Zenith STOL CH750 Technical specifications

Issued: 01.02.2020 Revision 0, Dat. 01.02.2020 AFM20200201
AFM
AIRPLANE FLIGHT MANUAL
ZENITH STOL CH 750
Serial number: 75-8316
Registration: HB-YRC

Zenith STOL CH 750 Airplane Flight Manual HB-YRC
Issued: 01.02.2020 Revision 0, Dat. 01.02.2020 Page 2-93
Airplane
Designer & Kit Manufacturer: ... Zenith Aircraft Company
Type: ...…………………………..... STOL CH 750
Builder: …………………………... Michel Ruf
Serial No: …………………………. 75-8316
Registration: …………………….. HB-YRC
The builder / owner is responsible for the appropriate correctness of the
content of this manual
Date of Issue: 01.02.2020
The Builder: Michel Ruf Signature:
Approval of Section 2 and Agreement of Sections 1, 6, 7 and 8 by EAS on
behalf of FOCA:
Date:
Name:
Stamp and Signature:
Partial approval (pages …) of Section 5 and agreement of sections 3, 4
by EAS on behalf of FOCA:
Date:
Name:
Stamp and Signature:
Final approval by EAS Certification:
Date:
Name:
Stamp and Signature:
This aeroplane is to be operated in compliance with information and
limitations contained herein.

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0.1 RECORD OF REVISIONS
Any revision of the present manual, except actual weight record, must be
recorded in the following table and in case of agreed sections endorsed by the
EAS.
The new or amended text in the revised pages will be indicated by a black
vertical line in the left hand margin, and the revision no. and the date will be
shown in the footer at the bottom of the page.
Rev.
No.
Affected
Section
Affected
Pages
Date
Approval
Date
Date
Inserted
Signature
0
First
Issue
First
Issue
01.02.2020

Zenith STOL CH 750 Airplane Flight Manual HB-YRC
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0.2 TABLE OF CONTENTS
GENERAL Section 1 Page 6-10
LIMITATIONS Section 2 Page 11-23
EMERCENCY PROCEDURES Section 3 Page 24-35
NORMAL PROCEDURES Section 4 Page 36-49
PERFORMANCE Section 5 Page 50-57
WEIGHT AND BALANCE / EQUIPMENT Section 6 Page 58-66
LIST
AIRCRAFT AND SYSTEMS DESCRIPTION Section 7 Page 67-85
ARCRAFT HANDLING, SERVICE & Section 8 Page 86-90
MAINTENANCE
SUPPLEMENTS Section 9 Page 90-93

Zenith STOL CH 750 Airplane Flight Manual HB-YRC
Issued: 01.02.2020 Revision 0, Dat. 01.02.2020 Page 6-93
1. GENERAL
1.1 INTRODUCTION
1.2 CERTIFICATION BASIS
1.3 WARNINGS, CAUTIONS & NOTES
1.4 DESCRIPTIVE DATA
1.5 THREE-VIEW DRAWING

Zenith STOL CH 750 Airplane Flight Manual HB-YRC
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1.1 INTRODUCTION
The aeroplane Flight Manual has been prepared to provide pilots and instructors
with information for the safe and efficient operation of this homebuilt airplane.
This manual includes the material required to be furnished to the pilot of
homebuilt airplanes. It may also contain references or supplemental data,
supplied by the equipment manufacturers.
1.2 CERTIFICATION BASIS
This type of aircraft is not certified in accordance with published Standard
Airworthiness Requirements.
It is authorized for flight in accordance with FOCA regulation MZ-275.001 in the
special category homebuilt.
1.3 WARNINGS, CAUTIONS AND NOTES
The following definitions apply to warnings, cautions and notes used in the flight
manual.
NOTE:draws the attention to any special item not directly
related to safety but which is important or unusual.
CAUTION:means that the non-observation of the
corresponding procedure leads to a minor or to a more or less
long term degradation of the flight safety.
WARNING:means that the non-observation of the
corresponding procedure leads to an immediate or important
degradation of the flight safety.

Zenith STOL CH 750 Airplane Flight Manual HB-YRC
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1.4 DESCRIPTIVE DATA
Kind of Airplane:
Side by side 2 place, bubble doors, single engine, high wing with struts, sheet
aluminum with blind and solid rivets, airplane
The landing gear is of conventional three gear design. Leas spring main gear
with independent hydraulic brakes and a steerable nose wheel.
The airplane is equipped with a 100hp Rotax 912 ULS engine turning a
ground adjustable 3-blade Warp-Drive propeller.
Specifications:
Wing Span ....................................................................................... 9.1 m
Wing Area .....................................................................................13.4 m2
Wing Chord ..................................................................................... 1.5 m
Horizontal Tail Span ........................................................................ 2.6 m
Horizontal Tail Area ........................................................................2.0 m2
Maximum Height (Rudder Tip)......................................................... 2.6 m
Length .............................................................................................. 6.7 m
Wheel Span (track) ......................................................................... 1.8 m
Maximum Take-Off Weight (MTOW): ............................................600 kg
Empty Weight..................................................................................360 kg
Useful Load………………………………………………… ................240 kg
Baggage Capacity (maximum) .........................................................18 kg
Wing Loading, Gross ............................................................... 26.8 kg/m2
Seats ........................................................................................................2
Tire Size
Main Gear...................................... 8.00 –6 in, 4 PLY, Max 20 psi
Nose Wheel .................................. 8.00 –6 in, 4 PLY, Max 20 psi

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DESCRIPTIVE DATA (CNTD)
Structural Limit Loads Clean
Positive .............................................................................+4.00 G
Negative ............................................................................-2.00 G
Structural Limit Loads Full Flaps
Positive .............................................................................+2.00 G
Negative ............................................................................-0.00 G

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1.5 THREE-VIEW DRAWING