# N828EX: 2013 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: 3927
- Year built: 2013
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: March 21, 2013
- Certificate issued: April 29, 2022
- Expires: April 30, 2029
- Mode S code: AB4F0D
- Registered owner: [Horizon Strategies Aviation LLC](https://openairdocs.org/faa-owner/HORIZON%20STRATEGIES%20AVIATION%20LLC)
- Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover)
- Owner type: LLC
- Owner's area on the map: 39.1815° N, 75.4736° W: Placed by OpenAirDocs at the center of ZIP code 19901, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=828EX
- Page: https://openairdocs.org/aircraft/N828EX

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 N828EX.

## FAA accident and incident reports

None matched to N828EX.

## Reports on N828EX not matched to an aircraft (1)

They name N828EX, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20040112002249I](https://openairdocs.org/incident/20040112002249I), Jan 12, 2004: Dhav DHC8102 (N828EX), State College, PA. (-23) After takeoff crew retracted flaps. #1 hydraulic (hyd) pressure went to zero with the hyd engine pump #1 caution light and all associated #1 hyd pressure…

## 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 N828EX not matched to an aircraft (29)

They name N828EX, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR HNAA2009062500203](https://openairdocs.org/sdr/HNAA2009062500203), Jun 20, 2009: LINE. LEAKING. LOSS OF NR 1 HYD SYS QTY ENROUTE. NR1 ISO VALVE CL ILLUMINATED AND SYS AT .4 QT AT SHUTDOWN. SERVICED NR 1 HYD SYS. RAN ACFT AND INSPECTED FOR LEAK. NOTED LEAK 
- [SDR HNAA2009010900384](https://openairdocs.org/sdr/HNAA2009010900384), Sep 25, 2008: SEAT TRACK. CORRODED. DURING C-CHECK, SEVERAL AREAS OF CORROSION WERE FOUND ON THE LT OTBD SEAT RAIL. THE SEAT RAIL WAS R&R.
- [SDR HNA2008F00002](https://openairdocs.org/sdr/HNA2008F00002), Jun 29, 2008: RADAR. FAILED. RADAR SPIKES RADAR FAILED ENROUTE TO FLO. THUNDERSTORM ACTIVITY WAS AHEAD OF THE FLIGHT. DISPATCHER AND CAPTAIN CHOSE TO HAVE FLIGHT RETURN. REMOVED AND REPLACE
- [SDR HNA2008F00001](https://openairdocs.org/sdr/HNA2008F00001), Jun 29, 2008: TRANSCEIVER. FAILED. RADAR SPIKES, RADAR FAILED ENROUTE, THUNDERSTORM ACTIVITY WAS AHEAD OF THE FLIGHT. DISPATCHER AND CAPTAIN CHOSE TO HAVE FLIGHT RETURN. REMOVED AND REPLACED RADA
- [SDR HNA2008F00000](https://openairdocs.org/sdr/HNA2008F00000), Jun 29, 2008: TRANSMITTER. FAILED. LOG PAGE 269950-2. RADAR SHOWS FAULT MESSAGES "STAB OFF" AND "IN FIT 6" IN FLIGHT. REMOVED AND REPLACED WEATHER RADAR TRANSMITTER UNIT. (K)
- [SDR HNAA0800031](https://openairdocs.org/sdr/HNAA0800031), Jan 9, 2008: PCU. DEFECTIVE. NR 2 PROPELLER FLUX OF 20 RPM ASSOCIATED WITH TORQUE FLUX OF 6%, RETURNED TO FIELD, PROPELLER SYNC OFF AT TIME OF FLUX, CYCLED PROPELLER SYNC DURING FINAL AND S
- [SDR HNAA0700243](https://openairdocs.org/sdr/HNAA0700243), Oct 18, 2007: PANEL. CORRODED. THE LEFT HAND WING PANEL 522AT WAS FOUND TO HAVE PITTING DAMAGE FROM CORROSION. REPLACED THE PANEL WITH A NEW PART FROM STORES.
- [SDR HNAA0700242](https://openairdocs.org/sdr/HNAA0700242), Oct 18, 2007: PLATE. CRACKED. CRACK AT FORWARD INBOARD CORNER OF LADDER PLATE ON PANEL 522AT WAS FOUND DURING INSPECTION. REPAIRED IAW EO 8-57-07-0242.
- [SDR HNAA0600119](https://openairdocs.org/sdr/HNAA0600119), Oct 2, 2006: GARLOCK SEAL. LEAKING. DURING CLIMBOUT AND CRUISE FLIGHT THE NR 2 ENGINE OIL PRESSURE SHOWED RAPID FLUCUATION AND DECREASE IN PRESSURE, CREW VERIFIED OIL LEAK FROM NR 2 NACELLE IN FLI
- [SDR HNAA0600111](https://openairdocs.org/sdr/HNAA0600111), Sep 6, 2006: CONNECTOR. LOOSE. NOSE GEAR UNSAFE AND GEAR HANDLE LIGHTS ILLUMINATED FOLLOWED BY GEARS CYCLING DOWN AND UP ONE TIME. FOUND LOOSE CONNECTOR PLUG IN RT GEAR WHEEL WELL FOR WOW SEN
- [SDR HNAA0500108](https://openairdocs.org/sdr/HNAA0500108), Dec 29, 2005: GENERATOR. LEAKING. RIGHT AC BUSS CAUTION LIGHT ILLUMINATED IN FLIGHT. REMOVED CONNECTOR FROM GENERATOR AND FOUND OIL IN CONNECTOR. REMOVED AND REPLACED AC GENERATOR.
- [SDR HNAA0400120](https://openairdocs.org/sdr/HNAA0400120), Sep 2, 2004: MOUNT. BROKEN. FLIGHT 4079 REPORTED A PROP VIBRATION DURING CLIMB, CRUISE, DESCENT WITH PROPS AT 900 RPM. MAINTENANCE FOUND THE RIGHT HAND INBOARD REAR MOUNT STRUT TO BE AT FA
- [SDR HNAA0407102](https://openairdocs.org/sdr/HNAA0407102), Jul 20, 2004: APU. VIBRATES. FLIGHT 4097 REPORTED THE APU VIBRATING THE WHOLE AIRCRAFT WITH AN ASSOCIATED BURNING SMELL IN THE AFT CABIN AREA. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE A
- [SDR PCAA0312151](https://openairdocs.org/sdr/PCAA0312151), Dec 17, 2003: ROLLER. DIRTY. FLIGHT 3972, CLEVELAND, MAIN PASSENGER DOOR WAS VERY DIFFICULT TO OPEN REPORTED THE FLIGHT ATTENDANT. BLEEDS WERE OFF. ASSISTANCE WAS NEEDED TO GET THE DOOR OPE
- [SDR PCAA0311135](https://openairdocs.org/sdr/PCAA0311135), Nov 2, 2003: SILL. GOUGED. WHILE IN ROUTINE MAINTENANCE, IT WAS DISCOVEERED THE BAG DOOR HANDLE HAD GOUGED THE UPPER BAG DOOR SILL ON AIRFRAME IN TWO PLACES. MAINTENANCE REPAIRED UPPER SI
- [SDR PCAA0308101](https://openairdocs.org/sdr/PCAA0308101), Aug 21, 2003: STRUT. BROKEN. DURING AN -A- LEVEL INSPECTION, THE RT ENGINE INBOARD AFT HORIZONTAL MOUNT STRUT ASSY WAS FOUND TO BE BROKEN. THE AFT HORIZONTAL MOUNT STRUT ASSY WAS REPLACED, 
- [SDR PCAA0301008](https://openairdocs.org/sdr/PCAA0301008), Jan 7, 2003: HAND RAIL. BROKEN. HAND RAIL STRUT ON RIGHT SIDE OF AIRSTAIR DOOR FOUND BROKEN. DOOR WOULD NOT OPEN. AIRSTAIR DOOR HAND RAIL SUPPORT STRUT REPLACED IN ACCORDANCE WITH DEHAVILLAND 
- [SDR PCAA0111158](https://openairdocs.org/sdr/PCAA0111158), Oct 31, 2001: PIN. WORN. DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, FOUND NOSE GEAR PISTON CAP PIN WORN.REPLACED NOSE GEAR SHOCK STRUT PISTON CAP PIN I
- [SDR PCAA0107073](https://openairdocs.org/sdr/PCAA0107073), Jul 17, 2001: HYDRAULIC SYSTEM. LOW. SYR FLIGHT 3800. CREW REPORTED A MOMENTARY LOSS OF NORMAL BRAKING AFTER LANDING. ALSO NR 1 HYDRAULIC ISOLATION CAUTION LIGHT ILLUMINATED FOR 2 TO 3 SECONDS. MAI
- [SDR PCAA0008052](https://openairdocs.org/sdr/PCAA0008052), Aug 4, 2000: STRUCTURE. CRACKED. MDT - DURING A SPOT INSPECTION, THE REAR FUSELAGE STRUCTURE WAS FOUND CRACKED AT FRAME 4 STRINGER 4, BOTH SIDES. REPAIRS WERE MADE IAW RD8-55-199. AIRCRAFT WAS 
- [SDR PCAA9900064](https://openairdocs.org/sdr/PCAA9900064), Dec 24, 1999: CABLE. KINKED. FLIGHT 3715- UPON ARRIVAL INTO BOS THE CREW COULD NOT OPEN THE PASSENGER DOOR. PASSENGERS WERE DEPLANED THROUGH THE RIGHT FORWARD EMERGENCY EXIT. MAINTENANCE IN
- [SDR PCAA9800783](https://openairdocs.org/sdr/PCAA9800783), Sep 9, 1998: TRANSMITTER. FAILED. AFTER TAKEOFF FROM SYR, THE NR 2 ENGINE OIL PRESSURE INDICATED 100 PSI. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM, 
- [SDR PCAA9800762](https://openairdocs.org/sdr/PCAA9800762), Mar 16, 1998: BULB. FAILED. ONE LIGHT INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M)
- [SDR PCAA9700619](https://openairdocs.org/sdr/PCAA9700619), Nov 16, 1997: BATTERY. DISCHARGED. LEFT CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTING SYSTEM POWER SUPPLY AT POSITION NR 600. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVI
- [SDR PCAA9700535](https://openairdocs.org/sdr/PCAA9700535), Sep 3, 1997: BULB. FAILED. LEFT AFT EXTERIOR EMERGENCY LIGHT DIM. REMOVED AND REPLACED LAMP. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR PCAA9700525](https://openairdocs.org/sdr/PCAA9700525), Aug 26, 1997: ENGINE. LOST POWER. LOST POWER ON NR 2 ENGINE AFTER TAKEOFF FROM PHL, THE ENGINE WAS SHUTDOWN AND THE A/C RETURNED TO FIELD. LANDED WITHOUT INCIDENT. MX INSPECTED NR 2 ENGINE AND R
- [SDR PCAA9700520](https://openairdocs.org/sdr/PCAA9700520), Aug 19, 1997: BULB. FAILED. SECOND EMERGENCY LIGHT IN FLOOR PATH INOP. REMOVED AND REPLACED BULB OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR PCAA9700474](https://openairdocs.org/sdr/PCAA9700474), Jul 6, 1997: LAMP. FAILED. AFT ISLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. ACTC: 7,916. (X)
- [SDR PCAA9700467](https://openairdocs.org/sdr/PCAA9700467), Jul 2, 1997: LAMP. FAILED. ONE CENTER AISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. ACTC: 7,881. (X)

## 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/N828EX/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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