# Service difficulty reports: N713CA, cancelled Aug 16, 2013

A list on [N713CA, cancelled Aug 16, 2013](https://openairdocs.org/deregistered/N713CA-2013-08-16.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 · 63 reports

- [SDR COMA2011092650071](https://openairdocs.org/sdr/COMA2011092650071.md): Mechanism · out of adjust · Sep 23, 2011 · N713CA · Cndair CL6002B19 · Passenger/Crew Doors
  > EN ROUTE FROM MSP TO CVG, RECEIVED PAX DOOR LATCH CAUTION MSG. STAYED ON ABOUT 15 MIN UNTIL WE HIT BUMPS AT 6000FT. EMERGENCY DECLARED, A/C DIVERTED TO ORD LANDED SAFELY. ADJUSTED PAX DOOR LATCH MECHANISM IAW CRJ AMM. OPS CHECK GOOD.
- [SDR COMA2011091950070](https://openairdocs.org/sdr/COMA2011091950070.md): Bulkhead · cracked · Sep 19, 2011 · N713CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD CRACKED AT TOP OF AFT CARGO TRACK. REMOVED DAMAGED AREA FABRICATED PARTS PER REO 601R-53-61-1541. INSTALLED ALL FABRICATED PARTS PER REO 601R-53-61-1541.
- [SDR COMA2011091550069](https://openairdocs.org/sdr/COMA2011091550069.md): Bulkhead · cracked · Sep 15, 2011 · N713CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD CRACKED AT LINTEL ATTACHMEMT AREA. REMOVED DAMAGE AREA OF REAR BULKHEAD AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230 AND REO 601R -53-61-4190.
- [SDR COMA2011091550068](https://openairdocs.org/sdr/COMA2011091550068.md): Bulkhead · dented · Sep 15, 2011 · N713CA · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD DENTED AND GOUGED JUST INBOARD OF CONNECTOR J257. REMOVED DAMAGE AREA OF REAR BULKHEAD JUST ABOVE LINTEL FITTING AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-4190.
- [SDR COMA2011091450067](https://openairdocs.org/sdr/COMA2011091450067.md): Beam · cracked · Sep 13, 2011 · N713CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK ON BOTTOM OF FS 280 BEAM AT RBL 9. REMOVED DAMAGE FABRICATED REPAIR PARTS AND INSTALLED IAW REO601R-53-11-171 REV D.
- [SDR COMA2011091250066](https://openairdocs.org/sdr/COMA2011091250066.md): Floor Support · corroded · Sep 12, 2011 · N713CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > COCKPIT FLOOR SUPPORT AT FS 280 IS HEAVILY CORRODED (CAMLOCK ANGLE). REPLACED CAMLOCK ANGLE P/N 600-34017-351S IAW SRM 51-42-06 AND 51-42-21.
- [SDR COMA2011091250065](https://openairdocs.org/sdr/COMA2011091250065.md): Beam · cracked · Sep 12, 2011 · N713CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK ON TOP ANGLE OF 280 BEAM AT RBL 9. REPAIRED 280 BEAM P/N 600-34017-595 IAW REO 601R-53-11-136 REV A DATED 11/01/07.
- [SDR COMA2011031750027](https://openairdocs.org/sdr/COMA2011031750027.md): Control Unit · failed · Mar 16, 2011 · N713CA · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > ON CLIMBOUT FROM BOS TO RDU WITH ANTI-ICE ON RECEIVED WING OVHT WARNING MSG AT ABOUT 3000FT. EMERGENCY DECLARED, FOLLOWED QRH, MSG STAYED ON OVER 40 SEC AND EXTINGUISHED WITH RT 14TH STAGE OFF. MSG DID NOT RETURN WITH ANTI-ICE IN STBY. A/C LANDED SAFELY IN
- [SDR COMA2009092150194](https://openairdocs.org/sdr/COMA2009092150194.md): Fuel Control · leaking · Sep 16, 2009 · N713CA · Cndair CL6002B19 · APU Engine Fuel and Control
  > EN ROUTE FROM JFK TO BNA CREW NOTICED FUMES IN THE COCKPIT. PERFORMED QRH, EMERGENCY DECLARED. A/C DIVERTED TO CRW LANDED SAFELY. INSPECTED A/C FOUND APU FUEL CONTROL LEAKING. REMOVED AND REPLACED APU FUEL CONTROL.
- [SDR COMA2009081150181](https://openairdocs.org/sdr/COMA2009081150181.md): Frame · cracked · Aug 11, 2009 · N713CA · Cndair CL6002B19 · Fuselage Main, Frame
  > LEFT FRAME CAP ANGLE BEND RADIUS AT FS 559.00 CRACKED AN BL 18.00. REPAIRED CRACK AT FS 559.00 IAW REO 601R-53-41-260.
- [SDR COMA2009062250154](https://openairdocs.org/sdr/COMA2009062250154.md): Coalescer Bag · dirty · Jun 20, 2009 · N713CA · Cndair CL6002B19 · Humidity Control System
  > ON T/O F/A AND PASSENGERS REPORTED A BURNING SMELL. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE, LANDED SAFELY. REMOVED AND REPLACED COALESCER BAGS. NO FURTHER DEFECTS NOTED.
- [SDR COMA2008122450045](https://openairdocs.org/sdr/COMA2008122450045.md): Controller · faulty · Dec 24, 2008 · N713CA · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > DURING CRUISE FLIGHT RECEIVED A LEFT WING ANTI-ICE MESSAGE, FLGIHT DIVERTED TO GSO. REPLACED THE ANTI-ICE CONTROLLER.
- [SDR COMA2008121750036](https://openairdocs.org/sdr/COMA2008121750036.md): Shutoff Valve · faulty · Dec 15, 2008 · N713CA · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > ON CLIMBOUT FROM CVG RECEIVED WING OVERHEAT WARNING MSG WITH SYSTEM ON, AND IN STANDBY. ACFT RETURNED TO CVG LANDED SAFELY. REMOVED AND REPLACED LEFT ANTI-ICE MODULATING SHUTOFF VALVE.
- [SDR COMA0860300](https://openairdocs.org/sdr/COMA0860300.md): Fire Bottle · intermittent · Jun 20, 2008 · N713CA · Cndair CL6002B19 · Fire Bottle, Fixed
  > EN ROUTE FROM CLE TO SYR RECEIVED CARGO BOTTLE LOW CAUTION MSG AT 28500, STAYED ON FOR 3 MIN THEN WENT OUT. EMERGENCY DECLARED, ACFT RETURNED BACK TO CLE AND LANDED SAFELY. REMOVED AND REPLACED CARGO FIRE BOTTLE. (S)
- [SDR COMA0860299](https://openairdocs.org/sdr/COMA0860299.md): Fire Bottle · intermittent · Jun 20, 2008 · N713CA · Cndair CL6002B19 · Fire Bottle, Fixed
  > EN ROUTE FROM CLE TO SYR RECEIVED CARGO BOTTLE LOW CAUTION MSG AT 28500. STAYED ON FOR 3 MIN THEN WENT OUT. EMERGENCY DECLARED, ACFT RETURNED BACK TO CLE AND LANDED SAFELY. REMOVED AND REPLACED CARGO FIRE BOTTLE. (S)
- [SDR COMA0860287](https://openairdocs.org/sdr/COMA0860287.md): Priority Valve · leaking · Jun 13, 2008 · N713CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT EXTEND. FLUID LEVEL OF HYD SYSTEM 3 WAS 5%. DECLARED EMERGENCY, PERFORMED EMERGENCY EXTENSION, LANDED WITHOUT INCIDENT. REPLACED MLG PRIORITY VALVE, WHICH WAS LEAKING AT EXPANSION FITTING. SERVICED SYSTEM 3. NO FURTHER DEFECTS. (S)
- [SDR COMA0860284](https://openairdocs.org/sdr/COMA0860284.md): Priority Valve · faulty · Jun 10, 2008 · N713CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > RECEIVED NOSE GEAR DISAGREE MESSAGE ON APPROACH. FOLLOWED QRH, DECLARED EMERGENCY. LANDING GEAR LOWERED ON RECYCLE. LANDED WITHOUT INCIDENT. REPLACED MGL PRIORITY VALVE. NO FURTHER DEFECTS. (S)
- [SDR COMA0860276](https://openairdocs.org/sdr/COMA0860276.md): Priority Valve · faulty · Jun 9, 2008 · N713CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON APPROACH INTO CVG DURING GEAR DOWN SELECTION RECEIVED GEAR DISAGREE MSG, EXECUTED MISAPPROACH. RAN QRH SECOND GEAR DOWN SELECTION WAS SUCCESSFUL. ACFT LANDED SAFELY IN CVG. REMOVED AND REPLACED NLG PRIORITY VALVE. (S)
- [SDR COMA0760728](https://openairdocs.org/sdr/COMA0760728.md): Transducer · faulty · Dec 14, 2007 · N713CA · Cndair CL6002B19 · Engine Oil Pressure
  > FLIGHT 9658 - DURING CRUISE FLIGHT RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, PERFORMED AN I.F.S.D. AND DIVERTED TO MDT. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE OIL PRESSURE TRANSDUCER.
- [SDR COMA0760727](https://openairdocs.org/sdr/COMA0760727.md): Pump · faulty · Dec 14, 2007 · N713CA · Cndair CL6002B19 · Turbine Engine Oil System
  > FLIGHT 9658 - DURING CRUISE FLIGHT RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, PERFORMED AN I.F.S.D. AND DIVERTED TO MDT. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE LUBRICATION AND SCAVENGE PUMP.
- [SDR COMA0760440](https://openairdocs.org/sdr/COMA0760440.md): Gearbox · overheated · Jun 17, 2007 · N713CA · Cndair CL6002B19 · Turbine Engine Reduction Gear
  > FLIGHT 5589 - EN ROUTE CVG-NAS RECEIVED A RIGHT ENGINE OIL HIGH TEMPERATURE INDICATION. FLIGHT RETURNED TO CVG. SERVICED RIGHT ENGINE AGB.
- [SDR COMA0660689](https://openairdocs.org/sdr/COMA0660689.md): Warning Message · illuminated · Dec 6, 2006 · N713CA · Cndair CL6002B19 · Central Warning
  > FLIGHT 5099 - NOSE WHEEL STEERING CAUTION MESSAGE DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. INSPECTED NWS SYSTEM, NO DEFECTS NOTED. PERFORMED OPS CHECK, NO DEFECTS NOTED IAW AMM 32-51-00.
- [SDR COMA0660195](https://openairdocs.org/sdr/COMA0660195.md): Warning System · malfunctioned · Feb 26, 2006 · N713CA · Cndair CL6002B19 · Stabilizer Position Indicating
  > FLIGHT 5843 - DURING TAKEOFF AT ORF RECEIVED A TRIM CONFIGURATION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED AN OPERATIONAL CHECK OF FLIGHT CONTROL TRIM SYSTEMS AND INTERROGATED HSTCU, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.
- [SDR COMA0560701](https://openairdocs.org/sdr/COMA0560701.md): Actuator · unreliable · Dec 9, 2005 · N713CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5653 - FLAPS FAIL CAUTION. REPLACED THE LT FLAP ACTUATOR.
- [SDR COMA0560678](https://openairdocs.org/sdr/COMA0560678.md): Warning System · activated · Dec 7, 2005 · N713CA · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLIGHT 5457 - DURING DCA APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, FLIGHT LANDED WITHOUT INCIDENT. 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 FURT
- [SDR COMA0560178](https://openairdocs.org/sdr/COMA0560178.md): Proximity Switch · malfunctioned · Mar 14, 2005 · N713CA · Cndair CL6002B19 · Door Warning System
  > FLIGHT 9452 CABIN DOOR OUTER HANDLE WARNING. REPLACED PROXIMITY SWITCH DI17.
- [SDR COMA0560048](https://openairdocs.org/sdr/COMA0560048.md): Wire · loose · Jan 11, 2005 · N713CA · Cndair CL6002B19 · Light System Wiring
  > FLIGHT 5509 - 3 EMERGENCY LIGHTS INOP. REPAIRED LOOSE WIRING.
- [SDR COMA0460416](https://openairdocs.org/sdr/COMA0460416.md): Frame · corroded · Jul 14, 2004 · N713CA · Cndair CL6002B19 · Fuselage Main, Frame
  > DURING A 72/48 MO INSP, TASK CRJ-2-142005, FOUND FUSELAGE FRAME CORRODED ON TOP EDGE. PERFORMED PERMANENT REPAIR IAW COMAIR EA 10-5310-00389.
- [SDR COMA0460257](https://openairdocs.org/sdr/COMA0460257.md): Warning Light · illuminated · Apr 13, 2004 · N713CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5205 FLAP FAIL CAUTION AFTER LANDING. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0460253](https://openairdocs.org/sdr/COMA0460253.md): Latch · open · Apr 10, 2004 · N713CA · Cndair CL6002B19 · Passenger/Crew Doors
  > FLIGHT 5219 CABIN DOOR HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. FOUND DOOR HANDLE IN OPEN POSITION. OPERATIONAL CHECK OF DOOR LATCH MECH WAS NORMAL.
- [SDR COMA0360572](https://openairdocs.org/sdr/COMA0360572.md): Bracket · cracked · Dec 19, 2003 · N713CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THERE WAS A CRACKED INTERCOSTAL SUPPORT BRACKET BEHIND HYDRAULIC SYSTEM NR 1 RETURN FILTER BOWL. REMOVED THE CRACKED BRACKET. FABRICATED AND INSTALLED A NEW BRACKET IAW WVAC EO 601R-53-4486.
- [SDR COMA0260722](https://openairdocs.org/sdr/COMA0260722.md): Landing Gear · Dec 17, 2002 · N713CA · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 5053 GEAR DISAGREE WARNING MESSAGE.COULD NOT DUPLICATE EXTENSION AND RETRACTION CHECKS ALL NORMAL. HYDRAULIC PUMPS AND RESERVOIR REPLACED FOR TROUBLESHOOTING.
- [SDR COMA0260704](https://openairdocs.org/sdr/COMA0260704.md): Thermister · malfunctioned · Dec 10, 2002 · N713CA · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > FLIGHT 5859 LT WINDOW HEAT CAUTION MESSAGE. SWAPPED CONTROLLER CONNECTIONS TO THE SPARE THERMISTORS, OPERATIONAL CHECK WAS NORMAL.
- [SDR COMA0260659](https://openairdocs.org/sdr/COMA0260659.md): Windshield Wiper · broken · Nov 19, 2002 · N713CA · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > FLIGHT 5080 COPILOTS WINDSHIELD WIPER CAME APART DURING T/O.REPALCED WIPER BLADE ASSY.
- [SDR COMA0260570](https://openairdocs.org/sdr/COMA0260570.md): Control Cable · lack of lube · Oct 5, 2002 · N713CA · Cndair CL6002B19 · Aileron Control System
  > AILERON CONTROLS SEEMED STIFFENER THEN NORMAL. LUBRICATED THE LEFT AND RIGHT AILERON CONTROL ASSEMBLY PER EO 27-069RB.
- [SDR COMA0260450](https://openairdocs.org/sdr/COMA0260450.md): Skin · Jul 24, 2002 · N713CA · Cndair CL6002B19 · Wing, Plate/Skin
  > I/H WING LOWER SKIN FUEL PANEL LANDINGS @ W.S. 106.40, 127.25, 264.00 AND 294.50 HAVE CORROSION FROM 0.010" - 0.012" DEEP.REMOVED CORROSION BY BLENDING. PERFORMED EDDY CURRENT INSP TO ENSURE COMPLETE DAMAGE REMOVAL. FLAP PEENED RE-WORKED AREAS, AND REAPPLIED P
- [SDR COMA0260449](https://openairdocs.org/sdr/COMA0260449.md): Skin · cracked · Jul 23, 2002 · N713CA · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR NIB IS DAMAGED AT F.S. 310.00CUT OUT DAMAGE AND INSTALLED STRAP P/N 601R-52-11-008-1 I/A/W CRJ EO 601R-52-11-008 REV B REPAIR A.
- [SDR COMA0260448](https://openairdocs.org/sdr/COMA0260448.md): Angle · cracked · Jul 22, 2002 · N713CA · Cndair CL6002B19 · Fuselage Fixed Partitions
  > THE ANGLES AT BL 27 LH AND RH AND INTERCOSTAL AT RBL 36 AT FS 484 WERE FOUND CRACKED.REMVOED DISCREPANT PARTS, FABRICATED AND INSTALLED AND REPLACEMENT PARTS I/A/W WVAC EO 601R-53-3380 DATED 07/22/02.
- [SDR COMA0260368](https://openairdocs.org/sdr/COMA0260368.md): Aileron · Jun 12, 2002 · N713CA · Cndair CL6002B19 · Aileron Control System
  > FLIGHT 5759 HEAVIER THAN NORMAL CONTROL FORCE REQUIRED FOR ROLL AND PITCH.INSPECTED FLIGHT CONTROLS AND CABLE TENSIONS. NO DEFECTS FOUND. FORCE CHECKS WITHIN LIMITS.
- [SDR COMA0260369](https://openairdocs.org/sdr/COMA0260369.md): Flap · Jun 11, 2002 · N713CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5285 FLAPS FAILED MESSAGE DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01
- [SDR COMA0260344](https://openairdocs.org/sdr/COMA0260344.md): Engine · failed · May 30, 2002 · N713CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > FLIGHT 5376 R/H ENGINE OIL PRESSURE WARNING - FAILED BY ENGINE FAILURE.REPLACED R/H ENGINE.
- [SDR COMA0260246](https://openairdocs.org/sdr/COMA0260246.md): Paint · Apr 10, 2002 · N713CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5012 AIRCRAFT ROLLS RIGHT WHEN FLAPS EXTENDED.SANDED ROUGH PAINT ON R/H OUTBD FLAP.
- [SDR COMA0260238](https://openairdocs.org/sdr/COMA0260238.md): Actuator · binding · Apr 6, 2002 · N713CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5234 FLAPS FAILED MESSAGE. R/H OUTBD FLAP IS TWISTED.REPLACED R/H OUTBD FLAP ACTUATORS,
- [SDR COMA0260237](https://openairdocs.org/sdr/COMA0260237.md): Actuator · malfunctioned · Apr 5, 2002 · N713CA · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5393 FLAPS FAIL MESSAGE. REPLACED THE LT INBOARD FLAP ACTUATORS.
- [SDR COMA0260143](https://openairdocs.org/sdr/COMA0260143.md): Bpsu · malfunctioned · Mar 2, 2002 · N713CA · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 5079 FLAPS FAIL MESSAGE AFTER T/O.REPLACED THE L/H BPSU.
- [SDR COMA0260097](https://openairdocs.org/sdr/COMA0260097.md): Landing Gear · Feb 13, 2002 · N713CA · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > FLIGHT 5557 GEAR DISAGREE WARNING, NLG DID NOT RETRACT.FOUND NLG FLAT - SERVICED NLG I/A/W M/M INSTRUCTIONS.
- [SDR COMA0260008](https://openairdocs.org/sdr/COMA0260008.md): Bushing · mislocated · Dec 28, 2001 · N713CA · Cndair CL6002B19 · Vertical Stabilizer
  > THE R/H SIDE VERTICAL STABILIZER HAS A MIGRATING BUSHING AT HORIZONTAL STABILIZER PIVOT POINT.REMOVED THE MIGRATING BUSHING. MACHINED AND CADMIUM PLATED A NEW NOMINAL SIZE BUSHING I/A/W WVAC EO 601R-55-2910. INSTALLED THE NEW BUSHING I/A/W CRJ AMM 20-26-00-910
- [SDR COMA0260007](https://openairdocs.org/sdr/COMA0260007.md): Frame · cracked · Dec 28, 2001 · N713CA · Cndair CL6002B19 · Fuselage Main, Frame
  > THE RT SIDE FRAME AND AFT DOUBLER AT FS 718.0 BETWEEN STRINGERS 10 AND 12 WAS CRACKED. REMOVED CRACKED SECTION OF FRAME AND AFT DOUBLER AND INSTALLED A NEW SECTION OF FRAME AND AFT DOUBLER IAW REO 601R-53-61-193 REV A AND WVAC EO 601R-53-2902A.
- [SDR COMA0260006](https://openairdocs.org/sdr/COMA0260006.md): Doubler · cracked · Dec 28, 2001 · N713CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > THE L/H SIDE AFT DOUBLER AT FS718.0 WAS CRACKED BETWEEN STRINGERS 10 AND 12.REMOVED CRACKED DOUBLER AND INSTALLED A NEW DOUBLER I/A/W REO 601R-53-61-193 REV A AND WVAC EO 601R-53-2902A.
- [SDR COMA0160206](https://openairdocs.org/sdr/COMA0160206.md): Skin · cracked · Feb 5, 2001 · N713CA · Cndair CL6002B19 · Wing, Plate/Skin
  > LT LOWER WING PLANK CRACKED AT ACCESS HOLES, 540 CB WS 76.161, 550 AB WS 163.00 AND 550 FB WS 274.319. BLENDED OUT DAMAGE AND ROTO-PEENED AS REQUIRED IAW REO 601R-57-21-030.

Next page: https://openairdocs.org/deregistered/N713CA-2013-08-16/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 = 'N713CA' AND deregistration_id = 'N713CA-2013-08-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N713CA-2013-08-16/reports

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