N368AA

Part: CHARGER — FAULTY (CABIN) · airframe 101,329 hrs · 16,188 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. THREE EXTERIOR EMERGENCY LIGHT BETWEEN THE RIGHT OVERWING EXIT AND THE R3 DOOR ARE INOPERATIVE. REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY ASSEMBLY AT M733 IAW AMM 33-51-07-002-006 AND 33-51-07-402-010. ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-51-07-402-010. SEE ALSO AALA20161116009.

Part: BATTERY — DISCHARGED (CABIN) · airframe 101,329 hrs · 16,188 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. THREE EXTERIOR EMERGENCY LIGHT BETWEEN THE RIGHT OVERWING EXIT AND THE R3 DOOR ARE INOPERATIVE. REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY ASSEMBLY AT M733 IAW AMM 33-51-07-002-006 AND 33-51-07-402-010. ACCOMPLISHED OPERATIONAL CHECK IAW AMM 33-51-07-402-010. SEE ALSO AALA20161116010.

Part: SKIN — CORRODED (BS 1207) · airframe 101,327 hrs · 16,186 cycles

EVIDENCE OF CORROSION FOUND AT BS 1207, S37R. FASTENERS PULL THROUGH AND CRACKING IN SKIN. REPAIRED FUSELAGE SKIN AND STRINGER IAW EA 263966.

Part: STRINGER — CORRODED (BS 1207) · airframe 101,328 hrs · 16,187 cycles

EVIDENCE OF CORROSION FOUNDAT BS 1207, STRINGER 37R. FASTENERS PULL THROUGH AND CRACKING IN SKIN. REPAIRED THE SKIN AND STRINGER IAW EA 263966.

Part: SHIM — CORRODED (BS 1219) · corrosion level 2 · airframe 101,327 hrs · 16,186 cycles

SKIN FOUND BULGING AT BS 1219, S38R. REMOVED AND REPLACED CORRODED SHIM IAW SRM 51-20-11-0G AND SRM 51-40-02-0G.

Part: SHIM — CORRODED (FUSELAGE) · airframe 101,327 hrs · 16,186 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. EVIDENCE OF CORROSION AT FUSELAGE STATION 1307 BUTT JOINT AND S38L. REMOVED FASTENERS AND STRINGER SPLICE AND FOUND FILLER SHIM CORRODED. REMOVED AND REPLACED FILLER SHIM AND REINSTALLED FASTENERS AND STRINGER SPLICE IAW SRM 51-40-02 AND EA 263977.

Part: CAP — MISSING (ZONE 200) · airframe 100,431 hrs · 16,004 cycles

AIRCRAFT WAS GROUNDED. AIR INTERRUPT. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT OVERWEIGHT. DURING TAKEOFF, THE F/O TRACK INDICATOR SWITCHED BACK AND FORTH FROM TRUE TO MAGNETIC. MAINTENANCE FOUND WIRE W011-0813-22 MISSING END CAP AND EXPOSED. INSTALLED NEW END CAP IAW SWPM 20-30-16. ACCOMPLISHED OPS TEST OF RT IRU IAW AMM 34-21-00 AND RT AND CENTER DCU IAW AMM 34-22-11. PERFORMED AUTOLAND TEST 30 AND TEST 40 IAW AMM 22-00-02. SYSTEM CHECK NORMAL.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 100,133 hrs · 15,951 cycles

AIRCRAFT WAS GNDED. STRINGER 35R IS CORRODED AT FS 784. REPAIRED STRINGER IAW SRM 53-00-03-2R & EA 260560.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 97,807 hrs · 15,427 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 35 - 41 ABC ARE INOPERATIVE. R & R EMERGENCY LIGHTS POWER SUPPLY M739. PERFORMED OPERATIONAL CHECK IAW 33-51-07. SYSTEM CHECKED NORMAL.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 97,517 hrs · 15,378 cycles

AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB WEATHER RADAR FAILED. RESET WEATHER RADAR TRANSCEIVER & PERFORMED OPERATIONAL TEST IAW AMM 34-43-00-715-001-001. SYS CHECKED NORMAL.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 96,303 hrs · 15,165 cycles

CORROSION ON HORIZONTAL STABILIZER CTR BOX SECTION AT APPROX FS 1783 & RBL 18. REMOVED CORROSION BY BLENDING & INSTALLED DOUBLER REPAIR IAW EA 55-038673 DATED 02-19-2015.

Part: FITTING — CRACKED (TE FLAP) · airframe 96,303 hrs · 15,165 cycles

RIGHT WING INBD MAIN FLAP MID FITTING CRACKED AT AFT SPAR OF FLAP IN LOWER AFT RADIUS. REPAIRED FITTING IAW SRM 57-53-02-2R REPAIR 1 & EA 57-038762.

Part: FITTING — DAMAGED (HORIZ STAB) · airframe 96,303 hrs · 15,165 cycles

HORIZONTAL STABILIZER PIVOT FITTING HAS TOOLING DAMAGE. REPAIRED FITTING IAW EA B767-53-03867.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 96,303 hrs · 15,165 cycles

INNER CHORD OTBD CANT ANGLE AT FS 903.5, LBL 89 & WL 200 IS OVAL. REPAIRED HOLE IAW EA 53-038627.

Part: STRAP — BROKEN (FUSELAGE) · airframe 96,303 hrs · 15,165 cycles

FUSELAGE STABILIZATION STRAP AT FS 460 & LBL 39.25 IS CRACKED ACROSS ENTIRE WIDTH, SEVERED. REPAIRED STRAP IAW EA 53-038541 DATED 02/10/2015.

Part: SKIN — DENTED (CARGO DOOR) · airframe 96,303 hrs · 15,165 cycles

BULK CARGO DOOR SKIN HAS A DENT WITH SHARP CREASE ON LOWER FWD CORNER. INSTALLED DOUBLER & FILLER REPAIR IAW SRM 52-30-01-2R-6.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,303 hrs · 15,165 cycles

CORROSION ON STRINGER 35 LT AT FS 1301. R & R SECTION OF STRINGER IAW EA 53-038477 DATED 02/05/15.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 96,303 hrs · 15,165 cycles

INTERCOSTAL WEB STIFFENER BETWEEN FS 574 & 584 AT RBL 40 IS CRACKED. R & R STIFFENER IAW AARD 53-30-00-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,303 hrs · 15,165 cycles

UPPER CHORD OF AFT CARGO COMPARTMENT FLOORBEAM AT FS 1175 IS CORRODED BETWEEN LBL 21 & RBL 22. R & R FLOORBEAM CHORD IAW AARD 51-00-05.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 96,303 hrs · 15,165 cycles

GALLEY MOUNT AT FS 287 & RBL 21 IS CORRODED. R & R FLOOR MOUNT IAW AARD 51-00-05-01.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 96,303 hrs · 15,165 cycles

GALLEY MOUNT AT FS 346 & RBL 46 IS CORRODED. R & R GALLEY MOUNT IAW AARD 51-00-05-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,303 hrs · 15,165 cycles

AFT CARGO UPPER FLOORBEAM CHORD AT FS 1197 IS CORRODED. R & R CHORD IAW AARD 51-00-05.

Part: LENS — MISSING (CABIN) · airframe 94,804 hrs · 14,904 cycles

RIGHT SIDE EMER LIGHT FWD OVERWING EXIT DOOR MISSING LENS. REPLACED LENS FOR RT SIDE EMER LIGHT FWD OVERWING EXIT DOOR. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 93,634 hrs · 14,723 cycles

LEFT SIDE FUSELAGE, EMERGENCY LIGHT AFT OF TE INOPERATIVE. REPLACED LAMP FOR LT SIDE FUSELAGE, EMERGENCY LIGHT AFT OF TE. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,634 hrs · 14,723 cycles

SEAT 34H EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 34H EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 93,634 hrs · 14,723 cycles

RIGHT NR 4 DOOR, EMERGENCY LIGHT LOWER AFT SIGN INOPERATIVE. REPLACED LAMP FOR LOWER AFT SIGN EMERGENCY LIGHT AT RT NR 4 DOOR. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 93,634 hrs · 14,723 cycles

FUSELAGE EMERGENCY LIGHT AT RT FWD OF CARGO DOOR INOPERATIVE. REPLACED LAMP FOR RT FUSELAGE EMERGENCY LIGHT FWD OF CARGO DOOR. OPERATIONS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 93,634 hrs · 14,723 cycles

LEFT NR 1 DOOR EMERGENCY EXIT LIGHT AT FWD LOWER CORNER MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT LIGHT AT LOWER FWD CORNER AT LT NR 1 DOOR. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,634 hrs · 14,723 cycles

RIGHT NR 1 DOOR, EMERGENCY LIGHT AT LOWER FWD CORNER INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LOWER FWD CORNER AT RT NR 1 DOOR. OPERATIONS CHECKED NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 93,141 hrs · 14,648 cycles

24H SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE FOR 24H SEAT MOUNTED EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: CONTROL VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 92,654 hrs · 14,565 cycles

LHR INFLIGHT MXP-JFK CREW REPORTED CABIN PRESS CONTROLLER 2 FAILED IN AUTO WITH CABIN PRESS CONTROLLER 1 AUTO ON MEL. FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT FLOW CONTROL & SHUT-OFF VLV. SYS GND CHECKED NORMAL OPERATION CLOSED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 91,382 hrs · 14,368 cycles

FORWARD GALLEY TO 6JH EMERGENCY LIGHTS DID NOT ILLUMINATE. REPLACED BATTERY PACK M730. OPERATIONS CHECKED NORMAL.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,211 hrs · 14,343 cycles

CORROSION AT STATION 412 & STRINGER 23 RT. REPLACED STRINGER & ACCOMPLISHED INTERNAL & EXTERNAL REPAIRS IAW SRM 53-00-03-2R-2.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 91,211 hrs · 14,343 cycles

CORROSION AT STATION 1207 & STRINGER 39 LT. INSTALLED DOUBLER IAW SRM 53-00-01-2R-1 REPAIR NR 1 & FEA 15696.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 86,972 hrs · 13,674 cycles

RIGHT NUMBER 2 EMERGENCY SIGN EXIT INOPERATIVE. REPLACED POWER SUPPLY ASSEMBLY FOR RIGHT NUMBER 2 EMERGENCY SIGN EXIT. OPS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 86,972 hrs · 13,674 cycles

LEFT NUMBER 2 EMERGENCY EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY ASSEMBLY FOR LEFT NUMBER 2 EMERGENCY EXIT SIGN. OPS CHECKS NORMAL.

Part: HOUSING — BROKEN (CABIN) · airframe 86,842 hrs · 13,656 cycles

EMERGENCY LIGHT AT SEAT 21H BROKEN. REPLACED HOUSING ASSEMBLY FOR SEAT 21H EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,494 hrs · 13,600 cycles

RIGHT NUMBER 1 LOWER PORTION OF EMERGENCY SIGN LIGHTS INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 LOWER PORTION OF EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 86,494 hrs · 13,600 cycles

RIGHT FUSELAGE EMERGENCY LIGHT JUST AFT OF WING FASTENER LOOSE. SECURED EMERGENCY LIGHT.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 86,035 hrs · 13,528 cycles

INTERCOSTAL ANGLE AT CEILING AREA OF FORWARD CARGO BETWEEN STATIONS 742 TO 764 AT RIGHT BUTTLINE 40 HAS 3 CRACKS. REPLACED INTERCOSTAL ANGLE BETWEEN STATIONS 742 TO 764 AT RIGHT BUTTLINE 40 PER AARD 53-30-00-01.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 86,035 hrs · 13,528 cycles

NUMBER 5 LEADING EDGE SLAT AT INBOARD END ON TRAILING EDGE WEDGE HAS DELAMINATION AT INBOARD EDGE. ACCOMPLISHED BODED REPAIR PER SRM 51-70-10.

Part: TORQUE BOX — CRACKED (LT PYLON) · airframe 86,035 hrs · 13,528 cycles

CRACK IN UPPER TORQUE BOX ON LEFT PYLON AT NUT PLATE HOLE. INSTALLED DOUBLER PER AARD 54-52-01-1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,035 hrs · 13,528 cycles

SHEAR TIE AT STATION 742 FROM STRINGER 38 TO 39 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,035 hrs · 13,528 cycles

SHEAR TIE AT STATION 742 FROM STRINGER 37 TO 38 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02.

Part: BUSHING — MIGRATED (RT PYLON) · airframe 84,903 hrs · 13,337 cycles

RIGHT PYLON MIDSPAR OUTBOARD LUG INBOARD BUSHING MIGRATED. REPLACED BUSHING PER EA B767-54-020452

Part: BUSHING — MIGRATED (LT PYLON) · airframe 84,945 hrs · 13,344 cycles

LEFT PYLON INBOARD ATTACHMENT FITTING INBOARD LUG BUSHING MIGRATED. REPLACED BUSHING PER EA B767-54-020452.

Part: BUSHING — MIGRATED (LT PYLON) · airframe 84,945 hrs · 13,344 cycles

LEFT PYLON INBOARD ATTACHMENT FITTING OUTBOARD LUG BUSHING MIGRATED. REPLACED BUSHING PER EA B767-54-020452.

Part: BUSHING — MIGRATED (RT PYLON) · airframe 84,945 hrs · 13,344 cycles

RIGHT PYLON MIDSPAR OUTBOARD LUG OUTBOARD BUSHING MIGRATED. REPLACED BUSHING PER EA B767-54-020452.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 79,947 hrs · 12,555 cycles

FUSELAGE SKIN CORRODED AT STATION 1219 STRINGER 37. INSTALLED DOUBLER AND TRIPLER PER E.A. B767-53-011824.

Part: SKIN — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 79,741 hrs · 12,514 cycles

CORROSION WAS FOUND ON THE FUSELAGE SKIN EMANATING UNDERNEATH A PREVIOUS FUSELAGE SKIN REPAIR BETWEEN STATION 1197 AND 1219 AND STRINGER 36 LEFT AND 37 LEFT. REPAIRED PER MAJOR EA B767-53-011824 DATED 16JUL10 767-300 STA 1219 AT S37L FUSELAGE SKIN REPAIR.

Part: BATTERY PACK — DAMAGED (CABIN) · airframe 77,404 hrs · 12,112 cycles

LEFT NUMBER ONE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED TERMINALS, BATTERY PACK, AND CLEANED SOCKETS.

Part: FSEU — INOPERATIVE (FLAP SYSTEM) · airframe 75,415 hrs · 11,785 cycles

MIA - AIRCRAFT EXPERIENCED FLAP DISAGREE AND LANDING GEAR ANNUNCIATOR WENT BLANK FLIGHT THEN INITIATED GO AROUND. EMERGENCY DECLARED, LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP SLAT ELECTRONICS UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: COMPUTER — MALFUNCTIONED (FLAP SYSTEM) · airframe 75,415 hrs · 11,785 cycles

MIA - AIRCRAFT EXPERIENCED FLAP DISAGREE AND LANDING GEAR ANNUNCIATOR WENT BLANK FLIGHT THEN INITIATED GO AROUND. EMERGENCY DECLARED, LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED GROUND PROXIMITY WARNING COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CLAMP — BROKEN (RT ENGINE) · airframe 75,257 hrs · 11,758 cycles

SJU - INFLIGHT SDQ-JFK. RIGHT DUCT LEAK ILLUMINATED. EMERGENCY DECLARED, LANDED SJU WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BROKEN CLAMP ON RIGHT ENGINE THERMAL ANTI-ICE VALVE DUCTING. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FAILSAFE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,373 hrs · 11,615 cycles

AFW - FAIL SAFE CHORD HAD CORROSION. REPAIRED UNDER MRB 767-3397 AND SRM 53-20-00.

Part: SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 74,373 hrs · 11,615 cycles

AFW - AFT CARGO LOWER SILL INNER CHORD HAD CORROSION. REPAIRED UNDER MRB 767-3398 AND SRM 53-20-00.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,373 hrs · 11,615 cycles

AFW - FORWARD CARGO DOOR LOWER MAIN SILL FAIL SAFE STRAP CORRODED. REPAIRED UNDER MRB 767-3393 AND SRM 53-20-00.

Part: LOGIC CARD — FAULTED (FIRE DETECTION) · airframe 73,367 hrs

REC INFLIGHT - NUMBER ONE ENGINE FIRE DETECTION LOOP ONE FAULTED WITH LEFT ENGINE LOOP TWO PLACARDED. RETURNED TO REC AND LANDED WITHOUT INCIDENT. REPLACED FIRE DETECTION SYSTEM LOGIC CARD AND TIGHTENED LOOSE LEFT ENGINE LOOP ONE LOWER AFT CONNECTOR AND REPLACED FAULTY LT ENGINE LOOP UPPER AFT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

MIA EMERGENCY LIGHT OVERHEAD SEAT 24B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,910 hrs

ORD - EMERGENCY LIGHT AT AFT ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,289 hrs

SFO - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL UNIT — INOPERATIVE (RT ENGINE) · airframe 68,992 hrs

GRU INFLIGHT T942/09NOV - RIGHT ENGINE FUEL SHUTOFF VALVE CIRCUIT BREAKER POPPED AFTER LEVEL OFF. RETURNED TO GRU AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE MAIN FUEL CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 68,897 hrs

ORD - OVERWING EMERGENCY LIGHT AT SEAT 20A HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20A. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

ORD - EMERGENCY LIGHT AT SEAT 23B HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — BROKEN (EMERGENCY LIGHTS)

ORD - EMERGENCY LIGHT AT SEAT 23B HAS BROKEN LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (COCKPIT)

JFK - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

DFW - EMERGENCY LIGHT ON RIGHT SIDE OF CABIN INOPERATIVE. REPLACED BULB FOR EMERGENCY LIGHT ON RIGHT SIDE OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — CRACKED (FUSELAGE)

AFW - FUSELAGE SKIN AT STATION 1219 AND 537 LEFT HAS CRACK. AREA IS 2 INCHES BY 11.7 INCHES. CUT OUT CORROSION AND FABRICATED AND INSTALLED DOUBLERS.

Part: EEC — INOPERATIVE (RT ENGINE)

DFW - INFLIGHT T997/06 RIGHT ENGINE FUEL VALVE MESSAGE WITH RIGHT ENGINE VALVE LIGHT ON APPROXIMATELY 40 MINUTES AFTER TAKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND ENGINE MAIN ENGINE CONTROL PER MCM 71 95 20 AND 73 94 02. REPLACED FIRE LEVER PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: FITTING — DAMAGED (LT WING)

AFW - LEFT HAND WING TERMINAL FITTING AT SPAR AT STATION 155 HAS BLENDOUT. AREA IS 0.30 AND DEPTH IS 0.135 INCH. DAMAGED AREA WAS BLENDED SMOOTH, VISUALLY INSPECTED, AND REFINISHED PER THE SRM. A REPLACEMENT FASTENER WITH 0.050 INCH CRES WASHER WAS INSTALLED WET WITH BMS526 SEALANT.

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM AT STATION 303 HAS CORROSION REMOVAL ON UPPER SURFACE AS SHOWN ON SKETCH, BEYOND SRM LIMITS. COMPLETELY RMOVED CORROSION. APPLY ALODINE TO BLENDED AREA. APPLY PRIMER. FILL WITH SEALANT. (M)

Part: SKIN — CORRODED (FUSELAGE)

FOUND CORROSION ON WING CTR SECTION, UPPER SKIN STATION 955 BETWEEN BL0 AND LBL 10 MINIMUM THICKNESS AFTER BLEND ON AFT EDGE O.144 INCHES. REMOVED FASTENERS IN AFFECTED AREA AND REMOVED CORROSION, PERFORMED EDDY CURRENT INSPECTION. REWORKED AREA WITH FLAP PEEN AND FINISHED PER SRM 51-20-01. REINSTALLED FASTENERS AND APPLIED FUEL BARRIER. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLASHLIGHT AT RIGH MID GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLASHLIGHT AT RIGHT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: ACTUATOR — LEAKING (RUDDER)

KEF - LEFT HYDRAULIC SYSTEM DECREASED TO .73 WITH THE RF SYMBOL DISPLAYED ON DESCENT QUANTITY INCREASED TO .76. REMOVED AND REPLACED CENTER RUDDER PCA LEAK COMING FROM THERE. AFTER REPLACEMENT OP AND LEAK CHECK OK. OK FOR SERVICE. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

ORD - FOUND SEAT 28AB EMERGENCY LIGHTS INOPERATIVE. RECONNECTED EMEREGNCY LIGHT CONNECTOR PLUG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: IRU — FAILED (E/E BAY)

MIA - FOS ATTITUDE HEADING AND VSI FAILED DURING CLIMB-OUT, SELECTING IRS TO ALT FIXED PROBLEM. CHECKED AND FOUND RIGHT IRU AT FAULT REPLACED RESET IRU PERFORMED ALL REQUIRED TEST PER M/M ALL CHECKS GOOD OK FOR SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - FLT 905 - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING SEATS 2H, 3H, 7H, AND 8H INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR EMERGENCY ESCAPE PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PIN — DAMAGED (CONNECTOR)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 37H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT PINS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

MIA - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT AT FLIGHT DECK INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EIT LIGHT AT 8B INOPERATIVE. SECURED EMERGENCY EIT LIGHT CONNECTOR AT WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT 32 THROUGH 41 RIGHT SIDE AND 25 THROUGH 41 LEFT SIDE, INOPERATIVE. REPAIRED WIRE ON SEAT 38 RIGHT SIDE AND SEATS 29 AND 35, LEFT SIDE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHTS AT 24B AND 39H INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT WIRES AT SEAT 24B AND 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 35A INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT PATH LIGHT CONNECTOR AT SEAT 35A. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SWITCH — DIRTY (CABIN)

LHR - FLT 104 - EN ROUTE JFK/LHR - DURING CRUISE, EMERGENCY LIGHTS ILLUMINATED AND REMAINED ILLUMINATED UNTIL LIGHT TEST SWITCH WAS ROTATED. AIRCRAFT PROCEEDED TO LHR AND LANDED WITHOUT INCIDENT. CLEANED CONTACTORS ON EMERGENCY LIGHT TEST SWITCH AT 1L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 790)

AFW - FLOORBEAM CORRODED BEYOND LIMITS. FILLED, PRIMED AND PAINTED PER ENGINEERING MRB 767-1492. (M)

Part: FRAME — CORRODED (BS 654)

AFW - FOUND AND BLENDED OUT AN AREA OF CORROSION ON THE UPPER AND LOWER SURFACES OF THE FRAME UPPER CHORD FORWARD FLANGE IN THE FORWARD CARGO COMPARTMENT. REFINISHED THE BLENDED AREA PER SRM. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB767-1497. (M)

Part: SILL — CORRODED (R2 DOORWAY)

AFW - FOUND AND BLENDED OUT TWO AREAS OF CORROSION ON THE FLOOR SUPPORT TEE AT THE R2 DOOR LOWER SILL. REFINISHED THE BLENDED AREAS PER SRM. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB767-1489. (M)

Part: FRAME — CORRODED (BS 1219)

AFW - FOUND AND BLENDED CORROSION ON THE UPPER SURFACE OF THE FRAME INNER CHORD AFT FLANGE IN THE AFT CARGO. THE BLEND OUT EXCEEDS SRM LIMITS. REFINISHED THE BLENDED AREA PER SRM. APPROVED FOR CONTINUED SERVIEC WITH NOTED CONDITION BY ENGINEERING PER MRB767-1494. (M)

Part: FRAME — CORRODED (BS 500)

AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER AND LOWER SURFACE OF THE FRAME INNER CHORD FORWARD FLANGE IN THE FORWARD CARGO COMPARTMENT. REFINISHED THE BLENDED AREA PER SRM. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB767-1496. (M)

Part: SEAT TRACK — CORRODED (BS 347)

AFW - FOUND AND BLENDED TWO AREAS OF CORROSION ON THE UPPER SURFACE OF THE UPPER FLANGE AT THE SEAT TRACK. REFINISHED THE BLENDOUTS PER SRM 53-00-52 FIG 101. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1495. (M)

Part: SOCKET — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 38H INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT SOCKET CONTACT WIRE AT PAX SEAT 38H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOOR BEAM — CORRODED (BS 347)

AFW - FLOOR BEAM AT STATION 347 HAS CORROSION. REMOVED ON UPPER SURFACE AT VARIOUS LOCATIONS. MATERIAL REMOVED IS BEYOND SRM LIMITS, PER MRG 767-1069. (M)

Part: LIGHT — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEATS 37E THROUGH 41E INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLIES AT PAX SEATS 37E THROUGH 41E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING ON RT SIDE OF COACH FOUND INOPERATIVE. REPAIRED CONNECTOR ON RT SIDE OF COACH. SYTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: SLIDE — DEFECTIVE (ENTRY DOOR)

LAX - DURING SLIDE SHOP RECEIVING INSPECTION, FOUND HOLE ABOVE LEFT RELIEF VALVE EMERGENCY EVACUATION SLIDE. REPAIRED SLIDE, SLIDE CHECKS GOOD. (X)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEAT ROWS 22HJ THROUGH 24HJ INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT ROW 24HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)