# Service difficulty reports: N941CA, cancelled Apr 18, 2018

A list on [N941CA, cancelled Apr 18, 2018](https://openairdocs.org/deregistered/N941CA-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 · 102 reports

- [SDR COMA20111850009](https://openairdocs.org/sdr/COMA20111850009.md): Sensing Element · failed · Jan 17, 2011 · N941CA · Cndair CL6002B19 · Pneumatic Indicating System
  > ON CLIMBOUT FROM JAX TO DCA RECEIVED RIGHT ANTI-ICE DUCT WARNING MSG. IN ICING CONDITIONS. EMERGENCY DECLARED, A/C DIVERTED TO GSO LANDED SAFELY. REMOVED AND REPLACED RIGHT FUSELAGE SENSING ELEMENT A40WK.
- [SDR COMA2010060450124](https://openairdocs.org/sdr/COMA2010060450124.md): Floorbeam · corroded · Jun 4, 2010 · N941CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM RBL 27 FS 618 AROUND NUT PLATE EXCEEDS DAMAGE LIMITATIONS. REMOVED CORROSION AND REPAIRED FLOORBEAM AT FS 618 RBL 27 IAW EA 10-5361-02977.
- [SDR COMA2010060150120](https://openairdocs.org/sdr/COMA2010060150120.md): Bulkhead · cracked · May 30, 2010 · N941CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING AT FS 621, LBL 36.2. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230 REV D.
- [SDR COMA2010060150200](https://openairdocs.org/sdr/COMA2010060150200.md): Bulkhead · cracked · May 30, 2010 · N941CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BULKHEAD WEB CRACKED FS 621.00, LBL 18, JUST ABOVE WL 73.0. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLERS IAW REO 601R-53-61-1285.
- [SDR COMA2009120250222](https://openairdocs.org/sdr/COMA2009120250222.md): Connector · shorted · Dec 2, 2009 · N941CA · Cndair CL6002B19 · Ice/Rain Protection System Wiring
  > DURING CLIMBOUT FROM CVG RECEIVED AN ANTI-ICE CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED SHORTED CONNECTOR (P58WK).
- [SDR COMA2009052750145](https://openairdocs.org/sdr/COMA2009052750145.md): Angle · cracked · May 24, 2009 · N941CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT 559 CAP ANGLE CRACKED AT FS 559.00, LBL 18.00. PERFORMED PERMANENT REPAIR IAW REO 601R-53-41-260.
- [SDR COMA2009052750144](https://openairdocs.org/sdr/COMA2009052750144.md): Angle · cracked · May 24, 2009 · N941CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT 559 CAP ANGLE CRACKED AT FS 559.00, RBL 18.00. PERFORMED PERMANENT REPAIR IAW REO 601R-53-41-260.
- [SDR COMA0860257](https://openairdocs.org/sdr/COMA0860257.md): Skin · damaged · May 23, 2008 · N941CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN HAS DAMAGE FROM DOOR PIN AT FWD LOWER POSITION AT FS 310.00. TRIMMED OUT DAMAGE AND INSTALLED REPAIR PARTS PER REO 601R53-21-180 AND SR 99-5140-0001.
- [SDR COMA0860252](https://openairdocs.org/sdr/COMA0860252.md): Fitting · cracked · May 21, 2008 · N941CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WHILE PERFORMING TASK CARD CRJ-2-122006, SPECIAL DETAILED INSP OF THE WINDSHIELD CENTER POST AND BULKHEAD AFT POST AT FS 202.75, FOUND LOWER RT POST FITTING TO BE CRACKED. REPLACED FITTING IAW CRJ SRM 51-42-21 PGS 1-21.
- [SDR COMA0860251](https://openairdocs.org/sdr/COMA0860251.md): Door Frame · cracked · May 21, 2008 · N941CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FRAME FS 338.9 IS CRACKED AT UPPER END. REPAIRED IAW REO 601R-52-11-402.
- [SDR COMA0860250](https://openairdocs.org/sdr/COMA0860250.md): Frame · cracked · May 21, 2008 · N941CA · Cndair CL6002B19 · Fuselage Main, Frame
  > CARGO COMPARTMENT UNDERFLOOR FRAME SECTOR AT FS 605 IS CRACKED. REMOVED AND REPLACED WITH SERV FRAME IAW CRJ SRM 51-42-06 AND COMAIR SR99-5140-0001.
- [SDR COMA0860249](https://openairdocs.org/sdr/COMA0860249.md): Bulkhead · cracked · May 21, 2008 · N941CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > TEMP REPAIR PREVIOUSLY APPLIED TO FS 559.0 BULKHEAD. REMOVED TEMP REPAIR AND PERFORMED PERMANENT REPAIR IAW COMAIR SR10-53-41-0001 REV A SECTION II.
- [SDR COMA0860248](https://openairdocs.org/sdr/COMA0860248.md): Pressure Panel · cracked · May 21, 2008 · N941CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > WHILE PERFORMING TASK CARD CRJ-2-162011, PRESSURE FLOOR SKIN DETAILED INSPECTION FOUND 2 CRACKS IN THE PRESSURE FLOOR SKIN BETWEEN RBL 9 AND LBL 9. CRACKS MEASURED 2.50" IN LENGTH. THE FLOOR SKIN WAS REPAIRED IAW BOMBARDIER REO 601R-53-41-103 REV D.
- [SDR COMA0860247](https://openairdocs.org/sdr/COMA0860247.md): Frame · corroded · May 21, 2008 · N941CA · Cndair CL6002B19 · Fuselage Main, Frame
  > DURING A 72/48 MO INSPECTION, TASK CRJ-2-142005, FOUND FUSELAGE FRAME CORRODED ON TOP EDGE AND CRACKED ON LOWER EDGE. PERFORMED PERMANENT REPAIR IAW REO 601R-53-11-136.
- [SDR COMA0860244](https://openairdocs.org/sdr/COMA0860244.md): Sill · corroded · May 14, 2008 · N941CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SEVERE CORROSION FOUND ON LEFT FLOOR SILL BETWEEN FS 349.00 AND FS 364.00. REMOVED AND SPLICED SECTION OF FLOOR SILL IAW EA 10-5320-02217.
- [SDR COMA0860051](https://openairdocs.org/sdr/COMA0860051.md): Unknown · unknown · Jan 4, 2008 · N941CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5262 - ON DESCENT INTO JFK RECEIVED PROX SYSTEM CAUTION MESSAGE. EMERGENCY DECLARED, MESSAGE WENT OUT BELOW 200 KTS AND BEFORE GEAR EXTENSION. ALL INDICATIONS WERE NORMAL DURING LANDING. INSPECTED PSEU NO FAULT CODES STORED. PERFORMED SYSTEM SELF TE
- [SDR COMA0760199](https://openairdocs.org/sdr/COMA0760199.md): Flap · malfunctioned · Feb 19, 2007 · N941CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5138 - FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT 0 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
- [SDR COMA0760010](https://openairdocs.org/sdr/COMA0760010.md): Warning Light · false activation · Jan 6, 2007 · N941CA · Cndair CL6002B19 · Engine Thrust Reverser
  > FLIGHT 5662 - DURING CLIMB THRU APPROX FL 180 LEFT REV UNLOCK MESSAGE CAME ON. FOLLOWED QRH AND RETURNED BACK TO PHF AND LANDED SAFELY. INSPECTED LEFT T/R AND STOW, DEPLOY AND THROTTLE LOCKOUT SWITCHES. ALL CHECKED GOOD. OPS CHECKED T/R, OPS CHECK GOOD.
- [SDR COMA0660584](https://openairdocs.org/sdr/COMA0660584.md): Pump · faulty · Oct 20, 2006 · N941CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > FLIGHT 5395 - HYD NR 3 LOW PRESSURE CAUTION MESSAGE AT FLIGHT LEVEL 290, QTY ZERO, PRESSURE 1400 PSI. FLIGHT DIVERTED TO CMH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 3A ACMP.
- [SDR COMA0660526](https://openairdocs.org/sdr/COMA0660526.md): Switch · malfunctioned · Sep 2, 2006 · N941CA · Cndair CL6002B19 · Engine Thrust Reverser
  > FLIGHT 5542 - RIGHT REV UNLOCK MESSAGE IN FLIGHT FROM MHT TO CVG, FLIGHT DIVERTED TO MDT AND LANDED WITHOUT INCIDENT. FOUND RIGHT THRUST REVERSER STOW SWITCH OUT OF RIG. RE-ADJUSTED STOW SWITCH, OPS CHECK GOOD.
- [SDR COMA0660521](https://openairdocs.org/sdr/COMA0660521.md): Warning Light · false activation · Sep 1, 2006 · N941CA · Cndair CL6002B19 · Engine Thrust Reverser
  > FLIGHT 5664 - RIGHT REV UNLOCK MESSAGE IN FLIGHT FROM CVG TO MSP. FLIGHT DIVERTED TO IND AND LANDED WITHOUT INCIDENT. TRANSFERRED TO DMI LIST PER MEL 78-30-01.
- [SDR COMA0660517](https://openairdocs.org/sdr/COMA0660517.md): Thrust Reverser · malfunctioned · Aug 30, 2006 · N941CA · Cndair CL6002B19 · Engine Thrust Reverser
  > FLIGHT 9463- EN ROUTE PIT-CVG RECEIVED A RIGHT ENGINE THRUST REVERSER CAUTION, FLIGHT DIVERTED TO CMH. DEFERRED THE RIGHT THRUST REVERSER PER MEL 78-30-01.
- [SDR COMA0660442](https://openairdocs.org/sdr/COMA0660442.md): Light · inoperative · Jul 19, 2006 · N941CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5233 - FIRST 5 ROWS OF FLOOR TRACK EMERGENCY LIGHTING INOPERATIVE. REPLACED THE FIRST SECTION OF FLOOR TRACK LIGHTING STRIP.
- [SDR COMA0660441](https://openairdocs.org/sdr/COMA0660441.md): Light · inoperative · Jul 19, 2006 · N941CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5233 - SECTION OF FLOOR TRACK EMERGENCY LIGHTING INOPERATIVE. DEFERRED INOPERATIVE SECTION OF FLOOR TRACK LIGHTING PER MEL 33-51-01.
- [SDR COMA0560506](https://openairdocs.org/sdr/COMA0560506.md): Actuator · faulty · Sep 17, 2005 · N941CA · Cndair CL6002B19 · Hydraulic System, Main
  > FLIGHT 5321 - DURING CLIMBOUT OF CVG THE NR 2 HYDRAULIC C/B TRIPPED. REPLACED THE NR 2 HYDRAULIC SOV ACTUATOR.
- [SDR COMA0560491](https://openairdocs.org/sdr/COMA0560491.md): Warning Light · illuminated · Sep 7, 2005 · N941CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLIGHT 5089- FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
- [SDR COMA0560414](https://openairdocs.org/sdr/COMA0560414.md): Outflow Valve · malfunctioned · Jul 27, 2005 · N941CA · Cndair CL6002B19 · Pressure Regulator/Outflow Valve
  > FLIGHT 5553 - CABIN ALTITUDE CAUTION MESSAGE. REPLACED THE PRIMARY OUTFLOW VALVE.
- [SDR COMA0560318](https://openairdocs.org/sdr/COMA0560318.md): Warning Light · false activation · May 22, 2005 · N941CA · Cndair CL6002B19 · Door Warning System
  > FLIGHT 5568 CARGO DOOR CAUTION MESSAGE. COULD NOT DUPLICATE. FOUND NO DEFECTS IN CARGO DOOR OR WARNING SYSTEM.
- [SDR COMA0560246](https://openairdocs.org/sdr/COMA0560246.md): Fcu · faulty · Apr 7, 2005 · N941CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5142 RECEIVED A FLAP FAIL CAUTION WHILE PARKED AT THE GATE. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.
- [SDR COMA0560118](https://openairdocs.org/sdr/COMA0560118.md): Warning Light · illuminated · Feb 4, 2005 · N941CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5130 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. C/W EXTENSION AND RETRACTION CHECKS, NO DEFECTS FOUND.
- [SDR COMA0560037](https://openairdocs.org/sdr/COMA0560037.md): Overheat Loop · malfunctioned · Jan 6, 2005 · N941CA · Cndair CL6002B19 · Overheat Detection
  > FLIGHT 9487 ANTI ICE DUCT WARNING. REPLACED THE RIGHT WHEEL WELL SENSING LOOP.
- [SDR COMA0560036](https://openairdocs.org/sdr/COMA0560036.md): Anti-Ice System · false indication · Jan 6, 2005 · N941CA · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > FLIGHT 4959 ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. INSPECTED AND OPERATIONAL CHECKS WERE NORMAL.
- [SDR COMA0460599](https://openairdocs.org/sdr/COMA0460599.md): Skin · corroded · Nov 10, 2004 · N941CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT DURING HEAVY MAINTENANCE CHECK (PAX DOOR DETAILED INSPECTION) THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH COMAIR ENGINEERING AUTHORIZATION EA 10-5210-00499. OK FOR RETURN TO SERVIC
- [SDR COMA0460228](https://openairdocs.org/sdr/COMA0460228.md): Bulkhead · cracked · Mar 29, 2004 · N941CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACKS IN FORWARD PRESSURE BULKHEAD AT PARKING BRAKE CABLE PASS THROUGH. REPAIRED IN ACCORDANCE WITH REO 601R-53-11-539.
- [SDR COMA0460197](https://openairdocs.org/sdr/COMA0460197.md): Duct · blown · Mar 12, 2004 · N941CA · Cndair CL6002B19 · Pneumatic Distribution System
  > FLIGHT 5200 RIGHT 14TH STAGE DUCT LEAK WARNING. FOUND 14TH STAGE BLEED DUCT BLOWN APART. REPLACED DUCT.
- [SDR COMA0460141](https://openairdocs.org/sdr/COMA0460141.md): Pcu · broken · Feb 10, 2004 · N941CA · Cndair CL6002B19 · Drag Control System
  > FLIGHT 5110 GROUND SPOILER DEPLOY MESSAGE DURING APPROACH. LEFT OUTBOARD SPOILER PCU BROKEN. REPLACED PCU.
- [SDR COMA0460018](https://openairdocs.org/sdr/COMA0460018.md): Warning Light · illuminated · Jan 4, 2004 · N941CA · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > FLIGHT 5833 ANTI ICE DUCT WARNING MESSAGE. COULD NOT DUPLICATE. SYSTEM OPERATION NORMAL.
- [SDR COMA0360135](https://openairdocs.org/sdr/COMA0360135.md): Acm · Mar 9, 2003 · N941CA · Cndair CL6002B19 · Cabin Cooling System
  > FLIGHT 5892 AFTER T/O - BURNING ODOR IN COCKPIT AND CABIN.INSPECTED AIRCRAFT, NO DEFECTS NOTED, FLIGHT CHECK SATISFACTORY.
- [SDR COMA0360060](https://openairdocs.org/sdr/COMA0360060.md): Apu · Jan 29, 2003 · N941CA · Cndair CL6002B19 · APU Oil System
  > FLIGHT 5729 APU LOW OIL PRESSURE WARNING.ADDED 2.5 QUARTS OF OIL TO APU.
- [SDR COMA0360029](https://openairdocs.org/sdr/COMA0360029.md): Apu · unwanted · Jan 14, 2003 · N941CA · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > FLIGHT 5807 STRONG FUEL SMELL WHEN APU STARTED.REPLACED APU.
- [SDR COMA0360010](https://openairdocs.org/sdr/COMA0360010.md): Priority Valve · unreliable · Jan 1, 2003 · N941CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5495 LANDING GEAR DISAGREE WARNING.REPLACED THE NLG PRIORITY VALVE.
- [SDR COMA0260580](https://openairdocs.org/sdr/COMA0260580.md): Lamp · inoperative · Oct 10, 2002 · N941CA · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS ROWS 2 THUR 5 ARE INOPERABLE.REPLACED FLEXIBLE LAMP ASSEMBLY.
- [SDR COMA0160843](https://openairdocs.org/sdr/COMA0160843.md): Web · cracked · Oct 22, 2001 · N941CA · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > DURING INSPECTION DISCOVERED A CRACK IN THE ENGINE SUPPORT BOX BEAM.PERFORMED TEMPORARY REPAIR TO UPPER AND LOWER WEBS F.S. 630 IN ACCORDANCE WITH CANADAIR REO 601R-53-61-345.
- [SDR COMA0160820](https://openairdocs.org/sdr/COMA0160820.md): Skin · chafed · Oct 16, 2001 · N941CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FLIGHT N/A, DURING REPAIR OF ENGINE BOX BEAM DISCOVERED A CHAFED AREA ABOVE THE BOX BEAM AT Z-MEMBER. REPAIRED IN ACCORDANCE WITH REO 601R-53-61-448.
- [SDR COMA0160640](https://openairdocs.org/sdr/COMA0160640.md): Switch · faulty · Aug 24, 2001 · N941CA · Cndair CL6002B19 · Door Warning System
  > FLIGHT #5612. DURING CLIMB OUT OF LIT AT 9000 FT. RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.REPLACED D117 PROXIMITY SWITCH IN MAIN CABIN DOOR.
- [SDR COMA0160455](https://openairdocs.org/sdr/COMA0160455.md): Flap · failed · Jul 10, 2001 · N941CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP CAUTION MESSAGE AFTER TAKE-OFF FROM GSP, AIRCRAFT RETURNED TO THE FIELD.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIREST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3 (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGE.
- [SDR COMA0160462](https://openairdocs.org/sdr/COMA0160462.md): Bpsu · worn · Jul 10, 2001 · N941CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP CAUTION MESSAGE DURING APPROACH INTO CVG, AN EMERGENCY WAS DECLARED, AIRCRAFT LANDED SAFETLY.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 3 (D AND E)4. REPLACED THE RIGHT BRAKE POSITIONING SENSING UNIT.
- [SDR COMA0160355](https://openairdocs.org/sdr/COMA0160355.md): Bushing · worn · Mar 28, 2001 · N941CA · Cndair CL6002B19 · Vertical Stabilizer, Attach Fittings
  > RIGHT VERT STAB BUSHING AT HORZ STAB PIVOT POINT WORN. REMOVED AND REPLACED BUSHING P/N 601R-55-31-001-5 IAW CRJ AMM 20-26-00-910-803. MACHINED BUSHING IAW WVAC EO 601R-55-2345. BORE WITHIN TOLERANCE IAW CRJ DRAWING 600-21058. REAMED BUSHING IAW CRJ DRAWIN
- [SDR COMA0160322](https://openairdocs.org/sdr/COMA0160322.md): Warning System · malfunctioned · Mar 15, 2001 · N941CA · Cndair CL6002B19 · Central Warning
  > T/O CONFIG MESSAGE DURING T/O. COULD NOT DUPLICATE. OPERATIONAL CHECK OF SYSTEM NORMAL.
- [SDR COMA0061059](https://openairdocs.org/sdr/COMA0061059.md): Computer · malfunctioned · Dec 17, 2000 · N941CA · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER.

Next page: https://openairdocs.org/deregistered/N941CA-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 = 'N941CA' AND deregistration_id = 'N941CA-2018-04-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N941CA-2018-04-18/reports

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