N7826B

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 58,835 hrs · 38,694 cycles

FWD SERVICE DOOR ESCAPE SLIDE LIGHT INOP<[01] REPLACED FWD SERVICE DOOR SLIDE LIGHT REF AMM 33-51-04

Part: LANDING GEAR — FAILED (NOSE) · airframe 58,123 hrs · 38,268 cycles

AFTER T/O AND AIRCRAFT IN CLEAN CONFIGURATION FO PUT THE GEAR HANDLE IN 'OFF' POSITION. NOSE GEAR EXTENED; MAIN DID NOT.<[01] 02 - INSPECTED PER [AMM 32-33-00-710-801-NG (OPERATIONAL TEST FOR THE NOSE LANDING GEAR - PERMANENT)]

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,002 hrs · 37,056 cycles

EMERGENCY EXIT AREA LIGHT IN RIGHT OVERWING ESCAPE HATCH INOP<[01] RELAMPED EMERGENCY EXIT AREA LIGHT IN RIGHT OVERWING ESCAPE HATCH AND TESTED GOOD IAW AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED AFT CARGO BAY AFT CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2); (4); (5) USING ER4043 FILLER ROD LOT NUMBER 1131216<BR>EQUIPMENT USED ; WELDING MACHINE E10583 CALIBRATION DUE DATE 01/2024;[02] REJECTION OF STEP 4: WELD DOES NOT MEET 125 RA SURFACE FINISH PER SRM 53-60-15-2R-1 STEP 4.B.(5). SEE TTG8Q00NDFT1;[03] COMPLETE REPAIR ON AFT CARGO BAY AFT CORNER SCUFF PLATE. IAW SRM 53-60-15-2R-1.;[04] VERIFIED CORRECTIVE ACTION COMPLETE AND VERIFIED MEASUREMENT TABLE COMPLETE.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<

Part: BAFFLE — CRACKED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

FCB BAFFLE IS CRACKED BETWEEN BS 400 TO BS 420 LBL 24 WL 156<[01] REMOVED AND REPLACED FCB BAFFLE BETWEEN BS400 TO BS420;LBL24;WL156.IAW SRM 51-40-02 AND DWG#143A7505 REV B.;[02] TASK CARD COMPLETE

Part: BAFFLE — CRACKED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

FCB BAFFLE IS CRACKED BETWEEN BS 400 TO BS 420 LBL 24 WL 156<

Part: SKIN — CORRODED (ZN 300 STABILIZE) · airframe 56,002 hrs · 37,056 cycles

SURFACE CORROSION ON UPPER CROWN SKIN UNDER VERT STAB FUSELAGE STA 1016 TO STA 1040 AND FROM STRINGERS S-2AR TO S-2AL.<[01] REMOVED FASTENERS BETWEEN BS1016- BS1040 FROM STR2AL-STR2AR IAW SRM 51-40-0<BR>1. ROIG; JOSUE (PENDING)<BR>01-SEP-2023 16:43:36<BR>EVALUATED DAMAGE REMOVAL AT MULTIPLE AREAS OF CORROSION ON UPPFER CROW SKIN BETWEEN BS1016- BS1040 FROM STR2AL-STR2AR. MAX MATERIAL REMOVED IN AREAS OF 13.0'LX2.5'W ACCOMPLISHED UT INSPECTION OF BLEND AREA'S LOWEST THICKNESS IS .061 IN ORIGINAL .063 AND .077 IN ORIGINAL .080 FOUNDTO BE OUT OF LIMITS PER 737-700 SRM 53-00-01 ALLOWABLE DAMAGE1 BECAUSE THERE IS MATERIAL REMOVAL AROUND MORE THAN THREE FASTENERS IN ALL GROUPS OF TEN.<BR>INSTALLED FASTENERS BTW BS 1016 - BS 1040; FROM STR 2AL - STR 2AR; PER SRM 51-40-02 AND ER 23-02136;[02] AS PER EA 23-153-02631; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.<BR>APPLIED DAMAGE IDENTIFICATION AS PER SWA MPM 52.07.01.02 PARAGRAPH 1;[03] VERIFIED COMPLETE.

Part: TRACK — CRACKED (ZN 300 STABILIZE) · airframe 56,002 hrs · 37,056 cycles

RT HORIZONTAL STAB UPPER FWD TRACK FOR PANEL 343AT CRACKED.<[01] REMOVED AND REPLACED RT HORIZONTAL STAB UPPER FWD TRACK FOR PANEL 343AT PER AMM 20-50-11-910-801 TABLE 204 AND RESTORED DECORATIVE FINISH PER AMM 51-21-99-300 801;[02] INSPECTED AND VERIFIED CORRECTIVE ACTION.

Part: WEB — CORRODED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

CORROSION ON FORWARD CARGO BAY DOOR CUT-OUT SUB-THRESHOLD WEB FROM STA 440+11 TO 460+10; RBL 28 TO 30; WL 156.<[01] VERIFIED APLICABILITY SRM 53-30-53-0I-2 FOR IDENTIFICATION<BR>AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE;[02] VERIFIED PARTIAL UPDATES FOR STEPS 3 AND 4.;[03] VERIFIED MEASUREMENT TABLE.;[04] VERIFIED STEP 5.;[05] REMOVED AND REPLACE ON FORWARD CARGO BAY DOOR CUT-OUT SUB-THRESHOLD WEB BETWEEN BS 440 - BS.492.4 RBL 28. WL 156 IAW SRM 51-10-02 PARG.9. C.;[06] REJECTED: SEVERAL BLIND RIVETS STEM NEGATIVE PROTRUSION EXCEEDS '-0.020 INCH' LIMITS PER SRM 51-40-02 FIG 9. GENERATED TTG8Q00N6K4E;[07] TASK COMPLETE

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

AFT CARGO AFT BULKHEAD SUPPORT HAS CORROSION AT BS 927; LBL 3; WL 180<[01] OK TO INSTALL GIVEN;[02] REMOVED AND REPLACED AFT CARGO AFT BULKHEAD SUPPORT PER SRM 51-40-02 AND DWG 1498118.;[03] VERIFIED CORRECTIVE ACTION 2.

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE AT STA 500C+2; +16; +18; RBL 24; WL 156.<[01] CORROSION AT SUPPORT ANGLE OF FWD CARGO BAY FLOOR SIDEWALL ON STA 500C+2; +16; +18; RBL 24; WL 156. PART WILL BE REPLACED AND ALL MAINTENANCE ACTIONS ACCOMPLISHED WITH CUSTOMER CARD # TTG8Q00MZNMR.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

CORROSION ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT STA 500A+2; +6; +10; +14; +18; 500B+2; +6; +18; RBL 24; WL 158.<[01] REPLACED ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BETWEEN BS 500A - BS500D RBL.24 WL 156.5 IAW SRM 51-10-02; PARAG.9.C. DWG# 143A7500 REV: A;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE; EXCEPT MEASUREMENT FIELD ITEM 14 PART NUMBER INCOMPLETE BY AMT.;[03] CARD COMPLETE.

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

CRACK ON FWD CARGO BAY BAFFLE ATTACH ANGLE AT STA 400+19.5; WL 155; RBL 24.<[01] REMOVED AND REPLACED FWD CARGO BAY BAFFLE ATTACH ANGLE AT STA 400+19.5; WL 155; RBL 24 IAW SRM 51-40-02 AND DWG # 143A7505;[02] VERIFIED STEP 1;[03] TASK CARD COMPLETE

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 56,002 hrs · 37,056 cycles

RT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND INSTALLED NEW RT HORIZONTAL STAB FWD UPPER SLIDE SEAL PER AMM 53-31-31.;[02] FINAL INSPECTION. JOB COMPLETE.;[03] FINAL INSPECTION. JOB COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

AFT CARGO FLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727E+14 - 787+2; LBL 21; WL 157<[01] THIS CARD WILL BE ACCOMPLISHED ON CUSTOMER CARD NBR: TTG8Q00MZS35;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

CORROSION ON FWD CARGO DOOR CUT-OUT FWD SHIELD AT STA 420+6 & 420+9; WL 156; RBL 24.<[01] THE STRUCTURAL ITEM DOES NOT HAVE ALLOWABLE DAMAGE ENTRIES. THEREFORE; MUST BE REPAIRED BY REPLACEMENT PER REF SRM 51-10-02-0G-0 PARAGRAPH 9;[02] VERIFIED STEP 2 IN PARTIAL.;[03] VERIFIED STEP 1 COMPLETE; STEP 2 IN PARTIAL.;[04] REPLACED ON FWD CARGO DOOR CUT-OUT FWD SHIELD AT BS. 420 - 440; WL 156; RBL 24 IAW SRM 51-10-02 PARG.9. C.;[05] VERIFIED CORRECTIVE ACTION #4.;[06] VERIFIED MEASUREMENTS.;[07] VERIFIED ALL STEPS COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE AT STA 460+18; 480+6; +10; 500A+14; 500B+17; 500C+13; LBL 24; WL 156.<[01] VERIFIED APPLICABILITY SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.;[02] SEE STEP 3 FOR APPLICABILITY FOR ALLOWABLE DAMAGE;[03] VERIFIED CORRECTIVE ACTION 1.;[04] REMOVED AND REPLACED ON FCB FLOOR TO SIDEWALL SUPPORT;AT BS396 TO BS500D;LBL 24;WL156;IAW SRM 51-40-02 AND DWG#143A7500 REV A.;[05] TASK COMPLETE;[06] VERIFIED MEASUREMENT TABLE.<BR>TASK COMPLETE

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

AFT CARGO HAS CORROSION ON FWD BULKHEAD SUPPORT AT BS 727+4; LBL 22; WL 155<[01] REMOVED AND REPLACED AFT CARGO FWD BULKHEAD SUPPORT AT BS727+4 PER SRM 51-40-02 AND DWG 144A9401;[02] VERIFIED MEASUREMENT TABLE.;[03] VERIFIED CORRECTIVE ACTION 1.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

AFT CARGO AFT BULKHEAD SUPPORT HAS CORROSION AT BS 927; RBL 13; WL 180<[01] THIS FAULT WILL BE ACCOMPLISHED ON NRC #: TTG8Q00MZT48;[02] TASK CARD COMPLETE

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

AFT CARGO FLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727B+4 - 727E+10; LBL 21; WL 156<[01] REMOVED AND REPLACED AFT CARGO FLOOR TO SIDEWALL SUPPORT FROM BS 727 TO BS 847 IAW SRM 51-40-02 AND DWG 146A7500.;[02] VERIFIED MEASUREMENT TABLE.<BR>TASK COMPLETE

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

CORROSION ON FORWARD CARGO COMPARTMENT DOOR CUT-OUT AFT SHIELD FROM STA 500 TO 500A; RBL 24; WL 156.<[01] THE STRUCTURAL ITEM DOES NOT HAVE ALLOWABLE DAMAGE ENTRIES. THEREFORE; MUST BE REPAIRED BY REPLACEMENT PER REF SRM 51-10-02-0G-0 PARAGRAPH 9;[02] REPLACED ON FWD CARGO DOOR CUT-OUT AFT SHIELD AT BS. 492.4 - BS 500A; WL 156; RBL 24 IAW SRM 51-10-02 PARG.9. C.;[03] TASK CARD COMPLETE

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

AFT CARGO FLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727+7 - 747+2; RBL 21; WL 156<[01] EFFECTIVITY SRM 53-60-53-0I-2 IDENTIFICATION 2 AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 ARE APPLICABLE TO A/C.;[02] VALIDATED APPLICABILITY SRM 53-00-53-1A-2 ALLOWABLE DAMAGE;[03] UPDATED THE TABLE.;[04] REPAIRED CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 727+7 - 747+2; RBL 21; WL 156 PER SRM 51-10-02 AND SRM 53-00-53-1A-2;[05] VERIFIED CORRECTIVE 3 AND 4 AND MEASUREMENT TABLE.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS535 S-27R WL150. MARKED<[01] VERIFIED STEP 4 COMPLETE; STEP 5 IN PARTIAL OK TO INSTALL GIVEN.;[02] REPAIRED FCB STRINGER 27R BETWEEN BS 500D AND 540 IAW SRM 53-00-03-2R-1 REPAIR 1;[03] VERIFIED MEASUREMENT TABLE.;[04] VERIFIED CORRECTIVE ACTION 2.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26R WL153. MARKED<[01] REPAIRED STRINGER NBR 26RH PER REF SRM 53-00-03-2R-1;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS535 S-23R WL164. MARKED<[01] VERIFIED STEPS 4 AND 5.;[02] RECEIVED NEW STRINGER SECTION FROM OSS ITEM HFAB53-STR-011 LOT NBR 1537299-1 AND PO NBR 934384 AND HAT CHANNEL ITEM 69-78188-1 LOT NBR 1530303-1.<BR><BR>LOCATED AND DRILLED PARTS PER REF SRM 53-00-03-2R-1 REPAIR 1;[03] VERIFIED CORRECTIVE ACTION 2.;[04] 'THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 23-153-02622';[05] VERIFIED CORRECTIVE ACTION #4.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. MARKED<[01] PERFOMED STRINGER REPAIR PER REF SRM 53-00-03-2R-1;[02] VERIFIED CORRECTIVE ACTION 1.;[03] VERIFIED MEASUREMENT TABLE.;[04] ALL STEPS COMPLETED

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 56,002 hrs · 37,056 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 4TH VERTICAL STIFFENER IS CRACKED.<[01] UPDATED MEASUREMENT CHART.;[02] REMOVED THE DAMAGE PART AND INSTALLED REPAIR PARTS AT R/H HORIZONTAL STAB. INSPAR RIB; STAB STA 129.5 4TH VERTICAL STIFFENER IAW SRM 55-10-09-2R-4.;[03] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 2 AND MEASUREMENT TABLE.

Part: PANEL — ERODED (ZN 500 LEFT WING) · airframe 56,002 hrs · 37,056 cycles

LT WING L/E PANEL 521UB HAS WIND EROSION ON CORNER (MARKED)<FABRICATED BONDED ALUMINUM FOIL PLY USING BMS 8-289 LOT: 1524505-2 AND INSTALLED USING BMS 5-128 LOT: 1536130-2. ASSEMBLED VACUUM BAG SYSTEM. PERFORMED 5X5 LEAK TEST, PASSED USING VACUUM GAUGE ID: ATS2107 DUE: 12/2023. CURED PLY USING THERMOMETER ID: ATS2208 DUE: 10/2023. REMOVED VACUUM BAG SYSTEM AND TRIMMED EXCESS MATERIAL. IAW SRM 51-70-14-2R-3 PARA 4.A.(3-5, 11)

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 56,002 hrs · 37,056 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED.<[01] UPDATED MEASUREMENT CHART.;[02] REMOVED THE DAMAGE PART AND INSTALLED REPAIR PARTS AT R/H HORIZONTAL STAB. INSPAR RIB; STAB STA 129.5 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[03] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 2 AND MEASUREMENT TABLE.

Part: SUPPORT — CRACKED (ZN 600 RIGHT WIN) · airframe 56,002 hrs · 37,056 cycles

(RIGHT WING) UPPER SURFACE PANEL BETWEEN #5 AND #6 SPOILERS; LOWER SURFACE SUPPORT GUSSETT IS CRACKED AT LOWER ATTACH FASTENER<[01] CORRECTION TO NRC; GUSSETT IS BETWEEN #7 AND 8 SPOILERS RIGHT WING;[02] REMOVED AND REPLACED (RIGHT WING) UPPER SURFACE PANEL BETWEEN #7 AND #8 SPOILERS; LOWER SURFACE SUPPORT GUSSETT P/N 115A2982-10 IAW SRM 51-40-02 AND AIPC 57-50-00-25.<BR>MEASUREMENT TABLE UPDATED.;[03] VERIFIED CORRECTIVE ACTION 2.

Part: PRESSURE DECK — CRACKED (ZN 100 FUS LOWER) · airframe 56,002 hrs · 37,056 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED AT STA 663+1.5; RBL 41; WL 203. (MARKED)<[01] UPDATED STEP 5.;[02] REPAIR OF HORIZONTAL PRESSURE DECK AT AT BS 663+1.5 RBL35 TO RBL 61 IAW SRM 53-40-51-2R-2 REPAIR 2; DWG 144A7730 AND AIPC 53-21-00-10B;[03] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 2 AND MEASUREMENT TABLE.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 54,899 hrs · 36,342 cycles

L2 DOOR EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK ON L2 DOOR AND PERFORMED OPS CHECK. OPS CHECK GOOD. NO FAULTS;;[02] AUDIT C/W

Part: SLIDE — LOW (ZN 200 FUS TOP) · airframe 54,745 hrs · 36,263 cycles

R1 ESCAPE SLIDE PRESSURE GAUGE BELOW GREEN<[01] REMOVED AND REPLACED FWD SERVICE DOOR SLIDE IAW AMM 25-66-01. REF TASKCARD TTG8Q00J9N8Z

Part: DOOR — FAULTY (ZN 700 LANDING G) · airframe 54,627 hrs · 36,190 cycles

AFTER T/O WHEN PLACING GEAR HANDLE TO OFF ALL 3 RED DISAGREE LIGHTS ILLUMINATED AND WE HEARD/FELT THAT EITHER A GEAR DOOR OR LANDING OR LANDING GEAR MOVED OUT OF THE RETRACTED POSITION. PUT THE HANDLE BACK UP AND LIGHTS WENT OUT. PUT IT BACK TO OFF FUNCTIONED NORMALLY. ALL BELOW 240 KTS<[01] PERFORMED MAIN LANDING GEAR AND NOSE LANDING GEAR OPERATIONAL TESTS IAW AMM 32-32-00. OPERATIONAL TESTS PASSED; NO DEFECTS NOTED.;[02] PERFORMED MAIN LANDING GEAR AND NOSE LANDING GEAR OPERATIONAL TESTS IAW AMM 32-32-00. OPERATIONAL TESTS PASSED; NO DEFECTS NOTED. AND AMM 32-33-00. REF L/P 2143027

Part: LIGHT — WORN (ZN 200 FUS TOP) · airframe 54,512 hrs · 36,128 cycles

PHOTOLUMINESCENT TRACK LIGHTING WORN AT FORWARD ENTRY RH SIDE SECTION AN.<[01] R+R FLOOR PROXIMITY PHOTOLUMINESCENT STRIP PER AMM 33-51-15

Part: GIRT BAR — OUT OF ADJUST (FWD SERVICE DOOR) · airframe 54,085 hrs · 35,862 cycles

GIRT BAR HOLDER CLASPS REPORTED LOOSE AT FORWARD SERVICE DOOR. ADJUSTED THE GIRT BAR RETENTION HOOKS IAW SIP.

Part: NONE — CRACKED (R1 DOOR) · airframe 53,523 hrs · 35,493 cycles

AFT GALLEY SERVICE DOOR LOWER PAN CRACKED ON FORWARD SIDE WITH DOOR OPEN. / [01] REMOVED AND REPLACED PAN ASSY REF AMM 52-41-31 AND AIPC 52-41-31

Part: LENS — LOOSE (R1 DOOR) · airframe 52,315 hrs · 34,775 cycles

EXIT SIGN LENS OVER FWD SERVICE DOOR FELL OFF / [01] REINSTALLED FWD SERVICE DOOR EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01 AND OK TO CONTINUE IN SERVICE.

Part: GIRT BAR — BROKEN (FWD ENTRY DOOR) · airframe 52,160 hrs · 34,689 cycles

FWD ENTRY DOOR GIRT BAR RELEASE STOP SLEEVE BROKEN / [01] R&R?D RELEASE STOP SLEEVE PER SIP

Part: GIRT BAR — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 51,796 hrs · 34,485 cycles

FORWARD ENTRY DOOR GIRT BAR DIFFICULT TO REMOVE FROM THE STOWED POSITION / [01] ADJUSTED SLIDE COVER CLIP PER AMM 5-66-00.

Part: LIGHT — FAILED (AFT CABIN) · airframe 51,604 hrs · 34,391 cycles

AFT R/H EMERGENCY LIGHT BATTERY PACK FAILED ; / [01] REMOVED AND REPLACED AFT R/H EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-06

Part: DOOR — LOOSE (L1 DOOR) · airframe 51,579 hrs · 34,376 cycles

FORWARD ENTRY DOOR (CAPT SIDE) SLIDE RETAINING CLIPS REPORTED LOOSE BY F/A AND OPS AGENT ; FORWARD ENTRY DOOR (CAPT SIDE) SLIDE RETAINING CLIPS REPORTED LOOSE BY FA AND OPS AGENT / [01] ADJUSTED FWD ENTRY DR (CPT SIDE) SLIDE RETAINING CLIPS REF AMM 52-11-00. OPS CK GOOD.

Part: NONE — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK INNER CHORD LOCATED BS303.9 AT LEVEL STR 17L LH SIDE AT FWD GALLEY AREA ; 2021-403943 / [16] REPLACED INNER CHORD LOC BS 277 TO BS 360 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 AND DWG 141A8110 SHEET 11 REV: -; [17] STEP 15 COMPLETED.; [18] CORRECTIVE STEP 16<BR>REPLACED INNER CHORD LOC BS 277 TO BS 360 AT LEVEL STR 17L LH SIDE AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 AND DWG 141A8110 SHEET 11 REV: -; [19] JOB COMPLETED AND CERTIFIED AS RII.

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 50,751 hrs · 33,909 cycles

CRACKED ANGLE BS 695, RBL 24.5 FLOOR STRUCTURE AT CENTER WING BOX. REMOVED ANGLE NO FOUND ALLOWABLE DAMAGE LIMITS IAW SRM 51-40-02, MEASURE OF CRACK IS L=1.58. PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO MORE FOUND DAMAGE. FORMED ANGLE IAW DWG 273A9112, SHEET 30, REV. HEAT TREATED TO 7075-T73 IAW DWG 273A9112 SHEET 30 REV- AND BAC 5602 TABLE IV AND TABLE XI. DRILLED HOLES IAW DWG 273A9112, SHEET 30, REV-, 51-40-05. APPLIED PROTECTIVE TREATMENT ON ANGLE AND NEW HOLES IAW SRM 52-40-02. INSTALLED REPAIR ANGLE IAW SRM 51-10-02 STEP 9, 51-40-02, AND DWG 273A9112 REV -.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CORROSION WATER SERVICE DOOR 146AR SUPPORT ANGLE LOCATED BETWEEN BS 907 TO BS 927 STR 25R TO STR 27R WL 168.1 AT LOWER FUSELAGE ; 2021-403934 / 14] REPLACED SUPPORT ANGLE ON WATER SERVICE DOOR 146AR LOCATED BETWEEN BS 907 TO BS 927 STR 25R TO STR 27R WL 168.1 AT IAW I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 DWG #147A7221 SHEET: 15 REV: B; [15] TASK COMPLETED

Part: SPAR — CORRODED (VERTICAL STAB) · airframe 50,751 hrs · 33,909 cycles

PITTING ON DORSAL FIN FRONT SPAR FITTING RH BOLT (STA 1016) AT VERTICAL STABILIZER (1EA) ; 2021-403818 / [01] REMOVED RH BOLT ON DORSAL FIN FRONT SPAR FITTING AT VERTICAL STABILIZER (STA 1016) IAW B737-700 AMM 55-30-00-000-801 STEP 2F(7)(B) AND PERFORMED GENERAL VISUAL INSPECTION ON BORE ADJACENT AREA AND NOT FOUND DAMAGE.; [02] STEP 1 COMPLETE CERTIFIED; [03] OK TO INSTALL NEW BOLT ON DORSAL FIN FRONT SPAR FITTING AT VERTICAL STABILIZER ON RH SIDE (STA 1016) IAW B737-700 AMM 55-30-00-400-801 STEP 3G(3).; [04] OK GRANTED; [05] INSTALLED NEW BOLT ON DORSAL FIN FRONT SPAR FITTING AT VERTICAL STABILIZER ON RH SIDE (STA 1016) IAW B737-700 AMM 55-30-00-400-801 STEP 3H(1)(D) THRU STEP 3H(1)(F).; [06] CORRECTIVE ACTION FROM STEP 5 INSTALLED NEW BOLT ON DORSAL FIN FRONT SPAR FITTING AT VERTICAL STABILIZER ON RH SIDE (STA 1016) IAW B737-700 AMM 55-30-00-400-801 STEP 3H(1)(D) THRU STEP 3H(1)(F). TOOL USED:TORQUE 40-200 P/N: QD2R200 S/N 0718904669 DUE DATE: 30 DEC 21; TORQUE 200-1000 P/N QD2R1000A S/N: 0319122576 DUE DATE 31 OCT 21; [07] COMPLETE STEP 6 RII CERTIFIED; [08] REMOVED AND REPLACED BOLT ON DORSAL FIN FRONT SPAR FITTING AT VERTICAL STABILIZER ON RH SIDE (STA 1016) IAW B737-700 AMM 55-30-00-000-801 STEP 2F(7)(B) AND IAW B737-700 AMM 55-30-00-400-801 STEP 3H(1)(D) THRU STEP 3H(1)(F). TOOL USED:TORQUE 40-200 P/N: QD2R200 S/N 0718904669 DUE DATE: 30 DEC 21; TORQUE 200-1000 P/N QD2R1000A S/N: 0319122576 DUE DATE 31 OCT 21.; [09] JOB COMPLETED AND CERTIFIED AS RII.

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 50,751 hrs · 33,909 cycles

CRACK LEADING EDGE RIB LOCATED AT ACCESS PANEL 314B LE STA 114.55 AT RT HORIZONTAL STABILIZER ; 2021-403770 / [11] INSTALLED NEW RIB AND FASTENER LOCATED AT ACCESS PANEL 341B LE STA 114.55 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 186A1001 REV: A; [12] STEP 11 COMPLETE RII CERTIFIED; [13] REPLACED LEADING EDGE RIB LOCATED AT ACCESS PANEL 341B LE STA 114.55 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 186A1001 REV: A; [14] REPLACED LEADING EDGE RIB LOCATED AT ACCESS PANEL 341B LE STA 114.55 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 186A1001 REV: A RII CERTIFIED

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

MISSING MATERIAL FLOOR PANEL 221CF AT PASSENGER CABIN ; 2021-403689 / [21] REPAIRED FLOOR PANEL 221CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [22] REPAIRED FLOOR PANEL 221CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.RII INSPECTION

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK ANGLE LOCATED BS500C BTW STR25L TO STR26L FWD CARGO COMPARTMENT ; 2021-403670 / [01] REMOVED ANGLE LOCATED BS500C BTW STR25L TO STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DUE TO NO FOUND ALLOWABLE DAMAGE ON SRM LENGTH OF CRACK IS 0.696 INCH AND PERFORMED VISUAL INSPECTION ON AREA AND NO FOUND DAMAGE TOOL USED CALIPER P/N: 500-752-20 S/N: B20317422 DUE DATE 05AUG22; [02] STEP 1 COMPLETED; [03] DRILLED NEW ANGLE LOCATED BS500C BTW STR25L TO STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-05; [04] OBTAINED OK TO INSTALL NEW ANGLE AND FASTENER LOCATED BS500C BTW STR25L TO STR26L FWD CARGO COMPARTMENT; [05] COMPLETE STEP 3 & 4 RII <BR>OK TO INSTALL GRANTED; [06] INSTALLED NEW ANGLE AND FASTENER LOCATED BS500C BTW STR25L TO STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 SHEET 5 REV B.; [07] REPLACED NEW ANGLE AND FASTENER LOCATED BS500C BTW STR25L TO STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 TEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 5 REV B.; [08] STEP 6 AND 7 COMPLETED RII<BR>JOB COMPLETED RII

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

BROKEN FLOOR PANEL 241AEF AT AFT GALLEY AND LAV ; 2021-403753 / [01] EVALUATED FLOOR PANEL 241AEF AT AFT GALLEY AND LAV AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 SRM 53-00-50-2R-1 REP 1; PAR 1A. DAMAGE SIZE IS L=1.48 W=1.11 TOOL USED CALIPER P/N 500-197-30 S/N A18135080 DUE DATE 31/JUL/22.; [02] COMPLETED STEP 1.; [03] REMOVED DAMAGED SKIN AND INSERT OF REPAIR AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1 PAR. 3 A TO D.; [04] COMPLETED STEP 3; [05] DRIED REPAIR AREA AS PER B737-700 SRM 53-00-50-2R-1 REP 1.PAR 3E; TOOL USED HOT BONDER P/N:HCS9200B S/N: 16122983 DUE DATE 16/DEC/21.; [21] REPAIRED FLOOR PANEL 241AEF AT AFT GALLEY AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [22] REPAIRED FLOOR PANEL 241AEF AT AFT GALLEY AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.RII INSPECTION

Part: ANGLE — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK ANGLE LOCATED BS500C BTW STR25 TO STR26R FWD CARGO COMPARTMENT. REMOVED ANGLE IAW SRM 51-40-02 DUE TO NO FOUND ALLOWABLE DAMAGE ON SRM LENGTH OF CRACK IS 0.202 INCH AND PERFORMED VISUAL INSPECTION ON AREA AND NO FOUND DAMAGE. DRILLED NEW ANGLE IAW SRM 51-40-05. INSTALLED NEW ANGLE AND FASTENER IAW SRM 51-40-02 AND DWG 143A7505 SHEET 6 REV D. REPLACED ANGLE IAW SRM 51-10-02 TEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 6 REV D.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN. REMOVED TIE CLIP IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AND DID NOT FIND MORE DAMAGE. CRACK LENGTH: 0.656. DRILLED NEW TIE CLIP IAW SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT ON OPENED HOLES IAW SRM 51-20-01. INSTALLED NEW TIE CLIP AND FASTENERS IAW SRM 51-40-02, DWG 141A1110, SHEET 18, REV AND DWG 141A8380 SHEET 14 REV.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK FLOOR PANEL 221BF AT PASSENGER CABIN ; 2021-403681 / [22] REPAIRED FLOOR PANEL 221BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [23] REPAIRED FLOOR PANEL 221BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.RII INSPECTION

Part: FRAME — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK FRAME ON BS 312 LOCATED BETWEEN STR5L TO STR6L LH SIDE AT FWD GALLEY AREA ; 2021-403722 / [30] REPAIRED FRAME ON BS 312 LOCATED BETWEEN STR5L TO STR6L LH SIDE AT FWD GALLEY AREA IAW B737-700 SRM 5,NG,NRC,2021-09-23 23:36:55,18Y,Y,MX,0,0,,CRACK FRAME ON BS 312 LOCATED BETWEEN STR5L TO STR6L LH SIDE AT FWD GALLEY AREA ; 2021-403722"

Part: NONE — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328; RBL30 AT FWD GALLEY AREA. REMOVED WEB AND FASTENERS LOCATED BETWEEN BS 312 TO BS 328, RBL 30 AT FWD GALLEY AREA IAW SRM 51-40-02 REMOVAL WEB AND DID NOT FIND ADDITIONAL DAMAGE. MEASURES OF LENGTH CRACK IS: 2.028 INCH. DRILLED NEW WEB - INTERCOSTAL IAW SRM 51-40-05. INSTALLED NEW WEB - INTERCOSTAL IAW SRM 51-40-02, AND DWG 141A5400, REV -.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK FLOOR PANEL 242AF AT PASSENGER CABIN ; 2021-403677 / [21] REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [22] REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.RII INSPECTION

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK FLOOR PANEL 241ADF AT AFT GALLEY AND LAVATORY ; 2021-403754 / [21] REPAIRED FLOOR PANEL 241ADF AT AFT GALLEY AND LAVATORY AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [22] REPAIRED FLOOR PANEL 241ADF AT AFT GALLEY AND LAVATORY AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII INSPECTION

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

MISSING MATERIAL FLOOR PANEL 221DF AT PASSENGER CABIN ; 2021-403679 / ; [22] REPAIRED FLOOR PANEL 221DF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [23] REPAIRED FLOOR PANEL 221DF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.RII INSPECTION

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CORROSION ANGLE LOCATED BETWEEN BS328 TO BS344 AND STR4L TO STR6L;WL287 AT PASSENGER CABIN ; 2021-403725 / [26] REPLACED ANGLE LOCATED BETWEEN BS328 TO BS344 AND STR4L TO STR6L;WL287 AT PASSENGER CABIN IAW SRM B737-700 51-10-02 AND DWG# 141A1180 REV. F. AND SRM B737-700 51-40-02. DUE TO ALLOWABLE DAMAGE NOT FOUND ON SRM B737-700 AND MUST BE REPLACED; RII

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK FLOOR PANEL 231JF AT PASSENGER CABIN ; 2021-403669 / [23] REPAIRED FLOOR PANEL 231JF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [24] REPAIRED FLOOR PANEL 231JF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1 RII INSPECTION

Part: ANGLE — CORRODED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CORROSION ANGLE LOCATED BETWEEN BS312 TO BS328 AND STR4L TO STR6L; WL288 AT PASSENGER CABIN ; 2021-403724 / [21] REPLACED ANGLE LOCATED BETWEEN BS312 TO BS328 AND STR4L TO STR6L; WL288 AT PASSENGER CABIN IAW SRM B737-700 51-10-02 AND DWG# 141A1180 REV. F DUE TO ALLOWABLE DAMAGE NOT FOUND ON SRM B737-700 AND MUST BE REPLACED; RII

Part: WEB — CORRODED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CORROSION WEB LOCATED BETWEEN STA.303.9 TO STA348.2 AND STR6L; WL282.1 APPROX.LH SIDE AT FWD GALLEY AREA ; 2021-403723 / [23] REPLACED WEB LOCATED BETWEEN STA.303.9 TO STA348.2 AND STR6L; WL282.1 APPROX.LH SIDE AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A8120 SHEET 12; REV B.; [24] CERTIFIED STEP 22 AND 23<BR>REPLACED WEB LOCATED BETWEEN STA.303.9 TO STA348.2 AND STR6L; WL282.1 APPROX.LH SIDE AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A8120 SHEET 12; REV B.

Part: NONE — CORRODED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CORROSION INNER CHORD FLOOR STRUCTURE LOCATED BETWEEN BS 312 - 344, RBL 58, WL 208.1. INSTALLED NEW INNER CHORD 1(EA) AND FASTENERS IAW SRM 51-40-02 AND DWG 141A8310 SHEET 25 REV-.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK FLOOR PANEL 242RF LOCATED AT AFT GALLEY AREA ; 2021-403768 / [17] REPAIRED FLOOR PANEL 242RF LOCATED AT AFT GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [18] REPAIRED FLOOR PANEL 242RF LOCATED AT AFT GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII INSPECTION

Part: NONE — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS328 TO BS344; LBL46 AT FWD GALLEY AREA ; 2021-403742 / [11] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS328 TO BS344; LBL46 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9 SRM AND DWG 141A5400 SHEET 44 REV-; [12] CERTIFIED STEP 9; 10 AND 11 RII

Part: NONE — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK STUD FRAME LOCATED ON BS294.5 AND STR17R AT FWD GALLEY AREA. INSTALLED REPAIR CLIP AND FASTENERS LOCATED AT BS 294.5 AND STR 17L IAW B737-700 SRM 51-40-02 AND 53-10-15-2R-7 REPAIR 7; [23] INSTALLED RII COMPLETE STEP 22; [24] REPAIRED STUD FRAME LOCATED AT BS 294.5 AND STR 17L IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7; [25] COMPLETE

Part: PLATE — CRACKED (R/H WING) · airframe 50,751 hrs · 33,909 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED BTW ORSS 270 TO ORSS 277 RT WING. REMOVED CORRUGATED PLATE IAW SRM 51-40-02, AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO FOUND ADDITIONAL DAMAGE. MEASUREMENT OF CRACK IS: 0.483 INCH. INSTALLED CORRUGATED PLATE IAW SRM 51-40-02, AND DRAWING 115A201-60, REV-.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACK FLOOR PANEL 221FF AT PASSENGER CABIN ; 2021-403623 / ; [24] REPAIRED FLOOR PANEL 221FF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [25] REPAIRED FLOOR PANEL 221FF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.

Part: PLATE — CRACKED (L/H WING) · airframe 50,751 hrs · 33,909 cycles

CRACKED CORRUGATED PLATE TRAILING EDGE BTW WS 253.00 TO WS 278.50 LT WING. REMOVED CORRUGATED PLATE IAW SRM 51-40-02, AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO FOUND ADDITIONAL DAMAGE. NO FOUND ALLOWABLE DAMAGE IN SRM. DRILLED NEW CORRUGATED PLATE IAW SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT ON NEW HOLES IAW SRM 51-20-01. INSTALLED CORRUGATED PLATE IAW SRM 51-40-02 AND DWG 115A2714 REV - REPLACED CORRUGATED PLATE IAW SRM 51-40-02, SRM 51-10-02 PARAGRAPH 9, AND DWG 115A2714 REV -.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

DELAMINATED FLOOR PANEL 221GF AT PASSENGER CABIN ; 2021-403622 / [23] REPAIRED FLOOR PANEL 221GF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [24] REPAIRED FLOOR PANEL 221GF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII INSPECTION

Part: PLATE — CRACKED (L/H WING) · airframe 50,751 hrs · 33,909 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED BTW WS 204.25 TO WS 228.25 LT WING ; 2021-403652 / [08] REPLACED CORRUGATED PLATE TRAILING EDGE AND FASTENERS LOCATED BTW WS 204.25 TO WS 228.25 LT IAW B737-700 SRM 51-10-02 TEM 9; SRM 51-40-02 AND DWG 115A2001 SHEET 30; REV A.; [09] COMPLETED STEP 8 REPLACED CORRUGATED PLATE TRAILING EDGE AND FASTENERS LOCATED BTW WS 204.25 TO WS 228.25 LT IAW B737-700 SRM 51-10-02 TEM 9; SRM 51-40-02 AND DWG 115A2001 SHEET 30; REV A.

Part: ANGLE — CRACKED (L/H WING) · airframe 50,751 hrs · 33,909 cycles

CRACK ANGLE TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 297 LT WING. REMOVED ANGLE IAW SRM 51-40-02. MEASURE OF CRACK IS 0.7852 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND FOUND NO MORE DAMAGE. DRILLED NEW ANGLE IAW SRM 51-40-05, APPLIED PROTECTIVE TREATMENT ON ALL OPEN HOLES NEW ANGLE IAW SRM 51-20-01. INSTALLED ANGLE IAW SRM 51-40-02, DWG 115A2982, SHEET 4, REV-. REPLACED ANGLE IAW SRM 51-10-02, 51-40-02, DWG 115A2982, SHEET 4, REV-.

Part: PLATE — CRACKED (R/H WING) · airframe 50,751 hrs · 33,909 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED BTW WS 228.25 TO WS 253.00 AT RT WING. REMOVED CORRUGATED PLATE TRAILING EDGE LOCATED BTW WS 228.25 TO WS 253.00 AT RT WING IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION AND NOT FOUND DAMAGE ON AREA. MEASURE OF CRACK IS L: 0.860; [03] STEP 2 INCORRECT. TOOK MEASURE OF CRACK IS L: 0.860. STEP 1 AND 3 CERTIFIED, INSTALLED NEW CORRUGATED PLATE TRAILING EDGE AND FASTENERS LOCATED BTW WS 228.25 TO WS 253.00 AT RT WING IAW SRM 51-40-02 AND DWG 115A2001 REV: A. REPLACED CORRUGATED PLATE TRAILING EDGE IAW SRM 51-10-02; SRM 51-40-02 AND DWG 115A2001 REV: A.

Part: WEB — CRACKED (L/H WING) · airframe 50,751 hrs · 33,909 cycles

CRACK WEB TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 297 LT WING. REMOVED WEB TRAILING EDGE IAW SRM 51-40-02. PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO FURTHER DAMAGE DRILLED NEW WEB TRAILING EDGE IAW SRM 51-40-05. APPLIED PROTECTIVE TREATMENT ON ALL OPEN HOLES NEW WEB IAW B737-700 SRM 51-20-01. NSTALLED WEB TRAILING EDGE IAW SRM 51-40-02, AND DWG 115A2512 SHEET 5 REV B.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

DELAMINATED FLOOR PANEL 222CF AT PASSENGER CABIN ; 2021-403625 / [23] REPAIRED FLOOR PANEL 222CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [24] REPAIRED FLOOR PANEL 222CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

DELAMINATED FLOOR PANEL 222AF AT PASSENGER CABIN ; 2021-403628 / [23] REPAIRED FLOOR PANEL 222AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [24] REPAIRED FLOOR PANEL 222AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.

Part: WEB — CRACKED (R/H WING) · airframe 50,751 hrs · 33,909 cycles

CRACK WEB TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 297 AT RT WING ; 2021-403659 / [09] INSTALLED WEB TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 297 AT RT WING I.A.W B737-700 SRM 51-40-02; 115A2512 SHEET 8 REV C.; [10] CORRECTED STEP 9:<BR>INSTALLED WEB TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 297 AT RT WING I.A.W B737-700 SRM 51-40-02; DWG 115A2512 SHEET 8 REV C.; [11] REPLACED WEB TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 297 AT RT WING I.A.W B737-700 SRM 51-10-02; 51-40-02 DWG 115A2512 SHEET 8 REV C; [12] COMPLETE TASK CERTIFIED

Part: SUPPORT BRACKET — CRACKED (R/H WING) · airframe 50,751 hrs · 33,909 cycles

CRACK SUPPORT BRACKET TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 297 RT WING ; 2021-403658 / [08] INSTALLED SUPPORT BRACKET LOCATED TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 297 RT WING I.A.W B737-700 SRM 51-40-02; DWG 115A2930 SHEET 8 REV-.; [09] REPLACED SUPORT BRACKET LOCATED TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 297 RT WING I.A.W. B737-700 SRM 51-10-02; 51-40-02 DWG 115A2930 SHEET 8 REV-.; [10] COMPLETE TASK CERTIFIED

Part: PLATE — CRACKED (R/H WING) · airframe 50,751 hrs · 33,909 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 265.00 RT WING. REMOVED CORRUGATED PLATE TRAILING EDGE IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO FOUND ADDITIONAL DAMAGE. INSTALLED CORRUGATED PLATE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 265.00 RT WING IAW SRM 51-40-02 AND DWG 115A2001 SHEET 29 REV: -. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 265.00 RT WING IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9. AND DWG 115A2001 SHEET 29 REV: -.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

DELAMINATED FLOOR PANEL 231CF AT PASSENGER CABIN ; 2021-403621 / [24] REPAIRED FLOOR PANEL 231CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1; REPAIR 1.; [25] REPAIRED FLOOR PANEL 231CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1; REPAIR 1.

Part: PLATE — CRACKED (R/H WING) · airframe 50,751 hrs · 33,909 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON WS 204.25 TO WS 228.25 RT WING. REMOVED CORRUGATED PLATE IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO FOUND ADDITIONAL DAMAGE. MEASUREMENT OF CRACK IS: 0.474. DRILLED NEW CORRUGATED PLATE TRAILING EDGE IAW SRM 51-40-05. AND APPLIED PROTECTIVE TREATMENT ON NEW HOLES IAW SRM 51-20-01. INSTALLED CORRUGATED PLATE IAW SRM 51-40-02 AND DWG 115A2001 REV A. REPLACED CORRUGATED PLATE IAW SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG 115A2001 REV: A.

Part: ANGLE — CRACKED (R/H WING) · airframe 50,751 hrs · 33,909 cycles

CRACK ANGLE TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 297 RT WING ; 2021-403660 / [08] INSTALLED ANGLE TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 297 RT WING I.A.W B737-700 SRM 51-40-02; DWG 115A2982 SHEET 4 REV-; [09] REPLACED ANGLE TRAILING EDGE LOCATED BTW ORSS 261 TO ORSS 297 RT WING I.A.W B737-700 SRM 51-10-02; 51-40-02 DWG 115A2982 SHEET 4 REV-; [10] CERTIFIED STEP 8 AND 9; TASK CARD COMPLETED

Part: PLATE — CRACKED (L/H WING) · airframe 50,751 hrs · 33,909 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED BTW WS 228.25 TO WS 253.00 LT WING ; 2021-403654 / 08] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED BTW WS 228.25 TO WS 253.00 LT WING IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02 PARAGRAPH 9 AND DWG 115A2001 REV: -; [09] COMPLETED STEP 8.; [10] CORRECT STEP 9 .<BR>COMPLETED STEP 7 INSTEAD 8.; [11] COMPLETED STEP 2.<BR>LATE ENTRY.; [12] COMPLETED STEP. 8.<BR>REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED BTW WS 228.25 TO WS 253.00 LT WING IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02 PARAGRAPH 9 AND DWG 115A2001 REV: -

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

DELAMINATED FLOOR PANEL 222DF AT PASSENGER CABIN ; 2021-403626 / [24] REPAIRED FLOOR PANEL 222DF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1 RII INSPECTION

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

DELAMINATED FLOOR PANEL 221EF AT PASSENGER CABIN ; 2021-403624 / [22] REPAIRED FLOOR PANEL 221EF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1 RII INSPECTION

Part: SUPPORT BRACKET — CRACKED (L/H WING) · airframe 50,751 hrs · 33,909 cycles

CRACK SUPPORT BRACKET LOCATED BTW ORSS 261 TO ORSS 297 AT LT WING ; 2021- 403645 / [01] REMOVED SUPPORT BRACKET LOCATED BTW ORSS 261 TO ORSS 297 AT LT WING DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS FOR CRACK IN SRM B737-700; IAW B737-700 SRM 51-40-02; MEASURE OF CRACK IS 0.614 TOOL USED CALIPER PN:500-752-20; SN:B20317422; DUE DATE: 05AUG22 SUPPORT BRACKET MUST BE REPLACED AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NOT FOUND MORE DAMAGE.; [02] COMPLETED STEP 1.; [03] DRILLED NEW SUPPORT BRACKET LOCATED BTW ORSS 261 TO ORSS 297 AT LT WING IAW B737-700 SRM 51-40-05; [04] DRILLED NEW SUPPORT BRACKET LOCATED BTW ORSS 261 TO ORSS 297 AT LT WING IAW B737-700 SRM 51-40-05; [05] APPLIED PROTECTIVE TREATMENT ON ALL OPEN HOLES NEW SUPPORT BRACKET LOCATED BTW ORSS 261 TO ORSS 297 AT LT WING IAW B737-700 SRM 51-20-01; [06] OK TO INSTALL NEW SUPPORT BRACKET LOCATED BTW ORSS 261 TO ORSS 297 AT LT WING; [07] STEP 5 AND 6 COMPLETED OK TO INSTALL GRANTED; [08] INSTALLED SUPPORT BRACKET LOCATED BTW ORSS 261 TO ORSS 297 AT LT WING I.A.W B737-700 SRM 51-40-02; DWG 115A2930 SHEET 7 REV-.; [09] REPLACED SUPORT BRACKET LOCATED BTW ORSS 261 TO ORSS 297 AT LT WING I.A.W. B737-700 SRM 51-10-02; 51-40-02 DWG 115A2930 SHEET 7 REV-.; [10] CERTIFIED STEP 8 AND 9<BR>TASK CARD COMPLETED

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 50,751 hrs · 33,909 cycles

CRACKED SUPPORT BRACKET, BS 695, BL 0. REPLACED THE SUPPORT BRACKET AND FASTENERS IAW SRM 51-40-02, AND DRAWING 273A9111, SHEET 10 REV -.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 50,751 hrs · 33,909 cycles

INOP EMERGENCY LIGHT BATTERY PACK BS 603 LH SIDE AT PASSENGER CABIN (1 EA) ; 2021-403545 / [01] REPLACED EMERGENCY LIGHT BATTERY PACK BS 603 LH SIDE AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-06-960-805.; [02] TASK COMPLETED <BR><BR>TEST OK

Part: SUPPORT WEB — CRACKED (#1 ENGINE) · airframe 50,751 hrs · 33,909 cycles

CRACK INBOARD FAN COWL SUPPORT WEB ON ENGINE 1 ; 2021-403482 / [01] REPLACED INBOARD FAN COWL SUPPORT WEB ON ENGINE 1 IAW B737-700 SRM 51-10-02 ITEM 9 ;B737-700 SRM 51-40-02 AND CMM 71-13-30; [02] CERTIFIED WORK PERFORMED.

Part: COLLAR — CRACKED (L2 DOOR SLIDE) · airframe 50,158 hrs · 33,601 cycles

AFT ENTRY DOOR ESCAPE SLIDES GIRT BAR RETAINING PIN PLASTIC SLEEVE IS CRACKED. ; / [01] REPLACED GIRT BAR STOP COLLAR PER SIP; [02] REPLACED GIRT BAR STOP COLLAR PER SIP

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,229 hrs · 33,086 cycles

AREA EMERGENCY LIGHT AT 6 FED INOP. RELAMPED AREA EMERGENCY LIGHT AT 6 FED REF AMM 33-51-03; OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,596 hrs · 32,717 cycles

EMERGENCY LIGHTS IN AFT CABIN AND AFT EXTERIOR INOPERABLE. CHARGED EMERGENCY LIGHT BATTERY & PERFORMED OPERATIONAL CHECK, IAW AMM 33-51-00. NO DEFECTS NOTED.

Part: TRUNNION — BULGED (LT MLG) · airframe 48,467 hrs · 32,642 cycles

L/H FWD TRUNNION SUPPORT FITTING HAS IMPACT DAMAGE AT THE LOWER INBD LUG; DAMAGE TO THE AFT FACE MEASURES LENGTH = .75; WIDTH = .30 & DEPTH =.10; DAMAGE CAUSED A BULGE TO THE OUTBD FACE OF LUG WHICH MEASURES LENGTH = .75; WIDTH = .25 AND WEIGHT = .075 / CW EA 20-157-01524 PART 1; PART 2 & REV IR

Part: SIGN — LOOSE (CABIN) · airframe 48,298 hrs · 32,547 cycles

FWD GALLEY CALL LIGHT INDICATOR FELL DOWN. REPLACED THE FWD ENTRY EMERGENCY LIGHT SIGN IAW AMM 33-51-01.

Part: PANEL — DELAMINATED (WNG-BDY FAIRING) · airframe 48,007 hrs · 32,372 cycles

WING TO BODY FAIRING 193B PANEL CORNERS FOUND DELAMINATED. / REPLACED WING TO BODY FAIRING PANEL 193B AS PER DOCUMENT41533

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 48,007 hrs · 32,372 cycles

EXTERNAL POWER RECEPTACLE SURROUND DOUBLER DAMAGE WITH .375"CRACK NOTED 4" UP FROM AFT LOWER CORNER JUST BELOW INITIAL RUBBING STRIP. / REPAIRED DOUBLER PER SRM.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 57,665 hrs · 28,838 cycles

L/H EMERGENCY EXIT LIGHT FAULTY AT ROW 9. / R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 57,665 hrs · 28,838 cycles

L/H EMERGENCY EXIT LIGHT FAULTY AT ROW 7. / R&R BATTERY PACK PER MM.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 57,665 hrs · 28,838 cycles

L/H EMERGENCY EXIT LIGHT FAULTY AT ROW 12. / R&R BATTERY PACK CHARGER PER MM.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 57,665 hrs · 28,838 cycles

R/H EMERGENCY EXIT LIGHT FAULTY AT ROW 9. / R&R BATTERY PACK CHARGER PER MM.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 57,665 hrs · 28,838 cycles

L/H EMERGENCY EXIT LIGHT FAULTY AT ROW 7. / R&R BATTERY PACK CHARGER PER MM.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 57,665 hrs · 28,838 cycles

R/H EMERGENCY EXIT LIGHT FAULTY AT ROW 9. / R&R BATTERY PACK PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,816 hrs · 31,681 cycles

RIGHT OVERWING EXIT SIDEWALL EMERGENCY FLOOD LIGHT AFT LIGHT INOPERATIVE. R&R LAMP IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,816 hrs · 31,681 cycles

FORWARD ENTRY HORSESHOE PANEL EMERGENCY CEILING LIGHT INOPERATIVE. R&R LAMP LIGHT IAW AMM.

Part: CAP — CRACKED (AFT CARGO) · airframe 46,816 hrs · 31,681 cycles

: CAPSTRIP FOR AFT CARGO PIT SIDEWALL PANEL 142KW JUST FWD OF THE DOOR IS CRACKED (P/N 453A2411-1) / VERIFIED NEW CAPSTRIP FOR AFT CARGO PIT SIDEWALL PNL 142KW JUST FWD OF THE DOOR I/A/W IPC 25-52-06-08 P/N 453A2411-1 A-TAG# A36851

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE CRACKED / REPAIRED AFT CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE ON BACK SHOP W/O 39968-1600-0009 IAW SWA EA NO. 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 46,816 hrs · 31,681 cycles

FWD CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED / FWD CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE BEEN REPAIR IN BACK SHOP ON N/R 39968/1400/0002 IAW SW EA # 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED / REPIARED AFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE ON BACK SHOP W/O 39968-1600-0010 IAW SWA EA NO. 1-A53-2076 REV. 11

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 46,816 hrs · 31,681 cycles

L2 FLOOR BEAM CORRODED AT BS. 986.5, BETWEEN LBL 4 TO LBL 52. REPAIRED FLOOR BEAM IAW SRM.

Part: STRIP — CORRODED (AFT CARGO THRESH) · airframe 46,816 hrs · 31,681 cycles

WHILE ACCESSING FOUND NUT PLATE STRIP P/N 146A8128-22 CORRODED ON INBD LOWER DOOR SILL STRAP STA 767+10' TO 794 RBL 24 / REMOVED CORRODED NUTPLATE STRIP AT AFT CARGO LOWER DOOR SILL STA 767+10' TO 794 RBL 24 I.A.W SRM 51-40-02-0G-0. EVALUATE STRIP NO ALLOWABLE LIMITS FOUND IN SRM 53-60-15-1A-1. FABRICATED NEW STRIP I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 146A8128. INSTALLED FABRICATED STRIP I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 146A8340.

Part: PANEL — CRACKED (L1 DOOR) · airframe 46,816 hrs · 31,681 cycles

L1 FORWARD MID COVE PANEL FOUND CRACKED ON LOWER END. REPAIRED IAW EA.

Part: RAIL — OUT OF TOLERANCE (AFT CARGO) · airframe 46,816 hrs · 31,681 cycles

REMOVE AND REPLACE EXISTING REPAIR ON AFT CARGO FLOOR RAIL BETWEEN STA 747 AND STA 767 RBL 13.8 / UPON FURTHER EVALUATION IT WAS DISCOVERED THAT THE AFT CARGO FLOOR RAIL AT STA 747 RBL 13.8 HAD SHYED ON SEVERAL FASTENERS AND FAILED TO MEET THE REQUIRED REPAIR SPECIFICATIONS VERIFIED NEW FLOOR RAIL TRACK AND REPAIR SPLICE IAW BOEING 737-700 SRM REF 53-00-03-2R-3 PG 20 FIG 5 PART # 7530558 A-TAG WN6375 VERIFIED MATERIAL FOR CHANNEL SPLICE REPAIR IAW BOEING 737-700 SRM REF 53-00-53-2R-3 LOCATED AND DRILLED CARGO FLR RAIL AND BOTH SPLICE CHANNELS IAW BOEING SRM 51-40-05-0G-0 TREATED AND PRIMED NEW SPLICE CHANNEL IAW AMM REF 51-21-72-370-8 INSTALLED NEW RAIL AND SPLICE REPAIR IAW BOEING DWG # 146A7501 ID: 0002 REV A

Part: INTERCOSTAL — CORRODED (BS 787) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT ON TOP OF WEB INTERCOSTAL CORRODED BETWEEN BS. 787 TO BS. 787+5, BETWEEN STR. 25R TO STR. 26R. / REPAIRED INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO RT Z ANGLE INTERCOSTAL CRACKED BETWEEN BS 727A TO BS 727B. R&R INTERCOSTAL IAW SRM & DWG.

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 46,816 hrs · 31,681 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE NR 2 RIB WEB CRACKED AT CENTER OF WEB CURVE. R & R THE WEB IAW DWG, SRM, & EA.

Part: PANEL — PULLED (FUSELAGE) · airframe 46,816 hrs · 31,681 cycles

PASSENGER CABIN; AFT WET AREA; FLOOR PANEL 242UF; UPPER SURFACE FIBERS PULLED OFF ACROSS WIDTH OF PANEL ON A MAJORITY OF THE UPPER SURFACE. / REEPAIRED FLOORBOARD PANEL 242UF UPPER SURFACE IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS 3 (A-N).

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 46,816 hrs · 31,681 cycles

PASSENGER CABIN; AFT WET AREA; FLOOR PANEL 241ABF; UPPER SURFACE FIBERS PULLED OFF ACROSS WIDTH OF PANEL APPROX 8'; 12'; 21'-24'; AND 29.5' FROM FORWARD EDGE. / REPAIRED UPPER SURFACE FACESHEET MISSING FIBERS WITH WET-LAY-UP REPAIR ON FLOORBOARD PANEL (241ABF) IN AFT WET AREA I/A/W B737-700 SRM 53-00-50-2R-1 (3) A-M (REV 68)

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 46,816 hrs · 31,681 cycles

CABIN FLOOR PANEL 231ZF AREA OF DELAM / REPAIRED AREA OF DELAM ON FLOORBOARD PANEL 231ZF IAW SRM 53-00-50-2R-4; PG'S 1; 2; 3 STEPS 3(A-N).

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 46,816 hrs · 31,681 cycles

PASSENGER CABIN; AFT WET AREA; FLOOR PANEL 241XF; UPPER SURFACE FIBERS PULLED OFF FULL LENGTH OF PANEL AT 2 EA AREAS APPROX 14'-17' FROM LEFT EDGE AND 14'-17' FROM RIGHT EDGE OF PANEL. / REPAIRED FLOOR BOARD 241 XF UPPER SURFACE IAW SRM 53-00-50-2R-1 PG'S 1 2 STEPS 3 (A-N)

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 46,816 hrs · 31,681 cycles

PASSENGER CABIN; AFT WET AREA; FLOOR PANEL 241ADF; UPPER SURFACE FIBERS PULLED OFF ACROSS WIDTH OF PANEL APPROX 7' AND 23' FROM FORWARD EDGE. / REPAIRED FLOORBOARD PANEL 241 ADF UPPER SURFACE FROM FWD EDGE IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS3(A-N).

Part: FAIRING — CORRODED (FUSELAGE) · airframe 46,816 hrs · 31,681 cycles

EXTERNAL LOWER FUSELAGE; MID FORWARD FAIRING 191D; DOUBLER AROUND OPENING FOR ATTACHED PANEL 191E IS CORRODED AT 2 EA HINGE LOCATIONS. / BLENDED CORROSION AT LOWER FUSELAGE FAIRING 191D DOUBLER AROUND OPENING FOR ATTACHED PANEL 181E. ORIGINAL .100; REMAINING .060; LOSS OF .040' FOUND OUT OF LIMITS IAW SRM 53-30-70-1A-1. REMOVED AND REPLACED DOUBLER IAW SRM 51-40-02-0G-0 AND DWG 149A7153 REV. D. APPLIED CIC TO NEW DOUBLER AND DISTURBED AREAS IAW AMM 51-21-91-620-802 TOOL # 27213 DUE: 02/05/2020

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 46,816 hrs · 31,681 cycles

PASSENGER CABIN; AFT WET AREA; FLOOR PANEL 242VF; UPPER SURFACE FIBERS PULLED OFF FULL LENGTH OF PANEL APPROX 2.5' FROM RIGHT EDGE. / REPAIRED FLOORBOARD PANEL 242VF UPPER SURFACE IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS 3(A-M)

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140DF HAS CORROSION AROUND FASTENER HOLES FWD AND AFT SIDE AND AROUND EDGES / VERIFIED LIMITS ON AFT CARGO FLOOR PANEL 140DF; LENGTH OF DAMAGE 90' MAX ALLOWED 20' FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-53-1A-1 FABRICATED NEW PANEL IAW BOEING DWG 453A2610 REVB; PL 453A2610 REV K

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

FWD CARGO COMPARTMENT CORROSION ON AFT SHIELD BETWEEN STA 500/500A RBL 25 WL 156 / REMOVED CORROSION ON AFT SHIELD BETWEEN BS 500-500A FWD CARGO RBL 25 WL156 ORIGINAL THICKNESS .020' MATERIAL REMOVED .006'; MATERIAL REMAINING .014'; MATERIAL FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FABRICATED & REPLACE AFT SHIELD BS 500-500A IAW DWG#143A8126 INSTALLED FABRICATED SHIELD IAW SRM 51-40-02-0G-0 APPLIED CIC IAW AMM 51-21-91

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

FWD CARGO COMPARTMENT FWD SHIELD AT STA 420+10' RBL 25 CORRODED / REMOVED CORROSION ON SHIELD AT BS 420+10.' RBL 25 ORIGINAL THICKNESS .020'; MATERIAL REMOVED .004'; MATERIAL REMAINING .0016' MATERIAL FOUNDD TO BE OUT OF LIMITS IAW S RM 53-00-53-1A-2 FIG 103 (D). REMOVED AND REPLACED FWD SHIELD AT BS 420-440 RBL 25 IAW SRM 51-40-02-0G-0 & DWG #143A8126

Part: SUPPORT ANGLE — CORRODED (FWD CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

FWD CARGO COMPARTMENT UPPER LH BKHD ANGLE STA 500D LBL 52 1/4 TURN RECEPTACLE CORRODED ON AFT SIDE / REMOVED AND REPLACED UPPER ANGLE AT FWD CARGO COMPT AFT BULK HEAD STA 500D FROM LBL 60 - RBL 60 IAW BOEING DRAWING 143A9481 REV A AND B 737 SRM 51-40-02-0G-0

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO COMPARTMENT RH CAP STRIPS HAVE EVIDENCE OF CORROSION / RECEIVED AND VERIFIED MATERIAL LOCATED AND DRILLED NEW RH CAP STRIPS IAW BOEING 737 SRM REF 51-40-05-0G-0 P/N 453A2611-13; 453A2611-9; 453A2611-11 & 453A2611-3 STA 727 TO 787 RBL 25

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140AF CORRODED AT FWD EDGE / REMOVED DAMAGE FROM AFT CARGO COMPARTMENT FLOOR PANEL 140AF AND CHECK LIMIT FOUND TO BE OUT OF LIMIT 42' LENTH MAX ALLOWED 20'; FABRICATED NEW PANEL P/N 453A2610-33 TREATED AND PRIMED PNL IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-1; SRM 51-40-02; DEG 453A2610 REV B AND AMM 51-21-72-370-804

Part: SUPPORT ANGLE — CORRODED (FWD CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

FWD CARGO COMPARTMENT STA 500D WL 156 FROM RBL 25 TO LBL 25 BKHD ANGLE CORRODED / REMOVED AND REPLACED LOWER ANGLE AT FWD CARGO COMPARTMENT AFT BULK HEAD STA 500 D WL 156 FROM LBL 25 - RBL 25 IAW BOEING DRAWING 143A9481 REV A AND B 737 SRM 51-40-02-0G-0

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO COMPARTMENT LH CAP STRIPS HAVE EVIDENCE OF CORROSION / EVALUATED EVIDENCE OF CORROSION ON AFT CARGO L/H CAP STRIPS; NO ALLOWABLE LIMITS TO BE FOUND IN SRM 53-00-53-1A-1 REPLACED L/H CAP STRIPS ON BENCH

Part: SUPPORT ANGLE — CORRODED (FWD CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

FWD CARGO COMPARTMENT UPPER LH BULKHEAD ANGLE STA 500D CORRODED LBL 53 TO LBL 60 IN RADIUS WL 196 / REMOVED AND REPLACED UPPER ANGLE AT FWD CARGO COMPT AFT BULK HEAD STA 500D WL 196 FROM LBL 60 - RBL 60 IAW BOEING DRAWING 143A9481 REV A AND B 737 SRM 51-40-02-0G-0 ACCOMPLISHED WORK IN NON ROUTINE NO. Y111970

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,816 hrs · 31,681 cycles

FORWARD CARGO COMPARTMENT Z ANGLE CORRODED BETWEEN BS 460 TO BS 480, LBL 25. R&R Z ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FWD CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

FWD CARGO COMPARTMENT UPPER LH BKHD ANGLE STA 500D LBL 40 AFT SIDE CORRODED AROUND FASTENER / REMOVED AND REPLACED UPPER ANGLE AT FWD CARGO COMPT AFT BULK HEAD STA 500D FROM LBL 60 - RBL 60 IAW BOEING DRAWING 143A9481 REV A AND B 737 SRM 51-40-02-0G-0 ACCOMPLISGED WORK IN NON ROUTINE NO Y111970

Part: ATTACH BRACKET — CRACKED (AFT SERVICE DOOR) · airframe 46,816 hrs · 31,681 cycles

AFT GALLEY SERVICE DOOR; PANEL 844DZ; ATTACH BRACKET CRACKED. / REMOVED AND REPLACED ATTACH BRACKET ON AFT GALLEY SERVICE DOOR PANEL 844 DZ IAW BOEING DWG 411A2119 REV E - A TAG A27572

Part: ATTACH BRACKET — CRACKED (AFT ENTRY DOOR () · airframe 46,816 hrs · 31,681 cycles

AFT ENTRY DOOR; PANEL 834DZ; ATTACH BRACKET CRACKED. / REMOVED AND REPLACED ATTACH BRACKET ON AFT GALLEY ENTRY DOOR PANEL 834 DZ IAW BOEING DWG 411A2119 REV - A TAG A27570

Part: INTERCOSTAL — CORRODED (ACB DOOR SURROUN) · airframe 46,816 hrs · 31,681 cycles

PRODUCTION REQUEST (W.K.) AFT CARGO DOOR SURROUND STRUCTURE; STA. 847 TO 847+8' STR. 25R INTERCOATAL CORRODED AT NUT PLATE LOCATIONS. (UPPON REMOVAL OF SHIELD ON NR Y111685 FOUND THAT THE MATING SURFACE CORRODED). / REMOVED CORROSION FROM AFT CARGO DOOR SURROUND STRUCTURESTA 847 - 847+8' STR 25R INTERCOSTAL IAW B737 SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS ORIG .063' REMAIN .050' LOSS .013' IAW B737 SRM 53-00-04-1A-1. REPLACED INTERCOSTAL WITH NEW FABRICATED INTERCOSTAL P/N 146A8322-12 IAW B737 SRM 51-40-02-0G-0 & BOEING DWG 146A8322 REV R & REV C & 146A8321 REV -

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 46,816 hrs · 31,681 cycles

RT HORIZONTAL STABILIZER LEADING EDGE #4 RIB FROM INBOARD ROOT CRACKED. R&R #4 RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 46,816 hrs · 31,681 cycles

RT HORIZONTAL STABILIZER LEADING EDGE #3 RIB FROM INBOARD ROOT CRACKED. R&R #3 RIB IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 46,816 hrs · 31,681 cycles

LT HORIZONTAL STABILIZER RIB #4, STAB STA 120.3 LOWER STIFFENER #4 CRACKED. REPAIRED STIFFENER #4 IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO COMPARTMENT RT Z ANGLE LOWER AND UPPER SURFACE CORRODED BETWEEN BS 867 TO BS 907+6, RBL 24. R&R RT Z ANGLE IAW SRM AND DWG.

Part: SHIELD — CORRODED (ACB DOOR CUT) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO DOOR SURROUND STRUCTURE AFT SHIELD STA 847 TO 867 RBL 22 WL 163 HAS CORROSION ON UPPER AND LOWER SURFACES / REMOVED CORROSION AND FOUND OUT OF LIMITS AND INSTALLED NEW SHIELD P/N 146A8127-8 IAW B737-700 SRM 51-40-02-0G-0; SRM 51-40-5-0G-0; AMM 51-21-91-620-82 AN DWG # 146A0081 REV 'A' AT AFT CARGO STA 847 TO 867 RBL 22'.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 46,816 hrs · 31,681 cycles

LT HORIZONTAL STABILIZER RIB #4, STAB STA 120.3 LOWER STIFFENER #2 CRACKED. REPAIRED STIFFENER #2 IAW SRM.

Part: WEB — CORRODED (ACB DOOR CUT) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO DOOR SURROUND STRUCTURE LOWER SILL VERTICAL WEB STA 847 TO 847+9' RBL 19 WL 160 HAS CORROSION ALL OVER / REMOVED CORROSION FROM AFT CARGO DOOR SURROUND STRUCTURE LOWER SILL VERTICAL WEB STA 847 TO 847+9 RBL 19 IAW B737 SRM 51-40-02-0G-0. FOUND OUT OF LIMITS ORG .045' REMAIN .035' LOSS .010' MORE THAN 10% REMOVED IAW B737 SRM 53-60-15-1A-1. REMOVED & REPLACED VERTICAL WEB P/N 146A8123-13 IAW B737 SRM 146A8120 & 146A0081.

Part: NUT PLATE — CRACKED (ACB DOOR CUT) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO DOOR SURROUND STRUCTURE AFT FRAME STA 847 NUTPLATE STRIP BELOW STR 22R IS CRACKED / REMOVED CRACKED NUTPLATE STRI P AT AFT CARGO DOOR SURROUND AFT FRAME; STA847 BELOW STR 22R I.A.W SRM 51-40-02-0G-0. FABRICATED NEW NUTPLATE STRIP I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 146A8201. INSTALLED FABRICATED NUTPLATE STRIP I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 146A8201.

Part: HOOK — CORRODED (ESCAPE STRAP) · airframe 46,816 hrs · 31,681 cycles

LT OVERWING ESCAPE EXIT, ESCAPE STRAP END HOOK CORRODED. R&R STRAP IAW AMM.

Part: CARGO TRACK — CORRODED (BS 927) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO COMPARTMENT TIE TRACK CORRODED AT NUTPLATE HOLE AT BS. 927+7, LBL 3. / R&R TIE TRACK IAW SRM & DWG.

Part: NUT PLATE — CORRODED (ACB DOOR CUT) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO DOOR SURROUND STRUCTURE NUTPLATE STRIP UNDER FLOOR STRAP STA 827+14' TO 847 RBL 18 WL 162 HAS CORROSION AROUND NUTPLATES / REMOVED CORRODED NUT PLATE STRIP AT AFT CARGO DOOR SURROUND STRUCTURE UNDER FLOOR STRAP STA 827+14' TO 847 RBL 18 WL 162 IAW SRM 51-40-02-0G-0. EVALAUTED STRIP NO ALLOWABLE LIMITS FOUND IN SRM 53-60-15-1A-1. FABRICATED NEW STRIP I.A.W SRM 51-40-05-0G 0 AND BOEING DWG 146A8128. INSTALLED & FABRICATED STRIP I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 146A8340.

Part: WEB — CORRODED (FUSELAGE) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO DOOR SURROUND STRUCTURE LOWER SILL WEB CORRODED BETWEEN BS 794 TO BS 827, RBL 26 ON UPPER SURFACE. R&R WEB IAW SRM AND DWG.

Part: NUT PLATE — CORRODED (ACB DOOR CUT) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO DOOR SURROUND STRUCTURE NUTPLATE STRIP UNDER FLOOR STRAP STA 787 TO 794 RBL 24 WL 156 HAS CORROSION AROUND NUTPLATES / REMOVED CORRODED NUTPLATE STRIP AT AFT CARGO DOOR SURROUND STRUCTURE UNDER FLOOR STRAP STA 787 TO 794 RBL 24 WL 158 I.A.W SRM 51-40-02-0G-0. EVALUATED STRIP NO ALLOWABLE LIMITS FOUND IN SRM 53-60-15-1A-1. FABRICATED NEW STRIP I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 146A8128. INSTALLED FABRICATED STRIP I.A.W SRM 51-40-02-0G-0 AN DBOEING DWG 146A0081.

Part: NUT PLATE — CORRODED (ACB DOOR CUT) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO DOOR SURROUND STRUCTURE NUTPLATE STRIP UNDER FLOOR STRAP STA 847+1' TO 847+6' RBL 18 WL 162 HAS CORROSION AROUND NUTPLATES / REMOVED CORRODED NUT PLATE STRIP AT AFT CARGO DOOR SURROUND STRUCTURE FLOOR STRAP STA 847+6 RBL 18 WL 162 IAW SRM 51-40-02-0G-0 EVALUATED STRIP NO ALLOWABLE LIMITS FOUND IN SRM 53-60-15-1A-1. FABRICATED NEW STRIP I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 146A8128. INSTALLED FABRICATED STRIP I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 146A0081.

Part: SHIELD — CORRODED (BS 767-794) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO DOOR SURROUND STRUCTURE FORWARD SHIELD CORRODED BETWEEN BS. 767 TO BS. 794, RBL 24 ON UPPER AND LOWER SURFACE. / REPAIRED SHIELD IAW SRM & DWG.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 46,816 hrs · 31,681 cycles

LT HORIZONTAL STABILIZER RIB #4, STAB STA 120.3 LOWER STIFFENER #3 CRACKED. REPAIRED STIFFENER #3 IAW SRM.

Part: WEB — CORRODED (BS 794-827) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO DOOR SURROUND STRUCTURE LOWER SILL VERTICAL WEB UPPER FLANGE BOTTOM SURFACE CORRODED BETWEEN BS. 794+9" TO BS. 827, RBL 19 AROUND NUTPLATES. / R&R WEB IAW SRM & DWG.

Part: HOOK — CORRODED (ESCAPE STRAP) · airframe 46,816 hrs · 31,681 cycles

RT OVERWING EMERGENCY EXIT, ESCAPE STRAP END HOOK CORRODED. R&R STRAP IAW AMM.

Part: SKIN — CRACKED (RT WING) · airframe 46,816 hrs · 31,681 cycles

RH WING; LOWER LEADING EDGE SLAT #8 NOSE SKIN AT ACTUATOR RIB (SS451.97) HAS INDICATION OF CRACK AT INBOARD FASTENER 2ND FROM AFT EDGE; MARKED. / REMOVED DAMAGE RH WING; LOWER LEADING EDGE SLAT #8 NOSE SKIN AT ACTUATOR RIB STA 451.97. FABRICATED REPAIR DOUBLER (.071 7075-T6) A TAG A23611. AND FILLER (7075-T6) A TAG IAW B-737 SRM 57-42-01-2R-8 REPAIR 8. INSTALLED REPAIR DOUBLER AND FILLERL TO SLAT # 8 STA 451.97 IAW B-737 SRM 57-42-01-2R-8 REPAIR 8 FIG 202 SH. 1. A-TAG-A75441 A-TAG-A23611.

Part: TIE DOWN — CRACKED (AFT CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT FLOOR TRACK STA 747 RBL 13.8 IS CRACKED IN RADIUS OF MOUNTING TAB UNDER TIEDOWN / REPLACED CRACKED TIE DOWN TRACK FROM STA 727-747; RBL 13.8 I.A.W B737 SRM 51-40-02 & BOEING DWG # 146A7500 TY:DWG;ID:0062; REV:-

Part: BRACKET — CRACKED (AFT CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT STA 727 BULKHEAD STRUCTURE BRACKET ASSY RBL 3 WL 165 IS CRACKED AT RIGHT ATTACH TAB / REMOVED AND REPLACED BRACKET ASSY AT AFT CARGO PIT STA 727 BULKHEAD STRUCTURE; RBL 3; WL 165 IAW BOEING DRAWING: 144A2600 REV. - AND B737 SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CORRODED (AFT CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT BILGE INTERCOSTAL STA 827-847 RBL 6 WL 155 HAS CORROSION ON INBOARD SIDE EMITTING FROM VERTICAL STIFFNER / REMOVED CORROSION FROM AFT CARGO PIT BILGE INTERCOSTAL STA 827 - 847 RBL 6 IAW B737 SRM 53-00-04-1A-1. FOUND TO BE OUT OF LIMITS ORIG .040' REMAIN .025' LOSS .015'IAW B737 SRM 53-00-04-1A-1. REMOVED & REPLACED INTERCOSTAL W/NEW P/N 146A8132-14 IAW B737 SRM 51-40-02-0G-0 & BOEING DWG 146A8130 REV B.

Part: PLATE — CORRODED (BS 747-807) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO BAY LT SIDE PLATE CORRODED BETWEEN BS 747 TO 807+15, LBL 24, ON UPPER AND LOWER SURFACES. R & R THE SIDE PLATE IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (AFT CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT BILGE INTERCOSTAL STA 807-827 RBL 6 WL 155 HAS CORROSION ON INBOARD AND OUTBOARD SIDES EMITTING FROM KEEL CHORD STR 27R / EVALUATED CORROSION DAMAGE ON AFT CARGO BILGE INTERCOSTAL STA 807 - 827 RBL 6 FOUND OUT OF LIMITS W/ 100% MATERIAL LOSS IAW B737 SRM 53-00-04-1A-1. REMOVED & REPLACED INTERCOSTAL W/ NEW FABRICATED INTERCOSTAL P/N 146A8132-18 IAW BOEING DWG 146A8132 REV B & A & 146A8130 REV B.

Part: FRAME — CORRODED (BS 767) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT LOWER FRAME EMITTING FROM UNDER FLOOR BEAM CORRODED AT BS. 767, LBL 12. REPAIRED FRAME IAW SRM & AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT FLOOR BEAM CORRODED ON UPPER SURFACE AT BS. 767+6, RBL 3. / REPAIRED FLOOR BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (AFT CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT STRINGER CLIP STA 767 AND STR 23L INBOARD LEG IS CRACKED AT TOP / REMOVED DAMAGED STRINGER CLIP STA 767 AND STR 23L IAW B737 SRM 51-40-02-0G-0. INSTALLED NEW STRINGER CLIP P/N 146A1010-4 ATAG A22186 IAW B737 SRM 51-40-02-0G-0. APPLIED CIC IAW B737 AMM 51-21-91-701.

Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT LEFT FRAME CHANNEL STA 787 LBL 30 WL 160 HAS CORROSION AROUND FASTENER HOLE / BLENDED DAMAGE AT AFT CARGO PIT LEFT FRAME CHANNEL STA 787 LBL 30 WL 160 AROUND FASTENER HOLE IAW B737 SRM 51-10 -02-0G-0 AND SRM 53-00-0 7- 1A-1 FIG 102 DETAIL C. VERIFIED WITH 10X MAG. CHECKED AND VERIFIED LIMITS. ORIGINAL MATERIAL THICKNESS .063'. REMAINING MATERIAL .050'. FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-07-1A-1 FIG 102 DETAIL C / TOOL ID # AAR 36646 / CAL DUE 02 OCT 19. REMOVED DAMAGED FRAME CHANNEL & INSTALLED NEW FRAME CHANNEL P/N 146A9403U89 A TAG A22285 IAW B737 SRM 51-40-02-0G-0 & DWG 146A9403. APPLIED CIC TO FRAME CHANNEL IAW B737 SRM 20-41-05.

Part: FRAME — DENTED (BS 727A) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT LEFT FRAME STA 727A INNER FLANGE IS DENTED LBL 26 2.5" ABOVE STR 25L. / REPAIRED STA 727A FRAME IAW EA.

Part: TIE DOWN — CORRODED (FWD CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

FWD CARGO COMPATMENT FLOOR; AFT TIE-DOWN PLATE ASSEMBLY HAS CORROSION ON LOWER SURFACE; BS 492 RBL24 WL156. / REMOVED CORROSION NO ALLOWABLE LIMITS TO BE FOUND IN SRM 53-00-53-1A-2 FOR AFT TIE DOWN PLATE AT BS492 RBL 24 WL 156 REPLACED AFT TIE DOWN PLATE ON BENCH. A TG # A21713.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT FLOORBEAM CORRODED ON UPPER SURFACE AT BS 767+6, LBL 8.1. REPAIRED CHANNEL PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT FLOORBEAM CORRODED ON UPPER SURFACE AT BS 767+6, LBL 3. REPAIRED CHANNEL PER EA.

Part: PLATE — CORRODED (BS 747-807) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT L/H SIDE PLATE CORRODED BETWEEN BS. 747 TO BS. 807+15, LBL 24, ON UPPER AND LOWER SURFACE. R&R SIDE PLATE IAW SRM AND DWG.

Part: TIE DOWN — CORRODED (FWD CARGO BAY) · airframe 46,816 hrs · 31,681 cycles

FWD CARGO COMPATMENT FLOOR; FWD TIE-DOWN PLATE ASSEMBLY HAS CORROSION ON UPPER AND LOWER SURFACE; BS 440 RBL24 WL156. / REMOVED CORROSION NO ALLOWABLE LIMITS TO BE FOUND IN SRM 53-00-53-1A-2 FOR FWD TIE DOWN PLATE AT BS 440 RBL 24 WL 156 REPLACED FWD TIE DOWN PLATE ON BENCH A TAG # A21729.

Part: CHANNEL — CORRODED (BS 727C-767) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT, RT SIDE PLATE CORRODED ON UPPER AND LOWER SURFACES BETWEEN BS. 727C+17 TO 767, RBL 24. R & R THE RT ZEE CHANNEL IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 46,816 hrs · 31,681 cycles

AFT CARGO PIT FLOORBEAM CORRODED ON UPPER SURFACE AT BS 767+6, RBL 8.1. REPAIRED CHANNEL PER EA.

Part: RETAINER — CRACKED (LEFT WING) · airframe 46,386 hrs · 31,411 cycles

LEFT WING #1 PYLON AFT SPAR SMALL VERTICAL BULB SEAL RETAINER CRACKED. / REMOVED AND REPLACED LEFT WING #1 PYLON AFT SPAR SMALL VERTICAL BULB SEAL RETAINER PER SRM 51-40-02 AND AMM 20-50-11.

Part: PRESSURE SWITCH — DEFECTIVE (APU) · airframe 46,363 hrs · 31,395 cycles

DIVERSION, APU LOW OIL PRESSURE LIGHT APU AUTOMATIC SHUTDOWN INFLIGHT. R&R LOW OIL PRESSURE SWITCH PER AMM.

Part: LUBRICATION UNIT — DEFECTIVE (APU) · airframe 46,363 hrs · 31,395 cycles

DIVERSION, APU LOW OIL PRESSURE LIGHT APU AUTOMATIC SHUTDOWN INFLIGHT. R&R APU LUBE MODULE IAW AMM.

Part: SLIDE — UNSECURE (DOOR) · airframe 46,357 hrs · 31,390 cycles

BOTTOM OF SLIDE DISCONNECTED FROM SAFETY HOOK GIRT BAR REMOVED FROM RETAINER CLIP. RESECURED BOTTOM OF SLIDE IAW MT.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 46,236 hrs · 31,307 cycles

CREW REPORTS ELECTRICAL SMELL WHEN FORWARD ENTRY LIGHT TURNED ON. R&R FORWARD EMERGENCY BATTERY PACK ASSEMBLY D10750 PER AMM.

Part: ENGINE — FOD (LEFT) · airframe 46,027 hrs · 31,179 cycles

DURING CLIMBOUT, STRONG FUMES IN THE CABIN AND COCKPIT (NON-ACRID, NON ELECTRICAL) LEVELED OFF, FUMES DISSIPATED. DIVERTED. COMPLIED WITH BIRD STRIKE BORESCOPE INSPECTION DUE TO PLASTIC AND BIRD DEBRIS IN CORE PER AMM. NO DEFECTS FOUND.

Part: HOUSING — LOOSE (EMERGENCY EXIT) · airframe 45,437 hrs · 30,828 cycles

RT OVERWING EMERGENCY EXT DOOR, LOWER HANDLE HOUSING NOT SECURED. SECURED HANDLE HOUSING PER AMM.

Part: HOUSING — LOOSE (EMERGENCY EXIT) · airframe 45,437 hrs · 30,828 cycles

LT OVERWING EMERGENCY EXIT DOOR, LOWER HANDLE HOUSING NOT SECURED. SECURED HANDLE HOUSING PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,306 hrs · 30,743 cycles

LT OVERWING EMERGENCY EXIT DOOR TOP THREE EMERGENCY EXIT LIGHTS INOP AT PANEL LOCATED AT FORWARD LOWER CORNER. R&R LAMPS IAW AMM.

Part: INTERCOSTAL — CRACKED (FWD FUSELAGE) · airframe 44,391 hrs · 30,148 cycles

INTERCOSTAL CRACKED AT STA. 312 48' LBL. / REMOVED AND REPLACED INTERCOSTAL REF SRM 51-40-02.

Part: ANGLE — CRACKED (AFT CARGO) · airframe 44,391 hrs · 30,148 cycles

LOWER SUPPORT ANGLE FOR AFT CARGO PANEL 141QW IS CRACKED. / REMOVED AND REPLACED PER SRM 51-40-02.

Part: STIFFENER — CRACKED (R/H WHEEL WELL) · airframe 44,391 hrs · 30,148 cycles

STIFFENER LOCATED IN RIGHT WHEEL WELL RBL 25 CRACKED. / REMOVED AND REPLACED PER SRM 51-40-02

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 43,825 hrs · 29,797 cycles

L1 DOOR EMERGENCY SLIDE INADVERTENTLY FELL OUT OF PACK. REINSTALLED SLIDE PER MT.

Part: MODULE — FAULTY (COCKPIT) · airframe 43,814 hrs · 29,790 cycles

AIR TURNBACK, UPON DEPARTURE, GEAR SELECTED UP. WE HEARD GEAR RETRACT, BUT HAD 3 RED GEAR LIGHTS ON SELECTOR. AFTER CLIMB FURTHER AND ABOUT FL180, RED GEAR LIGHTS WENT OUT. R&R LANDING GEAR CONTROL LEVEL MODULE PER MM.

Part: SENSOR — FAULTY (LE SLAT) · airframe 43,662 hrs · 29,696 cycles

DIVERSION, AMBER LEADING EDGE FLAPS TRANSMIT LIGHT CAME ON IN CRUISE. R&R LEADING EDGE SLAT NR 1 INBOARD SENSOR PER AMM.

Part: FASTENER — LOOSE (R1 DOOR) · airframe 43,464 hrs · 29,581 cycles

R1 DOOR GIRT BAR RETAINER LOOSE. R&R FASTENER PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 41,465 hrs · 28,312 cycles

L1 WINDOW ARCED AT TOP OF HEATING ELEMENT. R&R L1 WINDOW PER AMM.

Part: FLOOR SUPPORT — CRACKED (BS 847-867) · airframe 40,662 hrs · 27,786 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 847 TO 867, LBL 17. R & R THE FLOOR SUPPORT IAW SRM.

Part: FRAME — ELONGATED (AFT CARGO BAY) · airframe 40,663 hrs · 27,786 cycles

SUPPLEMENTAL INFORMATION: AFT CARGO STA. 847 FRAME HAS ELONGATED HOLE AT APPROX. LBL 20 AT AREA WHERE L/H TRANSITION ANGLE ATTACHES. / REPAIRED ELONGATED HOLE IN AFT CARGO; STATION FRAME 847; LBL 20' PER EA 1-753-31669 REV 1. SEE INDIVIDUAL WIPS AND TASKS FOR WORK ACCOMPLISHED.

Part: NONE — CORRODED (AFT CARGO BAY) · airframe 40,663 hrs · 27,786 cycles

AFT CARGO L/H TRANSITION ANGLE HAS SURFACE CORROSION AROUND FASTENER HOLES IN BETWEEN STA.727A AND STA. 807. / REMOVED AND REPLACED L/H TRANSITION ANGLE PER SRM 51-40-02

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 40,663 hrs · 27,786 cycles

AFT CARGO R/H TRANSITION ANGLE HAS SURFACE CORROSION AROUND FASTENER HOLES IN BETWEEN STA.727A AND STA. 767. / E105618-BLACKBURN; RICHARD - 09/07/2017 22:40 COMPLETE: REMOVED DAMAGED R/H TRANSITION ANGLE AND INSTALLED NEW SERVICEABLE R/H TRANSITION ANGLE FROM STA 727+4 TO STA 767 IAW SRM 51-40-02.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 40,663 hrs · 27,786 cycles

FWD CARGO FLOOR PANEL 120AF DENTED AND HAS CORROSION. / REMOVED AND REPLACED FLOOR PANEL 120AF IAW AMM 25-52-10.

Part: PLATE — CRACKED (LEFT WING) · airframe 40,663 hrs · 27,786 cycles

WAFFLE PLATE IS CRACKED; RIVET SHEARED ABOVE LEFT AFT STRUT FAIRING AT ORSS 261(MARKED). / REMOVED AND REPLACED WAFFLE PLATE ABOVE LEFT AFT STRUT FAIRING AT ORSS 261 PER SRM 51-40-02

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 40,663 hrs · 27,786 cycles

FWD CARGO AFT CORNER SCUFF PLATE CRACKED. / REMOVED AND REPLACED IAW SRM 51-40-02.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 40,662 hrs · 27,786 cycles

LT WING CENTER SECTION REAR SPAR VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 24+9. REPAIRED WEB PER SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 40,663 hrs · 27,786 cycles

FWD CARGO FWD CORNER SCUFF PLATE CRACKED. / REMOVED AND REPLACED IAW SRM 51-40-02.

Part: PLATE — CRACKED (LEFT WING) · airframe 40,663 hrs · 27,786 cycles

WAFFLE PLATE IS CRACKED; RIVET SHEARED ABOVE LEFT AFT STRUT FAIRING AT ORSS 261(MARKED). / REMOVED AND REPLACED WAFFLE PLATE ABOVE LEFT AFT STRUT FAIRING AT ORSS 261 PER SRM 51-40-02

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 40,663 hrs · 27,786 cycles

AFT CARGO FWD SCUFF PLATE CRACKED / REMOVED AND REPLACED PER TASK CARD 753-721-10-01

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 40,663 hrs · 27,786 cycles

AFT CARGO FLOOR PANEL 140CF HAS A CRACK AND SEVERAL DENTS. / REMOVED AND REPLACED FLOOR PANEL IAW AMM 25-52-10.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 40,663 hrs · 27,786 cycles

AFT CARGO ENTRY AFT CORNER SCUFF PLATE HAS A CRACK AT AFT SIDE. / REMOVED AND REPLACED PER TASK CARD 753-721-10-01

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 40,530 hrs · 27,708 cycles

AFT GALLEY FLASHLIGHT INOP. R&R FLASHLIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,446 hrs · 27,666 cycles

LT EMERGENCY BIN LIGHT INOP AT ROW 16. RELAMPED LIGHT PER AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,629 hrs · 27,201 cycles

FORWARD EMERGENCY LIGHT FAULTY. R&R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,629 hrs · 27,201 cycles

EMERGENCY LIGHT FAULTY AT BS 500. R&R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 39,629 hrs · 27,201 cycles

AFT EMERGENCY LIGHT FAULTY. R&R POWER SUPPLY IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 39,028 hrs · 26,808 cycles

L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. (DID NOT DEPLOY) REINSTALLED SLIDE PER MM.

Part: PLATE — CRACKED (RT WING) · airframe 38,238 hrs · 26,342 cycles

RT WING PANEL 651GB WIGGLE PLATE CRACKED. R&R WIGGLE PLATE PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 38,173 hrs · 26,304 cycles

LT OVERWING EXIT INDICATOR LENS LOOSE. SECURED LENS IAW SIP.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 36,522 hrs · 25,329 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,082 hrs · 24,526 cycles

R1 DOOR EMER LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 34,079 hrs · 23,968 cycles

R2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM & MT.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 34,079 hrs · 23,968 cycles

L2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM & MT.

Part: STRIP — BROKEN (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

AFT CARGO BAY FLOOR, PANEL CAP STRIP BROKEN BETWEEN BS 867 - 947, LBL 9. REPAIRED STRIP IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

INTERCOSTAL CRACKED BETWEEN BS 500A - 500B, LBL 20. R & R INTERCOSTAL IAW ER & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 500D, LBL 20. REPAIRED SUPPORT IAW SRM & DWG.

Part: TAIL CONE — CRACKED (TE FLAP) · airframe 34,079 hrs · 23,968 cycles

NUMBER 6 FLAP TRACK FAIRING TAIL CONE, CRACKED AT AFT UPPER HALF CORNER. REPAIRED TAIL CONE IAW SRM & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

INTERCOSTAL CRACKED, BETWEEN BS 500A - 500B, RBL 20. R & R INTERCOSTAL IAW EA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

FRAME TO STRINGER SUPPORT BRACKET CRACKED AT BS 500D, STRINGER 19L. R & R BRACKET IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

FRAME CORRODED AT BS 500D, RBL 20. REPAIRED FRAME IAW ER & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO 847, LBL 22. R & R SUPPORT IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

SKIN CORRODED AT BS 540, BETWEEN LBL 8 TO RBL 8. REPAIRED SKIN IAW ER & EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 34,079 hrs · 23,968 cycles

RIGHT HORIZONTAL STABILIZER STATION 92.70 RIB CRACKED AT 2ND & 3RD STIFFENERS IN THE LOWER AREA. REPAIRED RIB IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 328-344) · airframe 34,079 hrs · 23,968 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 -344, LBL 47. R & R INTERCOSTAL IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

GIRT BAR FITTING ATTACH BRACKET CORRODED AT BS 312, LBL 57. R & R FITTING IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

FORWARD CARGO COMPARTMENT, FWD BULKHEAD SUPPORT ANGLE CORRODED RT SIDE, BETWEEN STRINGER 25R TO 26R. R & R ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 34,079 hrs · 23,968 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 - 328, RBL 35. R & R INTERCOSTAL IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

GIRT BAR FITTING ATTACH BRACKET CORRODED AT BS 344, LBL 57. R & R FITTING IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 344-360) · airframe 34,079 hrs · 23,968 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 - 360, RBL 1. R & R THE INTERCOSTAL IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

FORWARD CARGO COMPARTMENT, AFT BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN STRINGER 24L - 25L. R & R ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO 328, LBL 47. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

INTERCOSTAL CRACKED BETWEEN BS 276 TO 294, RBL 2. R & R INTERCOSTAL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, RBL 45.5, FASTENER HOLE INBD FWD. REPAIRED FLANGE IAW EA & ER.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 34,079 hrs · 23,968 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, LBL 45.5, FASTENER HOLE INBD FWD & AFT. REPAIRED FLANGE IAW EA & ER.