Learjet 36A - Maximum Zero Wing and Tip Fuel Weight; Maximum Certified Takeoff Weight

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WEIGHT AND C.G. UNITS (CONT)
MAXIMUM CERTIFIED TAKEOFF WEIGHT
MODEL 35A:
• Serials 35·067 and subsequent not incorporating ECR 1495,
ECR 2234, AAK
77·8, or AAK 80·2 . . . . . . . . . . . 17,000 Pounds
• SerialS '35~067 thru 35·344 when incorporating
ECR 1495 orAAK 77·8 ................... .
• Serials 35·067 thru 35·344 when incorporating
AAK80·2 .............................. .
• Serials 35·345 and subsequent when incorporating
ECR2234 ............................. .
MODEL 36A:
• Serials 36·018 thru 36·045 not incorporating
AAK80·2 .............................. .
• Serials 36·018 thru 36-045 when incorporating
AAK80-2 .............................. .
• Serials 36-046 and subsequent ............... .
MAXIMUM ZERO WING AND TIP fUEL WEIGHT .
7,711 kg
18,000 Pounds
8,165 kg
18,300 Pounds
8,301 kg
18,300 Pounds
8,301 kg
18,000 Pounds
8,165 kg
18,300 Pounds
8,301 kg
18,300 Pounds
8,301 kg
13,500 Pounds
&,124 kg
All weights in excess of 13,500 pounds must consist
of wing and tip tank fuel, except as follows:
1. The Maximum Zero
Wing and Tip Fuel Weight may
be increased to 14,000 pounds by adding up to 500
pounds of additional fuselage fuel. The additional
fuselage fuel must be transferred prior to reaching
a total wing fuel quantity of
2250 pounds.
2. In the event the additional fuselage fuel cannot be
transferred,
VMO must be reduced to 325 KIAS.
FAA APPROVED 4-30-76
REISSUED 2-25-81, CHANGE 6
1-3
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