# N763CA: 2014 Cirrus Design SR20

- Status: Valid registration
- Airframe: [Cirrus Design SR20](https://openairdocs.org/model/cirrus-design-sr20) (registry code 2130000, 4 seats)
- Engine: [Continental IO-360-ES](https://openairdocs.org/engine/continental-io-360-es) (registry code 17160)
- Data sheets: [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH) (Cirrus Design Corporation), [TCDS E1CE](https://openairdocs.org/tcds/E1CE) (Continental Aerospace Technologies, Inc.) (OpenAirDocs)
- Serial number: 2251
- Year built: 2014
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: April 21, 2014
- Certificate issued: October 14, 2026
- Expires: October 31, 2033
- Mode S code: AA4CE0
- Registered owner: [Attar Aviation LLC](https://openairdocs.org/faa-owner/ATTAR%20AVIATION%20LLC)
- Location: [West Hills, CA](https://openairdocs.org/faa-place/CA/West%20Hills)
- Owner type: LLC
- Owner's area on the map: 34.2005° N, 118.6649° W: Placed by OpenAirDocs at the center of ZIP code 91307, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=763CA
- Page: https://openairdocs.org/aircraft/N763CA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 26 in force

### Matched by airframe (Cirrus Design SR20)

- [AD 2024-24-11](https://openairdocs.org/ad/2024-24-11): Power Lever · Cirrus Design SR20, SR22 and SR22T. Effective Dec 23, 2024
- [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 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009
- [AD 2008-14-13](https://openairdocs.org/ad/2008-14-13): Upper door hinge · Cirrus Design SR20 and SR22. Effective Aug 14, 2008
- [AD 2008-11-18](https://openairdocs.org/ad/2008-11-18): Heat exchanger · Cirrus Design SR20. Effective Jul 7, 2008
- [AD 2008-03-16](https://openairdocs.org/ad/2008-03-16): Rudder, aileron, and rudder-aileron interconnect rigging · Cirrus Design SR20 and SR22. Effective Mar 11, 2008
- [AD 2007-14-03](https://openairdocs.org/ad/2007-14-03): Cirrus Airplane Parachute System (CAPS) · Cirrus Design SR20 and SR22. Effective Aug 16, 2007
- [AD 2006-21-03](https://openairdocs.org/ad/2006-21-03): Brake caliper piston O-ring seals · Cirrus Design SR20 and SR22. Effective Nov 17, 2006
- [AD 2006-19-10](https://openairdocs.org/ad/2006-19-10): Adjust crew seat break-over bolts · Cirrus Design SR20 and SR22. Effective Oct 24, 2006
- [AD 2006-07-06](https://openairdocs.org/ad/2006-07-06): Wire harness · Cirrus Design SR20 and SR22. Effective May 11, 2006
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2002-24-08](https://openairdocs.org/ad/2002-24-08): Cable clamp · Cirrus Design SR20 and SR22. Effective Jan 24, 2003
- [AD 2002-21-02](https://openairdocs.org/ad/2002-21-02): Self-locking retaining nut · Cirrus Design SR20 and SR22. Effective Nov 8, 2002
- [AD 2001-25-03](https://openairdocs.org/ad/2001-25-03): Rivets In Elevator and Rudder · Cirrus Design SR20 and SR22. Effective Dec 17, 2001

### Matched by engine (Continental IO-360-ES)

- [AD 2023-17-04](https://openairdocs.org/ad/2023-17-04): Reciprocating Engine Oil System · F & M Enterprises' Model C6LC, C6LC-S or C6LC-L oil filter… (Stratus Tool Technologies STC SE09356SC or 2 others). Effective Oct 26, 2023
- [AD 2023-05-16](https://openairdocs.org/ad/2023-05-16): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 147 more. Effective Mar 15, 2023
- [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 2012
- [AD 2011-26-07](https://openairdocs.org/ad/2011-26-07): Engine · Continental Motors C-125-1, C-125-2, C145-2 and 48 more. Effective Jan 24, 2012
- [AD 2010-11-04](https://openairdocs.org/ad/2010-11-04): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 190 more. Effective Jun 16, 2010
- [AD 2000-23-21](https://openairdocs.org/ad/2000-23-21): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 164 more. Effective Dec 12, 2000
- [AD 97-26-17](https://openairdocs.org/ad/97-26-17): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 90 more. Effective Jan 23, 1998
- [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 92-04-09](https://openairdocs.org/ad/92-04-09): Rocker Shaft Hold Down Stud · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 41 more. Effective Jun 22, 1993
- [AD 91-19-03](https://openairdocs.org/ad/91-19-03): Oil Filter · Continental Motors 6-285-A, 6-285-B, 6-285-BA and 169 more. Effective Sep 29, 1991
- [AD 88-03-06](https://openairdocs.org/ad/88-03-06): Oil Filter · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 155 more. Effective Apr 15, 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

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

- [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008
- [AD 2008-06-28](https://openairdocs.org/ad/2008-06-28) (historical): Primary flight display · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 10, 2008
- [AD 2005-17-19](https://openairdocs.org/ad/2005-17-19) (historical): Crew seat recline locks · Cirrus Design SR20 and SR22. Effective Oct 13, 2005
- [AD 2002-05-05](https://openairdocs.org/ad/2002-05-05) (historical): Limitation Section - Cirrus Aircraft Parachute System (CAPS) Activation Cable · Cirrus Design SR20 and SR22. Effective Mar 19, 2002
- [AD 2023-04-08](https://openairdocs.org/ad/2023-04-08) (historical): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 141 more. Effective Feb 23, 2023
- [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 2009-24-51](https://openairdocs.org/ad/2009-24-51) (historical): Hydraulic lifters · Teledyne Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 156 more
- [AD 2002-13-04](https://openairdocs.org/ad/2002-13-04) (historical): Magneto impulse coupling stop pin · Teledyne Continental Motors C-125-1, C-125-2, C145-2 and 48 more. Effective Jul 12, 2002
- [AD 2000-08-51](https://openairdocs.org/ad/2000-08-51) (historical): Crankshaft · Teledyne Continental Motors IO-360-A, IO-360-AB, IO-360-B and 158 more

## Information bulletins (advisory) (19 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-11-50](https://openairdocs.org/saib/CE-11-50): Flight Controls, Flaps. Issued Aug 26, 2011
- [SAIB CE-08-12R1](https://openairdocs.org/saib/CE-08-12R1): Electrical Power. Issued Mar 16, 2011
- [SAIB CE-11-09](https://openairdocs.org/saib/CE-11-09): Navigation  Flight Management Computing Software System. Issued Jan 5, 2011
- [SAIB CE-09-46](https://openairdocs.org/saib/CE-09-46): Landing Gear, Nose. Issued Jul 31, 2009
- [SAIB CE-09-32](https://openairdocs.org/saib/CE-09-32): Navigation: Cirrus Aircraft Under-Glareshield GPS/WAAS Antenna Mount. Issued May 29, 2009
- [SAIB CE-09-01](https://openairdocs.org/saib/CE-09-01): Equipment - Emergency. Issued Oct 21, 2008
- [SAIB CE-07-08](https://openairdocs.org/saib/CE-07-08): Avidyne Primary Flight display (PFD). Issued Oct 31, 2006
- [SAIB CE-06-30](https://openairdocs.org/saib/CE-06-30): . Issued Feb 9, 2006
- [SAIB CE-06-07](https://openairdocs.org/saib/CE-06-07): . Issued Nov 4, 2005
- [SAIB CE-05-88](https://openairdocs.org/saib/CE-05-88): . Issued Sep 30, 2005
- [SAIB CE-05-77](https://openairdocs.org/saib/CE-05-77): . Issued Jul 27, 2005
- [SAIB CE-04-74](https://openairdocs.org/saib/CE-04-74): . Issued Aug 3, 2004
- [SAIB CE-03-09](https://openairdocs.org/saib/CE-03-09): . Issued Dec 16, 2002
- [SAIB CE-02-34](https://openairdocs.org/saib/CE-02-34): . Issued Jun 19, 2002
- [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016
- [SAIB NE-13-15](https://openairdocs.org/saib/NE-13-15): Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control Levers. Issued Feb 8, 2013
- [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-10-09](https://openairdocs.org/saib/NE-10-09): Reciprocating Engine Power Section: Hydraulic Valve Lifters. Issued Nov 20, 2009
- [SAIB CE-08-12](https://openairdocs.org/saib/CE-08-12) (historical): Electrical Power. Issued Feb 27, 2008

## NTSB investigations

None matched to N763CA.

## FAA accident and incident reports

None matched to N763CA.

## 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 N763CA not matched to an aircraft (98, newest 50)

They name N763CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR U2RA2012092148603](https://openairdocs.org/sdr/U2RA2012092148603), Sep 18, 2012: SKIN. DENTED. FUSELAGE EXTERIOR BS 1620 - 1640, BETWEEN S23-24R, TWO EACH DENTS FOUND IN SKIN.
- [SDR U2RA2012092148601](https://openairdocs.org/sdr/U2RA2012092148601), Sep 18, 2012: STRINGER SPLICE. CRACKED. AFT CARGO COMPARTMENT AT BS 1620 STRINGER SPLICE 23R WAS FOUND CRACKED.
- [SDR U2RA2012092148602](https://openairdocs.org/sdr/U2RA2012092148602), Sep 18, 2012: SKIN. DENTED. FUSELAGE EXTERIOR SKIN BETWEEN BS 1580 AND 1600 AND BETWEEN S25-26R DENTED.
- [SDR U2RA2012072348603](https://openairdocs.org/sdr/U2RA2012072348603), Jul 23, 2012: SKIN. MISREPAIRED. SKIN MISREPAIRED AT BS 490, BETWEEN S22-23R.
- [SDR U2RA2012072348602](https://openairdocs.org/sdr/U2RA2012072348602), Jul 23, 2012: SKIN. DENTED. FUSELAGE SKIN AT BS 450, BETWEEN S25-26R HAS DENT FOUND TO BE OUT OF SRM LIMITS.
- [SDR U2RA2012072348601](https://openairdocs.org/sdr/U2RA2012072348601), Jul 23, 2012: SILL. CORRODED. CORROSION FOUND AROUND FASTENER HOLES ABOVE AND BELOW ANGLE ON THE LT EMERGENCY EXIT SILL PLATE AT BS 1320 - 1360.
- [SDR U2RA2012072448601](https://openairdocs.org/sdr/U2RA2012072448601), Jun 28, 2012: FLOORBEAM. CORRODED. FLOORBEAM CORRODED AROUND FASTENER HOLES AT BS1600, BETWEEN LBL24 AND RBL24. REPAIRED IAW EA PD57-53-170.
- [SDR U2RA201206148602](https://openairdocs.org/sdr/U2RA201206148602), Jun 14, 2012: FITTING. GALLED. NR 1 ENGINE 1/B SIDE LOAD FITTING TWO FASTENER HOLES GALLING AND ELONGATED.
- [SDR U2RA201206148601](https://openairdocs.org/sdr/U2RA201206148601), Jun 14, 2012: FLOOR SUPPORT. CRACKED. FORWARD CARGO FLOOR SUPPORT WEB CRACKED UPPER AFT SECTIONS BS 657 AT LBL 7.55
- [SDR U2RA2012041648602](https://openairdocs.org/sdr/U2RA2012041648602), Apr 13, 2012: LONGERON. CRACKED. MAIN PASSENGER CABIN AREA, CRACK FOUND IN STRINGER S10L AT BS 625 EXTENDING FROM RIVET HOLE. CRACK LENGTH IS 0.125" LONG.
- [SDR U2RA2012041648601](https://openairdocs.org/sdr/U2RA2012041648601), Apr 13, 2012: LONGERON. CRACKED. MAIN PASSENGER CABIN AREA, 3 EA CRACKS FOUND IN STRINGER S7L AT BS 625, EACH CRACK IS 0.125" LONG.
- [SDR U2RA2012040548601](https://openairdocs.org/sdr/U2RA2012040548601), Apr 5, 2012: STRINGER. CRACKED. MAIN CABIN AT BS 1701, STRINGER 11R WAS FOUND TO BE CRACKED. CRACK LENGTH 1".
- [SDR U2RA2012032348602](https://openairdocs.org/sdr/U2RA2012032348602), Mar 23, 2012: STRINGER. CRACKED. MAIN CABIN AT BS 1701, STRINGER 16R FOUND TO BE CRACKED. CRACK LENGTH IS APPROX 1.5" LONG.
- [SDR U2RA2012032348601](https://openairdocs.org/sdr/U2RA2012032348601), Mar 23, 2012: INTERCOSTAL. CRACKED. INTERCOSTAL IN MAIN PASSENGER CABIN WAS FOUND TO BE CRACKED AT AFT LOWER END AT BS 1600 RBL 24. CRACK LENGTH IS 1.5" LONG.
- [SDR U2RA2012032148601](https://openairdocs.org/sdr/U2RA2012032148601), Mar 13, 2012: FLOORBEAM. CORRODED. AFT CARGO FLOORBEAM ZEE CHANNELS ARE CORRODED UNDER NUTPLATES AT BS 1325, BTW RBL 10 & LBL 15.
- [SDR U2RA2012021648602](https://openairdocs.org/sdr/U2RA2012021648602), Feb 15, 2012: INTERCOSTAL. CRACKED. E & E COMPARTMENT INTERCOSTAL CRACKED AT AFT END, BS 440 - 410 AT S23L.
- [SDR U2RA2012021648601](https://openairdocs.org/sdr/U2RA2012021648601), Feb 15, 2012: CUSP WEB. CORRODED. MAIN CABIN, CORROSION FOUND ON THE CUSP WEB BETWEEN BS 1620 TO 1640 AT RBL 54.
- [SDR U2RA20120105080](https://openairdocs.org/sdr/U2RA20120105080), Jan 5, 2012: STIFFENER. CRACKED. FORWARD CARGO COMPARTMENT AT BS 845 AND RBL 19, STIFFENER FOUND CRACKED.
- [SDR U2RA20110105079](https://openairdocs.org/sdr/U2RA20110105079), Jan 5, 2012: FLOOR SUPPORT. CORRODED. AFT CARGO FLOOR SUPPORT CHANNEL LOCATED AT BS 1510 AND LBL 15 FOUND TO BE CORRODED UNDER NUTPLATES.
- [SDR U2RA486DHN078](https://openairdocs.org/sdr/U2RA486DHN078), Dec 13, 2011: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT AT BS 1350 LBL 7.5, FLOOR SUPPORT WAS FOUND TO BE CORRODED.
- [SDR U2RA20111213077](https://openairdocs.org/sdr/U2RA20111213077), Dec 13, 2011: FRAME. DENTED. DENT FOUND ON TOP OF FRAME AT BS 690 S24L.
- [SDR U2RA2011120300076](https://openairdocs.org/sdr/U2RA2011120300076), Dec 3, 2011: INTERCOSTAL. CORRODED. BS 1681 S17R, AFT LOWER WEB INTERCOSTAL FOUND TO BE CORRODED.
- [SDR U2RA2011112948675](https://openairdocs.org/sdr/U2RA2011112948675), Nov 29, 2011: ANGLE. CORRODED. AFT CARGO COMPARTMENT - SPLICE ANGLES HAS SEVERAL AREAS OF CORROSION, BS1340 - 1345 RBL 2.7, LBL 2.90, LBL 7.55 AND LBL 10.95.
- [SDR U2RA2011112948674](https://openairdocs.org/sdr/U2RA2011112948674), Nov 29, 2011: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT, FLOOR SUPPORT "Z" CHANNEL FOUND TO BE CORRODED UNDER NUT-PLATES AT BS 1335 LBL 10.
- [SDR U2RA486DHN071](https://openairdocs.org/sdr/U2RA486DHN071), Oct 25, 2011: SKIN. DENTED. FUSELAGE SKIN BS 460, BETWEEN S23R AND S24R, DENTED. REPAIRED IAW SRM 53-00-01/REPAIR 2.
- [SDR U2RA20111017070](https://openairdocs.org/sdr/U2RA20111017070), Oct 17, 2011: ATTACH FITTING. CORRODED. R4 DOOR WEB & ATTACHING SUPPORT FOR FLOORBEAM AT BS1640 - 1681 REPLACED DUE TO CORROSION.
- [SDR U2RA20111014069](https://openairdocs.org/sdr/U2RA20111014069), Oct 14, 2011: FITTING. CORRODED. BS 1720 RBL 53, HEAVY CORROSION ON CORNER FITTING BELOW AFT PRESSURE BULKHEAD.
- [SDR U2RA20111014068](https://openairdocs.org/sdr/U2RA20111014068), Oct 14, 2011: BEAM. CRACKED. MAIN PASSENGER CABIN PRESSURE RESISTANT BEAM CRACKED AT FASTENER HOLE AT STA BS 1681 BL 0.
- [SDR U2RA20111014067](https://openairdocs.org/sdr/U2RA20111014067), Oct 14, 2011: FLOORBEAM. CORRODED. BS377 LBL45 - 62, HEAVY CORROSION ABOVE AND BELOW FLOORBEAM, AREA DAMAGE CUT-OUT 85 INCHES.
- [SDR U2RA20111014066](https://openairdocs.org/sdr/U2RA20111014066), Oct 14, 2011: CHANNEL. CORRODED. AFT CARGO ZEE CHANNEL FRAME SUPPORT, CORRODED AT BS 1320 RBL 10.
- [SDR U2RA201110140066](https://openairdocs.org/sdr/U2RA201110140066), Oct 14, 2011: FLOORBEAM. CORRODED. BS377 LBL 45-62, HEAVY CORROSION ABOVE AND BELOW FLOORBEAM. AREA DAMAGE CUT-OUT 85 INCHES.
- [SDR U2RA20111004003](https://openairdocs.org/sdr/U2RA20111004003), Oct 4, 2011: INTERCOSTAL. CRACKED. INTERCOSTAL AFT SIDE OF FLOORBEAM AT BS 1320 LBL45 BELOW SEAT TRACK IS CRACKED.
- [SDR U2RA20111004001](https://openairdocs.org/sdr/U2RA20111004001), Oct 4, 2011: SUPPORT. CORRODED. BS 336, LBL 53 FWD OF L1 DOOR HAS CORROSION, AROUND NUTPLATES AND HOLE DRILLED IN RADIUS WITH GOUGE INSIDE.
- [SDR U2RA](https://openairdocs.org/sdr/U2RA), Oct 4, 2011: SILL. CORRODED. MAIN CABIN, L1 DOOR LOWER SILL HAS CORROSION, APPROX 10 INCHES FROM FORWARD FRAME.
- [SDR U2RA486DHN062](https://openairdocs.org/sdr/U2RA486DHN062), Oct 4, 2011: CUSP WEB. CORRODED. BS 376 AT RBL 66, CUSP HAS CORROSION ON BOTTOM SIDE.
- [SDR U2RA486DHN061](https://openairdocs.org/sdr/U2RA486DHN061), Oct 4, 2011: SKIN. PUNCTURED. AFT CARGO COMPARTMENT, PUNCTURE IN BELLY FUSELAGE SKIN BTW BS 1661 - 1681.5 AT LBL 11, APPROX NR 10 SIZE HOLE.
- [SDR U2RA20110823001](https://openairdocs.org/sdr/U2RA20110823001), Aug 23, 2011: ANGLE. CORRODED. FORWARD CARGO LT BS 508 - 660, TRANSITION ANGLE CORRODED TOP AND BOTTOM.
- [SDR U2RA20110816001](https://openairdocs.org/sdr/U2RA20110816001), Aug 16, 2011: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT, FLOOR SUPPORT, LT SIDE WEB AT FUSELAGE STATION 1530 - 1640, HAS CORROSION ON NUTPLATE UNDER WEB.
- [SDR U2RA486DHN053](https://openairdocs.org/sdr/U2RA486DHN053), Aug 11, 2011: SUPPORT ANGLE. CORRODED. MAIN PASSENGER CABIN, R & R ANGLE BETWEEN STATION BS 1701 - 1702, RT SIDE OF BL 0 DUE TO CORROSION AT FASTENER HOLE.
- [SDR U2RA486DHN057](https://openairdocs.org/sdr/U2RA486DHN057), Aug 11, 2011: FLOOR SUPPORT. CORRODED. AFT CARGO FLOOR SUPPORT "Z" CHANNEL AT STATION 1510 AND LBL10 HAS CORROSION UNDER NUTPLATES.
- [SDR U2RA486DHN056](https://openairdocs.org/sdr/U2RA486DHN056), Aug 11, 2011: FLOOR SUPPORT. CORRODED. AFT CARGO FLOOR SUPPORT "Z" CHANNEL AT STATION BS1490 - 1500 AND LBL 7.55 CORRODED.
- [SDR U2RA486DHN055](https://openairdocs.org/sdr/U2RA486DHN055), Aug 11, 2011: FLOOR SUPPORT. CORRODED. AFT CARGO, RT SIDE FLOOR SUPPORT TO SLANT PANEL AT STATION BS 1200 - BS 1240 HAS CORROSION AROUND FASTENER HOLES.
- [SDR U2RA486DHN054](https://openairdocs.org/sdr/U2RA486DHN054), Aug 11, 2011: FLOOR SUPPORT. CORRODED. AFT CARGO FLOOR SUPPORT "Z" CHANNEL AT STATION BS 1510, RBL 10 HAS CORROSION UNDER NUTPLATES.
- [SDR U2RA486DHN052](https://openairdocs.org/sdr/U2RA486DHN052), Aug 11, 2011: INTERCOSTAL. DAMAGED. FORWARD CARGO COMPARTMENT, INTERCOSTAL BETWEEN FR620 AND FR640 AND BETWEEN S26L AND S27L IS DAMAGED AT FASTENER HOLE. DAMAGE MEASURES 2.75" X 0.75".
- [SDR U2RA486DHN051](https://openairdocs.org/sdr/U2RA486DHN051), Jul 29, 2011: DOOR. GOUGED. AFT CARGO COMPARTMENT DOOR HAS NICK (GOUGE) BETWEEEN FUSELAGE STATION BS1400 AND BS 1420 AND BTW S24R AND S25R.
- [SDR U2RA486DHN050](https://openairdocs.org/sdr/U2RA486DHN050), Jul 28, 2011: FLOORBEAM. DAMAGED. INSPECTION REVEALED THAT THE FLOORBEAM LOCATED AT FUSELAGE STATION 1681 AND LBL 10.5 HAS A HOLE.
- [SDR U2RA486DHN049](https://openairdocs.org/sdr/U2RA486DHN049), Jul 28, 2011: INTERCOSTAL. CRACKED. AFT CARGO CEILING AT FUSELAGE STATION 1320, RBL-44, INSPECTION REVEALED INTERCOSTAL WEB CRACKED. CRACK LENGTH APPROX 2".
- [SDR U2RA486DHN048](https://openairdocs.org/sdr/U2RA486DHN048), Jul 14, 2011: SHEAR WEB. CORRODED. FUSELAGE STA 1683 TO 1705 AT RBL 48, SEVERAL AREAS OF CORROSION ON SHEAR WEB.
- [SDR U2RAA486DHN047](https://openairdocs.org/sdr/U2RAA486DHN047), Jul 11, 2011: CHANNEL. CORRODED. FUSELAGE STA BS1688 TO BS1714 AT BL0, CORROSION ON CENTER HAT CHANNEL IN SEVERAL AREAS.
- [SDR U2RA486DHN046](https://openairdocs.org/sdr/U2RA486DHN046), Jul 11, 2011: FLOORBEAM. CORRODED. REMOVED R4 DOOR SURROUNDING WEB & ATTACHING SUPPORTS FOR FLOORBEAM REPLACEMENT. THRESHOLD WEB - CORRODED OUT OF LIMITS. WEB SUPPORTS, (PN 146N5246-6 & -8) 100 P

All 98: https://openairdocs.org/aircraft/N763CA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (138, 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 (Cirrus Design SR20)

- [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 SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [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 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 SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc
- [STC SA12227IB](https://openairdocs.org/stc/SA12227IB): Installation of the MT-Propeller Entwicklung GmbH MTV-9-B/188-50(). MT-Propeller Entwicklung GmbH
- [STC SA02216SE](https://openairdocs.org/stc/SA02216SE): Removal of mechanical link between engine throttle control and propeller RPM control. Installation of a separate RPM control lever, linkage between Cirrus RPM cable/cam followers, center console to accommodate three-lever configuration, new knobs for all levers, and new installation hardware (nuts, bolts, etc). Skyryse Inc
- [STC SA12064WI](https://openairdocs.org/stc/SA12064WI): Hardware and software updates for the Garmin G1000 Integrated Avionics System. Garmin International Inc
- [STC SA12084BO](https://openairdocs.org/stc/SA12084BO): Installation of the 700-00212-110 and the 700-00212-010 12-inch Vantage Displays Systems with Attitude Reference System and the 700-00236-000 Air Data Computers System. Avidyne Corporation
- [STC SA12080BO](https://openairdocs.org/stc/SA12080BO): Installation of Prodigy model 90901() LED Landing Light. Whelen Aerospace Technologies
- [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. 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 SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02551AK](https://openairdocs.org/stc/SA02551AK): Installation of SKYDISPLAY Aircraft Interface Device (AID). AeroDisplay LLC
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA03303CH](https://openairdocs.org/stc/SA03303CH): Installation of MT propeller model MTV-12-D/188-59(). McFarlane Aviation LLC
- [STC SA04575CH](https://openairdocs.org/stc/SA04575CH): Installation of access panel in accordance with Kelly Aerospace Thermal Systems Installation Manual NC-19-092, revision E, or later FAA approved revision. Kelly Aerospace Thermal Systems LLC
- [STC SA00199BO](https://openairdocs.org/stc/SA00199BO): Installation of Aerox Oxygen System. Aerox Aviation Oxygen Systems 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 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 SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA01170LA](https://openairdocs.org/stc/SA01170LA): : Installation of Sandel Avionics SN3308 Navigation Display Unit in accordance with FAA Approved Sandel Avionics Master Drawing List, Document No. ST8691LA-A-01, Revision "B", dated May 14, 2001, or later FAA approved revision. FAA Approved Airplane Flight Manual Supplement, Document No. ST8691LA-A-09, Revision "N/C", dated June 01, 2001, or later FAA approved revision. Sandel Avionics LLC
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02329AK](https://openairdocs.org/stc/SA02329AK): Installation of a fixed-mounted Max-Viz® Enhanced Vision System (EVS) Model 100 or Model 600 to include a sensor with conformal housing that displays imagery on any FAA-approved monitor with NTSC RS-170 video interface capability. PECO Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA01234WI-D](https://openairdocs.org/stc/SA01234WI-D): Installation of Bendix/King KMH 880 Multi-Hazard Awareness System or Bendix/King KGP 560 General Aviation Enhanced Ground Proximity Warning System (GA-EGPWS). Honeywell International Inc
- [STC SA04449CH](https://openairdocs.org/stc/SA04449CH): Retirement life extension of Cirrus Design Corporation aircraft model SR20 in accordance with FAA approved Master Drawing List, E00002953, Revision E, dated February 26, 2020, or later FAA approved revision. Cirrus Design Corporation
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04112CH](https://openairdocs.org/stc/SA04112CH): Installation of Appareo Systems, LLC Stratus ESG ADS-B transponder. Appareo Systems LLC
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments
- [STC SA00378BO](https://openairdocs.org/stc/SA00378BO): Installation of integrated wingtip exterior light assemblies. Cirrus Design Corporation

All 138: https://openairdocs.org/aircraft/N763CA/stcs.md

## Related

- Other Cirrus Design SR20 aircraft: https://openairdocs.org/model/cirrus-design-sr20/aircraft.md
- The Continental IO-360-ES engine: https://openairdocs.org/engine/continental-io-360-es.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.