Engineering Warbirds – Hamilton Standard Dome Seals – 52478

 

Manufacturer Hamilton Standard Propeller Co.
Aircraft Numerous (See List Below)

Propeller Models  23E, 24D, 33E Hamilton Standard Hydromatic Propellers
Part Number 52478, 52478-1
Proper Description SEAL – DOME & BARREL
AirCorps Aviation PMA Part Number 52478-ACP, 52478-1-ACP
NOW PMA APPROVED BY AIRCORPS AVIATION / AIRCORPS DEPOT

OVERVIEW / EXECUTIVE SUMMARY

No pilot or mechanic wants hydraulic fluid being slung by the propeller onto the engine or cowlings, or worse yet compromising visibility by coating windscreens. Propellers are becoming rarer and more costly, it isn’t uncommon to now see warbird props that are six figures. Proper maintenance and upkeep amid dwindling and aging parts supplies present long term challenges for our industry. Notably rubber parts produced 70-80 years ago have become rigid and embrittled; these common wear items and consumables are used extensively on props and accessories. AirCorps Aviation in Bemidji MN has found a niche in producing rubber parts, notably seals and dynafocal engine mounts for a variety of warbirds including the P-51, B-25, B-17, P-47, P-38, Wildcat, TBM, and more. The recent PMA of the 52478 and 52478-1 dome seal for 23E, 24D, and 33E series Hamilton Standard Hydromatic propellers represents the first propeller part under the FAA-PMA quality system at AirCorps Aviation. Read on to learn why we produced this seal and how this seal, produced with the original Hamilton Standard drawing, meets the dimensional specs required at installation …

BACKGROUND & LOCATION

Hamilton Standard Dome and Barrel Seal, or simply: Dome Seal, can be found on most WWII era Hamilton Standard propeller & hub assemblies. The oil seal between the barrel assembly and the dome assembly is formed by a compression type dome-barrel seal which seats between the inner diameter of the outboard barrel half (just inboard of the dome retaining nut). This trapezoidal shaped circular seal is stretched around the bottom of the fixed cam and installed between the Dome assembly and barrel assembly. This seal is available in two sizes, standard size and .025 oversized, and is responsible for retaining hydraulic fluid (in this case engine oil) inside of the propeller hub assembly.

OEM DESIGN

Hamilton Standard Propeller Co. designed the 52478 – Seal – Dome & Barrel on May 28, 1937.  The drawing was altered / revised a number of times into 1947.

Critical to the design and function of the AirCorps FAA-PMA seal is that the height and width dimensions must be inspected when installed and stretched over a mandrel.

STOCK VS. OVERSIZED SEAL

When the propeller dome is installed on the hub assembly, the preload between the cam gear in the dome and the blade gears on the propellers is controlled by the distance from the bottom face of the dome to its mating surface on the hub. Maintainers can adjust this height, and therefore adjust preload, to account for wear by using thin donut shaped shims to space the dome from the hub assembly.

The P-51 maintenance manual AN 01-60JE-2 page 181 provides guidance on how to do this as do other aircraft and Hamilton Standard maintenance manuals. The notes under figure 227 of AN 01-60JE-2 give reference to usage of the 52478-1 oversized dome seal.

The oversized seal (52478-1) is used when the total width of preload shims under the dome assembly exceeds .025″.

Hamilton Standard Propellers were furnished with both the stock 52478 & 52478-1 dome barrel seals. AirCorps recommends operators, and maintainers stock both seals.

This pair of seals can be purchased here. (52478-SET)

INSPECTION

This critical seal on the propeller requires inspection for cracks, pliability, and attention to prevent failure and leakage.

Some key questions in determining if your propeller seals needs to be inspected / tested / replaced / repaired:

    • – Is the status of seal unknown?
    • – Has the propeller been inspected, overhauled, or disassembled to perform ADs?
    • – Has the propeller been leaking fluid?

AirCorps recommends these additional inspections / actions.

  1. Propeller should be visually checked during pre-flight to verify there are no visible failures. Know your aircraft so any change will draw your attention.
  2. Check and note dome seal type being used stock size or oversized the next time the dome is removed. Consider replacing the seal proactively to set a baseline.
  3. Inspect dome seal for cracks, embrittlement, or rigidity. The seal should be pliable and the durometer of the rubber should be roughly 70. For reference, a typical eraser on a pencil is usually about 60 durometer. 
  4. Thoroughly inspect during each annual inspection
  5. As reference, the Aircraft Inspection & Maintenance Guide – P-51, 00-20A-2-P-51, 7-Nov-1947 outlines an inspection for propeller oil leakage at 25, 50, 100 hour inspections.

 

PROP DOME SEAL FAILURES

CRACKING / EMBRITTLEMENT

Visual of cracked 52478 Seal

New surplus and replacement seals are now typically over 70 years old and have a propensity to harden and be undersized when installed.

How to inspect – Visual Inspection
Tolerance of damage or wear : Zero
Solutions offered: Replacement of Seal

DESIGN DIFFERENCES & ADVANTAGES

The AirCorps Aviation FAA-PMA dome seal was designed to be identical to the original dome seals as no deficiencies in the OEM design have been noted. With that said, reverse engineering a component from a 1940’s era drawing can bring out its own challenges.

    • – Material Specification – Like almost all other WWII era manufacturers, Hamilton Standard produced a long list of internal specifications to control materials, finishes, and processes. The OEM drawings lists the internal Hamilton Standard Propellers Spec for Synthetic Rubber, which details physical properties and general requirements, but does not contain specific rubber blend information. As with many of these proprietary 1940s specifications, obsolete reference specifications and measurements are used. AirCorps was tasked with finding a material that met the requirements of the HSP.
    • – Geometry – As shown in the illustrations above, the dome seal is stretched to fit on the fixed cam. Just like a rubber band being pulled, the cross sectional width decreases as the material is stretched. The rate at which the cross sectional width shrinks as the ID expands is a result of the shape and cross sectional area of the seal. AirCorps engineering calculated, experimented, and measured multiple seals to ensure our seal consistently measures equal or within a few thousandths of an inch of originals.

APPLICABILITY AND USAGE

Where Used – Hydromatic Hamilton Standard Propeller Models: 23E50, 24D50, 33E60

Hamilton Standard 23E50 Propellers: 

23E50-107, 23E50-109, 23E50-119, 23E50-137, 23E50-155, 23E50-163, 23E50-179, 23E50-181, 23E50-189, 23E50-231, 23E50-233, 23E50-241, 23E50-247, 23E50-285, 23E50-287, 23E50-301, 23E50-311, 23E50-315, 23E50-321, 23E50-327, 23E50-389, 23E50-391, 23E50-393, 23E50-399, 23E50-455, 23E50-471, 23E50-473, 23E50-473, 23E50-489, 23E50-491, 23E50-495, 23E50-505, 23E50-543, 23E50-591, 23E50-797

Hamilton Standard 24D50 Propellers:

24D50-65, 24D50-71, 24D50-87

Hamilton Standard 33E60 Propellers:

33E60-13, 33E60-15, 33E60-31, 33E60-33, 33E60-35, 33E60-79, 33E60-85

Hamilton Standard Dome Assemblies:

59627, 59626, 54053, 55011, 55316, 54776, 55290, 57990, 55288, 59468, 59632, 61144, 59648

52478 & 52478-1 PROP DOME SEALS ARE COMMONLY INSTALLED ON THESE AIRCRAFT

AIRCRAFT PROPELLER MODEL BLADE NUMBER
P-51 MUSTANG 24D50 6523 & 6547
B-17 FLYING FORTRESS 23E50 6477
B-24 LIBERATOR 23E50 6477
B-25 MITCHELL 23E50 6477 & 6359
C-47 SKYTRAIN 23E50 6477
C-53 SKYTROOPER 23E50 6477
DOUGLAS DC-3 23E50 6477
C-54 SKYMASTER 23E50 6507
PBY CATALINA 23E50 6353
F4U, AU-1, FG-1D CORSAIR 23E50 6525
F6F HELLCAT 23E50 6541
TBM AVENGER 23E50 6359
LOCKHEED VENTURA 23E50 6477
SBD DAUNTLESS 23E50 6511
A-20 HAVOC / BOSTON 23E50 6353
A-26 INVADER 23E50 6359
C-82 PACKET 33E60 6491
C-69 CONSTELLATION 33E60 6491

 

WHEN PURCHASING

AirCorps Aviation has PMA approval for 52478-ACP and 52478-1-ACP  Seal – Dome and Barrel. Hamilton Standard Propellers were furnished with both the stock 52478 & 52478-1 dome barrel seals. AirCorps recommends operators, and maintainers stock both seals.

AirCorps can provide parts and answer questions related to this seal. AirCorps Depot also maintains a growing inventory of Hamilton Standard prop parts to support the continued airworthiness of airframes and propellers.

Contact Eric Trueblood for more information – erict@aircorpsaviation.com

AVAILABLE FOR PURCHASE

52478-SET

(QTY 1) 52478-ACP & (QTY 1) 52478-1-ACP

Seals – Dome and Barrel – STD and .025

PMA APPROVED

52478-ACP

(QTY 1) 52478-ACP

Seal – Dome and Barrel

PMA APPROVED

52478-1-ACP

(QTY 1) 52478-1-ACP

Seal – Dome and Barrel – .025 Oversized

PMA APPROVED

AIRCORPS ENGINEERING

Andy Smude

Andy Smude
Engineering Manager

Andy is the engineering manager at AirCorps Aviation. He completed his Bachelor of Aerospace Engineering and Mechanics at the University of Minnesota in 2008. He has over 15 years of experience in the Aerospace and Defense industry with Boeing and Northrop Grumman, working alongside US Navy, US Air Force, and international customers. Andy is honored to be using his experience and skills to contribute to the restoration and preservation of vintage and World War II aircraft.
 
The AirCorps Engineering team helps achieve the company’s mission by providing complete, quality design definition to internal and external customers. From internal customers like our Restoration and Fabrication teams, to external customers who are restoring, repairing and maintaining modern and historic aircraft. In his role at AirCorps, Andy manages a team of highly capable engineers who support this mission through Reverse Engineering, Design, and Certification. He is the primary interface with the FAA Certification Branch in the approval of PMA design data.

Contact us for more info on ways we can assist with your project!

Ryan Maier is AirCorps Aviation’s certification engineer who completed his Bachelors of Mechanical Engineering at NDSU in 2021. He has a background in aircraft integration through certification of Cloud Seeding and Atmospheric Research aircraft in North Dakota. Ryan is able to live his passion every day as part of the AirCorps team while researching original technical data to generate new PMA products to support and preserve the warbird Industry. Ryan owns and operates a Luscombe 8A and is continually invested in learning, supporting, and engineering historical aircraft.

Contact us for more info on ways we can assist with your project!

Ryan Maier
Certification Engineer

DISCLAIMER

WHILE AIRCORPS BELIEVES THAT THE INFORMATION CONTAINED THEREIN IS ACCURATE AND CORRECT, AIRCORPS DOES NOT WARRANT THE ACCURACY OR THE CORRECTNESS OF ANY DRAWINGS, MANUALS, OR THE INFORMATION (COLLECTIVELY THE “INFORMATION”) CONTAINED THEREIN. THE INFORMATION, DRAWINGS AND REFERENCE MATERIAL ARE SUPPLIED TO THE CUSTOMER ON AN “AS IS, WHERE IS” BASIS, WITH NO WARRANTY OR REPRESENTATION OF ANY KIND. VENDOR MAKES NO WARRANTIES, EITHER EXPRESS OR IMPLIED, WITH RESPECT TO MERCHANTABILITY OR FITNESS APPLICABLE TO THE INFORMATION, INCLUDING WITHOUT LIMITATION WARRANTIES AS TO THE ACCURACY OF THE INFORMATION, CONDITION, VALUE, MERCHANTABILITY, OR FITNESS FOR ANY PARTICULAR PURPOSE, WHETHER ARISING BY OPERATION OF LAW, COURSE OF DEALING OR USAGE OF TRADE, ARISING AT LAW OR IN EQUITY OR OTHERWISE. YOU ACKNOWLEDGE THAT YOU ARE NOT RELYING UPON ANY STATEMENT OR REPRESENTATION OF SELLER REGARDING THE INFORMATION. YOU AND VENDOR HEREBY EXPRESSLY WAIVE ANY CLAIM FOR INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, INCLUDING DAMAGES RESULTING IN PERSONAL INJURY AGAINST THE OTHER, AND WILL NOT BE LIABLE TO THE OTHER PARTY IN CONNECTION WITH THIS AGREEMENT UNDER ANY THEORY OF LIABILITY FOR ANY INCIDENTAL, SPECIAL, INDIRECT, PUNITIVE OR CONSEQUENTIAL DAMAGES OF ANY KIND, INCLUDING WITHOUT LIMITATION, ANY SUCH DAMAGES ARISING FROM BREACH OF CONTRACT, BREACH OF WARRANTY, NEGLIGENCE OR STRICT LIABILITY. ALL WORK SHOULD BE COMPLETED IN ACCORDANCE WITH FAA REGULATIONS AND APPROVED DATA.

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