- Holder
- Tarver Propellers LLC
- Revision
- 17
- Revised
- September 17, 2003
- Status
- Current
- Product
- Propeller
- Certification basis
- Part 14, CAR 14
- Models
- 2
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 2
| Model | Also known as | Note |
|---|---|---|
| F200 | Formerly Universal, Univair, South 80, Brown, Tarver, Kent Tarver | |
| F200-H | Formerly Universal, Univair, South 80, Brown, Tarver, Kent Tarver |
Airworthiness directives · 3
ADs whose products are models on this data sheet, matched by model and maker.
STCs approved under this data sheet · 1
What the data sheet says
From the PDF’s text layer, line by line: tables lose their columns. The PDF is the record.
DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
P-820
Revision No. 17
TARVER
(BROW N PROPELLER)
(SOUTH 80)
(UNIVAIR)
(KOPPE RS)
F200
F200-H
September 17, 2003
TYPE CERTIFICATE DATA SHEET NO. P-820
Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. 820) and other
approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in
accordance with pertinent aircraft data sheets and applicable portions of the Federal Aviation Regulations provided they are
installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other approved instructions.
Type Certificate Holder Tarver Propellers, LLC
1500 Rio Vista Drive, Hangar C4
Fallon, Nevada 89406
Type Automatic; mechanical (See NOTE 3)
Engine Shaft SAE No. 1, No. 2, No. 3 flanges; special flanges
Hub Material Steel
Blade Material Laminated birch or maple veneer with varnish or plastic covering all over, and with
monel or stainless steel tipping. (See NOTE 2)
No. of Blades Two
Hub Models F200, F200-H (See NOTES 1 and 3)
Blades
Eligible
Maximum
Continuous
Takeoff
Diameter
Approx. Maximum
Weight Complete
(For reference only)
(See Note 2) HP RPM HP RPM Limits (See Note 3)
OO-72B 65 2550 65 2550 72” 31 lbs.
OO-72C 150 2600 150 2800 72” 31 lbs.
OO-72D 150 2600 150 2800 72” 31 lbs.
OO-72E 150 2600 150 2800 72” 31 lbs.
OO-72F 150 2600 150 2800 72” 31 lbs.
OO-73D 150 2600 150 2800 73” 31 lbs.
OO-73E 150 2700 150 2800 73” 31 lbs.
OO-73F 150 2600 150 2800 73” 31 lbs.
OO-74A 150 2600 150 2800 74” 31 lbs.
OO-74B 165 2800 165 2800 74” 31 lbs.
OO-74C 165 2800 165 2800 74” 31 lbs.
OO-74E 180 2800 180 2800 74” 33 lbs.
OO-76B 165 2800 165 2800 76” 33 lbs.
OO-78B 150 2600 150 2800 78” 33 lbs.
Certification Basis Civil Air Regulations Part 14 effective July 15, 1942.
Page No. 1 2
Rev. No. 17 15
Page 2 of 2 P-820
Date of issuance of Type Certificate No. 804: May 16, 1945.
Date of application for Type Certificate unavailable.
Production Basis None
NOTE 1. Hub Model Designation.
Basic model designation
F 2 00 - H
Pitch control (if used)
Aeromatic blade shank size
Number of blades
Flange mountings
NOTE 2. Blade Model Designation.
Basic model designation
P OO - 78 A L
Left hand version
New design version differing from basic model physically and/or
aerodynamically
Propeller diameter in inches
Aeromatic blade shank size
If used, denotes the plastic covering.
NOTE 3. Pitch Control. The model F200 is automatic in operation, and requires no
controls. The Model F200-H incorporates a manual-hydraulic
pitch control which provides improved performance at altitude.
(Weight - Hydraulic cylinder - 1-3/4 lbs. Control valve,
transfer block, control cable and oil lines - 6 lbs.
approximately - dependent on installation.)
NOTE 4. Not applicable.
NOTE 5. Left Hand Models. The left hand version of an approved model propeller is eligible at the same rating and
diameter limitations as listed for the right hand model.
NOTE 6. Interchangeable Blades. Blades must be used only in pairs which have been matched in accordance with the
manufacturer's instructions.
Plastic covered blades with a "P" in the model designation are interchangeable with plastic covered blades
without a "P" in the model designation.
NOTES 7, 8 and 9. Not applicable.
.....END......