N613DL

Part: PAN — CRACKED (LAVATORY FLOOR) · airframe 92,435 hrs · 42,280 cycles

F/C LAVATORY FLOOR PAN HAS LARGE CRACK ALONG AFT WALL. REPLACED F/C LAV FLOOR PAN IAW ERA 06-494267-14MA.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 91,483 hrs · 41,938 cycles

INOPERATIVE EMERGENCY SLIDE BOTTLE HAS LOW PRESSURE. R & R SLIDE IAW JIC 7809.

Part: SKIN — DAMAGED (BS 529-610) · airframe 89,327 hrs · 41,198 cycles

LIGHTNING DAMAGE LWR FUSELAGE AT BS 610 - 529. REMOVED DAMAGE AT STA 610-529, STA 580 WITHIN LIMITS IAW SRM 53-10 TREATED AND PAINTED. REMOVED DAMAGE AT STA 590, 530 AND STA 560, 529, 712951. BHEC INSPECTED OPEN HOLES STA 590, STA 30 AND 560 STU 29 IAW SRM 53-00-01 WITH NO ITEMS. REPAIRED DAMAGE AT STA 590, 530 AND STA 560 529 IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 580-750) · airframe 89,327 hrs · 41,198 cycles

LIGHTNING DAMAGE, FWD FUSELAGE CROWN AT STA 750, RBL 52, STA 750, RBL 53, STA 630, LBL52 STA 620, LBL 52, STA 580, LBL 52. STA 750, RLR 52 AND LRL 53 AND STA 580, LBL 52 BLENDED FOUND TO BE WITHIN LIMITS IAW SRM 53-00, TREATED AND PAINTED. REMOVED DAMAGE, INSPECTED OPEN HOLE STA 630, STR 2L IAW SRM 53-00-01. REPAIRED STA 630, STR 2L IAW SRM 53-00, STA 620, LBL 52.

Part: SKIN — DAMAGED (BS 460-560) · airframe 89,327 hrs · 41,198 cycles

LIGHTNING DAMAGE FWD FUSELAGE CROWN AT STA 560, LBL 52, STA 490, LBL 52, STA 470 LBL, 52 STA 460, LBL 52. R & R DAMAGE, INSPECTED AND REPAIRED IAW SRM 53-00-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 89,327 hrs · 41,198 cycles

BS L20, LBL STR 1 HAS LIGHTNING STRIKE DAMAGE. DAMAGE MEASURES .045 DEEP. REMOVED DAMAGE IAW SRM 53-00-01 AND INSPECTED, NO CRACKS FOUND.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 87,790 hrs · 40,675 cycles

DR 2R EXIT LIGHT SIGN 2 BULBS INOP. RELAMPED DR 2R EMERGENCY EXIT SIGN. OK FOR SVC.

Part: LIGHT — BROKEN (SEAT 20D) · airframe 87,403 hrs · 40,515 cycles

MAINTENANCE DISCOVERED EMERGENCY LIGHT AT SEAT 20D BROKEN OFF. REPLACED LIGHT ASSEMBLY CHECKS OK.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 8,142 hrs · 38,316 cycles

DURING A SERVICE CHECK, MX FOUND THE LT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. MX REPAIRED THE WIRING. OPS CHECK WAS GOOD.

Part: INTERCOSTAL — CORRODED (BS 1400-1420) · airframe 76,343 hrs · 36,662 cycles

AFT CARGO COMPT BETWEEN STA 1400 THRU 1420 AT STR 28LT INTERCOSTAL HAS CORROSION ON FWD AND AFT SIDE AT LOWER LIP CP-53-153-01I. C/W AT SAA - SAT ON N/R 126682 JOB 82641000001.

Part: INTERCOSTAL — CORRODED (BS 620-640) · airframe 76,343 hrs · 36,662 cycles

FWD CARGO COMPT, RT SIDE STRUCTURE INTERCOSTAL AT STA 620 TO 640 S-21R EXFOLIATED CP 53-121-01. C/W AT SAA, SAT ON N/R 127276 JOB 82639630001.

Part: INTERCOSTAL — CORRODED (BS 740-760) · airframe 76,343 hrs · 36,662 cycles

FWD CARGO COMPT FLOOR STRUCTURE INTERCOSTAL STA 740-760 LBL 10.45 EXFOLIATED. C/W AT SAA, SAT ON N/R 127259 JOB 82640010001.

Part: SKIN — WORN (RT WING) · airframe 76,343 hrs · 36,662 cycles

CHAFING MARK (WORN) ON RIGHT WING LOWER SKIN SURFACE AT WS 321.5 DUE TO CONTACT WITH NR 2 PYLON ACCESS PANEL 445BR. C/W AT SAA, SAT ON N/R 127291 JBO 82638930001.

Part: INTERCOSTAL — CORRODED (BS 740-760) · airframe 76,343 hrs · 36,662 cycles

FWD CARGO COMPT FLOOR STRUCTURE INTERCOSTAL STA 740-760 RBL 16.10 FOUND CORROSION PREVIOUSLY BLENDED. C/W AT SAA, SAT ON N/R 127270 JOB 82640070001.

Part: SKIN — DENTED (BS 281 S17L) · airframe 76,343 hrs · 36,662 cycles

LT FUSELAGE STA 281 S17L MULTIPLE DENTS. C/W AT SAA, SAT ON N/R 103491 JOB 82630640001.

Part: SKIN — DENTED (BS 1610 S26R) · airframe 76,343 hrs · 36,662 cycles

RT LWR FUSELAGE STA 1610 S26R 1 EACH DENT. C/W AT SAA - SAT ON N/R 103479 JOB 82630610001.

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 76,343 hrs · 36,662 cycles

SHARP DENT ON AFT CARGO DOOR SKIN JUST AFT OF LOWER FRAMES SUPPORT RIB 5. C/W AT SAA - SAT ON N/R 103627 JOB 82632540001.

Part: SKIN — DAMAGED (BS 480) · airframe 76,343 hrs · 36,662 cycles

RT LWR FUSELAGE STA 480 S26R 1 DENT WITH CREASE. C/W AT SAA - SAT ON N/R 103572 JOB 82630430001.

Part: LONGERON — CORRODED (BS 1415) · airframe 76,343 hrs · 36,662 cycles

AFT CARGO COMPT STA 1415 LONGERON 29L HAS CORROSION CP53-155-01I. C/W AT SAA, SAT ON N/R 127284 JOB 82638440001.

Part: LONGERON — CORRODED (BS 1415) · airframe 76,343 hrs · 36,662 cycles

AFT CARGO COMPARTMENT STA 1415 LONGERON 29R HAS CORROSION. C/W AT SAA, SAT ON N/R 127283 JOB 82638460001.

Part: INTERCOSTAL — CRACKED (BS 860-879) · airframe 76,343 hrs · 36,662 cycles

MAIN CABIN STA 860 - 879 BL0 INTERCOSTAL UPPER ANGLE CRACKED AND BROKEN. C/W AT SAA - SAT ON N/R 127370 JOB 82639140001.

Part: MOUNT — GOUGED (ENGINE) · airframe 76,343 hrs · 36,662 cycles

NR 2 PYLON FWD OTBD ENG MOUNT HOLE INNER BORE IS DAMAGED GOUGED AT HOLE OPENING LWR SIDE AND HAS GROOVE (RING) IN CENTER OF BORE. C/W AT SAA - SAT ON N/R 118549 SAA JOB 82635410001 COMPLIED WITH ER/A 473675-14 REV 0.

Part: FLOORBEAM — CORRODED (BS 344) · airframe 76,343 hrs · 36,662 cycles

MAIN CABIN FLOORBEAM UPPER CAP SURFACE CORRODED AROUND FASTENER HOLES STA 344 LBL 10-LBL 20. REPLACED FLOORBEAM SECTION AT SAA SAT ON N/R CARD 127243.

Part: MOUNT — DAMAGED (BS 1685) · airframe 76,343 hrs · 36,662 cycles

3 ELONGATED HOLES MAIN CABIN AFT DECK PLATE STA 1685 LBL 51 LT FORWARD GALLEY MOUNT AREA. C/W ERA 474158-14 REV ORIG DATED 4/18/09 AT SAA SAT ON N/R CARD 126707.

Part: INTERCOSTAL — CORRODED (BS 740-760) · airframe 76,343 hrs · 36,662 cycles

FWD CARGO COMPARTMENT FLOOR STRUCTURE INTERCOSTAL STA 740-760 RBL 16.1 FOUND CORROSION PREVIOUSLY BLENDED, REPAIRED AT SAA SAT ON N/R CARD 127270.

Part: PAN — CORRODED (BS 700-720) · airframe 76,343 hrs · 36,662 cycles

FWD CARGO COMPT RT SIDE STRUCTURE LAV PAN EXFOLIATIED AROUND INLET STA 700 TO 720 S-20R TO S-23R. REPAIRED PER SRM 51-40-02 AT SAA IN SAT DURING HMV-4 ON N/R CARD 127347.

Part: INTERCOSTAL — CORRODED (BS 1420 S30) · airframe 76,343 hrs · 36,662 cycles

AFT CARGO COMPT STA 1420 LONGERON 30 INTERCOSTAL HAS CORROSION CP53-155-01I/REPAIRED AT SAA ON NRC126694 DURING HMV.

Part: FLOOR SUPPORT — DAMAGED (BS 1685 RBL 51) · airframe 76,343 hrs · 36,662 cycles

2 ELONGATED HOLES MAIN CABIN AFT DECK PLATE STA 1685 RBL 51 FWD OF GALLEY MOUNT AREA. REPLACED GALLEY MOUNT FITTING AND FLOOR SUPPORT PER SRM 51-40-05 DURING HMV AT SAA ON NRC 126708.

Part: STOP FITTING — NICKED (FWD CARGO DOOR) · airframe 76,343 hrs · 36,662 cycles

NICKED STOP PIN SUPPORT FITTING 1ST FROM THE BOTTOM AFT SIDE OF FWD CARGO DOOR. REPLACED STOP PIN FITTING DURING HMV AT SAA ON NRC114814.

Part: SKIN — DENTED (BS 690 S24R) · airframe 76,343 hrs · 36,662 cycles

RT LWR FUSELAGE STA 690 S24R 1 PROTRUDING DENT, C/W ERA 471188-14 REV ORIG DATED 4/18/09 AT SAA SAT ON N/R CARD 103584.

Part: SKIN — DENTED (BS 600 S15L) · airframe 76,343 hrs · 36,662 cycles

LT FUSELAGE STA 600 S15L MULTIPLE DENTS. REPAIRED DENT PER ERA473676-14REV ORG AT SAA DURING HMV ON NRC103493.

Part: SKIN — DENTED (BS 1681 S17R) · airframe 76,343 hrs · 36,662 cycles

RT FUSELAGE STA 1681 BELOW S17R 3 EACH DENTS. REPAIRED PER DELTA ERA 473673-14REV ORIG DURING HMV AT SAT ON NRC 103485.

Part: SKIN — CHAFED (NR 2 PYLON) · airframe 76,343 hrs · 36,662 cycles

CHAFING MARK (WORN) ON WING LOWER SKIN SURFACE AT WS321.5 DUE TO CONTACT WITH NR 2 PYLON ACCESS PANEL 445BR. REPAIRED PER ERA473679-14REVD DURING HMV AT SAA ON NRC127291.

Part: SKIN — DENTED (BS 620 S16L) · airframe 76,321 hrs · 36,651 cycles

ACCOMPLISH PERM REPAIR PER ERA468725-14REV ORIG ACTL LINE 2300 REF OMI LOG CN C06028120 FUSELAGE SKIN AND STRINGER STA620 STR16L DENTS C/W ERA468725-14REV ORIG DURING HMV AT SAT ON NRC120363.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 75,098 hrs · 36,243 cycles

ACB FLOOR PANEL BS 1330 TO 1460 HAS CORROSION ON TOP AND BOTTOM SURFACE. REMOVED AND REPLACED ACB FLOOR PANEL BS 1330-1460 IAW AMM.

Part: SKIN — CORRODED (FS 1690) · airframe 75,096 hrs · 36,241 cycles

FUSELAGE SKIN CORRODED AT AFT LAV SVC CUTOUT FS 1690, S-26R. SKIN BLENDED AND REINFORCED WITH AN EXTERNAL DOUBLER.

Part: CHANNEL — CORRODED (BS 1690) · airframe 75,096 hrs · 36,241 cycles

SUPPORT CHANNEL AFT OF AFT DUMP VALVE IS CORRODED BS 1690 RBL 24. REMOVED AND REPLACED SUPPORT CHANNEL DUE TO OUT OF LIMITS CORROSION.

Part: CHANNEL — CORRODED (BS 1685) · airframe 75,096 hrs · 36,241 cycles

CORROSION SUPPORT CHANNEL FWD OF AFT DUMP VALVE IS CORRODED BS 1685, RBL 14-24. REMOVED AND REPLACED SUPPORT CHANNEL DUE TO OUT OF LIMITS CORROSION.

Part: CHANNEL — CORRODED (BS1690) · airframe 75,096 hrs · 36,241 cycles

SUPPORT CHANNEL INBD OF AFT DUMP VALVE CORRODED ALL THE WAY THROUGH BS 1690 RBL 10. REMOVED AND REPLACED CHANNEL DUE TO OUT OF LIMITS CORROSION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,096 hrs · 36,241 cycles

FOUND SEVERAL EMERGENCY LIGHTS INOP IN PASSENGER COMPARTMENT. REMOVED AND REPLACED L-2 DOOR EMERGENCY LIGHTS BATTERY PACK, AND RELAMPED SEVERAL EMERGENCY LIGHTS PER AMM 33-51-07-902-001 AND PERFORMED SATISFACTORY OPS CHECK PER AMM 33-51-00-715-075.

Part: SKIN — CORRODED (BS 690 BL 0) · airframe 75,096 hrs · 36,241 cycles

DURING THE AGING AIRCRAFT INSPECTION, CORROSION WAS FOUND ON THE EXTERNAL SURFACE OF THE SKIN UNDERNEATH THE DME ANTENNA MOUNT AT STA 690 BETWEEN S-28L AND S-28R. THE CORROSION WAS REMOVED AND REPAIRED PER BOEING INSTRUCTIONS.

Part: SPLICE — CORRODED (FLOOR PANEL) · airframe 75,096 hrs · 36,241 cycles

CORROSION FWD CARGO BAY FLOOR PANEL SPLICE AT BS 748, RBL 13-20. REMOVED AND REPLACED SPLICE DUE TO CORROSION OUT OF LIMITS IAW SRM 51-40-02.

Part: SKIN — CORRODED (BS 536-630) · airframe 75,096 hrs · 36,241 cycles

DURING AN AGING AIRCRAFT INSPECTION, CORROSION WAS FOUND ON THE EXTERNAL SKIN UNDERNEATH THE ANTENNA MOUNTS AT STA 536 AND 630 BETWEEN S-28L AND S-28R. REPAIR WAS MADE PER BOEING INSTRUCTIONS.

Part: MOUNT — CORRODED (GALLEY) · airframe 75,096 hrs · 36,241 cycles

G1A GALLEY INBD MOUNT CORRODED. REPAIRED PER 51-30-01 ON NR 00136.

Part: MOUNT — CORRODED (GALLEY) · airframe 75,096 hrs · 36,241 cycles

G1A GALLEY AFT OUTBOARD GALLEY MOUNT CORRORED. REPAIRED ON NR 00142 PER 51-40-02.

Part: STIFFENER — CRACKED (BS 660 RBL 45) · airframe 75,096 hrs · 36,241 cycles

WEB STIFFENER CRACKED AT STATION 660 RBL 45. REPAIRED PER SRM 51-40-01 ON NR 00098.

Part: STIFFENER — CRACKED (BS 660) · airframe 75,096 hrs · 36,241 cycles

VERTICAL STIFFENER CRACKED AT STA 660 RBL 25. REPAIRED ON NR 00097 PER 51-20-01.

Part: STIFFENER — CRACKED (BS 680) · airframe 75,096 hrs · 36,241 cycles

VERTICAL WEB STIFFENER CRACKED AT STATION 680 RBL 25. REAPAIRED ON NR 00096 PER 51-20-01.

Part: CARGO TRACK — CORRODED (BS 1475) · airframe 75,096 hrs · 36,241 cycles

CORROSION CARGO TIE DOWN STATION 1475 RBL 12. REPAIRED PER 51-40-02 ON NR 00130.

Part: ANGLE — CRACKED (BS 680 RBL 25) · airframe 75,096 hrs · 36,241 cycles

ANGLE CRACKED AT STATION 680 RBL 25. REPAIRED ON NR 0095 PER 51-20-01.

Part: PAN — CRACKED (LAVATORY) · airframe 75,096 hrs · 36,241 cycles

AFT LAV PAN CRACKED AROUND RIGHT DUMP VALVE T HANDLE CUTOUT. REPAIRED PER ER/A 465404-14 REV ORG.

Part: FLOORBEAM — CORRODED (BS 739) · airframe 75,096 hrs · 36,241 cycles

CORROSION IN AND AROUND FASTENER HOLE AT BS 739, RBL 9 FLOORBEAM, OUT OF LIMITS. REPAIRED PER DELTA ER/A 465406-14 REV ORIG.

Part: FLOOR SUPPORT — CORRODED (BS 791-818) · airframe 75,096 hrs · 36,241 cycles

CORROSION IN AND AROUND FASTENER AND HOLES AT BS 791-818 RBL 7 FLOOR STRINGER. FLOOR STRINGER REMOVED AND REPLACED DUE TO CORROSION OUT OF LIMITS IAW SRM 51-40-02.

Part: BRACKET — DENTED (CARGO DOORWAY) · airframe 75,096 hrs · 36,241 cycles

FWD CARGO BAY CARGO SYSTEM STOP FITTING SUPPORT IS DENTED, FOUND ALSO TO BE CORRODED. REMOVED AND REPLACED STOP FITTING

Part: FLOOR SUPPORT — CORRODED (BS 701) · airframe 75,096 hrs · 36,241 cycles

CORROSION IN AND AROUND FASTENER HOLE AT BS 701 RBL 16 FLOOR STRINGER. CORROSION WAS OUT OF LIMITS. REPAIRED BY SPLICING IN NEW STRINGER FROM BS 670 TO FACTORY SPLICE AT BS 705 IAW AMM 53-87-01-801.

Part: STRINGER — CORRODED (BS 814-840) · airframe 75,096 hrs · 36,241 cycles

CORROSION IN AND AROUND FASTENERS AND HOLES AT BS 814-BS 840 RBL 16 FLOOR STRINGER. REMOVED AND REPLACED DUE TO CORROSION OUT OF LIMITS IAW SRM 51-40-02.

Part: SKIN — DENTED (FS 1738 S26-27L) · airframe 75,096 hrs · 36,241 cycles

DENT FROM INSIDE OUT STA 1738 BETWEEN STRINGERS 26L-27L. REPAIRED ON CUST CARD 00153.

Part: SILL — CORRODED (FS 610 RBL 23) · airframe 75,096 hrs · 36,241 cycles

FWD CARGO DOOR SILL STA 610 RBL 23 AT FWD SIDE OF AFT FITTING CORRODED.

Part: INTERCOSTAL — CORRODED (BS 1500-1508) · airframe 75,096 hrs · 36,241 cycles

CORROSION NOTED ON INTERCOSTAL SURFACE AND AT LOWER ANGLE AROUND FASTENERS AT STA 1500-1508 RBL 4. BLENDED CORROSION ON INTERCOSTAL, BLEND EXCEEDED ALLOWABLE LIMITS. REMOVED AND REPLACED INTERCOSTAL IAW DELTA SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,096 hrs · 36,241 cycles

WHILE ACCESSING AFT LAV SERVICE PAN FOUND SKIN UNDER LIP OF PAN TO HAVE CORROSION, OUT OF LIMITS. REPAIRED PER ER/A 465409-14 REV ORG.

Part: FLOOR SUPPORT — CORRODED (BS 655) · airframe 75,096 hrs · 36,241 cycles

FWD CARGO COMPARTMENT STA 655 BL, RBL 19, LOWER SIDE OF FLOOR SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT IAW SRM 51-40-02, SRM 51-40-05.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 75,096 hrs · 36,241 cycles

CORROSION NOTED ON FIXED FLOOR PANEL STA 1470-1510 AT NUTPLATE LOCATION APPROX AREA LBL 19. CORROSION REMOVED AND REPAIRED IAW ER 08-3376, DAL ER/A 456405-14 REV ORG.

Part: WEB — CRACKED (BS 1510 LBL 12) · airframe 75,096 hrs · 36,241 cycles

CRACK FOUND ON WEB DURING REMOVAL OF PAINT B/S 1520 LBL 12 COMMON TO Z STRINGER. REPAIRED ON CUST CARD 00126.

Part: SKIN — CORRODED (BS 630 BL 0) · airframe 75,096 hrs · 36,241 cycles

CORROSION AFTER REMOVAL OF ANTENNA, FOUND SKIN CORROSION AT BS 630 BL 0. REMOVED CORROSION AND REPAIRED IAW ATS ER 8-3328, DELTA ER/A 465407-14 DATED 24 OCT 2008.

Part: SHEAR TIE — CORRODED (BS 1701 S28-29R) · airframe 75,096 hrs · 36,241 cycles

SHEAR TIE IS CORRODED AT BS 1701 BETWEEN STRINGER 29R AND 28R. OUT OF LIMITS, REMOVED AND FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: FLOOR SUPPORT — CORRODED (BS 848-860) · airframe 75,096 hrs · 36,241 cycles

CORROSION AT FASTENERS HOLE ON PANEL SUPPORT BS 848-860, WL 154, ABOVE STRINGER 28L. REMOVED AND REPLACED PANEL SUPPORT.

Part: FLOOR SUPPORT — CORRODED (BS 1486-1530) · airframe 75,096 hrs · 36,241 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT NUTPLATE LOCATIONS BS 1510-1530 RBL 17. REPLACED DAMAGED SECTION OF FLOOR TO SIDEWALL SUPPORT PLATE BS 1486-1530. FABRICATED AND INSTALLED NEW SPLICE PLATE AT BS 1486 RBL 17.

Part: VALVE — CORRODED (AFT) · airframe 75,096 hrs · 36,241 cycles

CORROSION AFT DUMP VALVE INNER FLANGE IS CORRODED AND FASTENERS ARE PULLED THRU. REMOVED AND REPLACED AFT DUMP VALVE DUE TO CORROSION OUT OF LIMITS IAW AMM 20-11-00-201.

Part: SKIN — CORRODED (BS 535 BL 0) · airframe 75,096 hrs · 36,241 cycles

CORROSION AFTER ANTENNA REMOVAL FOUND ON SKIN AT BS 535 BL 0. REMOVED CORROSION AND REPAIRED IAW ER 08-3328/ER/A 465407-14 DATED 10/24/08.

Part: FLOOR SUPPORT — CORRODED (BS 1530) · airframe 75,096 hrs · 36,241 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE AT BS 1530 RBL 25 IS OUT OF LIMITS. REPLACED DAMAGED SECTION OF FLOOR TO SIDEWALL SUPPORT PLATE.

Part: FLOOR SUPPORT — CORRODED (BS 1510) · airframe 75,096 hrs · 36,241 cycles

CORROSION ON Z STRINGER LOWER SURFACE AT NUTPLATE LOCATION LBL 7.5 B/S 1510. REPAIRED ON CUSTOMER CARD 00069.

Part: STRAP — CORRODED (BS 1510) · airframe 75,096 hrs · 36,241 cycles

CORROSION AT BS 1510, LBL 17 THRU RBL 17 ON FLOOR PANEL SPLICE, OUT OF LIMITS AND REMOVED AND REPLACED IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (BS 1510) · airframe 75,096 hrs · 36,241 cycles

CORROSION ON Z STRINGER LOWER SURFACE NUTPLATE LOCATION RBL 7.5 BS 1510, OUT OF LIMITS. REMOVED AND REPLACED PART IAW SRM 51-40-02, DRD 53-60-53.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 72,140 hrs · 35,272 cycles

SMALL CRACK IN RT ELEVATOR UPPER SKIN FOUND DURING PAINT. CRACK FALLS IN CRITICAL AREA MAKING MAJOR REPAIR. REPAIRED ER SRM 55-20-01.

Part: ACTUATOR — BYPASSING (MLG DOORS) · airframe 67,935 hrs · 33,951 cycles

CREW REPORTS GEAR DOORS LIGHT AND EICAS MSG DISPLAYED DURING CLIMBOUT. CREW ALSO REPORTS NOSE A/G DISAGREE MSG. REMOVED AND REPLACED RT MLG DOOR. INTERLOCK ACTUATOR SOLENOID. FOUND TRUCK TILT ACTUATOR LEAK AND POSSIBLY BYPASSING. REMOVED AND REPLACED SAME IAW M/M. BOTH NEED OP AND LEAK CHECKED. CYCLED GEAR HANDLE AND OPERATED DOOR FROM GND SWITCH. ALL OPN NOW NML ON GND. JACKED ACFT, PERFORMED GEAR SWING. OPN NORMAL. ALL INDICATIONS OK. REMOVED MCO AND PLAC.

Part: BATTERY — DISCHARGED (SMOKE DETECTOR) · airframe 67,811 hrs · 33,907 cycles

R4 LAV SMOKE DETECTOR NO TEST. REPLACED BATTERY.

Part: WINDOW — CRACKED (COCKPIT) · airframe 65,201 hrs · 32,959 cycles

CAPT 1L WINDOW CRACKED AT FL 21000 AT 300 KTS. REPLACED CAPT 1L WINDOW AND WINDOW HEAT CONTROLLER.

Part: FUEL CONTROL — MALFUNCTIONED (NR 1 ENGINE) · airframe 62,447 hrs · 32,061 cycles

LEFT ENGINE LOST THRUST AFTER APPLICATION OF TAKEOFF THRUST. REPLACED LEFT ENGINE FUEL CONTROL UNIT.

Part: CONTROL UNIT — MALFUNCTIONED (SLATS) · airframe 61,877 hrs · 31,834 cycles

LEADING EDGE SLAT DISAGREE CAME ON 23,000 FT AT 300 KTS. SLOWED TO 235 KTS AND RTN TO LAND. FLAP/SLATS WERE UP WITH NO LIGHT FOR 10-15 MINS. WING AND ENG ANTI-ICE WAS ON. FSEU 1 AND 2 FAULTED SLAT LOSS. T/S PER FIM. ALL SLAT LOSS SWS CK GOOD FROM E5 RACK CONNECTORS. WHEN TAPPING ON LT OUTBOARD SW METER STARTED SHOWING SOME RESISTENCE. REPLACED LT OUTBOARD SW PER MM.

Part: COMPUTER — MALFUNCTIONED (E/E BAY) · airframe 61,742 hrs · 31,784 cycles

AS TAKEOFF POWER WAS APPLIED THE LEFT EPR ADVANCED THEN THE LEFT COMMAND SECTOR RETREATED. REPLACED TMC.

Part: SHUTTLE VALVE — FAILED (MLG) · airframe 56,893 hrs · 29,800 cycles

GEAR WOULD NOT RAISE AFTER T/O. FOLLOWED ABNORMAL PROCEDURE USING LOCK OVERRIDE AND GEAR RAISED NORMALLY. REPLACED TRUCK SHUTTLE VALVE PER M/M.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,609 hrs · 29,688 cycles

THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION JUST ABOVE THE STRINGER 19R SKIN LAP JOINT AT FS 771. THE CORROSION WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384898-14, REV A.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,607 hrs · 29,687 cycles

THE FUSELAGE SKIN AND UNDERLYING BEAR STRAP WERE FOUND DENTED AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT FS 1380 BETWEEN STRINGERS 22R & 23R. THE DAMAGE WAS REMOVED WITH A TRIMOUT AT THE DOOR EDGE. THE TRIMOUT WAS REPAIRED WITH 3 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 384808-14, REV A.

Part: PANEL — PUNCTURED (VERTICAL FIN) · airframe 56,607 hrs · 29,687 cycles

VERTICAL STABILIZER LT LOWER FWD SKIN (FWD TORQUE BOX) WAS DAMAGED DUE TO GROUND DAMAGE. REPAIRED PER ERA 423002-14

Part: SEAL — TORN (CARGO DOOR) · airframe 55,180 hrs · 29,018 cycles

FLIGHT CREW DECLARED EMERGENCY DURING CRUISE FLIGHT. HAD RT BLEED TRIP RENDERING RT PACK INOP. UNABLE TO MAINTAIN CABIN PRESSURE. FOUND AFT CARGO DOOR SEAL LEAKING AND TORN. ALSO HAD ABOUT ONE FOOT OF SEAL OUT OF RETAINER. R&R RT FAN AIR MOD VLV RR 490 DEG THERMAL SENSOR SWITCH RAN ENGS PER PFHB BLEED LIGHT OPS NORMAL PREFORMED EXCESSIVE CABIN PRESSURE LEAKAGE CK PER MM 05-21-24-2. REMOVED AFT CARGO DOOR SEAL AND LWR FWD RETAINER REPLACED LWR FWD SEAL RETAINER AND DOOR SEAL INSTALLATION.

Part: FAN — INOPERATIVE (AFT CARGO BAY) · airframe 50,787 hrs · 26,897 cycles

SMOKE REPORTED MID CABIN GALLEY RIGHT AFTER TAKEOFF. FOUND EICAS STATUS MSG SHOWING THAT NR 2 AFT EQUIP EXHAUST FAN INOP. NR 2 AFT EQUIP EXHAUST FAN FWD TO MCO AND PLAC.

Part: PUMP — FAILED (NR 2 ENGINE OIL) · airframe 48,069 hrs · 25,622 cycles

A/C 613 - FLT 1856 (DFW-TPA): MEM OPS CALLED TO LET US KNOWA/C DIVERTING TO THEIR STATION WITH ENGINE SHUTDOWN AND WILL BE ON GROUND IN 10 MINUTES. CREW CALLED 20 MINUTES LATER, NR 2 ENGINE OIL QTY WENT TO ZERO AND PRESSURE STARTED HEADING DOWN SO CREW WENT TO IDLE, NO HELP. OIL PRESSURE HIT RED AND CREW SHUTDOWN ENGINE. ENGINE WINDMILLED JUST UNDER 15 MINUTES. REPLACED ENGINE.

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

COMPRESSOR STALL WITH ENGINE ROLLBACK TO IDLE, NR 1 ENGINE. REPLACED ENGINE.

Part: FAN — FAILED (CABIN)

STRONG SMELL SIMILAR TO LIGHTED MATCHES THROUGHOUT CABIN AND COCKPIT. OCCURED DURING DESCENT AND THEN SLOWLY DISSIPATED. FOUND ECS/MSG AFT EQ EXH FAN 2 MSG AND C/B POPPED. REMOVED AND REPLACED AFT EQ EXH NO 2, RESET C/B, RAN PAX, NO SMELL NOTED.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

REPLACED OVERWING EMERGENCY LIGHT POWER SUPPLY, CHKS GOOD.

Part: DUCT — FAILED (RT WING LE)

RIGHT BLOWOUT DOOR ASSY FORWARD OF RT WING LEADING EDGE PANEL. 611EB MISSING, REF. 57-2551-25 ITEM 75, CAUSED BY A BLOWN DUCT IN THE RT WING LEADING IPC REF 36-11-01-03, ITEM 145.

Part: AIR DISTR — ODOR (CABIN)

BURNING ELECT/RUBBER SMELL IN CABIN AREA, SUSPECT OVERHEAD READING PNL. REMOVED POWER FROM BOTH UTILITY BUSSES. SMELL WAS MOST PRONOUNCED ON THE LT OF THE CABIN AROUND SEAT ROW 35/36. CHECKED CABIN WITH ALL LEVELS OF LIGHT AND FAN OPERATION UNABLE TO DETECT ANY LOCALIZED HEAT AREAS OR SMELL ANYWHERE THROUGHT THE CABIN.

Part: EEC — FAILED (NR 1 ENGINE)

DURING CLIMB-OUT THROUGH 7,000 FEET, LEFT ENGINE BEGAN TO SURGE REDUCING POWER. CORRECTED SURGING, BUT WHEN CLIMB POWER WAS AGAIN APPLIED, THE SURGING RESUMED. RETURNED LAX. REPLACED LT EEC. REPLACED LT PMA STATOR. REPLACED 14 STG CONVERTER VALVE AND 14 STG VALVE. ALL CKS NORMAL.

Part: NOSE COWL — ERROSION (ENGINE)

DURING INSPECTION, ENGINE NOSE COWL WAS FOUND WITH EROSION DAMAGE ON T/E COMPOSITE SKIN AT 6 O'CLOCK POSITION, APPROX 5 INCHES LONG. REPAIRED PER SRM 54-11-01 AND 51-70-03.

Part: SKIN — PUNCTURED (NR 8 SPOILER)

AT HMV, A .25 INCH HOLE WAS LOCATED 4.75 INCHES FROM AFT EDGE AND 16.5 INCHES FROM I/B EDGE OF NR 8 SPOILER. THIS WAS REPAIRED PER SRM 51-70-17 AS REFERRED FROM SRM 51-70-14.

Part: SKIN — DAMAGED (RT TE FLAP)

AT HMV, SET UP TO COMPLY WITH ERA 236853-14A CODE 6-57-53 PERM REPAIR WING RT FLAP AFT I/B LOWER SKIN PERMANENT REPAIR. REPAIR WAS ACCOMPLISHED PER ERA 236853-14 PERM REPAIR.

Part: FLOORBEAM — CORRODED (FS 324)

AT HMV, THE FLOORBEAM WAS FOUND TO BE CORRODED AT STA 324 BL0 TO RT HAND O/B END AROUND FASTENER HOLES. THE CORROSION WAS REMOVED PER SRM 51-10-00 AND WAS FOUND OUT OF LIMITS. REPAIR ITEMS WERE FABRICATED PER SRM 51-10-08 FIG 201 AND INSTALLED PER SAME.

Part: PLATE — CRACKED (NR 2 PYLON)

AT HMV, THE NR 2 PYLON WAS FOUND TO BE CRACKED AT THE UPPER FWD CORNER OF THE O/B PLATE OPENING. THE CRACK WAS ROUTED OUT PER SRM 54-51-01. HFEC FOUND NO DEFECTS. REPAIR DOUBLER DRILLED UP AND INSTALLED PER SRM 54-51-01.

Part: PLATE — CRACKED (NR 2 ENGINE)

AT HMV, THE NR 2 PYLON WAS FOUND TO HAVE TWO CRACKS ON THE UPPER FWD CORNER OF THE I/B PLATE OPENING. THE DAMAGE WAS REMOVED AND HFEC OF AREA CHECKED OK. REPAIR DOUBLERS WERE DRILLED UP AND INSTALLED PER SRM 54-51-01.

Part: FLOOR BEAM — CORRODED (FS 365)

AT HMV, THE FLOOR BEAM AT STA 365 WAS FOUND CORRODED AT RBL 3. THE CORROSION WAS REMOVED NOT WITHIN LIMITS PER SRM 53-00-51. REMOVED UPPER CAP LBL 12 IN TO RT O/B END. DRILLED AND INSTALLED REPLACEMENT SECTION OF FLOOR BEAM PER SRM 53-30-57 FIG 204.

Part: NOSE COWL — PUNCTURED (RT WING)

COWL WAS DAMAGED IN STORES, .50 INCH PUNCTURE IN OUTER SKIN AT CENTER OF PANEL AND IN THE 9 O'CLOCK POSITION. THE COWL WAS REPAIRED USING 9390 RESIN. SYSTEM APPROX SIZE OF REPAIR IS 4 INCHES, USING 2 REPAIR PLIES FOR EVERY DAMAGED PLY PER SRM 51-70-17.