N998DL

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 71,859 hrs · 52,200 cycles

EMERGENCY LIGHT AT 30ED INOP. R&R HARNESS OPS NML REF AMM 33-52. (LP5596570)

Part: LIGHT — INOPERATIVE (SEAT 28D) · airframe 71,580 hrs · 51,943 cycles

EMERGENCY ESCAPE PATH LIGHT INOP AT SEAT 28D. REPLACED THE LIGHT ASSY PER AMM 33-50.

Part: LINE — LEAKING (APU FUEL) · airframe 70,879 hrs · 51,332 cycles

AFT F/A SAID STRONG SMELL OF FUEL ONLY AFTER LANDING. THEN SMELL DISSIPATED BY THE TIME WE ARRIVED AT THE GATE. NO GO ODI. HAS EXCESSIVE AMOUNT OF FUEL IN APU FUEL LINE SHROUD DRAIN. POSSIBLE APU INLET CONTAMINATION. T/S FUEL LINE SHROUDS FOR LEAKS, NO FURTHER LEAKAGE WAS FOUND, INSPECTED APU INLET, INLET WAS CLEAN AND DRY. C/W AMDS NO GO ODI PNEUMATIC DIST. CABIN SMOKE/ODOR TROUBLESHOOTING W/C 2120-2367, NO FUEL SMELL EXIST. DISPATCH APPROVAL MCC (PAUL). REMOVED AND REPLACED L&R COALESSOR BAGS PER MD88 AMM 21-20, CKS GOOD. (LP5812698)

Part: DOOR FRAME — CRACKED (MLG WW) · airframe 70,879 hrs · 51,332 cycles

WHILE PERFORMING SVC CHECK FOUND 2" CRACK ON RT WHEEL WELL FWD FRAME BELOW DOOR PROX SWITCH. REPLACED RIGHT FWD WHEEL WELL DOOR JAMB PER BOEING DWG # 5930584. (LP5655004)

Part: LIGHT — MISWIRED (CABIN) · airframe 70,510 hrs · 51,008 cycles

LT/RT OVERWING EMER LIGHT STAYS WITH SHIP BATT OFF AND COMPLETELY DEAD. FOUND B5-105 MISWIRED AND AFT EXIT SIGNS INOP. REPLACED B5-105 AND 2 EXIT SIGN BULBS PER MD88 AMM 33-53 AND WDM 33-51. (LP5308368)

Part: WIRE — DAMAGED (CABIN) · airframe 70,304 hrs · 50,836 cycles

SEAT 24ED - 30ED, SEAT MOUNTED EMERGENCY LIGHT INOP. FOUND FUSE BLOWN IN PWR SUPPLY B5212. FOUND DAMAGED WIRE @ SEAT 30. REPAIRED WIRE IAW AMM 20-50. REPLACED FUSE IN PWR SUPPLY B5212 SYSTEM CKS GOOD. A/C OK FOR SVC. (LP4809443)

Part: BATTERY — DISCHARGED (CABIN) · airframe 70,210 hrs · 50,759 cycles

EMERGENCY LIGHTS INOP ROW 24LEFT AND RIGHT OVERWING EXITS THROUGH ROW 30. REPLACED BATTERY'S & PACK B5-212 ROW35 OVERHEAD REPLACED FUSES OF PACK OPS CKS PER AMM 33-53-00. (LP5236894)

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 70,194 hrs · 50,744 cycles

RT SIDE EMERG SEAT LIGHTS INOP. FOUND 2 FUSES BLOWN IN POWER SUPPLY. R/R FUSES PER MD88 AMM 33-51. (LP5236881)

Part: BATTERY PACK — UNKNOWN (EMERGENCY LIGHTS) · airframe 70,164 hrs · 50,719 cycles

FOUND EMERGENCY LIGHTS STILL ON FROM INBOUND FLIGHT AND PWR OFF. R/R BOTH BATTERY PACK ASSY REF MD88 AMM 33-53. SYSTEM OPS CK GOOD. (LP5236865)

Part: WIRE — SHORTED (EMERGENCY LIGHT) · airframe 69,831 hrs · 50,436 cycles

EMERGENCY EXIT ROW LIGHTS OUT ROW 24-29. T/S FOUND SEAT 29 WIRING SHORTING. REPAIRDED WIRING PER SWPM AND REPLACED FUSE IN AFT BAT. PACK B5-212 CKS GOOD PER MD88 AMM 33-53. (LP4807245)

Part: SKIN PANEL — NOT REPORTED (RT HORIZ STAB) · airframe 69,157 hrs · 49,847 cycles

AWR, MTC REQUEST: TO REPAIR HORIZ STAB UPPER SKIN PANEL. REMOVE AND INSTALL RT ELEVATOR HYD POWER CONTROL VALVE AND HYD LINES PER AMM 27-30-07-201.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 69,154 hrs · 49,846 cycles

DAMAGE FLOOR PANLES NR 693C AND 1003D AT CABIN PAX. FLOOR PANELS NR 693C AND 1003D AT CABIN PAX. WERE REPLACCED PER AMM 53-20-01-201 P 7.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,154 hrs · 49,846 cycles

CRACK ON FRAME Y=1510 CANT BTW 5 AND 6 HRS POSITION AT AFT ACCESORY COMPARTMENT. CRACK ON FRAME Y=1510 CANT BTW 5 AND 6 HRS POSITION AT AFT ACCESORY COMPARTMENT WAS REPAIRED PER ERA 497316-14MA REV ORG.

Part: SKIN PANEL — CRACKED (RT HORIZ STAB) · airframe 69,154 hrs · 49,846 cycles

CRACK OF 1.250" LENGTH WAS FOUND ON RT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL STA XH=-8.500. UPPER AFT SKIN WAS REPAIRED PER DWG SR09550028 REV D AND SRM 51-30-2 AND 51-30-5(ET). HFEC INSPECTION WAS ACCOMPLISHED ON RT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL STA XH=-8.500 AND NO CRACKS WERE FOUND AFTER TRIM OUT PER NDT SPM 06-10-01.001.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,154 hrs · 49,846 cycles

OUT OF LIMITS CORROSION ON LOWER BEAM AT MID CARGO COMPARTMENT DOOR JAMB BTW STA 652 AND 673. BEAM AT MID CARGO COMPARTMENT DOOR JAMB BTW STA 652 AND 673 WAS REPAIRED PER SRM 53-05 FIG 123 CORROSION LEVEL 2.

Part: PUMP — CLOGGED (RT ENGINE) · airframe 69,125 hrs · 49,824 cycles

ALTERNATE GEAR EXTENSION, CREW REPORTS THAT WHILE ENROUTE THE RIGHT HYDRAULIC SYSTEM BECAME INOPERATIVE WITH ZERO PRESSURE INDICATION. CREW USED ALTERNATE GEAR EXTENSION TO LOWER THE LANDING GEAR. MAINTENANCE FOUND RIGHT ENGINE DRIVEN PUMP AND CASE DRAIN FILTERS CLOGGED. MAINTENANCE FLUSHED LINES AND REPLACED THE RIGHT EDP, CASE DRAIN FILTER, AND RIGHT SYSTEM FILTERS. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,631 hrs · 49,431 cycles

EMERGENCY LIGHTS IN THE AFT TAIL ARE INOPERATIVE, UPPER. REMOVED AND REPLACED THE BATTERIES IN THE AFT LAVATORY. EMERGENCY LIGHTS OPS NORMAL IAW AMM 33-50.

Part: LIGHT — INOPERATIVE (SEAT 18D) · airframe 68,631 hrs · 49,431 cycles

SEAT 18D EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT, OPS OK IAW AMM 33-50.

Part: DOOR — MISSING (LE SLAT TRACK) · airframe 69,154 hrs · 49,846 cycles

LT WING LOWER SLAT TRACK COVER DOOR MISSING **DISPATCHER SELECT EXTENSION**. SLAT TRACK DOOR NR 6 LT WAS FABRICATED PER ERA 512356-14MA REV ORIGINAL SECTION II.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 67,873 hrs · 48,885 cycles

AFT MEGAPHONE INOP. REPLACED INOP MEGAPHONE PER AMM 25-60. CKS GOOD. S/N OFF: 3541.

Part: STRINGER — CRACKED (RT WING) · airframe 67,766 hrs · 48,806 cycles

MD88 - WINGS / STRINGERS / RH STRINGER #17 AT XCW 12 / CRACK. DTA MONITOR INSPECTION LOG REFERENCE ER/A 546518-14, SECTION I REPAIR IS PENDING A DTA EVALUATION FROM BOEING WITHIN 18 MONTHS. ER/A 546518-14AD REV A IS CURRENT. DTA RESTRICTION REMOVED, LOGPAGE TO BE TERMINATED. (LP2539364)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,379 hrs · 48,522 cycles

SEVERAL OVERHEAD EMERGENCY LIGHTS INOPERATIVE BETWEEN SEATS 13 AND 16. REMOVED AND REPLACED THE BATTERY PACKS IAW AMM 33-53.

Part: CAM — OUT OF ADJUST (TAILCONE RELEASE) · airframe 67,162 hrs · 48,349 cycles

DURING TAIL ESCAPE SLIDE CHANGE. FOUND THE TAILCONE RELEASE CAM CLOCKED INCORRECTLY. ADJUSTED THE TAIL CONE RELEASE CAM IAW AMM 53-53-02.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 65,609 hrs · 47,234 cycles

SEAT 30 DE SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. FOUND WIRE BROKEN AT CONTACT PIN IN CONNECTOR. TERMINATED THE WIRE IAW SWPM 20-90-03. CHECKED GOOD.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 64,513 hrs · 46,445 cycles

EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT ROW 15DE. REPLACED ESCAPE PATH LIGHT HARNESS REF AMM 33-51. OPS CHECK GOOD.

Part: ACCESS DOOR — CORRODED (WING) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR NR 1335C. ACCESS PLATE 1335C WAS REPLACED.

Part: STOP — CRACKED (CARGO DOOR) · airframe 64,043 hrs · 46,120 cycles

CRACKED FORWARD EDGE STOPS NR 1 AND NR 3 AT FORWARD CARGO COMPARTMENT DOOR. CRACKED FORWARD EDGE STOPS 1 AND 3 WERE REPLACED IAW SRM 51-30-1,51-30-5 AND DWG 5910141, REV FE.

Part: LANYARD — DAMAGED (L1 DOOR) · airframe 64,043 hrs · 46,120 cycles

BROKEN WIRES ON L1 EVACUATION SLIDE LANYARD CABLE, SN 00599. LANYARD CABLE WAS REPLACED IAW AMM 25-62-00-201.

Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON AREA OF SETTLEMENT OF AFT BOOST PUMP SECONDARY ACCESS COVER AT LT WING HEATER BLANKET. DUE TO EXCESSIVE DAMAGE LT WING HEATER BLANKET WAS REPLACED IAW AMM 30-80-02.

Part: WEB — WORN (CABIN DOOR) · airframe 64,043 hrs · 46,120 cycles

WEAR ON UPPER WEB OVER UPPER HINGE AT AFT CABIN PRESSURE BULKHEAD DOOR. DAMAGE WEB WAS REPAIRED IAW SRM 52-01, FIG 4, SHEET 3.

Part: HINGE — EXCESS PLAY (CARGO DOOR) · airframe 64,043 hrs · 46,120 cycles

FREE PLAY ON FWD/AFT HINGE AT FWD CARGO COMPARTMENT DOOR. FWD/AFT FWD CARGO DOOR HINGES WERE REMOVED IAW AMM 52-31-02-201. HINGES WERE REPAIRED IAW ER/A 497387-14MA, REV 13. REPAIRED HINGES WERE INSTALLED IAW AMM 52-31-02-201. FREE PLAY WAS CORRECTED.

Part: ATTACH FITTING — CRACKED (VERTICAL STAB) · airframe 64,043 hrs · 46,120 cycles

CRACK ON LT DORSAL FIN ATTACH FITTING. FITTING WAS INSTALLED IAW SRM 51-30-5 BOLTS WERE TIGHTEN IAW AMM 20 30 01.

Part: FRAME — CRACKED (LT WING) · airframe 64,043 hrs · 46,120 cycles

CRACK WAS FOUND ON LT WING MAIN FRAME STR 11, STA 160. TASK CARD WAS PERFORMED WITH CARD 5712-01030-03. LT WING MAIN FRAME STR 11 REPAIR RII SECTION.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON LT TIE TRACK BETWEEN Y=1322 AND Y=1220 AT C3 COMPARTMENT. TIE TRACK WAS REPLACED IAW SRM 51-10-4, 51-30-1 AND 51-30-5.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

AWR, HIDDEN DAMAGE. CRACKED LONGERON SPLICE ON LONGERON 30 BETWEEN Y=1287 AND Y=1309 AT AFT CARGO COMPARTMENT. LONGERON SPLICE WAS REMOVED, FABRICATED NEW SPLICE ADJUSTED AND DRILLED, INSTALL AND APPLIED CIC IAW SRM 51-30-5,53-02 PAR 12, 5I-IO-4, 51-10-3 PAR 38 AND DWG 3913291, REV F.

Part: PAN — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACK ON PAN FORWARD EDGE BETWEEN BEAM 4 AND 5 AT AFT SERVICE DOOR, SN 00969. CRACK ON PAN WAS REPAIRED IAW ETI-88-16-231 REV 1 AND ER/A 541548-14, REV ORIGINAL.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON RT & LT TIE TRACK BETWEEN STA Y=1003 AND Y=1155 AT AFT CARGO COMPARTMENT. NEW TIE TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-30-2, TIE TRACK LT WAS ATTENDED WITH NRC 00779.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON INTERNAL DOUBLER OF RADIO ALTIMETER CUTOUT ANTENNA LOCATED FROM STA Y=674-693 BETWEEN LONGERONS 30 AND 29LT. REMOVED FASTENERS STA Y=660 TO Y=693, LONG 30 AND LONG 29 LT IAW SRM 51-30-2 DOUBLER INTERNAL WAS REMOVED IAW SRM 51-30-2 DOUBLER INTERNAL WAS FABRICATED IAW DWG:5911412, DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5. CIC WAS APPLIED IAW SRM 51-10-3, PAR 38.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACKED FRAME STA Y=1510 CANT, POS 7 HRS AND 10 HRS AT AFT ACCESSORY COMPARTMENT. FRAMES UPPER SECTION AND LOWER SECTION LT SIDE WERE REPLACED IAW SRM 51-10-4, SRM 51-30-2, SRM 51-10-3 PAR 14.21 AND DWG 9911843, REV AC.

Part: FITTING — CRACKED (EMERGENCY EXIT) · airframe 64,043 hrs · 46,120 cycles

CRACKED CLIPS ON AFT UPPER INTERNAL STRUCTURE AT AFT RT EMERGENCY EXIT DOOR. CLIPS WERE REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9957735, REV G.

Part: BEAM — CRACKED (PAX DOOR) · airframe 64,043 hrs · 46,120 cycles

CRACK ON BEAM NR 1 FWD AND AFT EDGE AT MAIN ENTRY PASSENGER DOOR. BEAM WAS REPAIRED IAW SRM 52-05D, FIG 81 AND 82.

Part: EXHAUST DUCT — CRACKED · airframe 64,043 hrs · 46,120 cycles

CRACKED EXAHUST ON EXTERNAL FUSELAGE SKIN BETWEEN LONGERON 20 LT AND 21 LT STA Y=256 TO Y=275. CRACKS ON EXHAUST WAS REPAIRED WITH METHOD 1 POSTERILY WITH METHOD 2 OF ER/A 464964-14MA, REV C, ETI 88-14-237, REV ORIGINAL. FPI WAS ACCOMPLISHED ON WELDED AREAS, NO CRACKS WERE FOUND IAW ETI 88-14--273 AND NDT SPM 08-00-06, PAR 8.

Part: NOSE COWL — CRACKED (LT ENGINE) · airframe 64,043 hrs · 46,120 cycles

CRACKED LT NOSE COWLING LIP INTERNAL STRUCTURE. SERVICEABLE NOSE COWL WAS INSTALLED IAW AMM 71-10-01-201.

Part: STRAP — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACKED STRAP REPAIR ON LOWER DOOR JAMB BETWEEN STA Y=1193 TO Y=1212 AT AFT CARGO DOOR JAMB C3. STRAP WAS REPLACED IAW SRM 53-05, FIG 123, SHEET 3, -9.

Part: BEAM — CRACKED (R1 DOOR) · airframe 64,043 hrs · 46,120 cycles

CRACK ON BEAM NR 1 FWD EDGE AT R1 DOOR IN REF NRTC, SN 1600. BEAM WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9911579, REV L. BEAM WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9911579, REV L.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

PUNCTURE ON AFT VENTRAL STAIR OUTER SKIN, STA Y=1474, CANT. DAMAGE WAS REPAIRED IAW SRM 53-04-2 FIG1.

Part: TAB — DEBONDED (RUDDER) · airframe 64,043 hrs · 46,120 cycles

PART RACKS DISBONDED LOWER CUP AT RUDDER CONTROL TAB DUE TO WEIGHT AND BALANCE IS OUT OF LIMITS. THE RUDDER CONTROL TAB WAS REPLACED UNDER CARD SN 01633.

Part: SKIN — DAMAGED (TE FLAP) · airframe 64,043 hrs · 46,120 cycles

TOOLING MARKS ON UPPER SKIN AT LT WING OTBD FLAP INBD GUIDE VANE. UPPER SKIN AT LT WING OUTBD FLAP INBD GUIDE VANE WAS REPAIRED IAW SRM 57-03D, PAR 11.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER BETWEEN Y=1287 AND Y=1309 AND LONGERON 29 RT AND 30 AT C3 COMPARTMENT. DOUBLER WAS REPLACED IAW SRM 53-04-2, FIG 2.

Part: SKIN — CRACKED (ENTRY DOOR) · airframe 64,043 hrs · 46,120 cycles

CRACK ON DOOR SKIN BETWEEN BEAM NR 4 AND BEAM 5 AT FWD MAIN ENTRY DOOR. SKIN WAS REPAIRED IAW ERA 501106-14MA, REV C AND ETI-88-16-151, REV 2.

Part: DOUBLER — DENTED (TE FLAP) · airframe 64,043 hrs · 46,120 cycles

DENTS ON PREVIOUS REPAIR DOUBLER ON LT INBD FLAP INBD VANE LOWER SKIN. REPAIR DOUBLER ON LT WING INBD FLAP INBD VANE WAS REPLACED IAW SRM 57-03D, PAR 11.

Part: DOUBLER — WORN (CARGO DOOR) · airframe 64,043 hrs · 46,120 cycles

WORN LOWER FORWARD AFT OUTER SKIN DOUBLERS AT FORWARD CARGO COMPARTMENT DOOR. DOUBLERS WERE REPLACED IAW SRM 5I-30-2 AND ERA 486624-14, REV ORIGINAL.

Part: DEFLECTOR — CRACKED (LT WING) · airframe 64,043 hrs · 46,120 cycles

CRACKED DEBRIS DEFLECTOR AT LT WING T/E WING STA XCW=60. HFEC INSPECTION 1 CRACK WAS FOUND OF 2.064" IN LENGTH, CRACK STOPPED, HFEC WAS PERFORMED ON HOLES, NO CRACKS WERE FOUND AND DEBRIS DEFLECTOR WAS REPAIRED IAW NDTSPM 06-10-01.001, SRM 57-09D, FIG 42.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACKED FRAME CLIP, STA Y=1437 BETWEEN LONGERON 2LT TO 3LT AT AFT ACCESSORY COMPARTMENT. FRAME CLIP WAS REPLACED IAW SRM 53-14-4; 51-30-5; 51-10-2 AND 51-10-4.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACKED FRAME CLIP, STA Y=1446 CANT BETWEEN LONGERON 17LT TO 18LT AT AFT ACCESSORY COMPARTMENT. DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2, 53-03, FIG 3, DWG 9911859-85.

Part: FORMER — CRACKED (VERTICAL STAB) · airframe 64,043 hrs · 46,120 cycles

CRACKED FORMERS ON STA ZFS=23 AND ZFS=43 AT VERTICAL STABILIZER L/E RT SIDE. RIBS WERE REPAIRED IAW SRM 55-02, FIG 27. HFEC WAS ACCOMPLISHED ON FORMERS ON STA ZFS=23 AND ZFS=43 AT VERTICAL STABILIZER L/E RT SIDE NO CRACKS WERE FOUND AFTER STOP DRILL IAW NDT SPM 06-10-01.001.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 64,043 hrs · 46,120 cycles

DELAMINATION ON LOWER SKIN OTBD GUIDE VANE, OTBD FLAP AT RT WING. LOWER SKIN OTBD GUIDE VANE, OTBD FLAP AT RT WING WAS REPAIRED IAW SRM 57-03D, PAR 11.

Part: WEB — CRACKED (FUSELAGE) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON WEB FROM STA Y=1361 TO CANT 1485 AT VENTRAL STAIRWAY SHROUD ACCESSORY COMPARTMENT. THE MEASURES AFTER REMOVED CORROSION ON AREAS LOCATED AT STA 825.808, 905.902 + 11", MEASURE REMAINING THICKNESS AFTER REWORK IS 0.038" AND ORIGINAL THICKNESS IS 0.040", THEREFORE IS WITHIN LIMITS IAW ERA 511165-14MA, REV C. THE SECTION LOCATION 905.902+11" AT STA 960.000 MUST BE REPAIRED BECAUSE THE CRACKS ARE WITHIN LIMITS. THE AREA OUT OF LIMITS WAS REPAIRED IAW SRM 53-01, FIG 4, SHEET 4, PAGE 25 AND 51-30-2 EQ 38DLP-90-SM-U-MT-E-ES EXP DATA 22-JUL-16 N/C 1201 AND TRANSDUCER V260-RM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON INTERCOSTAL BETWEEN Y=1231 AND Y=1212, ABOVE LONGERON 29 LT AT C3 COMPARTMENT. INTERCOSTAL WAS REPLACED IAW DWG 5936071, REV W, SRM 51-30-2, 51-10-3, PAR 21, 14.

Part: FITTING — CRACKED (EMERGENCY EXIT) · airframe 64,043 hrs · 46,120 cycles

CRACKED CLIP ON FWD, UPPER INTERNAL STRUCTURE AT RT FWD EMERGENCY EXIT DOOR. CRACKED CLIP ON FWD, UPPER INTERNAL STRUCTURE WAS REPLACED IAW SRM 51-30-5 AND 51-30-2 AND DWG 9957735, REV G.

Part: ANGLE — CRACKED (SERVICE DOOR) · airframe 64,043 hrs · 46,120 cycles

CRACKED ANGLE ON BEAM, NR 1 FWD EDGE AT FWD GALLEY SERVICE DOOR. ANGLE WAS REPLACED IAW SRM 51-30-4, 51-30-5, 51-10-2, 51-10-3, PAR 14 AND 21 AND DWG 9911579, REV L.

Part: PAN — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACKED INNER PAN ON FWD EDGE AND BEAM NR 1 AT FWD CARGO COMPARTMENT DOOR. DAMAGE ON PAN, CRACKS 0.-906" AND 1.375" WERE STOPPED IAW SRM 51-01, PAR 21. NOTES: NEW DOUBLER WAS FABRICATED IAW SRM 52-03D, FIG 8 AND 51-10-2. WEIGHT REPAIR PARTS=0.992 LB, NEW DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-30-5, AND ERA 539918-14, REV ORIGINAL.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 64,043 hrs · 46,120 cycles

CRACK ON INTERCOSTAL NR 3 BETWEEN BEAM NR 4 AND 5 AT FORWARD MAIN ENTRY PASSENGER DOOR. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 64,043 hrs · 46,120 cycles

DELAMINATION ON UPPER SKIN AT INBD GUIDE VANE, STA XV2=169 OF RT OTBD FLAP. UPPER SKIN AT INBD GUIDE VANE STA XV2=169 OF RT OTBD FLAP WAS REPAIRED IAW SRM 57-03D, PAR 11 AND CARD 2000-8149-04.

Part: STRINGER — CRACKED (RT WING) · airframe 64,043 hrs · 46,120 cycles

CRACK OF 0.750" APPROXIMATELY WAS FOUND ON STR 17 AT RT LOWER WING XCW=12. STRINGER WAS REPAIRED IAW ER/A 546524-14, REV ORIGINAL AND ER/A 546518-14, REV ORIGINAL.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON WEB SURFACE STA Y=1218 BETWEEN LONGERONS 26 AND 25RT AT CARGO DOOR JAMB. REPAIRED IAW SRM 51-70-4, FIG 2.

Part: FITTING — CRACKED (R1 DOOR) · airframe 64,043 hrs · 46,120 cycles

CRACKED R1 DOOR AFT EDGE FITTING. FITTING WAS REPLACED IAW SRM 51-30-5, 51-10-3, PAR 14 AND 21, 51-10-1 AND DWG 9911579, REV L.

Part: FRAME — WORN (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

WEAR ON FRAME STA Y=1510 CANT AFT FACE BETWEEN 5 HRS TO 6 HRS AT AFT ACCESSORY COMPARTMENT. FRAME LOWER RT SIDE WAS REPLACED IAW SRM 51-30-2, SRM 51-10-4, SRM 51-10-3 PAR 14.21 AND DWG 9911843, REV AC.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON PREVIOUS REPAIR UNDER AFT LAVATORY SERVICE PANEL ACCESS AT FUSELAGE SKIN. AREA WAS REPAIRED IAW ER/A 547808-14, REV ORIGINAL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACKED LONGERON 12 LT, STA Y= 1437 AT AFT ACC COMPARTMENT. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: TAB — DAMAGED (RUDDER) · airframe 64,043 hrs · 46,120 cycles

PART RACKS DAMAGED, METALLIZED ON RUDDER CONTROL TAB. METALLIZED ON RUDDER CONTROL TAB WAS REPAIR IAW SRM 51-70-1A-D, PARA 23.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

OUT OF LIMITS FOR THICKNESS REMAIN ON PREVIOUS BLEND OUT, STA Y= 355 BETWEEN LONGERON 18 LT TO 19 LT AT OUTER FUSELAGE SKIN. AREA OUT OF LIMITS WAS REPAIRED. PERFORMED GENERAL VISUAL INSPECTION, INITIAL 8000 CYCLES REPETITIVE EVERY 8000 CYCLES IAW SRM 53-04-2.

Part: SKIN — DENTED (CARGO DOOR) · airframe 64,043 hrs · 46,120 cycles

DENTS ON OUTER SKIN, 5 EA BETWEEN BEAM 4 AND 5 AT FWD CARGO COMPARTMENT DOOR. DENTS WERE ATTENDED WITH ER/A 547800-14MA, REV ORIGINAL.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 64,043 hrs · 46,120 cycles

CRACK ON PRODUCTION DOUBLER AT C3 DOOR EXTERNAL HANDLE CUTOUT. CRACKED PRODUCTION DOUBLER WAS REPLACED IAW SRM 52-05D, FIG 30 AND 51-30-5 HFEC WAS PERFORMED, NO CRACKS WERE FOUND ON NEW DOUBLER.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

DELAMINATION ON FLOOR PANELS 769D, 693B, 389C, 313B, 541D, 465D, 617C, 541C AND 313C. FLOOR PANEL 541C, 465D, 617C, 389C AND 313C WERE FABRICATED IAW AMM 53-20-01-201. FLOOR PANEL 693B, 541D AND 313B ONLY 1 DAMAGE IN FERRULE AND THIS WAS INSTALLED IAW AMM 53-20-01-201. FLOOR PANEL 769D WAS ATTENDED WITH NON-ROUTINE TASK CARD NR 001-0720:2000-2636/050, SN 1376. FLOOR PANEL 693B WAS REPAIR IAW AMM25-00-00-801.

Part: FORMER — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACKED RT FORMER FWD FACE STA Y = 936, X= -6 A PROXY KEELBEAM AREA. CRACK WAS ATTENDED IAW SRM 53-05D, FIG 810D AND 51-30-5.

Part: DOUBLER — DAMAGED (CARGO DOOR) · airframe 64,043 hrs · 46,120 cycles

WORN AND BENT PREVIOUS PAN REPAIR DOUBLER STA Y= 1154 BETWEEN BEAM 1 AND 2 AT C3 DOOR. WORN AND BENT PREVIOUS PAN REPAIR DOUBLER STA Y= 1154 BETWEEN BEAM 1 AND 2 AT C3 DOOR WAS REPLACED IAW SRM 52-05, FIG 26B, SRM 51-30-1 AND SRM 51-30-2.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACKED LONGERON 9 RT, STA Y=1431, CANT AT AFT ACC COMPARTMENT. NEW LONGERON WAS REPLACED IAW SRM 51-30-2 AND 51-30-5. HFEC 01, CRACK OF 0.2" OF LENGTH ON LONGERON IAW NDT SPM 06-10-01.001.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

DENT ON FUSELAGE SKIN PREVIOUS DOUBLER REPAIR STA Y=256 BETWEEN AND LONGERON 19LT. REPAIR DOUBLER AND FILLER WERE REPLACED IAW ER/A 332142-14, REV A.

Part: SKIN — DENTED (CARGO DOOR) · airframe 64,043 hrs · 46,120 cycles

DENTS ON AFT COMPARTMENT DOOR EXTERNAL SKIN BETWEEN BEAM 3 AND 4, 5 E/A, BETWEEN STA Y=1193 AND 1211, C3. SEVERAL DENTS WERE MEASURED AND WAS ATTENDED WITH ER/A:547806-14, REV ORIGINAL. 10X AND DVI ON INTERNAL STRUCTURE WAS PERFORMED AND NO DAMAGE WAS FOUND IAW SRM 53-04-1, PAR 7E. HFEC INSPECTION WAS ACCOMPLISHED ON DENTS ON AFT COMPARTMENT DOOR EXTERNAL SKIN BETWEEN BEAM 3 AND 4, 7 EA, BETWEEN STA Y= 1155 AND 1174. NO CRACKS WERE FOUND IAW ER/A 547806-14, REV ORIGINAL.

Part: DOUBLER — DAMAGED (CARGO DOOR) · airframe 64,043 hrs · 46,120 cycles

WORN AND BENT PREVIOUS PAN REPAIR DOUBLER STA Y= 1212 BETWEEN BEAM 1 AND 2 ON C3 DOOR. WORN AND BENT PREVIOUS PAN REPAIR DOUBLER STA Y= 1212 BETWEEN BEAM 1 AND 2 ON C3 DOOR WAS REPLACED IAW SRM 52-05, FIG 26 B AND SRM 51-30-1 AND SRM 51-30-2.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACK ON CHANNEL AT FLOOR PANEL 693A. CRACK .165" WAS REPAIRED WITH SRM 53-05, FIGURE 131B.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACKED LONGERON 11 LT, STA Y=1431, CANT AT AFT ACCESSORY COMPARTMENT. LONGERON WAS REPLACED, LENGTH OF CRACK: 0.600" IAW SRM 51-30-2, 51-30-5, 51-10-4 AND 51-10-3, PAR 21, 14.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACKED INTERCOSTAL STA Y= 1497, CANT POS 10 HRS AT AFT ACCESSORY COMPARTMENT. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5 AND DWG 9911875, REV J.

Part: ACCESS DOOR — CORRODED (WING) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

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

Part: DOUBLER — CRACKED (LT MLG WW) · airframe 64,043 hrs · 46,120 cycles

CRACKED REPAIR DOUBLER ON FWD DOOR JAMB X=7, STA= 939 AT LT WHEEL WELL AREA. CHANNEL WAS REPLACED IAW SRM 51-10-4, SRM 51-30-2 AND SRM 51-30-5.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACKS ON CHANNEL AT FLOOR PANEL 389A. CRACKS .100", .125", .150" WERE REPAIRED IAW SRM 53-05, FIGURE 131B AND ER/A 481746-14, REV ORIGINAL.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON BARREL NUT HOLE NR 14 AT HORIZONTAL STABILIZER CENTER SECTION BOX STA XH= -7. CORROSION ON BARREL NUT HOLE 14 AT HORIZONTAL STABILIZER CENTER SECTION BOX STA XH=-7 WAS REPAIRED IAW ER/A 546502-14, REV ORIGINAL.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACK ON CHANNEL AT FLOOR PANEL 541A, CRACK .135" WAS REPAIRED IAW SRM 53-05, FIG 131B, SHEET 1.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

CRACK ON CHANNEL AT FLOOR PANEL NR 927E, CRACK .160" WAS REPAIRED IAW SRM 53-05, FIG 131B.

Part: BUSHING — CORRODED (WING) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

AWR HIDDEN DAMAGE: CORROSION ON LT UPPER T/E BUSHINGS, 10 EA BELOW HEATER BLANKET. BUSHINGS WERE REPLACED IAW PS-900-9-1, NR 06, PAR D, 1, A, SRM 51-30-10, PAR 7.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON LT BARREL NUT HOLES NR 14, 17 AND 26 AT HORIZONTAL STABILIZER UPPER SKIN. BOLTS AND BARREL NUTS 14, 17 AND 26 WERE REMOVED IAW SRM 51-30-0, BARREL NUT HOLES 14 & 26 WERE REPAIRED IAW ER/A 546501-14, REV ORIGINAL, AND BARREL NUT HOLE 17 WAS REPAIRED IAW ER/A 546514-14, REV ORIGINAL AND SRM 55-03, PARAGRAPH 30, FIG 32, BARREL NUT AND BOLTS WERE INSTALLED IAW SRM 51-30-0. BARREL NUTS WERE SEALED IAW SRM 51-20-0.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON BARREL NUT HOLE NR 14 AT HORIZONTAL STABILIZER CENTER SECTION BOX STA XH=7.234. CORROSION ON BARREL NUT HOLE 14 AT HORIZONTAL STABILIZER CENTER SECTION WAS REPAIRED IAW ER/A 546502-14, REV ORIGINAL.

Part: BUSHING — CORRODED (WING) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

AWR HIDDEN DAMAGE: CORROSION ON LT UPPER T/E BUSHINGS, 10 EA, BELOW HEATER BLANKET. BUSHINGS WERE REPLACED IAW PS-900-9-1, NR 06 PAR D, 1, A, SRM 51-30-10, PAR 7.

Part: SKIN — DAMAGED (RUDDER) · airframe 64,043 hrs · 46,120 cycles

DAMAGED METALLIZED COAT ON RUDDER RT, LT SIDES. SUMMARY METALLIZED COAT WAS REPAIRED IAW ERA 092613-14MA, REV A.

Part: FLOOR PANEL — CRACKED · airframe 64,043 hrs · 46,120 cycles

CRACK ON CHANNEL AT FLOOR PANEL NR 1003 F. CRACKS .125", .165" WERE REPAIRED IAW SRM 53-05, FIG. 131C, TREATED AND PAINTED IAW SRM 51-10-3 PARS. 14 AND 21, AND INSTALLED IAW SRM 51-30-2.

Part: DOOR FRAME — CORRODED (BS 375-417) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON DOOR JAMB BEAM, BS 375 TO 417 LONGERON 28R AT CARGO DOOR JAMB C1. SECTION OF DOOR JAMB WAS REPLACED IAW SRM 53-05, FIG 44A.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 64,043 hrs · 46,120 cycles

ONE CRACK WAS FOUND ON INBD UPPER HOLE OF THE HORIZONTAL STABILIZER RT REAR CAP. INBD UPPER HOLE WAS DRILLED TO SECOND OVERSIZE IAW SR09550032, REV B, BHEC INSPECTION WAS PERFORMED NO CRACKS WERE FOUND IAW DC-MD NDT SPM 01-10-01.003, SECOND OVERSIZE IS WITHIN TOLERANCE WITH SR09550032, REV. B, THEREFORE BUSHINGS WERE INSTALLED WITH ROUTINE 5510-01074-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 64,043 hrs · 46,120 cycles

NICKS ON FUSELAGE SKIN L1 HOOK CUTOUT PREVIOUS REPAIR. NICKS WERE REPAIRED IAW ETI-88-16-223 AND ER/A 546555-14 REV ORIGINAL.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 64,043 hrs · 46,120 cycles

LOST MATERIAL ON UPPER AND LOWER SKIN AT LT ELEVATOR DOUBLER SETTLEMENT AREA BS XHR 217. AREA WAS REPAIRED IAW SRM 55-01, FIG 4 AND SRM 51-30-8.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK ON FUEL ACCESS PLATE NR 1355C. ACCESS PLATE IS OUT OF LIMITS AND WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 397-403) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON CUSP WEB LOWER SURFACE OVER UPPER DOOR JAMB BEAM. BS 397 TO 403 X -51 TO X -57, LONGERON 18, RT CARGO DOOR JAMB C1. CORROSION WAS FOUND OUT OF LIMITS, AREA WAS REPAIRED IAW 53-05, FIG 131A-5, SHEET 1.

Part: FRAME — CRACKED (BS 1174) · airframe 64,043 hrs · 46,120 cycles

CRACK ON FRAME BS 1174 BETWEEN LONGERON 6 - 7L IN AFT CABIN PAX CEILING AREA. REPAIRED IAW ER/A 495237-14, REV-B.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCES DOOR NR 1410C. ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCES DOOR NR 1365C. REPLACED FUEL ACCESS PLATE.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR NR 1311C, ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCES DOOR NR 1371C. ACCESS PLATE WAS REPLACED.

Part: SUPPORT — CRACKED · airframe 64,043 hrs · 46,120 cycles

CRACKED SUPPORT ON AIR CONDITIONING "Y" DUCT. CRACKED SUPPORT ON AIR CONDITIONING Y-DUCT, WAS RESTORED, WELDED IAW ER/A 494638-14MA, REV B.

Part: FLOOR PANEL — PUNCTURED (NOT REPORTED) · airframe 64,043 hrs · 46,120 cycles

PUNCTURED FLOOR PANEL. FLOOR PANEL REPAIRED IAW AMM 25-00-00-801, PAR 3 D.

Part: FRAME — CORRODED (BS 1380) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON "T", FRAME BS 1380 PROYECTION LONGERON 27RT AT AFT ACC COMPARTMENT. FRAME WAS REPLACED IAW SRM 51-10-4, SRM 51-30-2, SRM 51-30-5 AND SRM 51-30-1.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCES DOOR NR 1357C. ACCESS PLATE WAS REPLACED.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 64,043 hrs · 46,120 cycles

DELAMINATION ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201 AND REPAIRED IAW AMM 25-00-00-801.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON COUNTERSINK ON FUEL ACCESS PLATE NR 1470C. ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON COUNTERSINK ON FUEL ACCESS PLATE NR 1462C. ACCESS PLATE WAS REPLACED.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON LT BARREL NUT HOLES NR 14, 17 AND 26 AT HORIZONTAL STABILIZER UPPER SKIN. BOLTS AND BARREL NUTS 14, 17 AND 26 WERE REMOVED IAW SRM 51-30-0, BARREL NUT HOLES 14 & 26 WERE REPAIRED IAW ER/A 546501-14, REV ORIGINAL, AND BARREL NUT HOLE 17 WAS REPAIRED IAW ER/A 546514-14, REV ORIGINAL AND SRM 55-03, PARA 30, FIG 32., BARREL NUT AND BOLTS WERE INSTALLED IAW SRM 51-30-0. BARREL NUTS WERE SEALED IAW SRM 51-20-0.

Part: INTERCOSTAL — CRACKED (BS 1271-1276) · airframe 64,043 hrs · 46,120 cycles

CRACK ON INTERCOSTAL LOWER SURFACE BETWEEN BS Y= 1271 TO 1276, X= 4 AT PAX CABIN. DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 1, 51-10-3, PAR 14 AND 21, 51-30-5.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR NR 1464C. ACCESS PANEL WAS REPLACED.

Part: BELLCRANK — CORRODED (RUDDER) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON RUDDER THROW LIMITER BELLCRANK AT AAC. BELLCRANK WAS REPLACED IAW AMM 20-30-01.

Part: WINDOW FRAME — CRACKED (BS 1079) · airframe 64,043 hrs · 46,120 cycles

CRACK ON RT WINDOW RING PAN FWD LOWER CORNER AT BS 1079. DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 122 ER/A 493648-14MA REV. A AND ER/A 487747-14MA REV. ORIGINAL.

Part: SKIN — DAMAGED (LT WING) · airframe 64,043 hrs · 46,120 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND, 7 DIFFERENT FASTENERS OF PSE, ON LOWER SKIN AT REAR SPAR BETWEEN XRS=163 TO 168 AT LT WING. THESE NRC IS ATTENDED WITH ER/A NR 546483-14AD, REV. ORIGINAL. THESE ER/A DOCUMENTS THE DEFERRAL OF THE SID INSPECTION DESCRIBED IN WC 5700-2231 UNTIL AN ALTERNATE METHOD IS DEVELOPED TO NDT INSPECT THE AREA. WILL BE MONITORED WITH LOG PAGE NR 2494531.

Part: CUSP WEB — CORRODED (BS 660-673) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON UPPER /LOWER RT CUSP WEB FROM BS 660 TO 673 X - 56 TO -60 DAMAGE WAS REPAIRED IAW SRM 53-05, FIGURE 131A-5 AND APPLIED CIC IAW SRM 51-10-3, PAR. 38. AND 51-30-2, 51-30-8.

Part: CUSP WEB — CORRODED (BS 1181-1189) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON UPPER /LOWER RT CUSP WEB FROM BS 1189 TO 1181 X 56. REPAIRED IAW SRM 53-05, FIG 131A-5, SHEET 1.

Part: TAB — DENTED (ELEVATOR) · airframe 64,045 hrs · 46,121 cycles

SEVERAL DENTS ON RT ELEVATOR CONTROL TAB. THE RH ELEVATOR TAB WAS REPLACED AND ITS INSTALLATION IS ACCOMPLISHED UNDER CARD 2730-4832. (LP2524153)

Part: CUSP WEB — CORRODED (BS 640-653) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON UPPER /LOWER RT CUSP WEB FROM BS 640 TO 653 X- 56 -60. REPAIRED IAW SRM 53-05 FIG. 131, 51-10-3 PAR. 14, 21 AND 38, 51-30-2, 51,-30-5.

Part: CUSP WEB — CORRODED (BS 696-672) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON UPPER RT CUSP WEB FROM BS 696 TO 672, X - 57. REPAIRED IAW SRM 53-05, FIG 131A-5 AND 131A-13, SRM 51-10-3 PAR. 14, 21 AND 38, AND SRM 51-30-2, 51-30-8.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON COUNTERSINK ON FUEL ACCESS PLATE NR 1363C. ACCESS PLATE 1363C WAS REPLACED.

Part: CUSP WEB — PUNCTURED (BS 1203) · airframe 64,043 hrs · 46,120 cycles

PUNCTURE ON LT CUSP WEB BS 1203 X 54. REPAIRED IAW SRM 51-01, PAR. 24, 51-10-3, PAR. 14 AND 21, 51-30-5.

Part: CUSP WEB — CORRODED (BS 1016) · airframe 64,043 hrs · 46,120 cycles

CRACK ON RT CUSP WEB BS 1016 X- 58 AT CPAX. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A.

Part: CUSP WEB — DAMAGED (BS 660-673) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON UPPER AND LOWER RT CUSP WEB FROM BS 660 TO 673 X - 56 -60 AT CPAX. DAMAGE WAS REPAIRED IAW SRM 53-05, FIGURE 131A-5 AND APPLIED CIC IAW SRM 51-10-3, PAR. 38. AND 51-30-2, 51-30-8.

Part: CUSP WEB — CORRODED (BS 503-520) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON UPPER, LOWER RT CUSP WEB FROM BS 503 TO 520 X - 57 . CUSP WEB REPLACED IAW SRM 51-10-3, PAR 14.21, SRM 51-10-4, SRM 51-30-2, SRM 51-30-5, SRM 51-30-1.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCES DOOR NR 1466C. ACCESS PLATE WAS REPLACED.

Part: PAN — CRACKED (BS 1060) · airframe 64,043 hrs · 46,120 cycles

CRACKED RT WINDOW RING PAN FORWARD LOWER CORNER AT BS 1060. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122, REF ER/A 493648-14MA, REV A.

Part: PAN — CRACKED (BS 788) · airframe 64,043 hrs · 46,120 cycles

CRACKED ON RING PAN RT SIDE ON UPPER FWD CORNER OF WINDOW 62 BS 788. RING PAN WAS REPAIR IAW SRM 53-05, FIG 122.

Part: PAN — CRACKED (BS 731) · airframe 64,043 hrs · 46,120 cycles

CRACKED ON RING PAN LT SIDE ON FWD LOWER CORNER AT WINDOW 55, BS 731. CRACK OF .165" ON RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122.

Part: PAN — CRACKED (BS 927) · airframe 64,043 hrs · 46,120 cycles

CRACKED ON RING PAN RT SIDE ON UPPER FWD CORNER OF WINDOW 76, BS 927. RING PAN WAS REPAIR IAW SRM 53-05, FIG 122.

Part: PAN — CRACKED (BS 1079) · airframe 64,043 hrs · 46,120 cycles

CRACKED ON RING PAN LT SIDE ON LOWER FWD CORNER OF WINDOW 91, BS 1079. CRACK OF .135" ON RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122.

Part: BOLT — DAMAGED (HORIZONTAL STAB) · airframe 64,043 hrs · 46,120 cycles

DAMAGED THREADS ON RT HORIZONTAL STABILIZER ATTACH POINT NR 3 EYE BOLT. RIGHT HORIZONTAL STABILIZER ATTACH POINT NR 3 EYEBOLT WAS REPLACED IAW CMM 27-30-2.

Part: FLOOR PANEL — DAMAGED (COCKPIT) · airframe 64,043 hrs · 46,120 cycles

BROKEN COCKPIT FLOOR BEHIND CENTER CONSOLE. FLOOR PANEL 120C WAS FABRICATED IAW AMM 53-20-01-201.

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON FLOOR PANEL 160G. FLOOR PANEL WAS FABRICATED IAW DWG 9957828.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK ON FUEL ACCESS PLATE NR 1303C. ACCESS PLATE WAS REPLACED.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 64,043 hrs · 46,120 cycles

DELAMINATED FLOOR PANEL. FLOOR PANEL FABRICATED IAW AMM 53-20 01-201.

Part: BEARING — FROZEN (RUDDER) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON SPLINES AND FROZEN BEARING AT RUDDER DRIVE TORQUE TUBE. RUDDER DRIVE TORQUE TUBE WAS REPLACED IAW AMM 27-20-03.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK ON FUEL ACCESS PLATE NR 1409C. ACCESS WAS REPLACED.

Part: DRIVE ASSY — CORRODED (RUDDER) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON SPLINES AT RUDDER DRIVE CRANK. RUDDER TORQUE TUBE CRANK WAS REPLACED IAW AMM 27-20-03.

Part: BUSHING — SCRATCHED (RT ELEVATOR) · airframe 64,043 hrs · 46,120 cycles

SCRATCH ON RT ELEVATOR ATTACH POINT BUSHING NR 2 001-0236:2730-4586/001 S/N: 01214. RIGHT ELEVATOR ATTACH POINT BUSHING NR 2 WAS REPLACED IAW CMM 27-30-2 AND DWG NR 5918028 ID:3, REV:M.

Part: FLOOR SUPPORT — CRACKED · airframe 64,043 hrs · 46,120 cycles

CRACK ON CHANNEL AT FLOOR PANEL 313A. CRACK WAS REPAIRED IAW SRM 53-05, FIG 131C, 51-10-3 PAR 14 AND 21, 51-30-2.

Part: CHANNEL — CRACKED · airframe 64,043 hrs · 46,120 cycles

CRACK ON CHANNEL AT FLOOR PANEL NR 256A LT. FLOOR PANEL WAS REPAIRED IAW SRM 53-05, PAR.145, 53-05, FIG 131C, 51-30-2, 51-10-3 PAR 14 AND 21.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 64,043 hrs · 46,120 cycles

DELAMINATION ON LOWER SKIN AT LT WING OTBD FLAP MID GUIDE VANE. CUT NEW WAS DONE AND DAMAGE WAS FOUND ON INTERNAL STRUCTURE THEREFORE IT IS OUT LIMITS IAW SRM 51-70-2D, PAR 6A AND SRM 57-03D, PAR 11. MID VANE WAS REPLACED.

Part: CUSP WEB — CORRODED (BS 451-459) · corrosion level 2 · airframe 64,043 hrs · 46,120 cycles

CORROSION ON UPPER /LOWER RT CUSP WEB FROM BS 451 - 459. X - 57. DAMAGE WAS REPAIRED IAW SRM 53-05, FIG 131A-14, 51-10-3 PAR 14 AND 21, 51-30-2.

Part: PAN — CRACKED (BS 1041) · airframe 64,043 hrs · 46,120 cycles

CRACK ON RT WINDOW RING PAN AFT LOWER CORNER AT BS 1041. REPAIR PARTS WERE INTALLED IAW SRM 51-30-2, 51-30-5 AND ERA 493648-14MA, REV. A.

Part: INTERCOSTAL — CRACKED (BS 1287-1309) · airframe 64,043 hrs · 46,120 cycles

CRACKED INTERCOSTAL X=0 BETWEEN BS 1287 AND 1309. NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-30-1.

Part: TAB — DENTED (LT ELEVATOR) · airframe 64,043 hrs · 46,120 cycles

INITIAL, SEVERAL DENTS ON ANTI-FLOAT TAB ON LT ELEVATOR, LT ELEVATOR ANTI-FLOAT TAB WAS REPLACED AND ITS INSTALLATION WAS ACCOMPLISHED UNDER JOB 001-0235, CARD 2730-4334.

Part: TAB — DENTED (LT ELEVATOR) · airframe 64,043 hrs · 46,120 cycles

DENTS ON GEARED TAB ON LT ELEVATOR. THE LT ELEVATOR GEARED TAB WAS REPLACED AND ITS INSTALLATION IS ACCOMPLISHED UNDER CARD 001-0235:2730-4334.

Part: TAB — DENTED (LT ELEVATOR) · airframe 64,043 hrs · 46,120 cycles

SEVERAL DENTS ON CONTROL TAB ON LT ELEVATOR. THE LT ELEVATOR TAB WAS REPLACED AND ITS INSTALLATION IS ACCOMPLISHED UNDER CARD 2730-4334.

Part: TAB — DENTED (RT ELEVATOR) · airframe 64,043 hrs · 46,120 cycles

SEVERAL DENTS ON RT ELEVATOR ANTI-FLOAT TAB. RT ELEVATOR ANTI-FLOAT TAB WAS REPLACED AND ITS INSTALLATION IS ACCOMPLISHED UNDER CARD 001-0239:2730-4832.

Part: TAB — DENTED (RT ELEVATOR) · airframe 64,043 hrs · 46,120 cycles

SEVERAL DENTS ON RT ELEVATOR GEARED TAB. THE RT ELEVATOR GEARED TAB WAS REPLACED AND IT INSTALLATION ON THE ACFT IS ACCOMPLISHED UNDER CARD 001--0239:2730-4832.

Part: SPAR — CRACKED (RT WING) · airframe 62,851 hrs · 45,293 cycles

RIGHT WING, BS 164 AFT LOWER SPAR CHORD CRACKED AT FLAP HINGE LOWER INBD ATTACH STUD. FOUND DURING HFEC. REWORKED IAW AMDS 5710-01110-06 AND ER/A 541737-14AD, ORIGINAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,443 hrs · 44,990 cycles

ACFT AFT CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. BATTERY AND CHARGER WAS REPLACED. CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,436 hrs · 44,985 cycles

ACFT MAINTENANCE FOUND SEAT 1-12 AISLE EMERGENCY LIGHTS INOPERATIVE. THE POWER SUPPLY WAS R & R. CHECKED OK.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 62,427 hrs · 44,980 cycles

MAINTENANCE FOUND THE LAST 5 ROWS OF THE CABIN AND TAIL CONE AREA EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED A FUSE. CHECKED OK.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 62,427 hrs · 44,980 cycles

ACFT EMERGENCY LIGHTS FOUND INOPERATIVE IN FIRST CLASS & BACK 10 ROWS. MAINTENANCE REPLACED RACK AT SEAT ROW 2 CD AND R & R FUSES AT AFT RACK 35DE. CHECKED OK.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 61,122 hrs · 44,085 cycles

MAINTENANCE FOUND FOUND EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. WIRING AT SEAT 29DE WAS REPAIRED IAW SPWM CHAPTER 20.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,287 hrs · 43,528 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT SEAT 3D WERE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: SKIN — CRACKED (BS 1463) · airframe 60,023 hrs · 43,345 cycles

CRACK IN FUSELAGE SKIN AND ATTACH ANGLE, FWD SIDE OF BS 1463 AT L-31. TAIL INTERIOR. REPAIRED IAW PRI530096-14, REV 1.

Part: FRAME — CRACKED (BS 1463) · airframe 60,023 hrs · 43,345 cycles

RIGHT VENT BOX FRAME BS 1463, AFT SIDE WEB CRACKED AT FASTENER AT 0200 POSITION. FRAME REPAIRED ON PRI/ERA 530243-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1485) · airframe 60,023 hrs · 43,345 cycles

CRACKED FRAME WEB AND INNER FRAME FLANGE, AFT SIDE OF BS 1485 . TAIL INTERIOR. REPAIRED IAW PRI 530093-14, REV 0 AND COMPLY WITH ERA 530093-14, REV ORIG.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,938 hrs · 43,294 cycles

LEFT AND RIGHT FUSELAGE EMERGENCY LIGHTS INOPERATIVE. INSTALLED NEW BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-53-00.

Part: LIGHT — INOPERATIVE (SEAT 28 DE) · airframe 59,938 hrs · 43,294 cycles

SEAT 28 DE, EMERGENCY LIGHT INOPERATIVE. REMOVED AND INSTALLED NEW AISLE SEAT LIGHT ASSY OPS CHECKED GOOD IAW AMM 33-53-01.

Part: LANYARD — DETACHED (R1 DOOR SLIDE) · airframe 58,811 hrs · 42,475 cycles

R1 DOOR ARMING LANYARD CAME LOOSE FROM SLIDE. MAINTENANCE REINSTALLED 1R DOOR GIRT BAR CABLE IAW AMM 25-62.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,297 hrs · 42,146 cycles

DURING SERVICE CHECK, NOTED THE SEAT MOUNTED EMERGENCY PATH LIGHTS AT SEATS 29DE AND 31DE WERE INOPERATIVE. REPLACED SEAT HARNESSES AT BOTH LOCATIONS IAW AMM 33-53 AND OPS CHECKED NORMAL.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 57,839 hrs · 41,860 cycles

DURING LINE CHECK, NOTED EXIT SIGN COVER OVER FORWARD RT OVERWING EXIT WAS MISSING. REPLACED EMERGENCY EXIT SIGN COVER AT RT OVERWING EXIT.

Part: LANYARD — DETACHED (GIRT BAR) · airframe 57,212 hrs · 41,402 cycles

THE FLIGHT CREW NOTED THAT THE R1 DOOR GIRT BAR LANYARD/CABLE HAD BECOME DETACHED FROM THE SLIDE COVER WHEN THE DOOR WAS BEING DISARMED. MX ATTACHED THE LANYARD TO THE SLIDE COVER ASSEMBLY IAW AMM 25-62.

Part: STRUCTURE — CRACKED (RT MLG DOOR) · airframe 56,464 hrs · 40,915 cycles

DURING SCHEDULED INSPECTION, THE RT MLG DOOR INTERCOSTAL WAS FOUND TO BE CRACKED 11" FROM THE FWD EDGE AND 13" FROM THE TOP OF THE DOOR. THE CRACKED INTERCOSTAL WAS REPLACED IAW SRM 51-30-2, FIGURE 6, AMM 20-10-15-201 STEP 5A 1 & 3, AND AMM 20-10-15-201 STEP 5B 2-7.

Part: FLOORBEAM — CORRODED (BS 1212) · airframe 56,464 hrs · 40,915 cycles

DURING SCHEDULED INSPECTION, THE AFT CARGO BAY FLOOR SUPPORT WAS NOTED TO HAVE AREAS OF CORROSION FROM STATION 1212 AT 28L TO 28R. CORROSION WAS DETERMINED TO BE OUT OF LIMITS AND THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-4, FIG 3 AND 3A, 51-30-2 & 51-30-5 STEP 7.

Part: SUPPORT BEAM — DAMAGED · airframe 56,464 hrs · 40,915 cycles

DURING SCHEDULED INSPECTION, THE LOWER T/E CAVITY AT THE FWD LOWER MLG CUTOUT PANEL SUPPORT WAS NOTED TO HAVE CORROSION ON FWD FACE AND THE AFT FACE IS GOUGED 14" AFT OF REAR SPAR STA XRS 86. DAMAGED SUPPORT BEAM WAS REPLACED IAW SRM 51-30-03.

Part: LANYARD — CORRODED (TAILCONE) · airframe 56,464 hrs · 40,915 cycles

DURING SCHEDULED CHECK, THE TAIL CONE SLIDE TOGGLE PIN WAS NOTED TO HAVE SURFACE RUST. A NEW TAIL CONE SLIDE DEPLOYMENT LANYARD ASSY WAS INSTALLED IAW AMM 25-62-01-201 AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: FLOORBEAM — CRACKED (BS 1231) · airframe 56,464 hrs · 40,915 cycles

DURING SCHEDULED INSPECTION, THE FLOOR SUPPORT FRAME IN THE AFT CARGO BAY AT STATION 1231 BETWEEN L28R & 29R WAS FOUND CRACKED. THE AFT CARGO BAY CRACKED FLOOR SUPPORT FRAME WAS REPLACED IAW SRM REFS: 51-30-2, 51-30-5 & 51-10-4.

Part: BOTTLE — LOW PRESSURE (L1 DOOR SLIDE) · airframe 56,464 hrs · 40,915 cycles

DURING SCHEDULED CHECK, THE L1 DOOR SLIDE PRESSURE WAS FOUND TO BE OUT OF THE "GREEN" ACCEPTABLE PRESSURE RANGE. THE SLIDE WAS REPLACED IAW AMM 25-62-00-201, PARA 2. INSTALLATION INSPECTION COMPLETED ON WC 5200-0572.

Part: PIN — STIFF (L1 DOOR SLIDE) · airframe 56,464 hrs · 40,915 cycles

DURING SCHEDULE CHECK, THE L1 SLIDE TOGGLE PIN WAS NOTED TO BE STIFF. THE L1 TOGGLE WAS REPLACED IAW AMM 25-62-00-201, PARA B(4) & (11) AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 56,464 hrs · 40,915 cycles

DURING SCHEDULED CHECK, CORROSION WAS FOUND ON THE AFT CARGO BAY THRESHOLD IN MULTIPLE LOCATIONS. THE DISCREPANCY INDICATED NO ALLOWABLE DAMAGE LIMITS WERE NOTED IN THE SRM. REPAIRS COMPLETED IAW SRM 53-05 PARA 140, FIGURE 123.

Part: PIN — STIFF (L2 DOOR SLIDE) · airframe 56,464 hrs · 40,915 cycles

DURING SCHEDULED INSP, THE L2 DOOR SLIDE TOGGLE PINS WERE NOTED TO BE STIFF WHEN INSPECTED. THE L2 SLIDE TOGGLE WAS REPLACED IAW AMM 25-62-00-201, PARA 2, STEPS D (4) & (8). THE REQUIRED INSPECTION WAS COMPLETED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,464 hrs · 40,915 cycles

DURING LINE MX, MX NOTED GROUND DAMAGE ON THE FWD EDGE SKIN OF THE MID (C-2) CARGO DOOR CUTOUT. DAMAGE WAS REPAIRED IAW ER/A 514326-14 AND THE REQUIRED INSPECTION WAS ACCOMPLISHED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,451 hrs · 40,241 cycles

DURING LINE CHECK, MX FOUND THAT BOTH OF THE OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: RECEPTACLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,214 hrs · 40,072 cycles

DURING SERVICE CHECK, MX ROW 15D EMERGENCY LIGHT INOPERATIVE. R & R SEAT MOUNTED EMERGENCY LIGHT RECEPTACLE. OPS CHECKED GOOD.

Part: LANYARD — MISROUTED (L1 DOOR SLIDE) · airframe 54,840 hrs · 39,818 cycles

L1 DOOR SLIDE LANYARD INCORRECTLY ROUTED AND FRAYED. REPLACED L1 DOOR SLIDE LANYARD PER MD88 AMM 25-62.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,995 hrs · 39,258 cycles

DURING SERVICE CHECK, MAINTENANCE FOUND SEAT 33D EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SEAT HARNESS AND LIGHT ASSEBLY PER AMM. OPERATION CHECKS GOOD.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 53,291 hrs · 38,834 cycles

TOOLING DAMAGE ON RT VERTICAL STAB STA ZFS=56 DAMAGE. REPAIRED ON ERA 499262-14AD.

Part: RELEASE SYSTEM — FAILED (TAILCONE) · airframe 53,291 hrs · 38,834 cycles

THE TAIL CONE RELEASE FUNCTIONAL TEST FAILED OPN 6908. THE PULL TEST SCALE READ 30 LBS, WHICH EXCEEDS ALLOWABLE LIMITS. (NO CORRECTIVE ACTION IDENTIFIED. TO144 2012-D0038)

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 53,291 hrs · 38,834 cycles

DURING PSV VISIT IN MSP, AN ELONGATED HOLE WAS FOUND ON RT SIDE OF STABILIZER L/E SKIN STA ZFS 56. FOUND WHILE ACCOMPLISHING OPS 1008. REPAIR ACCOMPLISHED ON ERA 499268-14AD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,288 hrs · 38,833 cycles

DUE ERA 481744-14 REV O CODE 5331-20. INSPECT AT THE FUSELAGE SKIN LEFT STATION 522-541, 560-579, 617-636 AND 636- 655 WINDOW BELT. COMPLIED WITH ERA 481744-14 REV ORIG. NO CRACKS FOUND PER SECTION 1 AND 2, STEPS 1, 2 AND 3. INSTALLED ID TAGS PER DAL PS900-5-2 NO 4. COMPLIED WITH STEP 4 PER SECTION 1 AND 2 OF ERA 481744-14 REV ORIGINAL. REF N/R 1.

Part: TRANSMITTER — MALFUNCTIONED (AC PACK) · airframe 51,729 hrs · 37,843 cycles

FLIGHT CREW NOTICED LEFT AIR CONDITIONING PACK INDICATOR READ 45 PSI (MAXIMUM IS 28 PSI). FLIGHT CREW TURNED OFF PACK. STILL READ 20 PSI. CREW ALSO NOTICED FAINT, HOT BURNING OIL SMELL ON CLIMBOUT. MAINTENANCE REPLACED LEFT AIR CONDITIONING SUPPLY PRESSURE TRANSMITTER PER AMM. UNABLE TO DUPLICATE SMELL ON GROUND. CREW COMMITTED THAT THERE WAS NO SMELL DURING CRUISE OR APPROACH. AIRCRAFT OK FOR SERVICE.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 49,878 hrs · 36,699 cycles

DURING LINE CHECK MX FOUND EMERGENCY LIGHT AT 27D TO BE INOPERATIVE. MX RE-SECURED PULLED WIRE FROM HARNESS. OPS OF THE LIGHT NOW CHECKS OK.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,881 hrs · 36,702 cycles

DURING LINE CHECK MX FOUND ALL ESCAPE PATH LIGHTS INOPERATIVE AFT OF ROW 31. MX RE-SECURED PULLED WIRE FROM SEAT 36F AND REPLACED FUSE IN BATTERY PACK BS-212. OPS OF LIGHTS NOW CHECKS GOOD.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 49,207 hrs · 36,237 cycles

PITTING, CORRODED UPPER BARREL NUT HOLE UPPER MID HORTZ PLATE. NR 13 BARREL NUT HOLE WAS REAMED, BUSHING INSTALLED IAW ERA 4 81750-14 REV ORIG. (DLM88101406)

Part: SKIN — CORRODED (BS 1150-1154) · corrosion level 2 · airframe 49,207 hrs · 36,237 cycles

CORROSION ON FUSELAGE SKIN STA 1150-1154, BTW L29RT AND L29LT. REPAIR ACCOMPLISHED REPAIR IAW 481749-14 REV.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 49,207 hrs · 36,237 cycles

PITTING CORROSION INSIDE BARREL NUT BORE UPPER MID PLATE RT HORTZ STAB BOX. BORE OF NR 13 BARREL NUT HOLE CORRODED. REMOVED AND REPAIRED IAW ERA 481750-14 REV ORIG. (DLM88101402)

Part: STRUCTURE — MISREPAIRED (BS 586 S22R) · airframe 49,207 hrs · 36,237 cycles

EXISTING REPAIR ST STA 586 STRINGER 22R EXCEEDS PROXIMITY REQUIREMENTS OUTLINED IN THE SRM RULES REPAIR IAW 53-04D, FIG 12B. (DLM88101409)

Part: SUPPORT FITTING — CORRODED (MLG) · corrosion level 2 · airframe 49,207 hrs · 36,237 cycles

PITTING, CORROSION ON GEAR SUPPORT FITTING BUSHING BORE. FABRICATED AND INSTALLED BUSHING IAW ERA 481737-14 AD REV ORIG AND EA 09-093885-03 AD REV B. (DLM88101408)

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,207 hrs · 36,237 cycles

CORROSION ON FWD DOOR JAMB PAN, PREVIOUS REPAIR STA Y=370 BTW LONGS 28RT AND 26 RT REPAIR IAW 53-05D, FIG 804D.

Part: SKIN — CORRODED (BS 579-587) · corrosion level 2 · airframe 49,207 hrs · 36,237 cycles

EXFOLIATION CORROSION ON FUS SKIN STA 579-587 BTW LONGS 30 AND 29 LT. REPAIR IAW SRM 53-04D FIG 12C.

Part: SKIN — DAMAGED (RUDDER) · airframe 49,207 hrs · 36,237 cycles

DAMAGED METALLIZED ON RUDDER SKIN REPAIR IAW OPN 1031. (DLM88101401)

Part: DOOR FRAME — CORRODED (BS 1155-1212) · corrosion level 2 · airframe 49,207 hrs · 36,237 cycles

CORROSION LWR DOOR JAMB BEAM PREVIOUS REPAIR STA1155-1212. REPAIR WAS ACCOMPLISHED IAW SRM 53-05, FIG 123. (DLM88101399)

Part: ATTACH FITTING — CORRODED (TAILCONE) · corrosion level 2 · airframe 49,207 hrs · 36,237 cycles

RUSTED ATTACH HARDWARE TAILCONE RELEASE CABLE. HARDWARE REPLACED IAW AMM20-30-201.

Part: FRAME — DAMAGED (BS 560-579) · airframe 49,207 hrs · 36,237 cycles

LIGHTNING STRIKE ON WINDOW BELT FRAME LOWER EDGE STA Y=560 TO 579 REPAIR PER ERA 481744-14 REV ORG (DLM88101404)

Part: WINDOW FRAME — DAMAGED (BS 617-636) · airframe 49,207 hrs · 36,237 cycles

LIGHTNING STRIKE ON WINDOW BELT FRAME FWD AND AFT EDGE STA Y=617 TO 636. REPAIR IAW ERA 481744-14, REV ORG. (DLM88101405)

Part: WINDOW FRAME — DAMAGED (BS 636-655) · airframe 49,207 hrs · 36,237 cycles

LIGHTNING STRIKE ON WINDOW BELT FRAME FWD AND AFT UPPER EDGE STA Y=636 TO 655 REPAIR IAW ERA 481744-14.

Part: WINDOW FRAME — DAMAGED (BS 522-541) · airframe 49,207 hrs · 36,237 cycles

LIGHTNING STRIKE ON WINDOW BELT FRAME LOWER EDGE STA Y=522 TO 541 REPAIR IAW ERA 481744-14, REV ORG. (DLM88101403)

Part: PAN — CORRODED (AFT LAV) · airframe 48,170 hrs · 35,609 cycles

CORROSION AT LWR FWD CORNER OF AFT LAV PAN. CORROSION IN DOOR SURROUND DOUBLER. CUT OUT CORROSION AND INSTALLED REPAIR DOUBLER.

Part: WIRE — DAMAGED (CABIN) · airframe 47,643 hrs · 35,292 cycles

EMERGENCY TRACK LIGHT AT 39ED INOP, WIRE BROKEN. REPLACED ELECT CONNECTOR.

Part: A/C PACK — INOPERATIVE (LEFT) · airframe 46,354 hrs · 34,490 cycles

CABIN PRESSURE FAILED WHILE DESCENDING OUT OF FL 330. CABIN PRESSURE CLIMBED ABOVE 10K DURING DESCENT PASSENGER O2 MASKS DEPLOYED, FLOW LIGHT FLICKERED SEVERAL TIMES. MAINTENANCE IN PROGRESS, REMOVED AND REPLACED LT WATER SEPARATOR TEMAMM. REPLACED LT PNEU PILOT PRESS REG PER AMM REPLACED LEFT A/C PILOT PRESSURE REGULATOR PER AMM SN ON 5421. REPLACED PRSOV PER AMM. REMOVED AND REPLACED RT AC FLOW CONTROL VLV OPN AND GOOD.

Part: TURBINE — FAILED (NR 1 ENGINE) · airframe 41,551 hrs · 31,447 cycles

ON CLIMBOUT THROUGH 7000 FT LEFT ENG HAD A LOUD BANG, STALL EGT CLIMBED THROUGH 770 DEGREES. OIL PRESSURE INDICATED ZERO ENGINE STOPPED RUNNING- CREW COMPLETED ENGINE SEVERE DAMAGE SHUTDOWN CHECKLIST. AFTER ARRIVAL OIL QTY APPEARED NORMAL, MTC CONFIRMED REAR TURBINE FAILURE AND BLADES IN TAILPIPE. RMVD/REPL FIRE BOTTLE PER AMM-NDS CK OUT209056. REPLACED ENGINE PER TRANSMITTAL 9T102235979. COMPLETED CK-OUT OF FIR BOTTLE PER AMM.

Part: LAMP — INOPERATIVE (MLG INDICATOR) · airframe 36,395 hrs · 27,912 cycles

UPON GEAR EXTENSION, RT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE. C/W LANDING GEAR UNSAFE, GEAR HANDLE DOWN QRH. VISUAL CONFIRMED. RELAMPED INDICATOR LIGHTS.

Part: DRIVE BELT — WORN (CARGO LOADING) · airframe 36,258 hrs · 27,824 cycles

AFTER LIFTOFF, F/A`S REPORTED AN ODOR IN CABIN. ODOR DISSIPATED QUICKLY, HAD A BURNED RUBBER SMELL AND WAS STRONGEST IN THE FWD CABIN. BOROSCOPED NR 1 AND 2 ENGINE NR 3 BEARING AREA. NO WETTING FOUND. BOROSCOPED NR 1 AND 2 ENGINES AREA AROUND BURNER CAN. NO WETTING NOTED. INSPECTED APU INLET FOR CONTAMINATION, NONE NOTED. FOUND MID CARGO LOADING SYSTEM SOURCE OF RUBBER SMELL. BELTS ON DRIVE WORN AND BROKEN. REPLACED SAME.

Part: PRESSURE SWITCH — FAILED (APU) · airframe 36,254 hrs · 27,820 cycles

SMOKE IN COCKPIT AND CABIN IMMEDIATELY AFTER TAKEOFF. REPLACED APU OIL PRESSURE SWITCH.

Part: OIL FILTER — CLOGGED (NR 1 ENGINE) · airframe 35,104 hrs · 26,993 cycles

ON CLIMBOUT GOT FLICKERING MASTER CAUTION THEN LT OIL STRAINER CLOGGED MSG. FOLLOWED IAW. REPLACED OIL FILTER, NO METAL OR CARBON.

Part: DUCT — SEPARATED (PNEUMATIC SYS) · airframe 32,163 hrs · 24,967 cycles

LOUD NOISE AND VIBRATION IN FLOOR FROM AFT F/A SEAT ON BACK, STARTED WHEN POWER APPLIED DURING T/O RUN. SLIGHTLY MORE NOTICEABLE ON C/P SIDE DURING FLIGHT NOISE AND VIBRATION WOULD INCREASE AS POWER INCREASE AND DECREASE AS THROTTLE RETARDED. FOUND PNEUMATIC DUCT SEPARATED. REPAIRED SAME.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,659 hrs · 20,964 cycles

FOUND ON LAYOVER, AFT EXTERIOR EMERGENCY LIGHTS INOP. REPLACED OVERWING EXIT LIGHTS POWER SUPPLY AND BATTERY PACK PER M/M. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,430 hrs · 20,788 cycles

LT AND RT WING EXT EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, CKS OK.

Part: WHEEL — BROKEN (NR 3 MAIN)

INSPECTED WHEELS FOR PASSENGER COMPLAINT OF FLAT TIRE. FOUND NR 3 MAIN WHEEL DAMAGED ON INSIDE. ALSO, RUBBING BRAKE. INNER BEARING HUB FAILURE, AXLE HAD NO DAMAGE. REPLACED WHEEL AND BRAKE ASSY.

Part: LINE — LEAKING (RT MLG WW)

AT TOP OF CLIMB FL350, NOTICED RIGHT HYD RESV LOW QTY LIGHT WITH RT HYD QTY AT 4 THEN 3. ACCOMPLISHED HYD QTY LOW CK LIST. WHEN RT HYD PUMP TURNED OFF QTY INCREASED TO 19 AND STEADY. FOUND HYD LINE IN RT W/W ABOVE A/C HYD PUMP CHAFED AND LEAKING. REPAIRED, LEAK CKS OK. OPERATED FLT CONTROL WITH RT ENG RUNNING, ALL CKS GOOD.

Part: FRAME — CORRODED (BS 1271)

APPROX 13 OF THE FS 1271 LOWER FRAME WAS FOUND CORRODED BETWEEN L29L AND L29R. REPAIRED PER ERA 332208-14.

Part: SKIN — DENTED (BS 1210)

SKIN AND BEARSTRAP AT THE AFT EDGE OF THE C3 DOOR CUTOUT WAS DAMAGED. DAMAGE IS LOCATED AT FS 1210, 12 ABOVE THE TANGENT POINT AT THE LWR AFT CORNER. REPAIRED PER ERA 332210-14.

Part: SKIN — DENTED (BS 216)

DENT FOUND IN FUSELAGE SKIN AT FS 211 TO FS 216 JUST BELOW L17L. REPAIRED PER ERA 332143-14.

Part: SKIN — DENTED (BS 260)

DENT FOUND IN FUSELAGE SKIN AT FS 257 TO FS 265 BETWEEN L18L TO L19L. REPAIRED PER ERA 332142-14.

Part: FRAME — CRACKED (BS 1418)

CRACKS WERE FOUND ON THE STA 1418 FRAME AT L-2R AND L-2R ON THE STA 1418 FRAME. THE CRACKS WERE TYPICAL OF THOSE FOUND IN DAC S/B 53-184, REV 1. THE CRACKS WERE DUE TO FATIGUE DAMAGE. REPAIRED PER ER/A 332146-14.

Part: RELAY — INOPERATIVE (E/E COMPT)

ON T/O STABILIZER TRIM WENT TO FULL NOSE DOWN. REPLACED NOSE DOWN TRIM RELAY R20-13.

Part: ENGINE — VIBRATION (NR 2)

AT INITIAL LEVEL OFF AT 350 NOTICED VIBRATION THROUGHOUT COCKPIT. AFTER T/S PROBLEM WAS DETERMINED TO ONLY OCCUR WHEN RT N1 RPM WAS BETWEEN 82 AND 83 PERCENT. PROBLEM VIBRATION WAS CONTINOUS WITH RT N1 BETWEEN 82 AND 83 REGARDLESS OF LT ENG SETTING. RT EPR APPROX 1.8 EGT 430 N2 87.5 FF 2900. C/W BOROSCOPE OF 6TH, 7TH AND 13TH STAGE COMP BLADES 1ST STG HPT BLADES AND 1ST AND 2ND STG LPT BLADES. NO DISCREPANCIES. CHECKED MAIN OIL FILTER AND RAN BOTH ENGS AT DIFFERENT PWR SETTINGS SEVERAL TIMES. NO PROBLEMS OF VIBRATIONS NOTED.

Part: TIRE — FAILED (RT MLG)

NR 4 TIRE BLEW ON TAKEOFF DAMAGING RT MLG DOOR AND RT FLAP PART OF TIRE WAS IN RT ENG INLET. BORESCOPED RT ENG AND RANENG AT FULL PWR, ALL NORMAL. REPLACED NR 3 AND NR 4 MLG WHEEL ASSYS.

Part: SMOKE DETECTOR — MALFUNCTIONED (AFT LAV)

ON PUSH BACK, AFT LAV COPILOTS SIDE SMOKE ALARM WENT OFF. LIGHT SMOKE CAME INTO MID CABIN. APU HAD BEEN STARTED 11 MIN PRIOR TO PUSH BACK AND PACKS OPERATED 4 TO 5 MIN. BEFORE PUSH BACK PACK TEMP GAUGE AT 90 DEG. RETURNED TO GATE WITH PACKS OFF, HAD PAX DEPLANE. RAN LEFT/RIGHT PKS WITH APU AIR, NO SMOKE NOTICED. REPLACED RT REAR LAV SMOKE DETECTOR RAN PACKS WITH ENGINES RUNNING, NO SMOKE.

Part: SPRING — BROKEN (RT NLG DOOR)

EXCESSIVE AIR NOISE COMING FROM NOSE GEAR AREA AFTER DEPART. AIRCRAFT RETURNED TO LGA. FOUND RT UPPER LOCK LINK SPRING BROKEN. DAMAGED RT NOSE GEAR DOOR.

Part: EEL WIRE — BROKEN (CABIN)

EMERGENCY LIGHT AT SEAT 25D IS INOP. REPAIRED BROKEN WIRE ON TRACK LIGHT, CHECKS GOOD.