# Service difficulty reports: N937SW

A list on [N937SW](https://openairdocs.org/aircraft/N937SW.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 · 187 reports

- [SDR SWIA2019102846613](https://openairdocs.org/sdr/SWIA2019102846613.md): Oil Cooler · malfunctioned · Oct 27, 2019 · N937SW · Cndair CL6002B19 · APU Oil System
  > AT CRUISE FL250 APU OIL TEMP CAUTION MSG DIVERTED TO KLBB. (FLT#5831) CLOSED REMOVED AND REPLACED APU OIL COOLER IAW AMM. FOUND APU OIL LEVEL TO BE LOW AND SERVICED APU OIL IAW AMM. OPS AND LEAK CHECK GOOD.
- [SDR SWIA2019072346086](https://openairdocs.org/sdr/SWIA2019072346086.md): Uplock · malfunctioned · Jul 22, 2019 · N937SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > LEFT MAIN GEAR DID NOT EXTEND ON FIRST ATTEMPT. GEAR HANDLE WAS RAISED UNTIL ALL GEAR SHOWED UP. THE GEAR WAS LOWERED AND SHOWED DOWN AND LOCKED. (FLT#5063) FO: 07/23/2019 CLOSED REMOVED AND REPLACED LEFT MAIN GEAR UPLOCK ASSY. OPS CHECKS GOOD NO LEAKS NOTED A
- [SDR SWIA2019052245908](https://openairdocs.org/sdr/SWIA2019052245908.md): Unknown · malfunctioned · May 22, 2019 · N937SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE ON CLIMB OUT 8,000 FEET. RIGHT MAIN DID NOT RETRACT. QRH PROCEDURE FOLLOWED. RTF. (FLT#5699) CLOSED / INTERROGATED PSEU AND FLAGGED R GEAR UP LOCK S18. JACKED AND SWUNG GEAR SEVERAL TIMES AND COMPLIED WITH FREE FALL IAW AMM. WITH NO DEFECTS NOT
- [SDR SWIA2018110945257](https://openairdocs.org/sdr/SWIA2018110945257.md): Warning Message · illuminated · Nov 8, 2018 · N937SW · Cndair CL6002B19 · Engine Oil Pressure
  > LEFT ENGINE OIL PRESSURE WARNING INFLIGHT. RAN QRH - FLIGHT CREW SHUTDOWN THE ENGINE. DIVERTED. (FLT#5073) FO: 11/09/2018 CLOSED REMOVED AND REPLACED LH ENGINE IAW AMM. OPS, RIG AND LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA2018062644835](https://openairdocs.org/sdr/SWIA2018062644835.md): Angle · corroded · Jun 5, 2018 · N937SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND CORROSION ON CARGO SURROUND LOWER COAMING, ON ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM.
- [SDR SWIA2018062644834](https://openairdocs.org/sdr/SWIA2018062644834.md): Hinge · gouged · Jun 2, 2018 · N937SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE AFT LAND WAS GOUGED. REPLACED THE DOOR HINGE IAW REO.
- [SDR SWIA2018062644833](https://openairdocs.org/sdr/SWIA2018062644833.md): Skin · dented · Jun 1, 2018 · N937SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PROTRUDING DENT FWD. OF BS 654.5, BETWEEN STRINGERS. 25R AND 26R. REPAIRED THE SKIN IAW REO.
- [SDR SWIA2018062644832](https://openairdocs.org/sdr/SWIA2018062644832.md): Skin · dented · Jun 1, 2018 · N937SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TWO PROTRUDING DENTS BETWEEN BS 682 AND 672.2, STRINGERS 25R AND 26R. REPAIRED THE SKIN IAW REO.
- [SDR SWIA2018062644831](https://openairdocs.org/sdr/SWIA2018062644831.md): Nose Cowl · dented · May 29, 2018 · N937SW · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > TWO DENTS ON THE LT ENGINE LIP SKIN AT THE 9 O'CLOCK POSITION. INSTALLED A NEW NOSE COWL ASSEMBLY IAW AMM.
- [SDR SWIA201744081](https://openairdocs.org/sdr/SWIA201744081.md): Bracket · bent · Dec 18, 2017 · N937SW · Cndair CL6002B19 · Main Landing Gear Attach Section
  > GEAR DISAGREE WITH NOSE DOOR OPEN WARNING MESSAGE. REPAIRED A BENT PROXIMITY BRACKET, ADJUSTED NLG SENSOR EXTENDED PROXIMITY SENSOR IAW AMM. JACKED AND SWUNG NLG IAW AMM. NO DEFECTS NOTED AT THIS TIME.
- [SDR SWIA2017120544010](https://openairdocs.org/sdr/SWIA2017120544010.md): Selector Valve · failed · Nov 27, 2017 · N937SW · Cndair CL6002B19 · Landing Gear Selector
  > AFTER GEAR RETRACTION ON CLIMBOUT THE NOSE GEAR STARTED TO SHUTTER AND WAS FOLLOWED BY A GEAR DISAGREE WARNING MSG. AFTER RUNNING THE QRH, THE MESSAGE WENT OUT AND LANDED / TAXIED NORMALLY. RETURNED TO FIELD. (FLT 5490) CLOSED REMOVED AND REPLACED NLG SELECTOR
- [SDR SWIA201642229](https://openairdocs.org/sdr/SWIA201642229.md): Floor Support · damaged · Jun 1, 2016 · N937SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO BAY FLOOR SUPPORT BETWEEN FS 562.72-621 DAMAGED. REPAIRED CARGO FLOOR SUPPORT IAW REO.
- [SDR SWIA201642228](https://openairdocs.org/sdr/SWIA201642228.md): Reinforcement · cracked · May 21, 2016 · N937SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CRACK FOUND ON REINFORCEMENT ANGLE OF FRAME AT BS 574 COMMON TO STR 20L. REPLACED REINFORCEMENT ANGLE FOR FRAME AT FS 574 COMMON TO STR 20L IAW STS EA. FUSELAGE PRESSURE LEAK TEST GOOD.
- [SDR SWIA201642227](https://openairdocs.org/sdr/SWIA201642227.md): Frame · corroded · May 20, 2016 · N937SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS 574, STGR 19L HAS EXFOLIATION CORROSION DAMAGE. R & R FRAME SECTOR AT FS 574.00 BETWEEN STR 6L-20L WITH SERVICEABLE PART IAW SRM. FUSELAGE PRESSURE LEAK CHECK GOOD.
- [SDR SWIA201642226](https://openairdocs.org/sdr/SWIA201642226.md): Bulkhead · dented · May 17, 2016 · N937SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > THE FORWARD SIDE OF THE AFT PRESSURE BULKHEAD, FS 621, HAS A DENT APPROXIMATELY 2" ABOVE THE FLOOR LEVEL JUST INBD OF LBL 27. COMPLIED WITH PERMANENT REPAIR OF FS 621.00 PRESSURE BULKHEAD WEB BETWEEN LBL 18.00 AND LBL 27.50 IAW REO. FUSELAGE PRESSURE LEAK CH
- [SDR SWIA201642235](https://openairdocs.org/sdr/SWIA201642235.md): Frame · corroded · May 16, 2016 · N937SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME AT APPROXIMATELY FS 574. REPLACED THE FRAME SECTION IAW REO. PRESSURE LEAK CHECKED GOOD.
- [SDR SWIA201642234](https://openairdocs.org/sdr/SWIA201642234.md): Floorbeam · corroded · May 16, 2016 · N937SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON UPPER FLOORBEAM AT APPROXIMATELY BS 605. REPAIRED IAW EA.
- [SDR SWIA201642225](https://openairdocs.org/sdr/SWIA201642225.md): Frame · corroded · May 16, 2016 · N937SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON LOWER FRAME APPROXIMATELY FS 605 LOWER CENTER FUSELAGE. R & R LOWER FRAME SECTOR LOCATED AT FS 605 WITH SERVICEABLE PART IAW REO. FUSELAGE PRESSURE LEAK CHECK GOOD.
- [SDR SWIA201642224](https://openairdocs.org/sdr/SWIA201642224.md): Pressure Deck · cracked · May 14, 2016 · N937SW · Cndair CL6002B19 · Fuselage Floor Panel
  > FS 460, IN BETWEEN LBL9.0 AND RBL 9.0 UNDER FLOORBOARD THERE IS A CRACK ON PRESSURE FLOOR. REPAIRED PRESSURE FLOOR AT FS 460 BETWEEN LBL 9.0 AND RBL 9.0 IAW REO. FUSELAGE PRESSURE LEAK CHECK GOOD.
- [SDR SWIA201642233](https://openairdocs.org/sdr/SWIA201642233.md): Vane · worn · May 13, 2016 · N937SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE L/E WORN FROM STOP AT APPROXIMATELY 6" FROM OTBD SIDE. REMOVED AND INSTALLED NEW OTBD VANE CAP FOR RT INBD FLAP, FLAP VANE L/E SKIN IAW SRM.
- [SDR SWIA201642232](https://openairdocs.org/sdr/SWIA201642232.md): Hinge · gouged · May 11, 2016 · N937SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > SERVICE DOORS CENTER HINGE IS GOUGED ON TOP AND BOTTOM OF THE HINGE. REPAIRED GOUGES ON TOP AND BOTTOM OF HINGE ON SERVICE DOOR IAW REO AND ADJUSTED SERVICE DOOR IAW AMM. OPS CHECK GOOD.
- [SDR SWIA201642231](https://openairdocs.org/sdr/SWIA201642231.md): Skin · dented · May 10, 2016 · N937SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT APPROXIMATELY AT BS 625 AT STRG 20L. REPAIRED IAW EA.
- [SDR SWIA201642230](https://openairdocs.org/sdr/SWIA201642230.md): Skin · dented · May 10, 2016 · N937SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT OTBD FLAP HAS DENTS. REPAIRED IAW STS EA.
- [SDR SWIA201641938](https://openairdocs.org/sdr/SWIA201641938.md): Strut · discharged · Mar 7, 2016 · N937SW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > MLG DISAGREE ON CLIMBOUT, NOSE GEAR DOOR WARNING AND WOW CAUTION. SERVICED NLG STRUT IAW AMM. CYCLED GEAR SEVERAL TIMES, NO FAULTS.
- [SDR SWIA201440296](https://openairdocs.org/sdr/SWIA201440296.md): Battery Pack · failed · Dec 6, 2014 · N937SW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS STAY ON IN ARMED POSITION. R & R BATTERY PACKS 2, 3, AND 4 IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR SWIA201439163](https://openairdocs.org/sdr/SWIA201439163.md): Charger · inoperative · Aug 17, 2014 · N937SW · Cndair CL6002B19 · Emergency Lighting
  > FORWARD FACING OVERHEAD EXIT ROW EXIT LIGHT OUT. R & R NR 2 EMERGENCY LIGHT BATTERY CHARGER AND NR 2 EMERGENCY LIGHT BATTERY PACK IAW AMM.
- [SDR SWIA201439017](https://openairdocs.org/sdr/SWIA201439017.md): Battery Pack · discharged · Aug 10, 2014 · N937SW · Cndair CL6002B19 · Emergency Lighting
  > AFT EMERGENCY LIGHTS INOPERATIVE. CHARGED THE BATTERIES.
- [SDR SWIA201438769](https://openairdocs.org/sdr/SWIA201438769.md): Support Bracket · cracked · Jul 14, 2014 · N937SW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED SUPPORT BRACKET, LT ENGINE, AFT OF NOSE COWL AT 12 O`CLOCK. C-CHECK, REMOVED SUPPORT BRACKET AND INSTALLED REPAIRED BRACKET IAW REO.
- [SDR SWIA201438771](https://openairdocs.org/sdr/SWIA201438771.md): Cup · corroded · Jul 10, 2014 · N937SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT HAND RAIL CUP ATTACHED TO PAX DOOR LOWER SILL ANGLE CORRODED. LOCATED AND DRILLED NEW AFT HAND RAIL CUP IAW SRM.
- [SDR SWIA201438770](https://openairdocs.org/sdr/SWIA201438770.md): Cup · corroded · Jul 10, 2014 · N937SW · Cndair CL6002B19 · Passenger/Crew Doors
  > FWD HAND RAIL CUP ATTACHED TO PAX DOOR LOWER SILL ANGLE CORRODED. LOCATED AND DRILLED NEW FWD HAND RAIL CUP IAW SRM.
- [SDR SWIA201438773](https://openairdocs.org/sdr/SWIA201438773.md): Angle · cracked · Jul 6, 2014 · N937SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT INTERCOSTAL ANGLE AT FS 621, STRINGER 14 LT, CRACKED. C-CHECK, R & R LT INTERCOSTAL ANGLE IAW SRM.
- [SDR SWIA201438772](https://openairdocs.org/sdr/SWIA201438772.md): Angle · cracked · Jul 6, 2014 · N937SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT INTERCOSTAL ANGLE AT BS 621, STRINGER 14 RT, CRACKED. C-CHECK, R & R RT INTERCOSTAL ANGLEIAW SRM.
- [SDR SWIA201438774](https://openairdocs.org/sdr/SWIA201438774.md): Structure · chafed · Jul 5, 2014 · N937SW · Cndair CL6002B19 · Landing Gear Doors
  > LT MLG DOOR CHAFED AT MOST FWD POINT. C-CHECK, R & R DAMAGED FILLER IAW REO.
- [SDR SWIA201438779](https://openairdocs.org/sdr/SWIA201438779.md): Rib · corroded · Jul 3, 2014 · N937SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT OTBD FLAP CORRODED ON INTERNAL RIB INBD OF FLAP STATION 254.96. C-CHECK, REMOVED RT OTBD FLAP AND INSTALLED A NEW FLAP IAW AMM.
- [SDR SWIA201438778](https://openairdocs.org/sdr/SWIA201438778.md): Bellcrank · chafed · Jul 3, 2014 · N937SW · Cndair CL6002B19 · Landing Gear Door Retract Section
  > LEFT MLG DOOR BELLCRANK ASSY CHAFED ON LOWER OTBD SIDE. C-CHECK, R & R BELLCRANK ASSY IAW AMM AND REO.
- [SDR SWIA201438777](https://openairdocs.org/sdr/SWIA201438777.md): Bellcrank · chafed · Jul 3, 2014 · N937SW · Cndair CL6002B19 · Landing Gear Door Retract Section
  > RT MLG DOOR BELLCRANK ASSY CHAFED ON LOWER OTBD SIDE. C-CHECK, BLENDED CHAFE ON RT MLG DOOR BELL CRANK ASSY LOWER OTBD SIDE IAW REO.
- [SDR SWIA201438776](https://openairdocs.org/sdr/SWIA201438776.md): Bulkhead · cracked · Jul 3, 2014 · N937SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 202 BULKHEAD HYD BAY WHERE EMERGENCY BRAKE ROD COMES THROUGH HOLE. C-CHECK, REPAIRED BULKHEAD IAW REO.
- [SDR SWIA201438775](https://openairdocs.org/sdr/SWIA201438775.md): Frame · cracked · Jul 3, 2014 · N937SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 193, LT SIDE FRAME CRACKED TRU BAY FLOOR. C-CHECK, PERFORMED PERMANENT REPAIR IAW REO.
- [SDR SWIA201438801](https://openairdocs.org/sdr/SWIA201438801.md): Lever · chafed · Jul 2, 2014 · N937SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FWD PULL-IN LEVER CHAFED. C-CHECK, BLENDED OUT DAMAGE ON FWD PULL-IN LEVER IAW REO.
- [SDR SWIA201438800](https://openairdocs.org/sdr/SWIA201438800.md): Wheel · chafed · Jul 2, 2014 · N937SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR SUPPORT WHEEL ARM CHAFED ON STAIR RAIL. C-CHECK, BLENDED OUT DAMAGE AND RESTORED FINISH TO THE PASSENGER DOOR SUPPORT WHEEL ARM IAW STS EA.
- [SDR SWIA201438799](https://openairdocs.org/sdr/SWIA201438799.md): Flap · chafed · Jul 2, 2014 · N937SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR VENT FLAP CHAFED IN TWO PLACE FROM ICE BREAK CABLE. C-CHECK, REPAIRED CHAFES TO PAX DOOR PRESSURE VENT FLAP IAW REO.
- [SDR SWIA201438798](https://openairdocs.org/sdr/SWIA201438798.md): Guide · chafed · Jul 2, 2014 · N937SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FORWARD UPPER GUIDE CHAFED. C-CHECK, MEASURED THE DEPTH OF THE CHAFING ON THE FWD UPPER PAX DOOR CENTERING PLATE AT.022". MAXIMUM ALLOWABLE DEPTH OF DAMAGE IS.040"? IAW REO. THIS DAMAGE IS WITHIN LIMITS.
- [SDR SWIA201438797](https://openairdocs.org/sdr/SWIA201438797.md): Guide · chafed · Jul 2, 2014 · N937SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT UPPER GUIDE CHAFED. C-CHECK, MEASURED THE DEPTH OF THE CHAFING ON THE AFT. UPPER PAX DOOR CENTERING PLATE AT.014"? MAXIMUM ALLOWABLE DEPTH OF DAMAGE IS.040"? IAW REO. THIS DAMAGE IS WITHIN LIMITS. NO FURTHER ACTION NECESSARY.
- [SDR SWIA201438796](https://openairdocs.org/sdr/SWIA201438796.md): Door Sill · corroded · Jul 2, 2014 · N937SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR LOWER SILL ANGLE CORRODED. C-CHECK, R & R PAX DOOR LOWER SILL ANGLE IAW SRM.
- [SDR SWIA201438795](https://openairdocs.org/sdr/SWIA201438795.md): Floorbeam · corroded · Jul 2, 2014 · N937SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AND CAP AT FS 349, LBL 36-20. C-CHECK, REPLACED FLOORBEAM ANGLE AT FS 349 BETWEEN LBL 36-LBL 20 IAW SRM.
- [SDR SWIA201438794](https://openairdocs.org/sdr/SWIA201438794.md): Structure · chafed · Jul 2, 2014 · N937SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT SIDE LOWER CENTER WING, CHAFING AT PANEL 193AB. C-CHECK, BLENDED AND REPAIRED IAW REO.
- [SDR SWIA201438793](https://openairdocs.org/sdr/SWIA201438793.md): Floor Support · corroded · Jul 2, 2014 · N937SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE CORROSION ON FLOOR SUPPORT FOR FLOOR PANEL 196AL. C-CHECK, REPAIRED IAW SRM.
- [SDR SWIA201438792](https://openairdocs.org/sdr/SWIA201438792.md): Hinge · gouged · Jul 2, 2014 · N937SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE LUG 1, FROM FWD END GOUGED. C-CHECK, REPAIRED HINGE IAW REO.
- [SDR SWIA201438791](https://openairdocs.org/sdr/SWIA201438791.md): Hinge · gouged · Jul 2, 2014 · N937SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE, LUG 10 FROM FWD END GOUGED. REPAIRED HINGE IAW REO.
- [SDR SWIA201438790](https://openairdocs.org/sdr/SWIA201438790.md): Hinge · gouged · Jul 2, 2014 · N937SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE, LUG 13 FROM FWD END GOUGED. C-CHECK, REPAIRED HINGE IAW REO.

Next page: https://openairdocs.org/aircraft/N937SW/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 = 'N937SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N937SW/reports

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