# Service difficulty reports: N913SW, cancelled Jan 24, 2023

A list on [N913SW, cancelled Jan 24, 2023](https://openairdocs.org/deregistered/N913SW-2023-01-24.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 · 215 reports

- [SDR SWIA202049252](https://openairdocs.org/sdr/SWIA202049252.md): Unknown · fire · Mar 11, 2020 · N913SW · Cndair CL6002B19 · Flight Compartment Equipment
  > CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 397685, WHEN AIRCRAFT WAS BEING REPOSITIONED FROM TERMINAL TO HANGAR FOR MX, APU WAS STARTED AND AS SOON AS THE APU GENERATOR WAS SELECTED ON A POPPING AND HISSING NOISES WERE HEARD FROM BEHIND AND A FIRE
- [SDR SWIA2020031049250](https://openairdocs.org/sdr/SWIA2020031049250.md): Post · cracked · Feb 22, 2020 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > COMPLY WITH FORM 337 FOR FS409+128 VERTICAL POST CRACKED AT INBOARD LOWER AFT RIVET IN RADIUS AT LBL27. CLASIFIED AS MAJOR REPAIR. (AGING A/C INSP - RO 3/7/2020) COMPLETED FORM M-337 FOR REPAIR AT FS409+128 VERTICAL POST AT LB27.
- [SDR SWIA2020031049249](https://openairdocs.org/sdr/SWIA2020031049249.md): Post · cracked · Feb 22, 2020 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > COMPLY WITH FORM 337 FOR FS409+128 VERTICAL POST CRACKED AT OUTBOARD LOWER AFT RIVET IN RADIUS AT LBL18. CLASIFIED AS MAJOR REPAIR. (AGING A/C INSP - RO 3/7/2020) COMPLETED FORM M-337 FOR REPAIR AT FS409+128 VERTICAL POST AT LBL18.
- [SDR SWIA2020031049102](https://openairdocs.org/sdr/SWIA2020031049102.md): Post · cracked · Feb 20, 2020 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ***** MAJOR ***** FS409+128 VERTICAL POST CRACKED AT OUTBOARD LOWER AFT RIVET IN RADIUS AT LBL18. (AGING AC INSP - RO 3/7/2020) REPAIRED FS409+128 VERTICAL POST CRACKED AT OUTBOARD LOWER AFT RIVET IN RADIUS AT LBL18 IAW REO.
- [SDR SWIA2020031049099](https://openairdocs.org/sdr/SWIA2020031049099.md): Post · cracked · Feb 20, 2020 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ***** MAJOR ***** FS409+128 VERTICAL POST CRACKED AT INBOARD LOWER AFT RIVET IN RADIUS AT LBL27. (AGING AC INSP - RO 3/7/2020) REPAIRED FS409+128 VERTICAL POST CRACKED AT INBOARD LOWER AFT RIVET IN RADIUS AT LBL27 IAW REO.
- [SDR SWIA2019061145973](https://openairdocs.org/sdr/SWIA2019061145973.md): Control Handle · failed · Jun 11, 2019 · N913SW · Cndair CL6002B19 · Landing Gear Selector
  > AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT; FOLLOWED BY A/SKID INBD AND PARK BRAKE SOV CAUTION MESSAGES. RETURNED TO FIELD. (FLT#5399) REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE ASSY IAW AMM. PERFORMED LANDING GEAR EXTENSION AND RETRACTION SEVERAL
- [SDR SWIA2019405065827](https://openairdocs.org/sdr/SWIA2019405065827.md): Servo Valve · failed · May 6, 2019 · N913SW · Cndair CL6002B19 · Landing Gear Steering System
  > STEERING INOP CAUTION IN FLIGHT. COMPLIED WITH QRH. (FLT#5311) CLOSED REMOVED AND REPLACED SERVO VALVE IAW AMM.
- [SDR SWIA2018110245220](https://openairdocs.org/sdr/SWIA2018110245220.md): Skin · dented · Oct 19, 2018 · N913SW · Cndair CL6002B19 · Trailing Edge Flaps
  > A DENT WAS FOUND ON THE RT INBD FLAP LOWER SKIN. REPAIRED THE SKIN IAW SRM 57-52-00.
- [SDR SWIA2018110245222](https://openairdocs.org/sdr/SWIA2018110245222.md): Frame · corroded · Oct 8, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 605 FRAME FOUND CORRODED. REMOVED AND REPLACED THE ENTIRE FRAME SECTOR IAW SRM 51-42-06.
- [SDR SWIA2018110245219](https://openairdocs.org/sdr/SWIA2018110245219.md): Floor Support · corroded · Oct 7, 2018 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT CORRODE AT BS 559. REMOVED AND REPLACED IAW SRM 51-42-06.
- [SDR SWIA2018110245218](https://openairdocs.org/sdr/SWIA2018110245218.md): Floor Support · corroded · Oct 7, 2018 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED AT BS 559. REMOVED AND REPLACED IAW SRM 51-42-06.
- [SDR SWIA2018110245217](https://openairdocs.org/sdr/SWIA2018110245217.md): Floorbeam · corroded · Oct 6, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > COCKPIT FLOORBEAM, BS 280 WAS CORRODED. REMOVED AND REPLACED THE COCKPIT FLOORBEAM ANGLE.
- [SDR SWIA2018110245216](https://openairdocs.org/sdr/SWIA2018110245216.md): Vane · gouged · Oct 5, 2018 · N913SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP VANE WAS GOUGED. REPAIRED IAW SRM 51-21-06.
- [SDR SWIA2018110245215](https://openairdocs.org/sdr/SWIA2018110245215.md): Vane · worn · Oct 5, 2018 · N913SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT OUTBOARD FLAP, OUTBOARD VANE MOUNT STRUCTURE WAS WORN. MEASURED REMAINING MATERIAL AND FOUND WITHIN LIMITS IAW REO 601R-57-53-195.
- [SDR SWIA2018110245221](https://openairdocs.org/sdr/SWIA2018110245221.md): Stringer Splice · cracked · Oct 4, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE WAS CRACKED AT ITS ATTACH POINT TO PASSENGER DOOR UPPER SILL, BS 379. REPAIRED THE STRINGER SPLICE IAW SRM 53-00-03.
- [SDR SWIA2018110245214](https://openairdocs.org/sdr/SWIA2018110245214.md): Strap · corroded · Oct 4, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION FOUND ONTHE CIRCUMFERENTIAL STRAP BELOW FRAME BS 333. BLENDED THE STRAP IAW SRM 51-21-06.
- [SDR SWIA2018110245213](https://openairdocs.org/sdr/SWIA2018110245213.md): Bracket · corroded · Oct 4, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CORROSION FOUND ON THE BRACKET ATTACHED TO FRAME AT BS 319. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-21.
- [SDR SWIA2018110245212](https://openairdocs.org/sdr/SWIA2018110245212.md): Frame · corroded · Oct 4, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION FOUND ON THE FWD AND AFT FACES OF THE FRAME AT BS 333. REMOVED THE CORROSION IAW SRM 51-21-06.
- [SDR SWIA2018110245211](https://openairdocs.org/sdr/SWIA2018110245211.md): Hinge · chafed · Oct 4, 2018 · N913SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > SERVICE DOOR INTERIOR HINGE CHAFED. REMOVED AND REPLACED THE SERVICE DOOR HINGE PLATE IAW SRM 51-41-21. OPS CHECKED GOOD
- [SDR SWIA2018110245210](https://openairdocs.org/sdr/SWIA2018110245210.md): Panel · gouged · Oct 4, 2018 · N913SW · Cndair CL6002B19 · Standard Practices/Structures
  > PANEL 326CR GOUGED. REPAIRED THE PANEL IAW REO 601R-55-32-384.
- [SDR SWIA2018110245209](https://openairdocs.org/sdr/SWIA2018110245209.md): Skin · corroded · Oct 3, 2018 · N913SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CORROSION FOUND ON THE INNER SKIN, AROUND FORWARD AND AFT ACCESS DOOR CUT-OUTS. REMOVED AND REPLACED THE PAX DOOR SKIN IAW SRM 51-42-06.
- [SDR SWIA2018110245208](https://openairdocs.org/sdr/SWIA2018110245208.md): Skin · chafed · Oct 3, 2018 · N913SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STAB PANEL WAS CHAFED ON THE INNER SKIN. R & R THE SKIN PANEL IAW SRM 51-12-00.
- [SDR SWIA2018110245207](https://openairdocs.org/sdr/SWIA2018110245207.md): Skin · chafed · Oct 3, 2018 · N913SW · Cndair CL6002B19 · Elevator, Plate/Skin
  > LEFT ELEVATOR SKIN PANEL WAS CHAFED. REPAIRED THE DAMAGE IAW SRM 51-12-00.
- [SDR SWIA2018110245206](https://openairdocs.org/sdr/SWIA2018110245206.md): Skin Panel · chafed · Oct 3, 2018 · N913SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING SKIN PANEL WAS CHAFED. BLENDED THE PANEL IAW SRM 51-41-02.
- [SDR SWIA2018110245205](https://openairdocs.org/sdr/SWIA2018110245205.md): Skin · chafed · Oct 3, 2018 · N913SW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > LEFT NACELLE SKIN PANEL WAS CHAFED AT MULTIPLE PLACES. REMOVED AND REPLACED THE SKIN IAW SRM 51-42-06.
- [SDR SWIA2018110245204](https://openairdocs.org/sdr/SWIA2018110245204.md): Cover · nicked · Oct 2, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Structure
  > TWO NICKS FOUND JUST AFT OF GROUND AIR LOW PRESSURE COVER. COMPLIED WITH PERMANENT REPAIR OF THE AREA IAW REO 601R-53-61-6734.
- [SDR SWIA2018110245203](https://openairdocs.org/sdr/SWIA2018110245203.md): Skin · dented · Oct 2, 2018 · N913SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > A DENT WAS FOUND ON THE CARGO DOOR SKIN, AT THE BOTTOM CORNER. REPAIRED THE CARGO DOOR SKIN IAW REO 601R-52-31-299.
- [SDR SWIA2018110245202](https://openairdocs.org/sdr/SWIA2018110245202.md): Structure · dented · Oct 2, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Structure
  > A DENT WAS FOUND ON THE AFT FUSELAGE TAIL. REPAIRED.
- [SDR SWIA2018110245201](https://openairdocs.org/sdr/SWIA2018110245201.md): Skin · dented · Oct 2, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > A DENT WAS FOUND AFT AND ABOVE THE LT ACM EXHAUST OPENING. REPAIRED THE DENT IAW REO 601R-51-00-309.
- [SDR SWIA2018110245200](https://openairdocs.org/sdr/SWIA2018110245200.md): Skin · dented · Oct 2, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TWO SMALL DENTS FOUND ON THE RT FUSELAGE BETWEEN BS 589 TO 605. REPAIRED IAW REO 601R-53-61-6734.
- [SDR SWIA2018110245199](https://openairdocs.org/sdr/SWIA2018110245199.md): Skin · dented · Oct 2, 2018 · N913SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > A DENT WAS FOUND ON THE RT BOTTOM FUSELAGE JUST OUTBOARD FROM NLG. REPAIRED IAW REO 601R-53-11-3333.
- [SDR SWIA2018080744974](https://openairdocs.org/sdr/SWIA2018080744974.md): Skin · damaged · Jul 30, 2018 · N913SW · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND ELONGATED DAMAGED SCREW HOLE UNDER THE LT MLG ACCESS PANEL ADJACENT TO THE MLG OPENING. BETWEEN LT WS 53.60 - 65.75. REPAIRED WING PLANK IAW REO.
- [SDR SWIA2018051744638](https://openairdocs.org/sdr/SWIA2018051744638.md): Engine · flamed out · May 6, 2018 · N913SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > CAPTAIN REPORTED THAT DURING APPROACH, RECEIVED A RT MAIN EJECTOR AND RT SCAVENGE EJECTOR CAUTION MESSAGES AND RIGHT AFTER TOUCH DOWN THE RT ENGINE FLAMED OUT. ENGINE SHUT DOWN AFTER THRUST REVERSER ACTIVATION. REMOVED AND REPLACED THE RT ENGINE ASSY IAW AM
- [SDR SWIA201642644](https://openairdocs.org/sdr/SWIA201642644.md): Stringer · damaged · Sep 16, 2016 · N913SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > DAMAGE TO STR 0 BETWEEN BS 409+80 AND 409.00+96. REMOVED AND INSTALLED THE STRINGER IAW SRM.
- [SDR SWIA201642643](https://openairdocs.org/sdr/SWIA201642643.md): Stringer · damaged · Sep 16, 2016 · N913SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > DAMAGE TO STRINGER 16R BETWEEN BS 409 - 409 + 32. REMOVED AND REPLACED THE STRINGER IAW SRM.
- [SDR SWIA201642648](https://openairdocs.org/sdr/SWIA201642648.md): Vane · chafed · Sep 10, 2016 · N913SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT FLAP VANE OTBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE OTBD LEADING EDGE IAW SRM.
- [SDR SWIA201642647](https://openairdocs.org/sdr/SWIA201642647.md): Vane · chafed · Sep 10, 2016 · N913SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT FLAP VANE CENTER OF LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE CENTER LEADING EDGE IAW SRM.
- [SDR SWIA201642646](https://openairdocs.org/sdr/SWIA201642646.md): Vane · chafed · Sep 10, 2016 · N913SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT FLAP VANE INBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE INBD LEADING EDGE IAW SRM.
- [SDR SWIA201642645](https://openairdocs.org/sdr/SWIA201642645.md): Vane · chafed · Sep 10, 2016 · N913SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT FLAP VANE INBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED LT FLAP VANE INBD LEADING EDGE IAW SRM.
- [SDR SWIA201440370](https://openairdocs.org/sdr/SWIA201440370.md): Skin · gouged · Dec 6, 2014 · N913SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > BS 627, OTBD OF STRINGER 4L, TWO GOUGES ON SKIN. REPAIRED IAW EA
- [SDR SWIA201440379](https://openairdocs.org/sdr/SWIA201440379.md): Panel · cracked · Dec 4, 2014 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PANEL 221BLC CRACKED AND MISSING 6 EA SPACERS. REPAIRED CRACKED PANEL IAW EA AND SRM.
- [SDR SWIA201440388](https://openairdocs.org/sdr/SWIA201440388.md): Door · chafed · Nov 29, 2014 · N913SW · Cndair CL6002B19 · Landing Gear Doors
  > RIGHT MLG DOOR HAS CHAFE ON AFT EDGE THRU INNER SKIN NEAR BRUSH. RT MLG DOOR WORKED IAW STS EA COMPLIED WITH STEPS 1 THRU END, IAW SRM, REPAIR COMPLETED. THIS IS A PERMANANT REPAIR.
- [SDR SWIA201440384](https://openairdocs.org/sdr/SWIA201440384.md): Vane · damaged · Nov 25, 2014 · N913SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBD FLAP VANE CENTER CAP FOUND TO BE OUT OF LIMITS. R & R LT INBD FLAP VANE CENTER L/E SKIN, CAP, IAW SRM AND DWG 601R14303, REV J.
- [SDR SWIA201440390](https://openairdocs.org/sdr/SWIA201440390.md): Seat Track · corroded · Nov 24, 2014 · N913SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL9 FS 559+86 TO 559+112 CORRODED. REPLACED THE SEAT TRACK IAW AMM AND REO.
- [SDR SWIA201440382](https://openairdocs.org/sdr/SWIA201440382.md): Pressure Panel · cracked · Nov 24, 2014 · N913SW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR CRACKED IN 2 PLACES AT FS 460 OTBD OF LBL 0.0 AND RBL 0.0. COMPLIED WITH REPAIR OF PRESSURE FLOOR 2 PLACES AT FS 460 OTBD OF BL 0.0. RT & LT SIDES REF REO. PRESSURE LEAK CHECK GOOD. COMPLIED WITH ST CARD LEAK CHECK GOOD. MATERIAL REMOVED WEI
- [SDR SWIA201440380](https://openairdocs.org/sdr/SWIA201440380.md): Lever · worn · Nov 24, 2014 · N913SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR PULL IN LEVER IS WORN. REPAIRED THE PASSENGER DOOR PULL IN LEVER IAW REO.
- [SDR SWIA201440378](https://openairdocs.org/sdr/SWIA201440378.md): Fairing · damaged · Nov 24, 2014 · N913SW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL TIP FAIRING 333AL HAS MULTIPLE ELONGATED HOLES. REPAIRED IAW EA.
- [SDR SWIA201440377](https://openairdocs.org/sdr/SWIA201440377.md): Door Sill · corroded · Nov 24, 2014 · N913SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT CARGO DOOR SILL HAS CORROSION AROUND NUTPLATE HOLES FS 574 TO 621. C-CHECK, RO 12/10/14, BLENDED LT CARGO DOOR SILL CORROSION AROUND NUTPLATE HOLES FS 574 TO 621 REF SRM, BLEND OUT OF LIMITS. R & R LT CARGO DOOR SILL REF SRM & REO.
- [SDR SWIA201440371](https://openairdocs.org/sdr/SWIA201440371.md): Bulkhead · damaged · Nov 24, 2014 · N913SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FWD FACE OF FS 621 REAR PRESSURE BULKHEAD HAS SCREW STRIKES BETWEEN ISOLATOR MOUNTS AS MARKED. C-CHECK, RO 12/10/14. BLENDED SEVERAL AREAS OF SCREW NICKS ON FS 621 AT ISOLATOR MOUNTS REF SRM. FOUND TO BE WITHIN LIMITS REF REO.
- [SDR SWIA201440369](https://openairdocs.org/sdr/SWIA201440369.md): Trunnion · damaged · Nov 24, 2014 · N913SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > FOUND AN OVERSIZED HOLE ON LT TRUNNION. REPAIRED THE LT TRUNION IAW REO.

Next page: https://openairdocs.org/deregistered/N913SW-2023-01-24/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 = 'N913SW' AND deregistration_id = 'N913SW-2023-01-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N913SW-2023-01-24/reports

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