N900DE

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 71,499 hrs · 52,872 cycles

LEFT AFT LAVATORY SMOKE DETECTOR CONTINUOUSLY SOUNDING. REM+REPL LT AFT LAV SMOKE DETECTOR PER AMM 26-13. OPS CK OK. (LP5595596)

Part: FRAME — CRACKED (RT MLG WW) · airframe 71,356 hrs · 52,729 cycles

DURING SVC CK FOUND RT FWD MAIN LANDING GEAR FRAME CRACK. REMOVED AND REPLACED RT MLG FWD O/B FRAME SECTION REF. ERA581024-14 REV. ORIGINAL - SECTION - II PERMANENT REPAIR. REPAIRED INTERCOSTAL 5930584-31 REF. SRM 53-01 FIG.2 SH.3. PENDING DOOR OPS CHECK. (594223) ADJUSTED RT DOOR OPEN SENSOR REF. AMM 32-60-05. OPS CHECK GOOD. OK FOR SERVICE. (LP5595500)

Part: FLOOR PANEL — UNSERVICEABLE (CARGO BAY) · airframe 70,719 hrs · 52,159 cycles

AFT CARGO FLOOR PANELS IN POOR CONDITION. UPON INSPECTION FOUND FLOOR PANEL 181HF TO BE IN SERVICABLE CONDITION. REMOVED, FABRICATED, AND INSTALLED PANELS 181FF AND 181DF PER AMM 25-52. (LP #4696698)

Part: ACTUATOR — LEAKING (THRUST REVERSER) · airframe 69,886 hrs · 51,435 cycles

LT TR OUTBOARD ACT. LEAKING AND STRUCTURAL DAMAGE AT TR FWD FLANGE 9:00 POS. (TR FAIRING IN CTR CARGO). R/R LT THRUST REVERSER PER AMM, 78-30-01-201 OPS CK OK. (LP4697803)

Part: PIN — DISLODGED (EVAC SLIDE) · airframe 69,391 hrs · 51,019 cycles

DURING WALK AROUND IN CABIN L1 DOOR MOUNTED ESCAPE SLIDE PARACHUTE PIN FOUND DISLODGED. ACCOMPLISHED JOB CARD 2561-01358-01A, DOOR L1 MOUNTED ESCAPE SLIDE. L1 DOOR ESCAPE SLIDE WAS R/R. (LP4991068)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,341 hrs · 50,975 cycles

OVHD EMERGENCY LIGHT INOP 18E 32E 36B. RELAMP PER AMM 33-50 OPS CHK GOOD. (LP4991033)

Part: SLIDING WINDOW — OBSTRUCTED (COCKPIT) · airframe 69,290 hrs · 50,928 cycles

SHIP 9000 - (ATB) AIR TURN BACK TO ICT DUE TO PRESSURIZATION ISSUES AND REPORT OF FO'S WINDOW LEAKING AIR. O2 MASKS DID NOT DEPLOY. CORRECTIVE ACTION: MAINTENANCE FOUND NO FAULTS ON CPC'S 1 OR 2. DEBRIS WAS FOUND AND REMOVED FROM FO'S SLIDING WINDOW. BOTH CPC'S WERE REPLACED AS PRECAUTION. C/W NO-GO-ODI PREVENTION TASKS AND PERFORMED A DUAL PACK CONFIDENCE CHECK. THE AIRCRAFT WAS RETURNED TO SERVICE. (LP5378892)

Part: STRUT — DISCHARGED (NLG) · airframe 68,977 hrs · 50,639 cycles

PERFORMED AND AIR TURN BACK DUE TO A NLG UNSAFE LIGHT ILLUMINATING DURING CLIMB OUT. THE NLG INDICATION PIN WAS NORMAL. THE CREW ASSUMED THAT THE GEAR DOORS WERE OPEN. THE GEAR WAS LOWERED AND ALL INDICATIONS WERE GOOD. MAINTENANCE PERFORMED THE NO GO ODI PREVENTION WORK CARDS AND SERVICED THE NOSE GEAR STRUT IAW WC 3221-6446. A SUCCESSFUL GEAR SWING WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (BS 1474) · airframe 68,942 hrs · 50,607 cycles

CRACKED FRAME, BS 1474, IN THE AFT ACCESORY COMPARTMENT. THE FRAME WAS REPAIRED IAW ETI-88-18-065, REV ORIG, AND ER/A 570717-14, REV ORIG.

Part: TERMINAL — BURNED · airframe 68,942 hrs · 50,607 cycles

SEVERAL TERMINALS NEXT TO THE STAIRS ON LT SIDE OF E&E BS 150 WAS BURNED. DAMAGED TERMINALS WERE REPLACED IAW SWPM 20-20-01.

Part: CONTROLLER — FAULTY (AC PACK) · airframe 68,421 hrs · 50,184 cycles

DURING WAKE UP FOUND LEFT PACK IN AUTO, WENT TO FULL HOT AND SMOKE IN THE CABIN. R&R LEFT PAC TEMP CONTROLLER IAW AMM -21-60, 818534. C/W NO GO ODI PREVENTION CHECKLIST. PERFORM WKCD 2120-2367. VERIFIED ACM FREE AND OIL LEVEL. WAS ABLE TO DUPLICATE WITH LEFT PACK IN AUTO-WENT FULL HOT. AFTER AUTO TEMP CONTROLLER REPLACEMENT LT PACK NOW OPS NML. A/C OK FOR SERVICE.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 67,816 hrs · 49,709 cycles

ROW 15 EMERGENCY LIGHT HARNESS BROKEN. R&R ROW 15 EMERGENCY LIGHT HARNESS. CKS GOOD. A/C OK FOR SVC.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 67,363 hrs · 49,383 cycles

NUMEROUS CABIN EMERGENCY LIGHTS INOPERATIVE. REPINED CONNECTORS AND RELAMPED AS REQUIRED ALL NOW CHECK NORMAL. (LP# 3832697)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,021 hrs · 49,098 cycles

EMERGENCY CEILING LIGHT INOPERATIVE. REPLACED THE BATTERY PACK B5-100 IAW MM 33-53-00.

Part: SPACER — DAMAGED (LT MLG DOOR) · airframe 66,895 hrs · 48,993 cycles

LT MLG DOOR SKID AND SPACER DAMAGED REF L/P 3444196. COMPLIED WITH TIME LIMITED REPAIR PER SECTION 1 OF ERA 562038-14 REV ORIG.

Part: BARREL — DAMAGED (TAILCONE) · airframe 66,773 hrs · 48,890 cycles

THE AFT DEPLOYED SWITCH FOR THE TAILCONE HAS A DAMAGED SET OF TURN BARRELS AND CABLE ENDS. WITH A SECOND CORRODED CABLE FROM THE EXTERNAL HANDLE SWITCH. REPLACED CABLES PER MD88 SRM 53-10-00 ON NR 3. (LP3444131)

Part: CABLE — CORRODED (TAILCONE) · airframe 66,763 hrs · 48,883 cycles

THE AFT DEPLOYED SWITCH FOR THE TAILCONE HAS A DAMAGED SET OF TURN BARRELS AND CABLE ENDS. WITH A SECOND CORRODED CABLE FROM THE EXTERNAL HANDLE SWITCH. REPLACED THE CABLES IAW SRM 53-10-00.

Part: RETAINER — BROKEN (TAILCONE HANDLE) · airframe 66,763 hrs · 48,883 cycles

NR 2 THE INTERNAL TAIL CONE HANDLE, RETAINER IS BROKEN. REPLACED BOTH RETAINERS IAW AMM 53-53-00.

Part: VANE — GOUGED (LT WING TE FLAP) · airframe 66,763 hrs · 48,883 cycles

LEFT WING OTBD FLAP INBOARD VANE GOUGED AT INBOARD UPPER SURFACE. REMOVED THE FLAP VANE IAW AMM 27-51-03.

Part: VANE — GOUGED (RT WING TE FLAP) · airframe 66,139 hrs · 48,391 cycles

FOUND THREE GOUGES ON INTERMEDIATE FLAP, RT WING, JUST AFT OF 2ND FLAP HINGE. REPLACED THE THE FLAP INBD FIXED VANE IAW AMM 27-51-03.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 65,909 hrs · 48,205 cycles

AFTER TURNING ON BOTH PACKS, HAD A BURNING PACK ODOR. PERFORMED ALT DUCT BURNOUT AND REPLACED COALESSER BAGS IAW 4950-2215 AND 2170-4139 CHECKED GOOD. FOUND HYD LEAK ON LT THRUST REVERSER CONTROL VALVE B-NUT, SECURED AND CHECKED GOOD. PERFORMED 2900-2002 AND 2900-2003. CLEANED APU INLET IAW 4900-1184. CHECKED GOOD, OK FOR SERVICE .

Part: LINE — LOOSE (THRUST REVERSER) · airframe 65,909 hrs · 48,205 cycles

ON WAKE UP AND PACK OPERATION SMOKE/HAZE IN CABIN. INITIAL INSPECTION. HEAVY DROPLETS ON RT T/R CONTROL VALVE CLEARED WIPED DOWN CONTROL VALVE, VYVLED T/R NO LEAK, NEEDS ENG RUN. TO CK HYD FILTERS. CLEANED COMPLETE AREA. PERFORMED ENG RUN NO LEAKS NOTED. PERFORMED ALTERNATE DUCT BURNOUT AND WATER BAGS. AFTER 20 MINUTES HYD FLUID AGAIN DRIPS FROM 3 DRAINS FWD OF APU INTAKE. SMALL LEAK AT RT T/R CONTROL VALVE. TIGHTENED LINE AT T/R CONTROL VALVE OPS CK LK CK GOOD. ALSO RAN ENGS NO LEAKS NOTED. A/C OK FOR SVC.

Part: LIGHT — INOPERATIVE (SEAT 29) · airframe 65,596 hrs · 47,965 cycles

SEAT 29 EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY.

Part: ACTUATOR — LEAKING (AIRSTAIR) · airframe 65,529 hrs · 47,919 cycles

DURING CRUISE, FL310 AFT F/A SMELLED FUMES OF DIRTY SOCKS. LEFT PACK IN FULL COLD. WENT TO MANUAL AND WARMER AND SEEMED LIKE FUMES DISSIPATED FOR REMAINDER OF FLIGHT. COMPLIED WITH WORKCARD 2120-2367 STEPS 1 THRU 4. FOUND AFT AIRSTAIR ACTUATOR LEAKING. REMOVED AND REPLACED THE ACTUATOR. FOUND APU INLET CONTAMINATED. CLEANED APU INLET IAW WORKCARD 4900-1184. COMPLIED WITH PNEUMATIC DISTRIBUTION DUCT BURNOUT.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT TEMP) · airframe 65,202 hrs · 47,671 cycles

DURING DEPARTURE, THE "NO MODE" LIGHT ILLUMINATED ON THE THRUST RATING PANEL IN CLIMB MODE AND THE "FLOW" LIGHT ILLUMINATED ON OVERHEAD PANEL. THE CABIN WOULD NOT PRESSURIZE. AN AIR TURN BACK WAS PERFORMED. AT GATE THE LEFT PACK WENT TO UN-COMMANDED FULL HOT IN MANUAL MODE. MAINTENANCE REPLACED THE COCKPIT TEMP CONTROLLER IAW AMM 21-61-06. DURING CHECK OF THE COCKPIT TEMP CONTROL SYSTEM THE LEFT TEMP CONTROL VALVE WAS FOUND TO BE MODULATION. MAINTENANCE REPLACED THE COCKPIT TEMP SENSOR IAW AMM 21-61-02. A DUAL PACK CONFIDENCE CHECK WAS PERFORMED PER WORK CARD 2132-1001 AND CHECKED OKAY. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 64,651 hrs · 47,252 cycles

FOUND CABIN EMERGENCY LIGHTS AT ROWS 20C AND 29C INOPERATIVE. CONNECTED THE WIRE ROW 29C IAW AMM 33-53. SEAT 20C. REPINNED CONNECTOR AT 20C, CHECKS NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,411 hrs · 47,053 cycles

AWR: LIGHTNING STRIKES ON PASSENGER CABIN WINDOW EXTERNAL CUTOUT BETWEEN STA Y=1079 TO Y=1098. WINDOW BELT LT WAS REPAIRED IAW ER/A 550277-14, REV ORIGINAL WILL BE MONITORED WITH LOG PAGE 2668777.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 63,904 hrs · 46,686 cycles

CORROSION ON SETTLEMENT AREA OF FWD BOOST PUMP SECONDARY ACCESS COVER AT LT WING. DUE TO CORROSION OUT OF LIMITS HEATER BLANKET WAS REMOVED AND NEW HEATER BLANKET WAS INSTALLED IAW AMM 30-80-02.

Part: SKIN — DAMAGED (RT MLG DOOR) · airframe 63,904 hrs · 46,686 cycles

WEAR AND PUNCTURE LOWER SKIN ON RT MAIN GEAR STRUT DOOR. LOWER SKIN ON RT MAIN GEAR STRUT DOOR WAS REPAIRED IAW SRM 51-70-2D, PAR 18B AND ACARD 2000-8149-08. WEAR WAS ATTENDED IAW NRC 20000123090, CARD 61, ZONE10.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON SETTLEMENT AREA OF AFT BOOST PUMP SECONDARY ACCESS COVER AT RT WING. DUE TO CORROSION OUT OF LIMITS, HEATER BLANKET WAS REMOVED AND NEW 1 WAS INSTALLED IAW AMM 30-80-02.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,904 hrs · 46,686 cycles

CRACKED INTERNAL STRUCTURE PAN UPPER AFT CORNER FWD CARGO DOOR. CRACK INTERNAL STRUCTURE PAN UPPER AFT CORNER FWD CARGO DOOR, C1, WAS REPAIRED IAW SRM 52-03D, FIG 8 AND ER/A 539918, REV ORIGINAL.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER AT AFT LAV SERVICE PANEL LOWER AREA. FUSELAGE SKIN WAS REPAIRED IAW ETI-88-16-207, REV 1 AND ER/A 547801-14, REV ORIGINAL.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

INITIAL: CORROSION ON FRAME OF STA Y=1380 BETWEEN LONGERONS 30 TO 28 RT AT AFT ACCESSORIES COMPARTMENT. AREA WAS REPAIRED IAW ETI-88-16-224 REV 4, SRM 51-30-5, 51-10-3 AND ER/A 546558-14, REV ORIGINAL.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 63,904 hrs · 46,686 cycles

CRACKED STOP FITTING NR 2 FORWARD EDGE AND 5 AFT EDGE BEAM PROJECTION AT FORWARD CARGO COMPARTMENT DOOR. STOPS NR 2 AND 5 WERE REPLACED IAW SRM 51-30-1 AND 51-30-5.

Part: PAN — CRACKED (CARGO DOOR) · airframe 63,904 hrs · 46,686 cycles

CRACKED INTERNAL STRUCTURE PAN FORWARD EDGE BETWEEN BEAMS 3 AND 4, FORWARD CARGO DOOR. PAN WAS REPAIRED IAW SRM 51-03-D, FIG 8.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,820 hrs · 47,404 cycles

FUSELAGE SKIN & DOUBLER AFT LAV SVC PANEL DOOR CUTOUT CORROSION. REPAIRED PER ER/A 547801-14. ACCOMPLISH SECTION II VISUAL INSPECTION EVERY 8000 FLIGHT CYCLES.

Part: DUCT — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACKED LT RADIO RACK EXHAUST DUCT AT FUSELAGE SKIN, STA Y=261 BETWEEN LONGERONS 20 LT AND 21 LT. EXAUST DUCT WAS REPAIRED IAW SR/A 464964-14 MA, REV C, METHOD 1.

Part: FLOOR PANEL — CORRODED (COCKPIT) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION FLOOR PANEL 120D A COCKPIT. NEW FLOOR PANEL WAS DRILLED IAW SRM 51-10-4, 51-30-2 AND 51-10-3, PAR 14 AND 21.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON DOOR JAMB WEB BETWEEN STA Y=1155 TO Y=1164 AT C3. WEB WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 DWG 5936442, REV A.

Part: GUIDE VANE — CRACKED (TE FLAP) · airframe 63,904 hrs · 46,686 cycles

CRACK ON RT INBD GUIDE VANE OF INBD FLAP. DAMAGE ON INBD GUIDE VANE OF INBD FLAP WAS REPAIRED IAW SRM 57-030, FIG 11 AND 51-70-2D.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORRODED TIE TRACK LT SIDE BETWEEN STA Y1222 TO STA Y1322 ALSO SPLICE BETWEEN STA Y1212 TO STA Y1231 AT C3. TIE TRACK AND SPLICE LT SIDE WERE REPLACED IAW SRM 51-30-5 AND 51-30-1.

Part: BRACKET — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON LT ELEVATOR OTBD BEARING BRACKET. LT ELEVATOR OTBD BEARING BRACKET WAS REPLACED FOR NEW BEARING BRACKET AND INSTALLED WITH CARD 2730-4234 JOB 001-0372.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACK ON FRAME OF STA Y=1338 BETWEEN LONGERONS 27 RT TO 26 RT AT AFT ACCESSORIES COMPARTMENT. FRAME OF STA Y=1338 WAS REPAIRED IAW ER/A 094719-14MA, REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACKS, 4EA, ON FRAME OF CANT STA Y=1510 BETWEEN 8:00 TO 9:00, 4:00, 5:00 AND 8:00 O'CLOCK POSITIONS AT AFT CARGO COMPARTMENT. FRAMES WERE REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3, PAR 21 AND 14.

Part: ATTACH FITTING — CRACKED (RT BULLET) · airframe 63,904 hrs · 46,686 cycles

CRACK AT INNER ATTACH FITTING ON RT ENGINE BULLET. STOP DRILL ACCOMPLISHED, CRACK WAS WELDED, WELDED AREA WAS BLENDED OUT AND STRESS RELIEVE WAS ACCOMPLISHED IAW ER/A 547807, REV ORIGINAL, FITTING WAS REMOVED AND REINTALLED IAW SRM 51-30-2.

Part: SKIN — CRACKED (TE FLAP VANE) · airframe 63,904 hrs · 46,686 cycles

CRACKED LOWER SURFACE OF INBD FLAP, INBD GUIDE VANE LT WING. DUE TO SEVERAL DAMAGED INBD FLAP, INBD GUIDE VANE LT WING WAS REPLACED WITH REPAIRED GUIDE VANE AND WILL BE INSTALLED WITH CARD 2710-4628.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON LT TRACK FROM STA Y=1003, Y=1212 AT C3. LT TIE TRACK WAS REPLACED IAW SRM 51-30-1/ 51-30-2 AND IPC 25-52-00-03L NR 410.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACK ON FRAME OF CANT STA Y=1485 BETWEEN LONGERONS 24 RT TO 25 RT AT AFT ACCESSORIES COMPARTMENT. FRAME WAS REPAIRED IAW SRM 53-05, FIG 43.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION OUT OF LIMITS ON FLOORBEAM STA Y=1307 AND X=20 LT, CABIN FLOOR STRUCTURE. FLOORBEAM WAS REPAIRED IAW 53-05, FIG 20A AND 51-10-4 AND 51-10-3, PAR 21, 14.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

REQUIRED REINFORCING ANGLES OF RT APB LOWER TEE CHORD CUT LINE REF CARD 5310-01449-01, STEP 13. RT APB LOWER TEE CHORD WAS REPAIRED IAW ETI-88-16-224, REV 1 AND ER/A 547797-14, REV ORIGINAL.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

REQUIRED REINFORCING ANGLES OF LT APB LOWER TEE CHORD CUT LINE REF CARD 5310-01449-01, STEP 9, LT APB LOWER TEE CHORD WAS REPAIRED IAW ETI 88-16-224, REV 1 AND ER/A 547797-14, REV ORIGINAL.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON STRAP STA Y=1338 BETWEEN LONGERON 28RT TO 29LT AFT FACE AT AFT CARGO COMPARTMENT. STRAP WAS REPLACED IAW SRM 51-30-5, 51-30-2, 51-30-1 AND 51-10-4.

Part: SKIN — WORN (TE FLAP VANE) · airframe 63,904 hrs · 46,686 cycles

INITIAL: WEAR ON SKIN UPPER SURFACE OF RT OTBD FLAP, INBD VANE ON OTBD LOWER CORNER OF T/E, RT WING. DAMAGED AREA WAS REPAIRED IAW SRM 51-03D, PART II AND CARD 2000-8149-03, 2652870, JOB 000-0005.

Part: SKIN — PUNCTURED (LT MLG DOOR) · airframe 63,904 hrs · 46,686 cycles

PUNCTURE LOWER SKIN ON LT MAIN GEAR STRUT DOOR. LWR SKIN ON LT MAIN GEAR STRUT DOOR WAS REPAIRED IAW SRM 51-70-2D, PAR 18B.

Part: ACCESS DOOR — CORRODED (LT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 1373C AT LT WING. DOOR 1373C WAS REPLACED.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACKED MLG DOOR JAMB FRAME, STA Y=937 RT WHEEL WELL. JAMB WAS REPLACED IAW SRM 51-30-2 AND 51-30-5, DWG 5930584, REV.

Part: ACCESS DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON SECONDARY ACCESS OF FUEL ACCESS DOOR NR 1410C AT RT WING. ACCESS PLATE WAS REPLACED.

Part: ACCESS DOOR — CORRODED (LT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 1361C AT LT WING. ACCESS DOOR 1361C WAS REPLACED.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON LONGERON 22 LT BETWEEN STA Y:1307 TO 1310 AT AFT CARGO COMPARTMENT. DUE TO EXCESSIVE CORROSION ON LONGERON 22 LT WAS REPAIRED AND SPLICE REPAIR IAW SRM 53-02, FIG 18.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON FUEL ON SECONDARY ACCESS 1307C AT LT WING. REPLACED FUEL PLATE IAW ER/A 530866-14 AND IPC 57-30-00.

Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON LONGERON 23 LT AND STA Y:1307. IN REF CARD 340, ZONE 100, C3. DUE TO EXCESSIVE CORROSION ON LONGERON 23LT WAS REPAIRED AND SPLICE REPAIR IAW SRM 53-02, FIG 18.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 63,904 hrs · 46,686 cycles

DELAMINATED ON SKIN UPPER SURFACE ON RT INBD FLAP OTBD VANE AT 20" OF INBD EDGE. DAMAGE AREA WAS REPAIRED IAW SRM 57-03D, PAR II.

Part: ACCESS DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR NR 1460C AT RT WING. FUEL ACCESS DOOR 1460C WAS REPLACED IAW SRM 51-22-2A. FUEL MEASURING MAGNETICS TICK WAS REPLACED UNDER CARD 311, ZONE 100.

Part: ACCESS DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 1414 C AT RT WING. ACCESS PLATE 1414C WAS REPLACED AND ACCESS FUEL PROBE WAS INSTALLED IAW AMM 28-00-00.

Part: ACCESS DOOR — CORRODED (LT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 1335C AT LT WING. ACCESS PLATE 1335C WAS REPLACED AND ACCESS FUEL PROBE WAS INSTALLED IAW AMM 28-00-00.

Part: VALVE — WORN (AC BAY) · airframe 63,904 hrs · 46,686 cycles

WEARS ON CORNERS OF RT AIR CONDITIONING DIVERTER VALVE. WEARS ON CORNERS RT DIVERTER VALVE WERE REPAIRED, WELDED IAW ERA 547805-14, REV ORIGINAL REPAIR WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACKED SKIN ON ELEVATOR ACCUMULATOR ACCESS CUTOUT, AFT UPPER CORNER LOCATED BETWEEN STA 1463 CANT AND 1474 CANT RT SIDE. SKIN DOUBLER WAS REPLACED IAW DWG 5917686-7, REV AA, SRM 51-30-5 AND 51-30-2.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 63,904 hrs · 46,686 cycles

CRACK ON LT RIBS INTERNAL STRUCTURE FIXED L/E STA ZFS=17.656 AND ZFS=23.500 APPROXIMATELY AND ELONGATED HOLES ON FORMER STA ZFS=30.000 AT VERTICAL STABILIZER. RIBS AND FORMER WERE REPAIRED IAW SRM 55-02, FIG 27, 51-30-2, 51-30-5, 51-10-2, 51-10-3 OAR 21 AND 14.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

HIDDEN DISCREPANCY CRACK ON RT CUSP STA Y=1193 BETWEEN X= 54 TO X=60 AT FLOOR STRUCTURE CABIN. CUSP WAS REPAIRED IAW SRM 53-05, FIG 131A.

Part: ACCESS DOOR — CORRODED (LT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 1303C AT LT WING. FUEL ACCESS DOOR 1303C WAS REPLACED.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON RT CUSP WEB BETWEEN X=54 TO X=60, STA Y=1108 TO Y=1131 AT FLOOR STRUCTURE CABIN. CUSP WEB BETWEEN STA Y=1108 TO 1131 WAS REPAIRED IAW SRM 53-05, FIG 131A-7.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 63,904 hrs · 46,686 cycles

CRACKED SKIN ON LT STA YV=160.688 APPROXIMATELY TIP FAIRING. AREA WAS REPAIRED IAW SRM 55-01, FIG 4, SHEET 2.

Part: SKIN — CRACKED (THRUST REVERSER) · airframe 63,904 hrs · 46,686 cycles

SEVERAL CRACKS ON OUTER SKIN OF THRUST REVERSER UPPER DOOR AT ENGINE NR 1. OUTER SKIN OF THRUST REVERSER WAS REPAIRED IAW AMM 78-30-07-801, FIG 803 AND SRM 51-10-3, PAR 14 AND 21.

Part: ACCESS DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 1436C AT RT WING. FUEL ACCESS DOOR 1436C WAS REPLACED.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACK ON LONGERON NR 12 LT AND STA Y=1437 AT AFT ACCESSORIES COMPARTMENT. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, 51-10-3 PAR 21, 14, 51-30-2 AND 51-30-5, CRACK ON LONGERON L=1.125.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

DELAMINATION AND FERRULES DAMAGED ON FLOOR PANELS 826B, 826C, 826D, 826E, 827C, 886B, 886C, 927B. FLOOR PANEL NR 826E WAS FABRICATED, FLOOR PANELS 8216C, 826B, 826D, 886C AND 927C DAMAGE FERRULES WERE REPLACED. AMM 53-20-01-201 AND FLOOR PANEL 927B WAS WORKED IAW CARD 277, ZONE 100.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACKED FIRST GENERATION FLOOR 313A, 1003A, 389A, 617A, 927E AND 541A. CRACK ON FLOOR PANELS WERE REPAIR 313A, 927E, AND 1003A IAW SRM 53-05, FIG 131C AND FLOOR PANELS 389A, 541A AND 617A WERE REPLACE IAW DWG 9952521, REV AZ.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACK ON LONGERON END BS 1338, LONGERON 15 RT. LONGERON END WAS REPLACED IAW SRM 51-30-5, 51-10-2, 51-10-3 PAR 21 AND 14, DWG 4912515, REV H 51-30-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACKED LONGERON END 1 AT STA Y=1338. LONGERON END WAS REPLACED IAW SRM 51-30-5, 51-10-2, 51-10-3 PAR 21, 14 AND DWG 4912515 REV H, 51-30-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACK ON LONGERON END 1338, LONGERON 7 LT. LONGERON END WAS REPLACED IAW SRM 51-30-5, 51-10-2, 51-10-3, PAR 21 AND 14 DWG 4912515, REV H, 51-30-2.

Part: SKIN — DENTED (ELEVATOR TAB) · airframe 63,904 hrs · 46,686 cycles

DENT ON LOWER FACE NEAR TO EDGE, 1EA AT RT ELEVATOR CONTROL TAB. REPAIRED IAW SRM 55-04, PAR 2 AND 51-70-2 AND CARD 2000-8149-01.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 63,904 hrs · 46,686 cycles

WEAR ON FWD/AFT LOWER PRODUCTION DOUBLERS AT FWD CARGO COMPARTMENT DOOR, C1. LOWER DOUBLERS FWD/AFT ON CARGO DOOR, C1 WERE REPLACED IAW SRM 51-30-2 AND ER/A 486624-14MA.

Part: SKIN — DENTED (ELEVATOR TAB) · airframe 63,904 hrs · 46,686 cycles

DENT ON RT ELEVATOR CONTROL TAB STA XHS=58. REPAIRED IAW SRM 55-04, PAR 2 AND 51-70-2 AND CARD 200-8149-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON REPAIR DOUBLER AT LT CABIN FLOOR CUSP WEB X=54 TO X=60 BETWEEN Y=1174 AND T=1193. REPAIR DOUBLER WAS ATTENDED IAW SRM 53-05 FIG 131A-3 AND 51-10-3, PAR 14, 21.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACKED RT CUSP WEB STA Y=845 X=54 TO 56 RT AT CPAX. AREA WAS REPAIRED IAW SRM 53-05, FIG 131-A.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACK ON RT CUSP WEB BETWEEN BS Y=862 TO 866 X=54 TO 56 AT CPAX. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-3.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACK ON LT CUSP WEB, STA Y=905 BETWEEN X=54 TO X=60 AT CABIN FLOOR STRUCTURE. LT CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON LT CUSP WEB X=54 TO X= 60, BETWEEN STA Y= 877 TO 880, CABIN FLOOR STRUCTURE. LT CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-4.

Part: ACCESS DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON SETTLEMENT AREA OF FUEL ACCESS DOOR 1409C AT RT WING. FUEL ACCESS DOOR WAS REPLACED.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON LT FLOOR CUSP WEB UPPER/LOWER SURFACE X=54 TO X=60 BETWEEN STA Y=1174 AND Y=1180, BETWEEN Y=1271 AND Y=1237. DAMAGE AREA BETWEEN Y=1174 TO 1180 WAS REPAIRED WITH CARD 103, A/C ZONE 201. DAMAGE AREA BETWEEN Y=1237 TO 1271, REPAIR WAS ACCOMPLISHED IAW SRM 53-05, FIG 131-A. AREA BETWEEN Y=1250 TO 1271 WAS CLEANED IAW PS 900-1-2-1 AND NO CORROSION WAS FOUND.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACK ON RT CUSP WEB, STA Y=883 TO 885, X=54 TO 56 AT CPAX. RT CUSP WEB, WAS REPAIRED IAW SRM 53-05, FIG 131 A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

INITIAL CORROSION ON LT CABIN FLOOR CUSP WEB UPPER/LOWER SURFACE BETWEEN STA Y=636 AND Y=655 BETWEEN X=54 TO X=60. FLOOR CUSP WEB WAS REPARED BETWEEN STA Y=636 AND STA Y=655 BTW X=54 TO X=60 IAW SRM 53-05, PAR 144, FIG 131A-6; 51-30-3 PAR 8, 51-30-1, 51-30-5 AND 51-10-3 PAR 38.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,904 hrs · 46,686 cycles

DELAMINATION AND FERRULES DAMAGED ON FLOOR PANELS NR`S 389B, 465B, 465C, 465D, 541B, 541D, 579E, 693C, 693D, 769B, 769C. FLOOR PANEL NR'S: 541D, 769C, 541B, 769B, 693C, 693D, 465B, 489B, 465D AND 465C WERE FABRICATED IAW AMM 53-20-01-201.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,904 hrs · 46,686 cycles

DELAMINATION AND FERRULES DAMAGED ON FLOOR PANELS NR`S 927B, 1003C, 1003D, 1073D, 1079B, 1174C, 1250C, W2. FLOOR PANELS NR`S 1003C, 1003D AND 1250C WERE FABRICATED IAW AMM 53-20-01-201. FLOOR PANELS NR`S 927B, 1079B, 1079D, 1174D, 1174C WERE REPLACED, FERRULES IAW AMM 53-20-01-201.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON LT CABIN FLOOR CUSP WEB UPPER, LOWER SURFACE AT X=54 TO X=60 BETWEEN STA Y=674 AND Y= 693. LT CUSP WEB FROM X=54 TO X=60 BETWEEN Y=674 AND Y=693 WAS REPAIRED IAW SRM 53-05, FIG 131A-7.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

AWR HIDDEN DISCREPANCY: CORROSION ON RT CUSP WEB BETWEEN STA Y: 518 TO 541 AND STA X: -54 TO -60 AT PASSENGER CABIN. CUSP WEB STA Y=518 TO 541 WAS REPAIRED IAW SRM 53-05, FIG 131A-5, SHEET 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,904 hrs · 46,686 cycles

DELAMINATION AND FERRULES DAMAGED ON FLOOR PANELS NR`S: 120E, 120C, 148A, 148B, 148C, 148D, 160A, 160B, 160C, 160D, 160E, 160F, 200B, 200D, 200E, 256C, 256B, 256D, 313C, 313D. FLOOR PANELS NR`S: 148A, 148B, 148C, 148D, 160A, 160B, 160C, 160D, 160E, 160F, 120C, 120E, 200B, 200C, 200D, 200E, 256B, 256C, 256D, 313C AND 313D WERE FABRICATED IAW AMM 53-20-01-201. FLOOR PANEL NR 313B WAS REPLACED, FERRULES IAW AMM 53- 20-01-201.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 63,904 hrs · 46,686 cycles

DAMAGED RUDDER FLAME SPRAY. DAMAGE FLAME SPRAY WAS REPAIRED IAW ER/A 092613-14MA REV A, SRM 51-70-1D, REP 23.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACKED COMPOSITE CHANNEL ON FIRST GENERATION FLOORS NR 1155A AND 1079A. COMPOSITE CHANNEL ON FIRST GENERATION FLOORS NR 1155A AND 1079A WERE REPAIRED IAW SRM 51-70-1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON LT CABIN FLOOR CUSP WEB UPPER, LOWER SURFACE BETWEEN STA Y=693 AND Y=712 AT X=54 TO X=60. CUSP WEB STA Y=693 AND 712 WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACKED LT CABIN FLOOR CUSP WEB UNDER PRODUCTION DOUBLER AT STA Y=844 BETWEEN X=54 TO X=60. WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-6.

Part: ACCESS DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR NR 1454C AT RT. FUEL ACCESS DOOR 1454C WAS REPLACED.

Part: ACCESS DOOR — CORRODED (LT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 1363C AT LT WING. ACCESS DOOR 1363C WAS REPLACED.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON LOWER DOOR JAMB REPAIR DOUBLER BETWEEN STA Y=636-Y 693 MID CARGO COMPARTMENT. DOUBLER ON LOWER DOOR JAMB WAS REPLACED IAW SRM 53-05, FIG 123 AND 51-30-5.

Part: ACCESS DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS DOOR NR 1462C AT RT WING. FUEL ACCESS DOOR 1462C WAS REPLACED.

Part: ACCESS DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS DOOR NR 1456C AT RT WING. FUEL ACCESS DOOR 1456C WAS REPLACED.

Part: ACCESS DOOR — CORRODED (LT WING) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 1355C AT LT WING. FUEL ACCESS DOOR 1355C WAS REPLACED.

Part: PAN — CRACKED (FUSELAGE) · airframe 63,904 hrs · 46,686 cycles

CRACK ON WINDOW RING PAN FWD UPPER CORNER STA Y=927 TO Y=946 AT CABIN STRUCTURE. AREA WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA, REV A AND 487747-14MA, REV A.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORRODED RT CUSP WEB BETWEEN STA Y=636 TO 655 X=54 TO 60 AT CPAX. DUE TO EXCESSIVE CORROSION ON CUSP WEB, THIS AREA WAS REPAIRED IAW. SRM 53-05, FIGURE 131A-17.

Part: SKIN — DAMAGED (BS 598-655) · airframe 63,904 hrs · 46,686 cycles

SEVERAL LIGHTNING STRIKES ON WINDOW BELTS FROM BS 598 TO 655 LONGERONS 11 - 14R. REPAIRED IAW ER/A 546537-14, REV ORIGINAL AND SRM 53-05, FIG 111.

Part: CUSP WEB — CRACKED (BS 607-608) · airframe 63,904 hrs · 46,686 cycles

CRACK ON LT CUSP WEB BTW BS 607-608 X 54 TO X 60. REPAIRED IAW SRM 53-05, FIG 131A-13, 51-10-3 PAR 38,-21-14, 51-30-2, 51-30-5.

Part: SEAT TRACK — CORRODED (BS 200-207) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON SEAT TRACK X 44 BETWEEN BS 200, TO 207 AT PAX CABIN. SEAT TRACK WAS REPAIRED IAW SRM 53-05, FIG 4F.

Part: CUSP WEB — CORRODED (BS 796-800) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON RT CUSP WEB FROM BS Y: 796 TO 800 AND X -54 TO -60 AT PAX CABIN. AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-1.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORRODED RT CUSP WEB PREVIOUS REPAIR STA Y=731 TO 750 X= 54 TO 60 RT AT CPAX. CUSP WEB PREVIOUS REPAIR WAS REPLACED IAW SRM 51-30-1, 51-30-2, 51-30-5, SRM 53-05, FIG 131A-751-10-3 PAR 14, 21, 38.

Part: CUSP WEB — CORRODED (BS 598-617) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORRODED RT CUSP WEB PREVIOUS REPAIR BETWEEN BS 598 TO 617 RBL 54 - 60 IN PAX CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131 A-14 SRM 51-30-02, 51-30-05, 51-10-03, PAR 14 AND 21.

Part: CUSP WEB — CRACKED (BS 809) · airframe 63,904 hrs · 46,686 cycles

CRACKED LT CABIN FLOOR CUSP WEB DOUBLER AT BS 809 BETWEEN X=54 TO X=60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A, 51-30-2, 51-30-5, 51-10-3 PAR 14 AND 21, 385.

Part: PAN — CRACKED · airframe 63,904 hrs · 46,686 cycles

CRACKED FWD LOWER CORNER OF LT RING PAN BETWEEN BS Y=712 TO Y=731, Y=1079 TO Y=1060, Y=1060 TO Y=1091 ATINTERNAL STRUCTURE. CRACKED RING PANS BETWEEN BS Y=712 TO Y=731, Y=1060 TO Y= 1079 AND Y=1041 TO Y=1060 WERE REPAIRED IAW SRM 53-05, FIG. 122, 51-30-02, 51-30-05. ER/A 487747-14-MA, REV. A AND ER/A 493648-14MA, REV. A .

Part: CUSP WEB — CORRODED (BS 218-226) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORRODED RT CUSP WEB PEVIOUS REPAIR BS 218 TO 226 RBL 54-60 IN PAX CABIN. PREVIOUS REPAIR WAS REPLACED IAW SRM 53-05, FIG 131A AND SRM 51-30-2.

Part: WINDOW FRAME — CRACKED · airframe 63,904 hrs · 46,686 cycles

CRACK ON AFT/ LOWER CORNER RT WING RING PAN BETWEEN BS 845 TO BS 864 IN CPAX. RING PAN RT AFT/LOWER WAS REPAIRED OAW SRM 53-05, FIG 122, PAR 139 ER/A 487747-14 MA, REV A ER/A 493648-14 MA, REV A.

Part: SEAT TRACK — CORRODED (BS 343-348) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON RT SEAT TRACK, PLUG X=-54 BETWEEN BS 343 TO 348. PLUG WAS REPLACED IAW SRM 53-05, FIG 4A.

Part: WINDOW FRAME — CRACKED · airframe 63,904 hrs · 46,686 cycles

CRACK ON RT RING PAN BETWEEN BS 731 TO BS 750 IN CPAX. RING PAN RT WAS REPAIRED IAW SRM 53-05, FIG 122, PAR 1339, ER/A 493647-14 MA REV "A", 487747-14 MA, REV A.

Part: WINDOW FRAME — CRACKED · airframe 63,904 hrs · 46,686 cycles

CRACK ON FWD/LOWER CORNER RT RING PAN BETWEEN BS 946 TO BS 965 IN CPAX. RING PAN RT FWD/LOWER WAS REPAIRED IAW SRM 53-05, FIG 122, PAR 139, ER/A 487747-14 MA, REV "A" 493648-14 MA REV A.

Part: CUSP WEB — CORRODED (BS 465-484) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORRODED RT CUSP WEB PREVIOUS REPAIR BETWEEN BS Y=465 TO 484 X=54 TO 60 RT AT CPAX. PREVIOUS REPAIR ON RT CUSP WEB WAS REPLACED IAW SRM 53-05, FIG 131A-7.

Part: SEAT TRACK — CORRODED (BS 935) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON REPAIR PLUG OF LT SEAT TRACK X 54 IN BS 935 AT PASSENGER CABIN. PLUG WAS REPLACED IAW SRM 53-05, FIG 4A.

Part: WINDOW FRAME — CRACKED · airframe 63,904 hrs · 46,686 cycles

CRACK ON FWD/LOWER RT RING PAN BETWEEN BS 560 TO BS 576 IN CPAX. RING PAN RT FWD/LOWER WAS REPAIRED IAW SRM 53-05, FID 122 AND ER/A 487747-14 MA, REV A, 493648-14 MA REV "A".

Part: WINDOW FRAME — CRACKED (BS 886-906) · airframe 63,904 hrs · 46,686 cycles

CRACK ON FWD/UPPER CORNER RT RING PAN BETWEEN BS 886 TO 906 IN CPAX. RING PAN RT FWD /UPPER WAS REPAIRED IAW SRM 53-05, FIG 122, PAR 139 ER/A 487747-14 MA, REV A, 493648-14 MA REV A.

Part: WINDOW FRAME — CRACKED · airframe 63,904 hrs · 46,686 cycles

CRACK ON AFT/ UPPER CORNER RT RING PAN BETWEEN BS 1079 TO 1098 IN CPAX. REPAIR UPPER CORNER RT RING PAN BETWEEN BS Y=1079 TO Y=1098 IN CPAX IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5 ER/A 493648-14 MA REV A, ER/A 487747-14MA, REV A.

Part: WINDOW FRAME — CRACKED (BS 576-598) · airframe 63,904 hrs · 46,686 cycles

CRACK ON FWD/LOWER RT WING PAN BETWEEN BS 576 TO 598 IN CPAX. RING PAN RT FWD/LOWER WAS REPAIRED IAW SRM 53-05, FIG 122 AND ERA 487747-14 MA, REV A ER/A 493648-14, REV A.

Part: WINDOW FRAME — CRACKED (BS 313-332) · airframe 63,904 hrs · 46,686 cycles

CRACK ON FWD/LOWER RT RING PAN BETWEEN BS 313 TO 332 IN CPAX. RING PAN RT LOWER/FWD WAS REPAIRED IAW SRM 53-05 FIG 122 AND ER/A 493647-14 MA REV A, 487747-14 MA REV A.

Part: WINDOW FRAME — CRACKED · airframe 63,904 hrs · 46,686 cycles

CRACKED UPPER AFT CORNERS OF LT RING PAN BETWEEN BS Y=769 TO Y=788 Y=1022 TO Y=1003 ALSO LOWER FWD CORNER BETWEEN BS Y=845 TO 864 AT INTERNAL STRUCTURE OF CABIN. UPPER AFT CORNERS OF LT RING PAN BETWEEN BS Y=769 TO Y=788 Y=1022 TO Y=1003 ALSO LOWER CORNER BETWEEN BS Y=845 TO Y=864 WERE REPAIRED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5, ER/A 487747-14MA REV A AND ER/A 493648-14MA REV A.

Part: FLOOR PANEL — CRACKED · airframe 63,904 hrs · 46,686 cycles

CRACKED AND DISBONDED, CHANNEL AT FLOOR PANEL NR 927A. CHANNEL AT FLOOR PANEL WAS BONDED AND REPAIR THE CRACKS IAW SRM 51-20-00, SRM 53-05, FIG 131B.

Part: WINDOW FRAME — CRACKED · airframe 63,904 hrs · 46,686 cycles

CRACKED UPPER FWD CORNER OF LT RING PAN BETWEEN BS 788 TO Y=807, 845 TO 864, 1003 TO 984 AT INTERNAL STRUCTURE OF CABIN. RING PAN LT OF CORNER FWD UPPER WERE REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 487747-14 MA REV "A", 493648-14 MA REV A.

Part: WINDOW FRAME — CRACKED (BS 275-294) · airframe 63,904 hrs · 46,686 cycles

CRACK ON FWD UPPER CORNER RING PAN BETWEEN BS Y=275-294 LT SIDE PASSENGER CABIN. FWD UPPER CORNER RING PAN BETWEEN BS Y=275-294 WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 493648-14MA REV A, ER/A 487747-14MA, REV A.

Part: WINDOW FRAME — CRACKED · airframe 63,904 hrs · 46,686 cycles

CRACKED UPPER FWD CORNER OF LT RING PAN BETWEEN BS Y=1098 TO Y= 1079 AND Y=1022 TO Y=1041 AT INTERNAL STRUCTURE OF CABIN. UPPER FWD CORNER OF LT RING PAN BETWEEN BS Y= 1079 TO Y=1098, AND Y=1022 TO Y=1041 WERE REPAIRED IAW SRM 53-05, FIG 122, 51-30-2, 51-30-5, ER/A 493648-14MA, REV A AND ER/A 487747-14MA, REV A. LONG OF CRACKS ARE FOLLOW: IN BS Y=1098 TO Y=1079 IS .128" AND BS Y=1022 TO 1041 IS .132".

Part: WINDOW FRAME — CRACKED · airframe 63,904 hrs · 46,686 cycles

CRACKED UPPER AFT CORNER OF LT RING PAN BETWEEN BS Y=1212 TO Y=1231 AT INTERNAL STRUCTURE OF CABIN. RING PAN LT OF CORNER AFT UPPER WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/A 487747-14 MA REV A, 493648-14 MA REV "A".

Part: FLOOR PANEL — CORRODED (PAX CABIN) · corrosion level 2 · airframe 63,904 hrs · 46,686 cycles

CORROSION ON FLOOR PANEL 160G IN PAX CABIN. DUE TO EXCESIVE CORROSION FLOOR PANEL WAS FABRICATED IAW SRM 51-10-02 AND DWG 9957828, REV AB.

Part: WINDOW FRAME — CRACKED (BS 1022-1231) · airframe 63,904 hrs · 46,686 cycles

CRACKED LOWER AFT CORNER OF LT RING PAN BETWEEN BS Y=1022 TO Y=1003, Y=1212 TO Y=1231 AT INTERNAL STRUCTURE CABIN. RING PAN LT OF CORNER AFT LOWER WERE REPAIRED IAW SRM 53-05, FIG 122.

Part: SKIN — DAMAGED (LT WING) · airframe 63,904 hrs · 46,686 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND, SEVEN DIFFERENT FASTENERS OF PSE, ON LOWER SKIN AT REAR SPAR BETWEEN XRS=163 TO 168 AT LT WING.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 63,015 hrs · 46,076 cycles

THE CREW ON FLIGHT 1565 FOUND THAT THE EMERGENCY EXIT PATH LIGHTS FROM ROW 31-38 INCLUDING THE CAT WALK WERE INOPERATIVE. MAINTENANCE FOUND SHORTED WIRES AT THE CATWALK ILLUMINATION ASSY L2.845.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 62,562 hrs · 45,741 cycles

MAINTENANCE FOUND EMERGENCY EXIT SEAT LIGHTS INOPERATIVE AT ROWS 31 TO 38. A SHORTED WIRE WAS FOUND AND REPAIRED AT SEAT 35DE.

Part: BLANKET — MISSING · airframe 60,608 hrs · 44,305 cycles

ICE & RAIN PROTECTION, WING, NO FOD HEATER BLANKET.

Part: ENGINE — POWER LOSS (NR 1) · airframe 59,656 hrs · 43,617 cycles

FLIGHT CREW DIVERTED THE ACFT FOLLOWING THE FAILURE OF NR 1 ENGINE POWER. MAINTENANCE HAS REPLACED THE ENGINE.

Part: PIN — BINDING (TAIL DOOR) · airframe 59,379 hrs · 43,426 cycles

DURING CHECK, MAINTENANCE FOUND THAT THE TAILCONE FAILED TO DROP AFTER THE DOOR WAS OPENED. MAINTENANCE FOUND THE TEE PIN BINDING IN THE CLIPS. MAINTENANCE REMOVED THE TEE PIN AND CLEANED PINS & CLIPS AND OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 59,211 hrs · 43,297 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE FROM ROWS 31 TO 36. MAINTENANCE SECURED A LOOSE CONNECTOR AND THE LIGHTS WERE OPERATIONAL.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,090 hrs · 42,503 cycles

DURING LINE CHECK, NOTED THE EMERGENCY EXIT LIGHT AT SEAT 34D INOPERATIVE. WIRE HARNESS REPLACED IAW AMM 33-50 AND OPS CHECKED NORMALLY.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 57,847 hrs · 42,359 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 3D IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: SPAR — CRACKED (RT WING) · airframe 57,627 hrs · 42,197 cycles

DURING SCHEDULED INSPECTION, A CRACK LESS THAN TWO INCHES WAS NOTED AT THE RIGHT WING REAR SPAR AT XRS 164 AT THE LOWER INBOARD FLAP HINGE FITTING ATTACH POINT. REPAIRED IAW ER/A 519928-14AD.

Part: SEAL DEPRESSOR — CRACKED (E/E BAY DOOR) · airframe 57,626 hrs · 42,196 cycles

NOSE WW UPPER E&E BAY DOOR SEAL DEPRESSOR PAN CRACKED AT LOWER AFT RADIUS. REPAIRED IAW ER/A 519813-14.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 57,626 hrs · 42,196 cycles

TAIL CONE EMERGENCY RELEASE CAM BASE FOR KEVLAR CABLE WORN. REPLACED CAM BASE IAW AMM 53-53-00.

Part: LATCH — WORN (TAILCONE RELEASE) · airframe 57,626 hrs · 42,196 cycles

TAIL CONE EMERGENCY RELEASE UPPER LT LATCH SPADE WORN. REPLACED UPPER AND LOWER LEFT LATCH SPADE.

Part: LATCH — WORN (TAILCONE RELEASE) · airframe 57,626 hrs · 42,196 cycles

TAILCONE EMERGENCY RELEASE LOWER LT LATCH SPADE WORN. REPLACED LOWER LT LATCH SPADE IAW AMM 53-53-00.

Part: LATCH — WORN (TAILCONE RELEASE) · airframe 57,626 hrs · 42,196 cycles

TAIL CONE EMERGENCY RELEASE LOWER RT LATCH SPADE WORN. REPLACED LATCH SPADE ASSEMBLY IAW AMM 53-53-00.

Part: PAN — CRACKED (DOOR FRAME) · airframe 57,626 hrs · 42,196 cycles

DURING SCHEDULED CHECK, A CRACK WAS FOUND AT THE LT AFT OVERWING EXIT DOOR FRAME UPPER PAN, AFT OF THE UPPER LATCH CUTOUT. REPAIRED IAW SRM 53-05, FIG 32.

Part: DOOR — OUT OF ADJUST (LT OVERWING) · airframe 57,626 hrs · 42,196 cycles

DURING SCHEDULED CHECK, LT AFT OVERWING EXIT WOULD NOT OPEN DURING OPS CHECKS AFTER MAINTENANCE. ADJUSTED THE DOOR FOR PROPER CLEARANCE AT THE DOOR CUTOUT IAW AMM 52-21-00-710-801.

Part: RECEPTACLE — WORN (TAILCONE) · airframe 57,626 hrs · 42,196 cycles

DURING SCHEDULED INSPECTION, ALL OF THE TAIL CONE GUIDE PIN RECEPTICALS FOR THE TAILCONE WERE FOUND TO TO BE WORN. REPLACED ALL GUIDE PIN RECEPTICALS IAW AMM 53-53.

Part: SLIDER — WORN (TAILCONE RELEASE) · airframe 57,715 hrs · 42,265 cycles

DURING CHECK, NOTED UPPER RIGHT TAIL CONE RELEASE SLIDING BLOCK WORN. SLIDING BLOCK REPLACED PER AMDS 5350-01077-0101.

Part: LANYARD — DISCONNECTED (DOOR SLIDE) · airframe 57,594 hrs · 42,173 cycles

PILOT REPORTED THE FWD GALLEY DOOR SLIDE COVER LANYARD HAD BECOME DISCONNECTED. MX REATTACHED THE LANYARD TO A SERVICEABLE CONDITION.

Part: FUSE — OPEN (EMERGENCY LIGHTS) · airframe 57,587 hrs · 42,168 cycles

EMERGENCY SEAT LIGHTS INOPERATIVE FROM ROW 31 AFT. FOUND FUSE OPEN IN B5-212 POWER SUPPLY. REPLACED FUSE IAW CMM 33-21. REPLACED BULBS IN SEAT 33DEF AND PERFORMED OPS TEST IAW AMM 33-53. EMERGENCY LIGHTS CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,578 hrs · 42,159 cycles

DURING LINE CHECK, FWD EMERGENCY EXIT ROW OVERHEAD ESCAPE LIGHTS WERE FOUND TO BE INOPERATIVE ON BOTH SIDES. REPLACED BATTERIES IAW AMM 33-53 AND OPERATION CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,010 hrs · 41,754 cycles

DURING ROUTINE LINE INSPECTION, IT WAS NOTED THAT THE EMERGENCY ESCAPE PATH LIGHTS WERE INOPERATIVE FROM ROW 31 AFT, INCLUDING THE TAILCONE. THE BATTERY PACK AT ROW 35 WAS REPLACED IAW AMM 33-50 AND THE SYSTEM TESTED NORMALLY.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIHGT) · airframe 56,601 hrs · 41,469 cycles

DURING SERVICE CHECK, THE SEAT MOUNTED EMERGENCY LIGHT WAS NOTED TO BE INOPERATIVE AT ROW 23DE. THE EMERGENCY LIGHT HARNESS WAS FOUND DAMAGED UNDER THE SEAT AND WAS REPLACED IAW AMM 33-53. THE SYS OPERATION THEN CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,893 hrs · 40,957 cycles

DURING SERVICE CHECK, LT AND RT AFT EMERGENCY EXIT HATCH OVERHEAD EXIT SIGNS INOPERATIVE. REPLACED BATTERIES IN AFT BATTERY PACK, BS 902. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,803 hrs · 40,895 cycles

DURING SERVICE CHECK, MX FOUND EMERGENCY LIGHTS FROM SEAT 31 TO SEAT 36 INOPERATIVE. MX R & R AFT ZONE EMERGENCY LIGHT POWER SUPPLY. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,985 hrs · 40,306 cycles

DURING SERVICE CHECK, MX FOUND SEAT 11 EMERGENCY ESCAPE PATHWAY LIGHTING INOPERATIVE. REPAIRED WIRING IAW SWPM. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,703 hrs · 40,109 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY LIGHTS FROM ROW 31 AFT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY (B5-212). OPERATION CHECKS NORMAL.

Part: SKIN — DENTED (BS 271 L29-30) · airframe 53,853 hrs · 39,530 cycles

DENT AT FUSELAGE STA 275 BETWEEN L30 AND L29. DENTED AROUND THE LOWER FUSELAGE DRAIN HOLE. ALL WORK ACCOMPLISHED PER ER/A 503114-14 REV ORIG.

Part: LONGERON — CORRODED (BS 1155-1211) · airframe 53,853 hrs · 39,530 cycles

AFT CARGO COMPARTMENT DOOR OPENING LOWER EDGE LONGERON 28R BEAM CORROSION ON UPPER SURFACE OF LOWER FLANGE FROM STA 1155 TO 1211. REPAIRED PER SRM 53-05 FIG 123A AND ER/A, 499523-14 MA.

Part: SKIN — CRACKED (BS 1437 L2-3R) · airframe 1 hrs · 1 cycles

FOUND SKIN CRACKED AT BS 1437 BETWEEN LONGERON 2-3R JUST BELOW THE VERTICAL STABILIZER, CUT OUT DAMAGE 1 INCH AND INSTALLED A DOUBLER PER ER/A 502977-14.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 53,786 hrs · 39,481 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND EMERGENCY ESCAPE PATHWAY LIGHT INOPERATIVE AT SEAT 29D. MAINTENANCE REMOVED AND REPLACED HARNESS. OPERATION CHECKS GOOD.

Part: FAN — JAMMED (CABIN) · airframe 52,564 hrs · 38,689 cycles

THE CREW ADVISED THAT SMELLED SMOKE IN THE AFT CABIN SHORTLY AFTER TAKEOFF FROM LGA. FLIGHT DIVERTED TO AN UNEVENTFUL EMERGENCY LANDING AT JFK. MAINTENANCE FOUND ALL OF THE RECIRCULATION FAN CIRCUIT BREAKERS TRIPPED AND THE FAN IMPELLER JAMMED. AFTER THE RECIRCULATION FAN WAS REPLACED, AND THE FUNCTIONAL CHECK WAS GOOD, THE AIRCRAFT RETURNED TO SERVICE.

Part: LANYARD — MISINSTALLED (DOOR SLIDE) · airframe 50,323 hrs · 37,131 cycles

ON LINE CHECK, MX FOUND ALL 3 DOOR SLIDE LANYARDS INSTALLED IMPROPERLY. MX REPOSITIONED DOOR SLIDE LANYARDS IAW MM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 49,727 hrs · 36,736 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. MX REPAIRED BROKEN WIRING AT SEAT. OPS OF LIGHT NOW CHECKS GOOD.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,318 hrs · 36,467 cycles

EXFOLIATION CORROSION ON FUSELAGE SKIN STA Y=759-760 BETWEEN LONGERONS 27RT AND 28 RT. REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04D FIG 53 AND 51-10-3 (DLM88101795).

Part: SKIN — DAMAGED (FUSELAGE) · airframe 49,318 hrs · 36,467 cycles

LIGHTNING STRIKE ON FUSELAGE SKIN STA Y=725 LONG 17LT ALSO WINDOW FRAME UPPER FORWARD SECTION BETWEEN STA Y=731 TO 750 LEFT SIDE. BLENDED AREAS, REMAINING THICKNESSES WITHIN LIMITS REF ERA 483330-14 REV ORIG AND SRM 53-04D FIG 38 TABLE B CONDITION 2 PAR 1 (DLM88101786).

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,318 hrs · 36,467 cycles

HIDDEN DAMAGE; EXFOLIATION CORROSION ON FUSELAGE SKIN STA Y=1098-1105 BETWEEN LONGERONS 28 RT AND 29 RT IN REF NR T0176385. DAMAGE AND CORROSION WERE REMOVED IAW SRM 51-30-5 AND 51-10-3. REPAIR PIECES WERE FABRICATED AND INSTALLED IAW SRM 53-04D FIG 53 (DLM88101794).

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 49,318 hrs · 36,467 cycles

EXFOLIATION CORROSION ON LOWER DOOR JAMB AT CENTRAL CARGO COMPARTMENT BETWEEN STA Y=636-693. PREVIOUS REPAIR REMOVED IAW SRM 51-30-7 AND 51-30-5. REPAIR PIECES WERE FABRICATED AND INSTALLED IAW SRMS 53-05 FIG 123, 51-10-4, AND 51-10-3 (DLM88101793).

Part: ROD END — CORRODED (EVAC SLIDE) · corrosion level 2 · airframe 49,318 hrs · 36,467 cycles

RUSTED ROD END OF EVACUATION SLIDE PLATFORM AT AFT ACCESSORY COMPARTMENT. ROD END WAS REMOVED AND REPLACED IAW AMM 20-30-01 (DLM88101790).

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 49,318 hrs · 36,467 cycles

HIDDEN DAMAGE; PITTING CORROSION ON LT HORIZONTAL STAB UPPER SKIN BARREL NUT BORES 2 EA. CORROSION REMOVED IAW PRI AMR0955137. HOLES WERE REWORKED IAW ERA 482830-14 REV ORIG AND AWR 0955137. REPAIR BUSHINGS WERE FABRICATED AND INSTALLED IAW ERA 482831-14 REV ORIG (DLM88101791).

Part: FRAME — CRACKED (FUSELAGE) · airframe 49,318 hrs · 36,467 cycles

CRACK ON FRAME 1510 BELOW RUDDER HYDRAULIC PACK ATTACH FITTING. DAMAGED SECTION WAS REMOVED, FABRICATED AND INSTALLED IAW SRMS 51-30-2, 51-10-3, AND 51-70-5 (DLM88101789).

Part: SUPPORT BRACKET — WORN (TAILCONE) · airframe 49,318 hrs · 36,467 cycles

WORN SUPPORT BRACKET ON TAIL CONE RELEASE SYSTEM. BRACKET REPLACED IAW SRM 51-30-2 AND 51-30-1, AND DOUGLAS DRAWING 9952641 REV E (DLM88101785).

Part: TAB — DAMAGED (ELEVATOR) · airframe 49,318 hrs · 36,467 cycles

LIGHTNING STRIKE ON LT ELEVATOR CONTROL TAB TRAILING EDGE INBOARD SECTION. THIS NRC WAS ACCOMPLISHED IAW OPN 1031 CARD 1090 - 1098 AND SRM S55-04 PAR 3.A AND 51-70-2D PAR 18B AND FIGURE 802D (DLM88101788).

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,318 hrs · 36,467 cycles

EXFOLIATION CORROSION ON SUPPORT STA Y=1350 BTW X=16 TO X=-16 BELOW AFT ENTRANCE DOOR. DAMAGE WAS CUTOUT AND REPAIR PIECES FABBED IAW PRI AMR0953778 REV ORIG. PARTS AND AREA WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 21. REPAIR PARTS INSTALLED IAW ERA 483340-14.

Part: COALESCER BAG — ODOR (CABIN AIR) · airframe 49,256 hrs · 36,438 cycles

RETURNED TO DEPARTURE AIRPORT, DUE TO AN ELECTRICAL ODOR IN THE AFT CABIN. ON CLIMB OUT F/A REPORTED AN ELECTRICAL ODOR IN THE REAR CABIN AREA. ODOR DISSIPATED AFTER 10 MINUTES CIRCUIT BREAKERS AND SYS IN THE COCKPIT WERE NORMAL. REPLACED THE RECIRCULATION FAN FILTER. ACCOMPLISHED OPERATIONS 5088/5089 AND REPLACED COALESCER BAGS. NO SMOKE OR ODOR DETECTED DURING INSP PROCEDURES.

Part: TURBINE — FAILED (NR 2 ENGINE) · airframe 48,145 hrs · 35,711 cycles

RT ENG FAILURE ON T/O CLIMB POWER. SPD 250 ALT 3000 LOUD BANG- EPR ROLLED BACK- TEMP RISE TO 800- SOME ROTATION UNTIL FUEL SHUT OFF. NO FIRE INDICATION. RTN TO FLL. AT GATE MTC FOUND TURBINE FAILURE. METAL IN TAILPIPE. WILL REQUIRE ENGINE CHANGE. REPLACED NR 2 ENG PER TRNAS 9T102AD.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 47,113 hrs · 35,016 cycles

HORIZONTAL STAB UPPER RT AFT SKIN CRACK ERA 460327-14AD. C/W PERMANENT REPAIR. REPLACED UPPER AFT SKIN PANEL PER EA 09-460214-12 REV D ME08.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 44,626 hrs · 33,387 cycles

RIGHT MAIN GEAR GREEN LIGHTS FAIL TO ILLUMINATE ON LANDING. FLIGHT CREW RELAMPED ON GO AROUND. OPERATION NORMAL FOR LANDING. MAINTENANCE RECORDED INFORMATION AND PERFORMED ANNUN/DIGITAL LIGHT TEST. LANDING GEAR INDICATOR LIGHTS CHECK NORMAL.

Part: PUMP — FAILED (NR 1 HYD SYS) · airframe 42,362 hrs · 31,878 cycles

AT ALT 230 CLEAN CONFIG LEFT HYD SYSTEM PRESSURE WENT TO ZERO. RAN CHECKLIST AND PER PROCEDURES REGAINED LEFT SYS PRESSURE AFTER TURNING ON AUX AND TRANS PUMPS. REPLACED LT ENGINE HYD PUMP, CASE DRAIN AND IN LINE PRESS FILTERS. RAN ENGINE CKS OK. LEAK CK OK.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 41,047 hrs · 31,044 cycles

FOUND HORIZ STAB RT UPPER AFT SKIN PANEL, CRACK REPAIR. THE UPPER AFT SKIN PANEL OF THE RT HORIZONTAL STABILIZER WAS FOUND WITH A 1.5" CRACK AT THE INBD AFT CORNER OF THE PANEL. THE CRACK WAS STOP DRILLED ON A TIME LIMITED BASIS PER ER/A 460327-14. THE DAMAGE WILL BE PERMANENTLY. REPAIRED THROUGH PART REPLACEMENT.

Part: CLAMP — LOOSE (AUG VALVE) · airframe 40,822 hrs · 30,908 cycles

AFTER T/O OUT OF LGA. GOT A TAIL COMPARTMENT TEMP HIGH ANNUNCIATOR. RAN QRH AND LIGHT EXTINGUISHED WHEN LEFT THROTTLE RETARDED TO IDLE. DIVERTED TO JFK. REPOSITION CLAMPS ON LT AUGMENTATION VALVE, RETORQUE SAME. AS PER MM, PERFORM PROC 36-00-00201. AUG VALVE AND ANTI-ICE SYSTEM CHECK, PERFORM HIGH POWER RUN-UP PER 72-00-00-501. RUN-UP CHECK GOOD.

Part: FUSE — BLOWN (BATTERY CHARGER) · airframe 32,399 hrs · 25,053 cycles

EMERGENCY EXIT PATHWAY LIGHTS INOP AT ROWS 31 THRU 38. REPLACED 5 AMP FUSE ON BATTERY CHARGER, OPS CHECK NORMAL.

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 30,001 hrs · 23,384 cycles

AT LIFT-OFF AT PNS THERE WAS NOTICEABLE POP SOUND A SLIGHT YAW TO THE AIRCRAFT FOLLOWED BY SMOKE IN THE CABIN AND A BURNING ODOR IN COCKPIT. SMELL / SMOKE DISSIPATED RAPIDLY AND NO OTHER ABNORMAL INDICATION NOTED FOR REMAINER OF FLIGHT NORMAL LANDING. FOUND EVIDENCE OF BIRDSTRIKE ON RT FLAP AND NR 2 ENGINE AROUND BLADE ROOT AREA. BOROSCOPED ENGINE PER MM. PERFORMED TAKEOFF POWER RUN PER PFHB. NTF. ALL PARAMETERS NORMAL.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 28,967 hrs · 22,671 cycles

AFT CABIN EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY, CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,930 hrs · 22,645 cycles

ON LAYOVER INSPECTION, FOUND EMERGENCY EXIT LIGHT AT PASSENGER SEAT 26DEF INOP. REPLACED EMERGENCY EXIT WHITE AISLE LIGHT AT SEAT 26DEF. CHECKS OK.

Part: COALESCER BAG — CONTAMINATED (A/C BAY) · airframe 27,414 hrs · 21,538 cycles

FUMES REPORTED BY F/A IN AFT CABIN. PERFORMED DUCT BURNOUT.

Part: RADAR — FAILED (COCKPIT) · airframe 24,506 hrs · 19,390 cycles

RADAR FAILED IN FLT R/T FAULT. REPLACED TRANSCEIVER AND INDICATOR.

Part: COALESCER — CONTAMINATED (CABIN)

RTO FOR BURNING SMELL IN COCKPIT SPEED 120KTS. REPLACED WATER SEPARATOR BAGS. RAN ENGINES AND APU. ALL CKS OK.

Part: OVEN — DIRTY (GALLEY)

DURING TAXI OUT, SMOKE FROM FIRST CLASS OVEN. FOUND BURNED PAPER MEAL TAG ATTACHED TO MEAL CARRIER. AIRCRAFT TAXIED BACK TO RAMP. MAINTENANCE REMOVED REMAINS OF TAG. CLEANED AND OPERATED OVEN. NO FURTHER SMOKE, OVEN OPERATED NORMALLY.

Part: STRUT — REQD SERVICE (NLG)

NOSE GEAR DOOR FAILED TO CLOSE AFTER T/O. REPACKED AND SERVICED NOSE STRUT.

Part: STRUT — REQD SERVICE (NLG)

AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. RETURNED TO CVG. SERVICED NOSE STRUT TO CORRECT.

Part: OVEN — SMOKING (FWD GALLEY)

FIRST CLASS GALLEY OVEN SMOKES, NO EVIDENCE OF FOOD SPILLAGE REPORTED. INSPECTED F/C OVEN, OPN NORMAL.

Part: ANGLE — CRACKED (NR 1 PYLON)

FOUND DURING C-2 LETTER CHECK, NR 1 ENG PYLON UPPER SKIN TO FUSELAGE SKIN ATTACH ANGLE WAS FOUND CRACKED .5 INCHES. INSTALLED REPAIR PER SRM 54-04A.