N917DL

Part: TIRE — FAILED (MLG) · airframe 80,966 hrs · 62,198 cycles

SDR REPORTED DUE TO NO 3 AND NO 4 TIRE COMING APART (ODI # 2019-00655) CAUSING RT INBD FLAP TE EDGE DAMAGE. RT I/B FLAP T/E EDGE DAMAGED. REPLACED RT I/B FLAP ASSY ON MD88 AMDS 2751-4324 FLAP, I/B (W/O OFF 88-2750-9-0007 S/N 00517. (LP6406327)

Part: TIRE — FAILED · airframe 80,966 hrs · 62,198 cycles

SDR REPORTED DUE TO NO 3 AND NO 4 TIRE COMING APART (ODI # 2019-00655) CAUSING COMPRESSOR DAMAGE TO NUMBER 2 ENGINE. THE TIRES WILL BE REPORTED ON A SEPARATE LOG AFTER THE AIRCRAFT HAS BEEN RETURNED TO SERVICE AND THE TIRE LOG SHEETS HAVE BEEN ENTERED. C/W JT8D-219 COMPRESSOR INLET CASE HUB OR FAN CHANGE. CARD 7100- 4680. COMPLIED WITH JT8D-219 COMPRESSOR INLET CASE HUB OR FAN CHANGE. CARD 7100-4680. 1ST STAGE HUB ASSY REMOVED: PN 821501. SN BBDUA06365. 1ST STAGE HUB ASSY INSTALLED: PN 821501. SN BBDUA31586. FTN 3D1729. COMPRESSOR INLET GROUP INSTALLED: PN 780830 SN PJ7975. COMPRESSOR INLET GROUP REMOVED: ??? PN 821501 SN BBDUA06365.??? DISK, & HUB 1ST OFF 03-7201-9-0016 S/N 06365 (LP1368995)

Part: TIRE — FAILED (MLG) · airframe 80,966 hrs · 62,198 cycles

BOTH RT MAIN TIRES BLOWN. RPLD BOTH RT MAIN WHEEL ASSYS PER MD88 AMM 32-40. S/N OFF DL1141 , S/N ON DL624. S/N OFF DL850, S/N ON DL708. (LP6406325)

Part: WINDOW — DAMAGED (COCKPIT) · airframe 80,116 hrs · 61,398 cycles

FO'S ESCAPE WINDOW APPEARS TO HAVE MELTED AND CRACKED. UPPER PORTION APPEARS WARPED. T/S FOUND THERMAL SWITCH ON F/O SLIDING WINDOW GLUED ON WITH WHAT APPEARS TO BE BLACK RTV. R/R F/O SLIDING WINDOW AND THERMAL SWITCH PER MD88 AMM 56-10. OPS AND LEAK CHECKS GOOD AT 4PSI. APPLIED CORRECT HEAT SINK COMPOUND TO THERMAL SWITCH AND VERIFIED/CORRECTED ALL OTHER COCKPIT THERMAL SWITCHES. ANTI FOG CHECKS GOOD AND VERIFIED IT CYCLES PROPERLY WITH TEMP GUN. A/C OK FOR SVC.

Part: SUPPORT — CORRODED (STAIR RAIL) · airframe 80,101 hrs · 61,386 cycles

RT SIDE VENTRAL AIR-STAIR HANDRAIL SUPPORT TUBES CORRODED AND BROKEN. REPLACED SUPPORT TUBE MPN 5936680-504. BEGAN ADJUSTING AIR STAIR DOOR PER MD88AMM 52-63. FINISHED ADJUSTMENT - TEST OPS NML PER MD88AMM 52-63. REPORTED DUE TO SAFETY CONCERN DURING EXITING. (LP5844849)

Part: CABLE — FRAYED (TAILCONE SLIDE) · airframe 80,084 hrs · 61,369 cycles

FOUND FRAYED KEVLAR CABLE FOR EMERGENCY EVACUATION TAIL CONE SLIDE. (CAT). NRC 00167: KEVLAR CABLE OF TAIL CONE SLIDE WAS REPLACED PER MD-88 AMM 53-53-00-401. (LP #1116831)

Part: SKIN — WORN (LT WING) · airframe 80,082 hrs · 61,368 cycles

WEAR ON LWR SKIN AT LEFT WING SETTLEMENT AREA OF HINGE FLAP FAIRING NO. 1 (AI). NRC 00148: WEAR WAS REPAIRED PER ETI-88-19-032 REV. 1 AND ER/A 556375-14 REV. A. ASSOCIATED ER/A 14-556375 ADDED FOR AC 0917. (LP #1112310)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 79,758 hrs · 61,086 cycles

SEAT MOUNTED ESCAPE PATH LIGHTS 19D & 23D INOP. SECURED LOOSE CONNECTORS UNDER SEATS IAW MD88 AMM 33-53-02. OPS CHECK GOOD. (LP4763709)

Part: FRAME — DAMAGED (BS 1079) · airframe 79,354 hrs · 60,753 cycles

TRANSFERRED FROM NR 10, LEFT SIDE FUSELAGE FRAME 1079, DAMAGED AT LONGERON L-21L. REPAIRED PER ERA 574949-14 REV A.

Part: SKIN — DAMAGED (BS 1070-1090) · airframe 79,354 hrs · 60,753 cycles

FUSELAGE SKIN DAMAGED, LEFT SIDE, STA.1070-1090 BETWEEN LEFT LONGERONS L22 AND L23. REF W/O:917_01/24/2019 LTO,DAMAGE BY BAGCART,TASK CARD NO:MD88 VIRTUAL,CARD/003, NR0003. DAMAGED SKIN REMOVED, AREA REPAIRED PER MD88 SRM 53-04-03 FIG.8. (LP0926431)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 79,329 hrs · 60,735 cycles

OVHD EMER LIGHTS INOP ROWS 20 - 26. REPLACED BATTERY PACK B5-104 AND BATTERIES PER AMM 33-53-00 EMERGENCY LIGHTS CHECK GOOD. (LP4765229)

Part: SKIN — DENTED (NR 2 NACELLE) · airframe 79,023 hrs · 60,495 cycles

LARGE DENT @ #2 ENGINE FOUR O'CLOCK POSITION OF ENGINE COWL. R/R #2 ENGINE NOSE COWL. PER MD88 AMM 71-10 COWL, NOSE, LT OFF 88-7110-9-0001 49591 ON 88-7110-9-0001 02258. (LP4754352)

Part: BRACKET — CRACKED (LT MLG WW) · airframe 78,593 hrs · 60,126 cycles

LT WHEEL WELL FRAME BRACKET MPN 5930584-33 CRACKED. REMOVED BRACKET (957441) DRILLED AND PAINTED NEW BRACKET. INSTALLED NEW BRACKET PER BOEING DRAWING 5930584. (LP0761217)

Part: DOOR FRAME — CRACKED (LT MLG WW) · airframe 78,593 hrs · 60,126 cycles

CRACK FOUND ON LEFT WHEEL WELL FRAME, BELOW DOOR RELEASE. REPLACED LT WHEEL WELL FWD DOOR JAMB PER BAC 5930584. (LP5352629)

Part: BATTERY — DISCHARGED (CABIN) · airframe 78,531 hrs · 60,066 cycles

SERVICE CHECK TAIL CONE CEILING LIGHTS INOP. AFT BATTERIES IN PACK INOP, CHANGED AND PERFORMED EMERGENCY LIGHT CHECK OPS CHECK OK IAW AMM 33-55. AFT TAIL CONE CEILING LIGHTS.

Part: CONDUIT — OUT OF POSITION (FUSELAGE) · airframe 78,439 hrs · 59,981 cycles

LOCKING CLAMP DID NOT CLEAR LOWER END OF CONDUITS BY AT LEAST 1/2 INCH REF TASK CARD 5350-01077-0101. REPOSITIONED CONDUITS PER TASK CARD 5350-01077-0101. (LP0720929)

Part: WASHER — MISSING (LOCK PIN) · airframe 78,439 hrs · 59,981 cycles

DURING INSPECTION ON LOWER LOCK RT LOCK PIN, FOUND LOCK PIN ASSEMBLY DIFFICULT TO SPRING RELEASE. SAME LOCK PIN ASSEMBLY IS MISSING WASHER ON ONE OF ITS ATTACH BOLTS. REPLACED MISSING HARDWARE, CLEANED AND RELUBED AS REQUIRED. (LP0720933)

Part: LOCK PIN — LACK OF LUBE · airframe 78,462 hrs · 59,999 cycles

DURING INSPECTION ON L/H LOCK PIN, FOUND LOCK PIN ASSEMBLY DIFFICULT TO SPRING RELEASE. CLEANED AND RE-LUBED AS REQUIRED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,327 hrs · 59,887 cycles

FOUND FWD CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACKS IAW AMM 33-50. OPS CHECKED GOOD. OK FOR SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,216 hrs · 59,800 cycles

AFT LAV SERVICE DOOR CUTOUT CORROSION AND DOUBLER REPAIR. LOCATED AT FS 1307 TO FS 1322 AND L-22L.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,216 hrs · 59,800 cycles

DURING WAKE UP FOUND AFT LAV SERVICE PANEL LOWER CUT OUT CRACKED. COMPLETED REPAIR AT AFT LAV SERVICE DOOR CUT-OUT PER ERA 570456-14 REV ORIG.

Part: UNKNOWN — ODOR (CABIN) · airframe 78,033 hrs · 59,652 cycles

AFT LEFT LAV SMOKE DETECTOR SOUNDED ON APPROACH AND LASTED FOR ABOUT 30 SECONDS. FLIGHT ATTENDENT REPORTED AN ELECTICAL SMELL THAT LASTED ABOUT TWO MINUTES (1 MINUTE BEFORE ALARM THROUGH ABOUT 30 SECONDS AFTER). C/W NO GO ODI PREVENTION PROGRAM ATA 2172 REF LOG 0626209. NO TROUBLE WAS FOUND AND SMOKE DETECTOR WAS REPLACED.

Part: FIRE WARNING — FALSE ACTIVATION (RT ENGINE) · airframe 77,482 hrs · 59,210 cycles

RIGHT ENGINE FIRE WARNING AURAL, NO LIGHTS. PERFORMED ENGINE FIRE TEST IAW AMM 26-20. NO 30 DAY HISTORY. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 77,242 hrs · 59,025 cycles

AFT LAV ALARM ON APPROACH FUMES/ODOR OBSERVED NO SMOKE OBSERVED. T/S PER ODI PREVENTION W/C 2120/2367 NO COMTAMINATION NOTED C/W DUCT BURNOUT PER W/C 7100-2619 VF REQUIRED PER ODI REF LOG PAGE 9889220.

Part: B-NUT — LOOSE (HYD PUMP) · airframe 77,203 hrs · 58,991 cycles

AFTER LANDING, THE LEFT HYDRAULIC PRESSURE AND QUANTITY WENT TO ZERO. SHORTLY AFTER, THE CABIN BEGAN TO FILL WITH SMOKE. THE PACKS WHERE SHUT OFF AND THE SMOKE DISSIPATED. MAINTENANCE FOUND THE B-NUT LOOSE ON THE HYDRAULIC LINE TO THE LEFT ENGINE DRIVEN HYDRAULIC PUMP FILTER MODULE. MAINTENANCE SECURED THE LINE AND REPLACED THE PUMP AND PTU.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 77,012 hrs · 58,839 cycles

FOUND R1 DOOR SLIDE PINS DISENGAGED. R&R R1 DOOR SLIDE PER W/C 2561-4964 OP CK GOOD.

Part: PIN — BROKEN (AC BAY) · airframe 77,012 hrs · 58,839 cycles

TAIL COMPARTMENT CENTER CAT WALK EMERGENCY LIGHT INOP. REPLACED BROKEN PIN PER SWPM 20-10-02, CKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,965 hrs · 58,803 cycles

EMERGENCY LIGHTS IN OVERWING EXIT SIGNS AT ROW 24, LEFT AND RIGHT, INOP. SWAPPED LAMPS NO HELP. REMOVED AND REPLACED B5-103 BATTERY PACK PER AMM 33-53. ALL TEST GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 75,785 hrs · 57,843 cycles

EMER LIGHTS (CELING) ROWS 11-14 INOP. FOUND BATTERIES IN B5-101 DEAD. R&R SAME PER AMM 33-53. OPS CK SAT.

Part: LIGHT — SPARKS (LAVATORY) · airframe 75,770 hrs · 57,829 cycles

SPARKS IN AFT LEFT LAVATORY FROM LIGHT. COMPLIED WITH ERA 560231-14, REPLACED THE SWITCH . CHECKED GOOD.

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 75,529 hrs · 57,639 cycles

CORROSION ON FLOOR PANEL 211BG. THE FLOOR PANEL REPAIRED IAW ER/A 504469-14MA.

Part: CABLE — TORN (TAILCONE) · airframe 75,294 hrs · 57,472 cycles

TORN TAILCONE CABLE ASSEMBLY. REPLACED THE CABLE IAW AMM 53-53 AND COMPLETED REQUIRED INSPECTION.

Part: SKIN — CRACKED (LT WING) · airframe 75,294 hrs · 57,472 cycles

LEFT WING CRACKED TE SKIN. REPAIRED IAW ER/A 494597-14AD MA, REV A.

Part: ANGLE — CRACKED (HORIZONTAL STAB) · airframe 75,294 hrs · 57,472 cycles

HORIZONTAL STABILIZER HAD A CRACKED ANGLE BETWEEN XHR=9.6 AND YV=158. REPLACED IAW SRM 51-30-2, AND 51-30-5.

Part: SKIN — DAMAGED (BS 580) · airframe 75,294 hrs · 57,472 cycles

DURING INSPECTION, AN INDICATION OF MATERIAL THINNING 0.051, SKIN. REMAINING WAS FOUND AT BS 580, L29R, JUST FWD OF PREVIOUS REPAIR. FUSELAGE SKIN WAS REPAIRED IAW ER/A 558084-14, REV ORIGINAL.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON THE ACCESS PANEL 1331C. REPLACED IAW AMM 28-40-04.

Part: STRUCTURE — CORRODED (BS 1260-1287) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

AFT CARGO BAY HAD CORROSION ALONG LONGERON 19 - 21L BETWEEN BS 1287 TO 1260. REPAIRED IAW ER/A 558085-14, REV ORIGINAL, AND ETI-88-17-144 REV ORIGINAL.

Part: CARGO TRACK — CORRODED (BS 325-506) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

FORWARD CARGO BAY CORROSION ON CARGO TRACK BS 325 - 506. THE CARGO TRACK WAS REPAIRED IAW ETI-88-17-142, REV 2, & ER/A 558077-14, REV ORIGINAL.

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · airframe 75,294 hrs · 57,472 cycles

CORROSION ON FLOOR PANEL 120D. THE FLOOR PANEL WAS REPLACED.

Part: INTERCOSTAL — CORRODED (BS 1380-1385) · airframe 75,294 hrs · 57,472 cycles

CORROSION ON INTERCOSTAL BS 1380 - 1385, LONGERONS 24L TO 24R. REPAIRED IAW SRM 51-70-5, FIG 1, 51-30-5 , 51-30-2, AND 51-10-3, PAR 21, 14.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON AREA OF SETTLEMENT AND COUNTERSINK ON FUEL TANK ACCESS PANEL. THE ACCESS WAS REPLACED IAW SRM 51-22-2A PAR. 6 COND. III.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

FUEL TANK ACCESS PANEL WAS CORRODED OUT OF LIMITS AND WAS REPLACED. IAW SRM 51-10-3.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

FUEL TANK ACCESS PANEL CORRODED OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A CONDITION II (A) (1).

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON AREA OF SETTLEMENT AND COUNTERSINK ON FUEL TANK ACCESS PANEL 1335C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6, COND II (B).

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

AFT CARGO COMPARTMENT: CORROSION ON ANGLE BELOW LT TIE TRACK BTW Y=1231-1250. SPLICES ANGLES WERE REPLACED PER SRM 53-24-0 & SRM 51-30-5.

Part: CARGO TRACK — CORRODED (BS 1007-1322) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON THE RIGHT CARGO TRACK, BS 1007 - 1322. THE CARGO TRACK WAS REPLACED IAW DWG 5936660, REV BZ, SRM 51-30-1 AND 51-30-2.

Part: CARGO TRACK — CORRODED (BS 1007-1322) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON LEFT CARGO TRACK FROM BS 1007 - 1322 . THE LEFT CARGO TRACK WAS REPLACED IAW SRM 51-30-2, AND 51-3-1.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 75,294 hrs · 57,472 cycles

RIGHT WING LOWER ACCESS DOOR CUTOUT XRS = 189.0 TO 214.0 CRACKED. REPAIRED IAW ETI-88-17-129 REV. 2 & ER/A 556392-14AD, REV ORIGINAL.

Part: SKIN — CRACKED (LT WING) · airframe 75,294 hrs · 57,472 cycles

CRACKS ON THE LT WING LOWER ACCESS DOOR CUTOUT XRS 189 - 214. REPAIRED IAW ETI-88-17-129, REV 2 & ER/A 556392-14AD, REV ORIGINAL.

Part: LONGERON — CORRODED (BS 1232-1309) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

AFT CARGO BAY HAD CORROSION ON LONGERON 21R, BS 1232 - 1309. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: SKIN — NICKED (LT WING TE FLAP) · airframe 75,294 hrs · 57,472 cycles

LEFT WING NICKED ON LOWER SURFACE SKIN AT INBD VANE INBD FLAP. INBD VANE INBD FLAP WAS REPAIRED IAW SRM 57-03D, PAR 11.

Part: FLOOR PANEL — CORRODED · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON FLOOR PANEL 120D. REMOVED AND REPAIRED THE FLOOR PANEL.

Part: ANGLE — CRACKED (BS 826-845) · airframe 75,294 hrs · 57,472 cycles

PAX CABIN CRACKED LT ANGLE BETWEEN BS 826 TO 845, LBL 42, Z -10 . THE ANGLE WAS REPAIRED IAW ER/A 498192-14MA REV ORIGINAL.

Part: SKIN — CORRODED (BS 105-115) · airframe 75,294 hrs · 57,472 cycles

LOOSE FASTENERS AND CORROSIONS ON LOWER SKIN FUSELAGE BETWEEN BS 105 - 115 AND LONGERONS 27L TO 27R . THE SKIN WAS REPLACED IAW DWG 5913421 REV V, SRM 51-30-2, AND 51-30-5.

Part: SERVICE PANEL — CORRODED (LAVATORY) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON AFT LAVATORY SERVICE PANEL. AFT LAVATORY SERVICE PANEL WAS REPLACED IAW SRM 51-10-4.

Part: DOUBLER — WORN (FUSELAGE) · airframe 75,294 hrs · 57,472 cycles

WEAR INTERNAL DOUBLER JUS ON UPPER CORNERS AT AFT LAVATORY SERVICE ACCESS TRAY. WEAR INTERNAL DOUBLER WAS REPAIRED PER DWG 5911423 REV CD AND ER/A 397822-14MA REV B.

Part: INTERCOSTAL — CORRODED · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON INTERCOSTAL BS 1322 TO 1338 BTW LONG 21 & 22L. INTERCOSTAL WAS REPLACED PER DWG.5911423 REV."CD" AND SRM 51-30-2 AND 51-30-5.

Part: LONGERON — CORRODED (BS 1287-1322) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

AFT CARGO BAY HAD CORROSION ON LONGERON 22L BETWEEN BS 1287 - 1322. THE DAMAGED LONGERON SECTION WAS REPLACED IAW SRM 53-02, FIG 18.

Part: SEAT TRACK — CORRODED (BS 200) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON SEAT TRACK RBL 44, BS 200. THE SEAT TRACK WAS REPLACED IAW SRM 51-10-4, 51-30-5, AND 51-30-1.

Part: FINGER DOUBLER — CRACKED (BS 256-275) · airframe 75,294 hrs · 57,472 cycles

CRACKED FINGER DOUBLER BS 256 - 275 BETWEEN LONGERONS 24 - 25L IN THE FWD CARGO BAY. THE FINGER DOUBLER WAS REPLACED IAW ER/A 273415-14, REV B, AND 51-30-2.

Part: FITTING — CORRODED (BS 173-197) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

FWD WET AREA HAD CORROSION ON FLOOR FITTINGS BS 173, & 197, RBL 53. THE FITTINGS WERE REPLACED IAW SRM 51-10-4, AND 51-30-1.

Part: INTERCOSTAL — CORRODED (BS 1309-1322) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

AFT CARGO BAY HAD CORROSION ON THE INTERCOSTAL BETWEEN BS 1309 - 1322, LONGERON 27R. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-02, 51-30-05, AND DWG 9936718, REV N.

Part: SKIN — DAMAGED (LT WING) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

WORN AND CORROSION ON LT WING LOWER SKIN XRS 111.500. AREA WAS REPAIRED IAW ER/A 556375-14, REV ORIG, AND ETI-88-17-115, REV ORIG.

Part: CUSP WEB — NOT REPORTED (BS 925-946) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

OUT LIMITS ON CUSP WEBS MEMBRANE BS 925 - 946, RBL 54 - 60. THE CUSP WEB WAS REPAIRED SRM 53-05, FIG 131A-4.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON THE LT WING FUEL TANK ACCESS PANEL. CUT OUT THE RUB STRIPS AND REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — NOT REPORTED (BS 826-845) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

OUT LIMIT ON CUSP WEBS MEMBRANE BS 826 TO 845 BETWEEN LBL 54 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-3.

Part: INTERCOSTAL — CORRODED (BS 1309-1322) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON INTERCOSTAL BETWEEN BS 1309 - 1322, LONGERONS 27 - 28L IN THE AFT CARGO BAY. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2, 51-30-5, AND DWG 9936718, REV N.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,294 hrs · 57,472 cycles

CRACKED INTERCOSTAL ON X=0 BTW STA Y=769 AND Y=788 ALSO ON X=3 BTW STA Y=1287 AND Y=1271 AT FLOOR STRUCTURE CABIN. INTERCOSTAL ON STA Y=769 TO Y=788 X=0, WAS REPLACED PER SRM 51-30-5 AND 51-30-2 REPAIR ON INTERCOSTAL STA Y=1271 TO 1287 X=3 AT FLOOR STRUCTURE CABIN WAS ACCOMPLISHED PER SRM 53-01 FIG 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON FLOOR SUPPORT BTW STA Y=160-200 AND X=-44. FLOOR SUPPORT BTW STA Y=160-200 AND X= -44 WAS REPLACED PER SRM 53-14-1 FIG 11 AND 51-10-4.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON FLOOR PANEL 120A, 120B AT COCKPIT CABIN. FLOOR PANELS NR 120A AND 120B AT COCKPIT WERE REPLACED PER SRM 51-10-4, 51-10-3 AND DWG 9957805 REV Y AND 9957824 REV R.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 75,294 hrs · 57,472 cycles

CRACKED CUSP WEB STA Y= 221 X=-46 RT SIDE AT CABIN PAX. CRACKED CUSP WEB STA Y= 221 X=-46 RT SIDE AT CABIN PAX WAS REPLACED PER SRM 51-30-2 AND DWG 9930538 REV CC.

Part: CUSP WEB — NOT REPORTED (FUSELAGE) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

AWR SECOND TIER: OUT LIMIT ON CUSP WEBS MEMBRANE STA Y=927 TO Y =946 BTW X=54 TO X=60 AT CABIN PAX. LT CUSP WEB FROM START Y=927 TO Y=946 BTW X=54 AND X=60 WAS REPAIRED PER SRM 53-05 FIG 131A-4.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 75,294 hrs · 57,472 cycles

DAMAGED FERRULES ON FLOOR PANELS 313C, 389C, 541D, 617D, 693C, 769B, 927B, 1079B, 1117C, 1115B, 1174C, 1174E, 1250C, 1250D, PAX CABIN. DUE TO SEVERE EXCESSIVE DAMAGES FLOOR PANEL NR 693C WAS REPLACED PER AMM 53-20-01-201 PARAGRAPH 7 FLOOR PANELS NR 313C, 389C, 541D, 617D, 769B, 927B, 1079B, 1115B- ,1117C, 1174C, 1174E, 1250C AND 1250D WERE REPLACED FERRULES PER AMM 53-20-01-201 PARAGRAPH 7.

Part: CUSP WEB — CRACKED (BS 905) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CRACKED CUSP WEB RBL 54, BS 905. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131A-1.

Part: CUSP WEB — CORRODED (BS 905-924) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORRODED OUT OF LIMITS CUSP WEB BS 905 - 924, RBL 54 TO 60. THE CUSP WEB WAS REPAIR IAW SRM 53-05, FIG 131A-13, SHEET 1.

Part: CUSP WEB — CRACKED (BS 1060-1065) · airframe 75,294 hrs · 57,472 cycles

CRACKED CUSP WEB BETWEEN RBL 54 AND 60, BS 1060 - 1065 IN THE CABIN. REPAIRED IAW SRM 53-05, FIG 131A.

Part: SEAT TRACK — DAMAGED (BS 357-766) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

AREAS OUT OF LIMITS ON THE SEAT TRACK LBL 54, 357 - 766. REPAIRED IAW SRM 53-05, FIG 4A.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 75,294 hrs · 57,472 cycles

CRACKED CHANNEL ON FLOOR PANEL. REPAIRED IAW SRM 53-05, FIG 131B, AND 131C.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON FLOORBEAM, BS 200 BTW LBL 7 - RBL 54. THE FLOORBEAM WAS REPLACED IAW SRM 53-14-1, FIG. 11, SRM 51-10-4, SRM 51-30-2, AND SRM 51-30-5.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 75,294 hrs · 57,472 cycles

CRACK ON SKIN OF FLOOR PANEL. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-01, FIG 4.

Part: RUB STRIP — CORRODED (LT WING) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

LEFT WING, FOUND CORROSION ON THE RUBSTRIPS UPPER SURFACE ACCESS PANEL OPENING 1311C. THE RUB STRIP WAS REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CRACKED (BS 446-456) · airframe 75,294 hrs · 57,472 cycles

A CRACK WAS FOUND ON THE LT CUSP WEB LBL 54 BETWEEN BS 446 AND 465. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-8.

Part: RUB STRIP — CORRODED (LT WING) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

LEFT WING, CORROSION FOUND ON RUBSTRIPS UPPER SURFACE ACCESS PANEL OPENINGS. THE RUBS STRIPS WERE REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CORRODED (BS 503-522) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON A REPAIR DOUBLER ON THE CUSP WEB RBL 54 - 60, BS 503 AND 522. THE AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-7.

Part: FLOORBEAM — CORRODED (BS 200) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON FLOORBEAM BS 200, RBL 44. THE FLOORBEAM WAS REPAIRED IAW SRM 53-05, FIG 20B.

Part: DIAPHRAGM — CORRODED (BS 200) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON DIAPHRAGM BS 200 AND RBL 43. THE DIAPHRAGM WAS REPAIRED IAW SRM 51-70-4, FIG. 2.

Part: CUSP WEB — CORRODED (BS 905-1022) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON THE CUSP WEB RBL 44 - 60, BS 905 - 1022. THE CORROSION WAS REMOVED, THE CUSP WEB WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 26, 21 AND 14.

Part: TAB — DENTED (HORIZONTAL STAB) · airframe 75,294 hrs · 57,472 cycles

HORIZONTAL STABILIZER HAD DENTS ON RT & LT CONTROL TABS UPPER & LOWER SURFACE. REPLACED THECONTROL TABS IAW SRM 51-50-2 PAR. 4.

Part: INTERCOSTAL — CRACKED (BS 941) · airframe 75,294 hrs · 57,472 cycles

RIGHT WHEEL WELL HAD A CRACKED INTERCOSTAL BS 941 AND RBL 7. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2, AND 51-30-5.

Part: CUSP WEB — CORRODED (BS 522-541) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORRODED REPAIR DOUBLER ON THE CUSP WEB RBL 54 - 60 BETWEEN BS 522 AND 541. THE REPAIR DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-05, SRM 53-05, FIG 131A-13, SHEET 1, AND SRM 53-05 FIG. 131A-13, SHEET 1.

Part: DOOR FRAME — CRACKED (RT OVERWING) · airframe 75,294 hrs · 57,472 cycles

RT OVERWING DOOR FRAME CRACKED. REPAIRED IAW SRM 53-05, PAR 42, FIG. 32.

Part: BEAM — CRACKED (L1 DOOR) · airframe 75,294 hrs · 57,472 cycles

L1 DOOR BEAM CRACKED ON BOTH CORNERS. THE BEAM WAS REPAIRED IAW SRM 52-05, PAR 68, FIG 81-82.

Part: FLOOR SUPPORT — OUT OF LIMITS · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON FLOOR SUPPORT BS 1007, 1079, 1155 BETWEEN LONGERONS 28L - 28R. OUT OF LIMITS PER SRM 53-01 FIG 1 SHEET 3.

Part: FLOOR SUPPORT — CORRODED (BS 1307-1338) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORRODED FLOOR SUPPORT AFT WET AREA BETWEEN BS 1307 - 1338, RBL 18. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-1 AND DWG 9936656, REV AM.

Part: VANE — WORN (RT WING TE FLAP) · airframe 75,294 hrs · 57,472 cycles

RIGHT WING WORN ON UPPER SURFACE SKIN AT THE OTBD FIXED GUIDE VANE INBD FLAP. REPAIRED THE GUIDE VANE IAW SRM 57-03 D, PAR 11.

Part: FLOORBEAM — CORRODED (BS 1155) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON THE FLOORBEAM AT BS 1155 BTW LONG 28L AND 28R IN THE CARGO BAY. THE FLOORBEAM ANGLE WAS REPLACED IAW SRM 51-30-5, AND DWG 5956705, REV AY.

Part: PAN — CRACKED (PAX DOOR) · airframe 75,294 hrs · 57,472 cycles

DOOR CRACKED ON UPPER FWD CORNER OF SEGMENT PAN AT FORWARD ENTRY DOOR. UPPER FWD CORNER OF SEGMENT PAN AT FWD ENTRY DOOR WAS REPAIRED IAW SRM 52-05, PAR 14, FIG 18A.

Part: FLOOR SUPPORT — CORRODED (BS 237-256) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION FOUND ON THE FLOOR SUPPORT BETWEEN BS 237 TO 256, LBL 33. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-4, AND SRM 51-30-5.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION AND CRACKS FOUND ON THE FLOOR PANEL 160G. FLOOR PANEL WAS REPLACED IAW 51-10-2, AND DWG 9957828, REV Y.

Part: LONGERON — CRACKED (BS 1429) · airframe 75,294 hrs · 57,472 cycles

AFT ACCESSORY BAY HAS A CRACKED LONGERON 16R, BS 1429. THE LONGERON WAS REPLACED IAW SRM 51-30-5, AND 51-30-2.

Part: RUB STRIP — CORRODED (RT WING) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

RIGHT WING HAS CORROSION ON THE RUBSTRIPS UPPER SURFACE. THE RUBSTRIPS WERE REPLACE IAW SRM 51-22-2A.

Part: CUSP WEB — PUNCTURED (BS 264) · airframe 75,294 hrs · 57,472 cycles

LEFT CUSP WEB SURFACE PUNCTURED AT LBL 44 TO 54, BS 264. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, PAR 144, FIG 131A-13.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 75,294 hrs · 57,472 cycles

RIGHT WING HAD NICKS ON LOWER SURFACE SKIN AT THE RT INBOARD VANE INBD FLAP. REPAIRED IAW SRM 57-03D, PAR 11, FIG 11.

Part: CUSP WEB — CORRODED (BS 570-712) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON CUSP WEB BETWEEN LBL 54 AND 60, BS 570 - 712. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-14.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

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

Part: STRUCTURE — DAMAGED (RT NACELLE) · airframe 75,294 hrs · 57,472 cycles

RIGHT PYLON HAD ELONGATED APRON FITTING HOLES. REWORKED, BUSHINGS WERE FABRICATED AND REPLACED IAW CMM 71-10-10 ERA 228793-14 & 266727-14 PAGE D601.

Part: TAB — DENTED (HORIZONTAL STAB) · airframe 75,294 hrs · 57,472 cycles

HORIZONTAL STABILIZER DENTED ON THE LT & RT ANTI FLOAT TAB UPPER SURFACE. THE ANTI FLOAT TABS WERE REPAIRED IAW SRM 55-04 P. 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON FLOOR SUPPORTS BTW STA Y=150-200 AND X=7, X=-7. FLOOR SUPPORTS WERE REPLACED PER SRM 51-30-1.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,294 hrs · 57,472 cycles

PAX CABIN, CRACK ON LONGERON NR 4 LT STA Y= 160 AT PASSENGER CABIN. LONGERON SECTION NR 4 LT BTW Y=150 TO Y= 170 WAS REPAIRED PER CARD AMDS 5330-01204-04, SR- 09530170 REV ORG AND SRM 53-02 FIG 18.

Part: SPACER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORROSION ON PREVIOUS REPAIR SPACER AT LOWER MID CARGO COMPARTMENT DOOR JAMB. PREVIOUS REPAIR SPACER WAS REPLACED PER SRM 53-05 FIGURE 123A.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,294 hrs · 57,472 cycles

AFT ACCESSORY COMPARTMENT, CRACKED LONGERON 3R ON STA Y=1429. LONGERON WAS REPAIRED PER SRM 53-02 FIG 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 75,294 hrs · 57,472 cycles

CRACK ON LONG 2R BTW STA Y = 541 AT PAX CABIN. REPAIRED LONG 2 R BTW STA Y=520 TO Y=560 PER SRM 53-02 FIG 18 SHEET 1.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 75,294 hrs · 57,472 cycles

WORN FWD LOWER DOUBLER ON THE FWD CARGO DOOR. THE DOUBLER WAS REPLACED IAW ER/A 486624-14 MA, REV ORIGINAL.

Part: DOUBLER — CORRODED (CUSP WEB) · corrosion level 2 · airframe 75,294 hrs · 57,472 cycles

CORRODED REPAIR DOUBLER ON CUSP WEB FROM RBL 54 TO 60 BETWEEN BS 712 AND 731. THE DOUBLER WAS REPLACED IAW SRM 53-05, FIG131A-10, 51-30-2, AND 51-30-5.

Part: ANGLE — CRACKED (RT OVRWG DOOR) · airframe 75,294 hrs · 57,472 cycles

CRACKED ANGLE ON UPPER CORNERS OF CHANNEL ON THE RT AFT OVERWING EXIT DOOR. THE ANGLES WERE REPLACED IAW DWG:9957735, REV G, SRM 51-30-2, AND 51-30-5.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 75,294 hrs · 57,472 cycles

CRACKED ANGLE ON FWD LT EMERGENCY DOOR STOP NR 1. THE ANGLE WAS REPLACED IAW 51-30-5, 51-30-2, AND DWG 9957735 REV. G.

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 75,294 hrs · 57,472 cycles

PUNCTURE ON FLOOR PANELS 826E, 826B. 826E AND 826B WERE REPLACED PER AMM 53-20-01-201.

Part: SKIN — DELAMINATED (HORIZ STAB TAB) · airframe 75,294 hrs · 57,472 cycles

HORIZONTAL STABILIZER, DELAMINATION ON LT ANTI-FLOAT TAB UPPER/LOWER SURFACE. ANTI-FLOAT TAB WAS REPAIRED PER SRM 55-04 P 3.

Part: PAN — CRACKED (BS 826) · airframe 75,294 hrs · 57,472 cycles

CRACK ON RING PAN LT SIDE, BS 826. THE RING PAN WAS REPAIRED IAW SRM 53-02, FIG 122, AND ER/A 487747-14MA, REV A, AND 493648-14MA, REV A.

Part: PAN — CRACKED (BS 1098) · airframe 75,294 hrs · 57,472 cycles

CRACK ON AFT LOWER CORNER RING PAN LT SIDE BS 1098. REPAIRED IAW SRM 53-05, FIG 122.

Part: PAN — CRACKED (BS 984-1003) · airframe 75,295 hrs · 57,472 cycles

CRACK IN REPAIR OF RING PAN LT BETWEEN BS 984 TO 1003. REPAIRED IAW SRM 53-05 FIG.122.

Part: ANGLE — CRACKED (BS 946-964) · airframe 75,295 hrs · 57,472 cycles

CRACKED AFT, UPPER ANGLE OF CORNER ON RING PAN BS 946 - 964. REPLACED IAW SRM 51-30-2, AND 51-30-5.

Part: PAN — CRACKED (BS 807-826) · airframe 75,295 hrs · 57,472 cycles

CRACKED FWD, LOWER CORNER OF RING PAN BETWEEN BS 807 - 826. REPAIRED IAW SRM 53-05, FIG 122.

Part: RAMP — WORN (TAILCONE) · airframe 74,400 hrs · 56,810 cycles

DURING TAILCONE FUNCTIONAL CHECK FOUND CAM BASE(RAMP) WORN. REPLACED CAM BASE IAW CARD 5350-01077-0101.

Part: BRACKET — CRACKED (TAILCONE) · airframe 74,400 hrs · 56,810 cycles

DURING TAILCONE FUNCTIONAL FOUND RT UPPER SPADE RECEPTACLE LOWER SUPPORT ANGLE BRACKET ATTACH RIVETS LOOSE. BRACKET CRACKED. FABRICATED NEW BRACKET. INSTALLED NEW BRACKET PER IPC 53- 50-00-30 ITEM 240 AND DWG 9911957-38. RII COMPLETE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 74,261 hrs · 56,707 cycles

R1 DOOR HAS AN EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS IAW AMM 33-53.

Part: CLAMP — UNSECURE (MANIFOLD) · airframe 73,968 hrs · 56,489 cycles

THE CREW DIVERTED THE AIRCRAFT DUE CABIN PRESSURIZATION ISSUES DURING CLIMB. SECURED CLAMP ON HOT AIR MANIFOLD. PERFORMED HULL LEAK CHECK AND SINGLE PACK CONFIDENCE CHECK. ALL CHECKS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,718 hrs · 56,295 cycles

EMERGENCY SEAT MOUNTED LIGHT AT FWD FA SEAT INOPERATVE. REPLACED THE LAMP, CHECKED GOOD.

Part: TIRE — FAILED (LT MLG) · airframe 73,237 hrs · 55,931 cycles

LEFT MLG FIXED DOOR DAMAGED BY IMPACT OF TIRE DEBRIS. REPLACED LT MLG - FIXED DOOR. IAW AMM 32-10.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 73,237 hrs · 55,931 cycles

LT WING OTBD OF LT MLG LOWER COMPOSITE ACCESS PANEL DAMAGED BY TIRE DEBRIS. REPAIRED OUTER SKIN IAW SRM 51-90-0 AND ERA 545756-14MA, REV ORIGINAL.

Part: TIRE — FAILED (MLG) · airframe 73,237 hrs · 55,931 cycles

NR 1 AND 2 MAIN TIRES BLOWN CAUSING DAMAGE TO MULTIPLE ITEMS AT LT MLG AND SURROUNDING AREAS. DAMAGED ITEMS ADDRESSED ON CARDS 1 THRU 20.

Part: TIRE — FAILED (MLG) · airframe 73,237 hrs · 55,931 cycles

ABORTED TAKEOFF BETWEEN 100-120 KNOTS IAW CREW REPORT DUE TO NR 1 AND NR 2 TIRE FAILURES. BOTH TIRES WERE REPLACED. LT ENGINE NOTED TO HAVE TIRE DEBRIS IN INLET. DETAILED INSPECTION COMPLETED WITH NO BOROSCOPE FINDINGS ON LP 8687116. LT ENGINE NOTED TO HAVE MINOR DAMAGE TO ACOUSTIC LINER AFT OF 1ST STAGE FAN DUE TO TIRE DEBRIS. REPAIRED DAMAGED AREA ON LP 8687118.

Part: START VALVE — MALFUNCTIONED (RT ENGINE) · airframe 73,194 hrs · 55,897 cycles

FLT 1515 RETURNED TO DEPARTURE DUE TO RT ENGINE START VALVE SHOWING OPEN AND RT ENGINE OIL TEMP RISING. R & R START VALVE IAW AMM.

Part: SKIN — CRACKED (BS 1361) · airframe 72,524 hrs · 55,423 cycles

FUSELAGE SKIN CRACKED AT ONE FASTENER ON RT SIDE BS 1361, JUST ABOVE PYLON. REPAIRED BY CUTOUT AND DOUBLER. ALL WORK ACCOMPLISHED AND RECORDED ON PRI 544231-14, REV 0 AND VERIFIED COMPLIES WITH FINAL ERA 544231-14, REV ORIGINAL SECTION I.

Part: SCUFF PLATE — CORRODED (AFT CARGO) · corrosion level 2 · airframe 72,524 hrs · 55,423 cycles

AFT CARGO, AFT SCUFF PLATE ATTACH FITTING HAS CORROSION. BLENDED CORROSION AND CHECKED LIMITS IAW SRM 53-01, PAGE 8 OUT OF LIMITS REPLACED PART. INSTALLED IAW SRM 53-01-01.

Part: THRESHOLD — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 72,524 hrs · 55,423 cycles

AFT CARGO THRESHOLD SILL CORRODED IN NUMEROUS PLACES. REPAIRED IAW ERA 499523-14MA REV ORIGINAL.

Part: DUCT — CRACKED (RAM AIR) · airframe 72,524 hrs · 55,423 cycles

RAM AIR DUCT IS CRACKED ON LT SIDE MID SPAN. RAM AIR DUCT WELD REPAIR COMPLETE REF; ERA420329-14MA. REV C.

Part: SKIN — CRACKED (BS 1361) · airframe 75,095 hrs · 57,334 cycles

SKIN BS 1361, LONGERON 14R CRACKED. REPAIRED IAW ER/A 544231-14 SECTION 1.

Part: DOOR FRAME — CRACKED (LT MLG) · airframe 72,487 hrs · 55,399 cycles

LT MLG FWD DOOR JAMB CRACKED. REMOVED DAMAGED CHANNEL, DRILLED UP NEW CHANNEL REPAIR SECTION. C/W ERA 543810-14, REV ORIGINAL SECTION II, PERMANENT REPAIR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,447 hrs · 53,316 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE CEILING EMERGENCY LIGHTS AT ROWS 10-15 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,063 hrs · 53,017 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING AT SEAT 11, 12, AND 14 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,927 hrs · 52,916 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE NOTED LIGHTED AREAS AND THE OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,746 hrs · 52,760 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING IN THE FIRST CLASS CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 68,275 hrs · 52,422 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT WAS STRIPPED OUT OF LOCATION AT SEAT ROW 14. MAINTENANCE R & R THE EMERGENCY PATH LIGHT ASSEMBLY AT ROW 14DE AND THE LIGHTS RETURNED TO AN OPERATIONAL STATE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 68,038 hrs · 52,252 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE SEAT EMERGENCY LIGHT AT SEATS 24DE TO BE INOPERATIVE. MAINTENANCE FOUND AND REPLACED A BAD PIGTAIL AND THE SEATS RETURNED TO AN OPERATIONAL STATE.

Part: FRAME — CORRODED (BS 1309) · corrosion level 2 · airframe 74,261 hrs · 56,707 cycles

AFT CARGO AFT SIDE OF FRAME HAS CORROSION BS 1309 BETWEEN LONGERONS 29L - 29R. INSTALLED REPAIR IAW SRM 53-03D FIG. 5.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,289 hrs · 51,712 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE AFT MOST SIDEWALL EMERGENCY PATHWAY LIGHT FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: FAN — INOPERATIVE (RECIRCULATION) · airframe 64,681 hrs · 49,926 cycles

ON DESCENT FOR LANDING, THE COCKPIT CREW AND THE F/A NOTICED AN ELECTRICAL ODOR CIRCULATING IN THE COCKPIT AND CABIN. THE CAPTAIN COMPLIED WITH THE QRH FOR SMOKE, PULLED THE CIRCUIT BREAKERS FOR THE RECIRCULATION FAN, AND THE ODOR SOON DISSIPATED. MX INSPECTED THE FAN AND ALSO NOTICED AN ODOR. THEN, WHEN AN ATTEMPT TO RUN THE FAN WAS MADE, THE CIRCUIT BREAKERS WOULD IMMEDIATELY TRIP. THE RECIRCULATION FAN WAS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,637 hrs · 49,897 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING ABOVE ROWS 11-15 WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: NOSE COWL — DAMAGED (NR 2) · airframe 64,533 hrs · 49,821 cycles

NR 2 ENG NOSE COWL INNER BARREL AT 9 O'CLOCK POSITION, SMALL AREAS OF WIRE MESH LOOSE. INSTALLED PERMANENT REPAIR IAW SRM 54-04AD.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 64,165 hrs · 49,539 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEATS 11D AND 23D OF THE CABIN WERE INOPERATIVE. MX REPLACED THE LIGHT ASSEMBLIES AT BOTH LOCATIONS AND ALSO REPLACED THE WIRE HARNESS AT SEAT 23D. A SATISFACTORY FUNCTIONAL CHECK OF THE WAS ACCOMPLISHED.

Part: SKIN — CRACKED (BS 1437) · airframe 63,837 hrs · 49,308 cycles

FUSELAGE SKIN, BS 1437 STRINGERS 2 - 4L CRACKED. REPAIRED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,806 hrs · 49,292 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE OVERHEAD EMERGENCY LIGHTING IN THE COCKPIT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,665 hrs · 49,203 cycles

OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CABLE — BROKEN (TAILCONE) · airframe 60,679 hrs · 47,125 cycles

BROKEN STRANDS ON TAIL CONE RELEASE SYSTEM CONTROL CABLE STA 1510 CANT 08 O'CLOCK POSITION. REPLACED CABLE PER MM 53-53-00-501.

Part: RIB — CRACKED (RT WING) · airframe 60,679 hrs · 47,125 cycles

CRACK AND BENT RT WING L/E RIB AND RIB CLIP STA XRS=79. REPAIRED PER ERA 492340-14 REV ORG.

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 60,679 hrs · 47,125 cycles

CRACK ON STIFFENER AT STA 1442 AT VERT STAB L/E INTERNAL STRUCTURE. REPLACED STIFFENER PER DWG 9911889 REV F.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,679 hrs · 47,125 cycles

CRACK ON FRAME STA Y=1322 BTWN LONG 17LT. REPAIRED PER ERA 491696-14 REV ORG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,679 hrs · 47,125 cycles

CRACK ON FRAME STA 1322 AND LONG 17 RT. REPAIRED PER ERA 491696-14 REV ORG.

Part: PAN — CRACKED (CARGO DOOR) · airframe 60,679 hrs · 47,125 cycles

CRACK ON PAN FWD EDGE OF FWD CARGO COMPT DOOR STA 373 AND BEAM NR 5 AT C1. REPAIRED PER SRM 52-03D.

Part: TUBE — WORN (TAILCONE) · airframe 60,679 hrs · 47,125 cycles

WORN FUSE TUBE OF TAIL CONE RELEASE CABLE AT 5 O'CLOCK POS STA 1510 CANT. REPLACED CABLE.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 60,679 hrs · 47,125 cycles

CORROSION ON RT CUSP WEB FROM STA Y=610 TO Y=617, Y=625 TO Y=637, Y=680 TO Y=693 AND Y=695 TO Y=712 BTW X=-54 TO X=-60 AT CABIN FLOOR STRUCTURE UPPER AND LOWER SURFACE. REPLACED WEB.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,679 hrs · 47,125 cycles

SEVERAL DENTS ON EXTERNAL FUS SKIN FROM STA Y=89 TO Y=110 AND LONG PROJECTION 16 LT TO 17 LT. REPAIRED PER ERA 4917014-14 REV ORG.

Part: STRUCTURE — CORRODED (HORIZ STAB) · airframe 60,679 hrs · 47,125 cycles

CORROSION ON RT HORIZ STAB FWD UPPER PLATE BARREL NUT HOLE. REPAIRED PER ERA 491695-14 REV ORG AND AMR 0955165.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,679 hrs · 47,125 cycles

DENT ON FUSE SKIN STA 216 TO 262. REPAIRED PER SRM 53-04D.

Part: TUBE — WORN (TAILCONE) · airframe 60,679 hrs · 47,125 cycles

WORN FUSE TUBE OF TAIL CONE RELEASE CABLE BTWN 6 AND 7 O'CLOCK. REPLACED TUBE.

Part: FASTENER — CORRODED (TAILCONE) · airframe 60,679 hrs · 47,125 cycles

RUSTED HARDWARE ON TAIL CONE RELEASE SYSTEM CONTROL CABLE HARDWARE STA 1510 CANT. REPLACED HARDWARE.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,679 hrs · 47,125 cycles

MISSING ID TAG AND DAMAGE ON C-3 FUSE TRIPLER STA 1212 BTW L23R AND 26R ERA097886-14. DOUBLER AND TRIPLER WERE REMOVED AND REPLACED IAW ERA 097886-15, REV B.

Part: PAN — CRACKED (CARGO DOOR) · airframe 60,679 hrs · 47,125 cycles

CRACKED PAN ON SETTLEMENT AREA OF AFT STOP NR 3 AT FWD LOWER CARGO COMP DOOR. REPAIR PER 52-05D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,679 hrs · 47,125 cycles

CRACK ON FRAME 1485 CANT AT 11 O'CLOCK POS. DAMAGE REMOVED, DOUBLER AND FILLER INSTALLED IAW ERA 492351-14 REV ORIG.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 60,590 hrs · 47,072 cycles

DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY PATHWAY LIGHT AT ROW 35 D/E INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE HARNESS UNDER SEAT. REPLACED HARNESS PER MAINTENANCE MANUAL.OPERATIONAL CHECK WAS GOOD.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 60,550 hrs · 47,044 cycles

CORROSION ON RT MLG SUPPORT FITTING AT OUTBOARD LOWER ATTACHMENT STUD AREA. REPAIR PER ERA 491701-14 AND AMR0957358 REV 3.

Part: LANYARD — DISCONNECTED (R1 DOOR SLIDE) · airframe 60,506 hrs · 47,017 cycles

FLIGHT CREW REPORTED THAT DOOR 1R GIRT BAR LANYARD CAME LOOSE. MAINTENANCE RE-SECURED DOOR 1R GIRT BAR LANYARD. AIRCRAFT OKAY FOR SERVICE.

Part: HINGE FITTING — CORRODED · airframe 60,107 hrs · 46,792 cycles

VERTICAL TO HORIZ STAB HINGE PLATES CORROSION ERA 488232-14, REV ORIG REF NRS 14-17 AND FINAL ERA SIGNED ON NR 5.

Part: ATTACH FITTING — CORRODED (VERTICAL STAB) · airframe 60,107 hrs · 46,792 cycles

BUSHINGS CORRODED HORIZ STAB ATTACH INBD LT AND RT BUSHINGS AT TOPO OF VERT STAB REPAIRED IAW ERA 488232-14, REV ORIG.

Part: LANYARD — MISROUTED (R1 DOOR) · airframe 59,978 hrs · 46,710 cycles

DURING LINE CHECK MAINTENANCE FOUND R1 DOOR SLIDE LANYARD ROUTED WRONG WAY. MAINTENANCE RE-ROUTED CABLE PER MM 25-62-00. (2010-D1400) (DLM88103242)

Part: FUEL LINE — LEAKING (APU) · airframe 59,966 hrs · 46,701 cycles

A JET FUEL SMELL CAUSING EYE IRRITATION WAS REPORTED IN THE COCKPIT AND CABIN WHEN THE PACKS WERE OPERATED WITH ENGINE OR APU. MAINTENANCE FOUND AN APU FUEL LEAK AT LINE LEADING. (2010-D1386) (DLM88103222)

Part: SOCKET — DAMAGED (EMERGENCY LIGHTS) · airframe 59,521 hrs · 46,397 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHT AT 2C INOPERATIVE. MX REPLACED LIGHT BULB SOCKET ASSY. OPERATION OF LIGHT NOW CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,269 hrs · 45,557 cycles

FOUND EMERGENCY LIGHT INOP AT SEAT 3 CD. REMOVED AND REPLACED EMERGENCY PATH LIGHT ASSY AT SEAT 3 CD, CHECKS OK.

Part: SKIN — DAMAGED (FS 560-655) · airframe 54,934 hrs · 43,400 cycles

LIGHTNING STRIKES ON WINDOW BELT AT WINDOWS 19L, 20L, AND 23L FS 560-655.

Part: SKIN — CRACKED (AILERON) · airframe 53,994 hrs · 42,755 cycles

DISBOND IN SKIN AND CRACK FOUND IN SPAR ON AILERON DURING SHOP VISIT. REPAIRED PER DELTA ERA 467537-14, REV A.

Part: DUCT — CONTAMINATED (AFT) · airframe 50,227 hrs · 40,309 cycles

AIRBORNE RETURN FOR SMOKE/FUMES IN CABIN. FIRST OFFICERS AFT LAV SMOKE DETECTOR ACTIVATED. MTC IN WORK DOING DUCT BURNOUT AND WASHING APU INLET. REMOVED AND REPLACED COALESCER BAGS CLEANED RESIDUAL OIL FROM APU INLET PERFORM FULL DUCT BURNOUT PER OPN 5089. NO SMOKE OR ODORS. REMOVED AND REPLACED COALESCER BAGS.

Part: OIL CAP — LEAKING (APU) · airframe 50,226 hrs · 40,308 cycles

DURING T/O, STRONG ODOR AND HAZE IN AFT CABIN. FOUND APU OIL CAP LEAKING AND APU INGESTED OIL. FOUND OIL LEAKING PAST OIL FILLER CAP SEAL. REPLACED CAP AND SEAL SERVICED TO FULL. CLEANED AREA LEAK CKS GOOD. REMOVED AND REPLACED COALESCER BAGS AND PERFORMED FULL DUCT BURN OUT PER OPN 5089.

Part: PUMP — FAILED (NR 2 ENGINE) · airframe 45,488 hrs · 36,812 cycles

ON T/O ROLL THE NR 2 ENGINE ROLL BACK AND SHUT DOWN. MTC INSPECTED THE INTAKE, EXHAUST AND FUEL CONTROL LINKAGE, NO TROUBLE FOUND. ENGINE WILL NOT START, NO FUEL FLOW. REPLACED FUEL PUMP AND CONTROL.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,825 hrs · 36,345 cycles

THE FUSELAGE SKIN WAS FOUND CORRODED NEAR AN ANTENNA CUTOUT IN THE BELLY SKIN AT FS 725 AND STRINGER 30. THE CORROSION DAMAGE WAS REMOVED WITH A 12 X 7.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 093726-14, REV A.

Part: VENT — STUCK (TAIL) · airframe 44,281 hrs · 35,923 cycles

TAIL COMPT HIGH LIGHT. ABORTED T/O 115 - 120 KTS. FOUND LEFT TAIL COMPARTMENT EXHAUST VENT FLAPPER STUCK CLOSED. FREED SAME.

Part: STRUT — DISCHARGED (NLG) · airframe 43,749 hrs · 35,525 cycles

ON DEPT WHEN GEAR HANDLE RAISED ALL GEAR IND IN TRANSIT AND MAIN GEAR WENT UP AND LOCKED EXCEPT NOSE GEAR STILL IND UNSAFE. GEAR DOOR OPEN LIGHT WAS OUT. REPLACED UP/LOCK SENSOR.

Part: DUCT — RUPTURED (NR 2 ENGINE) · airframe 43,299 hrs · 35,224 cycles

TEN MINUTES AFTER TAKEOFF GOT RIGHT ENGINE FIRE WARNING WITH BELLS, AURAL WARNING, AND LIGHT IN HANDLE. PER PROCEDURE REDUCED THROTTLE TO IDLE ALL INDICATION CEASED AT 1.30 EPR. OTHER INSTRUMENTS NORMAL, NO VIBRATIONS. REPLACED 13TH STAGE ANTI-ICE DUCT ON RIGHT ENGINE.

Part: SWITCH — MALFUNCTIONED (NLG) · airframe 39,172 hrs · 32,370 cycles

ON DEPT AFTER NORMAL RETRACTION RED NOSE GEAR LIGHT CAME ON. FOLLOWED CK LIST PROCEDURE TO RECYCLE, CAME DOWN NORMAL. ATTEMPTED TO RETRACT. NOSE GEAR REMAINED DOWN AND LOCKED. HANDLE PLACED BACK DOWN. ALL GEAR DOWN AND LOCKED. RETURNED TO CVG. REPLACED S1-412 INTERLOCK SW AND D1-32 PROX SW. JACKED NOSE AND CYCLED GEAR. GEAR IND NORMAL. LOWERED A/C AND REMOVED JACK PAD.

Part: ATTACH ANGLE — CRACKED (AFT FUSELAGE) · airframe 39,127 hrs · 32,333 cycles

THE LH FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE WAS FOUND CRACKED AT APPROXIMATELY STA 1474 CANT. THE CRACK WAS 0.5" LONG AND TYPICAL AS THAT SHOWN IN MD-88 SRM 53-05, FIG. 23. THE ANGLE IS MADE FROM 0.080" THICK SOLUTION HEAD TREATED A-286 CRES MATERIAL. THE CRACK WAS TRIMMED OUT AND THE ANGLE REINFORCED.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 36,881 hrs · 30,671 cycles

RT ENG HYD PUMP PRESS LINE LEAKING IN AFT BAG BIN BEHIND RT AFT BULKHEAD. INSTALLED NEW HYD LINE, RAN NR 2 ENG PER PFHB. NO LEAKS, ALL CHECKS NORMAL PER M/M.

Part: SLIDE — DAMAGED (SERVICE DOOR) · airframe 34,843 hrs · 29,133 cycles

DOOR 1R GIRT BAR DAMAGED. FOUND SLIDE PACK COMING APART. REPLACED SLIDE PACK ASSY.

Part: BRAKE — OVERTEMP (MLG) · airframe 34,394 hrs · 28,798 cycles

EXCESSIVE BRAKE CHATTER. DEGRADES STOPPING. ALLOWED BRAKES TO COOL FROM 225. OK FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2)

ON CLIMB OUT FROM JFK RT. ENGINE OIL PRESS WENT TO A 75 PSI OIL TEMP WAS STEADY OIL QTY INDICATION WAS 1-2 QTS HIGHER THAN ON GROUND. REDUCTION IN POWER TO IDLE RETURNED OIL PRESS TO NORMAL. FLIGHT CLXD. MAIN OIL SCREEN CHECKED OK. OIL LINE TEMP DECALS CKD OK. WILL ACCOMPLISH BREATHER PRESSURE CHECK WHEN AIRPORT NOISE CURFEW LIFTS AT 0630.

Part: SPAR CAP — OVERSIZED HOLES (LT/RT WING)

DURING INSTALLATION OF THE UPPER SURFACE HEATER BLANKETS FOR THE LEFT AND RIGHT WING THE HOLES COMMON TO THE UPPER CAP OF THE FRONT SPAR WERE NOT COLD WORKED. ERA 333738-14 ADDRESSED THE DISCREPANCY.

Part: SKIN — DENTED (BS 218-229)

A DENT WAS FOUND IN THE FUSELAGE SKIN BETWEEN FS 218 AND 229 AND BETWEEN LONGERONS 18L AND 19L. THE DAMAGE WAS REMOVED WITH A 11 X 6 CUTOUT AND REPAIRED PER ERA 333708-14 AT HMV.

Part: STRUT — REQD SERVICE (NLG)

AFTER GEAR RETRACTION NOSE GEAR RED UNSAFE LIGHT ILLUMINATED. LOWERED GEAR THEN RAISED, AGAIN THE NOSE GEAR RED UNSAFE LIGHT STAYED ILLUMINATED ACCOMPANIED BY AN AIR NOISE LIKE THE DOOR WAS POSSIBLY OPEN. RESERVICED AND GREASED NOSE STRUT, SWUNG GEAR AND IND NORMAL.

Part: COMP BLADE — DAMAGED (NR 1 ENGINE)

FLT ATTN IN AFT OF ACFT REPORTED LOUD EXCESSIVE NOISE FROM ENGINES. PERFORMED BORESCOPE ON NR 1 ENGINE 6TH AND 7TH STAGE COMPRESSOR DUE TO N1 FAN BLADE DAMAGE FOUND. DAMAGE TO 7TH STAGE OUT OF M/M LIMITS. REPLACED ENGINE.

Part: BULB — FAILED (CABIN)

ONE RED LIGHT OUT ON EMERGENCY TRACK LIGHTING F/O SIDE, ACROSS FROM AFT GALLEY. REPLACED ONE LIGHT BULB AND REPAIRED DAMAGED WIRING.

Part: LOCK SWITCH — FAILED (NLG)

AFTER GEAR RETRACTION ON TAKEOFF, PBI NOSE GEAR UNSAFE RED INDICATOR LIGHT REMAINED ON. CYCLED GEAR, NO HELP. C/B P38 PULLED TO SILENCE WARNING. REPLACED NOSE LOCK SWITCH, CYCLED GEAR AND OPERATION NORMAL.

Part: LANYARD — BROKEN (L2 DOOR)

ON PREFLIGHT, L-2 DOOR SLIDE LANYARD WIRE FOUND BROKEN. REPLACED LANYARD.

Part: ACTUATOR — LEAKING (RT MLG)

AT FLT LEVEL 350 NOTICED RIGHT HYD SYS QTY 6, SHUTDOWN RIGHT HYDRAULIC PUMP. WHEN PUMP TURNED BACK ON, THERE WAS NO SYS PRESS. FOUND RT MAIN GEAR RETRACT ACTUATOR CYLINDER LEAKING. REPLACED CYLINDER, OPERATION NORMAL.