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

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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SF1449 First Page Only.pdf PDF
Type 3 On Ramp QA_10_2_2025_FINAL.pdf PDF
1202SA22R9203 Amendment 0012.pdf PDF

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PLEASE READ INSTRUCTIONS

Pricing Workbook and B.2 Schedule of Items INSTRUCTIONS
Aircraft Type OfferedType 3Solicitation No.1202SA22R92031202SA22R9201
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 NameEnter 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/SeriesSelect 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 RateHourly Flight Rate will be automatically entered from the correct row in "Attachment 10" worksheet when the correct Make/Model/Series is selected.
Standard/RestrictedUse the drop-down list to select "Standard" or "Restricted"as appropriate.
Make and Model of EquipmentEnter 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 WeightWeight 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 AircraftSolicitation No.1202SA22R9203
Aircraft RequestedType 3
Offers Due DateSee Respective Solicitation
Contract Start Year2026
Contract Base1
Option Years1
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 DescriptionMake and ModelCapacity in Gallons
Tank
Hover to view B.4 (17)
JANET SULLIVAN:Bucket # 1
Bucket # 2
Call When Needed (CWN) Offer
Daily Availability Fire SuppressionAllowable Payload
JANET SULLIVAN:20262027
Bucket OfferAircraft 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 SuppressionAllowable Payload20262027
Tank OfferAircraft Equipped Weight (pounds)
Project Flight Rate (Hourly)Allowable Payload20262027
Bucket OfferAircraft Equipped Weight (pounds)
Bucket Weight
Project Flight Rate (Hourly)Allowable Payload20262027
Tank OfferAircraft 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.
NoALASKANoCARIBBEAN
NoCANADANoMEXICO

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:DescriptionCapacityQuantityUnit
(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 CodeDescriptionCostAccounting Method
ESExtended Standby (daily)$ 66.00* Min Crew * MAP
PDSubsistence Allowance (daily)$ 155.00* Min Crew * MAP
SCOther Charges$ 220.00100 * Estimated

Attachment 10

ATTACHMENT 10 - HELICOPTER SERVICES HOURLY FLIGHT RATES, FUEL CONSUMPTION, AND WEIGHT REDUCTION CHART
Effective May 16, 2025
COMPANYAIRCRAFT TYPEFUEL CONSUMPTIONMAY 16, 2025
HOURLY FLIGHT RATELOAD CALCULATION
(gal/hr)($/HR)Weight Reduction (lbs)
AIRBUS:SA 315B58$2,491.49180
AIRBUS:SA 316B58$2,491.49170
AIRBUS:SA 318C45$2,395.1780
AIRBUS:SA 319B45$2,396.29150
AIRBUS:AS 330J179$6,473.30N/A
AIRBUS:AS 332L1155$5,821.72550
AIRBUS:SA 341G45$2,333.33170
AIRBUS:AS 350B45$1,522.73130
AIRBUS:AS 350BA45$1,518.24130
AIRBUS:AS 350B145$1,521.61160
AIRBUS:AS 350B245$1,533.97160
AIRBUS:AS 350B344$1,513.85175
AIRBUS:AS 350B3e/H12544$1,482.37175
AIRBUS:AS 350D38$1,451.58130
AIRBUS:AS 355F158$1,798.94140
AIRBUS:AS 355F258$1,798.94140
AIRBUS:AS 365N187$2,954.74275
AIRBUS:BO 105CBS55$1,910.59180
AIRBUS:BK 11777$2,493.81160
AIRBUS:EC 12031$1,110.60NOT ESTABLISHED
AIRBUS:EC 130-B451$1,519.80NOT ESTABLISHED
AIRBUS:EC 13564$1,917.42220
AIRBUS:EC 135-P264$2,010.74NOT ESTABLISHED
AIRBUS:EC 135-P364$1,932.04NOT ESTABLISHED
AIRBUS:EC 14580$2,446.25220
AIRBUS:EC 145-T2/H 14583$2,402.06220
AIRBUS:EC 155B195$3,053.89NOT ESTABLISHED
AIRBUS:EC 225183$5,870.23650
BELL:47/Soloy (Scott's)23$979.98120
BELL:204B86$2,441.06200
BELL:204 Super B90$2,472.09200
BELL:205A188$2,410.48260
BELL:205 A1++90$2,425.99260
BELL:UH-1B86$2,394.97N/A
BELL:UH-1B Super88$2,410.48N/A
BELL:UH-1F88$2,480.19N/A
BELL:TH-1L88$2,410.48N/A
BELL:UH-1H (-13 engine)88$2,410.48N/A
BELL:UH-1H (-17 engine)90$2,425.99N/A
BELL:206BII25$1,145.02100
BELL:206BIII27$1,160.53130
BELL:206L132$1,385.94150
BELL:206L338$1,412.23180
BELL:206L438$1,412.23180
BELL:21090$2,425.99260
BELL:212100$2,739.64390
BELL:212HP100$2,739.64390
BELL:212 Single (Eagle)90$2,555.28260
BELL:214B160$4,172.96380
BELL:214B1145$3,896.99380
BELL:214ST133$5,088.96420
BELL:222A70$3,087.10NOT ESTABLISHED
BELL:222B83$3,187.92NOT ESTABLISHED
BELL:222UT83$3,187.92NOT ESTABLISHED
BELL:40744$1,494.74155
BELL:407HP (Eagle)44$1,462.14155
BELL:412110$2,800.33390
BELL:412HP110$2,800.33390
BELL: **REV 5/16/2025412EP110$2,800.33390
BELL:412EPX110$2,828.44390
BELL **REV 2/16/2542973$2,025.45135
BELL:50532$1,052.03130
BOEING:BV 107/CH 46180$5,644.59N/A
BOEING:BV 234/CH 47405$9,923.67N/A
HILLER:SL-3/420$866.7790
HILLER:H 1100B22$1,167.85130
HILLER:UH 12/Soloy23$983.35100
KAMAN:H43F85$2,243.31N/A
KAMAN:K-1200/K-Max86$2,800.83N/A
KAMOV:KA-32225$6,110.51NOT ESTABLISHED
LEONARDO HELICOPTERS:AW 119 KOALA55$1,739.70230
LEONARDO HELICOPTERS:AW 139129$3,678.46335
LEONARDO HELICOPTERS:EH 101211$7,191.41NOT ESTABLISHED
McDONNELL-DOUGLAS:500C23$1,172.23110
McDONNELL-DOUGLAS:500D/E28$1,211.01120
McDONNELL-DOUGLAS:520N32$1,221.79100
McDONNELL-DOUGLAS:530F34$1,395.82120
McDONNELL-DOUGLAS:600N41$1,516.44155
McDONNELL-DOUGLAS:900/90269$2,241.77210
ROBINSON:R 6624$915.78130
SIKORSKY:S 55T47$1,638.30170
SIKORSKY:S 58D/E83$2,653.90N/A
SIKORSKY:S 58T/PT6T-3115$3,372.01400
SIKORSKY:S 58T/PT6T-6115$3,372.01460
SIKORSKY:CH 53D425$9,571.73N/A
SIKORSKY:CH 54A/S 64E493$10,133.95N/A
SIKORSKY:CH 54B/S 64F512$10,281.30N/A
SIKORSKY:H 3/S 61 All Series170$5,896.45550
SIKORSKY:S 62A70$1,967.33300
SIKORSKY:S 70/UH 60135$5,687.97550
SIKORSKY:S 70/UH 60+135$5,815.01550
SIKORSKY:S 76A88$3,327.89NOT ESTABLISHED
SIKORSKY:S 76A+96$3,442.77NOT ESTABLISHED
SIKORSKY:S 76A++92$3,399.38NOT ESTABLISHED
SIKORSKY:S 76B111$3,418.57NOT ESTABLISHED
SIKORSKY:S 76C92$3,343.17NOT ESTABLISHED
SIKORSKY:S 76C+88$3,294.16NOT ESTABLISHED
SIKORSKY:S 76C++94$3,328.32NOT ESTABLISHED
SIKORSKY:S 92178$5,598.73NOT 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 HELICOPTERMODEL
LOAD CALCULATION
OAS-67/FS 5700-17 (11/03)N#
PILOT(S)DATE
MISSIONTIME
1DEPARTUREPAOAT
2DESTINATIONPAOAT
3HELICOPTER EQUIPPED WEIGHT
4FLIGHT CREW WEIGHT
5FUEL WT ( _gallons X 7 lbs per gal)
6OPERATING WEIGHT (3 + 4 + 5)
Non-JettisonableJettisonable
HIGEHOGEHOGE-J
7aPERFORMANCE REF

(List page/chart from FM)

7b COMP GROSS WT (FM Performance section)

8WT REDUCTION
(Req for all Non-Jettisonable)
9ADJUSTED WEIGHT
(7b minus 8)
10GROSS WT LIMIT

(FM Limitations Section)

11SELECTED WEIGHT
(Lowest of 9 or 10)
12OPERATING WEIGHT
((From Line 6)
13ALLOWABLE PAYLOAD
(11 minus 12)
14PASSENGERS/CARGO MANIFEST
15ACTUAL PAYLOAD (Total of all weights listed in item 14) Line 15 must not exceed Line 13 for the intended mission
PILOT SIGNATUREHazMat
MGR SIGNATUREYes 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 D1202SA22R9203/0009 ConformedNational Interagency Fire Center (NIFC)
ATTACHMENT 19 - COMPUTED GROSS WEIGHT TABLE FOR TYPE 1 AIRCRAFT (B.3(a), Attachment 11) – 4/12/2025
AircraftLine 7a: Performance ReferenceLine 7a: Computed Gross Weight HOGE-JLine 10: LimitationsNotes
5,000/30 7,750 ft DA8,000/25 11,000 ft DA
S-58TSTC SR09584RC, PT6T-6, Max Take Off Power, 100% Nr, No Anti-Abrasion Strips13,000 Fig 1-3, RFM11,300 Fig 2, STC13,000Ref STC Fig 1 for internal Non-J Line 10 WAT Limits
S-58TSTC SR09584RC, PT6T-6, Max Take Off Power, 93% Nr, No Anti-Abrasion Strips13,000 Fig 1-3, RFM10,900 Fig 2, STC13,000Ref STC Fig 1 for internal Non-J Line 10 WAT Limits
S-58TSTC 4570NM, PT6T-6, Max Take Off Power, 93-100% Nr, No Ant-Abrasion Strips13,000 Fig 1-3, RFM11,300 Fig 7-1-1A Sup 713,000Ref STC Fig 1 for internal Non-J Line 10 WAT Limits
S-58TSTC 4570NM, PT6T-3, Max Take Off Power, 93-100% Nr, No Ant-Abrasion Strips13,000 Fig 1-1, RFM11,300 Fig 7-1-1A Sup 713,000Ref STC Fig 1 for internal Non-J Line 10 WAT Limits
S-58TSTC 4570NM, PT6T-3, Max Take Off Power, 93-100% Nr, With Ant-Abrasion Strips13,000 Fig 1-1A, RFM11,300 Fig 7-1-1A Sup 713,000Ref STC Fig 1 for internal Non-J Line 10 WAT Limits
K-1200FMS No. 1, USFS Fire Fighting11,400 Fig S1-1, S1-5, S1-1110,300 Fig S1-1, S1-5, S1-1112,000Does not consider excess power available Ref FSM No. 1 Figure S1-6 as GW varies with Alt
K-1200Basic Flight Manual9,800 Fig 5-1, 5-5, 5-88,700 Fig 5-1, 5-5, 5-812,000Does not consider excess power available Ref FM Figure 5-6 as GW varies with Alt
AS-332 LRFM Sect 517,30015,70020,610WAT limit for HIGE and HOGE
Fig 5Fig 5Ref Fig 1a, RFM.
AS-332 L1Flight Manual Sup.10.618,250 Fig 216,645 Fig 220,610WAT limit for HIGE and HOGE
Ref Fig 1a, RFM.
S-61A, CompositeCT58-GE-100, RFMS 2019,60018,00022,000
MRB & TRBFig B-3, Fig 2Fig B-3, Fig 2
SK-61A, CompositeCarson STC SR01585NY, RFMS #10 S61 A/V, CT58-140-1, -217,500 Fig 1, Fig 516,200 Fig 1, Fig 522,000
MRB 100% Nr
SK-61A, Composite MRB, 103% NrCarson STC SR01585NY, RFMS #10 S61 A/V, CT58-140-1, -217,400 Fig 1, Fig 616,100 Fig 1, Fig 622,000
S-61 A/V, Composite MRB, 100% NrCarson STC SR01585NY, RFMS #10 S61 A/V, CT58-140-1, -217,500 Fig 1, Fig 516,200 Fig 1, Fig 522,000
S-61 A/V, Composite MRB, 103% NrCarson STC SR01585NY, RFMS #10 S61 A/V, CT58-140-1, -217,400 Fig 1, Fig 616,100 Fig 1, Fig 622,000
S-61 A/V, CompositeCT58-GE-140 (RFMS 10), RFMS 20 (CM&TRB)17,75016,60022,000
MRB & TRB, 106% NrFig 1, Fig 1&2Fig 1, Fig 1&2
AircraftLine 7a: Performance ReferenceLine 7a: Computed Gross Weight HOGE-JLine 10: LimitationsNotes
5,000/30 7,750 ft DA8,000/25 11,000 ft DA
S-61 L/N/NM, Composite MRB, 100% NrCarson STC SR01585NY, RFMS #6 S61 L/N/NM, CT58-140-1, -217,500 Fig 1, Fig 516,200 Fig 1, Fig 522,000
S-61 L/N/NM, Composite MRB, 103% NrCarson STC SR01585NY, RFMS #6 S61 L/N/NM, CT58-140-1, -217,500 Fig 1, Fig 616,200 Fig 1, Fig 622,000
S-61 L/N/NM, Composite MRB, 100% NrCarson STC SR01585NY, RFMS #7, L/N NM, CT-58-140-1, -217,400 Fig 7-4-2616,000 Fig 7-4-2622,000
S-61 A, Composite MRB, 105% NrCarson STC SR01585NY, RFMS-S61A-1,20,200 Fig 11-6A, 11-10a18,300 Fig 11-6A, 11-10a21,000
T58-GE-402
S-61 A, CompositeCarson STC SR01585NY & SR04122NY, RFMS-S61A-4, T58-GE-40220,200 Fig 11-6A, 11-10b18,500 Fig 11-6A, 11-10b21,000
MRB & TRB, 105% Nr
S-61 A, CompositeCarson STC SR01585NY & SR04122NY, RFMS-S61A-1, T58-GE-40220,200 Fig 11-6A, 11-10b18,500 Fig 11-6A, 11-10b21,000
MRB & TRB, 105% Nr
SH-3H, CompositeCarson STC SR01585NY, RFMS-SH3H-2,20,200 Fig 20-16, 21-3c18,300 Fig 20-16, 21-3c21,000
MRB, 105% NrT58-GE-402
SH-3H, CompositeCarson STC SR01585NY & SR04122NY, RFMS-SH3H-2 Rev B, T58-GE-40220,200 Fig 20-16, 21-3d18,500 Fig 20-16, 21-3d21,000
MRB & TRB, 105% Nr
H-60A, @ ATF .90RFM, 30-min, T700-GE-70016,700 Fig 7-2, 7-3, 7-415,250 Fig 7-2, 7-3, 7-422,000No 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 .95RFM, 30-min, T700-GE-70017,250 Fig 7-2, 7-3, 7-415,800 Fig 7-2, 7-3, 7-422,000
H-60A, @ ATF .95 BLRRFM, 30-min, T700-GE-70017,54516,12122,000
RFMS-UH60FF-1RFM Fig 7-2, 7-3RFM Fig 7-2, 7-3
RFMS Fig 7-4.2 sheetsRFMS Fig 7-4.2 sheets
24 and 26 of 4218 and 20 of 42
H-60A, @ ATF .96RFM, 30-min, T700-GE-70017,350 Fig 7-2, 7-3, 7-415,950 Fig 7-2, 7-3, 7-422,000
H-60A, @ATF .97RFM, 30-min, T700-GE-70017,45016,00022,000
Fig 7-2, 7-3, 7-4Fig 7-2, 7-3, 7-4
AircraftLine 7a: Performance ReferenceLine 7a: Computed Gross Weight HOGE-JLine 10: LimitationsNotes
5,000/30 7,750 ft DA8,000/25 11,000 ft DA
H-60A, @ATF .97 BLRRFM, 30-min, T700-GE-70017,77316,28822,000No HIRRS: add +1 to Specification Torque Available
RFMS-UH60FF-1RFM Fig 7-2, 7-3RFM Fig 7-2, 7-3per Engine % (Fig 7-3) per RFM Specific Q calculated via math
RFMS Fig 7-4.2 sheetsRFMS Fig 7-4.2 sheets(Fig 7-3) per RFM: Spec Q x TR = Q avail Transmission limited to 100%
24 and 26 of 4218 and 20 of 42BLR linear interpolate via supplement direction
H-60A, @ ATF .98RFM, 30-min, T700-GE-70017,625 Fig 7-2, 7-3, 7-416,125 Fig 7-2, 7-3, 7-422,000
H-60A, @ ATF 1.0RFM, 30-min, T700-GE-70017,800 Fig 7-2, 7-3, 7-416,250 Fig 7-2, 7-3, 7-422,000
H-60A+ @ ATF .90RFM, 10-min, T700-GE-701C or18,950 Fig 7A-2, 7A-4, 7A-617,350 Fig 7A-2, 7A-4, 7A-622,000No HIRRS: add +1 to Torque Available per Engine % (Fig 7A-4) per RFM Actual Q calculated via
T700-GE-701D/CCmath per RFM: Spec Q x TR = Q avail *Transmission limited to 100%
H-60A+ @ ATF .95RFM, 10-min, T700-GE-19,500 Fig 7A-2, 7A-4, 7A-617,800 Fig 7A-2, 7A-4, 7A-622,000BLR linear interpolation via supplement direction
orT700-GE-701D/CC
H-60A+ @ ATF .95 BLRRFM, 10-min, T700-GE-701C or20,06218,29722,000
T700-GE-701D/CCRFM Fig 7A-2, 7A-4RFM Fig 7A-2, 7A-4
RFMS-UH60FF-1RFMS Fig 7A-6.2 sheetsRFMS Fig 7A-6.2 sheets
34 and 36 of 4826 and 28 of 48
H-60A+ @ ATF .96RFM, 10-min, T700-GE-701C or19,650* Fig 7A-2, 7A-4, 7A-617,850 Fig 7A-2, 7A-4, 7A-622,000
T700-GE-701D/CC
H-60A+ @ATF .97RFM, 10-min, T700-GE-701C or19,650* Fig 7A-2, 7A-4, 7A-617,95022,000
T700-GE-701D/CCFig 7A-2, 7A-4, 7A-6
H-60A+ @ATF .97 BLRRFM, 10-min, T700-GE-701C or20,17118,48022,000
T700-GE-701D/CCRFM Fig 7A-2, 7A-4RFM Fig 7A-2, 7A-4
RFMS-UH60FF-1RFMS Fig 7A-6.2 sheetsRFMS Fig 7A-6.2 sheets
34 and 36 of 4826 and 28 of 48
H-60A+ @ ATF .98RFM, 10-min, T700-GE-701C or19,650* Fig 7A-2, 7A-4, 7A-618,100 Fig 7A-2, 7A-4, 7A-622,000
T700-GE-701D/CC
H-60A+ @ ATF .98 BLRRFM, 10-min, T700-GE-701C or20,17018,57122,000
T700-GE-701D/CCRFM Fig 7A-2, 7A-4RFM Fig 7A-2, 7A-4
RFMS-UH60FF-1RFMS Fig 7A-6.2 sheetsRFMS Fig 7A-6.2 sheets
34 and 36 of 4828 and 30 of 48
H-60A+ @ ATF 1.0RFM, 10-min, T700-GE-701C or19,650* Fig 7A-2, 7A-4, 7A-618,250 Fig 7A-2, 7A-4, 7A-622,000
T700-GE-701D/CC
AircraftLine 7a: Performance ReferenceLine 7a: Computed Gross Weight HOGE-JLine 10: LimitationsNotes
5,000/30 7,750 ft DA8,000/25 11,000 ft DA
H-60A+ @ ATF 1.0 BLRRFM, 10-min, T700-GE-701C or20,17018,74022,000No HIRRS: add +1 to Torque Available
T700-GE-701D/CCFig 7A-6.7, sheet 4 of 11Fig 7A-6.7, sheet 7 of 11per 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-1BLR linear interpolation via supplement direction
H-60L @ ATF .90RFM, 10-min, T700-GE-701C or T700-GE-701D/CC18,950 Fig 7A-2, 7A-4, 7A-617,350 Fig 7A-2, 7A-4, 7A-623,500
H-60L @ ATF .95RFM, 10-min, T700-GE-701C19,500 Fig 7A-2, 7A-4, 7A-617,800 Fig 7A-2, 7A-4, 7A-623,500
T700-GE-701D/CC
H-60L @ ATF .95 BLRRFM, 10-min, T700-GE-701C20,06218,29723,500
T700-GE-701D/CCRFM Fig 7A-2, 7A-4RFM Fig 7A-2, 7A-4
RFMS-UH60FF-1RFMS Fig 7A-6.2 sheetsRFMS Fig 7A-6.2 sheets
34 and 36 of 4826 and 28 of 48
H-60L @ ATF .96RFM, 10-min, T700-GE-701C19,700 Fig 7A-2, 7A-4, 7A-617,850 Fig 7A-2, 7A-4, 7A-623,500
T700-GE-701D/CC
H-60L @ ATF .97RFM, 10-min, T700-GE-701C19,75017,95023,500
T700-GE-701D/CCFig 7A-2, 7A-4, 7A-6Fig 7A-2, 7A-4, 7A-6
H-60L @ ATF .97 BLRRFM, 10-min, T700-GE-701C20,30318,48023,500
T700-GE-701D/CCRFM Fig 7A-2, 7A-4RFM Fig 7A-2, 7A-4
RFMS-UH60FF-1RFMS Fig 7A-6.2 sheetsRFMS Fig 7A-6.2 sheets
34 and 36 of 4826 and 28 of 48
H-60L @ ATF .98RFM, 10-min, T700-GE-701C19,850 Fig 7A-2, 7A-4, 7A-618,100 Fig 7A-2, 7A-4, 7A-623,500
T700-GE-701D/CC
H-60L @ ATF .98 BLRRFM, 10-min, T700-GE-701C20,43418,57123,500
T700-GE-701D/CCRFM Fig 7A-2, 7A-4RFM Fig 7A-2, 7A-4
RFMS-UH60FF-1RFMS Fig 7A-6.2 sheetsRFMS Fig 7A-6.2 sheets
34 and 36 of 4828 and 30 of 48
H-60L @ ATF 1.0RFM, 10-min, T700-GE-701C20,100 Fig 7A-2, 7A-4, 7A-618,250 Fig 7A-2, 7A-4, 7A-623,500
T700-GE-701D/CC
H-60L @ ATF 1.0 BLRRFMS-UH60FF-120,70018,74023,500
Fig 7A-6.5Fig 7A-6.5
sheet 4 of 11sheet 7 of 11
AircraftLine 7a: Performance ReferenceLine 7a: Computed Gross Weight HOGE-JLine 10: LimitationsNotes
5,000/30 7,750 ft DA8,000/25 11,000 ft DA
S-70A @ ATF .90RFM 55-1520-237-10HK, 10-min,18,850 Fig 7-2, 7-4,7-517,250 Fig 7-2, 7-4,7-523,500No 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 .95RFM 55-1520-237-10HK, 10-min19,500 Fig 7-2, 7-4,7-517,700 Fig 7-2, 7-4,7-523,500
T700-GE-701C
S-70A @ ATF .96RFM 55-1520-237-10HK, 10-min19,650 Fig 7-2, 7-4,7-517,750 Fig 7-2, 7-4,7-523,500
T700-GE-701C
S-70A @ ATF .98RFM 55-1520-237-10HK, 10-min19,750* Fig 7-2, 7-4,7-518,000 Fig 7-2, 7-4,7-523,500
T700-GE-701C
S-70A @ ATF 1.0RFM 55-1520-237-10HK, 10-min20,000* Fig 7-2, 7-4,7-518,150 Fig 7-2, 7-4,7-523,500
T700-GE-701C
S-70CTM 1-1520-237-10B, 10-min19,000 Fig 7-3, 7-617,500 Fig 7-3, 7-622,000No HIRRS: added 1.3% Torque to Torque Available Transmission limited to 100%
T700-GE-701A
S-70C @ ATF .95 BLRRFM H60A, 30-min, T700-GE-70017,54516,12122,000No HIRRS: add +1 to torque Available per, Engine % (Fig 7A-4) per H60 RFM,
RFMS-UH60FF-1RFM Fig 7-2, 7-3RFM Fig 7-2, 7-3Actual Q calculated via, math per
RFMS Fig 7-4.2 sheetsRFMS Fig 7-4.2 sheetsH60 RFM: Spec Q x TR = Q avail *Transmission limited to 100%
24 and 26 of 4218 and 20 of 42BLR linear interpolation via supplement direction
S-70C @ ATF .97 BLRRFM H60A, 30-min, T700-GE-70017,77316,28822,000
RFMS-UH60FF-1RFM Fig 7-2, 7-3RFM Fig 7-2, 7-3
RFMS Fig 7-4.2 sheetsRFMS Fig 7-4.2 sheets
24 and 26 of 4218 and 20 of 42
CH-47D 30-min PTITBFS-510 Rev 145,500*41,600*50,000*Values are lesser of either performance gross weight limit or structural limit.
30-min PTIT LimitFig 5-4, 5-7Fig 5-4, 5-7
CH-47D 10-min PTIT**BFS-510, T55-GA-71447,000* Fig 5-6, 5-1042,000* Fig 5-6, 5-1050,000**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, 7-1042,000* Fig 7-6, 7-1050,000**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 248,75044,50050,000**If RFM authorizes, otherwise use 30-min limit
10-min PTIT LimitFig 5-6Fig 5-6
CH-47D 10-minBFS-610 rev IR48,72044,30054,000
10-minFig 8.5-2Fig 8.5-2
AircraftLine 7a: Performance ReferenceLine 7a: Computed Gross Weight HOGE-JLine 10: LimitationsNotes
5,000/30 7,750 ft DA8,000/25 11,000 ft DA
BV-234LRRFMS 543,100* Fig 1-339,500* Fig 1-351,000*Values are lesser of performance gross weight limit or structural limit.
BV-234LRColumbia Helicopters43,100*39,500*51,000*Values are lesser of performance gross weight limit or structural limit.
RFMS BV-234 LR/UTFig 1-3Fig 1-3
BV-234UTRFMS 545,300* Fig 1-341,500* Fig 1-351,000*Values are lesser of performance gross weight limit or structural limit.
BV-107-IIRFMS 13-RDE-0532, Comp MRB18,500 Fig 4-917,000 Fig 4-922,000
CT58-140-1 or -2
KV-107-IIRFM KV-107-II, Fiberglass Rotor Blades18,50017,00022,000
CT58-140-1 or -2Fig 4-9Fig 4-9
CH-46ERFM, TC: R0013DE, T58-GE-16A22,050 Fig 5-3, 5-5, 5-920,200 Fig 5-3, 5-5, 5-924,300
S-64ERFM SA4045-104, 100% Nr38,700* Fig 4-5, 1-334,500* Fig 4-5, 1-342,000* Fig 1-3*GW Limit: Maximum Mode III Gross Weight
S-64E CMRBRFMS-024, OGE 100% Nr41,70036,30042,000**GW Limit: Maximum Mode III Gross Weight
Fig 1-3, 4-5Fig 1-3, 4-5Fig 1-3
S-64FRFM SA4047-5, 100% Nr41,500* Fig 4-22, 4-4, 1-336,400* Fig 4-22, 4-4, 1-347,000* Fig 1-3*GW Limit: Maximum Mode III Gross Weight
S-64F CMRBRFMS-017, OGE 100% Nr46,85042,75047,000**GW Limit: Maximum Mode III Gross Weight
Fig 1-3, 4-4Fig 1-3, 4-4Fig 1-3
CH-54ARFM HTS-110, SHI-102, EHI-11038,700 Fig 5-735,100 Fig 5-742,000**GW Limit: Maximum Mode III Gross Weight
CH-54A CMRBHTS-FMS-CMB-01A41,700 Fig 5-836,300 Fig 342000**GW Limit: Maximum Mode III Gross Weight
CH-54BRFM HTS-21042,00038,500 Fig 5-747,000**GW Limit: Maximum Mode III Gross Weight
Fig 5-7
CH-54B CMRBHTS-FMS-CMB-01B46,85042,75047000**GW Limit: Maximum Mode III Gross Weight
Fig 5-6Fig 5-6

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