N350GR

RAYTHEON AIRCRAFT COMPANY B300 · 2001 · Fixed-wing multi-engine · 2 engines · 19 seats · Valid Registration

Registered owner: JULIET BRAVO INC, TX (owner ≠ operator)

Operators of this aircraft

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

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

5 reports on file, 2011-09-21 – 2017-04-10.

OTHER · 2017-04-10 Matched by certificate designator
ATA 6320

Part: BOLT — LOOSE (EPICYCLIC/MAST) · airframe 6,975 hrs · 23,905 cycles

UPON REMOVAL OF THE EPICYCLIC ASSEMBLY FROM THE MAST IT WAS DISCOVERED THAT THE EPICYCLIC / MAST BOLTS (6EA) HAD BECOME LOOSE. THE 6 BOLTS ARE HELD IN PLACE BY 3 STAINLESS STEEL DOUBLE LOCKING TAB WASHERS AND DOUBLE LOCKED WITH A SPECIAL STAR WASHER. THE BOLT HOLDING THE STAR WASHER IN PLACE WAS PROPERLY SAFETIED AND APPEARED TO BE TORQUED.

Source: SDR 2017F00059
OTHER · 2017-04-04 Matched by certificate designator
ATA 6230

Part: MAST — LOOSE (MAIN ROTOR) · airframe 6,974 hrs · 23,905 cycles

DURING TBO REMOVAL OF EPICYCLIC GEAR FOUND THAT THE 6 MAST?EPICYCLIC BOLTS (P/N 350A37-1024-20) WHERE NOT TORQUED. CONTACTED AIRBUS HELICOPTERS TECH REP AND WAS REFERED TO SAFETY INFORMATION NOTICE NO. 2899-S-62, UPON FURTHER INSPECTION PER SIN FOUND THAT THE MAIN ROTOR MAST GROVE HAD WORN PAINT AS DID THE PHONIC WHEEL.

Source: SDR QMLA2017040417033
OTHER · 2015-07-08 Matched by certificate designator
ATA 5320

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 6,299 hrs · 20,192 cycles

CRACKS FOUND ON THE STRUCTURE WHERE THE NIGHT SCANNER IS MOUNTED. THE FWD CRACK IS APPROX 6 INCHES LONG, AT APPROX STATION 655, STARTING AT LBL 4" & ENDING AT RBL 2". THE CTR CRACK IS 0.5 INCHES LONG, ABOUT AN INCH AFT OF THE FWD CRACK, AT LBL 6". THE AFT TWO CRACKS ARE 0.5 INCHES LONG, ABOUT 12 INCHES AFT OF THE FWD CRACK, ONE AT LBL 2" & THE OTHER AT RBL 2".

Source: SDR QMLA2015070815055
OTHER · 2014-10-20 Matched by certificate designator
ATA 6220

Part: ADAPTER — CRACKED (MAIN ROTOR) · airframe 6,079 hrs · 18,969 cycles

FREQUENCY ADAPTER IS CRACKED ON THE YELLOW BLADE.

Source: SDR QMLA2014102014124
OTHER · 2011-09-21 Unresolved
ATA 7700

Part: INDICATOR — DAMAGED (NG) · airframe 5,132 hrs · 16,129 cycles

NG INDICATOR DIGITAL READOUT IS DIFFICULT TO READ IN DAYLIGHT CONDITIONS.

Source: SDR 2011FA0000616