Executive Virtual Assistant - with Excellent English Skills Wanted!

We are looking to expand our team! We are looking for a Virtual Assistant who can help with various technical tasks on demand.
We specialize in Engineering support and often we deal with technical information that is more complex, so a thorough understanding of English is required. In addition, frequent communication is not only important to our management but is required, so mastery of English is imperative. Previous engineering experience is a plus but NOT required.
MUST have mastery with Microsoft Word and Excel. You must be able to format a table of contents so that the page numbers automatically update.
This current job is freelance only, but our teaUpgrade to see actual infombers usually work an average of 10 to 20 hours a week, sometimes more during a high load time. At other times there may not be any work for several weeks.
The qualities you will need are:
- Outstanding attention to detail
- Strong communication skills
- Good time management skills
- Excellent proofreading, formatting, and English review skills.
- Thorough understanding of Microsoft Office and Google Drive document editing suites
- Training will be available where required, but ideally, you will be able to work confidently on your own

NOTE: Details are important in this job. Please follow the instructions below CAREFULLY and to the best of your ability. The total time to complete should take about 20 minutes. Failure to follow these instructions precisely will immediately result in a failed application.
1) If interested, please put in the subject: "ASESVA - Job Application – Formatted WORD document link INCLUDED" so I can be sure you have read and understood the job description.
2) Demonstrate your proficiency with Microsoft Word by formatting the unformatted sample text provided into a structured Word document. Your document must include:
• An automatic Table of Contents (TOC) generated exclusively using Microsoft Word’s native Table of Contents feature.
• Clearly structured headings and subheadings formatted using paragraph numbering style headings (e.g., 1.0, 1.1, 1.1.1, 1.1.1.1, etc.).
• Logical organization based on your interpretation of the technical content provided. You must read and comprehend the passage thoroughly to determine an appropriate heading hierarchy.
• A professional and visually appealing layout suitable for delivery to a customer, emphasizing clarity, readability, and consistency in formatting.
• Ensure the Table of Contents updates automatically when any headings or subheadings are modified.
3) In your application, include a download link to this formatted Microsoft Word document.
4) Finally, be sure to include a link to your resume and/or onlinejobs.ph profile.

Below is the unformatted text for you to format
=============================================================
PROVISIONING PARTS LIST FOR THE AUXILIARY EQUIPMENT SYSTEM
Scope. This report presents the Provisioning Parts List (PPL) for an auxiliary equipment system designed for use on a designated military helicopter platform. It has been prepared in accordance with the applicable Subcontract Data Requirement List (SDRL) and Statement of Work. This report was developed following guidelines from MIL-STDUpgrade to see actual infoB, DOD Requirements for a Logistic Support Analysis Record, and DOD 4100.38 M, Department of Defense Provisioning and Other Procurement Screening Manual.

Purpose. This report provides the PPL associated with the auxiliary equipment system installed on the specified military helicopter. The data elements listed for each part conform to the requirements detailed in the Statement of Work, referencing the applicable Data Element Descriptions (DED) as outlined in MIL-STDUpgrade to see actual infoB. The provisioning list includes common hardware components, bulk items, and specialized tools necessary for system operation and maintenance.

Hardware Configurations and Revisions. This report addresses the hardware configuration of the auxiliary equipment system as it existed on the date indicated on the report cover or latest revision page. Pending or subsequent design modifications after this date are not included within the scope of this document. Future changes to the equipment configuration will be evaluated regarding reliability impacts and appropriately documented in subsequent revisions.

AUXILIARY EQUIPMENT SYSTEM DESCRIPTION.
System Description Overview. The auxiliary equipment system described in this report is configured for internal installation in the designated military helicopter. It is designed to be crash-resistant and meets all necessary operational requirements for integration into the helicopter. The system is installed within the helicopter cabin, providing a safe and effective method for enhancing the helicopter's operational capabilities.

The system securely attaches to the cabin floor utilizing a restraint frame combined with a specialized arrangement of securing straps and tensioning mechanisms, ensuring stability under various operational conditions.

Designed for flexibility, this auxiliary equipment is configured as a removable hardware assembly. Operators can install or remove the equipment within a short period, depending on mission-specific needs. Importantly, installation does not require structural alterations to the helicopter's airframe or cabin.

Operation of the auxiliary equipment system is controlled by the operator via cockpit-mounted controls. With the system activated, electrical power from the helicopter energizes internal components to facilitate proper operation. Real-time measurement data from the system is transmitted to cockpit instrumentation through integrated sensors, providing operators with accurate status information during operation.

General Description of Major Components.
System Assembly. Each auxiliary system assembly comprises an outer container, an internal protective liner, and a central support assembly. The container houses the liner and the central support assembly, with dimensions designed for optimal integration within the helicopter cabin. Multiple identical system assemblies may be interconnected to form the complete system installation.

Outer Container. The outer container is constructed of an aluminum material, providing structural integrity and protection for the internal components. It includes an opening for the installation of the central support assembly. A built-in mechanism integrated into the container prevents the accumulation of debris between internal components. Carrying handles attached externally to the sides facilitate safe handling by multiple personnel. The system is engineered to withstand significant crash-related stresses without compromising structural integrity or cabin attachment.

Internal Liner. The internal liner, installed within the outer container, consists of a reinforced, flexible material designed for crash-resistance in compliance with relevant aviation safety regulations. An opening in the liner aligns with the corresponding opening in the outer container to accommodate the central support assembly.

Central Support Assembly. The central support assembly includes a cover plate secured to an internal mounting structure. The assembly provides simplified maintenance access to internal components. Integrated components within the assembly include:
A crashworthy part meeting relevant military safety standards.

Internal parts with protective parts compliant with applicable military specifications.

Indicator components and integrated sensors for accurate system monitoring.

A set of mechanisms supporting safe and controlled system operation.

Switches and associated level sensors.

Internal wiring and breakaway couplings for electrical and physical safety.

Air Handling Assemblies. Air handling assemblies provide connection between the system and the aircraft’s main interfaces. These assemblies support safe system integration and help regulate airflow during normal operation and system servicing.

Cable Assemblies. The system utilizes cable assemblies to connect to aircraft power sources and cockpit instrumentation. The first cable assembly supplies operational power and relays system status information to the cockpit. The second cable assembly provides power distribution to internal components and transmits sensor feedback to ensure continuous monitoring and control of system functions.