N336AA

Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,317 hrs · 19,004 cycles

STATION 500 J-CAP HAS CORROSION BOTTOM SIDE AT RIGHT OUTBOARD END AT MOUNTING NUT PLATE FOR ROLLER TRACK. REPLACED J-CAP PER SRM 53-00-07-2R 4.

Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,317 hrs · 19,004 cycles

FORWARD CARGO J-CAP HAS INTERGRANULAR CORROSION AT STATION 676 LEFT BUTTLINE 40. REPLACED J-CAP PER SRM 51-40-02.

Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,317 hrs · 19,004 cycles

J-CAP AT STATION 456 HAS INTERGRANULAR CORROSION BOTTOM SIDE AT LEFT OUTBOARD END AT MOUNTING NUT PLATE FOR ROLLER TRACK. INSTALLED J-CAP REPAIR PER SRM 53-00-07-2R.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,317 hrs · 19,004 cycles

FUSELAGE SKIN CORRODED AT STATION 1232 BETWEEN STRINGERS 37 AND 38 LEFT. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-01-2R.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 94,317 hrs · 19,004 cycles

INTERCOSTAL AT CEILING AREA OF FORWARD CARGO BETWEEN STATIONS 742 TO 764 AT RIGHT BUTTLINE 40 CRACKED. REMOVED AND REPLACED INTERCOSTAL PER AARD 53-30-00-1.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,317 hrs · 19,004 cycles

STRINGER SPLICE FOR STRINGER 36 RIGHT, JUST AFT OF STATION 434 HAS CORROSION ON OUTBOARD SIDE. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-03.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,317 hrs · 19,004 cycles

STRINGER 36 RIGHT, BETWEEN STATIONS 412 TO 434 HAS AREA OF CORROSION / ON BOTTOM INBOARD SIDE JUST FORWARD OF STRINGER SPLICE. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-03.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,317 hrs · 19,004 cycles

STRINGER 34 LEFT, BETWEEN STATIONS 412 TO 434 HAS 2 AREAS OF CORROSION. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-03.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,317 hrs · 19,004 cycles

STRINGER 39 LEFT BETWEEN STATIONS 412 TO 434 HAS AREA OF CORROSION ON OUTBOARD SIDE. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-03.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,317 hrs · 19,004 cycles

SHEAR TIE AT STATION 1540 BETWEEN STRINGERS 35 AND 36 LEFT. REPLACED SHEAR TIE PER SRM 51-10-02-0G.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,317 hrs · 19,004 cycles

SHEAR-TIE AT STATION 1540 BETWEEN STRINGERS 36 AND 37 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02-0G.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,317 hrs · 19,004 cycles

SHEAR TIE AT STATION 1540 BETWEEN STRINGERS 37 AND 38 LEFT CORRODED. REPLACED SHEAR TIE PER SRM 51-10-02-0G.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 94,317 hrs · 19,004 cycles

AFT CARGO DECK TO DOOR FRAME ANGLE HAS HEAVY CORROSION AT THE FORWARD END STATION 1263, RIGHT BUTTLINE 45. REPLACED SUPPORT ANGLE PER SRM 51-10-02.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 91,317 hrs · 18,403 cycles

L1 DOOR EXTERIOR AND LT OVERWING EMERGENCY LIGHTS INOPERATIVE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 91,317 hrs · 18,403 cycles

LEFT OVERWING EXTERIOR EMERGENCY EVACUATION LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK M736 AND OPERATIONAL CHECK IS NORMAL PER AMM 33-51-07.

Part: FITTING — CRACKED (RT WING) · airframe 91,101 hrs · 18,358 cycles

CRACK ON RIGHT WING AFT PITCHLOAD FITTING OUTBOARD TENSION BOLT HOLE BACKUP FITTING PLUG. INSTALLED FREEZE PLUG PER ECO 3194AD.

Part: IDG — INOPERATIVE (LT ENGINE) · airframe 91,080 hrs · 18,350 cycles

JFK - CREW REPORTED LEFT ENGINE DRIVE LIGHT ILLUMINATED ON TAKEOFF. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. DEFERRED NUMBER 1 GENERATOR PER MEL. REPLACED LEFT INTEGRATED DRIVE GENERATOR AT AFW ON 10/05/2011. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 89,846 hrs · 18,095 cycles

CORROSION WAS FOUND ON THE RIGHT KEEL BEAM LOWER PANEL LANDING INNER CHORD AT STATIONS 979 AND 1003. BOTH SPOTS OF CORROSION WERE LOCATED AT FASTENER SCREW HOLES FOR THE BELLY FAIRING PANELS. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-50-12-2R REPAIR 2 AND EA B767-53-017348 ACCOMPLISHED.

Part: MODULE — INOPERATIVE (CABIN) · airframe 85,017 hrs · 17,121 cycles

BIDIRECTIONAL EMERGENCY LIGHTS MOUNTED ON LEFT AND RIGHT AFT LAVATORY AREA INOPERATIVE. REPLACED BATTERY MODULE AT 38HJ SIDE GRILL PANEL. OPS CHECKED NORMAL.

Part: FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 84,537 hrs · 17,019 cycles

LIGHT CORROSION WAS FOUND ON THE AFT CARGO STATION 1263 FRAME INNER CHORD VERTICAL AFT SURFACE AT APPROXIMATELY RIGHT BUTTLINE 16. REMOVED CORROSION, ACCOMPLISHED SURFACE AND OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION FOR CRACKS. FABRICATED REPAIR ANGLE AND INSTALLED REPAIR ANGLE PER EA B767-53-008296.

Part: SLIDE — FAILED (CABIN) · airframe 84,537 hrs · 17,019 cycles

SLIDE DID NOT INFLATE. REPLACED SLIDE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 84,032 hrs · 16,913 cycles

EMERGENCY SEAT MOUNTED LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK.

Part: MODULE — INOPERATIVE (CABIN) · airframe 83,408 hrs · 16,787 cycles

IN SEAT EMERGENCY LIGHTING INOPERATIVE FROM 20H TO 30H. REMOVED AND REPLACED MODULE M9031. OPS CHECKED OK.

Part: TUBE — LEAKING (ENGINE OIL) · airframe 82,143 hrs · 16,532 cycles

LAX LEFT HAND ENGINE WAS SHUTDOWN DUE TO ZERO OIL PRESSURE. LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND OIL LINE KINKED AND LEAKING. REPLACED ENGINE OIL FILTER TUBE ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,544 hrs

LAX - EMERGENCY PORTABLE LIGHT AT COCKPIT DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT ASSEMBLY AT COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — BROKEN (EMERGENCY LIGHTS) · airframe 78,275 hrs

LAX - EMERGENCY LIGHT AT SEAT 27B HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 27B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LAMP — MISSING (EMERGENCY LIGHTS) · airframe 78,275 hrs

LAX - EMERGENCY LIGHT AT SEAT 27B HAS LAMP MISSING. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 27B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 78,275 hrs

LAX - EMERGENCY LIGHT AT SEAT 27B HAS LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 27B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHTS AT ENTRY DOORS ONE LEFT AND TWO RIGHT INOPERATIVE. REPLACED BULBS FOR EMERGENCY LIGHTS AT ENTRY DOORS ONE LEFT AND TWO RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — BROKEN (CABIN)

JFK - EMERGENCY LIGHT FIXTURE IN BUSINESS CLASS GALLEY RIGHT SIDE BROKEN. REPLACED LIGHT FIXTURE FOR EMERGENCY LIGHTS IN BUSINESS CLASS GALLEY RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PIN — BROKEN (CONNECTOR)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHT AT SEAT 31B INOPERATIVE. REPLACED BROKEN PIN AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

BOS - DURING OVERNIGHT MAINTENANCE, FOUND MID GALLEY RIGHT FORWARD SEAT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ILGHT AT ROW 2 THROUGH 10 DIM. REPLCED EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

IAD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS LEFT SIDE COACH SEATS 20B THROUGH 30B INOPERATIVE. REPLACED CONNECTOR AT SEAT 23B. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE SEAT PATH LIGHT AT SEAT 22H INOPERATIVE. RESEATED CONNECTOR AT SEAT 22H. SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — DISCONNECTED (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT 22H INOPERATIVE. RECONNECTED EMERGENCY EXIT SEAT PATH LIGHT WIRE AT SEAT 22H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — MISSING (ROW 19AB)

LAX - DURING OVERNIGHT MAINTENANCE, SEAT 19AB HAD ONLY ONE RED LIGHT ASSEMBLY FOR EMERGENCY EXIT ESCAPE PATH LIGHTING SYSTEM. INSTALLED SECOND EMERGENCY EXIT ESCAPE PATH LIGHTING ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: FLOORBEAM — CORRODED (BS 347)

AFW - FLOORBEAM AT STATION 347 HAS CORROSION REMOVAL ON UPPER SURFACE. ALODINE BLENDED AREA FABRICATE STRAP APPLY TWO COATS PRIMER FILL BLENDED AREA INSTALL STRAP WET. (M)

Part: FLOORBEAM — CORRODED (BS 287)

AFW - FLOORBEAM AT STATION 287 HAS CORROSION REMOVAL ON UPPER SURFACE. ALODINE BLENDED AREA FABRICATE STRAP APPLY TWO COATS PRIMER. INSTALL STRAP WET WITH SEALANT. (M)

Part: SUPPORT — CORRODED (BS 1480)

AFW - VERY FORWARD VERTICAL LEG OF L-2 DOOR FLOOR SUPPORT TEE (SPLASH GUARD) AT STATION 1480, HAD CORROSION BLEND BEYOND SRM LIMITS. REFER TO ATTACHED FIGURE, BLEND OUT CORROSION, ALODINED AND APPLY TWO COATS OF PRIMER. (M)

Part: FLOORBEAM — CORRODED (BS 325)

AFW - FLOORBEAM AT STATION 325 HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACE. ALODINE BLENDED AREA, FABRICATED STRAP. APPLY TWO COATS PRIMER, INSTALL STRAP WET WITH SEALANT. (M)

Part: FLOORBEAM — CORRODED (BS 875)

AFW - FLOORBEAM RBL 11 AND STATION 875 HAD A WEAR MARK AND LIGHT CORROSION BLENDED BEYOND LIMITS. BLEND OUT CORROSION, ROTO-PEEN AREA. ALODINE AND APPLY TWO COATS OF PRIMER AND FILL WITH SEALANT. (M)

Part: SKIN — CORRODED (WING)

AFW - FOUND CENTER WING UPPER SKIN HAD CORROSION BLENDED BEYOND SRM LIMITS, AT STATION 955 RBL 71. REPAIRED IAW MRB 767-1735. (M)

Part: SKIN — CORRODED (CARGO DOOR)

AFW - BULK CARGO DOOR HAD 5 SMALL AREAS OF CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED IAW MRB 767-1739. (M)

Part: BULB — FAILED (COCKPIT)

BOS - FLT 155 - DURING APPROACH LEFT MAIN LANDING GEAR DOWN AND LOCK LIGHTS INOPERATIVE AND ONE LIGHT ON RIGHT SIDE INOPERATIVE. CREW REQUESTED EMERGENCY EQUIPMENT TO STANDBY. AIRCRAFT LANDED BOS WITHOUT INCIDENT. PERFORMED BITE OF PROXIMITY UNIT, NO FAULTS OR EICAS MESSAGES NOTED. RELAMPED BOTH LEFT AND ONE RIGHT GEAR DOWN AND LOCK LIGHT BULBS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: RADAR TR UNIT — FAILED (E/E COMPT)

ORD - FLT 24 - WEATHER RADAR FAILED MESSAGE SAID ANTENNA TEST MODE. REPLACED WEATHER RADAR ANTENNA AND TRANSCEIVER AS PER MM ACCOMPLISHED REQUIRED TESTS. ALL CHECK NORMAL WEATHER RADAR OK FOR SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVENIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 24B INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PAX SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SKIN — DAMAGED (LT PYLON)

AFW - FOUND SIDE SKIN DAMAGE IS BEYOND SRM LIMITS AFTER BLEND OUT. SIDE SKIN BLENDED AND FINISHED PER MRB 767-1098. SIDE SKIN IS ACCEPTABLE FOR CONTINUED SERVICE WITH NOTED CONDITION PER ENGINEERING MRB 767-1098. (M)

Part: CART — DEFECTIVE (CABIN)

BHX - FLT NR 0024 - BUSINESS CLASS GALLEY WARMING CARTS OVERHEATS SEVERELY WITH ELECTRICAL SMELL. REPLACED BUSINESS CLASS GALLEY WARMING CART. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)