Torque Information; Alternator Drive Coupling Inspection & Maintenance - Planet ES-10024B-1 Maintenance Manual

6.3

Torque Information

Reference
Figure 6.1 (gear)
Figure 6.2 (belt)
Section 2.7
Section 2.7 (top & bottom)
Section 2.7 (top & bottom)
Figure 6.4
Section 2.7 (top & bottom)
Figure 6.4 (bottom only)
Figure 6.4 (top only)
* Use a 5/16 inch hex key to hold shaft while applying torque to output shaft nut.
** Attachment of Ground, Battery, Aux. or Field wires from the engine or airframe may use above torque unless
value differs from engine/airframe OEM torque. OEM torque specifications shall supersede HET value.
Always hold the bottom nut when applying torque to top nut to prevent over torque of bottom nut.
*** The engine/airframe OEM or the supplier of the drive coupling or belt drive may indicate a torque value for
the output shaft that differs from that listed in the Torque Table above. If the torque value differs, the engine/
airframe OEM torque value shall supersede the HET value above.
6.4 Alternator Drive Coupling Inspection & Maintenance
(ES-10024, ALV-9610, & ES-6024D)
A. Although the alternator drive coupling is provided by the engine or airframe manufacturer who have issued
manuals and/or instructions regarding their maintenance, the coupling is fundamental to the operation of
Hartzell Engine Technologies LLC (HET) alternator. As such, some general troubleshooting regarding
the coupling is offered here to prevent mis-diagnosis of what may seem to be an alternator fault. Refer to
Troubleshooting section 3.
(1) Check for any and all service information from the engine, airframe and the drive coupling
manufacturer concerning the installation, inspection, and replacement of the drive coupling.
(2) Check the general condition of the drive coupling (requires removal of the alternator).
(3) Check the shaft nut and cotter pin for damage (damage to these parts will indicate interference with
internal engine parts). If damaged, determine cause.
(4) Using the manufacturer's service information, check the condition of the gear teeth and the elastomer
insert. If damaged, replace or overhaul the drive coupling.
(5) Whenever the alternator is overhauled, HET recommends that the drive coupling be replaced. If
the alternator cannot be overhauled or repaired and is being replaced, the coupling should also be
replaced.
(6) To further aid inspection, Continental Motors includes drive coupling service information in the
appropriate engine manuals and also in service bulletins. (Refer to the latest CMI SB11-3 and/or SB95-
3B for drive coupling service information.)
24-30-01
Page: 6-2
© 2021 - Hartzell Engine Technologies - All rights reserved
Description Torque Value (US)
Output Shaft Nut
Output Shaft Nut*
Through Bolts
Ground Nut (NEG)**
Output Nut (POS)**
Screws (Brush Holder)
AUX Nut
Field Nut (F1 & F2)
Field Nut (F1 & F2)
Table 6.1 - Torque Specifications
Torque Value (SI)
25-37.5 ft-lbs*** 33.9-50.8 Nm
55-65 ft-lbs*** 74.6-88.1 Nm
45-50 in-lbs 5.08-5.65 Nm
25-30 in-lbs 2.82-3.39 Nm
70-85 in-lbs 7.91-9.60 Nm
11-14 in-lbs 1.24-1.58 Nm
25-30 in-lbs 2.82-3.39 Nm
12-15 in-lbs 1.36-1.69 Nm
6-8 in-lbs 0.68-0.90 Nm
Aircraft Alternator
Maintenance Manual
ES1031
Rev. A: 11 Aug. 2021