E1. AV-8 Crash Dollies Wing Horizontal Stab Vert Stab.pdf
PDF 4 MB Posted
- Solicitation number
- M0026426Q0130
- Issued by
-
United States Marine Corps
About this file
This document is a technical instruction manual with photographs for the assembly, installation, and transportation of AV-8B aircraft components, specifically the wing fixture and fuselage dolly used for crash testing and shipping operations.
The manual provides detailed photographic guidance for installing the wing, horizontal stabilizer, and vertical stabilizer onto the AV-8 wing dolly fixture. Key assembly procedures include: checking the stand for four wing mount bolts, one vertical stab bolt, and one horizontal stab link or hook; installing the horizontal stabilizer first with minimum four personnel to prevent damage; rotating the stab tip downward and rolling the rail into the stand with adjustments as needed; securing the horizontal stabilizer with a tie-down hook and turnbuckle; installing the vertical stabilizer rudder-down with Door 81 removed, requiring multiple personnel to prevent damage; and securing with a vertical stab bolt only after the rail is rolled into the stand. For wing installation, the manual specifies using either a CFR crane or Cobra crane, raising the wing platform past level to allow support braces to swing up, installing aft bolts first then forward bolts with some lateral movement required, sealing fuel lines prior to lowering to vertical position, using rubber pads or mats to protect from chain damage, and employing proper personnel positioning with a supervisor and personnel monitoring attach points. The fuselage dolly section addresses positioning the dolly with the wide end forward and anti-collision cutout to the rear, balancing fuselage weight with ten bags of Speedy Dry or sand plus 500 pounds of water when the engine is installed, using straps to control swinging and maintain level aircraft, employing proper personnel positioning during hoisting, ensuring all sling pins are installed and plungers locked (twelve total), verifying fuselage configuration matches sling position, centering crane cable, positioning speed brakes in retracted position, double-checking all safety areas before lifting, removing jacks immediately after fuselage height permits, backing the truck into position, using Speedy Dry bags under the nose for protection, positioning personnel at cradling points during fuselage placement, ensuring fasteners are flush to prevent panel damage, and confirming proper anti-collision light and lids fence positioning in their cutouts before securing for transport.
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Text version
AV-8 Wing Dolly Fixture
Wing, Horiz Stab, & Vert Stab installation photos with notes
REQUIRED SUPPORT EQUIPMENT FOR TRUCKING AV-8B
PETTIBONE CRANE (FOR LIFTING FUSELAGE W/ ENGINE)
WING/ENGINE FUSELAGE BEAM SLING (#75D110047-1001)
FUSELAGE SLING HOISTING ADAPTER (#75D110054-1001)
3EA AIRCRAFT JACKS
1EA WING STAND
1EA HYDRAULIC TEST STAND
AV-8B CRASH FIXTURES (Wing Fixture & Fuselage Dolly) 1EA LARGE FORKLIFT (For Loading / Unloading crash Fixtures)
REQUIRED ITEMS TO BE REMOVED FOR TRUCKING
A/C MUST BE DISARMED (SEAT/CANOPY CADS, BLOWDOWN BOTTLE CAD)
FUSELAGE STRAKES
CENTERLINE PYLON
WLG FAIRINGS
WLG STRUTS
HORIZONTAL STABILIZER
VERTICAL STABILIZER
IMPORTANT: Ensure all lines, hoses, and connectors are properly capped, plugged, and secured for transporting aircraft. The windscreen and canopy should have barrier paper applied to protect them from damage.
On the fuselage sling, you must verify that all pins are installed and the plungers are locked.
Total of 12 pins.
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File details come from the government source that posted it. Updated .