N325JF
Registered owner: N325JF OPERATING LLC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ADDISON JET MANAGEMENT INC (I5JA) | 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.
9 reports on file, 2002-09-17 – 2013-08-22.
Part: UNKNOWN — ODOR (CABIN) · airframe 12,828 hrs · 11,786 cycles
30 MINUTES BEFORE LANDING, DETECTED AN ELECTRICAL BURNING ODOR THROUGHT ENTIRE CABIN. TURNED OFF PC POWER SYS IMMEDIATELY AND ODOR SLOWLY WENT AWAY. F/A COULD NOT PINPOINT WHERE THE ODOR WAS COMING FROM. AFTER TURNING PC POWER OFF, GEN 1, 3, 2, AND 4 LOADS WERE 65, 75, 95, AND 90 RESPECTIVELY. ACFT LANDED SAFETLY. MX PERFORMED TROUBLESHOOTING IAW FIM 21-20-00-810-801-A, BLOCK 1-6, 8-10, NO FAULTS FOUND. MX PERFORMED OPS TEST OF PASSENGER PC POWER STATIC INVERTER COOLING FAN IAW AMM 24-20-03-700-802-A. OPS CHECKED GOOD, NO DEFECTS NOTED. COULD NOT DUPLICATE.
Part: FLEX HOSE — CHAFED (HYD SYSTEM) · airframe 12,662 hrs · 11,645 cycles
ON DESCENT AT 14,000FT, HYD 2 QTY LOW MESSAGE APPEARED, THEN FOLLOWED SHORTLY BY ENG 2 HYD PUMP FAIL MESSAGE. THE CREW DIVERTED DUE TO RUNWAY REQUIREMENT AND LANDED SAFELY. DURING VISUAL INSPECTION, PN 145-31063-409 HOSE FROM NR 2 ENGINE DRIVEN HYDRAULIC PUMP WAS FOUND TO BE WORN THROUGH DUE TO CHAFING. REPLACED THE HOSE WITH INTERCHANGEABLE, PN A9140-409. OPS CHECK AND LEAK CHECK GOOD.
Part: TUBE — BROKEN (NR 1 ENGINE) · airframe 12,646 hrs · 11,637 cycles
NR 1 ENGINE ANTI-ICE PRESSURE TRANSDUCER TUBE FOUND BROKEN AT TRANSDUCER AND ENGINE AIR INTAKE ANTI-ICE DUCT. R & R WITH NEW. OPS CHECKED GOOD.
Part: GCU — MALFUNCTIONED (ZONE 200) · airframe 12,000 hrs · 11,293 cycles
GEN 3 OFF BUS ON TAXI IN AFTER SHUTDOWN OF NR 2 ENGINE. SMELL OF SMOKE IN THE COCKPIT. PERFORMED FIM 21-20-00-810-801-A FOR SMELL OF SMOKE IN THE CABIN COCKPIT. NO ABNORMAL SMELL NOTED AT THIS TIME. AC RELEASED IAW MEL 24-31-01-2 CTRL # 768504B09. PLACARDS INSTALLED CW SP 24-31-01-2. PULLED C/B'S D8 & D9.
Part: WIRE — BROKEN (CABIN) · airframe 11,862 hrs · 11,174 cycles
3RD EMERGENCY FLOOR PROXIMITY STRIP LIGHT INOP, CONNECTOR WIRES BROKEN AT BASE. REMOVED DEFECTIVE UNIT AND INSTALLED SERVICEABLE (NEW) 3RD EMERGENCY FLOOR PROXIMITY STRIP LIGHT IAW EMB135 AMM TASK 33-50-12-000/400-801-A. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.
Part: WIRE — BROKEN (CABIN) · airframe 11,862 hrs · 11,174 cycles
2ND EMERGENCY FLOOR PROXIMITY STRIP LIGHT INOP, CONNECTOR WIRES BROKEN AT BASE. REMOVED DEFECTIVE UNIT AND INSTALLED SERVICEABLE (NEW) 2ND EMERGENCY FLOOR POXIMITY STRIP LIGHT IAW EMB135 AMM TASK 33-50-12-000/400-801-A. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.
Part: FILTER — UNKNOWN (FUEL SYSTEM) · airframe 11,596 hrs · 10,906 cycles
ON TAKEOFF ROLL "E1 FUEL IMPENDING BYPASS" MESSAGE WAS DISPLAYED ON EICAS. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE PERFORMED THE PROCEDURES PER THE EMB135 AMM AND REPLACED THE FILTER ELEMENT. NO VISUAL CONTAMINATION WAS FOUND IN THE FILTER ELEMENT.
Part: ENGINE — CONTAMINATED · airframe 8,774 hrs · 8,622 cycles
AFTER TAKEOFF AT APPROX 400 FT, PILOTS RECEIVED "LAV SMOKE" EICAS INDICATION. DECLARED EMERGENCY & RETURNED FOR LANDING AT DEPARTURE. ACFT GROUNDED UNTIL MX DETERMINES ROOT CAUSE. F/A INVESTIGATED ACFT LAV - OBSERVING NO FUMES OR SMOKE. ONCE ON THE GROUND FIRE DEPARTMENT COMPLETED EXTERNAL INSPECTION " NO INDICATION OF SMOKE OR FUMES". AFTER ALL PASSENGERS DEPLANED, FIRE DEPARTMENT BOARD TO INVESTIGATE LAV "NO INDICATION OF SMOKE OR FUMES". ACFT WAS TAKEN OUT OF SERVICE FOR MX EVALUATION. RESIDUAL ENG CLEANER IN BLEED AIR SYS & ASSOCIATED COMPONENTS. MX CONDUCTED ENG CORE WASHES DURING WEEKEND.
Part: WIRE — FAILED (LIGHT DIMMER)
WIRE NR W101-0072-20 WAS FOUND BURNED IN HALF DURING INSPECTION AND TROUBLE SHOOTING TO CORRECT AN MEL ON THE BACK LIGHTING ON THE PILOTS SIDE ELECTRONIC CLOCK. DURING INVESTIGATION IT WAS FOUND THAT THE SYSTEM DESIGN USED 20 GAUGE WIRE AT THE OUTPUT OF THE DC LAMP DIMMER THAT HAS AN INTERNAL CIRCUIT PROTECTION THAT TRIPS AT 16.75 AMPS WHICH EXCEEDS THE RATING FOR 20 GAUGE WIRE. RECOMMEND REEVALUATION OF SYSTEM DESIGN AND PROTECTION OF WIRING ON OUTPUT SIDE OF DC LAMP DIMMER.