N964DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,253 hrs · 56,988 cycles

EMERGENCY PATH LIGHTS SEATS 13-23 AND 31-36 INOP. R/R BATTERY PACK B5-211, BATTERY AND CHARGER B5-103 AND BATTERY AND CHARGER B5-212. OPS CHECK OK. (LP6658420)

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 76,108 hrs · 56,849 cycles

LAVATORY SMOKE DETECTION SYSTEMS LEFT AFT LAV SMOKE DET INOP. REPLACED NEW SMOKE DETECTOR, OP'S CK OK AND OK FOR SVC, MEL/PLACARD REMOVED. (LP1316338)

Part: UNKNOWN — ODOR (CABIN) · airframe 76,095 hrs · 56,835 cycles

BURNING RUBBER SMELL IN AFT CABIN CLIMBING THROUGH 7000FT LAST ABOUT 5 MIN. FWD FLIGHT ATTENDANT AND COCKPIT COULD NOT SMELL IT . NO ABNORMAL INDICATIONS IN COCKPIT. INSPECTED APU, HEAT EXCHANGERS AND RECIRCULATION FAN. NO DEFECTS NOTED. PERFORMED FULL DUCT BURNOUT PER WORKCARD 7100-2619. NO ODOR PRESENT .

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 76,052 hrs · 56,791 cycles

EMERGENCY LIGHTS INOP AT SEAT ROW 13DE. FOUND BROKEN HARNESS, REPLACED HARNESS. OPS CK GOOD REF MD88 AMM 33-52. (LP6584696)

Part: DOOR FRAME — CRACKED (RT MLG) · airframe 75,701 hrs · 56,439 cycles

R/H FWD GEAR DOOR FRAME CRACKED. REPLACED FRAME PER ERA 580223-14 REV. ORG. OPS CHECK RT GEAR DOOR GOOD, OK FOR SVC. QC OK TO CLOSE MON. (LP6028702)

Part: HYDRAULIC LINE — LOOSE (HYDRAULIC SYS) · airframe 75,510 hrs · 56,266 cycles

ON TAXI IN AFTER ENGINE SHUTDOWN AND APU AIR ON FA AND FO SMELL FUMES ON T.O. SMELLED FUMES BUT THEY DISSIPATED QUICKLY APU WAS OFF. FOUND LINE LEAKING ON LEFT ACCUMULATOR PRESSURE SWITCH. TIGHTENED LINES NO LEAKS NOTED CLEANED AREA NEEDS DUCT BURN. WASHED AFT EXTERIOR SECTION AND APU INTAKE. REPLACED BLOWN APU SURGE VALVE COUPLING PER AMM 49-50. C/W NO GO ODI PREVENTION W/C'S 4950-2215, 2120-2367 AND 2170-4139. MCC CONTACTED. (LP4695094)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,391 hrs · 56,158 cycles

EMERGENCY LIGHTS FOR ROWS 13-23 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY REF MD88 WDM 33-51-14. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4695023)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,391 hrs · 56,158 cycles

EMERGENCY LIGHTS FOR ROW 31-36 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY PER WDM 33-51-14 MD88. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4695022)

Part: LENS — MISSING (LT WING) · airframe 74,629 hrs · 55,519 cycles

LEFT WING TIP AFT POSITION LIGHT COVER MISSING. REMOVED & REPLACED LT AFT POS LIGHT ASSY PER AMM 33-43. OPS CHK GOOD.

Part: MOTOR — FAILED (PRIMARY TRIM) · airframe 73,449 hrs · 54,490 cycles

PRIMARY STABILIZER TRIM INOPERATIVE PASSING 10K AT 280KTS. THE CREW CHOSE TO MAINTAIN 280KTS DURING FLIGHT AND PERFORMED THE QRH PROCEDURES FOR PRIMARY TRIM INOPERATIVE. THE ALTERNATE TRIM OPERATED NORMALLY. AN EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE PRIMARY STABILIZER TRIM MOTOR IAW AMM AND RETURNED THE AIRCRAFT BACK TO SERVICE.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 73,379 hrs · 54,432 cycles

1L SLIDE PIN SLID OUT. NOT VISIBLE IN INSPECTION WINDOW. REM/REPL L-1 SLIDE ASSY IAW WC 2561-4964.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,921 hrs · 54,053 cycles

FUSELAGE SKIN BULGING AT THE BOTTOM END OF THE AFT LAVATORY SERVICE PANEL CUTOUT. POSSIBLE EVIDENCE OF CORROSION.

Part: PANEL — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 72,921 hrs · 54,053 cycles

INNER SURFACE OF FORWARD LAV SERVICE PANEL CORRODED- MARKED. REPLACED DOOR ASSY REF SRM 51-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,915 hrs · 54,046 cycles

EMERGENCY OVERHEAD LIGHTS INOP ROWS 10-14. REPLACED BATTERIES AT BATTERY PACK FOR EMERGENCY OVERHEAD LIGHTS ROW10-14 PER AMM 33-55.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,048 hrs · 53,362 cycles

SEAT 23D EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT AT 23D OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,536 hrs · 52,939 cycles

ROWS 18D AND 32D. AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LIGHT ASSY. OPS NORMAL. OK FOR SERVICE.

Part: CAP — DAMAGED (LT WING) · airframe 71,221 hrs · 52,670 cycles

LEFT WING L/E END CAP PANEL DAMAGED. COMPLIED WITH EA 413193-14MA.

Part: PANEL — DAMAGED (LT WING) · airframe 71,221 hrs · 52,670 cycles

LH WING LOWER SURFACE TE PANEL XW 550 DAMAGED. COMPLIED WITH PRI 556441-14 REVISION O AND ERA 556441-14, REV ORIGINAL.

Part: SKIN — UNKNOWN (LT WING) · airframe 71,221 hrs · 52,670 cycles

LEFT WING FIXED LEADING EDGE, LOWER WING SKIN. REPAIRED IAW ER/A 561246, REV C. COMPLIED WITH PRI 561246-14 REV C, REVISION O, REVISION 1, REVISION 2 AND ERA 561246-14, REV C, SECTION V WHICH CONSTITUTES A PERMANENT REPAIR.

Part: SPAR — BENT (LT WING) · airframe 72,921 hrs · 54,053 cycles

LT WING FRONT SPAR AT XFS=600 BENT LOWER CHORD.

Part: WEB — BENT (LT WING) · airframe 71,221 hrs · 52,670 cycles

LEFT WING INTERNAL WEB XW 536 FWD SPAR CAP BENT BENT UPWARDS .0675 AT HIGHEST POINT AT L/E LANDING, 19.5 INCHES IN LENGTH. COMPLIED WITH PRI 556442-14 REV O AND ERA 556442-14, REV ORIGINAL SECTION I.

Part: SKIN — DAMAGED (LT WING) · airframe 71,221 hrs · 52,670 cycles

LT WING O/B LEADING EDGE BEHIND NR 5 SLAT DAMAGED AND DENT ON LOWER WING SURFACE. C/W SECT 1 AND 2 OF ERA 561246-14 REV ORG.

Part: CABLE — FRAYED (TAILCONE) · airframe 70,285 hrs · 51,928 cycles

TAILCONE CABLE FRAYED. REPLACED TAILCONE CABLE IAW AMM 20-10-01.

Part: FASTENER — BROKEN (TAILCONE) · airframe 70,285 hrs · 51,928 cycles

TAILCONE SLIDE COVER SNAP IS BROKEN. DISCONNECTED DEPLOY LANYARD, REMOVED AND REPLACED SNAP, RECONNECTED DEPLOY LANYARD, O.K. FOR SERVICE. REQUIRED INSPECTION COMPLETED.

Part: RIVET — LOOSE (TAILCONE) · airframe 70,285 hrs · 51,928 cycles

TAILCONE UPPER LEFT LOCK BRACKET PULLING LOOSE FROM TAIL CONE. REMOVED LOOSE RIVETS AND INSTALLED NEW RIVETS PER MD88 SRM51-30-2.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 70,089 hrs · 51,785 cycles

OVERHEAD EMERGENCY LIGHTS AT THE L1 DOOR ARE INOPERATIVE. FOUND WIRE L767A22 CONNECTED TO GROUND OF NR 4 BULB AT FWD ATT WORK LIGHT, ENTRY LIGHT PANEL L2-155. FOUND THE NR 2 BULB GROUND JUMPED AC GROUND. RECONFIGURED IAW WDM, REMOVED JUMPER. SYSTEM OPS CHECKED GOOD IAW AMM 33-20.

Part: RESERVOIR — DEFECTIVE (HYDRAULIC SYS) · airframe 69,842 hrs · 51,615 cycles

AFTER TAKE-OFF BOTH LEFT AND RIGHT HYDRAULIC SYSTEMS FAILED. BOTH SYSTEMS CAME UP NORMAL ON DEPARTURE. AFTER RAISING THE LANDING GEAR AND TURNING OFF THE AUXILIARY AND TRANSFER HYDRAULIC PUMPS, BOTH SYSTEM PRESSURES REDUCED TO ZERO. QUANTITY LEVEL WAS 19L AND 11R. THE NOGO ODI WORK CARD 2932 WAS PERFORMED. MAINTENANCE REPLACED THE LEFT HYDRAULIC RESERVOIR, THE LEFT ENGINE HYDRAULIC PUMP, AND THE CASE DRAIN FILTER PER AMM 29-10. THE LANDING GEAR WAS CYCLED PER AMM 07-11 AND ALL CHECKED OK. NO AIR WAS FOUND IN SYSTEM. THE SYSTEM WAS BLED DOWN AND AN ENGINE RUN WAS PERFORMED WITH NO DEFECTS.

Part: DUCT — BLOWN (NR 1 ENGINE) · airframe 69,629 hrs · 51,474 cycles

PERFORMED AN AIR TURN BACK TO PHL DUE TO NUMBER 1 ENGINE FIRE INDICATION SHORTLY AFTER TAKEOFF. MAINTENANCE FOUND THE NOSE COWL ANTI-ICE DUCT BLOWN. MAINTENANCE REPLACED DAMAGED ANTI-ICE DUCTS AND UPPER COWL DUE TO HEAT DAMAGE. AN ENGINE RUN WAS PERFORMED AND THE ANTI-ICE CHECKED OKAY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 68,165 hrs · 50,431 cycles

AFT CARGO ENTRY LOWER JAMB CORRODED AT FWD AND AFT ENDS. DISCREPANT AREA REF ER/A 546990-14, REV O.

Part: COVER — UNSECURE (L1 DOOR) · airframe 68,165 hrs · 50,431 cycles

DOOR L1 SLIDE COVER NOT SECURED. R & R SLIDE.

Part: SKIN — DELAMINATED (LT ELEVATOR TAB) · airframe 68,165 hrs · 50,431 cycles

LT ELEVATOR CONTROL TAB UPPER SURFACE HAS .7500" SPOT OF DELAMINATION, BULGE, APPROXIMATELY 44" OTBD OF INBD END, 1" FWD OF T/E. REMOVED AND INSTALLED LT ELEVATOR CONTROL TAB IAW AMDS 2730-4634.

Part: SKIN — CORRODED (BS 588) · corrosion level 2 · airframe 67,631 hrs · 50,057 cycles

CORROSION DAMAGE ON SKIN AT BS 588 BETWEEN L30 AND L29. DUE PRI 545426-14, REV 6. DUE ERA 545426-14, REV ORIGINAL SECTION I PERM REPAIR. C/W PRI 545426-14, REV 6, 116607. C/W ERA 545426-14 REV ORIGINAL SECTION I PERM REPAIR. COMPARED PRI 545426-14, REV 6 AND ERA 545426-14, REV. ORIGINAL SECT I, PERM REPAIR, WITH NO CHANGES NOTED.

Part: SKIN — DAMAGED (BS 580) · corrosion level 2 · airframe 67,631 hrs · 50,057 cycles

ON WALK AROUND FOUND A BLISTER ON BOTTOM OF FUSELAGE AT APPROXIMATELY 580. THE SKIN IS ALSO CRACKED BETWEEN 2 RIVET HOLES. C/W REPAIR ON ERA 545426-14, REV ORIG, SECT. I, PERM REPAIR. COMPARED PRI 545426-14, REV 6 TO ERA 545426-14, ORIG, NO DIFFERENCES FOUND.

Part: UNKNOWN — UNKNOWN (NLG) · airframe 67,620 hrs · 50,049 cycles

THE CREW REPORTED THAT THE NLG MADE EXCESSIVE NOISE AFTER TAKEOFF WITH THE GEAR RETRACTED. THE FLIGHT WAS RETURNED. MAINTENANCE FOUND THAT THE RT NOSE GEAR DOOR WAS OPEN. INSPECTED DOOR AREA. NO DEFECTS NOTED. CLOSED DOOR. COMPLIED WITH MCC LOG TO SWING NOSE GEAR AND CHECK DOOR OPERATION IAW AMM 32-00-00 101. NO DEFECTS NOTED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 66,524 hrs · 49,274 cycles

MAINTENACE FOUND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. A BROKEN WIRE WAS FOUND AND REPAIRED AT SEAT 3D. OPS CHECKED OK.

Part: DOOR FRAME — CRACKED (RT MLG WW) · airframe 66,238 hrs · 49,049 cycles

ON WALK-AROUND FOUND RT MLG WW DOOR FWD FRAME CRACKED. REPAIRED IAW ERA 538458-14, REV ORIG.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 64,983 hrs · 48,209 cycles

MAINTENANCE FOUND THE EMERGENCY EXIT PATH LIGHT AT 20D INOPERATIVE MAINTENANCE REPLACED SEAT HARNESS AT SEAT 20D. OPS CKS GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 64,601 hrs · 47,930 cycles

MAINTENANCE FOUND RT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND THE DISCONNECT FOR THE LIGHT BEHIND THE WALL PANEL DISCONNECTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,353 hrs · 47,770 cycles

BOTH FORWARD OVERWING AUXILIARY EXIT LIGHTS INOPERATIVE. R & R BATTERY PACKS IAW WDM 33-51-12. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,876 hrs · 46,648 cycles

DURING A FUNCTIONAL CHECK FLIGHT, MAINTENANCE FOUND THAT TWO OVERHEAD EMERGENCY FLOOD LIGHTS AT SEAT 36 WERE INOPERATIVE. MAINTENANCE REPLACED THE TWO EMERGENCY LIGHTS AND THE LIGHTS RETURNED TO AN OPERATIONAL STATE.

Part: BUSHING — DAMAGED (RT WING) · airframe 62,867 hrs · 46,640 cycles

RT WING HEATER BLANKET T/E BUSHINGS, WERE FOUND ELOGATED AFTER HEATER PANEL REWORK. REPAIR WAS PERFORMED IAW ERA 525553-14AD, REV A.

Part: RIB — DAMAGED (HORIZONTAL STAB) · airframe 62,865 hrs · 46,639 cycles

CORROSION AND SCRATCHES WERE FOUND ON RIB. DAMAGE REMOVED IAW ER/A 524668-14, REV ORIG.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION ON RT HORIZONTAL STABILIZER. CORROSION REMOVED IAW SRM 55-03-D.

Part: PLATE — DAMAGED (HORIZONTAL STAB) · airframe 62,865 hrs · 46,639 cycles

SCRATCHES ON F PLATE BETWEEN HORIZONTAL STABILIZER CENTER BOX AND RT HORIZONTAL STABILIZER XH=-27.234. REPAIRED WITH A BUSHINGS IAW ER/A 524668-14.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 62,865 hrs · 46,639 cycles

SCRATCHES AND CORROSION ON RT HORIZONTAL STABILIZER XH=-27.234". SCRATCHES AND CORROSION REPAIRED ER/A 524668-14, REV ORIG AND ATI-88-14-047, REV 2.

Part: SKIN — CRACKED (BS 1418) · airframe 62,865 hrs · 46,639 cycles

TWO CRACKS WERE FOUND ON FUSELAGE SKIN BS 1418 BETWEEN LONGERONS 1 AND 2 RT. REPAIR WAS ACCOMPLISHED IAW ER/A 524531-14, AD REV ORIGINAL AND ETI -88-14-035, REV 4.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION ON HORIZONTAL STABILIZER LOWER FWD SECTION XH=-27.234. REPAIRED WITH A BUSHING IAW SRM 55-03D.

Part: DOOR FRAME — CRACKED (BS 423) · airframe 62,865 hrs · 46,639 cycles

CRACK ON INTERNAL DOUBLER AT LOWER AFT DOOR FRAME CORNER OF THE FWD CARGO BAY BS 423.5 BETWEEN LONGERONS 27-28 RT. REPAIRED IAW ER/A 521210-14AD, REV ORIGINAL AND ETI 88-14-032, REV 4.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

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

Part: DOUBLER — CRACKED (DOOR FRAME) · airframe 62,865 hrs · 46,639 cycles

CRACK ON INTERNAL DOUBLER AT LOWER AFT DOOR JAMB CORNER OF THE FWD CARGO COMPARTMENT AT FS, Y=423.5 BETWEEN LONGS 27-28RH, SM, ZONE 051, CARD 03. SUMMARY: REPAIR WAS ACCOMPLISHED IAW ER/A 521210-14AD, REV ORIGINAL AND ETI-88-14-032, REV 4. THIS REPAIR IS APPROVED AS TIME-LIMITED UNTIL DAMAGE TOLERANCE EVACUATION IS ACCOMPLISHED WITHIN 24 MONTHS, FRAME AS REQUIRED BY 14 CFR 25.571 AND 14 CFR 26 SUB PART IAW ER/A 521210-14AD, REV ORIGINAL SECTION II. RII COMPLETED, ASSOCIATED ER/A 00-521210 ADDED FOR AC 0964.

Part: STRINGER — DAMAGED (LT WING) · airframe 62,865 hrs · 46,639 cycles

CRACK AROUND THE FASTENER ON MAIN STRINGER 11 AT XRS=168 ON THE FWD FACE OF THE VERTICAL FLANGE AT LT WING. FITTING AND ANGLES WERE REMOVED IAW SRM 51-30-2, 51-30-5, DAMAGE ON STRINGER 11 WAS REMOVED IAW DWG SR09570100, REV A, NEW SECTION OF STRINGER 11 AND REPAIR PARTS WERE DRILLED IAW DWG SR04570100, REV A, COLD WORK WAS DONE IAW DWG SR 09570100, REV A, NEW SECTION AND REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14, 21, AND DWG SR 09570100, REVA AND ER/A 524676-14 AD REV ORIG, AREA WAS PAINTED AND SEALANT WAS APPLIED IAW DWG SR09570100, REV A AND SRM 51-20-. MAINTENACE INSPECTION REQUIREMENTS AS STATED ON SR09570100, ZONE15 INITIAL INSPECTION THRESHOLD 60,000, CYCLES AFTER SECTION 1 REPAIR, RII COMPLETED. ASSOCIATED ER/A 00-524676 ADDED.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 62,865 hrs · 46,639 cycles

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

Part: HINGE FITTING — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION FOUND ON FLAP HINGE FITTING, XRS=267 RT WING T/E. HINGE REPLACED IAW AMM 57-40-01 AND 27-50-02 AND HINGE BRACKET AND ACTUATOR REMOVED AND INSTALLED IAW AMM 27-52-02, LEAK CHECKED ACTUATOR WAS PERFORMED, NO LEAKS FOUND.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION ON COUNTERSINK OF FUEL TANK ACCESS PANEL 1307C. CORROSION REMOVED IAW SRM 51-22-2A. FOUND OUT OF LIMITS IAW SRM 51-22-2A, ACCESS PANEL WAS REPLACED.

Part: SKIN — CORRODED (BS 765-807) · airframe 62,865 hrs · 46,639 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET PANEL BETWEEN, BS 765 - 807 LONGERONS 27-30R. CORROSION REMOVED IAW SRM 51-10-3. (UT) WAS ACCOMPLISHED AND FOUND WITHIN LIMITS IAW SRM 53-01, PAR 57B (2) (A).

Part: ACCESS PANEL — CORRODED (WING) · airframe 69,195 hrs · 51,185 cycles

FUEL TANK ACCESS PANEL 1478C COUNTERSINKS CORRODED. REPAIRED THE ACCESS PANEL.

Part: WEB — CORRODED (BS 1155-1212) · airframe 69,195 hrs · 51,185 cycles

AFT CARGO LOWER DOOR FRAME WEB BS 1155-1212, BETWEEN LONGERONS 27 - 29R, CORRODED OUT OF LIMITS. THE WEB WAS REPLACED.

Part: SKIN — CORRODED (BS 759-765) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER BETWEEN BS 759.5 AND 765 BETWEEN LONGERONS 27 - 28R, MID CARGO COMPARTMENT. DOUBLER REMOVED, NEW DOUBLER WAS FABRICATED AND WAS TREATED PAINTED DOUBLER WAS INSTALLED IAW SRM 53-04, FIG 57.

Part: LONGERON — CRACKED (BS 1418) · airframe 62,865 hrs · 46,639 cycles

CRACKED LONGERON 2L BS 1418 AT AFT ACCESSORY COMPARTMENT. LONGERON SECTION WAS REMOVED IAW SRM 51-30-2 AND 51-30-5, NEW SECTION OF LONGERON AND SPLICE WERE FABRICATED AND DRILLED IAW SRM 53-02, FIG 18, NEW LONGERON SECTION AND SPLICE WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14. REPAIR PARTS WERE INSTALLED IAW SRM 53-02, FIG 18.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION RT HORIZONTAL STABILIZER LOWER AFT SECTION XH=27.234. CORROSION REMOVED AND REPAIRED IAW SRM 55-03D.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

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

Part: CUSP WEB — CORRODED (BS 1174-1250) · airframe 69,195 hrs · 51,185 cycles

LEFT CUSP WEB BS 1174-1250 X 54 TO 60 CORRODED. REPAIRED THE CUSP WEB.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION ON COUNTERSINK OF FUEL TANK ACCESS PANEL 1409C. CORROSION REMOVED IAW SRM 51-22-2A. FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION ON COUNTERSINK OF FUEL TANK ACCESS PANEL 1303C. CORROSION REMOVED IAW SRM 51-22-2A. FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL WAS REPLACED.

Part: FLOOR SUPPORT — CORRODED (BS 160-200) · airframe 69,195 hrs · 51,185 cycles

CORRODED FLOOR SUPPORT BS 160-200 X 7 TO -7. A NEW FLOOR SUPPORT INSTALLED.

Part: CUSP WEB — CORRODED (BS 864-886) · airframe 69,195 hrs · 51,185 cycles

PREVIOUS CUSP WEB REPAIR DOUBLER CORRODED. BS 864 - 886 BETWEEN X -54 TO -60. REPLACEMENT REPAIR FABRICATED AND INSTALLED.

Part: CUSP WEB — CORRODED (BS 1168) · airframe 69,195 hrs · 51,185 cycles

LEFT CUSP WEB BS 1168 X 54 - 60, FITTING CORRODED, REPLACED THE FITTING.

Part: TEE FITTING — CORRODED (BS 1170) · airframe 69,195 hrs · 51,185 cycles

LEFT CUSP WEB TEE FITTING CORRODED BEYOND LIMITS, BS 1170 BETWEEN X 54 - 60. A NEW TEE FITTING WAS INSTALLED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

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

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

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

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION WAS FOUND ON COUNTERSINKS OF FUEL TANK ACCESS PANEL 1470C. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL WAS REMOVED AND REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION FOUND ON COUNTERSINKS OF FUEL TANK ACCESS PANEL 1371C. CORROSION REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS IAW SRM 51-22-2A . ACCESS PANEL REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION FOUND ON COUNTERSINKS OF FUEL TANK ACCESS PANEL 1464C. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL REMOVED AND REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

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

Part: CUSP WEB — CORRODED (BS 886-905) · airframe 69,195 hrs · 51,185 cycles

PREVIOUS CUSP WEB REPAIR CORRODED, BS 886 - 905, X -54 TO -60. REPLACED THE REPAIR. FABRICATED AND INSTALLED. (LP# 1402161)

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION FOUND ON COUNTERSINKS OF FUEL TANK ACCESS PANEL 1363C. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM. ACCESS PANEL REPLACED AND REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION FOUND ON COUNTERSINK OF FUEL TANK ACCESS PANEL1367C. CORROSION REMOVED IAW SRM 51-22-2AAND FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL REPLACED AND REPLACED.

Part: CUSP WEB — CORRODED (BS 897-905) · airframe 69,195 hrs · 51,185 cycles

CUSP WEB CORRODED BS 897 - 905, X 54 - 60, REPAIR FABRICATED AND INSTALLED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION FOUND ON COUNTERSINK OF FUEL TANK ACCESS PANEL 1335C. CORROSION REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL REPLACED AND INSTALLED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION FOUND ON COUNTERSINK OF FUEL TANK ACCESS PANEL 1311C. CORROSION REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL WAS REPLACED AND REPLACED.

Part: LONGERON — CRACKED (BS 522) · airframe 62,865 hrs · 46,639 cycles

CRACK ON LONGERON 4R BS 522. CRACKED LONGERON WAS TRIMED AND NEW SECTION OF LONGERON INSTALLED IAW SRM 51-10-3, PAR 14-21 AND SRM 53-02, FIG 18. RII COMPLETED.

Part: FLOORBEAM — CORRODED (BS 1338) · airframe 69,195 hrs · 51,185 cycles

FLOORBEAM CORRODED BS 1338, X 18-54. UPPER CAP OF BEAM REPLACED.

Part: CUSP WEB — CORRODED (BS 636-655) · airframe 69,195 hrs · 51,185 cycles

CORROSION ON CUSP WEB PREVIUS REPAIR DOUBLER BS 636 - 655 BETWEEN X 54 - 60. PREVIOUS DOUBLER REPLACED.

Part: ANGLE — CORRODED (BS 200) · airframe 62,865 hrs · 46,639 cycles

CORROSION ON CUSP ANGLE BETWEEN BS 200 X=-58. CUSP ANGLE REPAIRED IAW SRM 53-05, FIG 55 AND ER/A 521188-14 MA REV ORIG.

Part: CUSP WEB — CORRODED (BS 446-465) · airframe 69,195 hrs · 51,185 cycles

CUSP WEB CORRODED, BS 446 - 465 X 54 TO 60. REPAIRED IAW SRM.

Part: CUSP WEB — CORRODED (BS 905-946) · airframe 69,195 hrs · 51,185 cycles

LEFT CUSP WEB, UPPER SURFACE CORRODED, BS 905 - 918 & 941 - 946 X 54-60. A REPAIR WAS FABRICATED AND REPLACED.

Part: LONGERON — CRACKED (BS 160) · airframe 62,865 hrs · 46,639 cycles

CRACK ON LONGERON 2L, BS 160. REMOVED SECTION OF LONGERON, NEW LONGERON SPLICES ADJUSTED AND DRILLED IAW SRM 51-30-2, 51-30-5, 51-10-3, PAR 14 AND 21 AND 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 541) · airframe 62,865 hrs · 46,639 cycles

CRACK ON LONGERON 4 LT BS 541. DAMAGED SECTION LONGERON WAS REMOVED, NEW SECTION AND SPLICES DRILLED AND AJUSTED, LONGERON AND SPLICES INSTALLED IAW SRM 53-02, FIG 18.

Part: CUSP WEB — CORRODED (BS 433-437) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION ON LT CUSP WEB, BS 433-437, BETWEEN X=54 AND X=60. CORROSION REMOVED IAW SRM 51-10-3, PAR 26, DAMAGE WAS REMOVED IAW SRM 53-05, FIG 131A-14, SHEET 1. REPAIR FABRICATED, TREATED, AND PAINTED IAW SRM 53-05, FIG 131A-14 AND SRM 51-10-3, PAR 14-21. REPAIR INSTALLED IAW SRM 53-05, FIG 131A-14.

Part: CUSP WEB — CORRODED (BS 370-377) · airframe 69,195 hrs · 51,185 cycles

CUSP WEB CORRODED, BS 370-377, X -54 AND X -60. DAMAGE REMOVED AND REPAIRED.

Part: WEB — DAMAGED (BS 218-224) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION AND BEND ON WEB BS 218-224 BETWEEN X -44 TO X -60. WEB REPLACED AND INSTALLED WITH NRC 20000005590.

Part: CUSP WEB — CORRODED (BS 446-465) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BETWEEN BS 446-465 X -54 TO X -60. DAMAGE REMOVED AND DOUBLERS FABRICATED IAW SRM 53-05, FIG 131A-14.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION FOUND ON COUNTERSINKS OF FUEL TANK ACCESS PANEL 1357C. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION FOUND ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL TANK ACCESS PANEL 143C. CORROSION REMOVED IAW SRN 51-22-2A AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL REPLACED.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION ON COUNTERSINK OF FUEL TANK ACCESS PANEL 1355C. CORROSION REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL REPLACED.

Part: CUSP WEB — CORRODED (BS 465-484) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION ON RT CUSP WEB REPAIR DOUBLER, X=-54-X=-60 BETWEEN BS 465 - 484. REPAIR DOUBLER REMOVED, REPAIR DOUBLER FABRICATED, AND INSTALLED IAW SRM 53-05, FIG 131A-13.

Part: LONGERON — CRACKED (BS 1287) · airframe 62,865 hrs · 46,639 cycles

CRACK AT LONGERON 12R BS 1287. SECTION OF LONGERON REMOVED, INSTALLED NEW SECTION LONGERON AND SPLICE IAW IAW SRM 53-02, FIG 18, 51-30-2 AND 51-305.

Part: CUSP WEB — CORRODED (BS 1210-1215) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION RT CUSP WEB X=-54 TO X=-60 BETWEEN BS 1210 -- 1215. CORROSION REMOVED AND FOUND OUT LIMITS IAW SRM 51-10-3, P26 AND ER/A 511165-14MA. AREA REPAIRED IAW SRM 51-70-4, AND INSTALLED IAW SRM 51-30-5.

Part: FLOORBEAM — CORRODED (BS 180) · airframe 69,195 hrs · 51,185 cycles

FLOORBEAM CORRODED AND FOUND OUT OF LIMITS, BS 180 BETWEEN X -7 TO X -44. SUPPORT REPLACED.

Part: CUSP WEB — CORRODED (BS 446-674) · airframe 62,865 hrs · 46,639 cycles

CORROSION ON LT CUSP WEB UPPER AND LOWER SURFACE, BS 446-465, 465-484, 513-522, 541-560, 627-636, & 655-674 BETWEEN X=54 AND X=60. CORROSION WAS REMOVED AND FOUND OUT LIMITS IAW ER/A 508307, REV A.

Part: STRUCTURE — CORRODED (BS 1154-1211) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION ON PREVIOUS REPAIR JAMB AT AFT LOWER CARGO COMPARTMENT, BS 1154-1211. REPAIRED IAW SRM 53-05 FIG 123. RII COMPLETED

Part: CUSP WEB — CORRODED (BS 927-946) · corrosion level 2 · airframe 62,865 hrs · 46,639 cycles

CORROSION ON LT CUSP WEB PREVIOUS REPAIR BETWEEN BS 927-946, X=54 TO X=60. CUSP WEB REPLACED.

Part: ENGINE — FAILED (RIGHT) · airframe 62,740 hrs · 46,541 cycles

REJECTED TAKEOFF AT APPROX 120KTS DUE TO SUSPECTED COMPRESSOR STALL WITH EGT RISING TO 677 ON RT ENGINE. MAINTENANCE FOUND METAL DEBRIS IN TAIL PIPE OF RT ENGINE. THE RT ENGINE REPLACED IAW AMDS CARD 7100-4682RT. LEAK & OPS CHECKED GOOD.

Part: ACCESS PANEL — LEAKING (RT WING) · airframe 61,509 hrs · 45,636 cycles

DURING SCHEDULED FLIGHT, DIVERTED, DUE TO A VISIBLE RT WING FUEL LEAK. MX REPLACED 2 LEAKING DOME NUTS AND SEAL ON RIGHT AFT BOOST PUMP TANK PLATE.

Part: FRAME — CRACKED (BS 1418) · airframe 61,189 hrs · 45,399 cycles

DURING SCHEDULED INSPECTION, THE B FRAME AFT OUTER FLANGE WAS FOUND CRACKED UNDER THE RADIUS BLOCK AT BS 1418 AT LONGERON 2R. REPAIRS ACCOMPLISHED IAW ER/A 516423-14.

Part: BLOCK — WORN (TAILCONE) · airframe 61,189 hrs · 45,399 cycles

DURING SCHEDULED INSPECTION, THE TAIL CONE RELEASE CABLE RT UPPER SLIDER BLOCK WAS DETERMINED TO BE WORN AT BS 1510 AT THE 2 O'CLOCK POSITION. A NEW SLIDER BLOCK WAS INSTALLED IAW AMM 53-53. FUNCTIONAL CHECKS ACCOMPLISHED IAW AMDS WC 5130-01077-0101 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: FRAME — CRACKED (BS 1418 S2R) · airframe 61,189 hrs · 45,399 cycles

DURING SCHEDULED INSPECTION, FRAME BS 1418 WAS FOUND CRACKED AT STRINGER 2R AT THE FWD FACE UPPER RADIUS. REPAIRS ACCOMPLISHED IAW ER/A 516423-14.

Part: SKIN — CORRODED (BS 570) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED INSPECTION, PILLOWING CORROSION WAS NOTED AT BS 570, AT LONGERON 30. REPAIRED IAW ER/A 516322-14.

Part: LONGERON — CRACKED (BS 1418) · airframe 61,189 hrs · 45,399 cycles

DURING SCHEDULED INSPECTION IN MSP, THE LONGERON 2R WAS FOUND CRACKED AT BS 1418. REPAIRED IAW ER/A 516515-14 AND SRM 53-02, FIG 18.

Part: LONGERON — CORRODED (BS 1287) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED INSPECTION, EXFOLIATION CORROSION WAS FOUND AT LONGERON L22 AT BS 1287. INSTALLED LONGERON SPLICES IAW SRM 53-02, FIG 18.

Part: FLOORBEAM — CRACKED (BS 886) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED INSPECTION, A CRACK WAS FOUND ON THE RT FLOORBEAM ATTACH FLANGE AT BS 886. REPAIRS ACCOMPLISHED IAW AMDS WC 5310-01415-0302.

Part: RECEPTACLE — CRACKED (TAILCONE) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED CHECK, THE TAILCONE UPPER LT LATCH RECEPTACLES (2EA) WERE FOUND TO BE CRACKED & MISSING HARDWARE. REPLACED BRACKETS AND LATCH HOUSING IAW SRM 51-30 AND COMPLETED THE REQUIRED INSPECTION.

Part: RECEPTACLE — CRACKED (TAIL CONE) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED INSPECTION, THE TAILCONE UPPER RT LATCH RECEPTACLE LOWER ATTACH BRACKET WAS FOUND TO BE CRACKED. FABRICATED AND INSTALLED NEW BRACKET IAW SRM 51-30.

Part: FRAME — CRACKED (TAILCONE) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED TAILCONE FUNCTIONAL CHECK, THE CANTED FRAME AT BS 1510 WAS FOUND TO BE CRACKED AT THE TAILCONE ALIGNMENT PIN BETWEEN THE 9 & 10 OCLOCK POSITION. COMPLETED REPAIR IAW ER/A 516370-14.

Part: FRAME — CRACKED (BS 1510) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED INSPECTION, THE CANTED FRAME AT BS 1510 WAS FOUND TO BE CRACKED AT THE TAILCONE ALIGNMENT PIN ABOVE THE LOWER RT LATCH. REPAIRED IAW ER/A 516318-14.

Part: FRAME — CRACKED (BS 1510) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED INSPECTION, FRAME 1510 WAS FOUND TO BE CRACKED AT THE TAIL CONE ALIGNMENT PIN, FIRST PIN ABOVE LWR LT LATCH ASSY. REPAIRS COMPLETED IAW ER/A 497316-14MA.

Part: CONDUIT — LOOSE (TAILCONE RELEASE) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED INSPECTION IN MSP, THE TAILCONE RELEASE CABLE CONDUITS WERE NOTED TO BE LOOSE AT STA 1510 AT THE 7 O`CLOCK POSITION. THE CLAMPS WERE REPLACED IAW AMM 20-10-11 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: SKIN — CRACKED (BS 1380) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED INSPECTION IN MSP, .1250" CRACKS WERE NOTED AT THE 3 RIVET HOLES AT BS 1380 NEAR LONGERON 13R. CRACKED AREA MATERIAL WAS REMOVED AND A FILLER & DOUBLER WAS INSTALLED IAW SRM 53-01, FIG 4 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: PLACARD — TORN (TAILCONE) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED INSPECTION IN MSP, THE TAILCONE INTERIOR RELEASE HANDLE PLACARD WAS FOUND TO BE TORN. THE REQUIRED PLACARD WAS REPLACED AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: SKIN — CRACKED (BS 1380) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED INSPECTION, A .1250" CRACK WAS NOTED AT THE A RIVET HOLE APPROX 2" ABOVE LONGERON 12R AT BS 1380. CRACKED AREA MATERIAL WAS REMOVED AND A FILLER & DOUBLER WAS INSTALLED IAW SRM 53-01, FIG 4, 53-01, PG 25. THE REQUIRED INSP WAS COMPLETED.

Part: RECEPTACLE — DAMAGED (TAILCONE RELEASE) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED INSPECTION OF THE TAILCONE FRAME, MULTIPLE GUIDE PIN RECEPTACLES WERE NOTED TO BE LOOSE OR WORN. MX REPLACED THE WORN RECEPTICLES IAW SRM 51-30 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: CABLE — FRAYED (TAILCONE RELEASE) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED INSPECTION IN MSP, THE TAILCONE CABLE WAS NOTED TO BE FRAYED. THE CABLE WAS REPLACED IAW AMM 53-53 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: BRACKET — DAMAGED (TAILCONE RELEASE) · airframe 61,180 hrs · 45,394 cycles

DURING SCHEDULED INSPECTION IN MSP, THE TAILCONE CABLE SPRING BRACKET WAS NOTED TO BE BENT AND WORN. MX INSTALLED NEW SPRING BRACKET IAW SRM 51-30 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 60,998 hrs · 45,248 cycles

DURING LINE INSPECTION, THE NR 1 LT DOOR SLIDE WAS NOTED TO BE DAMAGED. THE TYPE OR SPECIFIC DAMAGE WAS NOT CLEARLY IDENTIFIED IN THE LOGBOOK DISCREPANCY. THE SLIDE WAS REPLACED USING JOB INSTRUCTION CARD 2500-4484 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: CONNECTOR — FAILED (EMERGENCY LIGHTS) · airframe 58,991 hrs · 43,821 cycles

EMERGENCY PATHWAY LIGHTING AT ROW 30 IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS HAD FAILED. PINNED CONNECTOR AND FUNCTIONALLY CHECKED SYSTEM.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 57,939 hrs · 43,093 cycles

CREW HEARD A LOUD BANG WHICH WAS FOLLOWED BY THE NR 1 ENGINE SHUTTING DOWN. AN EMERGENCY WAS DECLARED, THE QRH COMPLIED WITH, AND THE FLIGHT DIVERTED TO A SAFE LANDING. CREW STATED THAT THERE WERE NO ADVERSE INDICATIONS PRIOR TO ENGINE FAILURE. MAINTENANCE HAS REPLACED THE NR 1 ENGINE AND THE AIRCRAFT HAS RETURNED TO SERVICE.

Part: RELEASE SYSTEM — WORN (TAILCONE) · airframe 57,630 hrs · 42,889 cycles

AIRCRAFT FAILED THE TAIL CONE FUNCTIONAL TEST ON 3 SEPARATE WORK CARDS. THE CONE FAILED TO DROP WHEN THE BAYONET SLIPPED PAST THE TRIGGER ARM ASSEMBLY. MAINTENANCE VERIFIED THAT THE BAYONET WAS ENGAGED CORRECTLY BUT AS IT WAS PULLED FORWARD THE TRIGGER PULLED UP AND OVER THE BAYONET (TO 229). ALSO, THE TAIL CONE INTERIOR HANDLE PULL TENSION TEST FAILED WHEN IT EXCEEDED 75 LBS. (TO 230). THEN IT FAILED WHEN THE TOP LATCHES RELEASED BEFORE THE LOWER LATCHES (TO 231). THIS WAS FOUND DURING MSP PSV VISIT.

Part: OIL CAP — UNSERVICEABLE (APU) · airframe 57,109 hrs · 42,520 cycles

FLIGHT ATTENDANTS REPORTED SMOKE IN THE AFT CABIN DURING CLIMB. COCKPIT CREW DIVERTED THE FLIGHT TO CVG AND LANDED WITHOUT FURTHER INCIDENT. NO EVIDENCE OF FIRE WAS FOUND AND NO EXTINGUISHERS WERE USED. MAINTENANCE IN CVG FOUND APU OILCAP LEAKING AND OIL CONTAMINATION ON THE INLET BOX OF THE APU. THE OIL CAP ASSEMBLY WAS REPLACED AND THE APU INLET ASSEMBLY WAS CLEANED BUT THEY WERE NOT ABLE TO REMOVE ALL OIL CONTAMINATION.

Part: REGULATOR — FAILED (BLEED AIR SYS) · airframe 56,264 hrs · 41,889 cycles

AT FL310 CREW RECEIVED LEFT AIR CONDITIONER TEMP HI MESSAGE. COCKPIT AND CABIN FILLED WITH HAZE. AFTER TURNING OFF LEFT HP BLEED THE HAZE CLEARED AND THE LEFT CONDITIONER TEMP HI MESSAGE WENT OUT. PHL MAINTENANCE PERFORMED ENGINE RUN BUT NO SMOKE OR ODOR WAS DETECTED. REPLACED FILTERS FROM PNEUMATIC PILOT REGULATOR AFTER THEY WERE FOUND DIRTY AND REPLACED THE PNEUMATIC PILOT REGULATOR ALSO. COMPLETED DUCT BURN OUT AND SYSTEM CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 55,670 hrs · 41,452 cycles

DURING LINE CHECK MAINTENANCE FOUND TAIL COMPARTMENT CENTER ESCAPE PATH LIGHT NEXT TO CATWALK INOPERATIVE. MAINTENANCE RE-TERMINATED WIRES TO THE LIGHT ASSEMBLY. OPERATION OF LIGHT NOW CHECKS OK.

Part: WIRE — DAMAGED (CABIN) · airframe 54,272 hrs · 40,511 cycles

MX FOUND THE EMERGENCY LIGHT AT 4CD TO BE INOPERATIVE. MX RE-TERMINATED THE WIRES. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: HEAT EXCHANGER — FUMES (NR 2 A/C PACK) · airframe 53,082 hrs · 39,730 cycles

IN CRUISE, PILOT NOTICED BURNING SMELL AND HAZE IN COCKPIT. HAZE WAS NOT VISIBLE IN CABIN. PILOT TURNED OFF PACK NR 2 AND SMELL AND HAZE DISSAPATED. NR 2 PACK PRESSURE PEGGED AT 5.0. MX RAN ENGINES AT SEVERAL POWER SETTINGS AND COULD NOT DUPLICATE. ENGINE BLEED AND A/C PACK OPERATION CHECKS GOOD. PERFORMED OPN 5088 AND NO TROUBLE WAS FOUND. PERFORMED A DUCT BURNOUT OPN 5089 AS PRECAUTIONARY. PNEUMATIC BLEED SYS AND A/C PACK SYS OPS CHECK GOOD.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 52,957 hrs · 39,671 cycles

EMERGENCY LIGHT IN 2C SEAT ASSY INOP. REPLACED SOCKET ASSY, CHECKS NORMAL.

Part: DOUBLER — CORRODED (BS 693) · airframe 48,595 hrs · 36,820 cycles

CORROSION ON THE BELLY INTERNAL DOUBLER AT FS 693 BETWEEN LONGERONS 29R AND 30R. 1 INCH BY 1.5 INCH CUTOUT DID NOT AFFECT THE SKIN. EXTERNAL REPAIR DOUBLER AND TRIPLER DUE TO PRESENCE OF THE C-2 DOOR EXTERNAL SURROUND DOUBLER. DTA SCHEDULED AT 24 MONTHS.

Part: SEAL — DETACHED (L2 DOOR) · airframe 42,335 hrs · 32,653 cycles

ON DEPARTURE VERY LOUD SQUEAL REPORTED COMING FROM AFT GALLEY DOOR. FOUND SEAL AT DOOR LOWER GATE DETACHED FROM RETAINER. NO DAMAGE TO SEAL. RE-ATTACHED SEAL AND PRESSURIZED AIRCRAFT TO 4.0 PSID. NO LEAKS NOTED AT DOOR. OK FOR SERVICE.

Part: SWITCH — FAILED (TEMP) · airframe 41,384 hrs · 31,974 cycles

THE 26K TAIL COMPT TEMP HIGH MASTER WARNING CAME ON. FOUND LEFT TEMP SWITCH STUCK IN CLOSED POSITION. REPLACED SAME.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 40,725 hrs · 31,509 cycles

AFT CABIN MEGAPHONE INOPERATIVE. REPLACED MEGAPHONE.

Part: ACTUATOR — UNKNOWN (RUDDER) · airframe 39,911 hrs · 30,945 cycles

REQD 6 DEG RT RUDDER, 1 DEG RT AILERON FOR LEVEL AND TRIMMED FLT. RETURNED CVG. REPLACED YAW DAMP ACTUATOR PER MM. PERFORMED RTS ON BOTH DFGC'S GO.

Part: INDICATOR — MALFUNCTIONED (ENG OIL SYSTEM) · airframe 37,950 hrs · 29,552 cycles

PASSING 20K LT ENGINE OIL QTY DECREASED ALL THE WAY TO ZERO. ENGINE POWER REDUCED TO IDLE.ON DECENT ALL INDICATIONS RETURNED TO NORMAL. CHECKED OIL AT TANK, FULL. INSPECTED OIL TEMP DECALS AND EXAUST AREA, OK. CREW REPORTED OIL PRESSURE DID NOT DECREASE. A/C OK FOR CONTINUED SERVICE. FWD LT ENGINE OIL QTY INDICATION DEFERRED PER MEL 79-00-03.

Part: DISPLAY — CONTAMINATED (COCKPIT) · airframe 36,764 hrs · 28,743 cycles

DURING APPROACH THE COCKPIT HAD A VERY STRONG ELECTRICAL SMELL AND SLIGHT HAZE IN THE AIR. THE ELEC/BURNING SMELL WAS VERY OVERPOWERING. WENT ONTO OXYGEN, DECLARED AN EMERGENCY AND LANDED. REPLACED F/O NAV DISPLAY.

Part: CHARGER — FAILED (E/E BAY) · airframe 36,635 hrs · 28,653 cycles

UPON ARRIVAL, FOUND COCKPIT FULL OF SMOKE. CABIN HAD SOME SMOKE VISIBLE WITH A SMOKEY ODOR. A/C BATTERY WAS ON POWER AND AIR WAS PROVIDED BY GRD UNITS. OPENED E+E ACCESS DOOR FOR T/S CKD E+E DOOR. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY CHARGER RELAY R2-56. BATTERY CHARGER OPS NORMAL. STARTED APU TO DRAW DOWN BATTERY. BATTERY VOLTAGE AND AMPS CHECK NORMAL.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 33,148 hrs · 26,258 cycles

FOUND DURING COMPLETION OF EO 9-85695-3AD REV A ME01 HEAT DAMAGE TO AIRCRAFT SIDE CONNECTOR OF BALLAST B6-51 ABOVE SEAT 12 D-E. REPLACED RECEPTACLE MB10R6, OPS CHECK NORMAL.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 28,972 hrs · 23,185 cycles

THE FUSELAGE SKIN WAS PUNCTURED BY GROUND EQUIPMENT AT FS 320 BETWEEN STRINGERS 18L AND 19L. THE DAMAGE WAS REMOVED WITH A 10 X 4 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER MD-88 SRM 53-04, FIG 12B AND ER/A 379271-14, REV A.

Part: APU — SMOKE (APU BAY) · airframe 27,940 hrs · 22,420 cycles

AIRCRAFT DIVERTED INTO ELP DUE TO HOT SMELL AND FUMES IN CABIN AND SMOKE DETECTOR GOING. MAINTENANCE FERRIED AIRCRAFT TO DFW. REPLACED APU AND PERFORMED OPN. 5088 DUCT BURNOUT.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

REAR EMERGENCY PATH LIGHTS INOP. REPLACED PWR SUPPLY. OPS NML.

Part: SEPARATOR BAG — DIRTY (CABIN)

AT CLIMB AFTER T/O FLT ATTENDANT REPORTED HOT OILY SMELL IN CABIN. ONLY LASTED A FEW SECONDS. PACK SET FOR WARM TEMP ANDTURNED TO COLD POSITION. CORR ACTION: INSPECTED ENG INLETS AND HYDRAULIC OVERFILL BOTTLES ALL NORMAL REPLACED WATER SEPERATOR BAGS NO SMELL NOTED RUNNING PACKS OFF APU OR ENG AIR.

Part: FLOOR PANEL — CRACKED (BS 1295)

MEMBRANE CRACKED STA 1295 OUTBOARD CABIN SUBFLOOR, LT SIDE VIEWED FROM BELOW. STARTED REMOVAL OF SUBFLOOR, REMOVED MEMBRANE, INSTALLED NEW MEMBRANE. REPAIRED PER SRM 53-05 FIG 100.

Part: SWITCH — MALFUNCTIONED (OVERHEAD COCKPIT)

WHEN IGNITION SWITCH WAS TURNED TO SYSTEM-B TO TURN ON ENGINE, ANTI-ICE SMOKED. REPLACED IGNITION SELECTOR SWITCH AND INVERTER RELAY R2-123.

Part: SKIN — DAMAGED (C3 DOOR CUTOUT)

THE FUSELAGE SKIN AND DOOR DOUBLER ALONG THE AFT EDGE OF THE C-3 DOOR CUTOUT HAVE SUSTAINED GROUND DAMAGE, JUST BELOW THE NR 3 DOOR STOP. REPAIRED PER DL ERA 271824-14.

Part: SEPARATOR BAGS — DIRTY (CABIN)

DURING CLIMBOUT, STRONG ODOR ENTERED CABIN, SMELLED OILY. WHEN HP BLEEDS WERE OFF ODOR CLEARED, RETURNED ATL. REPLACED WATER SEPARATOR BAGS. INSP ENG BLEED CAPS, EMPTIED HYD OVERFLOW BOTTLE. RAN ENGS, ALL CKS OK.

Part: CONNECTOR — FAILED (CABIN)

WHILE A/C LOCATED GATE A-11 ATL AT 0530 SMELLED SMOKE AND LIGHTING EXTINGUISHED RT SIDE OF CABIN. FOUND CANNON PLUG ROW 17DE BURNT AT OVHD LIGHT AND CEILING PANEL CHARRED. CANNON PULG P1-21-1 AND RECEPTACLE R-12105 WERE REPLACED, OPERATION NORMAL. PLUG AND RECEPTACLE MFG P/N MS3126F1415P AND M3124E14-15S.

Part: SKIN — CRACKED (NLG WW)

FOUND DURING E-2 LETTER CHECK, SKIN CRACKED AT NLG DOOR FWD HINGE CUTOUT RT SIDE. REPAIRED PER SRM 53-05 FIG 62.