# Service difficulty reports: N587CA, cancelled Aug 28, 2017

A list on [N587CA, cancelled Aug 28, 2017](https://openairdocs.org/deregistered/N587CA-2017-08-28.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR RDS121112SDR](https://openairdocs.org/sdr/RDS121112SDR.md): Pitot Tube · failed · Feb 23, 2011 · N587CA · Cvac 440 · Pitot/Static System
  > NR 2 PITOT SWITCH TRIPPED IN-FLIGHT, PULLED CIRCUIT BREAKER AS PRECAUTION, SMELLED "ELECTRICAL" ODOR PRIOR TO PITOT TRIPPING. NR 2 PITOT SYS CHECK. ALL ELECTRICAL CONNECTIONS AND BREAKER, NO "ELECTRICAL" ODOR. ALL IAW MM 34-11-1, PAGE 200-(3).
- [SDR RDS121108](https://openairdocs.org/sdr/RDS121108.md): Processor · failed · Aug 5, 2010 · N587CA · Cvac STC440T · Air Collision Avoidance System
  > TCAS INOP. FLAGGED ON ALL INDICATORS. SMELLED SMOKE. TCAS C/B PULLED. R & R TCAS PROCESSOR, PN 066-500002120, SN OFF 1547, SN ON 1687. TEST IAW CV640, MM CH 34-45-1, PG 400-1A.
- [SDR RDS121107](https://openairdocs.org/sdr/RDS121107.md): Relay · failed · Aug 3, 2010 · N587CA · Cvac 440 · Fire Detection
  > NR1 ENGINE FIRE LIGHT CAME ON INTERMITTENTLY DURING TURBULENCE AND ROUGH PAVEMENT. R & R FIRE DETECTOR BOX PN 33958-3, SN OFF 3654, ON 829 TEST OK. TEST IAW CH 20-1-PAGE 1-20.1-2-3 CV 440 MM. "NOTE" TAPPING ON FIRE DETECTOR PANEL COVER SIMULATED THE LIGHT C
- [SDR RDS121092](https://openairdocs.org/sdr/RDS121092.md): Pcu · failed · Jan 27, 2010 · N587CA · Cvac 440 · Propeller Controlling System
  > ON 6/18/09, WHILE TAXIING FOR TAKEOFF, OBSERVED SMOKE COMING FROM THE RT ENGINE, THE ENGINE WAS SHUTDOWN AND SECURED. THE PROPELLER MOVED OUT OF "FINE" PITCH POSITION CAUSING THE ENGINE TO OVERHEAT. THE CAUSE OF PROPELLER MOVEMENT WAS THE INTERNAL FAILURE OF
- [SDR JRA2009F00001](https://openairdocs.org/sdr/JRA2009F00001.md): Engine · overtemp · Jun 18, 2009 · N587CA · Cvac 440 · Engine (Turbine/Turboprop)
  > WHILE TAXIING FOR TAKEOFF, OBSERVED SMOKE COMING FROM THE RT ENGINE, ENGINE WAS SHUTDOWN AND SECURED. THE PROPELLER MOVED OUT OF "FINE" PITCH POSITION CAUSING THE ENGINE TO OVERHEAT, CAUSE OF PROPELLER MOVEMENT AT THIS TIME UNKNOWN. THE ENGINE NEEDS TO BE RE
- [SDR JRA2009F00000](https://openairdocs.org/sdr/JRA2009F00000.md): Filter · dirty · Mar 7, 2009 · N587CA · Cvac 440 · Engine Fuel Distribution
  > RT FUEL FILTER BLOCKED LIGHT CAME ON DURING TAKEOFF. TAKEOFF WAS WITH WATER METH (ON) AND WAS ABORTED, THE WARNING LIGHT WENT OUT ON POWER REDUCTION. MX PERFORMED AN INSP OF THE NR 2 FUEL FILTER, REMOVED AND REPLACED FUEL FILTER ENGINE NR 2, RUN UP CHECKED S
- [SDR JRA2008F00000](https://openairdocs.org/sdr/JRA2008F00000.md): Spring Assy · stretched · Nov 14, 2008 · N587CA · Cvac STC440 · Aileron Control System
  > AILERON CONTROL CABLES BINDING TO THE RIGHT FROM FULL LEFT POSITION. INSPECTION OF AILERON CONTROL CABLES REVEALED STRETCHED SPRING AT RUDDER INTERCONNECT. REMOVED AND REPLACED SPRING IAW 440 MM, SEC 8-2, PAGE 26. OPS CHECK OK. (K)
- [SDR RDS12120061](https://openairdocs.org/sdr/RDS12120061.md): Axle · cracked · Oct 18, 2006 · N587CA · Cvac 440 · Nose/Tail Landing Gear Strut/Axle
  > WHEN REMOVING NOSE AXLE TO C/W AD83-01-02 FOR THE 12,000 HOUR MAGNETIC PARTICLE TESTING. A CRACK AROUND THE AXLE FLANGE THAT THE BEARING SPACER RIDES AGAINST WAS NOTICED. REMOVED AND REPLACED WITH NEW AXLE, RETURNED AIRCRAFT TO SERVICE.
- [SDR JRAA587062305](https://openairdocs.org/sdr/JRAA587062305.md): Skin Panel · corroded · Jun 23, 2005 · N587CA · Cvac 640340D · Nacelle/Pylon, Plate/Skin
  > SURFACE CORROSION WAS FOUND ON THE RT IB SKIN PANEL AT APPROX STA 96.91. THIS CORRODION WAS NOTED UNDER THE INSULATION PANEL LOWER SIDE. REPLACEMENT OF SKIN PANEL IN PROGRESS. (K)
- [SDR JRAA587060705](https://openairdocs.org/sdr/JRAA587060705.md): Longeron · corroded · Jun 7, 2005 · N587CA · Cvac 440 · Wing, Longeron/Stringer
  > INTERGRANULAR CORROSION WAS FOUND ON THE LONGERON CHANNEL AT FUSELAGE BUTTOCK LINE 0, WING STATION 403.0. THIS CORROSION NOTED ON THE LT SIDE, 10 INCHES FORWARD OF THE REAR LOWER WING SPAR. ACCESS THROUGH THE LT WING IB DRY BAY PANEL. (K)
- [SDR 2004F00349](https://openairdocs.org/sdr/2004F00349.md): Check Valve · corroded · Aug 6, 2004 · N587CA · Cvac 440 · Water Injection System
  > BAK - DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PART REPLACED. (M)
- [SDR 2004F00347](https://openairdocs.org/sdr/2004F00347.md): Tube · corroded · Aug 6, 2004 · N587CA · Cvac 440 · Water Injection System
  > BAK - DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSOIN ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PARTS REPLACED. (M) JRAA
- [SDR 2004F00346](https://openairdocs.org/sdr/2004F00346.md): Transmitter · corroded · Aug 6, 2004 · N587CA · Cvac 440 · Water Injection System
  > DUIRNG WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. TRANSMITTER REPLACED. (M)
- [SDR 2004F00344](https://openairdocs.org/sdr/2004F00344.md): Door · corroded · Aug 6, 2004 · N587CA · Cvac 440 · Water Injection System
  > BAK - DUIRNG WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. DOOR REPLACED. (M)
- [SDR 2004F00343](https://openairdocs.org/sdr/2004F00343.md): Bellmouth · corroded · Aug 6, 2004 · N587CA · Cvac 440 · Water Injection System
  > DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION AND SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PARTS REPLACED. (M)
- [SDR JRAA0520042](https://openairdocs.org/sdr/JRAA0520042.md): Floorbeam · corroded · May 20, 2004 · N587CA · Cvac 440 · Fuselage Main, Floor Beam
  > DURING A SCID INSPECTION 53-20, CORROSION WAS FOUND ON FLOORBEAM AT STA 681.0 RT SIDE AT BELTFRAME. AN AREA OF APPROX 3 INCHES X 5 INCHES ON THIS FLOORBEAM WAS FOUND CORRODED AT BELTFRAME ATTACH POINT AROUND RIVETS. THE CORROSION HAD PROGRESSED THROUGH 50 PE
- [SDR JRAA0520041](https://openairdocs.org/sdr/JRAA0520041.md): Floorbeam · corroded · May 20, 2004 · N587CA · Cvac 440 · Fuselage Main, Floor Beam
  > DURING A SCID INSPECTION 53-20, A MISSING RIVET HEAD WAS FOUND AT STA 712.0. RT SIDE AT THE FLOORBEAM TO BELTFRAME ATTACH POINT. CORROSION WAS FOUND UNDER RIVET HEAD. NO OTHER RIVETS WERE FOUND TO BE CORRODED AT THIS TIME. RIVET REPLACEMENT IN PROGRESS AT
- [SDR JRAA0520043](https://openairdocs.org/sdr/JRAA0520043.md): Beltframe · corroded · May 20, 2004 · N587CA · Cvac STC440 · Fuselage Main, Frame
  > DURING A SCID INSPECTION, CORROSION WAS FOUND ON RT BELTFRAME STATION 665.0 AT FLOOR LINE. APPROX. 8.5 INCHES OF THE BELTFRAME IS CORRODED AT THE FLOORBEAM ATTACH POINT. SOME OF THE CORROSION EXTENDS BELOW THE FLOOR LINE. REPAIR IN PROGRESS AT THIS TIME.
- [SDR JRA2003F00000](https://openairdocs.org/sdr/JRA2003F00000.md): Line · leaking · Feb 27, 2003 · N587CA · Cvac 640340D · Hydraulic System, Main
  > AFTER MOVING THE LANDING GEAR HANDLE (DOWN) AND SELECTING FLAPS (DOWN); THE HYDRAULIC PRESSURE GAUGE READ ZERO PSI. NO FLUID WAS VISIBLE IN THE HYDRAULIC RESERVOIR SIGHT TUBE. WITH BYPASS VALVE SELECTOR (UP) BRAKES OPERATED. HYDRAULIC LINE WAS REPAIRED.
- [SDR JRA2002F00003](https://openairdocs.org/sdr/JRA2002F00003.md): Battery · overheated · Apr 24, 2002 · N587CA · Cvac 640340D · Battery/Charger System
  > AFTER ARRIVAL, AIRCRAFT POWERED BY BATTERY FOR 30 MIN. - FANS, LIGHTS, CARGO DOOR, ECT. WHEN POWERED UP, NOTED 18 V, TURNED ON BATT INTERLOCK OVERRIDE FOR A FEW MINUTES WITH GPU ON- BATTERY TEMP 120 DEGREES, FOLLOWED COM PROCEDURE AND LOWERED BATTERIES. BAT
- [SDR GAIA9644](https://openairdocs.org/sdr/GAIA9644.md): Frame · corroded · Dec 10, 1996 · N587CA · Cvac 440 · Nacelle/Pylon, Frame/Spar/Rib
  > DURING C-CHECK INSPECTION, FOUND CORROSION ON THE INBOARD LEFT NACELLE FRAME AT STATION 150. THE ABOVE DAMAGE WAS REPAIRED IAW KHA. EA NR CV-54-31. BY SPLICING IN A NEW SECTION OF NACELLE FRAME. THE ABOVE EA NR CV-54-31 WAS (DER) APPROVED ON FAA FORM 8110-3
- [SDR GAIA9623A](https://openairdocs.org/sdr/GAIA9623A.md): Inverter · failed · Jul 12, 1996 · N587CA · Cvac 440 · AC Inverter
  > YIP/OKC - FLT 587 - TWENTY NM FROM COLUMBIA, MISSOURI, THE ACFT FDR AND GPWS WARNING LIGHTS ILLUMINATED. ABOUT TEN SECONDS LATER, THE FLIGHT CREW NOTED SMOKE IN THE COCKPIT. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES, NOTIFIED ATC, DECLARED AN EMERGENCY

## 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 = 'N587CA' AND deregistration_id = 'N587CA-2017-08-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N587CA-2017-08-28/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.