N662DN

Part: WIRE — BROKEN (ZONE 200) · airframe 86,685 hrs · 40,219 cycles

SHIP 662 OVHD EMER LIGHT AT 8D INOP. CORRECTIVE ACTION: FOUND BROKEN WIRE AT TERMINAL ON EMERGENCY LIGHT. RECRIMPED WIRE PER SWPM CH 20 REF WDM 33-51-13. (6861776)

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 86,637 hrs · 40,194 cycles

SHIP 662 EMERGENCY LIGHT ON OVERHEAD BIN BETWEEN ROWS 11AB & 12AB INOP. CORRECTIVE ACTION: R+R POWER SUPPLY M735 IAW B757 AMM 33-51 LIGHT OPS NML. INSTALLED EMERGENCY LENS COVER ON OVERHEAD 11AB & 12AB PER B757 AMM 33-51. OPS CHK GD. (6861726)

Part: PROXIMITY SENSOR — FAULTED (GIRT BAR) · airframe 86,479 hrs · 40,089 cycles

SHIP 662 2R DOOR SLIDE INDICATOR LIGHT IS INOP. CORRECTIVE ACTION: R/R 2R SLIDE ARMED INDICATOR, R/R OTH FWD AND AFT GIRT BAR PROXIMITY SENSORS. FOUND C/B (P11-R34) DOOR GIRT BAR POPPED AND UNABLE TO RESET. FOUND RING TERMINAL BROKE AT R2 DOOR LIGHT. PROX BOX ALSO SHOWS TARGET NEAR WITH DOOR DISARMED. TARGET NEAR IS NORMAL REPLACED PROX S10221 AND OPS CHK NORMAL.

Part: STRINGER — CORRODED (APU BAY) · corrosion level 2 · airframe 86,170 hrs · 39,892 cycles

SHIP 662 APU BAY AT STA. 1885, STRINGER 17 AND AREA ADJACENT HAS EVIDENCE OF CORROSION DOT. CORRECTIVE ACTION: C/W ER/A 619908-14 REV ORIGINAL AT APU BAY STA 1885 STRINGER 17. (0496331)

Part: SKIN — DAMAGED (ZONE 100) · airframe 86,170 hrs · 39,892 cycles

SHIP 662 SECTION I REPAIR TO FUSELAGE SKIN AT STA1885 AND S-17R REQUIRES REPETITIVE INSPECTIONS PER SECTION II OF ERA 619908-14 CORROSION. CORRECTIVE ACTION: REF ERA 619908-14. (0495014)

Part: SKIN — DAMAGED (ZONE 100) · airframe 86,170 hrs · 39,892 cycles

SHIP 662 SECTION I REPAIR TO FUSELAGE SKIN AT STA1885 AND S-17R REQUIRES PERMANENT REPAIR PER SECTION III OF ERA 619908-14 CORROSION. CORRECTIVE ACTION: REF ERA 619908-14. (0495016)

Part: NONE — NONE (NONE) · airframe 86,168 hrs · 39,891 cycles

SHIP 662 LH FUSELAGE, STA 1640, BETWEEN S-14L TO S-15L HAS AN EXISTING REPAIR. I.D. TAG - ERA 670518-14AD REV O. CORRECTIVE ACTION: C/W ER/A 570518-14AD REV B AT LH FUSELAGE 1640 FRAME S14L TO S15L. (0491607)

Part: SKIN — BULGED (STA 440 STR 23R) · corrosion level 2 · airframe 86,168 hrs · 39,891 cycles

SHIP 662 SKIN BULGE FOUND AT APROX STA 440 STR 23R. CORRECTIVE ACTION: COMPLIED WITH ER/A 619846-14 REV ORIGINAL SKIN REPAIR AT STA 440 STR 23R(0489282)

Part: SKIN — CORRODED (CORROSION) · airframe 86,168 hrs · 39,891 cycles

SHIP 662 DTA MONITOR INSPECTION LOG REF ERA 619846-14 FUSELAGE / EXTERNAL SKIN / STA 440, BETWEEN S-22R AND S-23R / CORROSION. CORRECTIVE ACTION: REF ERA 619846-14. (1487941)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,672 hrs · 39,587 cycles

SHIP 662 EMERGENCY EXIT LIGHTS (PATHWAY) ROWS 12-15 INOP. CORRECTIVE ACTION: REMOVED & REPLACED BATTERY PACK PER 7577 AMM 33-51. OPS CHECK GOOD. (4274897)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,682 hrs · 39,592 cycles

SHIP 0662 EMERGENCY PATHWAY AISLE LIGHTS ROWS 12.15 INOPERATAIVE. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY BATTER CHARGER PER B757 AMM 33-51. OPS CHECK GOOD.

Part: PLATE — MISSING (L1 DOOR) · airframe 85,489 hrs · 39,475 cycles

SHIP 0662 DOOR 1L STOP PLATE MISSING FROM ONE LOCATION. CORRECTIVE ACTION INSTALLED ONE DOOR STOP PLATE REF B757 AMM 52-11. (9057863)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,490 hrs · 39,476 cycles

SHIP 0662 ROW 1DC CEILING EMERGENCY LIGHT INOPERATIVE. CORRECTIVE ACTION FOUND WIRE RING TERMINAL TO EMERGENCY LIGHT AT 1DC TO BE DEGRADED. RETERMINATED WIRE WITH RING TERMINAL PER B757 SWPM. OPS CHECKS GOOD PER B757 AMM 33-51. OK FOR SERVICE. (9057862)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,410 hrs · 39,436 cycles

SHIP 0662 SEAT 1C EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: RESEATED CONNECTOR UNDER SEAT, ALL CKS GOOD IAW B757 AMM 33-51. OK FOR SVC. (4109791)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,385 hrs · 39,422 cycles

SHIP SQUIB TEST FAILED EMERGENCY ESCAPE L ON TEST 1. CORRECTIVE ACTION: T/S PER B757 SSM 25-65-01. RELAY K10486 INOP. REMOVED AND REPLACE RELAY PER B757 AIPC 25-65-53. OP CHECK GOOD (4109758)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,253 hrs · 39,360 cycles

SHIP 662 LEFT CENTER ENT DOOR EICAS MSG AND LIGHT CAME ON WHEN CLIMBING THRU 3800 FT AFTER TAKEOFF. A/C WAS PRESSURIZING NORMALLY AND CONTINUED. CORRECTIVE ACTION: OPERATED L2 DOOR IAW B757 AMM 52-11. DOOR CLOSED NORMALLY INDICATION CHECK OK. (2394288)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,154 hrs · 39,300 cycles

SHIP 662 LT EMERGENCY ESCAPE SLIDE TEST FAILED. CORRECTIVE ACTION: T/S PER B757 FRM/FIM 25-65-00-815-802. SYSTEM RETURNED TO NORMAL. OK FOR SERVICE. (9394203)

Part: BOLT — BENT · airframe 84,811 hrs · 39,072 cycles

SHIP 662 L2 DOOR DOES NOT FULLY CLOSE. CORRECTIVE ACTION: REMOVED EXTERIOR HANDLES ON L2 DOOR DUE TO LOOSE RETAINERS FOUND IN BASKET CAM. ALSO FOUND BROKEN PEDETALS WHILE DISASSEMBLY. REMOVED INTERIOR DOOR LINING IN PREPERATION FOR FURTHER MAINT. REF B757 AMM 52-11. REMOVED DOOR SHAFTS PER B 757 AMM 52-11 CONT ON 9251698 FOUND LOWER HANDLE THRU BOLT BENT AND SHIMS DAMAGED. INSTALLED NEW BOLTS PLATFORMS & SHIMS PER B757 AMM 52-11. C/W REMAINING STEPS OF EXTERIOR HANDLE INSTALL PER B757 AMM 52-11 OPS

Part: NONE — NONE · airframe 84,808 hrs · 39,070 cycles

SHIP 662 R1 DOOR DIFFICULT TO ARM. CORRECTIVE ACTION: STRAP SECURING GIRT BAR FOLD CAME LOOSE FROM VELCRO INTERFERING WITH GIRT BAR PAWL MOVEMENT. RESECURED GIRT FOLD AND STRAP, OPS CHECK NORMAL. (9251688)

Part: NONE — NONE · airframe 84,776 hrs · 39,045 cycles

SHIP 662 2L DOOR WILL NOT ARM. CORRECTIVE ACTION: REMOVED LIFTER ASSY REF B757 CMM 52-11-15 AND INTALLED GIRT BAR LIFTER ASSY, ADJUSTED GIRT BAR MECHANISM PER B757 AMM 52-11, INSTALLED GIRT MECH AND BUSTLE PER B757 AMM 25-66-01. VERIFIED SLIDE.

Part: NONE — NONE · airframe 84,754 hrs · 39,029 cycles

SHIP 662 DTE, ER/A 602060-14AD; WING / LH OUTER / UPPER SKIN / TRAILING EDGE TAB BETWEEN WSTA 165.5 TO 177.5 / CORROSION. CORRECTIVE ACTION: REF ERA 602060-14AD. (2431706)

Part: NONE — NONE · corrosion level 2 · airframe 84,754 hrs · 39,029 cycles

SHIP 662 CORROSION ON UPPER CHORD REAR SPAR AFT FACE IRSS 188 AT LEFT WING TRAILING EDGE. CORRECTIVE ACTION: SUMMARY OF NRC 103 : UPPER CHORD REAR SPAR AFT FACE IRSS 188 AT LEFT WING TRAILING EDGE WAS REPAIRED PER ER /A 602060-14 REV ORIGINAL SECTION I : PERMANENT REPAIR. (2432151)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 CRACK ON FRAME STA 740 BTW S-21R AND S-22R AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF N.R.C. 00236. FRAME STA. 740 BTW S-21R AND S-22R AT FWD CARGO COMPARTMENT, WAS REPAIRED. PER. ER/A 601837-14, REV. ORIGINAL. SECTION I: PERMANENT REPAIR. (2421872)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 SEVERAL DENTS WERE FOUND ON FUSELAJE SKIN BTW STA 630- STA 650 BTW STRG 16 LH STRG 18 LH IN REFERENCE MONITOR 096-0001. CORRECTIVE ACTION: SUMMARY OF NRC 00410: FUSELAGE SKIN ON STA 620 TO 670, S-16L AND S-18L WAS REPAIRED PER. ER/A 601574-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. (2421165)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 DTE, ERA 601837-14 REV -, MONITOR INSPECTION LOG REPAIR AT STA 740 FRAME, BETWEEN S-21R & S-22R. CORRECTIVE ACTION: REF ERA 601837-14. (2420888)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 DTE, ER/A 601574-14; FUSELAGE / SKIN / STA. 620-670, S-16L & S- 18L / DENTS. CORRECTIVE ACTION: REF ERA 601574-14 (2420718)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 AWR. VISUAL INSPECTION WAS ACCOMPLISHED ON LH ENG DRAG FTG OPEN HOLES NBR 1 TO NBR 10 AND FOLLOWING DAMAGES WERE FOUND: HOLE #3 CORROSION ON SKIN AND FITTING AT 11 CLOCK POS; HOLE #4 SCRATCHES ON SKIN AND FITTING BTW 12 TO 3 CLOCK POS; HOLE #8 CORROSION ON SKIN AND FITTING BTW 3 TO 4 AND 10 TO 11 CLOCK POS & HOLE #9 SCRATCHES AND CORROSION ON SKIN AND FITTING BTW 11 TO 2 CLOCK POS PER TASK CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00396: LH ENG DRAG FTGCLAMP-UP HOLE # 2,HOLE #3, HOLE #4, HOLE #8 AND HOLE #9 WERE REPAIRED PER ER/A 601575-14AD REV. ORIGINAL, SECTION I PERMANET REPAIR. (2418235)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 DENT ON EXTERNAL FUSELAGE SKIN STA Y=680 STR= 26RH AT FUSELAGE. CORRECTIVE ACTION: SUMMARY OF NRC 00054: DENT ON EXTERNAL FUSELAGE SKIN STA Y=680 STR= 26RH WAS REPAIRED PER ER/A 601605-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. (2418177)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 DURING HFEC OPEN-HOLE INSPECTION BTW BS 1640 AND S- 14R, 2EA CRACKS WERE FOUND ON FRAME WEB LOWER INDB HOLE AT 4 CLOCK POS AND 9 CLOCK POS RESPECTIVELY. CONTACT LIAISON ENGINEERING FOR REPAIR INSTRUCTIONS. CORRCTIVE ACTION: SUMMARY OF NRC 00245: FRAME STA 1640 AND S-14RH WAS REPAIRED PER ER/A 601510-14AD REV.ORIGINAL , SECTION I: PERMANENT REPAIR. (2419457)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 DTE, ER/A 601605-14 FUSELAGE / SKIN / STA. 680, S-26R / DENT. CORRECTIVE ACTION:REF ERA 601605-14 REV ORG. (2417668)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 AD. A.A "EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA AT STA 1300 BTW S-26R TO S-27R. CONTACT LIAISON ENGINEERING FOR REQUIRED ACTIONS FOR THE REPAIRED AREA PRIOR TO FURTHER FLIGHT" IN REFERENCE CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00131: FRAME ON STA. 1300, BTW S-26R TO S-27R WAS REPAIRED PER. ER/A 601588-14AD REV. ORIGINAL SECTION I: PERMANENT REPAIR. (2415394)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 DTE, ER/A 601510-14AD; FUSELAGE / FRAME / STA. 1640, S-14R / FRAME WEB, TEE CLIP AND LOWER HINGE FITTING / CRACKS. CORRECTIVE ACTION: REF ERA 601510-14AD. (2411796)

Part: NONE — NONE · corrosion level 2 · airframe 84,753 hrs · 39,028 cycles

AIRCRAFT 0662, CORROSION UNDER PHENOLIC STRIP B STA 740 BTW LBL 16.10 AND LBL 19.00 AT FORWARD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED BEAM BTW STA 640-840 AND LBL 16.10-LBL 19.00 UNDER PHENOLIC STRIP AT FORWARD CARGO COMPARTMENT. (LP 2410877)

Part: NONE — NONE · corrosion level 2 · airframe 84,753 hrs · 39,028 cycles

AIRCRAFT 0662, CORROSION ON RIGHT SIDE PLATE AT STA 640, FWD CARGO COMPARTMENT. CORRECTIVE ACTION: RIGHT SIDE PLATE AT STA 640, FWD CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM 51-40-02-0G PAR 4 , PAR 5 , PAR 7 AND PAR 9. (LP 2408533)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

AIRCRAFT 0662, A.A. - A.D. DISBOND (4.800IN LENGTH X 1.600IN WIDTH) ALONG THE EDGE OF THE CUTOUT AT L1 DOOR CUTOUT. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED ON THE EDGE OF THE CUT OUT AT L1 DOOR STA 330- 355, S6L-S10L (SKIN AND BEAR STRAP) PER ER/A 601884-14AD REV. ORIGINAL, SECTION I. (LP 2408763)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 DTE, ERA 601588-14 REV -, MONITOR INSPECTION LOG REPAIR AT STA 1300 BOTTOM FRAME, BETWEEN S-26R & S-27R. CORRECTIVE ACTION: REF ERA 601588-14. (2407414)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 DENTS AND TOOL MARKS ON FRAME STA Y =1480 BTW STR= 26L / 27L AT AFT CARGO. CORRECTIVE ACTION: SUMMARY OF NRC 00552: FRAME STA Y =1480 BTW STR= 26L / 27L AT AFT CARGO WAS REPAIRED PER. B-757-200 SRM. (2406586)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 DTE, ER/A 601884-14AD FUSELAGE / SKIN / L1 DOOR CUTOUT SKIN & BEAR STRAP / STA 330-355, S6L-S10L / CRACK, DISBOND, INTERFERENCE AND ELONGATED HOLES. CORRECTIVE ACTION: REF ERA 601884-14AD. (2407209)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 601575-14AD. CORRECTIVE ACTION: REF ERA 601575-14AD. (2405789)

Part: NONE — NONE · corrosion level 2 · airframe 84,753 hrs · 39,028 cycles

SHIP 662 CORROSION ON FLOOR STRINGERS LBL 2.90,LBL 7.55,LBL 10.45 AND RBL 2.90,RBL 7.55,RBL 10.45 BTW STA 1495 TO STA 1520 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF N.R.C. 00183. FLOOR STRINGERS LBL 2.90, LBL 7.55, LBL 10.45 AND RBL 2.90, RBL 7.55, RBL 10.45, BTW STA 1495 TO STA 1520, AT AFT CARGO COMPARTMENT, WERE REPAIRED. PER. B757-200 SRM. (2406098)

Part: NONE — NONE · corrosion level 2 · airframe 84,753 hrs · 39,028 cycles

SHIP 662 CORROSION ON INTERCOSTAL RBL 10.45 BTW STA 660 AND STA 680, FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF N.R.C. 00163. INTERCOSTAL RBL 10.45 BTW STA 660 AND STA 680, FWD CARGO COMPARTMENT WAS REPAIRED. PER. B757-200 SRM. (2403487)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 AFTER REMOVED STABILIZER STRAP WAS FOUND CRACK ON WEB STA 1520 AND 1540 BTW RBL 45.0 IN REFERENCE NRC 525. CORRECTIVE ACTION: SUMMARY OF N.R.C. 00581. WEB STA 1520 AND 1540 BTW RBL 45.0 WAS REPAIRED. PER. B757-200 SRM. (2404155)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 BROKEN UP STABILIZATION STRAP AT STA 560 AND LBL 45.50, FWD CARGO COMPARTMENT.CEILING. CORRECTIVE ACTION: SUMMARY OF NRC 00158: STABILIZATION STRAP AT STA 560 AND LBL 45.50, FWD CARGO COMPARTMENT CEILING WAS REPAIRED PER B757-200 SRM. (2402774)

Part: NONE — NONE · corrosion level 2 · airframe 84,753 hrs · 39,028 cycles

SHIP 662 FRETTING CORROSION ON UPPER SKIN PANEL OF INBOARD FLAP BTW MF STA 285 AND MF STA 300.38, LEFT WING. CORRECTIVE ACTION: SUMMARY OF NRC 00118: UPPER SKIN PANEL OF INBOARD FLAP BTW MF STA 285 AND MF STA 300.38, LEFT WING WAS REPAIRED PER ER/A 514121-14MA REV A SECTION I. (2399247)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 CRACK ON INTERCOSTAL LBL 2.90 BTW STA 580 AND STA 600, FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00159: INTERCOSTAL LBL 2.90 BTW STA 580 AND STA 600, FWD CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM 51-70. (2397711)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 AWR. [AD // AA] VISUAL INSPECTION WAS ACCOMPLISHED ON RH ENG DRAG FTG OPEN HOLES NBR 1 TO NBR 10 AND FOLLOWING DAMAGES WERE FOUND: HOLE #2 CORROSION ON SKIN AND FITTING AT 9 CLOCK POS; HOLE #3 CORROSION ON SKIN AND FITTING BTW 8-10 CLOCK POS; HOLE #7 CORROSION ON SKIN AND FITTING AT 9 CLOCK POS; HOLE #8 CORROSION ON SKIN AND FITTING AT 8 CLOCK POS & HOLE #9 CORROSION ON FITTING AT 11 CLOCK POS PER TASK CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00345: HOLES #2, HOLE #3, HOLE #7, HOLE #8 AND HOLE #9 WERE REPAIR PER ER/A 601566-14AD REV. ORIGINAL SECTION I : REPAIR PERMANENT AND PRI 601566-14 REV. 2. (2393391)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 A.A. - A.D. DISBOND ON ISS 194, UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00046: A.A. - A.D DISBOND ON ISS 194, UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING WAS REPAIRED PER B757-200 S.R.M. (2389916)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 WHILE PERFORMING AMDS 2565-3003 STEP 12 RH SIDE , SLIDE CARRIER ACTUATOR LEAKS. CORRECTIVE ACTION: SUMMARY OF NRC 00516. RH OFF-WING ESCAPE SYSTEM ACTUATOR WAS REPLACED BY SERVICEABLE OFF-WING ESCAPE SYSTEM ACTUATOR PER B757-200 AMM 25-65. (2389027)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 MIGRATED INB. BUSHING ON RH PYLON FITTING ( UPPER LINK FWD END) AT NAC STA 163. CORRECTIVE ACTION: SUMMARY OF NRC 00322: BUSHINGS (2 EAS) OF ATTACH FITTING AT RH PYLON WERE REPLACED PER B757-200 SRM. (2387686)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 601566-14AD. CORRECTIVE ACTION: REF ERA 601566-14AD. (2386118)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 MIGRATED BUSHING OF ATTACH FITTING AT LH PYLON ENGINE 1. CORRECTIVE ACTION: SUMMARY OF NRC 00293: BUSHINGS (2AS) OF ATTACH FITTING AT LH PYLON WERE REPLACED PER B757-200 SRM. (2386454)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 A.A. - A.D. DISBOND ON OSS 438, LOWER SURFACE, LE SLAT 3 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00045: LOWER SURFACE, LE SLAT 3 TRAILING EDGE WEDGE, LH WING WAS REPAIRED PER B757 SRM. (2382706)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 A.A. - A.D. DISBOND ON OSS 572, UPPER SURFACE, LE SLAT 8 TRAILING EDGE WEDGE, RH WING. CORRETIVE ACTION: SUMMARY OF NRC 00022: UPPER SURFACE, LE SLAT 8 TRAILING EDGE WEDGE, RH WING. WAS REPAIRED PER B757-200 SRM. (2380023)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

SHIP 662 CORROSION ON MID FITTING AT SLIDE GIRT BAR DOOR 1L, 2R AND 4R. CORRECTIVE ACTION: SUMMARY OF NRC 00134: MID FITTING OF 1L, 2R AND 4R DOOR SLIDE GIRT BAR WERE REPLACED AND P/N VERIFIED PER B757-200 IPC 25-66. (2368658)

Part: NONE — NONE · airframe 84,753 hrs · 39,028 cycles

TORN HARNESS ASSY AT 4R AND 1R EMERGENCY ESCAPE SLIDES. CORRECTIVE ACTION: SUMMARY OF NRC 00133: HARNESS ASSY OF 4R AND 1R DOOR ESCAPE SLIDE WERE REPLACED AND P/N VERIFIED PER B757-200 IPC 25-66-01. (2368593)

Part: NONE — NONE · airframe 84,742 hrs · 39,024 cycles

SHIP 662 DOOR 1LEFT, HANDLE MISSING OUTSIDE PART. CORRECTIVE ACTION: INSTALLED COVER PER CMM 52-11-07. (8369291)

Part: STRAP — BROKEN · airframe 84,675 hrs · 38,992 cycles

SHIP 662 A STABILIZER STRAP WAS FOUND BROKEN AT STATION 345 ABOVE PNL 117BL. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0003:3220-9901/007 00016 REPAIR COMPLETED PER B757 SRM 53-00-51-2R-12, FLOORBOARD 221AF RE-INSTALLED, NOSE WHEEL WELL PANEL 117BL RE-INSTALLED AND LEAK CHECKED GOOD PER B757 AMM 05-51-24. (2261543)

Part: FLOOR PANEL — CORRODED · airframe 84,675 hrs · 38,992 cycles

SHIP 662 FOUND CORROSION ON FLOOR FRAME AROUND NUT PLATE HOLE AT STATION 345 UNDER THE AFT GALLEY FLOOR PNL 221AF. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0003:3220-9901/008 00022 EVALUATED DAMAGE AND REMOVED CORROSION AS PER 757-200 SRM 53-00-51-1A. CORROSION CONTAINED. (2260291)

Part: FUSE — BLOWN · airframe 84,671 hrs · 38,988 cycles

SHIP 662 EXTERIOR R1 DOOR EMERGENCY LIGHT OUT. CORRECTIVE ACTION: REPLACED R1 DOOR LAMP. REPLACED BATTERY PACK AT L26 CHARGER ( AFT OF COCKPIT DOOR IN CEILING). FOUND FUSE BLOWN IN L26 CHARGER. REPLACED FUSE. OPS CHECK OF R1 DOOR EXTERIOR LIGHT NOW GOOD. REFERENCE B-757 AMM 33- 51. (8738687)

Part: NONE — NONE · airframe 84,671 hrs · 38,988 cycles

SHIP 662 EXTERIOR R2 DOOR, OVERWING EXIT DOORS, AND AFT CARGO DOOR EMERGENCY LIGHTS OUT ON RIGHT SIDE. CORRECTIVE ACTION: REPLACED R2 DOOR AND AFT CARGO DOOR EXTERIOR EMERGENCY LIGHT LAMPS. REFERENCE B-757 AMM 33-51-06-962-001-001. ALSO REPLACED BATTERY PACK AT SEAT 8D CHARGER. REFERENCE B-757 AMM 33-51. (8738686)

Part: NONE — NONE · airframe 84,400 hrs · 38,821 cycles

SHIP 662 L2 DOOR ESCAPE SLIDE LIGHT INOP. CORRECTIVE ACTION: R/R L2 DOOR AFT TARGET/SWITCH. OPS CK OK REF B757 AMM 25-66. (8363334)

Part: NONE — NONE · airframe 84,317 hrs · 38,771 cycles

SHIP 662 L2 DOOR DISARM LIGHT WILL NOT EXTINGUISH. CORRECTIVE ACTION: REMOVED DEBRIS AS REQD. OPS NRML. (7866878)

Part: NONE — NONE · airframe 84,316 hrs · 38,770 cycles

SHIP 662 L1 DOOR INBOARD HANDLE COVER PLATE MISSING. CORRECTIVE ACTION: FORWARD COVER TO NEF 52-10-01 L1 DOOR HANDLE COVER PLATE MISSING. (7866874)

Part: NONE — NONE · airframe 84,256 hrs · 38,739 cycles

SHIP 662 DOOR 2L SLIDE ARMED LIGHT WILL NOT EXTINGUISH. CORRECTIVE ACTION: T/S PER B757 FIM 25-66. CYCLED DR ARMING NUMEROUS TIME. LIGHT CKS NORMAL. (7866830)

Part: SIGN — UNSECURE (EMERGENCY LIGHTS) · airframe 84,021 hrs · 38,592 cycles

SHIP 662 EMERGENCY EXIT SIGN OVER 2L DOOR IS LOOSE. CORRECTIVE ACTION: SECURED EMERGENCY LIGHT LENS AS REQ REF B 757 AMM 33-51. CKS GOOD. (7755938)

Part: GIRT BAR — FAILED INSP (L1 DOOR) · airframe 84,010 hrs · 38,587 cycles

SHIP 662 L1 DOOR GIRT BAR FAILS CHECK REF NR1. REMOVED AND INSTALLED GIRT BAR REF B757 AMM 25-66 AND TEST IAW B757 AMM 52-11. (1898102)

Part: GIRT BAR — NO TEST (L4 DOOR) · airframe 84,005 hrs · 38,585 cycles

SHIP 662 L4 DOOR GIRT BAR FAILS CHECK. REF. NR 3. CORRECTIVE ACTION: GIRT BAR CHANGED ON NR 3. REMOVED AND INSTALLED GIRT BAR REF B757 AMM 25-66, ADJUSTED AND TESTED REF B757 AMM 52-11. (1898105)

Part: GIRT BAR — FAILED INSP (L2 DOOR) · airframe 84,010 hrs · 38,587 cycles

SHIP 662 L2 DOOR GIRT BAR FAILS CHECK. CORRECTIVE ACTION: REMOVED AND INSTALLED GIRT BAR REF B757 AMM 25-66 ADJUSTED/TESTED OK REF B757 AMM 52-11. (1898531)

Part: GIRT BAR — FAILED INSP (R2 DOOR) · airframe 84,010 hrs · 38,587 cycles

SHIP 662 R2 DOOR GIRT BAR FAILS CHECK. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 017-0001:2560-01492-0101/004 00004. REMOVED AND INSTALLED GIRT BAR REF B757 AMM 25-66. ADJUSTED/TESTED OK REF B757 AMM 52-11. (1898532)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,807 hrs · 38,469 cycles

SHIP 662 RT SIDE OVERWING EXIT EMERGENCY LIGHTS INTERIOR AND EXTERIOR ARE INOP. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERY PACK IAW B757 AMM 33-51. OPS CHECKS GOOD. (7485552)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,479 hrs · 38,285 cycles

ON SERVICE CHECK MAINTENANCE FOUND CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK ON POWER SUPPLY M737, M730 AND M10468. SYSTEM OPERATION IS NORMAL.

Part: PANEL — DAMAGED · airframe 84,673 hrs · 38,989 cycles

SHIP 662 PANEL 511FB HAS DAMAGED EDGE BAND FASTENER HOLES. CORRECTIVE ACTION: REPAIRED PANEL PER B-757 SRM 51-70-08. REINSTALLED PANEL 511FB PER B-757 AMM 57-41-01. (6914680)

Part: BOTTLE — LOW PRESSURE (LT OVRWG SLIDE) · airframe 83,478 hrs · 38,283 cycles

LEFT WING ESCAPE SLIDE INFLATION BOTTLE PRESSURE SWITCH FAILED. CORRECTIVE ACTION: REPLACED BOTTLE. SYSTEM OPERATION IS NORMAL.

Part: SWITCH — MISSING (ARM LIGHT) · airframe 83,398 hrs · 38,231 cycles

(AIRCRAFT 662, L/P 6693427) L2 DOOR "SLIDE" ARM LIGHT SWITCH MISSING. CORRECTIVE ACTION: INSTALLED GIRT BAR ENGAGED WARNING LIGHT PER B757 AMM 52-11.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,312 hrs · 38,179 cycles

DURING A SERVICE INSPECTION, FOUND THE LT OVERWING EMERGENCY EXIT LIGHTS NOT WORKING. R & R BATTERY PACK IAW AMM 33-55. OPS CHECKED GOOD.

Part: ROLLER — OUT OF SEQUENCE (NLG DOOR) · airframe 83,271 hrs · 38,153 cycles

SHIP 0662 - ATB - DUE TO NOSE GEAR DOOR LIGHT ILLUMINATED WITH AIR NOISE AND VIBRATION. CORRECTIVE ACTION: NOTICED ROLLER AND STOP IN INTERLOCK ACTUATOR OUT OF SEQUENCE, PULLED MANUAL RELEASE AND ACTUATED DOOR CLOSE SWITCH ON NOSE GEAR PANEL, OP CKS NML. REPLACED INTERLOCK ACTUATOR PER AMM, SWUNG GEAR, OP CKS NML.

Part: SIGN — NOT REPORTED (CABIN) · airframe 83,113 hrs · 38,034 cycles

(AIRCRAFT 662, L/P 5447592) EMERGENCY EXIT SIGN OVER 2L NEEDS TO BE REINSTALLED. CORRECTIVE ACTION: REPLACED EXIT SIGN LENS @2L PER AMM 33-50.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 83,089 hrs · 38,025 cycles

R2 DOOR EXIT SIGN MISSING LENSE. CORRECTIVE ACTION: REPLACED MISSING SIGN CHECKS GOOD.

Part: PDU — OUT OF RIG (LE SLAT) · airframe 82,975 hrs · 37,977 cycles

SHIP 662 -DIV- DIVERTED TO DTW FOR A LEADING EDGE SLAT DISAGREE. CORRECTIVE ACTION: PERFORMED FIM 27-51, FOUND PDU CAM OUT OF RIG. ADJUSTED CABLES PERFORMED OPS TEST OF FLAP NML DRIVE PER AMM OP CKS GOOD.

Part: MODULE — MISSING (R1 DOOR) · airframe 82,975 hrs · 37,977 cycles

SHIP 662 SLIDE ARMED CAP ASSY MISSING DR 1R. CORRECTIVE ACTION: INSTALLED NEW LIGHT CAP MODULE - CKS GOOD. (5525653)

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,888 hrs · 37,939 cycles

EMERGENCY LIGHTS INOP ON FIRST 3 ROWS RT SIDE. REPLACED FUSE IN BATTERY POWER PACK. LIGHTS CK GOOD.

Part: METERING VALVE — DEFECTIVE (NLG STEERING) · airframe 82,742 hrs · 37,847 cycles

AIRCRAFT PULLING TO THE LEFT DURING TAKEOFF ROLL, PERFORMED LOW SPEED ABORTED TAKEOFF. REPLACED NWS METERING VALVE AND BOTH NOSE WHEELS TAXI CHECKS GOOD.

Part: FRAME — CRACKED (BS 1640) · airframe 82,351 hrs · 37,572 cycles

FRAME BS 1640, STRINGER 14L, SECOND FASTENER BELOW THE STRINGER, HAS A CRACK AT THE FASTENER, FWD SIDE. REPAIRED IAW PRI 570518-14AD, REV 0, COMPLIED WITH ERA 570518-14AD, REV ORIGINAL.

Part: SLIDE — DAMAGED (NOT REPORTED) · airframe 82,351 hrs · 37,572 cycles

SLIDE PACK BREAK AWAY PIN NOT LACED. REPLACED THE SLIDE PACK IAW AMDS CARD 2560-9901-LT.

Part: FRAME — CRACKED (BS 1640) · airframe 84,188 hrs · 38,697 cycles

SHIP 662 CRACK FINDINGS AT STA 1640 LHS FRAME PER EM 5311-01218-01 REPAIR ACCOMPLISHED PER ERA 570518-14AD. CORRECTIVE ACTION: ER/A 570518-14 WAS REVISED TO REV A. (0685716)

Part: SIGN — DAMAGED (LEFT) · airframe 82,172 hrs · 37,453 cycles

TWO LEFT EXIT SIGNS DAMAGED. REPLACED THE SIGNS IAW TOPP 50-00-25.

Part: SLIDE — DETACHED (L2 DOOR) · airframe 82,138 hrs · 37,432 cycles

SLIDE AT THE L2 DOOR DROPPED OUT OF BUSTLE. R & R THE DOOR SLIDE IAW WC 2566-9001-2L OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 81,148 hrs · 36,828 cycles

EMER LIGHT INOP L-1 UPPER. M731 BATTERY REPLACED ON NR-8. OPS CHECK GOOD OF EMERGENCY EXIT SIGNS IAW AMM 33-51.

Part: BATTERY — DISCHARGED (CABIN) · airframe 81,148 hrs · 36,828 cycles

EMER LIGHT INOP L-1 OUTER. M731 BATTERY REPLACED ON NR-8. OPS CHECK GOOD OF EMERGENCY EXIT LIGHTS IAW AMM 33-51.

Part: BATTERY — DISCHARGED (CABIN) · airframe 81,148 hrs · 36,828 cycles

EMER LIGHT INOP R-1 LOWER. REMOVED AND REPLACED M731 POWER PACK/BATTERY IAW AMM 33-51-07. OPS CHECK GOOD OF EMERGENCY EXIT LIGHTS IAW AMM 33-51.

Part: CONNECTOR — LOOSE (CABIN) · airframe 81,148 hrs · 36,828 cycles

EMER LIGHT INOP R-2 RED. CONNECTOR P33 FOUND LOOSE AND RESEATED IAW SWPM 20-60-06. PERFORMED SATISFACTORY OPERATIONAL CHECKS OF EMERGENCY LIGHTS IAW AMM 33-51.

Part: ACCESS PANEL — DELAMINATED (TE FLAP) · airframe 81,146 hrs · 36,827 cycles

FLAP SUPPORT STRUCTURE ACCESS PANEL 572AB HAS DELAMINATION ON UNDERSIDE. FOUND AREA OF ONE PLY DELAMINATED AND MISSING ON LOWER SKIN IAW SRM. REPAIRED FLAP TRACK FAIRING IAW SRM.

Part: STRINGER — CORRODED (BS 1620) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

AFT CARGO STRINGER 29L IS CORRODED AND CRACKED AT SPLICE JUST FWD OF FRAME BS 1620. REMOVED AND REPLACED AFT CARGO STRINGER IAW SRM.

Part: STRINGER — CORRODED (BS 1520) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

CORROSION ON STRINGER 28L BS 1520. FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED THE STRINGER IAW SRM.

Part: STRINGER SPLICE — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

UPON REMOVAL OF STRINGER 29L FOR REPLACEMENT IN AFT CARGO FOUND SPLICE AT STA 1620 S29L TO BE DAMAGED AND REQUIRES REPLACEMENT. FOUND TO BE OUT OF LIMITS IAW SRM. FABRICATED NEW SPLICE AND INSTALLED ON NR 00724.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

FWD CARGO BAY STA 654 LBL 10.45 CORROSION UNDER NUT PLATE. REMOVED CORROSION AND EVALUATED PER SRM. REMOVED AND REPLACED FLOOR STRINGER IAW B757 SRM AND DWG. REF ERA 548953-14 ORG.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

FUSELAGE SKIN IS CORRODED AND GOUGED INTERNALLY AT STA 1515 JUST O\B OF STRINGER 29R. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM. CUT OUT DAMAGE AREA AND REPAIRED IAW SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 81,146 hrs · 36,827 cycles

LEFT HAND FUSELAGE SKIN HAS A DENT IN CLOSE PROXIMITY OF A REPAIR AND OUT OF ALLOWABLE LIMITS AT STA 620 S-16L AND REQUIRES A REPAIR. COMPLIED WITH ERA 543881-14 REV B.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

FWD CARGO COMPT FS 879 FRAME SHEAR TIE IS CORRODED BETWEEN STR 28L&28R. REMOVED AND REPLACED FWD CARGO COMP SHEAR TIE AT FS 879 BETWEEN STRINGERS 28L & 28R IAW SRM.

Part: GATE — CORRODED (L1 DOOR) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

L1 DOOR UPPER GATE UNDER LEVELING COMPOUND HAS CORROSION. REMOVED AND REPLACED L1 DOOR UPPER GATE IAW AMM 52-11-38. OPS CHECK PERFORMED ON AMDS CARD.

Part: GATE — CORRODED (L4 DOOR) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

L4 DOOR LOWER GATE HAS CORROSION FROM FWR TO AFT ENDS. REMOVED & REPLACED L4 DOOR LOWER GATE IAW AMM 52-11.

Part: GATE — CORRODED (L1 DOOR) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

L1 DOOR LOWER GATE HAS CORROSION. REMOVED AND REPLACED L1 DOOR LOWER GATE IAW AMM 52-11.

Part: SKIN — DENTED (CARGO DOOR) · airframe 81,146 hrs · 36,827 cycles

AFT CARGO DOOR DENTS IN OUTER SKIN OF DOUBLER FWD LOWER CORNER. REMOVED PREVIOUS REPAIR AND APPLIED A NEW REPAIR ON THE AFT CARGO DOOR FWD LOWER CORNER OUTER SKIN IAW ERA 548947-14 REV O.

Part: WEB — CORRODED (BS 1300-1320) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

FOUND WEB CORRODED BETWEEN BS 1300 AND 1320, STRINGERS 27 AND 28. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02 AND 53-00-04. REMOVED, FABRICATED, AND INSTALLED A NEW WEB IAW SRM 51-40-02 AND DWG 146N5425 REV A.

Part: WEB — CORRODED (BS 1360-1380) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

AFT CARGO WEB IS CORRODED AT BS 1360-1380 BETWEEN STRINGER 27 & 28L. REMOVED CORROSION AND FOUND TO BE 100% MATERIAL LOSS AND IS BEYOND LIMITS IAW SRM 51-10-02 AND 53-00-04. REMOVED THE WEB IAW SRM 51-40-02. FABRICATED A NEW WEB IAW DRAWING 146N5410 REV B. LOCATED AND DRILLED WEB IAW DWG 146N5425 REV A AND INSTALLED THE WEB IAW SRM 51-40-02 AND DRAWING 146N5425 REV A ORIGINAL.

Part: FRAME — CORRODED (BS 1480) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

FRAME CORRODED IN AFT CARGO BAY BILGE AREA AT BS 1480 BETWEEN STRINGERS 29 AND 30R. REMOVED AND REPLACED THE FRAME SECTION IAW SRM 51-40-02 AND DWG 146N1015 REV D.

Part: CREASE BEAM — CORRODED (BS 970) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

RT CREASE BEAM IS CORRODED AT F.S 970 BELOW RT FWD EMERGENCY EXIT HATCH LOWER CUTOUT. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R CREASE BEAM WEB IAW DWG AND SRM. (2706309)

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

PASSENGER CABIN R\H CREASE BEAM IS CORRODED BETWEEN FS 1380 & FS 1400 RBL 63. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

LT NR 2 DOOR LOWER SILL UPPER SURFACE CORRODED ON FWD SUPPORT. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R&R NEW SUPPORT IAW SRM AND DRW.

Part: GATE — CORRODED (R2 DOOR) · corrosion level 2 · airframe 81,146 hrs · 36,827 cycles

R2 DOOR LOWER GATE HAS CORROSION. REMOVED & REPLACED 2R DOOR LOWER GATE IAW AMM 52-11-38.

Part: CREASE BEAM — CORRODED · airframe 81,146 hrs · 36,827 cycles

NR 2 DOOR LOWER SILL UPPER SURFACE INBD SUPPORT CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 53-30-15. REMOVED AND REPLACED CREASE BEAM IAW SRM 51-40-02, DWG 143N8322 REV K.

Part: SKIN — DENTED (BS 620) · airframe 81,146 hrs · 36,827 cycles

BS 620, STRINGER 16L SKIN DENTED. REPAIRED IAW ERA 543881-14 REV:B.

Part: SKIN — DENTED (BS 620) · airframe 79,003 hrs · 35,937 cycles

FOUND DENT AT LOCATION STR 16L, BS 620. FOUND DENT TO BE 1.125" L & 0.053" D. IAW SRM 53-00- 01, FIGURE 101, DETAIL 3, CRITERIA, A/Y RATIO TO BE 21.22, LESS THAN 30 IS OUT OF LIMITS. NOTE I DENT REPAIR MAY BE DELAYED WITH EXAMINATIONS AT EVERY 300 FLIGHT CYCLES & NOT TO EXCEED 24 MONTHS. REPAIR MUST BE MADE AT OR BEFORE NEXT C-CHECK. REMOVED SHARP EDGES OF DENT, TREATED, PRIMED, AND PAINTED AREA. DENT STICKER INSTALLED & ADDED TO ADF FILES. PERFORMED 10X INSPECTION, NO CRACKS NOTED. CHANGED TERM ACTION FROM HCK TO LCK IAW SRM 53-00-01, PAGE 103.

Part: SKIN — DENTED (BS 1685) · airframe 78,680 hrs · 35,803 cycles

DENT AT BS 1685, WL 154L .759 IN DIAMETER .124 IN DEPTH LT OF AFT LAV SERVICE PANEL. DENT NOT WITHIN ALLOWABLE LIMITS DEFERRED IAW SRM 53-00-01, FIG 101, PAGE 103, NOT I. DENT MUST BE INSPECTED EVERY 300 FLIGHT CYCLES. PERMANENT REPAIR MUST BE MADE NEXT C CHECK, NOT TO EXCEED 24 MONTHS.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 78,241 hrs · 35,606 cycles

43D EMERGENCY LIGHT INOPERATIVE. FOUND BROKEN WIRE FROM OTBD HARNESS CONNECTOR. REPAIRED IAW SWPM 20-30-12, OPS CHECKED OK.

Part: ENGINE — SHUTDOWN (LEFT) · airframe 77,046 hrs · 35,071 cycles

ACFT DIVERTED DUE TO LT ENGINE INFLIGHT SHUTDOWN. MAINTENANCE FOUND PMA STATOR SEVERELY COKED WITH OIL CONTAMINATION. INSPECTED AND MAIN OIL FILTER INSPECTED AND REPLACED. PMA ROTOR, STATOR AND SEAL REPLACED. PMA HARNESS AND BACKSHELLS INSPECTED. HIGH POWER RUN PERFORMED PER AMM. ALL INDICATIONS NORMAL.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,812 hrs · 34,971 cycles

SEAT 35D, EMERGENCY LIGHT AT SEAT INOPERATIVE. REPLACED EMERGENCY LIGHT SEAT HARNESS AT SEAT 35DEF. OPS CKS GOOD.

Part: SKIN — DAMAGED (BS 500-522) · airframe 76,657 hrs · 34,904 cycles

ER/A 523500-14, REV A, FUSELAGE, SKIN AT FS 500-522, S-27L, TOS-27R, ATG4 FORWARD ANTENNA, EXISTING REPAIR, INTERFERENCE,SUPPLEMENTAL INSPECTIONS. ER/A 523500-14, REV A, AT OR PRIOR TO 44,352 TOTAL FLIGHT CYCLES AND REPETITIVELY EVERY 4,798 FLIGHT CYCLES THEREAFTER ACCOMPLISH SECTION II SUPPLEMENTAL INSPECTIONS ASSOCIATED ER/A 00-523500 ADDED FOR AC 0662.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 75,446 hrs · 34,335 cycles

RT OVERWING EXIT LIGHT LENS IS MISSING. REPLACED THE LENS ASSY IAW MM 25-10.

Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 74,843 hrs · 34,095 cycles

SEAT 27D EMERGENCY PATH LIGHT BULBS & LENS COVER MISSING. INSTALLED BULBS & COVER.

Part: SKIN — DAMAGED (BS 720) · airframe 74,292 hrs · 33,894 cycles

LIGHTNING STRIKE BS 720, S14R. C/W ERA 526192, REV ORIG.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 74,206 hrs · 33,859 cycles

LIGHTNING BURN ON CARGO DOOR. REMOVED DAMAGE IAW SRM 52-30-01. FABRICATED DOUBLER AND FILLER IAW SRM 25-30-01. PERMANENT REPAIR IAW ERA526169-14, REV A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,206 hrs · 33,859 cycles

DURING CLIMB OUT AT 15,000 FT, SYSTEMS OK. BOTH FO AND PILOT FELT A LOUD BANG ASSOCIATED WITH LIGHTNING. COMPLIED WITH LIGHTNING STRIKE INSPECTION IAW AMM 05-51-19. FOUND MULTIPLE BURNS ALONG LOWER RT FUSELAGE. BURNISHED AND REPAIRED DAMAGE IAW SRM 53-00-01.

Part: SKIN — DAMAGED · airframe 74,223 hrs · 33,864 cycles

LIGHTNING STRIKE DAMAGE AT LOWER RT FUSELAGE, 27 INCHES BELOW AFT EDGE OF MID LAV SERVICE DOOR. REPAIRED FUSELAGE SKIN IAW ERA 526192-14, REV ORIG.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 73,806 hrs · 33,694 cycles

SEAT 27DEF EMERENCY LIGHTS INOPERATIVE. REPLACED UNDERSEAT CONNECTOR AT 27DEF IAW AMM 33-51.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHT) · airframe 73,585 hrs · 33,601 cycles

FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 39DEF. FOUND SEAT HARNESS BROKEN. REPLACED HARNESS. OPS CHECKED GOOD. OK FOR SERVICE.

Part: LATCH — OUT OF ADJUST (L2 DOOR) · airframe 73,406 hrs · 33,521 cycles

DOOR FWD UPPER LATCH IS RUBBING RECEIVER. REMOVED L2 DOOR GUIDE ARM ASSY AND REPLACED GUIDE ARM PIVOT PIN AND BUSHING AND REINSTALLED GUIDE, R & R L2 DOOR FWD UPPER LATCH FITTING IAW AMM 52-11. REMOVED EXTERIOR HANDLE AND SHAFTS AND REINSTALLED WITH NEW CLUTCH COLLAR AND CENTER SHAFT IAW AMM 52-11.

Part: TEAR STRAP — DEBONDED (FUSELAGE) · airframe 73,405 hrs · 33,521 cycles

FUSELAGE SKIN TEARSTRAP DISBOND, 5331-01238.

Part: DOOR SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 73,405 hrs · 33,521 cycles

AFT CARGO BAY INBD OF UPPER DOOR SILL BEAM WEB CORRODED FROM FS 1380-1440 RBL 21. OUT OF LIMITS SRM 53-60-15, PG 106, PAR 13, FIG VIII. INSTALLED NEW WEB DWG 146N5390 SHEET 1-7.

Part: SIGN — MISINSTALLED (CABIN) · airframe 73,467 hrs · 33,556 cycles

FAA REPORTS EMERGENCY SIGN ON BACKWARDS AT 27CDE. REPLACED SAME WITH CORRECT EMERGENCY SIGN. OK FOR SVC.

Part: WIRE HARNESS — FAILED (EMERGENCY LIGHTS) · airframe 72,929 hrs · 33,300 cycles

SEAT 1CD EMERGENCY LIGHT INOPERATIVE. FOUND WIRING HARNESS BAD. R & R WIRING HARNESS IAW CHAPER 20. OPS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,623 hrs · 33,159 cycles

EMERGENCY LIGHT AT SEAT 29D IS INOPERATIVE. REPLACED LIGHT ASSY OPS CHECKED NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 71,684 hrs · 32,787 cycles

FUSELAGE SKIN, STA 610, S-16L, DENT 506189-14.

Part: SKIN — DENTED (FS 1720 S-15L) · airframe 70,008 hrs · 32,133 cycles

SCRATCH AND DENTS ON FUSELAGE ON RT SIDE OF 4L DOOR. PERFORMED TEMP REPAIR IAW ERA511035-14, REV ORIG. PERFORMED PERMANENT REPAIR IAW ERA 511054-14, REV ORIG.

Part: SKIN — DENTED (FWD CARGO DOOR) · airframe 69,607 hrs · 31,958 cycles

ON ARRIVAL FOUND SMALL DENT IN FWD CARGO DOOR SKIN 23" AFT OF FWD EDGE AND 14" FROM BOTTOM EDGE. DENT EXCEEDS ALLOWABLE LIMIT. WILL REQUIRE PERMANENT REPAIR AT NEXT C-CHECK OR BEFORE 24 MONTHS WITH VISUAL INSPECTION EVERY 300 CYCLES. REF SRM 52-30-01, PG 103, STEP J. DATA RETRIVAL FORM C/W. DENT IS .020 INCH DEEP AND .5" LONG.

Part: A/C PACK — SMOKE (LEFT) · airframe 63,891 hrs · 29,627 cycles

BURNING ODOR NOTED AFTER TAKEOFF. SMOKE, FIRE OR FUMES, CHECKLIST COMPLIED WITH. ODOR DISSIPATED IN COCKPIT WITH LT PACK OFF. ODOR STILL NOTED IN CABIN FOR REMAINDER OF FLIGHT. MX INSPECTED EQUIPMENT COOLING AND RECIRCULATION FANS. OPENED LT ENG BUT NO OIL LEAKS WERE NOTED. INSPECTED 2.5 BLEED AND INLET AREA WITH NO TROUBLE FOUND. RAN BOTH ENGINES WITH ENGINE BLEED AND PACKS ON AND THERE WAS NOT ANY ODOR FROM AIR VENTS. AIR CONDITION SYS, OPS CHECK NORMAL.

Part: SKIN — DAMAGED (BS 1340 S3R) · airframe 45,328 hrs · 21,739 cycles

FUSELAGE/CROWN SKIN STA 1340, STR 3R REPAIR IAW ERA 090306-14C/W ERA 090306-14. ORIGINAL DIFFICULTY DATE: 5-27-2004

Part: LIGHT — INOPERATIVE (SEAT 23D) · airframe 63,210 hrs · 29,317 cycles

DURING LAYOVER CHECK, MX FOUND EMERGENCY LIGHT INOPERATIVE AT SEAT 23D. REPLACED LIGHT ASSY AT SEAT 23D.

Part: BUSHING — CORRODED (NLG TRUNNION) · airframe 62,485 hrs · 28,976 cycles

UPON REMOVAL OF NLG BUSHINGS FOR TRUNNION RT INBD AND OTBD FOUND PITTING CORROSION IN BORE/ ACCOMPLISHED ER/A 484137-14 REV ORIG AT SAA ON N/R CARD 174631(DL757102217).

Part: SUPPORT FITTING — DAMAGED (RT WING) · airframe 62,485 hrs · 28,976 cycles

WHILE ACCOMPLISHING EA 06-070332-03, AD REV J SPOT FACE DEPTH FOR HOLES MARKED 3 AND 4 ON NEW SUPPORT FITTING PN 012N8888-2 FOR THE RT WING WAS EXCEEDED TO ATTAIN 100 PERCENT SPOT FACE. COMPLIED WITH ER/A 484129-14 AD DURING HMV AT SAA ON N/R CARD 174576.

Part: FITTING — CRACKED (RT PYLON) · airframe 32,485 hrs · 28,976 cycles

FOUND 1 EA HOLE WITH POSSIBLE CRACK EXTENDING FROM IT INSIDE FUEL TANK. HOLE IDENTIFIED ON LWR R WING PYLON SIDE LOAD FITTING AREA AS A-24 / ACCOMPLISHED ER/A 484133-14AD REV A AT SAA.

Part: SUPPORT FITTING — DAMAGED (NACELLE) · airframe 62,485 hrs · 28,976 cycles

WHILE ACCOMPLISHING EA 06-070332-03, AD REV J, SPOTFACE DEPTH FOR HOLES MARKED 3 AND 4 ON NEW SUPPORT FITTING PN 012N8888-1 WAS EXCEEDED TO ATTAIN 100 PERCENT SPOTFACE.

Part: BULKHEAD — CHAFED (NR 1 PYLON) · airframe 62,485 hrs · 28,976 cycles

NR 1 PYLON AFT BULKHEAD INBD SIDE LWR AREA CHAFED. C/W ER/A 483509-14AD REV ORIG AT SAA DURING HMV ON N/R CARD 174461.

Part: BULKHEAD — CHAFED (NR 2 PYLON) · airframe 62,485 hrs · 28,976 cycles

AFTER REMOVAL OF NR 2 PYLON AFT BULKHEAD NAC STA 201 FOUND INBD SIDE LOWER CORNER CHAFED.

Part: BULKHEAD — CHAFED (NR 1 PYLON) · airframe 62,485 hrs · 28,976 cycles

NR 1 PYLON AFT BULKHEAD OTBD SIDE LWR AREA CHAFED. ACCOMPLISHED ER/A 483508-14AD, REV ORIG AT SAA DURING HMV ON N/R CARD 174462.

Part: SKIN — DAMAGED (NR 2 PYLON) · airframe 62,485 hrs · 28,976 cycles

AFTER REMOVAL OF LT SKIN ON NR2 PYLON, FOUND DAMAGED HOLE AT STA 114 UPPER CHORD AREA.

Part: FRAME — DAMAGED (NR 2 PYLON) · airframe 62,485 hrs · 28,976 cycles

AFTER SKIN REMOVAL ON NR2 PYLON OTBD SIDE RT FOUND 1 EA OVERSIZE HOLE FWD FRAME LWR HOLE AT STA 108. COMPLIED WITH ER/A 483519-14 REV ORIG AT SAA. DURING HMV ON N/R CARD 169569.

Part: SKIN — DENTED (BS 606 S17L) · airframe 62,485 hrs · 28,976 cycles

FUSELAGE EXTERNAL SKIN HAS A DENT STA 606 AND S-17L, COMPLIED WITH ER/A NR484136-14 REV ORIGINAL AT SAA SAT ON NON ROUTINE 169561.

Part: SKIN — DENTED (BS 1394-1396) · airframe 62,485 hrs · 28,976 cycles

3 DENTS ON LWR FUSELAGE SKIN EXTERIOR SURFACE BETWEEN S28R AND S29L AT STA 1394, 1395, AND 1396 AND SEVERAL SCRATCHES ON DENTED AREA. ACCOMPLISHED ER/A 484128-14 AT SAA DURING HMV ON N/R CARD 169560.

Part: SKIN — DENTED (BS 662) · airframe 62,485 hrs · 28,976 cycles

DENT ON FUSELAGE SKIN EXTERIOR SURFACE AT STA 662 BELOW LAP JOINT S19R.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 62,485 hrs · 28,976 cycles

MAIN CABIN FLOORBEAM SURFACE CORRODED STA 1640, LBL 2 FWD SIDE AT FASTENER HOLE. COMPLIED WITH ER/A 483503-14 REV ORIG AT SAA DURING HMV ON N/R CARD 166753.

Part: CUSP WEB — CORRODED (BS 620-640 S17R) · corrosion level 2 · airframe 62,485 hrs · 28,976 cycles

MAIN CABIN CUSP WEB CORRODED STA 620-640 AT STR 17R / REPLACED CUSP WEB DURING HMV AT SAA ON N/R CARD 163871.

Part: CUSP WEB — CORRODED (BS 1020-1040) · corrosion level 2 · airframe 62,485 hrs · 28,976 cycles

MAIN CABIN CUSP WEB CORRODED STA 1020-1040, DOUBLER FWD OF STA 1040 ALSO CORRODED, INBD STR 17R. REMOVED CORROSION ON CUSP WEB AND REPLACED DOUBLER AT STA 1040 AT SAA SAT ON NON ROUTINE CARD.

Part: CUSP WEB — CORRODED (BS 960-984) · corrosion level 2 · airframe 62,485 hrs · 28,976 cycles

MAIN CABIN CUSP WEB & ATTACHED STRUCTURE CORRODED STA 960-984 LT. R & R CUSP WEB AND ANGLE AT SAA SAT ON NON ROUTINE 166693.

Part: GATE — CORRODED (R2 DOOR) · airframe 62,485 hrs · 28,976 cycles

R2 DOOR LOWER GATE BOTTOM EDGE HAS PITTING. R & R NEW LOWER GATE ASSEMBLY AT SAA.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,485 hrs · 28,976 cycles

AFT FUSELAGE ACCESS DOOR 313AL OUTER SKIN AND INNER AREA HAS CORROSION RL012 / REPLACED AFT FUSELAGE DOOR AT SAA.

Part: SILL — CORRODED (BS 1380-1420) · corrosion level 2 · airframe 62,485 hrs · 28,976 cycles

AFT CARGO DOOR SILL UPPER CHORD CORRODED ON INTERIOR SIDE LOWER SURFACE AT NUTPLATES STA 1380-1420/ REPLACED AFT CARGO DOOR SILL AT SAA DURING HMV ON N/R CARD 166656.

Part: PAN — CORRODED (BS 700-720) · corrosion level 2 · airframe 62,485 hrs · 28,976 cycles

FWD CARGO LAV SERVICE PAN UPPER AND INBD DOUBLERS CORRODED STA 700-720 BETWEEN STRINGERS 20 & 22R. R & R LAV PAN DOUBLERS AT SAA SAT ON NON ROUTINE CARD 166673.

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 62,485 hrs · 28,976 cycles

CORROSION ON MAIN DECK FLOORBEAM UPPER CHORD TOP SURFACE STA 377 BETWEEN LBL 9 AND LBL 19. REPAIRED FLOORBEAM AT DURING HMV ON N/R CARD 164359.

Part: INTERCOSTAL — CORRODED (BS 1420-1440) · corrosion level 2 · airframe 62,485 hrs · 28,976 cycles

AFT CARGO INTERCOSTAL LOWER LEG CORRODED STA 1420-1440 BETWEEN STR 28 & 29L. R & R INTERCOSTAL DURING HMVAT ST AEROSPACE SAT ON NON ROUTINE 164231.

Part: CONNECTOR — LOOSE (CABIN) · airframe 61,985 hrs · 28,686 cycles

DURING SVC CK AD6, FOUND WHITE EMERGENCY ESCAPE PATH LIGHTS INOP AT SEAT ROWS 23FED, 38FED, AND 44FED, PLUS FWD LEFT OVERWING EXIT DOOR EXIT LIGHT INOP, AND ONE RED EMER ESCAPE PATH LIGHT INOP AT SEAT ROW 26FED. FOUND LOOSE CONNECTOR AT SEAT ROW 38FED, RECONNECTED SAME, OPS NORMAL. RELAMPED RED LIGHT AT SEAT 26FED, OPS NORMAL. REPLACED LT FWD ESCAPE DOOR EXIT SIGN AND RE-TERMINATED WIRING, OPS NORMAL. FWD 23FED AND 44FED EMER ESCAPE PATH LIGHTS TO MCO/PLAC33-51-03.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,293 hrs · 27,367 cycles

MAINTENANCE AT ATL, A LIGHTNING STRIKE WAS FOUND AT STA 508 BETWEEN S-28R AND S-28L. THE DAMAGE WAS TRIMMED OUT AND REPAIRED PER ER/A 06-232915-14 DATED 02-02-91. AT THE TIME OF ISSUE, AN MRR WAS NOT SUBMITTED. THIS SUBMITTAL CORRECTS THAT SITUATION.

Part: POWER CABLE — FRAYED (COCKPIT) · airframe 56,908 hrs · 26,297 cycles

F/O SEAT ELECTRICAL ARC AND SEAT UNPOWERED. PWR CORD FRAYED. REMOVED CORD. FWD TO MCO/PLAC MEL 25.11.01A. REPLACED PWR CORD ON F/O SEATS CKS GOOD MCO/PLAC REMOVED.

Part: WINDOW — CRACKED (PAX CABIN) · airframe 55,858 hrs · 25,802 cycles

ON MECHANICS PREDEPARTURE CHECK, FOUND A CRACKED OUTER PANE ON PASSENGER WINDOW 31ABC. ON FURTHER INSPECTION, FOUND WINDOW AT 30 ABC ALSO CRACKED. REPLACED BOTH OUTER PANES.

Part: IDG — INOPERATIVE (NR 2 ENGINE) · airframe 55,566 hrs · 25,690 cycles

ON TAKEOFF, AROUND 60 KTS RT ENG GEN DRIVE LIGHT ON WITH EICAS MSG. ABORTED T/O. REPLACED RT ENG IDG AND GCU. NO FAULTS ON BPCU.

Part: TIRE — FAILED (RT MLG) · airframe 51,567 hrs · 24,067 cycles

NR 3 MAIN TIRE FAILED DURING RTO. RT SIDE BRAKE TEMP AT 3 HIGHEST. REPLACED NR 3 WHEEL ASSY BRAKE TEMP AT 3 DOES NOT REQUIRE HIGH ENERGY STOP INSP.

Part: COMPRESSOR — FAILED (AFT CARGO) · airframe 49,271 hrs · 23,247 cycles

DURING DE-PLANING NOTICED SMOKE AND FUMES IN AFT CABIN FROM ROW 20 TO AFT GALLEY. REPLACED POTABLE WATER COMPRESSOR.

Part: WASHER — BROKEN (NR 8 SLAT) · airframe 48,954 hrs · 23,121 cycles

LEADING EDGE SLAT DISAGREE MESSAGE ON INITIAL FLAP EXTENSION. FOUND RETAINING NUT LOOSE AND LOCK WASHER BROKEN ON NR 8 SLAT INBOARD ROTARY ACTUATOR. REPLACED WASHER AND RE-TORQUED NUT.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 45,329 hrs · 21,740 cycles

FUSELAGE C2 DOOR OPENING FRAME AND SILL FS 1440, SILL CHORD REPLACEMENT AND FRAME SPLICE REPAIR. THE OUTER CHORD OF THE LOWER SILL BEAM OF THE C2 DOOR OPENING WAS FOUND WITH SEVERAL AREAS OF CORROSION AND REQUIRED REPLACEMENT. TO FACILITATE REPLACEMENT, THE FS 1440 FRAME OUTER CHORD AND WEB WERE CUT AND THE LOWER SECTIONS REMOVED. THE SILL CHORD WAS REPLACED AND THE FRAME SECTION SPLICED BACK WITH ALUMINUM REPAIR DOUBLERS PER ER/A 090314-14, REV A.

Part: SKIN — DELAMINATED (NR 4 SLAT) · airframe 45,328 hrs · 21,739 cycles

ACCOMPLISHED METAL BOND REPAIR TO UPPER INBOARD SKIN ON THE NUMBER 4 SLAT.

Part: SWITCH — FAILED (LAV DOOR LIGHT) · airframe 44,760 hrs · 21,540 cycles

ON TAXI IN THE FLIGHT ATTENDANT IN THE MID SECTION DETECTED SMOKE FROM THE MID LAV. REPLACED LAV DOOR LATCH LIGHT SWITCH.

Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 41,797 hrs · 20,296 cycles

REPLACED BATTERY PACK ON F/C CHARGER FOR SEAT PATH LIGHTING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,110 hrs · 19,054 cycles

EMERGENCY LIGHT AT 26D INOP. REPLACED BASE, CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,093 hrs · 18,542 cycles

R2 EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK, TESTS NORMAL NOW.

Part: ENGINE — FAILED (NR 1)

LOST NR 1 ENG EPR IND ON EICAS THEN ENG ROLLED BACK WITH AUDIBLE POP. F/A AND PASS REPORT FLAME FROM TAILPIPE. SHUTDOWN ENG AND DIVERTED TO CPR. REPLACED EEC.

Part: CONTROLLER — FAILED (E & E COMPT)

AUTO 1 PRESSURIZATION FAILURE AT 31,000 FT. CABIN ALT WARNING CAME ON, DID NOT EXCEED 10,000 FT. REPLACED 1 PRESS CONTROLLER. BITE FAULTS SELECT PANEL. REPLACED SAME. PRESS A/C, ALL OPS NORMAL.

Part: SKIN — LIGHTNING STRIKE (BS 400)

FUSELAGE/WINDOW BELT SKIN, LT, NR 1 WINDOW, STA 400. REPAIR FOR LIGHTNING STRIKES. THE LT WINDOW BELT SKIN AT STA 400 SUFFERED A LIGHTNING STRIKE ON THE FWD SIDE AND THE AFT SIDE OF THE NR 1 WINDOW CUTOUT. BOTH DAMAGED AREAS WERE CLEANED UP WITH .50 HOLES. ALUMINUM BUSHINGS WERE INSTALLED IN THE HOLES AND AN ALUMINUM DOUBLER WAS INSTALLED AROUND THE WINDOW PER ER/A 364571-14, REV B.

Part: ENGINE — FAILED (NR 2)

ON DESCENT AT APPROX FL240, THE RIGHT ENGINE FLAMED OUT WITH A SUDDEN YAW MOVEMENT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. DURING INSPECTION SMALL PIECES OF METAL WERE FOUND IN THE EXHAUST SECTION.