# Service difficulty reports: N242CJ, cancelled Jul 23, 2013

A list on [N242CJ, cancelled Jul 23, 2013](https://openairdocs.org/deregistered/N242CJ-2013-07-23.md).

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

- [SDR NSVA20120310469](https://openairdocs.org/sdr/NSVA20120310469.md): Rib · corroded · Mar 10, 2012 · N242CJ · Saab 340B · Wing, Rib/Bulkhead
  > REPAIRED CORROSION ON RIGHT WING RIB LOWER FLANGE AT WS 42.3 IAW TD 340-57-12-06.
- [SDR NSVA2011320](https://openairdocs.org/sdr/NSVA2011320.md): Skin Panel · cracked · Dec 5, 2011 · N242CJ · Saab 340B · Nacelle/Pylon, Plate/Skin
  > CRACK IN PREVIOUS REPAIR LT NACELLE INBD SKIN PANEL.
- [SDR NSVA2010139](https://openairdocs.org/sdr/NSVA2010139.md): Wire · broken · Aug 24, 2010 · N242CJ · Saab 340B · Flight Control System Wiring
  > NOSE PITCH TRIM INTERMITTENTLY ACTUATES NOSE DOWN IN FLIGHT. FIXED BROKEN WIRE ON SERVO ACTUATOR.
- [SDR NSVA201098](https://openairdocs.org/sdr/NSVA201098.md): Smoke Detector · defective · Jun 16, 2010 · N242CJ · Saab 340B · Smoke Detection
  > AVIONICS SMOKE LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR.
- [SDR NSVA201068](https://openairdocs.org/sdr/NSVA201068.md): Panel · damaged · Mar 30, 2010 · N242CJ · Saab 340B · Fuselage Miscellaneous Structure
  > MAJOR REPAIR FOR DENTS AND CORROSION ON RT CABIN SIDE PANEL AT STA 300 THROUGH STA 350 IAW TD 340-53-10-22.
- [SDR 2010F00076](https://openairdocs.org/sdr/2010F00076.md): Panel · damaged · Mar 30, 2010 · N242CJ · Saab 340B · Fuselage Main, Plate/Skin
  > PERMANENT MAJOR REPAIR TO FOR DENTS AND CORROSION ON RT CABIN SIDE PANEL AT STA 300 THROUGH STA 350, IAW TD 340-53-10-22 AND SDS-020175.
- [SDR NSVA2009074](https://openairdocs.org/sdr/NSVA2009074.md): Receptacle · damaged · Dec 6, 2009 · N242CJ · Saab 340B · External Power System
  > GPU RECEPTACLE DAMAGE, RAMP AGENT DROVE AWAY FROM AIRCRAFT WHILE GPU WAS STILL ATTACHED.
- [SDR NSVA2009017](https://openairdocs.org/sdr/NSVA2009017.md): Detector · malfunctioned · Apr 3, 2009 · N242CJ · Saab 340B · Overheat Detection
  > LEFT TAIL PIPE HOT LIGHT CAME ON IN FLIGHT, WENT OFF AFTER 3-5 MINUTES. ENGINE WAS NOT SHUT DOWN. REMOVED AND REPLACED LT TAIL PIPE ASSY WITH ALL 3 SPOT DETECTORS ON/OFF P/N:7071125-507, ALL 3 SPOT DETECTORS TSO: 183FH, IAW AMM 54-30-05-02. OPS CHECKS GOOD.
- [SDR NSVA2008025](https://openairdocs.org/sdr/NSVA2008025.md): Connector · dirty · May 9, 2008 · N242CJ · Saab 340B · Overheat Detection
  > TAIL PIPE HOT LIGHT IN FLIGHT. CLEANED CONNECTIONS ON TAILPIPE HOT LIGHT SENSORS, OPS CHECK GOOD IAW SAAB MM 26-12-00.
- [SDR NSVA20070177](https://openairdocs.org/sdr/NSVA20070177.md): Actuator · malfunctioned · Jul 6, 2007 · N242CJ · Saab 340B · Rudder Control System
  > RUDDER LIMIT LIGHT ILLUMINATED ON GROUND WHEN GUST LOCK RELEASED, NO RUDDER TRAVEL AVAILABLE. REMOVED AND REPLACED RUDDER LIMITER ACTUATOR P/N ON 8618M16 SN ON 008028A SN OFF 08009A IAW MM 27-21-53, OPS CHK GOOD.
- [SDR NSVA20070165](https://openairdocs.org/sdr/NSVA20070165.md): Warning Light · illuminated · Jun 25, 2007 · N242CJ · Saab 340B · Central Warning
  > ABORTED TAKEOFF DUE TO "CONFIG" MASTER WARNING. PERFORMED OPERATIONAL CHECK OF TAKEOFF CONFIGURATION WARNING IAW SAAB 340 AMM 31-50-00-05 STEP 3, NO DEFECTS NOTED.
- [SDR NSVA20070028](https://openairdocs.org/sdr/NSVA20070028.md): Control Quadrant · unknown · Feb 5, 2007 · N242CJ · Saab 340B · Engine Controls
  > FOUND FLIGHT IDLE OPEN LIGHT ILLUMINATED AFTER TAKEOFF. REPLACED CONTROL QUADRANT IAW SA AMM 76-10-05 FUNCTIONAL TEST REQUIRED, PN: 531624, SN ON: 023 SN OFF: 061. PERFORMED OPERATIONAL CHECK OF QUADRANT CONTROL IAW SA MM 71-00-00. OPERATIONAL CHECK GOOD.
- [SDR NSVA200600125](https://openairdocs.org/sdr/NSVA200600125.md): Light · odor · Aug 22, 2006 · N242CJ · Saab 340B · Passenger Compartment Lighting
  > STRONG BURNING ODOR COMING FROM AFT CABIN. FOUND ODOR COMING FROM AFT OVERHEAD LIGHT. REMOVED OVERHEAD LIGHT AND INSPECTED, NO DEFECTS WERE NOTICED.
- [SDR NSVA200600088](https://openairdocs.org/sdr/NSVA200600088.md): Autocoarsen Sys · malfunctioned · Jun 22, 2006 · N242CJ · Saab 340B · Propeller Feathering/Reversing
  > AUTO COARSEN ANNUNCIATOR ILLUMINATED UPON INITIAL POWER APPLICATION FOR TAKEOFF. TAXIED OFF THE RUNWAY AND RETURNED TO GATE. ANNUNCIATOR TURNED OFF AS SOON AS AUTO COARSEN SWITCH WAS TURNED OFF. PERFORMED AUTO COARSEN TEST IAW 61-22-00-05, OPS CHECK GOOD.
- [SDR NSVA200600082](https://openairdocs.org/sdr/NSVA200600082.md): Battery Pack · inoperative · Jun 20, 2006 · N242CJ · Saab 340B · Emergency Lighting
  > EMERGENCY LIGHT POWER PACK 3 INOP. REMOVED AND REPLACED NR 3 POWER PACK SUPPLY.
- [SDR NSVA200600080](https://openairdocs.org/sdr/NSVA200600080.md): Unknown · unknown · Jun 18, 2006 · N242CJ · Saab 340B · Standard Practices/Structures
  > T/O ROLL AUTOCOARSEN ON CWP CAME ON. TRIED TO RESET AND CAME ON AGAIN. PERFORMED AUTOCOARSEN COMPUTER TEST AND ADJUSTMENT, OPS CHECK GOOD.
- [SDR NSVA200600075](https://openairdocs.org/sdr/NSVA200600075.md): Connector · dirty · Jun 14, 2006 · N242CJ · Saab 340B · Engine BMEP/Torque Indicating
  > RT TORQUE INDICATION WENT TO ZERO DURING TAKE-OFF. THOROUGHLY CLEANED CANNON PLUGS FOR TORQUE SENSOR AND DEC CANNON PLUGS GROUND RAN A/C OPS CK GOOD TORQUE INDICATION IS NORMAL AT THIS TIME.
- [SDR 09082005A](https://openairdocs.org/sdr/09082005A.md): Control Panel · stuck · Sep 3, 2005 · N242CJ · Saab 340B · Propeller Controlling System
  > CONTROL TORQUE ON TAKEOFF SWITCH BROKEN, STUCK IN APR MODE. DEFERRED IN LGA, REMOVED AND REPLACED CTOT PANEL. OPS CHECK GOOD AND CLEARED MEL'S IN HYA.
- [SDR 09072005B](https://openairdocs.org/sdr/09072005B.md): Limiter · inoperative · Sep 2, 2005 · N242CJ · Saab 340B · Rudder Control System
  > RUDDER LIMITER INOP. MEL'ED.
- [SDR 08152005D](https://openairdocs.org/sdr/08152005D.md): Wire Harness · damaged · Aug 15, 2005 · N242CJ · Saab 340B · Fire Protection System Wiring
  > TAIL PIPE HOT LIGHT. REMOVED AND REPLACED 3 DETECTORS AND MIDDLE WIRE HARNESS.
- [SDR 08142005A](https://openairdocs.org/sdr/08142005A.md): Wire · broken · Aug 14, 2005 · N242CJ · Saab 340B · Fire Protection System Wiring
  > RT TAIL PIPE HOT LIGHT WILL NOT EXTINGUISH. REPAIRED BROKEN WIRE IN TAIL PIPE COWLING.
- [SDR 06252005](https://openairdocs.org/sdr/06252005.md): Engine · failed · Jun 25, 2005 · N242CJ · Saab 340B · Engine (Turbine/Turboprop)
  > RIGHT ENGINE FAILED INFLIGHT.
- [SDR 06232005B](https://openairdocs.org/sdr/06232005B.md): Transducer · malfunctioned · Jun 23, 2005 · N242CJ · Saab 340B · Engine Oil Pressure
  > RT ENGINE OIL PRESSURE LIGHT ILLUMINATED AFTER TOUCHDOWN, PROP PSI READS 0. REMOVED AND REPLACED TRANSDUCER, OPS CHECK GOOD.
- [SDR 06222005C](https://openairdocs.org/sdr/06222005C.md): Connector · loose · Jun 22, 2005 · N242CJ · Saab 340B · Engine Oil Pressure
  > LEFT OIL PRESSURE READS 0 PSI IN FLIGHT. FOUND LOOSE CONNECTOR ON OIL PRESSURE TRANSMITTER. CLEANED AND SECURED.
- [SDR 314041](https://openairdocs.org/sdr/314041.md): Smoke Detector · false indication · Nov 7, 2004 · N242CJ · Saab 340B · Smoke Detection
  > AVIONIC SMOKE LIGHT ILLUMINATE IN FLIGHT.
- [SDR 161041](https://openairdocs.org/sdr/161041.md): Connector · damaged · Jun 8, 2004 · N242CJ · Saab 340B · Electrical Connectors
  > LEFT OVERWING EMERGENCY EXIT SIGN INOP. FOUND WIRES IN CONNECTOR SEVERED, RE-INSTALLED IAW SAAB 33-50-00, OP CHECKED GOOD.
- [SDR NSVA200300019](https://openairdocs.org/sdr/NSVA200300019.md): Bearing · destroyed · Mar 7, 2003 · N242CJ · Saab 340B · Wheel/Ski/Float
  > FLIGHT CREW FELT NOSE WHEEL SHIMMY DURING LANDING AND TAXI AT PVD. MAINTENANCE WAS DISPATCHED TO AIRCRAFT AND REMOVED THE NOSE WHEELS AND FOUND THE LT INBOARD WHEEL BEARING FROZEN TO THE NLG AXLE FROM LACK OF LUBRICATION. MAINTENANCE REMOVED AND REPLACED THE
- [SDR NSVA0110](https://openairdocs.org/sdr/NSVA0110.md): Pressure Switch · leaking · Sep 1, 2001 · N242CJ · Saab 340B · Fuel Pressure Sensor
  > PILOT REPORTED FUEL LEAKING OUT OF NR 1 ENGINE DRAIN. MAINTENANCE OPENED COWLING AS NECESSARY OBSERVE FOR LEAKS, DISCONNECTED COMPONENT DRAIN LINES AT OV FUEL FILTER AND PRESSURE DIFFERENTIAL SWITCH WHILE RUNNING BOOST PUMP. ISOLATED LEAK TO FUEL PRESSURE DI

## 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 = 'N242CJ' AND deregistration_id = 'N242CJ-2013-07-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N242CJ-2013-07-23/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.