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Builders Page for the Zenith CH750 Cruzer

Following are the latest CH750 STOL photo assembly guides. The following is published to supplement (and not replace) the drawings. If a discrepancy arises between these photo assembly guides and the Drawings, the Drawings always take precedence. These documents are presented in the Adobe Acrobat file format for online viewing and easy printing. The photos are presented in low-resolution for quicker downloads.

NOTICE: These documents contain copyrighted information and are NOT FOR DUPLICATION OR DISTRIBUTION.

 
CH750 Cruzer Updates
LinkDocumentsRevisionLast Update
701-contstruct-manualSTOL CH 701 Basic Construction Manual
18 pages – 4th edition		4th ed.12/2003
CSConstruction Standards for Zenair Light AirplanesDraft1/07
introductionIntroduction to building – 18 pages10/025/14
TAIL – Rudder – Section RA
LinkDocumentsRevisionLast Update
C75-RA-1 part A – Rudder SkeletonRudder Skeleton Assembly C75-RA-1Rev. 1.23/23/17
C75-RA-1 part B – Rudder SkinRudder Skin, Assembly, C75-RA-2Rev. 1.23/09/17
C75-RA-2 FinFin, C75-RA-2 FinRev. 2.02/21/17
Horizontal Tail – Section TA
LinkDocumentsRevisionLast Update
C75-TA-1Horizontal Tail Assembly:C75-TA-1 StabilizerRevision 1.010/1/13
C75-TA-2Horizontal Tail Assembly:C75-TA-1 ElevatorRevision 1.010/1/13
Wings – Section WA
LinkDocumentsRevisionLast Update
C75-WA-1Wing Skeleton AssemblyRevision 1.17/24/20
C75-WA-2Wing Skins AssemblyRevision 1.19/28/16
Flaperons – Section AA
LinkDocumentsRevisionLast Update/b>
C75-AA-1-flaperonFlaperon Assembly: 75-AA-1 5/25/16
Fuselage – Section FA
LinkDocumentsRevisionLast Update
C75-FA-1Rear Fuselage Assembly:C75-FA-1 FuselageRevision 1.02/1/14
C75-FA-2Top Fuselage Skin & Rear Fuselage Assembly:C75-FA-2 FuselageRevision 1.02/25/14
C75-FA-3Fuselage Assembly – Baggage CompartmentRevision 1.06/13/14
C75-FA-4Forward Fuselage AssemblyRevision 1.06/13/14
C75-FA-5Firewall AssemblyRevision 1.012/03/14
C75-FA-6&7Joining the Rear and Forward Fuselage AssembliesRevision 1.012/21/15
Controls – Section C
LinkDocumentsRevisionLast Update
C75-CA-1Flaperon ControlsRevision 1.112/15/15
C75-CA-2Elevator ControlsRevision 1.0112/21/15
C75-CA-3Rudder ControlsRevision 1.012/21/15
C75-CA-3 rudder cables routingRudder Cables Routing – photos 5/16
Landing Gear – Section L
LinkDocumentsRevisionLast Update
C75-LA-1Nose Gear InstallationRevision 1.012/21/15
C75-LA-2Main Gear InstallationRevision 1.19/8/16
DRAWING: Section ZA
LinkDocumentsRevisionLast Update
C75-ZA-1Horizontal Tail MountingRevision 1.05/14
C75-ZA-2Vertical Tail MountingRevision 1.05/14
C75-ZA-3Rudder Cable Fairing and Elevator Cable PulleysRevision 1.05/14
C75-ZA-4Wing InstallationRevision 1.05/14
C75-ZA-6Control Deflections and StopsRevision 1.05/14
Finishing
LinkDocumentsRevisionLast Update
W&BCH 750 Cruzer Weight & Balance Report12/152/4/16
c75-finishing1-door-sillCabin Doors – Door SillRevision 1.09/16
c75-finishing2-door-frameDoor FramesRevision 1.09/16
c75-finishing3-bubbleCabin Doors – Door bubble windowRevision 1.09/16
c75-finishing4-latchesCabin Doors – LatchesRevision 1.09/16
UL Power UL350i / UL350iS Engine Installation
LinkDocumentsRevisionLast Update
Section 1Section 1 – Engine Mount InstallationRevision 1.05/29/12
Section 2Section 2 – Oil Cooler InstallationRevision 1.016/11/12
Section 3Section 3 – Baffling, Ignition, & Voltage RegulatorRevision 1.06/6/12
Section 4Section 4 – Fuel SystemRevision 1.06/18/12
Section 5Section 5 – ECU, EGT, OIL Pressure, OIL TemperatureRevision 1.08/8/12
Section 6Section 6 – Top & Bottom CowlRevision 1.08/17/12
Section 7Section 7 – Battery & Air Oil Separator InstallationRevision 1.010/5/12

This web site is published strictly for informational purposes. It is maintained to provide a forum for exchanging information about Zenair designs. Any pictures, diagrams, drawings or graphs, are used for general identification only, and are not to be taken to represent technical drawings or replicas of exact parts. You should not consider the educational material in the web site to be the practice of general aviation.

This site is not intended to replace, substitute for or supersede any technical information contained in the drawings, any Federal Aviation Administration regulations, or the manufacturer’s manuals.

Neither Zenith Aircraft Company (ZAC) nor the authors guarantee the accuracy or completeness of any information published herein and neither ZAC or any other authors shall be responsible for any errors, omissions, or damages arising out of use of this information. This site is offered with the understanding that ZAC and any other authors are supplying information but are not attempting to render engineering or other professional services. If such services are required, the assistance of an appropriate professional should be sought.

These statements are to be considered disclaimers of responsibility from anything published here.