SPECIAL AIRWORTHINESS INFORMATION BULLETIN
Aircraft Certification Service
Washington, DC
U.S. Department of Transportation
Federal Aviation Administration
NE-04-45

January 16, 2004

This is information only. Recommendations aren’t mandatory.

Introduction

This Special Airworthiness Information Bulletin (SAIB) alerts you, owners and operators of Woodward Governor propeller governors on reciprocating engines, that the propeller governors may have a non-heat treated flyweight head, which could lead to loss of speed governing on the propeller governor.

Background

On November 20, 2002, 19:00 local time, the pilots of a Twin Commander (Rockwell International) Model 700, noticed the R/H engine going into over speed condition. They immediately tried to reduce engine RPM by throttle and prop control with no success. They elected to shutdown and secure the R/H engine. They contacted the Toronto Center, declaring an emergency. They landed safely with no damage to the airframe or injury. We have confirmed that the propeller governor had an internal failure which caused the over speed condition. Inspection of the propeller governor found a 30-RPM over speed with full control of the governor over the entire RPM range.

The tear down inspection found that the drive spring was disconnected from the driver which allowed the flyweight head to rotate against the ends of two screws, causing the end of the screws to shear off. When the screws sheared off, the driver was no longer driving the flyweight head. The drive spring wore a groove in the mating surface of the flyweight head. It appears that this groove allowed the tang of the drive spring to come out of its hole in the driver.

Woodward Governor issued Service Bulletin (SB) 82402-61-001, December 8, 2003, to identify the possible affected governors by serial numbers, and inspection criteria for flyweight head and driver assemblies used on certain propeller governors. Detail inspection and part replacement descriptions are listed in temporary revision of Operation Maintenance Manuals 33092A, 33169, and 33194, December 8, 2003.

Three assemblies have shown excessive wear from the potential suspect lot.

The affected models for the 4508-042-flyweight head assembly are listed below:
 
210554 210727 A210703 A210803 B210572 C210719 F210882 R210571
210562 210731 A210709 A210804 B210709 C210801 H210800 R210573
210704 210732 A210710 A210805 B210710 D210710 J210800 R210650
210712 210733 A210711 A210806 B210713 D210713 L210571 R210707
210714 210751 A210713 A210839 B210719 D210719 L210573 R210755
210717 210753 A210719 A210880 B210800 D210800 L210650 R210880
210718 210758 A210728 A210881 B210801 D210882 L210755 R210909
210720 210907 A210787 A210883 B210883 E210710 L210880 R210913
210723 210918 A210800 A210885 C210572 E210713 L210909 R210924
210724 210934 A210801 A210899 C210710 F210710 L210913
210726 A210572 A210802 A210924 C210713 F210800 L210924

Recommendation

We recommend that you check serial numbers in accordance with Woodward Governor’s SB. If affected, please inspect propeller governors in accordance with temporary revision of Operation Maintenance Manuals 33092A, 33169, and 33194, dated December 8, 2003.

For Further Information Contact

Chung-Der Young, Aerospace Engineer, FAA Chicago Aircraft Certification Office, Propulsion Branch, ACE-118C, 2300 East Devon Avenue, Des Plaines, IL, 60018; phone (847) 294 7309; fax: (847) 294-7834; email: chung-der.young@faa.gov