# Service difficulty reports: N779CA, cancelled Nov 30, 2022

A list on [N779CA, cancelled Nov 30, 2022](https://openairdocs.org/deregistered/N779CA-2022-11-30.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 3 · 132 reports

- [SDR SWIA2020042350275](https://openairdocs.org/sdr/SWIA2020042350275.md): Floorbeam · out of limits · Apr 9, 2020 · N779CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > THE FLOOR BEAM CAP IS OUT OF LIMITS AT FS409+102 RBL9 (C-CHECK) RO 4/21/2020 REPAIRED FLOOR BEAM CAP AT FS 409+102 RBL 9.0. REF: CRJ-200 SRM AND REO.
- [SDR SWIA2020042350274](https://openairdocs.org/sdr/SWIA2020042350274.md): Floorbeam · out of limits · Apr 9, 2020 · N779CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > THE FLOOR BEAM CAP IS OUT OF LIMITS AT FS409+10 RBL9 (C-CHECK) RO 4/21/2020 REMOVED OUT OF LIMITS FLOOR BEAM CAP AT FS 409+10 RBL9 AND REPLACED IT WITH A NEW FLOOR BEAM CAP REF. BOMBARDIER REO, AND CRJ 200 SRM. COMPLIED WITH TASK CARD. SEE CONTINUATION FO
- [SDR SWIA2020042350273](https://openairdocs.org/sdr/SWIA2020042350273.md): Floorbeam · out of limits · Apr 9, 2020 · N779CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > THE FLOOR BEAM CAP IS OUT OF LIMITS AT FS409+98 LBL9 (C-CHECK) RO 4/21/2020 REPAIRED FLOOR BEAM CAP AT FS 409+98 LBL9 REF CRJ 200 SRM. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR DETAILS.
- [SDR SWIA2020042350278](https://openairdocs.org/sdr/SWIA2020042350278.md): Seat Track · corroded · Apr 7, 2020 · N779CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * THE SEAT TRACK AT LBL9.00 HAS CORROSION AT FS409.00+16. (MARKED) (C-CHECK) RO 4/21/2020 REMOVED AND INSTALLED NEW SEAT TRACK AT LBL9.00 AT FS409.00+16. REF. CRJ 200 AMM
- [SDR SWIA2020042350277](https://openairdocs.org/sdr/SWIA2020042350277.md): Stand Off · corroded · Apr 7, 2020 · N779CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * THE LH FLOOR SILL HAS 3EA STANDSOFFS THAT HAVE CORROSION BETWEEN FS409.00+64 TO FS409.00+80. (MARKED) (C-CHECK) RO 4/21/2020 REMOVED AND INSTALLED 3EA. NEW STANDOFFS AT LH FLOOR SILL FS 409.00+64 TO FS 409.00+80 REF. CRJ 200 SRM. SEE. CONTINUATION FOR D
- [SDR SWIA2020042350271](https://openairdocs.org/sdr/SWIA2020042350271.md): Floor Support · corroded · Apr 7, 2020 · N779CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FS 589-605 FLOOR BEAM CAP LBL 9 HAS CORROSION AROUND SCREW HOLES (C-CHECK) RO 4/21/2020 UPON FURTHER INVESTIGATION FOUND THE MARKED DAMAGE TO BE AT LOCATION FS586-FS605 LBL9. REPAIR FLOOR BEAM CAP. BLENDED OUT CORROSION AROUND SCREW HOLES ON THE FLOORBE
- [SDR SWIA2020042350270](https://openairdocs.org/sdr/SWIA2020042350270.md): Door Sill · corroded · Apr 7, 2020 · N779CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FLOOR EDGE MEMBER FS 559+80- 574 LBL 37 HAS CORROSION AROUND SCREW HOLES (C-CHECK) RO 4/21/2020 --BLENDED CORROSION FROM THE FLOOR EDGE MEMBER FS559+80 LBL37 "OUT OF LIMITS" REF BOMBARDIER REO.--REMOVED AND REPLACED FLOOR EDGE MEMBER FS559+80 - FS574 LBL3
- [SDR SWIA2020042350269](https://openairdocs.org/sdr/SWIA2020042350269.md): Structure · corroded · Apr 7, 2020 · N779CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FLOOR EDGE MEMBER FS 559+16- 559+112 LBL 37 HAS CORROSION AROUND SCREW HOLES (C-CHECK) RO 4/21/2020 --BLENDED CORROSION ON THE FLOOR EDGE MEMNER FS559+16 - FS559+112 LBL37 "OUT OF LIMITS" REF BOMBARDIER REO. --REMOVED AND REPLACED FLOOR EDGE MEMBER FS559
- [SDR SWIA2020042350268](https://openairdocs.org/sdr/SWIA2020042350268.md): Strap · corroded · Apr 7, 2020 · N779CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FLOOR STRAP AT FS 559 RBL 27-37 CORRODED (C-CHECK) RO 4/21/2020 REMOVED FLOOR STRAP AT FS 559 RBL 27-37 DUE TO BEING OUT OF LIMITS. INSTALLED NEW STRAP AT FS 559 RBL 27-37 REF. BOMBARDIER DWG AND CRJ 200 SRM. COMPLIED WITH ST
- [SDR SWIA2020042350267](https://openairdocs.org/sdr/SWIA2020042350267.md): Skin · worn · Apr 3, 2020 · N779CA · Cndair CL6002B19 · Wing, Plate/Skin
  > *LH WING LOWER PLANK FUEL ACCESS HOLE 540BB HAS PITTING OUTBD LANDING AREA (MARKED) (C-CHECK) RO 4/21/2020 COMPLIED WITH REPAIR LH WING LOWER PLANK FUEL ACCESS HOLE 540BB REF BOMBARDIER REO, COMPLIED WITH ST, CHECKS GOOD.
- [SDR SWIA2020042350276](https://openairdocs.org/sdr/SWIA2020042350276.md): Bracket · cracked · Apr 2, 2020 · N779CA · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR LINTEL BEAM AFT SIDE HAS A CRACKED BRACKET. ( MARKED). (C-CHECK) RO 4/21/2020 INSTALLED NEW REPLACEMENT CARGO DOOR LINTEL AFT BRACKET P/N 601R35050-109 AT FS.621 BULKHEAD WEB LBL.36 AS PER CRJ200 SRM, LEAK CHECKS GOOD
- [SDR SWIA2020042350266](https://openairdocs.org/sdr/SWIA2020042350266.md): Post · cracked · Apr 2, 2020 · N779CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CRACKS AT FS409+128 VERTICAL POST BL0.0 RH/LH AFT ANGLE. (MARKED) (C-CHECK) RO 4/21/2020 REMOVED AND REPLACED THE FS409+128 BL0 VERTICAL POST REF BOMBARDIER REO, CRJ200 SRM. COMPLIED WITH ST. LEAK CHECKS GOOD.
- [SDR SWIA2020032350265](https://openairdocs.org/sdr/SWIA2020032350265.md): Bulkhead · chafed · Apr 2, 2020 · N779CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > THE FS621.00 BULKHEAD HAS MULTIPLE CHAFES AT LBL9, LBL18, LBL27, LBL36, RBL9, RBL18, RBL27 AND RBL36. (MARKED). (C-CHECK) RO 4/21/2020 COMPLIED WITH PERMANENT REPAIR 621 BULKHEAD CHAFES REF REO, VERIFIED ALL APPLICABLE STEPS COMPLIED WITH, COMPLETED TASK
- [SDR SWIA2020042350264](https://openairdocs.org/sdr/SWIA2020042350264.md): Vane · chafed · Apr 2, 2020 · N779CA · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H I/B FLAP VANE L/E IS CHAFED AT THE CENTER LOCATION. (C-CHECK) RO 4/21/2020 REMOVED R/H I/B FLAP VANE L/E IS CHAFED AT THE CENTER LOCATION.. DUE TO OUT OF LIMITS CONDIDTION INSTALLED NEW R/H I/B FLAP VANE L/E AT THE CENTER LOCATION. REF. BOMBARDIER DWG
- [SDR SWIA2020042350263](https://openairdocs.org/sdr/SWIA2020042350263.md): Skin · chafed · Apr 2, 2020 · N779CA · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H I/B FLAP VANE L/E IS CHAFED AT THE I/B LOCATION. (C-CHECK) RO 4/21/2020 BLENDED CHAFE ON R/H I/B FLAP VANE L/E I/B LOCATION AND FOUND TO BE OUT OF LIMITS REF. BOMBARDIER REO & CRJ 200 SRM. REMOVED AND INSTALLED NEW R/H I/B FLAP VANE L/E I/B REF. BOMBAR
- [SDR SWIA2018062644822](https://openairdocs.org/sdr/SWIA2018062644822.md): Hinge · damaged · Apr 20, 2018 · N779CA · Cndair CL6002B19 · Fuselage, Door Hinge
  > ELONGATED HOLES ON PAX DOOR HINGE, FUSELAGE SIDE. REPLACED THE DOOR HINGE IAW SRM.
- [SDR SWIA201844815](https://openairdocs.org/sdr/SWIA201844815.md): Floor Support · corroded · Apr 20, 2018 · N779CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BETWEEN BS 559 TO 559+16. CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.
- [SDR SWIA2018062644821](https://openairdocs.org/sdr/SWIA2018062644821.md): Angle · corroded · Apr 19, 2018 · N779CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGH PRESSURE FLOOR ANGLE HAD NUMEROUS AREAS OF CORROSION FROM BS 409+128 - 559. REPAIRED IAW REO.
- [SDR SWIA2018062644830](https://openairdocs.org/sdr/SWIA2018062644830.md): Frame · corroded · Apr 18, 2018 · N779CA · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION FOUND ON THE FWD SIDE OF FRAME BS 605, STRINGERS 22L AND 23L. REMOVED THE CORROSION. WITHIN LIMTS IAW REIO.
- [SDR SWIA2018062644829](https://openairdocs.org/sdr/SWIA2018062644829.md): Strap · corroded · Apr 18, 2018 · N779CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LEFT PRESSURE FLOORBEAM STRAP HAD EVIDENCE OF CORROSION, BS 559 BETWEEN LBL 32 TO 43. REMOVED AND REPLACED THE STRAP IAW SRM.
- [SDR SWIA2018062644828](https://openairdocs.org/sdr/SWIA2018062644828.md): Frame · corroded · Apr 18, 2018 · N779CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME CORRODED AT BS 364, STRINGER 25L TO 25R. BLENDED THE FRAME IAW SRM.
- [SDR SWIA2018062644827](https://openairdocs.org/sdr/SWIA2018062644827.md): Frame · corroded · Apr 18, 2018 · N779CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME CORRODED AT BS 319 BETWEEN STRINGERS 25L TO 26R. REMOVED AND REPLACED THE FRAME SECTION IAW SRM.
- [SDR SWIA2018062644826](https://openairdocs.org/sdr/SWIA2018062644826.md): Floorbeam · corroded · Apr 17, 2018 · N779CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM, BS 349 NEAR SERVICE DOOR SILL WAS CORRODED. REMOVED COROSSION AND COMPLIED WITH ALL STEPS OF SRM AND REO.
- [SDR SWIA2018062644825](https://openairdocs.org/sdr/SWIA2018062644825.md): Skin · dented · Apr 17, 2018 · N779CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THE LOWER SKIN PANEL WAS DENTED BETWEEN BS 589 AND 605, BETWEEN STRINGERS 20L AND 21L. REPAIRED IAW REO.
- [SDR SWIA2018062644824](https://openairdocs.org/sdr/SWIA2018062644824.md): Skin · dented · Apr 17, 2018 · N779CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THE LOWER SKIN PANEL WAS DENTED BETWEEN BS 640 AND 718, BETWEEN STRINGERS 21R AND 25R. REPAIR IAW REO.
- [SDR SWIA2018062644820](https://openairdocs.org/sdr/SWIA2018062644820.md): Frame · corroded · Apr 17, 2018 · N779CA · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 349 FRAME, STRINGER 25 L & R WAS CORRODED. REPLACED THE FRAME IAW SRM.
- [SDR SWIA2018062644819](https://openairdocs.org/sdr/SWIA2018062644819.md): Door Sill · corroded · Apr 17, 2018 · N779CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION AROUND NUTPLATES ON THE CARGO DOOR SILL. REMOVED AND REPLACED THE DOOR SILL IAW SRM AND REO.
- [SDR SWIA2018062644823](https://openairdocs.org/sdr/SWIA2018062644823.md): Skin · cracked · Apr 16, 2018 · N779CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT BS 235, STRINGER 26L, REPAIRED THE SKIN IAW REO.
- [SDR SWIA2018062644816](https://openairdocs.org/sdr/SWIA2018062644816.md): Skin · dented · Apr 16, 2018 · N779CA · Cndair CL6002B19 · Elevator, Plate/Skin
  > THE TOP OF THE RT INBD ELEVATOR WAS DENTED. REPAIRED IAW REO.
- [SDR SWIA2018062644814](https://openairdocs.org/sdr/SWIA2018062644814.md): Skin · damaged · Apr 16, 2018 · N779CA · Cndair CL6002B19 · Elevator, Plate/Skin
  > LEFT TOP OF OTBD ELEVATOR TRAILING EDGE DAMAGED. REPAIRED IAW REO.
- [SDR SWIA2018062644813](https://openairdocs.org/sdr/SWIA2018062644813.md): Skin · dented · Apr 16, 2018 · N779CA · Cndair CL6002B19 · Elevator, Plate/Skin
  > RIGHT TOP TRAILING EDGE OF ELEVATOR DAMAGED. REPAIRED IAW REO.
- [SDR SWIA2018062644818](https://openairdocs.org/sdr/SWIA2018062644818.md): Skin · dented · Apr 14, 2018 · N779CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP LOWER SKIN DENTED. REPAIRED IAW SRM.
- [SDR SWIA201844817](https://openairdocs.org/sdr/SWIA201844817.md): Skin · dented · Apr 12, 2018 · N779CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND A DENT ON THE SKIN, BS 253 ABOVE STRINGER 23R. REPAIRED IAW REO.
- [SDR SWIA201642236](https://openairdocs.org/sdr/SWIA201642236.md): Wire · damaged · Jun 16, 2016 · N779CA · Cndair CL6002B19 · Fire Protection System Wiring
  > ANTI-ICE DUCT WARNING ON DESCENT. DECLARED AN EMERGENCY. REPLACED LOOP IN AFT EQUIPMENT BAY.
- [SDR SWIA201642143](https://openairdocs.org/sdr/SWIA201642143.md): Vane · chafed · Apr 24, 2016 · N779CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE OTBD CENTER L/E VANE CAP CHAFED BEYOND LIMITS. R & R LT INBD FLAP VANE OTBD CENTER L/E VANE CAP IAW SRM AND STS EA.
- [SDR SWIA201642039](https://openairdocs.org/sdr/SWIA201642039.md): Oil System · overserviced · Apr 6, 2016 · N779CA · Cndair CL6002B19 · Turbine Engine Oil System
  > THE LT ENGINE OIL TEMP WENT TO 198 AND OIL PRESSURE WENT DOWN TO 34. WHEN THE CREW WENT TO IDLE THE OIL PRESSURE DROPPED FURTHER INTO THE RED WITH ASSOCIATED LT ENGINE OIL PRESSURE WARNING MESSAGE. CAPTAIN SHUTDOWN THE LT ENGINE AND DECLARED AN EMERGENCY. F
- [SDR SWIA2015021340723](https://openairdocs.org/sdr/SWIA2015021340723.md): Battery Pack · discharged · Feb 12, 2015 · N779CA · Cndair CL6002B19 · Emergency Lighting
  > ALL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE RECHARGED LIGHTS, OPS GOOD IAW AMM.
- [SDR SWIA2014062338267](https://openairdocs.org/sdr/SWIA2014062338267.md): Mount · damaged · Jun 21, 2014 · N779CA · Cndair CL6002B19 · Engine Mount Section
  > LEFT ENGINE, FRETTING WEAR AT AFT MOUNT RIB. COMPLIED WITH REO. INSPECTED MAX ALLOWABLE GAP OF PYLON OTBD MOUNT RIB, AND FOUND TO BE WITHIN LIMITS.
- [SDR SWIA2014062338266](https://openairdocs.org/sdr/SWIA2014062338266.md): Pin · scored · Jun 21, 2014 · N779CA · Cndair CL6002B19 · Engine Mount Section
  > LEFT ENGINE, YOKE MOUNT PINS AND BOLTS SCORED. R & R LT ENGINE FWD YOKE MOUNT PINS AND BOLTS IAW AMM.
- [SDR SWIA2014062338265](https://openairdocs.org/sdr/SWIA2014062338265.md): Bushing · galled · Jun 21, 2014 · N779CA · Cndair CL6002B19 · Engine Mount Section
  > LEFT ENGINE, YOKE MOUNT LINK BUSHINGS ARE GALLED. R & R LT ENGINE YOKE LINK IAW AMM.
- [SDR SWIA201437572](https://openairdocs.org/sdr/SWIA201437572.md): Skin · corroded · May 2, 2014 · N779CA · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > LT PYLON AFT UPPER SKIN CORROSION ON SPLICE PLATE. C-CHECK REPLACED SPLICE PLATE IAW SRM.
- [SDR SWIA201437573](https://openairdocs.org/sdr/SWIA201437573.md): Skin · dented · May 1, 2014 · N779CA · Cndair CL6002B19 · Rudder, Plate/Skin
  > DENT IN RUDDER SKIN LT SIDE AT RS105.0. C-CHECK, BLENDED OUT DENT ON LT RUDDER SKIN AT RS105, REF SRM.
- [SDR SWIA201437575](https://openairdocs.org/sdr/SWIA201437575.md): Skin · corroded · Apr 28, 2014 · N779CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER WING PLANK ACCESS HOLE, 640BB HAS FRETTING. C-CHECK, BLENDED DAMAGED IN 3EA LOCATIONS REF REO.
- [SDR SWIA201437574](https://openairdocs.org/sdr/SWIA201437574.md): Skin · corroded · Apr 28, 2014 · N779CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER WING PLANK ACCESS HOLE, 540BB, HAS FRETTING. C-CHECK, BLENDED DAMAGED IN 3 EA LOCATIONS REF REO.
- [SDR SWIA201437578](https://openairdocs.org/sdr/SWIA201437578.md): Skin · cracked · Apr 26, 2014 · N779CA · Cndair CL6002B19 · Wing, Plate/Skin
  > CRACK ON LT WING PLANK, C-CHECK, REPAIRED CRACK ON LT WING PLANK REF REO.
- [SDR SWIA201437577](https://openairdocs.org/sdr/SWIA201437577.md): Plate · corroded · Apr 26, 2014 · N779CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR FLOOR PROTECTOR PLATE CORRODED. C-CHECK, BLENDED CORROSION ON SERVICE DOOR FLOOR PROTECTOR PLATE REF SRM.
- [SDR SWIA201437576](https://openairdocs.org/sdr/SWIA201437576.md): Window Frame · cracked · Apr 26, 2014 · N779CA · Cndair CL6002B19 · Fuselage Main, Structure
  > CRACK WINDSHIELD CTR POST, LT CTR CLIP, UPR RADIUS. C-CHECK, REPLACED CRACKED CTR POST LT CLIP WITH NEW CLIP REF SRM.
- [SDR SWIA201437586](https://openairdocs.org/sdr/SWIA201437586.md): Vane · chafed · Apr 25, 2014 · N779CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBD FLAP VANE CHAFED, INBD L/E. C-CHECK, BLENDED RT INBD FLAP VANE CHAFE WITH IN LIMITS AND RESTORED FINISH REF REO.
- [SDR SWIA201437585](https://openairdocs.org/sdr/SWIA201437585.md): Vane · chafed · Apr 25, 2014 · N779CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBD FLAP VANE CHAFED, CENTER L/E. C-CHECK, BLENDED RT INBD FLAP VANE CENTER L/E REF REO.
- [SDR SWIA201437584](https://openairdocs.org/sdr/SWIA201437584.md): Vane · chafed · Apr 25, 2014 · N779CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBD FLAP VANE CHAFED, OTBD L/E. C-CHECK, BLENDED RT INBD FLAP VANE OTBD L/E REF REO.

Next page: https://openairdocs.org/deregistered/N779CA-2022-11-30/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 = 'N779CA' AND deregistration_id = 'N779CA-2022-11-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N779CA-2022-11-30/reports

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