Previous Page Page 776 Next Page  
background image

767 

Federal Aviation Administration, DOT 

§ 29.853 

position) for a distance from that exit 
of not less than the width of the nar-
rowest passenger seat installed on the 
rotorcraft; 

(2) For rotorcraft that have a pas-

senger seating configuration, excluding 
pilot seats, of 19 or less, there may be 
minor obstructions in the region de-
scribed in paragraph (c)(1) of this sec-
tion, if there are compensating factors 
to maintain the effectiveness of the 
exit. 

[Doc. No. 5084, 29 FR 16150, Dec. 3, 1964, as 
amended by Amdt. 29–12, 41 FR 55472, Dec. 20, 
1976] 

§ 29.815

Main aisle width. 

The main passenger aisle width be-

tween seats must equal or exceed the 
values in the following table: 

Passenger seating capacity 

Minimum main passenger 

aisle width 

Less than 
25 inches 

from floor 

(inches) 

25 Inches 

and more 
from floor 

(inches) 

10 or less ...................................

12 

15 

11 through 19 ............................

12 

20 

20 or more .................................

15 

20 

1

A narrower width not less than 9 inches may be approved 

when substantiated by tests found necessary by the 
Administrator. 

[Doc. No. 5084, 29 FR 16150, Dec. 3, 1964, as 
amended by Amdt. 29–12, 41 FR 55472, Dec. 20, 
1976] 

§ 29.831

Ventilation. 

(a) Each passenger and crew compart-

ment must be ventilated, and each 
crew compartment must have enough 
fresh air (but not less than 10 cu. ft. per 
minute per crewmember) to let crew-
members perform their duties without 
undue discomfort or fatigue. 

(b) Crew and passenger compartment 

air must be free from harmful or haz-
ardous concentrations of gases or va-
pors. 

(c) The concentration of carbon mon-

oxide may not exceed one part in 20,000 
parts of air during forward flight. If the 
concentration exceeds this value under 
other conditions, there must be suit-
able operating restrictions. 

(d) There must be means to ensure 

compliance with paragraphs (b) and (c) 
of this section under any reasonably 
probable failure of any ventilating, 
heating, or other system or equipment. 

§ 29.833

Heaters. 

Each combustion heater must be ap-

proved. 

F

IRE

P

ROTECTION

 

§ 29.851

Fire extinguishers. 

(a) 

Hand fire extinguishers. For hand 

fire extinguishers the following apply: 

(1) Each hand fire extinguisher must 

be approved. 

(2) The kinds and quantities of each 

extinguishing agent used must be ap-
propriate to the kinds of fires likely to 
occur where that agent is used. 

(3) Each extinguisher for use in a per-

sonnel compartment must be designed 
to minimize the hazard of toxic gas 
concentrations. 

(b) 

Built-in fire extinguishers. If a 

built-in fire extinguishing system is re-
quired— 

(1) The capacity of each system, in 

relation to the volume of the compart-
ment where used and the ventilation 
rate, must be adequate for any fire 
likely to occur in that compartment. 

(2) Each system must be installed so 

that— 

(i) No extinguishing agent likely to 

enter personnel compartments will be 
present in a quantity that is hazardous 
to the occupants; and 

(ii) No discharge of the extinguisher 

can cause structural damage. 

§ 29.853

Compartment interiors. 

For each compartment to be used by 

the crew or passengers— 

(a) The materials (including finishes 

or decorative surfaces applied to the 
materials) must meet the following 
test criteria as applicable: 

(1) Interior ceiling panels, interior 

wall panels, partitions, galley struc-
ture, large cabinet walls, structural 
flooring, and materials used in the con-
struction of stowage compartments 
(other than underseat stowage com-
partments and compartments for stow-
ing small items such as magazines and 
maps) must be self-extinguishing when 
tested vertically in accordance with 
the applicable portions of appendix F 
of Part 25 of this chapter, or other ap-
proved equivalent methods. The aver-
age burn length may not exceed 6 
inches and the average flame time 
after removal of the flame source may 

VerDate Mar<15>2010 

10:12 Mar 18, 2014

Jkt 232046

PO 00000

Frm 00777

Fmt 8010

Sfmt 8010

Y:\SGML\232046.XXX

232046

pmangrum on DSK3VPTVN1PROD with CFR

  Previous Page Page 776 Next Page