FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N14211 and the event date: after April 9, 1948, when the previous aircraft’s registration ended, through this one’s cancellation.
Incident 19970619020299IGround Taxi, Other Airplane · Chicago, ILTaxiing for takeoff a fuel truck struck a wing. Slat assembly was replaced. Fuel truck driver fired. New training.Incident 19900720035519IFcd/Prec Ldg From Cruise · Pittsburgh, PANR1 system hydraulic low pressure light. Precautionary landing, NR1 engine hydraulic pump pressure line leaking.
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CALA9701247Hyd Line · leakingTHE A SYS HYD LOW PRESSURE LIGHT FLICKERED AND HYD QTY WAS ZERO WHILE EN ROUTE TO EWR. BOTH A HYD LOW PRESSURE LIGHTS ILLUMINATED STEADILY SHORTLY AFTERWARDS. THE LOSS OF A HYD SYS PRESSURE CHECKLIST WAS ACCOMP. A MANUAL GEAR EXTENSION AND ALTERNATE FLAP EXTSDR CALA9601724Sensor · out of adjustTHE GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION AFTER TAKEOFF FROM PHL. CYCLING OF THE GEAR LIGHT CIRCUIT BREAKER MADE NO CHANGE. THE AIRCRAFT WAS RETURNED TO PHL WHERE IT LANDED WITHOUT INCIDENT (THE AIRCRAFT HAD AIR RETURNED THE DAY BEFORE FOR THE GEASDR CALA9601376Frame · crackedINSPECTION FOUND A 2 INCH CRACK IN FRAME AT STA 380, STRINGER 21R. THE CRACK WAS STOP DRILLED IAW SRM 53-10-4. A DOUBLER, FILLER AND CLIP WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.SDR CALA9601374Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN FUSELAGE SKIN AT FS 765, STRINGER 19R. THE CRACKED AREA OF SKIN WAS REMOVED, REPAIR DOUBLER AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-30-2.SDR CALA9601373Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN ATTACH ANGLE AT STA 360, STRINGER 21R. THE ATTACH ANGLE WAS REMOVED IAW SRM 51-30-2, REPAIR ANGLES AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.SDR CALA9601372Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN ATTACH ANGLE AT STRINGER 22L STA 360. THE CRACKED SECTION WAS REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND 51-30-2.SDR CALA9601377Angle · crackedINSPECTION FOUND A .75 INCH CRACK FROM LAST FASTENER HOLE OF RT UPPER RAM AIR ATTACH ANGLE AT STA 540, STRINGER 14R. THE CRACKED SECTION OF ANGLE WAS CUT OUT, A NEW SECTION AND SPLICE ANGLE WERE FABRICATED AND INSTALLED IAW SRM 53-50-1, 51-40-3 AND 51-10-2.SDR CALA9601371Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN BETWEEN STRINGER 19L AND 20L AT STA 727. A MOD AND REPAIR WAS ACCOMPLISHED IAW BOEING DRAWING 65C28086 AND EA 5330-01198, OP 1 AND OP 2.SDR CALA9601375Angle · corrodedINSPECTION FOUND EXFOLIATION CORROSION AND SHEARED FASTENERS AT LT AFT CORNER OF E AND E DOOR CUTOUT SUPPORT STRUCTURE. THE T-ANGLE WAS REMOVED AND REPLACED IAW EC 5310-01233.SDR CALA9601110Harness · failedMAINTENANCE FOUND FEEDER HARNESS BURNT WHILE TROUBLESHOOTING THE APU. A STRINGER AT BELLY OF AIRCRAFT ABOUT 15 INCHES FORWARD OF APU COMPARTMENT AFT OF AFT PRESSURE BULKHEAD WAS FOUND BURNED DUE TO THE FEEDER HARNESS ARCING. A NEW HARNESS WAS SPLICED IN AND
Other aircraft with N14211 · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N14211 now.