# N769CA: Gates Lear Jet 28

- Status: Valid registration
- Airframe: [Gates Lear Jet 28](https://openairdocs.org/model/gates-lear-jet-28) (registry code 5170528, 9 seats)
- Engine: [GE CJ-610-8A](https://openairdocs.org/engine/ge-cj-610-8a) (registry code 30035)
- Data sheets: [TCDS A10CE](https://openairdocs.org/tcds/A10CE) (Learjet Inc.), [TCDS 1E16](https://openairdocs.org/tcds/1E16) (General Electric Company) (OpenAirDocs)
- Serial number: 004
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 12, 1999
- Certificate issued: November 20, 2023
- Expires: November 30, 2030
- Mode S code: AA632A
- Registered owner: [Wings Over Texas Holdings LLC](https://openairdocs.org/faa-owner/WINGS%20OVER%20TEXAS%20HOLDINGS%20LLC)
- Location: [Denton, TX](https://openairdocs.org/faa-place/TX/Denton)
- Owner type: LLC
- Owner's area on the map: 33.2276° N, 97.1843° W: Placed by OpenAirDocs at the center of ZIP code 76207, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=769CA
- Page: https://openairdocs.org/aircraft/N769CA

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): 23 in force

### Matched by airframe (Gates Lear Jet 28)

- [AD 2018-19-04](https://openairdocs.org/ad/2018-19-04): TE Flap Control System · Learjet 28, 29, 31 and 9 more. Effective Oct 23, 2018
- [AD 2007-04-18](https://openairdocs.org/ad/2007-04-18): Left- and right-hand standby fuel pump switches · Learjet 23, 24, 24A and 25 more. Effective Mar 23, 2007
- [AD 2005-13-36](https://openairdocs.org/ad/2005-13-36): Center ball of the aileron control cable · Learjet 23, 24, 24A and 21 more. Effective Aug 9, 2005
- [AD 2001-07-11](https://openairdocs.org/ad/2001-07-11): Main Landing Gear Tires · Learjet 23, 24, 24A and 25 more. Effective May 1, 2001
- [AD 99-16-03](https://openairdocs.org/ad/99-16-03): Horizontal Stabilizer Anti-Ice System · Learjet 23, 24, 24A and 22 more. Effective Sep 7, 1999
- [AD 95-20-03](https://openairdocs.org/ad/95-20-03): Airplane Flight Manual (AFM) - Altitude Limitations · Learjet 24, 24A, 24B and 24 more. Effective Nov 2, 1995
- [AD 92-19-12](https://openairdocs.org/ad/92-19-12): Oxygen Plumbing & Map Light Wires · Learjet 23, 24, 24A and 22 more. Effective Nov 17, 1992
- [AD 89-12-01](https://openairdocs.org/ad/89-12-01): Drag Chute Riser · Learjet 24, 24A, 24B and 22 more. Effective Jul 3, 1989
- [AD 86-05-05 R1](https://openairdocs.org/ad/86-05-05-R1): Battery Vent System · Learjet 23, 24, 24A and 20 more. Effective Jan 19, 1988
- [AD 86-22-05](https://openairdocs.org/ad/86-22-05): Flap Sector Mounting Brackets Inspection · Learjet 23, 24, 24A and 23 more. Effective Nov 10, 1986
- [AD 82-01-05 R2](https://openairdocs.org/ad/82-01-05-R2): Stall Warning Accelerometer Unit · Learjet 23, 24, 24A and 16 more. Effective Apr 10, 1986
- [AD 80-19-11 R1](https://openairdocs.org/ad/80-19-11-R1): Automatic Flight Control and Stall Warning Systems · Learjet 23, 24, 24A and 20 more. Effective May 20, 1985
- [AD 84-19-06](https://openairdocs.org/ad/84-19-06): Tab Control System · Learjet 24, 24A, 24B and 22 more. Effective Oct 22, 1984
- [AD 81-13-07](https://openairdocs.org/ad/81-13-07): Change to AFM Fuel Starvation · Learjet 23, 24, 24A and 20 more. Effective Jun 25, 1981
- [AD 80-26-02](https://openairdocs.org/ad/80-26-02): AFCS/AFC-SS Pitch Function · Learjet 23, 24, 24A and 16 more. Effective Jan 15, 1981
- [AD 80-19-09 R1](https://openairdocs.org/ad/80-19-09-R1): Jet Pumps · Learjet 23, 24, 24A and 20 more. Effective Dec 11, 1980
- [AD 80-07-09](https://openairdocs.org/ad/80-07-09): Cabin Main Entrance Upper Door · Learjet 23, 24, 24A and 20 more. Effective May 1, 1980

### Matched by engine (GE CJ-610-8A)

- [AD 2010-09-08](https://openairdocs.org/ad/2010-09-08): AFT Technologies combustion liners · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective May 28, 2010
- [AD 2001-10-12](https://openairdocs.org/ad/2001-10-12): Unapproved Parts · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Jun 7, 2001
- [AD 98-23-06](https://openairdocs.org/ad/98-23-06): Combustion Liner Assemblies · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Nov 20, 1998
- [AD 97-25-08](https://openairdocs.org/ad/97-25-08): General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Jan 2, 1998
- [AD 85-18-03](https://openairdocs.org/ad/85-18-03): Stage 1 Turbine Disk · General Electric CF700-2D, CF700-2D-2, CJ610-8A and 1 more. Effective Nov 15, 1985
- [AD 80-08-06 R1](https://openairdocs.org/ad/80-08-06-R1): Turbine Disks · General Electric CF700-2D, CF700-2D-2, CJ610-8A and 1 more. Effective Feb 2, 1981

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

- [SAIB 2026-07](https://openairdocs.org/saib/2026-07): MAIN LANDING GEAR ATTACH SECTION, Trunnion Pins. Issued Mar 19, 2026
- [SAIB NM-16-24](https://openairdocs.org/saib/NM-16-24): Fuselage: Main Plate/Skin. Issued Sep 15, 2016
- [SAIB NM-13-38](https://openairdocs.org/saib/NM-13-38): Flight Controls  Control Column Section. Issued Jun 24, 2013
- [SAIB CE-01-43](https://openairdocs.org/saib/CE-01-43): . Issued Sep 25, 2001
- [SAIB NE-08-49R1](https://openairdocs.org/saib/NE-08-49R1): Turbine Engine Combustion Section. Issued Sep 17, 2008
- [SAIB NE-08-49](https://openairdocs.org/saib/NE-08-49) (historical): Turbine Engine Combustion Section. Issued Sep 9, 2008

## NTSB investigations

None matched to N769CA.

## FAA accident and incident reports

None matched to N769CA.

## 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 N769CA not matched to an aircraft (23)

They name N769CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR COMA0160311](https://openairdocs.org/sdr/COMA0160311), Mar 12, 2001: LIGHT. MISWIRED. EMERGENCY FLOOR LIGHTS ARE INOP ROWS 1 THRU 5. FOUND WIRING BACKWARDS, REPAIRED WIRING AND SYSTEM TEST SATISFACTORY.
- [SDR COMA0160281](https://openairdocs.org/sdr/COMA0160281), Feb 21, 2001: WARNING SYSTEM. FALSE INDICATION. GROUND SPOILER UNSAFE CAUTION DURING TAXI. COULD NOT DUPLICATE. RESET SYSTEM, OPERATION CHECK NORMAL.
- [SDR COMA0060850](https://openairdocs.org/sdr/COMA0060850), Oct 28, 2000: BULB. BURNED OUT. EXTERIOR EMERGENCY LIGHT INOPERABLE. REPLACED LIGHT BULB.
- [SDR COMA0060791](https://openairdocs.org/sdr/COMA0060791), Oct 2, 2000: WARNING SYSTEM. ACTIVATED. FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
- [SDR COMA0060774](https://openairdocs.org/sdr/COMA0060774), Sep 24, 2000: LIGHT. FAILED. EMERGENCY LIGHT AT ROW 10 IS INOPERABLE. REPLACED LIGHT BULB.
- [SDR COMA0060684](https://openairdocs.org/sdr/COMA0060684), Aug 22, 2000: BULB. FAILED. FORWARD CEILING EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB.
- [SDR COMA0060642](https://openairdocs.org/sdr/COMA0060642), Aug 12, 2000: SMOKE. DETECTED. ''SMOKE TOILET'' CAUTION MESSAGE, WITH SMOKE ODOR AND HAZE IN CABIN. RAN AIRCRAFT UNTIL ODOR DISSIPATED. INSPECTED AIRCRAFT AND FOUND NO FAULTS. COULD NOT DUPLI
- [SDR COMA0060629](https://openairdocs.org/sdr/COMA0060629), Aug 5, 2000: PRESSURE SWITCH. MALFUNCTIONED. RIGHT HAND A/C T PACK HIGH PRESSURE MESSAGE. REPLACED THE PRESSURE SWITCH.
- [SDR COMA0060573](https://openairdocs.org/sdr/COMA0060573), Jul 13, 2000: SWITCH. MALFUNCTIONED. CABIN DOOR OUTER HANDLE CAUTION MESSAGE. REPLACED PROXIMITY SENSOR PS2MB.
- [SDR COMA0060567](https://openairdocs.org/sdr/COMA0060567), Jul 11, 2000: LIGHT. INOPERATIVE. FORWARD EMERGENCY FLOOR LIGHTS ARE INOPERABLE. REPLACED POWER STRIP ROWS 1 THROUGH 5.
- [SDR COMA0060522](https://openairdocs.org/sdr/COMA0060522), Jun 19, 2000: BPSU. MALFUNCTIONED. FLAPS FAIL CAUTION MESSAGE. REPLACED THE RIGHT HAND BPSU.
- [SDR COMA0060278](https://openairdocs.org/sdr/COMA0060278), Mar 22, 2000: DOWNLOCK TARGET. LOOSE. LANDING GEAR DISAGREE WARNING, LEFT HAND MLG INDICATED INTRANSIT. TIGHTENED LOOSE PROXIMITY TARGET ON LEFT HAND MLG UPLOCK.
- [SDR COMA0060182](https://openairdocs.org/sdr/COMA0060182), Feb 18, 2000: SWITCH. OUT OF ADJUST. CABIN DOOR OUTER HANDLE MESSAGE. ADJUSTED PROXIMITY SENSOR PS2MB.
- [SDR COMA0060179](https://openairdocs.org/sdr/COMA0060179), Feb 18, 2000: CONNECTOR. CONTAMINATED. CABIN DOOR OUTER HANDLE CAUTION MESSAGE. CLEANED PLUGGED WATER DRAINS AT DOOR SILL, SO WIRING CONNECTORS COULD DRY OUT. DOOR WARNING OPERATED NORMAL.
- [SDR COMA0060166](https://openairdocs.org/sdr/COMA0060166), Feb 17, 2000: LIGHT. INOPERATIVE. FLOOR PATH LIGHTING INOPERABLE ROW 9 AND AFT. DRIED WET WIRING CONNECTORS. SYSTEM OPERATIONAL NORMAL.
- [SDR COMA0060155](https://openairdocs.org/sdr/COMA0060155), Feb 14, 2000: WHEEL. CRACKED. MECHANIC REMOVED MAIN WHEEL ASSEMBLY FROM A/C DUE TO TIME CHANGE. DURING CLEANING OF WHEEL FOUND INBOARD SUBASSEMBLY WAS CRACKED AT SPOKE AREA WHERE LOT NR STAM
- [SDR COMA9960652](https://openairdocs.org/sdr/COMA9960652), Oct 25, 1999: TILLER. MALFUNCTIONED. AIRCRAFT PULLED SHARPLY TO RIGHT DURING TAKEOFF. REPLACED STEERING TILLER.
- [SDR COMA9960261](https://openairdocs.org/sdr/COMA9960261), Jun 10, 1999: RETRACT MECH. MALFUNCTIONED. FLAPS FAILED AFTER LANDING. RESET FLAP SYSTEM PER AD 98-20-01.
- [SDR COMA9960174](https://openairdocs.org/sdr/COMA9960174), Apr 26, 1999: FECU. MALFUNCTION. FLAP FAIL MESSAGE. REPLACED THE FECU.
- [SDR COMA9960173](https://openairdocs.org/sdr/COMA9960173), Apr 26, 1999: FECU. MALFUNCTIONED. FLAPS FAIL MESSAGE. REPLACED THE LEFT HAND BPSU AND THE FECU.
- [SDR COMA9960176](https://openairdocs.org/sdr/COMA9960176), Apr 25, 1999: BPSU. MALFUNCTION. FLAPS FAIL CAUTION MESSAGE. REPLACED THE LEFT HAND BPSU.
- [SDR COMA9960071](https://openairdocs.org/sdr/COMA9960071), Feb 16, 1999: BPSU. MALFUNCTIONED. FLAPS FAIL CAUTION MESSAGE. REPLACED THE LEFT HAND BPSU.
- [SDR COMA9960067](https://openairdocs.org/sdr/COMA9960067), Feb 13, 1999: BPSU. MALFUNCTIONED. FLAPS FAIL CAUTION MESSAGE. REPLACED THE RIGHT HAND BPSU.

## STCs that may be installed (OpenAirDocs) (40)

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 (Gates Lear Jet 28)

- [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 ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST12087CH](https://openairdocs.org/stc/ST12087CH): Installation replacement Cabin/Cockpit Handheld Fire Extinguishers. Avcon Industries Inc
- [STC ST02416SE](https://openairdocs.org/stc/ST02416SE): Installation of the replacement rate gyro, Butler National Part Number 501-1169-01 MOD A or 501-1169-02 MOD A. Symetric Industries, DBA Extant Aerospace
- [STC ST02417SE](https://openairdocs.org/stc/ST02417SE): Installation of the replacement stall warning vertical accelerometer, Butler National Part Number 02904001-101. Symetric Industries, DBA Extant Aerospace
- [STC ST01308WI](https://openairdocs.org/stc/ST01308WI): Installation of L-3 Communications Avionics Systems Inc. (Landmark) Terrain Awareness Warning System (TAWS) model TAWS8100. 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 ST04728NY](https://openairdocs.org/stc/ST04728NY): Installation of LAI CoolView Cabin Window. Lee Aerospace Inc
- [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 ST02004WI](https://openairdocs.org/stc/ST02004WI): Installation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI). Peregrine
- [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services 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 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 SA4999NM](https://openairdocs.org/stc/SA4999NM): Installation of lifeport patient loading and support system. LifePort LLC
- [STC ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST02500SE](https://openairdocs.org/stc/ST02500SE): The installation of the Garmin GDL-88 with the Flight Stream 210 to allow ADS-B(In) Flight Information Service Broadcast (FIS-B), independent of the ADS-B(Out) solution compliance. Butler National Corporation
- [STC SA1170GL](https://openairdocs.org/stc/SA1170GL): Except Model 55: Install Egan Aviation air ambulance stretcher P/N 125 using installation kit P/N 803, inverter/pump kit No. 808, 809, or 810. For Model 55, install air ambulance stretcher P/N 125 using installation kit P/N 804, medical oxygen system kit P/N 807, inverter/pump kit No. 808, 809, or810. Paul/ Lanna Egan LLC
- [STC ST02316LA](https://openairdocs.org/stc/ST02316LA): Installation of a Crane Aerospace & Electronics Tire Sensor Assembly. ELDEC Corporation
- [STC ST01734WI](https://openairdocs.org/stc/ST01734WI): Installation of an Emergency Pneumatic Reservoir Assembly, EAS P/N 1260001-02. EAS Corporation
- [STC ST03132CH](https://openairdocs.org/stc/ST03132CH): Installation of a single or dual Collins TDR-94/94D Mode S Transponder using existing control head, aircraft wiring, and antenna(s). Royal Air Inc
- [STC SA1489CE](https://openairdocs.org/stc/SA1489CE): Removal of 24-inch wide executive door and installation of 36-inch wide cargo door per AVCON Drawing List 36000 stamped FAA Approved with a date of May 8, 1979, July 3, 1980, November 15, 2010, or later approved revision for Learjet Models 25, 25A, 25B, 25C, 25D, 25F, 28, 29, 31, 31A, 35, 35A, 36, and 36A. Avcon Industries Inc
- [STC ST01195WI](https://openairdocs.org/stc/ST01195WI): Installation of Rosemount Pitot/Static Probes, altimeters, and associated equipment in Learjet 20 series aircraft to obtain Reduced Vertical Separation Minimum approval. Avcon Industries Inc
- [STC ST02540AT-D](https://openairdocs.org/stc/ST02540AT-D): Installation of replacement fuel tank sealant system. FFC Manufacturing
- [STC ST01842SE](https://openairdocs.org/stc/ST01842SE): Installation of a Sandel Avionics Horizontal Situation Indicator (HSI) and Attitude Direction Indicator (ADI). Butler National Corporation
- [STC SA30GL](https://openairdocs.org/stc/SA30GL): Installation of electronic engine synchronizer system. Ontic Engineering and Manufacturing Inc
- [STC SA1170CE](https://openairdocs.org/stc/SA1170CE): Stretcher installation in cabin area. Med-Flite of Midamerica Inc
- [STC ST01705NY](https://openairdocs.org/stc/ST01705NY): Installation must be in accordance with Section 1 of DECA Modification Summary MS02051, Rev 2, dated March 7, 2003. Logo Tech Manufacturing Inc
- [STC SA4918SW](https://openairdocs.org/stc/SA4918SW): Installation of windshield defog system. Jet East, Inc
- [STC SA3899WE](https://openairdocs.org/stc/SA3899WE): Installation of Collins F1S-84 Flight Instrument System. Learjet Inc
- [STC SA4218WE](https://openairdocs.org/stc/SA4218WE): Installation of Radio Corporation of America Primus-300SL Color Weather Radar System. Learjet Inc
- [STC SA4399NM](https://openairdocs.org/stc/SA4399NM): Installation of high frequency radio communications system. Learjet Inc
- [STC SA4403NM](https://openairdocs.org/stc/SA4403NM): Installation of third attitude indicator that meets the requirements of FAR 121.305(j). Learjet Inc
- [STC SA4433NM](https://openairdocs.org/stc/SA4433NM): Installation of communication and navigation systems electronic controls. Learjet Inc
- [STC SA4435NM](https://openairdocs.org/stc/SA4435NM): Installation of an emergency locator transmitter. Learjet Inc

### Approved for the engine (GE CJ-610-8A)

- [STC SE976SO](https://openairdocs.org/stc/SE976SO): Installation of an oil tank sight gauge on a G.E. oil tank, P/N6003T09P04. JSF Aviation Services Inc. Lists CJ610 Series
- [STC SE8674SW](https://openairdocs.org/stc/SE8674SW): Modification of the following engine oil tanks by adding a sight glass: 6002T03P01, 6002T03P03, 6003T09P01, 6003T09P02, 6003T09P03, 6003T09P04, 6003T89P01, 6003T89P02, 6003T03P02, 6002T03P04. Bizjet International Sales & Support Inc
- [STC SE1057SO](https://openairdocs.org/stc/SE1057SO): Installation of capacitance type probe with oil quantity indicating system in oil tank. Aircraft Equipment Certification Corporation. Lists CJ610 Series

## Related

- Other Gates Lear Jet 28 aircraft: https://openairdocs.org/model/gates-lear-jet-28/aircraft.md
- The GE CJ-610-8A engine: https://openairdocs.org/engine/ge-cj-610-8a.md

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