Aircraft Description
Seating for 8 Passengers
ADS-B Out / TCAS II Version 7.1 Installed
Belted Lavatory
Increased Maximum Take-Off Weight to 16,300 pounds
Incorporated IFA (Increase Flight Activity)
Inspection Program
IFA-D Inspection Performed 7/2024
AIRFRAME / TOTAL LANDINGS / ENGINES / APU / WEIGHT
AIRFRAME
Total Hours Since New 6 589:09 (As of October 01, 2024)
Total Cycles Since New 5 094 (As of October 01, 2024)
Certification Date April 2001
Current location Prague (Czech Republic)
ENGINES
Left Right
Description Pratt & Whitney JT15D-5 Pratt & Whitney JT15D-5
Serial number PCE-100182 PCE-100361
Total Hours Since New 8 779:44 10 425:07
(As of October 01, 2024)
Total Hours Since Overhaul 561:114 854:25
Cycles Since New 7 652 8 735
(As of October 01, 2024)
WEIGHTS
Maximum Take Off Weight 16 300 lb
Maximum Landing Weight 15 700 lb
Basic Empty Weight (As of July 11, 2024) 10 720 lb
Maximum Zero Fuel Weight 13 000 lb
Maximum Usable Fuel 733 gal
Incorporated IFA (Increase Flight Activity) Inspection Program
Inspection Type Last performed Next Due
A 6 421:01 6 821:01
B 6 421:01 7 221:01
C 6 421:01 8 021:01
D 6 421:01 9 621:01
Type of Unit Description
EFIS (Electronic Flight Instrument System) Collins Pro Line 4 (4-Tube)
RTU (Radio Tuning Unit) Dual RTU-870C
VHF Communication Radios Dual VHF-422C
ADC (Air Data Computer) Dual ADC-850D
AHC (Attitude Heading Computer) Dual AHC-85E
Radar Receiver/Transmitter Single Rockwell Collins RTA-854
ADF (Automatic Direction Finder) Single ADF-462
EGPWS (Enhanced Ground Proximity Warning System) Allied Signal Mark V
FMS (Flight Management System) Dual Collins AMS 5000
Navigation Radios Dual VIR-432
TCAS (Traffic Collision Avoidance System) Single TTR-921 TCAS II with 7.1
Compensation Unit Dual ICU-85
CVR (Cockpit Voice Recorder) L3 FA2100
Transponder with Enhanced Surveillance Dual TDR-94D Mode S
RA (Radio Altimeter) Single Rockwell Collins ALT-55B
DME (Distance Measuring Equipment) Dual DME-442
GPS sensor (Global Positioning System) Single Rockwell Collins GPS-4000S
FDR (Flight Data Recorder) Single Fairchild F1000
DAU (Data Acquisition Unit) Collins Aerospace DAU-650
ELT (Emergency Location Transmitter) Artex C406-1
ADS-B Out Installed under SB-34-4154
Number of passengers 8 Passenger configuration
Cabin configuration Centre four-place club seating arrangement, two forward facing aft seats, aft facing forward seat by the door and belted lavatory
Cabin equipment Airshow in flight information system with a single display in the forward bulkhead, three pull-out tables,
two 12 volt DC outlets
Notes Extended galley storage area, cockpit and cabin separated by sliding hard pocket door
Base paint color(s) Overall Matterhorn white
Stripe color(s) Black stripes
