N399SW
Registered owner: WOODARD STEVEN L, NM (owner ≠ operator)
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.
13 reports on file, 1995-07-03 – 1998-02-07.
Part: LVDT — DIRTY (NLG STEERING)
NOSE WHEEL STEERING FAILED DURING TAXI FOR TAKEOFF AT KEWR. PERFORMED NOSE WHEEL STEERING CONTROL BOX BITE CHECK PER MM 32-50-00, NO FAULTS INDICATED. PERFORMED INSPECTION OF CONNECTORS AND FOUND THE LINEAR VARIABLE DIFFERENTIAL TRANSFORMER (LVDT) DIRTY WITH TRACES OF GLYCOL. CLEANED THE LVDT AND PERFORMED CHECK IAW MM 32-50-00. ALL CHECKS NORMAL.
Part: BOOST PUMP — FAILED (LT WING)
CREW EXPERIENCED AN UNCOMMANDED NR 2 ENGINE SHUTDOWN WHILE ATTEMPING TO BALANCE FUEL USING CROSSFEED OPERATION. RESTARTED ENGINE AND LANDED WITHOUT INCIDENT. REPLACED BOTH LEFT WING AFT AND FWD FUEL BOOST PUMPS AND PERFORMED FUEL FEED LINE COUPLING VACUUM TEST PER BOEING M/M.
Earlier reports · 1995–1997 · 11 reports
1997
Part: CLIP — MISSING (T/R BLOCKER DOOR)
THRUST REVERSER BLOCKER DOOR CONTROL ARM PIN RETAINER CLIPS FOUND MISSING WITH ABNORMAL REGULARITY. SUBMITTER RECOMMENDATION: RE-DESIGN WITH DRILLED PIN AND INSTALL COTTER PIN VERSUS RETAINER CHIP.
1996
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED A2 CHECK, FOUND RT WING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK PER BOEING M/M.
Part: WIRE — BROKEN (CABIN)
DURING PRE-FLIGHT CHECK, FOUND 3 EMERGENCY EXIT TRACK LIGHTS INOP. RESPLICED WIRES AND OP CHECKED PER BOEING M/M.
Part: BATTERY — DISCHARGED (CABIN)
DURING SCHEDULED A2 CHECK, FOUND LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER BOEING M/M.
Part: WIRE — DISCONNECTED (CABIN)
DURING OVERNIGHT CHECK, FOUND EMERGENCY TRACK LIGHTING INOP BEHIND ROW 6. RECONNECTED WIRING ON TRACK LIGHT.
1995
Part: ENGINE — VIBRATION (RT POSITION)
NR 2 ENGINE ON TAKEOFF EXPERIENCED HIGH VIBRATION LIGHT AND READING OF 2.1. PERFORMED ENGINE RUN WITH ANTI-ICE SELECTED AND VIBES AT 1.8. PERFORMED BORESCOE OF RT ENGINE. NO ABNORMALTIES. NOTIFIED GE PER MM 72-00-00, PAGE 517, WITHIN OPS LIMITS. AS PRECAUTIONARY, DELIVERED AIRCRAFT TO GE FOR INSPECTION. FOUND PARTIAL FLAKING OF COATING FROM COMB GEAR. INSTALLED LOANER ENGINE. OPS NORMAL.
Part: ASYMMETRY BRAKE — FAILED (RT FLAP)
FLAPS FAILED AT 18 DEGREES. REPLACED DEFECTIVE RT FLAP ASYMMETRY BRAKE. OPS CHECK NORMAL. COMPLIED IAW 27-50-26.
Part: TIRE TREAD — SEPARATED (NR 3)
NR 3 TIRE TREAD SEPARATED CAUSING DAMAGE TO WOW HARNESS RIGHT GEAR. REPLACED WHEEL ASSY AND WOW HARNESS ASSY. TIRE HAD 171 LANDINGS. GEAR RETRACTION CHECK C/W.
Part: PUMP — LINE FAILED (LT ENG NR 1 HYD)
ON CLIMB, LOSS OF NR 1 HYDRAULIC FLUID QUANTITY. C/A - FOUND PRESSURE LINE FROM NR 1 ENGINE HYDRAULIC PUMP FAILED. REPLACED NR 1 ENGINE PUMP AND HYDRAULIC LINE. SERVICED SYSTEM, BLED SYSTEM, OPERATIONAL CHECK NORMAL.
Part: THROTTLE — EXCESS PLAY (NR 2 QUADRANT)
NR 2 ENGINE THROTTLE LEVER HAS EXCESSIVE PLAY AND FRICTION KNOB MALFUNCTIONING. REPLACED THROTTLE QUADRANT IAW 73-00/76-1101. RUN-UP AND OPS CHECK NORMAL.
Part: SOLENOID SWITCH — FAILED (RT QUADRANT)
RIGHT THRUST REVERSER STUCK AT IDLE AFTER GREEN LIGHT DURING DEPLOYMENT. FOUND SOLENOID NOT PULLING. REPLACED THROTTLE QUADRANT. OPS CHECK NORMAL, ENGINE POWER RUNS GOOD.