N861AA

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ABOVE AFT GALLEY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ABOVE AFT GALLEY DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SOCKET — DIRTY (EMERGENCY EXIT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHT AT LEFT OVERWING EMERGENCY EXIT DOOR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT STRIP CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AFT STAIRS)

DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR VENTRAL EMERGENCY LIGHT INOPERATIVE. REPLACED AFT STAIR VENTRAL EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BLADE — FAILED (NR 2 ENGINE)

IAH - FLT 1752 - AFTER TAKEOFF IAH WHILE CLIMBING THROUGH 5,500 FEET, CREW NOTICED A SEVERE VIBRATION THEN HEARD A NOISE. NR 2 ENGINE N1 DROPPED TO 48 PERCENT AND OIL TEMPERATURE WAS AT 130 DEGREES CELSIUS. RETARDED NR 2 THROTTLE AND FOLLOWED EMERGENCY ENGINE FAILURE/SHUTDOWN CHECKLIST. NR 1 CFR ADVISED NR 1 ENGINE WAS SMOKING AFTER LEAVING RUNWAY, BUT THEY FELT IT TO BE NORMAL. CREW SHUTDOWN NR 1 ENGINE ALSO. RETURNED AND LANDED IAH WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENGINE. SYSTEM GROUND CHECKED, NORMAL OPERATION. A 1ST STAGE HPT BLADE FAILED AT THE AIRFOIL APPROXIMATELY 2 INCHES FROM THE ROOT. THE FRACTURE IS THE RESULT OF STRESS RUPTURE. (X)

Part: FRAME — BENT (BS 970)

TUL - FRAME BENT AT FLANGE AND WEB STATION 970 BETWEEN STRINGER 25L AND 26L. FRAME REPAIRED PER SRM 51-40-3 WITH .071 INCH 7075T6 MATERIAL, MS2047008 FASTENERS, MS20970D6 FASTENERS IN WEB AND BACB30FQ6 FASTENERS IN FLANGE. (M)

Part: STRINGER — CORRODED (BS 1177)

TUL - FOUND STATION 1177 BELLY SKIN CORRODED AT STRINGER 29 RIGHT. REMOVED CORRODED SECTION STRINGER 29R AT STATION 1177 AND SPLICED IN NEW STRINGER PER SRM 53-10-3 FIG 1. (M)

Part: FRAME — BENT (BS 950)

TUL - FRAME BENT AT FLANGE AND WEB STATION 950F STRINGER 25L TO 26L. REPAIRED FRAME PER SRM 51-40-3 WITH .071 INCH 7075-T6 MATERIAL MS2047008 FASTENERS MS20470D6 FASTENERS IN WEB AND BACB30FQ6 FASTENERS IN FLANGE. (M)

Part: STRINGER — CORRODED (BS 670)

TUL - FOUND STATION 670 STRINGER 27L CORRODED. REPAIRED PER SRM 53-10-3. (M)

Part: SPLICE — FAILED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHTING WAS INOPERATIVE FROM SEAT ROWS 8 THROUGH 18. REPAIRED FAULTY SPLICES IN EMERGENCY FLOOR LIGHTING SYSTEM SEAT ROWS 8 THROUGH 18. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

DTW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT LIGHT AT FORWARD CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTOR AT FORWARD CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: MODULE — FAILED (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR WAS FOUND INOPERATIVE. RE-SEATED EMERGENCY EXIT LIGHT MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (CABIN)

MIA - DURING OVERNIGHT CHECK, L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — NEED REPAIR (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN MAIN CABIN INOPERATIVE. FOUND REVERSE POLARITY IN CABIN EMERGENCY FLOOR LIGHTS, REPAIRED EMERGENCY FLOOR LIGHT WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (BS 490-504)

TUL - FOUND CORROSION ON STRINGER 28R AT STATION 490 TO 504. REPLACED CORRODED SECTION OF STRINGER PER SRM 53-10-3. INSTALLED SKIN DOUBLER PER SRM 5-30-3. CUT OUT DAMAGE ON SKIN. (M)

Part: CASTING — MISDRILLED (BS 870)

TUL - FIGURE 8 HOLE STATION 870, CASTING IN LEFT MAIN WHEEL WELL. FIGURE 8 HOLE REPAIRED PER ESO 11697, DATED 3-17-97. (M)

Part: SLIDE — MALFUNCTIONED (PAX DOOR)

TUL - FOUND LEFT FORWARD ENTRY DOOR EVACUATION SLIDE DEPLOYED PER CARD 4993 DEFLATED TO AN UNUSABLE CONDITION IN LESS THAN 15 MIN, APPROX 8 MIN PER ITEM NR 7. FLAPPER VALVES LEAKING. REMOVED AND REPLACED SLIDE OR CARD 4493 ITEM. (M)

Part: STRINGER — CORRODED (BS 560)

TUL - FOUND CORROSION IN STRINGER 27L, JUST AFT OF FS 560 FLANGE. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-10-3. (M)

Part: SKIN — CORRODED (BS 700)

TUL - FOUND FUSELAGE SKIN CORRODED THROUGH AT STATION 700, INBOARD SIDE OF STRINGER 28R. REMOVED AND INSTALLED NEW SKIN SECTION AND SPLICED SKIN PER SRM 53-30-3 PAGE 5, FIG 1. (M)

Part: STRINGER — CORRODED (BS 1152-1158)

TUL - FOUND CORROSION ON STRINGER NR 30, STATION 1152-1158. CUT OUT CORRODED STRINGER. REPLACED CORRODED AREA WITH SPLICED STRINGER PER SRM 53-10-3. (M)

Part: STRUT SEAL — LEAKING (NLG)

TPA - FLT 0861 - DURING GEAR RETRACTION HAD A NOTICEABLE SHUTTER VIBRATION FROM THE NOSE GEAR AREA. RED NOSE GEAR DOOR WARNING LIGHT ILLUMINATED. RECYCLED GEAR TO NO AVAIL. LANDED TPA WITHOUT FURTHER INCIDENT. REPLACED STRUT SEALS AND SERVICED NOSE GEAR PER MM. LEAK AND TAXI CHECKED NORMAL PERFORMED GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)