# Service difficulty reports: N821AS, cancelled Jun 8, 2017

A list on [N821AS, cancelled Jun 8, 2017](https://openairdocs.org/deregistered/N821AS-2017-06-08.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 · 187 reports

- [SDR SWIA201642369](https://openairdocs.org/sdr/SWIA201642369.md): Warning Message · illuminated · Jul 28, 2016 · N821AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > AIRCRAFT RETURNED TO THE FIELD WITH A GEAR DISAGREE MESSAGE.
- [SDR SWIA201541566](https://openairdocs.org/sdr/SWIA201541566.md): Sensor · out of adjust · Nov 16, 2015 · N821AS · Cndair CL6002B19 · Landing Gear Position and Warning
  > NOSE DOOR OPEN, GEAR DISAGREE WARNING MESSAGE, AFTER GEAR IS SELECTED UP, PERFORMED QRH, MESSAGES CLEARED, RETURNED TO FIELD. ADJUSTED WOW SENSOR. SWUNG GEAR MULTIPLE TIMES. NO DEFECTS NOTED.
- [SDR SWIA2014121940422](https://openairdocs.org/sdr/SWIA2014121940422.md): Line · failed · Dec 18, 2014 · N821AS · Cndair CL6002B19 · Engine Fuel Distribution
  > DURING CLIMBOUT, NR 2 ENGINE ROLLED BACK TO IDLE. RETURNED TO FIELD. R & R RT ENGINE P3 LINE TO FUEL CONTROL TUBE ASSEMBLY WITH A SERVICEABLE UNIT IAW AMM. OPS CHECKED GOOD.
- [SDR SWIA201440083](https://openairdocs.org/sdr/SWIA201440083.md): Tube · broken · Nov 22, 2014 · N821AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR WIRE HARNESS UNDER TOP STEP HAS BROKEN TUBING, REPAIRED THE TUBING IAW GREO.
- [SDR SWIA201440081](https://openairdocs.org/sdr/SWIA201440081.md): Hinge · gouged · Nov 10, 2014 · N821AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE HALF LUG NR 27 FROM FORWARD SIDE HAS GOUGES. REPAIRED THE HINGE LUG IAW REO.
- [SDR SWIA201440079](https://openairdocs.org/sdr/SWIA201440079.md): Hinge · gouged · Nov 10, 2014 · N821AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR FUSELAGE SIDE HINGE HALF 6TH AND 8TH LUG FROM FORWARD SIDE HAVE GOUGES. BLENDED GOUGE ON PAX DOOR HINGE LUGS NR 6 AND NR 8 IAW REO.
- [SDR SWIA201440078](https://openairdocs.org/sdr/SWIA201440078.md): Structure · cracked · Nov 10, 2014 · N821AS · Cndair CL6002B19 · Fuselage Main, Structure
  > AFT CARGO BAY AT BS 605 HAS A CRACK AT CARGO DOOR. PERFORMED CUT OUT OF DAMAGED AREA ON FLOOR LANDING PLATE AT FS 605.0, REF REO. PERFORMED ET INSP ON REWORKED AREA AND UNDERLAYING STRUCTURE IAW REO. NO DEFECTS NOTED, BTAC NDT-9, TOUCHED UP REWORKED AREA R
- [SDR SWIA201440076](https://openairdocs.org/sdr/SWIA201440076.md): Angle · cracked · Nov 10, 2014 · N821AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9, BS 280 INBD ANGLE IS CRACKED AT UPPER RADIUS. INSTALLED FABRICATED INBD ANGLE IAW REO.
- [SDR SWIA201440075](https://openairdocs.org/sdr/SWIA201440075.md): Angle · cracked · Nov 9, 2014 · N821AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 280, RBL 9.0 INBD AND OTBD ANGELS ARE CRACKED AT UPPER RADIUS. R & R THE ANGLES IAW REO.
- [SDR SWIA201440073](https://openairdocs.org/sdr/SWIA201440073.md): Lever · worn · Nov 9, 2014 · N821AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FORWARD PULL IN LEVER LOBE WORN. REPAIRED IAW REO.
- [SDR SWIA201440069](https://openairdocs.org/sdr/SWIA201440069.md): Floor Skin · cracked · Nov 9, 2014 · N821AS · Cndair CL6002B19 · Fuselage Main, Structure
  > TRU BAY FLOOR SKIN IS CRACKED AT BS 193. REPAIRED TRU BAY FLOOR SKIN IAW REO.
- [SDR SWIA201440067](https://openairdocs.org/sdr/SWIA201440067.md): Bulkhead · cracked · Nov 9, 2014 · N821AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 202 BULKHEAD IS CRACKED AT THE PARKING BRAKE CABLE PASSTHROUGH HOLE. REPAIRED THE BULKHEAD IAW REO.
- [SDR SWIA201440066](https://openairdocs.org/sdr/SWIA201440066.md): Attach Angle · cracked · Nov 9, 2014 · N821AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE STRINGER TO BS 202 BULKHEAD IN AFT LOWER AREA OF NOSE HYDRAULIC COMPARTMENT. R & R ATTACH ANGLE IAW SRM AND EA.
- [SDR SWIA201440064](https://openairdocs.org/sdr/SWIA201440064.md): Structure · corroded · Nov 8, 2014 · N821AS · Cndair CL6002B19 · Standard Practices/Structures
  > CORROSION AROUND NUTPLATE HOLE UNDER PANEL 141BL. C-CHECK, REPAIRED IAW REO.
- [SDR SWIA201440062](https://openairdocs.org/sdr/SWIA201440062.md): Fitting · chafed · Nov 8, 2014 · N821AS · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT ENGINE THRUST REVERSER HAS BOTTOM INBD MAIN TRACK AFT END FITTING CHAFED, UPPER SIDE. REPAIRED THE THRUST REVERSER INBD LOWER MAIN TRACK AND ANCHOR FITTING IAW GREO.
- [SDR SWIA201440061](https://openairdocs.org/sdr/SWIA201440061.md): Attach Fitting · chafed · Nov 8, 2014 · N821AS · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > RIGHT MLG STRUT TO BELLCRANK ATTACHMENT POINT CHAFED. REMOVED AND INSTALLED BOLT ATTACHING RT MLG BELLCRANK TO THE ROD IAW SRM. BLENDED CHAFE DAMAGE ON RT MLG BELLCRANK IAW REO. BLEND FOUND TO BE WITHIN LIMITS IAW REO. RESTORED FINISH TO BLENDED AREA IAW
- [SDR SWIA201440057](https://openairdocs.org/sdr/SWIA201440057.md): Attach Fitting · chafed · Nov 8, 2014 · N821AS · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > LEFT MLG STRUT TO BELLCRANK ATTACHMENT POINT CHAFED. REMOVED AND INSTALLED SCREW ATTACHING BELLCRANK TO THE ROD IAW SRM 51-41-02. BLENDED CHAFE DAMAGE ON LT MLG STRUT-TO-BELL CRANK ATTACHMENT POINT REF REO. EVALUATION, ORIGINAL MATERIAL THICKNESS.140" TOOL
- [SDR SWIA201440056](https://openairdocs.org/sdr/SWIA201440056.md): Panel · cracked · Nov 8, 2014 · N821AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > COCKPIT PANEL 221ALC CRACKED & BROKEN IN MULTIPLE PLACES. REPAIRED DAMAGED AREAS ON PANEL IAW EA.
- [SDR SWIA201440055](https://openairdocs.org/sdr/SWIA201440055.md): Panel · chafed · Nov 8, 2014 · N821AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING BUTTE PANEL 694PB HAS CHAFE DAMAGE ON UPPER SURFACE. REPAIRED PANEL IAW EA.
- [SDR SWIA201440054](https://openairdocs.org/sdr/SWIA201440054.md): Skin · dented · Nov 8, 2014 · N821AS · Cndair CL6002B19 · Spoilers
  > RIGHT WING INBD GROUND SPOILER HAS MULTIPLE SMALL DENTS ON LOWER SURFACE. DENTS ARE WITHIN ALLOWABLE LIMITS, NO FURTHER ACTION REQUIRED, REF REO.
- [SDR SWIA201440053](https://openairdocs.org/sdr/SWIA201440053.md): Panel · failed · Nov 7, 2014 · N821AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT UPPER VISOR PANEL 326AL, FAILED GAP CHECK. REPAIR VISOR PANEL IAW REO.
- [SDR SWIA201440052](https://openairdocs.org/sdr/SWIA201440052.md): Panel · failed · Nov 7, 2014 · N821AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT UPPER VISOR PANEL 326AR FAILED GAP CHECK. REPAIR VISOR PANEL 326AR IAW REO.
- [SDR SWIA201440051](https://openairdocs.org/sdr/SWIA201440051.md): Skin · chafed · Nov 7, 2014 · N821AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO BAY DOOR EXTERIOR SKIN HAS SIX CHAFES AROUND THE RIM OF THE DOOR HANDLE. R & R THE DOOR HANDLE ASSY IAW SRM. PERFORMED OPS CHECK OF THE CARGO DOOR WARNING SYSTEM IAW AMM AND REO.
- [SDR SWIA201440050](https://openairdocs.org/sdr/SWIA201440050.md): Vane · cracked · Nov 6, 2014 · N821AS · Cndair CL6002B19 · Fuselage Main, Structure
  > BOTTOM VANE OF APU EXHAUST OUTLET IS CRACKED. REPAIED IAW REO.
- [SDR SWIA201440049](https://openairdocs.org/sdr/SWIA201440049.md): Structure · eroded · Nov 6, 2014 · N821AS · Cndair CL6002B19 · Turbine Engine Air Inlet Section
  > FOUND EROSION ON THE LT ENGINE NOSE COWL, 6 O'CLOCK POSITION, TO BE WITHIN LIMITS. REPAIRED IAW CMM AND REO.
- [SDR SWIA201438520](https://openairdocs.org/sdr/SWIA201438520.md): Fire Bottle · discharged · Jul 2, 2014 · N821AS · Cndair CL6002B19 · Fire Bottle, Fixed
  > IN FLIGHT GOT CARGO BOTTLE LOW MESSAGE. RETURNED TO DEPARTURE. R & R LT CARGO BOTTLE.
- [SDR SWIA201438423](https://openairdocs.org/sdr/SWIA201438423.md): Line · blown · Jun 25, 2014 · N821AS · Cndair CL6002B19 · Standard Practices/Structures
  > RETURNED TO FIELD WITH A BLOWN FIRE BOTTLE. REINSTALLED A DISCONNECTED LINE BLOWING HOT AIR ON THE FIRE BOTTLE.
- [SDR SWIA201438299](https://openairdocs.org/sdr/SWIA201438299.md): Fire Bottle · failed · Jun 21, 2014 · N821AS · Cndair CL6002B19 · Fire Bottle, Fixed
  > CARGO BOTTLE LOW MESSAGE. REPLACED THE SMALL CARGO FIRE BOTTLE.
- [SDR SWIA201437412](https://openairdocs.org/sdr/SWIA201437412.md): O-Ring · leaking · May 5, 2014 · N821AS · Cndair CL6002B19 · APU Engine Fuel and Control
  > WITH PACKS ON, APU STRONG FUEL ODOR THROUGHOUT FLIGHT DECK AND CABIN. WITH PACKS ON ENGINES ODOR DIMINISHES. REPLACED O-RING ON FUEL CONTROL ELBOW TO FUEL SOLENOID, LEAK AND OPS CHECKED GOOD IAW AMM.
- [SDR SWIA201436226](https://openairdocs.org/sdr/SWIA201436226.md): Light · inoperative · Feb 4, 2014 · N821AS · Cndair CL6002B19 · Emergency Lighting
  > LOWER EXIT LIGHTS ON MAIN CABIN DOOR & GALLEY SERVICE DOOR ARE BURNED OUT. FLT 2938 RELAMPED.
- [SDR SWIA201335501](https://openairdocs.org/sdr/SWIA201335501.md): Battery Pack · discharged · Dec 6, 2013 · N821AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT 2971 CHARGED EMERGENCY LIGHTS BATTERY PACKS.
- [SDR SWIA201333514](https://openairdocs.org/sdr/SWIA201333514.md): Wire · out of position · May 20, 2013 · N821AS · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY EXIT LIGHT NEAR MAIN CABIN DOOR DOES NOT ILLUMINATE. REPOSITIONED WIRES BEHIND EMERGENCY LIGHT.
- [SDR SWIA201333466](https://openairdocs.org/sdr/SWIA201333466.md): Proximity Switch · failed · May 12, 2013 · N821AS · Cndair CL6002B19 · Door Warning System
  > RECEIVED PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE. REPLACED PROXIMITY SWITCH. OPS CHECKED GOOD.
- [SDR SWIA201333224](https://openairdocs.org/sdr/SWIA201333224.md): Unknown · fumes · Apr 9, 2013 · N821AS · Cndair CL6002B19 · Air Distribution System
  > SMELLING FUMES IN CABIN. (FLT 2980) INSPECTED APU ENCLOSURE. BOTH AC PACKS HAVE NORMAL INDICATION WITH NO SIGNS OF OVERHEATING. NO SMOKE SMELLS NOTED.
- [SDR SWIA201333114](https://openairdocs.org/sdr/SWIA201333114.md): Fan · malfunctioned · Mar 31, 2013 · N821AS · Cndair CL6002B19 · Air Distribution Fan
  > ELECTRICAL SMOKE SMELL COMING FROM GALLEY A/C VENT. NO SMOKE AND NO PAX ON BOARD. (FLT 2962) REPLACED GALLEY EXHAUST FAN. OPS CHECK GOOD AT THIS TIME. P/N ON: AE0405A01 P/N OFF: AE0405A02 S/N ON: 1145 S/N OFF: L0865
- [SDR SWIA201332822](https://openairdocs.org/sdr/SWIA201332822.md): Light · inoperative · Feb 17, 2013 · N821AS · Cndair CL6002B19 · Emergency Lighting
  > OVERHEAD EMERGENCY EXIT ROW LIGHT BURNED OUT. (FLT 2850) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201332771](https://openairdocs.org/sdr/SWIA201332771.md): Brake · seized · Feb 7, 2013 · N821AS · Cndair CL6002B19 · Brake
  > LEFT MAIN BRAKE SEIZED. (FLT 2988) REPLACED NR 1 MLG WHEEL ASSEMBLY, RE-INSTALLED QUICK DISCONNECT. P/N 501071-1 S/N ON FEB01-3686 S/N OFF APR97-1354 P/N 5010520-1 S/N ON APR99-1669 S/N OFF NOV02-3692
- [SDR SWIA201232667](https://openairdocs.org/sdr/SWIA201232667.md): Floor Support · corroded · Dec 30, 2012 · N821AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT FS 621 LBL 9 UNDER FLOORBOARD 281JLF HAS FRETTING CORROSION. (C-CHECK) INSTALLED NEW FLOOR SUPPORT AT LBL 9 FS 574-621 IAW REO.
- [SDR SWIA201232666](https://openairdocs.org/sdr/SWIA201232666.md): Access Panel · corroded · Dec 30, 2012 · N821AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING ACCESS PANEL 650HB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) CORROSION AT LOWER WING PLANK COMMON TO PANEL 650HB REPAIRED IAW REO.
- [SDR SWIA201232665](https://openairdocs.org/sdr/SWIA201232665.md): Access Panel · corroded · Dec 30, 2012 · N821AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING ACCESS PANEL 650BB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 650BB REPAIRED IAW REO.
- [SDR SWIA201232664](https://openairdocs.org/sdr/SWIA201232664.md): Access Panel · corroded · Dec 30, 2012 · N821AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING ACCESS PANEL 640FB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) RIGHT LOWER WING PLANK CUTOUT COMMON TO PANEL 640FB REWORKED IAW REO.
- [SDR SWIA201232663](https://openairdocs.org/sdr/SWIA201232663.md): Access Panel · corroded · Dec 30, 2012 · N821AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING ACCESS PANEL 640DB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) RIGHT LOWER WING PLANK CUTOUT COMMON TO PANEL 640DB REWORKED IAW REO.
- [SDR SWIA201232662](https://openairdocs.org/sdr/SWIA201232662.md): Access Panel · corroded · Dec 30, 2012 · N821AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING ACCESS PANEL 640AB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) RIGHT LOWER WING PLANK ACCESS PANEL CUTOUT COMMON TO PANEL 640AB REWORKED IAW REO.
- [SDR SWIA201232661](https://openairdocs.org/sdr/SWIA201232661.md): Access Panel · corroded · Dec 30, 2012 · N821AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING ACCESS PANEL 640BB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK COMMON TO PANEL 640BB REPAIRED IAW REO.
- [SDR SWIA201232660](https://openairdocs.org/sdr/SWIA201232660.md): Access Panel · corroded · Dec 30, 2012 · N821AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING ACCESS PANEL 550HB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 550HB REPAIRED IAW REO.
- [SDR SWIA201232659](https://openairdocs.org/sdr/SWIA201232659.md): Access Panel · corroded · Dec 30, 2012 · N821AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING ACCESS PANEL 550AB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LEFT LOWER WING PLANK COMMON TO ACCESS PANEL 550AB REWORKED IAW REO.
- [SDR SWIA201232658](https://openairdocs.org/sdr/SWIA201232658.md): Access Panel · corroded · Dec 30, 2012 · N821AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING ACCESS PANEL 540EB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 540EB REWORKED IAW REO.
- [SDR SWIA201232657](https://openairdocs.org/sdr/SWIA201232657.md): Access Panel · corroded · Dec 30, 2012 · N821AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING ACCESS PANEL 540BB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) MARKED AREAS OF LOWER WING PLANK COMMON TO PANEL 540BB REWORKED IAW REO.
- [SDR SWIA201232656](https://openairdocs.org/sdr/SWIA201232656.md): Access Panel · cracked · Dec 30, 2012 · N821AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING ACCESS PANEL 510AB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 510AB REWORKED IAW REO.
- [SDR SWIA201232655](https://openairdocs.org/sdr/SWIA201232655.md): Bulkhead · cracked · Dec 28, 2012 · N821AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK NOTED AND MARKED ON FS 621 BULKHEAD WEB, FWD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING. (C-CHECK) REPAIRED FS 621 BULKHEAD WEB, FWD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING IAW REO.

Next page: https://openairdocs.org/deregistered/N821AS-2017-06-08/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 = 'N821AS' AND deregistration_id = 'N821AS-2017-06-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N821AS-2017-06-08/reports

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