N400WN

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 72,546 hrs · 43,059 cycles

ROW 16 AND 19 R/H EMERGENCY LIGHTS INOP<[01] R/R EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY AT STA 616 R/H AND AFT GALLEY CEILING R/H SIDE IAW AMM 33-51?06

Part: COVER — MISSING (ZN 200 FUS TOP) · airframe 72,169 hrs · 42,813 cycles

R1 DOOR SLIDE YELLOW COVER THAT COVERS PULL HANDLE UP IS MISSING.<[01] REPOSITIONED YELLOW SLIDE COVER IAW AMM 25-66-01.

Part: SKIN — CRACKED (ZN 500 LEFT WING) · airframe 71,300 hrs · 42,217 cycles

LEFT WING LOWER SKIN HAS A POSSIBLE CRACK AT FASTENER HOLE LOCATED O/B SIDE OF PYLON FAIRING & COMMON TO RUBSTRIP AT RIB 7, STR 10. INDICATION WAS SEEN WHILE PERFORMING NDT MANUAL PART 4 57-10-15. POSSIBLE CRACK HAD AN INDICATION OF APPROX. 45% FSH & WAS TO IMMEDIATE RT OF FASTENER HOLE. REMOVED FASTENER FOR HOLE PROBE, REWORKED RIVET HOLE BY REAMING TO 0.406 IAW SRM 51-40-02. COUNTERSINK REQUIRES REWORK. PERFORMED OPEN HOLE NDT INSP OF HOLE IAW NDT MANUAL PART 6 51-00-00 PROC. 16. INSP WAS INCONCLUSIVE DUE TO HOLE HAVING DAMAGE & MISSING MATERIAL INSIDE & COUNTERSINK. VISUALLY INSP OPEN HOLE AFTER REWORK. FOUND DAMAGE STILL REMAINING IN HOLE & COUNTERSINK AREA. REPAIR COMPLETED PER EA 23-157-01039.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 70,841 hrs · 41,925 cycles

FWD SERVICE DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REPLACED THE LIGHT ASSY IAW MM 33-51-01.

Part: STRINGER — ELONGATED (ZN 100 FUS LOWER) · airframe 70,388 hrs · 41,619 cycles

REJECT ELONGATED HOLE STRINGER 26L BS 520 AT FWD CARGO COMPARTMENT (1 EA) 2022-597095 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[02] REPLACED [7] STRINGER SECTION 26L; [1] HAT SECTION SPLICE; [4] SHIM (2E/A) LOCATED BTW BS 500D TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG# 143A3230 SHEET 37 REV A. SEE INDIVIDUAL SIGN OFF BELOW;[03] TASK CARD COMPLETED

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 70,388 hrs · 41,619 cycles

CRACKED SCUFF PLATE THRESHOLD IN THE FWD CARGO COMPARTMENT. REPAIRED THE SCUFF PLATE THRESHOLD IAW SRM 53-30-15-2R-1, REPAIR 1, PARAGRAPH 4.C, STEPS 2 & 4 - 7 AND BAC 5975.

Part: SUPPORT ANGLE — CRACKED (BS 500D S28L) · airframe 70,388 hrs · 41,619 cycles

CRACKED SUPPORT ANGLE, BS 500D STRINGER 28L IN THE FWD CARGO COMPARTMENT. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A7902, SHEET 126, REV A.

Part: STRINGER — CRACKED (BS 540 S22L) · airframe 70,388 hrs · 41,619 cycles

CRACKED STRINGER 22L, BS 540 IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1.

Part: STRINGER — CRACKED (BS 540 S26R) · airframe 70,388 hrs · 41,619 cycles

CRACKED STRINGER 26R, BS 540 IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1.

Part: WEB — CRACKED (BS 500D-520 S25R) · airframe 70,388 hrs · 41,619 cycles

CRACKED WEB, BS 500D-520, S25R IN THE FWD CARGO COMPARTMENT. REPLACED THE WEB IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A9801, SHEET 12, REV -.

Part: STRINGER — CRACKED (BS 540 S26L) · airframe 70,388 hrs · 41,619 cycles

CRACKED STRINGER 26L, BS 540 IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1.

Part: STRINGER — CRACKED (BS 540 S27R) · airframe 70,388 hrs · 41,619 cycles

CRACKED STRINGER 27R, BS 540, IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1.

Part: STRINGER — CRACKED (BS 540 S27L) · airframe 70,388 hrs · 41,619 cycles

CRACK STRINGER 27L LOCATED BS 540 IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1

Part: WEB — CRACKED (BS 500D-520 S28R) · airframe 70,388 hrs · 41,619 cycles

CRACKED WEB, BS 500D-520, S28R IN THE FWD CARGO COMPARTMENT. REPLACED THE WEB IAW SRM 51-10-02, AND DWG 143A7902, SHEET 26, REV A.

Part: STRINGER — CRACKED (BS 540 S23R) · airframe 70,388 hrs · 41,619 cycles

CRACKED STRINGER 23R, BS 540 IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-02-2R-1, REPAIR 1.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 70,388 hrs · 41,619 cycles

CRACKED FWD CORNER OF SCUFF PLATE IN THE FWD CARGO COMPARTMENT. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 70,388 hrs · 41,619 cycles

CRACKED FWD CORNER OF SCUFF PLATE IN THE AFT CARGO COMPARTMENT. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4.B, STEPS 2 - 7, AND BAC 5975.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 70,388 hrs · 41,619 cycles

CRACK ON SUPPORT ANGLE LOCATED TRAILING EDGE AT LEVEL ORSS 297 RT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, 51-40-02, AND DWG 115A3712, SHEET 6, REV B.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 70,388 hrs · 41,619 cycles

CRACK SUPPORT ANGLE AT LEVEL ORSS 297 TRAILING EDGE AT LT WING. REPLACED SUPPORT ANGLE AT LEVEL ORSS 297 TRAILING EDGE AT LT WING IAW SRM B737-700 51-40-02, AND SRM B737-700 51-10-02 ITEM 9.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 70,388 hrs · 41,619 cycles

BROKEN GALLEY 1 EMERGENCY EXIT LENS ASSY AT FWD GALLEY AREA. REPLACED THE GALLEY EMERGENCY EXIT LENS IAW AMM 33-51-01-960-802. OPS TESTED OK

Part: PLATE — CRACKED (LT WING) · airframe 70,388 hrs · 41,619 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT LT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02.

Part: FRAME — CRACKED (BS 727D S8-9L) · airframe 70,388 hrs · 41,619 cycles

CRACKED FRAME, BS 727D, STRINGERS 8L - 9L. REPAIRED THE FRAME IAW EA 1-A53-12114.

Part: STRINGER — CRACKED (BS 540 S23L) · airframe 70,388 hrs · 41,619 cycles

CRACKED STRINGER 23L, BS 540 IN THE FWD CARGO COMPARTMENT. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1.

Part: PLATE — CRACKED (LT WING) · airframe 70,388 hrs · 41,619 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 219, LT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02.

Part: LIGHT — BROKEN (CABIN) · airframe 70,388 hrs · 41,619 cycles

BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (4 EA) 2022-596937 / [01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-15-400-802

Part: FRAME — CRACKED (BS 747 S8-9L) · airframe 70,388 hrs · 41,619 cycles

CRACK FRAME, BS 747, STRINGERS 8L - 9L. REPAIRED THE FRAME IAW EA 1-A53-12114.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 70,388 hrs · 41,619 cycles

CRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL AT STAB STA 193.9 RIB AND 8.750 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.5 INCH. PERFORMED REPAIR ON THE LOWER SKIN IAW SRM 55-10-01-2R-11, REPAIR 11.

Part: SUPPORT ANGLE — CRACKED (BS 695) · airframe 70,388 hrs · 41,619 cycles

CRACK SUPPORT ANGLE BS 695 LBL 24.82. REPLACED SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 273A9110, SHEET 3, REV -.

Part: SUPPORT ANGLE — CRACKED (BS 695) · airframe 70,388 hrs · 41,619 cycles

CRACK SUPPORT ANGLE BS 695 LBL 0.07. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, AND DWG 273A9110, SHEET 3, REV.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 70,388 hrs · 41,619 cycles

CRACK SUPPORT ANGLE BS 695 RBL 24.82. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 273A9110, SHEET 3, REV -.

Part: NONE — CRACKED (LH HOR STAB) · airframe 70,238 hrs · 41,520 cycles

LEFT HORIZONTAL STABILIZER FORWARD LOWER SLIDER SEAL CRACKED. / [01] REMOVED AND REPLACED SLIDER SEAL PER SRM 51-40-02.;[02] REMOVED AND REPLACED SLIDER SEAL PER M/M 53-31-31.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 68,928 hrs · 40,638 cycles

COCKPIT EMERGENCY LIGHT SWITCH INOP. / [01] R&R COCKPIT EMERGENCY LIGHT SWITCH PER SWPM 20-83-11. OPS CHECK GOOD PER AMM 33-51-00.

Part: RETAINER — CRACKED (LH WING) · airframe 68,284 hrs · 40,250 cycles

LEFT WING FIXED TRAILING EDGE PANEL AT DEFLECTION RIB; COVE SEAL RETAINER CRACKED. ; / [01] REMOVED AND REPLACED COVE SEAL RETAINER BRACKET AT LEFT WING DEFLECTION RIB IN REF TO SRM 51-40-02; [02] INSPECTED WORK PERFORMED

Part: LIGHT — INOPERATIVE (R/H CABIN) · airframe 68,284 hrs · 40,250 cycles

BULLNOSE EMERGENCY LIGHT INOP 23DEF ; / [01] RELAMPED PER AMM 33-51-03

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,907 hrs · 39,412 cycles

LH EXTERIOR OVER WING EXIT EMERGENCY LIGHT INOP. ; / [01] R/R PACK CHARGER ASSY PER MM 33-51-06

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 66,594 hrs · 39,232 cycles

REF: FORWARD ENTRY DOOR OVERHEAD EMERGENCY LIGHT LENS CAME OFF (TTG8Q005X0LG) ; / [01] REMOVED AND REPLACED FORWARD ENTRY DOOR EXIT SIGN AND LENS ASSEMBLY PER AMM 33-51-01. OPS CHECK GOOD.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 66,550 hrs · 39,206 cycles

FORWARD ENTRY DOOR OVERHEAD EMERGENCY LIGHT LENS CAME OFF. ; / [01] C/W EA M-21-133-00720.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 66,325 hrs · 39,077 cycles

AFT CARGO DOOR AFT SCUFF PLATE CRACKED ; / [01] REMOVED AFT CARGO COMP. AFT CORNER SCUFF PLATE FOR WELDING REPAIR PER B737-700 AMM 53-11-02-020-801; [02] OK; [03] OK TO REINSTALL SCUFF PLATE; [04] ACCOMPLISHED WELDING REPAIR AT AFT CARGO AFT CORNER OUT-SIDE BY J.L WELDING FAA REPAIR STATION # JWR146K. AS PER REF B737-700 SRM 53-60-15-2R-1 BAC 5975.; [05] INSTALLED AFT CARGO AFT CORNER SCUFF PLATE AS PER REF B737-700 SRM 53-11-02-420-801; [06] VERIFIED INSTALLATION OF SCUFF PLATE CORNERS; [07] REPAIRED AFT CARGO SCUFF PLATE AFT CORNER AS PER REF B737-700 SRM 53-60-15-2R-1 BAC 5975.; [08] COMPLETED REPAIR

Part: COVER — OUT OF POSITION (R2 DOOR GIRT BAR) · airframe 66,325 hrs · 39,077 cycles

AFT SERVICE DOOR SLIDE GIRT MANUAL INFLATION COVER INCORRECTLY POSITIONED / [01] REPOSITIONED AFT SERVICE DOOR GIRT MANUAL INFLATION COVER; REF:AMM 25-66-01-400-803.; [02] VERIFIED STEP 1

Part: BAFFLE — CRACKED (BS 500A-500B) · airframe 66,325 hrs · 39,077 cycles

FWD CARGO COMP. BAFFLE BETWEEN STA 500A TRHU 500B STR.25L IS CRACKED ; / [01] REMOVED BAFFLE AS REF. B737-700 SRM 51-40-02-0G-0; [02] CUTED BAFFLE THROUGH ITS WEB FROM THE TOP FLANGE TO THE LIGHTING HOLE TO FACILITATE WIRE BUNDLE INSTALATION AS REF. B737-700 SRM 53-30-53-2R-1; [03] FABRICATED REPAIR ANGLE AS REF.B737-700 SRM 53-30-53-2R-1 MATERIAL USED 7075T6.032' PO#1644231; [04] VERIFIED STEPS#1; #2 AND #3.; [05] PERFORMED HFEC ROTO ON EXISTING FASTENER HOLES IN REPAIR ANGLE AND EXISITING FASTENER HOLE COMMON TO REPAIR AREA IAW NDTM PART 6;51-00-00 PROCEDURE 16.NO CRACKS.<BR>[NORTEC 600 ;B/C 166316]; [06] PERFORMED GENERAL VISUAL INSPECTION AT THE REPAIR AREA AND NO DEFECTS NOTED.; [07] OK TO INSTALL REPAIR; AND NEW BAFFLE.; [08] CORRECTING STEP # 7; OK TO TREAT AND PRIME REPAIR ANGLE.; [09] TREATED AND PRIMED REPAIR ANGLE PER B737-700 SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804.; [10] VERIFIED THE TREAT AND PRIME OF REPAIR ANGLE PER B737-700 SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804.; [11] OK TO INSTALL REPAIR ANGLE ON NEW BAFFLE AND OK TO INSTALL NEW BAFFLE.; [12] INSTALLED REPAIR ANGLE ON NEW BAFFLE TO FACILITATE WIRE BUNDLE INSTALLATION PER B737-700 SRM 53-30-53-2R-1 FIG 202 AND INSTALLED NEW BAFFLE BETWEEN STA 500A AND 500B LBL25 PER B737-700 SRM 51-40-02-0G-0 AND DWG # 143A7505

Part: ANGLE — CRACKED (BS 500A-500B) · airframe 66,325 hrs · 39,077 cycles

FOUND 1 CLIP CRACKED AT FWD CARGO COMP. BETWEEN STA 500A FWD THRU STA 500B ; / [01] REMOVED AND REPLACED CLIP P/N 143A7502-158 PER B737-700 SRM 51-40-02-0G-0 AND DWG #143A7505.; [02] VERIFIED REMOVAL AND REPLACEMENT OF CLIP P/N 143A7502-158 PER B737-700 SRM 51-40-02-0G-0 AND DWG #143A7505.

Part: BAFFLE — CRACKED (BS 500A-500B) · airframe 66,325 hrs · 39,077 cycles

FOUND 1 EACH BAFFLE CRACKED AT FWD CARGO COMP. BETWEEN STA 500A THRU 500B STR 25R ; / [01] FABRICATED ANGLE DOUBLER REPAIR; [02] VERIFIED CRACK DIMENSIONS AND LOCATION.; [03] FABRICATED REPAIR ANGLE PER B737-700 SRM 53-30-53-2R-1; MATERIAL USED 7075-T6.032' PO# 1641456.; [04] CUT OUT NEW BAFFLE TOP FLANGE TO LIGHTNING HOLE TO FACILITATE INSTALLATION OF WIRE BUNDLE PER B737-700 SRM 53-30-53-2R-1 FIG 202.; [05] VERIFIED STEPS 3 AND 4; FABRICATED REPAIR ANGLE PER B737-700 SRM 53-30-53-2R-1; MATERIAL USED 7075-T6.032' PO# 1641456. CUT OUT NEW BAFFLE TOP FLANGE TO LIGHTNING HOLE TO FACILITATE INSTALLATION OF WIRE BUNDLE PER B737-700 SRM 53-30-53-2R-1 FIG 202; [06] PERFORMED HFEC ROTO ON OPEN FASTENER HOLES ON REPAIR ANGLE AND BAFFLE IAW NDTM PART 6 ;51-00-00 PROCEDURE 16. NO CRACKS. [07] ACCOMPLISHED VISUAL INSPECTION; NO DEFECT NOTED. [12] REMOVED CRACKED BAFFLE FROM FWD CARGO BETWEEN STA 500A AND 500B PER B737-700 SRM 51-40-02-0G-0.; [13] VERIFIED REMOVED CRACKED BAFFLE FROM FWD CARGO BETWEEN STA 500A AND 500B PER B737-700 SRM 51-40-02-0G-0.; [14] OK TO INSTALL NEW BAFFLE.; [15] STARTED INSTALLATION OF REPAIR AND NEW BAFFLE BETWEEN STA 500A AND 500B RBL 24 PER B737-700 SRM 53-30-53-2R-1 AND B737-700 SRM 51-40-02-0G-0.; [16] COMPLETED INSTALLATION OF REPAIR ON NEW BAFFLE AND INSTALLED NEW BAFFLE PER B737-700 SRM 51-40-02-0G-0 AND DRWG #143A7505

Part: BAFFLE — CRACKED (BS 500B-500C) · airframe 66,325 hrs · 39,077 cycles

FOUND 1 EACH BAFFLE CRACKED AT FWD CARGO COMP. BETWEEN STA 500B THRU 500C STR 25R ; / [01] REMOVED BAFFLE AY; [02] CORRECTING STEP 1; REMOVED CRACKED BAFFLE FROM FWD CARGO COMP. BETWEEN STA 500B AND 500C PER B737-700 SRM 51-40-02-0G-0.; [03] LOCATED AND DRILLED NEW BAFFLE P/N 143A7510-12 PER B737-700 SRM 51-10-02-0G-0.; [04] VERIFIED STEPS 2 AND 3 CORRECTING STEP 1; REMOVED CRACKED BAFFLE FROM FWD CARGO COMP. BETWEEN STA 500B AND 500C PER B737-700 SRM 51-40-02-0G-0 <BR>LOCATED AND DRILLED NEW BAFFLE P/N 143A7510-12 PER B737-700 SRM 51-10-02-0G-0.; [05] OK TO INSTALL NEW BAFFLE.; [06] STARTED INSTALLATION OF NEW BAFFLE BETWEEN STA 500B AND 500C RBL 24 PER B737-700 SRM 51-40-02-0G-0.; [07] COMPLETED INSTALLATION OF NEW BAFFLE BETWEEN STA 500B AND 500C RBL24 PER B737-700 SRM 51-40-02-0G-0 AND DRWG #143A7505.; [08] VERIFIED COMPLETION OF INSTALLATION OF NEW BAFFLE BETWEEN STA 500B AND 500C RBL24 PER B737-700 SRM 51-40-02-0G-0 AND DRWG #143A7505.

Part: DOOR FRAME — CRACKED (R1) · airframe 66,325 hrs · 39,077 cycles

R- 1DOOR FUSELAGE CUTOUT CRACKED @ FORWARD JAMB EDGE UPPER LATCH FITTING. STARTED INSTALLATION OF NEW FRAME SECTION PER B737-700 SRM 51-40-02-0G-0 AND DRAWING # 141A8370.

Part: ANGLE — CRACKED (BS 500 S26L) · airframe 66,325 hrs · 39,077 cycles

FOUND CLIP CRACKED AT FWD CARGO COMP. STA 500 STR 26L AFT SECTION BILGE AREA ; / [01] REMOVED CLIP AND BAFFLE AT FWD CARGO COMP STA 500 STR 26L B737-700 SRM 51 40 02; [02] CERTIFIED REMOVAL OF CLIP AND BAFFLE AT STA 500 STR 26L PER B737-700 SRM 51-40-02-0G-0.; [03] VERIFIED STEPS 1 AND 2; [04] LOCATED AND DRILLED NEW BRACKET (CLIP) AS REFERENCE B737-700 SRM 51-10-02-0G-0; [05] TREATED AND PRIMED DRILLED HOLES AS REFERENCE B737-700 SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804; [06] CERTIFIED; [07] VERIFIED STEPS 4 AND 5.; [08] OK TO INSTALL CLIP AND BAFFLE.; [09] INSTALLED BAFFLE AND CLIP AS REFERENCE B737-700 SRM 51-40-02-0G-0; [10] REMOVED AND REPLACED CLIP AS REFERENCE B737-700 SRM 51-40-02-0G-0; [11] CERTIFIED INST.BAFFLE AND CLIP; [12] VERIFIED INSTALLATION OF BAFFLE AND CLIP

Part: ACCESS PANEL — DELAMINATED (HORIZONTAL STAB) · airframe 66,325 hrs · 39,077 cycles

L/H HORIZONTAL STABILIZER ACCESS PANEL #334 LB DELAMINATION ; / [01] REPLACED L/H HORIZONTAL STAB. ACCESS PANEL #334LB REF. B737-700 AMM 55-05-03-211-807. PANEL (COVER) WILL BE INSTALLED ON FAULT #TTG8Q004XDZ3; [02] REPLACED L/H HORIZONTAL STAB. ACCESS PANEL #334LB REF. B737-700 AMM 55-05-03-211-807. PANEL (COVER) WILL BE INSTALLED ON FAULT #TTG8Q004XDZ3; [03] VERIFIED 2;COMPLETE

Part: SIGN — BROKEN (MAIN CABIN) · airframe 66,325 hrs · 39,077 cycles

MAIN CABIN O/W CEILING EXIT SIGN IS BROKEN. ; / [01] REMOVED AND REPLACED MAIN CABIN O/W CEILING EXIT SIGN HOUSING IAW BOEING 737-700 AMM 33-51-01-960-801.; [02] VERIFICATION OF PARTS REPLACEMENT; [03] VERIFIED THE REMOVAL AND REPLACEMENT OF MAIN CABIN O/W CEILING EXIT SIGN HOUSING IAW BOEING 737-700 AMM 33-51-01-960-801.

Part: WEB — CORRODED (BS 827-867) · airframe 66,325 hrs · 39,077 cycles

CORROSION ON MAIN CABIN L/H O/B SEAT TRACK WEB FROM STA 827 TO STA 867.

Part: PLENUM — CRACKED (APU INLET) · airframe 66,325 hrs · 39,077 cycles

APU AIR INLET PLENUM TOP AFT PANEL ASSEMBLY CRACKED (PN:353A2010-16) ; / [01] RECEIVED NEW APU INLET PLENUM TOP AFT PANEL S/N: 588009-131702. INSTALLATION WILL BE PERFORMED ON TASK CARD TTG8Q0034VK5; [02] OK VERIFIED STATEMENT; [03] VERIFIED PART REPACEMENT; [04] VERIFIED PART REPLACEMENT

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 66,325 hrs · 39,077 cycles

MAIN CABIN FWD WET AREA FLOOR PANEL #221BF HAS A CORNER CRACKED AT AFT I/B AREA (MKD) ; / [01] CLEANED THE DAMAGEG AREA AND PREPARED DAMAGE AREA TO APPLY REPAIR REF B737-7 SRM 53-00-50-2R-9 .; [02] VERIFIED DAMAGED AREA IS CLEANED TO INSTALLED REPAIR PER B737-700 SRM 53-00-50-2R-9; [03] OK TO INSTALL REPAIR ON PANEL # 221BF; [04] MEASUREMENTS; [05] APPLIED REPAIR AT MAIN CABIN FLOOR PANEL 221BF REF B737- 700 SRM 53-00-50-2R-9.; [06] JOB COMPLETED; [07] RII VERIFIED REPAIR INSTALLED ON FLOOR PANEL # 221 BF AS PER B737-700 53-00-50-2R-9; [08] VERIFIED REPAIR ON PANEL # 221BF; [09] VERIFIED RII

Part: DUCT — CORRODED (THRUST REVERSER) · airframe 66,325 hrs · 39,077 cycles

NR 2 ENGINE INBOARD THRUST REVERSER INNER C DUCT INNER TRAILING EDGE SURFACE CORRODED ; / [01] PARTIALLY REMOVED CORROSION ON NR 2 ENG I/B T/R INNER C DUCT INNER T/E TO CHECK LIMITS. PER B-737-700 SRM 51-10-02-0G-0.; [02] VERIFIED PARTIAL REMOVAL OF CORROSION.; [03] MEASURED AREA PER B-737-700 SRM 54-30-01-1A-4 STEP 4.A(2) FIG 102 DETAIL C ;DEEPEST CORROSION PIT FOUND .028' FOUND OUT OF LIMITS; [04] VERIFIED OUT OF LIMITS.; [05] REMOVED #1 ENGINE I/B T/R REF B737-700 AMM 78-31-01-000-801 P/N 315A2295-673 S# 000750; [06] OK TO INSTALL SERVICEABLE T/R.; [07] ACCOMPLISHED #2 ENG INBOARD THRUST REVERSER INSTALLATION REFERENCE AMM 78-31-01-400-801-F00 P/N 315A2295-681 S/N 1371 UP TO STEP I.(9)(A) .TORQUE WRENCH B/C 16671 CALIBRATION DUE 01/26/22.; [08] VERIFIED STEP #7; [09] COMPLETED INSTALLATION OF #2 ENG INBOARD THRUST REVERSER REFERENCE AMM 78-31-01-400-801-F00 FROM STEP I.(10) TO I. (20) END OF TASK .PERFORMED ADJUSTMENT REFERENCE AMM 78-31-01-820-801-FOO SYSTEM LEAK CHECK; NO LEAKS NOTED;AND OPS CHECK NORMAL REFERENCE AMM 78-31-00-700-804-FOO;78-31-00-700-801-FOO;78-31-11-820-801-FOO;AND 78-31-03-700-801-FOO.NOTE: SLING P/N C78018-50 B/C# 160489 LOAD TEST DUE 08/2021;DYNAMOMETER B/C 160108 CALIBRATION DUE 26-SEP-21; PUSH PULL SCALE B/C 167240 CALIBRATION DUE 28-AUG-21;AND TORQUE WRENCH B/C 164347 CALIBRATION DUE 22-MAR-22.; [10] COMPLETED INSTALLATION T/R

Part: SUPPORT CHANNEL — CORRODED (BS 727A-847 S25L) · airframe 66,325 hrs · 39,077 cycles

AFT CARGO FLOOR SUPPORT 'Z' CHANNEL IS CORRODED AT 727A TO 847 S25L DOT # 3 ; / [01] REMOVED CORROSION AT Z CHANNEL STA 727A TO 847 S25 L PER REF B 737 - 700 SRM 51-10-02-0G-0; [02] JOB CERTIFIED; [03] VERIFIED REMOVAL CORROSION AT Z CHANNEL ; PENDING NDT; [04] PERFORMED UT THICKNESS INSP AT REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3; MIN THICKNESS NOTED 0.025'<BR>TOOL USED OLYMPUS 27MG BC:172139; [05] EVALUATE REWORKED AREA: ORIGINAL THICKNESS .040'; MATERIAL LOST .015'; MATERIAL REMAINING .025'. FOUND OUT OF LIMIT AS PER REF B737-700 SRM 53-00-53-1A-2; [06] VERIFIED MATERIAL LOSS IN REWORK AREA PER SRM 53-00-53. FABRICATION REQUIRED; [07] LOCATED; DRILLED AND FABRICATED AFT CARGO FLOOR 'Z' CHANEL AT STA 727A TO 847 S25L AS PER REF B737-700 SRM 51-40-05-0G-0; [08] VERIFIED. JOB ACCOMPLISHED. OK TO TREAT AND PRIMER; [09] TREADED AND PRIMED AFT CARGO FLOOR SUPPORT Z CHANEL AS PER REF B737-700 AMM 51-21-41-370-801; [10] VERIFIED TREAT AND PRIMER ;OK TO INSTALL NUTPLATE AND ANGLES; [11] ACCOMPLISHED CHART; [12] INSTALLED NUT PLATE AT ZEE CHANNEL AS PER REF 737-700 SRM 51-40-02; [13] CERTIFIED NUT-PLATES INSTALLATION; [14] VERIFIED NUT PLATE INSTALLATION.; [15] REMOVED CORROSION AFT CARGO FLOOR 'Z' CHANEL AT STA 727A TO 847 S25L. FOUND OUT OF LIMITS; FABRICATED AS PER REF B737-700 SRM 51-40-05-0G-0.; [16] VERIFIED WORK ACCOMPLISHED

Part: SUPPORT CHANNEL — CORRODED (BS 727A-767 S25R) · airframe 66,325 hrs · 39,077 cycles

AFT CARGO FLOOR SUPPORT 'Z' CHANNEL IS CORRODED AT 727A - 767 S25R ; / [01] REMOVED NUTPLATES TO ACCESS REMOVAL CORROSION AT AFT CARGO FLOOR SUPPORT Z CHANNEL AS PER REF B737 SRM 51-40-02-0G-0.; [02] REMOVED CORROSION AT FLOOR SUPPORT Z CHANNEL AS PER REF B737 SRM 51-10-02-0G-0.; CORROSION REMOVAL VERIFIED ON FLOOR SUPPORT Z CHANNEL PER SRM 50-10-02; [04] PERFORMED UT THICKNESS INSP AT REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THICKNESS NOTED 0.031'<BR>TOOL USED : OLYPUS 27MG BC:172139 EVALUATED AREA; ORIGINAL THICK .040; MAT LOST .009; MAT. REMAINING .031; FOUND TO BE OUT OF LIMITS AS PER REF B737 SRM 53-00-53-1A-2.; [06] VERIFIED EVALUATED AREA TO BE OUT OF LIMIT PER SRM 53-00-53; [07] LOCATED AND DRILLED NEW Z CHANNEL P/N BAC1496-377 AS PER REF B737 SRM 51-40-05-0G-0 AND SRM 53-70-53-0I-2 TABLE 2. VERIFIED JOB ACCOMPLISHED.

Part: FLOORBEAM — CRACKED (BS 328 RBL 20) · airframe 66,325 hrs · 39,077 cycles

FWD CABIN WET AREA FLOOR BEAM FWD FLANGE CRACKED AT FASTENER HOLE AT STA 328 RBL20. ; / [01] PERFORMED HFEC ON CRACK AT FWD CABIN WET AREA FLOOR BEAM THROUGH FASTENER HOLE AT STA 328 RBL 20 ; IAW NDTM PART 6 ;51-00-00; PROCEDURE 23.LENGTH OF CRACK : 1.181'; [02] VERIFIED CRACK DIMENSIONS AND LOCATIONTO THE DAMAGED FLOOR BEAM PER B737-700 SRM 51-40-02-0G-0CUT OUT AND REMOVED THE DAMAGED FLANGES OF THE UPPER CHORD OF THE FLOOR BEAM AT STA 328 FROM RBL 1.1 TO RBL 64.6 PER B737-700 SRM 53-10-51-2R-7 FIG 205.; [08] VERIFIED CUT OUT AND REMOVED THE DAMAGED FLANGES OF THE UPPER CHORD OF THE FLOOR BEAM AT STA 328 FROM RBL 1.1 TO RBL 64.6 PER B737-700 SRM 53-10-51-2R-7 FIG 205.;] TRIMMED OUT TOP EDGE OF STIFFENER AT THE REPAIR SPLICE AREA AND TRIMMED OUT THE FLANGE FROM THE TOP TWO FASTENERS OF THE MACHINED INTERCOSTAL ATTACHED TO FLOOR BEAM BL 24.82 PER B737-700 SRM 53-10-51-2R-7 STEP 4E;F. FLAP PEENED REWORKED AREAS PER SOPM 20-10-03. NEW T-CHORD AND SPLICE ANGLES PER B737-700 SRM 53-10-51-2R-7 FIG 205.; CONTINUE FABRICATION NEW T-CHORD AND SPLICE ANGLES PER B737-700 SRM 53-10-51-2R-7 FIG 205. FAB NEW T CHORD AND SPLICE PER B737-700 SRM 53-10-51-2R-7VERIFIED FABRICATION OF REPAIR PARTS PER B737-700 SRM 53-10-51-2R-7 FIG 205 PERFORMED DYE PENETRANT INSPECTION ON FABRICATED NEW T CHORD IAW SOPM 20-20-02. NO CRACKS FOUND.OK TO INSTALL REPAIR PARTS

Part: FLOOR SUPPORT — CRACKED (BS 285-294 BL 0) · airframe 66,325 hrs · 39,077 cycles

FLOOR STRUCTURE INTERCOSTAL CRACKED AT FASTENER HOLES BETWEEN STA 285.62 AND 294.5 BL0 ; / [01] EVALUATE DAMAGE AND VERIFIED P/N; [02] APPLIED EWIS PROTECTION AT AREA OF INTERCOSTAL PER B737-700 AMM 20-60-07-913-801.; [03] REMOVED CRACKER INTERCOSTAL PER B737-700 SRM 51-40-02-0G-0.; [04] VERIFIED REMOVAL OF CRACKED INTERCOSTAL BETWEEN STA 285.62 AND 294.5 BL0.; [05] LOCATED AND DRILLED NEW INTERCOSTAL PER B737-700 SRM 51-10-02-0G-0; [06] OK TO INSTALL NEW INTERCOSTAL RII; [07] OK TO INSTALL NEW INTERCOSTAL RII; [08] OK TO INSTALL; [09] INSTALLED INTERCOSTAL BETWEEN STA 285.62 AND 294.5 BL0 PER B737-700 SRM 51-40-02-0G-0 AND DRWG# 141A5400.; [10] VERIFIED INSTALLATION INTERCOSTAL BETWEEN STA 285.62 AND 294.5 BL0 PER B737-700 SRM 51-40-02-0G-0 AND DRWG# 141A5400.; [11] STEP 9 LATE ENTRY; AFTER INSTALLATION OF INTERCOSTAL; REMOVED EWIS PROTECTION PER B737AMM 20-60-07-913-801; [12] CERTIFIED EWIS PROTECTION REMOVAL

Part: SUPPORT — CORRODED (BS 303 S16-17L) · airframe 66,325 hrs · 39,077 cycles

** CORROSION ** @ FWD CABIN WET AREA L/H SIDE WALL FRAME SUPPORT L-1 D0OR CUTOUT FWD LOWER BETWEEN S-16L AND S-17L STA 303.9 ; / ACCOMPLISHED REPAIR AT L/H FRAME STA 303.9 INNER CHORD (AFT FLANGE) BETWEEN STR 16L AND 17L PER EA 21 153-01415.[06] PERFORMED HFEC ROTO ON OPEN FASTENER HOLES WITHIN REPAIR AREA OF L/H SIDE WALL FRAME SUPPORT STA 303.9 ;BET. S-16L AND S-17L; IAW NDTM PART 6 ; 51-00-00;PROCEDURE 16. NO CRACKS.; [07] PERFORMED HFEC ON REWORKED SURFACE OF LH SIDE WALL FRAME SUPPORT CUTOUT FWD LOWER AREA STA 303.0 BETWEEN S-16L AND S-17L IAW NDTM PART 6 ; 51-00-00 ;PROCEDURE 23. NO CRACKS FOUND.; [08] SUMMARY EA 21-153-01415 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO THE FAULT BARCODE TTG8Q0052M77.; [09] FASTENER REMOVED ON STEP 1 WAS INSTALLED ON CARD #TTG8Q005796W PER EA 21-153-01415-WIP1 STEP 11.; [10] ACCOMPLISHED REPAIR AT FRAME STA 303.9 BETWEEN 16L AND 17L PER EA 21-153-01415; CARD # TTG8Q005796W.; [11] RII. VERIFIED FRAME REPAIR AT STA 303.9 BETWEEN STG 16L AND 17L; [12] REPAIR ACCOMPLISHED PER EA 21-153-01415 ON TASK CARD NR TTG8Q005796W.

Part: SUPPORT — CORRODED (BS 303 S16-17L) · airframe 66,325 hrs · 39,077 cycles

** CORROSION ** @ FWD CABIN WET AREA L/H SIDE WALL FRAME SUPPORT L-1 D0OR CUTOUT FWD LOWER BETWEEN S-16L AND S-17L STA 303.9 ; / EA 21-153-01415-WIP1 IS COMPLETED AND SIGNED OFF ON CARD #TTG8Q005796W. VERIFIED ACCOMPLISHED REPAIR AT L/H FRAME STA 303.9 INNER CHORD (AFT FLANGE) BETWEEN STR 16L AND 17L PER EA 21 153-01415.

Part: FLOORBEAM — CRACKED (BS 332 RBL 32) · airframe 66,325 hrs · 39,077 cycles

FWD WET AREA FOOR SUPPORT BEAM CRACKED @ FWD FLANGE FASTENER HOLE RBL 32 AND STA 332 ; / [01] PERFORMED HFEC AND CONFIRMED CRACK AT FWD FLANGE FASTENER HOLE OF FWD WET AREA FLOOR SUPPORT BEAM RBL 32 AND STA 332 IAW NDT PART 6;51-00-00 PROCEDURE 23. CRACK LENGTH : 0.393'.; [02] ITEM ENTER IN ERROR - WRONG STA - THIS ITEM WILL ACCOMPLISHED ON N/R # TTG8Q0052WF4; [03] ITEM ENTER IN ERROR - WRONG STA - THIS ITEM WILL ACCOMPLISHED ON N/R # TTG8Q0052WF4 - CUT OUT AND REMOVED THE DAMAGED FLANGES OF THE UPPER CHORD OF THE FLOOR BEAM AT STA 328 FROM RBL 1.1 TO RBL 64.6 PER B737-700 SRM 53-10-51-2R-7 FIG 205.

Part: FLOORBEAM — CORRODED (BS 328 RBL 37-45) · airframe 66,325 hrs · 39,077 cycles

** CORROSION ** FWD CABIN WET AREA FLOOR BEAM UPPER FLANGE FWD 2EA FASTENER HOLES AT STA 328 RBL 37 AND RBL 45.5 ; / [01] REMOVED CORROSION AT FWD WET AREA;FLOOR BEAM UPPER FLANGE;FWD SIDE;2EA FASTENER HOLES.AT STA 328; RBL 37 AND RBL 45.5.PER B737-700 SRM 51-10-02-0G-0.; [02] VERIFIED CORROSION REMOVAL STEP # 1; [03] PERFORMED UT THICKNESS INSP ON REWORKED AREA AT ;FLOOR BEAM UPPER FLANGE;FWD SIDE;2EA FASTENER HOLES.AT STA 328; RBL 37 (MIN. THICKNESS .098'0 AND RBL 45.5 (MIN. THICKNESS .088'0) PER B-737 NDT PART 4; 51-00-00 PROC 3.; [04] AFTER UT THICKNESS CHECK; FOUND REWORKED AREA OUT OF LIMITS.PER B-737 700 SRM 53-10-51-1A-1.ORIGINAL THICKNESS 0.125''; MATERIAL REMAINING 0.088 '';MATERIAL REMOVED 0.037''; [05] VERIFIED CORROSION IS OUT OF LIMITS PER SRM 53-10-51-1A-1; [06] THIS N/R WAS ACCOMPLISHED ON TASK CARD #TTG8Q0052WF4 REPLACING UPPER T-CHORD AT FLOOR BEAM STA 328 BETWEEN RBL 1.1 AND RBL 64.6 PER SRM 53-10-51-2R-7 REPAIR 7 FIG 205.; [07] VERIFIED THIS N/R WAS ACCOMPLISHED ON TASK CARD #TTG8Q0052WF4 REPLACING UPPER T-CHORD AT FLOOR BEAM STA 328 BETWEEN RBL 1.1 AND RBL 64.6 PER SRM 53-10-51-2R-7 REPAIR 7 FIG 205.

Part: SUPPORT — CORRODED (BS 303 S16-17L) · airframe 66,325 hrs · 39,077 cycles

** CORROSION ** @ FWD CABIN WET AREA L/H SIDE WALL FRAME SUPPORT L-1 D0OR CUTOUT FWD LOWER BETWEEN S-16L AND S-17L STA 303.9 ; / ACCOMPLISHED REPAIR AT L/H FRAME STA 303.9 INNER CHORD (AFT FLANGE) BETWEEN STR 16L AND 17L PER EA 21 153-01415.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 66,325 hrs · 39,077 cycles

CABIN FLOOR PANEL 241ABF AFT I/B CORNER DISBONDED ; / [01] PREPARED DAMAGED AREA FOR REPAIR AT FLOOR PANEL #241ABT PER B737SRM 53-00-50-2R-9; [02] VERIFIED PREPARATION OF AREA FOR REPAIR.; [03] MEASUREMENT; [04] REPAIRED DAMAGED AREA AT FLOOR PANEL #241ABF PER B 737SRM 53-00-50-2R-9MATERIAL USED RESIN 50-A P/O#1692653 & FIBER GLASS P/O#1690463; [05] LATE ENTRY : VERIFIED STEP 3; [06] VERIFIED STEP 4; [07] VERIFIED STEP 4; [08] RII INSP COMPLETED FPO REPAIR; [09] ENTERED IN ERROR. INDEPENDENT INSPECTION IS NOT REQUIRED PER MPM.

Part: SUPPORT BRACKET — CRACKED (BS 500C S26L) · airframe 66,325 hrs · 39,077 cycles

FWD CARGO COMPARTMENT. BILGE SUPPORT BRACKET CRACKED @ S-26L STA 500C ; / [01] REMOVED BRACKET (CLIP) AT FWD CARGO COMP. STA 500 S-26L FWD SECTION PER SRM 51-40-02-0G; [02] VERIFIED <BR>REMOVED BRACKET (CLIP) AT FWD CARGO COMP. STA 500 S-26L FWD SECTION PER SRM 51-40-02; [03] LOCATED AND DRILLED NEW BRACKET (CLIP) AS REFERENCE B737-700 SRM 51-10-02-0G-0; [04] TREATED AND PRIMED DRILLED HOLES AS REFERENCE B737-700 SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804; [05] CERTIFIED; [06] VERIFIED STEPS 3 AND 4.; [07] OK TO INSTALL NEW CLIP [BRACKET].; [08] INSTALLED NEW BRACKET(CLIP) AS REFERENCE B737-700 SRM51-40-02-0G-0; [09] REMOVED AND REPLACED BRACKET(CLIP) AS REFERENCE B737-700 SRM 51-40-02-0G-0; [10] CERTIFIED INST. BRACKET; [11] VERIFIED REMOVAL AND REPLACEMENT OF BRACKET [CLIP]

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 66,325 hrs · 39,077 cycles

FWD CARGO COMPARTMENT GASSET CRACKED @ S-19R STA 500D ; / [01] REMOVED CRACKED GUSSET AT FWD CARGO STA 500D S-19R PER B737-700 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW GUSSET PER B737-700 SRM 51-10-02-0G-0.; [03] VERIFIED OK.; [04] OK TO INSTALL NEW GUSSET; [05] INSTALLED NEW GUSSET AT FWD CARGO COMP. STA 500D S-19R PER B737-700 SRM 51-40-02-0G-0.; [06] VERIFIED INSTALLATION OF NEW GUSSET AT FWD CARGO COMP. STA 500D S-19R PER B737-700 SRM 51-40-02-0G-0.; [07] VERIFIED INSTALLATION OF NEW GUSSET AT FWD CARGO COMP. STA 500D S-19R PER B737-700 SRM 51-40-02-0G-0.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 66,325 hrs · 39,077 cycles

CABIN FLOOR PANEL 241AEF UPPER SURFACE DELAMINATED ; / [01] CLEANED AT CABIN FLOOR PANEL 241AEF.OK. TO INSTALL REPAIR FIBERGLASS.; [02] VERIFIED CLEANING AREA; [03] VERIFIED CLEANING OF PANEL. OK TO INSTALL FIBER GLASS REPAIR; [04] CLEANED AND REPAIRED AT CABIN FLOOR PANEL 241AEF PER B -737-700 SRM.53-00-50-2R_8 MATERIAL USED. P.O.1150387 AND P.O. 1714421.; [05] VERIFIED PANEL REPAIR; [06] VERIFIED REPAIR; [07] VERIFIED THE CLEANING AND REPAIR AT CABIN FLOOR PANEL 241AEF PER B -737-700 SRM.53-00-50-2R_8 MATERIAL USED. P.O.1150387 AND P.O. 1714421.

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 66,325 hrs · 39,077 cycles

GASSET CRACKED @ FWD CARGO COMPARTMENT LEFT SIDE WALL S-19L ; STA 500D ; / [01] REMOVED GUSSET FROM FWD CARGO STA 500D S-19L PER B737-700 SRM 51-40-02-0G-0.; [02] VERIFIED REMOVAL OF REMOVED GUSSET FROM FWD CARGO STA 500D S-19L PER B737-700 SRM 51-40-02-0G-0.; [03] LOCATED AND DRILLED NEW PART AT FWD CARGO COM LEFT SIDE S-19L STA 500 D 737 -700 SRM 51-10-02 -0G-0; [04] VERIFIED OPEN HOLES AT NEW GUSSET FWD CARGO PER B737-700 SRM 51-10-02-0G-0; [05] VERIFIED. OK TO INSTALL NEW GUSSET.; [06] INSTALLED NEW GUSSET AT FWD CARGO STA 500 D STR- 19 L B-737 700 SMR 51-40 -02 -0G-0; [07] VERIFIED THE INSTALLATION OF NEW GUSSET AT FWD CARGO STA 500 D STR- 19 L B-737 700 SMR 51-40 -02 -0G-0

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 66,325 hrs · 39,077 cycles

R/H STAB. INSPAR RIB NO. 4 AT STAB STA 120.30 STIFFENER NO. 3 WITH A CRACK ; / [01] CUTOUT DAMAGE AT R/H STAB.RIB 4 STIFFENER #3 AS PER REF B737-700 SRM 55-10-09-2R-4; [02] VERIFIED CUTOUT DAMAGE AT R/H STAB. RIB 4. PENDING N.D.T; [03] PERFORMED HFEC INSP. ON REWORK AREA AT R/H STAB. RIB 4 STIFFENER #3 WEB IAW B737 NTM PT6 51-00-00 PROC. 23. NOTE: CRACK CONFIRMED LATE ENTRY-PERFORMED CUTOUT ON WEB AT R/H STAB.RIB#4 STIFFENER#3 AS PER REF B737-700 SRM 55-10-09-2R-4; [07] VERIFIED CUTOUT ON WEB AT R/H STB. RIB #4 STIFFENER #3; OK TO LOCATED AND DRILL THE REPAIR PARTS FIGURE202/REPAIR 4; [08] LOCATED AND DRILLED PARTS REPAED AS PER REF B737-700 ARM 55-10-09- 2R-4; [09] VERIFIED LOCATION OF DRILLED HOLES ON RIB #4 STIFFENER #3; OK TO INSTALL PART REPAIR; [10] INSTALLED PART REPAIR AT RIB #4 STIFFENER #3 AS PER REF B737-700 SRM 55-10-09-2R-4 INSPECTED INSTALLATION OF PARTS AT R/H STB. RIB #4 STIFFENER #3;

Part: FLOORBEAM — CORRODED (BS 270) · airframe 66,325 hrs · 39,077 cycles

FLIGHT DECK FLOOR STRUCTURE UNDERNEATH PANEL 211AF FORWARD SIDE OF BS 270 LATERAL BEAM HAS 2EA SPOTS OF CORROSION ON EXISTING REPAIR UPPER STRAP BL0 AND RBL 6. ; /

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 66,325 hrs · 39,077 cycles

LOWER FUSELAGE W/ W VERTICAL BULKHEAD STIFFENER CRACKED @ LOWER CHORD O/ B OF A/ C AIR EXIT EXHAUST STA 663.75 MKD ; / [01] REMOVED STIFFENER; [02] CORRECTING STEP 1; REMOVED STIFFENER AT RT W/W BULKHEAD STA 663.75 LOWER CHORD O/B OF A/C EXHAUST PER B737-700 SRM 51-40-02-0G-0.; LOCATED AND DRILLED NEW VERTICAL STIFFENER AT RT W/W STA 663.75 LOWER CHORD O/B OF EXHAUST REF B737-700 SRM 51-40-05-0G-0 AND DWG# 111A1000.; [06] VERIFIED STEP # 5; [07] OK TO INSTALL NEW ANGLE; [08] INSTALLED NEW VERTICAL STIFFENER AT RT W/W STA 663.75 LOWER CHORD O/B OF EXHAUST REF B737-700 SRM 51-40-02-0G-0 AND DWG# 111A1000.; [09] REINSTALLED GSE EXHAUST AT RT W/W STA 663.75 REF B737-700 SRM 51-40-02-0G-0.; [10] VERIFIED INSTALLATION OF NEW VERTICAL STIFFENER AT RT W/W STA 663.75 LOWER CHORD O/B OF EXHAUST REF B737-700 SRM 51-40-02-0G-0 AND DWG# 111A1000 AND VERIFIED REINSTALLATION OF GSE EXHAUST AT RT W/W STA 663.75 REF B737-700 SRM 51-40-02-0G-0.; [11] REMOVED AND REPLACED VERTICAL STIFFENER AT RT W/W STA 663.75 LOWER CHORD O/B OF EXHAUST REF B737-700 SRM 51-40-02-0G-0 AND DWG# 111A1000.

Part: BEAR STRAP — CRACKED (FUELAGE) · airframe 66,325 hrs · 39,077 cycles

CRACK FOUND AT PERIPHERY OF R1 DOOR BEAR STRAP CUTOUT. PERFORMED HFEC ROTO ON OPEN FASTENER HOLES WITHIN REPAIR AREA OF R1 DOOR CUTOUT IAW NDTM PART 651-00-00 PROCEDURE 16. NO CRACKS. PERFORMED COUNTERSINK INSPECTION ON OPEN FASTENER HOLES WITHIN REPAIR AREA OF R1 DOOR CUTOUT IAW NDTM PART 653-30-00 PROCEDURE 3. NO CRACKS. PERFORMED COUNTERSINK INSPECTION ON OPEN FASTENER HOLES WITHIN REPAIR AREA OF R1 DOOR CUTOUT IAW NDTM PART 653-30-00 PROCEDURE 3. NO CRACKS. THIS FAULT WAS RESOLVED ON OTHER FAULT #TTG8Q0050WRM.

Part: BEAR STRAP — CRACKED (BS 291 S8-9R) · airframe 66,325 hrs · 39,077 cycles

CRACK FOUND AT R1 DOOR CUTOUT INTERNAL. ; / DURING INSPECTION PER SB 737-53A1383 R1 (SWA SI 5313-I-15021-NG REV 2), CRACK DAMAGE WAS DISCOVERED ON THE FORWARD GALLEY DOOR SURROUND BEARSTRAP (P/N 141A3313-1) ON THE UPPER FORWARD CORNER IN A FASTENER HOLE AT STATION 291.5+4.5" BETWEEN STRINGER 8R AND STRINGER 9R. THE DAMAGE IS REPAIRABLE PER 737-700 SRM 53-10-01 REPAIR 6. SB 737-53A1383 R1 STATES TO CONTACT THE BOEING COMPANY.

Part: SKIN — CRACKED (L1 DOOR) · airframe 66,325 hrs · 39,077 cycles

L-1 DOOR ASSY AFT UPPER CORNER CRACKED AT EDGE MKD DOT ; / PERFORMED HFEC ON CRACK AT UPPER CORNER EDGE OF L-1 DOOR ASSY IAW NDTM PART 6 ;51-00-00 PROCEDURE 26. CRACK CONFIRMED WITH LENGTH : 0.196' VERIFIED REWORKED AREA IS IN LIMITS PER B737-700 SRM 51-10-02 -1A-1 FIG 103 DETAIL C; [09] OK TO TREAT AND PRIME REWORKED AREA; [10] TREATED REWORKED AREA WITH ALODINE AND PRIMER AS PER B737-700 SRM 51-20-01; [11] AFTER REWORK AREA FOUND OUT LIMITS MAT.LOSS 0.196''AS PER B-737-700 SRM 52-10-02-1A-1 FIG.103 DETAIL C.; [12] STEP 11; AFTER REWORKED AREA ON STEP 4 (REMOVING CRACK) FOUND OUT OF LIMITS PER B737-700 SRM 52-10-02-1A-1 FIG.103 DETAIL C. MATERIAL LOSS 0.196'; MAX. MAT. ALLOWED TO REMOVE 0.150'.; ACCOMPLISHED 0.040' INSURANCE CUT AT TRIMMED AREA AND EVALUATED SURFACE ROUGHNESS FOUND TO BE SMOOTHER THAN 63 MICROINCHES RA ON TRIMMED AREA REF B737-700 SRM 51-20-13-0G-0 AND EA# 21-151-01668-WIP1; TOOL USED B/C #171854.; [29] VERIFIED ACCOMPLISHED 0.040' INSURANCE CUT AT TRIMMED AREA AND EVALUATED SURFACE ROUGHNESS FOUND TO BE SMOOTHER THAN 63 MICROINCHES RA ON TRIMMED AREA REF B737-700 SRM 51-20-13-0G-0 AND EA# 21-151-01668-WIP1; TOOL USED B/C #171854.; [30] ACCOMPLISHED A GENERAL VISUAL INSPECTION; AS DEFINED IN 737-700 SRM 51-00-06 PARAGRAPH 3 OF ALL AREAS WITHIN THE REPAIR; [31] FABRICATED THE -1 REPAIR DOUBLER

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 66,325 hrs · 39,077 cycles

CRACK FOUND AT R1 DOOR CUTOUT INTERNAL. ; / EVALUATED CRACK STARTED FABRICATION OF DOUBLER AND TRIPLER FOR SKIN REPAIR AT R1 DOOR UPPER FWD CORNER PER B737-700 SRM 53-10-01-2R-6 FIG 202.; [16] VERIFIED FABRICATION OF DOUBLER AND TRIPLER FOR SKIN REPAIR AT R1 DOOR UPPER FWD CORNER PER B737-700 SRM 53-10-01-2R-6 FIG 202OVERSIZED EXISTING RIVET HOLES AT REPAIR AREA PER B737-700 SRM 53-10-01-2R-6 STEP 2K.; [23] INSTALLED COUNTERSINK REPAIR WASHERS IN THE INITIAL COUNTERSINK LOCATIONS PER B737-700 SRM 53-10-01-2R-6 STEP 4L.; [24] VERIFIED THE OVERSIZED EXISTING RIVET HOLES AT REPAIR AREA PER B737-700 SRM 53-10-01-2R-6 STEP 2KVERIFIED CONTINUATION OF FABRICATION OF REPAIR PARTS DOUBLER & TRIPLER PER B737-700 SRM 53-10-01-2R-6 REPAIR 6; [28] COMPLETED DRILLING AND TRIMMING PROCESS OF REPAIR PARTS DOUBLER & TRIPLER ( PENDING CHAMFER ) PER B737-700 SRM 53-10-01-2R-6; TABLE 201; FIG 202; REPAIR 6; [29] FABRICATED REPAIR PARTS FLAT SHIM [7] MAT. USED 2024-T3 CLAD .063IN AND FILLER [4] MAT. USED 2024-T3 CLAD .090IN PER B737-700 SRM 53-10-01-2R-6 REPAIR 6; TABLE 201; FIG 202; [30] COMPLETED FABRICATION OF REPAIR PARTS DOUBLER & TRIPLER PER B737-700 SRM 53-10-01-2R-6 REPAIR 6;<BR>TABLE 201; FIG 202; PARAGRAPH 4.E.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 66,325 hrs · 39,077 cycles

CRACK FOUND AT R1 DOOR CUTOUT INTERNAL. ; / EA 21-153-01327 WAS ATTACHED TO FAULT #TTG8Q0050WRM. CUT AND REMOVED DAMAGE FROM R1 DOOR BEAR STRAP PER B737-700 SRM 51-10-02-0G-0 AND SRM 53-10-01-2R-6 REPAIR 6, FIG 202

Part: BULKHEAD — PEELING (AFT CARGO) · airframe 66,325 hrs · 39,077 cycles

AFT CARGO FORWARD BULKHEAD PANEL # 142NWB HAS FIBERGLASS PEELING OFF ON LOWER RIGHT SIDE. ; / [01] CLEANED AND PREPARED PANEL #142NWB FOR REPAIR AS PER AMM 25-52-01-300-805 PARAGRAPH 4.C; [02] OK TO INSTALL REPAIR ON PANEL #142NBW; [03] OK TO INSTALL REPAIR; [04] REPAIRED DAMAGE AREA AFT CARGO FWD BULKHEAD PANEL 142NWB AS PER BOEING 737 AMM 25-52-01-300-805.MATERIAL USED EPOCAST 50/A P/O 1714421 PLUS BMS -3-7781 P/O 1694548.RESTORED ORIGINAL FINISHED.; [05] MEASUREMENTS; [06] VERIFY THAT REPAIR WAS DONE AS PER B737 AMM 25-52-01-300-805; [07] VERIFIED REPAIR ON PANEL 142MWB AS PER B737-700 AMM 25-52-01-300-805

Part: HOOK AND LOOP — LOOSE (EMERGENCY EXIT) · airframe 65,859 hrs · 38,764 cycles

RIGHT EMERGENCY EXIT DOOR COVER LOOSE. / INSTALLED NEW VELCRO PER SIP.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 64,564 hrs · 37,920 cycles

GIRT BAR R1 SERVICE DOOR OUT OF ALIGNMENT. RESECURED FWD SERVICE DOOR SLIDE IAW AMM.

Part: RETAINER — CRACKED (VERTICAL STAB L/) · airframe 64,200 hrs · 37,691 cycles

VERTICAL FIN PANEL 323AL HORIZONTAL RETAINER CRACKED / R&R VERTICAL FIN PANEL 323AL HORIZONTAL RETAINER PER SRM 51-40-02

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 64,200 hrs · 37,691 cycles

RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED / R&R RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL REF AMM 53-31-31.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 64,143 hrs · 37,654 cycles

L2 DOOR CAUTION INFLATABLE SLIDE SIGN NOT VISIBLE WITH SLIDE IN THE ARMED POSITION. / SECURED COVER AND SLIDE PER MT.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 63,351 hrs · 37,149 cycles

AFT NR 2 EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER SIP & MM.

Part: LIGHT — INOPERATIVE (ROW 22) · airframe 63,064 hrs · 36,965 cycles

R/H EMERGENCY BULL NOSE LIGHT INOP AT ROW 22. RELAMPED LIGHT IAW AMM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 62,265 hrs · 36,453 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 62,265 hrs · 36,453 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 62,265 hrs · 36,453 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING TOWER INBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 62,265 hrs · 36,453 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 62,265 hrs · 36,453 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 62,265 hrs · 36,453 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.

Part: PIVOT PIN — CORRODED (LT MLG) · airframe 62,000 hrs · 36,271 cycles

LT MAIN GEAR UPPER SIDE STRUT TO LOWER SIDE STRUT PIVOT PIN AREA CORRODED ON AFT SIDE. REPAIRED PIN PER EA.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 61,759 hrs · 36,101 cycles

ACB FWD SCUFF PLATE IS CRACKED / ACB FWD SCUFF PLATE WAS REPAIRED PER EA # 1-A53-2076 R11

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 61,759 hrs · 36,101 cycles

VAPOR BARRIER STIFFENER CRACKED AT BS 663, LBL 27. R&R STIFFENER IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 45. R&R INTERCOSTAL PER SRM AND DWG.

Part: FORMER — CRACKED (LT WING) · airframe 61,759 hrs · 36,101 cycles

LT WING FIXED LEADING EDGE INBOARD FAIRING SUPPORT FORMER CRACKED ON UPPER END. R&R FORMER IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 867+16, RBL 28. R&R SUPPORT IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED. R&R WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

FORWARD CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 420A, RBL 24. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767. R&R SUPPORT IAW SRM AND DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

AFT CARGO BAY FLOOR SUPPORT T-SPLICE CORRODED AT BS 772, LBL 7. R&R T-SPLICE PER SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 61,759 hrs · 36,101 cycles

AFT CARGO BAY RT FLOOR TRACK CORRODED BETWEEN BS 794 TO BS 887. R&R TRACK IAW SRM AND DWG.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

AFT CARGO BAY RT KEEL BEAM WEB CORRODED BETWEEN BS 787 TO BS 793. REPAIRED WEB IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

AFT CARGO BAY SUB THRESHOLD CORRODED BETWEEN BS 794 TO BS 847. R&R WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

FORWARD CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500C TO BS 500D, RBL 24. R&R SUPPORT IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FWD CARGO RH) · airframe 61,759 hrs · 36,101 cycles

***CORROSION***FOUND CORROSION IN THE FWD CARGO BAY BELOW THE FLOOR BS 500A+10 RBL2. MARKED ANTENA SUPPORT CHANEL. / REMOVED AND REPLACED ON FWD CARGO BAY BELOW THE FLOOR BS 500A+10 ANTENNA SUPPORT CHANNEL AT RB22 IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 & DWG #143A3233 59202U 31OCT18

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

FORWARD CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500 TO BS 500A, RBL 24. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 793. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

FORWARD CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 420 TO BS 440, RBL 24. R&R SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

INTERCOSTAL CORRODED AT BS 867 +16, RBL 22. R&R INTERCOSTAL IAW DWG AND SRM.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 61,759 hrs · 36,101 cycles

FORWARD SIDE OF VAPOR BARRIER STIFFENER CRACKED AT BS 663, LBL 7. R&R STIFFENER IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

AFT CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT CORRODED AT BS 947, BETWEEN RBL 21 TO LBL 10. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847. R&R SUPPORT IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

STRINGER CORRODED AT BS 927+2, STR 25L. REPAIRED STRINGER IAW SRM.

Part: DOUBLER — CRACKED (WHEEL WELL LH) · airframe 61,759 hrs · 36,101 cycles

LH REAR SPAR SEAL ASSEMBLY AT BS 663 LBL 14 IS CRACKED / REMOVED AND REPLACED L/H REAR SPAR SEAL ASSEMBLY AT BS 663 LBL 14 IAW SRM 51-40-02-0G-0 AND DWG # 111A1515

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

AFT CARGO BAY INTERCOSTAL CORRODED AT BS 727A, RBL 12. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

BULKHEAD TO SIDEWALL SUPPORT CORRODED AT BS 947, RBL 22. R&R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 727+5, LBL 10. REPAIRED SUPPORT PER ER AND EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 947, RBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 61,759 hrs · 36,101 cycles

AFT CABIN FLOOR PANEL 242XF IS BROKEN / DUE TO THE EXTENT OF DAMAGE; REPLACED AFT CABIN FLOOR PANEL 242XF WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 220. 57066U 10/17/18

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

STRINGER SUPPORT ANGLE CRACKED AT BS 294.5, STR 13L. R&R ANGLE IAW DWG & SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

STRINGER CLIP CRACKED AT BS 277, STR 10R. R&R STRINGER CLIP IAW SRM AND DWG.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

L1 DOOR FORWARD GIRT BAR FITTING BRACKET CORRODED AT BS 312, LBL 55. R&R BRACKET PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL PER SRM AND DWG.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

L1 DOOR AFT GIRT BAR FITTING BRACKET CORRODED AT BS 344, LBL 58. REPAIRED BRACKET PER SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

R1 DOOR MOPSILL CORRODED. R&R MOPSILL IAW SRM & DWG.

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 61,759 hrs · 36,101 cycles

FWD SERVICE DOOR CRACKED AT THE #5 BEAM / FSD #5 BEAM WAS REMOVED & REPLACED ON WORK ORDER: 510434. & CUSTOMER PO: 0520055-CMR.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294.5, RBL 1. R&R INTERCOSTAL PER DWG & SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

L1 DOOR MOPSILL CORRODED. R&R MOPSILL PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R&R INTERCOSTAL PER SRM AND DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 61,759 hrs · 36,101 cycles

R1 DOOR CRACKED AT THE NR 4 BEAM. R&R DOOR PER AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,759 hrs · 36,101 cycles

AFT CABIN FLOOR SUPPORT BEAM CORRODED AT BS 986, BETWEEN LBL 45 TO RBL 45. REPAIRED SUPPORT BEAM IAW ER AND EA.

Part: RETAINER — CRACKED (LT WING) · airframe 61,759 hrs · 36,101 cycles

LT WING T/E SEAL RETAINER ABOVE #1 PYLON AFT TIP IS CRACKED / REMOVED AND REPLACED LT WING T/E SEAL RETAINER ABOVE #1 PYLON AFT TIP P/N 115A2953-1 IAW. AIPC 57-50-00-25 AND SRM 51-40-02

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 61,759 hrs · 36,101 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS 665, RBL 40.5. REPAIRED DECK IAW EA.

Part: STRUCTURE — CRACKED (LT MLG WW) · airframe 61,759 hrs · 36,101 cycles

LT VAPOR BARRIER UPPER CHORD CRACKED AT BS 663, IN RADIUS ABOVE 3RD FASTENER INBOARD EDGE. REPAIRED CHORD IAW ER AND EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 61,759 hrs · 36,101 cycles

HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS 663 TO BS 675, LBL 39. REPAIRED DECK IAW ER AND EA.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 61,759 hrs · 36,101 cycles

LT WING OUTBOARD AT FLAP LOWER SURFACE DELAMINATED ON AFT INBOARD CORNER. REPAIRED AFT FLAP PER WO.

Part: COVER — BROKEN (CABIN) · airframe 61,759 hrs · 36,101 cycles

RT SIDE NR 4 BIN EMERGENCY LIGHT COVER BROKEN. R&R COVER PER AMM.

Part: LENS — LOOSE (CABIN) · airframe 61,759 hrs · 36,101 cycles

RT OVER WING EMERGENCY EXIT DOOR AFT LIGHT LENS LOOSE. SECURED LENS PER AMM.

Part: COVER — MISSING (CABIN) · airframe 61,313 hrs · 35,821 cycles

R2 DOOR EMERGENCY EXIT LOWER LIGHT COVER MISSING DIRECTIONAL ARROW. R&R COVER PER AMM.

Part: COVER — MISSING (CABIN) · airframe 61,313 hrs · 35,821 cycles

L2 DOOR EMERGENCY EXIT LOWER LIGHT COVER MISSING DIRECTIONAL ARROW. R&R COVER PER AMM.

Part: COVER — MISSING (CABIN) · airframe 61,313 hrs · 35,821 cycles

LT OVERWING EMERGENCY DOOR EXIT COVER ARROW MISSING. R&R COVER PER AMM.

Part: COVER — MISSING (CABIN) · airframe 61,313 hrs · 35,821 cycles

LT EMERGENCY WING EXIT LOWER LIGHT COVER MISSING DIRECTIONAL ARROW. R&R COVER PER AMM.

Part: LENS — UNSECURE (CABIN) · airframe 60,670 hrs · 35,394 cycles

AFT AISLE OVERWING EMERGENCY EXIT SIGN COVER LENS CAME OFF. SECURED LENS PER MM.

Part: RETAINING CLIP — OUT OF ADJUST (R1 DOOR) · airframe 60,251 hrs · 35,142 cycles

R1 DOOR GIRT BAR CLAMP OUT OF ADJUST. ADJUSTED CLIPS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,818 hrs · 34,248 cycles

LT OVERWING EMERGENCY EXIT DOOR EXTERNAL EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,592 hrs · 34,099 cycles

RIGHT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,295 hrs · 33,919 cycles

RT OVERWING EMERGENCY EXIT LIGHT BULB INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,293 hrs · 33,918 cycles

L1 DOOR OUTER EMERGENCY LIGHT INOP. R&R LIGHT PER AMM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 58,293 hrs · 33,918 cycles

AFT PRESSURE BULKHEAD OIL CANNING CONDITION BETWEEN STR 0.0 AND STR 3L, AT OUTER WEB POCKET. REPAIR BULKHEAD IAW SRM AND EA.

Part: BRACKET — CRACKED (LEFT WING) · airframe 58,290 hrs · 33,917 cycles

LT WING UPPER FIXED TRAINING EDGE PANEL (AFT OF ENGINE PYLON) FWD SEAL BRACKET CRACKED / REMOVED AND REPLACED LEFT WING UPPER FIXED TRAINING EDGE PANEL (AFT OF ENGINE PYLON) FWD SEAL BRACKET PER SRM 51-40-02

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,033 hrs · 33,757 cycles

RIGHT AFT SIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 57,138 hrs · 33,208 cycles

L1 DOOR EMERGENCY LIGHT BATTERY PACK INOP. R&R BATTERY PACK PER MM.

Part: COVER — BROKEN (CABIN) · airframe 56,368 hrs · 32,741 cycles

FRONT GALLEY "EXIT" PLACARD COVER BROKEN. R&R LIGHT ASSEMBLY IAW AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,341 hrs · 32,721 cycles

LEFT FORWARD ENTRY THRESHOLD EMERGENCY EXIT LIGHT, BULB INOPERATIVE. REPLACED THE BULB IAW MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,818 hrs · 32,409 cycles

EMERGENCY EXIT LIGHT INOP AT M1672. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,818 hrs · 32,409 cycles

EMERGENCY EXIT LIGHT M1674 BATTERY UNIT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,818 hrs · 32,409 cycles

EMERGENCY EXIT LIGHT INOP AT M1673. R&R BATTERY PACK PER AMM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 55,818 hrs · 32,409 cycles

CLIP CORRODED AT BS 773, RBL 21. R&R CLIP PER DWG AND SRM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 55,818 hrs · 32,409 cycles

L1 DOOR ESCAPE SLIDE SHROUD OUT OF ADJUST. ADJUSTED SLIDE IAW MT.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 55,818 hrs · 32,409 cycles

AFT CARGO BAY CARGO TIE-DOWN TRACK CRACKED AT BS 747, RBL 13. R&R TRACK IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 55,818 hrs · 32,409 cycles

INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, RBL 21. R&R INTERCOSTAL PER SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 55,818 hrs · 32,409 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 41. REPAIRED WEB IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,818 hrs · 32,409 cycles

FORWARD CARGO BAY SHIELD CORRODED BETWEEN BS 492 TO BS 500A, RBL 21. R&R SHIELD PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,818 hrs · 32,409 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 21. R&R SUPPORT PER SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 55,818 hrs · 32,409 cycles

LT OVERWING EMERGENCY LOWER SILL STRAP CORRODED AT BS 639. R&R STRAP PER DWG AND SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,818 hrs · 32,409 cycles

AFT CARGO BAY RT SHIELD CORRODED BETWEEN BS 767 TO BS 794, RBL 24. R&R SHIELD PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,818 hrs · 32,409 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727+4 TO BS 767. R&R SUPPORT PER DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,818 hrs · 32,409 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727+4 TO BS 767. R&R SUPPORT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,818 hrs · 32,409 cycles

SKIN CRACKED AT BS 540, BETWEEN STR 22L TO STR 23L. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,818 hrs · 32,409 cycles

RT WING NR 7 SLAT ACTUATOR ROD END ATTACH FITTING LOWER BULLNOSE SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,818 hrs · 32,409 cycles

RT WING NR 8 SLAT ACTUATOR ROD END ATTACH FITTING BULLNOSE SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,818 hrs · 32,409 cycles

RT WING NR 6 SLAT ACTUATOR ROD END ATTACH FITTING LOWER BULLNOSE SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIRT — LOOSE (L1 DOOR) · airframe 55,818 hrs · 32,409 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR SKIRT LOOSE. R&R SKIRT IAW MT.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 54,715 hrs · 31,728 cycles

L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER DETACHED. INSTALLED THE COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 54,432 hrs · 31,564 cycles

R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 53,537 hrs · 30,994 cycles

FORWARD LOWER ENER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 53,282 hrs · 30,871 cycles

L2 WINDOW ARCED THEN CRACKED, OUTER PANE ONLY. R & R NR 2 SLIDING WINDOW IAW MT.

Part: LENS — BROKEN (EXIT SIGN) · airframe 52,097 hrs · 30,228 cycles

L2 DOOR EMER EXIT SIGN LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 51,966 hrs · 30,144 cycles

L1 DOOR LOWER EMER EXIT SIGN LIGHT ASSEMBLY INOPERATIVE. R & R SIGN ASSEMBLY IAW AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 50,049 hrs · 29,020 cycles

L1 DOOR EMER EVAC SLIDES OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 50,049 hrs · 29,020 cycles

R1 DOOR EMER EVAC SLIDES OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 49,738 hrs · 28,834 cycles

MAIN LANDING GEAR WW FWD PRESS BULKHEAD WEB CRACKED AT BS 663, BETWEEN RBL 39.75 - 40.25. REPAIRED WEB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,738 hrs · 28,834 cycles

RIGHT NR 3 WINDOW FRAME CRACKED, 2ND FROM LOWER HOLE. REPAIRED FRAME IAW ACO.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 49,738 hrs · 28,834 cycles

MAIN LANDING GEAR WW FWD PRESS BULKHEAD WEB CRACKED AT BS 663, BETWEEN RBL 32.75 - 34.0. REPAIRED WEB IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,738 hrs · 28,834 cycles

LEFT EMER BULLNOSE LIGHT INOPERATIVE AT ROW 17. REPAIRED LIGHT IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,738 hrs · 28,834 cycles

LEFT NR 3 WINDOW FRAME CRACKED 3RD FROM LOWER HOLE. REPAIRED FRAME IAW EA.

Part: SWITCH — DIRTY (AFT GALLEY) · airframe 48,729 hrs · 28,275 cycles

AFT GALLEY EMER EXIT LIGHT SWITCH STICKING. CLEANED SWITCH CAP IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,729 hrs · 28,275 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 1 ABC. RELAMPED IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 47,814 hrs · 27,758 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT COVER LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: PLATE — CRACKED (LT WING) · airframe 45,337 hrs · 26,301 cycles

LT WING LOWER FIXED TE PANEL AFT OF ENGINE CRACKED WIGGLE PLATE. R & R WIGGLE PLATE IAW SRM & EA.

Part: IDG — MALFUNCTIONED (NR 2 ENGINE) · airframe 44,418 hrs · 255,738 cycles

AIR TURNBACK, AUTO THROTTLE WORKED FINE ON TAKE OFF, BUT SHORTLY AFTER LIFT OFF THE AIRCRAFT INDUCED & 8% SPLIT IN NR 1 & NR 2 N1S & THEN DISENGAGED. NR 2 THROTTLE WOULD NOT RESPOND TO INPUTS FOR A PERIOD OF TIME. R&R NR 2 IDG IAW MM.

Part: SENSOR — FAULTY (TE FLAP) · airframe 44,007 hrs · 25,515 cycles

DECLARED EMERGENCY SELECTED FLAPS 5 ON APPROACH NOTHING HAPPENED. EXTENDED FLAPS IAW QRH UNEVENTFUL WITH NO NOTICEABLE ROLL. R & R NR 3 FLAP SKEW SENSOR IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 43,123 hrs · 24,992 cycles

AFT EMERGENCY LIGHT BATTERY PACK M1673 FAILED CAPACITY FUNCTION CHECK. REMOVED AND REPLACED BATTERY PER AMM.

Part: LUG — DAMAGED (RT HORIZ STAB) · airframe 43,031 hrs · 24,943 cycles

RIGHT HORIZONTAL STAB CENTER SECTION UPPER FWD ATTACH LUG DAMAGED AT UPPER SIDE FROM WRAP AROUND PANEL. REPAIRED LUG PER EA.

Part: LUG — DAMAGED (RT HORIZ STAB) · airframe 43,031 hrs · 24,943 cycles

RIGHT HORIZONTAL STAB CENTER SECTION FWD UPPER AFT ATTACH LUG DAMAGED AT UPPER SIDE FROM WRAP AROUND PANEL. REPAIRED LUG PER EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 43,031 hrs · 24,943 cycles

AFT CARGO FLOOR TRACK AT STA 727D+5 LBL 3 HAS CORROSION AT JOGGLE FOR FLOOR STRAP. REPAIRED FLOORBEAM JOGGLE PER EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 43,031 hrs · 24,943 cycles

AFT CARGO FLOOR TRACK AT STA 727D+5 LBL 17.24 HAS CORROSION AT JOGGLE FOR FLOOR STRAP. REMOVED AND REPLACED TRACK PER SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 43,031 hrs · 24,943 cycles

AFT CARGO FLOOR TRACK AT STA 727D+5 RBL 3 HAS CORROSION AT JOGGLE FOR FLOOR STRAP. REPAIRED CHANNEL PER EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 43,031 hrs · 24,943 cycles

AFT CARGO FLOOR TRACK AT STA 727D+5 LBL 12.5 HAS CORROSION AT JOGGLE FOR FLOOR STRAP. REPAIRED FLOORBEAM JOGGLE PER EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 43,031 hrs · 24,943 cycles

AFT CARGO FLOOR TRACK AT STA 727D+5 LBL 8.1 HAS CORROSION AT JOGGLE FOR FLOOR STRAP. REPAIRED FLOORBEAM JOGGLE PER EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 43,031 hrs · 24,943 cycles

AFT CARGO FLOOR TRACK AT STA 727D+5 RBL 8 HAS CORROSION AT JOGGLE FOR FLOOR STRAP. REPAIRED CHANNEL PER EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

INTERCOSTAL CRACKED BS 312-328 LBL 46. REMOVED AND REPLACED PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CRACK IN FRAME AT AIR-CONDITIONING SUPPORT BRACKET FASTENER ABOVE STR 8R STA 747. REPAIRED FRAME PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CORROSION ON FLOOR SUPPORT BS 312-328 LBL 11. REMOVED AND REPLACED PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CRACK IN FRAME AT AIR-CONDITIONING SUPPORT BRACKET FASTENER ABOVE STR 8R STA 867. REPAIRED FRAME PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CABIN, FLOOR WEB AT STA 1028 LBL 24 HAS A CRACK AT THE PULLED FASTENER HOLE. REMOVED AND REPLACED WEB PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CORROSION ON FLOOR SUPPORT AT BS 767+5 RBL 3. REPAIRED JOGGLE PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CORROSION ON FLOOR SUPPORT AT BS 767+5 LBL 12 REPAIRED JOGGLE PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CRACK IN FRAME AT AIR CONDITIONING SUPPORT BRACKET FASTENER ABOVE STR 8R STA 480. REPAIRED FRAME PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CORROSION ON FLOOR SUPPORT BS 328-344 LBL 11. REMOVED AND REPLACED PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CRACK IN FRAME AT AIR-CONDITIONING SUPPORT BRACKET FASTENER ABOVE STR 8R STA 360. REPAIRED PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CORROSION ON FLOOR SUPPORT AT BS 767+5 LBL 8. REPAIRED JOGGLE PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CRACK IN FRAME AT AIR CONDITIONING SUPPORT BRACKET FASTENER ABOVE STR 8R STA 747. REPAIRED FRAME PER EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS 328-344 LBL 46. REMOVED AND REPLACED PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CRACK IN FRAME AT AIR-CONDITIONING SUPPORT BRACKET FASTENER ABOVE STR 8R STA 787. REPAIRED PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

STRINGER CLIP AT STR 18R, STA 986.5 CRACKED. REMOVED AND REPLACED CLIP PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CORROSION ON FLOORBEAM UPPER AFT FLANGE, STA 328 RBL 54. REPAIRED BEAM PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN FS 312-328 RBL 31. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CORROSION ON AFT GALLEY DOOR ENTRY AREA, Z ANGLE UPPER SURFACE SEVERAL PLACES. REMOVED AND REPLACED AFT GALLEY DOOR ENTRY Z ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CORROSION ON FLOORBEAM UPPER CAP AT STA 986 AT RBL 36.5. REPAIRED FLOORBEAM PER SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

PASSENGER CABIN NR 1 SEAT TRACK BS 727B LBL 45.5 FORWARD I/B HOLE (.247) INDICATES CRACKED WITH HFEC. REPAIRED PER EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

PASSENGER CABIN NR 4 SEAT TRACK BS 727B RBL 45.5 FORWARD I/B HOLE (.247) INDICATES CRACKED WITH HFEC. REPAIRED SEAT TRACK IAW EA 1-757-7910.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

AFT CARGO FLOOR SUPPORT, FLOOR STRAP AND COINCIDING ATTACH POINT AT STA 887 HAVE CORR. REMOVED AND REPLACED AFT CARGO FLOOR STRAP PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

AFT CARGO FLOOR SUPPORT, FLOOR STRAP AND COINCIDING ATTACH POINT BETWEEN 727D AND 727E HAVE CORROSION. REMOVED AND REPLACED AFT CARGO FLOOR STRAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

CORROSION ON FLOORBEAM UPPER CAP AT STA 986 AT RBL 44. REPAIRED FLOORBEAM PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,031 hrs · 24,943 cycles

AFT CARGO FLOOR SUPPORT, FLOOR STRAP AND COINCIDING ATTACH POINT BETWEEN 767 AND 787 HAVE CORROSION. REMOVED AND REPLACED AFT CARGO FLOOR STRAP PER SRM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 43,031 hrs · 24,943 cycles

WHEEL WELL BULKHEAD SKIN CRACKED STA 663 LBL 5 APPROX 18 INCHES LONG. REPAIRED DAMAGED AREA PER EA 1-A53-3376.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 43,031 hrs · 24,943 cycles

HORIZONTAL STIFFENER CRACKED FWD SIDE OF WHEEL WELL BULKHEAD STA 663 LBL 5 APPROX 4 INCHES ABOVE KEEL BEAM. REMOVED AND REPLACED STIFFENER PER SRM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 43,031 hrs · 24,943 cycles

LEFT WING T/E - UPPER SHELF SUPPORT ANGLE CRACKED (O/B OF NR 6 GROUND SPOILER). REMOVED AND REPLACED SUPPORT BRACKET PER SRM.

Part: BRACKET — CRACKED (WING) · airframe 43,031 hrs · 24,943 cycles

UPPER TRAILING EDGE PANEL BETWEEN FLAP, CENTER BRACKET CRACKED. REMOVED AND REPLACED PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 42,797 hrs · 24,795 cycles

FORWARD SERVICE DOOR EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,767 hrs · 24,778 cycles

EMERGENCY EXIT FLOOR TRACK LIGHTING INOP ROW 1. REPLACED FLOOR TRACK LIGHTING AT ROW 1 & OPS NORMAL PER MM.

Part: LENS — MISSING (CABIN) · airframe 42,166 hrs · 24,409 cycles

EEPLS LENS MISSING. INSTALLED LENS PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,657 hrs · 24,075 cycles

LEFT EEPLS INOP BETWEEN ROW 15 TO ROW 21. RELAMPED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,815 hrs · 23,574 cycles

SKIN CRACKED AT BS 394, STR 16L. REPAIRED SKIN IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 40,815 hrs · 23,574 cycles

R1 WINDOW FRAME LEFT UPPER CORNER POST OUTBOARD CRACKED. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 40,815 hrs · 23,574 cycles

L1 WINDOW FRAME LEFT UPPER CORNER POST OUTBOARD CRACKED. REMOVED AND REPLACED FRAME IAW SRM AND DWG.

Part: LENS — MISSING (CABIN) · airframe 40,260 hrs · 23,260 cycles

LEFT EMERGENCY EXIT LIGHT LENS MISSING AT ROW 8. REMOVED AND REPLACED LENS PER M/M.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 40,153 hrs · 23,194 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SIGN — BROKEN (CABIN) · airframe 40,102 hrs · 23,168 cycles

R1 DOOR EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: TAIL CONE — DELAMINATED (TE FLAP) · airframe 43,031 hrs · 24,943 cycles

RIGHT WING NR 7 CANOE TAIL CONE ASSY FOUND TO BE DELAMINATED ON BOTTOM. REMOVED AND REPLACED TAIL CONE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,910 hrs · 23,052 cycles

EEPLS INOP NEAR ROW 22. REMOVED AND REPLACED EEPLS IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 39,823 hrs · 23,000 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 39,082 hrs · 22,559 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: COVER — LOOSE (CABIN) · airframe 37,334 hrs · 21,555 cycles

LT EEPLS COVER LOOSE AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 36,689 hrs · 21,180 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,672 hrs · 21,167 cycles

LT EEPLS INOP AT ROW 17. REPAIRED EEPLS PER MM.

Part: GASPER FAN — FAULTY (CABIN) · airframe 36,613 hrs · 21,137 cycles

DURING DESCENT PASSING FL320, AFT FLIGHT ATTENDANT REPORTED STRONGER FUMES IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LENS — MISSING (CABIN) · airframe 36,163 hrs · 20,870 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: FLAP — PUNCTURED (LT WING) · airframe 36,163 hrs · 20,870 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING I/B AFT FLAP LOWER SURFACE PUNCTURED. REPAIRED AFT FLAP PER SRM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,113 hrs · 20,245 cycles

DURING SCHEDULE MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,113 hrs · 20,245 cycles

DURING SCHEDULE MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: BATTERY — FAILED (CABIN) · airframe 34,544 hrs · 19,907 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,338 hrs · 19,199 cycles

FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: COVER — MISSING (CABIN) · airframe 32,958 hrs · 18,986 cycles

FWD EEPS COVER MISSING. INSTALLED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 32,310 hrs · 18,589 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 3 TO ROW 23. REMOVED AND REPLACED COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 31,119 hrs · 17,851 cycles

DURING SCHEDULED MV3 CHECK, FOUND FWD EEPLS LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,391 hrs · 17,411 cycles

FWD EGRESS LIGHT INOP. R&R LIGHT ASSY PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,914 hrs · 17,119 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 8. REPAIRED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,914 hrs · 17,119 cycles

DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 930 TO BS 986, STR 17R, RBL 55. REMOVED AND REPLACED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,914 hrs · 17,119 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 55 TO RBL 5. REMOVED AND REPLACED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,914 hrs · 17,119 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 8. REPAIRED BEAM PER AAR EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,914 hrs · 17,119 cycles

DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CHORD CORRODED BETWEEN BS 305 TO BS 328, RBL 55. REPAIRED BEAM PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,914 hrs · 17,119 cycles

DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR FWD LOWER END CUTOUT FRAME CRACKED. REPAIRED FRAME PER SRM.

Part: LENS — MISSING (CABIN) · airframe 29,495 hrs · 16,843 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS LENS MISSING AT ROW 14. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 28,553 hrs · 16,284 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 28,553 hrs · 16,284 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: ENGINE — STALLED (LEFT) · airframe 27,739 hrs · 15,783 cycles

DECLARED EMERGENCY, NR 1 ENG COMPRESSOR STALLED, VIBRATION INDICATION AND N1 ROLLED BACK TO 15 PERCENT. REMOVED AND REPLACED NR 1 ENG PER MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 26,447 hrs · 15,004 cycles

L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 26,138 hrs · 14,798 cycles

EEPLS LENS MISSING AT ROW 10 ABC. INSTALLED LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,346 hrs · 14,340 cycles

DURING SCHEDULED HC1 CHECK, FWD RIGHT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,346 hrs · 14,340 cycles

DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,346 hrs · 14,340 cycles

DURING SCHEDULED HC1 CHECK, AFT LEFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 25,346 hrs · 14,340 cycles

DURING SCHEDULED HC1 CHECK, FWD LEFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 25,346 hrs · 14,340 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STAB STA 129.50, 17.5 " AFT OF LEADING EDGE SKIN. REPAIRED PER SWA EA.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 23,534 hrs · 13,268 cycles

EEPLS COVER MISSING AT ROW 3 ABC. INSTALLED COVER PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 20,996 hrs · 11,807 cycles

EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 20,701 hrs · 11,656 cycles

MID CABIN EEPLS LIGHT INOP. SECURED EEPLS CONNECTOR PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 20,617 hrs · 11,607 cycles

DURING SCHEDULED HC1 CHECK, LEFT OVERWING EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 20,617 hrs · 11,607 cycles

DURING SCHEDULED HC1 CHECK, RIGHT OVERWING EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 20,617 hrs · 11,607 cycles

DURING SCHEDULED HC1 CHECK, RIGHT AFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 20,617 hrs · 11,607 cycles

DURING SCHEDULED HC1 CHECK, LEFT AFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 20,617 hrs · 11,607 cycles

DURING SCHEDULED HC1 CHECK, LEFT EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 20,617 hrs · 11,607 cycles

DURING SCHEDULED HC1 CHECK, LEFT FWD CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHTS) · airframe 19,385 hrs · 10,887 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 11 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: STRIP — BROKEN (CABIN) · airframe 19,279 hrs · 10,821 cycles

EEPLS STRIP AT MID CABIN BROKEN. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: LIGHT — LOOSE (MID CABIN) · airframe 16,406 hrs · 9,257 cycles

LT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 12,701 hrs · 7,189 cycles

R1 DOOR EVAC SLIDE WOULD NOT SLIDE INTO BRACKET. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM.

Part: CONTROLLER — ARCED (COCKPIT WINDOW) · airframe 12,480 hrs · 7,068 cycles

ON DESCENT AT 12,000 FT AND 250 KIAS, COCKPIT R1 WINDOW OUTER PANE SHATTERED. ELECTRICAL ARCHING FROM HEATING ELEMENTS. REMOVED AND REPLACED COCKPIT R1 WINDOW AND RH WINDOW HEAT CONTROLLER PER MM.

Part: LAMP — INOPERATIVE (LT OVERWING EXIT) · airframe 10,650 hrs · 6,089 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 9,431 hrs · 5,381 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: STRIP — CRACKED (CABIN) · airframe 8,246 hrs · 4,713 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS SECTION CRACKED AT ROW NR 1. REMOVED AND REPLACED EEPLS SECTION PER MM.