# N956WP: 2023 Cirrus Design SR22

- Status: Valid registration
- Airframe: [Cirrus Design SR22](https://openairdocs.org/model/cirrus-design-sr22) (registry code 2130001, 4 seats)
- Engine: [Continental IO-550-N](https://openairdocs.org/engine/continental-io-550-n) (registry code 17215)
- Data sheets: [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH) (Cirrus Design Corporation), [TCDS E3SO](https://openairdocs.org/tcds/E3SO) (Continental Aerospace Technologies, Inc.) (OpenAirDocs)
- Serial number: 9332
- Year built: 2023
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: July 9, 2023
- Certificate issued: September 4, 2023
- Expires: September 30, 2030
- Mode S code: AD4CF3
- Registered owner: [Infinity Aviation LLC](https://openairdocs.org/faa-owner/INFINITY%20AVIATION%20LLC)
- Location: [Comstock, WI](https://openairdocs.org/faa-place/WI/Comstock)
- Owner type: LLC
- Owner's area on the map: 45.4965° N, 92.1768° W: Placed by OpenAirDocs at the center of ZIP code 54826, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=956WP
- Page: https://openairdocs.org/aircraft/N956WP

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): 34 in force

### Matched by airframe (Cirrus Design SR22)

- [AD 2024-24-11](https://openairdocs.org/ad/2024-24-11): Power Lever · Cirrus Design SR20, SR22 and SR22T. Effective Dec 23, 2024
- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 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 2009-26-01](https://openairdocs.org/ad/2009-26-01): Ice and Rain protection · Cirrus Design SR22. Effective Dec 21, 2009
- [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 2008-03-16](https://openairdocs.org/ad/2008-03-16): Rudder, aileron, and rudder-aileron interconnect rigging · Cirrus Design SR20 and SR22. Effective Mar 11, 2008
- [AD 2007-24-13](https://openairdocs.org/ad/2007-24-13): Install a drain hole in the left and right outboard wing tips · Cirrus Design SR22. Effective Dec 4, 2007
- [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-550-N)

- [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 2023-02-12](https://openairdocs.org/ad/2023-02-12): Engine Air Intake System · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Feb 17, 2023
- [AD 2020-16-11](https://openairdocs.org/ad/2020-16-11): SUMMARY: Reciprocating Cylinder Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 23 more. Effective Sep 21, 2020
- [AD 2016-16-12](https://openairdocs.org/ad/2016-16-12): Cylinder assemblies · Continental Motors LTSIO-520-AE, TSIO-520-A, TSIO-520-AE and 89 more. Effective Sep 15, 2016
- [AD 2014-05-29](https://openairdocs.org/ad/2014-05-29): SAP replacement parts manufacturer approval (PMA) investment cast cylinder assemblies · Continental Motors TSIO-520-A, TSIO-520-AE, TSIO-520-AF and 55 more. Effective Apr 25, 2014
- [AD 2012-10-13](https://openairdocs.org/ad/2012-10-13): Starter adapters · Continental Motors IO-550-N, TSIO-520-B, TSIO-520-BB and 14 more. Effective Jun 8, 2012
- [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 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 2007-16-10](https://openairdocs.org/ad/2007-16-10): Kelly Aerospace Power Systems turbochargers · Turbonormalizing system (Engine Technologies STC SE10589SC or SA10588SC). Effective Aug 23, 2007
- [AD 2004-08-10](https://openairdocs.org/ad/2004-08-10): Serial-numbered (SN) cylinders · Modify Teledyne Continental TSIO-520-NB engine (RAM Aircraft Limited Partnership STC SE09104SC or 4 others). Effective May 5, 2004
- [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 99-19-01](https://openairdocs.org/ad/99-19-01): No. 2 and No. 5 Crankshaft Inspections · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Sep 30, 1999
- [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 93-08-17](https://openairdocs.org/ad/93-08-17): Oil Pick-Up Tube · Continental Motors IO-470-A, IO-470-C, IO-470-D and 104 more. Effective Aug 23, 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 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

### 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 2011-25-51](https://openairdocs.org/ad/2011-25-51) (historical): Starter Adapter Gear Shaft · Continental Motors IO-550-N, TSIO-520-B, TSIO-520-BB and 14 more. Effective Dec 28, 2011
- [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 2009-16-03](https://openairdocs.org/ad/2009-16-03) (historical): Cylinder assemblies · Continental Motors IO-520-A, IO-520-B, IO-520-BA and 55 more. Effective Sep 9, 2009
- [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
- [AD 99-09-17](https://openairdocs.org/ad/99-09-17) (historical): Crankshaft · Teledyne Continental Motors IO-470-A, IO-470-C, IO-470-D and 114 more

## Information bulletins (advisory) (28 in force)

- [SAIB AIR-21-05R1](https://openairdocs.org/saib/AIR-21-05R1): Engine Exhaust; Inlet check valves on turbochargers used in the Tornado Alley Turbo, Inc. turbonormalizing systems. Issued Mar 29, 2021
- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-13-43R1](https://openairdocs.org/saib/CE-13-43R1): Aircraft Fuel Distribution System and Ice/Rain Protection System. Issued Sep 30, 2013
- [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-08-46](https://openairdocs.org/saib/CE-08-46): Powerplant Exhaust & Air Conditioning. Issued Sep 9, 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-20-05](https://openairdocs.org/saib/NE-20-05): POWERPLANT - Engine Camshaft Gear Tooth Fracture. Issued Apr 6, 2020
- [SAIB NE-18-16](https://openairdocs.org/saib/NE-18-16): POWERPLANT  Alternator Drive Coupling. Issued Jun 20, 2018
- [SAIB NE-17-11](https://openairdocs.org/saib/NE-17-11): POWERPLANT  Engine damage as a result of kickback. Issued May 10, 2017
- [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 NE-10-07](https://openairdocs.org/saib/NE-10-07): Reciprocating Engine Cylinder: Identification Information for Superior Air Parts, PMA Cylinder Heads for Teledyne Continental Motors (TCM) IO-520, TSIO-520,and IO-550 Series Engines.. Issued Nov 2, 2009
- [SAIB NE-09-08](https://openairdocs.org/saib/NE-09-08): Reciprocating Engine Cylinder Section. Issued Jan 30, 2009
- [SAIB NE-02-41](https://openairdocs.org/saib/NE-02-41): . Issued Aug 8, 2002
- [SAIB AIR-21-05](https://openairdocs.org/saib/AIR-21-05) (historical): Engine Exhaust; Inlet check valves on turbochargers used in the Tornado Alley Turbo, Inc. turbonormalizing systems. Issued Mar 17, 2021
- [SAIB CE-13-43](https://openairdocs.org/saib/CE-13-43) (historical): Aircraft Fuel Distribution System and Ice/Rain Protection System. Issued Aug 30, 2013
- [SAIB CE-08-12](https://openairdocs.org/saib/CE-08-12) (historical): Electrical Power. Issued Feb 27, 2008

## NTSB investigations

None matched to N956WP.

## FAA accident and incident reports

None matched to N956WP.

## 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 N956WP not matched to an aircraft (63, newest 50)

They name N956WP, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR W8PA980035](https://openairdocs.org/sdr/W8PA980035), Jan 30, 1998: LIGHT. DISCONNECTED. DEN- EMERGENCY TRACK LIGHTING AT ROWS 16 TO 19 IS INOP. REINSTALLED TRACK LIGHTING, OPS CHECK NORMAL.
- [SDR W8PA980020](https://openairdocs.org/sdr/W8PA980020), Jan 20, 1998: WIRE. DISCONNECTED. DEN - TWO EMERGENCY TRACK LIGHTS ARE INOP AT ROW 18. RECONNNECTED WIRES, AT ROW 18. OPS CHECK GOOD.
- [SDR W8PA980019](https://openairdocs.org/sdr/W8PA980019), Jan 16, 1998: WIRE. DISCONNECTED. EMERGENCY TRACK LIGHTING IS INOP AT ROWS 20 THROUGH 23. FOUND WIRE DISCONNECTED AT ROW 20. RECONNECTED WIRE, OPS CHECK NORMAL.
- [SDR W8PA980006](https://openairdocs.org/sdr/W8PA980006), Jan 5, 1998: LAMP. FAILED. DEN- EMERGENCY FLOOR TRACK LIGHTING AT ROW 18 IS INOP. RELAMPED, OPS CHECK GOOD.
- [SDR W8PA971553](https://openairdocs.org/sdr/W8PA971553), Dec 25, 1997: PIN. FAILED. EMERGENCY FLOOR TRACK LIGHTING AT ROW 21 IS INOP. REPLACED SOCKET PIN IN THE LIGHT AT ROW 21, OPS CHECK GOOD.
- [SDR W8PA971587](https://openairdocs.org/sdr/W8PA971587), Dec 22, 1997: CONNECTOR. DISCONNECTED. DEN - TRACK LIGHT AT ROW 18 IS INOP. REATTACHED LIGHT, OPS CHECK GOOD.
- [SDR W8PA971529](https://openairdocs.org/sdr/W8PA971529), Dec 16, 1997: LIGHT. LOOSE. DEN- AFT CABIN EMERGENCY FLOOR TRACK LIGHTING IS INOP. RESECURED LIGHT WIRES, OPS CHECK GOOD.
- [SDR W8PA971526](https://openairdocs.org/sdr/W8PA971526), Dec 10, 1997: LAMP. FAILED. DEN - EMERGENCY LIGHTS ARE INOP BETWEEN ROWS 18 AND 16. RELAMPED EMERGENCY LIGHTS BETWEEN ROW 16 AND 18. OPS CHECK GOOD.
- [SDR W8PA971515](https://openairdocs.org/sdr/W8PA971515), Dec 1, 1997: WIRE. DISCONNECTED. DEN- EMERGENCY FLOOR TRACK LIGHTING INOP NEAR OVERWING EXIT. RECONNECTED WIRE AT LIGHT FITTING, OPS CHECK GOOD.
- [SDR W8PA971446](https://openairdocs.org/sdr/W8PA971446), Sep 25, 1997: ENGINE. FAILED. FLT 321 - DEN - ON CLIMB-OUT AT 15000 FT, THE NR 2 ENGINE FAILED WITH A LOUD BANG. N1 AND N2 DECREASED RAPIDLY WITH THE EGT CLIMBING THROUGH 946 C. THE ENGINE W
- [SDR W8PA971368](https://openairdocs.org/sdr/W8PA971368), Jul 24, 1997: CONNECTORS. LOOSE. ROW 17 EMERGENCY TRACK LIGHTING IS INOPERABLE. CONNECTED WIRING CONNECTS AT ROW 17. OPS CHECK GOOD. (X)
- [SDR W8PA971330](https://openairdocs.org/sdr/W8PA971330), Jul 22, 1997: WIRE. LOOSE. EMERGENCY FLOOR TRACK LIGHTING INOPERABLE AT ROW 18. WIRES PULLED FROM LAMP. RECONNECTED WIRES, OPS CHECK GOOD. (X)
- [SDR W8PA971237](https://openairdocs.org/sdr/W8PA971237), Jul 7, 1997: LAMP. FAILED. ROW 12 FLOOR EMERGENCY LIGHT INOPERATIVE. RELAMPED. (X)
- [SDR W8PA971120](https://openairdocs.org/sdr/W8PA971120), Jun 8, 1997: SKIN. DAMAGE. LEFT AILERON UPPER SURFACE HAS PAINT DAMAGE. REMOVED LEFT AILERON AND LEFT AILERON TRIM TAB, PERFORMED BALANCE CHECK OF LEFT AILERON IAW SRM 51-60-01. (M)
- [SDR W8PA970735](https://openairdocs.org/sdr/W8PA970735), Jun 5, 1997: SKIN. CRACKED. FOUND AFT ENTRY DOOR, 2 INCHES BELOW LOWER HINGE CUTOUT, SKIN CRACKED BS 956.5, STRINGER 15L (AFT ENTRY DOORWAY). REMOVED DAMAGED AREA, FABRICATED AND INSTALLED
- [SDR W8PA971036](https://openairdocs.org/sdr/W8PA971036), Jun 2, 1997: HINGE. WORN. NR 1, NR 3 AILERON TAB WING IS WORN. REMOVED AND REPLACED AILERON TAB HINGE PER OHM 57-50-25. (M)
- [SDR W8PA971022](https://openairdocs.org/sdr/W8PA971022), Jun 2, 1997: SKIN. CRACKED. NR 6 SLAT, LOWER SURFACE SKIN (JUST BELOW INBOARD AUX TRACT) 3 FASTENERS EXHIBIT EVIDENCE OF CRACKS EMERGING FROM FASTENER HOLES. REMOVED DAMAGED AREA FROM NR 6
- [SDR W8PA970737](https://openairdocs.org/sdr/W8PA970737), Jun 2, 1997: STRINGER. DAMAGED. COMPLY WITH BSB 737-53-1170, STRINGER 18A WEB AT BS 727, INSPECT, REPAIR AND PREVENTIVE CHANGE. COMPLIED WITH BSB 737-53-1170. (M)
- [SDR W8PA971024](https://openairdocs.org/sdr/W8PA971024), Jun 1, 1997: SKIN. DAMAGED. FUSELAGE SKIN HAS OIL CAN AT BS 1081, RBL 1, WL 207. REMOVED DAMAGED SIN FABRICATED INSTALLED REPAIR DOUBLER PER SRM 52-00-01. (M)
- [SDR W8PA971025](https://openairdocs.org/sdr/W8PA971025), May 31, 1997: SKIN. DENTED. SKIN IS DENTED STATION 1134, WL 208.1 LEFT SIDE (DENT NR 033) A=1.250, Y=0.065, Y=19.23. DENT FOUND TO BE OUT OF LIMITS PER SRM 53-00-01. REMOVED DAMAGED SKIN, 
- [SDR W8PA970669](https://openairdocs.org/sdr/W8PA970669), May 31, 1997: SKIN. DENTED. FOUND SKIN DENTED BS 1088, WI 208.1, LEFT SIDE (DENT NR 034) A=1, Y=.085, A/Y=11.78, DENT FOUND TO BE OUT OF LIMITS PER 737 SRM 53-00-01. DENT OUT OF LIMITS PER
- [SDR W8PA970776](https://openairdocs.org/sdr/W8PA970776), May 30, 1997: PANEL. WORN. RIGHT HORIZONTAL STAB MIDDLE BALANCE BAY PANEL IS CHAFING AND GOUGING WEBS ON INBOARD AND OUTBOARD SIDES. REPAIRED RIGHT STAB MIDDLE BALANCE BAY PANEL PER SRM 5
- [SDR W8PA970774](https://openairdocs.org/sdr/W8PA970774), May 30, 1997: TIP. ERODED. CF811, LEFT STAB TIP HAS EROSION DAMAGE. REPAIRED PER SRM 55-10-30 AND 51-70-14. (M)
- [SDR W8PA970773](https://openairdocs.org/sdr/W8PA970773), May 30, 1997: RIB. WORN. LEFT HORIZONTAL STABILIZER TRAILING EDGE SUPPORT RIB AT ELEVATOR STATION 121.59 HAS SURFACE ABRASION ON OUTBOARD AND INBOARD SURFACES. RAPAIRED SUPPORT RIB PER 
- [SDR W8PA970772](https://openairdocs.org/sdr/W8PA970772), May 30, 1997: RIB. WORN. LEFT HORIZONTAL STABILIZER TRAILING EDGE SUPPORT RIB AT ELEVATOR STATION 149.12 HAS SURFACE ABRASION ON INBOARD SURFACE. REPAIRED SUPPORT RIB PER SRM 55-10-09. 
- [SDR W8PA970771](https://openairdocs.org/sdr/W8PA970771), May 30, 1997: RIB. WORN. LEFT HORIZONTAL STABILIZER TRAILING EDGE SUPPORT RIB AT ELEVATOR STATION 94.07 HAS SURFACE ABRASION ON OUTBOARD AND INBOARD SURFACES. REPAIRED LT HORIZ STAB T-T
- [SDR W8PA970770](https://openairdocs.org/sdr/W8PA970770), May 30, 1997: RIB. WORN. LEFT HORIZONTAL STABILIZER TRAILING EDGE SUPPORT RIB AT ELEVATOR STATION 66.54 HAS SURFACE ABRASION ON OUTBOARD SURFACE. REPAIRED SUPPORT RIB PER SRM 55-10-09. 
- [SDR W8PA970717](https://openairdocs.org/sdr/W8PA970717), May 30, 1997: INTERCOSTAL. BENT. INTERCOSTAL BENT AND ATTACH CLIP CRACKED AT STATION 320, WL 157, RBL 6. FABRICATED AND INSTALLED CLIP ON INTERCOSTAL AT STATION 320, WL 157, RBL 6 PER SRM 51-30
- [SDR W8PA970767](https://openairdocs.org/sdr/W8PA970767), May 29, 1997: DOOR. CORRODED. CORROSION INSIDE OF POTABLE WATER SERVICE DOOR NR 1501 PANEL BS 967. (M)
- [SDR W8PA970758](https://openairdocs.org/sdr/W8PA970758), May 29, 1997: SKIN. BUCKLED. FUSELAGE SKIN IS BUCKLED AT BS 947.5 AT SKIN LAP JUST FORWARD OF WATER SERVICE PANEL. FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED PER SRM 53-00-01. (M)
- [SDR W8PA970766](https://openairdocs.org/sdr/W8PA970766), May 28, 1997: SUPPORT. CORRODED. FOUND CORROSION ON FLOOR TO SIDE WALL SUPPORT AROUND FASTENER HOLES FROM STATION 380 PLUS 10 TO STATION 440 LEFT (CORROSION EXTENDS UNDER FLOOR PANEL AT STA 390
- [SDR W8PA970765](https://openairdocs.org/sdr/W8PA970765), May 28, 1997: SERVICE PANEL. CORRODED. CORROSION ON AFT LAVATORY SERVICE PANEL HINGE (AFT HINGE). REMOVED AND REPLACED HINGE PER SRM 51-40-02. (M)
- [SDR W8PA970764](https://openairdocs.org/sdr/W8PA970764), May 28, 1997: SUPPORT. CORRODED. FLOOR TO SIDE WALL SUPPORT CORRODED AROUND FASTENER HOLE AT STATION 500 PLUS 12 AND 500B PLUS 15 RIGHT. (M)
- [SDR W8PA970763](https://openairdocs.org/sdr/W8PA970763), May 28, 1997: SUPPORT. CORRODED. FLOOR TO SIDE WALL SUPPORT HAS CORROSION AROUND NUTPLATE HOLES AT STATION 400 TO STATION 420 RIGHT. (M)
- [SDR W8PA970762](https://openairdocs.org/sdr/W8PA970762), May 28, 1997: SERVICE PANEL. CORRODED. AFT LAVATORY SERVICE PANEL HAS CORROSION AROUND GROUND STUD. REMOVED AND REPLACED DOOR PER SRM 51-40-02. (M)
- [SDR W8PA970761](https://openairdocs.org/sdr/W8PA970761), May 28, 1997: INTERCOSTAL. CRACKED. AFT CARGO DOOR UPLOCK INTERCOSTAL IS CRACKED (ACCESS REQUIRED) AFT CARGO BAY. INSTALLED AFT CARGO DOOR UPLOCK INTERCOSTAL AS PER SRM 51-10-02, AND SRM 51-40-02.
- [SDR W8PA970760](https://openairdocs.org/sdr/W8PA970760), May 28, 1997: SUPPORT. CORRODED. FLOOR TO SIDE WALL SUPPORT HAS CORROSION AROUND NUTPLATE HOLES FROM STATION 460 TO STATION 500 LEFT. (M)
- [SDR W8PA970759](https://openairdocs.org/sdr/W8PA970759), May 28, 1997: BOLTS. CORRODED. WHILE WORKING FUSELAGE CARD 47 FOUND CORROSION AROUND FIRE BOTTLE MOUNT BOLTS. (M)
- [SDR W8PA970734](https://openairdocs.org/sdr/W8PA970734), May 28, 1997: LINES. KINKED. WHILE WORKING FUSELAGE 47 FOUND TWO KINKED LINE ON AFT FIRE BOTTLE. REMOVED DAMAGED LINES. REINSTALLED NEW LINES PER SRM 51-10-02 AND MM 26-21-11. (M)
- [SDR W8PA9711568](https://openairdocs.org/sdr/W8PA9711568), May 13, 1997: LENS. BROKEN. LENS FOR EMERGENCY TRACK LIGHTING AT ROW 14 NEEDS REPAIR. INSTALLED NEW LENS AT ROW 14. OPS CHECK GOOD. (X)
- [SDR W8PA970186](https://openairdocs.org/sdr/W8PA970186), Apr 18, 1997: CONNECTOR. LOOSE. AFT CABIN EMERGENCY FLOOR TRACK LIGHTING IS INOP. RESECURED CONNECTIONS. (M)
- [SDR W8PA970180](https://openairdocs.org/sdr/W8PA970180), Apr 8, 1997: LAMP. FAILED. EMERGENCY FLOOR TRACK LIGHT AT ROWS 14-18 IS INOP. REPLACED LAMPS. (M)
- [SDR W8PA970127](https://openairdocs.org/sdr/W8PA970127), Mar 30, 1997: LAMP. FAILED. EMERGENCY EXIT LIGHT AT THE RIGHT AFT DOOR IS INOP. REPLACED LAMPS. (M)
- [SDR W8PA970113](https://openairdocs.org/sdr/W8PA970113), Mar 20, 1997: LAMP. FAILED. EMERGENCY FLOOR TRACK LIGHT INOP AT ROW 18. REPLACED LAMP. (M)
- [SDR W8PA970070](https://openairdocs.org/sdr/W8PA970070), Feb 28, 1997: LAMP. FAILED. LEFT LOWER EMERGENCY LIGHT INOP. REPLACED LAMP. (M)
- [SDR W8PA970060](https://openairdocs.org/sdr/W8PA970060), Feb 18, 1997: LIGHT COVER. MISSING. FOUND EMERGENCY TRACK LIGHT COVER MISSING AT ROW 18. INSTALLED LIGHT COVER. (M)
- [SDR W8PA970057](https://openairdocs.org/sdr/W8PA970057), Feb 16, 1997: LIGHT. INOPERATIVE. FOUND EMERGENCY TRACK LIGHT INOP AT ROWS 19-21. RECONNECTED LIGHT SOCKET AT ROW 21. (M)
- [SDR W8PA970017](https://openairdocs.org/sdr/W8PA970017), Feb 6, 1997: LIGHT. INOPERATIVE. FOUND EMERGENCY TRACK LIGHT INOP AT ROWS 19-21. RECONNECTED LIGHT SOCKET AT ROW 21. (M)
- [SDR W8PA960172](https://openairdocs.org/sdr/W8PA960172), Dec 8, 1996: WIRE. LOOSE. FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROWS 1 AND 2, FIRST THREE LIGHTS. RECONNECTED PINS TO LIGHT SOCKETS. REPLACED BROKEN WIRE. (M)
- [SDR W8PA960175](https://openairdocs.org/sdr/W8PA960175), Nov 30, 1996: WIRE. LOOSE. FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROWS 4, 5, AND 6. RECONNECTED LOOSE WIRE TO LIGHT SOCKETS. (M)

All 63: https://openairdocs.org/aircraft/N956WP/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (147, 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 SR22)

- [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 SA12273IB](https://openairdocs.org/stc/SA12273IB): Installation of the MT-Propeller Entwicklung GmbH MTV-9-D/198-52() propeller. 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 SA12027IB](https://openairdocs.org/stc/SA12027IB): Installation of the MT-Propeller Entwicklung GmbH MTV-14-D/195-30() propeller. MT-Propeller Entwicklung GmbH
- [STC SA02558CH](https://openairdocs.org/stc/SA02558CH): Installation of a L-3 Communications Avionics Systems SmartDeck Flight Guidance and Display System. Acron Aviation Inc
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA02924CH](https://openairdocs.org/stc/SA02924CH): Installation of M-T Propeller model MTV-14-D/195-30( ) 4 bladed propeller. McFarlane Aviation LLC
- [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 SA10532SC](https://openairdocs.org/stc/SA10532SC): Installation of XM Satellite Radio Wireless equipment. Heads Up Technologies Inc
- [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 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 SA04468CH](https://openairdocs.org/stc/SA04468CH): Installation of Hartzell Propeller model 4C1-F650A1/76C04-0.6 or 4C1-F650A1/76C04B-0.6 i. Hartzell Propeller 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 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 SA10195SC](https://openairdocs.org/stc/SA10195SC): Installation of an engine driven vapor cycle air conditioning system. Air Comm 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

All 147: https://openairdocs.org/aircraft/N956WP/stcs.md

## Related

- Other Cirrus Design SR22 aircraft: https://openairdocs.org/model/cirrus-design-sr22/aircraft.md
- The Continental IO-550-N engine: https://openairdocs.org/engine/continental-io-550-n.md

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