N757QM
Registered owner: AERO MICRONESIA INC DBA, GU (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
LEFT ENGINE HIGH EGT. R & R LT ENGINE EEC IAW AMM.
RIGHT FMC INOPERATIVE. R & R RT FMC IAW AMM. OPS CHKD NORMAL.
FLIGHT MGE301, APU INFLIGHT START FAILED. FOUND APU DIFF PRESSURE SWITCH FAULTY. R & R DIFFERENTIAL PRESSURE SWITCH IAW AMM. OPS CHECK NORMAL, APU VERIFICATION FLIGHT SUCCESSFUL.
RIGHT BUSS TIE LIGHT ILLUMINATED. R & R RT GCU IAW AMM OPS CHECK NORMAL.
RIGHT ENG IDG INOPERATIVE. (DEFERRED PER MEL 24-00-01). R & R RT ENG IDG IAW AMM, OPS CHKD NORMAL.
RIGHT BUSS TIE TRIPS WHEN POWER TRANSFERED. R & R RT GCU IAW AMM, OPS CHECKED NORMAL.
LEFT FMC INOPERATIVE. R & R LT FMC IAW AMM. OPS CHECKED NORMAL.
RIGHT FMC INOPERATIVE. R & R THE LT FMC IAW AMM. OPS CHECKED NORMAL.
APU INOP. REPLACED APU PER TASK CARD.
FLIGHT MGE601. LT ENG LOW OIL PRESS AFTER LANDING. FOUND FAULTY EEC. R/R LH ENG EEC PER AMM, OPS CHECK NORMAL.
PERFORMED APU BITE PER FIM. FOUND LOW OIL PRESS APU DE-OIL SOLENOID FAULTY. REPLACED SAME PER AMM. OPS AND LEAK CHECK OK. SUCCESSFUL APU INFLIGHT START PERFORMED.
FLIGHT MGE601, AIR RETURN DUE LOW LEFT HYD QTY. FOUND HYD. FLEX LINE LEAK AT R MLG TILT ACTUATOR. R/R FLEX LINE AND SERVICED HYD. SYSTEM PER AMM. NO LEAKS DETECTED. AIRCRAFT RETURNED TO SERVICE.
FLIGHT MGE301, APU INFLIGHT START FAILED. OPEN
LEFT ENG HYDRAULIC PUMP. LEFT ENG EDP SHAFT FOUND SHEARED. R/R LEFT ENG EDP PER AMM. OPS CHECK, LEAK CHECK OK.
FLIGHT MGE301, RIGHT ENGINE HUNG START. FOUND UPPER IGNITER PLUG WORN TO LIMITS. REPLACED IGNITER PLUG PER AMM.
FLIGHT MGE301, RIGHT ENGINE HUNG START. FOUND FCU/EEC EPCS MESSAGE, REPLACED FCU PER AMM.
FLIGHT MGE301, WXR FAILED. REPLACED WXR DRIVE UNIT PER AMM.
RIGHT ENGINE SLOW TO START. REPLACED RT ENGINE STARTER IAW AMM.
FLIGHT MGE400 - AIR RETURN. LT & RT EICAS COMPUTER STATUS MESSAGE. PERFORMED EICAS BITE, FOUND NUISANCE FAULTS. CLEARED FAULTS PER FIM. SWAPPED LT & RT COMPUTERS IAW FIM. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.
FLIGHT MGE600, WXR FAIL. FOUND AND REPLACED FAULTY WXR TRANSCEIVER PER AMM.
FLIGHT MGE600 - ESI / (AIR RETURN) RIGHT ENGINE BLEED OFF MESSAGE ON T/O. NO DUCT PRESSURE ON RIGHT SIDE. PERFORMED FIM, FOUND RFCC LEAKING. REPLACED RFCC IAW AMM.
RIGHT PACK TEMP EICAS MESSAGE. REPLACED PACK TEMP CONTROLLER PER AMM. NO DEFECTS NOTED.
FLT. MGE502, WXR FAILED. PERFORMED OPS CHECK OF WEATHER RADAR SYSTEM. FOUND DRIVE UNIT FAILED. REPLACED DRIVE UNIT PER AMM. NO DEFECTS NOTED.
FLT MGE502, RT FMC INOP. REPLACED RH FMC PER AMM.
RIGHT ENGINE FUEL FLOW INDICATION INTERMITTENT. REPLACED FUEL FLOW TRANSMITTER IAW AMM.
APU PNEUMATICS INOPERATIVE. R & R APU ECU PER AMM. OPS CHECKED NORMAL.
FLT: MGE831, APU FUEL VAL EICAS. R & R APU FUEL SHUTOFF VALVE IAW AMM, OPS CHECK NORMAL.
MAJOR REPAIR: LEVEL 2 CORROSION FOUND AT BSTA 680-700 BETWEEN STRINGERS 26R/28R. REPAIRED CORROSION PER EO APA-0043-001 REV 1 DTD 28JUN2025 AND PER SRM 53-00-01 REPAIR 28.
AIR RETURN DUE TO MAIN CARGO FIRE WARNING DURING CLIMBOUTFOLLOWED BY POPPED CB. QRH CONSULTED, ACFT RETURNED TO HNL. MX T/S PER PRECISION AMM AND FOUND FAULTY SMOKE DETECTOR. R/R SAME, OPS CHK NORMAL. ACFT BACK IN SERVICE.
FLT: N/A (MX INSP.) ESI: RH ENG LPC 1ST STAGE BLADE #17 FOUND OUT OF LIMITS R/R #17 AND #35 FAN BLADES PER AMM NO DEFECTS NOTED.
FLIGHT DECK TEMP HOT. R & R STBY PACK TEMP CONTROLLER PER AMM.
FLT: MGE301. LH ENG DID NOT START ON IGNITOR 1 STARTED NORMAL ON BOTH. R/R LH ENG EXCITER 1 PER AMM.
FLT NO: N/A (MX INSP). ESI - PERFORMED RH ENG PNEUMATIC HEALTH CHECK. FOUND HS PILOT FAULTY. R/R RH ENG HS PILOT PER AMM 36-11-08. OPS CHECK NORMAL.
FLT NO: MGE 401. ESI - APU SHUTDOWN 2X WHILE ENG STARTING. PERFORMED ECU BITE CHECK FOUND REVERSE FLOW MSG. R/R PRESSURE SENSOR PER AMM 49-61-04. OPS CHECK GOOD.
FLT NO: N/A (MX INSP) ESI - FO MCDU INOP. REMOVED AND REPLACED FO MCDU PER AMM.
MGE 300, EVENT - AIR RETURN DUE TO NO LNAV/VNAV AND AUTO THROTTLE. DEFERRED LNAV / VNAV AND AUTO THROTTLE.
FLT NO: N/A, MX INSP, ESI - DISCREPANCY: LEFT FMC FAULT. SWAPPED LT AND RT FMC, FAULT FOLLOWED. PLACED RT FMC ON MEL. REMOVE AND REPLACED RT FMC PER AMM 34-61-00.
MGE 300 (EVENT) - AIR RETURN DUE TO: NO LNAV/VNAV, NO AUTO THROTTLE NO TMC INFO.
FLT NO. MGE 300 (EVENT). AIR RETURN DUE TO: NO INFO ON PROGRESS PAGE BURN, TIME WIND UNABLE TO MAINTAIN COURSE. TEMP SELECT FOR THROTTLES INOP. NO LNAV / VNAV. - SWAPPED FMC FOR TROUBLESHOOTING PER AMM 34-61-01, PERFORMED BITE TEST PER FIM 22-02 TASK 801 TEST NORMAL. PERFORMED MCDP BITE NO FAULTS FOUND. PERFORMED FIM 34-61 FT 823 NO FAULTS FOUND.
LH ENG STARTER VALVE DOESNT OPEN WHEN SWITCHED TO RUN. R/R LH ENG STARTER CONTROL VALVE IAW AMM 80-11-02-024-001-P001.
APU AUTO SHUTDOWN ON ENG START. REPLACED APU SURGE VALVE PER AMM 49-52-00
EPCS FAULT MESSAGE HCC/EEC. R/R ACTIVE CLEARANCE CONTROL VALVE IAW AMM 72-53-90/601.
LEFT ENG STARTER VALVE TAKES LONG TO CLOSE AFTER ENG START UP. R & R LH ENG STARTER CONTROL VALVE IAW AMM 80-11-02-024-001-P001.
APU ELECTRICAL LOAD FLUCTUATES. REPLACED APU ECU PER AMM. OPS CHECK GOOD.
FLT NO: MGE305 - EVENT (ETOPS- AIR RETURN) MULTIPLE EICAS MESSAGES. PERFORMED FIM AND FOUND LEFT EICAS COMPUTER INTERMITTENT. REPLACED LEFT EICAS COMPUTER PER AMM.
DURING C CHECK, CORROSION WAS FOUND ON THE LH WING LOWER SKIN AT WS 187-213. CORROSION WAS REPAIRED PER BOEING ENGINEERING INSTRUCTIONS.
DURING C CHECK, CORROSION WAS FOUND ON THE LEFT HORIZONTAL STABILIZER COMMON TO THE REAR SPAR BETWEEN STAB STA 104.25-128.25 AND 200.25-224.25. CORROSION WAS ADDRESSED AND REPAIRED PER BOEING ENGINEERING DRAWING.
DURING C CHECK, CORROSION WAS FOUND ON THE RH HORIZONTAL STAB BETWEEN STA 116.25-122.428, 140.25-148.48,153.61-156.17,164.53-174.10,176.299-180.10, 183.30-189.80,227.70-232.91,234.94-241.52, 267.43-276.25 AND 286.80-288.38. ALL WERE ADDRESSED AND REPAIRED PER BOEING ENGINEERING INSTRUCTIONS.
DURING C CHECK, CORROSION WAS FOUND ON THE RH WING LOWER SKIN AT WS 187-211. CORROSION WAS REPAIRED PER BOEING ENGINEERING INSTRUCTIONS.
FLT NO: MGE900 (REPOSITION FERRY). EVENT - APU IN-FLIGHT START FAILED DURING VERIFICATION. AIRCRAFT HEADING TO HEAVY MAINTENANCE FOR FURTHER TROUBLE-SHOOTING. THIS ITEM REMAINS OPEN.
MX FINDING - ESI DISCREPANCY: RH ENG TR INOP. REPLACED RHOB TR LVDT PER AMM
FLT NO: MGE891 - ESI R PACK TEMP. REPLACED RH PACK TEMP CONTROL VALVE
FLT NO: N/A (MX INSP.) L ENG SEC CONT STATUS MSG. R/R L ENG EEC PER AMM 73-21-04. OPS CHECK NORMAL.
FLT NO: N/A (MX ISNP.) ESI - RH MCDU INOP. R/R RH MCDU PER AMM 34-61-01. OPS CHECK NORMAL.
FLT NO: N/A (MX INSP.) ESI - R ENG HPSOV SEURED CLOSED. MEL 36-11-02. R/R R ENG HS PILOT PER AMM 36-11-08. OPS CHECK NORMAL.
FLT NO: N/A. (MEL 34-61-01C). ESI - RH MCDU INOP. R/R RH MCDU PER AMM 34-61-01. OPS CHECK NORMAL.
FLT NO: N/A (MX INSP). ESI - GEN FILTER SW ON APU BITE. R/R APU GEN FILTER SWITCH PER AMM 49-27-03. OPS CHECK NORMAL.
ESI - PERFORMED PNEUMATIC HEALTH CHECK ON R ENG. FOUND HS PILOT FAULTY. R/R R ENG HS PILOT PER AMM 36-11-08. PERFORMED PNEUMATIC HEALTH CHECK AFTER REPLACEMENT. HS PILOT OPERATING NORMAL.
FLT NO: N/A (MX INSP.) ESI - APU AUTO SHUTDOWN. R/R APU GEN FILTER SWITCH PER AMM 49-27-03. OPS CHECK NORMAL.
FLT NO: ESI - APU OIL HISTORY, AUTO SHUTDOWN. R/R APU PER AMM 49-11-01.
FLT NO: N/A (MX INSP.) ESI - APU INOP. R/R FUEL FLOW DIVIDER SOLENOID PER AMM 49-31-03.
FLT NO: N/A (MX INSP.) ESI - FUEL QTY IND AT FUEL PANEL INOP. R/R FUEL QTY IND. PER AMM 28-41-06.
FLT NO: N/A (MX FINDING). ESI - RH ENG FIRE LOOP 1 STATUS MESSAGE. REPLACED RH ENG FIRE LOOP 1.
FLT NO: MGE300. ESI - LEFT ENGINE FAILED TO START. RETURN TO GATE. PERFORMED IGNITION SYSTEM TEST, FOUND SYSTEM NO. 2 FAILED. REPLACED LH SYSTEM NO. 2 IGNITION LEAD.
FLT NO: N/A (MX INSP). ESI - DURING SVC CHECK, LH ENG STARTER OIL WAS DISCOLORED. EXAMINED CHIP DET AND FOUND METAL PARTICLES. R/R LH ENG STARTER PER AMM 80-11-01. OPS CHECK NORMAL.
FLT: N/A (MX FINDING). ESI - APU WILL NOT START. REPLACED APU STARTER PER AMM. APU OPS CHECK GOOD.
FLT. NO: MGE411 ESI - EICAS R PACK TEMP. PERFORMED FIM 21-51 FT 803. FOUND RH MIX MANIFOLD SENSOR FAULT LIGHT. REPLACED SENSOR PER AMM 21-61-02.
FLT. NO: MGE410. ESI - RH ENG SEC CONT STATUS MESSAGE. RETURN TO GATE. REMOVED AND REPLACED RIGHT EEC IAW AMM 73-21-04. RAN ENGINE. OPS CHECK SATISFACTORY.
FLT NO.: N/A (MX FINDING). ESI - FLIGHT DECK TEMP CONTROL INOP. REPLACED LH PACK LOW LIMIT VALVE.
FLT NO.: N/A (MX FINDING). ESI - RH ENGINE BLEED LIGHT SLOW TO COME ON AFTER ENGINE SHUTDOWN. REPLACED RH PRSOV PER AMM. NO DEFECTS NOTED.
FLT NO.: MGE 410. EVENT (AIR RETURN) - R ENG EGT 731 DEGREES DURING CLIMB THROUGH 6,000 FT. PERFORMED FIM 71-05 FT 812. PERFORMED OVERTEMP VISUAL INSP PER AMM. PERFORMED BLEED TEST AND AND AMM TEST 6 & 9. NO DEFECTS NOTED. AICRAFT RETURNED TO SERVICE.
FLT NO: MGE 411. ESI - DUCT PSI SPLIT R-36, L-19. PERF/APU PG FOUND LEFT DUCT PRESS 36 AND RIGHT 6. PERFORMED PNEUMATIC HEALTH CHECK ON THE RIGHT ENG. FOUND HS PILOT FAILING. R/R HS PILOT PER AMM 36-11-08. PERFORMED HEALTH AGAIN AND PASSED.
FLT NO: MGE411. ESI - RH ENG BLEED OFF LIGHT. R/R RH ENG PRSOV PER AMM 36-11-09.
FLT NO: MGE411. ESI - LH PACK AUTO INOP STBY SELECTED. FOUND CRACK ON WATER EXTRACTOR. R/R WATER EXTRACTOR PER AMM 21-51-04.
FLT NO: N/A (MX INSP.) ESI - RH ENG FIRE LOOP 2 STATUS MSG. R/R RH ENG FIRE LOOP 2 PER AMM 26-11-01.
FLT NO: MGE411. ESI - RH ENG FIRE LOOP 1 INOP. REMOVED AND REPLACED RH ENG FIRE LOOP 1 PER AMM 26-11-01.
FLT NO: MGE 503. ESI - ENG BLEED VALVE WITH ANTI ICE DURING CLIMB MSG. REPLACED AIR SUPPLY OVERTEMP LIMITING SENSOR 450 PER AMM 36-11-13. NO LEAKS NOTED.
ESI - HMG VALVE INOP. R/R HMG CONTROL UNIT PER AMM 24-25-02. OPS CHECK NORMAL PER AMM 24-25-00.
FLT NO: N/A (MX INSP.) ESI - FLT DECK TEMP SELECT INOP. R/R STBY PACK CONTROLLER PER AMM 21-51-14. OPS CHECK NORMAL.
FLT NO: N/A (MX INSP.) ESI - RH ENG #2 IGNITOR PLUG AND LEAD FOUND WORN. R/R#2 ENG IGNITOR PLUG AND LEAD PER AMM 74-21-02 / 74-21-01 OPS CHECK NORMAL.
FLT NO: N/A. (MX INSP.) ESI - APU BLEED INOP HISTORY. R/R APU PER AMM 49-11-01.
FLT NO: N/A (MX INSP.) ESI - APU BLEED INOP. REPLACED RH APU MONOPOLE.
FLT NO: N/A (MX INSP.) ESI - APU BLEED INOP. REPLACED APU FLOW SENSING MODULE.
FLT NO: N/A (MX INSP.) ESI - APU FAILED TO START. REPLACED APU STARTER.
FLT NO: N/A (MX INSP.) ESI - NO APU BLEED PRESSURE. R/R APU POWER CONTROL UNIT PER AMM 49-61-05.
FLT NO: MGE301. ESI - APU FAULT. R/R APU POWER CONTROL UNIT PER AMM 49-61-05.
FLT NO.: N/A (MX INSP.) ESI - RH ACM INOP. REPLACED RH ACM.
FLT NO: N/A (MX INSP.) ESI - RH ENGINE IGNITER PLUG FAILED INSPECTION. REPLACED RH ENG IGNITER PLUG.
FLT NO.: N/A (MX INSP.) ESI - RH STARTER OIL CONTAMINATED DURING DURING INSPECTION. REPLACED RH STARTER.
FLT NO: MGE305. ESI - RH ENG FIRE LOOP 1 FAULTY (STATUS MESSAGE). REMOVED AND REPLACED RH ENG FIRE LOOP 1 PER AMM 26-11-01. OPS CHECK NORMAL.
FLT NO: MGE503. ESI - CONDENSATION IN FLIGHT DECK FROM LEFT PACK. REPLACED LH WATER EXTRACTOR PER AMM 21-51-04.
FLT NO: MGE411. ESI - L ENG BLEED OFF EICAS MESSAGE CLIMBING THROUGH FL330. REPLACED L ENG ANTI ICE VALVE PER AMM 30-21-03. OPS CHK NORMAL.
FLT NO: MGE301. EVENT - AIR RETURN DUE TO R1 WINDOW CRACKED. R/R R1 WINDOW PER AMM 56-11-01. ACFT RETURNED TO SERVICE.
FLT NO: MGE901. ESI - APU FAILED TO START ON GROUND. FOUND FAULTY APU ECU. REPLACED ECU AND PERFORMED APU OPS CHECK PER THE APPLICABLE MANUAL. NO ISSUES.
FLT NO: MGE9002. ESI - LH ENG BLEED OFF WITH ENG ANTI ICE ON. REPLACED LH ENGINE ANTI ICE VALVE. OPS CHK NORMAL.
FLT NO: N/A (MX INSP). ESI - LH ENG HI STAGE LIGHT AND MSG WITHOUT ENGINES OPERATING. REPLACED LEFT HIGH STAGE PILOT PER AMM 36-11-08, PROBLEM STILL EXISTED. PERFORMED WIRING CHECK PER WDM 36-11-12. FOUND CONNECTOR D1064 CONTAMINATED, CLEANED CONNECTOR PER SWPM 20-60-01. NO DEFECTS NOTED.
FLT NO: N/A (MX INSP). ESI - RH ENG 2.5 BLEED ACTUATOR SECONDARY CHANNEL INDICATION MISSING. REPLACED 2.5 BLEED ACTUATOR PER AMM 75-32-01. OPS CHECK GOOD.
FLT NO: N/A (MX INSP). ESI - R FMC FAILED. REPLACED RIGHT FMC. OPS CHECK GOOD.
FLT NO: N/A (MX INSP). ESI - RIGHT PACK OUT TEMP WARM. REMOVED AND REPLACED RIGHT CONDENSER IAW AMM 21-51-10. OPS CHECK GOOD.
SUPPLEMENTAL INFORMATION: PERFORMED FIM 73-21 F/T 804, FOUND L ENG REQUIRES REPLACEMENT. REPLACED L ENG PER TASK CARD 71-999-00-01.
FLT. NO. N/A (MX). ESI - FOUND APU COOLING FAN DISCHARGE DUCT ASSY. DAMAGED. REPLACED APU COOLING FAN DISCHARGE DUCT PER AMM 49-51-03.
FLT NO. N/A. (MX). ESI - APU FAILED TO START. REPLACED APU STARTER PER AMM 49-41-01.
FLT NO. MGE410. EVENT. LEFT OIL PRESS ZERO FOLLOWED BY LEFT ENG FAILURE DURING CLIMB OUT. QRH COMPLETED - AIR RETURN FOR OVERWEIGHT LANDING. THIS ITEM IS OPEN - AIRCRAFT IS CURRENTLY OUT OF SERVICE FOR FURTHER INSPECTION AND CORRECTIVE ACTION.
ESI - LEFT ENG SLOW TO START. REMOVED AND REPLACED L ENG STARTER PER AMM 80-11-01.
FLT NO. N/A (MX) ESI - FLT DECK TRIM AIR VALVE POSITION INDICATION BLANK ON EICAS. R/R TRIM AIR VALVE PER AMM 21-61-07. OPS CHECK NORMAL.
FLT NO. MGE300. ESI - RIGHT PACK TEMP INOP LIGHT (MEL 21-61-03). REMOVED AND REPLACED RIGHT PACK REHEATER IAW AMM 21-51-07. RIGHT PACK NORMAL.
FLT. NO: MGE300. ESI - L ENG BLEED OFF STATUS MSG. PERFORMED L ENG PNEUMATIC HEALTH CHECK FOUND HPSOV FAULTY. R/R L ENG HPSOV PER AMM 36-11-07.
FLT. NO: N/A (MX INSP). ESI - PERFORMED PNEUMATIC HEALTH CHECK ON L ENG AND FOUND HS PILOT FAULTY. R/R L ENG HS PILOT PER AMM 36-11-08.
FLT NO. N/A (MX INSP). ESI - FOUND APU ECU FAULT. REMOVED AND REPLACED ECU.
FLT NO. MGE710. ESI - LEFT GENERATOR DRIVE LIGHT INOP. REMOVED AND REPLACED LEFT ENGINE IDG.
FLT. NO. N/A (MX INSP.). ESI - FOUND P2 SENSOR FAULT ON ECU. REMOVED AND REPLACE P2 SENSOR.
FLT. NO. MGE710. ESI - APU PNEUMATICS INOP, ECU FLAGGED FLOW SENSING MODULE. REMOVED AND REPLACED FLOW SENSING MODULE.
FLT. NO. N/A (MX INSP.). ESI - FOUND LEFT ENG #1 IGNITER WORN. REMOVED AND REPLACE LEFT ENG #1 IGNITER.
L ENG BLEED VALVE DID NOT CLOSE ON ENGINE SHUTDOWN. REMOVED AND REPLACED LEFT ENGINE PRSOV IAW AMM 36-11-09 LEAK CHECK OK.
FOUND R PACK EXHAUST DUCT DAMAGED. REMOVED AND REPLACED EXHAUST DUCT PER AMM 21-51-00.
REPLACED APU SURGE VALVE DUE TO NO DUCT PRESSURE.
APU INOP DUE TO FAULY APU FUEL SHUTOFF VALVE ACTUATOR. R/R APU FUEL SHUTOFF VALVE ACTUATOR.
LEFT ENGINE REPACED DUE TO HAVING A HISTORY OF HUNG START AND HIGH EGT READINGS DURING TAKE OFF.
REFER TO LP 43189 ITEM 4 LEFT ENG FUEL VALVE IND. MEL 73-21-03. REMOVED AND REPLACED FUEL CONTROL UNIT PER AMM 73-21-01. OPS CHECK NORMAL.
RIGHT PACK TEMP EICAS MSG INTERMITTENT DISPLAYED AND R PACK OFF EICAS MSG WOULD NOT DISPLAY WHEN THE PACK WAS NOT OPERATING. DURING THE RIGHT PACK TEMP CONTROLLER BITE, THE ALTITUDE SWITCH WAS FLAGGED AND REPLACED PER THE APPLICABLE AMM. NO FAULTS WERE NOTED DURING THE BITE CHECK AFTER REPLACEMENT.
FUEL TEMP INDICATION INTERMITTENT AND PLACED ON MEL. THE FUEL TEMP WAS DETERMINED TO BE THE CAUSE OF THE DISCREPANCY AND REPLACED PER THE APPLICABLE AMM.
AFT DET FAN STATUS MESSAGE. R/R AFT BLOWER ASSEMBLY.
LEFT ENGINE ANTI ICE VALVE PLACED ON MEL DUE TO ISSUES DURING MANUAL OPERATION. ANTI ICE VALVE WAS REPLACED AND CONFIRMED OPERATIONAL PER THE APPLICABLE AMM.
AIRCRAFT ARRIVED WITH R ENG SEC CONT STATUS MSG DISPLAY ON THE LOWER EICAS. DURING INTERROGATION OF THE EPCS MAINTENANCE PAGE, ALL THE SECONDARY CHANNEL PARAMETERS WERE MISSING FROM THE RIGHT ENG. THE EEC WAS REPLACED AND CONFIRMED OPERATIONAL PER THE APPLICABLE AMM.
L ENG HPSOV FAILED DURING PNEUMATIC SYSTEM HEALTH CHECK. R/R HPSOV.
LEFT ENGINE BLEED VALVE MSG DURING ENG ANTI ICE OPERATION. HIGH STAGE SYSTEM FOUND FAULTY AND PLACED ON MEL INITIALLY. DURING A BLEED HEALTH CHECK, THE LEFT ENG HIGH STAGE PILOT WAS FOUND FAULTY AND REPLACED. THE HEALTH CHECK WAS PERFORMED AGAIN AND THE HIGH STAGE SYSTEM PASSED PER THE APPLICABLE AMM, THE MEL WAS THEN CLEARED.
LH ENG BLEED VALVE MSG DURING ENG COWL ANTI ICE OPERATION. HPSOV WAS SECURED CLOSED AND PLACED ON MEL. DURING A HEALTH CHECK OF THE HIGH STAGE SYSTEM PER THE AMM, THE HP PILOT FAILED THE CROSSOVER CHECK. THE HP PILOT WAS REPLACED AND CONFIRMED OPERATIONAL DURING THE HIGH STAGE SYSTEM HEALTH CHECK.
RH ENG BLEED OFF DURING COWL ANTI ICE OPERATION. RIGHT ENGINE ANTI ICE VALVE FOUND DEFECTIVE. VALVE WAS REPLACED AND CONFIRMED OPERATIONAL PER THE AMM.
R PACK TEMP EICAS MESSAGE INTERMITTENT. A DEFECTIVE PACK TEMP CONTROL VALVE WAS DISCOVERED AND REPLACED PER THE AMM.
R/R L ENG TAI VALVE IAW AMM 30-21-00.
APU PNEUMATICS INOP. R/R APU FLOW SENSING MODULE IAW AMM 49-53-08.
LEFT ENGINE HOT START OCCURED DURING THE ATTEMPT. FURTHER INSPECTION FOUND DISCREPANCIES IN THE 2.5 BLEED VALVE SYSTEM. ENGINE WAS REMOVED AND SENT FOR REPAIR. ONCE REPAIRED, ENGINE WAS RE-INSTALLED ON THE AIRCRAFT.
RIGHT ENGINE WAS REPLACED DUE TO A HIGH OIL CONSUMPTION.
AIRCRAFT AIR RETURN DUE TO RIGHT ENGINE EGT EXCEEDING LIMITATIONS DURING CLIMB. (DISCREPANCY IS CURRENTLY OPEN)
RH HF INOP IN FLIGHT. RH HF TRANSCEIVER FOUND DEFECTIVE AND REPLACED.
DURING ENGINE RUN, R ENG SEC CONT STATUS MESSAGE DISPLAYED ON EICAS. EEC WAS FOUND FAULTY AND REPLACED.
RH ENGINE REPLACEMENT ACCOMPLISHED DUE TO OUT OF LIMIT BORESCOPE FINDING DURING A SCHEDULED INSPECTION.
DURING SERVICING OF THE RH STARTER, THE DRAIN PORT WAS FOUND DAMAGED WHICH REQUIRED A REPLACEMENT OF THE STARTER.
WEATHER RADAR INOP. FURTHER INSPECTIONS FOUND A DAMAGED FLEXIBLE WAVEGUIDE WHICH WAS REPLACED AND CONFIRMED OPERATIONAL DURING THE WEATHER RADAR OPS CHECK PER THE APPLICABLE AMM.
ON 12/23/2021, ACFT AIR RETURNED TO GUAM AS A PRECAUTION DUE TO THE LEFT ENGINE EGT AT 655 ON CLIMB OUT. CONTINUOUSLY INDICATING IN YELLOW ON CLIMB. REMOVED AND REPLACED LEFT ENGINE PER AMM 71-00-02.
DURING C-CHECK INSPECTIONS, THE RIGHT WHEEL WELL PRESSURE DECK WAS FOUND WITH MULTIPLE AREAS OF SEVERE CORROSION THAT FELL OUTSIDE OF THE SRM LIMITATIONS. THE CORROSION WAS REPAIRED PER EO APA-0034-001.
DISCREPANCY: REPLACE DUE TO HISTORY L ENG REV CONT, L ENG SEC CONT. CORRECTIVE ACTION: R/R EEC ALTERNATOR REF AMM 73-21-05. OK FOR CONT SVC.
DISCREPANCY - LEFT MAIN FUEL TANK IND AT FUELING STATION INOP. CORRECTIVE ACTION - REMOVED AND REPLACED L FUEL LOAD SELECT INDICATOR IAW AMM 28-41-06. OPS CHECK OK.
DISCREPANCY: L MAIN FUEL TANK QTY IND AT FUELING STATION INOP. CORRECTIVE ACTION: REMOVED AND REPLACED L MAIN FUEL LOAD SELECT INDICATOR IAW AMM 28-41-06. OPS CEHCK OK.
COCKPIT TEMP RUNNING WARM. REMOVED AND REPLACED LEFT PACK CONDENSER REF AMM 21-51-10 PG 401.
APU STARTER BRUSHES WORN. REMOVED AND REPLACED APU STARTER REF AMM 49-41-01.
DISCREPANCY: "L ENG FIRE LP 1" DURING CLIMB OUT FROM PPG. CORRECTIVE ACTION: FOUND L ENG FIRE LP 1 DAMAGED. REMOVED AND REPLACED L ENG FIRE DETECTION 1 LOOP IAW AMM 26-11-01. OPS CEHCK OK.
DISCREPANCY: R ENG LH TR LWR BLOCKER DOOR DAMAGED. CORRECTIVE ACTION: REMOVED AND REPLACED BLOCKER DOOR IAW AMM 78-31-10. OPS CEHCK OK.
DISCREPANCY: L ENG START VALVE INOP CORRECTIVE ACTION: REMOVED AND REPLACED L ENG START CONTROL VALVE IAW AMM 80-11-02. OPS CEHCK OK.
DISCREPANCY: C2 HYD ELEC PUMP INOP CORRECTIVE ACTION: REMOVED AND REPLACED C2 HYD ELEC PUMP ELCU IAW AMM 29-11-67. OPS CEHCK OK.
CREW REPORTED L AUX PITOT EICAS MESSAGE DURING CLIMB OUT. REMOVED AND REPLACED L AUX PITOT PROBE IAW AMM 34-11-01. PERFORMED PROBE HEAT ADJUSTMENT AND TEST IAW AMM 30-31-00 PG 501. OPS CHECK GOOD.
LEFT ENGINE STARTER FAILED TO ENGAGE DUE TO A SHEARED SHAFT. STARTER WAS REPLACED AND AIRCRAFT WAS PLACED BACK INTO SERVICE
DISCREPANCY - L ENG OIL QTY IND FLUCTUATES IN FLIGHT CORRECTIVE ACTION - REMOVED AND REPLACED LEFT ENG OIL QTY TRANSMITTER IAW AMM 79-31-01. OPS CHECK AND LEAK CHECK OK.
DURING HEALTH CHECK, FOUND DISCREPANCY WITH L ENG HS PILOT VALVE PER AMM 36-00-22. REPLACED L ENG HS PILOT VALVE PER AMM 36-11-19. OPS AND LEAK CHK GOOD.
DURING HEALTH CHECK, FOUND DISCREPANCY WITH L ENG HPSOV PRESS. REGULATOR PER AMM 36-00-22. REPLACED L ENG HPSOV PRESS. REGULATOR. OPS AND LEAK CHK GOOD.
APU OIL PRESSURE DIFFERENTIAL INDICATOR FOUND EXTENDED DURING INSPECTION WHILE SERVICING OIL. FILTER WAS REPLACED ALTHOUGH NO CONTAMINATION WAS FOUND DURING INSPECTION OF THE REMOVED FILTER.
APU GENERATOR DIFFERENTIAL PRESSURE SWITCH WAS FOUND FAULTY AND REPLACED DUE TO AN APU FAULT DURING START. APU OPERATED NORMALLY AFTER REPLACEMENT.
APU IN FLIGHT START FAILED DUE TO A FAULTY INLET DOOR ACTUATOR. UNIT WAS REPLACED AND PLACED APU BACK INTO SERVICE.
APU OPERATING HIGH EGT AND EXCEEDED LIMIT... REPLACED APU ASSY.
WITH APU BLEED ON AND ONE PACK SWITCHED OFF, BLEEDS FLUCTUATE. REPLEACED FLOW SENSING MODULE.
REF LP 42712 MEL 49-11-01-01 APU PNUEMATIC FUNCTION. REMOVED AND REPLACED PILOT PRESSURE REGULATOR ON LH ENG REF AMM 36-00-23. OPS CHECK OK. MEL CLEARED.
LEFT ENG BLEED OFF AT FLIGHT IDLE. DISCREPANCY WAS DUE TO A CONFIRMED HP PILOT WHICH WAS REPLACED AND CONFIRMED OPRATIONAL DURING ENGINE RUNS.
LEFT ENG IDG WAS DEFERRED PER MEL 24-00-02 LP 42681 ITEM 3. REMOVED AND REPLACED LH ENG IDG IAW AMM 24-11-01 P401. OPS CHECK IAW AMM 24-11-00 P503 NORMAL. MEL CLEARED.
REF. LP 42673 MEL 36-11-02 LH ENG HPSOV SECURED CLOSED. REMOVED AND REPLACED LEFT ENG. PRSOV/HPG VALVE AUTO RELAY K10198. OPS CHECK OK. MEL CLEARED.
LEFT PDIU FAULT FOUND ON EPCS PAGE. PDIU WAS REPLACED.
LEFT GEN OFF AND LEFT BUS OFF DURING TAXI. MX FOUND A FAULTY BTB AT THE LEFT SYSTEM WHICH WAS REPLACED AND CONFIRMED OPERATIONAL DURING THE OPS CHECK.
AIRCRAFT AIR RETURNED DUE TO LEFT ENG BLEED OFF ON TOP OF CLIMB. HIGH PRESSURE SYSTEM WAS PLACED ON DEFERRAL.
APU DOOR STUCK OPEN DUE TO FAULTY INLET DOOR SWITCH. SWITCH WAS REPLACED, SYSTEM CONFIRMED OPERATIONAL.
REFER TO LOGPAGE 42666 ITEM 4. LEFT ENG BLEED LIGHT EXTINGUISHED DURING ENGINE RUN. REMOVED AND REPLACED PRSOV REGULATOR PER AMM 36-11-19. OPERATIONAL CHECK NORMAL.
REFER TO LOGPAGE 42606 ITEM 2. LEFT ENG BLEED OFF LIGHT. PERFORMED PNEUMATIC HEALTH CHECK REF AMM 36-00-22, FOUND PRESSURE REGULATING SHUT-OFF VALVE FAULTY. REMOVED AND REPLACED PRSOV PER AMM 36-11-09. OPERATIONAL CHECK NORMAL.
CABIN AUTO 1 INOP. REMOVED AND REPLACED #1 CABIN PRESSURE CONTROLLER IAW AMM 21-31-02. BITE TEST OK. NO FAULT NOTED.
RIGHT HF INOP. REMOVED AND REPLACED R HF TRANSCEIVER IAW AMM 23-11-03. RADIO CHECK NORMAL.
EICAS: L ENG. BLEED OFF, LOSS OF DUCT PRESSURE. REPLACED L ENG PRSOV REGULATOR.
APU AUTO SHUTDOWN ON BLOCK IN. APU ECU FOUND FAULTY. ECU REPLACED AND APU CONFIRMED OPERATIONAL.
LEFT HIGH STAGE PRESSURE SYSTEM WOULD NOT OPERATE AT IDLE UNTIL POWER IS INCREASED. ISSUE WAS FOUND DUE TO A FAULTY HPSOV AND HP PILOT. THIS FORM WILL ONLY REPORT THE HPSOV. THE HP PILOT WILL BE REPORTED ON A SEPARATE SDR.
LEFT HIGH STAGE PRESSURE SYSTEM WOULD NOT OPERATE AT IDLE UNTIL POWER IS INCREASED. ISSUE WAS FOUND DUE TO A FAULTY HPSOV AND HP PILOT. THIS SDR REPORTS THE HP PILOT, THE HPSOV WAS PREVIOUSLY REPORTED ON A SEPARATE SDR.
CABIN AUTO 2 INOP FOUND DUE TO A FAULTY CABIN PRESS CONTROLLER. CONTROLLER WAS REPLACED AND CONFIRMED OPERATIONAL
CABIN AUTO 1 STATUS MESSAGE DISPLAYED IN FLIGHT. ISSUE WAS ISOALTED TO A FAULTY AC MOTOR. UNIT WAS REPLACED AND CONFIRMED OPERATIONAL.
REFER TO LOGPAGE 42406 ITEM 1. RIGHT FORWARD FUEL BOOST PUMP INOP. FOUND AND REPAIRED BROKEN WIRE AT P33 PANEL IAW SWPM 20-30-12. FOUND INSTALLED BOOST PUMP REF LOGPAGE 42423 BAD FROM STOCK. RE-INSTALLED REMOVED FUEL BOOST PUMP IAW AMM 28-22-03. OPS CHECK NORMAL.
RH WINDOW HEAT INOP. ISSUE WAS ISOLATED TO A FAULTY WINDOW HEAT CONTROL UNIT WHICH WAS REPLACED AND CONFIRMED OPERATIONAL.
WX FAIL INTERMITTENTLY. REMOVED AND REPLACED WX RT WITH GOOD UNIT PER AMM 34-43-01. OPS CHECK AND BITE TEST OK.
DISCREPANCY: WX RADAR INOPERABLE. TRR FAIL INDICATION. GOOD TEST PATTERN BUT NO RETURNS. CORRECTIVE ACTION: REMOVED AND REPLACED WX RT, IAW AMM 34-43-01. GROUND OPERATIONS CHECK NORMAL.
DISCREPANCY WX RADAR FAIL/INOPERABLE + TERRAIN. CORRECTIVE ACTION: REMOVED AND REPLACED WX RT, IAW AMM 34-43-00. OPERATIONS CHECK NORMAL AND NO FAULT NOTED ON RT BITE TEST.
REF NRC CARD NO 001. FOUND ON A8 CHECK RIGHT ENGINE UPPER IGNITER LEAD CERAMIC BURNT OR MELTED. REMOVED AND REPLACED RIGHT ENGINE UPPER IGNITER LEAD. OPERATIONS CHECK OK, REF. AMM 74-21-01.
RIGHT PACK TEMPERATURE CONTROLLER ALT SWITCH BITE. REMOVED AND REPLACED RIGHT PACK ALTITUDE SWITCH, IAW AMM 21-51-17. PERFORMED RIGHT PACK TEMPERATURE CONTROLLER BITE TEST, IAW AMM 21-51-14 NORMAL.
CABIN AUTO INOPERABLE IN CLIMB (AIR RETURN). REMOVED AND REPLACED AUTO 2 AC MOTOR, PER AMM 21-31-05. PERFORMED AUTO 2 CABIN PRESSURE CONTROLLER POST INSTALLATION TEST, PER AMM 21-31-02 SATISFACTORY.
CABIN AUTO INOP IN CLIMB (AIR RETURN). REMOVED AND REPLACED OUTFLOW VALVE ACTUATOR, PER AMM 21-31-05. PERFORMED AUTO 2 CABIN PRESSURE CONTROLLER POST INSTALLATION TEST, PER AMM 21-31-02 SATISFACTORY.
DISCREPANCY, WX RADAR INTERMITTENT. CORRECTIVE ACTION: REMOVED AND REPLACED WXR ANTENNA WITH DRIVE UNIT ASSEMBLY, IAW AMM 34-43-05. OPERATIONS CHECK OK.
ETOPS SIGNIFICANT ITEM-RT HF TRANSCEIVER INOPERATIVE.
DISCREPANCY: APU INOPERABLE. CORRECTIVE ACTION: REMOVED AND REPLACED APU STARTER, IAW AMM 49-41-01. OPERATIONS CHECK OK.
CABIN ALT AUTO 2 STATUS MESSAGE. REMOVED AND REPLACED CABIN PRESSURE CONTROL 2, IAW AMM 21-31-02. OPERATIONAL CHECK NORMAL. NO FURTHER ISSUES AFTER.
RT ENGINE FIRE LOOP 2 STATUS MESSAGE DISPLAYED ON EICAS DUE TO A FAULTY FIRE DETECTOR ELEMENT. PART WAS REPLACED AND CONFIRMED OPERATIONAL.
LT ENGINE ANTI ICE VALVE WAS INOPERATIVE WHEN SELECTED IN FLIGHT. VALVE ASSEMBLY WAS REPLACED AND CONFIRMED OPERATIONAL.
RIGHT ENGINE START VALVE INOPERABLE. REMOVED AND REPLACED RIGHT ENGINE STARTER CONTROL VALVE IAW AMM 80-11-02. PERFORMED OPERATIONAL CHECK IAW AMM 70-00-00/201 SATISFACTORY.
L ENG BLEED VALVE EICAS MESSAGE ON CLIMB FL320 WITH ENG ANTI-ICE ON. REMOVED AND REPLACED LEFT REVERSE FLOW CHECK VALVE IAW AMM 35-11-18. PERFORMED OPERATIONAL CHECK IAW AMM 36-00-20 NORMAL
LEFT AND RIGHT BLEED FLUCTUATION ON APPROACH ASSOCIATED WITH HOT PACK TEMPERATURE. FOR TROUBLESHOOTING REPLACED LEFT PACK FLOW CONTROL VALVE.
LH ENG FUEL FLOW TRANMISTTER WAS FOUND LEAKING AT THE CASE ASSY. THE UNIT WAS REPLACED WITH NO ISSUES DURING THE OPERATIONAL CHECK
R ENG FIRE LP 1 EICAS MESSAGE. TROUBLESHOT PER FIM 26-11 FAULT TREE 802. PERFORMED FIRE LOOPS RESISTANCE CHECK PER TABLE 101 ALL CHECK WITHIN LIMITS. PROBLEM ISOLATED TO FIRE CONTROL PRINTED CARD M683. REMOVED AND REPLACED, PERFORMED ENG/APU/CARGO FIRE TEST SATISFACTORY.
RH ENG FIRE LOOP 1 STATUS MESSAGE. ISSUE WAS ISOLATED TO A DAMAGED FIRE LOOP CIRCUIT CARD
RH ENG LOW OIL PRESSURE LIGHT AND EICAS MESSAGE INTERMITTENT. MX FOUND AND REPLACED FAULTY LOW OIL PRESSURE SWITCH
RH ENG BLEED FLUCTUATED IN FLIGHT. MX FOUND AND REPLACED A LEAKING RFCC WITHOUT FURTHER DEFECTS
RH ENG IGNITION SYS 1 CIRCUIT BREAKER EXTENDED DURING START. ISSUE WAS ISOLATED TO A SHORTED IGNITION LEAD AND REPLACED WITHOUT FURTHER ISSUES
APU ABORTED START. TROUBLE SHOT AND FOUND STARTER BRUSHES WORN. REPLACED STARTER, PERFORMED OPERATIONAL CHECKS AND NUMEROUS STARTS WITH NO ISSUES. APU OK FOR SERVICE.
RH ENGINE HUNG START AFTER PUSHBACK. ASSOCIATED WITH EICAS MESSAGE R ENG SEC CONT. PROBLEM ISOLATED TO EEC REPLACEMENT. REPLACED RIGHT EEC -ENGINE IDLE RUN NORMAL.
RH FLIGHT MANAGEMENT COMPUTER FAILED PRIOR TO PUSHBACK. PART WAS REPLACED AND CONFIRMED OPERATIONAL
RH ENG STARTER HAD ABNORMAL FINDINGS DURING ROUTINE SERVICING. PART WAS REPLACED WITHOUT FURTHER DEFECTS
RH ENGINE BLEED FLUCTUATES IN FLIGHT. ISSUE WAS ISOLATED TO A LEAKING PNEUMATIC LINE AT THE HP LIOT WHICH WAS REPLACED
RIGHT ENG STARTER WAS REPLACED DUE TO OUT OF LIMIT CHIP DETECTOR FINDINGS DURING ROUTINE SERVICING OF THE STARTER.
L1 WINDOW ARCING IN FLIGHT. PROBLEM WAS ISOLATED TO A FAULTY WINDOW HEAT CONTROLLER
ETOPS SIGNIFICANT ITEM: REF. MEL FOR F/O PITOT PROBE EICAS MSG. REMOVED AND REPLACED F/O PITOT PROBE AND OPS CHECKED NORMAL PER AMM 30-31-00. CLEARED DMI PLACARD REMOVED.
ETOPS SIGNIFICANT ITEM: REF. MEL FOR CABIN ALT AUTO 2 STATUS MESSAGE, REMOVED AND REPLACED CABIN PRESSURE CONTROLLER 2 PER AMM 21-31-02. OPS CHECK NORMAL, NO FURTHER FAULT STATUS MESSAGE NOTED. CLEARED DMI PLACARD REMOVED.
MGE301 FLIGHT INTO PNI, CREW EXPERIENCED RIGHT ENGINE BLEED FAILURE ALONG WITH RIGHT PACK INOP. CREW FOLLOWED QRH AND LANDED SAFELY IN PNI. MAINTENANCE CREW REPLACED RH 14TH STAGE PILOT VALVE AND PERFORMED OPERATIONAL CHECK WITH NO ABNORMALITIES. AIRCRAFT PLACED BACK IN SERVICE.
L ENGINE ANTI-ICE INOPERATIVE.
DURING HEAVY MAINTENANCE PHASE "C" CHECK, FOUND UPPER SKIN SURFACE CORROSION ON HORIZONTAL STABILIZER REQUIRING MAJOR REPAIR.
DURING HEAVY MAINTENANCE PHASE "C" CHECK, FOUND DENT ON #1 ENGINE EXHAUST CONE REQUIRING REPAIR.
DISCREPANCY - TAT PROBE CAUTION MSG ASSOCIATED WITH LOTS OF AP, AT, VNAV, LNAV, EPR GAGE, SOME OF THE PERFORMANCE DATA. REMOVED AND REPLACED TAT CURRENT SENSING RELAY.
TAT PROBE CAUTION MESSAGE ASSOCIATED WITH LOTS OF OF AP, AT, VNAV, LNAV, EPR GAGE, SOME OF THE PERFORMANCE DATA. REMOVED AND REPLACED TAT PROBE.
APU REMOVED AND REPLACED DUE TO HIGH EGT HISTORY DURING OPERATION.
ETOPS SIGNIFICANT ITEM (NON-EVENT). WX RADAR ONLY WORKS INTERMITTENTLY.
ETOPS SIGNIFICANT ITEM (NON-EVENT). NR 1 ENG ANTI-ICE VALVE INOP.
APU DUCT PRESSURE LOW.
RT ENG BLEED OFF LITE, R PACK OFF LITE ON DURING CLIMB OUT.
HF RADIO DOES NOT TRANSMIT OR RECEIVE.
DURING CLIMB OUT, CAPTAIN`S AIRSPEED, VERTICAL SPEED, AND ALTIMETER FAILED. CREW AIR RETURNED TO DEPARTURE AIRPORT AND THE PROBLEM WAS ADDRESSED BY MX.
2 HOURS PRIOR TO LANDING, THE CAPT WINDSHIELD SHATTERED. THE FLIGHT CREW DECLARED AN EMERGENCY, DESCENDED IN ALTITUDE AND LANDED SAFELY AT 0846Z.
CAPT WINDSHIELD SHATTERED 1 HOURS AFTER TAKE OFF, PRIOR TO THE WINDSHIELD SHATTER, CREW NOTICED ARCING IN FIGHT. WINDSHIELD AND WINDOW HEAT CONTROLLER WAS REPLACED PER APPLICABLE AMM, ALL TEST VERIFIED SATISFACTORY PER OPS CHECK IN APPLICABLE AMM.
AFT CARGO FIRE BOTTLE NR 2 DISCHARGE LINE BROKEN. REPLACED DISCHARGE LINE TUBE PER AMM 26-23-02. WORK ACCOMPLISHED ON ATS JOB 722361 NRC 00348.
CARGO FIRE BOTTLE SUPPORT ANGLE CRACKED AT BS 1188 WL 16 161 LBL 5. REMOVED, FABRICATED AND REPLACED IAW SRM 51-40-02, 51-20-01 AND DWG 453N2800 AS DOCUMENTED ON ATS JOB 722361 CARD 00300.
FWD ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED LIGHT AND PERFORMED SATISFACTORY LIGHT TEST PER AMM 33-51-06. DOCUMENTED ON ATS JOB 722361 CARD 00061.
FIRE BOTTLE ATTACH ANGLE CRACKED AT BULKHEAD 1180 LBL 5 WL188. REMOVED, FABRICATED AND INSTALLED ANGLE IAW SRM 51-40-02, SRM 51-40-05, SRM 51-20-01 AND DWG 453N2700 AS DOCUMENTED ON ATS JOB 722361 CARD 00318.
PUNCTURE IN FLOOR PNL FWD CARGO COMPARTMENT BS 688. REMOVED, FABRICATED AND INSTALLED FLOOR PNL PER SRM 51-40-05, 51-40-02, 51-40-03, 51-40-06, 51-20-01 AND DWG 453N1805 AS DOCUMENTED ON ATS JOB 722361 CARD 00056.
MAIN CARGO BAY FLOOR SPLICE BS 1020 IS CRACKED AT CARGO HANDLING SIDE RAIL ATTACH POINT LBL50. DOCUMENTED ON ATS JOB 722361 CARD 00019. REMOVED AND FABRICATED, INSTALLED NEW SPLICE PLATE PER DWG 144N5020 AND SRM 51-40-02.
DAMAGED FLOOR SUPPORT BS1016 WL208.10 LBL 25-LBL 45. REMOVED AND REPLACED PER SRM 51-40-02 AS DOCUMENTED ON ATS JOB 722361 CARD 00274.
FUSELAGE SKIN DENT BS 1400 3" BELOW STR 25L. REPAIRED PER ER 17-01586 ON JOB 722361.
BS 1640 BULKHEAD UPPER SUPPORT LBL8 HAS CORROSION ON AFT SIDE(LVL 2). REMOVED, FABRICATED AND REPLACED SUPPORT (MAJOR REPAIR) PER SRM 51-21-14, 51-21-15, 51-40-02, 53-60-53 AND DWG PL 453N1010. WORK ACCOMPLISHED ON ATS JOB 722361 CARD 00304.
NR 2 PYLON FWD SUPPORT FOR PNL NR 445AR CHAFED FWD SUPPORT (CHORD). REMOVED AND REPLACED PER SRM 51-40-05, 51-40-08 DWG 313N3052 AND 313N3018 AND SRM 51-40-02 WORK ACCOMPLISHED ON ATS JOB 722361 NRC 00279.
LVL 2 CORROSION ON MAIN CARGO DOOR HINGES 3-6. REMOVED AND REPLACED HINGES PER ER 17-01722 REV 1R DTD 3/21/2017 WITH 8110-0 DTD MARCH 20 2017. WORK DOCUMENTED ON JOB 722361 CARD 00118
LT WINGLET LWR AFT CORNER HAS AREA OF CORROSION BLENDED AND REFINISHED PER ER-17-01606 REV 1R, CORROSION LVL 1, MAJOR REPAIR. WORK ACCOMPLISHED ON JOB 722361 CARD 00294.
LT WING ATTACH BRACKET ABOVE FWD END OF TRUNNION LINK IS GOUGED. REMOVED AND REPLACED ATTACH BRACKET PER SRM 51-40-02 AND GOOD FUNCTIONAL CHECK OF BONDING WIRE PER SWPM 20-20-10. WORK ACCOMPLISHED ON JOB 722361 NRC 00150.
LT PYLON CUTOUT FOR PNL 434BL, AFT FLANGE IS CHAFED. REMOVED, FABRICATED AND REPLACED AFT FLANGE (PLATE) PER SRM 54-51-71, 51-40-02 AND DWG 313N3022. WORK PERFORMED ON JOB 722361 NRC 00282.
FORWARD ACCESS DOOR 113AL CORRODED AT AFT EDGE AND NEAR DRAIN VALVE, CORROSION LEVEL 2. REPAIRED PER ER 17-01609 REV 1R WORK DOCUMENTED ON JOB 722361 CARD 00124.
ON DESCENT INBOUND, AIRCRAFT EXPERIENCED R1 WINDOW OUTER PANE HAD CRACKED. EMERGENCY PROCEDURES WERE FOLLOWED AND ACFT LANDED IN THE NEAREST SUITABLE AIRPORT, SAFTELY.