# Service difficulty reports: N866AS, cancelled Jul 30, 2023

A list on [N866AS, cancelled Jul 30, 2023](https://openairdocs.org/deregistered/N866AS-2023-07-30.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 · 165 reports

- [SDR SWIA2019111246758](https://openairdocs.org/sdr/SWIA2019111246758.md): Pressure Switch · failed · Nov 12, 2019 · N866AS · Cndair CL6002B19 · Fuel Pressure Indicator
  > ABORTED TAKE OFF. LOW FUEL PRESSURE CAUTION MSG. FLT OR GROUND SPOILER MASTER CAUTION WARNING. BRAKE TEMPS LEFT 3/2 RIGHT 3/2. BELOW 80 KIAS. FLIGHT # 5037 CLOSED FOR THE LOW FUEL PRESSURE CAUTION MSG. MXC CONFIRMED WITH THE CREW THAT IT WAS A LH LOW FUEL P
- [SDR SWIA2018111345262](https://openairdocs.org/sdr/SWIA2018111345262.md): Frame · corroded · Oct 20, 2018 · N866AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FS589.00, STGR27 AND STGR26R €“ FRAME SHOWS SIGNS OF CORROSION ON THE FWD SIDE. (C-CHECK) RO: 11/12/2018REPLACED CORRODED FRAME SECTION AT FS 589.00 @STGR 20L IAW REO. PRESSURE LEAK CHECK GOOD.
- [SDR SWIA2018111345258](https://openairdocs.org/sdr/SWIA2018111345258.md): Bulkhead Web · cracked · Oct 20, 2018 · N866AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS.280.00 LOWER WEB HAS CRACKS AT LBL9 AND RBL9. (C-CHECK) RO: 11/12/2018 COMPLIED WITH REPAIR OF THE FS280 BULKHEAD WEB. PERFORMED ALL STEPS IAW REO.
- [SDR SWIA2018111345261](https://openairdocs.org/sdr/SWIA2018111345261.md): Stringer · cracked · Oct 18, 2018 · N866AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > CLIP ON THE UPPER SIDE OF STGR3L, FS282.00 IS CRACKED. (C-CHECK) RO: 11/12/2018 REMOVED AND INSTALLED NEW CLIP ON THE UPPER SIDE OF STGR3L, FS282.00. IAW SRM. PRESSURE LEAK CHECK GOOD.
- [SDR SWIA2018111345260](https://openairdocs.org/sdr/SWIA2018111345260.md): Doubler · corroded · Oct 18, 2018 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON DOUBLER FOR THE PASSENGER DOOR LOWER SILL FS349.00. (C-CHECK) RO: 11/12/2018 REMOVED CORROSION FROM DOUBLER LOCATED UNDER FLOOR SILL JUST AFT OF PAX DOOR CUTOUT IAW SRM.
- [SDR SWIA2018111345259](https://openairdocs.org/sdr/SWIA2018111345259.md): Skin · dented · Oct 15, 2018 · N866AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT IN FUSELAGE SKIN AT FS639.00 JUST BELOW STGR2R. (C-CHECK) RO: 11/12/2018 DRESSED BACK DENT IN FUSELAGE SKIN AT FS639.00 JUST BELOW STGR2R IAW REO.
- [SDR SWIA201844132](https://openairdocs.org/sdr/SWIA201844132.md): Bracket · failed · Jan 10, 2018 · N866AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > GEAR DISAGREE NOSE GEAR WOULD NOT RETRACT. (FLT#2944) CLOSED REMOVED AND REPLACED BRACKET IAW AMM. SWUNG GEAR OPS GOOD.
- [SDR SWIA201744067](https://openairdocs.org/sdr/SWIA201744067.md): Bracket · damaged · Dec 14, 2017 · N866AS · Cndair CL6002B19 · Nose/Tail Landing Gear
  > NOSE GEAR DISAGREE. REMOVED AND REPLACED THE NR 2 WOW AND CENTERED HARNESS ASSY IAW AMM. OPS CHECKED GOOD. REMOVED AND REPLACED CENTERING SENSOR BRACKET IAW CMM. OPS CHECKED GOOD.
- [SDR SWIA201743582](https://openairdocs.org/sdr/SWIA201743582.md): Control Unit · failed · Jul 31, 2017 · N866AS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL, RETURNED TO THE FIELD. EMERGENCY DECLARED. REPLACED THE FLAP LEVER AND FECU. AND RERIGGED THE RIGHT BPSU. SYSTEM OP CHECKS GOOD.
- [SDR SWIA201743256](https://openairdocs.org/sdr/SWIA201743256.md): Carbon Seal · leaking · May 1, 2017 · N866AS · Cndair CL6002B19 · Turbine Engine Oil System
  > SMOKE IN THE COCKPIT AND A SMOKE CARGO WARNING MESSAGE. DIVERTED. REMOVED AND REPLACED THE NR 1 CARBON SEAL. LEAK CHECKED AND OIL CONSUMPTION CHECKED GOOD.
- [SDR SWIA2017050243256](https://openairdocs.org/sdr/SWIA2017050243256.md): Unknown · smoke · May 1, 2017 · N866AS · Cndair CL6002B19 · Air Distribution System
  > SMOKE IN COCKPIT AND SMOKE CARGO WARNING MESSAGE, DIVERTED. OPEN.
- [SDR SWIA201642833](https://openairdocs.org/sdr/SWIA201642833.md): Panel · chafed · Oct 22, 2016 · N866AS · Cndair CL6002B19 · Wing, Plate/Skin
  > PANEL 684BB CHAFED ON FWD EDGE. REPAIRED IAW EA.
- [SDR SWIA201642831](https://openairdocs.org/sdr/SWIA201642831.md): Plate · cracked · Oct 22, 2016 · N866AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CARGO SKIN PROTECTIVE PLATE HAS CRACKS AROUND FASTENER HOLES. ( LOCATED & DRILLED HOLES ON NEW CARGO PROTECTIVE PLATE IAW SRM.
- [SDR SWIA201642832](https://openairdocs.org/sdr/SWIA201642832.md): Skin · worn · Oct 21, 2016 · N866AS · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > RIGHT NACELLE CORE COWL HAS WEAR AT LATCH AREA CAUSED BY BLOCKER DOOR. FABRICATED AND INSTALLED REPAIR PLATE IAW CMM. BLENDED NR 6 BLOCKER DOOR TO OBTAIN THE CORRECT CLEARENCE IAW CMM, CLEARANCE CHECKED GOOD.
- [SDR SWIA201541442](https://openairdocs.org/sdr/SWIA201541442.md): Landing Gear · malfunctioned · Sep 25, 2015 · N866AS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE MESSAGE WITH WOW MESSAGE. RETURNED TO DEPARTURE. SERVICED NLG, BLED SYSTEM. OPS CHECKED GOOD.
- [SDR SWIA201541008](https://openairdocs.org/sdr/SWIA201541008.md): Warning Message · false activation · Apr 7, 2015 · N866AS · Cndair CL6002B19 · Engine Thrust Reverser
  > "RT REV UNLOCKED" CAUTION MSG IN FLIGHT. COMPLIED WITH QRH PROCEDURE ON EMER1-16, LANDED NEAREST SUITABLE AIRPORT. TROUBLESHOT RIGHT THRUST REVERSER UNLOCK MESSAGE DURING FLIGHT IN REFERENCE TO FIM, CHECK FOR GROUND ONTHROTTLE LOCKOUT GEARBOX SOLENOID, NO D
- [SDR SWIA201439820](https://openairdocs.org/sdr/SWIA201439820.md): Tube · damaged · Nov 5, 2014 · N866AS · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR CONVOLEX DAMAGED. C-CHECK, R & R CONVOLEX TUBING WITH NEW, IAW REO.
- [SDR SWIA201439879](https://openairdocs.org/sdr/SWIA201439879.md): Piccolo Tube · chafed · Oct 31, 2014 · N866AS · Cndair CL6002B19 · Wing Main, Frame Structure
  > LEFT WING OTBD PICCOLO TUBE HAS CHAFING FROM L/E RIB BETWEEN 530JZ AND 530KZ. C-CHECK, REPAIRED CHAFE ON OTBD PICCOLO TUBE IAW STS EA.
- [SDR SWIA201439878](https://openairdocs.org/sdr/SWIA201439878.md): Piccolo Tube · damaged · Oct 31, 2014 · N866AS · Cndair CL6002B19 · Wing Main, Frame Structure
  > LT WING OTBD PICCOLO TUBE HAS DRILL START 38.5" FROM OTBD EDGE. C-CHECK, CLEANED AND WELDED DRILL START IAW STS EA.
- [SDR SWIA201439877](https://openairdocs.org/sdr/SWIA201439877.md): Piccolo Tube · dented · Oct 31, 2014 · N866AS · Cndair CL6002B19 · Wing Main, Frame Structure
  > LT WING OTBD PICCOLO TUBE HAS A DENT 38.5" FROM OTBD EDGE. C-CHECK, REPAIRED DENT IN OTBD PICCOLO TUBE IAW STS EA.
- [SDR SWIA201439876](https://openairdocs.org/sdr/SWIA201439876.md): Piccolo Tube · gouged · Oct 31, 2014 · N866AS · Cndair CL6002B19 · Wing Main, Frame Structure
  > LEFT WING OTBD PICCOLO TUBE HAS GOUGE NEAR WELD AT INBD FLANGE. C-CHECK, REPAIRED GOUGE ON INBD FLANGE IAW STS EA.
- [SDR SWIA201439875](https://openairdocs.org/sdr/SWIA201439875.md): Skin · gouged · Oct 23, 2014 · N866AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, LOWER FORWARD AREA, RT LOWER DME ANTENNA FOOT PRINT HAS A MINOR GOUGE. C-CHECK, REPAIRED LWR FUSELAGE BETWEEN FS 409.0+48 & 409.00+64, S25R-S26R IAW STS EA.
- [SDR SWIA201439874](https://openairdocs.org/sdr/SWIA201439874.md): Skin · gouged · Oct 23, 2014 · N866AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ON FUSELAGE SKIN LOWER FORWARD AREA, LT LOWER DME ANTENNA FOOT PRINTS HAS MINOR GOUGES 2 LOCATIONS. C-CHECK, REPAIRED LWR FUSELAGE BETWEEN FS 409.0+48 & 409.00+64, S25L-S26L IAW STS EA.
- [SDR SWIA201439873](https://openairdocs.org/sdr/SWIA201439873.md): Skin · nicked · Oct 23, 2014 · N866AS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FWD LOWER CORNER OF PAX DOOR CUT OUT HAS NICKS. C-CHECK, BLENDED FWD LOWER CORNER FUSELAGE SKIN AT PAX DOOR CUT OUT TO A SMOOTH FINISH, IAW STS EA.
- [SDR SWIA201439872](https://openairdocs.org/sdr/SWIA201439872.md): Hinge · gouged · Oct 22, 2014 · N866AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR MOUNTED PIANO HINGE HALF HAS WEAR GROOVES AND GOUGES ON LUGS 12 LOCATIONS SEEN WITH DOOR OPENED AND CLOSED. BLENDED DAMAGED AREA TO A SMOOTH FINISH, IAW REO.
- [SDR SWIA201439871](https://openairdocs.org/sdr/SWIA201439871.md): Hinge · gouged · Oct 22, 2014 · N866AS · Cndair CL6002B19 · Fuselage, Door Hinge
  > FUSELAGE MOUNTED PAX DOOR PIANO HINGE HALF HAS A GOUGE ON LUG, 6TH FROM AFT END. C-CHECK, BLENDED DAMAGED AREA TO A SMOOTH FINISH, IAW REO.
- [SDR SWIA201439870](https://openairdocs.org/sdr/SWIA201439870.md): Floor Support · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS529.00, RBL 47. C-CHECK, CORROSION ON RT FLOOR ANGLE AT FS 529.00, RBL 47, WAS BLENDED IAW REO.
- [SDR SWIA201439869](https://openairdocs.org/sdr/SWIA201439869.md): Floor Support · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 499 TO 513, RBL 47. C-CHECK, CORROSION ON RT FLOOR ANGLE AT FS 499 TO FS 513, RBL 47, WAS BLENDED IAW REO.
- [SDR SWIA201439868](https://openairdocs.org/sdr/SWIA201439868.md): Floor Support · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 473.15 RBL 47. REMOVED CORROSION BY BLENDING IAW REO.
- [SDR SWIA201439867](https://openairdocs.org/sdr/SWIA201439867.md): Floor Support · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 461, RBL 47. BLENDED OUT CORROSION IAW REO.
- [SDR SWIA201439866](https://openairdocs.org/sdr/SWIA201439866.md): Floor Support · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS449.85, RBL 47. C-CHECK CORROSION ON RIGHT FLOOR ANGLE AT FS 449.85, RBL 47, WAS BLENDED IAW REO.
- [SDR SWIA201439865](https://openairdocs.org/sdr/SWIA201439865.md): Floor Support · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FUSELAGE FLOOR ANGLE HAS CORROSION AT FS 544, LBL47. C-CHECK, BLENDED CORROSION IAW REO.
- [SDR SWIA201439864](https://openairdocs.org/sdr/SWIA201439864.md): Floor Support · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FUSELAGE FLOOR ANGLE HAS CORROSION AT AFT SIDE OF FS 513. C-CHECK, CORROSION ON LEFT FLOOR ANGLE AFT OF FS 513 WAS BLENDED IAW REO.
- [SDR SWIA201439863](https://openairdocs.org/sdr/SWIA201439863.md): Floor Support · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR ANGLE HAS CORROSION AT FS499 TO 513 LBL47. C-CHECK, CORROSION ON LT FLOOR ANGLE FS 499-FS 513 AT LBL 47 WAS BLENDED IAW REO.
- [SDR SWIA201439862](https://openairdocs.org/sdr/SWIA201439862.md): Floor Support · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FUSELAGE FLOOR ANGLE CORRODED AT FS461, LBL 47. C-CHECK, REMOVED CORROSION ON LT FUSELAGE FLOOR ANGLE AT FS 461, LBL47 IAW REO.
- [SDR SWIA201439861](https://openairdocs.org/sdr/SWIA201439861.md): Floor Support · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FUSELAGE FLOOR ANGLE CORRODED AT BS 449.85, LBL 47. REMOVED CORROSION BY BLENDING IAW REO.
- [SDR SWIA201439840](https://openairdocs.org/sdr/SWIA201439840.md): Seat Track · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FUSELAGE SEAT TRACK CORRODED AT BS 559+112 LBL 9. REPLACED THE SEAT TRACK IAW REO.
- [SDR SWIA201439839](https://openairdocs.org/sdr/SWIA201439839.md): Seat Track · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT FUSELAGE SEAT TRACK CORRODED BS 559+80 - 559+96. R & R THE SEAT TRACK SECTION IAW REO.
- [SDR SWIA201439838](https://openairdocs.org/sdr/SWIA201439838.md): Seat Track · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FUSELAGE SEAT TRACK CORRODED AT BS 559+80 - 559+96 LBL 9. R & R THE SEAT TRACK SECTION IAW REO.
- [SDR SWIA201439837](https://openairdocs.org/sdr/SWIA201439837.md): Seat Track · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FUSELAGE SEAT TRACK CORRODED AT BS 612 - 617 LBL 9. R & R THE SEAT TRACK SECTION, IAW REO AND SRM.
- [SDR SWIA201439836](https://openairdocs.org/sdr/SWIA201439836.md): Floor Support · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FUSELAGE FLOOR SUPPORT IS CORRODED AROUND NUTPLATE HOLE BS 605 - 621. REMOVED CORROSION IAW REO.
- [SDR SWIA201439835](https://openairdocs.org/sdr/SWIA201439835.md): Floor Support · corroded · Oct 20, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT BS 559+80 - 559+112 IS CORRODED. CORROSION WAS BLENDED AND FOUND WITHIN LIMITS IAW REO AND SRM.
- [SDR SWIA201439834](https://openairdocs.org/sdr/SWIA201439834.md): Line · cracked · Oct 20, 2014 · N866AS · Cndair CL6002B19 · APU Engine Fuel and Control
  > APU FUEL LINE HAS A CRACKED WELD AT SUPPORT BRACKET INSIDE PRESSURE BOX. C-CHECK, REINFORCED FUEL LINES FUEL PRESSURE BOX IAW REO.
- [SDR SWIA201439833](https://openairdocs.org/sdr/SWIA201439833.md): Attach Angle · gouged · Oct 19, 2014 · N866AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFT CARGO FLOORBEAM ATTACHMENT TO THE BS 621 PRESSURE BULKHEAD AT LBL27 HAS GOUGE. C-CHECK, REPAIRED AFT CARGO FLOOR RAIL FITTING ON FS 621 LBL 27.00 IAW REO.
- [SDR SWIA201439832](https://openairdocs.org/sdr/SWIA201439832.md): Angle · cracked · Oct 19, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 484, RBL 36, OTBD CLIP IS CRACKED. C-CHECK, INSTALLED REPAIR ANGLE IAW REO.
- [SDR SWIA201439860](https://openairdocs.org/sdr/SWIA201439860.md): Link · chafed · Oct 18, 2014 · N866AS · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT ENGINE BLOCKER BLOCKER DOOR LINKS HAVE CHAFE DAMAGE AT FORWARD END. REPAIRED DAMAGE ON LT ENG BLOCKER DOOR LINKS IAW REO.
- [SDR SWIA201439831](https://openairdocs.org/sdr/SWIA201439831.md): Post · cracked · Oct 18, 2014 · N866AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL POST AT FS 409+128, RBL 18 OBD SIDE IS CRACKED. C-CHECK R & R THE VERTICAL POST AT FS409+128, RBL18 OTBD IAW REO.
- [SDR SWIA201439830](https://openairdocs.org/sdr/SWIA201439830.md): Bulkhead Web · cracked · Oct 18, 2014 · N866AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK NOTED ON FS 621 BULKHEAD WEB, FWD FACE, ALONG HEEL LINE AT RBL27.5, APPROXIMATELY WL90. C-CHECK, INSTALLED ALL REPAIR PARTS IAW REO.
- [SDR SWIA201439829](https://openairdocs.org/sdr/SWIA201439829.md): Skin · chafed · Oct 18, 2014 · N866AS · Cndair CL6002B19 · Ailerons
  > RT AILERON UPPER SKIN SHROUD CHAFED IN 2 LOCATION, BOTH SIDES OF OTBD HINGE. C-CHECK, BLENDED RT AILERON UPPER SKIN SHROUD IN 2EA LOCATIONS, BOTH SIDES OF OTBD HINGE IAW REO.
- [SDR SWIA201439828](https://openairdocs.org/sdr/SWIA201439828.md): Skin · chafed · Oct 18, 2014 · N866AS · Cndair CL6002B19 · Ailerons
  > LEFT AILERON UPPER SKIN SHROUD CHAFED IN 2 LOCATION, INBD OF INBD HINGE AND OTBD OF CENTER HINGE. C-CHECK, BLENDED THE LT AILERON UPPER SKIN SHROUD, 2EA, CHAFES, INBD OF INBD HINGE AND OT OTBD CENTER HINGE IAW REO.

Next page: https://openairdocs.org/deregistered/N866AS-2023-07-30/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 = 'N866AS' AND deregistration_id = 'N866AS-2023-07-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N866AS-2023-07-30/reports

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