Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR V6NA2023041001Skin Splice · corrodedAT SCHEDULED INSPECTION, UPON REMOVAL OF LOWER FORWARD WING ACCESS PANEL, DISCOVERED LOWER FORWARD WING SPLICE CORRODED AT F.S 384, B.L. 10L-10R BEYOND ALLOWABLE LIMITATIONS PER THE LEARJET 45 STRUCTURAL REPAIR MANUAL.SDR V6NA20201013001Skin · chafedAT SCHEDULED INSPECTION DISCOVERED RIGHT WING LEADING EDGE TO HAVE CHAFE DAMAGE, SCUFF MARKS BLENDED OUT. REMAINING MATERIAL THICKNESS DETERMINED TO BE APPROVED FOR CONTINUED SERVICE BY FAA DER, DERT-405106-CE.SDR V6NA202007286001Windshield · crackedSHORTLY AFTER CLIMBING THROUGH 10,000 FEET THE RIGHT WINDSHIELD CRACKED. LEVELED OFF AT 10,800 FEET AND REQUESTED DESCEND TO 10,000 FEET. THE INNER LAYER WAS STILL SOLID AND ALL OTHER SYSTEMS WERE WORKING NORMALLY. CONTINUED TO DESTINATION WITHOUT FURTHER INCISDR V6NA20190410003Skin · corrodedAT PAINT POST STRIPPING INSPECTION DETERMINED THE BELOW LISTED AREAS ON SKINS WERE CORRODED. CORROSION REMOVED AND DETERMINED BEYOND MANUFACTURES RECOMMENDATION.SDR V6NA201904100002Skin · corrodedAT PAINT POST STRIPPING INSPECTION DETERMINED THE BELOW LISTED AREAS WERE CORRODED. CORROSION REMOVED AND DETERMINED BEYOND MANUFACTURES RECOMMENDATION.SDR V6NA20190411005Skin · corrodedAT PAINT POST STRIPPING INSPECTION, DETERMINED RIGHT THRUST REVERSER UPPER SKIN TO BE CORRODED. SKIN REPLACED WITH ONE FABRICATED PER APPROVED DATA IN FAA DER DRAWING.SDR V6NA20190411003Skin · corrodedAT POST PAINT INSPECTION, DETERMINED RIGHT THRUST REVERSER LOWER SKIN TO BE CORRODED. SKIN REPLACED WITH ONE FABRICATED PER APPROVED FAA DER DRAWING.SDR V6NA201904100001Fairing · corrodedAFTER PAINT STRIPPING PROCESS DETERMINED VERTICAL STABILIZER TOP AFT FAIRING TO BE CORRODED. CORROSION WAS REMOVED AND DOUBLER REPAIR INSTALLED PER APPROVED DATA IN FAA DER DRAWING.SDR V6NA2018050701Skin · corrodedCORROSION WAS DISCOVERED AT THE FOLLOWING LOCATIONS. CORROSION WAS MECHANICALLY CLEANED. CORROSION WAS BEYOND. MANUFACTURE ACCEPTED STRUCTURAL REPAIR MANUAL.SDR V6NA20180214001Angle · corrodedWHILE PERFORMING 9600 HOUR INSPECTION DISCOVERED LAND ANGLE AT BS 520 TO BE CORRODED. CORROSION WAS ON AFT SURFACE LOWER POSITION AND DETERMINED TO BE OUT OF LIMITS. OPENSDR V6NA20180103002Skin · corrodedWHILE PERFORMING 9600 HOUR INSPECTION, DETERMINED RIGHT WING OUTBOARD LOWER SKIN UPPER SURFACE TO HAVE CORROSION AT WS 260 AT COVE SURFACE INTERFACE. CORROSION DETERMINED OUT OF LIMITS. CORROSION CLEANED, SURFACE BLENDED, FILLED WITH EPOXY PASTE AND DOUBLER ISDR V6NA20150629001Windshield · crackedENROUTE AT APPROX FL 220 THE RT COCKPIT WINDSCREEN SHATTERED, ACCOMPANIED WITH A LOUD BANG NOISE. WE ADVISED ATC THAT WE NEEDED TO DIVERT & REQUESTED A LOWER ALTITUDE. WE WERE GIVEN A DESCENT CLEARANCE TO 1000 FEET BELOW OUR ALTITUDE UPON WHICH WE REQUESTED SDR EXO2006F00000Adc · failed30 MIN INTO FLIGHT, AC EXP MULTIPLE FAILURES, WITH LOSS OF NR 1 ADC, LOSS OF CABIN PRESS WITH CABIN EXCEEDING 10,000 BUT NO MORE THAN 11,000 FT, CABIN O2 MASKS DID NOT DEPLOY. EMER CHECK LIST FOR ALL FAILURES AND LOSS OF CABIN PRESS WERE INITIATED, FOLLOWED,