- Registered owner
- Arrow Plane Lc
- Location
- Provo, UT
- Owner type
- LLC
- Serial number
- 5168
- Year built
- 2007
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 21, 2007
- Certificate issued
- February 7, 2008
- Expires
- September 30, 2029
- Mode S code
- A6A6B4
Gulfstream Aerospace GV-SP (G550)TCDS A12EAAirframe · Gulfstream Aerospace GV-SP (G550)TCDS E00057ENEngine · Rolls-Royce Deutschland BR700-710C411
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 28
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2004 | 1 |
|---|---|
| 2005 | 2 |
| 2006 | 5 |
| 2007 | 1 |
| 2009 | 1 |
| 2011 | 2 |
| 2012 | 2 |
| 2013 | 3 |
| 2014 | 2 |
| 2016 | 3 |
| 2017 | 2 |
| 2018 | 1 |
| 2021 | 1 |
| 2022 | 2 |
| 2023 | 4 |
| 2025 | 1 |
| 2026 | 1 |
Airframe · Gulfstream Aerospace GV-SP (G550)
AD 2026-13-02NavigationAD 2023-10-02Indicating/Recording System, NavigationAD 2023-02-02Landing Gear SystemInformation bulletins that may apply · 3
Advisory, not mandatory.
Airframe · Gulfstream Aerospace GV-SP (G550)
SAIB CE-19-20Flight Compartment WindowsSAIB NM-10-13Navigation: Flight Management SystemSAIB NM-10-12Navigation: Flight Management SystemNTSB investigations
No NTSB investigations matched to N528APMatched 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 Gulfstream Aerospace GV-SP (G550) aircraft
FAA incident reports
No FAA accident or incident reports matched to N528APMatched 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 Gulfstream Aerospace GV-SP (G550) aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR K5SR2019061129337Control Unit · failedRIGHT WINDSHILED STOPPED HEATING AFTER 45 TO 60 MIN WITH NO CASS MESSAGE OF FAILURESDR K5SR2016T27503Socket · burnedWHILE PERFORMING AN AIRCRAFT SERVICE CHECK, FOUND EXTERIOR LOGO LIGHTS INOPERATIVE. PERFORMED TROUBLESHOOTING AND FOUND THAT THE P3 AND J3 PLUG AND CONNECTOR HAD SHORTED AT PIN DD AND MELTED THE PIN AND FEMALE PIN RECEPTACLE. CONNECTOR AND PLUG ARE LOCATED INSDR K5SR2015112327126Brake Assy · crackedWHILE PERFORMING THE NR 1 AND NR 2 WHEEL AND TIRE CHANGE. UPON REMOVING THE WHEEL ASSEMBLIES FROM THE ACFT FOUND NR 1 AND NR 2 BRAKE ASSEMBLY CARBON ROTOR ASSEMBLIES TO BE CRACKED AND BROKEN OFF FROM THE KEY WAY GUIDES IN SEVERAL PLACES. R & R NR 1 AND NR 2 SDR K5SR2014092426219Elbow · crackedWHILE PERFORMING A SERVICE CHECK ON THE ACFT, NOTICED HYDRAULIC FLUID LEAKING FROM THE LT MLG WHEEL WELL. ON FURTHER INVESTIGATION, FOUND AUXILARY SYS SUCTION LINE LEAKING. REMOVED LINE ASSY AND FOUND 90 DEGREE ELBOW CRACKED. R & R SUCTION LINE AND 90 DEGRESDR 2010FA0000759Cable · damaged(K5SR) WHILE PERFORMING A 500 HR/12 MONTH INSP ON THE LT ENGINE, DISCOVERED THE EMERGENCY FUEL SHUTOFF CABLE HAD UN-TWISTED AT THE CABLE END GOING FROM THE FUEL SHUTOFF VALVE. R & R WITH NEW CABLE ASSY. OPD CKD SATISFACTORY.SDR B8M2009F00000Connector · unsecureWHILE PERFORMING CMP 27301 RUDDER SYS HARD-OVER PREVENTION SYS OPS TEST. FOUND THAT SYS FAILED CHECK. TROUBLESHOOTING THE SYS FOUND CONNECTOR PLUG NR 155A26P3 PIN NR 3 GOING TO RUDDER HARD OVER SWITCHES WAS NOT LOCKED INTO PLUG ASSY. RESECURED PIN NR 3 INTO
STCs that may be installed · 486
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.