TM 1-1670-260-12&P 0011 00
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12. POST RECOVERY DISABLED HELICOPTER PROCEDURES
Before returning a recovered helicopter to flight status perform the following:
a. Inspection of tail-boom is mandatory if drogue chute is used.
b. Contact Commander, U.S. Army Aviation and Missile Command.
(1) Ensure that the recovery parameters (limitations) listed in Table 4
have not been exceeded. If Table 4 parameters have been exceeded or
it cannot be determined that Table 4 parameters were met, then contact
AMSAM-RD-AE-I-P-A (Mr. Lee Bumbicka) for corrective action or disposi-
Table 4 Recovered Helicopter Recovery Parameters (Limitations)
Parameter
Value
Units
Max victim vehicle weight
20,000
LB
Maximum speed
40
KIAS
Maximum bank angle
20
Degrees
Maximum rate of climb
1000
FPM
Maximum rate of descent
1000
FPM
Center of gravity location
201 - 207 Inches (Sta)
Maximum landing sink rate (note 1) 5.6
FPS
Angle of Attack
-2 to 3 Degrees
Terrain Lifting Limits - Fore/Aft Slope + 12
Degrees
Terrain Lifting Limits - Lateral Slope + 15
Degrees
Use of Drogue Chute
No
-
NOTE
If maximum sink rate cannot be determined then perform Hard
Landing Inspection per Table 6.
(2) Verify that the recovered helicopter utilized the main rotor blade
tiedown attachment points listed in Table 5. If the recovered heli-
copter used main rotor blade tiedown attachment points other than
those listed in Table 5 or did not use any main rotor blade tiedown
attachment points, then contact AMSAM-RD-AE-I-P-A (Mr. Lee Bumbicka)
for corrective action or disposition.
Table 5 Recovered Helicopter Main Rotor Blade Tiedown Substantiated Attachment Points
Blades Attachment Location Rating
Forward MLG Training Arm-mooring Ring Excellent
Forward Pylon Rack Good
Forward Right Upper MLG Shock Strut Poor
Aft MLG Jack Pad Excellent
Aft FS 450 Jack Fitting Good
Aft Pylon Rack Good
Forward and Aft Wing Tip Lugs Excellent
0011 00-15
tion.