2-8 Figure 2-15.  Sample excerpt from TCDS A00009CH (continued). A00009CH -2- Airspeed Limits  S/N 1005 thru 1147: V ne Never Exceed Speed  200 KIAS  no Maximum Structural Cruising Speed  165 KIAS  V o (2900 lbs) Operating Maneuvering Speed  135 KIAS  Vo  (2600 lbs) Operating Maneuvering Speed  126 KIAS  (2200 lbs) Operating Maneuvering Speed  116 KIAS  V fe Maximum Flap Extension Speed  100 KIAS  pd Maximum Parachute Deployment Speed 135 KIAS  S/N 1148 thru 1877, 1879 thru 1885, and S/N 1005 thru 1147 if Cirrus Service Bulletin SB 20-01- 00 is complied with: V ne Never Exceed Speed  200 KIAS  no Maximum Structural Cruising Speed  165 KIAS  V o (3000 lbs) Operating Maneuvering Speed  131 KIAS  Vo  (2600 lbs) Operating Maneuvering Speed  122 KIAS  (2300 lbs) Operating Maneuvering Speed  114 KIAS  V fe Maximum Flap Extension Speed  100 KIAS  pd Maximum Parachute Deployment Speed 135 KIAS  S/N 1878, 1886 and subsequent: Vne  Never Exceed Speed  200 KIAS  Vno  Maximum Structural Cruising Speed  163 KIAS  Vo  (3050 lbs) Operating Maneuvering Speed  130 KIAS  Vfe  Maximum Flap Extension Speed  104 KIAS  Vpd  Maximum Parachute Deployment Speed 133 KIAS  C.G. Range  S/N 1005 thru 1147: Forward Limits: 138.7 inches at 2110 lbs with a straight line taper to 141.0 inches at 2694 lbs, and  143.0 inches at 2900 lbs.  Aft Limits: 144.6 inches at 2110 lbs, with straight line taper to 147.4 inches at 2570 lbs, and to  147.9 inches at 2745 lbs, and 148.2 inches at 2900 lbs.  S/N 1148 thru 1877, 1879 thru 1885, and S/N 1005 thru 1147 if Cirrus Service Bulletin SB 20-01- 00 is complied with: Forward Limits: 138.7 inches at 2110 lbs with a straight line taper to 141.0 inches at 2694 lbs, and  144.1 inches at 3000 lbs.  Aft Limits: 144.6 inches at 2110 lbs, with straight line taper to 147.4 inches at 2570 lbs, and to  148.1 inches at 2900 lbs, and 148.0 inches at 3000 lbs.  S/N 1878, 1886 and subsequent: Forward Limits: 137.8 inches at 2100 lbs with a straight line taper to 139.1 inches at 2700 lbs, and  to 140.7 inches at 3050 lbs  Aft Limits: 148.1 inches at 2100 lbs, with straight line to 148.1 inches at 3050 lbs.  Empty Weight  C.G. Range  None  Maximum Weight  S/N 1005 thru 1147: Takeoff and Landing: 2900 lbs.  S/N 1148 thru 1877, 1879 thru 1885, and S/N 1005 thru 1147 if Cirrus Service Bulletin SB 20-01- 00 is complied with: Takeoff:  3000 lbs.  Landing:  2900 lbs.  Zero Fuel:  S/N 1878, 1886 and subsequent: Takeoff and Landing: 3050 lbs. 