# N812ME: 2002 Cessna 550

- Status: Valid registration
- Airframe: [Cessna 550](https://openairdocs.org/model/cessna-550) (registry code 2076604, 8 seats)
- Engine: [Pratt & Whitney Canada 530A](https://openairdocs.org/engine/pratt-whitney-canada-530a) (registry code 52153)
- Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE) (Textron Aviation Inc.) (OpenAirDocs)
- Serial number: 550-1023
- Year built: 2002
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 29, 2016
- Certificate issued: December 27, 2023
- Expires: December 31, 2030
- Mode S code: AB11E2
- Registered owner: [Big Blue Sky Aviation Co](https://openairdocs.org/faa-owner/BIG%20BLUE%20SKY%20AVIATION%20CO)
- Location: [Midland, TX](https://openairdocs.org/faa-place/TX/Midland)
- Owner type: Corporation
- Owner's area on the map: 31.9973° N, 102.0779° W: Placed by OpenAirDocs: center of Midland, TX, 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=812ME
- Page: https://openairdocs.org/aircraft/N812ME

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 (Cessna 550)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-07-01](https://openairdocs.org/ad/2025-07-01): Air Data Computer · Synthetic Vision Electronic Flight Information System (Arrow STC SR09595RC or ST01523WI). Effective May 15, 2025
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2015-17-12](https://openairdocs.org/ad/2015-17-12): Air conditioning · Freon air conditioning system (Textron STC SA3849SW or 3 others). Effective Sep 29, 2015
- [AD 2013-09-11](https://openairdocs.org/ad/2013-09-11): Air Conditioning · Cessna 500, 501, 550 and 5 more. Effective Jul 5, 2013
- [AD 2007-11-17](https://openairdocs.org/ad/2007-11-17): Wires for the positive and negative terminal studs of the engine and/or auxiliary power unit (APU) fire extinguishing bottles. · Cessna 500, 501, 550 and 5 more. Effective Jul 6, 2007
- [AD 2006-19-04](https://openairdocs.org/ad/2006-19-04): Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 more. Effective Oct 17, 2006
- [AD 2006-06-03](https://openairdocs.org/ad/2006-06-03): Airplane flight manual (AFM) · Cessna 500, 501, 550 and 3 more. Effective Apr 20, 2006
- [AD 2004-08-15](https://openairdocs.org/ad/2004-08-15): TAWS8000 terrain awareness warning systems (TAWS) · Cessna 421, 500, 501 and 18 more. Effective Jun 7, 2004
- [AD 2004-09-05](https://openairdocs.org/ad/2004-09-05): Brake Stator Disks · Cessna 500, 501, 550 and 1 more. Effective Jun 2, 2004
- [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001
- [AD 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001
- [AD 97-05-03 R1](https://openairdocs.org/ad/97-05-03-R1): Global Positioning Systems · BAE Systems Avro 146-RJ100A, BAe 146-200A, Jetstream Model 4101 and 27 more. Effective Apr 20, 1999
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 98-04-38](https://openairdocs.org/ad/98-04-38): AFM - Limitations Section - Icing · Cessna 500, 501, 550 and 2 more. Effective Mar 25, 1998
- [AD 95-25-10](https://openairdocs.org/ad/95-25-10): Outflow/Safety Valve · Cessna 441, 500, 550 and 1 more. Effective Jan 22, 1996
- [AD 95-22-01](https://openairdocs.org/ad/95-22-01): Fluorescent Lighting System · Aerospace Lighting Fluorescent lighting systems, A310-203, A310-204 and 74 more. Effective Dec 4, 1995
- [AD 94-19-06](https://openairdocs.org/ad/94-19-06): Crew Oxygen Masks · 328 Support Services 328-100, 328-300, 500 and 17 more. Effective Oct 6, 1994
- [AD 94-01-04](https://openairdocs.org/ad/94-01-04): Traffic Alert and Collision Avoidance System · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 136 more. Effective Feb 4, 1994
- [AD 93-05-15](https://openairdocs.org/ad/93-05-15): Thrust Reverser Throttle Load Limiter · Cessna 500, 501, 550 and 4 more. Effective Apr 23, 1993
- [AD 90-07-10 R1](https://openairdocs.org/ad/90-07-10-R1): Air Conditioning System · Cessna 550, 551 and S550 with STC SA2698SW. Effective May 29, 1990
- [AD 90-06-13](https://openairdocs.org/ad/90-06-13): Vertical Gyro · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 14 more. Effective Mar 30, 1990
- [AD 89-16-10](https://openairdocs.org/ad/89-16-10): Fuel Flow Transmitter · Cessna 550 and 551. Effective Sep 7, 1989
- [AD 88-06-02](https://openairdocs.org/ad/88-06-02): Electrical Power · Cessna 550 and S550. Effective May 10, 1988
- [AD 80-09-09](https://openairdocs.org/ad/80-09-09): Dual Flight Director Installation · Cessna 500, 501, 550 and 1 more. Effective May 12, 1980
- [AD 79-12-06](https://openairdocs.org/ad/79-12-06): Upper & Lower Spar Cap Stems · Cessna 500, 501, 550 and 1 more. Effective Apr 10, 1980

### Matched by engine (Pratt & Whitney Canada 530A)

None in force.

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

- [AD 2006-04-10](https://openairdocs.org/ad/2006-04-10) (historical): Identification sleeves · Cessna Aircraft Company, The 500, 550, 560 and 3 more. Effective Mar 24, 2006

## Information bulletins (advisory) (5 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB NM-14-08](https://openairdocs.org/saib/NM-14-08): Fuselage: Aerodynamic Fairings. Issued Jan 23, 2014
- [SAIB CE-12-19](https://openairdocs.org/saib/CE-12-19): Fuel: Aircraft Fuel System on Cessna Model 500/501/550 Airplanes. Issued Mar 1, 2012
- [SAIB CE-10-49R1](https://openairdocs.org/saib/CE-10-49R1): Equipment/Furnishings Drain Mast Heater. Issued Jan 5, 2011
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021
- [SAIB CE-10-49](https://openairdocs.org/saib/CE-10-49) (historical): Equipment/Furnishings Drain Mast Heater. Issued Sep 23, 2010

## NTSB investigations

None matched to N812ME.

## FAA accident and incident reports

None matched to N812ME.

## 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 N812ME not matched to an aircraft (163, newest 50)

They name N812ME, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR MWEA070254](https://openairdocs.org/sdr/MWEA070254), Oct 17, 2007: HANDLE. FAILED. LEFT FIRE HANDLE DOES NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED FIRE HANDLE ASSEMBLY.
- [SDR MWEA070253](https://openairdocs.org/sdr/MWEA070253), Oct 17, 2007: ATTACH ANGLE. DAMAGED. LEFT DORSAL FIN ATTACH ANGLE HAS FASTENER HEAD PULLED THROUGH ANGLE, FRAME STATION 1439.9. REMOVED FASTENER, FABRICATED AND INSTALLED ANGLE.
- [SDR MWEA070252](https://openairdocs.org/sdr/MWEA070252), Oct 16, 2007: STIFFENER. CORRODED. STIFFENER CORRODED ON CANTED BULKHEAD FRAME STATION 1431 LEFT ADJACENT TO STRINGER 11 LEFT. REMOVED STIFFENER AT CANTED BULKHEAD, FABRICATED AND INSTALLED STIFF
- [SDR MWEA070251](https://openairdocs.org/sdr/MWEA070251), Oct 14, 2007: FASTENER. MISSING. LEFT ENGINE THRUST REVERSER, BOTH LEFT AND RIGHT STANGS ARE MISSING RIVETS AT THE TIP. INSTALLED FASTENERS.
- [SDR MWEA070245](https://openairdocs.org/sdr/MWEA070245), Oct 12, 2007: ANGLE. CRACKED. FORWARD CARGO DOOR HAS A CRACK ON THE OUTER PAN RADIUS AT UPPER FORWARD AREA 1.25 INCHES LONG. FABRICATED AND INSTALLED ANGLE.
- [SDR MWEA070244](https://openairdocs.org/sdr/MWEA070244), Oct 12, 2007: BLOCK. CORRODED. CORROSION ON FRAME TO STRINGER TIE RADIUS BLOCKS AT CANTED FRAME STATION 1446 AT STRINGER 12 LEFT & 14 LEFT. REMOVED DAMAGE, FABRICATED AND INSTALLED RADIUS BLO
- [SDR MWEA070186](https://openairdocs.org/sdr/MWEA070186), Aug 21, 2007: CONNECTOR. DISCONNECTED. SEAT 6 A/B OXYGEN MASK DOOR DID NOT OPEN WHEN THE OXYGEN SYSTEM SWITCH WAS ACTIVATED. CONNECTED PSU CONNECTOR.
- [SDR MWEA070067](https://openairdocs.org/sdr/MWEA070067), Mar 29, 2007: BATTERY. INOPERATIVE. FORWARD EMERGENCY FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED BATTERY.
- [SDR MWEA060305](https://openairdocs.org/sdr/MWEA060305), Dec 22, 2006: SYMBOL GENERATOR. DEFECTIVE. NR 2 SYMBOL GENERATOR CIRCUIT BREAKER D-12 POPPED. REMOVED & REPLACED SYMBOL GENERATOR.
- [SDR MWEA060288](https://openairdocs.org/sdr/MWEA060288), Oct 28, 2006: DOOR FRAME. CORRODED. FORWARD CARGO DOOR FRAME CORRODED ON THE OUTER SURFACE, LOCATED AT THE AFT LOWER STOP FITTING. FABRICATED AND INSTALLLED DOUBLER.
- [SDR MWEA060287](https://openairdocs.org/sdr/MWEA060287), Oct 28, 2006: DOOR FRAME. CORRODED. FORWARD CARGO DOOR FRAME CORRODED ON THE OUTER SURFACE, LOCATED AT THE FORWARD, LOWER STOP FITTING. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA060283](https://openairdocs.org/sdr/MWEA060283), Oct 26, 2006: WEB. CORRODED. CORROSION ON DOOR CUTOUT LONGERON 28 VERTICAL WEB OUTBOARD FACE (THRESHOLD ATTACH) Y 1160-1206 X -16 AFT CARGO PIT. FABRICATED AND INSTALLED WEB.
- [SDR MWEA060279](https://openairdocs.org/sdr/MWEA060279), Oct 25, 2006: BOLT. CHAFED. LEFT UPPER FORWARD ENGINE MOUNT BOLT HAS CHAFED MARKED AT MID AREA SHAFT.
- [SDR MWEA060278](https://openairdocs.org/sdr/MWEA060278), Oct 25, 2006: BOLT. GOUGED. NUMBER ONE ENGINE LOWER YOKE ATTACH BOLT GOUGED.
- [SDR MWEA060277](https://openairdocs.org/sdr/MWEA060277), Oct 24, 2006: MOUNT. CORRODED. RIGHT UPPER FORWARD ENGINE MOUNT YOKE INNER CUP HAS CORROSION AT THE 7 TO 9 O'CLOCK POSITION.
- [SDR MWEA060281](https://openairdocs.org/sdr/MWEA060281), Oct 23, 2006: BOLT. CHAFED. RIGHT LOWER FORWARD ENGINE MOUNT BOLT IS CHAFED. MARKS AT MID AREA OF SHAFT.
- [SDR MWEA060280](https://openairdocs.org/sdr/MWEA060280), Oct 23, 2006: BOLT. CORRODED. RIGHT UPPER FORWARD ENGINE MOUNT BOLT HAS CORROSION ON SHAFT.
- [SDR MWEA060274](https://openairdocs.org/sdr/MWEA060274), Oct 23, 2006: WEDGE. DAMAGED. FOUND DAMAGED FASTENER HOLES, RIGHT ELEVATOR OUTBOARD, TRAILING EDGE WEDGE.
- [SDR MWEA060273](https://openairdocs.org/sdr/MWEA060273), Oct 21, 2006: STOP FITTING. CORRODED. FOUND MID CARGO DOOR STOP FITTING NR 12 IS CORRODED.
- [SDR MWEA060244](https://openairdocs.org/sdr/MWEA060244), Oct 19, 2006: SUPPORT ANGLE. CORRODED. THRESHOLD INBOARD SUPPORT ANGLE UPPER SURFACE, Y 11 55 X 8, AFT CARGO BAY IS CORRODED.
- [SDR MWEA060245](https://openairdocs.org/sdr/MWEA060245), Oct 18, 2006: SHEAR TIE. CORRODED. CORROSION ON FRAME LOWER SKIN ATTACH ANGLE Y 655 X + 2 BETWEEN LONGERON 30 AND 29 LEFT CENTER CARGO BAY.
- [SDR MWEA060243](https://openairdocs.org/sdr/MWEA060243), Oct 18, 2006: STOP FITTING. CORRODED. AFT CARGO DOOR LOWER STOP FITTINGS 13 & 14 HAVE SURFACE CORROSION.
- [SDR MWEA060242](https://openairdocs.org/sdr/MWEA060242), Oct 16, 2006: SKIN. DELAMINATED. RIGHT WING INBOARD TRAILING EGDE FLAP, OUTBOARD FIXED VANE DELAMINATED 18 - 22 INCHES FROM END, TOP SURFACE.
- [SDR MWEA060236](https://openairdocs.org/sdr/MWEA060236), Oct 15, 2006: WEB. CORRODED. FOUND CORROSION ON DOOR CUT OUT LONGERON 28 VERTICAL WEB, OUTBOARD FACE Y 1160-1206 X-16 AFT CARGO PIT.
- [SDR MWEA060237](https://openairdocs.org/sdr/MWEA060237), Oct 14, 2006: FRAME. CRACKED. FOUND CRACK IN FRAME AT STATION 1463 RIGHT BELOW LONGERON 17 RIGHT.
- [SDR MWEA060239](https://openairdocs.org/sdr/MWEA060239), Oct 13, 2006: SUPPORT. CHAFED. FOUND CORROSION ON DOOR CUT OUT THRESHOLD SUPPORT VERTICAL WEB, LONGERON 28 RIGHT, Y 640-690 X-15 CENTER.
- [SDR MWEA060234](https://openairdocs.org/sdr/MWEA060234), Oct 10, 2006: DOOR FRAME. CORRODED. FORWARD CARGO DOOR FRAME CORRODED ON THE OUTER SURFACE, LOCATED AT THE LOWER STOP FITTING.
- [SDR MWEA060233](https://openairdocs.org/sdr/MWEA060233), Oct 10, 2006: DOOR FRAME. CORRODED. FORWARD CARGO DOOR FRAME CORRODED ON THE OUTER SURFACE, LOCATED AT THE FORWARD LOWER STOP FITTING.
- [SDR MWEA060228](https://openairdocs.org/sdr/MWEA060228), Oct 9, 2006: BRACKET. CORRODED. AFT CARGO BAY, UPPER SURFACE OF FORWARD BRACKET AT ANGLE TO BEAM HAS CORROSION ABOVE DOOR CUT OUT Y STATION = 1169, Z = 7 X =58. FABRICATED AND INSTALLED DOUBLE
- [SDR MWEA060229](https://openairdocs.org/sdr/MWEA060229), Oct 9, 2006: BEAM. CORRODED. AFT CARGO BAY, UPPER SURFACE OF BEAM HAS CORROSION ABOVE DOOR CUT OUT, Y STA = 1177, Z=7, X=58. --
- [SDR MWEA060227](https://openairdocs.org/sdr/MWEA060227), Oct 9, 2006: LONGERON. CORRODED. LONGERON 28 LT AT FASTENER ATTACH AREA FRAME AT Y 730-769, X-14.
- [SDR MWEA060226](https://openairdocs.org/sdr/MWEA060226), Oct 9, 2006: LONGERON. CORRODED. CORROSION ON LONGERON 28 RT AND AT FASTENER ATTACH AREA FRAME AT Y 712-750,X-14.
- [SDR MWEA060223](https://openairdocs.org/sdr/MWEA060223), Oct 6, 2006: ATTACH ANGLE. CORRODED. CORROSION ON LOWER FRAME ANGLE LONGERON ATTACH Y 731 X=10 TO X-15, BETWEEN LONGERON 29 LEFT AND 28 RIGHT CENTER CARGO BAY.
- [SDR MWEA060221](https://openairdocs.org/sdr/MWEA060221), Oct 6, 2006: WEB. CORRODED. CORROSION ON AFT CARGO DOOR CUT OUT UPPER WEB AREA, LONGERON 19 X -58Y 1170-1190Z-6 UPPER SURFACE.
- [SDR MWEA060235](https://openairdocs.org/sdr/MWEA060235), Oct 5, 2006: ATTACH ANGLE. CORRODED. CORROSION FOUND ON FRAME, LOWER SKIN ATTACH ANGLE, Y 674 X + 2, BETWEEN LONGERON 30 AND 29 LEFT CENTER CARGO BAY. FABRICATED AND INSTALLED LOWER SKIN ATTACH ANG
- [SDR MWEA060220](https://openairdocs.org/sdr/MWEA060220), Oct 4, 2006: FRAME. CORRODED. CORROSION ON FRAME AT LONGERON 30 ATTACHMENT Y 11, 17 X-2 TO X-2.
- [SDR MWEA070016](https://openairdocs.org/sdr/MWEA070016), Sep 22, 2006: WIRE. DAMAGED. EMERGENCY FLOOR TRACK LIGHT AT ROW 1 IS INOPERATIVE. SPLICED WIRES FOR FLOOR TRACK LIGHT AT ROW 1.
- [SDR MWEA060192](https://openairdocs.org/sdr/MWEA060192), Sep 4, 2006: SKIN. LIGHTNING STRIKE. NUMBER 2 LIGHTNING STRIKE ON LEFT ELEVATOR TOP SIDE RIVET. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA060168](https://openairdocs.org/sdr/MWEA060168), Aug 16, 2006: LAMP. INOPERATIVE. THE RED SECTION OF EMERGENCY FLOOR TRACK LIGHTS ARE INOPERATIVE, RELAMPED.
- [SDR MWEA060044](https://openairdocs.org/sdr/MWEA060044), Apr 25, 2006: INDICATOR. INOPERATIVE. HEADINGS DRIFTED 10 DEGREES APART. CAPTAINS COMPASS TRACKING INDICATOR DOES NOT SHOW ANY MOVEMENT. REMOVED AND REPLACED CAPTAINS REMOTE MAGNETIC INDICATOR.
- [SDR MWEA050113](https://openairdocs.org/sdr/MWEA050113), Oct 6, 2005: SILL. CORRODED. FORWARD CARGO DOOR SILL HAS MODERATE CORROSION. BLENDED CORROSION.
- [SDR MWEA050112](https://openairdocs.org/sdr/MWEA050112), Oct 6, 2005: STATIC WICK. LIGHTNING STRIKE. RIGHT HORIZONTAL OUTBAORD TRAILING EDGE STATIC WICK MOUNTING BASE HAS LIGHTNING STRIKE DAMAGE. REMOVED AND REPLACED STATIC WICK.
- [SDR MWEA050111](https://openairdocs.org/sdr/MWEA050111), Oct 6, 2005: RUB STRIP. CRACKED. LEFT AILERON INBOARD HINGE RUBSTRIP IS CRACKED. FABRICATED AND INSTALLED FILLER.
- [SDR MWEA050110](https://openairdocs.org/sdr/MWEA050110), Oct 6, 2005: SKIN. CRACKED. LEFT OUTBOARD FLAP AT STATION 262, UPPER SKIN IS CRACKED. FABRICATED AND INSTALLED DOULBER.
- [SDR MWEA050109](https://openairdocs.org/sdr/MWEA050109), Oct 6, 2005: DOUBLER. DENTED. SLAT HORN ON THE LEFT WING HAS A DENT. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA050020](https://openairdocs.org/sdr/MWEA050020), Feb 4, 2005: MEGAPHONE. INOPERATIVE. MEGAPHONE FOUND INOPERATIVE DURING CABIN CHECK. INSTALLED SERVICEABLE MEGAPHONE.
- [SDR MWEA050012](https://openairdocs.org/sdr/MWEA050012), Jan 20, 2005: BOTTLE. DISCHARGED. TAILCONE EVACUATION SLIDE BOTTLE IS LOW. REMOVED AND REPLACED TAILCONE EVACUATION SLIDE.
- [SDR MWEA040217](https://openairdocs.org/sdr/MWEA040217), Dec 6, 2004: SKIN. DENTED. FUSELAGE SKIN HAS A DENT AT FRAME STATION 322.5 TO 329 ONE INCH BELOW LONGERON 23 RIGHT TO 24 RIGHT. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040216](https://openairdocs.org/sdr/MWEA040216), Nov 30, 2004: BEAM. CORRODED. CORROSION AROUND LIGHTENING HOLE ON TOP OF NR 3 RIGHT FORWARD EMERGENCY EXIT DOOR BEAM. FABRICATED AND INSTALLED DOUBLER.
- [SDR MWEA040215](https://openairdocs.org/sdr/MWEA040215), Nov 24, 2004: SKIN. DENTED. FUSELAGE SKIN DENT AT STATION 1305, LONGERON 19 RIGHT IS WITHIN 1 INCH OF LONGERON AND NO LONGER MEETS CONDITION PER STRUCTURAL REPAIR MANUAL. FABRICATED AND IN

All 163: https://openairdocs.org/aircraft/N812ME/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (324, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Cessna 550)

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST01823WI](https://openairdocs.org/stc/ST01823WI): Installation of Garmin GTS Traffic Sensor with Garmin GTX 3000 Mode S Transponders with ADS-B Out. Blackhawk Aerospace Technologies Inc
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST12344IB](https://openairdocs.org/stc/ST12344IB): Replacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST02016WI](https://openairdocs.org/stc/ST02016WI): Installation of the Meggitt Wireless Tire Pressure Sensor. 3S Certification LLC
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST11216DS](https://openairdocs.org/stc/ST11216DS): Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft. BHE & Associates Ltd
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST02718LA](https://openairdocs.org/stc/ST02718LA): Modification to replace the existing standby instrument. Acron Aviation Inc
- [STC ST03292CH](https://openairdocs.org/stc/ST03292CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development, Inc
- [STC ST09854AC](https://openairdocs.org/stc/ST09854AC): Installation of a Lumin Media Server. L2 Aviation
- [STC ST155CH](https://openairdocs.org/stc/ST155CH): Installation of BF Goodrich Avionics systems TCAS791 traffic alert and collison avoidance system I (TCASI). Acron Aviation Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST04742NY](https://openairdocs.org/stc/ST04742NY): Installation of SkyVue 1000 Cockpit Upgrade including dual Avidyne IFD540 FMS with LPV i. Aerospace Design & Compliance LLC
- [STC ST04736NY](https://openairdocs.org/stc/ST04736NY): True Blue TS28 Emergency Battery Power Supply Replacement. Aerospace Design and Compliance LLC
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST02427LA](https://openairdocs.org/stc/ST02427LA): Installation of Dual Garmin GTN 6XX/7XX Series Global Navigation System with Structural Antenna and WAAS approval; Garmin GMA 35 Audio Panel; and Dual Garmin GTX 33 Mode S Transponders, Weather Radar, and ADS-B Link. JETTECH LLC
- [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST02029WI](https://openairdocs.org/stc/ST02029WI): Installation of Garmin GI 275 Standby Instrument and GSB 15 USB Port. Blackhawk Aerospace Technologies
- [STC SA1773SO](https://openairdocs.org/stc/SA1773SO): Installation of a third stand-by attitude gyro and dedicated power supply AIM P/N PE 24-1RM. Summit Aviation Inc
- [STC ST02444AT-D](https://openairdocs.org/stc/ST02444AT-D): Installation of a Honeywell Mark VIII EGPWS System. Summit Aviation Inc
- [STC ST01070DE](https://openairdocs.org/stc/ST01070DE): Installation of the Curtiss-Wright Fortress Flight Data Recorder (with Cockpit Voice Recorder). Peregrine
- [STC SA7408SW](https://openairdocs.org/stc/SA7408SW): Installation of Heads Up checklist(electronic verbal checklist). Heads Up Technologies Inc
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST01985WI](https://openairdocs.org/stc/ST01985WI): Installation of the Garmin GI-275 I Electronic Standby Instrument (ESI). Peregrine
- [STC ST02004WI](https://openairdocs.org/stc/ST02004WI): Installation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI). Peregrine
- [STC ST00011WI](https://openairdocs.org/stc/ST00011WI): Installation of Concorde RG380E/40 and 40B battery. Aero-Mach Wilco LLC
- [STC SA1297GL](https://openairdocs.org/stc/SA1297GL): Installation of Cleveland main wheels and brakes. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA882GL](https://openairdocs.org/stc/SA882GL): Install aircraft wheel and brake conversion kit 199-137. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC ST01994WI](https://openairdocs.org/stc/ST01994WI): Installation of Honeywell Primus Elite Enhanced Functionality Modification and Honeywell Primus Elite Drop-in Modification. TurboJet Engineering Pty Ltd
- [STC ST04281AT](https://openairdocs.org/stc/ST04281AT): Installation for the Upgrade of the NZ-2000 FMS computer for software version NZ6. Chippewa Aerospace Inc
- [STC ST04473CH](https://openairdocs.org/stc/ST04473CH): Installation of a Honeywell RDR -7000 Weather Radar System. Honeywell International Inc
- [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC
- [STC ST00617WI](https://openairdocs.org/stc/ST00617WI): Installation of Bendix/King EFS-50 Two-Tube (EFIS) Electronic Flight Instrumentation System. For 550 (S/N 0002 thru 0733). Blackhawk Aerospace Technologies Inc
- [STC ST00624WI](https://openairdocs.org/stc/ST00624WI): Installation of Bendix/King EFS-50 Five-Tube (EFIS) Electronic Flight Instrumentation System. FOr 550 (S/N 0002 thru 0733). Blackhawk Aerospace Technologies Inc
- [STC ST01149WI](https://openairdocs.org/stc/ST01149WI): Installation of IS&S Air Data System with Reduced Vertical Separation Minimum (RVSM) compliant Dual Air Data System. Blackhawk Aerospace Technologies Inc
- [STC ST01162WI](https://openairdocs.org/stc/ST01162WI): Reduced Vertical Separation Minimum (RVSM) group airworthiness approval of the Cessna Aircraft Model 500, 501, 550 and 551. Blackhawk Aerospace Technologies Inc
- [STC ST01197WI](https://openairdocs.org/stc/ST01197WI): Installation of Universal Avionics EFI-550 2-Display EFIS System. Data required: (1) Columbia Avionics, Inc. Master Document List No. 30141165, Revision 3, dated September 24, 2003; and (2) FAA Approved Flight Manual Supplement 30141180, dated September 30, 2003, or later FAA Approved Revisions to (1) or (2). Blackhawk Aerospace Technologies Inc
- [STC ST01466WI](https://openairdocs.org/stc/ST01466WI): Installation of Universal Avionics EFI-890R Flat Panel EFIS System. Blackhawk Aerospace Technologies Inc
- [STC ST01691WI](https://openairdocs.org/stc/ST01691WI): Installation of Garmin GTN Series GPS/Comm/Nav Systems with optional Garmin GDL-69/A XM Weather Data Link, GTX-33 Series Transponders and optional Bendix/King KMR-675 Marker Beacon Receiver. Blackhawk Aerospace Technologies Inc
- [STC ST01929WI](https://openairdocs.org/stc/ST01929WI): Installation of Garmin G700 TXi EFIS system and GWX 75 Weather Radar. Blackhawk Aerospace Technologies Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST02989AT](https://openairdocs.org/stc/ST02989AT): Installation of a modified Glareshield. Continental Aerospace Technologies Inc
- [STC ST04566NY](https://openairdocs.org/stc/ST04566NY): Installation of the Garmin 400W, Rockwell Collins TCAS 4000 / Dual TDR-94D Transponder. Mid Canada Mod Center
- [STC ST02642AT](https://openairdocs.org/stc/ST02642AT): Installation of a RVSM Air Data System. Carlisle Interconnect Technologies Inc
- [STC SA4510NM](https://openairdocs.org/stc/SA4510NM): Installation of Dual Honeywell EDZ-805 Electronic Flight Instrument System, with options. Honeywell International Inc

All 324: https://openairdocs.org/aircraft/N812ME/stcs.md

## Related

- Other Cessna 550 aircraft: https://openairdocs.org/model/cessna-550/aircraft.md
- The Pratt & Whitney Canada 530A engine: https://openairdocs.org/engine/pratt-whitney-canada-530a.md

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