1990 DORNIER 228 212

1990

DORNIER

228-212

Used

DORNIER 228-212 EASA COMPLIANT

16477.0

Total Time: 16,477 Hours/30,647 landings

ENGINES AND STATUS: Engine type Garrett TPE 331-10GT-511D L/H R/H Time since new 4408 3840 Time since overhaul 428 3840 Cycles since new 4997 8270 Cycles since overhaul 916 8270 Time Since Hot Section 0 431 Note: Engines have 7000 hour TBO

490

SMOH

0

3900

SMOH

Propeller S/n CDA4424 CDA4255 Time since overhaul 696 696

VHF com Bendix/King KY 196A Dual VHF nav including GS Bendix/King KN 53 Dual Transponder Bendix/King KT76A Dual ADF Bendix/King KR87 Dual Weather Radar Bendix/King RDS 82VP DME Bendix/King KDM-706 Radio alt Bendix/King KRA 405 RMI Bendix/King KNI-582 Dual HSI Bendix/King KPI-552 Dual Audio Control System BeckerAS3100-1 Autopilot/Flight Director Bendix/King KFC-250 Flight Data recorder Sundstrand 17M700-274 Cockpit Voice Recorder Sundstrand 980-6005-76 ELT Arte ELT C 406-2 GPS Garmin GPS 400 GPS Alli KLN 900 TCAS ll Honeywell EGPWS

Air Conditioning System Carbon Brakes Anti-Skid Brakes Dual 43 amp hour batteries Anti-Gravel protection De-ice, complete Auto Pilot GPS

2005

8/10

19

Commuter, 19 passenger seats 2 crew seats, double stretcher option

WEIGHT DATA: Maximum Take Off Weight 6,400 kg 14,109 lbs Maximum Landing Weight 6,100 kg 13,448 lbs Maximum Zero Fuel Weight 5,940 kg 13,095 lbs Empty Operating Weight 3,960 kg 8,730 lbs Fuel Capacity 2,441 kg 4,251 lbs Payload 1,796 kg 3,952 lbs

Utilizing the manufacturer’s recommend program in Chapter 5 of the maintenance manual for time limits and maintenance checks. Aircraft will be delivered with a fresh Export Certificate of Airworthiness.