# Service difficulty reports: N196CA, cancelled Jan 25, 2006

A list on [N196CA, cancelled Jan 25, 2006](https://openairdocs.org/deregistered/N196CA-2006-01-25.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 2 · 76 reports

- [SDR 2006FA0000047](https://openairdocs.org/sdr/2006FA0000047.md): Window Frame · cracked · Jan 11, 2006 · N196CA · Emb EMB120RT · Fuselage Main, Structure
  > PILOTS SIDE WINDOW LOWER STRUCTURAL BEAM IS CRACKED AT LEFT WINDSHIELD AFT BEAM. NORMAL OPS. (K)
- [SDR SWIA200211201](https://openairdocs.org/sdr/SWIA200211201.md): Engine · overtemp · Sep 2, 2002 · N196CA · Emb EMB120RT · Engine (Turbine/Turboprop)
  > ON CLIMBOUT (LEFT) T6 RAISED WITH POWER REDUCTION. T6 CONTINUED TO RISE TO THE POINT OF T6 WARNING. T6 FINALLY CAME DOWN TO ABOUT 684 DEGREES, PRODUCING NO TORQUE. DID A PRECAUTIONARY ENGINE SHUTDOWN. RETURNED TO LAX. REMOVED AND REPLACED LEFT ENGINE IAW
- [SDR SWIA200211150](https://openairdocs.org/sdr/SWIA200211150.md): Control Box · malfunctioned · Aug 17, 2002 · N196CA · Emb EMB120RT · Landing Gear Retraction/Extension System
  > LEFT LANDING RED LIGHTS REMAIN ON (A & B) WITH GEAR HANDLE SELECTED. INSTALLED SERVICEABLE LANDING GEAR RELAY BOX ASSY, SWUNG LANDING GEAR 35 PLUS TIMES. OPS CHECKS GOOD.
- [SDR SWIA200211114](https://openairdocs.org/sdr/SWIA200211114.md): Battery · discharged · Aug 1, 2002 · N196CA · Emb EMB120RT · Emergency Lighting
  > DURING TAXI FOR TAKEOFF, FLOOR LEVEL EMERGENCY LIGHTING FROM ROW 6 TO AFT OF AIRCRAFT ILLUMINATED. COULD NOT BE EXTINGUISHED. REPLACED EMERGENCY LIGHT BATTERY AT ROW 8. OPS CHECK GOOD.
- [SDR SWIA200211025](https://openairdocs.org/sdr/SWIA200211025.md): Striker · out of adjust · Jul 4, 2002 · N196CA · Emb EMB120RT · Door Warning System
  > AFTER TAKEOFF, CARGO DOOR LIGHT ILLUMINATED, MASTER WARNING DOORS AND DOOR CAPTION ON MAP ILLUMINATED. WARNING DOES NOT OCCUR ON GROUND. RETURNED TO RDD. ADJUSTED CARGO DOOR AFT STRIKER PLATE. OPS CHECK GOOD.
- [SDR SWIA200210835](https://openairdocs.org/sdr/SWIA200210835.md): Wire Harness · faulty · May 6, 2002 · N196CA · Emb EMB120RT · Landing Gear System Wiring
  > WITH GEAR HANDLE DOWN THE LANDING GEAR REMAINED UP AND LOCKED. LEFT THE GEAR HANDLE DOWN AND ON GO-AROUND THE LANDING GEAR CAME DOWN AND LOCKED. REPLACED WIRING HARNESS FOR LEFT MAIN LANDING GEAR PROXIMITY SENSOR. OPS CHECKS GOOD.
- [SDR SWIA200210765](https://openairdocs.org/sdr/SWIA200210765.md): Battery · discharged · Mar 29, 2002 · N196CA · Emb EMB120RT · Emergency Lighting
  > FORWARD FLOOR EMERGENCY LIGHTS ARE OUT. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-02. OPS CHECK GOOD.
- [SDR SWIA200210600](https://openairdocs.org/sdr/SWIA200210600.md): Wire Harness · malfunctioned · Jan 24, 2002 · N196CA · Emb EMB120RT · Turbine Engine System Wiring
  > LEFT EEC FAILED ON TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE UPPER WIRE HARNESS IAW POWER PLANT BUILDUP MANUAL 71-00-00. OPS CHECKED IAW MM 71-00-00. ALL PARAMETERS GOOD. P/N ON 31159-11-01, S/N OFF AA9663.
- [SDR SWIA200110574](https://openairdocs.org/sdr/SWIA200110574.md): Structure · cracked · Dec 12, 2001 · N196CA · Emb EMB120RT · Passenger/Crew Doors
  > C-CHECK, PAX DOOR LOWER AFT TRACK, CRACK ON DOOR STRUCTURE. PERFORMED REPAIR ON PASSENGER DOOR UNDER LOWER AFT TRACK PER SB 120-052-0034.
- [SDR SWIA200110355](https://openairdocs.org/sdr/SWIA200110355.md): Fastener · loose · Nov 14, 2001 · N196CA · Emb EMB120RT · Fluid Service Doors
  > SERVICE DOOR LIGHT ILLUMINATED ON CLIMB THROUGH 10,000 FEET. LIGHT WENT OUT ON DESCENT WHILE SLOWING. RETURNED TO FAT. FOUND 1 CAMLOCK ON INBOARD FUEL SERVICE DOOR LOOSE. RESECURED CAMLOCK AND INSPECTED ALL SERVICE DOORS MICROSWITCHES. NO FAULTS FOUND. W
- [SDR SWIA200110159](https://openairdocs.org/sdr/SWIA200110159.md): Uplock Sensor · dirty · Sep 8, 2001 · N196CA · Emb EMB120RT · Landing Gear Position and Warning
  > RIGHT 'A' RED GEAR LIGHT DID NOT EXTINGUISH AFTER TAKEOFF. ALL GEAR DOORS REMAINED OPEN WITH GEAR SELECTED IN UP POSITION. CYCLED AS PER QRH.CLEANED AND INSPECTED RIGHT MAIN UPLOCK SENSORS AND SWUNG GEAR 20+ TIMES. NO FAULTS FOUND.
- [SDR SWIA200110045](https://openairdocs.org/sdr/SWIA200110045.md): Window Post · cracked · Jul 18, 2001 · N196CA · Emb EMB120RT · Fuselage Main, Structure
  > CRACK FOUND IN RIGHT POST BETWEEN DIRECT VIEW WINDOW AND WINDSHIELD.FABRICATED AND INSTALLED DOUBLER IAW SB120-053-0010/3-18-88.
- [SDR SWIA972351](https://openairdocs.org/sdr/SWIA972351.md): Battery · discharged · Feb 6, 2001 · N196CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT STAY ON WHEN TURNED ON. REPLACED FORWARD EMERGENCY LIGHT BATTERY. OPS CHECKS GOOD. P/N ON: D366-04-00, S/N ON: 1213, S/N OFF: 349.
- [SDR SWIA972350](https://openairdocs.org/sdr/SWIA972350.md): Fire Loop · damaged · Feb 5, 2001 · N196CA · Emb EMB120RT · Fire Detection
  > RIGHT DET INOP ENGINE/WW LIGHT ILLUMINATED INFLIGHT. RETURNED TO LAX. INSTALLED SERVICEABLE ENGINE FIRE DETECTION LOOP ON RIGHT ENGINE IAW MM 26-11-00. OPS CHECKS GOOD. S/N ON: 92233, S/N OFF: 80052.
- [SDR SWIA972214](https://openairdocs.org/sdr/SWIA972214.md): Sequence Valve · malfunctioned · Dec 22, 2000 · N196CA · Emb EMB120RT · Landing Gear Door Actuator
  > ON DEPARTURE RETRACTED LANDING GEAR, RIGHT MAIN WOULD NOT RETRACT. BOTH A & B RED LIGHTS ILLUMINATED. CREW IN AIRCRAFT BEHIND US NOTED THE RIGHT GEAR WOULD NOT RETRACT. NOSE/LEFT RETRACTED FINE. RETURNED TO PDX. TROUBLESHOT SYSTEM, FOUND RIGHT GEAR SEQUENC
- [SDR SWIA972068](https://openairdocs.org/sdr/SWIA972068.md): Actuator · stuck · Oct 15, 2000 · N196CA · Emb EMB120RT · Elevator Tab Control System
  > AT SETTINGS BEYOND 1.0 UNITS NOSE DOWN, ELEVATOR TRIM WHEEL STICKS. THE ELECTRIC TRIM WHEEL ACTUATOR IS INCAPABLE OF OVERCOMING BEING STUCK, BUT IT CAN BE MANUALLY FORCED. NOTICEABLE AT SPEEDS GREATER THAN APPROXIMATELY 250 KIAS. REMOVED MOISTURE AND LUBED
- [SDR SWIA971978](https://openairdocs.org/sdr/SWIA971978.md): Harness · chafed · Sep 15, 2000 · N196CA · Emb EMB120RT · Engine RPM Indicating System
  > LEFT NH GAUGE BOTH ANALOG AND DIGITAL INOP DURING FLIGHT. ANALOG NEEDLE JUMPING BETWEEN 10 - 70 PERCENT AND DIGITAL JUMPING 90 - 150 PERCENT NH. DIVERTED TO PDX FROM RDM. REMOVED AND REPLACED LEFT NH GAUGE IAW 77-11-00. ALSO PERFORMED RESISTANCE CHECK OF W
- [SDR SWIA971615](https://openairdocs.org/sdr/SWIA971615.md): Uplock · out of adjust · Nov 28, 1999 · N196CA · Emb EMB120RT · Landing Gear Position and Warning
  > UPON GEAR RETRACTION THE RIGHT MAIN GEAR RED A LIGHT WORLD NOT EXTINGUISH. ALSO HEARD BANGING SOUNDS AND FELT VIBRATION. RETURNED TO FAT. ADJUSTED RIGHT MLG UPLOCK INDICATION PLUNGER SCREW IAW 32-61-01. ALL GEAR SWING CHECKS GOOD.
- [SDR SWIA971447](https://openairdocs.org/sdr/SWIA971447.md): Pin · bent · Mar 31, 1999 · N196CA · Emb EMB120RT · Landing Gear Door Retract Section
  > RIGHT MAIN FORWARD GEAR DOOR HAS COME UNLATCHED TWO TIMES IN LAST TWO FLIGHTS. STRAIGHTENED LOCK PIN AND FUNCTION APPEARS NORMAL ON GROUND.
- [SDR COMA9810148](https://openairdocs.org/sdr/COMA9810148.md): Lamp · failed · Jun 28, 1998 · N196CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY FLOOR LIGHT AT ROW 9 IS INOPERABLE. REPLACED LAMP.
- [SDR COMA9810146](https://openairdocs.org/sdr/COMA9810146.md): Actuators · malfunction · Jun 23, 1998 · N196CA · Emb EMB120RT · Trailing Edge Flap Actuator
  > INBOARD FLAPS ASYMMETRY WARNING DURING TAKEOFF. REPLACED THE INBOARD FLAPS ACTUATORS.
- [SDR COMA9810139](https://openairdocs.org/sdr/COMA9810139.md): Mechanism · malfunctioned · Jun 16, 1998 · N196CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP ASYMMETRY, INBOARD FLAPS WOULD NOT DEPLOY. COULD NOT DUPLICATE DISCREPANCY, SYSTEM OPERATIONAL CHECK SATISFACTORY.
- [SDR COMA9810085](https://openairdocs.org/sdr/COMA9810085.md): Support · cracked · Apr 6, 1998 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > CREW PREFLIGHT INSPECTION FOUND ONE RIVET HEAD BROKEN OFF IN FUSELAGE SKIN, LEFT HAND SIDE, FRAME NR 9, JUST BELOW CAPTAIN'S DV WINDOW. FURTHER INVESTIGATION REVEALED A CRACKED SKIN SUPPORT AT THAT LOCATION. THE SUPPORT WAS REPLACED PER AERODESIGN REPORT NR
- [SDR COMA9710502](https://openairdocs.org/sdr/COMA9710502.md): Actuator · failed · Dec 21, 1997 · N196CA · Emb EMB120RT · Trailing Edge Flap Actuator
  > FLAP CONTROL FAULT WARNING. REPLACED THE RIGHT OUTBOARD FLAP ACTUATOR.
- [SDR COMA9710470](https://openairdocs.org/sdr/COMA9710470.md): Autopilot · malfunctioned · Nov 4, 1997 · N196CA · Emb EMB120RT · Autopilot System
  > AUTO PILOT AND TRIM FAIL WARNINGS DURING TAKEOFF. DEFERRED AUTO PILOT SYSTEM PER MEL.
- [SDR COMA9710464](https://openairdocs.org/sdr/COMA9710464.md): Angle · cracked · Oct 23, 1997 · N196CA · Emb EMB120RT · Wing Miscellaneous Structure
  > DURING 2C INSPECTION, TASK 5320-244-02I FOUND WING TO FUSELAGE FAIRING ATTACH ANGLE PART NR 120-31657-002 CRACKED. REPAIRED ANGLE IAW APPROVED AERO-DESIGN REPORT 1226-3 REV A 2-18-95.
- [SDR COMA9710463](https://openairdocs.org/sdr/COMA9710463.md): Sill · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 161-01Z, FOUND LEFT HAND CARGO FLOOR SILL CORRODED BEYOND LIMITS. REPLACED CORRODED SILL IAW EMB 120 SRM.
- [SDR COMA9710462](https://openairdocs.org/sdr/COMA9710462.md): Cables · worn · Oct 22, 1997 · N196CA · Emb EMB120RT · Aileron Control System
  > WHILE PERFORMING TASK 5720-681-01I ON RIGHT WING, 2C INSPECTION, FOUND BOTH AILERON CABLES WORN BADLY AT NACELLE FAIR LEADS. REPLACED CABLES IAW EMB 120 MM.
- [SDR COMA9710461](https://openairdocs.org/sdr/COMA9710461.md): Control Cable · worn · Oct 22, 1997 · N196CA · Emb EMB120RT · Aileron Control System
  > WHILE PERFORMING TASK 5720-581-01I ON LEFT WING, 2C INSPECTION, FOUND BOTH AILERON CABLES WORN BADLY AT NACELLE FAIRLEADS. REPLACED CABLES IAW EMB 120 MM.
- [SDR COMA9710460](https://openairdocs.org/sdr/COMA9710460.md): Buttstrap · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION, TASK 5310-132-01I, FOUND NR 1 RIGHT SIDE BUTTSTRAP CORRODED BEYOND LIMITS. REPLACED BUTTSTRAP IAW SRM EMB-120.
- [SDR COMA9710459](https://openairdocs.org/sdr/COMA9710459.md): Crossbeam · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTIN TASK 5310-132-01I, FOUND RIGHT CROSSBEAM AT FRAME 16 CORRODED BEYOND LIMITS. REPLACED CROSSBEAM IAW EMB 120 SRM.
- [SDR COMA9710458](https://openairdocs.org/sdr/COMA9710458.md): Crossbeam · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION, TASK 5320-142-03I, FOUND RIGHT CROSSBEAM AT FRAME 23 CORRODED BEYOND LIMITS. REPLACED CROSSBEAM IAW EMB 120 SRM.
- [SDR COMA9710457](https://openairdocs.org/sdr/COMA9710457.md): Sill · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION, TASK 162-01Z, FOUND RIGHT FORWARD CARGO SILL CORRODED BEYOND LIMITS. REPLACED SILL IAW EMB-120-SRM.
- [SDR COMA9710456](https://openairdocs.org/sdr/COMA9710456.md): T Section · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION, TASK 5310-132-O1I FOUND RIGHT FRAME 16 T-SECTION CORRODED BEYOND LIMITS. REPLACED T-SECTION IAW EMB-120 SRM.
- [SDR COMA9710455](https://openairdocs.org/sdr/COMA9710455.md): Buttstrap · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 161-01Z, FOUND LEFT HAND CARGO THRESHOLD BUTTSTRAP CORRODED BEYOND LIMITS. REPLACED BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.
- [SDR COMA9710454](https://openairdocs.org/sdr/COMA9710454.md): Butt Plate · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 5310-131-01I REVEALED CENTER BUTT PLATE TO BE CORRODED. REPLACED CENTER BUTT PLATE USING APPROVED AERODESIGN REPORT NR 1671-1.
- [SDR COMA9710453](https://openairdocs.org/sdr/COMA9710453.md): Buttstrap · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 5310-131-01I REVEALED CENTER BUTTSTRAP TO BE CORRODED. REPLACED BUTTSTRAP USING EMB SRM STANDARD PRACTICES.
- [SDR COMA9710452](https://openairdocs.org/sdr/COMA9710452.md): Buttstrap · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 5310-131-01I REVEALED LEFT BUTTSTRAP TO BE CORRODED. REPLACED BUTTSTRAP USING EMB SRM STANDARD PRACTICES.
- [SDR COMA9710451](https://openairdocs.org/sdr/COMA9710451.md): Buttstrap · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 0 152-01Z, REVEALED LEFT HAND BUTTSTRAP TO BE CORRODED. REPLACED BUTTSTRAP USING EMB SRM STANDARD PRACTICES.
- [SDR COMA9710450](https://openairdocs.org/sdr/COMA9710450.md): Buttstrap · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 161-01Z REVEALED LEFT HAND CARGO BUTTSTRAP TO BE CORRODED. ALSO, FOUND THAT CARGO LINING SCREW HAD BEEN SCREWED INTO STRAP. REPLACED BUTTSTRAP USING EMB SRM STANDARD PRACTICES.
- [SDR COMA9710449](https://openairdocs.org/sdr/COMA9710449.md): Buttstrap · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 5320-147-03I REVEALED CENTER BUTTSTRAP TO BE CORRODED. REPLACED BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.
- [SDR COMA9710448](https://openairdocs.org/sdr/COMA9710448.md): Sill · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 5310-131-O1I REVEALED RIGHT FLOOR SILL (UNDER LAV) TO HAVE HEAVY CORROSION. REPLACED SILL USING EMB 120 SRM STANDARD PRACTICES.
- [SDR COMA9710447](https://openairdocs.org/sdr/COMA9710447.md): Sill · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 5310-131-01I REVEALED LEFT SILL (UNDER GALLEY) TO BE CORRODED. REPLACED SILL USING EMB 120 SRM STANDARD PRACTICES.
- [SDR COMA9710446](https://openairdocs.org/sdr/COMA9710446.md): Sill · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 5310-141-03I REVEALED LEFT NR 2 SILL TO BE CORRODED. REPLACED SILL USING EMB 120 SRM STANDARD PRACTICES.
- [SDR COMA9710445](https://openairdocs.org/sdr/COMA9710445.md): Sill · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 151-01Z REVEALED RIGHT SILL TO BE CORRODED. REPLACED SILL USING EMB 120 SRM STANDARD PRACTICES.
- [SDR COMA9710444](https://openairdocs.org/sdr/COMA9710444.md): Crossbeam · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 5310-131-O1I REVEALED LEFT FLOOR CROSSBEAM AT FRAME 15 TO BE CORRODED. REPLACED CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.
- [SDR COMA9710443](https://openairdocs.org/sdr/COMA9710443.md): Crossbeam · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 141-01Z REVEALED FLOOR CROSSBEAMS LEFT AT FRAME 20 AND LEFT AT FRAME 23 (BOTH THE SAME PART NUMBER) TO HAVE CORRODED BEYOND LIMITS. REPLACED CROSSBEAMS USING EMB 120 SRM STANDARD PRACTICES.
- [SDR COMA9710442](https://openairdocs.org/sdr/COMA9710442.md): Crossbeam · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 151-01Z REVEALED RIGHT FLOOR CROSSBEAM AT FRAME 33 TO BE CORRODED BEYOND LIMITS. REPLACED CROSSBEAM USING EMB120 SRM STANDARD PRACTICES.
- [SDR COMA9710441](https://openairdocs.org/sdr/COMA9710441.md): T Section · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 5310-131-01I REVEALED LEFT CENTER T-SECTION TO BE CORRODED BEYOND LIMITS. REPLACED T-SECTION USING EMB 120 SRM STANDARD PRACTICES.
- [SDR COMA9710439](https://openairdocs.org/sdr/COMA9710439.md): T Section · corroded · Oct 22, 1997 · N196CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 2C INSPECTION TASK 141-012 REVEALED T-SECTION AT FRAME 23 TO BE CORRODED. REPLACED T-SECTION USING EMB 120 STANDARD PRACTICES.

Next page: https://openairdocs.org/deregistered/N196CA-2006-01-25/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 = 'N196CA' AND deregistration_id = 'N196CA-2006-01-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N196CA-2006-01-25/reports

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