N796FD

Part: SEAT TRACK — CRACKED (BS 580-) · airframe 71,532 hrs · 27,098 cycles

MAIN CABIN - STA 580 SEAT TRACK IS CRACKED ACCOMPLISHED FEDEX EA # F-5310-T0361001-P1 : FUSELAGE - MAINFRAME - SEAT TRACK STA 580 LBL 45, CRACKED FLANGE

Part: CUSP WEB — CRACKED (BS 640-660) · airframe 71,532 hrs · 27,098 cycles

MAIN CUSP AREA STA 640-660 LBL 62.5 AS VIEWED FROM BOTTOM FILLER PN BACF3F020B197NN CRACKED AT FASTENER LOCATION ACCOMPLISHED FEDEX EA # F-5321-T0361228-P1 FUSELAGE - CARGO COMP FLOORS - MAIN CABIN - STA 640 - LBL - 62.5 - CRACKED

Part: STUB FRAME — CRACKED (BS 580) · airframe 71,532 hrs · 27,098 cycles

MAIN CABIN FLOOR - STUB BEAM IS CRACKED REPAIRED STUB BEAM IAW FEDEX DWG SR57-53-004 AND EA: F-5310-T0361029: FUSELAGE - MAINFRAME - STA 580 FLOOR BEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR - REPAIR DOCUMENTATION AND REPETITIVE INSPECTIONS PER SR57-53-004

Part: NOZZLE — CRACKED (NR 2 ENG EXHAUST) · airframe 70,973 hrs · 26,707 cycles

NR 2 ENGINE EXHAUST NOZZLE 9 O'CLOCK POSITION MOUNT FLANGE CRACKED. REPAIRED NR 2 ENGINE EXHAUST NOZZLE 9 O'CLOCK POSITION MOUNT FLANGE, PER CMM 78-11-01 REP 2-1.

Part: TRANSITION PANEL — GOUGED (BS 1510) · airframe 70,973 hrs · 26,707 cycles

AFT CARGO PIT LH STA 1510 TRANSITION PANEL HAS GOUGE REPAIRED TRANSITION PANEL L/H STA 1510 IAW B757 SRM 53-00-53-2R DUE TO TRANSITION PANEL GOUGE FOUND TO BE OUT OF LIMITS PER B757 SRM 53-00-53-1A, DETAIL V.

Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 70,973 hrs · 26,707 cycles

TAIL SECTION LT LOWER HORIZONTAL STAB SEAL FAIRING DENTED/CRACKED. REPAIRED TAIL SECTION LT LOWER HORIZONTAL STAB SEAL FAIRING, IAW FEDEX EA NR F-5350- T0356088-P1 FUSELAGE-AERODYNAMIC FAIRINGS-LT HORIZONTAL STABILIZER TO BODY LWR BLADE ASSY DAM.

Part: FAIRING — CRACKED (HORIZONTAL STAB) · airframe 70,973 hrs · 26,707 cycles

TAIL SECTION L/H LOWER HORIZONTAL STAB. SEAL FAIRING DENTED/ CRACKED. REPAIRED TAIL SECTION L/H LOWER HORIZONTAL STAB SEAL FAIRING IAW FEDEX EA# F-5350- T0356088

Part: ANGLE — CRACKED (NR 2 NACELLE) · airframe 70,973 hrs · 26,707 cycles

NR 2 PYLON 445BL HAS A CRACKED CLIP. REMOVED, FABBED, AND REPLACED NEW CLIP IAW BOEING DWG 313N5022 REV AB.

Part: BARRIER — CRACKED (NR 2 NACELLE) · airframe 70,973 hrs · 26,707 cycles

NR 2 ENGINE INBOARD UPPER PYLON FWD AREA JUST ABOVE THE INBOARD T/R PLASTIC SHIELD IS CRACKED IN TWO PLACES. REPAIRED NR 2 ENGINE INBOARD AFT FLUID BARRIER ON 2 EA AREAS, IAW FEDEX EA F-5450-T0356144-P1, NACELLES/PYLON - WING PYLON/STRUT NR #2 (RT) PYLON INBOARD FLUID BARRIER STIFFENER, CRACK REPAIR.

Part: BRACKET — CRACKED (RT WG FUEL DOOR) · airframe 70,973 hrs · 26,707 cycles

RT WING FUEL DOOR SWITCH BRACKET CRACKED STREAMER ATTACHED. REMOVED AND REPLACED BRACKET PER BOEING DWG NR 284N1138 AND B757 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,973 hrs · 26,707 cycles

CABIN SEAT TRACK CORRODED BS 365, BL 44R - BL 47R. ACCOMPLISHED EA# F-5310-T0356090-P1 FUSELAGE - MAINFRAME - SEAT TRACK - STA 365 - RBL 45.50 - CORROSION.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,973 hrs · 26,707 cycles

CABIN SEAT TRACK CORRODED BS 342- BS 372, BL 7L REMOVED CORROSION AS REQUIRED IAW B757 SRM 51-10-02. MAX ALLOWABLE MAT REMOVAL .020, REMOVED .030. FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101 DET "I". FABRICATED NEW SEAT TRACK AND INSTALLED IAW FEDEX EA F-5310-T0356136 "FUSELAGE - MAINFRAME - STA 345-377 (RBL 13 & LBL 7) SUPERNUMERARY SEAT TRACK - MATERIAL SUB" AND VENTURA DWG 3470 REV G.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 70,973 hrs · 26,707 cycles

CABIN FLOOR BEAM CORRODED BS 375, BL354L. REMOVED CORROSION IAW B757 SRM 51-10-02. DAMAGE FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-51-1A. ACCOMPLISHED FLOOR BEAM REPAIR IAW FEDEX EA "F-5310-T0356115-P1. FUSELAGE-MAINFRAME, MAIN CABIN FLOOR BEAM STA 377-LBL 35-SRM REPAIR CLARIFICATION AND B757 SRM 53-00-51-2R DETAIL I REPAIR II.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 70,973 hrs · 26,707 cycles

FLOOR BEAM NUTPLATE IS CORRODED BS 1681-RBL47. REMOVED NUTPLATE BRACKET IAW B757 SRM 51-40-02. MAT ID 7075-T6 ALUMINIUM SHEET PO NR 964704.1, IAW BOEING PL 146N5693 REV C AND BOEING DWG 146N5693 REV B. FABRICATED NUTPLATE STRIP IAW BOEING DWG 146N5693 REV B. APPLIED ALODINE, PRIME AND PAINT IAW B757 SRM 51-20-01-0G. INSTALLED NUTPLATE STRIP IAW B757 SRM 51-40-02. PART MARKED IAW GMM 07-0-1000 STEP 7B. INSTALLED NUTPLATE STRIP IAW BOEING DWG # 146N5300 REV C AND B757 SRM 51-40-02-0G AND SRM 53-60-51-2R.

Part: SEAL — CRACKED (EXHAUST NOZZLE) · airframe 70,973 hrs · 26,707 cycles

#1 ENG EXHAUST NOZZLE O/B UPPER SPRING LEAF CRACKED REMOVED AND REPLACED SPRING LEAF PER B757 SRM 51-40-02-0G AND REF IPC 78-11-01-03

Part: BULKHEAD — CRACKED (NR 2 NACELLE) · airframe 70,973 hrs · 26,707 cycles

#2 PYLON HYDRAULIC BAY,AFT OF BULKHEAD THE OTBD LWR FWD CORNER ATTACH CLIP IS CRACKED REMOVED AND REPLACED CLIP PER BOEING DWG #313N3052

Part: WIRE — BROKEN (CABIN) · airframe 69,693 hrs · 25,879 cycles

FOUND EMERGENCY EXIT LIGHT AFT OF THE COCKPIT DOOR INOP REMOVED THE LIGHT FOUND 2 BROKEN WIRES REPINNED CONNECTOR D4524 ON THE EMERGENCY EXIT LOCATION LIGHT. LIGHT OPS CHECKS NORMAL REF SWP 33-51-12 PG 904 NO PART WAS CHANGED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 68,845 hrs · 25,304 cycles

DURING A SERVICE CHECK, FOUND THE EXTERNAL RT DOOR SLIDE LIGHT INOPERATIVE. REPLACED THE LAMP, OPS CHECKED GOOD IAW 33-51-06-2-1.

Part: WIRE HARNESS — DAMAGED (COOLING FAN) · airframe 68,841 hrs · 25,302 cycles

EQUIPMENT OVERHEAT EICAS MESSAGE DURING CLIMBOUT. HAD A STATUS MESSAGE FOR EQPT CLG FLOW AND EQPT CLG FAN, CIRCUIT BREAKER TRIPPED FOR ALTERNATE COOLING FAN. AFTER TOUBLESHOOTING, FOUND WIRE BUNDLE W4104, CONTAINING WIRES W4104-0008-16, -0009-16, -0010-16, -0011-16, AND -0012-16, FUSED TOGETHER. REMOVED AND REPLACED ALL DAMAGED WIRES IAW SWPM 20-30-12. TERMINATED NEW WIRES AT CONNECTOR D1628 IAW SWPM 20-61-11. RANG OUT WIRES BETWEEN RELAY K344, AND D1628. OPS CHECKED GOOD IAW AMM 21-58-06-5.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 68,580 hrs · 25,123 cycles

PRIOR TO LOADING, RAMP DISCOVERED PUNCTURE IN FUSELAGE FWD OF MAIN CARGO DOOR. REPAIRED IAW EA F-5330-T0336569 PT 1 AND 2.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,520 hrs · 25,088 cycles

R1 EMERGENCY SLIDE LIGHT INOPERATIVE DURING A TEST. REPLACED THE LAMP AND OPS CHECKED NORMAL IAW MM 33-51-06. ACFT OK FOR SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,545 hrs · 24,424 cycles

AFT FUSELAGE SKIN HAS A BULGED AREA BS 1540 STRINGER 28R. FOUND SHEAR TIE CORRODED. REMOVED IAW SRM 51-40-02-OG, FABRICATED IAW B DWG 140N2002, REV B , HEAT TREATED IAW FORM FAS 0119, REV O AND INSTALLED SHEAR TIE IAW DWG 140N2002, REV B AND SRM 51-40-02-OG .

Part: CABLE — UNSECURE (EVAC SLIDE) · airframe 663 hrs · 23,573 cycles

R1 DOOR DISARMING HANDLE WILL ONLY GO HALFWAY, WILL NOT MOVE INTO THE GREEN ZONE ENTIRELY. IAW AMM 25-66-10-2-0 FOUND CORD FROM SLIDE STUCK IN FWD GIRT BAR. SECURED CORD, GIRT BAR & SLIDE CHECKED NORMAL.

Part: SLIDING WINDOW — OUT OF ADJUST (COCKPIT) · airframe 66,103 hrs · 23,382 cycles

CAPTAIN'S SLIDING WINDOW WILL NOT OPEN. ADJUSTED CAPTAIN`S SLIDING WINDOW IAW AMM 56-11-02-5. OPERATIONS CHECKED GOOD.

Part: REPAIR — SCRATCHED (FUSELAGE) · airframe 65,973 hrs · 23,289 cycles

FUSELAGE EXTERIOR SKIN, EXISTING REPAIR FINDING LT SIDE THERE ARE SCRATCHES ON THE EXTERIOR OF THE EXISTING REPAIR BODY STATION 439 - 449 BETWEEN STRINGER 26 - 27. REMOVED & NEW REPAIR CARRIED OUT AS PER PART 1 OF EA F-5310 -T0310235. TITLE FUSELAGE MAIN FRAME EXISTING EXTERIOR SKIN REPAIR BETWEEN BS - 439 & 449 & BETWEEN 26L & 28L REPAIR. SEE SNRM N00141 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 65,973 hrs · 23,289 cycles

AFT CARGO COMPARTMENT LT SIDE EXISTING REPAIR FINDING BS 1580 AT STRINGER 25 - 26. AFTER OUTER J CHANNEL REMOVED FOUND ELONGATED HOLE. AFT CARGO COMPARTMENT AT STA 1580 STR 25-26 ELONGATED HOLE ACCOMPLISH AS PER EA 5310- T0310064 P1 TITLE : FUSELAGE - MAINFRAME - AD 2006-11-11- FUSELAGE STA 1580. FRAME INBOARD CHORD REPAIR BETWEEN STRINGERS S-24L AND S-27L. REPAIR CLASSIFIED AS MAJOR.

Part: FASTENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

FUSELAGE AFT CARGO EXISTING REPAIR RT SIDE THE FASTENERS ARE CORRODED AT BS 1440 - 1460 & STRINGER 26 - 27. ACCOMPLISHED EA F-5330-T0310527 P1 TITLE AD 2006-11-11 FUSELAGE SKIN REPAIR NR 2 CARGO DOORWAY LOWER AFT EDGE BETWEEN BS 1410 TO BS 1445. REPAIR CLASSIFIED AS MAJOR.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 65,973 hrs · 23,289 cycles

FUSELAGE AFT CARGO EXISTING REPAIR RT SIDE THE FASTENERS ARE CORRODED AT BS 1420 - 1440 & STRINGER 26 - 27. ACCOMPLISHED F-5330-T0310527 PT 1 TITLE : AD 2006-11-11- FUSELAGE SKIN REPAIR NR 2 CARGO DOORWAY LOWER AFT EDGE BETWEEN BS 1410 TO BS 1445. REPAIR CLASSIFIED AS MAJOR.

Part: FASTENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

FUSELAGE AFT CARGO EXISTING REPAIR RT SIDE THE FASTENERS ARE CORRODED AT BS 1440 - 1460 & STRINGER 25 - 26. ACCOMPLISHED EA F-5330-T0310527 P1 TITLE : AD 2006-11-11 FUSELAGE SKIN REPAIR NO.2 CARGO DOORWAY LOWER AFT EDGE BETWEEN BS 1410 TO BS 1445. REPAIR CLASSIFIED AS MAJOR.

Part: FITTING — CHAFED (NR 2 PYLON) · airframe 65,973 hrs · 23,289 cycles

NUMBER 2 PYLON AFT BULKHEAD OTBD LOWER CORNER ANGLE FOUND CHAFED MARK. REPAIR CARRIED OUT AS PER EA F-5450-T0311030A PART 1 [REPAIR ON NR 2 PYLON AFT BULKHEAD FITTING, OUTBD FLANGE LOWER CORNER ]. REPAIR IS MAJOR.

Part: FITTING — CHAFED (NR 1 PYLON) · airframe 65,973 hrs · 23,289 cycles

NR 1 PYLON AFT BULKHEAD OTBD LOWER CORNER ANGLE CHAFED. REPAIR CARRIED OUT AS PER EA F-5450-T0311029A PART 1 [REPAIR ON NR 1 PYLON AFT BULKHEAD FITTING, OUTBD FLANGE LOWER CORNER]. REPAIR IS MAJOR.

Part: SKIN — DAMAGED (BS 1400-1420) · airframe 65,973 hrs · 23,289 cycles

FUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1400 - 1420 BETWEEN STRINGER 27 - 28L. REPAIRED IAW EA F-5310-T0310066 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CRACKED (BS 1681) · airframe 65,973 hrs · 23,289 cycles

BS 1681 STRINGER 7L FRAME INBD FLANGE AFT EDGE FOUND CRACKED. REPAIRED IAW EA F-5310-T0309884. CLASSIFIED AS MINOR.

Part: STRINGER — CRACKED (BS 1500) · airframe 65,973 hrs · 23,289 cycles

BS 1500, STRINGER 14R CRACKED. REPAIRED IAW EA F-5310-T0309688 PART 1. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

CABIN FLOORBEAM CORRODED ON THE UPPER SIDE AT BS 365 FROM RBL 10 TO THE RT SIDE. REPAIRED IAW E.A F-5310- T0310519 B PART 1. PEPAIR CLASSIFIED AS MAJOR.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 65,973 hrs · 23,289 cycles

RIGHT WING OTBD TE MAIN FLAP NOSE SKIN LE FOUND CHAFED AT 2.5 INCHES FROM OTBD EDGE. REPAIRED IAW EA F-5750-T0309844 P1. REPAIR CLASSIFIED AS MAJOR.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

AFT CARGO COMPARTMENT STATION 1618 STRINGER 18L, STRINGER HAS CORROSION FOUND AFTER SPLICE. REMOVED IAW SNRM N02602. ACCOMPLISHED EA F-5310-T0309662, TITLE FUSELAGE MAINFRAME SPLICE REPAIR FOR CORRODED STRINGER 18L AT STATION 1618. REPAIR CLASSIFIED AS MAJOR.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,973 hrs · 23,289 cycles

CABIN STATION 1521 - 1519 STRINGER 14R, STRINGER CRACKED. COMPLIED WITH EA F-5310-T0309688 PART 1 TITLE FUSELAGE MAINFRAME SPLICE REPAIR FOR CRACKED STRINGER. REPAIR CLASSIFIED AS MAJOR .

Part: SPLICE PLATE — GOUGED (FUSELAGE) · airframe 65,973 hrs · 23,289 cycles

AFT CARGO COMPARTMENT, STATION 1520, STRINGER 23R - 25R FRAME SPLICE PLATE HAS GOUGE MARKS. GOUGED SPLICE PLATE AT STA 1520, STR 23R-25R, REMOVED AND REPLACED WITH NEW SPLICE PLATE FABRICATED AS PER DWG 146N1042 SHT 4 REV B AND INSTALLED IAW DWG 146N1017 SHT 3 REV D. REPAIR IS MAJOR.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

AFT CARGO COMPARTMENT STATION 1618 STRINGER 20L, STRINGER SPLICE CORROSION AFTER ACCESS. REPAIR CARRIED OUT IAW EA F-5310-T0310628 PART 1. LOCAL FABRICATION TO REPLACE CORRODED THROUGH STRINGER CHANNEL SPLICE. REPAIR IS MAJOR.

Part: SKIN — SCRATCHED (CABIN DOOR) · airframe 65,973 hrs · 23,289 cycles

CABIN L2 DOOR OUTER SKIN FOUND SCRATCHES. COMPLIED WITH EA F-5210-T0310189. REPAIR CLASSIFIED AS MAJOR.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

EMPENNAGE APU AIR INLET DOOR CUT OUT MIDDLE STRAP FOUND CORROSION AT STATION 1825 STRINGER 3R - 6R AFTER APU AIR INLET DOOR HOUSING REMOVED. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-80-15 TABLE 101 ALLOWABLE DAMAGE 1 REV 112 & REPAIR CARRIED OUT AS PER SRM 53-80-15 FIG 202. REPAIR 2 DETAIL 1 REV 112. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

CABIN STATION 688 - 710 RBL 24.75 SEAT TRACK BOTTOM FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-10-02 REV 112. REWORKED AREA CLEANED UP DEPTH OF 0.065" FOUND EXCEED 0.040" LIMIT AS PER SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 REV 112. SEAT TRACK REPAIR CARRIED OUT FROM STA 688 TO STA 750 RBL 24.75 AS PER SRM 53-00-52 OPTION 1 REPAIR 1 FIG 201 REV 112. REPAIR CLASSIFIED AS MAJOR.

Part: RIB — WORN (TE FLAP) · airframe 65,973 hrs · 23,289 cycles

LEFT WING INBD TE AFT FLAP INBD RIB FOUND WORN AT AFT FLAP STATION 78.30, IAW SRM 57-53-02 IDENTIFICATION 1 FIG 1 SHEET 4 OF 8. RIB REMOVED AND REPLACED WITH NEW RIB IAW DWG 113N2800 SHT 4 REV B AND SRM 51-40-02 REV 112. REPAIR IS MAJOR.

Part: FITTING — DAMAGED (NR 2 PYLON) · airframe 65,973 hrs · 23,289 cycles

DURING COMPLYING EO F-7120-7-5000 PT 1, FIG 1 SHEET 1 STEP 7, AFTER REMOVAL OF NR 2 PYLON AFT ENG MOUNT FWD & AFT SHEAR BOLT FLANGE BUSHINGS, HOLES TWO EACH OUT OF DWG TOLERANCE. REPAIR CARRIED OUT AS PER EA F-5450-T0309191 PART 1 [ PYLONS STRUCTURES - SB-757-71- 0093 - OVERSIZED MOUNT HOLES ON NR 1 & NR 2 STRUT AFT ENGINE MOUNT BULKHEAD FITTINGS]. REPAIR IS MAJOR.

Part: FITTING — DAMAGED (NR 1 PYLON) · airframe 65,973 hrs · 23,289 cycles

DURING COMPLYING EO F-7120-7-5000 PT1, FIG 1 SHEET 1 STEP 7, AFTER REMOVAL OF NR 1 PYLON AFT ENG MOUNT FWD & AFT SHEAR BOLT FLANGE BUSHINGS, FOUND BUSHING HOLES TWO EACH OUT OF DWG TOLERANCE. REPAIR CARRIED OUT AS PER EA F-5450-T0309191 PART 1 [ PYLONS STRUCTURES - SB-757-71- 0093 - OVERSIZED MOUNT HOLES ON NR 1 & NR 2 STRUT AFT ENGINE MOUNT BULKHEAD FITTINGS]. REPAIR IS MAJOR.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

EMPENNAGE APU AIR INLET DOOR CUT OUT FWD STRAP HAS CORROSION AT STATION 1787 STRINGER 3R - 6R AFTER APU AIR INLET DOOR HOUSING REMOVED. STA 1787 STR 3R - 6R APU INLET DOOR CUT-OUT CORROSION THROUGH FWD STRAP REMOVED AND REPLACED WITH NEW STRAP P/N 148N3138-20 AS PER BOEING DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR

Part: STRINGER SPLICE — CORRODED (BS 1617) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

AFT CARGO BAY BS 1617 STRINGER 18L, STRINGER SPLICE CORRODED. REMOVED AND REPLACED WITH NEW STRINGER SPLICE IAW DWG 146N3700 SHT.13 REV.B. MAJOR REPAIR.

Part: SEAT TRACK — CHAFED (BS 860-880) · airframe 65,973 hrs · 23,289 cycles

BS 860 - 880 LBL 24.75 SEAT TRACK INNER FLANGE FOUND CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 112. FOUND OUT OF LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 REV 112. REPAIRED IAW SRM 53-00-52 OPTION 1 REPAIR 1 FIG 201 REV 112. REPAIR CLASSIFIED AS MAJOR.

Part: SUPPORT ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

EMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORROSION AT BS 1789, STRINGER 3R. REMOVED AND REPLACED WITH NEW SUPPORT ANGLE DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.

Part: SUPPORT ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

EMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORRODED AT BS 1790 - 1825, STRINGER 6R. REMOVED AND REPLACED WITH NEW ANGLE DWG 148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.

Part: SUPPORT ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 66,481 hrs · 23,189 cycles

EMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORROSION BETWEEN BS 1790 - 1825, STRINGER 3R. REMOVED AND REPLACED WITH NEW SUPPORT ANGLE IAW DWG 148N3105 SHT 1 REV C REPAIR CLASSIFIED AS MAJOR.

Part: SUPPORT ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

EMPENNAGE APU AIR INLET DOOR CUT OUT SUPPORT ANGLE FOUND CORRODED AT BS 1789, STRINGER 6R. REMOVED AND REPLACED WITH NEW SUPPORT ANGLE IAW DWG 148N3105 SHT 1 REV C REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (BS 1570-1590) · airframe 65,973 hrs · 23,289 cycles

BS 1570 - 1590 RBL 45.5 SEAT TRACK FOUND CHAFED. SEAT TRACK REMOVED IAW SRM 51-10-02 REV 111. REWORK AREA AND FOUND OUT OF LIMITS PER SRM 53-00-52 ALLOWANCE DAMAGE 1 FIG 101 REV 112. SEAT TRACK REMOVED AS PER SRM 51-40-02 REV 112. NEW SEAT TRACK FABRICATED AS IAW DWG 146N5137 SHT 2 REV . SEAT TRACK INSTALLED IAW DWG 146N5120 SHT 30 REV. REPAIR CLASSIFIED AS MAJOR.

Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 65,973 hrs · 23,289 cycles

CABIN STATION 1370 - 1390 LBL 45.5 SEAT TRACK CROWN FOUND CHAFED. CABIN STATION 1370 - 1390 LBL 45.5 SEAT TRACK CHAFED MARK. REMOVED IAW SRM 51-10-02 REV 111. REWORKED AREA, CLEANED UP DEPTH 0.03 INCHES FOUND EXCEED 0.02 INCHES LIMIT IAW SRM 53-00-52 ALLOWANCE DAMAGE 1 FIG 101 REV 112. SEAT TRACK REMOVED FROM STATION 1320 - 1540 LBL 45.5 IAW SRM 51-40-05 REV 112. NEW SEAT TRACK FABRICATED IAW DWG 146N5134 SHT 1 REV & INSTALLED IAW DWG 146N5120 SHT 29 REV. REPAIR CLASSIFIED AS MAJOR.

Part: CREASE BEAM — CHAFED (FUSELAGE) · airframe 65,973 hrs · 23,289 cycles

CABIN STATION 790 - 800 RT CREASE BEAM INBD CHORD FOUND CHAFED. COMPLIED WITH EA F- 5310- T0309882 A PART 1 TITLE FUSELAGE MAINFRAME REPAIR FOR RT CREASE BEAM CHORD AT STATION 790 TO 800. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

CABIN STATION 297 RBL 36 - RBL 46 FLOORBEAM TOP SURFACE FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 111. REWORK AREA EVALUATED, MATERIAL THK REMOVED 0.040 INCHES. FOUND EXCEED 10% LIMIT IAW SRM 53-00-5, ALLOWABLE DAMAGE 1 FIG 101 REV 112. FLOORBEAM UPPER ANGLE REMOVED FROM STATION 297 RBL 2 TO 68 IAW SRM 51-40-02 REV 112. NEW FLOORBEAM UPPER ANGLE FABRICATED & INSTALLED IAW DWG 141N5165 SHT 3 REV B. REPAIR CLASSIFIED AS MAJOR.

Part: FRAME — CHAFED (FUSELAGE) · airframe 65,973 hrs · 23,289 cycles

CABIN STATION 1681 STRINGER 9R - 11R FRAME HAS CHAFED MARKS. COMPLIED WITH EA F-5310-T0309911 PART 1 TITLE FUSELAGE MAINFRAME CHAFE MARK BLEND OUT. CUT OUT FUSELAGE FRAME AT BS 1681 BETWEEN STRINGER 10R & 11R REPAIR. REPAIR CLASSIFIED AS MAJOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,973 hrs · 23,289 cycles

BS 1660 RBL 12 FLOORBEAM UPPER FLANGE FOUND CORRODED ON UPPER & LWR SURFACES. REMOVED IAW SRM 51-10-02 REV 111. REWORKED AREA EVALUATED & FOUND MATERIAL LOSS MORE THAN 50% IAW SRM 53-00-51 FIG 101 ALLOWANCE DAMAGE 1 REV 111. FLOORBEAM REMOVED AT STATION 1661 RBL 70 TO LBL 70 IAW SRM 51-40-02 REV 112. NEW FLOORBEAM FABRICATED IAW DWG 146N5110 SHT 3 REV B & INSTALLED IAW DWG 146N5090 SHT 6 REV. REFER TO SRM N00230 FOR WORK DETAIL REPAIR CLASSIFIED AS MAJOR.