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789 

Federal Aviation Administration, DOT 

§ 29.1027 

the oil is contaminated to a degree 
(with respect to particle size and den-
sity) that is greater than that estab-
lished for the engine under Part 33 of 
this chapter. 

(3) The oil strainer or filter, unless it 

is installed at an oil tank outlet, must 
incorporate a means to indicate con-
tamination before it reaches the capac-
ity established in accordance with 
paragraph (a)(2) of this section. 

(4) The bypass of a strainer or filter 

must be constructed and installed so 
that the release of collected contami-
nants is minimized by appropriate lo-
cation of the bypass to ensure that col-
lected contaminants are not in the by-
pass flow path. 

(5) An oil strainer or filter that has 

no bypass, except one that is installed 
at an oil tank outlet, must have a 
means to connect it to the warning 
system required in § 29.1305(a)(18). 

(b) Each oil strainer or filter in a 

powerplant installation using recipro-
cating engines must be constructed and 
installed so that oil will flow at the 
normal rate through the rest of the 
system with the strainer or filter ele-
ment completely blocked. 

[Amdt. 29–10, 39 FR 35463, Oct. 1, 1974, as 
amended by Amdt. 29–22, 49 FR 6850, Feb. 23, 
1984; Amdt. 29–26, 53 FR 34218, Sept. 2, 1988] 

§ 29.1021

Oil system drains. 

A drain (or drains) must be provided 

to allow safe drainage of the oil sys-
tem. Each drain must— 

(a) Be accessible; and 
(b) Have manual or automatic means 

for positive locking in the closed posi-
tion. 

[Amdt. 29–22, 49 FR 6850, Feb. 23, 1984] 

§ 29.1023

Oil radiators. 

(a) Each oil radiator must be able to 

withstand any vibration, inertia, and 
oil pressure loads to which it would be 
subjected in operation. 

(b) Each oil radiator air duct must be 

located, or equipped, so that, in case of 
fire, and with the airflow as it would be 
with and without the engine operating, 
flames cannot directly strike the radi-
ator. 

§ 29.1025

Oil valves. 

(a) Each oil shutoff must meet the re-

quirements of § 29.1189. 

(b) The closing of oil shutoffs may 

not prevent autorotation. 

(c) Each oil valve must have positive 

stops or suitable index provisions in 
the ‘‘on’’ and ‘‘off’’ positions and must 
be supported so that no loads resulting 
from its operation or from accelerated 
flight conditions are transmitted to 
the lines attached to the valve. 

§ 29.1027

Transmission and gearboxes: 

general. 

(a) The oil system for components of 

the rotor drive system that require 
continuous lubrication must be suffi-
ciently independent of the lubrication 
systems of the engine(s) to ensure— 

(1) Operation with any engine inoper-

ative; and 

(2) Safe autorotation. 
(b) Pressure lubrication systems for 

transmissions and gearboxes must 
comply with the requirements of 
§§ 29.1013, paragraphs (c), (d), and (f) 
only, 29.1015, 29.1017, 29.1021, 29.1023, and 
29.1337(d). In addition, the system must 
have— 

(1) An oil strainer or filter through 

which all the lubricant flows, and 
must— 

(i) Be designed to remove from the 

lubricant any contaminant which may 
damage transmission and drive system 
components or impede the flow of lu-
bricant to a hazardous degree; and 

(ii) Be equipped with a bypass con-

structed and installed so that— 

(A) The lubricant will flow at the 

normal rate through the rest of the 
system with the strainer or filter com-
pletely blocked; and 

(B) The release of collected contami-

nants is minimized by appropriate lo-
cation of the bypass to ensure that col-
lected contaminants are not in the by-
pass flowpath; 

(iii) Be equipped with a means to in-

dicate collection of contaminants on 
the filter or strainer at or before open-
ing of the bypass; 

(2) For each lubricant tank or sump 

outlet supplying lubrication to rotor 
drive systems and rotor drive system 
components, a screen to prevent en-
trance into the lubrication system of 
any object that might obstruct the 

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