Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR WRNA20080011Slide · no testDURING OPERATIONAL TEST, THE R-1 DOOR ESCAPE SLIDE/RAFT FAILED TEST, DID NOT FULLY INFLATE. REPLACED ESCAPE SLIDE/RAFT CONTACTED MAINTENANCE STATION WERE TEST WAS ACCOMPLISHED. SLIDE BOTTLE PRESSURE INDICATOR WAS IN THE 'GREEN', SLIDE DEPLOYED BUT DID NOT FUSDR WRNA200700060Duct · brokenDURING TAKE OFF, NR 2 ENGINE EGT EXCEEDED 960 C, POWER WAS REDUCED BELOW TAKEOFF SETTING, EGT DROPPED BELOW 945 C. DURING CLIMB, NR 2 ENGINE MANIFOLD PRESS 10 PSI, BLEED VALVE REGULATOR LIGHT ON, THEN NR 2 -B- LOOP LIGHT ILLUMINATED, SWITCHED TO -A- LOOP, -A-SDR WRNA200700014Servo Valve · failedAFTER LANDING, NR 3 BRAKE TEMP, WENT TO 700C. INSPECTED IAW 05-51-16, FOUND HEAT DAMAGE REQUIRING BOGIE BEAM REPLACEMENT. TEST OF NR 3 SERVO VALVE INDICATED SERVO VALVE TO BE FAULTY. REPLACED BOGIE BEAM IAW MM 32-11-14, PG 401-411. REPLACED NR 3 BRAKE IAW SDR WRNA200600042Rod End · brokenDURING HEAVY MAINTENANCE WHILE PERFORMING SB A300-27-189, ROD END ON RIGHT ELEVATOR BLUE SYSTEM SERVO SPRING ROD ASSEMBLY, WAS FOUND BROKEN.SDR WRNA200700021Frame · corrodedDURING M72 CHECK, CORROSION WAS FOUND, AFT FUSELAGE FRAME 58 AT STRINGER 39R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS IAW DISPOSITION MSN 207/04 FROM FAA FORM 8110-3 DATED 1-22-07.SDR WRNA200700020Skin · corrodedDURING M72 CHECK, CORROSION WAS FOUND AT AFT EXTERNAL FUSELAGE AT FR 58 BETWEEN STR 24R AND 28R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER IAW REPAIR DISPOSITION MSN 207/03 THROUGH FAA FORM 8110-3 DATED 1-17-07.SDR WRNA200600034Engine · making metalNR 1 ENGINE STALLED 3 TO 4 TIMES, EGT 909 C. REDUCED POWER TO IDLE AND RETURNED TO FIELD FOR SAFE LANDING. POST FLIGHT INSPECTION FOUND METAL IN TAIL PIPE, ENGINE WAS REPLACED IAW 71-00-00 AND AIRCRAFT RETURNED TO SERVICE.SDR WRNA200600016Actuator · unserviceableAFTER TAKEOFF, SEVERE VIBRATION FELT BELOW COCKPIT AFTER GEAR SELECTOR VALVE IN NEUTRAL. RECYCLED GEAR UP AND DOWN, VIBRATION REOCCURRED AFTER PLACING LEVER IN NEUTRAL. YELLOW NOSE GEAR DOOR LIGHT ILLUMINATED ON BOTH GEAR POSITION INDICATORS. RETURNED FOR NSDR WRNA20050030Outflow Valve · unserviceableAFTER TAKEOFF USING SYSTEM NR1 NOTICED AFT OUTFLOW VALVE STAYED FULL OPEN. OPPOSITE SYSTEM SELECTED, NO HELP, UNABLE TO CLOSE MANUALLY. WITH BOTH PACKS ON COULD MAINTAIN 8500 FT CABIN ALTITUDE AT 14000 FT. DUMPED FUEL TO SAFE LANDING WEIGHT (APPROX 2600 GALS)SDR DHL2003368002Proximity Switch · dirtyUNABLE TO RAISE LANDING GEAR LEVER PAST THE OFF POSITION FOR GEAR RETRACTION. TROUBLESHOT PER FIM 32-30-00. SYSTEM NR 1, SENSORS NR 4 & NR 7, FAIL BITE TEST. SYSTEM NR 2 OPS CHECKED OK PER FIM 32-30-00. SYSTEM NR 1 TRANSFERRED TO DMI 12494, PER MEL 32-31-0SDR DHL2003368001Smoke Detector · malfunctionedLAV SMOKE DETECTOR SOUNDED HAD TO BE DISCONNECTED. OPS CHECKED SMOKE DETECTOR IAW M/M 26-17-00. OPS CHECKED GOOD.SDR WRNA200200008Dampener · unserviceableAfter Take off unable to retract landing gear with system 1 or 2. Followed abnormal procedures and returned to airport. Landing normal.Corrective Action: Found L/H MLG pitch dampner at fault. R&R'd dampner I/A/W 32-11-15 Op's check satisfactory. Aircraft returSDR 2001F00152Actuator · inoperativeGROUND AUXILIARY FAULT LIGHT REMAINED ON AFTER TAKEOFF AND DURING CLIMB. AIRCRAFT LANDED NORMAL. REMOVED AND REPLACED AUXILIARY VALVE ACTUATOR IAW 21-31-17. OPS CHECKED GOOD. CLEAR DMI NR 1879. AIRCRAFT RETURNED TO SERVICE. (M)