N528AP

GULFSTREAM AEROSPACE GV-SP (G550) · 2007 · Valid Registration

Registered owner: ARROW PLANE LC, UT (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
ELEVATE JET, LLC (B8MA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

O · 2019-06-04 Matched by certificate designator
ATA 3040

RIGHT WINDSHILED STOPPED HEATING AFTER 45 TO 60 MIN WITH NO CASS MESSAGE OF FAILURE

Source: SDR K5SR2019061129337 · FAA SDRS
O · 2016-05-02 Matched by certificate designator
ATA 3340

WHILE 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 IN LT ELECTRONIC EQUIPMENT RACK, LEER, REF DES 327VB49. P3 AND J3 CONNECTOR AND PLUG ASSY WERE R & R. OPS CHECK OF LOGO LIGHTS WERE SATISFACTORY.

Source: SDR K5SR2016T27503 · FAA SDRS
O · 2015-11-20 Matched by certificate designator
ATA 3240

WHILE 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 BRAKE ASSEMBLIES.

Source: SDR K5SR2015112327126 · FAA SDRS
K · 2014-09-18 Matched by certificate designator
ATA 2920

WHILE 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 DEGREE FITTING WITH NEW PARTS. LEAK CHECKED SATISFACTORY.

Source: SDR K5SR2014092426219 · FAA SDRS
O · 2010-07-14 Matched by certificate designator
ATA 7603

(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.

Source: SDR 2010FA0000759 · FAA SDRS
O · 2009-11-04 Matched by certificate designator
ATA 2720

WHILE 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 CONNECTOR PLUG 155A26P3 AND PERFORMED RUDDER HARD-OVER PREVENTION CHECK. WITH SATISFACTORY RESULTS. (K)

Source: SDR B8M2009F00000 · FAA SDRS