N860AA

Part: LIGHT — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. REPLACED FIRST CLASS EMERGENCY EXIT FLOOR PATH DAMAGED SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DAMAGED (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, COACH EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. REPLACED COACH EMERGENCY EXIT FLOOR PATH DAMAGED SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AIRSTAIR)

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

Part: LIGHT — INOPERATIVE (AIRSTAIR)

DFW - DURING OVERNIGHT MAINTENANCE, AIRSTAIR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED AIRSTAIR OVERHEAD EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: ANGLE — DAMAGED (BS 330)

TUL - FOUND HORIZONTAL CHORD ANGLE ABOVE FORWARD LEG OF LEFT TRUNNION FITTING HAS CUT FROM PREVIOUS WEB REPAIR. INSTALLED DOUBLER STRAP 51-40-00-1. (M)

Part: FAN — FAILED (ACM BAY)

MIA - FLT 1403 - DESCENDING THROUGH 8000 FEET AT MIA, A STRONG ELECTRICAL AND PLASTIC ODOR OCCURRED THROUGH OUT CABIN. DECLARED EMERGENCY AND LANDED MIA WITHOUT INCIDENT. REPLACED GASPER FAN. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AIRSTAIRS)

TUL - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (AFT AIRSTAIR)

TUL - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED CONNECTOR TO AFT AIRSTAIR EMERGENCY EXIT LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — OUT OF POSITION (ROW 22)

DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT ROW 22 INOPERATIVE. REPOSITIONED WIRES ON BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DEFECTIVE (ROW 7DEF)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN FIRST AND COACH CABIN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH FLAP JUMPER WIRE AT SEAT ROW 7DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRINGER — CORRODED (BS 689)

TUL - CORROSION INSIDE STRINGER 28R, STA 689. INSTALLED STRINGER REPAIR IAW SRM 53-10-3 FIGURE 1. TST: 61,081.50 HOURS. CYCLES: 38,758. (X)

Part: SKIN — CORRODED (BS 682-686)

FUSELAGE SKIN CORRODED OUTBOARD SIDE OF STR 28R, STA 684. CUT OUT CORRODED SKIN, INSTALLED REPAIR IAW SRM 53-30-3, FIG 1. TST: 61,081.50 HOURS. CYCLES: 38,758. (X)

Part: SKIN — CRACKED (PASSENGER DOOR)

TUL - FORWARD ENTRY DOOR LOWER HINGE CUT-OUT IS CRACKED. REPAIRED PER SB 727-53-0198 FIG 4. DOUBLER IS .063 INCH AISI 15-5PH HEAT TREATED TO 150-170 KSI CADMIUM PLATED. FASTENERS ARE BACB30KK6A AND BACB30KK8A. TST: 61,081.50 HOURS. CYCLES: 38,758. (X)

Part: LIGHT — DEFECTIVE (AIR STAIRS)

DFW - DURING OVERNIGHT CHECK, AIR STAIR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AIR STAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — FAILED (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN COACH CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — CORRODED (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS FOR LAST SIX FEET OF TRACK INOPERATIVE. SPLICED NEW WIRE IN EMERGENCY EXIT FLOOR PATH LIGHT STRIP. (M)

Part: OIL PUMP — LOOSE (NR 1 ENGINE)

TPA - FLT 1029 - EN ROUTE DCA-MIA - AT 33,000 FEET, NR 1 OIL TEMP WENT INTO CAUTION ZONE AND OIL QTY DECREASED TO 1 GALLON. OIL QTY CONTINUED TO DECREASE, OIL TEMP STAYED IN THE CAUTION FOR 15 MINUTES AND NR 1 ENGINE WAS SHUTDOWN. DELCARED AN EMERGENCY AND DIVERTED TO TPA. LANDED TPA WITHOUT INCIDENT. REPLACED NR 1 ENGINE, SYSTEM GROUND CHECKED NORMAL OPERATION. THE CAUSE FOR ENGINE REMOVAL AND SHUTDOWN WAS FAILURE OF THE 4/5 SCAVENGE PUMP. AT ENGINE TEAR DOWN, THE 4/5 SCAVENGE PUMP HOUSING ASSY MOUNTING BOLTS WERE FOUND LOOSE. FINDINGS DURING DISASSEMBLY REVEALED ONE EACH MOUNT BOLTS LYING IN THE NR 4 BEARING HOUSING WITH SAFETY WIRE BROKEN, AND THE OTHER TWO MOUNT BOLTS WERE HAND TIGHT. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT PASSENGER SEAT ROW 19 INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT PASSENGER SEAT ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FUEL TANSFER SYS — MALFUNCTIONED (NR 3 TANK)

DTW - FLT 0583 - DURING CRUISE FROM BDL/ORD, LATERAL FUEL IMBALANCE NOTED. NR 3 FUEL TANK WOULD NOT DECREASE. AIRCRAFT AIR INTERRRUPTED AND LANDED DTW WITHOUT INCIDENT. INSPECTED FUEL PANEL AND TRANSFERRED FUEL FROM TANK NR 3 TO TANKS 1 AND 2. UNABLE TO DUPLICATE ON GROUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. ACCOMPLISHED FUNCTIONAL CHECK, FLIGHT WITH NORMAL OPERATION. (X)

Part: STIFFENER — CRACKED (NLG TRUNNION)

TUL - RIGHT FORWARD VERTICAL STIFFENER FOR NOSE LANDING GEAR TRUNNION SUPPORT FITTING CRACKED 2 PLACES AT CENTER FASTENERS, STA 302. REMOVED AND INSTALLED NEW STIFFENER. TST: 56,297. CYCLES: 36,203. (X)

Part: DOOR FRAME — CRACKED (BS 950)

TUL - AFT CARGO DOOR FRAME CRACKED IN 2 PLACES AT THE FORWARD LOWER STEP FITTING FS 950F. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SB 727-53A0199 NSC-1 DATED 11-29-90. TST: 56,297 HOURS. CYCLES: 36,203. (X)

Part: BELL FRAME — MISDRILLED (BS 660)

TUL - BELL FRAME DAMAGED (DRILLED AT RADIUS). INSTALLED DOUBLER PER SRM 53-10-4. TST: 56,297. CYCLES: 36,203. (X)

Part: BELL FRAME — MISDRILLED (BS 680/700/720)

TUL - BELL FRAME DAMAGED (DRILLED) STA 680 ABOVE STR 26L, STA 700 AND STA 720. BELL FRAME REPAIRED PER SRM 51-40-3. TST: 56,297 HOURS. CYCLES: 36,203. (X)

Part: ANGLE — CRACKED (WS 224)

TUL - LOWER CHORD ANGLE AT NR 4 FLAP TRACK IS CRACKED. REPAIRED CHORD ANGLE PER ESO 11697 DATED 5-6-97. TST: 56,297 HOURS. CYCLES: 36,202. (X)

Part: STRINGER — CORRODED (BS 970-990)

TUL - CORROSION ON STR 27R BETWEEN BS 970 AND BS 990, 8 INCHES AFT OF LOWER CORNER FOR CARGO DOOR CUT-OUT. REMOVED CORRROSION AND REPAIRED PER ESO 11697 DATED 5-1-97 AND SRM 51-40-4. TST: 56,297 HRS. CYCLES, 36,203. (X)

Part: STRINGER — CRACKED (WS 656)

TUL - WING TANK STR 9 CRACKED AT UPPER FRAME ATTACHMENT. STOP DRILLED CRACK AND REPAIRED PER SB 727-57A159. TST: 56,297 HRS. CYCLES, 56,203. (X)

Part: BELL FRAME — DENTED (BS 950)

TUL - DENT IN BELL FRAME AT BS 950F BETWEEN STR 25L AND STR 26L. CUT OUT DENT AND INSTALLED DOUBLER PER SRM 53-10-4 PAGES 3A TO 6. TST: 56,297. CYCLES: 36,203. (X)

Part: STRINGER — CRACKED (WS 656.5)

TUL - STR 9 UPPER CRACKED AT STA 656.50 (INSIDE WING). REPAIRED PER SB 727-57A159. TST: 56,297 HOURS. CYCLES: 36,203. (X)

Part: STRINGER — CORRODED (BS 950)

TUL - CORROSION ON STR 27R BETWEEN STA 950E AND STA 950F AROUND WATER FLAPPER DRAIN. REMOVED AND BLENDED OUT CORROSION AND REPAIRED PER SRM 51-40-4 AND ESO 11697 DATED 5-1-97. TST: 56,297 HRS. CYCLES, 36,203. (X)

Part: SPLICE — CORRODED (BS 680)

TUL - CORROSION ON STR 26R PRODUCTION SPLICE AT STA 680. REPLACED CORRODED SPLICE PLATE WITH NEW PART PER SRM 51-20-01-1. TST: 56,297. CYCLES, 36,203. (X)

Part: LEVER — LACK OF LUBE (LANDING GEAR)

EWR - FLT 554 - DURING APPROACH TO EWR WHEN LANDING GEAR EXTENDED, ALL THREE GEAR RED LIGHTS ON FORWARD PANEL REMAINED ILLUMINATED AFTER THREE GREEN LIGHTS ILLUMINATED. F/E ANNUNCIATOR PANEL INDICATIONS WERE NORMAL. VISUALLY CONFIRMED ALL GEAR DOWN AND LOCKED AND AIRCRAFT LANDED EWR WITHOUT INCIDENT. CHECK REVEALED LANDING GEAR HANDLE WAS SELECTED DOWN, BUT NOT LOCKED IN DETENT. CLEANED AND LUBRICATED GEAR SELECTOR MECHANISM. ALL GEAR SELECTION AND LIGHT INDICATIONS CHECKED NORMAL. (M)

Part: TRACK — CORRODED (LT TE FLAP)

AFW - FOUND FLAP TRACK CORRODED. NR 4 TRACK RECEIVED FROM SHOP ON E58 1814356, INSTALLED NR 4 TRACK ONE 58 1814340. (M)

Part: STRINGER — CORRODED (BS 1150)

AFW - FOUND CORRODED STRINGER. REPAIRED STRINGER IAW SRM 53-10-3. (M)

Part: STRINGER — CORRODED (BS 958)

AFW - FOUND STRINGER CORRODED. REPAIRED PER SRM 53-10-3. (M)

Part: SHEAR TIE — CORRODED (BS 700)

AFW - FOUND SHEAR TIE CORRODED. REMOVED AND REPLACED SHEAR TIE WITH NEW PART. (M)

Part: SKIN — CORRODED (BS 700)

AFW - FOUND SKIN CORRODED. REPAIRED SKIN PER SRM 53-30-3. (M)

Part: SKIN — CORRODED (BS 950)

AFW - FOUND FUSELAGE SKIN CORRODED. REPAIRED PER SRM 53-30-3. (M)

Part: WEB — CORRODED (BS 950)

AFW - FOUND WEB CORRODED. REMOVED AND INSTALLED NEW WEB. (M)

Part: SKIN — CORRODED (FUSELAGE)

AFW - FOUND CORRODED FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-3-3. (M)

Part: BOLT — RUSTED (LT TE FLAP)

AFW - FOUND MID MOUNT BOLT RUSTED. REPLACED MOUNT BOLTS PER 52-10-G. REINSTALLED FLAP TRACK PER 57-53-7. (M)

Part: SKIN — CORRODED (BS 1008)

AFW - FOUND FUSELAGE SKIN CORRODED AT STATION 1008, STATION 30-29. INSTALLED EXTERNAL DOUBLER STATION 1010 STRINGER 30 AS PER SRM 53-30-3. INSTALLED STRINGER SPLICE STATION 1000 TO 1020 STRINGER 30 AS PER SRM 53-10-3. (M)

Part: TRACK — CORRODED (RT TE FLAP)

AFW - AFT SPAR FITTING CORRODED. INSTALLED NEW NR 5 FLAP TRACK SPAR FITTING. (M)

Part: TRACK — RUSTED (LT TE FLAP)

AFW - TWO AFT MOUNT BOLTS RUSTED. REPLACED MOUNT BOLTS PER 52-10-6. REINSTALLED FLAP TRACK PER 57-53-2. (M)

Part: SUPPORT — CORRODED (BS 570)

AFW - FOUND CORROSION ON FLOOR SUPPORT AT STATION 570, ABOVE STRINGER 28R. INSTALLED NEW STRAP ALODINE, PRIMED AND PAINTED AS PER SRM 52-10. (M)

Part: BRACKET — CORRODED (CARGO COMPT)

AFW - FOUND CORROSION ON TOP OF ALL CARGO NET TIE DOWN BRACKETS, AT DOOR CUTOUT. REPLACED CARGO NET TIE DOWN BRACKETS. (M)

Part: SUPPORT — CORRODED (BS 640-720)

AFW - FOUND SUPPORT CORRODED. REMOVED AND REPLACED DAMAGED AREA. (M)

Part: STRINGER — CORRODED (BS 950)

AFW - FOUND STRINGER 29L BETWEEN STATION 950E AND 950F HAD CORROSION BLENDED BEYOND SRM LIMITS. INSTALLED A REPAIR STRAP PER MRB 727-0015. (M)

Part: SWITCH — DEFECTIVE (F/E PANEL)

MCI - FLT 1714 - AFTER TAKEOFF MCI DURING CLIMB-OUT, ELECTRICAL ODOR NOTED IN COCKPIT. ACCOMPLISHED ABNORMAL PROCEDURES AND ODOR DISSIPATED. AIRCRAFT RETURNED TO MCI AND LANDED WITHOUT INCIDENT. REPLACED SWITCH AND TERMINALS AT F/E PANEL FOR CENTER FUEL TANK LEFT FORWARD BOOST PUMP. ACCOMPLISHED GROUND ENGINE RUN AND OPERATED PACKS WITH NO ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO ELECTRICAL ODOR NOTED. (M)

Part: RETAINING NUT — LOST TORQUE (NR 3 BEARING)

AFTER TAKEOFF SLC CLIMBING THROUGH FL 323, NR 3 ENG FAILED WITH NO OIL PRESS OR N2 IND AFTER FAILURE. ACCOMP ENG FAILURE AND PRECAUTIONARY SHUTDOWN CHECKLIST FOR NR 3 ENG AND A/C RETURNED W/O INCIDENT. REPLACED NR 3 ENG. ACCOMP LK CHKS AND GROUND ENG RUN WITH NO DEFECTS FOUND. SYS GROUND CHECKED NORM OPS. ENG SHUTDOWN RESULTED FROM FAILURE OF THE NR 3 BEARING STACK. THE HARDWARE WAS ALLOWED TO ROTATE ON STUB SHAFT WHEN THE RETAINING NUT LOST ITS INSTALLATION TQ. EVENTUALLY, RESULTANT WEAR CAUSED THE STUB SHAFT AND BEARING HARDWARE TO FAIL WHICH SEIZED THE N2 ROTOR. PWA S/B 5905, WHICH INCORP A PINNED NR 3 BEARING STACK ASSY, HAD NOT BEEN PERFORMED ON ENG. REPAIRED AND RETURNED TO SERV. (M)