N963DL

Part: SPAR — CRACKED (LT WING) · airframe 76,242 hrs · 57,465 cycles

DURING W/C 5710-01110-01A, HAD A CRACK INDICATION L/H WING REAR SPAR XRS 164 AT 5 O'CLOCK POSITION. CRACK APPROX. 1/4" IN LENGTH. REPAIR ACCOMPLISHED ON R/C DECK 5710-01110-02 AND ERA 583270-14 , REV. 0. (LP6658370)

Part: SPAR — DAMAGED (LT WING) · airframe 76,237 hrs · 57,462 cycles

LEFT WING REAR SPAR XRS 1640 LOWER STUD HOLES DAMAGE. C/W PRI 583270-14REV O THRU REV 6.

Part: CAP — DAMAGED (VERTICAL STAB) · airframe 76,237 hrs · 57,462 cycles

UPPER VERTICAL STAB CAP DAMAGED. RMVD DAMAGE AREA FABRICATED DOUBLER PER MD88 SRM 55-32 FIG 4. INSTALLED REPAIR DOUBLER PER MD 88 SRM 55-32 FIG 4 (LP1379844)

Part: SPAR — CRACKED (LT WING) · airframe 76,237 hrs · 57,462 cycles

DUE TO LEFT WING SPAR CRACK XRS 164 - THIS LOG PAGE IS BEING CREATED TO TRACK THE DTE REQUIREMENTS PER ER/A 583270-14AD REV ORIGINAL. REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LONGER THAN 24 MONTHS FROM REPAIR ACCOMPLISHMENT. DAMAGE TOLERANCE ANALYSIS IS REQUIRED IN ACCORDANCE WITH PROCEDURES ESTABLISHED BY FAA ADVISORY CIRCULAR 120-93. THIS ENTRY CORRECTS THE REPAIR APPROVAL FROM 750 DAYS TO 27NOV2021. REPAIR LOG FOR THIS DAMAGE WILL BE REPORTED AS SOON AS THE LOG FOR DAMAGE IS ENTERED. (LP583270)

Part: ATTACH BRACKET — CRACKED (TAILCONE) · airframe 76,237 hrs · 57,462 cycles

TAIL CONE ATTACH BRACKET CRACKED ON TAIL CONE @2:00 POSITION. REMOVED AND REPLACED TAIL CONE ASSY PER MD88 AMM 53-53 TAILCONE, AFT U OFF 88-5353-9-0002 S/N 00036. (LP1360531)

Part: LATCH — LOOSE (TAILCONE) · airframe 76,237 hrs · 57,462 cycles

LH UPPER LATCH ARM LOOSE/WORN. REPLACED LH UPPER LATCH ARM PER MD88 AMM 53-53, OPS CHECK GOOD, (LP1359437)

Part: SMOKE DETECTOR — MALFUNCTIONED (AFT LAVATORY) · airframe 76,054 hrs · 57,283 cycles

AFT LAV SMOKE ON CAPT SIDE CHIRPING. R & R AFT LAV SMOKE DECTOR OP CKS GOOD OK FOR SVC.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 75,788 hrs · 57,019 cycles

DURING SVC CK FOUND FIRST 7 ROWS OF EEPLS LIGHTING INOP. REPLACED BLOWN FUSE ON EMERGENCY POWER SUPPLY B5-211 OPS CK GOOD PER MD88 AMM 33-53. OK FOR SVC. (LP5966718)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,770 hrs · 57,001 cycles

DURING SVC FOUND AFT O/W EXIT SIGNS INOP. R/R AFT O/W EXIT SIGN BATTERIES PER MD88 M/M 33-53 OPS CHECK GOOD. (LP5966705)

Part: LIGHT — DAMAGED (CABIN) · airframe 75,626 hrs · 56,871 cycles

EMERGENCY EXIT SIGN COVER AND BULBS MISSING LOCATION 602. REPLACED EMER EXIT SIGN ASSY PER MD 88 AMM 33-51E.

Part: PIN — BROKEN (BOTTLE) · airframe 75,314 hrs · 56,598 cycles

PUT LANDING GEAR HANDLE DOWN TO LAND. LOUD BANG AND A/C SHUDDER. RIGHT HYDRAULICS LOST. RAN QRH PROCEDURES AND LANDED. FOUND R/H BOTTLE PIN BROKE. REPLACED BOTTLE PIN PER MD88 AMM 57-40-02 AND REPLACED R/H MLG RETRACT ACTUATOR PER MD88 AMM 32-32-02. LEAK CHECK AND OPS GOOD. CYCLED MLG SEVERAL TIMES WITH NO DEFECTS NOTED.

Part: DEFLECTOR — MISSING (NLG) · airframe 74,023 hrs · 55,500 cycles

BOTH DEBRIS DEFLECTORS MISSING ON NOSE WHEEL. REPLACED BOTH LT AND RT NLG DEBRIS DEFLECTORS PER MD88 AMM 32-20. SDR REPORTED DUE TO POSSIBILITY THAT PARTS MAY HAVE DEPARTED THE AIRCRAFT DURING FLIGHT. (LP5039454)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,985 hrs · 55,467 cycles

4EA OVHD EMERGENCY LIGHTS INOP AT SEAT ROWS 32-14. REMOVED AND REPLACED BATTERY PACK PER MD88 AMM 33-55. OPS CHECK GOOD . OK TO RETURN TO SERVICE. (LP5039443)

Part: WIRE — BROKEN (VENTRAL STAIRS) · airframe 73,646 hrs · 55,166 cycles

VENTRAL STAIR CEILING PANEL EMERGENCY LIGHT IS NOT ILLUMINATING. MAINTENANCE FOUND A BROKEN WIRE AT THE CONNECTOR FOR THE LIGHT HOUSING. THE WIRE WAS REPAIRED AND THE LIGHT WIRE WAS RESOCKETED IAW SWPM 20-31. OPERATIONAL CHECK OF THE LIGHT WAS GOOD.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 73,459 hrs · 54,995 cycles

LEFT HORIZONTAL STAB UPPER SPAR CAP WAS CRACKED, 1.75 INCHES FROM THE LOWER INBD BOLT, THROUGH THE UPPER INBD BOLT. IAW 5510-01074-19, STEP 8. HORIZONTAL STAB REPLACED ON JOB 000-0006: 5510-4135.

Part: SKIN — DAMAGED (RT MLG DOOR) · airframe 73,459 hrs · 54,995 cycles

FASTENERS LOOSE AND PULLING THROUGH THE OUTER SKIN ON THE RT MLG DOOR. REPLACED THE RT MLG DOOR IAW AMM 32-12-01.

Part: WEB — CRACKED (BS 1485) · airframe 73,459 hrs · 54,995 cycles

WEB CRACKED AFT SIDE OF LT TAIL COMPARTMENT VENT BOX, BS 1485. REPAIRED IAW SRM 53-03D, PARA 44, FIG 50.

Part: RELEASE CABLE — DETERIORATED (TAILCONE) · airframe 73,459 hrs · 54,995 cycles

LEFT TAILCONE RELEASE CABLE WAS IN POOR CONDITION. THE CABLE WAS REPLACED, AND RIGGED IAW C 5350-01077-0101.

Part: STRUCTURE — CORRODED · corrosion level 2 · airframe 73,459 hrs · 54,995 cycles

AFT CARGO DOOR AREA HAD CORROSION JUST BELOW THE SCUFF PLATE AT AFT END OF DOORWAY. ALL CORROSION REMOVED, AND FOUND OUT OF LIMITS IAW SRM 53-05, PARA 140, FIG 123. REPAIR OPTION 1. DRILLED NEW HOLES ON THE PAN, DOUBLER AND FILLER. TREATED AND PRIMED THE PAN, FILLER AND AREAS COMMON TO REPAIR IAW SRM 51-10-3. INSTALLED THE REPAIR IAW SRM 53-05, PARA 140, FIG 123, OPTION 1.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 72,060 hrs · 53,898 cycles

DIV TO MSP DUE TO RIGHT MAIN LANDING GEAR UNSAFE LIGHT WITH GEAR UP. NO FAULTS ON PSEU. NO DISCREPANCIES NOTED ON GEAR SWING. NO OTHER DISCREPANCIES NOTED AFTER DETAILED INSPECTION. REPLACED RT RETRACT ACTUATOR PRECAUTIONARY.

Part: ENGINE — FAILED (RIGHT) · airframe 71,629 hrs · 53,575 cycles

RIGHT ENGINE FAILED DURING CLIMBING OUT. OIL PRESSURE AROUND 60 PSI PRIOR TO FAILURE AND OIL TEMP FLUCUATING FOLLOWED QRH PROCEDURE AND SHUT ENGINE DOWN. VIBRATION EVEN AFTER SHUTDOWN. 800 DEGREES EGT NOTED. REPLACED THE NR 2 ENGINE IAW AMDS 7100-4682.

Part: LIGHT — INOPERATIVE (SEAT 17D) · airframe 71,590 hrs · 53,548 cycles

DURING AN EMERGENCY LIGHT CHECK, 17D SEAT LIGHT INOPERATIVE. REPLACED THE LIGHT ASSY, OPS CHECKED GOOD AMM 33-53.

Part: CONTROL VALVE — DEFECTIVE (AC BAY) · airframe 70,349 hrs · 52,551 cycles

ON APPROACH ENG ANTI-ICE WAS SELECTED ON, WE THEN NOTICE A HOT OR BURNING SMELL. THE LEFT PACK CONTROL SHOWED FULL COLD, BUT THE PACK WAS CYCLING ON AND OFF. LEFT PACK WAS TURNED OFF SMELL STOPPED. CREW VERBAL REPORTS HOT DUCT SMELL - NO OILY ODOR. TROUBLE SHOT PER AMM TASK 2120-2307 = DID PACK BURNOUT PER TASK 7100-2619. DID NOT DUE STEP 11 REPLACEMENT OF LT & RT WATER SEPARATOR BAGS. FOUND LT PACK UNABLE TO CONTROL TEMP. WORKS GOOD IN MANUAL BUT NOT AUTO, AS PER TSM 21-50 SECTION 2 FOUND TEMP CONTROL VALVE INOP. ORDERED PART. REMOVED AND REPLACED LT PACK TEMP CONTROL VALVE PER MM 21-61. OPS AND LEAK CHECK GOOD. COMPLETED BURNOUT PER AMDS 7100-2619. NO SMELL NOTED.

Part: WARNING MESSAGE — MULTIPLE FAIL · airframe 70,344 hrs · 52,549 cycles

DURING TAKEOFF ROLL HEADING COMPARATOR DISPLAYED WITH HEADING OFF 3 DEGREES. AFTER ROTATION CAPTAINS HEADING OFF 60 DEGREES AND ATTITUDE 45 DEGREES OFF. WINDSHEAR WARNINGS AND MAP FAILED ON NR 2. RETURNED TO DEPARTURE. FALSE WINDSHEAR WARNING ON FINAL. REPLACED THE NR 1 IRU IAW AMM. REPLACED CAPTAIN`S RDMI IAW AMM DUE TO INTERMITTENT HDG FLAG. OPS CHECKED GOOD. PERFORMED TEST OF NR 2 EFIS MAP MODE IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,341 hrs · 52,547 cycles

COCKPIT AND GALLEY EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERIES IN THE EMERGENCY LIGHT MODULE. CHECKED GOOD.

Part: ACTUATOR — LEAKING (MLG) · airframe 70,037 hrs · 52,320 cycles

ON ARRIVAL AT GATE, DETECTED A BURNING, ACRID HYD FLUID ODOR IN COCKPIT. FOUND LEFT MAIN GEAR RETRACT ACTUATOR LEAKING. TIGHTENED LINES. CLEANED APU INLET AND PERFOMED A DUCT BURNOUT.

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 69,989 hrs · 52,298 cycles

EMERGENCY LIGHTS ROW 18 D-E AND 28-D-E INOPERATIVE. REPLACED THE LIGHT ASSY. REPLACED THE LIGHTT EXTENSION 28 D-E. TESTED NORMAL.

Part: SWITCH — FAILED (MLG HANDLE) · airframe 69,928 hrs · 52,249 cycles

DURING APPROACH, WHEN THE GEAR HANDLE WAS PLACED DOWN THE 3 RED UNSAFE LIGHTS STAYED ILLUMINATED. THE ALTERNATE GEAR EXTEND WAS USED AND THE 3 GREEN SAFE LIGHTS ILLUMINATED. THE AIRCRAFT WAS LANDED WITH THE GEAR DOORS DOWN. MAINTENANCE FOUND THE LANDING GEAR HANDLE TO BE STIFF AND CHECKED THE LINKAGE AT LANDING GEAR CONTROL VALVE IN RIGHT WHEEL WELL WITH NO DEFECTS NOTED. THE LANDING GEAR CONTROL CABLES WERE INSPECTED AND NO DEFECTS WERE NOTED. THE LANDING GEAR HANDLE SWITCH S1-89 WAS REPLACED. A GEAR SWING WAS PERFORMED AND ALL CHECKED OKAY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 69,149 hrs · 51,679 cycles

SHIP 0963 REPORTED SMOKE ODOR DURING LAST 7 MINUTES OF FLIGHT WITH RT AFT LAVATORY SMOKE DETECTOR SOUNDING. NO SMOKE WAS VISIBLE OR SOURCE LOCATED. ON GROUND, SMOKE DETECTOR WOULD NOT TEST. REPLACED BOTH AFT LAVATORY SMOKE DETECTORS AND COMPLETE DUCT BURNOUT ACCOMPLISHED ALONG WITH COALESCER BAGS CHANGE. NO FURTHER ODOR APPARENT. MAINTENANCE DID FIND A HYDRAULIC LINE LEAKING AND THIS WAS REPAIRED.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 69,078 hrs · 51,626 cycles

EMERGENCY LIGHT INOPERATIVE AT 12D. PINNED THE CONNECTOR IAW SWPM 20. OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,820 hrs · 51,413 cycles

SEAT MOUNTED EMERGENCY LIGHTS FROM ROW 1 THROUGH ROW 12 INOPERATIVE. REPLACED BATTERY PACK.

Part: SKIN — DAMAGED · airframe 68,609 hrs · 51,254 cycles

DURING X-RAY INSPECTION OF APB SPLICE, FOUND LT SPLICE LOCATION BETWEEN LONGERONS 26-27L WITH 2-4 FASTENER CONFIGURATION. MARKED SPLICE LINE ON APB SKIN. REPAIRED IAW PRI 549408-14 REV 0 AND COMPLIED WITH ERA 549408-14 REV ORIG.

Part: SKIN — DAMAGED (RUDDER) · airframe 68,609 hrs · 51,254 cycles

RUDDER EXTERIOR SKIN BONDED REPAIR DOUBLER COMING APART/PEELING OFF ON RT SIDE. REPLACED RUDDER ASSY IAW MM 27-20-01. RTS AND SENSOR CHECK ACCOMPLISHED ON AMDS CARD 2210-7849.

Part: WIRE — PULLED (EMERGENCY LIGHTS) · airframe 68,233 hrs · 50,957 cycles

FOUND EMERGENCY LIGHTS INOPERATIVE FROM 1C TO 12D. FOUND WIRES PULLED FROM CONNECTOR AT BOTTOM OF SEAT LEG 1D. REPAIRED WIRES IAW SWPM 20-10-03. NO HELP. R & R FIRST CLASS BATTERY CHARGER IAW AMM 33-53. OPS CHECK NORMAL. OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 67,809 hrs · 50,633 cycles

MAINTENANCE FOUND THE EMERGENCY PATH LIGHT AT SEAT ROW 17DE INOPERATIVE. MAINTENANCE RESECURED THE SEAT CONNECTOR. THE EMERGENCY PATH LIGHT CHECKED OK.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 67,809 hrs · 50,633 cycles

CVG MAINTENANCE FOUND THE EMERGENCY PATH LIGHT AT SEAT ROW 1CD INOPERATIVE. MAINTENANCE RESECURED THE SEAT CONNECTOR. THE EMERGENCY PATH LIGHT CHECKED OK.

Part: LIGHT — INOPERATIVE (ROW 11) · airframe 67,686 hrs · 50,568 cycles

THE FLIGHT CREW OF FLIGHT 1378, FOUND AN EMERGENCY EXIT PATH LIGHT INOPERATIVE AT SEAT ROW 11. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 11. THE LIGHT CHECKED OK.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 65,395 hrs · 48,898 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE SEAT ROW 16ED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN CONNECTOR AND THE LIGHTS TESTED SATISFACTORILY.

Part: CABLE — OUT OF TOLERANCE (CONTROL COLUMN) · airframe 64,653 hrs · 48,373 cycles

DURING APPROACH THE CONTROL COLUMN STICKS IN PITCH AT 140KTS WHEN COLUMN PULLED BACK, REPEATED 5 TIMES. MAINTENANCE CHECKED ELEVATOR SYS AND INSPECTED FOR BROKEN/BINDING PULLEYS IN THE UPPER TAIL, UNDER COCKPIT FLOOR, AND BAG BIN CEILINGS. NO PROBLEMS WERE FOUND. INSPECTED ELEVATOR BOOSTED ACTUATOR ATTACHING HARDWARE AND NO PROBLEM WAS FOUND. ELEVATOR CABLES 3, 4, 5, AND 6 EACH HAD LOW TENSION BY 10LBS. ADJUSTED CABLE TENSIONS IAW AMM 27-30-00. SAFETIED AND INSPECTED CABLES AND CABLE ROUTING. NO DEFECTS FOUND.

Part: OVEN — ODOR (GALLEY) · airframe 63,588 hrs · 47,586 cycles

F/A REPORTED THAT THE FORWARD GALLEY OVEN SMOKED DURING OPERATION AND DESCRIBED IT AS AN ELECTRICAL ODOR. CABIN CREW ADVISED THE COCKPIT THAT THE OVEN WAS TURNED OFF AND THE CIRCUIT BREAKER WAS PULLED. GALLEY POWER WAS TURNED OFF. INSPECTION OF GALLEY OVEN ELECTRICAL PLUG/OUTLET COMPLETED AND NO TROUBLE WAS IDENTIFIED WITH IT, REPLACED THE OVEN.

Part: INDICATOR — MALFUNCTIONED (BRAKE PRESSURE) · airframe 63,512 hrs · 47,540 cycles

AFTER GEAR EXTENSION, LT & RT BRAKE PRESSURE DROPPED TO 800PSI. HYDRAULIC QUANTITY AND PRESSURE WERE NORMAL. CREW DECLARED EMERGENCY. BRAKES OPERATED NORMALLY DURING LANDING ROLLOUT. MAINTENANCE R & R THE BRAKE PRESSURE INDICATOR.

Part: CUSP WEB — CORRODED (BS 769-788) · corrosion level 2 · airframe 63,503 hrs · 47,536 cycles

CORROSION ON PREVIOUS REPAIR OF RT CUSP WEB X=-54 TO X=60, BETWEEN BS 769 - 788. CORROSION WAS REMOVED IAW SRM 51-30-2, 55-05, FIG 13 1A-13, 51-10-3 PAR 14 AND 21, AND 51-10-3, PAR 38 AND PS 900-5-1 N 04.

Part: BUSHING — CORRODED (BLANKET MOUNT) · corrosion level 2 · airframe 63,401 hrs · 47,459 cycles

CORROSION FOUND ON LT WING HEATER BLANKET AFT MOUNTING BUSHINGS. MOUNTING BUSHING REMOVED AND REPLACED IAW EA 04-070683-03 AD REV L.

Part: HEATER BLANKET — DEBONDED (WING) · airframe 63,397 hrs · 47,456 cycles

DEBONDS OF, 12.000" X 0.500", IN OTBD EDGE AFFECTED FOR VOID OF 115 SQUARE", 14.000" X 0.500" IN OTBD EDGE AFFECTED FOR VOID OF 185 SQUARE", 55.000" X 0.500" IN INBD EDGE AFFECTED FOR VOID OF 1104 SQUARE", 12.000" X 0.500" IN INBD EDGE AFFECTED FOR VOID OF 45 SQUARE", ON RT WING HEATER BLANKET, SM CARD 10, ZONE 0, SUMMARY. REPAIR WAS ACCOMPLISHED IAW ETI 88-14-071, REV 7, ER/A 526807-14, REV ORIGINAL.

Part: HEATER BLANKET — OUT OF LIMITS (WING) · airframe 63,397 hrs · 47,456 cycles

DURING INSPECTION, VOIDS WERE FOUND OF 24.6 PERCENT THEREFORE THIS LT HEATER BLANKET IS OUT OF LIMITS IAW FIG 1 VOIDS ACCEPTANCE CRITERIA, 1, A. CARD 3, ZONE 00. THIS NRC WAS ACCOMPLISHED IAW ETI -88-14-071, REV 7, ER/A 526807-14, REV ORG.

Part: HEATER BLANKET — OUT OF LIMITS (WING) · airframe 63,397 hrs · 47,456 cycles

DURING INSPECTION, VOID WERE FOUND OF 25 PERCENT THEREFORE THIS RT HEATER BLANKET IS OUT OF LIMITS IAW FIA. 1 VOIDA ACCEPTANCE CRITERIA 1, A CARD 4, ZONE 00. REPAIR WAS ACCOMPLISHED IAW ETI 88-14-071, REV 7 & ER/A 526807-14, REV ORIGINAL.

Part: STRUCTURE — DEBONDED (LT WING) · airframe 63,397 hrs · 47,456 cycles

DEBONDS OF 9.00" X 0.500" IN OTBD EDGE AFFECTED FOR VOID OF 16 SQUARE IN AND 58.00 X .0500" IN INBD EDGE AFFECTED FOR VOID OF 877 SQUARE IN ON LT WING HEATER, SM CARD 9, ZONE 00 SUMMARY. THIS NRC WAS ACCOMPLISHED IAW ETI-88-14-071, REV 7, ER/A 526807-14, REV ORG.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 63,401 hrs · 47,459 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND THAT THE EMERGENCY ESCAPE PATH LIGHTS WERE INOPERATIVE AT G2. THE WIRING WAS REPAIRED AND THE LIGHTS RETURNED TO AN OPERATIONAL STATE.

Part: FORMER — CORRODED (APU DOOR) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FORMERS OF RT APU DOOR. DAMAGE FORMERS WERE REMOVED, FABRICATED AND INSTALLED IAW DWG 5914654, & SRM 51-30-2.

Part: FAIRING — CRACKED (VERTICAL STAB) · airframe 63,395 hrs · 47,455 cycles

LT UPPER FAIRING CRACKED, CRACK STOP DRILLED, REPAIR DOUBLER FABRICATED, REPAIR TREATED, PAINTED, AND INSTALLED IAW RA/524672-14, REV ORIGINAL.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 63,395 hrs · 47,455 cycles

LOW BRIGHTNESS ON 2 SELF ILLUMINATED EXIT SIGNS AT PASSENGER CABIN. BOTH REPLACED.

Part: SKIN — CORRODED (BS 750-788) · airframe 69,249 hrs · 51,754 cycles

SKIN REPAIR AT BS 750-788 L26-L29R CORRODED. REPAIRED IAW SRM 53-04 57, ETI -800-14-090 AND ER/A 525378-14 REV. ORIG.

Part: FRAME — CRACKED (BS 446) · airframe 63,395 hrs · 47,455 cycles

CRACK ON FRAME BS 446 BETWEEN LONGERONS 19 - 20RT. DAMAGE WAS REMOVED AND NEW SECTION OF FRAME WAS INSTALLED IAW SRM 53-03D, FIG 2A.

Part: FITTING — CORRODED (RT AILERON) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION FOUND ON RT AILERON SECTOR FITTING UPPER BORE. CORROSION REMOVED AND BUSHINGS FABRICATED IAW ER/A 524801-14, REV ORIGINAL.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,395 hrs · 47,455 cycles

CRACK ON LONGERON 12L AT FRAME BS 1437. NEW SECTION OF LONGERON WAS REPLACED IAW SRM 51-30-2, 51-10-3, PAR 14 AND 21, AND DWG 5911433, REV B5.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FRAME BS 1309 BETWEEN LONGERONS 29LT-29RT. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-03, FIG. 2A, 51-10-4, 51-10-3 PAR. 21, 14, PS-900-5-1, NR 04, 51-30-5, 51-10-3 PAR. 38.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON LOWER TEE FITTING OF FRAME BS 1380 LONGERONS 28LT - 28RT. FRAME REPLACED IAW DWG 9912246, REV DE AND ER/A 525569-14 REV. ORIG. ETI 88-14-085 REV 2.

Part: FRAME — CRACKED (BS 1510) · airframe 63,395 hrs · 47,455 cycles

CRACK ON FRAME BS 1510. FRAME REPLACED IAW SRM 51-30-2 AND DWG 9911843, REV AC.

Part: FRAME — CRACKED (BS 1510) · airframe 63,395 hrs · 47,455 cycles

CRACK ON FRAME BS 1510, BETWEEN LONGERONS 1 & 2R. FRAME REPLACED IAW SRM 51-3-2 AND DWG 9911843, REV AC.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PANEL 1365C AT COUNTER-SINK HOLES AND SETTLEMENT AREA. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL REPLACED.

Part: ATTACH FITTING — CRACKED (BS 1437) · airframe 63,395 hrs · 47,455 cycles

CRACK .125 INCHES, ON LT DORSAL FIN ATTACH FITTING LOCATED ON UPPER AFT SIDE OF BS 1437 BULKHEAD. LEFT DORSAL FITTING WAS REPLACE IAW SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PANEL 1363C AT SETTLEMENT AREA AND COUNTERSINK HOLES. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-22-2A, ACCESS PANEL REPLACED.

Part: INTERCOSTAL — CORRODED (BS 769-788) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 769-788 AND LONG 28R AT MID CARGO COMPARTMENT. INTERCOSTAL REPLACED IAW SRM 51-30-2, 51-30-5, AND 53-24-0D.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PLATE 1357C AT SETTLEMENT AREA AND COUNTERSINK HOLES. CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA FUEL ACCESS DATE NR 1357C WAS REMOVED AND IS OUT OF LIMITS IAW SRM 51-22-2A. FUEL ACCESS PLATE WAS REPLACED.

Part: SPACER — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON PREVIOUS REPAIR SPACER OF LOWER MID CARGO DOOR FRAME BS 636-693. SPACER WAS REPLACED IAW SRM 53-05, FIG 123.

Part: BEAM — CRACKED (SERVICE DOORWAY) · airframe 63,395 hrs · 47,455 cycles

CRACKED NR 1BEAM AFT EDGE AT FORWARD SERVICE DOOR. IN REF CARD 28 ZONE 58. FITTING, RETAINER, SEAL, AND BEAM WERE REMOVED IAW SRM 51-30-1 AND 51-30-2. NEW BEAM WAS DRILLED IAW SRM 51-40-0, NEW BEAM WAS TREATED AND PAINTED IAW SRM 51-40-3 PARA 14 AND 21, NEW BEAM WAS INSTALLED IAW SRM 51-30-2, AND FITTING, RETAINER, AND SEAL WERE INSTALLED IAW SRM 51-30-1 AND 51-30-2.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON RT HORIZONTAL STABILIZER BARREL NUT HOLE. CORROSION REMOVED AND BUSHINGS FABRICATED IAW SRM 55-03D PAR 30.

Part: SKIN — CRACKED (BS 1474) · airframe 63,395 hrs · 47,455 cycles

CRACKED FUSELAGE SKIN BS 1474 LONGERONS 21 - 22R CRACKED. REPAIRED IAW SRM 53-01, FIG 02.

Part: DOUBLER — CRACKED (DOOR FRAME) · airframe 63,395 hrs · 47,455 cycles

CRACK ON INTERNAL DOUBLER AT LOWER AFT DOOR FRAME CORNER BS 423.5 IN PROJECTION LONGERON 27R. REPAIRED IAW SRM 53-05, FIG 105 AND ER/A 525564-14 REV ORIG.

Part: ATTACH ANGLE — CRACKED (BS 1406-1435) · airframe 63,395 hrs · 47,455 cycles

CRACKS ON DORSAL FIN ATTACH ANGLE OF BS 1406 - 1435 LONGERONS 1- 2L. ATTACH ANGLE WAS REPLACED IAW DWG 591288, REV BD AND SRM 51-30-5.

Part: SKIN — CRACKED (NR 2 SLAT) · airframe 63,395 hrs · 47,455 cycles

CRACKED INNER SKIN ON SLAT PANEL 2, XOS 222. DAMAGE REMOVED IAW SRM 57-09, FIG 108. DOUBLER AND FILLER WERE FABRICATED IAW SRM 57-09, FIG 10B. REPAIR TREATED, PAINTED AND INSTALLED IAW SRM 51-10-3, PAR 14/21 AND SRM 57-09, FIG 10B.

Part: ATTACH ANGLE — CRACKED (VERT TO FUSE) · airframe 63,395 hrs · 47,455 cycles

CRACKED ANGLE TO ATTACH TOP FUSELAGE TO VERTICAL STAB RT SIDE STA Y=1405 AND Y=1437 APPROXIMATELY, H1L1-SM, CARD 168, ZONE 100. ANGLE WAS REPLACE IAW DWG 5912188, REV BD AND SRM 51-30-5. RETAIN FOR RECORDS BY PRIMARY STRUCTURE.

Part: INTERCOSTAL — CORRODED (BS 1149-1155) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 1149-1155 LONGERONS 29-30R. CORROSION ON INTERCOSTAL, FASTENER AN INTERCOSTAL WERE REMOVED, DUE TO EXCCESIVE DAMAGE BE REPLACED, NEW INTERCOSTAL WAS DRILLED, AREA WAS TREATED AND PAINTED, NEW INTERCOSTAL WAS INSTALLED CIC WAS APPLIED IAW SRM 51-30-2 51-30-5, 51-10-3 PAR 21, 14 AND 38.

Part: SEAT TRACK — CORRODED (BS 1155-1206) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON SEAT TRACK BS 1155-1206. CORROSION REMOVED IAW SRM 51-10-3, PAR 26 AND FOUND OUT OF LIMITS. SEAT TRACK REPLACED IAW SRM 51-10-4, SRM-51-30-2, 51-30-1, AND51-30-5.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,395 hrs · 47,455 cycles

CRACK ON MID CARGO COMPARTMENT DOOR OUTER AFT PAN BELLOW STOP FITTING NR 4. MID CARGO COMPARTMENT DOOR OUTER AFTER PAN BELOW STOP FITTING NR 4 WAS REPAIRED IAW SRM 52-05, FIG 50.

Part: FLOOR SUPPORT — CORRODED (BS 1174-1193) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 1174-1193 IN AFT CARGO BAY. FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-4, 51-10-3 PARS 21 AND 14, 51-30-1 AND 51-30-2 AND DWG 5936660, REV BZ.

Part: LONGERON — CRACKED (BS 997) · airframe 63,395 hrs · 47,455 cycles

CRACKED OTBD LONGERON 20L BS 997 ABOVE LT MLG W/W. LONGERON REPAIRED IAW SRM 53-02, FIG 22.

Part: ACCESS PANEL — CORRODED (WING) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON COUNTERSINKS OF FUEL TANK ACCESS PANEL 1454C. CORROSION REMOVED IAW SM 51-22-2A AND FOUND OUT OF LIMITS. ACCESS PANEL WAS REPLACED.

Part: ANGLE — CRACKED (BS 1451) · airframe 63,395 hrs · 47,455 cycles

CRACKED FRAME ANGLE AT BS 1451 BETWEEN LONGERONS 3, 4, 6, 7L, & 5 - 6R IN AFT ACCESSORY BAY, FRAME ANGLES REMOVED IAW SRM 51-30-2 AND NEW FABRICATED IAW DWG 9911960-9 AND 10. INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: DOUBLER — CRACKED (BS 1451) · airframe 63,395 hrs · 47,455 cycles

CRACK ON REPAIR DOUBLER BS 1451 BETWEEN LONGERONS 1 - 3L IN AFT ACCESSORY BAY. DOUBLER REMOVED IAW SRM 51-302. DOUBLER FABRICATED IAW D DING 991/860, REV L. DOUBLER INSTALLED IAW SRM 51-36-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON RT FUEL ACCESS PANEL 1462C. CORROSION REMOVED IAW SRM 51-22 2A. FOUND OUT OF LIMITS IAW SRM 51-22-2A. FUEL ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PANEL 1410C. CORROSION REMOVED IAW SRM 51-22-2A. FOUND OUT OF LIMITS IAW SRM 51-22-2A. FUEL TANK ACCESS PANEL WAS REPLACED.

Part: LONGERON — CORRODED (BS 1321) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON LONGERON, RT AND LT SIDE, AT BS 1321. LONGERON SECTION WAS REPLACED IAW SRM 53-14-3, FIG 4: 51-10-3, PAR 21 AND 14, & 51-30-2 AND 51-30-5 AND DWG 5936667, REV CD.

Part: CUSP WEB — CRACKED (BS 249) · airframe 63,395 hrs · 47,455 cycles

CRACKED RT CUSP WEB LOWER SURFACE BS 249. CUSP WEB REPLACED IAW SRM 51-30-2, 51-30-5 AND 51-30-1 AND ER/A 525372-14 REV ORIG.

Part: FRAME — CORRODED (BS 1320) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FRAME BS 1320, LONGERON 30 AT AFT CARGO BAY. FRAME WAS REPAIRED IAW SRM 53-03, FIG 2A.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,395 hrs · 47,455 cycles

LONGERON 18L CRACKED AT BS 1437 AFT ACCESSORY BAY. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,395 hrs · 47,455 cycles

CRACK FOUND ON LONGERON 3L BS 1437 IN AFT ACCESSORY BAY. SECTION OF LONGERON REMOVED IAW SRM 51-30-2 AND 51-30-5. A NEW LONGERON SECTION WAS FITTED AND DRILLED IAW SRM 53-02, FIG 18. A NEW SPLICE WAS FABRICATED IAW SRM 53-01, FIG 18. NEW SPLICE AND LONGERON SECTION TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14. NEW SPLICE AND LONGERON SECTION INSTALLED IAW SRM 51-30-2 AND 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,395 hrs · 47,455 cycles

CRACK ON LONGERON 4R BS 1437 IN AFT ACCESSORY BAY. SECTION OF LONGERON REMOVED IAW SRM 52-30-2 AND 51-30-05 AND A NEW SECTION WAS FITTED AND DRILLED IAW SRM 53-02, FIG 18. NEW SPLICE FABRICATED IAW SRM 53-02, FIG 18. NEW SPLICE AND SECTION OF LONGERON INSTALLED IAW SRM 51-30-2 AND 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,395 hrs · 47,455 cycles

CRACK FOUND ON LONGERON 3R BS 1437 IN AFT ACCESSORY BAY. SECTION OF LONGERON REMOVED IAW SRM 51-30-2 AND 51-30-5. NEW LONGERON SECTION WAS FITTED AND DRILLED IAW SRM 53-02, FIG 18. A NEW SPLICE WAS FABRICATED IAW SRM 53-02, FIG 18. NEW SPLICE AND LONGERON SECTION TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14. NEW SPLICE AND LONGERON SECTION INSTALLED IAW SRM 53-02, FIG 18 AND 51-30-2.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,395 hrs · 47,455 cycles

CRACK FOUND ON LONGERON 4L BS 1437 IN AFT ACCESSORY BAY. SECTION OF LONGERON WAS REMOVED IAW SRM 51-30-2 AND 51-30-05 AND A NEW SECTION WAS FITTED AND DRILLED IAW SRM 53-02 FIG 18. A NEW SPLICE WAS FABRICATED IAW SRM 53-02 FIG 18. NEW SPLICE AND LONGERON SECTION WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 21 AND 14. NEW SPLICE AND LONGERON SECTION WERE INSTALLED IAW SRM 53-02 FIG 18 AND 51-30-2.

Part: FRAME — CRACKED (BS 1437) · airframe 63,395 hrs · 47,455 cycles

CRACK ON FRAME AT BS 1437 BETWEEN L8-9L IN AFT ACCESSORY COMPARTMENT. CRACK ON FRAME WAS REPAIRED IAW ER/A 519146-14 MA REV ORIGINAL.

Part: ACCESS PANEL — CORRODED (WING) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PANEL 1367C AT COUNTERSINK HOLES AND SETTLEMENT AREA. CORROSION REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS IAW SRM 51-22-2A ACCESS PANEL WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 946-984) · airframe 63,395 hrs · 47,455 cycles

DAMAGE ON CUSP WEB BS 946-984. CUSP WEB BLENDED OUT. FOUND OUT OF LIMITS, REPAIRED IAW SRM 53-05, FIG 131A-13 .

Part: ANGLE — CORRODED (BS 200) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON ANGLE BS 200 X=-54. REMOVED AND REPLACED ANGLE IAW SRM 53-05, FIG 55.

Part: SKIN — CORRODED (BS 1085-1134) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON WING TO FUSELAGE FAIRINGS RUB STRIP SETTLEMENT AREA RT FROM BS 1085 - 1134 BETWEEN LONGERONS 28-30R. ANCHOR NUTS WERE REMOVED. CORROSION REMOVED AND FOUND WITHIN LIMITS IAW SRM 53-4, PAR 57 B (2)(A) AND DWG 5936033.

Part: ACCESS PANEL — CORRODED (WING) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PANEL 1361C. CORROSION REMOVED IAW SRM 51-22-2A. FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL REPLACED AND INSTALLED.

Part: CUSP WEB — CORRODED (BS 1150-1193) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON CUSP WEB, BS 1150-1174 AND 1174-1193 BETWEEN X=-54 AND X-60. REPAIRED IAWJRM 51-10-3, PARAY 26-14-21 AND SRM 53-05, FIG 131 AS.

Part: SKIN — CORRODED (BS 788-802) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON WING TO FUSELAGE FAIRINGS RUB STRIP SETTLEMENT AREA RT FROM BS 788-802 BETWEEN LONGERONS 28-29. ANOHER NUT AND FASTENERS WERE REMOVED, CORROSION REMOVED AND FOUND WITHIN LIMITS IAW SRM 53-4, PAR 57 B 2, A AND DWG 5936046, REV "A".

Part: DOOR FRAME — CRACKED (NLG WW) · airframe 63,395 hrs · 47,455 cycles

CRACKED NLG WW RT DOOR FRAME AT BS 46. DAMAGE REMOVED, REPAIR FABRICATED AND INSTALLED IAW SRM 53-05, FIG 110.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON LT FUEL ACCESS PANEL 1371C COUNTERSINK HOLE. ACCESS PANEL REPAIRED IAW SRM 51-22-2A, PAR 6, CONDITION II.

Part: LONGERON — CORRODED (BS 1321) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON LONGERON 30R BS 1321. LONGERON SECTION WAS REPLACED IAW SRM 53-14-3, FIG 4, 51-10-3 PAR 21 AND 14, 51-30-5 AND 51-30-2.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 63,395 hrs · 47,455 cycles

CRACKED FWD AND AFT SPAR SUPPORT OF MID CARGO COMPARTMENT DOOR BARRIER. SPARS SUPPORT WERE REMOVED IAW SRM 51-10-4 NEW SPARS SUPPORT WERE DRILLING IAW SRM 51-10-4 SUPPORT WERE TREATED AND PAINTED IAW SRM 51-10-3 SPARS SUPPORTS WERE INSTALLED IAW SRM 51-30-1.

Part: SPAR — WORN (CARGO DOOR) · airframe 63,395 hrs · 47,455 cycles

WORN FWD AND AFT SPARS AT MID CARGO DOOR BARRIER. SPARS WERE REMOVED IAW SRM 51-30-1. SPARS WERE FABRICATED IAW SRM 53-24-0, PAGE 26, FIG -13. SPARS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14/21. SPARS WERE INSTALLED IAW SRM 51-30-2 AND 51-30-1. RE-WRITE TO CARD 240, ZONE 100 AND 20000014581.

Part: ACCESS PANEL — CORRODED (WING) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PANEL 1460C. COOROSION REMOVED IAW SRM 51-22-2A. FOUND OUT OF LIMITS IAW SRM 51-22-2A. FUEL ACCESS PANEL WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 906) · airframe 63,395 hrs · 47,455 cycles

CRACK WAS FOUND 0.390" ON RT CUSP WEB UPPER SURFACE AT BS 906 X=-55. DAMAGE REMOVED, REPAIR PARTS FABRICATED, REPAIR TREATED AND PAINTED, NEW REPAIR INSTALLED, SPLICE AND FASTENERS INSTALLED IAW SRM 51-30-2 AND 51-30-5, 53-05, FIG 131A-1, 51-10-3, PAR 14 AND 21.

Part: CUSP WEB — CORRODED (BS 1231-1271) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON CUSP WEB, BS 1231-1250 AND BS 1250-1271 BETWEEN X=-54 AND X=-60. DAMAGED REMOVED, REPAIRS FABRICATED, REPAIRS TREATED AND PAINTED, REPAIRS INSTALLED IAW SRM 53-05, FIG 131A-13, 51-10-3, PAR 14 AND 21 AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 1193-1212) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON RT CUSP WEB UPPER SURFACE, BS 1193 -1212 BETWEEN X= -54 AND X=-60. REMOVED CORROSION, FABRICATED REPAIR DOUBLER IAW SRM 53-05, FIG 131 A-5, TREATED PRIMED NEW REPAIR IAW SRM 51-10-3 PARA 14 & 21. INSTALLED REPAIR IAW SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 1099-1102) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON RT CUSP WEB BETWEEN BS 1099-1102 AND X=-54 - X=-60. CUSP WEB REPAIRED IAW SRM FIG 131A-10.

Part: TAB — DELAMINATED (RUDDER) · airframe 63,395 hrs · 47,455 cycles

DELAMINATED RUDDER CONTROL TAB UPPER CORNER. RUDDER CONTROL TAB WAS REPAIRED IAW SRM 51-70-1A, PAR 23 AND JIC CARD 2000-8149-03, JOB 000-0047 AND SRM 51-90-0, PARA 1-5E.

Part: CUSP WEB — CORRODED (BS 844-846) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON RT CUSP WEB UPPER SURFACE BS 844-846 BETWEEN X=-54, X=-60 AT PAX CABIN. FASTENERS WERE REMOVED. DAMAGE ON STA Y= 836 TO 845 WAS REMOVED. NEW REPAIR PARTS WAS FABRICATED NEW REPAIR PARTS WAS TREATED AND PAINTED AND THE NEW REPAIR PARTS WAS INSTALLED IAW SRM 51-30-2 AND SRM 51-10-1, PAR 14 AND 21 ALSO SRM 53-05, FIG 131, A -4 AREA WAS IDENTIFIED IAW PS900-5-1 NR 04.

Part: CUSP WEB — CORRODED (BS 655-712) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON RT CUSP WEB UPPER SURFACE BS 655-674, Y=674-693, BS 693-712 BETWEEN X=-54 TO X=-60. CORROSION REMOVED, AREA WORKED AND CRACKS FOUND 3.4" , 3.5", 2 1" X 15", 3 A 1X2, DOUBLER AND FILLER FABRICATED, AREA TREATED AND PAINTED. REPAIRS INSTALLED IAW SRM 51-30-2 AND 51-30-5, PAR 26 51-70-04, FIG 2, 51-10-3 PAR 14-21.

Part: ANGLE — CORRODED (BS 200) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON ANGLE BS 200 X=-54 . REMOVED AND REPLACED ANGLE IAW SRM 53-05, FIG 55 AND 51-10-3 PAR 14 AND 21.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,401 hrs · 47,459 cycles

DURING HEAVY CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT IN CEILING AT ROW 11 INOPERATIVE. MAINTENANCE REPLACED THE LAMP AND THE FUNCTIONAL TESTED GOOD.

Part: STRUCTURE — CORRODED (RT WING TE FLAP) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FLEX JOINT LINK AT RT WING INBD FLAP. CORROSION REMOVED IAW SRM 51-10-3, PAR 26 AND FLEX JUINT LINK WAS MEASURED, THE MAX DIAMETER OF HOLE IS 0.194" AND DIAMETER MEASURED 0.211" THEREFORE IT IS OUT OF LIMITS IAW DWG NR 5935915 AND FLEX JUINT LINK WAS R & R FOR NEW LINK IAW AMM- 27-51-07, JOB COMPLETED.

Part: FAIRING — CORRODED (WING TO BODY) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON WING TO FUSELAGE FAIRINGS, RUB STRIP SETTLEMENT AREA RT FROM STA Y=727 TO Y=747 BETEEN LONG 22-LONG 26 RT, MRB 53-100-01, H1L1-SM, CARD 204 ZONE 100. CORROSION WAS REMOVED AND REWORKED AREA WAS MEASURED TREATED AND PAINTED IAW SRM 51-10-3 PAR 26, 21 AND 14. UT, WAS ACCOMPLISHED ORIGINAL THICKNESS BETWEEN 727-747 AREA 0.063" AND MINIMUM REMAINING THICKNESS AREA 0.059". AREA IS WITHIN LIMITS IAW SRM 53-04, PAR 57B 2, A AND WG 5936046, REV A. PERFORMED VISUAL, INITIALLY WITHIN 8000 CYCLES AFTER WITH REPETITIVE INTERVAL OF 8000 CYCLES IAW SRM 53-04, PAR 57D.

Part: CUSP WEB — CORRODED (CABIN) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON LT CUSP WEB. CUSP WEB WAS REMOVED, AND A NEW CUSP WEB WAS DRILLED AND INSTALLED IAW SRM 51-10-3, PAR 14, 21, 38, 51-30-2, 51-30-5, 51-30-1.

Part: FRAME — CRACKED (BS 1437) · airframe 63,395 hrs · 47,455 cycles

CRACKED ON ANGLE OF FRAME, BS 1437 BETWEEN LONGERONS 1 - 2 R. ANGLE REMOVED, HFEC INSPECTED, TREATED AND PAINTED AND ANGLE INSTALLED IAW SRM 51-30-5, 51-10-3 PAR 14 AND 21.

Part: ACCESS PANEL — CORRODED (WING) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PANEL NR 1409C. ACCESS PANEL REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (WING) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PANEL NR 1303C, ACCESS PANEL REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CORRODED (BS 642) · airframe 69,249 hrs · 51,754 cycles

CUSP WEB CORROSION BS 642, X -54 TO -60. DAMAGE REMOVED , DOUBLER REPAIR INSTALLED.

Part: LONGERON — CRACKED (BS 1338) · airframe 63,395 hrs · 47,455 cycles

CRACKED LONGERON 1 BS 1338. LONGERON REPLACED IAW SRM 51-30-5 AND DWG.

Part: CUSP WEB — CORRODED (BS 560-579) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON PREVIOUS REPAIR OF CUSP WEB BETWEEN BS 560-579 AND X=-54-X=-60 AT PASSENGER CABIN FLOOR STRUCTURE, SM, IN REF ORNRC 76, ZONE 201 / 20000010594, MRB 53-037-01, CARD 264, ZONE 201. FASTENERS WERE REMOVED NEW REPAIR PARTS WAS FABRICATED, NEW REPAIR PARTS WAS TREATED AND PAINTED ALSO NEW REPAIR PARTS WAS INSTALLED IAW SRM 51-30-5 AND 51-10-3, PAR 14-21, ALSO SRM 53-05, FIG 131A-14 AREA WAS IDENTIFIED IAW PS 900-5-1, NR 04.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PLATE NR 1307C AT COUNTERSINK HOLES SETTLEMENT AREA (AYP) IN REF CARD 42, ZONE 00, MBR 57-083-02, H1L1-AYP, CARD78, ZONE 00. CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA WERE REMOVED IAW SRM 51-22-2A. COUNTERSONK HOLES WERE MEASURED MAX DIAMETER ALLOWABLE IS 0.660" AND MAX DIAMETER MEASURED IS 0.747" IN 7 HOLES, THEREFORE IT IS OUT OF LIMITS IAW SRM. FUEL TANK ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120, JOB 001-0385.

Part: ACCESS PANEL — CORRODED (WING) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PANEL NR 1414C. CORROSION REMOVED IAW SRM 51-22-2A. FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL REPLACED.

Part: CUSP WEB — CORRODED (BS 495) · airframe 69,249 hrs · 51,754 cycles

RIGHT CUSP WEB CORRODED BS 495, X -54 TO -60. DAMAGE REMOVED DOUBLER AND A NEW REPAIR INSTALLED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PLATE NR 1355C AT SETTLEMENT AREA AND COUNTERSINK HOLES IN REF CARD 42, ZONE 00. CORROSION ON COUNTERSINK HOLES ON SETTLEMENT AREA WERE REMOVED IAW SRM 51-22-2A COUNTERSINK HOLES WERE MEASURED MAX DIAMETER IS .532" NAD MAX DIAMETER MEASURED IS .600" IN (3) ADJACENT HOLES THEREFORE IT IS OUT OF LIMITS IAW SRM 51-22-2A, FUEL TANK ACCESS DOOR IAW REPLACED AND WILL BE INSTALLED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PLATE NR 1470 AT COUNTERSINK HOLES AND SETTLEMENT AREA, AYP, IN REF CARD 41, ZONE 00, MRB 57-083-02, H1L1-AYP, CARD 82, ZONE 00. CORROSION ON FUEL ACCESS PLATE NBI 1470 ON COUNTERSINK HOLES AND SETTLEMENT AREA WERE REMOVED IAW SRM 51-22-2A. COUNTERSINK HOLES WERE MEASURED MAX DIAMTER ALLOWABLE IS .532" AND MAX DIAMETER MEASURED IS 540" IN 9 HOLES, THEREFORE IT IS OUT OF LIMITS IAW SRM 51-22-2A, FUEL TANK ACCESS DOOR WAS REPLACE AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001-0391.

Part: ACCESS PANEL — CORRODED (WING) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON ACCESS PANEL NR 1456C. CORROSION REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS IAW SRM. ACCESS PANEL REPLACED.

Part: FRAME — CRACKED (BS 1338 BULKHEAD) · airframe 63,395 hrs · 47,455 cycles

CRACKED FORMER ON AFT PRESSURE BULKHEAD, STA 1338 BETWEEN LONG 7-8 AT RT AFT LAVATORY AREA, (H1L1 - SM, ZONE 58, CARD 22. SUMMARY: CRACKED FORMER WAS REMOVED AND NEW FORMER WAS INSTALLED IAW SRM 51-30-1, 51-30-2 AND 51-30-6 AND 51-10-4.

Part: PANEL — CORRODED · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON AFT INBD, OTBD RIB HOLES AT SLAT PANEL 0 STA XIS 40, LW. CORROSION ON SLAT TRACK AFT INBD/OTBD. HOLES WAS REMOVED, AND BUSHINGS WERE FABRICATED, AND TREATED AND INSTALLED IAW SRM 57-02, PAR 9, TABLE 1 AND SRM 51-10-3, PAR 21 AND SRM 51-30-10, PAR 7 AND 8.

Part: CUSP WEB — CORRODED (BS 937-943) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON LT CUSP WEB PREVIOUS REPAIR DOUBLER BETWEEN STA Y=937, Y=943, X=54, X=60 AT CABIN FLOOR STRUCTURE, MRB 53-037-01. DOUBLER WAS REPLACED IAW MD-88R SRM 53-05, FIG 131A-2.

Part: DOUBLER — CORRODED (BS 674-693) · airframe 69,249 hrs · 51,754 cycles

CORROSION ON PREVIOUS REPAIR X 54 TO 64 AND BS 674-693. REPAIR DOUBLER WAS REMOVED, AND A NEW REPAIR FABRICATED, TREATED, PAINTED AND INSTALLED.

Part: PANEL — CORRODED · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON RIB HOLES OF SLAT PANEL 1 STA XIS=136 (LW). HOLES FWD WERE CLEANED IAW PS 900-1-2-1, NR 01 AND THEREFORE OUT OF LIMITS IAW SRM 57-02, PAR 9, TABLE 1, AND CORROSION ON HOLES AFT WERE REMOVED, BUSHINGS WERE FABRICATED, AND TREATED, AND INSTALLED IAW SRM 57-02, PAR 9 AND SRM 51-10-3 PAR 21, AND SRM 51-30-10 7 AND 8. FINAL ID Q0.935" AFT.

Part: PANEL — CORRODED (SLATS) · corrosion level 2 · airframe 63,395 hrs · 47,455 cycles

CORROSION ON RIB HOLES OF SLAT PANEL 1 STA XIS=136 (LW). HOLES FWD WERE CLEANED IAW PS 900-1-2-1, NR 01 AND THEREFORE OUT OF LIMITS IAW SRM 57-02, PAR 9, TABLE 1 AND CORROSION ON HOLES AFT WERE REMOVED, BUSHINGS WERE FABRICATED, AND TREATED , AND INSTALLED IAW SRM 57-02, PAR 9 AND SRM 51-10-3, PAR 21 AND SRM 51-30-10, 7 AND 8. FINAL ID: Q 0.935" AFT.

Part: RIB — CORRODED (SLAT TRACK) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON OTBD FWD AND AFT HOLES, RIB OF SLAT PANEL 1 STA XIS=83. CORROSION WAS REMOVED IN HOLE FWD AND AFTER SLAT TRACK, BUSHINGS WERE FABRICATED,TREATED AND INSTALLED IAW SRM 57-02, PAR 9 AND SRM 51-10-3, PAR 21 AND SRM 51-30-10, PAR 7 AND 8 FINAL ID DIAMETER 1.0655 FWD AND 1.060 AFT.

Part: LONGERON — WORN (BS 1401-1418) · airframe 63,395 hrs · 47,455 cycles

WEAR FOUND ON LONGERON 8 LT BETWEEN BS 1401 - 1418 AFT ACCESSORY COMPARTMENT. LONGERON WAS BLEND OUT LONGERON IS OUT LIMITS, LONGERON WAS REMOVED, NEW LONGERON WAS ADJUSTED AND DRILLED, SPLICE WAS FABRICATED LONGERON AND SPLICE WERE INSTALLED. NEW LONGERON AND SPLICE WERE IDENTIFIED IAW SRM 53-01, 51-30-2, 51-10-4 53-02 FIG. 18, 51-10-3 PAR 14 AND 21 AND P.S. 900-5-1 NR.4. RII COMPLETED BY INSPECTION STAMP INSPECTOR HAG 200802796.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,395 hrs · 47,455 cycles

CRACK ON LONGERON 16 RT AT BS 1437 AFT ACCESSORY COMPARTMENT. (A/A) (SM) (CARD 35 ZONE 61). LONGERON CRACKED WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. LONGERON WAS DRILLED AND TRIMED IAW SRM 51-10-4. LONGERON NEW WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 141,21. NEW SECTION LONGERON WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CRACKED (BS 1437) · airframe 63,395 hrs · 47,455 cycles

CRACK ON LONGERON 16 LT AT BS 1437 AFT ACCESSORY COMPARTMENT. LONGERON CRACKED WAS REMOVED IAW SRM 51-30-5. DRILLED AND TRIMED NEW SECTION LONGERON IAW SRM 51-10-4. NEW LONGERON WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21. NEW SECTION LONGERON WAS INSTALLED IAW SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (WING) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PLATE NR 1436C AT SETTLEMENT AREA AND COUNTERSINK HOLES IN REF CARD 41, ZONE 00, MRB 57-083-02, H1L1 -AYP. CORROSION ON COUNTERSINK HOLES ON SETTLEMENT AREA WERE REMOVED IAW SRM 51-22-2A. CONTERSINK HOLES WERE MEASURED AND MAX DIAMETER ALLOWABLE IS .660" AND MAX DIAMETER MEASURED IS .796" IN (3) ADJACENT HOLES THEREFORE WAS FOUND OUT OF LIMITS IAW SRM 51-22-2A. FUEL ACCES PLATE 1436C WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001- 0391. PRIMARY STRUCTURE. CORROSION LEVEL 2.

Part: CUSP WEB — CORRODED (CABIN) · airframe 63,395 hrs · 47,455 cycles

CORROSION LT CUSP WEB BETWEEN EX=54- 64 AND STA Y=435 AT PAX CABIN, ZONE 201, CARD 40. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131A-14 REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 131A-14. REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 14 AND 21. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5. REPAIR WAS IDENTIFIED IAW PS 100-5-1 D4.

Part: ACCESS PANEL — CORRODED (WING) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON FUEL ACCESS PLATE NR 1466C AT SETTLEMENT AREA AND COUNTERSINK HOLES IN REF CARD 41, ZONE 00, MRB 57-083-02, CORROSION ON COUNTERSINK HOLES ON SETTLEMENT AREA WERE REMOVED IAW SRM 51-22-2A. CONTERSINK HOLES WERE MEASURED AND, MAX DIAMETER ALLOWABLE IS .532" AND MAX DIAMETER MEASURED IS .558" IN (3) ADJACENT HOLES THEREFORE WAS FOUND OUT OF LIMITS IAW SRM 51-22-2A. FUEL ACCES PLATE 1466C WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0390, JOB 001- 0391.

Part: WEB — CORRODED (BS 1338) · airframe 63,395 hrs · 47,455 cycles

CORROSION ON AFT SURFACE OF WEB AT BS 1338 BETWEEN LONGERONS 26RT AND 26LT AT AFT CARGO COMPARTMENT (C3) MRB 53-100-04, CARD 238, ZONE 201. FASTENERS ON AREA WERE REMOVED, CORROSION ON AFT SURFACE OF WEB WAS REMOVED. WAS ACCOMPLISHED ORIGINAL THICKNESS IS 0.040" AND REAMING THICKNESS IS 0.038" IAW ER/A 511165-14MA, REV B. REWORKED AREA WAS TREATED AND PAINTED AND NEW FASTENERS WERE INSTALLED IAW SRM 51-30-5; 51-10-3 P.26,14,21 AND 38 AND ER/A 511165-14MA, REV B. EQUIPMENT: PANAMETRICS NDT 35. TRANSDUCER: SOUOPER U2605M.

Part: CUSP WEB — CORRODED · airframe 63,395 hrs · 47,455 cycles

CORROSION ON RT CUSP WEB UPPER SURFACE, STA Y=1134-1136, Y= 1174-1193 BETWEEN X=-44 AND X=-54, H1L1-SM, MRB 53-037-01,CARD 128, ZONE 201. CORROSION WAS REMOVED IAW SRM 51-10-3, PA26 WAS ACCOMPLISHED, ORIGINAL THICKNESS MISS15 0.020" AND REMAINING THICKENESS 15 0.019" THEREFORE IS WITHIN LIMITS IAW ER/A 511165-14MA, REV-B, REWORKED AREAS WERE TREATED AND PAINTED, CIC WAS APPLIED, REPAIR WAS IDENTIFIED IAW ER/A 511165-14MA, REV-B. EQUIPMENT. PANAMETRIC NDT 35 TRANSDUCER. SONOPEN V260SM EXP DATE. 18-MAR 15 REF AMX PND 112, ASSOCIATED ER/A 00-511165 ADDED FOR AC 0963.

Part: FITTING — WORN (TAILCONE) · airframe 63,395 hrs · 47,455 cycles

WORN GUIDE PIN FITTINGS, ON TAIL CONE SETTLEMENT AREA. DAMAGE GUIDE PIN FITTINGS A E/A ON TAIL CONE SETTLEMENT AREA WERE REPLACED IAW SRM 51-30-2.

Part: CUSP WEB — CORRODED · airframe 63,395 hrs · 47,455 cycles

CORROSION ON LT CUSP WEB BETWEEN X54-X64 AND STA Y=457 AT PAX CABIN. CORROSION AND FASTENERS WAS REMOVED, AREA WAS MEASURED AND M.F.E.C INSPECTION WAS PERFORMED, DAMAGE WAS REMOVED, REPAIR PARTS WERE FABRICATED AND NEW REPAIR PARTS WERE TREATED, PAINTED AND INSTALLED IAW SRM 51-30-2, 51-10-3 PAR 26, 14, 25; 53-05, FIG 131A-14 AND ER/A 508307-14 MA. REV A. (VR) WAS ACCOMPLISHED ORIGINAL THICKNESS IS .020", REMANING THICKNESS IS .018" THERE FOR ITS WITHIN LIMITS IAW ER/A 508307-14MA, REV A.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 63,395 hrs · 47,455 cycles

CRACKED PAN ON RT FWD OVERWING EMERGENCY EXIT DOOR AT STOP FITTING NR 12, CARD 35 ZONE 201, INNER SKING, STOP FITTING AND CLIP WERE REMOVED CRACK WAS AS STOP DRILL DOUBLER WAS STOPPED, FABRICATED, TREATED, PAINTED, INSTALLED AND IDENTIFIED IAW SRM 51-30, 1, 51-30-2 51-30-5, 51-10-2, 51-01 51-10-3 PARA 14 AND 21 AND 52-05D FIG.51.

Part: SKIN — CORRODED (TE FLAP VANE) · corrosion level 2 · airframe 69,402 hrs · 51,873 cycles

SKINS ON LT OUTBD FLAP MID GUIDE VANE AT 15 INCH FROM INBD END. DAMAGED BY CORROSION THEY ARE OUT OF LIMITS BY REPAIR IAW SRM 57-03D PAR II. OUTBD FLAP MID GUIDE VANE WAS REPLACED.

Part: INTERCOSTAL — CRACKED (BS 953-958) · airframe 63,395 hrs · 47,455 cycles

CRACKED INTERCOSTAL AT RT MLG DOOR INTERNAL STRUCTURE BETWEEN STA Y=953 AND Y=958 IN REF: CARD 5, ZONE 8, CARD 8, ZONE 18. INTERCOSTAL WAS REMOVED IAW SRM 51-30-2 INTERCOSTAL WAS MFG, ADJUSTED AND DRILLED IAW DWG 5930583, REV DA INTERCOSTAL WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14/21 INTERCOSTAL WAS INSTALLED IAW DWG 5930583, REV DA AND SRM 51-30-2.

Part: STRUCTURE — GOUGED (BS 1298) · airframe 63,395 hrs · 47,455 cycles

GOUGE UNDER LT CUSP WEB BETWEEN X=44 TO 54 AND BS 1298 . INSTALLED PLUG IAW SRM 53-01.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 63,395 hrs · 47,455 cycles

CRACKED PAN ON RT AFT OVERWING EMERGENCY EXIT DOOR AT AFT RUB LOCK AREA. INNER SKIN, STOP FITTING AND CLIP WERE REMOVED. CRACK WAS FABRICATED, PAINTED, INSTALLED AND IDENTIFIED IAW SRM 52-05 D, FIG 51, 51-30-1, 51-30-2, 51-10-4, 51-01, 51-10-3 PARA 14 AND 21. RETAIN FOR RECORDS BY PRIMARY STRUCTURE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,430 hrs · 46,795 cycles

DURING LINE CHECK, NOTED EMERGENCY EXIT SIGN INOPERATIVE AT ROW 24 ABC. THE EXIT SIGN ASSEMBLY WAS REPLACED AND OPERATION CHECKED NORMALLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,257 hrs · 46,691 cycles

DURING LINE CHECK, NOTED EMERGENCY LIGHTS OUT AT ROWS 34D AND 36D. REPLACED BATTERY IN POWER SUPPLY IAW AMM 33-52 AND OPS CHECKED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,257 hrs · 46,691 cycles

DURING LINE CHECK, NOTED 12 NON-SEQUENTIAL CABIN STANDBY, EMERGENCY, LIGHTS INOPERATIVE. REPLACED LAMPS AS REQUIRED AND OPS CHECKED NORMAL.

Part: FLANGE — GOUGED (TAILCONE) · airframe 61,082 hrs · 45,925 cycles

DURING SCHEDULED C-CHECK, THE TAILCONE FWD FLANGE WAS NOTED TO BE GOUGED FROM THE TAILCONE RELEASE CAM. DAMAGE WAS REPAIRED IAW ER/A 515976-14.

Part: RECEPTACLE — DAMAGED (TAIL CONE) · airframe 61,171 hrs · 45,972 cycles

DURING SCHEDULED INSPECTION, 12 PIN RECEPTICLES WERE FOUND TO BE WORN & GOUGED. REPLACED WORN ALIGNMENT PIN RECEPTACLES IAW AMM 53-53-00.

Part: SPRING — INOPERATIVE (TAILCONE RELEASE) · airframe 61,171 hrs · 45,972 cycles

DURING SCHEDULED INSPECTION, THE LOWER RT TAILCONE RELEASE LEVER WAS FOUND TO NOT TO HAVE SPRING TENSION TO THE CLOSED POSITION. INDEXED SPRING IAW AMM 53-53-00-501, STEP 6 OF AMDS 5350-01077-0101.

Part: PIN — LOOSE (TAILCONE RELEASE) · airframe 61,171 hrs · 45,972 cycles

DURING SCHEDULED INSPECTION, THE TAILCONE ALIGNMENT PIN AT THE 12 O`CLOCK POSITION WAS FOUND TO BE LOOSE. TIGHTENED ALIGNMENT PIN IAW AMM 53-53-00.

Part: CABLE — FRAYED (TAILCONE RELEASE) · airframe 61,171 hrs · 45,972 cycles

DURING SCHEDULED CHECK, THE TAILCONE INTERIOR CABLE WAS FOUND TO BE FRAYED. REPLACED LANYARD CABLE IAW AMM 53-53-00.

Part: SPRING — OUT OF POSITION (TAILCONE RELEASE) · airframe 61,171 hrs · 45,972 cycles

DURING SCHEDULED INSPECTION, THE UPPER RT TAILCONE RELEASE LEVER WAS FOUND TO NOT TO HAVE SPRING TENSION TO THE CLOSED POSITION. INDEXED SPRING IAW AMM 53-53-00-501 STEP 6 OF AMDS 5350-01077-0101.

Part: SPRING — INOPERATIVE (TAILCONE RELEASE) · airframe 61,171 hrs · 45,972 cycles

DURING SCHEDULED INSPECTION, THE UPPER LT TAILCONE RELEASE LEVER WAS FOUND TO NOT TO HAVE SPRING TENSION TO THE CLOSED POSITION. INDEXED SPRING IAW AMM 53-53-00-502, STEP 6 OF AMDS 5350-01077-0101.

Part: BATTERY PACK — MISINSTALLED (EMERGENCY LIGHTS) · airframe 60,944 hrs · 45,837 cycles

DURING ROUTINE MX CHECK, THE CABIN EMERGENCY CEILING LIGHTS WERE NOTED TO BE INOPERATIVE FROM ROW 17 TO 21. THE BATTERY PACK WAS FOUND TO BE IMPROPERLY SEATED. THE BATTERIES WERE REPLACED, THE POWER SUPPLY WAS SEATED PROPERLY AND THE SYS OPERATION CHECKED NORMALLY IAW AM 33-54-00.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,729 hrs · 45,701 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 22DE IN THE CABIN WAS INOPERATIVE. MX FOUND THE SEAT WIRE HARNESS HAD FAILED, REPLACED IT, AND FUNCTIONALLY CHECKED THE SYS.

Part: SPAR CAP — CRACKED · airframe 60,591 hrs · 45,597 cycles

DURING SCHEDULED INSPECTION OF LOWER SPAR CAP, XRS 164, A .1875 CRACK INDICATION EMANATING FROM LOWER SECTION OF FITTING. REPAIRED IAW AMDS WC 5710-01110-1201.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,796 hrs · 45,020 cycles

DURING EMERGENCY LIGHT TEST, EMERGENCY CEILING LIGHTS ROWS 15-20 WERE INOPERATIVE, REPLACED BATTERY PACK AND TESTED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,149 hrs · 43,887 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE FROM ROWS 17-20. MAINTENANCE REMOVED AND REPLACED BATTERY PACK AT ROW 17-18 PER AMM. OPERATION CHECKS GOOD.

Part: WIRE HARNESS — INOPERATIVE (CABIN) · airframe 58,036 hrs · 43,806 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 2C IN THE CABIN, WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 57,754 hrs · 43,630 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE ESCAPE HATCH AT ROW 26 HAD ALL FAILED. AFTER REPLACING THE BATTERIES IN THE POWER SUPPLY DID NOT CORRECT THE PROBLEM MAINTENANCE REPLACED ALL THE LAMPS IN THE SIGN AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: WIRE — SHORTED (CABIN) · airframe 57,665 hrs · 43,566 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 1-12 AND ROWS 31-38 OF THE CABIN WERE INOPERATIVE. MAINTENANCE FOUND A WIRE SHORTED AT THE EXIT IDENTIFIER BY DOOR L1 AND APPLIED THE PROPER REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,594 hrs · 43,534 cycles

DURING CURRENT PSV IN MSP, A CRACK TO THE FUSELAGE SKIN WAS FOUND AT STA 1418, S-2L. THE CRACK IS EMANATING FROM THE THRID FASTENER HOLE COMMON TO SHEAR TIE. REPAIR ACCOMPLISHED PER ER/A 498623-14.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,594 hrs · 43,534 cycles

AFT CARGO CORROSION AT FRAME STA 1231 SHEAR TIE BETWEEN L29R AND L30R. FABRICATED PART PER DWG 9919603-85, HEAT TREATED PER PS900-4-1 AND REMOVAL AND REPLACEMENT PER SRM 51-01 PG 1. (NO LOG OR NRC REF PROVIDED)

Part: SKIN — CRACKED (BS 1418) · airframe 63,395 hrs · 47,455 cycles

DURING CURRENT PSV, FUSELAGE SKIN WAS FOUND CRACKED BS 1418, S2R. CRACK IS EMANATING FROM THE THIRD FASTENER HOLE COMMON TO SHEAR TIE. REPAIRED IAW ER/A 498624-14.

Part: CABLE — BROKEN (CABIN) · airframe 56,564 hrs · 42,803 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 27DE INOPERATIVE. PHL MAINTENANCE FORWARD TO MCO FOR PART WAS NOT IN STOCK. ONCE IN ATL MAINTENANCE REPLACED BROKEN CABLE ASSEMBLY FOR LIGHT. OPERATION OF LIGHT OK AND MCO REMOVED.

Part: CHARGER — INOPERATIVE (CARGO BAY) · airframe 56,411 hrs · 42,685 cycles

DURING LINE CHECK MAINTENANCE COULD NOT TEST EMERGENCY ESCAPE PATH LIGHT FROM FA PANEL BUT CHECKED OK FROM COCKPIT. MAINTENANCE REPLACED OVERWING LIGHT BATTERY CHARGER AND BATTERY PACK PER IPC 33-50. OPERATION OF LIGHTS NOW CHECKS OK.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 55,309 hrs · 41,938 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY PATH LIGHT AT ROW 10 INOPERATIVE. MX REINSERTED TERMINAL PIN INTO CLIP HSG. OPERATION OF LIGHT NOW CHECKS GOOD.

Part: SYMBOL GENERATOR — OVERHEATED (COCKPIT) · airframe 55,045 hrs · 41,774 cycles

ON TAKEOFF ROLL F/O INSTRUMENTS WENT OUT. CREW CONTINUED TAKEOFF AND AT 10,000 FT WHILE IN CONTACT WITH DISPATCH, AN ACRID ODOR AND VISIBLE SMOKE ENTERED INTO THE COCKPIT. BOTH PILOTS DONNED O2 MASKS, DECLARED EMERGENCY, AND RETURNED TO DEPARTURE. SMOKE DISSIPATED AND F/O INSTRUMENTS CAME BACK ON AFTER LANDING. ONCE AT GATE CREW TURNED OFF ALL ELECTRICAL COMPONENTS. MX DUPLICATED SMELL AS SYMBOL GENERATOR OVERHEATED. MX REPLACED THE NR2 PFD, NAV DISPLAY, AND SYMBOL GEN. COMPLIED WITH OPN 5088, ALL INSTRUMENTS CHECK OK.

Part: BATTERY — NOT SEATED (CABIN) · airframe 54,812 hrs · 41,614 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY CEILING LIGHTS FROM ROW 17 THRU 21 INOPERATIVE. MAINTENANCE RELAMPED AND NO HELP. INSPECTED BATTERY AND NOTICED WAS NOT SEATED IN BATTERY PACK. BATTERY WAS INSTALLED PROPERLY AND NOW OPERATION OF LIGHTS CHECK OK. 04NOV/MSP/ 624927 (DLM88103033)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,986 hrs · 40,303 cycles

ON I/O FOUND LOWER SEAT EMER EXIT SEAT 10 DE INOPERATIVE. RELAMPED SAME AND BLEW FUSE ON BALLAST REPLACED FUSE OPS, NML.

Part: ENGINE — SMOKE (NR 1) · airframe 49,915 hrs · 38,282 cycles

DURING CRUISE, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. BOTH AFT LAV SMOKE DETECTORS WERE GOING OFF. ENGINE ANTI-ICE ON, LT PACK TURNED OFF SMOKE OUT. CAPTAIN DECLARED EMERGENCY ON APPROACH. LANDED AT SCHEDULED DESTINATION. REPLACED NR 1 ENGINE.

Part: INLET — CONTAMINATED (APU) · airframe 49,892 hrs · 38,266 cycles

BOTH AFT LAV SMOKE DETECTORS WENT OFF AFTER TAKEOFF FOR BUF BOTH ENG ANTI-ICE ON FOR TAKEOFF, NO SMOKE, SLIGHT ODOR DETECTED, DISSIPATED RAPIDLY. SUSPECT DE-ICE FLUID INGESTION. APU INLET CLEAN PERFORMED ALT DUCT BURNOUT PER AIJC OPN 5090 AND REPLACED WATER SEPARATOR BAGS PER AIJC 7904. ALL CHECKS GOOD.

Part: SEAL — WORN (APU OIL CAP) · airframe 49,879 hrs · 38,254 cycles

SMOKE IN CABIN AND COCKPIT. RTB - SMOKE DISSIPATED ON LANDING FOUND APU INLET CONTAMINATED WITH ENG OIL 042620, PERFORMED OP 5088. FOUND APU OIL CAP SEAL WORN. REPLACED SAME. RAN APU LEAKS NOTED. PERFORMED OP 5089. PNEUMATIC SYS DUCT BURN.

Part: VANE — ERODED (LT WING TE FLAP) · airframe 48,692 hrs · 37,445 cycles

DURING HMV3 ERODED LOWER SURFACE OF INBD FIXED VANE LT INBD FLAP WAS FOUND. EROSION WAS REPAIRED IAW SRM 57-03 PARA 8D FIG 9A.

Part: TAB — DENTED (LT ELEVATOR) · airframe 48,692 hrs · 37,445 cycles

DURING HMV3 DENTS WERE FOUND ON UPPER SURFACE OF LT ELEVATOR GEARED TAB. DENTS WERE REPAIRED IAW DRD 55-04D PARA 2A 2 FIG1 AND PARA 3A FIG 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,692 hrs · 37,445 cycles

DURING HMV 3 FIVE CRACKS WERE FOUND ON FUSELAGE AT STATIONS:Y=189 OF .093",Y=190 OF .031",Y=191 OF .093",Y=193 OF.078" AND Y=196 OF .062"; AND THE LONGERON 22 LT CRACKS WERE REPAIRED IAW EA 09-069085-12AD REV D.

Part: TAB — DELAMINATED (ELEVATOR) · airframe 48,692 hrs · 37,445 cycles

DURING HMV3 DELAMINATION WAS FOUND ON LOWER SURFACE OF LT ELEVATOR GEARED TAB. DELAMINATION WAS REPAIRED IAW DRD 55-04D PARA 3A FIG 2.

Part: TAB — WORN (ELEVATOR) · airframe 48,692 hrs · 37,445 cycles

DURING HMV3 WEAR WAS FOUND ON TRAILING EDGE OF LT ELEVATOR GEARED TAB. WEAR WAS REPAIRED IAW DRD 55-04D PARA 3D FIG 2.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 48,692 hrs · 37,445 cycles

TRANSFERRED FROM OMI C/N C12317161 DUE ERA 465882-14 REV A CODE 9-53-31-20 ACTL 2300 FWD CARGO DOOR CUTOUT FORWARD EDGE DAMAGE. ACCOMPLISHED PERMANENT REPAIR IAW ERA 465882-14 REV A.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,692 hrs · 37,445 cycles

DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN AT STA Y=1437 BETWEEN LONG 3 AND 4LT. CRACK WAS REPAIRED IAW SRM 53-04D FIG 27.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 47,850 hrs · 36,883 cycles

FUSELAGE SKIN BENT AND TORN AT FORWARD EDGE OF C-1 CARGO DOOR. DAMAGE WAS CUT OUT AND A REPAIR DOUBLER AND TRIPLER WERE INSTALLED.

Part: SHAFT — SHEARED (FUEL PUMP) · airframe 43,815 hrs · 34,179 cycles

AT 18,000 FEET THE NUMBER 1 ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. REMOVED FUEL CONTROL AND FUEL PUMP. FOUND SHAFT SHEARED ON PUMP. REPLACED PUMP PER AMM AND REINSTALLED FUEL CONTROL. CHECK ENG RUN OK PER AMM.

Part: LEVER — BYPASSING (LANDING GEAR) · airframe 41,919 hrs · 32,846 cycles

ON CLIMBOUT LANDING GEAR DID NOT RETRACT, 3 RED LIGHTS INITIALLY THEN THREE GREEN UPON EXTENSION. STOWED LANDING GEAR BYPASS LEVER.

Part: A/C PACK — MALFUNCTIONED (BOTH) · airframe 40,066 hrs · 31,514 cycles

DUE TO COLD CABIN BOTH A/C PACKS RUN FULL HOT MANUAL AT FL 360 CAUSING BOTH PACKS TO OVERHEAT AND TRIP OFF. CABIN PRESSURE WAS LOST AND O2 MASKS AUTOMATICALLY DEPLOYED. CREW INITIATED A RAPID DESCENT TO 10,000 FT. AFTER PACKS COOLED, RESET AND REGAINED PRESSURIZATION. FLIGHT DIVERTED TO AMA FOR MTC. BOTH A/C PACKS PLACARD AT AMA BY MTC AND AIRCRAFT MTC FERRIED TO DFW FOR O2 GEN REPLACEMENTS.

Part: ODOR — DETECTED (CABIN) · airframe 35,364 hrs · 28,208 cycles

PASSENGERS AND CREW REPORT BURNING ODOR IN CABIN AROUND ROW 22A/B/C SHORTLY AFTER T/O ATL. ODOR DISSIPATED QUICKLY. PERFORMED DUCT BURNOUT.

Part: ENGINE — FAILED (NR 2) · airframe 35,285 hrs · 28,158 cycles

AFTER GEAR RETRACTION THERE WAS A STRONG BURNED RUBBER ODOR IN THE COCKPIT AND THE CABIN THAT DISSIPATED AFTER SEVERAL MINUTES. NO OTHER ABNORMAL INDICATION. FLT ATTN REPORTED THAT A SIMILAR ODOR OCCURRED THIS MORNING ON DEPARTURE FROM DAB. REPLACED NR 2 ENGINE, PERFORMED DUCT BURNOUT.

Part: BATTERY — OVERHEATED (E&E BAY) · airframe 34,649 hrs · 27,712 cycles

ACRID ODOR AND WHITE SMOKE EMITTING FROM VENT AFT OF NOSE GEAR, UNDER E&E COMPARTMENT. FOUND SHIPS MAIN BATTERIES OVERHEATING. FOUND SHIP`S MAIN BATTERIES OVERHEATING. REMOVED BATTERY & REPLACED LT & RT BATTERY CHARGER & TESTED BOTH THERMAL SENSORS, BOTH OK BUT REPLACED AS PRECAUTION. SYSTEM TESTS OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,747 hrs · 27,048 cycles

DURING HMV-2, THE DENT IN THE SKIN BETWEEN STA 218 & STA 256 JUST ABOVE L-25R. TRIMMED OUT SKIN TO REMOVE A GOUGE. REPAIRED IAW MD-88 SRM 53-04, FIGURE 12B.

Part: SKIN — DENTED (STA 437 @ L-20R) · airframe 33,747 hrs · 27,048 cycles

DURING HMV-2, INSPECTION FOUND A DENT IN THE FUSELAGE SKIN FROM STA 435 TO STA 439 @ L-20R. THE C1 DOOR INTERNAL SURROUND DOUBLER WAS NOT DAMAGED. THE DENT WAS REMOVED RESULTING IN A CUTOUT MEASURING 4.375 INCHES (FWD/AFT) X 2.125 INCHES (UP/DOWN). A DOUBLER REPAIR WAS ACCOMPLISHED PER MD-88 SRM 53-04, FIGURE 12B, SHEET 4 (CLASS 1 EXTERNAL REPAIR), EXCEPT THE UPPER & LOWER FINGER DOUBLERS WERE ENDED AT THE C1 DOOR INTERNAL DOUBLER.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 32,216 hrs · 25,863 cycles

DURING CLIMBOUT, L HYD QTY AND PRESS DECREASING. FOLLOWED CHECKLIST, RETURNED TO ATL. REMOVED PRESS LINE FLEX HOSE AT FILTER MODULE. INSTALLED NEW CASE DRAIN FILTER RETURN FLEX LINE REDUCER AND PACKING. NO LEAKS NOTED DURING ENGINE RUN.

Part: BEARING — UNSERVICEABLE (RT SPOILER MIXER) · airframe 31,655 hrs · 25,436 cycles

AILERON IN RIGHT ROLL HANGS UP. RPLD PIVOT BEARING AT RT SPOILER MIXER. NOW OPS NML

Part: ENGINE — CRACKED (NR 1 ENGINE) · airframe 30,399 hrs · 24,489 cycles

FLIGHT CREW REPORTED NR 1 LOST POWER ABOUT 15 MILES OUT OF CAE ENGINE WAS NOT SHUT DOWN UNTIL AFTER TOUCHDOWN. DURNING INSP MTC FOUND FUEL MISTING INTO THE COLD STREAM ON START ATTEMPT. PRIMARY FUEL MANIFOLD CRACKED. REPLACED SAME

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 30,002 hrs · 24,198 cycles

TAIL CONE EMERGENCY EXIT IDENTIFIERS INOP. REPLACED AFT CABIN POWER SUPPLY, CKS OK.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 29,375 hrs · 23,746 cycles

THE LOWER JAMB OF THE C3 CARGO DOOR OPENING WAS FOUND WITH CORROSION AT THE DOOR STOP SET SCREW LOCATIONS. THE CORROSION WAS BLENDED AWAY AND THE JAMB REPAIRED WITH A TITANIUM ''ZEE'' SECTION REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PER MD-88 SRM 53-05 AND ER/A 378917-14.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,318 hrs · 23,697 cycles

AT LIFT OFF AFT F/A DETECTED FUMES. PERFORMED DUCT BURNOUT, NO FUMES NOTED.

Part: GENERATOR — FAILED (NR 1 ENGINE) · airframe 28,787 hrs · 23,291 cycles

AFTER LEFT ENGINE START GEN HAD HARD TRANSFER. AFTER TAKEOFF LOST LEFT GENERATOR AND WOULD NOT RESET PRE POM PROC. REPLACED CSD AND GENERATOR. P/N 696233B & 976J252-8.

Part: COALESCER — CONTAMINATED (CABIN)

FUMES IN CABIN AFTER BLEED AIR FROM APU. INSPECTED APU FOR LEAKS, NONE FOUND. DRAINED HYD OVERFLOW BOTTLES, PERFORMED DUCT BURNOUT. REPLACED WATER SEPARATOR BAGS.

Part: PBE — IND POPPED (COCKPIT)

COCKPIT PBE VISUAL SERVICE IND POPPED. REPLACED MASK, OK FOR SERVICE.

Part: DUCT — LEAKING (TAIL COMP)

ON INITIAL TAKOFF GOT TAIL COMP TEMP HI LIGHT. PER POM RETURNED ATL. FOUND LEFT ACM AIR OUTLET RUBBER DUCT LEAKING. REPLACED DUCT OPERATION NORMAL.

Part: AHRS — INOP (NR 1)

ON TAKEOFF ROLL AT 100 KNOTS, BOTH AHRS FAILED. FAILURE OCCURRED AFTER HITTING A BUMP ON RUNWAY. ABORTED TAKEOFF. REPLACED NR 1 AHRS AND RESEATED NR 1 AHRS. CHECKED SECURITY OF CADC, SYMBOL GENERATOR AND DFGC NR 1 AND NR 2, OPERATION NORMAL.