N583UP
Registered owner: UNITED PARCEL SERVICE CO, KY (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
FOUND RT WING OTBD FLAP SUPPORT STRUT LOWER INSERT, COVE ATTACH WORN OUT , WBL 695. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" AROUND HEATED AREA , IAW NDT MANUAL PART 1 51-01-01 REV:182. NO DEFECT WAS FOUND
FOUND MAIN DECK SIDE CARGO DOOR SAFETY NET FRAYED. (REPLACE)
FOUND NR 1 MAIN ENTRY DOOR ROTARY SNUBBER OUT OF LIMITS.
CHAFING- EDGE, NR 2 ENG RT T/R LOWER FORWARD DOOR AFT SIDE. (REPLACE) PAPER FINAL CHECK COMPLETED
CHAFING - BRACKET , NR 1 ENG LT CORE COWL SUPPORT ROD SUPPORT FITTING. (REPLACE). INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.107 AND GOODRICH CMM IPL 71-13-23 REV.47. REVIEWED TASK PER GMM-MTX 09.05.01.09.
DEBONDED SKIN, LOWER FACE OF LT WING NR 3 FLAP TRACK AFT FAIRING. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" AROUND HEATED AREA , NDT MANUAL PART 1 51-01-01 REV:182. NO DEFECT WAS FOUND.
NR 26 V.C FLAP, OUTBOARD MOLDING SEAL DAMAGE. (REPAIR) 1. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP : 1.1 REMOVE THE RAIN EROSION SHIELDS AND CLEAN. 1.2 APPLY THE SEALANT TO REPAIR AREA CURED AT 70ðF FOR 48 HOURS. 2. CONDITION CHECK IS SATISFACTORY. 3. ATTACHMENTS ARE UPLOADED.
EROSION, L/E, NR 4 PYLON 481B PANEL. IAW SRM 54-51-70-1A-1, REV 107. REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR. REMOVE THE ERODED MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA ( L : 5.7", W : 0.3", D : 1 PLY, AT L/E, 22.5" FROM OUTBD EDGE ). APPLY ADHESIVE TO THE REPAIR AREA, CURED AT 80F FOR 10 HOURS. CONDITION CHECK IS SATISFACTORY.
CHAFED RUB STRIP, NR 3 ENG LT CORE COWL T/E INNER UPPER SIDE.
BROKEN- MOLDING SEAL, L/H WING NO.3 V.C FLAP INBD SIDE CORD MOLDING. (REPAIR) 1. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP : 1.1 REMOVE THE RAIN EROSION SHIELDS AND CLEAN. 1.2 APPLY THE SEALANT TO REPAIR AREA CURED AT 70ðF FOR 48 HOURS. 2. CONDITION CHECK IS SATISFACTORY. 3. ATTACHMENTS ARE UPLOADED.
NO.22 V.C FLAP INBOARD MOLDING SEAL DAMAGE. (REPAIR) 1. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP : 1.1 REMOVE THE RAIN EROSION SHIELDS AND CLEAN. 1.2 APPLY THE SEALANT TO REPAIR AREA CURED AT 70ðF FOR 48 HOURS. 2. CONDITION CHECK IS SATISFACTORY. 3. ATTACHMENTS ARE UPLOADED.
CHAFED RUB STRIP, NR 3 ENG RT CORE COWL T/E INNER UPPER SIDE.
NR 7 FLAP TRACK AFT TAIL CONE, LOWER SKIN FOUND TAPE APPLY. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" AROUND HEATED AREA , IAW NDT MANUAL PART 1 51-01-01 REV:182. NO DEFECT WAS FOUND.
DEBONDED SKIN, LOWER FACE OF LT WING NR 4 FLAP TRACK AFT FAIRING. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" AROUND HEATED AREA, IAW NDT MANUAL PART 1 51-01-01 REV:182. NO DEFECT WAS FOUND
FAULT- CHAFING- BRACKET ASSY, NO.3 ENG L/H CORE COWL HOLD OPEN ROD STOWAGE. (REPLACE). INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.107 AND GOODRICH CMM IPL 71-13-23 REV.47. REVIEWED TASK PER GMM-MTX 09.05.01.09.
CHAFED RUB STRIP, NR 3 ENG RT CORE COWL INNER FACE AFT UPPER EDGE.
CHAFED BRACKET ASSY, NR 3 ENG RT CORE COWL HOLD OPEN ROD STOWAGE. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.107 2. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.107 AND CMM IPL 71-13-24 REV.50 3.
BROKEN- MOLDING SEAL, L/H WING NO.9 V.C FLAP INBD SIDE MOLDING. (REPAIR) 1. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP : 1.1 REMOVE THE RAIN EROSION SHIELDS AND CLEAN. 1.2 APPLY THE SEALANT TO REPAIR AREA CURED AT 70ðF FOR 48 HOURS. 2. CONDITION CHECK IS SATISFACTORY. 3. ATTACHMENTS ARE UPLOADED.
**SDR FILED OPEN** FAULT- BROKEN- MOLDING SEAL, L/H WING NO.1E V.C FLAP INBD SIDE MOLDING. (REPAIR) 1. I.A.W. 747-400F SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP : 1.1 REMOVE THE RAIN EROSION SHIELDS AND CLEAN. 1.2 APPLY THE SEALANT TO REPAIR AREA CURED AT 70ðF FOR 48 HOURS. 2. CONDITION CHECK IS SATISFACTORY. 3. ATTACHMENTS ARE UPLOADED.
CHAFED RUB STRIP, NR 3 ENG LT CORE COWL INNER FACE AFT UPPER EDGE.
NR 2 ENGINE INLET COWL 12 O CLOCK POS . CRACK MEASURES 11IN PART IS ON TABLE IN S/M SHOP. BEGAN REMOVAL OF INLET LIP SKIN SECTION. ALL RIVETS REMOVED. SOME TOPSIDE HI-LOKS REMOVED (HAVE TO BE DRILLED). IAW SRM 51-40-02
NR 2 ENGINE INLET COWL 12 O CLOCK POS . CRACK MEASURES 11IN DRILLED 4 EA. COUNTERSINK HOLES FOR HOIST SLING ATTACHMENT POINT PLUGS (BOLTS) I/A/W SRM 51-40-02. INLET SKIN SEALANT APPLIED I/A/W CMM 71-11-16.
DURING WALKAROUND FOUND FLOOR PANEL NEAR 15L SPONGY. INSTALLED FLOOR PANEL REF AMM 53-21-02. REF GMM 04-02. PERFORMED A FINAL GVI FOR THE REPLACEMENT OF FLOOR PANEL 15L NO DEFECT NOTED. OK FOR RETURN TO SERVICE. C/W PER SREO-42648-REQ1 THIS CLEARS DEFERRAL
FOUND CRACK AT FORWARD LOWER CARGO DOOR CUTOUT AFT LOWER CORNER. C/W EO 95458-REQ1.
FOUND FLOORBOARD ABOVE AFT EQUIPMENT COOLING FANS DAMAGED, APPROX STA 2270, LEFT OF CENTER, ROUTED TO SHEETMETAL. OKAY TO INSTALL FABRICATED FLOORBOARD LOCATED AROUND STA 2270. DONE PER GMM 04-02. INSTALLED FLOOROARD. REF AMM 53-21-02.
OPEN, DURING CRUISE FLIGHT #4 ENG. OIL QUANITY DROPPED TO ZERO. OVER THE NEXT 20 MINUTES THE OIL PRESSURE DROPPED STEADILY REACHIMG 10 PSI(RED ZONE) THEN IT FLUCTUATED BETWEEN 10-13 BEFORE STEADY RED WE SHU C/W MASTER CHIP DETECTOR INSPECTION REFERENCE: TASK 79-21-05-202-024-J00 AT REQUEST OF POWER PLANT ENGINEERING , NO DEFECTS NOTED
DURING CRUISE FLIGHT #4 ENG. OIL QUANITY DROPPED TO ZERO. OVER THE NEXT 20 MINUTES THE OIL PRESSURE DROPPED STEADILY REACHIMG 10 PSI(RED ZONE) THEN IT FLUCTUATED BETWEEN 10-13 BEFORE STEADY RED WE SHU #4 ENGINE CHANGED.C/W MASTER CHIP DETECTOR INSPECTION REFERENCE: TASK 79-21-05-202-024-J00 AT REQUEST OF POWER PLANT ENGINEERING , NO DEFECTS NOTED.
**SDR FILED OPEN**FAULT - AGING A/C INSPECTION: FOUND NO.2 FLAP TRACK GENEVA CAM SUPPORT ROLLER WORN OUT 1EA. (REPLACE) COMPLETED SDR
AGING A/C INSPECTION: FOUND NO.1 FLAP TRACK GENEVA CAM SUPPORT ROLLER WORN OUT 1EA. (REPLACE) COMPLETED SDR. OPEN
AGING A/C INSPECTION: FOUND NO.2 FLAP TRACK GENEVA CAM SUPPORT ROLLER WORN OUT 1EA. (REPLACE). REPLACED WORN CAM SUPPORT ROLLER PER AMM 27-51-00.
AGING A/C INSPECTION: FOUND NO.1 FLAP TRACK GENEVA CAM SUPPORT ROLLER WORN OUT 1EA. (REPLACE). REPLACED WORN CAM ROLLER. AMM 27-51-00.
NUMBER 15 KRUEGER FLAP BULLNOSE FITTING LINK CORROSION (2EA) (AGING A/C INSPECTION) (REPLACE). INSTALLED KRUEGER FLAP BULLNOSE FITTING PER AMM: 27-81-00.
FOUND MAIN DECK CARGO HANDLING TRAY OF LOCK ROLLER TRAY ASSY CORROSION AT STA 1940. .I.A.W AMM 25-58-01-004-001 AND AMM 25-58-01-404-006 REV.111 REPLACED LOCK ROLLER TRAY ASSY TOTAL 1 EA.
FOUND MAIN DECK FLOOR SUPPORT FITTING PLATE CORROSION AT 1720 RBL 18 (REPLACE). FABRICATE PARTS (P/N:457U1042-8) PER BOEING DWG NO:457U1042 SH 2 REV."A";PL REV."G"; PSDL REV."-" AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH 9.08 REV: 7B REQUIREMENT. I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE.
*SDR FILED OPEN* FAULT - FOUND MAIN DECK FLOOR FITTING PLATE WORN AT STA 651 LBL 90. (REPLACE) OK TO WORK
FOUND MAIN DECK FLOOR FITTING PLATE WORN AT STA 651 LBL 90. (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED FITTING.
FOUND NO.3 SPOILER NEW PARTS SKIN DENT. (REPAIR). ERFORM DETAIL CLEAN AND EDGE SEAL AT REPAIR AREA I.A.W. 747-400F SRM 51-70-10-2R-0 PARAGRAPH 22 REV.101. I.A.W AMM 51-24-11-477-083 REV.111, REPAINT REWORK AREA. JOB COMPLETED AND CONDITION CHECK NORMAL AND PARTS INFO ATTACHED.
LOWER FACE OF MAIN DECK CARGO FLOOR BEAM SUPPORT, STA 1820, RBL 13.
*SDR FILED OPEN* FAULT - CORROSION - STRIP, LOWER FACE OF MAIN DECK CARGO FLOOR BEAM SUPPORT, STA 1820, RBL 36 (REPLACE) OK TO WORK
CORROSION - STRIP, LOWER FACE OF MAIN DECK CARGO FLOOR BEAM SUPPORT, STA 1820, RBL 36 (REPLACE). .I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE. I.A.W. AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND. REVIEW COMPLETE
CORROSION - STRIP, LOWER FACE OF MAIN DECK CARGO FLOOR BEAM SUPPORT, STA 1880, LBL 54, TOTAL: 1EA (REPLACE) OK TO WORK. OPEN
*SDR FILED OPEN* FAULT - CORROSION - STRIP, LOWER FACE OF MAIN DECK CARGO FLOOR BEAM SUPPORT, STA 1880, LBL 36 (REPLACE) OK TO WORK
CORROSION - STRIP, LOWER FACE OF MAIN DECK CARGO FLOOR BEAM SUPPORT, STA 1880, LBL 36 (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE. I.A.W. AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - STRIP, LOWER FACE OF MAIN DECK CARGO FLOOR BEAM SUPPORT, STA 1860, LBL 36 AND LBL 52, TOTAL: 2EA (REPLACE) OK TO WORK. OPEN
CORROSION - STRIP, LOWER FACE OF MAIN DECK CARGO FLOOR BEAM SUPPORT, STA 1920 RBL 23 (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - STRIP, LOWER FACE OF MAIN DECK CARGO FLOOR BEAM SUPPORT, STA 1860, LBL 36 AND LBL 52, TOTAL: 2EA (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED FITTING AND PLATE. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - STRIP, LOWER FACE OF MAIN DECK CARGO FLOOR BEAM SUPPORT, STA 1880, LBL 54, TOTAL: 1EA (REPLACE). .I.A.W AMM 20-51-01-912-008 REV 111 REPLACED FITTING. .I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND. REVIEWED
CORROSION - STRIP, LOWER FACE OF MAIN DECK CARGO FLOOR BEAM SUPPORT, STA 1920, RBL 81 (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED FITTING. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - STRIP, LOWER FACE OF MAIN DECK CARGO FLOOR BEAM SUPPORT , STA 1580, LBL 80 (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED FITTING. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 760 LBL 20. (REPLACE). FABRICATE PARTS (P/N:457U1042-8) PER BOEING DWG NO:457U1042 SH 2 REV."A";PL REV."G" ; PSDL REV."-" AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH 9.08 REV: 7B REQUIREMENT. I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
*SDR FILED OPEN* FAULT - CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 1840 LBL 50 & LBL 60. (REPLACE) OKAY TO WORK
*SDR FILED OPEN* FAULT - CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE STA 2040 RBL 26. (REPLACE) OKAY TO WORK
*SDR FILED OPEN* FAULT - CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 1900 LBL 50 & LBL 60. (REPLACE) OKAY TO WORK
CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 1840 LBL 50 & LBL 60. (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE TOTAL 2EA. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 1820 LBL 50. (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
**SUPPLEMENTAL SDR** FAULT - CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE STA 2040 RBL 26. (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED FITTING. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND. REVIEW COMPLETE
FOUND MAIN DECK CARGO HANDLING TRAY OF LOCK ROLLER TRAY ASSY CORROSION AT STA 680. (REPLACE). REMOVE LOCK ROLLER TRAY ASSY PARTS TO NEW LOCK ROLLER TRAY I.A.W SRM 51-40-02-0G REV.101. I.A.W BOEING CMM 25-57-31 REV.08 REPLACED TRAY, NUT, RIVET AND PIN ASSY TOTAL 26 EA. JOB COMPLETED AND CONDITION CHECK NORMAL
CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 1900 LBL 50 & LBL 60. I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE TOTAL 2 EA. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 1800 LBL 50. (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED FITTING. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 800 LBL 30. (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED FITTING. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 800 LBL 80. (REPLACE). .I.A.W AMM 20-51-01-912-008 REV 111 REPLACED FITTING. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
FOUND MAIN DECK CARGO HANDLING TRAY OF LOCK ROLLER TRAY CORROSION AT STA 1940. (REPLACE). I.A.W AMM 25-58-01-004-001 AND AMM 25-58-01-404-006 REV.111 REPLACED LOCK ROLLER TRAY ASSY TOTAL 1 EA. JOB COMPLETED AND CONDITION CHECK NORMAL.
CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 1800 RBL 80. IAW AMM 20-51-01-912-008 REV 111 REPLACED PLATE. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - PLATE, MAIN DECK FLOOR PANEL SUPPORT PLATE, STA 1780 RBL 95. (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 680 RBL 20. (REPLACE). FABRICATE PARTS (P/N:457U1042-8) PER BOEING DWG NO:457U1042 SH 2 REV."A";PL REV."G" ; PSDL REV."-" AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH 9.08 REV: 7B REQUIREMENT. I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND
*SDR FILED OPEN* FAULT - CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 1820 LBL 50. (REPLACE) OKAY TO WORK
CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 640 LBL 95. (REPLACE). FABRICATE PARTS (P/N:457U1042-8) PER BOEING DWG NO:457U1042 SH 2 REV."A";PL REV."G" ; PSDL REV."-" AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH 9.08 REV: 7B REQUIREMENT. I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - PLATE, MAIN DECK FLOOR PNL SUPPORT PLATE, STA 1782 & 1798 RBL 90. (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE TOTAL 2 EA. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - PLATE, MAIN DECK FLOOR SUPPORT PLATE, STA 1880 LBL 50 & LBL 60. (REPLACE). I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE TOTAL 2 EA. .I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
MAIN DECK FLOOR SUPPORT PLATE LOWER SURFACE, STA 1820 LBL 60. (REPLACE). .I.A.W AMM 20-51-01-912-008 REV 111 REPLACED PLATE. I.A.W AMM 51-24-13-607-010 REV 111 APPLY CORROSION PREVENTIVE COMPOUND.
CORROSION - TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1770 RBL 10. (REPAIR). REPAIR DAMAGE AREA I.A.W EGAT WORK SHEET NO.40668 (SRM 53-00-52-2R-12 REV.101 DETAIL I ).
CORROSION - CHORD, MAIN DECK CARGO FLOOR BEAM UPPER CHORD, STA 980 LBL 90 (REPAIR). REPAIR DAMAGE AREA I.A.W UPS EO-91154-REQ1 REV2. JOB COMPLETED.
CORROSION - PLATE, MAIN DECK CARGO FLOOR PNL SUPPORT PLATE, STA 1500 LBL 10. (REPAIR) INSTALL FABRICATE PART I.A.W. SRM 51-40-02-0G REV.101 AND BOEING DWG NO:65B38407 SH 1 REV.C. PAPER CHECK OK.
CORROSION - CHORD, MAIN DECK FLOOR BEAM UPPER CHORD, STA 760 LBL 30~50. (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-91155-REQ1 REV.1 AND EGAT WORK SHEET NO.40674 ( SRM 53-00-51-2R-3 REV.101) THAT EO AND EGAT WORK SHEET ATTACH TO NRC:T3F18E004V3R2. JOB COMPLETED.
CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1882 RBL 98.58 (REPAIR). REPAIR DAMAGE AREA I.A.W.EGAT WORK SHEET NO.40650 ( SRM 53-00-52-2R-6 REV.101 ) AND UPS EO-91171-REQ1 REV.1 ( TATA ATTACHING TO NRC NO.T3F18004V31D. JOB COMPLETED.
CORROSION - CHORD, MAIN DECK FLOOR BEAM UPPER CHORD, STA 640 LBL 75.92 ~ LBL 98.58 (REPAIR). I.A.W AMM 20-51-01-912-008 REV 111 INSTALLED FITTING AT STA 600 TO STA 680 LBL 90 ~ 110. REPAIR DAMAGE AREA I.A.W UPS EO-91168-REQ1 REV1.
CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1920 LBL 33.69. (REPAIR). REPAIR DAMAGE AREA I.A.W UPS EO-91170-REQ1 REV1 AND EGAT WORK SHEET NO.40664 (SRM 53-00-52-2R-6 REV.101). JOB COMPLETED.
CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1782 RBL 10 (REPAIR). REPAIR DAMAGE AREA I.A.W EGAT WORK SHEET NO.40668 (SRM 53-00-52-2R-12 REV.101 DETAIL I ). JOB COMPLETRED.
CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1850 ~ 1860 RBL 10 (REPAIR). REPAIR DAMAGE AREA I.A.W. EGAT WORK SHEET NO.40665 ( SRM 53-00-52-2R-12 REV.101 DETAIL III ). JOB COMPLETED.
CORROSION - CHORD, MAIN DECK CARGO FLOOR BEAM UPPER CHORD, STA 980 LBL 100. (REPAIR). REPAIR DAMAGE AREA I.A.W UPS EO-91154-REQ1 REV2 THAT EO ATTACH TO NRC NO.T3F18E004V32L.
MAIN DECK CARGO TRACK LOWER SURFACE, STA 510 LBL 70. (REPAIR). INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.101 AND BOEING DRAWING NO:65B01874 SHEET 13 REV: B.
CORROSION - CARGO TRACK, MAIN DECK, CARGO TRACK LOWER SURFACE, STA 1810 RBL 10 (REPAIR). REPAIR DAMAGE AREA I.A.W EGAT WORK SHEET NO.40668 (SRM 53-00-52-2R-12 REV.101 DETAIL I ). JOB COMPLETRED.
*SDR FILED OPEN* FAULT - CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1782 RBL 10 (REPAIR) OKAY TO WORK
FAULT - CORROSION - PLATE, MAIN DECK CARGO TRACK LOWER SURFACE, STA 480~500 LBL 110.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV.101 INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.101 AND BOEING DWG N0: 65B08300 SHEET 6 REV:E
*SDR FILED OPEN* FAULT - CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1850 ~ 1860 RBL 10 (REPAIR) I.A.W AMM 25-57-01-004-193 REV 111 REMOVED STA 1850 ~ 1860 RBL 10 AREA PDU FOR ACCESS.
CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1823 RBL 10 (REPAIR). REPAIR DAMAGE AREA I.A.W EGAT WORK SHEET NO.40668 (SRM 53-00-52-2R-12 REV.101 DETAIL I ) AND UPS SREO-47894-REQ1 REV1. JOB COMPLETRED.
CRACK - FITTING, L/H WING NO.3 SPOILER ACTUATOR ROD END FITTING. (REPLACE). .I.A.W AMM 27-61-02-404-012 REV.111 STEP 3.I ADJUST NO.3 SPOILER TO FLAP CLEARANCE. COMPLETED RII CHECK FOR INSTALL NO.3 SPOILER REF WORK ACTION 3 & 6.
*SDR FILED OPEN* FAULT - CORROSION - CARGO TRACK, MAIN DECK, CARGO TRACK LOWER SURFACE, STA 1810 RBL 10 (REPAIR) OKAY TO WORK
*SDR FILED OPEN* FAULT - CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 2096 RBL 10. (REPAIR) CONDITION CHECK OK.
*SDR FILED OPEN* FAULT - CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 2095 LBL 11.33 (REPAIR) PERFORMED CHROMIC ACID ANODIZING I.A.W. WORK SHEET NO.:40604 STEP 12 AND SPWPS-AN-004 REV.:23 AND SPDS-AN-001 REV.:39 (REFER TO SHOP LOG NO:2024-0115)
*SDR FILED OPEN* FAULT - CORROSION - CHORD, MAIN DECK FLOOR BEAM UPPER CHORD, STA 880 LBL 78 (REPAIR) COMPLETED RII EI NO.F2024A53M-1918 SEQUENCE A STEP 14. REV.0
*SDR FILED OPEN* FAULT - CORROSION - CARGO TRACK, MAIN DECK, CARGO TRACK LOWER SIDE, STA 1810 RBL 98.58 (REPAIR) CONDITION CHECK OK.
*SDR FILED OPEN* FAULT - CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1830 RBL 98.58 (REPAIR) OKAY TO WORK
*SDR FILED OPEN* FAULT - CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1882 RBL 98.58 (REPAIR) CONDITION CHECK OK.
*SDR FILED OPEN* FAULT - R/H WING OUTBD AILERON LOWER T/E SURFACE A LOT OF PLACE CORROSION & DISCHARGER STATIC & UPPER SURFACE ONE PLACE (REPAIR) INSTALL RIGHT WING OUTBOARD AILERON FITTING AND WEDGE I.A.W SRM 51-40-02-0G REV.101 AND DWG NO:65B02149 SHEET 3 REV.B AND DWG NO:65B02154 SHEET 2 REV.D
CORROSION - CHORD, MAIN DECK FLOOR BEAM UPPER CHORD, STA 760 LBL 65~70. (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-91155-REQ1 REV.1 AND EGAT WORK SHEET NO.40674 ( SRM 53-00-51-2R-3 REV.101). JOB COMPLETED.
CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1954 RBL 10. (REPAIR). REPAIR DAMAGE AREA I.A.W. EGAT WORK SHEET NO.40665 ( SRM 53-00-52-2R-12 REV.101 DETAIL III ). .JOB COMPLETED.
FAULT - CORROSION - TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 520 LBL 90. (REPAIR). FABRICATED PART I.A.W EGAT WORK SHEET NO.40615. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.101 AND BOEING DWG NO:65B14747 SHEET 9 REV:B AND DWG NO: 65B14747 SHEET 7 REV:B REVIEW COMPLETE
CORROSION - CARGO TRACK, MAIN DECK, CARGO TRACK LOWER SIDE, STA 1810 RBL 98.58 (REPAIR). REPAIR DAMAGE AREA I.A.W.EGAT WORK SHEET NO.40655 ( SRM 53-00-52-2R-6 REV.101 ) AND UPS EO-91171-REQ1 REV.1.
DISBOND - SKIN, RH VERTICAL STABILIZER PANEL P/N: 186U1007-4 INNER SKIN, TOTAL: 2 AREA (COMPOSITE REPAIR).NDT PERFORM UT INSPECTION FOR REPAIRED AREA AND PLUS 6 INCHES AROUND HEATED AREA, PER NTM PART1 51-01-01 AND 51-40-00 REV:177, RESULT: NO DEFECT FOUND. CLEAN, SEAL AND FINISH THE REWORKED AREA I.A.W. 747-400F SRM 51-70-10-2R-0 PARAGRAPH 22 REV.101.
CORROSION - CHORD, MAIN DECK FLOOR BEAM UPPER CHORD, STA 880 LBL 78 (REPAIR). I.A.W AMM 20-51-01-912-008 REV 111 INSTALLED FITTING AT STA 840 TO STA 920 LBL 75. REFERENCE UPS EO-90994-REQ1 REV.1 FOR MAIN DECK CARGO FLOOR PANEL INSTALLATION.
*SDR FILED OPEN* FAULT - CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1823 RBL 10 (REPAIR) CONDITION CHECK OK.
CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 2095 LBL 11.33 (REPAIR). I.A.W AMM 53-21-02-004-001 REV.111 REMOVE MAIN DECK CARGO FLOOR PANELS AND PERFORM G.V.I CHECK RESULT WAS NORMAL. REFERENCE UPS EO-90994-REQ1 REV.1 FOR MAIN DECK CARGO FLOOR PANEL INSTALLATION. REPAIR DAMAGE AREA I.A.W EGAT WORK SHEET NO.40604 (SRM 53-00-52-2R-12 REV.101 DETAIL III ).
CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOEWR SURFACE STA 2070 RBL 10 (REPAIR). REPAIR DAMAGE AREA I.A.W. EGAT WORK SHEET NO.40665 ( SRM 53-00-52-2R-12 REV.101 DETAIL III ). JOB COMPLETED.
**SUPPLEMENTAL SDR** FAULT - CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 2096 RBL 10. (REPAIR). REPAIR DAMAGE AREA I.A.W EGAT WORK SHEET NO.40669 (SRM 53-00-52-2R-12 REV.101 DETAIL III ). JOB COMPLETRED. REVIEW COMPLETE
*SDR FILED OPEN* FAULT - CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1954 RBL 10. (REPAIR) OKAY TO WORK
RIGHT WING OUTBD AILERON LOWER T/E SURFACE A LOT OF PLACE CORROSION & DISCHARGER STATIC & UPPER SURFACE ONE PLACE (REPAIR). I.A.W AMM 20-51-01-912-008 REV.111 INSTALL RH WING OUTBD AILERON LOWER PANEL. CONDITION CHECK NORMAL.
CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOWER SURFACE, STA 1830 RBL 98.58 (REPAIR). REPAIR DAMAGE AREA I.A.W.EGAT WORK SHEET NO.40655 ( SRM 53-00-52-2R-6 REV.101 ) AND UPS EO-91171-REQ1 REV.1. JOB COMPLETED.
*SDR FILED OPEN* FAULT - CORROSION - CARGO TRACK, MAIN DECK CARGO TRACK LOEWR SURFACE STA 2070 RBL 10 (REPAIR) CONDITION CHECK OK.
R/H WING STA OLES 1525.45 FRONT SPAR FIXED PNL SUPPORT FITTING ROD CORROSION (AGING A/C INSPECTION). (REPLACE). I.A.W AMM 20-51-01-912-008 REV.111 REPLACED THE ROD.
**SDR FILED OPEN**FAULT - AGING A/C INSPECTION : FOUND NO.8 SPOILER SUPPORT FITTING COLLAR CRACK. (REPLACE) REVIEWED
AGING A/C INSPECTION : FOUND LH WING OUTBD AILERON T/E & DISCHARGE CORROSION. (REPLACE). I.A.W AMM 20-51-01-912-008 REV.111 INSTALL LH WING OUTBD AILERON LOWER PANEL. CONDITION CHECK NORMAL.
CORROSION - CHORD, MAIN DECK FLOOR BEAM UPPER CHORD, STA 640 LBL 97 (REPAIR). REPAIR DAMAGE AREA I.A.W UPS EO-91168-REQ1 REV1 THAT EO ATTACH TO NRC:T3F18E004V3UU. JOB COMPLETED
CORROSION - CHORD, MAIN DECK FLOOR BEAM UPPER CHORD, STA 740 LBL 5 ~ 10 (REPAIR). ACCOMPLISHED JOB I.A.W. UPS EO-91144-REQ1 REV.1- JOB COMPLETED.
R/H WING STA : OLES 1581 FRONT SPAR SURFACE ONE HI-LOCK COLLAR CRACK (AGING A/C INSPECTION). (REPLACE). INSTALL NEW FASTENER I.A.W SRM 51-40-02-0G REV.101 AND BOEING DWG NO:112U5630 SH.1 REV.A.
**SUPPLEMENTAL SDR** FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT L/H UNDER FLOOR, STA 1140, MID SPAR (REPAIR). ACCOMPLISH REPAIR PER EO-91079-REQ1 AND EGAT EI F2024A57M-1845, REV. 0 AND 1. REVIEWED
**SUPPLEMENTAL SDR** FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1100, S-20C (REPAIR). ACCOMPLISH REPAIR PER EO-91079-REQ1 AND EGAT EI F2024A57M-1845, REV. 0 AND 1. REVIEWED
**SUPPLEMENTAL SDR** FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1060+11", S-24C~S-25C (REPAIR). ACCOMPLISH REPAIR PER EO-91079-REQ1 AND EGAT EI F2024A57M-1845, REV. 0 AND 1 (REF. T3F18E004ZX7Q) PRIOR TO FURTHER FLIGHT. REVIEWED
**SUPPLEMENTAL SDR** FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1040 + 12", S-27C (REPAIR). ACCOMPLISH REPAIR PER EO-91079-REQ1 AND EGAT EI F2024A57M-1845, REV. 0 AND 1. REVIEWED
CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1060+6" S-25C (REPAIR). ACCOMPLISH REPAIR PER EO-91079-REQ1 AND EGAT EI F2024A57M-1845, REV. 0 AND 1.
**SUPPLEMENTAL SDR** FAULT - R/H WING STA OLES 1483.95 , 1493.45 FRONT SPAR FIXED PNL 2EA SUPPORT FITTING ROD CORROSION (AGING A/C INSPECTION). (REPLACE). I.A.W AMM 20-51-01-912-008 REV.111 REPLACED THE ROD. REVIEWED
**SUPPLEMENTAL SDR** FAULT - AGING A/C INSPECTION : FOUND NO.8 SPOILER SUPPORT FITTING COLLAR CRACK. (REPLACE) INSTALL NEW FASTENER I.A.W SRM 51-40-02-0G REV.101 AND BOEING DWG NO:65B11642 SH.1 REV.G. REVIEWED
CORROSION - CARGO TRACK MAIN DECK CARGO TRACK LOWER SURFACE, STA 1938 LBL 33.69 (REPAIR). REPAIR DAMAGE AREA I.A.W UPS EO-91170-REQ1 REV1 AND EGAT WORK SHEET NO.40664 (SRM 53-00-52-2R-6 REV.101) THAT EO ATTACH TO NRC.T3F18E004V3X1. JOB COMPLETED.
MAIN DECK CARGO TRACK LOWER SURFACE, BS 760-780 LBL 33.99 (REPAIR). FABRICATE PARTS IAW DWG NO:69B04257 SH 1 REV."E";PL REV."A" AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH 9.08 REV: 7B REQUIREMENT<BR>2. INSTALL WITH NEW PART IAW SRM 51-40-02-0G REV.101 AND BOEING DWG NO:65B38250 SH 17 REV: A AND SH 19 REV 3. JOB COMPLETED
AGING A/C INSPECTION: FOUND OUTBD SIDE UPPER SKIN CORROSION OF RH WING OUTBD MID FLAP . OPEN
R/H WING STA : OLES 1581 FRONT SPAR SURFACE ONE HI-LOCK COLLAR CRACK (AGING A/C INSPECTION). (REPLACE) REVIEWED
**SDR FILED OPEN**FAULT - R/H WING STA OLES 1525.45 FRONT SPAR FIXED PNL SUPPORT FITTING ROD CORROSION (AGING A/C INSPECTION). (REPLACE) 1. I.A.W AMM 20-51-01-912-008 REV.111 REPLACED THE ROD.<BR>2. COND CHECK NORMAL.<BR><BR>IPC VERIFIED AND SERVICEABLE TAG NO.:037893.<BR>ATTACHMENTS ARE UPLOADED.
**SDR FILED OPEN**FAULT - R/H WING STA OLES 1483.95 , 1493.45 FRONT SPAR FIXED PNL 2EA SUPPORT FITTING ROD CORROSION (AGING A/C INSPECTION). (REPLACE) 1. I.A.W AMM 20-51-01-912-008 REV.111 REPLACED THE ROD.<BR>2. COND CHECK NORMAL.<BR><BR>IPC VERIFIED AND SERVICEABLE TAG NO.:037894.<BR>ATTACHMENTS ARE UPLOADED.
*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT L/H UNDER FLOOR, STA 1140, MID SPAR (REPAIR) CHECK NORMAL.
*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1100, S-20C (REPAIR) CHECK NORMAL.
*SDR FILED OPEN* FAULT - CORROSION - CHORD, MAIN DECK FLOOR BEAM UPPER CHORD, STA 740 LBL 5 ~ 10 (REPAIR) CHECK NORMAL.
*SDR FILED OPEN* FAULT - CORROSION - CHORD, MAIN DECK FLOOR BEAM UPPER CHORD, STA 640 LBL 100 (REPAIR) OK TO WORK
*SDR FILED OPEN* FAULT - AGING A/C INSPECTION : FOUND LH WING OUTBD AILERON T/E & DISCHARGE CORROSION. (REPLACE) 1.REMOVE THE DAMAGED STRIPS. PREPARE THE BONDING SURFACES AND BOND THE NEW STRIPS WITH RESIN CURED AT 80ðF FOR 10 HOURS WITH CONSTANT PRESSURE I.A.W. 747 CMM 57-51-91 PARAGRAPH 1.F REV.207.<BR>2.CONDITION CHECK IS SATISFACTORY.<BR>3.ATTACHMENT ARE UPLOAD.
CORRODED PLATE, MAIN DECK CARGO FLOOR PANEL SUPPORT PLATE, STA 1500 RBL 10 (REPAIR) INSTALL FABRICATE PART I.A.W. SRM 51-40-02-0G REV.101 AND BOEING DWG NO:65B38407 SH 1 REV.C. PAPER CHECK OK.
*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1060+6" S-25C (REPAIR) CHECK NORMAL.
*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1040 + 12", S-27C (REPAIR) CHECK NORMAL.
*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1060+11", S-24C~S-25C (REPAIR) CHECK NORMAL.
AGING A/C INSPECTION: FOUND OUTBD SIDE UPPER SKIN CORROSION OF RH WING OUTBD MID FLAP . (REPAIR). ACCOMPLISH REPAIR PER EO-91145-REQ1 AND EGAT EI F2024A57M-2025, REV. 0 (REF. T3F18E0050D3G) PRIOR TO FURTHER FLIGHT.
CRACK - DURING PERFORM EO-26756-JIC002 FOUND SKIN CRACK AT STA 980 S-38R. (REPAIR). REPAIR DAMAGE AREA I.A.W EGAT WORK SHEET NO.40581, SRM 53-20-01-2R-2 REV.101 AND UPS EO-91158-REQ1 REV1. JOB COMPLETED.
CRACK - SKIN, UPPER FACE OF L/H WING NO.5 V.C. FLAP FOLDING NOSE, NEAR INBD ARM LOWER FITTING. (REPAIR). ACCOMPLISHED UPS EO-91129-REQ1 REV1.
CRACK - STRINGER, L/H WING NO.7 V.C FLAP INNER FACE STRINGER. (REPLACE). I.A.W AMM 27-81-02-404-010 REV.111 STEP E(6) TO E(33) ADJUST NO.7 V.C FLAP.
*SUPPLEMENTAL SDR* FAULT - FOUND L1 ENTRY DOOR LATCH ROLLER DAMAGED AT AFT-LOWER SIDE. IAW AMM 20-11-28-964-010 REV. 111 REPLACE L1 ENTRY DOOR LATCH ROLLER AT AFT-LOWER SIDE. ALL PAPERWORK C/W
FOUND L1 ENTRY DOOR LATCH ROLLER DAMAGED AT AFT-LOWER SIDE. OPEN
DISBOND RH VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL DISBOND P/N: 186U1007-4 (SHEET METAL RMV AND REINSTALL PNL). REMOVED THE EXISTING FASTENERS I.A.W SRM 51-40-02-0G REV.101. ACCOMPLISHED JOB I.A.W SRM 51-40-02-0G REV.101 AND UPS EO-90959-REQ1 REV1. JOB COMPLETED.
DISBOND, LH VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL DISBOND P/N: 186U1006-3 (REPLACE). REMOVED THE EXISTING FASTENERS I.A.W SRM 51-40-02-0G REV.101. ACCOMPLISHED JOB I.A.W UPS EO-90958-REQ1 REV1.
CRACKED BRACKET, ATTACH FRONT SPAR OF L/H WING INBD L/E UPPER RIB ILES 338. (REPLACE) REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV.101. INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.101 AND BOEING DWG NO: 65B13921 SH 2 REV:H, 112U2001 SH 5 REV:B.
*IN FLIGHT SHUT DOWN* AT FL350, #4 ENGINE SHOWED REDUCED THRUST AND DID NOT RESPOND TO THRUST LEVEL INPUT. THERE WERE NO EICAS MSGÃâ¬â¢S OR CAUTION INDICATIONS ON THE ENG PAGE. CREW ELECTED TO SHUT DOWN #4 ENGINE. R&R #4 ENGINE PS3 LINE NEAR 8 OÃâ¬â¢CLOCK POSITION BEHIND FAN DISCHARGE AIR TUBE IAW AMM 70-20-01. OPS AND LEAK CHECK GOOD. PERFORMED POWER ASSURANCE TEST #10 IAW AMM 71-00-00. ALL PARAMETERS NORMAL AND WITHIN LIMITS.
LH HAND WING LEADING EDGE FLAP #8 HAS 2 DENTS/WEAR MARKS WHERE IT APPEARS TO BE RUBBING STABILIZING BARS ON LEADING EDGE OF WING. FOUND NO DAMAGE TO STAB BARS RESTORED FINISHES. COMPLETED STEPS 1-4 AND 7 OF EO-89403-REQ1. C/W EO-89403-REQ1
*SDR FILED OPEN* LH WING LEADING EDGE FLAP #9 HAS DENT AROUND OUTBOARD HINGE. ACCOMPLISHED UT IAW NDTSPM PART 4, 51-00-00, MINIMUM MATERIAL REMAINING .032Ãâ¬?. ACCOMPLISHED HFEC IAW NDTSPM PART 6, 51-00-00 NO CRACKS DETECTEDÃâ¬Â¦
*SDR FILED OPEN* LH HAND WING LEADING EDGE FLAP #8 HAS 2 DENTS/WEAR MARKS WHERE IT APPEARS TO BE RUBBING STABILIZING BARS ON LEADING EDGE OF WING. FOUND DENT 13Ãâ¬? FROM OUTBD EDGE .6Ãâ¬? IN DIAMETER .020Ãâ¬? DEEP WITH .032Ãâ¬? MATERIAL REMAINING. FOUND SECOND DENT 22.5Ãâ¬? FROM OUTBD EDGE .5Ãâ¬? IN DIAMETER .009Ãâ¬? DEEP WITH .038Ãâ¬? MATERIAL REMAINING. DAMAGES LOCATED IN FOLDING NOSE SKIN ASSY. (65B15167)
*** SUPPLEMENTAL SDR *** LH WING LEADING EDGE FLAP #9 HAS DENT AROUND OUTBOARD HINGE. COMPLIED WITH EO-89401-REQ3
LEFT O/B MIDFLAP HAS THE LOWER SKIN PULLED AWAY FROM CORE AND IS DELAMINATED OUTBOARD OF #1 CANOE FAIRING.***SM39/LMX2***HGR*** FABRICATED, CLEANED AND INSTALLED CORE PLUG. STARTED 250 DEGREE CURE. REF: SRM 57-53-01-2R-1 REPAIR 1, AND SRM 51-70-07-0G-0. REPAIR CURED AND FINISHED REF SRM 51-70-07-OG-O AND 57-53-01-2R-1. THIS CLEARS THE DEFERRAL
*SDR FILED OPEN* LEFT O/B MIDFLAP HAS THE LOWER SKIN PULLED AWAY FROM CORE AND IS DELAMINATED OUTBOARD OF #1 CANOE FAIRING.***SM39/LMX2***HGR*** FABRICATED, CLEANED AND INSTALLED CORE PLUG. STARTED 250 DEGREE CURE. REF: SRM 57-53-01-2R-1 REPAIR 1, AND SRM 51-70-07-0G-0.
FAULT - FOUND APU FIRE SHUTDOWN MODULE SUPPORT CORROSION AT RIGHT BODY GEAR WHEEL WELL, STA 1457 WL 91 AREA ACCOMPLISHED PERMANENT REINFORCING REPAIR PER USP EO-84739-REQ1
FAULT - CORROSION - CHORD, VERTICAL STABILIZER AUXILIARY STRUCTURE FRONT SPAR, LE STA 6 B, STA 2280 ACCOMPLISHED PERMANENT REINFORCING REPAIR PER UPS EO-84712-REQ1
FAULT - CORROSION - MAIN DECK FLOOR BEAM, STA 2360, LBL - 47 (REPLACED)
FAULT - FOUND MAIN DECK FLOOR PANEL 241AG DISBOND, STA 1220 - 1264, LBL 97 - 117 (REPAIR) REVIEWED
FAULT - FOUND MAIN DECK FLOOR PANEL 241XF DISBOND, STA 1220 - 1260, LBL 11 - 33 (REPAIR) REVIEWED
FAULT - FOUND MAIN DECK FLOOR PANEL 241DG DISBOND, STA 1260 - 1300, LBL 33 - 76 (REPAIR) REVIEWED
FAULT - CRACK - FND UPPER DECK TENSION TIE FWD CHANNEL, AT R/H STA 840 (REPAIR), PLEASE SPECIFY THE REASON FOR "REJECT"
FAULT - CRACK, FND UPPER DECK TENSION TIE AFT CHANNEL, AT R/H STA 740 (REPAIR).
FAULT - CRACK, FND UPPER DECK TENSION TIE FWD CHANNEL, AT RH STA 820 (REPAIR) COMPLETED PAPER FINAL CHECK
FAULT - CRACK, FND UPPER DECK TENSION TIE FWD CHANNEL, AT L/H STA 840 (REPAIR) COMPLETED PAPER FINAL CHECK.
R/H SIDE FUSELAGE SKIN DENT AFT OF THE AFT CARGO DOOR STR 37R 38R COMPLIED WITH ALL WORK STEPS
EMERGENCY LIGHT IN-OP MAIN DECK CREW ENTRY DOOR AFT POSITION . RELAMP NO HELP ASSY P/N 30-0407-3 . REF # 342045.ITEM DEFERRED PER MEL 33-51-1-0 .REPLACED BATTERY & CHARGER ASSY AT POS M5170 IAW AMM 33 51 04, OPS CHECK GOOD THIS CLEARS M 735652. AIPC 24-34-00 50C.
INSPECTION TYPE: C3 EMERGENCY LIGHT LENS DAMAGE AT UPPER DECK DOORWAY PATH (L05734), IAW AMM 33-51-07-002-009, 33-51-07-402-015 REV 99.03. RPL UPPER DECK EMERGENCY LIGHT ASSY AND PERFORMED EMERGENCY LIGHT TEST, RESULT WAS SATISFACTORY.
INSPECTION TYPE: C3 UPPER DECK EMERGENCY LIGHT BASE BROKEN AT STA 410 (L5730), IAW AMM 33-51-07-002-009, 33-51-07-402-015 REV 99.03. RPL UPPER DECK EMERGENCY LIGHT BASE AND PERFORMED EMERGENCY LIGHT TEST, RESULT WAS SATISFACTORY.
INSPECTION TYPE: C3 ALTERNATE SURFACE FINISH AND OVERSIZED HOLES FOR SUPPORT (P/N : 65B38409-4) OF MAIN DECK OUTBOARD GUIDE RESTRAINT NEAR STA 2110 - 2200 RBL 98.58. REPAIR IAW BOEING SR 4-4884430222 AND UPS EO B747-5310-78041-A.
INSPECTION TYPE: C3 CRACK WAS FOUND ON BRACKET (P/N : 146U1020-17) IN AFT CARGO COMPONENT AT STA 1920. REPAIR IAW BOEING SR 4-4868001341 AND UPS EO B747-5310-78008-A.
INSPECTION TYPE: C3 CORROSION ON CLIP (P/N:65B07853-34) ON RT WING OUTBOARD LEADING EDGE CAVITY RIB ASSY NEAR OLES 1509.95. REPLACE NEW PART, IAW 747-400F SRM 51-40-02-0G, REV 89.00 AND BOEING DWG 65B07853 SH 3, REV A.
INSPECTION TYPE: C3 CORROSION ON FWD CARGO COMPARTMENT HANGER SUPPORT (P/N:453U1563-31) NEAR STA 986. REPLACE NEW PART, IAW 747-400F SRM 51-40-02-0G, REV 89.00, BOEING DWG 453U1563 SH 11 REV B DWG 453U1183 SH 1 REV B AND DWG 453U1183 SH 3 REV B.
ENROUTE, THE FO SMELLED AN ELECTRICAL ODOR AND NOTICED THE RIGHT SIDE WINDOW ARCING. TURNED THE RIGHT WINDOW HEAT OFF. RAN SMOKE, FIRE, FUMES, AND WINDOW DAMAGE CHECKLIST. CONTACTED MMOC AND DECIDED TO CONTINUE. REMOVED & REPLACED R2 WINDOW IAW AMM IAW 56-11-02/401.
INSPECTION TYPE:NA**ATB, AC OOS ** RESULTED IN ATB ON CLIMBOUT PASSING =11000' WHILE ACCELERATING THROUGH 310 KTS WITH AUTOPILOT ENGAGED "STAB TRIM 2", "STAB TRIM 3" ADVISORY EICAS MSG ILLUMINATED ALONG WITH >AUTOPILOT CAUTION MSG. EMERGENCY DECLARED, JETTISONED 110,000# OF FUEL, REBALANCED FUEL & PERFD DAMAGE ASSESS BEFORE LANDING. EMERG TERMINATED IN TAXI.COMPLETED BOW TS-B747-274000721ÿ½ALL TESTS COMPLETED SATISFACTORILYÿ½R/R TRIM CNTL SWITCHES MM27-41-1-401 & FCC-C MM 22-1-01/MM 22-10-00/501. R/R OF SRM-L MM 27-41-01 FCU-C, MM 27-51-51 AND STAB POSITION TRANSMITTER CENTER MM 27-48-01.
**AIR TURN BACK** DUE TO FLAPS PRIMARY AND FLAPS DRIVE EICAS USED.
INSPECTION TYPE:AOG DENTS ON FUSELAGE SKIN (P/N:65B04488-14) BETWEEN STA 1540 - STA 1560, S-44R TO S-46R. IN ADDITION, THE SHEAR TIE (P/N : 69B03680-1) HAS ALSO BEEN DAMAGED AT STA 1560, BETWEEN S-44R AND S-45R REPAIR IAW SRID : 3-4362758360 AND EO B747-5330-71198-A.
FOUND THE UPPER DECK EMERGENCY LIGHT INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY AND PERFORMED EMERGENCY LIGHT TEST, RESULT WAS SATISFACTORY, IAW AMM 33-51-04-902-001-001, REV 93.01.
FOUND THE UPPER DECK EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY AND PERFORMED AN EMERGENCY LIGHT TEST, RESULT WAS SATISFACTORY IAW AMM 33-51-04-902-001-001 REV 93.01.
CORROSION FOUND ON THE NR 3 RAM AIR DUCT INLET, FWD AREA NEAR BS 899.15. REPAIR IAW SRM 51-40-02-0G, REV 83.01.
CORROSION FOUND ON THE ANGLE OF THE NR 1 RAM AIR DUCT INLET, FWD AREA NEAR BS 899.15. REPAIRED IAW SRM 51-40-02-0G, REV 83.01.
CORROSION FOUND ON THE NR 3 RAM AIR DUCT INLET, FWD AREA NEAR BS 899.15. REPAIRED IAW SRM 51-40-02-0G, REV 83.01.
DAMAGE FOUND ON THE MAIN DECK CARGO FLOOR PANEL 212LF, BS 300.46 - 319.38. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B747-5320-42648-A.
DAMAGE FOUND ON THE MAIN DECK CARGO FLOOR PANEL 212PF, BS 319.99 - 340. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B747-5320-42648-A.
CORROSION FOUND ON THE UPPER DECK FLOOR SUPPORT BETWEEN BS 400 - 460, LBL 24.17. REPAIRED IAW SRM 51-40-02-0G, REV 83.01.
CORROSION FOUND ON THE LOWER WING TO BODY FAIRING SUPPORT FRAME AT BS 987, LBL 9, & RBL 9. REPAIR IAW SRID 3-4305694203, AND EO B747-5310-70055-A.
A CRACK WAS FOUND ON THE MAIN DECK FLOOR STRUCTURE NEAR BS 2280. REPAIRED IAW SRID 3-4305023558, AND EO B747-5310-70053-A.
CORROSION FOUND ON THE MAIN DECK FLOOR SUPPORT, BS 2118, LBL 98.58. REPAIRED IAW SRM 51-40-02-0G, REV 83.01.
CORROSION ON SEAT TRACK OF MAIN DECK AT BS 1580, LBL 98.58.REPAIR IAW SRID: 3-4311008769 AND EO B747-5310-69960-A
INSPECTION TYPE:D1, CORROSION ON WEB, SPLICE DOUBLER OF MAIN DECK FLOOR STRUCTURE BETWEEN STA 480 TO STA 540. INSTALL NEW PART IAW SRM 51-40-02-0G REV 83.01.
CORROSION FOUND ON THE SEAT TRACK, MAIN DECK AT BS 2102, LBL 98.58. REPAIR IAW SRM 53-00-52-2R-6, REV 83.01.
DAMAGE WAS FOUND ON THE MAIN DECK CARGO FLOOR PANEL 272NF AT BS 2139.98 - 2220. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B747-5320-42648-A.
CORROSION FOUND ON THE MAIN DECK CARGO SUPPORT BETWEEN BS 2188 - 2200, RBL 98.58. REPAIRED IAW SRID 3-4276577034, AND EO B747-5310-69843-A.
DAMAGE FOUND ON THE MAIN DECK CARGO FLOOR PANEL 272CF AT BS 2039.98 - 2139.82. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B747-5320-42648-A.
CRACK FOUND ON THE MAIN FLOOR SUPPORT AT BS 2343,NEAR RBL 56. REPAIRED IAW SRID:3-4281362936, AND EO B747-5310-69997-A.
INSPECTION TYPE:D1, COROSSION ON CAP UPPER OF MAIN DECK FLOOR STRUCTURE AT STA 720, NEAR RBL 98.58. REPAIR IAW EO B747-5310-69861-A.
BROKEN AND CORRODED MAIN DECK FLOOR SUPPORT AT BS 1800, RBL 117. REPAIRED IAW SRID: 3-4281362704 AND EO B747-5310-6996-A.
CORROSION FOUND ON THE UPPER CHORD OF THE MAIN DECK FLOOR STRUCTURE BETWEEN BS 1320 AND 1340, LBL 75.92. REPAIRED THE FLOOR SUPPORT IAW EO B747-5310-70012-A.
CORROSION FOUND ON THE UPPER CHORD OF THE MAIN DECK FLOOR STRUCTURE BETWEEN BS 1326, LBL 75.92. REPAIRED IAW EO B747-5310-70012-A.
INSPECTION TYPE:D1, CORROSION UPPER CHORD OF MAIN DECK FLOOR STRUCTURE AT STA 1280, RBL 75. REPAIR IAW SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 REV 83.01.
CORROSION FOUND ON THE UPPER CAP OF MAIN DECK FLOORBEAM AT BS 720, LBL 98.58. REPAIRED IAW EO B747-5310-70001-A.
CORROSION FOUND ON THE UPPER CAP OF MAIN DECK FLOORBEAM AT BS 480, LBL 100. REPAIRED IAW EO B747-5310-69999-A.
CORROSION FOUND ON THE UPPER CAP OF MAIN DECK FLOORBEAM AT BS 660, BETWEEN RBL 33.99 AND RBL 75.92. REPAIRED IAW SRID: 3-4286359239, AND EO B747-5310-70028-A.
CORROSION FOUND ON THE UPPER CAP OF THE MAIN DECK FLOORBEAM AT BS 1860, RBL 75.92. REPAIRED IAW SRID 3-4286334063, AND EO B747-5310-70000-A.
CORROSION FOUND ON THE UPPER CAP OF MAIN DECK FLOORBEAM AT BS 1800, RBL 98.58. REPAIRED IAW SRID 3-4286320620, AND EO B747-5310-70029-A.
CORROSION FOUND ON THE SEAT TRACK IN THE MAIN DECK AT BS 998, LBL 98. REPAIRED IAW SRM 53-00-52-2R-6, REV 83.01.
CORROSION FOUND ON THE SEAT TRACK IN THE MAIN DECK AT BS 965, LBL 97, REPAIRED IAW SRM 53-00-52-2R-6, REV 83.01.
CORROSION FOUND ON THE SEAT TRACK ON THE MAIN DECK AT BS 863 - 880, RBL 97. REPAIRED IAW SRM 53-00-52-2R-6, REV 83.01.
CORROSION ON UPPER CAP OF MAIN DECK FLOORBEAM AT BS 760, BETWEEN LBL 11.33 AND LBL 33.99. REPAIRED IAW EO B747-5310-69881-A.
CORROSION FOUND ON THE SEAT TRACK ON THE MAIN DECK AT BS 725, LBL 11.33. REPAIRED IAW EO B747-5310-69891-A, AND SRM 53-00-52, REPAIR 12, REV 83.01.
CORROSION FOUND ON THE CAP UPPER OF THE MAIN DECK FLOOR STRUCTURE AT BS 2060, BETWEEN LBL 33.69 AND RBL 11.33. REPAIRED IAW EO B747-5310-69966-A
CORROSION ON CAP UPPER OF MAIN DECK FLOOR STRUCTURE AT BS 600, NEAR LBL 11. REPAIR IAW EO B747-5310-69446-A.
CORROSION ON CAP UPPER OF MAIN DECK FLOOR STRUCTURE AT BS 800, LBL 112. REPAIR IAW EO B747-5310-69963-A.
CORROSION FOUND ON THE CAP UPPER OF MAIN DECK FLOOR STRUCTURE AT BS 2060, LBL 18. REPAIR IAW EO B747-5310-69966-A.
CORROSION FOUND ON THE SEAT TRACK OF MAIN DECK FLOOR STRUCTURE AT BS 992, LBL 98. REPAIRED IAW SRM 53-00-52-2R-6, REV 83.01.
INSPECTION TYPE:D1, COROSSION ON UPPER CAP OF MAIN DECK FLOOR STRUCTURE AT STA 1780, LBL 42.94. REPAIR IAW EO B747-5310-69825-A
INSPECTION TYPE:D1, COROSSION ON UPPER CHORD OF MAIN DECK FLOOR STRUCTURE AT STA 1960, NEAR RBL11.33. REPAIR IAW EO B747-5310-69798-A.
INSPECTION TYPE:D1, CORROSION ON UPPER CHORD OF MAIN DECK FLOOR STRUCTURE AT STA 1220, NEAR RBL 98.58. REPAIR IAW EO B747-5310-69797-A.
INSPECTION TYPE:D1, CORROSION ON CAP UPPER OF MAIN DECK FLOORBEAM AT STA 1860, NEAR RBL 75.92. REPAIR IAW EO B747-5310-69762-A.
INSPECTION TYPE:D1, CORROSION ON CAP UPPER OF MAIN DECK FLOOR STRUCTURE AT STA 1860, NEAR LBL 33.69. REPAIR IAW EO B747-5310-69801-A.
CORROSION FOUND ON THE UPPER CAP OF MAIN DECK FLOORBEAM AT BS 1840, BETWEEN LBL 11.33 AND RBL 11.33. REPAIR IAW SRID 3-4302144479, AND EO B747-5110-70015-A.
CORROSION FOUND ON THE UPPER CAP OF MAIN DECK FLOORBEAM AT BS 2280, LBL 68. REPAIRED IAW SRM 53-00-51-2R-3, REPAIR 3, REV 83.01 AND EO B747-5310-70107-A.
COROSSION FOUND ON THE UPPER CAP OF MAIN DECK FLOORBEAM AT BS 1860, BETWEEN LBL 11.33, AND RBL 11.33. REPAIR IAW SRID 3-431119191, AND EO B747-5310-70088-A.
INSPECTION TYPE:D1, CORROSION ON SEAT TRACK OF MAIN DECK FLOOR STRUCTURE AT STA 1487, NEAR LBL 11.33. REPAIR IAW EO B747-5310-69800-A.
INSPECTION TYPE:D1, CORROSION ON UPPER CHORD OF MAIN DECK FLOORBEAM AT STA 1940, NEAR RBL 33.69. REPAIR IAW EO B747-5310-69760-A.
INSPECTION TYPE:D1, CORROSION ON CAP UPPER OF MAIN DECK FLOOR STRUCTURE AT STA 1840, NEAR LBL 33.69. REPAIR IAW EO B747-5310-69764-A.
INSPECTION TYPE:D1, CORROSION ON SEAT TRACK OF MAIN DECK FLOOR STRUCTURE AT STA 1868, RBL 98. REPAIR IAW SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 REV 83.00.
INSPECTION TYPE:D1, CORROSION ON SEAT TRACK OF MAIN DECK FLOOR STRUCTURE AT STA 2135, RBL 88. REPAIR IAW SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 REV 83.00.
INSPECTION TYPE:D1, CORROSION ON UPPER CHORD OF MAIN DECK FLOOR STRUCTURE AT STA 1321, RBL 98. REPAIR IAW SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 REV 83.00.
INSPECTION TYPE:D1, CORROSION CHORD OF MAIN DECK FLOOR STRUCTURE AT STA 1460 AND STA 1464, RBL 75. REPAIR IAW SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 REV 83.01.
INSPECTION TYPE:D1, CORROSION CHORD OF MAIN DECK FLOOR STRUCTURE AT STA 1032, LBL 34. REPAIR IAW SRM 53-00-52-1A-1 ALLOWALBE DAMAGE 1 REV 83.01.
INSPECTION TYPE:D1, CORROSION ON UPPER CAP OF MAIN DECK FLOORBEAM AT STA 1800, BETWEEN RBL 75.92 TO RBL 98.58. REPAIR IAW EO B747-5310-69766-A.
CORROSION FOUND ON THE MAIN LANDING GEAR DOOR AREA SUPPORT STRUCTURE BEAM AT BS 1329, BETWEEN LBL 16 AND RBL 16. REPAIRED IAW EO B747-5320-69824-A.
INSPECTION TYPE:D1, CORROSION ON UPPER CAP OF MAIN DECK FLOORBEAM AT STA 1800, BETWEEN RBL 75.92 TO RBL 98.58. REPAIR IAW EO B747-5310-69766-A.
CORROSION FOUND ON THE MAIN LANDING GEAR DOOR AREA SUPPORT STRUCTURE BEAM AT BS 1308, BETWEEN LBL 16 AND RBL 16. REPAIR THE BEAM IAW EO B747-5320-69824-A.
CORROSION FOUND ON THE MAIN DECK SEAT TRACK AT BS 1895, LBL 33.69. REPAIRED IAW SRID:3-4305555651, AND EO B747-5310-69967-B.
CORROSION ON MAIN LANDING GEAR DOOR AREA SUPPORT STRUCTURE BEAM AT BS 1468, RBL 3. REPAIRED IAW EO B747-5320-69824-A.
CORROSION FOUND ON THE MAIN LANDING GEAR DOOR AREA SUPPORT STRUCTURE BEAM AT BS 1287, BETWEEN LBL 16 AND RBL 16. REPAIR IAW EO B747-5320-69824-A.
CRACKS FOUND ON THE LT HORIZONTAL STABILIZER TRAILING EDGE UPPER RIB AT HSS 421.5. REPAIRED IAW SRID 3-4281233668, AND EO B747-5510-69998-A.
CRACKS WERE FOUND ON THE LT HORIZONTAL STABILIZER TRAILING EDGE AT HSS BL 421.5. REPAIRED IAW SRID 3-4281233668, AND EO B747-5510-69998-A.
CRACKS WERE FOUND ON THE LT HORIZONTAL STABILIZER TRAILING EDGE LOWER RIB AT HSS 421.5. REPAIR IAW SRID 3-4281233668, AND EO B747-5510-69998-A.
CRACK FOUND ON THE NR 2 PYLON TEE FITTING, NAC STA 377.6. REPAIR IAW SRID 3-4318687981, AND EO B747-5410-70064-A.
INSPECTION TYPE:D1, CORROSION ON UPPER CAP OF MAIN DECK FLOORBEAM AT STA 1800, BETWEEN RBL 75.92 TO RBL 98.58. REPAIR IAW EO B747-5310-69766-A.
CORROSION ON CAP UPPER OF MAIN DECK FLOOR STRUCTURE AT BS 620, BETWEEN LBL 11.33 AMD RBL 11.33. REPAIRED IAW EO B747-5310-70011-A.
INSPECTION TYPE:D1, COROSSION ON CAP UPPER OF MAIN DECK FLOOR STRUCTURE STA 620, BETWEEN RBL 33.99 AND 55.5. REPAIR IAW EO B747-5310-69799-A.
CORROSION FOUND ON THE SHEAR WEB IN THE MAIN DECK, FLOOR STRUCTURE AT BS 520, NEAR RBL 80. REPAIRED IAW EO B747-5310-69945-A.
CORROSION FOUND ON THE UPPER CAP OF MAIN DECK FLOORBEAM AT BS 640, LBL 115. REPAIRED IAW SRID 3-4288692262, AND EO B747-5310-70030-A.
CORROSION FOUND ON THE SEAT TRACK IN THE MAIN DECK AT BS 1852, LBL 75.92. REPAIR IAW SRID 3-4305072151 AND EO B747-5310-69961-A.
CORROSION FOUND ON THE MAIN DECK SEAT TRACK AT BS 1871, LBL 33.69. REPAIRED IAW 3-4305555651 AND EO B747-5310-69967-B.
CORROSION FOUND ON THE MAIN DECK SEAT TRACK BS 1859, LBL 11.33 AND THE EXISTING REPAIRS WERE FOUND BETWEEN BS 1860 - 1880, & BS 1900 TO 1920. REPAIRED IAW SRID: 3-4308601451, AND EO B747-5310-69962-A.
INSPECTION TYPE:D1, CORROSION ON UPPER CAP OF MAIN DECK FLOORBEAM AT STA 1800, BETWEEN RBL 75-92 TO RBL 95.58. REPAIR IAW EO B747-5310-69766-A.
CORROSION FOUND ON THE BRACKET OF MAIN DECK CARGO DOOR AT BS 1780 - 1850. REPAIRED IAW EO B747-5320-69567-A.
CORROSION FOUND ON THE WEB AT BS 1241, RBL 94. REPAIRED IAW EO B747-5710-69975-A.
CORROSION FOUND ON THE WEB AT BS 1241, LBL 91. REPAIRED IAW EO B747-5710-69992-A.
INSPECTION TYPE:D1, CRACK ON RT WING NR 7 SPOILER SUPPORT FITTING. REPAIR IAW SRM 57-51-13 REPAIR 1 REV 83.01.
DAMAGE FOUND ON THE MAIN DECK CARGO FLOOR PANEL 261AF AT BS 1739.98 - 1859.82. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B747-5320-42648-A.
INSPECTION TYPE: 18, DENT DAMAGE ON FUSELAGE SKIN AT BS 1803, STRINGER 38R. REPAIRED THE SKIN IAW SRID 4-3907941343 AND EO B747-5330-66147-A.
UPPER DOCK EMERGANCY ESCAPE HARNESS HOLDER COVER HOOK AND LOOP WORN OUT. REPLACED THE COVER AND CHECKED OK IAW 25-60-00.
FOUND A PUNCTURE THROUGH OUTER SKIN OF MCD. REPAIRED IAW EO 5230-64430-A.
ISOLATORS AFT SIDE OF L1 DOOR DAMAGED. REPLACED 8 INTERIOR TRIM ISOLATORS IAW SRM 51 40.
ENG 3 FIRE LB B INTERMITTENT STATUS MESSAGE APPEARED AT CRUISE PHASE OF FLIGHT REPLACED NR 3 ENG LOOP B FIRE DET CARD ASSY PER MM 26 10 01. NO HELP A1983212 1-1-17. CLEARED AND SECURED CONNECTOR D4154P AND OPS CK GOOD PER MM 26 11 00.
AFTER LOADING AIRCRAFT, MAINTENANCE WAS CLOSING THE MAIN CARGO DOOR NORMALLY, THE DOOR STOPPED 2-3 INCHES SHOT OF CLOSING. MAINTENANCE THEN TRIED TO CLOSE THE DOOR MANUALLY BUT THE DOOR MECHANISM FAILED AND INTERNALLY PUNCHED A 1 INCH HOLE. FOUND BROKEN HOOK ACTUATOR ROD ASSY. R&R WITH NEW ROD ASSY PER AMM 52-32-11 AND PERFORMED SIDE CARGO DOOR OUTER SKIN AND INTERNAL BONDED DOUBLER PUNCTURE REPAIR AS PER EO B747-5230-62631A, OPS TEST OF MAIN DECK DOOR TEST NORMAL PER AMM 52-32-01/601.
MAIN DECK SIDE CARGO DOOR OUTER SKIN AND INTERNAL BONDED DOUBLER PUNCTURE REPAIR BETWEEN STA 1787-1793 WL 216. ACCOMPLISHED EO B747-5230-62631A DEFERRED TO EO B747-5230-62631-A DI D591902, MC NOTIFIED. A/C OK FOR SVC.
INSPECTION TYPE:N/A, EMERGENCY LIGHT (DM 1205895) MCD CARGO DECK CEILING INOP. RELAMPED NO HELP. R&R POWER SUPPLY PER MM 33-51-04. OPS CHECK GOOD. SOURCE REF 33-51-04
NR 11 LT KRUEGER FLAP OUTER SKIN DAMAGED. REPAIRED IAW EO B747-5740-62329-A.
INSPECTION TYPE: C4, A CRACK WAS FOUND ON THE FRAME DOUBLER AT BS 820 , STRINGER 10A TO 11L. REPLACED IAW EO B747-5310-62098-A.
INSPECTION TYPE: C4, CORROSION WAS FOUND ON THE MAIN DECK SEAT TRACK AT BS 1827 , LBL 75. REPAIRED IAW SRM 53-00-52-2R-6 REPAIR 6 REV.77 AND EO B747-5310-62130-A.
INSPECTION TYPE: C4, A CRACK WAS FOUND ON THE FRAME DOUBLER AT BS 840 , STRINGER 10A TO 11L. THE PART WAS REPLACED IAW EO B747-5310-62099-A.
INSPECTION TYPE: C4, A CRACK WAS FOUND ON THE FRAME DOUBLER AT BS 840 , STRINGER 10A TO 11R PART REPLACED IAW EO B747-5310-62099-A
INSPECTION TYPE :C4, A CRACK WAS FOUND ON THE FRAME AT BS 840 , STRINGER 10A TO 11R. REPLACED THE PART IAW EO B747-5310-62099-A.
INSPECTION TYPE: C4, A CRACK WAS FOUND ON THE FRAME DOUBLER AT BS 820 , STRINGER 10A TO 11R. REPAIRED IAW SRM 53-20-07-2R-R , REPAIR 2 REV.77 AND EO B747-5310-62098-A.
INSPECTION TYPE: C4, A CRACK WAS FOUND ON THE FRAME AT BS 820 , STRINGER 10A TO 11R. REPAIRED IAW SRM 53-20-07-2R-2 , REPAIR 2 REV.77 AND EO B747-5310-62098-A.
INSPECTION TYPE: C4, A CRACK WAS FOUND ON THE LT SIDE BODY GEAR W/W AFT BULKHEAD WEB AT BS 1480. REPAIRED IAW SRM 53-40-08-2R-1 REPAIR 1 REV.77 AND EO B747-5310-62128-A
SMOKE BARRIER DOOR TO UPPER DECK IS DIFFICULT TO OPEN AND CLOSE .ADJUSTED & LUBRICATED THE DOOR HINGE. ACFT OK FOR SERVICE.
HOLE IN FLOOR PANEL AT BS 2082 OB PANEL LESS THAN 3 INCHES. FABRICATED A NEW FLOOR PANEL IAW EO B747-5320-61311.
BLEED 1 EICAS, BLEED OVER PRESSURE 1, STATUS FRAME 36105900, FUEL DUMP 80.000 LBS, FOUND BLEED-1 PRESSURE REGULATING VALVE, CONTROLLER FAIL OPEN MSG 36226. DEFERRED NR 1 ENGINE PRV SYSTEM IAW MEL 36-11-8-3. R&R NR 1 ENG PRV AND PRVC PER MM 36-11-20 AND 36-11-10. NO DEFECTS NOTED. OPERATED ENG TO T/O POWER FOR 3 MINS. NO NR 1 ENG BLEED FAULTS. THIS CLEARS M580665. PLACARD REMOVED.
OIL QTY ON NR 2 ENGINE SLOWLY DROPPED. WHEN THE OIL QTY REACHED ONE QUART, CREW SHUTDOWN ENGINE AS A PRECAUTION. REPLACED BLOWN SEAL ON THE IN LINE FUEL/OIL HEAT EXCHANGER IAW AMM 79-21-01. ENGINE RAN FOR 30 MINS WITH NO LEAKS OR QTY LOSS.
LOWER AFT CARGO DOOR FWD LWR CORNER SKIN DAMAGED. REMOVED 4" X 5" OF DOOR SKIN. FILLER DOUBLER REPAIR IAW EO B747-5230-59472-B.
MCD FLOORBEAM HAS CORROSION ON UPPER CAP BS 1740, LBL 23.0 TEMPORARY REPAIR IAW EO B747-5310-59073-A. PERMANENT REPAIR WITHIN 250 FLIGHT CYCLES.
DAMAGED AREA AREA AROUND SEVERAL INSERTS FLOORBOARD PUNCTURED. THIS IS A MAJOR REPAIR FABRICATED A NEW FLOORBOARD REF EO B747-5320-58932-A.
SMOKE BARRIER ON RT SIDE WALL AFT OF BS 400, WORN AND TORN. REPAIRED IAW AMM 25-52-01-308-034.
INSPECTION TYPE:C, LT WING INBD MID FLAP UPPER T/E PANEL DELAMINATED. FIBERGLASS LAYUP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A, 1, FIG 5, REV 74.
INSPECTION TYPE: C, RT WING INBD FORE FLAP UPPER T/E WEDGE DELAMINATED. FIBERGLASS LAYUP REPAIR PERFORMED IAW SRM 51-70-07 PAR 5A, 1, FIG 5, REV 74.
INSPECTION TYPE: C, EMP FUSELAGE SKIN AT BS 2360, S15L FWD OF LT HORIZONTAL STABILIZER L/E FOUND CRACKED. EMP FUSELAGE SKIN AT BS 2360 TO 2380, STR S15L AREA REPAIRED IAW HX RI NO RI-53-61-11023, REV A AND EO B747-530-58327-A. CLASSIFIED AS A MAJOR REPAIR.
INSPECTION TYPE: C, RT WING INBD FORE FLAP L/E FAIRING DELAMINATED. FIBERGLASS LAYUP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A, 1, FIG 5, REV 74.
INSPECTION TYPE: C, RT WING INBD MID FLAP OTBD L/E FAIRING CHAFING. FIBERGLASS LAYUP REPAIR PERFORMED IAW SRM 51-70-07.
INSPECTION TYPE: C, BS 980 - 1000 S38L DRAG SPLICE FITTING ATTACHED SKIN AREA TWO EACH HOLES AT LOWER ROW FASTENERS WERE FOUND THROUGH THICKNESS CRACKED BOTH RUNNING AT 5 O'CLCOK POSITION, LOOKING INBD. REPAIRED IAW SRM 53-20-01-2R-2, REPAIR 2, FIG 201, DET III REV 74. ORIGINAL .
INSPECTION TYPE:C, LEFT WING INBD MID FLAP LOWER PANEL DENTED. METAL HOT BOND REPAIR PERFORMED IAW EO B747-5750-58302-A AND RI-57-50-11015, REV A.
NR 4 ENGINE FAILED AT 13000. R & R NR 4 ENGINE IAW TC71-000-00-01.
RIGHT WING INBD MID FLAP COVE PANEL OTBD LWR CORNER SKIN CHAFED AND CRACKED, REPAIR IAW EO B747-5750-57205-A.
LEFT WING INBD MID FLAP COVE PANEL OTBD T/E CORNER CHAFED, LWR SURFACE REPAIR IAW EO.
DISBOND ON VERTICAL STABILIZER PANEL LT SIDE. REPAIRED IAW EO B747-5530-56500-A.
.2500" HOLE IN OUTER SKIN OF VERTICAL STABILIZER PANEL. REPAIRED IAW EO 5530-56500-A.
FUSELAGE SKIN PUNCTURED AT BS 2060 S36 - 37L. REPAIRED IAW SRM 53-00-01-2R PROCEDURE 1, REPAIR 1.
STRINGER 37L DAMAGED AT BS 2060. REPAIR IAW EO 5310-56484-A
FLOOR PANEL BS 2000-2100, LBL 98.58-115.140 DAMAGED. FABRICATED A NEW FLOOR PANEL IAW EO 747-5320-55567-A .
CAPTAIN`S FORWARD WINDOW HAD SMOKE AND SPARKS. REPLACED L-1 WINDSHIELD.
DURING CLIMB OUT, SMELLED FUMES LIKE ELECTRICAL BURNED WIRES. RAN SMOKE, FIRE, FUMES, QRH, ISOLATED RT UTILITY BUSS, FUMES DISSAPATED. ACCOMPLISHED AMM TASK 05-51-56 SMOKE AND FUMES IN CABIN AND FIM PROCEDURE 21-00-00-812-810. FOUND MESSAGE 21716, REPLACED FLIGHT DECK VENT FAN. PERFORMED REPAIR CONFIRMATION RAN ALL REQUIRED SYSTEMS IAW FIM 21-00-00-812-810. ALL INDICATIONS NORMAL. NO FUMES OR SMOKE APPEARED.
C INSPECTION, RT SIDE FUSELAGE LONGERON BOX LOWER SKIN PANEL CRACKED AND FASTENER HOLES ENLARGED. PERMANENT REPAIR ACCOMPLISHED IAW RI-53-40-10471, REV A AND EO 5330-53545-A.
C INSPECTION, AFT CARGO BAY LATERAL FLOOR SUPPORT WEB DAMAGED. REPAIRED FLOOR SUPPORT WEB BETWEEN BS 1672-1680, RBL49-56.5 IAW RI-53-65-10470, REV A AND EO 5310-53533-A. MAJOR REPAIR.
FLOORBOARD DAMAGED. REPAIRED IAW EO B747-5320-53030-A.
FLOOR PANEL DAMAGED. REPAIRED IAW EO B747-5320-53030-A.
MAIN CARGO DECK FLOOR PANEL BS 1232, POS 12 AREA. FABRICATED FLOOR PANEL IAW EO B747-5320-52840-B.
FLOORBOARD POS 12L HAS A LARGE SOFT AREA UNDER NON SKID FS1155, LBL 112. FABRICATED NEW FLOORBOARD IAW EO-B747-5320-51775-A.
BS 1980 LT OTBD FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50-2R-1.
AFT CARGO COMP LATERAL FLOORBEAM DAMAGED. REPAIRED IAW EO B747-5320-50672A.
INSPECTION TYPE: D, FLOORBEAM AT BS 2360, LBL 30 - 37" CORRODED. FLOORBEAM UPPER TEE REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 63 JUST BETWEEN LBL 53.65 AND RBL 53.65.
INSPECTION TYPE: D, MAIN DECK SEAT TRACK FOUND CORRODED AT BS 2285, RBL 33.9. REPAIRED IAW SRM 53-00-52-2R6, REPAIR 6, FIG 201, REV 63. CLASSIFIED AS A MAJOR REPAIR.
INSPECTION TYPE: D, RT WING OTBD T/E MID FLAP T/E UPPER SURFACE DELAMINATED AT 51" FROM OTBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 5.
INSPECTION TYPE: D, AFT CARGO BAY BS 1820 FLOORBEAM UPPER TEE LBL 18.4 FOUND CRACKED. REPAIRED IAW R53-62-37447 REV A & EO B747-5310-48441-A, CLASSIFIED AS A MAJOR REPAIR.
INSPECTION TYPE: D, RT WING OTBD MID FLAP T/E UPPER SURFACE DELAMINATED AT 34" OTBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 63.
INSPECTION TYPE: D, RT WING O/B T/E FORE FLAP L/E FAIRING DELAMINATED AT MOST O/B. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1), FIG 5, REV 63.
INSPECTION TYPE: D, RT WING OTBD FORE FLAP L/E FAIRING DELAMINATED AT MID AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 5, REV 63.
INSPECTION TYPE: D, AFT CARGO BS 1920 CEILING PANEL SUPPORT FOUND CORRODED. AFT CARGO BS 1920 CEILING PANEL SUPPORT SPLICE REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 63, JUST BETWEEN LBL 94.5 AND 94.5.
INSPECTION TYPE: D, MAIN DECK BS 1500 RBL 77" FLOOR SUPPORT CRACKED. FLOOR SUPPORT REPAIRED IAW SRM 53-00-52-2R-13. REPAIR 13, FIG 201, MAJOR REPAIR.
INSPECTION TYPE:D, M/D LT BS 820 TENSION TIE FWD CHANNEL ON HOLE FOUND CRACKED. REPAIRED IAW SRM 53-20-30-2R, REPAIR 1, REV 63, HX RS R-53-25-37443-A & B747-5310-48484-A, ORIG MATL: BAC1494-186-2024T42.
INSPECTION TYPE: D, MAIN DECK BS 740 TENSION TIE FWD CHANNEL TWO HOLES FOUND CRACKED. REPAIRED IAW SRM 53-20-30-2R REPAIR 1 REV 63, HX RS R-53-25-37443-A & EO B747-5310-48484-A, ORIG MATL: BAC1494-206-2024T42, CLASSIFIED AS A MAJOR REPAIR, ACCOMPLISH INITIAL INSP OF THE REPAIR AREA IAW SRM 53-20-30-2R1.
INSPECTION TYPE: D, LT WING OTBD FORE FLAP L/E FAIRING DELAMINATED AT INBD AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 63.
INSPECTION TYPE: D, LT WING INBD FORE FLAP L/E DELAMINATED AT NR 3 FLAP TRACK INBD AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 63.
INSPECTION TYPE:D, M/D LT BS 820 TENSION TIE AFT CHANNEL ONE HOLE FOUND CRACKED. REPAIRED IAW SRM 53-20-30-2R REPAIR 1 REV 63, HX RS R-53-25-37443-A & EO B747-5310-48484-A, ORIG MATL: BAC1494-186-2024T42.
INSPECTION TYPE: D, MAIN DECK BS 1500, LBL 77" FLOOR SUPPORT CRACKED. FLOOR SUPPORT REPAIRED SRM 52-00-52-2R-13. REPAIR 13, FIG 201, MAJOR REPAIR.
INSPECTION TYPE: D, BS 2652, S11-12L SKIN CRACKED INSIDE APU FIRE BAY. REPAIRED IAW R-53-81-37445 REV A & EO B747-5330-48410-A .
INSPECTION TYPE: D, RT WING I/B MID FLAP LOWER SURFACE DENTED AT 16" COUNT FROM O/B EDGE. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10-2R, REPAIR 2, FIG 203, REV 63.
DENT IN FUSELAGE SKIN AT STA 1922. REPAIRED IAW EO B747-5330-42286-A.
INSPECTION TYPE:C, U/D EMERGENCY LIGHT L5767, L5733 AND M4915 FOUND INOPERATIVE. EMERGENCY LIGHT BATTERY (M5169) REPLACED AND OPS CHECK FOUND NORMAL. (AMM 33-51-04)
INSPECTION TYPE:C, LT BS 2231 BETWEEN STR 21 TO 22 CRACK FOUND AT THE REVEAL PANEL DOUBLER & REVEAL PANEL (OUTER LAYER) FROM THE FASTENER HOLE RUNNING FWD & AFT BS 2231 BTN STR 21-22L REVEAL PANEL DOUBLER & REVEAL PNL REPAIRED IAW RS R53-00-36952 & B747-5310-41922. 3" CRACK IN LENGTH & CRACK STOP AT EXISTING HOLE. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL CLAD2024T3-0050" AS REPAIR DOUBLER. REPAIR SIZE IS 5.625" X 10.25"
INSPECTION TYPE:C, FWD CARGO DOOR FWD LWR DOOR SEAL RETAINER FOUND CHIPPED. FWD CARGO DOOR FWD LWR DOOR SEAL RETAINER REPAIRED IAW HX RS NR R-52-00-36968 REV A AND EO NR B747-5230-41797-A. RETAINER MATERIAL: BAC1494-171-2024-0 H.T. TO T42. THICKNESS 0.040". REPAIR LENGTH 7.5". THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. CHIPPED AREA IS .1250" X .5".
INSPECTION TYPE:C, M/DECK RT BS 880 TENSION TIE AREA 2 HOLES CRACK FOUND AT FRAME WEB BOTH CRACK APPROX 1/16" LONG. RT BS 880 TENSION TIE ATTACHED FRAME REPAIRED IAW RS R53-25-36964 & EO B747-5310-41833-A REF NRC FGV512967 FOR WORKING DETAIL.
INSPECTION TYPE:C, M/D RT BS 880, TENSION TIE AREA 2 HOLES CRACKS FOUND AT FWD CHANNEL. M/D RT BS 880 TENSION TIE BAC1494-206-2024T42 REPAIRED IAW HX RS R-53-25-36964 REV A & EO B747-5310-41833-A. REF NRC FGV512967 FOR WORKING DETAIL.
INSPECTION TYPE:C, STA860 LT TENSION TIE FASTENER HOLE FOUND 2EA FASTENER HOLES CRACKED AT FWD CHANNEL LAYER AS MARKED. M/D BS860 LT TENSION TIE FWD CHANNEL REPAIRED IAW RS R53-25-36963 EO B747-5310-41901-A. REFER NRC FGV512991 FOR WORKING DETAIL
INSPECTION TYPE:C, M/D STA 860 RT TENSION TIE FASTENER HOLE FOUND 2EA FASTENER HOLES CRACKED AT FRAME LAYER. M/D STA 860 RT TENSION TIE ATTACHED FRAME REPAIRED IAW RS R53-25-36963 & EO B747-5310-41901-A. REF NRC FGV512991 FOR WORKING DETAIL
INSPECTION TYPE:C, STA860 LT TENSION TIE FOUND FASTENER NR INCORRECT IAW EO B747-5310-41035, FIG 3. BS860 LT TENSION TIE & ATT FRAME REPAIRED, FRAME DOUBLER, TRIPLER STEEL PLATE REPLACED IAW RS R53-25-36963 & B747-5310-41901. FINAL CUTOUT FRAME LENGTH 51.375". THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR REPAIR LENGTH IS 54.125" FOR FRAME AND 31.25" FOR TENSION TIE.
INSPECTION TYPE:C, M/D BS 860 RT TENSION TIE FOUND FASTENER NR INCORRECT IAW EO B747-5310-41035, FIG 3. M/D BS 860 RT TENSION TIE & ATT FRAME REPAIRED, FRAME DOUBLER, TRIPLER STEEL PLATE REPLACED IAW RS R53-25-36963 & B747-5310-41901. FINAL CUTOUT FRAME LENGTH 51.375" THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR REPAIR LENGTH IS 54.125" FOR FRAME & 31.25" FOR TENSION TIE.
INSPECTION TYPE:C M/D STA 880 RT TENSION TIE FASTENER (BAC1494-206-2024T42) CONFIGURATION INCORRECT IAW EO B747-5310-41035, FIG 3. M/D BS 880 RT TENSION TIE, ATTACHED FRAME REPAIRED & FRAME DOUBLER, TRIPLER, STEEL PLATE REPLACED IAW RS R-53-25-36964 REV A AND EO B747-5310-41833-A. FINAL CUT FRAME LENGTH 55". TENSION TIE FINAL CUT LENGTH 23.75". THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR. ACCOMPLISHED IAW DWG 142U1023 SHEET 2 VIEW IC3-1.
INSPECTION TYPE:C, M/D STA 880 LT TENSION TIE FASTENER (BAC1294-206-2024T42) CONFIGURATION INCORRECT IAW EO B747-5310-41035, FIG 3. M/D BS880 LT TENSION TIE, ATTACHED FRAME REPAIRED. FRAME DOUBLER, TRIPLER, STEEL PLATE REPLACED IAW RS R-53-25-36964 REV A & EO B747-5310-41833-A. FINAL CUT FRAME LENGTH 55". TENSION TIE FINAL CUT LENGTH 23.75". THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR. CORRECT CONFIG ACCOMPLISHED IAW DWG 142U1023, SHT2, VIEW IC3-1.
INSPECTION TYPE:C, M/D LT BS 2231 BELOW STR 16L, 1 EA HOLE FOUND CRACKED AT INNER CHORD APPROX 0.060" IN LENGTH RUNNING FWD. LT BS 2231 BELOW STR 16L INNER CHORD REPAIRED IAW HX RS NR R-53-82-36946, REV A & EO B747-5310-41832-A REF NRC FGV511654 FOR WORKING DETAIL.
INSPECTION TYPE:D, M/D FLOORBEAM UPPER CHORD FOUND CORROSION AT STA 980 RBL 75-80. M/D FLOORBEAM AT BS980 BTN RBL55 TO RT MOST OTBD AREA UPR CHORD REPAIRED IAW RS R53-25-36948, REV A & EO B747-5310-41600-A. ORG THICKNESS IS 0.148", BLEND DEPTH REMAINS 0.050" CUTOFF LENGTH IS 56" TOTAL REPAIR LENGTH IS 65".
INSPECTION TYPE:C, M/D LT BS 2231 1 EA FASTENER HOLE CRACK FOUND AT FRAME STRAP STR 16 BRACKET MOST UPPER FASTENER HOLE. RUNNING FWD AND AFT THROUGH THICKNESS. M/D LT BS 2231 FRAME STRAP, CHORD REPAIRED IAW HX RS R-53-82-36946, REV A AND EO B747-5310-41832-A AT STR 16L AREA. STRAP CRACK THROUGH THICKNESS FINAL REMOVED SEGMENT IS 2-1"X18.75". CHORD CRACK LENGTH FINAL CUTOUT IS 0.75X0.8", CLASSIFIED AS A MAJOR REPAIR. THIS REPAIR IS TIME LIMITED TO 18846 TAC PENDING DAMAGE TOLERANCE ANALYSIS.
INSPECTION TYPE:D, RT WING OTBD MID FLAP LWR T/E OTBD AREA EXISTING REPAIR (NON-STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, SURVEY SEQ NR 583-F1-15 FUSELAGE AT BETWEEN BS2565 TO BS2598 & STR 2R-4R AREA EXISTING REPAIR DOES NOT CORRELATE TO A SRM. SURVEY 583-F1-15 AT BETWEEN BS2565-BS2598 FX SKIN BETWEEN S2R & S4R REPAIRED IAW HX RS R53-81-36936 REV A & EO B747-5330-41624-A & MSG HKA-IPXA-11-0027-06B. CLAP EXISTING CHAFED MARK 0.049" THICKNESS, CUTOUT 3.26"X17". THIS REPAIR CLASSIFIED AS MAJOR REPAIR.
INSPECTION TYPE:D, RT WING OTBD FORE FLAP OTBD L/E AREA EXISTING REPAIR (NON-STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, RT WING OTBD FORE FLAP OTBD L/E AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C.
INSPECTION TYPE:C, RT WING OTBD FORE FLAP L/E EDGE MID AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:D, RT WING OTBD FORE FLAP L/E INBD AREA EXISTING REPAIR (NON-STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:D, RT WING OTBD AFT FLAP T/E WEDGE LWR SURFACE OTBD AREA EXISTING REPAIR (NON-STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, RT WING OTBD AFT FLAP LOWER SURFACE T/E INBD AREA EXISTING REPAIR (NO REPAIR RECORD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 58.
INSPECTION TYPE:D, RT WING INBD AILERON UPPER SURFACE INBD AREA EXISTING REPAIR (NO REPAIR RECORD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, RT WING OTBD AFT FLAP LWR SURFACE INBD FLAP PANEL AREA EXISTING REPAIR (NO REPAIR RECORD). FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:D, RT WING INBD AFT FLAP UPPER SURFACE T/E MID AREA EXISTING REPAIR (NON-STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C RT WING OTBD AFT FLAP LWR SURFACE MID FLAP PNL AREA EXISTING REPAIR (NO REPAIR RECORD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 58.
INSPECTION TYPE:D, RT WING INBD FORE FLAP T/E LWR SURFACE MID FLAP HAS A NON STANDARD REPAIR. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 58.
INSPECTION TYPE:D, RT WING INBD FORE FLAP L/E LWR SURFACE OTBD AREA HAS A NON STANDARD REPAIR. REDO FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 58.
INSPECTION TYPE:D, RT WING INBD MID FLAP MID L/E AREA WITH A NON STANDARD REPAIR. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:D, RT WING INBD FORE FLAP L/E OTBD AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 58.
INSPECTION TYPE:C, RT WING INBD FORE FLAP L/E LWR SURFACE OTBD AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 58.
INSPECTION TYPE:D, RT WING INBD MID FLAP L/E MID AREA EXISTING REPAIR (NON-STANDARD) REDO. FIBREGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:D, RT WING INBD MID FLAP T/E UPPER SURFACE INBD AREA EXISTING REPAIR (NON-STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:D, FUS SECTION 48 TAIL CONE EXTERIOR SURFACE SKIN RT AT STA 2658 BELOW APU INLET DOOR CUTOUT APP. 20" SURFACE SKIN CRACKED. FX SECTION 48 TAIL CONE EXTERIOR SURFACE BONDED SKIN AT RT STA 2654 TO 2658 AND STR 11R-12R AREA REPAIRED IAW HX RS R53-81-36928 REV A & EO B747-5330-41608-A. ORG MAT'L IS BONDED SKIN CLAD 2024T3 -0.016" (2 PLIES), CRACK LENGTH 2.5", FINAL CUTOUT: 2.625" X 4.375". THIS REPAIR LIMIT IS 17346 CYCS.
INSPECTION TYPE:C, LT WING OTBD AILERON UPPER L/E INBD SKIN PANEL FOUND CHAFING, WORN. LT WING OTBD AILERON UPPER L/E INBD SKIN PANEL AT BTN AIL STA84.75-126 AREA SKIN REPAIRED IAW RS R57-60-36959 & B747-5750-41883. FINAL CUTOUT SIZE 7.5" X 41.25" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL 2024T3-0.050" AS REPAIR SKIN SECTION & SPLICE PLATE. REPAIR SIZE IS 7.25" X 70".
INSPECTION TYPE:C, LT WING OTBD AILERON UPPER L/E O/B SKIN PANEL FOUND CHAFING WORN LT WING OTBD AIL UPR L/E OTBD SKIN PNL AT BTN AIL STA243.375-257.75 AREA SKIN REPAIRED IAW RS R57-60-36959 & B747-5750-41883. FINAL CUTOUT SIZE 7" X 14.375" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL 2024T3-0.050" AS REPAIR SKIN SECTION & SPLICE PLATE. REPAIR SIZE IS 6.875" X 17.312".
INSPECTION TYPE:C, EMP EXTERIOR SURFACE SKIN AT BS2598 RT H/STAB LOWER CUTOUT (UPR OF TAIL JACK SUPPORT) FOUND LOCK FASTENER PULLED THE SKIN PLATE. REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 58.
INSPECTION TYPE:D, RT WING INBD AFT FLAP L/E MID AREA EXISTING REPAIR (NON-STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:D, EMPENNAGE EXTERIOR SURFACE SKIN AT BS 2598 RT H/STAB LOWER CUTOUT (UPR OF TAIL JACK SUPPORT) FOUND HI-LOK PULLED. THE SKIN PLATE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 58.
INSPECTION TYPE:D, RT WING INBD MID FLAP T/E UPR SURFACE MID AREA EXISTING REPAIR (NON-STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:D, RT W IB MID FLAP LWR SURFACE T/E MID AREA EXISTING REPAIR (NON-STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:D, RT WING INBD MID FLAP LOWER SURFACE T/E OTBD AREA EXISTING REPAIR (NON-STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, M/D BS 985, RBL 77 FOUND SEAT TRACK CRACKED. MAIN DECK BS909 TO BS1000 RBL75-92 SUBSTITUTE SEAT TRACK REPAIRED IAW SRM53-00-52 REPAIR13, FIG 201 REV58. ORG MAT'L IS BAC1509-100404- 6061T6511, 3.125" CRACK LENGTH AT BS982 RBL75-92", FINAL REPAIR SECTION CUT LENGTH IS 89-125", CLASSIFIED AS A MAJOR REPAIR WITH MAT'L AS REPLACED SECTION & SPLICE. TOTAL REPAIR LENGTH IS 95".
INSPECTION TYPE:C, CLARIFY THE EXISTING REPAIR CONFIGURATION ON VERTICAL STAB LT LWR AREA CORRELATE TO SRM REPAIR SURVEY SEQ NR 583-S4-01. VERT STAB LT LWR AREA REF SURVEY SEQ 583-S4-01 METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R REPAIR4 FIG201 SHT3. THIS IS CLASSIFIED AS MAJOR REPAIR. REPAIR DOUBLER SIZE 6" X 7.375". FINAL CUTOUT SIZE 3" X 4.375" LOC: VERT STAB LT LWR AREA FIN STA260. REF RS R55-35-36943 & EO B747-5530-41599 FOR REPEAT INSPECTION.
INSPECTION TYPE:C, LT WING INBD FORE FLAP LWR T/E INBD AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:D, LT WING OTBD AFT FLAP T/E INBD AREA EXISTING REPAIR (NON-STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING OTBD FORE FLAP T/E MID AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING INBD MID FLAP UPPER T/E MID AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING OTBD FORE FLAP L/E OTBD AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING INBD FORE FLAP LOWER SURFACE T/E OTBD AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING INBD AFT FLAP UPPER T/E MID AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING INBD MID FLAP UPPER T/E OTBD AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING OTBD FORE FLAP L/E MID AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING OTBD FORE FLAP L/E MID AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING OTBD AFT FLAP T/E MID AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING OTBD FORE FLAP L/E MID AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING INBD FORE FLAP LOWER SURFACE T/E MID AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 12, REV 58.
INSPECTION TYPE:C, LT WING INBD MID FLAP UPPER T/E MID AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERFLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING INBD MID FLAP UPPER T/E MID AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING OTBD FORE FLAP L/E INBD AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, REV 58.
INSPECTION TYPE:C, LT WING INBD FORE FLAP LOWER SURFACE T/E OTBD AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING OTBD FORE FLAP L/E MID AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING OTBD AFT FLAP T/E INBD AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:C, LT WING INBD FORE FLAP LWR T/E MID AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5C, FIG 2, REV 58.
INSPECTION TYPE:D, NWW RT SIDE PANEL, 1 EA STIFFENER FOUND CRACKED BETWEEN BS 280-330 AT WL 180, CRACK LENGTH APPROX .1250" LONG FROM STIFFENER FWD EDGE. STIFFENER REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 58 AT BETWEEN BS 280-300 AT WL 180 AREA.
INSPECTION TYPE:D, LT WING INBD FORE FLAP LWR T/E MID AREA HAS A NON STANDARD REPAIR. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, FIG 2, REV 58.
INSP TYPE:D, FWD CARGO DOOR BS 660 AFT DRIVE ARM FITTING SUPPORT BRACKET FOUND CRACKED. FWD CARGO DOOR BS 660 DRIVE ARM FITTING SUPPORT BRACKET REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 58.
INSPECTION TYPE:C, RT LWR PITOT-STATIC PROBE AREA NUT PLATES REQUIRE REPLACEMENT REF EO B747-3410-35109-C, FIG 10. RT LWR PITOT-STATIC PROBE AREA NUT PLATES REPLACED IAW EO B747-3410-35109-C, FIG 11.
INSPECTION TYPE:C, RT UPPER PITOT-STATIC PROBE AREA NUT PLAGES REQUIRE REPLACEMENT REF EO B747-3410-35109-C, FIG 7. RT UPPER PITOT-STATIC PROBE AREA NUT PLATES REPLACED IAW EO B747-3410-35109-C, FIG 8.
INSPECTION TYPE:D, EMP APU COMPT FWD B/H AFT FACE LT LOWER FOUND ONE LOCATION CRACKED. APU COMPT FWD B/H AFT FACE BS 2658 LBL 30" & WL 265 AREA WEB REPAIRED IAW HX RS R53-80-36922, REV A & EO B747-5310-41623-A. ORG MAT'L T1-6AL-4V-0.020" ANNEALED CRACK LENGTH 0.70". REPAIR SIZE IS 7" X 8.875". REPAIR TIME LIMIT: UNTIL 35000 CYCS.
INSPECTION TYPE:C, LT UPPER PITOT-STATIC PROBE AREA NUT PLATES REQUIRE REPLACEMENT REF EO B747-3410-35109-C, FIG 1, LT UPPER PITOT-STATIC PROBE AREA NUT PLATES REPLACED IAW EO B747-3410-35109-C, FIG 2.
INSPECTION TYPE:C, LT LWR PITOT-STATIC PROBE AREA NUT PLATES REQUIRE REPLACEMENT REF EO B747-3410-35109-C, FIG 4. LT LWR PITOT-STATIC PROBE AREA NUT PLATES REPLACED IAW EO B747-3410-35109-C, FIG 5.
INSPECTION TYPE:C, - L1 DOOR FWD CUTOUT UPPER REVEAL PANEL STOP FITTING. DOUBLER CRACKED L1 DOOR FWD CUTOUT UPR REVEAL PANEL STOP FITTING DOUBLER REPLACE AND INSTALLED IAW SRM 57-10-02 AND 51-40-02, REV 58.
INSPECTION TYPE:C, M/D L1 DOOR HINGE CUTOUT DOUBLER SUSPECT CRACK MAIN DECK L1 DOOR UPPER HINGE CUTOUT DOUBLER. REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 58.