Learjet 36A - Maximum Allowable Landing Weight; Center-Of-Gravity Envelope; Aircraft Certified for 17,000 Pounds Takeoff Weight

111.111 ••••• 1
WBGHT AND C.G. UMlTS (CONI')
MAXIMUM AllOWABlE lANDING WEIGHT
The landing weight is limited by the most restrictive of the following
requirements:
• Maximum Certified Landing Weight.
Perform Hard
or Overweight Landing Inspection
(Chapter 5, 35/36/35N36A Maintenance Manual) if
Maximum Certified Landing Weight is exceeded. I
• Maximum Landing Weight for the nmway and ambient conditions
as determined from the applicable lANDING DISTANCE chart in
Section
V.
• Maximum Landing Weight (Approach Climb or Brake Energy Um-
ited) for altitude and temperature as determined from the applicable
figure entitled
lANDING WEIGHT UMITS in Section V.
CENTER-oF-GRAVITV ENVELOPE
• Aircraft Certified for 17,000 Pounds Takeoff Weight. The for-
ward C.G. limit is Fuselage Station (F.S.) 366.31 (5% MAC) for all
weights
up to and including 10,000 pounds and tapers through ES.
375.96 (16.66% MAC) at 17,000 pounds to ES. 376.31 (17.09%
MAC) at 17,250 pounds. The aft C.G. limit is ES. 387.00 (30%
MAC) for all weights. Refer to Rgure 1-1.
• Aircraft Certified for 18,000 Pounds Takeoff Weight. The for-
ward
C.G. limit is Fuselage Station (F.S.) 366.31 (5% MAC) for all
weights up to and including 10,000 pounds and tapers through ES.
377 .34 (18.33% MAC) at 18,000 pounds to ES. 377.69 (18.76%
MAC) at 18,250 pounds. The aft C.G. limit is ES. 387.00 (30%
MAC) at all weights. Refer to Rgure 1-2.
• Aircraft Certified for 18,300 Pounds Takeoff Weight. The for-
ward
C.G. limit is Fuselage Station (F.S.) 366.31 (5% MAC) for all
weights up to and including 10,000 pounds and tapers through ES.
377.75 (18.83% MAC) at 18,300 pounds to ES. 378.03 (19.17%
MAC) at 18,500 pounds. The aft C.G. limit is ES. 387.00 (30%
MAC) at all weights. Refer to Figure 1-3.
FAA APPROVED 4-30-76
REISSUED 2-25-81, CHANGE 10
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