# N151AW: Piper PA-18-150

- Status: Valid registration
- Airframe: [Piper PA-18-150](https://openairdocs.org/model/piper-pa-18-150) (registry code 7101828, 2 seats)
- Data sheets: [TCDS 1A2](https://openairdocs.org/tcds/1A2) (Piper Aircraft Inc.) (OpenAirDocs)
- Serial number: 18-7709032
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Certificate issued: May 20, 2025
- Expires: May 31, 2032
- Mode S code: A0CDFB
- Registered owner: [Maples Charles K](https://openairdocs.org/faa-owner/MAPLES%20CHARLES%20K)
- Location: [Bonsall, CA](https://openairdocs.org/faa-place/CA/Bonsall)
- Owner type: Individual
- Owner's area on the map: 33.2853° N, 117.1978° W: Placed by OpenAirDocs at the center of ZIP code 92003, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=151AW
- Page: https://openairdocs.org/aircraft/N151AW

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 17 in force

### Matched by airframe (Piper PA-18-150)

- [AD 2025-02-11](https://openairdocs.org/ad/2025-02-11): Rudder Structure · FS 2001 J5A (Army L-4F), J5A-80, J5B (Army L-4G) and 67 more. Effective Mar 20, 2025
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2015-08-04](https://openairdocs.org/ad/2015-08-04): Wings · FS 2000 L-14, AE-1, HE-1 and 77 more. Effective Jun 3, 2015
- [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006
- [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001
- [AD 96-09-06](https://openairdocs.org/ad/96-09-06): Air Filter Assemblies · Maule Aerospace Technology 7ACA, 7ECA, 7FC and 180 more. Effective Jun 7, 1996
- [AD 85-06-04](https://openairdocs.org/ad/85-06-04): Fuel Tank · FS 2001 AE-1, HE-1, J5A-80 and 60 more. Effective May 4, 1985
- [AD 81-06-08](https://openairdocs.org/ad/81-06-08): Lower Fuselage Attachment Tab · Piper PA-18-150. Effective Nov 19, 1981
- [AD 78-10-03](https://openairdocs.org/ad/78-10-03): Fuel Venting · FS 2001 AE-1, HE-1, J5A-80 and 66 more. Effective May 23, 1978
- [AD 69-23-03](https://openairdocs.org/ad/69-23-03): Lower Longeron Inspection · Piper PA-18-150. Effective Nov 15, 1969
- [AD 68-05-01](https://openairdocs.org/ad/68-05-01): Exhaust Mufflers · FS 2001 J5A-80, J5A (Army L-4F), J5B (Army L-4G) and 67 more. Effective Mar 31, 1968
- [AD 62-02-05](https://openairdocs.org/ad/62-02-05): Rudder Cable Attachment Lug · Piper PA-18, PA-18-105 (Special), PA-18-125 (Army L-21A) and 5 more
- [AD 61-16-05](https://openairdocs.org/ad/61-16-05): Control Cable Replacement · Piper PA-18-150, PA-18A-135, PA-18A-150 and 6 more. Effective Jul 26, 1961
- [AD 60-10-08](https://openairdocs.org/ad/60-10-08): Fuel Selector Valve · Piper PA-18, PA-18-105 (Special), PA-18-125 (Army L-21A) and 30 more. Effective Jul 15, 1960
- [AD 53-04-01](https://openairdocs.org/ad/53-04-01): Control Stick Attachment · Piper PA-18, PA-18-105 (Special), PA-18-125 (Army L-21A) and 16 more

### Historical (superseded or no longer in force)

- [AD 99-01-05 R1](https://openairdocs.org/ad/99-01-05-R1) (historical): Wings · FS 2000 L-14, AE-1, HE-1 and 73 more. Effective Jan 14, 2014
- [AD 99-01-05](https://openairdocs.org/ad/99-01-05) (historical): Wing Lift Struts or Forks · FS 2000 L-14, AE-1, HE-1 and 73 more. Effective Feb 8, 1999

## Information bulletins (advisory) (2 in force)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB ACE-96-04](https://openairdocs.org/saib/ACE-96-04): . Issued Aug 7, 1996
- [SAIB CE-03-02](https://openairdocs.org/saib/CE-03-02) (historical): . Issued Oct 8, 2002

## NTSB investigations

None matched to N151AW.

## FAA accident and incident reports

None matched to N151AW.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N151AW not matched to an aircraft (114, newest 50)

They name N151AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 151AW0041](https://openairdocs.org/sdr/151AW0041), Sep 23, 2004: BULB. INOPERATIVE. LEFT OVERWING FWD EMERGENCY LIGHT BULB IS OUT. REPLACED BULB, CHECKS GOOD.
- [SDR 151AW0025](https://openairdocs.org/sdr/151AW0025), Jul 9, 2004: COUPLER. MALFUNCTIONED. YAW DAMPER DISENGAGES INTERMITTENTLY. REPLACED YAW DAMPER COUPLER PER MM 27-12-31. SYSTEM TEST NORMAL.
- [SDR 151AW0040](https://openairdocs.org/sdr/151AW0040), Jul 2, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT BS 727B AT STR 16 RT. REPLACED TIE CLIP IAW SRM 51-10-02.
- [SDR 151AW0038](https://openairdocs.org/sdr/151AW0038), Jul 2, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT BS 907 AT STR 6 RT. REPLACED TIE CLIP IAW SRM 51-10-02.
- [SDR 151AW0037](https://openairdocs.org/sdr/151AW0037), Jul 2, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT BS 578 AT STR 9 RT. REPLACED TIE CLIP IAW SRM 51-10-02.
- [SDR 151AW0007](https://openairdocs.org/sdr/151AW0007), Jul 2, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT BS 277 AT STR 16 RT. REPLACED TIE CLIP PER SRM 51-10-02.
- [SDR 151AW0036](https://openairdocs.org/sdr/151AW0036), Jul 2, 2004: FRAME. CRACKED. FUSELAGE FRAME CRACKED AT BS 907 AT STR 9 LT. REPAIRED CRACK PER SRM 53-00-07.
- [SDR 151AW0035](https://openairdocs.org/sdr/151AW0035), Jul 2, 2004: FRAME. CRACKED. FUSELAGE FRAME CRACKED AT BS 847 AT STR 9 RT. REPAIRED CRACK IAW SRM 53-00-07.
- [SDR 151AW0034](https://openairdocs.org/sdr/151AW0034), Jul 2, 2004: FRAME. CRACKED. FUSELAGE FRAME CRACKED AT FS 807 AT STR 9 LT. REPAIRED CRACK PER SRM 53-00-07.
- [SDR 151AW0033](https://openairdocs.org/sdr/151AW0033), Jul 2, 2004: FRAME. CRACKED. FUSELAGE FRAME CRACKED AT BS 787 AT STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07.
- [SDR 151AW0032](https://openairdocs.org/sdr/151AW0032), Jul 2, 2004: FRAME. CRACKED. FUSELAGE FRAME CRACKED AT BS 747 AT STR 9 RT. REPAIRED CRACK IAW SRM 53-00-07.
- [SDR 151AW0031](https://openairdocs.org/sdr/151AW0031), Jul 2, 2004: FRAME. CRACKED. FUSELAGE FRAME CRACKED AT BS 727E AT STR 9 LT. REPAIRED CRACK PER SRM 53-00-07.
- [SDR 151AW0030](https://openairdocs.org/sdr/151AW0030), Jul 2, 2004: FRAME. CRACKED. FUSELAGE FRAME CRACKED AT BS 480 AT STR 9 RT. REPAIRED CRACK IAW SRM 53-00-07.
- [SDR 151AW0029](https://openairdocs.org/sdr/151AW0029), Jul 2, 2004: FRAME. CRACKED. FUSELAGE FRAME CRACKED AT BS 480 AT STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07.
- [SDR 151AW0028](https://openairdocs.org/sdr/151AW0028), Jul 2, 2004: FRAME. CRACKED. FUSELAGE FRAME CRACKED AT BS 400 AT STR 9 LT. REPAIRED CRACK PER SRM 53-00-07.
- [SDR 151AW0027](https://openairdocs.org/sdr/151AW0027), Jul 2, 2004: FRAME. CRACKED. FUSELAGE FRAME CRACKED AT BS 400 AT STR 9 RT. REPAIRED CRACK PER SRM 53-00-07.
- [SDR 151AW0006](https://openairdocs.org/sdr/151AW0006), Jul 2, 2004: FRAME. CRACKED. FUSELAGE FRAMES CRACKED AT BS 380 STR 9 RT. CRACK REPAIRED PER SRM 53-00-07.
- [SDR 151AW0004](https://openairdocs.org/sdr/151AW0004), Jul 2, 2004: STRINGER. CRACKED. STRINGER 16 RT AT BS 500C HAS TWO CRACKS. REPAIRED CRACKS IAW SB737-53-1145.
- [SDR 151AW0026](https://openairdocs.org/sdr/151AW0026), Jul 2, 2004: STRINGER. CRACKED. STRINGER 16 LT AT BS 500C HAS THREE CRACKS. REPAIRED CRACKS PER SB737-53-1145.
- [SDR 151AW0019A](https://openairdocs.org/sdr/151AW0019A), Jul 2, 2004: SKIN. CRACKED. FUSELAGE SKIN CRACKING AT SEVERAL LOCATIONS UNDER EXISTING REPAIR INSTALLED WITH BLIND FASTENERS FROM BS727E TO BS767 STR18 RT TO STR20 RT. REPAIRED PER EA 53-1
- [SDR 151AW0011](https://openairdocs.org/sdr/151AW0011), Jul 2, 2004: STRINGER. CRACKED. CRACK IN STR 7 LT AT BS 344. REPLACED STRINGER SECTION PER SRM 51-10-03.
- [SDR 151AW0018](https://openairdocs.org/sdr/151AW0018), Jul 2, 2004: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AT BS 360 LT STR 13. FABRICATED INTERCOSTAL AND INSTALLED PER EA 53-145.
- [SDR 151AW0008](https://openairdocs.org/sdr/151AW0008), Jul 2, 2004: FRAME. CRACKED. BS 639 LT FRAME I/B CHORD, WEB, AND O/B CHORD CRACKED. REPLACED I/B AND O/B CHORDS PER SRM 51-40-02 AND REPAIRED WEB PER SRM 51-70-13.
- [SDR 151AW0003](https://openairdocs.org/sdr/151AW0003), Jul 2, 2004: SPLICE. CRACKED. STRINGER SPLICE CRACKED AT STRINGER 4 RT AT BS 907 AND AT STRINGER 4 LT AT BS 907. REPLACED STRINGER SPLICE AT 4 RT AND 4 LT PER SRM 51-40-02.
- [SDR 151AW0022](https://openairdocs.org/sdr/151AW0022), Jul 2, 2004: SKIN. CRACKED. NR 2 SLAT HAS CRACKS AT TWO FASTENERS ON LOWER SURFACE NEAR O/B AUX TRACK. REPAIRED PER SRM 57-43-01.
- [SDR 151AW0020](https://openairdocs.org/sdr/151AW0020), Jul 2, 2004: SKIN. DAMAGED. INCORRECT REPAIR AT BS 360 STR 24 RT AT INTERSECTION OF SKIN LAP AND BUTT JOINT. REPLACED EXISTING REPAIR PER EA 53-148A.
- [SDR 151AW0024](https://openairdocs.org/sdr/151AW0024), Jul 2, 2004: ANGLE. CRACKED. CRACK IN ANGLE ON AFT SIDE OF AFT DOOR FRAME OF L1 DOOR AT THE NR 2 STOP FITTING. REPLACED ANGLE.
- [SDR 151AW0023](https://openairdocs.org/sdr/151AW0023), Jul 2, 2004: BOLT. LOOSE. FOUND 7 RUDDER FLANGE BOLTS LOOSE. TORQUED AND REPLACED BOLTS AS REQUIRED PER SB 737-55A1087.
- [SDR 151AW00220](https://openairdocs.org/sdr/151AW00220), Jul 2, 2004: STRUCTURE. CRACKED. NR 2 SLAT HAS CRACKS AT TWO FASTENERS ON LOWER SURFACE NEAR O/B AUX TRACK. REPAIRED PER SRM 57-43-01.
- [SDR 151AW0021](https://openairdocs.org/sdr/151AW0021), Jul 2, 2004: SKIN. CRACKED. RIGHT PYLON UPPER SKIN AT NAC STA 213 LBL 10 CRACKED AT PANEL CUTOUT. REPAIRED PER SB 737-54-1035.
- [SDR 151AW00200](https://openairdocs.org/sdr/151AW00200), Jul 2, 2004: SKIN. MISREPAIRED. INCORRECT REPAIR AT BS 360 STR 24 RT AT INTERSECTION OF SKIN LAP AND BUTT JOINT. REPLACED EXISTING REPAIR PER EA 53-148A.
- [SDR 151AW0019](https://openairdocs.org/sdr/151AW0019), Jul 2, 2004: SKIN. CRACKED. FUSELAGE SKIN CRACKING AT SEVERAL LOCATIONS UNDER EXISTING REPAIR INSTALLED WITH BLIND FASTENERS FROM BS 727E TO BS 767 STR 18 LT TO STR 20 LT. REPAIRED PER EA 
- [SDR 151AW0017](https://openairdocs.org/sdr/151AW0017), Jul 2, 2004: KEELBEAM. CRACKED. CORROSION ON KEEL BEAM AT BS 500D STR 28 RT. REPAIRED PER EA 53-144.
- [SDR 151AW0016](https://openairdocs.org/sdr/151AW0016), Jul 2, 2004: SKIN. DAMAGED. SKIN REPAIR FORWARD OF WATER SERVICE DOOR AT STR 24 LT BS 927 IS TOO CLOSE TO SKIN LAP. REPLACED REPAIR PER EA 53-135.
- [SDR 151AW0015](https://openairdocs.org/sdr/151AW0015), Jul 2, 2004: SKIN. CRACKED. THREE CRACKS UNDER AN IMPROPER REPAIR AT STR 20 LT BS 727D, REPAIR TOO CLOSE TO SKIN LAP AT STR 20 LT BS 967, AND REPAIR INSTALLED WITH BLIND FASTENERS AT STR 2
- [SDR 151AW0014](https://openairdocs.org/sdr/151AW0014), Jul 2, 2004: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT STR 25 RT BETWEEN BS 927 AND BS 947. REPAIRED PER SRM 53-00-01.
- [SDR 151AW0013](https://openairdocs.org/sdr/151AW0013), Jul 2, 2004: ATTACH ANGLE. CRACKED. FLOOR TO FRAME TRANSITION ANGLE CRACKED AT BS 639 LT. REPAIRED PER SRM 51-70-12.
- [SDR 151AW0010](https://openairdocs.org/sdr/151AW0010), Jul 2, 2004: FLOOR SUPPORT. CRACKED. SUPPORT ANGLE CRACKED AT BS 807 FRAME RIGHT BUTTOCK LINE 22. REPLACED SUPPORT ANGLE PER SRM 51-10-2.
- [SDR 151AW0009](https://openairdocs.org/sdr/151AW0009), Jul 2, 2004: FRAME. CRACKED. BS 639 RT FRAME I/B WEB, AND O/B CRACKED. REPLACED PER SRM 51-10-2, REPAIRED WEB PER SRM 51-70-13, AND REPAIRED PER EA 53-148-1.
- [SDR 151AW0005](https://openairdocs.org/sdr/151AW0005), Jul 2, 2004: FRAME. CRACKED. O/B SIDE OF FLOOR FRAME CRACKED AT BS 639. REPAIRED FLOOR CHORD ANGLE PER SRM 51-70-12 AND SRM 51-40-02.
- [SDR 151AW00030](https://openairdocs.org/sdr/151AW00030), Jul 2, 2004: SPLICE. CRACKED. STRINGER SPLICE CRACKED AT STRINGER 4 RT AT BS 907 AND AT STRINGER 4 LT AT BS 907. REPLACED STRINGER SPLICE AT 4 RT AND 4 LT PER SRM 51-40-02.
- [SDR 151AW0002](https://openairdocs.org/sdr/151AW0002), Jul 2, 2004: FLOORBEAM. CRACKED. EXISTING DOUBLER AT RIGHT FWD SIDE OF BS 540 FLOORBEAM AT BL 0 CRACKED AND UNDERSIDE OF BS 540 LINK BEAM AT BL 0 CRACKED. REPLACED LINK BEAM AND LEFT AND RIGHT 
- [SDR 151AW0001](https://openairdocs.org/sdr/151AW0001), Jul 2, 2004: SCUFF PLATE. CRACKED. FWD CORNER SCUFF PLATE AND AFT CORNER SCUFF PLATE OF L1 DOOR HAVE SMALL CRACKS. WELDED CRACKS PER BAC 5975.
- [SDR AWXA200300375](https://openairdocs.org/sdr/AWXA200300375), Apr 15, 2003: SKIN. CRACKED. PHX - MAJOR REPAIR - DURING INSPECTION A 1.875 INCH CRACK WAS FOUND ON FUSELAGE SKIN AT BS 763, STR 19 RT. MAINTENANCE PERFORMED TEMPORARY REPAIR BY CUTTING OUT
- [SDR AWXA200300374](https://openairdocs.org/sdr/AWXA200300374), Apr 15, 2003: SKIN. CRACKED. PHX - MAJOR REPAIR - DURING INSPECTION A 2.625 INCH CRACK WAS FOUND ON FUSELAGE SKIN AT BS 740, STR 19 RT. MAINTENANCE PERFORMED TEMPORARY REPAIR BY CUTTING OUT
- [SDR AWXA200300373](https://openairdocs.org/sdr/AWXA200300373), Apr 15, 2003: SKIN. CRACKED. PHX - MAJOR REPAIR - DURING INSPECTION A 3.5 INCH CRACK WAS FOUND ON FUSELAGE SKIN AT BS 748, STR 18 RT. MAINTENANCE PERFORMED TEMPORARY REPAIR BY CUTTING OUT D
- [SDR AWXA200300324](https://openairdocs.org/sdr/AWXA200300324), Mar 28, 2003: LIGHT. BROKEN. FLIGHT CREW REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8 LT WAS BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 8
- [SDR AWXA200300250](https://openairdocs.org/sdr/AWXA200300250), Mar 10, 2003: SKIN. CRACKED. PHX - MAJOR REPAIR - DURING INSPECTION A CRACK WAS FOUND ON L/H FUSELAGE BETWEEN BS 500D AND BS 520, BELOW STRINGER 12 L/H. MAINTENANCE CUTOUT DAMAGED AREA OF S
- [SDR AWXA200300012](https://openairdocs.org/sdr/AWXA200300012), Jan 4, 2003: BATTERY. INOPERATIVE. FLIGHT CREW REPORTED THAT THE AFT RT EMERGENCY FLASHLIGHT DOES NOT HAVE FLASHING RED LIGHT. MAINTENANCE REMOVED AND REPLACED THE AFT RT EMERGENCY FLASHLIGHT BAT
- [SDR AWXA200200622](https://openairdocs.org/sdr/AWXA200200622), Jul 7, 2002: COVER. CRACKED. DURING C-18 CHECK A 3 INCH CRACK WAS FOUND IN THE UPPER AFT END RADIUS OF THE KEELBEAM MOUNTING COVER JUST BELOW THE AFT LT MOUNT OF THE AUXILLARY HYDRAULIC PUM

All 114: https://openairdocs.org/aircraft/N151AW/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (414, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Piper PA-18-150)

- [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, LLC
- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA01147WI](https://openairdocs.org/stc/SA01147WI): Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Concorde Battery Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA02525LA](https://openairdocs.org/stc/SA02525LA): Installation of Wheel and Brake Assemblies. Game Aerospace LLC
- [STC SA01704LA](https://openairdocs.org/stc/SA01704LA): Installation of the Grove Disk Brake System. Grove Aircraft Landing Gear Systems Inc
- [STC SA02211AK](https://openairdocs.org/stc/SA02211AK): Installation of components to change thrust line orientation. Steve Pierce
- [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC
- [STC SA02200AK](https://openairdocs.org/stc/SA02200AK): Fabrication of replacement engine exhaust system assembly (P/N PA18ESA). Power Flow Systems Inc
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA575WE](https://openairdocs.org/stc/SA575WE): Belly master spray system. Texas Transland LLC
- [STC SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system. Shady Aviation LLC
- [STC SA11854CH](https://openairdocs.org/stc/SA11854CH): Installation of modified exhaust system in lieu of original components. Dakota Cub Aircraft Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA11841BO](https://openairdocs.org/stc/SA11841BO): Installation of T3 Tailwheel Suspension System suspension. T3 Tailwheel Suspension System
- [STC SA02764SE](https://openairdocs.org/stc/SA02764SE): Installation of Acme Aero Shock landing gear shock absorbers. Acme Suspensions LLC
- [STC SA02765SE](https://openairdocs.org/stc/SA02765SE): Installation of Acme Stinger tailwheel landing gear shock absorber. Acme Suspensions LLC
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA03898NY](https://openairdocs.org/stc/SA03898NY): Installation and maintenance of ORATEX covering and coating material. Aircraft Design & Certification Ltd
- [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation
- [STC SA02580AK](https://openairdocs.org/stc/SA02580AK): Installation of Airframes Alaska Replacement Suspension. Airframes Alaska LLC
- [STC SA02191AK](https://openairdocs.org/stc/SA02191AK): Fabrication and installation of Dakota Cub extended wings and associated flaps and ailerons. Dakota Cub Aircraft Inc
- [STC SA02582AK](https://openairdocs.org/stc/SA02582AK): Installation of Airframes Alaska Brake Pedal and Master Cylinder Assembly. Airframes Alaska LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02579AK](https://openairdocs.org/stc/SA02579AK): Installation of Swing bar. Willow Mountain Ranch
- [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc
- [STC SA00715AT](https://openairdocs.org/stc/SA00715AT): Installation of Aqua Floats Model 2200. Outpost X Aviation Inc
- [STC SA518CE](https://openairdocs.org/stc/SA518CE): Install Aqua Model 1900 floats. Outpost X Aviation Inc
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc
- [STC SA04563AT](https://openairdocs.org/stc/SA04563AT): Installation of Sensenich propeller model 2G0M6 C82BGF or 2G0M7 C82BGF. Sensenich Propeller Company
- [STC SP04490AT](https://openairdocs.org/stc/SP04490AT): Installation of Sensenich propeller model 2G0M8/C82BGF. Sensenich Propeller Company
- [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC
- [STC SA02233AK](https://openairdocs.org/stc/SA02233AK): Installation of high visibility fuel sight gauge. Dakota Cub Aircraft Inc
- [STC SA00417BO](https://openairdocs.org/stc/SA00417BO): Installation of T3 Tailwheel Suspension Systems Suspension. T3 Tailwheel Suspension Systems
- [STC SA02175AK](https://openairdocs.org/stc/SA02175AK): Fabrication of Airframes Alaska LLC Heavy Duty Standard Length or 3-inch Extended Main Landing Gear. Airframes Alaska LLC
- [STC SA01606CH](https://openairdocs.org/stc/SA01606CH): Installation of alternate electro-hydraulic power pack system for operation of main wheel skis. F.Atlee Dodge Aircraft Services
- [STC SA3-180](https://openairdocs.org/stc/SA3-180): Installation of Wipaire Skis, Inc. (Aircraft Skis) (FluiDyne) (Federal) Main Skis, Model C2200, Tail Ski, Model CTF2200 or CT3000, and Parts Kit No. W-PMA-001, issued February 26, 2001. F.Atlee Dodge Aircraft Services
- [STC SA3-328](https://openairdocs.org/stc/SA3-328): Installation of Model C-2200 main skis and Model AWT-2500 or AWT-2500A tail wheel skis. F.Atlee Dodge Aircraft Services
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA44AL](https://openairdocs.org/stc/SA44AL): Auxiliary wing fuel tanks. Wilbur Repair Service Marquerite Benson or Anne Wilbur

All 414: https://openairdocs.org/aircraft/N151AW/stcs.md

## Related

- Other Piper PA-18-150 aircraft: https://openairdocs.org/model/piper-pa-18-150/aircraft.md

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