Revised ROU Boot StF Test Plan v1.pdf
PDF 298 KB Posted
- Attached to
- USAF Safe-to-fly Boot Program
- Solicitation number
- AFLCMC-ROUK-26-0005
About this file
Safe-to-Fly (StF) Test Plan for Commercial and Government Off-the-Shelf (COTS, GOTS) Boots
This memorandum from the Air Force Life Cycle Management Center (AFLCMC) establishes the certification requirements and testing standards for boots worn by Air Force aircrew to qualify as Safe-to-Fly (StF). The document specifies that all test data and results supporting COTS StF determinations must be dated within one year of submission. The Air Force recognizes that NSN boots managed by the Defense Logistics Agency (DLA) may be designated AF StF following review of technical requirements in applicable Purchase Descriptions (PD) or Military Specifications (MILSPEC) and StF determination by the Aircrew Performance Materiel Leader or appropriately delegated authority.
StF boots must comply with multiple dimensional and performance requirements, including maximum length of 16 inches, height of 11.5 inches, and width of 5.5 inches (for the largest size/width specified). Boot heights are gender-specific: female boots must measure 9-¾ ± ½ inches on size 10RF and male boots 10 ± ½ inches on size 10R, graduating up and down between sizes. Approved colors are Coyote (498), Legacy Sage Green (1641), Desert Tan (499), or Black, with other colors requiring Aircrew Performance Material Leader approval. Boots must meet flame resistance per NFPA 1971 Test Four, thermal conductive heat resistance per NFPA 1971 Tests One and Two, water resistance per AATCC 127, and safety toe compliance with ASTM F2412 and F2413 (Impact I/75, Compression C/75, and Electrical Hazard EH) if equipped. The document categorizes boots by temperature range—hot weather (>70°F), temperate weather (≥32°F to 70°F), cold weather (-20° to 32°F), and extreme cold weather (-20°F to -49°F or below)—each with specific associated specifications and additional requirements such as slip testing and rubber outsole cold flex testing. Manufacturers must identify Berry Amendment (10 U.S.C 2533a) compliance, and after initial or subsequent three-year StF approval, vendors may submit a memo stating the boot model has not changed in materials or processing practices rather than resubmitting full testing data, unless field discrepancies are identified. Approved StF boots receive three-year certification, with the contact point for questions being Mr. Don Fleury at (508) 206-3071 or donald.f.fleury.civ@army.mil.
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| File | Type | Posted |
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| USAF Safe to fly Boots RFI v2.pdf | ||
| dafi36-2903 Feb 2026.pdf |
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Text version
DEPARTMENT OF THE AIR FORCE
AIR FORCE LIFE CYCLE MANAGEMENT CENTER
WRIGHT-PATTERSON AIR FORCE BASE OHIO
MEMORANDUM FOR RECORD
FROM: AFLCMC/ROU
Human Systems Program Office 1981 Monahan Way Wright-Patterson AFB, OH 45433
SUBJECT: Safe-to-Fly (StF) Test Plan for Commercial and Government Off-the-Shelf (COTS, GOTS) Boots
1. The purpose of this Test Plan is the certification of boots worn by Air Force (AF) aircrew as Safe-to-Fly (StF). Any application of the below test methods to articles, not readily identified as footwear for AF use, is in violation of its designated use. If applied to articles not readily identified as footwear, all risks and consequences associated with its use in the environment become the responsibility of the individual user(s). All test data and results provided to support COTS StF determinations shall be within one year from the date of submission.
2. StF Definition. AF StF boots must conform, at a minimum, to the following:
Note: NSN boots managed by the Defense Logistics Agency (DLA), including those for other services, can be designated AF StF after a review of the technical requirements in the associated Purchase Description (PD) or Military Specification (MILSPEC) and a StF determination made by the Aircrew Performance Materiel Leader, equivalent, or appropriately delegated authority.
a. Footwear (boots) shall abide by the following dimensions for the largest size/width called out in the cited specification or PDs (e.g. Men’s 16 EEEE or Women’s 11 EE):
(1) Length: less than or equal to 16 inches
(2) Height: less than or equal to 11.5 inches
(3) Width: less than or equal to 5.5 inches
Note: Items measuring outside of these dimensions shall be addressed on a case-by-case basis by the Human Systems Division Program Office (AFLCMC/ROU) and the Aircrew Performance Material Leader, equivalent or appropriately delegated authority.
b. Boot Height.
(1) Female: The height of the finished boot, measured from the bottom of the heel tread to the top of the back of the boot, shall be 9-¾ ± ½ inches on size 10RF and shall graduate up and down between sizes and widths.
(2) Male: The height of the finished boot, measured from the bottom of the heel tread to the top of the back of the boot, shall be 10 ± ½ inches on size 10 R and shall graduate up and down between sizes and widths.
c. Boot color is primarily Coyote (498), Legacy Sage Green (1641), Desert Tan (499), or
Black; other colors/shades may be allowed by specific approval of the Aircrew Performance Material Leader, equivalent or appropriately delegated authority as required and/or requested.
d. Construction methods include the “Sidewall” or “Cup” construction method along with the Direct Molded System (DMS), Welt, Stitch-down, and Injected molded construction processes. Maximum dimensioning in paragraph 2 above must not be exceeded. Other constructions may be allowed, if appropriate, after being addressed by the Aircrew Performance Material Leader, equivalent or appropriately delegated authority.
e. Flame resistance. The boots shall meet the Flame Resistance Test Four requirements of NFPA 1971, Standard on Protective Ensemble for Structural Firefighting (2007 Edition).
The areas of the boot to be tested are in accordance with Figure 8-5.5.2 of NFPA 1971;
however, a sixth area is added to include the nylon quarter side panels. The requirement that the boot shall not melt, or drip does not apply, although the boot shall not exhibit any burn-through (Reference: Sections 7-10.1 and 8.5.5). The boot shall be considered to have failed the burn-through test when burn-through is observed through all layers of the quarter panel and lining components. The rubber outsole is not subject to the flame resistance requirements.
f. Upper heat resistance. The boots shall meet the Thermal Conductive Heat Resistance
Test One requirements of NFPA 1971, Standard on Protective Ensemble for Structural Firefighting, 2007 Edition (NFPA 1971, Section 8-7).
g. Sole heat resistance. The boots shall meet the Thermal Conductive Heat Resistance
Test Two requirements of the NFPA 1971, Standard on Protective Ensemble for Structural Firefighting, 2007 Edition (NFPA 1971, Section 8-8).
h. Water Resistance. The boots shall be tested for their resistance to rain or water spray in accordance with AATCC 127 Water Resistance: Hydrostatic Pressure Testing.
i. Safety Toe options, steel or composite, are allowed in any boot otherwise authorized StF. Compliance with ASTM F2412 and ASTM F2413 Impact (I/75), Compression (C/75), and Electrical Hazard (EH) is required. Maximum dimensioning in paragraph 2 above must not be exceeded.
3. Type Boot temperature ranges and some associated specifications (MILSPEC and PD) are:
a. Hot weather (>70ºF): StF boots shall comply with the requirements listed in paragraphs 1 and 2, above, and conform to either PD-WNUV-11-01 - HW, ST, (BOOT, HOT WEATHER, INDUSTRIAL) or GL-PD-09-02 - HW, FR, (BOOTS, COMBAT, HOT WEATHER - FLAME RESISTANT) with, or without, a Safety-Toe option. They will not require waterproofing, only water resistance (AATCC TM-22).
b. Temperate Weather (≥ 32ºF to 70ºF): StF boots shall comply with the requirements listed in paragraphs 1 and 2, above, and conform to the tests as described in Purchase Descriptions PD 77AESG-06-01A or PD 77AESG-06-03A, as appropriate, with or without a Safety-Toe option.
c. Intermediate Cold/Wet Weather (14ºF to 32ºF): No StF boots have been AF certified in this specific temperature range.
d. Cold weather (-20º to 32ºF) or Extreme Cold weather (-20ºF to -49ºF, or below): StF boots shall comply with the requirements of WNU 99 PD 17007, Service Boots, Cold Weather or GL-PD-19-03A, Boot, Combat, Cold Weather.
Note: The amount and type of insulation used, will be stated by the vendor/manufacturer.
The “clo” (average insulation) value (ASTM C518 Standard Test Method for Steady State Thermal Transmission Properties by Means of the Heat Flow Meter Apparatus) for the type and amount of insulation used will be determined and reported by the vendor/manufacturer.
The whole boot clo tested on a thermal instrumented foot model in accordance with ASTM F1291 Standard Test Method for Measuring the Thermal Insulation of Clothing Using a Heated Manikin, will be reported by the vendor/manufacturer, if determined. Government testing and analysis may be required to determine, or verify, the prediction modeling temperature/time ranges to frostbite for the candidate boots.
e. Cold Weather and Extreme Cold Weather boots may be required to meet, or exceed, any of the requirements for Slip testing in accordance with SATRA Method TM 144. The minimum Coefficient of Friction (CoF) performance required for the below listed surface conditions shall be:
Normal cold weather outer sole boots: Area CoF Wing surface (Hydraulic mode) Flat 0.24 Rough Ice surface (Frost mode) Heel 0.09 Quarry Tile (Wet mode) Forepart 0.58 Polycoated Concrete (5% Sodium Laural Sulphate (NaLS) in H20
Heel 0.02
Anti-Slip, cold weather outer-sole boots: Area CoF Wing surface (Hydraulic mode) Flat 0.24
Forepart 0.24 Rough Ice surface (Frost mode) Heel 0.17
Forepart 0.24 Quarry Tile (Wet mode) Polycoated Concrete (5% Sodium Laural Sulphate (NaLS) in H20
Forepart 0.61 Heel 0.24
j. Rubber outsoles shall be tested for Cold Flex (@-23° C) and meet requirement of 500%
@ 7,500 flexes when tested in accordance with ASTM D-1052 Test Method for measuring Rubber Deterioration – Cut Growth Using Ross Flexing Apparatus.
4. Certificate of Compliance (C of C) from a manufacturer’s vendor certifying whole-boot, components, and/or materials meet a PD or MIL-SPEC requirement, in lieu of a specific test report, may be submitted for consideration for acceptance depending on the intended use and established requirements for each boot type. Data supporting the C of C may be requested.
5. The manufacturer shall identify whether the boot model/style submitted for certification meets Berry Amendment (10 U.S.C 2533a) criteria. Only Berry Amendment compliant materials/capabilities or Berry waivered materials may be submitted for consideration for acceptance.
6. After the initial, or subsequent three-year StF approval, and at the discretion of the Senior Material Leader representative, vendors may submit a memo stating the boot make/model has not changed in materials, nor processing practices, and is still fully Berry Amendment compliant. Reasons for requiring a full StF submission, with sample boots and all required testing data, versus a memo, are noted discrepancies from the field or other noted or reported discrepancies with the materials and/or processing practices for the boot.
7. This document supersedes all previous versions of this boot StF plan, specifically, AFLCMC/WNU Safe-to-Fly Test Plan for boots, dated 1 August 2022.
8. The Aircrew Performance Material Lead Engineer POC for this StF plan is Mr. Don Fleury at (508) 206-3071 or donald.f.fleury.civ@army.mil.
NICHOLE TAYLOR, NH-04, DAF
Chief Engineer, Human Systems Division AFPEO Combat Readiness
Attachment:
ROU Process for StF Boots mailto:donald.f.fleury.civ@army.mil
Attachment ROU Process for StF COTS Boots
The ROU process for StF COTS boots is outlined in the graphic below. Vendors provide data and boot samples at their convenience. The data (not older than 1-year from submission date) is reviewed and compared to the StF requirements by the assigned engineer(s). A package is prepared that establishes the boots meet all required StF criteria as outlined in the StF plan and coordinated for review and approval. The package includes a boot StF checklist (detailing the requirements and referencing the testing results), testing/pass/fail results, a MAJCOM StF boot memo, a Vendor StF boot memo and a revised AF StF boot list memo.
A vendor StF letter (cc AAFES) is prepared for each specific manufacturer model/style for a three-year period. Multiple boot model/styles may be included in a single memo. The revised StF list is attached to the MAJCOM letter and uploaded on various Aircrew Flight Equipment (AFE) sites. The letters are signed by the Chief of Human System Division or designated representative. Once the package is approved, signed/dated letters are sent to the manufacturer indicating the specific commercial boot style(s) is approved as StF for three years. Note the vendor letter includes a statement to the effect that any material or manufacturing changes will void the StF approval unless the Vendor coordinates the planned change and obtains AF approval from AFLCMC/ROU Materiel Leader and certification package resubmission, beforehand. The MAJCOM StF letter is provided to inform the major AF commands that a new boot has been added to the StF lists or an existing boot has been recertified for an additional three years.
NOTE: New sample boots, supplanted by the recertification process with newer boots, or withdrawn by the vendor for consideration, may be returned to the vendor per their request.
Otherwise, they will be disposed of.
Vendor Submits Data to ROU
ROU reviews data as determined by workload Passing
YES
NO
Notify Vendor of Failure
Prepare Staffing e- Package for Branch and Division levels
Send Signed letters from HSD Chief to AF
AFE Reps, vendors, and AF DLA Reps
Notify -AAFES Update AFUO webpage with Revised StF boot List
Missing/Revised Test Data
| 2026-04-08T14:51:22-0400 | |
| TAYLOR.NICHOLE.L.1388626557 |
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