NTSB investigations · 1
Matched to this aircraft by N718DA and the event date: up to this one’s cancellation.
FAA incident reports · 6
FAA accident and incident reports matched to this aircraft by N718DA and the event date: up to this one’s cancellation.
Incident 19960709022459IClimb · Salt Lake City, UTNarrative: delta flt 706, a Lockheed L-1011, N718DA, departed seattle int'l, WA at approx. 0830 PDT under VFR conditions. While enroute to atlanta, ga and climbing through flight level 170, the flight crew noted a low oil quantity light on the left engine.…Incident 19920602021499IForced/Precautionary Landing · Atlanta, GASmoke in cabin on climb. Returned. Landed safely. Evacuation. Some slides did not deploy. Air cycle machine faulty.Incident 19860331052889IGround Taxi, Other Airplane · West Palm Beach, FLDuring taxi after runup following an aborted takeoff the right gear left hard surface and became mired in the sand.Incident 19800602052569ITakeoff Ground Roll · Chicago, IL#2 Engine would not develop more than idle power. High pressure fuel shutoff valve frozen.Incident 19780818049119INormal Cruise · Dallas, TXDiverted due to loss of NR1 generator. NR2 generator already inoperative. Integrated drive generator no 708542N.Incident 19780410009789IFinal Approach · San Diego, CACrew unable to fully extend flaps for landing. Found flap track had separated from aircraft.
Service difficulty reports · 32
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DLL10991808Skin · crackedWING LT UPPER SKIN, IWS 395, CRACK REPAIR. AN EXISTING CRACK IN THE LEFT UPPER WING SKIN AT IWS 395 PROGRESSED BEYOND THE ALLOWABLE SRM LIMIT. THE CRACK STARTED AT THE AFT EDGE OF THE SKIN AND PROGRESSED FWD. THE CRACK IS TYPICAL OF THE SRM, BUT IS NOW 2.3 SDR DLL10991806Skin · crackedWING RT LOWER AFT SKIN IWS 425.7, STRINGER 3, CRACK REPAIR. THE LOWER AFT SKIN OF THE RT WING WAS FOUND WITH A 4.5 LONG CRACK AT THE STRINGER 3 RUNOUT AT IWS 425.7. THE CRACK WAS CUTOUT OF THE SKIN AND REPAIRED WITH THREE ALUMINUM DOUBLERS PER ER/A 367909-14SDR DLL10991805Frame · crackedFUSELAGE FRAME FS 1183, WL 280.6, CRACK REPAIR. A TYPICAL CRACK WAS FOUND IN THE FS 1183 FUSELAGE FRAME AT WL 280.6. THE CRACK WAS STOP DRILLED AND REPAIRED PER LACO S/B 093-53-A271 AND ER/A 367927-14, REV A.
See all 32 reportsOther aircraft with N718DA · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N718DA is registered now to the first aircraft listed.