N661GT

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 75,409 hrs · 9,612 cycles

COCKPIT EMERGENCY FLASH LIGHT INOP. R&R BATTERY OPS CHECKED GOOD PER AMM 25-05-03.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 75,254 hrs · 9,572 cycles

EICAS RT BLEED ISOLATION VALVE MESSAGE ON TOUCHDOWN. CHECKED THE RT ISOLATION VALVE, RT BLEED ISOLATION VALVE MESSAGE CLEARED. OPS CHECKED NORMAL IAW AMM 36-11-00.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,204 hrs · 9,563 cycles

L3 AND L4 EMERGENCY LIGHT OUTSIDE WILL NOT STAY LIT. REMOVED AND REPLACED BATTERY ASSY IAW 33-51-07/ 201, OPS CHECKED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,204 hrs · 9,563 cycles

L2 & L4 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LAMPS, OP CHECKED GOOD IAW AMM 33-51-16-201.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 75,106 hrs · 9,546 cycles

THE EXTERIOR EMERGENCY LIGHTS, MID L, TYPE 1, AND SLIDE INOPERATIVE. CHARGED BATTERY PACK M378-EMERGENCY LIGHT (L1089) OP CHECK NORMAL IAW B 767 AMM 33-51-01.</P>)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 75,106 hrs · 9,546 cycles

EMERGENCY LIGHT (EXTERIOR) AFT L DOOR SLIDE (L397) INOPERATIVE. CHARGED EMERGENCY BATTERY PACK M378. EMERGENCY LIGHT L397. OP CHECK NORMAL IAW AMM 33-51-07.</P>)

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,106 hrs · 9,546 cycles

EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BULBS. OPS CHECKED NORMAL IAW AMM 33-51-07.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,034 hrs · 9,528 cycles

EXTERIOR EMERGENCY LIGHTS INOPERATIVE. AT DOORS L2, AND R2. REPLACED THE LAMPS IAW AMM 33-51-16. OPS CHECKED OK.

Part: PUMP — WARNING LIGHT (FUEL BOOST) · airframe 74,999 hrs · 9,522 cycles

RIGHT CENTER FUEL PUMP LOW PRESSURE LIGHT ON. REMOVED AND REPLACED THE FUEL BOOST PUMP AND OPS CHECKED IAW AMM 28-42-00, OPS CHECKED GOOD.

Part: APU — MALFUNCTIONED · airframe 74,970 hrs · 9,516 cycles

DURING LANDING, APU DID NOT START, APU FAULT LIGHT ILLUMINATED. THE APU CONTROL UNIT BITE TEST ACCOMPLISHED IAW AMM 49-61-05. TEST PASSED.

Part: WARNING LIGHT — ILLUMINATED (FUEL PUMP) · airframe 74,970 hrs · 9,516 cycles

RT CENTER FUEL PUMP PRESSURE LIGHT AT ENGINE START.

Part: ACTUATOR — MALFUNCTIONED (LT RAM AIR) · airframe 74,929 hrs · 9,507 cycles

DURING A PREFLIGHT, LEFT PACK TEMP MESSAGE AUTO SELECTED, STANBY OK. REMOVED AND REPLACED THE LT RAM AIR INLET DOOR ACTUATOR IAW AMM 21-53-03, PERFORMED AN OPS TEST OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 74,918 hrs · 9,504 cycles

LEFT PACK TEMP AFTER BLOCK OUT, SWITCHED TO STANDBY IAW QRH. ACCOMPLISHED AMM 21-31-00/501 CABIN PRESSURE CTL TEST & 21-51-00/601 PACK INSPECTION, TESTED OK. CONTROLLER BITE RESET, NO FAULTS.

Part: APU — MALFUNCTIONED · airframe 74,841 hrs · 9,487 cycles

APU FAULTED ON FIRST ATTEMPT AFTER LANDING. SECOND ATTEMPT SUCCESSFUL. PERFORMED APU BITE IAW FIM 49-11 FT 987, OIL PRESSURE, CLEARED FAULT, SYSTEM OK. FIRST START ATTEMPTED GOOD, APU OPS CHECK NORMAL IAW AMM 49-11-00.

Part: ISOLATION VALVE — STICKING (RT A/C PACK) · airframe 74,797 hrs · 9,479 cycles

RIGHT PACK ISOLATION VALVE STICKING. REMOVED AND REPLACED THE RIGHT PACK ISOLATION VALVE IAW AMM 36-11-04. OPS CHECKED OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 74,758 hrs · 9,470 cycles

"APU FAULT" EICAS MESSAGE ON FIRST START ATTEMPT AFTER LANDING. SECOND ATTEMPT WAS SUCCESSFUL, PERFORMED FIM 49-11 FT 987 NO FAULTS FOUND. SYSTEM TEST OK. OPS CHECKED APU NORMAL 05 GOOD STARTS & SYSTEM NORMAL IAW AMM 49-11-00.

Part: ACTUATOR — FAILED (RAM AIR INLET) · airframe 74,758 hrs · 9,470 cycles

LEFT PACK TEMP ILLUMINATED IN FLIGHT. PERFORMED BITE ON LEFT PACK CONTROLLER, FAULTED FOR RAM INLET ACTUATOR. REMOVED AND REPLACED LEFT PACK INLET DOOR ACTUATOR IAW AMM 21-53-03, OPS CHECKED GOOD, NO FAULTS NOTED.

Part: LINE — LOOSE (VALVE SURGE) · airframe 74,716 hrs · 9,460 cycles

APU AUTO SHUTDOWN AT GATE. FOUND SURGE VALVE SENSE LINE LOOSE AT FILTER .TIGHTENED SURGE LINE IAW AMM 49-53-06 1400-009, OPS CHECKED APU IAW AMM 49-00-00. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (LT A/C PACK) · airframe 74,716 hrs · 9,460 cycles

LEFT PACK TEMP EICAS MESSAGE AT FL.390 ACCOMPLISHED QRH PROCEDURE. PERFORMED BITE ON LEFT PACK CONTROLLER, FAULTED THE RAM INLET ACTUATOR. INSPECTED CLEARED AND RESEATED THE CONNECTOR. PERFORMED BITE NO FAULTS NOTED IAW FIM 21-51- F/T 803.

Part: APU — MALFUNCTIONED · airframe 74,677 hrs · 9,454 cycles

APU FAULT, DID NOT START AFTER 3 ATTEMPTS. APU REPLACED IAW AMM 49-11-01, OPS AND LEAK CHECKED OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 74,678 hrs · 9,455 cycles

LEFT PACK TEMP EICAS. LEFT PACK RESET ACCOMPLISHED NO FAULTS NOTED I.A.W AMM 21-62-00&NBSP;</P>)

Part: STARTER — FAILED (APU) · airframe 74,677 hrs · 9,454 cycles

APU INOPERATIVE, FAULT LIGHT ILLUMINATED. REMOVED AND REPLACED APU STARTER MOTOR IAW AMM 49-41-00, OPS CHECKED NORMAL.

Part: WARNING LIGHT — ILLUMINATED (APU) · airframe 74,644 hrs · 9,447 cycles

APU INOPERATIVE FAULT LIGHT ILLUMINATED.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 EXHAUST FAN) · airframe 74,644 hrs · 9,447 cycles

STATUS MESSAGE AFT NR 2 EQUIPMENT EXHAUST FAN 2. PERFORM FIM 21-26 FT 806, NO FAULT NOTED RESET SYSTEM NORMAL.

Part: ISOLATION VALVE — MALFUNCTIONED (LEFT BLEED) · airframe 74,641 hrs · 9,445 cycles

LEFT BLEED ISOLATION VALVE EICAS DISPLAYED DURING LEFT ENGINE SHUTDOWN AT BLOCKS. PERFORMED FIM 36-10 FT 827, AND FOUND HIGH RESITANCE IN VALVE (0.6 TO 0.9 OHM ) OPS CHECKED NORMAL IAW AMM 36-11-04.

Part: ISOLATION VALVE — FAILED (LT ENGINE) · airframe 74,641 hrs · 9,445 cycles

LEFT BLEED ISOLATION VALVE EICAS DISPLAYED DURING LEFT ENGINE SHUTDOWN IN BLOCKS. PERFORMED FIM 36-10 FT827 FOUND HIGH RESISTANCE IN VALVE (0.6 TO 0.9 OHMS) OPERATIONAL CHECK NORMAL IAW MM 36-11-04.

Part: IDG — MALFUNCTIONED (LEFT) · airframe 74,633 hrs · 9,444 cycles

LT. GEN DRIVE DISCONNECT LIGHT INOPERATIVE. TESTED OK. REMOVED AND REPLACED THE LEFT IDG IAW AMM 24-11-01, OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 74,641 hrs · 9,445 cycles

AFTER TAKE OFF, FWD EQPT OVERHEAT DISPLAYED COMPLIED WITH QRH AND WAS ABLE TO CLEAR MESSAGE. PERFORMED EQUIP COOLING TEST IAW MM 21-58-00. SYSTEM CHECKED NORMAL NO FAULTS NOTED.

Part: CONNECTOR — DIRTY (IDG) · airframe 74,606 hrs · 9,435 cycles

DURING ENGINE RUNS, THE RIGHT IDG DISCONNECT LIGHT ILLUMINATED AND WILL NOT RESET. CLEANED THE CONNECTOR AND RECONNECTED IDG IAW AMM 24-11-01. OPS CHEKED NORMAL.

Part: UNKNOWN — NOISE · airframe 74,604 hrs · 9,434 cycles

DURING CLIMB OUT AT 8000 MSL, HEARD A LOUD NOISE, SLIGHT YAW ALL PARAMETERS NORMAL, NO MESSAGES, NORMAL OPS. ACCOMPLISHED TEST, FIVE GROUND TEST MAX POWER ASSURANCE SATISFACTORY IAW AMM 71-00-00-735, PIMU BIT CHECKED GOOD IAW 77-35-00.

Part: STARTER — INOPERATIVE (APU) · airframe 74,571 hrs · 9,427 cycles

APU FAULT EICAS MESSAGE. APU DID NOT START. R & R THE APU STARTER IAW AMM 49-11-01, OPS CHECKED GOOD, NO DEFECT NOTED AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 74,551 hrs · 9,421 cycles

LEFT BLEED ISOLATION VALVE MESSAGE. CYCLED THE LEFT ISOLATION VALVE SWITCH. ISOLATION VALVE OPS NORMAL. NO MESSAGE NOTED IAW 36-10-00.

Part: ACTUATOR — FAULTED (LT A/C PACK) · airframe 74,458 hrs · 9,397 cycles

LT PACK TEMP EICAS, DURING ENGINE START INOPERATIVE. LIGHT ON LT PACK RESET SWITCH(<P>PERFORMED BIT OF L PACK TEMP CONTROLLER, HAS RAM AIR ACTUATOR FAULT IAW FIM 21-51 FT 803, RESET L PACK &AMP; PERFORMED BIT SAT GREEN GO LIGHT ILLUMINATED, FAULTS LIGHT CLEARED, PACK OPS CHECKED GOOD.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 74,400 hrs · 9,384 cycles

STATUS CABIN ALTITUDE AUTO 2. PERFORMED FIM 21-31 FT 803 BITE TEST CHECK BOTH 1 & 2 PRESSURE CONTROLLERS, NO FAULTS SYSTEM OK PER FIM 21-31 FT 803</DIV>)

Part: FAN — FAILED (EQUIPMENT BAY) · airframe 74,268 hrs · 9,359 cycles

FWD EQUIPMENT FAN EICAS MESSAGE DISPLAY. REMOVED AND REPLACED THE FWD EQUIPT EXHAUST FAN IAW AMM 21-58-06. OPS CHECKED NORMAL.

Part: VALVE — FAILED (APU) · airframe 74,243 hrs · 9,355 cycles

APU FAULT AND AUTO SHUTDOWN, APU FAULT ON ECU GEN FILTER. FOLLOWED FIM TASK 49-11, FAULT TREE 969. FOUND SCAVENGE FILTER ELEMENT BAD. R & R IAW AMM 49-29-03-004 001. OPS CHECKED GOOD. INSPECTED MAGNETIC CHIP DETECTOR, NO METAL FOUND IAW 49-27-04-206-0014. R & R THE LOW OIL PRESSURE S/W AND ECU. NO HELP. ORIGINAL ECU REINSTALLED. REMOVED AND REPLACED APU SURGE VALVE, OPS CHECKED IAW 49-53-01, OPS CHECKED GOOD.

Part: STARTER — INOPERATIVE (APU) · airframe 74,174 hrs · 9,341 cycles

APU AUTO SHUTDOWN, PERFORMED FIM 49-11. FAULT TREE 998. NO DEFECTS NOTED, ALL POPOUT INDICATORS FLUSH. R & R THE OIL PRESSURE SCAVANGE FILTER IAW B767 AMM 49-27-03. SUSPECT DIFFERENTIAL PRESSURE SWITCH . DURING TROUBLESHOOTING, FOUND APU STARTER INOPERATIVE. REMOVED AND REPLACED OIL PRESSURE SWITCH AND STARTER. OPS CHECKED NORMAL IAW AMM 49-41-01-401.

Part: GCU — FAILED (LEFT) · airframe 74,183 hrs · 9,345 cycles

DURING CLIMB, THE LEFT GENERATOR EICAS MASSAGE, COMPLIED WITH QRH, AFTER RESET OF THE LEFT GENERATOR, THE OFF EICAS MESSAGE APPEARED AGAIN. TROUBLESHOT IAW FIM 24-20, TASK 804 AND FOUND THE LEFT GENERATOR GCU FAILED. R & R THE LEFT GCU & OPS CHECKED GOOD IAW MM 24-22-02.

Part: DRIVE UNIT — MALFUNCTIONED (WX RADAR) · airframe 74,133 hrs · 9,334 cycles

WEATHER RADAR LEFT AND RIGHT SYSTEMS STATUS MESSAGES. REMOVED AND REPLACED WEATHER RADAR DRIVE UNIT AND OPS CHECKED GOOD IAW AMM 34-43-05.

Part: IDG — LACK OF LUBE (RIGHT) · airframe 74,112 hrs · 9,329 cycles

EICAS FOR RT GENERATOR DRIVE AND DRIVE LIGHT ILLUMINATED IN FLIGHT. IT WENT OFF A FEW MOMENTS LATER. FOUND THE RIGHT IDG NEEDING OIL. SERVICED IAW MM 12-13-03. IDG TEST RAN OK IAW MM 71-00-00.

Part: IDG — UNDERSERVICED (RIGHT) · airframe 74,112 hrs · 9,329 cycles

EICAS FOR RT GENERATOR DRIVE, AND GENERATOR DRIVE LIGHT ILLUMINATED IN FLIGHT. IT WENT OFF A FEW MINUTES LATER. FOUND THE RIGHT IDG LOW ON OIL. SERVICED IAW AMM 12-13-04.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE EEC) · airframe 74,064 hrs · 9,320 cycles

AFTER PUSH BACK, RT ENGINE EEC EICAS MESSAGE, RETURN TO BLOCKS. ACCOMPLISHED TEST OF RIGHT EPCS/PIMU EEC IAW AMM 77-35-00. ALL CHECKED GOOD.

Part: SEAL — MISSING (LT ENGINE) · airframe 73,838 hrs · 9,271 cycles

LEFT ENGINE ABRADABLE SHROUD SMOOTHER SEAL MISSING AT SMALL AREAS, LOCATED AT 6 O' CLOCK. CLEANED AND REPAIRED ABRADABLE SHROUD IAW AMM 72-32-00-308-001-H00.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN TEMP) · airframe 73,861 hrs · 9,275 cycles

MID CABIN TEMP MESSAGE, OPS CHECKED IAW FIM TASK 21-61-804. OPS CHECKED OK, MESSAGE CLEARED.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 73,687 hrs · 9,243 cycles

MID CABIN TEMP ADVISORY MESSAGE ON GROUND WITH APU BLEED ON. CLEANED MID CABIN FILTERS PERFORMED BITE ON AUX ZONE TEMP CONTROLER HAD MID CABIN FAULT CLEARED FAULT AND TESTED OK IAW AMM 21-61-00.

Part: FILTER — DIRTY (CABIN TEMP) · airframe 73,583 hrs · 9,222 cycles

MID CABIN ZONE TEMP INOPERATIVE. CLEANED ALL AIRCRAFT ZONE TEMP SENSOR FILTERS IAW AMM 21-61-09. MID CABIN ZONE TEMP NORMAL, NO FAULTS IAW AMM 21-61-00 .

Part: STRUCTURE — DAMAGED (RT WING SLAT) · airframe 73,568 hrs · 9,219 cycles

RIGHT WING LE SLAT LOWER TRAILING EDGE DAMAGED.

Part: CONTROLLER — MALFUNCTIONED · airframe 73,557 hrs · 9,217 cycles

STATUS MESSAGE FOR RT ENGINE HPSOV INDICATED. REMOVED & REPLACED THE HIGH PRESSURE CONTROLLER ASSY. SYS OPS CHECKED GOOD IAW AMM 36-11-08.

Part: CONNECTOR — NOT SEATED · airframe 73,516 hrs · 9,207 cycles

EICAS MESSAGE RT ENGINE HPSOV , QRH PERFORMED. FOUND THECONNECTOR D10984 NOT SEATED , INSPECTED THE CONNECTOR, RESEATED AND TIGHTENED OPS CHECKED IAW AMM 36-23-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (SHUTOFF VALVE) · airframe 73,510 hrs · 9,206 cycles

EICAS MESSAGE FOR RT ENG HPSOV. QRH PERFORMED. CLEAR MESSAGE IAW AMM 31-40-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 73,510 hrs · 9,206 cycles

EICAS MESSAGE FOR RT SIDE WINDOW. QRH PERFORMED, RAN BITE CHECK OF THE RT SIDE WINDOW HEAT CONTROL. NO DEFECTS NOTED IAW AMM 30-41-00.

Part: WINDOW — MALFUNCTIONED (R3) · airframe 73,516 hrs · 9,207 cycles

EICAS MESSAGE FOR RT SIDE WINDOW, QRH PERFORMED. R & R THE R3 WINDOW IAW AMM 56-11-10 OPS CHECKED GOOD.

Part: AUTOPILOT SYS — MALFUNCTIONED (RIGHT) · airframe 73,505 hrs · 9,204 cycles

WITH RT AUTOPILOT ON, DESCENDING FROM 360 TO 280 IN VNAV. AUTOPILOT DID NOT WORK PROPERLY AND STOP (1) RATE OF CLIMB (2) CAPTURE ALT OF 280. AUTOPILOT DID FLY THROUGH 280 TO APROX. FL279-2788, BEFORE DISCONNECTION OF AP TO STOP DESCENT AND LEVEL OFF AND RETURN TO FL280. TASK 22-00-02-742 REVIEWED FLT FAULT HISTORY THE MCDP NO FLIGHT FAULT RECORDED, RAN PITCH CHECK 4, 8, 30 CHECK AND 40 CHECK IAW MM 22-10-00, OPS CHECK NORMAL.

Part: WARNING MESSAGE — FALSE INDICATION (TEMP CONTROLLER) · airframe 73,480 hrs · 9,201 cycles

EICAS MESSAGE FOR MID CABIN TEMP, MID CABIN CONTROLLER INOPERATIVE. RESET CABIN TEMP CONTROLLER IAW AMM 21-61-00. OPS CHECKED GOOD.

Part: VALVE — FAILED (FUEL CROSSFEED) · airframe 73,461 hrs · 9,196 cycles

FUEL MIGRATION FROM RT MAIN TANK TO LT MAIN TANK THROUGHOUT FLIGHT. FUEL WAS EQUAL AT TAKE OFF AND ON BLOCK IN. LT MAIN TANK 8.2, RT MAIN TANK 6.8. FMC FUEL BURN EQUAL. REMOVED AND REPLACED TWO CROSSFEED VALVES IAW AMM 28-22-00, OPS CHECKED NORMAL

Part: CONTROLLER — FAULTED (CABIN TEMP) · airframe 73,441 hrs · 9,193 cycles

MID CABIN TEMP EICAS. BITE CHECKED THE AUX TEMP CONTROLLER IAW AMM 21-61-00. MID CABIN TEMP FAULT. CLEARED FAULT & OPS TESTED GOOD. NO FAULTS. GREEN GO LIGHT. COOLING PACK SYSTEM OPS GOOD IAW AMM 21-51-00.

Part: SLIDE — UNWANTED DEPLOY (R4 DOOR) · airframe 73,397 hrs · 9,184 cycles

R4 DOOR EMERGENCY SLIDE DEPLOYED. REMOVED AND REPLACED THE SLIDE PACK IAW AMM 25-66-01.

Part: REGULATOR VALVE — MALFUNCTIONED (A/C PACK) · airframe 73,355 hrs · 9,177 cycles

PACK AUTO CONTROL DRIVES TEMP TO FULL COLD -15C. REMOVED & REPLACED THE TRIM AIR PRESSURE REGULATOR VALVE OPS & LEAK CHECKED GOOD IAW AMM 21-61-06-404-020.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 73,334 hrs · 9,172 cycles

TEMP NOT CONTROL IN AUTO. REMOVED AND REPLACED THE ZONE TEMP CONTROLER IAW AMM 21-61-03 OPS TEST OK.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 73,301 hrs · 9,165 cycles

DURING ENGINE RUN, EICAS INDICATION HARD FAULT FOR CABIN ALT AUTO 1. REMOVED AND REPLACED AUTO 1 CABIN PRESSURE CONTROLLER IAW AMM 20-40-01, 21-31-02, AND FIM 21-31. CHECKED SATISFACTORY.

Part: WIRE — UNSECURE · airframe 73,301 hrs · 9,165 cycles

1ST CLASS WIRE NOT SECURE. BIRD CAGGED CHAFES IN THREE PLACES ON PSU. REARRANGED WIRING TO PREVENT CHAFING AND SECURED IAW SWPM 20-10-12.

Part: PLENUM — DAMAGED (HEAT EXCHANGER) · airframe 73,301 hrs · 9,165 cycles

LEFT AC BAY AIR PLENUM FLANGE HOLES ARE DAMAGED FLANGES FOR HEAT EXCHANGER. REMOVED AND REPLACED THE AIR PLENUM IAW AMM 21-51-02-404-019.

Part: SEAL — WORN (ACCESS PANEL) · airframe 73,301 hrs · 9,165 cycles

RIGHT WING FUEL ACCESS PANEL WORN. REMOVED AND REPLACED THE ACCESS PANEL SEALS IAW AMM 28-11-10-900-001 THROUGH STEP 1.

Part: HOUSING — CRACKED (AIR FILTER) · airframe 73,301 hrs · 9,165 cycles

FWD CARGO AFT L/S AIR FILTER HOUSING CRACKED AT CORNER. REPAIRED FWD CARGO AFT L/S AIR FILTER HOUSING IAW B767-300 SRM 51-70-02 FIG 21</P>)

Part: DOOR — OUT OF ADJUST (LAVATORY) · airframe 73,301 hrs · 9,165 cycles

A4 LAVATORY WASTE BIN FLAPPER DOOR DOES NOT CLOSE AS REQUIRED. ADJUSTED HARDWARE ON THE FLAPPER DOOR IAW SRM 51-40-02-06-0.

Part: SEAL — WORN (FUEL CELL) · airframe 73,301 hrs · 9,165 cycles

CENTER FUEL TANK PANEL HAS ONE WORN SEAL. REMOVED ABD REPLACED THE FUEL TANK PANEL SEAL IAW AMM 28-11-10-908-001 THROUGH STEP 1.

Part: SEAL — WORN (ACCESS PANEL) · airframe 73,301 hrs · 9,165 cycles

LT WING FUEL ACCESS PANEL SEAL WORN. REMOVED AND REPLACED THE SEAL IAW AMM 28-11-10-908-001 THROUGH STEP 1.

Part: SEAL — LOOSE (APU INLET DOOR) · airframe 73,301 hrs · 9,165,491 cycles

APU INLET DOOR SEAL ASSY IS LOOSE. REMOVED AND REPLACED APU INLET DOOR SEAL ASSY IAW AMM 49-15-09.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,301 hrs · 9,165 cycles

EMERGENCY LIGHTS FROM SEAT ROW 29 TO 42 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-07-422.

Part: SCREEN — DAMAGED (FUEL CELL) · airframe 73,301 hrs · 9,165 cycles

FUEL TANK SCREEN IN THE RT WING DAMAGED. REMOVED AND REPLACED SCAVENGE SYSTEM PICK-UP SCREEN. SEALED SCREEN TO LOWER SKIN OF FUEL TANK IAW AMM 28-11-00-300-060 AND CLAMPED SCREEN TO THE SYSTEM LINES IAW 20-10-11-964-001.

Part: EXTINGUISHER — CORRODED (LAVATORY) · airframe 73,301 hrs · 9,165 cycles

AUTOMATIC FIRE EXTINGUISHER FOR LAVATORY WASTE CAN CORRODED ALONG SEAM. AFT LAV CENTER LH(<P>REMOVED AND REPLACED AUTOMATIC FIRE EXTINGUISHER FOR LAV WASTE CAN FOR AFT CENTER L/H LAV IAW B767 AMM 26-24-01-400-801</P>)

Part: FIRE SEAL — DAMAGED (LAVATORY) · airframe 73,301 hrs · 9,165 cycles

LAVATORY WASTE BASKET FIRE SEALS ARE DAMAGED INBD UPPER AND LOWER SEALS. REMOVED AND REPLACED THE SEALS IAW SRM 51-40-02-06-0 PAGE 2.

Part: OXYGEN GEN — INOPERATIVE (LAVATORY) · airframe 73,301 hrs · 9,165 cycles

R1 LAVATORY OXYGEN MASK DEPLOYED AND GENERATOR. REMOVED AND REPLACED THE OXYGEN GENERATOR AND REPACKED OXYGEN MASKS IAW AMM 35-21-13-402-324-002 AND AMM 35-21-13-502-353-002.

Part: WIRE — CHAFED (RT NACELLE) · airframe 73,301 hrs · 9,165 cycles

WIRES RUBBING ON RT ENG INBD SIDE. REMOVED AND REPLACED THE WIRE IAW SWPM 20-10-11 AND SWPM 26-11-21. OPS CHECKED GOOD IAW AMM 26-11-00.

Part: SUPPRESSION SYS — MALFUNCTIONED · airframe 73,301 hrs · 9,165 cycles

CARGO FIRE BOTTLE DISCHARGE LIGHT IS ON. TROUBLESHOT IAW FIM TASK 26-23 FAULT TREE 813. RESET DISCHARGE LINE PRESSURE SWITCHES 5661 AND 5662. RETESTED CARGO FIREX SYSTEM IAW AMM 26-23-00. TESTED SATISFACTORY.

Part: BLADE — DAMAGED (NR 2 FAN) · airframe 73,301 hrs · 9,165 cycles

NR 2 ENGINE FAN BLADE NR 23 SMALL NICK LE ONE INCH FROM TIP. REMOVED THE NICK ON THE BLADE IAW AMM 72-31-02-308-045-H00, FOUND TO BE WITHIN LIMITS IAW AMM 72-31-02-308-045H00 FIG 801.

Part: BATTERY — INOPERATIVE (MASTER) · airframe 73,301 hrs · 9,165 cycles

ACFT BATTERY NOT CHARGING PROPERLY POSSIBLE OVERCHARGE CONDITION. REMOVED AND REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER IAW AMM 24-31-01, AND 24-31-62. MAIN BATTERY OPS CHECKED GOOD.

Part: EXTINGUISHER — CORRODED (LAVATORY) · airframe 73,301 hrs · 9,165 cycles

AFT LAVATORY AUTOMATIC FIRE EXTINGUISHER FOR WASTE CAN HAS CORROSION. REPLACED THE FIRE EXTINGUISHER IAW AMM 26-24-01-400-801.

Part: CIRCUIT CARD — OUT OF POSITION (FIRE DETECTION) · airframe 73,301 hrs · 9,165 cycles

DURING ENGINE RUN, EICAS INDICATION HARD FAULT, FOR LT ENG FIRE LOOP 2. TROUBLESHOT IAW FIM 26-11-00 AND WDM 26-11-11. FOUND FIRE DETECTOR AND OVERHEAT CARDS SWAPPED. CARDS INSTALLED PROPERLY, OPS CHECKED IAW AMM 26-11-00. OPS CHECKED GOOD.

Part: PANEL — BENT (NR 1 NACELLE) · airframe 75,301 hrs · 9,165 cycles

#1 ENG O/B COWL CENTER ATTACH POINT, HINGED ACCESS PANEL BENT HAS SHARP EDGES FWD END (NRI3277)(<P>REMOVED DAMAGE FORM FWD EDGE OF ACCESS HINGED ACCESS PANEL IAW SRM 54-42-01. 80" MATERIAL REMOVED FROM EDGE. AREA FOUND TO BE WITHIN LIMITS IAW 54-42-01 FIG 101 DETAIL IV.</P>)

Part: SCREEN — DAMAGED (FUEL CELL) · airframe 73,301 hrs · 9,165 cycles

1 EA FUEL TANIC SCREEN INT THE LT WING DAMAGED. REMOVED AND REPLACED SCAVENGE SYSTEM PICK-UP SCREENS ON R/H. SEALED SCREEN TO LOWER SKIN OF FUEL TANK IAW AMM 28-11-00-300-060 AND CLAMPED SCREEN TO THE SYSTEM LINES IAW AMM 20-10-11-964-001.

Part: TRANSMITTER — FAILED (APU OIL QTY) · airframe 73,301 hrs · 9,165 cycles

DURING ENG RUN, EICAS INDICATION HARD FAULT, AFTER VISUAL OIL LEVEL VERIFICATION OF SERVICING APU OIL QTY. REMOVED AND REPLACED APU OIL QTY TRANSMITTER IAW AMM 49-94-03. OPS CHECK GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 35) · airframe 73,301 hrs · 9,165 cycles

SEAT 35 GFD FAILED OXYGEN MASK DROP. REMOVED AND REPLACED OXYGEN MASK IAW AMM 25-23-01. OPS CHECKED GOOD IAW AMM 35-21-00.

Part: CONTROLLER — MALFUNCTIONED (NR 1 ENGINE PRV) · airframe 73,301 hrs · 9,165 cycles

NR 1 ENG PRV CONTROLLER FOR PRESSURE WAS NOT BETWEEN 40-67. REMOVED AND REPLACED THE NR 1 ENG PRV CONTROLLER IAW AMM 36-11-19.

Part: DOOR — LOOSE (GALLEY WASTE) · airframe 73,301 hrs · 9,165 cycles

AFT GALLEY WASTE BIN DOOR DOES NOT CLOSE AS REQUIRED. SECURED HARDWARE IAW SRM 51-40-02-06-0.

Part: CIRCUIT CARD — OUT OF POSITION (FIRE DETECTION) · airframe 73,301 hrs · 9,165 cycles

DURING ENGINE RUNS, EICAS INDICATION HARD FAULT (L ENG OH LP1). TROUBLESHOT IAW FIM 26-11-00 AND WDM 26-11-12 FOUND FIRE DETECTOR AND OVERHEAT CARDS SWAPPED CARD INSTALLED PROPERLY OPERATION CHECK PERFORMED IAW IAW AMM 26-11-00 OPERATION CHECK GOOD.

Part: DOOR — MISSING (OXYGEN MASK) · airframe 73,301 hrs · 9,165,360 cycles

LAVATORY OXYGEN MASK DOOR MISSING. INSTALLED THE DOOR IAW SMR 51-40-02-060.

Part: HOUSING — CRACKED (FILTER) · airframe 73,301 hrs · 9,165 cycles

FWD CARGO AFT FILTER HOUSING CRACKED AT CORNER. REPAIRED FWD CARGO AFT AIR FILTER HOUSING IAW SRM51-70-03 FIG21.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 73,301 hrs · 9,165 cycles

L2 DOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED L2 DOOR EMERGENCY EXIT LIGHT IAW AMM 33-51-10.

Part: GROUND STUD — CORRODED (LAVATORY) · airframe 73,301 hrs · 9,165 cycles

AFT CENTER LAV R/S SHELF WHERE AUTOMATIC FIRE EXTINGUISHER MOUNTS TO LAV WASTE CAN GROUND SCREW CORRODED. REMOVED AND REPLACED GROUND SCREW IN AC-4 LAV AUTOMATIC FIRE EXTINGUISHER IAW B767 SRM 51-40-02-060 AND B767 AMM 20-11-00-910-002.</P>)