Aviat Husky A-1, A1B

Number of Active Aircraft: NA Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 2
Empty Weight: 1190 lbs
Max Weight 1800 lbs
Useful Load: 610 lbs
Engine Name LYC O-360-C1G
Engine Number 1
Horsepower 280 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 20000 ft
Max Fuel 52 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 122 kts
GPH (75% BHP): 9.5
MPG (75% BHP) 12.8
Range (75% BHP): 581 nm
Fuel Cost Per Seat Mile 0.23 $
Fuel Cost Per Hour 57 $
MPG per 1000 lbs of Payload 7.83
F-T (Speed^2/FuelBurn) 15.7 HP
F-T Payload 9.6 kts
MPH To HP: 4.4 kts
T/O Roll - T/O over 50 FT OBST 200 ft / 625 ft

SA00013NY Installation of AFC-500 full flow engine oil filter P/N AFC-500. Amended 12/1/1995
SA00068SE (PAGE 1) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00165BO Installation of Avidyne Corporation Datalink Coupler part number 700-00015-000 per Avidyne Corporation Master Document List Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions. Issued 2/20/2003
SA00194BO Installation of P/N 2042 Landing Gear Warning System for amphibian aircraft. Reissued 1/23/2009
SA00243BO (1 OF 5) Installation of Centurion Consulting Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100) or without roll steering (p/n 0025-5200). Amended 7/21/2011
SA00280BO Installation of PK 2250A Amphibious Floats. Amended 3/9/2012
SA00298DE Installation of a modification system to add additional cabin heat and reconfigure the carburetor heater design. Issued 6/16/1997
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00478CH (PAGE 2) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00478CH (PAGE 3) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00637CH Installation 2100 Amphibian/Seaplane Floats Kit No 10D1-6009. Amended 7/23/2008
SA00668SE Installation of vortex generators on the wing leading edge and underside of the horizontal stabilizer. Amended 6/12/2009
SA00780SE (PAGE 3) Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE dated February 1 2001 or later FAA approved revision. Amended 5/11/2010
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00954SE (2 OF 2) Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711 Report 106P Revision B dated August 2 2001 or later FAA approved revision. Amended 8/11/2003
SA01015SE Installation of eligible Alaska Tire and Rubber Company TSO-C62d Tires as listed in Approved Model List SA01015SE dated November 7 2001 or later FAA approved revision. Amended 10/4/2012
SA01026SE (PAGE 1) Improved fuel gascolator assembly. Amended 12/19/2012
SA01026SE (PAGE 2) Improved fuel gascolator assembly. Amended 12/19/2012
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01233SE Manufacture of Alaskan Bushwheel Inc. (ABI) tail wheel and fork assembly per ABI Document ABI-3200B Revision A dated April 28 2005 or later FAA approved revision.  Amended 5/22/2012
SA01238SE Installation of EDO 689-2130 floats and a gross weight increase of up to 2200 pounds. Issued 7/17/2003
SA01240SE (3 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006
SA01251SE The manufacture of a Sunvisor System. Amended 2/28/2012
SA01416SE Installation of a butterfly valve in the oil cooler inlet duct Amended 2/7/2012
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01446SE Installation of Hartzell HC-C2YR-1BF/F8477-4 propeller Reissued 11/4/2004
SA01473SE (1 OF 5) Installation of a GTX 32 (mode C) GTX 33 (mode S) or GTX 33D (mode S with diversity) Remote Transponde Amended 5/21/2008
SA01487SE-D (Page 2) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01606CH Installation of alternate electro-hydraulic power pack system for operation of main wheel skis. Amended 4/16/2010
SA01658SE Installation of a side opening window. Issued 3/16/2006
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (1 OF 5) Installation of an antenna Amended 2/15/2007
SA01701LA Installation of AM-Safe Inflatable Restraint System on pilot and co-pilot seats.  Reissued 3/24/2008
SA01721CH Installation of Baumann Model BF2150A floats per Baumann Drawing List BF-2150A-01 Rev B dtd 9/19/02 or later FAA approved revisions. Issued 10/28/2002
SA01765SE Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels Part Number (P/N) ABI-1010. Amended 10/11/2012
SA01800SE (PG 1) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01861SE (PAGE 1)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01933LA-D Page 2 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
SA01933LA (1 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006
SA01988SE (PAGE 1) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009
SA02015SE-D Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Amended 2/5/2014
SA02019SE-D Page 2 Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/19/2012
SA02023CH Installation of an MT-Propeller model MTV-15-B/210-58 and spinner assembly P-277-B. Reissued 10/22/2007
SA02032AK Installation of Model L2500A skis on main landing gear. Issued 4/7/1995
SA02033AT (PAGE 4) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) Amended 7/25/2008 0:00
SA02049AK Fabrication and installation of Airglas Engineering Co. Inc. Model LTC18 cargo pod/bell Reissued 10/28/2011
SA02110CH (PAGE 3) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02119SE Page 1 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02134AK Installation of an extended baggage compartment per AvAlaska Inc. Aviat A-1 extended baggage master drawing list latest FAA approved revision. Issued 3/4/1999
SA02149AK Installation of GX50/60 GPS Navigator Capstone configured MX20 Multi-Function Display and UAT transceiver. Reissued 5/17/2013
SA02153AK Installation of Burl s Aircraft Rebuild Magnum I tail wheel penetration tail ski per Burl s Aircraft Rebuild LLC Master Data List No. MDL-3234-1 latest FAA approved revision. Issued 12/22/1999
SA02153LA-D (Page 1) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
SA02168AK (PG 1) Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. Issued 3/23/2001
SA02168AK (PG 2) Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. Issued 3/23/2001 1:00
SA02172AK Fabrication and installation of Airglas Inc. Model LC18 cargo pod kit  Amended 6/14/2010
SA02203AK (PAGE 3)  Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
SA02212AK (PG 3) Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Amended 5/4/2011
SA02217AK (1 OF 5) Installation of Garmin AT Model GDL90 UAT Data Link System in accordance with Garmin AT Inc. GDL 90 UAT Master Data List P/N 560-0278-01 Revision A dated November 12 2004 or later FAA approved revision.  Amended 12/1/2004
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02288AK Installation of Alpha Omega Suspension System (AOSS) in place of original bungees Issued 4/26/2007
SA02293AK (3 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02321AK Installation of EDO 89-2000 floats modified Issued 8/29/2008
SA02360AK Fabrication and installation of Airglas Inc. Model GLH3000 hydraulically retractable wheel skis Amended 11/25/2013
SA02396AK Replacement of Sky International Inc. landing gear strut assemblies with Floats Alaska LLC. +3 Issued 5/30/2012
SA02509NY Installation of R Issued 2/12/2008
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 2) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02838CH nstallation of Wipaire Skis Main Wheel Skis Model Issued 5/11/2010
SA02870CH Installation of MT Propeller model MTV-9-B/(198-200) -52 and matching spinner Amended 3/21/2012
SA02934CH Installation of the Custom Fiberglass Molding Inc. (CFMI) Model Alaskan 2500 Main Landing Gear Skis in accordance with Custom Fiberglass Molding Inc. installation design data listed on AML No. SA02934CH or later FAA Approved revision. Issued 3/2/2011
SA02987CH Installation of the Electroair Electronic Ignition System Amended 7/23/2013
SA03148NY (PAGE 2 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA03858AT Installation of Power Flow Systems Inc. (PFS) tuned exhaust system. Issued 6/21/2010
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA09502AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-881-20/30. Amended 9/19/2000
SA10463SC Installation of Lycoming Engines Model IO-360-A1D6 engine and an MT Propeller Model MTV-15-B/205-58.  Reissued 12/14/2005
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA122CH Surrendered and incorporated into STC SA00478CH. Surrendered 6/14/2002
SA1512WE (2 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007 0:00
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA21NW Installation of a 70 pound baggage compartment in either or both EDO 89-2000 89A-2000 or 689-2130 floats Amended 9/25/2009
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
SA2586NM (PAGE 4) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2670CE Operation of airplane using leaded or unleaded automotive gasoline wiht minimum antiknock index.  Amended 4/28/2010
SA3-423 Installation of CT-3000 tail ski on airplanes equipped with Scott 3200 or 3400 tail wheels. Amended 4/16/2010
SA39CH Installation of amphibian landing gear position advisory system. Reissued 6/29/2011
SA4005NM (PG 5) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA5156NM (PG 3) Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 7/29/2010 0:00
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA563CH Authorizes installation of engines equipped w/Unison Limited Authority Spark Advance Regulator (LASAR) ignition system w/Cylinder Head Temp. (CHT) monitoring capability on airframes. engines. Reissued 2/10/2009
SA5924NM Installation of RPM instrument. Amended 11/24/1997
SA5925NM Installation of oil pressure/temperature instrument. Amended 12/8/1997
SA5926NM Installation of manifold pressure instrument. Amended 8/15/1993
SA593CH (4 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
SA71GL Installation of air filters Reissued 6/20/2000
SA7965SW Application of fabric and polyurethane finishing system. Amended 7/15/1994
SA96CH Installation of Baumann Model BF-2100 floats. Reissued 10/23/2001
ST00961LA Installation of MASS Systems fire extinguisher cartridges as replacements for Walter Kidde Aerospace fire extinguisher cartridges in fire extinguisher bottles installed in the airplane models noted on the FAA Approved Model List dated June 29 2000 or later FAA approved revisions. These fire extinguisher cartridges are in accordance with the MASS Systems Master Drawing List No. 30980-1 Slug Thrower Cartridges Master Drawing List Reissued 7/13/2011
AirFrame
Fusulage Construction
Airframe Material
Number of Doors
Wing
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
--Aileron
Aileron Type
Aileron Trim
Aileron Control System
--Flap
Flap Type
Wing Flap Actuation
Empennage
Empennage Type
Empennage Rib Material
Empennage Skin Material
Rudder Trim
Yaw Trim Actuator
Yaw Control System
Pitch Trim
Pitch Control System
Pitch Trim Actuator
Landing Gear
Landing Gear Type
Retractable
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Cabin
Instrument Panel
Flight Control
Number of Seats
Heating
Window Defrost
Cooling
Profiles
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Engine
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Geared
Cooled
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller
Propeller Manufacturer
Propeller Model
Number of Blades
Minimum Diameter
Maximum Diameter
Propeller Type
Propeller Governor
Fuel System
Fuel System Type
Approved Fuel Type 1
Approved Fuel Type 2
Approved Fuel Type 3
Fuel Capacity (G)
Tank Type 1 Location
Tank Type 1 Capacity (G)
Tank Type 2 Location
Tank Type 2 Capacity (G)
Usable Fuel (G)
Oil Capacity (Quarts)
Electrical System
Power Source
Power Storage
System Voltage
Alternator Amp
Battery Voltage
Battery Amp/Hour
Limitations
Maximum T/O Weight (lbs)
Maximum LDG Weight (lbs)
Standard Empty Weight (lbs)
Useful Load (lbs) 0
Station 1 Baggage Location
Max Weight Station 1 (lbs)
Station 2 Baggage Location
Max Weight Station 2(lbs)
Station 3 Baggage Location
Max Weight Station 3(lbs)
Wing Loading (lbs/sq.ft)
Vne (KCAS)
Vno (KCAS)
Va(Max Gross) (KCAS)