N407KZ

Part: FLEX LINE — CRACKED (ZONE 700) · airframe 65,579 hrs · 11,641 cycles

AFTER ROTATION, RECEIVED GEAR TILT EICAS MSG. GEAR SYNOPTIC PAGE SHOWED LEFT BODY GEAR TILT MSG. FOUND LT BODY GEAR POSITIONING ACTUATOR HYD LINE CRACKED. REPLACED THE LINE WITH TEMPORARY FLEX LINE IAW GMM 3.25.1 AND AMM 20-11-18.

Part: MODULE — FAULTED (ZONE 700) · airframe 63,524 hrs · 11,372 cycles

CREW DECLARED EMERGENCY INTO ANC. BODY GEAR STEERING EICAS CAUTION MSG (INFLIGHT) &AMP; BODY GEAR STEERING SYS STS MSG.(<P>FOUND MMSG 32041, REPLACED LT BGS HYD CONT MODULE AND FUNCTION CHECKS OK, NO LEAKS FOUND IAW B747-400 AMM 32-53-04 REV 113, B747-400 IPC 32-53-51-10 REV89.

Part: VALVE — FAULTED (ZONE 400) · airframe 61,643 hrs · 11,120 cycles

BLEED 2 EICAS MESSAGE.(<P>R/R ENG 2 PRV IAW AMM 36-11-19. OPS CHK GOOD ON RUN-UP PER AMM 71-00-00. DMI 223140 CLOSED</P>)

Part: ACTUATOR — WARNING MESSAGE (SPEED BRAKE) · airframe 60,569 hrs · 10,969 cycles

SPEED BRAKE ARMED MEMO MSG AT 50KTS, CONFIG SPOILER MASTER WARNING AT 60KTS. RTO(<P>ITEM TRANFERED TO MDDR 217813 PER MEL 27-62-01 CAT C DUE DATE 10OCT24. LP 1829529 M3: R/R SPEEDBRAKE ACTUATOR IAW AMM 27-62-07. OPS CHECK GOOD. DMI 217813 CLOSED.</P>)

Part: TRU — FAULTED (NR 2) · airframe 59,481 hrs · 10,822 cycles

"DC 2 DIST" CIRCUIT BREAKER POPPED IN FLIGHT ALONG WITH MULTIPLE EICAS MESSAGE FAULTS.(<P>REMOVED AND REPLACED "DC 2 DIST" CIRCUIT BEAKER AND DC BUS #2 TRU. PER AMM 20-60-05. NO FURTHER DEFECTS NOTED.</P>)

Part: ENGINE — WARNING MESSAGE (NR 3) · airframe 59,395 hrs · 10,810 cycles

#3 ENGINE OIL FILTER ADVISORY MESSAGE(<P>REF TO M3, R/R #3 ENG IAW ATLAS REQUEST IAW AMM 71-00-02.</P> / <P>LP 1847107 M3: R/R #3 ENG PER ATLAS REQUEST. LEAKS CHECK GOOD AT THIS TIME. MAX POWER ASSURANCE RUNS ARE C/W IAW AMM 71-00-02 (W/O 132392)</P>)

Part: BATTERY — EXPIRED (ELT) · airframe 58,819 hrs · 10,725 cycles

FOUND MDC FIXED ELT BATTERY EXPIRED DATE DUE AT DEC 2021(<P>1) IAW AMM 23-24-01-002-001 &AMP; 23-24-01-402-004 REV 110 R/R ELT B00779. 2) IAW AMM 23-24-00-730-802 REV 100 PERFORMED ELT INSTALLATION TEST AND THE RESULT WAS GOOD</P>)

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 58,819 hrs · 10,725 cycles

WHEN PERFORM EMERGENCY LIGHT BATTERY PACK CAPACITY TEST, FOUND BATTERY M5168 OUT OF LIMIT(<P>1) IAW AMM 33-51-04-902-001-001 REV 110 R/R EMERGENCY LIGHT BATTERY M5168. 2) IAW AMM 33-51-04-902-001-001 REV 110 PERFORMED EMERGENCY LIGHT BATTERY INSTALLATION TEST AND THE RESULT WAS GOOD</P>)

Part: REVEAL — CRACKED (RELEASE HANDLE) · airframe 58,819 hrs · 10,725 cycles

LH 5 DOOR FWD CUTOUT, DOOR RELEASE HANDLE AREA REVEAL PANEL CRACK. STA 2240 WL 250(<P>1) REPAIR DAMAGE AREA IAW W/S 40322 (SRM 53-60-15-2R-7 REV 100). 2) JOB COMPLETED &AMP; CONDITION CHECK NORMAL</P>)

Part: SKIN — CORRODED (LT WING) · airframe 58,819 hrs · 10,725 cycles

BULGE - SKIN, LWR FACE OF LH WING T/E INBD FORE FLAP LWR SKIN WBL 395 - WBL 407, FRONT SPAR(<P>1) PERFORM PERMANENT REPAIR OH LH WING T/E INBD FORE FLAP LWR SKIN WBL 395 - WBL 407, FRONT SPAR IAW EGAT EI T2024A57-1049 REV 1. 2) CONDITION CHECK IS GOOD</P>)

Part: SKIN — DEBONDED (LT AILERON) · airframe 58,819 hrs · 10,725 cycles

DISBOND - FILLER, AFT OTBD SIDE OF LH WING INBD AILERON WBL 515(<P>1) PERFORM REPAIR OF DISBOND SKIN DAMAGE AT LH WING INBD AILERON T/E OUTBD SIDE LWR SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR DETAILED REWORK INFO. REF SRM 57-60-01-01-1 REV 100, SRM 57-60-01-2R-1 REV 100 &AMP; SRM 51-70-17-0G-0 REV 100. 2) CONDITION CHECK IS GOOD.</P>)

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 58,819 hrs · 10,725 cycles

FOUND EMERGENCY LIGHT BATTERY M5169 CAPACITY TEST OUT OF LIMIT(<P>1) IAW AMM 33-51-04-002-009-001 &AMP; 33-51-04-402-012-001 REV 110 R/R EMERGENCY LIGHT BATTERY POWER SUPPLY M5169. 2) IAW AMM 33-51-04-902-001-001 REV 110 R/R EMERGENCYLIGHT BATTERY AT M5169. 3) IAW AMM 33-51-04-402-012-001 &AMP; 33-51-04-902-001-001 REV 110 PERFORMED EMERGENCY LIGHT BATTERY &AMP; POWER SUPPLY INSTALLATION TEST &AMP; THE RESULT WAS GOOD</P>)

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 56,751 hrs · 10,412 cycles

CABIN ALT AUTO FAILED JUST AFTER TAKEOFF. EICAS MSGS: "CABIN ALT AUTO" & "OUTFLOW VLV L" DISPLAYED. RT OUTFLOW VALVE PREVIOUSLY DEFERRED.(<P>REMOVED AND REPLACED CABIN PRESSURE CONTROLLER A PER AMM 21-31-02. CPCS-A &AMP; -B GROUND TESTS PASSED, NO FAULTS NOTED. OUTFLOW VALVE R REMAINS ON DEFERRAL.&NBSP;</P>)

Part: KEELBEAM — CORRODED · airframe 52,075 hrs · 9,649 cycles

CORROSION - KEEL BEAM. KEEL BEAEM INNER SURFACE STA 1287 STA 1303(<P>1. REMOVE THE AFFECTED FASTENERS IAW SRM 51-40-02 REV 94. 2. BLEND OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 94. 3. ACCOMPLISH EI T2022A53M-955 REV 1. 4. JOB COMPLETED</P>)

Part: PCA — BROKEN · airframe 52,075 hrs · 9,649 cycles

FOUND RH WING INBD AILERON PCA ROD ENG BROKEN(<P>1. IAW AMM 27-11-12-002-001 REV 103 AND AMM 27-11-12-402-010 REV 103 REPLACED RH WING INBD AILERON PCA</P>)

Part: BATTERY PACK — FAILED INSP · airframe 52,075 hrs · 9,649 cycles

WHEN PERFORM EMERGENCY LIGHT PACK CAPACITY TEST FOUND M5168, M5169 ; M5170 BATTERY FAIL(<P>1. IAW AMM 33-51-04-902-001-001 REV 103 REPLACED EMERGENCY LIGHT BATTERY ASSY AT M5168, M5169 &AMP; M5170. 2. IAW AMM 33-51-04-902-001-001 REV 103 PERFORMED EMERGENCY LIGHT BATTERY ASSY INSTALLATION TEST AND THE RESULT WAS SATISFACTORY

Part: SKIN — BROKEN · airframe 52,075 hrs · 9,649 cycles

BROKEN - SKIN AND CAP, RH WING INBD AILERON TE WEDGE OUTBD END(<P>1. PERFORM REPAIR OF RH WING INBD AILERON, PLEASE REFER THE JOB CARD ATTACHING SHEET FOR THE DETAILED REWORKING INFORMATION. 2. CONDITION CHECK IS SATISFACTORY</P>)

Part: PCA — BROKEN · airframe 52,075 hrs · 9,649 cycles

FOUND LH WING INBD AILERON PCA ROD END BROKEN(<P>1. IAW AMM 27-11-12-002-001 REV 103 AND AMM 27-11-12-402-010 REV 103 REPLACE LH WING INBD AILERON PCA</P>)

Part: SKIN — GOUGED · airframe 52,075 hrs · 9,649 cycles

GOUGE DAMAGE ON THE RH WING LOWER SKIN INNER SURFACE NEAR WS 1454.00(<P>1. BLENEDE OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 94. 2. PERFORM NDT INSPECTION REFER TO JOB CARD ATTACHING SHEET #0317165 AND DATA SHEET CONTROL #689376-1, 6893716-2, 6893716-3. 3. REPAIR THE DAMAGE AREA IAW EI T2022A57M-960 REV 3. 4. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: BEARING — BROKEN · airframe 52,075 hrs · 9,649 cycles

FWD MAIN ENTRY DOOR #1 LH EXTERIOR HANDLE BEARING BROKEN(<P>1. IAW AMM TASK 52-11-13-004-001 REV 103 AND AMM TASK 52-11-13-404-017 REV 103 REPLACED L1 DOOR EXTERIOR HANDLE BEARING. 2. CONDITION CHECK NORMAL</P>)

Part: KEELBEAM — CORRODED · airframe 52,075 hrs · 9,649 cycles

CORROSION - KEEL BEAM, KEEL BEAM INNER SURFACE, STA 1329 - 1344(<P>1. REMOVE THE AFFECTED FASTENERS IAW SRM 51-40-02 REV 94. 2. BLEND OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 94. 3. ACCOMPLISH EI T2022A53M-955 REV 1. ORIGINAL EI ATTACHING WITH W/O 6880625. 4. JOB COMLETED

Part: KEELBEAM — CORRODED · airframe 52,075 hrs · 9,649 cycles

CORROSION - KEEL BEAM, KEEL BEAM LWR CHORD STA 1370 STA - 1380(<P>1. REMOVE THE AFFECTED FASTENERS IAW SRM 51-40-02 REV 94. 2. BLEND OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 94 3. ACCOMPLISH EI T2022A53M-955 REV 1. ORIGINAL EI ATTACHING WITH W/O 6880625. 4. JOB COMPLETED</P>)

Part: ACTUATOR — INOPERATIVE · airframe 52,075 hrs · 9,649 cycles

FUNCTION FAIL DUE TO RH WLG ALTERNATE EXTENSION SYSTEM TEST. FOUND THE RH WLG ROTARY ACTUATOR ROTATION ACTION CAN'T STOP(<P>1. IAW AMM 32-36-01-004-001 REV 103 AND AMM 32-36-01-404-009 REV 103 REPLACED RH WLG ALTERNATE ROTARY ACTUATOR. 2. CONDITION CHECK NORMAL</P>)

Part: ACTUATOR — INOPERATIVE · airframe 52,075 hrs · 9,649 cycles

FUNCTION FAIL - DUE TO LH WING ALTERNATE EXTENSION SYSTEM TEST. FOUND THE LH WLG ROTARY ACTUATOR ROTATION ACTION CAN'T STOP(<P>1. IAW AMM 32-36-01-004-001 REV 103 AND AMM 32-36-01-404-009 REV 103 REPLACED LH WLG ALTERNATE ROTARY ACTUATOR. 2. CONDITION CHECK NORMAL</P>)

Part: KEELBEAM — CORRODED · airframe 52,075 hrs · 9,649 cycles

CORROSION - KEEL BEAM. INNER SURFACE OF KEEL BEAM, STA 1405 - 1427(<P>1. REMOVE THE AFFECTED FASTENERS AIW SRM 51-40-02 REV 94. 2. BLEND OUT THE DAMAGE AREA IAW SRM 51-10-02 REV 94. 3. ACCOMPLISH EI T2022A53M-955 REV 1. ORIGINAL EI ATTACHING WITH W/O 6880625</P>)

Part: FITTING — CRACKED · airframe 52,075 hrs · 9,649 cycles

CRACK-FOUND LH LONGERON EXTENSION FITTING HAS CRACK AT STA 1480. DIMENSION ABOUT 0.5"(<P>1. REPAIR THE LH SIDE LONGERON EXTENSION FITTING IAW EI# T2022A07M-887 REV 0 &AMP; T2022A53M-954 REV 1 AND DWG # 65B15254 SH 10 REV G, 65B15254 SH 16 REV F, 65B01162 SH 14 REV A. 2. ACCOMPLISHED EO #4453A818 PAR 1-2, 3 REV 19. 3. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

Part: BEARING — MISSING (AILERON PULLEY) · airframe 49,073 hrs · 9,168 cycles

RIGHT WLG WHEEL WELL AILERON CONTROL CABLE AA PULLEY BEARINGS MISSING, HOUSING CORRODED AT WS 364.(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;"><SPAN>REMOVED AND REPLACED RH WING / AILERON CONTROL CABLE PULLEY AT WS 364 PER B747-400 AMM 20-11-12-020-801,&NBSP;</SPAN>FUNCTIONAL CHECK GOOD PER B747-400 AMM 27-11-00-825-029.</P>)

Part: LINE — FAILED (HYD SYSTEM) · airframe 47,183 hrs · 8,869 cycles

GEAR TILT ADVISORY AND STATUS MESSAGE. REPLACED GEAR TILT HYDRAULIC LINE, IAW AMM 32-13-15-034-007 AND AMM 32-13-15-434-020. OPERATIONS CHECK GOOD.

Part: WEB — CRACKED (LT BLG WW) · airframe 44,044 hrs · 8,322 cycles

CRACK - WEB, FWD FACE OF LH BODY GEAR W/W AT BULKHEAD, STA 1480.(<P>REPAIRED DAMAGED AREA IAW SRM 53-40-08, REPAIR 1 REV. 88 AND EI NO. T2020A53M-808, REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: BEARING — DAMAGED (L1 DOOR) · airframe 44,044 hrs · 8,322 cycles

FOUND L1 DOOR FWD UPPER BEARING DAMAGE.(<P>IAW AMM 52-11-01-735-080 REV. 97, REPLACED L1 DOOR FWD UPPER BEARING ROLLER. CONDITION CHECK NORMAL.</P>)

Part: CONNECTOR — LOOSE (BLEED AIR SYS) · airframe 41,038 hrs · 7,784 cycles

ADVISORY "BLEED 2" AFTER TAKE OFF THRUST WAS ADVANCED. THE TAKE OFF WAS REJECTED AT APPROXIMATELY 80 KNOTS.(<P>ITEM TRANSFERRED TO MDDR #111197 PER MEL 36-21-04. JUMPERED OVER-PRESSURE SWITCH ENGINE NR 2. CAT C. DUE 15MAY19.</P><P>LP 1058712 - M5/M6: REVIEWED FAULT HISTORY. CMC REPORTED "BLEED 2 HIGH PRESS S/O VLV FAIL" MSG #36002. PERFORMED WIRING CHECKS IAW FIM 36-11 TASK 802 AND WDM 36-11-42. FOUND OPEN CCT BETWEEN HPSOV (V347) (NO 1.2.3 LINE) AND ASCTU (DM 7957BA) (E15 . F15 PIN) AND GND LINE. THEN FOUND CONNECTION (D4210P) LOOSE AND IN THE INCORRECT POSITION. RE-TIGHTENED IT AND WIRING CHECK OK BETWEEN ASCTU&NBSP; AND HPSOV IAW WDM 36-11-42. CONFIRMED HPSOV AND PRV OPS CHECK WITH ENGINE RUN. ALL MSG CLEARED, MDDR # 111197 CLOSED AND MCC NOTIFIED.&NBSP;&NBSP;</P>)

Part: CONTROL MODULE — MALFUNCTIONED · airframe 36,667 hrs · 7,063 cycles

STAB TRIM STATUS MESSAGE WITH NO LAND 3 MESSAGE. REPLACED THE STAB TRIM POSITION TRANSMITTER, CONTROL MODULE, AND STAB TRIM / RUDDER MODULE.

Part: SUPPORT BEAM — CRACKED (RUDDER) · airframe 36,135 hrs · 6,988 cycles

RIGHT VERTICAL STAB T/E PANEL SUPPORT BEAM AT RUDDER STA 382.4, FOUND CRACKED. THE SUPPORT BEAM CAP ANGLE WAS REPAIRED IAW SRM 55-30-13-2R-2, REPAIR 2, FIG 202.

Part: COVER — CRACKED (NLG) · airframe 36,135 hrs · 6,988 cycles

NLG LEFT MOUNT BOLT COVER PANEL, FOUND THE BOLT HOLE CRACKED AT BS 400. REPAIRED IAW RL-53-00-12519, REV A.

Part: SUPPORT BEAM — CRACKED (RUDDER) · airframe 36,135 hrs · 6,988 cycles

VERTICAL STAB T/E PANEL SUPPORT BEAM AT RUDDER STA 332, FOUND CRACKED. THE SUPPORT BEAM CAP ANGLE WAS REPAIRED IAW SRM 55-30-13-2R-2, REPAIR 2, FIG 202.

Part: SUPPORT BEAM — CRACKED (RUDDER) · airframe 36,135 hrs · 6,988 cycles

RIGHT VERTICAL STAB, T/E PANEL SUPPORT BEAM AT RUDDER STA 307.5 FOUND CRACKED. THE SUPPORT BEAM CAP ANGLE WAS REPAIRED IAW SRM 55-30-13-2R-2, REPAIR 2, FIG 202.

Part: SUPPORT BEAM — CRACKED (RUDDER) · airframe 36,135 hrs · 6,988 cycles

VERTICAL STAB TIE PANEL SUPPORT BEAM AT RUDDER STA 307.5 FOUND CRACKED. VERTICAL STAB T/E PANEL SUPPORT BEAM CAP ANGLE REPAIRED IAW SRM 55-30-13-2R-2, REPAIR 2, FIG 202.

Part: SUPPORT BEAM — CRACKED (RUDDER) · airframe 36,135 hrs · 6,988 cycles

RIGHT VERTICAL STAB T/E PANEL SUPPORT BEAM AT RUDDER STA 357.4, FOUND CRACKED. THE SUPPORT BEAM CAP ANGLE WAS REPAIRED IAW SRM 55-30-13-2R-2, REPAIR 2, FIG 202.

Part: STIFFENER — CRACKED (APU FIREWALL) · airframe 36,135 hrs · 6,988 cycles

APU FIREWALL FWD FACE AT BS 2658, NR 2 STIFFENER FOUND CRACKED. THE FIREWALL STIFFENER WAS REPAIRED IAW RL-53-83-12510, REV A.

Part: SUPPORT BEAM — CRACKED (RUDDER) · airframe 36,135 hrs · 6,988 cycles

LEFT VERTICAL STAB T/E PANEL SUPPORT BEAM AT RUDDER STA 357.4 , FOUND CRACKED. THE SUPPORT BEAM CAP ANGLE WAS REPAIRED IAW SRM 55-30-13-2R-2, REPAIR 2, FIG 202.

Part: SUPPORT BEAM — CRACKED (RUDDER) · airframe 36,135 hrs · 6,988 cycles

VERTICAL STAB T/E PANEL SUPPORT BEAM AT RUDDER STA 332, FOUND CRACKED. THE SUPPORT BEAM CAP ANGLE WAS REPAIRED IAW SRM 55-30-13-2R-2, REPAIR 2, FIG 202.

Part: SUPPORT BEAM — CRACKED (RUDDER) · airframe 36,135 hrs · 6,988 cycles

LT VERTICAL STAB T/E PANEL SUPPORT BEAM AT RUDDER STA 382.4, FOUND CRACKED. SUPPORT BEAM CAP ANGLE WAS REPAIRED IAW SRM 55-30-13-2R-2, REPAIR 2, FIG 202.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 35,173 hrs · 6,839 cycles

"ENG FIRE NR 1" EICAS. RAN CHECK LIST INDICATION EXTINGUISHED NO BOTTLES DISCHARGED.

Part: FEEDER CABLE — CHAFED · airframe 30,595 hrs · 6,077 cycles

FOUND POWER FEEDER CABLE W5022-013-00 CHAFING WITH CEILING SCREW AT FWD CARGO. REPAIRED THE FEEDER CABLE IAW SWPM 20-30-14, 20-30-13 REV63 AND WDM 24-21-11 REV19 AND CONDITION CHECKED NORMAL. PERFORMED ECU STATIC TEST AND THE RESULT WAS SATISFACTORY IAW AMM 71-00-00-805-160-100 REV 87.

Part: ACTUATOR — FAILED (MLG) · airframe 30,595 hrs · 6,077 cycles

FND RH WING LANDING GEAR ALTERNATE MOTOR FUNCTION FAIL. REPLACED THE RT WING ALT ELECTRIC ACTUATOR IAW AMM 32-36-01-004-001 REV 87 AND AMM 32-36-01-404-009 REV 87. CONDITION CHECK NORMAL.