1._Question_QCI_1_RE_NOAA_Configuration_Sheet.xlsx
XLSX spreadsheet 23 KB Posted
- Attached to
- Beechcraft King Air 350 for NOAA AOC
- Solicitation number
- 1305M219RNMAN0004
About this file
Vendor Qs (1 of 2)
View the file
Other files
Show all 14
On GovTribe
Work with this file
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
Sheet1
| CLIN | CLIN Description as recorded on installation review sheet | CLIN Description as recorded on contract amendments | Contract Mod | Date Added | Supplier | Assoc. Avcon Dwg No. | FM21 | RFP/SOW For New A/C | Notes |
| 0001 | King Air 350CER | Basic | 09/17/07 | HBC | Basic Aircraft | X | |||
| 0002 | Camera Ports 18-21 inch | Basic | 09/17/07 | Avcon | X | Both 21 inch | both to be identical size, location, and capabilities as FM-21 - except both are required to be 21 in diameter - clarification question drafted | ||
| 0003 | Provide and install custom pressure plates for camera ports | Basic | 09/17/07 | Avcon | 1618118 | X | X | Noted that the 21 inch requirement actually applies to the pressure plate, not the camera port itself | |
| 0004 | Engineering for quick install/deinstall of camera optical flats | Basic | Avcon | 01409001, 01409003 | X | X | |||
| 0005 | Camera Port Dome for one of two ports | Basic | 09/17/07 | Avcon | 161050-015 | X | Installation of aft port dome and flat floor for aft dome only. Is this required for the new aircraft? | ||
| 0006 | Provide and install a drift sight port 7.5 inch diameter downward looking port | Basic | 09/17/07 | Avcon | 1618113 | X | X | ||
| 0007 | Provide and install extended range fuel tank configuration | Basic | 09/17/07 | HBC | X | only if 350CER | |||
| 0008 | Provide and install bubble windows | Basic | 09/17/07 | Avcon | 1618111, 1618112 | X | X | HBS to provide bubble window kit for dual standard bubble windows | |
| 0009 | Provide and install window blanks | Basic | 09/17/07 | Avcon | 1618101 | X | X | ||
| 0010 | Provide and install power inverters for aft power stations | Basic | 09/17/07 | Avcon | 350-10001 | X | X | Installed in AC Cabinet | |
| 0011 | Provide and install antenna ports 12 inch diameter upward looking | Basic | 09/17/07 | Avcon | 1618102 | X | X | Includes 6 overhead pin locations for equipment racks. | |
| 0012 | Provide and install rack stations aft including power | Basic | 09/17/07 | Avcon | 1618103, 1618110 | X | X | Separate line items for equipment racks and for power | |
| 0013 | Provide and install intercom system for 8 aft stations | Basic | 09/17/07 | Avcon | 1618106, 1618125 | X | X | ||
| 0014 | Provide and install upgrade avionics Garmin 165 GPS | Basic | 09/17/07 | Avcon | 1618105-003 | X | X | Is the Garmin 165 GPS available. Garmin 625 (or GDL 88) as replacement? DZUS rail mounting will be an issue. | |
| 0015 | Provide and install HG-9550 radar altimeter | Basic | 09/17/07 | Avcon | 1618109-003, 1618123 | X | X | provisions only; see CLIN 0031 |
No equipment for Avcon to purchase. Install wiring (no R/T rack), antenna wiring, antenna doublers (blanking panels), sidewall connector, display connector (no panel cutout).
| 0016 | Provide and install Skytrac Satcom System with AFF | Basic | 09/17/07 | Avcon | 1618108-003, 1618122 | X | ISAT-100 installed on FM-21. See CLIN 0028 | ||
| 0017 | Provide and install Wolfsburg RT-5000 System | Basic | 09/10/08 | Avcon | 1618107-003, 1618123 | X | Is the required for the new aircraft | ||
| 0018 | Provide and install Collins TCN-500 System | Basic | 09/10/08 | Avcon | 1618104-003 | X | Is the required for the new aircraft | ||
| 0019 | PC-1 Install standard option engine wash rings on both engines | PC-1 | Amendment 3 21 Apr 2008 | 04/21/08 | HBC | X | Is the required for the new aircraft | ||
| 0020 | PC-2 Pressure dome redesign | PC-2 | Amendment 3 21 Apr 2008 | 04/21/08 | Avcon | X | Included CLIN 0020A | ||
| 0020A | PC-02A Additional pressure dome | PC-02A | Amendment 3 21 Apr 2008 | 04/21/08 | Avcon | 1618115 | X | Is the required for the new aircraft | |
| 0021 | PC-03 Additional overhead pins | PC-03 | Amendment 3 21 Apr 2008 | 04/21/08 | Avcon | 1618102 | X | Included CLIN 0011 | |
| 0022 | PC-04 Additional Avcon rack | PC-04 | Amendment 3 21 Apr 2008 | 04/21/08 | Avcon | 1618103 | X | Is the required for the new aircraft | |
| 0023 | PC-05 RVSM testing Flight Testing Only) | PC-05 | Amendment 3 21 Apr 2008 | 04/21/08 | Aero Mach | X | X | Verify RVSM STC has been update to include configuration of FM-21. | |
| 0024 | PC-06 Additional low power drops | PC-06 | Amendment 3 21 Apr 2008 | 04/21/08 | Avcon | 1618120 | X | X | |
| 0024A | PC-06A CAT 5 cable installation | PC-06A | Amendment 3 21 Apr 2008 | 04/21/08 | Avcon | 1618120 | X | X | |
| 0025 | PC-07 Additional paper manuals (1 set) | PC-07 | Amendment 3 21 Apr 2008 | 04/21/08 | HBS | X | Do not believe this will be required on this purchase | ||
| 0026 | PC-09 Antenna installation | PC-09 | Amendment 3 21 Apr 2008 | 04/21/08 | Avcon | X | Is the required for the new aircraft | ||
| 0027 | PC-10 Oversized forward camera port | PC-10 | Amendment 3 21 Apr 2008 | 04/21/08 | Avcon | X | Is the required for the new aircraft | ||
| 0028 | PC-11 ISAT - 100 upgrade with phone | PC-11 | Amendment 3 21 Apr 2008 | 04/21/08 | Avcon | 1618108-003 | X | Is the required for the new aircraft | |
| 0029 | PC-13 Air-to-Air antenna for TACAN | PC-13 | Amendment 3 21 Apr 2008 | 04/21/08 | Avcon | X | Is the required for the new aircraft | ||
| 0030 | PC-14 Strakes, dual raisback | PC-14 | Amendment 3 21 Apr 2008 | 04/21/08 | Avcon | X | X | Will be installed during production and replaced with SM strakes during bubble windows installation | |
| 0031 | PC-15 Cockpit indicator (HG9550 Radar Altimeter) | PC-15 | Amendment 3 21 Apr 2008 | 04/21/08 | Avcon | X | X | part of provisions | |
| 0032 | PC-16 RT-5000 to RT-5000P-25 | PC-16 | Amendment 3 21 Apr 2008 | 04/21/08 | Avcon | X | Is the required for the new aircraft | ||
| 0034 | PC-19 Provide and install STC Frakes Exhaust Stacks | PC-19 | Amendment 7 30 Jan 2009 | 04/21/08 | HBC | deleted | deleted from FM 21 requirements; used to add oxygen & power drops | ||
| 0035 | PC-20 Provide and install Sky Connect Tracker Mission management Unit | PC-20 | Amendment 5 24 Jun 2008 | 04/21/08 | HBC | X | Is the required for the new aircraft | ||
| 0036 | PC-21 Provide and install folding right aft jump seat located at the bubble window to match interior colors | PC-21 | Amendment 6 10 Sep 2008 | 09/10/08 | Avcon | X | Is the required for the new aircraft | ||
| 0036 | PC-22 Provide and install 2 oxygen drops in the aft cabin and two portable oxygen bottles | PC-22 | Amendment 7 30 Jan 2009 | 01/30/09 | Avcon | 1618136, 1618137 | X | Is the required for the new aircraft | |
| 0036 | PC-23 Provide and install hard wired power drops at all intercom stations plus 4 a/c power headsets | PC-23 | Amendment 7 30 Jan 2009 | 01/30/09 | Avcon | 1618120 | X | Is the required for the new aircraft | |
| Items Requiring Additional Clarification |
| Aft Forward Facing Electric Flushing (Recirculating) Lavatory | X | Was included on FM-21 VIP interior; not included in "Slick Interior" option; it this required on the new aircraft or do we remove from FM-21 to support common cabin layout | |
| L-Shaped Curtain / L-Shaped Web | Not included in "Slick Interior" option. Partitions were included in FM-21; is this option required on the new aircraft and is this required on FM-21 to support common cabin interior layout | ||
| Crash Ax (Loose Equipment) | Not included in "Slick Interior" option. Is this option required on the new aircraft? | ||
| Cobham DACS | Not included in "Slick Interior" option. Is this option required on the new aircraft? | ||
| MADRAS Digital Flight Data Recorder (DFDR) | Not included in "Slick Interior" option. Is this option required on the new aircraft? | ||
| One (1) Yr Flt Mgmt System Database Region Subscription Pkg | Not included in "Slick Interior" option. Is this option required on the new aircraft? | ||
| One (1) Yr Jepp Charts Subscription Pkg | Not included in "Slick Interior" option. Is this option required on the new aircraft? | ||
| 130-9031-0001 Engine Wash Drain Kit | Not included in "Slick Interior" option. Is this option required on the new aircraft. | ||
| P&W Engine Service (PWES) FAST Engine Trend Monitor System (w/DTU) | Not included in "Slick Interior" option. Is this option required on the new aircraft? | ||
| 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. Intended use is 9-inch format aerial photography, but may be used for other optical or hyperspectral sensors. Port to include a 21 inch diameter pressure-certified Corning 7980 Fused Silica optical glass and external protective mechanical sliding door, along with metal blank-off plate that can be installed instead of optical glass. Installation to include an optical flat defogging system designed to prevent glass fogging from high altitude transits. | X | Does FM-21 have this capability? If not, do we need to include this in CLIN 2001 to standardize cabin layout? | |
| 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. Intended use is 9-inch format aerial photography, but may be used for other optical or hyperspectral sensors. Port to include a 21 inch diameter pressure-certified Corning 7980 Fused Silica optical glass and external protective mechanical sliding door, along with metal blank-off plate that can be installed instead of optical glass. Installation to include an optical flat defogging system designed to prevent glass fogging from high altitude transits. | X | Does FM-21 have this capability? If not, do we need to include this in CLIN 2001 to standardize cabin layout? | |
| 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). Contractor to determine best location and surrounding infrastructure based on detector vendor’s requirements and recommendations (see below for system description and installation considerations). If required for certification, the Contractor shall provide a mounting cage to meet g-load and crash load limits. If the option for this modification is selected, the Government will provide an RSX-5 unit as Government Furnished Equipment for fit and function certification. If the installation includes a non-metallic pressure interface, the Contractor shall provide a metal blank-off plate for use when the gamma sensor system is not installed. | X | Does FM-21 have this capability? If not, do we need to include this in CLIN 2001 to standardize cabin layout? | |
| Optical port capability for the forward gamma sensor port. If the forward gamma sensor port is selected, this secondary option is for a drop-in assembly that would replace the pressure interface with a plate incorporating an optical window and external protective sliding door (preferably also mounted to the plate, rather than the surrounding airframe, to reduce the installation/removal effort when switching between systems). The instrument well would also require mounting provisions for the camera system, and an optical flat defogging system. | X | Does FM-21 have this capability? If not, do we need to include this in CLIN 2001 to standardize cabin layout? | |
| 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). Contractor to determine best location and surrounding infrastructure based on detector vendor’s requirements and recommendations (see below for system description and installation considerations). If required for certification, the Contractor shall provide a mounting cage to meet g-load and crash load limits. If the option for this modification is selected, the Government will provide an RSX-5 unit as Government Furnished Equipment for fit and function certification. If the installation includes a non-metallic pressure interface, the Contractor shall provide a metal blank-off plate for use when the gamma sensor system is not installed. | x | Does FM-21 have this capability? If not, do we need to include this in CLIN 2001 to standardize cabin layout? | |
| Optical port capability for the aft gamma sensor port. If the aft gamma sensor port is selected, this secondary option is for a drop-in assembly that would replace the pressure interface with a plate incorporating an optical window and external protective sliding door (preferably also mounted to the plate, rather than the surrounding airframe, to reduce the installation/removal effort when switching between systems). The instrument well would also require mounting provisions for the camera system, and an optical flat defogging system. | x | Does FM-21 have this capability? If not, do we need to include this in CLIN 2001 to standardize cabin layout? | |
| Oceanic Package (2nd GPS and HF 9000 w/selCal) | X | This is required for the new aircraft; is it required for FM-21 CLIN 2001 to standardize cabin layout? | |
| Secondary Nav Package (2nd DME and 2 nd ADF) | X | This is required for the new aircraft; is it required for FM-21 CLIN 2001 to standardize cabin layout? | |
| 24 inch Extended Pedestal | X | This is required for the new aircraft; is it required for FM-21 CLIN 2001 to standardize cabin layout? |
File details come from the government source that posted it.