Grumman American AA1C Lynx, T-CAT

Number of Active Aircraft: 114 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 2
Empty Weight: 1060 lbs
Max Weight 1600 lbs
Useful Load: 540 lbs
Engine Name LYC O-235-L2C
Engine Number 1
Horsepower 115 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 11500 ft
Max Fuel 22 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 117 kts
GPH (75% BHP): 7
MPG (75% BHP) 16.7
Range (75% BHP): 276 nm
Fuel Cost Per Seat Mile 0.18 $
Fuel Cost Per Hour 42 $
MPG per 1000 lbs of Payload 9.03
F-T (Speed^2/FuelBurn) 19.6 HP
F-T Payload 10.6 kts
MPH To HP: 10.2 kts
T/O Roll - T/O over 50 FT OBST 890 ft / 1590 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 1) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010
SA00079SE Installation of low oil pressure warning in conjunction with ADC (Oberg) oil filter. Amended 11/10/1994
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00161BO (2 OF 3 Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005 0:00
SA00187AT Installation of carbon steel brake discs P/N AA-20. Reissued 11/14/1994
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00238SE Installation of Aviation Development Corporation s sump mounted chip detector Issued 10/31/1995
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
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
SA00269BO (2 OF 3) Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ) Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1 and Avidyne Mounting Tray P/N 700-00034-000. Reissued 4/9/2010
SA00281BO Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ) Sensor Systems Inc. Antenna P/N S67-1575-109 or equivalent and optional Avidyne Mounting Tray P/N 700-00165-000 Amended 4/24/2012
SA00290BO ( PAGE3) Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX Reissued 7/1/2010 0:00
SA00393SE Installation of the G/S 2500 and G/S2500R Aircraft Security Alarm System. Issued 12/6/1996
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
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
SA00985CH Replace Lycoming O-235-C2C with O-235-K2C engine or Lycoming O-235-C2C engine modified by Precision Engine STC SE00988CH. Issued 2/8/1999
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
SA01240SE (1 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
SA01250WI Installation of Concorde Sealed Lead-acid (VRSLA) battery Reissued 7/30/2012
SA01280CH Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) Issued 8/29/2000
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01470AT Installation of composite spinner. Amended 10/13/2000
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
SA01487SE-D (Page 2) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
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
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 (3 OF 5) Installation of an antenna Amended 2/15/2007
SA01800SE (PG 2) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01861SE (PAGE 2)  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 (2 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
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 4) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02013CH Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). Amended 5/2/2011
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 1) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. Amended 7/25/2008
SA02119SE Page 2 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02153LA-D (Page 2) 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
SA02212AK (PG 4) 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 5) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02268CH (PAGE 6) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02283SE Page 2 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02547AT (PG 2) 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 3) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02795AT Installation of a PXE7300SR In-Flight Entertainment System Issued 2/12/2004
SA02987CH Installation of the Electroair Electronic Ignition System Amended 7/23/2013
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA09382SC Installation of extended range fuel tanks. Issued 10/1/1997
SA1009NW Installation of a dorsal fin (P/N 5302040-1) and associated assemblies Issued 8/21/1980
SA1010CE Installation of wing leading edge cuffs. Amended 8/21/1984
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
SA1012NW Installation of auxiliary fuel tank models 2 TAFTA and 4 TAFTA and incresed gross weight Reissued 7/17/1984
SA1016NW Installation of a Lycoming O-360-A4M engine Sensenich 76EM8-0-62 propeller and AA-5 elevator system Issued 8/28/1980
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA10NW Installation of VA-3 fiberglass wheel fairings. Reissued 12/30/1992
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA11NW Installation of VA-2 wheel fairings. Reissued 12/30/1992
SA1208NW Installation of a Lycoming engine with Sensenich propeller Issued 4/3/1981
SA1209NW Relocation of battery from forward face of firewall to aft baggage compartment bulkhead. Amended 4/29/1991
SA1313CE Chrome-plated brake disc installation. Amended 6/20/1977
SA1410SW Mitchell automatic flight system AK301 consisting of Century I autopilot with optional omni tracker. Reissued 7/10/1984
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1735GL Installation of Master Nag warning system. Amended 3/21/1994
SA1745SO Installation of Appalachian Access. stainless steel brake rotors P/N 75-20. Reissued 2/6/1995
SA191NE Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. Reissued 10/4/1984
SA2096NM Installatino of a Lycoming O320-D2H Issued 5/26/1983
SA2104WE Installation of Brittain Models B2C and BSS flight control systems. Reissued 10/20/1972
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA2129NM Installation of a Lycoming O-320-E2G engine AA-5A engine mount cowling air induction and a McCauley 1C172/ SBTM/7359 propeller. Reissued 4/8/1991
SA2138NM Installation of a belly mounted Norton Radome a radar unit mounting hole in the belly pressure vessel a drop chute access hole in the pressure vessel near the rear door rerouted primary control cables with associated support brackets and an electronic rack in the aircraft cabin.  Issued 7/22/1988
SA2169NM Installation of a Sensenich 72 CK series propeller Gulfstream American spinner (P/N 506006-50) engine oil cooler on a Lycoming O-235-C2C engine. Reissued 4/29/1991
SA2190NM Page 2 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2267SO Installation of an instrument panel overlay and glove box door. Issued 3/7/1988
SA2274SO Installation of a glare shield assembly. Issued 3/7/1988
SA2477SW Installation of Lycoming O-320 or O-290 engine. Reissued 3/20/1989
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
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
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
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
SA3234WE Installation of Piper oil cooler and associated installation components. Issued 7/8/1976
SA330NE Replace original brake discs w/William C. Roberts stainless steel discs P/N 201-120-SS. (M20M s/n 27-0001 thru 27-0116) Reissued 6/18/2002
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA3565SW Modification of torque tube assembly. Amended 12/15/1989
SA3695WE Installation of Lycoming O-235-C2C engine and McCauley1A105/SCM7154 propeller. No installation data required. Placards required with this installation: At the fuel filler caps - 80/87 MIN OCTANE AVGAS (AA-1C UTILITY CATEGORY) Issued 7/7/1978
SA4005NM (PG 1) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4005NM (PG 5) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4106SW Increase gross weight to 1560 lbs. for AA-1 1560 lbs. for AA-1A and1600 lbs. for AA-1B. Reissued 3/20/1989
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA4387NM Installation of Lycoming 0-320-A C or E series engine and a Sensenich 74DM6-0-58/64 or 74DM7-0-58/64 propeller. Amended 6/13/1991
SA4708NM Installation of bolts to strengthen the nose gear torque tube assembly. Issued 2/28/1989
SA4722NM Installation of a hat shelf in the aft baggage compartment. Issued 4/17/1989
SA4740NM Installation of a landing light in the left wing tip or in both wing tips. Reissued 4/9/2012
SA4849SW Install fuel flow transducer in fuel line and install fuel flowmeter/totalizer in aircraft Amended 10/26/1984
SA4917NM Modification of upper engine cowl. Issued 4/16/1990
SA4994NM Installation of split nose bowl. Issued 12/5/1990
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
SA5197NM Installation of split cowl nose bowl. Issued 11/4/1991
SA5656NM Installation of burglar alarm system. Reissued 7/21/1993
SA5656NM (PAGE 1) Installation of burglar alarm system. Reissued 7/21/1993
SA5775NM Replacement of rudder tip with Aviation Red Lexan tip with flashing anticollision light located inside. Issued 10/2/1992
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
SA5934NM Installation of cockpit sunvisor. Reissued 3/24/2003
SA593CH (1 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009
SA5987SW Installation of main landing gear fairing clean-up kit. Issued 7/30/1985
SA615EA (PAGE 1) 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
SA66NW Installation of Van s Aircraft model BA-4 fiberglass wheel fairings. Amended 9/23/1994
SA69NW Installation of Matney s engine charge air-air filter assembly. (AA-1B AA-1 AA-1A 1969 AND ON) (AA-5 1972 1973 AND 1974 ONLY) Amended 10/8/1974
SA71GL Installation of air filters Reissued 6/20/2000
SA761NE Modifications to lower engine cowling with landing gear boot adapter and change to upper engine cowling with a split nose bowl configuration. Issued 6/18/1990
SA762NE ONE ONLY- Installation of pilot and copilot control column stick type grip. S/N AA1C0071 Amended 7/18/1990
SA7952SW Installation of conventional landing gear. Reissued 1/14/1993
SA7974SW Installation of wheel pant fairings. Amended 1/10/2006
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
SA809NW Installation of fixed (flush) cowl flap nose gear strut fairing and retainer. Issued 7/20/1979
SA810NW Installation of main landing gear fairings from the AA-5 series aircraft incorporating sheet metal covers over rubber in place of stock rubber parts. Amended 1/23/1981
SA8431SW Installation of R15VON alternator control unit. Amended 1/6/1994
SA868GL Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index. Surrendered 3/5/2004
SA991NW Installation of model AA-5A engine mount cowling and carburetor air box Issued 7/17/1980
ST00811CH Installation of Mitchell Aircraft Products gauge cluster. Issued 1/30/1998
ST02547AT (2 OF 2) Installation of a voice alert system. Amended 5/13/2003
ST10405SC  Installation of a composite propeller spinner Part Number TCB506006-502 in accordance with Drawing Number 2501 Spinner Composite- AA-1 AA-1A AA-1B & AA-1C Issued 4/27/2005
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)