# N570UA: Cessna 150H

- Status: Valid registration
- Airframe: [Cessna 150H](https://openairdocs.org/model/cessna-150h) (registry code 2071818, 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: 15067929
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, utility
- Airworthiness date: January 24, 1968
- Certificate issued: August 17, 2016
- Expires: August 31, 2029
- Mode S code: A7502C
- Registered owner: [Bohl Howard M](https://openairdocs.org/faa-owner/BOHL%20HOWARD%20M)
- Location: [Temecula, CA](https://openairdocs.org/faa-place/CA/Temecula)
- Owner type: Individual
- Owner's area on the map: 33.5109° N, 117.0215° W: Placed by OpenAirDocs at the center of ZIP code 92592, 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=570UA
- Page: https://openairdocs.org/aircraft/N570UA

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): 42 in force

### Matched by airframe (Cessna 150H)

- [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 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 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 93-24-15](https://openairdocs.org/ad/93-24-15): Instrument Panel Light Rheostat · Cessna F150F, F150G, F150H and 26 more. Effective Feb 11, 1994
- [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 72-03-03 R3](https://openairdocs.org/ad/72-03-03-R3): Wing Flap Actuators Jack Screw · Cessna F150F, F150G, F150H and 83 more. Effective Oct 15, 1984
- [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 80-11-04](https://openairdocs.org/ad/80-11-04): Cracked Nutplates · Cessna 150F, 150G, 150H and 22 more. Effective Jun 2, 1980
- [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 67-31-04](https://openairdocs.org/ad/67-31-04): Removal Of Glove Compartment · Cessna 150G and 150H. Effective Nov 29, 1967
- [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 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 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) (16 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-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 N570UA.

## NTSB investigations on N570UA not matched to an aircraft (2)

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

- [NTSB ENG09IA007](https://openairdocs.org/ntsb/ENG09IA007), Jun 10, 2009: Boeing 757-222 (N570UA), Denver, CO, incident, minor damage. Probable cause: There was a malfunction of the electronic engine control (EEC) burner pressure (Pb) sensor that had an abnormally high indication that resulted in an excessive amount of fuel being pumped into the…
- [NTSB CHI01LA331](https://openairdocs.org/ntsb/CHI01LA331), Sep 24, 2001: Boeing 757-222 (N570UA), Indianapolis, IN, no damage. Probable cause: the inadequate crew/group coordination and the parking brakes not set by the pilot in command.

## FAA accident and incident reports

None matched to N570UA.

## Reports on N570UA not matched to an aircraft (2)

They name N570UA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Accident 20090610010509A](https://openairdocs.org/incident/20090610010509A), Jun 10, 2009: Boeing 757222 (N570UA), Denver, CO, Minor damage. (-23) A torch like flame was seen coming from the right engine exhaust during engine start following push back. Ground personnel signaled to the crew to shut…
- [Accident 20010923027589A](https://openairdocs.org/incident/20010923027589A), Sep 23, 2001: Boeing 757222 (N570UA), Indianapolis, IN, No damage. (-23) On 09/23/01, united airlines B-757-222, aircraft registration number N570UA, operating under flight #153 (ind to ord), was pushed back from Indianapolis…

## 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 N570UA not matched to an aircraft (122, newest 50)

They name N570UA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR CALA2013112093136](https://openairdocs.org/sdr/CALA2013112093136), Nov 18, 2013: STOP PIN. OUT OF ADJUST. ON LANDING, BETWEEN 100 FT RA & TOUCHDOWN RECEIVED A RAFT ENTRY DOOR EICAS MESSAGE. ADJUSTED DOOR STOP PINS IAW MM. DOOR CLOSES NORMAL WITH NO EICAS MESSAGES WH
- [SDR CALA2013111592951](https://openairdocs.org/sdr/CALA2013111592951), Nov 13, 2013: SCUFF PLATE. LOOSE. DOOR 4R LOWER SCUFF PLATE IS LEAKING AT FWD LOWER CORNER & BOTH VERTICAL SEAMS. SEVERAL SCREWS CANNOT BE TIGHTENED & JUST SPIN. REMOVED MODIFIED & INSTALLED SCU
- [SDR CALA2013103192538](https://openairdocs.org/sdr/CALA2013103192538), Oct 30, 2013: SCUFF PLATE. LEAKING. DOOR SEAL LEAK 4R. PERFORMED A VISUAL INSPECTION OF THE DOOR, DOOR FRAME & SEAL FOUND TO BE GOOD. PRESSURIZED AIRCRAFT & FOUND LOWER SCUFF PLATE LEAKING AT FWD 
- [SDR CALA2013102292262](https://openairdocs.org/sdr/CALA2013102292262), Oct 22, 2013: PANEL. CORRODED. AFT CARGO COMPARTMENT FLOOR SIDE PANEL HAS A 1 IN BY 1.5 AREA OF CORROSION. LOCATED APPROXIMATE STATION 1424 LBL 24, JUST AFT OF CARGO TIE DOWN. REMOVED CORROSI
- [SDR CALA2013100791800](https://openairdocs.org/sdr/CALA2013100791800), Oct 6, 2013: ENGINE. MALFUNCTIONED. NR 1 ENG EGT & N1 RED LINED, RTFL. NR 1 ENGINE EGT & N1 RED LINED DURING TAKE-OFF 3,000 TO 4,000 FT THEN RETURNED TO NORMAL OPERATING PARAMETERS WITH SLIGHT ENG
- [SDR CALA2013092791516](https://openairdocs.org/sdr/CALA2013092791516), Sep 26, 2013: ALTIMETER. DEFECTIVE. STANDBY ALTIMETER VIBRATOR INTERMITTENTLY STICKS & IS EXTREMELY LOUD. R & R STANDBY ALTIMETER, OPERATIONS CHECKED NORMAL.
- [SDR CALA2013082290675](https://openairdocs.org/sdr/CALA2013082290675), Aug 21, 2013: CONNECTOR. LOOSE. EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 8-10 FLOOR. SECURED EMERGENCY LIGHT CONNECTION PER WDM. OPERATIONS CHECKED OKAY.
- [SDR CALA2013081390389](https://openairdocs.org/sdr/CALA2013081390389), Aug 12, 2013: STRUCTURE. DISLODGED. L4 DOOR HAS STRUCTURE HANGING FROM SLIDE PACK. REPAIRED IAW MM25-66-01-0 400A.
- [SDR CALA2013081290370](https://openairdocs.org/sdr/CALA2013081290370), Aug 11, 2013: SEAL. LEAKING. RIGHT ENGINE APPEARS TO CONSUME MORE OIL THAN THE LEFT. RT ENGINE APPEARS TO HAVE LEAK AT DE-OILER BREATHER OUTLET AREA. SERVICED WITH 7 QTS. AVERAGE OIL CONS. 
- [SDR CALA2013080890276](https://openairdocs.org/sdr/CALA2013080890276), Aug 6, 2013: FLOOR PANEL. DAMAGED. SOFT SPOT IN FLOOR UNDER F/A JUMP SEAT AT L2 DOOR. INSTALLED INTERIM REPAIR IAW SRM.
- [SDR UALA2013061304099](https://openairdocs.org/sdr/UALA2013061304099), Jun 10, 2013: COVER. OUT OF POSITION. FLOOR EMERGENCY LIGHTING STRIP END COVER OFF, PART IS IN COCKPIT. REPLACED END CAP.
- [SDR UALA2013043003018](https://openairdocs.org/sdr/UALA2013043003018), Apr 28, 2013: OXYGEN SYSTEM. LOW PRESSURE. OXYGEN SYSTEM IS LOW. SERVICED CREW OXYGEN TO FULL. OPS & LEAK CHECKED GOOD PER AMM.
- [SDR UALA2013040302198](https://openairdocs.org/sdr/UALA2013040302198), Apr 3, 2013: LIGHT. DISCONNECTED. EMERGENCY LIGHTS FROM SEAT ROW 8 TO ROW 12 INOPERATIVE. CONNECTED LOOSE EMERGENCY LIGHT, OPS CHECKED OK.
- [SDR UALA2013040302197](https://openairdocs.org/sdr/UALA2013040302197), Apr 2, 2013: SWITCH. ENGAGED. EMERGENCY EXIT LIGHT SWITCH WILL NOT ARM PROPERLY FOUND EMERGENCY LIGHTS CONTROL PUSH BUTTON SWITCH ENGAGED AT AFT ATTENDANT'S PANEL P22 ENGAGED. DISENGAGED SWI
- [SDR UALA2013032902037](https://openairdocs.org/sdr/UALA2013032902037), Mar 28, 2013: HANDLE. FAULTY. LEFT FORWARD ENT DOOR EICAS, RTFL. DOOR 1 LEFT INTERIOR DOOR HANDLE MOVING OUT OF THE CLOSED POSITION IN FLIGHT.
- [SDR UALA2013032701959](https://openairdocs.org/sdr/UALA2013032701959), Mar 26, 2013: SKIN. DENTED. FUSELAGE SKIN DENT BETWEEN BS 1500-1520 STR 25-26L. MAJOR REPAIR ACCOMPLISHED. FUSE SKIN REPAIR INSTALLED IAW ECRA 5331-01698. REPAIRED IAW ECRA 5331-01698.
- [SDR UALA2013032701956](https://openairdocs.org/sdr/UALA2013032701956), Mar 26, 2013: STRAP. CORRODED. CORROSION ON SPLICE STRAP STA 1400 BETWEEN STR 29-30. REPAIR INSTALLED IAW ECRA 5331-01701 BETWEEN BS 1384-1406 & STR 28L-27R.
- [SDR UALA2013032701958](https://openairdocs.org/sdr/UALA2013032701958), Mar 25, 2013: ANTENNA. DAMAGED. LOWER FWD FUSELAGE VHF ANTENNA HAS DELAMINATION AND SURFACE CORROSION MARKED. REMOVED AND REPLACED LOWER FWD FUSELAGE VHF ANTENNA IAW B757 AC MM 23-12-03 GND TE
- [SDR UALA2013032501874](https://openairdocs.org/sdr/UALA2013032501874), Mar 24, 2013: SKIN. DAMAGED. FORWARD LOWER FUSELAGE EXTERIOR SKIN BS 500 BETWEEN STR 28-29L. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 3 PG201-206.
- [SDR UALA2013032501873](https://openairdocs.org/sdr/UALA2013032501873), Mar 24, 2013: FRAME. CORRODED. CORROSION ON FORWARD SIDE OF FRAME BS 1460 BETWEEN S29-30L. REPAIRED IAW ECRA 5310-05711.
- [SDR UALA2013032501872](https://openairdocs.org/sdr/UALA2013032501872), Mar 24, 2013: STRUCTURE. CORRODED. FOUND CORROSION FWD AND AFT SIDE STA 1400 BETWEEN 29L-30L.
- [SDR UALA2013032501870](https://openairdocs.org/sdr/UALA2013032501870), Mar 24, 2013: THRESHOLD. DAMAGED. TOOL DAMAGE AT S15L BS 1702-1717. REPAIRED IAW ECRA 5331-01697.
- [SDR UALA2013032501869](https://openairdocs.org/sdr/UALA2013032501869), Mar 24, 2013: THRESHOLD. BULGED. REPAIR DOUBLER BS 1710 STR 15L BULGED. INSPECTED THRESHOLD, REPAIRED PER ECRA 5331-01697. MAJOR REPAIR
- [SDR UALA2013032701957](https://openairdocs.org/sdr/UALA2013032701957), Mar 24, 2013: SKIN. DENTED. DENT 3" FORWARD OF DOOR 2L, 4" BELOW THE SILL. INSPECTED DENT SMOOTH NOT FASTENERS STRIPED INVOLVED SRMS 3 00 01. DENT IS 2"X.062"DEEP, SMOOTH, NO CRACKS GOUGES
- [SDR UALA2013032501868](https://openairdocs.org/sdr/UALA2013032501868), Mar 23, 2013: STRUCTURE. DENTED. DENT FOUND AT UPPER FUSELAGE BS 651.5 BETWEEN STR 2L-4L FOUND TO BE OUT OF LIMITS PER SRM 53-00 -01 FIG 101 DETAIL III. MAJOR REPAIR ACCOMPLISHED: REPAIR DAMAGE
- [SDR UALA2013032501867](https://openairdocs.org/sdr/UALA2013032501867), Mar 23, 2013: SKIN. DENTED. DENT IN UPPER CROWN AREA BS 653.8 2.5 INCHES BELOW S3R. REPAIRED IAW ECRA5331-01700.
- [SDR UALA2013032501866](https://openairdocs.org/sdr/UALA2013032501866), Mar 23, 2013: SKIN. DENTED. DENT FOUND AROUND RIVET BS 646 BETWEEN STR 3-4R, FOUND TO BE OUT OF LIMITS PER SRM 53-00-01 FIG 101 PG102. REPAIRED DAMAGE PER ECRA 5331-01700.
- [SDR UALA2013022201067](https://openairdocs.org/sdr/UALA2013022201067), Feb 21, 2013: CONTROL PANEL. FAULTY. CAPT AUDIO CONTROL PANEL - SERV INPH BUTTON DOES NOT STAY DOWN. REPLACED AUDIO CONTROL PANEL WITH THE FIRST OBSERVER'S PANEL, CHECKS GOOD. DF FIRST OBSERVER AUD
- [SDR UALA2013022101052](https://openairdocs.org/sdr/UALA2013022101052), Feb 21, 2013: LIGHT. INOPERATIVE. EXT EMERGENCY LIGHTS AT DOOR 2R AND 4R INOP. RELAMPED 2EA LIGHTS AT DOOR 2R AND 4R, OP CHECKED GOOD.
- [SDR UALA2013010900161](https://openairdocs.org/sdr/UALA2013010900161), Jan 8, 2013: BULB. INOPERATIVE. R4 DOOR SLIDE LIGHT DOES NOT ILLUMINATE WHEN ARMED. REPLACED BULBS, OPS NORMAL.
- [SDR UALA2012122707420](https://openairdocs.org/sdr/UALA2012122707420), Dec 25, 2012: GIRT BAR. OBSTRUCTED. DOOR 4L WILL NOT ARM. REMOVED ICE FROM GIRT BAR AND UPPER DOOR HINGE & APPLIED ICE RELEASE.
- [SDR UALA2012121207177](https://openairdocs.org/sdr/UALA2012121207177), Dec 8, 2012: OXYGEN SYSTEM. LOW PRESSURE. CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED CREW O2 TO LIMITS AS PER AMM. BEFORE SERV 1200 PSI. AFTER SERV 1500 PSI.
- [SDR UALA2012102506144](https://openairdocs.org/sdr/UALA2012102506144), Oct 25, 2012: COVER. LOOSE. EMERGENCY EXIT LIGHT STRIP LOOSE AT ROW 12. REPLACED SECTION OF PLASTIC CLEAR COVER ON EEL STRIP.
- [SDR UALA2012102206050](https://openairdocs.org/sdr/UALA2012102206050), Oct 20, 2012: BLOCK. OUT OF ADJUST. CAN'T LOCK F/O COCKPIT SLIDING WINDOW. ADJUSTED CAM BLOCK UPPER AFT CORNER IAW MM BECAUSE AFT UPPER CORNER OF WINDOW NEEDED TO BE POSITIONED OUTBOARD .1 OF A IN
- [SDR UALA2012102206009](https://openairdocs.org/sdr/UALA2012102206009), Oct 19, 2012: COOLING FAN. FAULTY. SLIGHT ELEC BURNING SMELL TAXI IN THEN EQUIP CLG OVERHEAT AFTER ENGINE SHUT DOWN. FOUND CB FOR FWD EQ COOLING FAN NR 1 OPEN. REPLACED FAN PER MM, OPS CHECK NORM
- [SDR UALA2012082404765](https://openairdocs.org/sdr/UALA2012082404765), Aug 22, 2012: SLIDE. DEPLOYED. AT DEPARTURE TIME, DOOR 2L SLIDE DEPLOYED BY CREW. REMOVED AND REPLACED SLIDE AND ASSIST BOTTLE ASSY IAW AMM.
- [SDR UALA2012081604560](https://openairdocs.org/sdr/UALA2012081604560), Aug 14, 2012: JAM-NUT. BINDING. REPEAT WRITE UP. CAPT'S WINDOW BINDING WON`T UNLOCK AFTER PRESSURE CYCLE. CHECK CAPTS SLIDING WINDOW PER AMM. FOUND LOWER AFT LINK ARM JAM NUT NOT TIGHT. CHECKE
- [SDR UALA2012080704238](https://openairdocs.org/sdr/UALA2012080704238), Aug 6, 2012: CONTACT. DIRTY. ENGINE BOTTLE 1 DISCHARGE LIGHT INOPERATIVE. TROUBLESHOT PANEL LIGHT SWITCH BY SWAPPING WITH RIGHT SWITCH NEEDS NEW ENGINE FIRE PANEL. CLEANED CONTACTS AND HOUS
- [SDR UALA2012061103229](https://openairdocs.org/sdr/UALA2012061103229), Jun 9, 2012: UNKNOWN. UNKNOWN. FUEL TRANSFER FROM RT WING TO CENTER TANK AT CRUISE, WENT FROM 14.5-0-14.5 AT TOP OF CLIMB. ACCOMPLISHED BITE OF FQIS. NO FAULTS FOUND. SELF TEST GOOD. ALL THRE
- [SDR UALA2012060803140](https://openairdocs.org/sdr/UALA2012060803140), Jun 7, 2012: INDICATOR. TRIPPED. SLOWING FOR APPROACH, RECEIVED TRAILING EDGE FLAP DISAGREE EICAS. SUPPLEMENTAL DATA UPDATE, FLAPS LOCKED AT 21 WHEN FLAP. HANDLE WAS MOVED TO 25, RAN QRH CHECKL
- [SDR UALA2012030501398](https://openairdocs.org/sdr/UALA2012030501398), Mar 5, 2012: COMPRESSOR. FAULTY. AFTER CLIMBOUT CREW STATED NO WATER FROM THE LAV FAUCETS AND HAD VIBRATION. CREW REPORTS POTABLE WATER SYSTEM DRAINED TO EMPTY IN FLIGHT. FOUND LARGE BLOCK OF I
- [SDR UALA2012022001014](https://openairdocs.org/sdr/UALA2012022001014), Feb 20, 2012: ACTUATOR. UNRELIABLE. DUE TO RECENT RELIABILITY ISSUES REPLACED THE ELEVATOR ASYMMETRY LIMITER ACTUATOR.
- [SDR UALA2012012500509](https://openairdocs.org/sdr/UALA2012012500509), Jan 25, 2012: STOP FITTING. GOUGED. FWD CARGO PIT AFT 2ND FROM THE BOTTOM STOP FITTING HAS A DEEP GOUGE. REPLACED REF IPC53-63-51- 010.
- [SDR UALA2011111606284](https://openairdocs.org/sdr/UALA2011111606284), Nov 15, 2011: MODULE. FAULTY. FIRE SYS FAIL LIGHT INOPERATIVE. REPLACED M10445 S2 FAIL LIGHT ANNUNCIATOR AND ACP'D OPERATIONAL TEST OF ENGINE FIRE AND OVERHEAT DETECTION SYSTEM PER MM, CHECK
- [SDR UALA2011091905035](https://openairdocs.org/sdr/UALA2011091905035), Sep 18, 2011: WINDSHIELD. DEFECTIVE. FIRST OFFICERS WINDSHIELD CONNECTOR J1 DOES NOT SIT PARALLEL TO TERMINAL. REPLACED F/O NR 1 WINDSHIELD.
- [SDR UALA2011082204459](https://openairdocs.org/sdr/UALA2011082204459), Aug 22, 2011: TURBINE. OVERTEMP. NR 2 ENG EGT EXCEEDED 645 DEGREES, NOT DURING SURGE. PEAK EGT WAS 656. FOUND EGT EXCEEDENCE NR 2 ENG. EGT RED 656 FOR :29SEC EGT REDLINE 640 FOR :28.8SEC 615 FO
- [SDR UALA2011072603830](https://openairdocs.org/sdr/UALA2011072603830), Jul 25, 2011: GIRT BAR. LACK OF LUBE. DOOR 1R SLIDE ARMING LEVER STIFF BUT FUNCTIONAL. ACCOMPLISHED CHECK OF GIRT BAR MECHANISM, OP CHECKS GOOD. ACCOMPLISHED LUBE OF GIRT BAR FITTINGS. INSTALLED BUS
- [SDR UALA2011061302869](https://openairdocs.org/sdr/UALA2011061302869), Jun 10, 2011: ANGLE. CRACKED. EXTERNAL FUSELAGE ANGLE AT BS 1180 COMMON TO BODY FAIRING FRAME AT LBL 11 HAS A 1 INCH CRACK IN ANGLE RADIUS. MAJOR REPAIR ACCOMPLISHED OF FUSELAGE FAIRING SUPP
- [SDR UALA2011061302868](https://openairdocs.org/sdr/UALA2011061302868), Jun 10, 2011: CREASE BEAM. CORRODED. CORROSION AROUND FASTENER ON CREASE BEAM AT RT STA 1050. COMPLETED REPAIR IAW EA PD 57-53-129.
- [SDR UALA2011060802818](https://openairdocs.org/sdr/UALA2011060802818), Jun 7, 2011: CREASE BEAM. CORRODED. CORROSION AROUND FASTENERS ON CREASE BEAM AT RT FS 1166. MAJOR REPAIR ACCOMPLISHED: AFTER CORROSION REMOVAL FOUND OUT OF LIMITS PER SRM. FABRICATED REPAIR PER I

All 122: https://openairdocs.org/aircraft/N570UA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (356, 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 150H)

- [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 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 SA1052SW](https://openairdocs.org/stc/SA1052SW): Installation of Lycoming O-320-E2D engine according to STC SA1034SW on floatplane version. 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 356: https://openairdocs.org/aircraft/N570UA/stcs.md

## Related

- Other Cessna 150H aircraft: https://openairdocs.org/model/cessna-150h/aircraft.md
- The Continental 0-200 series engine: https://openairdocs.org/engine/continental-0-200-series.md

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