N306US

Cancelled 2006

Deregistered aircraft · 1989 Airbus Industrie A320-211 · CFM International CFM56 series

Cancelled
August 3, 2006
Status when cancelled
Triennial form not returned
Serial number
060
Year built
1989
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
October 16, 1989
Certificate issued
September 26, 1989
Last registry action
December 16, 2003
Mode S code
A3376F
Owner when cancelled
Northwest Airlines Inc
Owner type
Corporation

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

NTSB investigations · 1

Matched to this aircraft by N306US and the event date: up to this one’s cancellation.

FAA incident reports · 3

FAA accident and incident reports matched to this aircraft by N306US and the event date: up to this one’s cancellation.

Service difficulty reports · 11

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 0101283206Fan · failedDURING DESCENT, AN ELECTRICAL BURNING ODOR WAS NOTICED IN THE COCKPIT FOLLOWED BY VENT BLOWER FAULT MESSAGE. COMPLIED WITH COM PROCEDURES, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AVIONICS VENTILATION INLET BLOWER FAN AND Mar 31, 2001 · N306US · Airbus A320211 · Air Distribution FanSDR 0100733206Computer · malfunctionedSHORTLY AFTER LIFT-OFF, RECEIVED SMOKE AFT CARGO SMOKE MESSAGE. FOLLOWED ECAM AND COM PROCEDURES AND RETURNED TO DEPARTURE FIELD FOR NORMAL LANDING. MAINTENANCE REPLACED THE SPENT FIRE EXTINGUISHER BOTTLE AND THE FLIGHT WARNING COMPUTER. OPERATIONAL CHECK OFeb 23, 2001 · N306US · Airbus A320211 · Central ComputersSDR 000443206Stringer · corrodedDuring "M" check found corrosion on stringer 41RH. Repaired per EA32-173634.Jan 6, 2000 · N306US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 0000443206Stringer · corrodedDURING M-CHECK, FOUND CORROSION ON STRINGER 41 RT. REPAIRED PER EA32-173634.Jan 6, 2000 · N306US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9802463206Connector · looseDURING MAINTENANCE TEST OF THE EMERGENCY LIGHTS, FOUND ESCAPE PATH LIGHTS INOPERATIVE AT SEAT ROWS 25C, 26C, AND 27C. MAINTENANCE SECURED LOOSE CANNON PLUG. OPERATIONAL CHECK OK.Feb 10, 1998 · N306US · Airbus A320211 · Emergency LightingSDR 9720503206Sensor · failedUPON GEAR EXTENSION, CREW RECEIVED ECAM MESSAGE LGCIU 1 FAULT AND LGCIU 2 FAULT. CREW DECLARED AN EMERGENCY. FOLLOWED ECAM AND COM PROCEDURES. GRAVITY EXTENDED LANDING GEAR AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH NOSE LANDING GEAR DOOR CLOSEOct 31, 1997 · N306US · Airbus A320211 · Landing Gear Position and WarningSDR 9627373206Battery · dischargedDURING LINE CHECK, EMERGENCY LIGHTS FAILED CIDS PANEL CHECK. REPLACED BATTERIES AND POWER SUPPLY BETWEEN RIGHT OVERWING EXITS, OPERATIONAL CHECK GOOD.Dec 30, 1996 · N306US · Airbus A320211 · Emergency LightingSDR 9621093206Engine · failedDURING TAKEOFF ROLL, THE NR 1 ENGINE EXPERIENCED A CONTAINED FAILURE. TAKEOFF WAS ABORTED AT 75 KNOTS. MAINTENANCE FOUND METAL IN TAILPIPE. REMOVED AND REPLACED THE NR 1 ENGINE.Oct 3, 1996 · N306US · Airbus A320211 · Engine (Turbine/Turboprop)SDR 9618943206Battery · dischargedDURING LINE MAINTENANCE, THE FORWARD LEFT AND LEFT OVERWING EMERGENCY LIGHTS FAILED THE EMERGENCY LIGHTS BATTERY CHECK. REPLACED BATTERY PACKS, OPERATIONAL CHECK OK.Sep 2, 1996 · N306US · Airbus A320211 · Emergency LightingSDR 9616033206Tire · flatDURING TAKEOFF ROLL, RECEIVED BRAKES HOT AND DELAY TAKEOFF MESSAGES. TAKEOFF WAS ABORTED BETWEEN 60 AND 70 KNOTS. AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE FOUND THE NR 1 TIRE FLAT. REPLACED NR 1 AND NR 2 TIRES. LEAK CHECK OK.Jul 28, 1996 · N306US · Airbus A320211 · TireSDR 9514173206Vbv Sensor · malfunctionedDURING CLIMB AT 10,000 FEET, RECEIVED ECAM MESSAGE ENG 2 COMPRESSOR VANE ACCOMPANIED WITH NO RAPID THROTTLE MOVEMENT. AIRCRAFT RETURNED TO DTW DUE TO LACK OF PARTS IN SJU TO ADDRESS THE PROBLEM. THE AIRCRAFT LANDED WITHOUT INCIDENT AND THE VBV SENSOR WAS REPSep 9, 1995 · N306US · Airbus A320211 · Compressor Bleed Valve