# N280WA: 2022 Iai GULFSTREAM G280

- Status: Valid registration
- Airframe: [Iai GULFSTREAM G280](https://openairdocs.org/model/iai-gulfstream-g280) (registry code 4500314, 21 seats)
- Engine: [Honeywell AS907-2-1G](https://openairdocs.org/engine/honeywell-as907-2-1g) (registry code 33400)
- Data sheets: [TCDS A61NM](https://openairdocs.org/tcds/A61NM) (Gulfstream Aerospace LP), [TCDS E00010LA](https://openairdocs.org/tcds/E00010LA) (Honeywell Aerospace US LLC) (OpenAirDocs)
- Serial number: 2239
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 13, 2022
- Certificate issued: September 7, 2022
- Expires: September 30, 2029
- Mode S code: A2CFF0
- Registered owner: [Western Two LLC](https://openairdocs.org/faa-owner/WESTERN%20TWO%20LLC)
- Location: [Phoenix, AZ](https://openairdocs.org/faa-place/AZ/Phoenix)
- Owner type: LLC
- Owner's area on the map: 33.4516° N, 112.0699° W: Placed by OpenAirDocs at the center of ZIP code 85004, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=280WA
- Page: https://openairdocs.org/aircraft/N280WA

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): 10 in force

### Matched by airframe (Iai GULFSTREAM G280)

- [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 2026-09-04](https://openairdocs.org/ad/2026-09-04): Flight Controls · Gulfstream Aerospace LP Gulfstream G280. Effective Jun 12, 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 2023-04-02](https://openairdocs.org/ad/2023-04-02): Navigation · Gulfstream Aerospace LP Gulfstream G280. Effective Apr 7, 2023
- [AD 2021-17-14](https://openairdocs.org/ad/2021-17-14): Wings · Gulfstream Aerospace LP Gulfstream G280. Effective Oct 14, 2021
- [AD 2020-26-12](https://openairdocs.org/ad/2020-26-12): Flight controls · Gulfstream Aerospace LP Gulfstream G280. Effective Feb 1, 2021
- [AD 2020-15-02](https://openairdocs.org/ad/2020-15-02): Fuselage · Gulfstream Aerospace LP Gulfstream G280. Effective Aug 27, 2020
- [AD 2017-22-14](https://openairdocs.org/ad/2017-22-14): Navigation · Bombardier BD-100-1A10 (Challenger 300), BD-500-1A10, BD-500-1A11 and 13 more. Effective Dec 20, 2017

### Matched by engine (Honeywell AS907-2-1G)

- [AD 2023-24-04](https://openairdocs.org/ad/2023-24-04): Engine Fuel and Control · Honeywell International AS907-1-1A and AS907-2-1G. Effective Jan 10, 2024
- [AD 2018-04-13](https://openairdocs.org/ad/2018-04-13): Engine Controls Section · Honeywell International AS907-1-1A, AS907-2-1A, AS907-2-1G and 1 more. Effective Apr 12, 2018

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N280WA.

## FAA accident and incident reports

None matched to N280WA.

## 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 N280WA not matched to an aircraft (14)

They name N280WA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR WRLA97048](https://openairdocs.org/sdr/WRLA97048), Jul 6, 1997: TAILCONE. DAMAGED. DURING PERFORMANCE OF 'A' CHECK, REPAIR AGENCY PERSONNEL ATTEMPTED TO LOWER TAILCONE WHILE UPPER SAFETY HOOKS WERE STILL ENGAGED. ACTION DAMAGED TAILCONE ACTUAT
- [SDR WRLA97047](https://openairdocs.org/sdr/WRLA97047), Jul 6, 1997: BATTERY PACK. DISCHARGED. DURING FLIGHT CREW PREFLIGHT, FLIGHT CREW RECEIVED 'LOW BATT' ALERT WHEN PERFORMING EMERGENCY LIGHTING TEST. AIRCRAFT REMOVED FROM SERVICE FOR MAINTENANCE. MAIN
- [SDR WRLA97045](https://openairdocs.org/sdr/WRLA97045), Jul 2, 1997: HYD LINE. CRACKED. DURING INITIAL CLIMB-OUT, FLIGHT CREW NOTED THAT LANDING GEAR HANDLE WOULD NOT MOVED TO THE 'RETRACT' POSITION, PREVENTING THE LANDING GEAR FROM RETRACTING. FLI
- [SDR WRLA97025](https://openairdocs.org/sdr/WRLA97025), Jun 6, 1997: CIRCUIT BREAKER. TRIPPED. DURING TAXI, FLIGHT CREW WAS UNABLE TO PARALLEL BUS AFTER NR 3 ENGINE STA RT. AIRCRAFT RETURNED TO GATE. MAINTENANCE PERSONNEL DEPOWERED AIRCRAFT AND RESET CIRC
- [SDR WRLA97011](https://openairdocs.org/sdr/WRLA97011), Apr 1, 1997: OIL FILTER. CLOGGED. DURING APPROACH TO LANDING, FLIGHT CREW NOTED 'NR 1 ENGINE OIL FILTER CLOGGED' ALERT ON EAD. FLIGHT CREW PERFORMED ABNORMAL PROCEDURES, SHUTTING DOWN NR 1 ENGIN
- [SDR WRLA97009](https://openairdocs.org/sdr/WRLA97009), Feb 24, 1997: T-FITTING. LOOSE. DURING INITIAL CRUISE, FLIGHT CREW NOTED LOSS OF POTABLE WATER IN BOTH STORAGE TANKS. FLIGHT CREW ELECTED TO DIVERT AIRCRAFT TO WIKB FOR MAINTENANCE TROUBLE-SHO
- [SDR WRLA96035](https://openairdocs.org/sdr/WRLA96035), Sep 4, 1996: SELECTOR. BINDING. WHEN ON FINAL APPROACH AT EDDB, FLIGHT CREW SELECTED GEAR DOWN. ALL GEAR INDICATION UNSAFE. FLIGHT CREW UTILIZED ABNORMAL PROCEDURES EXTENDING LANDING GEAR, UTI
- [SDR WRLA96023](https://openairdocs.org/sdr/WRLA96023), May 19, 1996: FUEL PUMP. LEAKING. AIRCRAFT SUSTAINED A 'HARD-LANDING' WRSJ. DURING MM REQUIRED INSPECTION, FUEL LEAK NOTED AT FUEL BOOST AND TRANSFER PUMPS (4 EACH) ON NR 1 AND NR 3 FUEL TANKS. 
- [SDR WRLA96006](https://openairdocs.org/sdr/WRLA96006), Feb 1, 1996: TRANSDUCER WIRE. BROKEN. ON TAXIING OUT, FLIGHT CREW RECEIVED A NR 3 TIRE PRESSURE/WHEEL TRANSDUCER ALERT. LEVEL 2. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE DISCO
- [SDR WRLA95041](https://openairdocs.org/sdr/WRLA95041), Sep 25, 1995: HYD PUMP. INOPERATIVE. AS AIRCRAFT TAXIED TO THE RUNWAY AT LAX, THE FLIGHT CREW EXPERIENCED A FAILURE OF THE NR 3 HYDRAULIC SYSTEM. THE CAPTAIN ELECTED TO RETURN TO THE GATE. MAINTENA
- [SDR WRLA95033](https://openairdocs.org/sdr/WRLA95033), Jul 2, 1995: SHUT-OFF VALVE. FAILED. DURING TAXI, CREW RECEIVED 2/3 HYDRAULIC REVERSIBLE MOTOR PUMP DISAGREE ALERT. FLIGHT CREW ELECTED TO RETURN TO GATE. AIRCRAFT RETURNED WITHOUT INCIDENT. MAINTE
- [SDR WRLA95031](https://openairdocs.org/sdr/WRLA95031), Jun 14, 1995: INTERLOCK CYL. FAILED. AFTER TAKEOFF, CAPTAIN OBSERVED LANDING GEAR WOULD NOT RETRACT. CAPTAIN ELECTED TO RETURN TO AIRPORT OF DEPARTURE. AIRCRAFT RETURNED TO BLOCKS WITHOUT FURTHER I
- [SDR WRLA95026](https://openairdocs.org/sdr/WRLA95026), May 1, 1995: DETECTOR. BROKEN. DURING INITIAL CRUISE, APPROXIMATELY 2 HOURS AFTER TAKEOFF, NR 1 ENGINE 'FIRE DETECTION' FAIL ANNUNCIATED. FLIGHT CREW ELECTED TO DIVERT TO ALTERNATE AIRPORT. A
- [SDR WRLA95025](https://openairdocs.org/sdr/WRLA95025), May 1, 1995: FIRE LOOP. LOOSE. DURING INITIAL CRUISE, APPROXIMATELY 1.5 HOURS AFTER TAKEOFF, NR 1 ENGINE 'FIRE DETECTION' FAIL ANNUNCIATED. FLIGHT CREW ELECTED TO RETURN TO DEPARTURE AIRPORT.

## STCs that may be installed (OpenAirDocs) (12)

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 (Iai GULFSTREAM G280)

- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST12191IB](https://openairdocs.org/stc/ST12191IB): Installation of the Gogo Galileo HDX. Sky Service F.B.O. Inc
- [STC ST04560AT](https://openairdocs.org/stc/ST04560AT): Replacement of the existing Honeywell HTF7000 engine upper and lower thrust reverser door assemblies with Quiet Technology Aerospace modified upper and lower thrust reverser door assemblies. Quiet Technology Aerospace
- [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST04339AT-D](https://openairdocs.org/stc/ST04339AT-D): Installation of Air Ionizer System. Gulfstream Aerospace Corporation
- [STC ST01011DE](https://openairdocs.org/stc/ST01011DE): Demonstration of Aircraft Compatibility to Wireless Fidelity (WiFi) Data Transmissions (Ground & Flight). West Star Aviation
- [STC ST04272AT-D](https://openairdocs.org/stc/ST04272AT-D): Installation of an XM Satellite Weather Receiver and Antenna. Gulfstream Aerospace Corporation
- [STC ST04288AT-D](https://openairdocs.org/stc/ST04288AT-D): Activation of Future Air Navigation System (FANS) software function. Gulfstream Aerospace Corporation
- [STC ST04271AT-D](https://openairdocs.org/stc/ST04271AT-D): Installation of a Jump Seat. Gulfstream Aerospace Corporation
- [STC ST04274AT-D](https://openairdocs.org/stc/ST04274AT-D): Installation of Rockwell Collins Second IFIS. Gulfstream Aerospace Corporation
- [STC ST11931IB](https://openairdocs.org/stc/ST11931IB): Installation of Gogo AVANCE L5/LX5 System. Sky Service F.B.O Inc

## Related

- Other Iai GULFSTREAM G280 aircraft: https://openairdocs.org/model/iai-gulfstream-g280/aircraft.md
- The Honeywell AS907-2-1G engine: https://openairdocs.org/engine/honeywell-as907-2-1g.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.