Champion 7ECA Citabria (115)

Number of Active Aircraft: NA Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 2
Empty Weight: 1060 lbs
Max Weight 1650 lbs
Useful Load: 590 lbs
Engine Name LYC O-235-C1
Engine Number 1
Horsepower 115 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 12000 ft
Max Fuel 35 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 99 kts
GPH (75% BHP): 10
MPG (75% BHP) 9.9
Range (75% BHP): 277 nm
Fuel Cost Per Seat Mile 0.3 $
Fuel Cost Per Hour 60 $
MPG per 1000 lbs of Payload 5.84
F-T (Speed^2/FuelBurn) 9.8 HP
F-T Payload 5.8 kts
MPH To HP: 8.6 kts
T/O Roll - T/O over 50 FT OBST 450 ft / 715 ft

A2309WE  Installation of Madras Air Service Part Number 104 Wing Tips Amended 10/4/1985
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
SA00068SE (PAGE 1) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010
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
SA00087NY Installation of Cu-Sonde Meteorological Measurement/system models CS-1A or CS-1B and installation of Cu-Sonde Model CS-1B-RF with AIRDAT-9600. Reissued and Amended 8/22/1995
SA00091BO Installation of Lycoming O-360-C2E engine Sensenich 76EM8S9-0-56 propeller and Bellanca 8GCBC cowling and engine mount. Issued 8/21/1998
SA00096BO Installation of Lycoming O-360-C2E engine Sensenich 76EM8S9-0-56 propeller Bellanca 8GCBC cowling and engine mount. Issued 1/11/1999
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
SA00191AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00196AT Installation of Appalachian Accessories carbon steel brake discs that have melonite surface treatment P/N AA-17. Reissued 11/14/1994
SA00212BO Installation of Lycoming O-320-A2B engine and Sensenich 74DM6S8-1-52 propeller limited to 7ECA serial number 328 ONLY. Issued 3/9/2005
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00232SE Installation of vortex generators on the wings and tail surfaces. Amended 4/12/2005
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
SA00433NY Installation of Airwolf remote mounted engine oil filter model AFC-500 or AFC-600 on multi engine fixed wing light aircraft incorporating Franklin reciprocating engines of 450 horsepower or less. Amended 10/31/2012
SA00434SE ..Installation of modified front and rear wing spars in accordance with instructions sketches and photographs submitted with January 14 1996 letter from Rainbow Flying Service to the FAA or later FAA approved data . Issued 5/2/1997
SA00445AT Installation of Canadian Aircraft Products Model 67-2000 floats. Issued 3/23/1994
SA00464DE Installation of a Textron Lycoming O-360-C2A engine and McCauley model 1A200HFA8041 or 1A200FA8054 propeller. Approved for serial number 439-73 ONLY. Issued 11/14/2001
SA00478CH (PAGE 1) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00478CH (PAGE 3) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
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
SA00795SE Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2131 Revision A dated April 22 2001 and Installation Manual MA2132 Revision A dated April 22 2001 or later FAA approved revision of either of these documents. NOTE: If more than five vortex generators are damaged or missing the aircraft is not airworthy. Amended 7/19/2001
SA00823SE  );INSERT INTO stc_table VALUES ( Fabrication and Installation of Rainbow Flying Service front and rear wing spars and modified wing ribs Amended 8/8/2006
SA00860SE Installation of Rainbow Flying Service fuselage formers. Issued 12/24/2000
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA01014AT Convert Aeronca 7DC to a 7AC per C.W. Lasher Report 4316 E. Issued 4/15/1996
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
SA01089SE Improved replacement floor boards. Issued 5/17/2002
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01158WI (2 OF 2) Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. Amended 3/29/2005 1:00
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
SA01240SE (3 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
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 1) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01555AT Install Continental Model A-65-8 McCauley Model 1A90 propeller and engine accessories on Ballanca 7AcA airplane S/N 44-72. Issued 2/11/1998
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
SA01750CH Installation of Swing Type Engine Mount per Air-Energy Service Inc. installation instructions AESI D1018 Rev A dtd 7/31/2001 or later FAA approved revisions. Reissued 10/23/2004
SA01761SE ONE-ONLY: Installation of electrical system including Starter Alternator and Battery and systems modifications S/N 7AC-5704 Issued 5/15/2007
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 1 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
SA01944CH (1 OF 2) Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. Issued 3/5/2004
SA01988SE (PAGE 1) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
SA02033AT (PAGE 1) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. Amended 7/25/2008
SA02110CH (PAGE 1) 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
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
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
SA02212AK (PG 1) 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
SA02268CH (PAGE 1) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02321AK Installation of EDO 89-2000 floats modified Issued 8/29/2008
SA02370AK Option (1) Installation of a replacement main tank fuel valve Reissued 5/13/2010
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02566CH Installation of the Custom Fiberglass Molding Inc. (CFMI) Model 1500 Aircraft Main Landing Gear Skis. Amended 3/6/2009
SA02604CH Installation of a battery powered engine starting system. Issued 7/24/2008
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02795AT Installation of a PXE7300SR In-Flight Entertainment System Issued 2/12/2004
SA02979CH Installation of the Lycoming O-320-A2B engine in accordance with H. O. Aircraft Inc. Installation Manual Document No. IM-7ECA-320 Rev. IR dated 5/12/2011 FAA approved on 7/1/2011 or later FAA approved revision. Issued 7/1/2011
SA02987CH Installation of the Electroair Electronic Ignition System Amended 7/23/2013
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA1-319 Continental C85-12 engine. Issued 
SA10077SC Installation of push-button starter system. Amended 4/26/2005
SA1008WE Installation of Poly-Fiber covering material. Reissued 5/27/2003
SA10126SC (1 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
SA105NW Mounting and wiring for occasional installation and use of Barnes Engineering Company airborne fire spotter system. Issued 4/30/1974
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
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
SA1151NW Installation of North American Industries Inc. Model 135 pistol grip Amended 3/29/2002
SA1177WE WECO carburetor temperature monitor. Issued 1/1/1960
SA124EA Shur-Vent fuel tank filler cap. Issued 1/1/1960
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
SA1351WE (PG 1) Replace existing fabric on wings fuselage empennage and/or control surfaces with Ceconite101 material. (262A Series -12) Amended 8/19/1983
SA1351WE (PG 2) Replace existing fabric on wings fuselage empennage and/or control surfaces with Ceconite101 material. (262A Series -12) Amended 8/19/1983 0:00
SA1358GL Install Model R2800 retractable skis. Issued 3/7/1989
SA1417GL Install Model R2800 retractable skis. Issued 10/12/1989
SA1470NM Installation of a six-foot shorter span wing two 6.5 gallon auxiliary wing tanks a Continental O-200-A engine a McCauley 1A101/GCM6948 propeller a 3-inch propeller spacer a gross weight increase to 1317 pounds. Reissued 3/16/1992
SA1487NM Installation of a Lycoming O-360-C1A engine Hartzell HC-C2YK-4CF/FC7666A-2 propeller and associated systems Amended 11/14/1984
SA1504GL Surrendered and incorporated into STC SA241CH. Surrendered 6/14/2002
SA150SO Installation of surface fabric attachment clip. Reissued 6/3/1991
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1536WE Installation of larger rudder. Reissued 6/5/1969
SA1562GL Install Lycoming engine model O-320-A2B and Sensenich propeller 74DM6S8-1-56 and other associated components. Approved for installation on Bellanca Model 7ECA Serial Number 1246-78 only. Issued 3/28/1991
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1674NM Installation of a Continental C85-12F engine and a McCauley 1B90/CM7143 propeller Issued 9/17/1982
SA1679NM Installation of a Teledyne Continental A75-8 with McCauley 1B90CM7042 propeller Issued 7/28/1982
SA1684NM Replacement of the original Teledyne continental A-65-8 engine with a Teledyne Continental A75-8 engine and McCauley 1B90CM7042 propeller Issued 8/17/1982
SA1735GL Installation of Master Nag warning system. Amended 3/21/1994
SA174WE Remove Right-Hand Cabin Door to facilitate Aerial Photographs parachute etc.  Issued 7/8/1962
SA1768GL Install Aero Fabricators shoulder harness and seat belt assembly. Issued 7/1/1992
SA1786NM Installation of enlarged rear side window skylight left wing 5.5 gallon auxiliary fuel tank and Cleveland wheels and brakes (as used on the 7ECA). Issued 3/31/1983
SA18CE Installation of Pee-Kay Model 1800 or B1800 (TSO-C27-2) seaplane floats. Reissued 12/23/1980
SA1912NM Installation of Schneider wheel skis 6-inch x 10-inch aluminum wheel adapters and 29x11.0-10 8-ply minimum tires on main landing gear. Issued 12/25/1983
SA191NE Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. Reissued 10/4/1984
SA1970CE Operation of airplanes on unleaded automotive gasoline Amended 3/5/2012
SA1974SO Installation of Appalachian Accessories stainless steel brake discs. Reissued 9/29/1995
SA19SO Installation of left and/or right auxiliary fuel tank(s). Reissued 6/24/1996
SA2-227 Windshield manufactured in accordance with Luminous Plastics Inc. Drawing LP-102 and 202. Reissued 4/9/1979
SA2-934 Installation of fiberglass covering IAW Instruction No. 39-5. Reissued 9/10/1996
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA216AL Install L-2500A skis. Issued 1/1/1960
SA216SW Conversion of aircraft to tri-cycle gear configuration. Issued 1/1/1960
SA217AL Install L-1650A or L-2000A skis. Issued 1/1/1960
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
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
SA220SO Tow bar release mechanism and safety tow link. Reissued 10/3/2011
SA2309WE Installation of Madras Air Service Part No. 104 wing tips. Amended 8/19/1983
SA232SO Change Aeronca Model 7AC powerplant from Teledyne Continental Motors (TCM) model C65-8 to TCM model C85-12 or C85-12F or change Aeronca model 7BCM from TCM model C85-8 series engine to the C85-12 or C85-12F in accordance with Star Aircraft Company Instruction S.A. 301 and Report No. 300R. Either modification can use the Sensenich model 72GK propeller with pitch settings from 44 through 50 inches. The Notes Section of Type Certificate Data Sheet P-170 has information concerning required plates flange adapters etc. Reissued 7/23/2003
SA2335SO Installation of Appalachian Accessories P/N 73-5 brake discs. Reissued 9/29/1995
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2354NM Installation of a Lycoming O-360-C1A and a Hartzell HC-C2YK-4CF/FC7666A-2 propeller and associated systems Reissued 11/14/1985
SA241CH Install Ceconite 101 fabric. Amended 7/11/2006
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 1) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008
SA25RM Installation of Christen Model 801 Inverted Oil System. Issued 3/28/1974
SA261AL Installation of Airglas Model L2000 and L-1650 wheel replacement skis. Amended 11/22/1968
SA266AL Installation of L-2500 skis. Amended 6/21/1968
SA2683NM Installation of Precise Flight Inc. stand-by vacuum system (SVS) Amended 3/10/2005
SA2687NM (PAGE 1) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000
SA2693NM (PAGE 1) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009
SA2699CE Installation of aileron spades. Amended 9/19/1991
SA2710WE Installation of carburetor heat box bearings. Issued 6/15/1973
SA274WE Fuel system modification. Issued 1/1/1960
SA283AL Installation of Hartzell HC 82XL-1 -2 or -6 propeller hub with 7636D-4 blades or HC-C2YL-1B hub with 76634 blades and appropriate Woodward governor. Amended 7/22/1969
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA2856SO Installation of Basic Type BPE-14 Model No. 1008 air driven alternator. Issued 11/7/1990
SA286EA Edo 60-1320 floats. Issued 1/1/1960
SA3-214 Installation of Wipaire Skis Model3000 main skis and Model 1000 tail ski. Reissued 2/16/1993
SA3-215 Laminated plastic and fiberglass nose cowl D-576P. Issued 1/1/1960
SA3-303 Reinforced plastic instrument panel (exact duplicate of 5-150). Issued 1/1/1960
SA3-322 Door modified to seaplane door. Issued 1/1/1961
SA3-361 Installation of Wipaire Skis Model C-2200 main and Model CTF-2200 tail wheel skis. Reissued 2/16/1993
SA3-362 Installation of Wipaire Skis Model C-2200 main and Model CTF-2200 tail wheel skis. Reissued 2/16/1993
SA3-368 Installation of Wipaire Skis Model A2000A main wheel replacement ski. Reissued 2/16/1993
SA3-372 Installation of Lycoming O-235-C1 -C1A -C1B -C1C -C2A -C2B -C2C -H2C -K2A -K2B -L2A or-L2C series engines and appropriate propellers or Teledyne O-200A -B or -C series engines and appropriate propellers. Reissued 7/8/2009
SA3-424 Installation of Wiparie Skis Model CTF-2200 (Acft Skis) (FluiDyne) (Federal) tail ski on airplanes equipped with Scott Model 3000 tail wheel. Reissued 2/16/1993
SA3-432 Install two auxiliary fins one ventral fin and Pee-Kay Model1800 floats. Reissued 12/23/1980
SA3-435 Install Continental A-75-8 or A-75-8F engine. Reissued 1/29/1999
SA3-496 Install two auxiliary fins one ventral fin and Pee-Kay Model 1800 floats. Reissued 12/23/1980
SA3-515 Skis L-1500A on main gear and L-1200A on nose gear. Issued 1/1/1960
SA3-523 Install four auxiliary and one ventral fin and Pee-Kay Model1800 floats. Reissued 12/23/1980
SA3-6 Installation of Pee-Kay Model1500 floats. Reissued 12/23/1980
SA3-628 Installation of Wipaire Skis Model3000 main and Model 1000 nose skis. Reissued 2/16/1993
SA3019WE Installation of 8.50 x 6.00 4-ply rated Type III aircraft tires. Issued 4/30/1975
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
SA312CH Installation of shoulder harness and crotch straps. Issued 3/23/1995
SA323AL Installation of McCauley 1A175- GM8042 propeller. Issued 5/21/1969
SA334CE Installation of Pee-Kay Model 1800 or B1800 (TSO-C27-2) seaplane floats and two auxiliary fins. Reissued 12/23/1980
SA3358NM Production of aircraft wing ribs as specified in W. N. Kutner s Report #1 STC Request for Wing Ribs.  Reissued 12/5/2008
SA33CE If Champion Part Number 7-480 door is installed remove two of AN 380-2-2 cotter pins and two of AN 393-3 flat head pins as necessary to remove one door. If American Champion Part Number 7-1265 door is installed remove quick release pins to remove one door. Reissued 3/6/2013
SA33GL Installation of EDO Model 88A-1650 floats. Reissued 3/29/1983
SA34CH Installation of Cleveland Main Wheels 40-28 and brakes 30-19. Amended 5/16/2005
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA356CH Installation of seaplane safety covers. Issued 5/22/1995
SA3618NM Application of polyurethane finishing system. Issued 7/15/1987
SA3697NM Convert from tricycle gear configuration into conventional gear confuguration Issued 2/18/1987
SA374GL Remove tri-cycle landing gear and install main landing gear and tail wheel. Approved for installation on serial No. 128 only. Issued 12/16/1979
SA37NW Installation of a Continental O-200-A engine a McCauley propeller and a Whelan strobe light Issued 4/9/1973
SA3829NM Installation of aluminum wing spars in accordance with FAA Approved Drawing List No. 001 Revision C dated March 6 1986 and installation instructions BHM-000 Revision E dated April 21 1987 or later FAA-approved revision. Amended 9/9/2004
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA4-1009 Eonite covering on complete airplane. Issued 1/1/1970
SA4-1210 Installation of Eonnex cover on aircraft surfaces. Reissued 8/19/1980
SA4-1636 Tri-cycle landing gear. Issued 1/1/1960
SA4-276 BN-1 propeller spinner. Issued 1/1/1960
SA4-338 Addition of exhaust stacks with venturi pump control valve and tank for insect control work. Issued 1/1/1960
SA4-359 Glass cloth with resin. Issued 1/1/1960
SA4-369 Lift strut assemblies. Issued 1/1/1960
SA4-444 Carburetor and cabin hot air muff with replaceable air inlet and outlet. Issued 1/1/1960
SA4-699 R003-232-72T propeller with Continental C-90-12 engine. Issued 1/1/1960
SA4-836 Ceconite 101 covering of entire airframe. Issued 1/1/1960
SA4-840 Fabric replaced with glass cloth on wings fuselage empennage and/or control surfaces. Issued 1/1/1960
SA4-97 Installation of an auxiliary five-gallon tank in wing Reissued 11/19/2012
SA4005NM (PG 1) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4094NM Installation of Oilamatic engine preoiler. Amended 6/28/1991
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA4302NM (PAGE 1) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA4375WP Installation of saddle blocks as replacement for landing gear attachment U-bolts (P/N 1-9805). Issued 10/29/1981
SA442AL Installation of 8.50x6 4- or 6-ply rated Goodyear or UniRoyal tires. Amended 11/7/1973
SA4503NM Install Ceconite covering material. Reissued 2/25/2011
SA4624NM Installation of F. Atlee Dodge springs 2097 and 2127 to replace bungee cords on ski equipped airplanes. Issued 2/21/1990
SA4760NM Replace wing rib PK screws with Marson Klick fast rivets (pop rivets). Amended 2/22/1996
SA4773NM Installation of replacement metal leading edge. Reissued 2/6/1992
SA483AL Installation of McCauley 1B90-LCM-7534 propeller. Reissued 1/31/2008
SA4896NM Installation of modified front folding seats. Issued 8/9/1990
SA489EA Installation of ARP Inc. carburetor ice detection system Models 107AP (-12 -R-12 -24 and -R-24 series) in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Precision A ir-Motive (Facet or Marvel-Schebler) MA-2 MA-3 MA-3SPA MA-4 MA-4-5 MA-4SPA MA-5 MA-6 MA-6AA and HA-6 series carburetors. Amended 12/5/2002
SA4933NM Removal of 13-gallon fuel tank and mechanical brakes and installation of 18-gallon wing tanks and hydraulic brakes. Issued 5/15/1990
SA4950NM Installation of a Franklin 4AC-199-E3 Hp. engine. Issued 6/26/1990
SA4NW Installation of Plane Booster Wing Tips Issued 8/17/1972
SA5-49 Tires and tubes 25x11x4. Issued 1/1/1960
SA5-68 Airglass Engineering L1500A main and L1200A nose skis. Issued 1/1/1960
SA507CH Installation of Cleveland based hydraulic toe brake rudder pedal system. Reissued 4/22/2005
SA513AL Installation of Hartzell model HC-C2YL-1BF/F8468A-8R constant speed propeller. Reissued 4/26/2007
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA520AL Installation of leading edge cuff stall fences tip fences. Amended 2/2/1977
SA531CH Installation of Mitchell oil pressure gauge and oil temperature gauge. Issued 7/16/1996
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
SA5656NM Installation of burglar alarm system. Reissued 7/21/1993
SA5656NM (PAGE 1) Installation of burglar alarm system. Reissued 7/21/1993
SA5739NM Installation of aluminum flange extension angles for attaching ribs to BHM metal spars. Issued 7/10/1992
SA5755NM Installation of a propeller anti theft device. Issued 8/5/1992
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 (1 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009
SA608AL Install leading edge cuff. (7KCAB land only) Amended 8/31/1977
SA615EA (PAGE 2) Installation of Whelen Anti-Collision Strobe Light Systems Part Number 01-0770006-( ) 01-0770028-( ) 01-0770029-( ) 01-0770062-( ) 01-0770900-( ) and 01-0771055-( ) as replacement for originally installed anti-collision lights. Reissued 7/6/2010
SA630WE Installation of oil filter assemblies. (NAVION A AND B with optional engine) Reissued 8/29/1974
SA639NW Installation of a Lycoming O-320-A2D engine Sessenich 74DM6S8-1-56 propeller and larger carburetor fuel inlet lines installed Reissued 11/8/1978
SA648NW Shorten wings by removing just the tip bows and adding stronger wing struts and fuselage strut brackets Issued 8/3/1978
SA670NW Installation of Citrabria cowling baffling and a 1A100/ACM 7254 propeller Issued 9/26/1978
SA693CE Replace existing engine induction air filter with AC Spark Plug filter. Reissued 6/20/2000
SA6AL L-1500A A1650A or L-2000A main skis and L-1200A nose ski. Issued 1/1/1960
SA71GL Installation of air filters Reissued 6/20/2000
SA726AL Installation of Northland Aviation main landing gear U clamps. Issued 4/16/1982
SA728AL Installation of Schneider Model SWS-4000 main wheel skis and Schneider Model SWS-1000 tail wheel skis. Issued 6/25/1982
SA732GL Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index. Surrendered 3/5/2004
SA73CH Installation of Wing Strut Fittings P/N SAR 2-893 or SAR 2-893-1 and stiffeners P/N 2-5009 in accordance with Safe Air Repair Installation Instructions SAR 2-5007 no revisions dated April 30 1993 or later FAA approved revisions. Reissued 4/22/2005
SA745EA Installation of Edo Model 88-88-1650A floats. Reissued 9/17/1982
SA753GL Incorporated into STC SA00478CH. Surrendered 6/14/2002
SA754CE Install Aero Model M1500 M1800 or M2000 main skis. (7GCAA w/oleo) Reissued 2/12/2004
SA755CE Install Model M1500 M1800 or M2000 main skis. (7GCBC w/landing gear) Reissued 2/13/2004
SA779NW Installation of a Continental engine and McCauley propeller Issued 6/12/1979
SA7965SW Application of fabric and polyurethane finishing system. Amended 7/15/1994
SA798EA Installation of Monitair exhaust gas combustion monitor kit. Reissued 2/14/1972
SA800EA (PAGE 1) Installation of Aviation White Anti-Collision Strobe Lights. Whelen Models A429 A430 A434 A450 A408 (white) A408R/W or A47OR/W (red/white) A500 A625 or A650 and associated power supplies or Model SA strobe light system. Amended 7/6/2010
SA8075SW (PAGE 1) Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER) Reissued 11/10/2003
SA8431SW Installation of R15VON alternator control unit. Amended 1/6/1994
SA847GL Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index STC SE800GL approved 87 minimum antiknock index. Surrendered 3/5/2004
SA89AL Installation of auxiliary fuel tanks. Amended 2/7/1975
SA938NW Replacement of the original landing gear original wheels and mechanical brakes modification of vertical stabilizer and forward fuselage structure Issued 5/12/1980
SA942GL Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index. Surrendered 3/5/2004
SA974NW Installation of a Continental engine and a McCauley propeller Issued 7/3/1980
SA977NW Installation of automatic flagmen Model No. 5A. Reissued 8/27/2001
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)