Pricing Workbook T3_xx_xx 9_3_2025_OnRamp.xlsx
XLSX spreadsheet 4 MB Posted
- Attached to
- On-Ramp for Multiple Award Task Order (MATOC) Contract for Type 3 Helicopter Support Services
- Solicitation number
- 1202SA22R9203-0012
- Issued by
-
Department of Agriculture Forest Service
About this file
This document is a Pricing Workbook for a Type 3 Helicopter Support Services contract with the United States Forest Service (USFS). The workbook provides detailed instructions for vendors to submit pricing proposals for helicopter services, specifically for fire suppression and related missions including fire monitoring, initial attack, prescribed fire, aerial ignition, short-haul, rappel, and administrative activities. Vendors must submit a separate pricing workbook for each aircraft offered, with specific requirements for completing blue-highlighted fields such as aircraft registration, make/model, hourly flight rates, equipment details, and operational capabilities.
Key submission details include a notice of intent deadline of 15 October 2025 at 12 PM Mountain Standard Time, with full proposals due by 31 October 2025 at 12 PM Mountain Standard Time. The contract is an on-ramp opportunity for the Multiple Award Task Order (MATOC) contract, allowing new vendors to join existing Type 3 helicopter service providers. The contract will support wildland fire management programs, with a contract start year of 2026 and one option year. Vendors must specify their aircraft's capabilities, including Call-When-Needed daily availability, hourly project prices, operational regions, and additional equipment offerings.
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Other files
| File | Type | Posted |
|---|---|---|
| SF1449 First Page Only.pdf | ||
| Type 3 On Ramp QA_10_2_2025_FINAL.pdf | ||
| 1202SA22R9203 Amendment 0012.pdf |
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PLEASE READ INSTRUCTIONS
| Pricing Workbook and B.2 Schedule of Items INSTRUCTIONS | |||||
| Aircraft Type Offered | Type 3 | Solicitation No. | 1202SA22R9203 | 1202SA22R9201 | |
| Submit ONE Pricing Workbook (PW) for EACH aircraft offered. Pricing Workbooks are identified by Type and whether they represent offers for available Modern aircraft and future Modern aircraft for transitional line items.** Individual copies should be named as follows, replacing the italicized placeholders with aircraft-specific information: |
"Pricing Workbook_T3_FAARegistrationNumber_CompanyName.xlsx" e.g. Pricing Workbook_T3_N123SJ_Smith&JonesHelicopters.xlsx.
Please do not include "#" in the registration number. See Section E.10 OFFER SUBMITTAL FORMAT for additional instructions on submitting proposal documents.
| 1202SA22R9202 | ||
| Each Pricing Workbook will include offers for Call-When-Needed fire suppression daily availability and hourly project prices for the base and all option years. | 1202SA22R9203 |
| Step 1. Navigate to the "Offered Aircraft" worksheet, fill in blue highlighted fields | |||
| Offeror Name | Enter offeror's FULL name as it appears on proposal documents, please do not abbreviate. | ||
| Aircraft Offered | |||
| FAA Registration # | Enter the FAA registration number in this field starting with N or C. It will be entered for you in the correct field of each detail offer tab (i.e. "Item 1", if offered using Schedule of Items, will be filled out automatically) | ||
| Select | |||
| Make/Model/Series | Select the cell, then USE THE PICKLIST to select the exact "Aircraft Type" (from Attachment 10) from the drop-down list. This list is taken from the "Aircraft Type" field of the "Attachment 10" worksheet in this workbook. If your version of Excel is older, this pick list may not function. In that case, copy and paste the desired Aircraft from the "Aircraft" column of "Attachment 10" worksheet in this workbook. Alternate spellings will not retrieve the correct values for Hourly Flight Rate. |
Please ensure that the selected Make/Model/Series matches closely the aircraft on offer: there may be more than one line that includes the Make and Model (i.e. "S-70A") but represents different variants and might not retrieve the correct Flight Rate. If you cannot find your aircraft, please contact the Contract Officer for assistance.
| Hourly Flight Rate | Hourly Flight Rate will be automatically entered from the correct row in "Attachment 10" worksheet when the correct Make/Model/Series is selected. |
| Standard/Restricted | Use the drop-down list to select "Standard" or "Restricted"as appropriate. |
| Make and Model of Equipment | Enter the Make and Model of included equipment (tank and/or bucket as appropriate.) |
i.e. "SEI Industries Bambi HL5000" or "Bambi HL5000" or "Simplex FAS internal tank". There is provision for entering up to 2 buckets. The model name should match that used in the technical proposal specifications.
Capacity in Gallons Enter bucket and/or tank capacity in gallons.
Call-When-Needed For Call-When-Needed (CWN) offers, fill in CWN Daily Availability (Fire Suppression) for each year, and the Project (hourly) Flight rate for each year. If this is a CWN offer ONLY, Select "Yes" from the drop-down list, and do not select "Yes" to submit offer on EU Schedule of Items.
For tank offers, fill in Tank Offer line and enter Equipped Weight.
For bucket configuration offers, fill in Bucket Offer line and enter Equipped Weight and Bucket Weight in appropriate fields.
For ALL offers, enter Allowable Payload (Line 13) from Attachment 11. INTERAGENCY HELICOPTER LOAD CALCULATION.
Equipped Weight Equipped Weight, Bucket Helicopters: Equipped weight equals the Empty Weight (as listed in the Weight and Balance Data) plus the weight of lubricants and onboard equipment required by contract, including but not limited to survival kit, rappel anchor or first aid kit. Does not include the weight of the bucket and any associated suspension hardware.
Equipped Weight, Tanked Helicopters: Equipped weight equals the Empty Weight (as listed in the Weight and Balance Data) plus the weight of lubricants and onboard equipment required by contract, including but not limited to survival kit, rappel anchor or first aid kit. Includes the weight of a fixed tank and snorkel.
| Bucket Weight | Weight of bucket and associated suspension hardware. | |
| Hover to view Attachment 11 |
JANET SULLIVAN:
Allowable Payload Enter Allowable Payload - Line 13 from Attachment 11. INTERAGENCY HELICOPTER LOAD CALCULATION
Principal Base of Operations Section B Continuation of SF 1449:
Enter Location Name (airport name) and full address as required in Section B.
B.17 GOVERNMENT PILOT TRAINING Contractor will/will not authorize Government Pilot Training in accordance with Attachment 20.
Instructions: Select "Will" or "Will Not" from the drop-down list in the blue highlighted cell.
This form defaults to "Will"
B.30 OPERATIONS IN ALASKA, CARIBBEAN, CANADA, OR MEXICO Contractor will select areas of operations where they willing to accept orders and have authorization as indicated in their FAA 135 Operation Specifications. If accepting work in Alaska, contractor shall meet the requirements of Attachment 3 prior to mobilizing to Alaska.
Select "Yes" from drop-down that is on the left of each area that is authorized and you are willing to accept. Default is "No"
B.31 ADDITIONAL OFFERED EQUIPMENT The Offeror may offer items or services in addition to those listed below. Where no provision is made for a daily rate, the cost for furnishing such equipment shall be included in the daily availability rate. Offeror shall provide specifications on the items or services offered. Offered items may be awarded based on the needs of the Government and when prices are determined to be reasonable.
INSTRUCTIONS: Enter appropriate description, capacity (include units i.e. 5,000 gallons), quantity available, unit for price (hour, day etc) and unit price offer for any additional equipment included in CWN Project offers. You may insert additional rows if needed. (hover to see examples)
JANET SULLIVAN:
| Step 2. To offer additional aircraft, copy ENTIRE workbook for EACH aircraft offered and submit separately | |
| Copies should be named indicating aircraft registration number and offeror name and as detailed above. |
If a completed workbook is copied, details should be changed on the "Offered Aircraft" worksheet as needed.
* Excel Tips: Hover over cells with red triangle in corner to view notes. Right-Click to toggle notes "show/hide". This will also allow making the note bigger. When filling out blue fields on worksheets, use TAB to navigate to the next field. Re-size the page view slider (vertical dots in lower right corner) to expose Item Tabs to the right.
Offered Aircraft
| Pricing Workbook Offered Aircraft | Solicitation No. | 1202SA22R9203 |
| Aircraft Requested | Type 3 | |
| Offers Due Date | See Respective Solicitation | |
| Contract Start Year | 2026 | |
| Contract Base | 1 | |
| Option Years | 1 |
| OFFEROR NAME |
| Aircraft Offered |
FAA Registration # (Beginning with N or C) JANET SULLIVAN: For Transitional Item Replacement Aircraft where the FAA registration is not available, enter the full Serial Number
| Standard/Restricted | |
| Aircraft Make/Model/Series | |
| Government Hourly Flight Rate |
JANET SULLIVAN: Linked to: Attachment 10 May 16, 2025 Government Hourly Flight Rates
| Equipment Description | Make and Model | Capacity in Gallons | ||
| Tank | ||||
| Hover to view B.4 (17) | ||||
| JANET SULLIVAN: | Bucket # 1 | |||
| Bucket # 2 |
| Call When Needed (CWN) Offer | ||||
| Daily Availability Fire Suppression | Allowable Payload | |||
| JANET SULLIVAN: | 2026 | 2027 | ||
| Bucket Offer | Aircraft Equipped Weight (pounds) |
JANET SULLIVAN: Equipped Weight, Bucket Helicopters: Equipped weight equals the Empty Weight (as listed in the Weight and Balance Data) plus the weight of lubricants and onboard equipment required by contract (i.e., including but not limited to survival kit, rappel anchor, first aid kit). Does not include the weight of the bucket and any associated suspension hardware.
Equipped Weight, Tanked Helicopters: Equipped weight equals the Empty Weight (as listed in the Weight and Balance Data) plus the weight of lubricants and onboard equipment required by contract (i.e., including but not limited to survival kit, rappel anchor, first aid kit). Includes the weight of a fixed tank and snorkel.
| Bucket Weight | ||||
| Daily Availability Fire Suppression | Allowable Payload | 2026 | 2027 | |
| Tank Offer | Aircraft Equipped Weight (pounds) |
| Project Flight Rate (Hourly) | Allowable Payload | 2026 | 2027 | |
| Bucket Offer | Aircraft Equipped Weight (pounds) | |||
| Bucket Weight | ||||
| Project Flight Rate (Hourly) | Allowable Payload | 2026 | 2027 | |
| Tank Offer | Aircraft Equipped Weight (pounds) |
SECTION B: CONTINUATION OF SF 1449 Principal Base of Operations JANET SULLIVAN: Principal Base of Operations: The primary operating location of a 14 CFR 121, 133, 135 or 137 certificate-holder as established by the certificate holder.
JANET SULLIVAN: Equipped Weight, Bucket Helicopters: Equipped weight equals the Empty Weight (as listed in the Weight and Balance Data) plus the weight of lubricants and onboard equipment required by contract (i.e., including but not limited to survival kit, rappel anchor, first aid kit). Does not include the weight of the bucket and any associated suspension hardware.
Equipped Weight, Tanked Helicopters: Equipped weight equals the Empty Weight (as listed in the Weight and Balance Data) plus the weight of lubricants and onboard equipment required by contract (i.e., including but not limited to survival kit, rappel anchor, first aid kit). Includes the weight of a fixed tank and snorkel.
| Airport Base | |
| Address | |
| City, State |
B.17 GOVERNMENT PILOT TRAINING
Contractor Will authorize Government Pilot Training in accordance with Attachment 20.
| B.26 ACCEPTABLE SCHEDULE (enter only if "Other" has been selected for CLIN) |
| Note: All Personnel shall be under the same work schedule except for Maintenance Personnel. Maintenance Personnel may work a 14/14 schedule. If maintenance personnel work 14 days on, they must take 14 days off, unless approved by the Contracting Officer. Days off schedule may vary. A 14/14 schedule must be requested by checking “Other” and subject to approval by the Contracting Officer. |
If "Other" is selected on Schedule of Items, Enter only the CLIN here and the proposed Schedule
| B.30 OPERATIONS IN ALASKA, CARIBBEAN, CANADA, OR MEXICO | |||||
| Contractor will select areas of operations where they willing to accept orders and have authorization as indicated in their FAA 135 Operation Specifications. If accepting work in Alaska, contractor shall meet the requirements of Attachment 3 prior to mobilizing to Alaska. | |||||
| No | ALASKA | No | CARIBBEAN | ||
| No | CANADA | No | MEXICO |
B.31 ADDITIONAL OFFERED EQUIPMENT
The Offeror may offer items or services in addition to those listed below. Where no provision is made for a daily rate, the cost for furnishing such equipment shall be included in the daily availability rate. Offeror shall provide specifications on the items or services offered. Offered items may be awarded based on the needs of the Government and when prices are determined to be reasonable.
Daily rates for additional equipment will be paid only if ordered by the CO. (hover to see examples)
JANET SULLIVAN:
JANET SULLIVAN:
JANET SULLIVAN: For Transitional Item Replacement Aircraft where the FAA registration is not available, enter the full Serial Number
JANET SULLIVAN: Linked to: Attachment 10 May 16, 2025 Government Hourly Flight Rates
| JANET SULLIVAN: | Description | Capacity | Quantity | Unit | |
| (Day, Hour, etc) | Unit Price | ||||
| $ | |||||
| $ | |||||
| $ | |||||
| $ | |||||
| $ |
BIDDERS MAY QUALIFY THEIR BIDS - BIDDERS SHALL INDICATE BELOW THE MAXIMUM NUMBER OF EU LINE ITEMS THEY ARE WILLING TO ACCEPT
| Extended Cost Estimate Components | |||
| Pay Item Code | Description | Cost | Accounting Method |
| ES | Extended Standby (daily) | $ 66.00 | * Min Crew * MAP |
| PD | Subsistence Allowance (daily) | $ 155.00 | * Min Crew * MAP |
| SC | Other Charges | $ 220.00 | 100 * Estimated |
Attachment 10
| ATTACHMENT 10 - HELICOPTER SERVICES HOURLY FLIGHT RATES, FUEL CONSUMPTION, AND WEIGHT REDUCTION CHART |
| Effective May 16, 2025 |
| COMPANY | AIRCRAFT TYPE | FUEL CONSUMPTION | MAY 16, 2025 | ||
| HOURLY FLIGHT RATE | LOAD CALCULATION | ||||
| (gal/hr) | ($/HR) | Weight Reduction (lbs) | |||
| AIRBUS: | SA 315B | 58 | $2,491.49 | 180 | |
| AIRBUS: | SA 316B | 58 | $2,491.49 | 170 | |
| AIRBUS: | SA 318C | 45 | $2,395.17 | 80 | |
| AIRBUS: | SA 319B | 45 | $2,396.29 | 150 | |
| AIRBUS: | AS 330J | 179 | $6,473.30 | N/A | |
| AIRBUS: | AS 332L1 | 155 | $5,821.72 | 550 | |
| AIRBUS: | SA 341G | 45 | $2,333.33 | 170 | |
| AIRBUS: | AS 350B | 45 | $1,522.73 | 130 | |
| AIRBUS: | AS 350BA | 45 | $1,518.24 | 130 | |
| AIRBUS: | AS 350B1 | 45 | $1,521.61 | 160 | |
| AIRBUS: | AS 350B2 | 45 | $1,533.97 | 160 | |
| AIRBUS: | AS 350B3 | 44 | $1,513.85 | 175 | |
| AIRBUS: | AS 350B3e/H125 | 44 | $1,482.37 | 175 | |
| AIRBUS: | AS 350D | 38 | $1,451.58 | 130 | |
| AIRBUS: | AS 355F1 | 58 | $1,798.94 | 140 | |
| AIRBUS: | AS 355F2 | 58 | $1,798.94 | 140 | |
| AIRBUS: | AS 365N1 | 87 | $2,954.74 | 275 | |
| AIRBUS: | BO 105CBS | 55 | $1,910.59 | 180 | |
| AIRBUS: | BK 117 | 77 | $2,493.81 | 160 | |
| AIRBUS: | EC 120 | 31 | $1,110.60 | NOT ESTABLISHED | |
| AIRBUS: | EC 130-B4 | 51 | $1,519.80 | NOT ESTABLISHED | |
| AIRBUS: | EC 135 | 64 | $1,917.42 | 220 | |
| AIRBUS: | EC 135-P2 | 64 | $2,010.74 | NOT ESTABLISHED | |
| AIRBUS: | EC 135-P3 | 64 | $1,932.04 | NOT ESTABLISHED | |
| AIRBUS: | EC 145 | 80 | $2,446.25 | 220 | |
| AIRBUS: | EC 145-T2/H 145 | 83 | $2,402.06 | 220 | |
| AIRBUS: | EC 155B1 | 95 | $3,053.89 | NOT ESTABLISHED | |
| AIRBUS: | EC 225 | 183 | $5,870.23 | 650 | |
| BELL: | 47/Soloy (Scott's) | 23 | $979.98 | 120 | |
| BELL: | 204B | 86 | $2,441.06 | 200 | |
| BELL: | 204 Super B | 90 | $2,472.09 | 200 | |
| BELL: | 205A1 | 88 | $2,410.48 | 260 | |
| BELL: | 205 A1++ | 90 | $2,425.99 | 260 | |
| BELL: | UH-1B | 86 | $2,394.97 | N/A | |
| BELL: | UH-1B Super | 88 | $2,410.48 | N/A | |
| BELL: | UH-1F | 88 | $2,480.19 | N/A | |
| BELL: | TH-1L | 88 | $2,410.48 | N/A | |
| BELL: | UH-1H (-13 engine) | 88 | $2,410.48 | N/A | |
| BELL: | UH-1H (-17 engine) | 90 | $2,425.99 | N/A | |
| BELL: | 206BII | 25 | $1,145.02 | 100 | |
| BELL: | 206BIII | 27 | $1,160.53 | 130 | |
| BELL: | 206L1 | 32 | $1,385.94 | 150 | |
| BELL: | 206L3 | 38 | $1,412.23 | 180 | |
| BELL: | 206L4 | 38 | $1,412.23 | 180 | |
| BELL: | 210 | 90 | $2,425.99 | 260 | |
| BELL: | 212 | 100 | $2,739.64 | 390 | |
| BELL: | 212HP | 100 | $2,739.64 | 390 | |
| BELL: | 212 Single (Eagle) | 90 | $2,555.28 | 260 | |
| BELL: | 214B | 160 | $4,172.96 | 380 | |
| BELL: | 214B1 | 145 | $3,896.99 | 380 | |
| BELL: | 214ST | 133 | $5,088.96 | 420 | |
| BELL: | 222A | 70 | $3,087.10 | NOT ESTABLISHED | |
| BELL: | 222B | 83 | $3,187.92 | NOT ESTABLISHED | |
| BELL: | 222UT | 83 | $3,187.92 | NOT ESTABLISHED | |
| BELL: | 407 | 44 | $1,494.74 | 155 | |
| BELL: | 407HP (Eagle) | 44 | $1,462.14 | 155 | |
| BELL: | 412 | 110 | $2,800.33 | 390 | |
| BELL: | 412HP | 110 | $2,800.33 | 390 | |
| BELL: **REV 5/16/2025 | 412EP | 110 | $2,800.33 | 390 | |
| BELL: | 412EPX | 110 | $2,828.44 | 390 | |
| BELL **REV 2/16/25 | 429 | 73 | $2,025.45 | 135 | |
| BELL: | 505 | 32 | $1,052.03 | 130 | |
| BOEING: | BV 107/CH 46 | 180 | $5,644.59 | N/A | |
| BOEING: | BV 234/CH 47 | 405 | $9,923.67 | N/A | |
| HILLER: | SL-3/4 | 20 | $866.77 | 90 | |
| HILLER: | H 1100B | 22 | $1,167.85 | 130 | |
| HILLER: | UH 12/Soloy | 23 | $983.35 | 100 | |
| KAMAN: | H43F | 85 | $2,243.31 | N/A | |
| KAMAN: | K-1200/K-Max | 86 | $2,800.83 | N/A | |
| KAMOV: | KA-32 | 225 | $6,110.51 | NOT ESTABLISHED | |
| LEONARDO HELICOPTERS: | AW 119 KOALA | 55 | $1,739.70 | 230 | |
| LEONARDO HELICOPTERS: | AW 139 | 129 | $3,678.46 | 335 | |
| LEONARDO HELICOPTERS: | EH 101 | 211 | $7,191.41 | NOT ESTABLISHED | |
| McDONNELL-DOUGLAS: | 500C | 23 | $1,172.23 | 110 | |
| McDONNELL-DOUGLAS: | 500D/E | 28 | $1,211.01 | 120 | |
| McDONNELL-DOUGLAS: | 520N | 32 | $1,221.79 | 100 | |
| McDONNELL-DOUGLAS: | 530F | 34 | $1,395.82 | 120 | |
| McDONNELL-DOUGLAS: | 600N | 41 | $1,516.44 | 155 | |
| McDONNELL-DOUGLAS: | 900/902 | 69 | $2,241.77 | 210 | |
| ROBINSON: | R 66 | 24 | $915.78 | 130 | |
| SIKORSKY: | S 55T | 47 | $1,638.30 | 170 | |
| SIKORSKY: | S 58D/E | 83 | $2,653.90 | N/A | |
| SIKORSKY: | S 58T/PT6T-3 | 115 | $3,372.01 | 400 | |
| SIKORSKY: | S 58T/PT6T-6 | 115 | $3,372.01 | 460 | |
| SIKORSKY: | CH 53D | 425 | $9,571.73 | N/A | |
| SIKORSKY: | CH 54A/S 64E | 493 | $10,133.95 | N/A | |
| SIKORSKY: | CH 54B/S 64F | 512 | $10,281.30 | N/A | |
| SIKORSKY: | H 3/S 61 All Series | 170 | $5,896.45 | 550 | |
| SIKORSKY: | S 62A | 70 | $1,967.33 | 300 | |
| SIKORSKY: | S 70/UH 60 | 135 | $5,687.97 | 550 | |
| SIKORSKY: | S 70/UH 60+ | 135 | $5,815.01 | 550 | |
| SIKORSKY: | S 76A | 88 | $3,327.89 | NOT ESTABLISHED | |
| SIKORSKY: | S 76A+ | 96 | $3,442.77 | NOT ESTABLISHED | |
| SIKORSKY: | S 76A++ | 92 | $3,399.38 | NOT ESTABLISHED | |
| SIKORSKY: | S 76B | 111 | $3,418.57 | NOT ESTABLISHED | |
| SIKORSKY: | S 76C | 92 | $3,343.17 | NOT ESTABLISHED | |
| SIKORSKY: | S 76C+ | 88 | $3,294.16 | NOT ESTABLISHED | |
| SIKORSKY: | S 76C++ | 94 | $3,328.32 | NOT ESTABLISHED | |
| SIKORSKY: | S 92 | 178 | $5,598.73 | NOT ESTABLISHED | |
| AVERAGE GALLON JET FUEL: $6.44 PRICE: |
**Less than 10% difference from February to May, so no change to Flight Rate
Attachment 11
| Solicitation No. 1202SA22R9203 United States Forest Service (USFS) |
| Helicopter Support Services (HSS) National Interagency Fire Center (NIFC) |
SECTION D CONTRACT DOCUMENTS EXHIBITS/ATTACHMENTS
| ATTACHMENT 11 - INTERAGENCY HELICOPTER LOAD CALCULATION(B.3, B.19(a)(3), B.15(a)(6), B.15(b)(2)) | |||||||
| INTERAGENCY HELICOPTER | MODEL | ||||||
| LOAD CALCULATION | |||||||
| OAS-67/FS 5700-17 (11/03) | N# | ||||||
| PILOT(S) | DATE | ||||||
| MISSION | TIME | ||||||
| 1 | DEPARTURE | PA | OAT | ||||
| 2 | DESTINATION | PA | OAT | ||||
| 3 | HELICOPTER EQUIPPED WEIGHT | ||||||
| 4 | FLIGHT CREW WEIGHT | ||||||
| 5 | FUEL WT ( _gallons X 7 lbs per gal) | ||||||
| 6 | OPERATING WEIGHT (3 + 4 + 5) | ||||||
| Non-Jettisonable | Jettisonable | ||||||
| HIGE | HOGE | HOGE-J | |||||
| 7a | PERFORMANCE REF |
(List page/chart from FM)
7b COMP GROSS WT (FM Performance section)
| 8 | WT REDUCTION |
| (Req for all Non-Jettisonable) | |
| 9 | ADJUSTED WEIGHT |
| (7b minus 8) | |
| 10 | GROSS WT LIMIT |
(FM Limitations Section)
| 11 | SELECTED WEIGHT |
| (Lowest of 9 or 10) | |
| 12 | OPERATING WEIGHT |
| ((From Line 6) | |
| 13 | ALLOWABLE PAYLOAD |
| (11 minus 12) | |
| 14 | PASSENGERS/CARGO MANIFEST |
| 15 | ACTUAL PAYLOAD (Total of all weights listed in item 14) Line 15 must not exceed Line 13 for the intended mission | |
| PILOT SIGNATURE | HazMat | |
| MGR SIGNATURE | Yes No__ |
Attachment 11 Instructions
ATTACHMENT 11 - INTERAGENCY HELICOPTER LOAD CALCULATION (B.3,
B.19(a)(3), B.15(a)(6), B.15(b)(2))
Vendors shall use Computed Gross Weight in load calculations for submitting proposals (see Attachment 19 Computed Gross Weight for applicable aircraft.) For field operations use current temperature and elevation for performance planning.
An Out of Ground (OGE) power check will be performed for either the takeoff or landing, whichever is most restrictive. Refer to Tech Bulletin No. IATB 17-01, dated November 10, 2016. Bulletins can be found at: http://www.fs.fed.us/fire/av_safety/promotion/Technical_Bulletins/index.html.
Instructions:
A load calculation must be completed daily. A new calculation is required when operating conditions change (± 1000’ in elevation or ± 5oC in temperature) or when the Helicopter Operating Weight changes (such as changes to the Equipped Weight, changes in flight crew weight or a change in fuel load).
All blocks must be completed. Pilot must complete all header information and Items 1-13. Helicopter Manager completes Items 14 & 15.
1. DEPARTURE – Name of departure location and current Pressure Altitude (PA, read altimeter when set to 29.92) and Outside Air Temperature (OAT, in Celsius) at departure location.
2. DESTINATION – Name of destination location and PA & OAT at destination. If destination conditions are unknown, use MSL elevation from a map and Standard Lapse Rate of 2o C/1000’ to estimate OAT.
Check the box in Line 1 (Departure) or Line 2 (Destination) to indicate the most restrictive values used to obtain Computed Gross Weight in Line 7b.
3. HELICOPTER EQUIPPED WEIGHT – Equipped Weight equals the Empty Weight (as listed in the Weight and Balance Data) plus the weight of lubricants and onboard equipment required by contract (i.e., survival kit, rappel bracket).
4. FLIGHT CREW WEIGHT – Weight of the Pilot and any other assigned flight crewmembers on board (i.e., Co-pilot, flight engineer, navigator) plus the weight of their personal gear to include PFD-s.
5. FUEL WEIGHT – Number of gallons onboard (with one decimal) X the weight per gallon (Jet A Fuel = 7.0 lbs/gal) rounded up to the next whole number.
6. OPERATING WEIGHT – Add items 3, 4 and 5.
7a. PERFORMANCE REFERENCES – List the specific Flight Manual supplement and hover performance charts used to derive Computed Gross Weight for Line 7b. Separate charts may be required to derive HIGE, HOGE and HOGE-J. HIGE: use Hover-In-Ground-Effect, External/Cargo Hook Chart (if available). HOGE & HOGE-J: use Hover-Out-Ground-Effect charts for all HOGE operations.
| 7b. COMPUTED GROSS WEIGHT - For proposal purposes only, use the computed gross weight performance standards listed in Attachment 19 for Type 1 aircraft. The computed gross weight standard selected shall conform to the minimum performance standard as specified within the flight manual or flight manual supplement. Contact the contracting officer prior to proposal submittal when a helicopter or STC is not listed or the Attachment 19 performance calculation is assessed as an error. |
| 8. WEIGHT REDUCTION – The Government Weight Reduction is required for all |
“non-jettisonable” loads. The Weight Reduction is optional (mutual agreement between Pilot and Helicopter Manager) when carrying jettisonable loads (HOGE-J) where the pilot has total jettison control. The appropriate Weight Reduction value, for make & model, can be found in the current helicopter procurement document (contract).
9. ADJUSTED WEIGHT – Line 7b minus Line 8.
10. GROSS WEIGHT LIMITATION – Enter applicable gross weight limit from Limitations section of the basic Flight Manual or the appropriate Flight Manual Supplement. This may be Maximum Gross Weight Limit for Take-Off and Landing, a Weight/Altitude/Temperature (WAT) limitation or a Maximum Gross Weight Limit for External Load (jettisonable). Limitations may vary for HIGE, HOGE and HOGE-J.
Refer to Tech Bulletin No. 2011-03, dated September 14, 2011. Bulletins can be found at: http://www.fs.fed.us/fire/av_safety/promotion/Technical_Bulletins/index.html
11. SELECTED WEIGHT – The lowest weight, either line 9 or 10, will be entered for all loads. Applicable limitations in the Flight Manual must not be exceeded.
12. OPERATING WEIGHT – Use the value entered in Line 6.
13. ALLOWABLE PAYLOAD – Line 11 minus Line 12 is the maximum allowable weight (passengers and/or cargo) that can be carried for the mission. Allowable Payload may differ for HIGE, HOGE and HOGE-J.
14. PASSENGERS AND/OR CARGO – Enter passenger names and weights and/or type and weights of cargo to be transported. Include mission accessories, tools, gear, baggage, etc. A separate manifest may be used.
15. ACTUAL PAYLOAD – Total of all weights listed in Item 14. Actual payload must not exceed Allowable Payload for the intended mission profile, i.e. HIGE, HOGE or HOGE-J.
Both Pilot and Helicopter Manager must review and sign the form. Check if HazMat is being transported. Manager must inform the pilot of type, quantity, and location of HazMat onboard.
Attachment 19
| Helicopter Support Services (HSS) | SECTION D | 1202SA22R9203/0009 Conformed | National Interagency Fire Center (NIFC) |
| ATTACHMENT 19 - COMPUTED GROSS WEIGHT TABLE FOR TYPE 1 AIRCRAFT (B.3(a), Attachment 11) – 4/12/2025 |
| Aircraft | Line 7a: Performance Reference | Line 7a: Computed Gross Weight HOGE-J | Line 10: Limitations | Notes | |
| 5,000/30 7,750 ft DA | 8,000/25 11,000 ft DA | ||||
| S-58T | STC SR09584RC, PT6T-6, Max Take Off Power, 100% Nr, No Anti-Abrasion Strips | 13,000 Fig 1-3, RFM | 11,300 Fig 2, STC | 13,000 | Ref STC Fig 1 for internal Non-J Line 10 WAT Limits |
| S-58T | STC SR09584RC, PT6T-6, Max Take Off Power, 93% Nr, No Anti-Abrasion Strips | 13,000 Fig 1-3, RFM | 10,900 Fig 2, STC | 13,000 | Ref STC Fig 1 for internal Non-J Line 10 WAT Limits |
| S-58T | STC 4570NM, PT6T-6, Max Take Off Power, 93-100% Nr, No Ant-Abrasion Strips | 13,000 Fig 1-3, RFM | 11,300 Fig 7-1-1A Sup 7 | 13,000 | Ref STC Fig 1 for internal Non-J Line 10 WAT Limits |
| S-58T | STC 4570NM, PT6T-3, Max Take Off Power, 93-100% Nr, No Ant-Abrasion Strips | 13,000 Fig 1-1, RFM | 11,300 Fig 7-1-1A Sup 7 | 13,000 | Ref STC Fig 1 for internal Non-J Line 10 WAT Limits |
| S-58T | STC 4570NM, PT6T-3, Max Take Off Power, 93-100% Nr, With Ant-Abrasion Strips | 13,000 Fig 1-1A, RFM | 11,300 Fig 7-1-1A Sup 7 | 13,000 | Ref STC Fig 1 for internal Non-J Line 10 WAT Limits |
| K-1200 | FMS No. 1, USFS Fire Fighting | 11,400 Fig S1-1, S1-5, S1-11 | 10,300 Fig S1-1, S1-5, S1-11 | 12,000 | Does not consider excess power available Ref FSM No. 1 Figure S1-6 as GW varies with Alt |
| K-1200 | Basic Flight Manual | 9,800 Fig 5-1, 5-5, 5-8 | 8,700 Fig 5-1, 5-5, 5-8 | 12,000 | Does not consider excess power available Ref FM Figure 5-6 as GW varies with Alt |
| AS-332 L | RFM Sect 5 | 17,300 | 15,700 | 20,610 | WAT limit for HIGE and HOGE |
| Fig 5 | Fig 5 | Ref Fig 1a, RFM. | |||
| AS-332 L1 | Flight Manual Sup.10.6 | 18,250 Fig 2 | 16,645 Fig 2 | 20,610 | WAT limit for HIGE and HOGE |
| Ref Fig 1a, RFM. | |||||
| S-61A, Composite | CT58-GE-100, RFMS 20 | 19,600 | 18,000 | 22,000 | |
| MRB & TRB | Fig B-3, Fig 2 | Fig B-3, Fig 2 | |||
| SK-61A, Composite | Carson STC SR01585NY, RFMS #10 S61 A/V, CT58-140-1, -2 | 17,500 Fig 1, Fig 5 | 16,200 Fig 1, Fig 5 | 22,000 | |
| MRB 100% Nr | |||||
| SK-61A, Composite MRB, 103% Nr | Carson STC SR01585NY, RFMS #10 S61 A/V, CT58-140-1, -2 | 17,400 Fig 1, Fig 6 | 16,100 Fig 1, Fig 6 | 22,000 | |
| S-61 A/V, Composite MRB, 100% Nr | Carson STC SR01585NY, RFMS #10 S61 A/V, CT58-140-1, -2 | 17,500 Fig 1, Fig 5 | 16,200 Fig 1, Fig 5 | 22,000 | |
| S-61 A/V, Composite MRB, 103% Nr | Carson STC SR01585NY, RFMS #10 S61 A/V, CT58-140-1, -2 | 17,400 Fig 1, Fig 6 | 16,100 Fig 1, Fig 6 | 22,000 | |
| S-61 A/V, Composite | CT58-GE-140 (RFMS 10), RFMS 20 (CM&TRB) | 17,750 | 16,600 | 22,000 | |
| MRB & TRB, 106% Nr | Fig 1, Fig 1&2 | Fig 1, Fig 1&2 |
| Aircraft | Line 7a: Performance Reference | Line 7a: Computed Gross Weight HOGE-J | Line 10: Limitations | Notes | |
| 5,000/30 7,750 ft DA | 8,000/25 11,000 ft DA | ||||
| S-61 L/N/NM, Composite MRB, 100% Nr | Carson STC SR01585NY, RFMS #6 S61 L/N/NM, CT58-140-1, -2 | 17,500 Fig 1, Fig 5 | 16,200 Fig 1, Fig 5 | 22,000 | |
| S-61 L/N/NM, Composite MRB, 103% Nr | Carson STC SR01585NY, RFMS #6 S61 L/N/NM, CT58-140-1, -2 | 17,500 Fig 1, Fig 6 | 16,200 Fig 1, Fig 6 | 22,000 | |
| S-61 L/N/NM, Composite MRB, 100% Nr | Carson STC SR01585NY, RFMS #7, L/N NM, CT-58-140-1, -2 | 17,400 Fig 7-4-26 | 16,000 Fig 7-4-26 | 22,000 | |
| S-61 A, Composite MRB, 105% Nr | Carson STC SR01585NY, RFMS-S61A-1, | 20,200 Fig 11-6A, 11-10a | 18,300 Fig 11-6A, 11-10a | 21,000 | |
| T58-GE-402 | |||||
| S-61 A, Composite | Carson STC SR01585NY & SR04122NY, RFMS-S61A-4, T58-GE-402 | 20,200 Fig 11-6A, 11-10b | 18,500 Fig 11-6A, 11-10b | 21,000 | |
| MRB & TRB, 105% Nr | |||||
| S-61 A, Composite | Carson STC SR01585NY & SR04122NY, RFMS-S61A-1, T58-GE-402 | 20,200 Fig 11-6A, 11-10b | 18,500 Fig 11-6A, 11-10b | 21,000 | |
| MRB & TRB, 105% Nr | |||||
| SH-3H, Composite | Carson STC SR01585NY, RFMS-SH3H-2, | 20,200 Fig 20-16, 21-3c | 18,300 Fig 20-16, 21-3c | 21,000 | |
| MRB, 105% Nr | T58-GE-402 | ||||
| SH-3H, Composite | Carson STC SR01585NY & SR04122NY, RFMS-SH3H-2 Rev B, T58-GE-402 | 20,200 Fig 20-16, 21-3d | 18,500 Fig 20-16, 21-3d | 21,000 | |
| MRB & TRB, 105% Nr | |||||
| H-60A, @ ATF .90 | RFM, 30-min, T700-GE-700 | 16,700 Fig 7-2, 7-3, 7-4 | 15,250 Fig 7-2, 7-3, 7-4 | 22,000 | No HIRRS: add +1 to Specification Torque Available per Engine % (Fig 7-3) per RFM Specific Q calculated via math (Fig 7-3) per RFM: Spec Q x TR = Q avail Transmission limited to 100% |
| H-60A, @ ATF .95 | RFM, 30-min, T700-GE-700 | 17,250 Fig 7-2, 7-3, 7-4 | 15,800 Fig 7-2, 7-3, 7-4 | 22,000 | |
| H-60A, @ ATF .95 BLR | RFM, 30-min, T700-GE-700 | 17,545 | 16,121 | 22,000 | |
| RFMS-UH60FF-1 | RFM Fig 7-2, 7-3 | RFM Fig 7-2, 7-3 | |||
| RFMS Fig 7-4.2 sheets | RFMS Fig 7-4.2 sheets | ||||
| 24 and 26 of 42 | 18 and 20 of 42 | ||||
| H-60A, @ ATF .96 | RFM, 30-min, T700-GE-700 | 17,350 Fig 7-2, 7-3, 7-4 | 15,950 Fig 7-2, 7-3, 7-4 | 22,000 | |
| H-60A, @ATF .97 | RFM, 30-min, T700-GE-700 | 17,450 | 16,000 | 22,000 | |
| Fig 7-2, 7-3, 7-4 | Fig 7-2, 7-3, 7-4 |
| Aircraft | Line 7a: Performance Reference | Line 7a: Computed Gross Weight HOGE-J | Line 10: Limitations | Notes | |
| 5,000/30 7,750 ft DA | 8,000/25 11,000 ft DA | ||||
| H-60A, @ATF .97 BLR | RFM, 30-min, T700-GE-700 | 17,773 | 16,288 | 22,000 | No HIRRS: add +1 to Specification Torque Available |
| RFMS-UH60FF-1 | RFM Fig 7-2, 7-3 | RFM Fig 7-2, 7-3 | per Engine % (Fig 7-3) per RFM Specific Q calculated via math | ||
| RFMS Fig 7-4.2 sheets | RFMS Fig 7-4.2 sheets | (Fig 7-3) per RFM: Spec Q x TR = Q avail Transmission limited to 100% | |||
| 24 and 26 of 42 | 18 and 20 of 42 | BLR linear interpolate via supplement direction | |||
| H-60A, @ ATF .98 | RFM, 30-min, T700-GE-700 | 17,625 Fig 7-2, 7-3, 7-4 | 16,125 Fig 7-2, 7-3, 7-4 | 22,000 | |
| H-60A, @ ATF 1.0 | RFM, 30-min, T700-GE-700 | 17,800 Fig 7-2, 7-3, 7-4 | 16,250 Fig 7-2, 7-3, 7-4 | 22,000 | |
| H-60A+ @ ATF .90 | RFM, 10-min, T700-GE-701C or | 18,950 Fig 7A-2, 7A-4, 7A-6 | 17,350 Fig 7A-2, 7A-4, 7A-6 | 22,000 | No HIRRS: add +1 to Torque Available per Engine % (Fig 7A-4) per RFM Actual Q calculated via |
| T700-GE-701D/CC | math per RFM: Spec Q x TR = Q avail *Transmission limited to 100% | ||||
| H-60A+ @ ATF .95 | RFM, 10-min, T700-GE- | 19,500 Fig 7A-2, 7A-4, 7A-6 | 17,800 Fig 7A-2, 7A-4, 7A-6 | 22,000 | BLR linear interpolation via supplement direction |
| orT700-GE-701D/CC | |||||
| H-60A+ @ ATF .95 BLR | RFM, 10-min, T700-GE-701C or | 20,062 | 18,297 | 22,000 | |
| T700-GE-701D/CC | RFM Fig 7A-2, 7A-4 | RFM Fig 7A-2, 7A-4 | |||
| RFMS-UH60FF-1 | RFMS Fig 7A-6.2 sheets | RFMS Fig 7A-6.2 sheets | |||
| 34 and 36 of 48 | 26 and 28 of 48 | ||||
| H-60A+ @ ATF .96 | RFM, 10-min, T700-GE-701C or | 19,650* Fig 7A-2, 7A-4, 7A-6 | 17,850 Fig 7A-2, 7A-4, 7A-6 | 22,000 | |
| T700-GE-701D/CC | |||||
| H-60A+ @ATF .97 | RFM, 10-min, T700-GE-701C or | 19,650* Fig 7A-2, 7A-4, 7A-6 | 17,950 | 22,000 | |
| T700-GE-701D/CC | Fig 7A-2, 7A-4, 7A-6 | ||||
| H-60A+ @ATF .97 BLR | RFM, 10-min, T700-GE-701C or | 20,171 | 18,480 | 22,000 | |
| T700-GE-701D/CC | RFM Fig 7A-2, 7A-4 | RFM Fig 7A-2, 7A-4 | |||
| RFMS-UH60FF-1 | RFMS Fig 7A-6.2 sheets | RFMS Fig 7A-6.2 sheets | |||
| 34 and 36 of 48 | 26 and 28 of 48 | ||||
| H-60A+ @ ATF .98 | RFM, 10-min, T700-GE-701C or | 19,650* Fig 7A-2, 7A-4, 7A-6 | 18,100 Fig 7A-2, 7A-4, 7A-6 | 22,000 | |
| T700-GE-701D/CC | |||||
| H-60A+ @ ATF .98 BLR | RFM, 10-min, T700-GE-701C or | 20,170 | 18,571 | 22,000 | |
| T700-GE-701D/CC | RFM Fig 7A-2, 7A-4 | RFM Fig 7A-2, 7A-4 | |||
| RFMS-UH60FF-1 | RFMS Fig 7A-6.2 sheets | RFMS Fig 7A-6.2 sheets | |||
| 34 and 36 of 48 | 28 and 30 of 48 | ||||
| H-60A+ @ ATF 1.0 | RFM, 10-min, T700-GE-701C or | 19,650* Fig 7A-2, 7A-4, 7A-6 | 18,250 Fig 7A-2, 7A-4, 7A-6 | 22,000 | |
| T700-GE-701D/CC |
| Aircraft | Line 7a: Performance Reference | Line 7a: Computed Gross Weight HOGE-J | Line 10: Limitations | Notes | |
| 5,000/30 7,750 ft DA | 8,000/25 11,000 ft DA | ||||
| H-60A+ @ ATF 1.0 BLR | RFM, 10-min, T700-GE-701C or | 20,170 | 18,740 | 22,000 | No HIRRS: add +1 to Torque Available |
| T700-GE-701D/CC | Fig 7A-6.7, sheet 4 of 11 | Fig 7A-6.7, sheet 7 of 11 | per Engine % (Fig 7A-4) per RFM Actual Q calculated via math per RFM: Spec Q x TR = Q avail *Transmission limited to 120% | ||
| RFMS-UH60FF-1 | BLR linear interpolation via supplement direction | ||||
| H-60L @ ATF .90 | RFM, 10-min, T700-GE-701C or T700-GE-701D/CC | 18,950 Fig 7A-2, 7A-4, 7A-6 | 17,350 Fig 7A-2, 7A-4, 7A-6 | 23,500 | |
| H-60L @ ATF .95 | RFM, 10-min, T700-GE-701C | 19,500 Fig 7A-2, 7A-4, 7A-6 | 17,800 Fig 7A-2, 7A-4, 7A-6 | 23,500 | |
| T700-GE-701D/CC | |||||
| H-60L @ ATF .95 BLR | RFM, 10-min, T700-GE-701C | 20,062 | 18,297 | 23,500 | |
| T700-GE-701D/CC | RFM Fig 7A-2, 7A-4 | RFM Fig 7A-2, 7A-4 | |||
| RFMS-UH60FF-1 | RFMS Fig 7A-6.2 sheets | RFMS Fig 7A-6.2 sheets | |||
| 34 and 36 of 48 | 26 and 28 of 48 | ||||
| H-60L @ ATF .96 | RFM, 10-min, T700-GE-701C | 19,700 Fig 7A-2, 7A-4, 7A-6 | 17,850 Fig 7A-2, 7A-4, 7A-6 | 23,500 | |
| T700-GE-701D/CC | |||||
| H-60L @ ATF .97 | RFM, 10-min, T700-GE-701C | 19,750 | 17,950 | 23,500 | |
| T700-GE-701D/CC | Fig 7A-2, 7A-4, 7A-6 | Fig 7A-2, 7A-4, 7A-6 | |||
| H-60L @ ATF .97 BLR | RFM, 10-min, T700-GE-701C | 20,303 | 18,480 | 23,500 | |
| T700-GE-701D/CC | RFM Fig 7A-2, 7A-4 | RFM Fig 7A-2, 7A-4 | |||
| RFMS-UH60FF-1 | RFMS Fig 7A-6.2 sheets | RFMS Fig 7A-6.2 sheets | |||
| 34 and 36 of 48 | 26 and 28 of 48 | ||||
| H-60L @ ATF .98 | RFM, 10-min, T700-GE-701C | 19,850 Fig 7A-2, 7A-4, 7A-6 | 18,100 Fig 7A-2, 7A-4, 7A-6 | 23,500 | |
| T700-GE-701D/CC | |||||
| H-60L @ ATF .98 BLR | RFM, 10-min, T700-GE-701C | 20,434 | 18,571 | 23,500 | |
| T700-GE-701D/CC | RFM Fig 7A-2, 7A-4 | RFM Fig 7A-2, 7A-4 | |||
| RFMS-UH60FF-1 | RFMS Fig 7A-6.2 sheets | RFMS Fig 7A-6.2 sheets | |||
| 34 and 36 of 48 | 28 and 30 of 48 | ||||
| H-60L @ ATF 1.0 | RFM, 10-min, T700-GE-701C | 20,100 Fig 7A-2, 7A-4, 7A-6 | 18,250 Fig 7A-2, 7A-4, 7A-6 | 23,500 | |
| T700-GE-701D/CC | |||||
| H-60L @ ATF 1.0 BLR | RFMS-UH60FF-1 | 20,700 | 18,740 | 23,500 | |
| Fig 7A-6.5 | Fig 7A-6.5 | ||||
| sheet 4 of 11 | sheet 7 of 11 |
| Aircraft | Line 7a: Performance Reference | Line 7a: Computed Gross Weight HOGE-J | Line 10: Limitations | Notes | |
| 5,000/30 7,750 ft DA | 8,000/25 11,000 ft DA | ||||
| S-70A @ ATF .90 | RFM 55-1520-237-10HK, 10-min, | 18,850 Fig 7-2, 7-4,7-5 | 17,250 Fig 7-2, 7-4,7-5 | 23,500 | No HIRRS: add +1 to Torque Available per Engine % (Fig 7-4) per RFM Actual Q calculated via math per RFM: Spec Q x TR = Actual Q avail *Transmission limited to 120% |
| T700-GE-701C | |||||
| S-70A @ ATF .95 | RFM 55-1520-237-10HK, 10-min | 19,500 Fig 7-2, 7-4,7-5 | 17,700 Fig 7-2, 7-4,7-5 | 23,500 | |
| T700-GE-701C | |||||
| S-70A @ ATF .96 | RFM 55-1520-237-10HK, 10-min | 19,650 Fig 7-2, 7-4,7-5 | 17,750 Fig 7-2, 7-4,7-5 | 23,500 | |
| T700-GE-701C | |||||
| S-70A @ ATF .98 | RFM 55-1520-237-10HK, 10-min | 19,750* Fig 7-2, 7-4,7-5 | 18,000 Fig 7-2, 7-4,7-5 | 23,500 | |
| T700-GE-701C | |||||
| S-70A @ ATF 1.0 | RFM 55-1520-237-10HK, 10-min | 20,000* Fig 7-2, 7-4,7-5 | 18,150 Fig 7-2, 7-4,7-5 | 23,500 | |
| T700-GE-701C | |||||
| S-70C | TM 1-1520-237-10B, 10-min | 19,000 Fig 7-3, 7-6 | 17,500 Fig 7-3, 7-6 | 22,000 | No HIRRS: added 1.3% Torque to Torque Available Transmission limited to 100% |
| T700-GE-701A | |||||
| S-70C @ ATF .95 BLR | RFM H60A, 30-min, T700-GE-700 | 17,545 | 16,121 | 22,000 | No HIRRS: add +1 to torque Available per, Engine % (Fig 7A-4) per H60 RFM, |
| RFMS-UH60FF-1 | RFM Fig 7-2, 7-3 | RFM Fig 7-2, 7-3 | Actual Q calculated via, math per | ||
| RFMS Fig 7-4.2 sheets | RFMS Fig 7-4.2 sheets | H60 RFM: Spec Q x TR = Q avail *Transmission limited to 100% | |||
| 24 and 26 of 42 | 18 and 20 of 42 | BLR linear interpolation via supplement direction | |||
| S-70C @ ATF .97 BLR | RFM H60A, 30-min, T700-GE-700 | 17,773 | 16,288 | 22,000 | |
| RFMS-UH60FF-1 | RFM Fig 7-2, 7-3 | RFM Fig 7-2, 7-3 | |||
| RFMS Fig 7-4.2 sheets | RFMS Fig 7-4.2 sheets | ||||
| 24 and 26 of 42 | 18 and 20 of 42 | ||||
| CH-47D 30-min PTIT | BFS-510 Rev 1 | 45,500* | 41,600* | 50,000 | *Values are lesser of either performance gross weight limit or structural limit. |
| 30-min PTIT Limit | Fig 5-4, 5-7 | Fig 5-4, 5-7 | |||
| CH-47D 10-min PTIT** | BFS-510, T55-GA-714 | 47,000* Fig 5-6, 5-10 | 42,000* Fig 5-6, 5-10 | 50,000 | **If RFM authorizes, otherwise use 30-min limit |
| 10-min PTIT Limit | *Values are lesser of performance gross weight limit or structural limit. | ||||
| CH-47D 10-min PTIT** | TAN-210 Rev 2, | 47,000* Fig 7-6, 7-10 | 42,000* Fig 7-6, 7-10 | 50,000 | **If RFM authorizes, otherwise use 30-min limit |
| 10-min PTIT Limit | *Values are lesser of performance gross weight limit or structural limit. | ||||
| CH-47D 10-min PTIT** | BFS-210 rev 2 | 48,750 | 44,500 | 50,000 | **If RFM authorizes, otherwise use 30-min limit |
| 10-min PTIT Limit | Fig 5-6 | Fig 5-6 | |||
| CH-47D 10-min | BFS-610 rev IR | 48,720 | 44,300 | 54,000 | |
| 10-min | Fig 8.5-2 | Fig 8.5-2 |
| Aircraft | Line 7a: Performance Reference | Line 7a: Computed Gross Weight HOGE-J | Line 10: Limitations | Notes | |
| 5,000/30 7,750 ft DA | 8,000/25 11,000 ft DA | ||||
| BV-234LR | RFMS 5 | 43,100* Fig 1-3 | 39,500* Fig 1-3 | 51,000 | *Values are lesser of performance gross weight limit or structural limit. |
| BV-234LR | Columbia Helicopters | 43,100* | 39,500* | 51,000 | *Values are lesser of performance gross weight limit or structural limit. |
| RFMS BV-234 LR/UT | Fig 1-3 | Fig 1-3 | |||
| BV-234UT | RFMS 5 | 45,300* Fig 1-3 | 41,500* Fig 1-3 | 51,000 | *Values are lesser of performance gross weight limit or structural limit. |
| BV-107-II | RFMS 13-RDE-0532, Comp MRB | 18,500 Fig 4-9 | 17,000 Fig 4-9 | 22,000 | |
| CT58-140-1 or -2 | |||||
| KV-107-II | RFM KV-107-II, Fiberglass Rotor Blades | 18,500 | 17,000 | 22,000 | |
| CT58-140-1 or -2 | Fig 4-9 | Fig 4-9 | |||
| CH-46E | RFM, TC: R0013DE, T58-GE-16A | 22,050 Fig 5-3, 5-5, 5-9 | 20,200 Fig 5-3, 5-5, 5-9 | 24,300 | |
| S-64E | RFM SA4045-104, 100% Nr | 38,700* Fig 4-5, 1-3 | 34,500* Fig 4-5, 1-3 | 42,000* Fig 1-3 | *GW Limit: Maximum Mode III Gross Weight |
| S-64E CMRB | RFMS-024, OGE 100% Nr | 41,700 | 36,300 | 42,000* | *GW Limit: Maximum Mode III Gross Weight |
| Fig 1-3, 4-5 | Fig 1-3, 4-5 | Fig 1-3 | |||
| S-64F | RFM SA4047-5, 100% Nr | 41,500* Fig 4-22, 4-4, 1-3 | 36,400* Fig 4-22, 4-4, 1-3 | 47,000* Fig 1-3 | *GW Limit: Maximum Mode III Gross Weight |
| S-64F CMRB | RFMS-017, OGE 100% Nr | 46,850 | 42,750 | 47,000* | *GW Limit: Maximum Mode III Gross Weight |
| Fig 1-3, 4-4 | Fig 1-3, 4-4 | Fig 1-3 | |||
| CH-54A | RFM HTS-110, SHI-102, EHI-110 | 38,700 Fig 5-7 | 35,100 Fig 5-7 | 42,000* | *GW Limit: Maximum Mode III Gross Weight |
| CH-54A CMRB | HTS-FMS-CMB-01A | 41,700 Fig 5-8 | 36,300 Fig 3 | 42000* | *GW Limit: Maximum Mode III Gross Weight |
| CH-54B | RFM HTS-210 | 42,000 | 38,500 Fig 5-7 | 47,000* | *GW Limit: Maximum Mode III Gross Weight |
| Fig 5-7 | |||||
| CH-54B CMRB | HTS-FMS-CMB-01B | 46,850 | 42,750 | 47000* | *GW Limit: Maximum Mode III Gross Weight |
| Fig 5-6 | Fig 5-6 |
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