N650Z

No registry detail on file · not in current registry

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.

7 reports on file, 1998-01-05 – 2007-12-18.

OTHER · 2007-12-18 Matched by certificate designator
ATA 3230

Part: BOTTLE — LEAKING (MLG)

EMERGENCY GEAR PNEUMATIC BOTTLE HAS TO BE SERVICED REPEATEDLY.

Source: SDR VQMA121807001
AFFECT SYSTEMS; WARNING INDICATION · 2007-08-24 Matched by certificate designator
ATA 3411

Part: STATIC PORT — LEAKING · airframe 11,709 hrs · 9,922 cycles

SPLIT IN ALTIMETERS (RT ALTIMETER INDICATES 400 FOOT HIGHER THAN LT ALTIMETER AT 41,000 FT MSL) VERIFIED SPLITS IN ALTIMETERS AND PILOTS PITOT/STATIC SYS. INSTALLED NEW CO-PILOTS STATIC PORT FITTING P/N CM2933-7. LEAK CHECK, SAND, FILLED, PRIMED, PAINTED AND RVSM SKIN WAVINESS SATISFACTORY.

Source: SDR M000999
OTHER · 2007-08-09 Matched by certificate designator
ATA 3230

Part: BOTTLE — LEAKING (MLG) · airframe 11,697 hrs · 9,912 cycles

GEAR PNEUMATIC BLOWDOWN BOTTLE IS LEAKING.

Source: SDR VQMA081907001
FLUID LOSS · 2007-03-19 Matched by certificate designator
ATA 2910

Part: HOSE — CRACKED (HYD SYSTEM) · airframe 11,490 hrs · 9,728 cycles

LT UPPER ACTUATOR LINE WAS FOUND TO HAVE A CRACK IN THE ELBOW, CAUSING A HYDRAULIC FLUID LEAK. MATERIAL IN THE ELBOW OF THE HOSE LOOKS GRAINY AS IS STRESSED WHILE FORMING.

Source: SDR 03192007650Z
WARNING INDICATION · 2007-01-08 Matched by certificate designator
ATA 2741

Part: UNKNOWN — UNKNOWN (TRIM SYSTEM) · airframe 11,398 hrs · 9,658 cycles

DISCREPANCY (PRIMARY TRIM INDICATOR DOES NOT MOVE FULL RANGE.) DURING FLIGHT, FLIGHT CREW OBSERVED INTERMITTENT FAILURE OF THE HORIZONTAL STABILIZER PRIMARY TRIM (CLACKER). UPON ARRIVAL, FLIGHT CREW PERFORMED ALL PRE AND POST TAKEOFF OPERATIONAL CHECKS AND OBSERVED A HORIZONTAL STABILIZER TIME FAILURE ANNUNCIATION AND MASTER CAUTION WARNING. ADDITIONALLY, THE FLIGHT CREW FOUND THAT THEY WERE UNABLE TO OPERATE THE TRIM WITH THE PRIMARY SYSTEM BEYOND THE -10.5 POSITION. THE AIRCRAFT WAS FLOWN USING A SPECIAL FLIGHT PERMIT FOR FURTHER TROUBLESHOOTING AND REPAIR.

Source: SDR 01082007650Z
OTHER · 1998-01-05 Unresolved
ATA 2710

Part: CONTROL CABLE — WORN (RT WING)

RIGHT WING AILERON CABLE (OUTBOARD, AFT) WORN THROUGH CLAD. FOUND DURING OPERATION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE CHANGE, ALL PRIMARY CONTROL SURFACES.

Source: SDR 98ZZZX705
OTHER · 1998-01-05 Unresolved
ATA 2710

Part: CONTROL CABLE — FRAYED (RT AILERON)

RIGHT WING AILERON CABLE, (INBOARD, FORWARD) HAS BROKEN WIRES IN SEVERAL STRANDS AT CABLE PULLEYS WS 88.00. FOUND DURING OPERATION 10, CONTINUOUS INSPECTION PROGRAM NR SMP650-1. SUBMITTER RECOMMENDED A MANDATORY 4,800-HOUR CABLE HCANGE, ALL PRIMARY CONTROL SURFACES.

Source: SDR 98ZZZX704