# N160AA: 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: 2391
- Year built: 2007
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: February 14, 2007
- Certificate issued: December 29, 2022
- Expires: December 31, 2029
- Mode S code: A0F1AF
- Registered owner: [Sauerbrey Andreas M](https://openairdocs.org/faa-owner/SAUERBREY%20ANDREAS%20M)
- Location: [Steamboat Springs, CO](https://openairdocs.org/faa-place/CO/Steamboat%20Springs)
- Owner type: Individual
- Owner's area on the map: 40.4756° N, 106.8229° W: Placed by OpenAirDocs: center of Steamboat Springs, CO, 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=160AA
- Page: https://openairdocs.org/aircraft/N160AA

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 N160AA.

## FAA accident and incident reports

None matched to N160AA.

## 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 N160AA not matched to an aircraft (53, newest 50)

They name N160AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR HALA0000188](https://openairdocs.org/sdr/HALA0000188), Jun 18, 2000: TIRE. FAILED. FLT 12 - SFO - ATC ADVISED OF POSSIBLE TIRE FAILURE, FOLLOWED COMPANY PROCEDURS, AND FOUND TIRE NR 2 (LEFT MAIN) IS BLOWN. REMOVED AND REPLACED NR 1, 2 AND 6 MA
- [SDR HALA0000128](https://openairdocs.org/sdr/HALA0000128), Apr 22, 2000: LINK. INOPERATIVE. LAX - FLT 1 - UPON GEAR RETRACTION AFTER TAKEOFF, A STRONG VIBRATION WAS FELT. GEAR WAS CYCLED, VIBRATION PERSISTED. FURTHER INVESTIGATION FOUND FORWARD LEFT NL
- [SDR HALA0000002](https://openairdocs.org/sdr/HALA0000002), Dec 31, 1999: WATER SEPARATOR. CONTAMINATED. HNL - FLT 01 - FUEL FUMES AND SMELL INTERMITTENT COCKPIT. REMOVED AND REPLACED NR 1 PACK WATER SEPARATOR, GROUND RUN OK. LEAK CHECK, SMELL CHECK OK. (X)
- [SDR HALA9900145](https://openairdocs.org/sdr/HALA9900145), Jun 27, 1999: FITTING. DAMAGED. ON CLIMB-OUT, STANDBY ALTIMETER APPROX 2,500 FEET LOWER THAN CAPT AND F/O. ALTIMETER AND STANDBY AIRSPEED IND INDICATING 40 KNOTS LOW DURING CRUISE AND CLIMB. C
- [SDR HALA9900143](https://openairdocs.org/sdr/HALA9900143), Jun 24, 1999: COALESCER. DIRTY. FLT 1 - LAX - CLOSE TO TOP OF CLIMB FA CALLED AND SAID SMOKE IN ALL CABINS PERFORMED CHECKLIST AND RETURNED TO LAX. SMOKE CLEARED ON THE WAY BACK TO LAX. REPLAC
- [SDR AALA990521](https://openairdocs.org/sdr/AALA990521), May 21, 1999: SKIN. CORRODED. TUL - FOUND FUSELAGE SKIN CORRODED AT BS 1216. INSTALLED DOUBLER PER SRM 53-20-00. (M)
- [SDR AALA990520](https://openairdocs.org/sdr/AALA990520), May 20, 1999: SKIN. CORRODED. TUL - FOUND FUSELAGE SKIN CORRODED AT FUSE STATION 127B. INSTALLED DOUBLER PER SRM 53-20-00. (M)
- [SDR AALA990543](https://openairdocs.org/sdr/AALA990543), Apr 16, 1999: BRACKET. CORRODED. TUL - FOUND BRACKET INSIDE LONGERON AT 45R STATION 1787 CORRODED. REPAIRED AND INSTALLED DOUBLER PER ESO 7349, DATED 4/16/99. (M)
- [SDR AALA990525](https://openairdocs.org/sdr/AALA990525), Apr 14, 1999: SKIN. DAMAGED. TUL - LEADING EDGE DAMAGED INBOARD SIDE OF NR 1 SLAT TRACK ICE DOOR. REMOVED DAMAGE AND NECESSARY FASTENERS, INSTALLED AND SECURED DOUBLER WET IAW SRM 57-10-00 
- [SDR AALA990524](https://openairdocs.org/sdr/AALA990524), Apr 14, 1999: LONGERON. CORRODED. TUL - FOUND CORROSION ON BOTTOM SIDE OF LONGERON 50R. REPAIRED LONGERON PER ONE TIME ESO 7349 DATED 4/13/99. (M)
- [SDR AALA990522](https://openairdocs.org/sdr/AALA990522), Apr 14, 1999: DOUBLER. CORRODED. TUL - FOUND CORROSION ON DOUBLER UNDER ANTENNA ATTACH POINTS, AND 16 INCH LONG CRACK IN BELLY SKIN DISCOVERED DURING DOUBLER REMOVAL AREA BETWEEN LONGERON 51L A
- [SDR AALA990501](https://openairdocs.org/sdr/AALA990501), Apr 12, 1999: TRUNNION. CORRODED. TUL - FOUND MLG AFT TRUNNION FORWARD FITTING INSIDE BORE CORRODED AND AFT FACE OF FITTING CORRODED. INSTALLED SERVICEABLE BUSHING AND SPACER PER SRM 57-20-00. (
- [SDR AALA990499](https://openairdocs.org/sdr/AALA990499), Apr 12, 1999: JAMB. CORRODED. TUL - FORWARD LOWER CORNER OF FORWARD CX DOOR JAMB CORRODED AT RADIUS BETWEEN STATION 879-899. BLENDED CORROSION IAW DC1010 SRM 51-21-01/ESO 7349. (M)
- [SDR AALA990496](https://openairdocs.org/sdr/AALA990496), Apr 12, 1999: INTERCOSTAL. CORRODED. TUL - FOUND CORROSION AROUND ANTENNA HOLE BETWEEN STRINGER 52 AND 51R. REMOVED CORROSION PER SRM 51-21-01 VOL II. INSTALLED NEW ANTENNA BAY PER AARD 51-01-00-5.
- [SDR AALA990487](https://openairdocs.org/sdr/AALA990487), Apr 10, 1999: DOUBLER. CORRODED. TUL - FOUND CORROSION ON SKIN SPLICE DOUBLER. INSTALLED REPAIR DOUBLERS PER ESO 7349 DATED 08 APR 99. (M)
- [SDR AALA990480](https://openairdocs.org/sdr/AALA990480), Apr 9, 1999: SKIN. CORRODED. TUL - FOUND CORROSION ON FUSE SKIN UNDER TEMPORARY SKIN DOUBLER IN AREA OF STATION 879 FROM STRINGER 43L TO 47L. REPAIRED PER ESO 7349 DATED 04-08-99. (M)
- [SDR AALA990523](https://openairdocs.org/sdr/AALA990523), Apr 8, 1999: FRAME. CORRODED. TUL - FOUND CORROSION UNDER FRAME, INBOARD OF RIGHT LOADING TRAY. BLENDED CORROSION IAW SRM 51-21-01 VOL II. REPAIRED FRAME AT STATION 1781 IAW DC1010 SRM 53-30
- [SDR AALA990500](https://openairdocs.org/sdr/AALA990500), Apr 7, 1999: LONGERON. CORRODED. TUL - FOUND CORROSION ON BOTTOM OF LONGERON 49L AT STATION 1741. FABRICATE REPLACEMENT STRINGER AND AFT SPLICE INSTALLED STRINGER SRM 53-10-00. (M)
- [SDR AALA990498](https://openairdocs.org/sdr/AALA990498), Apr 7, 1999: LONGERON. CORRODED. TUL - FOUND LONGERON 51L CORRODED INSIDE AT STATION 1100. REMOVED CORROSION IAW SRM 51-21-01 VOL II. REMOVED AND REPLACED CORRODED, STRINGER 51L, SECTION WITH N
- [SDR AALA990497](https://openairdocs.org/sdr/AALA990497), Apr 7, 1999: LONGERON. CORRODED. FOUND STRINGER CORRODED HEAVILY ALONG RIGHT SIDE AND UNDERNEATH FLANGE AT STATION 879, STRINGER 52. CORROSION WAS REMOVED IAW DC1010 MM SRM 52-21-01 VOL II. REP
- [SDR HALA9900047](https://openairdocs.org/sdr/HALA9900047), Feb 10, 1999: LINK. BROKEN. LAX - FLT 09 - (LOG PAGE NR 4832289). AFTER TAKEOFF, VIBRATION FROM NOSE WHEEL DOOR. F.A. OBSERVED RT DOOR NOT RETRACTED. AIRCRAFT MADE AN UNEVENTFUL LANDING IN
- [SDR HALA9800268](https://openairdocs.org/sdr/HALA9800268), Jul 30, 1998: LINE. LEAKING. FLT 21 - SEA - AFTER TAKEOFF LANDING GEAR LEVER WOULD NOT MOVE. REPLACED LEAKING HOSE ON LEFT TRIM ACTUATOR. RESET HYDRAULIC FUSE, SERVICED AND BLED HYDRAULIC S
- [SDR HALA9800165](https://openairdocs.org/sdr/HALA9800165), Jun 14, 1998: CIRCUIT BREAKER. TRIPPED. FLT 482 - PPT - LEFT EMERGENCY AC BUS OFF LIGHT ILLUMINATED. FOLLOWING CHECKS AND FOUND CIRCUIT BREAKER B-20 (TR 1 INPUT) POPPED. RESET, SYSTEM RETURNED TO NORM
- [SDR HALA9700286](https://openairdocs.org/sdr/HALA9700286), Nov 26, 1997: FIRE LOOP. MALFUNCTIONED. FLT 939 - HNL - ENGINE NR 2 LOOP 'B' LIGHT FLICKERED AFTER TAKEOFF FOR 2-3 MINUTES, NORMAL REST OF FLGHT. GROUND CHECK OF NR 2 ENGINE 'B' LOOP, CHECKED GOOD. (M
- [SDR HALA9700172](https://openairdocs.org/sdr/HALA9700172), Sep 12, 1997: HEAT EXCHANGER. DAMAGED. HNL - FLT 26 - E-6 LOG PAGE NR 4102029. AIRCRAFT MADE AIR TURN-BACK TO HNL. NR 3 MANIFOLD FAIL ILLUMINATED DURING CLIMB. NOTE: MANIFOLD PRESSURE, 45 PSI. MANIFO
- [SDR HALA9700171](https://openairdocs.org/sdr/HALA9700171), Sep 10, 1997: LINK. BROKEN. LAX - FLT HA01 - E-6 LOG PAGE NR 4102025. AIRCRAFT MADE AIR TURN-BACK TO LAX DUE LEFT NOSE GEAR DOOR DID NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED LEFT HA
- [SDR AALA971347](https://openairdocs.org/sdr/AALA971347), Jul 28, 1997: SHEAR TIE. CORRODED. TUL - FOUND CORROSION ON SHEAR TIE STATION 1975 LONGERON 49L TO 49R. INSTALLED NEW SHEAR TIE PER SRM 53-00-00. (M)
- [SDR AALA971338](https://openairdocs.org/sdr/AALA971338), Jul 26, 1997: SKIN. CORRODED. TUL - FOUND RIVET HEADS POPPED AND BULGED IN FUSE SKIN STATION 899, 46L. INSTALLED FUSELAGE PLATE REPAIR PER SRM 53-20-00 FIG 6. (M)
- [SDR AALA971346](https://openairdocs.org/sdr/AALA971346), Jul 25, 1997: SKIN. CORRODED. TUL - FOUND CORROSION ON INSIDE OF BELLY SKIN BETWEEN STATION 1997-2012 AND LONGERON 48L-48R. INSTALLED DOUBLER PER SRM 53-20-00, AARD 51-01-00-05 P1 ESO 7349 D
- [SDR AALA971331](https://openairdocs.org/sdr/AALA971331), Jul 25, 1997: LONGERON. CORRODED. TUL - LONGERON 43R IS CORRODED AT STATION 1099. REMOVED LONGERON AND SPLICED IN NEW SECTION PER SRM 53-10. (M)
- [SDR AALA971329](https://openairdocs.org/sdr/AALA971329), Jul 25, 1997: SKIN. CORRODED. TUL - DURING C-CHECK, FOUND CORROSION ON LOWER FUSELAGE SKIN FROM STATION 1936 TO 1998 BETWEEN LONGERONS 48L TO 48R. REMOVED AND REPLACED SKIN SECTION FROM 1936
- [SDR AALA971348](https://openairdocs.org/sdr/AALA971348), Jul 24, 1997: SEAT TRACK. CORRODED. TUL - FOUND CORROSION ON LEFT SEAT TRACK IN G1 GALLEY AREA STATION 771 TO 791. REMOVED AND REPLACED SEAT TRACK PER SRM 53-70-00. (M)
- [SDR AALA971325](https://openairdocs.org/sdr/AALA971325), Jul 24, 1997: CASTING. CORRODED. TUL - DURING C-CHECK, FOUND CORROSION ON BARREL NUT CASTING IN LOWER FORWARD CORNER OF AFT CARGO DOOR OPENING AT STATION 1781 AND LONGERON 42L. REMOVED AND REPL
- [SDR AALA971324](https://openairdocs.org/sdr/AALA971324), Jul 24, 1997: ANGLE. CORRODED. TUL - FOUND DURING C-CHECK, CORROSION ON STATION 1781 CHORD ANGLE BETWEEN LONGERONS 42L AND 43L IN AFT CARGO. REMOVED CORRODED SECTION OF ANGLE AND INSTALLED NE
- [SDR AALA971317](https://openairdocs.org/sdr/AALA971317), Jul 24, 1997: TEE CAP. CRACKED. TUL - CRACK IN TEE CAP ON RT SIDE, INSIDE C.A.C. AT LONGERON 38R AND STA 1156. INSTALLED STRAP AND ARROWHEAD DOUBLER PER ESO 7349 DATED 7-23-97. TST: 71,127 HOU
- [SDR AALA971321](https://openairdocs.org/sdr/AALA971321), Jul 23, 1997: DUCT. CORRODED. TUL - CORROSION ON FORWARD CARGO CHILL DUCT WEB BOTTOM SIDE OF CEILING, STA 775 TO STA 805 AT MINUS 25 OF CENTERLINE. REMOVED DAMAGED AREA, INSTALLED DOUBLER PE
- [SDR AALA971320](https://openairdocs.org/sdr/AALA971320), Jul 23, 1997: AIR DUCT. CORRODED. TUL - CONDITIONED AIR DUCT CORRODED UNDER LEFT SIDE OF ELEVATOR COAT CLOSET AT APPROXIMATELY STA 771. REMOVED DAMAGED AREA. INSTALLED FILLER AND DOUBLER PER SRM
- [SDR AALA971319](https://openairdocs.org/sdr/AALA971319), Jul 23, 1997: SEAT TRACK. CORRODED. TUL - CORROSION ON SEAT TRACK NR 3 STA 775. SPLICED IN NEW SEAT TRACK PER SRM 53-70-00. TST: 71,127.03 HOURS. CYCLES: 29,268. (X)
- [SDR AALA971318](https://openairdocs.org/sdr/AALA971318), Jul 23, 1997: SEAT TRACK. DAMAGED. TUL - CORROSION ON SEAT TRACK AT BS 775. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER PER SRM 53-00-01. TST: 71,127.30 HOURS. CYCLES: 27,268. (X)
- [SDR AALA971314](https://openairdocs.org/sdr/AALA971314), Jul 22, 1997: FLOOR TRACK. CORRODED. TUL - LEFT FLOOR TRACK IN 61A GALLEY CORRODED INSIDE TRACK CHANNEL AT APPROXIMATELY 771. SPLICED IN NEW SEAT TRACK PER SRM 53-70-00. TST: 71,127.03 HOURS. CYCLE
- [SDR AALA971313](https://openairdocs.org/sdr/AALA971313), Jul 22, 1997: FLOOR TRACK. CORRODED. TUL - LEFT FLOOR TRACK IN 61A GALLEY CORRODED INSIDE TRACK CHANNEL AT APPROXIMATELY STA 791. REPLACED LEFT FLOOR TRACK STA 791 PER SRM 51-10-1. TST: 71,127.03 H
- [SDR AALA971326](https://openairdocs.org/sdr/AALA971326), Jul 21, 1997: CASTING. CORRODED. DURING C-CHECK, FOUND BARREL NUT CASTING CORRODED IN LOWER FORWARD CORNER OF AFT CARGO DOOR OPENING AT STATION 1787 AND LONGERON 42L. REMOVED AND REPLACED CASTI
- [SDR AALA971293](https://openairdocs.org/sdr/AALA971293), Jul 20, 1997: DOUBLER. CORRODED. TUL - CORROSION ON SKIN SPLICE FINGER DOUBLER IN CENTER CARGO. REPLACED FINGER DOUBLER PER ESO 7349 DATED 7-17-97. TST: 71,127 HOURS. CYCLES: 29,268. (X)
- [SDR AALA971392](https://openairdocs.org/sdr/AALA971392), Jul 16, 1997: STANCHION. CORRODED. TUL - FOUND CORROSION ON CART LIFT OUTBOARD AFT CORNER STANCHION. BLEND AND SMOOTH PER ESO 7349 DATED 7-16-97. (M)
- [SDR AALA971260](https://openairdocs.org/sdr/AALA971260), Jul 11, 1997: SKIN. CORRODED. TUL - CORROSION ON FUSELAGE SKIN INSIDE CENTER GEAR SPACE. REPAIRED PER SRM 51-00-01. TST: 71,127 HOURS. CYCLES: 29,268. (X)
- [SDR AALA971292](https://openairdocs.org/sdr/AALA971292), Jul 1, 1997: FALSE SPAR. CORRODED. TUL - CORROSION ON FALSE SPAR, UPPER CAP. BLENDED AND SMOOTHED PER ESO 7349 DATED 7-10-97. TST: 71,127:03 HOURS. CYCLES: 29,268. (X)
- [SDR AALA961261](https://openairdocs.org/sdr/AALA961261), Aug 24, 1996: STRINGER. CORRODED. TUL - FOUND CORROSION BETWEEN STRINGER AND FUSELAGE SKIN AT STATION 879 STRINGER 43L, FUSELAGE SKIN HAD CRACKS BETWEEN FASTENERS. STRINGER SPLICED PER SRM 53-10
- [SDR AALA960128](https://openairdocs.org/sdr/AALA960128), Jan 23, 1996: INNER CYLINDER. CRACKED. LAX - DURING B-CHECK, CRACK FOUND ON NLG INNER CYLINDER AT AFT SIDE OF GEAR NEAR LOWER TORQUE LINK. REPLACED NLG INNER CYLINDER. SERVICED NLG STRUT WITH OIL AND
- [SDR AALA960028](https://openairdocs.org/sdr/AALA960028), Jan 9, 1996: CONNECTOR. LOOSE. SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 11C INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 11C. SYSTE
- [SDR AALA960027](https://openairdocs.org/sdr/AALA960027), Jan 9, 1996: STRIP. DEFECTIVE. SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 18C INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY PAX SEAT ROW 18C. SYSTEM GROUND CH

All 53: https://openairdocs.org/aircraft/N160AA/unmatched-reports.md

## 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/N160AA/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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