| 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 |
