N328AA

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,638 hrs · 19,871 cycles

ESCAPE PATH LIGHT AT SEAT 19H INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR ESCAPE PATH LIGHT AT SEAT 19H. OPERATIONS CHECKED NORMAL.

Part: PIN — DEFECTIVE (EMERGENCY LIGHT) · airframe 100,638 hrs · 19,871 cycles

ESCAPE PATH LIGHT AT SEAT 27H INOPERATIVE. REPLACED PIN FOR ESCAPE PATH LIGHT AT SEAT 27H. OPERATIONS CHECKED NORMAL.

Part: SOCKET — INOPERATIVE (CABIN) · airframe 100,638 hrs · 19,871 cycles

ESCAPE PATH LIGHT AT SEAT 26H INOPERATIVE. REPLACED SOCKET FOR ESCAPE PATH LIGHT AT SEAT 26H. OPERATIONS CHECKED NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 98,214 hrs · 19,385 cycles

DENT IN FUSELAGE SKIN AT CENTER WING CAVITY VENT. INSTALLED DOUBLER REPAIR PER SRM 53-00-01-2R14 AND EA B767-53-0274498.

Part: SLAT — DAMAGED (RT WING) · airframe 98,214 hrs · 19,385 cycles

FOUR EACH LIGHTNING STRIKES, 52 INCHES FROM INBOARD END OF NUMBER 10 SLAT. INSTALLED FLUSH DOUBLER REPAIR PER SRM 57-43-01-2R-2 AND EA COMP-57-027345.

Part: SLAT — DAMAGED (RT WING) · airframe 98,214 hrs · 19,385 cycles

NUMBER 10 RIGHT SLAT HAS LIGHTNING STRIKES 52 INCHES FROM INBOARD END. INSTALLED FLUSH DOUBLER REPAIR PER SRM 57-43-01-2R-2 AND EA COMP-57-027345.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 98,024 hrs · 19,347 cycles

EMERGENCY EXIT LIGHT UNARMED LIGHT CAP HAS ONE BULB INOPERATIVE. REPLACED BULB FOR EMERGENCY EXIT UNARMED LIGHT CAP. SYSTEM CHECKED NORMAL OPERATION.

Part: SENSOR — DIRTY (CARGO DOOR) · airframe 95,271 hrs · 18,788 cycles

DURING CRUISE, CREW REPORTED FORWARD CARGO DOOR UPPER EICAS MESSAGE. FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT. CLEANED SENSOR AND TARGET. SYSTEM GROUND CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 94,129 hrs · 18,556 cycles

NUMEROUS FIRST CLASS EMERGENCY LIGHTS AND FORWARD RIGHT AND LEFT NUMBER 1 DOORS INOPERATIVE. REPLACED BATTERY PACK LEFT SIDE FIRST CLASS EMERGENCY LIGHTS. OPS CHECK NORMAL.

Part: SPAR — CRACKED (LT PYLON) · airframe 93,106 hrs · 18,349 cycles

CRACK WAS FOUND ON THE LEFT PYLON FORWARD UPPER SPAR WEB COMMON TO THE INTEGRATED DRIVE GENERATOR POWER FEEDER CABLE PASS THROUGH. REPAIRED UPPER SPAR WEB PER EA B767-54-017641.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,106 hrs · 18,349 cycles

CORROSION DAMAGE ON FUSELAGE STRINGER 39 LEFT AT APPROXIMATELY STATION 1307. INSTALLED SPLICE REPAIR PER EA B767-53-017629.

Part: COVER — MISSING (CABIN) · airframe 92,543 hrs · 18,236 cycles

BUSINESS CLASS GALLEY FLOOR PATH EMERGENCY LIGHT MISSING COVER. REPLACED MISSING EMERGENCY LIGHT COVER. OPS CHECK NORMAL.

Part: LENS — MISSING (CABIN) · airframe 91,316 hrs · 17,988 cycles

MID GALLEY EMERGENCY LIGHT MISSING LENS. REPLACED LENS. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,316 hrs · 17,988 cycles

MID GALLEY EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPS CHECK NORMAL.

Part: SENSOR — OUT OF ADJUST (CARGO DOOR) · airframe 89,784 hrs · 17,675 cycles

JFK - CAPTAIN REPORTED FORWARD CARGO DOOR INDICATION SHOWING DOOR NOT CLOSED AFTER TAKEOFF. EMERGENCY DECLARED RETURNED JFK LANDED WITHOUT INCIDENT. ADJUSTED FORWARD CARGO DOOR DOWN SENSOR. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: LENS — MISSING (CABIN) · airframe 87,818 hrs · 17,273 cycles

EMERGENCY LIGHT AT SEAT 27B HAS MISSING LENS. REPLACED LENS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,818 hrs · 17,273 cycles

EMERGENCY LIGHT AT SEAT 27B INOPERATIVE. REPLACED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,818 hrs · 17,273 cycles

EMERGENCY LIGHT AT SEAT 26H INOPERATIVE. REPLACED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,829 hrs · 17,276 cycles

EMERGENCY LIGHT EXIT OVERWING CROSS AISLE FLOOD LIGHT AT L9027 INOPERATIVE. REPLACED MODULE AND BATTERY ASSY, M9029 NO HELP.

Part: SEAL — LEAKING (HYDRAULIC SYS) · airframe 87,742 hrs · 17,258 cycles

CREW REPORTED HYDRAULIC SYSTEM DROPPED TO .11 AND RIGHT ENGINE LOW PRESSURE LIGHT ILLUMINATED. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND RIGHT PUMP OUTPUT LINE AT PYLON SEAL LEAKING. REPLACED DAMAGED SEAL.

Part: SKIN — CORRODED (FUSELAGE) · airframe 82,984 hrs · 16,306 cycles

AFW FUSELAGE SKIN AT SECTION 48 HAS LIGHT CORROSION BETWEEN STRINGER 30 AND 32 LT AND BETWEEN STATION 1809 AND 1832. AREA OF DISCREPANCY IS 4.8 INCHES BY 20 INCHES. REPAIRED PER MRB 767 3283.

Part: FITTING — DAMAGED (VERTICAL STAB) · airframe 82,984 hrs · 16,306 cycles

AFW VERTICAL STABILIZER RIB FITTING AT RUDDER STATION 380.769 WAS DAMAGED FROM STATIC DISCHARGE. REPAIRED PER MRB 767 3269.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 82,984 hrs · 16,306 cycles

AFW RT OUTER CHORD AT STATION 1809 HAD HOLES REAMED TO 0.285 INCH AND 0.280 INCH. REPAIRED PER MRB 767 3264.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,984 hrs · 16,306 cycles

AFW FLOOR BEAM AT STATION 325 HAD CORROSION REMOVAL ON UPPER SURFACE OF HORIZONTAL FLANGES. AREA OF DISCREPANCY IS 2.0 INCH BY 1.5 INCH WITH A DEPTH OF 0.027 INCH AND 0.028 INCH. REPAIRED PER MRB 767 3254.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 82,984 hrs · 16,306 cycles

AFW STRINGER 37 RT WAS CORRODED FROM STATION 424 TO STATION 445. REPAIRED IN ACCORDANCE WITH SRM 53-00-03-1R2 AND MRB 757 3259.

Part: SWITCH — INOPERATIVE (FUEL FILTER) · airframe 82,639 hrs

JFK INFLIGHT T117/23MAY. CREW REPORTED BOTH ENGINE FUEL FILTER CLOG INDICATIONS. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED LT AND RT ENGINE FUEL FILTERS. REPLACED LT AND RT ENGINE FUEL FILTER DIFFERENTIAL PRESSURE SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHT AT SEAT 30H MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS)

JFK - EMERGENCY LIGHT AT SEAT 30H MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: ACM — SEIZED (A/C BAY)

JFK INFLIGHT T40/12APR FLIGHT ATTENDANT REPORTED LOUD NOISE UNDER BUSINESS CLASS GALLEY FOLLOWED BY VIBRATION AND SMOKE IN CABIN. LANDED JFK WITHOUT INCIDENT. FOUND LEFT HAND AIR CYCLE MACHINE SEIZED. REPLACED LEFT HAND AIR CYCLE MACHINE. ALSO REPLACED A PRECAUTION LEFT HAND LOW LIMIT VALVE AND LEFT HAND TEMPERATURE CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)

Part: SKIN — CORRODED (BS 1582)

AFW - FUSELAGE SKIN AT STATION 1582 AT BUTT SPLICE BETWEEN SECTION 46 AND 48 HAD CORROSION. CUT OUT CORROSION AT STATION 1582 AT BUTT SPLICE BETWEEN SECTION 46 AND 48 AND INSTALLED REPAIR DOUBLER PER DRAWING 146T3340.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)

LAX - SEAT MOUNTED AND AFT LEFT LAVATORY BULKHEAD MOUNTED EMERGENCY LIGHTS FROM 31AB THROUGH 38AB INOPERATIVE. REPLACED MODULE M9034 AND BATTERY PACK FOR INOPERATIVE SEAT MOUNTED AND AFT LEFT LAVATORY BULKHEAD MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — DAMAGED (PYLON)

AFW - LEFT AND RIGHT HAND PYLON SKINS AT STATION 250 HAD GROOVE WORN FROM THRUST REVERSER SEAL RETAINER. GROOVE WAS BLENDED AND HIGH FREQUENCY EDDY CURRENT INSPECTION PERFORMED. NO CRACKS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY PATH LIGHTING ZONE 3 AT ROWS 20 TO 30 INOPERATIVE. REPLACED BATTERY PACK AT ZONE 3 FOR EMERGENCY PATH LIGHTING AT ROWS 20 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

LAX - MID GALLEY EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRING UNDER MID GALLEY CABIN FLOOR FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: COMPUTER — INOPERATIVE (AUTOPILOT)

LAX - INFLIGHT T032 RETURNED TO LAX DUE TO AILERON LOCKOUT, RUDDER RATIO EICAS MESSAGE AND ALL THREE AUTOPILOTS INOPERATIVE. LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION AND REPLACED LEFT AND RIGHT HAND AIR DATA COMPUTERS (4040800912 FROM HONEYWELL), LEFT AND RIGHT HAND STABILIZER TRIM, AILERON MODULE (285T0015117MODD FROM BOEING) AND AUTOPILOT MODE CONTROL PANEL (8221492102 FROM ROCKWELL COLLINS). SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

SFO - EMERGENCY LIGHT AT SEAT 28AB INOPERATIVE. REPAIRED BROKEN WIRE AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 28AB. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — FAULTY (CABIN)

SFO EMERGENCY LIGHT AT SEAT 33B INOPERATIVE. REPLACED EMERGENCY LIGHT CONNECTOR AT SEAT 33A/B. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--

Part: SKIN — DAMAGED (FUSELAGE)

MCI FUSELAGE SKIN HAD A TEMPORARY REPAIR WITH BLIND FASTENERS PER AARD 53-00-50-3. ORIGINAL REPAIR IS 18 INCHES AFT OF EXISTING REPAIR. DAMAGE IS LOCATED RIGHT SIDE OF FUSELAGE AFT OF C-1 DOOR ON THE PART NUMBER 143T3520 SKIN AFT OF STATION 654 BETWEEN 29R AND 30R. AREA IS 3.0 X 3.0 INCH. REMOVED PREVIOUS REPAIR INSTALLED WITH BLIND FASTERNERS. CLEANED UP PREVIOUS TRIMOUT AND INSTALLED PERMANENT REPAIR PER SRM 53-00-01-2, FIGURE 214 FOR PERMANENT REPAIR AND MRB 767-2544 FOR MINIMUM LENGTH REQUIREMENT BETWEEN REPAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — FAULTY (CABIN)

AAX - MAINTENANCE OBSERVED EMERGENCY LIGHT AT SEAT 25H INOPERATIVE. REPLACED CONNECTOR PLUG AT SEAT 25H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LINE — LEAKING (NR 2 ENGINE)

GIG - FLT 972 - EN ROUTE GIG-JFK, APPROXIMATELY 30 MINUTES AFTER TAKEOFF LOST ALL RIGHT SIDE HYDRAULIC SYSTEM FLUID. DECLARED EMERGENCY, RETURNED GIG AND LANDED WITHOUT FURTHER INCIDENT. REPLACED HYDRAULIC DRIVEN PUMP PRESSURE LINE. FLUSHED RIGHT ENGINE. RAN BOTH ENGINES PER THE MM. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTROLLER — FAILED (COCKPIT)

YYT - FLT 38 - AT FL360, CREW OBSERVED ARCHING ON RIGHT FORWARD WINDSHIELD. WINDSHIELD BEGAN BUBBLING THEN CRACKING. INNER PAIN REMAINED INTACT. DIVERTED AND LANDED YYT WITHOUT INCIDENT. REPLACED RIGHT SIDE FORWARD WINDSHIELD. REPLACED WINDOW HEAT CONTROLLER. PERFORMED WINDOW HEATING SYSTEM CHECK PER THE MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PANEL — DEFECTIVE (COCKPIT)

LHR - FLT 66 - EN ROUTE LHR - APPROXIMATELY 20 MINUTES PRIOR TO LANDING A BURNING ELECTRICAL SMELL WAS NOTICED IN COCKPIT. LANDED WITHOUT INCIDENT. REPLACED AUTO FLIGHT MODE CONTROL SELECT PANEL AND CAPTAINS DME/VOR PANEL. ACCOMPLISHED MCDP TEST 40. INSPECTED WINDOW HEAT CONNECTIONS AND COOLING DUCTS. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M)

Part: WIRE — BROKEN (ROW 20-30)

ORD - DURING MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT ROWS 20H THROUGH 30H WOULD NOT ILLUMINATE. REPAIRED EMERGENCY EXIT LIGHT CHAFED WIRE AT SEAT ROW 28H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED AFT LEFT ENTRY DOOR EMERGENCY EXIT LIGHT CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT ROW 32H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT ROW 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 933)

AFW - WHILE IN FOR MBV MAINTENANCE FOUND TWO AREA OF CORROSION ON THE UPPER SURFACE OF THE UPPER FLANGE OF THE FLOORBEAM AT STATION 933 LBL 11. AFTER BLENDING, THE AREAS WERE DYE CHECKED SHOT/ROTO PEENED PER SRM 51-20-06. REFINISHED PER SRM AND FILLED WITH BMS5-95 SEALANT. (M)

Part: SIGN — MISSING (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT SIGN AT LT AISLE FORWARD END OF MAIN CABIN MISSING. REPLACED EMERGENCY EXIT SIGN AT LT AISLE FORWARD END OF MAIN CABIN. (X)

Part: LIGHT — DEFECTIVE (COCKPIT)

SFO - DURING OVERNIGHT CHECK, COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED COCKPIT EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 325)

AFW - FOUND AND BLENDED OUT CORROSION ON THE 141T5113-9 FLOORBEAM. BLEND OUT EXCEEDED SRM LIMITS. REFINISHED BLENDOUT PER SRM. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1405. (M)

Part: FLOORBEAM — CORRODED (BS 1180)

AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF FLOORBEAM 146T5141-1. THE BLEND OUT EXCEEDS SRM LIMITS. REFINISHED BLENDOUT PER SRM 51-20-01. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1407. (M)

Part: FLOORBEAM — CORRODED (BS 851-937)

AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACES OF THE FLOORBEAMS AT LBL 33 AND RBL 33. TWELVE BLENDOUTS ON LBL 33 AND EIGHT ON RBL 33. THE BLEND OUTS EXCEED SRM LIMITS. APPROVED AND REFINISHED BLENDED AREAS. SHIMMED TO PREVENT PULLUP OF THE CHORD FLANGE WHEN THE FLOOR PANEL WERE REINSTALLED. APPROVED BY ENGINEERING PER MRB767-1409. (M)

Part: BEAM — CORRODED (CARGO DOOR)

AFW - FOUND AND BLENDED OUT CORROSION ON THE INNER SURFACE OF THE 140T2603-3 INNER CHORD ON THE FWD CARGO DOOR. THE BLENDOUTS EXCEEDED SRM LIMITS. FOR FOUR BLEND OUTS TRIMMED OUT DISCREPANT AREAS. FABRICATED AND INSTALLED REPAIR STRAPS USING 7075-T6 ALUMINUM. TWO BLENDOUTS CONTINUED IN SERVICE WITH NOTED CONDITION. APPROVED BY ENGINEERING PER MRB 767-1411. (M)

Part: SUPPORT — CORRODED (BS 1480)

AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE FLOOR SUPPORT TEE. THE BLEND OUT EXCEEDS SRM LIMITS. REFINISHED BLENDED AREA AND INSTALLED FILLER AS REQUIRED. APPROVED BY ENGINEERING PER MRB 767-1406. (M)

Part: BEAM — CORRODED (CARGO DOOR)

AFW - FOUND AND BLENDED OUT CORROSION ON THE INNER SURFACE OF THE 140T2603-3 CHORD ON THE AFT CARGO DOOR. SIX REWORKED AREAS EXCEED SRM LIMITS. AT THREE LOCATION FABRICATED AND INSTALLED REPAIR STRAP USING 7075-T6. THE THREE REMAINING AREA WERE REFINISHED AND CONTINUED IN SERVICE WITH NOTED CONDITION. APPROVED BY ENGINEERING PER MR8767-1410. (M)

Part: SKIN — CORRODED (BS 751.5)

AFW - FOUND AND BLENDED OUT DAMAGE ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN. THE BLEND OUT EXCEEDS SRM LIMITS. (M)

Part: SKIN — CORRODED (BS 954)

AFW - WING BOX UPPER SKIN CORRODED ON UPPER SURFACE. AFTER BLENDING FOUND DAMAGE BEYOND SRM LIMITS. SHOT PEENED AND REFINISHED BLENDED AREAS. INSTALLED REPAIR CHORD ON LEFT SIDE. CONTINUED RIGHT SIDE IN SERVICE WITH NOTED CONDTION. APPROVED BY ENGINEERING PER MRB767-1413. (M)

Part: CONNECTOR — BROKEN (CAIBN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 37H INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 23B INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: OVEN — DIRTY (GALLEY)

LHR - FLT 106 - EN ROUTE JFK/LHR DURING CRUISE, FIRST CLASS GALLEY NR 2 OVEN HAD DIRTY INTERIOR CAUSING SMOKE WHEN OVEN DOOR WAS OPENED. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO LHR AND LANDED WITHOUT INCIDENT. CLEANED INTERIOR OF FIRST CLASS GALLEY NR 2 OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO SMOKE NOTED. (M)

Part: FLOOR BEAM — CORRODED (BS 347)

TUL - FLOOR BEAM CORRODED. AFTER BLENDING FOUND BEYOND SRM LIMITS. ALODINED AND FILLED BLENDED AREA. FABRICATED AND INSTALLED REPAIR STRAP USING .063 INCH 7075-T6 ALUMINUM. PRIMED FLOOR BEAM AND STRAP. APPROVED BY ENGINEERING PER MRB 767-1155. TST: 38,277.19 HRS. CYCLES, 7,672. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 37H FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT HARNESS CONNECTOR AT PASSENGER SEAT 37H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT 26HJ INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)