N67158

Part: SPRING — WRONG PART (R1 DOOR) · airframe 44,935 hrs · 6,614 cycles

SUPPORT TASK CABIN - R1 DOOR SLIDE DEPLOYMENT BAR AFTER POSITION SEPARATION LINK ATTACH SPRING FOUND INCORRECT PARTS. CABIN R1 DOOR SLIDE DEPLOYMENT BAR AFTER POSITION SEPARATION LINK ATTACH SPRING REPLACED AS EPR EA 2566-01036 REV A AND CMM 25-66-30.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 44,935 hrs · 6,614 cycles

767-53-3-0164U CABIN - RT STA 412 RBL 20 SEAT TRACK FLANGE FOUND CRACKED. CABIN RT STA 344 TO STA 412 RBL 20 SEAT TRACK REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 NEW TRACK FABRICATED DETAIL REF NRC 5754156 (200-0920) ATT MAINTENANCE WORKSHEET FORM 44.0008 ITEM 1 TO ITEM 5 ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (STA 325) · airframe 44,935 hrs · 6,614 cycles

BS 325 LBL 26 TO 55 FLOORBEAM CORRODED. REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201. HFEC NO CRACK FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,164 hrs · 5,577 cycles

L2 DOOR THRESHOLD EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,164 hrs · 5,577 cycles

EMERGENCY EXIT LIGHT FWD OF CARGO DOOR IS INOPERATIVE. RELAMPED LIGHT, OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,996 hrs · 5,416 cycles

LEFT WING SLIDE GROUND ILLUMINATION LIGHT INOP, EXTERIOR EMERGENCY LIGHT AT STATION 1230. REPLACED EMERGENCY LIGHT ASSY, OP CHECKED GOOD PER MM 33-51-06.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 34,016 hrs · 5,139 cycles

CABIN - BS 325 LBL 27- LBL 60 FLOOR SUPPORT FOUND CORRODED. CABIN BS 325 LBL 16- LBL 62 FLOORBEAM SUPPORT REPAIRED PER SRM 53-00-51 REPAIR 1, FIG 201. HFEC NO CRACK FOUND.

Part: SKIN — GOUGED (FUSELAGE) · airframe 34,016 hrs · 5,139 cycles

FOUND FASTENER AT STA 368 AROUND S-30 DAMAGED BY LIGHTNING STRIKE. TOTAL DAMAGE 0,250 IN RIVET HEAD DAMAGE 0,091 IN. PER SRM 53-00-01 P103 TABLE III DETAIL IV NEEDS FASTENER REPLACEMENT WITHIN 50 FLIGHT CYCLES. PERFORMED INTERIM REPAIR PER PART 1-2. PERFORM INSPECTIONS AT INTERVALS NOT TO EXCEED 30 DAYS AND ACCOMPLISH A PERMANENT REPAIR WITHIN 90 DAYS. REFERENCE L/P 9100380 FOR INTERIM REPAIRS AT STATION 325, 347 AND 412. ALL WORK WAS PERFORMED FROM ECRA 5330-03837. INSPECTED INTERIM REPAIR AT STATION 368 IAW ECRA 5330-03837, PART 2, NO DEFECTS NOTED. INSPECTED AREA, REF ECRA 5330-03837 PART II, REPAIR SECURE. NO FURTHER DAMAGE. DIP REMAINS. FUSELAGE SKIN STA 368 S30L REPAIRED AS PER ECRA 5330-03837 REV D PART 3 ITEM 3 AND BLIND FASTENER REPLACED SOLID FASTENER AS PER SRM 53-00-01 REPAIR 8 FIG 201. HFEC NO CRACK FOUND. FOUND LIGHTNING STRIKE DMG, STA 368, STR 30LT, AT RIVET PER SRM 53-00-01, ALLOWABLE DMG 1, PG 103,TABLE 3, C/W REPAIR 8 W/I 50 FLT CYC''S. ISSUED DIP CONTROL NR D 089867 PER EC/RA 5330-03837 REV A FOR INTERIM REPAIR AT LOCATION STA 368 S-30 REVISE INSPECTIONS TO BE PERFORMED AT INTERVALS NOT TO EXCEED 30 DAYS AND ACCOMPLISH A PERMANENT REPAIR WITHIN 90 DAYS. PER MRB DIP EXT DATED 08-30-08, LIMITS REVISED AS FOLLOWS: 1) RIR: EVERY 30 DAYS & 2) T/A: W/I 90 DAYS.

Part: SKIN — GOUGED (FUSELAGE) · airframe 34,016 hrs · 5,139 cycles

LIGHTNING STRIKE DAMAGE AT 4 LOCATIONS SEE L/P 8072815 STA 111, 129, 412 STA 111 S-30 DMG DIAM 0.184 IN RIVET HEAD DMG 0.066 IN. STA 129 S-30 DMG DIAM 0.170 IN RIVET HEAD DMG 0.056 IN. STA 412 S-30 DMG DIAM 0.147 IN RIVET HEAD DMG 0.071IN. WITHIN LIMITS PER SRM 53-00-01. BURNISHED, PUT ON DIP WILL NEED TO REPLACE WITHIN 50 FLIGHTS REFERNCE ECRA 5330-03837 CORRECT STATION NUMBERS ARE AS FOLLOWS (325, 347, AND 412) PERFORMED INTERIM REPAIR AT STATIONS (325, 347 AND 412) PERFROM INSPECTIONS AT INTERVALS NOT TO EXCEED 30 DAYS AND ACCOMPLISH REPAIR WITHIN 90 DAYS . SEE L/P 8072815 FOR INTERIM REPAIR ATE STATION 368. INSPECTED INTERIM REPAIRS IAW ECRA 5330-03837, STATORS 325 347 AND 412 NO DEFECTS NOTED. INSPECTED AREA REF ECRA 5330-03837 PART II, REPAIR FASTER SECURE. DIP REMAINS. FX SKIN STA 325 S31L SKIN REPAIRED AS PER ECRA 5330-03837 REV D PART 3 ITEM 1. BS 347 AND BS 412 ARE ACCEPTABLE AS PER ECRA 5330-03837 REV D PART 3 ITEM 2 AND 4 . STA 368.8 SKIN REPAIRED AS PER ECRA 5330-03837 REV D ITEM 3. REF L/P 8072815, FOUND LIGHTNING STRIKE DMG, STA 111, 129 & AMP;412, STR 30LT PER SRM 53-00-01, ALLOWABLE DMG 1, PG 103, W/I 50 FLT CYC''S C/W REPAIR 8. ISSUED DIP CONTROL D 089877 PER EC/RA 5330-03837 REV A CORRECT LOCATIONS ARE AS FOLLOWS, (STA 325, 347 AND 412 S-30). REVISE INSPECTIONS TO READ, PERFORM AT INTERVALS NOT TO EXCEED 30 DAYS AND ACCOMPLISH A PERMANENT REPAIR WITHIN 90 DAYS. PER MRB DIP EXT DATED 08-30-08, LIMITS REVISED AS FOLLOWS: 1) RIR: EVERY 30 DAYS & AMP; 2) T/A: W/I 90 DAYS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,016 hrs · 5,139 cycles

CABIN - BS 303 LBL 26-44 FLOOR SUPPORT FOUND CORRODED. CABIN - BS 303 LBL 7 TO LBL 62 FLOOR SUPPORT BEAM UPPER FLANGE REPAIRED PER SRM 33-00-51 REPAIR 1, FIG 201. HFEC NO CRACK FOUND.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 23,287 hrs · 3,667 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 30-60. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.

Part: STIFFENER — CRACKED (BS 275) · airframe 23,287 hrs · 3,667 cycles

INSPECTION FOUND NR 2 PYLON I/B CLIP, FRAME, AND STIFFENER CRACKED AT STA 275. THE CLIP, FRAME, AND STIFFENER WERE REPLACED IAW SRM 51-10-02.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 23,287 hrs · 3,667 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 25-60. REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (BS 303-325) · airframe 23,287 hrs · 3,667 cycles

INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303-325, LBL 32. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02 AND 51-40-02.

Part: SKIN — CRACKED (BS 285) · airframe 23,287 hrs · 3,667 cycles

INSPECTION FOUND NR 2 PYLON I/B MID-SPAR AREA ONE EACH FASTENER HOLE HAD A 0.06" CRACK IN SKIN AT STA 285. THE SKIN WAS REPAIRED IAW ECRA 5430-01784.

Part: ENGINE — FAILED (RIGHT) · airframe 17,434 hrs · 2,801 cycles

ON TAKEOFF, AT APPROXIMATELY 90 KNOTS, RT ENGINE FAILED. REPLACED ENGINE.