- Registered owner
- Hawker 800xp LLC
- Location
- Fort Lauderdale, FL
- Owner type
- LLC
- Serial number
- 258570
- Year built
- 2002
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 16, 2002
- Certificate issued
- April 13, 2021
- Expires
- April 30, 2028
- Mode S code
- A70ABE
Raytheon HAWKER 800XPTCDS A3EUAirframe · Raytheon HAWKER 800XPTCDS E6WEEngine · Garrett TFE731 series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Garrett TFE731 model are included below.
On this page
Airworthiness directives that may apply · 70
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 5 |
|---|---|
| 1975 | 1 |
| 1978 | 1 |
| 1980 | 1 |
| 1982 | 1 |
| 1983 | 1 |
| 1986 | 1 |
| 1989 | 1 |
| 1990 | 2 |
| 1992 | 1 |
| 1993 | 1 |
| 1994 | 3 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 4 |
| 1998 | 3 |
| 1999 | 2 |
| 2000 | 4 |
| 2001 | 7 |
| 2002 | 1 |
| 2003 | 4 |
| 2004 | 2 |
| 2005 | 5 |
| 2006 | 5 |
| 2007 | 1 |
| 2008 | 4 |
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 1 |
| 2012 | 1 |
| 2013 | 1 |
| 2014 | 2 |
| 2016 | 1 |
| 2023 | 1 |
| 2026 | 1 |
Airframe · Raytheon HAWKER 800XP
AD 2026-13-02NavigationAD 2023-10-02Indicating/Recording System, NavigationAD 2014-15-08FuelInformation bulletins that may apply · 6
Advisory, not mandatory.
Airframe · Raytheon HAWKER 800XP
SAIB AIR-21-15R1Navigation SystemSAIB CE-20-10Air Distribution System: Loss of Cabin PressureSAIB NM-15-24Landing GearSAIB NM-14-05Wing: AileronsSAIB NM-11-60Landing GearEngine · Garrett TFE731 series
SAIB NE-06-70Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N553BWMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Raytheon HAWKER 800XP aircraft
FAA incident reports
No FAA accident or incident reports matched to N553BWMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Raytheon HAWKER 800XP aircraft
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EXFA2025FA0000730Warning Message · false activationUPON REDUCING POWER FOR DESCENT FLIGHT CREW NOTICED HYDRAULIC LOW PRESSURE LIGHTS ON. COULD NOT DUPLICATE ON THE GROUND.SDR 2025FA0000730Hydraulic System · low pressure#1 AND #2 HYDRAULIC LOW PRESSURE LIGHT ON. HYDRAULIC @ 2300PSI. PERFORMED GEAR FREE LANDING PROCEDURE.SDR EXFA2025120800728Pipe · crackedWHILE IN CRUISE FLIGHT, CREW NOTED HYDRAULIC LOW PRESSURE LIGHTS ON, ENGINES 1 AND 2 WITH A HYDRAULIC PRESSURE OF 2300 PSI. CREW DIVERTED TO AN ALTERNATE AIRPORT EXTENDING LANDING GEAR MANUALLY PRIOR TO LANDING.SDR 2025FA0000728Hydraulic Line · leakingHYDRAULIC LOW PRESSURE LIGHTS #1 AND #2 FLIGHT LIGHTS IN HYDRAULIC PRESSURE INDICATOR READ 2300 PSI. CREW PERFORMED FREEFALLING LANDING GEAR PROCEDURE.SDR 2025FA0000729Instrument Panel · faultedSTANDBY INSTRUMENT INOPSDR 9JLA2014042106478Relief Valve · leakingDURING ACFT FUELING IT WAS NOTED THAT FUEL WAS LEAKING FROM THE SPPR PRESS RELIEF VLV. THE VLV WAS R & R WITH AN OVERHAULED UNIT, OFF PN 1159000-1, SN FR024BM.SDR 9JLA2013081606462Accumulator · leakingTHE FLIGHT CREW REPORTED THAT DURING PREFLIGHT CHECKS, HYD FLUID WAS NOTED LEAKING IN THE REAR EQUIPMENT BAY. MX FOUND THE RESERVOIR WAS VENTING TO THE OVERBOARD DRAIN AND IDENTIFIED THE NORMAL ACCUMULATOR PRESSURE TO BE LOW AND LEAKING INTERNALLY INTO THE RESSDR 9JLA2013052206457Valve · leakingPRESSURE FUEL SERVICING VALVE WAS LEAKING. VALVE REPLACED WITH AN INSPECTED UNIT. FUNCTIONAL AND LEAK CHECKED SATISFACTORY.SDR 9JLA2013011803545Indicator · defectiveDURING THE POST FLIGHT INSPECTION, THE NR 1 ENGINE OIL FILTER BYPASS INDICATOR WAS NOTED IN THE BYPASS POSITION. A SOAP WAS TAKEN AND RESULTS WERE NORMAL. THE BYPASS INDICATOR, PN 3070246-4 ON THE ENGINE WAS SUSPECT TO BE DEFECTIVE AND WAS REPLACED IAW SB TFSDR 9JLA2013011803542Inverter · defectiveTHE CREW REPORTED THAT NR 2 INVERTER FAILED DURING FLIGHT. TROUBLESHOOTING IDENTIFIED THE NR 2 INVERTER DEFECTIVE. THE DEFECTIVE INVERTER WAS REMOVED AND A REPAIRED UNIT WAS INSTALLED. FUNCTIONAL CHECKED SATISFACTORY. ACFT WAS RETURNED TO SERVICE.SDR 9JLA2012073103534Sensor · defectiveTHE CREW REPORTED THAT DURING THE POST FLIGHT CHECKS, THE STALL CHANNEL 1 AND 2 WILL NOT IDENT. TROUBLESHOOTING IDENTIFIED THE F3 FUSE AS BEING OPEN BECAUSE OF HIGH RESISTANCE IN THE RT AIRFLOW SENSOR PN 1703-12, SN 1569. THE AIRFLOW SENSOR AND THE FUSE WERE RSDR 9JLA2012052303524Fuel Control · defectiveLT ENGINE WOULD NOT GO TO IDLE THRUST WITH THROTTLE LEVER IN THE IDLE POSITION. TROUBLESHOOTING IDENTIFIED THE ENGINE FUEL CONTROL WAS DEFECTIVE. INSTALLED A REPAIRED UNIT. FUNCTIONAL CHECKED SATISFACTORY.
STCs that may be installed · 285
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Raytheon HAWKER 800XP
STC ST01305WI-DModification 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.STC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.STC ST12360WIInstallation of the Gogo Wi-Fi System, AVANCE L3 or AVANCE L5,