N994DL

Part: SENSOR — SPARKS (WINDOW HEAT) · airframe 72,389 hrs · 52,400 cycles

CAPTAIN`S SIDE W/S HEAT TEMP SENSOR SPARKING. SECURED WIRING OK FOR SVC REF AMM CHAP 20.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,125 hrs · 52,153 cycles

FIRST CLASS SEATS EMERGENCY LIGHTS INOP. R/R FWD BATTERY PACK REF MD-88 AMM 33-50 OPS CK NORMAL OK FOR SVC. (LP6104452)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,997 hrs · 52,031 cycles

FIRST CLASS EMERGENCY LIGHTS INOP. REPLACED B5-211 BATTERY PACK AND POWER SUPPLY AT STA 388R IAW AMM 33-53 - ALL CKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,434 hrs · 51,509 cycles

AFT WING PLUG DOOR EXIT SIGNS, LT AND RT, UPPER ARE INOPERATIVE. REMOVED AND REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 71,362 hrs · 51,443 cycles

FOUND FIRST CLASS SEAT EMERGENCY LIGHTS INOPERATIVE. DISCOVERED BLOWN FUSE IN POWER SUPPLY PACK. REPLACED SAME PER MD88 AMM 33-53. SYSTEM CHECKS GOOD. OK FOR SERVICE.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 71,009 hrs · 51,144 cycles

EMERGENCY LIGHTS INOP AT 10DC AND 23DE. RELAMPED NO HELP, FOUND DAMAGED ON BOTH WIRE HARNESSES. REPLACED BOTH HARNESSES PER MD88 AMM 33-52, OPS CHKS GOOD AC OK FOR SVC. (LP5553492)

Part: FUSE — BLOWN (BATTERY PACK) · airframe 70,795 hrs · 50,945 cycles

F/C EMERG LIGHTS INOP. REPLACED FUSES ON BATTERY PACK PER AMM 33-53. CKS GOOD. A/C OK FOR SVC. (LP5733058)

Part: DOOR — MISSING (OIL SERVICE) · airframe 70,003 hrs · 50,302 cycles

CREW REPORTS OIL SERVICE DOOR MISSING ON RT ENG. PERFORMED INSPECT RT ENG OIL SERVICE ERA 501258-14 MA, ACCOMPLISH PERMANENT REPAIR PER MD88 CMM 71-10, WITRH NEW OIL SERVICE DOOR. OPS CHECK GOOD. SDR REPORTED DUE TO POSSIBILITY THAT THE DOOR COULD HAVE DEPARTED THE AIRCRAFT DURING FLIGHT.(LP5209876)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,038 hrs · 49,441 cycles

EMERGENCY LIGHT AT PASSENGER SEAT 19D IS INOP. R&R EMERGENCY LIGHT ASSY REF AMM 33-50. OPS CHECKS GOOD.

Part: LANYARD — WORN (TAILCONE SLIDE) · airframe 68,872 hrs · 49,308 cycles

WORN SLIDE LANDYARD ATTACHED AT THE TAILCONE. THE LANDYARD WAS REPLACED IAW AMM 53-53-00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 68,868 hrs · 49,306 cycles

CRACK ON FITTING STA Y=1437 BTW LONG 2R-3R AT AFT ACCESSORIES COMPARTMENT. FITTING STA Y=1437 BTW LONG 2R-3R AT AFT ACCESSORIES COMPARTMENT WAS REPLACED PER DWG 4918093 REV C AND SRM 51-30-1, 51-30-5.

Part: BULKHEAD — CRACKED (RT COWLING) · airframe 68,868 hrs · 49,306 cycles

CRACK IN NOSE COWLING AFT BULKHEAD IN STA. YN= 50.950 BETWEEN 6 TO 8 O’CLOCK POSITION AT RT ENGINE. NOSE COWL P/N:5930645-505,S/N: 002396 WAS REMOVED AND SERVICEABLE NOSE COWL P/N:5930645-509 S/N DL65 WAS INSTALLED PER AMM 71-10-01-201.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,868 hrs · 49,306 cycles

DURING INSPECTION, CORROSION WAS FOUND ON THE INTERNAL DOUBLER OF THE AFT LAVATORY SERVICE PANEL. THE DOUBLER WAS REPAIRED IAW ERA 568604-14, REV ORIGINAL, AND ETI-88-18-049, REV 1.

Part: SERVICE PANEL — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 68,868 hrs · 49,306 cycles

CORROSION ON AFT LAVATORY SERVICE PANEL. CORROSION LEVEL 2 AFT LAVATORY SERVICE PANEL WAS REPLACED PER SRM 51-30-2, 51-30-5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 68,868 hrs · 49,306 cycles

CRACK ON FRAME WEB STA Y= 1463 CANT AT 2 HRS POSITION IN AFT ACCESSORIES COMPARTMENT. FRAME WEB STA Y= 1463 CANT AT 2 HRS POSITION WAS REPLACED PER SRM 53-14-4 FIG 3 AND 51-30-5 AND 51-30-2.

Part: LANYARD — DAMAGED (EVAC SLIDE) · airframe 68,868 hrs · 49,306 cycles

BROKEN WIRES ON LANYARD OF SLIDE AT FWD PASSENGER ENTRANCE DOOR (L1), ALSO ON LANYARD OF SLIDE AT AFT SERVICE DOOR (L2). LANYARD OF SLIDE AT FWD PASSENGER ENTRANCE DOOR (L1), ALSO ON LANYARD OF SLIDE AT AFT SERVICE DOOR (L2) WERE REPLACED PER AMM 25-62-00 STEP 2 PARAGRAPH D-4.

Part: ENGINE — FAILED (RIGHT) · airframe 68,805 hrs · 49,256 cycles

AIR TURN BACK DUE TO A RIGHT ENGINE PROBLEM. AT 9000 FEET, CREW HEARD A COMPRESSOR STALL AND OBSERVED RIGHT EGT FLASHING. THE THROTTLES WERE SET BACK TO IDLE FOR REST OF FLIGHT. AN EMERGENCY WAS DECLARED. MAINTENANCE FOUND TURBINE DAMAGE AND REPLACED THE RIGHT ENGINE.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,740 hrs · 48,492 cycles

SEAT ROW 28 EMERGENCY LIGHT INOPERATIVE. REPLACED THE SEAT WIRE HARNESS, OPS CHECKED GOOD IAW AMM 33-53.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 66,270 hrs · 47,366 cycles

VERTICAL STABILIZER, LT AND RT SIDE LEADING EDGE SKINS AND SPARS CRACKED. REPAIRED IAW AMOC 17-080, & 17-081. COMPLIED WITH PRI 557746-14 REV 0, 1, & 2, AND ERA 557746-14 AD, REV 0.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 66,270 hrs · 47,366 cycles

VERTICAL STAB FRONT SPAR CAP LT SIDE HAS FOUR LE ATTACH HOLES INDICATING CRACKS. HOLES WERE STEPPED UP TO .265, NDT CRACK FREE AND BUSHINGS FABRICATED AND INSTALLED ON PRI 557746-14 FABRICATED AND DRILLED REPAIR STRAP IAW DWG SG09550005-7001. REPAIRED IAW PRI 557746-14, REV 0, 1, & 2. COMPLIED WITH ERA 557746-14, REV O.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 70,894 hrs · 51,031 cycles

VERT STAB FRONT SPAR L.E. ATTACH HOLE HAS CRACK IND RH SIDE. ESTABLISHING LOG FOR DTE TRACKING PER ER/A 557746-14AD. CURRENT REVISION OF ER/A 557746-14AD IS REV. A. THIS LOGPAGE IS NOW TERMINATED. SUPPLEMENTAL INSPECTION REQUIREMENTS ARE NOW TRACKED VIA LOGPAGE 1011548. (LP2979969)

Part: FRAME — CRACKED (BS 1463) · airframe 66,270 hrs · 47,366 cycles

DURING FRAME INPECTION, FOUND A THREE INCH CRACK, BS 1463 BETWEEN STRINGERS 7, AND 8R. REMOVED DAMAGED THE DAMAGE AND REPAIRED IAW PRI 557741-14, REV 0, 1, & 2. COMPLIED WITH SECTION 1 PERMANENT REPAIR IAW ERA 557741-14, REV ORIG.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 66,270 hrs · 47,366 cycles

VERTICAL STAB FRONT SPAR LE ATTACH POINT HAS A CRACK INDICATION, RT SIDE. HOLES WERE STEPPED, FABRICATED AND INSTALLED IAWPRI 557746-14, FABRICATED AND DRILLED A REPAIR STRAP IAW DWG SG09550005-7001. REPAIRED IAW PRI 557746-14, REV 0, 1, 2. COMPLIED WITH ERA 557746-14AD, REV 0.

Part: FRAME — CRACKED (BS 1463) · airframe 66,270 hrs · 47,366 cycles

BS 1463 FRAME CRACKED. COMPLIED WITH PRI 557741-14, REV 0, 1, & 2.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 66,270 hrs · 47,366 cycles

VERTICAL STAB L/E HAS FOUR ATTACH HOLES INDICATING CRACKS ON LEFT SIDE OF L/E SKIN. STEPPED HOLES TO .265 IAW PRI 557746-14 REV . VERIFIED CRACK FREE IAW NDT SPM 06-10-001.003. REPAIRED IAW PRI 557746-14 REV 0, 1, & 2. COMPLIED WITH ERA 557746-14AD, REV ORIG.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 65,980 hrs · 47,155 cycles

EMERGENCY LIGHT AT ROW 18 INOPERATIVE. FOUND CONNECTOR UNDER SEAT 18E DISCONNECTED. CONNECTED AND OPS CHECKED NORMAL IAW AMM 33-53

Part: LIGHT — INOPERATIVE (TAILCONE) · airframe 65,222 hrs · 46,621 cycles

TWO EMERGENCY LIGHT'S OUT AFT TAILCONE AREA. RELAMPED 2EA EMERGENCY LIGHT'S AFT TAIL CONE AREA. OP'S CK GOOD.

Part: WIRE — PINCHED (NLG) · airframe 65,222 hrs · 46,621 cycles

NOSE GEAR RED UNSAFE LIGHT WITH GEAR HANDLE IN UP POSITION . GEAR INDICATIONS NORMAL WITH GEAR DOWN . QRH COMPLETED AND UNSAFE INDICATION REMAINED , WITH GEAR HANDLE UP. FOUND PROX SENSOR D1-32 INTERMITTENT OPEN AND NOTED PINCHED WIRE IN CONDUIT. REPLACED D1 -32 (MPN 8-922-01) IAW AMM 32-60-05 201. GEAR SWING ACCOMPLISHED. OPS CKD GOOD.

Part: WIRE — SHORTED (CABIN) · airframe 64,302 hrs · 45,956 cycles

ROW 31 AND AFT EMERGENCY LIGHTS WILL NOT TEST. FOUND SHORTED WIRES AT TAIL CONE EMERGENCY LIGHT, L2-846. REPAIRED WIRES REF WDM 33-51-14. REPLACED FUSES ON AFT EMERGENCY POWER SUPPLY REF SWPM 20-10 AND WDM 33-51-14. OPS CHECK GOOD OF EMERGENCY LIGHTS.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 64,265 hrs · 45,930 cycles

DURING CHECK, ROWS 31-36 EMERGENCY LIGHTS FOUND FUSE F1 OF R5-212 INOPERATIVE. REPLACED THE FUSE IAW BSWPM 20- CHECKED OK.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 63,634 hrs · 45,484 cycles

DENTS ON INBD FLAP INBD VANE UPPER SKIN AT LT WING. DUE TO SEVERALS DENTS LT WING INBD FLAP, INBD VANE WAS REPLACED IAW AMM 27-50.

Part: INTERCOSTAL — CRACKED (BS 174-194) · airframe 63,633 hrs · 45,483 cycles

CRACKED INTERCOSTAL BS 174 -194 . INTERCOSTAL REPAIRED IAW SRM 53-01 FIG 3.

Part: STRINGER — CRACKED (LT WING) · airframe 63,633 hrs · 45,483 cycles

CRACK ON STRINGER 11 APPROXIMATELY BS XRS=164 IN-TANK AT LT WING. CRACK ON STR 11 WAS REPLACED IAW DWG SR 09570100, REV B, CARD JIC 5712-01030-03 AND ER/A 543225-14AD REV ORIGINAL.

Part: SUPPORT FITTING — CORRODED (MLG ACTUATOR) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON RETRACT ACTUATOR SUPPORT FITTING BORE AND OTBD FACE AT LT MLG. THIS REPAIR WAS PERFORMED IAW ER/A 543221-14AD, REV ORIGINAL.

Part: SKIN — DELAMINATED (LT ELEVATOR TAB) · airframe 63,633 hrs · 45,483 cycles

DELAMINATED UPPER, LOWER SKIN ON LT ELEVATOR GEARED TAB. GEARED TAB WAS REPLACED AND LEVATOR GEARED TAB WILL BE INSTALLED AND ADJUSTED UNDER CARD 2730-4334.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION WAS FOUND ON 7 FASTENER HOLES COMMON TO THE RT LOWER WING SKIN AND THE ACCESS DOOR CUTOUT, AT THE BS XRS 196, 197, 198.5, 200.5, 206, 207 AND 209 BETWEEN STR 12 AND 15. HOLES WERE REPAIRED IAW ER/A 543214-14AD, REV ORIGINAL.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,633 hrs · 45,483 cycles

CRACKED ON FWD PAN EXTERNAL FACE JUST AROUND BLIND NUT BETWEEN BEAM 2 AND 3 AT AFT CARGO COMPARTMENT DOOR. FWD PAN EXTERNAL WAS REPAIRED IAW ETI-88-16-139 REV 1 AND ERA 545083-14 REV ORIG.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,633 hrs · 45,483 cycles

CRACKED OTBD PAN, OTBD FACE BETWEEN PROJECTION BEAM 1 AND 2, AND MECHANISM CAM AT FWD CARGO COMPARTMENT DOOR. PAN WAS REPAIRED IAW ETI-88-16-126, REV 1 AND ERA 543220-14 REV ORIGINAL.

Part: DOUBLER — CRACKED (BS 101-110) · airframe 63,633 hrs · 45,483 cycles

CRACKED PREVIOUS REPAIR DOUBLER ON FUSELAGE SKIN BETWEEN BS 101 TO BS 110 AND PROJECTION LONGERON 27LT. DOUBLER WAS REPLACED IAW SRM 53-05, FIG 158, 51-30-2, 51-30-5, 51-30-11 AND 51-10-3 PAR 14 AND 21.

Part: DOUBLER — CRACKED (BS 99) · airframe 63,633 hrs · 45,483 cycles

CRACKED PREVIOUS REPAIR DOUBLER ON FUSELAGE SKIN BS 99 AND PROJECTION OF LONGERON 28R. DOUBLER WAS REPLACED IAW SRM 53-05, FIG 158, 51-30-2, 51-30-5.

Part: CHANNEL — CRACKED · airframe 63,633 hrs · 45,483 cycles

CRACK ON PREVIOUS REPAIR AND CHANNEL FLOOR PANEL 927E. FLOOR PANEL 927E WAS REPLACED IAW SRM 51-10-4 AND 51-10-3, PAR 21 AND 14.

Part: CHANNEL — CRACKED · airframe 63,633 hrs · 45,483 cycles

CRACKS ON PREVIOUS REPAIR AND CHANNEL FLOOR PANEL 927E. FLOOR PANEL 927E WAS REPLACED IAW SRM 51-10-4 AND 51-10-3, PAR 21 AND 14.

Part: CARGO TRACK — CORRODED (BS 1218-1320) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON LT CARGO TRACK BETWEEN BS 1320 - 1218 IN AFT CARGO COMPARTMENT. CARGO TRACK WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1414C AT RT WING. ACCESS PLATE WAS REPLACED.

Part: SKIN — DAMAGED (BS 1003-1022) · airframe 63,633 hrs · 45,483 cycles

SCRATCH ON WINDOW BELT BETWEEN BS 1003-1022 AT RT EXTERNAL FUSELAGE. WINDOW BELT WAS REPAIRED IAW ER/A 543202-14, REV.

Part: CARGO TRACK — CORRODED (BS 1218-1320) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON LT CARGO TRACK BETWEEN BS 1320 - 1218 IN AFT CARGO COMPARTMENT. CARGO TRACK WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — DAMAGED (BS 1003-1022) · airframe 63,633 hrs · 45,483 cycles

SCRATCH ON WINDOW BELT BETWEEN BS 1003-1022 AT RT EXTERNAL FUSELAGE. WINDOW BELT WAS REPAIRED IAW ER/A 543202-14, REV.

Part: CARGO TRACK — CORRODED (BS 1212-1320) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON RT CARGO TRACK BETWEEN BS 1212 - 1320. CARGO TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1414C AT RT WING. ACCESS PLATE WAS REPLACED.

Part: CARGO TRACK — CORRODED (BS 1212-1320) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON RT CARGO TRACK BETWEEN BS 1212 - 1320 IN AFT CARGO COMPARTMENT. CARGO TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON BARREL NUT HOLE NR 26 AT LT HORIZONTAL ESTABILIZER UPPER SKIN BS XH=27.2. REPAIR WAS PERFORMED IAW ER/A 543212-14, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 769-788) · airframe 63,633 hrs · 45,483 cycles

LIGHTNING STRIKE ON LT FUSELAGE SKIN WINDOW BELT FWD LOWER CORNER BETWEEN BS 769 TO 788. AREA WAS REPAIRED IAW ER/A 545088-14, REV ORIG AND ETI-88-16-107, REV 3.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON BARREL NUT HOLE NR 26 AT LT HORIZONTAL ESTABILIZER UPPER SKIN BS XH=27.2. REPAIR WAS PERFORMED IAW ER/A 543212-14 REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON RT WING FUEL ACCESS 1470C COUNTERSINK HOLES. FUEL ACCESS PLATE 1470C WAS REPLACED IAW SRM 51-22-2A.

Part: SKIN — DAMAGED (BS 769-788) · airframe 63,633 hrs · 45,483 cycles

LIGHTNING STRIKE ON LT FUSELAGE SKIN WINDOW BELT FWD LOWER CORNER BETWEEN BS 769 - 788. AREA WAS REPAIRED IAW ER/A 545088-14, REV ORIGINAL AND ETI-88-16-107, REV 3.

Part: SKIN — DAMAGED (BS 750-769) · airframe 63,633 hrs · 45,483 cycles

LIGHTNING STRIKE ON LT FUSELAGE SKIN. WINDOW BENT AFT LOWER CORNER BETWEEN BS 750 TO 769 . AREA WAS REPAIRED IAW ER/A 545088-14, REV ORIGINAL AND ETI -88-16-107. RII INSPECTION WAS VERIFIED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OFFUEL ACCESS PLATE NR 1357C AT LT WING. COUNTERSINK HOLES ON ACCESS PLATE 1357C AT LT WING REMOVED, COUNTERSINK HOLES WERE MEASURED, MAX DIAMETER ALLOWABLE IN 8 HOLES IS 0.532 IN AND MAX DIAMETER MEASSURED IN 8 HOLES IS 0.547 IN THEREFORE WAS FOUND OUT OF LIMITS IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1357C AT LT WING. COUNTERSINK HOLES ON ACCESS PLATE 1357C AT LT WING REMOVED, COUNTERSINK HOLES WERE MEASSURED, MAX DIAMETER ALLOWABLE IN 8 HOLES IS 0.532 IN AND MAX DIAMETER MEASURED IN 8 HOLES IS 0.547 IN THEREFORE WAS FOUND OUT OF LIMITS IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON RT WING FUEL ACCESS 1470C COUNTERSINK HOLES. FUEL ACCESS PLATE 1470C WAS REPLACED IAW SRM 51-22-2A.

Part: SKIN — DAMAGED (BS 750-769) · airframe 63,633 hrs · 45,483 cycles

LIGHTNING STRIKE ON LT FUSELAGE SKIN. WINDOW BENT AFT LWR CORNER BETWEEN BS 750 TO BS 769. AREA WAS REPAIRED IAW ER/A 545088-14, REV ORIGINAL AND ETI -88-16-107. RII INSPECTION WAS VERIFIED.

Part: FRAME — CORRODED (BS 1307) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION OUT OF LIMITS ON FRAME BS 1307 BETWEEN LONGERON 29 LT AND 29 RT AT C3. THE FRAME WAS REPAIRED IAW SRM 53-03, FIG 2A.

Part: INTERCOSTAL — CRACKED (BS 937) · airframe 63,633 hrs · 45,483 cycles

CRACK ON INTERCOSTAL, X=58, BS 937 AT AREA HYD. GROUND SERVICING ACCESS W/W, SIDE LT. INTERCOSTAL WAS REPLACED IAW DWG 5930584, REV BY SRM 53-14-3, 51-30-5 AND 51-30-2.

Part: FERRULE — DAMAGED (FLOOR PANEL) · airframe 63,633 hrs · 45,483 cycles

DAMAGED FERRULE ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1363C. ACCESS PLATE NR 1363C WAS REPLACED UNDER CONDITION III IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1335C AT LT WING. ACCESS PLATE NR 1335C WAS REPLACED UNDER CONDITION III IAW SRM 51-22-2A.

Part: CHANNEL — CRACKED · airframe 63,633 hrs · 45,483 cycles

CRACKED CHANNELS ON FLOOR PANEL. THE NEW CHANNEL INSTALLED IAW SRM 51-30-1, SRM 51-10-4, SRM 51-10-3, PAR 14 - 21, AND DWG 9936639, REV P.

Part: ANGLE — CRACKED (BS 1485) · airframe 63,633 hrs · 45,483 cycles

CRACK ON ANGLE BS 1485 AT THE TWO O`CLOCK POSITION AT AFT ACCESORY COMPARTMENT. THE ANGLE FABRICATED AND REPLACED IAW DGW 9911842, REV DH AND SRM 51-30-2 AND 51-30-5.

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 63,633 hrs · 45,483 cycles

ELONGATED HOLES ON FWD/AFT HINGES AT MID CARGO COMPARTMENT DOOR. FWD/AFT HINGES WERE REMOVED IAW AMM 52-31-02. FWD/AFT HINGES WERE REPAIRED IAW ER/A 10-521061-14MA REV. ORIGINAL. HINGES WERE INSTALLED IAW AMM 52-31-02.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1365C AT LT WING. ACCESS PLATE NR 1365C WAS REPLACED UNDER CONDITION III IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1472C AT RT WING. ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON RT WING FUEL ACCESS 1476C COUNTERSINK HOLES, 2 EA. ACCESS PLATE NR 1476C WAS REPLACED UNDER CONDITION III IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1311C AT LT WING. ACCESS PLATE NR 1311C WAS REPLACED UNDER CONDITION III IAW SRM 51-22-2A.

Part: INTERCOSTAL — CORRODED (BS 1307-1322) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON INTERCOSTAL JUST UNDER RT CARGO TRACK BETWEEN BS 1307 - 1322 IN AFT CARGO COMPARTMENT. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2.

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 63,633 hrs · 45,483 cycles

ELONGATED HOLES ON FWD, AFT HINGES AT FWD CARGO COMPARTMENT. HINGES WERE REMOVED IAW AMM 52-31-02. FWD/AFT HINGES WERE REPAIRED IAW ER/A 497387-14MA, REV B. HINGES WERE INSTALLED IAW AMM 52-31-02.

Part: STRUCTURE — NOT REPORTED (BULKHEAD) · airframe 63,633 hrs · 45,483 cycles

PRESSURE DOME LOWER CHARD SPLICE FOUND BETWEEN LONGERON 26, 27 RT/LT IN DISCREPANCY TO INSPECTION CARD 5310-01414-1701 AT AFT CARGO COMPARTMENT. AREA WAS REPAIRED IAW ER/A 593209-14, REV ORIGINAL AND ETI 88-16-114, REV 1.

Part: STRUCTURE — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON RT, LT ELEVATOR SECTOR. LT ELEVATOR SECTOR WAS REPLACED UNDER CARD 2730-4234, JOB 001-0357 AND RT ELEVATOR SECTOR WAS REPLACED AND IS INSTALLED UNDER CARD 2730-4234, JOB 001-0357.

Part: FRAME — CRACKED (BS 1463) · airframe 63,633 hrs · 45,483 cycles

CRACK UPPER FRAME CUP, BS 1463, LONG 18LT AT AFT ACCESSORY COMPARTMENT. FRAME WAS REPAIRED IAW SRM 53-01, FIG 2, 51-01, 53-14-4, FIG 3, 51-30-2, 51-30-5.

Part: ROD END — WORN (LT ELEVATOR) · airframe 63,633 hrs · 45,483 cycles

FREE PLAY ON ROD END OF ANTI-FLOAT TAB PUSH ROD AT LT ELEVATOR. ANTI-FLOAT TAB PUSH ROD ASSY AT LT ELEVATOR WAS REPLACED IAW AMM 27-30-14 AND STEP 5B AT AMM 27-30-14 WILL BE PERFORMED WITH CARD 2730-4831, JOB 001-0231 AND FREE PLAY WAS CORRECTED.

Part: VANE — WORN (LT WING TE FLAP) · airframe 63,633 hrs · 45,483 cycles

WORN OTBD FLAP INBD VANE L/E AT LT WING. REPAIRED IAW SRM 57-03D, PAR 11.

Part: FAIRING — CRACKED (RT ELEVATOR) · airframe 63,633 hrs · 45,483 cycles

CRACKED GEARED TAP FIXED FAIRING ON BS XET=89 AT RT ELEVATOR. FAIRING WAS REPAIRED IAW SRM 51-30-2, 51-30-8, 51-10-3, PAR 14 AND 21 AND 55-01, FIG 2, SHEET 2.

Part: STRAP — CORRODED (BS 1287-1307) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON STRAP JUST ABOVE FINGER DOUBLER PRODUCTION BETWEEN LONGERON 26 LT AND 25 LT BS 1307 TO BS 1287 AT AFT CARGO COMPARTMENT. FASTENER WAS REMOVED, DAMAGE ON BS 1276 TO BS 1294 WAS REMOVED. NEW SECTION FINGER DOUBLER WAS FABRICATED, DRILLING AND ADJUSTED AND INSTALLED IAW SRM 53-04, FIG 12E AND SRM 51-10-4. FINGER DOUBLER BETWEEN BS 1295 - BS 1307 WAS INSPECTED AND NO DAMAGE WAS FOUND.

Part: BRACKET — WORN (HORIZONTAL STAB) · airframe 63,633 hrs · 45,483 cycles

WEAR ON RT HORIZONTAL STABILIZER FWD SPAR ANTI-FLOAT TAB BRACKET. ANTI-FLOAT TAB BRACKET AT FWD SPAR ON RT HORIZONTAL STABILIZER WAS REPLACED IAW AMM 20-30-01.

Part: INTERCOSTAL — CORRODED (BS 769-788) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON INTERCOSTAL BETWEEN LONG 26RT AND 27LT, BS 788 TO BS 769 AT MID CARGO COMP. DUE TO EXCESIVE CORROSION INSTERCOSTAL WAS REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 14 ,21 DWG 9915554, REV: J.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 63,633 hrs · 45,483 cycles

DELAMINATED FLOOR PANEL. FLOORS PANEL FABRICATED IAW AMM 53-20-01-201.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 63,633 hrs · 45,483 cycles

DENT ON LOWER SKIN OF RT GEARED TAB AT HORIZONTAL STABILIZER. LOWER SKIN OF RT GEARED TAB AT HORIZONTAL STABILIZER WAS REPAIRED IAW SRM AND 1031 CARD 2000-8149-04.

Part: FRAME — WORN (BS 1338) · airframe 63,633 hrs · 45,483 cycles

WEAR ON FRAME, BS 1338 AREA APU COMPARTMENT ATA FT ACCESSORY COMPARTMENT. FRAME WAS REPAIRED IAW ER/A 094719-14MA, REV A.

Part: FRAME — CORRODED (BS 1287) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION FOUND OUT OF LIMITS AT FRAME ANGLE ON BS 1287. FRAME ANGLE BETWEEN LONGERONS 26L-26R WAS R & R IAW SRM 53-14-3 AND 51-30-2 AND 51-10-3 PAR 21 AND 14; 51-30-5.

Part: CUSP WEB — CRACKED (BS 1212-1231) · airframe 63,633 hrs · 45,483 cycles

CRACKED LT CUSP WEB BETWEEN X=44-X=54, BETWEEN BS 1212 TO 1231. REMOVE DAMAGE AND DOUBLER WAS FABRICATED IAW SRM 53-05, FIG 131A-1, 51-30-2, 51-10-3, PAR 38.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 63,633 hrs · 45,483 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: INTERCOSTAL — CORRODED (BS 1212-1231) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON INTERCOSTAL JUST ABOVE LONGERON 29L BS 1212 - 1231 IN AFT CARGO COMPARTMENT. INTERCOSTAL WAS REPLACED IAW SRM 53-14-3, 51-30-2, 51-30-5, 51-10-2, 51-10-4, 51-10-3 PAR 21, 14 AND 38.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 63,633 hrs · 45,483 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: SKIN — DAMAGED (RUDDER) · airframe 63,633 hrs · 45,483 cycles

EXPOSED MATERIAL AND DAMAGE COAT PAIN ON RUDDER ACCESS NR 6502G, 6508G, 6513G. EXPOSED MATERIAL AND DAMAGE COAT PAIN ON RUDDER ACCESS NBR 6502G, 6508G, 6513G WERE REPAIRED IAW SRM 51-70-1A, PAR 23.

Part: DOUBLER — WORN (LT WING TE FLAP) · airframe 63,633 hrs · 45,483 cycles

WORN REPAIR DOUBLER ON OTBD FLAP MID VANE BS XVZ=254 AT LT WING. OTBD FLAP MID VANE BS XVZ= 254 AT LT WING WAS REPAIRED IAW SRM 57-03D PAR.

Part: DUCT — CRACKED (RAM AIR) · airframe 63,633 hrs · 45,483 cycles

CRACKS ON RAM AIR DUCT. CRACKS ON RAM AIR "Y" DUCT WERE REPAIRED, WELDED IAW ER/A 503276-14MA, REV C AND AREA WAS TREATED AND PAINTED IAW ER/A 503276-14MA, REV C AND SOPM 20-60-1.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON RT WING FUEL ACCESS 1410C COUNTERSINK HOLES, 5 E/A. CORROSION ON COUNTERSINK HOLES AT FUEL ACCESS 1410C WAS REMOVED, COUNTERSINK HOLES WERE MEASURED ELONGATION CONTINUED THEREFORE IT IS OUT OF LIMITS THEN FUEL ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: FORMER — CRACKED (BS 1510) · airframe 63,633 hrs · 45,483 cycles

CRACK ON CANTED FORMER BS 1510, 10:00, O' CLOCK POSITION AT AFT ACCESSORY COMPARTMENT. FRAME, BS 1510 WAS REPLACED IAW DWG 9911843, REV: AC AND SRM 51-30-2.

Part: FLOOR PANEL — PUNCTURED (NOT REPORTED) · airframe 63,633 hrs · 45,483 cycles

PUNCTURED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: INTERCOSTAL — CRACKED (BS 937) · airframe 63,633 hrs · 45,483 cycles

CRACK ON INTERCOSTAL X=58, BS 937 AT AREA HYD GROUND SERVICEABLE ACCESS W/W. CRACKED INTERCOSTAL X=58, 937 RT AT AREA HYD GROUND SERVICEABLE ACCESS W/W WAS REPLACED IAW DWG 5930584-57, REV BY AND SRM 51-30-2 AND 51-30-5.

Part: CHANNEL — CRACKED (BS 937) · airframe 63,633 hrs · 45,483 cycles

CRACK ON FWD CHANNEL BS 937 X=4 BETWEEN LT/RT MLG WW. CRACKS ON FWD CHANNELS WERE REPAIRED IAW SRM 53-05D, FIG 821D.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 63,633 hrs · 45,483 cycles

DELAMINATED INBD FLAP OTBD VANE XOVIF=68 BELOW RUB STRIP, ON LT WING. VANE REPAIRED IAW SRM 57-03D, PAR II.

Part: SKIN — DAMAGED (RT WING TE FLAP) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

DELAMINATED OTBD FLAP MID VANE LOWER SURFACE BS XVZ=220 AT RT WING. DAMAGE TO THE INTERNAL STRUCTURE OF THE MID VANE OF THE RT WING FLAP ARE OUT OF LIMITS BY CORROSION FOR REPLACE AND REPAIR. OTBD FLAP MID VANE AT RT WING WAS REPLACED IAW SRM 57-50-14, FIG 2 AND IPC 27-50-04-01A.

Part: SUPPORT — CRACKED (BS 927) · airframe 63,633 hrs · 45,483 cycles

CRACK ON BEAM SUPPORT ON BS 927 BELOW SEAT TRACK LBL 4 -12. BEAM SUPPORT WAS REMOVED, NEW BEAM SUPPORT WAS REPLACED AND INSTALLED IAW SRM 51-30-5.

Part: SUPPORT — CRACKED (RAM AIR DUCT) · airframe 63,633 hrs · 45,483 cycles

CRACKS ON ATTACH POINT SUPPORTS ON RAM AIR DUCT 3EA. CRACKS ON ATTACH POINT SUPPORTS ON RAM AIR DUCT WERE REPAIRED, WELDED IAW ER/A 494638-14MA REV B AND SOPM 20-10-19, PAR C4 AND TREATED AND PAINTED IAW SRM 51-10-3.

Part: SKIN — DENTED (LT WING LE SLAT) · airframe 63,633 hrs · 45,483 cycles

TWO DENTS ON PREVIOUS REPAIR DOUBLER OF LT WING SLAT PANEL NR 2. SLAT PANEL NR 2 OF LT WING WAS REPLACED AND WAS REMOVED, INSTALLED ON CARD NR 105, ZONE 10.

Part: DOOR FRAME — CRACKED (BS 1358) · airframe 63,633 hrs · 45,483 cycles

CRACKED FITTING ON VENTRAL DOOR JAMB STRUCTURE BS 1358, X=11, Z15 AT AFT PRESSURE BULKHEAD. FITTING ON VENTRAL DOOR JAMB WAS REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3 PAR 21, 14 AND 51-3-5.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1303C AT LT WING. CORROSION WAS FOUND ON SETTLEMENT AREA AND FUEL ACCESS 1303C WAS REPLACED UNDER CONDITION III IAW SRM 51-22-2A.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 63,633 hrs · 45,483 cycles

CRACK ON FLOOR PANEL AND DISBONDED CHANNEL NR 200A. FLOOR PANEL WAS REPAIRED IAW SRM 51-70-01D, PARA 10.

Part: FLOORBEAM — CRACKED (BS 927) · airframe 63,633 hrs · 45,483 cycles

CRACK ON FLOORBEAM BS 927 BELOW SEAT TRACK LBL 54. FLOORBEAM WAS REMOVED & REPLACED IAW SRM 51-30-2, 51-30-5 AND 51-30-1.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1409C AT RT WING. CORROSION WAS FOUND ON SETTLEMENT AREA AND FUEL ACCESS 1409C WAS REPLACED UNDER CONDITION III IAW SRM 51-22-2A.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,633 hrs · 45,483 cycles

CRACK ON LONGERON 4R BS 1437. LONGERON REPAIRED IAW SRM 53-02, FIG 18, SRM 51-10-2A, 51-10-4, 51-10-3, PAR 14, 21, SRM 51-30-2, AND 51-30-5 A.

Part: CUSP WEB — CORRODED (BS 1060-1117) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON RT CUSP BETWEEN BS 1060-1079, & 1098-1117 BETWEEN RBL 54 TO 60. REPAIRED IAW SRM 53-05, FIG 131A-7 AND 51-10-3, PAR 21-14.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 63,633 hrs · 45,483 cycles

CORROSION ON LT WING FUEL ACCESS 1367C COUNTERSINK HOLES. REPAIRED IAW CONDITION II IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 63,633 hrs · 45,483 cycles

CORROSION ON RT WING FUEL ACCESS 1456C COUNTERSINK HOLES. FUEL ACCESS 1456C WAS REPAIRED BY CONDITION II IAW SRM 51-22-2A.

Part: LONGERON — CRACKED (BS 905) · airframe 63,633 hrs · 45,483 cycles

CRACKED LONGERON 4R AND BS 905. REPAIRED IAW SRM 53-02 FIG 18, 51-10-3 PARR 14, 21 AND 51-30-2.

Part: FLOOR SUPPORT — CRACKED (BS 769-788) · airframe 63,633 hrs · 45,483 cycles

CRACKED ON REPAIR DOUBLER AND CRACKED BEYOND STOP DRILL ON FLOOR SUPPORT X 00 BETWEEN BS 788 - 769. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-5 51-10-4 51-10-3 PAR 14, 21 AND DWG: 9936580, REV BW.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,633 hrs · 45,483 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: SEAT TRACK — CORRODED (BS 894-934) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON RT SEAT TRACK, BS 894 - 934 AND X -54 AT FLOOR STRUCTURE. SEAT TRACK REPAIRED IAW SRM 53-05 FIG 4A AND 51-10-3 PAR 14, 21.

Part: STOP FITTING — CRACKED (EMERGENCY EXIT) · airframe 63,633 hrs · 45,483 cycles

CRACKS ON DOOR STOP CLIPS NRS 1 AND 12 AT LT AFT OVERWING EMERGENCY EXIT. CLIPS WERE REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-2, 51-10-3 PAR 14/21 AND DWG 9957735, REV G.

Part: CUSP WEB — CORRODED (BS 1174-1193) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON CUSP WEB RT X=-54 TO X=-60 BETWEEN BS 1174 AND BS 1193. DAMAGE WAS REMOVED, NEW ITEMS WERE FABRICATE IAW SRM 53-05, FIG 131A-1 53-05 PAR 166 ORIGINAL.

Part: CUSP WEB — CORRODED (BS 596-617) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 596-617 AND RBL 54 - 60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, 51-10-3 PAR 14 AND 21, 51-30-2, 51-30-5.

Part: SUPPORT — CRACKED (HORIZONTAL STAB) · airframe 63,633 hrs · 45,483 cycles

CRACKED NUT ON HORIZONTAL STABILIZER LONGITUDINAL TRIM ACTUATING MECHANISM UPPER SUPPORT. NUT ON HORIZONTAL STABILIZER LONGITUDINAL TRIM ACTUATING MECHANISM UPPER SUPPORT WAS REPLACED IAW AMM 27-41-1.

Part: FERRULE — DAMAGED (FLOOR PANEL) · airframe 63,633 hrs · 45,483 cycles

DAMAGE FERRULES ON FLOOR PANEL. REPLACED FERRULE IAW AMM 53-20-01-201.

Part: CUSP WEB — CRACKED (BS 232) · airframe 63,633 hrs · 45,483 cycles

CRACKED WEB, BS 232 X=34-60 RT AT W1. NEW CUSP WEB WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-4, 51-10-3, PAR 14/21, 51-30-1, 51-30-2, 51-30-5.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1377C AT LT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CORRODED (BS 1234) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON RT CUSP WEB BS 1234 BETWEEN X=-54 TO X=-60 AT PAX CABIN. CUSP WEB WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 131A-7 AND 51-10-3, PAR 21 AND 14.

Part: SKIN — DAMAGED (RUDDER) · airframe 63,633 hrs · 45,483 cycles

EXPOSED METALLIZED AND DAMAGED PAINT ON RT AND LT SKINS OF RUDDER. METALLIZED AND DAMAGED PAINT ON RT AND LT SKIN OF RUDDER WAS REPAIRED IAW ER/A 092613-14MA, REV A.

Part: SKIN — DENTED (CARGO DOOR) · airframe 63,633 hrs · 45,483 cycles

DENT FWD EDGE BETWEEN BEAM 1 AND 3 OUTER SKIN AT AFT CARGO COMPARTMENT DOOR. DENTS WERE ATTENDED IAW ETI-88-16-115, ERA 543210-14, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1371C AT LT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1307C AT LT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: STRUCTURE — BROKEN (RUDDER) · airframe 63,633 hrs · 45,483 cycles

BROKEN LOWER SECTION OF RUDDER L/E. LOWER SECTION OF RUDDER L/E WAS REPAIRED IAW SRM 51-70-01AD PAR 3.

Part: BRACKET — DAMAGED (ELEVATOR) · airframe 63,633 hrs · 45,483 cycles

DAMAGE ON LT OTBD BEARING BRACKET JUST IN BEARING AREA AT ELEVATOR MECHANISM. LT OTBD BEARING BRACKET WAS REPLACED IAW AIPC 27-30-00 AND WILL BE INSTALLED UNDER JIC A/C 0994, CARD 2730-4234.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1436C AT RT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: STRAP — CRACKED (L1 DOOR) · airframe 63,633 hrs · 45,483 cycles

CRACKED STRAP ON BEAM NR 6 AT L1 DOOR. STRAP ON BEAM NR 6 AT WAS REPLACE IAW SRM 51-30-2, 51-10-3 PAR 14 AND 21, AND 51-10-4.

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON FLOOR PANEL 160G AT W1. FLOOR PANEL WAS REPLACED IAW SRM 51-30-2, 51-10-2 AND 51-10-3, PAR 14, 21, 38 AND DWG: 9957828. REV "Y".

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1373C AT LT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1355C AT LT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: SKIN — DENTED (CARGO DOOR) · airframe 63,633 hrs · 45,483 cycles

SEVERAL DENTS OUTER SKIN BETWEEN BEAM 2 AND 5 AT AFT CARGO COMPARTMENT DOOR. DENTS WERE ATTENDED IAW ETI-88-16-115, ERA 543210-14, REV ORIGINAL. PERFORM A GVI OF THE DAMAGED AREAS WITHIN EVERY 3, 800 FLIGHT CYCLES. AFTER SECTION I ACCOMPLISHED OF ERA 543210-14, REV ORIGINAL.

Part: INTERCOSTAL — CRACKED (L1 DOOR) · airframe 63,633 hrs · 45,483 cycles

CRACKED INTERCOSTAL BETWEEN BEAMS 4-5 AT L1 DOOR. INTERCOSTAL BETWEEN BEAM 4-5 L1 DOOR WAS REPLASE IAW SRM 51-30-2, 51-10-3 PAR. 14 AND 21, 51-10-4 AND DWG: 9955763, REV: M.

Part: CUSP WEB — CORRODED (BS 529) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON LT CUSP WEB ON BS 529 BETWEEN X=57 TO X=60 AT PAX CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-9.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PLATE NR 1466C AT RT WING. ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A.

Part: EXHAUST DUCT — CRACKED (APU) · airframe 63,633 hrs · 45,483 cycles

CRACKED APU EXHAUST DUCT AT FUSELAGE SKIN. EXHAUST DUCT APU AT FUSELAGE SKIN WAS REPAIRED, REWELDED IAW ER/A 473221-14 MA, REV ORIGINAL.

Part: CUSP WEB — CORRODED (BS 1155-1174) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON PREVIOUS CUSP WEB REPAIR DOUBLER BETWEEN BS 1155 AND 1174, RT X -44 TO X -60. CORROSION WAS ATTENDED IAW SRM 51-30-2, 51- 10-3, PARS 14 AND 21, 53-05, FIG 131A-5.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 63,633 hrs · 45,483 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: FRAME — CRACKED (BS 1322) · airframe 63,633 hrs · 45,483 cycles

CRACKED FRAME BS 1322 AND LONGERON 17L. DAMAGED FRAME AREA WERE REMOVED, HFEC INSPECTION WAS PERFORMED ON FRAME, REPAIR PARTS AND REWORKED AREA WERE TREATED, PAINTED, INSTALLED IAW SRM 51-10-2, 51-10-2A, 51-10-3 PAR 14/21, 51-30-1, 51-30-2, 51-30-5, 51-30-3, NDT SPM 06-10-01-001 AND ER/A 493697-14MA, REV B.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,633 hrs · 45,483 cycles

CRACK ON LONGERON 16L AND BS 1437 AT AFT ACCESSORY COMPARMENT. SECTION OF LONGERON WAS REPLACED IAW SRM 53-14, 4, 51-30-2, 51-30-5, 51-10-4, 51-10-1, 51-10-3 PAR 14, 21.

Part: CUSP WEB — CRACKED (BS 826-845) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

DUE TO EXCESSIVE CORROSION ON CRACKED CUSP WEB BETWEEN BS 826 AND 845, RBL 54 - 60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-16, 51-10-3 PAR 14 AND 21, 51-30-2.

Part: DOOR FRAME — CORRODED (BS 329-700) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON WEB BETWEEN LONGERON 9 - 24R BS 629 - 700 MID CARGO BAY DOOR FRAME. CORROSION REMOVED IAW SRM 51-10-3, PAR 26, 14, 21 UT MD/DC NDT SPM 04-00-07, PAR 5, FIG 3.

Part: CHANNEL — CRACKED · airframe 63,633 hrs · 45,483 cycles

CRACKS ON FLOOR CHANNEL. CHANNEL REPAIRED IAW 53-05, FIG 131B.

Part: CUSP WEB — CORRODED (BS 1036-1038) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON LT CUSP WEB X=55 TO X=60 BETWEEN BS 1036 TO BS 1038 AT FLOOR CABIN STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14, 51-30-5, 51-10-3 PAR 21, 14 AND 38.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,633 hrs · 45,483 cycles

DURING REMOVAL OF THE STOP WAS FOUND CRACK ON INNER PAN OF AFT CARGO DOOR. REPAIRED IAW SRM 52-03-D FIG 10. FOUND WITHIN LIMITS IAW SRM 52-03, FIG. 10.

Part: MEMBRANE — CORRODED (BS 210-218) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION FOUND ON MEMBRANE, X -52 TO -56, BS 210 - 218. REPAIRED IAW SRM 51-10-3, PAR 26, 14, 21 AND 38 AND ER/A 511165-14MA, REV C.

Part: CUSP WEB — CORRODED (BS 806-817) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

DUE TO EXCESSIVE CORROSION ON CUSP WEB X=-54 TO X=-60 BETWEEN BS 806 AND 817. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, FIG 131A-2, 51-10-3 PAR 14 AND 21, 51-30-2.

Part: SKIN — DAMAGED (BS 389-408) · airframe 63,633 hrs · 45,483 cycles

LIGHTNING STRIKE ON LT FUSELAGE SKIN WINDOW BELT LOWER EDGE AND LOWER CORNER BETWEEN BS 389 TO BS 408. DAMAGE WAS BLENDED OUT, IAW SRM 53-05, FIG 111. AREA WAS MEASURED: BLENDED OUTS WERE FOUND IN ZONE 3 AND NO CRITICAL ZONE THEREFORE ALL ARE WITHIN LIMITS IAW SRM 53-05 FIG. 111.

Part: PAN — CRACKED (BS 927-946) · airframe 63,633 hrs · 45,483 cycles

CRACK ON LT RING PAN UPPER FWD CORNER BETWEEN BS 927 TO 946. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5 53-05, FIG 122, 51-10-3, PAR 14,21 AND ER/A 487747-14MA REV A AND ER/A 493648-14MA, REV A.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 63,633 hrs · 45,483 cycles

WEAR ON FWD/AFT DOUBLERS ON LOWER CORNERS AT FWD CARGO COMPARTMENT DOOR. DOUBLERS WERE REMOVED, NEW DOUBLERS WERE FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2, 51-10-3, PAR 21 AND 14, ER/A 486624-14MA, REV ORIGINAL

Part: PAN — CRACKED (BS 769-788) · airframe 63,633 hrs · 45,483 cycles

CRACK ON LT RING PAN UPPER FWD CORNER BETWEEN BS 769 TO 788. RING PAN WAS REPAIRED IAW SRM 51-30-5, 51-30-2 53-05, FIG 122, 51-10-3 PAR 14,21 AND ER/A 487747-14MA, REV A AND ER/A 493648-14MA, REV A.

Part: PAN — CRACKED (BS 351-864) · airframe 63,633 hrs · 45,483 cycles

CRACKED RT RING PAN FWD UPPER CORNER BETWEEN BS 351-370, 370-389, 845-864. RING PAN RT FWD UPPER CORNER BETWEEN BS 351-370, 370-389, 845-864 WERE REPAIRED IAW SRM 53-05, FIG 122 AND 51-30-2, 51-30-05, ERA 487747-14MA, REV A 493648-14MA, REV A.

Part: SEAT TRACK — CORRODED (BS 506-509) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON PLUG AT RT SEAT TRACK, X=-54 BS 506-509 AT FLOOR STRUCTURE. PLUG WAS REMOVED, NEW PLUG WAS INSTALLED IAW SRM 51-30-1, 53-10-3, PAR 21, 14, 53-05, FIG 4A.

Part: SEAT TRACK — CORRODED (BS 579) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON LT PLUG SEAT TRACK, X=54, BS 579. PLUG WAS REMOVED, NEW PLUG WAS INSTALLED IAW SRM 51-30-1, 53-10-3, PAR 21, 14, 53-05, FIG 4A.

Part: SPAR — DAMAGED (RT WING) · airframe 63,633 hrs · 45,483 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND 7 DIFFERENT FASTENERS OF DE PSE AT RT LOWER WING SKIN REAR SPAR BETWEEN XRS=162 TO XRS=168. REPAIRED IAW ER/A 543200-14AD. REV, ORIGINAL FROM THE SECTION II.

Part: SKIN — NOT REPORTED (BS 1418) · airframe 63,633 hrs · 45,483 cycles

DISCREPANT AREA WAS FOUND ON FUSELAGE SKIN, EXTERNAL DOUBLER REPAIR AT BS 1418 AND BETWEEN LONGERON 1 AND 3 RT. THE ER/A 498486-14, REV. ORIGINAL WAS GENERATED AND FROM SECTION I: ER/A REVISION REQUIRED, AMOC IAW SID AD 2004-11-07.

Part: PAN — CRACKED (BS 750-1231) · airframe 63,633 hrs · 45,483 cycles

CRACKED RT RING PAN AFT UPPER CORNER BETWEEN BS 750-769, 1117-1136, 1136-1155, 1174-1193, 1212-1231. RING PAN RT AFT UPPER CORNER BETWEEN BS 750-769, BS 1117-1136, BS 1136-1155, BS 1174-1193, BS 1212-1231 WERE REPAIRED IAW SRM 51-30-2, 51-30-5, SRM 53-05, FIG 122, ERAS 487747-14MA, REV A, AND 493648-14MA, REV A.

Part: SEAT TRACK — CORRODED (BS 679-826) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON LT PLUG SEAT TRACK X=22, BS 579-826. PLUG WAS REMOVED, NEW PLUG WAS INSTALLED IAW SRM 51-30-1, 53-10-3 PAR 21, 14, 53-05 FIG 4A.

Part: PAN — CRACKED (BS 313-446) · airframe 63,633 hrs · 45,483 cycles

CRACKED LT RING PAN UPPER FWD CORNER BETWEEN BS 313-332 AND AFT LWR CORNER BETWEEN BS Y=427-446. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5, 51-10-3 PAR 14, 21 ON BS 427-446 AND BS 313-332 HFEC WAS ACCOMPLISHED ON RING PAN, UPPER FWD CORNER AND NOT CRACKS WERE FOUND IAW NDT SPM 06-10-01- 001, ER/A 487747-14MA, REV A, AND ER/A 493648-14MA, REV A.

Part: PAN — CRACKED (BS 579-598) · airframe 63,633 hrs · 45,483 cycles

CRACK ON LT RING PAN UPPER FWD CORNER BETWEEN BS 579 TO 598. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122, 51-10-3, PAR 14,21 AND ER/A 487747-14MA, REV A AND ER/A 493648-14MA, REV A. LONG OF CRACK IS 0.450".

Part: PAN — CRACKED (BS 984-1003) · airframe 63,633 hrs · 45,483 cycles

CRACK ON LT RING PAN UPPER AFT CORNER BETWEEN BS 984 TO 1003. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122, 51-10-3, PAR 14, 21 AND ER/A 487747-14MA REV A AND ER/A 493648-14MA, REV A.

Part: SEAT TRACK — CORRODED (BS 1288-1291) · corrosion level 2 · airframe 63,633 hrs · 45,483 cycles

CORROSION ON PLUG AT SEAT TRACK X=-22, BS 1288-1291 AT FLOOR STRUCTURE. PLUG WAS REPLACED IAW SRM 51-30-1, 51-10-3, PAR 21 AND 14 AND 53-05, FIG 4A.

Part: PAN — CRACKED (BS 807-1198) · airframe 63,633 hrs · 45,483 cycles

CRACKED RT RING PAN FWD LOWER CORNER BETWEEN BS 807-826, 1022-1041, 1079-1098. RING PAN RT FWD LWD CORNER BETWEEN BS 807-826, 1022-1041, 1079-1098 WERE REPAIRED IAW SRM 53-05, FIG 122 AND SRM 51-30-2, 51-30-05, ERA`S 493648-14MA REV A 487747-14MA, REV A.

Part: SPAR — DAMAGED (LT WING) · airframe 63,633 hrs · 45,483 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND 7 DIFFERENT FASTENERS OF THE PSE AT LT LOWER WING SKIN REAR SPAR BETWEEN BS XRS =162 TO XRS=168. THIS NRC WILL BE ATTENDED BY THE ER/A 543200-14AD. REV ORIGINAL. FROM THE SECTION II.

Part: PAN — CRACKED (BS 750-769) · airframe 63,633 hrs · 45,483 cycles

CRACK ON LT RING PAN LOWER FWD CORNER BETWEEN BS 750 TO 769. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 122, 51-10-3, PAR 14,21 AND ER/A 487747-14MA, REV A AND ER/A 493648-14MA, REV A.

Part: SKIN — WORN (RT WING TE FLAP) · airframe 63,633 hrs · 45,483 cycles

WORN INBD AFT CORNER ON RT WING OTBD FLAP OTBD GUIDE VANE. INBD AFT CORNER ON RT WING OTBD FLAP OTBD GUIDE VANE WAS REPAIRED IAW SRM 57-03D, PAR II.

Part: STRUCTURE — CRACKED (LT MLG WW) · airframe 63,475 hrs · 45,383 cycles

LEFT WHEEL WELL FWD OF GEAR DOOR BELOW GEAR DOOR SENSOR IS CRACKED. PERFORMED REPAIR IAW ERA 543814-14, REV ORIG SECTION II PERMANENT REPAIR.

Part: CHANNEL — CRACKED (DOOR FRAME) · airframe 63,475 hrs · 45,383 cycles

RIGHT WHEEL WELL DOOR JAMB CHANNEL, FWD OF GEAR DOOR CRACKED BELOW DOOR SENSOR. REMOVED WHEEL WELL DOOR JAMB CHANNEL. DRILLED UP REPLACEMENT JAMB AND BEGAN INSTALLING WHEEL WELL DOOR JAMB. PERFORMED REPAIR AS PER ERA 543814-14 REV ORIG SECTION II PERMANENT REPAIR.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 63,475 hrs · 45,383 cycles

THE AFT EQUIPMENT BAY EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE RETERMINATED 2 CONNECTORS AND THE LIGHTS CHECKED OK.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 61,859 hrs · 44,267 cycles

DURING LINE CHECK, MAINTENANCE FOUND THEY COULD NOT CONTROL THE EXTERIOR EMERGENCY LIGHTING AT THE OVERWING EXIT, IT WOULD REMAIN ON WHEN THE CONTROL SWITCH WAS TURNED OFF. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED LIGHT AND THE OPS CHECK WAS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,270 hrs · 43,879 cycles

MAINTENANCE FOUND RT AFT BATTERY POWER SUPPLY INOPERATIVE, EMERGENCY LIGHTING. BATTERY POWER SUPPLY WAS REPLACED IAW AMM 33-53.

Part: PIN — PULLED · airframe 61,025 hrs · 43,711 cycles

DURING CHECK, MAINTENANCE FOUND THE L-1 DOOR SLIDE PINS PULLED. MAINTENANCE R & R THE L-1 DOOR SLIDE.

Part: ENGINE — FAILED (NR 1) · airframe 60,914 hrs · 43,630 cycles

FLIGHT RETURNED TO DEPARTURE WITH THE NR 1 ENGINE HAVING PROBLEMS. FLIGHT CREW REPORTED ALL PARAMETERS WENT TO -0-. THE NR 2 ENGINE WAS SHUTDOWN. MAINTENANCE FOUND METAL IN TAIL PIPE AND HAVE REPLACED THE ENGINE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 59,771 hrs · 42,864 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 24DE INOPERATIVE. FOUND CONNECTOR IN THE WIRE HARNESS UNPLUGGED, CONNECTED AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 59,216 hrs · 42,484 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING FOR THE EQUIPMENT BAY IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE FOUND WIRES BROKEN AT THE TERMINAL. THEY RETERMINATED THE WIRE AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 65,201 hrs · 46,611 cycles

RADIO ALTIMETER ANTENNA DOUBLER CORRODED, NEW DOUBLER FABRICATED AND INSTALLED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,035 hrs · 41,742 cycles

DURING LINE CHECK, NOTED LT & RT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AND OPS CHECKED GOOD.

Part: COALESCER BAG — ODOR (CABIN) · airframe 56,353 hrs · 40,590 cycles

AFTER DEPARTING, DURING CLIMBOUT, THE FLIGHT RETURNED WHEN F/A REPORTED STRONG ELECTRICAL ODOR THROUGHOUT THE CABIN BUT PRIMARILY NEAR THE FWD GALLEY. PILOT REPORT ALSO INDICATES "WE SMELLED POLLEN IN COCKPIT". MX ACCOMPLISHED AN ELECTRICAL SMOKE INSPECTION IAW AMM 05-50-01, FIG 102 WITH NO TROUBLE FOUND. MX ALSO COMPLETED THE PNEUMATIC SYS DUCT BURNOUT IAW WC 7100-2619. BOTH WATER SEPARATOR COALESCER BAGS WERE REPLACED IAW WC 2120-4269. COMPLIED WITH THE PNEUMATIC DISTRIBUTION CABIN SMOKE/ODOR TROUBLESHOOTING IAW WC 2120-2367.

Part: SKIN — SCRATCHED (BS 207) · airframe 56,282 hrs · 40,547 cycles

BLEND OUT IN SKIN AT BS 207 S18L. BLEND SCRATCH, OUT OF LIMITS. REPAIRED IAW ERA 508147-14 AND SRM 53-04-5 AND 53-04-1.

Part: THRESHOLD — CORRODED (BS 1155-1212) · airframe 56,242 hrs · 40,521 cycles

DURING SCHEDULED MX, CORROSION ON CARGO DOOR THRESHOLD FROM BS 1155 - 1212. REMOVED CORROSION, FOUND TO BE IN LIMITS IAW SRM 53-01, 53-05, FIG 123, SHEET 2. R & R DAMAGED DOUBLERS, FABRICATED, AND INSTALLED IAW SRM 53-05, 51-30-4.

Part: THRESHOLD — CORRODED (BS 1179-1189) · airframe 56,242 hrs · 40,521 cycles

DURING SCHEDULED MX, CORROSION WAS FOUND AT THE AFT CARGO BAY THRESHOLD BS 1179-1189. R & R IAW SRM 53-03.

Part: THRESHOLD — CORRODED (BS 636-693) · airframe 56,242 hrs · 40,521 cycles

DURING SCHEDULED MX, CORROSION WAS FOUND ON THE MID CARGO BAY DOOR THRESHOLD PLATE AT BS 636-693. R & R CORRODED THRESHOLD PLATE IAW SRM 53-05.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,119 hrs · 40,436 cycles

DURING SERVICE CHECK, FOUND COCKPIT/L1/R1 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM. OPERATION CHECKS GOOD.

Part: SKIN — DAMAGED (BS 598-617) · airframe 56,017 hrs · 40,369 cycles

FUSELAGE SKIN DAMAGE BETWEEN STA 598 AND STA 617 AND BETWEEN STR 29R AND 27R. ACCOMPLISHED SECTION 1 TIME LIMITED REPAIR INSTRUCTION IAW ERA 511149-14, REV O. INSTALLED REPAIR IAW PERMANENT REPAIR INSTRUCTIONS ON ERA 511149-14 REV O.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 55,911 hrs · 40,304 cycles

C-1 CARGO DOOR SILL & PAN CORRODED. REPAIRED IAW SRM 53-05, FIG 44 AND ER/A 510399-14 REV ORIG.

Part: THRESHOLD — CORRODED (CARGO DOORWAY) · airframe 55,911 hrs · 40,304 cycles

CORROSION ON C-1 DOOR THRESHOLD. REPAIRED IAW SRM 53-05, FIG 44 AND ERA 510399-14 REV ORIG.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 55,911 hrs · 40,304 cycles

C-1 DOOR SURROUND STRUCTURAL PAN & LOWER SILL CORRODED. PERM REPAIR PRI 510399-14, REV 0-REV 1. FINAL ER/A 510399-14, REV ORIG ALL STEPS C/W AND MATCH PRI 510399-14, REV 0-REV 1. ER/A 510399-14 REV ORIG READ AND MATCHED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 55,214 hrs · 39,845 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY ESCAPE PATHWAY LIGHT ROW 12D INOPERATIVE. MX REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT UNDER SEAT 12D. OPS CHECKS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 54,576 hrs · 39,406 cycles

JUST PRIOR TO LEVEL OFF, THE FLIGHT CREW NOTICED A DISTINCT ELECTRICAL ODOR THROUGHOUT THE AIRCRAFT. FLIGHT ATTENDANTS AND PILOTS REPORTED MILD EYE IRRITATION. ODOR DISSIPATED AFTER 10 MINUTES AND NO SECONDARY INDICATIONS OF SMOKE OR HAZE WERE NOTED. STILL SOME VERY LIGHT ODOR 30 - 40 MINUTES AFTER INITIAL DETECTION, THEN A STRONG ODOR REAPPEARED ON APPROACH. SEEMED TO BE STRONGER IN THE BACK AND BY THE AIR CONDITIONING DUCTS AND VENTS. MAINTENANCE PERFORMED PNEUMATIC DUCT BURNOUT PER AMM.

Part: LAMP — INOPERATIVE (TAILCONE) · airframe 54,307 hrs · 39,209 cycles

FLIGHT CREW FOUND ON PDC, TAIL COMPARTMENT LIGHTS INOPERATIVE. TROUBLESHOT AND RELAMPED. OPS CHECKED GOOD.

Part: INLET — CONTAMINATED (APU) · airframe 53,800 hrs · 38,888 cycles

FLIGHT CREW REPORTED BURNING OIL SMELL IN CABIN WITH APU INLET WET AND APU LEAKING OIL. MAINTENANCE CHECKED APU FOR LEAKS AND OIL CAP SEAL CONDITION. NO LEAKS NOTED. PERFORMED DUCT BURNOUT. CLEANED INLET. AIRCRAFT OKAY FOR SERVICE.

Part: TRANS PANEL — DAMAGED (CARGO BAY) · airframe 53,766 hrs · 38,866 cycles

AFT CARGO BIN NR 6 HAS HOLE IN THE TRANSITION FLOOR AFT OF DOORWAY 3, IN BY 3/4 INCH. REPAIRED TRANSITION FLOOR PANEL UPPER SRM/DRD 53-24-0D. TIME LIMITED INSTRUCTIONS. REPAIR OF TRANSITION PANEL ACCOMPLISHED ON LOG # 244776006.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 56,242 hrs · 40,521 cycles

PUNCTURE HOLE AT TRANSITION FLOOR PANEL IN AFT BAG BIN. PUNCTURE IS 3 X 1.75. FABRICATED FWD CARGO BAY FLOOR PANEL NR 121NF, FROM 5040-400005GC2 ALUMINUM COMPOSITE LOT 1063129 IAW SRM 51-10-11, FIG 1 AND INSTALLED IAW AMM 25-52-01-201, SECT. 3. B. (1)(5). SHOULD READ AFT CARGO BAY FLOOR PANEL NR 181JF.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,256 hrs · 38,553 cycles

FUSELAGE SKIN CRACKED AT STA 1418 S-2R. CRACK EMANATING AFT OF THE UPPER MOST FASTENER HOLE COMMON TO SHEAR TIE. REPAIRED PER ERA 498486-14 REV ORIG.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,479 hrs · 38,022 cycles

DURING SERVICE CHECK, FOUND LARGE DENT APPROXIMATELY 39 INCHES AFT OF L1 DOOR, 1 FOOT ABOVE FLOOR LINE. REPAIRED IAW SRM 53-02, FIG 18C ON N/R CARDS 1-6.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,475 hrs · 38,017 cycles

DURING SVC CHECK FOUND LARGE DENT APPROX 39 INCHES AFT OF L1 DOOR AT EXISTING REPAIR. REPAIRED PER SRM 53-04D FIG 12C.

Part: LANYARD — OUT OF POSITION (L2 DOOR SLIDE) · airframe 50,804 hrs · 36,924 cycles

DURING LINE CHECK MX FOUND L2 DOOR SLIDE LANYARD INSTALLED IMPROPERLY. MX REPOSITIONED DOOR SLIDE LANYARD IAW AMM 25-62-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 50,333 hrs · 36,628 cycles

FLIGHT CREW DIVERTED ACFT DUE TO AFT LAVATORY SMOKE DETECTORS SOUNDING WITH LIGHT HAZE AND ODOR IN THE CABIN. MX COMPLIED WITH OPN 5088 - AND NO TROUBLE WAS FOUND. BORESCOPED BOTH ENGINES - NO ISSUES. RAN ENGINES FOR 20 MINUTES AT POWER - NO SMOKE OR ODORS. PERFORMED DUCT BURNOUT AND REPLACED AFT SMOKE DETECTOR. OK FOR SERVICE.

Part: OIL SYSTEM — LEAKING (APU) · airframe 50,327 hrs · 36,622 cycles

DURING CLIMBOUT, BOTH OF THE AFT LAVATORIES SMOKE DETECTORS ALARMS SOUNDED WITH LIGHT HAZE AND ODOR IN THE AFTCABIN. CLEARED AND ALARMS STOPPED WHEN CLIMBING THROUGH 12K FT SO FLIGHT CONTINUED TO DESTINATION. UPON ARRIVAL, MX FOUND THE APU LEAKING OIL AND REPLACED THE APU. MX PERFORMED OPS 5089 DUCT BURN OUT AND REPLACED BOTH COALESCER BAGS.

Part: SKIN — GOUGED (STA 313-335) · airframe 49,019 hrs · 35,786 cycles

FOUND 22 INCH GOUGE WITH CREASE ON LT SIDE OF FUSELAGE AT STA 313-335. FINGER DOUBLER WAS REMOVED IAW SRM 53-04D FIG 12B. NEW FINGER DOUBLER WAS FABRICATED IAW SRM 53-04D FIG 12B AND SRM 51-10-3 PAR 14 AND 23. FINGER DOUBLER WAS INSTALLED IAW SRM'S 51-30-2 AND 51-30-5.

Part: SKIN — CORRODED (STA 1209) · airframe 49,019 hrs · 35,786 cycles

EXFOLIATION CORROSION ON INNER FUSELAGE SKIN STA Y=1209 BTW LONGERONS 30 AND 29RT. CORROSION WAS REMOVED AND REPAIR PIECES WERE FABRICATED AND INSTALLED IAW ERA480772-14 REV ORIG.

Part: SUPPORT — CORRODED (STA 1350) · airframe 49,019 hrs · 35,786 cycles

EXFOLIATION CORROSION ON SUPPORT UNDER LOWER DOOR JAMB OF VENTRAL DOOR BTW X=4 TO X=10VAT STA Y=1350. DAMAGE WAS REMOVED AND REPAIR PARTS WERE FABRICATED, TREATED, AND INSTALLED IAW ERA 480767-14 REV ORIG.

Part: SKIN — DAMAGED (LT ELEVATOR TAB) · airframe 49,019 hrs · 35,786 cycles

LIGHTNING STRIKE DAMAGE ON LT ELEVATOR GEARED TAB T/E. LT ELEVATOR GEARED TAB T/E WAS REPAIRED IAW SRM 55-04 PAR 34 AND OPN 1031 CARD 1213-1221.

Part: FITTING — CORRODED (MLG SUPPORT FITT) · airframe 49,019 hrs · 35,786 cycles

PITTING CORROSION ON LT GEAR SUPPORT FITTING BUSHING BORE. LT GEAR SUPPORT FITTING BUSHING BORE WAS MACHINED TO CLEAN UP CORROSION IAW ERA 480222-14AD REV ORIG. FINAL SIZE ID 2.535. FLOURESCENT DYE INSP PERFORMED IAW EA 09-093855-03 AD OPN 0104 PAR J NOTE A. NO CRACKS NOTED. BORE TREATED IAW ERA 480222-14AD.

Part: SUPPORT — SCRATCHED (RT MLG) · airframe 49,019 hrs · 35,786 cycles

SCRATCHES ON TRANSITION STEP OF RT GEAR SUPPORT BUSHING BORE. RT MLG SUPPORT BUSHING BORE WAS MACHINED AT TRANSITION STEP TO CLEAN UP DAMAGED SURFACE IAW ERA 480222-14AD REV ORIG. REMAINING WALL THICKNESS BETWEEN BUSHING AND BEARING 1.223, BEARING BORE ID 2.316. FLOURESCENT DYE INSP PERFORMED IAW EA 09-093855-03 AD OPN 0204, PAR J, NOTE A. NO CRACKS NOTED. RT GEAR SUPPORT BUSHING WAS FAB & INST IAW DWG 4935859, EA 09-093855-03 AD OPN 0204 AND DWG AMR0957288 AND ERA480222-14AD REV ORIG.

Part: BEAM — CORRODED (C2 DOOR FRAME) · airframe 49,019 hrs · 35,786 cycles

EXFOLIATION CORROSION OVER BEAM OF C2 LOWER DOOR JAMB. FASTENERS WERE REMOVED IAW SRM 51-30-5. CORROSION REMOVED IAW SRM 51-10-3 PAR 26. THICKNESS FOUND OUT OF LIMITS IAW SRM 53-05 FIG 123 SHEET 2. REPAIR DOUBLERS, FILLER AND SPACER WERE FABRICATED AND INSTALLED IAW SRM'S 53-05, FIG 123 SHEET 3 AND 51-10-3 P 14-21.

Part: BEAM — CORRODED (C3 DOOR FRAME) · airframe 49,019 hrs · 35,786 cycles

EXFOLIATION CORROSION ON UPPER SURFACE OF AFT CARGO COMPARTMENT DOOR JAMB BEAM. CORROSION WAS REMOVED IAW SRM 51-10-3 PAR 26 AND AREA WAS FOUND OUT OF LIMITS IAW SRM 53-05 FIG 123 SHEET 2. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM'S 53-05 FIG 123 AND 51-10-3.

Part: UNKNOWN — DAMAGED (BS 632-679) · airframe 48,471 hrs · 35,478 cycles

FUSELAGE DAMAGE LT SIDE STA 632.5/660.5/679. REPAIRED IAW ERA 478513-14.

Part: SENSOR — DAMAGED (SLATS) · airframe 44,081 hrs · 32,781 cycles

SLAT DISAGREE LIGHT AT LANDING, ON GO-AROUND INDICATIONS NML AT FLAPS 15. RECONFIG AND SLATS NML AT FLAPS 23 AND 28. OPS CHECKS NML ALL CONFIGS. CHECKED CABLE DRUM, OK. FOUND D1-65 SENSOR DAMAGED. REPLACED SENSOR, CHECKS GOOD.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 41,338 hrs · 31,150 cycles

RT HORIZONTAL STABILIZER SKIN WAS FOUND CRACKED IN UPPER SKIN, 0.75 IN. LONG. THE CRACK WAS CUT OUT OF THE SKIN AND A NEW SKIN WILL BE INSTALLED WITHIN 2000 FLIGHT HOURS.

Part: RESERVOIR — LEAKING (LEFT) · airframe 37,980 hrs · 28,889 cycles

LEFT SYSTEM HYDRAULIC PRESSURE WENT TO -0- QUANTITY WAS NORMAL IN FLIGHT. REPLACED LEFT SYSTEM RESERVOIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,387 hrs · 26,259 cycles

SKIN DENTED AT STATION 389 BELOW LONGERON 23L. AREA REPAIRED IAW ERA 090912-14.

Part: CHARGER — UNSERVICEABLE (E/E BAY) · airframe 33,677 hrs · 25,754 cycles

SMOKE FROM DRAIN HOLE OF E & E COMPARTMENT. FOUND BATTERIES BEING OVERCHARGED. REPLACED LEFT AND RIGHT BATTERIES, BATTERY CHARGER AND BATTERY CHARGER CIRCUIT BREAKER AS PER AMA BULLETIN 04-T1. PERFORMED BATTERY CHARGER SYSTEM TEST PER M/M 24-30-02-201, CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,626 hrs · 24,359 cycles

OVERWING EMERGENCY LTS COME ON WHEN COCKPIT EMERGENCY LIGHT SWITCH IS PLACED IN THE OFF POSITION. REPLACED OVERWING EMERGENCY LIGHT BATTERY RACK. OPS NML.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,626 hrs · 24,359 cycles

OVERWING EMERGENCY LTS. COME ON WHEN COCKPIT EMERGENCY LIGHT SWITCH IS PLACED IN THE OFF POSITION. REPLACED OVERWING EMERGENCY LIGHT BATTERY RACK-OPS NORMAL.

Part: BATTERY — DISCHARGED (OVERWING LIGHTS) · airframe 30,531 hrs · 23,600 cycles

RT AND LT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED OVERWING EMERGENCY LIGHT POWER SUPPLY BATTERY AND R2-271 RELAY.

Part: PACKING — LEAKING (NR 2 ENGINE) · airframe 27,937 hrs · 21,743 cycles

RIGHT HYD QTY FELL TO 1 QUART. TURNED OFF RT SYSTEM. FOUND RT FWD OUTBOARD MODULE FITTING LEAKING FROM PACKING. REPLACED PACKING.

Part: TURBINE — FAILED (NR 2 ENGINE) · airframe 27,812 hrs · 21,653 cycles

IN CRUISE AT 28K FEET HEARD BANG ON RT SIDE. RIGHT ENGINE SHUT DOWN. CREW WENT THROUGH POM PROCEDURE, FUEL LEVER OFF. THEN NOTICED OIL PRESS AND QTY AT ZERO. DID NOT TRY RESTART. WINDMILLED FOR APPROX 20 MINUTES WITH NO OIL PRESSURE. ON INSPECTION MTC FOUND TURBINE FAILED, WAS CONTAINED. ENGINE CHANGE.

Part: HARNESS — OPEN (10DE) · airframe 27,600 hrs · 21,491 cycles

EMERGENCY PATH LIGHT AT SEAT 10DE INOP. FOUND WIRE AT SEAT HARNESS BROKEN. RPLD PATH LIGHT SEAT WIREHARNESS. LIGHT CKS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 25,114 hrs · 19,666 cycles

FIRST CLASS EMERGENCY TRACK LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY PACK. NOW CHECKS OK.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,604 hrs · 19,314 cycles

ONE EMERGENCY FLASHLIGHT AFT CABIN RED LIGHT NOT FLASHING. REPLACED FLASHLIGHT.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 24,344 hrs · 19,119 cycles

FOUND EMERGENCY CABIN FLOOR LIGHTING INOP AT F/C SEATS. REPLACED EMERGENCY LIGHT POWER SUPPLY. EMERGENCY LIGHTS TEST NORMAL.

Part: DUCT — DISLODGED (APU BAY) · airframe 24,235 hrs · 19,030 cycles

APU FIRE WARNING OFF/AGENT, BOTTLES DISCHARGED. REPLACING FIRE BOTTLES, FOUND APU SURGE VALVE DUCT CLAMP AND BOOT BLOWN OFF. HOT SURGE AIR CAUSED FIRE INDICATION. REPLACED BOOT AND LEAK CHECKED. REPLACED FIRE BOTTLES. A/C RETURNED TO SERVICE.

Part: DUCT — RUPTURED (APU) · airframe 24,206 hrs · 19,016 cycles

APU FIRE WARNING SOUNDED WHILE AT GATE RUNNING APU FOR 5 MIN WITH GEN AND PACKS ON. CREW SHUTDOWN APU AND FIRED NR 1 EXTINGUISHER. FOUND FLEX COUPLING AT SURGE CONTROL VALVE BLOWN. REPLACED NR 1 FIRE EXTINGUISHER AND PUT APU ON MCO 49-00-01A.

Part: SLIDE — DEPLOYED (TAIL CONE)

TAIL CONE AND SLIDE FOUND DEPLOYED. REPLACED SLIDE AND REINSTALLED TAIL CONE. DEPLOYMENT WAS SUCCESSFUL.

Part: BATTERY PACK — DISCHARED (CABIN)

EMERGENCY EXIT TRACK LIGHTS (FLOOR) INOP IN FIRST CLASS CABIN. REPLACED BATTERY PACK AND PWR SUPPLY, LIGHTS CK OK.

Part: SLIDE — FAILED (AFT GALLEY)

AFT GALLEY DOOR SLIDE DID NOT DEPLOY WHEN DOOR WAS OPENED ACCIDENTLY SLIDE WAS ARMED. REPLACED DOOR SLIDE.

Part: HYD PUMP — FAILED (NR 1 ENGINE)

HYD PRESS ON LEFT SIDE DECREASED DURING CLIMBOUT. DID CHECKLIST, PRESS OK W/AUX TRANS PUMP ON. REPLACED LT ENG DRIVEN PUMP AND FILTER PRESS AND LEAK CKD GOOD ON ENG RUN.

Part: TE SKIN — CRACKED (RUDDER TAB)

DURING SHOP INSPECTION, RUDDER TAB WAS FOUND WITH 2 CRACKS ON THE TRAILING EDGE. ONE WAS 7 INCHES LONG AT 30 INCHES FROM THE TOP, THE OTHER WAS 2 INCHES LONG AT 3 INCHES FROM THE BOTTOM. REPAIRED CRACKS PER SRM 51-70-1A, NR 18 1A NR 18.

Part: PAN — GOUGED (AFT CARGO DOOR)

DURING C-2 LETTER CHECK, C-3 BAG BIN DOOR AFT PAN GOUGED AT HOLD OPEN. REPAIRED PER SRM 52-05 FIG 27 SH 1-3.