N671UP

Part: CONTROL MODULE — MALFUNCTIONED (AURAL WARNING)

ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN. TAKEOFF WARNING HORN SOUNDS WHEN THRUST LEVERS ARE ADVANCED WITH THE FOLLOWING CONDITIONS: FLAPS 20, TRIP 4.9 UNITS. REMOVED AND REPLACED AURAL WARNING CONTROL LOGIC MODULE PER MM -31-26-03

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE: ASV AFT MOST CEILING EMERGENCY LIGHT INOP. REF LP915141. RELAMPED AFT MOST CEILING EMERGENCY LIGHT OPS CHECK GOOD THIS CLEARS M 248535.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTS IN UPPER DECK DOOR FRAME INOPERATIVE. RELAMPED OPS CK NORMAL

Part: ATTACH FITTING — CRACKED (FUSELAGE)

INSPECTION TYPE:MX FWD LOWER CARGO COMPARTMENT AFT END VERTICAL RESTRAINT ATTACH STRUCTURE LOCATED FAR LEFT SIDE IS CRACKED ON I/B UPPER LEG OF FRAME BOTTOM SIDE. REMOVED CRACKED RESTRAINT FITTING IAW SRM 51-30-02. INSTALLED NEW RESTRAINT FITTING IAW SRM 51-30-02.

Part: ATTACH FITTING — CRACKED (FUSELAGE)

INSPECTION TYPE:MX FWD LOWER CARGO COMPT POS 5 AFT RT O/B VERTICAL RESTRAINT ATTACH STRUCTURE APPEARS CRACKED AT FWD I/B BOLT HOLE. VERIFIED CRACK WITH HEFC. INSTALLED NEW SUPPORT FITTING IAW SRM 51-30-02.

Part: SEAT TRACK — CRACKED (FUSELAGE)

INSPECTION TYPE:MX FWD LOWER CARGO COMPARTMENT AFT END VERTICAL RESTRAINT ATTACH STRUCTURE O/B LEFT SIDE HAS LARGE AMOUNT OF CORROSION ON SEAT TRACK. SEAT TRACK IS ALSO CRACKED. REMOVED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-10-05 FIG 5. FABBED NEW SECTION OF SEAT TRACK IAW 53-10-05. FABBED REPAIR ANGLES IAW SRM 51-10-01. INSTALLED NEW TRACK AND REPAIR ANGLES.

Part: ATTACH FITTING — CRACKED (FUSELAGE)

INSPECTION TYPE:MX FWD LOWER CARGO COMPARTMENT AFT END VERTICAL RESTRAINT ATTACH STRUCTURE IS CRACKED ON LOWER LEG OF FRAME. LOCATED ON 2ND FROM RIGHT ATTACH STRUCTURE. INSTALLED NEW VR ATTACH FITTING IAW 51-30-02.

Part: LIGHT — INOPERATIVE (MAIN CARGO BAY)

INSPECTION TYPE:PFLT MAIN DECK CARGO AFT EMERGENCY EXIT LIGHT IN CEILING INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AS PER MM 33-51-07, OPS CHECK OK.

Part: STRUCTURE — CORRODED (WING BOX) · airframe 73,888 hrs · 20,926 cycles

INSPECTION TYPE:SP CENTER WING BOX UPPER SKIN HAS EXFOLIATION CORROSION APPROX 4 INCHES IN DIAMETER STA 1110, RBL 104. REPAIRED AREA IAW ENGINEERING FILE 747-57-20016.

Part: ANGLE — CRACKED (WING BOX) · airframe 73,888 hrs · 20,926 cycles

INSPECTION TYPE:SP STA 1140 ON RT SIDE UNDERNEATH SECOND FLOOR PNL, I/B AND BENEATH DUCTING A 2 INCH CRACK WAS FOUND AND CORROSION ON CTR WING BOX.

Part: STRUCTURE — CORRODED (FUSELAGE)

INSPECTION TYPE:IN AT STA 1140 RT UNDERNEATH SECOND FLOOR PANEL I/B BENEATH DUCTING FOUND CRACK AND CORROSION ON CONTROL WING BOX.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 72,316 hrs · 20,588 cycles

VINSPECTION TYPE:C-2 M/D - LT BS 1265 FRAME NR 2 DOOR STOP FTG AREA FOUND TWO FASTENER HOLES CRACKED. ONE CRACK AT FRAME INNER CHORD. ANOTHER CRACK AT FRAME WEB. CHORD AND WEB REPLACED IAW UPS EO B747-5310-12070-F APPENDIX E.

Part: RIB — CRACKED (NR 1 PYLON) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2, NR 1 PYLON - RESERVOIR LT STRUCTURE RIB CRACK FOUND AS MARKED. NR 1 PYLON HYD RESERVOIR LT RIB REPLACED PER SRM 51-10-01. LEAK CHECKED SATISFACTORY PER MM 29-11-00.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 U/D - BS 480-520 RBL 65 SEAT TRACK FOUND HEAVY CORROSION DURING FLOOR COVERING REMOVED. TIE DOWN TRACK REPLACED AS PER SRM 51-10-01.

Part: TRUNNION — CRACKED (NLG WW) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 NLG W/W - LT BS 380 TRUNNION FITTING MOST FWD LOWER HOLE FOUND CRACKED AT 5 O''CLOCK AND 11 O''CLOCK POSITION (LOOKING O/B). THE DISCREPANT CRACK STOP DRILLED, OPEN HOLE HFEC INSP C/O & NLG W/W LT BS 380 TRUNNION FITTING AND FOUND CRACK FREE. DETAIL VISUALLY INSP C/O & NO DEFECTS FOUND. TRUNNION FITTING REPAIRED AS PER RS-53-24-34657. THIS REPAIR IS TIME LIMITED FOR 24 MONTHS OR 500 CYCLES. TRUNNION FITTING TO BE REPLACED AT THE NEXT C-CHECK.

Part: STOP — CRACKED (DOOR FRAME) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 M/D - L3 DOOR STOP SUPPORT FTG FOUND CRACKED AT BS 1265 S-23L. STOP FTG REPLACED AS PER SRM 51-10-01 WITH HX S/TAG FF069231.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 CABIN - RT NR 3 MED CUTOUT FWD FRAME BELOW LOWER STILL FOUND 1 FASTENER HOLE CRACK AT FRAME WEB. WEB REPLACED IAW UPS EO B747-5310-12070-F APPENDIX E.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 M/D - BS 1241 RBL 17-25 BELOW FLOOR CANTED PRESS DECK FOUND CORR. BS 1241 RBL 16 TO 28 CANTED PRESS DECK REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 M/D - BS 1241 RBL 17-25 BELOW FLOOR CANTED PRESS DECK FOUND CORR. BS 1241 RBL 16-28 CANTED PRESS DECK REPAIRED AS PER SRM 51-40-02 FIG 1.

Part: SPLICE PLATE — CRACKED (FUSELAGE) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 NLG W/W STA 400 S-44L SPLICE PLATE FOUND CRACK AT CORNER RADIUS. HFEC INSP C/OUT AS PER NTM PT6, 51-00-00 FIG 1. NIL CRACK FOUND AT AFT HOLES OF PREVIOUS CRACKED HOLE. EXISTING REPAIR DOUBLER REINSTALLED AS PER SRM 51-30-02.

Part: STOP FITTING — CRACKED (DOOR FRAME) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 M/D - L3 DOOR STOP SUPPORT FTG FOUND CRACKED AT BS 1265 S3L. STOP FTG REPLACED AS PER SRM 51-10-01 WITH HX S/TAG FF 069231.

Part: STOP FITTING — CRACKED (DOOR FRAME) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 M/D - R3 DOOR FWD CUTOUT STOP FITTING FOUND CRACK AT NR 5. STOP FTG REPLACED AS PER SRM 51-10-01 WITH HX S/TAG FF 069341.

Part: STOP FITTING — CRACKED (DOOR FRAME) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 M/D- R3 DOOR FWD CUTOUT STOP FITTING FOUND CRACKED NR 3. STOP FTG REPLACED AS PER SRM 51-10-01 WITH HX S/TAG FF069228.

Part: FITTING — CRACKED (L3 DOOR) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 M/D - L3 DOOR STOP SUPPORT FITTING FOUND CRACKED AT BS 1265 S-23L. STOP FITTING REPLACED AS PER SRM 51-10-01.

Part: SPLICE PLATE — CRACKED (FUSELAGE) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 NLG W/W STA 400 S-44R SPLICE PLATE FOUND CRACK AT CORNER RADIUS. HFEC INSP C/OUT AS PER NTM PT6 51-00-00 FIG 1. CRACK FOUND AT AFT HOLE AT SPLICE FITTING, BUT NIL CRACK AFTER AFT HOLE REF SCATCH ON CWS 330869. EXISTING REPAIR DOUBLER REINSTALLED AS PER SRM 51-30-02.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 NOSE W/W TUNNEL - LT BS 320 VERTICAL BEAM WEB BTN 4TH & 5TH CLIP (COUNT FROM TOP) FOUND CRACK AT STAND OFF HOLE APPROX .125 INCH LONG. BS 320 LT WEB REPLACED PER SRM 51-10-01 & 51-30-02.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 NOSE W/W TUNNEL - RT BS 320 VERTICAL BEAM WEB BTN 4TH & 5TH CLIP FOUND CRACK AT STANDOFF HOLW APPROX .125 & .0625 INCH LONG. CRACKED WEB REPLACED PER SRM 51-10-01 & 51-30-02.

Part: FRAME — CRACKED (NR 4 PYLON) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2, NR 4 PYLON AFT TORQUE BULKHEAD LT CHORD ABOVE LOWER SPAR FITTING FOUND 1 HOLE CRACK AT 2 O''CLOCK POSITION (LOOKING FWD) APPROX 0.100 INCH LONG. NR 4 PYLON AFT TORQUE BULKHEAD LT CHORD ABOVE LWR SPAR FITTING REPAIRED AS PER HX RS R54-53-34658.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C2 EMP - RT UPPER FUSELAGE SKIN FOUND CRACKED AT STA 2654 TO STA 2658 WL 314 STR 9R (AS MARK). EMP - RT UPPER FUSELAGE SKIN REPAIRED AS PER SRM 53-30-03 FIG 1A.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 NOSE W/W TUNNEL - LT BS 300 VERTICAL BEAM WEB BETWEEN 1ST & 2ND CLIP (COUNT FROM TOP) FOUND CRACK AT LOWER STAND OFF HLE APPROX .375 & .25 INCH LONG. LT BS 300 VERTICAL BEAM WEB REPLACED AS PER SRM 51-10-01 & 51-30-02.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 NOSE W/W TUNNEL RT BS 300 VERTICAL BEAM WEB BETWEEN 1ST & 2ND CLIP (COUNT FROM TOP) FOUND LOWER STANDOFF HOLE CRACKED APPROX .25 INCH & .375 INCH LONG. CRACKED WEB REPLACED PER SRM 51-10-01.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 M/D L3 DR FWD CUTOUT LWR CORNER REVEAL FOUND CRACKED. LWR CORNER REVEAL FTG REPLACED IAW SRM 51-10-01 WITH HX S/TAG FF069254.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 M/D - L5 DOOR FWD CUTOUT UPPER REVEAL DOUBLER FOUND CRACKED AT BS 2230 STR 15-16. DOUBLER REPLACED AS PER SRM 51-10-01.

Part: PANEL — CRACKED (CAIBN) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 M/D - L3 DR FWD CUTOUT UPPER REVEAL CRACKED AT LWR EDGE AREA. REVEAL PANEL REPLACED AS PER SRM 51-10-01.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 FWD CARGO COMPT AFT BHD BS 1000 RBL 34 UPPER EDGE SHEAR TIE CRACKED. SHEAR TIE REPLACED AS PER SRM 51-10-01.

Part: SUPPORT — CORRODED (FAIRING) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 BODY FAIRING SUPPORT STA 880 RBL 0 - 60 FOUND CORRODED. BODY FAIRING SUPPORT REPAIR AT BS 880 BL 0 TO RBL 40 PER SRM 53-50-04 FIG 2.

Part: SUPPORT — CORRODED (FAIRING) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 BODY FAIRING SUPPORT STA 920 RBL 60 - LBL 60 FOUND CORRODED. BODY FAIRING SUPPORT REPAIR AT BS 920 LBL 60 TO RBL 60 PER SRM 53-50-04 FIG 2.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 72,316 hrs · 20,588 cycles

INSPECTION TYPE:C-2 M/D -L3 DOOR FWD CUTOUT REVEAL FOUND CRACKED AT NR 3 TO 4 STOP FITTING AREA AS MARK. REVEAL PANEL REPLACED IAW SRM 51-10-01 WITH HX S/TAG FF069197.

Part: COMPUTER — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE:N/A, WHILE CLIMBING THRU FL 345 TO FL 350 (500 FT TO GO), AT 500 FT PER MINUTE THE A-AUTOPILOT PITCHED UP TO CAPTURE THE ALTITUDE WITH A 1500 TO 2000 FPM CLIMB. CREW HAD TO INTERCEDE TO PREVENT OVERSHOOT IN RVSM AIRSPACE. RESEATED A A/P PITCH CHANNEL AND TESTED PER MM 22-12-01. NO FAULTS FOUND.

Part: THRUST REVERSER — FAILED (NR 4 ENGINE)

INSPECTION TYPE:IN PIREP NR 4 THRUST REVERSER FAILED TO DEPLOY. REMOVED AND REPLACED NR 4 T/R PDU PER MM 78-31-01 AND INSTALLED NEW FLEX SHAFT PER MM 78-31-02, OPS TEST OK PER MM 78-31-00. S/N ON P-2527, SHAFT P/N ON 121652-1. CLEARED M208055, REMOVED PLACARD.

Part: FRAME — CRACKED (FUSELAGE)

INSPECTION TYPE:N/A L/H BODY GEAR THE FLYING DOOR FRAME IS SEPARATING FROM AIRCRAFT FRAM E ***SUPPLEMENTAL MRR*** INSTALLED REPAIR DOUBLER ON AFT END OF FRAME PER SRM 51-40-03.

Part: HARNESS — DAMAGED (COCKPIT)

INSPECTION TYPE:N/A, INS PWR RELAY NR 3 POPPED C/B. INS ASHU NR 3 POPPED C/B. ALT INS NR 3 POPPED C/B. NR 3 INS WARN LIGHT CAME ON. NR 2 AFT AND NR 3 FWD BOOST PUMP C/B POPPED. INSTRUMENT SWITCHING PROBLEM. *S/D* REPAIRED WIRE BUNDLE W84 AND REPLACED INU NR 2. SYS OPS CK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A REF M199323, EMERGENCY LIGHT ON CEILING AFT OF P6 C/B PNL INOP IN TEST. TROUBLESHOOTING PER WDM 33-51-12 PG 1, FOUND OPEN CIRCUIT AT CONNECT OR DX328 PIN 4. REPAIRED AND OPERATION TEST PER MM 33-51-00, OK. CLEARED AND REMOVED PLACARD.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHT OVER UPPER RIGHT ESCAPE DOOR INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-51-04, OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, UPPER DECK CREW EVAC DOOR AFT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK ASSY PER MM 33-51-04, OPS CK OK.

Part: TORQUE TUBE — DISCONNECTED (TE FLAP)

AIR TURN BACK TO OAK, DUE TO R/T INBD FLAP INOP AT 1 DEGREE POSITION. FOUND RIGHT INBD FLAP TORQUE TUBE COUPLING DISCONNECTED. SECURED COUPLING, SAFETIED AND RIGGED IAW MM 27-51-01. GROUND FLAP OPERATION AND COCKPIT INDICATION CHECKS NORMAL.

Part: LIGHT — FAILED (CABIN)

INSPECTION TYPE:W/E AT L1 CREW ENTRY DOOR THE FWD CIRCULAR AND RECTANGULAR EMERGENCY LIGHTS FAILED TO ILLUMINATE. REPLACED BATTERY PACK FOR FWD L1 DOOR EMERGENCY LIGHTS, SYSTEM OPS CHECK OK.

Part: PANEL — CRACKED (NR 3 PYLON)

INSPECTION TYPE:N/A, APPROX 11 INCH CRACK ON NR 3 PYLON I/B SIDE FWD OF LOWER ACCESS PANEL. PERFORM CONDUCTIVITY TEST AND VISUAL INSPECTION PER BOEING LETTER 99-00318H. *S/D* COMPLISHED CONDUCTIVITY TEST AND VISUAL INSPECTION PER BOEING REQUEST LETTER 99-00318H.

Part: RETRACT MECH — LACK OF LUBE (RT MLG)

INSPECTION TYPE:N/A, UPON THE SECOND DEPARTURE THE RIGHT WING GEAR WOULD NOT TILT. LANDING GEAR LEVER WILL NOT MOVE TO THE UP POSITION. COMPLETED CHECKLIST AND RETURNED TO KIX. BOTH PRIMARY AND ALT AGREE. ***REFERENCE UPS99430415 FOR REPEAT WRITE-UP*** JACKED ACFT AND FOUND RIGHT WING GEAR DID NOT TILT POSITION DUE TO THE GEAR PIVOT POINT LACKED LUBRICATION. COMPLETED LUBRICATION OF ALL LANDING GEAR COMPONENTS. TILT INDICATION OP'S CHECKED NORMAL AS PER MM 32-61-04.

Part: RETRACT MECH — MALFUNCTIONED (RT MLG)

INSPECTION TYPE:N/A, UPON DEPARTURE RIGHT WING GEAR WOULD NOT TILT. LANDING GEAR LEVER WILL NOT MOVE TO THE UP POSITION. CREW COMPLETED CHECKLIST AND RETURNE D TO KIX. ***REFERENCE UPS99430416 FOR REPEAT WRITE-UP*** INSPECTED ALL LANDING GEAR, NO DEFECTS FOUND PER MM 32-21-00, AND 32 -11-00. CHECKED AND RESEATED LOGIC CARDS IN THE M-93 AND M-809 ON RIGHT WING GEAR TILT LOGIC CARDS AND CHECKED PRIM AND ALT TILT. SENSORS FOUND WERE NORMAL PER MM 32-61-04 PAGE 201.

Part: BATTERY PACK — DISCHARGED (CREW DOOR)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS AT CREW SERVICE DOORS INOP. REPLACED BATTERY PACK AT M312 CHARGER PER MM 33-51-04, INCLUDING CHARGING VOLTAGE AND GROUND.

Part: BATTERY — DISCHARGED (CABIN)

REF M-175337: UPPER DECK DOOR EMERGENCY LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT BY UPPER DECK DOOR. DEFERRAL REMAINS OPEN DUE TO EXIT LIGHT INOP AT UPPER DECK DOOR.

Part: BULB — FAILED (CABIN)

INSPECTION TYPE-N/A, FWD L1 DOOR EMER LIGHT IS INOP. INSTALLED LT BULB, OP CHK OK.

Part: LIGHT — INOPERATIVE (L1 DOOR)

L1 DOOR AFT EMERGENCY LT INOP, REBULBED NO HELP. REPLACED BATTERY PACK, OPS CK OK. OFF P/N S1356B37, S/N OFF UPS-21, ON P/N S1356B37, S/N ON 27285.

Part: CSD SEAL — LEAKS (NR 3 ENGINE)

INSPECTION TYPE-N/A, SHUTDOWN NR 3 ENG AT 2342Z DUE TO LOW OIL QUANTITY, LESS THAN .5 GAL. LANDED UNEVENTFULLY AT 0052Z. *S/D* PRES NR 3 ENG GEAR CASE, VERIFIED OIL LEAKING FROM CSD GANG DR. STEADY STREAM AT 4 PSI. REMOVED AND REPLACED NR 3 ENG CSD GARLOCK SEAL, TRANSFER TUBE SEALS AND SHAFT SEALS, REPRESSURIZED GEAR CASE AND NO LEAKS NOTED. ENG NR 3 OPS AND LEAK CK OK PER MM 24-00-00. CSD DISC/ RECONNECT OPS CK.

Part: OXYGEN BOTTLES — LEAKED (COCKPIT)

INSPECTION TYPE-N/A, AIR TURNBACK CREW OXY AFTER APPROX 1 HR 15 MIN OF FLT DECREASED TO 750 PSI, 25 MIN LATER AT 1855Z OXY WAS DOWN TO 580 PSI. CYCLED ALL OXY REGS AND OPENED SOV TO FULL OPEN AND PRESS APPEARS TO HOLD. REMOVED AND REPLACED BOTH BOTTLES IAW 12-15-08 P/N ON/OFF 801307-00, S/N ON UPPER 411975, S/N OFF 240552, S/N OFF 962285, LEAK CKS OK.

Part: LAMP — FAILED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT BY L1 DOOR AFT INOP. RELAMPED, OPS CKS GOOD.

Part: SKIN — CORRODED (BS 1050)

INSPECTION TYPE-C, CENTRE SECTION WING BOX: CENTRE WING TANK UPPER SKIN IS CORRODED AT BS 1050 BETWEEN RBL 82 AND RBL 88. REMOVED CORROSION OF UPPER SKIN AT BS 1050 RBL 82 TO RBL 88 ACC SRM 51-10-01, WITHIN LIMITS ACC SRM 57-30-01. REMOVED CORROSION OF STR 27-C UPPER CHORD BS 1050 RBL 80, OUT OF LIMIT ACC SRM 57-10-01. REPAIRED UPPER CHORD ACC EFN 747-57-0357 (KLM DFX 97-028).

Part: WEB — CRACKED (BS 2120-2140)

INSPECTION TYPE-C, BS 2120 TO BS 2140 STR 28 LT WEB BETWEEN FLOORBEAMS ADJACENT FOUND TO BE CRACKED. CRACKED WEB OUT OF LIMITS ACC SRM 53-10-01 AT BS 2120 TO BS 2140 STR 28 LT. REPLACED WEB ACC SRM 51-30-02.

Part: FLOORBEAM — CORRODED (BS 1800)

INSPECTION TYPE: C. FLOORBEAM UPPER CHORD BS. 1800 IS CORRODED AT RBL. 94. FLOORBEAM UPPER CHORD AT BS. 1800 RBL. 94 OUT OF LIMITS I.A.W. SRM. 53-10-01 FIG.1. REPAIRED FLOORBEAM UPPER CHORD AT BS. 1800 RBL. 94. I.A.W. SRM.53-10-07.

Part: INTERCOSTAL — CORRODED (BS 1900-1920)

INSPECTION TYPE: C. FOUND CRACKED INTERCOSTAL DUE TO CORROSION ON (WRONG) EXISTING REPAIR UNDER CARGO TRACKS AND ENDSTOP FITTING AT LBL 24.5 AND LBL.45, BETWEEN BS 1900/1920. REPLACED INTERCOSTALS ACC. SRM.51-30-02.

Part: DOOR BEAM — CORRODED (CARGO DOOR)

INSPECTION TYPE: C. FOUND CORROSION AROUND ANCHOR NUTS AT LOWER DOOR BEAM. REMOVED CORROSION ACC. 51-10-01 BLEND OUTS OF LIMIT PER SRM 52-00-02. REPAIRED LOWER BEAM ACC. KLM DFX 97-027. REPAIR APPROVED PER UPS EFN 747-52-0062.

Part: PANEL — CORRODED (FUSELAGE)

INSPECTION TYPE: C. FOUND CORROSION IN ADF ATTACHMENT PLATE ON KEEL BEAM PANEL 191HH AND TOP SKIN FROM PANEL ANTENNA SUPPORT PLATE. REPLACED ACC SRM 51-30-02 CORROSION REMOVED ON SKIN PANEL ACC SRM 51-10-01 IN LIMITS ACC SRM 53-30-01.

Part: SKIN — CORRODED (RT WING)

INSPECTION TYPE: C. FOUND CORROSION ON LOWER SIDE OF UPPER SKIN BETWEEN THE FRONT SPAR CHORD AT ILES 847. REMOVED STRIP OF RABBET AREA, PANEL AND L.E. RIB ACC. SRM.51-30-02. REMOVED CORROSION ACC. SRM.51-10-01. OUT OF LIMITS ACC SRM. 57-30-01 FIG 1. REPAIRED ACC KLM DFX 97-026 ISSUE NR 2. APPROVED PER UPS EFN 747-57-0355. INSTALLED STRIP OF RABBET AREA PANEL AND L.E. RIB ACCORDING SRM. 51-30-02.

Part: CARGO TRACK — CORRODED (BS 1910)

INSPECTION TYPE: C. FOUND CORROSION ON CARGO TRACK UNDER ENDSTOP FITTING AT RBL 45, BS 1910. CORROSION WAS OUT OF LIMITS. REPAIRED TRACK ACC. SRM 53-10-05.

Part: FRAME — CRACKED (BS 2040)

INSPECTION TYPE: C. FOUND CRACK IN LOWER FRAME CUT-OUT CORNERS AT BS 2040, LBL AND RBL 17.5. REPAIRED CU-TOUT CORNER BS 2040 LBL 17.5 ACC. SRM 53-10-04, FIG.43. REPAIRED CUT-OUT CORNER BS 2040 RBL 17.5 ACC. KLM DFX 97-025, ISSUE NR 2. REPAIR APPROVED PER UPS-EFN 747-53-0802.

Part: FRAME — CRACKED (BS 1900)

INSPECTION TYPE: C. FOUND CRACK IN FRAME WEB AND FRAME-INNER FLANGE AT BS.1900, BETWEEN S41/42 LT. REMOVED FRAME SECTION BETWEEN INITIAL SPLICES AT S34 AND 43L. FOUND MORE CRACKS IN FRAME AFTER REMOVING. (NO INSP. AREA). INSTALLED NEW FRAME SECTION ACCORDING TO SRM.51-30-02/05.

Part: STRINGER — CORROSION (BS 2176)

INSPECTION TYPE: C. FOUND CRACK DUE TO CORROSION IN STRINGER-END AT BS. 2176, S46R. REPAIRED STRINGER ACCORDING SRM. 53-10-03 FIG.1.

Part: FLOORBEAM — CORRODED (BS 1580)

INSPECTION TYPE-C, MAIN DECK FLOOR STRUCTURE: FLOORBEAM UPPER CHORD BS 1580 IS CORRODED ON LOWER SIDE OF FLANGE AT LBL 70. CORROSION FOUND TO BE BEYOND LIMITS OF SRM 53-10-01. FLOORBEAM UPPER CHORD BS 1580 LBL 0 TO OUTBOARD REPLACED ACC TO SRM 51-30-02.

Part: LONGERON — CRACKED (BS 1350\1480)

INSPECTION TYPE: C. DUE TO CRACK AT BSTA 1480 AT OVERWING LONGERON LT SIDE. REPLACE LT OVERWING LONGERON UPPER CHORD FROM STA 1350 TO BSTA.1480 PER SB 747-53-2291. REPLACED O/W LONGERON AT STA.1350 THROUGH 1480 LT ACCORDING SB 747-53-2291 AND DWG. 624U0008 SHEETS 3 AND 4.

Part: TRUNNION FITTING — CORRODED (NLG)

INSPECTION TYPE: C. FOUND DURING INSPECTION OF NLG FITTINGS, CORROSION ON THE INBOARD SIDE FACE OF RT AND LT TRUNNION CAP AND SOME CORROSION ON THE INSIDE OF BOTH FITTINGS. REPAIRED LT AND RT NLG TRUNNION FITTINGS ACC. SRM.53-10-08. MACHINED LT TRUNNION FITTING BORE TO 4.330 INCH DIAMETER. MACHINED RT TRUNNION FITTING BORE TO 4.2953 INCH DIAMETER. REMOVED MATERIAL IN LIMIT ACC. SRM. 53-10-08 PAGE 7.

Part: FRAME — CRACKED (BS 2160)

INSPECTION TYPE: C. FOUND CRACK IN LOWER FRAME WEB CUTOUT CORNER AT BS 2160, S49/48LT. REPAIRED FRAME WEB CUTOUT CORNER ACCORDING SRM 53-10-04 FIG. 43.

Part: SHEAR TIE — CRACKED (BS 1780)

INSPECTION TYPE: C. FOUND CRACKS IN SHEAR TIE STRINGER CUTOUTS AT BS.1780 BETWEEN S46/47 AND S43/44 LT. REMOVED DAMAGED SECTIONS OF SHEAR TIES AND REPAIRED SHEAR TIES ACC. SRM.53-10-04, FIG. 3.

Part: SHEAR TIE — CRACKED (BS 1820)

INSPECTION TYPE: C. FOUND CRACKS IN SHEAR TIE STRINGER CUT-OUTS AT BS 1820, BETWEEN S43/44, S45/46, S46/47 LT. REMOVED DAMAGED SHEAR TIES AND REPAIRED SHEAR TIES ACC. SRM 53-10-04 FIG 3A.

Part: INTERCOSTAL — CRACKED (BS 1840)

INSPECTION TYPE: C. FOUND CRACK IN ATTACHMENT ANGLE OF INTERCOSTAL TO FRAME AT BS 1840, RBL 34. REPLACED ATTACHMENT ANGLE ACC. SRM.51-30-02.

Part: SHEAR TIE — CRACKED (BS 1840)

INSPECTION TYPE: C. FOUND CRACKS IN SHEAR TIE STRINGER CUTOUTS AND SKIN ATTACHMENT AT BS.1840, BETWEEN S43/44, S45/46 AND S46/47LT. REMOVED DAMAGED SHEAR TIES AND REPAIRED SHEAR TIES ACC SRM.53-10-04, FIG.42.

Part: FLOORBEAM — CORROSION (BS 2060)

INSPECTION TYPE: C. FLOOR BEAM UPPER CHORD BS.2060 IS CORRODED BEYOND LIMITS AT LBL 51. CORROSION AT BS 2060 LBL 151. REMOVED ACC TO SRM 51-10-01, FOUND TO BE BEYOND LIMITS OF SRM 53-10-01, REPLACED UPPER CHORD ACC. SRM 53-10-0 7 FIG. 12.

Part: SHEAR TIE — CRACKED (BS 1740)

INSPECTION TYPE: C. FOUND CRACK ON SHEAR TIE AT SKIN ATTACHMENT AT BS.1740 BETWEEN S-44/45 LT. REMOVED DAMAGED SECTION OF SHEAR TIE AND REPAIRED SHEAR TIE ACCORDING SRM 53-10-04 FIG. 3.

Part: FRAME — CRACKED (BS 1520)

INSPECTION TYPE: C. FOUND CRACK IN FRAME INNER FLANGE AT END OF LEG OF SIDE GUIDE ATT. BRACKET, AT BS.1520, BETWEEN S-40/39LT. STOP DRILLED CRACK AND REPAIRED FRAME INNER CHORD ACC. SRM 53-10-04, FIG. 66.

Part: SHEAR TIE — CORROSION (BS 2340)

INSPECTION TYPE: C. FOUND CORROSION ON SHEAR TIE FLANGE TO SKIN AT BS 2340, S44/46R. REMOVED DAMAGED SECTION OF SHEAR TIE AND REPAIRED SHEAR TIE ACC. SRM 53-10-04, FIG 3.

Part: FRAME WEB — CRACKED (BS 2060)

INSPECTION TYPE: C. FOUND CRACK IN LOWER FRAMEWEB CUTOUT CORNER AT BS. 2060, LBL.17.5. REPAIRED CUTOUT CORNER ACC. SRM.53-10-04 FIG.43.

Part: FRAME — CRACKED (BS 2020)

INSPECTION TYPE: C. FOUND CRACK IN LOWER FRAME CUTOUT CORNER AT BS 220 LBL 17.5. REPAIRED CUTOUT CORNER ACC. SRM.53-10-04 FIG. 43.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS UNARMED LIGHT REMAINS ON AND EXIT LIGHTS ARE ILLUMINATED WITH SWITCH IN ARMED. REPLACED MODULE ASSY EMERGENCY DTR, CHECK DONE (P/N 69B46010-24) (S/N D00407) ON, (P/N 69B46010-24) (S/N D00196) OFF.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS ON THE MAIN DECK L-1 DOOR OVERHEAD INOP. RELAMPED OVERHEAD EMERGENCY LIGHTS ON THE L-1 DOOR, CHECKS GOOD.

Part: PRESSURE SWITCH — DEFECTIVE (NR 4 ENGINE)

INSPECTION TYPE-N/A, PERFORMED PRECAUTIONARY SHUTDOWN OF NR 4 ENGINE DUE TO START VALVE LIGHT ILLUMINATION. REPLACED NR 4 START VALVE PRESSURE SWITCH.

Part: CONTROL MODULE — INOPERATIVE (FLIGHT DECK)

INSPECTION TYPE: W/E. EMERGENCY LIGHT DISARMED, INDICATOR LIGHT FAILED TO ILLUMINATE IN DISARM OR ARM POSITION. REMOVED AND REPLACED EMERGENCY LIGHT CONTROL MODULE.

Part: SKIN — CRACKED (BS 2726-2733)

INSPECTION TYPE DLY, EMPENNAGE LEFT SIDE 8 TO 9 INCH CRACK ABOUT MIDDLE OF EXHAUST SECTION, CRACKED COMPLETELY THROUGH INTO APU SECTION, AFT OF HORIZONTAL STABILIZER BETWEEN FS 2726 TO 2733 WL 320. REPAIRED APU HOUSING SECTION SKIN SECTION, SEALED AND PAINTED PER SRM 53-30-03 FIG 1A.

Part: BATTERY — DISCHARGED (CABIN)

MAINTENANCE REPORTED, 3 EMERGENCY EXIT LIGHTS OUT IN MAIN DECK, 1 IN L1 ENTRY DOOR AND 2 ON CEILING. ITEM DEFFERED.

Part: FIRE LOOP — MALFUNCTIONED (APU)

WHILE IN FLIGHT AND WITH APU OFF, APU DET LOOP-A ILLUMINATES OCCASIONALLY, SETTING OFF APU FIRE SIGNAL. APU FIRE LOOP-A PLACARDED INOP PER MEL 26-7 ASSIGNED M-103273.

Part: EEL — INOPERATIVE (COCKPIT)

MAINTENANCE REPORTED FORWARD LT SIDE EMERGENCY EXIT LIGHT ON CREW SERVICE DOOR INOP. DEFERRED DOOR PER MEL 33-13, DEACTIVIATED PER 25-11. MRR FILED OPEN PENDING MX CORRECTIVE ACTION.

Part: CONNECTOR — INOPERATIVE (CABIN)

FORWARD (LEFT SIDE) EMERGENCY EXIT LIGHT ON CREW SERVICE DOOR INOP. REPLACED CANNON PLUG ON DX 327. REPLACED X325. LIGHTS OPERATE, BUT NOT NORMALLY. CONTINUE ON DMI. PN ON 30-0454-3, P/N OFF 30-0454-3. S/N ON UPS 0470, S/N OFF UP10954.

Part: BATTERY PACK — DISCHARGED (ESCAPE SLIDE)

WHILE ON GROUND, MAINT FOUND EMERGENCY LIGHTS AT ESCAPE SLIDE INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD (P/N 9008-4) ON, (S/N 5342) OFF.

Part: BULB — FAILED (CREW SVC DOOR)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHT BY CREW SERVICE DOOR, X325 INOP. RELAMPED, OPS CK OK.

Part: PRESSURE DECK — CORRODED (BS 1290)

WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND CORROSION AT PRESSURE DECK BS 1290 TO 1300 LBL 75. REMOVED CORROSION AT PRESS DECK BS 1290 TO 1300 ACC SRM 51-10-01, CORR NOT IN LIMITS ACC SRM 53-10-01. REPAIRED PRESS DECK FROM BS 1290 TO 1300 LBL 75, SRM 53-10-07 FIG 2.

Part: CHORD — CRACKED (BS 1000)

WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND CRACKS IN THE LOWER CHORD AT STATION 1000, BETWEEN STRINGERS 46 AND 47R AND STRINGERS 46 AND 47L. MAINTENANCE REPLACED THE LOWER CHORD PARTLY WITH REPAIR KIT PER SRM 51-30-02.

Part: FRAME — CRACKED (BS 194)

WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE TOP SIDE OF FRAME. MAINTENANCE REPLACED THE FRAME IAW SRM 51-30-02/05.

Part: WEB — CRACKED (BS 260)

WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE NOSE LANDING GEAR WHEELWELL CRAWL-WAY AT STATION 260, WL 160 IN OUTBOARD CORNER OF CUT-OUT, LEFT HAND AND RIGHT HAND SIDE. MAINTENANCE REPAIRED IAW SRM 53-10-04.

Part: SHEAR TIE — CRACKED (BS 1660)

WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE SHEAR TIE AT STATION 1660, BETWEEN STRINGERS 46 AND 47L IN THE AFT CARGO COMPARTMENT. MAINTENANCE REMOVED THE DAMAGED SHEAR TIE AND REPAIRED SHEAR TIE IAW SRM 53-10-04.

Part: STRINGER — CORRODED (BS 1000)

WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE STRINGERS UNDER END STOP FITTINGS AT STATION 1000, STRINGER 47R AND STRINGER 45L IN FORWARD CARGO COMPARTMENT. MAINTENANCE REPAIRED THE STRINGERS IAW SRM 53-10-03.

Part: FITTING — CORRODED (NR 1 FLAP TRACK)

WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND FLAP TRACK NR 1 FORWARD SUPPORT FITTING AT WBL 743 INNER BORE CORRODED. MAINTENANCE REPLACED THE FITTING ASSY IAW IPC 57-12-11 ITEM 370.

Part: CORNER — CRACKED (L4 DOOR)

WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND A CRACK IN AFT LOWER CORNER OF DOOR 4 LT, DURING INTERNAL INSPECTION. MAINTENANCE REPAIRED THE CRACK IAW SRM 52-10-02 FIGURE 10.

Part: SKIN — DELAMINATED (LT TE AFT FLAP)

WHILE ON GROUND, MAINTENANCE FOUND LT WING INBOARD FLAP, AFT SECTION FWD SIDE, 2 INCH BY 4 INCH AREA OF DELAMINATION JUST AFT OF NR 3 CANOE. REPAIRED FLAP ROCK GUARD PER SRM 51-40-06.

Part: SKIN — DELAMINATED (RT TE AFT FLAP)

WHILE ON GROUND, MAINTENANCE FOUND RT WING INBOARD FLAP SECTION, AFT FLAP SECTION FWD SIDE, 1 INCH BY 4 INCH DELAM SECTION JUST AFT OF NR 6 CANOE. REPAIRED ROCK GUARD ON FLAP AND PAINTED IAW SRM 51-40-06.

Part: SKIN — DELAMINATED (RT TE FLAP)

WHILE ON GROUND, MAINTENANCE FOUND RT WING INBOARD FLAP FWD SIDE, 2 INCH BY 6 INCH DELAM SECTION. REPAIRED FLAP ROCK GUARD AND PAINTED IAW SRM 51-40-06.

Part: EEL LAMP — INOP (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND UPPER DECK, LT DOOR SILL EMERGENCY LIGHT INOP. RELAMPED, OPS CK OK.

Part: EEL — INOP (UPPER DECK)

WHILE ON GROUND IN ANC, MAINTENANCE FOUND THE UPPER DECK ESCAPE DOOR HAS AN INOP FWD EMERGENCY LIGHT. MAINTENANCE RELAMPED, OPS CK GOOD.

Part: PANEL — CRACKED (LT WING)

WHILE ON GROUND MAINTENANCE FOUND LEFT WING FLYING PANEL INBD TRAILING EDGE NEXT TO FUSELAGE HAS 14 INCH CRACK (TOP OF WING). REMOVED PANEL. DRILLED HOLES IN NEW PANEL AND STARTED INSTALLATION. FINISHED INSTALLATION OF NEW PANEL AS PER M/M 57-22-01.

Part: LE SKIN — CRACKED (LT TE MID FLAP)

WHILE ON GROUND MAINTENANCE FOUND LT WING, INBD MID FLAP LEADING EDGE INBD SECTION HAS A HOLE APPROX 1 INCH DIAMETER AND A CRACK EMANATING FROM IT THAT IS APPROX 10 - 12 INCHES LONG. REPAIRED PER SRM 747-51-40-9.

Part: EEL BATT PACK — DISCHARGED (FLIGHT DECK)

(SUPPLEMENTAL MRR) MAINTENANCE REPORTED THAT ON PRE-FLIGHT, THE EMERGENCY EXIT SIGN ABOVE THE CREW SERVICE DOOR WOULD NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK. WORKS OK.

Part: FIRE LOOPS — MALFUNCTIONED (NR 2 ENGINE)

WHILE EN ROUTE TO SNN, FLIGHT CREW REPORTED AT ALTITUDE NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED. INDICATIONS WERE B-LOOP SHOWING 8.7 ON THE COMPARTMENT INDICATOR. ACCOMLISHED ENGINE FIRE BOLD FACE AND CHECKLIST ITEMS IN ACCORDANCE WITH SECTION II OF THE AOM. CHANGED FOUR DUAL FIRE DETECTOR WIRES P/N 895396, 89439, 895397, 895899. CHANGED BOTH FIRE BOTTLES S/N M2200 AND M1162, FIRE TEST OK ON LOOPS A AND B.

Part: CLAMP — FAILED (NR 2 ENGINE)

FLIGHT CREW REPORTED, FIRE INDICATION ON NR 2 ENGINE. SHUTDOWN ENGINE VIA CHECKLIST. ALL INDICATIONS OF FIRE OUT, FL 330, TIME 0355Z. AFTER ENGINE WAS SECURED, OIL PRESSURE MAINTAINED 18-20 PSI, DISCHARGED FIRE BOTTLE. REMOVED AND REPLACED FIRE BOTTLE PER MM 26-21-03. INSPECTED ENGINE, FOUND BLEED AIR LEAK AT PRESSURE RELIEF VALVE. REPLACED CLAMP AND LEAK CHECKED GOOD. ACCOMPLISHED INSPECTION PER MM 72-00+00 698-17, NO DEFFECTS.

Part: FIRE LOOP — DIRTY (NR 4 A)

PILOT REPORTED THAT ON CLIMBOUT, FIRE DETECTION LIGHT ILLUMINATED WITH A FAULT INDICATION. THE NR 4 A-LOOP INDICATED A SHORT. AFTER 15 MINUTES, SHORT CORRECTED ITSELF. CLEANED CONTACT ON NR 4 A-LOOP, NR 4 A-CARD, OPS CHECK OK.

Part: SKIN — CRACKED (LT MID FLAP)

MAINTENANCE REPORTED LEFT O/B MID FLAP PANEL CRACKED ACROSS FITTING AT ABOUT CENTER OF PANEL. REPAIRED PER SRM 51-40-09.

Part: EEL — BROKEN (UPPER DECK)

DURING 'DAILY' CHECK, MAINTENANCE REPORTED UPPER DECK EMERGENCY LIGHT ASSY BROKEN. REPLACED LIGHT ASSY.