BOLT TIGHTENING
GENERAL
NEVER
over tighten a bolt. Tighten ONLY when and as instructed. Particular care is necessary
when tightening bolts which pass through aluminum tubes with no solid internal support. BEFORE
installing bolts, check that the grip-length is correct.
Refer to FAA Advisory Circular AC65-9A, Page 129 for additional information.
Bolts and nuts should be clean and dry before installation. Threads should not be oiled. Bolts and
nuts with damaged threads and/or rough ends should not be used.
Whenever possible, bolts should be installed with the head on TOP or in the FORWARD position.
This positioning tends to prevent the bolt from slipping out if the nut is accidentally lost. There may
be specific instances where the assembly instructions specify a particular bolt orientation. DO NOT
contradict the assembly instructions in such a case.
IMPORTANT:
Nylock (locknuts) nuts and lock nuts should NEVER be used more than TWICE as
they become less vibration resistant with each removal.
Castle Nuts should only be tightened to the specified degree of tightness and must always be used
with a Cotter Pin for security. Refer to Figure 1-6 on the previous page for the proper method of
bending Cotter Pins.
NOTE:
When Castle Nuts are tightened, the Cotter Pin holes may not line up with the slots in the
nut when the torque setting is reached. Back off to the nearest slot. A Castle Nut must NEVER be
over tightened to permit lining up the safety hole with the next tighter slot.
WARNING: A bolt which is subject to rotation in flight will use a Castle Nut. A Castle Nut
relies on a Cotter Pin to prevent it from backing off. Always ensure Castle Nuts are
secured with a Cotter Pin.
WHENEVER
Possible, it is preferred to rotate the nut onto the bolt as opposed to rotating the bolt
onto the nut.
HOLE SIZE
Typically a 1/4” bolt will be going into a 1/4” hole. If the fit has interference it is
advisable to slightly clear the hole with the corresponding drill bit. Do not “thread” the bolt into a
drilled hole. Do not HAMMER, BEAT, JAM or any other means of force on a bolt through a hole.
Above applies to all hole sizes.
PART ASSEMBLY
Allowing manufacturing tolerances, it is on occasion whereas the bolt will not
easily go thru both parts. If the fit between the two parts has interference, it is advisable to slightly
clear the hole with the corresponding drill bit. Do not “thread” the bolt into the interference. Do
not HAMMER, BEAT, JAM or any other means of force on a bolt through the fittings.
Section 1
7
Air-Tech, Inc
Summary of Contents for MAX Sprint
Page 1: ...ASSEMBLY MANUAL AIRFRAME KIT 99110 S ___DATE__ __j_ DOC 872 01 AT...
Page 4: ......
Page 9: ...AN4 26a 10240 LEFT SIDE ASSEMBLY SHOWN REPEAT FOR RIGHT SIDE 1 1 2...
Page 10: ...BLANK PAGE 6 3b Section 4 6 Air Tech Inc...
Page 14: ...RIBS 40169 WITH VELCRO IN SECTION 12 WING TIP NOTICE...
Page 19: ...Section 4 15 Air Tech Inc...
Page 21: ...BLANK PAGE 6 3b Section 4 17 Air Tech Inc...
Page 44: ...40333 Section 2 2 Air Tech Inc...
Page 45: ...RUDDER COVER AND RUDDER LEADING EDGE Section 2 3 Air Tech Inc...
Page 46: ...RUDDER LEADING EDGE AND CONTROL ARM Section 2 4 Air Tech Inc...
Page 47: ...RUDDER LEADING EDGE AND CONTROL ARM Section 2 5 Air Tech Inc...
Page 48: ...3 Section 2 6 Air Tech Inc...
Page 49: ...Section 2 7 Air Tech Inc...
Page 50: ...Section 2 8 Air Tech Inc...
Page 51: ...RUDDER BALANCE STRUT Section 2 9 Air Tech Inc...
Page 52: ...Section 2 10 Air Tech Inc...
Page 53: ...RUDDER HINGE BOLT Section 2 11 Air Tech Inc...
Page 54: ...BLANK PAGE Section 2 12 Air Tech Inc...
Page 56: ...40275 Section 2 14 Air Tech Inc...
Page 57: ...STABILIZER LEADING EDGE ASSEMBLY Section 2 15 Air Tech Inc...
Page 61: ...BLANK PAGE Section 2 19 Air Tech Inc...
Page 66: ...Section 3 3 Air Tech Inc...
Page 68: ...Section 5 2 Air Tech Inc...
Page 69: ...Section 5 3 Air Tech Inc...
Page 70: ...Section 5 4 Air Tech Inc...
Page 71: ...Section 5 5 Air Tech Inc...
Page 72: ...YOU TUBE SEARCH QUICKSILVER AILERON INSTALL Section 5 6 Air Tech Inc...
Page 73: ...Section 5 7 Air Tech Inc...
Page 76: ...F O R W A R D TRIKE GENERAL ARRANGEMENT Section 6 3 Air Tech Inc...
Page 77: ...BLANK PAGE 6 3b Section 6 4 Air Tech Inc...
Page 81: ...6 7 Section 6 8 Air Tech Inc...
Page 84: ...RIGHT SIDE SHOWN Section 6 11 Air Tech Inc...
Page 86: ...Section 6 13 Air Tech Inc...
Page 89: ...Drill to 5 16 Section 8 2 Air Tech Inc...
Page 91: ...SEAT MOUNT ASSEMBLY AN4 17a 10150 2 places rear AN4 15a 10120 Section 8 4 Air Tech Inc...
Page 92: ...0 0 Section 8 5 Air Tech Inc...
Page 93: ...VERTICAL 91111 Control Cable 70389 AILERON CONTROL CABLE GUARD ATTACH 40337...
Page 94: ......
Page 95: ...10045 AN3 16a 4...
Page 97: ...22 1 4 to aft end of tube Section 8 10 Air Tech Inc...
Page 102: ...KING POST ASSEMBLY FWD King Post 40205 Section 9 3 Air Tech Inc...
Page 109: ...TOP VIEW Section 10 4 Air Tech Inc...
Page 110: ...Section 10 5 Air Tech Inc...
Page 113: ...Section 10 8 Air Tech Inc...