# N355AA: 1980 Cessna 152 - Status: Valid registration - Airframe: [Cessna 152](https://openairdocs.org/model/cessna-152) (registry code 2071835, 2 seats) - Engine: [Lycoming 0-235 series](https://openairdocs.org/engine/lycoming-0-235-series) (registry code 41505) - Data sheets: [TCDS 3A19](https://openairdocs.org/tcds/3A19) (Textron Aviation Inc.), [TCDS E-223](https://openairdocs.org/tcds/E-223) (Lycoming Engines) (OpenAirDocs) - Serial number: 15284224 - Year built: 1980 - Type: Fixed wing single engine - Engine type: 4 cycle - Airworthiness: Standard, utility - Airworthiness date: February 9, 1980 - Certificate issued: December 30, 2013 - Expires: December 31, 2029 - Mode S code: A3F761 - Registered owner: [Above All Aviation Inc](https://openairdocs.org/faa-owner/ABOVE%20ALL%20AVIATION%20INC) - Location: [Santa Barbara, CA](https://openairdocs.org/faa-place/CA/Santa%20Barbara) - Owner type: Corporation - Owner's area on the map: 34.4795° N, 120.0841° W: Placed by OpenAirDocs at the center of ZIP code 93117, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=355AA - Page: https://openairdocs.org/aircraft/N355AA 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. The registry lists only the engine series, so ADs for every Lycoming 0-235 model are included. ## ADs that may apply (OpenAirDocs): 41 in force ### Matched by airframe (Cessna 152) - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [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 2009-10-09 R2](https://openairdocs.org/ad/2009-10-09-R2): Rudder Control System · Cessna 150F, 150G, 150H and 23 more. Effective Sep 12, 2011 - [AD 2011-10-09](https://openairdocs.org/ad/2011-10-09): Seat Rails and Roller Housing Inspections · Cessna 150A, 150B, 150C and 221 more. Effective Jun 17, 2011 - [AD 2008-22-18](https://openairdocs.org/ad/2008-22-18): Ballistic Recovery Systems, Inc. (BRS) · BRS-150 Parachute Recovery System (Ballistic Recovery Systems STC SA64CH). Effective Dec 9, 2008 - [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 2000-06-01](https://openairdocs.org/ad/2000-06-01): Fuel Strainer Assembly · Cessna 150F, 150G, 150H and 163 more. Effective May 5, 2000 - [AD 97-01-13](https://openairdocs.org/ad/97-01-13): Fuel, Oil and Hydraulic Hoses · Cessna 150, 150A, 150B and 232 more. Effective Feb 3, 1997 - [AD 96-12-23](https://openairdocs.org/ad/96-12-23): Wing Stall Fence Height · Wing leading cuff, wing tips and upper surface flow fences (Williams Robert or Barbara STC SA1371SW). Effective Jul 31, 1996 - [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996 - [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 87-21-05](https://openairdocs.org/ad/87-21-05): Placard - Spins · Cessna 150, 150A, 150B and 15 more. Effective Oct 13, 1987 - [AD 86-24-07](https://openairdocs.org/ad/86-24-07): Engine Controls Installation · Cessna 150C, 150D, 150E and 142 more. Effective Jan 7, 1987 - [AD 83-22-06](https://openairdocs.org/ad/83-22-06): Aileron Hinge Pin · Cessna 152, 172N, 172P and 18 more. Effective Nov 8, 1983 - [AD 80-25-07 R1](https://openairdocs.org/ad/80-25-07-R1): Oil Coolers · American Champion 7ECA, 7GCAA, 7GCBC and 39 more. Effective Sep 24, 1981 - [AD 81-05-01](https://openairdocs.org/ad/81-05-01): Fuel Tank Capacity · Cessna 152, 172N, 172P and 3 more. Effective Mar 2, 1981 - [AD 80-11-04](https://openairdocs.org/ad/80-11-04): Cracked Nutplates · Cessna 150F, 150G, 150H and 22 more. Effective Jun 2, 1980 - [AD 80-06-03](https://openairdocs.org/ad/80-06-03): Wing Flap Cable Clamp · Cessna 150M, 152, 172N and 3 more. Effective Apr 21, 1980 - [AD 80-01-06](https://openairdocs.org/ad/80-01-06): Flap Actuator Assembly · Cessna 152, 172RG, A152 and 2 more. Effective Jan 7, 1980 - [AD 79-02-06](https://openairdocs.org/ad/79-02-06): Exhaust System · Cessna 152 and A152. Effective Jan 25, 1979 ### Matched by engine (Lycoming 0-235 series) - [AD 2026-17-10](https://openairdocs.org/ad/2026-17-10): Reciprocating Engine Cylinder Section · Lycoming Engines O-235, O-235-A, O-235-AP and 159 more. Effective Sep 14, 2026 - [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 2022-16-03](https://openairdocs.org/ad/2022-16-03): Engine (RECIPROCATING) · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-F and 236 more. Effective Aug 15, 2022 - [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 2012-03-07](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 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 98-17-11](https://openairdocs.org/ad/98-17-11): Crankshafts · Continental Motors A-65-3, A-65-8, A75-8 and 90 more. Effective Oct 19, 1998 - [AD 98-01-06](https://openairdocs.org/ad/98-01-06): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 184 more. Effective Feb 13, 1998 - [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 95-03-10](https://openairdocs.org/ad/95-03-10): Push Rods · Lycoming Engines O-235, O-235-A, O-235-AP and 38 more. Effective Jan 24, 1996 - [AD 93-19-04](https://openairdocs.org/ad/93-19-04): Carburetors · Continental Motors A-65-1, A-65-12, A-65-12F and 184 more. Effective Oct 18, 1993 - [AD 90-04-06 R1](https://openairdocs.org/ad/90-04-06-R1): Propeller Governor External Oil Line · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 427 more. Effective May 28, 1991 - [AD 88-02-04](https://openairdocs.org/ad/88-02-04): Carburetors · Lycoming Engines O-235-C1C, O-235-H2C, O-235-L2A and 4 more. Effective Feb 1, 1988 - [AD 81-16-05](https://openairdocs.org/ad/81-16-05): Magnetos · Lycoming Engines AEIO-320-E1B, AEIO-320-E2B, AEIO-360-B1G6 and 234 more. Effective Aug 6, 1981 - [AD 80-25-02 R2](https://openairdocs.org/ad/80-25-02-R2): Pushrods · Lycoming Engines O-235, O-235-A, O-235-AP and 30 more. Effective Jan 13, 1981 - [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 78-25-01](https://openairdocs.org/ad/78-25-01): Condensers · Lycoming Engines O-235-L2C. Effective Dec 8, 1978 - [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 66-06-03](https://openairdocs.org/ad/66-06-03): Connecting Rod Assemblies · Lycoming Engines GO-435-C2 (O-435-17), GO-435-C2A, GO-435-C2A2 and 317 more. Effective Jan 16, 1969 ### Historical (superseded or no longer in force) - [AD 2009-10-09 R1](https://openairdocs.org/ad/2009-10-09-R1) (historical): Rudder stop · Cessna 150F, 150G, 150H and 23 more. Effective Dec 11, 2009 - [AD 2009-10-09](https://openairdocs.org/ad/2009-10-09) (historical): Rudder stop · Cessna 150F, 150G, 150H and 21 more. Effective Jun 17, 2009 - [AD 87-20-03 R2](https://openairdocs.org/ad/87-20-03-R2) (historical): Seat Tracks · Cessna 150A, 150B, 150C and 212 more. Effective Sep 24, 1990 - [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 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) (15 in force) - [SAIB 2025-11](https://openairdocs.org/saib/2025-11): RUDDER CONTROL SYSTEM. Issued Dec 22, 2025 - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB CE-17-12](https://openairdocs.org/saib/CE-17-12): Horizontal Stabilizer Elevator Attach Points. Issued May 11, 2017 - [SAIB CE-16-03](https://openairdocs.org/saib/CE-16-03): VERTICAL TAIL Aft Fin Attachment Fitting. Issued Oct 9, 2015 - [SAIB CE-12-14](https://openairdocs.org/saib/CE-12-14): Three Alternative Methods of Compliance for AD 2011-10-09. Issued Jan 25, 2012 - [SAIB CE-10-40R1](https://openairdocs.org/saib/CE-10-40R1): Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanes. Issued Jul 30, 2010 - [SAIB CE-09-42](https://openairdocs.org/saib/CE-09-42): Lights - Landing Light, Beacon Light and Taxi Light Switch Applications. Issued Jul 24, 2009 - [SAIB CE-09-01](https://openairdocs.org/saib/CE-09-01): Equipment - Emergency. Issued Oct 21, 2008 - [SAIB CE-06-46R1](https://openairdocs.org/saib/CE-06-46R1): . Issued Sep 18, 2006 - [SAIB CE-90-03R2](https://openairdocs.org/saib/CE-90-03R2): . Issued Aug 26, 2002 - [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-14-13](https://openairdocs.org/saib/NE-14-13): Reciprocating Engine - Cylinder Mounting Studs. Issued Mar 24, 2014 - [SAIB NE-06-32R1](https://openairdocs.org/saib/NE-06-32R1): Reciprocating Engine - Crankshaft. Issued Sep 10, 2008 - [SAIB NE-05-89](https://openairdocs.org/saib/NE-05-89): . Issued Sep 30, 2005 - [SAIB NE-01-22](https://openairdocs.org/saib/NE-01-22): . Issued May 11, 2001 - [SAIB CE-10-40](https://openairdocs.org/saib/CE-10-40) (historical): Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanes. Issued Jul 27, 2010 - [SAIB CE-06-46](https://openairdocs.org/saib/CE-06-46) (historical): . Issued May 24, 2006 - [SAIB CE-90-03R1](https://openairdocs.org/saib/CE-90-03R1) (historical): . Issued Jul 27, 2000 ## NTSB investigations None matched to N355AA. ## FAA accident and incident reports None matched to N355AA. ## 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 N355AA not matched to an aircraft (102, newest 50) They name N355AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR AALA20150417007](https://openairdocs.org/sdr/AALA20150417007), Apr 17, 2015: FLASHLIGHT. DEFECTIVE. EMERGENCY FLASHLIGHT IN AFT GALLEY UNDER RT FLIGHT ATTENDANT SEAT IS BAD. R & R FLASHLIGHT IAW AMM 25-60-00. SYS CHECKED NORMAL. - [SDR AALA20150308003](https://openairdocs.org/sdr/AALA20150308003), Mar 8, 2015: FAN. FAULTY. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. AIRCRAFT RETURNED FOR SMOKE IN THE CABIN & BURNING SMELL. FOUND RT RECIRCULATION FAN TO - [SDR AALA20150129004](https://openairdocs.org/sdr/AALA20150129004), Jan 29, 2015: SKIN. CRACKED. LEFT WING SKIN OTBD BOLT HOLE AT AFT PITCH LOAD FITTING HAS A CRACK INDICATION. ACCOMPLISHED REPAIR IAW C3194AG 0001. - [SDR AALA20141019014](https://openairdocs.org/sdr/AALA20141019014), Oct 19, 2014: PRESSURE SWITCH. INOPERATIVE. CENTER HYD SYS PRESS LOSS DURING TAKE-OFF. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED AIR DRIVEN PUMP CONTROL - [SDR AALA20140908007](https://openairdocs.org/sdr/AALA20140908007), Aug 30, 2014: CHARGER. INOPERATIVE. RIGHT OVERWING EXIT SIGN FAILED TEST. REPLACED BATTERY & CHARGER M732. - [SDR AALA20140908006](https://openairdocs.org/sdr/AALA20140908006), Aug 30, 2014: BATTERY PACK. DISCHARGED. SEAT MOUNTED ESCAPE PATH LIGHT FROM ROWS 22 TO 27HJ FAILED BATTERY TEST. REPLACED BATTERY PACK M1209. - [SDR AALA20140908005](https://openairdocs.org/sdr/AALA20140908005), Aug 30, 2014: BATTERY. DISCHARGED. OVERHEAD EMER LIGHTS FROM ROWS 12 TO 28HJ FAILED BATTERY TEST. REPLACED BATTERY & CHARGER M732. - [SDR AALA20140908004](https://openairdocs.org/sdr/AALA20140908004), Aug 30, 2014: LIGHT. INOPERATIVE. OVERHEAD EMER LIGHT ON RT SIDE BETWEEN G4 & G5 FAILED TEST. REPLACED LAMP FOR OVERHEAD EMER LIGHT. OPERATIONS CHECKED NORMAL. - [SDR AALA20140908003](https://openairdocs.org/sdr/AALA20140908003), Aug 30, 2014: LIGHT. INOPERATIVE. OVERHEAD EMER LIGHT NEAR LT NR 1 DOOR INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMER LIGHT. OPERATIONS CHECKED NORMAL. - [SDR AALA20140908002](https://openairdocs.org/sdr/AALA20140908002), Aug 30, 2014: LIGHT. INOPERATIVE. OVERHEAD EMER LIGHT AT FAR LT FWD OF G6 INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMER LIGHT. OPERATIONS CHECKED NORMAL. - [SDR AALA20140908001](https://openairdocs.org/sdr/AALA20140908001), Aug 30, 2014: PORTABLE LIGHT. INOPERATIVE. FLIGHT DECK PORTABLE EMER LIGHT INOPERATIVE. REPLACED FLIGHT DECK PORTABLE EMER LIGHT. OPERATIONS CHECKED NORMAL. - [SDR AALA20140702004](https://openairdocs.org/sdr/AALA20140702004), Jul 2, 2014: LIGHT. INOPERATIVE. EMERGENCY LIGHT AT LT NR 1 DOOR INOPERATIVE & LENS LOOSE. REPLACED LAMP & SECURED LENS FOR EMER LIGHT AT LT NR 1 DOOR. OPERATIONS CHECKED NORMAL. - [SDR AALA20140519009](https://openairdocs.org/sdr/AALA20140519009), May 19, 2014: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT AT SEAT 29B INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT SEAT 29B. OPERATIONS CHECKED NORMAL. - [SDR AALA20140519007](https://openairdocs.org/sdr/AALA20140519007), May 19, 2014: LIGHT. INOPERATIVE. RIGHT INTERIOR LOWER AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR RT INTERIOR LOWER AFT OVERWING EMERGENCY EXIT LIGHT. OPERATIONS CHECKED NO - [SDR AALA20140519006](https://openairdocs.org/sdr/AALA20140519006), May 19, 2014: LIGHT. INOPERATIVE. LEFT NR 4 DOOR, UPPER AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR UPPER AFT EMERGENCY EXIT LIGHT AT LT NR 4 DOOR. OPERATIONS CHECKED NORMAL. - [SDR AALA20140223001](https://openairdocs.org/sdr/AALA20140223001), Feb 23, 2014: LIGHT. INOPERATIVE. RT HAND EMERGENCY FLOOD LIGHT IN FWD GALLEY CEILING AREA INOPERATIVE. REPLACED LAMP FOR RT HAND EMERGENCY FLOOD LIGHT IN FWD GALLEY CEILING AREA, OPERATIONS CHE - [SDR AALA20131206003](https://openairdocs.org/sdr/AALA20131206003), Dec 6, 2013: LIGHT. INOPERATIVE. RT SIDE EXTERIOR FUSELAGE MOUNTED NR 5 SLIDE ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR RT SIDE EXTERIOR FUSELAGE MOUNTED NR 5 SLIDE ILLUMINATION LIGHT. - [SDR AALA20131022009](https://openairdocs.org/sdr/AALA20131022009), Oct 21, 2013: LIGHT. INOPERATIVE. RT NR 1 DOOR HANDLE EXIT ILLUMINATION LIGHTS INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOOR HANDLE EXIT ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL. - [SDR AALA20131022008](https://openairdocs.org/sdr/AALA20131022008), Oct 21, 2013: LIGHT. INOPERATIVE. LT NR 1 DOOR HANDLE EXIT ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 1 DOOR HANDLE EXIT ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL. - [SDR AALA20131022007](https://openairdocs.org/sdr/AALA20131022007), Oct 21, 2013: LIGHT. INOPERATIVE. NR 3 LT SIDE EXTERIOR EXIT ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR NR 3 LEFT SIDE EXTERIOR EXIT ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL - [SDR AALA20131022006](https://openairdocs.org/sdr/AALA20131022006), Oct 21, 2013: LIGHT. INOPERATIVE. NR 3 RT SIDE EXTERIOR EXIT ILLUMINATION INOPERATIVE. REPLACED LAMP FOR NR 3 RT SIDE EXTERIOR EXIT ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL. - [SDR AALA20130907003](https://openairdocs.org/sdr/AALA20130907003), Sep 7, 2013: LIGHT. INOPERATIVE. LT FS 2ND FROM AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT FS 2ND FROM AFT EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL. - [SDR AALA20130907002](https://openairdocs.org/sdr/AALA20130907002), Sep 7, 2013: LIGHT. INOPERATIVE. LT EXTERIOR FS, AFT OVERWING LIGHT, FWD LAMP INOPERATIVE. REPLACED LAMP FOR LT WING EMERGENCY LIGHT. OPERATION CHECKED NORMAL. - [SDR AALA20130411007](https://openairdocs.org/sdr/AALA20130411007), Apr 11, 2013: INTERCOSTAL. GOUGED. DEEP GOUGES ON TOP OF INTERCOSTAL, BELOW GALLEY FLOOR FROM FRAME STATIONS 325 TO 346, LCL 40. INSTALLED NEW ANGLE PER AARD 51-00-05-1. - [SDR AALA20130417017](https://openairdocs.org/sdr/AALA20130417017), Apr 10, 2013: FLOORBEAM. CORRODED. LIGHT CORROSION AROUND TEN SCREW HOLES ON UNDERSIDE OF FLOORBEAM AT STATION 325, RIGHT BUTTLINES 8 TO 54. REMOVED CORROSION PER SRM 51-10-02-0G AND ACCOMPLISHED - [SDR AALA20130417016](https://openairdocs.org/sdr/AALA20130417016), Apr 10, 2013: FLOORBOARD. CORRODED. CORROSION AROUND THREE FLOORBOARD SCREW HOLES AT STATION 325, LEFT BUTTLINES 17 TO 32 AND 49. REMOVED CORROSION PER SRM 53-00-51-1A-1 AND ACCOMPLISHED REPAIR PE - [SDR AALA20130410020](https://openairdocs.org/sdr/AALA20130410020), Apr 10, 2013: FLOORBEAM. CORRODED. LIGHT CORROSION AROUND SIX SCREW HOLES ON TOP AT STATION 325, RIGHT BUTTLINE 5 TO LEFT BUTTLINE 17. REMOVED CORROSION PER SRM 53-00-51-1A-1 AND ACCOMPLISHED REP - [SDR AALA20130120001](https://openairdocs.org/sdr/AALA20130120001), Jan 20, 2013: LIGHT. INOPERATIVE. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT 26B INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT 26B. OPS CHECK NORMAL. - [SDR AALA20121221012](https://openairdocs.org/sdr/AALA20121221012), Dec 21, 2012: LIGHT. UNSECURE. LEFT NUMBER 1 DOOR EMERGENCY FLOOD LIGHT INOPERATIVE. SECURED LEFT NUMBER 1 DOOR FLOOD LIGHT ASSEMBLY IN PLACE. OPS CHECK NORMAL. - [SDR AALA20121110001](https://openairdocs.org/sdr/AALA20121110001), Nov 10, 2012: COOLING FAN. MALFUNCTIONED. LHR - CREW REPORTED ODOR OF HOT PLASTIC IN FLIGHT DECK. NO SMOKE NOTED AND ODOR GRADUALLY ABATED. FLIGHT LANDED LHR WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERV - [SDR AALA20120705008](https://openairdocs.org/sdr/AALA20120705008), Jul 5, 2012: LENS. BROKEN. EMERGENCY AISLE LIGHT LENS COVER AT SEAT 20C BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY AISLE LIGHT AT SEAT 20C. OPS CHECK NORMAL. - [SDR AALA20120305012](https://openairdocs.org/sdr/AALA20120305012), Mar 5, 2012: CONTROL PANEL. FAILED. JFK - INFLIGHT RDU-LHR. CREW REPORTED ONE AIR TRAFFIC CONTROLLER TRANSPONDER WAS ALREADY ON MEL WHEN 2ND ATC TRANSPONDER FAILED. FLIGHT DIVERTED, LANDED WITHOUT - [SDR AALA20120214MIA03](https://openairdocs.org/sdr/AALA20120214MIA03), Feb 14, 2012: LIGHT. INOPERATIVE. LEFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT FUSELAGE EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20120214MIA02](https://openairdocs.org/sdr/AALA20120214MIA02), Feb 14, 2012: LIGHT. INOPERATIVE. RIGHT NUMBER 2 EXTERIOR DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20120214MIA01](https://openairdocs.org/sdr/AALA20120214MIA01), Feb 14, 2012: LIGHT. INOPERATIVE. RIGHT FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT FUSELAGE EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20120206DFW01](https://openairdocs.org/sdr/AALA20120206DFW01), Feb 6, 2012: RELIEF VALVE. INOPERATIVE. DFW - CREW REPORTED ON CLIMBOUT, RIGHT ENGINE PRESSURE RELIEF VALVE EICAS MESSAGE AND RIGHT BLEED LIGHT ON OVERHEAD. EMERGENCY DECLARED FLIGHT RETURNED DFW LAND - [SDR AALA20120130TUL08](https://openairdocs.org/sdr/AALA20120130TUL08), Jan 27, 2012: LIGHT. INOPERATIVE. EMERGENCY CEILING LIGHT IN FORWARD GALLEY FORWARD OF FLIGHT ATTENDANT JUMPSEAT INOPERATIVE. REPLACED LAMP. OPS CHECK NORMAL. - [SDR AALA20120130TUL07](https://openairdocs.org/sdr/AALA20120130TUL07), Jan 27, 2012: LIGHT. INOPERATIVE. EMERGENCY CEILING LIGHT AT 2B INOPERATIVE. REPLACED LAMP FOR EMERGENCY CEILING LIGHT AT 2B. - [SDR AALA20120128DFW02](https://openairdocs.org/sdr/AALA20120128DFW02), Jan 27, 2012: LIGHT. INOPERATIVE. LEFT FUSELAGE EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT FUSELAGE EXTERIOR EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20120103MIA03](https://openairdocs.org/sdr/AALA20120103MIA03), Jan 2, 2012: LIGHT. INOPERATIVE. RIGHT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20120103MIA02](https://openairdocs.org/sdr/AALA20120103MIA02), Jan 2, 2012: LIGHT. INOPERATIVE. RIGHT FUSELAGE FORWARD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT FORWARD EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20120103MIA01](https://openairdocs.org/sdr/AALA20120103MIA01), Jan 2, 2012: LIGHT. INOPERATIVE. RIGHT FUSELAGE AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT AFT EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20111014AFW01](https://openairdocs.org/sdr/AALA20111014AFW01), Oct 11, 2011: SPAR. CRACKED. CRACK IN THE LEFT PYLON STRUT FORWARD UPPER SPAR WEB AROUND THE POWER FEEDER CABLE CUTOUT. ACCOMPLISHED DOUBLER PER EA B767-54-019565. - [SDR AALA20110614TUL01](https://openairdocs.org/sdr/AALA20110614TUL01), Jun 12, 2011: SIGN. INOPERATIVE. RIGHT NUMBER 1 DOOR EMERGENCY SIGN INOPERATIVE. REPLACED EMERGENCY SIGN ASSEMBLY FOR RIGHT NUMBER 1 DOOR. OPS CHECK NORMAL. - [SDR AALA20110612MIA02](https://openairdocs.org/sdr/AALA20110612MIA02), Jun 12, 2011: LIGHT. INOPERATIVE. THE 28H OVERHEAD CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR 28H OVERHEAD CEILING EMERGENCY LIGHT. OPS CHECK NORMAL. - [SDR AALA20110208MIA01](https://openairdocs.org/sdr/AALA20110208MIA01), Feb 8, 2011: SHUTOFF VALVE. INOPERATIVE. MIA - CREW REPORTED LEFT HIGH PRESSURE SHUT-OFF VALVE EICAS INDICATION IN FLIGHT. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOV - [SDR AALA20101118GRU01](https://openairdocs.org/sdr/AALA20101118GRU01), Nov 18, 2010: COMPRESSOR. STALLED. GRU - CAPTAIN REPORTED LOUD BANG AND RIGHT ENGINE COMPRESSOR STALL (SINGLE ENGINE TIME 20 MINUTES). THE CREW RECEIVED A FIRE LIGHT ON RIGHT ENGINE AND PULLED A - [SDR AALA2009011100306](https://openairdocs.org/sdr/AALA2009011100306), Jan 11, 2009: LIGHT. INOPERATIVE. SFO- LEFT HAND AFT EXTERIOR DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED LIGHT ASSEMBLY AT LEFT HAND AFT EXTERIOR DOOR. - [SDR AALA200802411A](https://openairdocs.org/sdr/AALA200802411A), Oct 26, 2008: START VALVE. FAILED. MIA INFLIGHT - CREW REPORTED ENGINE STARTER CUTOUT INDICATION 15 MINUTES AFTER TAKEOFF. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED START VALVE FOR NU - [SDR AALA200802387](https://openairdocs.org/sdr/AALA200802387), Sep 20, 2008: LAMP. INOPERATIVE. DFW EXTERIOR EMERGENCY LIGHT AT AFT LT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT AFT LT. SYSTEM GROUND CHECKED NORMAL OPS. All 102: https://openairdocs.org/aircraft/N355AA/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) (329, 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 (Cessna 152) - [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, LLC - [STC SA00709CH](https://openairdocs.org/stc/SA00709CH): Installation of replacement wing root vent described by Dwg Nos. 8-30-96-1& 8-30-96-2, no rev, both dtd 8/30/96, or later FAA app rev. Gallagher Aviation, 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 SA02069AK](https://openairdocs.org/stc/SA02069AK): Fabrication and installation of the Airglas, Inc., Landes PA32-206LA Nose Fork equipped with up to a 8.50 x 6 tire. Airglas Inc - [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 SA01134DE](https://openairdocs.org/stc/SA01134DE): Installation of EarthX ETX680-24-TSO Lithium Battery. EarthX 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 SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc - [STC SA04075CH](https://openairdocs.org/stc/SA04075CH): Installation of Dynon EFIS-D10A EAA sales kit part number 102778-000. Dynon Avionics Inc - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor 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 SA01330LA](https://openairdocs.org/stc/SA01330LA): Installation of alternate avionics support assembly. Radiorax Aviation Systems LLC - [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd - [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 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 SA00088WI](https://openairdocs.org/stc/SA00088WI): Installation of replacement stabilizer and elevator tips. Curry Aviation LLC - [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc - [STC SA1219EA](https://openairdocs.org/stc/SA1219EA): Installation of a Sensenich Model 72CKS6-0-56 -54 or -52 metal propeller and a S72CK spinner assembly. Sensenich Propeller Company - [STC SA02575AK](https://openairdocs.org/stc/SA02575AK): Installation of the nose tire scraper P/N TSL-100. Aero Twin Inc - [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine - [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC - [STC SA00897WI](https://openairdocs.org/stc/SA00897WI): Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. Aero-Mach Wilco LLC - [STC SA00406WI](https://openairdocs.org/stc/SA00406WI): Installation of replacement flap trailing edge bulbs with AOG Drawing. Athena Aircraft, LLC - [STC SA00709SE](https://openairdocs.org/stc/SA00709SE): Installation of replacement control surface skin panels. Athena Aircraft, LLC - [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation - [STC SA2433CE](https://openairdocs.org/stc/SA2433CE): Installation of aileron and/or flap gap seals. Curry Aviation LLC - [STC SA2515CE](https://openairdocs.org/stc/SA2515CE): Installation of replacement wing tips. Curry Aviation LLC - [STC SA2851CE](https://openairdocs.org/stc/SA2851CE): Installation of wheel fairings. Curry Aviation LLC - [STC SA909CE](https://openairdocs.org/stc/SA909CE): Install STOL kit (wing leading edge cuffs, drooped tips, stall fences and aileron gap seals). (152 LANDPLANE). Curry Aviation LLC - [STC SA01827WI](https://openairdocs.org/stc/SA01827WI): Installation of LED Position Lights. Aero-Mach Wilco LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications 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 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 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC - [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC - [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc - [STC SA220SO](https://openairdocs.org/stc/SA220SO): Tow bar, release mechanism, and safety tow link. Fliegen Works Inc. d/b/a Pacific Aerial Tow Hooks All 329: https://openairdocs.org/aircraft/N355AA/stcs.md ## Related - Other Cessna 152 aircraft: https://openairdocs.org/model/cessna-152/aircraft.md - The Lycoming 0-235 series engine: https://openairdocs.org/engine/lycoming-0-235-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.