N76202

Part: ACCUMULATOR — LOW (THRUST REVERSER) · airframe 69,260 hrs · 30,061 cycles

RIGHT THRUST REVERSER ACCUMULATOR LOW LIGHT ILLUMINATED. FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. SERVICED RT REVERSER ACCUMULATOR. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 68,932 hrs · 29,887 cycles

MID CARGO DOOR STOP PAD FITTING FROM STATIONS 1520 TO 1522 CRACKED. REPLACED STOP PAD FITTING IAW AARD 51-00-05-1.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 68,932 hrs · 29,887 cycles

MID CARGO DOOR STOP PAD FITTING FROM STATIONS 1220 TO 1222 CRACKED. REPLACED STOP PAD FITTING IAW AARD 51-00-05-1.

Part: FORMER — CRACKED (LE SLAT) · airframe 68,832 hrs · 29,822 cycles

RIGHT WING LE NR 4 SLAT TRACK INBD FORMER IS CRACKED. INSTALLED RT WING NR 4 INBD FORMER DOUBLER IAW WORK CARD 57-98-06 & EA MD80-57-035343.

Part: RESERVOIR — LEAKING (HYDRAULIC SYS) · airframe 68,764 hrs · 29,787 cycles

CREW REPORTED RT HYD PRESS LOW ANNUNCIATOR ILLUMINATED WHEN RT ENG HYD PUMP SWITCH WAS SELECTED TO HIGH FROM LOW DURING DESCENT. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT HYD RESERVOIR. RT ENG HYD PUMP SCHEDULED TO BE REPLACED MECHANICS STILL WORKING ON ACFT.

Part: VALVE — LOOSE (NLG STRUT) · airframe 68,634 hrs · 29,720 cycles

MEX CREW REPORTED NLG FAILED TO RETRACT AFTER TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED MEX & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LOOSE NLG STRUT AIR SERVICE VLV & DAMAGED O RING. SYS GND CHECKED NORMAL, OPERATION CLOSED.

Part: TRANSMITTER — FAULTY (BRAKE SYSTEM) · airframe 63,841 hrs · 27,236 cycles

DFW - CREW REPORTED RIGHT BRAKE PRESSURE GAUGE WENT TO RED BAND. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT BRAKE PRESSURE TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: GEARBOX — LEAKING (LT ENGINE) · airframe 62,841 hrs · 26,736 cycles

MCI - CREW REPORTED LEFT ENGINE LOW OIL PRESSURE MESSAGE AND PRESSURE INDICATION FLUXUATING IN THE RED, NOTED OIL QUANTITY AT ZERO. CAPTAIN PERFORMED IN-FLIGHT SHUTDOWN OF LEFT ENGINE (SINGLE ENGINE TIME 20 MINS). EMERGENCY DECLARED, FLIGHT LANDED MCI WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT MCI ON 05/19/2012 DUE TO LEAKING GEARBOX. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: RELAY — FAILED (LANDING GEAR) · airframe 61,908 hrs · 26,253 cycles

DFW - CREW REPORTED WITH GEAR DOWN FOR LANDING AND WHEN SELECTING LANDING FLAPS AURAL "LANDING GEAR" WARNING HORN CAME ON AND WOULD NOT SILENCE EVEN THOUGH GEAR HAD NORMAL DOWN AND LOCKED INDICATION. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AURAL WARNING CONTINUED DURING LANDING AND TAXI. AIRCRAFT REMOVED FROM SERVICE. REPLACED RELAY R2-295. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: DOOR FRAME — GOUGED (FUSELAGE) · airframe 60,727 hrs · 25,690 cycles

FWD ENTRY DOOR: DOOR JAMB HAS DAMAGE ON AFT FACE OF DOOR JAMB INTERNAL STATION 199 WATERLINE 72. DOUBLER INSTALLED AFT FACE OF DOOR JAMB STATION 199 WATERLINE 72 PER EA MD80-53-018868.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,727 hrs · 25,690 cycles

LEFT CUSP SHEET AT STATION 1174 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,727 hrs · 25,690 cycles

STATION 1212 TO 1218 LONGERON 28 RIGHT, CORROSION ON WEB. SPLICED IN A NEW SECTION PER SRM 51-30-02, 51-30-05 AND AARD 53-10-00-24.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,727 hrs · 25,690 cycles

CORROSION ON VERTICAL LEG OF DOOR BEAM AT STATION 680. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-10-00-3.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,727 hrs · 25,690 cycles

CARGO STATIONS 1271 TO 1287 INTERCOSTAL CRACKED BETWEEN CABIN FLOORBEAMS BUTTLINE 0. REPLACED INTERCOSTAL AT STATIONS 1271 TO 1287 BETWEEN CABIN FLOORBEAMS PER AARD 51-10-00-5.

Part: SKIN — DAMAGED (ENTRY DOOR) · airframe 60,727 hrs · 25,690 cycles

FORWARD ENTRY DOOR AFT UPPER OUTER SKIN AT NUMBER 1 BEAM HAS DEEP TOOLING MARKS FROM PREVIOUS REPAIR. RE-WORKED DENTED AREA. DYE CHECKED AND FOUND NO CRACK INDICATIONS. FABRICATED AND INSTALLED INTERNAL REPAIR DOUBLER FROM .025" 7075-T6 MATERIAL PER BOEING DOCUMENT: SG09530001.

Part: BRACE — CRACKED (FUSELAGE) · airframe 60,727 hrs · 25,690 cycles

TORQUE BRACE CRACKED AFT OF STAIR RETRACT ACTUATOR AT STATION 1485 LONGERON 23 RIGHT. INSTALLED BRACE ANGLE PER AARD 51-10-00.

Part: MEMBRANE — DENTED (FUSELAGE) · airframe 60,727 hrs · 25,690 cycles

STRUCTURE DENTED IN TWO PLACES DIRECTLY UNDER FLOORBOARD CP-3 ON LEFT SIDE AT STATION 133. INSTALLED DOUBLER PER AARD 53-20-00-16 PAGE 2.

Part: CUSP WEB — DAMAGED (FUSELAGE) · airframe 60,727 hrs · 25,690 cycles

HOLE IN LEFT CUSP AT APPROXIMATELY STATION 1177. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,727 hrs · 25,690 cycles

SKIN DAMAGED AFT OF FRAME 237 BETWEEN LONGERONS 17 AND 18 LEFT. INSTALLED DOUBLER PER SRM 53-04-00 FIGURE 12B SHEET 34.

Part: SKIN — CANNING (FUSELAGE) · airframe 60,727 hrs · 25,690 cycles

FUSELAGE SKIN AT LEFT ALTERNATE STATIC PORT OIL CANNED BEYOND LIMITS. INSTALLED NEW SECTION OF SKIN PER SRM 53-04-00 FIGURE 12C SHEETS 5 AND 11 AND SRM 53-04-00 FIGURE 12E.

Part: WEB — CORRODED (FUSELAGE) · airframe 60,727 hrs · 25,690 cycles

CABIN HAS CORROSION IN SUB FLOOR WEBBING BETWEEN STATIONS 160 TO 200 AND BETWEEN 6 INCHES LEFT AND RIGHT OF CENTER LINE. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,727 hrs · 25,690 cycles

CORROSION ON SUB-FLOOR UNDER G-1 GALLEY DRAIN PAN. INSTALLED DOUBLER ON SUB-FLOOR UNDER G-1 GALLEY DRAIN PAN PER AARD 53-20-00-16.

Part: PAN — CRACKED (WINDOW) · airframe 60,727 hrs · 25,690 cycles

WINDOW PAN CRACKED AT AFT UPPER EAR AT STATION 1041 LEFT. INSTALLED DOUBLER PER AARD 53-10-00-25.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,727 hrs · 25,690 cycles

CORROSION AROUND FORWARD GIRT BAR ATTACH HOLES OF AFT SERVICE DOOR THRESHOLD. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: BLEED VALVE — INOPERATIVE (ENGINE) · airframe 53,956 hrs

STL NUMEROUS COMPRESSOR STALLS WHEN ADVANCING POWER. AIRCRAFT REMOVED FROM SERVICE. REPLACED RATIO BLEED CONTROL AND VALVE. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: FRAME — CRACKED (BS 1510) · airframe 52,146 hrs · 21,768 cycles

LT CANTED FRAME AT TAIL CONE STATION 1510 CRACKED. LENGTH OF CRACK IS 3/4 INCH. INSTALLED DOUBLER IN ACCORDANCE WITH ESO 80559 DATED 22 SEP 2008.

Part: FITTING — CRACKED (SPOILER) · airframe 52,146 hrs · 21,768 cycles

GROUND SPOILER FITTING ASSEMBLY AT FORWARD INBD CORNER WING STATION 91 CRACKED. LENGTH OF CRACK IS 1.5 INCH. REPLACED CASTING.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT AFT STAIRWELL FORWARD INOPERATIVE. REPINNED CONNECTOR FOR EMERGENCY LIGHT AT AFT STAIRWELL FORWARD. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ORD - TWO EMERGENCY LIGHTS IN AFT CABIN AT LOWER SLIDE INOPERATIVE. REPLACED BATTERY PACK B527 FOR EMERGENCY LIGHTS IN AFT CABIN AT LOWER SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ORD - FIRST CLASS CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK OVER SEAT ROW DEF IN FIRST CLASS FOR CEILING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TURBINE — FAILED (RT ENGINE)

DFW - INFLIGHT T1573 RIGHT HAND ENGINE HAD A CONTAINED TURBINE FAILURE AT 5600 FEET. AIRCRAFT LANDED OVERWEIGHT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING INOPERATIVE AT SEAT ROWS 8 THROUGH 10. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BLADE — BIRD INGESTION (ENGINE)

EN ROUTE BJX-DFW, ON TAKEOFF, AIRCRAFT EN COUNTERED MULTIPLE BIRD STRIKES. RIGHT ENGINE BEGAN SURGING. RETURNED TO BJX WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED DAMAGED 1ST STAGE FAN BLADES, FRONT AND REAR OUTER FAN CASES PER MX CHECK MANUAL CARDS 72-91-11 AND 72-94-12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — CORRODED (FUSELAGE)

TUL - FOUND PIT IN FUSELAGE SKIN AFT OF FORWARD DOOR STATION 427 LONGERON 25R. CUT OUT DAMAGE (OUTER SKIN) INSTALLED FILLER AND DOUBLER PER SRM 53-05 FIG 82. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

TUL - FOUND FORWARD LEFT EMERGENCY EXIT DOOR JAMB UPPER WEB CRACKED AT STATION 872, 876. INSTALLED DOUBLER ON FORWARD LEFT EMERGENCY EXIT DOOR JAMB UPPER WEB PER SRM 53-05 FIG 32. (M)

Part: DOOR FRAME — CRACKED (FUSELAGE)

TUL - FOUND FORWARD RIGHT EMERGENCY EXIT DOOR JAMB UPPER WEB CRACKED AT STATION 872, 876 (TWO PLACES). INSTALLED DOUBLER ON FORWARD RIGHT EMERGENCY EXIT DOOR JAMB UPPER, PER SRM 53-05 FIG 32. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND AFT LEFT EMERGENCY EXIT DOOR JAMB UPPER WEB CRACKED STATION 1004. INSTALLED DOUBLER ON LEFT EMERGENCY EXIT DOOR JAMB UPPER WEB PER SRM 53-05 FIG 32. (M)

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT)

TUL - FOUND RIGHT AFT OVERWING EXIT JAMB IS CRACKED UPPER SIDE AFT OF CENTER. INSTALLED DOUBLER PER SRM 53-05-00 FIG 32. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND SMALL AREA OF CORROSION LEFT CUSP STATION 545 EXTENDING FROM BELOW BRACKET. INSTALLED DOUBLER AT STATION 545 LEFT SIDE CUSP PER AARD 53-00-00-02. (M)

Part: GALLEY TRACK — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON FORWARD GALLEY TIE DOWN FITTING. REPLACED WITH NEW TIE DOWN FITTING PER SRM 51-01. (M)

Part: SCREW — LOOSE (BOOST PUMP)

EN ROUTE LGB-DFW, AT 24,000 FEET SMALL FUEL LEAK NOTICED. NO DISCREPANCY IN FUEL BURN OR IMBALANCE. CLIMBED TO 33,000 FEET AND LEAK INCREASED TO A STEADY STREAM. DECLARED EMERGENCY, DIVERTED TO ELP AND LANDED WITHOUT INCIDENT. RETORQUED BOOST FUEL PANEL SCREWS TO BOOST PUMP. PANEL UNDER HEATER BLANKET. LEAK CHECK OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (CABIN)

RDU - DURING OVERNIGHT CHECK, EMERGENCY LIGHT AT AFT VENTRAL STAIR BROKEN. REPLACED EMERGENCY LIGHT AT AFT VENTRAL STAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL STRIP — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 16D TO 20D FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PASSENGER SEAT ROWS 16D AND 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)