Hamilton Standard Division | Hamilton Sundstrand Airworthiness Directives

6 ADs indexed for Hamilton Standard Division | Hamilton Sundstrand aircraft.

Models

Recent ADs

2013-16-10

final rule

Airworthiness Directives; Hamilton Standard Division and Hamilton Sundstrand Corporation Propellers

Unsafe Condition: The amount of corrosion detected during major inspections (MI) could result in propeller failure and loss of airplane control.

Effective: Sep 19, 2013 Category: propeller Compliance: Within 45 days after the effective date of this AD for Hamilton Sundstrand Corporation propeller ...

Why matched: Airworthiness Directives; Hamilton Standard Division and Hamilton Sundstrand Corporation Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

96-25-20

final rule

Hamilton Standard 14RF and 14SF Series, and Hamilton Standard/British Aerospace Model 6/5500/F Propellers

Unsafe Condition: Failure of critical control components, including transfer tube assemblies, actuator assemblies, and propeller control units (PCUs), could result in loss of propeller control and subsequent loss of...

Effective: Feb 7, 1997 Category: propeller Compliance: within 6,000 hours time in service (TIS), or 3 years, whichever occurs first, after the effective...

Why matched: Hamilton Standard 14RF and 14SF Series, and Hamilton Standard/British Aerospace Model 6/5500/F Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

96-08-02

final rule

Hamilton Standard Models 14RF-9, 14RF-19, 14RF-21; and 14SF-5, 14SF-7, 14SF-11, 14SFL11, 14SF-15, 14SF-17, 14SF-19, and 14SF-23; and Hamilton Standard/British Aerospace 6/5500/F Propellers

Unsafe Condition: Separation of a propeller blade due to cracks initiating in the blade taper bore, which can result in aircraft damage and possible loss of aircraft control.

Effective: May 9, 1996 Category: propeller Compliance: No later than July 31, 1996 for Model 14RF-9 and February 28, 1997 for other affected propeller m...

Why matched: Hamilton Standard Models 14RF-9, 14RF-19, 14RF-21; and 14SF-5, 14SF-7, 14SF-11, 14SFL11, 14SF-15, 14SF-17, 14SF-19, and 14SF-23; and Hamilton Standard/British Aerospace 6/5500/F Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

95-22-12

final rule

Hamilton Standard 14RF, 247F, 14SF, and 6/5500/F Series Propellers

Unsafe Condition: Control Unit Servo Ballscrew Internal Spline Assembly

Effective: May 6, 1996 Category: propeller

Why matched: Hamilton Standard 14RF, 247F, 14SF, and 6/5500/F Series Propellers

93-06-06

final rule

HAMILTON STANDARD Models 14RF-9, 14RF-19, and 14RF-21, and Models 14SF-5, 14SF-7, 14SF-11, 14SF-15, 14SF-17, 14SF-19, and 14SF-23 Propellers, and Hamilton Standard-British Aerospace Model 6/5500/F-1 propellers

Unsafe Condition: Loss of control of the propeller blade pitch due to propeller control unit (PCU) ballscrew quill wear.

Effective: Jul 6, 1993 Category: propeller Compliance: Within 10 hours time in service (TIS) after the effective date; within 30 hours TIS; within 60 da...

Why matched: HAMILTON STANDARD Models 14RF-9, 14RF-19, and 14RF-21, and Models 14SF-5, 14SF-7, 14SF-11, 14SF-15, 14SF-17, 14SF-19, and 14SF-23 Propellers, and Hamilton Standard-British Aerospace Model 6/5500/F-1 propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

81-13-06 R2

final rule

HAMILTON STANDARD: Hydromatic (noncounterweighted) propellers with aluminum blades

Unsafe Condition: Propeller blade failure due to corrosion and fatigue in the blade fillet and shank area, particularly under the teflon friction reduction strip and the resin corrosion barrier.

Effective: Sep 15, 1989 Category: propeller Compliance: Within 90 days after July 1, 1982, or within 18 months since last inspection, whichever occurs later

Why matched: HAMILTON STANDARD: Hydromatic (noncounterweighted) propellers with aluminum blades

Technical illustration of an aircraft propeller assembly
Problem area Propeller

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