Blade trimmer tool
$1553
Blade trimmer tool
Available on back-order
The 56-9918-00 is the dedicated fixture used to bend main rotor blade trim tabs while adjusting blade coning. The Mi-8AMT maintenance manual describes it in section 012.10.00 and illustrates the tool in Figure 60. A specialist product catalog also records the newer reference NVKV.303674.001 for the same tool type.
The fixture has only two principal elements: a bracket and a handle. The bracket is made from 30KhGSA steel, is 400 mm long and contains a deep groove lined with protective fabric. The handle is manufactured from 20 × 18 mm steel tube and is attached to the bracket. This simple construction is application-specific and should not be replaced by an improvised lever.
For use, the tool is placed over the trim tab until it reaches the stop. The technician then applies a smooth force to the handle to bend the tab in the required direction. The manual links this operation to main rotor blade coning adjustment, so the amount and direction of correction must come from the approved rotor tracking procedure rather than from the tool itself.
The tool does not measure blade track and does not establish the required correction. It provides controlled mechanical leverage after the maintenance result has been evaluated with the appropriate tracking equipment. Excessive or abrupt loading can damage the trim tab or blade structure, which is why the procedure specifically calls for smooth force.
Aircraft-family reference: Mil Mi-8. This external reference does not replace the approved maintenance manual.
The primary manual gives a mass of 0.7 kg. This corrects the earlier generalized value of 0.8 kg on the product page. Search forms 56.9918.00 and 56 9918 00 are included as alternative punctuation, while NVKV.303674.001 is recorded as a documented newer designation. None of these forms should be treated as proof of interchangeability without dimensional confirmation.
Before use, inspect the bracket for deformation, cracks and damaged protective lining. Check the handle attachment and ensure the groove is clean so that the trim tab surface is not scored. Because no independently verified product photograph was found, the gallery uses the exact maintenance-manual illustration instead of an invented or visually similar image.
This card retains the existing price and Pre-Order status. Condition is recorded as New, Warranty as 6 Months and YOM as 2026. The estimated lead time remains 90–120 days subject to confirmation. The supplied tool should be checked against the drawing, dimensional requirements and any passport or inspection record included with the delivery.
An inquiry should identify the helicopter modification, quantity and required documentation. Other Mi-8 / Mi-17 ground tools linked from this page are related only through the maintenance category. They are not substitutes for the 56-9918-00 fixture and must not be used to bend rotor-blade trim tabs unless their approved documentation explicitly permits it.
More items are available in the Ground Support Equipment category.
Related products in this batch: 246-9977-00, 8AT-9907-00, 8A-9901-00/A, 8MT-9925-00. They belong to the same ground-support category but are not interchangeable.
Product Type: Main rotor blade trimmer bending tool / trim-tab bending fixture
Designation: 56-9918-00
Alternative Designations: 56.9918.00; 56 9918 00; NVKV.303674.001; НВКВ.303674.001
Function: Bending main rotor blade trim tabs during blade coning adjustment
Application / Where Used: Mi-8AMT main rotor maintenance; Mi-8 family maintenance tooling where specified by documentation
Construction: Bracket and handle
Bracket Material: 30KhGSA steel
Bracket Length: 400 mm
Bracket Groove: Deep groove lined with protective fabric
Handle: Steel tube 20 × 18 mm attached to the bracket
Operating Method: The tool is placed fully onto the trim tab and smooth force is applied to the handle
Mass: 0.7 kg
Estimated Lead Time: 90–120 days, subject to confirmation
Technical Documentation: Mi-8AMT Maintenance Manual, section 012.10.00, item 2.6.19, Figure 60
All shipments are carried out from our international warehouse in Dubai (UAE), as well as from our partners’ remote warehouses.
In Stock — items available in stock at the Dubai warehouse are dispatched within 5–10 business days after receiving 100% prepayment.
Remote Stock — items available at our partners’ remote warehouses are supplied within an average of 30–45 business days after receiving 100% prepayment.
Pre-Order — made-to-order products are manufactured and delivered within an average of 45–60 business days. Payment terms: 50% advance payment to start production, with the remaining 50% paid before dispatch from the Dubai warehouse after full readiness for shipment.
Returns & Changes (Restocking Fee)
For selected items, a RESTOCKING FEE of 10% may apply in case of return, order cancellation, or changes to the order specifications. This condition applies only to certain products and is confirmed at the order approval stage.
Warranty
All products are covered by a standard 6-month warranty.
Extended warranty is available upon request and is agreed individually; it may affect the final product price.
The 56-9918-00 is the dedicated fixture used to bend main rotor blade trim tabs while adjusting blade coning. The Mi-8AMT maintenance manual describes it in section 012.10.00 and illustrates the tool in Figure 60. A specialist product catalog also records the newer reference NVKV.303674.001 for the same tool type.
The fixture has only two principal elements: a bracket and a handle. The bracket is made from 30KhGSA steel, is 400 mm long and contains a deep groove lined with protective fabric. The handle is manufactured from 20 × 18 mm steel tube and is attached to the bracket. This simple construction is application-specific and should not be replaced by an improvised lever.
For use, the tool is placed over the trim tab until it reaches the stop. The technician then applies a smooth force to the handle to bend the tab in the required direction. The manual links this operation to main rotor blade coning adjustment, so the amount and direction of correction must come from the approved rotor tracking procedure rather than from the tool itself.
The tool does not measure blade track and does not establish the required correction. It provides controlled mechanical leverage after the maintenance result has been evaluated with the appropriate tracking equipment. Excessive or abrupt loading can damage the trim tab or blade structure, which is why the procedure specifically calls for smooth force.
Aircraft-family reference: Mil Mi-8. This external reference does not replace the approved maintenance manual.
The primary manual gives a mass of 0.7 kg. This corrects the earlier generalized value of 0.8 kg on the product page. Search forms 56.9918.00 and 56 9918 00 are included as alternative punctuation, while NVKV.303674.001 is recorded as a documented newer designation. None of these forms should be treated as proof of interchangeability without dimensional confirmation.
Before use, inspect the bracket for deformation, cracks and damaged protective lining. Check the handle attachment and ensure the groove is clean so that the trim tab surface is not scored. Because no independently verified product photograph was found, the gallery uses the exact maintenance-manual illustration instead of an invented or visually similar image.
This card retains the existing price and Pre-Order status. Condition is recorded as New, Warranty as 6 Months and YOM as 2026. The estimated lead time remains 90–120 days subject to confirmation. The supplied tool should be checked against the drawing, dimensional requirements and any passport or inspection record included with the delivery.
An inquiry should identify the helicopter modification, quantity and required documentation. Other Mi-8 / Mi-17 ground tools linked from this page are related only through the maintenance category. They are not substitutes for the 56-9918-00 fixture and must not be used to bend rotor-blade trim tabs unless their approved documentation explicitly permits it.
More items are available in the Ground Support Equipment category.
Related products in this batch: 246-9977-00, 8AT-9907-00, 8A-9901-00/A, 8MT-9925-00. They belong to the same ground-support category but are not interchangeable.
Product Type: Main rotor blade trimmer bending tool / trim-tab bending fixture
Designation: 56-9918-00
Alternative Designations: 56.9918.00; 56 9918 00; NVKV.303674.001; НВКВ.303674.001
Function: Bending main rotor blade trim tabs during blade coning adjustment
Application / Where Used: Mi-8AMT main rotor maintenance; Mi-8 family maintenance tooling where specified by documentation
Construction: Bracket and handle
Bracket Material: 30KhGSA steel
Bracket Length: 400 mm
Bracket Groove: Deep groove lined with protective fabric
Handle: Steel tube 20 × 18 mm attached to the bracket
Operating Method: The tool is placed fully onto the trim tab and smooth force is applied to the handle
Mass: 0.7 kg
Estimated Lead Time: 90–120 days, subject to confirmation
Technical Documentation: Mi-8AMT Maintenance Manual, section 012.10.00, item 2.6.19, Figure 60
All shipments are carried out from our international warehouse in Dubai (UAE), as well as from our partners’ remote warehouses.
In Stock — items available in stock at the Dubai warehouse are dispatched within 5–10 business days after receiving 100% prepayment.
Remote Stock — items available at our partners’ remote warehouses are supplied within an average of 30–45 business days after receiving 100% prepayment.
Pre-Order — made-to-order products are manufactured and delivered within an average of 45–60 business days. Payment terms: 50% advance payment to start production, with the remaining 50% paid before dispatch from the Dubai warehouse after full readiness for shipment.
Returns & Changes (Restocking Fee)
For selected items, a RESTOCKING FEE of 10% may apply in case of return, order cancellation, or changes to the order specifications. This condition applies only to certain products and is confirmed at the order approval stage.
Warranty
All products are covered by a standard 6-month warranty.
Extended warranty is available upon request and is agreed individually; it may affect the final product price.