N195GA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Alpine Aviation, Inc. (TIMA) | Operator | on 2008-05-23 | Operator named in NTSB report |
Accident & incident history
Operated by ALPINE AVIATION INC (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.
23 reports on file, 1995-10-31 – 2005-11-04.
Part: CIRCUIT BOARD — SHORTED (MLG)
THE GEAR HANDLE PLACED IN THE DOWN POSITION, GEAR FAILED TO GO DOWN AND THE CIRCUIT BREAKER POPPED. FOLLOW INSPECTION, FOUND A BROKEN WIRE. (K)
Part: LINE — LEAKING (LT WING HYD)
NOSE GEAR WARNING LIGHT ILLUMINATED WHEN LANDING GEAR EXTENDED. GEAR DEPLOYED AFTER 15 TO 20 SECONDS. PROBLEM WAS A LEAK IN THE HYDRAULIC LINE. THE LINE DEVELOPED A PIN HOLE LEAK BECAUSE OF CORROSION FROM THE INSIDE OF THE LINE. (K)
Part: LINE — LEAKING (HYDRAULIC SYS)
NOSE GEAR WARNING LIGHT ILLUMINATED WHEN LANDING GEAR EXTENDED. GEAR DEPLOYED AFTER 15 TO 20 SECONDS. PROBLEM WAS A LEAK IN THE HYDRAULIC LINE. THE LINE DEVELOPED A PIN HOLE LEAK BECAUSE OF CORROSION FROM THE INSIDE OF THE LINE. (K)
Earlier reports · 1995–2003 · 20 reports
2003
Part: BULKHEAD — CRACKED (FUSELAGE)
BULKHEAD FOUND TO BE CRACKED AT INSPECTION. (CNTRL NR 81)
2001
Part: CONTROL CABLE — DEFECTIVE (T/E FLAP)
INSPECTION OF FLAP CABLES AS OUTLINED IN MFG SB AS REQUIRED BY AD REVEALED THE LEFT OUTBOARD FLAP CABLE DEFECTIVE. THE CABLE HAD STARTED TO UNWIND.
Part: PANEL — DEBONDED (LT WING)
LEFT INBOARD UPPER WING PANEL AFT OF WING SPAR DE-BONDING BETWEEN UPPER WING SKIN AND HONEYCOMB INSIDE FUEL BAY AREA.
Part: TRIM TAB — CORRODED (RUDDER)
RUDDER TAB HORN, CORRODED
Part: TRIM TAB — CORRODED (LT ELEVATOR)
ELEVATOR TRIM TAB HORN CORRODED
2000
Part: BULKHEAD — CRACKED (FUSELAGE)
UPON INSPECTION OF THE INTERIOR SIDE WALL, A CRACK WAS FOUND. THE CRACK WAS LOCATED ON BULKHEAD 273 AT THE BEND ON THE BULKHEAD. THE CRACK WAS APPROXIMATELY ONE INCH IN LENGTH. REFER TO THE ATTACHED PICTURE. (X)
Part: RELAY — STUCK (LT NACELLE)
FLT 9493 - MIA-FLL - LANDING GEAR RELAY HAD A RINGING NOISE AND BURNING SMELL, RELAY POPPED. REMOVED AND REPLACED K3 RELAY. OPERATIONAL CHECK GOOD. (M)
1998
Part: KEEL WEB — DAMAGED (LT NACELLE)
AT SCHEDULED INSPECTION, DETERMINED THE LEFT NACELLE INBOARD KEEL ASSEMBLY TO FAIL CONDUCTIVITY TEST PER RAYTHEON SERVICE BULLETIN 54-3071 PART 2, VISUAL INSPECTIONS PROVED SATISFACTORY PER PART 1 OF SAME BULLETIN. SCHEDULED REPETITIVE VISUAL INSPECTIONS UNTIL KEEL IS REPLACED. SCHEDULED KEEL REPLACEMENT PER RAYTHEON SERVIEC BULLETIN 54-3071. (M)
Part: KEEL — DAMAGED (LT NACELLE)
AT SCHEDULED INSPECTION, DETERMINED THE LEFT NACELLE INBOARD KEEL ASSEMBLY TO FAIL CONDUCTIVITY TEST PER RAYTHEON SERVICE BULLETIN 54-3071 PART II. VISUAL INSPECTIONS PROVED SATISFACTORY PER PART I OF SAME BULLETIN. SCHEDULED REPETITIVE VISUAL INSPECTIONS UNTIL KEEL IS REPLACED. SCHEDULED KEEL REPLACEMENT PER RAYTHEON SB 54-3071. (X)
Part: KEEL WEB — DAMAGED (RT NACELLE)
AT SCHEDULED INSPECTION DETERMINED THE RIGHT NACELLE INBOARD KEEL ASSEMBLY TO FAIL CONDUCTIVITY TEST PER RAYTHEON SERVICE BULLETIN 54-3071 PART 2. VISUAL INSPECTIONS PROVED SATISFACTORY PER PART 1 OF SAME BULLETIN. SCHEDULED REPETITIVE VISUAL INSPECTIONS UNTIL KEEL IS REPLACED. SCHEDULED KEEL REPLACEMENT PER RAYTHEON SERVICE BULLETIN 54-3071. (M)
1997
Part: ACTUATOR — FAILED (RT MLG)
FLT 7476 - MCO-MIA - WHEN GEAR IS RETRACTED RED HANDLE STAYS ILLUMINATED. RIGHT MAIN STAYS STUCK IN TRANSIT. DUE TO WEATHER IN MCO, FLT CONTINUED TO MIA WITH GEAR DOWN. REMOVED AND REPLACED RIGHT MAIN GEAR ACTUATOR. (M)
Part: FIRE LOOP — OUT OF POSITION (LT ENGINE)
FLT 7188 - MCO-FLL - LEFT T-HANDLE ILLUMINATED IN FLIGHT. REPOSITIONED FIRE LOOP AWAY FROM EXHAUST STACK.
Part: FIRE LOOP — OUT OF POSITION (LT ENGINE)
MCO/FLL - FLT 7188 - PILOT REPORT: LEFT T-HANDLE ILLUMINATED IN-FLIGHT. REPOSITIONED FIRE LOOP AWAY FROM EXHAUST STACK.
Part: BLAST TUBE — BROKEN (RT LIPHEAT)
FLT 471 - ON TAKEOFF, RIGHT FIREWALL T-HANDLE ILLUMINATED AT 90 KNOTS. REPLACED INLET LIPHEAT BLAST TUBE. OK FOR SERVICE.
Part: TUBE ASSY — CRACKED (RT ENG PY LINE)
FLT - 402 - TPA-MIA - RIGHT ENGINE WENT TO ZERO TORQUE IN FLIGHT. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO TPA. DETERMINED PY AIR LINE TO BE CRACKED. REPLACED PY AIR LINE. REPLACED ISOLATOR MOUNTS AND CHECKED PROPELLER DYNAMIC BALANCING. AIRCRAFT RELEASED TO SERVICE. (M)
Part: GEAR HANDLE — NOT STOWED (LANDING GEAR)
FLT 194 - PBI-JAX - AT POSITIVE RATE, GEARUP, GEAR HANDLE COMES UP INTRANSIT. LIGHTS EXTINGUISH BUT GEAR REMAINS DOWN AND 3 GREEN THEN RELAY CIRCUIT BREAKER POPS. DETERMINED EMERGENCY EXTENSION HANDLE NOT PROPERLY STOWED. REST HANDLE, OPS CHECK SATISFACTORY ON JACKS AND TEST FLIGHT. (M)
Part: FIRE LOOP — FAILED (RIGHT)
FLT 410 - FPO-MIA - DURING TAKEOFF, RIGHT FIRE PULL HANDLE ILLUMINATED. REMOVED AND REPLACED RIGHT FORWARD FIRE LOOP. OP CHECKED GOOD. (M)
1996
Part: CLAMP — LOOSE (HEATER)
FLT 162 - MIA-TCB - RIGHT 'T' HANDLE ILLUMINATED FOR 2 SECONDS WHEN MAX TAKEOFF POWER WAS APPLIED. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. RESECURED CLAMP ON HEATER TUBE INLET. (M)
Part: UPLOCK SW — OUT OF ADJUST (LANDING GEAR)
FLT 393 - MIA-DAB - LANDING GEAR HANDLE LIGHTS CAME ON IN FLIGHT, GEAR CAME UP ABOUT 1/2 WHEEL. EXTENDED GEAR HAD THREE GREEN. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. PLACED AIRCRAFT ON JACKS CYCLED GEAR. GEAR STAYED UP. ADJUSTED BOTH MAIN UP-POSITION SWITCHES. CYCLED GEAR 4 TIMES. OPS CHECK GOOD. AIRCRAFT RELEASED TO SERVICE (M)
1995
Part: GEAR SWITCH — OUT OF ADJUST (NLG)
MIA/MCO - FLT 427 - PILOT REPORT: NOSE GEAR UNSAFE INDICATION WHILE AIRBORNE, SAFE INDICATION ON GROUND. MAINTENANCE: HAD AIRCRAFT FERRIED TO MIA, GEAR DOWN AND LOCKED, TROUBLESHOT AND ADJUSTED NOSE GEAR DOWNLOCK SWITCH. AIRCRAFT RELEASED.