N454PA

Part: FIRE WARNING — FALSE ACTIVATION (ZONE 200) · airframe 97,024 hrs · 16,197 cycles

CREW REPORTED DURING CRUISE, CARGO FIRE MAIN DECK ZONE 11 EICAS MSG. FOUND MESSAGE 26330/26331 NOT ACTIVE. CREW CONFIRMED NO ACTUAL SMOKE/FIRE ON MAIN DECK. CARGO CONSISTS OF FLOWERS. SMOKE DETECTOR TEST PASSED PER AMM 26-14-01. NO FURTHER DEFECTS NOTED

Part: EXHAUST FAN — ODOR (ZONE 200) · airframe 97,012 hrs · 16,195 cycles

SMOKE SMELL IN COCKPIT. R & R COOLING EXHAUST FAN PER AMM 21-58-01. OPS CHK NORMAL.

Part: MODULE — FAILED (EXTINGUISHER) · airframe 94,118 hrs · 15,766 cycles

ARCING SOUND HEARD FROM OVERHEAD PANEL ACCOMPANIED MOMENTARILY BY FIRE LIGHTS IN APU FIRE SWITCH.(<P>REMOVED AND REPLACED ENG/ APU FIRE EXT MODULE PER B747 AMM 26-10-02. R/R CIRCUIT CARD A22 REF AMM 26-10-01. OPS TEST GOOD, NO DEFECTS NOTED AT THIS TIME.&NBSP;</P>)

Part: PCB — DAMAGED (ZONE 200) · airframe 93,725 hrs · 15,709 cycles

APU FIRE SWITCH ILLUMINATED INTERMITTENTLY FOR SEVERAL HOURS. A FEW TIMES FIRE APU WARNING EICAS MESSAGE ALSO DISPLAYED FOR A SPLIT SECOND. ALSO, CAN HEAR APU FIRE SWITCH DISCONNECTING.(<P>REMOVED AND REPLACED AFOLTS CARD A22 PER AMM 26-10-01/401. INSPECTED FIRE CONTROL MODULE WIRE BUNDLES, NO CHAFFING NOTED. ALL ELECTRICAL CONNECTORS SECURE. INSPECTED FIRE LOOPS IN APU COMPARTMENT, NO DEFECTS NOTED.&NBSP;</P>)

Part: FIRE WARNING — FALSE ACTIVATION (APU BAY) · airframe 92,581 hrs · 15,539 cycles

APU FIRE MSG. COMPLIED WITH QRH 8.1. DISCHARGED APU FIRE BOTTLE(<P>DEACTIVATED APU AND TRANSFER TO DMI 217433 PER MEL 26-22-01 CAT C DUE DATE 5OCT24. R/R APU FIRE EXT BOTTLE &AMP; GND CHECK GOOD PER AMM 26-22-01/401 &AMP; AIPC 26-22-01-02A. DMI 217433 CLOSED.</P>)

Part: OIL SYSTEM — PRESSURE LOSS (NR 1 ENGINE) · airframe 91,676 hrs · 15,397 cycles

ENG 1 IFSD (OIL QTY & PRESSURE LOSS). R & R #1 ENG PER WO 133424. C/W ENG IDLE RUN IAW AMM 71-00-00, OPS CHECK GOOD. NO FAULTS OR LEAKS.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 89,962 hrs · 15,141 cycles

RHW I/B AFT FLAP FOUND DELAMINATION. PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.C. NO FURTHER DEFECTS NOTED</P>)

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 89,962 hrs · 15,141 cycles

EMP - L/H HORI STAB MOST O/B WEB FOUND CRACK(<P>WEB REPLACED AS PER SRM 51-10-02 AND NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 89,962 hrs · 15,141 cycles

EMP - L/H HORI STAB MOST O/B WEB LOWER CHORD FOUND CRACK(<P>LOWER CHORD REPLACED AS PER SRM 51-10-02 AND NEW LOWER CHORD HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW LOWER CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 89,962 hrs · 15,141 cycles

EMP L/H HORI STAB MOST O/B WEB UPPER CHORD FOUND CRACK(<P>UPPER CHORD REPLACED AS PER SRM 51-10-02 AND NEW UPR CHORD HOLES TRANSFERED AS PER SRM 51-40-05 AND NEW UPR CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: CLOSEOUT PANEL — CRACKED (BS 1241 LBL77-99) · airframe 89,962 hrs · 15,141 cycles

M/D STA 1241 LBL 77-99 CLOSEURE PNL FOUND CRACK(<P>CLOSURE PNL REPLACED AS PER SRM 51-10-02 AND NEW PANEL HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW PANEL INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 89,962 hrs · 15,141 cycles

EMP L/H HORI STAB MOST O/B T/E WEDGE 'U' CHANNEL FOUND CRACK(<P>CRACK CHANNEL REPLACED AND INSTALLED AS PER RI-55-10-16734 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 89,962 hrs · 15,141 cycles

LHW O/B FORE FLAP FOUND  DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 89,962 hrs · 15,141 cycles

RHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.C. NO FURTHER DEFECTS NOTED</P>)

Part: BEAM — CORRODED (BS 1780-1920) · corrosion level 2 · airframe 89,962 hrs · 15,141 cycles

AFT CARGO DOOR INNER SURFACE LOWER DOOR LINER CLOSE OUT BEAM SURFACE CORR FROM STA 1780-1920 SEVEN PLACES(<P>BEAM 6 LOCATIONS CORROSION REMOVED WITHIN SRM 52-30-02-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS, 1 LOCATION REPAIRED AS PER RI-52-30-16736 REV A AT STA 1820-1840. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — PUNCTURED (NR 2 NACELLE) · airframe 89,962 hrs · 15,141 cycles

#2 ENG R/H CORE UPPER SECTION 10" (COUNT FROM AFT) EXT SURFACE FOUND PUNCH HOLE(<P>#2 ENG R/H CORE COWL UPPER SECTION TITANIUM FAIRING EXTERNAL DOUBLER REPAIRED AS PER SRM 54-45-01-2R-7 REPAIR 7. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 89,962 hrs · 15,141 cycles

LHW O/B FORE FLAP FOUND  DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA IAW SRM 51-70-07 PAR 5.A. NO FURTHER DEFECTS NOTED.</P>)

Part: STRUCTURE — CRACKED (BS 1240) · airframe 89,962 hrs · 15,141 cycles

FX AIRCON BAY LH STA 1240 LBL 105" O/B CENTER SECTION LOWER CHORD CRACK(<P>CRACK CHORD REPLACED AS PER SRM 51-10-01 AND NEW CHORD HOLE TRANSFERRED AS PER SRM 51-40-05 AND NEW CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: LAMP — BROKEN (EMERGENCY LIGHT) · airframe 89,962 hrs · 15,141 cycles

FOUND EMERGENCY LIGHTS L5735, L1853 AND L1854 LAMP BROKEN(<P>EMERGENCY LIGHTS L5735, L1853 AND L1854 LAMP REPLACED AND TEST IS NORMAL IAW AMM 33-51-00</P>)

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 89,962 hrs · 15,141 cycles

EMP R/H HORI STAB MOST O/B WEB LOWER CHORD FOUND CRACK(<P>LOWER CHORD REPLACED AS PER SRM 51-10-02 AND NEW LOWER CHORD HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW LOWER CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: WEB — UNKNOWN (BS 1840-1860) · airframe 89,962 hrs · 15,141 cycles

MDDR 177930 REF EA-4453A0008 REV 0 AFT CARGO COMPARTMENT LATERAL BEAM UPPER FLOOR WEB AT STA 1840-1860 LBL 45.5 PERMANENT REPAIR (WITHIN 2000FC AFTER REPAIR OR WITHIN 24 MONTHS WHICHEVER OCCURS EARLIER(<P>WEB REPLACED AS PER SRM 51-10-02 AND NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: FITTING — CRACKED (BS 1480) · airframe 89,962 hrs · 15,141 cycles

L/H BS 1480 LONGERON EXTENSION FITTING 1EA CRACK WAS FOUND AT EXISTING TRIMMED OFF AREA APPROX 5/16 IN LENGTH(<P>LONGERON EXTENSION FITTING REPLACEMENT CARRIED OUT AS PER ATLAS AIR EO 4453A818 R19 PART 3. NO FURTHER DEFECTS NOTED</P>)

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 89,962 hrs · 15,141 cycles

EMP - R/H HORI STAB MOST O/B WEB UPPER CHORD CRACK(<P>UPPER CHORD REPLACED AS PER SRM 51-10-02 AND NEW UPPER CHORD HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW UPPER CHORD INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 89,962 hrs · 15,141 cycles

EMP RH HORI STAB MOST O/B WEB FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER SRM 55-10-09-2R-13 REPAIR 13 FIG 201. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DENTED (VERTICAL STAB) · airframe 89,962 hrs · 15,141 cycles

EMP - VERT FIN R/H SURFACE MOST UPPER AREA FWD FIXED PANEL FOUND DENT MARK(<P>DENT AREA REPAIRED AS PER RI-55-00-16750 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 89,962 hrs · 15,141 cycles

EMP R/H HORI STAB MOST O/B T/E WEDGE 'U' CHANNEL CRACK(<P>'U' CHANNEL REPLACED AS PER RI-55-10-16735 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: ENGINE — SMOKE (NR 3) · airframe 89,576 hrs · 15,081 cycles

ON CLIMBOUT THROUGH 800FT EICAS "CREW REST SMOKE". NOTICED HAZE COMING FROM CREW REST AREA.  MESSAGE DISAPPEARED ON DECENT THROUGH 3500FT.(<P>REPLACED #3 ENGINE THEN OPERATIONAL AND LEAK CHECKS NORMAL IAW W/C 71-099-02-01 AND SMELL CHECK NORMAL IN COCKPIT AND CREW REST PER AMM 71-00-00.&NBSP;</P>)

Part: WATER SEPARATOR — UNKNOWN (UNKNOWN) · airframe 89,508 hrs · 15,073 cycles

SMOKE CREW REST EICAS IMMEDIATELY AFTER ROTATION AND A SMELL OF SOMETHING BURNING. EICAS AND SMELL WENT AWAY AFTER 1-2 MINUTES. REPEAT WRITE-UP, REF LP 1723752.(<P>NO FAULTS FOUND IN CMC. PERFORMED FIRE SET SYS GROUND TEST PER AMM 26-11-00, TEST PASS. PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-56, NO DEFECTS NOTED OR FOUND. REMOVED AND REPLACED #1 PACK WATER SEPARATOR COALESCER BAG PER AMM 21-51-05/201, OPS CHECK GOOD.</P>)

Part: WEB — CRACKED (BS 1840 LBL47) · airframe 85,956 hrs · 14,495 cycles

AFT CGO STA 1840 L/H LBL 47 (NEAR L/H O/B CGO TRACK) FLOOR TORQUE BOX SKIN CRACKED.(<P>AFT CARGO COMPT BETWEEN STA 1840 & 1860 LBL 50, LATERAL BEAM INSTL WEB P/N: 65B06314-250 PUNCTURE HOLE AREA REPAIRED IAW RI NO. RI-53-00-16013 REV.A. THIS REPAIR IS A TIME-LIMITED REPAIR.

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

L/H STAB TIP FAIRING RIB #9 (COUNT FROM FWD) FOUND CRACKED(<P>HORI STAB TIP RIB - STRUCTURE WITH 11 RIBS-REPAIR</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

NOSE NLG W/W FWD L/H CORNER SKIN DOUBLER AREA 1EA FASTENER HOLE FOUND CRACKED ON THE SECOND LAYER (CHORD) (COUNT FROM LOWER) STA 240.(<P>NOSE NLG W/W FWD L/H CORNER SKIN DOUBLER AREA ATTACH CHORD 1EA FASTENER HOLE CRACK REPAIRED.</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

LHW O/B MID FLAP CTR L/E FOUND DELAMINATION (127" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A&NBSP;</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

LHW O/B FORE FLAP L/E FOUND DELAMINATION (77" TO O/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A&NBSP;</P>)

Part: NONE — NONE · airframe 82,337 hrs · 13,903 cycles

LH WING L/E CAVITY LES 884.47 (NEAR REFUEL PNL) SUPPORT BEAM FOUND CRACK(<P>LH WING FIXED L/E LOWER SURFACE PANEL SUPPORT BEAM REPAIR AT ILES 848.5-908.5</P>)

Part: NONE — NONE · airframe 82,337 hrs · 13,903 cycles

NOSE NLG W/W FWD L/H AND R/H CORNER MOD DOUBLERS SHORT EDGE MARGINS(<P>NOSE NLG W/W FWD L/H AND R/H CORNER MOD DOUBLERS SHORT EDGE MARGINS REPAIRED</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

RHW O/B FORE FLAP L/E FOUND DELAMINATION (127" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

RHW O/B FORE FLAP L/E FOUND DELAMINATION (24" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A&NBSP;</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

RHW I/B FORE FLAP L/E CTR AREA FOUND DELAMINATION (155" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A&NBSP;</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

NOSE NLG W/W FWD RH CORNER SKIN DOUBLER AREA 1EA FASTENER HOLE FOUND CRACKED ON THE NO.2 AND NO.3 LAYER (CHORD AND BULKHEAD CHORD)(COUNT FROM LOWER) STA 240(<P>NOSE NLG W/W FWD RH CORNER SKIN DOUBLER AREA ATTACH CHORD AND BULKHEAD CHORD 1EA FASTENER HOLE CRACK REPAIRED</P>)

Part: NONE — NONE · airframe 82,337 hrs · 13,903 cycles

LHW I/B MID FLAP O/B RIB AFT AREA ANGLE BRACKET FOUND CRACKED(<P>FABRICATE THE REPLACEMENT CLIP FROM 7075T651 BARE PLATE</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

RHW O/B FORE FLAP L/E FOUND DELAMINATION (71" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A&NBSP;</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

RHW I/B MID FLAP L/E FOUND DELAMINATION (3" TO O/B, 18" TO AFT)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A&NBSP;</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

LHW O/B MID FLAP L/E FOUND DELAMINATION (235" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A&NBSP;</P>)

Part: NONE — NONE · airframe 82,337 hrs · 13,903 cycles

M/D - BALL MAT PNL FOUND BROKEN AT STA 1860-1920 RBL 55-77 BOTH LH AND RH FWD CORNER(<P>M/D - STA 1860-1920 RBL 55-77 CASTER PANEL DOUBLER REPAIRED AS PER RI-25-50-15357 REV.B.</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

L/H STAB TIP FAIRING RIB #2 (COUNT FROM FWD) FOUND CRACKED(<P>HORI STAB TIP RIB - STRUCTURE WITH 11 RIBS-REPAIR</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

RHW O/B MID FLAP L/E FOUND DELAMINATION (116" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A&NBSP;</P>)

Part: NONE — NONE · airframe 82,337 hrs · 13,903 cycles

AIRCRAFT DAMAGE LOG CONTROL ITEM D16-001 - RH NOSE GEAR DOOR STA 292 DENT 1"X0.0312" A/Y=32 WITHIN LIMITS PER SRM 52-80-01-1A-1 DETAIL V.(<P>SOLID RIVET INSTALLED AS PER SRM 52-80-01-1A-1 ALLOWABLE DAMAGE 1 REV.93, 20OCT2021.</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

#4 PYLON VALVE ACCESS PNL #482EL 1EA HOLE FOUND ELONGATION(<P>#4 PYLON V/V ACCESS PNL #482EL FASTENER HOLE REPAIR</P>)

Part: NONE — NONE · airframe 82,337 hrs · 13,903 cycles

R/H BLG I/B W/W DOOR I/B EDGE FOUND DEFORMED(<P>R/H AFT MLG O/B AFT SECONDARY DOOR AFT BEAM DEFORMATION REPAIR</P>)

Part: NONE — NONE · airframe 82,336 hrs · 13,903 cycles

#4 ENG R/H CORE COWL EXHAUST LWR EDGE FOUND SEVERAL RIVET HOLES CRACKED.(<P>#4 ENG R/H CORE COWL PRECOOLER EXTERNAL DOUBLER REPAIR.</P>)

Part: NONE — NONE

APU FIRE HANDLE LIGHT FLICKERS AND MAKES CLICKING NOISE WITH NO FIRE WARNING HORN.(<P>FOUND DAMAGED WIRE IN APU COMPARTMENT. APU FIRE DETECTION DEFERRED PER DDG 26-15-01-01B, MDDR 155418.</P> / <P>LP 1488596 - FOUND WIRE DAMAGE AT APU COMPT INSIDE WIRE # W720-452-18R AND N720-451-18R. THEN REPLACED DAMAGED WIRE PER WDM 26-15-11 AND APU FIRE WARN TEST NORMAL PER AMM 26-15-00 MDDR # 155418 CLOSED.</P> / <P>&NBSP;</P>)

Part: SLEEVE — DIM (ZONE 700)

ON 06TH OCTOBER 2021, WE HAVE FOUND ON OUR ASSEMBLY SHOP AN OVERSIZE SLEEVE ITEM 600 ON ATTACHED SKETCH , THIS SLEEVE P/N 65B19933-1 S/N R2018-75406 IS MATCHED SET WITH THE OUTER CYLINDER P/N 161U1505-10 S/N BFG3300 INSTALLED ON THE FRESH OVERHAUL GEAR WLG RH FOR THE N454PA. THE LANDING GEAR WAS OVERHAULED ON 13TH AUGUST 2021. IT MEANS THAT WE HAVE MAKE A MISTAKE BY INSTALLING A STANDARD SLEEVE P/N 65B19993-1 INSTEAD THE OVERSIZE ONE. WE HAVE SENT MEMORANDUM N°37464 REQUEST TO BOEING TO AUTORIZE THIS ASSEMBLY.

Part: MODULE — FAULTED (FIRE WARNING) · 13,707 cycles

INTERMITTENT FIRE BELL/MASTER WARNING IN CLIMB, CRUISE AND DESCENT, NO OTHER INDICATIONS. REMOVED AND REPLACED MAWEA MASTER MODULE A, AND MASTER MODULE B, OPS CHECK GOOD IAW AMM 31-51-00.

Part: PROBE — MALFUNCTIONED (NR 2) · airframe 76,218 hrs · 12,710 cycles

#2 EGT INDICATION ON UPPER EICAS ERRATIC AND CONSTANTLY FLUCTUATING AND GOING BLANK. ENGINE #2 ALL 8 EGT PROBES REPLACED. ENG NR 2 W13 HARNESS ALSO REPLACED. ENG NR 2 RUN TESTED NORMAL IAW AMM 77-21-02.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 74,507 hrs · 12,365 cycles

FOUND EMERGENCY LIGHT POWER PACK FUNCTIONAL FAIL.(<P>IAW AMM 33-51-04-902-001-001 REV 97, REPLACED EMERGENCY LIGHT POWER PACK M5170 AND PERFORMED POWER SUPPLY TEST, THE RESULT WAS SATISFACTORY.&NBSP;</P>)

Part: CONNECTOR — DAMAGED (PUMP MOTOR) · airframe 74,507 hrs · 12,365 cycles

FOUND FUEL BOOST PUMP TANK NO.2-AFT M23 CONNECTOR DAMAGE AT LH W/W.(<P>1) IAW SWPM 20-61-11 REV 72 AND WDM 28-22-33 REV 27, REPLACED FUEL BOOST PUMP TANK NO.2 AFT CONNECTOR (DM23) AT LH WING W/W.</P><P>2) IAW WDM 28-22-33 REV 27, PERFORMED WIRE CONTINUITY CHK AND RESULT IS SATISFIED.</P><P>3) IAW AMM 28-22-03-704-091-002 REV 97, PERFORM FUEL BOOST PUMP TANK NO.2 AFT M23 OPERATIONAL TEST AND RESULT WAS SATISFACTORY.</P>)

Part: CONNECTOR — DAMAGED (PUMP MOTOR) · airframe 74,507 hrs · 12,365 cycles

DAMAGE: FOUND THE CONNECTOR DAMAGE OF MOTOR -OVRD/JTSN 3 AFT, EQUIPMENT NO:M226.(<P>1) IAW SWPM 20-61-11&NBSP; REV 72 AND WDM 28-31-26 REV 27, REPLACED MOTOR-OVRD/JTSN 3 AFT CONNECTOR DM226 AT R/H W/W AND THE CONDITION CHECKED NORMAL.</P><P>2) IAW WDM 28-31-26 REV 27, PERFORM WIRE CONTINUITY CHECK AND RESULT IS SATISFIED.</P><P>3) IAW AMM 28-31-01-704-021-002 REV 97, PERFORMED NO. 3 OVRD/JTSN &AMP; PUMP TEST AND THE RESULT WAS SATISFACTORY.</P>)

Part: CONNECTOR — DAMAGED (BOOST PUMP) · airframe 74,507 hrs · 12,365 cycles

FOUND FUEL BOOST PUMP TANK NO. 3-AFT M31 CONNECTOR DAMAGE AT R/H W/W.(<P>1) IAW SWPM 20-61-11 REV. 72 AND WDM 28-22-34 REV. 27, REPLACED FUEL BOOST PUMP TANK NO. 3-AFT CONNECTOR DM31 AT R/H W/W AND CONDITION CHECKED NORMAL.</P><P>2) IAW WDM 28-22-34 REV 27, PERFORM WIRE CONTINUITY CHK AND RESULT IS SATISFIED.</P><P>3) IAW AMM 28-22-03-704-091-002 REV 97, PERFORM FUEL BOOST PUMP TANK NO. 3-AFT M31 OPERATIONAL TEST AND RESULT WAS SATISFACTORY.</P>)

Part: FLOORBEAM — CORRODED (BS 2300) · airframe 74,507 hrs · 12,365 cycles

CORROSION ON THE ANGLE OF FLOOR BEAM CAP AT STA 2300, NEAR LBL 11.(<P>ACCOMPLISHED EI NO. T2020A53M-265 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SHEAR TIE — CORRODED (BS 1777) · airframe 74,507 hrs · 12,365 cycles

FOUND SHEAR TIE CORROSION AT STA 1777, LBL 107 AND LBL 110.(<P>ACCOMPLISHED EI NO. T2020A53M-146 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SEAT TRACK — CRACKED (BS 1920) · airframe 74,507 hrs · 12,365 cycles

FOUND SEAT TRACK CRACK AT STA 1920 RBL 98, M/D FLOOR.(<P>ACCOMPLISHED REPAIR IAW SRM 53-60-52-01-1 REV. 87 AND EI NO. T2020A53M-164 REV. 1 AND BOEING DWG NO. 65B38251 SH 62 REV. A, SH 66 REV. -, SH 67 REV. A. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: FLOORBEAM — CORRODED (BS 1740) · airframe 74,507 hrs · 12,365 cycles

FOUND CORROSION AT STA 1740 LBL 110. M/D FLOOR STRUCTURE UPPER CAP.(<P>REMOVE DAMAGED PART IAW SRM 51-40-02 REV. 87. INSTALL NEW PART IAW SRM 51-40-02 REV. 87 AND EI NO. T2020A53M-262 REV.1 AND DWG NO. 65B17764 SHEET 4, REV. E AND DWG NO. 14641941 SHEET 79, REV. D. JOB COMPLETED.</P>)

Part: CONNECTOR — DAMAGED (PUMP MOTOR) · airframe 74,507 hrs · 12,365 cycles

DAMAGE: FOUND THE CONNECTOR DAMAGE OF MOTOR-OVRD/JTSN 2 FWD, EQUIPMENT NO. 222.(<P>1) IAW SWPM 20-61-11 REV 72 AND WDM 28-31-23 REV 27, REPLACED MOTOR-OVRD/JTSN 2 FWD CONNECTOR (DM222) AT LH WING W/W.</P><P>2) IAW WDM 28-31-23 REV 27, PERFORM WIRE CONTINUITY CHK AND RESULT IS SATISFIED.</P><P>3) IAW AMM 28-31-01-704-021-002 REV 97, PERFORMED NO.2 FWD OVRD/JTSN PUMP TEST AND THE RESULT WAS SATISFACTORY.</P>)

Part: CONNECTOR — CRACKED (PUMP MOTOR) · airframe 74,507 hrs · 12,365 cycles

CRACK - FOUND JTSN/OVRD CTR RH (M225) PUMP CONNECTOR CRACK.(<P>1) IAW SWPM 20-61-11 REV 22 AND WDM 28-31-21 REV 27, REPLACED CONNECTOR DM225 OF JTSN/OVRD CTR RH W/W AND THE CONDITION CHECKED NORMAL.</P><P>2) IAW WDM 28-31-21 REV 29, PERFORM WIRE CONTINUITY CHK AND RESULT IS SATISFIED.</P><P>3) IAW AMM 28-31-00-715-151 REV 97, PERFORMED CTR RH OVRD JETTISON PUMP OPERATIONAL TEST, THE RESULT WAS SATISFACTORY.</P>)

Part: SKIN — CHAFED (RT AILERON) · airframe 74,507 hrs · 12,365 cycles

CHAFING AILERON, R/H WING INBD AILERON OTBD SIDE WBL 515 AREA.(<P>REMOVE THE CHAFING MATERIAL AND CLEAN. MEASURE THE DAMAGE AREA (L = 0.8", W = 0.2" AT AFT EDGE, AT OTBD EDGE, AT R/H WING INBD AILERON UPPER SKIN PNL) BOND REPAIR PLIES USE WET LAYUP WITH RESIN. CURE AT 150 DEGREES F FOR 180 MINUTES AND MAINTAIN A MINUMUM VACUUM PRESSURE AT 22. IAW 747-400F SRM 57-60-01-2R-1, REFER TO SRM 51-70-06-0G-0 REV. 87. CONDITION CHECK SATISFACTORY.</P>)

Part: FLOORBEAM — WORN (BS 1380) · airframe 74,507 hrs · 12,365 cycles

WORN DAMAGE IN FASTENER HOLES OF MAIN DECK FLOOR BEAM UPPER CHORDS AND INTERCOSTAL AT STA 1380, RBL 11.(<P>ACCOMPLISHED EI NO. T2020A53M-154 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: CONNECTOR — DAMAGED (PUMP MOTOR) · airframe 74,507 hrs · 12,365 cycles

DAMAGE: FOUND THE CONNECTOR DAMAGE OF MOTOR-OVRD/JTSN 2 AFT, EQUIPMENT NO. M223.(<P>1) IAW SWPM 20-61-11 REV 72 AND WDM 28-31-25 REV 27, REPLACED MOTOR-OVRD/JTSN AFT CONNECTOR (DM223) AT L/H WING W/W.</P><P>2) IAW WDM 28-31-25 REV 27, PERFORM WIRE CONTINUITY CHK AND RESULT IS SATISFIED.</P><P>3) IAW AMM 28-31-01-704-021-002 REV 97, PERFORMED NO. 2 AFT OVRD/JTSN PUMP AND THE TEST RESULT WAS SATISFACTORY.</P>)

Part: FLOORBEAM — DENTED (AFT CARGO BAY) · airframe 74,507 hrs · 12,365 cycles

DENT - WEB, AFT CARGO FLOOR STRUCTURE AT STA 1673 RBL 16.(<P>ACCOMPLISHED JOB IAW EI NO. T2020A53M-111 REV. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.&NBSP;</P>)

Part: SKIN — DENTED (RUDDER) · airframe 74,507 hrs · 12,365 cycles

DENT - SKIN, V. STAB LEFT UPPER RUDDER EXTERNAL SURFACE SKIN DENT AT RUD STA 282.(<P>CUT OUT THE DAMAGED MATERIAL AND CLEAN. MEASURE THE DAMAGED AREA (L = 1.5", W = 0.7", D =3, PLIES. 52.5" FROM AFT EDGE. 22.5" FROM UPPER EDGE AT RUD STA 282) BOND THE REPAIR PLIES USE PREPREG LAYUP WITH FILM ADHESIVE. CURE AT 260 DEGREES F FOR 130 MINUTES AND MAINTAIN A MINIMUM PRESSURE AT 22 IN/HG IAW B747-400 SRM 55-40-01-2R-0. REFER TO SRM 51-70-07-0G-0 REV. 87. CONDITION CHECK WAS SATISFACTORY.</P>)

Part: CONNECTOR — DAMAGED (PUMP MOTOR) · airframe 74,507 hrs · 12,365 cycles

CRACK: FOUND JTSN/OVRD CTR LH (M224) PUMP CONNECTOR CRACK.(<P>1) IAW SWPM 20-61-11 REV 72 AND WDM 28-31-22 REV 27, REPLACED JTSN/OVRD CTR LH PUMP CONNNECTOR (DM224) AT LH W/W.</P><P>2) IAW WDM 28-31-22 REV 27, PERFORMED WIRE CONTINUITY CHK AND RESULT IS SATISFIED.</P><P>3) IAW AMM 28-31-00-715-151 REV 97, PERFORMED CTR LH OVRD/JTSN PUMP OPERATIONAL TEST, THE RESULT WAS SATISFACTORY.</P>)

Part: CONNECTOR — DAMAGED (PUMP MOTOR) · airframe 74,507 hrs · 12,365 cycles

DAMAGE: FOUND THE CONNECTOR DAMAGE OF MOTOR-OVRD/JTSN 3 FWD EQUIPMENT NO.M227.(<P>1) IAW SWPM 20-61-11 REV 72 AND WDM 28-31-2 REV 27, REPLACED MOTOR-OVRD/JTSN 3 FWD CONNECTOR DM227 AT RH W/W AND CONDITION CHECKED NORMAL.</P><P>2) IAW WDM 28-31-24 REV 27, PERFORM WIRE CONTINUITY CHK AND RESULT IS SATISFIED.</P><P>3) IAW AMM 28-31-01-704-021-002 REV 97, PERFORMED NO.3 FWD OVRD/JTSN PUMP TEST AND THE RESULT WAS SATISFACTORY.</P>)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 74,507 hrs · 12,365 cycles

TEST FAIL: FOUND EMERGENCY BATTERY PACK M5168 CAN NOT STAY ON 15 MINS.(<P>1) IAW AMM 33-51-04-002-009-001 REV 97, REMOVED EMERGENCY BATTERY POWER PACK ASSY M5168.</P><P>2) IAW AMM 33-51-04-402-012-001 REV 97, INSTALLED EMERGENCY BATTERY POWER PACK ASSY M5168.</P><P>3) IAW AMM 33-51-04-402-012-001 REV 97, STEP D PERFORMED POWER SUPPLY TEST AND THE RESULT WAS SATISFACTORY.</P>)

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 73,023 hrs · 12,104 cycles

LOW OIL QUANTITY NR 1 ENGINE. REMOVED AND REPLACED THE NR 1 ENGINE. C/W PER WORK CARD 71044-02-01. OPS CK NORMAL.

Part: WINDOW — CRACKED (CABIN) · airframe 71,740 hrs · 11,853 cycles

RIGHT SIDE CREW REST PASSENGER WINDOW CRACKED.&NBSP;&NBSP;(<P>REMOVED AND REPLACED RIGHT SIDE CREW REST PASSENGER WINDOW, OUTER PANE IAW AMM 56-21-01.&NBSP;</P>)

Part: JUMPER — DAMAGED · airframe 68,293 hrs · 11,258 cycles

EQUIPMENT COOLING MESSAGE. INSTALLED A JUMPER IAW DDG 21-58-07A, MESSAGE CLEARED.

Part: CASTER — DAMAGED (BS 1780-1840) · airframe 67,088 hrs · 11,032 cycles

MAIN DECK CARGO BALL MAT CASTER SUPPORT BASE FOUND BROKEN AT BS 1780 TO 1840, RBL 31 TO 56, THE CASTER SUPPORT BASE WAS REPAIRED IAW EO 4425A500, REV 1.

Part: FRAME — CHAFED (NR 2 NACELLE) · airframe 67,088 hrs · 11,032 cycles

NR 2 ENGINE RT CORE COWL INNER WALL FRAME FOUND CHAFED. REPAIRED IAW E0-1971A169.

Part: HOUSING — DAMAGED (CARGO DOOR SILL) · airframe 67,088 hrs · 11,032 cycles

MAIN DECK CARGO DOOR SILL HANDLING CASTER HOUSING FOUND DAMAGED. REPAIRED.

Part: STIFFENER — CRACKED (APU FIREWALL) · airframe 67,088 hrs · 11,032 cycles

APU FIREWALL FWD FACE NR 2 STIFFENER, RBL 32 FOUND CRACKED AT BS 2658. THE STIFFENER WAS REPAIRED IAW RL-53-83-12420, REV A.

Part: SKIN — SCRATCHED (BS 1860) · airframe 67,088 hrs · 11,032 cycles

EXTERNAL SKIN AT BS 1860 BETWEEN STRINGERS 46L & 47L SCRATCHED. THE SKIN WAS REPAIRED.

Part: CARGO NET — TORN (BS 1980) · airframe 67,088 hrs · 11,032 cycles

BULK CARGO, BS 1980, LT CARGO NET TORN REPAIRED IAW CMM 25-50-00, REV 33, AND RI-25-50-12411, REV A.

Part: FRAME — CRACKED (BS 2669) · airframe 67,088 hrs · 11,032 cycles

APU BAY FRAME AT BS 2669.52 CRACKED. THE FRAME WAS REPAIRED IAW SRM 51-70-11, FIG 1.

Part: SPLICE — CHAFED (BS 1232-1232) · airframe 67,088 hrs · 11,032 cycles

FUSELAGE BS 1232 FOUND CHAFED. REPAIRED IAW RI-53-00-12422, REV B.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 67,088 hrs · 11,032 cycles

RIGHT HORIZONTAL STAB LWR HSS 327 FOUND DENTED. THE SKIN WAS BLENDED AND REWORKED IAW HX-55-10-12428, REV A.

Part: SKIN — CHAFED (NR 2 NACELLE) · airframe 67,088 hrs · 11,032 cycles

NR 2 ENGINE, RT CORE COWL PRECOOLER EXHAUST DUCT INLET CASE FOUND CHAFED. REPAIRED IAW EO 4471A029, REV 4.

Part: SEAT TRACK — DEFORMED (BS 1840) · airframe 67,088 hrs · 11,032 cycles

M/D BALL MAT STA 1780 TO 1840 RBL 13 TO 31 FWD LH REPAIRED AREA FOUND DEFORM(<P>M/D STA 1780 TO STA 1840 RBL 13" TO RBL 31" BALL MAT PANEL LHS SUBJECT RAIL REPLACED IAW SRM 51-10-02</P>)

Part: TORQUE BOX — PUNCTURED (BS 1660-1680) · airframe 67,088 hrs · 11,032 cycles

AFT CARGO BETWEEN BS 1660 AND 1680, LT FLOOR TORQUE BOX METAL PANEL PUNCTURED. REPAIRED IAW RI-51-00-12419, REV A.

Part: SPLICE — CHAFED (BS 1230) · airframe 67,088 hrs · 11,032 cycles

FUSELAGE SPLICE FITTING AT BS 1230 FOUND CHAFED. REPAIRED IAW RI-53-00-12422, REV B.

Part: WARNING MESSAGE — ILLUMINATED (STARTER) · airframe 66,522 hrs · 10,939 cycles

EICAS MESSAGE FOR STARTER CUTOUT AT START OF TAKEOFF.

Part: FIRE DETECTOR — WARNING MESSAGE (NR 1 NACELLE) · airframe 61,160 hrs · 9,964 cycles

NR 1 ENGINE FIRE LOOP B STATUS MESSAGE. REMOVE AND REPLACED THE UPPER AFT DETECTOR ASSY IAW AMM 26-11-02. OPS CHECKED GOOD, NO FAULTS.

Part: DETECTOR — FAULTY (COCKPIT) · airframe 60,889 hrs · 9,921 cycles

EICAS EQUIPMENT COOLING MSG DISPLAYED. FOLLOWED FIM TASK 21-58-02-102-035. REMOVED, CLEANED AND REINSTALLED FLIGHT DECK FLOW DETECTOR IAW MM 21-58-02. GROUND OPS CHECK NORMAL. REF LP 78029, REPLACED FLIGHT DECK LOW FLOW DETECTOR AND OPERATES NORMAL.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 60,534 hrs · 9,863 cycles

UPPER DECK EMERGENCY LIGHT INOPERATIVE, REAR LIGHT ASSY. T/S FOUND EMERGENCY LIGHT POWER SUPPLY AT FAULT BS 590, RT EQUIPMENT M5169 IAW WDM 33-51-71, PAGE 1. REPLACED WITH SERVICEABLE POWER SUPPLY ASSY. OP'S CHECKED NORMAL IAW AMM 33-51-04.

Part: FITTING — CRACKED (BS 1480) · airframe 59,326 hrs · 9,659 cycles

LONGERON EXTENSION FITTING HAD ONE CRACK FOUND ON RT BS 1480, LONGERON EXTERSION FITTING APPROXIMATELY .3125" IN LENGTH. REPAIRED IAW EO:4453A818, PART 2 AND PART 4.

Part: SKIN — CRACKED (BS 2231) · airframe 59,326 hrs · 9,659 cycles

L5 DOOR CUTOUT, BS 2231, STR 21L TO STR 22L REVEAL SKIN FOUND CRACKED. L5 ENTER DOOR BS 2231, STR 22L REVEAL DOUBLER CRACK AREA REPAIRED IAW SRM 53-60-15-2R-3, REPAIR 3 AND ATLAS EO4453B178.

Part: PANEL — CRACKED (BS 600-660) · airframe 59,326 hrs · 9,659 cycles

FWD CARGO BS 600-660 CTR BALL MATERIAL PANEL UPPER SURFACE FOUND CRACK. FWD CARGO BS 600-660 CTR BALL MATERIAL PANEL UPPER SURFACE CRACKED AREA REPAIRED IAW EO: 4425A467, REV O.

Part: FLOOR PANEL — DAMAGED (BS 1740-1840) · airframe 59,326 hrs · 9,659 cycles

BS 1740-1840, LBL 35-70, FLOOR PANEL FOUND DAMAGED. FLOOR PANEL FABRICATED AND REPLACED IAW R1-53-65-11224, EO 4453B180.

Part: FITTING — CRACKED (BS 1480) · airframe 59,326 hrs · 9,659 cycles

LONGERON EXTENSION FITTING ONE CRACK WAS FOUND ON RT BS 1480, LONGERON EXTENSION FITTING APPROXIMATELY .3125" LENGTH. REPAIRED IAW EO: 4453A818 PART 1 AND PART 3.

Part: FLOOR PANEL — DAMAGED (BS 1740-1860) · airframe 59,326 hrs · 9,659 cycles

FLOOR PANEL BS 1740-1860, RBL 35-70 FOUND DAMAGED. FLOOR PANEL FABRICATED AND REPLACED IAW R1-53-65-11224, EO4453B180.

Part: SEAT TRACK — CORRODED (BS 1870 - 1946) · corrosion level 2 · airframe 59,326 hrs · 9,659 cycles

CABIN BS 1900-1920, RBL 11.33" SEAT TRACK FOUND CORROSION. CABIN-BS 1870 TO 1946.45, RBL 11.33" SEAT TRACK REPAIRED IAW RI: RI-53-65-11220, REV A AND EO: 4453B 176, REV O.

Part: FLOOR PANEL — DAMAGED (BS 1840-1940) · airframe 59,326 hrs · 9,659 cycles

BS 1840-1940, LBL 35-70, FLOOR PANEL FOUND DAMAGED. FLOOR PANEL FABRICATED AND REPLACED IAW R1-53-65-11224, EO 4453B180.

Part: FRAME — CHAFED (NR 2 NACELLE) · airframe 59,326 hrs · 9,659 cycles

NR 1 LEFT CORE COWL NR 2 FRAME FOUND CHAFING NR 1 LT CORE COWL NR 2 FRAME CHAFING MARK AREA REPAIRED IAW NR; RE 71-13-11226, REV A, EO 44TSA.61 REV 0.

Part: TIRE — DAMAGED (MLG) · airframe 57,946 hrs · 9,444 cycles

AFTER TAKEOFF, UNABLE TO RAISE GEAR. BODY GEAR ADVISORY MESSAGE ALONG WITH GEAR TILT ADVISORY MESSAGE. IN WORK DURING THE CURRENT AOG EVENT NR 11 TIRE REPLACED IAW MM 32-45-01 AND FOUND CONDUIT DAMAGED. REPLACED CONDUIT IAW MM 32-13-00. PERFORMED GEAR RETRACTION IAW MM, OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,777 hrs · 9,400 cycles

ON CHECK, FOUND CREW EMERGENCY LANDING LIGHT L1382 DIM, CREW EMERGENCY LIGHT L1382. REPLACED THE LAMP AND CHECKED OK IAW AMM 33-51-00.

Part: ACTUATOR — LEAKING (RT MLG) · airframe 57,041 hrs · 9,271 cycles

DURING CRUISE, AN EICAS MESSAGE HYD QTY LOW1, COMPLETED CHECK LIST. LATER SYS1 QTY WENT TO ZERO. EICAS MESSAGE HYD SYS PRESS 1, COMPLETED CHECK LIST. LATER HAD AN EICAS MESSAGE HYD SYS 1 OVERHEAT, COMPLETED CHECK LIST. FOUND HYD LEAK FROM RT MLG WW TRUCK POSITION ACTUATOR FUSE. RIGHT O-RING AND BACK UP RING OF POSITION ACT FUSE. THEN NR 1 HYD SYS LEAK CHECK OK IAW AMM 32-13-24-501.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 568,119 hrs · 9,237 cycles

DURING CRUISE FLIGHT, IDS DU STATUS MESSAGE, WITH MOMENTARY CAP ND BLANK 30 MINUTES, LATER MSG ERASED, BOTH EVENTS CONTAIN ELECTRICAL BURNING ODOR IN COCKPIT, NO RETURN; AFTER 30 MINUTES AND WORKED NORMALLY,MSG 31186 FOUND UPON ARRIVAL CAPT ND WORKS NORMAL, INSPECTED CAPT'S ND DU AND COOLING SCREEN, NO FAULT FOUND, AS PRECAUTION SWAPPED CAPTAIN`S DISPLAY UNIT WITH LOWER EICAS DISPLAY UNIT BOTH OPERATE NORMAL IAW MM AND NOT EVIDENCE OF BURNING.

Part: COUPLER — DAMAGED (HF COMMS) · airframe 56,597 hrs · 9,202 cycles

RIGHT HF INOPERATIVE, LEFT HF ALREADY DEFERRED, HF DATA RIGHT STATUS MESSAGE. SWAPPED RT HF ANTENNA & NBSP; CABLE FROM CENTER COUPLER BACK TO RT COUPLER AND OPS CHECK GOOD.

Part: INDICATION SYS — MALFUNCTIONED · airframe 56,530 hrs · 9,192 cycles

DURING DECENT FROM FL200, F/O VERTICAL DEVIATION INDICATOR SHOWED 4300 FT LOW WHILE CAPTAIN`S VDI SHOWED 600 FT HIGH. BOTH MARRIED UP WITH SAME INDICATION AT 140000 FEET, COMPLIED WITH AMM 34-12-00. BOTH CAPTAIN'S AND F/O`S ADC CHECKED GOOD.

Part: HINGE — BROKEN (RAM AIR DOOR) · airframe 51,428 hrs · 8,312 cycles

NR 2 PACK STATUS MESSAGE. FOUND NR 2 PACK RAM AIR INLET DOOR HINGE BROKEN. ALSO FOUND INLET DOOR ACTUATION LINK SEPARATED. REMOVED INLET DOOR ASSEMBLY, ACTUATION LINK AND INLET DOOR ACTUATOR IAW CDL 21-62-01.

Part: SEAT TRACK — CRACKED (BS 1560-1580) · airframe 51,372 hrs · 8,302 cycles

MAIN DECK CARGO SEAT TRACK CRACKED BETWEEN BS 1560 - 1580, RBL 75.92. REPAIRED CRACK & ACCOMPLISHED EI NR T2014A53B-358. CONDITION CHECKED NORMAL.

Part: FEEDER CABLE — BURNED (PDU) · airframe 51,372 hrs · 8,302 cycles

FOUND PDU WIRE CABLE ASSY BURN OUT AT MAIN DECK CARGO AT BS 2020 LBL 52, REPLACED PDU CABLE IAW SWPM 20-10-12.

Part: FRAME — CRACKED (BS 1840) · airframe 51,372 hrs · 8,302 cycles

CRACK ON FRAME BS 1840 BETWEEN S11-12R. REPAIRED CRACK AND ACCOMPLISHED EI NR T2014A53B-377, REV 2. CONDITION CHECKED NORMAL.

Part: FRAME — CRACKED (BS 1860) · airframe 51,372 hrs · 8,302 cycles

CRACK ON FRAME, BS 1860 BETWEEN S10-11R. REPAIRED CRACK, ACCOMPLISHED EI NR T2014A53B-378, REV 1. CONDITION CHECK NORMAL.

Part: SEAT TRACK — BROKEN (BS 1640-1680) · airframe 51,372 hrs · 8,302 cycles

MAIN DECK CARGO SEAT TRACK BROKEN BETWEEN BS 1640 TO 1680, LBL 11.33. REPAIRED DAMAGE AREA & ACCOMPLISHED EI NO T2014A53B-344. CONDITION CHECKED NORMAL.

Part: COWLING — DENTED (NR 2 ENGINE) · airframe 46,972 hrs · 7,494 cycles

DURING WALK AROUND INSPECTION IN CVG MAINTENANCE FOUND THE NR 2 ENGINE INLET NOSE COWL LEADING EDGE DENTED (SUSPECTED BIRD STRIKE) AT APPROX 12 O' CLOCK POSITION MEASURING 7.750 INCHES IN LENGTH X 3.0 INCHES WIDTH AND 0.2 INCH DEPTH. AFTER DETAIL VISUAL INSPECTION (10X MAGNIFYING GLASS) IT WAS VERIFIED THAT NO SHARP CREASES AND/OR CRACK CONDITION EXISTS. INLET COWL P/N: 224-2101-543 S/N:2777001. DISPOSITION WAS MADE TO PERFORM TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS.

Part: DOOR — CRACKED (RT WLG) · airframe 45,947 hrs · 7,333 cycles

RIGHT WING LANDING GEAR - SHOCK STRUT INBOARD DOOR FAIRING - LEADING EDGE&NBSP HAS CRACK MEASURING & NBSP;1.437 IN.&NBSP; DAMAGE FOUND TO BE BEYOND THE LIMITS OF SRM 52-80-02, FIGURE 101 ALLOWABLE DAMAGE 4 PER SRM 51-70-02, FIGURE 101 ALLOWABLE DAMAGE GENERAL. PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 OF EO 4452A159 FAA 8110-3 19SEP12&NBSP.

Part: SUPPORT — CRACKED (BS 1920) · airframe 44,582 hrs · 7,077 cycles

MAIN DECK SIDE CARGO DOOR AREA AT BS 1920, SIDEWALL SUPPORT CRACKED AND RIVET SHEARED. TIME LIMITED REPAIR ACCOMPLISHED. REPEAT DETAILED VISUAL INSPECTION REQUIRED PRIOR TO EVERY FLIGHT WITH THE PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 1000 FLIGHT HOURS.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 43,111 hrs · 6,805 cycles

DURING INSPECTION AS REQUIRED BY EO 4453A301 REV C CRACKS WERE FOUND AT 2 FASTENER HOLES AT BS 760 RT TENSION TIE, FORWARD CHANNEL &NBSP; (THE DAMAGE WAS REPAIRED AS IAW STEP 6 OF PART 2 OF EO 4453A301 REV C. PART 2 OF EO 4453A674&NBSP;REQUIRES AND INITIAL INSPECTION AT 20,000 FLIGHT CYCLES AND REPEAT INSPECTIONS AT EVERY 3,000 FLIGHT CYCLES THEREAFTER.)

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 43,111 hrs · 6,805 cycles

DURING INSPECTION AS REQUIRED BY EO 4453A301 REV C A CRACK WAS FOUND AT FASTENER HOLE AT&NBSP; BS 760 LT TENSION TIE, AFT CHANNEL. (THE DAMAGE WAS REPAIRED IAW STEP 6 OF PART 1 OF EO 4453A301 REV C. REPEAT INSPECTIONS ARE REQUIRED IAW PART 2 OF EO 4453A672 WITH INITIAL INSPECTION AT 20,000 FLIGHT CYCLES AND REPEATED EVERY 3,000 FLIGHT CYCLES THEREAFTER.)

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 43,111 hrs · 6,805 cycles

DURING INSPECTION AS REQUIRED BY EO 4453A301 REV C A CRACK WAS FOUND AT 1 FASTENER HOLE ON BS 760 LT TENSION TIE, FORWARD CHANNEL. (THE DAMAGE WAS REPAIRED IAW STEP 6 OF PART 1 OF EO 4453A301 REV C. INITIAL INSPECTION REQUIRED AT 20,000 FLIGHT CYCLES AND REPEAT INSPECTION EVERY 3,000 FLIGHT CYCLES THERE AFTER IAW&NBSP;PART 2 OF EO 4453A673.&NBSP;)

Part: SCOOP — DAMAGED (LT WING) · airframe 42,973 hrs · 6,786 cycles

THE LEFT WING VENT SCOOP INLET AREA WAS FOUND TO BE DAMAGED.&NBSP; (PRELIMINARY INSPECTION REVEALED FATIGUE CRACKS ON VENT SCOOP ASSEMBLY WHICH ARE NOT REPAIRABLE.&NBSP; THE&NBSP; VENT SCOOP ASSEMBLY WILL BE REPLACED&NBSP;ONCE PARTS BECOME AVAILABLE. AIRCRAFT IS AOG.&NBSP;).

Part: PANEL — CRACKED (LT WING) · airframe 42,438 hrs · 6,834 cycles

THE LEFT WING, LOWER, LEADING EDGE PANEL FORWARD OF THE INBOARD FUEL ACCESS DOOR HAS A CRACK MEASURING 3 INCHES LONG. A TIME LIMTED REPAIR WAS ACCOMPLISHED IAW PART 1 OF EO 4457A388 8110-3 DATED 11NOV11 AND SRM 51-10-02.

Part: BEARING — WORN (SPOILER) · airframe 41,007 hrs · 6,450 cycles

DURING INITIAL CLIMB, A RHYTHMIC VIBRATION IN AIRFRAME WAS FELT. ALSO FELT & NBSP; THROUGH LEVEL OFF AND CRUISE. ACCOMPLISHED CONDITIONAL INSPECTION IAW AMM 05-51-38-201 &AMP; SERVICE LETTER 747-SL-02-005-F. NR 4 SPOILER WAS FOUND TO HAVE EXCESSIVE PLAY AND THE RIGHT BODY GEAR STRUT FIXED BRACKET BEARING WAS WORN. THE SPOILER CONTROL PACKAGE WAS REPLACED IAW AMM27-61-05. THE BRACKET WAS ALSO REPLACED IAW AMM 32-14-06. ALL CHECKS WERE NORMAL.

Part: SWITCH — DIRTY (ESCAPE HATCH) · airframe 35,215 hrs · 5,576 cycles

DURING TAKEOFF ROLL RECEIVED STATUS MESSAGE - UPPER DECK ESCAPE HATCH OPEN. UPPER DECK HATCH LINER REMOVED FOR DVI, DOOR FRAME, SKIN, SEAL, AND MECHANISM CHECKED WITH NO DEFECTS FOUND. LINER RE-INSTALLED. DOOR OPEN AND CLOSE WITH MICRO-SWITCH CLEANED AND OPERATIONAL CHECKED PER AMM 52-71-01 OK. MESSAGE ERASED. CONDITIONAL INSPECTIONS ACCOMPLISHED PER AMM 05-51-10 & 05-51-26.

Part: SKIN — DAMAGED (RUDDER) · airframe 33,769 hrs · 5,367 cycles

DAMAGE WAS FOUND TO THE RT UPPER RUDDER EXTERNAL SURFACE MID-AREA WITH DENT 1.0 INCHES IN DIAMETER. PERMANENT REPAIR WAS ACCOMPLISHED BY ENGINEERING ORDER 4455A033. THIS EO IS CLASSIFIED AS "MAJOR" AS DEFINED IN FAR 43 APPENDIX A.

Part: NOZZLE — CRACKED (NR 2 EXHAUST) · airframe 39,448 hrs · 6,525 cycles

NUMBER TWO EXHAUST NOZZLE HAS TWO CRACKS. ENGINEERING ORDER 4478A114 ACCOMPLISHED STOP DRILL AS INTERIM REPAIR AND 3 CYCLE REINSPECTION. NOZZLE MUST BE REPLACED BEFORE NEXT A CHECK. THIS EO APPROVED BY FAA 8110-3 DATED 11 JAN 2010.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,769 hrs · 5,367 cycles

DAMAGE WAS FOUND TO THE FUSELAGE SKIN RIGHT BS 2655. INTERIM REPAIR WAS PERFORMED AS PER SRM 53-00-00 AND REPEAT INSPECTION EVERY 6,000 FLIGHT CYCLES PER ENGINEERING ORDER 4453A316. THIS REPAIR IS CLASSIFIED AS "MAJOR" AS DEFINED IN FAR 43 APPENDIX A.

Part: DOOR — DAMAGED (APU BAY) · airframe 33,769 hrs · 5,367 cycles

DAMAGE WAS FOUND ON LEFT APU COMPARTMENT DOOR, A "MAJOR REPAIR" WAS PERFORMED BY ENGINEERING ORDER 4452A075 AS PER SRM 52-00-00 FIGURE 201.

Part: FLAP — DELAMINATED (WING) · airframe 33,769 hrs · 5,367 cycles

DURING AIRCRAFT C-CHECK INSPECTION DENT/DELAMINATION WAS FOUND ON THE LT & RT TRAILING EDGE FLAPS AND THE LT INBOARD AILERON. PERMANENT REPAIR WAS ACCOMPLISHED PER SRM 57-53-01 FIGURE 201 REPAIR 1 TABLE 1, SRM 51-70-17 FIGURE 5 AND SRM 57-60-01 FIGURE 201 AS PER ENGINEERING ORDER 4457A222. THIS EO IS CLASSIFIED AS "MAJOR" PER FAR 43 APPENDIX A.

Part: SEAL DEPRESSOR — DAMAGED (CARGO BAY) · airframe 32,249 hrs · 5,156 cycles

AFT LOWER CARGO SEAL DEPRESSOR DAMAGED AT UPPER AFT CORNER. ACCOMPLISHED PART 1 OF EO 4453A275 SINCE REPAIR DEVIATES FROM SRM EO WAS APPROVED VIA FAA FORM 8110-3 ISSUED 30 AUG 2009. A VISUAL INSPECTION IS REQUIRED EVERY FLIGHT CYCLES UNTIL PERMANENT REPAIR CAN BE COMPLETED AT AIRCRAFT'S NEXT A-CHECK.

Part: TIRE — SEPARATED (LANDING GEAR) · airframe 31,951 hrs · 5,115 cycles

AIR TURNBACK DUE TO GEAR MONITOR AND GEAR TILT EICAS MESSAGE CAUSED BY NUMBER 12 TIRE CAP SEPARATION. REPAIRS ACCOMPLISHED PER AMM, WDM, SRM. TIRE REPLACED PER AMM 32-45-01.

Part: FAIRING — DAMAGED (ZONE 300) · airframe 31,300 hrs · 5,019 cycles

WHILE ATTEMPTING TO REPLACE THE MISSING LEFT OUTBOARD HORIZONTAL STABILIZER STATIC DISCHARGER, MAINTENANCE FOUND A PORTION OF THE STABILIZER TIP FAIRING DAMAGED. A REPLACEMENT WAS RECEIVED AND INSTALLED PER SRM 51-10-02.

Part: WARNING MESSAGE — FALSE ACTIVATION (FIRE BOTTLE) · airframe 30,709 hrs · 4,934 cycles

EICAS MESSAGE BTL LOW ENGINE A APPEARED ON CLIMB-OUT AT 1000 FEET, ALSO BOTTLE A DISCHARGE LIGHT ON OVERHEAD ALSO ILLUMINATED. AT APPROX 20,000 FEET ALL LIGHTS EXTINGUISHED. "REMOVED BOTTLE, WEIGHED AND REINSTALLED. OPENED MEL 26-20-1. SQUIB TEST ACCOMPLISHED AND VERIFIED SQUIB INTEGRITY."

Part: PANEL — DAMAGED (MAIN DECK) · airframe 29,425 hrs · 4,750 cycles

DURING LOADING OF MAIN DECK DAMAGE WAS FOUND ON THE CEILING PANEL BETWEEN STA 620 AND 720 AT RBL 17.0. DAMAGE WAS FOUND TO BE OVER LIMIT EO 4425A100 WAS ISSUED CONSISITING OF A TEMPORARY REPAIR AND DVI EACH A-CHECK ACFT DEPARTED.

Part: DISPLAY — INOPERATIVE · airframe 27,115 hrs · 4,408 cycles

CAPTAIN'S PFD WENT BLANK DURING A POWER INTERRUPTION AT PUSHBACK. CYCLED EIU LEFT, CENTER, RIGHT CIRCUIT BREAKERS. OPERATION NORMAL AFTERWARDS IAW MM 31-61-00."

Part: TIE ROD — BROKEN (RT WING MLG WW) · airframe 26,844 hrs · 4,367 cycles

ON WALKAROUND FOUND A TIE ROD AND CLEVIS BROKEN ON THE RT WING GEAR WHEEL WELL AT WBL 238.38 FIXED TRAILING EDGE UPPER RIB. REMOVED DAMAGED PARTS AND VISUALLY INSPECTED AREA IN ACCORDANCE WITH EO 4457A140. (A)

Part: NOZZLE — CRACKED (NR 2 ENGINE) · airframe 26,726 hrs · 4,346 cycles

DURING WALK AROUND A 15" LONG CRACK WAS FOUND ON THE NR 2 ENGINE EXHAUST NOZZLE ON THE UPPER RIGHT QUADRANT. AN INTERIM REPAIR WAS ACCOMPLISHED PER EO 4478A069 AND 8110-3 DATED 27 APRIL 2008 ISSUED.

Part: RCCB — MULTIPLE FAIL · airframe 25,661 hrs · 4,180 cycles

AIR TURN BACK DUE TO MULTIPLE ELECTRICAL FAILURES. NR 1 COMMUNICATION PANEL, E/E COOLING CARD, T/E FLAPS/FLAPS PRIMARY, ELEC BCU 1, ALL FUEL CROSSFEED MSG'S, CREW O2 LOW, YAW DAMPER LOWER, FUEL TANK TO ENGINE, TORQUE LIMITER, FUEL PUMP 2 STATUS MESSAGES APPEARED. FWD FUEL PUMP 2 FAILED AND RESET. REPLACED RELAY NR R7224 IAW MM 24-33-01 AND RCCB NR C2243 IAW MM 24-33-01 AND 24-60-01. FUNCTIONAL CHECKS SATISFACTORY. REMOVED AND REPLACED BATTERY TFR RELAY AND RCCB, PN 9131-8506 AND BACC18AF60; SN 12151 AND 50150.

Part: BLADE — CRACKED (HPT ROTOR) · airframe 23,590 hrs · 3,857 cycles

ESN 704330 - HPT STAGE 1 BLADES 68EA FOUND WITH UNDER PLATEFORM CORROSION AND CRACKS.

Part: BLADE — CRACKED (HPT ROTOR) · airframe 23,590 hrs · 3,857 cycles

ESN 704330 - HPT STAGE 2 BLADES 74EA FOUND WITH UNDER PLATEFORM CORROSION AND CRACKS.

Part: SEAT TRACK — BROKEN (BS 1450) · airframe 23,906 hrs · 3,910 cycles

MAIN DECK CENTER GUIDE LEFT SEAT TRACK AT STATION 1450 LBL 12 HAS 9 INCHES OF VERTICAL LIP BROKEN. DEFERRED 15 CYCLES AS PER MA A45300-08:00 FAA 8110-3.

Part: UNKNOWN — UNKNOWN (CARGO OVERTEMP) · airframe 23,098 hrs · 3,787 cycles

EQUIPMENT COOLING EICAS MSG DISPLAYED DURING PUSHBACK FOLLOWED BY "E/E COOLING CARD" EICAS. A/C RETURN TO GATE. A/C TEMP IN FWD CARGO COMP HAD INCREASED TO 37°C. A/C SHUTDOWN AND COOLED W/ AN AC CART FOR 30 MIN. ALL MSGS CLEARED PER AMM 21-23-00 AND 12-01-00. A/C MX RD AT 0200Z/29.

Part: IDG — FAILED (NR 2) · airframe 21,442 hrs · 3,544 cycles

ELEC BUSS ISLN 4, NO LAND 3, ENG 2&3 REV, ELEC GEN 2, NR 1 CDU INTERMITTENT. REPLACED NR 2 IDG PER MM 24-11-01 AND REPLACED NR 2 GCU PER MM 24-23-01. OPS CHECK NORMAL. IT IS BELIEVED THAT NR 2 GEN WAS CAUSING ALL OTHER INDICATIONS TO FLUCTUATE. GCU P/N 746011L; S/N 1952. IDG P/N AND S/N INCLUDED ABOVE.

Part: CONTROL MODULE — FAILED (HORIZ STAB) · airframe 21,114 hrs · 3,493 cycles

DUAL SRM FAILURE: CMC MSGS 27201 AND 27001. REPLACED RIGHT STAB TRIM CONTROL MODULE PER MM 27-41-04.

Part: WARNING MESSAGE — ACTIVATED (COCKPIT) · airframe 20,935 hrs · 3,460 cycles

NR 4 ENGINE FUEL VALVE STATUS MESSAGE WITH CMC 74574. DEFERRED PER DDPG 73-31-2.

Part: IDG — FAILED (NR 1) · airframe 19,782 hrs · 3,246 cycles

CREW REPORTED THEY DISCONNECTED NR 2 IDG; NR 1 ON DEFERRAL. OPENED MEL 24-11-1-1 FOR NR 2 IDG, REMOVED AND REPLACED NR 1 IDG.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 19,003 hrs · 3,162 cycles

CREW REPORTED EICAS MESSAGE NR 1 ELEC DRIVE DISPLAYED. COMPLIED WITH DDG 24-11-1A, OPENED MEL.

Part: FMC — FAILED · airframe 18,615 hrs · 3,107 cycles

CREW REPORTED 'ALT ALERT SYS' STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED RIGHT HAND FMC, PERFORMED GROUND TEST OF MAWEA CARD CIRCUIT. ALL OPS NORMAL PER 34-61-01.

Part: HMU — FAILED (NR 3 ENGINE) · airframe 17,241 hrs · 2,906 cycles

CREW REPORTED NR 3 ENGINE FLAMEOUT ON CLIMBOUT, CRUISE, AND DESCENT. IN FLIGHT ENGINE SHUTDOWN. REMOVED AND REPLACED NR 3 ENGINE HMY IAW MM 73-21-14. ALL PARAMETERS NORMAL AFTER ENGINE RUN.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 16,087 hrs · 2,731 cycles

DURING PUSH OUT OF HANGAR AFTER A-CHECK, AIRCRAFT'S LT STABILIZER IMPACTED THE RUDDER OF A 767. DAMAGED AREA REPAIRED PER MM 55-10-01, AREA INSPECTED PER MM 05-00-00. ALL OPS CHECKS NORMAL.

Part: SQUIB — NO TEST (FIRE BOTTLE) · airframe 15,728 hrs · 2,677 cycles

ON PREFLIGHT, FOUND FORWARD CARGO FIRE BOTTLE -D- SQUIB WOULD NOT TEST. REMOVED AND REPLACED SQUIB PER AMM 26-23-02. NO HELP FOUND LAMP FOR -D- BOTTLE WOULD NOT TEST WHEN LAMP WAS PRESSED. REMOVED LAMP HOLDER AND CLEANED PER AMM 26-23-02. OPS CHECK NORMAL.

Part: SWITCH — INOPERATIVE (NLG STEERING) · airframe 11,755 hrs · 2,034 cycles

BODY GEAR STEERING IND SYSTEM INOP. DEFERRED BODY GEAR SYSTEM PER MEL 32-52-2 ON DMI NR 33945. REMOVED AND REPLACED PRIMARY SWITCH ON LT BODY GEAR RT ACTUATOR PER MM 32-53-16. OPS CHK OK.

Part: CONTROL PANEL — FAILED (VHF COMMS) · airframe 11,665 hrs · 2,019 cycles

ALL VHF COMMUNICATIONS FAILED, NO TRANSMIT OR RECEIVE ON ANY RADIO. SWAPPED F/O'S FREQUENCY SELECT PANEL WITH CENTER POSITION AND DEFERRED PER MEL 23-24-1.

Part: LIMITER — FAILED (BRAKE TORQUE) · airframe 11,501 hrs · 1,994 cycles

BRAKE LIMITER EICAS MESSAGE ON CLIMBOUT. REPLACED BRAKE TORQUE LIMITER POSITION NR 5 PER MM 32-42-20. CMC TEST SATISFACTORY.

Part: RELAY — FAILED (ANTI ICE SYSTEM) · airframe 9,757 hrs · 1,708 cycles

AFTER ENGINE START, STATUS MSG NAI-VLV NR 3 DISPLAYED. REPLACED ANTI-ICE VALVE RELAY PER AMM 30-21-00, OPERATIONAL CHECK OK ON ENGINE RUN.

Part: GCU — MALFUNCTIONED (NR 1) · airframe 9,604 hrs · 1,683 cycles

AFTER SWITCHING FROM APU TO SHIPS POWER RECEIVED EICAS MSG (ELEC GEN OFF 1), (ELEC GEN OFF 2), (ELEC GEN OFF 3). SWAPPED NR 1 AND NR 2 GCU, RECYCLED C/B'S, ENGINE START NORMAL IAW AMM 71-00-00.

Part: LINE — DENTED (HYD SYSTEM) · airframe 9,379 hrs · 1,647 cycles

AFTER T/O NOSE GEAR WOULD NOT RETRACT. STATUS MESSAGE -GEAR DISAGREE-, -GEAR MONITOR-, -GEAR DOOR-. REPLACED DENTED HYDRAULIC LINE & BROKEN STOP BRACKET IN NOSE WHEEL WELL, PERFORMED INSPECTION OF NOSE WHEEL WELL & NO FURTHER DAMAGE. GEAR SWING ACCOMPLISHED PER AMM 12-15-05, ALL OPS NORMAL.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 9,379 hrs · 1,647 cycles

EICAS WARNING CONFIG FLAPS & CONFIG STAB. RESET NR 3 GCU PER MM 24-20-00, ALL SYSTEMS CHECKED NORMAL, GROUND TEST PASSED.

Part: ENGINE — LEAKING (NR 2) · airframe 8,101 hrs · 1,425 cycles

NR 2 ENGINE OIL FILTER BYPASS WARNING IN CRUISE RAPID LOSS OF OIL QUANTITY FROM 14 QUARTS TO 3 QUARTS. AS PER QUICK REF HANDBOOK NR 2 ENGINE SHUTDOWN PROCEDURES.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 7,624 hrs · 1,340 cycles

AFTER STARTING ENG 1 & 4, OPERATING CONRTOL CHECK HYD PSI NR 3 FELL TO 80PSI, VERY SLOW TO COME UP, SPI VERY SLOW TO RESPOND. HYD SYSTEM FAULT LIGHT LOW PSI LIGHT CAME ON. DEFERRED NR 3 DEMAND PUMP, ON 4/17/04 R&R NR 3 ACMP, OPS AND LEAK CK OK.

Part: CIRCUIT CARD — FAILED (STALL WARNING) · airframe 6,270 hrs · 1,015 cycles

IN CRUISE STICK SHAKER CAME ON STEADY A/S & ATTITUDE NORMAL. PULLED R STICK SHAKER C/B. DEFERRED TO DMI 32052 AS MEL 27-32-01. INSTALLED PLACARDS. REMOVED AND REPLACED A10 STALL WARNING CARD.

Part: WARNING SYSTEM — ACTIVATED (EICAS) · airframe 5,693 hrs · 1,004 cycles

ON ENGINE START EICAS MESSAGE ENGINE 4 FUEL VALVE WAS DISPLAYED. RESEATED LOGIC CARD Y5BA12 IN ACC WITH MM 73-22-14 WET MOTORED ENGINE IAW MM 71-00-00 ENG PERFORMED NORMAL MESSAGE ERASED.

Part: WARNING LIGHT — ILLUMINATED (NR 4 ENGINE)

EICAS MESSAGE, ENG 4 FUEL VALVE, AFTER ENGINE START. CYCLED NR 4 ENGINE FIRE HANDLE PER MM 26-21-00/01, FUEL VALVE RESET. ENGINE WET BLEED, FOUND FUEL VALVE OPERATING NORMALLY.

Part: CONTROLLER — MALFUNCTIONED (CABIN) · airframe 3,521 hrs · 619 cycles

ZONE TEMP: CABIN FILLER WITH SMOKE - RESET - TEMP STARTED DOWN - TEMP TO 36 SMOKE AGAIN. T/S SYSTEM ORDERED ZONE TEMP CONTROLLER DEFERRED TRIM AIR SYSTEM MEL 21-61-9B CATC. INSPED TRIM AIR DUCTS AND VLVS. NO DEFECTS NOTED. FAULTY ZONE TEMP CONTROLLER

Part: CONTROL MODULE — FAILED (LEFT STAB. TRIM) · airframe 1,885 hrs · 323 cycles

TRIM #2 & #3 FAILED AFTER T/O IN BOTH AUTO & MANUAL. A/C RETURNED TO MIA. REMOVED & REPLACED STAB. TRIM UNIT AS PER MM 27-41-06. OPS CHECK NORMAL.