# Service difficulty reports: N962CA, cancelled Feb 12, 2018

A list on [N962CA, cancelled Feb 12, 2018](https://openairdocs.org/deregistered/N962CA-2018-02-12.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 · 109 reports

- [SDR COMA2011121950100](https://openairdocs.org/sdr/COMA2011121950100.md): Flap · failed · Dec 18, 2011 · N962CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH INTO MHT WHEN SELECTING FLAPS TO 8 DEG RECEIVED FLAPS FAIL CAUTION MSG. FLAPS FAILED AT 0 DEG. COMPLIED WITH QRH PROCEDURES, A/C LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION. TRANSFERRED TO DEFE
- [SDR COMA2011112150092](https://openairdocs.org/sdr/COMA2011112150092.md): Pump · failed · Nov 18, 2011 · N962CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > ON T/O FROM EVV RECEIVED GEAR DISAGREE, NOSE GEAR DID NOT MOVE. EMERGENCY DECLARED, QRH FOLLOWED, A/C RETURNED TO EVV LANDED SAFELY. REMOVED AND REPLACED HYD SYSTEM 3A PUMP. OPS CHECK GOOD.
- [SDR COMA2010071250146](https://openairdocs.org/sdr/COMA2010071250146.md): Bulkhead · cracked · Jul 12, 2010 · N962CA · 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 AND DEVIATION REPAIR REO 601R-53-61-3721.
- [SDR COMA2010071250145](https://openairdocs.org/sdr/COMA2010071250145.md): Angle · cracked · Jul 12, 2010 · N962CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 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 COMA2010071250144](https://openairdocs.org/sdr/COMA2010071250144.md): Angle · cracked · Jul 12, 2010 · N962CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 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.
- [SDR COMA2010071250143](https://openairdocs.org/sdr/COMA2010071250143.md): Floor Skin · cracked · Jul 8, 2010 · N962CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CRACK IN PRESSURE FLOOR SKIN AT FS 461.00. CRACK IS APPROX 2.5 TO 3.0 INCHES LONG. PERFORMED TEMPORARY REPAIR TO PRESSURE FLOOR WEB AT FS 461.00 IAW REO 601R-53-41-103.
- [SDR COMA2010060150119](https://openairdocs.org/sdr/COMA2010060150119.md): Pump · failed · May 29, 2010 · N962CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > AT BOS DURING T/O ROLL AT 110KTS RECEIVED HYD 3B CAUTION MSG. THEN IN CLIMBOUT AFTER GEAR HANDLE UP, RECEIVED NOSE DOOR WARNING AND GEAR DISAGREE. EMERGENCY DECLARED, A/C RETURNED TO BOS LANDED SAFELY. REMOVED AND REPLACED HYD 3B PUMP. NO FURTHER DEFECTS.
- [SDR COMA0860390](https://openairdocs.org/sdr/COMA0860390.md): Wire Harness · failed · Sep 12, 2008 · N962CA · Cndair CL6002B19 · Landing Gear System Wiring
  > ON CLIMBOUT, RECEIVED ANTI-SKID CAUTION MSG. EMERGENCY DECLARED, A/C RETURNED BACK AND LANDED SAFELY. REMOVED AND REPLACED RT MLG OB ANTI-SKID WIRE HARNESS. (K)
- [SDR COMA086368](https://openairdocs.org/sdr/COMA086368.md): Accumulator · empty · Aug 24, 2008 · N962CA · Cndair CL6002B19 · Hydraulic Power Accumulator, Main
  > ON APPROACH INTO DAY RECEIVED PARKING BRAKE SOV AND 1/B ANTI-SKID MSG WHEN GEAR WAS LOWERED. EMERGENCY DECLARED, ABORTED APPROACH. ACFT LANDED SAFELY ON 2ND APPROACH. FOUND NR 3 HYD BRAKE ACCUMULATOR (I/B BRAKES) TO HAVE ZERO PRESS. SERVICED ACCUMULATOR.
- [SDR COMA0760708](https://openairdocs.org/sdr/COMA0760708.md): Connector · faulty · Dec 11, 2007 · N962CA · Cndair CL6002B19 · Light System Wiring
  > ROW 8 FLOOR EMERGENCY LIGHTING INOP. REPLACED ROW 5 EMERGENCY LIGHT JUMPER. NO FURTHER DEFECTS.
- [SDR COMA0760707](https://openairdocs.org/sdr/COMA0760707.md): Wire · chafed · Dec 11, 2007 · N962CA · Cndair CL6002B19 · Light System Wiring
  > ROW 8 FLOOR EMERGENCY LIGHTING INOP. REPAIRED CHAFED WIRE AT ROW 5 JUMPER. NO FURTHER DEFECTS.
- [SDR COMA0760706](https://openairdocs.org/sdr/COMA0760706.md): Connector · faulty · Dec 11, 2007 · N962CA · Cndair CL6002B19 · Light System Wiring
  > ROW 8 FLOOR EMERGENCY LIGHTING INOP. REPLACED ROW 5 EMERGENCY LIGHT JUMPER. NO FURTHER DEFECTS.
- [SDR COMA0760459](https://openairdocs.org/sdr/COMA0760459.md): Target · loose · Jun 29, 2007 · N962CA · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 5531 - RECEIVED GEAR DISAGREE MESSAGE UPON GEAR RETRACTION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND RIGHT MLG UPLOCK TARGET LOOSE. SECURED TARGET, ADJUSTED PROX SENSOR. NO FURTHER DEFECTS.
- [SDR COMA0760446](https://openairdocs.org/sdr/COMA0760446.md): Skin · cracked · Jun 19, 2007 · N962CA · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AFT OF NOSE LANDING GEAR CUTOUT AT RIGHT RADIUS IS CRACKED. REPAIRED FUSELAGE SKIN AFT OF NOSE LANDING GEAR CUTOUT RIGHT SIDE, IAW REO 601R-53-11-048.
- [SDR COMA0760101](https://openairdocs.org/sdr/COMA0760101.md): Handle · unknown · Jan 30, 2007 · N962CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5120 - PASSENGER DOOR OTR HANDLE CAUTION MESSAGE INFLIGHT. A/C DIVERTED TO GSO AND LANDED SAFELY. TRANSFERRED TO DMI LIST 52-70-01-1.
- [SDR COMA0660647](https://openairdocs.org/sdr/COMA0660647.md): Duct · worn · Nov 21, 2006 · N962CA · Cndair CL6002B19 · Air Distribution System
  > FLIGHT 5202 - EN ROUTE DCA-BOS RECEIVED A LEFT PACK OFF FAIL STATUS MESSAGE AND PRESSURIZATION PROBLEM, CREW DECLARED AN EMERGENCY AND DIVERTED TO PHL. FLIGHT LANDED WITHOUT INCIDENT. REPLACED UPPER DUCT FOR THE LEFT AIR CONDITIONING PACK.
- [SDR COMA0660624](https://openairdocs.org/sdr/COMA0660624.md): Priority Valve · faulty · Nov 11, 2006 · N962CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5247 - UPON SELECTING GEAR DOWN RECEIVED GEAR DISAGREE WARNING. REMOVED AND REPLACED MLG PRIORITY VALVE.
- [SDR COMA0660623](https://openairdocs.org/sdr/COMA0660623.md): Selector Valve · faulty · Nov 11, 2006 · N962CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5247 - UPON SELECTING GEAR DOWN RECEIVED GEAR DISAGREE WARNING. REMOVED AND REPLACED MLG SELECTOR VALVE.
- [SDR COMA0660349](https://openairdocs.org/sdr/COMA0660349.md): Servo · faulty · May 13, 2006 · N962CA · Cndair CL6002B19 · Autopilot Main Servo
  > FLIGHT 5373 - EN ROUTE BOS - JFK ENCOUNTERED JAMMING OF THE AILERON SYSTEM, CREW DECLARED AN EMERGENCY AND PERFORMED QRH FOR AILERON SYSTEM JAM. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE AILERON SERVO SVO-85A.
- [SDR COMA0660319](https://openairdocs.org/sdr/COMA0660319.md): Caution Message · illuminated · Apr 30, 2006 · N962CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5092 - FLAP FAILED AT 25 DEGREES DURING TAXI. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE FIRST EVENT, MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3, (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
- [SDR COMA0660301](https://openairdocs.org/sdr/COMA0660301.md): Window · cracked · Apr 12, 2006 · N962CA · Cndair CL6002B19 · Flight Compartment Windows
  > FLIGHT 5177 - DURING DESCENT FOR DCA APPROACH THE RIGHT WINDSHIELD CRACKED. REPLACED THE RIGHT WINDSHIELD.
- [SDR COMA0660140](https://openairdocs.org/sdr/COMA0660140.md): Unknown · unknown · Feb 12, 2006 · N962CA · Cndair CL6002B19 · Standard Practices/Structures
  > FLIGHT 5250 - DURING CRUISE FLIGHT ENCOUNTERED NOTICEABLE GENTLE OSCILLATION IN AFT CABIN, DEACTIVATED AUTO-PILOT AND YAW DAMPERS OSCILLATION PERSISTED. AIRCRAFT REQUIRED EXCESSIVE TRIM FOR COORDINATED FLIGHT. PERFORMED ISOLATION CHECKS OF PCU'S, NO FLUCTUAT
- [SDR COMA0560742](https://openairdocs.org/sdr/COMA0560742.md): Flap System · malfunctioned · Dec 21, 2005 · N962CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5789 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 09-20-01.
- [SDR COMA0560610](https://openairdocs.org/sdr/COMA0560610.md): Buss · unreliable · Nov 16, 2005 · N962CA · Cndair CL6002B19 · Light System Wiring
  > FLIGHT 5015 - THE AFT SECTION OF THE EMERGENCY FLOOR PATH LIGHTING INOPERABLE. REPLACED POWER STRIP.
- [SDR COMA0560545](https://openairdocs.org/sdr/COMA0560545.md): Flap System · malfunctioned · Oct 10, 2005 · N962CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5400 - FLAPS FAIL CAUTION. CND, INSPECTED FLAPS SYSTEM AND FOUND NO FAULTS.
- [SDR COMA0560519](https://openairdocs.org/sdr/COMA0560519.md): Servo Valve · malfunctioned · Sep 22, 2005 · N962CA · Cndair CL6002B19 · Nose/Tail Landing Gear
  > FLIGHT 5757- NWS CAUTION. REPLACED THE ELECTRO HYD SERVO VALVE.
- [SDR COMA0560311](https://openairdocs.org/sdr/COMA0560311.md): Reservoir · unreliable · May 18, 2005 · N962CA · Cndair CL6002B19 · Hydraulic Reservoir, Main
  > FLIGHT 5142 - GEAR DISAGREE WARNING. REPLACED THE NR 3 HYDRAULIC RESERVOIR.
- [SDR COMA0560052](https://openairdocs.org/sdr/COMA0560052.md): Pdu · faulty · Jan 18, 2005 · N962CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5786 DURING APPROACH TO CVG RECEIVED A FLAP FAIL MESSAGE AT 20 DEGREE SETTING. REPLACED THE FLAP POWER DRIVE UNIT.
- [SDR COMA0460650](https://openairdocs.org/sdr/COMA0460650.md): Bpsu · malfunctioned · Nov 24, 2004 · N962CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5815 - FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU.
- [SDR COMA0460627](https://openairdocs.org/sdr/COMA0460627.md): Bpsu · malfunctioned · Nov 16, 2004 · N962CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLT 5497 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU.
- [SDR COMA0460502](https://openairdocs.org/sdr/COMA0460502.md): Oil System · overserviced · Sep 6, 2004 · N962CA · Cndair CL6002B19 · Engine Oil Indicating System
  > FLIGHT 5207 DURING CLIMBOUT OF CVG RECEIVED AN OIL TEMPERATURE CAUTION ON ENGINE NR 2. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. DRAINED EXCESSIVE OIL FROM GEARBOX, PERFORMED GROUND RUNS WITH SATISFACTORY RESULTS.
- [SDR COMA0460369](https://openairdocs.org/sdr/COMA0460369.md): Floorbeam · corroded · Jun 15, 2004 · N962CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CARGO BAY FLOORBEAM CAP AT LBL 9 CORRODED BETWEEN FS 589 AND FS 610. REMOVED CORRODED CAP AND INSTALLED NEW CAP P/N 601R35031-3 I/A/W CRJ SRM 51-42-13 AND CRJ SRM 51-42-06.
- [SDR COMA0460370](https://openairdocs.org/sdr/COMA0460370.md): Frame · cracked · Jun 15, 2004 · N962CA · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME RADIUS CRACKED ABOVE STRINGER 10 AT LEFT HAND FS 718. FRAME RADIUS CRACKED BELOW STRINGER 11 AT LEFT HAND FS 718. PREVIOUS REPAIR HOLE PATTERN BETWEEN STRINGER 10 AND 11 WILL NOT ALLOW FOR EO 53-027. REMOVED AND REPLACED SECTION OF FS 718.00. COMPLIE
- [SDR COMA0460371](https://openairdocs.org/sdr/COMA0460371.md): Skin · cracked · Jun 15, 2004 · N962CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK CRACKED AT WS 148.019. COMPLIED WITH EO 57-020 REV A. MODIFICATIONS OF THE LEFT WING LOWER WING PLANK AT WS 148.
- [SDR COMA0460372](https://openairdocs.org/sdr/COMA0460372.md): Intercostal · damaged · Jun 15, 2004 · N962CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK FOUND RIGHT SIDE CABIN ON CABLE INTERCOSTAL UNDER EMERGENCY EXIT BETWEEN 409 AND 128 TO 559 PRESSURE FLOOR SKIN. REPAIRED DAMAGE ON CABLE INTERCOSTAL UNDER EMERGENCY EXIT IAW REO 601R-53-41-223.
- [SDR COMA0460373](https://openairdocs.org/sdr/COMA0460373.md): Skin · corroded · Jun 15, 2004 · N962CA · Cndair CL6002B19 · Wing, Plate/Skin
  > FRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 650CB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE AT 650CB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANEL 650CB IAW CRJ AMM
- [SDR COMA0460374](https://openairdocs.org/sdr/COMA0460374.md): Skin · corroded · Jun 15, 2004 · N962CA · Cndair CL6002B19 · Wing, Plate/Skin
  > FRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 650BB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE AT 650BB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANEL 650BB IAW CRJ AMM
- [SDR COMA0460375](https://openairdocs.org/sdr/COMA0460375.md): Skin · corroded · Jun 15, 2004 · N962CA · Cndair CL6002B19 · Wing, Plate/Skin
  > FRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 650BB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE AT 650BB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANED 650BB IAW CRJ AMM
- [SDR COMA0460376](https://openairdocs.org/sdr/COMA0460376.md): Skin · corroded · Jun 15, 2004 · N962CA · Cndair CL6002B19 · Wing, Plate/Skin
  > FRETTING DAMAGE NOTED ON LEFT HAND WING PLANK LOWER ACCESS HOLE AT 550 CB. BLENDED FRETTING AREAS IAW 601R-57-21-030. ALODINED AND PRIMED IMW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON PANEL 550 CB AMM 51-80-00. BOND CHECK GOOD.
- [SDR COMA0460377](https://openairdocs.org/sdr/COMA0460377.md): Intercostal · cracked · Jun 15, 2004 · N962CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON LEFT SIDE CABIN ON CABLE INTERCOSTAL UNDER EMERGENCY EXIT BETWEEN 409 AND 28 AND 559 PRESSURE FLOOR SKIN. REPAIRED DAMAGE ON CABLE INTERCOSTAL UNDER EMERGENCY EXIT IAW REO 601R53-41-223.
- [SDR COMA0460378](https://openairdocs.org/sdr/COMA0460378.md): Floorbeam · corroded · Jun 15, 2004 · N962CA · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CARGO BAY FLOORBEAM CAP AT LBL 27 HAS SURFACE CORROSION. REMOVED CORRODED CAP AND INSTALL NEW (P/N 601R35031) IAW CRJ SRM 51-42-06 AND 51-42-13. LOCATED AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1049 AND REO 601R-53-61-1046.
- [SDR COMA0460379](https://openairdocs.org/sdr/COMA0460379.md): Skin · corroded · Jun 15, 2004 · N962CA · Cndair CL6002B19 · Wing, Plate/Skin
  > FRETTING DAMAGE NOTED ON RIGHT HAND WING LOWER ACCESS HOLE AT 640FB. BLENDED FRETTING AREAS OF RIGHT HAND ACCESS HOLE AT 640FB IAW REO 601R-57-21-030. ALODINED AND PRIMED IAW CRJ SRM 51-21-11. PERFORMED ELECTRICAL BOND CHECK ON FUEL PANEL 640FB IAW CRJ AMM
- [SDR COMA0460380](https://openairdocs.org/sdr/COMA0460380.md): Skin · punctured · Jun 15, 2004 · N962CA · Cndair CL6002B19 · Engine Cowling System
  > RIGHT LOWER TRANS COWL HAS PUNCTURE THRU OUTER SKIN. REPAIRED RIGHT HAND LOWER TRANS COWL IAW AERODESIGN REPORT 5170-1.
- [SDR COMA0460072](https://openairdocs.org/sdr/COMA0460072.md): Signal Cond Unit · malfunctioned · Jan 19, 2004 · N962CA · Cndair CL6002B19 · Engine BMEP/Torque Indicating
  > FLIGHT 5499 RT ENGINE VIBRATION CAUTION DURING T/O. REPLACED THE SIGNAL CONDITIONER.
- [SDR COMA0460050](https://openairdocs.org/sdr/COMA0460050.md): Monitor · malfunctioned · Jan 12, 2004 · N962CA · Cndair CL6002B19 · Engine Indicating System
  > FLIGHT 5701 RIGHT ENGINE VIBRATION INDICATION DURING T/O. COULD NOT DUPLICATE. RESET VIBRATION MONITOR, RUN CHECKS WERE NORMAL.
- [SDR COMA0460013](https://openairdocs.org/sdr/COMA0460013.md): Warning Light · illuminated · Jan 4, 2004 · N962CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLIGHT 5791 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0360492](https://openairdocs.org/sdr/COMA0360492.md): Frame · cracked · Oct 29, 2003 · N962CA · Cndair CL6002B19 · Fuselage Main, Frame
  > RT 718 FRAME CRACKED. REPAIRED IAW SERVICE BULLETIN 601R-53-055.
- [SDR COMA0360457](https://openairdocs.org/sdr/COMA0360457.md): Diode · malfunctioned · Oct 14, 2003 · N962CA · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > FLIGHT 5771 RT WINDSHIELD HEAT CAUTION MESSAGE. REPLACED THE DIODE BOARD ASSY.
- [SDR COMA0360323](https://openairdocs.org/sdr/COMA0360323.md): Warning Light · illuminated · Jul 15, 2003 · N962CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5698 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0360064](https://openairdocs.org/sdr/COMA0360064.md): Buss · Jan 30, 2003 · N962CA · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5785 ROW 1 EMERGENCY FLOOR LIGHTING IS INOP.CLEANED WATER CONTAMINATIN FROM LIGHT STRIP.

Next page: https://openairdocs.org/deregistered/N962CA-2018-02-12/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 = 'N962CA' AND deregistration_id = 'N962CA-2018-02-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N962CA-2018-02-12/reports

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