# TCDS P14NE: Hartzell Propeller Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Hartzell Propeller Inc.
- Revision: 1
- Revised: August 10, 1990
- Product: Propeller
- Certification basis: Part 35
- Data sheet PDF: https://openairdocs.org/files/sha256/f3/d3/f3d39b7c6332ca9627c870a6a03b8e39be3522421ab44904d25119676a5d5999
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B1C7AB603AB34BF4852567120049BCB4.0001
- Page: https://openairdocs.org/tcds/P14NE

## Models (1)

As the data sheet lists them.

- HC-A6A-3

## 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
P14NE
HARTZELL
HC-A6A
Revision 1
August 10, 1990
TYPE CERTIFICATE DATA SHEET NO. P14NE
Propellers of models described herein conforming with this data sheet, (which is part of Type Certificate No. P14NE) 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 Hartzell Propeller Inc.
Piqua, Ohio 45356
Type Constant speed; hydraulic (See NOTES 3 and 4)
Engine flange Special flange 5-1/8" bolt circle with twelve 9/16" bolts
Hub material Aluminum alloy
Blade material See below
Number of blades Six
Hubs eligible HC-A6A-3
Blades Maximum Approx. Max. Wt. Complete
Eligible Continuous Takeoff Diameter (For Reference Only) Blade
(See NOTE 2) HP RPM HP RPM Limits (See NOTES 3 and 7) Construction
A10460 1492 1700 1492 1700 108" 184 lb. Aramid Composite
Certification Basis Federal Aviation Regulations Part 35 effective October 14, 1980, with Amendments 1
through 5
Type Certificate No. P14NE issued February 27, 1987
Date of Application for Type Certificate October 31, 1985
Production Basis Production Certificate No. 10
NOTE 1. Hub Model Designation.
Hub model designation
HC - A 6 A - 3 A
Denotes minor change not affecting eligibility
Denotes specific design features (See NOTE 4)
A denotes Special Flange 5-1/8" bolt circle with twelve 9/16"
bolts and two 5/8" dowel holes
Number of blades
Identifies basic design
Hartzell controllable

P14NE 2
NOTE 2. Blade Model Designation.
Blade model designation
A 104 60 E K
An external de-ice element is installed
An internal de-ice element is installed
Basic model or template
Basic diameter in inches
Blade shank configuration
NOTE 3. Pitch Control. Eligible with the following governors:
Woodward Model x210xxx or x210x-xxx series
Maximum Out-Put Pressure 800 PSI
NOTE 4. (1) Feathering. The -3 model incorporates feathering and unfeathering features.
(2) Reversing. The -3 model is approved for installation as a reversing propeller with appropriate
reversing controls.
NOTE 5. Left-Hand Models.  The left-hand version of an approved model propeller is approved at the same rating and
diameter as listed for right-hand model.  (See NOTES 1 and 2.)
NOTE 6. Interchangeability:  Not applicable.
NOTE 7. Accessories.
(a) Propeller Spinner
(1) With Hartzell spinners (weight of spinner extra).
(b) Propeller Deicing.
(1) With Goodrich 77-xxx or 65-xxx or 67-xxx deicing kit when installed in accordance with
manufacturer's instructions (Goodrich Report 59-728) ( ); or Goodrich Drawing No. 7E-1633
NOTE 8. Shank Fairings.  Not applicable
NOTE 9. Special Limits.  Not applicable
NOTE 10. Special Notes.  Aircraft installation must be approved as part of the aircraft type certificate upon compliance
with the applicable aircraft airworthiness requirements.
...END...
```

## ADs (2, in force first)

- [AD 2006-24-07](https://openairdocs.org/ad/2006-24-07): Propeller blades · Hartzell Propeller BHC-C2Y, HC-A2V, HC-A3V and 52 more. Effective Jan 3, 2007
- [AD 2003-22-05](https://openairdocs.org/ad/2003-22-05): Composite blades · Hartzell Propeller HC-A6A-3. Effective Nov 13, 2003

## STCs approved under this data sheet (1)

- [STC SP00582NY](https://openairdocs.org/stc/SP00582NY): Installation of Prop-Guard Polyurethane Protective Tape on the leading edge of metal propellers.. McFarlane Aviation, Inc.

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