N910DE

Part: SKIN — CORRODED (SERVICE PANEL) · airframe 66,570 hrs · 52,073 cycles

CORROSION FOUND JUST AFT OF LAV SVC PANEL. CORROSION ALSO NOTED FURTHER AFT AT PRESSURE DOME AREA. SKIN IS BULGED AND SEPARATED AT SEAM. AREA MARKED. BLENDED CORROSION NEAR AFT LAV SVC PNL. FOUND TO BE WITHIN LIMITS PER MD88 SRM 53-04-1. RESTORED FINISH. CORROSION AT P-DOME REPAIRED PER ERA 584197-14 REV ORG SECT I TEMPORARY REPAIR. REPETITIVE INSPECTIONS AND PERMANENT REPAIR TRACKED ON LOG 1421319. REPAIR STEPS DOCUMENTED ON PRI 584197-14 REV 1 WHICH MATCHES ERA 584197-14 REV ORG.RII COMPLIED WITH.

Part: INLET — CONTAMINATED (APU) · airframe 65,568 hrs · 51,134 cycles

WHILE BOARDING FLIGHT LEADER AND CAPT SMELLED BURNING OIL ORDER IN COCKPIT AND FWD CABIN FOUND OIL AROUND APU NON REM DOORS. T/S PER NO GO ODI FOUND APU INLET CONTAMINATED PERFORMED DUCT BURN OUT PER WORK CARD 7100-2619 LEACK CHECK LEFT AND RIGHT PACK NO LEAKS NOTED NO ODER OR FUMES AT THIS TIME. (LP9890222)

Part: DOOR FRAME — CRACKED (RT MLG DOOR) · airframe 65,434 hrs · 51,002 cycles

R/H FWD MAIN LANDING GEAR WHEEL FRAME IS CRACKED. ACCOMPLISHED SEC I TIME LIMITED REPAIR PER ER/A 578803-14 REV ORIGINAL. ASSOCIATED ER/A 14-578803. REPLACED R/H MLG FWD DOOR JAMB PER RI SEC II REF BOEING DWG #5930584. LANDING GEAR DOOR OPS CHECK GOOD REF MD88 AMM 32-10-01-501. (LP #5921822)

Part: LIGHT — DAMAGED (CABIN) · airframe 65,225 hrs · 50,826 cycles

EMERGENCY LIGHT ASSY DAMAGED AT 32D. REPLACED LIGHT ASSY AT 32D OPS NL REF AMM 33-52. (LP5800382)

Part: CONNECTOR — DAMAGED (CABIN) · airframe 64,889 hrs · 50,554 cycles

SEAT 13DE AND 21DE EMERGENCY PATH LIGHTS INOP. REPAIRED CONNECTORS, REF SWPM 20-90. NOW CHECKS GOOD. (LP5845377)

Part: DOOR FRAME — CORRODED (BS 399-415) · corrosion level 2 · airframe 64,583 hrs · 50,303 cycles

AWR. CORROSION ON LWR DOOR JAMB BTW STA 399 TO 415 AT FWD CARGO COMPARTMENT. REPAIR ON LWR DOOR JAMB BTW STA 399 TO 415 AT FWD CARGO COMPARTMENT WAS PERMORMED PER DC9MD80 SRM 53-05 FIG. 44A, ETI-88-19-006 REV. 1 AND ERA 575056-14 REV. ORIG. (LP0927609)

Part: SPACER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,581 hrs · 50,302 cycles

AWR. INITIAL INSPECTION. CORROSION ON SPACER IN LWR BEAM PREVIOUS REPAIR AT AFT CARGO DOOR CUT OUT LWR AREA. CORROSION LEVEL 2. SPACER ON BEAM PREVIOUS REPAIR AT AFT CARGO DOOR WAS REPLACED PER SRM 53-05 FIG 123. (LP0922716)

Part: COOLING FAN — ODOR (COCKPIT) · airframe 64,500 hrs · 50,238 cycles

BURNING SMELL WHEN INSTR COOLING FAN RUNNING PULL C/B ODOR GOES AWAY. C/W NO GO ODI PREV 2172 PER AMDS W/C 2120-2367. VERIFIED INST COOLING FAN IS BAD CAUSING THE NOISE AND BURNING SMELL IN COCKPIT. APU INLET IS CLEAN. REMOVED AND REPLACED INST COOLING FAN REF AMM 21-50. OPS CKS GOOD. NO MORE NOISE OR BURNING SMELL. (LP5335382)

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,518 hrs · 49,394 cycles

EMERGENCY LIGHTS DOOR 2 LEFT INOP. REMOVED AND REPLACED TWO EMERGENCY 'D' CELL BATTERIES FOR THE OVER EMERGENCY LIGHTS AT DOOR 2L. OPERATIONAL CHECK GOOD IAW AMM 33-50. P/N AD4002P.

Part: ACTUATOR — FAILED (RT NLG DOOR) · airframe 62,786 hrs · 48,803 cycles

DURING CLIMB OUT, A NOISE AND VIBRATION FROM NOSE GEAR AREA INCREASED WITH AIRSPEED. RETURNED TO DEPARTURE. RIGHT NOSE GEAR DOOR FOUND OPEN. REPLACED RIGHT DOOR MECHANICAL ACTUATOR IAW AMM. NOSE GEAR SWING CHECK PERFORMED.

Part: WIRE — SHORTED (ACARS) · airframe 62,625 hrs · 48,678 cycles

ACARS PRINTER WIRE BUNDLE SHORTING ON AIRCRAFT STRUCTURE. PULLED & COLLARED ACARS PRINTER C/B F18. REMOVED ACARS PRINTER. FOUND 4 WIRES SHORTING TO GROUND. REPAIRED WIRING PER SOPW AND WDM 23-24-01 SH 1 PG 2. REROUTED WIRE BUNDLE TO MAKE CANNON PLUG ACCESSIBLE TO PRINTER. REPLACED ACARS PRINTER - OPS CHECKS AND TESTS GOOD.

Part: CABLE — FRAYED (TAILCONE) · airframe 60,464 hrs · 46,960 cycles

DURING TAILCONE INSPECTION FOUND CABLE FRAYED. R & R TAILCONE CABLE IAW AMM 53-53-0.

Part: SHAFT — WORN (L1 DOOR) · airframe 59,781 hrs · 46,425 cycles

WEAR ON L1 MECHANISM DOOR SHAFT ASSY P/N4915850-1. REPLACED SHAFT ASSY PER MD 88 AMM 26-62-00-201 , 52-11-01-201 (LP# 2828265)

Part: LONGERON — CRACKED (BS 1431) · airframe 59,781 hrs · 46,425 cycles

AFT ACCESORIES COMPARTMENT CRACK LONGERON 12R, BS 1431 BULKHEAD. REPAIRED IAW ETI-88-16-462 REV. 1 AND ER/A 552834-14.

Part: HOUSING — WORN (CARGO DOOR) · airframe 59,781 hrs · 46,425 cycles

WEAR ON AFT CARGO DOOR HANDLE HOUSING. HOUSING WAS REMPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: PAN — CRACKED (CARGO DOOR) · airframe 59,781 hrs · 46,425 cycles

CRACKED PAN BELOW STOP FITTING NR 2 ON FWD CARGO DOOR FWD EDGE. REPAIRED IAW ETI-88-16-480 REV. 2 AND ER/A 552866-14.

Part: DOOR FRAME — CRACKED (RT MLG DOOR) · airframe 59,781 hrs · 46,425 cycles

CRACKED FWD DOOR JAMB CHANNEL BS 937 AND RBL 5. RH MLG JAMB CHANNEL WAS REPAIRED IAW ERA 552882-14.

Part: DOUBLER — CORRODED (SERVICE PANEL) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON AFT LAVATORY SERVICE PANEL INNER DOUBLER. THE DOUBLER WAS REPLACED IAW ER/A 552849-14 REV: ORIGINAL.

Part: PAN — CRACKED (SERVICE DOOR) · airframe 59,781 hrs · 46,425 cycles

CRACK ON INNER PAN FWD LOWER CORNER AT FWD SERVICE DOOR. INNER PAN FWD LOWER CORNER AT FWD SERVICE DOOR WAS REPAIRED IAW ETI 88-16-483 REV.3 AND ER/A 552873-14 REV. ORIGINAL.

Part: PAN — CRACKED (CARGO DOOR) · airframe 59,781 hrs · 46,425 cycles

CRACKED PAN BELOW STOP FITTING NR 2 ON FWD CARGO COMPARTMENT DOOR FWD EDGE. CRACKED PAN WAS REPAIRED IAW ER/A 552873-14 REV: ORIGINAL, MESSAGE 16-0778-08B AND ETI-88-16-483 REV: NR 3.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 59,781 hrs · 46,425 cycles

CRACKED CHANNEL ON CABIN FLOOR PANEL 769G. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-05 PAR. 145 FIG.

Part: FRAME — CRACKED (BS 1485) · airframe 59,781 hrs · 46,425 cycles

AFT ACCESORIES COMPARTMENT, CRACK ON FRAME BS 1485 BETWEEN LONGERONS 15 - 16L. THE FRAME WAS REPAIRED IAW ER/A 552836-14 REV. ORIGINAL. MESSAGE 16-0739-04B AND ETI -88-16-464 REV .ORIGINAL.

Part: FORMER — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,425 cycles

FUSELAGE, CRACKED FORMER STA Y=907 AND X=-60 AT RT FILLET PANEL. FORMER WAS REPAIRED PER SRM 53-01 FIG 2.

Part: HINGE — DAMAGED (FUSELAGE) · airframe 59,781 hrs · 46,425 cycles

ELONGATED HOLES ON HINGES AT AFT UPPER INBOARD SIDE OF THE FUSELAGE DOOR CARGO JAM. HINGES AT AFT UPPER INBOARD SIDE OF THE FUSELAGE DOOR CARGO JAMB WERE REPLACED PER SRM 51-30-5 AND DWG 9957945 REV J.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,425 cycles

AFT ACCESSORIES COMPARTMENT: CRACK ON FRAME STA Y=1485 CANT LONG 7R TO 9R. AREA WAS REPAIRED PER SRM 53-03 FIG. 49 AND SRM 51-30-2, 51-30-5 AND 51-30-1.

Part: HINGE — DAMAGED (CARGO DOOR) · airframe 59,781 hrs · 46,425 cycles

C2 CARGO DOOR, ELONGATED HOLES ON CARGO DOOR HINGES C2. HOLES WERE REWORKED PER ERA 497387-14MA REV B AND DOORS HINGES WAS REMOVED /INSTALLED PER AMM 52-31-02-201.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON TWO HOLES ON LWR ACCESS CUTOUT ADJACENT TO STRINGER 12 AT XRS=210 AT LT WING. LWR ACCESS CUT OUT WAS REPAIRED PER ER/A 552851-14AD REV ORIGINAL AND ETI 88-16-474 REV 1 REPAIR, APPROVAL IS LIMITED TO 67,000 TOTAL CYCLES ONLY.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 59,781 hrs · 46,425 cycles

CRACKED CABIN FLOOR PANEL NR: 389A, 693A, 617G, 1079E, 256E AND 389G. FLOOR PANELS 256E, 389G AND 1079E WERE REPAIRED PER SRM 53-05 PAR 145 FIG 131C. FLOOR PANEL 617G WAS REPAIRED PER SRM 53-01 FIG 4. FLOOR PANEL 693A WAS REPLACED PER SRM 51-10-4. FLOOR PANEL 389A WAS REPLACED WITH NRC 01049.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,425 cycles

CRACK ON GENERATION FLOOR PANEL NR: 541F, 927E, 1079A, 389A, 769A AND 256A. FLOOR PANELS 541F, 927E AND 256A WERE REPAIRED PER SRM 53-05 PAR 145 FIG 131B AND 131C. FLOOR PANEL 769A WAS REPAIRED PER SRM 53-01 FIG 4. FLOOR PANEL 1079A WAS REPAIRED PER SRM 51-20-0. FLOOR PANEL 389A WAS REPLACED PER SRM 51-10-4.

Part: CARGO TRACK — CORRODED (BS 1007-1322) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

AFT CARGO BAY HAS CORROSION ON THE RT CARGO TRACK BETWEEN BS 1007 - 1155, AND BS 1212 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1 AND DWG 5936660 REV. BZ.

Part: SKIN — PUNCTURED (CARGO DOOR) · airframe 59,781 hrs · 46,425 cycles

PUNCTURE ON FWD CARGO COMPARTMENT DOOR INNER SKIN. FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER. ERA 094625-14.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,425 cycles

AFT ACCESSORIES COMPARTMENT: CRACK ON INTERCOSTAL BTW STA Y=1485 CANT TO Y=1497 CANT BTW LONG PROJECTION 18L TO 22L. INTERCOSTAL WAS REPLACED PER DWG 9917701 REV AND SRM 51-30-2 AND 51-30-5.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

AFT ACCESSORY COMPARTMENT: CORROSION ON BULKHEAD, INTERCOSTALS, RT/LT CAP AND RT/LT BEAM AT AFT STAIRWAY WALKING BRIDGE. DUE EXCESSIVE CORROSION BULKHEAD NR 2 WAS REPLACED PER SRM 51-30-2.

Part: SUPPORT — CORRODED (BS 1117-1155) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

AFT CARGO COMPARTMENT: CORROSION ON ZEE SUPPORT ABOVE RT CARGO TRACK BETWEEN BS 1117 TO 1155. THE SUPPORT WAS REPLACED IAW SRM 51-30-1 , 51-30-5 AND DWG 5936660 REV:BZ.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON SECONDARY ACCESS PANEL 1410C. THE ACCESS PANELS WAS REPLACED IAW 51-10-3.

Part: FRAME — CRACKED (BS 1510) · airframe 59,781 hrs · 46,425 cycles

AFT ACCESORIES COMPARTMENT HAD A CRACK ON FRAME BS 1510. THE FRAME WAS REPLACED IAW SRM 51-30-02.

Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON FLOOR PANEL. REPAIRED IAW ER/A 504469-14MA.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON FUEL ACCESS PANEL 1333C . INSTALLED A NEW ACCESS PANEL IAW AMM 28-00-00.

Part: DOOR — CRACKED (RT WING) · airframe 59,781 hrs · 46,425 cycles

RT WING HAS A CRACKED INBD FLIGHT SPOILER BUTTE DOOR XRS 184. REPAIR THE DOOR IAW SRM 51-70-4 FIG.1 (SHEET 1).

Part: FINGER DOUBLER — CORRODED (BS 1193-1309) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON THE FINGER DOUBLER BETWEEN BS 1193 - 1309, LONGERONS 25 - 26L. FINGER DOUBLER WAS REPLACED IAW SRM 53-34-0 FIG, 3 AND 51-10-1 FIG 36.

Part: SKIN — BULGED (RT WING TE FLAP) · airframe 59,781 hrs · 46,425 cycles

PROTUBERANCE ON LOWER SKIN OF RT WING OUTBD FLAP OUTBD GUIDE VANE AT XV2=321. REPAIRED IAW SRM 57-03 D PAR. 11 (LP#2808044)

Part: SPLICE — CRACKED (BS 988) · airframe 59,781 hrs · 46,425 cycles

CRACKED SPLICE BS 988 AND LBL 7. REPAIRED IAW ER/A 413026-14MA.

Part: DOUBLER — CORRODED (BS 340-427) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

FWD CARGO BAY HAS CORROSION ON A PREVIOUS REPAIR DOUBLER AT LOWER DOOR FRAME PAN BS 370 TO 427. THE REPAIR DOUBLERS WAS REPLACED IAW ER/A 526949-14 REV.ORIG. AND ER/A 383732-14 REV.ORIG.

Part: FRAME — CRACKED (BS 1431) · airframe 59,781 hrs · 46,425 cycles

AFT ACCESORIES BAY HAS A CRACK ON THE FRAME LOWER CAP BS 1431 LONGERONS 11 & 12R. THE FRAME WAS REPAIRED IAW ER/A 552832-14 REV. ORIGINAL AND ETI-88-16-460 REV. 2.

Part: CARGO TRACK — CORRODED (BS 1007-1322) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

AFT CARGO BAY HAS CORROSION ON THE LT CARGO TRACK BS 1007 - 1322. REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: FRAME — CORRODED (BS 1393) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

AFT ACCESORIES COMPARTMENT, CORROSION ON FRAME BS 1393 LBL 3 TO LBL 10, BETWEEN LONGERONS 25 - 28L. AREA WAS REPAIRED IAW SRM 51-70-5 FIG 1.

Part: SKIN — NOT REPORTED (LT WING) · airframe 59,781 hrs · 46,425 cycles

DURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND (SEVEN DIFFERENT FASTENERS OF PSE) ON LOWER SKIN REAR SPAR BTW XRS=163 TO 168 AT LT WING. ATTENDED WITH ER/A NR 552817-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,425 cycles

AFT ACCESSORIES COMPARTMENT, CRACK ON WEB OF FRAME STA Y= 1380 LONG 21 LT. WEB OF FRAME STA Y= 1380 LONG 21 WAS REPAIRED PER SRM 51-70-4 FIG 2 (SHEET 2).

Part: SKIN — NOT REPORTED (RT WING) · airframe 59,781 hrs · 46,425 cycles

DURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND (SEVEN DIFFERENT FASTENERS OF PSE) ON LOWER SKIN REAR SPAR BTW XRS=163 TO 168 AT RT WING. ATTENDED WITH ER/A NR 552817-14AD REV ORIGINAL.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 59,781 hrs · 46,425 cycles

DOORS, CRACK ON ANGLES AT STA Y=389 AND BEAM 1, 2 AND 5 FWD CARGO COMPARTMENT INNER STRUCTURE. NO CRACKS WERE FOUND ON ANGLES STA Y=389 BEAM 1 AND 2. CRACK ANGLE ON STA 389 BEAM 5 WAS REPLACED PER DWG 9957664 REV N AND SRM 51-30-5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON FLOOR SUPPORT OF STA Y 427 BTW LONG 28L TO 28R. FLOOR SUPPORT OF STA Y 427 BTW LONG 28L TO 28R WAS REPLACED PER SRM 51-10-4 AND 51-10-1 FIG 33 (SHEET 9).

Part: ACCESS DOOR — CORRODED (WING) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON COUNTERSINKS AND SETTLING SURFACE OF FUEL ACCESS PLATES 1335C AND 1311C. FUEL ACCESS DOORS WAS REPLACED PER SRM 51-22-2A PAR 6.

Part: INTERCOSTAL — CORRODED (BS 1309-1322) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON INTERCOSTAL BS 1309 - 1322 AND LONGERONS 27 - 28R. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 9936718 REV. N.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 59,781 hrs · 46,425 cycles

VERTICAL STABILIZER LEADING EDGE HAD LOOSE FASTENERS ABOVE THE SPLICE. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 55-03 PAR 27 FIG 29 (SHEET 1 AND 2).

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 59,781 hrs · 46,425 cycles

LEFT WING HAD SEVERAL NICKS AND DENTS ON THE INBD FLAP INBD GUIDE VANE PREVIOUS REPAIR DOUBLER. REPAIRED IAW SRM 57-03 D PAR.11.

Part: FRAME — CRACKED (BS 1346) · airframe 59,781 hrs · 46,425 cycles

WEAR AND A CRACK ON TITANIUM FRAME BS 1346, LONGERONS 28L TO 28R. REPAIRED IAW ER/A 094719-14MA REV. A.

Part: CUSP WEB — CRACKED (BS 1294) · airframe 59,781 hrs · 46,425 cycles

CRACKED RT CUSP WEB BS 1294, RBL 54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131.

Part: FRAME — CRACKED (BS 1322) · airframe 59,781 hrs · 46,425 cycles

CRACKED FRAME BS 1322 LONGERON 17R. THE FRAME WAS REPAIRED IAW ER/A 493697-14MA REV. B.

Part: FLOOR SUPPORT — CRACKED (BS 1271-1287) · airframe 59,781 hrs · 46,425 cycles

CRACK ON THE FLOOR SUPPORT BETWEEN BS 1271 - 1287 RBL 3. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 53-01 FIG2.

Part: FRAME — CRACKED (BS 1322) · airframe 59,781 hrs · 46,425 cycles

CRACKED FRAME ON BS 1322 LONGERON 17L. THE FRAME WAS REPAIRED IAW ER/A 493697-14MA REV. B.

Part: VANE — WORN (RT WING TE FLAP) · airframe 59,781 hrs · 46,425 cycles

WEAR ON LEADING EDGE OF RT WING OUTBD FLAP INBD GUIDE VANE. THE VANE WAS REPAIRED IAW SRM 57-03D PAR.11.

Part: FLOOR SUPPORT — CORRODED (BS 1309-1350) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

FLOOR SUPPORT CORRODED AND RBL 20 BS 1309 - 1350. REPLACED THE FLOOR SUPPORT IAW SRM 51-30-1.

Part: DOUBLER — DAMAGED (AFT CARGO BAY) · airframe 59,781 hrs · 46,425 cycles

AFT CARGO BAY HAS WEAR ON FWD AND AFT LWR CORNERS OF PRODUCTION DOUBLERS. THE DOUBLERS WERE REPLACED IAW SRM 51-30-2.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 59,781 hrs · 46,425 cycles

CRACKED CHANNEL AND SPACER ON THE FLOOR PANEL 826D. THE CHANNEL AND SPACER WERE REPLACED IAW DWG 9936639 REV. P.

Part: CUSP WEB — CRACKED (BS 806) · airframe 59,781 hrs · 46,425 cycles

FOUND A CRACK ON THE RT CUSP WEB BS 806, LBL 45. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-20.

Part: CUSP WEB — CORRODED (BS 1174-1193) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON THE LT CUSP WEB REPAIR, BS 1174 - 1193. THE CUSP WEB REPAIR WAS REPLACED IAW SRM 53-05 FIG 131A-6.

Part: CUSP WEB — CRACKED (BS 809-810) · airframe 59,781 hrs · 46,425 cycles

A CRACK WAS FOUND ON THE LT CUSP WEB BS 809 - 810, LBL 60 - 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-05. FIG. 131A-1.

Part: CUSP WEB — CORRODED (BS 1067-1076) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION FOUND ON THE RT CUSP WEB BS 1067 - 1076. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131-A.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON FLOORBEAM BS 200 BETWEEN RBL 7 TO 44. THE FLOORBEAM WAS REPLACED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-4, SRM 51-10-3 PAR 14 & 21 AND DWG S2929169 REV. B.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 59,781 hrs · 46,425 cycles

DELAMINATED FLOOR PANELS NR 250D, 256C, 256D, 389B, 313C, 465C, 693C, 826D, 886C, 1079D AND 1250C. DAMAGE INSERT WERE REPLACED ON FLOOR PANEL NRS: 250D, 256C, 256D, 389B, 313C, 465C, 693C, PER AMM53-20-01-201. AND FLOOR PANELS NR: 826D,886C,1079D, AND 1250C WERW FABRICATED PER AMM 53-20-01-201.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,425 cycles

CRACK ON RT CUSP WEB STA Y=809, X=54 TO 60. CRACKS ON CUSP WEB WAS ATTENDED PER SRM 53-05 FIG 131A-4.

Part: DOUBLER — WORN (FUSELAGE) · airframe 59,781 hrs · 46,425 cycles

HIDDEN DAMAGE, WORN INTERNAL PRODUCTION TITANIUM DOUBLER ON STA Y=1307 BTW LONGERONS 28L-22L. INTERNAL PRODUCTION TITANIUM DOUBLER WAS REPLACED PER DWG 5911423 REV CD AND SRM 51-10-4 AND 51-10-3 PAR 14.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON FLOOR SUPPORT OF STA Y= 195 BTW STA X=16 TO X=42. FLOOR SUPPORT STA Y= 195 BTW STA X=16 TO X=42 WAS REPLACE PER SRM 51-10-4,51-30-2,51-30-5 AND 51-10-3 PAR 14 AND 21.

Part: BEAM — CRACKED (L1 DOOR) · airframe 59,781 hrs · 46,425 cycles

CRACKED L1 DOOR BEAM AFT REPAIR DOUBLER BEAM 1. BEAM NR 1 AFT SIDE WAS REPAIRED PER SRM 52-05 PAR 76 FIG 97.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON FLOOR SUPPORT FROM STA Y=160-200 AND STA X=-44. FLOOR SUPPORT STA Y=160-200 AND STA X=-44 WAS REPLACED PER SRM 51-10-4,51-30-2,51-30-5 AND 51-10-3 PAR 14 AND 21.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON LT CUSP WEB BTW STA Y=543 TO Y=548 AND Y=582 TO Y=594, X=54-60. CUSP WEB ON STA Y=543 TO Y=548 AND Y=582 TO Y=594 WERE REPAIRED PER SRM 53-05 FIG 131 A- 14.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,425 cycles

CRACKED INTERCOSTAL ON LOWER SIX PULLEY BRACKET. INTERCOSTAL ON LOWER SIX PULLEY BRACKET WAS REPAIRED PER SRM 53-01 FIG 2, SRM 51-30-2 AND 51-30-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON PREVIOUS REPAIR PLUG AT Y=1000 X=-54. PREVIOUS REPAIR PLUG WAS REPLACED PER SRM 53-05 FIG 4A (SHEET 1) AND SRM 51-30-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON FLOOR SUPPORT FROM STA Y=160 TO Y=200 AND X 7. SUPPORT WAS REPLACED PER SRM 51-10-4 AND DWG 9936534 REV ORG.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,425 cycles

CRACK ON GENERATION FLOOR PANEL NBR 541A. GENERATION FLOOR PANEL NBR 541A WAS REPAIR THE CRACK PER SRM 53-05 PAR 145 FIG 131B.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,781 hrs · 46,425 cycles

CABIN FLOOR STRUCTURE, CRACK ON INTERCOSTAL BTW STA Y=769 TO Y= 788 X= 0. INTERCOSTAL STA Y=769 TO Y=788 WAS REPLACE PER SRM 51-30-5, 51-30-2 AND DWG 9936580 REV BW.

Part: SKIN — WORN (TE FLAP VANE) · airframe 64,581 hrs · 50,302 cycles

INITIAL: WEAR ON TRAILING EDGE LOWER SKIN (OUTBD AFT CORNER) OF RT WING OUTBD FLAP ONBD GUIDE VANE. PERMANENT REPAIR WAS ACCOMPLISHED PREVIOUSLY, NO FURTHER ACTION IS REQUIRED, PLEASE CLOSE THIS LOG. (LP2788780)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON LT CUSP WEB BTW STA Y=712 TO 719 BTW X=54 TO 60 AT PAX CABIN. CUSP WEB BTW STA Y=712 TO Y=719 AND BTW X=54 TO X=60 WAS REPAIRED PER SRM 53-05 FIG.131A-10.

Part: CUSP WEB — CORRODED (BS 522-590) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON CUSP WEB BS 522-530, BS 554-560 AND BS 581-590. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-14.

Part: CUSP WEB — CORRODED (BS 598-712) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON LT CUSP WEB, LWR AND UPPER SURFACE BETWEEN LBL 60 - 44 AND BS 598 - 712. THE WEB WAS REPLACED IAW DWG 9930538 REV BF, SRM 51-30-2,51-30-1 AND 51-30-5.

Part: SPACER — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

AFT CARGO BAY, CORROSION ON PREVIOUS REPAIR SPACER AT DOOR JAMB BEAM. PREVIOUS REPAIR SPACER AT DOOR JAMB BEAM WAS REPLACED PER DC-9/MD-80 SRM 51-30-5 AND SRM 53-05 FIG. 123.

Part: DOUBLER — CRACKED (L1 DOOR) · airframe 59,781 hrs · 46,425 cycles

CRACKED L1 DOOR EXTERNAL DOUBLER AFT LOWER SECTION. EXTERNAL SKIN WAS REPAIRED IAW SRM 52-05 PARAGRAP 39 FIGURE 37.

Part: LONGERON — CRACKED (BS 522) · airframe 59,781 hrs · 46,425 cycles

CRACKED LONGERON 4R AT CROWN BS 522. THE LONGERON WAS REPAIRED IAW SRM 53-02 PAR.12 FIG.18.

Part: DIAPHRAGM — CORRODED (BS 185-200) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

DIAPHRAGM CORROSION BS 185 TO 200 AND RBL 50 TO 54. REPAIRED IAW SRM 51-70-4.

Part: CUSP WEB — CORRODED (BS 668-703) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CUSP WEB CORROSION ON BS 668 - 670, BS 678 - 681 AND BS 700 - 703. CUSP WEB REPAIRED IAW SRM 53-05 FIG. 131-A.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 59,781 hrs · 46,425 cycles

FWD RT EMERGENCY EXIT DOOR PAN CRACKED BETWEEN STOPS 4 AND 5. REPAIRED IAW SRM 52-05-FIG. 51

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 59,781 hrs · 46,425 cycles

CRACK ON INSIDE ANGLE AT STOP FITTING 2, THE PAN AT STOP 14 CRACKED. REPAIRED IAW SRM 52-05 FIG. 51.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON FLOOR SUPPORT BS 160 - 200 AND LBL 54. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-4.

Part: FLOORBEAM — CORRODED (BS 180) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION WAS FOUND ON THE FLOORBEAM BS 180 RBL 7 - 44. THE FLOORBEAM WAS REPLACED IAW SRM 51-10-4.

Part: VANE — DEBONDED (RT WING TE FLAP) · airframe 59,781 hrs · 46,425 cycles

DISBONBED PREVIOUS REPAIR DOUBLER ON LOWER SKIN AT STA XOVIF = 58 ON RT WING INBD FLAP OUTBD GUIDE VANE. FLAP OUTBD GUIDE VANE ARE OUT BOUNDS BY CORROSION IAW SRM 57-03D PAR.11 AND INBD FLAP OUTBD GUIDE VANE WAS REPLACED IAW AMM 27-51-03.

Part: CUSP WEB — CORRODED (BS 446-465) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON LT CUSP WEB PREVIOUS REPAIR, BS 446 - 465. THE REPAIR WAS REPLACED IAW SRM 53-05 FIGURE 131A-13 AND SRM 51-30-5.

Part: PAN — CRACKED (BS 807 & 1060) · airframe 59,781 hrs · 46,425 cycles

A CRACK ON RT FWD UPPER CORNER BS 807 AND RT FWD LOWER CORNER BS 1060 OF WINDOW RING PAN. REPAIRED IAW SRM 53-05 FIG. 122, ER/A 487747-14MA REV. A, AND ER/A 493648-14MA REV. A.

Part: SKIN — CRACKED (BS 807-828) · airframe 59,781 hrs · 46,425 cycles

CRACK ON LH FWD UPPER CORNER WINDOW RING PAN BTW BS 807 AND 828. REPAIRED IAW SRM 53-05 FIG. 122, ER/A 487747-14MA REV. A AND ER/A 493648-14MA REV. A.

Part: WEB — PUNCTURED (BS 203) · airframe 59,781 hrs · 46,425 cycles

A PUNCTURED WEB AT BS 203, LBL 22 AND 44. THE WEB WAS REPAIRED IAW SRM 53-01 FIG 4, AND 51-10-3 PAR 14, 21, 38.

Part: PAN — CRACKED (BS 1079) · airframe 59,781 hrs · 46,425 cycles

CRACK ON LH AFTER UPPER CORNER BS 1079 OF WINDOW RING PAN AT CABIN PASSENGER. REPAIRED IAW SRM 53-05 FIG. 122, ER/A 487747-14MA REV. A AND ER/A 493648-14MA REV. A.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON FUEL TANK ACCESS PANELS 1303C AND 1409C. THE ACCESS PANELS 1409C AND 1303C WERE REPLACED IAW SRM:51-22-2A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON W2 FLOORBEAMS Y=1322 AND Y=1338 BWT X=60 AND X=-60. FLOORBEAMS WERE REPAIRED PER SRM 53-05 FIG 20 AND 51-10-3 PAR 14, 21, 26.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

CORROSION ON FLOOR SUPPORT. REPLACED IAW SRM 51-10-4, SRM 51-10-3 PAR. 14 & 21 AND DWG 3936190 REV. ORIGINAL .

Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 59,781 hrs · 46,425 cycles

LT WING, CORROSION ON UPPER/LWR SURFACES OF LT OUTBD FLAP OUTBD GUIDE VANE AT TRAILING EDGE AREA UPPER SKIN: 48 INCH FROM INBD END TO 61INCHES, ALSO SMALL POINT OF CORROSION AROUND FASTENERS AT 71INCH FROM INBD END. LWR SKIN: 10 INCH FROM INBD END TO 17 INCH. REPLACED SO VANE BY SRM 57-03D PAR 11. LT OUTBD FLAP OUTBD GUIDE VANE WITH P/N 5910043-509 AND S/N AJ-2 WAS REPLACED.

Part: SIDEWALL PANEL — DAMAGED (AFT AIRSTAIR) · airframe 59,649 hrs · 46,333 cycles

AFT AIRSTAIR SIDE WALL PANEL ON CAPTAIN'S SIDE AT TOP IF STEPS NEAR EXIT DOOR BENT DOWN AND PREVENTING EGRESS. REPAIRED IAW ERA.

Part: ENGINE — MAKING METAL (NR 2) · airframe 59,532 hrs · 46,241 cycles

THE NUMBER 2 ENGINE SHUTDOWN AT FL340 AND THE FLIGHT WAS DIVERTED. MAINTENANCE FOUND METAL ON THE CHIP DETECTOR. THE NUMBER 2 ENGINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (LT MLG WW) · airframe 59,175 hrs · 45,949 cycles

FOUND LT FWD MLG WHEEL WELL FRAME CRACKED. REMOVED AND REPLACED THE FRAME IAW DRAWING 5930584.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 58,321 hrs · 45,290 cycles

AFT CARGO COMPARTMENT, FLOOR DAMAGED BETWEEN ST 1136-1155 FLOOR DAMAGE. R & R AFT CARGO FLOOR BETWEEN BS 1136-1155 IAW AMM 25-52.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 58,321 hrs · 45,290 cycles

FOUND AFT CARGO FLOOR DAMAGED BETWEEN BS 1250-1271. R & R AFT CARGO FLOOR BETWEEN BS 1250-1271 IAW AMM 25-52.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,197 hrs · 43,750 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE AFT OVERWIND EMERGENCY EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE OPS CHECK WAS GOOD.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 55,249 hrs · 43,120 cycles

RAMP REPORTED THE AFT CARGO FLOOR HAS METAL STICKING UP. REPAIRED THE FLOOR IAW SRM 53-05D.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,040 hrs · 42,992 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS ROWS 31-36CD WERE INOPERATIVE. MAINTENANCE REPLACED THE CHARGER FOR THE POWER SUPPLY BATTERIES AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: SUPPORT ANGLE — CRACKED (BS 178) · airframe 54,671 hrs · 42,733 cycles

CRACKED SUPPORT ANGLE AND PREVIOUS DOUBLER REPAIR ON STA 178, FIXED L/E, SM, CARD 5, ZONE 10. FASTENERS WERE REMOVED IAW SRM 51-30-5 AND 51-30-2, PREVIOUS REPAIR DOUBLER AND ANGLE WERE FABRICATED IAW ETI-88-14-240 AND DWG 9937517, REPAIR AND ANGLE WERE TREATED AND PAINTED IAW SRM 51-10-3 P14 AND 21, REPAIR DOUBLER AND ANGLE WERE INSTALLED IAW SRM 51-30-5 AND ETI-88-14-240.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 54,671 hrs · 42,733 cycles

CORROSION ON LWR AFT CARGO DOOR JAMB BETWEEN STA Y=1155-1212, C3, SM, MBR 53-019-02. FASTENERS, CORROSION, SEAL DEPRESSURE WERE REMOVED, REWORKED AREA WAS MEASURED, BEAM DOUBLER WAS REMOVED, NEW BEAM DOUBLER WAS FABRICATED, SPACER AND NUTS STRIP WERE FABRICATED REWORKED AREA AND REPAIR PARTS WERE TREATED/PAINTED, REPAIR PARTS AND SEAL DEPRESSURE WERE INSTALLED IAW SRM 51-10-3 PAR. 14, 21, 26, 38 53-05, FIG 123, ORIGINAL 0.280" REMAINING .213" IS OUT OF LIMITS AND BEAM WAS REPAIRED IAW SRM 53-05, FIG 123.

Part: CONTROL PANEL — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 54,671 hrs · 42,733 cycles

DURING CHECK, MAINTENANCE FOUND THE EXIT SIGNS ABOVE THE L2 SERVICE DOOR ARE DIM. REPLACED THE CONTROL PANEL AND THE OPS CHECK WAS GOOD.

Part: SHEAR TIE — CRACKED (BS 1380) · airframe 54,671 hrs · 42,733 cycles

CRACKED SHEAR TIE BETWEEN SKIN AND FRAME BS 1380 LONGERONS 13 - 14 R. REPAIRED IAW IAW SRM 51-30-2, SRM 53-14-4, FIG 1, SRM 51-10-3, PAR 14 - 21, AND INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: BEAM — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 54,671 hrs · 42,733 cycles

CORROSION FOUND ON LOWER DOOR JAMB BEAM DOUBLER REPAIR BETWEEN STA Y=636 TO Y=693 AT MID CARGO COMPARTMENT, MRB 53-018-02, SM, DOUBLER WAS REPLACED IAW SRM 53-05, FIG 123, SRM 51-30-5.

Part: CUSP WEB — CORRODED (BS 839-842) · corrosion level 2 · airframe 54,671 hrs · 42,733 cycles

CORROSION ON LT CUSP WEB X 55 TO X 60 BETWEEN BS 839-842. REPAIRED IAW SRM 53-05, FIG 131A-21, SRM 51-10-3 P 14 AND 21, SRM 51-30-2 AND 51-30-5, AND SRM 51-10-5, P 38.

Part: DOOR FRAME — DAMAGED · corrosion level 2 · airframe 54,671 hrs · 42,733 cycles

GENERAL SURFACE CORROSION ON REPAIR DOUBLER AT FWD LOWER CARGO DOOR JAMB BETWEEN BS 370-389, C1, MRB 53-017-02. PREVIOUS REPAIR WAS REPLACED IAW ER/A 383732-14, REV ORIGINAL.

Part: BEAM — CRACKED (BS 180) · airframe 54,671 hrs · 42,733 cycles

CRACKED BEAM N.6 AROUND HOLE FASTENER STA 180 APROX AT FWD ENTRANCE. CRACK ON BEAM N6 AREA DAMAGE WAS REMOVED DOUBLER AND FILLER WERE FABRICATES, WERE TREATED AND PAINTED AND WERE INSTALLED IAW ERA 413018-14MA AND SRM 51-30-5.

Part: BEAM — CRACKED (L1 DOOR) · airframe 54,671 hrs · 42,733 cycles

CRACKED BEAM NR 8 AFT SECTION AT FWD L1 DOOR. FASTENERS INNER SKIN AND EXTERNAL SKIN WERE REMOVED, CRACK WAS STOPPED, DOUBLER WAS FABRICATED, TREATED AND PAINTED AND DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-05-D, 51-10-3 AND 51-30-5.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 52,618 hrs · 41,309 cycles

DURING LINE CHECK, NOTED SEAT 25D EMERGENCY EXIT ROW LIGHT WAS INOPERATIVE. SECURED LOOSE CONNECTOR, OPS NORMAL.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,320 hrs · 41,114 cycles

DURING LINE CHECK, NOTED SEAT MOUNTED EMERGENCY LIGHTS AT THE FORWARD EMERGENCY EXIT ROW WERE INOPERATIVE. WIRE HARNESS REPLACED IAW AMM 33-52-01 AND OPS CHECKED NORMAL.

Part: ENGINE — SHUTDOWN (RIGHT) · airframe 51,563 hrs · 40,580 cycles

RETURNED TO DEPARTURE WITH TWO RT ENGINE SHUTDOWNS AFTER TAKEOFF. PILOT REPORT INDICATED RT ENGINE FAILURE AT 250 KTS AND 11,000 FT. ENGING EGT REACHED 800 DEG C AND THE RT FIRE T-HANDLE WAS PULLED AND THE BOTTLE DISCHARGED. THE ACFT LANDED SAFELY AND WITHOUT FURTHER INCIDENT. MT FOUND TURBINE DAMAGE AND METAL IN THE TAIL PIPE. THE RT ENGINE WAS REPLACED IAW WC 7200-2647, 7200-8284-RT AND 7100-4682-RT, THE FIRE BOTTLE WAS REPLACED ON LOG PAGE.

Part: FRAME — CRACKED (BS 1510) · airframe 50,852 hrs · 40,084 cycles

DURING SCHEDULED INSPECTION, THE BS 1510 FRAME WAS FOUND TO BE CRACKED AT THE 12 O`CLOCK POSITION FOR THE TAILCONE ALIGNMENT HOLE. REPAIRS WERE ACCOMPLISHED IAW ER/A 497316-14MA.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 50,852 hrs · 40,084 cycles

DURING SCHEDULED MX, THE TAILCONE RELEASE CAM ASSY WAS FOUND TO BE WORN AT THE UPPER LT POSITION AT STA 1510. THE UPPER LT TAILCONE RELEASE BASE WAS REPLACED IAW AMM 53-53-00 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: RELEASE MECH — WEAK (TAILCONE) · airframe 50,852 hrs · 40,084 cycles

DURING SCHEDULED MX, THE TAILCONE EXTERNAL RELEASE HANDLE SPRING CLIPS WERE FOUND TO BE WEAK. THE SPRING CLIPS WERE REPLACED IAW AMM 53-53 AND OPS CHECKED GOOD. THE REQUIRED INSPECTION WAS COMPLETED.

Part: SKIN — CRACKED (BS 1418 S2R) · airframe 50,852 hrs · 40,084 cycles

DURING SCHEDULED CHECK IN MSP, A CRACK IN THE FUSELAGE SKIN WAS FOUND AT STA 1418, NEAR S-2R. REPAIR WAS ACCOMPLISHED IAW ER/A 514037-14AD.

Part: CLAMP — DAMAGED (TAILCONE) · airframe 50,852 hrs · 40,084 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE SYS LOCKING CABLE CLAMP AND CONDUIT WAS OUT OF ALLOWABLE LIMITS. SOME CABLE BRACKETS WERE FOUND BROKEN AND REPLACED. ALSO, ALL OF THE TAILCONE RECEPTACLES IDENTIFIED AS WORN BEYOND LIMITS WERE REPLACED. THE CABLE WAS ADJUSTED BACK TO CORRECT CLEARANCE AND RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,462 hrs · 39,048 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND CEILING EMERGENCY LIGHT ROW 27 INOPERATIVE. REPLACED LAMP, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,462 hrs · 39,048 cycles

EMERGENCY CEILING LIGHT ROW 32R INOPERATIVE. REPLACED LAMP PER AMM. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,462 hrs · 39,048 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND FORWARD LEFT OVERWING EMERGENCY EXIT PATHWAY LIGHT HAS ONE BULB INOPERATIVE. REPLACED BULB, OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,462 hrs · 39,048 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND ROW 1 AND 2 LEFT EMERGENCY CEILING LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES PER AMM. OPERATION CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,462 hrs · 39,048 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND ROW 4 LEFT/RIGHT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERIES PER AMM. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

DURING SERVICE CHECK, MAINTENANCE FOUND FIRST CLASS EMERGENCY PATHWAY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER AMM. OPERATION CHECKS GOOD.

Part: ENGINE — FAILED (NR 2) · airframe 47,361 hrs · 37,637 cycles

AFTER TAKEOFF RIGHT ENGINE FAILED. FOLLOWED QRH PROCEDURE AND PULLED FIRE HANDLE. FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DAMAGE TO NOSE BULLET AND EXTENSIVE FAN DAMAGE. THE 8TH STAGE BLEED DUCT WAS ALSO DAMAGED. REPLACED RIGHT ENGINE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 47,281 hrs · 37,584 cycles

RIGHT FWD OVERWING EXIT OVERHEAD EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPS CHECK OK REF MD88 AMM 33-51.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 46,809 hrs · 37,251 cycles

DURING LINE CHECK, MAINTENANCE FOUND RIGHT AND LEFT FORWARD UPPER EMERGENCY EXIT SIGNS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER AND BATTERY. OPERATION CHECKS NORMAL.

Part: FLOORBEAM — CORRODED (BS 1322) · airframe 45,350 hrs · 36,259 cycles

DURING HMV, CORROSION WAS FOUND ON FLOORBEAM STA Y=1322, BTW X=-20 AND X=33 AT PAX CABIN. FLOORBEAM WAS REPAIRED IAW SRM 53-05, FIG 79A.

Part: CUSP WEB — CORRODED (PAX CABIN) · airframe 45,350 hrs · 36,259 cycles

DURING HMV, CORROSION WAS FOUND ON RT CUSP WEB X=-54 TO X=-60 UPPER/LOWER SIDE FROM STA Y=1231 TO 1238B AT PAX CABIN. CUSP WEB WAS REPLACED IAW DRD 53-20-02D.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 45,350 hrs · 36,259 cycles

DURING HMV CORROSION AND SCRATCHES WAS FOUND ON LT MLG SUPPORT FITTING BEARING BORE. LT MLG SUPPORT FITTING WAS REPAIRED IAW ER/A 487788-14AD, REV ORIG.

Part: DOOR FRAME — DAMAGED (CARGO BAY) · airframe 45,350 hrs · 36,259 cycles

DURING HMV ELONGATED SEAT SCREW HOLES WAS FOUND AT MID CARGO COMPARTMENT LWR DOOR JAMB BEAM Y=674 AND Y=655. DOOR JAMB BEAM WAS REPAIRED IAW SRM 53-05, PARA 140, FIG 123.

Part: SKIN — CORRODED (BS 1105-1107) · airframe 45,350 hrs · 36,259 cycles

DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN AT FUSELAGE FILLET FAIRING RUB STRIP SETTLEMENT AREA STA Y=1105 TO 1107, LONGERON 28 LT. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D, FIG 53.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 45,350 hrs · 36,259 cycles

DURING HMV, SCRATCHES AND CORROSION WAS FOUND ON RT MLG SUPPORT FITTING BEARING BORE. RT MLG SUPPORT FITTING WAS REPAIRED IAW EA 09-093855-03AD, REV B.

Part: CUSP WEB — CORRODED (PAX CABIN) · airframe 45,350 hrs · 36,259 cycles

DURING HMV, CORROSION WAS FOUND ON RT CUSP WEB X=-54, TOX=-60 AT UPPER SIDE STA Y=416, STA Y=428. CUSP WEB WAS REPLACED IAW DRD 53-20-02D.

Part: TAB — DAMAGED (ELEVATOR) · airframe 45,350 hrs · 36,259 cycles

DURING HMV, LIGHTNING STRIKE WAS FOUND ON LT ELEVATOR GEAR TAB T/E APROX STA XHS=140. GEAR TAB WAS REPAIRED IAW SRM 55-04, PARA 3A.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 45,350 hrs · 36,259 cycles

DURING HMV, CORROSION WAS FOUND ON LT MLG SUPPORT FITTING BUSHING BORE VERTICAL WALL. SUPPORT FITTING WAS REPAIRED IAW ER/A 487788-14AD, REV ORIG.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 45,350 hrs · 36,259 cycles

DURING HMV, CORROSION WAS FOUND ON LT HORIZ STABILIZER UPPER SKIN FWD PANEL BARREL NUT HOLE NR 1, STA XH=28. BARREL NUT HOLE WAS REPAIRED IAW ER/A 487784-14 REV ORIG.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 45,350 hrs · 36,259 cycles

DURING HMV, CORROSION WAS FOUND ON AFT PASSENGER ENTRANCE DOOR JAMB LWR SECTION X=17 TO X-=17. DOOR JAMB WAS REPAIRED IAW ER/A 487789-14, REV ORIG.

Part: CUSP WEB — CRACKED (PAX CABIN) · airframe 45,350 hrs · 36,259 cycles

DURING HMV, A CRACK WAS FOUND ON RT CUSP WEB STA Y=1170, BTW X=-54 AND X=-60 AT PAX CABIN FLOOR STRUCTURE. CUSP WEB WAS REPLACED IAW DRD 53-20-02D.

Part: FITTING — CORRODED (RT MLG) · airframe 45,350 hrs · 36,259 cycles

DURING HMV CORROSION WAS FOUND ON RT MLG SUPPORT FITTING BUSHING BORE. RT MLG SUPPORT FITTING WAS REPAIRED IAW EA 09-093855-03AD, REV B.

Part: TAB — DENTED (RT ELEVATOR) · airframe 45,350 hrs · 36,259 cycles

DURING HMV, DENTS WERE FOUND ON RT ELEVATOR CONTROL TAB UPPER SKIN, APROX STA XHS=66 TO 86. CONTROL TAB WAS REPAIRED IAW SRM 55-04, PARA 3A.

Part: FITTING — CORRODED (LT MLG) · airframe 45,350 hrs · 36,259 cycles

DURING HMV, CORROSION WAS FOUND ON LT MLG SUPPORT FITTING BUSHING BORE. LT MLG SUPPORT FITTING BUSHING BORE WAS REPAIRED IAW ER/A 487788-14AD, REV ORIG.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 45,350 hrs · 36,259 cycles

DURING HMV, CORROSION WAS FOUND ON RT HORIZ STABILIZER UPPER SKIN FWD PANEL BARREL NUT HOLE, NR 1, STA XH=28. BARREL NUT HOLE WAS REPAIRED IAW ER/A 487784-14 REV ORIG.

Part: SKIN — DAMAGED (BS 1060-1250) · airframe 45,350 hrs · 36,259 cycles

LIGHTNING STRIKE ON LT WINDOW BELT LOWER AFT/FWD CORNERS BTW STA 1060 AND 1079,1079 AND 1098,1231 AND 1250 FS. LIGHTNING STRIKES WERE BLEND IAW SRM 53-05, FIG 111. EDDY CURRENT INSP ACCOMPLISHED, NO CRACKS FOUND. AREAS TREATED IAW SRM 51-10-3 AND ERA 486640-14 REV, ORIG STA Y 1060-1079,1079-1098 AND ERA 488777-14 REV ORIG ON STA 1231-1250.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 43,183 hrs · 34,806 cycles

FOUND ON CHECK - EMERGENCY TRACK LIGHT OUT AT 28CD. FND BROKEN WIRE AT SEAT CONNECTOR OTBD SIDE OF SEAT ASSY. NO PARTS AVAIL TO CORRECT. FWD TO MCO AND PLAC IAW MEL33-00-24 ONLY ONE LIGHT INOP AT THIS SEAT LOCATION.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 43,174 hrs · 34,802 cycles

FOUND ON CHECK EMER LIGHT OUT AT 34CD. FND WIRE BROKEN AT SEAT TRACK CONNECTOR. REPLACED CONNECTOR AND PINS. OPS CK OK.

Part: SKIN — GOUGED (FS 206) · airframe 39,838 hrs · 32,243 cycles

FUSELAGE SKIN GOUGED NEAR FS 206 AND L-6L. DAMAGE CUT OUT AND REPAIR DOUBLER INSTALLED PER ERA 470387-14 AND SRM 53-04 FIG 12B.

Part: SKIN — DENTED (FS 1322-1388) · airframe 39,838 hrs · 32,243 cycles

SKIN DENTS AT FS 1322-1388, L-24L-26L DUE TO GROUND DAMAGE. DAMAGE WAS CUTOUT AND REPAIR DOUBLERS WERE INSTALLED.

Part: HYDRAULIC LINE — LEAKING (FS 750) · airframe 36,870 hrs · 28,650 cycles

NOSE WHEEL STEERING LINE LEAKING AT LEFT LONGERON 20 AT FS 750. NO EXTERNAL DAMAGE TO LINE. REMOVED BAG BIN WALL ON LEFT SIDE OF BIN 4.225052. REPAIRED L WITH RING LOC REPAIR. PRESSURIZED LINE, NO LEAKS NOTED. REINSTALLED BAG BIN WALL.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 36,796 hrs · 28,552 cycles

AT TOP OF DESCENT RT ENGINE REMAINED AT FULL THROTTLE POS HAD NO CONTROL WITH THROTTLES. SHUT DOWN RIGHT ENGINE AND LANDED. FLT DATA RECORDER REMOVED AND BOROSCOPE PERFORMED. NO PROBLEMS FOUND ON BOROSCOPE BUT FDR SHOWS EGT, ENG SPEEDSAND TEMPS ALL OUT OF LIMITS REQUIRING NR 2 ENGINE CHANGE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 34,947 hrs · 26,549 cycles

ON TAKEOFF ROLL, NR 2 ENGINE WOULD NOT ACCELERATE ABOVE IDLE POWER ABORTED TAKEOFF BELOW 80 KTS. OPENED NR 2 ENG COWL TO INSP FUEL CONTROL LINKAGE, NO OBVIOUS DAMAGE. INSP ALL HARD LINES TO FCU FOR SECURITY - NTF. CHECKED MOISTURE TRAP, TRAP DRY. FOUND BELLOWS UNDER SERVICED. SUPP SAME PER M/M. RAN ENG FOUND PT PWR OUT OF ADJUSTMENT. C/W PFHB TESTS 9077 TEST C, D, AND P, ALL CHECKS GOOD. A/C OK FOR SERVICE.

Part: SKIN — GOUGED (FUSELAGE) · airframe 33,219 hrs · 25,319 cycles

FUSELAGE SKIN GOUGED ADJACENT TO A PREVIOUS REPAIR AT STATION 617 AND LONGERON 29L. REPAIRED IAW ERA 095589-14.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,215 hrs · 25,317 cycles

THE FUSELAGE SKIN WAS FOUND DENTED BETWEEN FS 1271 & 1287 AND BETWEEN LONGERONS 26R & 30. THE DENT DAMAGE WAS REMOVED WITH A 25 X 18.5 INCHES CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 095859-14.

Part: VALVE — UNRELIABLE (AFT) · airframe 27,987 hrs · 21,692 cycles

LOSS OF PRESSURIZATION, DECOMPRESSION GRADUAL. DESCENT BELOW 10,000 DIVERT TO BDL - REPLACED LEFT PRSOV

Part: STRUT — UNDERSERVICED (NOSE GEAR) · airframe 22,963 hrs · 18,003 cycles

AIR RETURN -- NOSE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF - SERVICED NOSE STRUT - SWINGS OK

Part: TIRE — FAILED (MLG)

NUMBER 4 TIRE LOST RECAP AFTER T/O, DAMAGE TO BRAKE, FLAP, AND ENGINE FAN BLADES. REPAIRED ALL, REPLACED FAN.

Part: SKIN — DENTED (BS 244)

DENT WAS FOUND IN THE FUSELAGE SKIN AT APPROX FS 242 BETWEEN L17L AND L18L. REPAIRED PER ERA 333169-14, REV B.

Part: SKIN — GOUGED (BS 617)

A GOUGE WAS FOUND IN THE FUSE SKIN UNDER THE C2 CARGO DOOR CUTOUT, LOCATED APPROX AT FS 617, BETWEEN L30 AND L28L. REPAIRED PER ERA 333157-14, REV B.

Part: SKIN — DENTED (BS 229-237)

A FUSELAGE SKIN DENT WAS FOUND BETWEEN FS 229 AND FS 237, BETWEEN L18L AND 20L. REPAIRED PER ERA 333159-14, REV A.

Part: SKIN — DENTED (BS 297)

TWO DENTS WERE FOUND AT FS 297 BETWEEN L18L AND L20L. REPAIRED PER ERA 333179-14, REV A.

Part: SKIN — DENTED (BS 465)

A DENT WAS FOUND AT APPROX FS 465 AND L20R IN THE FUSELAGE SKIN. REPAIRED PER ERA 333158-14, REV A.

Part: FRAME — CRACKED (BS 1418)

MTC FOUND A CRACK AT L2L AND L2R ON THE STA 1418 FRAME. THESE CRACKS ARE TYPICALLY COVERED BY EO 9-63538-3, BUT THE EO AND RELATED SB DO NOT COVER THIS AC. REPAIRED PER ERA 333164-14.

Part: BATTERY PACK — DISCHARGED (BS 1100)

ON LAYOVER, FOUND FLOOR TRACK LIGHTING ON RT SIDE FROM APPROX STA 1100 AFT WOULD NOT COME ON. REPLACED THE BATTERY PACK B5-107. LIGHTS TESTED NORMAL.

Part: APU — FAILED (AFT FUSELAGE)

DURING CLIMBOUT, CABIN FILLED WITH BLUE SMOKE. RETURNED TO ATL. BOTH PACKS ON AND SMOKE DET CAPTS SIDE AFT WENT OFF. FOUND APU LEAKING OIL. REPLACED APU.

Part: LINE — LOOSE (RT HYD SYST)

IN-FLIGHT AT CRUISE, RT HYD QTY DECREASED RAPIDLY BELOW 4 QUARTS. AMBER LIGHT CAME ON. TURNED OFF RT SYS PUMPS PER PROCEDURE AND QTY STOPPED DECREASING. HYD LEAK FOUND ON GROUND.

Part: FILLER CAP — DAMAGED (NR 2 ENGINE)

AT FL220 THE RT ENG LOW OIL PRESS MESSAGE APPEARED ON THE EOAP. OIL PRESS WAS AT 33 PSI AND OIL QTY WAS AT ZERO. SHUTDOWN ENG AND DIVERTED TO IAD DUE TO CROSS WINDS AT DCA AND LONGER RUNWAY AT IAD. CONTRACT MAINTENANCE FOUND THE NR 2 ENG OIL FILTER CAP O-RING WAS CUT. REPLACED O-RING AND C/W M/M INSP REQ FOR WINDMILLING.

Part: HOSE — LEAKING (NR 2 ENGINE)

ACFT DIV TO MCO, RIGHT HYD SYS QUANTITY DECREASED RAPIDLY TOWARDS ZERO, PRESS FOLLOWED. FOLLOWED RIGHT HYD SYS FAILURE PROCEDURE. REPLACED NR 2 ENGINE HYD PRESSURE LINE, OPERATION NORMAL.

Part: STRIKER ANGLE — CRACKED (LT MLG WW)

CRACK, .1250 INCH, ON MLG W/W AFT O/B STRIKER. FOUND AT C-1 LTR CK. REPAIRED PER SRM 53-05, FIG 81A.

Part: STRIKER — CRACKED (RT MLG WW)

ONE INCH CRACK AT MLG W/W AFT O/B STRIKER. FOUND AT C-1 LTR CK. REPAIRED PER SRM 53-05, FIG 81A.