# Service difficulty reports: N435SW, cancelled Feb 16, 2023

A list on [N435SW, cancelled Feb 16, 2023](https://openairdocs.org/deregistered/N435SW-2023-02-16.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 5 · 241 reports

- [SDR SWIA2019122747416](https://openairdocs.org/sdr/SWIA2019122747416.md): Support Bracket · cracked · Dec 22, 2019 · N435SW · Cndair CL6002B19 · Main Landing Gear
  > CRACKED RT MLG BRAKE TRANSDUCER SUPPORT BRACKET. REMOVED & REPLACED THE SUPPORT BRACKET IAW SRM. CHECKED GOOD.
- [SDR SWIA2019122747418](https://openairdocs.org/sdr/SWIA2019122747418.md): Rivet · cracked · Dec 17, 2019 · N435SW · Cndair CL6002B19 · Engine Air Intake System
  > LEFT ENGINE NOSE COWL HAD ON CRACKED RIVET INSIDE THE INLET ON INBD SIDE. REPLACED THE RIVET ON THE LT ENG NOSE COWL IAW SRM.
- [SDR SWIA2019122747393](https://openairdocs.org/sdr/SWIA2019122747393.md): Plate · broken · Dec 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Main, Structure
  > UPPER ATTACHMENT PLATE BROKEN FOR PRESSURE BOX / FUEL SHROUD AT F.S. 559.00. REMOVED BROKEN UPPER ATTACHMENT PLATE FOR PRESSURE BOX/FUEL SHROUD AT FS 559.0 AND LOCATED, DRILLED-UP AND INSTALLED WITH NEW ATTACHMENT PLATE PN C68C38.REF SRM AND TR51-42.
- [SDR SWIA2019122747422](https://openairdocs.org/sdr/SWIA2019122747422.md): Housing · cracked · Dec 10, 2019 · N435SW · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT THRUST REVERSER PDU HOUSING WAS CRACKED. REMOVED AND REPLACED THE THRUST REVERSER PDU IAW IAW AMM 78-32-03-000-801 AND AMM 78-32-03-400-801. OPS CHECKED GOOD.
- [SDR SWIA2019122747381](https://openairdocs.org/sdr/SWIA2019122747381.md): Anchor · broken · Dec 5, 2019 · N435SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RH FLAP STUB FAIRING WING REAR SPAR FLAP FITTING (ANCHOR POINT) BROKEN. REMOVED AND REPLACED BROKEN RH FLAP STUB FAIRING WING REAR SPAR FLAP FITTING (ANCHOR POINT) WITH NEW FITTING INSTALLED WITH 2EA NEW LOCK FASTENERS AND NUTS. REF SRM.
- [SDR SWIA2019122747404](https://openairdocs.org/sdr/SWIA2019122747404.md): Bolt · chafed · Nov 29, 2019 · N435SW · Cndair CL6002B19 · Elevator Structure
  > RH ELEVATOR #1 HINGE MOUNT BOLT IB RETAINER CHAFED. REPLACED AND SAFTIED RH ELEVATOR #1 HINGE MOUNT BOLT IB RETAINER WITH NEW PLATE AND HARDWQARE 2EA BOLTS AND WASHERS REF SRM.
- [SDR SWIA2019122747396](https://openairdocs.org/sdr/SWIA2019122747396.md): Angle · damaged · Nov 27, 2019 · N435SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 FWD ANGLE HAS ELONGATED HOLE BETWEEN LBL 9 AND RBL 9 (C-CHECK) RO 12/24/2019 REPAIRED FS280 FWD ANGLE ELONGATED HOLE BETWEEN LBL 9 AND RBL 9 REF CRJ200 SRM.
- [SDR SWIA2019122747374](https://openairdocs.org/sdr/SWIA2019122747374.md): Stand Off · broken · Nov 25, 2019 · N435SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FOUND 2EA BROKEN STANDOFFS. REMOVED AND REPLACED AT THE AFT SIDE OF REAR PRESSURE BULKHEAD FS625 IAW SRM.
- [SDR SWIA2019122747427](https://openairdocs.org/sdr/SWIA2019122747427.md): Pulley Bracket · cracked · Nov 22, 2019 · N435SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PULLEY BRACKET IS CRACKED AT BS 621 BETWEEN LBL 18 AND LBL 27. REMOVED AND REPLACED PULLEY BRACKET IAW SRM.
- [SDR SWIA2019122747430](https://openairdocs.org/sdr/SWIA2019122747430.md): Fitting · cracked · Nov 21, 2019 · N435SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FLOOR SUPPORT FITTING AT FS460.00 LBL27 INBOARD CASTING IS CRACKED AT FWD CORNER. REMOVED FLOOR SUPPORT FITTING AT FS460.00 LBL27 INBOARD CASTING IAW SRM. LOCATED, DRILLED EXISTING FASTENER HOLES TO REPLACEMENT SUPPORT FITTING IAW SRM. INSTALLED A NEW FLO
- [SDR SWIA2019122747432](https://openairdocs.org/sdr/SWIA2019122747432.md): Stiffener · cracked · Nov 20, 2019 · N435SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LEFT STIFFENER WAS CRACKED AT AFT SIDE OF BULKHEAD BS 621, STRINGER 16L INSTALLED A NEW STIFFENER IAW SRM.
- [SDR SWIA2019122747435](https://openairdocs.org/sdr/SWIA2019122747435.md): Crossbeam · cracked · Nov 15, 2019 · N435SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 280 CROSSBEAM WAS CRACKED AT 2 PLACES, LBL 9 AND RBL 9, PERFORMED A REPAIR IAW REO.
- [SDR SWIA2019122747437](https://openairdocs.org/sdr/SWIA2019122747437.md): Floor Support · damaged · Nov 14, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT RBL 9 FROM BS 409+118 TO 559+10 DAMAGED. REPLACED THE DAMAGED SECTION OF THE FLOOR SUPPORT IAW REO.
- [SDR SWIA201912747395](https://openairdocs.org/sdr/SWIA201912747395.md): Floor Support · damaged · Nov 14, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REPAIR FLOOR BEAM AT LBL9 FS409+118 TO FS559+10. REPLACED DAMAGED SECTION OF FLOOR BEAM PER REO 601R-53-41-2636 REV.
- [SDR SWIA2019122747441](https://openairdocs.org/sdr/SWIA2019122747441.md): Floor Panel · cracked · Nov 13, 2019 · N435SW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR PANEL WAS CRACKED AT FS 461 LBL 0 -9 AND FS 461 RBL 0 - 9. REPAIRED THE PRESSURE FLOOR PANEL IAW REO.
- [SDR SWIA2019122747470](https://openairdocs.org/sdr/SWIA2019122747470.md): Plate · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER PLATE JUST INBOARD OF THE LT FLOOR SUPPORT AT APPROXIMATELY BS 308, LBL 41. REMOVED CORROSION ON THE AFFECTED AREA IAW SRM.
- [SDR SWIA2019122747469](https://openairdocs.org/sdr/SWIA2019122747469.md): Cup · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CORROSION ON FORWARD AND AFT PAX DOOR HANDRAIL CUPS. REMOVED AND REPLACED FWD AND AFT PAX DOOR HANDRAIL CUPS IAW SRM.
- [SDR SWIA2019122747468](https://openairdocs.org/sdr/SWIA2019122747468.md): Floor Support · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT HAD CORROSION BETWEEN FS 295 AND FS 310. REMOVED CORROSION ON THE AFFECTED AREA IAW SRM.
- [SDR SWIA2019122747467](https://openairdocs.org/sdr/SWIA2019122747467.md): Support · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 574 - 605, RT FLOOR EDGE MEMBER HAS CORROSION AROUND SEVERAL SCREW HOLES. REMOVED CORROSION IAW SRM. ALL REWORKED AREAS ACCEPTABLE IAW REO..
- [SDR SWIA2019122747466](https://openairdocs.org/sdr/SWIA2019122747466.md): Mount · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CORROSION ON FORWARD AND AFT INBOARD MOUNT PLATES FOR GALLEY ATTACHMENT INBOARD OF RBL 9. REMOVED CORROSION FROM THE MOUNT PLATE IAW SRM. REPLACED THE MOUNT PLATE IAW SRM.
- [SDR SWIA2019122747465](https://openairdocs.org/sdr/SWIA2019122747465.md): Door Sill · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL WAS CORRODED AROUND SEVERAL SCREW HOLES. REMOVED CORROSION FROM THE CARGO DOOR SILL IAW SRM 51-21-06. ALL REWORKED AREAS ARE ACCEPTABLE IAW REO.
- [SDR SWIA2019122747464](https://openairdocs.org/sdr/SWIA2019122747464.md): Floor Support · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPORT BETWEEN BS 349 AND 409+5 WAS CORRODED. REMOVED CORROSION ON THE AFFECTED AREA IAW SRM.
- [SDR SWIA2019122747463](https://openairdocs.org/sdr/SWIA2019122747463.md): Duct · out of alignment · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Cabin Cooling System
  > LEFT ACM RAM AIR DUCT. FIT CHECK FAILED. TOP HOLES OF RAM AIR DUCT DO NOT LINED UP WITH AIRCRAFT SIDE HOLES. REPAIRED THE RAM AIR DUCT IAW REO.
- [SDR SWIA2019122747462](https://openairdocs.org/sdr/SWIA2019122747462.md): Floor Support · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FLOOR BEAM AT 559.0 LBL 9 HAS CORROSION (C-CHECK) RO 12/24/2019 REMOVED CORROSION ON LBL 9 FLOOR BEAM CAP FROM FS409+118 TO FS559+10, OUT OF LIMITS. REPAIRED.
- [SDR SWIA2019122747461](https://openairdocs.org/sdr/SWIA2019122747461.md): Seat Track · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON THE SEAT TRACK AT RBL 9 BETWEEN BS 364 AND 394. REMOVED CORROSION FROM THE AFFECTED AREA.
- [SDR SWIA2019122747460](https://openairdocs.org/sdr/SWIA2019122747460.md): Angle · cracked · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SURROUND AT FWD CAM TRACK SUPPORT LOWER ANGLE CRACKED. REPLACED FWD CAM TRACK SUPPORT LOWER ANGLE IAW SRM AND DWG. MAJOR REPAIR.
- [SDR SWIA2019122747459](https://openairdocs.org/sdr/SWIA2019122747459.md): Floor Support · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT BS 559, RBL 9 WAS CORRODED. REMOVED CORROSION FROM BS409+118 TO 559+10. FOUND OUT OF LIMITS, REPAIRED.
- [SDR SWIA2019122747458](https://openairdocs.org/sdr/SWIA2019122747458.md): Floor Support · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BETWEEN BS 559+64 - 559+80, RBL 9, WAS CORRODED. EXFOLIATED BEYOND REPAIR. 100% MATERIAL LOSS. OUT OF LIMITS. FABRICATED AND INSTALLED A NEW REPLACEMENT FLOOR SUPPORT. INSTALLED IAW DWG.
- [SDR SWIA2019122747457](https://openairdocs.org/sdr/SWIA2019122747457.md): Floor Support · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT BETWEEN BS 409+32 AND 409+48 WAS CORRODED. REMOVED CORROSION ON THE AFFECTED AREA IAW SRM.
- [SDR SWIA2019122747455](https://openairdocs.org/sdr/SWIA2019122747455.md): Seat Track · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK BETWEEN BS 409+16 AND 409+120 WAS CORRODED. THE SEAT TRACK WAS REPLACED IAW REO.
- [SDR SWIA2019122747453](https://openairdocs.org/sdr/SWIA2019122747453.md): Floor Support · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9 FLOOR SUPPORT CAP, INBOARD FLANGE WAS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 409+6 AND 409+118. REMOVED AND INSTALLED A NEW FLOOR SUPPORT CAP IAW DRAWING.
- [SDR SWIA2019122747450](https://openairdocs.org/sdr/SWIA2019122747450.md): Floor Support · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR SUPPORT CAP INBOARD FLANGE HAD CORROSION AT MULTIPLE LOCATIONS BETWEEN BS 409+6 AND 409+118. INSTALLED A NEW FABRICATED FLOOR SUPPORT CAP IAW SRM.
- [SDR SWIA2019122747448](https://openairdocs.org/sdr/SWIA2019122747448.md): Floor Support · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9 FLOOR SUPPORT CAP INBOARD FLANGE HAD CORROSION AT MULTIPLE LOCATIONS BETWEEN BS 409+118 AND 409+128. REMOVED CORROSION AND FOUND OUT OF LIMITS, REPAIRED.
- [SDR SWIA2019122747446](https://openairdocs.org/sdr/SWIA2019122747446.md): Floor Support · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR SUPPORT CAP INBOARD FLANGE HAD CORROSION AT MULTIPLE LOCATIONS BETWEEN BS 409+118 AND 409+128. REMOVED CORROSION AND FOUND OUT OF LIMITS, REPAIRED.
- [SDR SWIA2019122747445](https://openairdocs.org/sdr/SWIA2019122747445.md): Seat Track · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK WAS CORRODED BETWEEN BS 409+48 AND 409+118. REPLACED THE SEAT TRACK IAW REO.
- [SDR SWIA2019122747443](https://openairdocs.org/sdr/SWIA2019122747443.md): Floor Support · corroded · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH FLOOR SUPPORT WAS CORRODED BETWEEN BS 409+32 AND 409+80. REMOVED CORROSION ON THE AFFECTED AREA. IAW SRM.
- [SDR SWIA2019122747411](https://openairdocs.org/sdr/SWIA2019122747411.md): Panel · chafed · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP PANEL 584JB IS CHAFFED AT ACTUATOR NOTCH. REPAIRED THE LT INBD FLAP PANEL.
- [SDR SWIA2019122747409](https://openairdocs.org/sdr/SWIA2019122747409.md): Panel · chafed · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP PANEL 584MB IS CHAFED AT THE ACTUATOR NOTCH. REPAIRED LT INBD FLAP PANEL IAW EA934, CURED AND FINISHED.
- [SDR SWIA2019122747387](https://openairdocs.org/sdr/SWIA2019122747387.md): Isolator · broken · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > * FS621 BULKHEAD HAS 8 EACH BROKEN ISOLATORS. REMOVED AND REPLACED 8 EACH BROKEN ISOLATORS WITH NEW ON FS621 BULKHEAD REF CRJ 200 SRM.
- [SDR SWIA2019122747384](https://openairdocs.org/sdr/SWIA2019122747384.md): Isolator · broken · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 ISOLATOR BRACKET IS BROKEN, R/H SIDE, MARKED. (C-CHECK) RO 12/24/2019 REMOVED AND REPLACED BROCKEN ISOLATOR WITH NEW ISOLATOR FS621 R/H SIDE REF CRJ 200 SRM.
- [SDR SWIA2019122747372](https://openairdocs.org/sdr/SWIA2019122747372.md): Angle · bent · Nov 12, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO SURROUND FWD CAM TRACK SUPPORT LOWER FWD ANGLE BENT. REPLACED FWD CAM TRACK SUPPORT LOWER FWD ANGLE. REF SRM 51-42-06 AND DWG 601R35050 REV AC / COMPLIED WITH TASK CARD 51-900-1003 MAJOR REPAIR
- [SDR SWIA2019122747456](https://openairdocs.org/sdr/SWIA2019122747456.md): Floor Support · cracked · Nov 11, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BRACKET AT APPROX. BS 461 LBL 36, WAS CRACKED AT ITS FORWARD CORNER. REMOVED AND REPLACED THE FLOOR SUPPORT BRACKET IAW SRM AND DWG.
- [SDR SWIA2019122747454](https://openairdocs.org/sdr/SWIA2019122747454.md): Strap · corroded · Nov 11, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOORBEAM STRAP AT BS 559, RBL 27 - 45 WAS CORRODED. REMOVED AND REPLACED THE STRAP IAW SRM AND DWG.
- [SDR SWIA2019122747452](https://openairdocs.org/sdr/SWIA2019122747452.md): Floor Panel · corroded · Nov 11, 2019 · N435SW · Cndair CL6002B19 · Fuselage Floor Panel
  > RIGHT SIDE PRESSURE FLOOR PANEL WAS CORRODED AT MULTIPLE SPOTS. REPAIRED THE FLOOR PANEL IAW REO.
- [SDR SWIA2019122747451](https://openairdocs.org/sdr/SWIA2019122747451.md): Strap · corroded · Nov 11, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRAP AT BS 559, LBL 27 - 45 WAS CORRODED. REMOVED CORROSION IAW SRM
- [SDR SWIA2019122747449](https://openairdocs.org/sdr/SWIA2019122747449.md): Floor Support · corroded · Nov 11, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT SIDE PRESSURE FLOOR SUPPORT ANGLE WAS CORRODED AT MULTIPLE SPOTS. REPAIRED BY BLENDING IAW REO.
- [SDR SWIA2019122747447](https://openairdocs.org/sdr/SWIA2019122747447.md): Floor Panel · corroded · Nov 11, 2019 · N435SW · Cndair CL6002B19 · Fuselage Floor Panel
  > LEFT SIDE PRESSURE FLOOR SILL PANEL IS CORRODED IN MULTIPLE SPOTS. REPAIRED BY BLENDING IAW REO.
- [SDR SWIA2019122747444](https://openairdocs.org/sdr/SWIA2019122747444.md): Angle · cracked · Nov 11, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT BS 625.3 UPPER ANGLE WAS CRACKED. REMOVED AND REPLACED IAW SRM, DWG, AND REO.
- [SDR SWIA2019122747442](https://openairdocs.org/sdr/SWIA2019122747442.md): Angle · cracked · Nov 11, 2019 · N435SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT BS 625.3 UPPER ANGLE WAS CRACKED. REMOVED THE ANGLE IAW SRM. LOCATED AND DRILLED A NEW ANGLE IAW SRM, INSTALLED IAW DWG 601-35012, REV D, AND REO.
- [SDR SWIA2019122747440](https://openairdocs.org/sdr/SWIA2019122747440.md): Fairing · corroded · Nov 11, 2019 · N435SW · Cndair CL6002B19 · Aerodynamic Fairings
  > FWD FUSELAGE UNDER FAIRINGS 191AB AND 192BB BETWEEN STRINGERS 24 LT AND RT AT BS 409+96 MOUNT HOLES WERE CORRODED. REMOVED CORROSION FROM FWD FUSELAGE UNDER FAIRINGS MOUNT HOLES, BLENDED AREAS FOUND TO BE OUT OF LIMITS, APPLICABLE REO FOR THIS AREA STATES TH

Next page: https://openairdocs.org/deregistered/N435SW-2023-02-16/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 = 'N435SW' AND deregistration_id = 'N435SW-2023-02-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N435SW-2023-02-16/reports

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