N969DL

Part: ENGINE — OVERTEMP (LEFT) · airframe 74,718 hrs · 55,736 cycles

SHIP 969 - IFSD & ATB - DUE TO LEFT ENGINE HIGH OIL TEMPERATURE. FLT CREW REPORTED AT 2000 FT THAT OIL TEMP WAS AT 165DEG AND WHEN POWER WAS ADDED, OIL TEMP WENT TO 200 DEGREES. FOLLOWED QRH SHUT DOWN ENGINE AND RETURNED TO ATL. CORRECTIVE ACTION: MTC FOUND BOTH OIL TEMP DECALS YELLOW BOXES HAD TURNED BLACK. ENGINE CHANGED. (LP6605372)

Part: CONNECTOR — BROKEN (CABIN) · airframe 74,146 hrs · 55,203 cycles

EMER. LIGHT @ SEAT 16ED INOP. FOUND PLASTIC SEAT CONNECTOR BROKEN OFF RETERMINATED AS REQUIRED. OPS CHECK GOOD OK FOR SVC. (LP5926682)

Part: BATTERY — DISCHARGED (CABIN) · airframe 74,146 hrs · 55,203 cycles

EMER. LIGHTS OUT ON OVERHEAD @ ROWS 18,21,24,25. R/R BATTERIES AT B5-103 PER AMM 33-53 AND WM 33-51-12. OPS CK GOOD. (LP5926683)

Part: COWLING — CORRODED (LT ENGINE) · airframe 72,198 hrs · 53,505 cycles

CORROSION ON LIP OF NOSE COWLING BTW 1 TO 2 HRS AT LT ENGINE. REPLACED NOSE COWLING.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 72,198 hrs · 53,505 cycles

CRACK ON RH AFT OVERWING EMERGENCY EXIT DDOR JAMB TOP AREA. CRACK ON RT AFT OVERWING EMERGENCY EXIT DDOR JAMB TOP AREA WAS REPAIRED PER SRM 53-05 FIG 32.

Part: TAB — DELAMINATED (RUDDER) · airframe 72,198 hrs · 53,505 cycles

DELAMINATED RUDDER CONTROL TAB LT/RT SIDE (MID HINGE AREA). DELAMINATED RUDDER CONTROL TAB LT/RT SIDE (MID HINGE AREA) WAS REPAIRED PER ERA 092613-14MA REV "A" AND PER SRM 51-70-1A, PAR 23.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 72,198 hrs · 53,505 cycles

CRACK ON RH FWD OVERWING EMERGENCY EXIT DDOR JAMB TOP AREA. ON RT FWD OVERWING EMERGENCY EXIT DDOR JAMB TOP AREA WAS REPAIRED PER SRM 53-05 FIG 32.

Part: TAB — CRACKED (LT AILERON) · airframe 72,198 hrs · 53,505 cycles

HIDDEN CRACKS: CRACKS ALONG T/E ON LT AILERON CONTROL TAB, DURING PAINT REMOVAL (IN REF NRC S/N 00017). ON REFERENCE OF NRC SERIAL NR 00325: CRACKS ALONG T/E ON LT AILERON CONTROL TAB, WERE REPAIRED PER SRM 51-70-1A P 18. PERFORM DECAL CONDITION INSPECTION EVERY "C" CHECK PER TOPP MANUAL 30-10-70 PAG 14.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 72,198 hrs · 53,505 cycles

WORN EXTERNAL DOUBLERS (2 E/AS) AT FWD CARGO DOOR. EXTERNAL DOUBLERS WERE REPLACED PER ER/A 486624-14MA REV ORIGINAL AND SRM 51-30-2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 71,845 hrs · 53,214 cycles

FOUND EMERGENCY EXIT LIGHT SIGN INOP DURING LIGHT CKS AT ROW 24 BOTH SIDES. R&R BATTERY PACK AT ROW 24 IAW MM 33-53. EXIT SIGNS LIGHT CKS NORM. OK FOR SVC.

Part: WIRE — BROKEN (DASH) · airframe 71,322 hrs · 52,776 cycles

SMALL AMOUNT OF SMOKE AND ODOR DETECTED FROM UNDER CAPTAIN'S DASHBOARD. REDUCED LIGHTS. SMOKE STOPPED. FOUND WIRE TERMINALS FOR BACK LIGHTNING FOR LANDING LIGHTS PANEL BURNT. RETERMINATED RING TERMINALS ON WIRES PER WDM CHAPTER 20. REINSTALLED WIRES ON CONNECTOR. PERFORMED NO-GO ODI PREVENTION IAW W/C 2120-2367. NO OTHER DEFECTS NOTED. PERFORMED LIGHTS CHECK ALL OP'S NORMAL. OK FOR SERVICE. (LP4182354)

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 70,921 hrs · 52,453 cycles

CREW VERBAL, F/C LAV SMOKE ALARM SOUNDED ON TAXI IN. FLIGHT NUMBER WAS NOT SPECIFIED. R&R DETECTOR.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 70,821 hrs · 52,373 cycles

DURING SVC FOUND 5 OVERHEAD EMERGENCY LIGHTS INOP IN FIRST CLASS. RELAMPED. NO HELP. R&R BATTERIES IN BATTERY PACK B5-100. NO HELP. R&R BATTERY PACK ASSY B5-100 PER WDM 33-51-12. EMERGENCY LIGHTS NOW OPS OK.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 70,419 hrs · 52,052 cycles

DURING SVC CK- FOUND TWO CABIN EMERGENCY BATTERY PACKS BAD. REMOVED & REPLACED BATTERY PACKS AT SEAT ROWS 25 & 29 PER MD88 AMM 33-53. (LP3309106)

Part: PIN — PULLED (L1 DOOR SLIDE) · airframe 70,153 hrs · 51,837 cycles

L1 DOOR SLIDE PINS PULLED. R & R L1 DOOR SLIDE IAW AMDS 2561-4964.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,076 hrs · 51,767 cycles

COCKPIT AND ENTRY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-53. OPS CHECKED GOOD.

Part: FIRE WARNING — FALSE ACTIVATION (RT ENGINE) · airframe 69,389 hrs · 51,204 cycles

RIGHT ENGINE FIRE LOOP B LIGHT ILLUMINATED WITH OAP FIRE DETECTOR LOOP MESSAGE. IAW QRH, PERFORMED LOOP TEST ON SYSTEM A, TESTED NORMAL. COULD NOT DUPLICATE FAULT. TESTED SEVERAL TIMES AND LOOPS INDIVIDUALLY. NO HISTORY. ACFT OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,180 hrs · 51,044 cycles

CEILING EMERGENCY LIGHTS OUT AT SEATS 16, 17, 18, 19, 20, 26, 27, 28, 29, AND 30. REPLACED BATTERIES AT POWER UNITS SN-22713 AND SN-27406. REFERENCE AMM 33-53-00-401. OPS CHECK OK. PN'S ON FOUR 41B004AD07G3 BATTERIES.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 69,129 hrs · 51,006 cycles

SEVERAL SEAT MOUNTED EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPAIRED THE WIRING IAW AMM 20-50.

Part: BATTERY — DISCHARGED (CABIN) · airframe 67,988 hrs · 50,141 cycles

EMER CEILING LIGHTS ROW 17-19 INOP. REPLACED BATTERIES FOR B5-102 EMER LIGHTS REF AMM 33-53. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,715 hrs · 49,939 cycles

BACK HALF OF CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED THE BATTERY PACKS AT B5-106 & B5-103. CHECKS GOOD. ACFT OK FOR SERVICE.

Part: FRAME — CRACKED (BS 1485) · airframe 67,228 hrs · 49,540 cycles

TAIL INTERIOR CANTED FRAME WEB AT BS 1485 HAS 1/2 INCH CRACK. INSTALLED REPAIR IAW SRM 51-70-5.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 66,870 hrs · 49,285 cycles

EMERGENCY OVERWING LIGHTS INOPERATIVE, R & R EMERGENCY POWER SUPPLY AND BATTERY IAW AMM 33-53. OPS CK NORMAL. AIRCRAFT OK FOR SERVICE. EMERGENCY POWER SUPPLY.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,733 hrs · 49,182 cycles

ALL EMERGENCY LIGHTS INOPERATIVE. R & R FWD ATTEND SWITCH S1-387. OPS CK GOOD, REF WDM 33-51-11.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,416 hrs · 48,950 cycles

MSP MAINTENANCE FOUND THE EMERGENCY PATH LIGHTING INOPERATIVE BETWEEN SEAT ROWS 25 AND 31. THE BATTERY PACK WAS REPLACED AND GROUND WIRE L1844B16N WAS FOUND LOOSE AND WAS RESECURED.

Part: CONNECTOR — DAMAGED (WATER HEATER) · airframe 66,214 hrs · 48,797 cycles

FWD LAV WATER HEATER CONNECTOR P1-385 HEAT DAMAGE. REPLACED P1-385 IAW SWPM CH20 AND R & R WATER HEATER AMM 38-11, OPS AND LEAK CK GOOD.

Part: HEATER — ODOR (LAV WATER) · airframe 66,193 hrs · 48,784 cycles

AFTER TAKEOFF, A F/A REPORTED THAT THE CABIN FILLED WITH A WHITE COLORED HAZE WITH AN ELECTRICAL ODOR. THE QRH WAS FOLLOWED AND THE GALLEY AND SIDEWALL LIGHTS WERE TURNED OFF. THE SMOKE SLOWLY DISSIPATED. THE ACFT WAS DIVERTED. MAINTENANCE PERFORMED AMDS TROUBLESHOOTING WC 2120-2367, SMOKE/ODOR IN CABIN. THE FORWARD LAVATORY WATER HEATER WAS FOUND AT FAULT. THE WATER HEATER WAS DEFERRED IAW MEL 38-00-01A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,621 hrs · 48,404 cycles

FLL MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE FROM SEAT ROWS 1 THROUGH 10. AN EMERGENCY BATTERY PACK WAS REPLACED AND THE LIGHTS CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,180 hrs · 48,102 cycles

MAINTENANCE FOUND CABIN EMERGENCY LIGHT INOPERATIVE. THE OVERWING BATTERY PACK RELAY R2-271 AND BATTERY PACK B5-49 WAS REPLACED.

Part: AXLE — CORRODED (RT NLG) · airframe 64,632 hrs · 47,694 cycles

EVIDENCE OF CORROSION ON RT NLG AXLE SHAFT, REF CRD 3200-01207-0101. RT AXLE SHAFT IAW AMDS 6221-6192.

Part: AXLE — CORRODED (LT NLG) · airframe 64,632 hrs · 47,694 cycles

EVIDENCE OF CORROSION ON LT NLG AXLE SHAFT. R & R LT NLG AXLE SHAFT IAW AMDS 3221-6192.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,997 hrs · 47,251 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE CEILING MOUNTED EMERGENCY LIGHTS INOPERATIVE AT ROWS 17-20. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES AND THE OPS CHECK WAS GOOD.

Part: LANYARD — MISINSTALLED (R1 DOOR SLIDE) · airframe 63,148 hrs · 46,699 cycles

MAINTENANCE FOUND THE R1 DOOR SLIDE RELEASE LANYARD INSTALLED IMPROPERLY. THE LANYARD WAS REMOVED AND REINSTALLED.

Part: PIN — PULLED (ESCAPE SLIDE) · airframe 63,148 hrs · 46,699 cycles

MAINTENANCE FOUND L1 DOOR SLIDE PIN PULLED. SLIDE WAS REPLACED.

Part: CONNECTOR — DISCONNECTED (EMEGENCY LIGHTS) · airframe 63,148 hrs · 46,699 cycles

EMERGENCY LIGHTS INOPERATIVE AT 22D AND 28D. CONNECTED THE CONNECTOR AND REPLACED LIGHT ASSY AT 22D, OPS CHECKED GOOD AMM 33-53.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 62,920 hrs · 46,540 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MAINTENANCE FOUND BROKEN TERMINALS AT THE AFT STAIRWAY EMERGENCY LIGHT L2646 AND REPAIRED THEM. THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: CUSP WEB — CORRODED (BS 930-936) · corrosion level 2 · airframe 62,077 hrs · 45,920 cycles

CORROSION ON LT CUSP WEB REPAIR DOUBLER X=54 TO X=60 BETWEEN BS 930 - 936. NEW REPAIR INSTALLED IAW SRM 53-05 FIG 131A-1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,066 hrs · 45,915 cycles

DURING CHECK, MAINTENANCE FOUND MULTIPLE OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROW 27, 28 LT AND 30B. MAINTENANCE R & R THE BATTERY PACK LOCATED AT 29DE AND THE LIGHTS RETURNED TO AN OPERATIONAL STATE.

Part: RETAINER — CRACKED (EMERGENCY EXIT) · airframe 67,752 hrs · 49,964 cycles

CORROSION AND A CRACK ON LOWER SECTION OF PRESSURE SEAL RETAINER OF RT FWD OVER WING EMERGENCY EXIT DOOR. THE SEAL RETAINER WAS REMOVED DRILLED AND INSTALLED IAW SRM 57-30-2 AND 57-10-4.

Part: PANEL — DELAMINATED (LT WING TE FLAP) · airframe 61,933 hrs · 45,822 cycles

DELAMINATED TRAILING EDGE METALIC HONEYCOMB PANEL FROM XRS 500 - 838, LT WING. REPAIRED IAW ERA 526957-14 & ETI-88-14-095 REV 2

Part: WEB — CORRODED (BS 363-370) · airframe 67,752 hrs · 49,964 cycles

CORROSION ON FWD WEB BS 363-370, LONGERONS 24 -28R AT FWD CARGO DOOR FRAME. CORRODED AREA WAS TRIMMED OUT, FILLER AND DOUBLER FABRICATED AND INSTALLED PER ER/A.

Part: HEATER BLANKET — DEBONDED (LT WING) · airframe 61,933 hrs · 45,822 cycles

DURING INSPECTION, VOIDS WERE FOUND OF A TOTAL AREA OF 37 PERCENT ON LT WING HEATER BLANKET. AREA WAS REPAIRED IAW ERA 527365-14 REV ORIG.

Part: HEATER BLANKET — DAMAGED (RT WING) · airframe 61,933 hrs · 45,822 cycles

DURING INSPECTION, VOIDS WERE FOUND OF A TOTAL AREA OF 23.6% ON RT WING HEATER BLANKET AREA REPAIRED IAW ER/A N./ 527365-14 REV ORIG.

Part: RETAINER — CRACKED (EMERGENCY EXIT) · airframe 67,752 hrs · 49,964 cycles

CORROSION AND A CRACK WAS FOUND ON LOWER SECTION OF PRESSURE SEAL RETAINER OF FWD OVER WING EMERGENCY EXIT DOOR. REMOVED DAMAGED AREA, REWORKED, TREATED, PAINTED AREA AND INSTALLED.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FUEL ACCESS PLATE 1365C COUNTERSINK AREA ON LEFT WING. CORROSION REMOVED, FOUND OUT OF LIMITS. REPLACED ACCESS PANEL.

Part: HEATER BLANKET — DEBONDED (RT WING) · airframe 61,933 hrs · 45,822 cycles

NINE DEBONDED AREAS ON RT WING HEATER BLANKET WERE FOUND AT INBD AREA . DAMAGE WAS REPAIRED IAW ERA 527365-14 REV ORIG..

Part: STRUCTURE — DELAMINATED (BUTTE DOOR) · airframe 61,933 hrs · 45,822 cycles

DELAMINATION ON LT MID BUTTE DOOR MID SECTION UPPER AND LOWER FACE AT LT WING. NEW BUTTE DOOR WAS ADJUSTED DRILLED INSTALLED IAW SRM 51-30-1,51-30-2.

Part: HEATER BLANKET — DEBONDED (LT WING) · airframe 61,933 hrs · 45,822 cycles

DBONDED AREAS ON LT WING HEATER BLANKET WERE FOUND AT INBD EDGE. REPAIRED IAW ERA 52736514 REV ORIG.

Part: BAR — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FLEX JOINT LOWER BAR FOUR LT FLAPS. REPAIRED IAW ERA 526968-14 REV ORIGINAL.

Part: SLAT TRACK — CORRODED (RT WING) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON SLAT TRACK FITTING FOR RT SLAT PANEL. FITTING RIBS HOLES AFTER REWORKED WERE FOUND DEFORMED. REPAIRED IAW ERA 526960-14 REV ORIGINAL.

Part: DOUBLER — CRACKED (BS 1485 WEB) · airframe 61,933 hrs · 45,822 cycles

CRACK FOUND ON REPAIR DOUBLER FOR WEB BS 1485 LONGERON 25R. DAMAGED REPAIR DOUBLER REMOVED, DOUBLER FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 53-03 D FIG 43.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,933 hrs · 45,822 cycles

PUNCTURE ON FUSELAGE SKIN BETWEEN Y 1497 & Y 1510 AT 05:00 O'CLOCK. FUSELAGE SKIN WAS FOUND WITH OIL CAN CONDITION ON THE REPAIRED AREA. PREVIOUS REPAIR DOUBLER WAS REMOVED AND NEW DOUBLER WAS FABRICATED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-2, 51-10-3 PAR 14, 21 AND 53-01 FIG. 4.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 61,933 hrs · 45,822 cycles

PUNCTURE ON FUSELAGE SKIN. REPAIRED IAW ERA 526949-14 REV ORIGINAL.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 61,933 hrs · 45,822 cycles

CRACK FWD AND AFT UPPER LINING ATTACH ANGLES ON UPPER EDGE OF L1 PASSENGER ENTRY DOOR. ANGLES FABRICATED IAW DWG 5956563. TREATED AND PAINTED IAW SRM 51-10-3 PAR 14 AND 21, AND INSTALLED IAW SRM 51-30-2.

Part: ATTACH BRACKET — CRACKED (BS 1416) · airframe 61,933 hrs · 45,822 cycles

CRACK ON BRACKET TO PNEUMATIC PRESSURE TRANSMITER BS 1416 , LONGERON 12L. BRACKET REMOVED, A NEW BRACKET FABRICATED, TREATED AND PAINTED, AND INSTALLED IAW AMM 36-20-01-201, SRM 51-30-2, DWG 5910249 REV "CM", 51-10-3 PAR 21 AND 14, 51-30-5, AMM 36-20-01-201, 36-20-01-2.

Part: LONGERON — CRACKED (BS 1437) · airframe 61,933 hrs · 45,822 cycles

CRACK FOUND ON LONGERON 12L AT BS 1437. LONGERON REMOVED, NEW SECTION AND SPLICE WERE DRILLED, ADJUSTED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-4, 53-02 FIG. 18 AND 51-10-3 PAR 21 AND 14.

Part: ANGLE — DAMAGED (CARGO DOOR) · airframe 61,933 hrs · 45,822 cycles

ELONGATED HOLES ON ANGLE FOR AFT CARGO DOOR BARRIER SUPPORT. ANGLE REMOVED, FABRICATED, TREATED, PRIMED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-3 PAR.21 & 14. AND DWG 5926003 REV.AB ITEMS -107 & -108.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 61,933 hrs · 45,822 cycles

CRACK FOUND ON SUPPORT OF FWD GUSSET AT FWD CARGO DOOR BARRIER. SUPPORT REMOVED IAW SRM 51-30-1, NEW SUPPORT DRILLED IAW SRM 51-10-4, TREATED AND PAINTED IAW SRM 51-10-3 PAR 14 AND 21 AND INSTALLED IAW SRM 51-30-1.

Part: ANGLE — WORN (CARGO DOOR) · airframe 61,933 hrs · 45,822 cycles

ANGLES TO ATTACH LATCHES ON AFT CARGO DOOR BARRIER WORN. ANGLES REMOVED IAW SRM 51-30-1. NEW ANGLES WERE INSTALLED IAW SRM 51-30-1.

Part: ANGLE — DAMAGED (CARGO DOOR) · airframe 61,933 hrs · 45,822 cycles

ELONGATED HOLES ON ANGLE IN MID CARGO DOOR BARRIER SUPPORT. DOUBLER REMOVED, AND A NEW DOUBLER FABRICATED, TREATED AND PAINTED, INSTALLED IAW SRM 51-10-3 PAR 21 AND 14, 51-30-2, 53-24-0 FIG, 13 AND DWG 5926003 REV. AB.

Part: STEP — CORRODED (VENTRAL STAIR) · airframe 61,933 hrs · 45,822 cycles

CORROSION FOUND ON STEPS 3, 5, 6, 12, 13, AND 15 OF VENTRAL STAIRWAY. STEPS 3 AND 6 FOUND WITHIN LIMITS IAW SRM 53-01 FIG. 01. STEPS 5, 12, 13, & 15 WERE FABRICATED IAW SRM 51-30-5, 51-10-1, 51-10-3 PARAGRAPH 14 AND 21 AND DWG 9410381 REV 5.

Part: DOUBLER — DAMAGED (CARGO DOOR) · airframe 61,933 hrs · 45,822 cycles

ELONGATED HOLES ON PREVIOUS REPAIR OF AFT CARGO DOOR BARRIER SUPPORT. PREVIOUS REPAIR REMOVED IAW SRM 51-30-2. DAMAGE REMOVED IAW SRM 53-01 FIG.4, NEW DOUBLER FABRICATED IAW SRM 53-01 FIG. 4. NEW DOUBLER AND AREA WERE TREATED AND PAINTED IAW SRM 51-10-3 FIG.14 AND 21 INSTALLED IAW SRM 51-3-2.

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 61,933 hrs · 45,822 cycles

DEBONDED FLOOR PANEL . FLOOR PANEL BONDED IAW SRM 51-20-0.

Part: SUPPORT — DAMAGED (CARGO DOOR) · airframe 61,933 hrs · 45,822 cycles

ENLOGATED HOLES FOUND ON SUPPORT OF MID CARGO DOOR BARRIER. SUPPORT REMOVED, NEW SUPPORTS FABRICATED,TREATED AND PAINTED IAW SRM 51-10-3 PAR 21 AND 14, 51-30-2, 53-24-0 FIG 13 AND DWG 5926003 REV AB.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 61,933 hrs · 45,822 cycles

CRACKS ON HOLD OPEN SUPPORT OF AFT CARGO COMPARTMENT DOOR. SUPPORT WAS REMOVED IAW SRM 51-30-2, SUPPORT WAS FABRICATED IAW SRM 51-10-2 AND DWG 5956273, REV B, SUPPORT WAS TREATED AND PAINTED IAW SRM 51-10-03, PAR 14/21 SUPPORT WAS INSTALLED IAW SRM 51-30-5.

Part: FRAME — CRACKED (BS 1380) · airframe 61,933 hrs · 45,822 cycles

CRACKED FRAME BS 1380 BETWEEN LONGERONS 13 - 14R. CRACKED FRAME WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. NEW FABRICATE IAW DWG 9912246, REV CY.

Part: GUSSET — WORN (CARGO DOOR) · airframe 61,933 hrs · 45,822 cycles

GUSSETS WORN OF FWD CARGO DOOR BARRIER MID CARGO DOOR BARRIER AND AFT CARGO DOOR BARRIER. GUSSETS WERE REMOVED IAW SRM 53-24-0 D, GUSSETS WERE FABRICATED IAW SRM 53-24-0 D. STRAPS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14-21. NEW STRAPS MID WERE INSTALLED IAW SRM 51-30-1 AND 51-30-2.

Part: STRUCTURE — CRACKED (BS 261) · airframe 61,933 hrs · 45,822 cycles

CRACK ON PRIMARY STAND BY EXHAUST AREA BETWEEN LONGERONS 21-22L BS 261. EXHAUST DUCT WAS REMOVED, DAMAGE AREA WAS REMOVED, REPAIR SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-3 PAR 14/21 AND ERA 464964-14MA.

Part: CAP — CRACKED (TAIL INTERCOSTAL) · airframe 61,933 hrs · 45,822 cycles

INTERCOSTAL ON TAIL CONE HAS A CRACKED CAP. CAP BEADED AND STOP DRILLED IAW SRM 53-05 . CRACK WELDED AND REWORKED IAW SRM 51-05. CAP TREATED AND PAINTED IAW SRM 51-10-3 PAR. 14 AND 21 AND INSTALLED IAW SRM 51-30-1.

Part: FLOOR SUPPORT — BROKEN (CABIN) · airframe 61,933 hrs · 45,822 cycles

BROKEN HAT CHANNEL FOR FLOOR PANEL. HAT CHANNEL REPAIRED. IAW SRM 51-70-1 D PAR.10.

Part: ANGLE — CRACKED (BS 1463) · airframe 61,933 hrs · 45,822 cycles

CRACKED ANGLE TO ATTACH WEB BS 1463 TO LT WEB BETWEEN PROJECTION LONGERONS 3 - 5L. NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-5 AND DWG 9911839, REV DN.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 61,933 hrs · 45,822 cycles

CRACK ON UPPER ANGLE LOCATED LT EMERGENCY OVERWING EXIT FWD DOOR UPPER SECTION. NEW ANGLE WAS FABRICATED IAW DWG 9957735, REV G. NEW ANGLE WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 21/14 NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: FRAME — CRACKED (BS 1463) · airframe 61,933 hrs · 45,822 cycles

CRACKED FRAME BS 1463 BETWEEN L8 - 9R. REMOVED IAW SRM 51-30-5. FABRICATED IAW DWG 9911839, REV DP. TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14, INSTALLED IAW SRM 51-30-5.

Part: FRAME — CRACKED (BS 1380) · airframe 61,933 hrs · 45,822 cycles

CRACK ON FRAME BS 1380 AT LONGERON 15L . FRAME REMOVED IAW SRM 51-30-2 AND 51-30-5, NEW FRAME FABRICATED IAW DWG 9912246, REV CY. NEW FRAME WAS TREATED AND PAINTED IAW SRM 51-10-30, PAR 14 AND 21.

Part: LONGERON — CRACKED (BS 1431) · airframe 61,933 hrs · 45,822 cycles

CRACK ON LONGERON 9R BS 1431. DAMAGED LONGERON REMOVED IAW SRM 53-02, FIG 18 AND 51-30-2. NEW SECTION DRILLED AND ADJUSTED IAW SRM 51-10-4 AND 53-02, FIG 18. REPAIR FABRICATED IAW SRM 53-02, FIG 18 AND 51-10-2 NEW LONGERON SECTION AND REPAIR WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21.

Part: SUPPORT — CRACKED (BS 1485) · airframe 61,933 hrs · 45,822 cycles

CRACKED LT AND RT STRUCTURE SUPPORTS AT BS 1485 X-10 AND X-10 OVER TORQUE TUBE AFT ACESORY COMPARTMENT. DAMAGE SUPPORTS WERE REMOVED IAW SRM 51-30-5 NEW SUPPORTS WERE DRILLED AND ADJUSTED IAW SRM 51-10-4 AND DWG 9911992 REV NEW SUPPORT WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 14-21. NEW SUPPORT WERE INSTALLED IAW SRM 51-30-5.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 61,933 hrs · 45,822 cycles

CRACK FOUND ON VERTICAL STABILIZER SKIN STA ZFS=18 LT SIDE FWD SECTION. INSTALLED REPAIR ON THE SKIN IAW SRM 55-01 FIG.2.

Part: DOOR — BENT (LT WING SLAT) · airframe 61,933 hrs · 45,822 cycles

BENT SLAT DOOR LT WING, FOUND OUT OF LIMITS. DOOR WAS FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-3, PARA 14 AND 21 AND ER/A 51235-14MA.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 61,933 hrs · 45,822 cycles

CRACKED FLOOR SUPPORT BS 1098. SUPPORT AND BRACKET REMOVED, SUPPORT DRILED, TREATED AND PAINTED. NEW SUPPORT AND BRACKET INSTALLED, CIC WAS APPLIED IAW SRM 51-10-3 AND 51-30-5, 51-30-2.

Part: BULKHEAD — CORRODED (BS 1338) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON BASE INNER FACE OF PRESSURE DOME BS 1338, BETWEEN LONGERONS 27L-27R. DAMAGE SECTION WAS REMOVED IAW SRM 53-03, FIG. 37. REPAIR FABRICATED IAW SRM 53-03, FIG 37, REPAIR INSTALLED IAW SRM 51-30-2, 51-30-5, 51-30-1 AND 53-03, FIG 37 AND ER/A 512884-14 MA.

Part: PAN — CRACKED (DOOR FRAME) · airframe 61,933 hrs · 45,822 cycles

CRACK ON PAN OF LT EMERGENCY OVERWING AFT EXIT DOOR AFT MID SECTION. NEW DOUBLER WAS FABRICATED, DRILLED, TRIMED, AND INSTALLED IAW SRM 52-05D, FIG 51.

Part: LONGERON — CRACKED (BS 1431) · airframe 61,933 hrs · 45,822 cycles

CRACK ON LONGERON 10 RT AT BS 1431 AFT ACCESSORY BAY. LONGERON SECTION WAS REMOVED IAW SRM 51-30-2, NEW LONGERON SECTION DRILLED IAW SRM 51-10-4. NEW SPLICE FABRICATED IAW SRM 53-02, FIG 18 AND NEW LONGERON SECTION AND SPLICE INSTALLED IAW SRM 53-02, FIG 18, 51-30-2.

Part: WEB — CRACKED (BS 1437) · airframe 61,933 hrs · 45,822 cycles

CRACK ON WEB AT BS 1437 BETWEEN LONGERONS 8-9L. REPAIR ACCOMPLISHED IAW ER/A 519146-14MA, REV ORIGINAL.

Part: LONGERON — CRACKED (BS 1437) · airframe 61,933 hrs · 45,822 cycles

CRACK ON LONGERON 4R BS 1437. DAMAGE REMOVED IAW SRM 53-02 AND 53-05. NEW LONGERON SECTION AND SPLICE WERE DRILLED AND ADJUSTED IAW SRM 51-10-4. NEW SECTION LONGERON AND SPLICE WERE TREATED IAW SRM 51-10-3, PAR 14.21 NEW LONGERON SECTION AND SPLICE WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: BRACKET — CORRODED (RT WING SPOILER) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON BRACKET ASSY OF OUTBOARD FLIGHT SPOILER ON RT WING STA XTE 290. CORRODED BRACKET REPLACED IAW AMM 27-60-00/501, 20-30-01 AND 20-10-17.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 61,933 hrs · 45,822 cycles

CRACKS ON RIBS AF VERTICAL STABILIZER L/E LT SIDE ZFS=36, 30, 23, 18 CARD 25, ZONE 65. RIBS WERE REMOVED ZFS=36-30-23-18, CRACKS WERE STOPS DRILLED, ANGLES THE REPAIR WERE FABRICATED, ANGLES THE FABRICATED WERE TREATED AND PAINTED, REPAIR PARTS WERE INSTALLED ON THE RIBS.

Part: FITTING — CORRODED (SLAT TRACK) · airframe 67,752 hrs · 49,964 cycles

SLAT NR 5 TRACK FITTINGS CORRODED. REPLACED THE SLAT TRACK FITTING.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 61,933 hrs · 45,822 cycles

RIBS CRACKED AT VERTICAL STABILIZER LEADING EDGE RIGHT SIDE ZFS=50,43,23. RIBS REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-2, 51-10-2, 51-10-3 PAR 14-21, AND 55-02, FIG 27.

Part: SKIN — DAMAGED (BS 685) · airframe 61,933 hrs · 45,822 cycles

DAMAGED ON FUSELAGE SKIN AT BS 685 BETWEEN LONGERONS 1-2L. BLENDED AND FOUND OUT LIMITS IAW SRM 53-04-1P.SD. REPAIR PERFORMED IAW SRM 53-04-2, P 3C, 2, A, 1, A.

Part: ATTACH ANGLE — CRACKED (BS 1463) · airframe 61,933 hrs · 45,822 cycles

CRACK FOUND ON ATTACH ANGLE FOR WEB FWD FACE BS 1463 LONGERONS 18-19R. ATTACH ANGLE REMOVED IAW SRM 51-30-2 AND NEW INSTALLED IAW SRM 51-30-2.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FUEL ACCESS PANEL NR 1361C COUNTERSINK AREA LT WING. CORROSION REMOVED AND FOUND OUT OF LIMITS. ACCESS PANEL REPLACED IAW SRM 51-22-2A.

Part: ANGLE — CRACKED (BS 1463 FRAME) · airframe 61,933 hrs · 45,822 cycles

CRACKED ANGLE ON FRAME AFT FACE BS 1463 BETWEEN LONGERONS 8 - 9L. ANGLE REMOVED IAW SRM 51-30-5, FABRICATED NEW ANGLE IAW DRAWING 9911839 REV DP, TREATED, & PAINTED IAW SRM 51-10-3, AND INSTALLED IAW SRM 51-30-5.

Part: SKIN — WORN (BS 1497-1510) · airframe 61,933 hrs · 45,822 cycles

WORN INNER SURFACE OF PREVIOUS REPAIR AT FUSELAGE SKIN BETWEEN STA Y=1497-Y=1510 AND 5 O`CLOCK POSITION. DAMAGE REMOVED, REPAIR FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 53-34-0, FIG.5 AND 51-10-3 PAR 14 AND 21.

Part: SUPPORT — DAMAGED (CARGO DOOR) · airframe 61,933 hrs · 45,822 cycles

ELONGATED HOLES ON PREVIOUS REPAIR OF FWD CARGO DOOR BARRIER SUPPORT, H1L2-SM, CARD 139, ZONE 100. SUMMARY DAMAGE AS REMOVED, NEW DOUBLER WAS FABRICATED, DOUBLER WAS TREATED AND PAINTED, DOUBLER WAS INSTALLED IAW SRM 51-30-2, 53-01 FIG 4, 53-01 FIG 4, 51-10-3, PAR 14 AND 21, 51-30-2.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 61,933 hrs · 45,822 cycles

DAMAGE CHANNEL OF FLOOR PANELS 826D AND 886C. REPLACED CHANNELS. REMOVED SRM 51-30-1, DRILLED SRM 51-10-4, INSTALLED DWG 9936639, REV P.

Part: FRAME — CRACKED (BS 1510) · airframe 61,933 hrs · 45,822 cycles

CRACK ON FRAME, BS 1510, AFT FACE 1 O`CLOCK POSITION, AFT ACCESSORY BAY. FRAME REMOVED AND REPLACED IAW SRM 53-14-4, FIG 3.

Part: WEB — CRACKED (NLG WW) · airframe 61,933 hrs · 45,822 cycles

CRACK ON WEB, Y=42 ABOVE OF FWD LT CORNER DOOR FRAME OF NLG. WEB WAS REMOVED AND INSTALLED IAW SRM 51-30-2.

Part: LONGERON — CRACKED (BS 1437) · airframe 61,933 hrs · 45,822 cycles

CRACK ON LONGERON 5L BS 1437. LONGERON SECTION REMOVED IAW SRM 51-30-5. NEW LONGERON SECTION AND REPAIR SPLICE INSTALLED IAW SRM 51-10-4, SRM 51-10-3, PAR 14 -21, SRM 51-30-2 AND 51-30-5.

Part: BULKHEAD — CORRODED (BS 1338) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON DOUBLER BASE OF PRESSURE DOME, BS 1338, LONG 30. CORROSION REMOVED AND WAS FOUND OUT OF LIMITS, DOUBLER WAS FABRICATED IAW DWG 5910130, REV "ET", TREATED AND PAINTED IAW SRM PARA 14-21 AND INSTALLED IAW SRM 51-30-2 / 51-30-5.

Part: CARGO TRACK — CORRODED (BS 1003-1155) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON RT CARGO TRACK FROM BS 1003 - 1155. FOUND TO BE OUT LIMITS. REMOVED AND REPLACED IAW SRM 51-30-1, 51-10-3, PAR 14/21 AND 51-30-2.

Part: FITTING — CORRODED (BS 1338) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON ANGLE FITTING AT LOWER WEB AFT FACE BS 1338 LONGERON 29R IN AFT CARGO BAY . REMOVED FITTING, & NEW FITTING WAS DRILLED IAW SRM 51-10-4, NEW FITTING ANGLE WAS TREATED, PAINTED AND WAS INSTALLED IAW SRM 51-30-2, 50-30-5.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 61,933 hrs · 45,822 cycles

CRACK FOUND ON FITTING OF RT HORIZONTAL STAB INBOARD LEADING EDGE XH=9. LEADING EDGE REMOVED AND DAMAGE ON FITTING WAS REMOVED, FLUORESCENT PENETRANT INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND, NEW FITTING DRILLED AND INSTALLED IAW SRM 55-12-0D FIG. 801D AND AMM 55-10-01-201.

Part: DOUBLER — CORRODED (BS 760-776) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION FOUND ON SETTLEMENT AREA AT REPAIR DOUBLER BS 760 - 776 BETWEEN LONGERONS 27 - 29R. REPAIR DOUBLER REMOVED, NEW DOUBLER FABRICATED AND INSTALLED IAW SRM 51-30-5 53-04, PAR 57 AND 51-10-3.

Part: DOOR FRAME — CORRODED (BS 1212) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON AFT DOOR FRAME BS 1212 LONGERON 26 RT. DAMAGE AREA WAS REMOVED, FILLER AND DOUBLER WERE FABRICATED, NDT CHECK AND WERE TREATED AND PAINTED, REPAIR PARTS WERE INSTALLED IAW SRM 51-10-3 PAR. 21, 14, 38 AND 53-01, FIG. 2.

Part: CUSP WEB — CORRODED (BS 984-1003) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON LT REPAIR DOUBLER ON CUSP WEB BETWEEN BS 984-1003 AND X= 54-60 AT PAX CABIN. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A.

Part: SKIN — DAMAGED (RUDDER) · airframe 61,933 hrs · 45,822 cycles

DAMAGED METALIZED COATING ON BOTH FACES OF RUDDER. RUDDER REPAIRED IAW AC 0969, CARD 2000-8149-01 AND SRM 51-10-1AD, PAR 23.

Part: SEAT TRACK — CORRODED (BS 213-215) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

WEAR AND CORROSION ON RT SEAT TRACK, X -44, BS 213-215. SEAT TRACK REMOVED, NEW SEAT TRACK WAS DRILLED, TREATED, PAINTED, AND INSTALLED IAW SRM 53-05, FIG 4F, 51-30-5, 51-30-2, 51-30-1, 51-10-3.

Part: FLOORBEAM — CORRODED (BS 1166) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FLOORBEAM ANGLE BS 1166 AND X 54-60. FLOORBEAM ANGLE AND CORROSION REMOVED, REWORKED AREA WAS MEASURED, OUT OF LIMITS, NEW FLOORBEAM ANGLE DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-10-3, PARA 14, 21, 26, 38, 53-01, FIG 1 AND 51-30-5.

Part: FITTING — CORRODED (BS 1309) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FITTING BS 1309 BETWEEN LONGERONS 18-19L. CORROSION REMOVED IAW SRM 51-10-3. FITTING REPLACED IAW DWG 9912243 AND INSTALLED IAW SRM 51-30-5.

Part: SKIN — CORRODED (BS 1309-1322) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON EXTERNAL REPAIR AROUND AFT LAVATORY SERVICE PANEL BS 1309-1322. REPAIR REMOVED, NEW FABRICATED, TREATED, PAINTED AND INSTALLED IAW ER/A 469473-14 REV ORIG.

Part: WEB — CRACKED (BS 1474) · airframe 61,933 hrs · 45,822 cycles

CRACK ON RT WEB BS 1474 LONGERON 25R AFT ACCESSORY BAY. CRACK STOPPED IAW SRM 53-01, FIG 2, NEW DOUBLER WAS FABRICATED IAW SRM 53-01, FIG 2 NEW DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21. NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — DAMAGED (RUDDER TAB) · airframe 61,985 hrs · 45,859 cycles

DAMAGE METALIZED COAT ON BOTH FACES OF RUDDER TAB. RUDDER TAB WAS REPAIRED IAW SRM 51-70-1AD, PA 23.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FUEL ACCESS PLATE NR 1335C COUNTERSINK AND SETTLEMENT AREA AT LT WING. CORROSION ON COUNTERSINK WAS REMOVED AND MAXIMUM DIAMETER ALLOWABLE IS 0.660" AND WERE FOUND 3 COUNTERSINK ADJACENTS OUT OF LIMITS MEASURED 0.673", 0.672" AND 0.674 ON ACCESS PLATE 1335C THEREFORE ACCESS WAS REPLACED IAW SRM 51-22-2A, CONDITION II. TOOL USED CHAMFER GAGE, PN 1127, SN 35465.

Part: SLAT TRACK — CORRODED (LT WING) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON HOLES OF INBD AND MID SLAT TRACK FITTING AT LT WING SLAT PANEL. REPAIRED SRM 57-02, PAR 9.

Part: SLAT TRACK — CORRODED (LT WING) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON HOLES OF INBD, MID AND OTBD SLAT TRACK FITTING LOCATED ON LT WING. REPAIRED IAW SRM 57-02, PAR 9.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FUEL ACCESS PANEL 1462C, COUNTERSINK AREA AT RT WING. CORROSION REMOVED AND WAS FOUND OUT OF LIMITS. ACCESS PANEL REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FUEL ACCESS PANEL 1355 COUNTERSINK AREA ON LT WING. CORROSION WAS REMOVED AND WAS FOUND OUT OF LIMITS. ACCESS PANEL REPLACED IAW SRM 51-22-2A.

Part: LONGERON — CRACKED (BS 1437) · airframe 61,933 hrs · 45,822 cycles

CRACK ON LONGERON 12LT BS 1437. LONGERON REMOVED, NEW SECTION AND SPLICE DRILLED AND ADJUSTED, NEW SECTION OF LONGERON AND SPLICE TREATED AND PAINTED, NEW SECTION OF LONGERON AND SPLICE INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-4, 53-02 FIG 18, AND 51-10-3, PAR 21 AND 14.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FUEL ACCESS PANEL 1456C COUNTERSINK AREA LT WING. CORROSION REMOVED AND WAS FOUND OUT OF LIMITS. ACCESS PANEL REPLACED IAW SRM 51-22-2A.

Part: SEAT TRACK — CORRODED (BS 937-1002) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON RT SEAT TRACK, BS 1002, 954 AND 937, X=-54. DAMAGE REMOVED IAW SRM 53-05, FIG 4A, 51-10-3 PAR 14, 21 AND 38.

Part: CUSP WEB — CRACKED (BS 801-805) · airframe 61,933 hrs · 45,822 cycles

CRACKED CUSP WEB BETWEEN BS 801-805 X=-54- X=-60. CUSP WEB REMOVED, NEW CUSP WEB FABRICATED AND INSTALLED IAW SRM 53-14-02, SRM 53-05 FIG 131A, SRM 51-10-3 PAR 14, 21.

Part: CARGO TRACK — CORRODED (BS 1211-1309) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON RT CARGO TRACK BS 1211 - 1309. CARGO TRACK REPLACED IAW SRM 51-30-1 AND 51-30-2.

Part: DOUBLER — CORRODED (BS 927-946) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON LT PRODUCTION DOUBLER BETWEEN STA Y=927-946 AND STA X=54 TO 60 AT PAX CABIN. CUSP WEB REPLACED IAW SRM 5305K, FIG 131, PREVIOUS WEB WAS REMOVED, NEW. CUSP WEB WAS FABRICATED, REPAIR PARTS TREATED PAINTED AND INSTALLED IAW SRM 53-05, FIG 131 AND 51-10-3 AND 51-30-2 PRIMARY STRUCTURE CORROSION LEVEL 2. CUSP WEB REPLACED IAW SRM 5305, FIG 131 PREVIOUS WEB WAS REMOVED, NEW CUSP WEB WAS FABRICATED REPAIR PARTS TREATED PAINTED AND INSTALLED IAW SRM 53-05, FIG 131 AND 51-10-3 AND 51-30-2.

Part: CARGO TRACK — CORRODED (BS 1220-1322) · airframe 67,752 hrs · 49,964 cycles

THE LEFT CARGO TRACK CORRODED, BS 1220-1322, BETWEEN LONGERON 27 - 28L. THE CARGO TRACK WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 200-218) · airframe 67,752 hrs · 49,964 cycles

CUSP WEB CORRODED BS 200-218, X -54. THE CUSP WEB WAS REPLACED.

Part: FLOORBEAM — CORRODED (BS 256) · airframe 67,752 hrs · 49,964 cycles

FLOORBEAM CORRODED BS 256, X=22 TO -22. FLOORBEAM WAS REMOVED AND REPLACED.

Part: DOUBLER — CORRODED (BS 1287-1309) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON INTERNAL DOUBLER BS 1287-1309 BETWEEN LONGERONS 20-22L. REMOVED, DRILLED AND TRIMMED TREATED AND PAINTED DOUBLER. DOUBLER INSTALLED IAW IAW SRM 51-30-2 AND DWG 5936021, REV EH. PARTS AND INTERNAL DOUBLER WERE REMOVED, NEW DOUBLER WAS DRILLED AND TRIMMED, TREATED AND PAINTED PARTS , PARTS AND DOUBLER WERE INSTALLED IAW DC9/MD80 IAW DC9/MD80: SRM 51-30-2 AND DOUGLAS DWG 5936021 REV.

Part: CUSP WEB — CORRODED (BS 190-200) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON RT CUSP WEB, BS 190 - 200 X-54 - X-60. REMOVED AND REPLACED IAW SRM 53-05, FIG 55.

Part: ATTACH FITTING — CORRODED (NR 2 SLAT) · airframe 67,752 hrs · 49,964 cycles

NR 5 LEADING EDGE SLAT ATTACH FITTING CORRODED. SLAT REPLACED.

Part: CUSP WEB — CORRODED (BS 453-458) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON RT CUSP WEB PREVIOUS REPAIR DOUBLER BETWEEN BS 453-458, X=-54 TO X=-60. PREVIOUS REPAIR DOUBLER REMOVED, NEW REPAIR FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-5 AND 53-05, FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 493-501) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON RT CUSP WEB PREVIOUS REPAIR DOUBLER BETWEEN BS 493-501, X=-54 TO X=-60. REPAIR REMOVED, REPAIR DOUBLERS FABRICATED, TREATED AND PAINTED, AND REPAIR INSTALLED IAW SRM 51-30-5, 51-30-2 AND 53-05, FIG 131-A-13.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 61,933 hrs · 45,822 cycles

CRACK ON PAN BELLOW STOP FITTING NR 4 AT AFT CARGO DOOR. C3, H1L2-SM, ZONE 100/ CARD 241, C1. CRACK WAS STOPPED DRILLED IAW SRM 52-05D, FIG 50 DOUBLER WAS FABRICATED IAW SRM 51-10-3, PAR 14 AND 31 DOUBLER WAS INSTALLED IAW SRM 51-30-2. RII COMPLETED BY INSPECTION STAMP, INSPECTOR, RCC 200700741, TECHOPS DELTA ID 049617.

Part: FITTING — CORRODED (SLAT TRACK) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON HOLES OF SLAT TRACK FITTING AT RT WING SLAT PANEL 2 MID OTBD AND INBD SECTION, SM CARD 2, ZONE 12. SLAT TRACK HOLES WERE REPAIRED WITH A BUSHINGS IAW SRM 57-02, PAR 9 AND ER/A 525374-14 REV ORIGINAL.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON LT BARREL NUT NR 11 AND 12 HORIZONTAL STABILIZER. CORROSION REMOVED, BARREL NUT HOLES WERE REAMED AND BUSHINGS WERE FABRICATED AND INSTALLED. IAW IAW SRM 55-30D, PAR 30.

Part: FLOOR SUPPORT — CORRODED (BS 184-194) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 184-194, X=50-X=54 . FLOOR SUPORT REMOVED AND REPLACED IAW SRM 53-14-10-4; 51-10-3.

Part: CUSP WEB — DAMAGED (BS 842) · airframe 61,933 hrs · 45,822 cycles

RT CUSP WEB DAMAGED BS 842, X:-60. DAMAGE AREA WAS REMOVED, REPAIR PARTS FABRICATED AND REPAIR TREATED AND PAINTED AND INSTALLED.

Part: CUSP WEB — DAMAGED (BS 504-511) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON RT CUSP WEB PREVIOUS REPAIR DOUBLER BETWEEN BS 504 -511, X:-54-X:-60. REPAIR DOUBLER WAS REMOVED, NEW REPAIR FABRICATED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-5, 51-10-3, PAR 14,21 AND 338 ER/A 398191-14 MA, REV B.

Part: FLOOR SUPPORT — CORRODED (BS 1309-1345) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 1309 - 1345, X=-17 . FLOOR SUPPORT REPLACED IAW DWG 9936656 REV AN AND SRM 51-30-1.

Part: CUSP WEB — CORRODED (BS 636-642) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON LT CUSP WEB BETWEEN BS 636 - 642 X=54 TO X=60. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131A-7, SHEET 1, REPAIR FABRICATED IAW SRM 53-05, FIG 131, A-7, SHEET 4, REPAIR TREATED AND PAINTED IAW SRM 53-05, FIG 131A-7, SHEET 7, AND REPAIR INSTALLED IAW SRM 53-05, FIG 131A-7.

Part: CUSP WEB — CRACKED (BS 1201) · airframe 61,933 hrs · 45,822 cycles

CRACK ON LT CUSP WEB BS 1201 X=54 - 60. DAMAGE AREA REMOVED, REPAIR FABRICATED, TREATED AND PAINTED, REPAIR INSTALLED IAW SRM 51-10-3, PAR 21, 14 53-05, FIG 131A-13.

Part: SEAT TRACK — CORRODED (BS 808-813) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON SEAT TRACK X=-54 BS 808-813. PREVIOUS REPAIR REMOVED IAW SRM 51-30-1. NEW REPAIR INSTALLED IAW SRM 53-04, FIG 4A, SHEET 1.

Part: CUSP WEB — CORRODED (BS 1110-1117) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON RT CUSP WEB LOWER SUFACE BETWEEN BS 1110 - 1117, X- 44 - X-60. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 51-10-3, PAR 26, SRM 53-05, FIG 131A-13 AND ER/A 511165-14MA REV B.

Part: CUSP WEB — CORRODED (BS 1231-1250) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON RT CUSP WEB UPPER & LOWER SURFACES BETWEEN BS 1231-1250, X=-54 TO X=-60. CORROSION WAS REMOVED AND FOUND OUT OF LIMITS. REPAIRED IAW SRM 51-10-3, PAR 26, ER/A 511165-14 MA, REV A AND 53-05, FIG 131A-13.

Part: LONGERON — CRACKED (BS 1309) · airframe 61,933 hrs · 45,822 cycles

CRACKED LONGERON 8RT BS 1309. SECTION OF LONGERON REMOVED IAW SRM 51-30-2, 53-02, FIG 18. NEW SECTION OF LONGERON AND REPAIR WERE TRIMMED AND DRILLED IAW SRM 53-02, FIG 18, TREATED AND PAINTED IAW SRM 51-10-3 PAR 14 AND 21. NEW SECTION OF LONGERON AND REPAIR SPLICE INSTALLED IAW SRM 53-02, FIG 18, 51-30-2 AND 51-30-5.

Part: SEAT TRACK — WORN (BS 591-595) · airframe 61,933 hrs · 45,822 cycles

WORN PLUG ON LT SEAT TRACK, X=22, BS 591-595. PLUG WAS REMOVED, NEW PLUG INSTALLED IAW SRM 53-05, FIG 4A, SHEET 2.

Part: CUSP WEB — CRACKED (BS 867-869) · airframe 61,933 hrs · 45,822 cycles

CRACKED RT CUSP WEB BETWEEN BS 867 - 869 X=-54 X=-60 . CRACK WAS STOP DRILLED, PERFORM HFEC, FABRICATED DOUBLER. DOUBLER WAS TREATED, PAINTED, AND INSTALLED APPLYED IC IAW SRM 51-01, PAR 21, 53-05, FIG 131A-10, 51-10-3 AND 51-30-2.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FUEL ACCESS PLATE NBR 1409C COUNTERSINK AND SETTLEMENT AREA AT RT WING SUMMARY: BLEND OUT REPAIR IS NOT PERMITTED ON THE UPPER WING ACCESS DOOR, PN 3912757, DUE TO THE REDUCED AREA OF THE CONDUCTIVE INTERFACE THEREFORE ACCESS PLATE NR 1409C WAS REPLACED IAW SRM 51-22-2A.

Part: FRAME — CRACKED (BS 1510) · airframe 61,933 hrs · 45,822 cycles

CRACK FOUND ON FRAME, BS 1510 . DAMAGE WAS CUT-OUT, HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS FOUND IAW ERA 497316-14 MA REV. ORIG. DOUBLER AND FILLER FABRICATED, TREATED, PAINTED AND INSTALLED I.A.W. ER/A 497316-14 MA REV. ORIGINAL.

Part: SEAT TRACK — DAMAGED (BS 825-830) · airframe 61,933 hrs · 45,822 cycles

PREVIOUS REPAIR PLUG ON SEAT TRACK CORRODED X=-54 BETWEEN BS 825-830. . REPAIR PLUG REMOVED IAW SRM 51-30-1 NEW PLUG INSTALLED IAW SRM 53-05, FIG 4A.

Part: SEAT TRACK — DAMAGED (BS 826) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON LT SEAT TRACK PLUG, X 54, BS 826. REPAIR PLUG WAS REMOVED IAW SRM 51-30-1. NEW PLUG INSTALLED IAW SRM 53-05, FIG 4A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FUEL ACCESS PLATE NRS 1454C AND 1436C AT LT WING, MRB 5732-083, SM. CORROSION ON COUNTERSINKS AT FUEL ACCESS PLATE NR 1454C WAS REMOVED AND MAXIMUM DIAMETER ALLOWABLE IS 0.532" ND WERE FOUND 4 COUNTERSINKS ADJACENTS OUT OF LIMITS, MEASURED 0.557", 0.554", 0.547" AND 0.541" ON ACCESS PLATE NR 1454C THEREFORE ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A, CONDITION II. CORROSION ON COUNTERSINKS AT FUEL ACCESS PLATE NR 1436C AS REMOVED AND MAXIMUM DIAMETER ALLOWABLE IS 0.660" AND WERE FOUND 3 COUNTERSINKS ADJACENT OUT OF LIMITS, MEASURED: 0.671", 0.672" AND 0.670" ON ACCESS PLATE NBR 1436C THEREFORE ACCESS PLATE WAS REPLACED IAW SRM 51-22-2A, CONDITION II.

Part: DOUBLER — CORRODED (BS 817-827) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON LEFT PRODUCTION DOUBLER BETWEEN BS 817-827, X=54-60. DOUBLER REMOVED IAW SRM 51-30-2 AND CORROSION REMOVED IAW SRM 51-10-3. FOUND WITHIN LIMITS. AREA TREATED, PAINTED AND REPAIR INSTALLED IAW SRM 51-30-2 AND ER/A 511165-14MA, REV B.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 61,933 hrs · 45,822 cycles

CORROSION ON FLOOR SUPPORT AT PASSENGER CABIN, STA= 1174, X=16 LOWER SURFACE. REPLACED FLOOR SUPPORT. NEW FLOOR SUPPORT WAS DRILLED AND ADJUSTED, TREATED AND PAINTED, AND INSTALLED IAW SRM 51-30-5, 51-10-4, 51-10-3 PAGE. 14, 21.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,351 hrs · 45,434 cycles

FLIGHT CREW DISCOVERED THAT THE EMERGENCY LIGHTING IN THE COCKPIT WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BULB — UNSECURE (EMERGENCY LIGHT) · airframe 60,964 hrs · 45,201 cycles

DURING SERVICE CHECK, NOTED THE LEFT OVERWING EMERGENCY EXIT SIGN WAS NOT ILLUMINATING. BULBS SEATED AND OPS CHECKED NORMALLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,613 hrs · 44,949 cycles

OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 28-31. REPLACED BATTERY PACK. OPS CHECKED GOOD IAW AMM 33-53-00.

Part: LANYARD — DETACHED (GIRT BAR) · airframe 60,560 hrs · 44,917 cycles

R1 DOOR SLIDE COVER RELEASE LANYARD HAD BECOME DETACHED FROM THE GIRT BAR. LANYARD WAS ATTACHED AMM 25-62.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,328 hrs · 44,740 cycles

DURING ROUTINE LINE CHECK, MX FOUND ALL EMERGENCY EXIT LIGHTS QUICKLY DISCHARGING AND BECOMING INOPERATIVE AFTER A FEW SECONDS. REPLACED ALL EMERGENCY EXIT LIGHT BATTERY PACKS IAW AMM 33-53 AND OPS CHECKED NORMALLY.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 59,559 hrs · 44,191 cycles

DURING SCHEDULED INSPECTION, THE LT HORIZONTAL STABILIZER CENTER SKIN EXHIBITED AN NDT CRACK INDICATION. SURFACE COATINGS WERE REMOVED AND ANOTHER NDT CHECK WAS ACCOMPLISHED AND THE CRACK INDICATION WAS VERIFIED AT THE AFT INBD CORNER. THE HORIZONTAL STABILIZER WAS REPLACED IAW AMM 55-10-00-201, AND ER/A 507849-14AD, REV E STEPS 3-4.

Part: BULKHEAD WEB — CRACKED (BS 1437) · airframe 59,557 hrs · 44,189 cycles

DURING SCHEDULED C-CHECK, A CRACK WAS FOUND ON BULKHEAD WEB AREA LOCATED AT FRAME BS 1437, JUST OTBD, AT THE 4918093-504 FITTING; COMMON TO THE 9953016-3 WEB. ADDITIONAL CRACKS WERE FOUND IN THE BULKHEAD AREA LOCATED AT FRAME BS 1437, NEAR THE 4918093-503 / -504 FITTINGS. PERMANENT REPAIR INSTALLED IAW ER/A 514849-14.

Part: SKIN — CRACKED (BS 1418) · airframe 59,557 hrs · 44,189 cycles

DURING SCHEDULED INSPECTION, SKIN WAS FOUND CRACKED BS 1418. REPAIRED IAW ER/A 514704-14AD.

Part: BULKHEAD WEB — CRACKED (BS 1437) · airframe 59,557 hrs · 44,189 cycles

DURING C-CHECK, A CRACK WAS FOUND ON THE BULKHEAD WEB AREA LOCATED AT FRAME BS 1437, JUST OTBD OF THE 4918093-503 FITTING, COMMON TO THE TO THE 9953016-3 WEB. ADDITIONAL CRACKS WERE FOUND IN THE BULKHEAD AREA ON THE WEB 9953016-3, NEAR L2L AND L2R, AND ON THE UPPER OUTER CAP NEAR L2R. PERMANENT REPAIR WAS ACCOMPLISHED IAW ER/A 514849-14.

Part: BULKHEAD WEB — CRACKED (BS 1437) · airframe 59,557 hrs · 44,189 cycles

DURING SCHEDULED INSPECTION, A CRACK WAS FOUND ON THE BULKHEAD WEB AREA LOCATED AT FRAME STA Y= 1437, JUST OTBD OF THE FITTING, COMMON TO THE TO THE WEB. ADDITIONAL CRACKS WERE FOUND IN THE BULKHEAD AREA ON THE WEB NEAR L2L AND L2R, AND ON THE UPPER OUTER CAP NEAR L2R. REPAIR ACCOMPLISHED IAW ER/A 514849-14.

Part: SKIN — CRACKED (BS 1418) · airframe 59,557 hrs · 44,189 cycles

DURING SCHEDULED INSPECTION, FOUND CRACK ON AFT SIDE OF BS 1418 UPPER SIDE OF L2R LOCATED UNDER SKATE ANGLE. REPAIRED IAW ER/A 514704-14AD. THIS DISCREPANCY ADDRESSES A CRACK AT THE 4TH FASTENER HOLE ABOVE L-3R. THE SAME REPAIR SCHEME APPLIES IAW ER/A 514704-14AD TO THIS CORRESPONDING AREA.

Part: SKIN — CRACKED (BS 1418 L2R) · airframe 59,557 hrs · 44,189 cycles

DURING SCHEDULED INSPECTION, FOUND SKIN CRACKED BS 1418 UPPER SIDE OF L2R LOCATED UNDER SKATE ANGLE. REPAIRED IAW ER/A 514704-14AD.

Part: BRACKET — WORN (TAILCONE RELEASE) · airframe 59,557 hrs · 44,189 cycles

DURING SCHEDULED MX CHECK, THE UPPER TAIL CONE LANYARD SPRING BRACKET WAS NOTED TO BE WORN. THE UPPER TAIL CONE SPRING BRACKET WAS REPLACED IAW SRM 51-01.

Part: RECEPTACLE — WORN (TAILCONE LATCH) · airframe 59,557 hrs · 44,189 cycles

DURING SCHEDULED MX CHECK, THE UPPER RT TAIL CONE LATCH RELEASE RECEPTACLE WAS NOTED TO BE WORN. THE UPPER RT TAIL CONE RELEASE RECEPTACLE WAS REPLACED IAW AMM 53-53 .

Part: PIN — WORN (TAILCONE RELEASE) · airframe 59,557 hrs · 44,189 cycles

DURING SCHEDULED CHECK, THE TAIL CONE RELEASE T-PIN WAS NOTED TO BE WORN. THE TAIL CONE RELEASE T-PIN WAS REPLACED IAW AMM 53-53.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 59,557 hrs · 44,189 cycles

DURING SCHEDULED MX CHECK, NUMEROUS TAILCONE ALIGNMENT PIN RECEPTACLES WERE NOTED TO BE WORN (15EA). WORN RECEPTACLES WERE REPLACED IAW DWG-9911957.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 59,557 hrs · 44,189 cycles

DURING SCHEDULED INSPECTION, THE C3 CARGO DOOR FRAME LOWER SILL AREA WAS NOTED TO HAVE CORROSION. REPAIRED IAW SRM 53-05, FIG 123A.

Part: CLAMP — WORN (TAILCONE) · airframe 59,557 hrs · 44,189 cycles

DURING SCHEDULED CHECK, THE UPPER RT UPPER LATCH CLAMP SLOT FOR THE TAILCONE LATCH ATTACHMENT WAS NOTED TO BE WORN. MX REPLACED THE RT UPPER LATCH CLAMP IAW AMM 53-53.

Part: LANYARD — MISINSTALLED (GIRT BAR) · airframe 59,527 hrs · 44,175 cycles

FLIGHT CREW REPORTED THAT THE DOOR R1 GIRT BAR WAS NOT ATTACHED TO THE SLIDE. MX REINSTALLED THE LANYARD FROM THE GIRT BAR TO THE SLIDE COVER.

Part: WEB — CRACKED (CATWALK) · airframe 59,290 hrs · 44,004 cycles

REPORT OF AFT CATWALK NOT LINING UP. FOUND CRACK ON SIDE OF CATWALK - RT SIDE FLAP. REPAIRED CRACK IN RT SIDE CATWALK WEB IAW SRM 53-01, FIG 2. OPS CHECKS GOOD. CLEARED MCO AND REMOVED PLACARDS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,741 hrs · 43,594 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN ROWS 24-36 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,814 hrs · 42,909 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE COCKPIT AND THE FIRST CLASS GALLEY SECTION HAD ALL FAILED. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING LINE CHECK, MAINTENANCE FOUND THAT BOTH OF THE EXTERIOR EMERGENCY FLOOD LIGHTS AND SEVERAL CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY (B5-49) AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 55,748 hrs · 41,510 cycles

AFT CARGO COMPARTMENT, LT SIDE OF AFT PRESSURE BULKHEAD AFT SIDE OF WEB AT STA 1338, EXFOLIATED CORROSION. REMOVED CORROSION, MATERIAL LOSS FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS, INSTALLED REPAIR IAW DC9/MD80 SRM 51-70-4 FIG 2, DURING PSV AT ST AEROSPACE SAN ANTONIO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 55,748 hrs · 41,510 cycles

CORROSION ON AFT CARGO COMPARTMENT FUSELAGE FRAME LOWER FLANGE AFT SIDE AT STA 1136 BETWEEN LONGERON 29R AND LONGERON 30. REMOVED CORROSION ON FRAME, MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE, FABRICATED REPAIR ANGLES AND FILLERS AND INSTALLED REPAIR IAW DC9/MD80 SRM 51-70-5 FIG 2 AT ST AEROSPACE SAN ANTOINO DURING PSV.

Part: PANEL — CORRODED (E&E BAY) · airframe 55,748 hrs · 41,510 cycles

CORROSION ON E & E COMPARTMENT, CEILING WEB PANEL AT STA 14 LBL 13. REMOVED CORROSION, MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW DC9/MD80 SRM 53-01. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9/MD80 SRM 53-01 FIG 4. DURING PSV AT ST AEROSPACE SAN ANTONIO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,748 hrs · 41,510 cycles

FWD CARGO DOOR AREA FLOOR SUPPORT STRUCTURE CRACKED FS 370 L26L. REMOVED DAMAGE ON FLOOR SUPPORT, FABRICATED ANGLE REPAIR AND FILLER, INSTALLED REPAIR PER DC9/MD80 SRM 51-70-5 PG 12 DURING PSV AT ST AEROSPACE SAN ANTONIO.

Part: LIGHT — DAMAGED (SEAT 25D) · airframe 51,550 hrs · 38,585 cycles

EMERGENCY LIGHT AT SEAT 25D INOP. FOUND LIGHT ASSY DAMAGED. R & R EMERGENCY LIGHT ASSY AT SEAT 25D. OPS CK NML.

Part: LIGHT — INOPERATIVE (ROW 25 D&E) · airframe 51,501 hrs · 38,549 cycles

DURING L/O FOUND ROW 25 ED EMERGENCY TRACK LIGHT AFT RED LIGHT ASSY INOP. REPLACED LIGHT ASSY. RED LENS INSTALLED. OPS NORMAL.

Part: SLIDE — UNWANTED DEPLOY (L-2 DOOR) · airframe 48,870 hrs · 36,748 cycles

L-2 DOOR SLIDE ACCIDENTAL DEPLOYMENT WITH NO INFLATION. REMOVED OLD SLIDE PACK. INSTALLED NEW SLIDE PER AMM 25-62-00-201 FOR SERVICE.

Part: SKIN — GOUGED (NR 2 NACELLE) · airframe 45,952 hrs · 34,834 cycles

DUE SPLSKD SRM REPAIR 53-04 DENT/GOUGE NR 2 PYLON ABOVE LGN 19R FWD OF STA 1309. REPAIRED PER SRM 53-04D FIG 12B CLASS 2. REINSPECT DUE AT 15000 CYCLES. DATA RETRIEVAL SENT.

Part: TIRE — FAILED (NR 1 MLG) · airframe 45,038 hrs · 34,206 cycles

A/C ARRIVED AT GATE E-7, NR 1 MLG TIRE SHREDDED DAMAGING NR 2 AFT BRAKE LINE, LT STRUT CLAMP, SPLASH GUARD, LT INBOAD FLAP (DENT), LT FUSELAGE (MARK), NR 1 ENG NOSE COWL (UNDERSIDE - MARK).

Part: BATTERY — WEAK (EMERGENCY LIGHT) · airframe 44,565 hrs · 33,913 cycles

FOUND OVERWING EMERGENCY EXIT IDENTIFIER LIGHTS INOP. REPLACED BATTERIES. EMERGENCY LIGHTS CHECK GOOD.

Part: B-NUT — LOOSE (HYD SYSTEM) · airframe 41,605 hrs · 31,984 cycles

NORMAL LANDING AND TAXI WHILE APPROACHING GATE. APU STARTED, FLT ATTENDANT REPORTED CABIN FILLING WITH SMOKE. APU/PNEUMATICS SHUTDOWN. CABIN DOORS AND EMERGENCY EXITS OPENED TO VENT. SMOKE DISSIPATED. L2 DOOR SLIDE WAS INADVERTANTLY DEPLOYED. MTC DISCOVERED THE LEFT THRUST REVERSER ACCUMULATOR HYD LINE B-NUT LOOSE AND SQUIRTING HYD FLUID. TIGHTENED SAME, LEAK CHECKS GOOD. ALL EMERGENCY EQUIPMENT OPERATED NORMALLY.

Part: TURBINE — FAILED (APU) · airframe 37,768 hrs · 29,292 cycles

SMOKE ODOR IN THE CABIN. REPLACED APU FOR LEAKAGE.

Part: SWITCH — LEAKING (APU) · airframe 37,762 hrs · 29,288 cycles

ON T/O FLT ATTENDANT REPORTED SMOKE IN THE CABIN AND LAVATORY SMOKE DETECTORS GOING OFF, ATB BACK TO JAX. FOUND APU INLET CONTAMINATED WITH APU OIL. PERFORMED OPN 5088 AND OPN 5089 DUCT BURNOUT. OIL LEAK FROM APU LOW OIL PRESSURE SWITCH BODY. DEACTVATED APU AND FORWARD TO MCO AND PLACARD.

Part: PACKING — DETERIORATED (RUDDER S/O VALVE) · airframe 37,511 hrs · 29,107 cycles

SMOKE ALARM SOUNDED WITH ENGINE A/I ON. ODOR NOTED IN PACK SYSTEM. REPLACED O-RING AT RUDDER SHUTOFF VALVE. CLEANED AFT FUSELAGE SECTION AND COMPLETED ALTERNATE DUCT BURNOUT. CHECKS GOOD.

Part: ENGINE — FIRE (NR 2) · airframe 36,460 hrs · 28,330 cycles

ON TAXI OUT ANOTHER AIRCRAFT REPORTED SMOKE AND OR FIRE ON NR 2 ENGINE. REPLACED ENGINE.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 32,794 hrs · 25,833 cycles

DURING HMV-2, WEAR TO THE UPPER AFT CORNER OF THE UNDERLYING SKIN DOUBLER SURROUNDING THE AFT LAV. SERVICE DOOR JAMB. DAMAGE WAS REMOVED AND REPAIR DOUBLER INSTALLED.

Part: SKIN — CORRODED (LH FUSELAGE) · airframe 32,794 hrs · 25,833 cycles

DURING HMV-2, CORROSION WAS FOUND ALONG FUSELAGE SKIN BETWEEN L-28L TO L-29L AND STA 692-718. CORROSION WAS BLENDED AND PERMANENT REPAIR MADE PER SRM 53-04 FIGURE 12B.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 28,739 hrs · 22,872 cycles

ON L/O FOUND FWD CBN WHITE EMERGENCY LIGHTS INOP AT SEAT ROWS 10,11,12,13. REPAIRED DAMAGED WIRE AT SEATROW 1R--RPLCD PWR SUPPLY PER M/M. ALL LIGHTS CK GOOD

Part: WARNING LIGHT — ILLUMINATED (NR 1 ENGINE) · airframe 26,724 hrs · 21,406 cycles

LEFT ENG OIL STRAINER CLOG LIGHT ON. C/E POM SHUT DOWN ENG. REMOVED NR 1 OIL FILTER, CHECKED FOR CONTAMINATION, NO VISABLE CONTAMINATION NOTED. REPLACED FILTER, RAN ENG. NO LEAKS AND NO RETURN OF MSG. FWD ANNUCIATION TO MCO/PLAC MEL 79-00-05.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 26,428 hrs · 21,176 cycles

EN ROUTE, RECEIVED LEFT ENGINE OIL STRAINER CLOGGED MSG. SHUTDOWN ENGINE PER POM AND DIVERTED TO RDU. FOUND OIL FILTER LOADED WITH CARBON. REPLACED SAME.

Part: PACK — MALFUNCTIONED (RIGHT)

DURING CRUISE FLIGHT, FLIGHT ATTENDANT COMPLAINED OF A BURNING ODOR IN CABIN. DESECENDED AND SHUT OFF THE LEFT A/C PACK WITHIN 1 MIN. THE RIGHT PACK TEMP VLV OPENED TO FULL HOT WITH THE RIGHT PACK TEMP CONTROL IN AUTO. TURNED THE LEFT PACK ON, TURNED OFF THE RT PACK AND WITHIN 3 MINS THE BURNING ODOR DISSIPATED IN THE CABIN. DID DUCT BURN-OUT PER M/M. CKD OPERATION OF BOTH PACKS, PACK OPERATION NORMAL, REPLACED COALESCER BAGS.

Part: STRUT — REQUIRED SERVICE (NLG)

RED NOSE GEAR LIGHT STAYED ON WITH HANDLE IN UP POSITION. RECYCLED GEAR PER POM. SAME RESULT. ALL GEAR INDICATED NORMAL WITH GEAR HANDLE DOWN. FOUND NOSE STRUT UNDERSERVICED. SERVICED STRUT PER M/M. CHECK FOR LEAKS. NO LEAKS. JACKED AIRCRAFT SWUNG NOSE LANDING GEAR. ALL INDICATION NORMAL.

Part: OVEN — FAILED (GALLEY)

FWD GALLEY OVEN OVERHEATED AND STARTED SMOKING, PULLED C/B AND DISCONNECTED GALLEY POWER, SMOKED STIPPED. REPLACED OVEN/OPS OK.

Part: SKIN — DENTED (BS 446)

THE FUSELAGE SKIN WAS FOUND TO HAVE A DENT AT FS 446 BETWEEN STRINGER 28R AND 29R. THE DENT WAS CUT OUT WITH DIMENSIONS OF 10.5 FWD/AFT BY 9.75 UP/DOWN. A DOUBLER WAS PLACED OVER THIS AREA. IT WAS APPROVED BY FAA/DER FORM 8110-3 AND DER DESIGNATION SO-867.

Part: FRAME — CRACKED (BS 1418)

MAINTENANCE FOUND A 1.0 CRACK AT FS 1418 AND A 1.25 CRACK AT STA 1418, L-2L AT THE TYPICAL LOCATIONS REFERENCE BY S/B 53-184, REV 1. THIS ER/A WAS REPAIR PER THIS S/B AND APPROVED BY FAA/DER FORM 8110-3, DER DESIGNATION NM-2145.

Part: SKIN — DENTED (BS 237)

THE FUSELAHE SKIN WAS FOUND TO HAVE A DENT AT FS 237 BETWEEN STR 18L AND 20L. THE DENT WAS CUT OUT WITH DIMENSIONS OF 9 FWD/AFT BY 12 UP/DOWN. THE DAMAGE WAS REPAIRED WITH A DOUBLER AND APPROVED BY FAA/DER FORM 8110-3, DER DESIGNATIOIN SO-889.

Part: SKIN — DENTED (BS 218)

THE FUSLAGE SKIN WAS FOUND TO HAVE A DENT AT FS 218 BETWEEN STR 18L AND 20L. THE DENT WAS CUT OUT WITH THE DIMENSIONS OF 2 FWD/AFT BY 2.75 UP/DOWN. A REPAIR DOUBLER WILL BE INSTALLED ON THIS LOCATION.

Part: WIRE — LOOSE (COCKPIT)

ON SHORT FINAL, LOUD POP WITH SPARK. SMALL AMOUNT OF SMOKE FROM UNDER CAPT GLARESHIELD UNDER THE NOSE LIGHT SWITCH. TIGHTENED GND WIRE ON PNL LIGHTS. CHECKED OPN OF ALL LIGHTS IN AND AROUND CAPT GLARESHIELD, ALL OK.

Part: COMPRESSOR — DAMAGED (NR 1 ENGINE)

LOUD BANG AND EPR DROP ON NR 1 ENGINE WHEN THROTTLES ADVANCED TOWARD TAKEOFF POWER OF 1.87 EPR. AIRSPEED +/- 20KEPR BETWEEN 1.5 AND 1.6 WHEN TAKEOFF ABORTED. NORMAL BRAKING AND EXIT FROM RUNWAY. ENGINE INGESTED FOD, ENGINE CHANGED.

Part: EEL LENSE COVER — MISSING (CABIN)

EMERGENCY LIGHT COVER MISSING, ROW 1, 12 AND 26. REPLACED LENS COVERS.

Part: COWL — DENTED (ENGINE)

DURING INITIAL INSPECTION, A DENT WAS FOUND AT THE 9 O/C POSITION ON THE L/E LIP SKIN. THIS DENT WAS REPAIRED PER SRM 54-04A.