North American Navion L-17

Number of Active Aircraft: 11 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1945 lbs
Max Weight 2950 lbs
Useful Load: 1005 lbs
Engine Name CONT O-470-7
Engine Number 1
Horsepower 185 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 17000 ft
Max Fuel 60 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 130 kts
GPH (75% BHP): 12
MPG (75% BHP) 10.8
Range (75% BHP): 563 nm
Fuel Cost Per Seat Mile 0.14 $
Fuel Cost Per Hour 72 $
MPG per 1000 lbs of Payload 10.89
F-T (Speed^2/FuelBurn) 14.1 HP
F-T Payload 14.2 kts
MPH To HP: 7 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 0 ft

SA00024NY Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Amended 10/3/2012
SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
SA00079NY Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Amended 10/31/2012
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00089DE Installation of a left fuselage cabin baggage door assembly. Reissued 7/18/2001
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00241LA Relocate vertical stabilizer from three degrees to zero degrees. Reissued 8/19/1996
SA00243BO (3 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
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
SA00520DE Limited to installation on Navion A serial number NAV-4-1560 ONLY. Issued 7/17/2003
SA00556AT Installation of Appalachian Accessories carbon steel brake discs P/N AA-27A. Reissued 1/24/1995
SA00576NY Installation of an IMI Cash Model EX-2207-44 or EX-2207-45 differential pressure relief valve downstream of the Hartzell A1-B propeller governor. Issued 3/5/1997
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00680SE (2 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00899SE Modification of Hat Aux. Landing Gear Drag Brace Support P/N 145-34161 to P/N 145-34161DOC in accordance with Deluca of California Inc. Drawing List 145-34161DOC-DL Revision N/C dated March 29 1996 or later FAA approved revision. Issued 3/27/2001
SA00950NY Modification of forward cockpit seats and provisions for installation of upper torso restraint system. Reissued 6/2/2005
SA00954SE (1 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
SA01026SE (PAGE 1) Improved fuel gascolator assembly. Amended 12/19/2012
SA01035CH Installation of McCauley Propeller Model D3A36C435/80VEA-0. Reissued 9/23/2005
SA01062SE Install structural reinforcement for increased engine weight and provisions for increased gross weight  Issued 3/11/2002
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
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01473SE (3 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
SA01493LA Limited to installation on serial number NAV-4-1403. Issued 7/11/2003
SA01516AT Installation of Vision Micro Systems Inc. VM1000/EC100 digital/analog engine instrumentation and caution advisory system. Amended 10/24/2008
SA01560WI-D Installation of the Honeywell KFD 840 Primary Flight Display System. );INSERT INTO stc_table VALUES ( REQUIRED DATA: AML No. 159-08325-0002 Revision - dated 12-1-2009. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate. Amended 7/22/2010
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (3 OF 5) Installation of an antenna Amended 2/15/2007
SA01703SE Fuel system alteration to transfer fuel from the auxiliary tank to the main tanks Issued 10/4/2006
SA01772CH Installation of combustion heater kit P/N CD11007K8 per C&D Asociates heater installation instructions IN11007K8 latest FAA approved revision. Issued 2/20/2003
SA01800SE (PG 3) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01860NY (2 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 3)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01923LA Installation of the P-1000 Digital Electronic Tachometer. Issued 1/23/2007
SA01933LA (3 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01988SE (PAGE 4) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02015SE-D Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Amended 2/5/2014
SA02018SE-D (PAGE 2) Provisions installation of Garmin GPS/XM Antennas in accordance with FAA Approved Model List (AML) SA02018SE-D dated January 4 2011 or later FAA approved revision and FAA Approved GPS/XM Antenna STC Master Drawing List Document No.: 005-00638-01 Revision 1 Issued 1/4/2011 0:00
SA02019SE-D Page 2 Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/19/2012
SA02033AT (PAGE 3) 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
SA02119SE Page 2 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02125SE Installation of a Continental E-225-4 engine a Hartzell HC-12V20-7D propeller with V8433N blades and associated accessories and hardware with the existing updraft cooling system in Navion A serial number (s/n) NAV-4-182 4 per Substantiating Data for E-225 Engine Installation In Navion A Model Aircraft Issued 4/22/2011
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 2) Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. Issued 3/23/2001 1:00
SA02217AK (3 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 0:00
SA02265SE Installation of a camera housing Amended 11/1/2013
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02403AK Install a South Wind Model 940D heater Issued 4/23/2013
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02547AT (PG 3) Installation of a Voice Alert System. Amended 8/28/2007 0:00
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
SA02930NY Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3 G2 and G1 as primary Cylinder Head Temperature (CHT) Exhaust Gas Temperature (EGT) and Turbine Inlet Temperature (TIT) Instruments. Reissued 6/12/2012
SA03286CH Install an electronic engine ignition system Issued 1/13/2014
SA09019AC-D Installation of S-TEC System 55 two axis automatic flight guidance system with optional autotrim system Model ST-580. Amended 8/20/2001
SA09283AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-724-20/30. Amended 2/25/1998
SA09284AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-725. Amended 3/4/2002
SA09384AC-D Installation of S-TEC manual electic trim system model ST-835. Amended 3/5/2002
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA1-396 Navion retract links 143-33165 and 143-33165-10 modified. Issued 
SA1-575 External electrical power receptacle. Amended 1/1/1960
SA1-635 HC-A2x20-4/8433 propeller. Issued 1/1/1996
SA1-88 Elimination of carburetor heater muff on aircraft with downdraft cooling systm and Bendix PS5BD carburetor. Issued 1/1/1996
SA10126SC (2 OF 2) Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.  Amended 10/23/2003
SA10236SC (1 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10682SC Installation of alternator and voltage regulator Reissued 11/16/2007
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA1088NE Installation of a Lycoming Textron TIO-540S1AD engine and a Hartzell HC-E2YR-1BF/8477-4 constant speed propeller. Amended 6/13/1995
SA10921SC Installation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulators Issued 11/10/2008
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1124SW Installation of modified wing tips. Reissued 1/23/1989
SA1177WE WECO carburetor temperature monitor. Issued 1/1/1960
SA1190CE Installation of King KFC 200 flight control system (2 axis). Reissued 2/28/2000
SA1219SO Installation of Adjustable  Amended 4/6/1981
SA1246WE Alternator kit 6555-2 and 6555-2-2 Jasco . Amended 10/28/1976
SA1315WE Installation of Mixture Monitor (exhaust gas temperature probe gage and selector) in accordance with Delta Products Part Lists A-192 and A-193 or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9 1981 or later FAA approved revision and/or Drawing List MM-127 dated November 15 1981 or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29 1968 copy attached or later FAA approved revision. Reissued 4/15/2011
SA143SO Control wheel. Issued 1/1/1960
SA1488WE Installation of Brittain Industries Inc. Model B2C Flight Control System Reissued 1/30/2013
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1554GL Installation of On-Board engine analyzer system. Issued 1/24/1991
SA1579WE Installation of Brittain Industries B-4A flight control system. Reissued 10/20/1972
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1582WE Installation of control position indicator (CPI) system. Reissued 3/12/1970
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA162EA Modification of Navion retract link assembly 145-34106. Issued 1/1/1960
SA1678WE Installation of Brittain B-5 flight control system. Reissued 10/20/1972
SA1716WE Installation of exhaust gas temperature (EGT) system. Amended 3/20/1970
SA179WE Main landing gear retract link assembly ANS 0003. Issued 1/1/1960
SA1890NM Installation of single piece windshield. Reissued 1/29/2007
SA200CE Nose and main gear retracting link replacement. Issued 1/1/1960
SA2120WE Installation of Brittain Industries NAV-2B flight control system. Reissued 6/21/2013
SA2190NM Page 2 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2232NM Lower canopy height 4 inches. Reissued 6/10/2002
SA2261NM Installation of Hoskins Model CFS-1000A -1001A FT-100 or FT-101 fuel flow indicating system. Reissued 1/30/1998
SA2350NM Page 2 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2377NM Installation of a Beech Model 278-100-7/278-214-82 propeller with associated spinner and back-up plate. Issued 4/27/1984
SA249EA Airborne mechanisms dry vacuum pump and regulator. Reissued 1/9/1992
SA252WE Nose landing gear retract link assembly ANS 0004. Issued 1/1/1960
SA253GL Installation of a Continental E-225-4 engine modified in accordance with STC SE23SW in lieu of a Continental E-225-4 which was installed. Reissued 1/16/1992
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 3) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2619WE Installation of Pathfinder Model P1-( ) autopilot system. Reissued 9/30/1998
SA2620WE Installation of Pathfinder Model P2-( ) autopilot system. Reissued 9/30/1998
SA2653WE Installation of Beryl D Reissued 7/14/2011
SA2654WE Installation of Pathfinder Model P2A( ) autopilot. Amended 7/3/1979
SA2683NM Installation of Precise Flight Inc. stand-by vacuum system (SVS) Amended 3/10/2005
SA2687NM (PAGE 2) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000 0:00
SA268SW Automatic pilot AK116. Issued 1/1/1960
SA2693NM (PAGE 2) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009 0:00
SA278SO Main and nose landing gear retract links. Issued 1/1/1960
SA292CE Nose gear shimy damper. Issued 1/1/1960
SA2946WE Istallation of new design cabin air valve. Reissued 1/23/1989
SA2961WE Installation of Pathfinder autopilot systems and/or electric pitch trim systems. Reissued 9/30/1998
SA298SW Autopilot AF-512A or AF-512B. Issued 1/1/1960
SA299SW Autopilot AF-510A. Issued 1/1/1960
SA3-176 Electric remote compass. Issued 1/1/1960
SA3-191 Arcon B automatic rudder control. Amended 4/26/1966
SA3-31 Alternate repair parts for bulkhead. Issued 1/1/1960
SA3-492 Window and windshield. Issued 1/1/1960
SA3-532 Fabriction and installation of rotating beacon brackets on aircraft with Grimes D-7080-1 light. Issued 1/1/1960
SA3-60 Bushing in attachment plate hole of Palo Alto alteration of angle of incidence of horizontal stabilizer. Issued 1/1/1960
SA3077SW-D Mitchell automatic flight system AK553 consisting of Century I autopilot with optional omni tracker. Reissued 6/21/1984
SA308EA (1 OF 2) Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Marvel-Schebler MA-2 MA-3 MA-4 MA-4-5 MA-6 and HA-6 series carburetors. (Normal Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.) Amended 11/20/1978
SA3224SW-D Mitchell automatic flight system AK701 consisting of Century I autopilot with optional omni tracker. Reissued 12/7/1983
SA3225SW-D Mitchell automatic flight system AK704 consisting of Century IIB autopilot with optional radio coupler. Reissued 12/7/1983
SA3328SO Install landing gear wheel cover. Reissued and Amended 12/17/1999
SA334SW Installation of InterAv Alternator. Reissued 7/20/1981
SA3447WE Installation of steel engine mounting brackets. Reissued 1/23/1989
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA3638WE Installation of new air induction system with a filter on the alternate air source. (NAVION H Normal and Utility Category) Reissued 3/11/2004
SA3639WE Installation of warning light intended to prevent inadvertent operation of the aircraft on the aircraft on the tip tank fuel system while in the landing or take-off configuration i.e. gear down. Reissued 3/11/2004
SA3640WE Installation of flap lower close out strip. Reissued 8/19/1996
SA36CE Zip tip wing tips. Issued 1/1/1960
SA36GL Install Cleveland Aircraft Products wheel and brake conversion kit P/N 199-52. Reissued 10/28/1980
SA374WE Modified carburetor air intake system. Issued 1/1/1960
SA3776NM Installation of continental TSIO-520-T engine McCauley D3A34C402/90DFA-10 propeller and associated installation ocomponents. (NAVION A (L-17B) S/N NAV-4-1560(N4560K)) (NAVION A (L-17C) S/N NAV-4-1560(N4560K)) Reissued 1/13/2000
SA3786WE Installation of a tubular engine mount cowling cooling baffles air induction system and cowl flap mechanism Reissued 3/6/2013
SA379NW Installation of a 3-bladed McCauley D3A32C90-M/S-82NC-2 propeller on a Continental IO-470-H engine Issued 11/26/1976
SA3821WE Installation of single piece windshield canopy side and rear windows. Reissued 1/23/1989
SA3837NM Flush rivet fuselage skins(double dimpling). Issued 5/20/1987
SA3862NM Page 2 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA3935WE Installation of an air/oil separator. Reissued 9/28/2001
SA3936WE Installation of an air/oil separator. Reissued 9/28/2001
SA4-1007 Installation of balance weights(Brittain Aircraft P/N 3010) on leading edge of Navion ailerons. Reissued 9/17/1987
SA4-1121 Increase in allowable gross weight from 2850 to 3100 pounds per STC SA4-915 when equipped with 20 gallon wing-tip tanks (Brittain Aircraft P/N 1000) installed. Reissued 9/17/1987
SA4-1165 Installation of Firestone Model DFA-180 or Bodell BMI-2000 wheel in lieu of Firestone 6C5 or Goodrich 613MD wheel (on nose gear). Reissued 6/26/2003
SA4-118 Hartzell HC-12X20-7C/8433-0 propeller including governor kit. Reissued 3/11/2004
SA4-1432 Fiberglass vertical stabilizer tip assembly ANS 0001 and Grimes rotating beacon G-8400A-8-12 or D-7080-1-12. Issued 1/1/1960
SA4-146 Globe gyro-stabilizer. Issued 1/1/1960
SA4-1483 Fiberglass vertical fin tip and Grimes rotating beacon F-7080-1-12 or G-8400A-8-12. Issued 1/1/1960
SA4-1626 Fiberglass nose wheel streamlined fairing. Reissued 8/19/1996
SA4-229 1. Removal or original step and installing Retractable step and handle. );INSERT INTO stc_table VALUES ( );INSERT INTO stc_table VALUES ( 2. Installation in accordance with Robert Douthitt Reissued 2/11/2004
SA4-241 Change in incidence angle of horizontal stabilizer for Symons Engineering kit. Issued 
SA4-313 Toe brake kit and parking brake. Reissued 8/19/1996
SA4-35 Wing root-fuselage fiberglass contoured fairings at leading edge of wing and aluminum fairings contoured to existing fillet at inboard end of wing flaps extending aft to station 226. Issued 1/1/1960
SA4-363 Autopilot and optional add-on coupler BI-300 BI-301 or BI-304. Reissued 10/1/1973
SA4-685 Aerofilter 30409A with element 1A0235. Issued 1/1/1960
SA4-915 Installation of Brittain Mark II20-gallon wing tip tanks(P/N 2009). Reissued 8/17/1987
SA4-925 Magnetic flight director 2000. Issued 1/1/1960
SA4005NM (PG 3) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4022WE Installation of toe brakes and revised rudder pedals at pilot station. Reissued 1/23/1989
SA4154WE Installation of tubular engine mount cowling cooling baffles air induction system and cowl flap mechanism Reissued 3/6/2013
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA4302NM (PAGE 3) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989 0:00
SA4358WE Installation of landing gear door kit. Reissued 3/6/2013
SA4426NM Installation of aileron gap seals. Amended 2/7/1986
SA46GL Install Cleveland Aircraft Products wheel and brake conversion kit P/N 199-52A. Reissued 10/28/1980
SA4721NM Installation of SynCon alarm system. Amended 5/8/1990
SA477NW Installation of a Lycoming engine and a Hartzell propeller Issued 7/8/1977
SA4882NM Installation of Moonshadow full view canopy. Reissued 4/26/2005
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA5180NM Installation of engine as modified by STC SE5177NM. Amended 2/27/1992
SA543SW Installation of Alcor turbocharger on aircraft modified to Continental IO-470-H engines. Reissued 9/30/2002
SA54WE Installation of single-piece windshield and side windows. Reissued 8/1/1973
SA5581SW Installation of ALCOR true-flow/ totalizer system. Requires STC SE5583SW which can be installed on aircraft equipped with Teledyne Continental engines IO-360 L/TSIO-360 TSIO-360 TIO-360 TSIO-470 GTSIO-520 L/TSIO-520 TSIO-520 IO-520 and IO-470. The approved model numbers listed may not be inclusive. Amended 9/30/2002
SA5656NM Installation of burglar alarm system. Reissued 7/21/1993
SA5656NM (PAGE 1) Installation of burglar alarm system. Reissued 7/21/1993
SA570WE Exhaust system. Issued 1/1/1960
SA572NW Installation of a Lycoming GO-480-C1D6 engine Hartzell HC-83X20-2A/9333C-3 three bladed propeller modified carburetor heat box modified engine mount and cowling oil radiator with flush type ram air inlet and external scoop modified cowl flap paper carburator air filter and duel battery system Issued 3/22/1978
SA5812NM Installation of a Lycoming GO-480-G1D6 engine. Limited to installation on serial number NAV-4-2258B ONLY. Issued 6/19/1992
SA5830NM Installation of a Continental IO-520-L engine and McCauley D3A32C88 propeller. Limited to installation on serial number NAV-4-1499 ONLY.  Issued 9/22/1992
SA5890NM Installation of wing leading air vent system. Reissued 8/19/1996
SA589WE Full flow oil filter F-94056 and F-94056-12 with element E-3560 MEL 800. Reissued 10/5/1976
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 (3 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
SA6038NM Installation of control wheels. Issued 7/21/1993
SA604WE B-4 flight control system including PC-1 pitch assist AH-1 altitude hold and NAV-1 navigation. Reissued 10/1/1973
SA630WE Installation of oil filter assemblies. (NAVION A AND B with optional engine) Reissued 8/29/1974
SA644WE Dynertial pitch assist PC-1 and optional altitude hold AH-1. Reissued 10/1/1973
SA662WE Hi-Lo sensitivity adaptor BI-400 and autopilot with NAV-1 navigation coupler and heading lock. Reissued 10/1/1973
SA695CE Install Frantz oil filter. Amended 1/20/1987
SA7088NM Installation of a Teledyne Continental Motors IO-550B engine McCauley D3A32C409C/82NDB-2 propeller tubular engine mount cowling baffles air induction system and cowl flap mechanism Reissued 3/6/2013
SA71GL Installation of air filters Reissued 6/20/2000
SA750SW Installation of tiptank fairings and drain cover. Reissued 12/10/1984
SA751SW Revised nose gear doors and fixed main gear wheel fairings. Reissued 12/10/1984
SA752WE Lycoming GO-480-BID engine and Hartzell BC-S2X20/9333C-3 propeller. Reissued 10/5/1993
SA758WE Installation of modified Navion main landing gear wheel and axle. Eligible only on the Navion aircraft models which have Goodrich (Hayes expander tube brakes) wheels Models 6057MD or G-14-720-NO-1. Reissued 9/14/2000
SA769WE Lear Romec fuel pump R6-15980 on Continental E-185-3 engine. Issued 1/1/1960
SA798EA Installation of Monitair exhaust gas combustion monitor kit. Reissued 2/14/1972
SA8357SW-D Installation of S-TEC system 65 two axis automatic flight guidance system Model ST-491. Amended 2/28/2002
SA8363SW-D Installation of S-TEC System 60 two axis automatic flight guidance system with optional autotrim system Model ST-504. Amended 2/27/2002
SA8375SW-D Installation of S-TEC System Issued 11/1/1993
SA878WE N-2 flight control system. Reissued 10/1/1973
SA917EA Installation of Grimes aviation white anti-collision strobe light system two light or three light series 555 for wing tips and tail P/N 30-0555-( ). Reissued 6/4/2007
SA955NW Installation of a Continental E-225-4 engine using updraft cooling with a Hartzell HC-12X20-5/8433-O propeller  Issued 6/27/1980
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)