# TCDS P-820: Tarver Propellers LLC

- Type: Type certificate data sheet
- Status: Current
- Holder: Tarver Propellers LLC
- Revision: 17
- Revised: September 17, 2003
- Product: Propeller
- Certification basis: Part 14, CAR 14
- Data sheet PDF: https://openairdocs.org/files/sha256/e2/e0/e2e0db63daa6e8c041aed99fc996cf40c2dd4bbd173e109982b948447986a07e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2DEC4CB525F48E7C86256E12006B1C10.0001
- Page: https://openairdocs.org/tcds/P-820

## Models (2)

As the data sheet lists them.

- F200
- F200-H

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
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......
```

## ADs (3, in force first)

- [AD 73-20-08](https://openairdocs.org/ad/73-20-08): Tipping · Tarver Propellers 220, F200 and F200-H. Effective Oct 4, 1973
- [AD 47-50-13](https://openairdocs.org/ad/47-50-13): Hub · Tarver Propellers F200
- [AD 50-34-01](https://openairdocs.org/ad/50-34-01): Retaining Flanges · Tarver Propellers F200

## STCs approved under this data sheet (1)

- [STC SP01222WI](https://openairdocs.org/stc/SP01222WI): Installation of Aircraft Development propeller vortelators.. Aircraft Development Co

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