# Service difficulty reports: N882AS, cancelled Mar 6, 2023

A list on [N882AS, cancelled Mar 6, 2023](https://openairdocs.org/deregistered/N882AS-2023-03-06.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 · 145 reports

- [SDR SWIA2019090646261](https://openairdocs.org/sdr/SWIA2019090646261.md): Strut · failed · Sep 5, 2019 · N882AS · Cndair CL6002B19 · Landing Gear Door Actuator
  > AFTER TAKE OFF RECEIVED GEAR DISAGREE ON LEFT MAIN, SHOWED RED BOX. COMPLIED WITH QRH, DIVERTED AND PROCEEDED WITH NORMAL LANDING, NO FURTHER INDICATIONS. (FLT#3765) FO: 09/06/2019 CLOSED REMOVED AND REPLACED RT MLG OUTER DOOR CLOSING STRUT ASSY IAW AMM. OPS C
- [SDR SWIA20190405668](https://openairdocs.org/sdr/SWIA20190405668.md): Selector Valve · failed · Mar 25, 2019 · N882AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON APPROACH RECEIVED THE NOSE DOOR AND GEAR DISAGREE WARNINGS. THE NOSE GEAR WAS NOT SHOWING DOWN AND GREEN. PER THE QRH, CYCLED THE GEAR, AND THEN PULLED THE LANDING GEAR MANUAL RELEASE HANDLE AND THE NOSE GEAR CAME DOWN AND LOCKED ALSO 3 GREEN
- [SDR SWIA2017050243255](https://openairdocs.org/sdr/SWIA2017050243255.md): Cargo Track · corroded · May 2, 2017 · N882AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO TRACK OTBD FLANGE IS CORRODED BS 574 - 589, LBL 9. REMOVED AND REPLACED THE CARGO TRACK IAW REO AND SRM.
- [SDR SWIA2017050243254](https://openairdocs.org/sdr/SWIA2017050243254.md): Bulkhead Web · cracked · May 2, 2017 · N882AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB HAS SIX CRACK INDICATIONS. REPAIRED THE BULKHEAD WEB IAW REO.
- [SDR SWIA2017050243253](https://openairdocs.org/sdr/SWIA2017050243253.md): Skin · cracked · May 2, 2017 · N882AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT NLG WHEEL WELL CUT OUT IS CRACKED, BS 235, LBL 6 AND RBL 6. REPAIRED IAW REO.
- [SDR SWIA2017050243252](https://openairdocs.org/sdr/SWIA2017050243252.md): Bulkhead Web · damaged · May 2, 2017 · N882AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 BULKHEAD WEB FAILED NDT INSPECTION AT LINTEL FITTING. REPAIRED THE BULKHEAD WEB IAW REO.
- [SDR SWIA2017050243251](https://openairdocs.org/sdr/SWIA2017050243251.md): Frame · corroded · May 2, 2017 · N882AS · Cndair CL6002B19 · Fuselage Main, Frame
  > AFT CARGO, BS 605 FRAME CORRODED BETWEEN STRINGERS 22 AND 24L. REMOVED AND REPLACED THE FRAME IAW SRM.
- [SDR SWIA2017050243250](https://openairdocs.org/sdr/SWIA2017050243250.md): Attach Fitting · corroded · May 2, 2017 · N882AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FLOORBEAM ATTACH FITTING AT BS 621, LBL 27 IS CORRODED ON THE INBD SIDE AND GOUGED ON TOP SIDE. REMOVED AND REPLACED THE ATTACH FITTING IAW REO.
- [SDR SWIA2017050243249](https://openairdocs.org/sdr/SWIA2017050243249.md): Attach Fitting · gouged · May 2, 2017 · N882AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FLOORBEAM ATTACH FITTING BS 621 BULKHEAD FORWARD SIDE, RBL 27 GOUGED. REMOVED AND REPLACED THE ATTACHMENT FITTING IAW REO.
- [SDR SWIA2017050243248](https://openairdocs.org/sdr/SWIA2017050243248.md): Cargo Track · corroded · May 2, 2017 · N882AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO TRACK OTBD FLANGE CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW SRM.
- [SDR SWIA2017050243247](https://openairdocs.org/sdr/SWIA2017050243247.md): Floorbeam · cracked · May 2, 2017 · N882AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 280 FLOORBEAM CRACKED LBL 9 AND RBL 9. REPAIRED IAW REO.
- [SDR SWIA2017050243246](https://openairdocs.org/sdr/SWIA2017050243246.md): Seat Track · buckled · May 2, 2017 · N882AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > INBD SEAT TRACK BUCKLED BETWEEN BS 589 AND 605, LBL 27. INSTALLED A NEW SEAT TRACK IAW SRM.
- [SDR SWIA2017050243244](https://openairdocs.org/sdr/SWIA2017050243244.md): Skin · damaged · May 2, 2017 · N882AS · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER WINGLET SKIN PANEL DAMAGED. REMOVED AND REPLACED RT WINGLET LOWER SKIN IAW SRM.
- [SDR SWIA2017050243243](https://openairdocs.org/sdr/SWIA2017050243243.md): Not Reported · damaged · May 2, 2017 · N882AS · Cndair CL6002B19 · Fuselage Structure (General)
  > DAMAGE AT FS 349.0 BETWEEN STR 19R AND 20R. REPAIRED IAW REO AND SRM.
- [SDR ASOA20160913008A](https://openairdocs.org/sdr/ASOA20160913008A.md): Dimmer · burned · Sep 13, 2016 · N882AS · Cndair CL6002B19 · Passenger Compartment Lighting
  > PILOT REPORTED BURNING ODOR TOWARD LAV AREA. MX REMOVED AND REPLACED THE POWER UNIT DIMMER ON ROW 11AB, 12AB, AND 14AB IAW AMM 33-21-04. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR ASOA2015032012440](https://openairdocs.org/sdr/ASOA2015032012440.md): Switch · shorted · Mar 19, 2015 · N882AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR VERY DIFFICULT TO OPEN. REQUIRED 2 PEOPLE TO OPEN. AFTER PUSHING IT APPROXIMATELY HALF WAY, IT FREE-FELL AS NORMAL. FOUND ASD POWER ASSIST SWITCH SHORTED CAUSING DOOR TO CLOSE BY ITSELF. REPLACED PANEL ASSY IAW AMM 33-22-00.
- [SDR ASOA2015010511998](https://openairdocs.org/sdr/ASOA2015010511998.md): Door · binding · Dec 30, 2014 · N882AS · Cndair CL6002B19 · Passenger/Crew Doors
  > UNABLE TO OPEN MAIN CABIN DOOR. FELT LIKE FORWARD ASSIST MECHANISM WAS STILL ENGAGED AND RESISTING OUR EFFORTS TO PUSH DOOR OPEN. DOOR OPENED BY ITSELF A FEW MINUTES LATER. PASSENGER DOOR POWER ASSIT SYSTEM: POWER ASSIST SUB-SYSTEM, MOTOR, CONTROL SWITCH, C
- [SDR ASOA2014122311922](https://openairdocs.org/sdr/ASOA2014122311922.md): Skin · gouged · Dec 4, 2014 · N882AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SEVERAL GOUGES FOUND ON FUSELAGE SKIN. BLENDED GOUGES IAW SRM 51-12-00 AND TR-51-31. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-31. REPAIRED IAW EA 25-2014-363. MAJOR REPAIR.
- [SDR ASOA2014121211882](https://openairdocs.org/sdr/ASOA2014121211882.md): Skin · gouged · Dec 2, 2014 · N882AS · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING LOWER WING ACCESS HOLE FOR ACCESS PANEL 650HB, JUST INBD OF WS 314.50 HAS SCRATCHES IN 2 PLACES REQUIRING ROTO PEENING. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH GREO 601R-57-21-030 AND EC/TC EO 600-57-81.
- [SDR ASOA2014121211881](https://openairdocs.org/sdr/ASOA2014121211881.md): Bulkhead · gouged · Dec 2, 2014 · N882AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD GOUGED RBL 27.50. REPAIRED IAW EC/TC REO 601R-53-61-2155.
- [SDR ASOA2014121211880](https://openairdocs.org/sdr/ASOA2014121211880.md): Bulkhead · gouged · Dec 2, 2014 · N882AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FWD FACE GOUGED LBL 18.00. REPAIRED IAW REO 601R-53-61-2155. MAJOR REPAIR.
- [SDR ASOA2014121211879](https://openairdocs.org/sdr/ASOA2014121211879.md): Bulkhead · gouged · Dec 2, 2014 · N882AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FWD FACE GOUGED AT LBL 36.2 JUST BELOW CARGO DOOR TRACK CROSS MEMBER. REPAIRED IAW REO 601R-53-61-2155.
- [SDR ASOA2014121211878](https://openairdocs.org/sdr/ASOA2014121211878.md): Attach Angle · cracked · Dec 2, 2014 · N882AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CARGO DOOR TRACK ATTACH ANGLE IS CRACKED AT BS 621. REMOVED AND REPLACED THE ATTACH ANGLE IAW IAW SRM 51-42-21.
- [SDR ASOA2014122311921](https://openairdocs.org/sdr/ASOA2014122311921.md): Angle · cracked · Nov 30, 2014 · N882AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE AT BS 625, S14L IS CRACKED, MORE THAN 1" INCH, AFT EQUIP BAY PRESSURE BULKHEAD. R & R THE ANGLE IAW SRM 51-42-21.
- [SDR ASOA2014121211877](https://openairdocs.org/sdr/ASOA2014121211877.md): Angle · cracked · Nov 30, 2014 · N882AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE AT BS 625, S14R IS CRACKED. R & R THE ANGLE IAW SRM 51-42-21.
- [SDR ASOA2014121211876](https://openairdocs.org/sdr/ASOA2014121211876.md): Attach Bracket · cracked · Nov 30, 2014 · N882AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FUSELAGE STRINGER TO BULKHEAD ATTCHE BRACKET CRACKED AT BS 280 STRINGER 3. REPAIRED IAW SRM 51-42-06-00, SRM 51-42-06-00 AND 51-21-11-00.
- [SDR ASOA2014121211875](https://openairdocs.org/sdr/ASOA2014121211875.md): Flap · gouged · Nov 30, 2014 · N882AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR ICE BREAKER CABLE GOUGING PRESSURE VENT FLAP DURING OPS. REPAIRED IAW REO 601R-52-11-1040.
- [SDR ASOA2014122311920](https://openairdocs.org/sdr/ASOA2014122311920.md): Mount · corroded · Nov 26, 2014 · N882AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > GALLEY FLOOR MOUNT PLATE INBD OF RBL 9.00 BETWEEN FS 295.00 AND FS 333.00 THE TOP PLATE IS CORRODED. BLENDED CORROSION & EVALUATED MOUNT PLATE & CAP PLATE. PARTS ARE OUT OF LIMITS IN REF TO SRM 51-21-06 & TR 53-27. THIS REPAIR IS CLASSIFIED AS A MAJOR REPA
- [SDR ASOA2014121211874](https://openairdocs.org/sdr/ASOA2014121211874.md): Frame · corroded · Nov 26, 2014 · N882AS · Cndair CL6002B19 · Fuselage Main, Frame
  > STUB FRAMES AT BS 349 CORRODED. REPAIRED IAW SRM 51-21-06-00.
- [SDR ASOA2014121211873](https://openairdocs.org/sdr/ASOA2014121211873.md): Seat Track · corroded · Nov 26, 2014 · N882AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 559 CORRODED. DETERMINED BEYOND LIMITS IAW SRM 53-21-49, PAGE BLOCK 101-199, FIGURE 101. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-01-11-000-802 & REO 601R-53-00-485.
- [SDR ASOA2014121211872](https://openairdocs.org/sdr/ASOA2014121211872.md): Floor Support · corroded · Nov 25, 2014 · N882AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON RT PRESSURE FLOOR SUPPORT BS 513. REPAIRED IAW SRM 51-21-06-00 & 51-42-21-00. MAJOR REPAIR.
- [SDR ASOA2014121211871](https://openairdocs.org/sdr/ASOA2014121211871.md): Floor Support · corroded · Nov 25, 2014 · N882AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON LT PRESSURE FLOOR SUPPORT BS 499 - 513. REPAIRED IAW SRM 51-21-06-00 & 51-42-21-00. MAJOR REPAIR.
- [SDR ASOA2014121211870](https://openairdocs.org/sdr/ASOA2014121211870.md): Door Sill · corroded · Nov 25, 2014 · N882AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL FWD CORNER AT BS 319.70 IS CORRODED. DETERMINED OUT OF LIMITS IAW SRM TR 53-27. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-21, 51-41-02, AND DWG 601R38338. MAJOR REPAIR.
- [SDR ASOA2014121211869](https://openairdocs.org/sdr/ASOA2014121211869.md): Floor Support · corroded · Nov 25, 2014 · N882AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BETWEEN BS 310 - 319.70 IS CORRODED. BLENDED AND FOUND OUT OF LIMITS IAW SRM 51-21-06-00. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06, 51-42-06, 51-42-20, AND 51-42-21.
- [SDR ASOA2014122311919](https://openairdocs.org/sdr/ASOA2014122311919.md): Door Frame · corroded · Nov 24, 2014 · N882AS · Cndair CL6002B19 · Fuselage Main, Structure
  > AVIONIC DOOR SURROUNDING FRAME AT BS 364 BETWEEN S24L - 24R CORRODED. BLENDED DAMAGE IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW SRM TR 53-33 53-00-31. REPAIRED IAW GREO 601R-53-21-676, REV B.
- [SDR ASOA2014122311918](https://openairdocs.org/sdr/ASOA2014122311918.md): Connector · broken · Nov 24, 2014 · N882AS · Cndair CL6002B19 · Light System Wiring
  > EMERGINCY LIGHT WIRE CONNECTOR BROKEN OFF FUSELAGE SIDE JUST FWD OF SERVICE DOOR. REPLACED EMERGENCY LIGHT WIRE CONNECTOR IAW ESPM 20-16-00. OPS TESTED THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. OPS TESTED GOOD.
- [SDR ASOA2014121211868](https://openairdocs.org/sdr/ASOA2014121211868.md): Hinge · gouged · Nov 24, 2014 · N882AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE HALF HAS TWO GOUGED LUGS AT NR 2 AND NR 18. REPAIRED IAW REO 601R-52-11-1347. MAJOR REPAIR.
- [SDR ASOA2014121211867](https://openairdocs.org/sdr/ASOA2014121211867.md): Isolator · broken · Nov 24, 2014 · N882AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FWD FACE HAS BROKEN ISOLATOR. R & R ISOLATOR IAW SRM 51-42-06.
- [SDR ASOA2014080811035](https://openairdocs.org/sdr/ASOA2014080811035.md): Light · unsecure · Aug 7, 2014 · N882AS · Cndair CL6002B19 · Emergency Lighting
  > PAX DOOR ENTRY FWD BULKHEAD EMERGENCY FLOOD LIGHT COVER & LIGHT BAR ARE UNSECURE. R & R PAX DOOR ENTRY FWD BULKHEAD FLOOR EMERGENCY FLOODLIGHT IAW AMM 33-51-19. OPS CHECK GOOD.
- [SDR ASOA2014061710674](https://openairdocs.org/sdr/ASOA2014061710674.md): Cover · missing · Jun 13, 2014 · N882AS · Cndair CL6002B19 · Emergency Lighting
  > FLOOR LIGHT COVER MISSING BY MAIN DOOR, LIGHT LENS/ COVERS, INCLUDING EMERGENCY LIGHT. REPLACED LIGHT COVER IAW AMM 33-51-10 DEFER CLEARED PLACARD REMOVED.
- [SDR ASOA2014013109819](https://openairdocs.org/sdr/ASOA2014013109819.md): Battery Pack · failed · Jan 27, 2014 · N882AS · Cndair CL6002B19 · Emergency Lighting
  > NR 1 INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-04, OPS CHECKED GOOD.
- [SDR ASOA2014011009741](https://openairdocs.org/sdr/ASOA2014011009741.md): Switch · dirty · Jan 6, 2014 · N882AS · Cndair CL6002B19 · Passenger/Crew Doors
  > F/A TRIED OPENING CABIN DOOR AT GATE AND WOULDN'T OPEN. F/O TRIED TO OPEN IT AND IT OPENED WITH DIFFICULTY. AFTER DOOR OPENED, IT STARTED TO RETRACT ON IT'S OWN. PULLED CIRCUIT BREAKERS. CLEANED POWER ASSIST SWICH. OPS CHECKED GOOD IAW AMM 52-60-00.
- [SDR ASOA2013061203821](https://openairdocs.org/sdr/ASOA2013061203821.md): Door · unknown · Jun 8, 2013 · N882AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WOULD NOT OPEN. ONCE IT OPENED, STARTED TO RETRACT UNCOMMANDED. PERFORMED OP'S TEST OF THE PASSENGER DOOR POWER ASSIST MOTOR IAW AMM 52-11-08. OP'S CHECKED GOOD.
- [SDR ASOA2013052203642](https://openairdocs.org/sdr/ASOA2013052203642.md): Light · shorted · May 17, 2013 · N882AS · Cndair CL6002B19 · Passenger Compartment Lighting
  > CLIMBING THRU 15K, BOTH THE F/O AND CAPT SMELLED HOT ELECTRICAL/ BURNING PLASTIC ODOR. DIVERTED, ONE OF THE GALLEY OVERHEAD LIGHTS HAD A SHORTED, CAUSING THE ODOR AS NOTED. R & R LIGHT ASSY IAW AMM 33-26-01. OPS CHECKED GOOD.
- [SDR ASOA2013032603256](https://openairdocs.org/sdr/ASOA2013032603256.md): Lamp · inoperative · Mar 22, 2013 · N882AS · Cndair CL6002B19 · Emergency Lighting
  > NR 1 CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP AND OPS CHECKED GOOD IAW AMM 33-51-010.
- [SDR ASOA2013021203009](https://openairdocs.org/sdr/ASOA2013021203009.md): Wire · chafed · Feb 1, 2013 · N882AS · Cndair CL6002B19 · Fuel System Wiring
  > WIRE FOR FUEL QTY PROBE IN PANEL 540BB HAS CHAFE DAMAGE, BECAUSE STANDOFF FOR CLAMP IS NOT LOCATED IN CORRECT POSITION. REPAIRED IAW REO 601R-20-12-111 AND REO 601R-57-21-1862, REV A.
- [SDR ASOA2013021203008](https://openairdocs.org/sdr/ASOA2013021203008.md): Bulkhead · damaged · Jan 28, 2013 · N882AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 409+128 PRESSURE BULKHEAD AT LBL 18 HAS TWO TOOLING MARKS, WORST IS APPROX 1.5" L X.125 W X.010 D. REPAIRED IAW REO 601R-53-41-1654.
- [SDR ASOA2013021203007](https://openairdocs.org/sdr/ASOA2013021203007.md): Web · chafed · Jan 26, 2013 · N882AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SKIN JUST FWD OF FS 559 INBD OF LBL 9 HAS THREE CHAFES WITHIN A 1 INCH AREA. DEEPEST APPROX.010 DEEP. REPAIRED IAW REO 601R-41-1655R.
- [SDR ASOA2013020702980](https://openairdocs.org/sdr/ASOA2013020702980.md): Floor Support · cracked · Jan 26, 2013 · N882AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 460 FLOOR SUPPORT FITTING OTBD OF RBL 9 CRACKED. REMOVED DAMAGED FLOOR SUPPORT FITTING AT FS 460 OTBD OF RBL 9 IAW SRM 51-42-21 & 51-42-06. LOCATED FASTENER HOLES ONTO NEW SERVICEABLE FLOOR FITTING IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE FLOOR SUPPO
- [SDR ASOA2013020702979](https://openairdocs.org/sdr/ASOA2013020702979.md): Floor Support · cracked · Jan 26, 2013 · N882AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484 FLOOR SUPPORT CLIP RBL 27 CRACKED. REMOVED CLIP AT FS 484.00, RBL 27, LOCATED DRILLED UP AND INSTALLED NEW CLIP PN 601R31171-9 IAW SRM 51-40-11 AND SRM 51-42-21.

Next page: https://openairdocs.org/deregistered/N882AS-2023-03-06/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 = 'N882AS' AND deregistration_id = 'N882AS-2023-03-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N882AS-2023-03-06/reports

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