N198HB
Registered owner: ATI JET INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ATI Jet Inc. (G41A) | Certificate holder | — | Matched 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.
7 reports on file, 2005-05-21 – 2016-03-07.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 8,157 hrs · 5,803 cycles
DIVERTED BACK AFTER TAKEOFF, RT RED UNSAFE LG LIGHT REMAINS ON AFTER GEAR RETRACTION. UNABLE TO DUPLICATE DISCREPANCY. JACKED ACFT & APPLIED HYD POWER. CYCLED GEAR 10 TIMES WITH NO DISCREPANCIES NOTED. LOWERED INBD GEAR DOORS, CLEANED & LUBED DOOR MICRO SWITCHES. FLEXED MICRO SWITCH HARNESS WITH NO DISCREPANCIES NOTED. CYCLED GEAR 5 TIMES IAW AMM 32-30-00. OPERATIONS CHECKED NORMAL.
Part: UNKNOWN — ODOR (CABIN) · airframe 5,999 hrs · 4,403 cycles
(PART 91) BIRD STRIKE: WHILE ROTATING VR I PIC NOTICED A SMALL BIRD FLY DOWN LEFT SIDE OF ACFT. WHILE CLIMBING OUT AND ENTERING DOWNWIND, CREW NOTICED BURNING SMELL THAT LASTED A FEW SECONDS. TURNED OF CREW AND CABIN FANS AND SMELL WENT AWAY. CIRCLES AIRPORT AT 4500 AND ALL ENGINE INDICATIONS WERE NORMAL. CONTINUED ON TO DESTINATION (CMH) WITHOUT INCIDENT. AFTER SHUTDOWN, PIC INSPECTED ACFT FOR ANY DAMAGE AND NOTICED BIRD FEATHERS ON LH ENG FAN BLADES. MX C/A: BORESCOPE INSPECTION COMPLETED ON LH ENG, NO DEFECTS NOTED. ACCOMPLISHED POWER RECOVERY WASH, GROUND RUN AND ENGINE OPS CHECK GOOD.
Part: TRANSDUCER — CORRODED (ZONE 100) · airframe 4,363 hrs · 3,228 cycles
THE CREW NOTED ZERO HYDRAULIC PRESSURE FOLLOWED BY ERRATIC PRESSURE INDICATIONS ON THE HYDRAULIC PRESSURE GAUGE. THERE WAS NO INDICATION OF HYDRAULIC SYSTEM FAILURE DUE TO THE LACK OF THE ANNUNCIATOR LIGHT INDICATIONS. AFTER LOWERING THE FLAPS AND GEAR THE PRESSURE GAUGE STABILIZED AT 1700 PSI AND THE CREW DIVERTED TO FLL. UPON SUCCESSFUL LANDING AT FLL THE CREW TAXIED TO BOMBARDIER. BOMBARDIER TROUBLESHOT AND FOUND PRESSURE TRANSDUCER CORRODED. REMOVED AND REPLACED PRESSURE TRANSDUCER.
Part: SWITCH — STICKING (LT MLG ACTUATOR)
NO GEAR DOWN INDICATION (GREEN LIGHT). CYCLED GEAR, STILL NO DOWN AND LOCKED ON LT SIDE. NOSE AND RT OK. ACTIVATED EMERGENCY BLOW DOWN AND LIGHT CAME ON. MADE NORMAL LANDING. MAINT FOUND BALL AND SWITCH STICKING. LUBED AND ADJUSTED. (K)
Part: CONTROL UNIT — BURNED (CABIN) · airframe 3,746 hrs · 2,762 cycles
SMELLED ELECTRICAL ODOR, RECOG PULSE BREAKER POPPED, RETURNED TO CMH AIRPORT. UNIT BURNED INTERNALY, REPLACED UNIT, AND OPS CHECK NORMAL.
Part: RADOME — DEBONDED · airframe 2,975 hrs · 2,119 cycles
NOSE RADOME DELAMINATION LARGE AREA ON NOSE.REQUIRED OVERHAUL
Part: SUPPORT BRACKET — CRACKED (RUDDER) · airframe 2,257 hrs · 1,618 cycles
UPON REINSTALLATION OF RUDDER ASSY, FOUND RUDDER SUPPORT BRACKET AND STIFFENER ANGLE CRACKED UNDER RUDDER PRIMARY TRAVEL STOP AT FRAME STA 48. PROBABLE CAUSE: RUDDER OVER TRAVELING AGAINST PRIMARY STOP, WHEN GUST LOCK NOT INSTALLED AND WHEN PARKED OUTSIDE N WINDY CONDITIONS. REC: ENSURE FLIGHT CONTROL GUST LOCKS ARE INSTALLED WHEN PARKED OUTSIDE. (EA09200505204) (K)