# Service difficulty reports: N983CA, cancelled Jun 8, 2017

A list on [N983CA, cancelled Jun 8, 2017](https://openairdocs.org/deregistered/N983CA-2017-06-08.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 · 167 reports

- [SDR SWIA201440173](https://openairdocs.org/sdr/SWIA201440173.md): Wire Harness · faulty · Nov 26, 2014 · N983CA · Cndair CL6002B19 · Landing Gear System Wiring
  > WOW INPUT CAUTION MESSAGE RECEIVED DURING GEAR RETRACTION. MESSAGE DISAPPEARED AFTER LANDING GEAR REACHED SELECTED POSITION. FLT 2378. REPLACED RT OTBD MAIN HARNESS SUB ASSEMBLY IAW AMM. PERFORMED GEAR SWING, SYS OPS CK GOOD, PN TR17300-130-00-001-1.
- [SDR SWIA201440003](https://openairdocs.org/sdr/SWIA201440003.md): Pcu · failed · Nov 18, 2014 · N983CA · Cndair CL6002B19 · Hydraulic System, Main
  > DIVERTED DUE TO HYD 2A LOW PRESSURE CAUTION AT CRUISE. R & R PCU ASSY IAW AMM. OPS CHECK GOOD, NO LEAKING NOTED.
- [SDR SWIA201439644](https://openairdocs.org/sdr/SWIA201439644.md): Seat Track · damaged · Oct 12, 2014 · N983CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT SIDE AFT SEAT TRACK HAS DAMAGE BS 559.0+54. C-CHECK, THE DAMAGE WAS TRIMMED, NDT ENSURED A CRACK FREE CONDITION, AND THE REWORKED AREA WAS RESTORED TO MATCH IAW EA.
- [SDR SWIA201439651](https://openairdocs.org/sdr/SWIA201439651.md): Floor Support · corroded · Oct 10, 2014 · N983CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT UPPER CAP AT LBL 9 BS 569-619. C-CHECK, REPLACED THE FLOOR SUPPORT IAW SRM AND REO.
- [SDR SWIA201439650](https://openairdocs.org/sdr/SWIA201439650.md): Floor Support · corroded · Oct 10, 2014 · N983CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT UPPER CAP AT LBL 27 BS 569-619. C-CHECK, REPLACED THE FLOOR SUPPORT IAW REO.
- [SDR SWIA201439649](https://openairdocs.org/sdr/SWIA201439649.md): Strap · corroded · Oct 8, 2014 · N983CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR STRAP AT BS 310 TO 280, LBL 36 CORROSION OUT OF LIMITS. C-CHECK, REMOVED AND INSTALLED NEW FABRICATED FLOOR CAP STRAP, PN: 601R38670-55 IAW SRM.
- [SDR SWIA201439660](https://openairdocs.org/sdr/SWIA201439660.md): Skin · chafed · Oct 7, 2014 · N983CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBD FLAP VANE L/E SKIN OTBD END CHAFED. REPLACED THE SKIN IAW SRM AND REO.
- [SDR SWIA201439659](https://openairdocs.org/sdr/SWIA201439659.md): Skin · chafed · Oct 7, 2014 · N983CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INB FLAP VANE L/E SKIN AT INBD END CHAFED. REPLACED THE SKIN IAW SRM AND REO.
- [SDR SWIA201439658](https://openairdocs.org/sdr/SWIA201439658.md): Skin · chafed · Oct 7, 2014 · N983CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBD FLAP VANE L/E SKIN CHAFED. REPLACED THE SKIN IAW REO.
- [SDR SWIA201439664](https://openairdocs.org/sdr/SWIA201439664.md): Floor Support · corroded · Oct 6, 2014 · N983CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > UPPER FLOOR SUPPORT AT FS 609 AND 603, LBL 9 HAS CORROSION AT NUTPLATE LOCATIONS. C-CHECK, RO: 10/21/2014, REPLACED FLOOR SUPPORT UPPER CAP ANGLE AT LBL 9 FS 569 - FS 619, PN: 601R35031-3, IAW SRM AND REO.
- [SDR SWIA201439663](https://openairdocs.org/sdr/SWIA201439663.md): Support · mechanic error · Oct 6, 2014 · N983CA · Cndair CL6002B19 · Wing Main, Frame Structure
  > RIGHT WING L/E SUPPORT STRUCTURE DAMAGED AT TACK RIVET LOCATIONS AT WS 341, UPPER AND LOWER SUPPORT FLANGE. C-CHECK, PERFORMED PERMANENT REPAIR ON RT WING L/E SUPPORT STRUCTURE IAW STS EA.
- [SDR SWIA201439662](https://openairdocs.org/sdr/SWIA201439662.md): Hinge · gouged · Oct 6, 2014 · N983CA · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE HALF ON DOOR SIDE HAS GOUGES AT LUGS NR 8, NR 10 AND LAST LUG, FROM FWD TO AFT OF ACFT. REPAIRED IAW REO.
- [SDR SWIA201439655](https://openairdocs.org/sdr/SWIA201439655.md): Bulkhead Web · cracked · Oct 6, 2014 · N983CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621, BULKHEAD WEB HAS CRACK AT LBL 27.5 AT TOP OF CARGO DOOR TRACK. C-CHECK, REPAIRED IAW REO.
- [SDR SWIA201439654](https://openairdocs.org/sdr/SWIA201439654.md): Bulkhead Web · cracked · Oct 6, 2014 · N983CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621, BULKHEAD WEB HAS TWO CRACKS AT RBL 27.5. C-CHECK, REPAIRED IAW REO.
- [SDR SWIA201439653](https://openairdocs.org/sdr/SWIA201439653.md): Stiffener · cracked · Oct 6, 2014 · N983CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 409+128 VERTICAL POST AT RBL 18.0 IS CRACKED ON INBD AFT RADIUS. C-CHECK, R & R THE POST IAW SRM.
- [SDR SWIA201439652](https://openairdocs.org/sdr/SWIA201439652.md): Stiffener · cracked · Oct 6, 2014 · N983CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409 +128 VERTICAL POST AT BL 0 IS CRACKED ON LT SIDE AFT RADIUS. C-CHECK, R & R VERTICAL POST IAW REO.
- [SDR SWIA201439648](https://openairdocs.org/sdr/SWIA201439648.md): Door Sill · cracked · Oct 6, 2014 · N983CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL CRACKED. C-CHECK, REPAIRED IAW REO.
- [SDR SWIA201439647](https://openairdocs.org/sdr/SWIA201439647.md): Frame · cracked · Oct 6, 2014 · N983CA · Cndair CL6002B19 · Fuselage Main, Frame
  > AFT CARGO BAY AT BS 605, STRINGER 9 LT SIDE ABOVE CARGO DOOR CUTOUT. FRAME IS CRACKED AT RADIUS. C-CHECK, REPAIRED THE FRAME IAW REO.
- [SDR SWIA201439657](https://openairdocs.org/sdr/SWIA201439657.md): Skin · chafed · Oct 5, 2014 · N983CA · Cndair CL6002B19 · Ailerons
  > LEFT AILERON LOWER L/E SKIN CHAFED AT OTBD END. C-CHECK, BLENDED LT AILERON LOWER L/E SKIN IAW REO.
- [SDR SWIA201439661](https://openairdocs.org/sdr/SWIA201439661.md): Skin · chafed · Oct 4, 2014 · N983CA · Cndair CL6002B19 · Ailerons
  > RT AILERON PANEL 699AB IS CHAFED. DRILLED AND LOCATED NEW AILERON LOWER SKIN PANEL IAW REO.
- [SDR SWIA201439656](https://openairdocs.org/sdr/SWIA201439656.md): Skin · gouged · Oct 4, 2014 · N983CA · Cndair CL6002B19 · Ailerons
  > GOUGE IN PANEL 599AB. C-CHECK, BLENDED LT AILERON LOWER L/E SKIN 559AB IAW REO.
- [SDR SWIA201439646](https://openairdocs.org/sdr/SWIA201439646.md): Skin · dented · Oct 4, 2014 · N983CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > LEFT SIDE FUSELAGE SKIN AT BS 409 JUST BELOW STRINGER 16L IS DENTED. C-CHECK, REWORKED IAW EA.
- [SDR SWIA201439645](https://openairdocs.org/sdr/SWIA201439645.md): Skin · dented · Oct 4, 2014 · N983CA · Cndair CL6002B19 · Passenger/Crew Doors
  > DENT FOUND ON PAX DOOR OUTER SKIN. C-CHECK, REWORKED IAW EA.
- [SDR SWIA2014061738200](https://openairdocs.org/sdr/SWIA2014061738200.md): Tiller · failed · Jun 13, 2014 · N983CA · Cndair CL6002B19 · Landing Gear Steering System
  > DURING FLIGHT, STEERING INOPERATIVE MESSAGE ILLUMINATED. RAN QRH THREE TIMES. MESSAGE PERSISTS. RETURN TO DEPARTURE. ON LANDING GEAR DOWN LANDING CHECK TRIED 1 MORE TIME IT WORKED AND ON TAXI MSG RETURNED. INTERROGATED NOSE STEERING ECU FLAGGED CAPTAIN'S STE
- [SDR SWIA201437761](https://openairdocs.org/sdr/SWIA201437761.md): Wire · broken · May 28, 2014 · N983CA · Cndair CL6002B19 · Light System Wiring
  > INTERIOR EMERGENCY LIGHT ON FWD WINDSCREEN INOPERATIVE. REPAIRED BROKEN WIRE ON FWD WINDSCREEN EMERGENCY LIGHT.
- [SDR SWIA201436660](https://openairdocs.org/sdr/SWIA201436660.md): Charger · failed · Mar 8, 2014 · N983CA · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT ROW SIDE WALL LIGHT DOES NOT ILLUMINATE. FLT 5571 REPLACED AFT BATTERY CHARGER & BATTERY, PN AD-2013-1A, SN ON 67803 & SN OFF 64830.
- [SDR SWIA201436659](https://openairdocs.org/sdr/SWIA201436659.md): Battery Pack · discharged · Mar 7, 2014 · N983CA · Cndair CL6002B19 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS NOT WORKING. REPLACED ALL FOUR BATTERY SUPPLY PACKS & REPLACED NR 1 & NR 3 BATTERY CHARGER, PN AD-2013-1A, SN ON 64830, SN OFF 99705, SN ON 68386, SN OFF 107279, SN ON 77156, SN OFF 67887, SN ON 105763 & SN OFF 72165.
- [SDR SWIA201436578](https://openairdocs.org/sdr/SWIA201436578.md): Light · inoperative · Feb 27, 2014 · N983CA · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT AT MIDDLE OF CABIN HAS BURNED OUT LIGHT BULB. FLT 6495 RELAMPED.
- [SDR SWIA201436369](https://openairdocs.org/sdr/SWIA201436369.md): Bulkhead · gouged · Feb 18, 2014 · N983CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BULKHEAD 621 IN AFT EQUIPMENT BAY Z MEMBER HAS A GOUGE APPROXIMATELY 8 INCHES DOWN FROM TOP, MEASURES 0.32 INCHES X 0.4 INCHES WITH A DEPTH OF.027 INCHES. C-CHECK REPAIRED IAW REO.
- [SDR SWIA201436251](https://openairdocs.org/sdr/SWIA201436251.md): Battery · discharged · Feb 2, 2014 · N983CA · Cndair CL6002B19 · Emergency Lighting
  > OVERHEAD CEILING EMERGENCY EXIT FWD SIGN DOES NOT ILLUMINATE. FLT 5482 CHARGED BATTERY & ALL EMERGENCY LIGHTS ARE OPERATIVE.
- [SDR SWIA201436121](https://openairdocs.org/sdr/SWIA201436121.md): Light · inoperative · Jan 24, 2014 · N983CA · Cndair CL6002B19 · Emergency Lighting
  > LAST OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT 5621 RELAMPED.
- [SDR SWIA201436050](https://openairdocs.org/sdr/SWIA201436050.md): Light · inoperative · Jan 17, 2014 · N983CA · Cndair CL6002B19 · Emergency Lighting
  > NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 6426 RELAMPED.
- [SDR SWIA201436028](https://openairdocs.org/sdr/SWIA201436028.md): Light · inoperative · Jan 15, 2014 · N983CA · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT SIGN ABOVE ROW 8 IS BURNED OUT. FLT 6372 RELAMPED.
- [SDR SWIA201435924](https://openairdocs.org/sdr/SWIA201435924.md): Light · inoperative · Jan 2, 2014 · N983CA · Cndair CL6002B19 · Emergency Lighting
  > NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 5412 RELAMPED.
- [SDR SWIA201335508](https://openairdocs.org/sdr/SWIA201335508.md): Battery Pack · discharged · Dec 4, 2013 · N983CA · Cndair CL6002B19 · Emergency Lighting
  > NR 3 EMERGENCY OVERHEAD LIGHT & EMERGENCY OVERHEAD EXIT SIGN AT ROW 8 DO NOT ILLUMINATE. FLT 6394 ALLOWED ELBP TO CHARGE 7 WARM UP.
- [SDR SWIA201334845](https://openairdocs.org/sdr/SWIA201334845.md): Light · inoperative · Oct 7, 2013 · N983CA · Cndair CL6002B19 · Emergency Lighting
  > NR 4 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT#5622 RELAMPED.
- [SDR SWIA201333544](https://openairdocs.org/sdr/SWIA201333544.md): Bracket · failed · May 23, 2013 · N983CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > NOSE DOOR AND GEAR DISAGREE WARNING MESSAGES, FOLLOWED QRH AND MANUALLY EXTENDED GEAR. REPLACED THE NLG LOWER AFT WEIGHT OFF WHEELS SENSOR BRACKET AND ADJUSTED THE WEIGHT OFF WHEELS SENSOR IAW AMM. PERFORMED SEVERAL GEAR SWINGS WITH NO DEFECTS NOTED. OPS CHE
- [SDR SWIA201333524](https://openairdocs.org/sdr/SWIA201333524.md): Wire Harness · failed · May 22, 2013 · N983CA · Cndair CL6002B19 · Landing Gear System Wiring
  > NOSE-GEAR UP DISAGREE MASTER WARNING. REPLACED NR 1 DOWNLOCK, NLG HARNESS IAW AMM. PERFORMED GEAR SWINGS. OPS CHECK GOOD, PN: 17300-253.
- [SDR SWIA201333178](https://openairdocs.org/sdr/SWIA201333178.md): Door Seal · collapsed · Apr 8, 2013 · N983CA · Cndair CL6002B19 · Passenger/Crew Doors
  > LOSS OF PRESSURIZATION DUE TO PORTION OF PAX DOOR SEAL COLLAPSING. (FLT 6266) REPLACED PAX DOOR SEAL. LEAK CHECKS AND OPS CHECKS GOOD.
- [SDR SWIA201333146](https://openairdocs.org/sdr/SWIA201333146.md): Wire Harness · failed · Apr 2, 2013 · N983CA · Cndair CL6002B19 · Landing Gear System Wiring
  > RECEIVED GEAR DISAGREE WARNING MESSAGE SHOWING NOSE GEAR HASH MARKS. (FLT 6367) REPLACED NR 1 DOWNLOCK PROX SENSOR NLG HARNESS IAW AMM. GEAR SWINGS NORMALLY.
- [SDR SWIA201332951](https://openairdocs.org/sdr/SWIA201332951.md): Battery Pack · discharged · Mar 5, 2013 · N983CA · Cndair CL6002B19 · Emergency Lighting
  > UPPER EMERGENCY EXIT SIGN AT ROW 8 CD AND LOWER EMERGENCY EXIT SIGN IN ROW 8 A/B DO NOT ILLUMINATE. (FLT 6369) FOUND BATTERY PACK FOR EMERGENCY LIGHTS ON OVERWING EXITS TO BE LOW ON POWER. SWITCHED TO ARM AND CHARGED BATTERY.
- [SDR SWIA201332900](https://openairdocs.org/sdr/SWIA201332900.md): Floor Support · cracked · Feb 15, 2013 · N983CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 621 LEFT FLOOR SUPPORT ANGLE IS CRACKED JUST I/B OF CARGO SILL. (C-CHECK) REPLACED THE LEFT CARGO FLOOR SUPPORT ANGLE AT FS 621 IAW REO.
- [SDR SWIA201332905](https://openairdocs.org/sdr/SWIA201332905.md): Structure · cracked · Feb 8, 2013 · N983CA · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > LEFT ENGINE PYLON TRAILING EDGE HAS CRACK AND DELAMINATION. (C-CHECK) REPAIRED CRACK AND DELAMINATION AT LEFT ENGINE PYLON TRAILING EDGE IAW STS EA.
- [SDR SWIA201332901](https://openairdocs.org/sdr/SWIA201332901.md): Post · cracked · Feb 8, 2013 · N983CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK NOTED AND MARKED IN FS 409+128 VERTICAL POST AT RBL 18, O/B C-CHANNEL IN AFT RADIUS. (C-CHECK) REMOVED AND REPLACED VERTICAL POST O/B SIDE AT FS 409+128 RBL 18 IAW REO.
- [SDR SWIA201332547](https://openairdocs.org/sdr/SWIA201332547.md): Arm · out of adjust · Jan 10, 2013 · N983CA · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON ARRIVAL, COULD NOT OPEN THE MAIN CABIN DOOR. (FLT 5311) ADJUSTED INNER RELEASE ARM POWER TENSION AND INSPECTED OUTER HANDLE LINKAGES WITH NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR SWIA201232503](https://openairdocs.org/sdr/SWIA201232503.md): Handle · jammed · Dec 31, 2012 · N983CA · Cndair CL6002B19 · Passenger/Crew Doors
  > CANNOT OPEN THE MAIN CABIN DOOR FROM THE OUTSIDE. (FLT 5349) OPENED PAX DOOR IAW AMM. AFTER INITIAL ATTEMPT DOOR HANDLE NO LONGER JAMMED. OP CHECK NORMAL UPON NUMEROUS ATTEMPTS.
- [SDR SWIA201232282](https://openairdocs.org/sdr/SWIA201232282.md): Light · inoperative · Dec 3, 2012 · N983CA · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY OVERHEAD LIGHT 1 AND 2, AND EMERGENCY FLOOR LIGHT 8A BURNED OUT. (FLT 5393) RELAMPED EMERGENCY.
- [SDR SWIA201232157](https://openairdocs.org/sdr/SWIA201232157.md): Strut · failed · Nov 12, 2012 · N983CA · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE WARNING MESSAGE WITH NOSE WHEEL REMAINING IN DOWN AND LOCKED POSITION. WOW INPUT CAUTION MESSAGE APPEARED AS WELL. (FLT 5412) REMOVED AND REPLACED NLG SHOCK STRUT ASSEMBLY IAW AMM. P/N: 16050-115 S/N: DLC976/04 P/N: OFF 16050-115 S/N: OFF D
- [SDR SWIA201231954](https://openairdocs.org/sdr/SWIA201231954.md): Antenna · failed · Oct 12, 2012 · N983CA · Cndair CL6002B19 · Air Collision Avoidance System
  > CAPTAIN'S RADIO ALTIMETER AND FIRST OFFICER'S RADIO ALTIMETER DIFFER MORE THAN 300 FEET FROM 2500 FEET. (FLT 5565) REPLACED THE F/O'S RECEIVE ANTENNA IN REFERENCE TO THE CRJ 200 MM. P/N: 567-2002 S/N OFF: NSN
- [SDR SWIA201231779](https://openairdocs.org/sdr/SWIA201231779.md): Wire Harness · failed · Sep 12, 2012 · N983CA · Cndair CL6002B19 · Landing Gear System Wiring
  > GEAR DISAGREE WARNING MESSAGE ASSOCIATED WITH YELLOW INDICATION FOR NOSE GEAR. (FLT 5310) REPLACED NLG DOWNLOCK NR 1 HARNESS (PSIGA) ASSEMBLY IN REFERENCE TO AMM.

Next page: https://openairdocs.org/deregistered/N983CA-2017-06-08/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 = 'N983CA' AND deregistration_id = 'N983CA-2017-06-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N983CA-2017-06-08/reports

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