# Service difficulty reports: N830AS, cancelled Jun 9, 2020

A list on [N830AS, cancelled Jun 9, 2020](https://openairdocs.org/deregistered/N830AS-2020-06-09.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 · 122 reports

- [SDR ASOA2015042412644](https://openairdocs.org/sdr/ASOA2015042412644.md): Door · binding · Apr 22, 2015 · N830AS · Cndair CL6002C10 · Passenger/Crew Doors
  > MAIN CABIN DOOR WILL NOT OPEN OR CLOSE. REMOVED FWD UPPER PANEL ON PAX DOOR. INSPECTED OUTTER HANDLE STOW MECH. NO DEFECTS NOTED. LUBED STOW MECH. IAW NMM 12-20-52. OPS CHECKED DOOR LATCH MECH. IAW AMM 52-11-03. OPS CHECK GOOD AT THIS TIME.
- [SDR ASOA2014091011202](https://openairdocs.org/sdr/ASOA2014091011202.md): Door · lack of lube · Sep 7, 2014 · N830AS · Cndair CL6002B19 · Passenger/Crew Doors
  > COULD NOT OPEN PAX DOOR FROM THE OUTSIDE, HAD TO GO IN THRU THE SERVICE DOOR AND OPEN THE DOOR FROM THE INSIDE. CLEANED AND LUBED PAX DOOR. PERFORMED OPS CK IAW AMM 52-11-00. NO DEFECTS NOTED.
- [SDR ASOA2014081411058](https://openairdocs.org/sdr/ASOA2014081411058.md): Pushrod · out of adjust · Aug 10, 2014 · N830AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR WONT OPEN EASILY. FOUND PUSHROD TO LATCH CAM TORQUE TUBE TO BE OUT OF ADJUSTMENT. ADJUSTED PUSHROD IAW AMM 52-11-21. OPS CHECKED GOOD IAW AMM 52-11-00.
- [SDR ASOA2014081311038](https://openairdocs.org/sdr/ASOA2014081311038.md): Door · lack of lube · Aug 9, 2014 · N830AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE AT GATE. CLEANED AND LUBED PAX DOOR IAW AMM 12-20-52. OPS CHECKED GOOD IAW AMM 52-11-00.
- [SDR ASOA2014050910471](https://openairdocs.org/sdr/ASOA2014050910471.md): Sign · inoperative · May 5, 2014 · N830AS · Cndair CL6002B19 · Emergency Lighting
  > LIGHTED FLOOR LEVEL EXIT SIGN INOPERATIVE AT LEFT EMERGENCY EXIT. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2014050210459](https://openairdocs.org/sdr/ASOA2014050210459.md): Light · inoperative · Apr 28, 2014 · N830AS · Cndair CL6002B19 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT NR 4 INOPERATIVE. R & R LIGHT ASSY IAW AMM 33-51-21. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2013121909664](https://openairdocs.org/sdr/ASOA2013121909664.md): Lens · missing · Dec 15, 2013 · N830AS · Cndair CL6002B19 · Emergency Lighting
  > NR 3 EMERGENCY CEILING LIGHT COVER MISSING. INSTALLED COVER IAW AMM 33-51-16. NO FURTHER DEFECT NOTED.
- [SDR ASOA2013120509592](https://openairdocs.org/sdr/ASOA2013120509592.md): Skin · cracked · Nov 19, 2013 · N830AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LT WING FUEL ACCESS PANEL 540EB HAS AN INDICATION ON THE INBD SIDE APPROX.5 X.25" 50 PERCENT FSH FAILED NDT INSPECITON. COMPLIED WITH ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV K.
- [SDR ASOA2013120509591](https://openairdocs.org/sdr/ASOA2013120509591.md): Skin · cracked · Nov 17, 2013 · N830AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER WING PLANK RT BOOST PUMP CUT OUT LANDING FOR ACCESS PANEL HAS MULTIPLE INDICATIONS NOTED ON HORIZONTAL AND VERTICAL SURFACES 50 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE FAILED NDT INSPECTION. REMOVED CORROSION IAW SRM 51-21-06.
- [SDR ASOA2013120509589](https://openairdocs.org/sdr/ASOA2013120509589.md): Bulkhead · cracked · Nov 15, 2013 · N830AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX.3" IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH ECTC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541 REV D, DATED: 10/31/2011.
- [SDR ASOA2013120509588](https://openairdocs.org/sdr/ASOA2013120509588.md): Lens · damaged · Nov 12, 2013 · N830AS · Cndair CL6002B19 · Emergency Lighting
  > LT CABIN EMERGENCY LIGHT SECTIONS FAIL INSPECTION. COVERS ARE CRACKED AND CRAZED AND LIGHTS ARE FADED. REMOVED DAMAGED SECTIONS AND INSTALLED SERVICEABLE IAW AMM 33-51-01-400-806.
- [SDR ASOA2013120509587](https://openairdocs.org/sdr/ASOA2013120509587.md): Light · damaged · Nov 12, 2013 · N830AS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT SECTIONS NR 1 AND 2 FAIL INSPECTION. LENS ARE CRACKED AND CRAZED AND LIGHT STRIPS ARE FADED AND DIM. REMOVED DAMAGED LIGHTS AND INSTALLED SERVICEABLE LIGHTS IAW AMM 33-51-01-400-806.
- [SDR ASOA2013120509586](https://openairdocs.org/sdr/ASOA2013120509586.md): Angle · cracked · Nov 12, 2013 · N830AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 625 ANGLE CRACKED. REMOVED ANGLE IAW SRM 51-42-21. LOCATED, DRILLED & INSTALLED NEW ANGLE IAW SRM 51-40-11 & 51-42-21.
- [SDR ASOA2013120509585](https://openairdocs.org/sdr/ASOA2013120509585.md): Intercostal · cracked · Nov 12, 2013 · N830AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAS BETWEEN STRINGERS 12A & 13A LT AT FS 625 ARE CRACKED. REMOVED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.
- [SDR ASOA2013120509584](https://openairdocs.org/sdr/ASOA2013120509584.md): Floorbeam · corroded · Nov 11, 2013 · N830AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FLOORBEAM AFT ANGLE IS CORRODED AROUND FASTENER HOLES FROM LBL 9 TO RBL 9. R & R ANGLE IAW REO 601R-53-11-926, REV B. COMPLIED WITH EC/TC REO 601R-53-11-926 IAW REO 601R-53-11-926, REV B.
- [SDR ASOA2013120509583](https://openairdocs.org/sdr/ASOA2013120509583.md): Seat Track · corroded · Nov 11, 2013 · N830AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BETWEEN BS 409 AND 409+128 HAS CORROSION AROUND FASTENERS. FABRICATED, DRILLED AND LOCATED NEW SEAT TRACK IAW REO 601R-53-00-485. REMOVED SEAT TRACK IAW SRM 51-41-02-00 AND INSTALLED IAW REO 601R-53-00-485.
- [SDR ASOA2013120509582](https://openairdocs.org/sdr/ASOA2013120509582.md): Seat Track · corroded · Nov 11, 2013 · N830AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK BETWEEN BS 409 AND 409+128 HAS CORROSION AROUND FASTENERS. FABRICATED NEW SEAT TRACK SECTION, LOCATED AND DRILLED PREPPED SURFACE AND TOP COATED IAW REO 601R-53-00-485. REMOVED SEAT TRACK IAW SRM 51-41-02-00 AND INSTALLED IAW REO 601R-53-00-485.
- [SDR ASOA2013120509581](https://openairdocs.org/sdr/ASOA2013120509581.md): Isolator · broken · Nov 11, 2013 · N830AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FORWARD FACE HAS BROKEN ISOLATORS. REMOVED BROKEN ISOLATORS IAW SRM 51-42-10 AND REPLACED IAW SRM 51-42-13.
- [SDR ASOA2013120509580](https://openairdocs.org/sdr/ASOA2013120509580.md): Seat Track · corroded · Nov 10, 2013 · N830AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 9 CORRODED FROM BS 364-394. REMOVED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR ASOA2013120509579](https://openairdocs.org/sdr/ASOA2013120509579.md): Floor Support · corroded · Nov 10, 2013 · N830AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER COMPARTMENT FLOOR SUPPORT CORRODED AT LBL 45 FROM BS 349-379. REMOVED FLOOR SUPPORT IAW SRM 51-42-66. LOCATED & DRILLED NEW FLOOR SUPPORT IAW 51-40-11.
- [SDR ASOA2013120509578](https://openairdocs.org/sdr/ASOA2013120509578.md): Floorbeam · corroded · Nov 10, 2013 · N830AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 280 FLOORBEAM FWD ANGLE CORRODED LBL 9 - RBL 9. REMOVED ANGLE IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06 & 51-42-21.
- [SDR ASOA2013120509577](https://openairdocs.org/sdr/ASOA2013120509577.md): Skin · corroded · Nov 10, 2013 · N830AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING SKIN ACCESS HOLE -640BB HAS AERAS OF CORROSION. COMPLIED WITH ECTC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV K.
- [SDR ASOA2013120509576](https://openairdocs.org/sdr/ASOA2013120509576.md): Handle · out of adjust · Nov 10, 2013 · N830AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HANDLE IS DIFFICULT TO OPEN FROM OUTSIDE, INNER DOOR PLUNGER IS TOUGH TO CLOSE, PAX DOOR LATCH CAUTION MESSAGE IN FLIGHT. ADJUSTED THE PULL-IN LEVER TORQUE TUBE PUSH ROD & THE LATCH CAM TORQUE TUBE PUSH ROD IAW AMM 52-11-21-820-802, SUBTASK 52-11-21-
- [SDR ASOA2013120509575](https://openairdocs.org/sdr/ASOA2013120509575.md): Floorbeam · cracked · Nov 10, 2013 · N830AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 280, FLOORBEAM ANGLE HAS THREE CRACKS AT LBL 9 - RBL 9. REMOVED FLOORBEAM ANGLES IAW SRM 51-42-21. REPLACED DURING INCORPORATION OF REO 601R-53-11-926.
- [SDR ASOA2013120509574](https://openairdocs.org/sdr/ASOA2013120509574.md): Floor Support · cracked · Nov 10, 2013 · N830AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 484 FLOOR SUPPORT PREVIOUS REPAIR ANGLE IS CRACKED, AT RBL 36.00. REMOVED & INSTALLED NEW ANGLE IAW 51-42-21 AND REO 601R-53-41-059. FABRICATED ANGLE IAW REO 601R-53-41-059, FROM S6144-14.
- [SDR ASOA2013120509573](https://openairdocs.org/sdr/ASOA2013120509573.md): Skin · chafed · Nov 8, 2013 · N830AS · Cndair CL6002B19 · Ailerons
  > LEFT AILERON UPPER L/E IS CHAFED IN SEVERAL AREAS, ALL ALONG L/E SURFACE. DEEPEST CHAFE APPROX.005 DEEP. COMPLIED WITH STEPS NR 1 THRU NR 3 OF REO 601R-57-60-013, REV NC AND COMPLIED WITH EC/TC REO 601R-57-60-013 IAW REO 601R-57-60-013.
- [SDR ASOA2013120509572](https://openairdocs.org/sdr/ASOA2013120509572.md): Skin · cracked · Nov 4, 2013 · N830AS · Cndair CL6002B19 · Wing, Plate/Skin
  > .8 INCH CRACK IN RT WING LOWER WING PLANK. COMPLIED WITH EC/TC REO 601R-57-21-130 01 AND REO 601R-57-21-130, REV J. COMPLIED WITH EC/TC REO 601R-57-21-131 AND REO 601R-57-21-131, REV A.
- [SDR ASOA2013102909270](https://openairdocs.org/sdr/ASOA2013102909270.md): Handle · stiff · Oct 25, 2013 · N830AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR HANDLE IS DIFFICULT TO OPEN FROM OUTSIDE. IT IS ALSO DIFFICULT TO STOW THE HANDLE INSIDE AT TIMES. DID FIT AND CLEARANCE CHECK OF DOOR HANDLE, OPS CHECK GOOD IAW AMM 52-11-03.
- [SDR ASOA2013072408768](https://openairdocs.org/sdr/ASOA2013072408768.md): Handle · lack of lube · Jul 22, 2013 · N830AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR WONT OPEN FROM OUTSIDE. PERFORMED OPS TEST OF PAX DOOR SEVERAL TIMES, AND LUBED PAX DOOR HANDLE INNER MECHANISM. OPS GOOD IAW AMM 52-11-00 ACFT OK FOR SERVICE.
- [SDR ASOA2013061403823](https://openairdocs.org/sdr/ASOA2013061403823.md): Door · binding · Jun 10, 2013 · N830AS · Cndair CL6002B19 · Passenger/Crew Doors
  > CREW REPORTS THAT THE PASSENGER DOOR IS DIFFICULT TO OPEN. REMOVED EXCESS AMOUNT OF GREASE FROM PASSENGER DOOR LOCKPINS AND CAMLOCKS IAW AMM 12-20-52. NO FURTHER DEFECTS NOTED.
- [SDR ASOA2013032603255](https://openairdocs.org/sdr/ASOA2013032603255.md): Latch · lack of lube · Mar 22, 2013 · N830AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LATCH HARD TO CLOSE OR OPEN. LUBRICATED PASSENGER DOOR HANDLE LATCH. OPS CHECKED OK MM 52-10-00.
- [SDR ASOA2013012402902](https://openairdocs.org/sdr/ASOA2013012402902.md): Lens · broken · Jan 21, 2013 · N830AS · Cndair CL6002B19 · Emergency Lighting
  > R & R THE LT SIDE ABOVE WING EMERGENCY LIGHT HOUSING BROKEN. R & R THE LT SIDE EMERGENCY LIGHT COVER IAW AMM 33-51-21. OPS CHECK GOOD. CDL CLEARED. MCC NOTIFIED.
- [SDR ASOA2013012402901](https://openairdocs.org/sdr/ASOA2013012402901.md): Lens · broken · Jan 21, 2013 · N830AS · Cndair CL6002B19 · Emergency Lighting
  > LEFT SIDE AFT ABOVE WING EMERGENCY LIGHT HSG BROKEN. R & R THE LT SIDE EMERGENCY LIGHT COVER IAW AMM 33-51-21. OPS CHECK GOOD. CDL CLEARED. MCC NOTIFIED.
- [SDR ASOA2013012402900](https://openairdocs.org/sdr/ASOA2013012402900.md): Lens · broken · Jan 21, 2013 · N830AS · Cndair CL6002B19 · Emergency Lighting
  > RIGHT SIDE ABOVE WING EMERGENCY LIGHT HSG BROKEN. R & R THE RT SIDE EMERGENCY LIGHT COVER IAW AMM 33-51-21. OPS CHECK GOOD. CDL CLEARED. MCC NOTIFIED.
- [SDR ASOA2012062101816](https://openairdocs.org/sdr/ASOA2012062101816.md): Tire · failed · Jun 17, 2012 · N830AS · Cndair CL6002B19 · Tire
  > RIGHT NOSE TIRE BLEW AT V1 (ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION). PERFORMED VISUAL INSP OF NLG AND DOORS IAW AMM-32-20-00. NO DEFECTS NOTED AT THIS TIME. R & R RT AND LT NOSEWHEEL AND TIRE ASSY IAW AMM-32-42-01. (SD
- [SDR ASOA201201643](https://openairdocs.org/sdr/ASOA201201643.md): Fixture · burned · May 4, 2012 · N830AS · Cndair CL6002B19 · Passenger Compartment Lighting
  > BURNING ODOR IN COCKPIT AND GALLEY AREA. (WORK LIGHTS) R & R BURNED GALLEY LIGHT FIXTURE. OPS CHECKED GOOD IAW AMM 33-26-047.
- [SDR ASOA201102335](https://openairdocs.org/sdr/ASOA201102335.md): Apu · smoke · Dec 8, 2011 · N830AS · Cndair CL6002B19 · APU Core Engine
  > AFTER APU SHUTDOWN, THERE WAS A LARGE AMOUNT SMOKE COMING FROM APU EXHAUST AREA AUXILIARY POWER UNIT APU. DOOR POSITION VERIFIED CLOSED. R & R APU ASSEMBLY IAW AMM 49-10-00. OPS AND LEAK CHECKED GOOD.
- [SDR ASOA201102243](https://openairdocs.org/sdr/ASOA201102243.md): Housing · broken · Nov 25, 2011 · N830AS · Cndair CL6002B19 · Emergency Lighting
  > WARDROBE AFT EMERGENCY LIGHT HOUSING BROKEN. R & R FLOOR LEVER EMERGENCY FLOOD LIGHT HOUSING ON WARDROBE IAW AMM 33-51-19-000-801 & 33-51-19-400-801. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.
- [SDR ASOA201102225](https://openairdocs.org/sdr/ASOA201102225.md): Angle · corroded · Nov 21, 2011 · N830AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR THRESHOLD ANGLE CORRODED. REMOVED SILL ANGLE IAW SRM 51-42-21. SILL ANGLE AND INSTALLED IAW SRM 51-40-11 AND SRM 51-42-21.
- [SDR ASOA201102197](https://openairdocs.org/sdr/ASOA201102197.md): Crossbeam · corroded · Nov 16, 2011 · N830AS · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION ON CROSSBEAM AT 349 AND RBL 41 TO RBL 42. REPAIRED IAW SRM 51-24-06 AND REO 601R-53-21-2224.
- [SDR ASOA201102248](https://openairdocs.org/sdr/ASOA201102248.md): Bracket · cracked · Nov 14, 2011 · N830AS · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD RAIL SUPPORT BOTTOM BRACKET CRACKED. REMOVED CARGO DOOR FWD RAIL SUPPORT BRACKET FOR REPLACEMENT IAW SRM 51-41-02 & SRM 51-42-06. DRILLED NEW SUPPORT BRACKET IAW SRM 51-40-11 & ALODINED HOLES IAW SRM 51-21-11. INSTALLED NEW BRACKET ONTO CARGO
- [SDR ASOA201102247](https://openairdocs.org/sdr/ASOA201102247.md): Stand Off · cracked · Nov 14, 2011 · N830AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO COMPARTMENT AFT BULKHEAD STAND OFF BRACKET CRACKED RT PRESSURE BULKHEAD 1ST FROM FLOOR. REMOVED AND INSTALLED NEW STAND OFF MOUNT IAW SRM 51-77-00, 51-42-13.
- [SDR ASOA201102179](https://openairdocs.org/sdr/ASOA201102179.md): Bulkhead · cracked · Nov 14, 2011 · N830AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT EQUIPMENT BAY, PRESSURE BULKHEAD RT CLIP CRACKED AT FS 625.
- [SDR ASOA201102246](https://openairdocs.org/sdr/ASOA201102246.md): Stand Off · cracked · Nov 10, 2011 · N830AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO COMPARTMENT AFT BULKHEAD STAND OFF BRACKET CRACKED RT PRESSURE BULKHEAD 1ST FROM FLOOR. REMOVED AND INSTALLED NEW STAND OFF MOUNT IAW SRM 51-77-00, 51-42-13.
- [SDR ASOA201102245](https://openairdocs.org/sdr/ASOA201102245.md): Threshold · corroded · Nov 10, 2011 · N830AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR THRESHOLD CORRODED. REMOVED CORROSION IAW SRM 51-21-06. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REPAIRED IAW SRM 51-42-21 AND 51-42-06.
- [SDR ASOA201102165](https://openairdocs.org/sdr/ASOA201102165.md): Structure · cracked · Nov 10, 2011 · N830AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT EQUIPMENT BAY, PRESSURE BULKHEAD RT CLIP CRACKED AT FS 625. R & R FWD CARGO DOOR INNER SEAL RETAINER IAW SRM 51-40-11-001-001 AND SRM 51-41-02-001-001.
- [SDR ASOA201102152](https://openairdocs.org/sdr/ASOA201102152.md): Floorbeam · corroded · Nov 10, 2011 · N830AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT FS 349. RBL 41 TO RBL 42. REPAIRED IAW REO 601R-53-21-2224, STEP 1 & 2.
- [SDR ASOA201102151](https://openairdocs.org/sdr/ASOA201102151.md): Cargo Track · corroded · Nov 10, 2011 · N830AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRORED AT FS 559.00 + 80 AND LBL 27. REMOVED CARGO TRACK IAW AMM 53-01-11-000-802. INSTALLED CARGO TRACK IAW AMM 20-21-00-910-801.
- [SDR ASOA201102150](https://openairdocs.org/sdr/ASOA201102150.md): Cargo Track · corroded · Nov 10, 2011 · N830AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRORED AT 559.00 + 80 AND LBL 9. REMOVED CARGO TRACK IAW AMM 53-01-11-000-802. INSTALLED CARGO TRACK IAW AMM 20-21-00-910-801.
- [SDR ASOA201102149](https://openairdocs.org/sdr/ASOA201102149.md): Cargo Track · corroded · Nov 10, 2011 · N830AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK CORRORED AT 559.00 + 80 AND RBL 9. REMOVED CARGO TRACK IAW AMM 53-01-11-000-802. INSTALLED CARGO TRACK IAW AMM 20-21-00-910-801. REPLACE DAMAGED SEAT TRACK.

Next page: https://openairdocs.org/deregistered/N830AS-2020-06-09/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 = 'N830AS' AND deregistration_id = 'N830AS-2020-06-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N830AS-2020-06-09/reports

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