N339AA

Part: TAT PROBE — INOPERATIVE (ZONE 200) · airframe 96,146 hrs · 19,362 cycles

LAX PILOT REPORTED TAT READING WAS INTERMITTENT & NEEDLE MOVING ERRATICALLY. FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TWO RELAYS & TAT PROBE. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: CHARGER — DEFECTIVE (EMERGENCY LIGHT) · airframe 91,197 hrs · 18,363 cycles

EMERGENCY SEAT MOUNTED ESCAPE LIGHTING PATH STAYED ON FROM ROWS 20HJ TO 30HJ AFTER REMOVING POWER FROM AIRCRAFT. REMOVED AND REPLACED BATTERY CHARGER MODULE ASSEMBLY AND BATTERY PACK LOCATED AT SEAT 25HJ SIDEWALL. OPS CHECKED NORMAL.

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHT) · airframe 91,197 hrs · 18,363 cycles

EMERGENCY SEAT MOUNTED ESCAPE LIGHTING PATH STAYED ON FROM ROWS 20HJ TO 30HJ AFTER REMOVING POWER FROM AIRCARFT. REMOVED AND REPLACED BATTERY CHARGER MODULE ASSEMBLY AND BATTERY PACK LOCATED AT SEAT 25HJ SIDEWALL. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,359 hrs · 17,991 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 10H INOPERATIVE. REPLACED LAMP FOR 10H SEAT MOUNTED EMERGENCY LIGHT. OPS CHECK NORMAL.

Part: MODULE — INOPERATIVE (CABIN) · airframe 84,976 hrs · 17,092 cycles

SEAT EMERGENCY LIGHTS AT 10AB TO 18AB INOPERATIVE. REPLACED MODULE M9028 FOR SEAT EMERGENCY LIGHTS AT 10AB TO 18AB. OPS CHECKED NORMAL.

Part: BUSHING — DAMAGED (RT PYLON) · airframe 84,007 hrs · 16,896 cycles

RIGHT PYLON ONLY THE INBOARD MOST AND OUTBOARD MOST MIDSPAR BUSHINGS WERE FOUND TO MOVE BY USING LIGHT PRESSURE. ACCOMPLISHED BORE/FASTENER HOLE REWORK PER EA B767-54-009486.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,007 hrs · 16,896 cycles

AN 8 INCH SECTION OF STRINGER 39 LEFT JUST BEFORE THE PRODUCTION STRINGER SPLICE AT STATION 1307 CORRODED. ACCOMPLISHED SPLICE REPAIR PER EA B767-53-009270.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,997 hrs · 16,892 cycles

CORROSION WAS FOUND ON THE LEFT SECTION 46 WING-TO-BODY FAIRING SCREW HOLES COMMON TO THE FUSELAGE SKIN. AFTER CORROSION WAS REMOVED, 5 SCREW HOLES LOCATED BETWEEN STATIONS 1092 TO 1137 AND STRINGERS 37 AND 38 LEFT. HIGH FREQUENCY EDDY CURRENT WAS ACCOMPLISHED TO ENSURE ALL CORROSION HAD BEEN REMOVED. BOEING APPROVED TO REPAIR THE HOLES BY INSTALLING INTERNALLY COUNTERSUNK FREEZE PLUGS PER THE SRM. EA B767-53-009310.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 83,997 hrs · 16,892 cycles

CORROSION WAS FOUND ON THE AFT CARGO DOOR NUMBER 4 BEAM INNER CHORD AT D STATION 175 COMMOM TO A NUT PLATE SCREW HOLE. THE CORROSION WAS REMOVED BY BLENDING LEAVING A MINIMUM REMAINING THICKNESS OF 0.093 INCH FROM PARENT THICKNESS OF 0.125. A REPAIR STRAP OF 0.063 INCH 7075-T6 WAS INSTALLED OVER THE BLEND EXTENDING 3 FASTENERS ON EITHER SIDE OF DEEPEST LOCATION. ALODINE, PRIMER AND CIC WERE APPLIED TO THE AREA FOR CORROSION PREVENTION. EA COMP-52-009208.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,997 hrs · 16,892 cycles

SEVERE CORROSION WAS FOUND AT STATION 780 BETWEEN STRINGER 34 RIGHT AND STRINGER 35 RIGHT AT THE LOWER SKIN PANEL AFT EDGE. INSTALLED DOUBLER PER SRM 53-0-01-02R.

Part: BEAM — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 83,997 hrs · 16,892 cycles

CORROSION ON THE AFT CARGO DOOR NUMBER 4 BEAM INNER CHORD AT STATION 175 COMMON TO A NUT PLATE SCREW HOLE. CORROSION WAS REMOVED AND REPAIR STRAP OF 0.063 INCHES 7075-T6 WAS INSTALLED OVER THE BLEND EXTENDING 3 FASTENERS ON EITHER SIDE OF THE DEEPEST LOCATION. ALODINE, PRIMER AND CIC WERE APPLIED TO THE AREA FOR CORROSION PREVENTION. EA COMP-52-009208.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 83,997 hrs · 16,892 cycles

PERFORMED SCHEDULED MAINTENANCE WORK CARD 0357. EMERGENCY LIGHTS FAILED TO ILLUMINATE FOR 10 MINUTES. PERFORMED MAINTENANCE WORK CARD 279A TO REPLACE EMERGENCY LIGHT POWER SUPPLY BATTERIES DURING CURRENT HEAVY C-CHECK.

Part: VALVE — FAULTY (AC PACK) · airframe 82,240 hrs · 16,524 cycles

PBI - INFLIGHT JFK-MIA. AIR INTERRUPT DUE TO RIGHT PACK FAILED EN ROUTE AND LEFT PACK ALREADY ON PLACARD. EMERGENCY DECLARED LANDED PBI WITHOUT INCIDENT. AIRCRAFT WAS FLOWN TO MIA FOR REPAIRS. ELBOW DUCT FROM AIR CYCLE MACHINE TURBINE TO REHEATER SHOWED SIGNS OF LEAKAGE WHERE TURBINE INLET TEMPERATURE BULB SCREWED IN. REPLACED TURBINE UNIT TEMPERATURE CONTROL MPN22023234, LOW LIMIT VALVE, AND THE TEMPERATURE BULB MPN2340239001 FOR THE RIGHT PACK. REPLACED AIR CYCLE MACHINE MPN6806404 SERIES 4 FOR THE LEFT PACK. SYSTEM GROUND CHECKED NORMAL.

Part: PDU — LEAKING (LE SLAT) · airframe 80,599 hrs · 16,188 cycles

MIA - CREW REPORTED ELECTRIC BURNING SMELL AND HAZE IN COCKPIT. LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND THE LEFT WING POWER DRIVE UNIT DRIVE MOTOR PUMP LEAKING HYDRAULIC FLUID. REPLACED BOTH HEAT EXCHANGERS, RECIRCULATION FANS, AND SLAT POWER DRIVE UNIT SHAFT SEALS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: STRINGER — CORRODED (BS 421-443 S36R) · airframe 78,744 hrs · 15,807 cycles

AFW FORWARD CARGO STRINGER WAS CORRODED. AREA OF DISCREPANCY WAS 22 INCHES IN LENGTH. REPAIRED PER SRM 53-00-03 2R2 WITH EXCEPTIONS PER MRB 767 3258.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,744 hrs · 15,807 cycles

AFW FORWARD CARGO STRINGER WAS CORRODED. AREA OF DISCREPANCY WAS 21 INCHES IN LENGTH. REPAIRED PER SRM 53-00-03 2R2 WITH EXCEPTIONS PER MRB 767 3256.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,744 hrs · 15,807 cycles

AFW FORWARD CARGO STRINGER WAS CORRODED. AREA OF DISCREPANCY WAS 22 INCHES IN LENGTH. REPAIRED PER SRM 53-00-03 2R2 WITH EXCEPTIONS PER MRB 767 3260.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SFO - EMERGENCY EXIT LIGHTS AT LEFT AND RIGHT OVERWING INOPERATIVE. REPLACED BATTERY PACK AT M1209 FOR INOPERATIVE EMERGENCY EXIT LIGHTS AT LEFT AND RIGHT OVERWING. SYSTEM GROUND CHEKCED NORMAL OPERATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

JFK- EMERGENCY FLOOR PATH LIGHT AT SEAT 22B IS MISSING LENS AND BULBS ARE INOPERATIVE. REPLACED LENS AND BULBS FOR EMERGENCY FLOOR PATH LIGHT AT SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LAX - EMERGENCY LIGHTS FROM SEAT 2B TO 9B, 2H TO 9H AND 20H TO 26H INOPERATIVE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS FROM SEAT 2B TO 9B, 2H TO 9H AND 20H TO 26H. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SWITCH — INOPERATIVE (ZONE 100)

LAX - INFLIGHT T0019/15 LEFT ENGINE ROLLED BACK AT 300 FEET. FULL CONTROL MOVED CUTOFF AND RUN. ENGINE NORMAL AT TOUCHDOWN. THROTTLES PARKED UP THROUGH TOUCHDOWN AND ROLLOUT. REVERSED NORMALLY. REPLACED LEFT HAND ENGINE FUEL FILTER AND LEFT AND RIGHT HAND FUEL CUT OFF SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS FROM SEATS 31A TO 37A INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR EMERGENCY LIGHTS FROM SEATS 31A TO 37A. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS)

JFK - LEFT HAND EMERGENCY LIGHTS AT ROWS 31 TO 37 INOPERATIVE. REPLACED BATTERY PACK AND BATTERY CONTROL MODULE AT ROW 35AB FOR LEFT HAND EMERGENCY LIGHTS AT ROWS 31 TO 37. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: OVEN — MALFUNCTIONED (GALLEY)

LAX - FLT 33 - HEAVY SMOKE EMERGING FROM THE FIRST CLASS GALLEY. MAINTENANCE FOUND RESIDUE IN CONTACT WITH THE OVEN HEATING ELEMENT. REMOVED AND REPLACED OVEN. GROUND OPS CHECK NORMAL. (M)

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED LEFT OVERWING EMERGENCY EXIT LIGHTS BALLAST. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLASHLIGHT — INOPERATIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, FORWARD CENTER RIGHT FLIGHT ATTENDANT EMERGENCY EXIT FLASHLIGHT INOPERATIVE. REPLACED FORWARD CENTER RIGHT FLIGHT ATTENDANT EMERGENCY EXIT FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONTROLLER — FAILED (CABIN PRESSURE)

JFK - FLT 15 - EN ROUTE JFK-LAX - SHORTLY AFTER TAKEOFF EICAS MESSAGE INDICATED NO NR 1 AND 2 CABIN ALTIMETER INDICATION. MANUAL MODE ALLOWED LIMITED VALVE CONTROL. RETURNED TO JFK AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 AUTO PRESSURE CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — DEFECTIVE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEAT 33H INOPERATIVE. REPLACED CONNECTOR AND PINS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — DISCONNECTED (CABIN)

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

Part: PHONE — SHORTED (CABIN)

ICT - FLT 201 - EN ROUTE CREW REPORTED ELECTRICAL BURNING SMELL IN AFT CABIN. LANDED ICT WITHOUT INCIDENT. REPLACED AT&T PASSENGER PHONE. SYSTEM GROUND CHECK NORMAL OPERATION. PHONE SHORTED OUT. (M)

Part: WIRE — BROKEN (ROW 17 HJ)

SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT 17 HJ TO 30 HJ INOPERATIVE. REPAIRED WIRES AT 17 HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SOCKET — DEFECTIVE (LT EMER EXIT)

SFO - DURING OVERNIGHT MAINTENANCE, LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT SOCKET IN LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — LOOSE (CARGO COMPT)

RDU - FLT 174 - DURING CRUISE, FORWARD CARGO OVERHEAT STATUS MESSAGE AND OVERHEAD LIGHT ILLUMINATED IN FLIGHT. AIR INTERRUPTED BACK TO RDU AND LANDED WITHOUT INCIDENT. NO SIGN OF SMOKE OR HOT CONDITION. SECURED CANNON PLUG ON TEMPERATURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FLOORBEAM — CORRODED (BS 855-999)

AFW - FLOORBEAM AT RBL 33 HAD CORROSION BLENDED BEYOND SRM LIMITS. ROTO-PEEN BLENDED AREAS PER SRM. ALODINED ALL BARE ALUM SURFACES FINISH BLENDED AREAS WITH 2 COATS BMS 10-11 PRIMER. FILL BLENDS WITH BMS PROSEAL 870. (M)

Part: FLOORBEAM — CORRODED (BS 780-920)

AFW - FLOORBEAM AT LBL 11 HAD CORROSION BLENDED BEYOND SRM LIMITS. ROTO-PEEN, BLENDED AREAS PER SRM. ALODINE ALL BARE ALUM SURFACES FINISH BLENDED AREAS WITH 2 COATS OF BMS10-11 PRIMER. FILL BLENDS WITH BMS5-95 PROSEAL 870. (M)

Part: FLOORBEAM — CORRODED (BS 1565)

AFW - FLOORBEAM AT STATION 1565 LBL 77 HAD CORROSION BLENDED BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OUT OF 301 1/2H STAINLESS STEEL .050 INCH THICK. ALODINE ALL BARE ALUMINUM SURFACE FINISH BLEND AND REPAIR PARTS WITH 2 COATS BMS10-11 PRIMER FILL BLENDS WITH BMS5-92. INSTALL REPAIR STRAP WET WITH BMS5-95. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

AFW - FLOORBEAM AT RBL 54 HAS CORROSION BLENDED BEYOND SRM LIMITS. ROTO PEEN BLENDED AREA PER SRM, ALODINED ALL BARE ALUM SURFACES. FINISH BLENDED WITH 2 COATS OF BMS10-11, PRIMER FILL BLENDS WITH BMS 5-95 PROSEAL 870. (M)

Part: FLOORBEAM — CORRODED (BS 266)

AFW - FLOORBEAM AT STATION 266 RBL 26 HAD CORROSION BLENDED BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OUT OF 301.5 INCH STAINLESS STEEL .050 INCH THICK. ALODINE, FINISH BLEND AND REPAIR PARTS WITH 2 COATS OF BMS10-11 PRIMER, FILL BLENDS WITH BMS 5-92. INSTALL REPAIR STRAP WET WITH BMS 5-95 SEALANT. (M)

Part: WIRE — LOOSE (CABIN)

SFO - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY CROSS AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED SPLICE ON FORWARD GALLEY CROSS AISLE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT SIGN AT LEFT AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED EMERGENCY EXIT SIGN WIRE AT LEFT AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: OVEN — DEFECTIVE (GALLEY)

SFO - FLT 0035 - DURING APPROACH TO SFO, ELECTRICAL ODOR NOTED IN CABIN WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT LANDED SFO WITHOUT INCIDENT. REPLACED MID-GALLEY NR 3 OVEN. SYSTEM GROUND CHECKED, NORMAL OPERATION WITH NO ELECTRICAL ODOR NOTED. (X)

Part: IDG — FAILED (LT ENGINE)

ORD - FLT 0682 - LEFT GENERATOR DRIVE LIGHT FLICKERED BEGINNING AND DURING CLIMB-OUT. DRIVE LIGHT CAME ON CONTINUOUSLY AFTER 1.5 HOURS OF FLIGHT. LEFT GENERATOR DRIVE DISCONNECTED. 5383/PLACARDED LT GEN INOP PER MEL 24-1. SERVICED BOTH ENG IDG TO OVERFLOW. APU OIL LEVEL FULL. ACCOMPLISHED MPM 24-01. ENTERED IN MIC. AUTH 4-193DC-B. REMOVED AND REPLACED IDG IAW MM 24-11-01-4-2. OPS CHECK GOOD, LEAK CHK GOOD. DISC GOOD. OPS CHECK GOOD AFTER DISCONNEECT. REMOVED MEL 4-193DC-B AND CLEARED MIC. (X)

Part: WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT FORWARD CROSS AISLE INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT FORWARD CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL WIRE — BROKEN (CABIN)

SFO - DURING OVERNIGHT CHECK, RT FORWARD GALLEY EMERGENCY FLOOR LIGHT FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY RT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)

Part: EEL CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PAX SEAT 20 AB INOPERATIVE. RESERCURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PAX SEAT 20 AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT PAX SEAT 17AB INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PAX SEAT 17AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)