- Holder
- Tarver Propellers LLC
- Revision
- 17
- Revised
- September 17, 2003
- Status
- Current
- Product
- Propeller
- Certification basis
- Part 14, CAR 14
- Models
- 3
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 3
| Model | Also known as | Note |
|---|---|---|
| 220 | ||
| 220-1 | Formerly Universal, Univair, South 80, Brown, Tarver, Kent Tarver | |
| 220-H | Formerly Universal, Univair, South 80, Brown, Tarver, Kent Tarver |
Airworthiness directives · 1
ADs whose products are models on this data sheet, matched by model and maker.
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-833
Revision No. 17
TARVER
(BROWN PROPELLER)
(SOUTH 80)
(UNIVAIR)
(KOPPERS)
220
220-1
220-H
September 17, 2003
TYPE CERTIFICATE DATA SHEET NO. P-833
Propellers of models described herein conforming with this data sheet (which is a part of Type Certificate No. 833) and other
approved data on file with the Federal Aviation Administration, meets 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. 20 spline
Hub Material Steel
Blade Material Laminated birch or maple veneer with plastic covering all over, and with monel or
stainless steel tipping
No. of Blades Two
Hub Models 220, 220-1, 220-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)
O-74A 235 3000 235 3000 74” 48 lbs.
O-78 190 2550 190 2550 78” 51 lbs.
O-78A 200 2550 200 2550 78” 51 lbs.
O-82A 200 2550 200 2550 82” 54 lbs.
O-85 200 2550 205 2600 85” 55 lbs.
O-85AZ 145 2050 145 2050 85” 55 lbs.
O-86A 200 2550 200 2550 86” 55 lbs.
O-93 240 1925 260 2200 93” 59 lbs.
Certification Basis Civil Air Regulations Part 14 effective July 15, 1942.
Date of issuance of Type Certificate No. 833: December 12, 1945.
Date of application for Type Certificate unavailable.
Production Basis None
Page No. 1 2
Rev. No. 17 16
P-833 Page 2 of 2
NOTE 1. Hub Model Designation.
Basic model designation
2 2 0 - H
Pitch control (if used)
Aeromatic blade shank size
Number of blades
Engine shaft size
NOTE 2. Blade Model Designation.
Basic model designation
P O - 88 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 220 is automatic in operation and requires no controls. The Model 220-1
incorporates a manual-mechanical pitch control which provides improved performance at altitude (additional
weight 11 lbs.). The Model 220-H incorporates a manual-hydraulic pitch control which provides improved
performance at altitude (additional weight; propeller attachments 10 lbs., Regulator valve and oil lines 2 lbs.,
Control cable 2 lbs.).
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.
NOTES 7, 8 and 9. Not applicable.
.....END.....