1995 DORNIER 328-100

Avionics

i. Honeywell Primus 2000 post Enhanced General Avionics Upgrade, refer to SB328-31-256
ii. Dual Primus II Integrated Radio System
iii. Dual Integrated Avionics Computers
iv. Flight Management System
v. Auto Pilot System
vi. Mode-S Transponders
vii. Dual Mode-S Transponder (3053 only)
viii. 8.33kHz spacing (3053 only)
ix. AHRS-AH800 installed
x. EGPWS installed refer to SB-328-34-465 (single Display Unit)
xi. TCAS II Change 7.1 installed (PN 4066010-914)
xii. FDR 57 Parameters installed (SB-328-31-354)
xiii. CVR installed
xiv. ELT ARTEX 406 installed
xv. HF-950 System installed

Engines

i. Pratt & Whitney Canada PW119C installed Left and Right
ii. Maintenance ‘on-condition’ & ECTM program

Propeller
i. Hartzell 6 Blade Dual Acting Constant Speed Propeller HD-E3C-3B/E13890()K installed Left and Right
ii. TBO 6,000 FH, Thrust Bearing change all 2,000 FH

Auxiliary Power Unit
i. Allied Signal Engines (Garrett APU Div.) GTCP-36-150[DD] installed

Interior / Exterior

i. Standard Galley (AFT Right) fitted
ii. Standard Lavatory (AFT Right) fitted
iii. Standard Overhead Storage Compartments
iv. Current LOPA 7 Seat as shown under Paragraph 4

Additional Information

AERORESCUE FLEET

1. MSN: 3051 Tail: VH-PPQ Manufactured: Aug 1995
2. MSN: 3052 Tail: VH-PPV Manufactured: Aug 1995
3. MSN: 3053 Tail: VH-PPG Manufactured: Mar 1996
4. MSN: 3057 Tail: VH-PPF Manufactured: Oct 1995
5. MSN: 3059 Tail: VH-PPJ Manufactured: Nov 1995