N989DL

Part: UNKNOWN — ODOR (CABIN) · airframe 68,580 hrs · 49,642 cycles

SHIP 0989 - FUME/DIV - CLIMBING THROUGH 15,00 FEET FLIGHT ATTENDANT REPORTED STRONG BURNING SMELL AROUND DOOR 2L. NO VISIBLE SMOKE AND SMELL DISSIPATED BY TOP OF CLIMB. QRH WAS REFERENCED AND ALTHOUGH THE FUMES DECREASED, CAPTAIN AND DISPATCH DECIDED TO DIVERT TO RDU. CORRECTIVE ACTION: COMPLIED WITH MD88 NOGO ODI PROCEDURE WC 2120-2367. APU INLET CLEAN. RAN PACKS WITH APU AND ENGINES. NO SMELL DETECTED. INSPECTED LIGHTS AND AREAS ABOVE PSUS AND CABIN CEILING PANELS. ALL ELECTRICAL COMPONENTS AND WIRING IN DOOR 2L AREA NORMAL. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS. NO TROUBLE FOUND. (LP4807398

Part: FAIRING — MISSING (TE FLAP) · airframe 68,229 hrs · 49,322 cycles

LT WING NR 1 FLAP SECONDARY FAIRING MISSING. FWD TO CDL 57-50-03. PLAC INSTALLED. DISP. APPROVED. REPORTED DUE TO FACT THAT PART MAY HAVE DEPARTED AIRCRFAT IN FLIGHT. (LP5353136)

Part: FAIRING — MISSING (TE FLAP) · airframe 68,229 hrs · 49,322 cycles

RT WING NR 1 FLAP SECONDARY FAIRING MISSING. FWD TO CDL 57-50-03. PLAC INSTALLED. DISP. APPROVED. REPORTED DUE TO POSSIBILITY OF PART COMING OFF OF AIRCRAFT DURING FLIGHT. (LP5353137)

Part: LANYARD — WORN (SLIDE) · airframe 65,874 hrs · 47,487 cycles

LANYARD WORN ON TAIL SLIDE. REPLACED THE LANYARD IAW ERA 562889-14AD.

Part: HANDLE — OUT OF ADJUST (TAILCONE) · airframe 65,874 hrs · 47,487 cycles

DURING FUNCTIONAL CHECK OF TAIL CONE RELEASE SYSTEM FOUND AFT ENTRY DOOR NORMAL OPERATING HANDLE AND EMERGENCY OPERATING HANDLE HARD TO OPEN AND CLOSE. DOOR CENTERING ADJUSTMENT C/W ON N/R 282.

Part: CABLE — FRAYED (TAILCONE RELEASE) · airframe 65,874 hrs · 47,487 cycles

FRAYED TAILCONE RELEASE CABLE, TWELVE O'CLOCK. REPLACED THE CABLE AND ADJUSTED AS NECESSARY IAW AMM 53-53-00.

Part: CABLE — FRAYED (TAILCONE RELEASE) · airframe 65,874 hrs · 47,487 cycles

FRAYED TAIL CONE RELEASE CABLE, AT THE 10 O'CLOCK POSITION. REPLACED THE CABLE AND ADJUSTED AS NECESSARY IAW AMM 53-53-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,423 hrs · 47,112 cycles

SKIN DAMAGE AT STA 313 L-23L TO L-25L. CUT OUT DAMAGED SECTION 15 3/16" BY 32 1/2" AND REPAIRED FUSELAGE SKIN AT STA 313 L23L TO L25L IAW SRM 53-04 FIG 12C AND ERA 556439-14 REV O AND ERA 560498-14 REV O.

Part: LONGERON — DENTED (FUSELAGE) · airframe 65,423 hrs · 47,112 cycles

FUSELAGE BS 313 LONGERON 23L UPPER FLANGE IS DENTED IN. CUT OUT DAMAGED SECTION 57.24" AND REPAIRED LONGERON AT STA 285 TO 342 L23L IAW SRM 53.02 FIG 18.

Part: LONGERON — DEFORMED (FUSELAGE) · airframe 65,423 hrs · 47,112 cycles

DAMAGE (DEFORMATION) TO LONGERON AT STA 313 L-24L. REMOVED AND REPLACED PREVIOUSLY REPAIRED LONGERON SECTION AND 2 EACH SPLICES STA 313 L-24L IAW SRM 53-02 FIG 18.

Part: FORMER — CRACKED (FUSELAGE) · airframe 65,423 hrs · 47,112 cycles

CRACKED FORMER AT SAT 313 L-24L. REMOVED DAMAGED FORMER STA 313 L-26L TO L-22L FABRICATED NEW FROM 2024.0 .050 HEAT TREATED TO 2024-T42 AND INSTALLED NEW FORMER SECTION IAW MD-88 SRM 53-03 D FIG 3 SRM 51-30-05 AND DWG 9911526 REV AZ.

Part: SPRING — BROKEN (DOOR) · airframe 64,095 hrs · 46,189 cycles

AFT DOOR EMERGENCY RELEASE MECHANISM SPRING BROKEN. REINSTALLED NEW SPRING.

Part: LIGHT — INOPERATIVE (SEAT 23E) · airframe 62,435 hrs · 44,995 cycles

SEAT 23E EMERGENCY AISLE SEAT LIGHT INOPERATIVE. R & R SEAT 23E EMERGENCY AISLE SEAT LIGHT ASSY IAW AMM 33-53.

Part: LIGHT — INOPERATIVE (ROW 15) · airframe 61,920 hrs · 44,621 cycles

MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT ROW 15 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY.

Part: SKIN — DENTED (RT WING SLAT) · airframe 61,042 hrs · 44,016 cycles

RIGHT WING L/E AT MID POINT SLAT NR 3, FOUND DENT ON POST FLIGHT. REMOVED NR 3 SLAT IAW CARD 2700-4224-RH-03. OK TO INSTALL SLAT. COMPLETED INSTALLING SLAT IAW CARD 2700-4224, RH-03.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 60,811 hrs · 43,851 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF RT WING ACCESS PANEL 1436C. THE ACCESS PANEL WAS REPLACED.

Part: BUSHING — CORRODED (RT WING) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION AND ELONGATED BUSHING ON T/E OF HEATER BLANKET PANEL AT RT WING. ELONGATED BUSHING WERE ATTENDED WITH NRC 2000075937, CARD NR 10, ZONE 14 AND ER/A 537776-14AD, REV A AND ETI-88-15-316, REV 4.

Part: STRUCTURE — CRACKED · airframe 60,690 hrs · 43,756 cycles

ACFT HAS A CRACK ON CENTER FUEL TANK STRINGER ENDS 15 AND 16. STRINGERS ENDS 15 AND 16 WERE REPLACED IAW SRM 51-30-5 , 51-30-1 AND DWG 5935855.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON RT UPPER HEATER BLANKET ACCESS PLATE CUTOUT EDGE NR 1409C AND 1410C AT RT WING. DUE TO EXCESSIVE DAMAGE ON HEAT BLANKET PANEL WAS REPLACED IAW AMM 30-80-02.

Part: LONGERON — CRACKED · airframe 60,690 hrs · 43,756 cycles

CRACKED LONGERON 15 AND XCW=18 INSIDE OF CENTERTANK, RT SIDE. CRACK ON LONGERON 15 WAS REPAIRED IAW ER/A 537768-14, REV ORIGINAL AND 537774-14, REV ORIGINAL REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE FROM DATE OF FAA APPROVAL ONLY.

Part: LONGERON — CRACKED · airframe 60,690 hrs · 43,756 cycles

CRACKED LONGERON 16 AND XCW 18 INSIDE OF CENTER TANK RT SIDE. CRACK ON LONG 16 WAS REPAIRED IAW ER/A 537768-14, REV ORIGINAL AND 537774-14 REV ORIGINAL. REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE FROM DATE OF FAA APPROVAL ONLY.

Part: SKIN — DAMAGED (RT WING) · airframe 60,690 hrs · 43,756 cycles

ELONGATED HOLES ON RT WING UPPER SKIN AFT EDGE HEATER BLANKET AREA. ELONGATED HOLES WERE PERFORMED WITH ER/A 537776-14AD, REV A AND ETI 88-15-316.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON LT UPPER HEATER BLANKET ACCESS PLATE CUTOUT EDGE NR 1303C AND 1307C AT LT WING. DUE TO EXCCESIVE DAMAGE ON HEATER BLANK PANEL WAS REPLACED IAW AMM 30-80-02.

Part: ACCESS PANEL — DELAMINATED (LT WING) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

ACFT HAS CORROSION AND DELAMINATION ON LT SECONDARY ACCESS PANELS NR 1303C AND 1307C AT LT WING. ACCESS PLATE 1307C WAS REPAIRED IAW ERA 530866-14AD, REV ORIGINAL AND ACCESS PLATE 1303C WAS REPLACE DUE TO EXCESSIVE DAMAGE.

Part: SKIN — DAMAGED (BS 1231-1250) · airframe 60,690 hrs · 43,756 cycles

ACFT AD INITIAL, LIGHTNING STRIKE ON RT FUSELAGE WINDOW BELT SKIN UPPER AFT CORNER BETWEEN BS 1231-1250. AREA WAS REPAIRED IAW ER/A 537761-14AD, REV ORIGINAL AND SRM 51-10-3, PAR 14, 21, AND SRM 51-30-5.

Part: FRAME — CORRODED (BULKHEAD) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION FOUND ON AFT PRESSURE BULKHEAD LOWER FRAME. REPLACED IAW SRM 53-03 FIG 37 , 51-10-3, 51-30-5, 51-30-2, 51-30-1 AND ER/A 537800-14.

Part: CARGO TRACK — CORRODED (BS 1003-1322) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

THE CARGO TRACK HAS CORROSION BETWEEN BS 1003 - 1322. REPLACED IAW SRM 51-30-1.

Part: ACCESS PANEL — DELAMINATED (RT WING) · airframe 60,690 hrs · 43,756 cycles

DELAMINATION ON RT SECONDARY ACCESS PANEL 1410C ON RT WING. THE ACCESS PANEL WAS REPAIRED IAW ERA NR 530866-14MA REV ORIGINAL.

Part: SKIN — DAMAGED (BS 400) · airframe 60,690 hrs · 43,756 cycles

ACFT HAD LIGHTNING STRIKE FUSELAGE BS 400 LONGERONS 1-2R. LONGERON AND SKIN WAS REPAIRED WITH PERMANENT REPAIR IAW SRM 53-04-2, FIG 2, SHEET 26 AND 53-02, FIG 18.

Part: STIFFENER — CRACKED (BS 1338) · airframe 60,690 hrs · 43,756 cycles

ACFT HAS A CRACK ON STIFFENER END, BETWEEN PROJECTION LONGERON 12LT AND 11LT AT PRESSURE BULKHEAD BS 1338. STIFFENER END WAS REPLACED IAW SRM 51-30-1, 51-30-5, SRM 51-10-4, AND 51-10-3 PAR 14, 21.

Part: SKIN — CRACKED (BS 1437) · airframe 60,690 hrs · 43,756 cycles

CRACKED FUSELAGE SKIN, BS 1437 BETWEEN LONGERONS 2 - 3R. SKIN WAS REPAIR IAW ERA 537758-14, REV ORIGINAL.

Part: SKIN — CRACKED (BS 1418) · airframe 60,690 hrs · 43,756 cycles

CRACKS ON FUSELAGE SKIN, LENGTH 0.156" AND 0.125", ON BS 1418 BETWEEN LONGERON 2L AND 3L AND BETWEEN LONGERON 2R AND 3R, LENGTH .156". IN SAME STATION REASON FOR RE-WRITE : SHIMS BELOW LONGERON AFT STRAPS 2L, 2R DOES NOT COVER THE ENTIRE AREA OF INTENDED CONTACT. SHIMS WERE REPLACED IAW ER/A 537756-14AD, REV ORIGINAL, SRM 51-30-5, 51-10-3 PAR 14 AND 21, 51-10-9 THE MAINTENANCE REQUIREMENTS WILL BE PERFORMED UNDER LOG 2117450. CRACKS ON FUSELAGE SKIN WAS REPAIRED IAW ER/A 537756-14AD REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION WAS FOUND ON THE COUNTERSINK OF THE ACCESS PANEL 1335C. THE ACCESS PANEL WAS REPLACED.

Part: DOUBLER — CORRODED (BS 1315) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

ACFT HAS CORROSION ON PRODUCTION DOUBLER CUTOUT OF AFT LAVATORY SERVICE PANEL AT LONGERON 22L, BS 1315. COMPLIED WITH STEPS 1-5 OF ERA 538253-14, REV ORIGINAL.

Part: DUCT — CRACKED (RADIO RACK) · airframe 60,690 hrs · 43,756 cycles

RADIO RACK COOLING EXHAUST DUCT CRACKED. REPAIRED IAW ER/A 464964-14MA, REV C.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

HAS CORROSION ON COUNTERSINK AND ELONGATED HOLES OF FUEL ACCESS PLATE NR 1373C. ACCESS PLATE 1373C WAS REPLACE AND WILL INSTALL UNDER CARD 2800-0120.

Part: ACCESS PANEL — DAMAGED (RUDDER) · airframe 60,690 hrs · 43,756 cycles

ACFT HAS DAMAGED METALIZED ON ACCESS PLATE 6502A. ACCESS PLATE 6502A WAS REPAIRED IAW SRM 51-70-1A, PAR 23.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

HAS CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1414C. FUEL ACCESS 1414C WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0340.

Part: ACCESS PANEL — CRACKED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK, WEAR AND CRACK SUPPORT ON FUEL ACCESS PANEL 1361C. THE ACCESS PANEL WAS REPLACED.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 60,690 hrs · 43,756 cycles

ACFT HAS A DELAMINATED INBD FLAP OTBD GUIDE VANE LOWER AND UPPER SKIN LT WING. DUE TO SEVERAL DAMAGE INBD FLAP OTBD GUIDE VANE WAS REPLACE WITH REPAIRED INBD FLAP OTBD GUIDE VANE.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION FOUND ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS NR 1311C. FUEL ACCESS NR 1311C WAS REMOVED AND WILL BE INSTALLED UNDER CARD 2800-0120.

Part: SKIN — CRACKED (BS 1418) · airframe 60,690 hrs · 43,756 cycles

ACFT HAS CRACKS ON FUSELAGE SKIN, LENGTH 0.156"AND 0.125", ON BS 1418 BETWEEN LONGERON 2LT AND LONG 3LT. 1 CRACK ON FUSELAGE SKIN, LENGTH 0.156", ON BS 1418 BETWEEN LONGERON 2RT AND LONG 3RT, CARD 8, ZONE 65. CRACKS ON FUSELAGE SKIN WERE REPAIRED IAW ER/A 537756-14 AD, REV ORIGINAL.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION FOUND ON REPAIR OF FRAME, BS 1309 BETWEEN LONGERON 28R & 28L . REPAIR REPLACED IAW SRM 53-03D, FIG 2A, 51-30-2, 51-30-5 & 51-10-3.

Part: LONGERON — CRACKED (BS 1429) · airframe 60,690 hrs · 43,756 cycles

ACFT HAS A CRACK ON LONGERON 3RT AND BS 1429 AT AFT ACCESSORY COMPARTMENT. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: SCOOP — CRACKED (VERTICAL STAB) · airframe 60,690 hrs · 43,756 cycles

ACFT HAS A CRACK ON VERTICAL STABILIZER INTAKE AIR SCOOP LT SIDE APPROXIMATELY BS Y=1478. CRACK ON VERTICAL STABILIZER INTAKE AIR SCOOP LT SIDE APPROXIMATELY BS=Y=1478 WAS REPAIRED AND FPI WAS ACCOMPLISHED AND WELDED AREA OF INTAKE AIR SCOOP LT SIDE NO CRACKS WERE FOUND IAW ER/A 420329-14MA, REV C. PERFORM REPETITIVE VISUAL INSPECTIONS WITHIN EVERY "C"-CHECK, LIMIT 4000 FLIGHT HOURS OR 547 DAYS IAW ER/A 420329-14MA, REV C.

Part: SKIN — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

ACFT HAS CORROSION AND DELAMINATION OTBD FLAP MID GUIDE FLAP VANE LOWER SKIN AT LT WING. DUE TO SEVERAL DAMAGE OTBD FLAP MID GUIDE VANE FLAP AT LT WING WAS REPLACED WITH REPAIRED MID GUIDE VANE AND WILL BE INSTALLED WITH CARD 5730-0631.

Part: BEAM — CORRODED (BS 1155-1212) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

FOUND CORROSION ON REPAIR DOUBLER OF THE LOWER DOOR FRAME BEAM BETWEEN BS 1155 - 1212. SPACER WAS REPLACED IAW SRM 53-05, FIG 123, 51-30-5 AND 51-10-3 PAR.14, 21 AND 38.

Part: FRAME — WORN (BS 1510) · airframe 60,690 hrs · 43,756 cycles

FOUND WEAR ON LT LOWER FRAME, BS 1510, BELOW SERVICE LIGHT SWITCH AT AFT ACCESSORY COMPARTMENT. FRAME WAS REPLACED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.

Part: FRAME — CRACKED (BS 1510) · airframe 60,690 hrs · 43,756 cycles

ACFT HAS A CRACK ON FRAME BS 1510. THE FRAME WAS R & R IAW SRM 51-30-2, 51-10-4 AND 51-10-3.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

ACFT HAS CORROSION ON RT BARREL NUT HOLES ON HORIZONTAL STABILIZER. REPAIRED IAW ER/A 537764-14, REV ORIG.

Part: PAN — CRACKED (BS 426) · airframe 60,690 hrs · 43,756 cycles

FOUND A CRACK ON PAN BETWEEN BS 426 AND BEAM 5. REPAIRED IAW ER/A 537772-14, REV: ORIGINAL.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION FOUND ON THE HORIZONTAL STAB. REPAIRED IAW ERA 537766-14, REV ORIGINAL.

Part: FLOOR PANEL — BROKEN (NOT REPORTED) · airframe 60,690 hrs · 43,756 cycles

ACFT HAS A BROKEN FLOOR PANEL. FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: SEAT TRACK — CORRODED (BS 795-797) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION FOUND ON THE SEAT TRACK FROM BS 795 - 797 AND LBL 54. THE SEAT TRACK WAS REPAIRED IAW SRM 53-05 FIG 4F.

Part: STUD — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION WAS FOUND ON THE UPPER STUDS OF RT WING OTBD FLAP HINGE XW 333. THE STUDS WERE REPLACED IAW AMM 57-40-01-201.

Part: SCOOP — CRACKED (INTAKE) · airframe 60,706 hrs · 43,767 cycles

A CRACK FOUN ON WELD OF VERTICAL STABILIZER INTAKE AIR SCOOP APPROXIMATELY BS ZFS=11.562. CRACKS ON VERTICAL STAB INTAKE AIR SCOPP APPROXIMATELY STA ZFS 11.562 WERE WELDED AND FPI WAS ACCOMPLISHED ON WELDED AREAS AND NO CRACK WERE FOUND IAW MD SRM 55-05 PAR 4C.

Part: FLOOR PANEL — BROKEN (NOT REPORTED) · airframe 60,690 hrs · 43,756 cycles

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

Part: STIFFENER — CRACKED (BS 1338) · airframe 60,690 hrs · 43,756 cycles

CRACK FOUND ON STIFFENER END BETWEEN LONGERONS 16 - 17L PRESSURE BULKHEAD BS 1338. STIFFENER WAS REPLACED IAW SRM 51-30-1, 51-30-5, 51-30-4, 51-10-3 PAR 14 AND 21 AND DWG 9915558, REV BA.

Part: FLOOR PANEL — WORN (NOT REPORTED) · airframe 60,690 hrs · 43,756 cycles

WEAR FOUND ON FERRULE OF FLOOR PANEL. THE FLOOR PANEL WAS REPLACED IAW AMM 53-20-01-201, PAR 7.C.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION FOUND ON HORIZONTAL STABILIZER. HORIZONTAL STABILIZER WAS REPAIRED IAW ERA 537754-14, REV ORIGINAL AND SRM 55-03, PAR 30.

Part: SCOOP — CRACKED (INTAKE) · airframe 60,706 hrs · 43,767 cycles

A CRACK WAS FOUN ON WELD OF VERTICAL STAB INTAKE AIR SCOOP APPROXIMATELY BS ZFS=4.75 UPPER/ AFT EDGE. CRACKS ON VERTICAL STAB. INTAKE AIR SCOOP APPROXIMATELY BS ZFS 4.75 AFT EDGE WERE WELDED AND FPI WAS ACCOMPLISHED ON WELDED AREAS AND NO CRACKS WERE FOUND IAW 55-05, PAR.4C.

Part: INTERCOSTAL — CRACKED (BS 1476) · airframe 60,690 hrs · 43,756 cycles

CRACKED INTERCOSTAL BS 1476 AND LONGERON 20L. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-01, FIG 2, SHEET 3, 51-30-2, 51-30-5.

Part: SKIN — DAMAGED (RUDDER FAIRING) · airframe 60,690 hrs · 43,756 cycles

DAMAGE METALLIZED ON FAIRING OF RUDDER. FAIRING OF RUDDER WAS REPAIRED IAW SRM 51-70-1A, PAR 23.

Part: ANGLE — CRACKED (BS 1463) · airframe 60,690 hrs · 43,756 cycles

A CRACK WAS FOUND ON DORSAL ANGLE BS 1463. THE ANGLE WAS REPAIR IAW SRM 53-05, FIG 23.

Part: SEAT TRACK — CORRODED (BS 727-730) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION FOUND ON RT SEAT TRACK X-54 AND BETWEEN BS BS 727 - 730. REPAIRED IAW SRM 53-05, FIG 4A.

Part: FLOOR SUPPORT — CORRODED (BS 1155) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION FOUND ON FLOOR SUPPORT 1155 BETWEEN LONGERON 28 -29R ABOVE DOOR FRAME WEB. CORROSION WAS REMOVED IAW SRM 51-10-3 PAR. 21, 14, 26, 38 AND FOUND OUT LIMITS AND WAS REPLACED IAW DWG 5936660, REV B2.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 60,690 hrs · 43,756 cycles

DELAMINATION AT FLOOR PANEL. THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: ANGLE — CORRODED (BS 1338) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION FOUND ON THE AFT CARGO BAY PRODUCTION DOUBLER ANGLE BS 1338 BETWEEN LONGERONS 28R TO 28L. THE DOUBLER ANGLE WAS REPAIRED IAW DWG 9915561, REV C, G, SRM 51-30-1, 51-30-2, 51-30-5 AND 51-30-3.

Part: LONGERON — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION FOUND ON REPAIR OF LONGERON 29R BETWEEN BS 1287 - 1309. REPAIR WAS REPLACED IAW SRM 53-02, FIG 19, SHEET 2, SRM 51-30-5 AND 51-10-3, PARS 14, 21 AND 38.

Part: SEAT TRACK — CORRODED (BS 450) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION FOUND ON RT SEAT TRACK X-54, BS 450. REPAIRED IAW SRM 53-05, FIG 4A.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 60,690 hrs · 43,756 cycles

A CRACKED WEB AT BS 430 BETWEEN LONGERONS 27-28R IN THE FWD CARGO DOOR FRAME. REPAIRED IAW SRM 53-01, FIG 4, SHEET 4, SRM 51-10-3, PAR 14, 21, 38, AND 51-30-2.

Part: FLOOR PANEL — WORN (NOT REPORTED) · airframe 60,690 hrs · 43,756 cycles

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

Part: FLOOR PANEL — BROKEN (NOT REPORTED) · airframe 60,690 hrs · 43,756 cycles

BROKEN FLOOR PANEL 256D. THE FLOOR PANEL REPLACED IAW AMM 53-20-01-201.

Part: STIFFENER — CRACKED (BS 1338 BULKHEAD) · airframe 60,690 hrs · 43,756 cycles

A CRACK WAS FOUND ON THE STIFFENER END, LONGERON 14L AT THE PRESSURE BULKHEAD BS 1338. STIFFENER WAS REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-3 PAR 21 & 14, SRM 51-10-4, AND DWG 9915558 REV BA J.

Part: DOUBLER — CORRODED (AFT PRESS BLKHD) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON AFT CARGO BAY PRESSURE BULKHEAD LOWER PRODUCTION DOUBLER. THE DOUBLER WAS REPLACED IAW D-DWG 5910130, REV EG AND SRM 51-30-2, 51-30-5 AND 51-10-3.

Part: FRAME — CRACKED (BS 1474) · airframe 60,690 hrs · 43,756 cycles

CRACKS FOUND ON FRAME BS 1474 AND LONGERON 18L. THE FRAME WAS REPAIRED IAW SRM 53-01, FIG 2.

Part: LONGERON — CRACKED (BS 1338) · airframe 60,690 hrs · 43,756 cycles

ACFT HAS A CRACK ON LONGERON END 29L, BS 1338 AT AFT CARGO COMPARTMENT. LONGERON END WAS REPLACED IAW SRM 51-10-4/51-30-5 AND SRM 51-10-3.

Part: FLOOR PANEL — PUNCTURED (NOT REPORTED) · airframe 60,690 hrs · 43,756 cycles

PERFORATED FLOOR PANEL. THE FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201.

Part: STIFFENER — CRACKED (BS 1338) · airframe 60,690 hrs · 43,756 cycles

CRACKED STIFFENER END, LONGERON 14 RT AT PRESSURE BULKHEAD, BS 1338. STIFFENER WAS REPLACED IAW SRM 51-30-5, 51-10-4, 51-10-3, 51-30-1 PAR 21 AND 14 AND DWG 991558, REV BA.

Part: STIFFENER — CRACKED (BS 1418) · airframe 60,690 hrs · 43,756 cycles

CRACKED STIFFENER BS 1418. STIFFENER REPLACED IAW SRM 51-30-5 AND DWG 5913595- 81.

Part: STIFFENER — CRACKED (BS 1338 BULKHEAD) · airframe 60,690 hrs · 43,756 cycles

CRACKED STIFFENER END, LONGERON 15L AT PRESSURE BULKHEAD BS 1338. STIFFENERS WERE REPLACED IAW SRM 51-30-1, 51-30-5, 51-10-4, 51-10-3, PAR 21 AND 14 AND DWG 991558, REV BA.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 60,690 hrs · 43,756 cycles

CRACKED FLOOR PANEL. REPAIRED IAW SRM 53-05, FIG 131C, 51-10-3, PAR 14 AND 21 AND 53-01.

Part: FRAME — DAMAGED (BS 1437) · airframe 60,690 hrs · 43,756 cycles

ELONGATED HOLES ON FRAME ANGLE BS 1437 BETWEEN LONGERONS 2-3R. FRAME ANGLE WAS REPLACE IAW SRM 53-14-4, FIG 3 AND 51-30-5.

Part: LUG — BENT (RT ELEVATOR TAB) · airframe 60,690 hrs · 43,756 cycles

BENT LUG MID HINGE OF ANTI-FLOAT TAB AT RT ELEVATOR. HINGE WAS REMOVED AND A NEW HINGE WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2,51-30-1, 51-10- 4, AND 51-10-3.

Part: EXHAUST DUCT — WORN (APU) · airframe 60,690 hrs · 43,756 cycles

WEAR ON EXHAUST DUCT LT, AC, AT AFT ACCESSORY COMPARTMENT. EXHAUST DUCT WAS REPAIRED IAW SRM 51-30-2, ER/A 387296-14.

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · airframe 60,690 hrs · 43,756 cycles

ACFT HAS ELONGATED HOLE ON FUEL ACCESS PANEL 1367C. ACCESS PANEL WAS REPLACED.

Part: TRUNNION — CORRODED (RT MLG) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

ACFT CORROSION ON RT MLG SUPPORT BUSHING BORE. DAMAGE ON BUSHING BORE WAS REPAIRED IAW CARD 5740-01139-04B, DWG SR09570087, NOTE 11, REV B.

Part: SKIN — DAMAGED (RUDDER) · airframe 60,690 hrs · 43,756 cycles

ACFT HAS EXPOSED COMPOSITE MATERIAL ON RUDDER CONTROL TAB. RUDDER CONTROL TAB WAS REPAIRED IAW SRM 51-70-1AD PARR 23A. BALANCE AND WEIGHT CHECKS WILL BE ATTENDED WITH CARD 18 ACFT ZONE 65, W/O 20000077129.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON FRAME LOWER SECTION BS 1380 AT ACCESSORY COMPARTMENT. FRAME SECTION REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9912246, REV CE.

Part: CUSP WEB — CORRODED (BS 667-672) · corrosion level 2 · airframe 63,685 hrs · 45,885 cycles

CORROSION ON RT CUSP WEB BETWEEN RBL 54 TO 60, BS 667 - 672. REPAIRED IAW SRM 53-05 FIG 131A -12.

Part: STRUCTURE — CORRODED (MLG DOOR) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION AT RT MLG FIXED DOOR, AREA COVERED BY RUB STRIP. MLG FIXED DOOR WAS REPLACED IAW AMM 32-12-01.

Part: SLAT TRACK — DAMAGED (LT WING) · airframe 60,690 hrs · 43,756 cycles

ELONGATED HOLES ON SLAT TRACK DOOR NR 1 AT LT WING. SLAT TRACK DOOR NR 1 LT WAS REPLACED IAW ERA: 512356-14MA, REV ORIG SEC II.

Part: CUSP WEB — CORRODED (BS 636-648) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON LT CUSP WEB BETWEEN LBL 54 - 60, BS 636 - 648. THE CUSP WEB WAS REPAIR IAW SRM 51-30-5 AND 53-05, FG 131A-7.

Part: SKIN — DAMAGED (RUDDER) · airframe 60,690 hrs · 43,756 cycles

ACFT HAS DAMAGED METALIZED ON RUDDER SKIN BOTH SIDE. METALLIZED ON RUDDER SKIN BOTH SIDE WAS REPAIRED IAW SRM 51-70-1A AND JIC 9818779 CARD 200-8149-05.

Part: TAB — DENTED (RT ELEVATOR) · airframe 60,690 hrs · 43,756 cycles

SEVERAL DENTS FOUND ON THE CONTROL TAB UPPER SURFACE OF THE RIGHT ELEVATOR. REPAIRED IAW SRM 55-04, PAR 2.

Part: WEB — DAMAGED (BS 194-198) · airframe 60,690 hrs · 43,756 cycles

TOOL DAMAGE ON MEMBRANE BS 194 AND X=41 ALSO ON BS 198 AND X=23. MEMBRANE WAS REPAIRED IAW SRM 51-70-4, FIG 2, SRM 51-10-3, PAR 14, 21 SRM 51-30-2, SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 1174-1193) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON CUSP WEB REPAIR DOUBLER BETWEEN BS 1174 - 1193 BETWEEN LBL 54-60. DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A-5, 51-30-2, 51-10-3 PAR 21, 14, 38 AND 51-30-1.

Part: SKIN — DAMAGED (BS 827) · airframe 60,690 hrs · 43,756 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN, BS 827 BETWEEN LONGERONS 1 - 2R. THE SKIN WAS REPAIRED IAW SRM 53-04-2, PAR 3.C 2, A, 1, A.

Part: GUIDE VANE — WORN (LT WING TE FLAP) · airframe 60,690 hrs · 43,756 cycles

WEAR ON OTBD FLAP, OTBD FLAP VANE UPPER AND LOWER SKIN INBD EDGE AT LT WING. REPAIRED IAW SRM 57-03, PAR II AND OPN 1031.

Part: CUSP WEB — CORRODED (BS 262-465) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION OUT LIMITS ON RT CUSP WEB LBL 54 - 60 BETWEEN BS 262-264 AND 452-465. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14 AND 51-10-3 PAR 21 AND 14.

Part: WEB — CRACKED (BS 1352) · airframe 60,690 hrs · 43,756 cycles

CRACKED WEB NEXT TO PULLEY BRACKET BS 1352, RBL 18. WEB WAS REPAIRED IAW SRM 53-01, FIG 2, SHT. 4 AND SRM 51-10-3, PAR 14 AND 21, SRM 51-30-5.

Part: SKIN — DAMAGED (BS 681) · airframe 60,690 hrs · 43,756 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN BS 681 BETWEEN LONGERONS 2-3R. SKIN REPAIRED IAW SRM 53-04-2, PAR 3.C, 2, A,1,A.

Part: CUSP WEB — CORRODED (BS 827-840) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER ON LT CUSP WEB BETWEEN RBL 54 - 60 AND BS 827 - 840. THE DOUBLER WAS REMOVED, A NEW DOUBLER FABRICATE, TREATED. PAINTED, AND INSTALLED IAW SRM 51-30-2, 53-05, FIG 131, 51-10-3, PAR 21, 14.

Part: CUSP WEB — CORRODED (BS 237-503) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON RT CUSP WEB REPAIR DOUBLER LBL 54 - 60 BETWEEN BS 237 - 241 AND 484 - 503. DOUBLERS WERE REPLACED IAW SRM 53-05, FIG 131A- 7, 51-30-2 AND 51-30-5.

Part: RIB — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON HOLES OF RIBS BS XOS=380 AND XOS=429 AT LT WING SLAT PANEL NR 4. CORROSION ON HOLES OF RIB BS XOS=429 OF SLAT PANEL 4 WAS REPAIRED IAW SRM 57-02, PAR 9 AND BS XOS=380 WAS REPAIRED WITH ER/A 537759-14, REV ORIGINAL.

Part: TAB — DELAMINATED (LT ELEVATOR) · airframe 60,690 hrs · 43,756 cycles

DELAMINATED LT ELEVATOR ANTI-FLOAT TAB. DUE TO EXCESSIVE DAMAGE, FOUND THE ANTI-FLOAT TAB WAS REPLACED IAW SRM 55-04 P.2.

Part: DOOR — CORRODED (LT MLG) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION FOUND ON LT OTBD MLG DOOR, AREA COVERED BY RUB STRIP. OTBD MLG DOOR WAS REPLACED IAW AMM 32-12-01.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF ACCESS PANEL 1456C. THE ACCESS PANEL WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON SETTLEMENT AREA OF FUEL ACCESS PLATE 1371C. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1454C. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK OF ACCESS PANEL 1307C, LT WING. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1478C. REPLACED THE ACCESS PANEL.

Part: RIB — CORRODED · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON RIBS XOS=286 AND XOS=332, REPAIRED IAW SRM 57-02, PAR 9.

Part: RIB — CORRODED (LT WING SLAT) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON RIB XOS=83 AND HOLES XOS=166 AT LT WING SLAT PANEL NR 1. CORROSION ON HOLES RIB BS XOS=83 AND XOS=166 AT LT WING SLAT PANEL NR 1 WAS REMOVED IAW SRM 57-02, PAR 9.

Part: LONGERON — CRACKED (BS 522-524) · airframe 60,690 hrs · 43,756 cycles

CRACKED LONGERON 4R BETWEEN BS 522 - 524. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-30-2, 51-30-5 AND 51-10-3 PARR 14, 21.

Part: WEB — PUNCTURED (BS 160-200) · airframe 60,690 hrs · 43,756 cycles

PUNCTURES ON FLOOR MEMBRANE X54 BETWEEN BS 160 - 200 AT LT AREA. DAMAGE FASTENERS WERE REMOVED, DOUBLER WAS FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2, 53-01, FIG 2 , 51-10-3 PAGE 14 AND 21.

Part: LONGERON — WORN (BS 1408) · airframe 60,690 hrs · 43,756 cycles

WEAR LONGERON 8R BS 1408. THE LONGERON 8 WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 60,690 hrs · 43,756 cycles

GOUGE ON LT INBD FLAP, INBD SKIN LOWER SECTION BS XCW=76-78. REPAIRED IAW SRM 57-03D, FIG 8, SRM 51-10-3, PAR 14, 21, AND SRM 51-30-8.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS NR 1410C. THE ACCESS PLATE WAS REPLACED.

Part: RIB — CORRODED (NR 5 SLAT) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORRODED RIB XOS 580 - 610, LT WING SLAT NR 5. R & R SLAT IAW AMM 27-80-1.

Part: INTERCOSTAL — CORRODED (BS 1212-1155) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON INTERCOSTAL BETWEEN LONGERON 29 AND 30R BS 1212 - 1219 AND BS 1148-1155 IN AFT CARGO COMPARTMENT. INTERCOSTALS REPLACED IAW DGW: 5936071, REV: W.51-10-3, PAR. 14, 21, 26, AND 38, AND 51-10-4.

Part: TAB — DENTED (LT ELEVATOR) · airframe 60,690 hrs · 43,756 cycles

SEVERAL DENTS FOUND ON CONTROL TAB UPPER SURFACE ON LEFT ELEVATOR. CONTROL TAB REPLACED.

Part: PAN — CRACKED (BS 1041-1250) · airframe 60,690 hrs · 43,756 cycles

CRACK ON LT WINDOW RING PAN UPPER /AFT CORNER BETWEEN BS 1041-1060, AND 1231-1250. DAMAGE WAS REMOVED, NDT INSPECTION CHECK, NO CRACKS. ANGLES AND SHIMS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-30-5, SRM 53-05, FIG 122 AND ER/AS 487747-14MA, REV A, 493648-14MA, REV A.

Part: PAN — CRACKED (BS 1060-1079) · airframe 60,690 hrs · 43,756 cycles

CRACK ON WINDOW RING PAN BETWEEN BS 1060-1079. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 139, 51-30-2, 51-30-5, 51-10-2, 51-10-4, 51-10-3, PAR 14,21 AND ER/AS 487747-14, MA REV A, 493648-14 MA, REV A, SRM 53-05, FIG 222.

Part: PAN — CRACKED (BS 1174-1193) · airframe 60,690 hrs · 43,756 cycles

CRACK ON WINDOW RING PAN BETWEEN BS 1174-1193, 1155-1174, AND 1098-1117 AT FWD LOWER CORNER RT SIDE. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 139, 51-30-2, 51-30-5, 51-10-2, 51-10-4, 51-10-3, PAR 14, 21 AND ER/A 487747-14MA, REV A, ER/A 493648-14MA REV A, SRM 53-05 FIG 122.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1464C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS 1363C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1436. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A .

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE NR 1476 C, AYP, CARD 66, ZONE 00. FUEL ACCESSS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS 136. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2.

Part: STRUCTURE — CORRODED (BS 579-598) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON REPAIR DOUBLER BETWEEN SEAT TRACK X 54 AND 60, BS 579-598 DAMAGE REPAIR DOUBLER WAS REPLACED IAW SRM 53-05, FIG 131A-13 , 51-30-2 AND 51-30-5 , 51-10-3 PAR 14 AND 21.

Part: SKIN — CRACKED (BS 1380) · airframe 60,690 hrs · 43,756 cycles

CRACKED FUSELAGE SKIN AT BS 1380, BETWEEN LONGERONS 13-14L. REPAIRED IAW SRM 51-30-2, 51-30-5, 53-04, FIG 18, 51-10-3, PAR 14 AND 21.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1379C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: PAN — CRACKED (BS 1098-1079) · airframe 60,690 hrs · 43,756 cycles

CRACK ON WINDOW RING PAN BETWEEN BS 1098-1079, 1060-1079 AT FWD LOWER CORNER POSITION RT SIDE. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 139, SRM 51-30-2, 51-30-5, 51-10-2, 51-10-4, 51-10-3 PAR 14, 21 AND ERA 487747-14MA, REV A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS NR 1357C. THE FUEL ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1470C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: PAN — CRACKED (BS 1079-1174) · airframe 60,690 hrs · 43,756 cycles

CRACK ON WINDOW RING PAN BETWEEN BS 1155-1174, 1136-1155, 1117-1136 AND 1098-1079. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 139, SRM 51-10-2, 51-10,4, 51-10-3 PAR 14, 21, SRM 51-30-2, 51-30-5, AND ERAS 487747-14MA REV A, 493648-14MA REV A, SRM 53-05, FIG 122.

Part: PAN — CRACKED (PAX DOOR) · airframe 60,690 hrs · 43,756 cycles

CRACKED PAN ON FWD UPPER OF FWD PASSENGER PAN ON FWD UPPER CORNER OF FWD PASSENGER ENTRANCE DOOR L1. DUE TO EXCESSIVE DAMAGE OUT OF LIMITS ON ENTRANCE DOOR L1 WILL BE REPLACE.

Part: PAN — CRACKED (BS 579-905) · airframe 60,690 hrs · 43,756 cycles

CRACK ON RING PAN BETWEEN BS 886-905, 655-674, 579-598 AND 769-788 FWD UPPER CORNER RT SIDE. RING PAN WAS REPAIRED IAW SRM 53-5, FIG 139, SRM 51-30-2, 51-30-5, 51-10-2, 51-10-4, 51-10-3 PAR 14, 21 AND ERAS 487747-14MA, REV A, 493648-14MA, REV. A, SRM 53-05 FIG 122.

Part: PAN — CRACKED (BS 579-807) · airframe 60,690 hrs · 43,756 cycles

CRACK ON LT WINDOW RIN PAN UPPER/FWD CORNER BETWEEN BS 579-598, 788-807 AT CABIN STRUCTURE. DAMAGE REMOVED, NDT INSPECTION CHECK NO CRACKS ANGLES AND SHIMS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-30-5. SRM 53-05 FIG 122 AND ERA 487747-14MA REV A, 493648-14MA REV A.

Part: PAN — CRACKED (BS 807-1060) · airframe 60,690 hrs · 43,756 cycles

CRACK ON LT WINDOW RING PAN LOWER/FWD CORNER BETWEEN BS 807-826, 1041-1060. DAMAGE REMOVED NDT INSPECTION CHECK NO CRACKS, ANGLES AND SHIMS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-30-5 J. AVI/A 152126 AND ERA 487747-14MA REV A, 493648-14MA, REV A 53-05, FIG 122, 53-05, FIG 122.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 1355C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2.

Part: PAN — CRACKED · airframe 60,690 hrs · 43,756 cycles

CRACKED PAN AT AFT LT EMERGENCY EXIT DOOR UPPER FWD AREA. DOUBLER WAS INSTALLED IAW SRM 52-05D, FIG 51, 51-30-1, 51-30-2, 51-30-5, 51-10-3 PARAGRAPH 14 AND 21.

Part: SEAT TRACK — CORRODED (BS 822-826) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON SEAT TRACK REPAIR BS 826 - 822 LBL 54. REPAIR WAS REPLACED IAW SRM 53-05, FIG 4A AND SRM 51-10-3, PAR 14, 21.

Part: SEAT TRACK — CORRODED (BS 527-533) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON SEAT TRACK REPAIR BS 527 - 533 LBL 22. REPAIR WAS REPLACED IAW SRM 51-30-1.

Part: SEAT TRACK — CORRODED (BS 730-736) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON SEAT TRACK BS 730 - 736 ON PREVIOUS REPAIR X 54. PLUG WAS REPLACED IAW SRM 51-30-1 AND 53-05, FIG 4A.

Part: PAN — CRACKED (BS 1060-1098) · airframe 60,690 hrs · 43,756 cycles

CRACK ON LT WINDOW RING PAN LOWER/FWD CORNER BETWEEN BS 1060-1079, AND 1079-1098. REPAIRED IAW SRM 53-05, FIG 122, 51-30-2 , 51-30-5 , 51-10-3, PAR 14 AND 21 AND 51-10-4 AND ERA 493648-14MA, REV A.

Part: PAN — CRACKED (BS 598-1079) · airframe 60,690 hrs · 43,756 cycles

CRACK ON LT WINDOW RING PAN LOWER/AFT CORNER BETWEEN BS 598-617, 769-788, 1060-1079. REPAIRED IAW SRM 53-05, FIG 122, 51-30-2 , 51-30-5 , 51-10-3 PAR. 14 AND 21 AND SRM 51-10-4 AND ERA 493648-14MA, REV A.

Part: SKIN — DENTED (NR 5 SLAT LE) · airframe 60,690 hrs · 43,756 cycles

DENT FOUND ON RT NR 5 SLAT PANEL L/E. FOUND WITHIN LIMITS IAW SRM 57-03D, FIG 18. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND IAW SRM 57-03, FIG 18. STEP 6A AND NDT SPM 06-10-01.001.

Part: SEAT TRACK — CORRODED (BS 436-441) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON SEAT TRACK BS 436 - 441 ON PREVIOUS REPAIR X 54. PLUG WAS REPLACED IAW SRM 53-05, FIG 4A AND 51- 30-1. PRIMARY STRUCTURE.

Part: SEAT TRACK — CORRODED (BS 379-465) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON RT REPAIR PLUG OF SEAT TRACK, X -54 AND BETWEEN BS 379-381, 429-431 AND 463-465. PLUG WAS REPLACED IAW SRM 53-05, FIG 4A AND 51-30-1I. ALARCON 593421. PRIMARY STRUCTURE.

Part: SEAT TRACK — CORRODED (BS 932-938) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

CORROSION ON SEAT TRACK BS 932 - 938 ON PREVIOUS REPAIR X 54. PLUG WAS REPLACED IAW SRM 53-05, FIG 4A AND 51-30-1I.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,690 hrs · 43,756 cycles

ACFT AFT LAV SERVICE PANEL CUTOUT STRAP HAS CORROSION ON THE LOWER AFT CORNER. COMPLIED WITH STEPS 1-5 OF ERA 538253-14, REV ORIGINAL C/W HFEC INSPECTION OF CUTOUT AREAS IAW STEP 6 OF ERA 538253-14, REV ORIGINAL SECTION I TIME LIMITED REPAIR WITH NO ITEMS NOTED. COMPLIED WITH ERA 538253-14, SECTION 1, TIME LIMITED REPAIR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,613 hrs · 43,705 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 27-31 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,871 hrs · 41,813 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE OVERHEAD AISLE EMERGENCY EXIT LIGHTS WERE INOPERATIVE AT ROW 14ABC AND 32BC. MAINTENANCE REPLACED THE LAMPS AND THE OPS CHECKED GOOD.

Part: RESERVOIR — FAILED (HYD SYSTEM) · airframe 57,473 hrs · 41,552 cycles

LEFT HYDRAULIC SYSTEM FAILED DURING CRUISE AT 24,000 FEET. HYDRAULIC PRESSURE ZERO AND QUANTITY INCREASED TO 19 QTS. MAINTENANCE R & R THE LT SYSTEM HYDRAULIC RESERVOIR AND THE SYSTEM RETURNED TO A FUNCTIONAL STATE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,346 hrs · 41,467 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,135 hrs · 41,344 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY CEILING LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE POWER SUPPLY, REPLACED BATTERIES AT ROW 24-26, AND REPLACED CRUSHED WIRE SPLICES AT ROWS 27-28. THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 56,147 hrs · 40,743 cycles

DURING LINE CHECK, SEAT MOUNTED EMERGENCY LIGHTS AT 10D AND 14D WERE INOPERATIVE. SEAT WIRE HARNESS AT 10D REPLACED AND PIG TAIL AT 14D REPLACED IAW AMM 33-53-01 AND OPS CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 55,808 hrs · 40,503 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 24-26 OF THE CABIN WERE INOPERATIVE. MX REPAIRED SOME WIRE SPICES IN THE WIRING HARNESS AND THE SYS RETURNED TO NORMAL OPERATION.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 55,808 hrs · 40,503 cycles

CRACK INDICATION LT HORIZONTAL STAB REAR SPAR CAP, AT UPPER ROW INBD BOLT IN INSPECTION AREA. ACCOMPLISHED SPAR CAP SPLICE REPAIR IAW SR09550027-7001, REV LEVEL "D" AND ER/A 518518-14AD REV-ORIGINAL.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 55,788 hrs · 40,490 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE MECHANISM CAM BASE WAS WORN OUT OF ALLOWABLE LIMITS. THE CAM BASE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII WAS SATISFACTORY.

Part: ATTACH FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 55,788 hrs · 40,490 cycles

DURING SCHEDULED MX CHECK, CORROSION WAS NOTED ON THE RT HORIZONTAL STABILIZER AFT OTBD PIVOT ATTACH FITTING. THE PIVOT ATTACH FITTING BORE WAS REPAIRED IAW SRM 55-02, STEP C AND NEW BUSHINGS WERE INSTALLED IAW SRM 55-02, PG 115.

Part: SHEAR TIE — CORRODED (BS 1287) · corrosion level 2 · airframe 55,788 hrs · 40,490 cycles

DURING SCHEDULED INSPECTION, CORROSION WAS FOUND IN THE AFT CARGO BAY AT BS 1287 SHEAR TIE FROM L28R-28L. REPAIR SPLICE INSTALLED IAW SRM 53-03D, FIG 3.

Part: SILL — CORRODED (BS 640-685) · corrosion level 2 · airframe 55,788 hrs · 40,490 cycles

DURING SCHEDULED MX , CORROSION WAS NOTED ON THE MID CARGO DOOR SILL L28R AREA FROM BS 640-685. REPAIRED IAW ERA 499523-14MA AND SRM 53-05-FIG 123.

Part: STRUCTURE — CORRODED (BS 1290) · corrosion level 2 · airframe 55,788 hrs · 40,490 cycles

DURING SCHEDULED MX, CORROSION WAS NOTED IN THE AFT CARGO BIN AT BS 1290 L29R. INSTALLED REPAIR CHANNEL IAW SRM 53-02, PAR 13, FIG 19.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,523 hrs · 40,294 cycles

DURING ROUTINE LINE CHECK, THE FORWARD OVERWING EMERGENCY EXIT SIGNS WERE NOTED TO BE INOPERATIVE ON BOTH SIDES OF THE ACFT. THE OVERWING EXIT LIGHT BATTERY WAS REPLACED IAW AMM 33-53 AND OPS CHECKED NORMALLY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,330 hrs · 40,168 cycles

DURING ROUTINE LINE CHECK, THE LT & RT FWD OVERWING EXIT SIGNS WERE FOUND TO BE INOPERATIVE. 4 BULBS WERE REPLACED AND SYS OPS CHECKED GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,213 hrs · 40,095 cycles

A DENT WAS NOTED ON FUSELAGE SKIN 48 INCHES AFT AND 24 INCHES BELOW THE FWD LAVATORY SERVICE PANEL. REPAIR ACCOMPLISHED IAW ER/A 515893-14.

Part: GIRT BAR — DISCONNECTED (L2 DOOR SLIDE) · airframe 52,741 hrs · 38,401 cycles

THE PILOT DISCOVERED THE GIRT BAR BRACKET AT DOOR 2L, TO BE DISCONNECTED. MAINTENANCE REINSTALLED THE BRACKET AND RETURNED THE AIRCRAFT TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LGIHTS) · airframe 52,717 hrs · 38,385 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES IN AFT OVERWING PACK, FORWARD PACK, BATTERIES AND ONE LAMP. OPS CHECKED GOOD. AIRCRAFT OKAY FOR SERVICE.

Part: PAN — CORRODED (FUSELAGE) · airframe 1 hrs · 1 cycles

AFT LAV SERVICE PAN INSIDE ACCESS DOOR BELOW DUMP VALVE HAS CORROSION. REMOVED AND REPLACED LAV SERVICE PAN PER SRM 51- 30. LONGERON 22 LEFT BETWEEN FS 1309 TO FS 1322 THE UPPER FLANGE WAS TRIMMED OFF TO ACCOMMODATE THE REMOVAL OF THE SERVICE PAN REF ER/A 500978-14 REV O. ALSO BLIND FASTENERS WERE INSTALLED WHERE ACCESS WAS NOT AVAILABLE FOR SOLID RIVETS REF ER/A 501002-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,019 hrs · 37,929 cycles

DURING PSV VISIT MSP FOUND AFT LAV SERVICE PAN OUTER SKIN CORRODED. DISCREPANCY REQUIRED REMOVAL OF PAN AND INSTALL A NEW PAN. THE UPPER FLANGE OF LONGERON 22L HAD TO BE REMOVED TRIMMED OFF. TRIM IS BETWEEN FS 1309 AND FS 1322 MEASURING 10.0" LONG.

Part: RELEASE SYSTEM — OUT OF ADJUST (TAILCONE) · airframe 52,019 hrs · 37,929 cycles

THE TAIL CONE FAILED TO DROP. CABIN INTERIOR PULL TEST DID NOT FUNCTION. NO CORRECTIVE ACTION IDENTIFIED PER TO NRC 122. MRR 121256. MAINTENANCE FOUND THE INTERIOR LOCK CABLE TO BE BINDING IN THE SUPPORT FITTING. THE SYSTEM WAS RE-RIGGED AND ADJUSTED PER MD-88 AMM 53-53-02. RII ACCOMPLISHED.

Part: SKIN — DAMAGED (BS 400 S1-2R) · airframe 51,297 hrs · 37,475 cycles

LIGHTNING STRIKE A, REMOVED DAMAGED FASTENER. STEPPED UP DAMAGED AREA FASTENER HOLE, T BS 400, STR 1-2R, TO .250 IN SRM MD-80 53-04-00, CONDITION 2. PERFORMED HFEC INSP OF AREA IAW SRM 53-04D, FIG 38, COND 2. EB. NO CRACKS INDICATION INSTALLED TEMPORARY REPAIR IAW SRM 53-04, FIG 38.

Part: SKIN — DAMAGED (BS 197) · airframe 51,297 hrs · 37,475 cycles

LIGHTNING STRIKE, INSPECTED IAW SRM 53-04. FOUND TO BE IN CONDITION 2 PERFORMED, RKS RT SIDE OF FUSELAGE AT BS197, STR 3R/ BS 331, STR 1-2R/STA, REMOVED EDDY CURRENT INSP ACTION FOR SRM 53-04D, FIG 38, COND. 2N, 560 STR 2-3R BS 617, STR 2-3R, CRACKS INDICATED. INSTALLED BLIND FASTENERS IAW SRM 53-04 TREATED AND PAINTED.

Part: SPAR — DAMAGED (VERTICAL STAB) · airframe 50,254 hrs · 36,767 cycles

DURING PSV IN MSP & INSP PER MD80-55A067/DAL EA 09-470871-12 ELONGATED HOLES WERE FOUND IN THE 5911394 LT SPAR CHORD, AT THE 12TH & 17TH HOLES ABOVE THE ZFS=52, SPLICE FIXED L/E TO REMOVABLE L/E SKIN SPLICE. THE HOLES WERE OPENED IN THE SPAR CHORD TO PROVIDE ACCESS FOR CLEAN & ROUND HOLES. THE REPAIR WAS A STRAP BASED ON ATTACHED BOEING REPAIR DWG SG09550005-7001. THE MATING HOLES IN THE REMOVABLE L/E SKIN THAT WERE DMG'D WERE REPAIRED PER ERA#493602-14 HOLES 12&17 WERE OVERSIZED TO .388 DIA WITH .437ED&.400 OVERSIZED WITH .437ED&.400 OVERSIZED WITH .468ED RESPECTIVELY.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 49,581 hrs · 36,363 cycles

DURING FLIGHT, THE OVERHEAD LIGHT AT ROW 31D WAS EMITTING SMOKE FROM BALLAST. F/A THEN TURNED OFF THE OVERHEAD LIGHTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MX FOUND LIGHT SOCKET MELTED AT 32DE. BULB WAS REMOVED AND FORWARDED TO MCO/PLACARD 33-00-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,276 hrs · 36,202 cycles

DURING LINE CHECK MX FOUND OVERWING EXIT SIGNS AT LT AND RT AT ROW 24 INOPERATIVE. MX REPLACED BATTERY PACK B5-103. SIGNS NOW ILLUMINATE PROPERLY.

Part: DEFLECTOR — DAMAGED (NLG) · airframe 48,594 hrs · 35,771 cycles

RETURNED TO DEPARTURE, NLG WOULD NOT RETRACT AFTER TAKEOFF. MX FOUND RT SPRAY DEFLECTOR WEARSTRIP FWD NUTPLATE PULLED AND SCREW STICKING OUT, CAUSING CONTACT WITH WHEEL WELL STRUCTURE DURING RETRACTION, R & R RT SPRAY DEFLECTOR HALF. SWUNG NLG CHECKED GOOD.

Part: SKIN — DAMAGED (BS 322 L22-24L) · airframe 47,306 hrs · 34,917 cycles

SUNKEN FASTENERS ON PREVIOUS REPAIR OF FUSELAGE SKIN BTW STAY=318-322 AND LON 23L ALMOST MISSING REPAIR REFERENCE IN SAME PREVIOUS REPAIR STA Y=322 LONGS 22L TO 24L. WAS REPLACED IAW PRI AMR0953755 AND ERA 480216-14 REV ORIG.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · airframe 47,265 hrs · 34,895 cycles

CORROSION ON LOWER BEAM STA Y=370-247 AT FWD CARGO COMP DOOR JAMB. RE-WRITE; SEVERAL RIVETS IMPROPERLY INSTALLED AND INCORRECT WASHERS INSTALLED UNDER HI-LOCK NUTS. RIVETS AND WASHERS WERE REPLACED IAW SRM'S 51-30-2 AND 51-30-5.

Part: ACCESS DOOR — DAMAGED (LT WING) · airframe 47,265 hrs · 34,895 cycles

ELONGATED SCREW HOLE AND FRETTING CORROSION ON SLAT TRACK ACCESS DOOR NR 1132C AND 1165C OF LT WING LW. ACCESS DOOR WAS REPAIRED IAW ERA 480223-14 REV, ORIG AND SRM 51-10-3.

Part: BEAM — CORRODED (DOOR FRAME) · airframe 47,265 hrs · 34,895 cycles

EXFOLIATION CORROSION ON LOWER BEAM STA Y=370-427 AT FWD CARGO COMP DOOR JAMB. DOOR JAMB WAS REPAIRED IAW SRM'S 51-30-2, 53-05D, AND 51-10-3.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · airframe 47,265 hrs · 34,895 cycles

CORROSION ON LOWER BEAM STA Y=636-693 AT MID CARGO COMP DOOR JAMB. BEAM WAS REPAIRED IAW SRM'S 51-30-1, 51-30-2, 51-10-3 PAR 2B, AND 53-05 FIG 123.

Part: BEAM — CORRODED (DOOR FRAME) · airframe 47,265 hrs · 34,895 cycles

EXFOLIATION CORROSION ON LOWER BEAM STA Y=1155-1212 AT AFT CARGO COMP DOOR JAMB. BEAM WAS REPAIRED IAW SRM'S 51-30-5, 51-10-3, AND 53-05 FIG 123.

Part: TAB — DENTED (RT ELEVATOR) · airframe 47,265 hrs · 34,895 cycles

DENT ON RT ELEVATOR CONTROL TAB UPPER SKIN VHS. RT ELEVATOR CONTROL TAB UPPER SKIN VHS WAS REPAIRED IAW SRM 55-05 PAR 3A AND OPN 1031 CARD 1102-1110. TAB WAS BALANCED IAW SRM 55-20-2D.

Part: LINK — WORN (VENTRAL CATWALK) · airframe 47,265 hrs · 34,895 cycles

BENT LINK AND WORN ARM OF VENTRAL CATWALK CONTROL MECHANISM STA 1485 CANT X=-10. LINK, ARM AND HARDWARE OF VENTRAL CATWALK CONTROL MECHANISM WAS REPLACED IAW AMM 20-30-01-201.

Part: TAB — NICKED (RT ELEVATOR) · airframe 47,265 hrs · 34,895 cycles

NICK ON RT ELEVATOR CONTROL TAB T/E INBD SECTION VHS. RT ELEVATOR CONTROL TAB T/E INBD SECTION VHS WAS REPAIED IAW SRM 55-04 PAR 3A AND OPER 1031 CARD 1111-1119. TAB BALANCED IAW 55-20-2D.

Part: TUBE — DENTED (STA 1510) · airframe 47,265 hrs · 34,895 cycles

WORN FUSELAGE TUBE OF TAILCONE RELEASE CONTROL CABLE STA 1510 CANT 5 O'CLOCK POSITION. TUBE WAS REPLACED IAW AMM 20-30-01-201. TAIL CONE RELEASE CONTROL CABLE WILL BE ADJUSTED ON NR T0164941.

Part: RELEASE CABLE — FRAYED (TAILCONE) · airframe 47,265 hrs · 34,895 cycles

BROKEN STRANDS ON TAILCONE RELEASE CABLE STA 1510 CANT 11 O'CLOCK POSITION. CABLE WAS REPLACED IAW AMM 20-10-17-201. CABLE WAS ADJUSTED AND OPS CHECKED IAW AMM 53-53-00-501.

Part: STIFFENER — CRACKED (BS 1350) · airframe 47,265 hrs · 34,895 cycles

CRACK ON STIFFENER AT STA Y=1350 AND X=0 AT P-DOME UPPER SIDE. CRACKED STIFFENER WAS REPALCED IAW SRM'S 51-30-2 AND 51-30-5 AND 51-10-4. EMERGENCY EXIT MECHANISM ARM ASSY WAS REMOVED AND REINSTALLED TO FACILITATE MX IAW CMM 52-22-02.

Part: SKIN — DENTED (STA 232) · airframe 47,265 hrs · 34,895 cycles

DENT ON FUSELAGE SKIN STA Y=232 LONGERONS 17 AND 18 LT. DAMAGED AREA WAS R & R IAW SRM 53-04 FIG 12B, SRM 51-10-4 AND SRM 51-10-3. REPAIR WAS IDENTIFIED IAW PS 900-5-1 NR 4.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,787 hrs · 34,608 cycles

SEAT 1C EMERGENCY FLOOR LIGHTS INOP. REPLACED POWER SUPPLY B5-23 CK OK. REPLACED POWER SUPPLY B5-23 AND POWER SUPPLY AND BATTERY PACK AB 3D - LIGHTS CK GOOD - RELAMPED AND REPLACED LENS AT 01C - M REMOVED.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 41,212 hrs · 31,119 cycles

AFTER LANDING AND STARTING APU, PASSENGER AND FLIGHT ATTENDANT IN COACH COMPLAINED OF ACRID, ELEC TYPE ODOR IN MAIN CABIN, SHUTDOWN APU AND WITH EXT AIR AND POWER ODOR WENT AWAY. MTC IN PROGRESS. FOUND HYD LEAK IN TAIL COMPARTMENT, LEFT SYSTEM AND APU INLET CONTAMINATION.

Part: METER — FAILED (NR 2 ENGINE) · airframe 31,856 hrs · 24,670 cycles

AC CROSSTIE LOCKOUT LIGHT ON. LT GEN LOAD FLUC FROM .4 TO.6, RT GEN VOLTS FREQ OK BUT LOAD AT ZERO. WHEN RT GEN RESET LOST ALL ELEC PWR MOMENTARILY. RT GEN BACK TO OFF AND THEN LT GEN PICKED UP LOAD OK. REPLACED LOAD METER.

Part: CONNECTOR — BURNED (ACARS) · airframe 31,689 hrs · 24,557 cycles

UPON ARRIVAL CREW INFORMED MAINTENANCE ACARS C/B POPPING AND WILL NOT RESET. FOUND ACARS AUX UNIT AND RACK CONNECTOR WITH BURNED PINS. REPLACED UNIT.

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 30,432 hrs · 23,669 cycles

DURING TAXI OUT SMOKE/FUMES ENTERED CABIN. DISAPPEARED WHEN APU WAS SHUT DOWN. FOUND "B' NUT LOOSE ON HYD LINE TO LT THRUST REVERSE MODULE. HYD FLUID LEAKED INTO 48 SECTION AND OVERBOARD. DUCT BURNOUT IN PROGRESS.

Part: ENGINE — FAILED (#1 ENGINE) · airframe 28,943 hrs · 22,641 cycles

ON DEPARTURE FROM HOU ON FLT 0532 LT ENGINE FAILED AT 10500 FT. RETURNED TO HOU. ENGINE OIL PRESS WENT TO -0- AFTER FAILURE WINDMILLED FOR 12-18 MINS WITH -0- OIL PRESS. ENGINE CHANGE REQURIED DUE TO -0- OIL PRESS

Part: BLANKET — BURNED (RIGHT WING) · airframe 28,698 hrs · 22,475 cycles

WHILE INSPECTING RT WING FUEL LEAK. FOUND APPX 4.5 INCH DIA BURNED AREA IN RT WING HEATER BLANKET.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,040 hrs · 22,013 cycles

FOUND EMERGENCY LIGHT INOP AT 14 D/E. RELAMPED LIGHT, CHECKS GOOD.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 27,077 hrs · 21,324 cycles

LEFT HYD QTY 4 COMPLIED W/POM, WHEN SYS REPRESSURIZED ON APPROACH GOT ZERO PRESSURE INDICATION. FOUND T/R LINE LEAKING IN 48 SECTION. REMOVED AND REPLACED SAME, SERV HYD. OK FOR SERVICE.

Part: CONNECTOR — LOOSE (ROW 15) · airframe 25,338 hrs · 20,007 cycles

SEAT 15 EMERGENCY TRACK LIGHT INOP. RESEATED PIN INTO CONNECTOR AT SEAT LIGHT.

Part: COALESCER BAG — CONTAMINATED (AFT) · airframe 25,330 hrs · 20,003 cycles

IN FLT FUMES AND SMELL THROUGHOUT AFT CABIN AREA. DIVERTED TO LIT. PERFORMED DUCT BURNOUT. REPLACED COALESCER BAGS.

Part: OVEN — DIRTY (GALLEY) · airframe 24,824 hrs · 19,630 cycles

LAV 1L SMOKE DETECTOR DISCONNECTED AFTER BUZZER GOING OFF. THERE WAS A SLIGHT SMOKE ODOR IN FIRST CLASS. BUT COULD NOT BE TRACED BEFORE IT DISSIPATED. FOUND FIRST CLASS OVEN CAUSING SMOKE ODOR IN F/C. REPLACED SAME.

Part: SKIN — DENTED (BS 219)

DENT WAS FOUND AT STA 218 BETWEEN L18L AND L19L. REPAIRED PER ERA 331654-14.

Part: SKIN — DENTED (BS 221)

SEVERAL DENTS WERE FOUND IN THE FUSE SKIN AT FS 216 TO 229 BETWEEN L17 AND 18L. REPAIRED PER ERA 331653-14.

Part: SKIN — CREASED (BS 235)

THE FUSELAGE SKIN AFT OF THE L1 DOOR WAS FOUND WITH A CREASEFROM STA 230 TO 240 BETWEEN L18 AND 19L. REPAIRED PER ERA 331647-14.

Part: FRAME — CRACKED (BS 1418)

FS 1418 FRAME WAS CRACKED AT L2R. CRACK WAS APPROX 1 IN LENGTH. REPAIRED PER ERA 331637-14.

Part: COFFEEMAKER — FAILED (AFT GALLEY)

OUTBOARD COFFEEMAKER IN AFT GALLEY STARTED SMOKING, C/B PULLED. INSPECTED AREA, REPLACED COFFEEMAKER AND OPS CKS OK.

Part: STRUT — REQD SERVICE (NLG)

NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOUND WATER IN NOSE STRUT FLUID RESERVICED. CHECKED NORMAL DURING RETRACTION.

Part: ANGLE — CRACKED (KEEL BEAM)

FOUND DURING D-1 LETTER CHECK, KEEL BEAM AFT ANGLE CRACKED BOTH ENDS. INSTALLED DOUBLER PER MM 53-05 FIG 101.

Part: CONTROL CABLE — BROKEN (LT LE SLAT)

LEFT 0 SLAT PARTIALLY DEPLOYED. FOUND LEFT 0 SLAT CABLE BROKEN, LEFT 0 SLAT RETRACT AND EXTEND PULLEY AND BRACKETS BROKEN. REPLACED LEFT 0 SLAT, EXTEND AND RETRACKT CABLES AND REPLACED BROKEN PULLEYS AND BRACKETS. RIGGED SLATS AS PER MM.