Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF2009040400039Apu · failedAPU HAD AUTO SHUTDOWN DURING PACKS ON AND ELEC LOAD FAULT LGT ILLUM AND A STRONG SHORT CIRCUIT ODOR. APU SECOND START WAS UNSUCCESSFUL IAW AMM 05-51-56 PAGE 201, INSPECTED CABIN BY ODOR AND IAW AMM 21-00-21, PAGE 201, CHECKED AIR CONDITIONING PACKS AND NO ODORSDR 2008FA0000477Selector · inoperativeAIR TURN BACK, CABIN ALT, CABIN ALTITUDE LIGHT EICAS MSG DISPLAYED OPERATIONAL AND MANUAL MODE RESTORED CABIN PRESS CABIN AUTO INOP 1 AND 2. IAW AMM 21-31-01/401. CABIN PRESSURE SELECTOR WAS REPLACED AND WAS ACCOMPLISHED CABIN PRESSURE CONTROL SYS, OPS TEST SDR ANCF200600050Servo · malfunctionedDURING DESCENT AT 15.000 FT, SPEED 290 EICAS MSG AUTOPILOT COME ON WITH CAUTION LIGHT, AUTOPILOT WAS DISENGAGED BY IT SELF. DURING APP THE ELEVATOR WAS VERY HARD TO OPERATE, BEING NECESSARY, EXCESSIVE FORCE CONTROL BY THE PILOT. PILOT FLYING. DURING FLARE THSDR ANCF200600042Sensor · defectiveT/O ABORTED AT 80 KTS DUE TO THE E/E ACCESS DOOR UNLOCKED INDICATION. THIS ITEM IS DIFERRRED TO DMI NO 141, MEL 52-71-1 CAT C, THE DIFERRED ITEM WAS CLOSED REPLACING THE PROXIMITY SENSOR DEFECTIVE, IAW FIM 32-09-03 PAGE 105 BLOCK 1 TO 8, BITE PROCEDURE FOR TSDR ANCF200400042Wire · chafedEICAS MSG L GEN DRIVE DISPLAYED GEN DRIVE LIGHT ILLUMINATED GEN DRIVE DISCONECTED IAW FIM 24-30-00 FIG 107 BLOCKS 1-2-11. PROCEDURE WAS PERFORMED AND FOUND CHAFING BETWEEN LINES 4-5 IN CONNECTOR D10964. IT WAS REPAIRED IAW WDM 24-11-21.SDR ANCF200400032Indicator · malfunctioned(ERRONEOUS NAV. INDICATIONS, ILS UNREADABLE, HDG UNREADABLE, THERE IS A DIFFERENT INFORMATION BETWEEN L AND R. ALL A/P DOES NOT ENGAGE AND DOES NOT MAINTAIN ALTITUDE) PERFORMED ILS TEST IAW AMM 34-31-00 PG 501-508, NOTHING ABNORMAL FOUND, ALL TASK WERE PERFORMSDR ANCF200400017Module · failedUNSCHEDULE STAB TRIM DISPLAYED DURING TAKE OFF ROLL. CHECKED SAMS NO FAULTS BALLS SET-CARRIED OUT FIM 27-09-00 FIG 106A BLOCKS 1+2 STAB TRIM TRIED WITH C/C SWS STAB TRIM ALT SWS MOVEMENT CORRECT-CUT OUT SWS TRIED AND FUNCTION ON (NO MOVEMENT). IAW AMM 27-41-SDR ANCF200200017Target · out of adjustEICAS MESSAGE LE SLAT ASYM, LEADING EDGE LIGHT ILLUMINATED WITH THE FLAP LEVER IN UP, BOTH FLAP POINTERS WERE IN 1/2. DURING FLAP/SLAT RETRACTION ON CLIMB-OUT PHASE. PERFORMED PROCEDURE IAW FIM 27-81-00 PAGE 134 AND WAS ADJUSTED CLEARANCE AT SENSOR TARGET S-SDR ANCF200200003Indicator · malfunctionedDURING FLIGHT WITH NORMAL FUEL FLOW THE RT TANK SHOWED DIFFERENCE BETWEEN TOTAL FUEL QTY AND FUEL QTY OF FMC ADDITIONALLY, WAS PRESENTED FUEL DISAGREE PROG 2, AND FUEL CONFIGURATION WAS PRESENT TWICE. CREW PROCEEDED TO RETURN TO EDR. CORRECTIVE ACTION: PERSDR ANCF200100005Pump · failedDURING FLIGHT FROM FRA TO SJU RH EDP HYD LOW PRESSURE CAME ON, FLIGHT PROCEDED TO BAQ. RT EDP WAS REPLACED IAW AMM 29-11-05, TEST WAS SATISFACTORYSDR ANCF9702Engine · failedBOG/LON - FLT 016 - REJECTED TAKEOFF. ENGINE NR 2 EGT WENT TO RED RANGE FOR 15 SECONDS, ENGINE STALLED, ENGINE OPERATION NORMAL AFTER THRUST REDUCED TO IDLE AND POWER RE-APPLIED. RT ENGINE WAS CHANGED, TESTED ON GROUND WITH ENGINE RUN-UP OK. (X)