# N153AA: 2007 Aviat A-1B

- Status: Valid registration
- Airframe: [Aviat A-1B](https://openairdocs.org/model/aviat-a-1b) (registry code 2210406, 2 seats)
- Engine: [Lycoming O-360-A1P](https://openairdocs.org/engine/lycoming-o-360-a1p) (registry code 42259)
- Data sheets: [TCDS A22NM](https://openairdocs.org/tcds/A22NM) (Aviat Aircraft Inc.), [TCDS E-286](https://openairdocs.org/tcds/E-286) (Lycoming Engines) (OpenAirDocs)
- Serial number: 2386
- Year built: 2007
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: January 16, 2007
- Certificate issued: September 30, 2019
- Expires: September 30, 2029
- Mode S code: A0D555
- Registered owners: [Horn Jack E](https://openairdocs.org/faa-owner/HORN%20JACK%20E), [Horn Marcia L](https://openairdocs.org/faa-owner/HORN%20MARCIA%20L)
- Location: [Erie, CO](https://openairdocs.org/faa-place/CO/Erie)
- Owner type: Co-owned
- Owner's area on the map: 40.0541° N, 105.0187° W: Placed by OpenAirDocs at the center of ZIP code 80516, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=153AA
- Page: https://openairdocs.org/aircraft/N153AA

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): 22 in force

### Matched by airframe (Aviat A-1B)

- [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 2020-16-06](https://openairdocs.org/ad/2020-16-06): Horizontal Stabilizer Structure · Aviat A-1, A-1A, A-1B and 2 more. Effective Sep 1, 2020

### Matched by engine (Lycoming O-360-A1P)

- [AD 2026-04-11](https://openairdocs.org/ad/2026-04-11): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 605 more. Effective Apr 8, 2026
- [AD 2017-16-11](https://openairdocs.org/ad/2017-16-11): Reciprocating Engine Power Section · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-360-B1G6 and 93 more. Effective Aug 15, 2017
- [AD 2012-19-01](https://openairdocs.org/ad/2012-19-01): Crankshafts · Lycoming Engines AEIO-360-A1A, AEIO-360-A1B, AEIO-360-A1B6 and 321 more. Effective Oct 24, 2012
- [AD 2012-03-07](https://openairdocs.org/ad/2012-03-07): Carburetor · Lycoming Engines GO-435, GO-435-C2 (O-435-17), GO-435-C2A and 389 more. Effective Mar 27, 2012
- [AD 2009-26-12](https://openairdocs.org/ad/2009-26-12): Cylinder assemblies · Engine Components Reciprocating Engine Cylinder Assemblies, AEIO-320-D1B, AEIO-320-D2B and 264 more. Effective Feb 4, 2010
- [AD 2007-04-19 R1](https://openairdocs.org/ad/2007-04-19-R1): SAP cylinder assemblies · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 314 more. Effective May 7, 2007
- [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 2006-10-21](https://openairdocs.org/ad/2006-10-21): ECi connecting rods · Engine Components Reciprocating Engine Connecting Rods, AEIO-360-B1B, AEIO-360-B1D and 171 more. Effective Jun 22, 2006
- [AD 2004-10-14](https://openairdocs.org/ad/2004-10-14): Crankshaft gear · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 642 more. Effective Jun 25, 2004
- [AD 98-02-08](https://openairdocs.org/ad/98-02-08): Crankshaft · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 216 more. Effective Mar 30, 1998
- [AD 97-15-11](https://openairdocs.org/ad/97-15-11): Cylinder kits · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 538 more. Effective Aug 12, 1997
- [AD 96-09-10](https://openairdocs.org/ad/96-09-10): Oil pump · Lycoming Engines AEIO-320-E1A, AEIO-320-E1B, AEIO-320-E2A and 334 more. Effective Jul 15, 1996
- [AD 95-26-02](https://openairdocs.org/ad/95-26-02): Aviation Gasoline · Lycoming Engines IO-320-B1A, IO-320-B1B, IO-320-B1C and 182 more. Effective Jan 24, 1996
- [AD 92-12-05](https://openairdocs.org/ad/92-12-05): Piston Pins · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 532 more. Effective Jul 10, 1992
- [AD 89-04-02](https://openairdocs.org/ad/89-04-02): Carburetors · Continental Motors O-470-11, O-470-11-CI, O-470-11B and 175 more. Effective Mar 8, 1989
- [AD 80-06-05](https://openairdocs.org/ad/80-06-05): Magnetos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 254 more. Effective Mar 28, 1980
- [AD 75-08-09](https://openairdocs.org/ad/75-08-09): Oil Pump Drive Shaft · Lycoming Engines AEIO-360-A1B, AEIO-360-A1B6, AEIO-360-A1C and 365 more. Effective Aug 18, 1977
- [AD 69-24-03](https://openairdocs.org/ad/69-24-03): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 321 more. Effective Nov 29, 1969
- [AD 67-01-04](https://openairdocs.org/ad/67-01-04): Oil Filters · Full flow oil filter (Superior Flow STC SA401SW or 2 others). Effective Jan 2, 1967
- [AD 63-22-03](https://openairdocs.org/ad/63-22-03): Carburetors · Continental Motors GO-300-A, GO-300-B, GO-300-C and 143 more. Effective Dec 2, 1963

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

- [AD 2024-21-02](https://openairdocs.org/ad/2024-21-02) (historical): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 548 more. Effective Dec 5, 2024
- [AD 2008-19-05](https://openairdocs.org/ad/2008-19-05) (historical): Parallel Valve'' reciprocating engines · Engine Components Reciprocating Engine Cylinder Assemblies, AEIO-320-D1B, AEIO-320-D2B and 262 more. Effective Oct 20, 2008
- [AD 2005-26-10](https://openairdocs.org/ad/2005-26-10) (historical): ECi cylinder assemblies. · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 413 more. Effective Jan 31, 2006
- [AD 81-18-04 R2](https://openairdocs.org/ad/81-18-04-R2) (historical): Engine Oil Pump Driven Impeller and Shaft · Textron Lycoming, AVCO AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 376 more. Effective Jun 7, 1982

## Information bulletins (advisory) (6 in force)

- [SAIB CE-17-18](https://openairdocs.org/saib/CE-17-18): Engine Exhaust System, Muffler Cracking. Issued Jun 20, 2017
- [SAIB NE-19-08](https://openairdocs.org/saib/NE-19-08): Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve Cylinders. Issued May 2, 2019
- [SAIB NE-08-32R1](https://openairdocs.org/saib/NE-08-32R1): Propeller Governor  Idler Gear Shaft Set Screw. Issued May 13, 2016
- [SAIB NE-14-13](https://openairdocs.org/saib/NE-14-13): Reciprocating Engine - Cylinder Mounting Studs. Issued Mar 24, 2014
- [SAIB NE-13-06](https://openairdocs.org/saib/NE-13-06): Pushrod Shroud Spring Retainers, Engine Components Part No. AEL14995, for Lycoming Engines 320, 360, and 540 Series Engines. Issued Nov 21, 2012
- [SAIB NE-06-32R1](https://openairdocs.org/saib/NE-06-32R1): Reciprocating Engine - Crankshaft. Issued Sep 10, 2008
- [SAIB NE-08-32](https://openairdocs.org/saib/NE-08-32) (historical): Propeller Governor Set Screw. Issued Jul 3, 2008

## NTSB investigations

None matched to N153AA.

## NTSB investigations on N153AA not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB NYC89IA063](https://openairdocs.org/ntsb/NYC89IA063), Dec 30, 1988: McDonnell Douglas DC-10 (N153AA), Atlantic Ocean (Atlantic Ocean), incident, no damage

## FAA accident and incident reports

None matched to N153AA.

## Reports on N153AA not matched to an aircraft (1)

They name N153AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19920117002849I](https://openairdocs.org/incident/19920117002849I), Jan 17, 1992: Doug DC1010 (N153AA), San Francisco, CA, Minor damage. Tire blew out on landing rollout. Aircraft was towed to gate.

## 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 N153AA not matched to an aircraft (24)

They name N153AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR HALA0100166](https://openairdocs.org/sdr/HALA0100166), Jul 7, 2001: COMPUTER. ATB - FLT 22 - DURING CLIMB-OUT AT 225 KTS WHEN RETRACTION SLATS, STICK SHAKER ACTIVATED. WE RE-EXTENDED THE SLATS AND STICK SHAKER STOPPED. NOTE SLAT RESET LIG
- [SDR HALA0100160](https://openairdocs.org/sdr/HALA0100160), Jul 5, 2001: PIN. LAS - FLT 3 - FOUND LEFT MLG TRUCK SWIVEL PIN APPEARS TO BE COMING OUT ON INBOARD SIDE OF TRUCK. JACKED AIRCRAFT, REINSTALLED PIN PR MM 32-12-01. NO FURTHER ACT
- [SDR HALA0000378](https://openairdocs.org/sdr/HALA0000378), Nov 5, 2000: SENSOR. OUT OF ADJ. FLT 15 - SFO - RIGHT MAIN LANDING GEAR DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR, NO HELP. DUMPED FUEL. AN UNEVENTFUL LANDING WAS MADE IN SFO. F
- [SDR HALA0000010](https://openairdocs.org/sdr/HALA0000010), Jan 4, 2000: TRANSMITTER. OUT OF ADJUST. LAX - FLT 23 - AIRCRAFT DIVERTED TO LAX FOR FLAP PROBLEM. FLAPS INDICATED ABOUT 1-2 DOWN ON LEFT WING AND CONFIRMED VISUALLY THAT FLAPS WERE DOWN. VERIFIED FLAP
- [SDR HALA9900007](https://openairdocs.org/sdr/HALA9900007), Jan 8, 1999: WIRE. SHORTED. HNL - FLT 939 - EMERGENCY FLOOR LIGHTS ARE ON. REPAIRED SHORTED WIRE BEHIND L1 DOOR EXIT ICON. OPS CHECK OK. (M)
- [SDR HALA9800398](https://openairdocs.org/sdr/HALA9800398), Nov 22, 1998: VALVE. FAILED. TUL - FLT 4103 - START VALVE ILLUMINATED INFLIGHT ON NR 3 ENGINE. A/C RETURNED TO TUL, WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED NR 3 ENGINE ST
- [SDR HALA9800342](https://openairdocs.org/sdr/HALA9800342), Oct 10, 1998: PROXIMITY BOX. FAILED. PDX - FLT 25 - NOSE GEAR UNSAFE LIGHT ILLUMINATED DURING CLIMB AT 20,000 FT VISUAL INSPECTION OF VIEWING PORT REVEALED NOTHING OBVIOUS. LIGHT EXTINGUISHED AT 26
- [SDR HALA9800184](https://openairdocs.org/sdr/HALA9800184), Jul 5, 1998: POWER SUPPLY. INOPERATIVE. HNL - FLT 03 - LOG PAGE NR 4824872 - EMERGENCY LIGHT MID-POWER SUPPLY FAILED TEST. (X)
- [SDR HALA9800116](https://openairdocs.org/sdr/HALA9800116), May 3, 1998: BATTERY CHARGER. FAILED. HNL - FLT 26 - LOG PAGE 4096350 - ON PRE-FLIGHT IN HNL FOUND EMERGENCY LIGHT TEST INOPERATIVE. BITE TEST SHOWED OVERWING BATTERY PACK INOPERATIVE. REPLACED BATT
- [SDR HALA96192](https://openairdocs.org/sdr/HALA96192), Dec 28, 1996: ENGINE. DAMAGED. LAX - FLT 921 - AIRCRAFT 153 DIVERTED TO LAX NR 2 ENGINE VIBRATION FELT IN THE RUDDER PEDALS AND IN THE AFT CABIN AT POWER SETTINGS ABOVE 95 PERCENT N2. WHEN PO
- [SDR HAL96058](https://openairdocs.org/sdr/HAL96058), Sep 9, 1996: FLOOR BEAM. CRACKED. DURING CHECK, FOUND 3 CRACKS IN AFT FLOOR BEAM LOWER CAP STATION Y 1501, AT STATION X EACH CRACK IS APPROX 1 INCH LONG. INSTALLED FABRICATED DOUBLERS IAW ESO 73
- [SDR HAL960059](https://openairdocs.org/sdr/HAL960059), Sep 9, 1996: ANGLE. CRACKED. FOUND CORROSION AND METAL SPLIT AT TOP OF VERTICAL SUPPORT ON FALSE REAR SPAR 3 FEET FROM WHEEL WELL ON THE RIGHT TRAILING EDGE. REMOVED CORROSION AND INSTALLED
- [SDR HALA960053](https://openairdocs.org/sdr/HALA960053), Sep 3, 1996: WEB. CRACKED. DURING CHECK, FOUND CRACK ON WEB 46 RIGHT INBOARD OF ACCESS DOOR 142AZ ON THE INBOARD SIDE OF WEB APPROX 18 INCHES AFT THE FORWARD BULKHEAD. INSTALLED DOUBLER P
- [SDR HALA960052](https://openairdocs.org/sdr/HALA960052), Sep 3, 1996: ROLLER TRACK. CORROSION. FOUND CORROSION ON TOP SIDE OF INBOARD RIGHT ROLLER TRACK, STATION 824 TO STATION 859. REMOVED AND REPLACED RIGHT ROLLER TRACK STARTING AT AT STATION 824 PER SR
- [SDR HAL960056](https://openairdocs.org/sdr/HAL960056), Sep 3, 1996: CARGO TRACK. CORROSION. DURING CHECK, FOUND CORROSION ON CENTER ROLLER TRACK AT STATION 979 TO STATION 1099. FABRICATED NEW ROLLER TRACK AND INSTALLED PER SRM 51-10-00-1. (M)
- [SDR HAL960055](https://openairdocs.org/sdr/HAL960055), Sep 3, 1996: SUPPORT. CORRODED. DURING CHECK, FOUND CORROSION ON BOTTOM OF FLOOR BEAM VERTICAL SUPPORT 19 INCHES RIGHT OF CENTER LINE AT FRAME ATTACH POINT. REPLACED VERTICAL SUPPORT AS PER SR
- [SDR HAL960051](https://openairdocs.org/sdr/HAL960051), Sep 3, 1996: DOUBLER. CORRODED. DURING CHECK, FOUND THE LOWER LEFT LEADING EDGE SACRIFICIAL DOUBLER CORRODED WHERE THE INBOARD LATCH FOR ACCESS PANEL 517AB CONTACTS IT. INSTALLED DOUBLER AFTER
- [SDR HAL960046](https://openairdocs.org/sdr/HAL960046), Sep 3, 1996: FITTING. CORRODED. DURING CHECK, FOUND STRINGER 52 TERMINAL FITTING CORRODED BETWEEN STATION 795 AND 798 AS MARKED. REMOVED AND REPLACED STRINGER TERMINAL FITTING AT STATION 795 P
- [SDR HAL960045](https://openairdocs.org/sdr/HAL960045), Sep 3, 1996: ANGLE. CORRODED. DURING CHECK, FOUND CORROSION ON THE BELT FRAME ANGLE STATION 979, AFT SIDE, FROM STRINGER 51 RIGHT TO STRINGER 51 LEFT. CUT OUT CORRODED ANGLE AND INSTALLED NE
- [SDR HAL960044](https://openairdocs.org/sdr/HAL960044), Sep 3, 1996: ANGLE. CORRODED. DURING CHECK, FOUND CORROSION ON SURFACE OF BELT FRAME AT STATION 1841. CORROSION WAS ON THE LOWER 'J' ANGLE LIP. REMOVED AND REPLACED THE LOWER 'I' ANGLE WITH 
- [SDR HALA96112](https://openairdocs.org/sdr/HALA96112), Aug 11, 1996: BATTERY. DISCHARGED. FLT NR 4 - HNL - FOUND EMERGENCY FLOOR PATH LIGHTING ON RIGHT SIDE OF AIRCRAFT ON. SELECTOR SWITCH IN OFF POSITION. REPOSITIONED SEAT LIGHT CONNECTOR AT ROW 1H.
- [SDR HAL9684](https://openairdocs.org/sdr/HAL9684), Jun 29, 1996: CONTROLLER. MALFUNCTIONED. LAX - FLT 04 - AIRCRAFT WOULD NOT PRESSURIZE IN AUTO MODE SHORTLY AFTER TAKEOFF FROM LAX. F/A SAID R-4 DOOR AND L-4 DOOR NOT PLUGGING PROPERLY AFTER TAKEOFF. MA
- [SDR HALA95164](https://openairdocs.org/sdr/HALA95164), Nov 27, 1995: ATTACH BOLT. CRACKED. LAX - DURING ACCOMPLISHMENT OF SPECIAL CARD ITEM NR 3950-1F, FOUND RIGHT FORWARD VERTICAL STABILIZER ATTACH BOLT CRACKED, LOCATED UNDER LEADING EDGE WRAP AROUND
- [SDR HAL95053](https://openairdocs.org/sdr/HAL95053), Apr 26, 1995: SUPPORT BEAM. CRACKED. ITEM WAS DISCOVERED DURING GENERAL CHECK (WALKAROUND) IN LAX. CHECK B-4, VISUAL WAS CONFIRMED WITH DYE PENETRANT. 2 CRACKS .125 - .25 INCH LONG OUT OF RIVET HOL

## STCs that may be installed (OpenAirDocs) (168, 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 (Aviat A-1B)

- [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 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 SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc
- [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc
- [STC SA11177SC](https://openairdocs.org/stc/SA11177SC): Installation of a Hartzell Propeller Inc. model HC-C2YR-IN/NG8301-3 propeller. Hartzell Propeller LLC
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA02396AK](https://openairdocs.org/stc/SA02396AK): Replacement of Sky International Inc. landing gear strut assemblies with Floats Alaska, LLC. +3 extended gear, part numbers 45017-501HD-3X and 45017-502HD-3X. Seaplanes North LLC
- [STC SA02589AK](https://openairdocs.org/stc/SA02589AK): Installation of the Hartzell Model 3C1-R430A1/80C01 Propeller. Momentum Aeronautics Holdings LLC
- [STC SA01240SE](https://openairdocs.org/stc/SA01240SE): Installation of secondary voltage indication system. Visual Instruments LLC
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02765SE](https://openairdocs.org/stc/SA02765SE): Installation of Acme Stinger tailwheel landing gear shock absorber. Acme Suspensions LLC
- [STC SA39CH](https://openairdocs.org/stc/SA39CH): Installation of an Amphibian Landing Gear Position Advisory System/Laser Gear Advisory System. Wipaire Inc
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [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 SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC
- [STC SA01416SE](https://openairdocs.org/stc/SA01416SE): Installation of a butterfly valve in the oil cooler inlet duct. Westview Aviation LLC
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, 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 SA02838CH](https://openairdocs.org/stc/SA02838CH): Installation of Wipaire Skis Main Wheel Skis Model C2200. F.Atlee Dodge Aircraft Services
- [STC SA3-423](https://openairdocs.org/stc/SA3-423): Installation of CT-3000 tail ski on airplanes equipped with Scott 3200 or 3400 tail wheels. F.Atlee Dodge Aircraft Services
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA02023CH](https://openairdocs.org/stc/SA02023CH): Installation of an MT-Propeller model MTV-15-B/210-58 and spinner assembly P-277-B. McFarlane Aviation LLC
- [STC SA02870CH](https://openairdocs.org/stc/SA02870CH): Installation of MT Propeller, model MTV-9-B/(198-200) -52, MTV-9-B-C-R-M/CR 198-200-52, MTV-15-B-C-R-M/CR 210-58, MTV-15-B/(205-210)-58, MTV-15-B/203-52 and MTV-15-B-C-R-M/CR-203-52, with matching spinner. McFarlane Aviation LLC
- [STC SA02568AK](https://openairdocs.org/stc/SA02568AK): Installation of Airframes Alaska Aluminum Lift Struts. Airframes Alaska LLC
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC SA01721CH](https://openairdocs.org/stc/SA01721CH): Installation of Baumann Model BF2150A floats per Baumann Drawing List BF-2150A-01, Rev B, dtd 9/19/02 or later FAA approved revisions. Baumann Floats LLC
- [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA02288AK](https://openairdocs.org/stc/SA02288AK): Installation of Alpha Omega Suspension System (AOSS) in place of original bungees. Burl's Aircraft LLC
- [STC SA02153AK](https://openairdocs.org/stc/SA02153AK): Installation of Burl's Aircraft Rebuild Magnum I tail wheel Penetration ski. Burl's Aircraft Rebuild LLC
- [STC SA03819NY](https://openairdocs.org/stc/SA03819NY): Installation and maintenance of Oratex 6000 Covering and Coating System. Lanitz-Prena Folien Factory GmbH
- [STC SA01015SE](https://openairdocs.org/stc/SA01015SE): Installation of eligible Alaska Bushwheel, Inc. wheels and TSO-C62d tires. ABI LLC
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA02553AK](https://openairdocs.org/stc/SA02553AK): Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener. Keller Engineering Group LLC
- [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies

All 168: https://openairdocs.org/aircraft/N153AA/stcs.md

## Related

- Other Aviat A-1B aircraft: https://openairdocs.org/model/aviat-a-1b/aircraft.md
- The Lycoming O-360-A1P engine: https://openairdocs.org/engine/lycoming-o-360-a1p.md

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