N307US

Cancelled 2006

Deregistered aircraft · 1990 Airbus Industrie A320-211 · CFM International CFM56 series

Cancelled
August 3, 2006
Status when cancelled
Triennial form not returned
Serial number
106
Year built
1990
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
May 8, 1990
Certificate issued
April 24, 1990
Last registry action
January 20, 2004
Mode S code
A33B26
Owner when cancelled
Northwest Airlines Inc
Location
St Paul, MN
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.

Service difficulty reports · 9

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

SDR 0301393207Line · leakingTHIRTY MINUTES INTO FLIGHT, LOST ALL HYDRAULIC FLUID IN YELLOW SYSTEM. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED LEAKING PARKING BRAKE LINE IN RIGHT WHEEL WELL. OPERATIONAL CHECK GOOD AND NO EVIDENCE OF LEAKAGE IN YELLJul 28, 2003 · N307US · Airbus A320211 · Hydraulic System, MainSDR 0100523207Hydraulic Line · leakingDURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED COM PROCEDURES, CONTINUED TO FINAL DESTINATION, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC LINE BETWEEN THE AUTO BRAKE SELECTOR AND PARK BRAKE VALVE. NO OTHER LEAK NOTED.Feb 16, 2001 · N307US · Airbus A320211 · Hydraulic System, MainSDR 0100393207B-Nut · looseDURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED ECAM AND COM PROCEDURES. CONTINUED TO FINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE SECURED A LOOSE B-NUT AT THE YELLOW SYSTEM BRAKE ACCUMULATOR. SERVICED SYSTEM WITH NO OTHER LEAKS NFeb 1, 2001 · N307US · Airbus A320211 · Hydraulic System, MainSDR 9710403207Bulb · failedDURING LINE MAINTENANCE, FOUND ALL FOUR OVERWING EMERGENCY EXIT HANDLE LIGHTS INOPERATIVE. REPLACED LIGHT BULBS, OPERATIONAL CHECK OK.May 28, 1997 · N307US · Airbus A320211 · Emergency LightingSDR 9623303207Power Supply · inoperativeDURING LINE MAINTENANCE, FOUND AFT EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED EPSU, OPERATIONAL CHECK OK.Nov 4, 1996 · N307US · Airbus A320211 · Emergency LightingSDR 9604173207Nut · crackedDURING '1C1' CHECK, LEFT ENGINE CHANGE FOUND THE FORWARD ENGINE MOUNT FORWARD ATTACH NUTS CRACKED. FURTHER INVESTIGATION REVEALED THAT IMPROPER CONFIGURATION NUTS WERE PREVIOUSLY INSTALLED (P/N LH7461T144D) PROPER CONFIGURATION IS (VN401B144). REPLACED ENGINFeb 14, 1996 · N307US · Airbus A320211 · Engine Mount SectionSDR 9504693207Floor Support · corrodedDURING THE INTERMEDIATE LAYOVER VISIT, THE AFT GALLEY FLOOR SUPPORT AT Y=1165 BETWEEN FRAME 68 AND 69 WAS FOUND CORRODED ON THE LOWER SURFACE OF THE UPPER FLANGE. CORROSION IN LOCALIZED AROUND ONE FASTENER ATTACH HOLE FOR FLOOR BOARDS AT APPROXIMATELY X=3942.Mar 17, 1995 · N307US · Airbus A320211 · Fuselage Miscellaneous StructureSDR 9503753207Seat Track · corrodedDURING INTERMEDIATE LAYOVER CHECK, FOUND CORROSION ON THE UPPER FLANGE OF THE SEAT TRACK AT Y = +765, FRAME 18. CORROSION WAS AT A NUT CLIP LOCATION. REPAIRED PER NWA EA 32-96360.Mar 10, 1995 · N307US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR 9504683207Sill · corrodedDURING INTERMEDIATE LAYOVER VISIT, CORROSION WAS FOUND ON THE INBOARD FLANGE OF THE RIGHT AFT CABIN DOOR LOWER SILL. CORROSION WAS FOUND AROUND EXISTING NUT PLATES. REPAIR ACCOMPLISHED PER NWA EA 32-96362.Feb 17, 1995 · N307US · Airbus A320211 · Fuselage Miscellaneous Structure