# Service difficulty reports: N984CA, cancelled May 3, 2017

A list on [N984CA, cancelled May 3, 2017](https://openairdocs.org/deregistered/N984CA-2017-05-03.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 · 174 reports

- [SDR SWIA201641882](https://openairdocs.org/sdr/SWIA201641882.md): Reservoir · failed · Feb 12, 2016 · N984CA · Cndair CL6002B19 · Hydraulic Reservoir, Main
  > RETURNED TO DEPARTURE, DUE TO A GEAR DISAGREE. R & R NR 3 HYDRAULIC RESERVOIR IAW AMM. OPS CHECKS GOOD, NO LEAKS NOTED.
- [SDR SWIA201540793](https://openairdocs.org/sdr/SWIA201540793.md): Water Separator · contaminated · Feb 27, 2015 · N984CA · Cndair CL6002B19 · Humidity Control System
  > RETURNED TO THE FIELD FOR SMOKE IN THE LAV. CREW REPORTED SMOKE COMING FROM GASPERS. FOUND GLYCOL IN WATER SEPARATOR. REPLACED NR 1AND NR 2 WATER SEPARATORS. OPS CHECKS GOOD.
- [SDR SWIA201440016](https://openairdocs.org/sdr/SWIA201440016.md): Skin · gouged · Nov 14, 2014 · N984CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > WHILE PERFORMING BLENDING FOR EXTERIOR SKIN GOUGES FOR ADF ANTENNA ON MX TRANS 11509318, DISCOVERED 4 EACH LIGHTNING STRIKES AT ADF ANTENNA MOUNT HOLES. C-CHECK, UPON FURTHER INVESTIGATION, FOUND TO BE OLD TOOLING MARKS INSTEAD OF LIGHTNING STRIKES. ALSO FOU
- [SDR SWIA201440046](https://openairdocs.org/sdr/SWIA201440046.md): Vane · chafed · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE CHAFED AT OTBD L/E. BLENDED THE CHAFE IAW REO.
- [SDR SWIA201440045](https://openairdocs.org/sdr/SWIA201440045.md): Vane · chafed · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE CHAFED AT INBD L/E. BLENDED THE CHAFE IAW REO.
- [SDR SWIA201440042](https://openairdocs.org/sdr/SWIA201440042.md): Hinge · gouged · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE 5TH LUG BACK IS GOUGED ON THE FUSELAGE SIDE. BLENDED AND FOUND WITHIN LIMITS. IAW REO.
- [SDR SWIA201440040](https://openairdocs.org/sdr/SWIA201440040.md): Skin · debonded · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING OTBD L/E 630KL IS DEBONDED. BONDED RT WING OTBD L/E, 630KL IAW REO.
- [SDR SWIA201440038](https://openairdocs.org/sdr/SWIA201440038.md): Skin · debonded · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING INBD L/E 620JL IS DEBONDED. BONDED RT WING INBD L/E IAW REO.
- [SDR SWIA201440037](https://openairdocs.org/sdr/SWIA201440037.md): Seat Track · corroded · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9.0 FROM BS 599 - 599+86 CORRODED. R & R THE SEAT TRACK IAW AMM & REO.
- [SDR SWIA201440035](https://openairdocs.org/sdr/SWIA201440035.md): Seat Track · corroded · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9.0 BS 409+126 - 599 HAS CORROSION. R & R SEAT TRACK IAW AMM & REO.
- [SDR SWIA201440034](https://openairdocs.org/sdr/SWIA201440034.md): Seat Track · corroded · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9.0 FROM BS 399 - 409+126 HAS CORROSION. R & R SEAT TRACK IAW AMM & REO.
- [SDR SWIA201440033](https://openairdocs.org/sdr/SWIA201440033.md): Seat Track · corroded · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 9.0 FROM BS 399 - 409+126 HAS CORROSION. R & R SEAT TRACK IAW AMM & REO
- [SDR SWIA201440032](https://openairdocs.org/sdr/SWIA201440032.md): Pressure Deck · cracked · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR AT BS 458 - 462 CRACKED BETWEEN BL 0.0 AND RBL 9.0. REPAIRED IAW REO. PERFORMED PRESSURIZATION CHECK IAW AMM.
- [SDR SWIA201440031](https://openairdocs.org/sdr/SWIA201440031.md): Pressure Deck · cracked · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR AT BS 458 - 462 CRACKED BETWEEN BL 0.0 AND LBL 9.0. REPAIRED IAW REO. PERFORMED PRESSURIZATION CHECK IAW AMM.
- [SDR SWIA201440030](https://openairdocs.org/sdr/SWIA201440030.md): Bulkhead Web · cracked · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK AT FWD PRESSURE BULKHEAD WEB COMMON TO PARKING BRAKE FITTING, 3 O'CLOCK POSITION WHEN LOOKING FORWARD, REPAIRED IAW REO. PRESSURE CHECKED GOOD.
- [SDR SWIA201440019](https://openairdocs.org/sdr/SWIA201440019.md): Bulkhead Web · cracked · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK NOTED ON FS621 BULKHEAD WEB, FWD FACE, ALONG LBL36.2 AT APPROXIMATELY WL 75 NEAR FLOOR LEVEL. C-CHECK, REPAIRED CRACK IAW REO. PARTS REMOVED WEIGHT 0.01 LBS, REPLACEMENT PARTS WEIGH 0.40 LBS, NET WEIGHT GAINED 0.39 LBS. SCALE TUC 1755, DUE 30 JUN 2015
- [SDR SWIA201440018](https://openairdocs.org/sdr/SWIA201440018.md): Bulkhead Web · cracked · Nov 8, 2014 · N984CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK NOTED ON BS 621 BULKHEAD WEB, FWD FACE ALONG BL 0 AT WL 90. C-CHECK. REPAIRED CRACK ON FS 621 BULKHEAD IAW REO. PRESSURE CHECK GOOD. COMPLIED WITH ST 51-900-1003, WEIGHED CUT OUT DAMAGED WEB SECTION AT.002 LBS AND REPAIR PARTS WITH ADDED FASTENERS AT
- [SDR SWIA201440044](https://openairdocs.org/sdr/SWIA201440044.md): Panel · cracked · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Standard Practices/Structures
  > PANEL 221CLC HAS CRACKS AROUND SCREW HOLE. REPAIRED CRACKS AROUND SCREW HOLE ON PANEL IAW EA.
- [SDR SWIA201440043](https://openairdocs.org/sdr/SWIA201440043.md): Vane · chafed · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING INBD FLAP VANE L/E CHAFED 91.5 INCHES FROM OTBD END. BLENDED CHAFE IAW REO.
- [SDR SWIA201440041](https://openairdocs.org/sdr/SWIA201440041.md): Panel · cracked · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Fuselage Structure (General)
  > PANEL 222CLC, HAS CRACKS AROUND SCREW HOLE. REPAIRED PANEL IAW EA.
- [SDR SWIA201440039](https://openairdocs.org/sdr/SWIA201440039.md): Vane · chafed · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING INBD FLAP VANE L/E CHAFED 43 INCHES FROM OTBD END. BLENDED CHAFE IAW REO AND SRM. FOUND WITHIN LIMITS IAW REO.
- [SDR SWIA201440036](https://openairdocs.org/sdr/SWIA201440036.md): Vane · chafed · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING INBD FLAP VANE L/E CHAFED 7.5" FROM OTBD END. BLENDED IAW REO. FOUND WITHIN LIMITS IAW REO.
- [SDR SWIA201440028](https://openairdocs.org/sdr/SWIA201440028.md): Skin · dented · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP HAS DENT ON LOWER SKIN OUTBD OF PANEL 584AB. REPAIRED IAW EA.
- [SDR SWIA201440024](https://openairdocs.org/sdr/SWIA201440024.md): Attach Fitting · chafed · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Landing Gear Doors
  > LEFT MLT DOOR ROD ATTACH LUG ON DOOR IS CHAFED. C-CHECK, R & R THE LT MLG DOOR ATTACHMENT LUG REF SRM & REO.
- [SDR SWIA201440023](https://openairdocs.org/sdr/SWIA201440023.md): Rod End · chafed · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Landing Gear Door Retract Section
  > LEFT MLG DOOR ROD END IS CHAFED AT THE BELLCRANK END. R & R THE LT MLG DOOR STRUT IAW AMM, DWG AND REO.
- [SDR SWIA201440022](https://openairdocs.org/sdr/SWIA201440022.md): Bellcrank · chafed · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Landing Gear Door Retract Section
  > LT MLG DOOR BELLCRANK END IS CHAFED AT THE DOOR ROD CONNECTION END. R & R THE LT MLG DOOR BELLCRANK ASSY REF AMM, COMPLIED WITH REO AND DWG.
- [SDR SWIA201440021](https://openairdocs.org/sdr/SWIA201440021.md): Rod End · chafed · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Landing Gear Door Retract Section
  > RIGHT MLG DOOR ROD END IS CHAFED AT THE BELLCRANK END. R & R THE RT MLG DOOR STRUT.
- [SDR SWIA201440020](https://openairdocs.org/sdr/SWIA201440020.md): Bellcrank · chafed · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Landing Gear Door Retract Section
  > RT MLG DOOR BELLCRANK END IS CHAFED AT THE DOOR ROD CONNECTION END. C-CHECK, OUT OF LIMITS IAW DWG. R & R RT MLG DOOR BELLCRANK ASSY, REF AMM, CW REO.
- [SDR SWIA201440017](https://openairdocs.org/sdr/SWIA201440017.md): Vane · chafed · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE CHAFED AT CENTER L/E. BLENDED IAW REO.
- [SDR SWIA201440015](https://openairdocs.org/sdr/SWIA201440015.md): Vane · gouged · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RT WING INBD FLAP VANE L/E HAS SMALL GOUGE 27.5" FROM OTBD END. BLENDED IAW REO.
- [SDR SWIA201440014](https://openairdocs.org/sdr/SWIA201440014.md): Vane · chafed · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Trailing Edge Flaps
  > RT WING INBD FLAP VANE L/E CHAFED 70.5" FROM OTBD END. BLENDED AND REPAIRED IAW REO.
- [SDR SWIA201440012](https://openairdocs.org/sdr/SWIA201440012.md): Skin · chafed · Nov 7, 2014 · N984CA · Cndair CL6002B19 · Ailerons
  > LEFT AILERON UPPER L/E CHAFED. LT AILERON UPPER L/E SHROUD FOUND TO BE OUT OF LIMITS IAW REO REPLACED.
- [SDR SWIA201440048](https://openairdocs.org/sdr/SWIA201440048.md): Skin · failed · Nov 6, 2014 · N984CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENTED LT FUSELAGE SKIN PANEL ON NOSE, BELOW CAPTAIN'S WINDOW. REPAIRED IAW REO.
- [SDR SWIA201440029](https://openairdocs.org/sdr/SWIA201440029.md): Panel · damaged · Nov 6, 2014 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PANEL 326AR, ZONE 300 FAILED GAP CHECK. CONTOURED VISOR PANEL. FOUND WITHIN LIMITS IAW REO.
- [SDR SWIA201440027](https://openairdocs.org/sdr/SWIA201440027.md): Panel · failed · Nov 6, 2014 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PANEL 326BR, ZONE 300 FAILED GAP CHECK, CONTOURED VISOR PANEL. FOUND WITHIN LIMITS IAW REO.
- [SDR SWIA201440026](https://openairdocs.org/sdr/SWIA201440026.md): Panel · failed · Nov 6, 2014 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PANEL 326BL, ZONE 300, FAILED GAP CHECK, CONTOURED VISOR PANEL IAW REO AND AMM.
- [SDR SWIA201440025](https://openairdocs.org/sdr/SWIA201440025.md): Panel · damaged · Nov 6, 2014 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PANEL 326AL ZONE 300, FAILED GAP CHECK, CONTOURED VISOR PANEL 326AL. FOUND WITHIN LIMITS IAW REO.
- [SDR SWIA2014061938226](https://openairdocs.org/sdr/SWIA2014061938226.md): Torque Link · galled · Jun 17, 2014 · N984CA · Cndair CL6002B19 · Engine Mount Section
  > LT ENGINE FORWARD MOUNT TORQUE LINK ASSEMBLY HAS GALLING IN BUSHING. INSTALLED NEW LINK ON THE LT ENGINE FWD YOKE MOUNT IAW AMM.
- [SDR SWIA2014061938225](https://openairdocs.org/sdr/SWIA2014061938225.md): Bushing · galled · Jun 17, 2014 · N984CA · Cndair CL6002B19 · Engine Mount Section
  > LT ENGINE FORWARD MOUNT YOKE BUSHING HAS GALLING. INSTALLED NEW LT ENGINE FWD YOKE MOUNT IAW AMM.
- [SDR SWIA201437643](https://openairdocs.org/sdr/SWIA201437643.md): Lamp · burned out · May 19, 2014 · N984CA · Cndair CL6002B19 · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHT IS BURNED OUT. R & R LT OVERWING EXTERIOR EMERGENCY LIGHT LAMP IAW AMM.
- [SDR SWIA201437668](https://openairdocs.org/sdr/SWIA201437668.md): Autopilot Sys · disconnected · May 17, 2014 · N984CA · Cndair CL6002B19 · Auto Flight System
  > AUTOPILOT INITIATED UNCOMMANDED PITCH CHANGE A/P WAS MANUALLY DISCONNECTED, FLIGHT PATH CORRECTED AND REENGAGED WITHOUT FURTHER INCIDENT. PERFORMED SERVO SPIN TEST IAW AMM. NO DEFECTS NOTED AND NO RELEVENT MDC MESSAGES WERE FOUND.
- [SDR SWIA201437403](https://openairdocs.org/sdr/SWIA201437403.md): Bushing · damaged · May 7, 2014 · N984CA · Cndair CL6002B19 · Engine Mount Section
  > LEFT ENGINE AFT MOUNT THRUST SHAFT SPHERICAL BUSHING AND SPHERICAL BUSHING HOUSING HAS CORRODED. REPLACED LT ENGINE AFT MOUNT THRUST SHAFT SPHERICAL BUSHING AND SPHERICAL BUSHING HOUSING IAW AMM.
- [SDR SWIA201437053](https://openairdocs.org/sdr/SWIA201437053.md): Lamp · burned out · Apr 6, 2014 · N984CA · Cndair CL6002B19 · Emergency Lighting
  > FORWARD EMERGENCY LIGHT OVERHEAD LIGHT IS BURNED OUT, REPLACED LAMP.
- [SDR SWIA201436785](https://openairdocs.org/sdr/SWIA201436785.md): Sign · burned out · Mar 16, 2014 · N984CA · Cndair CL6002B19 · Emergency Lighting
  > LOWER RIGHT OVERWING EXIT EMERGENCY SIGN IS BURNED OUT. REPLACED SIGN AND INVERTER.
- [SDR SWIA201334853](https://openairdocs.org/sdr/SWIA201334853.md): Light · inoperative · Oct 7, 2013 · N984CA · Cndair CL6002B19 · Emergency Lighting
  > CEILING EMERGENCY LIGHT IN AFT POSITION BURNED OUT. FLT#5374 RELAMPED, PN 1317.
- [SDR SWIA201334381](https://openairdocs.org/sdr/SWIA201334381.md): Light · inoperative · Aug 22, 2013 · N984CA · Cndair CL6002B19 · Emergency Lighting
  > CEILING POD LIGHT ABEAM BURNED OUT. FLT#6224 RELAMPED.
- [SDR SWIA201333497](https://openairdocs.org/sdr/SWIA201333497.md): Pump · failed · May 17, 2013 · N984CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > RECEIVED GEAR DISAGREE WARNING MSG. BY THE TIME WE RAN CHECKLIST, ISSUE SELF-CORRECTED. NO PROBLEMS WITH LANDING GEAR EXTENSION ON LANDING. REPLACED 3A ELECTRIC HYD PUMP IAW AMM, PN: 848847, SN ON: MX572122, SN OFF: MX520285.
- [SDR SWIA201333361](https://openairdocs.org/sdr/SWIA201333361.md): Web · cracked · Apr 14, 2013 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TRU WEB IS CRACKED AT FS 193 RIGHT. (C-CHECK) REPAIRED TRU WEB AT FS 193.00 RIGHT IAW REO.
- [SDR SWIA201333360](https://openairdocs.org/sdr/SWIA201333360.md): Web · cracked · Apr 14, 2013 · N984CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TRU WEB IS CRACKED AT FS 193 LEFT. (C-CHECK) INSTALLED REPAIR ON TRU WEB FS 193 LEFT IAW REO.
- [SDR SWIA201333359](https://openairdocs.org/sdr/SWIA201333359.md): Cap · worn · Apr 13, 2013 · N984CA · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP, INBD FLAP VANE CAP IS WORN BEYOND LIMITS. (C-CHECK) REPLACED WORN LEFT INBD FLAP, INBD FLAP VANE CAP IAW SRM.

Next page: https://openairdocs.org/deregistered/N984CA-2017-05-03/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 = 'N984CA' AND deregistration_id = 'N984CA-2017-05-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N984CA-2017-05-03/reports

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