J.2_Schedule_B._Pricing_Schedule.xlsx
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- Beechcraft King Air 350 for NOAA AOC
- Solicitation number
- 1305M219RNMAN0004
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Solicitation: 1305M219RNMAN0004 Attachment: J.2 CLIN 0001: New Beechcraft King Air 350, Twin Engine Turboprop, Aircraft modified and configured in accordance with the Statement of Work (SOW).
| NOTE: Only one aircraft, King Air 350 ('Slick'), King Air 350C, or King Air 350CER, will be ordered as part of CLIN 0001, which will be determined at time of award. | |
| Notional Approach | $ |
| 0001A | King Air 350 ('Slick') | $ | 0001B | KIng Air 350C (with OEM Cargo Door option, without HW heavyweight certification) | $ | 0001C | King Air 350 CER (with OEM Cargo Door and Extended Range fuel tanks, includes HW heavyweight certification) | $ |
| Options list for modified King Air 350 ('Slick') | Options list for modified King Air 350C (non-HW) | Options list for modified King Air 350CER | ||||||
| 0001A.1 | 0300 Worldwide Weather and ACARS In-Flight Communication | $ | 0001B.1 | 0300 Worldwide Weather and ACARS In-Flight Communication | $ | 0001C.1 | 0300 Worldwide Weather and ACARS In-Flight Communication | $ |
| 0001A.2 | 0310 United States Weather | $ | 0001B.2 | 0310 United States Weather | $ | 0001C.2 | 0310 United States Weather | $ |
| 0001A.3 | 0290 AXXESS II System with Wireless Handset accessibility + Wi-Fi (International) | $ | 0001B.3 | 0290 AXXESS II System with Wireless Handset accessibility + Wi-Fi (International) | $ | 0001C.3 | 0290 AXXESS II System with Wireless Handset accessibility + Wi-Fi (International) | $ |
| 0001A.4 | Aftermarket cargo door | $ | 0001B.4 | Not Applicable | $ | 0001C.4 | Not Applicable | $ |
| 0001A.5 | Wing hardpoint set (one hardpoint on each wing) and wiring to support pylons and science probes | $ | 0001B.5 | Wing hardpoint set (one hardpoint on each wing) and wiring to support pylons and science probes | $ | 0001C.5 | Wing hardpoint set (one hardpoint on each wing) and wiring to support pylons and science probes | $ |
| 0001A.6 | Modification for two upward looking ports for temporary antenna installation or passive sensors. | $ | 0001B.6 | Modification for two upward looking ports for temporary antenna installation or passive sensors. | $ | 0001C.6 | Modification for two upward looking ports for temporary antenna installation or passive sensors. | $ |
| 0001A.7 | Modification for a small (approx 7.5 inch square) downward looking port in the cabin. | $ | 0001B.7 | Modification for a small (approx 7.5 inch square) downward looking port in the cabin. | $ | 0001C.7 | Modification for a small (approx 7.5 inch square) downward looking port in the cabin. | $ |
| 0001A.8 | Modification for a downward looking port in center of cabin flooring and aft of the wing spar that penetrates aircraft skin, identical in location, size and capabilities to the existing port in FM-21. | $ | 0001B.8 | Modification for a downward looking port in center of cabin flooring and aft of the wing spar that penetrates aircraft skin, identical in location, size and capabilities to the existing port in FM-21. | $ | 0001C.8 | Modification for a downward looking port in center of cabin flooring and aft of the wing spar that penetrates aircraft skin, identical in location, size and capabilities to the existing port in FM-21. | $ |
| 0001A.9 | Modification for a downward looking port in the cabin flooring and aft of the forward port (if either forward port option is selected) or in the same location as the aft port in FM-21 (if no forward port is selected), that penetrates aircraft skin, identical in size and capabilities to the existing port in FM-21. | $ | 0001B.9 | Modification for a downward looking port in the cabin flooring and aft of the forward port (if either forward port option is selected) or in the same location as the aft port in FM-21 (if no forward port is selected), that penetrates aircraft skin, identical in size and capabilities to the existing port in FM-21. | $ | 0001C.9 | Modification for a downward looking port in the cabin flooring and aft of the forward port (if either forward port option is selected) or in the same location as the aft port in FM-21 (if no forward port is selected), that penetrates aircraft skin, identical in size and capabilities to the existing port in FM-21. | $ |
| 0001A.10 | Modification to accommodate a Gamma Sensor System, the RSI RSX-5, in approximately the same location as the forward downlooking port on FM-21 (centerline, aft of the wing spar). | $ | 0001B.10 | Modification to accommodate a Gamma Sensor System, the RSI RSX-5, in approximately the same location as the forward downlooking port on FM-21 (centerline, aft of the wing spar). | $ | 0001C.10 | Modification to accommodate a Gamma Sensor System, the RSI RSX-5, in approximately the same location as the forward downlooking port on FM-21 (centerline, aft of the wing spar). | $ |
| 0001A.11 | Optical port capability for the forward gamma sensor port. | $ | 0001B.11 | Optical port capability for the forward gamma sensor port. | $ | 0001C.11 | Optical port capability for the forward gamma sensor port. | $ |
| 0001A.12 | Modification to accommodate a Gamma Sensor System, the RSI RSX-5, in approximately the same location as the aft downlooking port on FM-21 (across from the entry door, not necessarily on the centerline). | $ | 0001B.12 | Modification to accommodate a Gamma Sensor System, the RSI RSX-5, in approximately the same location as the aft downlooking port on FM-21 (across from the entry door, not necessarily on the centerline). | $ | 0001C.12 | Modification to accommodate a Gamma Sensor System, the RSI RSX-5, in approximately the same location as the aft downlooking port on FM-21 (across from the entry door, not necessarily on the centerline). | $ |
| 0001A.13 | Optical port capability for the aft gamma sensor port. | $ | 0001B.13 | Optical port capability for the aft gamma sensor port. | $ | 0001C.13 | Optical port capability for the aft gamma sensor port. | $ |
| CLIN 0002: Discounts for Spare parts, supplies, and additional infrastructure (e.g. racks, seats, etc. in addition to initial order under CLIN 0001 and 1001) as specified in the SOW. |
| New Parts Discount: _________% from cost |
| Overhauled Parts Discount: _________% from cost |
| Materials Discount: _________% from cost |
| *Offeror can include other discounts, if applicable. |
| CLIN 0003: Rates for Suggested Services, including training and additional engineering support as described in the SOW |
| Services |
| Regular Loaded Labor Rate: $____________/per hour |
| Overtime Loaded Labor Rate: $____________/per hour |
| *Labor Rates will be incorporated into resulting contract |
| **If more than one labor category is applicable, offeror is to provide Labor Rates for all applicable labor categories. |
| Training | |
| Provide Pricing for Suggested Training (e.g. pilot, mechanic, technical, etc.) for delivery of CLIN 0001 & Option CLIN 1001 | |
| $________________ | |
| *Provide Suggested Training as Appropriate |
| CLIN 1001: New Beechcraft King Air 350, Twin Engine Turboprop, Aircraft modified and configured in accordance with the Statement of Work (SOW). |
| NOTE: Only one aircraft, King Air 350 ('Slick'), King Air 350C, or King Air 350CER, will be ordered as part of CLIN 1001, which will be determined at time of award. |
Optional CLIN, if exercised, will be exercised within five (5) years of contract award
| Notional Approach with final year inflation added. | $ | ||
| 1001A | King Air 350 ('Slick') | % increase per year from CLIN 0001A: |
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B KIng Air 350C (with OEM Cargo Door option, without HW heavyweight certification) % increase per year from CLIN 0001B:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C King Air 350 CER (with OEM Cargo Door and Extended Range fuel tanks, includes HW heavyweight certification) % increase per year from CLIN 0001C:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
| Options list for modified King Air 350 ('Slick') | Options list for modified King Air 350C (non-HW) | Options list for modified King Air 350CER | ||
| 1001A.1 | 0300 Worldwide Weather and ACARS In-Flight Communication | % increase per year from CLIN 0001A.1: |
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B.1 0300 Worldwide Weather and ACARS In-Flight Communication % increase per year from CLIN 0001B.1:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C.1 0300 Worldwide Weather and ACARS In-Flight Communication % increase per year from CLIN 0001C.1:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
1001A.2 0300 Worldwide Weather and ACARS In-Flight Communication % increase per year from CLIN 0001A.2:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B.2 0300 Worldwide Weather and ACARS In-Flight Communication % increase per year from CLIN 0001B.2:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C.2 0300 Worldwide Weather and ACARS In-Flight Communication % increase per year from CLIN 0001C.2:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
1001A.3 0290 AXXESS II System with Wireless Handset accessibility + Wi-Fi (International) % increase per year from CLIN 0001A.3:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B.3 0290 AXXESS II System with Wireless Handset accessibility + Wi-Fi (International) % increase per year from CLIN 0001B.3:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C.3 0290 AXXESS II System with Wireless Handset accessibility + Wi-Fi (International) % increase per year from CLIN 0001C.3:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
1001A.4 Aftermarket cargo door % increase per year from CLIN 0001A.4:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B.4 Aftermarket cargo door % increase per year from CLIN 0001B.4:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C.4 Aftermarket cargo door % increase per year from CLIN 0001B.4:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
1001A.5 Wing hardpoint set (one hardpoint on each wing) and wiring to support pylons and science probes % increase per year from CLIN 0001A.5:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B.5 Wing hardpoint set (one hardpoint on each wing) and wiring to support pylons and science probes % increase per year from CLIN 0001B.5:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C.5 Wing hardpoint set (one hardpoint on each wing) and wiring to support pylons and science probes % increase per year from CLIN 0001C.5:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
1001A.6 Modification for two upward looking ports for temporary antenna installation or passive sensors. % increase per year from CLIN 0001A.6:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B.6 Modification for two upward looking ports for temporary antenna installation or passive sensors. % increase per year from CLIN 0001B.6:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C.6 Modification for two upward looking ports for temporary antenna installation or passive sensors. % increase per year from CLIN 0001C.6:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
1001A.7 Modification for a small (approx 7.5 inch square) downward looking port in the cabin. % increase per year from CLIN 0001A.7:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B.7 Modification for a small (approx 7.5 inch square) downward looking port in the cabin. % increase per year from CLIN 0001B.7:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C.7 Modification for a small (approx 7.5 inch square) downward looking port in the cabin. % increase per year from CLIN 0001C.7:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
1001A.8 Modification for a downward looking port in center of cabin flooring and aft of the wing spar that penetrates aircraft skin, identical in location, size and capabilities to the existing port in FM-21. % increase per year from CLIN 0001A.8:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B.8 Modification for a downward looking port in center of cabin flooring and aft of the wing spar that penetrates aircraft skin, identical in location, size and capabilities to the existing port in FM-21. % increase per year from CLIN 0001B.8:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C.8 Modification for a downward looking port in center of cabin flooring and aft of the wing spar that penetrates aircraft skin, identical in location, size and capabilities to the existing port in FM-21. % increase per year from CLIN 0001C.8:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
1001A.9 Modification for a downward looking port in the cabin flooring and aft of the forward port (if either forward port option is selected) or in the same location as the aft port in FM-21 (if no forward port is selected), that penetrates aircraft skin, identical in size and capabilities to the existing port in FM-21. % increase per year from CLIN 0001A.9:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B.9 Modification for a downward looking port in the cabin flooring and aft of the forward port (if either forward port option is selected) or in the same location as the aft port in FM-21 (if no forward port is selected), that penetrates aircraft skin, identical in size and capabilities to the existing port in FM-21. % increase per year from CLIN 0001B.9:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C.9 Modification for a downward looking port in the cabin flooring and aft of the forward port (if either forward port option is selected) or in the same location as the aft port in FM-21 (if no forward port is selected), that penetrates aircraft skin, identical in size and capabilities to the existing port in FM-21. % increase per year from CLIN 0001C.9:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
1001A.10 Modification to accommodate a Gamma Sensor System, the RSI RSX-5, in approximately the same location as the forward downlooking port on FM-21 (centerline, aft of the wing spar). % increase per year from CLIN 0001A.10:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B.10 Modification to accommodate a Gamma Sensor System, the RSI RSX-5, in approximately the same location as the forward downlooking port on FM-21 (centerline, aft of the wing spar). % increase per year from CLIN 0001B.10:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C.10 Modification to accommodate a Gamma Sensor System, the RSI RSX-5, in approximately the same location as the forward downlooking port on FM-21 (centerline, aft of the wing spar). % increase per year from CLIN 0001C.10:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
1001A.11 Optical port capability for the forward gamma sensor port. % increase per year from CLIN 0001A.11:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B.11 Optical port capability for the forward gamma sensor port. % increase per year from CLIN 0001B.11:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C.11 Optical port capability for the forward gamma sensor port. % increase per year from CLIN 0001C.11:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
1001A.12 Modification to accommodate a Gamma Sensor System, the RSI RSX-5, in approximately the same location as the aft downlooking port on FM-21 (across from the entry door, not necessarily on the centerline). % increase per year from CLIN 0001A.12:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B.12 Modification to accommodate a Gamma Sensor System, the RSI RSX-5, in approximately the same location as the aft downlooking port on FM-21 (across from the entry door, not necessarily on the centerline). % increase per year from CLIN 0001B.12:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C.12 Modification to accommodate a Gamma Sensor System, the RSI RSX-5, in approximately the same location as the aft downlooking port on FM-21 (across from the entry door, not necessarily on the centerline). % increase per year from CLIN 0001C.12:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
1001A.13 Optical port capability for the aft gamma sensor port. % increase per year from CLIN 0001A.13:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001B.13 Optical port capability for the aft gamma sensor port. % increase per year from CLIN 0001B.13:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________% 1001C.13 Optical port capability for the aft gamma sensor port. % increase per year from CLIN 0001C.13:
YR2: ________%
YR3: ________%
YR4: ________%
YR5: ________%
| CLIN 2001 | Standardization upgrades and modifications, to include the avionics upgrade, for NOAA's King Air 350CER aircraft, serial number FM-21, FAA registration N68RF. The intent of this CLIN is for the required modifications to modify NOAA's King Air 350CER aircraft with serial number FM-21 so that it copies, as close as practicable, the cabin layout, instrumentation and avionics package of the CLIN 0001 aircraft. | |
| $________________________ | ||
| % increase per year from CLIN 2001: | ||
| YR2: ________% | ||
| YR3: ________% | ||
| YR4: ________% | ||
| YR5: ________% |
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