CR-MM-1-0-00
PS-28 Cruiser
PS-28N Cruiser
CHAPTER 1 – GENERAL
Date of issue: 2021-01-15
Revision No.: 25
1 - 5
1.2.2 Main Technical Data
Wing
•
Span………………………………………………….. ... 8.600 m
(28.21 ft)
•
Area ........................................................................... 12.3 m
2
(132.30 sq.ft)
•
MAC .......................................................................... 1,500 mm
(59.10 in)
•
Wing loading ............................................................. 49 kg/m
2
(10.00 lb/sq.ft)
•
Aileron area ............................................................... 0.40 m
2
(4.31 sq.ft)
•
Flap area ................................................................... 0.65 m
2
(7.00 sq.ft)
Fuselage
•
Length ………..…………………………………….…..6.680 m
(21.91 ft)
•
Width ......................................................................... 1.280 m
(50.40 in)
•
Height………………………………………………… ... 2.340 m
(7.67 ft)
•
Cockpit width ............................................................. 1.170 m
(46.00 in)
Horizontal tail unit
•
Span .......................................................................... 2.930 m
(9.61 ft)
•
HTU area ................................................................... 2.2 m
2
(23.70 sq.ft)
•
Elevator area ............................................................. 0.8 m
2
(8.60 sq.ft)
Vertical tail unit
•
Height ........................................................................ 1.07 m
(3.51 ft)
•
VTU area ................................................................... 1 m
2
(10.70 sq.ft)
•
Rudder area .............................................................. 0.4 m
2
(4.30 sq.ft)
Landing gear
•
Wheel track ............................................................... 1.520 m
(4.98 ft)
•
Wheel base ............................................................... 2.030 m
(6.66 ft)
•
Nose landing gear wheel diameter ........................... 343 mm
(13.50 in)
•
Main landing gear wheel diameter ............................ 343 mm
(13.50 in)