N760AS

Part: FRAME — CRACKED (BS 500F) · airframe 73,107 hrs · 42,063 cycles

FS 500F IS CRACKED AT WIRE PENETRATION HOLE BELOW STR 20L. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07-2R-13. THIS IS A CAT B REPAIR WITH A THRESHOLD OF 66000 CYCLES AND AN INTERVAL OF 24,000 CYCLES. CYCLES AT TIME OF REPAIR 42.063.

Part: FRAME — CRACKED (BS 500B) · airframe 73,107 hrs · 42,063 cycles

FS 500B IS CRACKED AT WIRE PENETRATION HOLE BELOW STR 20L. ACFT GROUNDED. REPAIRED FRAME IAW SRM 53-00-07-2R-13. THIS IS A CAT B REPAIR WITH A THRESHOLD OF 66000 CYCLES AND AN INTERVAL OF 24,000 CYCLES. CYCLES AT TIME OF REPAIR 42,063.

Part: SUPPORT FITTING — CRACKED (RT MLG) · airframe 73,107 hrs · 42,063 cycles

RIGHT WING LANDING GEAR BEAM SUPPORT FITTING CRACKED AT UPPER FASTENER HOLE 4TH FROM INBD. ACFT GROUNDED. ACCOMPLISHED INSPECTIONS TO RT MLG BEAM AFT SUPPORT FITTING IAW EA NR 400-57EA-17060. THIS IS A CATEGORY C REPAIR RT WING MLG BEAM AFT SUPPORT FITTING MUST BE R & R BEFORE ACFT REACHES 54,063 ACFT TOTAL FLT CYCLES. REFER TO EL TYPE EA 400-573A-17061 FOR FITTING R & R.

Part: SKIN — CRACKED (BS 294-280) · airframe 73,107 hrs · 42,063 cycles

FUSELAGE SKIN IS CRACKED AT THE R1 DOOR LOWER HINGE CUTOUT NDT HAS VERIFIED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN IAW 53-10-01-2R-15. THIS IS A CAT B REPAIR WITH AN INSPECTION THRESHOLD OF 60000 TOTAL FLT CYCLES OR 3,000 FLT CYCLES FROM INSTALLATION OF REPAIR. TOTAL FLT CYCLES AND HRS AT TIME OF REPAIR 42,063 CYCLES 73,106: 32 HRS, FOR INTERVAL AND METHOD, REF D6-38669.

Part: RIB — CRACKED (RT WING) · airframe 73,107 hrs · 42,063 cycles

RT WING RT WS 135 RIB CHORD CRACKED. ACFT GROUNDED. REPAIRED RT WS 135 RIB CHORD IAW EA 400-57EA-17072.

Part: SKIN — DELAMINATED (NR 3 SLAT) · airframe 73,107 hrs · 42,063 cycles

NR 3 SLAT OTBD LOWER T/E DELAMINATED. ACFT GROUNDED. BONDED PERMANENT REPAIR TO NR 3 SLAT, OTBD LOWER T/E DELAMINATION IAW BOEING SRM 51-70-10-2R-4, REPAIR NR 4.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 72,652 hrs · 41,774 cycles

F/A REPORTED THAT EXIT SIGN ROW 16 DEF FELL DOWN DURING FLIGHT/IS NOT SECURE. ACFT GROUNDED. R & R EXIT SIGN ASSY ON WALL OF ROW 16 DEF AS REQUIRED. OPS CHECKED GOOD, IAW AMM 33-51-11.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 72,212 hrs · 41,473 cycles

F/A REPORTS EMERGENCY EXIT LIGHT COVER MISSING AT ROW 17 RT SIDE. ACFT GROUNDED. INSTALLED NEW EMERGENCY EXIT LIGHT COVER.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 71,062 hrs · 40,718 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER FELL OFF. ACFT GROUNDED. REPLACED L1 DOOR EMERGENCY EXIT LIGHT ASSY IAW WDM 33-51-12. OPS TEST NORMAL.

Part: SKIN — GOUGED (BS 516-540) · airframe 70,893 hrs · 40,614 cycles

LEFT FUSELAGE SKIN AT GROUND A/C DOOR CUTOUT IS GOUGED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AT AC DOOR CUTOUT IAW SRM 53-30-01-2R-2. THIS IS A CATEGORY B REPAIR WITH INSPECTION THRESHOLD OF 30,000 FLT CYCLES, FLT CYCLES AFTER REPAIR WITH INSPECTION INTERVAL, FLT CYCLES OF 30,000, FLT CYCLES AT TIME OF REPAIR 40,614.

Part: ANGLE — CORRODED (BS 545) · corrosion level 2 · airframe 70,893 hrs · 40,614 cycles

KEEL BEAM INTERIOR AFT ANGLE CORRODED, FWD ACCESS AREA AFT OF ROTATING BEACON. ACFT GROUNDED. REMOVED CORRODED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-12-1A-1 DETAIL 7. REMOVED ANGLE FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-40-05-0G-0 AND 51-40-02-0G-0.

Part: DOUBLER — CORRODED (BS 539-543) · corrosion level 2 · airframe 70,893 hrs · 40,614 cycles

LOWER ROTATING BEACON ATTACH DOUBLER CORRODED, INSIDE KEEL BEAM FWD ACCESS AREA. ACFT GROUNDED. REMOVED CORRODED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-12-1A-1, DETAIL 7. REMOVED DOUBLER FABRICATED NEW DOUBLER AND INSTALLED IAW SRM 51-40-05-0G-0 AND 51-40-02-0G-0, W 1, O .050, R 0, L 7.0, D .050.

Part: SKIN — GOUGED (BS 516-540) · airframe 70,893 hrs · 40,614 cycles

LT FUSELAGE SKIN AT GROUND, ACFT DOOR CUTOUT IS GOUGED. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AT ACFT DOOR CUTOUT IAW SRM 53-30-01-2R-2. THIS IS A CATEGORY B REPAIR WITH INSPECTION THRESHOLD OF 30,000 FLT CYCLES, FLT CYCLES AFTER REPAIR WITH INSPECTION INTERVAL FLT CYCLES OF 30,000, FLT CYCLES AT TIME OF REPAIR 40,614.

Part: CHANNEL — CORRODED (BS 986-1006) · corrosion level 2 · airframe 70,893 hrs · 40,614 cycles

AFT WASTE WATER DRAIN MAST CHANNEL IS CORRODED. ACFT GROUNDED. REPAIRED THE AFT WASTE WATER DRAIN MAST CHANNEL IAW EA 400, 53EA, 15136.

Part: SKIN — CRACKED (R2 DOOR) · airframe 70,893 hrs · 40,614 cycles

R2 DOOR CRACKED IN SKIN FWD LWR CORNER NDT VERIFIED. ACFT GROUNDED. REPAIRED R2 CRACKED FWD LOWER SKIN IAW SRM 53-00-01-2R-32, REPAIR 32. THIS REPAIR IS A CATEGORY B REPAIR AND REG INSPECTION WITH THRESHOLD OF 66000 AND INTERVAL OF 24000 FLIGHT CYCLES CURRENT A/C CYCLES 40164.

Part: FLOORBEAM — CRACKED (BS 710) · airframe 70,893 hrs · 40,614 cycles

FOUR CRACKS IN BBL 0.07 FLOORBEAM WEB LT SIDE AT BS 710.1. ACFT GROUNDED. REPAIRED BBL 0.07 FLOORBEAM WEB LT SIDE AT BS 710 IAW ASA T/C AD20080421-400-57-6.

Part: ARM — OUT OF ADJUST (L1 DOOR) · airframe 69,998 hrs · 40,093 cycles

L1 DOOR IS DIFFICULT TO LATCH CLOSE. ACFT GROUNDED. ADJUSTED L1 DOOR GUIDE ARM IAW MM 52-11-00-705-007 PG 2, STEPS 3H (1 AND 2).

Part: FLOOR PANEL — CRACKED (BS 500) · airframe 67,646 hrs · 38,751 cycles

DENT FOUND IN FWD CARGO BAY FLOOR PANEL AT APPROXIMATELY FS 500 WITH SMALL CRACK APPROX 1 INCH IN LENGTH. ACFT GROUNDED. FABRICATED NEW FLOOR PANEL IAW SRM 51-40-05-0G-0 AND 53-30-53-01-1.

Part: FRAME — CRACKED (BS 500F) · airframe 67,646 hrs · 38,751 cycles

FRAME BS 500F RT SIDE IS CRACKED AT 1 INCH WIRE PENETRATION HOLE EXTENDING INBD FROM EDGE OF HOLE APPROX .75" IN THE FWD CARGO BAY. ACFT GROUNDED. REPAIRED CRACKED FRAME IAW SRM 53-00-07-2R-13.

Part: STIFFENER — CORRODED (BS 1128) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

APU BAY INLET CUTOUT AFT OTBD ANGLE CORRODED FOUND DURING AFT STRAP REPAIR. ACFT GROUNDED. APU BAY INLET CUTOUT AFT OTBD ANGLE REMOVED. FABRICATED NEW AND INSTALLED IAW SRM 51-40-02-0G-0 AND 51-40-05-0G, 0 W, .6 O, .06 R, 0 L ,1" D .06.

Part: STRINGER — CORRODED (BS 1088-1129) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

APU INLET DUCT CUTOUT LOWER STRINGER CORRODED. ACFT GROUNDED. R & R STRINGER IAW SRM 51-40-02-0G-0.

Part: CHANNEL — CRACKED (BS 500A) · airframe 67,646 hrs · 38,751 cycles

FWD CARGO BAY CENTER CHANNEL BS 500A FOR VHF NR 1 ANTENNA IS CRACKED. ACFT GROUNDED. REMOVED, FABRICATED NEW AND INSTALLED NEW CHANNEL IAW SRM 51-40-02-0G-0.

Part: ATTACH BRACKET — CRACKED (BS 500A) · airframe 67,646 hrs · 38,751 cycles

FWD CARGO BAY CENTER CHANNEL FOR NR 1 VHF ANTENNA STA 500A AFT ATTACH BRACKET IS CRACKED. ACFT GROUNDED. REMOVED ATTACH BRACKET FOR NR 1 VHF ANTENNA SUPPORT CHANNEL FABRICATED AND INSTALLED NEW BRACK IAW DWG 65-45783 AND SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 500F-500G) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

DURING REMOVAL OF BS 500G BULKHEAD LOWER CENTER ANGLE FOUND FLOOR SUPPORT CORRODED AT RBL 13.8. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-53-1A1. REMOVED CORRODED SECTION OF SUPPORT, FABBED AND INSTALLED NEW SECTION IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0, FIG 2, W 1", O .070, R .050, L 3", D .020.

Part: FRAME — CRACKED (BS 348) · airframe 67,646 hrs · 38,751 cycles

BS 348.2 FRAME LOWER ANGLE WAS FOUND CRACKED AT LWR FASTENER HOLE. ACFT GROUNDED. R & R FRAME IAW SRM 51-40-02-0G-0.

Part: SUPPORT FRAME — CRACKED (L1 MOP SILL) · airframe 67,646 hrs · 38,751 cycles

UPON REMOVAL OF THE L1 MOP SILL THE BS 348.20 FRAME LOWER ANGLE WAS FOUND CRACKED AT LOWER FASTENER HOLE. ACFT GROUNDED. R & R FRAME ANGLE IAW SRM 51-40-02-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 877-947) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

AFT CARGO BAY BS 907, S26R FLOOR SUPPORT CORRODED AT NUTPLATE. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1, FIG 101. REPAIRED SUPPORT IAW SRM 53-00-53-2R-2.

Part: SHEAR TIE — CORRODED (BS 867) · airframe 67,646 hrs · 38,751 cycles

AFT CARGO PIT SHEAR TIE AT BL0, BS 867 CORRODED. ACFT GROUNDED. SHEAR TIE REPAIR IAW SRM 53-00-07-2R-17, REPAIR 17.

Part: SHEAR TIE — CORRODED (BS 927) · airframe 67,646 hrs · 38,751 cycles

SHEAR TIE, BL 0 CENTER AND RT IN AFT CARGO BAY CORRODED. ACFT GROUNDED. SHEAR TIE REPAIRED IAW SRM 53-00-07-2R-7, REPAIR 7 AND 53-00-07-2R-17, REPAIR 17 .

Part: ANGLE — CORRODED (TRANSITION PANEL) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

AFT CARGO BAY LT BS 827-947, S25L, FLOOR TRANSITION ANGLE HAS NUMEROUS AREAS OF CORROSION. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1. REMOVED, FABRICATED NEW AND INSTALLED NEW TRANSITION PANEL IAW SRM 51-40-02-0G-0, W 3.0", O .040, R .000, L 120.00, D .040.

Part: ATTACH ANGLE — CORRODED (BS 727E-767) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

AFT CARGO LT LOWER SIDEWALL LOWER ATTACHMENT LANDING CORRODED AROUND SCREW HOLES IN MULTIPLE AREAS FROM BS 727E-767. ACFT GROUNDED. REMOVED CORRODED AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1. REMOVED, FABRICATED NEW AND INSTALLED NEW TRANSITION PANEL IAW SRM 51-40-02-0G-0.

Part: ATTACH ANGLE — CORRODED (BS 727D-727F) · airframe 67,646 hrs · 38,751 cycles

AFT CARGO RT LOWER SIDEWALL LOWER ATTACHMENT LANDING CORRODED AROUND SCREW HOLES IN MULTIPLE AREAS FROM BS 727D-727 F. ACFT GROUNDED. REMOVED, FABRICATED AND INSTALLED NEW TRANSITION PANEL IAW SRM 51-40-02-0G-0, 51-40-05-0G-0-W.

Part: FLOORBEAM — CORRODED (BS 947) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

FLOORBEAM BS 947.5 RBL 12 AREA HAS CORROSION. ACFT GROUNDED. REPAIRED FLOORBEAM IAW EA 12265 REV.

Part: ATTACH ANGLE — CORRODED (BS 727-727F) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

AFT CARGO, LT LOWER SIDEWALL, ATTACHMENT LANDING CORRODED AROUND SCREW HOLES IN MULTIPLE AREAS FROM FWD BULKHEAD OF AFT CARGO TO FRAME 727 F. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1. REMOVED, FABRICATED NEW AND INSTALLED NEW TRANSITION PANEL ATTACH ANGLE IAW SRM 51-40-02-0G-0.

Part: STRINGER — CRACKED (R1 DOOR) · airframe 67,646 hrs · 38,751 cycles

R1 DOOR STRINGER CRACKED AT FS 294.5 AND S-14R. ACFT GROUNDED. R & R R1 DOOR STRINGER ANGLE AT FS 294.5 AND S-14R IAW SRM 51-40-02.

Part: STRINGER — CRACKED (R1 DOOR) · airframe 67,646 hrs · 38,751 cycles

R1 DOOR STRINGER CRACKED AT FS 294.5 AND S10R. ACFT GROUNDED. R & R STRINGER IAW SRM 51-40-02.

Part: STRINGER — CRACKED (R1 DOOR) · airframe 67,646 hrs · 38,751 cycles

R1 DOOR STRINGER CRACKED AT FS 294.5 AND S-13R. ACFT GROUNDED. R & R R1 DOOR STRINGER ANGLE AT FS 294.5 AND S-13R IAW SRM 51-40-02.

Part: STRINGER — CRACKED (R1 DOOR) · airframe 67,646 hrs · 38,751 cycles

R1 DOOR STRINGER CRACKED AT FS 294.5 AND S14R. ACFT GROUNDED. R & R R1 DOOR STRINGER IAW SRM-51-40-02.

Part: TRANSITION PANEL — CORRODED (BS 500G) · airframe 67,646 hrs · 38,751 cycles

TRANSITION PANEL ON LT SIDE AT FS 500G IS CORRODED. ACFT GROUNDED. TRANSITION PANEL REMOVED, FABRICATED NEW AND INSTALLED IAW SRM 51-40-02.

Part: STRINGER — CRACKED (R1 DOOR) · airframe 67,646 hrs · 38,751 cycles

R1 DOOR STRINGER 12R CRACKED AT BS 294.5. ACFT GROUNDED. R & R R1 DOOR STRINGER IAW SRM 51-40-02.

Part: STRINGER — CRACKED (BS 294.5) · airframe 67,646 hrs · 38,751 cycles

R2 DOOR STRINGER 11R CRACKED AT BS 294.5. ACFT GROUNDED. R & R R1 DOOR STRINGER ANGLE IAW SRM 51-40-02.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

AFT CARGO BAY NR 1 FLOOR PANEL HAS CORROSION AROUND HOLES. ACFT GROUNDED. BLENDED CORRODED AREA FOUND TO BE OUT OF LIMITS. FABRICATED, LOCATED AND DRILLED NEW FLOOR PANEL IAW SRM 51-30-01-0G-0 AND SRM 53-60-53-1A-1.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 67,646 hrs · 38,751 cycles

FLOORBEAM CRACKED AT FS 540 AND RBL 24.75 - 45.50. ACFT GROUNDED. R & R FLOORBEAM ANGLE IAW SRM 51-40-02.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 67,646 hrs · 38,751 cycles

FLOORBEAM CRACKED IN TWO PLACES AT BS 540 BETWEEN BL 0.0 AND RBL 24.75. ACFT GROUNDED. R & R FLOORBEAM IAW SRM 51-40-02.

Part: FLOOR PANEL — CORRODED (BS 859-948) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

AFT CARGO BAY NR 5 FLOOR PANEL HAS MANY AREAS OF CORROSION ON LOWER SURFACE. ACFT GROUNDED. BLENDED CORROSION FOUND TO BE OUT OF LIMITS, FABRICATED NEW FLOOR PANEL IAW SRM 51-30-01, 51-40-05.

Part: FLOOR PANEL — CORRODED (BS 500) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

FWD CARGO BAY NR 4 FLOOR PANEL HAS CORRODED ON LWR AFT SIDE. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-53-1A-1, FIG 101. FABRICATED NEW FLOOR PANEL IAW SRM 51-30-01-0G-0-W.

Part: FLOORBOARD — CORRODED (BS 772-859) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

AFT CARGO BAY NR 4 FLOORBOARD CORRODED AROUND HOLES. ACFT GROUNDED. FABRICATED, LOCATED AND DRILLED NEW FLOORBOARD IAW SRM 53-60-53-1A-1, FIG 1 AND SRM 51-40-05-0G-0.

Part: FLOOR SUPPORT — CORRODED (BS 312-328) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

FLOOR SUPPORT CORRODED AT FS 315, RBL 15. ACFT GROUNDED. R & R FLOOR SUPPORT IAW SRM 51-40-02-0G-0.

Part: FRAME — CRACKED (BS 500C) · airframe 67,646 hrs · 38,751 cycles

BS 500C FRAME IS CRACKED AT INBD HOLE OF THE AC BRACKET ATTACH POINT. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609 400-53-1-760.

Part: FRAME — CRACKED (BS 500F) · airframe 67,646 hrs · 38,751 cycles

BS 500F FRAME IS CRACKED AT INBD HOLE OF THE BRACKET ATTACH POINT. ACFT GROUNDED. REPAIRED FRAME IAW AD 20062609 400-53-1-760.

Part: FRAME — CRACKED (BS 727D) · airframe 67,646 hrs · 38,751 cycles

LEFT FRAME IS CRACKED AT INBD HOLE OF THE ATTACH POINT. ACFT GROUNDED. CUT OUT DAMAGE AREA FABRICATED, LOCATED, DRILLED AND INSTALLED TWO REPAIR ANGLES AT LT FRAME IAW T/C AD 20062609-400-53-1-760.

Part: FRAME — CRACKED (BS 727B) · airframe 67,646 hrs · 38,751 cycles

RIGHT FRAME IS CRACKED AT TWO HOLES OF THE BRACKET ATTACH POINT. ACFT GROUNDED. CUT OUT DAMAGE AREA, FABRICATED, LOCATED AND DRILLED AND INSTALLED TWO REPAIR ANGLES AT FRAME IAW T/C AD 20062609-400-53-1-760.

Part: SILL — CORRODED (BS 294-360) · corrosion level 2 · airframe 67,646 hrs · 38,751 cycles

L1 DOOR MOP SILL CORRODED. ACFT GROUNDED. R & R L1 DOOR MOPSILL IAW SRM 51-40-02-0G-0, W 2", O .090, R .078, L 7FT, D .012.

Part: ATTACH ANGLE — CRACKED (BS 360) · airframe 67,646 hrs · 38,751 cycles

INTERCOSTAL ATTACH ANGLE IS CRACKED AT BS 360, S9L. ACFT GROUNDED. R & R ATTACH ANGLE IAW EA 400, 53EA 12281, REV. CAT B REPAIR IAW SRM 51-00-06.

Part: GUSSET — CRACKED (BS 312) · airframe 67,646 hrs · 38,751 cycles

L1 DOOR FWD SIDE BS 312 AT STRINGER 14L GUSSET CRACKED. ACFT GROUNDED. R & R GUSSET IAW SRM 51-40-02-0G-0.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 67,646 hrs · 38,751 cycles

RT INBD FOREFLAP UPPER SURFACE EXISTING DOUBLER IS DELAMINATED. ACFT GROUNDED. REPAIRED RT INBD FOREFLAP UPPER SURFACE EXISTING DOUBLER IAW SRM 51-70-10-2R-4, REPAIR 4.

Part: ATTACH FITTING — CRACKED (BS 360) · airframe 67,646 hrs · 38,751 cycles

INTERCOSTAL ATTACH FITTING IS CRACKED AT BS 360, S9L. ACFT GROUNDED. R & R FITTING IAW SRM 51-40-02-0G-0.

Part: FRAME — CRACKED (BS 360) · airframe 67,646 hrs · 38,751 cycles

FRAME AT BS 360 CRACKED BETWEEN STR 8-9L. ACFT GROUNDED. REPAIRED FRAME IAW ASA T/C AD20062609-400-53-1-760.

Part: HINGE FITTING — CRACKED (BS 1138) · airframe 67,646 hrs · 38,751 cycles

INBD OF SKATE ANGLE ON VERTICAL STAB LT SIDE, AFT OF THE HINGE FITTING IS CRACKED. ACFT GROUNDED. PERFORMED EDGEBLEND OF FREE FLANGE OF DAMAGED AREA, FOUND TO BE WITHIN LIMITS IAW SRM 55-30-10-1A-1.

Part: STRINGER CLIP — CRACKED (BS 400) · airframe 67,646 hrs · 38,751 cycles

BS 400 STRINGER CLIP 8R IS CRACKED. ACFT GROUNDED. R & R STRINGER CLIP IAW SRM 51-40-02-0G0.

Part: ANCHOR FITTING — CORRODED (AFT CARGO BAY) · airframe 67,646 hrs · 38,751 cycles

AFT CARGO BAY FWD ANCHOR PLATE TORN AND CORRODED ON MATING SURFACE. ACFT GROUNDED. RECEIVED NEW PART LOCATED AND DRILLED FASTENER HOLES ON NEW PART FOR AFT CARGO FWD ANCHOR PLATE IAW SRM 51-40-05-0G-0, FIG 2 DETAIL I, REMOVED CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53-1A-1, FIG 101, DETAIL V.

Part: DOOR FRAME — CRACKED (BS 492) · airframe 67,646 hrs · 38,751 cycles

FWD CARGO BAY DOOR CUT OUT AFT FRAME CRACKED AT LWR AND UPPER STOP FITTINGS. ACFT GROUNDED. R & R CRACKED FRAME IAW SRM 51-40-02-0G-0.

Part: FRAME — CRACKED (BS 500) · airframe 67,646 hrs · 38,751 cycles

FWD CARGO AFT SIDE FRAME BS 500 LOWER CORNER CLOSE OUT PANEL CRACKED. ACFT GROUNDED. R & R DOUBLER ON FWD CARGO AFT SIDE FS 500 LOWER CLOSE OUT PANEL IAW SRM 51-40-02.

Part: WEB — DAMAGED (BS 794-800) · airframe 67,646 hrs · 38,751 cycles

AFT CARGO BAY DOORWAY FWD FRAME REVEAL WEB IS GOUGED AND CREASED OVER FRAME ON LOWER END. ACFT GROUNDED. FABRICATED NEW FRAME REVEAL WEB IAW SRM 51-40 05, TABLE I.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 64,845 hrs · 36,957 cycles

EMERGENCY EXIT SIGN ABOVE RT OVERWING EXIT DOORS FELL OFF. FOUND LENS LOCKING FEATURE BROKEN. R & R RT OVERWING EXIT LIGHT ASSY REF CMM 33-20-67. EMERGENCY LIGHT OPS CK GOOD. NO OTHER DEFECTS NOTED.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 64,769 hrs · 36,910 cycles

EMERGENCY LIGHT EXIT LOCATOR SIGN ON NR 4 GALLEY ADJACENT TO R-2 DOOR IS BROKEN. REF WDM SUPPLEMENT 33-51-42 R & R L1191 LIGHT ASSY AND PERFORMED TEST IAW MM 33-51-02-715-001. OPS NORMAL.

Part: FLOORBEAM — CORRODED (BS 993) · corrosion level 2 · airframe 64,154 hrs · 36,545 cycles

LEFT AFT MAIN CABIN UNDER FLOOR STRUCTURES, GALLERY SUPPORT ANGLE UPPER SURFACE HAS CORROSION AROUND FASTENERS HOLES (2EA). BS 993, LBL 44, LBL37. ACFT GROUNDED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED, AND REPLACED SUPPORT ANGLE IAW BAC DWG 69-77477 AND SRM 53-60-51, FIG 101, DETAIL VII.

Part: CHANNEL — CORRODED (BS 947-985) · corrosion level 2 · airframe 64,154 hrs · 36,545 cycles

AFT MAIN CABIN UNDER FLOOR STRUCTURES, L2 DOOR LOWER SILL DRAIN PAN SUPPORT CHANNEL UPPER SURFACE HAS CORROSION STARTING AT BS 967 AND RUNNING UNDER G4 GALLERY. ACFT GROUNDED. REMOVED CORROSION ORIG .071 MATERIAL LOST .031 REMAINING .040 38.0LWX2.0W. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 101, DETAIL VII. R & R CHORD IAW SRM 51-40-02 CICED IAW AMM 51-21-31.

Part: FLOORBEAM — CORRODED (BS 995) · corrosion level 2 · airframe 64,154 hrs · 36,545 cycles

RIGHT AFT MAIN CABIN UNDER FLOOR STRUCTURES, G4 GALLERY SUPPORT ANGLE UPPER SURFACE HAS CORROSION AROUND FASTENERS HOLES. BS 992. RBL33-RBL47. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED FABRICATED AND REPLACED ZEE IAW DWG 69-77477 AND SRM 53-60-51, FIG 101, DETAIL 7.

Part: FLOORBEAM — CORRODED (BS 986.5) · corrosion level 2 · airframe 64,154 hrs · 36,545 cycles

FOUND CORROSION ON LOWER SURFACE OF FLOORBEAM. BS 986.50 AT AFT GIRT BAR ATTACH FITTING UNDER FLOOR, CORROSION FOUND. REMOVED, FABRICATED AND REPLACED TEE CAP IAW SRM 53-00-51, REPAIR 2.

Part: WEB — CORRODED (BS 986) · corrosion level 2 · airframe 64,154 hrs · 36,545 cycles

LEFT AFT MAIN CABIN UNDER FLOOR STRUCTURES, FLOOR WEB UPPER SURFACE HAS CORROSION IN FWD EDGE AREA , BS 986, LBL45- LBL33. REMOVED CORROSION FOUND TO BE OUT OF LIMITS REMOVED, FABRICATED, AND REPLACED WEB IAW DWG 65C33582 AND SRM 53-60-51, FIG 101, DETAIL 7.

Part: FLOORBEAM — CORRODED (BS 985) · corrosion level 2 · airframe 64,154 hrs · 36,545 cycles

AFT MAIN CABIN UNDER FLOOR STRUCTURES , FLOORBEAM UPPER SURFACE HAS CORROSION AROUND FASTENERS HOLE LBL 42. BS 985. ACFT GROUNDED. REMOVED CORROSION ORIG .150 MATERIAL LOST .012 REMAINING .138 6.0L X 2.0W. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 101, DETAIL VII. ALL REPAIR INFO & DOCUMENTATION ACCOMPLISHED ON CUST CARD NR-00042/OPS 9942.

Part: CHANNEL — CORRODED (BS 947-992) · airframe 64,154 hrs · 36,545 cycles

MAIN CABIN UNDER FLOOR STRUCTURES, R-2 DOOR LOWER SILL DRAIN PAN SUPPORT CHANNEL UPPER SURFACE HAS CORROSION IN SEVERAL AREAS BETWEEN BS947 AND BS992. ACFT GROUNDED. REMOVED CORROSION ORIG .071 MATERIAL LOST .003 REMAINING .068 29.0LX1.5W. FOUND TO BE WITHIN LIMITS IAW SRM 53-60-15, FIG 101, DETAIL VI TOOL ID T8225N ALODINED AND PRIMED IAW SRM 51-20-01. PAINTED IAW AMM 51-21-99. MARKED BLEND OUT AREA IAW AMM 51-21-31/701 APPLIED CIC IAW AMM 51-21-31.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 64,154 hrs · 36,545 cycles

LEFT AFT MAIN CABIN UNDER FLOOR STRUCTURES, FLOORBEAM UPPER SURFACE HAS BARE METAL SPOT AROUND FASTENERS HOLE AT LBL 33.BS967. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE WITHIN LIMITS IAW SRM 53-60-51, FIG 101, DETAIL VII.

Part: TORQUE TUBE — CRACKED (LT WING) · airframe 64,154 hrs · 36,545 cycles

LEFT WING TORQUE TUBE IS CRACKED. R & R CRACKED BUMPER IAW CMM 57-53-22. REMOVED AND REINSTALLED BALLSCREW AND GIMBLE ASSY IAW CMM 57-53-22 AND AMM 27-51-73. OPS CHECKED GOOD IAW AMM 27-51-00.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 64,149 hrs · 36,544 cycles

WHILE ACCOMPLISHING T/C 48105000, FOUND CORROSION ON FLOORBEAM BS 986.50 AT AFT GIRT BAR ATTACH FITTING UNDER FLOOR. CORROSION FOUND ON LOWER SURFACE OF FLOORBEAM & NUTPLATE. EXTENSIVE ACCESS REQUIRED TO EVALUATE AREA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,752 hrs · 35,163 cycles

REF AD 20090206 400 53 1 STEP 10 STA 500E LT FRAME HAS A CRACK. REMOVED DAMAGE AREA ON FRAME BOOT AT STR 21L. REPAIRED FRAME REF SRM 53 00 08 REPAIR 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,752 hrs · 35,163 cycles

REF AD 20090206 400 53 1 STEP 17 STA 500E RT FRAME HAS A CRACK. REMOVED DAMAGED AREA ON FRAME 500E AT 21R STR. COMPLETED STA 500E FRAME AT STR 21R REF SRM 53 00 07 REPAIR 13 AND EA 400 53EA 06597.

Part: BAFFLE — CRACKED (CARGO BAY) · airframe 61,338 hrs · 34,918 cycles

FOUND BAFFLE RT STR 26 FWD SIDE OF STA 500F IS CRACKED. REPLACED BAFFLE AT BS 500F STR 26R IAW SRM 51 40 02 & DWG 69 41473.

Part: FITTING — CRACKED (FUSELAGE) · airframe 61,338 hrs · 34,918 cycles

FOUND CLIP THAT ATTACHES BAFFLE TO FRAME AT STA 500F RT STR 26 IS CRACKED. REMOVED FABRICATED AND INSTALLED CLIP IAW DWG 69 51411 SRM 51 40 05, SRM 51 20 01, SRM 51 40 02, DWG 69 41473 AT BS 500F STR 26RT.

Part: FITTING — CRACKED (FUSELAGE) · airframe 61,338 hrs · 34,918 cycles

WHILE WORKING, FOUND CLIP THAT ATTACHES BAFFLE TO FRAME AT STA 500E STR 26 IS CRACKED. DAMAGE ON CLIP AT BAFFLE AT BS 500E ST26L FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED CLIP IAW SRM 51 40 02 FIG 8 & SRM 51 40 02 STEP 4B C. SDR 120073.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,338 hrs · 34,918 cycles

SEVERAL BULL NOSE EXIT LIGHTS INOP. REPLACED BATTERY PACK M1479.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 61,338 hrs · 34,918 cycles

SEVERAL BULLNOSE EMER EXIT LIGHTS INOP. REPLACED BATTERY PACK M1134.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 61,338 hrs · 34,918 cycles

CORROSION WHILE WORKING TO CLOSE AFT CARGO BAY. FOUND LT CARGO TRACK CORRODED AND SEVERED AT BS 727B+3 LBL 17 WL 156. REPAIRED CARGO TRACK AT BS 727B+3 LBL 17 WL 156 IAW SRM 53 00 53 REPAIR 2 DWG 65 46592.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,338 hrs · 34,918 cycles

LEFT BS 601 FRAME WEB CRACKED AT LBL 64 WL 203. REPAIRED THE BS 601 FRAME WEB AT LBL 64 WL 203 IAW ASA EA 400 53EA 06042.

Part: TIE DOWN — CRACKED (CARGO BAY) · airframe 61,338 hrs · 34,918 cycles

AFT CARGO FLOOR TRACK TIE DOWN AT BS 727D+5 RBL 12.5 WL 156 CRACKED. REMOVED CRACKED AFT CARGO FLOOR TRACK TIE DOWN BS 727+4 TO 747+10 RBL 12.5 WL 156 AND INSTALLED NEW TRACK PER SRM 51 40 02.

Part: MOUNT — CRACKED (VHF COMM) · airframe 61,338 hrs · 34,918 cycles

NR 3 VHF ANTENNA MOUNT WAS FOUND TO BE CRACKED. REMOVED NR 3 VHF 3 ANTENNA MOUNT AND INSTALLED NEW MOUNT PER SRM 51 40 02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,338 hrs · 34,918 cycles

BS 500F STR 26LT STRINGER CLIP IS CRACKED. R&R STRINGER CLIP.

Part: MOUNT — CRACKED (VHF ANTENNA) · airframe 61,338 hrs · 34,918 cycles

NR 3 VHF ANTENNA MOUNT WAS FOUND TO BE CRACKED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,338 hrs · 34,918 cycles

BS 500F STR 26R STRINGER CLIP IS CRACKED. ACCOMPLISHED STRINGER CLIP REPAIR PER ASA 400 53EA 06148 ER 11 03403.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,338 hrs · 34,918 cycles

BS 500G STR 26R CLIP IS CRACKED. BS 500G STR26R CLIP REPAIRED PER ASA EA NUMBER 400 53EA 06148 ER11 03403 REV A.

Part: SILL — CRACKED (FUSELAGE) · airframe 61,338 hrs · 34,918 cycles

AFT CARGO DOOR UP SILL INSTLN SILL WEB AT STA 846.5 STR 18R WAS FOUND CRACKED. REPAIRED WED AT BS 846.5 STR 18R PER B737 400 SRM 51 70 13 51 40 03 53 60 15 AND BAC DWG 65 47956.

Part: SKIN — CRACKED (AC DOOR) · airframe 61,338 hrs · 34,918 cycles

RT A/C BAY DOOR IS CRACKED AT FWD INBOARD CORNER. REPAIRED CRACK IN THE UPPER SURFACE SKIN OF THE RT A/C BAY DOOR AT FWD INBD CORNER IAW B737 400 SRM 51 70 05.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,338 hrs · 34,918 cycles

WEB CRACKED AT BS 845.5 847 S27R WL 140.

Part: WEB — CRACKED (FUSELAGE) · airframe 61,773 hrs · 34,815 cycles

WEB CRACKED AT BS 648.5 847 S27R WL 140. REMOVED CRACKED WEB INTERCOSTAL FABRICATED WEB AND ATTACHING STIFFENERS STRAPS. INSTALLED PARTS PER SRM 53 60 15 REPAIR 1 AND SRM 51 40 02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,338 hrs · 34,918 cycles

FUSELAGE SKIN HAS A SUBSURFACE CRACK AT BS 727D+3 JUST BELOW STR 23R. ACCOMPLISHED FUSELAGE SKIN REPAIR PER ASA ER 11 03655 ASA EA 400 533A 06137.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,338 hrs · 34,918 cycles

CORROSION LT W/W LT KEEL BEAM HAS CORROSION AT SURROUNDING AREAS OF NUT PLATES FROM BS 674 BS 727 WL 148 (LOWER SURFACE OF LOWER CHORD). REMOVED NUT PLATES BLENDED CORROSION. DAMAGE ALL WITHIN LIMITS. REFINISHED SURFACES AND REPLACED NUT PLATES PER B737 400 SRM 53 60 12.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,338 hrs · 34,918 cycles

LONGITUDINAL FLOORBEAM UPPER CHORD IS CRACKED AT BS 665 BL 0 WL 208. REPAIRD LONGITUDINAL FLOORBEAM UPPER CHORD PER ASA EA 400 57EA 06079.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 61,338 hrs · 34,918 cycles

FLOOR SUPPORT IS CRACKED AT BS 359 BL 0 WL 208. REMOVED AND REPLACED INTERCOSTAL PER B737 400 SRM 51 40 02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,867 hrs · 31,667 cycles

EMERGENCY EXIT LIGHTS AT AFT ENTRY DOOR AND AFT CEILING GO ON FOR TWO SECONDS AND THEN OFF. REPLACED M1197 BATTERY PACK REF MM 33 51 51, OPS NORMAL PER SAME.

Part: GUIDE ARM — LOOSE (L1 DOOR) · airframe 55,113 hrs · 31,235 cycles

L1 DOOR HARD TO OPEN & CLOSE. FOUND L 1 DOOR GUIDE ARM LOOSE & OUT OF ADJUSTMENT. R&R GUIDE ARM & ADJUSTED REF. AMM 52 11 21 004 404 007 015 B00. L 1 DOOR STILL HARD TO CLOSE REMOVED DOOR LINER & ADJUSTED HORZ ROD & ALL DOOR STOP PINS REF. AMM 52 11 21 004 015 B00. REINSTALLED DOOR LINER REF. AMM 52 11 31 404 009 B00. ACCOMPLISHED DOOR OPS TEST (TESTED GOOD) HANDLE FORCE NOW WITHIN LIMITS REF. 52 11 00 755 051 B00.

Part: STRINGER CLIP — CRACKED (BS 380) · airframe 54,769 hrs · 31,033 cycles

STRINGER CLIP CRACKED. REPLACED CLIP PER ASA DWG A53100265816.

Part: INTERCOSTAL — CRACKED (BS 380-400) · airframe 54,769 hrs · 31,033 cycles

INTERCOSTAL CRACKED AND FASTENER HOLES STA 380-400. REMOVED CORRODED INTERCOSTAL INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-40-2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

STRINGER CLIP CRACKED. REPLACED CLIP PER ASA DWG A53100265816.

Part: STRINGER CLIP — CRACKED (BS 887) · airframe 54,769 hrs · 31,033 cycles

STRINGER CLIP CRACKED. REPLACED CLIP PER DWG A53100265816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

STRINGER CLIP CRACKED. REPLACED CLIP PER ASA DWG A53100265816.

Part: STRAP — CRACKED (FLOOR SUPPORT) · corrosion level 2 · airframe 54,769 hrs · 31,033 cycles

FLOORBEAM STABILIZER STRAP BROKEN/CRACKED. REMOVED CRACKED SECTION OF STRAP FABRICATED REPAIR FILLER AND STRAP INSTALLED FILLER AND STRAP IAW SRM 51-70-13 FIG 1.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 52,326 hrs · 29,609 cycles

LEFT WING OUTBOARD AFT FLAP TE IS DELAMINATED AT INBOARD CORNER. REMOVED DELAMINATED SECTION. INSTALLED FILLER DOUBLER AND BONDED REPAIR PER SRM 51-70-10.

Part: INTERCOSTAL — CORRODED (BS 747-767) · airframe 54,769 hrs · 31,033 cycles

INTERCOSTAL CORRODED STA 747 767 STR 26R. REMOVED CORRODED INTERCOSTAL INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51 40 2.

Part: INTERCOSTAL — CORRODED (BS 787-793) · airframe 54,769 hrs · 31,033 cycles

AFT CARGO PIT CORRODED INTERCOSTAL STA 787 TO STA 793 STR 26R AREA. REMOVED DAMAGED INTERCOSTAL, LOCATED, DRILLED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-40-02 AND 51-40-05.

Part: SKIN — DENTED (TE FLAP) · airframe 54,769 hrs · 31,033 cycles

NUMEROUS DENTS ON LT OTBD TE OF AFT FLAP LOWER SURFACE. PREPPED DAMAGED AREA FABRICATED AND INSTALLED REPAIR AND DOUBLER AND FILLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 54,769 hrs · 31,033 cycles

LT OTBD AFT FLAP LOWER SURFACE DENTED PREPPED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: STRINGER CLIP — CORRODED (BS 727 S25L) · corrosion level 2 · airframe 54,769 hrs · 31,033 cycles

STRINGER CLIP IS CORRODED. REPLACED CLIP PER SRM 51-40-02 AND DWG 69-35352 B.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NUMBER 5 SPOILER LOWER SURFACE DENTED. REMOVED DAMAGED AREA AND INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51 70 10.

Part: SKIN — DELAMINATED (NR 5 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NR 5 SPOILER INSERTS CORRODED/SKIN DELAMINATED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

L1 DOOR CUTOUT INNER CHORD SPLICE PLATE IS CORRODED. REPLACED SPLICE PLATE PER SRM 51 40 05.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 54,769 hrs · 31,033 cycles

CRACK IN LT ELEVATOR UPPER SKIN O/B OF TAB CONTROL ROD. REMOVED DAMAGED AREA OF SKIN, PREPPED AREA AND REPAIR, INSTALLED REPAIR PLIES IAW 737 400 SRM 51 70 10 REPAIR 1.

Part: SKIN — DENTED (NR 4 SLAT) · airframe 54,769 hrs · 31,033 cycles

NR 4 SLAT T/E WEDGE UPPER SURFACE IS DENTED. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — CHAFED (RT IB MID FLAP) · airframe 54,769 hrs · 31,033 cycles

RT INBD MID FLAP T/E WEDGE CHAFED. REMOVED AND REPLACED T/E WEDGE IAW B737 400 SRM 51 40 02.

Part: SKIN — CHAFED (TE FLAP) · airframe 54,769 hrs · 31,033 cycles

RT OB MID FLAP TE SKIN IS CHAFED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR GENERAL.

Part: FRAME — CRACKED (BS 616) · airframe 54,769 hrs · 31,033 cycles

RT FUSELAGE INNER FRAME CHORD CRACKED AT STA 616. REMOVED CRACKED SECTION FABRICATED AND INSTALLED FILLER AND STIFFENER ANGLE IAW ASA EO 5310 02528.

Part: SKIN — DELAMINATED (NR 3 SLAT) · airframe 54,769 hrs · 31,033 cycles

NR 3 SLAT T/E WEDGE DELAMINATED AT INBD AND OTBD ENDS. PREPPED DELAMINATED AREAS FABRICATED AND INSTALLED REPAIR CORE FILLER AND DOUBLER IAW SRM 51-70-10 REPAIR 4.

Part: FRAME — CRACKED (BS 616) · airframe 54,769 hrs · 31,033 cycles

LT FUSELAGE FRAME INNER CHORD CRACKED AT STA 616. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND STIFFENING ANGLE IAW EO 5310 02528.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

L1 DOOR UPPER HINGE CUTOUT SKIN AND BEARSTRAP CRACKED. REMOVED DAMAGE FABRICATED AND INSTALLED BEARSTRAP FILLER REPAIR DOUBLER REPAIR FILLER IAW ASA EA 400 53EA 00284.

Part: BEAR STRAP — CRACKED (BS 297-307) · airframe 54,769 hrs · 31,033 cycles

L1 DOOR LOWER HINGE CUTOUT SKIN AND BEARSTRAP CRACKED REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR TRIPLER, REPAIR DOUBLER, REPAIR FILLERS, STRUCTURAL FILLER IAW ASA EA 400-53EA-00284.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION INSTALLED REPAIR ANGLES AND FILLERS PER ASA EA 400 53EA 00267.

Part: FRAME — CORRODED (BS 500D) · airframe 54,769 hrs · 31,033 cycles

FRAME AT STA 500D IS CORRODED. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 51-70-11 REPAIR 2.

Part: WEB — DAMAGED (BS 755) · airframe 54,769 hrs · 31,033 cycles

RT SHEAR WEB IS SCRATCHED STA 755. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 13.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

CRACKED INTERCOSTAL AT STA 277. REMOVED CRACKED INTERCOSTAL, INSTALLED NEW INTERCOSTAL IAW B737 400 SRM 51 40 02.

Part: SHEAR TIE — GOUGED (BS 303) · airframe 54,769 hrs · 31,033 cycles

SHEAR TIE STA 303.1 STR 15L IS GOUGED. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW B737 400 SRM 51 30 01 AND BOEING DRAWING 65 17684.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

FLOORBEAM CORRODED. REPLACED BEAM CHORD PER SRM 51 40 02.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,769 hrs · 31,033 cycles

INNER CHORD AT R2 DOOR WAY IS CORRODED. REMOVED CORRODED INNER CHORD FABRICATED AND INSTALLED INNER CHORD IAW SRM 51 40 02.

Part: FRAME — CRACKED (BS 907) · airframe 54,769 hrs · 31,033 cycles

FRAMED CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400-53EA-00267.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED STA 867 STR 8 9L. CUTOUT DAMAGE FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER IAW ASA EA 400 53EA 00267.

Part: SKIN — DENTED (LE SLAT) · airframe 54,769 hrs · 31,033 cycles

NR 5 SLAT UPPER SURFACE HAS DENT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: BEAM — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

MAIN CABIN STUB BEAM CRACKED RT STA 601 RBL 65. TRIMMED OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND STIFFENING ANGLE IAW ASA EA 400 53EA 00269.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER EA 400 53EA 00267.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED STA 787 STR 8 9L. CUTOUT DAMAGE FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER IAW ASA EA 400 53EA 00267.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267.

Part: FRAME — CRACKED (BS 727) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400-53EA-164.

Part: SILL — CORRODED (BS 277-360) · corrosion level 2 · airframe 54,769 hrs · 31,033 cycles

L1 DOOR CUTOUT SILL BEAM CHORD IS CORRODED. REMOVED CORRODED CHORD REPLACED SILL BEAM CHORD IAW B737 400 SRM 51 40 02 B DRAWING 65 17688 AND ASA EA 400 53EA 00208.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

SHEAR WEB CORRODED AT STA 370 LT SIDE. REMOVED CORRODED AREA OF WEB, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 13.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION INSTALLED REPAIR ANGLES AND FILLERS PER ASA EA 400 53EA 00267.

Part: STRINGER CLIP — CRACKED (BS 706 S10R) · airframe 54,769 hrs · 31,033 cycles

CABIN FRAME STA 706 STRINGER CLIP CRACKED AT STA 10R. REMOVED DAMAGED CLIP, LOCATED DRILLED NEW CLIP AND INSTALLED IAW B737 400 SRM 51 40 03.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

CABIN STRINGER CLIP CRACKED AT STA 380 STR 8. REMOVED DAMAGED CLIP, LOCATED DRILLED AND INSTALLED REPLACEMENT STRINGER CLIP IAW B737 400 SRM 51 40 02 PG 2 AND 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267.

Part: STRAP — GOUGED · airframe 54,769 hrs · 31,033 cycles

INTERCOSTAL TIE STRAP STA 295 IS GOUGED REMOVED GOUGED STRAP INSTALLED NEW STRAP IAW B737 400 SRM 51 40 02 ASA EA 400 53EA 00199.

Part: FRAME — CRACKED (BS 440) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400-53EA-00267.

Part: FRAME — CRACKED (BS 727) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,769 hrs · 31,033 cycles

FLOOR STRAP CORRODED STA 1016 LBL 2. REMOVED CORRODED STRAP, INSTALLED REPLACEMENT STRAP IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (BS 747) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER EA 400 53EA 00267.

Part: STRINGER CLIP — CORRODED (BS 727G S26R) · airframe 54,769 hrs · 31,033 cycles

STRINGER CLIP CORRODED. REMOVED CORRODED STRINGER CLIP FABRICATED AND INSTALLED REPLACEMENT CLIP IAW B737 400 SRM 51 30 01 AND 51 40 02.

Part: FRAME — CRACKED (BS 747) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER EA 400-53EA-00267.

Part: FRAME — CRACKED (BS 400) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400-53EA-00267.

Part: FRAME — CRACKED (BS 727) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER EA 400 53EA 00267.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

CABIN STRINGER CLIP CRACKED AT STA 500B STR 16R. REMOVED DAMAGED CLIP, LOCATED DRILLED AND INSTALLED REPLACEMENT STRINGER CLIP IAW B737 400 SRM 51 40 02 PG 2 AND 4 AND 51 40 05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLERS PER EA 400 53EA 00267.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

SHEAR WEB CORRODED LT STA 400. REMOVED CORRODED AREA OF WEB, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 13.

Part: INTERCOSTAL — CRACKED · airframe 54,769 hrs · 31,033 cycles

INTERCOSTAL STA 295 STR 4L IS CRACKED REMOVED CRACKED INTERCOSTAL INSTALLED NEW INTERCOSTAL IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267.

Part: FRAME — CRACKED (BS 787) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400-53EA-00267.

Part: FRAME — CRACKED (BS 400) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

CABIN STRINGER CLIP CRACKED STA 907 STR 8R. REMOVED DAMAGED CLIP, LOCATED DRILLED AND INSTALLED REPLACEMENT STRINGER CLIP IAW B737 400 SRM 51 40 02 PG 2 AND 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 54,769 hrs · 31,033 cycles

FLOORBEAM CORRODED STA 344. REMOVED CORRODED SECTION OF UPPER CHORD. FABRICATED AND INSTALLED REPLACEMENT CHORD REPAIR ANGLES CHORD AND STRAPS IAW ASA EA 40053EA 0227.

Part: FRAME — CRACKED (BS 907) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

FLOORBEAM CORRODED. REPLACED FLOORBEAM PER SRM 53 10 51.

Part: SKIN — CHAFED (NR 4) · airframe 54,769 hrs · 31,033 cycles

NUMBER 4 SLAT TE WEDGE LOWER SKIN IS CHAFED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR FILLER AND DOUBLERS PER SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 54,769 hrs · 31,033 cycles

R1 DOOR CUTOUT INNER CHORD MOP SILL IS CORRODED. REMOVED CORRODED MOP SILL AND INSTALLED NEW MOP SILL IAW B737 400 SRM 51 40 02.

Part: FRAME — CRACKED (BS 440) · airframe 54,769 hrs · 31,033 cycles

FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER EA 400 53EA 00267.

Part: INTERCOSTAL — CORRODED (BS 767-787) · corrosion level 2 · airframe 54,769 hrs · 31,033 cycles

AFT CARGO PIT CORRODED INTERCOSTAL STA 767 TO STA 787 RBL 24. REMOVED DAMAGED INTERCOSTAL LOCATED DRILLED INSTALLED REPLACEMENT INTERCOSTAL IAW B737 400 SRM 51 40 02 AND 51 40 05.

Part: WEB — CORRODED (BS 800-847) · corrosion level 2 · airframe 54,769 hrs · 31,033 cycles

AFT CARGO PIT DOOR SILL WEB CORRODED AROUND NUT PLATES ON LOWER SIDE STA 800 TO 847 RBL 20 TO RBL 28. REMOVED DAMAGED SILL WEB LOCATED DRILLED INSTALLED REPLACEMENT SILL WEB IAW SRM 51-40-02 PG 3

Part: SKIN — DENTED (RT IB AFT FLAP) · airframe 54,769 hrs · 31,033 cycles

RT INBD AFT FLAP UPPER SURFACE HAS DENT. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51 70 10 REPAIR 4.

Part: CARGO TRACK — DAMAGED (CARGO BAY) · airframe 54,769 hrs · 31,033 cycles

CARGO TRACK TIE DOWN HAS DAMAGED LUGS STA 787. REMOVED DAMAGED SECTION OF TRACK, FABRICATED AND INSTALLED REPLACEMENT TRACK PLATES ANGLES IAW B737 400 SRM 53 00 50 REPAIR 2 FIG 201.

Part: STRAP — CORRODED · corrosion level 2 · airframe 54,769 hrs · 31,033 cycles

AFT CARGO PIT DOOR OPENING SILL PLATE TAPERED STRAP CORRODED STA 775 TO STA 855 RBL 24. REMOVED DAMAGED STRAP LOCATED DRILLED INSTALLED A REPLACEMENT STRAP IAW B737 400 SRM 51 40 02.

Part: SKIN — DENTED (NR 9 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NUMBER 9 SPOILER UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLER PER SRM 51 70 10.

Part: WEB — CORRODED (BS 452-489) · corrosion level 2 · airframe 54,769 hrs · 31,033 cycles

FWD CARGO PIT DOOR THRESHOLD WEB CORRODED STA 452 TO STA 489 RBL 26 TO RBL 29. REMOVED DAMAGED THRESHOLD WEB LOCATED DRILLED INSTALLED REPLACEMENT WEB IAW B737 400 SRM 51 40 02 FIG 9 PG 31 33.

Part: SKIN — DENTED (FOREFLAP) · airframe 54,769 hrs · 31,033 cycles

RT INBD FOREFLAP UPPER SURFACE DENTED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (NR 7 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NR 7 SPOILER UPPER SURFACE DENTED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (TE FLAP) · airframe 54,769 hrs · 31,033 cycles

RIGHT INBOARD AFT FLAP LE IS DENTED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER AND SPLICE PLATE PER SRM 57-53-01.

Part: SKIN — DENTED (FOREFLAP) · airframe 54,769 hrs · 31,033 cycles

RT INBD FOREFLAP UPPER SURFACE DENTED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NUMBER 5 SPOILER UPPER SURFACE IS DENTED. INSTALLED REPAIR DOUBLER PER SRM 51 70 10.

Part: SKIN — CHAFED (FOREFLAP) · airframe 54,769 hrs · 31,033 cycles

RT INBD FOREFLAP UPPER SURFACE CHAFED ON INBD END. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (NR 8 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NR 8 SPOILER LOWER SURFACE DENTED. PREPPED DENTED AREA FABRICATED AND INSTALLED REPAIR AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (NR 5 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NR 5 SPOILER LOWER SURFACE DENTED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — PUNCTURED (NR 4 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NR 4 SPOILER LOWER SURFACE DENTED AND PUNCTURED AT WBL 114. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10.

Part: SKIN — DENTED (NR 7 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NUMBER 7 SPOILER LOWER SURFACE DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51 70 10.

Part: SKIN — DENTED (NR 1 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NUMBER 1 SPOILER LOWER SURFACE DENTED. INSTALLED REPAIR DOUBLER PER SRM 51 70 10.

Part: SKIN — DENTED (NR 2 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NUMBER 2 SPOILER LOWER SURFACE IS DENTED. INSTALLED REPAIR DOUBLER PER SRM 51 70 10.

Part: SKIN — DENTED (NR 9 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NUMBER 9 SPOILER UPPER SURFACE IS DENTED. INSTALLED REPAIR DOUBLER PER SRM 51 70 10.

Part: SKIN — PUNCTURED (FOREFLAP) · airframe 54,769 hrs · 31,033 cycles

RIGHT INBOARD FOREFLAP DENTED AND PUNCTURED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 51 70 10.

Part: SKIN — DENTED (NR 4 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NR 4 SPOILER HAS DENTS ON LOWER SURFACE IN LINE WITH ACTUATOR. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.

Part: SKIN — DENTED (NR 8 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NUMBER 8 SPOILER HAS PROTRUDING DENT ON UPPER SURFACE. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER PER SRM 57 70 01.

Part: SKIN — PUNCTURED (RT WING FLAP) · airframe 54,769 hrs · 31,033 cycles

RT WING I/B FORE FLAP LOWER SURFACE HAS VARIOUS DENTS WBL 73-93. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10.

Part: SKIN — DENTED (TE FLAP) · airframe 54,769 hrs · 31,033 cycles

LT OTBD AFT FLAP LOWER SURFACE IS DENTED PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (TE FLAP) · airframe 54,769 hrs · 31,033 cycles

RIGHT OUTBOARD AFT FLAP LOWER SURFACE DENTED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 51 70 10.

Part: SKIN — DENTED (NR 1 SPOILER) · airframe 54,769 hrs · 31,033 cycles

NUMBER 1 SPOILER LOWER SURFACE DENTED. INSTALLED REPAIR DOUBLER PER SRM 51 70 10.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 54,769 hrs · 31,033 cycles

LT OTBD AFT FLAP DENTED ON LOWER SURFACE. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (TE FLAP) · airframe 54,769 hrs · 31,033 cycles

LEFT INBOARD MID FLAP TE WEDGE UPPER SURFACE IS DENTED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 51 70 10.

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 54,769 hrs · 31,033 cycles

AFT CARGO DOOR HAS DENT ON EXTERNAL SKIN DOUBLER REMOVED AND REPLACED AFT CARGO DOOR IAW B737 400 AMM 52 31 404 022 B00.

Part: SKIN — DENTED (NR 3 SPOILER) · airframe 54,769 hrs · 31,033 cycles

33 SPOILER UPPER SURFACE HAS DENT. PREPPED DAMAGED AREA FABRICATED AND INSTALLED REPAIR AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.

Part: SKIN — DENTED (CARGO DOOR) · airframe 54,769 hrs · 31,033 cycles

BELOW AFT CARGO DOOR LARGE DENTS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW B737 400 SRM 53 00 01 REPAIR 31.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 51,993 hrs · 29,562 cycles

WATER SERVICE TRUCK PULLED AWAY FROM AIRCRAFT WITH THE HOSE CONNECTED TO SERVICE PANEL RIPPING OUT NIPPLE AND PAN ATTACHMENT. REMOVED AND REPLACED PAN AND ASSOCIATED FITTING IAW SRM 51-40-02 & EA5330 02272.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,916 hrs · 28,985 cycles

INTERCOSTAL CRACKED. REPLACED INTERCOSTAL IAW EA 5310 02729.

Part: SHEAR TIE — CRACKED (BS 360) · airframe 50,915 hrs · 28,984 cycles

BODY FRAME TO SKIN ATTACHMENT SHEAR TIE CRACKED. SHEAR TIE REPLACED WITH MADE REPAIR PART IAW SRM 51-40-05.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 51,002 hrs · 29,044 cycles

INTERCOSTAL O/B FLANGE ATTACHMENT ANGLE CRACKED. INTERCOSTAL ATTACHMENT ANGLE REPAIRED IAW ERO 6993 AND EA 5310 02729. REPAIR TO BE INSPECTED PER ASA DWG A 5310023893 EVERY 6000 FLT CYCLES.

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 50,915 hrs · 28,984 cycles

NR 5 SLAT TRAILING EDGE DELAMINATED ON O/B END. NR 5 SLAT TRAILING EDGE DELAMINATION AT O/B END REPAIRED IAW SRM 51-70-10.

Part: SKIN — GOUGED (BS 767-787) · airframe 50,915 hrs · 28,984 cycles

THREE INCH GOUGE AT FUSELAGE SKIN. REPAIRED GOUGE IAW SRM 53-00-01 FIG 201 REPAIR 31.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 51,002 hrs · 29,044 cycles

INTERCOSTAL WEB CRACKED. INTERCOSTAL WEB REPLACED IAW ERO 6993 AND EA 5310 02729. REPAIR TO BE INSPECTED PER ASA DWG A 5310023893.

Part: BEARING — ERODED (R1 DOOR) · airframe 50,428 hrs · 28,712 cycles

CATERING REPORTED THE L1 DOOR INOPERABLE. FERRIED TO SEA, REMOVED AND REPLACED R1 DOOR PER AMM.

Part: STOP — WORN (R2 DOOR) · airframe 49,541 hrs · 28,182 cycles

R2 SLIDE PACK LOOSE. R2 SLIDE PACK LOWER ATTACH FITTING DOES NOT ENGAGE FITTING ON DOOR. REMOVED AND REPLACED R2 SLIDE ASSY PER MM 25-61-35. REMOVED AND REPLACED R2 DOOR LINER ASSY PER MM 52-41-31. SHIMMED R2 DOOR SLIDE SUPPORT ASSY STOP EO 2560 01395. SLIDE ASSY SEATED AGAINST DOOR LINER.

Part: FAN — UNKNOWN (LEFT) · airframe 48,529 hrs · 27,635 cycles

EXITING COCKPIT THE F/O FOUND THE LT CABIN RECIRCULATION FAN CKT BKR OPEN OUT. REPLACED RECIRCULATION FAN WIRING AND RELAYS AT J 20 BOX IAW LOG PGS 6198774 AND 6198776 AS A PRECAUTIONARY MEASURE.

Part: FRAME — CORRODED (BS 500 S28R) · corrosion level 2 · airframe 47,703 hrs · 27,156 cycles

FOUND CORROSION ON FRAME REPAIRED FRAME PER SRM 53 00 07.

Part: FRAME — CORRODED (BS 500C) · corrosion level 2 · airframe 27,156 hrs · 27,156 cycles

FOUND FWD CARGO PIT FRAME TO SKIN AT BSTA 500C CORRODED. FRAME TO SKIN ATTACHMENT REPAIRED PER SRM 53 00 07.

Part: FRAME — CORRODED (BS 520) · corrosion level 2 · airframe 47,703 hrs · 27,156 cycles

FOUND SKIN TO FRAME ATTACH ANGLE CORRODED AT BSTA 520 BETWEEN STR 27R AND 28R. ATTACH ANGLE REPLACED IAW SRM 51 30 01 5300 07 AND 51 40 02.

Part: FRAME — DENTED (BS 767) · airframe 47,703 hrs · 27,156 cycles

FOUND AFT CARGO FRAME DENTED. REPAIRED WITH FABRICATED REPAIR PART PER SRM 51 70 11.

Part: SKIN — CHAFED (RT PYLON) · corrosion level 2 · airframe 47,703 hrs · 27,156 cycles

RT PYLON IB SKIN CHAFED AT LE. REPAIRED PER EA 5430 01150.

Part: FRAME — CORRODED (BS 500B) · corrosion level 2 · airframe 47,703 hrs · 27,156 cycles

FOUND FWD CARGO PIT FRAME TO SKIN AT BSTA 500B CORRODED. REPAIRED PER SRM 53 00 07.

Part: FLOORBEAM — CORRODED (BS 986) · corrosion level 2 · airframe 47,703 hrs · 27,156 cycles

FOUND FLOORBEAM CORRODED. REPLACED FLOORBEAM PER EA 5310 01697.

Part: FRAME — CORRODED (BS 520) · corrosion level 2 · airframe 47,703 hrs · 27,156 cycles

FOUND SKIN TO FRAME ATTACH ANGLE CORRODED AT BS 520 BETWEEN STR 27R AND 28R. ATTACH ANGLE REPLACED IAW SRM 51 30 01 53 00 07 AND 51 40 02.

Part: FRAME — DENTED (BS 767) · corrosion level 2 · airframe 47,703 hrs · 27,156 cycles

FOUND AFT CARGO FRAME DENTED. REPAIRED WITH FABRICATED PART IAW SRM 51 70 11.

Part: FRAME — CORRODED (BS 500C) · corrosion level 2 · airframe 47,703 hrs · 27,156 cycles

FOUND FWD CARGO FRAME TO SKIN AT BSTA 500C CORRODED. REPAIRED PER SRM 53 00 07.

Part: SKIN — GOUGED (WS 380-402) · airframe 47,703 hrs · 27,156 cycles

FOUND RT OB AFT FLAP LE GOUGED. REPAIRED PER SRM 57 43 01 FIG 201.

Part: GUIDE — OUT OF ADJUST (L1 DOOR) · airframe 46,519 hrs · 26,505 cycles

L1 DOOR WILL NOT CLOSE FROM THE INSIDE UNLESS THE AFT PART OF THE DOOR IS PUSHED OUTBD WHILE CLOSING. REMOVED AND REPLACED BOTTOM GUIDE PLATE PER AMM 52 11 00 PG 407-408.

Part: RIB — CRACKED (WING)

GYR - FOUND WING RIB LOWER CHORD IS CRACKED APPROXIMATELY .5 INCH LONG, CHORD TO SKIN ATTACH TEE AFT OF STRINGER. REPLACED DAMAGED RIB LOWER CHORD. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND MAIN DECK FLOORBEAM UPPER T-CAP STATION 360 HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE. REPAIRED FLOORBEAM. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

GYR - FOUND FORWARD CARGO COMPARTMENT, STATION 520 RBL 3, LOWER FRAME SHEAR TIE 100 PERCENT EXFOLIATED. FABRICATED AND INSTALLED 65-46534-9 SHEAR TIE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND MAIN DECK FLOORBEAM STATION 294.5 HAS CORROSION FROM LBL 12 TO RBL 50. REPAIRED FLOORBEAM T-CAP CHORD. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

GYR - FOUND R1 DOOR THRESHOLD CREASEBEAM AT STATION 294.5 APPROX RBL 55, CORRODED IN NUMEROUS AREAS OF UPPER SURFACE. REMOVED AND REPLACED R-1 DOOR THRESHOLD CHORD STATION 262 TO 380 RBL 55 PER SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - FOUND MAIN DECK FLOORBEAM AT FS 294.5 APPROX LBL 12 TO RBL 50, UPPER T-CAP HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE. BLENDED CORROSION CK OUT OF LIMITS. REMOVED 'T' AND FABRICATED NEW 'T' AND INSTALLED 'T' AND REPAIR ANGLE PER SRM 53-10-51. (M)

Part: ATTACH FITTING — CORRODED (FUSELAGE)

GYR - FOUND ATTACH FITTING CORRODED. REPLACED ATTACH FITTING. (M)

Part: SKIN — DENTED (FUSELAGE)

GYR - FOUND DENT IN FUSELAGE SKIN, AF6 OF L-1 DOOR 8 FEET ABOVE VERTICAL. REPAIRED DENT IN FUSELAGE STATION 360 TO 380, STRINGER 17L AND 18L REF SRM 53-00-01 FIG 201. (M)

Part: CREASE BEAM — CORRODED (FUSELAGE)

GYR - FOUND R1 DOOR THRESHOLD CREASEBEAM AT STATION 294.5 APPROX RBL 55, CORRODED IN NUMEROUS AREAS OF UPPER SURFACE. REMOVED AND REPLACED R1 DOOR THRESHOLD CHORD STATION 262 TO 380 RBL 55 PER SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

GYR - MAIN DECK FLOORBEAM AT STATION 294.5 APPROX LBL 12 TO RBL 50, UPPER T-CAP HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE. BLENDED CORROSION CK OUT OF LIMITS. REMOVED 'T' AND REPAIR ANGLE EPR SRM 53-10-51. (M)

Part: SHEAR TIE — CORRODED (FUSELAGE)

GYR - FOUND FORWARD CARGO COMPARTMENT, STATION 520 RBL 3, LOWER FRAME SHEAR TIE 100 PERCENT EXFOLIATED. FABRICATED AND INSTALLED 65-46534-9 SHEAR TIE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 45 TO RBL 25 AND WL 207. REPAIRED IAW SRM. (M)

Part: STRINGER — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND CORROSION AT BS 520 STRINGER 27R AND WL 148.5 FORWARD CARGO BAY. REPAIRED IAW SRM. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND AFT CARGO BAY DOOR CUTOUT STRUCTURE U-CHANNEL HAS AREAS OF CORROSION BS 796-847, RBL 28 AND WL 155. REPAIRED IAW SRM. (M)

Part: SKIN — CORRODED (FUSELAGE)

PAE - DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED ON INTERIOR SKIN AT BS 500F, WL 149 AND STRINGER 27R. REPAIRED IAW SRM. (M)

Part: WIRE — BROKEN (CABIN)

SEA - DURING PREFLIGHT, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE. REPLACED BROKEN WIRES OPERATIONAL CHECKED NORMAL. (M)

Part: WIRE — DISCONNECTED (ROW 18-19)

PDX-FOUND EMERGENCY TRACK LIGHTS INOP AT ROW 18-19, DISCONNECTED.RECONNECTED TRACK LIGHTS, OPERATION CHECKED NORMAL, NO DEFECTS NOTED.

Part: BULKHEAD — GOUGED (CARGO BAY)

SEA-DURING MAINTENANCE CHECK FOUND, FWD CARGO PIT LT, RT, AND CTR BULKHEAD PANEL GOUGED. REPAIRED I.A.W. EA 2550-01093.

Part: WIRE — BROKEN (MID CABIN)

PDX - PRIOR TO FLIGHT 95, THE MID CABIN EMERGENCY TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPAIRED BROKEN WIRE AT MODULE M1388 AND THE LIGHTS OPERATED NORMALLY. (M)

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 26,994 hrs · 15,953 cycles

PDX - DURING MAINTENANCE CHECK, THE R-1 DOOR WAS DIFFICULT TO OPEN. LUBED DOOR HANDLE MECHANISM AND THE DOOR OPERATED NORMALLY. (X)

Part: DOOR — OUT OF RIG (PAX DOOR)

PDX - PRIOR TO FLIGHT 712, THE L1 DOOR WAS DIFFICULT TO CLOSE. LUBRICATED AND RIGGED L1 DOOR, DOOR OPERATED NORMALLY. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN OPERATED NORMALLY INITIALLY AND THEN BECAME INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X)

Part: FLOORBEAM — CORRODED (BS 967)

PHX - DURING SCHEDULED SI CHECK, THE FORWARD AND AFT TOP FLANGED OF THE FLOORBEAM AT STATION 967, LBL 14-21 AND 23-33 WAS FOUND TO BE CORRODED. REPAIRED PER SRM 53-00-51 FIG 202. (M)

Part: FLOORBEAM — DAMAGED (BS 986.5)

PHX - DURING SCHEDULED SI CHECK, THE TOP FLANGES OF THE FLOORBEAM AT STATION 986.5, LBL 33 - RBL 30 WERE FOUND TO BE GOUGED AND CORRODED. REPAIRED PER EA 5310-01697. (M)

Part: SKIN — LIGHTNING STRIKE (BS 360)

PHX - DURING SCHEDULED SI CHECK, THE EXTERNAL FUSELGE SKIN AT BS 360, STRINGER 17L WAS FOUND TO HAVE 2 LIGHTNING STRIKES. REPAIRED PER SRM 53-00-01, FIG 223. (M)

Part: CHORD — CORRODED (BS 947.5)

PHX - DURING SCHEDULED SI CHECK, THE RIGHT INNER CHORD AT THE R2 DOOR STATION 947.5 TO 957.5 WAS FOUND TO BE CORRODED. REPAIRED PER SRM 51-40-02. (M)

Part: FLOORBEAM — CORRODED (BS 947.5)

PHX - DURING SCHEDULED SI CHECK, THE FORWARD AND AFT FLANGES OF THE FLOORBEAM AT STATION 947.5, LBL 12-RBL 10 WERE FOUND TO BE CORRODED. REPAIRED PER EA 5310-01702. (M)

Part: FRAME — DENTED (BS 727)

PHX - DURING SCHEDULED SI CHECK, THE AFT CARGO COMPARTMENT TOP OF MAIN FRAME WAS FOUND TO BE DENTED AT BS 727E 30 INCHES BELOW STRINGER 22R AND BS 727F ABOVE STRINGER 25R. REPAIRED PER EA 5310-01701. (M)

Part: FLOORBEAM — CORRODED (BS 344)

PHX - DURING SCHEDULED SI CHECK, THE FLOORBEAM CAP UPPER SURFACE AT STATION 344, LBL 40-56 WAS FOUND TO BE CORRODED. REPAIRED PER SRM 53-00-51, FIG 203. (M)

Part: FLOORBEAM — CORRODED (BS 312)

PHX - DURING SCHEDULED SI CHECK, THE FLOORBEAM CAP UPPER SURFACE AT STATION 312 LBL 12 TO RBL 12 WAS FOUND TO BE CORRODED. REPAIRED PER SRM 53-10-01 FIG 205. (M)

Part: SUPPORT — CRACKED (RT AILERON)

PHX - DURING SCHEDULED SI CHECK, THE RT AILERON INBOARD HINGE SUPPORT WAS FOUND TO BE CRACKED AT THE NUTPLATE, OUTBOARD SIDE. REPAIRED PER EA 5740-01177. (M)

Part: WIRE — FAILED (ROW 6)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTING WAS FOUND TO BE INOPERATIVE AT ROWS 6-9. REPLACED WIRING HARNESS AT ROW 6, LIGHTS OPERATED NORMALLY. (M)

Part: CONNECTOR — LOOSE (CABIN)

KTN - FLT 73 - PRIOR TO FLT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 22-25 WOULD NOT ILLUMINATE DURING TEST. SECURED LOOSE CONNECTOR AT ROW 25 AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT NR 62 - CREW REPORTED AFT 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M)

Part: WIRE — DISCONNECTED (CABIN)

SEA - FLT NR 279 - CREW REPORTED, AFT MOST SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTING WAS INOPERATIVE. INSTALLED NEW LENS COVER AND SECURED TRACK AND WIRING, LIGHTS OPERATED NORMALLY. (M)

Part: END STOP — DEFECTIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 5 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED END STOP SECTION AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 5 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: WIRE — DISCONNECTED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE AFT 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL WIRING — DISCONNECTED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 22 THROUGH 26 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL WIRING — DISCONNECTED (AFT GALLEY)

SEA - FLT 625 - THE AFT 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED WIRING AT AFT GALLEY NR 3 AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 25 AFT. RECONNECTED WIRING AT ROW 25 AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING ON AFT TRACK AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL WIRING — DISCONNECTED (CABIN)

JNU - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING ON AFT TRACK AND LIGHTS OPERATED NORMALLY. (X)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - FLT NR 191 - CREW REPORTED AFT SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE. REPAIRED WIRING CONNECTION ON AFT TRACK AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD AND AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AT FORWARD AND AFT TRACKS AND LIGHTS OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

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

Part: EEL ASSY — INOPERATIVE (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD RED EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LIGHTS AND OPERATED NORMALLY. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - CHECK, AFT THREE TRACK LIGHTS INOP. MAINTENANCE RECONNECTED LIGHTS. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - CHECK, AFT THREE TRACK LIGHTS INOP. MAINTENANCE RECONNECTED WIRING. (W)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - AFT THREE PEEPLS LIGHTS INOP. MAINTENANCE RECONNECTED WIRING. (M)

Part: EEL WIRING — DISCONNECTED (CABIN)

SEA - DURING MAINTENANCE CHECK, THE FORWARD FOUR AND AFT FLOOR TRACK EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (W)

Part: EEL TRACK — DAMAGED (CABIN)

SEA - PILOT REPORTED, LAST 5 EMERGENCY TRACK LIGHTS DO NOT ILLUMINATE. REPLACED LIGHT SECTION AT ROW 26 AND SECURED LIGHT LENS. (W)

Part: EEL WIRING — LOOSE (CABIN)

PDX - CHECK, FLOOR TRACK LIGHTS INOP AT ROWS 28-36. MAINTENANCE RECONNECTED LOOSE BUS WIRE IN TRACK. (W)