# N150AW: 1964 Cessna 150D - Status: Valid registration - Airframe: [Cessna 150D](https://openairdocs.org/model/cessna-150d) (registry code 2071810, 2 seats) - Engine: [Continental 0-200 series](https://openairdocs.org/engine/continental-0-200-series) (registry code 17020) - Data sheets: [TCDS 3A19](https://openairdocs.org/tcds/3A19) (Textron Aviation Inc.), [TCDS E-252](https://openairdocs.org/tcds/E-252) (Continental Aerospace Technologies, Inc.) (OpenAirDocs) - Serial number: 15060572 - Year built: 1964 - Type: Fixed wing single engine - Engine type: 4 cycle - Airworthiness: Standard, normal - Airworthiness date: April 25, 1964 - Certificate issued: May 15, 2025 - Expires: May 31, 2032 - Mode S code: A0CA44 - Registered owner: [Johnson Seth](https://openairdocs.org/faa-owner/JOHNSON%20SETH) - Location: [Gulfport, MS](https://openairdocs.org/faa-place/MS/Gulfport) - Owner type: Individual - Owner's area on the map: 30.4730° N, 89.1442° W: Placed by OpenAirDocs at the center of ZIP code 39503, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=150AW - Page: https://openairdocs.org/aircraft/N150AW 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 Continental 0-200 model are included. ## ADs that may apply (OpenAirDocs): 36 in force ### Matched by airframe (Cessna 150D) - [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 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 2004-19-01](https://openairdocs.org/ad/2004-19-01): Upper shoulder harness adjusters · Cessna F150G, F150H, F150J and 129 more. Effective Nov 1, 2004 - [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 88-15-06](https://openairdocs.org/ad/88-15-06): Battery Location · Cessna 150, 150A, 150B and 23 more. Effective Aug 3, 1988 - [AD 79-10-14 R1](https://openairdocs.org/ad/79-10-14-R1): Fuel Tank Venting · Cessna 140A, 150, 150A and 172 more. Effective May 30, 1988 - [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 83-17-06](https://openairdocs.org/ad/83-17-06): Aileron Balance Weights · Flap actuated aileron droop system (Sierra Industries STC SA1382WE or 5 others). Effective Sep 1, 1983 - [AD 81-15-03](https://openairdocs.org/ad/81-15-03): Engine Inlet Air Filters · Replace existing engine induction air filter (Brackett Aero Filters STC SA693CE or SA71GL). Effective Jul 20, 1981 - [AD 79-08-03](https://openairdocs.org/ad/79-08-03): Electrical System · Cessna 120, 140, 140A and 152 more. Effective Jun 6, 1979 - [AD 77-02-09](https://openairdocs.org/ad/77-02-09): Wing Flap System · Cessna 150, 150A, 150B and 61 more. Effective Feb 3, 1977 - [AD 75-15-08](https://openairdocs.org/ad/75-15-08): Engine Lubrication · Filtrator Company Engine Crankcase Breather and Vacuum Pump… (D'Shannon Products STC SA2219WE). Effective Sep 10, 1975 - [AD 74-06-02](https://openairdocs.org/ad/74-06-02): AVCON Mufflers · Lycoming 150 and160 hp Model O-320-( ) engine (Williams Robert or Barbara STC SA750CE or 3 others). Effective Mar 18, 1974 - [AD 73-23-07](https://openairdocs.org/ad/73-23-07): Defective Spar Attachment Fittings · Cessna 150, 150A, 150B and 68 more. Effective Nov 19, 1973 - [AD 71-22-02](https://openairdocs.org/ad/71-22-02): Cracks In Nose Gear Fork · Cessna 150, 150A, 150B and 52 more. Effective Nov 9, 1971 - [AD 68-17-04](https://openairdocs.org/ad/68-17-04): Stall Warning System · Cessna 150, 150A, 150B and 63 more. Effective Sep 7, 1968 - [AD 67-03-01](https://openairdocs.org/ad/67-03-01): Exhaust Gas Heat Exchangers · Cessna 150, 150A, 150B and 10 more. Effective Jan 14, 1967 ### Matched by engine (Continental 0-200 series) - [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 96-12-06](https://openairdocs.org/ad/96-12-06): Engine Timing · Continental Motors O-200-A, O-200-B, RR O-200-A and 2 more. Effective Jul 18, 1996 - [AD 94-05-05 R1](https://openairdocs.org/ad/94-05-05-R1): Cylinder Rocker · Continental Motors C-125-1, C-125-2, C145-2 and 59 more. Effective Feb 13, 1996 - [AD 95-21-15](https://openairdocs.org/ad/95-21-15): Aviation Gasoline · Continental Motors A-65-8, C85-12F, C85-12FJ and 77 more. Effective Nov 28, 1995 - [AD 93-22-05](https://openairdocs.org/ad/93-22-05): Carburetor Air Intake Housing Assemblies · Continental Motors C90-12F, C90-12FH, C90-12FJ and 22 more. Effective Dec 14, 1993 - [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 93-10-02](https://openairdocs.org/ad/93-10-02): Missing Cylinder Valve Retainer Key · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 180 more. Effective Aug 12, 1993 - [AD 93-11-03](https://openairdocs.org/ad/93-11-03): Incorrect Connecting Rod · Continental Motors O-200-A, O-300-A, O-300-C and 1 more. Effective Jul 13, 1993 - [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 81-07-06](https://openairdocs.org/ad/81-07-06): AC Fuel Pumps · Continental Motors A-65-1, A-65-12, A-65-12F and 60 more. Effective Apr 1, 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 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 ### Historical (superseded or no longer in force) - [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 86-26-04](https://openairdocs.org/ad/86-26-04) (historical): Shoulder Harness Adjuster · Cessna Aircraft Company, The 120, 140, 140A and 134 more. Effective Jan 6, 1987 - [AD 2009-24-52](https://openairdocs.org/ad/2009-24-52) (historical): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 192 more - [AD 94-14-12](https://openairdocs.org/ad/94-14-12) (historical): Octane Aviation Gasoline · Teledyne Continental Motors A-65-8, C85-12, E185-11 and 68 more ## Information bulletins (advisory) (15 in force) - [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-01-41R2](https://openairdocs.org/saib/CE-01-41R2): Flight Controls. Issued Oct 1, 2007 - [SAIB NE-18-27](https://openairdocs.org/saib/NE-18-27): POWERPLANT Rocker Shaft Boss Inspection. Issued Sep 10, 2018 - [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016 - [SAIB NE-13-04](https://openairdocs.org/saib/NE-13-04): Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing Inspection. Issued Oct 31, 2012 - [SAIB NE-03-45](https://openairdocs.org/saib/NE-03-45): . Issued Jun 27, 2003 - [SAIB CE-98-21R1](https://openairdocs.org/saib/CE-98-21R1): . Issued Jun 10, 1998 - [SAIB ACE-98-21](https://openairdocs.org/saib/ACE-98-21): . Issued Dec 31, 1997 - [SAIB ACE-96-11](https://openairdocs.org/saib/ACE-96-11): . Issued Dec 10, 1996 - [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-01-41R1](https://openairdocs.org/saib/CE-01-41R1) (historical): Cracks in plastic or non-metallic control wheels. Issued Jan 10, 2007 ## NTSB investigations None matched to N150AW. ## FAA accident and incident reports None matched to N150AW. ## Reports on N150AW not matched to an aircraft (1) They name N150AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19990423025099I](https://openairdocs.org/incident/19990423025099I), Apr 23, 1999: Boeing 7373G7 (N150AW), Albuquerque, NM. (-23) Aircraft diverted into bq and declared emergency after APU fire warn light illuminated. Landed at 2135C on 4/19/1999. Contract mx inspected APU awxa sent… ## 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 N150AW not matched to an aircraft (145, newest 50) They name N150AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 150AW0024](https://openairdocs.org/sdr/150AW0024), Jul 3, 2004: TRANSDUCER. INOPERATIVE. AUTO THROTTLE WILL DISENGAGE AND NOT RE-ENGAGE UNTIL FLAPS RETRACTED AND ALL LIGHTS OUT. SEEMS NR 1 THROTTLE LAGS BEHIND NR 2 AFTER TOGA IS PUSHED. PLACED AUTO - [SDR 150AW0023](https://openairdocs.org/sdr/150AW0023), Jun 14, 2004: SENSOR. OUT OF ADJUST. AUTO THROTTLE WILL KICK OFF ON TAKEOFF PRIOR TO REACHING TAKE OFF THRUST. WILL NOT RE-ENGAGE UNTIL FLAPS ARE RETRACTED AND ALL LIGHTS OUT. ADJUSTED PLA SYNCHRO - [SDR 150AW0042](https://openairdocs.org/sdr/150AW0042), May 25, 2004: FRAME. CRACKED. APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 400 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACK PER SRM 53-00-07. - [SDR 150AW0041](https://openairdocs.org/sdr/150AW0041), May 25, 2004: FRAME. CRACKED. APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 500C BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. - [SDR 150AW0040](https://openairdocs.org/sdr/150AW0040), May 25, 2004: FRAME. CRACKED. APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 663 AT STR 2 RT. REPAIRED CRACK PER SRM 53-00-07. - [SDR 150AW0039](https://openairdocs.org/sdr/150AW0039), May 25, 2004: FRAME. CRACKED. APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 663 AT STR 3 RT. REPAIRED CRACK PER SRM 53-00-07. - [SDR 150AW0038](https://openairdocs.org/sdr/150AW0038), May 25, 2004: FRAME. CRACKED. APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 400 BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07. - [SDR 150AW0037](https://openairdocs.org/sdr/150AW0037), May 25, 2004: FRAME. CRACKED. APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 480 BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK IAW SRM 53-00-07. - [SDR 150AW0036](https://openairdocs.org/sdr/150AW0036), May 25, 2004: FRAME. CRACKED. APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS827 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACK IAW SRM 53-00-07. - [SDR 150AW0035](https://openairdocs.org/sdr/150AW0035), May 25, 2004: FRAME. CRACKED. APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 727E BETWEEN STR 8 LT AND STR 9 LT. REPAIRED CRACK PER SRM 53-00-07. - [SDR 150AW0034](https://openairdocs.org/sdr/150AW0034), May 25, 2004: FRAME. CRACKED. APPROX .040 CRACK IN FUSELAGE FRAME AT BS 312 AT STR 6 LT. REPAIRED CRACK PER SRM 53-00-07. - [SDR N150AW0010](https://openairdocs.org/sdr/N150AW0010), May 25, 2004: FRAME. CRACKED. APPROX .040 INCH CRACK IN FUSELAGE FRAME AT BS 480 BETWEEN STR 8 RT AND STR 9 RT. REPAIRED CRACKS PER SRM 53-00-07. - [SDR 150AW0027](https://openairdocs.org/sdr/150AW0027), May 25, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT STRINGER 13 RT BS 867. REPLACED STRINGER TIE CLIP PER SRM 51-10-002. - [SDR 150AW0029](https://openairdocs.org/sdr/150AW0029), May 25, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT STRINGER 6 RT BS 597. REPLACED STRINGER TIE CLIP IAW SRM 51-10-02. - [SDR 150AW0033](https://openairdocs.org/sdr/150AW0033), May 25, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT STRINGER 4 RT BS 616. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. - [SDR 150AW0032](https://openairdocs.org/sdr/150AW0032), May 25, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT STRINGER 8 LT BS 597. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. - [SDR 150AW0031](https://openairdocs.org/sdr/150AW0031), May 25, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT STRINGER 7 LT BS 597. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. - [SDR 150AW0030](https://openairdocs.org/sdr/150AW0030), May 25, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT STRINGER 4 RT BS 597. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. - [SDR 150AW0028](https://openairdocs.org/sdr/150AW0028), May 25, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT STR 18 RT BS 747. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. - [SDR 150AW0026](https://openairdocs.org/sdr/150AW0026), May 25, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT STRINGER 16 RT BS 727E. REPLACED STRINGER TIE CLIP PER SRM 51-10-02. - [SDR 150AW0025](https://openairdocs.org/sdr/150AW0025), May 25, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIP CRACKED AT STRINGER 4 RT BS 727B. STRINGER TIE CLIP REPLACED IAW SRM 51-10-02. - [SDR N150AW0003](https://openairdocs.org/sdr/N150AW0003), May 25, 2004: STRINGER CLIP. CRACKED. STRINGER TIE CLIPS CRACKED AT THE FOLLOWING LOCATIONS: STRINGER 4 RT BS 727D, STRINGER TIE CLIPS REPLACED IAW SRM 51-10-02. - [SDR N150AW0022](https://openairdocs.org/sdr/N150AW0022), May 25, 2004: KEELBEAM. CORRODED. CORROSION ON THE HORIZONTAL FLANGE OF THE KEEL BEAM AT STR 28 RT SPLICE AT BS 500C + 9.0. REPAIRED PER EA NR 53-087. - [SDR N150AW0021](https://openairdocs.org/sdr/N150AW0021), May 25, 2004: BEAR STRAP. CORRODED. CORROSION BETWEEN STRAP AND SKIN AT BS 490 AT STR 28 RT AND IMPROPER REPAIR AT STR 27 RT AT BS 476 PER AD 2002-07-10 AND SB737-53A1177. REPAIRED PER EA NR 53-09 - [SDR N150AW0019](https://openairdocs.org/sdr/N150AW0019), May 25, 2004: PRESSURE PANEL. CORRODED. CORROSION AT BS 1016 AT LOWER DRAIN HOLE ON FORWARD SIDE OF THE PRESSURE PANEL. REPAIRED PER SRM 53-80-08. - [SDR N150AW0018](https://openairdocs.org/sdr/N150AW0018), May 25, 2004: FLOORBEAM. CORRODED. BS 1016 AT RBBL 14 CORROSION AT FLOORBOARD ATTACH HOLE. REPLACED FLOORBEAM T-CAP PER SRM 51-10-2. - [SDR N150AW0017](https://openairdocs.org/sdr/N150AW0017), May 25, 2004: ANGLE. CORRODED. L-ANGLE CORRODED AT BS 1016 TOP OF FLOOR IN AFT LAVATORY AREA. REPLACED ANGLE PER SRM 51-10-2. - [SDR N150AW00170](https://openairdocs.org/sdr/N150AW00170), May 25, 2004: ANGLE. CORRODED. L-ANGLE CORRODED AT BS 1016 TOP OF FLOOR IN AFT LAVATORY AREA. REPLACED ANGLE PER SRM 51-10-2. - [SDR N150AW0016](https://openairdocs.org/sdr/N150AW0016), May 25, 2004: SKIN. DAMAGED. IMPROPER REPAIR INSTALLED AT BS 887 AT STR 20 RT AND AT BS 500A AT STR 10 LT ACCORDING TO AD2002-07-10 AND SB737-53A1177. REPLACED EXISTING REPAIRS PER SRM 53-0 - [SDR N150AW0015](https://openairdocs.org/sdr/N150AW0015), May 25, 2004: BULKHEAD. CRACKED. VERTICAL STIFFENER ON THE AFT SIDE OF BS 178 BULKHEAD IS CRACKED AT LBBL 5.7 AND WL 184. REPAIRED AREA PER SRM 53-10-8. - [SDR N150AW0014](https://openairdocs.org/sdr/N150AW0014), May 25, 2004: BULKHEAD. CRACKED. HFEC REVEALED A CRACK INDICATION AT FASTENER AT RBBL 10.5 AND WL 234 ON THE BS 178 BULKHEAD. REPAIRED AREA PER SRM 53-10-8. - [SDR N150AW0013](https://openairdocs.org/sdr/N150AW0013), May 25, 2004: BULKHEAD. CRACKED. HFEC REVEALED CRACK INDICATIONS ON THE I/B SIDE OF VERTICAL STRAP ON THE BS 178 BULKHEAD AT RBBL 5.7 AND WL 201 AND THE I/B SIDE OF THE VERTICAL STRAP AT LBBL 5 - [SDR N150AW0012](https://openairdocs.org/sdr/N150AW0012), May 25, 2004: SPLICE. CRACKED. STRINGER SPLICE CRACKED AT BS 907 AT STR 4 LT AND AT STR 4 RT. REPLACED STRINGER SPLICE AT STR 4 LT AND STR 4 RT PER SRM 51-10-02. - [SDR N150AW0011](https://openairdocs.org/sdr/N150AW0011), May 25, 2004: FRAME. CRACKED. BS 747 FRAME CRACKED AT STR 13 LT. REPAIRED PER SRM 51-70-11. - [SDR N150AW0009](https://openairdocs.org/sdr/N150AW0009), May 25, 2004: SKATE ANGLE. WORN. FORWARD END OF LEFT SKATE ANGLE FOR VERTICAL DORSAL FIN IS WORN AT BS 1016. REPLACED SKATE ANGLE PER SRM 51-10-02. - [SDR N150AW0008](https://openairdocs.org/sdr/N150AW0008), May 25, 2004: BULKHEAD. DAMAGED. DRILL MARK ON AFT PRESSURE BULKHEAD AT RBL 37.5 AT THE MOISTURE BARRIER RETAINER. REPAIRED PER SRM 53-80-08. - [SDR N150AW0007](https://openairdocs.org/sdr/N150AW0007), May 25, 2004: WEB. CRACKED. CRACK AT CUTOUT IN WEB, 4 INCHES FOWRARD OF L-2 DOOR AT STR 11 LT. REPAIRED PER SRM 51-70-13. - [SDR N150AW0006](https://openairdocs.org/sdr/N150AW0006), May 25, 2004: ATTACH ANGLE. CRACKED. FRAME SHELF ATTACH ANGLES CRACKED AT BS 294.5 AT STR 12 RT, STR 11 RT, AND AT STR 10 RT. REPLACED ANGLES PER SRM 51-10-02. - [SDR N150AW0005](https://openairdocs.org/sdr/N150AW0005), May 25, 2004: THRESHOLD. CRACKED. FORWARD CORNER OF THE FORWARD CARGO DOOR THRESHOLD IS CRACKED. REPAIRED PER BAC 5975. - [SDR N150AW0004](https://openairdocs.org/sdr/N150AW0004), May 25, 2004: SEAT TRACK. CRACKED. STATION 727B SEAT TRACK AT RBBL 24.82 OUTBOARD FLANGE AND SEAT TRACK AT RBBL 45.57 INBOARD AND OUTBOARD FLANGES HAVE A CRACK ON THE UPPER CHORD ON THE HORIZONTA - [SDR N150AW0002](https://openairdocs.org/sdr/N150AW0002), May 25, 2004: SKIN. DAMAGED. LEADING EDGE OF WING DAMAGED OUTBOARD END OF THE NUMBER 5 SLAT. REPAIRED PER SRM 51-70-17. - [SDR N150AW0001](https://openairdocs.org/sdr/N150AW0001), May 25, 2004: WEB. DAMAGED. WEB DAMAGED AFT OF R-2 DOOR. REPLACED WEB PER SRM 51-10-02. - [SDR AWXA200300239](https://openairdocs.org/sdr/AWXA200300239), Mar 10, 2003: PROXIMITY SENSOR. DAMAGED. DURING TAKEOFF ROLL AT LAS EN ROUTE FOR OAK THE MASTER CAUTION LIGHT ILLUMINATED FOLLOWED BY NO. ENGINE AFT BOOST PUMP LIGHT, REJECTED TAKEOFF AT APPROXIMATELY - [SDR AWXA200201199](https://openairdocs.org/sdr/AWXA200201199), Dec 14, 2002: BATTERY. DISCHARGED. EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THAT THE AFT EMERGENCY FLASHLIGHT BATTERY WAS DEAD. REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT, OPERATIONAL CH - [SDR AWXA200201198](https://openairdocs.org/sdr/AWXA200201198), Dec 13, 2002: BATTERY. DISCHARGED. EMERGENCY EQUIPMENT - DURING INSPECTION MAINTENANCE FOUND THE FORWARD GALLEY EMERGENCY FLASHLIGHT HAD A WEAK BATTERY. REMOVED AND REPLACED THE FORWARD GALLEY EM - [SDR AWXA200201196](https://openairdocs.org/sdr/AWXA200201196), Dec 12, 2002: CONTROL SWITCH. INOPERATIVE. AIR TURN BACK ON CLIMB OUT, EXPERIENCED RUDDER AND TRIM PROBLEMS. UNABLE TO TRIM THE RUDDER, WITH AN INDICATION OF ONLY 2 UNITS, LEFT TRIM WILL NOT MOVE. REQUIR - [SDR AWXA200201182](https://openairdocs.org/sdr/AWXA200201182), Dec 10, 2002: BATTERY. DISCHARGED. EMERGENCY EQUIPMENT - DURING INSPECTION THE EMERGENCY FLASHLIGHT JUST ABOVE THE FORWARD FLIGHT ATTENDANT SEAT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REP - [SDR AWXA200201174](https://openairdocs.org/sdr/AWXA200201174), Dec 8, 2002: MEC. FAULTY. ON DESCENT CAUTION PANEL INDICATED RT ENG FAILED. COMPLETED ENG SHUTDOWN. RESTARTED NR 2 ENG. MX REMOVED NR 2 ENG FUEL FILTER & INSPECTED FILTER & HIGH PRESSURE - [SDR AWXA200201154](https://openairdocs.org/sdr/AWXA200201154), Nov 19, 2002: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING 8-DAY CHECK A 1 1/2" CRACK WAS FOUND ON THE FUSELAGE SKIN AFT LOWER SIDE OF THE R/H WING TO BODY FAIRING AT BS 727E, STR 23 R/H. MAI - [SDR AWXA200201153](https://openairdocs.org/sdr/AWXA200201153), Nov 19, 2002: SKIN. CRACKED. MCN - MAJOR REPAIR - DURING 8-DAY CHECK A 3" LONG CRACK WAS FOUND ON THE FUSELAGE SKIN FORWARD OF THE AFT CARGO DOOR AT BS 767, STR 21 R/H. MAINTENANCE CUTOUT D All 145: https://openairdocs.org/aircraft/N150AW/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) (355, 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 150D) - [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 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 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 SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation - [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 SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX 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 SA00037WI](https://openairdocs.org/stc/SA00037WI): Installation of B & C Specialty Products BC100-1 battery. B & C Specialty Products 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 SA00871SE](https://openairdocs.org/stc/SA00871SE): Installation of cockpit sunvisors. Rosen Sunvisor Systems LLC - [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 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 SA00897WI](https://openairdocs.org/stc/SA00897WI): Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. Aero-Mach Wilco LLC - [STC SA403CE](https://openairdocs.org/stc/SA403CE): Installation of Wipaire Skis Inc. Model A-2000A (Aircraft Skis) (FluiDyne) (Federal) Main and NA-800 Nose Skis. F.Atlee Dodge Aircraft Services - [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 SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc - [STC SA1034SW](https://openairdocs.org/stc/SA1034SW): Installation of Lycoming O-320-E2D engine and Sensenich 74DM or McCauley 1C172TM propeller. Quantum Swiss LLC - [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 All 355: https://openairdocs.org/aircraft/N150AW/stcs.md ## Related - Other Cessna 150D aircraft: https://openairdocs.org/model/cessna-150d/aircraft.md - The Continental 0-200 series engine: https://openairdocs.org/engine/continental-0-200-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.