N876AA

Part: FRAME — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON FRAME STATION 370 BELOW FLOOR LINE RBL 65. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER ESO 11697 ATED 9-14-2001. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

TUL - FOUND SATION 1130 TOP OF FLOORBEAM BETWEEN LEFT SEAT TRACKS CORRODED. FABRICATED AND INSTALLED REPAIR STRAP PER ESO 11697 DATED 9-17-01. (M)

Part: SPLICE — CORRODED (FUSELAGE)

TUL - FOUND LIGHT CORROSION ON END OF STRINGER SPLICE, STATION 686, STRINGER 28R. REMOVED AND REPLACED WITH NEW STRINGER SPLICE PER SRM 51-10-1. (M)

Part: SKIN — CORRODED (LT WING)

TUL - FOUND LOWER WING SKIN CORRODED 18 INCHES BY 3 INCHES, INBOARD OF THE LEFT PLENUM INBOARD ANGLE STATION 830 TO 810. REPAIRED LEFT PLENUM CORROSION (WING SKIN) WITH DOUBLERS PER ESO 11697 DATED 12-08-00. (M)

Part: SKIN — CORRODED (RT WING)

TUL - FOUND LOWER WING SKIN CORRODED 12 INCHES BY 3 INCHES, INBOARD OF RIGHT PLENUM INBOARD ANGLE MULTIPLE AREAS. REPAIRED RIGHT PLENUM CORROSION (WING SKIN) WITH DOUBLERS PER ESO 11697 DATED 12-08-00. (M)

Part: SKIN — CORRODED (LT WING)

TUL - FOUND LOWER WING SKIN LEFT PLENUM HAS SEVERE CORROSION 6 INCHES BY 4 INCHES, IN PREVIOUSLY WORKED AREA LBL 32.2 STRINGER 55 AND 53. REPAIRED LEFT PLENUM CORROSION (WING SKIN) WITH DOUBLERS PER ESO 11697 DATED 12-08-00. (M)

Part: FITTING — CORRODED (BULKHEAD)

TUL - FOUND RBL 28 BULKHEAD ATTACH FITTING HAS HEAVY CORROSION 1 INCH BY .250 INCH, AT STATION 1178-1183 UNDER CABIN FLOOR. INSTALLED NEW FITTING AT RBL 28 ATTACH POINT SRM 51-10-1 AND 51-30-2. (M)

Part: STIFFENER — CORRODED (WING)

TUL - FOUND VERTICAL STIFFENER CORRODED AT AROUND WIRE TERMINAL. FABRICATED AND INSTALLED DOUBLER PER SRM 57-10-4. (M)

Part: LIGHT — INOPERATIVE (CABIN)

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

Part: LIGHT — INOPERATIVE (CABIN)

DFW DURING OVERNIGHT MAINTENANCE L2 OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — CORRODED (CENTER WING)

TUL - FOUND CORROSION ON WING CENTER SECTION LOWER SKIN AFT OF STRINGER 5 BETWEEN RBL 18.55 AND RBL 30.77 AND FORWARD OF STRINGER 5 BETWEEN RBL 18.55 AND RBL 30.77, MAX THICKNESS 113, AFTER CORROSION REMOVAL. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 57-30-3. REPAIR STRAP ADDED PER ESO 11697 DATED 6/19/00. (M)

Part: LIGHT — BROKEN (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT ON FORWARD GALLEY DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT ON FORWARD GALLEY DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AIRSTAIRS)

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

Part: FRAME — CRACKED (BS 910)

TUL - RIGHT W/W STATION 190-913.5 STUB FRAME 2.25 INCH CRACK IN FRAME AT FASTENER STATION 910. INSTALLED REPAIR PER SRM 53-10-2. (M)

Part: WEB — CRACKED (BS 1303)

TUL - APPROX .5 INCH CRACK AT LIGHTENING HOLE AT STATION 1303. STOP DRILLED CRACK AND INSTALLED REPAIR PER 51-40-2. (M)

Part: BEAM — CRACKED (BS 1183)

TUL - FOUND STATION 1183 BULKHEAD, LBL 8, BERTICAL BEAM HAS 1.25 INCH CRACK IN OUTBOARD FLANGE AT LOWER END OF BEAM. STOP DRILLED CRACK AND INSTALLED REPAIR PER SERVICE BULLETIN 727-53-0175.. (M)

Part: SKIN — CRACKED (BS 312)

TUL - FOUND FUSELAGE FORWARD ENTRY LOWER HINGE CUT OUT, SKIN HAS .25 INCH CRACK. ROUTED OUT DAMAGE, INTALLED DOUBLER PER SERVICE BULLETIN 727-53-0198. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TUL - LEFT AND RIGHT OVERWING EXIT EMERGENCY LIGHT, SHORTED TO GROUND INOP. RESPLICED IN NEW LIGHT ASSY. (M)

Part: WIRE — BROKEN (CABIN)

MIA - DURING OVERNIGHT CHECK, RIGHT EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE AT RIGHT AFT EXIT LIGHT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — CRACKED (BS 303)

TUL - FOUND 303.9 FRAME HAS SMALL CRACK EXTENDING FROM CUTOUT/RADIUS FOR STRINGER 16L INTERCOSTAL VIEWED FROM COCKPIT SIDE OF WEB. REPAIRED PER SB 727-53-0153. (M)

Part: SKIN — CORRODED (WING)

FOUND CORROSION ON LOWER SKIN ABOVE RIGHT PRIMARY HEAT EXCHANGER 2 INCH BY 2 INCH. INSTALLED DOUBLER AND TRIPLER PER SRM 57-30-3 FIG 9 AFTER CORROSION REMOVAL. (M)

Part: ANGLE — CORRODED (BS 1176)

TUL - FOUND CORROSION AROUND BOLT HOLE OF 1176 CHORD ANGLE TIED DOWN CABLE EYE BOLT RBL 48 INCHES. INSTALLED SERVICEABLE STRAP PER ESO 11697 DATED 10/21/97. (M)

Part: FRAME — DENTED (BS 580)

TUL - BELL FRAME DENTED STATION 580, BETWEEN STRINGER 24L AND 25L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-10-4 PAGE 3. (M)

Part: STRINGER — CRACKED (BS 344)

TUL - STRINGER 5 RIGHT STATION 344 CRACKED TWO PLACES AT LAV ATTACH BRACKET. REMOVED DAMAGED SECTION OF STRINGER AND SPLICED STRINGER PER SRM 53-10-3. (M)

Part: ANGLE — CORRODED (BS 344-354)

TUL - FOUND CORROSION ON CREASE ANGLE FROM FS 344 TO 354 RIGHT SIDE. REMOVED CORRODED SECTION AND INSTALLED NEW SECTION. (M)

Part: FLOORBEAM — CORRODED (BS 1070)

TUL - FOUND CORROSION ON TOP OF FLOORBEAM. INSTALLED DOUBLER ON FLOORBEAM PER SRM 53-10-8. (M)

Part: FLOORBEAM — CORRODED (BS 344)

TUL - STATION 344 RBL 15 CORROSION ON TOP OF FLOORBEAM. REMOVED CORROSION, FOUND BEYOND LIMITS. REMOVED DAMAGED AREA OF FLOORBOARD INSTALLED DOUBLER PER SRM 53-10-8 PAGE 9CDE AND INSTALLED FILLER FOR REMOVED AREA. (M)

Part: WEB — CRACKED (WS 120)

TUL - WEB CRACKED UNDER NR 7 SPOILER ACTUATOR CASTING, TWO PLACES. REMOVED DAMAGED SECTION OF WEB AND INSTALLED WEB REPAIR PER BOEING SERVIEC BULLETIN 727-57-158. (M)

Part: STRINGER — CORRODED (BS 1030)

TUL - FOUND SKIN BULGE AT STRINGER 27L, STATION 1030. CUT OUT CORRODED SECTION OF STRINGER 27L AND INSTALLED DOUBLER SPLICE PER SRM 53-10-3. (M)

Part: FRAME — DENTED (BS 1090)

TUL - BELL FRAME STATION 1090 ABOVE STRINGER 26L, DENTED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER IAW SRM 53-10-4. (M)

Part: STRINGER — CORRODED (BS 720)

TUL - STRINGER 27R BLOWN OUT OUTBOARD SIDE STATION 720 PLUS 10 INCHES. REMOVED DAMAGED SECTION OF STRINGER SPLICED IN NEW SECTION PER SRM 53-10-3 FIG 1. (M)

Part: STIFFENER — CRACKED (BS 686.5)

TUL - INSPAR STIFFENER UPPER NR 10 CRACKED AT STATION 686.50 LT WING TANK. STOP DRILLED CRACK INSTALLED DOUBLER PER BOEING SB 727-57A159. (M)

Part: SKIN — GOUGED (BS 840)

TUL - GOUGE IN SKIN AT STRINGER 2R, STATION 840 BLENDED BEYOND LIMITS. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3. (M)

Part: STRINGER — CRACKED (WS 686.5)

TUL - TOP WING STRINGER CRACKED AT WS 686.50 AFT CENTER LINE. REPAIRED STRINGER PER BOEING SERVICE BULLETIN 727-57A159. (M)

Part: LIGHT — DEFECTIVE (AFT STAIRS)

DFW - DURING OVERNIGHT CHECK, AFT STAIRS EMERGENCY LIGHT INOPERATIVE. REPLACED AFT STAIRS EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STRINGER — CORRODED (BS 1178)

TUL - FOUND STRINGER 22L AND END FITTING CORRODED FROM STATION 1178 TO 1183. REPLACED STRINGER 22L AFT END FITTING AT STATION 1183 AND SPLICED STRINGER PER SRM 53-10-3 AND CUT OUT SECTION OF SKIN AND INSTALLED FILLER AND DOUBLER PER SRM 53-30-3. (M)