Science Modifications

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AircraftZenith PortsNadir PortsModified WindowsExternal AntennasWing Pylon MountsOptical WindowsDropsonde CapabilitySonobuoy CapabilitySampling ProbesInstrument RacksPowerSeating CapacityComms/SATCOMNotable Features
B777None4x Small (27” x 19”, angled), 2x Large (44” x 40”)4 (23” x 16” oval)NoneNoneNumerous optionsNRD-41 and RD-41AXTCD or similarNumerous options~20, numerous115V 60Hz/400Hz  @30A, 28V DC @ 5AUp to 200None listedHigh seating capacity, Power Upgrades, House Keeping Rack, Nadir Portals, XCS & AMP (operator console/ EE-power provisions) modifications, Conf Tables), DropSonde tube Instl FY25, Lower Fuse skin Doublers Acreage 
P-31x 16”, 1x radiometer boat (2 instruments), 1x 3” port, 1x KT-19, mod. engineer hatch3 fuselage, 2 large, 1 small, 6 oblique, bomb bay,  side looking ports with motorized door7 (4 P-3 bubble + 3 DC-8 style)Various GPS + splitters10 pylonsAvailableDropsonde + free fallYes (pressurized tube)Available~20 (10 double), numerous115V 60Hz, 400Hz, 28V DCUp to 24INMARSAT, CERTUS, VOIPAir Science Data System, EGI, KT-19, AIS, bomb bay deployments,  INMARSAT and CERTUS SATCOM systems, VOIP, WiFI, USB,18Kip payload, Radome/Tailcone mods, Iridium Phone, Upgraded ICS.
B-2001 Zenith inlet, 1 Zenith portal fwd of windshield2 (29.5x29.5, 26.75x22.5), shutters C/S.2 lateral portalsGPS, research antennae2 wingtip pylons (32kg max each)BK-7 panesAft nadirNone notedYes, PS connectionsMultiple115V-60Hz@3X10A,4200W, 28V DC, 3X50AUp to 4Iridium SATCOM voice/textApplanix AVX210, FMS, Stormscope, EGPWS, research panels. HALO 275 GVW Upgrade to 14k lbs, 5-blade Raisbeck Propellers, Raisbeck Strakes, High Flotation gear doors, Saddle tanks, Rasibeck Ram Air, Butterfield Anti-ice,AVCON portals, Norton Radome, ferry tanks, wingtip pylon. MD302-SAM, WX Radar 
ER-23 on wing pods2 (Q-bay), 1 (Nose), 4 (Wing pods), 1 (Centerline)NoneUHF, VHF, HF, GPS, VOR/ILS, ADFWing podsNone notedNone notedNone notedT/P probes, multiple baysQ-bay racks (up to 825 lbs)Not specifiedSingle pilotNAVREC, INSNose pod, aft cavity, tailcone, cheek, wingtips
C-20ANone notedCustom mount UAVSARNone notedNone notedNone notedNone notedNone notedNone notedNone noted1 UAVSAR rackNot specifiedMinimal (crew only)Not specifiedUAVSAR dedicated
G-IIINone noted2 (18.16 in x 18.16 in) with FOD shuttersNone7 antennas (3 GPS, 2 Iridium, 1 Applanix, 1 ADS-B/UAT)NoneOptical panesDropsonde (through baggage)None notedYes18U racks + risersStandard 115V 60Hz, 28V DC, 2x150AA, 80 A of 120 VAC /60 Hz power, 15 A of 14 VDC, 20 A of 5 VDCUp to 10IridiumApplanix AVX210, NASDAT, Engineer’s station. Upgraded ICS. Refreshed engines HSI . 
G-IVNone notedNone specifiedOptical optionHF, VHF, UHFNone notedYes (optional)Not specifiedNot specifiedNot specifiedNot specified28V DC, 115V AC4 double + 5 singleIridium GO!, Short BurstShirt-sleeve cabin, cargo door 64x81.5, AirSAR
SR-22Yes (Rear Window) Yes (cargo pod)None notedVHFNone notedNone notedNone notedNone notedAir Data sampling 28V, 25A4G1000, STEC55X, MGL-AP, SVDU1800 EFIS,GNS650, EMSFDC Automonmy  Air data Probe installation (Baseline), Cargo Pod, S-Tec 55X Autopilot, GMA 35 Remote Audio Panel, GDU 1060 Touchscreen Flight Display / MFD, MD 302 Standby Attitude Module,
 GTN 650 WAAS / GPS Navigator/Com Transceiver, 
GTN 750 WAAS / GPS Navigator/Com Transceiver, GTX 345 Transponder, Flightstream 210 BlueTooth Link, EDM 930 Engine Monitoring System, research ADAHRS, AIR DATA 100 AIR DATA PROBE
LC40None notedNone notedNone notedVHFNone notedNone notedNone notedNone notedNone notedFDC Instl.12VDC, 50A4MGL-EFIS,G1000, STEC55XPROF-Trainer, Chase Aircraft,  55X Autopilot • GMA-35 AUDIO PANEL, GDC 74 Air Data Computer, GDU 600 PFD,  GRS 77 AHRS,  GTN 650 WAAS / GPS Navigator/Com Transceiver, GTN 750 WAAS / GPS Navigator/Com Transceiver,  GTX 345 Transponder, MD 302 Standby Attitude Module,  Flightstream 210 BlueTooth Link, WX-500 Stormscope

Table 1 : Aircraft Research Capabilities: Science Modifications and Payload Accommodations