N132AA

Part: SENSOR — MALFUNCTIONED (MLG)

HNL - FLT 23 - ALL 3 GEAR UNSAFE LIGHTS CAME ON, APPROX 3-4 SECONDS IN CRUISE FLIGHT. CHECKED HYD SYSTEM 3, PRESSURE READ 3200 PSI, HYD QTY READ 9 QTS. LEFT PUMP ON AND RT PUMP OFF. CHECKED GEAR VISUAL INDICATORS, OK. (M)

Part: PUMP — FAILED (HYD SYSTEM)

HNL - FLT 212 - NR 2 HYD QTY DROPPED TO 1 GALLON AND NR 2 SYSTEM PRESSURE WENT OT ZERO. FOLLOWED CHECKLIST AND LANDED NORMALLY. REPLACED NR 2 LEFT ENGINE DRIVEN HYD PUMP. SERVICED NR 2 HYD RES PUMP, LEAK CHECK OK. (M)

Part: SOCKET — WORN (NR 1 ENGINE)

FLT 932 - HNL - NR 1 ENGINE B LOOP INOPERATIVE. REMOVED AND REPLACED WORN SOCKETS AT R5-8014 PINS V/P. GROUND TEST OF NR 1 ENGINE B LOOP OK. (M)

Part: LOOP — MALFUNCTIONED (NR 2 ENGINE)

LAX - FLT 03 - MANIFOLD FAIL ENGINE NR 2 LIGHT AND MASTER WARNING LIGHTS FLICKERED DURING TAKEOFF ROLL UNTIL AND DURING CRUISE FLIGHT, TEMP AND PRESS GAUGES INDICATE NORMAL READINGS. REPLACED NR 2 MANIFOLD UPPER LOOP P/N 5932361. REQS OPS CHECK. RESET C/B''S, OPS CHECK NORMAL. ACCOMPLISHED TAKEOFF POWER RUN 2 MIN. MCT 2 MIN AND CL POWER 5 MIN WITH NR 2 ACM ON. NO FAULTS NOTED. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

TUL - FOUND FLOOR SUPPORT AT FLOOR LINE STRINGER 27R HAS CORROSION STATION 1902-1921. REPAIRED WEB AT STRINGER 27R, STATION 1902-1921 PER ESO 7349, DATED 6/7/2000. (M)

Part: CONNECTOR — LOOSE (ROW 7 HJ)

DFW - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 7HJ INOPERATIVE. RESEATED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR PIN AT SEAT 7HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SLIDE — DEFECTIVE (PAX DOOR)

IAD - AT GATE, L2 SLIDE FELL OUT BUT DID NOT SUCCESSFULLY DEPLOY. REPLACED L2 SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CARGO POD — CONTAMINATED (CARGO COMPT)

TPA - FLT 207 - AFTER TAKEOFF MIA DURING CLIMB-OUT, FUMES WERE NOTED BY F/A IN LOWER LOBE GALLEY. AIRCRAFT DUMPED FUEL AND DIVERTED TO TPA, LANDING WITHOUT INCIDENT. SOURCE OF FUMES WAS DETERMINED TO BE RESIDUAL ODOR FROM EMPTY CARGO POD IN AFT CARGO COMPARTMENT. REMOVED EMPTY CARGO POD AND AIRCRAFT MAINTENANCE FERRY TPA/MIA. PRECAUTIONARY CHECKED ALL OVENS OPERATION IN LOWER LOBE GALLEY WITH NO DEFECTS NOTED. REPLACED 3 PBE UNITS FROM MAIN CABIN USED DURING THE EVENT. SYSTEMS GROUND CHECKED NORMAL OPERATION WITH NO FUMES NOTED. (M)

Part: ROLLER TRAY — CORRODED (BS 1701-1786)

TUL - OMNI ROLLER TRAY IS CORRODED 4TH FROM DOOR. MANUFACTURED AND INSTALLED NEW TRAY PER 51-01-00-05. (M)

Part: LONGERON — CORRODED (BS 1099-1156)

TUL - LONGERON 48 LEFT CORRODED FROM STATION 1099 TO 1156. MANUFACTURED AND SPLICED IN NEW SECTION OF LONGERON 48L FROM STATION 1089 TO 1156 PER SRM 53-10-00 FIG 5. (M)

Part: SKIN — CORRODED (BS 1119)

TUL - SKIN CORRODED UNDER TEAR STRIP AT STATION 1119 BETWEEN LONG 47L AND 48L. INSTALLED DOUBLER AT STRINGER 48L FS 1119 PER SRM 53-20-00 FIG 6. (M)

Part: LONGERON — CORRODED (BS 1099-1119)

TUL - FOUND LONGERON 48L HAS CORROSION ON OUTBOARD BOTTOM LEG AFT OF STATION 1099 AND ALSO CORRODED BETWEEN STATION 1099 AND STATION 1119. SPLICED IN NEW SECTION OF LONGERON 48L FROM STATION 1089 TO FS STATION 1159 PER SRM 53-10-00 FIG 5. (M)

Part: BEARING — CORRODED (LT TE FLAP)

TUL - OUTBOARD FLAP, OUTBOARD HINGE BEARING BORE HAS CORROSION IN BORE INNER DIAMETER. BORED HINGE BEARING BORE TO 2.344 TO REMOVE CORROSION. EXCEEDS CMN 7327, 57-44-09 PAGE 407 LIMITS, MFG AND INSTALLED NEW BUSHING PER MM 57-44-08. (M)

Part: BEARING — CORRODED (LT TE FLAP)

TUL - OUTBOARD FLAP, INBOARD HINGE BEARING BORE HAS CORROSION IN BORE INNER DIAMETER. BORED HINGE BEARING BORE TO 2.344 TO REMOVE CORROSION (EXCEEDS CMM 7327, 57-44-09 PAGE 407 LIMITS) MFG AND INSTALLED NEW BUSING PER MM 57-44-08. (M)

Part: CYLINDER — LEAKING (LT MLG DOOR)

SFO - FLT 65 - EN ROUTE/JFK/SFW, DURING CRUISE, SYSTEM NR 3 HYDRAULIC QTY BEGAN TO DECREASE. ACCOMP ABNORMAL PROCEDURES FOR SYSTEM NR 3 HYD QTY LOSS AND A/C PROCEEDED TO SFO. ACCOMPLISHED ALTERNATE GEAR EXTENSION AND AICRAFT LANDED SFO WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR DOOR CYLINDER. SERVICED SYSTEM NR 3 HYDRAULICS AND RESTOWED ALTERNATE GEAR EXTENSION HANDLE. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)

Part: WINDOW — CRACKED (CABIN)

MIA - FLT 588 - EN ROUTE SDQ/JFK DURING CRUISE, CABIN WINDOW OUTER PANE AT PAX SEAT 12A CRACKED ALONG EDGE OF FRAME. AIRCRAFT DIVERTED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED OUTER WINDOW PANE AND SEAL AT PAX SEAT 12A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: TR DRIVE — DEFECTIVE (NR 2 ENG)

HNL - FLT NR 14 - DURING CLIMB-OUT, FLT CREW NOTED IMPAIRED CLIMB PERFORMANCE AND SOME AILERON AND RUDDER TRIM REQUIRED TO MAINTAIN WINGS LEVEL. A/C RETURNED TO HNL AND LANDED W/O INCIDENT. AFTER ARRIVAL, NR 2 ENG RT TRANSLATOR COWL NOTED PARTIALLY DEPLOYED. COWL MANUALLY STOWED AND NR 2 REVERSER PLACARDED INOP. SUBSEQUENTLY AT LAX/26, REPLACED NR 2 ENG RT REVERSER HALF AND REPLACED CORE HOUSING AND DRIVE CABLE ON LT REVERSER HALF. ACCOMPLISHED THRUST REVERSER RIGGING BUT CONTINUED PLACARD. SUBSEQUENTLY AT JFK/28, REPLACED NR 2 ENG LT REVERSER HALF, NR 2 ENG THRUST REVERSER DRIVE AND SHUTOFF VLV. ACCOMP LEAK AND GROUND CHECK WITH NO DEFECTS FOUND. SYS GROUND CHECKED NORMAL OPERATION. (M)