# N650TW: 1997 Cessna 650

- Status: Valid registration
- Airframe: [Cessna 650](https://openairdocs.org/model/cessna-650) (registry code 2076802, 12 seats)
- Engine: [Garrett TFE731 series](https://openairdocs.org/engine/garrett-tfe731-series) (registry code 29001)
- Data sheets: [TCDS A9NM](https://openairdocs.org/tcds/A9NM) (Textron Aviation Inc.), [TCDS E6WE](https://openairdocs.org/tcds/E6WE) (Honeywell Aerospace US LLC) (OpenAirDocs)
- Serial number: 650-7082
- Year built: 1997
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 23, 1998
- Certificate issued: March 23, 2024
- Expires: March 31, 2031
- Mode S code: A88E78
- Registered owner: [Kwafr LLC](https://openairdocs.org/faa-owner/KWAFR%20LLC)
- Location: [Richland Hills, TX](https://openairdocs.org/faa-place/TX/Richland%20Hills)
- Owner type: LLC
- Owner's area on the map: 32.7936° N, 97.1939° W: Placed by OpenAirDocs at the center of ZIP code 76118, 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=650TW
- Page: https://openairdocs.org/aircraft/N650TW

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Garrett TFE731 model are included.

## ADs that may apply (OpenAirDocs): 61 in force

### Matched by airframe (Cessna 650)

- [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 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 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [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 2005-13-21](https://openairdocs.org/ad/2005-13-21): Actuator control unit (ACU) · Cessna 650. Effective Jul 29, 2005
- [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 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2002-14-24](https://openairdocs.org/ad/2002-14-24): Side Brace Mechanism Assembly of Main Landing Gear · Cessna 650. Effective Aug 26, 2002
- [AD 97-12-01](https://openairdocs.org/ad/97-12-01): Wire Bundle Assembly · Cessna 650. Effective Jun 19, 1997
- [AD 96-25-12](https://openairdocs.org/ad/96-25-12): Auxiliary Power Units · BAE Systems HS 748 Series 2A, HS 748 Series 2B, 707-100 Long Body and 74 more. Effective Jan 13, 1997
- [AD 95-24-10](https://openairdocs.org/ad/95-24-10): Tires · Cessna 650 and Tires. Effective Feb 21, 1996
- [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 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 92-27-08](https://openairdocs.org/ad/92-27-08): Elevator Control · Cessna 650. Effective Jan 4, 1993
- [AD 90-25-06](https://openairdocs.org/ad/90-25-06): DME Antenna Cable Connectors · Cessna 650. Effective Dec 11, 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 90-01-03](https://openairdocs.org/ad/90-01-03): Attitude and Heading Reference System · Bombardier ATR42-300, DHC-8-101, DHC-8-102 and 16 more. Effective Feb 5, 1990
- [AD 89-03-16](https://openairdocs.org/ad/89-03-16): Avionics Bus Relays · Cessna 650. Effective Apr 5, 1989
- [AD 88-23-04](https://openairdocs.org/ad/88-23-04): AFM Changes -- Elevator · Cessna 650. Effective Feb 21, 1989
- [AD 88-24-16](https://openairdocs.org/ad/88-24-16): Cabin Electrical Power · Cessna 650 and S550. Effective Dec 12, 1988
- [AD 87-06-02](https://openairdocs.org/ad/87-06-02): Electronic Flight Instrument Systems Symbol Generators · ATR - GIE Avions de Transport R gional ATR42-200, ATR42-300, ATR42-320 and 19 more. Effective May 11, 1987
- [AD 86-14-01](https://openairdocs.org/ad/86-14-01): Attitude Heading Reference System · ATR - GIE Avions de Transport R gional ATR42-200, ATR42-300, ATR42-320 and 19 more. Effective Jul 14, 1986
- [AD 85-03-51](https://openairdocs.org/ad/85-03-51): Aircraft Battery Inspection · Cessna 552 and 650. Effective Apr 11, 1985
- [AD 84-08-02 R1](https://openairdocs.org/ad/84-08-02-R1): Placard-Usable Fuel · Cessna 650. Effective Jan 28, 1985

### Matched by engine (Garrett TFE731 series)

- [AD 2016-07-02](https://openairdocs.org/ad/2016-07-02): Failure of the interstage turbine transition duct · Honeywell International TFE731-4, TFE731-4R, TFE731-5AR and 2 more. Effective May 5, 2016
- [AD 2014-12-52](https://openairdocs.org/ad/2014-12-52): Engines · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 11 more. Effective Jul 28, 2014
- [AD 2012-17-05](https://openairdocs.org/ad/2012-17-05): First stage low-pressure turbine (LPT1) rotor assembly · Honeywell International TFE731-4, TFE731-4R, TFE731-5 and 3 more. Effective Oct 2, 2012
- [AD 2010-06-11](https://openairdocs.org/ad/2010-06-11): Second stage low-pressure compressor rotor (LPCR) discs · Honeywell International TFE731-2, TFE731-2A, TFE731-2C and 16 more. Effective Apr 21, 2010
- [AD 2008-19-12](https://openairdocs.org/ad/2008-19-12): ITT duct · Honeywell International TFE731-4, TFE731-4R, TFE731-5 and 3 more. Effective Oct 27, 2008
- [AD 2008-02-19](https://openairdocs.org/ad/2008-02-19): High pressure (HP) turbine rotor assemblies · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 15 more. Effective Mar 6, 2008
- [AD 2005-13-07](https://openairdocs.org/ad/2005-13-07): Turbine rotor discs. · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Jul 27, 2005
- [AD 2005-05-15](https://openairdocs.org/ad/2005-05-15): (LPT) stage 1 disks · Honeywell International TFE731-2, TFE731-2C, TFE731-3 and 5 more. Effective Apr 18, 2005
- [AD 2001-23-09](https://openairdocs.org/ad/2001-23-09): Fan Rotor Discs · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Dec 21, 2001
- [AD 2000-15-09](https://openairdocs.org/ad/2000-15-09): HPC Impeller · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 20 more. Effective Oct 10, 2000
- [AD 98-17-01 R1](https://openairdocs.org/ad/98-17-01-R1): Flex Fuel Tube · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Nov 29, 1999
- [AD 97-04-03](https://openairdocs.org/ad/97-04-03): First stage low pressure turbine (LPT) seal plates · Honeywell International TFE731-2A, TFE731-3C and TFE731-3CR. Effective May 5, 1997
- [AD 96-05-03](https://openairdocs.org/ad/96-05-03): Fan rotor disks · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 13 more. Effective Apr 2, 1996
- [AD 96-04-01](https://openairdocs.org/ad/96-04-01): Fan Rotor Assembly · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Mar 15, 1996
- [AD 95-07-02](https://openairdocs.org/ad/95-07-02): Low Pressure Turbine Disks · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 3 more. Effective Jun 19, 1995
- [AD 94-23-05](https://openairdocs.org/ad/94-23-05): Honeywell International TFE731-3A and TFE731-3AR. Effective Dec 1, 1994
- [AD 94-07-03](https://openairdocs.org/ad/94-07-03): Turbine Nozzles · Honeywell International TFE731-2A, TFE731-3, TFE731-3A and 4 more. Effective Jun 6, 1994
- [AD 92-02-18](https://openairdocs.org/ad/92-02-18): Inflight Operation · Honeywell International TFE731-5BR. Effective Feb 10, 1993
- [AD 92-21-06](https://openairdocs.org/ad/92-21-06): Low Pressure Turbine (LPT) Rotor Disks · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 2 more. Effective Nov 27, 1992
- [AD 90-24-06](https://openairdocs.org/ad/90-24-06): Thermocouple Lead Assemblies · Honeywell International TFE731-2, TFE731-2A, TFE731-3 and 8 more. Effective Nov 13, 1990
- [AD 90-03-04](https://openairdocs.org/ad/90-03-04): High Pressure Turbine Rotor Discs · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 1 more. Effective Feb 22, 1990
- [AD 88-18-03](https://openairdocs.org/ad/88-18-03): High Pressure Turbine Rotor Disc · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 1 more. Effective Jul 21, 1989
- [AD 86-03-01](https://openairdocs.org/ad/86-03-01): Turbine Interstage Transition Ducts · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 4 more. Effective Feb 24, 1986
- [AD 82-23-03 R1](https://openairdocs.org/ad/82-23-03-R1): High Pressure Compressor Impellers · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Dec 9, 1983
- [AD 81-24-08](https://openairdocs.org/ad/81-24-08): Turbine Interstage Transition Ducts · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 2 more. Effective Jan 6, 1982
- [AD 80-16-04](https://openairdocs.org/ad/80-16-04): Tie Rod · Honeywell International TFE731-2, TFE731-3 and TFE731-3R. Effective Aug 7, 1980
- [AD 78-22-10](https://openairdocs.org/ad/78-22-10): Low Pressure Rotor Thrust Ball Bearings · Honeywell International TFE731-2, TFE731-3 and TFE731-3R. Effective Nov 13, 1978
- [AD 75-07-10](https://openairdocs.org/ad/75-07-10): Transfer Gearbox Vertical Bevel Gear Bearing · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective May 1, 1975
- [AD 74-23-05](https://openairdocs.org/ad/74-23-05): Fuel Pumps · Honeywell International TFE731-2. Effective Nov 14, 1974
- [AD 74-11-06](https://openairdocs.org/ad/74-11-06): Fuel Control Computer · Honeywell International TFE731-2. Effective Sep 23, 1974
- [AD 74-18-16](https://openairdocs.org/ad/74-18-16): Fuel Control Computer · Honeywell International TFE731-2. Effective Sep 6, 1974
- [AD 74-18-12](https://openairdocs.org/ad/74-18-12): Fuel Control Orifice Assembly · Honeywell International TFE731-2. Effective Sep 3, 1974
- [AD 74-13-09](https://openairdocs.org/ad/74-13-09): Fuel Pump Assemblies · Honeywell International TFE731-2. Effective Jul 31, 1974
- [AD 89-22-16](https://openairdocs.org/ad/89-22-16): Engine Acceleration or Deceleration · Honeywell International TFE731-2, TFE731-5, TFE731-5AR and 1 more

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

- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 98-17-01](https://openairdocs.org/ad/98-17-01) (historical): Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Oct 13, 1998
- [AD 96-18-13](https://openairdocs.org/ad/96-18-13) (historical): Fan rotor disk · Honeywell International TFE731-2, TFE731-2A, TFE731-3 and 10 more. Effective Nov 12, 1996
- [AD 86-11-05](https://openairdocs.org/ad/86-11-05) (historical): Fan Rotor Discs · Honeywell International TFE731-2, TFE731-3 and TFE731-3R

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

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB CE-10-49R1](https://openairdocs.org/saib/CE-10-49R1): Equipment/Furnishings Drain Mast Heater. Issued Jan 5, 2011
- [SAIB CE-10-29R1](https://openairdocs.org/saib/CE-10-29R1): Lights  Aft Side Ledger Divider Light. Issued May 21, 2010
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NE-06-70](https://openairdocs.org/saib/NE-06-70): . Issued Sep 25, 2006
- [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 N650TW.

## FAA accident and incident reports

None matched to N650TW.

## Reports on N650TW not matched to an aircraft (2)

They name N650TW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19930513018439I](https://openairdocs.org/incident/19930513018439I), May 13, 1993: Boeing 767205 (N650TW), Salt Lake City, UT. Zero oil pressure NR1 engine. Shutdown. Landed at Salt lake. Improperly thrust wire on NR3 bearing breather line.
- [Incident 19880427019589I](https://openairdocs.org/incident/19880427019589I), Apr 27, 1988: Boeing 767205 (N650TW), St Louis, MO. APU low oil quantity alert. Diverted unable to find leaks. Replaced oil and continued flight.

## 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 N650TW not matched to an aircraft (55, newest 50)

They name N650TW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR TWAA0104608](https://openairdocs.org/sdr/TWAA0104608), Mar 12, 2001: SKIN. DELAMINATED. DURING CHECK-C THE RT WING OTBD T/E FLAP OTBD END, 48 INCHES FROM THE OTBD END AND 7.5 IN FROM THE T/E HAD A 5 IN BY 3.75 IN DELAMINATION. INSTALLED REPAIR 9 IN
- [SDR TWAA0104504](https://openairdocs.org/sdr/TWAA0104504), Mar 9, 2001: SKIN. DELAMINATED. DURING CHECK-C MAINT ON THE RT WING THE NUMBER 8 L/E SLAT, 61 IN FROM OTBD END AND 7 IN FROM THE WEDGE T/E, HAD 3.5 BY 5.75 INCH DELAMINATION. INSTALLED 8 IN BY
- [SDR TWAA0019902](https://openairdocs.org/sdr/TWAA0019902), Dec 22, 2000: COFFEEMAKER. FAULTY. COFFEE MAKER NUMBER 6 WAS EMITTING A BURNED WIRE SMELL. CREW TURNED OFF THE COFFEE MAKER. MAINTENANCE REPLACED IT. CHECK-C 9-10-00 MCI.
- [SDR TWAA0018702](https://openairdocs.org/sdr/TWAA0018702), Nov 25, 2000: STRINGER. DAMAGED. STRINGER 33R WAS FOUND DAMAGED UNDER DENTS AT STA 414 AND STA 470. REPLACED BOTH STRINGER SECTIONS AT 414 AND 470 STATIONS, PER SRM 53-00-03, FIG 202. CHECK-C 9
- [SDR TWAA0017701](https://openairdocs.org/sdr/TWAA0017701), Nov 2, 2000: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOORBEAM CAP AT STA 1351, BETWEEN STRINGER 33L AND 39L. REPLACED FLOORBEAM CAP AT STA 1351 PER SRM 51-10-02.
- [SDR TWAA0017607](https://openairdocs.org/sdr/TWAA0017607), Oct 30, 2000: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOORBEAM STA 1285, FROM STRINGER 34R TO 39R. REPLACED FLOORBEAM PER SRM 51-40-02 AND SPM 6-70-01.
- [SDR TWAA0017606](https://openairdocs.org/sdr/TWAA0017606), Oct 27, 2000: FLAP TRACK. CRACKED. THE LT WING T.E. NUMBER 3 FLAP TRACK AFT FAIRING HAD A ONE INCH CRACK INBD FWD EDGE, AND HAD A ROUGH EDGE. REPAIRED CRACK AND ROUGH EDGE PER SRM 51-70-03, PAGE 
- [SDR TWAA0017605](https://openairdocs.org/sdr/TWAA0017605), Oct 23, 2000: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK, THE CABIN FLOORBEAM TOP HAD CORROSION AT RBL 35 AND RBL 80 IN, STA 303. REMOVED CORRODED SECTION BETWEEN LBL 35 AND RBL 80, STA 303, P
- [SDR TWAA0017516](https://openairdocs.org/sdr/TWAA0017516), Oct 23, 2000: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN FLOORBEAM AT STA 325, RBL 64 INCHES. REMOVED CORRODED FLOORBEAM AND INSTALLED NEW SECTION OF T CAP AT STA 325
- [SDR TWAA0017515](https://openairdocs.org/sdr/TWAA0017515), Oct 23, 2000: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN FLOORBEAM AT STA 287, LBL 36 IN TO RBL 80 IN. REMOVED CORRODED FLOORBEAM AND REPLACED FLOORBEAM T CAP AT STA 
- [SDR TWAA0017514](https://openairdocs.org/sdr/TWAA0017514), Oct 18, 2000: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK, FOUND CORROSION ON AFT CARGO FLOORBEAM CAP AT STA 1395, STRINGER 33L. REMOVED CORRODED FLOORBEAM CAP AND INSTALLED NEW SECTION FROM LB
- [SDR TWAA0017513](https://openairdocs.org/sdr/TWAA0017513), Oct 17, 2000: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK THE FWD CARGO COMPT CARGO FLOORBEAM CAP HAD CORROSION AT STA 368, RBL 36 IN, AT NUT PLATE HOLE. REMOVED BEAM CAP FROM RBL 15 TO RBL 45 
- [SDR TWAA0017512](https://openairdocs.org/sdr/TWAA0017512), Oct 17, 2000: SUPPORT BRACKET. CORRODED. DURING OP 16 MAINT CHECK, LT AFT SERVICE DOOR THRESHOLD SUPPORT HAD CORROSION FROM STA 1480 TO 1548, STRINGER 20L. REMOVED AND REPLACED INBOARD FLOOR SUPPORT T 
- [SDR TWAA0017511](https://openairdocs.org/sdr/TWAA0017511), Oct 13, 2000: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK AT STA 1307 BETWEEN STRINGER 39R AND 38R, FOOT ON FLOORBEAM HAD CORROSION. REPLACED CORRODED FORMER FOOT WITH STOCK MATERIAL. PROTECTIV
- [SDR TWAA0015309](https://openairdocs.org/sdr/TWAA0015309), Sep 30, 2000: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK, AT STA 1109, TOP OF FLOORBEAM HAD CORROSION FROM STRINGER 33R TO 33L, TOP AND BOTTOM SIDES. REMOVED CORRODED BEAM CAP AND MADE NEW CAP
- [SDR TWAA0015308](https://openairdocs.org/sdr/TWAA0015308), Sep 27, 2000: RIB. CRACKED. DURING OP 16 MAINT CHECK, THE RIGHT I/B ELEVATOR, FWD OF FRONT SPAR, FOURTH RIB FROM THE I/B END WAS CRACKED. REPAIRED DAMAGED AREA WITH GRAPHITE BOND REPAIR PE
- [SDR TWAA0015307](https://openairdocs.org/sdr/TWAA0015307), Sep 27, 2000: SKIN. DELAMINATED. DURING OP 16 MAINT CHECK, THE RIGHT I/B ELEVATOR HAD SMALL DELAMINATION AREA OF PREVIOUS REPAIR, 5.5 INCHES FWD OF L/E AND 51 INCHES O/B OF I/B END. REMOVED OLD
- [SDR TWAA0015306](https://openairdocs.org/sdr/TWAA0015306), Sep 27, 2000: SKIN. CRACKED. DURING OP 16 MAINT CHECK, ON THE RIGHT I/B ELEVATOR A SMALL CRACK WAS FOUND IN THE ELEVATOR UPPER SKIN 35 IN FWD OF T/E AND 14 INCHES O/B OF THE I/B END, AND A 
- [SDR TWAA0015305](https://openairdocs.org/sdr/TWAA0015305), Sep 26, 2000: FLOORBEAM. CORRODED. DURING OP 16 MAINT CHECK AT STA 1087, TOP OF FLOORBEAM HAD CORROSION FROM 33R TO 33L, ON TOP AND BOTTOM OF TOP. REMOVED DAMAGED T-CAP AND MADE NEW PER DRAWING 1
- [SDR TWAA0015004](https://openairdocs.org/sdr/TWAA0015004), Sep 22, 2000: SKIN. DAMAGED. DURING OP 16 MAINT CHECK ON THE LT WING, TOP T/E 24 INCHES FROM O/B END OF O/B AILERON HAD BURNED/DAMAGED SPOT. REWORKED PER SRM 57-60-02, FIG 201, SHEET 2, AND
- [SDR TWAA0010002](https://openairdocs.org/sdr/TWAA0010002), Jun 25, 2000: LIGHT. CONTAMINATED. THE EGRESS LIGHTS WERE INOPERATIVE AT MID GALLEY AND ROW 18 TO 23, RT SIDE. FOUND LIGHTS WET. REMOVED AND DRIED THE LAMPS AND ALL CONNECTIONS. CHECK-C 6-4-00 LA
- [SDR TWAA0010004](https://openairdocs.org/sdr/TWAA0010004), Jun 24, 2000: LIGHT. INOPERATIVE. THE OUTSIDE EMERGENCY LIGHT AT THE LEFT SIDE FWD CABIN DOOR WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 6-4-00 LAX.
- [SDR TWAA0009003](https://openairdocs.org/sdr/TWAA0009003), Jun 7, 2000: SKIN. MISREPAIRED. DURING CHECK-C MAINT, FOUND PREVIOUS 7 INCH BY 12.5 INCH REPAIR ON RT WING O/B FLAP, O/B END LOWER SURFACE LOCATED 32 INCHES FROM O/B END. APPLIED HOT BOND REPA
- [SDR TWAA0009002](https://openairdocs.org/sdr/TWAA0009002), Jun 7, 2000: STRINGER. CORRODED. DURING CHECK-C MAINT, FOUND .375 INCH CORROSION AT FUSELAGE STA 456, STRINGER 33R. INSTALLED 14 INCH STRINGER DOUBLER REPAIR PER SRM 53-00-03, PAGE 215. CUT OUT
- [SDR TWAA0005603](https://openairdocs.org/sdr/TWAA0005603), Apr 12, 2000: LIGHT. INOPERATIVE. THE EMERGENCY LIGHT AFT OF THE AFT CARGO DOOR, LT COACH EGRESS LIGHTS, AND TWO OVERWING ESCAPE DOORS EXIT SIGNS WERE INOPERATIVE. REPLACED THE LAMPS AND CLEANED
- [SDR TWAA0005102](https://openairdocs.org/sdr/TWAA0005102), Apr 2, 2000: BATTERY PACK. INOPERATIVE. THE RT SIDE CABIN OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE BETWEEN ROW 30 AND THE AFT GALLEY. REPLACED THE BATTERY PACK. CHECK-C 2-21-00 LAX.
- [SDR TWAA0003706](https://openairdocs.org/sdr/TWAA0003706), Feb 20, 2000: SKIN. DENTED. DURING CK-C 2C, FOUND THE INBOARD AFT FLAP TOP SURFACE HAS A DENT 33.5 INCH FROM THE INBOARD END, 3 INCH FROM THE TRAILING EDGE. FILLED THE DENT WITH HYSOL 934,
- [SDR TWAA0003028](https://openairdocs.org/sdr/TWAA0003028), Feb 20, 2000: SKIN. DELAMINATED. DURING CHECK-C MAINT, THE RT WING OTBD FLAP 4 FEET 4 INCHES FROM OTBD END, 10.5 INCHES FROM TE HAD DELAMINATION .75 INCH BY 0.5 INCHES. CLEANED UP DAMAGED AREA 
- [SDR TWAA0003027](https://openairdocs.org/sdr/TWAA0003027), Feb 20, 2000: SKIN. DAMAGED. DURING OP 16 MAINT CHECK, THE RT WING INBD FLAP LE OTBD OF AFT FLAP ACTUATOR ROD, BULLNOSE WAS WORN. REMOVED MULTIPLE LAYERS OF PAINT TO MATERIAL SURFACE. FOUND
- [SDR TWAA0003026](https://openairdocs.org/sdr/TWAA0003026), Feb 20, 2000: SKIN. DAMAGED. DURING CHECK-C MAINTENANCE, THE RT WING INBD FLAP OTBD END FWD BULLNOSE WAS WORN. REMOVED MULTIPLE LAYERS OF PAINT TO MATERIAL SURFACE. FOUND NO DAMAGE. APPLIED
- [SDR TWAA0003025](https://openairdocs.org/sdr/TWAA0003025), Feb 20, 2000: SKIN. DAMAGED. DURING CHECK-C MAINTENANCE, THE RT WING INBD AILERON UPPER SURFACE, 38.75 IN FWD OF TE, 16 INCHES OTBD OF INBD END, HAD A DENT. INSTALLED 2 LAYER GRAPHITE 4.5 I
- [SDR TWAA0003024](https://openairdocs.org/sdr/TWAA0003024), Feb 20, 2000: SKIN. DAMAGED. DURING CHECK-C MAINT, THE RT WING OTBD FLAP INBD END, TOP SURFACE 36 INCHES FWD OF THE TE AND 1.25 INCHES FROM THE INBD END, A FLAP REPAIR WAS WORN THROUGH. REM
- [SDR TWAA0002802](https://openairdocs.org/sdr/TWAA0002802), Feb 16, 2000: WIRE. CUT. THE EGRESS LIGHTS WERE INOPERATIVE ON RT SIDE OF CABIN ROWS 27 TO 35. REPLACED THE FEEDER CABLE. CHECK-C 11-12-99 LAX.
- [SDR TWAA9917102](https://openairdocs.org/sdr/TWAA9917102), Dec 16, 1999: BATTERY. DISCHARGED. THE EMERGENCY CEILING LIGHTS WERE INOPERATIVE ON RT SIDE OF CABIN, ROW 22 AFT. REPLACED POWER SUPPLY. CHECK-C 11-7-99 LAX.
- [SDR TWAA9915806](https://openairdocs.org/sdr/TWAA9915806), Nov 10, 1999: SKIN. DELAMINATED. DURING CHECK-C MAINT, FOUND AT LOWER O/B SURFACE OF NUMBER 8 SLAT, THE T/E WEDGE HAD DELAMINATION 6 INCHES FROM THE T/E. INSTALLED HOT BOND REPAIR PER SRM 51-70
- [SDR TWAA9915303](https://openairdocs.org/sdr/TWAA9915303), Nov 10, 1999: SKIN. DELAMINATED. DURING CHECK-C MAINT, THE NUMBER 11 LE SLAT HAD DELAMINATION AT LOWER INBD SURFACE, 6 INCHES FROM THE TE. INSTALLED METAL HOT BOND REPAIR PER SRM 51-70-10, PER 
- [SDR TWAA9915304](https://openairdocs.org/sdr/TWAA9915304), Nov 7, 1999: SKIN. MISREPAIRED. DURING CHECK-C MAINT, THE LEFT WING NUMBER 3 LE SLAT, TOP SIDE AT OTBD END, FOUND THE PATCH COVER HAD COME OFF OF THE METAL SURFACE. INSTALLED A 3.5 INCH IN BY 
- [SDR TWAA9906005](https://openairdocs.org/sdr/TWAA9906005), Apr 19, 1999: SKIN. CRACKED. THE TOP SURFACE OF NR 4 LE SLAT, AFT EDGE WEDGE, HAD A 2 IN CRACK WITH .125 IN HOLE APPROX 42 IN INBD AND 9 IN FROM TE. INSTALLED DOUBLER REPAIR PER 767 SRM 51-
- [SDR TWAA9902302](https://openairdocs.org/sdr/TWAA9902302), Feb 7, 1999: SKIN. DELAMINATED. DURING CHECK-C, MAINTENANCE FOUND NR 5 L/E SLAT INBD TOP DELAMINATED 3 INCH BY 3 INCH. REMOVED DELAMINATED SKIN AND INSTALLED FILLER AND METAL HOT BOND REPAIR P
- [SDR TWAA9901401](https://openairdocs.org/sdr/TWAA9901401), Jan 15, 1999: SKIN. DAMAGED. THE NR 6 LE SLAT PANEL TRAILING EDGE AT INBD TOP END HAD REPAIR BLOWN OFF. INSTALLED HOT BOND REPAIR AS REQUIRED BY SRM 51-70-10, PAGE 26 FIG 10. CHECK-C 10-28-
- [SDR TWAA9818808](https://openairdocs.org/sdr/TWAA9818808), Nov 24, 1998: SKIN. DELAMINATED. FOUND 12 INCH BY 12 DELAMINATION ON UPPER SURFACE OF NR 6 L/E DEVICE, AT O/B END. INSTALLED METAL TO METAL HOT BOND REPAIR PER 767 SRM 51-70-10. CHECK-C 10-28-9
- [SDR TWAA9818409](https://openairdocs.org/sdr/TWAA9818409), Nov 1, 1998: SKIN. DELAMINATED. DURING CHECK-C MAINT, FOUND NR 6 LEADING EDGE SLAT, O/B SIDE REPAIR DELAMINATED. REPLACED CORRODED HONEYCOMB AND INSTALLED 12.5 IN BY 13 IN METAL OVERLAY PER SR
- [SDR TWAA9818410](https://openairdocs.org/sdr/TWAA9818410), Oct 31, 1998: SKIN. DELAMINATED. DURING CHECK-C MAINT, FOUND RT WING NR 10 LEADING EDGE SLAT TOP DELAMINATED O/B OF CENTER, AND I/B OF OLD PATCH, 2 IN WIDE BY 4 IN LONG. REMOVED PREVIOUS REPAIR
- [SDR TWAA9818412](https://openairdocs.org/sdr/TWAA9818412), Oct 30, 1998: SKIN. DELAMINATED. DURING CHECK-C MAINT, FOUND REPAIR COMING LOOSE ON THE LEADING EDGE OF LT WING, AFT OF OF NR 6 LEADING EDGE SLAT I/B SIDE. REMOVED DELAMINATED REPAIR, REPLACED 
- [SDR TWAA9818411](https://openairdocs.org/sdr/TWAA9818411), Oct 30, 1998: SKIN. DELAMINATED. DURING CHECK-C MAINT, FOUND NR 6 LEADING EDGE SLAT I/B REPAIR HAD DELAMINATION. REMOVED DELAMINATED DOUBLER AND REPAIRED DAMAGED CORE AND INSTALLED 10 BY 12 IN 
- [SDR TWAA9812703](https://openairdocs.org/sdr/TWAA9812703), Aug 4, 1998: BATTERY PACK. DISCHARGED. MAINT FOUND EMERGENCY LIGHT EQUIPMENT NRS L308, L311, L333 WERE INOPERATIVE ON TEST. REPLACED BATTERY PACK. CHECK-C 7-21-98 LAX.
- [SDR TWAA9812130](https://openairdocs.org/sdr/TWAA9812130), Jul 24, 1998: SKIN. CRACKED. DURING CHECK-C MAINT, FOUND LT WING O/B FLAP LOWER SKIN WITH 2 IN CRACK APPROX 18 IN FROM I/B END AND APPROX 12 IN FROM T/E. CUT OUT DAMAGED AREA AND INSTALLED 
- [SDR TWAA9812131](https://openairdocs.org/sdr/TWAA9812131), Jul 21, 1998: SKIN. TORN. DURING CHECK-C MAINT, FOUND NR 5 SPOILER T/E 1.5 IN TEAR IN SPOILER PANEL. REPAIRED PER SRM. INSTALLED LAYER ADHESIVE AND LAYER FABRIC AND HOT BOND 6 BY 6 PER S
- [SDR TWAA9802203](https://openairdocs.org/sdr/TWAA9802203), Feb 11, 1998: OIL REGULATOR. LEAKING. STL - FLT 842 - AIRCRAFT WAS OPERATING WITH THE LT GENERATOR PLACARDED INOPERABLE PER MEL. IN-FLIGHT, THE APU AUTO SHUTDOWN WITH EICAS MSG - APU LOW OIL PRESS. 
- [SDR TWAA9716004](https://openairdocs.org/sdr/TWAA9716004), Feb 1, 1997: VANE BLEED CONTL. OUT OF ADJUST. JFK - DURING CRUISE, NR 2 ENGINE SUFFERED COMPRESSOR STALL. ADJUSTED ENGINE VANE BLEED CONTROL (EVBC). OPERATIONAL CHECK AND ENGINE RUN NORMAL. (M)

All 55: https://openairdocs.org/aircraft/N650TW/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (227, 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 650)

- [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 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 ST00452WI](https://openairdocs.org/stc/ST00452WI): Installation of an AlliedSignal Avionics Inc, CAS 67A traffic Alert and Collison Avoidance system (TCAS II). Duncan Aviation Inc
- [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 ST03292CH](https://openairdocs.org/stc/ST03292CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development, Inc
- [STC ST00296WI](https://openairdocs.org/stc/ST00296WI): Installation of a TCAS-791 traffic alert and collision avoidance system (TCAS I). 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 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 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 ST01070DE](https://openairdocs.org/stc/ST01070DE): Installation of the Curtiss-Wright Fortress Flight Data Recorder (with Cockpit Voice Recorder). Peregrine
- [STC ST10167SC](https://openairdocs.org/stc/ST10167SC): Installation of interior lighting system. Heads Up Technologies Inc
- [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 ST00029IB](https://openairdocs.org/stc/ST00029IB): Installation of Deviations to FAA STC ST02654LA. Mid Canada Mod Center
- [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 ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC d/b/a West Star Aviation
- [STC ST04503CH](https://openairdocs.org/stc/ST04503CH): Upgrade Dual Honeywell FMZ-2000 / NZ 6.1 With WAAS-LPV in accordance with StandardAero Master Data List 1039558, Revision (C), Dated May 20, 2021 or later FAA approved revision. StandardAero Business Aviation Services LLC
- [STC ST04638NY](https://openairdocs.org/stc/ST04638NY): Installation of the GOGO Avance L3 System. MidCanada Mod Center
- [STC ST01015WI](https://openairdocs.org/stc/ST01015WI): Installation of the Collins FDS-2000 EFIS. Blackhawk Aerospace Technologies Inc
- [STC ST01016WI](https://openairdocs.org/stc/ST01016WI): Installation of a dual Collins AHS-3000A AHRS. Blackhawk Aerospace Technologies Inc
- [STC ST01227WI](https://openairdocs.org/stc/ST01227WI): Installation of IS&S Air Data System. Data required: (1) Columbia Avionics, Inc. Master Document List No. 30141324, Revision 3, dated January 21, 2004; and (2) FAA Approved Flight Manual Supplement 30141339, dated January 28, 2004, or later FAA Approved Revisions to (1) or (2). Blackhawk Aerospace Technologies Inc
- [STC ST01257WI](https://openairdocs.org/stc/ST01257WI): Reduced Vertical Separation Minimum (RVSM) group airworthiness approval of Cessna Model 650 Citation III Aircraft. Blackhawk Aerospace Technologies Inc
- [STC ST01309WI](https://openairdocs.org/stc/ST01309WI): Installation of a Honeywell MK-VIII EGPWS system. Data required: (1) Columbia Avionics, Inc. Master Document List No. 30141108, Revision 2, dated February 21, 2005; and (2) FAA Approved Flight Manual Supplement 30141123, dated February 25, 2005, or later FAA Approved Revisions to (1) or (2). Blackhawk Aerospace Technologies Inc
- [STC ST01446WI](https://openairdocs.org/stc/ST01446WI): Installation of Universal Avionics EFI-890R Flat Panel EFIS System . Blackhawk Aerospace Technologies Inc
- [STC ST01683WI](https://openairdocs.org/stc/ST01683WI): 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 ST01853WI](https://openairdocs.org/stc/ST01853WI): Installation of Garmin GTS Traffic Sensor with Garmin GTX 3000 Mode S Transponders and ADS-B Out. 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 ST00963LA](https://openairdocs.org/stc/ST00963LA): ONE ONLY STC, SN 650-0005: Installation of Honeywell Total Aircraft Information system (TAIS). Honeywell International Inc
- [STC ST00691LA](https://openairdocs.org/stc/ST00691LA): Installation of Honeywell/Racal Intermediate gain satellite communication system. Honeywell International Inc
- [STC SA3461NM](https://openairdocs.org/stc/SA3461NM): Installation of a Honeywell, Inc. FMZ-800 Flight Management System (FMS). Honeywell International Inc
- [STC SA3451NM](https://openairdocs.org/stc/SA3451NM): Installation of Sperry SPZ-8000 Digital Integrated Flight Control System. Honeywell International Inc
- [STC SA5030NM](https://openairdocs.org/stc/SA5030NM): Addition of Honeywell GPS sensor unit to FAA approved Honeywell FMS installation. Honeywell International Inc
- [STC SA2269NM](https://openairdocs.org/stc/SA2269NM): ONE ONLY STC, SN 650-0005; Installation of dual Sperry EDZ-601 Electronic Flight Instrument Systems (EFIS) and a Global GNS-500A VLF/Omega Navigation System with a NDB-2 Data Base. Honeywell International Inc
- [STC SA6046NM](https://openairdocs.org/stc/SA6046NM): Installation of Primus 2000 integrated avionics system. Honeywell International Inc
- [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST00882DE](https://openairdocs.org/stc/ST00882DE): Installation of Becker Avionics BXT6553 transponder. Peregrine
- [STC ST01027DE](https://openairdocs.org/stc/ST01027DE): Installation of MarathonNorco Aerospace Inc Nickel Cadmium battery in place of existing Nickel Cadmium main aircraft battery/batteries. MarathonNorco Aerospace Inc
- [STC ST04359NY](https://openairdocs.org/stc/ST04359NY): Installation of Interior Modifications. Ramm Aerospace Inc
- [STC ST00934DE](https://openairdocs.org/stc/ST00934DE): Installation of Becker Avionics BXT6553 transponder. Peregrine
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST00835DE](https://openairdocs.org/stc/ST00835DE): Installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out and In functionality using the Garmin GTX 335R and GTX 345R Transponders plus qualified position sensor. Peregrine
- [STC ST02654LA](https://openairdocs.org/stc/ST02654LA): Installation of lnSight® Display System, EIU, TAWS Class A, and UNS-1Fw SBAS FMS (with ADS-B Out function). Universal Avionics Systems Incorporated

All 227: https://openairdocs.org/aircraft/N650TW/stcs.md

## Related

- Other Cessna 650 aircraft: https://openairdocs.org/model/cessna-650/aircraft.md
- The Garrett TFE731 series engine: https://openairdocs.org/engine/garrett-tfe731-series.md

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