N40061

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 64,735 hrs · 26,248 cycles

LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW ILLUMINATED DURING PREFLIGHT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW AMM 33-51-01. OPS CHECKED GOOD. ACFT OKAY FOR SERVICE.

Part: INDICATOR — FAILED (L1 DOOR SLIDE) · airframe 64,481 hrs · 26,106 cycles

L1 DOOR SLIDE PRESSURE INDICATOR INOPERATIVE. REPLACED THE SLIDE PRESSURE INDICATOR IAW MM 25-61-03-2, OPS CHECKED GOOD IAW MM 25-61-03-5.

Part: LAMP — INOPERATIVE (TEST SWITCH) · airframe 64,451 hrs · 26,093 cycles

LEFT FWD ENTRY DOOR REMOTE SLIDE PRESSURE PRESS TO TEST LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 25-61-03-2. PERFORMED OPERATIONAL TEST OF L1 ESCAPE SLIDE REMOTE PRESS TO TEST SWITCH IAW AMM 25-10-03-5. SWITCH OPS CHECKED GOOD, OK FOR SERVICE.

Part: INDICATOR — INOPERATIVE (L1 DOOR SLIDE) · airframe 63,890 hrs · 25,786 cycles

L1 DOOR EVAC SLIDE PRESSURE TEST LIGHT INOPERATIVE. REMOVED AND REPLACED THE L1 DOOR REMOTE SLIDE PACK PRESSURE INDICATOR ASSY IAW AMM 25-61-03-2-0, ACCOMPLISHED ADJUSTMENT & TEST IAW MM 25-61-03- 5-0, OPS CHECKED NORMAL.

Part: BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 63,507 hrs · 25,608 cycles

LEFT WING INBOARD FLAP ASSEMBLY OUTBOARD STRAP HOLE FOUND CORRODED. REPAIRED IAW CMM 57-52-01 AND EA 8-5750-T0328621 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: BRACKET — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 63,507 hrs · 25,608 cycles

LEFT WING INBOARD FLAP ASSEMBLY OUTBOARD PIVOT HOLE FOUND CORROSION. REPAIRED IAW CMM 57-52-01 AND EA 8-5750-T0328621 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 63,507 hrs · 25,608 cycles

LEFT HAND WING OUTBOARD FLAP LOWER INNER WEDGE FOUND DAMAGED. REPAIRED IAW SRM 57-20-00 VOLUME I FIGURE 10 AND EA 8-5750-T0328820 PART 1. CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: CARGO TRACK — CORRODED (BS 1882-1887) · airframe 63,507 hrs · 25,608 cycles

AFT CARGO BAY, CARGO TRACK FOUND CORRODED AT BS 1882 - 1887 RBL 64. REPAIRED IAW SRM 53-70-00 FIGURE 1 VOLUME I. CLASSIFIED AS MAJOR IAW GMM 6-2-100.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 63,507 hrs · 25,608 cycles

DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT WING FUEL ACCESS PANEL FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 68 SHEET 2 VOLUME I.

Part: SKIN — CRACKED (NR 10 SLAT) · airframe 63,507 hrs · 25,608 cycles

DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT WING SLAT TRACK NR 10 CUT-OUT, AFT OUTBOARD CORNER NR 14 FOUND CRACKED APPROXIMATE LENGTH 0.3 INCHES. REPAIRED IAW SRM 57-10-00 FIGURE 68 SHEET 1 VOLUME I.

Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 63,507 hrs · 25,608 cycles

LEFT INBOARD ELEVATOR ASSEMBLY OUTER EDGE DAMAGED. REPAIRED IAW SRM 55-10-00 FIGURE 8 VOLUME I AND EA 8-5520-T0328753 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 63,507 hrs · 25,608 cycles

RIGHT WING AT XORS 593 RIB REINFORCEMENT DOUBLER FOUND CRACKED. DOUBLER REMOVED IAW SRM 51-35-01 VOLUME II. NEW DOUBLER FABRICATED IAW DRAWING ARB1249 REVISION Z. FABRICATED AND INSTALLED IAW SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: DOUBLER — CRACKED (RT WING) · airframe 63,507 hrs · 25,608 cycles

RIGHT WING LEADING EDGE LOWER INTERIOR SURFACE FRONT SPAR XORS 593 FOUND INNER BEADED DOUBLER CRACKED. DOUBLER REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.

Part: PRESSURE SWITCH — FAILED (L1 DOOR SLIDE) · airframe 62,671 hrs · 25,172 cycles

L1 DOOR SLIDE REMOTE PRESSURE LIGHT BROKEN. REPLACED SLIDE PRESSURE REMOTE SWITCH AND BATTERIES IAW AMM 25-61-03-2. OPS CHECK GOOD. AIRCRAFT OK F0R CONTINUED SERVICE.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 615 hrs · 24,490 cycles

L1 DOOR LIGHT TEST NOT ILLUMINATING. R & R L1 DOOR SLIDE CHARGE LIGHT ASSEMBLY IAW AMM 25-61-03-2. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE AT THIS TIME.

Part: REGULATOR VALVE — FAULTY (BLEED AIR SYS) · airframe 613 hrs · 24,395 cycles

DURING DESCENT AT APPROX 12,000 FEET TURNED ON ENG & WING ANTI-ICE. IMMEDIATELY NR 1 AIR SYS SHOWED A NR 1 ENG MANIFOLD FAILURE. NR 1 AIR SYS INDICATED RED & NR 1BLEED AIR INDICATED CLOSED. WITH NR 1THROTTLE IDLE, NR 1 AIR SYS REMAINED RED UNTIL TAXI TO GATE. THERE WERE NO LEVEL 2 OR LEVEL 3 ALERTS DURING FLIGHT. R & R NR 1 PRESS REGULATOR VLV IAW AMM 36-12-01-4. OPERATIONS & LEAK CHECKED GOOD.

Part: ACCUMULATOR — LOW PRESSURE (L1 DOOR) · airframe 611 hrs · 24,326 cycles

L1 DOOR ACCUMULATOR IS OUT OF GREEN BAND. SERVICED L1 DOOR ACCUMULATOR.

Part: SWITCH — DIRTY (R1 DOOR) · airframe 611 hrs · 24,322 cycles

R1 DOOR WILL NOT OPEN, ELECTRICALLY, FROM OUTSIDE OR INSIDE WITH SWITCH. FOUND UP LIMIT SWITCH PLUNGER/BEARING DIRTY. REMOVED DIRT/RESIDUEFROM PLUNGER/BEARING AND DOOR OPERATED NORMAL.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 611 hrs · 24,304 cycles

L-1 DOOR PNEUMATIC ASSIST BOTTLE PRESS LOW. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-11-03-2, NO DEFECTS NOTED.

Part: BATTERY — DISCHARGED (L1 DOOR) · airframe 611 hrs · 24,289 cycles

L1 DOOR SLIDE LIGHT WILL NOT ILLUMINATE. R & R BATTERIES & RELAMPED DOOR SLIDE & OPERATIONS CHECKED NORMAL IAW 25-61-03-2.

Part: BATTERY — DISCHARGED (L1 DOOR) · airframe 611 hrs · 24,284 cycles

L1 DOOR SLIDE LIGHT WILL NOT ILLUMINATE. AMM 25-61-03-2-0 R & R BATTERIES & RELAMPED DOOR SLIDE. OPERATIONS CHECKED NORMAL IAW 25-61-03-2.

Part: SKIN — DELAMINATED (RT HORIZ STAB) · airframe 60,737 hrs · 24,060 cycles

RIGHT HORIZONTAL STAB FAIRING ASSEMBLY LOWER RIVETED HAS DELAMINATION ON INNER SKIN. REPAIRED RT HORIZONTAL STAB FAIRING ASSEMBLY IAW SRM 51-71-00 VOL II.

Part: BRACKET — CRACKED (NR 1 PYLON) · airframe 60,737 hrs · 24,060 cycles

NUMBER 1 PYLON AT APPROX STATION YN 295, FOUND BRACKET CRACKED AFT OF PRE COOLER. R & R BRACKET AUB7031-25 IAW DWG AUB7031.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 60,737 hrs · 24,060 cycles

MAIN DECK FLOOR STATION 1821 RBL 47 SEAT TRACK WORN, SEAT TRACK EXCEEDS WEAR LIMITS IAW SRM 53-70-00 VOL 1. R & R DAMAGED SEAT TRACK SECTION IAW SRM 53-70-00 VOL I.

Part: PANEL — DELAMINATED (TE FLAP) · airframe 60,737 hrs · 24,060 cycles

LEFT WING OTBD FLAP FAIRING PANEL 535DR WAS FOUND DELAMINATION DURING CLOSING. REPAIRED IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02 VOL II.

Part: SKIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 60,737 hrs · 24,060 cycles

LEFT WING OTBD AILERON LOWER SURFACE SKIN PANEL HAS MILD CORROSION SPOTS. REMOVED CORROSION IAW SRM 57-10-00 VOL 1. INSTALLED EXTERNAL DOUBLER IAW SRM 57-10-00 V1 FIG 6 SHEET 1. WEIGHT & BALANCE COMPLIED WITH IAW SRM 57-50-00 PG 1.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 60,737 hrs · 24,060 cycles

LOWER FUSELAGE 1 ACM COMPARTMENT STATION 575 - 595 OTBD OF HEAT EXCHANGER DUCT LIGHT SURFACE CORROSION ON STIFFENER. R & R NEW INTERCOSTAL IAW DWG ACA3816.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,737 hrs · 24,060 cycles

RIGHT WING UPPER SURFACE APPROX 30 INCHES AFT OF R3 DOOR LOWER ANGLE AT SUPPORT FOR FAIRING PANEL 152DT IS CRACKED. FABRICATED & INSTALLED NEW ANGLE IAW DWG ANB7142.

Part: PANEL — DELAMINATED (NR 2 NACELLE) · airframe 60,737 hrs · 24,060 cycles

NR 2 ENGINE LT PICKLE BARREL PANEL 361DL DELAMINATED AT FWD LOWER CORNER. REPAIRED IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02 VOL II.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 60,737 hrs · 24,060 cycles

NUMBER 2 ENG LT SIDE PICKLE BARREL PANEL 363EL DELAMINATED AT FWD LOWER CORNER. REPAIRED IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02 VOL II.

Part: PANEL — DELAMINATED (RT WING) · airframe 60,737 hrs · 24,060 cycles

RIGHT WING INBD LOWER SURFACE FWD AT FUSELAGE PANEL ARC0446-504 HAS DELAMINATED. REPAIRED IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02 VOL II.

Part: PANEL — DELAMINATED (LT WING) · airframe 60,737 hrs · 24,060 cycles

LEFT LOWER REAR CAP WING ROOT PANEL ASSEMBLY 541AB DELAMINATED ON FWD OTBD CORNER. REPAIRED IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02.

Part: PANEL — DENTED (VERTICAL STAB) · airframe 60,737 hrs · 24,060 cycles

NUMBER 2 ENG PICKLE BARREL 364NR HAS DENT. REPAIRED IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02 VOL II.

Part: PANEL — DAMAGED (VERTICAL STAB) · airframe 60,737 hrs · 24,060 cycles

RIGHT PICKLE BARREL PANEL 362DR BOLT HOLE ON PANEL IS TO DEEP. REPAIRED IAW SRM 51-71-00 VOL II & PAINT IAW SRM 51-21-02 VOL II.

Part: PANEL — DELAMINATED (RT WING) · airframe 60,737 hrs · 24,060 cycles

RIGHT OVERWING PANEL ARC0274-508 DELAMINATION ON LOWER SIDE. REPAIRED DELAMINATION IAW SRM 51-71-00 VOL. II & PAINT IAW SRM 51-21-02 VOL II.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 60,737 hrs · 24,060 cycles

MAIN DECK FLOOR STATION 755 LBL47 SEAT TRACK IS WORN. REPLACED SEAT TRACK SECTION IAW SRM 53-70-00 VOL 1.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 60,737 hrs · 24,060 cycles

MAIN DECK FLOORS STATION 1741 LBL 47 TWO EACH SEAT TRACK WORN. REMOVED AREA OF DAMAGED SEAT TRACK IAW SRM 53-70-00 VOL 1.

Part: DOOR — DELAMINATED (LT MLG) · airframe 60,737 hrs · 24,060 cycles

LEFT MLG STRUT DOOR HAS DELAMINATION ON FWD LOWER SECTION AT SPLIT SECTION MARKED. REPAIRED MLG STRUT DOOR IAW SRM 51-71-00 VOL II.

Part: DOOR — DELAMINATED (LT MLG) · airframe 60,737 hrs · 24,060 cycles

LEFT MLG STRUT DOOR HAS DELAMINATION ON FWD LOWER CORNER. REPAIRED MLG STRUT DOOR FORWARD LOWER CORNER IAW SRM 51-71-00 VOL II.

Part: PANEL — DELAMINATED (LT WING) · airframe 60,737 hrs · 24,060 cycles

LEFT LOWER REAR CAP WING ROOT PANEL ASSEMBLY SHOWS DELAMINATION & EVIDENCE OF CORROSION. REPAIRED PANEL ARC0446-503 PER SRM 81-71-00 VOL.II

Part: PANEL — DELAMINATED (RT WING) · airframe 60,737 hrs · 24,060 cycles

RIGHT WING ARC0357-502 DELAMINATION ON EDGES MARKED. REPAIRED PANEL IAW SRM 51-71-00 VOL II & PAINTED PANEL IAW SRM 51-21-02 VOL II.

Part: DOOR — DAMAGED (RT WING SLAT) · airframe 60,737 hrs · 24,060 cycles

RIGHT WING SLAT DRIVE MECHANISM DOOR HINGE SCREW PULLING THROUGH DOOR. REPAIRED IAW SRM 51-71-00 VOL II & PREP PAINTED IAW SRM 51-21-02.

Part: PANEL — DELAMINATED (RT WING) · airframe 60,737 hrs · 24,060 cycles

RIGHT INBD WING LOWER SURFACE HINGE PANEL ARC0286-502 FWD EDGE HAS CORROSION & IS DELAMINATING. REMOVED LIGHT SURFACE CORROSION ON SURFACE IAW SRM 51-21-01 VOL I & REPAIRED DELAMINATION ON HINGE PANEL AT FWD EDGE IAW SRM 51-71-00 VOL II.

Part: DOUBLER — CRACKED (MLG WW BLKHD) · airframe 60,737 hrs · 24,060 cycles

CENTER WHEEL WELL AT RBL 31.5 BS 1389 FACTORY MACHINED DOUBLER IS CRACKED ON VERTICAL FLANGE. REPLACED IAW DWG NEA6078, AEA0526 & SRM 51-33-01 VOL 2.

Part: DOUBLER — CRACKED (MLG WW BLKHD) · airframe 60,737 hrs · 24,060 cycles

CENTER MLG WHEEL WELL WEB WALL AT BS 1389 FACTORY MACHINED DOUBLER IS CRACKED ON VERTICAL FLANGE. REPLACED IAW DWG NEA6078, AEA0526 & SRM 51-33-01 VOL 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,737 hrs · 24,060 cycles

AFT CARGO COMPARTMENT AFT FUSELAGE WASTE TANK COMP STATION 2004 TO 2008 RBL 26, BETWEEN FLOOR & AFT BULKHEAD, LEVEL 2 CORROSION ON PART AGA7551-504 LOWER SURFACE. REPAIRED FLOOR SUPPORT IAW 53-00-01 VOL 1 PAGE 18 FIG 4.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 60,737 hrs · 24,060 cycles

AFT CARGO COMPARTMENT AFT FUSE WASTE TANK COMP STATION 1986 RBL 26 PART AWD7142-507 APPROX 1/2 INCH CRACK AT INBD RIVET. R & R CRACKED BRACKET IAW SRM 51-33-01 VII.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 59,957 hrs · 23,619 cycles

DURING PREFLIGHT L1 DOOR SLIDE LOW PRESSURE LIGHT ILLUMINATED, SLIDE STILL INTACT. REMOVED AND REPLACED L1 SLIDE IAW MM 25-61-02-4 AND 25-61-01-2.

Part: BATTERY — DISCHARGED (L1 DOOR) · airframe 59,769 hrs · 23,529 cycles

L1 DOOR SLIDE TEST LIGHT INOPERATIVE. R & R BATTERIES & OPERATIONS CHECKED IAW MD-10-10 AMM 25-61-01-2, OK FOR SERVICE.

Part: MEC — FAILED (NR 3 ENGINE) · airframe 59,034 hrs · 23,138 cycles

DURING DESCENT, NR 3 ENGINE FLAMED OUT. NO FIRE OR ABNORMAL INDICATIONS. ATTEMPTED ONE RESTART, RAN ALL APPLICABLE QRH CHECKLIST. FUEL AT FLAME OUT 8K, 7K, 8K. ENGINE WINDMILL 15 MIN AFTER FLAMEOUT. REMOVED NR 3 ENG FUEL PUMP AND MEC IAW MM 73-12-01-2.

Part: ADG — INOPERATIVE · airframe 58,035 hrs · 22,623 cycles

ADG DEPLOYED, NO HYDRAULICS AND NO ELECTRICAL. UNIT BURNED. R & R ADG IAW AMM 24-22-01-4.

Part: SPAR — CRACKED (ZONE 500) · airframe 58,033 hrs · 22,620 cycles

LOWER LEFT WING, XOR 345 OTBD ROLL/MIDDLE BOLT HOLE SHOWING CRACK INDICATION. REAMED HOLE WITH CRACK INDICATION TO .325 REF SRM 51-21-01, VOL II PERFORMED HFEC OPEN HOLES INSPECTION IAW NDT SPM 93K0393, NO INDICATION FOUND. PERFORMED FINAL LEAK CHECK IAW MM 28-00-00-2. NO LEAKS NOTED.

Part: BATTERY — INOPERATIVE (ESCAPE SLIDE) · airframe 56,697 hrs · 21,915 cycles

SLIDE RAFT PRESSURE TEST LIGHT INOPERATIVE. RELAMPED SWITCH, NO HELP. REPLACED BATTERIES FOR PRESSURE LIGHT IAW SMP. OK FOR SERVICE. REPLACED BATTERIES FOR PRESSURE LIGHT IAW SMP. OK FOR SERVICE.

Part: SKIN — DENTED (A/C BAY DOOR) · airframe 55,404 hrs · 21,246 cycles

NR 1 AIRCON COMPARTMENT DOOR - FOUND DENT MARK. REPAIRED AS PER EA 8-5240-143736. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 111.

Part: SKIN — MISREPAIRED (BS 635 S44-45L) · airframe 55,404 hrs · 21,246 cycles

LOWER FUSELAGE AT STATION 635, STRINGER 44L TO STRINGER 45L, TO CARRY OUT REPAIR AS AS PER SRM, FOUND EXISTING REPAIR NOT AS PER SRM. NO PREVIOUS REPAIR RECORD FOUND. EXISTING REPAIR AT LOWER FUSELAGE STA 635 STRINGER 44L TO STRINGER 45L REMOVED AND REPLACED WITH NEW REPAIR PARTS AS PER SRM 53-20-00 FIG 13 VOLUME I REVISION 96. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111. INITIAL INSPECTION TO BE CARRIED OUT AT 8,000 FLIGHT CYCLES AND REPETITIVE INSPECTION TO BE CARRIED OUT AT 4750 FLIGHT CYCLES.

Part: SEAT TRACK — DAMAGED (BS 930-935) · airframe 55,404 hrs · 21,246 cycles

CABIN - LT STA 930 - 935 X=47.5 SEAT TRACK FOUND DAMAGED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 929 TO STATION 989 X=47.5 AS PER SRM 53-70-00 FIG 1 VOLUME I REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 55,404 hrs · 21,246 cycles

RT WING OTBD FLAP LOWER SURFACE AREA JUST INBD OF OTBD HINGE FOUND DENT. RT WING OTBD FLAP LOWER SURFACE AREA JUST INBD OF OTBD HINGE DENT AREA REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 7, VOLUME I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 111.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 55,404 hrs · 21,246 cycles

RT WING OTBD FLAP LOWER SURFACE OTBD OF INBD HINGE FOUND DENT. REPAIRED AS PER SRM 57-10-00 FIG 7 VOLUME I REVISION 96. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.

Part: SKIN — DAMAGED (NR 4 SLAT) · airframe 55,404 hrs · 21,246 cycles

RT WING NR4 SLAT LOWER SURFACE INBD AFT EDGE FOUND DAMAGED. DAMAGED SKIN AT LOWER SURFACE OF RT WING NR4 SLAT INBD AFT EDGE, TRIMMED AND CARRIED OUT REPAIR IAW SRM 57-10-00, FIG 31, VOLUME I, REV 96. SLAT OPS AND GAP CHECK CARRIED OUT FOUND SATISFACTORY IAW AMM 27-80-01-4, REV 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: SKIN — DAMAGED (RT WING) · airframe 55,404 hrs · 21,246 cycles

RIGHT WING NR 3 SLAT TRACK DOOR CUTOUT FOUND DAMAGED. REPAIR CARRIED OUT AS PER SRM 57-00-01 FIG 1A VOLUME I REVISION 96. REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 111.

Part: SUPPORT FITTING — CRACKED (CARGO DOOR FRAME) · airframe 55,404 hrs · 21,246 cycles

CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 96 AND EXISTING REPAIR DOUBLER AND TRIPLER REMOVED AND REPLACED AS PER EA 8-5310-143731. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: LONGERON — CORRODED (BS 1521 L32L) · airframe 55,404 hrs · 21,246 cycles

LOWER FUSELAGE - STA 1521, LONGERON 32L FOUND EXFOLIATION CORROSION. LONGERON REPAIRED IAW EA NR 8-5310-132479. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.

Part: BEAM — CRACKED (CARGO DOOR FRAME) · airframe 55,404 hrs · 21,246 cycles

CRACK INDICATION FOUND ON 1ST LAYER BEAM FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 3 LOWER JAMB FITTING AT HOLE A. REPAIRED AS PER EA 8-5310-143730. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: BEAM — CRACKED (CARGO DOOR FRAME) · airframe 55,404 hrs · 21,246 cycles

CRACK INDICATION FOUND ON 2ND LAYER BEAM FROM TOP DURING HFEC OPEN HOLE. INSPECTION ON 0.520" HOLE AT MAIN CARGO DOOR NR 3 LOWER JAMB FITTING AT HOLE A. REPAIRED AS PER EA 8-5310-143730. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.

Part: SUPPORT BRACKET — CRACKED (L3 DOOR) · airframe 55,404 hrs · 21,246 cycles

CABIN - L3 MED PLUG NR 6 DOOR BEAM SUPPORT BRACKET FOUND CRACKED. DAMAGED SUPPORT BRACKET AT CABIN L3 MED PLUG NR6 DOOR BEAM REMOVED IAW SRM 51-31-01 VOLUME II, REV 96. NEW SUPPORT BRACKET FABRICATED IAW DWG ADA3754 REV F AND INSTALLED IAW EA 8-5210-132476. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.

Part: BEAM — DAMAGED (ZONE 200) · airframe 55,404 hrs · 21,246 cycles

CABIN - L3 MED PLUG NR4 DOOR BEAM SUPPORT BRACKET FOUND DAMAGED. DAMAGED SUPPORT BRACKET AT CABIN L3 MED PLUG NR4 DOOR REMOVED IAW SRM 51-31-01 REV 96, VOLUME II. NEW SUPPORT BRACKET FABRICATED IAW DWG ADA3752, REV E AND INSTALLED IAW EA 8-5210-132476 TITLE : DOORS - L3 PASSENGER DOOR CRACKED. HORIZ BEAM - FABRICATION. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 111.

Part: THRUST REVERSER — DAMAGED (NR 3) · airframe 54,813 hrs · 20,956 cycles

NR 3 THRUST REVERSER UNLOCK WILL NOT EXTINGUISH. CYCLED REVERSER NUMEROUS TIMES ON GROUND, NO JOY. ITEM ENTERED AS MX WRITE UP IN ERROR. ITEM IS A PILOT WRITE UP, BOS U REVERSER HAS HEAVY DAMAGE, IN THE PROCESS OF TAKING PICTURES AND MAKING A PARTS LIST. R & R NR 3 ENG LT FAN REVERSER ASSY IAW AMM 78-32-11-2 AND WORKCARDS 78T3701L-3. OPS CHECKS GOOD. OK FOR SERVICE. NR 3 ENG - R & R RT THRUST REVERSER MAIN DRIVE CABLE IAW MM 78-32-07-02.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 52,438 hrs · 19,835 cycles

LT WING LWR SURFACE T/E FOUND CRACK ON SKIN PANEL REF IPC 57-32-60-01 ITEM 210 VIEW "A". REPAIRED PANEL IAW SRM 51-71-00 PAR 18 B & SRM 57-10-00 FIG 73 SHT 5 VOL I.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 52,438 hrs · 19,835 cycles

RT WING UPPER SURFACE, LIGHT CORROSION ON UPPER SKIN BEVER TAIL. REPAIRED AREA IAW EA 8-5710-120494.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 52,438 hrs · 19,835 cycles

FOUND SEVERE EXFOLIATION CORROSION ON SEAT TRACK AT STA 1923 X=-57, Z=-19. REPAIR IAW SRM 53-70-00 VOL 1 FIG 13 SHEET 1-2.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 52,438 hrs · 19,835 cycles

DURING INSP OF HORIZ STAB UPPER AND LOWER CONSTANT SECTION SKIN PLANK FLANGE, FOUND 4 PANEL WITH CRACK IN FLYABLE LIMIT, P/N 7208-1, P/N 7207-1, P/N 7205-1, P/N 7204-1, SEE ATTACHED INSPECTION FINDING FORM. REPAIRED AREA IAW EA NR 8-5510-120477.

Part: FITTING — CRACKED (ZONE 600) · airframe 52,438 hrs · 19,835 cycles

RT WING OUTBD FLAP CRACK ON FITTING. REPAIRED AREA IAW EA 8-5750-120139.

Part: SKIN — CRACKED (ZONE 500) · airframe 52,438 hrs · 19,835 cycles

LT WING OUTBD FLAP CRACK ON LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 VOL I.

Part: WEB — CRACKED (NR 3 PYLON) · airframe 52,438 hrs · 19,835 cycles

AFTER REMOVAL ACCESS PANEL ON PYLON NR 3 WITH OAN J/C 0600B430-1JR FOUND HORIZ WEB WITH CRACKS. REPAIRED CRACKS IAW SRM 54-00-01 FIG 2B SHT 2 & FIG 13 SHT 6 VOL I.

Part: BRACKET — CRACKED (ZONE 600) · airframe 52,438 hrs · 19,835 cycles

PERFORMED INSP AFTER REMOVAL PANEL RT WING WITH OAN J/C MD10-2780620-1JR FOUND NR 3 CRACKS ON BRACKETS, RT WING DROOPED LEADING EDGE INTERNAL SIDE. REPAIRED AREA IAW SRM 57-00-01 FIG 10 SHT 1 VOL I.

Part: SKIN — CRACKED (ZONE 500) · airframe 52,438 hrs · 19,835 cycles

LT WING L/E CHORD FIXED PANEL FOUND CRACK. REPAIRED WING LOWER L/E STRINGER DOUBLER IAW SRM 57-10-00 FIG 49 VOL I.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 52,438 hrs · 19,835 cycles

LT WING LOWER SURFACE FOUND EXISTING REPAIR ON BEAVER TAIL NOT IN COMPLIANCE WITH SRM 57-00-01 VOL I FIG 8. ACCOMPLISHED EA 8-5710-120488.

Part: DOUBLER — CORRODED (ZONE 600) · corrosion level 2 · airframe 52,438 hrs · 19,835 cycles

RT WING MODERATE EXFOLIATION CORROSION ON LOWER BEAVER TAIL. ACCOMPLISHED EA NR 8-5710-120489.

Part: CAP — CRACKED (BULKHEAD) · airframe 52,438 hrs · 19,835 cycles

THE LOWER BULKHEAD CAP IS CRACKED IN 3 PLACES. LOWER LUG AT STR NR 43 FWD AND AFT, STR NR 44 AFT RT WING. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHT 3 VOL I.

Part: CAP — CRACKED (BULKHEAD) · airframe 52,438 hrs · 19,835 cycles

LOWER BULKHEAD CAP LUG IS CRACKED FWD SIDE. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHEET 2-3-4 VOL I.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 52,438 hrs · 19,835 cycles

LT HORIZONTAL STABILIZER. 1 DENT AND 1 CRACK, LONG .25 INCH ON UPPER SKIN PANEL, FROM STA XE 67 TO STA XE 73. REPAIR PANEL IAW SRM 55-00-01 VOL 1 FIG 3 SHEET 2.

Part: PANEL — CRACKED (ZONE 300) · airframe 52,438 hrs · 19,835 cycles

LT HORIZONTAL STABILIZER 1 DENT AND 1 CRACK, LONG .25 INCH ON UPPER SKIN PANEL, FROM STA XE 67 TO STA XE 73. REPAIR PANEL IAW SRM 55-00-01 VOL 1 FIG 3 SHEET 2.

Part: SKIN — CRACKED (ZONE 800) · airframe 52,438 hrs · 19,835 cycles

CENTER CARGO DOOR FOUND CRACK ON LOWER FWD SIDE EXT SKIN DOOR. REPAIRED SKIN IAW SRM 52-10-00 FIG 17 VOL I.

Part: SKIN — CRACKED (RUDDER) · airframe 52,438 hrs · 19,835 cycles

VERTICAL STABILIZER, RUDDER CRACK AND SUSPECT INTERNAL CORROSION ON SKIN UPPER FWD RUDDER. REPAIRED AREA IAW SRM 55-10-00 FIG 3 VOL I.

Part: SKIN — CRACKED (RT WING LE) · airframe 52,438 hrs · 19,835 cycles

RT WING EXT L/E CRACK ON SKIN (NEAR OLD REPAIR). REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 68 SHT 2.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 52,438 hrs · 19,835 cycles

LT HORIZONTAL STABILIZER DENT ON INBOARD L/E, DIM: 3 INCH BY 1.5 INCH BY .100 INCH. REPAIR AREA IAW SRM 55-00-01 FIG.3 SHT 2 VOL.1.

Part: SKIN — LOOSE (ZONE 600) · airframe 52,438 hrs · 19,835 cycles

RT WING OUTBD FLAP NR 80 FASTENERS LOOSE ON LOWER SKIN. REPAIR AREA IAW SRM 57-20-00 FIG.11 VOL.I.

Part: LIGHT — INOPERATIVE (L1 DOOR RAFT) · airframe 51,058 hrs · 19,136 cycles

L1 DOOR RAFT BOTTLE PRESS TO TEST LIGHT INOP. REMOVED L1 DOOR LWR SLIDE RAFT COVER, REPLACED BATTERIES, L1 DOOR LOW PRESS BOTTLE LIGHT PRESS TO TEST GOOD. REINSTALLED L1 DOOR LWR SLIDE RAFT COVER IAW FX DC10 MM 25-61-01-2 TIMCO MECH 97827,7389. REMOVED L1 DOOR LOWER SLIDE-RAFT COVER. REPLACED BATTERIES, L1 DOOR LOW PRESSURE BOTTLE LIGHT PRESS TO TEST GOOD. REINSTALLED L1 DOOR LOWER SLIDE-RAFT COVER IAW DC10 MM 25-61-01-2.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 51,055 hrs · 19,129 cycles

CORROSION ON UPPER SURFACE OF WEB AT MCD CUTOUT, AROUND NR 7 DOOR LATCH FITTING. REMOVED CORROSION IAW DC10-10 SRM 51-21-01 PG 28 VOL II, FOUND OUT OF LIMITS IAW DC10-10 SRM 53-00-01 PG 8 VOL II. REPAIRED OUT OF LIMITS AREA IAW FED EX EA 8-5310-105173 TITLED FUSELAGE, MDCD JAMB LOWER SILL CORROSION AT SPOOL 7, REPAIR. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW FED EX 8-5310-105173.

Part: RAIL — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,055 hrs · 19,129 cycles

CENTER LOWER CARGO, CORROSION ON DOOR JAMB OUTER RAIL FS 1682 LONGERON 43R. COMPLIED WITH FEDEX EA 8-5310-105182 FUSELAGE, CENTER CARGO DOOR RAIL CORROSION AT STA 1681 REPAIR.

Part: SEAT TRACK — CRACKED (BS 731-771) · airframe 51,055 hrs · 19,129 cycles

SEAT TRACK CRACKED NEAR NR 7 MCD LATCH FITTING REMOVED SEAT TRACK AT LBL 108 STA 731 TO 771 IAW DC/10MD10 SRM 53-70-00, VOL 1 PG 6 A. FABRICATED HAT CHANNEL AND SPLICE PLATE 7075T6 .050" PO 543247.6 HAT CHANNEL S4932154-N00 PO 563619.1 IAW DC/MD 10 SRM 53-70-00 VOL 1 PG 6. FABRICATED SEAT TRACK. REPAIR S4929149 PO 564954 IAW DC/MD10 SRM 53-70-00 VOL I PG 6. ALODINED AND PRIMED IAW DC/MD 10 SRM 51-21-01 VOL I PG 1-15. INSTALLED SEAT TRACK AND SEALED IAW DC/MD 10, SRM 53-70-00 VOL 1 PG 7.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 51,055 hrs · 19,129 cycles

RT HORIZONTAL AT STA. XE87 UPPER SKIN PLANK STRINGER 4 IS CRACKED. ACCOMPLISHED REPAIR IAW EA 8-5510-105177-STABILIZERS-HORIZ.-RT AFT OUTB. UPPER PANEL S4R CRACK AT XE 87-REPAIR. MECH 2579

Part: SKIN — CRACKED (ZONE 600) · airframe 51,055 hrs · 19,129 cycles

INSPECT/REPAIR/MOD LT AND RT TEE CAPS, CARD E8-5310-7-3327 PT.4. C/W FUSELAGE-AD96-18-11-LT AND RT 1156 BULKHEAD TEE AND SKIN CRACK-REPAIR. MAJOR REPAIR.

Part: BULKHEAD — CRACKED (ZONE 500) · airframe 51,055 hrs · 19,129 cycles

INSPECT/REPAIR/MOD LT AND RT TEE CAPS. CARD E8-5310-7-3327 PT.3. C/W E8--5310-105179- FUSELAGE-AD 96-18-11-LT AND RT 1156 BULKHEAD TEE AND SKIN CRACK-REPAIR. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,055 hrs · 19,129 cycles

FWD PIT BILGE STA-879 LOWER SURFACE OF TOP FLANGE OF OF WEB CORRODED AT LONGERON 43R. REMOVED CORROSION, TRIMMED OUT DAMAGE IAW DC/MD10 SRM 53-00-01 FIG 9 SHT 9. REMOVED FLOOR SUPPORT, STRAPS AND FILLERS IAW DC/MD 10 SRM 51-31-01 PAGE 1 VOLII. REPLACED FLOOR SUPPORT, STRAPS AND FILLERS IAW DC/MD10 SRM 51-31-01 PAGE 1 VOL II AND 53-00-01 FIG 9 SHT 9.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 51,055 hrs · 19,129 cycles

FOUND CRACK IN SUPPORT FITTING BELOW MAIN CARGO DOOR FWD ALIGNMENT FITTING, BETWEEN LATCH ROLLERS NR 2 AND NR 3. REMOVED AND REPLACED LOWER SUPPORT FITTING AND PLATE BETWEEN NR 2 AND NR 3 LATCH ROLLERS IAW DC/MD SRM 51-33-01 VOL II PGE 1, 51-21-01 VOL II PGE 1-19.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,055 hrs · 19,129 cycles

FWD PIT BILGE STA 879 LWR SURFACE OF TOP FLANGE OF WEB CORRODED AT LONGERON 43R. ACCOMPLISHED REPAIR PER EAM FUSELAGE FWD LOWER CARGO DOOR JAMB FRAME STA 866 CHORD REPAIR {8-5310-105181}.

Part: SILL — DENTED (ZONE 100) · airframe 51,055 hrs · 19,129 cycles

FWD CARGO DOOR CUT-OUT AFT SILL SEAL RETAINER DENTED STA 959 LONGERON 38R. REPAIRED IAW DC/MD SRM 53-50-00 VOL I, PAGE 132 AND EA 8-5310-105180 FUSELAGE FWD LOWER CARGO DOOR JAMB FRAME STA 959 CHORD AND SKIN REPAIR.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,055 hrs · 19,129 cycles

FWD PIT BILGE STA 879 LWR SURFACE OF TOP FLANGE OF WEB CORRODED AT LONGERON 43R. ACCOMPLISHED REPAIR PER EA FUSELAGE FWD LOWER CARGO DOOR JAMB FRAME STA 866 CHORD REPAIR {8-5310-105181}.

Part: DOUBLER — DAMAGED (ZONE 200) · airframe 51,055 hrs · 19,129 cycles

EXTERNAL FUSELAGE FROM FWD TO AFT SIDE LOWER EDGE CARGO DOOR CUT-OUT, SKIN DAMAGED ALONG SILL CUT-OUT, UPPER CARGO DOOR. REMOVED AND REPLACED DOUBLERS AT STA 629, 662, 676, 693 AND 762 AT MAIN CARGO DOOR LOWER SKIN IAW DC/MD10 SRM 51-33-01 VOL II PAGE 1 AND DC/MD10 53-50-00 VOL I.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 51,055 hrs · 19,129 cycles

RIGHT WING UPPER SKIN HAS SEVERAL AREAS OF SURFACE CORROSION XW118- XORS 264 (32 AREAS MARKED). REMOVED CORRODED AREAS NR 1 THRU NR 32 IAW DC10 SRM 57-10-00 FIG 59 VOL I AREAS NR 1 THRU NR 21 AND NR 23, NR 25, THRU NR 32 FOUND TO BE WITHIN LIMITS IAW DC10 SRM 57-10-00 FIG 59 VOL I AND 57-10-00 FIG 61 VOL I. AREA NR 22 STR 6 STA XORS 152, ORIG THICKNESS .230, MATERIAL REMOVED .027, REMAINING THICKNESS .0203 AREA NR 24 STR 24 STA XORS 139.5 ORIG THICKNESS .225, MAT. REMOVED .026, REMAINING THICKNESS .199 FOUND TO BE OUT OF LIMITS. REWORKED OUT OF LIMITS AREAS PER EA 8-5730-105174-WINGS, RT UPPER WING SKIN CORROSION AT STRG 6 XORS 139.5 AND 152 -REPAIR.

Part: SKIN — DENTED (ZONE 600) · airframe 51,055 hrs · 19,129 cycles

RIGHT WING L/EDGE FWD OF PRESSURE "REFUEL" PANEL AT XORS 510 TO XORS 538 DENTED 2 AREAS. REMOVED, REPLACED, FABBED AND INSTALLED DOUBLER IAW DC10 SRM 57-00-01 FIG 4 SHEET 2 VOL I . ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II.

Part: SKIN — DENTED (ZONE 600) · airframe 51,055 hrs · 19,129 cycles

RIGHT WING L/EDGE FWD OF PRESSURE "REFUEL" PANEL AT XORS 510 TO XORS 538 DENTED 2 AREAS. REMOVED, REPLACED, FABBED AND INSTALLED DOUBLER IAW DC10 SRM 57-00-01 FIG 4 SHEET 2 VOL I, ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 51,055 hrs · 19,129 cycles

FOUND MAIN CARGO COMPARTMENT STA.999 48RBL SEAT TRACK GOUGED. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC/MD SRM 51-31-01 VOL II PG 1, 53-70--00 VOL1 PG 5, 51-21-01 VOL II PG1-18.

Part: SPAR CAP — CRACKED (ZONE 300) · airframe 51,055 hrs · 19,129 cycles

FOUND RIGHT AFT OUTBOARD SPAR CAP CRACKED FROM HOLE TO HOLE AND INSIDE THE BOREHOLE (NOTIFY STRUCTURES ENGINEERING PRIOR TO FURTHER FLIGHT). E8-5510-7-3310 PT.4. REPAIRED RIGHT AFT OUTBOARD SPAR CAP IAW FEDEX EA 8-5510-105170-STABLIZER HORIZ.- AD92-22-10-R/H UPPER AFT SPAR SPLICE-REPAIR. MECH 4315 QC364 MAJOR REPAIR

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 51,055 hrs · 19,129 cycles

FOUND MAIN CABIN SEAT TRACK FROM STA 1507 TO 1587 AT LBL 48. REMOVED AND REPLACED SEAT TRACK SECTION IAW MD/DC1 SRM 53-70-00 FIG 2A VOLI, 51-31-01 VOLII PG 1 AND 51-21-01 VOLII . MAJOR REPAIR.

Part: SEAT TRACK — GOUGED (ZONE 600) · airframe 51,055 hrs · 19,129 cycles

FOUND MAIN CARGO COMPARTMENT STA 795 RBL 48,SEAT TRACK IS GOUGED. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC/MD10 SRM 53-70-00 FIG 1 VOL.I, 51-21-01 VOL II PG1-18. MAJOR REPAIR, MECH 2579, QC227.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 51,055 hrs · 19,129 cycles

FOUND MAIN CARGO COMPARTMENT SEAT TRACK AT LBL10 AT STA 1521 IS GOUGED. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC/MD10 SRM 51-31-01 VOL II,53-70-00 VOL I FIG 1 AND 5. MAJOR REPAIR MECH 110847, QC423.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 51,055 hrs · 19,129 cycles

FOUND MAIN CARGO COMPARTMENT STA 535 RBL 28, SEAT TRACK GOUGED. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC/MD10 SRM 53-70-00 PAGE 21 VOL I, 51- 31-0 VOL II PG 1,53-70-00 VOL I FIG 1 PG 4.

Part: FITTING — CORRODED (CARGO DOOR) · airframe 51,055 hrs · 19,129 cycles

MAIN CARGO DOOR LOWER DOOR FITTINGS (SPOOLS) HAVE EVIDENCE OF CORROSION AT SERRATED PLATE ATTACH POINTS. (04 APRIL 07) REQUIRE REMOVAL FOR FURTHER INSPECTION ,ALL 7 SPOOL FITTINGS. FOUND SPOOLS 1-7 WITH CRACK INDICATIONS, AND A CRACK IN NR 7 LOWER LATCH SUPPORT FITTING BELOW WEB. REMOVED AND REPLACED NR 1-7 SPOOL FITTINGS IAW DC10-10 SRM 51-33-01. REAMED ATTACH HOLES IN NR 7 JAMB BEAM TO REMOVE CRACK, VERIFIED CRACK REMOVAL IAW NDT SPM 06-10-01.003, NO CRACK INDICATION. INSTALLED REPAIR BUSHINGS PER SRM 53-50-00 VOL I, 51-39-01 VOL II P4. RIGGED AND OPS CHECKED MCD IAW DC 10-10 AMM 52-34-00-5. OPS CHECK GOOD.

Part: WIRE — PULLED (FIRE BOTTLE) · airframe 48,764 hrs · 17,946 cycles

NR 2 ENGINE FIRE BOTTLE HAS 2 WIRES PULLED FROM PRESS SWITCH ON INBOARD BOTTLE. REMOVED AND REPLACED NR 2 FIREBOTTLE SWITCH CONNECTOR P1-1264 IAW BSWPM 20-31-03. REMOVED AND REPLACED TERMINAL STRIP S3-403 IAW BSWPM 20-20-03. REPLACED WIRING 2W253L22 AND 2W258A22N IAW BSWPM 20-10-01 AND DC10-10MM 26-21-01-05, LOW PRESSURE TEST GOOD IAW DC10-10MM 26-21-06-2.

Part: CONTROL UNIT — MALFUNCTIONED (AURAL WARNING) · airframe 48,447 hrs · 17,775 cycles

PASSING 10000 FT ACCELERATING THROUGH 260 KNOTS. THE AURAL OVERSPEED WARNING SOUNDED (SLATS RETRACTED) CLEAN CONFIGURATION SLOWED AND RECYCLED SLATS AND ACCELERATED AGAIN PASSING 260 KNOTS THE WARNING CAME ON AGAIN. ALSO TRIED CADC BOTH 1 AND BOTH ON 2 AND THE HORN STILL SOUNDED. REMOVED AND REPLACED AURAL WARNING UNIT IAW DC10-10 MM 31-51-00-5. OPS CHECK GOOD IAW DC10-10MM 31-51-00- 5. OK FOR SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 47,941 hrs · 17,533 cycles

NR 2 ENGINE OIL LEAK. ON CLIMBOUT NR 2 ENG OIL QTY DROPPED 18 QTS TO 9 QTS ON FINAL NR 2 OIL READ 3 QTS, AFTER LANDING NR 2 OIL QTY WAS 9 PTS. REMOVED & REPLACED B-SUMP SCAVENGE LINE IAW MM 79-00-01-1. FUEL SHROUD REMOVED AND REPLACED REF WRI 73-10/0359. RAN NR 2 ENG HIGH PWR PER JRH OPENED NR 2 ENG CORE COWL CHECKED FOR LEAKS, NO LEAKS NOTED. CLOSED NR 2 ENG CORE COWL PER AMM 79-00-01-1.

Part: SWITCH — MALFUNCTIONED (AC PACK DOOR) · airframe 46,572 hrs · 16,894 cycles

THE AIR COND DOORS LIGHT ILLUMINATED CLIMBING OUT AT 7.5 PSID. THE LIGHT WENT OUT AT 4.0 PSID. FOLLOWED QRH PROCEDURES, RETURNED TO MEMPHIS. RELEASED FOR SERVICE PER MEL/CDL: 52-04-04 CATEGORY: C EXPIRATION: 16APR04 MEL 52-04-04: AIR CONDITIONING DOOR CAUTION LIGHT INOP. VERIFY AND RECORD IN AML/EAML AIR CONDITIONING DOOR IS CLOSED AND LOCKED BY VISUAL INSPECTION PRIOR TO EACH DEPARTURE. VERIFIED DOORS CLOSED AND LOCKED PRIOR TO DEPARTURE. OK TO CONTINUE. MX REMOVED AND REPLACED LEFT AIR COND DOOR WARNING SWITCH P1- 1618. ALSO REPAIRED BROKEN WIRE AT TERMINAL STRIP S3-490. SYS OPS CHECK OK.

Part: BOLT — INCORRECT (TE FLAP) · airframe 46,498 hrs · 16,861 cycles

I/B FLAP O/B FITTING BOLT HAS THE INCORRECT BOLT IN THIS POSITION. *S/D* MX INSTALLED CORRECT BOLT IN A FOREMENTIONED POSITION.

Part: FRAME — CORRODED (E/E BAY DOOR) · airframe 46,248 hrs · 16,736 cycles

THE LOWER INNER FRAME OF THE AFT AVIONICS COMPARTMENT DOOR 115AZ HAS SEVER CORROSION. REMOVED DOOR IAW M/M 52-41-01-2, REMOVED CORRODED PARTS IAW SRM 51-31-01, NEW CAP ANGLES FABBED ON MAE TRAVLER T4/392156 AND T2/392154. SPLICE FABBED ON T2/392153, INTERCOSTALS FABBED ON T2/392148 AND T2/392152. INSTALLED NEW PARTS IAW SRM 51-31-01. INSTALLED DOOR IAW M/M 52-41-01-2.

Part: DRIVE CHAIN — OUT OF RIG (ZONE 800) · airframe 46,248 hrs · 16,736 cycles

COMPLY WITH EA 8-5211-73858. DOORS- ENTRY DEVIATION TO FWD PAX DOOR DRIVE CHAIN RIGGING. CLOSING ACTION ON 01/03/04 ON N/R S00024. COMPLIED WITH EA 8-5211-73858.

Part: BULKHEAD — GOUGED (ZONE 500) · airframe 46,248 hrs · 16,736 cycles

COMPLY WITH EA 8-5710-73861 WINGS MAIN FRAME GOUGE REPAIR XORS 562.390 FLAP BULKHEAD UPPER CAP (LT). CLOSING ACTION ON N/R S00027, ON 13/30/03. COMPLIED WITH EA 8-5710-73861.

Part: SUPPORT FITTING — WORN (THRUST REVERSER) · airframe 46,248 hrs · 16,736 cycles

COMPLY WITH EA 8-7832-73857. EXHAUST - THRUST REVERSER - REWORK OF WORN AREA ON T-R SUPPORT FITTING. CLOSING ACTION ON N/R S00022 ON 12/29/03. COMPLIED WITH EA 8-7832-73857.

Part: CAP — GOUGED (T/E FLAP) · airframe 46,248 hrs · 16,736 cycles

COMPLY WITH EA 8-5710-73861. WINGS MAIN FRAME GOUGE REPAIR XORS 562.390 FLAP BULKHEAD UPPER CAP (LT). CLOSING ACTION ON N/R S00027, ON 13/30/03. COMPLIED WITH EA 8-5710-73861.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 46,248 hrs · 16,736 cycles

COMPLY WITH EA 8-5310-73862. FUSELAGE MAINFRAME- MINOR DEVIATION TO SRM SEAT TRACK SPLICE. CLOSING ACTION ON 12/24/03. ON N/R S00031. COMPLIED WITH EA 8-5310-73862.

Part: HINGE — CORRODED (T/E FLAP) · airframe 46,248 hrs · 16,736 cycles

COMPLY WITH EA 8-5740-73863. WINGS- RIGHT INBOARD FLAP, REWORK OF CORROSION IN AFT HINGE ASSY PIVOT BORE. CLOSING ACTION ON 12/24/03. ON N/R S00032. COMPLIED WITH EA 8-5740-73863.

Part: BRACKET — CORRODED (WING) · airframe 46,248 hrs · 16,736 cycles

COMPLY WITH EA 8-5740-73859 REV A WINGS - RT OUTBOARD HINGE BRACKET - SIDE LOAD FITTING HOLE REPAIR (P/N ARC0153). COMPLIED WITH EA 8-5740-73859.

Part: FITTING — CORRODED (T/E FLAP) · airframe 44,233 hrs · 15,816 cycles

RIGHT WING OUTBOARD FLAP - AT REAR SPAR JUST INBOARD OF TOP MOUNT BOLT FOR INBOARD HINGE SUPPORT FITTING IS CORRODED. REMOVED AND REPLACED FITTING PER SRM 51-21-00 VOL 2.

Part: ENGINE — INOPERATIVE (NR 2)

NR 2 ENGINE FLAMED OUT NOTICED WHEN ENGINE ANTI-ICE TURN ON AND NR 2 A/I DISAGREE LIGHT CAME ON. *S/D* REMOVED AND REPLACED LINE ENGINE, OPS CK OK.

Part: TARGET SENSOR — BROKEN (LT MLG)

LEFT MAIN GEAR INDICATION ON BOTH PANELS REMAINED RED AFTER RETRACTION. RAN CHECK LIST PROCEDURES WITHOUT SUCCESS. SUBMITTER FEELS THE GEAR IS RETRACTING AND EXTENDING OK, BUT LIGHTS STAY RED. FOUND TARGET SENSOR ON MAIN GEAR DOOR BROKEN. REPLACED TARGET SENSOR PER MM 32-6.