Hartzell HC-B3-2 Series Owner's Manual And Logbook page 26

H. The following list specifies life limits for pitch change rod
part number C-1169-2 only. Pitch change rods listed are life
limited only on the specified applications.
(1) Propeller Models on FAA Type Certified Aircraft
NONE
(2) Propeller Models on Aircraft without FAA Type Certificate
Aircraft/Engine/Propeller
Aircraft: Antonov AN-38-100
Engine: Honeywell - TPE331-14( )
Propeller: HC-B5MA-5A/M11276N(C)K-3
2. Periodic Inspections
A. The HC-B3TN-3UL/LT10173N-21R propeller installed on
Advanced Aerodynamics & Structures model 450 "Jetcruzer"
is required to have repetitive blade inspection for erosion
and/or corrosion at intervals not to exceed 24 months or
600 hours of operation, whichever occurs first. Inspection
methods and procedures are described in Hartzell Service
Bulletin HC-SB-61-181A.
FAA APPROVED
by: ______________________________ date: ____________
Manager, Chicago Aircraft Certification Office,
AIRWORTHINESS LIMITATIONS
Propeller Owner's Manual
ACE-115C
Federal Aviation Administration
139
Pitch Change
Rod Life Limit
12,053 hours
61-00-39
Rev. 17 Apr/20
Page 8