| Airframe Status |
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| Total Time: | 8073 (April 2010) | Total Landings: | 7065 |
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| Engine Status |
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| Pratt & Whitney | PT6A-135 3600 hr TBO |
| Time since New: | 8073 | 8073 | |
| Time since O/H: | 965 | 965 | |
| Overhauls by Dallas Airmotive (1/07) |
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| Propellers |
| Hartzell 4 Blade HC-B4tN-3B |
| Left | Right |
| 965 | 965 |
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INTERIOR Six Place Seating Covered in Tan Leather with Tan Carpet and Removable Vinyl Liner. Dual Executive Tables Each with 14V DC. Forward Refreshment Center with Heated Coffee Storage. Aft Belted Potty. All Wood Work was Replaced in January 2006 and Finished in Vintage Rosewood High Gloss.
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EXTERIOR
Overall Matterhorn White with Royal blue and Aviation Grey Accent Stripes. New 4/2002
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AVIONICS
- Dual Garmin GNS-480 Nav/Comms (WAAS Enabled)
- Sperry SPI 400 Flight Director System
- Sperry SPZ-200A Autopilot Control System w/Pitch Trim
- Sandel 3500 EFIS
- MX20 MFD
- Dual Garmin GNS480 GPS
- Garmin GTX300/GTX327 Transponders
- Dual RMI and ADF
- Collins WXR-300 Radar
- Collins ALT 50A Radar Altimeter
- GDL-69A XM Radio/Weather Datalink
- L3 Skywatch SKY497 Traffic Avoidance System
- Honeywell KGP-560 Ground Proximity Warning
- Sperry C-14-43 Compass
- Shadin Digital Data Fuel Flow Sensor
- PMA 8000 Audio Panel w/Digital Record/Playback
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| 2006 - Over $100K was spent on avionics upgrades including new wiring for all avionics. Instrument panel was removed and powder coated. Active Traffic can be displayed on the Sandel, MX20 and GNS480. Complete weather displayed on MX20. XM radio is available to crew and cabin. Jeppesen Enroute, Approach and Airport Diagrams displayed on MX20.
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ADDITIONAL EQUIPMENT
- Brake De-Ice
- 4 Blade Hartzell Props with Prop Sync
- Auto-Feather
- Forward and Aft Partitions
- Concord Lead Acid Battery
- Complete Cabin Intercom System with Aux and XM Connections
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INSPECTION STATUS
- Phase 1-2 Inspection CW 3/2010 by Monarch Air, Next Due 3/2012 (8,840)
- Phase 3 Inspection Due 10/2010 (8,549)
- Phase 4 Inspection CW 11/2009, Next Due 11/2011 (8,751)
- All 6 Year Inspections CW 3/2007 by Monarch Air
- Wing Bolt Inspection CW 5/2007 by Monarch Air
- Both Nacelle Fuel Cells Re-Certified 3/2007
- New Right Wing aux and Outboard Fuel Cells 5/2007
- All New Engine Mounts and Hoses Installed at Engine Overhaul
- Current Part 135
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WEIGHTS
| Empty Weight | 7,142 lbs |
| Max Take-Off Weight | 10,950 lbs |
| Useful Load | 3,808 lbs |
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Incidents
August 2006 - Per a written report provided by Raytheon Aircraft, King Air LA-74 was involved in a landing incident at Addison Airport, Addison Texas. The main landing gear would not fully extend. The aircraft landed with the main gear partially extended. The R/H and L/H main gear folded upon landing causing damage to the R/H and L/H nacelles, R/H main gear doors, R/H and L/H outboard flaps, L/H inboard flap, R/H wing center section forward spar, aft lower fuselage, ventral fin and tailcone.
Repairs were performed per Raytheon Aircrafts recommendations. Repairs were performed by Monarch Aviation utilizing Raytheon provided drawings. The engines were overhauled by Dallas Airmotive. The propellers were overhauled by Byam Propeller.
The aircraft has flown 1,070 hours since the repairs
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