# Service difficulty reports: N879AS

A list on [N879AS](https://openairdocs.org/aircraft/N879AS.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 6 · 292 reports

- [SDR SWIA2019122747318](https://openairdocs.org/sdr/SWIA2019122747318.md): Reveal · broken · Dec 18, 2019 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CABIN INNER LINER PANEL 261ALW INNER WINDOW REVEAL SLIDE ATTACHMENT POINT IS BROKEN AND DETACHED (C-CHECK) RO:12/24/2019REPLACED CABIN INNER LINER PANEL 261ALW INNER WINDOW REVEAL IAW ZODIAC AEROSPACE CMM.
- [SDR SWIA2019122747353](https://openairdocs.org/sdr/SWIA2019122747353.md): Skin · eroded · Dec 14, 2019 · N879AS · Cndair CL6002B19 · Ailerons
  > RH AILERON UPPER SKINN SURFACE ABOVE N0. 2 AND NO. 3 HINGE BOLTS IS PEELED BACK AWAY FROM THE AILERON BETWEEM WS 317.85 AND WS 321.32 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED DAMAGED AILERON SKIN IAW CRJ 200 SRM AND TASK CARD. NO WEIGHT CHANGE REQUI
- [SDR SWIA2019122747352](https://openairdocs.org/sdr/SWIA2019122747352.md): Attach Fitting · cracked · Dec 12, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK CONDITION FOUND IN THE AREA OF THE REPAIR REF 601R-53-61-1230 FS 621 BULKHEAD LINTEL AREA. 1' LONG IN THE RADIUS OF THE CLEAT ATTACHED TO LINTEL FITTING AND A SHEARED FASTNER ALSO COMMON TO FS 625.30 AND LINTEL FITTING (C-CHECK) RO:12/24/2019REP
- [SDR SWIA2019122747326](https://openairdocs.org/sdr/SWIA2019122747326.md): Stringer · corroded · Dec 8, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FOUND STR 27 TO BE CORRODED BETWEEN FS 333 AND FS349 REPAIRED STR 27 AT FS 333- 349 IAW SRM.
- [SDR SWIA2019122747325](https://openairdocs.org/sdr/SWIA2019122747325.md): Buttstrap · corroded · Dec 6, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Structure
  > BUTTSTRAP AT FS 333 IS CORRODED IN SEVERAL LOCATIONS BETWEEN STRINGER 24L AND 24R COMPLIED WITH MAJOR REPAIR OF BUTTSTRAP AT F.S. 333 IAW REO AND SKYWEST TASK CARD MAJOR REPAIR FORM 337 ATTACHED. 1.2 LBS REMOVED 1.8 LBS ADDED FOR A +.7 LBS ADDED
- [SDR SWIA2019122747243](https://openairdocs.org/sdr/SWIA2019122747243.md): Support Bracket · cracked · Dec 4, 2019 · N879AS · Cndair CL6002B19 · Wing, Attach Fittings
  > RIGHT WING ANTI-ICE DUCT SUPPORT BRACKET UNDER LEADING EDGE PANEL 630AZ WAS CRACKED. REMOVED AND REPLACED DUCT SUPPORT BRACKET IAW AMM.
- [SDR SWIA2019122747242](https://openairdocs.org/sdr/SWIA2019122747242.md): Bracket · cracked · Dec 3, 2019 · N879AS · Cndair CL6002B19 · Wing, Attach Fittings
  > LEFT WING ANTI-ICE DUCT SUPPORT BRACKET UNDER LEADING EDGE PANEL 520DZ WAS CRACKED. REMOVED AND REPLACED THE DUCT BRACKET IAW AMM.
- [SDR SWIA2019122747299](https://openairdocs.org/sdr/SWIA2019122747299.md): Floorbeam · corroded · Dec 2, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FOUND PITTING CORROSION ON EDGE OF LBL/RBL 27 FLOOR BEAM CAPS AT FS 424. (C-CHECK) RO:12/24/2019BLENDED COROSION IAW CRJ-200-REO FOUND TO BE OUT OF LIMITS, DISPOSITION FOR CORROSION BLENDS FOUND ON REO, COMPLIED WITH ALL REQUIRED STEPS.
- [SDR SWIA2019122747241](https://openairdocs.org/sdr/SWIA2019122747241.md): Stiffener · cracked · Nov 22, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > F.S. 621 BULKHEAD LOWER AFT STIFFENER O/B OF LBL 36 IS CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM.
- [SDR SWIA2019122747240](https://openairdocs.org/sdr/SWIA2019122747240.md): Cascade · cracked · Nov 22, 2019 · N879AS · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT ENGINE THRUST REVERSER CASCADE AT THE 12 O'CLOCK POSITION WAS CRACKED. REMOVED AND REPLACED THE LT ENGINE THRUST REVERSER IAW AMM.
- [SDR SWIA2019122747345](https://openairdocs.org/sdr/SWIA2019122747345.md): Angle · corroded · Nov 18, 2019 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH FS621.0 TO FS625 UPPER INTERCOSTAL ANGLE AT BL 45, STRINGER 14R, WL 97.5 IS CRACKED APPROX 0.3" LONG. (C-CHECK) RO:12/24/2019REMOVED AND REPLACED INTERCOSTAL P/N 601-35012-52 WITH SERVICEABLE INTERCOSTAL IAW CRJ200 SRM.
- [SDR SWIA2019122747341](https://openairdocs.org/sdr/SWIA2019122747341.md): Frame · corroded · Nov 17, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS333.00 CORRODED IN SEVERAL LOCATION BETWEEN STGR24R AND STGR24L AND BETWEEN STGR20L TO STGR21L. COMPLIED WITH MAJOR REPAIR UPON FURTHER INVESTIGATION FOUND FRAME BETWEEN STRINGER 24R AND 24L TO BE CORRODED AT FS 319.70 AND CORRODED AT FS 333 BET
- [SDR SWIA2019122747329](https://openairdocs.org/sdr/SWIA2019122747329.md): Floor Support · corroded · Nov 17, 2019 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH FLOOR SILL CORRODED BETWEEN FS409.00 AND 409.00+112. REPAIRED CORRODED AREAS AS REQUIRED COMMON TO LH FLOOR SILL FROM FS409.00 TO FS409+112 IAW REO
- [SDR SWIA2019122747328](https://openairdocs.org/sdr/SWIA2019122747328.md): Floor Support · corroded · Nov 17, 2019 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH CABIN FLOOR SILL CORRODED FROM FS409 TO FS409.00+112. REPAIRED CORRODED AREAS AS REQUIRED COMMON TO RH FLOOR SILL FROM FS409.00 TO FS 409+112 IAW REO ALL STEPS COMPLETE.
- [SDR SWIA2019122747327](https://openairdocs.org/sdr/SWIA2019122747327.md): Floor Support · corroded · Nov 17, 2019 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH CABIN FLOOR SILL CORRODED FROM FS349.00 TO FS409.0 ALONG RBL 42. REMOVED CORROSION FROM CABIN FLOOR RBL42 AT FS349 TO FS409 IAW REO.
- [SDR SWIA2019122747323](https://openairdocs.org/sdr/SWIA2019122747323.md): Angle · corroded · Nov 17, 2019 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH CAP ANGLE CORRODED BETWEEN FS409.00 AND 409.00+112 AT LBL 9.00 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED CORRODED CAP ANGLE WITH NEWLY FABRICATED CAP ANGLE AT LBL9 BETWENN FS409 AND FS409+112 IAW CRJ200 SRM DRAWING. TASK CARD ISSUED, M-337 COMPLETE
- [SDR SWIA2019122747322](https://openairdocs.org/sdr/SWIA2019122747322.md): Angle · corroded · Nov 17, 2019 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT CAP ANGLE CORRODED BETWEEN FS409.00 AND 409.00+112 AT RBL 9.00 REMOVED AND REPLACED CORRODED CAP ANGLE WITH NEWLY FABRICATED CAP ANGLE AT RBL9 BETWEEN FS409 AND FS409+112 IAW SRM AND DRAWING.
- [SDR SWIA2019122747316](https://openairdocs.org/sdr/SWIA2019122747316.md): Floor Support · out of limits · Nov 17, 2019 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H CABIN FLOOR SILL PANEL AT F.S.424.00 IS OUT OF LIMITS OF REO 601R-53--41-666 FOUND REMAINING THICKNESS TO BE WITHIN LIMITS PER REO.
- [SDR SWIA2019122747354](https://openairdocs.org/sdr/SWIA2019122747354.md): Plate · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Passenger/Crew Doors
  > FWD PAX DOOR SERATED PLATE IS CORRODED. REPLACED FWD PAX DOOR SERATED PLATE IAW AMM.
- [SDR SWIA2019122747351](https://openairdocs.org/sdr/SWIA2019122747351.md): Bracket · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT LOWER FRAME BRACKET CORRODED AT BS 349 AND STRINGER 18R. CORROSION WAS FOUND ON THE DOUBLER AFTER REMOVING THE RT LOWER FRAME BRACKET AT BS 349 AND STRINGER 18R IAW SRM. DOUBLER WAS REPAIRED IAW SRM.FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM AND LO
- [SDR SWIA2019122747350](https://openairdocs.org/sdr/SWIA2019122747350.md): Frame Splice · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AND SPLICE CORRODED AT FS 621.00 BETWEEN STR 26R AND STR 26L. (C-CHECK) RO:12/24/2019REPAIRED CORROSION DAMAGE FRAME SPLICE AT F.S. 621 BY BLENDING IAW CRJ200 SRM AND FOUND TO BE WITHIN LIMITS IAW CRJ200 SRM.
- [SDR SWIA2019122747349](https://openairdocs.org/sdr/SWIA2019122747349.md): Frame · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS 559.00+112 CORRODED BETWEEN STGR25. REMOVED CORROSION AND REPLACED SPLICE ANGLE IAW SRM.
- [SDR SWIA2019122747348](https://openairdocs.org/sdr/SWIA2019122747348.md): Frame · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS 605.00 CORRODED BETWEEN STGR16R AND STGR17R. (C-CHECK) RO:12/24/2019BLENDED CORROSION ON F.S.605 FRAME AT STGR 17R - 16R IAW CRJ200 SRM, FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW CRJ200 SRM. ORIGINAL FRAME THICKNESS 0.050" MATERIAL R
- [SDR SWIA2019122747344](https://openairdocs.org/sdr/SWIA2019122747344.md): Frame · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS 605.00 CORRODED BETWEEN APPROX STGR 25R AND STGR 24L. REPAIRED FRAME AT FS 605 IAW SRM
- [SDR SWIA2019122747342](https://openairdocs.org/sdr/SWIA2019122747342.md): Anchor Fitting · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT ANCHOR FITTING IS CORRODED AROUND BOLT HOLES. REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING IAW AMM.
- [SDR SWIA2019122747339](https://openairdocs.org/sdr/SWIA2019122747339.md): Seat Track · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT TRACK CORRODED FROM APPRX FS409+126 TO FS559+8.00 AT RBL9 (C-CHECK) RO:12/24/2019REMOVED, FABRICATED AND INSTALLED R/H FLOOR SEAT TRACK FROM FS409+126 TO FS559+8.00 AT RBL9 IAW BOMBARDIER REO.
- [SDR SWIA2019122747338](https://openairdocs.org/sdr/SWIA2019122747338.md): Bracket · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RH LOWER FRAME BRACKET CORRODED AT FS 319.70 AND STRG18R. REMOVED AND REPLACED R/H LOWER FRAME BRACKET IAW SRM.
- [SDR SWIA2019122747336](https://openairdocs.org/sdr/SWIA2019122747336.md): Strap · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR TENSION STRAPS CORRODED ON UPPER SURFACE AT FS 424.00 LBL 27.0 TO LBL 36.0 AND RBL 27.0 TO RBL 36.0 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED PRESSURE FLOOR TENSION STRAPS AT F.S. 424.00 LBL/RBL 27 TO 36 IAW CRJ 200 SRM.
- [SDR SWIA2019122747335](https://openairdocs.org/sdr/SWIA2019122747335.md): Plate · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Passenger/Crew Doors
  > AFT PAX DOOR SERRATED PLATE IS CORRODED ON THE AFT SIDE. (C-CHECK) RO:12/24/2019REMOVED AND REPLACED AFT PAX DOOR SERRATED PLATE IAW AMM.
- [SDR SWIA2019122747334](https://openairdocs.org/sdr/SWIA2019122747334.md): Floor Support · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH CABIN FLOOR SILL UPPER SURFACE LBL 36.0 TO LBL 45.0 FS 409+128 TO FS 559.00 HAS AREAS OF CORROSION. COMPLIED WITH MAJOR REPAIR FLOOR-SILL UPPER SURFACE CORROSION AT LBL 36.0 TO LBL 45.0, BETWEEN FS. 409+128 TO 559.00 IAW REO AND TASK CARD MAJOR REPAIR.
- [SDR SWIA2019122747332](https://openairdocs.org/sdr/SWIA2019122747332.md): Anchor Fitting · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Passenger/Crew Doors
  > FWD PAX DOOR ANCHOR FITTING IS CORRODED AROUND BOLT HOLES. REPLACED FWD PAX DOOR ANCHOR FITTING IAW AMM.
- [SDR SWIA2019122747331](https://openairdocs.org/sdr/SWIA2019122747331.md): Floor Support · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT CABIN FLOOR SILL UPPER SURFACE RBL36.0 TO RBL 45.0 FS 409+128 TO FS 559.00 HAS AREAS OF CORROSION. REMOVED CORROSION ON R/H PRESSURE FLOOR SILL PANEL FROM FS409+128 TO FS 559 IAW REO DISPOSITION 1.1 AND 1.2..055 ORIGINAL THKNESS -.008 =.047 REMAINING
- [SDR SWIA2019122747330](https://openairdocs.org/sdr/SWIA2019122747330.md): Frame · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS 589.00 CORRODED BETWEEN APPROX STGR 26R AND STGR 25L. REMOVED AND REPLACED FRAME SECTOR AT F.S. 589.00 BETWEEN STR 26R AND STR 25L IAW SRM COMPLIED WITHMAJOR REPAIR TASK CARD MAJOR REPAIR.
- [SDR SWIA2019122747324](https://openairdocs.org/sdr/SWIA2019122747324.md): Frame · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME STRAP AT FS621.00 CORRODED BETWEEN APRROX STGR26R AND STGR26L. REPAIRED CORROSION DAMAGE ON F.S.621 FRAME STRAP BETWEEN STGR25L AND 25R IAW BOMBARDIER REO.
- [SDR SWIA2019122747321](https://openairdocs.org/sdr/SWIA2019122747321.md): Intercostal · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL BETWEEN STGR 17L TO 16L AT F.S. 310 IS CORRODED. REMOVED&REPLACED PAX DOOR INTERCOSTAL AT STR16 BETWEEN F.S. 295-F.S.310L IAW CRJ 200 SRM COMPLETED AND FORM 337 ATTACHED PART FOR PART REPLACEMENT NO WT CHANGE
- [SDR SWIA2019122747315](https://openairdocs.org/sdr/SWIA2019122747315.md): Anchor Fitting · cracked · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Passenger/Crew Doors
  > FWD PAX DOOR ANCHOR FITTING IS CRACKED ON THE FWD SIDE. (C-CHECK) RO:12/24/2019REMOVED AND REPLACED FWD PAX DOOR ANCHOR FITTING IS CRACKED ON THE FWD SIDE. IAW AMM.
- [SDR SWIA2019122747298](https://openairdocs.org/sdr/SWIA2019122747298.md): Strap · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR TENSION STRAP SMALL AREA OF CORROSION ON UPPER SURFACE FS 559.00 BETWEEN BL 0.0 AND LBL9.0. BLENDED CORROSION ON PRESSURE FLOOR STRAP AT FS599.0 BETWEEN BL0.0 TO LBL9.0 IAW SRM ORIGINAL THICKNESS.063" REMOVED.005" LEAVING.058".
- [SDR SWIA2019122747293](https://openairdocs.org/sdr/SWIA2019122747293.md): Seat Track · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT TRACK CORRODED FROM APPRX FS559+8.00 TO FS559+91.00 AT LBL9 (C-CHECK) RO:12/24/2019REPLACED L/H FLOOR SEAT TRACK IAW BOMBARDIER REO.
- [SDR SWIA2019122747292](https://openairdocs.org/sdr/SWIA2019122747292.md): Seat Track · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT TRACK CORRODED FROM APPRX FS559+8.00 TO FS559+91.00 AT RBL9 (C-CHECK) RO:12/24/2019REPLACED R/H FLOOR SEAT TRACK IAW BOMBARDIER REO.
- [SDR SWIA2019122747289](https://openairdocs.org/sdr/SWIA2019122747289.md): Seat Track · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT TRACK CORRODED FROM APPRX FS409+126 TO FS559+8.00 AT LBL9 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED LH FLOOR SEAT TRACK FROM FS409+126 TO FS559+8 AT LBL9 IAW BOMBARDIER REO.
- [SDR SWIA2019122747288](https://openairdocs.org/sdr/SWIA2019122747288.md): Seat Track · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT TRACK CORRODED FROM APPRX FS399 TO FS409+126 AT RBL9 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED RH SEAT TRACK AT FS399 TO FS409+126 RBL IAW CRJ-200 AMM.
- [SDR SWIA2019122747287](https://openairdocs.org/sdr/SWIA2019122747287.md): Seat Track · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT TRACK CORRODED FROM APPRX FS399 TO FS409+126 AT LBL9 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED LH SEAT TRACK FROM FS399 TO FS409+126 AT LBL9 IAW CRJ-200 AMM.
- [SDR SWIA2019122747285](https://openairdocs.org/sdr/SWIA2019122747285.md): Seat Track · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT TRACK CORRODED FROM APPRX FS364 TO FS409 AT LBL9 (C-CHECK) RO:12/24/2019REMOVED AND REPLACEDL/H FLOOR SEAT TRACK FROM FS364 TO FS409 IAW CRJ200 AMM.
- [SDR SWIA2019122747284](https://openairdocs.org/sdr/SWIA2019122747284.md): Seat Track · corroded · Nov 16, 2019 · N879AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT TRACK CORRODED FROM APPRX FS364 TO FS409 AT RBL9 (C-CHECK) RO:12/24/2019REMOVED AND REPLACED R/H FLOOR SEAT TRACK FROM FS364 TO FS409 IAW CRJ200 AMM.
- [SDR SWIA2019122747311](https://openairdocs.org/sdr/SWIA2019122747311.md): Handle · chafed · Nov 15, 2019 · N879AS · Cndair CL6002B19 · Galley Doors
  > SERVICE DOOR INNER HANDLE CHAFED. (C-CHECK) RO:12/24/2019REPAIRED AREA IAW CRJ 200 SRM REFERENCE CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA2019122747310](https://openairdocs.org/sdr/SWIA2019122747310.md): Cap · dented · Nov 15, 2019 · N879AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD AND AFT UPPER CORNER CAPS DENTED AND FASTENER CHAFED. COMPLIED WITH REO. REF CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA2019122747309](https://openairdocs.org/sdr/SWIA2019122747309.md): Plate · chafed · Nov 15, 2019 · N879AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD CENTERING PLATE CHAFED. REMOVED CHAFE DAMAGE. MAX DEPTH OF DAMAGE MEASURED AT,015" FOUND TO BE WITHIN LIMITS IAW REO.
- [SDR SWIA2019122747308](https://openairdocs.org/sdr/SWIA2019122747308.md): Flap · chafed · Nov 15, 2019 · N879AS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR PRESSURE VALVE FLAP CHAFED BY ICE BREAK CABLE. (C-CHECK) RO:12/24/2019REPAIRED PAX DOOR PRESSURE VALVE FLAP IAW REO.
- [SDR SWIA2019122747296](https://openairdocs.org/sdr/SWIA2019122747296.md): Retainer · corroded · Nov 15, 2019 · N879AS · Cndair CL6002B19 · Passenger/Crew Doors
  > UPPER RH CORNER OF PAX DOOR SEAL RETAINER HAS AREA OF CORROSION (C-CHECK) RO:12/24/2019REMOVED AND REPLACED RH CORNER OF PAX DOOR SEAL RETAINER IAW CRJ-200 SRM & SRM REO
- [SDR SWIA2019122747297](https://openairdocs.org/sdr/SWIA2019122747297.md): Frame · corroded · Nov 14, 2019 · N879AS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS 349.00 CORRODED BETWEEN STGR25R AND STGR25L. REMOVED AND REPLACED FRAME AT FS 349 IAW CRJ200 SRM AND TASK CARD.

Next page: https://openairdocs.org/aircraft/N879AS/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 = 'N879AS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N879AS/reports

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