STC LIST

Installation of the Model 31A interior as a refurbishment to other Learjet models.

Installation of a gravel runway operations kit.

Installation of Marquardt target towing system (high speed operation).

Installation of Learjet Model 36A fuselage fuel cells.

Installation of provisions for a cabin centerline mounted camera with an in-flight opening door.

Attachment of Marquardt Target Towing System.

Installation of 9KVA, 3-phase inverter system, consisting of 3 J.E.T. SI-3000A Inverters.

Installation of Dual J.E.T. SI-3003B, 3-phase, 400 H2, 3000 VA inverters.

Underwing Hardpoints (Wing Pylon External Stores installation).

(ADS-B) Dual GTX-3000 Transponders, GDL-88 Automatic Dependent Surveillance-Broadcast “ADS-B In” with Wide Area Augmentation System (WAAS) Global Positioning System (GPS) sensor and Flight Stream 210 Bluetooth Connectivity installed for “ADS-B Out” compliance.

Replacement Stall Warning Vertical Accelerometer installation, Butler National Part Number 02904001-101.

Replacement Rate Gyro installation, Butler National Part Number 501-1169-01 MOD A or 501-1169-02 MOD A.

(ADS-B) Dual Garmin GTX-33ES Mode-S transponders and single or dual Garmin GTN 650 / 750 panel mounted navigation and global positioning system (GPS) units, or dual Garmin GTX-335R and / or GTX-345R Mode-S transponders and single or dual Garmin GTN 650 / 750 / 625 / 725 panel mounted navigation and GPS units.

Installation of replacement circuit boards for the FC-110 autopilot, in accordance with Master Drawing List (MDL) 01807002, Revision C, dated March 30, 2011 or later FAA-approved revision.

Installation of a Sandel Avionics Horizontal Situation Indicator (HSI) and Attitude Direction Indicator (ADI).

Installation of a Collins AHC-3000A Series Attitude Heading Computer (AHRS).

Internal Wing Hardpoints.

Installation of the Quiet Lear Hushkit or Avcon Noise Suppressor.

Learjet 35A S / N 35A611 only.

Provisions for installation of Special Mission Equipment and modification of extended range tip tanks to incorporate a dry bay.

Installation of Rosemount Pitot / Static Probes, altimeters, and associated equipment in Learjet 20 series aircraft to obtain Reduced Vertical Separation Minimum approval.

Install extended range tip tanks.

Increase landing weight to 16000 pounds.

Incease wing / tip zero fuel weight to 14500 pounds.

Increase takeoff weight to 19600 pounds.

Increase landing weight to 16000 pounds with extended range tip tanks.

Increase zero wing and tip fuel weights to 14500 pounds with extended range tip tanks.

Increase takeoff weight to 19600 pounds with extended range tip tanks.

Install plugs in place of windows and on top of airplane.

Increased Gross Takeoff Weight, Zero Fuel Weight, and Increased Landing Weight.

Install Increased Fuel Capacity, Increased Gross Weight, Increased Zero Fuel Weight, and Increased Landing Weight.

Tip Tank Baggage Compartments.

Installation of extended wingtip fuel tanks and underwing stores.

Avcon Fins (Aft Body Strakes for drag efficiency / aircraft stability).

Installation of MTR-101 reeling machine on one of both wings.

Install pressure cans over scanners.

Installation of external device under either left or right wing. RM-30A Reeling Machine TRX9 with 1748D11 Finned Sphere ALQ-167 Jamming Pod or ALQ-188 Jamming Pod.

Install equipment racks in cabin.

Install a forward-looking infrared (FLIR) camera turret.

Equipment Rack.

Structural provision for Daedalus IR scanner.

3000psi Hydraulic System.

Installation of dual openable hatches on the belly of the fuselage.

Provisions for a towing arm on the fuselage belly.

Installation of provisions for Infra-Red Scanner.

Equipment Console.

Installation of provisions for chaff dispenser and electronic counter measuring (ECM) equipment consoles.

Learjet 35 S / N 35-006 only.

Provisions for ECM equipment consoles and chaff dispensing equipment.

Installation of camera equipment rack on existing seat rails.

Equipment Console.

RH forward emergency exit.

Dual Camera installation.

Flight inspection console installation (structural provisions only).

Installation of provisions for Garnet radar and equipment racks.

Inverter Mounting Provisions.

Tailcone Radome installation.

Inverter Mounting Provisions.

Portable electronic console installation on existing seat rails.

Installation of structural provisions for infra-red scanning equipment.

Installation of operable hatch on right side of fuselage.

Installation of an optical oblique window in both sides of fuselage.

Fuselage baggage avionics rack (structural provisions only).

Structural installation for aft avionics console.

Installation of film cassette rack.

Installation of radar equipment console on seat rails.

Installation of provisions for Daedalus scanner into previously approved camera / flare doors. (MODELS INCORPORATING STC’s SA891CE, SA961CE, SA1281CE 0R SA1377CE).

Installation of external, underwing stores / hardpoints on the bottom surface of both wings.

Aerial Camera Radome and interchangeable structural plug.

Installation of Sierra Electronics rack in passenger compartment.

Attachment of Hayes TRX-3 tow target system or Hayes Universal tow targets.

Structural provisions for infra-red scanning equipment.

Structural provision for NASA – Daedalus IR scanner.

Installation of a Maritime Patrol surveillance system (Sierra Research).

Installation of structural plug.

Pod and aerodynamic fairing for target towing equipment.

Belly Radome installation and structural provisions for an airborne surveillance radar.

Instrumentation rack and inverter rack in baggage compartment.

Installation of mounting plates in the tail cone for mounting of electrical inverters.

Installation of electronic consoles on cabin seat rails.

Structural provision for NASA – Daedalus IR scanner.

Replacement of 24” Executive Door with 36” Cargo Door.

Structural plug installation in right side of forward fuselage when camera door is removed.

Dry Ice Dispenser.

Dry Ice Dispenser.

Structural provision for particle measuring probe.

Structural provision for particle measuring probe.

Install lower cabin door designed to accept a carousel flare dispensing unit capable of being reloaded in flight.

Install lower cabin door designed to accept a carousel flare dispensing unit capable of being reloaded in flight.

Structural provision for Jelco infra-red scanner.

Structural provision for Jelco infra-red scanner.

Structural provisions for infrared scanning equipment.

Structural provisions for infrared scanning equipment.

Install structural provisions on right hand side of airplane for removable camera door.

Install structural provisions on right hand side of airplane for removable camera door.

Andrea Radio Corp. (A-81) five station interphone system installation.

Datum Console Rack.

Datum Console Rack.

Installation of dry ice dispenser.

Installation of dry ice dispenser

Provisions for infra-red scanning equipment.

Provisions for infra-red scanning equipment.

Lower cabin door designed to accommodate a flare rack capable of being reloaded in flight.

Lower cabin door designed to accommodate a flare rack capable of being reloaded in flight.

Installation of drift (navigation) sight to be used in conjunction with aerial photography equipment.

Installation of drift (navigation) sight to be used in conjunction with aerial photography equipment.

Installation of drift (navigation) sight to be used in conjunction with aerial photography equipment.

Install lower cabin door to accommodate aerial photography equipment.

Install lower cabin door designed to accommodate flare racks.

Installation of lower cabin door designed to accommodate aerial photography equipment.

Lower cabin door designed to accommodate four flare racks for cloud seeding.

Dual Camera / Intervalometer.

Camera Door RC-10 Wild Aerial Camera… OR Relocate optical window port.

Sperry SPZ500LR Automatic Flight Control System – Only Use with STC SA994NW.

6 Pole Rotary Squat Switches.

Access Doors in Engine Nacelle.

Installation of cabin door closing system.

Replacement of plunger type landing gear squat switch with rotary type switch.

RX Drag Reduction System.

Mark II Performance System Installation – Recontoured Wing and Flap Leading Edge, Wind Vortex Generator Removal, Wing Stall Strips, etc.

Mark II Performance System Installation – Recontoured Wing and Flap Leading Edge, Wind Vortex Generator Removal, Wing Stall Strips, etc.

Mark II Performance System Installation – Recontoured Wing and Flap Leading Edge, Wind Vortex Generator Removal, Wing Stall Strips, etc.

Mark II Performance System Installation – Recontoured Wing and Flap Leading Edge, Wind Vortex Generator Removal, Wing Stall Strips, etc.

Installation of the Mark II performance system, including recontoured wing leading edge, recontoured flap leading edge, wing vortex generator removal, installation of wing stall strips and other minor refinements.

One or two 90 Gallon Fuselage Auxiliary Fuel Tank(s), in accordance with Branson.

Quick change cargo restraint system.

Structural provisions for cargo restraint system.

Install tail cone cargo compartment (300 lbs capacity).

Install mid-fuselage cargo compartment (500 lbs capacity).

Installation of Branson flight crew emergency exit.

Cargo Liner.

Installation of cabin cargo retention net system.

Installation of cargo restraint system.

Installation of Rosemount Pitot / Static Probes, altimeters, and associated equipment.

Installation of pressure dome provision for an infra-red scanner in the camera door.

(Dual Camera / Sensor) Provisions for Special Missions Equipment.

Portable electronic console installation on existing seat rails (structural provisions only).

Equipment console, two observation windows, a modified landing / taxi light system, relocation of pitot tubes and provisions for the installation of a (FLIR) Forward Looking InfraRed.

Sierra electronic console rack installed on existing aircraft seat tracks in place of seats or accessories.

External Baggage Pod installation.

Electronics Rack provisions.

Cargo Pod installation.

Replacement feeder tank lower door and backing plate installation.

PPG Industries Windshields.

Jump seat installation.

Additional crew seat installation on inboard seat tracks.

Electronic Console provisions installed on aircraft seat tracks (structural provisions only).

Co-Pilot Brake Modification

Replace Main Landing Gear Door Bracket

Nose Wheel Steering

Replace Passenger Entrance Door with Wide Cargo Door

Openable Window Co-Pilot Emergency Exit

Cargo Interior

Special Mission Equipment Revision

Camera Window, with option to allow Unpressurized Operations when Optical Glass is removed and Camera Door is open

Installation of provisions for electronic equipment racks on seat rails

Installation of flight inspection console on seat track (structural provisions only)

Dual or Single Camera & Optional Navigation Sight

Dual or Single Camera & Optional Navigation Sight

Sierra Flight Inspection Console Structural Provisions

Installation of structural provisions for flight inspection console mounted on seat tracks

Passenger Shoulder Harness

Passenger Shoulder Harness

36″ Cargo Door

36″ Cargo Door

Portable electronic console installation on existing seat rails

Portable electronic console installation on existing seat rails

Camera Port Optical Glass for Dual Aerial Camera

Installation of Litton LTN-76 inertial navigation system (INS) with photogrammetric integrated control system (PICS) 76-24 program.

Sierra utility flight inspection equipment installation

Sierra utility flight inspection equipment installation

Provisions for a Litton IFIRS camera in the tailcone

Installation of Sierra Electronics rack in aft baggage compartment

Sierra Electronic Console

Tailcone Baggage Compartment

Tailcone Baggage Compartment

Side Facing Jump Seat

Side Facing Jump Seat

Sierra Utility Flight Inspection Equipment Rack

Sierra Electronics Console

Reduce Height Swivel Seat

Dual camera installation

500 S / N 350 or higher.

Dual camera installation.

Install Sierra data console on left hand seat rails

Optical Glass Window in Emergency Exit Door

Optical Glass Window in Emergency Exit Door

Hinged Nose Compartment Door

Anti-Collision Warning System

Provisions for magnetometer

Provisions for tandem / dual cameras

Provisions for Daedalus Scanner

Removable Baggage Compartment

Installation of provisions for a magnetometer

Provisions for the installation of tandem cameras.

Installation of provisions for a scanner

Honeywell YG-1761B LaserNav Inertial Navigation System

Interior Kit for Beech 1900C

Optional Interior Configuration – Ninth Seat

Removable External Baggage Compartment Pod

Hinged Nose Compartment Door

Structural Provisions – Sierra Semi-Automatic Flight Inspection System Model 8512 SAFIS CONSOLE on Seat Rack

Left Emergency Exit

C39A Stretchers

Forward Facing Jump Seat

Cargo Door Teardrop Window

External Baggage Compartment Pod

Flight Inspection Console Provisions

Flight Inspection Console Provisions

Installation of inverter rack mounted on seat tracks

Installation of inverter rack mounted on seat tracks.

Installation of inverter rack mounted on seat tracks.

Cloud Physics Probe

Camera Window with Sliding Door Cover & Drift Sight

Camera Window KA-79 Camera Mount Structural Plug

Sierra Electronic Console Seat Rails

Camera Window Intervalometer Drift Sight

Litton LTN-72 LTN-76 Inertial Navigation System

Installation of portable airway checking equipment rack on existing seat rails.

Installation of portable airway checking equipment rack on existing seat rails.

Installation of portable airway checking equipment rack on existing seat rails.

Sierra Utility Flight Inspection Equipment Rack

Sierra Electronic Console

Sierra Electronic Console

Sierra Electronic Console

Sierra Electronic Console

Sierra Electronic Console

Sierra Electronic Console

Supplemental DC Power Isolated Instrument Bus

Communication & Navigation Antennae on Upper & Lower Fuselage

Baggage Door

Installation of camera provisions and camera window

Anti-Collision Warning System