# TCDS P-896: Hartzell Propeller Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Hartzell Propeller Inc.
- Revision: 1
- Revised: October 12, 1956
- Product: Propeller
- Data sheet PDF: https://openairdocs.org/files/sha256/41/43/41435a87dac6bc38d379e703ea587315c2d7ef8bf0f5042a67966916b0169e43
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7A27E6C2DFF8D4F28525671200487018.0001
- Page: https://openairdocs.org/tcds/P-896

## Models (1)

As the data sheet lists them.

- HC-102YF-1

## What the data sheet says

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

```text
Page No. 1 2
Rev. No. 1 1
DEPARTMENT OF  TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
P-896
Revision 1
HARTZELL
HC-102Y
October 12, 1956
PROPELLER SPECIFICATION
Propellers of models described herein conforming with these specifications and approved data on file with the Civil Aeronautics
Administration are rated as airworthy for use in certificated aircraft in accordance with pertinent aircraft specifications and
applicable portions of the Civil Air Regulations, provided they are installed, operated, and maintained as prescribed by the
manufacturer.
Type Certificate Holder Hartzell  Propeller, Inc.
Piqua, Ohio
Type Constant speed; hydraulic  (see Note 3)
Engine shaft Special flange  4" B.C.
Hub material Aluminum alloy
Blade material Aluminum alloy
Number of blades Two
Hubs eligible HC-102YF-1   (See Note 1.)
Blades
Eligible
Maximum
Continuous Takeoff Diameter
Approx. Max. Wt. Complete
(for reference only)
(See Note 2) HP RPM HP RPM   Limits (See Note 3)
8848-0
to
8848-8
240 2600 240 2600 88"  -  80"
(-0 to -8)
60 lbs.
Certification basis Type Certificate No. 896
Production basis Production Certificate No. 10 issued to:
Hartzell Industries, Inc.
Piqua, Ohio
NOTE 1. Hub Model Designation
Hub model designation
HC - 10 2 Y F - 1 A
Denotes minor change not affecting eligibility
L denotes left hand rotation
Denotes specific design features  (see Note 4)
F denotes special flange, 4" BC
Hartzell blade shank size
Number of blades
Identifies basic design
Hartzell controllable
NOTE 2. Blade model designation

P-896 2
Blade model designation
L 88 48 - 3
Number of inches cut off from basic diameter
Basic model or template
Basic diameter in inches
Denotes left hand blade
NOTE 3. Pitch Control.  Eligible with the Hartzell constant speed control, which includes the Woodward X210XXX
series governor models.  Additional weight 4.5 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 as listed for the right-hand model.  See Notes 1 and 2.
NOTES 6, 7, 8, and 9.  Not applicable.
....END....
```

## ADs (5, in force first)

- [AD 2007-26-09](https://openairdocs.org/ad/2007-26-09): Initial blade inspections · Hartzell Propeller BHC-C2Y, BHC-G2YF-1, BHC-I2YF-1 and 67 more. Effective Jan 30, 2008
- [AD 2005-14-11](https://openairdocs.org/ad/2005-14-11): Failed propeller blade · Hartzell Propeller BHC-92W, BHC-92ZF-1, BHC-92ZF-3 and 391 more. Effective Aug 17, 2005
- [AD 2001-23-08](https://openairdocs.org/ad/2001-23-08): Propeller Hubs · Hartzell Propeller BHC-C2Y, BHC-G2YF-1, BHC-I2YF-1 and 23 more. Effective Dec 24, 2001
- [AD 2006-18-15](https://openairdocs.org/ad/2006-18-15) (historical): Front cylinder half of the propeller hub · Hartzell Propeller BHC-C2Y, BHC-G2YF-1, BHC-I2YF-1 and 24 more. Effective Sep 25, 2006
- [AD 77-12-06](https://openairdocs.org/ad/77-12-06) (historical): Blade Shank · Hartzell Propeller BHC-12YF-4, BHC-C2Y, BHC-G2YF-1 and 115 more. Effective Dec 21, 1977

## 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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