N871AA

Part: LIGHT — INOPERATIVE (AIRSTAIR)

DFW DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT IN AIR STAIR VENTURI INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN AIR STAIR VENTURI. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

MIA DURING OVERNIGHT MAINTENANCE AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: WIRE — BROKEN (MLG)

MCI - FLT 1370 - AFTER TAKEOFF DURING CLIMB, LEFT GEAR RED WARNING LIGHT ILLUMINATED. REPAIRED WIRE FOR LEFT MAIN GEAR UPLOCK SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION. REPLACED LANDING GEAR ACCESSORY UNIT AS PRECAUTION. (M)

Part: CONNECTOR — DAMAGED (CABIN)

MIA - DURING OVERNIGHT MAINTENANCE, EXIT ESCAPE PATH LIGHTS CENTER STRIP INOPERATIVE. REPLACED MID-AISLE LIGHT STRIP CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (CABIN)

DFW - FOUND DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. TIGHTENED AFT AIRSTAIR EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (AFT STAIRS)

DFW - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIR STAIRS EMERGENCY EXIT LIGHT ASSEMLBY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: STIFFENER — CORRODED (BS 184.8)

TUL - OUTBOARD LOWER VERTICAL STIFFENER, CORROSION BELOW TANK STUB PLATE. DRILLED UP AND INSTALLED NEW STIFFENER PER ESO 11697 DATED 11/18/99, SEALED FASTENERS INTERNALLY; LEAK CHECKED. STIFFENER, OK, TANK CLEAR, CLOSE, LEAK CHECK. (X)

Part: SKIN — CORRODED (WING)

TUL - LOWER WING SKIN INSIDE PLENUM ARM, STR S5L, BUTT SPLICE AFT SKI SECTION, RBL 27-28 HAS SKIN EXFOLIATED AROUND RIVETS. INSTALLED FILLER, DOUBLER AND TRIPLER PER SRM 57-30-3, AND ESO 11697 DATED NOVEMBER 18, 1999. TST: 59,603 HOURS. CYCLES: 35,983. (X)

Part: SHEAR TIE — CORRODED (BS 1166)

TUL - AFT SIDE 1166 FRAME/SHEAR TIE LOWER LEG CORRODED FROM STR 28L - STR 27L. REMOVED AND REPLACED SHEAR TIE FROM STR 28L - STR 27 AT STA 1166 PER SRM 51-10-1. TST: 59,603 HOURS. CYCLES: 35,983. (X)

Part: SKIN — CREASED (BS 1140)

TUL - SKIN DENTED AND CREASED OVER STR 21L AT BS 1140. CUT OUT 3 INCH BY 3 INCH SECTION OF SKIN, DID AN INTERNAL INSPECTION OF SURROUNDING STRUCTURE, NO ADDITIONAL DEFECTS FOUND. REPAIRED SKIN WITH SOLID RIVET REPAIR PER SRM 53-30-3 FIG 3. TST: 59,603 HOURS. CYCLES: 35,983. (X)

Part: SKIN — CRACKED (BS 1110)

TUL - ONE INCH LONG CRACK IN FUSELAGE SKIN SIX FEET FORWARD OF TAIL SKID. SJU REPORTS CORROSION IN AREA OF CRACK. CRACKED/CORRODED SKIN AND SHEAR TIE REMOVED AND REPLACED WITH NEW SHEAR TIE AND SKIN DOUBLER T3-2024-0.071 INCH PER REPAIR SRM 53-30-3, FIG 1. TST: 59,320 HOURS. CYCLES: 35,833. (X)

Part: LIGHT — FAILED (AFT STAIRS)

TPA - DURING OVERNIGHT MAINTENANCE, AFT AIRSTAIRS THRESHOLD EMERGENCY EXIT LIGHT WOULD NOT TEST. REPLACED AFT AIRSTAIRS THRESHOLD EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DEFECTIVE (AFT AIRSTAIRS)

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

Part: GEAR WARNING — ACTIVATED (NLG)

ORD - FLT 1461 - EN ROUTE MCO-ORD, NOSE GEAR RED LIGHT ILLUMINATED AFTER GEAR EXTENSION, RECYCLED GEAR AND LIGHT WENT OUT. LANDED ORD WITHOUT INCIDENT. JACKED AIRCRAFT NOSE, ACCOMPLISHED GEAR SWING THREE TIMES. UNABLE TO DUPLICATE ON GROUND. SYSTEM GROUND CHECKED NORMAL OPERATION. LUBRICATED GEAR LINKAGE. (M)

Part: LIGHT — INOPERATIVE (AFT STAIR)

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

Part: WIRE — SHORTED (GALLEY)

BNA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTING WOULD NOT ILLUMINATE. REPAIRED SHORTED WIRE IN EMERGENCY FLOOR LIGHTING AT FORWARD GALLEY SIDEWALL LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (BS 840-850)

TUL - FOUND CORROSION BULGE IN WING LOWER SKIN CENTER SECTION STATION 840-850 RT ABOVE PRIMARY HEAT EXCHANGER. BLENDED CORROSION FROM AREA AND INSTALLED DOUBLER PER SRM 57-30-3. (M)

Part: SKIN — CORRODED (BS 836)

TUL - FOUND CORROSION BULGE IN WING LOWER SKIN WING CENTER SECTION STATION 836 LEFT ABOVE PRIMARY HEAT EXCHANGE. PERFORMED REPAIR ON WING LOWER SKIN WING CENTER SECTION AT STATION 836 ABOVE PRIMARY HEAT EXCHANGER IAW BOEING 727 SRM CH 57-30-3 PAGE 5 FIG 9. (M)

Part: FITTING — CORRODED (TE FLAP)

TUL - NR 4 FLAP TRACK FORWARD SUPPORT FITTING CORRODED. REMOVED NR 4 FORWARD FLAP TRACK FORWARD SUPPORT AND REPLACED WITH SERVICEABLE LIKE UNIT. (M)

Part: GEAR BEAM — CORRODED (LT MLG)

TUL - FOUND CORROSION ON LOWER MLG BEAM AT AREA. REPAIR PER ESO 11697, DATED 11-17-97. (M)

Part: KEEL BEAM — CRACKED (BS 870)

TUL - KEEL BEAM CRACKED RIGHT SIDE JUST AFT OF 870. REPAIRED IAW ESO 11697 DATED 10-15-97 AND SB 53-208. (M)

Part: SKIN — CRACKED (BS 1090)

TUL - SKIN GOUGED, GOUGE HAS CRACK AT STATION 1090 STRINGER 28R. NDT GOUGE, FOUND TO BE CRACKED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3. (M)

Part: FRAME — BENT (BS 1070)

TUL - FOUND STATION 1070 FRAME BENT UPPER FLANGE STRINGER 27R-26R. STRAIGHTENED DENT INSTALLED DOUBLER PER AARD 53-10-07-3 51-40-3 AND 53-10-4. (M)

Part: ANGLE — CORRODED (WS 368-410)

TUL - CORROSION ON FRONT SPAR LOWER CHORD ANGLE ON LOWER PANEL LANDING SURFACE STATION 368 TO 410. INSTALLED 301 .25 HARD STAINLESS DOUBLER .050 BY 2.625 INCH BY 55 INCHES PER AARD 57-20-00-2. (M)

Part: FLOORBEAM — CORRODED (BS 380)

TUL - TOP OF FLOORBEAM CORRODED STATION 380, RBL 23 INCHES TO RBL 60 INCHES. REMOVED CORROSION FROM FLOORBEAM STATION 380 RBL 23 INCHES TO RBL 60 INCHES PER SRM 51-10-6 AND INSTALLED REPAIR ANGLE TO UPPER AFT FLANGE (CHORD ANGLE) STATION 380 RBL 47 INCHES TO 61 INCHES PER AARD 53-10-07-2 FIG 2 PAGE 4 DATED 3-20-96. TREATED AND PRIMED PER SRM 51-10-2. (M)

Part: FRAME — CORRODED (BS 1166)

TUL - BELT FRAME AT STRINGER 16R STATION 1166 CORRODED. BLENDED OUT CORROSION PER SRM 51-10-6. CUT OUT CORROSION, INSTALLED FILLER AND DOUBLER PER SRM 53-10-4. TREATED AND PRIMED ALL PARTS. (M)

Part: FLOORBEAM — CORRODED (BS 1110)

TUL - FOUND CORROSION TOP OF FLOORBEAM STATION 1110 RBL 10. INSTALLED DOUBLER PER SRM 53-10-8. (M)

Part: SIGN — DEFECTIVE (CABIN)

DTW - DURING OVERNIGHT CHECK, AFT GALLEY DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED AFT GALLEY DOOR EMERGENCY EXIT SIGN. PRECAUTIONARY REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (BS 720)

AFW - FUSELAGE SKIN CORRODED AT STATION 720F. INSTALLED DOUBLER PER MRB 727-0032. (M)

Part: SKIN — CORRODED (BS 682)

AFW - FOUND CORROSION ON SKIN AT STATION 682 ABOVE STRINGER 27L. REMOVED CORRODED SECTION OF SKIN AND INSTALLED DOUBLER PER SRM 53-30-3. (M)

Part: SKIN — CORRODED (BS 683)

AFW - FOUND CORROSION ON SKIN AT STATION 683 AND STRINGER 26R. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-30-3. (M)

Part: SKIN — CORRODED (BS 698)

AFW - FOUND CORROSION ON SKIN AT STATION 698 AND STRINGER 26RF. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED REPAIR IAW SRM 53-30-3. (M)

Part: SKIN — CORRODED (CENTER WING)

TUL - INTERGRANULAR CORROSION BOTTOM CENTER WING SKIN ABOVE LT PRIMARY HEAT EXCHANGER, AND ABOVE RT PRIMARY HEAT EXCHANGER. CORROSION REMOVED. FLAP PEENED, ALODINED, AND PRIMED PER ESO 11697. TST, 49,700 HOURS. CYCLES, 30,826. (X)

Part: WHEEL — FAILED (NR 2 POSITIION)

MIA - FLT 0993 - UPON ARRIVAL AT THE GATE IN MIA, NR 2 MAIN WHEEL WAS DISCOVERED FLAT AND MISSING APPROXIMATELY 50 PERCENT OF THE INBOARD WHEEL HALF WITH STONE DEFLECTOR BENT AND SCORING TO NR 2 BRAKE. REPLACED NR 1 AND NR 2 MAIN WHEEL AND TIRE ASSEMBLIES. ALSO, REPLACED STONE DEFLECTOR AND NR 2 BRAKE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: DOOR FRAME — CRACKED (FORWARD GALLEY)

TUL - FLT 1393 - EN ROUTE DFW/TUL DURING CRUISE, AIR LEAK NOTED AT FORWARD GALLEY DOOR. AIRCRAFT LANDED TUL WITHOUT INCIDENT. CHECKED FORWARD GALLEY DOOR AREA AND FOUND UPPER AFT CORNER AREA OF DOOR SKIN BULGING OUT AND DOOR FRAME CRACKED FROM GATE HINGE DOWN APPROXIMATELY 6 INCHES. REPLACED FORWARD GALLEY DOOR. ACCOMPLISHED PRESSURIZATION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: DUCT — CRACKED (NR 2 ENGINE)

JFK - FLT 1251 - AFTER TAKEOFF EWR DURING CLIMB-OUT, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED WHEN NR 2 POWER LEVER WAS RETARDED TO IDLE. JETTISONED FUEL AND AIRCRAFT DIVERTED TO JFK, LANDING WITHOUT INCIDENT. REPAIRED NR 2 ENGINE FIREWALL THERMO ANTI-ICE DUCT FOUND CRACKED. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)