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14 CFR Ch. I (1–1–14 Edition) 

§ 25.511 

§ 25.511

Ground load: unsymmetrical 

loads on multiple-wheel units. 

(a) 

General.  Multiple-wheel landing 

gear units are assumed to be subjected 
to the limit ground loads prescribed in 
this subpart under paragraphs (b) 
through (f) of this section. In addi-
tion— 

(1) A tandem strut gear arrangement 

is a multiple-wheel unit; and 

(2) In determining the total load on a 

gear unit with respect to the provisions 
of paragraphs (b) through (f) of this 
section, the transverse shift in the load 
centroid, due to unsymmetrical load 
distribution on the wheels, may be ne-
glected. 

(b) 

Distribution of limit loads to wheels; 

tires inflated. The distribution of the 
limit loads among the wheels of the 
landing gear must be established for 
each landing, taxiing, and ground han-
dling condition, taking into account 
the effects of the following factors: 

(1) The number of wheels and their 

physical arrangements. For truck type 
landing gear units, the effects of any 
seesaw motion of the truck during the 
landing impact must be considered in 
determining the maximum design loads 
for the fore and aft wheel pairs. 

(2) Any differentials in tire diameters 

resulting from a combination of manu-
facturing tolerances, tire growth, and 
tire wear. A maximum tire-diameter 
differential equal to 

2

3

of the most un-

favorable combination of diameter 
variations that is obtained when tak-
ing into account manufacturing toler-
ances, tire growth, and tire wear, may 
be assumed. 

(3) Any unequal tire inflation pres-

sure, assuming the maximum variation 
to be 

±

5 percent of the nominal tire in-

flation pressure. 

(4) A runway crown of zero and a run-

way crown having a convex upward 
shape that may be approximated by a 
slope of 1

1

2

percent with the hori-

zontal. Runway crown effects must be 
considered with the nose gear unit on 
either slope of the crown. 

(5) The airplane attitude. 
(6) Any structural deflections. 
(c) 

Deflated tires. The effect of de-

flated tires on the structure must be 
considered with respect to the loading 
conditions specified in paragraphs (d) 
through (f) of this section, taking into 

account the physical arrangement of 
the gear components. In addition— 

(1) The deflation of any one tire for 

each multiple wheel landing gear unit, 
and the deflation of any two critical 
tires for each landing gear unit using 
four or more wheels per unit, must be 
considered; and 

(2) The ground reactions must be ap-

plied to the wheels with inflated tires 
except that, for multiple-wheel gear 
units with more than one shock strut, 
a rational distribution of the ground 
reactions between the deflated and in-
flated tires, accounting for the dif-
ferences in shock strut extensions re-
sulting from a deflated tire, may be 
used. 

(d) 

Landing conditions. For one and 

for two deflated tires, the applied load 
to each gear unit is assumed to be 60 
percent and 50 percent, respectively, of 
the limit load applied to each gear for 
each of the prescribed landing condi-
tions. However, for the drift landing 
condition of § 25.485, 100 percent of the 
vertical load must be applied. 

(e) 

Taxiing and ground handling condi-

tions.  For one and for two deflated 
tires— 

(1) The applied side or drag load fac-

tor, or both factors, at the center of 
gravity must be the most critical value 
up to 50 percent and 40 percent, respec-
tively, of the limit side or drag load 
factors, or both factors, corresponding 
to the most severe condition resulting 
from consideration of the prescribed 
taxiing and ground handling condi-
tions; 

(2) For the braked roll conditions of 

§ 25.493 (a) and (b)(2), the drag loads on 
each inflated tire may not be less than 
those at each tire for the symmetrical 
load distribution with no deflated tires; 

(3) The vertical load factor at the 

center of gravity must be 60 percent 
and 50 percent, respectively, of the fac-
tor with no deflated tires, except that 
it may not be less than 1g; and 

(4) Pivoting need not be considered. 
(f) 

Towing conditions. For one and for 

two deflated tires, the towing load, 
F

TOW,

must be 60 percent and 50 percent, 

respectively, of the load prescribed. 

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