PA-18 150

Number of Active Aircraft: 2186 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 2
Empty Weight: 983 lbs
Max Weight 1750 lbs
Useful Load: 767 lbs
Engine Name Lycoming O-320
Engine Number 1
Horsepower 150 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 19000 ft
Max Fuel 36 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 100 kts
GPH (75% BHP): 7
MPG (75% BHP) 14.3
Range (75% BHP): 436 nm
Fuel Cost Per Seat Mile 0.21 $
Fuel Cost Per Hour 42 $
MPG per 1000 lbs of Payload 10.96
F-T (Speed^2/FuelBurn) 14.3 HP
F-T Payload 11 kts
MPH To HP: 6.7 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 500 ft

SA00008NY Installation of Airwolf Model AFC-500 full flow engine oil filter P/N AFC-500. Amended 5/11/1994
SA00019SE Installation of an Easy Rider Model Cub Scout kayak on models equipped with Edo Model 89A-2000 floats. Issued 10/22/1993
SA00035NY Installation of Lycoming O-360-A3A A4A A4M A4P C2A or C4P engine and Sensenich 76EM8-0 (pitch settings 52 -57 incl.) or McCauley1A200/FA8242 propeller Amended 7/15/2013
SA00055DE Installation of replacement cabin door. Reissued 6/21/1999
SA00068SE (PAGE 1) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010
SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00083DE Installation of an additional cross tube to the upper cabin structure. Reissued 6/21/1999
SA00116DE Installation of Replacement Vertical Stabilizer. Reissued 6/21/1999
SA00142DE Installation of a replacement horizontal stabilizer. Reissued 6/21/1999
SA00150DE Installation of Replacement Elevator Frame. Reissued 6/21/1999
SA00151DE Installation of replacement Rudder Frame. Reissued 6/21/1999
SA00194BO Installation of P/N 2042 Landing Gear Warning System for amphibian aircraft. Reissued 1/23/2009
SA00207AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-67. Reissued 11/14/1994
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
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
SA00248DE Installation of attach fittings for shoulder harness restraint system front and rear seat. Amended 11/25/1996
SA00261AT Installation of basic type BYE-14 Model No. 1008 air driven alternator. (PA-18 Series except PA-18-150 and PA-18A-150) Issued 6/22/1993
SA00275SE Fabrication and installation of vortex generators mounted on the wings and a tail strake mounted on either side of the empennage. Reissued 1/26/2012
SA00281NY Installation of Goodyear Tundra 26 x 10.5 x 6 (6 ply) or 8:50 x 6 Tires and Tubes in accordance with Cub Crafters Inc. Master Drawing List MDL104200 Revision C dated January 21 2002 or later Federal Aviation Administration (FAA) approved revision. );INSERT INTO stc_table VALUES (  Reissued 1/26/2012
SA00388NY Install extended baggage compartment and baggage net in accordance with Cub Crafters Inc. Master Drawing List MDL105400 Revision D dated November 2 1999 or later Federal Aviation Administration (FAA) approved revision and its listed data. Reissued 3/20/2012
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
SA00411SE Installation of Cub Crafters extended landing gear kit. Reissued 1/26/2012
SA00414SE Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft. Reissued 1/26/2012
SA00415SE Installation of Cub Crafters fuel system kit. Reissued 1/26/2012
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
SA00494SE Replace existing fuselage stringers with Cub Crafters Inc. Model 105700 stringers in accordance with Cub Crafters Inc. Master Drawing List MDL 105700 Revision B dated January 8 1998 and its listed date or later Federal Aviation Administration approved revision. Reissued 1/26/2012
SA00495SE Replace existing floor boards with Cub Crafters Inc. Model 102600 floor boards in accordance with Cub Crafters Inc. Master Drawing List MDL 102600 Revision E dated December 15 1997 and its listed data or later Federal Aviation Administration approved revision. Reissued 1/26/2012
SA00522SE : Installation of certain Lycoming O-320 series engines McCauley or Sensenich propeller and associated hardware per Cub Crafters Master Drawing List MDL103000 Revision B dated April 17 1998 or later Federal Aviation Administration (FAA) approved revision. Reissued 1/26/2012
SA00530SE Installation of vortex generators on leading edge of upper side of wing. Amended 5/29/2009
SA00543SE Replace existing engine cowling channels and stiffeners with Cub Crafters Inc. Model 105350 channels in accordance with Cub Crafters Inc. Master Drawing List MDL 105350 Revision E dated July 10 1998 and its listed data or later Federal Aviation Administration approved revisions. Reissued 1/26/2012
SA00561SE Install Sensenich 80 inch diameter wood propeller model W80DM in accordance with Cub Crafters Inc. Master Drawing List MDL 103110 Revision new dated May 26 1998 and its listed data or later Federal Aviation Administration (FAA) approved revision. Reissued 1/26/2012
SA00562SE Install McCauley 82 inch diameter metal propeller model 1A175/GM8241 GM8242 GM8243 or GM8244 in accordance with Cub Crafters Inc. Master Drawing List MDL 103120 Revision new dated May 26 1998 and its listed data or later Federal Aviation Administration (FAA) approved revision. Reissued 1/26/2012
SA00572SE Installation of modified instrument panel in accordance with Cub Crafters Inc. Master Drawing List MDL 102700 Revision E dated August 24 1998 or later Federal Aviation Administration (FAA) approved revision. );INSERT INTO stc_table VALUES ( );INSERT INTO stc_table VALUES ( NOTE: This installation includes provisions for mounting radios and instruments in a new instrument panel. Any additions or changes to the original equipment radios or instruments will require separate FAA approval. The maximum weight of the equipment installed in the panel should not exceed that specified by Cub Crafters Installation Instructions 102700-11 Revision C dated August 24 1998 or later FAA-approved revision. Reissued 1/12/2012
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00680SE (5 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00703SE Install right side access door in accordance with Cub Crafters Inc. Master Drawing List MDL 105900 Revision B dated May 25 1999 and its listed data or later Federal Aviation Administration approved revision. Reissued 1/26/2012
SA00713CH Install Wipaire Model 2100 Amphibian/Seaplane floats. Amended 10/23/1998
SA00718SE Installation of oil cooler hoses and baffles in accordance with Cub Crafters Inc. Master Drawing List MDL 103300 Revision A dated July 2 1999 and its listed data or later Federal Aviation Administration approved revision. Reissued 1/26/2012
SA00750SE Install boot cowling and firewall assembly in accordance with Cub Crafters Inc. Master Drawing List MDL105300 Revision A dated October 26 1999 and its listed data. Reissued 1/26/2012
SA00753SE Install engine baffles in accordance with Cub Crafters Inc. Master Drawing List MDL103800 Revision B dated August 30 1999 and its listed data or later Federal Aviation Administration approved revision. Reissued 1/26/2012
SA00780SE (PAGE 1) 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
SA00856SE Install refueling steps in accordance with Cub Crafters Inc. Master Drawing List MDL103440 Revision - dated November 30 1999 or later Federal Aviation Administration (FAA) );INSERT INTO stc_table VALUES ( approved revision. Reissued 1/26/2012
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00932SE Installation of the Stewart wing tip assembly in accordance with Stewart Wing Tip Assembly Master Drawing List SWT 3001 dated April 8 2001 or later FAA approved revision. Amended 1/25/2002
SA00951SE Install headliner in accordance with Cub Crafters Inc. Master Drawing List MDL 105600 Rev. A dated July 30 2001 or later FAA approved revision. Reissued 1/26/2012
SA00954WI Installation of Concorde RG Series Battiers in Piper Single Engine Airplanes. Issued 4/2/2001
SA00997CH Installation of Gross Weight Increase Kit No. 10B1-6521 in accordance with Wipaire Inc. Installation Drawing No. 10B1-6521 no revision dated December 17 1998 or later FAA approved revisions. Amended 3/1/2011
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
SA01057SE Install IFR Panel instruments primary/alternate static system and heated pitot tube in accordance with the Equipment List below. This installation applies to one aircraft only Serial Number 9930CC current registration N117RB. The Sandel Avionics SN3308 Navigation Display shall be maintained in accordance with Sandel Document No. 90106-IM Revision G(2) dated April 3 2001 Section 6 Instructions for Continued Airworthiness or later Federal Aviation Administration accepted revision. (Bulb );INSERT INTO stc_table VALUES ( replacement interval of 225 hours or 1 year whichever comes first). Title 14 Code of Federal Regulations part 43 is considered adequate for the remainder of the installation. Reissued 1/26/2012
SA01063CH Installation of a Scott Model 3200 Tail Wheel with the AESI #T.S.05P Tail Spring. Reissued 2/16/2006
SA01100AT Installation of Composite Spinner. Amended 3/31/2004
SA01101AT Installation of Madras Air Service (MAS) wing tips. Issued 8/2/1996
SA01126SE Install windows in accordance with Cub Crafters Master Drawing List CR102500-3 dated July 24 2002 or later Federal Aviation Administration approved revisions. Since there are no special instructions for continued airworthiness required Title 14 Code of Federal Regulation part 43 is considered adequate for the maintenance of the installation. Reissued 1/26/2012
SA01147WI Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Reissued 7/30/2012
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01158SE Install heavy duty tail wheel assembly in accordance with Cub Crafters Inc. Master Document List Report CR123300-3 Revision D dated July 15 2003 or later Federal Aviation Administration approved revision. This modification does not require specific continued airworthiness instructions. Federal Aviation Regulation 43 is adequate to insure Continued Airworthiness of this modification. Reissued 1/26/2012
SA01224AT Installation of wheel hub cabs with valve stem access door. Amended 4/17/1998
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
SA01240SE (4 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
SA01242SE Fabrication of PA-18 Inspection Covers in accordance with Cub Crafters Inc. Master Drawing List Report CR124500-3 dated July 14 2003 or later Federal Aviation Administration (FAA) approved revision. The inspection covers must be installed in accordance with Cub Crafters Inc. Installation Instructions Report CR124500-2 dated June 23 2003 or later FAA-approved revision. Reissued 1/26/2012
SA01247SE Install heated pitot tube and new static system Reissued 1/26/2012
SA01251SE The manufacture of a Sunvisor System. Amended 2/28/2012
SA01258SE Installation of the Automatic Flagman Dispenser Models in accordance with Automatic Flagman Master Drawing Lists specified in attached AML or later FAA approved revision.This STC supercedes several existing STC Issued 9/5/2003
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
SA01343WI Installation of B&C Specialty Products BC400 alternator Issued 7/28/2005
SA01350SE Install replacement wing assembly in accordance with Cub Crafters Inc. Master Drawing List 123400MDL Revision C dated December 8 2003 and Installation Instructions Document CR123410II Revision NC dated September 23 2003 or later Federal Aviation Administration approved revision. Reissued 1/26/2012
SA01377SE Install B and C alternator model 400-2 (with thermocouples and regulator B0201-1) Electronics International (EI) MUX-8A data recorder EI ASC-5A super clock EI FM-VA Volt Amp functional module and supplemental instrument panel in a PA-18 150 Reissued 1/26/2012
SA01378SE Install replacement fuselage tube or tube reinforcement Reissued 1/26/2012
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
SA01473SE (4 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
SA01487SE-D (Page 2) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01516SE Replacement of the Scott Master Brake Cylinder (Non-Vented Diamphram type) with a Steve Amended 7/16/2007
SA01606CH Installation of alternate electro-hydraulic power pack system for operation of main wheel skis. Amended 4/16/2010
SA01633SE Gross weight increase modification manufactured in accordance with );INSERT INTO stc_table VALUES ( Report 130000MDL Revision NC and installed in accordance with Report 130000II Revision NC or later Federal Aviation Administration (FAA) approved revisions. );INSERT INTO stc_table VALUES ( );INSERT INTO stc_table VALUES ( Mandatory Installations: To be eligible for this modification all of the following six required Supplemental Type Certificates must be installed: SA92NW (180 hp Engine Installation) SA00275SE (Vortex Generators) SA00411SE (Extended Landing Gear) SA01158SE (Heavy Duty Tailwheel Assembly) SA01350SE );INSERT INTO stc_table VALUES ( (Replacement Wing Assembly) SA4095NM (Replacement Fuselage Frame). Reissued 1/26/2012
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
SA01695SE (4 OF 5) Installation of an antenna Amended 2/15/2007
SA01704LA Installation of the Grove Disk Brake System Issued 12/21/2004
SA01714WI (Page 1) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
SA01734SE (PG 3) Application of Stewart Systems synthetic fabric covering system to aircraft fuselage wings tail surfaces control surfaces and related parts. Amended 3/23/2011
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
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 1)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
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-D Page 1 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
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
SA01933LA (3 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01944CH (2 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 0:00
SA01986SE Cub Crafters extended range fuel tanks Issued 3/27/2009
SA01988SE (PAGE 1) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009
SA01988SE (PAGE 5) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02000SE Installation of Aerocet Model 2200 Twin Seaplane Floats Issued 5/8/2009
SA02007AK Installation of main landing gear long step no. 3195. Amended 5/23/2006
SA02011AK Fabrication and installation of top deck assembly x-brace. Issued 4/15/1994
SA02015SE-D Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Amended 2/5/2014
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
SA02019SE-D Page 2 Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/19/2012
SA02024AK Fabrication of F. Atlee Dodge part no. 3236 muffler shroud assembly. Issued 9/2/1994
SA02025AK Fabrication of F. Atlee Dodge part no. 3182 preheater shroud assembly. Issued 9/2/1994
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
SA02043AK Fabrication and installation of pilot s seat belt attachment brackets. Issued 12/13/1995
SA02049AK Fabrication and installation of Airglas Engineering Co. Inc. Model LTC18 cargo pod/bell Reissued 10/28/2011
SA02058AK Fabrication of Replacement Stabilizer Assembly (P/N 3219). Issued 8/23/1996
SA02060AK Fabrication of Replacement Elevator Assembly (P/N 3220). Issued 8/23/1996
SA02066AK Fabrication of Aircraft Tiedown Bracket Assembly (P/N 3197). Issued 12/30/1996
SA02068AK Fabrication and installation of Airglas Engineering Company Inc. Model LT32PA-18 belly tank kit and electric auxiliary fuel transfer system. Issued 1/17/1997
SA02085AK Modification to front seat to allow seat back to fold forward. Issued 8/19/1997
SA02087CH Installation of MT-Propeller model MTV-15-C/200-50 or MTV-15-B/210-58 constant speed propeller Issued 3/22/2005
SA02091AK Installation of Airglas LW2500 fixed wheel penetration skis. Issued 9/22/1997
SA02093AK Installation of hourmeter airspeed switch. Issued 10/17/1997
SA02094AK Fabrication and Installation of the F Atlee Dodge Rear Seat Heater. Issued 10/24/1997
SA02110CH (PAGE 2) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02115AK Fabrication and installation of 30.5 gallon wing fuel tank sight gages. Amended 1/20/2004
SA02119SE Page 1 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02119SE Page 2 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02128AK Fabrication and installation of Airframes Inc. Fuselage in accordance with Airframes Inc. Master Data List AF 18 dated November 10 1998 or later FAA accepted revision Reissued 1/16/2008
SA02128LA Installation of aileron and flap hinge repair bushings Amended 6/10/2009
SA02134SE  Control gap seals manufactured in accordance with the latest Federal Aviation Administration (FAA) approved revision of Cub Crafters Drawing RM0601 installed in accordance with the installation instructions listed in AML SA02134SE and maintained in accordance with the maintenance manual supplement listed in AML SA02134SE.  Issued 6/16/2011
SA02138AK Fabrication and installation of a light weight battery and bracket under the rear seat. Issued 5/5/1999
SA02139AK Fabrication and installation of a leading edge slot mod in Piper PA-18 wing. Issued 5/6/1999
SA02152AK Fabrication and installation of F. Atlee Dodge 3-inch extended Main Landing Gear P/N 3284. Issued 12/10/1999
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
SA02154AK (PAGE 2) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005 0:00
SA02170AK Installation of McCauley propellers Models 1A175-GM8241 through 1A175-GM8244. Issued 1/3/2001
SA02171AK Installation of a 24-gallon right wing fuel tank P/N DC18049-24G-25R and 24-gallon left wing fuel tank P/N DC10849-24G-32L. Amended 1/8/2008
SA02172AK Fabrication and installation of Airglas Inc. Model LC18 cargo pod kit  Amended 6/14/2010
SA02175AK Fabrication of Airframes Alaska LLC Heavy Duty Amended 1/7/2013
SA02183AK Fabrication of replacement engine exhaust system assembly (P/N PA18ESA). Amended 4/24/2003
SA02187AK Fabrication and installation of the Airframes Inc. 4-inch wider frame assembly/fuselage P/N AF18-4 in accordance with Airframes Inc. Master Data List AF18-4 Revision A dated April 8 2003 or later FAA approved revisions. Reissued 1/16/2008
SA02189AK Fabrication and installation of p/n 3344 main landing gear safety cable kit for 3-inch extended main landing gear. Applies only to planes modified by installation of 3-inch extended main landing gear per STCs SA02152AK or SA02175AK. Issued 1/11/2002
SA02191AK Fabrication and installation of Dakota Cub extended wings and associated flaps and ailerons. Issued 2/1/2002
SA02200AK Fabrication of replacement engine exhaust system assembly (P/N PA18ESA). Amended 8/19/2010
SA02203AK (PAGE 1) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
SA02204AK Fabrication of replacement engine exhaust system assembly. Limited to airplanes equipped with FAA approved installations of Textron Lycoming O-320 model series engines having a compression ratio of 8.5:1 and a rated power of 160 hp for all operations. Issued 4/29/2003
SA02211AK Installation of components to change thrust line orientation Issued 4/27/2004
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
SA02214AK Installation of Alpha Omega Suspension System in place of original bungees or bungees and hydasorbs. Amended 11/15/2005
SA02216AK Installation of cargo belly pod. Reissued 3/24/2008
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
SA02217AK (4 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
SA02233AK Installation of high visibility fuel sight gauge. Reissued 10/28/2010
SA02234AK Installation of a high Pressure Brake Master Cylinder assembly DCA1248-1260. Issued 1/13/2005
SA02236AK Fabrication and installation of F. Atlee Dodge Heavy Duty Standard Length Main Landing Gear P/N 3225A in accordance with F. Atlee Dodge Master Data List No. 3225-1.5 Revision: None dated March 14 2005 or later FAA approved revisions. );INSERT INTO stc_table VALUES (  Issued 3/29/2005
SA02246LA Installation of a flap handle extension. Amended 11/16/2010
SA02253AT Remove existing engine cowling engine exhaust system and propeller and install new engine baffling-cooling shroud complete new exhaust system and a McCauley model 1A200/FA8242 propeller. Amended 2/6/2008
SA02259AK Installation of a Micro Systems Inc. VM1000 Engine Monitoring System. Issued 11/17/2005
SA02262AK Manufacture weld-on float fittings in accordance with Airframes Inc. Master Drawing List AF591078 Revision A dated November 24 2005 or later FAA approved revision. Install in accordance with Installation Instructions II591078 Revision O dated February 22 2006 or later FAA approved revision. Maintain in accordance with Instructions for Continued Airworthiness ICA591078 Revision O dated November 28 2005 or later FAA accepted revision Reissued 1/16/2008
SA02268CH (PAGE 5) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02273AK Installation of Performance Air Motive Inc. (PAMI) PA-18 Muffler Amended 8/24/2006
SA02280AK Installation of a Maule Fuel Selector Valve.  Amended 11/29/2006
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02293AK (1 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02294AK Installation of a fuselage cowl (boot cowl) battery box system. Issued 8/3/2007
SA02295AK Installation of a high capacity fule gascolator assembly. Issued 8/21/2007
SA02299AK Installation of a replacement fuel selector valve. Issued 9/13/2007
SA02309AK Installation of a stabilizer trim system Issued 4/17/2008
SA02316AK Installation of 8.50-6 and 8.50-10 tires Issued 9/5/2008
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
SA02373AK Installation of heavy duty landing gear Reissued 6/14/2010
SA02375AK Installation of PA-18 jacking lugs Issued 6/7/2010
SA02378AK Installation of structural provisions for a fuselage side mounted baggage door in accordance with Alaska Aircraft Products LLC drawing number 8029 Revision - dated May 27 2010 or later FAA approved revision. Issued 2/9/2011
SA02384AK Installation of a cabin forward battery box in accordance with Willow Mountain Ranch Drawing No. WMR-FBB-05 Rev. A dated May 13 2011 or later FAA approved revision. Issued 6/28/2011
SA02411AK Installation of floor mounted front seat belt attachments Issued 5/21/2013
SA02421AK Installation and rigging of F.Atlee Dodge Model F.A. DODGE X-1 wheel replacement skis Issued 12/23/2013
SA02423AK Relocation of Circuit Breakers and Switches to the Instrument Panel Reissued 1/10/2014
SA02424AK The fabrication and installation of a header-less fuel system Issued 2/3/2014
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02508CH Installation of reversible MT-Propeller model MTV-15-B-C-R-(M)/CR210-58 or TV-15-C-C-R-(M)/CR200-50 constant speed propeller Issued 12/21/2007
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02532AT Installation of subject Michelin tires on appropriate aircraft. For Michelin 5 6 8 and 10-inch rim diameter tires on General Aviation Aircraft. Issued 6/5/2002
SA02566CH Installation of the Custom Fiberglass Molding Inc. (CFMI) Model 1500 Aircraft Main Landing Gear Skis. Amended 3/6/2009
SA02655AT (2 OF 2) Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft. Amended 9/1/2004 0:00
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 1) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02738CH (PAGE 2) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02751CH Installation of McCauley Propeller model 1A200FA824X Amended 6/25/2012
SA02828CH Installation of the Lycoming IO-390-A1A6 engine MT model MTV-15-B/210-58 constant speed propeller and associated accessories  Reissued 6/14/2010
SA02906CH Installation of the reversible MT-Propeller model MTV-15-B-C-R(M)/CR210-58 two bladed hydraulic constant speed propeller  Issued 11/8/2010
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
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
SA03034CH Installation of new engine baffling assembly and new oil coolers in accordance with Installation Instructions Doc. No. RR-1100 Rev. IR dated January 04 2011 or later FAA approved revision. Issued 11/17/2011
SA03035CH Installation of new lower cowling and new air box assembly in accordance with Installation Instructions Doc. No. RR-900 Rev. IR dated January 04 2011 or later FAA approved revision. Issued 11/17/2011
SA03061CH Installation of Lycoming O-360 engine and either Sensenich 76EM8 or McCauley 1A200FA propeller and associated equipment in accordance with Svenn Issued 12/22/2011
SA03111AT Installation of Gomolzig Quietflight low noise silencer P/N PA-18-606500. Issued 5/26/2005
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA1-155 McCauley fixed pitch MET-L-PROP1A170/GM7448 with Lycoming O-290-D2 engine. Reissued 8/15/2006
SA1-156 McCauley fixed pitch MET-L-PROP1A170/GM7446 with Lycoming O-290-D engine. Reissued 8/15/2006
SA1-32 McCauley fixed pitch MET-L-PROP1A170/GM7450 and 1A170/GM7452 with Lycoming O-290-D2 engine. Reissued 8/15/2006
SA1-33 McCauley fixed pitch MET-L-PROP1A170/GM7450 and 1A170/GM7452 with Lycoming O-290-D2 engine. Reissued 8/15/2006
SA1-349 Installation of Glider tow hook. Amended 11/16/1987
SA1-383 Lube oil filter PB 55-1. Issued 
SA1-41 McCauley fixed pitch MET-L-PROP1A170/GM7450 1A170/GM7452 and1A170/GM7454 propellers with Lycoming O-320-A1A engine. Reissued 8/15/2006
SA1-510 Installation of Sur-Vent fuel tank filler cap manufactured. Reissued 5/11/1994
SA1-59 McCauley fixed pitch MET-L-PROP1A170/GM7448 and 1A170/GM7450 with Lycoming O-290-D engine. Reissued 8/15/2006
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
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
SA10236SC (3 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA1033EA Replace steel oil cooler lines with Aeroquip type 303-8 hose using AN-823-8D elbows AN-816-8D nipples and AN-321-8 hose fittings. Issued 1/29/1976
SA105NW Mounting and wiring for occasional installation and use of Barnes Engineering Company airborne fire spotter system. Issued 4/30/1974
SA1064GL Surrendered and incorporated into STC SA00478CH. Surrendered 6/14/2002
SA10682SC Installation of alternator and voltage regulator Reissued 11/16/2007
SA1080SW Mitchell automatic flight system AK293 consisting of Century II autopilot with optional radio coupler. Reissued 7/9/1984
SA1081SW Mitchell automatic flight system AK294 consisting of automatic stabilizer and optional omni tracker. Reissued 7/9/1984
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA1086WE Escape chutes relocated. Issued 1/2/1980
SA10921SC Installation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulators Issued 11/10/2008
SA1099WE Install fiberglass reinforced plastic floats. Reissued and Amended 7/31/1998
SA109CE Installation of Pee-Kay Model 1800 floats. Reissued 12/23/1980
SA1105SO Installation of Bendix ALA-51 radio altimeter and GPW-83 ground proximity warning system. Amended 6/19/1986
SA1151NW Installation of North American Industries Inc. Model 135 pistol grip Amended 3/29/2002
SA1162NW Installation of an extended rear baggage compartment a fishing pole compartment and a belly-mounted Grimes Model 437 light Issued 2/2/1981
SA1177WE WECO carburetor temperature monitor. Issued 1/1/1960
SA117AL Installation of Cunningham auxiliary fuel belly tank. Amended 6/30/1997
SA1181NW Installation of Antique Tire and Rubber Company Tundra Tire and Cleveland wheels and brakes Issued 2/13/1981
SA1187NW Installation of metal leading edge extension and a metal skin replacement on the aft fuselage Issued 3/5/1981
SA1187WE Either a Collins Radio Company or a United Data Control Inc. cockpit voice recorder system. Surrendered 4/14/2008
SA1191SO Installation of Aqua Model1500 floats. Reissued 4/30/1990
SA11RM Installation of modified axles wheels and brakes Amended 7/13/1999
SA1203SO Installation of Fiberfloat Model2400( ) floats. Issued 2/12/1981
SA1236WE Modification of elevators. Surrendered 4/14/2008
SA123NW Installation of a modified landing gear axle to accommodate Goodyear 29x13x5 airwheel and tire assembly with Cleveland brakes Issued 8/2/1974
SA1243CE Installation of Cleveland wheels and brakes and optional wheel fenders per Flanagan Aircraft Co. Drawing List No.5 stamped FAA Approved with a date of July 7 1976 for PA-18 Serial Number 18-8118 May 17 1977 for all other PA-18 airplanes and September 29 1977 for installation of optional 24 x 10 x 6 Muskeg King tires. Reissued 1/26/2012
SA1244CE Replacement landing gear components per Flanagan Aircraft Co. Drawing No. 1-9.01 stamped FAA Approved with a date of July 7 1976 or later Federal Aviation Administration (FAA) approved revision. Reissued 1/26/2012
SA1245CE Replace existing Scott Reissued 1/26/2012
SA126SO Installation of wing fabric attachment clips. Reissued 6/3/1991
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
SA1329WE Collins 621A-3 air traffic control transponder system. Surrendered 4/14/2008
SA1330WE Class E cargo compartment reduced to accommodate crew rest area. Surrendered 4/14/2008
SA1333CE Installation of replacement engine mount fabricated per Flanagan Aircraft Co. Drawing List 1-14.00 stamped FAA Approved with a date of June 3 1977 or later Federal Aviation Administration approved revision. Reissued 1/26/2012
SA1337GL Install Aero Ski Manufacturing Co. Inc. Model R2800 Retractable Skis. Issued 11/15/1988
SA1350WE Replace existing fabric on wings fuselage empennage and/or control surfaces with fiberglass cloth. Reissued 3/6/1969
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
SA1366CE Installation of a third seat removable cross member and reinforced baggage compartment floor per Cub Crafters Master Document List 123600-1 Revision N/C dated December 4 2002 or later Federal Aviation Administration approved revision. Reissued 1/26/2012
SA1368CE Cabin metalization installation of new boot cowl firewall swing up side windows larger baggage door and inspection access in aft fuselage per Flanagan Aircraft Drawing List No. 1-10.00 (less Drawing 1-11.02) stamped FAA Approved on September 12 1977 or later. Reissued 1/26/2012
SA1369CE Electrical System and Instrument Panel modification. DATA REQUIRED: Flanagan Aircraft Co. Drawing List 1-12.00 Revision 2 dated August 15 1977 or later Federal Aviation Administration approved revisions. Reissued 1/26/2012
SA136AL Installation of Lycoming O-320 engine. Amended 5/14/1968
SA1370CE Revised fuel gaging and dual fuel feed line installation from both tanks. Two wing fuel tanks standard. Reissued 1/26/2012
SA1398WE Removal of right-hand door to permit aircraft to engage in special operations such as aerial photography parachute jumping etc. Issued 1/1/1960
SA1401WE Structural modification of lower rudder. Surrendered 4/14/2008
SA1415WE ONE ONLY STC SN 18-832: Installation of Lycoming 0-320-A2B Engine and McCauley 1A17OGM7448 Propeller. Issued 5/15/1967
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA141AL Removal of agricultural hatch. Issued 1/1/1960
SA1425GL Surrendered and incorporated into STC SA241CH. Surrendered 6/14/2002
SA143AL Enlarged instrument panel. Issued 1/1/1960
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA150AL Installation of cockpit operated cowl flap winterization kit. Amended 7/29/1969
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1522NM Installation of stamped aluminum wing ribs. Issued 10/25/1982
SA1526NM Installation of Piper landing gear vee assemblies P/Ns 10033-5 10033-6 with P/Ns J-10033-( ). Reissued 1/29/1999
SA1544NM Installation of cabane vee. Reissued 1/29/1999
SA1548NM Installation of hydra strut. Reissued 1/29/1999
SA1554NM Installation of Jensen Aircraft fuel valve plug No. 011-2. Reissued 1/29/1999
SA1555NM Installation of Jensen Aircraft fuel valve No. 011-1. Reissued 1/29/1999
SA1568NM Installation of Cleveland wheels and brakes. Reissued 1/29/1999
SA1576NM Installation of muffler. Reissued 1/29/1999
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1580GL Install shoulder harness and seat belt assembly. Reissued 7/9/1998
SA1585NM Installation of replacement long-life lift strut. Reissued 1/29/1999
SA1586CE Modified brake master cylinder. Issued 5/9/1980
SA1588CE Modified airplane widening fuselage and increasing gross weight. Reissued 5/28/2008
SA159CE Installation of Pee-Kay Model 1800 floats. Reissued 12/23/1980
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1627NM Installation of Antiqua Tire and Rubber Company (30 x 13 x 6) Tundra Tires (tubeless) and Cleveland model 40-75D wheels and model 30-52D brakes Issued 4/28/1982
SA1635GL Installation of Cleveland main wheels 40-86A and brakes 30-56F. Issued 8/14/1991
SA1639WE Replacement of any of three original 40 KVA alternators with Westinghouse 40 KVA system consisting of alternator P/N 976J843-1 and regulator P/N 915F363-1. Surrendered 4/14/2008
SA1646CE Replacement of bushing type pulley pulley in aileron control system. Issued 4/24/1981
SA165WE 178 maximum passenger interior. Surrendered 4/14/2008
SA1678NM Installation of replacement wing ribs. Issued 11/18/1982
SA1761WE Replacement of any of three original 60 KVA alternators and voltage regulators with Westinghouse 60 KVA system. Surrendered 4/14/2008
SA17RM Replacement for Piper P/N 10033 Landing Gear Vee Amended 6/5/1997
SA1900NM Installation of Schneider wheel skis 6-inch to 10-inch aluminum wheel adapters and 8.50-10 6-ply tires on main landing gear. Issued 11/12/1982
SA1904NM Installation of Schneider wheel skis 6-inch to 10-inch aluminum wheel adapters and 29x11.0-10 8 ply minimum tires on main landing gear. Issued 12/12/1982
SA1961CE Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index (RON + MON)/2. Intermixing with aviation gasoline also approved. Amended 6/23/1992
SA196EA Astek Mach airspeed warning switch. Surrendered 4/14/2008
SA1989SO Installation of Canadair Marconi CMA-771 MK II Dual Omega Navigation System. Issued 9/8/1986
SA2-952 Installation of fiberglass covering. Reissued 9/10/1996
SA2040AK Installation of vented fuel cap assembly (P/N 3267). Issued 9/7/1995
SA2040WE Installation of Brittain Industries B2C or ACS-1 flight control system. Reissued 10/20/1972
SA2103CE Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index (RON+MON)/2. Intermixing with aviation gasoline also approved. Amended 6/23/1992
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)