N764AS

Part: STRINGER — CORRODED (BS 540) · corrosion level 2 · airframe 72,030 hrs · 47,290 cycles

END FITTING AT BS 540 STRINGER 22R IS CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE END FITTING IAW SRM 51-40-02-0G.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 72,030 hrs · 47,290 cycles

L1 DOOR LOWER HINGE CUT OUT SHOWS CRACK INDICATION IN HOLE. GROUNDED, YES. CRACKS FOUND AT UPPER AND LOWER HINGE CUT OUTS REPAIR OF BOTH CRACKS TO BE REPAIRED ON MIG5 OK33947 W/O 1013489 2000/0110.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 72,030 hrs · 47,290 cycles

L1 DOOR UPPER HINGE CUT OUT SHOWS CRACK INDICATION IN HOLE MARKED. GROUNDED, YES. REPAIRED CRACKS AT UPPER AND LOWER HINGE CUT OUTS IAW EA 400-53EA-17876. THIS IS A CATEGORY B REPAIR WITH STAGE 1 APPROVAL 2ND AND 3RD STAGE DT DATA TO DEMONSTRATE COMPLIANCE WITH 14 CFR PT 25.571 SHALL BE SUBMITTED NO LATER THAN 12 MOS. AFTER AIRPLANE IS RETURNED TO SERVICE.

Part: SKIN — CRACKED (BS 330) · airframe 72,030 hrs · 47,290 cycles

FUSELAGE SKIN CRACKED AT THE R1 DOOR LOWER AFT CORNER. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-10-01-2R 2 REP 2.

Part: SKIN — CRACKED (BS 727E) · airframe 72,030 hrs · 47,290 cycles

CRACK IN FUSELAGE SKIN BS 727E +3 BELOW STRINGER 22L. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-00-01 REP. 31.

Part: FRAME — CRACKED (BS 360) · airframe 72,030 hrs · 47,290 cycles

FUSELAGE FRAME AT BS 360 INSULATION STAND OFF HOLE BETWEEN STRINGERS 19 AND 20R SHOWS CRACK INDICATION IAW T/C AD20152308-400-53-11. ACFT GROUNDED. REPAIRED THE DAMAGE IAW EA 400-53EA-17811.

Part: LENS — BROKEN (CABIN) · airframe 71,586 hrs · 46,936 cycles

R2 DOOR EXIT LIGHT BROKEN. ACFT GROUNDED. REGLUED COVER-REINSTALLED COVER REF AMM 33-51-11.

Part: STRINGER — CORRODED (BS 1129-1156) · corrosion level 2 · airframe 69,511 hrs · 45,218 cycles

APU TORQUE BOX CENTER STRINGER, AFT OF MAIN CUTOUT HAS A CORROSION. ACFT GROUNDED. APU TORQUE BOX CENTER STRINGER AFT OF MAIN CUTOUT, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1 AND R & R IAW SRM 51-40-02.

Part: SKIN — CRACKED (BS 974-967) · airframe 69,511 hrs · 45,218 cycles

AFT ENTRY DOOR CUTOUT FWD LWR CORNER IS CRACKED. ACFT GROUNDED. REPAIRED SKIN ASSY IAW SRM 53-00-01-2R-32. THIS IS A CAT B REPAIR WITH A INTERVAL OF 24,000 CYCLES AND A THRESHOLD OF 66000 CYCLES AT TIME OF REPAIR 45,218.

Part: ARM — OUT OF RIG (L1 DOOR) · airframe 67,862 hrs · 43,880 cycles

FORWARD L-1 DOOR VERY DIFFICULT TO CLOSE FROM INSIDE. NOT CLOSING PROPERLY NEED TO PUSH UP ON HIGH RT CORNER SAME TIME AS FINAL LATCH. ACFT GROUNDED. INSP FWD L1 DOOR FOUND DOOR TO BE OUT OF RIG AT GUIDE ARMS AND VARIOUS PORTS AROUND THE DOOR. RECOMMEND DOOR RE-RIG REF AMM 52-11-00. UPPER AFT CORNER OF DOOR STILL BINDING. ACCOMPLISHED GUIDE ARM ADJUSTMENT REF MM 52-11-00-825. ACCOMPLISHED DOOR TEST FORCE CHECK REF MM 52-11-00-755. OPS AND RIG GOOD REF MM 52-11-00.

Part: SKIN — CRACKED (BS 747-767) · airframe 67,789 hrs · 43,819 cycles

FUSELAGE SKIN IS CRACKED S25L AT LAP JOINT BETWEEN BS 747 AND 767. ACFT GROUNDED. REPAIRED FUSELAGE SKIN IAW SRM 53-00-01-2R-31, REPAIR 31, FIG 201 DETAIL XV.

Part: SKIN — CRACKED (BS 947-967) · airframe 67,511 hrs · 43,587 cycles

FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT FS 947.5+ 10 AT STRINGER 17R. CRACK ORIGINATES UNDER DOOR THRESHOLD AND TERMINATES AT FASTENER JUST FWD OF THRESHOLD PLATE. VERIFIED CRACK WITH HFEC PER BOEING NDT MANUAL PART 6, 51-00-00 PROCEDURE 23. ACFT GROUNDED. REPAIRED R2 DOOR CUTOUT AT 947.5+10 AT STR 17R IAW SRM 53-00-01-2R-32, REPAIR 32, THIS IS A CATEGORY B REPAIR THAT REQUIRES INSPECTION AT 24,000 FLIGHT CYCLE INTERVALS WITH A THRESHOLD OF 66,000 FLIGHT CYCLES CURRENT FLIGHT CYCLES IS 30,507 AT TIME OF REPAIR COMPLETED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 66,796 hrs · 42,953 cycles

EMERGENCY LIGHTS AT ROWS 20ABC AND 23ABC INOPERATIVE. ACFT GROUNDED. R & R BATTERY PACK AT BS 747, IAW MM 33-51-51-962-015. OPS CHECKED GOOD.

Part: CUSP WEB — CORRODED (BS 727B-727C) · corrosion level 2 · airframe 66,780 hrs · 42,944 cycles

CUSP WEB BS 727B-727C WAS FOUND TO HAVE CORROSION. ACFT GROUNDED. BLENDED AREA, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW SRM 53-60-13-1A-1, FIG 101-51-40-02-0G-0.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 66,780 hrs · 42,944 cycles

PANEL NR 5827 LANDING ON THE NR 2 ENGINE PYLON HAS A CRACK PROTRUDING FROM THE AFT OTBD CORNER. ACFT GROUNDED. REPAIRED NR 2 PYLON STRUT SKIN IAW EA 400, 54 EA 13042.

Part: WINDOW FRAME — CORRODED (BS 470) · corrosion level 2 · airframe 66,780 hrs · 42,944 cycles

RIGHT WINDOW CASTING DOUBLER AT BS 470 HAS CORROSION. ACFT GROUNDED. REMOVED AND DRILLED AND INSTALLED NEW WINDOW CASTING IAW SRM 5140-02-0G-0.

Part: STRINGER — CORRODED (BS 470) · corrosion level 2 · airframe 66,780 hrs · 42,944 cycles

STRINGER 13R AT BS 470 HAS CORROSION. ACFT GROUNDED. REPAIRED STRINGER 13R, STA 470 IAW EA 400, 53 EA, 13052 REV NEW ISSUED 17JUL14 IAW ASSOCIATED FAA FORM 8100-9 THIS IS A DAMAGE TOLERANCE, CAT B REPAIR FIRST AND SECOND STAGE APPROVAL HAS BEEN PROVIDED THIRD STAGE APPROVAL IS REQUIRED BEFORE ACFT REACHES 75000 TOTAL FLT CYCLES AT TASK NOTIFICATION SENT W 1", O .060", R .049", L 3", D .011.

Part: WINDOW FRAME — CORRODED (BS 450) · corrosion level 2 · airframe 66,780 hrs · 42,944 cycles

RIGHT WINDOW CASTING DOUBLER AT BS 450 HAS CORRODED. ACFT GROUNDED. R & R WITH A NEW RT WINDOW CASTING AT STA 450 IAW SRM 51-40-02-0G-0, W 1", O .120, R .109, L 2", D .011.

Part: STRINGER — CORRODED (BS 490) · corrosion level 2 · airframe 66,780 hrs · 42,944 cycles

STRINGER 13R AT BS 490 HAS CORROSION. ACFT GROUNDED. REPAIRED STRINGER IAW EA 400, 53 EA, 13052 REV NEW.

Part: STRINGER — CORRODED (BS 410) · corrosion level 2 · airframe 66,780 hrs · 42,944 cycles

STRINGER 13R AT BS 410 HAS CORROSION. ACFT GROUNDED. REPAIRED STRINGER IAW EA 400 53EA, 13052 REV NEW.

Part: STRINGER CLIP — CRACKED (BS 663) · airframe 66,780 hrs · 42,944 cycles

FRAME BS 663.75, STRINGER 10L HAS A CRACKED STRINGER CLIP, CRACKED AT INBD FASTENER. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G-0 AND 51-40-5-0G-0.

Part: ATTACH ANGLE — CORRODED (BS 550) · corrosion level 2 · airframe 66,780 hrs · 42,944 cycles

RT STR 14R ATTACHED ANGLE AT STA 550 HAS CORROSION ON THE AFT EDGE. ACFT GROUNDED. MATERIAL LOSS 100 PERCENT DUE TO EXFOLIATION. R & R ATTACH ANGLE IAW SRM 51-40-02-0G-0, W .60, O .125, R .00, L .80, D .125.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 66,780 hrs · 42,944 cycles

RT WING INBD FLAP EXTERIOR MID FLAP INBD END HAS CHAFING DAMAGES. ACFT GROUNDED. REPAIRED RT WING INBD MID FLAP IAW SRM 57-53-01-2R-3 REPAIR 3.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 65,839 hrs · 42,130 cycles

RT HORIZONTAL STABILIZER BOTTOM SKIN CRACKED ON REAR SPAR 5 FT FROM INBD ROOT. ACFT GROUNDED. REPAIRED SKIN IAW SRM 55-10-01-2R-13.

Part: STRINGER — CORRODED (APU BAY) · corrosion level 2 · airframe 64,887 hrs · 42,318 cycles

APU INLET CUTOUT IN APU COMPARTMENT UPPER STRINGER IS CORRODED. ACFT GROUNDED. R & R UPPER STRINGER IAW SRM 51-40-02-0G-0.

Part: GUIDE — OUT OF ADJUST (R2 DOOR) · airframe 65,551 hrs · 41,895 cycles

F/A REPORTED R2 DOOR HARD TO OPEN & CLOSE. ACFT GROUNDED. ADJUSTED TOP HINGE GUIDE ARM DOOR. OPS AND CLOSES NORMAL IAW MM 52-13-00. OPS CHECKED GOOD IAW MM 52-13-00-705-003.

Part: ENGINE — ODOR (NR 1) · airframe 65,300 hrs · 41,688 cycles

F/A REPORTED SMOKE IN CABIN DURING CLIMB THROUGH 12,000 FT, ACCOMPLISHED QRH ITEMS, SMOKE SUBSIDED. RETURNED FOR NORMAL LANDING. ACFT GROUNDED. DIVERSION TIME 7 MINUTES. COMPLETED CONDITIONAL INSP, REF MM 05-51-56-200-801 & 21-00-01-101. NO LEAKING FLUIDS OR ELECTRICAL SMELLS OR BURNS NOTED. OPERATED BOTH PACKS AND BOTH RECIRC FANS WITH APU BLEED AIR. NO SMOKE OR ODORS NOTED IN CABIN OR COCKPIT. RESEARCHED ACFT HISTORY & NOTED NR 2 ENGINE FAN LUBE PERFORMED. COMPLETED ENG RUN & SLIGHT ODOR ON NR 2 ENGINE PERSISTED. DID HIGH POWER RUN OF BOTH ENGS AND FUMES WENT AWAY. REPLACED BOTH HEPA FILTERS LT & RT REF MM 21-21-23. OPS NORMAL.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 65,027 hrs · 41,461 cycles

L2 EMERGENCY SLIDE LIGHT INOPERATIVE. ACFT GROUNDED. R & R CHARGER REF MM 33-51-51.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,968 hrs · 41,415 cycles

ROW 27, AISLE EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED EMERGENCY BATTERY CHARGING UNIT IAW 33-50-00. OPS TEST NORMAL AT THIS TIME.

Part: HINGE — LOOSE (L1 DOOR) · airframe 64,565 hrs · 41,083 cycles

L1 DOOR EXTREMELY DIFFICULT TO LATCH, CLOSED WITH DOOR HANDLE, ACFT GROUNDED. L1 DOOR UPPER MOUNT HINGE LOWER PLATE ON AIR FRAME SIDE HAS LOOSE MOUNT BOLTS. TIGHTENED AS REQUIRED. LUBED HINGE AREAS. DOOR OPERATES NORMAL.

Part: DOOR — LACK OF LUBE (L1) · airframe 64,413 hrs · 40,959 cycles

F/A REPORTED L1 DOOR DIFFICULT TO LOCK, HANDLE HITS SOMETHING INTERMITTENTLY JUST PRIOR TO FULL DOWN. ACFT GROUNDED. LUBRICATED ALL EXTERIOR LUB FITTINGS ON L-1 DOOR. DOOR OPS NORMAL REF 12-25-21.

Part: ROLLER — LACK OF LUBE (L2 DOOR) · airframe 64,278 hrs · 40,838 cycles

L2 DOOR IS STICKY. ACFT GROUNDED. LUBE L2 DOOR ROLLERS REF MM 12-25-11 AND OPS CK AFT L2 DOOR CK GOOD REF MM 52-13-00.

Part: HINGE — LACK OF LUBE (L2 DOOR) · airframe 63,641 hrs · 40,266 cycles

F/A REPORTS AFT ENTRY DOOR IS HARD TO OPEN. ACFT GROUNDED. LUBED ENTRY DOOR HINGES. OPS NORMAL.

Part: DOOR — LACK OF LUBE (R2) · airframe 63,641 hrs · 40,266 cycles

R2 DOOR DIFFICULT TO OPEN & CLOSE. ACFT GROUNDED. C/W GVI OF R2 DOOR , CLEANED AND LUBED DOOR ASSY. PERFORMED AMM TASK 52-41-00 PROC C. HANDLE TORQUE WITHIN LIMITS.

Part: FRAME — CRACKED (BS 500B) · airframe 63,614 hrs · 40,242 cycles

FRAME AT BS 500B, LT SIDE FRAME AT BS 500B, LT SIDE HAS A CRACK AT THE FASTENER DIRECTLY ABOVE AND INBD OF THE 1 DIA WIRE PENETRATION HOLE APPROX .1250" LONG EXTENDING INBD BELOW STRINGER 20L, REPAIRED FRAME AT STA 500B IAW ASA EA 400 53, EA 10317.

Part: RIB — CHAFED (LT WING) · airframe 63,614 hrs · 40,242 cycles

LEFT OTBD FIXED WING T/E RIB AT WS 415 IS CHAFED. ACFT GROUNDED. R & R OTBD LT FIXED WING T/E FITTING IAW SRM 51 40 02 0G 0 AND AMM 20 50 11 912 002, FIG 203.

Part: FRAME — DENTED · airframe 63,614 hrs · 40,242 cycles

AFT CARGO FRAME AT BS 727C DENTED ABOVE 23R. ACFT GROUNDED. REPAIRED FRAME IAW EA 400 53, EA 10243.

Part: FRAME — DENTED (BS 500E) · airframe 63,614 hrs · 40,242 cycles

FWD CARGO BS 500E S24L FRAME DENTED. ACFT GROUNDED. REPAIRED FWD CARGO FRAME IAW EA 400-53EA-10241 REV NEW.

Part: BAFFLE — BENT (BS 400-420) · airframe 63,614 hrs · 40,242 cycles

LEFT BAFFLE BETWEEN BS 400 AND 420 IS BENT. ACFT GROUNDED. R & R BAFFLE IAW SRM 51-40-02-0G-0.

Part: BAFFLE — CRACKED (BS 460-480) · airframe 63,614 hrs · 40,242 cycles

FWD CARGO BAY LEFT BAFFLE BETWEEN BS 460 - 480 IS CRACKED. ACFT GROUNDED. R & R BAFFLE IAW SRM 51-40-02-0G-0.

Part: FAILSAFE — CORRODED (BS 500G) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

FWD CARGO BS 500G FAILSAFE CORRODED AT S28R. ACFT GROUNDED. R & R FAILSAFE IAW SRM 51-40-02-0.

Part: SEAT TRACK — GOUGED (BS 727B-927) · airframe 63,614 hrs · 40,242 cycles

SEAT TRACK AT LBL 45.5 FROM BS 727B - 927 HAS NUMEROUS NICKS AND GOUGES. R & R SEAT TRACK IAW SRM 51 40 02 0G 0.

Part: SEAT TRACK — GOUGED (BS 727B-927) · airframe 63,614 hrs · 40,242 cycles

SEAT TRACK AT LBL 24.75 FROM BS 727B TO 927 HAS NUMEROUS NICKS AND GOUGES. R & R SEAT TRACK IAW SRM 51-40-02-0G-D AND EA 400-53EA-04953 REV.

Part: SKIN — DENTED (BS 727G-747) · airframe 63,614 hrs · 40,242 cycles

PROTRUSION IN SKIN AT BETWEEN BS 727G AND 747, APPROX 2 ABOVE STR 25R. ACFT GROUNDED. REPAIRED DENT IAW EA 400 53EA 10272, REV NEW DATED 02MAY13.

Part: BAFFLE — CORRODED (BS 747-767) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

UPON WORKING AFT CARGO RT TRANSITION PANEL, FOUND CORRODED ON BAFFLE STA 747 - 767 AT S26R. FABRICATED NEW BAFFLE AND INSTALLED IAW SRM 51-40-02, STEP 4-B A-C.

Part: BAFFLE — CORRODED (BS 747-767) · corrosion level 3 · airframe 63,614 hrs · 40,242 cycles

ON WORKING AFT CARGO RT TRANSITION PANEL, FOUND CORRODED ON BAFFLE BS 747 TO 767 AT S26R. FABRICATED NEW BAFFLE AND INSTALLED IAW SRM 51-40-02, STEP 4-B A-C, ACFT GROUNDED.

Part: FLOORBOARD — GOUGED (AFT CARGO) · airframe 63,614 hrs · 40,242 cycles

AFT CARGO FLOORBOARD SEVERAL DEEP GOUGES. FABRICATED NEW FLOORBOARD IAW SRM 51-40-05.

Part: SHEAR TIE — CORRODED (BS 807) · airframe 63,614 hrs · 40,242 cycles

AFT CARGO BS 807 FRAME AT SKIN CORRODED NEXT TO STRINGER 27L. REMOVED CORROSION BY BLENDING, FOUND TO BE OUT OF LIMITS DUE TO EXISTING REPAIR. REPAIRED SHEAR TIE IAW SRM 53 00 07, FIG 101 AND 53 05 07 REPAIR 3, CATEGORY B REPAIR, CONTACT ENGINEERING FOR METHODS AND INTERVALS PRIOR TO THE THRESHOLD W 1", O .045, R 0 L 6", D 0.

Part: SHEAR TIE — CORRODED (BS 807) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CARGO BAY SHEAR TIE CORRODED BS 807, STR 27. REMOVED CORRODSION, FOUND TO BE OUT OF LIMITS. REPAIRED SHEAR TIE IAW SRM 53-00-07, FIG 101 AND 53-00-07,

Part: SHEAR TIE — CORRODED (BS 767) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CARGO BAY AT BS 767 O/B OF S25L ON FRAME AT SKIN CORROSION REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED SHEAR TIE IAW SRM 53-00-07, FIG 101 AND 53-00-07.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RIGHT INBD FOREFLAP CHAFED ON CENTER UPPER SIDE. REPAIRED RT INBD FOREFLAP IAW SRM 51 70 10 2R 4.

Part: MOUNT — GOUGED (ANTENNA) · airframe 63,614 hrs · 40,242 cycles

FWD CARGO COMP ANTENNA MOUNT CRACKED BETWEEN BS 500 - 500A AND S28R - S28L. R & R ANTENNA MOUNT IAW SRM 51 40 02 0G 0.

Part: SEAT TRACK — CORRODED (BS 520-540) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

UPON DISPLACEMENT OF LINK FROM BS 520 TO 540 LBL 45 FOR SEAT TRACK REPAIR FOUND FWD ATTACH HOLE EXFOLIATED. R & R PIVOT LINK IAW AMM 20-50-11-912-002, FIG 203.

Part: SKIN — CHAFED (BS 1016) · airframe 63,614 hrs · 40,242 cycles

WHILE WORKING RT SKATE ANGLE FOUND CHAFING ON SKIN AT BS 1016, JUST INBD OF SKATE ANGLE. ACFT GROUNDED. CHAFING DAMAGE FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-01-1A, FIG 101. REPAIRED DAMAGE IAW EA 400-53 EA 10277.

Part: CUSP WEB — CORRODED (BS 727G-747) · airframe 63,614 hrs · 40,242 cycles

AFT CABIN CUSP WEB BETWEEN STA 727G AND 747 STR 17R IS CORRODED. ACFT GROUNDED. R & R CUSP WEB IAW SRM 51 40 02.

Part: BAFFLE — CRACKED (BS 500E) · airframe 63,614 hrs · 40,242 cycles

FWD CARGO BAY S26L BAFFLE CRACKED AT BS 500E. ACFT GROUNDED. R & R BAFFLE IAW SRM 51-40-02.

Part: BAFFLE — CRACKED (BS 500E) · airframe 63,611 hrs · 40,241 cycles

FWD CARGO BAY S26R BAFFLE CRACKED AT BS 500E. ACFT GROUNDED. R & R BAFFLE IAW SRM 51-40-02.

Part: FLOORBEAM — DAMAGED (BS 807) · airframe 63,614 hrs · 40,242 cycles

ON REMOVAL OF SEAT TRACK, FOUND DOUBLE DRILLED HOLE IN FLOORBEAM, FS 807, LBL 45.5. ACFT GROUNDED. REPAIRED 807 FLOORBEAM IAW ASA EA 400 53EA 10257, REV NEW DATED 30APR13.

Part: BRACKET — CRACKED (COCKPIT) · airframe 63,614 hrs · 40,242 cycles

NOSE GEAR VIEWING WINDOW SUPPORT BRACKET IN FLT DECK CRACKED. ACFT GROUNDED. R & R SUPPORT BRACKET IAW SRM 51-40-02-06-0. STEP 4B.

Part: SKIN — DENTED (NR 3 SPOILER) · airframe 63,614 hrs · 40,242 cycles

LT WING T/E NR 3 SPOILER UPPER SURFACE HAS PROTRUDING DENT MID SPAN APPROX 6 FROM L/E. ACFT GROUNDED. REPAIRED NR 3 SPOILER IAW SRM 51 70 10 2R 4, REPAIR 4.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RT INBD FLAP WEDGE LWR INBD SIDE OF WEDGE HAS DENT ON PREVIOUS REPAIR. REPAIRED RT INBD FLAP WEDGE LWR INBD SIDE OF WEDGE IAW SRM 51-70-10 2R 4, REPAIR 4.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RT INBD FLAP WEDGE OTBD LWR T/E CHAFED. REPAIRED RT INBD FLAP WEDGE OTBD LOWER T/E IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RIGHT INBD FLAP WEDGE LWR INBD SIDE OF WEDGE HAS CHAFE. REPAIRED RT INBD FLAP WEDGE LOWER INBD SIDE IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RIGHT INBD FLAP WEDGE LWR SIDE CENTER OF WEDGE HAS DENT ON PREVIOUS REPAIR. REPAIRED RT INBD FLAP WEDGE LWR SIDE CENTER OF WEDGE IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 47,373 hrs · 26,351 cycles

RT INBD FLAP WEDGE LWR SIDE HAS DENT NEXT PREVIOUS REPAIR. REPAIRED RT INBD FLAP WEDGE LOWER SIDE IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

WEB ON TOP OTBD FWD CORNER OF PRESSURE DECK IS CORRODED STA 663 RBL 60. REMOVED SHEAR TIE, FABRICATED TREATED AND APPLIED PRIMER AND TOP COAT IAW AMM 51-21-21-307-014, BAC 65-45409, SRM 51-40-02. INSTALLED NEW SHEAR TIE.

Part: RIB — CRACKED (RT WING) · airframe 63,614 hrs · 40,242 cycles

DURING INSPECTION, FOUND LOWER RIB ATTACH FITTING AT RT WING RIB NR 4 WBL 135.5 BETWEEN STRINGERS 4 AND 4 TO BE CRACKED AT AFT RADIUS. ACFT GROUNDED. REPAIRED CRACKED LOWER RIB CHORD IAW EA 400 57, EA 10305.

Part: BEAM — CORRODED (BS 727A-727B) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

UPON REMOVAL OF SEAT TRACK, FOUND LONGITUDINAL BEAM LBL 45.5 FS 727A CORRODED. ACFT GROUNDED. REPAIRED AREA IAW EA AD2008-0506-400-57-118, REV NEW.

Part: FLOOR SUPPORT — CRACKED (BS 668) · airframe 63,614 hrs · 40,242 cycles

LONGITUDINAL FLOOR SUPPORT 24R CRACKED AT CENTER FASTENER ACCESS RADIUS FS 668.0. ACFT GROUNDED. REPAIRED LONGITUDINAL FLOOR SUPPORT IAW EA AD20060506-400-57-117 REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 560-727A) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

LONGITUDINAL FLOORBEAM, LBL 45.5 CORRODED AT FS 670.0 BELOW FLOOR LEVEL. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE ACCEPTABLE FOR CONTINUE SERVICE IAW EA 400-57EA-10206, REV NEW.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RT WING OTBD MIDFLAP T/E WEDGE INNER SKIN IS CREASED IN THREE AREAS AT OTBD END. REPAIRED RT WING OTBD MIDFLAP T/E WEDGE INNER SKIN AT OTBD END IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

LT WING INBD FOREFLAP UPPER SURFACE HAS FOUR LONG DENTS AT A PREVIOUS REPAIRED. REPAIRED LT WING INBD FOREFLAP UPPER SURFACE IAW SRM 51-70-10-2R 4, REPAIR 4.

Part: CHANNEL — CRACKED (BS 500-500A) · airframe 63,614 hrs · 40,242 cycles

FWD CARGO COMP ANTENNA MOUNT CRACKED BETWEEN BS 500 - 500A AND S28R - S28L. R & R ANTENNA MOUNT IAW SRM 51 40 02 0G 0.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 46,138 hrs · 20,842 cycles

LEFT WING OTBD FORE FLAP, OTBD END LOWER SURFACE HAS A GROUP ON DENTS. REPAIRED LT OTBD FOREFLAP OTBD LOWER END IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RT WING OTBD MIDFLAP T/E WEDGE INNER SKIN IS CREASED AT CENTER OF FLAP REPAIRED RT WING OTBD MIDFLAP T/E WEDGE INNER SKIN AT CENTER OF FLAP IAW SRM 51 70 10 2R 4, REPAIR 4.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

LEFT WING OTBD FORE FLAP UPPER SURFACE IS DENTED ON OTBD END. REPAIRED IAW SRM 51-70-10, REPAIR 4.

Part: CARGO TRACK — DAMAGED (BS 500B) · airframe 63,614 hrs · 40,242 cycles

FWD CARGO BAY, CARGO TRACK RBL 8 HAS DILL HOLES AT BS 500B. REPAIRED CARGO TRACK IAW SRM 53-00-53, REPAIR 1.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

LEFT WING OTBD AFT FLAP INBD END LOWER SURFACE HAS MULTIPLE DENTS. REPAIRED LT WING OTBD AFT FLAP INBD LOWER END IAW SRM 51-70-10, REP 4.

Part: CHANNEL — CORRODED (BS 420-440) · airframe 63,614 hrs · 40,242 cycles

FWD CARGO BAY LT ZEE CHANNEL CORRODED BETWEEN BS 420-440. ACFT GROUNDED. R & R LT ZEE CHANNEL IAW SRM 51-40-02-0G-0 .

Part: STRINGER SPLICE — CORRODED (BS 500A-500B) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

FWD CARGO BAY S19L SPLICE CORRODED BETWEEN BS 500A - 500B. ACFT GROUNDED. REMOVED AND INSTALLED NEW STRINGER SPLICE IAW SRM 53-00-53, FIG 201.

Part: CREASE BEAM — CORRODED (BS 500B-528) · airframe 63,614 hrs · 40,242 cycles

RT CREASE BEAM INNER CHORD IS CORRODED FROM SPLICE AT STA 500B TO SPLICE AT STA 528 ALONG ENTIRE LENGTH. REPAIRED RT CREASE BEAM INNER CHORD IAW SRM 51-70-12-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 727D-767) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CARGO COMPARTMENT BS 727D -767 S24R FLOOR SUPPORT CORRODED. REMOVED, FABRICATED NEW AND INSTALLED AFT CARGO RT FLOOR SUPPORT FROM STA 727D -767 IAW SRM 51 40 02, STEP B1 A-C W 4.0, O .040, R .030, L 12.00, D .010

Part: FLOORBEAM — CORRODED (BS 294) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

BS 294, FLOORBEAM HAS CORROSION ON TOP SURFACE AT LBL 10. BLENDED OUT CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51 FIG 101 DETAIL IX. R & R FLOORBEAM UPPER TEE IAW SRM 51-40-05, AND SRM 51-40-02 STEPS 4 AND 7. APPLIED PROTECTIVE FINISHES TO NEW TEE IAW BSOPM 20-43-03 AND SOPM 20-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 867-887) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CARGO PIT BETWEEN BS 867 AND 887 ABOVE 27R FLOOR SUPPORT HAS CORROSION ACFT GROUNDED. BLENDED CORROSION CHECKED LIMITS FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGED FABRICATED NEW SECTION AND INSTALLED IAW SRM 53-60-53, FIG 101, 51-40-02 AND 53-00-53.

Part: SILL — CORRODED (BS 320-328) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

L1 MOPSILL HAS MULTIPLE AREAS OF CORROSION. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-10-15. R & R MOPSILL IAW SRM 51-40-02 AND AMM 20-50-11-912.

Part: FLOOR SUPPORT — CORRODED (BS 930-948) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CARGO BAY AT BS 947.5 ABOVE 27R FLOOR SUPPORT HAS CORROSION. BLENDED CORROSION CHECK LIMITS FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE. FABRICATED NEW SECTION AND INSTALLED IAW SRM 53-60-53, FIG 101 51-10-02, 53-00-53.

Part: CUSP WEB — CORRODED (BS 767-787) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CABIN CUSP WEB BETWEEN BS 767 AND 787 17R HAS CORROSION. R & R CUSP WEB IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 727F-817) · airframe 63,614 hrs · 40,242 cycles

AFT CARGO COMPT STA BS 747 BS 737, S25L PREVIOUS REPAIR CORRODED ON FLOOR SUPPORT. ACFT GROUNDED. INSTALLED NEW CHANNEL AND REPAIR ANGLES IAW SRM 53 00 53 FIG 201 W 1.00 O .063 R .059 L 9.00 D .004.

Part: FLOOR SUPPORT — CORRODED (BS 820-740) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CARGO COMPT STA BS 827 S26R FLOOR SUPPORT CORRODED. BLENDED CORRODED CHECKED LIMITS FOUND TO BE OUT OF LIMITS CUT OUT DAMAGED FABRICATED NEW SECTION AND INSTALLED IAW SRM 53-60-53 FIG 101 51-10-02 , 53-00-53.

Part: SHEAR TIE — CORRODED (BS 866-867) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CARGO BAY SHEAR TIE AT BS 867 BETWEEN 26 AND 27L CORRODED. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REPAIRED SHEAR TIE IAW SRM 53-00-07, FIG 101 AND 53-00-07, REPAIR 3 CATEGORY B.

Part: CUSP WEB — CORRODED (BS 727D-727E) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CABIN CUSP WEB BETWEEN STA 727D AND STA 727E 17L HAS CORROSION. ACFT GROUNDED REMOVED CORRODED FOUND TO BE OUT OF LIMITS IAW SRM 53 60 13. R & R WEB IAW SRM 51-40-02 W .75, O .032, R .028, L 1.25, D .004.

Part: CUSP WEB — CORRODED (BS 727B-727C) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CABIN CUSP WEB BETWEEN BS 727B AND 727C S17L HAS CORROSION. BLENDED CORROSION AREA BLENDED AREAS DETERMING TO BE OUT OF LIMITS IAW SRM 53-60-13, FIG 101, DET V. R & R SECTION OF WEB IAW SRM 51-40-02, STEP 4 AND 7.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

TEE FITTING AT BS 986.5 CORRODED AT SEVERAL LOCATIONS FROM LBL 45 TO RBL 44. ACFT GROUNDED. BLENDED CORROSION IAW SRM 51-40-02. REPAIRED DAMAGED TO TEE FITTING IAW EA 15063 AND EA 400-53EA-10174, REV NEW.

Part: FLOOR SUPPORT — CORRODED (BS 907-927) · airframe 63,614 hrs · 40,242 cycles

AFT CARGO BAY BETWEEN BS 907 AND 927, ABOVE S27L, FLOOR SUPPORT HAS CORROSION. BLENDED CORROSION IAW SRM 51 10 02, FOUND TO BE OUT OF LIMITS IAW SRM 53 60 53. R & R FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 727D-767) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CARGO COMPARTMENT STA BS 727D - 767 S24R FLOOR SUPPORT CORRODED. REMOVED, FABRICATED NEW AND INSTALLED AFT CARGO RT FLOOR SUPPORT FROM STA 727D - 767 IAW SRM 51 40 02, STEP B1 A-C W 4.0, O .040, R .030, L 12.00, D .010.

Part: FRAME — CORRODED (BS 990) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

R2 GALLEY SERVICE DOOR STA 986, FRAME AT TOPSIDE OF FLOOR HAS OPEN HOLE ON BACKSIDE OF FRAME AND FRAME HAS CORRODED. ACFT GROUNDED. BLENDED CORRODED IAW SRM 51-10-02, MAT REMAINING IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-15. R & R DAMAGED LWR FRAME SEGMENT IAW EA 15077 AND EA 453EA 10214, DATED 23APR13, REV NEW.

Part: STRINGER CLIP — GOUGED (BS 480) · airframe 63,614 hrs · 40,242 cycles

FWD CARGO BS 480, STR 22L, STRINGER CLIP GOUGED R & R STRINGER CLIP IAW SRM 51 40 02 0G 0.

Part: DOOR FRAME — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

R2 DOOR BS 958 SURROUND FRAME LOWER EDGE AT TOPSIDE OF FLOOR HAS A DEEP GOUGE AND CORRODED. REPAIRED IAW EA 400-53EA-10168.

Part: FRAME — GOUGED (BS 400) · airframe 63,614 hrs · 40,242 cycles

FWD CARGO BS 400, FRAME GOUGED AT S25R. R & R SPLICE IAW SRM 51 40 02 0G 0, ITEM 4, PAGE 2.

Part: DOOR FRAME — CRACKED (BS 492) · airframe 63,614 hrs · 40,242 cycles

FWD CARGO DOORWAY AFT FRAME CRACKED. ACFT GROUNDED. R & R FWD CARGO DOORWAY AFT FRAME IAW SRM 51 40 02 0G 0.

Part: DOOR FRAME — CRACKED (BS 940) · airframe 63,614 hrs · 40,242 cycles

FWD CARGO DOORWAY FWD FRAME CRACKED. ACFT GROUNDED. R & R FWD FWD DOOR FRAME IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 772) · airframe 63,614 hrs · 40,242 cycles

AFT CARGO BS 772 CORRODED FLOOR SUPPORT LBL15. REPAIRED FLOOR SUPPORT IAW EA 400-53EA-10126.

Part: SUPPORT — CORRODED (BS 727-847) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CARGO BAY FROM BS 727 TO STA 847 ABOVE 26L TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-60- 53. R & R TRANSITION PANEL IAW SRM 51-40-02, W 2.75, O .040, R .015, L 65, D .025.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RT OTBD AFT FLAP CHAFED AT NR 8 FAIRING. REPAIRED CHAFE ON RT OTBD AFT FLAP IAW SRM 51-70-10-2R-0, REPAIR 4, PARA 20, PG 48.

Part: SEAT TRACK — GOUGED (BS 727B-927) · airframe 63,614 hrs · 40,242 cycles

SEAT TRACK AT RBL 24.75 FROM STA 727B TO STA 927 HAS NUMEROUS NICKS AND GOUGES. ACFT GROUNDED. R & R SEAT TRACK IAW SRM 53-00-52-2R-4 AND EA 400-53EA-04953, REV NEW.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RT OTBD MID FLAP INBD L/E CHAFED. REMOVED TWO DOUBLERS AND FILLERS IAW SRM 51-40-02. FABRICATED TWO REPAIR DOUBLERS AND ONE FILLER IAW SRM 57-53-01, FIG 201, CAD PLATED DOUBLER NR 2 IAW SRM 57-53-01, FIG 201, PRIMED TWO REPAIR PARTS AND ONE FILLER IAW AMM 51-21-21-307-014. INSTALLED TWO DOUBLERS AND ONE FILLER IAW SRM 57-53-01, FIG 201, EA 15037 AND EA 400-57EA-10134.

Part: SEAT TRACK — GOUGED (BS 540-727) · airframe 63,614 hrs · 40,242 cycles

SEAT TRACK AT RBL 24.75 FROM BS 540 TO 727 HAS NUMEROUS GOUGES. R & R SEAT TRACK IAW AMM 20-50-11-912-002, FIG 203.

Part: FRAME — CRACKED (BS 500B) · airframe 63,614 hrs · 40,242 cycles

FRAME AT BS 500B, RT SIDE HAS A CRACK AT THE 1 DIA WIRE PENETRATION HOLE APPROX .2500 LONG EXTENDING INBD FROM EDGE OF HOLE BELOW STRINGER 20R. REMOVED DAMAGE AND REPAIRED AREA ON FRAME BS 500B, STR 20 RT IAW SRM 53 00 07, REP 13.

Part: SEAT TRACK — GOUGED (BS 480-520) · airframe 63,614 hrs · 40,242 cycles

SEAT TRACK AT LBL 45.5 FROM STA 480 TO STA 520 HAS NUMEROUS NICKS AND GOUGES. ACFT GROUNDED. REPAIRED SEAT TRACK AT LBL 45.5 IAW SRM 53 00 52, REP 2 AND ASA EA 400 53EA 04953, REV NEW DATED 09MAR11.

Part: TRANSITION PANEL — CORRODED (BS 727-767) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CARGO PIT BS 727 - 807 ABOVE 26R TRANSITION PANEL IS CORRODED. REMOVED, FABRICATED NEW AND INSTALLED AFT CARGO BAY RT TRANSITION PANEL FROM BS 727 - 727D IAW SRM 51-40-02, STEP B1.

Part: FLOOR SUPPORT — CORRODED (BS 727) · airframe 63,614 hrs · 40,242 cycles

AFT CARGO BAY, BS 727, CENTER FLOOR SUPPORT NUT PLATE RUSTED AND CORROSION ON SUPPORT. BLENDED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53. R & R CENTER FLOOR SUPPORT IAW SRM 51-40-02.

Part: SEAT TRACK — GOUGED (BS 727-727B) · airframe 63,614 hrs · 40,242 cycles

SEAT TRACK AT LBL 45.5 FROM BS 727 TO 727B HAS NUMEROUS NICKS AND GOUGES. ACFT GROUNDED. R & R SEAT TRACK IAW SRM 51-40-02-0G-0 AND EA 400-53EA-04953, REV NEW.

Part: STRUCTURE — CHAFED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RT OTBD AFT FLAP CHAFED AT NR 8 FAIRING. REPAIRED CHAFE ON RT OTBD AFT FLAP IAW SRM 51-70-10-2R-0, REPAIR 4, PARA 20, PG 48.

Part: SEAT TRACK — GOUGED (BS 540-727) · airframe 63,614 hrs · 40,242 cycles

SEAT TRACK AT RBL 45.5 FROM BS 540 TO 727 HAS NUMEROUS NICKS AND GOUGES. REMOVED AND REPLACED SEAT TRACK IAW AMM 20-50-11-912-002 FIG 203.

Part: SEAT TRACK — GOUGED (BS 540-727) · airframe 63,614 hrs · 40,242 cycles

SEAT TRACK AT LBL 24.75 FROM BS 540 TO 727 HAS NUMEROUS NICKS AND GOUGES. R & R SEAT TRACK IAW SRM 51-40-02 AND EA 400 53EA 04953, REV NEW.

Part: SEAT TRACK — GOUGED (BS 727-727B) · airframe 63,614 hrs · 40,242 cycles

SEAT TRACK AT RBL 45.5. FROM BS 727 TO 727B HAS NUMEROUS NICKS AND GOUGES. R & R TRACK IAW SRM 51 40 02 AND ASA EA 400 53EA 04953 REV NEW .

Part: SEAT TRACK — GOUGED (BS 727B-927) · airframe 63,614 hrs · 40,242 cycles

SEAT TRACK AT RBL 45.5 FROM STA 727B TO STA 927 HAS NUMEROUS NICKS AND GOUGED. R & R SEAT TRACK AT RBL 45 IAW SRM 51 40 02 0G 0.

Part: FLOOR SUPPORT — CORRODED (BS 772) · airframe 63,614 hrs · 40,242 cycles

AFT CARGO PIT JUST AFT OF STA 772 AND BY 27L FLOOR SUPPORT IS CORRODED AROUND SCREW HOLE A250-034, LBL3. REPAIRED AFT CARGO FLOOR SUPPORT IAW ASA 400 53EA 10126.

Part: SEAT TRACK — GOUGED (BS 540-727) · airframe 63,614 hrs · 40,242 cycles

SEAT TRACK AT LBL 45.5 FROM BS 540 TO 727 HAS NUMEROUS NICKS AND GOUGES. R & R SEAT TRACK IAW AMM 20-50-11-912-002, FIG 203.

Part: SEAT TRACK — GOUGED (BS 727-727B) · airframe 63,614 hrs · 40,242 cycles

SEAT TRACK AT LBL 24.75 FROM BS 727 TO 727B HAS NUMEROUS NICKS AND GOUGES. R & R SEAT TRACK IAW 400 51 40 02 AND ASA EA 400 53EA 04953 REV NEW DATED 09MAR11.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RT INBD FOREFLAP CHAFED ON CENTER UPPER SIDE. REPAIRED IAW SRM 51-70-10-2R-4.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

LEFT OTBD FORE FLAP HAS A DENT 16 INCHES INBD OF CENTER SUPPORT AND 4 INCHES FROM T/E A=.10 AND Y=0.025 A/Y=.4 FOUND TO BE OUT OF LIMITS OF SRM 57-53-01, PG 109, FIG 101, DETAIL VIII. BONDED REPAIR IAW SRM 51 70 10, REPAIR 4.

Part: SILL — CORRODED (BS 927-1006) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

L2 DOORWAY MOPSILL IS CORRODED. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15. LOCATED AND DRILLED IAW SRM 51-40-05 INSTALLED NEW L2 SILL IAW SRM 51-40-02.

Part: STRINGER — CORRODED (BS 1088-1138) · airframe 63,614 hrs · 40,242 cycles

APU COMPARTMENT RAM AIR OPENING HAS CORROSION ON THE BOTTOM OF OPENING. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-80-13 AD2. R & R STRINGER IAW SRM 51-40-02,

Part: SILL — CORRODED (BS 958-986) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

R2 DOOR MOPSILL IS CORRODED. ACFT GROUNDED. BLENDED R2 MOPSILL IAW SRM 51-10-02 MATERIAL REMAINING IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-15. R & R MOPSILL IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CHAFED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RT OTBD FOREFLAP ROLLER SUPPORT ANGLE CHAFED OTBD OF OTBD FLAP. R & R IAW SRM 51 40 02.

Part: STRAP — CRACKED (BS 328) · airframe 63,614 hrs · 40,242 cycles

AVIONICS BAY CEILING SUPPORT STRAP CRACKED BS 328, RBL 46. ACFT GROUNDED. R & R CEILING STRAP IAW SRM 51-40-02.

Part: STRAP — CRACKED (BS 309-347) · airframe 63,614 hrs · 40,242 cycles

AVIONICS BAY CEILING SUPPORT STRAP CRACKED BS 328, RBL 32. ACFT GROUNDED. R & R CEILING STRAP IAW SRM 51-40-02.

Part: SKIN — DENTED (NR 1 SPOILER) · airframe 63,614 hrs · 40,242 cycles

NR 1 SPOILER LOWER SURFACE HAS A DENT 4.3 FROM INBD EDGE & 7 FROM FWD EDGE A=0.15 Y=0.020 A/Y=7.5. OUT OF LIMITS IAW SRM 57 70 01, FIG 101, SHEET 7. REPAIRED DENT ON NR 1 SPOILER LOWER SURFACE IAW SRM 51-70-10-2R-0. REPAIR 4 PARA 20, PG 48.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

RT INBD AFT FLAP CHAFED. ACFT GROUNDED. REPAIRED RT INBD AFT FLAP IAW SRM 51-70-10.

Part: SKIN — CHAFED (NR 3 SLAT) · airframe 63,614 hrs · 40,242 cycles

LT WING NR 3 SLAT INBD CORNER AND ABOVE ACTUATOR SURFACE IS CHAFED. REPAIRED LT WING NR 3 SLAT INBD CORNER AND ABOVE ACTUATOR SURFACE IAW SRM 51-70-10, REPAIR 4.

Part: SKIN — CHAFED (NR 2 SLAT) · airframe 63,614 hrs · 40,242 cycles

LT WING NR 2 SLAT INBD L/E INTER SURFACE IS CHAFED. REPAIRED IAW SRM 51-70-10, REPAIR 4, PARA 20, PG 48.

Part: SKIN — CHAFED (NR 5 SPOILER) · airframe 63,614 hrs · 40,242 cycles

NR 5 SPOILER IS CHAFED ON LOWER SURFACE, ACFT GROUNDED. R & R AND REPLACED NR 5 SPOILER IAW AMM 27-62-12-004-001, STEP 2 D.1 THRU 10 AND EA 400-57EA-10219 AND DWG 66-46-452 AND SMM 27-62-12-404 012, STEP 3.E.3 THRU 5.

Part: SKIN — CHAFED (NR 2 SLAT) · airframe 63,614 hrs · 40,242 cycles

LEFT WING NR 2 SLAT OTBD INTER SURFACE OF T/E ON CORNER IS CHAFED. REPAIRED IAW SRM 51-70-10, REPAIR 4, PARA 20, PG 48.

Part: FLOORBOARD — CORRODED (BS 727F) · corrosion level 2 · airframe 63,614 hrs · 60,242 cycles

AFT CARGO NR 2 FLOORBOARD SPLICE IS CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED NEW SPLICE IAW SRM 51-30-01, STEP 8AB.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 63,614 hrs · 40,242 cycles

FWD CARGO NR 1 FLOORBOARD DAMAGED. FABRICATED, LOCATED AND DRILLER NEW FLOORBOARD IAW SRM 51 40 05 06 P, FIG 9, TABLE 5.

Part: FLOORBOARD — GOUGED (AFT CARGO) · airframe 63,614 hrs · 40,242 cycles

AFT CARGO NR 2 FLOORBOARD HAS DEEP GOUGES. FABRICATED, LOCATED AND DRILLED NEW FLOORBOARD IAW SRM 51-40-05.

Part: ACCESS PANEL — DAMAGED (LT WING TE FLAP) · airframe 63,614 hrs · 40,242 cycles

LEFT T/E FLAP PANEL NR 8407 HAS ELONGATED FASTENER HOLE. FABRICATED NEW FLAP ACCESS PANEL IAW SRM 51 70 10, PARA 18, PG 43.

Part: FLOORBOARD — GOUGED (AFT CABIN) · airframe 63,614 hrs · 40,242 cycles

AFT CARGO NR 4 FLOORBOARD HAS EXISTING LINE REPAIR AND SEVERAL DEEP GOUGES. FABRICATED, LOCATED AND DRILLER NEW FLOORBOARD IAW SRM 51-40-05 AND 51-20-01 AND SOPM 20-41-02.

Part: FLOORBEAM — CORRODED (BS 772) · corrosion level 2 · airframe 63,614 hrs · 40,242 cycles

AFT CARGO FLOORBEAM SPLICE TEE HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS FABRICATED NEW SPLICE IAW SRM 51 30 01, STEP 8 A-B.

Part: FLOORBOARD — GOUGED (FWD CARGO) · airframe 63,614 hrs · 40,242 cycles

FWD CARGO FLOORBOARD HAS SEVERAL DEEP GOUGES. FABRICATED NEW FLOORBOARD IAW SRM 51-40-05.

Part: FLOORBOARD — GOUGED (CARGO BAY) · airframe 63,614 hrs · 40,242 cycles

AFT CARGO NR 3 FLOORBOARD HAS SEVERAL DEEP GOUGES. FABRICATED NEW FLOORBOARD IAW SRM 51 40 05.

Part: DOOR — OUT OF ADJUST (R2) · airframe 63,449 hrs · 40,103 cycles

R2 DOOR HARD TO CLOSE. FOUND FWD UPPER LATCH ROD END HITTING LATCH FITTING. DOOR NOT CLOSING PARALLEL, UPPER LATCH ROLLERS NOT ENGAGING AT THE SAME TIME. UPPER FWD LATCH ROLLERS WORN. REPLACED UPPER FWD LATCH ROLLER REF AMM 52-41-00, COMPLETED PARALLEL ADJUSTMENT TO TOP HINGE GUIDE ARM. UPPER LATCH ROD CLEARANCE GOOD. LATCH ROLLER ENGAGEMENT GOOD. REF AMM 52-41-00. FOUND LOWER LATCH ROD END PLAY OUT OF LIMITS, SHIMS MISSING. SHIMMED LOWER LATCH ROD AS REQUIRED REF AMM 52-41-00.

Part: WINDOW — FAILED (COCKPIT) · airframe 61,837 hrs · 38,680 cycles

UNABLE TO CLOSE CAPTAINS SLIDING WINDOW. ACFT GROUNDED. REMOVED WINDOW TO INSPECT FOR DAMAGE. FOUND LOWER AFT ROLLER TO BE ABOUT 1.5 TURNS OUT (LOOSE). TIGHTENED SPECIAL BOLT FOR ROLLER AND TIGHTENED SET SCREW. REF MM 56-12-11 CHECKED ADJUSTMENT OF NR 2 SLIDING WINDOW (LEFT). NO ADJUSTMENT REQUIRED, REF MM 56-12-11. INSTALLED WINDOW, REF MM 56-12-11.

Part: GUIDE ARM — OUT OF ADJUST (L1 DOOR) · airframe 61,554 hrs · 38,431 cycles

F/A REPORTS L1 DOOR HANDLE VERY DIFFICULT TO ENGAGE. ADJUSTED FWD DOOR (L 1) GUIDE ARM REF MM 52-11-00-700-007, PG NR 2, STEP G. OPS NORMAL.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 61,131 hrs · 38,044 cycles

R2 DOOR EXIT SIGN COVER FALLING OFF. SECURED EXIT LIGHT COVER ABOVE DOOR. LOOSE HARDWARE TIGHTENED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,928 hrs · 37,860 cycles

UPPER FASTENER HOLE OF THE LOWEST ISOLATOR (STR 17) AT STA 500D HAS A CRACK INDICATION RT SIDE. REPAIRED FRAME 500D AT STR 17R IAW ASA EA 400 53EA 07570 REV NEW DATED 01 MAR 12.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,928 hrs · 37,860 cycles

CRACK FOUND IN FRAME 500F LEFT PROPAGATING FROM THE 1.04 INCH WIRE PENETRATION HOLE INBOARD APPROX .350 LONG. REPAIRED LT FRAME AT STA 500F WIRE PENETRATION HOLE IAW B737 400 SRM 53 00 07 REPAIR 13.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,928 hrs · 37,860 cycles

MFEC SHOWS CRACK INDICATION APPROX 1' LONG IN CHEM MILLED AREA BELOW STR 23L BS 720D+2" BELOW EMER EXIT LIGHT. REPAIRED DAMAGED AREA IAW B737 400 SRM 53 00 01 REPAIR 31.

Part: FRAME — CRACKED (BS 500F) · airframe 60,928 hrs · 37,860 cycles

CRACK FOUND IN FRAME BS 500F, PROPOGATING FROM THE 1.04' WIRE PENETRATION HOLE APPROX 70' LONG. REPAIRED FRAME IAW SRM 53-00-07, CATEGORY B REPAIR.

Part: TORQUE LINK — BINDING (L2 DOOR) · airframe 60,595 hrs · 37,579 cycles

L2 DOOR BINDS WHILE OPENING AND CLOSING UPPER AND LOWER DOOR ARMS ARE DRAGGING ON CAM PLATES INT MIG2C 277488. FOUND L2 DOOR TORQUE TUBE WORN AND OUT OF LIMITS. RELACED DOOR TORQUE LOWER RADIUS LINK UPPER HINGE LINK AND UPPER CAM PLATE REF 52 13 141 OPS AND PRESSURE CHECKS NORMAL. NO LEAKS NOTED MIG2C 277488.

Part: WINDOW — BINDING (COCKPIT) · airframe 60,436 hrs · 37,444 cycles

CAPTAIN'S SLIDING WINDOW CATCHES AND BINDS OPENING AND CLOSING. REPLACED PILOTS SLIDING WINDOW AS REQ REF AMM 56 12 11, OPS CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,335 hrs · 37,351 cycles

EMERGENCY LIGHTS FAILED OPS CHECK WHILE CHECKING LIGHT FUNCTION. ACCOMPLISHED FUNCTIONAL TEST THE FOLLOWING LIGHTS EXTINGUISHED IN LESS THAN 5 MINUTES. THE REST REMAINED ON FOR 10 MINS. LEFT SIDE OF AIRCRAFT AFT OF L 1 DOOR AFT OF L 2 DOOR. RIGHT SIDE OF AIRCRAFT AFT EMERGENCY EXIT DOOR RIGHT W/B RIGHT R2 DOOR. THE 16 HR RECHARGE STARTED AT 9:30PM 11 11 2011 REF MM33 51 02 735 026. FUNCTIONAL CHECK GOOD PER MM 33 51 02 735 026. THE 16HR RECHARGE STARTED AT 2:00PM 11 12 2011. THE 16HR BATTERY CHARGE COMPLETED ON 6:00AM 11 13 2011.

Part: SNUBBER — MALFUNCTIONED (L1 DOOR) · airframe 58,860 hrs · 36,056 cycles

L1 DOOR SNUBBER DOES NOT SEEM TO ENGAGE DURING DOOR OPENING OR CLOSING. REMOVED AND REPLACED SNUBBER IAW B737 400 AMM 52 11 71. OPS NORMAL.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 58,657 hrs · 35,884 cycles

L2 (AFT ENTRY DOOR) SLIDE POSITION NEEDS ADJUSTMENT. GIRT BAR DRAGS AND BINDS. REPOSITIONED L2 SLIDE PER B737 400 AMM 25 61 35.

Part: SKIN — DENTED (TE FLAP) · airframe 58,334 hrs · 35,608 cycles

LEFT WING OUTBOARD TRAILING EDGE FLAP UPPER SURFACE HAS DENT 11.25 INCH FROM INBOARD EDGE AND 4.75 INCH FROM TRAILING EDGE. DEPTH = 0.055 INCH MAJOR AXIS = 2.07 INCH MINOR AXIS = 1.23 INCH. REPAIRED TRAILING EDGE FLAP UPPER SURFACE IAW B737 400 SRM 51 70 10.

Part: SUPPORT — CHAFED (LT PYLON) · airframe 58,334 hrs · 35,608 cycles

LEFT PYLON OUTBOARD FAN COWL SUPPORT CHORD IS CHAFED NAC STA 129.074 TO 196.70. REPAIRED LEFT PYLON O/B CHORD IAW EA 400 54EA 04609.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

EXTERNAL SKIN CORRODED AT BS 727G+8 AT STR 23R. REMOVED DAMAGE FABRICATED REPAIR PARTS AND INSTALLED IAW ASA EA 400 53EA 04772.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 312 FRAME SPLICE MISSING MATERIAL AT ONE OF FOUR END FASTENERS. REPAIRED FRAMES IAW ASA EA 400 53EA 04649 REV NEW DATED 26 JAN 2011.

Part: STRUCTURE — DELAMINATED (TE FLAP) · airframe 58,334 hrs · 35,608 cycles

RIGHT WING INBOARD FORE FLAP EXISTING REPAIR DELAMINATED. REPAIRED DAMAGED AREA IAW B737 400 SRM 51-70-10 REPAIR 4.

Part: SKIN — DENTED (SKIN) · airframe 58,334 hrs · 35,608 cycles

LEFT INBOARD FORE FLAP LOWER SURFACE HAS MULTIPLE DENTS. REPAIRED DAMAGED AREA IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

WHILE REPLACING STRINGER TIE CLIP AT BS 500A STR 10R FOUND STRINGER CRACKED. REPAIRED CRACKED STRINGER IAW B737 400 SRM 53 00 03 FIG 201 REPAIR 3.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

STRINGER TIE CLIP AT BS 500A STR 10 R CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW B737 400 SRM SRM 51 40 02 PG 2.

Part: SKIN — WORN (MIDFLAP) · airframe 58,334 hrs · 35,608 cycles

RT WING OUTBOARD MID FLAP LOWER SURFACE CHAFE ON EXISTING REPAIR. REMOVED REPAIR DOUBLER AND REPAIRED MID FLAP LOWER SKIN IAW B737 400 SRM 51 70 10 PG 256.

Part: SUPPORT — CHAFED (RT PYLON) · airframe 58,334 hrs · 35,608 cycles

RIGHT PYLON I/B FAN COWL SUPPORT CHORD IS CHAFE NAC STA 166 50 TO 196.70. REPAIRED RIGHT PYLON CHORD IAW EA 400 54EA 04609.

Part: BUTTSTRAP — DAMAGED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

AD 2010 05 13 FUSELAGE SKIN INSPECTION SKIN BUTT STRAP IS SCRIBE LINED 6.25 INCH LONG X 0.0035 INCH DEEP AT BS 727G SCRIBE UPPER END IS 0.824 INCH DISTANCE FROM STR 2L AND LOWER END IS 2.668 INCH DISTANCE FROM STR 5L. REMOVED AND REPLACED BUTT STRAP IAW B737 400 SRM 51 40 02.

Part: SUPPORT — CHAFED (RT PYLON) · airframe 58,334 hrs · 35,608 cycles

RIGHT PYLON OUTBOARD FAN COWL SUPPORT CHORD IS CHAFED NAC STA 166.50 TO 196.70. REPAIRED RT PYLON O/B CHORD IAW EA 400 54EA 04609.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 328 FRAME SPLICE MISSING MATERIAL AT ONE OF FOUR END FASTENERS. REPAIRED FRAMES IAW ASA EA 400 53EA 04649 REV NEW DATED 26 JAN 2011.

Part: SUPPORT — CHAFED (LT PYLON) · airframe 58,334 hrs · 35,608 cycles

LEFT PYLON I/B FAN SUPPORT CHORD IS CHAFED NAC STA 129.074 TO 196.70. REPAIRED LEFT I/B CHORD IAW EA 400 54EA 04609.

Part: BUTTSTRAP — DAMAGED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

AD 2010 05 13 FUSELAGE SKIN INSPECTION SKIN BUTT STRAP IS SCRIBE LINED 17.50 INCH LONG X 0.0025 INCH DEEP AT BS 908 5.117 INCH DISTANCE FROM STR 7L AND 5.739 INCH DISTANCE FROM STRINGER 10L. REMOVED AND REPLACED BUTT STRAP IAW B737 400 SRM 51 40 02.

Part: BUTTSTRAP — DAMAGED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

AD 2010 05 13 FUSELAGE SKIN INSPECTION SKIN BUTT STRAP IS SCRIBE LINED 24.062 INCH LONG X 0.003 INCH DEEP AT BS 727G 6.316 INCH DISTANCE FROM STR 10L AND 2.893 INCH DISTANCE FROM STR 14L. REMOVED AND REPLACED BUTT STRAP IAW B737 400 SRM 51 40 02.

Part: BUTTSTRAP — DAMAGED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

AD 2010 05 13 FUSELAGE SKIN INSPECTION SKIN BUTT STRAP IS SCRIBE LINED 7.600 INCH LONG X 0.003 INCH DEEP AT BS 727G 7.050 INCH DISTANCE FROM STR 5L AND 4.550 INCH DISTANCE FROM STRINGER 7L. REMOVED AND REPLACED BUTT STRAP IAW B737 400 SRM 51 40 02.

Part: BUTTSTRAP — DAMAGED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

AD 2010 05 13 FUSELAGE SKIN INSPECTION SKIN BUTT STRAP IS SCRIBE LINED 9.250 INCH LONG X 0.003 INCH DEEP AT BS 500C SCRIBE UPPER END IS 7.875 INCH DISTANCE FROM STR 2L AND LOWER END IS 1.510 INCH DISTANCE FROM STRINGER 4L. REMOVED AND REPLACED BUTT STRAP IAW B737 400 SRM 51 40 02.

Part: BUTTSTRAP — DAMAGED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

AD 2010 05 13 FUSELAGE SKIN INSPECTION SKIN BUTT STRAP IS SCRIBE LINED 7.5 INCH LONG X 0.001 INCH DEEP AT BS 500C SCRIBE UPPER END 2.590 INCH DISTANCE FROM STR 4R AND LOWER END 0.680 INCH DISTANCE FROM STR 5R. REMOVED AND REPLACED BUTT STRAP IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 727D RT FRAME CRACKED BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR IAW ASA TASK CARD AD20062609 400 53 104.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

STR TIE CLIP AT BS 727C STR TR CRACKED. REMOVED AND REPLACED STR CLIP IAW 737 400 SRM 51 40 02 PG 2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

STRINGER TIE AT BS 727A STR 9R CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW B737 400 SRM 51 40 02 PG 2.

Part: PLATE — CHAFED (RT WING) · airframe 58,334 hrs · 35,608 cycles

RIGHT WING NR 6 FLAP TRANSMISSION OUTBOARD TORQUE TUBE INSPECTION PLATE CHAFED. REMOVED DAMAGED PLATE FABRICATED REPLACEMENT PART AND INSTALLED IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 747 RT FRAME CRACKED BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR IAW ASA TASK CARD AD20062609 400 53 104.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 827 LT FRAME CRACKED BETWEEN STR 8L 9L. REPAIRED CRACKED FRAME IAW ASA TASK CARD AD20062609 400 53 104 REV DATED 12/06/10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 787 LT FRAME CRACKED BETWEEN STR 8L 9L. REPAIRED CRACK FRAME IAW ASA TASK CARD AD20062609 400 53 104 REV DATED 12/06/10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 867 RT FRAME CRACKED BETWEEN STR 8R AND 9R. REPAIRED FRAME IAW ASA TASK CARD AD20062609 400 53 104

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

SEAT TRACK AT STA 560 653 RBL 45 HAS BROKEN LUGS. REMOVED AND REPLACED SEAT TRACK IAW B737 400 SRM 51 40 02 AND B737 400 AMM 20 50 11 912 002.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 787 RT FRAME CRACKED BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR IAW ASA TASK CARD AD20062609 400 53 104.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

STRINGER TIE CLIP AT BS 727A STR 8R CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW B737 400 SRM 51 40 02 PG 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 907 LT FRAME CRACKED BETWEEN STR 8L 9L. REPAIRED CRACKED FRAME IAW ASA TASK CARD AD20062609 400 53 104 REV DATED 12/06/10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 727B RT FRAME CRACKED BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR IAW ASA TASK CARD AD20062609 400 53 104.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 727F LT FRAME CRACKED BETWEEN STR 8L AND 9L. REPAIRED CRACKED FRAME IAW ASA TASK CARD AD20062609 400 53 104 REV DATED 12/06/10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

SEAT TRACK AT BS 660 AND 727+6 HAS CORRODED AREAS. REMOVED AND REPLACED SEAT TRACK IAW B737 400 SRM 51 40 02 AND B737 400 AMM 20 50 11.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 907 RT FRAME CRACKED BETWEEN STR 8R AND 9R. REPAIRED FRAME IAW ASA TASK CARD AD20062609 400 53 104.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

SEAT TRACK AT BS 663 TO 727 LBL 24 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 827 RT FRAME CRACKED BETWEEN STR 8R AND 9R. REPAIRED FRAME IAW ASA TASK CARD AD20062609 400 53 104.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 747 LT FRAME CRACKED BETWEEN STR 8L 9L. REPAIRED CRACKED FRAME IAW ASA TASK CARD AD20062609 400 53 104 REV DATED 12/06/10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 867 LT FRAME CRACKED BETWEEN STR 8L 9L. REPAIRED CRACKED FRAME IAW ASA TASK CARD AD20062609 400 53 104 REV DATED 12/06/10.

Part: SKIN — DENTED (TE FLAP) · airframe 58,334 hrs · 35,608 cycles

LT OUTBOARD MAIN FLAP HAS SHARP DENT ON THE UPPER SURFACE APPROX 0.50 INCH FROM OUTBOARD END 0.320 INCH DEEP 0.50 INCH WIDE A/Y = 21.74. REPAIRED DENT IAW B737 400 SRM 51 70 10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 727F RT FRAME CRACKED BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR IAW ASA TASK CARD AD20062609 400 53 104.

Part: FRAME — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

BS 727D LT FRAME CRACKED BETWEEN STR 8L AND 9L. REPAIRED CRACKED FRAME IAW ASA TASK CARD AD20062609 400 53 104 REV DATED 12/06/10.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

STA 907 STRINGER SPLICE CRACKED AT STR 4L. REMOVED AND REPLACED STRINGER SPLICE IAW B737 400 SRM 51 40 02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

APU LOWER SHROUD SKIN EDGE CRACKED AT MATING FLANGE ON RT SIDE 20 INCHES OF FWD END. REPAIRED APU LOWER SHROUD IAW EA 400 49EA 04607.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

SEAT TRACK AT LBL 45 BETWEEN 670 & 680 HAS AREAS ON CORROSION. REMOVED AND REPLACED SEAT TRACK WITH P/N BAC1520 841 TAG A54037 IAW B737 400 SRM 51 40 05 FIG 2 AND B737 400 AMM 20 50 11 912 002 FIG 203.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,334 hrs · 35,608 cycles

APU LOWER SHROUD SKIN EDGE CRACKED AT MATING FLANGE ON RT SIDE 20 INCHES AFT OF FWD END. REPAIRED APU LOWER SHROUD IAW EA 400 49EA 04607.

Part: SKIN — CHAFED (TE FLAP) · airframe 58,334 hrs · 35,608 cycles

LEFT WING OUTBOARD AFT FLAP LOWER SURFACE CHAFED AT NR 2 FLAP TRACK FAIRING OUTBOARD SIDE APPROX WS 278. REPAIRED IAW ASA EA 400 57EA 04662.

Part: DOUBLER — CHAFED (FOREFLAP) · airframe 58,334 hrs · 35,608 cycles

LEFT WING OUTBOARD FORE FLAP INBOARD LEADING EDGE REPAIR DOUBLER CHAFED WING STA 205. REPAIRED FORE FLAP IAW B737 400 SRM 57 53 01 FIG 201.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 58,334 hrs · 35,608 cycles

VERT STAB LT FWD SKATE ANGLE CHAFED. FABRICATED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51 30 01 FIG 7 & 51 40 02.

Part: FLAP — CHAFED (LT WING) · airframe 58,334 hrs · 35,608 cycles

LT WING OUTBOARD MID FLAP INBOARD LEADING EDGE CHAFED. REPAIRED MID FLAP IAW B73 400 SRM 57 53 01 FIG 201.

Part: FLAP — CHAFED (RT WING) · airframe 58,334 hrs · 35,608 cycles

RT WING OUTBOARD MID FLAP INBOARD LEADING EDGE CHAFE. REPAIRED MID FLAP IAW B737 400 SRM 57 53 01 FIG 201.

Part: DOUBLER — CHAFED (FOREFLAP) · airframe 58,334 hrs · 35,608 cycles

LEFT WING OUTBOARD FORE FLAP OUTBOARD LEADING EDGE REPAIR DOUBLER IS CHAFED. REPAIRED FORE FLAP IAW B737 400 SRM 57 53 01 FIG 201.

Part: WEB — CHAFED (LT WING) · airframe 58,334 hrs · 35,608 cycles

LEFT WING TRAILING EDGE FLAPWELL WEB CHAFED. REMOVED DAMAGED PLATE FABRICATED REPLACEMENT PART AND INSTALLED IAW BOEING DWG 65 69646.

Part: SUPPORT ANGLE — CRACKED (AILERON) · airframe 58,334 hrs · 35,608 cycles

LEFT WING AILERON BALANCE BAY SUPPORT ANGLE CRACKED (FWD OF TAB CONTROL ROD). REMOVED & REPLACED ANGLE IAW B737 400 SRM 51 40 02.

Part: SKIN — GOUGED (RT WING) · airframe 58,334 hrs · 35,608 cycles

RT WING L/E GOUGED AT APPROX WS 178. REPAIRED LEADING EDGE IAW B737 400 SRM 57 41 01 FIG 101.

Part: ROLLER — LACK OF LUBE (L1 DOOR) · airframe 56,890 hrs · 34,322 cycles

FLIGHT ATTENDANT REPORTS L1 DOOR HARD TO CLOSE, FWD ENTRY DOOR FAILS THE OPEN TEST REF AMM 52 11 00 755 051 PG 2 PARA 5 [C] ,1 DOOR DOES NOT OPEN AT 600 IN LBS OR LESS [62572]. LUBE DOOR AND ROLLERS AND HINGES REF 52 11 00 705 PGS 1 THRU 8. ALSO TORQUE WAS BELOW 600 [500] TO OPEN, OPS CHECK GOOD MM 52 11 00 755 051 PG 2 ITEM 5 AB AND C.

Part: SKIN — DAMAGED (NR 4 SPOILER) · airframe 55,381 hrs · 32,995 cycles

NR 4 GROUND SPOILER LWR SURFACE HAS GRAVEL DAMAGE. REMOVED AND INSTALLED NEW SPOILER.

Part: SKIN — CRACKED (LT WING) · airframe 55,381 hrs · 32,995 cycles

LEFT WING UPPER FIXED LE SKIN CRACKED APPROX 14 INCH INBD OF NR 1 PYLON ABOVE NR 1 K FLAP. REPAIRED BY CUTTING OUT DAMAGE INSTALLED FILLER AND DOUBLER.

Part: SKIN — GOUGED (MAIN CARGO DOOR) · airframe 55,381 hrs · 32,995 cycles

MAIN CARGO DOOR INNER SKIN IS GOUGED BETWEEN LATCHES 6/7 10 INCHES FROM LOWER EDGE JUST BELOW SEQUENCE VALVE NR 2. REPAIRED MAIN CARGO DOOR INNER SKIN AND FOUND OUT OF LIMITS.

Part: DOOR FRAME — CRACKED (BS 312) · airframe 55,381 hrs · 32,995 cycles

FORWARD SERVICE DOOR (R1) AFT FRAME CRACKED. INSTALLED NEW AFT FRAME PER SRM 51-40-02 AND DWG 65 45871.

Part: ANGLE — CRACKED (SERVICE DOOR) · airframe 55,381 hrs · 32,995 cycles

FWD SERVICE DOOR AFT CORNER ANGLE CRACKED. REMOVED AND REPLACED WITH NEW ANGLE.

Part: BRACKET — CRACKED (SERVICE DOOR) · airframe 55,381 hrs · 32,995 cycles

FWD SERVICE DOOR AFT CORNER BRACKET CRACKED. REMOVED AND REPLACED WITH NEW BRACKET.

Part: STOP FITTING — CRACKED (SERVICE DOOR) · airframe 55,381 hrs · 32,995 cycles

FWD SERVICE DOOR AFT CORNER STOP FITTING CRACKED. REMOVED AND REPLACED WITH NEW SERVICEABLE STOP FITTING.

Part: SKIN — DENTED (HORIZ STAB) · airframe 55,381 hrs · 32,995 cycles

RT HORIZONTAL STABILIZER LEADING EDGE DENTED. PERMANENTLY REPAIRED RT HORIZONTAL STABILIZER.

Part: DOOR FRAME — GOUGED (CARGO DOOR) · airframe 55,381 hrs · 32,995 cycles

MAIN CARGO DOOR FRAME IS GOUGED JUST BELOW NR 7 LATCH. REPAIRED DOOR.

Part: SKIN — CHAFED (TE FLAP) · airframe 55,381 hrs · 32,995 cycles

RT OUTBOARD MID FLAP LOWER AFT SKIN UPPER SURFACE IS CHAFED AT 34 AFT TRACK. REPAIRED SKIN.

Part: SKIN — DENTED (BS 897) · airframe 55,381 hrs · 32,995 cycles

EXTERNAL SKIN DENTED AT BS 897 BETWEEN STR 14R AND 15R. CUTOUT DAMAGE INSTALLED REPAIR.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 55,381 hrs · 32,995 cycles

NR 7 FLAP TRACK PITTING CORROSION IN VARIOUS PLACES. REMOVED AND REPLACED TRACK.

Part: SKIN — GOUGED (BS 727E) · airframe 55,381 hrs · 32,995 cycles

GOUGE IN FUSELAGE SKIN RT 6 INCHES FWD BS 727E 1 INCH BELOW STR 23R. DAMAGE REMOVED AND REPAIR COMPLETED.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,381 hrs · 32,995 cycles

PROTRUDING DENT IN FUSELAGE SKIN 12 INCHES FWD OF BS 727F BELOW STR 24R. REPAIRED PER SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,381 hrs · 32,995 cycles

PROTRUDING DENT IN FUSELAGE SKIN 2 INCHES FWD OF BS 547. REPAIRED FUSELAGE SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,381 hrs · 32,995 cycles

CLOSE OUT WEB CRACKED AT BS 851 ABOVE STR 25R.

Part: SKIN — CHAFED (TE FLAP) · airframe 55,381 hrs · 32,995 cycles

RIGHT O/B MID FLAP AFT LOWER SKIN OUTER SURFACE IS CHAFED ON PREVIOUS REPAIR DOUBLER AT NR 1 AFT TRACK. RIGHT O/B MID FLAP AFT LOWER SKIN OUTER SURFACE WAS REPAIRED.

Part: MOUNT — CRACKED (VHF ANTENNA) · airframe 55,381 hrs · 32,995 cycles

NUMBER 2 VHF ANTENNA MOUNT IS CRACKED. REPLACED ANTENNA MOUNT.

Part: SILL — GOUGED (BS 400) · airframe 55,381 hrs · 32,995 cycles

MED LOWER SILL WEB IS GOUGED JUST AFT OF NR 4 LATCH RECEPTACLE. BLENDED AND TREATED AREA.

Part: MOUNT — CRACKED (VHF COMM) · airframe 55,381 hrs · 32,995 cycles

NR 2 VHF ANTENNA MOUNT IS CRACKED. REMOVED AND INSTALLED SERVICEABLE ANTENNA MOUNT.

Part: WEDGE — DEBONDED (MIDFLAP) · airframe 55,381 hrs · 32,995 cycles

LT IB MID FLAP TE WEDGE LOWER SURFACE HAS A DISBOND. REPAIRED.

Part: SLAT — DELAMINATED (NR 5) · airframe 55,381 hrs · 32,995 cycles

NR 5 SLAT UPPER O/B TRAILING EDGE IS DELAMINATED. REPAIRED SLAT.

Part: SKIN — DENTED (TE FLAP) · airframe 55,381 hrs · 32,995 cycles

SHARP DENT ON THE LT INBOARD FORE FLAP UPPER SURFACE. REPAIRED FORE FLAP.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,381 hrs · 32,995 cycles

CORROSION ON FLOOR PANEL SPLICE FLOOR STRUCTURE. FABRICATED NEW SPLICE PLATE INSTALLED NUT PLATES RESTORED FINISH.

Part: SKIN — DELAMINATED (RT WING FOREFLAP) · airframe 55,381 hrs · 32,995 cycles

RT IB FORE FLAP UPPER SURFACE HAS A DELAMINATING PREVIOUS REPAIR 35 INCHES FROM OB END. REPAIRED PER SRM.

Part: SKIN — GOUGED (FOREFLAP) · airframe 55,381 hrs · 32,995 cycles

LT OB FORE FLAP LEADING EDGE SKIN IS GOUGED IN MULTIPLE AREAS. REPAIRED SKIN.

Part: SKIN — GOUGED (FOREFLAP) · airframe 55,381 hrs · 32,995 cycles

RT OB FORE FLAP LE SKIN IS GOUGED IN MULTIPLE AREAS. REPAIRED PER SRM. BLENDED DAMAGE, INSTALLED REPAIR DOUBLER.

Part: SKIN — DENTED (HORIZ STAB) · airframe 55,381 hrs · 32,995 cycles

DENT ON LT LE OF HORIZONTAL STAB 138" FROM ROOT. PERMANENT REPAIRED.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 55,381 hrs · 32,995 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT. REPLACED SUPPORT.

Part: SKIN — GOUGED (VENT DOOR) · airframe 55,381 hrs · 32,995 cycles

MAIN CARGO DOOR FWD VENT DOOR INNER SKIN IS GOUGED. REPLACED MED FWD VENT DOOR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,337 hrs · 32,955 cycles

THREE (3) INCH CRACK FOUND IN EXTERIOR SKIN AT STA 727 STR 25R. REPAIRED SKIN PER SRM.

Part: HYDRAULIC LINE — DAMAGED (MLG WW) · airframe 55,076 hrs · 32,732 cycles

AT FL 370 ENG 2 SYSTEM B LOW PRESSURE LIGHT ILLUMINATED. HYD B SYSTEM SHOWED 40 PERCENT THEN DROPPED TO 1 PERCENT. ELEC B LIGHT ILLUMINATED ALONG WITH FEEL DIFFERENTIAL PRESSURE LOSS OF SYS B. REPLACED HYDRAULIC LINE AND HOSE. OP AND LEAK CHECK GOOD.

Part: NUT — LOOSE (L1 DOOR) · airframe 52,983 hrs · 30,858 cycles

L1 DOOR WILL NOT CLOSE FOUND GUIDE ARM ROD END JAMB NUT LOOSE. SECURED LOOSE JAMB NUT. L1 DOOR OPS CHECK GOOD.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 52,704 hrs · 30,603 cycles

SEAT TRACK AT BS 480 BS 520 RBL 20 FOUND FLOORBEAM HAVING ADDITIONAL FASTENER HOLE AT BS 500 FROM PREVIOUS INSTALLATION AND HOLE WOULD FALL DIRECTLY UNDER SEAT TRACK. REPAIRED ADDITIONAL FASTENER HOLE AT BS 500 FROM PREVIOUS INSTALLATION DIRECTLY UNDER SEAT TRACK RBL 25 PER ASA EA 400 53EA 00161. PERMANENT REPAIR TO SUBJECT BEAM ACCOMPLISHED AT NEXT HEAVY CHECK NO LATER THAN 18 MONTHS FROM 05 NOV 2008.

Part: GUST LOCK — LACK OF LUBE (L2 DOOR) · airframe 52,698 hrs · 30,599 cycles

L2 DOOR GUST LOCK INOP. THOROUGHLY CLEANED AND LUBED L 2 DOOR GUST LOCK. PERFORMED OPS CHECK APPROX 20 TIMES WITH NO FAILURE. OPS NORMAL.

Part: SPAR — DELAMINATED (LT AILERON) · airframe 52,642 hrs · 30,555 cycles

LT WING AILERON FRONT SPAR DELAMINATED I/B CORNER. REMOVED AND REPLACED LT AILERON IAW B737 400 MM 27 11 11.

Part: LIGHT — MISWIRED (CARGO BAY) · airframe 52,642 hrs · 30,555 cycles

CABIN MAIN CARGO LIGHT 15AMP CIRCUIT BREAKER C9001 FAIL TO TRIP WHEN FWD UPPER CARGO LIGHT WAS MISWIRED ALLOWING POSITIVE TO GROUND CAUSING J10 BOX TO BURN UNTIL ELECTRICAL CIRCUIT OPENED. REFERENCE PEMCO WDM 33 30 02 PAGE 3 SHEET 1. REPAIRED IAW AAR EA 12982 AND ASA EA 3330 01021. REBUILT J 10 BOX INSPECTED AND REPLACED DAMAGED WIRING. INSPECTED AND REPAIRED AS REQUIRED ADJACENT WIRE RUNS FROM J10 BOX TO CARGO OVERHEAD LIGHTING.

Part: SKIN — DENTED (MIDFLAP) · airframe 52,642 hrs · 30,555 cycles

LT INBOARD MID FLAP T/E WEDGE HAS MULTIPLE DENTS ON A PREVIOUS REPAIR ON THE LOWER SURFACE. REMOVED DAMAGED DOUBLER, FABBED REPLACEMENT DOUBLER AND BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REP 4.

Part: SKIN — DENTED (FOREFLAP) · airframe 52,642 hrs · 30,555 cycles

LT OUTBOARD FORE FLAP HAS MULTIPLE DENTS ON THE LOWER SURFACE INBOARD END. REMOVED DAMAGED AREAS, FABBED FILLERS AND DOUBLERS AND BONDED THE REPAIRS IAW B737 400 SRM 51 70 10 REP 4.

Part: SKIN — DENTED (NR 1 SPOILER) · airframe 52,642 hrs · 30,555 cycles

LEFT WING NR 1 SPOILER LOWER SURFACE HAS MULTIPLE DENTS. PREPPED REPAIR AREA, FABBED REPAIR PARTS & BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REP 4.

Part: SKIN — GOUGED (FOREFLAP) · airframe 52,642 hrs · 30,555 cycles

LT OUTBOARD FOREFLAP L/E IS GOUGED 6 INCHES FROM INBOARD END. REMOVED DAMAGED SKIN, FABBED, HEAT TREATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 52,642 hrs · 33,555 cycles

RT WING AFT I/B FORE FLAP DELAMINTATED ON LOWER SURFACE. PREPARED DAMAGED AREA AND PREPARED 3 EACH REPAIR PLYS AND BONDED IAW B737 400 SRM 51 70 16 PG 17.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · corrosion level 2 · airframe 52,642 hrs · 33,555 cycles

FWD CARGO BAY RT INTERCOSTAL STR 25R STA 500 500A CRACKED AT NUT PLATE HOLE. REMOVED INTERCOSTAL, LOCATED, DRILLED NEW INTERCOSTAL, INSTALLED NEW INTERCOSTAL IAW B737 400 SRM 51 40 02 05.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 52,642 hrs · 33,555 cycles

AFT CARGO FLOOR SUPPORT AT STA 727F LBL 8.10 1 EA HOLE AND 1 EACH DEEP DRILL START. REMOVED DAMAGED SECTION OF FLOOR SUPPORT, FABRICATED CHANNEL REPAIR PARTS, LOCATED, DRILLED AND INSTALLED IAW AAR EA 12953 AND ASA EA 5310 02826.

Part: SKIN — PUNCTURED (RT ELEVATOR) · airframe 52,642 hrs · 33,555 cycles

RIGHT ELEVATOR UPPER SURFACE SMALL PUNCTURE 6 INCHES FROM TRAILING EDGE AND 4 FEET FROM I/B END. PREPARED REPAIR AREA, APPLIED RESIN AND BONDED TWO LAYERS OF GRAPHITE CLOTH IAW B737 400 SRM 51 70 03 REPAIR 2.

Part: HINGE FITTING — GOUGED (LT AILERON) · airframe 52,642 hrs · 33,555 cycles

UPON REMOVAL OF LT WING AILERON FOUND NR 1 HINGE LUG ON FITTING GOUGED IN 2 PLACES. REMOVED NR 1 HINGE FITTING DAMAGE FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED AND INSTALLED A REPLACEMENT FITTING IAW B737 400 SRM 51 40 02 AND AAR EA 12969 ASA EA 5750 02509.

Part: SHEAR TIE — DAMAGED (BS 380) · airframe 52,642 hrs · 33,555 cycles

ACCOMPLISH SHEAR TIE REPAIR AT STA 380 BETWEEN STA 25L AND 26L REF ASA EA 5310 02675 ITEM 7 IAW SRM 53-00-07 (EDGE DISTANCE AT FASTENER HOLES BELOW MINIMUM). REMOVED DAMAGED SHEAR TIE, LOCATED DRILLED AND INSTALLED A REPLACEMENT SHEAR TIE IAW SRM 53-00-07 FIG 201.

Part: WEB — CRACKED (FUSELAGE) · airframe 52,642 hrs · 33,555 cycles

CABIN FLOOR WEB CRACKED STA 986 LBL 30. REMOVED DAMAGED WEB, FABRICATED REPAIR PARTS, LOCATED, DRILLED, INSTALLED A REPLACEMENT PANEL FLOOR WEB IAW B737 400 SRM 51 40 02 PG 293.

Part: FRAME — CHAFED (FUSELAGE) · airframe 52,642 hrs · 33,555 cycles

COCKPIT RT FRAME WEB CHAFED STA 211.8 AFT SIDE ABOUT 21 INCHES ABOVE FLOOR LEVEL. BLENDED AREA TO REMOVE DAMAGE. HFEC INSPECTED, NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER AND INSTALLED IAW AAR EA 12950 AND ASA EA 5310 02821.

Part: SKIN — CHAFED (TE FLAP) · airframe 52,642 hrs · 33,555 cycles

LT WING O/B MID FLAP LOWER SURFACE CHAFED O/B OF NR 1 FLAP TRACK. REMOVED DAMAGED AREA OF SKIN, FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 PG 254.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,642 hrs · 33,555 cycles

APU TORQUE BOX TOP BULB FRAME STRINGER CORRODED. REMOVED DAMAGED FRAME STRINGER, LOCATED DRILLED AND INSTALLED A REPLACEMENT STRINGER IAW B737 400 SRM 51 40 02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 52,642 hrs · 33,555 cycles

APU TORQUE BOX BOTTOM STRINGER CORRODED. REMOVED APU TORQUE BOX BOTTOM STRINGERS LOCATED DRILLED AND INSTALLED REPLACEMENT STRINGERS IAW B737 400 SRM 51 40 02 PG 2-5.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,642 hrs · 33,555 cycles

L2 DOOR THRESHOLD WEB STA 967 TO STA 980 CORRODED UNDER INNER CHORD. REMOVED DAMAGED WEB, FABRICATED HEAT TREATED, LOCATED, DRILLED AND INSTALLED A REPLACEMENT WEB IAW B737 400 SRM 51 40 02.

Part: SKIN — CHAFED (FOREFLAP) · airframe 52,642 hrs · 33,555 cycles

RT WING O/B FORE FLAP I/B LEADING EDGE CHAFED FROM CONTACT WITH CAVITY PANEL. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND DOUBLER IAW B737 400 SRM 51 53 01 FIG 201 AND INSTALLED.

Part: SKIN — DENTED (TE FLAP) · airframe 52,642 hrs · 33,555 cycles

RT WING AFT I/B TRAILING EDGE FLAP LOWER SURFACE DENTED IN 4 SPOTS. REMOVED DAMAGED SKIN, FABRICATED FILLER AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,642 hrs · 33,555 cycles

DURING HEAVY MAINTENANCE WHILE ACCOMPISHING INSPECTIONS OF R1 DOOR LOWER CUTOUTS PER EM 5330 02085 TWO FASTENER HOLES WERE FOUND ELONGATED. FABRICATED FREEZE PLUGS FOR HOLE REPAIR FABRICATED REPLACEMENT STIFFENER ANGLE FILLER TAPERED FILLER AND SINGLE REPAIR DOUBLER. INSTALLED IAW AAR EA 12932 AND ASA EA 5310 02827.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 52,642 hrs · 33,555 cycles

E&E BAY SHEAR TIE CORRODED STA 344 RBL 12. REMOVED DAMAGED SHEAR TIE, FABRICATED SHEAR TIE AND DOUBLER, LOCATED, DRILLED, INSTALLED IAW B737 400 SRM 53 00 07 FIG 201.

Part: INTERCOSTAL — CORRODED (BS 947-967) · corrosion level 2 · airframe 52,642 hrs · 33,555 cycles

AFT CABIN FLOOR INTERCOSTAL CORRODED AT STA 947 AT LBL 40. REMOVED DAMAGED INTERCOSTAL LOCATED DRILLED INSTALLED A REPLACEMENT INTERCOSTAL IAW B737 400 SRM 51 40 02.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,642 hrs · 30,555 cycles

AFT CABIN L2 DOOR THRESHOLD INNER CHORD CORRODED STA 946 TO 992. REMOVED DAMAGED INNER CHORD, DRILLED, INSTALLED A REPLACEMENT INNER CHORD IAW B737 400 SRM 51 40 02 PG 2 4.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,642 hrs · 33,555 cycles

APU INLET FRAME RT SIDE OF TORQUE BOX CORRODED. REMOVED DAMAGED FRAME STIFFENER, LOCATED DRILLED AND INSTALLED REPLACEMENT STIFFENER IAW B737 400 SRM 51 40 02 PG 2-5.

Part: THRESHOLD — CORRODED (BS 907-1006) · corrosion level 2 · airframe 52,642 hrs · 33,555 cycles

AFT CABIN FLOOR R2 DOOR THRESHOLD INNER CHORD CORRODED STA 946 TO STA 992 AREA. REMOVED DAMAGED INNER CHORD, LOCATED DRILLED AND INSTALLED REPLACEMENT INNER CHORD IAW B737 400 SRM 51 40 02 51 40 05.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,642 hrs · 33,555 cycles

AFT CABIN FLOORBEAM STA 986 CORRODED AT EXISTING UPPER CHORD REPAIR RBL 40 TO LBL 40. REMOVED DAMAGED UPPER CHORD, FABRICATED REPAIR TEE SECTIONS REPAIR SPLICES, HEAT TREATED, LOCATED, DRILLED AND INSTALLED IAW AAR EA 12922 AND ASA EA 5310 02823.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,642 hrs · 33,555 cycles

AFT CARGO COMPARTMENT STA 1006 FRAME CORRODED STR 22R AND 24R. CUT OUT DAMAGED AREA OF FRAME, FABRICATED REPAIR PARTS AND SPLICE DOUBLER, LOCATED, DRILLED AND INSTALLED IAW B737 400 SRM 53 00 07 FIG 201 AND 51 40 02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 52,642 hrs · 33,555 cycles

AFT CABIN FLOORBEAM STA 967 CORRODED RBL 40 TO LBL 40. CUT OUT DAMAGED AREA OF UPPER CHORD, FABRICATED REPAIR PARTS, LOCATED, DRILLED, INSTALLED REPAIR PARTS UPPER CHORD IAW B737 400 SRM 53 00 51 FIG 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,642 hrs · 33,555 cycles

AFT CABIN FLOORBEAM STA 947 CORRODED AT EXISTING UPPER CHORD REPAIR LBL 40 TO RBL 40. REMOVED DAMAGED UPPER CHORD, FABRICATED REPAIR TEE SECTION, REPAIR SPLICES AND STRAPS, LOCATED, DRILLED AND INSTALLED IAW AAR EA 12921 AND ASA EA 5310 02824.

Part: SKIN — CHAFED (NR 3 SLAT) · airframe 52,642 hrs · 30,555 cycles

LEFT WING NR 3 SLAT T/E WEDGE LOWER SURFACE CHAFED CENTER AREA. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER BONDED IAW B737 400 SRM REPAIR 4.

Part: SKIN — CHAFED (LE SLAT) · airframe 52,642 hrs · 33,555 cycles

LT WING NR 2 LEADING EDGE SLAT LOWER SURFACE CHAFED AT O/B TRAILING EDGE WEDGE. REMOVED DAMAGED SKIN, FABRICATED FILLER SKIN AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — CHAFED (LE SLAT) · airframe 52,642 hrs · 33,555 cycles

LT WING NR 3 SLAT LOWER SURFACE I/B CORNER CHAFED. REMOVED DAMAGED AREA OF SKIN, FABRICATED FILLER SKIN AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (SPOILER) · airframe 52,642 hrs · 33,555 cycles

LT WING I/B GROUND SPOILER HAS SEVERAL DENTS ON UPPER SURFACE. REMOVED DAMAGED IN 4 EACH AREAS, PREPARED AREAS, FABRICATED FILLERS AND DOUBLERS, BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (NR 9 SPOILER) · airframe 52,642 hrs · 30,555 cycles

RIGHT WING NR 9 SPOILER UPPER SURFACE 2 DENTS CLOSE TOGETHER. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER BONDED IAW SRM 51-70-10 REPAIR 2.

Part: SKIN — DENTED (NR 7 SPOILER) · airframe 52,642 hrs · 30,555 cycles

RT WING NR 7 SPOILER UPPER SURFACE AREAS OF MULTIPLE DENTS. REMOVED DAMAGED AREAS, FABRICATED FILLERS AND DOUBLERS BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: FRAME — CORRODED (FUSELAGE) · airframe 52,642 hrs · 33,555 cycles

FWD CARGO BAY STA 520 FRAME CORRODED AT STA 520 BETWEEN STR 27R AND STR 28R PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR DOUBLER AND SHEAR TIE, FABRICATED, LOCATED, DRILLED AND INSTALLED A REPLACEMENT SHEAR TIE AND DOUBLER IAW B737 400 SRM 53 00 07 FIG 201.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,642 hrs · 33,555 cycles

FWD CARGO BAY KEEL BEAM CHORD CORRODED AT STA 500 AT 1.5 INCHES I/B OF DRAIN HOLE. CUT OUT DAMAGED AREA. HFEC INSPECTED NO DEFECT NOTED. FABRICATED FILLER ANGLE SPLICE, LOCATED, DRILLED AND INSTALLLED IAW B737 400 SRM 53 30 12 REPAIR 2 FIG 201 AND ASA EA 5310 02822.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 52,642 hrs · 30,555 cycles

LEFT WING INBOARD AFT FLAP EXHAUST GATE WORN ON UPPER SURFACE. REMOVED DAMAGED UPPER PANEL, LOCATED, DRILLED AND INSTALLED A REPLACEMENT UPPER PANEL IAW B737 400 SRM 51 40 02 51 40 05.

Part: SKIN — DAMAGED (NR 5 SPOILER) · airframe 52,642 hrs · 33,555 cycles

RIGHT WING NR 5 SPOILER LOWER SURFACE DAMAGED. PREPARED DAMAGED AREA, FABRICATED REPAIR PARTS AND BONDED DOUBLERS IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (SPOILER) · airframe 52,642 hrs · 30,555 cycles

LT WING NR 2 SPOILER DENTED ON UPPER SURFACE 12 INCHES FROM O/B END. PREPARED DAMAGED AREA, FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (LE SLAT) · airframe 52,642 hrs · 33,555 cycles

LT WING I/B MID FLAP TRAILING EDGE WEDGE DENTS ON LOWER SURFACE. REMOVED DAMAGED AREA, FABRICATED SKIN AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 52,642 hrs · 33,555 cycles

LEFT WING I/B AFT FLAP UPPER SURFACE AREAS OF DENTS. PREPARED DAMAGED AREA, FABRICATED DOUBLERS, TREATED, REPAIRED AND BONDED IAW SRM 51-70-10 REPAIR 2.

Part: SKIN — DENTED (NR 2 SPOILER) · airframe 52,642 hrs · 30,555 cycles

LEFT WING NR 2 SPOILER DENTED ON UPPER SURFACE 12 INCHES FROM O/B END. PREPARED DAMAGED AREA, FABRICATED DOUBLER AND BONDED IAW 737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (TE FLAP) · airframe 52,642 hrs · 33,555 cycles

RT AFT FLAP LOWER SURFACE DENTED WITHIN EDGE BAND. REMOVED, DAMAGED SKIN, FABRICATED FILLER AND DOUBLER, BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,642 hrs · 30,555 cycles

BODY STATION 616 LT SIDE INNER CHORD IS CRACKED AT WL 200 (REF SECTION 5 OF EO 5310 0528). CUT OUT DAMAGED AREA, FABRICATED FILLER STIFFENING ANGLE LOCATED DRILLED AND INSTALLED IAW EO 5310 02528.

Part: SKIN — CHAFED (MID FLAP) · airframe 52,642 hrs · 33,555 cycles

RIGHT O/B MID FLAP LOWER SURFACED CHAFED BELOW NR 7 FLAP CARRIAGE. REMOVED DAMAGED AREA OF SKIN, FABRICATED REPAIR PARTS IAW B737 400 SRM 51 70 10 PG 214 AND BONDED IAW B737 400 SRM 51 70 10 PG 254.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,642 hrs · 30,555 cycles

AFT CARGO DOOR LOWER THRESHOLD WEB CORRODED STA 805 TO STA 840 RBL 27 RBL 31 WL 147 WL 151. REMOVED DAMAGED WEB LOCATED DRILLED AND INSTALLED A REPLACEMENT WEB IAW B737 400 SRM 51 40 02 PARA 5 FIG 9 AND 10.

Part: SKIN — DENTED (FUSELAGE) · airframe 52,642 hrs · 30,555 cycles

EXT FUSELAGE DENTED AT STA 490 BETWEEN STR 21L AND STR 22L MEASURES A = 3.0 INCHES Y = 1.1 INCHES A Y=27. TRIMMED OUT DENT DAMAGE, HFEC INSPECTED TRIMMED OUT, NO DEFECT NOTED. FABRICATED REPAIR PARTS, LOCATED, DRILLED, INSTALLED FILLER DOUBLER AND TRIPLER IAW AAR EA 12944 ASA EA 5330 02395.

Part: SKIN — DENTED (SPOILER) · airframe 52,642 hrs · 30,555 cycles

LT WING NR 0 SPOILER DENTED ON LOWER SURFACE NEAR CENTER AT T/E. REMOVED DAMAGED AREA, PREPARED AREA, FABRICATED FILLER AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DAMAGED (BS 989-1016) · airframe 52,642 hrs · 30,555 cycles

SKIN CREASE ON FWD SIDE OF STA 1016 1.5 INCHES ABOVE STR 13L. REMOVED DAMAGED SKIN PANEL PREPARED AND BONDED DOUBLER TO NEW SKIN LOCATED DRILLED AND INSTALLED NEW PANEL IAW SRM 51-70-10 & 51-40-02.

Part: SKIN — DENTED (SPOILER) · airframe 52,642 hrs · 30,555 cycles

LEFT WING NR 0 SPOILER DENTED ON LOWER SURFACE NEAR CENTER AT TRAILING EDGE. REMOVED DAMAGED AREA, PREPARED AREA, FABRICATED FILLER AND DOUBLER BONDED IAW 737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (NR 1 SPOILER) · airframe 52,642 hrs · 33,555 cycles

LT WING NR 1 SPOILER DENTED 2 INCHES FROM LEADING EDGE 10 INCHES FROM O/B EDGE. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER BONDED IAW B737 400 SRM 51 70 01 REPAIR 4.

Part: SKIN — CHAFED (LE SLAT) · airframe 52,642 hrs · 33,555 cycles

RT WING L NR 4 LEADING EDGE SLAT I/B TRAILING EDGE WEDGE HEAVY CHAFE AT I/B END. REMOVED DAMAGED AREA, FABRICATED SKIN AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: LINK — WORN (FLAP TRANMISSION) · airframe 52,151 hrs · 30,110 cycles

NR 5 FLAP TRANSMISSION UPPER BALL LINK WORN. REPLACED TRANSMISSION REF 27-51-71-004-001 AND 27-51-71-404-026.

Part: TORQUE TUBE — CHAFED (L2 DOOR) · airframe 51,909 hrs · 29,887 cycles

L2 MAIN ENTRY PASSENGER DOOR LOWER DOOR HINGE CHAFING ON HARDWARE MIG2C 222915 INT REMOVED AND REPLACED TORQUE TUBE RADIUS LING ASSY AND TORQUE TUBE SPLINED END REF AMM 52 13 11. VERIFIED ALL MIG2C 222915. ITEMS CLEARED.

Part: DOOR — BROKEN (T/E FLAP) · airframe 50,870 hrs · 28,969 cycles

COULD NOT LOWER T/E FLAPS BEYOND 10 DEGS ON APPROACH INTO KTN. REMOVED DAMAGED RIGHTHAND INBOARD FLAP MID FLAP TORQUE DOOR WHICH WAS IMPEDING FLAP TRANSLATION. DOOR REPLACEMENT DEFERRED PER CDL.

Part: CUSP WEB — CORRODED (BS 312-332) · airframe 50,628 hrs · 28,751 cycles

MAIN CABIN LEFT STA 312 332 LBL 56 CUSP WEB HAS CORROSION AT L1 DOOR CUTOUT. REMOVED CORROSION FOUND OUT OF LIMITS. FABRICATED NEW CUSP WEB USING MATERIAL 7075 T6.40. INSTALLED NEW CUSP WEB IAW BAC DWG 65 17688 AND SRM 737 400 51-40-2.

Part: ATTACH ANGLE — CORRODED (BS 328-344) · airframe 50,628 hrs · 28,751 cycles

MAIN CABIN FS 328 344 LBL 60 CUSP WEB ATTACH ANGLE HAS CORROSION. FABRICATED AND INSTALLED NEW ANGLE IAW BAC DWG 65 17688 AND BAC 737 400 SRM 51-40-2.

Part: ATTACH ANGLE — CORRODED (BS 312-328) · airframe 50,628 hrs · 28,751 cycles

MAIN CABIN FS 316 328 LBL 60 CUSP WEB ATTACH ANGLE HAS CORROSION. REMOVED CORROSION FROM ANGLE ORG MATERIAL .090, REMOVED MATERIAL .020 REMAINING .070, FOUND OUT OF LIMITS. OBTAINED DRILLED AND INSTALLED NEW ANGLE IAW B737 400 SRM 51-40-2.

Part: WEB — DAMAGED (FUSELAGE) · airframe 50,628 hrs · 28,751 cycles

MAIN CABIN CUSP WEB STA 355 RBL 58 HAS ELONGATED 1 4 INCH HOLE. REMOVED WEB IAW 737 SRM 51-40-2 OBTAINED NEW WEB P/N 6545875 62 P/O 0740866 DRILLED AND INSTALLED PER BAC DRAWING 65 45875

Part: STRINGER — CRACKED (FUSELAGE) · airframe 50,628 hrs · 28,751 cycles

FWD CARGO COMPARTMENT STA 500A STG 19L CRACKED IN UPPER FLANGE. INSTALLED SPLICE REPAIR TO STG 19L STA 500A IAW B737 400 SRM 53-30-03 FIG 1 AND FIG 101 AND 53-00-03 FIG 201.

Part: INTERCOSTAL — CRACKED (BS 400) · airframe 50,628 hrs · 28,751 cycles

STA 400 LBL 24.75 INTERCOSTAL BELOW SEAT TRACK CRACKED. FABRICATED AND INSTALLED NEW INTERCOSTAL WEB IAW BAC DWG 69 73054 AND SRM 51-40-2.

Part: ATTACH ANGLE — DAMAGED (BS 277-291) · airframe 50,628 hrs · 28,751 cycles

CLIP WEB ATTACH ANGLE STA 277 291 RBL 56 HAS 6 EACH ELONGATED HOLES. FABRICATED AND INSTALLED NEW ANGLE IAW BAC DWG 69 37402 AND 65 45875.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 50,628 hrs · 28,751 cycles

MAIN CABIN STA 312 LBL 12 RBL 20 FLOORBEAM HAS CORROSION ON TEE CAP. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW B73753 10 51 FIG 101 (SHEET 11 OF 16). REMOVED AND REPLACED UPPER CHORD IAW B737 SRM 53-10-51 FIG 2D (SHEET 1 4).

Part: FRAME — CRACKED (BS 380) · airframe 50,628 hrs · 28,751 cycles

MAIN CABIN STA 380 RT AT STR 8 & 9 FRAME HAS CRACK AT OVERHEAD BIN BRACKET HOLE. REMOVED DAMAGE AREA NOT VERIFIED CRACK CONTAINED IAW 737 NOT MANUAL PART 6 CH 51-00-00 FIG 23. REPAIRED AREA IAW SRM 53-00-7 FIG 201 B737 400.

Part: FRAME — CRACKED (BS 400) · airframe 50,628 hrs · 28,751 cycles

MAIN CABIN STA 400 BETWEEN STR 8R AND 9R FRAME CRACKED AT HAT BIN ATTACH BRACKET POINT. REMOVED DAMAGED AREA IAW B737 400 SRM 57 00 7 NDT VERIFIED NO CRACK. IAW B737 NOT MANUAL PART 6 CH 51-00-00 FIG 23. FABRICATED AND ATTACHED REPAIR PARTS IAW B737 400 SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,628 hrs · 28,751 cycles

MAIN CABIN STA 440 BETWEEN STR 8R AND 9R FRAME CRACKED AT HAT BIN ATTACH BRACKET POINT. CUT OUT DAMAGE AREA IAW SRM 53-00-7 NOT VERIFIED CRACKED CONTAINED IAW 737 NDT MANUAL PART 6 CH 51 00 00 FIG 23. REPAIRED IAW B737 400 SRM 53-00-7 DETAIL II.

Part: ATTACH ANGLE — CRACKED (BS 278-293) · airframe 50,628 hrs · 28,751 cycles

MAIN FRAME AT FWD SERVICE DOOR CUTOUT BS 294 BETWEEN STR 10R AND 11R ANGLE CRACKED AT AFT END LWR SIDE OF INTERCOSTAL. REMOVED AND REPLACED ANGLE P/N 65 45807.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,628 hrs · 28,751 cycles

MAIN CABIN AT FWD SERVICE DOOR CUTOUT BS 277 BETWEEN STG 14R HAS CRACK AT FWD END OF INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL IAW BAC 737 400 SRM 51-40-2.

Part: INTERCOSTAL — CRACKED (BS 294) · airframe 50,628 hrs · 29,751 cycles

MAIN CABIN AT FWD SERVICE DOOR CUTOUT BS 294 BETWEEN STR 11R AND 12R HAS CRACK IN AFT END OF INTERCOSTAL ANGLE. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE IAW B737 SRM 51-40-2 AND BAC DWG 65 45007.

Part: ATTACH ANGLE — CRACKED (BS 294) · airframe 50,628 hrs · 28,751 cycles

MAIN CABIN AT FWD SERVICE DOOR CUTOUT BS 294 BETWEEN STR 12R AND 13R CRACK IN AFT END OF INTERCOSTAL ANGLE. REMOVED AND REPLACED ANGLE IAW B737 400 SRM 51-40-2 AND BAC DWG 65 45807.

Part: WEB — CRACKED (BS 294) · airframe 50,628 hrs · 28,751 cycles

FWD MAIN CABIN STA 294 STG 11L WEB CRACKED. REMOVED AND REPLACED INTERCOSTAL WEB IAW BAC DWG 65 17684 PEMCO EA PD 37 53 987 AND ALASKA EA 5310 02747.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,628 hrs · 28,751 cycles

MAIN CABIN CUSP WEB ANGLE AT BOTTOM OF RI DOOR CUTOUT STA 277 318 HAS CORROSION. REMOVED AND REPLACED CUSP WEB ANGLE IAW 737 400 SRM 51-40-2, 51-40-5 AND 53-10-15 FIG 101 SHT 13.

Part: INTERCOSTAL — CRACKED (BS 294) · airframe 50,628 hrs · 28,751 cycles

FWD SIDE OF L1 DOOR CUTOUT STR 16L BS 294 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW BAC DWG 65 17684 PEMCO EA PD 37 53 987 AND ALASKA EA 5310 02747.

Part: INTERCOSTAL — CRACKED (BS 294) · airframe 50,628 hrs · 28,751 cycles

MAIN CABIN AT FWD SERVICE DOOR CUTOUT BS 294 BETWEEN STG 9R AND 10R HAS CRACK AT AFT END OF INTERCOSTAL ANGLE. REMOVED AND REPLACED INTERCOSTAL ANGLE IAW BAC DWG 65 45807 AND 51 40 1 BOEING 737 400 SRM.

Part: ATTACH FITTING — CRACKED (BS 294-303) · airframe 50,628 hrs · 28,751 cycles

FWD SIDE OF L1 DOOR CUTOUT STR 11L BS 294 ATTACH CLIP CRACKED. REMOVED AND REPLACED ATTACH CLIP IAW BAC DWG 66 14210 PEMCO EA PD 37 53 987 AND ALASKA EA 5310 02747.

Part: INTERCOSTAL — CRACKED (BS 294) · airframe 50,628 hrs · 28,751 cycles

FWD SIDE OF L1 DOOR CUTOUT STR 12L BS 294 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW PEMCO EA PD 37 53 987 AND ALASKA EA 5310 02747.

Part: INTERCOSTAL — CRACKED (BS 294-303) · airframe 50,628 hrs · 28,751 cycles

FWD SIDE OF L1 DOOR CUTOUT STR 7L BS 294 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW BAC DWG 65 17684 PEMCO EA PD 37 53 987 AND ALASKA EA 5310 02747.

Part: ANGLE — CORRODED (BS 312-332) · airframe 50,628 hrs · 28,751 cycles

MAIN CABIN STA 312 - 332 LBL 56 SHEAR WEB ANGLE HAS CORROSION. REMOVED CORROSION. ORIGINAL MAT'L .090 REMOVED .028. BEYOND SERVICE LIMITS. REPLACED SHEAR WEB ANGLE IAW B737 400 SRM 51-40-02 & BAC DWG 65 17688.

Part: SKIN — DENTED (BS 1032) · airframe 49,900 hrs · 28,362 cycles

DENT ON EMPENNAGE SKIN AT STA 1032 BETWEEN STRINGERS 25L AND 24L, 2.5 INCHES FROM LAP SEAM RIVET ROW. REPAIRED SKIN IAW ASA EA 5330 02216, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER.

Part: SKIN — DAMAGED (RT AILERON) · airframe 49,900 hrs · 28,362 cycles

RT AILERON IS DAMAGED AT FWD SPAR UPPER SKIN. REPAIRED AILERON IAW SRM 51-70-17 REPAIR 7 AND ASA EA 5750 02373.

Part: FRAME — CRACKED · airframe 49,900 hrs · 28,362 cycles

R1 DOOR SURROUND STRUCTURE FWD STUB FRAME CRACKED 3/4 WAY UP IN O/B FLANGE RADIUS. REMOVED R1 STUB FRAME, FABRICATED, TREATED & PRIMED, TOPCOATED AND INSTALLED NEW STUB FRAME IAW SRM 51-30-01, 51-40-02 AMM 51-21-21 PG 704 & 706 AND ASA EA 5210 01133.

Part: SKIN — DELAMINATED · airframe 49,900 hrs · 28,362 cycles

RT AILERON CONTROL TAB HAS DELAM DAMAGE AT TRAILING EDGE I/B CORNER. REPAIRED RT AILERON TAB IAW SRM 51-70-16 PG 12 REPAIR 1.

Part: GIRT BAR — CORRODED (L2 DOOR SLIDE) · airframe 49,900 hrs · 28,362 cycles

L2 DOOR SLIDE GIRT BAR CORRODED AND PITTED. REMOVED FROM SLEEVE PER TC 45125011. REMOVED AND REPLACED L2 DOOR SLIDE GIRT BAR PER CMM 25-66-07 PG 664 STEPS 14 (A, B, C AND D).

Part: FRAME — GOUGED · airframe 49,900 hrs · 28,362 cycles

AFT CARGO DOOR AFT FRAME REPAIR IS GOUGED. REPAIRED FRAME IAW ASA EA 5310 02725.

Part: FLAP TRACK — WORN (NR 4 FLAP) · airframe 49,900 hrs · 28,362 cycles

NR 4 FLAP TRACK SIDE LOAD LINK LOOSE. REMOVED AND REPLACED NR 4 FLAP TRACK SIDE LOAD LINK IAW AMM 27-51-27 STEP 5D (2) (B) PG 411 AND AMM 20-50-11.

Part: SKIN — DELAMINATED (RIGHT AILERON) · airframe 49,900 hrs · 28,362 cycles

RIGHT AILERON LOWER SURFACE IS SEPARATING. REPAIRED RIGHT AILERON LOWER SURFACE DAMAGE IAW SRM 51-70-03 REPAIR 6 PG 16.

Part: SKIN — DELAMINATED (RT AILERON) · airframe 49,900 hrs · 28,362 cycles

RIGHT AILERON FWD SPAR IS SEPARATING AT I/B UNDER LWR SURFACE. REPAIRED RIGHT AILERON I/B LWR SURFACE DAMAGE IAW SRM 51-70-03 REPAIR 6 PG 16 AND EA 5760 01011.

Part: SKIN — DELAMINATED (RIGHT AILERON) · airframe 49,900 hrs · 28,362 cycles

RIGHT AILERON I/B FWD UPPER SURFACE PANEL IS SEPARATING AT EDGE. REPAIRED RIGHT AILERON UPPER SURFACE DAMAGE IAW SRM 51-70-03 REPAIR 6 PG 16.

Part: WEB — CORRODED (BS 807-847) · corrosion level 2 · airframe 49,900 hrs · 28,362 cycles

AFT CARGO DOOR SILL WEB HAS AREAS OF CORROSION. REMOVED DAMAGED WEB SILL LOCATED AND DRILLED NEW SILL AND INSTALLED IAW SRM 51-40-02, 51-10-02 AND SOPM 20 41 05.

Part: SKIN — DENTED (FUSELAGE) · airframe 49,900 hrs · 28,362 cycles

FUSELAGE SKIN IS DENTED OVER A STRINGER AND IN ADJACENT BAYS. CUT OUT DAMAGED AREA OF SKIN FABRICATED AND INSTALLED REPAIR FILLER DOUBLER AND TRIPLER IAW SRM 53-00-01 FIG 201 REPAIR 31.

Part: OVEN — ODOR (NR 1 GALLEY) · airframe 48,641 hrs · 27,598 cycles

FWD GALLEY OVEN CAUSES STRONG ELEC ODOR AND TRIPS GALLEY PWR. DEFERRED OVENS INOP COLLARDED CB'S PER MEL.

Part: FRAME — CORRODED (BS 794) · airframe 46,167 hrs · 26,242 cycles

AFT CARGO DOOR CUTOUT FWD FRAME HAS CORROSION ON FRAME AND WEB. REPLACED FRAME PER SRM 51 40 02.

Part: SHEAR TIE — CORRODED (BS 500C) · corrosion level 2 · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON SHEAR TIE. REMOVED CORROSION FOUND OUT OF LIMITS. REPLACED SHEAR TIE PER SRM 53 00 07 FIG 201 REPAIR 3.

Part: SKIN — DAMAGED (BS 867-937) · airframe 46,167 hrs · 26,242 cycles

FOUND FUSELAGE SKIN DAMAGED, REPAIRED PER EA 5330 02079.

Part: FRAME — CORRODED (BS 589) · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON LWR EDGE FRAME UNDER PRESSURE SEAL ON RT FWD OVER WING EXIT. REPAIRED PER EA 5220 01012.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON LT AFT EMERGENCY EXIT HATCH ON LWR EDGE FRAME UNDER PRESSURE SEAL. REPAIRED LT AFT EMERGENCY EXIT HATCH LOWER EDGE FRAME UNDER PRESSURE SEAL IAW EA 5220 01013.

Part: FRAME — CRACKED (NR 2 PYLON) · airframe 46,167 hrs · 26,242 cycles

NR 2 ENGINE PYLON CRACK IN FRAME. REPAIRED PER EA 5440 01050 AND ER 06 1834.

Part: DOOR FRAME — CHAFED (BS 795) · airframe 46,167 hrs · 26,242 cycles

AFT CARGO DOOR FWD LWR FRAME IS CHAFED. REMOVED AND REPALCED FWD LWR CARGO DOOR FRAME ON AFT CARGO DOOR PER SRM 51 40 02.

Part: SHEAR TIE — CORRODED (BS 500C S26-27R) · corrosion level 2 · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON SHEAR TIE. REMOVED CORROSION FOUND OUT OF LIMITS REPAIRED SHEAR TIE PER SRM 53 00 07 FIG 201 REPAIR 3.

Part: FAILSAFE — CORRODED (BS 787 FRAME) · corrosion level 2 · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON FAILSAFE. REMOVED AND REPLACED FAILSAFE PER SRM 51-40-02.

Part: STRINGER — CORRODED (BS 445-480 S28L) · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON STRINGER AROUND FASTENERS. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53 00 03.

Part: SHEAR TIE — CORRODED (BS 500C S28L-28R) · corrosion level 2 · airframe 46,167 hrs · 26,242 cycles

FOUND SHEAR TIE CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS. REPAIRED SHEAR TIE PER SRM 53 00 07 FIG 201 REPAIR 3.

Part: FRAME — CORRODED (BS 787) · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON FRAME. REPAIRED DAMAGED PER SRM 51 70 11.

Part: SHEAR TIE — CORRODED (BS 460 S28L-28R) · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON AFT SIDE OF SHEAR TIE REPAIR DOUBLER. REMOVED AND REPAIRED PER SRM 53 00 07.

Part: FRAME — CORRODED (BS 500A S27-28R) · airframe 46,167 hrs · 26,242 cycles

FOUND FRAME SHEAR TIE CORRODED. REPAIRED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (BS 500C) · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON SHEAR TIE. REMOVED CORROSION FOUND OUT OF LIMITS. REPAIRED SHEAR TIE PER SRM 53 00 07 FIG 201 REPAIR 3.

Part: DOOR FRAME — CORRODED (BS 794-847) · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON AFT CARGO DOOR CUTOUT LOWER CHORD. REMOVED AND REPLACED PER EA 5310 02613.

Part: SHEAR TIE — CORRODED (BS 500C) · corrosion level 2 · airframe 46,167 hrs · 26,242 cycles

FOUND SHEAR TIE CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS. REPAIRED SHEAR TIE PER SRM 53 00 07 FIG 201 REPAIR 3.

Part: ANGLE — CORRODED (BS 827) · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON AFT CARGO DOOR OPENING SUB THRESHOLD ANGLE. REMOVED CORROSION FABRICATED REPAIR PARTS INSTALLED REPAIR PER SRM 51 40 02.

Part: SHEAR TIE — CORRODED (BS 500C) · corrosion level 2 · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON SHEAR TIE. REMOVED CORROSION FOUND OUT OF LIMITS. REPAIRED SHEAR TIE PER SRM 53 00 07 FIG 201 REPAIR 3.

Part: SHEAR TIE — CORRODED (BS 460 S28RL) · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON AFT SIDE OF SHEAR TIE REPAIR DOUBLER. REMOVED AND REPAIRED PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON SHEAR TIE. REMOVED DAMAGED SECTION OF SHEAR TIE FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53 00 07.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,167 hrs · 26,242 cycles

FOUND SHEAR TIE CORRODED. REMOVED DAMAGED SHEAR TIE FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53 00 07.

Part: STRINGER — DAMAGED (BS 878) · airframe 46,167 hrs · 26,242 cycles

FOUND STRINGER DAMAGED. REMOVED AND REPLACED STRINGER WITH NEW ITEM PER SRM 53 00 03 REPAIR 1.

Part: SHEAR TIE — CORRODED (BS 500B) · corrosion level 2 · airframe 46,167 hrs · 26,242 cycles

FOUND SHEAR TIE CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS REMOVED FABRICATED AND INSTALLED FRAME REPAIR PER SRM 53 00 07 FIG 201.

Part: SHEAR TIE — CORRODED (BS 500B) · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON FRAME SHEAR TIE. REMOVED AND REPLACED SHEAR TIE PER SRM 53 00 07 REPAIR 3.

Part: SHEAR TIE — CORRODED (BS 500D) · airframe 46,167 hrs · 26,242 cycles

FOUND SHEAR TIE CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS REPAIRED FABRICATED AND INSTALLED FRAME PER SRM 53 00 07 FIG 201.

Part: SHEAR TIE — CORRODED (BS 460) · airframe 46,167 hrs · 26,242 cycles

FOUND CORROSION ON FRAME SHEAR TIE. REMOVED CORROSION FOUND OUT OF LIMITS REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PER SRM 53 00 07 FIG 201.

Part: SHEAR TIE — DAMAGED (BS 907) · airframe 46,167 hrs · 26,242 cycles

FOUND SHEAR TIE HAS OBLONG HOLE. REMOVED AND REPLACED SHEAR TIE PER SRM 51 40 02.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 46,167 hrs · 26,242 cycles

FOUND STRINGER DAMAGED. REPAIRED PER SRM 53 00 03 FIG 201 REPAIR 1.

Part: SHEAR TIE — DAMAGED (FUSELAGE)

FOUND SHEAR TIE DAMAGED. REMOVED AND REPAIRED PER SRM 53 00 07 REPAIR 1.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 46,167 hrs · 26,242 cycles

FOUND SHEAR TIE DAMAGED. REMOVED AND REPAIRED PER SRM 53 00 07 REPAIR 1.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 46,167 hrs · 26,242 cycles

FOUND SHEAR TIE DAMAGED. REMOVED AND REPAIRED PER SRM 53 00 07 REPAIR 1.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 46,167 hrs · 26,242 cycles

AFT CARGO DOOR CUTOUT FWD FRAME HAS CORROSION JUST O/B OF CARGO LIGHT SWITCH AND IN 2 O/B THRESHOLD FASTENER HOLES. REMOVED CORROSION AND REPAIRED FRAME SEGMENT PER SRM 51 40 02 FIG 8.

Part: CARGO TRACK — CORRODED (FS 787)

SEA - FOUND AFT CARGO PIT TIE DOWN TRACK CORRODED AT THRESHOLD AREA. REMOVED AND REPLACED AFT CARGO PIT RT TIE DOWN TRACK IAW B737-400 SRM 53-00-53, FIG 201. (M)

Part: TAB — BROKEN (ELEVATOR)

RT ELEVATOR TAB OB FWD LWR CORNER HAS EDGE DAMAGE. REMOVED DAMAGED ELEVATOR TAB, ORDERED AND REPLACED ELEVATOR TAB IAW AMM. (K)

Part: WEDGE — DENTED (TE FLAP)

OKC - FOUND RIGHT INBOARD TE MID FLAP WEDGE DENTED WITH A CRACK. REMOVED DAMAGE FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW B737 SRM 51-70-10. (M)

Part: SKIN — DELAMINATED (NR 3 SLAT)

OKC - FOUND LEFT WING NR 3 L/E SLAT T/E WEDGE IS DELAMINATED AT INBOARD AND OUTBOARD ENDS WITH EDGE POTTING DETERIORATED. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR CORES AND DOUBLERS IAW B737 SRM.

Part: SKIN — DENTED (FUSELAGE)

OKC - FOUND RIGHT EXIT FUSELAGE SKIN HAS SEVERAL AREAS OF DAMAGE, FS 1007-1010 BETWEEN STRINGER 12R AND 14R CREASE AT FS 1010 AND DENT AT STATION 1007. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED A REPLACEMENT SKIN PANEL IAW AS EA 5330-01905 AND AAR EA 10857. (M)

Part: WEDGE — DELAMINATED (NR 2 SLAT)

OKC - FOUND LEFT WING NR 2 L/E NR 2 SLAT T/E WEDGE IS DELAMINATED AT OUTBOARD END AND EDGE POTTING DETERIORATED AT THE INBOARD END. REMOVED DAMAGE FABRICATED AND INSTALLED A REPAIR CORE AND DOUBLER IAW B737 SRM 51-70-10 REPAIR 7. (M)

Part: WEDGE — DELAMINATED (NR 4 SLAT)

OKC - FOUND RIGHT WING NR 4 L/E SLAT INBOARD SIDE OF TRAILING EDGE WEDGE HAS SLIGHT DELAMINATION AND INBOARD AND OUTBOARD EDGE POTTING IS DETERIORATED. REMOVED DAMAGE FABRICATED AND INSTALLED A REPAIR CORE AND DOUBLER IAW B737 SRM 51-70-10 REPAIR 7. (M)

Part: WEDGE — DENTED (TE FLAP)

OKC - FOUND LEFT INBOARD TRAILING EDGE FLAP HAS SEVERAL DENTS. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 51-70-10 PAGE 8. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

OKC - FOUND RIGHT STRINGER 11R AT BS 1007 STRINGER CLIP IS CRACKED. REMOVED DAMAGED STRINGER CLIP, ORDERED AND INSTALLED A NEW STRINGER CLIP IAW B737 SRM. (M)

Part: STRINGER CLIP — CRACKED (FUSELAGE)

OKC - FOUND RIGHT STRINGER 12R AT BS 1007 STRINGER CLIP IS CRACKED. REMOVED DAMAGED STRINGER CLIP, ORDERED AND INSTALLED A NEW STRINGER CLIP IAW B737 SRM. (M)

Part: SKIN — DENTED (NR 6 L/E SLAT)

PAE - NR 6 SLAT TRAILING EDGE HAS A DENT. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM, REPAIR 21. (K)

Part: WIRE — EXPOSED (CABIN)

ANC - FOUND FLOOR TRACK LIGHTING WIRING COMPLETELY EXPOSED AND DISCONNECTED AT ROWS 9-10. RECONNECTED WIRING AND INSTALLED PROTECTIVE COVER ON TRACK ROWS 9-10. OPS CHECK GOOD. (M)

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT)

FAI - FOUND FLOOR TRACK LIGHTING AT ROW 15 COVER DISLODGED CAUSING ONE SECTION OF WHITE LIGHTS TO FAIL. RECONNECTED WIRES AND REPLACED PROTECTIVE COVER AS REQUIRED. (M)

Part: WEB — GOUGED (FS)

GYR - AFT CARGO PIT DOOR SILL SUPPORT WEB HAS TOOLING MARKS ON OUTBOARD SIDE. REPLACED WEB PER SRM 53-60-15. (M)

Part: SKIN — GOUGED (FUSELAGE)

GYR - FOUND FUSELAGE SKIN DENT/GOUGED AT BS 847 BETWEEN S-24R AND S-25R. REPAIRED IAW EA 5330-01688. (M)

Part: SKIN — CHAFED (NR 1 PYLON)

GYR - NR 1 PYLON SKIN CHAFED OUTBOARD SIDE AT WING INTERFACE. REPAIRED NR 1 PYLON OUTBOARD SKIN IAW ASA EA 5430-01128. (M)

Part: SKIN — WORN (NR 2 PYLON)

GYR - NR 2 PYLON SKIN WORN INBOARD SIDE 22-30 INCHES FORWARD OF MIDSPAR FITTING. REPAIRED NR 2 PYLON INBOARD SKIN IAW ASA EA 5430-01128. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND STATION 344 LBL 12 TO LBL 24 FLOORBEAM HAS CORROSION TOP AND BOTTOM SIDES. REPAIRED PER SRM 51-70-12 FIG 1. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND CORROSION ON UPPER T-CAP FLOORBEAM. REPAIRED IAW ASA EA 5310-02310. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

GYR - FOUND AFT PIT, CORROSION ON SKIN DOUBLER STATION 1006. REPAIRED IAW EA 5330-1743. (M)

Part: ANGLE — CORRODED (R1 DOOR)

GYR - FOUND R-1 DOOR 'L' ANGLE HAS CORROSION THE FULL LENGTH OF THE ANGLE. REMOVED AND REPLACED THE 'L' ANGLE PER SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND STATION 360 RBL 39 TO RBL 55 FLOORBEAM HAS CORROSION TOP AND BOTTOM AROUND SCREW HOLES, GALLEY AND SEAT TRACK FITTINGS. REMOVED CORROSION AND CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-51. FABRICATED 2 AND 3 AND FILLER PARTS PER SRM 53-30-51 AT STATION 360, RBL 89 TO RBL 55. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND FLOORBEAM HAS SCREW HOLES WITH CORROSION. REPAIRED FLOORBEAM IAW SRM 53-10-01. (M)

Part: FLAP TRACK — CORRODED (T/E FLAP)

GYR - NR 2 FLAP TRACK HAS PITTING ON LOWER SIDE OF THE UPPER TRACK. REPLACED FLAP TRACK FITTING PER AMM 27-51-49. (M)

Part: SKIN — CHAFED (LT PYLON)

GYR - FOUND LEFT ENGINE PYLON OUTBOARD SKIN CHAFFED AT WING INTERFACE. REPAIRED IAW EA 5430-01128. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

GYR - FOUND STATION 376, RBL 11, FLOOR SUPPORT SCREW HOLE HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT STATION 376, RBL 11, IAW SRM 51-40-02. (M)

Part: SKIN — WORN (NR 2 PYLON)

GYR - NR 2 PYLON SKIN WORN OUTBOARD SIDE 22-30 INCH FORWARD OF MIDSPAR FITTING. REPAIRED NR 2 PYLON SKIN OUTBOARD IAW ASA EA 5430-01128. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND FLOORBEAM HAS CORROSION AT STATION 294.5 TOP AND BOTTOM SIDES. REPAIRED IAW SRM 53-10-51 FIG 205. (M)

Part: SKIN — TORN (RUDDER)

GYR - UPON RUDDER REMOVAL FOUND DAMAGE TO UPPER SKIN OF RUDDER BALANCE ARM. REPAIRED IAW ASA EA 5540-01086. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

SEA - DURING SERVICE CHECK, FOUND SECTION 1 NEAR ROW 1 FLOOR TRACK LIGHTING INOPERATIVE. REATTACHED LOOSE CONNECTION, SYSTEM OPERATIONAL CHECKED GOOD. (M)

Part: SKIN — DENTED (CARGO DOOR)

DURING C-CHECK, FOUND AFT CARGO DOOR SKIN REQUIRES REPLACEMENT. REPAIRED IAW SRM. (M)

Part: ANGLE — CRACKED (NR 1 PYLON)

DURING C-CHECK, NR 1 PYLON CRACKED L ANGLE AT INBOARD END OF FAIRING STIFFENER. REPAIRED IAW SRM. (M)

Part: SHROUD — CHAFED (APU BAY)

DURING C-CHECK, FOUND APU SHROUD SKIN CHAFED. REPAIRED IAW EA. (M)

Part: ANGLE — CRACKED (RT WING)

PAE - DURING C-CHECK, FOUND RIGHT WING TRAILING EDGE HAS A CRACKED ANGLE AT RSS 545. REPAIRED IAW SRM. (M)

Part: SKIN — LIGHTNING STRIKE (FUSELAGE)

PAE - DURING C-CHECK, FOUND LIGHTNING STRIKES ON FUSELAGE SKIN AT BS 273.5, 360, 447 AND STRINGERS 2L AND 3L AND 76. REPAIRED IAW SRM. (M)

Part: CHANNEL — CRACKED (PYLON)

PAE - DURING C-CHECK, FOUND PYLON PANEL NR 5836 SUPPORT CHANNEL IS CRACKED. REPAIRED IAW SRM. (M)

Part: STIFFENER — WORN (T/E FLAP)

PAE - DURING C-CHECK, FOUND RIGHT MID FLAP PYLON CUTOUT STIFFENER ARE WORN. REPAIRED IAW SRM. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTING AT ROW 18 INOPERATIVE. RECONNECTED WIRE, OPERATIONAL CHECKED NORMAL. (M)

Part: WIRE — LOOSE (CABIN)

PDX - DURING LINE CHECK, FOUND FLOOR TRACK LIGHTS INOPERATIVE AT ROW 20. RECONNECTED LOOSE WIRES OPERATIONAL CHECK NORMAL. (M)

Part: WEB — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION ON SUB THRESHOLD WEB BS 795-847 AND RBL 18 AFT CARGO BAY. REMOVED AND REPLACED WEB IAW SRM. (M)

Part: ROLLER — BROKEN (SLIDING WINDOW)

SFO - DURING LINE CHECK, FOUND FIRST OFFICERS SLIDING FORWARD WINDOW ROLLER BROKEN. REMOVED WINDOW AND REMOVED AND REPLACED LOWER TRACK ROLLER, REINSTALLED WINDOW, OPERATIONS CHECK NORMAL. (M)

Part: HINGE — LACK OF LUBE (L1 DOOR)

SEA - BEFORE FLIGHT, FLIGHT ATTENDANT REPORTED L1 DOOR DIFFICULT TO OPEN. LUBED DOOR AND HINGE POINTS, OPERATIONAL CHECK NORMAL. (M)

Part: SKIN — DAMAGED (FUSELAGE)

SEA-DURING SCHEDULED 'C' CHECK THE LOWER FUSELAGE BELLY WAS FOUND TO BE CREASED ALONG STA 460 RIVET LINE STRINGER 27R TO 25L. REPAIRED PER SRM.

Part: SKIN — DAMAGED (CROWN)

SEA DURING SCHEDULED 'C' CHECK THE FUSELAGE SKIN ON CROWN STA 860, STRINGER 1L, HOLE UNDER DORSAL FIN. REPAIRED PER EA 5330-01461.

Part: SKIN — DAMAGED (FUSELAGE)

SEA-DURING SCHEDULED 'C' CHECK THE LOWER FUSELAGE BELLY WAS FOUND TO BE CREASED ALONG STA 480 RIVET LINE BELOW THE FORWARD CARGO DOOR CUTOUT FROM STRINGER 27L TO 26R. REPAIRED PER SRM.

Part: LATCH — INOPERATIVE (PAX DOOR)

ANC - DURING MAINTENANCE CHECK, THE FORWARD ENTRY DOOR HOLD OPEN LATCH WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED AND RELEASED PER MEL 52-7B. MAINTENANCE SUBSEQUENTLY CLEANED AND LUBRICATED THE LATCH ASSEMBLY, THE HOLD OPEN LATCH OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 13-16 WERE FOUND TO BE INOPERATIVE. RECONNECTED LOOSE WIRING/CONNECTOR AND LIGHTS OPERATED NORMALLY. (M)

Part: CONNECTOR — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 19 WERE FOUND INOPERATIVE. RECONNECTED DISCONNECTED CONNECTOR AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (ROW 13)

GEG - PRIOR TO FLIGHT 570, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 13. RECONNECTED WIRING AT ROW 13 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT SEVERAL LOCATIONS. RELAMPED 2 EACH LIGHTS AND REPAIRED WIRING TO FLOOR TRACK LIGHTS, LIGHTS OPERATED NORMALLY. (X)

Part: RELEASE ASSY — FAILED (R1 DOOR)

PDX - DURING MAINTENANCE CHECK, THE R1 DOOR HOLD OPEN LEVER ASSY WAS FOUND TO NOT HOLD THE DOOR IN THE OPEN POSITION, AND WOULD NOT LOCK. REPLACED LEVER ASSEMBLY AND DOOR HOLD OPEN OPERATED NORMALLY. (M)

Part: COLLAR — LOOSE (PAX DOOR)

SEA - PRIOR TO FLT 179, THE R1 DOOR WAS FOUND TO BE STUCK OPEN. FOUND COLLAR LOOSE. REINSTALLED COLLAR AND DOOR OPERATED NORMAL. (M)

Part: BATTERY — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT DOOR EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. REPLACED THE BATTERY AND BATTERY CHARGER AND LIGHTS OPERATED NORMALLY. (M)

Part: CHARGER — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT DOOR EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. REPLACED THE BATTERY AND BATTERY CHARGER AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHT — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD TWO RED EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M)

Part: LIGHTS — INOPERATIVE (CABIN)

SEA - PRIOR TO FLT 330, SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN THE AFT CABIN AREA. REPLACED WIRING HARNESS AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

PDX - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: GUIDE ARM ROLLER — INOPERATIVE (L-2 DOOR)

SIT - FLT 72 - PRIOR TO DEPARTURE, RAMP PERSONNEL REPORTED THE L-2 DOOR WOULD NOT LATCH IN THE HOLD OPEN POSITION. FERRIED AIRCRAFT TO SEA. REPLACED THE UPPER GUIDE ARM ROLLER ASSEMBLY AND THE DOOR OPERATED NORMALLY IN THE HOLD OPEN POSITION. (M)

Part: BATTERY PACKS — DISCHARGED (CABIN)

SEA - DURING MAINTENANCE CEHCK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 11, 14, 15 AND 18. REPLACED BATTERY PACKS AT ROWS 11,14, AND 18 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE THREE FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROW 3 AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED TRACK WIRING IN AFT CABIN AND LIGHTS OPERATED NORMALLY. (W)

Part: DOOR MECHANISM — LACK OF LUBE (FWD CABIN)

SEA - L1 DOOR BINDS ON CLOSING. MAINTENANCE LUBED TOP HINGE AND OPS CHECKED NORMAL. (Z)