| AIRFRAME |
|
TOTAL TIME |
9,825.0 |
LANDINGS |
7,118 |
|
| ENGINES |
|
| PRATT & WHITNEY JT15D-4s |
L/H |
R/H |
| SERIAL #: |
PCE70517 |
PCE70315 |
| TSN: |
9569.8 |
8061.8 |
| CSN: |
7270 |
5109 |
| TSO: |
3208 |
8107.5 |
| DUE OH: |
292 |
2090 |
|
|
| AVIONICS |
|
| AUTOPILOT: |
HONEYWELL SPZ-500 |
| RVSM ADDU: |
DUAL IS&S ADDUs |
| FLIGHT DIRECTORS: |
HONEYWELL FZ-500 |
| COM: |
DUAL COLLINS VHF-20A |
| NAVS: |
COLLINS VIR-32 AND COLLINS VIR-30 |
| DME: |
DUAL COLLINS DME-42 |
| ADF: |
DUAL COLLINS ADF-60 |
| TPDR: |
DUAL GARMIN CTX-330 (MODE S) |
| RDR ALT: |
HONEYWELL AA-200 |
| WEATHER RADAR: |
HONEYWELL RDS-82 |
| GPS: |
GARMIN GNS-530AW W/ TAWS |
| GPS: |
GARMIN GNS-430AW |
| FMS: |
UNIVERSAL UNS-1K |
| HIGH FREQ: |
BENDIX KING KHF-950 HF |
| TCAD / TCAS: |
BFG SKYWATCH HD |
| MFD: |
GARMIN MX-20 |
| ELT: |
ARTEX 406 MHZ (INTERNAL NAV INTERFACE) |
|
|
| ADDITIONAL EQUIPMENT / STC's |
|
DUAL COLLINS RMI, KMR-675 MARKER BEACON RECEIVER, GILL LEAD ACID BATTERIES, ALUMINUM DORSAL FIN, RADOME QUICK RELEASE, MAX T/O WEIGHT INCREASE TO 14,500 LBS. |
|
| MAINTENANCE |
|
ON CESSCOM, PHASE 1 THRU 5 COMPLETE, 10,000 HR INSPECTIONS & NDT COMPLETED, ALL FORCAST MAINTENANCE FOR NEXT 200 HOURS COMPLETED, OVERHAULED BRAKES INSTALLED |
|
| SPECIAL MISSION EQUIPMENT – DUAL AIRWORTHINESS CERTS |
|
AVCON DUAL CAMERA PORT INSTALLATION WITH ACCESSORY KIT TO ALLOW QUICK CONVERSION FROM RESRICTED CATAGORY TO TRANSPORT CATEGORY, SCIENTIFIC POWER DISTRIBUTION SYSTEM, SCIENTIFIC RACKS, 110VAC & 28VDC DISTRIBUTION PANELS. |
|
| EXTERIOR |
|
OVERALL WHITE WITH BLUE ACCENT STRIPES. |
|
| SPECIFICATIONS AND/OR DESCRIPTIONS RE PROVIDED AS INTRODUCTORY INFORMTION ONLY AND DO NOT CONSTITUTE REPRESENTATIONS OR WARRANTIES OF AVMATS. ACCORDINGLY, YOU SHOULD RELY ON YOUR OWN INSPECTION OF THE AIRCRAFT. THIS AIRCRAFT IS SUBJECT TO PRIOR SALE OR WITHDRAWAL FROM THE MARKET |
| May 2011 |
