N199GA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| GULFSTREAM INT'L AIRLINES | Operator | on 2000-03-18 | Operator named in NTSB report |
Accident & incident history
Operated by GULFSTREAM INT'L AIRLINES (per NTSB report)
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.
16 reports on file, 1995-10-30 – 2001-12-05.
Part: COWLING — CRACKED (NACELLE)
SEVERAL CRACKS WERE FOUND ON THE INSIDE OF THE AIR INLET COWL (HOT LIP) THESE CRACKS RUN HORIZONTALLY AND VERTICALLY ALONG THE WELD THE POSSIBLE CAUSE MIGHT BE THE HARMONICS OF THE VIBRATIONS FROM THE ENGINE AND PROPELLER. POSSIBLY GOING TO A THICKER GAUGE OF METAL MIGHT STRENGTHEN THE AREA SINCE HIGH TEMPERATURES AND VIBRATIONS ARE FOUND IN THE AREA.
Part: HINGE BRACKET — CORRODED (RT STABILIZER)
DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M)
Part: HINGE BRACKET — CORRODED (ELEVATOR)
DURING SCHEDULED MAINTENANCE, LEFT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR CENTER HINGE BRACKET. (M)
Part: HINGE BRACKET — CORRODED (ELEVATOR)
DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M)
Part: HINGE BRACKET — CORRODED (LT STABILIZER)
DURING SCHEDULED MAINTENANCE, LEFT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR CENTER HINGE BRACKET. (M)
Earlier reports · 1995–1999 · 11 reports
1999
Part: POWER PACK — FAILED (LANDING GEAR)
FLT 9332 - EYW-TPA - LANDING GEAR CIRCUIT BREAKER POPPED IN FLIGHT. RESET AND POPPED AGAIN. EXTENDED GEAR VIA ALTERNATE GEAR EXTENSION PROCEDURES. REPLACED POWER PACK MOTOR. PERFORMED SATISFACTORY LANDING GEAR RETRACTION/EXTENSION CHECKS. (M)
1997
Part: CIRCUIT BREAKER — TRIPPED (LANDING GEAR)
MIA/TPA - FLT 7405 - GEAR CIRCUIT BREAKER TRIPPED IN FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. FERRIED AIRCRAFT TO MIA. SERVICED HYDRAULIC SYSTEM WITH AIRCRAFT ON JACKS. PERFORMED EXTENSION AND RETRACTION. NO DEFECTS NOTED.
Part: WIRE — CHAFED (RIGHT MLG)
FLT 483 - MIA-MCO - LANDING GEAR INDICATOR CIRCUIT BREAKER TRIPPED ON IN FLIGHT. REPAIRED CHAFED WIRES AT RIGHT MLG UPLOCK SWITCH. OPS CHECKED GOOD ON JACKS. (M)
Part: BUSHINGS — WORN (NLG DRAG BRACE)
FLT 167 - EYW-TPA - LANDING GEAR CIRCUIT BREAKER POPS OUT WHEN LANDING GEAR IN TRANSIT DURING BOTH EXTEND AND RETRACT. CIRCUIT BREAKER WILL NOT RESET ONCE GEAR IS LOCKED UP BUT CIRCUIT BREAKER WILL RESET WHEN GEAR LOCKED DOWN. REMOVED AND REPLACED NOSE GEAR DRAG BRAKE BUSHINGS. SWUNG GEAR. OPS CHECK SATISFACTORY ON JACKS. (M)
Part: BRACKETS — CORRODED (LT/RT ELEVATOR)
AT SCHEDULED EMPARAGE INSPECTION, DETERMINED BOTH LEFT AND RIGHT ELEVATOR OUTBOARD HINGE ATTACH BRACKETS TO BE EXFOLIATED. REPLACED OUTBOARD HINGE ATTACH BRACKETS FOR LEFT AND RIGHT ELEVATORS. (M)
1996
Part: DIODE — SHORTED (LANDING GEAR)
FLT 401 - MCO-TPA - GEAR WARNING HORN CAN NOT BE SILENCED WHEN POWER IS REDUCED. RESOLDERED BROKEN WIRE TO, AND REPLACED, BLOCKING DIODE CR109.
Part: PC BOARD — SHORTED (LANDING GEAR)
FLT 153A - PBI-MIA - GEAR WARNING HORN CANNOT BE SILENCED WHEN POWER IS PULLED BACK FOR DESCENT. REPLACED E175 PC BOARD. GEAR SWING AND OPS CHECK GOOD. AIRCRAFT RELEASED FOR SERVICE. (M)
Part: AIR DISTR — SMOKE (COCKPIT)
FLT 398A - FLL-MIA - SMOKE COMING OUT OF CAPTAIN AND FIRST OFFICERS ACM VENTS IN FLIGHT. LASTED ABOUT 10 SECONDS. PERFORMED GROUND RUN UP NO SMOKE NOTED. OPERATED ALL SYSTEMS NO DEFECTS NOTED. POSSIBLE CONDENSATION FROM THE AIR CYCLE MACHINE AIR CONDITIONING SYSTEM VENTS.
Part: POWER LEVER — OUT OF ADJUST (COCKPIT)
FLT 408 - TPA-MIA - GEAR WARNING HORN WILL NOT SILENCE WITH BUTTON WHEN POWER IS REDUCED BELOW 84-89 PERCENT N1 (GEAR UP). ADJUSTED POWER LEVER SWITCHES IAW MM 32-60-00. (M)
Part: ENGINE — FAILED (LEFT)
FLT 410 - FPO-MIA - ON CLIMB-OUT FROM FPO, ODORAND SMOKE EMULATING FROM THE FLOOR OF THE COCKPIT. LEFT ENGINE INDICATIONSWERE ERRATIC, SHUTDOWN LEFT ENGINE. RELIEVED CABIN PRESSURE TO EVACUATERESIDUAL SMOKE. DECLARED AN EMERGENCY, RETURNED TO FPO AND LANDED WITHOUTFURTHER INCIDENT. REMOVED AND REPLACED THE LEFT POWER PLANT ASSEMBLY ANDROUTED THE REMOVED UNIT TO OVERHAUL VENDER FORANALYSIS.
1995
Part: RETRACT MECH — FAILED (LANDING GEAR)
FLT NR 479 - TPA-MIA - LANDING GEAR FAILED TO EXTEND, BREAKER POPPED. INSPECTED HYDRAULIC SYSTEM, ACCUMULATION SYSTEM AND ELECTRICAL SYSTEM NO DEFECTS NOTED. SWUNG GEAR ON JACKS NO DEFECTS NOTED.