Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR SAJFCALS100029Longeron Fitting · crackedDURING 10C AND 2D CHECK, CRACK WAS FOUND AT LT SIDE LONGERON FITTING. THE CRACK LENGTH IS .1875". TRIMMED OUT THE CRACKED AREA AND DEFERRED THE MEASUREMENT OF GAPS IAW MFG (SR 1-193896515).SDR SAJFCALS100030Stringer · corrodedLEVEL II CORROSION WAS FOUND AT LOWER STRINGER 2, STATION 285 OF LT HORIZONTAL STAB STRUCTURE DURING D-CHECK. TRIMMED OUT THE CORRODED STRINGER AND FABRICATED A PORTION OF NEW STRINGER IAW DWG 65B03555. INSTALLED THE NEW STRINGER WITH REPAIR ANGLE AND FASTESDR SAJFCALS100020Skin · crackedDURING TRANSIT CHECK, FOUND A POP-UP SKIN WITH A 0.5 INCH LENGTH CRACK LOCATED ON S44R, BS 1728. CHECKED INTERIOR SKIN AND DISCOVERED CORROSION COMMON TO INTERIOR BELLY SKIN ALONG S44R EDGE. DETAILED VISUAL INSP ON ADAJCENT STRUTURE FOUND OTHER 2 SKIN CRACKS ASDR SAJFCAL2010002Socket · arcedCABIN LOG RECORD, THE FIRST CLASS GALLEY 1 WORK LT INOP. REMOVED GALLEY 1 WORK LT FOUND LIGHT ASSY LAMP HOLDERS ARCED. INSPECT GALLEY 1 CEILING CONDITION CHECK NORMAL, THERE IS NO WATER LEAK CONDITION FOUND. AFTER REPLACED GALLEY 1 LIGHT ASSY, THE SYS WAS SDR SAJFCALS098044Tire · rupturedAFTER ACFT TOOK OFF, RUNWAY FOUND TIRE DEBRIS OF TIRE NR 8 DUE TO DELAMILATION. TIRE NR 8 DE-LAMINATED, THIS TIRE IS 4TH RETREADED. DAMAGED STRUCTURE REPAIR IS IN PROCESS AT AMS STA 3. MORE DETAILED STRUCTURAL DAMAGES ARE STILL PENDING FOR REPORTS FROM AMS SSDR SAJ2008F00000Stringer · corrodedDURING 8C CHECK, N168CL AFT CARGO BAY BILGE AREA STRINGER S50R WAS FOUND CORRODED, AT STA 1840, STA 1860, STA 1880, STA 1920. (S)SDR CALS097002Pump · contaminatedRTO AT SGN DUE TO ENG-3 CONT MSG COME ON DURING T/O ROLL, THE DETAILED DESCRIPTION AS FOLLOWS: 1) DUE TO ENG-3 SVA ACTUATOR FAILURE TO CAUSE N2 OVERSPEED AND ENG-3 CONT MSG DURING A/C TAKE OFF ROLLING. 2) EEC FAULT MSG: ENG-3 SVA FAIL, ENG-3 OVERSPEED GOVERNOR