Page
81
Section 29
Maintenance & Inspection
Dragonfly 582/912
PARACHUTE & ELT MOUNTING
STEP
INSTRUCTIONS
for Assembly, for Disassembly reverse the order!
PART NO.
STAGE CERT.
1
Set Second Chantz 1100 lb. Parachute on root tube, mark holes
Loose.
2
Slide parachute mount assembly onto top of root tube as shown ( 1” space
between Parachute and Gap Seal.) and Mark holes both sides. Remove
Parachute and Drill 2 each 3/16” holes through root tube aligned with
parachute flange holes.
3
Replace parachute and Bolt AN3-26A or AN3-25A , 3/16” washer, parachute
mount bracket, 3/16” washer, AN half nut.
Snug.
4
Install ELT in Bracket. Bracket should have been installed in Section 16
Wing
Attach w/ 3/16” Stainless Broad Head Pop Rivets ½” Grip w/ Plastic Saddles
behind plate to hold securely. Or if they become loose, replace w/ AN23-25
Clevis Bolts by drilling all the way through tube.
NOTE: Insure ELT
Locking Band is in place (buckle up) prior too Riveting.
(1)
Recommended Special Tools:
None
(2)
The parts needed to perform the task:
Replace worn/damaged parts as needed, listed above. Max. Wear (defined 1.1.8.1)
(3)
Type of maintenance:
Inspection=Line & Replacement=Heavy
(when it involves replacement of structural components.) &
Parachute Components.
(4)
Certification needed to accomplish the task:
Line=LSRI Inspection or above, Heavy=LSRM Maintenance or above.
see:
3 Level of Certification in this manual
(5)
Detailed instructions and diagrams as needed to perform the task, listed above and adjacent page.
Every Annual or 100 Hrs., Inspect for Cracks, Corrosion, Elongation of holes & Fasteners for Wear & Security.
Inspect and maintain BRS & bridals in accordance with manufacturer’s instructions.
ELT Mount located on the front top of Left Wing Inboard Compression Strut.
NOTE: ELT must be inspected every 12 calendar months in accordance with FAR 91.207 (d)
Battery Replacement
Regulations require ELT batteries to be replaced after one hour of operation or after 50 percent of the battery's useful life. The
one-hour usage requirement is cumulative--if the ELT is used two times for half an hour each, then the transmitter has been used
for a cumulative total of one hour and the battery must be replaced. Battery useful life, for the purpose of battery replacement, is
determined by the battery manufacturer. The date of the next required battery replacement must be marked on the ELT and in the
aircraft records.
Common Exceptions
The most common exceptions to the ELT requirements are for aircraft used in training within a 50-mile radius of their base of
operations, aircraft used in aerial application (crop-dusters) and aircraft undergoing certification testing. Additionally, an
exception is made for operation of an aircraft while the ELT is removed for service or replacement; the aircraft may then be
operated without an ELT, providing appropriate entries have been made in the aircraft records and the aircraft is placarded noting
that the ELT is not installed. This exception for operation during periods of service or replacement is only applicable for up to 90
days from the date the transmitter was removed for the aircraft.
(6)
Method to test/inspect to verify the task was accomplished properly.
Insure that all procedures were followed correctly
and there is proper non-binding movement to moving parts and that fasteners were tightened as instructed. When flight
controls are involved, assure that they are operating properly.
Section 29 Parachute & ELT Mounting
Section 29
Summary of Contents for 912 Dragonfly
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Page 37: ...Page 36 Note for Hydraulic Brakes see Appendix B Drawing 7 ...
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Page 79: ...Page 78 Wiring1 jpg Drawing 28a ...
Page 80: ...Page 79 Wiring2 jpg Drawing 28b ...
Page 81: ...Page 80 elecLights jpg Drawing 28c ...
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Page 92: ...Page 91 Appendix B Brakes Manual for BX1320 BX1000 Appendix B Page 1 ...
Page 93: ...Page 92 Appendix B Page 2 ...
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Page 104: ...Page 103 Figure 1a Description of Display Pages ...
Page 105: ...Page 104 Figure 1b Description of Display Pages ...
Page 138: ...Page 137 Appendix C EIS 4000 912 914 ...
Page 139: ...Page 138 Appendix C EIS 4000 912 914 ...
Page 140: ...Page 139 Appendix C EIS 4000 912 914 ...
Page 141: ...Page 140 Appendix C EIS 4000 912 914 End Appendix C ...
Page 155: ...Page 154 Appendix E2 Powerfin Prop Page 2 ...
Page 156: ...Page 155 Appendix E2 Powerfin Prop Page 3 ...
Page 157: ...Page 156 Appendix E2 Powerfin Prop Page 4 ...
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Page 159: ...Page 158 Appendix E2 Powerfin Prop Page 6 ...
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Page 164: ...Page 163 Appendix E2 Powerfin Prop Page 11 End of Appendix E2 ...
Page 187: ...Page 186 By Memphis Soaring FIGURE 3 Common Signals ...