# Service difficulty reports: N820AS

A list on [N820AS](https://openairdocs.org/aircraft/N820AS.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 · 161 reports

- [SDR ASOA2015012312076](https://openairdocs.org/sdr/ASOA2015012312076.md): Inverter · inoperative · Jan 21, 2015 · N820AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT INOPERATIVE NEAR OVERWING EMERGENCY DOOR. R & R THE EMERGENCY LIGHT INVERTER, LT SIDE FWD OF EMERGENCY DOOR IAW AMM 33-51-07. OPS CHECK GOOD.
- [SDR ASOA2014102311477](https://openairdocs.org/sdr/ASOA2014102311477.md): Sign · inoperative · Oct 18, 2014 · N820AS · Cndair CL6002B19 · Emergency Lighting
  > LIGHTED FLOOR-LEVEL EXIT SIGN INOPERATIVE AT LT EMERGENCY EXIT. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2014100911397](https://openairdocs.org/sdr/ASOA2014100911397.md): Connector · damaged · Oct 6, 2014 · N820AS · Cndair CL6002B19 · Light System Wiring
  > LIGHTED FLOOR-LEVEL EXIT SIGN AT LEFT EMERGENCY EXIT INOPERATIVE. R & R WIRE SPLICE CONNECTORS IAW SPM 20-17-31. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2014100311371](https://openairdocs.org/sdr/ASOA2014100311371.md): Door · lack of lube · Sep 30, 2014 · N820AS · Cndair CL6002B19 · Passenger/Crew Doors
  > F/A COULD NOT OPEN PASSENGER DOOR FROM THE IN SIDE GROUND CREW HAD TO OPEN DOOR. LUBE THE HARDWARE AND PERFOMED. OPS CHECK IAW AMM 52-11-03, CHECK GOOD ACOK TO SERVICE.
- [SDR ASOA2014071110854](https://openairdocs.org/sdr/ASOA2014071110854.md): Door · out of limits · Jul 10, 2014 · N820AS · Cndair CL6002B19 · Service Doors
  > RIGHT TRU DOOR DOES NOT FIT PROPERLY, PARTICULARLY IN RVSM AREA. TRIMMED TO FIT RIGHT TRU DOOR IAW AMM 52-44-11. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.
- [SDR ASOA2014071110853](https://openairdocs.org/sdr/ASOA2014071110853.md): Door · out of limits · Jul 10, 2014 · N820AS · Cndair CL6002B19 · Service Doors
  > LEFT TRU DOOR DOES NOT FIT PROPERLY, PARTICULARLY IN RVSM AREA. TRIMMED TO FIT LT TRU DOOR IAW AMM 52-44-11. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.
- [SDR ASOA2014050710467](https://openairdocs.org/sdr/ASOA2014050710467.md): Sign · inoperative · May 3, 2014 · N820AS · Cndair CL6002B19 · Emergency Lighting
  > EXIT SIGN INOPERATIVE. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2014041710379](https://openairdocs.org/sdr/ASOA2014041710379.md): Sign · inoperative · Apr 14, 2014 · N820AS · Cndair CL6002B19 · Emergency Lighting
  > LEFT EMERGENCY EXIT LIGHTED FLOOR LEVEL EXIT SIGN INOPERATIVE. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD.
- [SDR ASOA2014041710378](https://openairdocs.org/sdr/ASOA2014041710378.md): Sign · damaged · Apr 14, 2014 · N820AS · Cndair CL6002B19 · Emergency Lighting
  > GALLEY LIGHTED FLOOR LEVEL EXIT SIGN DAMAGED. R & R SIGN IAW AMM 33-51-10. SYS OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2014032810206](https://openairdocs.org/sdr/ASOA2014032810206.md): Sign · inoperative · Mar 24, 2014 · N820AS · Cndair CL6002B19 · Emergency Lighting
  > FLOOR LEVEL EXIT SIGN INOPERATIVE AT LT OVERWING. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD.
- [SDR ASOA2014032810205](https://openairdocs.org/sdr/ASOA2014032810205.md): Light · inoperative · Mar 24, 2014 · N820AS · Cndair CL6002B19 · Emergency Lighting
  > FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. R & R LIGHT ASSY IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD.
- [SDR ASOA2014011609764](https://openairdocs.org/sdr/ASOA2014011609764.md): O-Ring · failed · Jan 6, 2014 · N820AS · Cndair CL6002B19 · Turbine Engine Oil System
  > AFTER TAKEOFF, RECEIVED RT OIL PRESSURE WARNING MESSAGE ACCOMPANIED WITH FLUCTUATIONS OF 25-36 PSI C/W QRH RETURNED TO DEPARTURE. ACFT RETURNED TO DEPARTURE AFTER TAKE OFF, EMERGENCY DECLARED. R & R RT ENGINE OIL PRESSURE SWITCH O-RING IAW AMM-79-31-03, LEA
- [SDR ASOA2013031303195](https://openairdocs.org/sdr/ASOA2013031303195.md): Sill · corroded · Feb 19, 2013 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR LOWER SILL FROM FS 295 - 364 AT STRINGER LOCATION 18L IS CORRODED AT MULTIPLE LOCATIONS TO INCLUDE HANDRAIL STOW CUPS. REPAIRED FLOOR SILL FS 215 -364 IAW EO CL600-2B19-53-I00135.
- [SDR ASOA2013031303194](https://openairdocs.org/sdr/ASOA2013031303194.md): Bulkhead · cracked · Feb 18, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT BL 0.0 WL 142 APPROX 1.0" IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-4823 AND REO 601R-53-61-1285, REV D, DATED 10/31/2011.
- [SDR ASOA2013031303193](https://openairdocs.org/sdr/ASOA2013031303193.md): Bulkhead · cracked · Feb 18, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50 WL 130 APPROX.2" IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-61-1541 REF D.
- [SDR ASOA2013031303192](https://openairdocs.org/sdr/ASOA2013031303192.md): Angle · cracked · Feb 18, 2013 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT SIDE OF REAR PRESSURE BULKHEAD HAS RT FS 621 - 625 OBLIQUE ANGLE CRACKED AT THE RADIUS APPROX.40" LONG. R & R RT FS 625 OBLIQUE ANGLE & SEALED IAW SRM REF 51-42-06, PN 601-35012-52.
- [SDR ASOA2013031303191](https://openairdocs.org/sdr/ASOA2013031303191.md): Frame · corroded · Feb 15, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, Frame
  > MAIN AVIONIC COMPARTMENT FUSELAGE FRAME BS 333 IS CORRODED AT STR 26R. REMOVED CORRODED FRAME SEGMENT & SERVICEABLE REINFORCING ANGLE IAW SRM 51-42-06 & 51-42-21. INSTALLED NEW FRAME SECTOR AND REINSTALLED SERVICEABLE REINFORCING ANGLE IAW SRM 51-42-06 & 51
- [SDR ASOA2013031303190](https://openairdocs.org/sdr/ASOA2013031303190.md): Frame · corroded · Feb 15, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, Frame
  > MAIN AVIONIC COMPARTMENT FUSELAGE FRAME 319 IS CORRODED AT STR 26L. REMOVED FRAME SECTOR IAW SRM 51-42-06. LOCATED & DRILLED NEW FRAME SECTOR IAW 51-40-11. INSTALLED NEW FRAME SEGMENT IAW SRM 51-42-06 & 51-42-21.
- [SDR ASOA2013031303189](https://openairdocs.org/sdr/ASOA2013031303189.md): Frame · corroded · Feb 15, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, Frame
  > MAIN AVIONIC COMPARTMENT FUSELAGE FRAME BS 310 CORRODED AT STR 26R. REMOVED FRAME SECTOR IAW SRM 51-42-06 & 51-42-21. TRIMMED FRAME SECTOR TO FIT AND LOCATED DRILL DEBURR IAW SRM 51-40-11 & 51-42-06 & 51-21-11. INSTALLED FRAME SEGMENT IAW SRM 51-42-06 & 5
- [SDR ASOA2013031303188](https://openairdocs.org/sdr/ASOA2013031303188.md): Intercostal · corroded · Feb 15, 2013 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MAIN AVIONIC COMPARTMENT DOOR CUTOUT INTERCOSTAL BETWEEN FS 349 AND 364 BETWEEN STR 26-27R IS CORRODED. REMOVED CORRODED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW INTERCOSTAL AND INSTALLED IAW SRM 51-42-06 AND 51-42-21.
- [SDR ASOA2013031303187](https://openairdocs.org/sdr/ASOA2013031303187.md): Angle · cracked · Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9 ANGLE ON OTBD SIDE AT FS 280 IS CRACKED. REMOVED ANGLE IAW SRM 51-42-21. LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-42-21 & 51-40-11.
- [SDR ASOA2013031303186](https://openairdocs.org/sdr/ASOA2013031303186.md): Attach Angle · cracked · Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CO-PILOTS SIDE WINDOW POST AFT LOWER ATTCHMENT ANGLE IS CRACKED. R & R CO-PILOTS SIDE WINDOW POST AFT LOWER ATTACHMENT ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-21.
- [SDR ASOA2013031303185](https://openairdocs.org/sdr/ASOA2013031303185.md): Attach Angle · cracked · Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PILOTS SIDE WINDOW POST AFT LOWER ATTACHMENT ANGLE IS CRACKED. R & R PILOT SIDE WINDOW POST AFT LOWER ATTACHMENT ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-21.
- [SDR ASOA2013031303184](https://openairdocs.org/sdr/ASOA2013031303184.md): Door Frame · corroded · Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage Main, Structure
  > MAIN AVIONICS COMPARTMENT DOOR CUTOUT FRAME AT FS 349 BETWEEN STRINGERS 26L AND 27L ARE CORRODED. REMOVED CORRODED FS 349 LWR FRAME SEGMENT IAW SRM 51-42-06 & 51-42-21. DRILLED & LOCATED NEW FRAME. INSTALLED NEW FS 349 LWR FRAME SEGMENT IAW SRM 51-42-06 & 51
- [SDR ASOA2013031303183](https://openairdocs.org/sdr/ASOA2013031303183.md): Intercostal · corroded · Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > MAIN AVIONICS COMPARTMENT DOOR CUTOUT INTERCOSTAL BETWEEN FS 349 AND 364 STRINGER 26L - 27L IS CORRODED. REMOVED CORRODED INTERCOSTAL, LOCATED & DRILLED NEW IAW SRM 51-42-06. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.
- [SDR ASOA2013031303182](https://openairdocs.org/sdr/ASOA2013031303182.md): Seat Track · corroded · Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT CABIN FLOOR 3RD SECTION OF SEAT TRACK IS CORRODED AT FS 449.85, 473.15, 513 AND 544 RBL 9. R & R RT CABIN FLOOR 3RD SECTION OF SEAT TRACK WITH A NEW SEAT TRACK IAW AMM 51-01-11-000-802 AND 51-01-11-400-802.
- [SDR ASOA2013031303181](https://openairdocs.org/sdr/ASOA2013031303181.md): Seat Track · corroded · Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT CABIN FLOOR 2ND SECTION OF SEAT TRACK IS CORRODED AT FS 394, 409+8 AND 409+86 RBL 9. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-020-002, FIG 401.B 1-3. LOCATED & DRILLED NEW SEAT TRACK IAW SRM 51-40-11-00. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-40
- [SDR ASOA2013031303180](https://openairdocs.org/sdr/ASOA2013031303180.md): Seat Track · corroded · Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT CABIN FLOOR FWD SEAT TRACK CORRODED AT FS 364 RBL 9. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-020-002, FIG 1B 1-3. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-420-001 FIG 401B 1-8.
- [SDR ASOA2013031303179](https://openairdocs.org/sdr/ASOA2013031303179.md): Seat Track · corroded · Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT CABIN FLOOR 3RD SECTION OF SEAT TRACK IS CORRODED AT FS 449.85, 473.15, 513 AND 544 LBL 9. REMOVED SEAT TRACK IAW AMM 53-01-11-000-801. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802. FABRICATED SEAT TRACK IAW REO 601R-53-00-485.
- [SDR ASOA2013031303178](https://openairdocs.org/sdr/ASOA2013031303178.md): Seat Track · corroded · Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT CABIN FLOOR 2ND SECTION OF SEAT TRACK IS CORRODED AT FS 394, 409+8 AND FS 409+16 LBL 9. REMOVED SEAT TRACK IAW AMM 53-01-11-000-801. LOCATED, DRILLED AND COUNTERSUNK NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED NEW SEAT TRACK IAW AMM 51-01-11-400-802.
- [SDR ASOA2013031303177](https://openairdocs.org/sdr/ASOA2013031303177.md): Seat Track · corroded · Feb 14, 2013 · N820AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT FWD SEAT TRACK IS CORRODED AT FS 364, LBL 9. R & R LT CABIN FLOOR FWD SEAT TRACK WITH A NEW SERVICEABLE RAIL IAW AMM 53-01-11-000-802 AND 53-01-11-400-802.
- [SDR ASOA2013031303176](https://openairdocs.org/sdr/ASOA2013031303176.md): Structure · cracked · Feb 13, 2013 · N820AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR AFT VERTICAL MEMBER CRACKED INSIDE OF DOOR AT LOWER AFT DOOR STOP FITTING. R & R AFT VERTICAL MEMBER IAW SRM 51-42-06.
- [SDR ASOA2013031303175](https://openairdocs.org/sdr/ASOA2013031303175.md): Skin · cracked · Feb 13, 2013 · N820AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR INNER SKIN CRACKED AT THE UPPER FWD STOP BRACKET. CUT AWAY DAMAGE TO CARGO DOOR INNER SKIN & CHANNEL WITH CAP ANGLE AT WL 97.25. NDT PERFORMED FOR CUT LINES, REFER TO FORM NDT-9. FABRICATED REPAIR PARTS, HEAT TREATED PARTS REQUIRED FROM TO CONDITI
- [SDR ASOA2013031303174](https://openairdocs.org/sdr/ASOA2013031303174.md): Light · failed · Feb 12, 2013 · N820AS · Cndair CL6002B19 · Emergency Lighting
  > SERVICE DOOR INNER HANDLE EXIT SIGN LIGHT FAILED FUNCTIONAL TEST. REMOVED LIGHT IAW AMM 33-51-09-000-802. INSTALLED SERVICEABLE LIGHT IAW AMM 33-51-09-400-802.
- [SDR ASOA2013031303173](https://openairdocs.org/sdr/ASOA2013031303173.md): Bulb · inoperative · Feb 11, 2013 · N820AS · Cndair CL6002B19 · Emergency Lighting
  > CABIN LIGHTING FAILED TESTS. R & R BULBS IAW AMM 33-21-01-000-801. OPS CHECKED GOOD IAW AMM 33-21-07-400-801.
- [SDR ASOA2013031303172](https://openairdocs.org/sdr/ASOA2013031303172.md): Light · failed · Feb 11, 2013 · N820AS · Cndair CL6002B19 · Emergency Lighting
  > FLOOR EMERGENCY LIGHTS FAILED. INSTALLED SERVICEABLE LIGHT IAW AMM 33-51-01-400-801.
- [SDR ASOA2012120402590](https://openairdocs.org/sdr/ASOA2012120402590.md): Handle · lack of lube · Nov 30, 2012 · N820AS · Cndair CL6002B19 · Passenger/Crew Doors
  > ON ARRIVAL TO ACFT FOUND MAIN CABIN DOOR OUTER HANDLE JAMMED CLOSED, MISALIGNED WITH RECESSED RECEPTICAL. HAD TO PRY HANDLE OUT TO OPEN DOOR DOES NOT APPEAR TO CLOSE PROPERLY. CLEANED AND LUBED PAX DOOR HANDLE AND PERFORMED OPS CHECKED IAW AMM 52-11-23.
- [SDR ASOA2012101802379](https://openairdocs.org/sdr/ASOA2012101802379.md): Door · lack of lube · Oct 16, 2012 · N820AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR STICKS AND IS REPORTED TO BE DIFFICULT TO OPEN AND CLOSE. LUBRICATED PAX DOOR IAW AMM 52-10-00. OPS CHECKED GOOD, REF 12-20-52.
- [SDR ASOA2012081002049](https://openairdocs.org/sdr/ASOA2012081002049.md): Valve · failed · Aug 6, 2012 · N820AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > "GEAR DISAGREE "MASTER WARNING COMPLIED WITH QRH CYCLED GEAR TOOK APPROX 60 SEC FOR GEAR TO COME UP RT MAIN WAS SLOW TO COME DOWN HDY 3 PRESSURE WAS 2700PSI. EMERGENCY DECLARED AS A PRECAUTION. R & R PRIORITY VALVE IAW AMM 32-32-15 IPC REF 32-32-10 ITEM 205
- [SDR ASOA201200980](https://openairdocs.org/sdr/ASOA201200980.md): Flap System · failed · Mar 20, 2012 · N820AS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL, 20 DEGREES, UPON SELECTING FLAPS 30 DEGREES SPEED 180 KTS. EMERGENCY DECLARED, COMPLIED WITH EC/TC AD 2009-06-12. NO FAULTS. OK FOR SERVICE
- [SDR ASOA201200498](https://openairdocs.org/sdr/ASOA201200498.md): Windshield · failed · Feb 14, 2012 · N820AS · Cndair CL6002B19 · Flight Compartment Windows
  > AT FL300 THE CAPTAINS WINDSHIELD BEGAN TO SPARK AND DELAMINATED RESULTING IN A CRACKED WINDSHIELD. FOLLOWED QRH, DIVERTED. R & R LT WINDSHIELD IAW AMM 56-11-01. LEAK AND OPS CHECKED GOOD.
- [SDR ASOA201102385](https://openairdocs.org/sdr/ASOA201102385.md): Circuit Breaker · tripped · Dec 19, 2011 · N820AS · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHTS TURN ON WHEN SWITCH IS TURNED TO ARM. FOUND CIRCUIT BREAKER OPEN, CLOSED CIRCUIT BREAKER, OPS CHECKED GOOD IAW AMM 33-51-00.
- [SDR ASOA201102090](https://openairdocs.org/sdr/ASOA201102090.md): Coalescer Bag · contaminated · Nov 1, 2011 · N820AS · Cndair CL6002B19 · Humidity Control System
  > ODOR IN CABIN ON GROUND AND IN FLIGHT. ODOR LIKE DIRTY SOCKS. OPS CHECK OF THE PACKS RT AND LT. OPS CHECKED GOOD, NO ODOR WITH REF TO AMM 21-51-00.
- [SDR ASOA201101943](https://openairdocs.org/sdr/ASOA201101943.md): Fcu · failed · Oct 11, 2011 · N820AS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL MESSAGE IN FLIGHT GOING FROM 0 TO 8 DEGREES. EMERGENCY DECLARED AS A PRECAUTION. R & R FECU IAW AMM 27-51-05. OPS CHECKED GOOD.
- [SDR ASOA201100581](https://openairdocs.org/sdr/ASOA201100581.md): Intercostal · cracked · Mar 16, 2011 · N820AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LWR FWD INTERCOSTAL IN DRAIN RAMP AREA IS CRACKED. REMOVED UNSERVICABLE LWR FWD INTERCOSTAL AND INSTALLED SERVICABLE INTERCOSTAL IAW SRM 51-42-06 AND SRM 51-42-21. PAX DOOR LWR INNER STRUCTURE. THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY.
- [SDR ASOA201100519](https://openairdocs.org/sdr/ASOA201100519.md): Attach Angle · corroded · Mar 16, 2011 · N820AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LWR ATTACH ANGLES (5 EA) ARE CORRODED. REMOVED PAX DOOR LWR ATTACH ANGLES. LOCATED AND INSTALLED NEW ATTACH ANGLES IAW SRM 51-42-06.
- [SDR ASOA201100497](https://openairdocs.org/sdr/ASOA201100497.md): Floor Support · corroded · Mar 16, 2011 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO BAY FLOOR CAP STRIP BETWEEN STR9L AND STR27L AND FS 589 IS CORRODED. REMOVED FLOORBEAM CAP AND REPLACED WITH NEW STRIP IAW SRM 51-42-06. MAJOR REPAIR.
- [SDR ASOA201100496](https://openairdocs.org/sdr/ASOA201100496.md): Floorbeam · cracked · Mar 16, 2011 · N820AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CARGO BAY FLOORBEAM CAP AT LBL9 OTBD FLANGE AT FS 589 IS CRACKED. REPAIRED FLOORBEAM IAW EC/TC REO 601R-53-61-4009 AND REO 601R-53-61-4009. MAJOR REPAIR.
- [SDR ASOA201100619](https://openairdocs.org/sdr/ASOA201100619.md): Sill · corroded · Mar 13, 2011 · N820AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL HAS CORROSION ACROSS SILL FROM FWD TO AFT FRAMES. REMOVED UNSERVICEABLE SERVICE DOOR SILL. INSTALLED SERVICEABLE DOOR SILL IAW SRM 51-42-21. THIS IS A MAJOR REPAIR SILL PLATE FOR THE SERVICE DOOR, FABRICATED AND INSTALLED IAW EO 600-53-0687
- [SDR ASOA201100580](https://openairdocs.org/sdr/ASOA201100580.md): Plate · corroded · Mar 13, 2011 · N820AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR SEAL PLATE IS CRACKED AT FS 589. R & R CARGO DOOR SEAL PLATE IAW SRM 51-42-06. THIS IS A MAJOR REPAIR. RII FOUND TO BE SATISFACTORY.

Next page: https://openairdocs.org/aircraft/N820AS/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 = 'N820AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N820AS/reports

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