FS 621 TO FS 559+112. REMOVED LBL 27.0 FLOOR SUPPORT CAP FROM FS 559+112 TO FS 621 IAW SRM 51-42-21. LOCATED AND DRILLED FASTENER HOLES IN SERVICEABLE LBL27 FLOOR SUPPORT CAP
- [SDR ASOA201100466](https://openairdocs.org/sdr/ASOA201100466.md): Intercostal · cracked · Mar 11, 2011 · N829AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484, INTERCOSTAL CLIP IS CRACKED AT LBL 36. REINSTALLED PULLEY MOUNTS IAW CRJ 200 AMM 20-24-00-910-801. REPAIR TO THE INTERCOSTALS AT FS 484 BETWEEN BL 27 AND BL 36 IS COMPLETED IAW REO 601R-53-41-059 AND MEETS WITH ALL THEIR REQUIREMENTS. FOUND TO BE SA
- [SDR ASOA201100476](https://openairdocs.org/sdr/ASOA201100476.md): Drag Angle · cracked · Mar 10, 2011 · N829AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED & INSTALLED NEW DRAG ANGLE PN 600-31907-17 IAW SRM 51-42-06/-13.
- [SDR ASOA201100463](https://openairdocs.org/sdr/ASOA201100463.md): Floorbeam · corroded · Mar 10, 2011 · N829AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 TRANSVERSE BEAM FWD "J" CHANNEL CORRODED FROM LBL 9 TO RBL 9. INSTALLED NEW CHANNEL IAW SRM 51-42-06.
- [SDR ASOA201100462](https://openairdocs.org/sdr/ASOA201100462.md): Floorbeam · corroded · Mar 10, 2011 · N829AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 TRANSVERSE BEAM UPPER AFT "J" CHANNEL IS CORRODED FROM LBL 18 TO RBL 36 AT SEVERAL LOCATIONS. FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-00 AND REMOVED CORROSION IAW SRM 51-21-06.
- [SDR ASOA201100461](https://openairdocs.org/sdr/ASOA201100461.md): Floorbeam · corroded · Mar 10, 2011 · N829AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM AT FS 349.00 HAS CORROSION FROM RBL 27 TO RBL 36. REMOVED FLOORBEAM IAW SRM 51-21-06. REPAIRED FLOORBEAM THREATED FOR CORROSION PREVENTION IAW SRM 51-21-11, SRM 51-25-06 AND SRM 51-25-16. AND REINSTALLED IAW SRM 51-42-13, 51-42-15 AND 51-45-00.
- [SDR ASOA201100460](https://openairdocs.org/sdr/ASOA201100460.md): Frame · corroded · Mar 10, 2011 · N829AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME AT FS 319.70 HAS SEVERAL AREAS OF CORROSION BETWEEN STR 25L AND STR 25R. FOUND CORROSION DAMAGE ON FRAME SECTOR AT FS 319.70 BETWEEN STRINGERS 25L AND 25R TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-00. NEW SERVICEABLE FS 319.70 FRAME S
- [SDR ASOA201100459](https://openairdocs.org/sdr/ASOA201100459.md): Frame · corroded · Mar 10, 2011 · N829AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME AT FS 333.00 HAS SEVERAL AREAS OF CORROSION ON FWD SIDE OF FRAME BETWEEN STR 25L AND STR 25R. FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-00. REMOVED, LOCATED, DRILLED, AND INSTALLED FRAME IAW SRM 51-40-11, 51-42-06 & 51-42-21.
- [SDR ASOA201100529](https://openairdocs.org/sdr/ASOA201100529.md): Light · unserviceable · Mar 9, 2011 · N829AS · Cndair CL6002B19 · Lighting System
  > PAX DOOR INTERIOR HANDLE "PULL TO EXIT" SIGN WORN. INSTALLED NEW SERVICEABLE PAX DOOR "PULL TO EXIT" BETA LIGHT IAW AMM 33-51-09-400-801. FUNC TEST GOOD IAW AMM 33-51-09-720-801.
- [SDR ASOA201100446](https://openairdocs.org/sdr/ASOA201100446.md): Seat Track · corroded · Mar 7, 2011 · N829AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEBLE SEAT TRACKS IAW AMM 53-01-11-400-802.
- [SDR ASOA201100445](https://openairdocs.org/sdr/ASOA201100445.md): Floorbeam · cracked · Mar 7, 2011 · N829AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280.0 FLOORBEAM CLIPS CRACKED AT RBL 9 AND LBL 9. REMOVED AND REPLACED FLOORBEAM FWD CLIPS IAW SRM 51-42-21, REO 60R-53-11-2088 & REO 601R-53-11-926.
- [SDR ASOA201100444](https://openairdocs.org/sdr/ASOA201100444.md): Light · inoperative · Mar 7, 2011 · N829AS · Cndair CL6002B19 · Emergency Lighting
  > RT NR1 POSITION LIGHT INOPERATIVE. INSTALLED NEW LIGHT.
- [SDR ASOA201001782](https://openairdocs.org/sdr/ASOA201001782.md): Unknown · odor · Nov 14, 2010 · N829AS · Cndair CL6002B19 · Air Distribution System
  > RECEIVED RT PACK HIGH TEMP CAUTION. MESSAGE DURING CLIMB WITH PACK IN MANUAL MODE. FLIGHT ATTENDANT REPORTED A BURNING SMELL/FOG IN THE CABIN. QRH ACTIONS RETURNED TEMP TO NORMAL RANGE, ALL ASSOCIATED CONDITIONS RETURNED TO NORMAL. PERFORMED OPS CHECK OF R
- [SDR ASOA201000398](https://openairdocs.org/sdr/ASOA201000398.md): Proximity Switch · out of adjust · Mar 17, 2010 · N829AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON DEPARTURE,WHEN SELECTING GEAR UP, RECEIVED "GEAR DISAGREE" WARNING MSG. COMPLIED WITH QRH AND RETURNED TO DEPARTURE. CVR CB OPENED ON RETURN TO GATE. (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED). UPON INSPECTION FAULT CODE S-18 FAR (RT GE
- [SDR ASOA20100049](https://openairdocs.org/sdr/ASOA20100049.md): Bulkhead · cracked · Jan 15, 2010 · N829AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REPAIRED CRACKED LT 202.75 PRESSURE BULKHEAD IAW EC/TC REO 601R-53-11-563 ON WO 145548. JC7020037 1/16/10, ITEM: 1. REPAIRED CRACKED LT 202.75 PRESSURE BULKHEAD IAW EC/TC REO 601R-53-11-563 ON WO 145548. JC7020037 1/16/10.
- [SDR ASOA201000049](https://openairdocs.org/sdr/ASOA201000049.md): Bulkhead · cracked · Jan 15, 2010 · N829AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LEFT FS 202.75 PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE HOLE. REPAIRED CRACKED LT 202.75 PRESSURE BULKHEAD IAW EC/TC REO 601R-53-11-563 ON WO 145548. REPAIRED CRACKED LT 202.75 PRESSURE BULKHEAD IAW EC/TC REO 601R-53-11-563 ON WO 145548.
- [SDR ASOA200901342](https://openairdocs.org/sdr/ASOA200901342.md): Flap System · failed · Dec 3, 2009 · N829AS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 30 DEG ON APPROACH (EMERGENCY DECLARED).
- [SDR ASOA200901104](https://openairdocs.org/sdr/ASOA200901104.md): Light · inoperative · Oct 4, 2009 · N829AS · Cndair CL6002B19 · Emergency Lighting
  > LOWER EMERGENCY LIGHT IN PAX ENTRY AREA INOP.
- [SDR ASOA200900728](https://openairdocs.org/sdr/ASOA200900728.md): Door · binding · Jun 28, 2009 · N829AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HARD TO OPEN.

Next page: https://openairdocs.org/deregistered/N829AS-2015-02-20/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 = 'N829AS' AND deregistration_id = 'N829AS-2015-02-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N829AS-2015-02-20/reports

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