What it approves
Installation of McCauley model 4HFR34C764/94LMB-0 propellers.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
FAA FORM 8110-2(10-68) PAGE 1 of 3 PAGES Number SA1385GL This certificate issued to McCauley Propeller Systems 7751 East Pawnee Wichita, KS 67207
Part 3 of the Civil Air Regulations.
See Type Certificate Data Sheet A9EA for complete certification basis.
Original Product-Type Certificate Number : A9EA Make : Viking Air Limited (DeHavilland Aircraft) Model : DHC-6-300
Installation of McCauley Propeller Systems propeller model 4HFR34C764/94LMB-0 in accordance with McCauley Technical Report No. 707, no revision, dated March 8, 1989 and McCauley Drawing No. D-60040, Change Number 7204, dated March 10, 1989, or later FAA approved revision.
1. Compatibility of this design change with previously approved modifications must be determined by the installer.
2. FAA Approved Airplane Flight Manual Supplement dated May 17, 1989, or later FAA approved revision, is required.
…continued on page 3 of 3…
This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.
Date reissued : July 19, 2006
( Signature) Thaddeus D. Krolicki, Jr.
Manager, Propulsion Branch Chicago Aircraft Certification Office
(Title) Date of application: September 24, 1988
Date of issuance : May 17, 1989
3. Aircraft specifications are the same as listed on Aircraft Specification Data Sheet No. A9EA
Propeller and Propeller Limits
2 McCauley 4HFR34C764 hubs with 94LMB-0 blades
Diameter: 94 to 92 inches
Propeller blade angle at 30 inches:
Feathered: +86.8° ± 0.3° Takeoff Low Pitch: +17.5° (22.0° pickup) Idle Blade Angle: +11.5° Reverse Blade Angle: -10.0° ± 0.4°
Tolerances for takeoff Low Pitch and Idle Blade Angle are contained in McCauley Technical Report 707.
Minimum propeller ground idle RPM for continuous operation shall not be less than 1034 RPM.(47% Np); however, propeller may be feathered on the ground and idled at rotational speeds below 400 propeller shaft RPM (18% Np)
4. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Bombardier-Rotax GmbH | DHC-6-300 | A9EA |