# Service difficulty reports: N417SW, cancelled Nov 5, 2022

A list on [N417SW, cancelled Nov 5, 2022](https://openairdocs.org/deregistered/N417SW-2022-11-05.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 · 148 reports

- [SDR SWIA202156493](https://openairdocs.org/sdr/SWIA202156493.md): Warning Message · false activation · Mar 2, 2021 · N417SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > D:GEAR DISAGREE WARNING WHEN DEPLOYING GEAR DN FOR LANDING. THE WARNING WAS BRIEF, ONLY A SECOND OR TWO, ACCOMPANIED BY A NOSE DOOR OPEN WARNING. ALL 3 GEAR INDICATED DOWN AND LOCKED, THEN BOTH WARNING MESSAGES CLEARED. COMPLETED QRH WHERE APPLICABLE WITH NO C
- [SDR SWIA2019080146110](https://openairdocs.org/sdr/SWIA2019080146110.md): Cap · cracked · Jun 12, 2019 · N417SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 9 BEAM CAP FROM FS409+4 TO FS409+118 CRACKED. REPLACED FLOOR BEAM CAP FROM FS409+4 TO FS409+118 IAW REO.
- [SDR SWIA2019080146109](https://openairdocs.org/sdr/SWIA2019080146109.md): Floor Support · corroded · Jun 6, 2019 · N417SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON THE LEFT HAND FLOOR SILL FS409.00+96 - FS409.00+128. C-CHECK. REPAIRED LEFT HAND FLOOR SILL IAW REO AND SRM.
- [SDR SWIA2019080146111](https://openairdocs.org/sdr/SWIA2019080146111.md): Skin · chafed · Jun 4, 2019 · N417SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN HAS SEVERAL CHAFES/SCRATCHES AT APU EXHAUST OPENING AFT END. REPAIRED IAW REO.
- [SDR SWIA2019080146112](https://openairdocs.org/sdr/SWIA2019080146112.md): Plate · corroded · May 30, 2019 · N417SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR BOTTOM PLATE ASSEMBLY CORRODED. INSTALLED NEW SERVICE DOOR BOTTOM PLATE ASSEMBLY IAW SRM.
- [SDR SWIA2019050145816](https://openairdocs.org/sdr/SWIA2019050145816.md): Bracket · failed · May 1, 2019 · N417SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WITH NOSE GEAR UNSAFE. PERFORMED QRH PROCEDURE AND LANDING GEAR CAME DOWN WITH NOSE DOOR UNSAFE MESSAGE ON. RECEIVED HYD 3 HI TEMP MESSAGE ON FINAL APPROACH. (FLT#5723) CLOSED REPLACED NOSE LANDING GEAR CENTERING SENSOR BRACKET IAW AMM AND PERFOR
- [SDR SWIA2019021945533](https://openairdocs.org/sdr/SWIA2019021945533.md): Unknown · noisy · Feb 19, 2019 · N417SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE UPON T/O WITH LOUD CLANKING NOISES. WHEN BRINGING THE GEAR DOWN FOR LANDING, LOUD CLANKING SOUND COULD BE HEARD AGAIN. (FLT#5011) CLOSED PERFORMED OPERATIONAL CHECK IAW AMM. SWUNG ALL LANDING GEARS MULTIPLE TIMES. COULD NOT DUPLICATE PROBLEM. OPS
- [SDR SWIA2018100245118](https://openairdocs.org/sdr/SWIA2018100245118.md): Uplock · failed · Oct 2, 2018 · N417SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON CLIMB OUT WE SELECTED GEAR UP. NOSE GEAR DID NOT COME UP AND WE GOT A GEAR DISAGREE WARNING MSG. RAN QRH AND ABOUT 30 SECONDS AFTER TURNING ON HYDRAULIC PUMPS, NOSE GEAR CAME UP. ON LANDING, GEAR CAME DOWN NORMALLY. REPOSITION FLIGHT - NO PAX (FLT 1357) CLO
- [SDR SWIA2018072644904](https://openairdocs.org/sdr/SWIA2018072644904.md): Coalescer Bag · odor · Jul 26, 2018 · N417SW · Cndair CL6002B19 · Humidity Control System
  > PACKS GAVE OFF A BURNING SMELL IN FLIGHT IN BOTH THE CABIN AND COCKPIT. (FLT 3134) CLOSED REMOVED AND REPLACED RT AND LT WATER SEPARATOR COALESCERS, IAW AMM. UPON OPERATIONAL TEST OF THE PACKS, FOUND NO SMELL PRESENT IN COCKPIT OR GALLEY. ALSO REMOVED AND REPL
- [SDR SWIA201743408](https://openairdocs.org/sdr/SWIA201743408.md): Angle · corroded · Jun 6, 2017 · N417SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL CORRODED. INSTALLED NEW DOOR SILL ANGLE IAW SRM.
- [SDR SWIA201743407](https://openairdocs.org/sdr/SWIA201743407.md): Stiffener · gouged · Jun 5, 2017 · N417SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > GOUGE LOCATED ON BACK SIDE OF REAR PRESSURE BULKHEAD ON UPPER VERTICAL STIFFENER AT BS 621, BL 0. REPAIRED THE STIFFENER IAW REO.
- [SDR SWIA201743404](https://openairdocs.org/sdr/SWIA201743404.md): Frame · corroded · Jun 4, 2017 · N417SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AVIONICS BAY FRAME BS 333 CORRODED STRINGERS 25L - 26R. REMOVED AND REPLACED THE FRAME SECTOR IAW SRM.
- [SDR SWIA201743406](https://openairdocs.org/sdr/SWIA201743406.md): Skin · chafed · Jun 3, 2017 · N417SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE CHAFED ON OTBD SIDE. REMOVED THE WORN OUT OF LIMITS LEADING EDGE SKIN CAP FROM THE RIGHT HAND INBOARD FLAP OUTBOARD SECTION AND INSTALLED NEW SKIN IAW SRM.
- [SDR SWIA201743403](https://openairdocs.org/sdr/SWIA201743403.md): Pressure Deck · cracked · Jun 3, 2017 · N417SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR SKIN CRACKED BS 459, RBL 3 & 7. REPAIRED PRESSURE FLOOR IAW REO. PRESSURE CHECKED OKAY.
- [SDR SWIA201743405](https://openairdocs.org/sdr/SWIA201743405.md): Skin · chafed · Jun 2, 2017 · N417SW · Cndair CL6002B19 · Ailerons
  > LEFT AILERON UPPER SKIN LEADING EDGE CHAFED. REPLACED THE AILERON UPPER LE SKIN IAW SRM.
- [SDR SWIA201743402](https://openairdocs.org/sdr/SWIA201743402.md): Bulkhead · cracked · Jun 2, 2017 · N417SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 REAR PRESSURE BULKHEAD FORWARD FACE CRACKED AT BL 0, 58 INCHES ABOVE FLOOR. REPAIRED THE PRESSURE BULKHEAD IAW REO.
- [SDR SWIA201743401](https://openairdocs.org/sdr/SWIA201743401.md): Fitting · worn · Jun 2, 2017 · N417SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > MLG BAY FORWARD FAIRING RIGHT SIDE ATTACH FITTINGS WORN OUT OF LIMITS. REMOVED AND REPLACED THE FAIRING FITTINGS IAW SRM.
- [SDR SWIA201743400](https://openairdocs.org/sdr/SWIA201743400.md): Skin · dented · May 30, 2017 · N417SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED BETWEEN BS 409+16 & 409+32, STRINGER 18 & 19L. REPAIRED IAW REO.
- [SDR SWIA201743075](https://openairdocs.org/sdr/SWIA201743075.md): Skin · damaged · Feb 16, 2017 · N417SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND HOLE IN SKIN ON TOP OF FUSELAGE APPROXIMATELY BS 605 ABOUT 12 INCHES LT OF CENTERLINE. REPAIRED THE SKIN IAW SRM.
- [SDR SWIA201642373](https://openairdocs.org/sdr/SWIA201642373.md): Switch · failed · Jul 30, 2016 · N417SW · Cndair CL6002B19 · Cabin Cooling System
  > LEFT PACK DEFERRED. RIGHT PACK HIGH TEMP AND SHUTDOWN. CREW DEPLOYED O2 MASKS AND DECLARED EMERGENCY. RETURNED TO FIELD. R & R RT PACK OVER TEMPERATURE COMPRESSOR SWITCH IAW AMM. OPS CHECK GOOD AT THIS TIME. PN ON 750659-17AEC, SN ON 0093, PN OFF 750659-
- [SDR SWIA201642372](https://openairdocs.org/sdr/SWIA201642372.md): Shutoff Valve · failed · Jul 29, 2016 · N417SW · Cndair CL6002B19 · Cabin Cooling System
  > LEFT PACK DEFERRED. RT PACK AUTO SHUTDOWN. CREW DECLARED EMERGENCY. RETURNED TO FIELD. R & R PRESSURE REGULATING/SHUTOFF VALVE IAW AMM. PN ON 979998-2 SNON 5336, PN OFF 979998-2, SN OFF 4453. R & R BLEED AIR SHUTOFF VALVE IAW AMM. PN ON 3215622-1, SN ON
- [SDR SWIA201541649](https://openairdocs.org/sdr/SWIA201541649.md): Outflow Valve · obstructed · Nov 30, 2015 · N417SW · Cndair CL6002B19 · Pressure Regulator/Outflow Valve
  > AT CABIN ALTITUDE CAUTION MESSAGE, DESCENDED TO FL 240 DURING DESCENT CABIN ALTITUDE CLIMBED QUICKLY AND MASK DROPPED. RAN QRH FOR EMERGENCY DESCENT. DIVERTED, FOUND A LARGE PIECE OF INSULATION BLANKET STUCK IN THE PRIMARY OUT FLOW VALVE, NOT ALLOWING IT TO
- [SDR SWIA201541269](https://openairdocs.org/sdr/SWIA201541269.md): Frame · cracked · May 7, 2015 · N417SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME AT BS 589 OUTER FLANGE IS CRACKED COMMON TO STRINGER 18L. REPAIRED THE FRAME IAW EA.
- [SDR SWIA201541268](https://openairdocs.org/sdr/SWIA201541268.md): Frame · cracked · May 7, 2015 · N417SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME AT BS 605 OUTER FLANGE IS CRACKED AT FASTENERS COMMON TO STR 18L. REPAIRED THE FRAME IAW EA.
- [SDR SWIA201541266](https://openairdocs.org/sdr/SWIA201541266.md): Bulkhead · cracked · May 7, 2015 · N417SW · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > CRACKS ON FS 280 BULKHEAD WEB AT LBL 9 AND RBL 9. COMPLIED WITH REPAIR TO BULKHEAD WEB FS 280.00 LBL 20.75-RBL 20.75 IAW REO.
- [SDR SWIA201541267](https://openairdocs.org/sdr/SWIA201541267.md): Panel · out of tolerance · May 3, 2015 · N417SW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > HORIZONTAL STABILIZER VISOR PANEL 326AR FAILED GAP CHECK. RECONTOURED VISOR PANEL 326AR IAW REO AND AMM.
- [SDR SWIA201541265](https://openairdocs.org/sdr/SWIA201541265.md): Angle · damaged · Apr 29, 2015 · N417SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 559 LOWER CAP ANGLES BL 9.00 AND 18.00 LT SIDE AND RT SIDE. REPAIR AND REINFORCEMENT FOR FS559.00 LOWER CAP ANGLES BL 9.00 AND 18.00 LT SIDE AND RT SIDE IAW REO.
- [SDR SWIA201440292](https://openairdocs.org/sdr/SWIA201440292.md): Structure · damaged · Dec 4, 2014 · N417SW · Cndair CL6002B19 · Fuselage Main, Structure
  > MULTIPLE BIRD STRIKE DAMAGING RT L/E AND LT NOSE AND FUSELAGE DURING LANDING. REPAIRED IAW REO.
- [SDR SWIA201439205](https://openairdocs.org/sdr/SWIA201439205.md): Battery Pack · inoperative · Aug 24, 2014 · N417SW · Cndair CL6002B19 · Emergency Equipment
  > F/A FLASHLIGHT IS INOPERATIVE. REPLACED FLASHLIGHT BATTERIES.
- [SDR SWIA201438510](https://openairdocs.org/sdr/SWIA201438510.md): Wire Harness · damaged · Jun 30, 2014 · N417SW · Cndair CL6002B19 · Landing Gear System Wiring
  > EXTENDED GEAR AND IT TOOK ABNORMALLY LONG TIME TO COME DOWN. LOUD POPPING SOUND FROM NOSE WHEEL. OVERFLEW AIRPORT. ATC CONFIRMED GEAR DOWN BEFORE LANDING. COULD NOT DUPLICATE. R & R THE NLG DOWNLOCK WIRE HARNESS IAW AMM.
- [SDR SWIA2014061738206](https://openairdocs.org/sdr/SWIA2014061738206.md): Light · inoperative · Jun 16, 2014 · N417SW · Cndair CL6002B19 · Emergency Lighting
  > RIGHT AFT EMERGENCY LIGHT INOPERATIVE. R & R RT AFT EMERGENCY LIGHT IAW AMM.
- [SDR SWIA201436673](https://openairdocs.org/sdr/SWIA201436673.md): Bushing · corroded · Mar 12, 2014 · N417SW · Cndair CL6002B19 · Engine Mount Section
  > DURING C-CHECK, LEFT ENGINE MOUNT LINK BUSHINGS FOUND PITTED AND WORN., REPLACED LT ENGINE MOUNT LINK BUSHINGS IAW AMM.
- [SDR SWIA201335657](https://openairdocs.org/sdr/SWIA201335657.md): Light · inoperative · Dec 17, 2013 · N417SW · Cndair CL6002B19 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT IN AFT CABIN IS BURNED OUT. FLT 2598 RELAMPED.
- [SDR SWIA201335473](https://openairdocs.org/sdr/SWIA201335473.md): Light · inoperative · Dec 3, 2013 · N417SW · Cndair CL6002B19 · Emergency Lighting
  > NR 2 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. SERVICE RELAMPED.
- [SDR SWIA201335190](https://openairdocs.org/sdr/SWIA201335190.md): Charger · failed · Nov 5, 2013 · N417SW · Cndair CL6002B19 · Emergency Lighting
  > FWD EMERGENCY OVERHEAD LIGHT DOES NOT ILLUMINATE. SERVICE REPLACED BATTERY CHARGER ASSEMBLY NR 1 IAW AMM.
- [SDR SWIA201334755](https://openairdocs.org/sdr/SWIA201334755.md): Paint · misinstalled · Sep 29, 2013 · N417SW · Cndair CL6002B19 · Trailing Edge Flaps
  > ON FINAL APPROACH AT APPROXIMATELY 1000' FT AGL, FLAPS 45°, ON SPEED, TRIMMED OUT. AIRCRAFT BEGAN SUDDEN LT ROLL WITH AUTOPILOT OFF. SIGNIFICANT RWD TRIM ADDED TO CORRECT & FLY AIRCRAFT. NO ASSOCIATED EICAS MESSAGES DISPLAYED. FLT#2583 FOUND EXCESSIVE PAI
- [SDR SWIA201334738](https://openairdocs.org/sdr/SWIA201334738.md): Light · inoperative · Sep 23, 2013 · N417SW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY CEILING POD LIGHT BURNED OUT. FLT#2636 RELAMPED.
- [SDR SWIA201334398](https://openairdocs.org/sdr/SWIA201334398.md): Transceiver · failed · Aug 28, 2013 · N417SW · Cndair CL6002B19 · Ground Proximity System
  > CONFIGURE WARNING & GROUND SPOILER DEPLOY MESSAGE. FLT#2643 REPLACED NR 1 RAD ALT TRANSCEIVER ALT-55B & NR 1 SECU IAW AMM. PN ON OFF 49-164-20, SN ON 03377, SN OFF 03060, PN ON OFF 622-2855-011, SN ON 21DJR & SN OFF 4PHW.
- [SDR SWIA201334103](https://openairdocs.org/sdr/SWIA201334103.md): Bulkhead · damaged · Jul 12, 2013 · N417SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > HOLE IN FS621 BULKHEAD ON LBL 31.4 & 2.3" ABOVE CARGO FLOOR. C-CHECK REPAIR TO FS621 BULKHEAD WEB. CUT AWAY DAMAGED AREA ON FS621 BULKHEAD WEB AT LBL 31.4 & 2.3" ABOVE CARGO FLOOR & INSTALLED DOUBLER FROM 2024-T3 IAW REO.
- [SDR SWIA201334105](https://openairdocs.org/sdr/SWIA201334105.md): Vane · chafed · Jul 10, 2013 · N417SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBD FLAP VANE CHAFED ON INBD END. C-CHECK BLENDED LT INBD FLAP VANE INBD END IAW REO.
- [SDR SWIA201334104](https://openairdocs.org/sdr/SWIA201334104.md): Vane · chafed · Jul 10, 2013 · N417SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBD FLAP VANE CHAFED ON OTBD END.. C-CHECK BLENDED LT INBD FLAP VANE OTBD END IAW REO.
- [SDR SWIA201334106](https://openairdocs.org/sdr/SWIA201334106.md): Post · cracked · Jul 9, 2013 · N417SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > VERTICAL POST ON FS409.0 +128 RBL 18.0 HAS CRACK ON INBD SIDE OF POST. C-CHECK REPLACED VERTICAL POST AT FS409.0 + 128 RBL 18.0 INBD SIDE IAW REO.
- [SDR SWIA201332974](https://openairdocs.org/sdr/SWIA201332974.md): Windshield · cracked · Mar 8, 2013 · N417SW · Cndair CL6002B19 · Flight Compartment Windows
  > F/O WINDSHIELD CRACKED IN CRUISE. (FLT 2611) REPLACED F/O WINDSHIELD IAW AMM. P/N: NP-139321-6 S/N ON: 2214H5385 S/N OFF: 2140R6529
- [SDR SWIA201231930](https://openairdocs.org/sdr/SWIA201231930.md): Buckle · out of adjust · Oct 8, 2012 · N417SW · Cndair CL6002B19 · Flight Compartment Equipment
  > FLIGHT ATTENDANT SEATBELT BUCKLE IS HARD TO UNLATCH. (FLT 6533) ADJUSTED FLIGHT ATTENDANT SEATBELT BUCKLE.
- [SDR SWIA201231733](https://openairdocs.org/sdr/SWIA201231733.md): Light · inoperative · Sep 10, 2012 · N417SW · Cndair CL6002B19 · Emergency Lighting
  > NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5658) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201231634](https://openairdocs.org/sdr/SWIA201231634.md): Light · inoperative · Aug 29, 2012 · N417SW · Cndair CL6002B19 · Emergency Lighting
  > NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5652) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201230484](https://openairdocs.org/sdr/SWIA201230484.md): Door · lack of lube · Apr 20, 2012 · N417SW · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 5232) LUBRICATED MAIN CABIN DOOR IN REF TO AMM.
- [SDR SWIA201229548](https://openairdocs.org/sdr/SWIA201229548.md): Light · inoperative · Feb 4, 2012 · N417SW · Cndair CL6002B19 · Emergency Lighting
  > NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6190) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201229293](https://openairdocs.org/sdr/SWIA201229293.md): Light · inoperative · Jan 18, 2012 · N417SW · Cndair CL6002B19 · Emergency Lighting
  > NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5327) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201229141](https://openairdocs.org/sdr/SWIA201229141.md): Light · inoperative · Jan 3, 2012 · N417SW · Cndair CL6002B19 · Emergency Lighting
  > NR 1 RIGHT SIDE OVERWING EMERGENCY LIGHT IS OUT. (FLT 5302) RELAMPED EMERGENCY LIGHT.

Next page: https://openairdocs.org/deregistered/N417SW-2022-11-05/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 = 'N417SW' AND deregistration_id = 'N417SW-2022-11-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N417SW-2022-11-05/reports

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