# Service difficulty reports: N958CA, cancelled Apr 18, 2018

A list on [N958CA, cancelled Apr 18, 2018](https://openairdocs.org/deregistered/N958CA-2018-04-18.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 · 116 reports

- [SDR COMA2012021650009](https://openairdocs.org/sdr/COMA2012021650009.md): Beam · cracked · Feb 15, 2012 · N958CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK INDICATION FOUND ON UPPER VERTICAL BEAMS. REPAIRED DAMAGED AREAS IAW REO 601R-53-41-1545.
- [SDR COMA2012021650008](https://openairdocs.org/sdr/COMA2012021650008.md): Beam · cracked · Feb 15, 2012 · N958CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK INDICATION FOUND ON UPPER VERTICAL BEAM. REPAIRED DAMAGED AREA IAW REO 601R-53-41-1545.
- [SDR COMA2010122450263](https://openairdocs.org/sdr/COMA2010122450263.md): Bpsu · faulty · Dec 24, 2010 · N958CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > DURING CLIMBOUT OF JFK RECEIVED A FLAPS FAIL MESSAGE. CREW DECLARED AN EMERGENCY AND AIRCRAFT RETURNED TO JFK, LANDED SAFELY. REPLACED THE LEFT WING BRAKE POSITIONING SENSING UNIT (BPSU).
- [SDR COMA2010122050262](https://openairdocs.org/sdr/COMA2010122050262.md): Flap · failed · Dec 17, 2010 · N958CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON CLIMBOUT FROM DTW RECEIVED FLAPS FAIL CAUTION MSG, FLAPS FAILED AT 8 DEG. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION.
- [SDR COMA2010101450221](https://openairdocs.org/sdr/COMA2010101450221.md): Wire Harness · faulty · Oct 12, 2010 · N958CA · Cndair CL6002B19 · Flight Control System Wiring
  > EN ROUTE FROM CVG TO BWI RECEIVED FLAPS FAIL MSG, FLAPS AT 0 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY IN BWI. REMOVED AND REPLACED RIGHT WING BPSU WIRE HARNESS.
- [SDR COMA2010101250220](https://openairdocs.org/sdr/COMA2010101250220.md): Bpsu · failed · Oct 11, 2010 · N958CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > EN ROUTE FROM MEM TO OMA RECEIVED FLAPS FAIL MSG, FLAPS AT 0 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY IN OMA. REMOVED AND REPLACED LEFT BPSU.
- [SDR COMA2010091550199](https://openairdocs.org/sdr/COMA2010091550199.md): Drag Brace · failed · Sep 13, 2010 · N958CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > DURING LANDING AT MDW RECEIVED GEAR DISAGREE, NOSE LANDING GEAR RED. FOLLOWED QRH, EMERGENCY DECLARED. A/C DIVERTED TO ORD LANDED SAFELY. REMOVED AND REPLACED NOSE LANDING GEAR DRAG BRACE.
- [SDR COMA2010072950161](https://openairdocs.org/sdr/COMA2010072950161.md): Wire Harness · broken · Jul 28, 2010 · N958CA · Cndair CL6002B19 · Landing Gear System Wiring
  > ON APPROACH INTO MEM RECEIVED O/B ANTI-SKID CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED RIGHT MLG O/B WIRE HARNESS BTMS SUB ASSY.
- [SDR COMA2010051050114](https://openairdocs.org/sdr/COMA2010051050114.md): Skin · gouged · May 8, 2010 · N958CA · Cndair CL6002B19 · Wing, Plate/Skin
  > DURING NDT INSPECTION FOUND RIGHT WING LOWER PLANK ATTACHMENT HOLE AT WS 45.00 AND WS 65.75 HAS GOUGED. REPAIRED BY REAMING HOLE IAW EA 10-5721-02949.
- [SDR COMA2010050550113](https://openairdocs.org/sdr/COMA2010050550113.md): Angle · cracked · May 5, 2010 · N958CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559.00 RBL 9 CRACKED AT CAP ANGLE. REPAIRED FS 559 CAP ANGLE AT RBL 9 IAW REO 601R-53-41-260 RT REP, 601R-53-41-609 AND DEVIATION 601R-53-41-1206.
- [SDR COMA2010050550112](https://openairdocs.org/sdr/COMA2010050550112.md): Angle · cracked · May 5, 2010 · N958CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559.00 RBL 18.00 CRACKED AT CAP ANGLE. REPAIRED FS 559 CAP ANGLE AT RBL 18 IAW REO 601R-53-41-260 RT REP, 601R-53-41-609 AND DEVIATION 601R-53-41-1206.
- [SDR COMA2010040550111](https://openairdocs.org/sdr/COMA2010040550111.md): Angle · cracked · May 4, 2010 · N958CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559.00 LBL 18.00 CRACKED AT CAP ANGLE. REPAIRED FS 559 CAP ANGLE AT LBL 18 IAW REO 601R-53-41-260 LT REP.
- [SDR COMA2010050450110](https://openairdocs.org/sdr/COMA2010050450110.md): Angle · cracked · May 4, 2010 · N958CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559.00 LBL 9 CRACKED AT CAP ANGLE. REPAIRED FS 559 CAP ANGLE AT LBL 9 IAW REO 601R-53-41-260 LT REP.
- [SDR COMA2010050150109](https://openairdocs.org/sdr/COMA2010050150109.md): Web · cracked · May 1, 2010 · N958CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK IN WEB ABOVE CARGO DOOR TRACK FS 621.00. REPAIRED CRACK IN WEB ABOVE CARGO DOOR TRACK AT FS 621 IAW CRJ REO 601R-53-61-1541 REV B.
- [SDR COMA2010012550023](https://openairdocs.org/sdr/COMA2010012550023.md): Apu · seized · Jan 23, 2010 · N958CA · Cndair CL6002B19 · APU Core Engine
  > DURING TAXI APU SEIZED AND SHUT DOWN WITH A PUNGENT ELECTRICAL SMELL. SMOKE EXITING FROM APU DOOR. RECEIVED APU FAULT CAUTION MSG. REMOVED AND REPLACED APU.
- [SDR COMA2010010850011](https://openairdocs.org/sdr/COMA2010010850011.md): Sensor · obstructed · Jan 7, 2010 · N958CA · Cndair CL6002B19 · Door Warning System
  > AFTER T/O RECEIVED PAX DOOR LATCH CAUTION, FOLLOWED BY PAX DOOR WARNING MSG'S. EMERGENCY DECLARED, FOLLOWED QRH AND RETURNED TO MSP LANDED SAFELY. INSPECTED PAX DOOR, FOUND SNOW AND GREASE BETWEEN PROX SENSORS AND TARGETS. CLEANED FOD OUT FROM BETWEEN SENSO
- [SDR COMA2009081050175](https://openairdocs.org/sdr/COMA2009081050175.md): Warning System · malfunctioned · Aug 5, 2009 · N958CA · Cndair CL6002B19 · Door Warning System
  > ON CLIMBOUT YHZ RECEIVED PAX DOOR WARNING MSG. PERFORMED QRH, EMERGENCY DECLARED. A/C RETURNED TO YHZ LANDED SAFELY. INSPECTED PAX DOOR LATCHING MECHANISM, NO DEFECTS NOTED. OPS CHECK OF PAX DOOR GOOD.
- [SDR COMA2009041550116](https://openairdocs.org/sdr/COMA2009041550116.md): Skin · cracked · Apr 13, 2009 · N958CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING PLANK CRACKED ON BOTTOM SIDE JUST O/B OF JACK PAD. DAMAGED AREA TRIMMED OUT TO REMOVE CRACK AND REPAIR DOUBLERS INSTALLED PER REO 601R-57-21-130.
- [SDR COMA2009040850112](https://openairdocs.org/sdr/COMA2009040850112.md): Skin · cracked · Apr 8, 2009 · N958CA · Cndair CL6002B19 · Wing, Plate/Skin
  > RT LOWER WING PLANK HAS CRACK INDICATION AT FUEL TANK ACCESS HOLE, FOR PANEL 650BB. BLENDED ACCESS HOLE CUTOUT TO REMOVE CRACK INDICATION IAW REO 601R-57-21-30, REV G.
- [SDR COMA2008112650010](https://openairdocs.org/sdr/COMA2008112650010.md): Reservoir · failed · Nov 25, 2008 · N958CA · Cndair CL6002B19 · Hydraulic Reservoir, Main
  > EN ROUTE FROM CVG TO YYZ RECEIVED NR 2 EDP CAUTION MSG AND NR 2 HYDRAULIC SYSTEM LOW PRESSURE CAUTION MSG. A/C DIVERTED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED NR 2 HYDRAULIC SYSTEM RESERVOIR.
- [SDR COMA0860219](https://openairdocs.org/sdr/COMA0860219.md): Skin · cracked · Apr 10, 2008 · N958CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING PLANK CRACKED ON BOTTOM SIDE JUST O/N OF JACK PAD. PERMANENT REPAIR OF THE LOWER WING PLANK WS 148.019 LEFT IAW REO 601R-57-21-130.
- [SDR COMA0860155](https://openairdocs.org/sdr/COMA0860155.md): Warning System · malfunctioned · Mar 1, 2008 · N958CA · Cndair CL6002B19 · Door Warning System
  > FLIGHT 5359 - ON CLIMBOUT FROM LEX, RECEIVED PAX DOOR WARNING MESSAGE, MESSAGE WENT OUT 15-20 SECONDS LATER. RAN QRH AND AIRCRAFT RETURNED BACK TO LEX AND LANDED SAFELY. PERFORMED OPS CHECK OF PAX DOOR WARNING SYSTEM. OPS CHECK GOOD AND NO DEFECTS FOUND.
- [SDR COMA0760617](https://openairdocs.org/sdr/COMA0760617.md): Secu · malfunctioned · Oct 25, 2007 · N958CA · Cndair CL6002B19 · Drag Control System
  > ON FINAL RECEIVED GLD NOT ARMED MESSAGE AS WELL AS CAS MISCOMPARE STATUS MESSAGE. PERFORMED GO-AROUND AND QRH. GLD DID NOT DEPLOY. LANDED WITHOUT INCIDENT. NO FAULTS IN SECU. PERFORMED SECU BITE AND SPOILER SYSTEM TEST. RESET SYSTEM. PERFORMED SEVERAL O
- [SDR COMA0760581](https://openairdocs.org/sdr/COMA0760581.md): Circuit Breaker · unknown · Sep 23, 2007 · N958CA · Cndair CL6002B19 · Engine Oil Pressure
  > FLIGHT 5330 - ON TAKEOFF NOTED THAT NR 1 ENGINE OIL PRESSURE READ ZERO. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. RESET CIRCUIT BREAKER 1M1. NO FURTHER DEFECTS.
- [SDR COMA0760209](https://openairdocs.org/sdr/COMA0760209.md): Trim Switch · faulty · Feb 23, 2007 · N958CA · Cndair CL6002B19 · Stabilizer Control System
  > FLIGHT 5106 - DURING CLIMBOUT OF RDU PITCH TRIM ACTIVATED UNCOMMANDED INTERMITTENTLY, FLIGHT RETURNED TO RDU. REPLACED THE CAPTAIN'S PITCH TRIM SWITCH.
- [SDR COMA0660620](https://openairdocs.org/sdr/COMA0660620.md): Connector · faulty · Nov 6, 2006 · N958CA · Cndair CL6002B19 · Light System Wiring
  > FLIGHT 5064 - THE EMERGENCY LIGHTS IN GALLEY AND FIRST SECTION OF FLOOR LIGHTING FAILED TO ILLUMINATE. REPLACED DEFECTIVE ELECTRICAL CONNECTOR FOR THE AFFECTED EMERGENCY LIGHTING SYSTEM.
- [SDR COMA0660550](https://openairdocs.org/sdr/COMA0660550.md): Windshield · cracked · Sep 22, 2006 · N958CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5574 - CAPTAIN'S WINDSHIELD CRACKED ON APPROACH. NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S WINDSHIELD.
- [SDR COMA0660273](https://openairdocs.org/sdr/COMA0660273.md): Apu · warning light · Mar 23, 2006 · N958CA · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > FLIGHT 5436 - APU FAULT CAUTION MESSAGE. APU AUTO SHUTDOWN ON GROUND. DEFERRED APU.
- [SDR COMA0560573](https://openairdocs.org/sdr/COMA0560573.md): Pseu · malfunctioned · Oct 27, 2005 · N958CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5684- PROX SYSTEM FAULT. REPLACED THE PSEU.
- [SDR COMA0560532](https://openairdocs.org/sdr/COMA0560532.md): Flap System · malfunctioned · Oct 2, 2005 · N958CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5093 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0560375](https://openairdocs.org/sdr/COMA0560375.md): Cabin Pressure · malfunctioned · Jul 2, 2005 · N958CA · Cndair CL6002B19 · Cabin Pressure Control System
  > AIRCRAFT CABIN NOT CLIMBING, DELTA P 4.2. CABIN PRESSURE SYSTEM OPS CHECK NORMAL. NO DEFECTS FOUND.
- [SDR COMA0560027](https://openairdocs.org/sdr/COMA0560027.md): Warning System · malfunctioned · Jan 4, 2005 · N958CA · Cndair CL6002B19 · Drag Control System
  > FLIGHT 5650, FLIGHT SPOILER FAULT AND GROUND SPOILER FAULT. RESET THE SPOILER SYSTEM, COULD NOT DUPLICATE. OPERATIONAL CHECK SATISFACTORY.
- [SDR COMA0460622](https://openairdocs.org/sdr/COMA0460622.md): Window · cracked · Nov 14, 2004 · N958CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5905 CO-PILOTS SIDE WINDOW CRACKED. REPLACED WINDOW.
- [SDR COMA0460531](https://openairdocs.org/sdr/COMA0460531.md): Door · open · Sep 10, 2004 · N958CA · Cndair CL6002B19 · Service Doors
  > GROUND POWER SERVICE DOOR WAS LEFT OPEN. INSPECTED DOOR AREA FOR DAMAGE. NO DEFECTS FOUND. SECURED DOOR.
- [SDR COMA0460346](https://openairdocs.org/sdr/COMA0460346.md): Pitot Line · contaminated · May 31, 2004 · N958CA · Cndair CL6002B19 · Pitot/Static System
  > FLIGHT 5229 IAS CAUTION DURING T/O. REMOVED WATER FROM PITOT LINES, SYSTEM TEST SATISFACTORY.
- [SDR COMA0460239](https://openairdocs.org/sdr/COMA0460239.md): Control Unit · malfunctioned · Apr 2, 2004 · N958CA · Cndair CL6002B19 · Brake Anti-Skid Section
  > FLIGHT 5322 ANTI SKID CAUTION DURING T/O. REPLACED THE ASCU.
- [SDR COMA0460230](https://openairdocs.org/sdr/COMA0460230.md): Selector Valve · failed · Mar 27, 2004 · N958CA · Cndair CL6002B19 · Landing Gear Selector
  > FLIGHT 5624 GEAR DISAGREE WARNING MLG DID NOT EXTEND. REPLACED THE MLG SELECTOR VALVE.
- [SDR COMA0460183](https://openairdocs.org/sdr/COMA0460183.md): Pitot Line · contaminated · Mar 5, 2004 · N958CA · Cndair CL6002B19 · Pitot/Static System
  > FLIGHT 5221 EFIS COMP MON WARNING DURING T/O. REMOVED WATER FROM PITOT SYSTEM, SYSTEM TEST SATISFACTORY.
- [SDR COMA0460059](https://openairdocs.org/sdr/COMA0460059.md): Wire · loose · Jan 15, 2004 · N958CA · Cndair CL6002B19 · Light System Wiring
  > FLIGHT 5090 FORWARD FLOOR EMERGENCY LIGHT IS INOP. SECURED LOOSE WIRE CONNECTION. OPERATIONAL CHECK SATISFACTORY.
- [SDR COMA0360328](https://openairdocs.org/sdr/COMA0360328.md): Wire · disconnected · Jul 17, 2003 · N958CA · Cndair CL6002B19 · Light System Wiring
  > FLIGHT 5368 EMERGENCY FLOOR PATH LIGHTING IS INOP. RECONNECTED POWER STRIP AT ROW 6.
- [SDR COMA0360256](https://openairdocs.org/sdr/COMA0360256.md): Idg · failed · Jun 2, 2003 · N958CA · Cndair CL6002B19 · AC Generation System
  > FLIGHT 5781 RT ENGINE IDG MESSAGE. REPLACED THE RT IDG.
- [SDR COMA0360085](https://openairdocs.org/sdr/COMA0360085.md): Spring · broken · Feb 5, 2003 · N958CA · Cndair CL6002B19 · Cargo/Baggage Doors
  > FLIGHT 5542 CARGO DOOR CAUTION MESSAGE.REPLACED THE DOOR HANDLE LATCH SPRING.
- [SDR COMA0260518](https://openairdocs.org/sdr/COMA0260518.md): Strut · Sep 5, 2002 · N958CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5517. WHEN THE GEAR HANDLE WAS RAISED AFTER T/O A "GEAR DISAGREE" AND "NOSE DOOR OPEN" WARNING MESSAGE ACTIVATED.CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD LANDING SAFELY.SERVICED THE NOSE LANDING GEAR STRUT.
- [SDR COMA0260484](https://openairdocs.org/sdr/COMA0260484.md): Mechanism · misrigged · Aug 13, 2002 · N958CA · Cndair CL6002B19 · Landing Gear Door Retract Section
  > FLIGHT 5296 AND 5703 BANGING AND THUMPING NOISE FROM NLG WITH GEAR RETRACTED; WITH GEAR DOWN NOSE DOORS OPEN WARNING.ADJUSTED THE NLG DOORS ACTUATING MECHANISM.
- [SDR COMA0260482](https://openairdocs.org/sdr/COMA0260482.md): Connector · Aug 13, 2002 · N958CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5295 EMERGENCY FLOOR PATH LIGHTS, ROWS 2-9, ARE INOPERABLE.SECURED LOOSE WIRE CONNECTOR, OPERATION SATISFACTORY.
- [SDR COMA0260398](https://openairdocs.org/sdr/COMA0260398.md): Connector · loose · Jun 27, 2002 · N958CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5200 EMERGENCY FLOOR PATH LIGHTS INOP BETWEEN ROWS 2 AND 6.SECURED LOOSE WIRE CONNECTION AT ROW 6.
- [SDR COMA0260370](https://openairdocs.org/sdr/COMA0260370.md): Light · Jun 16, 2002 · N958CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5483 EMERGENCY LIGHTS ARE INOP.COULD NOT DUPLICATE. ALL EMERGENCY LIGHTS FUNCTION.
- [SDR COMA0260356](https://openairdocs.org/sdr/COMA0260356.md): Seal · leaking · Jun 5, 2002 · N958CA · Cndair CL6002B19 · Engine Oil Indicating System
  > FLIGHT 5570 R/H ENGINE LOW OIL PRESSURE WARNING.REPLACED THE ACCESSORY GEAR BOX DRIVE SEALS AT AXIS D,F,&BB.
- [SDR COMA0160957](https://openairdocs.org/sdr/COMA0160957.md): Beam · cracked · Dec 8, 2001 · N958CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W CANADAIR REO 601R-53-61-366.
- [SDR COMA0160956](https://openairdocs.org/sdr/COMA0160956.md): Beam · cracked · Dec 8, 2001 · N958CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > ENGINE SUPPORT BEAM CRACK.REPAIRED DAMAGE IN ACCORDANCE WITH CANADAIRE REO 601-53-61-345.

Next page: https://openairdocs.org/deregistered/N958CA-2018-04-18/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 = 'N958CA' AND deregistration_id = 'N958CA-2018-04-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N958CA-2018-04-18/reports

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