N304NV
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.
10 reports on file, 2015-04-13 – 2020-05-12.
Part: BATTERY — FAILED (CABIN) · airframe 42,444 hrs · 31,952 cycles
EPSU BATTERY FIN# 10WL FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 42,063 hrs · 31,762 cycles
ESPU TEST FAILS ON OPERATIONAL CHECK. / REPLACED BATTERY ON ESPU.
Part: COVER — MISSING (CABIN) · airframe 41,989 hrs · 31,719 cycles
L1 DOOR FRAME LEFT LOWER SIDE EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED LENS ON L1 DOOR FRAME LT LOWER SIDE IAW AMM 33-51-16-400-001-A OPS CHKS NORMAL.
Part: FITTING — LEAKING (HYD SYSTEM) · airframe 41,851 hrs · 31,635 cycles
(RMERGENCY DECLARED) LOSS OF GREEN HYD SYS / R&R FLEX HOSE OLD ELBOW FITTING"
Part: SKIN — DENTED (NR 2 NACELLE) · airframe 33,768 hrs · 27,712 cycles
NR 2 NACELLE DENTED. REPAIRED IAW SRM 54-10-11 REPAIR 6.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,994 hrs · 26,864 cycles
AFT FLIGHT ATTENDANT EMER FLASHLIGHT BATTERY INOPERATIVE. R & R AFT FLIGHT ATTENDANT EMER FLASHLIGHT BATTERY IAW 25-60-00. OPERATIONS CHECKED NORMAL AT THIS TIME.
Part: HYDRAULIC LINE — LEAKING (LT ENGINE) · airframe 31,445 hrs · 26,604 cycles
IN CRUISE FLIGHT, LOST GREEN HYD SYS QTY. RECEIVED THE FOLLOWING ECAM, HYD G RESERVOIR LO LVL, FOLLOWED ECAM, AOM & QRH PROCEDURES, INCLUDING ALTERNATE LANDING GEAR EXTENSION IAW LOG PAGE 500385. LEAKING HYD LINE REPLACED ON LT ENG GREEN SYS HYD PRESS SWITCH. SYS SERVICED IAW AMM 12-12-29, SYS BLED IAW AMM 29-00-00-870. SYS LEAK CHECKED IAW DRY MOTOR 71-00-00-710, LEAK CHECKED GOOD.
Part: MEGAPHONE — FAULTY (CABIN) · airframe 31,442 hrs · 26,603 cycles
FLIGHT ATTENDANT REPORTS BOTH FWD & AFT MEGA PHONES TEST PROPERLY, BUT WILL NOT PROPERLY PROJECT, MAGNIFY, VOICE. AFT MEGA PHONE OPERATIONS CHECKED NORMAL. FWD MEGA PHONE REPLACED & CHECKED GOOD IAW AMM 25-65-51-710-002-A.
Part: UNKNOWN — OSCILLATES (FUSELAGE) · airframe 30,829 hrs · 26,314 cycles
DURING CRUISE AT 38000 FT, AIRCRAFT OSCILLATED IN YAW WITH A FREQUENCY OF ABOUT 1/2 A SECOND, FROM LEFT TO RIGHT, RUDDER TRIM INDICATOR SHOWED LEFT. LEFT RUDDER TRIM VARYING BETWEEN L0.8 TO L1.2 128000 LBS M0.78 SMOOTH AIR AUTO PILOT 1 ON ENGINE VIB NORMAL, FLIGHT CONTROL NORMAL WITH AUTO PILOT OFF, THERE WAS NO CHANGE IN THE OSCILLATION INCREASED SPEED IAW QRH. AIRCRAFT VIBRATIONS S.6.18 WITH NO CHANGE UPON RETURNING TO NORMAL SPEED. THE OSCILLATION WENT AWAY & THE RUDDER TRIM INDICATOR STABILIZED TOTAL TIME OF OSCILLATING WAS LESS THAN 5 MINS. PERFORMED FAC SYSTEM TEST IAW AMM 22-60-00-PB 501 ONFIG 00 ALL PASS.
Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 30,001 hrs · 25,925 cycles
AIRCRAFT PULLS TO LT ON LANDING & AT HIGH TAXI SPEEDS, TAXIED ACFT. PERFORMED TSM 32-51-00-810-823-A, SUBTASK 32-51-00-710-050-A. ACFT DEVIATES 2.5 DEGREES TO THE LT. COMPLIED WITH TSM UP TO 3A - STEP 8. ACFT RETURNED TO SERVICE UPON CONTINUED MONITORING OF NWS TO ASSESS ACFT LATERAL DEVIATION.