N2G

ISRAEL AIRCRAFT INDUSTRIES GULFSTREAM 200 · 2004 · Fixed-wing multi-engine · 2 engines · 19 seats · Valid Registration

Registered owner: PERFORMANCE AVIATION LLC, VA (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Dominion Aviation Services, Inc. (ODAA)Certificate holderMatched by certificate designator

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, 1998-10-15 – 2007-12-19.

FLT CONT AFFECTED · 2007-12-19 Matched by certificate designator
ATA 5510

Part: ACCESS PANEL — OUT OF ADJUST · airframe 3,457 hrs

PILOT REPORTED RUDDER PEDALS BINDING FOUND DURING PREFLIGHT, WITH RT PEDAL FORWARD AND LT PEDAL AFT. AFTER APPLYING PRESSURE TO PEDALS WITH FEET, PEDALS BECAME UNBOUND WITH POPPING NOISE HEARD. INSPECTED RUDDER SYSTEM. FOUND RUDDER BINDING AT PANEL SCREW FOR LOWER CONTROL COLUMN ACCESS, FORWARD, DUE TO BEND IN PANEL. REMOVED SCREWS AND ADJUSTED PANEL FOR BETTER CLEARANCE. REPLACED SCREWS WITH SHORTER VERSION OF SAME. RUDDER SYSTEM OPERATED NORMALLY. REFERENCE MM, CHAPTER 27.

Source: SDR ODAA121907001
VIBRATION/BUFFET · 2007-11-29 Matched by certificate designator
ATA 3246

Part: BEARING — LACK OF LUBE (NLG WHEEL) · airframe 3,442 hrs · 2,564 cycles

PILOT REPORTED NOSE WHEEL VIBRATION AFTER TAKEOFF ROTATION DURING CLIMBOUT. AIRCRAFT DIVERTED TO HOME BASE. NO REPORTED VIBRATION DURING TAKEOFF OR LANDING ROLL OUT. REMOVED LT AND RT NOSE WHEEL ASSEMBLIES. BALANCED LT AND RT NOSE WHEELS, INSPECTED AND REPACKED NOSE WHEEL BEARINGS.

Source: SDR 2G
OTHER · 1998-10-16 Matched by certificate designator
ATA 3460

Part: CDU — MALFUNCTIONED (COCKPIT)

CDU TRIPS BREAKER AT POWER-UP. SUBMITTER STATED FOURTH FAILURE OF THIS AIRCRAFT. AIRCRAFT TT: 187 HOURS. SUBMITTER STATED SUPPOSED TO BE FIXED BY 'MOD E', BUT HONEYWELL CANNOT SUPPLY THEM. THESE ALL ARE 'MOD C'.

Source: SDR 98ZZZX4130
OTHER · 1998-10-16 Matched by certificate designator
ATA 3460

Part: CDU — FAILED (COCKPIT)

FMS CDU FAILED ON POWER-UP. TOTALLY DEAD. SUBMITTER STATED THIRD FAILURE OF THIS PART ON THIS AIRPLANE. AIRCRAFT TT: 165.2 HOURS.

Source: SDR 98ZZZX4129
OTHER · 1998-10-15 Matched by certificate designator
ATA 3460

Part: CDU — FAILED (COCKPIT)

FMS CONTROLLED/DISPLAY UNIT TOTALLY DEAD. TEARDOWN SHOWED BAD POWER SUPPLY, PER HONEYWELL REP. SIMULTANEOUS FAILURE WITH OTHER SIDE. AIRCRAFT TT: 26.8 HOURS.

Source: SDR 98ZZZX4127