# TCDS P-877: Textron Aviation Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Textron Aviation Inc.
- Revision: 10
- Revised: October 12, 2016
- Product: Propeller
- Data sheet PDF: https://openairdocs.org/files/sha256/b9/5c/b95c0a1f2e81a19c3be209b3af52728d1c3ecdc8998b8a2df7e7cabaa76a0c9a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9089E9C5F24CD017862580FE00587647.0001
- Page: https://openairdocs.org/tcds/P-877

## Models (1)

As the data sheet lists them.

- 214

## 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. 8 6 
 
DEPARTMENT OF TRANSPORATION 
FEDERAL AVIATION ADMINISTRATION 
 
 
P-877  
Revision 10  
 Textron Aviation   
 214  
October 12, 2016  
 
TYPE CERTIFICATE DATA SHEET NO. P-877 
 
Propellers of models described herein conforming with this specification 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 a nd 
applicable portions of the Civil Air Regulations provided they are installed, operated,  and maintained as prescribed by the 
manufacturer. 
 
Type Certificate Holder Textron Aviation Inc. 
 One Cessna Boulevard 
 Wichita, KS  67215 
 
Type Certificate Holder Record Beech Aircraft Company transferred to 
 Raytheon Aircraft Company on April 15, 1996 
 
 Raytheon Aircraft Company transferred to 
 Hawker Beechcraft Corporation on March 26, 2007 
 
 Hawker Beechcraft Corporation transferred to 
 Beechcraft Corporation on April 12, 2013 
 
 Beechcraft Corporation transferred to  
 Textron Aviation Inc. on October 12, 2016 
 
Type Constant speed; hydro-mechanical  (see NOTES 3 and 4) 
 
Engine shaft SAE # 20 spline shaft 
 
Hub material Steel 
 
Blade material See below 
 
Number of blades 2 
 
Hub model eligible 214-100 series (see NOTE 1) 
 
 
 
Blades 
Eligible 
 
Maximum 
Continuous 
 
 
Takeoff 
 
 
Diameter 
Approx. Max. 
Wt. Complete 
(for reference only) 
 
 
Blade 
(See Note 2) HP RPM HP RPM Limits (See Notes 3,4, & 7) Construction 
214-211-96 to 240 1925 260 2180 96" - 93" 78 lbs. Laminated birch veneer; 
214-211-93       cellulose nitrate covering; 
brass, Everdure, or 
stainless steel tipping. 
        
272-234-101 to 325 2000 375 2180 101" - 88" 95 lbs. Aluminum alloy 
272-234-88

P-877 2 Rev. 10 
 
Certification Basis Type Certificate No. 877 
 
Production Basis Production Certificate No. 501 
 
 
NOTE 1. Hub Model Designation 
Basic model
Minor change not affecting eligibility
Basic drawing identity
214 - 1 05
 
 
 
NOTE 2. Blade Model Designation 
Basic blade model
Minor change (when used) not affecting eligibility
Propeller diameter in inches
214 - 211 96 1
Basic blade design
- -
 
 
NOTE 3. Pitch Control.  Eligible only with Beech control unit 214-200 and Beech governor B200-250.  Additional  
 weight of governor 3-1/2 lbs.  (Weight of transmission is included in approximate weight of propeller  
 listed above. 
 
NOTE 4. Feathering.   Eligible only with Beech full feathering control. 
 
NOTE 5. Left-Hand Models.  Not applicable. 
 
NOTE 6. None 
 
NOTE 7. Accessories.   
 (a) Propeller Deicing 
  (1) Eligible with Beech fluid deicer slinger ring included in Item (b)(1). 
  (2) Eligible with Beech no. 279-404 (Goodrich No. 37572) propeller deicer fluid feed 
   strips when installed in accordance with instructions issued by Beech. 
 (b) Propeller Spinner 
  Eligible with: 
  (1) Beech spinner 272-102 (additional weight 6 lbs.) (For aluminum blades only) 
  (2) Beech spinner 268-203 (additional weight 7 lbs.) 
  (3) Beech spinner 50-960010 (additional weight 7 lbs.) (For wood blades only) 
 
 
 
....END....
```

## ADs (1, in force first)

- [AD 76-10-12](https://openairdocs.org/ad/76-10-12): Textron 214, B200 (propeller), R201 and 2 more. Effective Jun 2, 1976

## STCs approved under this data sheet (1)

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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.