N327AA

Part: SKIN — CRACKED (LE SLAT) · airframe 100,102 hrs · 18,871 cycles

NUMBER 9 SLAT LEADING EDGE LOWER SURFACE HAS A CRACK AT A FASTENER 36 INCHES FROM THE INBOARD SIDE. INSTALLED DOUBLER REPAIR PER SRM 57-43-01-2R.

Part: SKIN — CRACKED (LE SLAT) · airframe 100,102 hrs · 18,871 cycles

NUMBER 9 SLAT LEADING EDGE LOWER SURFACE HAS A CRACK AT A FASTENER 36 INCHES FROM OUTBOARD END. INSTALLED DOUBLER REPAIR PER SRM 57-43-01-2R.

Part: AILERON — DAMAGED (LT WING) · airframe 100,102 hrs · 18,871 cycles

DAMAGE TO TRAILING EDGE OF LEFT INBOARD AILERON. ACCOMPLISHED HOT BOND REPAIR PER SRM 51-70-17.

Part: TORQUE BOX — CRACKED (LT PYLON) · airframe 100,102 hrs · 18,871 cycles

EVIDENCE OF CRACKS ON LEFT PYLON UPPER TORQUE BOX SKIN, LOCATED AT GENERATOR FEEDER CABLE PASS THROUGH FORWARD NUTPLATES. INSTALLED DOUBLER REPAIR PER AARD 54-52-01-1.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 100,102 hrs · 18,871 cycles

NUMBER 11 SLAT TRAILING EDGE WEDGE DISBONDED. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10-2R.

Part: SWIVEL — CORRODED (RT MLG) · corrosion level 2 · airframe 95,136 hrs · 17,865 cycles

CORROSION WAS FOUND ON THE RIGHT MAIN LANDING GEAR SIDE STRUT SWIVEL FITTING. THE CORROSION IS LIMITED TO THE OUTBOARD LUG OUTBOARD FACE, CHAMFER, AND BORE OF THE MAIN PIVOT JOINT TO THE MLG SIDE STRUT., THE CORROSION WAS REMOVED BY MACHINING THE LUG FACE AND BORE AND INSTALLING A OVERSIZED BUSHING ALL AUTHORIZED PER EA B767-57-016970 REV ORIG.

Part: PROBE — DEFECTIVE (TAT) · airframe 94,986 hrs · 17,832 cycles

LAX - CREW REPORTED TAT PROBE EICAS MESSAGE APPEARED ON UPPER EICAS AND TAT ANNUNICATOR LIGHT ON OVERHEAD PANEL ALSO ILLUMINATED. EMERGENCY DECLARED, FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. REPLACED TOTAL AIR TEMPERATURE PROBE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FSEU — MALFUNCTIONED (ZONE 100) · airframe 93,771 hrs · 17,586 cycles

MIA - CREW REPORTED DURING APPROACH FLAT SLAT ASSYMETRY. EMERGENCY DECLARED LANDED MIA WITHOUT INCIDENT. ACCOMPLISHED BITE OF FLAP SLAT ELECTRONICS UNIT AND FOUND FAULT CODE M548 AND M603. RESET SYSTEM AND OPERATED FLAPS SEVERAL TIMES AND NO FAULTS NOTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: FLEX LINE — LEAKING (HORIZ STAB) · airframe 93,217 hrs · 17,474 cycles

LAX - CREW REPORTED CENTER HYDRAULIC QUANTITY LOSS. EMERGENCY DECLARED LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND HORIZONTAL STAB SECONDARY BRAKE LINE LEAKING. INSTALLED FLEX LINE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 91,408 hrs · 17,098 cycles

STATION 157 AT STRINGER 24 RIGHT DAMAGED. ACCOMPLISHED DOUBLER REPAIR PER EA B767-53-010531.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,539 hrs · 16,921 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 19HJ TO 38HJ DIM. REPLACED BATTERY PACKS AT SEATS 26HJ AND 38HJ. OPS CHECK NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 90,539 hrs · 16,921 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM ROW AB TO ROW 20AB VERY DIM AND STAY "ON" WITH SWITCH TURNED OFF. REPLACED BATTERY MODULE AT 11AB GRILL. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,539 hrs · 16,921 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM ROW AT AB TO ROW 20AB VERY DIM AND STAY "ON" WITH SWITCH TURNED OFF. REPLACED BATTERY PACK AT 3AB SIDE GRILL. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,539 hrs · 16,921 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM ROW AT AB TO ROW 20AB VERY DIM AND STAY "ON" WITH SWITCH TURNED OFF. REPLACED BATTERY PACK AT 11AB SIDE GRILL. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 85,572 hrs

JFK - EMERGENCY EXIT SIGN AT MID GALLEY LEFT SIDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT LEFT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROL UNIT — INOPERATIVE (WINDOW HEAT) · airframe 84,549 hrs · 84,549 cycles

AFW INFLIGHT T9660/28JUN. LT NR 1 OUTER WINDSHIELED CRACKED DURING FLIGHT. RETURNED TO AFW AND LANDED WITHOUT INCIDENT. REPLACED LT FORWARD WINDOW HEAT CONTROL UNIT. REPLACED LT FORWARD WINDSHIELD AND WIPER. SYSTEM GROUND CHECKED NORMAL OPERATION. (S)

Part: SILL — CORRODED (BS 610-615) · airframe 84,547 hrs · 15,710 cycles

AFW FORWARD CARGO DOOR CUT OUT, LOWER MAIN SILL, OUTER CHORD HAS CORROSION REMOVAL BETWEEN STA 615 AND 610. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED PER MRB 767 3213. AREA OF DISCREPANCY IS 2.7 INCHES LONG AND IS THE WIDTH OF THE FLANGE WITH A DEPTH OF 0.230 INCHES. (S)

Part: KEELBEAM — CORRODED (BS 1219 S38L) · airframe 84,547 hrs · 15,710 cycles

AFW - KEEL BEAM AT STATION 1219 HAD CORROSION REMOVED FROM THE VERTICAL AND HORIZONTAL FLANGES. REPAIRED PER MRB 767-3237. VERTICAL FLANGE: 0.4 INCH BY 0.9 INCH WITH A DEPTH OF 0.050 INCH. HORIZONTAL FLANGE: 0.8 INCH BY 2.4 INCH WITH A DEPTH OF 0.160 INCH. (S)

Part: WEB — CORRODED (FUSELAGE) · airframe 84,547 hrs · 15,710 cycles

AFW - CLOSURE PANEL WEB, PRESSURE DECK HAS CORROSION REMOVAL. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED PER MRB 767 3214. AREA OF DISCREPANCY IS A DEPTH OF 0.082 INCHES. (S)

Part: FLOORBEAM — CORRODED (BS 325) · airframe 84,547 hrs · 15,710 cycles

AFW - FLOORBEAM UPPER CAP AT STATION 325 HAD CORROSION. REMOVED FROM THE HORIZONTAL FLANGES FROM RT BUTTLINE 11 TO RT BUTTLINE 50. REPAIRED PER MRB 767-3220. (S)

Part: SEAT TRACK — CORRODED (BS 341) · airframe 84,547 hrs · 15,710 cycles

AFW - SEAT TRACK HAS CORROSION REMOVAL. REPAIRED PER MRB 767 3216. (S)

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 84,547 hrs · 15,710 cycles

AFW - SEAT TRACK HAS CORROSION REMOVAL. REPAIRED PER MRB 767 3216. (S)

Part: SEAT TRACK — CORRODED (BS 341) · airframe 84,547 hrs · 15,710 cycles

AFW - SEAT TRACK HAS CORROSION REMOVAL. REPAIRED PER MRB 767 3216. (S)

Part: CAPACITOR — MISSING (CABIN) · airframe 82,522 hrs

JFK - EMERGENCY LIGHT AT MID GALLEY MISSING CAPACITOR. REPLACED CAPACITOR FOR EMERGENCY LIGHT AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN)

JFK - EMERGENCY LIGHT AT SEAT ROW 3HJ INOPERATIVE. REPAIRED EMERGENCY LIGHT AT SEAT ROW 3HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)

LAX - EMERGENCY FLOOR LIGHT AT MID GALLEY INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY FLOOR LIGHT AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: RETAINER — DAMAGED (THRUST REVERSER)

AFW - LEFT AND RIGHT HAND PYLON SKINS INBOARD AND OUTBOARD AT STATION 250 HAS GROOVE WORN FROM THRUST REVERSER SEAL RETAINER. BLENDED GROOVE PER MRB NUMBER 767 2842 AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION. NO CRACKS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: TRANSMITTER — INOPERATIVE (HYD SYSTEM)

JFK T019/05 EN ROUTE JFK-LAX LOSS OF LEFT SYSTEM HYDRAULIC QUANTITY AND PRESSURE. RETURNED JFK AND LANDED WITHOUT INCIDENT. REPLACED LEFT SYSTEM HYDRAULIC QUANTITY TRANSMITTER PER MM 29-33-02-4. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — BROKEN (CABIN)

SFO) RT SIDE MID GALLEY EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE UNDER CARPET FOR RIGHT SIDE MID GALLEY EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: WEDGE — DELAMINATED (TE FLAP)

DURING OVERNIGHT MAINTENANCE, RIGHT OUTBOARD TRAILING EDGE FLAP TRAILING EDGE WEDGE HAS .75 BY .375 INCH HOLE AND 41 INCH CRACK IN THE LOWER SKIN SURFACE OUTBOARD OF THE OUTBOARD HINGE FAIRING. DAMAGE COVERED WITH SPEED TAPE FOR FERRY TO AFW FOR FURTHER EVALUATION/REPAIR. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SJU - DURING OVERNIGHT MAINTENANCE, FOUND FIRST CLASS GALLEY EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. REPLACED FIRST CLASS GALLEY EMERGENCY ESCAPE PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CABIN)

DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING SEAT 32H INOPERATIVE. SECURED CONNECTOR AT SEAT LEG FOR 32H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — LOOSE (CABIN)

DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING ROW 17B THROUGH 28B INOPERATIVE. SECURED EMERGENCY LIGHT POWER SUPPLY CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATIONS.

Part: CONNECTOR — LOOSE (CABIN)

JFK - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT 32H INOPERATIVE. RECONNECTED LOOSE CONNECTOR AT SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DIRTY (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32H INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONNECTORS AT SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — DAMAGED (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 17H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 17H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LAMP — DEFECTIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 31HJ INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HOLDER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

LAX - DURING OVERNIGHT MAINTENANCE, AFT RIGHT SIDE EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED AFT RIGHT SIDE EMERGENCY EXIT LIGHT AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: PUMP — LEAKING (FUSELAGE)

JFK - FLT 120 - EN ROUTE JFK-CDG - DURING CRUISE DETECTED FUEL IMBALANCE BETWEEN RIGHT NAIN AND LEFT MANI FUEL TANKS. FUEL WAS BALANCED EQUAL. FUEL CONTINUED TO IMBALANCE. RETURNED JFK AND LANDED WITHOUT INCIDENT. REPLACED RIGHT SIDE FORWARD BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: HANDLE — OUT OF ADJ (PAX DOOR)

IAD - FLT 77 - PASSING THROUGH 27000 FEET, RECEIVED UPPER EICAS MESSAGE-CAUTION-L FWD ENT DOOR LIGHT WITH ASSOCIATED ENTRY DOORS LIGHT ON OVERHEAD ANNUNCIATOR. THE DOOR HANDLE WAS OPENING AS AIRCRAFT CLIMBED. AIRCRAFT WAS DESCENDED TO FL2500 AND HANDLE BEGAN TO DROP. HANDLE WOULD NOT STAY DOWN UNTIL THE DESCENT. LANDED IAD WITHOUT INCIDENT. INTERIOR DOOR HANDLE OUT OF ADJUSTMENT. READJUSTED DOOR HANDLE SYSTEM GROUND CHECK NORMAL OPERATION. (M)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ON THE RIGHT SIDE OF THE MID-GALLEY INOPERATIVE. REPAIRED WIRING BEHIND THE EMERGENCY EXIT LIGHT ON THE RIGHT SIDE OF THE MID-GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CAM — BROKEN (LT WING SLIDE)

SFO - DURING OVERNIGHT MAINTENANCE, LEFT HAND OVER WING SLIDE COMPARTMENT INFLATION CABLE DISCONNECT CAM BROKEN. REPLACED LEFT HAND OVER WING SLIDE CAM ASSEMBLY AND PRECAUTIONARY REPLACED LEFT HAND OVER WING SLIDE BOTTLE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — LOOSE (AFT LAVATORY)

SFO - DURING OVERNIGHT MAINTENANCE, DISCOVERED EMERGENCY EXIT FLOOD LIGHT AT AFT RIGHT HAND LAVATORY POSITION INOPERATIVE. RE-SECURED EMERGENCY EXIT FLOOD LIGHT AT AFT RIGHT HAND LAVATORY POSITION. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: O-RINGS — BROKEN (LT IDG)

ORD - FLT 682 - WHILE CRUISING AT 41:000 NORMAL ENGINE POWER SETTING TWO AND ONE-HALF HOURS AFTER TAKEOFF, LEFT GENERATOR DRIVE LIGHT STARTED RAPID FLICKERING AND INTERMITTENT 'LT GEN DRIVE' EICA MESSAGE. TEN MINUTES LATER, LT GENERATOR DRIVE WAS DISCONNECTED. FOUND LT GENERATOR DELTA P-FILTER BOWL O-RING BROKEN IN HALF. REPLACED O-RING AND SERVICED IDG. RESET BUS POWER ON LT L-BUS, RESET GENERATOR AND PERFORMED ENGINE RUN. GENERATOR CHECKS GOOD. NO LEAKS NOTED. (X)

Part: LIGHT — BROKEN (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT INDICATOR ASSEMBLY AT RIGHT AFT LAVATORY FORWARD POSITION FOUND INOPERATIVE. REPLACED EMERGENCY EXIT INDICATOR LIGHT ASSEMBLY AT RIGHT AFT LAVATORY FORWARD POSITION. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: IDG — FAILED (RT ENGINE)

BHX - RIGHT GEN DRIVE ILLUMINATED, RIGHT GEN CAUTION EICAS IDG SENSOR FAIL EICAS, RT IDG DISCONNECTED. REMOVED AND REPLACED COOLER AND IDG ASSEMBLY, LEAK CHECK OK PER MM EMP 108437. OPERATIONAL CHECK NORMAL CLEARED MEL 8-471DC-B CLEARED MIC SHEET. (M)

Part: FLOOR BEAM — CORRODED (BS 850-870)

AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE CABIN FLOOR BEAMS. THE DAMAGE EXCEEDS SRM LIMITS. REMOVED FLOOR BEAM FROM STA 841 TO STA 876.8. SPLICED IN NEW SECTION OF FLOOR BEAM APPROVED BY ENGINEERING PER MRB 767-1393. TST: 44,482.55 HOURS. CYCLES: 7,804. (X)

Part: DOOR — CORRODED (CARGO COMPT)

AFW - FOUND AND BLENDED OUT CORROSION ON THE INNER SURFACE OF THE INNER CHORD ON THE AFT CARGO DOOR. SEVEN BLEND-OUTS EXCEED SRM LIMITS. TRIMMED OR BLENDED CORROSION AREAS AS REQUIRED. ALODINED AND PRIMED AREA. FABRICATED AND INSTALLED FILLERS USING 7075-T6 ALUMINUM. APPROVED BY ENGINEERING PER MRB 767-1394. (X)

Part: SUPPORT — CORRODED (BS 1544-1546)

AFW - FOUND AND BLENDED OUT TWO AREAS OF CORROSION ON THE FLOOR SUPPORT TEE FOR THE AFT GALLEY. BLEND-OUTS EXCEEDED SRM ALLOWABLE LIMITS. REFINISHED BLENDED AREAS. ARPPROVED FOR CONTINENTAL SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1392. TST: 44,482.55 HOURS. CYCLES: 7,804. (X)

Part: TEST SWITCH — DEFECTIVE (AFT F/A PANEL)

ORD - FLT 0037 - EN ROUTE ZRH/ORD DURING CRUISE, PASSENGER EMERGENCY EXIT LIGHTING ILLUMINATED AND COULD NOT BE EXTINGUISHED. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO ORD, LANDING WITHOUT INCIDENT. REPLACED EMERGENCY EXIT LIGHTING TEST SWITCH 528 AT AFT F/A PANEL. REPLACED BATTERY PACKS. SYSTEM GROUND CHECKED, NORMAL OPERATIONAL. (X)

Part: FLOOR BEAM — CORRODED (BS 347)

AFW - FLOOR BEAM FOUND CORRODED, BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND FILLED BLENDED AREA. FABRICATED AND INSTALLED REPAIR STRAP, USING .050 INCH 301 HALF HARD STAINLESS STEEL. APPROVED BY ENGINEERING PER MRB 767-1064. (M)

Part: FLOOR BEAM — CORRODED (BS 287)

AFW - FLOOR BEAM AT STATION 287 RBL 30 TO RBL 64 HAD CORROSION BLENDED BEYOND SRM LIMITS. REMOVED CORROSION, PRIMED. FILLED WITH BMS 5-95, FABRICATED AND INSTALLED REPAIR STRAP. (M)

Part: FLOOR BEAM — CORRODED (BS 955)

AFW - FLOOR BEAM AT RBL 11.06 STATION 955 HAD CORROSION REMOVED BEYOND SRM LIMITS. BLENDED CORROSION. CHECKED, NO CRACKS. REFINISHED AREA CONTINUED IN SERVICE. (M)

Part: FLOOR BEAM — CORRODED (BS 1480)

AFW - FOUND FLOOR BEAM CORRODED BEYOND SRM LIMITS AFTER BLENDING. ALODINED BLENDED AREA. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 HALF HARD STAINLESS STEEL. APPROVED BY ENGINEERING EPR MRB 767-1067. (M)

Part: SKIN — CORRODED (BS 957)

AFW - HEAVY CORROSION REMOVED ON CENTER WING UPPER SKIN AT AFT DRAIN LOWER CHORD TO FLOOR BEAM T-EXTRUSION WAS CUT AND REMOVED. BLENDED AREAS OF CORROSION AND TREATED, PRIMED AND PAINTED. FABRICATED T-EXTRUSION REPAIR. (M)