N68053

Part: O-RING — BLOWN (TRIM MOTOR) · airframe 78,320 hrs · 33,421 cycles

SHORTLY AFTER DEPARTURE AT FL170 RECEIVED HYD 3 ELEV OFF. WE NOTICED THE HYD 3 FLUID DECREASING RAPIDLY BELOW 4 GALLONS, WENT THROUGHT THE VARIOUS HYD CHECKLISTS. "HYD 3 ELEV OFF" LEVEL ONE THE "HYD QTY LOW" THE "HYD 3 FAIL". COMPLETED QRH AND DID MANUAL GEAR EXTENSION, AS PER CHECKLIST. WALK AROUND SHOWED SYSTEM 3 RESERVOIR TOTALLY EMPTY OF FLUID. NO LEAKS SHOWING FORWARD OF AND INCLUDING APU AREA. COMPARTMENT OF RMP 2-3 AND RESERVOIR NR 2 SHOWS SIGNS IN LOWER PORTIONS OF EXCESS HYDRAULIC LEAK. DURING REFILL OF NR 3 SYSTEM, HYDRO FLUID BEGAN FLOWING OUT OF COMPARTMENT JUST FORWARD OF APU MAIN DOOR. FOUND RIGHT STAB TRIM MOTOR O-RING BLOWN OUT AT THE BASE. WE HAVE MOTOR W/KIT IN STOCK IND.

Part: PUMP — MALFUNCTIONED (OIL QUANTITY) · airframe 77,846 hrs · 33,113 cycles

AFTER ENGINE START & TAXI OUT, ENG NR 3 OIL QUANTITY REMAINED AT 11. IMMEDIATELY AFTER TAKEOFF AT 800 FT OIL QTY DROPPED TO 4, THEN BOXED AMBER AT 3. OIL TEMP WAS HIGHER (127 DEG) THAN THE OTHER ENGINES. OIL PRESS APPEARED NORMAL. PULLED THE ENGINE BACK AND OIL QTY NEVER GOT ABOVE 9 WITH OIL TEMPERATURE STAYING 15-20 DEG HIGHER THAN OTHER ENGINES. NEVER SHUT ENGINE DOWN IN FLIGHT. CHECKED MASTER CHIP DETECTOR, LUBE AND SCAVENGE INLET STRAINER, AND SUPPLY FILTER ELEMENT, NO METALLIC PARTICLES OR EXCESSSIVE CONTAMINATION NOTED, R & R NR 3 LUBE AND SCAVENGE PUMP IAW AMM 79-20-04-2, LEAK & OPS CHECKED GOOD. RAN ENG AT HIGH POWER FOR 30 MINS, NO DEFECTS NOTED. SYSTEM OK FOR SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 77,691 hrs · 33,018 cycles

AFT FUSELAGE STA 1986 L46L SKIN CORROSION. REPAIRED DAMAGED SKIN PER SRM 53-20-00, VOL I, FIG 6 SHEET 13.

Part: BEAM — CRACKED (BS 1256-1305) · airframe 77,691 hrs · 33,018 cycles

L3 DOOR NR 1 UPPER BEAM CRACKED ON THE AFT END. REMOVE AND REPLACED THE BEAM.

Part: FLOOR SUPPORT — CORRODED (BS 655) · airframe 77,691 hrs · 33,018 cycles

MAIN CABIN, BS 655, RBL 86 FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG AEA7415, AND SRM 51-31-01 VOL2

Part: DOOR FRAME — DAMAGED (MAIN CARGO) · airframe 77,691 hrs · 33,018 cycles

MAIN CARGO LOWER DOOR FRAME AND FITTING NR 5 LATCH SPOOL HAS A DEEP BLEND OUT. REMOVED DAMAGE AND INSTALLED A REPAIR IAW SRM 53-50-00.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 77,691 hrs · 33,018 cycles

MAIN CABIN, RT APPROX 1521 RBL 48 SEAT TRACK IS WORN. REMOVED AND REPLACED DAMAGED SEAT TRACK SECTION FROM EXISTING SPLICES AT STA 1491 TO 1551 REF SRM 53-70-01 FIG 1 VOL. 1, SRM 51-31-01 V 2, DWG SR 10-53-002, MAJOR REPAIR.

Part: SUPPORT — CORRODED (BS 1521) · airframe 77,691 hrs · 33,018 cycles

CENTER CARGO BAY BS 1521, LONGERON 43R SUPPORT BRACE HAS CORROSION. REMOVED AND REPLACED THE SUPPORT BRACE IAW SRM 53-00-01, FIG 9, SHEET 3.

Part: BEAM — CRACKED (R3 DOOR) · airframe 77,691 hrs · 33,018 cycles

R3 DOOR UPPER BEAM AFT SIDE STOP FITTING IS BROKEN. REMOVE AND REPLACE BEAM PER DWG ADA0006-1 & SRM 51-31-01 V II.

Part: BEAM — CRACKED (R3 DOOR) · airframe 77,691 hrs · 33,018 cycles

R-3 DOOR UPPER BEAM AFT SIDE STOP FITTING IS BROKEN. REMOVE AND REPLACE BEAM PER DWG ADA0006-1 & SRM 51-31-01 V II.

Part: DOUBLER — CRACKED (BS 1721) · airframe 77,691 hrs · 33,018 cycles

LOWER FUSELAGE, CENTER CARGO DOOR, SUSPECTED CRACK ADJACENT TO ACTUATOR ARM LINK. REPAIRED IAW SRM 52-00-01, VOL I, FIG 9, SHT 6, PG 47 &48.

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 77,691 hrs · 33,018 cycles

RIGHT HORIZONTAL STAB HSS 56, WEB CRACKED AT THE FWD OF RIB. REPAIRED IAW SRM 55-00-01, VOL 1, FIG 9.

Part: CHANNEL — CORRODED (BS 2007) · airframe 77,691 hrs · 33,018 cycles

AFT WASTE TANK BAY, RT HAT CHANNEL HAS CORROSION. THE HAT CHANNEL WAS REMOVED AND REPLACED IAW DRAWING NJC6040.

Part: TEE FITTING — CRACKED (BULKHEAD) · airframe 77,691 hrs · 33,018 cycles

L/H STA. 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39L HAS A .250 IN. CRACK AT THE LOWER FASTENER HOLE. L/H STA. 595 BULKHEAD TEE CAP REPAIRED REF E.A. 8-5310-T0332347. REPAIR CLASSIFIED AS MAJOR.

Part: BEAM — BROKEN (R3 DOOR) · airframe 77,691 hrs · 33,018 cycles

R-3 DOOR UPPER BEAM AFT SIDE STOP FITTING IS BROKEN. REMOVED & REPLACED BEAM PER DWG ADA0006-1 & SRM 51-31-01 V II.

Part: SKIN — CRACKED (LT WING) · airframe 77,691 hrs · 33,018 cycles

LT WING TELESCOPING DUCT L/E CUTOUT UPPER OUTBD CORNER IS CRACKED. LT WING TELESCOPING DUCT L/E CUTOUT UPPER O/B CORNER REPAIRED IAW SRM 57-10-00.

Part: DOUBLER — CRACKED (LT WING) · airframe 77,691 hrs · 33,018 cycles

LEFT WING FIXED L/E, NR 10 SLAT TRACK CUTOUT AFT INBD CORNER CRACKED. INSTALLED REPAIR DOUBLER AND FILLER AT NOTED LOCATION IAW SRM 57-10-00, FIG 68, VOL1.

Part: PANEL — MALFUNCTIONED (ELECTRICAL) · airframe 77,437 hrs · 32,880 cycles

ELECTRICAL PANEL HAS TWO ON LIGHTS FOR EMERGENCY POWER, SHOULD HAVE ONE OFF AND ON. REMOVED AND REPLACED ESCP IAW AMM 24-08-02-4 AND PERFORMED ADJUSTMENT AND TEST IAW 24-08-02-5. OPS CHECKED GOOD.

Part: SWITCH — FAILED (MLG HANDLE) · airframe 77,133 hrs · 32,723 cycles

AFTER TAKEOFF, WITH GEAR HANDLE IN THE UP POSTION , RECEIVED THREE RED GEAR UNSAFE LIGHTS. CONFIGURATION PAGE SHOWED THREE GEAR UNSAFE ALSO. RAN QRH INCLUDING PUTTING GEAR HANDLE DOWN AND RECEIVED THREE GREEN INDICATIONS. RETRACTED GEAR HANDLE AND RECEIVED THE SAME GEAR UNSAFE INDICATIONS. ALL RETRACTIONS FELT NORMAL. AFTER APPROX 20 MINUTES AT A SPEED OF 230, ALL INDICATIONS WENT NORMAL , CONTINUED FLIGHT. LANDING WAS NORMAL. FOUND COM 1 WIRE LOOSE ON SWITCH IAW WDM 32-63-01, TRIED TO RETIGHTENED SCREW BUT WOULD NOT TIGHTEN. REMOVED AND REPLACED GEAR HANDLE CONTROL SWITCH S1-431 IAW AMM 32-61-04-2, OPS CHECKED GOOD. ACCOMPLISHED PSEU FUNCTIONAL RTS TEST IAW AMM 31-71-01-2. ALL TESTS PASSED. OK FOR SERVICE.

Part: DOOR — FAILED (MLG) · airframe 76,839 hrs · 32,555 cycles

AFTER TAKE OFF, WHEN RETRACTING THE MLG, THE LEFT MAIN GEAR STAYED UNSAFE FOR ABOUT ONE MINUTE LONGER THAN THE OTHER TWO GEAR. THE CONFIG PAGE AGREED WITH THE PANEL INDICATORS AS BEING UNSAFE. THE UNSAFE INDICATION WENT AWAY BY ITSELF AND THERE WERE NO OTHER PROBLEMS REMAINDER OF FLIGHT. FOUND L/E MIN LANDING GEAR ACTUATOR SUPPORT STRUCTURE BROKEN WHERE ACTUATOR ATTACHES TO MLG DOOR FRAME, REMOVED AND REPLACED MLG DOOR IAW MM 32-14-01-2.

Part: MONITOR — NO TEST (ESCAPE SLIDE) · airframe 76,722 hrs · 32,494 cycles

DURING PREFLIGHT, NOTICED RIGHT SIDE AIRCRAFT SLIDE TEST WOULD NOT ILLUMINATE. REMOVED AND REPLACED PRESSURE INDICATOR. OPS NORMAL.

Part: SWITCH — FAILED (L1 DOOR) · airframe 76,285 hrs · 32,274 cycles

L1 DOOR WILL NOT CLOSE CORRECTLY WITH SWITCH. CLOSES ALL THE WAY, THEN REVERSES TO OPEN DOOR WHEN HOLDING SWITCH DOWN IN THE CLOSED POSITION. MEL 52-10-01: L1 DOOR ELECTRIC DOOR ACTUATOR - INOP. FOR EMERGENCY EGRESS, USE PNEUMATIC SYSTEM TO OPERATE DOOR." INSIDE SWITCH OPERATES DOOR INCORRECTLY. R&R L1 EXTERNAL DOOR SWITCH S1-1013 REF WDM52-11-01, PERFROMED OPS CHECK PER MM 52-10-01-05. DOOR OPS CHECKS NORMAL.

Part: LAMP — INOPERATIVE (SLIDE TEST LIGHT) · airframe 75,892 hrs · 32,086 cycles

CABIN DOOR FWD RT SLIDE TEST LIGHT INOPERATIVE. REPLACED THE LAMP. OPS CHECKED GOOD IAW 25-61-03-5.

Part: TRANSDUCER — FAULTY (HORIZ STAB) · airframe 754 hrs · 31,852 cycles

WHEN PUSHING THROTTLES UP FOR TAKEOFF, STAB TRIM WAS SET AT 4.4. WE IMMEDIATELY GOT RED BOX ON EAD. TAKEOFF WAS REJECTED. R & R NR 2 HORIZONTAL STAB LVDT IAW MM 27-45-01-4. R & R NR 2 FCC PRECAUTIONARY IAW 22-01-03-4.

Part: CABLE — DAMAGED (VSV) · airframe 754 hrs · 31,831 cycles

REJECTED TAKEOFF DUE TO NR 3 ENGINE NOT SPOOLING UP TO TAKEOFF POWER. REJECT SPEED LESS THAN 80 KIAS NR 1 & 2 APPROX 103% N1, NR 3 STOPPED ACCELERATING AT APPROX 96 % N1 WHERE THROTTLE POSITION HAD NO FURTHER EFFECT. TROUBLESHOT IAW FIM 71-00-00-2 FIM AND IN CONJUCTION WITH MTSI 73-21/1233. PERFORMED VSV FOLLOWUP CABLE PULL CHECK IAW AMM 73-20-01-2. OPS CHECKED BAD. REQUIRED 12 LBS TO PULL AND LIMIT IS 8 LBS. ALSO NOTED EXCESSIVE WEAR IN CABLE ENDS. REPLACED NR 3 ENGINE VSV FOLLOWUP CABLE AND PERFORMED VSV RIG IAW AMM 73-20-01-2. PERFORMED MAX POWER ASSURANCE RUN ON ALL 3 ENGINES. NO DESCREPANCIES NOTED AND THROTTLE ALLIGMENT WAS GOOD AT 99.8% N1. VSV LINES LEAK CHECKED GOOD.

Part: SENSOR — DIRTY (LANDING GEAR) · airframe 753 hrs · 31,770 cycles

RIGHT GEAR UNSAFE WITH GEAR HANDLE DOWN. PUT GEAR UP & BACK DOWN. GREEN INDICATION PRIMARY & SECONDARY THE SECOND TIME. PSEU FAULTED RT GEAR UP & LATCHED AB SENSOR DISAGREE. INSPECTED & CLEANED SENSOR & TESTED IAW AMM 32-61-15-4.

Part: SENSOR — FAILED (RT MLG) · airframe 753 hrs · 31,769 cycles

UNSAFE GEAR INDICATION, RT MAIN GEAR ON TAKEOFF ROLL. ABORTED TAKEOFF AT APPROX 50 KTS. REJECT CHECKLIST ACCOMPLISHED. RT MAIN GEAR UP LATCHED INDICATION SENSOR INOPERATIVE. OBSERVE CARGO CONTAINER LOADING RESTRICTIONS & VERIFY AFFECTED POSITIONS ARE VOIDED ON WEIGHT & BALANCE. PSEU SENSOR READOUT SHOWS RGUPLCHB REQUIRES ADJUSTMENT. ADJUSTED UPLATCH SENSOR IAW AMM 32-61-15-4, NO HELP. R&R RT UPLATCH SENSOR MPN 8-627-01 IAW AMM 32-61-15-4, RECHECKED SENSOR CLEARANCE, ALL CHECKS WITHIN LIMITS. OP`S CHECKS NORMAL IAW AMM 31-70-01 AND 32-61-15-011-05. A/C OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 750 hrs · 31,599 cycles

L1 DOOR SLIDE PRESS TO TEST LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-01.

Part: SKIN — CRACKED (FUSELAGE) · airframe 748 hrs · 31,472 cycles

SUSPECT CRACK AT THE NR 3 PACK BAY DOOR, UPPER LT CORNER SKIN SURROUND CUT OUT, RUNNING THROUGH A RIVET.

Part: SKIN — CORRODED (RT ELEVATOR) · airframe 748 hrs · 31,470 cycles

RIGHT OTBD ELEVATOR BOTTOM SKIN AFT FROM LE CORRODED. R & R RT OTBD ELEVATOR IAW AMM 27-30-02-4.

Part: SKIN — CRACKED (TE FLAP) · airframe 748 hrs · 31,470 cycles

RIGHT WING, INBD FLAP UPPER SKIN APPROX 10 INCHES FWD OF TE HAS 1" CRACK ON SKIN. REPAIRED IAW SRM 57-10-00 FIG 85. TRACKING EA T 8-5750-T0316953.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 748 hrs · 31,470 cycles

SEAT TRACK WORN LOBE. SPLICE IN NEW SECTION.

Part: SEAT TRACK — WORN (BS 810) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK STATION APPROX 810, LBL 25 HAS DAMAGED LOBE.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

NUMBER 3 PACK RT SIDE LONGERON 33 IS CORRODED, APPROX STATION 555. CUT OUT OLD DAMAGE SECTION OF LONGERON, 24", & INSTALLED NEW LONGERON & SPLICE IAW SRM53-00-01 VOL 2.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED, STATION 1384 LT 27.50. REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED, STATION 1641 LT 47.50. REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED, STATION 1561 LT 47.50. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED STATION 879 LT 8.50. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00- FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED STATION 1390 LT 8.50. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED STATION 1641 LT 8.50. REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED STATION 1540 LT 8.5. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAN DECK SEAT TRACK DAMAGED STATION 1530 LT 8.50. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED STATION 1641 RT 45.50. REPLACED DAMAGED SECTION OF SEAT TRACK IAW RM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED STATION 939 45.50 RT. R & R SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED, STATION 1510 LT 47.50. REPLACED DAMAGED SEAT TRACK SECTION IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED STATION 1648 - 1658 RT, 4 PLACES. REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED STATION 1735 LT 47.50. REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED STATION 1641 RT 27.50. REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED, STATION 1520 LT 47.50. REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: PULLEY — DAMAGED (L1 DOOR) · airframe 748 hrs · 31,470 cycles

L1 DOOR THREE UPPER FWD PULLEYS ARE DAMAGED, AND BROKEN. REMOVE AND REPLACE PULLEYS PER AMM 52-10-02-2 .CHECKED FOR PROPER ALLIEMENT AND RIGGED PER AMM 52-11-00-5.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MIAN DECK SEAT TRACK DAMAGED STATION 879 RT 27.50. R & R SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

MAIN DECK SEAT TRACK DAMAGED STATION 1382 LT 8.50. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1.

Part: PANEL — DELAMINATED (LT WING) · airframe 748 hrs · 31,470 cycles

LEFT WING UPPER SURFACE TRAPEZOID PANEL, ARC0274-503, HAS DELAMINATION APPROX 11 1/2" X 12". REPAIR PANEL ARCO274-503 IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 748 hrs · 31,470 cycles

LEFT WING SPOILER NR 4 HAS DELAMINATION APPROX 4 1/2 X 7 1/2 UPPER SURFACE. REPAIRED SPOILER NR 4 IAW SRM 51-71-00 VOL II. PREP & PAINT IAW SRM 51-21-02 VOL II.

Part: SKIN — CRACKED (FUSELAGE) · airframe 748 hrs · 31,470 cycles

NUMBER 3 PACK DOOR CUT OUT AFT CORNER HAS A 1 INCH LONG CRACK FROM EDGE OF CUT OUT TO RIVET & PAST 1/2 INCH. REPAIRED IAW SRM 53-50-00 FIG 3A.

Part: SWITCH — DAMAGED (ESCAPE SLIDE) · airframe 746 hrs · 31,387 cycles

ON COCKING CHECK, CRACKED R1 DOOR SLIDE RAFT BOTTLE PRESSURE INDICATOR PUSH BUTTON COVER, WITH SWITCH COVER CRACKED, BUTTON WILL NOT SPRING RETURN BACK TO NORMAL UNTESTED POSITION. REMOVED, INSPECTED, AND REINSTALLED R1 REMOTE SLIDE BOTTLE PRESSURE SWITCH. FOUND SWITCH TO BE IN OPERATIONAL ORDER AND PERFORMED OPS CHECK IAW MD-10 AMM 25-61-03-5. OPS CHECKED GOOD.

Part: SKIN — CRACKED (LT WING) · airframe 73,807 hrs · 30,922 cycles

SUSPECTED CRACK AT INBD CUT OUT OF THE NR 6 SLAT. HFEC LT WING INBD CUT OUT NR 6 SLAT CRACK INDICATED IAW NTSP M06-10-01 BY NDT. INSTALLED REPAIR DOUBLER & FILLER IAW SRM & APPLIED TOP COAT.

Part: CHAIN — BROKEN (L1 DOOR) · airframe 73,626 hrs · 30,826 cycles

WHEN REMOVING ACCESS PANEL TO DEPRESSURIZE PNEUMATIC DRIVE RESERVOIR AIR MOTOR, DRIVE CHAIN DROPPED OUT OF PANEL FOR THE L1 DOOR. CHAIN WAS BROKEN. L1 PNEUMATIC MOTOR REPLACED ON WORK CARD 52C1101. INSTALLED NEW CHAIN ASSEMBLY ON PNEUMATIC AIR MOTOR TO ELEC MOTOR FOR L1 DOOR IAW DWG ABA7941. OPERATIONAL CHECK OF L1 DOOR PNEUMATIC ACTUATION SYS WAS PERFORMED ON WORK CARD 52C1101 STEPS 5 THRU 12.

Part: PUSH-PULL CABLE — FAILED (NR 2 THROTTLE) · airframe 73,398 hrs · 30,701 cycles

DURING INITIAL DESCENT FROM FL 350, NR 2 THROTTLE FROZE AT 83 PERCENT N1. DESCENDED TO WARMER AIR, 4000FT. HELD FOR 25 MINUTES TO TRY & FREE. ACCOMPLISHED PRECAUTIONARY SHUTDOWN & QRH PROCEDURES. REMOVED AND REPLACED THE THROTTLE PUSH PULL CABLE FRROM THE ENGINE TO THE DRUM IAW AMM 76-11-01-2.

Part: STIFFENER — CRACKED (BS 1139-1159) · airframe 72,502 hrs · 30,274 cycles

CENTER ACCESSORY COMPARTMENT RT VERTCAL STIFFENER AT DOMED PRESSURE PANEL CRACKED. MARKED OTBD OF CARGO FIRE BOTTLE ABOVE L43R REMOVED NYB60427-7 ATTACHMENT ANGLE AND -89 DOUBLER REF SRM 51-30-00, VOL II. DRILLED MET NEW -7 AND -89 ANGLE REF DWG NYB6042 AND INSTALLED NEW -7 ANGLE AND -89 DOUBLER, REF DWG NYB6042.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 72,502 hrs · 30,274 cycles

HORIZONTAL STAB LT PANEL ALC7439-1 HAS APPROX. THREE INCH CRACK AT AFT CLOSING RIB BETWEEN THREE HOLES ALSO APPROX FOUR INCH CRACK ALONG STRINGER 1 AND 3 BETWEEN AFT CLOSING RIB AND XE 43. REPAIRED IAW EA 8-5510-90823.

Part: SKIN — CORRODED (BS 1999) · corrosion level 2 · airframe 72,502 hrs · 30,274 cycles

AFT FUSELAGE WASTE TANK BAY INTERAL SKIN CORRODED BS 1999, L45-46L. REMOVED CORROSION AND BLENDED OUT CORROSION ON UPPER SURFACE OF KEEL PLANK IAW SRM 51-21-01 VOL II. NDT MAPPED AREA FOR MATERIAL THICKNESS, FOUND SKIN THICKNESS TO BE LESS THAN .100" IN ISOLATED AREAS. FABRICATED AND INSTALLED DOUBLER IAW SRM 51-33-01, VOL II.

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 72,502 hrs · 30,274 cycles

NR 1 PYLON UPPER SPAR WEB, CRACK FOUND IN THE INBD SIDE APROX. 15" FWD OF THE AFT END OF THE PYLON; CRACKED FORM BOLT HOLE TO THE EDGE OF THE WEB AND INBD FROM THE BOLT HOLE. HEC VERIFIED. NR 1 PYLON UPPER SPAR WEB R & R ON EA T8 5450-T0301674 P1. NOTE: ENGINE AND PYLON REMOVED AND REINSTALLED FOR REPAIR.

Part: SPAR CAP — CRACKED (ZONE 300) · airframe 72,502 hrs · 30,274 cycles

LEFT HORIZONTAL STAB UPPER SURFACE, AFT SPAR CAP, FOUND DISCOUNTINITY IN AFT BARREL NUT HOLE. LOCATED AT 1.25" BELOW TOP SURFACE ON AFT OTBD FACE. SPAR CAP REPAIRED IAW EA 8-5510-T0301356.

Part: FRAME — CORRODED (BS 1997) · airframe 72,502 hrs · 30,274 cycles

AFT WASTE TANK COMPARTMENT FRAME CORRODED AT BS 1997 FROM LONGERON 49L TO LONGERON 49R. REMOVED CORROSION IAW SRM 51-21-01 VOLII. REMOVED AND REPLACED EXISTING SPLICE IAW SRM 51-31-01 VOL II.

Part: ACTUATOR — BROKEN (CARGO DOOR) · airframe 72,502 hrs · 30,274 cycles

CENTER CARGO DOOR ACTUATOR IS BROKEN. REMOVED AND INSTALLED A SERVICABLE ACTUATOR IAW MM 52-32-01-2. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 1841-2007) · airframe 72,502 hrs · 30,274 cycles

CORROSION FOUND ON SEVERAL MAIN DECK FLOOR SUPPORTS OVER A WIDESPREAD AREA FROM BS 1841 TO 2007. REPLACED, CLEANED AND PRIMED IAW SRM 51-21-00 AND 51-21-00. SEAT TRACK REPLACED BS 1880, IAW SRM 53-70-00.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 71,116 hrs · 29,610 cycles

CNTR WW LT SIDEWALL HAS CRACK EXTENDING OUT OF PREVIOUS REPAIR STOP DRILL. 24 IN FWD OF STA 1521, ABD 4 IN. DOWN FROM UPPER BULCKHEAD. INSTALLED REPAIR REF W/C T8-5310-157353, SEQ 236.

Part: SKIN — CRACKED (ZONE 100) · airframe 71,116 hrs · 29,610 cycles

PACK SYS ACCESS DOOR FOR SYS 1, AFT TOP CORNER FOR CUT OUT AT APPROXIMATELY STATION 590 APPEARS TO BE CRACKED. REPAIRED NR 1 PACK DOOR CUTOUT UPPER AFT CORNER IAW SRM 53-50-00 FOR WORKSTEPS.

Part: SKIN — CRACKED (ZONE 100) · airframe 71,116 hrs · 29,610 cycles

PACK EXHAUST DOOR CUTOUT BELOW NR 2 AIR CONDITIONING BAY DOOR APPEARS TO HAVE A CRACK AT 1 OF THE UPPER AFT FASTENER HOLES. MWT. REPAIRED EXHAUST DOOR CUTOUT REF SRM 53-20-00, FIG 2.

Part: SHEAR TIE — CORRODED · airframe 69,784 hrs · 28,952 cycles

FWD CARGO DOOR SILL INSIDE LIGHTNING HOLE AFT OF THE AFT PWR ROLLER, HEAVY CORROSION EMITTING ON DAMAGED SHEAR CLIP AND LWR SIDE OF THE N/P STRAP. REPLACED CORRODED SHEAR CLIP IAW SRM 51-33-01.

Part: CONTROL HANDLE — STIFF (MLG) · airframe 69,299 hrs · 28,724 cycles

WHEN THE LANDING GEAR WAS SELECTED TO DOWN POSITION THE LDG GEAR HANDLE WAS DOWN AND IN GOT UNSAFE RED INDICATION ON ALL LDG GEAR INDICATORS FOR BOTH THE PRIMARY AND SECONDARY GEAR POSITION INDICATORS FOR A GOOD 10 SECONDS. AFTER CYCLING THE GEAR HANDLE IN AND OUT A COUPLE OF TIMES. FINALLY GOT DOWN AND LOCKED INDICATIONS. GEAR HANDLE FEELS A LITTLE STIFF. CLEANED THE LANDING GEAR CONTROL MECHANISM IAW MM 32-31-02-7. HANDLE NOW RETURNS TO THE FULLY RETRACTED POSITION WITH ALL GEAR INDICATIONS NORMAL. OK FOR SERVICE.

Part: MECHANISM — OUT OF RIG (MLG) · airframe 69,269 hrs · 28,709 cycles

ON FINAL APPROACH, AFTER PUTTING GEAR HANDLE DOWN AND WAITING TWICE THE NORMAL TIME FOR GREEN INDICATION, ALL 3 GEAR WERE STILL RED, HANDLE WAS CHECKED IN AND HYDRO QTY AND PRESSURE WERE BOTH GOOD. ELECTED TO CYCLE GEAR AFTER A LONG PAUSE AGAIN, THE GEAR FINALLY CAME DOWN. UNEVENTFUL LANDING. RIGGED LANDING GEAR CONTROL MECHANISM REF AMM 32-31-02-2 AND PERFORMED GEAR SWING REF AMM 32-30-00-5. GEAR HANDLE AND SWING OPS CHECK GOOD, NO FAULTS NOTED.

Part: LANDING GEAR — MALFUNCTIONED · airframe 68,437 hrs · 28,375 cycles

ON INITIAL GEAR EXTENSION ALL 3 WERE UNSAFE ON BOTH PRIMARY & SECONDARY INDICATORS WENT AROUND COMPLIED WITH QRH CYCLED GEAR UP THEN DOWN. GOT 3 GREEN. UNEVENTFUL LANDING. JACKED ACFT IAW MM 07-11-00-2 RETRACTED GEAR OPS CHECK GOOD. UPON EXTENDING LANDING GEAR GEAR HANDLE DID NOT SNAP BACK IN AFTER RELEASING IT WITH 3 UNSAFE GEAR INDICATIONS. TAPED GEAR HANDLE AND IT SNAPED IN WITH SAFE INDICATIONS IAW MM 32-31-02-7, CLEANED AND LUBED HANDLE. OPERATED LANDING GEAR DOOR HANDLE 3 MORE TIMES WITH NO FAULTS OR UNSAFE INDICATIONS. OPS CHECKS GOOD. ACFT OK FOR SERVICE

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE) · airframe 68,164 hrs · 28,261 cycles

GOT "LOW OIL QTY" LEVEL NR2 ENGINE FOLLOWED SOON AFTER QTY GOING TO "0". OIL PRESSURE DROPPED TO ABOUT 5 PSI. SHUTDOWN NR 2 ENGINE AND DIVERTED. REMOVED AND REPLACED NR 2 ENGINE IAW WORKCARD 71T1101 & 71T1701, OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: SWITCH — SPARKS (TAXI LIGHT) · airframe 68,025 hrs · 28,217 cycles

SPARKS FLEW OUT OF PANEL WHEN OPERATING TAXI LIGHT. R & R NOSE TAXI/LANDING LIGHT SWITCH S1-236 IAW MM 33-00-00-2. PERFORMED OPS CHECK OF NOSE TAXI/LANDING LIGHTS IAW MM 33-42-00-4. COMPLIED WITH PART 2 OF EA 8-3340-140173. NOSE TAXI/LANDING LIGHTS OPS CHECK SATISFACTORY. MEL CLEARED, PLACARD REMOVED. ACFT OK FOR SERVICE. COMPLY WITH EA 8-3340-140173 REV NO POS P2. REF WRI 33-40/6469 FOR REPLACEMENT OF SWITCH S1-236. COMPLIED WITH PART 2 OF EA 8-3340-140173. OPS CHECK SATISFACTORY IAW MM 33-42-00-4. ACFT OK FOR SERVICE.

Part: SWITCH — SPARKS (LANDING LIGHTS) · airframe 68,025 hrs · 28,217 cycles

WHILE TURNING ON LT AND RT LANDING LIGHTS AND NOSE LIGHT NOTICED SPARKS FROM LIGHT SWITCHES. UNABLE TO DETERMINE WHICH SWITCH ACTUALLY SPARKED. WHILE CHECKING PROBLEM, FOUND NOSE GEAR TAXI LIGHT TOGGLE LOOSE FROM SWITCH, BUT FOUND NOTHING ELSE OBVIOUS WRONG WITH SWITCHES. TRIED SEVERAL TIMES, BOTH INDIVIDUALLY AND TOGETHER, TO DUPLICATE PROBLEM BUT COULD NOT. ACFT OK TO CONTINUE SERVICE.

Part: WARNING LIGHT — ILLUMINATED (SLATS) · airframe 66,945 hrs · 27,760 cycles

SLAT DISAGREE LIGHT LEVEL 2 ON SHORT FINAL, 36R MEM NO CONTROL ISSUES, ACFT STABLE AND HAD BEEN CONFIGURED FOR LONG TIME ALREADY. PERFORMED GO AROUND, RAN QRH, RECONFIGURED, NO MORE LITES. UNEVENTFULL LANDING. PSEU HAD NO FAULTS STORED AND RTS OK. FCC'S HAD NO FAULTS PERTAINING TO THIS DISCREPANCY. CAPTAIN STATED IN TURN-OVER THAT THE FLAPS/SLATS WERE EXTENDED/CONFIGURED "FOR A LONG TIME ALREADY" AND THAT THE ALERT OCCURED "AT 500 FT". HOWEVER, C/W WITH MM 27-84-00-5, APPLICABLE PROCEDURES. OPS CHECKS NORMAL, NO HISTORY FOR 99 DAYS, OK TO CONTINUE.

Part: RIB — CRACKED (ZONE 600) · airframe 66,886 hrs · 27,723 cycles

RIGHT WING O/B AILERON LOWER SKIN FOUND EXISTING DOUBLER. REPAIRED AREA IAW SRM 57-00-01 FIG 10 SHT 1 VOL I

Part: LONGERON — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,886 hrs · 27,723 cycles

WING TO FUSELAGE FAIRING FOUND CORROSION WITH EXFOLIATION ON LONGERON. REPAIRED AREA IAW EA 8-5310-131034.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,886 hrs · 27,723 cycles

MAIN CARGO DOOR FOUND MODERATE CORROSION WITH EXFOLIATION ON DOOR SILL JAMB UNDER GUIDE FITTING. REPAIRED AREA IAW EA NR 8-5310-128551.

Part: SKIN — DENTED (ZONE 100) · airframe 66,886 hrs · 27,723 cycles

EXT FUSELAGE LWR SURFACE FOUND DENT ON SKIN 3 INCH BY 1.50 INCH. REPAIRED AREA IAW SRM 53-20-00, FIG 6, SHT 9 /10, VOL I.

Part: SKIN — CRACKED (ZONE 100) · airframe 66,886 hrs · 27,723 cycles

EXT FUSELAGE UNDER WING TO FUSELAGE FAIRING FOUND CRACK ON REPAIR DOUBLER RT SIDE. REPAIRED AREA IAW DWG SR10530073 AND EA NR 8-5310-35912.

Part: FITTING — CRACKED (LT WING TE FLAP) · airframe 66,886 hrs · 27,723 cycles

LT WING INB FLAP SUPPORT STRUCTURE FOUND FITTING P/N ANB7394-501 WITH CRACK AND FOUR ATTACHMENT HOLES (FOR ANB7118-501 FITTING ) WITH CORROSION ON BORES AND ON LUG FACES. REPAIRED AREA IAW EA NR 8-5340-128563.

Part: DOOR FRAME — CRACKED (ZONE 800) · airframe 66,886 hrs · 27,723 cycles

MAIN CABIN, FOUND CRACKS ON LWR AFT JAMB DOOR 3 LT. REPAIRED LWR DOOR JAMB IAW SRM 53-50-00 FIGURE 19 SHT 2 VOL I.

Part: DOOR FRAME — CRACKED (ZONE 800) · airframe 66,886 hrs · 27,723 cycles

MAIN CABIN, FOUND CRACK ON FWD UPPER JAMB DOOR 3 LT. REPAIRED UPPER DOOR JAMB WEB IAW SRM 53-50-00 FIGURE 19 SHT 1 VOL I.

Part: SUPPORT FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 66,886 hrs · 27,723 cycles

RT WING INBD FLAP SUPPORT STRUCTURE FOUND FITTING P/N ANB7394-502 WITH GOUGE AND 4 ATTACHMENT HOLES (FOR ANB7118-502 FITTING) WITH CORROSION ON BORES AND ON LUG FACES. REPAIRED AREA IAW EA 8-5340-128544.

Part: ATTACH FITTING — CRACKED (ZONE 500) · airframe 66,886 hrs · 27,723 cycles

LT UPPER BULKHEAD LUG CRACKED. REPAIRED AREA IAW SRM 57-20-00, FIG 38, STEP 1-6 AND 11/12, VOL I.

Part: SKIN — DELAMINATED (LT WING) · airframe 66,886 hrs · 27,723 cycles

LT WING INT T/E FOUND SKIN PANEL UNBONDED LWR SIDE. REPAIRED PANEL IAW SRM 51-71-00, CHAP 16, VOL II.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,886 hrs · 27,723 cycles

MAIN DECK FLOOR PANELS AND SEAT TRACKS 1 EA 1 INCH LONG MODERATE CORROSION LOWER CHANNEL. REPAIRED AREA IAW SRM 53-70-00, FIG 13, SHT 1, VOL I.

Part: SKIN — WORN (ZONE 600) · airframe 66,886 hrs · 27,723 cycles

RT WING SLATS DROOPED FOUND DEEP WEAR ON ANTIFRICTION AND EXT SKIN. REPAIRED AREA IAW SRM 57-10-00, FIG 15, SHT 1, VOL I.

Part: SKIN — CRACKED (ZONE 600) · airframe 66,886 hrs · 27,723 cycles

RT WING EXT SKIN L/E FOUND CRACK ON UPPER EXT SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00, FIG 68, SHT 2, VOL I.

Part: ANGLE — CRACKED (RT WING LE SLAT) · airframe 66,886 hrs · 27,723 cycles

RT WING SLATS DROOPED FOUND ANGLES WITH CRACK ON INT DROOPED. REPAIRED AREA IAW SRM 57-00-01, FIG 10, SHT 1, VOL I.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,886 hrs · 27,723 cycles

FWD CARGO COMP AREA INSP SEVERE CORROSION WITH EXFOLIATION ON BEAM. REPAIRED AREA IAW SRM 53-00-01, FIG 9, SHT 7, VOL I.

Part: SKIN — WORN (ZONE 600) · airframe 66,886 hrs · 27,723 cycles

RT WING L/E FOUND NR 2EA DEEP WEAR ON EXT SKIN .050 INCH BY .25 INCH DEEP .60 INCH. REPAIRED AREA IAW SRM 57-10-00, FIG 39 AND 15, VOL I.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,886 hrs · 27,723 cycles

FWD CARGO COMPT AREA INP SEVERE CORROSION ON BEAM LOWER PANEL FLOOR. REPAIRED BEAM IAW SRM 53-00-01, FIG 9, SHT 8, VOL I AND SRM 53-70-00, FIG 18, VOL I.

Part: SKIN — CRACKED (ZONE 600) · airframe 66,886 hrs · 27,723 cycles

RT WING L/E FOUND CRACK ON LOWER EXT SKIN. REPAIRED AREA IAW SRM 57-10-00, FIG 68, SHT 2, VOL I.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,886 hrs · 27,723 cycles

FWD CARGO COMPT AREA INSP MODERATE CORROSION CAP ANGLE. REPAIRED AREA IAW SRM 53-30-00, FIG 8 AND 5, VOL I.

Part: RIB — CRACKED (ZONE 600) · airframe 66,886 hrs · 27,723 cycles

RT WING L/E FOUND CRACK ON INT RIB LOWER SIDE L/E. REPAIRED AREA IAW SRM 57-00-01, FIG 10, SHT 1, VOL I.

Part: RIB — CRACKED (ZONE 600) · airframe 66,886 hrs · 27,723 cycles

RT WING L/E FOUND CRACK ON RIB LOWER INT L/E. REPAIRED AREA IAW SRM 57-00-01, FIG 10, SHT 1, VOL I.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 66,886 hrs · 27,723 cycles

EXTERNAL FUSELAGE EXISTING DOUBLER ON SKIN. REPAIRED SKIN IAW SRM 53-20-00, FIG 6, SHT 7 AND 8, VOL I.

Part: SKIN — UNKNOWN (ZONE 500) · airframe 66,886 hrs · 27,723 cycles

LT WING INBD FLAP UPPER SKIN FOUND EXISTING FLUSH DOUBLER. REPAIRED AREA IAW SRM 57-10-00, FIG 85, VOL I.

Part: SKIN — UNKNOWN (ZONE 300) · airframe 66,886 hrs · 27,723 cycles

HORIZ STAB RT INBD ELEVATOR UPPER SKIN FOUND EXISTING DOUBLER. REPAIRED AREA IAW SRM 55-10-00, FIG 8, VOL I.

Part: SKIN — UNKNOWN (ZONE 300) · airframe 66,886 hrs · 27,723 cycles

HORIZ STAB RT INBD ELEVATOR UPPER SKIN FOUND, EXISTING DOUBLER. REPAIRED AREA IAW SRM 55-10-00, FIG 8, VOL I.

Part: SKIN — UNKNOWN (ZONE 300) · airframe 66,886 hrs · 27,723 cycles

HORIZ STAB RT INBD ELEVATOR UPPER SKIN FOUND, EXISTING DOUBLER. REPAIRED AREA IAW SRM 55-10-00, FIG 8, VOL I.

Part: SKIN — UNKNOWN (LT WING TE FLAP) · airframe 66,886 hrs · 27,723 cycles

LT WING INBD FLAP UPPER SKIN FOUND EXISTING DOUBLER. REPAIRED AREA IAW SRM 57-00-01, FIG 86, VOL I AND EA NR 8-5750-128552.

Part: SKIN — UNKNOWN (ZONE 100) · airframe 66,886 hrs · 27,723 cycles

EXTERNAL FUSELAGE SKIN EXISTING FLUSH DOUBLER. REPAIRED AREA IAW SRM 53-20-00, FIG 6, SHT 7 AND 8, VOL I.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,886 hrs · 27,723 cycles

MAIN DECK BALLMATS SEAT TRACK FOUND CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00, FIG 1, VOL I.

Part: SKIN — DENTED (ZONE 800) · airframe 66,886 hrs · 27,723 cycles

AFT CARGO COMPT DOOR FOUND DENT 2 INCH BY 3 INCH DEPTH .14 INCH ON EXTERNAL SKIN. REPAIRED AREA IAW SRM 52-10-00, FIG 17, VOL I.

Part: SKIN — CRACKED (LT WING) · airframe 66,886 hrs · 27,723 cycles

LT WING OTBD FLAP INBD HINGE (ONBOARD) FOUND CRACK ON SKIN (REMOVED PART). REPAIRED AREA IAW SRM 57-00-01, FIG 4, SHT 2, VOL I.

Part: SKIN — CRACKED (ZONE 500) · airframe 66,886 hrs · 27,723 cycles

LT WING OTBD FLAP OTBD HINGE FOUND CRACK ON SKIN. REMOVED PART.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 66,886 hrs · 27,723 cycles

LT WING INBD FLAP LWR SKIN BROKEN. REPAIRED AREA IAW SRM 57-00-01, FIG 4, SHT 2, VOL I.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,886 hrs · 27,723 cycles

FWD CARGO COMPT AREA DURING INSP FOUND SEVERE CORROSION WITH EXFOLIATION ON CHANNEL. REPAIRED CHANNEL IAW SRM 53-70-00, FIG 7, SHT 2, VOL I.

Part: FRAME — CRACKED (ZONE 100) · airframe 66,886 hrs · 27,723 cycles

FWD AVIONIC COMPT INSP FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00, FIG 11, VOL I.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 66,886 hrs · 27,723 cycles

MAIN DECK FLOOR PANELS AND SEAT TRACKS SEVERE CORROSION ON SEAT TRACK AND SPLICES. REPAIRED SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL I.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 66,886 hrs · 27,723 cycles

MAIN CABIN CRACK ON FWD UPPER WEB JAMB DOOR NR 3 RT. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHEET VOL I.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 66,886 hrs · 27,723 cycles

MAIN CABIN CRACKS ON LOWER AFT JAMB DOOR WEB NR 3 RT. REPAIRED AREA IAW SRM 53-50-00, FIG 19, SHT 2, VOL I.

Part: BEAM — CRACKED (ZONE 100) · airframe 66,886 hrs · 27,723 cycles

FWD CARGO COMPT AREA INSPECTION FOUND CRACK ON BEAM. REPAIRED BEAM IAW SRM 53-60-01, FIG 3, VOL I.

Part: FITTING — CRACKED (ZONE 600) · airframe 66,886 hrs · 27,723 cycles

FITTING CRACKED. REPAIRED AREA IAW SRM 57-00-01, FIG 11, VOL I.

Part: FITTING — CRACKED (ZONE 100) · airframe 66,886 hrs · 27,723 cycles

CAC CRACK ON FITTING FRAME. REPAIRED AREA IAW SRM 53-30-00, FIG 7, VOL I.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 66,886 hrs · 27,723 cycles

MAIN DECK FLOOR PANELS AND SEAT TRACKS FOUND CORROSION WITH EXFOLIATION ON TRACK. REPAIRED AREA IAW SRM 53-70-00, FIG 1, SHT 1 AND 2, VOL I.

Part: SKIN — CHAFED (ZONE 200) · airframe 65,076 hrs · 26,703 cycles

LT FUSELAGE EXTERNAL SKIN CHAFED JUST FORWARD OF MAIN CARGO DOOR CUT-OUT UPPER AREA. AREA IS CHAFED BY TAB ATTACHMENT TO UPPER DOOR CORNER. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 FIG 1A VOL I, 53-32-01 FIG 2 VOL III AND EA 8-5330-109167-FUSELAGE SKIN CHAFED AT STA 620 ABOVE 12LREPAIR. ORIGINAL THICKNESS .068, MATERIAL REMOVED .022, REMAINIG THICKNESS .046.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

FS 1184 RBL 107.50 NR 10 SEAT TRACK CORRODED AROUND FASTENER HOLES (LOWER SIDE). REMOVED, FABRICATED AND INSTALLED SEAT TRACK SPLICE IAW DC10 SRM VOLUME I 53-70-00 FIG 1.

Part: SPAR CAP — CORRODED (ZONE 600) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

RT WING HAS CORROSION ON AFT UPPER SPAR CAP STA.XORS 718 TO733. REMOVED CORROSION IAW DC/MD SRM 51-21-01 VOLII AND FEDEX EA 8-5710-109151, WINGS, RT WING SPAR CORROSION BETWEEN STA XORS 480-733. REPAIR, ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOLII.

Part: LATCH — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

NR 5 MAIN CARGO DOOR LATCH SPOOL BOLT HOLES HAVE CORROSION. REAMED HOLES TO .520 WITH NO FURTHER EVIDENCE OF CORROSION. REPAIRED IN REF TODC/MD10 SRM 53-50-00 VOLI PAGE 81.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

IN THE AFT PIT, THE SEAT TRACKS AT ABOUT BS 1787 TO BS 1981, RBL 20R AND LBL 20L BS 1841 LBL 59L HAVE DEBRIS, LIGHT CORROSION AND MINOR SCRATCHES. REMOVED, FABRICATED, AND INSTALLED TRACKS IAW DC/MD10 SRM 53-70-00 VOL I FIG 1 SHT 1- 4, AND DAC DRAWING AGA 3855 REV.N.

Part: LATCH — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

NR 4 MAIN CARGO DOOR LATCH SPOOL BOLT HOLES HAVE CORROSION. REAMED ALL 4 BOLT HOLES AT NR 4 LATCH SPOOL LOCATION TO .460 IAW DC10 SRM 53-50-00 FIG 17 VOLI. NO FURTHER EVIDENCE OF CORROSION REMAINS.

Part: SKIN — CORRODED (RT WING TE) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

RIGHT WING TRAILING EDGE UPPER SURFACE CLOSE OUT PANEL IS BULGED AT SEVERAL LOCATIONS BETWEEN NR 2 AND NR 5 SPOILER AREA. REMOVED CORROSION IAW DC/MD10 SRM 51-21-01 VOLII AND FEDEX EA 8-5710-109151 WINGS, RT WING SPAR CORROSION BETWEEN STA XORS 480-733-REPAIR, ALODINED AND PRIMED IAW DC/MD10 SRM 51-21-01 VOLII.

Part: SPOOL — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

NR 1 MAIN CARGO DOOR LATCH SPOOL BOLT HOLES HAVE CORROSION. REAMED ALL 4 BOLT HOLES NR 2 LATCH SPOOL BOLT HOLES IAW DC10 SRM 53-50-00 FIG 17 VOLI TO .460. NO FURTHER EVIDENCE OF CORROSION REMAINS.

Part: SPAR CAP — CORRODED (RT WING) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

RIGHT WING HAS CORROSION ON AFT UPPER SPAR CAP AT XORS=718 TO XORS=733 ENTERED IN ERROR, SEE SDR NR 07-1838 N/R N00804 FOR CORRECTIVE ACTION.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

RIGHT WING T/EDGE UPPER SURFACE CLOSE-OUT PANEL IS BULGED AT SEVERAL LOCATIONS, BETWEEN NR 2 AND NR 5 SPOILER AREA.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

AFT CARGO COMPARTMENT AT STA 1942 FROM L51L TO L51R FRAME HAS CORROSION. REMOVED AND REPLACED STIFFENERS IAW DC/MD10 SRM 51-31-01 AND 51-33-01. AFTER CORROSION REMOVAL. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC/MD10 SRM 53-30-00 FIG 8 VOL I.

Part: SPAR CAP — CORRODED (ZONE 500) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

LEFT WING UPPER REAR SPAR CAP HAS CORROSION ON AFT UPPER SURFACE AT XORS 480-490. [SUP 05-16-07] REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW FEDEX E.A. 8-57-109150 STEP 2 (LT WING CORROSION BETWEEN XORS=480-800)ALODINED AND PRIMED DC10 SRM 51-21-01 VOL II. MINOR REPAIR.

Part: SEAT TRACK — CORRODED (BS 705-745) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

CABIN SEAT TRACK HOLE AREAS AT LBL 76 FS 675-735 HAVE CORROSION REMOVED CORROSION IAW DC10-SRM VOL II 51-21-01 PG 28 ORIG THICKNESS .080 REMOVED .039 FOUND TO BE OUT OF LIMITS IAW DC10 SRM VOL I 53-70-00 FIG 5. REMOVED AND REPLACED SEAT TRACK IAW DC10 SRM 53-70-00 VOL I FIG 1 SHT 2.

Part: SEAT TRACK — WORN (BS 1248-1351) · airframe 65,076 hrs · 26,703 cycles

MAIN DECK SEAT TRACK SCALLOP WORN STA 1300 RBL 27 BLENDED AND FOUND TO BE OUT OF LIMITS PER MD10/DC10 SRM 53-70-00 VOL I PG 21. REMOVED SEAT TRACK SECTION RBL 27 STA 1248 TO STA 1351 PER MD10/DC10 SRM 53-70-00 VOL I PG 21. SEAT TRACK MATERIAL IS 4929150 PER MD/DC10 SRM 53-42-01 PG 13 FIG 5 VOL III. SCALLOPED SEAT TRACK PER DC10 SRM 53-70-00 VOL I MATERIAL ID FOR SPLICE HAT 4932154-1200 PO NR 570758-3 AND SPLICE PLATE 7075-T6 .050" PO NR 57122.5 PER MD 10 DC10 SRM 53-70-00 FIG I VOL I. FABRICATED SEAT TRACK, SPLICE PLATE AND SPLICE HAT PER MD10/DC10 SRM 53-70-00 VOL I. ALODINED AND PRIMED SEAT TRACK, SPLICE PLATE SPLICE HAT PER MD/DC10 SRM 51-21-01 PG 1 VOL I.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 65,076 hrs · 26,703 cycles

FOUND MAIN DECK LEFT SIDE SEAT TRACK SCALLOP WORN AT STA 1265 LBL 8. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK SECTION IAW DC/MD10 SRM 53-70-00 VOL I FIG 5 SHT 1 AND 53-42-01 VOL III PAGE 5.

Part: SPAR CAP — CORRODED (ZONE 500) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

LEFT WING REAR SPAR CAP HAS CORROSION MIGRATING UNDER WING SKIN AT ST XORS 600-606. [SUP 05-16-07] REMOVED CORROSION IAW DC10 SRM 51-21-01 VOLII ,ORIG THICKNESS .300 REMAINING .290 FOUND TO BE WITHIN LIMITS IAW 57-20-00 VOLII.REMOVED AND REPLACED FASTENERS,ALODINED AND PRIMED IAW DC10 SRM 51-33-01 VOL II,51-21-01. MINOR REPAIR.

Part: SEAT TRACK — GOUGED (BS 908-1005) · airframe 65,076 hrs · 26,703 cycles

MAIN DECK LT SIDE SEAT TRACK HAS GOUGE AT STA 943 LBL 27 REMOVED CORROSION IN REF TO DC10/MD10 SRM 51-21-01 VOL II, FOUND TO BE OUT OF LIMITS IAW DC10/MD10 SRM 53-70-00 VOL 1 FIG 5. REMOVED SEAT TRACK AND SPLICE IAW DC10/ MD 10 SRM 51-31-01 VOL II PG 1 MAT ID FOR SEAT TRACK S4929147, PO NR 571386.1 MAT ID FOR SPLICE IS 4932154, MAT ID FOR PLATE IS .050" 7075-T6. SCALLOPED SEAT TRACK IAW DC10/MD 10 SRM 53-70-00 VOL I. FABRICATED SPLICE AND SPLICE PLATE IAW DC10/MD 10 SRM 53-70-00 VOL I PGS 3-6A. FABRICATED SEAT TRACK IAW DC10/MD10 SRM 53- 70-00 VOL I PG 22. ALODINED AND PRIMED SEAT TRACK AND SPLICE AND SPLICE PLATE IN REF TO DC10/ MD10 SRM 51-21-01 VOL II PGS 24 AND 21.

Part: SEAT TRACK — CRACKED (BS 1129) · airframe 65,076 hrs · 26,703 cycles

MAIN DECK LT SIDE SEAT TRACK IS CRACKED AT STA 1220 LBL 27 REMOVED SEAT TRACK FROM STA 1129 /1229 LBL 27 IAW DC10-SRM 51-31-01 VOL II MAT ID FOR SEAT TRACK 4929147 IAW DC10 SRM 53-42-01 VOL III PAGE 7 MATERIAL ID FOR SPLICE HAT AND SPLICE PLATE 4932154 AND 7075 T6 .050 IAW DC10 SRM 53-70-00 PAGE 5 VOL I. FABRICATED, DRILLED AND COUNTERSUNK NEW SEAT TRACK SECTION AND SPLICED REPAIR IAW DC10-SRM 53-70-00 FIG 5 VOL I. ALODINED AND PRIMED IAW DC-10 SRM 51-21-01 PAGE 1. INSTALLED SEAT TRACK AND SPLICES REPAIR IAW DC10 SRM 51-31-01 VOL II PAGE 1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 65,076 hrs · 26,703 cycles

MAIN DECK LEFT SIDE SEAT TRACK SCALLOP WORN AT STA 1139 LBL8. REMOVED, FABRICATED AND INSTALLED SEAT TRACK SECTION IAW DC/MD10 SRM 53-70-00 VOL I FIG1 SHT 1, 53-70-00 VOL 1 FIG 5 SHT 1 AND 51-21-01 VOL II PAGE 21, 25.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 65,076 hrs · 26,703 cycles

FOUND MAIN DECK SEAT TRACK SCALLOP WORN STA 1777 RBL 27. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK SECTION DC/MD10 SRM 53-42-01 VOL III FIG 5 AND 53-70-00 VOL I FIG 1 SHT 1 AND 51-21-01 VOL II PAGE 21, 25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

MAIN DECK LT SIDE SEAT TRACK HAS CORROSION AT STA 935 LBL 27. WORK ACCOMPLISHED IN CONJUNCTION WITH NON ROUTINE. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW DC10-MD10 SRM 53-70-00 VOL I FIG 5 FROM STA 905 TO STA 1005. CLASSIFIED AS MAJOR, REPLACED SEAT TRACK AT LBL 27 STA 905 TO STA 1005 DC10/MD10 SRM 51-31-01 VOL II ALL SIGN OFFS ACCOMPLISHED ON NON ROUTINE DUE TO ANOTHER WRITE UP IN SAME TRACK.

Part: SPAR CAP — CORRODED (ZONE 500) · airframe 65,076 hrs · 26,703 cycles

LEFT WING UPPER SPAR CAP HAS CORROSION MIGRATING UNDER SKIN PLATE AT XORS 645-671. [SUP 05-16-07] REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW FEDEX E.A 8-5710-109150 STEP 3 (LT WING CORROSION BETWEEN XORS=412-800- REPAIR). ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II. MINOR REPAIR.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 65,076 hrs · 26,703 cycles

MAIN DECK SEAT TRACK SCALLOP WORN STA 1356 RBL47 REMOVED, FABRICATED AND INSTALLED SEAT TRACK SPLICE PLATE AND HAT SECTION IAW DC/MD10 SRM 51-33-01 VOL II PAGE 1-30 AND 53-70-00 VOL I PAGE 3-6.

Part: SEAT TRACK — WORN (BS 1551-1671) · airframe 65,076 hrs · 26,703 cycles

MAIN DECK SEAT TRACK SCALLOP WORN STA 1621 RBL 47 REMOVED FLOOR BOARDS FROM STA 1561-1741. BROKEN SCALLOP FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-70-00 VOL I FIG 5. REMOVED SEAT TRACK FROM STA 1551-1671 RBL 47 IN REF WITH DC10 SRM 53-70-00, VOL I FIG 1. FABRICATED SEAT TRACK AND SPLICE PLATE IAW DC10 SRM 53-70-00 VOL I. ALODINED AND PRIMED IAW 51-21-01 SRM DC-10 PG 1-30 VOL II. INSTALLED SEAT TRACK AND SPLICE IAW DC10 SRM 51-35-01 PG 1 VOL II. INSTALLED FLOORBOARD IAW AMM 53-21-08-2 DC10-10 PG 1-4 (FIG 201 SHEET 1). INSTALLED RBL 47 SEAT TRACK AT STA 1551-1676 INSTALLED FLOOR BOARD AT STA 1561-1741.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

FOUND CORROSION ON SEAT TRACK FROM STA 695 TO 735 LBL28. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK SECTION IAW DC/MD10 SRM 53-70-00 VOL I FIG 1 SHT 1 AND 53-70-00 VOL1 FIG 5 SHT 2 AND 51-21-01 VOL II.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

MAIN DECK LT SIDE SEAT TRACK HAS CORROSION AT STA 1204 LBL 27. BLENDED AREA AND FOUND OUT OF LIMITS IAW DC10 SRM 53-70-00 FIG 5 VOL I. REMOVED SEAT TRACK FROM STA 1049/1129 LBL 27 IAW DC10 SRM 53-70-00 FIG I VOL III, MAT ID FOR SEAT TRACK 4929147 IAW DC10 SRM 53-42-01 VOL III PAGE 7. FABRICATED DRILLED AND COUNTERSUNK SEAT TRACK AND SPLICES HAT AND PLATE IAW SRM 53-70-00 FIG 5 VOL I. ALODINED AND PRIMED IAW DC10 SRM 51-21-01 VOL II PAGES 1-2. INSTALLED SEAT TRACK AND SPLICES REPAIR IAW DC10 SRM 51-31-01 VOL II PAGE 2 CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

FOUND CORROSION ON SEAT TRACK AT STA 605 LBL 28. REMOVED, FABRICATED AND INSTALLED SEAT TRACK SECTION IAW DC/MD10 SRM 53-70-00 VOL I FIG 1 SHT 1 AND 53-70-00 VOL I FIG 5, SHT 2 AND 51-21-01 VOL II PAGE 21.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 65,076 hrs · 26,703 cycles

MAIN DECK SEAT TRACK HAS GOUGE AND WORN AT STA 1016 LBL 8. REMOVED, FABRICATED, INSTALLED SEAT TRACK SECTION IAW DC/MD10 SRM 53-70-00 VOL I FIG 5 SHT 5, 53-70-00 VOL I FIG 1 PAGE 3-6A. MAJOR REPAIR.

Part: TEE FITTING — CORRODED (ZONE 200) · airframe 65,076 hrs · 26,703 cycles

AFT PRESSURE BULKHEAD TEE FITTING CORRODED AT STA 2007 BL 0. REMOVED DAMAGE AND REPAIRED TEE FITTING IAW MD/DC10 SRM 53-40-00 VOL I FIG 16 PAGE 93.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 65,076 hrs · 26,703 cycles

MAIN DECK SEAT TRACK SCALLOP WORN STA 1490 RBL 47. REMOVED, FABRICATED, INSTALLED SEAT TRACK SECTION IAW DC/MD10 SRM 53-70-00 VOL I PAGE 22 AND 53-42-01 VOL III, MAJOR REPAIR.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 65,076 hrs · 26,703 cycles

MAIN DECK LEFT SIDE SEAT TRACK WORN AT STA 1119 LBL 47. REMOVED,FABRICATED, INSTALLED SEAT SECTION IAW DC/MD10 SRM 53-70-00 VOL I PAGE FIG1 SHEET 1 AND 51-21-01 VOL II PAGE 21, 25.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 65,076 hrs · 26,703 cycles

MAIN DECK LEFT SIDE SEAT TRACK WORN AT STA 1089 LBL 47. REMOVED, FABRICATED, INSTALLED SEAT TRACK SECTION IAW DC/MD10 SRM 53-70-00 VOL I FIG 5 SHT 1 AND 2,51-21-01 VOL II PAGE 21 AND 25.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 65,076 hrs · 26,703 cycles

MAIN CARGO DOOR LOWER SILL NR 6 SPOOL LATCH BACKUP FITTING IS CRACKED. [SUP 05-18-07] REMOVED AND REPLACED NR 6 SPOOL LATCH BACKUP FITTING IAW DC/MD10 SRM 51-33- 01,PAGE 1 VOLII AND EA 8-5230-110682. MINOR REPAIR.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 65,076 hrs · 26,703 cycles

MAIN CARGO DOOR-LOWER SILL- NR 2 SPOOL LATCH-BACKUP FITTING- IS CRACKED. [SUP 05-18-07] REMOVED AND REPLACED NR 2 SPOOL LATCH BACKUP FITTING IAW DC/MD10 SRM 51-33-01. VOLII PAGE1 AND EA 8-5230-110682[FUSELAGE-MAIN CARGO DOOR LOWER JAMB FITTING INSPECTION AND DOOR RIG. MINOR REPAIR

Part: FITTING — CRACKED (CARGO DOOR) · airframe 65,076 hrs · 26,703 cycles

MAIN CARGO DOOR LOWER SILL NR 7 SPOOL LATCH BACKUP FITTING IS CRACKED. [SUP 05-21-07] REMOVED AND REPLACED NR 7 SPOOL LATCH BACKUP FITTING IAW DC/MD10 SRM 51-33-01 PG1 VOL II AND EA 8-5230-110682, DAC DRAWING AFA 2132 REV B. MINOR REPAIR

Part: FITTING — CRACKED (CARGO DOOR) · airframe 65,076 hrs · 26,703 cycles

MAIN CARGO DOOR-LOWER SILL-33 SPOOL LATCH-BACKUP FITTING IS CRACKED. [SUP 05-18-07] REMOVED AND REPAIRED NR 3 SPOOL BACKUP FITTING IAW DC/MD10 SRM 51-33-01 AND EA 8-5230-110682. MINOR REPAIR

Part: SEAT TRACK — WORN (ZONE 200) · airframe 65,076 hrs · 26,703 cycles

MAIN DECK LEFT SIDE SEAT TRACK SCALLOP WORN AT STA1385 LBL 27. FABRICATED, ALODINED, PRIMED AND INSTALLED SEAT TRACK SECTION IN REF TO DC10 SRM 53-70-01 VOL 1,51-21-01 VOL.II AND 51-31-01 VOL II.

Part: SEAT TRACK — CRACKED (BS 1501) · airframe 65,076 hrs · 26,703 cycles

FOUND MAIN DECK SEAT TRACK CRACKED STA 1501 RBL8. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED SEAT TRACK SPLICE PLATE AND SPLICE HAT IAW DC/MD 10 SRM 51-21-01 VOL I, PAGE 1-30. FOR FINAL INSTALLATION OF SEAT TRACK SEE N/R N00567.

Part: SEAT TRACK — CRACKED (BS 1581) · airframe 65,076 hrs · 26,703 cycles

FOUND MAIN DECK SEAT TRACK CRACKED STA 1581 RBL8. REMOVED AND REPLACED SEAT TRACK SECTION IAW STA 1501-1581 IAW DC/MD 10 SRM 53-70- 00 VOL I AND 51-31-01 VOL.II PAGE 1-30. SEE N/R NOO567-SDR NR 07-1694.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

LT HORIZONTAL STAB EXTERNAL SKIN HAS CORROSION ON UPPER SURFACE AT REAR SPAR XE 48.5. ALL WORK ACCOMPLISHED ON FEDEX EA.8-5500-110623-STAB, LT SIDE-UPPER AFT SPAR.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

RIGHT WING UPPER SURFACE HAS CORROSION JUST O/B OF TRUNNION DOUBLER. [SUP 05-21-07] REMOVED COROSION FROM WING SKIN,ORIG THICKNESS .495,AMOUNT REMAINING.476,MATERIAL LOSS .019 FOUND TO BE WITHIN LIMITS IAW DC/MD SRM 57-10-00 FIG.61 VOL I,51-20-00 FIG2 VOL III AND EA 8-5710-109149. ALODINED,PRIMED, APPLIED TOPCOAT IAW DC/MD 51-21-01 VOL II. MINOR REPAIR

Part: FLOORBEAM — CORRODED (BS 735) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

FLOOR STRUCTURE CORROSION AROUND CLIP NUT ATTACHMENT STA 735 RBL 58-72. REMOVED AND REPLACED SUPPORT AEAO397-503 IN REFERENCE TO MD/DC SRM 51-35-01 VOL II PG 1. REPAIR CLASSIFIED AS MAJOR.

Part: FLOOR SUPPORT — CORRODED (ZONE 900) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

FS 1219 BL 94 RT FLOORBOARD ATTACH ANGLE CORRODED AROUND FASTENER HOLE. REMOVED AND REPLACED SUPPORT AEA0397-533 IN REFERENCE TO MD/DC 10 SRM 51-33-01 VOLII PG.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

LEFT WING TRAILING EDGE UPPER SURFACE AT STA XORS 405-415 CLOSEOUT STRAP AND REAR SPAR ARE CORRODED. . [SUP 05-06-07] REMOVED AND REPLACED CLOSE-OUT STRAP IAW DAC DRAWING ARC0771,DC10 SRM 51-31-01 VOL II AND 51-33-01 VOL II.REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL II FOUND TO BE WITHIN LIMITS IAW FEDEX EA 8-5710-109150.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 65,076 hrs · 26,703 cycles

LEFT WING TRAILING EDGE UPPER SURFACE CLOSEOUT PANEL IS BULGED AT THE NR 3 SPOILER AREA. INSTALLED L/W T/EDGE PANELS BETWEEN NR 2 AND 5 SPOILERS. CORROSION REMOVAL TO BE ACCOMPLISHED ON FEDEX N/R N000828-SDR 07-1740.

Part: STIFFENER — CRACKED (ZONE 400) · airframe 63,887 hrs · 26,068 cycles

FOUND VERTICAL STIFFENER (P/N AUB 7358-1) ON NR 3 PYLON AT LT T/R, CENTER HINGE CRACKED.

Part: HINGE FITTING — CRACKED (THRUST REVERSER) · airframe 62,707 hrs · 25,465 cycles

NR 3 LT THRUST REVERSER CENTER HINGE SUPPORT EXTRUSION ON INSIDE OF PYLON IS CRACKED AT TOP.**S/D COMING**

Part: ANGLE — CRACKED (THRUST REVERSER) · airframe 62,707 hrs · 25,465 cycles

NR 3 ENGINE LT THRUST REVERSER CENTER HINGE SUPPORT EXTRUSION INSIDE PYLON IS CRACKED AT TOP REF: SNRM 798. REMOVED CRACKED HINGE SUPPORT. INSTALLED HINGE SUPPORT EXTRUSION AS REQ., REF SRM 51-31-01 (REF N/R N00798).

Part: INSULATION — BURNED (FUSELAGE) · airframe 62,707 hrs · 25,465 cycles

CAC, FUSELAGE INSULATION BLANKETS SEVERLY BURNED AROUND SYS 1-2 AND SYS 1-3, PNEUMATIC AIR DUCT. CHECKED PNEUMATIC SYSTEMS PER JRH AND LEAK CHECKED,OP'S AND LEAK CHECHED OK.FOUND INSULTION BLANKETS SECURED & TOUCHING DUCT. NEW INSULTATION BLANKETS INSTALLED IAW MM 25-28-00.

Part: SENSOR — MALFUNCTIONED (NR 2 AOA) · airframe 62,549 hrs · 25,384 cycles

AFTER T/O WHEN WE WERE RETRACTING SLATS WE GOT THE STICK SHAKER STALL WARNING & FLASHING SLAT RESET LIGHT. RETURNED TO SLATS EXTEND THE WARNING STOPPED HAD TO FLY WITH SLATS EXTENDED AND RETURNED TO IND, NORMAL CONFIGURATION LANDING. PERFORMED AT/SC TEST FOUND AT/SC BAD & AOAS VANE BAD. CHANGED NR 2 AOA SENSOR.

Part: PANEL — CRACKED (CARGO BAY) · airframe 61,934 hrs · 25,071 cycles

COMPLY WITH EA8-2550-55440, EQUIP/FURNISHINGS LWR CARGO, REPAIR OF STA 1841 CENTER/AFT PARTITION. COMPLIED WITH EA8-2550-55440.

Part: FITTING — CORRODED (TE FLAPS) · airframe 60,249 hrs · 24,302 cycles

RIGHT WING OUTBOARD FLAP, SUPPORT FITTING HOUSING FOR NR 3 VANE TRACK SUPPORT FITTING HAS CORRODED FASTENERS ON SIDES.

Part: SUPPORT — MISSING (NR 2 NACELLE) · airframe 60,249 hrs · 24,302 cycles

NR 2 ENG CORE COWL FWD LT AND RT HINGE LINK/ROD SUPPORT FOUND MISSING. ALSO FOUND CRACKS AT LT AND RT VERTICAL STIFFENERS AT HINGE FITTING CUTOUTS FOR LINK ATTACHMENT. REPLACED LINK ASSY AND WELDED CRACKS. SUSPECT CRACKS CAUSED DUE TO MISSING ROD.

Part: SKIN — CORRODED (TE FLAP) · airframe 60,249 hrs · 24,302 cycles

RT WING OUTBOARD FLAP, NR 4 FLAP VANE ATTACH HORN HAS 2 CORRODED AREAS AROUND HOLES. REPLACED NR 4 FLAP VANE ATTACH HORN PER M/M 27/50/03/2 AND TORQUED BOLTS PER M/M 20/50/20.

Part: SKIN — CORRODED (TE FLAP) · airframe 60,249 hrs · 24,302 cycles

RIGHT WING OUTBOARD, D-FLAP, NR 5 FLAP VANE ATTACH HORN HAS TWO CORRODED / PITTED HOLES. REPLACED NR 5 FLAP VANE HORN PER M/M 27/50/03/2 AND TORQUED PER 20/50/02.

Part: SKIN — CORRODED (TE FLAP) · airframe 60,249 hrs · 24,302 cycles

RIGHT WING OUTBOARD FLAP VANE, NR 3 FLAP VANE ATTACH HORN HAS TWO CORRODED/PITTED HOLES. REPLACED PER M/M 27-50-03-2 AND TORQUED PER M/M 20-50-20.

Part: SKIN — CORRODED (TE FLAP) · airframe 60,249 hrs · 24,302 cycles

RIGHT WING OUTBOARD FLAP VANE NR 2 FLAP VANE ATTACH HORN HAS 2 CORRODED/PITTED HOLES. REPAIRED PER EA 8-5750-68462.

Part: HORN — CORRODED (TE FLAP) · airframe 60,249 hrs · 24,302 cycles

RIGHT WING OUTBOARD FLAP VANE NR 1 FLAP VANE ATTACH HORN HAS PITTED AFT HOLE.

Part: TRANSDUCER — OUT OF ADJUST (AUTOPILOT SYS) · airframe 59,786 hrs · 24,081 cycles

AIRCRAFT RESPONDED AS IN PREVIOUS WRITE-UPS AT LEVEL OFF FL330, PORPOISING /- 500 IN ALT HOLD, SAME RESULT AP 1 OR 2. DISCONNECTED THE AP AND SLOWED 20 KNOTS, AIRPLANE WAS DIFFICULT TO CONTROL, VSI /- 1000 FPM AND ALTITUDE /- 200 FT. DESCENDED TO FL 290, NO IMPROVEMENT. DIVERTED TO SLC. WHEN HYD PRESSURE APPLIED CHECKED ELEVATORS FOR MOVEMENT BY PHYSICALLY TRYING TO MOVE ELEVATOR SURFACES. NO MOVEMENT WAS NOTICED. CHECKED AUTO PITCH TRIM LVDT NULLS. FOUND CHANNEL A NULL TO BE 574 MVAC, JAM NUT WAS LOOSE ON THE LVDT. FOUND CHANNEL-B NULL TO BE 175 MVAC. ADJUSTED AUTO PITCH TRIM LVDT'S NULL. OPS CHECKED AUTO PITCH TRIM SYSTEM PER MM 22-22-00-5, SYSTEM TESTED NORMAL.

Part: SPAR — CRACKED (HORIZ STAB)

REF EO 8-5510-7-3312 PT 4, RT HORIZ STAB, FWD SPAR, UPPER CHORD, FWD TANG CRACKED AT 2ND HOLE I/B OF CLOSING RIB PLANE. CRACK MOVES AFT FROM HOLE .375 INCH. TRIMMED OUT CRACKED AREA PER SRM 55-20-00, FABRICATED DOUBLER, FILLER, SHIM PER SRM 55-20-00. INSTALLED DOUBLER PER SRM 55-20-00.

Part: SKIN — CRACKED (HORIZ STAB)

HORIZONTAL STAB HAS ONE CRACK .948 INCH LONG IN THE AFT UPPER CONSTANT SECTION PANEL. CRACK STARTS AT AFT BOLT HOLE GOING FWD AND CRACK IS WITHIN FLYABLE LIMITS. REPETITIVE INSP PART 1 AT 24 MONTHS INTERVALS AND SPECIAL INSP TO START PART 2 AT 3 MONTHS INTERVALS PER WORK CARD WO 8-5510-7-2307H3, PT 1 AND 2 REF AD 88-03-08.

Part: MIXER BRACKET — CRACKED (SPOILER CONTROL)

LT LATERAL CONTROL MIXER BRACKET ASSY WAS FOUND CRACKED ON HFEC INSP, PART 1 OF EO 8-2760-7-3310 C1. CRACK IS .25 INCH LONG ON RT LEG OF BRACKET AT RADIUS.