N469WN

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 70,962 hrs · 42,652 cycles

FWD MEGAPHONE INOPERATIVE. REMOVED AND REPLACED FWD MEGAPHONE BATTERIES IAW AMM 25-64-00

Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 70,885 hrs · 42,596 cycles

CRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE HSS 105.26, LT HORIZONTAL STAB. REPLACED RIB LEADING EDGE ACCESS PANEL 331B IAW SRM 51-40-02, AND DWG 186A1001, SHEET 10, REV A.

Part: ACCESS PANEL — DAMAGED (ZONE 500) · airframe 70,885 hrs · 42,596 cycles

ELONGATED HOLES ON ACCESS PANEL 561BB TRAILING EDGE ON LT WING.

Part: ACCESS PANEL — DAMAGED (ZONE 500 T/E) · airframe 70,885 hrs · 42,596 cycles

ELONGATED HOLES ON ACCESS PANEL 561BB LT WING T/E. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: SUPPORT ANGLE — CRACKED (ZONE 600 T/E) · airframe 70,885 hrs · 42,596 cycles

CRACK ON SUPPORT ANGLE OF ACCESS PANEL 651FB RT WING T/E. REPLACED THE SUPPORT ANGLE LOCATED AT ACCESS PANEL 651FB IAW SRM 51-10-02, ITEM 9, AND DWG 115A2710, SHEET 6, REV B. MEASURE OF CRACK IS: 0.112 INCH.

Part: ANGLE — CRACKED (ZONE 500) · airframe 70,885 hrs · 42,596 cycles

CRACKED ANGLE REAR SPAR AREA AT IRSS 140 UPPER POSITION AT LT WING. REPLACED ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2000, SHEET 21, REV -.

Part: FRAME — WRONG PART (ZN 100 FUS LOWER) · airframe 70,885 hrs · 42,596 cycles

BS 328 FRAME STRAP FROM S20 - 22R, DOES NOT MATCH WITH CONFIGURATION TASK 5311-I-17336-NG, FIGURE 15 2025-740400. REPAIRED THE FRAME IAW EA 25-153-03344-WIP1.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 70,885 hrs · 42,596 cycles

CRACKED SUPPORT ANGLE, LOCATED BS 807, RBL 21, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, AND DWG 146A0081, SHEET 25, REV A.

Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 70,885 hrs · 42,596 cycles

ELONGATED HOLE ON ACCESS PANEL 661CB TRAILING EDGE ON RT WING.

Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 70,885 hrs · 42,596 cycles

ELONGATED HOLE ACCESS PANEL 661BB ON RT WING.

Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 70,885 hrs · 42,596 cycles

ELONGATED HOLE ON ACCESS PANEL 661AB TRAILING EDGE ON RT WING.

Part: ANGLE — CRACKED (ZONE 500) · airframe 70,885 hrs · 42,596 cycles

CRACK ON ANGLE LOCATED AL LEVEL ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 115A2930, SHEET 7, REV -.

Part: ANGLE — CRACKED (ZONE 600 T/E) · airframe 70,885 hrs · 42,596 cycles

CRACK ON ANGLE LOCATED AT LEVEL ORSS 272 DEFLECTION CONTROL RIB AREA RT WING T/E. REPLACED THE ANGLE IAW SRM 51-40-02, AND SRM 51-10-02, ITEM 9.

Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 70,885 hrs · 42,596 cycles

ELONGATED HOLE ACCESS PANEL 661BB, RT WING. REPAIRED THE ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: ACCESS PANEL — DAMAGED (ZONE 600 T/E) · airframe 70,885 hrs · 42,596 cycles

ELONGATED HOLE ON ACCESS PANEL 661CB RT WING T/E. REPAIRED THE ACCESS PANEL 661CB IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: ANGLE — CRACKED (ZONE 600) · airframe 70,885 hrs · 42,596 cycles

CRACK ON ANGLE LOCATED AT LEVEL ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING. REPLACED THE ANGLE IAW SRM 51-40-02, AND SRM 51-10-02, ITEM 9.

Part: ACCESS PANEL — DAMAGED (ZONE 600 T/E) · airframe 70,885 hrs · 42,596 cycles

ELONGATED HOLE ON ACCESS PANEL 661AB, RT WING T/E. REPAIRED ACCESS PANEL 661AB IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: ANGLE — CRACKED (ZONE 500 T/E) · airframe 70,885 hrs · 42,596 cycles

CRACK ON ANGLE LOCATED AT LEVEL ORSS 272 DEFLECTION CONTROL RIB AREA LT WING T/E. REPLACED THE ANGLE IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9.

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 70,885 hrs · 42,596 cycles

DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA). REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) IAW AMM 33-51-15-400-802.

Part: BEAM — CRACKED (ZONE 800) · airframe 70,885 hrs · 42,596 cycles

CRACK INDICATION ON RADIUS OF FORWARD SERVICE DOOR BEAM NR 4. LENGTH OF CRACK: 0.200 INCH. EO 5241-C-14093 OR 5241-C-14344 WILL BE ADDED TO REPAIR ORDER FOR REPAIR. REPLACED BEAM 4 IAW SRM 51-40-02, DWG 141A6516, SHEET 92, REV -, & EA 5241-C-14093-NG.

Part: BEAM — CRACKED (ZONE 800) · airframe 70,885 hrs · 42,596 cycles

CRACK INDICATION ON RADIUS OF FORWARD SERVICE DOOR BEAM NR 4. LENGTH OF CRACK: 0.200 INCH. EO 5241-C-14093 OR 5241-C-14344 WILL BE ADDED TO REPAIR ORDER FOR REPAIR. 2025-740276.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 70,885 hrs · 42,596 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 695 LBL 24.75 WE 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 695 LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW SRM 51-10-02, ITEM 9, AND DWG 273A9110, SHEET 6, REV A.

Part: PRESSURE DECK — CRACKED (ZONE 100) · airframe 70,885 hrs · 42,596 cycles

CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT LBL 31 BETWEEN BS 663 - 675 IN THE MAIN WHEEL WELL. CRACK LENGTH: 0.186 INCH. REPAIRED HORIZONTAL PRESSURE DECK WEB AT LBL 60 - LBL 45.75, BS 663 - 675 IN THE MAIN WHEEL WELL IAW SRM 52-40-51-2R-A, REPAIR 2.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 70,885 hrs · 42,596 cycles

CRACKED FWD CORNER SCUFF PLATE AT FWD CARGO BAY. REPAIRED FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 70,885 hrs · 42,596 cycles

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

Part: SKIN — CRACKED (ZONE 600 SLAT) · airframe 70,885 hrs · 42,596 cycles

CRACK LOWER SURFACE OF LEADING EDGE SLAT NR 8 NOSE SKIN AT ACTUATOR LOCATION. AROUND FASTENER AT RT WING.

Part: SKIN — CRACKED (ZONE 600 SLAT) · airframe 70,885 hrs · 42,596 cycles

CRACKED LOWER SURFACE OF LEADING EDGE SLAT NR 8 NOSE SKIN AT ACTUATOR LOCATION AROUND FASTENER AT RT WING. REPAIRED LOWER SURFACE OF LEADING EDGE SLAT 8 NOSE SKIN AT ACTUATOR LOCATION AT RT WING IAW SRM-57-42-01-2R-8-REPAIR 8.

Part: SKIN — CRACKED (ZN 500 LEFT WING) · airframe 70,885 hrs · 42,596 cycles

CRACKED LOWER SURFACE OF LEADING EDGE SLAT NR 1 NOSE SKIN AT ACTUATOR LOCATION. AROUND FASTENER AT LT WING.

Part: SKIN — CRACKED (ZONE 500 SLAT) · airframe 70,885 hrs · 42,596 cycles

CRACKED LOWER SURFACE OF LEADING EDGE SLAT NR 1 NOSE SKIN AT THE ACTUATOR LOCATION, AROUND FASTENER AT LT WING. REPAIRED LOWER SURFACE OF LEADING EDGE SLAT 1 NOSE SKIN AT ACTUATOR LOCATION, AT LT WING IAW SRM 57-42-01-2R-8, REPAIR 8.

Part: SKIN — CRACKED (ZONE 500 SLAT) · airframe 70,885 hrs · 42,596 cycles

CRACKED LOWER SURFACE OF LEADING EDGE SLAT NR 2 NOSE SKIN AT ACTUATOR LOCATION AROUND FASTENER AT LT WING. REPLACED LEADING EDGE SLAT 2 AND PERFORMED ADJUSTMENT AND OPERATIONAL TEST ARE OK LT WING IAW AMM 27-81-21-000-801, & AMM 27-81-21-400-801.

Part: SLIDE — UNSECURE (ZONE 800) · airframe 70,300 hrs · 42,187 cycles

L2 SLIDE DRAGGING. SECURED LOOSE SLIDE MATERIAL PER AMM 25-66-00.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 69,976 hrs · 41,980 cycles

R2 DOOR EMERGENCY LIGHT INOP. RELAMPED R2 DOOR EMERGENCY LIGHT BULB IAW AMM 33-51-04. OPS CHECK GOOD.

Part: SEAT BACK — OUT OF ADJUST (ZONE 200) · airframe 69,969 hrs · 41,975 cycles

SEAT ROW 12DEF WILL NOT STAY UPRIGHT<[01] TIGHTENED ALL SEATS IN ROW 12 DEF AS PER AMM 25-22-00

Part: CHARGER — TRIPPED (ZONE 200) · airframe 69,078 hrs · 41,429 cycles

C/B LIGHTING EMERGENCY CHGR RF P18-3 B10 POPPED<[01] R+R?D R/H AFT BATTERY CHARGER (M1672) AND BATTERY PACK IAW AMM 31-51-06. EMERGENCY LIGHTS OPS CHK GOOD ALL INDICATIONS NORMAL.

Part: BATTERY PACK — FAULTED (ZONE 200) · airframe 69,078 hrs · 41,429 cycles

REF PREVIOUS LOG PAGE LP 2937321 C/B LIGHTING EMERGENCY CHGR RF P18-3 B10 POPPED<[01] FOUND EMERGENCY EXIT LIGHT BATTERY PACK POPPING THE C/B (M1672) REF LP 2937321 FOR FINAL CORRECTIVE ACTION.

Part: LATCH — LOOSE (ZN 800 DOOR) · airframe 67,784 hrs · 40,638 cycles

FWD MAIN ENTRY DOOR SLIDE LATCH ASSY CAME LOOSE.<[01] RESECURED FWD ENTRY DOOR SLIDE LATCH IAW TASK 725-61-06 AC OK FOR SERVICE

Part: SLIDE — OUT OF ADJUST (FWD SERVICE DOOR) · airframe 66,036 hrs · 39,548 cycles

FWD SERVICE DOOR SLIDE HANGS DOWN TO LOW<[01] REMOVED AND REPACKED SLIDE GIRT BAR REF MT725-61-06

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 65,320 hrs · 39,096 cycles

SEAT 9C EMER LIGHT COVER FELL OFF<[01] OK TO CONTINUE PER MEL 33-15-02. SP1;[02] R&R?D LENS PER AMM 33-51-03

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 65,073 hrs · 38,942 cycles

AFT ENTRY DOOR ESCAPE SLIDE SKIRT CONTACTS THRESHOLD; UNABLE TO CLOSE DOOR PROPERLY.<[01] RE-TUCKED AED ESCAPE SLIDE Z-FOLD INTO SLIDE PACK IAW AMM INTRODUCTION STEP 2.B.;[02] VERIFIED CORRECTIVE ACTION ITEMS; DOOR OPENS AND CLOSES PROPERLY; AND MEASUREMENT FIELDS CARD COMPLETE.

Part: SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 65,073 hrs · 38,942 cycles

FWD L/H FAIRING SUPPORT FOR PANEL 192E IS CRACKED<[01] REMOVED AND REPLACED SUPPORT BRACKET P/N 149A7712-41 PER SRM 51-40-02 AND DWG 149A7701;[02] VERIFIED MEASUREMENT FIELD.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 65,073 hrs · 38,942 cycles

LT. HORIZONTAL STAB UPPER FORWARD SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED LT HORIZONTAL STAB UPPER FORWARD SLIDE SEAL IAW AMM 53-31-31-000-802 AND AMM 53-31-31400-802. VERIFIED SAFETIES.<BR>SCREW GUN: ID: 4441B CAL DUE: 09/2024.;[02] VERIFIED CORRECTION ACTION 1 AND MEASUREMENT TABLE

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 65,073 hrs · 38,942 cycles

CORROSION ON FWD SHIELD AT ACB BS767 - BS787 RBL21 WL157.<[01] REMOVED AND REPLACED ACB FWD. SHIELD. IAW SRM 51-40-02 AND DWG # 146A0081

Part: WEB — CORRODED (ZN 200 FUS TOP) · airframe 65,073 hrs · 38,942 cycles

CORROSION ON WEB AT ACB BS787+4 RBL19 WL157.<[01] REMOVED AND REPLACED WEB INTERCOSTAL P/N 146A8123-22 LOT. 1551095-1. LOCATE BS.787 - 794 RBL 19 WL 158 PER SRM 51-40-02. DWG# 1468123; DWG# 146A8120.<BR>AND REINSTALLED FOR FOM FASTENERS AND INTERCOSTAL WEB LOCATED BETWEEN BS 787 - 794 RBL 25 WL 158 PER SRM 51-40-02.DWG# 146A8320.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.<BR>JOB COMPLETE.

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 65,073 hrs · 38,942 cycles

CRACKED PNEUMATIC-DUCT SUPPORT BRACKET AT STA 540+4 LBL 6; WL 163.<[01] REMOVED AND REPLACED PNEUMATIC-DUCT SUPPORT BRACKET P/N 212A1116-1 LOT:1549921-1 IAW SRM 51-10-02; SRM 51-40-02 DWG# 212A1101.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.<BR>JOB COMPLETE.

Part: ATTACH FITTING — CRACKED (BS 947 LBL 10) · airframe 65,073 hrs · 38,942 cycles

ACB AFT BULKHEAD ATTACH FITTING CRACKED BS947 LBL10 WL180.<[01] REMOVED AND REPLACED FITTING WITH P/N 149A8113-6 LOT. 1510339-2. LOCATED AT BS947 LBL10 WL180. IAW SRM 51-10-02; SRM 51-40-02; DWG# 149A8103.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.<BR>JOB COMPLETE.

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 65,073 hrs · 38,942 cycles

ACB WASTE COMPARTMENT BULKHEAD ATTACH ANGLE CRACKED BS867 LBL11 WL167.<[01] REMOVED AND REPLACED SUPPORT BRACKET WITH P/N 149A8109-114 LOT 1540507-1 LOCATED AT BS 867 LBL 11 WL 167 IAW SRM 51-40-02 DWG# 149A8102.;[02] VERIFIED CORRECTIVE ACTIONS. JOB COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 65,073 hrs · 38,942 cycles

CORROSION AT ACB ON FLOOR TO SIDEWALL SUPPORT BS727 - BS807 LBL21 WL156.<[01] REMOVED AND REPLACED AFT CARGO FLOOR TO SIDEWALL SUPPORT<BR>FROM BS 727 TO BS 847 LBL 21 WL 156 IAW SRM 51-40-02 AND DWG 146A7500.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.;[03] TASK CARD IS COMPLETE

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 65,073 hrs · 38,942 cycles

CORROSION AT ACB ON FLOOR TO SIDEWALL SUPPORT BS727A - BS767 RBL21 WL156.<[01] REMOVED AND REPLACED NEW FLOOR TO SIDEWALL ON ACB BS727 - BS767 RBL21 WL156. IAW SRM 51-40-02-0G-0; DWG 146A7500.-;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.<BR>JOB COMPLETE.

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 65,073 hrs · 38,942 cycles

FWD CARGO BAY BS500C; L/H FLOOR TO SIDEWALL SUPPORT BRACKET AFT SIDE; CRACKED. (MARKED)<[01] REMOVED AND REPLACED LH FLOOR TO SIDEWALL SUPPORT BRACKET AFT SIDE ON FCB BS500C;IAW DGW#143A7505 REV A. AND SRM 51-40-02.;[02] VERIFIED CORRECTION ACTION 1 AND MEASUREMENT TABLE

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 65,073 hrs · 38,942 cycles

FWD CARGO BAY BS400; L/H FLOOR TO SIDEWALL SUPPORT BRACKET AFT SIDE; CRACKED. (MARKED)<[01] REMOVED AND REPLACED LH FLOOR TO SIDEWALL SUPPORT BRACKET AFT SIDE ON FCB BS400;IAW DWG#143A7505 REV B AND SRM 51-40-02.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] VERIFIED CORRECTION ACTION 1 AND MEASUREMENT TABLE

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 65,073 hrs · 38,942 cycles

FWD CARGO BAY BS400; R/H FLOOR TO SIDEWALL SUPPORT BRACKET AFT SIDE; CRACKED. (MARKED)<[01] REMOVED AND REPLACED RH FLOOR TO SIDEWALL SUPPORT BRACKET AFT SIDE ON FCB BS400;IAW DWG#143A7505 REV B.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] VERIFY ALL STEPS COMPLETED;[04] VERIFIED CORRECTION ACTION 1 AND MEASUREMENT TABLE

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 65,073 hrs · 38,942 cycles

FWD CARGO BAY BS500C; L/H FLOOR TO SIDEWALL SUPPORT BRACKET FWD SIDE; CRACKED. (MARKED)<[01] REMOVED AND REPLACED LH FLOOR TO SIDEWALL SUPPORT BRACKET FWD SIDE ON FCB BS500C;IAW DWG#143A7505 REV B AND SRM 51-40-02.;[02] VERIFIED CORRECTION ACTION 1 AND MEASUREMENT TABLE

Part: FLOOR PANEL — PULLED (ZN 200 FUS TOP) · airframe 65,073 hrs · 38,942 cycles

FLOOR PANEL 231XF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FABRICATED FLOOR PANEL 231XF IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE: AND DRAWING 144A5810 ID 0126;[02] VERIFIED JOB COMPLETE AND MEASUREMENT TABLE

Part: PANEL — CRACKED (BS 540 RBL 1) · airframe 65,073 hrs · 38,942 cycles

MID CABIN; WING CENTER SECTION BREAK PANEL IS CRACKED AT I/B FASTENER; BS 540; RBL 1; WL 208 (MARKED)<[01] REMOVED AND REPLACED BREAK PANEL WING CENTER SECTION BS 540 RBL 1 TO RBL 24 WL 208 IAW SRM 51-40-02 AND AIPC 53-42-11-66;[02] VERIFIED CORRECTIVE ACTION ITEMS; AND MEASUREMENT FIELDS CARD COMPLETE; EXCEPT PARTS STILL OPEN FOR AMT.;[03] UPDATED PART REMOVAL;[04] VERIFIED ACTION 3.<BR>JOB COMPLETE.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 65,073 hrs · 38,942 cycles

LH HORIZONTAL STABILIZER RIB AT STAB STA 129.50 CRACKED AT 3RD STIFFENER FROM FRONT<[01] REMOVED THE DAMAGED PART INSTALLED REPAIR PARTS ON LH HORIZONTAL STABILIZER STA 129.50 RIB 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4.;[02] VERIFIED MEASUREMENTS TABLE.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 65,073 hrs · 38,942 cycles

RT HORIZ STAB L/E PANEL 341B HAS CRACKED RIB AT L/E STA 78.29<[01] UPON FURTHER INVESTIGATION NO DAMAGE FOUND AT RT HORIZ. STAB L/E PANEL 341B AT RIB L/E STA 78.29 IAW SRM 51-10-02;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.

Part: PRESSURE DECK — CRACKED (ZN 100 FUS LOWER) · airframe 65,073 hrs · 38,942 cycles

CRACK IN HORIZONTAL PRESSURE DECK BS 670 WL 202 RBL 41.5. CRACK IS APPROX 1/2 INCH LONG MARKED IN RED.<[01] REPAIRED HORIZONTAL PRESSURE DECK BETWEEN BS 663 TO BS 675 WL 202 RBL 30 TO RBL 60 PER SRM 53-40-51-2R-2 REPAIR 2;[02] ACCOMPLISHED THE APPLICATION OF CIC IAW AMM 51-05-01-210-802 14-JAN-2024 14:37 UTC ON CCN: TTG8Q00QQ5VA.<BR><BR>ALL STEPS ARE COMPLETE.

Part: PANEL — CORRODED (RT WG FUEL GAUGE) · airframe 65,073 hrs · 38,942 cycles

RIGHT WING FUELING GAUGE PANEL IS CORRODED AT THE I/B MIDDLE FASTENER (MARKED)<[01] PARTIAL WORK UPDATE ON STEP 1.;[02] PARTIAL WORK STEP 2;[03] UPDATED STEP 2;[04] CERTIFIED STEP 1 AND 2 PARTIAL WORK;[05] COMPLETED WORK STEP 1;[06] COMPLETED STEP 3;[07] VERIFIED COMPLETE STEPS 1;2 AND 3; MEASUREMENTS TABLE OK; CARD COMPLETE.;[08] USED COMPONENTS;[09] VERIFIED ALL AMT STEPS COMPLETE.

Part: FLOOR SUPPORT — CRACKED (ZN 200 FUS TOP) · airframe 64,335 hrs · 38,471 cycles

FLOOR SUPPORT INTERCOASTAL AT STATION 540 IN AIR CONDITIONING DISTRIBUTION BAY LOCATED LEFT OF CENTER LINE IS CRACKED<[01] REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL AT STATION 540 LEFT HAND SIDE PER SRM 51-40-02

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 64,133 hrs · 38,343 cycles

EXTERNAL EMERGENCY LIGHT COVER MISSING ON LEFT OUTSIDE OVERWING EXIT<[01] INSTALLED LENS PER AMM 33-51-04

Part: COVER — MISSING (ZN 200 FUS TOP) · airframe 64,133 hrs · 38,343 cycles

REF PREVIOUS LOG PAGE 2284096 FOR LH OVER WING EXTERNAL EMERGENCY LIGHT COVER M REF PREVIOUS LOG PAGE 2284096 FOR LH OVER WING EXTERNAL EMERGENCY LIGHT COVER MISSING EMERGENCY LIGHT CONSIDERED INOP.<[01] OPS CK'D LIGHT GOOD PER AMM 33-51-00

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,082 hrs · 38,310 cycles

EMERGENCY AREA LIGHT AT 9CBA INOP.<[01] REMOVED AND REPLACED BATTERY PACK FOR AREA LIGHT AT 9CBA. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,082 hrs · 38,310 cycles

L/H EMERGENCY OVERWING LIGHT INOP.<[01] REMOVED AND REPLACED L/H EMERGENCY OVERWING LIGHT IAW AMM 33-51-04

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,082 hrs · 38,310 cycles

EMERGENCY AREA LIGHT AT 12CBA INOP.<[01] REMOVED AND REPLACED BATTERY PACK FOR AREA LIGHT AT 12CBA. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,082 hrs · 38,310 cycles

R/H EMERGENCY OVERWING LIGHT INOP.<[01] REMOVED AND REPLACED R/H EMERGENCY OVERWING LIGHT IAW AMM 33-51-04. OPS CHECKS GOOD

Part: PANEL — ELONGATED (ZN 600 RIGHT WIN) · airframe 62,770 hrs · 37,459 cycles

RH WING LOWER SKIN FIXED TRAILING EDGE PANEL HAS FIVE ENLARGED FASTENER HOLES<[01] REPAIRED IAW SRM 57-51-01-2R-1 AND SRM 51-70-05 2R-8 AND SRM 51-70-14. PERFORMED A NDT TEST PER 737 NDT PART 1 51-01-01. NO DELAMINATION FOUND.;[02] REFINISH REPAIR AREA PER SRM 51-70-05-2R8 AND AMM 51-21-99.;[03] REPAIRED IAW SRM 57-51-01-2R-1 AND SRM 51-70-05 2R-8 AND SRM 51-70-14. PERFORMED A NDT TEST PER 737 NDT PART 1 51-01-01. NO DELAMINATION FOUND.

Part: PLATE — CRACKED (ZN 400 NACELLE/P) · airframe 62,485 hrs · 37,286 cycles

AFT OF 2 ENG PYLON FIXED PANEL WAFFLE PLATE CRACKED<[01] REMOVED AND REPLACED WAFFLE PLATE <BR>REF SRM 51-40-02

Part: GIRT BAR — OUT OF ALIGNMENT (ZN 800 DOOR) · airframe 62,400 hrs · 37,220 cycles

L2 DOOR SLIDE GIRT IS OUT OF CONTAINER TOO FAR<[01] REMOVED SLIDE AND REPACKED SLIDE GIRT IAW B737-700 AMM 25-66-01. GAP CHECK IN COMPLIANCE.

Part: BATTERY — FAILED (ZN 200 FUS TOP) · airframe 62,400 hrs · 37,220 cycles

AFT R/H EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST<[01] REMOVED AND REPLACED BATTERY PACK FOR AFT R/H EMERGENCY LIGHTS OPS CHECK GOOD PER AMM 33-51-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 62,400 hrs · 37,220 cycles

MID R/H EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST<[01] REMOVED AND REPLACED MID R/H EMERGENCY LIGHT BATTERY PACK OPS CHECK GOOD PER AMM 33-51-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 62,400 hrs · 37,220 cycles

MID L/H EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST<[01] REMOVED AND REPLACED L/H EMERGENCY LIGHT BATTERY PACK OPS CHECK GOOD PER AMM 33-51-06

Part: ROPE — LOOSE (ZN 200 FUS TOP) · airframe 62,400 hrs · 37,220 cycles

R/H E/E EMERGENCY ROPE NOT STOWED COMPLETELY<[01] RE-STOWED AND SECURED RH E/E EMERGENCY ROPE; PER AMM 25-61-10

Part: FITTING — CRACKED (ZN 800 DOOR) · airframe 62,400 hrs · 37,220 cycles

L1 DOOR AFT SIDE UPPER STOP FITTING CRACKED<[01] REMOVED STOP FITTING AT L1 DOOR UPPER AFT SIDE AND BEGAN INSTALLATION OF REPLACEMENT STOP FITTING PER SRM 51-40-02;[02] COMPLETED INSTALLATION OF L1 DOOR UPPER AFT SIDE STOP FITTING PER SRM 51-40-02.;[03] INSTALLED AND ADJUSTED L1 DOOR AFT SIDE UPPER STOP PIN PER AMM 52-11-00.

Part: GIRT BAR — DAMAGED (ZN 900 LAV/GALLE) · airframe 62,322 hrs · 37,172 cycles

AFT SERVICE DOOR GIRT BAR PLASTIC PIECE MISSING<[01] INSTALLED NEW SPACER PER SIP

Part: BRACKET — CRACKED (R//H WING) · airframe 61,221 hrs · 36,468 cycles

R/H WING I/B UPPER STABILIZER LINK FWD BRACKET CRACKED R/H WING I/B UPPER STABILIER LINK FWD BRACKET CRACKED / [01] REMOVED AND REPLACED BRACKET PER. SRM REF. 51-20-02.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 61,019 hrs · 36,322 cycles

L1 SLIDE FELL OUT OF CASE / [01] REPOSTIONED AND SECURED SLIDE PER MM 25-66-01

Part: BATTERY PACK — FAILED (AFT CABIN) · airframe 60,520 hrs · 35,981 cycles

AFT R/H EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK / [01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.

Part: LIGHT — INOPERATIVE · airframe 59,572 hrs · 35,384 cycles

EMER LIGHTS BATTERY PACK M1675 INOP. REMOVED AND REPLACED; AND PERFORMED GOOD TEST OF; EMER LIGHT BATT PACK M1675 IAW AMM 33-51-06-960-805.;

Part: WIRE — BROKEN (FWD LAV) · airframe 59,572 hrs · 35,384 cycles

FWD LAV EXIT LIGHT GROUND WIRE BROKEN / [01] RETERMINATED FWD LAV EXIT LIGHT GROUND WIRE W4152-0152-20 INTO GROUND BLOCK GD3782 PER SWPM 20-90-15 AND WDM 33-51-21.<BR>CRIMPER: I.D.: E-3195; CAL DUE: 09/2022;[02] VERIFIED CORRECTIVE ACTION 1.;[03] PERFORMED GOOD FUNCTIONAL TEST OF FWD LAV EMER EXIT IND L1187 IAW AMM 33-51-01-960-801.;[04] STEP 1 COMPLETED; AND VERIFIED CORRECTIVE ACTIONS STEP 3.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

STR CLIP DENTED AND HAS SUSPECTED CRACK; STR 14R BS 344 / [01] REMOVED STR CLIP ON STR 14R BS 344 IAW SRM 51-40-02-0G-0;[02] UPDATED MEASUREMENTS;[03] FABRICATED NEW STR CLIP; MADE FROM BAC1493-852 7075-T62; LOT#1473167-1 IAW SRM 51-40-05-0G-0 AND DWG 141A1150;[04] APPLIED A CHEMICAL CONVERSION COATING TO NEW STR CLIP IAW SRM 51-20-01-0G-0 AND APPLIED PRIMER TO NEW STR CLIP IAW SOPM 20-41-02 AND DWG 141A1150;[05] VERIFIED CORRECTIVE ACTION 4; OK TO INSTALL;[06] INSTALLED STR CLIP STR 14R BS 344 IAW SRM 51-40-02-0G-0 AND DWG 141A1150;[07] VERIFIED CORRECTIVE ACTION 3;[08] VERIFIED CORRECTIVE ACTION 6

Part: FRAME — CRACKED · airframe 59,572 hrs · 35,384 cycles

BS 312 FRAME CRACKED AT STR 5L / [01] REQUEST NDI FOR END OF CRACK;[02] HFEC INSPECTED AND VERIFIED CRACK; PER NDTM PT6 51-00-00 PROCEDURE 23; END OF CRACK MARKED WITH RED;[03] EQUIP ID FOR CORRECTIVE ACTION 2; ATS729;[04] UPDATED MEASUREMENT FIELD;[05] REMOVED DAMAGED AREA 0.3'X 1.0' PER SRM 51-10-02-0G-0;[06] VERIFIED CORRECTIVE ACTIONS STEP 5.;[07] REQUEST NDI TO PERFORM HFEC INSP OF TRIMED EDGE FOR CRACK FREE CONDITION;[08] HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. TOOL N500 ATS729.;[09] REMEASURED DAMAGE TRIM OUT FOR SUBMITTAL TO ENGINEERING AND FOUND DIMENSIONS TO BE:<BR>A: 0.250'<BR>B: 0.200';[10] VERIFIED CORRECTIVE ACTION 9. CORRECT MEASUREMENTS OF DAMAGE TRIM OUT ARE A: 0.250' <BR>B: 0.200';[11] REPAIRED BS 312 FRAME AT STR 5L AS PER EA 22-153-00527;[12] VERIFIED ALL ITEMS COMPLETED. REPAIRED PERFORMED PER 22-153-00527-WIP1 (N469WN - ATS(PAE) - REPAIR - BS 312 FRAME INNER CHORD BETWEEN S-5L AND S-6L) TTG8Q00AY1KQ;[13] VERIFIED ALL ITEMS COMPLETED. REPAIRED PERFORMED PER 22-153-00527-WIP1 (N469WN - ATS(PAE) - REPAIR - BS 312 FRAME INNER CHORD BETWEEN S-5L AND S-6L) TTG8Q00AY1KQ

Part: NONE — CRACKED (R1 DOOR) · airframe 59,572 hrs · 35,384 cycles

CRACK AND EDGE DAMAGE ON FSD CUTOUT FWD FRAME ON FITTING FOR FSD UPPER HINGE CUTOUT; LOCATED AT BS 295 STR 10R (MARKED) / [01] REQUEST NDI FOR END OF CRACK;[09] LOCATED AND DRILLED NEW FSD UPPER HINGE BOX I.A.W SRM 51-40-05-0G-0 AND BOEING DWGS 141A8353;141A8350;141A6504 OK TO INSTALL.[14] INSTALLED 100% TEMPORARY AND PERMANENT FASTENER ON REPAIR AREA BEFORE SQUEEZE OUT TIME I.A.W SOPM 20-50-19;[15] VERIFIED CORRECTIVE ACTION #14;[16] OK TO INSTALL STUB FRAME.;[17] VERIFIED CORRECTIVE ACTION 16; OK TO INSTALL GIVEN.;[18] INSTALLED NEW UPPER HINGE BOX I.A.W SRM 51-40-02-0G-0 AND BOEING DWGS 141A8353;141A8350;141A6504;141A8370.;[19] INSTALLED UPPER HINGE PANEL 141A8359-2 BS294 STR 10 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8350;141A8370.;[20] INSTALLED UPPER STUB FRAME BS294 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8370;141A8350;141A8350;[21] INSTALLED SPLICE FRAME TO INTERCOSTAL BS294 STR 10 I.A.W SRM 51-40-02-0G-0 BOEING DWG 141A8370;141A8350;[22] VERIFIED RII CORRECTIVE ACTIONS 18;19;20 AND 21.;[23] INSTALLED FSD UPPER AND FWD CUTOUT LINER RETAINER I.A.W SRM 51-40-02-OG-0 AND AMM 25-21-35-420-801;[24] REMOVED AND REPLACED FSD UPPER HINGE BOX BS295 STR10 I.A.W. SRM 51-40-02-0G-0 AND BOEING DWGS 141A8353;141A8350;141A6504;141A8370;[25] VERIFIED CORRECTIVE ACTIONS 23 AND 24. RII BUYBACK ACCOMPLISHED ON CORRECTIVE ACTION 22.

Part: STRINGER — CRACKED · airframe 59,572 hrs · 35,384 cycles

STR 15L IS CRACKED AT BS 295.5 / REMOVED FASTENER ON STRINGER 15 L BTW B/S 277 TO B/S 303.9 IAW SRM 51-40-02;[04] UPDATE STEP #1 PARTIAL;[05] UPDATE STEP #2 PARTIAL;[06] UPDATE STEP #3 PARTIAL;[07] VERIFIED WORK;[08] VERIFIED CORRECTIVE ACTIONS 1-3;[09] REQUEST NDI TO VERIFY CRACK FREE CONDITION OF ALL OPEN HLOES AND COUNTERSINKS FOR CRACK FREE CONDITION OF STR 15L STA 277-303.9;[10] HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16; NO CRACKS NOTED. <BR>EQUIP USED: NORTEC 600 ID: ATS1465 EQUIP USED: MINIMITE ID: ATS240REMOVED DAMAGE SECTION OF STRINGER 15L AT BS 286 - BS 294.5 + 6 IAW SRM 53-00-03-2R-1 REPAIR 1;[13] REMOVED DAMAGED SECTION OF STRINGER 15L AT BS 286-294.5 +6 IAW SRM 51-10-0G-0.;[14] VERIFIED CORRECTIVE ACTION 13 ONLY FOR DAMAGE REMOVAL ON STRINGER 15L.] FABRICATED NEW STRINGER SECTION FROM BAC1498-161#7075T62-C; LOT#1313891-1 AND HAT SECTION FROM P/N 69-78188-16 IAW SRM 53-00-03-2R-1 REPAIR 1 TABLE 203;[18] APPLIED A CHEMICAL CONVERSION COATING TO ALL REPAIR PARTS AND BARE SURFACES IAW AMM 51-20-01-0G-0 AND SRM 53-00-03-2R-1 REPAIR 1 PARG 4.(I). APPLIED PRIMER TO ALL REPAIR PARTS AND BARE SURFACES IAW SOPM 20-41-02 AND SRM 53-00-03-2R-1 REPAIR 1 PARG 4.(J);[19] VERIFIED CORRECTIVE ACTION 17 AND 18;[20] OK TO INSTALL REPAIR PARTS AT STR 15 L/H BS 277-303.9;REMOVED DAMAGED SECTION OF STRINGER 15L AT BS 286-294.5 +6 IAW SRM 51-10-02-0G-0.;[25] ACCOMPLISHED REPAIR PER EA#: 22-153-00520.;

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

PANEL 193AR HAS DELAMINATION TO OUTER SURFACE 30' FROM I/B EDGE; 7' FROM FWD EDGE / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-40-70-0I-1 FIG 2 TABLE 2 ITEM 18. <BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PARA 4A(6). <BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-05-2R-1 PER SRM 53-40-70-2R-1 TABLE 201. <BR>REMOVED DELAMINATED PLIES APPROX.6.0'X14.5 IN DIAMETER AND CLEANED REPAIR AREA IAW SRM 51-70-05-2R-1 PARA 4A-B.;[02] VALIDATED APPLICABILITY OF SRM 51-70-05-2R-1.;[03] VERIFIED CORRECTIVE ACTIONS 1; 2.;[04] FABRICATED; INSTALLED REPAIR PLIES AND SET TO CURE; USING BMS 5-129 GR5 LOT# 1482238-1 AND BMS 8-79ST120 LOT# 1482266-2 WITH BONDER/NCX000523/11051262. IAW SRM 51-70-05-2R-1 PARA4.C-E.;[05] CURED REPAIR PLIES; UNBAGGED AND LIGHTLY SANDED IAW SRM 51-70-05-2R-1 PARA 4.E AND G. PERFORM POST CURE NDI IAW SRM 51-70-05-2R-6 PARA 4.F.;[06] PERFORM POST CURE NDI IAW SRM 51-70-05-2R-1 PARA 4.F.;[07] VERIFIED CORRECTIVE ACTION ITEMS 4 - 6.<BR><BR>UT INSPECTED REPAIR PER NDTM PART 4; 51-00-02. NO DISBONDS NOTED.<BR>CAL ID: ATS2341 S/N: 190848104;[08] APPLIED BMS10-21 TYPE III CONDUCTIVE COATING ;CURED THEN TESTED GOOD IAW AMM 51-21-71-370-801 PARA 3 D STEPS 1-4 & 7. REF CAL TOOL MULTIMETER ID ATS1658 SN 34000350.<BR>RESTORED THE FINISH USING BMS10-103 PRIMER & BMS10-60 ENAMEL IAW SRM 51-70-05-2R-1 PARA 4 STEP G.;[09] PANEL 193AR DELAMINATION ON THE OUTER SURFACE 30' FROM I/B EDGE 7' FROM THE FWD EDGE WAS REPAIRED IAW SRM 51-70-05-2R-1;[10] INSPECTION COMPLETE

Part: STRINGER CLIP — CRACKED (FWD FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

CRACKED STR CLIP STR 13L BS 294 / [01] REMOVED STR CLIP ON STR 13L BS 294 IAW SRM 51-40-02-0G-0.;[02] UPDATED MEASSUREMENTS.;[03] FABRICATED NEW STR CLIP; MADE FROM BAC1489-360 7075-T62; LOT# 1464682-1 IAW SRM 51-40-05-0G-0 AND DWG 141A1311;[04] APPLIED A CHEMICAL CONVERSION COATING TO NEW STR CLIP IAW SRM 51-20-01-0G-0 AND APPLIED PRIMER TO NEW STR CLIP IAW SOPM 20-41-02 AND DWG 141A1311;[05] VERIFIED CORRECTIVE ACTION 4; OK TO INSTALL;[06] INSTALLED STR CLIP STR 13L BS 294 IAW SRM 51-40-02-0G-0 AND DWG 141A1311;[07] VERIFIED CORRECTIVE ACTION 3;[08] VERIFIED CORRECTIVE ACTION 6

Part: ANGLE — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACKED LOWER ANGLE COMMON TO CABLE GUARD INTERCOSTAL STA 694; LBL 1; WL 204. / [01] REMOVED DAMAGED LOWER ANGLE COMMON TO CABLE GUARD INTERCOSTAL STA 694; LBL 1; WL 204 PER SRM 51-40-02-0G-0.;[02] REMOVED FWD VERTICAL ANGLE COMMON TO CABLE GUARD INTERCOSTAL STA 694; LBL 1; WL 204-208 FOR ACCESS PER SRM 51-40-02-0G-0.;[03] FABRICATED LOWER ANGLE; LOCATED HOLES; DRILLED; DEBURRED; AND APPLIED CHEMICAL CONVERSION COATING PO#812834 IAW SRM 51-40-05; AND BOEING DWG 273A9112. OK TO APPLY PRIMER.;[04] VERIFIED CORRECTIVE ACTION #3;[05] FABRICATED LOWER ANGLE; LOCATED HOLES; DRILLED; DEBURRED; AND APPLIED CHEMICAL CONVERSION COATING PO#812834 IAW SRM 51-40-05; AMM51-21-41-370-802; AND BOEING DWG 273A9112. OK TO APPLY PRIMER.;[06] APPLIED PRIMER LOWER ANGLE IAW AMM 51-21-72-370-809. OK TO INSTALL.;[07] VERIFIED CORRECTIVE ACTION #6;[08] INSTALLED LOWER ANGLE COMMON TO CABLE ON INTERCOSTAL STA 694; LBL 1; WL 204 IAW SRM 51-40-02/0G01 AND DWG 273A9112;[09] VERIFIED CORRECTIVE ACTION ITEM 8;[10] VERIFIED CORRECTIVE ACTION ITEM 8

Part: STRINGER CLIP — CRACKED (FWD FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

STR CLIP DENTED AND HAS SUSPECTED CRACK; STR 14L BS 344 / [01] UPON FURTHER INVESTIGATION FOUND DAMAGED STR CLIP TO BE AT BS 344; STR 14R.;[02] VERIFIED CORRECT LOCATION OF STRINGER CLIP TO BE AT BS344; S-14R;[03] WORK WILL BE ACCOMPLISHED ON JOB# TTG8Q00AWCDA;[04] VERIFIED WORK WILL BE ACCOMPLISHED ON JOB# TTG8Q00AWCDA

Part: INTERCOSTAL — CRACKED · airframe 59,572 hrs · 35,384 cycles

BS 294.5 -312 RBL20 WL208 INTERCOSTAL IS CRACK. / [01] NO ALLOWABLE LIMITS FOUND ON SRM FOR CRACK ON SPECIFIC INTERCOSTAL PART TO BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PAR.9.C;[02] REMOVED INTERCOSTAL BS294.5-312 RBL16 WL208-WL200 I.A.W SRM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW INTERCOSTAL BS294.5-312 RBL16 WL208-WL200 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 141A5400 OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION ITEMS 1 THROUGH 3. VERIFIED PART DRILLED PER SRM 51-40-05-0G-0 AND BOEING DWG 141A5400. OK TO INSTALL GIVEN.;[05] INSTALLED INTERCOSTAL ON BS 294.5-312 RBL20 WL 208 IAW SRM 51-40-05-0G-0 AND BOEING DWG 141A5400;[06] VERIFIED CORRECTIVE ACTION ITEM 5.;[07] VERIFIED CORRECTIVE ACTION ITEM 5

Part: FLOOR PANEL — DEBONDED (FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

FLOOR PANEL 242UF HAS SEVERAL DISBANDED DENTS TO UPPER SURFACE / [01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIG 6 TABLE 6 . <BR>NUMEROUS DENTS/DELAMINATION'S ON UPPER SURFACE PANEL 242UF EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-50-1A-1 PARA 4 F.<BR>REPAIRS TO BE ACCOMPLISHED IAW SRM 53-00-50-2R-1 AS GIVEN IN SRM 53-00-50-2R-0 .[15] FLOOR PANEL 242UF WITH SEVERAL DISBONDED DENTS TO UPPER SURFACE WERE REPAIRED IAW SRM 53-00-50-2R-1.;[16] VERIFIED CORRECTIVE ACTION 15;[17] VERIFIED CORRECTIVE ACTION 15

Part: ATTACH ANGLE — CRACKED · airframe 59,572 hrs · 35,384 cycles

VERTICAL ATTACH ANGLE IS CRACKED COMMON TO CABLE GUARD INTERCOSTAL STA 694; RBL 1; WL 204-208. / REMOVED DAMAGED ATTACH ANGLE COMMON TO CABLE GUARD INTERCOSTAL STA 694; RBL 1; WL 204-208 PER SRM 51-40-02-0G-0.;[04] DISPLACED CABLE GUARD INTERCOSTAL STA 694; BL0-RBL 24 WL 204-208 FOR ACCESS PER SRM 51-40-02-0G-0.;[05] DISPLACED CABLE GUARD INTERCOSTAL STA 694; BL0-LBL 24 WL 204-208 FOR ACCESS PER SRM 51-40-02-0G-0.;[06] FABRICATED LOWER ANGLE; LOCATED HOLES; DRILLED; DEBURRED; AND APPLIED CHEMICAL CONVERSION COATING PO#812834 IAW SRM 51-40-05; AND BOEING DWG 273A911. OK TO APPLY PRIMER.;[07] VERIFIED CORRECTIVE ACTION #3;[08] FABRICATED LOWER ANGLE; LOCATED HOLES; DRILLED; DEBURRED; AND APPLIED CHEMICAL CONVERSION COATING PO#812834 IAW SRM 51-40-05; AMM 51-21-41-370-802; AND BOEING DWG 273A911. OK TO APPLY PRIMER.;[09] FABRICATED VERTICAL ATTACH ANGLE; LOCATED HOLES; DRILLED; DEBURRED; AND APPLIED CHEMICAL CONVERSION COATING PO#812834 IAW SRM 51-40-05; AMM 51-21-41-370-802; AND BOEING DWG 273A911. OK TO APPLY PRIMER.;[10] APPLIED PRIMER VERTICAL ATTACH ANGLE IAW AMM 51-21-72-370-804. OK TO INSTALL.;[11] VERIFIED CORRECTIVE ACTION #10;[12] INSTALLED VERTICAL ATTACH ANGLE ON INTERCOSTAL STA 694 RBL 1 WL 204-208 IAW SRM 51-40-02/0G01 AND DWG 273A911

Part: CREASE BEAM — CORRODED (AFT FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON CREASEBEAM WEB STA 707-714; RBL 65; WL 208 ON UNDERSIDE OF WEB COMMON TO INNER CHORD. / [01] UPDATED TABLE;[02] REMOVED CORROSION ON CREASEBEAM WEB STA 707-714; RBL 65; WL 208 ON UNDERSIDE OF WEB COMMON TO INNER CHORD PER SRM 51-10-02-0G-0. MAX MATERIAL REMOVED WAS .029' 1' BY 5'; FROM .045'. OUT OF LIMITS PER SRM 53-40-13-1A-1; 53-40-13-01-1; MEASURED DEPTH WITH 0-1 MICROMETER SPHERICAL; ID# IS000459; S/N# 67127987; EXPIRES 01/2023.;[03] REMOVED DAMAGED CREASEBEAM WEB STA 706-716; RBL 65-RBL 70; WL 208 PER SRM 51-40-02-0G-0.;[04] REMOVED 2 EA STIFFENERS COMMON TO CREASEBEAM WEB AT STA 708; 714; RBL 65-70; WL 208 PER SRM 51-40-02-0G-0.;[05] VERIFIED CORRECTIVE ACTION #2;[06] RECIEVED FABRICATED AND HEAT TREATED CREASEBEAM WEB FROM O.S.S. PER CUSTOMER CARD# 856303-SWA;[07] VERIFIED CORRECTIVE ACTION 6.;[08] LOCATED AND DRILLED AND DEBURRED NEW CREASEBEAM WEB; STA 706-716; RBL 65-RBL 70; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG# 144A5900; REV C; DWG#144A5920; REV E.;[09] APPLIED CHEMICAL CONVERSION COATING ON CREASEBEAM WEB STA 706-716; RBL 65-RBL 70; WL 208 PER SRM 51-20-01-0G-0; SOPM 20-43-03. OK TO PRIME.;[10] VERIFIED CORRECTIVE ACTIONS 8 AND 9.;[11] PRIMED NEW CREASEBEAM WEB; STA 706-716; RBL 65-RBL 70; WL 208 PER SRM 51-20-01-0G-0. OK TO INSTALL.;[12] VERIFIED CORRECTIVE ACTION 11.;[13] INSTALLED NEW CREASEBEAM WEB BS 706-716; RBL 65-70; WL 208 PER SRM 51-40-02-0G-0 AND BOEING DWG 144A5900.;

Part: SUPPORT — MISSING (FWD CARGO BAY) · airframe 59,572 hrs · 35,384 cycles

FORWARD CARGO BAY AFT BULKHEAD SUPPORT CLIP BS 500D STRINGER 24 R/H IS MISSING / [01] LOCATED AND DRILLED NEW SUPPORT CLIP AT BS 500D STR 24R PER SRM 51-40-05-0G-0 AND DWG 143A7902. OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED OK TO INSTALL.;[03] INSTALLED NEW SUPPORT CLIP AT BS 500D STR 24R PER SRM 51-40-02-0G-0; AND DWG 143A7902.;[04] VERIFIED CORRECTIVE ACTION STEP 3.;[05] COMPLETE

Part: ATTACH ANGLE — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACKED ATTACH ANGLE COMMON CABLE GUARD INTERCOSTAL STA 694; RBL 24; WL 204. / [01] UPDATED TABLE;[02] REMOVED DAMAGED ATTACH ANGLE COMMON TO CABLE GUARD INTERCOSTAL STA 694; RBL 24; WL 204 PER SRM 51-40-02-0G-0.;[03] FABRICATED LOWER ANGLE; LOCATED HOLES; DRILLED; DEBURRED; AND APPLIED CHEMICAL CONVERSION COATING PO#812834 IAW SRM 51-40-05; AND BOEING DWG 273A9110. OK TO APPLY PRIMER.;[04] VERIFIED CORRECTIVE ACTION #3;[05] FABRICATED LOWER ANGLE; LOCATED HOLES; DRILLED; DEBURRED; AND APPLIED CHEMICAL CONVERSION COATING PO#812834 IAW SRM 51-40-05; AND BOEING DWG 273A9110 AMM 51-21-41-370-802. OK TO APPLY PRIMER.;[06] APPLIED PRIMER LOWER ANGLE IAW AMM 51-21-370-809. OK TO INSTALL.;[07] VERIFIED CORRECTIVE ACTION #6;[08] INSTALLED ATTACH ANGLE COMMON CABLE GUARD ON INTERCOSTAL STA 694; RBL; WL 204 IAW SRM 51-40-02/0G01 AND DWG 273A9112;[09] VERIFIED CORRECTIVE ACTION ITEM 8;[10] VERIFIED CORRECTIVE ACTION ITEM 8

Part: FLOORBEAM — CRACKED (FWD FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

328 FLOORBEAM IS CRACKED ON UPPER CHORD COMMON TO FWD FASTENER HOLE; RBL 21; WL 208. / [01] UPDATED TABLE;[12] FABRICATED REPAIR PARTS ITEM 1 T-CHORD(1EA) FROM BAC1505-100224 7050-T76511 LOT #5070057-1;ITEM 2 ANGLE(2EA)FROM BAC1490-2811 7075T62 LOT #1453731-1;ITEM 3 ANGLE(2EA)FROM BAC1490-2900 7075T62 LOT # 5072759-4;ITEM 4 SHIM(9EA)FROM 2024T3 .100'B LOT#1437054-1;ITEM 5 ANGLE(1EA)FROM BAC1490-2651 7075-T6 LOT#1376388-2 AND ITEM 6 FILLER (3EA)FROM 7075T6 0.020 LOT#1472548-1 ALL I.A.W SRM 53-10-51-2R-7 REPAIR 7 PAR 4.H-M;[13] FABRICATED REPAIR PARTS ITEM 4 SHIM (1EA)FROM 7075T6 C. 0.071'LOT #1459410-1;PART ITEM 4 SHIM(1EA)FROM 7075T6 C. 0.080'LOT # 1379745-2 ALL I.A.W SRM 53-10-51-2R-7 REPAIR 7 PAR 4.H-M;[20] INSTALLED REPAIR PARTS ITEM 1 T-CHORD(1EA) ;ITEM 2 ANGLE(2EA);ITEM 3 ANGLE(2EA);ITEM 4 SHIM(11EA);ITEM 5 ANGLE(1EA);ITEM 6 FILLER (3EA);STIFFENERS BS328 BL0(1EA);RBL8(1EA);RBL15(1EA);RBL23(1EA);RBL34(1EA);RBL45(1EA) RBL55 AND INTERCOSTAL BS328-BS344 RBL25 WL208-WL200 ALL I.A.W SRM 53-10-51-2R-7 REPAIR 7 PAR 4.O-S;[21] INSTALLED FLOOR SUPPORTS BS312-BS328 RBL11;RBL34 WL208 AND FASTENER ON AND ADJACENT TO THE REPAIR I.A.W SRM 53-10-51-2R-7 REPAIR 7 PAR 4.S AND SRM 51-40-02-0G-0 COMPLETED ALL REPAIR PROCESS I.A.W SRM 53-10-51-2R-7 REPAIR 7 ALTERNATIVE 2;

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 59,572 hrs · 35,384 cycles

FWD PASSENGER CABIN FLOOR PANEL 221BF HAS A DELAMINATED PREVIOUS REPAIR ON THE UPPER SKIN AFT AREA / FOUND THREE ADDITIONAL DAMAGE AREAS: THE FIRST IS LOCATED ON THE INBOARD EDGE; 8' FROM THE AFT EDGE; THE SECOND IS LOCATED ON THE INBOARD EDGE; 13' FROM THE AFT EDGE AND THE THIRD IS LOCATED ON THE OUTBOARD EDGE STARTING 2.5' FROM THE FORWARD EDGE AND RUNS 19.5' TOWERED THE AFT EDGE. ALL DAMAGE AREAS; INCLUDING THE ORIGINAL WRITE-UP; ON THE FLOOR PANEL ARE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F AND WILL BE REPAIRED IAW SRM 53-00-50-2R-1. REMOVED AN APPROXIMATE 16.5'X3' AREA OF DISBONDED PREVIOUS REPAIR PLIES LOCATED ON THE AFT EDGE OF THE PANEL; ALSO REMOVED A 19.5'X1' AREA OF DAMAGED TOOLSIDE PLIES LOCATED ALONG THE OUTBOARD EDGE; AN APPROXIMATE 5.6'X4' AREA OF DISBONDED TOOLSIDE PLIES LOCATED ON THE INBOARD EDGE; 8' FROM THE AFT EDGE. AND AN APPROXIMATE 2'X.25' AREA OF DISBONDED TOOLSIDE PLIES LOCATED ON THE INBOARD EDGE; 13' FROM THE AFT EDGE REMOVED REMAINDER OF PREVIOUS REPAIR INCLUDING UNIDENTIFIED CORE; IAW SRM 53-00-50-2R-0 PARA 5.B; AND FOUND NEW REPAIR DIMENSION TO BE BEYOND THE SCOPE OF SRM 53-00-50-2R-1 AS WELL AS ALL OTHER SPECIFIC REPAIRS APPLICABLE TO THIS FLOORBOARD.;[04] ROBBED AIRWORTHY PANEL 221BF FROM A/C N465WN ON FAULT TTG8Q00AWE84 SINCE THE ORIGINAL PANEL WAS NOT REPAIRABLE PER SRM 53-00-50-2R-6 BECAUSE DAMAGE WAS GREATER THAN 10 SQUARE INCHES

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 59,572 hrs · 35,384 cycles

AFT PASSENGER CABIN FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS. / [01] IDENTIFIED FLOOR PANEL 242UF IAW SRM 53-00-50-0I-1 FIG6. TABLE6. FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS IAW SRM53-00-50-1A-1 PARA4.F. DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1. FABRICATED REPAIR PLIES OUT OF BMS 9-3 TYPE H-2 LOT#1475360-2; IAW SRM 53-00-50-2R-1 PARA3. K.1.(A) OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 4. OKAY TO INSTALL PLIES;[06] INSTALLED REPAIR PLIES WITH BMS 8-201 TY4 LOT# 1464982-6; VACUUM BAGGED; LEAK CHECKED GOOD USING GAUGE ATS2241; S/N UNKOWN AND SCALE ATS2275 S/N P1662216 IAW SRM 53-00-50-2R-1 PARA 3.K.1-L.1;[07] VERIFIED CORRECTIVE ACTION 6;[08] REPAIR PLIES CURED IAW SRM 53-00-50-2R-1 PARA 3 STEP M (1) (B) . REF CAL TOOL THERMOMETER ID ATS1777 SN 34910028WS . CAL TOOL VACUUM GAUGE ID ATS2845 SN 542505520 .;[09] VERIFIED CORRECTIVE ACTION #8;[10] INSTALLED ALL PREVIOUSLY REMOVED INSERTS USING BMS 5-28TY19 LOT#AK1KP5960K AND BMS 5-107 LOT#AK0DP4051K IAW SRM 53-00-50-2R-1 PARA 3N AND BOEING DWG 147A5810-95.<BR>INSERTS NEED CURE;[11] CURED ALL INSERTS THAT WERE PREVIOUSLY INSTALLED ON STEP 10 USING THERMOMETER ID: ID ATS1777 SN 34910028WS IAW SRM 53-00-50-2R-1 PARAGRAPH 3.N.;[12] ADDING REFERENCE TO ITEM 10: 'BOEING DWG 147A5810 ID:0095';[13] VERIFIED CORRECTIVE ACTIONS 10-12;[14] AFT CABIN PASSENGER FLOOR PANEL 242UF UPPER SKIN WITH AREAS OF PULLED STRANDS WERE REPAIRED IAW SRM 53-00-50-2R-1

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 59,572 hrs · 35,384 cycles

AFT PASSENGER CABIN FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS. / [01] IDENTIFIED PART AND MATERIAL ID PER SRM 53-00-50-0I-1 FIG.6; SHT.1; AN TABLE 6. FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS PER SRM 53-00-50-1A-1 PAR.4B STEP 2. A REPAIR WILL BE ACCOMPLISHED PER SRM 53-00-50-2R-1.<BR><BR>REMOVED DAMAGED SKIN WITH NO CONTAMINATION NOTED PER SRM 53-00-50-2R-1 PAR.3 STEPS A-C AND E & F.;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2;[04] FABRICATED REPAIR PLIES WITH FIBER GLASS CLOTH BMS 9-3 TYPE H2 STYLE 1581 LOT#1475360-2 PER SRM 53-00-50-2R-1 PAR.3K(1)(A). OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION 4. OKAY TO INSTALL PLIES;[06] INSTALLED PLIES WITH BMS 8-201 LOT# 1478412-1; VACUUM BAGGED AND VERIFIED 5X5 USING VACUUM GAUGE ID: ATS2483 S/N: UNKNOWN IAW SRM 53-00-50-2R-1 PAR.3.K.(1).(B-C) AND L.(1).;[07] VERIFIED CORRECTIVE ACTION 6;[08] SET PLIES TO CURE UNDER HEAT LAMP USING THERMOMETER ID: ATS1777 S/N: 34910028WS; CURED PLIES AND UNBAGGED PLIES IAW SRM 53-00-50-2R-1 PARA 3.M.(1).;[09] JOB COMPLETE.;[10] VERIFIED CORRECTIVE ACTIONS 8 AND 9;[11] VERIFIED CORRECTIVE ACTIONS 8 AND 9

Part: NONE — CORRODED (AFT FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON 986 FLOORBEAM UPPER CHORD AT LBL 44 AND AT RBL 44; WL 208. / [01] VERIFY APPLICABILITY PER SRM 53-70-51-1A-1; NSTALLED L/H BS986 RBL1-LBL55 T-CHORD REPAIR I.A.W SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 2 PAR.4.N-O.;INSTALLED R/H BS986 RBL22-RBL55 T-CHORD REPAIR I.A.W SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 2 PAR.4.N-O.; INSTALLED REPAIR ON L/H FLANGE RBL1-LBL55 AND R/H FLANGE RBL22-RBL55 OF THE UPPER CHORD BS986 WL208 I.A.W 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 2 PAR 1- 4.S

Part: SUPPORT — CORRODED (AFT FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON FLOOR SUPPORT STA 986-1006; LBL 8-LBL 17; WL 208. / [01] NO ALLOWABLE LIMITS FOUND ON SRM FOR FLOOR SUPPORT BS986-1006 LBL8-LBL17 WL208 PART TO BE REMOVED AND REPLACED I.A.W.SRM 51-10-02-0G-0 PAR 9.C;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED FLOOR SUPPORT BS986-1006 LBL8-LBL17 WL208 I.A.W SRM 51-40-02-0G-0;[04] UPDATED P/N;[05] LOCATED AND DRILLED NEW FLOOR SUPPORT BS986-1006 LBL8-LBL17 WL208 IAW SRM 51-40-05-0G-0 AND DWG 145A5600;[06] VERIFIED CORRECTIVE ACTION ENTRY 5. OK TO INSTALL GIVEN.;[07] REQUEST OK TO INSTALL DUE TO PERMISSION GIVEN ON CORRECTIVE ACTION 6 IS EXPIRED.;[08] VERIFIED CORRECTIVE ACTION 7; OK TO INSTALL;[09] LOCATED AND DRILLED NEW FLOOR SUPPORT BS986-1006 LBL8-LBL17 WL208 IAW SRM 51-40-05-0G-0 AND DWG 147A5600;[10] CORRECTION FOR STEP 5 ; DWG SHOULD READ 147A5600. & LOCATED AND DRILLED NEW FLOOR SUPPORT BS986-1006 LBL8-LBL17 WL208 IAW SRM 51-40-05-0G-0 AND DWG 147A5600;[11] INSTALLED NEW FLOOR SUPPORT BS986-1006 LBL8-LBL17 WL208 IAW SRM 51-40-05-0G-0 AND DWG 147A5600;[12] VERIFIED CORRECTIVE ACTION 9-11;[13] VERIFIED CARD COMPLETE;[14] UPDATED MEASUREMENT TABLE.;[15] CERTIFIED UPDATE OF MEASUREMENT TABLE.;[16] EDITED N/A REASONS AND CORROSION LEVEL ON MEASUREMENT TABLE.;[17] CERTIFIED EDIT.

Part: STRAP — CORRODED (AFT FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON AFT SHEARWEB STRAP STA 1016-1018; RBL 3; WL 208. / [01] NO ALLOWABLE LIMITS FOUND ON SRM FOR SHEAR WEB STRAP BS1016-1018 RBL3 WL208 PART TO BE REMOVED AND REPLACED I.A.W.SRM 51-10-02-0G-0 PAR 9.C;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED SHEAR WEB STRAP BS1016-1018 RBL3 WL208 I.A.W SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW AFT SHEAR WEB STRAP BS1016-1018 RBL3 WL208 IAW SRM 51-40-05-0G-0 AND DWG 147A5730;[05] VERIFIED CORRECTIVE ACTION ENTRY 4. OK TO INSTALL GIVEN.;[06] OK TO INSTALL;[07] VERIFIED OK TO INSTALL;[08] INSTALLED NEW SHEAR WEB STRAP BS1006-1028 LBL3 WL208 IAW SRM 51-40-02-0G-0 AND DWG 147A5730;[09] VERIFIED CORRECTIVE ACTION STEP 8.;[10] COMPLETE;[11] UPDATED MEASUREMENT 15.;[12] CERTIFIED EDIT OF MEASUREMENT TABLE.

Part: FLOOR PANEL — CRACKED (CABIN FLOOR) · airframe 59,572 hrs · 35,384 cycles

AFT PASSENGER CABIN FLOOR PANEL 242XF UPPER SKIN IS CRACKED. / [01] AFT PASSENGER CABIN FLOOR PANEL 242XF WITH UPPER SKIN CRACK WAS REPLACED DUE TO THE EXTENT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A.(1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: STRAP — CORRODED (AFT FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON SHEARWEB STRAP STA 1006-1028; LBL 3-LBL 8; WL 208. / [01] NO ALLOWABLE LIMITS FOUND ON SRM FOR SHEAR WEB STRAP BS1006-1028 LBL3-LBL8 WL208 PART TO BE REMOVED AND REPLACED I.A.W.SRM 51-10-02-0G-0 PAR 9.C;[02] VERIFIED CORRECTIVE ACTION STEP 1;[03] REMOVED SHEAR WEB STRAP BS1006-1028 LBL3-LBL8 WL208 I.A.W SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW SHEAR WEB STRAP BS1006-1028 LBL3-LBL8 WL208 IAW SRM 51-40-05-0G-0 AND DWG 147A5600;[05] VERIFIED CORRECTIVE ACTION ENTRY 4. OK TO INSTALL GIVEN.;[06] OK TO INSTALL SHEAR WEB STRAP;[07] VERIFIED OK TO INSTALL SHEAR WEB STRAP.;[08] OK TO INSTALL;[09] INSTALLED NEW SHEAR WEB STRAP BS1006-1028 LBL3-LBL8 WL208 IAW SRM 51-40-02-0G-0 AND DWG 147A5600;[10] VERIFIED ALL STEPS;[11] COMPLETE;[12] UPDATED MEASUREMENT 15.;[13] CERTIFIED EDIT OF MEASUREMENT TABLE.;[14] EDITED N/A REASONS AND CORROSION LEVEL ON MEASURMENT TABLE.;[15] CERTIFIED EDIT.

Part: NONE — CORRODED (R2 DOOR) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON AFT SERVICE MOPSILL STA 953-992.8; RBL 45-54; WL 208. / [01] VERIFY APPLICABILITY PER SRM 53-70-15-1A-1 ALLOWABLE DAMAGE 1;[02] REMOVED CORROSION ON ASD MOPSILL 40'X 2' BS953-BS993 RBL45-RBL54 WL 208 ORIGINAL MATERIAL THICKNESS IS 0.080 LOWEST MATERIAL THICKNESS IS 0.065 ALL I.A.W SRM 53-70-15-1A-1 ALLOWABLE DAMAGE 1 PAR 4.D(2)(A) FIG103 DETAIL D;E;[03] DIAL DEPTH GAGE USED<BR>ID NCX000697<BR>S/N UNKNOWN;[04] PART TO BE OUT LIMITS AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.A(1);[05] OUT LIMIT STATEMENT ADDED;[06] VERIFIED CORRECTIVE ACTION STEPS 1;2;3 AND 4;;[07] REMOVED ASD MOPSILL I.A.W SRM 51-40-02-0G-0;[08] LOCATED AND DRILLED NEW MOPSILL AFT SERVICE DOOR IAW SRM 51-40-05-0G-0 AND DWG 147A8701. OK TO INSTALL.;[09] VERIFIED CORRECTIVE ACTION 8. <BR><BR>OK TO INSTALL;[10] INSTALLED 100% TEMPORARY AND PERMANENT FASTENERS ON NEW MOPSILL AFT SERVICE DOOR BEFORE SQUEZEE OUT TIME EXPIRE;BMS5-95 C-20 USED AT 16-FEB-2022- UTC 23:50 IAW SOPM 20-50-19; SRM 51-40-02-0G-0 AND DWG 147A8501.;[11] CORRECTION ON DWG# 147A8501 STEP 8 MISTAKE ENTERED 147A8701.;[12] INSTALLED NEW AFT SERVICE MOPSILL I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A8501.;[13] VERIFIED CORRECTIVE ACTION 10-12;[14] VERIFIED CARD COMPLETE;[15] UPDATED OF MEASUREMENT TABLE.;[16] CERTIFIED UPDATE OF MEASUREMENT TABLE.

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 59,572 hrs · 35,384 cycles

FWD PASSENGER CABIN FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS. / [01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 221DF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-50D ITEM 158.;[02] VERIFIED CORRECTIVE ACTION 1

Part: STRINGER — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACK ON STRINGER TIE STA 277; AT STR 9R; RBL 46; WL 261; FWD SIDE OF FRAME. / [01] REMOVED DAMAGED STRINGER TIE STA 277; AT STR 9R; RBL 46; WL 261 ON FWD SIDE OF FRAME PER SRM 51-40-02-0G-0.;[02] HFEC INSPECTED DAMAGED STRINGER TIE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP USED: NORTEC 600 ID: ATS1465;[03] UPON FURTHER INVESTIGATION FOUND STRINGER TIE STA 277 AT STR 9R; RBL 46; WL 261; FWD SIDE OF FRAME TO BE CRACK FREE ON STEP 2. OK TO REINSTALL STRINGER TIE.;[04] VERIFIED CORRECTIVE ACTION #3;[05] INSTALLED STR TIE AT STR 9 RH RBL 46 WL 261 FWD SIDE OF FRAME IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A1110 APPLIED CPC IAW AMM 51-21-91-620-802;[06] VERIFIED CORRECTIVE ACTION 5. PART REINSTALLED.;[07] VERIFIED ALL WORK ACCOMPLISHED.

Part: NONE — CRACKED (FWD FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

CRACK ON 294 FLOORBEAM UPPER CHORD RBL 52; WL 208 COMMON TO FSD MOPSILL. / [01] NO ALLOWABLE LIMIT FOR CRACK ON SPECIFIC LOCATION DAMAGE TO BE REMOVED AND REPAIRED I.A.W SRM 51-10-02-0G-0 AND SRM 53-10-51-2R-16 REPAIR 1609] HFEC INSPECTED CUT EDGE AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED<BR>DURING TIME OF INSPECTION. EQUIP ID#:ATS2353 S/N:60005195684.<BR><BR>HFEC INSPECTED OPEN HOLES IN THE REPAIR AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16; NO CRACKS NOTED DURING TIME OF INSPECTION. <BR>EQUIP ID#: ATS2353 S/N:60005195684 EQUIP ID#: ATS1411 S/N:MM12030Z012384<BR><BR>PART 4.C(3): N/A;[12] FABRICATED REPAIR PARTS<BR>ITEM 1 REPAIR CHORD(1EA)FROM BAC1503-101052 7050 LOT#1426405-1.<BR>ITEM 2 ANGLE (2EA)FROM 7075-T0 LOT #1462657-1 HT ON COSTUMER RO NO 855848-SWA.<BR>ITEM 3 STRAP(1EA) <BR>ITEM 4 TAPERED FILLER (2EA)<BR>ITEM 5 TAPERED FILLER(2EA) FROM 7075-T6 0.071 C LOT #1459410-1<BR>ITEM 7;8 SHIM(1EA) FROM 7075T6 0.032 C LOT # 1457911-2 ALL I.AW SRM 53-10-51-2R-16 REPAIR 16 ALTERNATIVE 2 PAR.4.D-I.;19] INSTALLED REPAIR PARTS ITEM 1-8 IAW SRM 53-10-51-2R-16 REPAIR 16 ALTERNATIVE 2 PAR.4.L-O AND EA NO 22-153-00426 REV A ATTACHED ON TTG8Q00ASQ09;[21] 'FLOOR BEAM UPPER CHORD SPLICED AT RBL 23 TO RHS OUTBD END PER 737-700 SRM 53-10-51-2R-16 (REPAIR 16) WITH DEVIATIONS PER EA 22-153-00426.';

Part: FLOOR PANEL — DAMAGED (CABIN FLOOR) · airframe 59,572 hrs · 35,384 cycles

FWD PASSENGER CABIN FLOOR PANEL 221BF HAS DAMAGED INSERTS. / [01] IDENTIFIED PANEL 221BF IAW SRM 53-00-50-0I-1 FIG 2; TABLE 2. <BR><BR>CLEANED PANEL IAW SRM 53-00-50-2R-0 PARA 5. A. (1). <BR><BR>REMOVED (1) EACH CORRODED BLIND INSERTS AND (19) EACH CORRODED THROUGH INSERTS AROUND THE PERIPHERY OF PANEL IAW SRM 53-00-50-2R-0 PARA 5. B (2).;[02] REMOVED AN ADDITIONAL 6 INSERTS IAW SRM 53-00-50-2R-0 PARA 4.B.(2).;[03] THIS FLOOR PANEL WAS REPLACED WITH A SERVICEABLE FLOOR PANEL (141A5810-56) ON FAULT TTG8Q00AQBXM.;[04] ADDITIONAL INFO; ROBBED AIRWORTHY PANEL 221BF FROM A/C N465WN ON FAULT TTG8Q00AWE84 SINCE THE ORIGINAL PANEL(TTG8Q00AQBXM) WAS NOT REPAIRABLE PER SRM 53-00-50-2R-6 BECAUSE DAMAGE WAS GREATER THAN 10 SQUARE INCHES.;[05] PART REPLACED WITH SERVICEABLE ROBBED PART FROM A/C 469

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 59,572 hrs · 35,384 cycles

FWD PASSENGER CABIN FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS. / [01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 222BF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-50D ITEM 96.;[02] VERIFIED CORRECTIVE ACTION 1

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 59,572 hrs · 35,384 cycles

PASSENGER CABIN FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F.<BR>DUE TO THE EXTENT OF DAMAGE CUT NEW FLOOR PANEL FROM BMS 4-23TY2 LOT#1479169-1 IAW SRM 53-00-50-2R-0 PARA 1A(NOTE) AND BOEING DWG 144A5810-127.;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-0.;[03] INSTALLED THROUGH INSERTS USING BMS5-107 CLASS 1 LOT#AK0DP4051K. SET TO CURE USING HEAT LAMP AND THERMOMETER ID:ATS2208 S/N:43300740WS. COMPLETED SUCCESSFUL CURE; AND INSTALLED SEALANT TAPE BMS8-283TY1 LOT#0CN050418. IAW BOEING DWG 144A5810-127; AND BAC5085 FIGURE 15 PAR.8.4.2.2 (A-H);[04] ADDITION TO LINE 3: ADDED PART MARK TO PANEL 241AF;[05] VALIDATED LINE 4;[06] ADDITION TO LINE 4: ADDING PART MARK REFERENCE IAW BOEING DWG 144A5810-127; AND BOEING DWG 140A1008;[07] VERIFIED CORRECTIVE ACTIONS 1-6

Part: INTERCOSTAL — CORRODED · airframe 59,572 hrs · 35,384 cycles

CORROSION ON INTERCOSTAL UPPER SURFACE STA 294-312; LBL 10; WL 208. / [01] UPDATE MEASUREMENTS;[02] REMOVED INBTERCOSTAL ON UPPER SURFACE STA 294-312; LBL 10; WL 208 IAW. SRM 51-40-02-0G-0 ITEM 7.D;[03] DISPLACED INTERCOSTAL BETWEEN BS 294-312; BL0 WL 208 IAW SRM 51-40-02.;[04] LOCATED AND DRILLED NEW INTERCOSTAL P/N 141A5690U1 STA 294-312; LBL 10; WL 208 IAW SRM 51-40-05-0G-0 AND DWG 141A5600;141A5600. OK TO INSTALL.;[05] NO ALLOWABLE LIMIT FOUND FOR CORROSION ON SRM FOR INTERCOSTAL ON UPPER SURFACE STA 294-312; LBL 10; WL 208 IAW.PART TO BE REMOVE AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR.9.C;[06] VERIFIED CORRECTIVE ACTION ITEMS 1 THROUGH 5. VERIFIED NO ALLOWABLE LIMIT FOUND FOR CORROSION IN SRM FOR INTERCOSTAL ON UPPER SURFACE STA 294-312; LBL 10; WL 208 PART TO BE REPAIRED BY REPLACEMENT I.A.W SRM 51-10-02-0G-0 PAR.9.C. VERIFIED NEW INTERCOSTAL P/N 141A5690U1 STA 294-312; LBL 10; WL 208 DRILLED IAW SRM 51-40-05-0G-0 AND DWG 141A5600;141A5600. OK TO INSTALL GIVEN.;[07] INSTALLED INSTERCOSTAL ON STA 294-312; LBL 10; WL 208 AND REINSTALLED INTERCOSTAL BETWEEN BS 294-312; BL0 WL 208 IAW SRM 51-40-05-0G-0 AND DWG 141A5600;[08] VERIFIED CORRECTIVE ACTION ITEM 7.;[09] JOB TASK IS ACCOMPLISHED.;[10] MAINTENIX IS NOT ALLOWING TO UNCHECKED P/N 141A5410Y8 INTERCOSTAL BECAUSE WE HAVE INSTALLED INTERCOSTAL P/N 141A5690U1. ALSO; SEE STEP 4 AND 7. JOB TASK IS ACCOMPLISHED.;[11] VERIFIED ALL WORK COMPLETE.;[12] EDITED MEASUREMENT TABLE;[13] CERTIFIED EDIT.

Part: ATTACH ANGLE — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACKED INTERCOSTAL ATTACH ANGLE STA 380-400; RBL 41; WL 208. / [01] REMOVED DAMAGED INTERCOSTAL ATTACH ANGLE STA 380-400; RBL 41; WL 208 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL ATTACH ANGLE STA 380-400; RBL 41; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG#143A5400; REV A. OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTION 2.;[04] INSTALLED NEW INTERCOSTAL ATTACH ANGLE STA 380-400; RBL 41; WL 208 PER SRM 51-40-02-0G-0; DWG# 143A5400; REV A. JOB IS COMPLETE.;[05] VERIFIED CORRECTIVE ACTION 4.

Part: SHIELD — CORRODED (FWD CARGO) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON FORWARD CARGO BAY SHIELD AT B.S. 420+16; R.B.L. 24. / [01] EVALUATED CORROSION ON SHIELD BS 420+16 RBL 24 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] LOCATED; DRILLED; INSTALLED NUTPLATES ON NEW FCB SHIELD BS420-440; RBL 24 PER DWG143A0080; SRM 51-40-05-0G-0; AND SRM 51-40-02-0G-0;[04] ADDED PARTS;[05] VERIFIED CORRECTIVE ACTION ENTRY 3. CARD COMPLETE.

Part: SUPPORT — CORRODED · airframe 59,572 hrs · 35,384 cycles

CORROSION ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 500A+2; 500A+6; 500A+10; 500A+14; 500B+10 AND 500C+10; R.B.L. 25. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500A+6 RBL 25 WL 156 FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2473;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] LOCATED AND DRILLED NEW FCB FLOOR TO SIDEWALL SUPPORT BS500A-500D; RBL 25 PER DWG143A7500; AND SRM 51-40-05-0G-0;[04] VERIFIED CORRECTIVE ACTION ENTRY 3. CARD COMPLETE.

Part: NONE — CORRODED (R1 DOOR) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON FWD SERVICE MOPSILL STA 296; RBL 55-56; STA 304; RBL 56-57; STA 323-335; RBL 57-58; WL 208. / [01] VERIFY APPLICABILITY PER SRM 53-10-15-1A-2;[02] REMOVED CORROSION ON FSD MOPSILL BS328 RBL 57 WL 208 ORIG.MATERIAL THICKNESS 0.080 LOWEST REMAINING MATERIAL 0.066 CORROSION FOUND TO BE OUT LIMITS ALL I.A.W SRM 53-10-15-1A-2 PAR 4.E (2)(A)DETAIL D;G PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.A(1);[03] VERIFIED CORRECTIVE ACION 1 AND 2;[04] REMOVED FSD MOPSILL I.A.W SRM 51-40-02-0G-0;[05] LOCATED AND DRILLED NEW FWD SERVICE MOPSILL STA 262 - BS 359 RBL 55 - RBL 58 WL 208 IAW SRM 51-40-05-0G-0; SRM 51-40-08-0G-0 AND DWG 141A8310. OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION #5;[07] OK TO INSTAL LGIVEN;[08] INSTALLED 100% TEMPORARY AND PERMANENT FASTENERS(BEFORE SQUEZEE OUT TIME EXPIRE BMS 5-95 C-20 USED AT 14 FEB 2022 22:00 UTC)NEW FWD SERVICE MOPSILL STA 262 - BS 359 RBL 55 - RBL 58 WL 208 IAW SRM 51-40-02-0G-0; DWG 141A8310;141A0631 AND SOPM 20-50-19.;[09] VERIFIED CORRECTIVE ACTIONS STEP 8.;[10] INSTALLED NEW FWD SERVICE DOOR MOPSILL IAW SRM 51-40-02-0G-0; DWG 141A8310;141A0631;[11] VERIFIED CORRECTIVE ACTION 10;[12] UPDATED MEASUREMENT 15.;[13] CERTIFIED EDIT OF MEAUSUREMENT TABLE.

Part: INTERCOSTAL — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACKED INTERCOSTAL STA 344-360; LBL 11; WL 208. / [01] REMOVED DAMAGED INTERCOSTAL STA 344-360; LBL 11; WL 200-208 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL STA 344-360; LBL 11; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG#141A5400; REV B. OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION 1 AND 2;[04] INSTALLED NEW INTERCOSTAL STA 344-360; LBL 11; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-03-0G-0; DWG#141A5400; REV B;;[05] VERIFIED CORRECTIVE ACTION #4;[06] VERIFIED TASK COMPLETE

Part: ATTACH ANGLE — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACKED INTERCOSTAL ATTACH ANGLE STA 500D-520; BL0; WL 208. / [01] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT BS 500D-520 BL0 WL208 IAW SRM 51-40-05; SRM 51-40-02 BOEING DWG 143A5400;[02] VERIFIED CORRECTIVE ACTION 1. PART REPLACED.;[03] VERIFIED ALL WORK ACCOMPLISHED.

Part: INTERCOSTAL — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACKED INTERCOSTAL ATTACH ANGAL STA 380-400; RBL 9; WL 208. / [01] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT BS 380-400 RBL9 WL208 IAW SRM 51-40-05;SRM 51-40-02 BOEING DWG 143A5400;[02] VERIFIED CORRECTIVE ACTION 1. PART REPLACED.;[03] VERIFIED ALL WORK ACCOMPLISHED.

Part: INTERCOSTAL — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACKED INTERCOSTAL STA 344-360; RBL 32; WL 208. / [01] UPDATED TABLE;[02] REMOVED DAMAGED INTERCOSTAL STA 344-360; RBL 32; WL 208 PER SRM 51-40-02-0G-0.;[03] LOCATED AND DRILLED NEW INTERCOSTAL STA 344-360; RBL 32; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG#141A5400. OK TO INSTALL.;[04] VERIFIED CORRECTIVE ACTION 1 AND 2;[05] VERIFIED CORRECTIVE ACTION 3;[06] INSTALLED NEW INTERCOSTAL STA 344-360; RBL 32; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-03-0G-0; DWG#141A5400.;[07] VERIFIED CORRECTIVE ACTION #6;[08] VERIFIED TASK COMPLETE

Part: INTERCOSTAL — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACKED INTERCOSTAL STA 328-344; LBL 44; WL 208. / [01] UPDATE MEASUREMENTS;[02] REMOVED INTERCOSTAL ON STA 328-344; LBL 44; WL 208 IAW SRM 51-40-02-0G-0 TEM 7.D RECEIVE PO/LOT 234228/033194. OK TO INSTALL;[03] REMOVED INTERCOSTAL ON STA 328-344; LBL 44; WL 208 IAW SRM 51-40-02-0G-0 TEM 7.D RECEIVED PO/LOT 234228/033194 LOCATED HOLES; DRILLED; AND DEBURRED IAW SRM 51-40-05. OK TO INSTALL.;[04] VERIFIED CORRECTIVE ACTOR ITEMS 1-3<BR>OK TO INSTALL;[05] INSTALLED INTERCOSTAL ON STA 328-344; LBL 44; WL 208; IAW SRM 51-40-02-0G-0 ITEM 7.D AND DWG 141A5400;[06] VERIFIED CORRECTIVE ACTION ITEM 5.<BR><BR>* * FLOOR PANEL FASTENER HOLES REQUIRE LOCATING AND DRILLING .;[07] LOCATED AND DRILLED FASTENER FLOOR PANEL HOLE IAW SRM 51-40-05-0G-0 AND BOEING DWG 141A5400;[08] VERIFIED CORRECTIVE ACTION 7.

Part: INTERCOSTAL — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACKED INTERCOSTAL STA 344-360; BL0; WL 208. / [01] REMOVED DAMAGED INTERCOSTAL STA 344-360; BL0; WL 200-208 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL STA 344-360; BL0; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG#141A5400. OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION 1 AND 2;[04] INSTALLED NEW INTERCOSTAL STA 344-360; BL0; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-03-0G-0; DWG#141A5400.;[05] VERIFIED CORRECTIVE ACTION #4;[06] VERIFIED TASK COM[PLETE

Part: BRACKET — CORRODED (L1 DOOR) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON FWD ENTRY GIRT BAR FITTING SUPPORT BRACKET STA 344; LBL 58; WL 209. / [01] NO LIMITS FOUND ON SRM FOR FED GIRT BAR FITTING SUPPORT BRACKET BS344 LBL58 WL209 PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED FED GIRT BAR FITTING SUPPORT BRACKET BS344 LBL58 WL209 I.A.W SRM 51-40-02-0G-0;[03] VERIFIED CORRECTIVE 1 AND 2.;[04] RECEIVED;LOCATED;DRILLED AND INSTALLED NEW FITTING SUPPORT BRACKET BS 344 LBL 58 WL 209 PO 738946-ATS MAT USED 7050T7451 LOT #1307835 HEAT TREATMENT AND FABRICATION VERIFIED IAW DWG ATSFAB-104-301;141A5220 AND SRM 51-40-02-0G-0;51-40-05-0G.;[05] VERIFIED CORRECTIVE ACTION ENTRY 4.

Part: BRACKET — CORRODED (L1 DOOR) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON FWD ENTRY GIRT BAR FITTING SUPPORT BRACKET STA 312; LBL 54; WL 209. / [01] NO LIMITS FOUND ON SRM FOR FED GIRT BAR FITTING SUPPORT BRACKET BS312 LBL54 WL209 PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED FED GIRT BAR FITTING SUPPORT BRACKET BS312 LBL54 WL209 I.A.W SRM 51-40-02-0G-0;[03] VERIFIED CORRECTIVE ACTION 1 AND 2.;[04] RECEIVED;LOCATED;DRILLED AND INSTALLED NEW FITTING SUPPORT BRACKET BS 312 LBL 58 WL 209 PO 738946-ATS MAT USED 7050T7451 LOT #1307835 HEAT TREATMENT AND FABRICATION VERIFIED IAW DWG ATSFAB-104-301;141A5220 AND SRM 51-40-02-0G-0;51-40-05-0G.;[05] VERIFIED CORRECTIVE ACTION ENTRY 4.

Part: INTERCOSTAL — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACKED INTERCOSTAL STA 312-328; RBL 31; WL 208. / [01] REMOVED INTERCOSTAL AT BS312-328; RBL31; WL208; IAW SRM 51-40-02. LOCATED HOLES; DRILLED; AND DEBURRED NEW INTERCOSTAL PO#234228 IAW SRM 51-40-05-0G-0; FIGURE 4.; SHEET 2 AND BOEING DWG141A5400. OK TO INSTALL INTERCONSTAL.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. OK TO INSTALL GIVEN.;[03] INSTALLED NEW INTERCOSTAL AT STA 312-328; RBL 31; WL 208; IAW SRM 51-40-02-0G-0; STEP 7.; D. AND BOEING DWG141A5400.;[04] VERIFIED CORRECTIVE ACTION ENTRY 3.;[05] VERIFIED CARD COMPLETE.

Part: SKIN — CRACKED (R/H HORIZ. STAB.) · airframe 59,572 hrs · 35,384 cycles

RT HORIZONTAL STAB LOWER IN-SPAR SKIN, CRACKED INBOARD OF RIB AT HSS 193.90, CRACK IS .200' LONG & 17.2' FROM FRONT SPAR. REMOVED DAMAGED SECTION IAW SRM 55-10-01-2R-11 PARA 4A; 4B(2) AND 4C. NO INITIAL REPAIR OR MULTIPLE SITE DAMAGE NOTED. HFEC INSPECTED CUTOUT AREA IAW NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. FABRICATED REPAIR. APPLIED CHEMICAL CONVERSION COATING TO REPAIR PARTS & SKIN AT REPAIR AREA IAW SRM 55-10-01-2R-11 PARA 4 G THROUGH 4M. PRIMED REPAIR & AREA IAW SRM 55-10-01-2R-11 PARA 4N. INSTALLED REPAIR IAW SRM 55-10-01-2R-11 PARA 4O & 4P.

Part: INTERCOSTAL — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACKED INTERCOSTAL STA 312-328; LBL 44; WL 208. / [01] UPDATED MEASUREMENTS.;[02] REMOVED INTERCOSTAL ON STA 312-328; LBL 44; WL 44; WL 208 IAW SRM 51-40-02-0G-0 ITEM 7.D AND RECEIVE PO/LOT 233222/033530. OK TO INSTALL;[03] REMOVED INTERCOSTAL ON STA 312-328; LBL 44; WL 208 IAW SRM 51-40-02-0G-0 TEM 7.D RECEIVE PO/LOT 234228/033194 LOCATED HOLES; DRILLED; AND DEBURRED IAW SRM 51-40-05. OK TO INSTALL.;[04] VERIFIED CORRECTIVE ACTION ITEMS 1-3<BR>OK TO INSTALL;[05] INSTALLED INTERCOSTAL ON STA 312-328; LBL 44; WL 208 IAW SRM 51-40-02-0G-0 ITEM 7.D AND DWG 141A5400;[06] VERIFIED CORRECTIVE ACTION ITEM 5.<BR><BR>* * FLOOR PANEL FASTENER HOLES REQUIRE LOCATING AND DRILLING .;[07] LOCATED AND DRILLED FASTENER FLOOR PANEL HOLE IAW SRM 51-40-05-0G-0 AND BOEING DWG 141A5400;[08] VERIFIED CORRECTIVE ACTION 7.

Part: NONE — CORRODED (FWD CABIN) · airframe 59,572 hrs · 35,384 cycles

CORRODED BS 312 FLOORBEAM LBL 36-LBL 42; WL 208. NO ALLOWABLE LIMITS IN SRM. REMOVED CORROSION IAW SRM 51-10-02-0G-0. NDI UT INSPECTION, FOUND REPAIRABLE IAW SRM 53-10-51-2R-15 REPAIR 15, FLAP PEEN BLENDED AREAS IAW SRM 53-10-51-2R-15 REPAIR 15 PAR.4.B(2). PERFORMED DVI OF THE DAMAGE AREA IAW SRM 53-10-51-2R-15 REPAIR 15 PAR.4.C. NO OTHER DAMAGED FOUND. FABRICATED STRAP & 2 FILLERS IAW SRM 53-10-51-2R-15 REPAIR 15 PARG. 4. (D-I). APPLIED A CHEMICAL CONVERSION COATING IAW SRM 53-10-51-2R-15 REPAIR 15 PARG. 4.J. & SRM 51-20-02-0G-0. APPLIED PRIMER IAW SRM 53-10-51-2R-15 REPAIR 15 PARG. 4.K. AND SOPM 20-41-02. INSTALLED REPAIR IAW SRM 51-40-02-0G-0 & SRM 53-10-51-2R-15 REPAIR 15 PARG. 4.(L-O) FIG.204.

Part: INTERCOSTAL — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACKED INTERCOSTAL STA 277-294; RBL 1; WL 208. / [01] REMOVED DAMAGED INTERCOSTAL STA 277-294; RBL 1; WL 208 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL STA 277-294; RBL 1; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG# 141A5400;. OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTIONS 1-2. OK TO INSTALL;[04] INSTALLED NEW INTERCOSTAL STA 277-294; RBL 1; WL 208 PER SRM 51-40-02-0G-0; DWG# 141A5400. JOB IS COMPLETE.;[05] VERIFIED COMPLETION OF STEP 1.;[06] VERIFIED CORRECTIVE ACTION 4. ALL WORK COMPLETE.

Part: CHANNEL — CRACKED (L1 DOOR) · airframe 59,572 hrs · 35,384 cycles

FWD ENTRY DOOR MOPSILL IS CRACKED COMMON TO 303 FRAME; LBL 59; WL 209. / [01] VERIFY APPLICABILITY PER SRM 53-10-15-1A-1 PAR.4.C(1)(A);[02] NO ALLOWABLE TYPICAL FIGURE LIMIT FOUND ON SRM 53-10-15-1A-1 PAR.4.C(1)(A) FOR SPECIFIC CRACK ON BS303 LBL 59 WL209 PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C;[03] REMOVED FED MOPSILL I.A.W SRM 51-40-02-0G-0;[04] VERIFIED CORRECTIVE ACTIONS 1;2 AND 3.;[05] LOCATED AND DRILLED NEW FWD ENTRY DOOR MOPSIL IAW SRM 51-40-05-0G-0 AND DWG 141A8110.;[06] OK TO INSTALL;[07] VERIFIED CORRECTIVE ACTIONS #5 AND #6<BR>OK TO INSTALL GIVEN;[08] INSTALLED 100% TEMPORARY AND PERMANENT FASTENES BEFORE SQUEZEE OUT TIME EXPIRE SEALANT USED BMS 5-95 C-20 APPLIED AT 11-FEB-2022 17:30 UTC.AT FWD ENTRY DOOR MOPSILL BS 270 -360 LBL59 WL 209 IAW SOPM 20-50-19; SRM 51-40-02-0G-0 AND DWG 141A81110;[09] VERIFIED CORRECTIVE ACTION 8.;[10] INSTALLED FWD ENTRY DOOR MOPSILL BS 270 -360 LBL59 WL 209 IAW SRM 51-40-02-0G-0 AND DWG 141A81110;[11] VERIFIED CORRECTIVE ACITON ENTRY 10.

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 500B+6; 500B+14; 500C+2 AND 500C+13 L.B.L. 25. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500B+6 RBL 25 WL 156 FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2473; FLOOR TO SIDEWALL SUPPORT TO BE REPLACED ON CUST CARD# TTG8Q00ANGLK;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE.

Part: SUPPORT ANGLE — CORRODED (L1 DOOR) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON FWD ENTRY SCUFFPLATE SUPPORT ANGLE COMMON TO FWD ENTRY MOPSILL STA 317-323; 337-341; LBL 59-60; WL 209. / [01] NO ALLOWABLE LIMITS FOUND ON SRM PART TO BE REMOVED AND REPLACED I.A.W.SRM 51-10-02-0G-O PAR 9.C;[02] VERIFIED CORRECTIVE ACTION 1;[03] LOCATED AND DRILLED NEW FWD ENTRY SCUFFPLATE SUPPORT ANGLE COMMON TO FWD ENTRY DOOR MOPSIL IAW SRM 51-40-05-0G-0 AND DWG 141A8110.;[04] OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTIONS #3 AND #4<BR>OK TO INSTALL GIVEN;[06] INSTALLED NEW FWD ENTRY SCUFFPLATE SUPPORT ANGLE COMMON TO FWD ENTRY MOPSILL BTW BS 308-344 LBL 60 WL 209 IAW SRM 51-40-02-0G-0 AND DWG 141A8110;141A8230.;[07] VERIFIED CORRECTIVE ACTION 6. ANGLE INSTALLED.;[08] VERIFIED ANGLE REPLACED. ALL WORK ACCOMPLISHED.;[09] UPDATED MISSING MEASUREMENT 13.;[10] CERTIFIED EDIT OF MEASUREMENT TABLE.

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 480+14; 480+18; 500+4; 500+5; 500+10; 500+18; 500A+6; 500A+10; 500A+14 AND 500A+18; L.B.L. 25. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 480+18 LBL 25 WL 156 FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2473;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] LOCATED AND DRILLED NEW FCB LH FLOOR TO SIDEWALL SUPPORT; BS 396-500D; IAW SRM51-40-05-0G-0; DWG 143A7500.;[04] VERIFIED CORRECTIVE ACTION #3

Part: INTERCOSTAL — CRACKED · airframe 59,572 hrs · 35,384 cycles

CRACKED INTERCOSTAL ATTACH ANGLE STA 380-400; BL0; WL 208. / [01] NO DAMAGE LIMITS GIVEN IN SRM PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED CRACK DAMAGED INTERCOSTAL ATTACH ANGLE BETWEEN BS 380 AND 400 BL O WL 208 LOCATED AND DRILLED NEW INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-05-0G-0 OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION ITEMS 1 AND 2;<BR>OK TO INSTALL;[04] INSTALLED NEW INTERCOSTAL ATTACH ANGLE BETWEEN BS 380-400 BLO WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A5400 APPLIED CPC IAW AMM 51-21-91-620-802;[05] VERIFIED CORRECTIVE ACTION ITEM 4. VERIFIED NEW INTERCOSTAL ATTACH ANGLE INSTALLED BETWEEN BS 380-400 BLO WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A5400 APPLIED CPC IAW AMM 51-21-91-620-802.;[06] JOB TASK IS ACCOMPLISHED.;[07] VERIFIED COMPLETE;[08] VERIFIED COMPLETE

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS767+10 - BS787; 749; 727E+2; 727D+10; BS727C. LBL21. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727D+10 LBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2473;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] LOCATED AND DRILLED ACB NEW FLOOR TO SIDEWALL SUPPORT PER SRM 51-40-05-0G-0 AND DWG 146A7500;[04] VERIFIED CORRECTIVE ACTIONS STEP 3.;[05] CORRECTED MEASUREMENT FIELD

Part: SHIELD — CORRODED (AFT CARGO) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767+7 RBL22. / [01] EVALUATED CORROSION ON SHIELD BS 767+7 RBL 22 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] LOCATED AND DRILLED NEW SHIELD AT AFT CARGO BAY BS767 TO BS794 RBL22; PER SRM 51-40-05-0G-0 AND DWG 146A0081.;[04] VERIFIED CORRECTIVE ACTION #3<BR>OK TO INSTALL SHIELD AT AFT CARGO BAY BS767 TO BS794 RBL22 GIVEN;[05] INSTALLED NEW SHIELD AT AFT CARGO BAY BS767 TO BS794 RBL22; PER SRM 51-40-02-0G-0 AND DWG 146A0081.;[06] VERIFIED CORRECTIVE ACTION 5.;[07] WORKSCOPE COMPLETE.;[08] CORRECTED MEASUREMENT TABLE;[09] CERTIFIED

Part: SPLICE — CORRODED (AFT FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON FLOOR SUPPORT SPLICE AT ACB BS887 BL0 TO RBL12. / [01] EVALUATED CORROSION ON FLOOR SUPPORT SPLICE BS 887 BL 0 TO RBL 12 WL 168; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] LOCATED AND DRILLED NEW FLOOR SUPPORT SPLICE AT ACB BS887 BL0 TO RBL12; PER SRM 51-40-05-0G-0 AND DWG 147A7500.;[04] VERIFIED CORRECTIVE ACTION 3. PART TO BE INSTALLED ON TTG8Q004GE79;[05] CORRECTED MEASUREMENT TABLE

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727A+18 - BS767 RBL21. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727A+18 RBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2473;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] LOCATED AND DRILLED NEW ACB FLOOR TO SIDEWALL SUPPORT AT BS727- BS767 PER SRM 51-40-05-0G-0 AND DWG 146A7500;[04] VERIFIED CORRECTIVE ACTION #3;[05] CARD COMPLETE

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 59,572 hrs · 35,384 cycles

CRACKED STIFFENER BEHIND WATER SERVICE PANEL AT ACB BS914 RBL11. / [01] EVALUATED STIFFENER BS 914 RBL 11 WL 169; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] REMOVED CRACKED STIFFENER BEHIND WATER SERVICE PANEL AT ACB BS 914; RBL 11. PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW STIFFENER BEHIND WATER SERVICE PANEL AT ACB BS 914; RBL 11. PER AIPC 52-49-00-02 AND SRM 51-40-05-0G-0. OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION #3 AND 4;[06] SEALED AND INSTALLED NEW STIFFENER BEHIND WATER SERVICE PANEL AT ACB BS914; RBL11. PER AIPC 52-49-00-02; AMM 51-31-00-390-801; AND SRM 51-40-02-0G-0;[07] VERIFIED CORRECTIVE ACTION 6;[08] VERIFIED JOB COMPLETE

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 59,572 hrs · 35,384 cycles

PASSENGER CABIN FLOOR PANEL 231EF IS DELAMINATED ON UPPER SURFACE. / [01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 231EF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-81 ITEM 35.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 59,572 hrs · 35,384 cycles

CRACKED STIFFENER BEHIND WATER SERVICE PANEL AT ACB BS918 RBL11. / [01] EVALUATED CRACKED STIFFENER; BS 918 RBL 11 WL 170; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-2-0G-0;[02] UPDATED MEASUREMENT FIELD;[03] VERIFIED CORRECTIVE ACTION ENTRY 1.;[04] REMOVED CRACKED STIFFENER BEHIND WATER SERVICE PANEL AT BS 918; RBL 11. PER SRM 51-40-02-0G-0;[05] LOCATED AND DRILLED NEW STIFFENER BEHIND WATER SERVICE PANEL AT ACB BS 918; RBL 11. PER AIPC 52-49-00-02 AND SRM 51-40-05-0G-0. OK TO INSTALL.;[06] VERIFIED CORRECTIVE ACTION #4 AND 5;[07] SEALED AND INSTALLED NEW STIFFENER BEHIND WATER SERVICE PANEL AT ACB BS918; RBL11. PER AIPC 52-49-00-02; AMM 51-31-00-390-801; AND SRM 51-40-02-0G-0;[08] VERIFIED CORRECTIVE ACTION 7;[09] VERIFIED JOB COMPLETE

Part: INTERCOSTAL — CORRODED (AFT CARGO) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS787+8 RBL6. / [01] EVALUATED CORROSION ON INTERCOSTAL BS 787+8 RBL 6 WL 153-154; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] REMOVED ACB INTERCOSTAL AT BS787 - BS807; RBL6 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED ACB NEW INTERCOSTAL AT BS787 - BS807; RBL6; WL154 PER SRM 51-40-05-0G-0 AND DWG 146A8130. OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION ENTRY 4. OK TO INSTALL GIVEN.;[06] INSTALLED ACB NEW INTERCOSTAL AT BS787 - BS807; RBL6; WL154 PER SRM 51-40-02-0G-0 AND DWG 146A8130.;[07] VERIFIED CORRECTIVE ACTION #6;[08] VERIFIED CORRECTIVE ACTION #6

Part: TRACK — CORRODED (AFT CARGO BAY) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON TRACK AT ACB BS727A RBL13. MARKED. / [01] EVALUATED CORROSION AT BS 727A RBL 13 WL 156; FOUND 0.020 REMOVED FROM ORIG 0.071 IN 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2473; TRACK TO BE REPLACED ON CUST CARD #TTG8Q00AN518;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE

Part: SUPPORT ANGLE — CORRODED (AFT FUSELAGE) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS947 LBL7 TO RBL17. / [01] EVALUATED CORROSION ON BULKHEAD SUPPORT BS 947 LBL 7 TO RBL 17 WL 179; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] LOCATED; DRILLED; AND DEBURRED NEW AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS947 LBL10 TO RBL23 PER SRM 51-40-05-0G-0 AND DWG 149A8117 AND DWG 149A8110;[04] VERIFIED CORRECTIVE ACTION #3;[05] OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION #5<BR>OK TO INSTALL GIVEN;[07] INSTALLED NEW AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS 947 LBL 7 TO RBL 17 IAW SRM 51-40-02-0G-0; DWG 149A8117 AND DWG 149A8110;[08] VERIFIED CORRECTIVE ACTION ITEM 7;[09] VERIFIED CORRECTIVE ACTION ITEM 7;[10] CORRECTED MEASUREMENT TABLE

Part: RAIL — CORRODED (AFT CARGO) · airframe 59,572 hrs · 35,384 cycles

CORROSION ON RAIL AT ACB BS927+18 RBL3. / [01] EVALUATED CORROSION ON RAIL AT BS 927+18 RBL 3 WL 179; FOUND 0.020 REMOVED FROM ORIG 0.063 IN 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2473;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] REMOVED ACB RAIL AT BS947 -887; RBL3 PER SRM 51-40-02-0G-0;[04] FABRICATED ACB NEW RAIL USING BAC1509-100146#7050T76511 LOT# 1464919-1 AT BS947 -887; RBL3 PER SRM 51-40-05-0G-0 AND DWG 147A7501;[05] VERIFIED CORRECTIVE ACTION ENTRY 4.;[06] RECEIVED RAIL FROM OSS ANODIZE ON PO#855827-SWA;[07] VERIFIED CORRECTIVE ACTION 6. OK TO PRIME.;[08] APPLIED PRIMER TO ACB NEW RAIL PER AMM 51-21-72-370-804. OK TO INSTALL RAIL;[09] VERIFIED CORRECTIVE ACTION 8. OK TO INSTALL RAIL.;[10] INSTALLED ACB NEW RAIL USING AT BS947 -887; RBL3 PER SRM 51-40-02-0G-0 AND DWG 147A7501;[11] VERIFIED CORRECTIVE ACTION ITEM 10.;[12] VERIFIED CORRECTIVE ACTION ITEM 10.;[13] CORRECTED MEASUREMENT TABLE

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 59,572 hrs · 35,384 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / [01] UPDATED MEASUREMENT TABLE AND VERIFIED SRM 53-60-15-2R-1 TO BE CORRECT;[02] WELDED CRACKS ON ACB; AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(2) AND (4)<BR>WELDING MACHINE CAL ID: E10583; S/N; KJ256554;[03] VERIFIED CORRECTIVE ACTIONS 1-2;[04] PT INSPECTED WELDED AREAS IAW SOPM 20-20-02. NO CRACKS NOTED. EQUIP USED: RADIOMETER ID: ATS2561-1;2;3;[05] SANDED WELD REPAIR AREAS PER SRM 53-60-15-2R-1 PARA 4.B.(5);[06] VERIFIED CORRECTIVE ACTION 5.

Part: ANGLE — CRACKED (CENTER WING) · airframe 59,572 hrs · 35,384 cycles

CRACKED VERTICAL STIFFENER ANGLE ON B.S. 663 LOWER COMPOSITE BULKHEAD AT L.B.L. 27; W.L. 150; ON AFT SIDE. / [01] REMOVED VERTICAL STIFFENER ANGLE BS663 LBL27 WL150-WL163 ON AFT SIDE OF LOWER COMPOSITE BLKHD IAW SRM 51-40-02.;[02] LOCATED; DRILLED; AND DEBURRED NEW VERTICAL STIFFENER ANGLE BS663 LBL27 WL150-WL163 IAW SRM 51-40-05 AND DWG #111A1000.;[03] VERIFIED CORRECTIVE ACTION 1 AND 2;[04] INSTALLED NEW VERTICAL STIFFENER ANGLE BS663 LBL27 WL150-WL163 IAW SRM 51-40-02 AND DWG #111A1000.;[05] VERIFIED CORRECTIVE ACTION #4;[06] VERIFIED TASK COMPLETE

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 58,299 hrs · 34,598 cycles

CABIN FLOOR PANEL 231ZF HAS PUNCTURE AT INBD EDGE DOT A-21-02 ; / [01] EVALUATED PANEL 231ZF AND FOUND A DENT WITH PUNCTURE AT INBD/EDGE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-2 PAR 1A REV74.; [02] BOND TEST IAW B737 NDT PART 4; 51-00-05. NO DEFECTS NOTED. TOOL#31823; DUE 05OCT21; [03] REMOVE INSERT. CLEAN AND PREP AREA FOR REPAIR. APPLIED POTTING COMPOUND TO REPAIR. IAW SRM 53-00-50-2R-2 PAR3A-I REV74. REPAIRED PUNCTURE AT INBD/EDGE OF PANEL 231ZF. IAW SRM 53-00-50-2R-2 SRM 53-00-50-2R-0.

Part: CIRCUIT BREAKER — TRIPPED (SPEED BRAKES) · airframe 57,498 hrs · 34,131 cycles

SPEED BRAKE FAILED TO DEPLOY AUTOMATICALLY ON LANDING; AUTO SPEED BRAKE CIRCUIT ; SPEED BRAKE FAILED TO DEPLOY AUTOMATICALLY ON LANDING; AUTO SPEED BRAKE CIRCUIT BREAKER FOUND POPPED. / REMOVED AND REPLACED AUTO SPEED BRAKE ACTUATOR PER AMM 27-62-31. OPS CHECKS GOOD. THIS CLEARS MEL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,394 hrs · 33,479 cycles

RIGHT OVERWING EXIT EMERGENCY LIGHT LENS MISSING. REPLACED LIGHT LENS, PER M/M 33-51-04.

Part: COVER — INCORRECT (EMERGENCY LIGHT) · airframe 56,093 hrs · 33,301 cycles

RIGHT OVERWING EXIT, CENTER AFT EMERGENCY EXIT LIGHT LENS NOT BILINGUAL. REMOVED AND REPLACED RIGHT OVERWING EXIT SIGN WITH CORRECT LIGHT COVER, REF AMM 33-51-01.

Part: GIRT BAR — STUCK (L1 DOOR) · airframe 55,530 hrs · 32,942 cycles

FORWARD ENTRY GIRT BAR STUCK. LUBRICATED THE GIRT BAR IAW AMM 25-66-01, OPS NORMAL.

Part: BATTERY — FAULTY (MEGAPHONE) · airframe 55,458 hrs · 32,896 cycles

FWD MEGAPHONE INTERMITTENT. R & R FWD MEGAPHONE BATTERYS IAW AMM 25-64-00

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 54,842 hrs · 32,514 cycles

CREW REPORTS BOTH FWD FLASHLIGHTS NOT BLINKING. REMOVED AND REPLACED BOTH FWD FLASHLIGHT BATTERIES REF AMM 25-64-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,824 hrs · 32,503 cycles

FWD SERVICE DOOR LWR EXIT SIGN INOP WHEN TESTING EMERGENCY LIGHTING SYSTEM. / R&R BATTERY PACK AT EMERGENCY LIGHT POWER SUPPLY M1674 PER AMM.

Part: NUT PLATE — BROKEN (DOOR FRAME) · airframe 54,825 hrs · 32,503 cycles

BROKEN NUTPLATE IN AFT CARGO DOOR FRAME ANGLE AT STRINGER 19 STA 794. MARKED / REMOVED AND REPLACED NUT PLATE PER SRM 51-40-02

Part: GUSSET — CRACKED (BS 500D) · airframe 54,824 hrs · 32,503 cycles

FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET PER SRM.

Part: GUSSET — CRACKED (BS 500D-520) · airframe 54,824 hrs · 32,503 cycles

INTERCOSTAL WEB UNDER SEAT TRACK BETWEEN BS. 500D TO BS. 520, RBL 45 HAD CRACKED FASTENER HOLE. / R&R INTERCOSTAL WEB PER SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 54,824 hrs · 32,503 cycles

FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET PER SRM.

Part: FLOOR PANEL — DAMAGED · airframe 54,825 hrs · 32,503 cycles

FLOOR PANEL 241MF NEEDS TO BE REPLACED DUE TO DENT DAMAGE AND LOOSE FIBERS ON PANEL / REMOVED AND REPLACED FLOOR PANEL 241MF WITH SERVICEABLE PANEL PER AMM 53-21-00

Part: FLOOR PANEL — DAMAGED · airframe 54,825 hrs · 32,503 cycles

REMOVE AND REPLACE FLOOR PANELS DUE TO DENT DAMAGE AND LOOSE FIBERS ON PANELS; 241SF; 241JF; 241EF; 241QF AND 242JF. / REMOVED AND REPLACED FLOOR PANELS 241SF; 241JF; 241EF; 241QF AND 242JF PER AMM 53-21-00.

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 54,825 hrs · 32,503 cycles

LEFT OUTBOARD AFT FLAP; INBOARD TRAILING EDGE LOWER SURFACE HAS DISBOND. / REPAIRED PER SRM 57-53-01-2R-4 AND 51-70-10.

Part: CONNECTOR — CRACKED (CABIN) · airframe 54,824 hrs · 32,503 cycles

SEAT 19DEF, OHD BIN AFT EMERGENCY EXIT LIGHT (D11336) FEMALE PLUG P/N AMCO2PA03WWC IS CRACKED. / R&R PLUG D11336 PER WDM.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 54,824 hrs · 325,003 cycles

CABIN FLOORBOARD TRANSITION INTERCOSTAL SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO RBL 25. / R&R SUPPORT PER SRM.

Part: LOCK — MISSING (STOP FITTING) · airframe 54,825 hrs · 32,503 cycles

AFT CARGO DOOR; FWD STOP SECOND FROM THE BOTTOM MISSING LOCKING CLIP AND MAY REQUIRE ADJUSTMENT. / ADJUSTED STOP PIN AND INSTALLED LOCKING CLIP PER AMM 52-31-00

Part: ANGLE — CORRODED (BS 727B-817) · airframe 54,825 hrs · 32,503 cycles

AFT CARGO COMPARTMENT L/H SIDE TRANSITION ANGLE HAS CORROSION IN SEVERAL AREA FROM BS.727B +13; LBL 20 TO BS 817. / REMOVED AND REPLACED LH TRANSITION ANGLE FROM STA 727-847 PER SRM 51-40-02 WITH PART NUMBER 146A7502-27

Part: ANGLE — CORRODED (BS 727B-767) · airframe 54,825 hrs · 32,503 cycles

AFT CARGO COMPARTMENT TRANSITION ANGLE BS 727B+8 TO BS 767 RBL 20; HAS CORROSION IN SEVERAL AREAS. (MARKED.) / REMOVED AND REPLACED R/H TRANSITION ANGLE PART # 146A7502-51 FROM STA.727 TO STA.767 PER SRM 51-40-02.

Part: SUPPORT BRACKET — BROKEN (BS 727) · airframe 54,825 hrs · 32,503 cycles

AFT CARGO COMPARTMENT BS 727 BULKHEAD PANEL SUPPORT BRACKET BROKEN RBL 4; WL 161. / REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 54,824 hrs · 32,503 cycles

AFT ENTRY DOOR SLIDE IS CATCHING LOWER DOOR FRAME WHEN CLOSING THE DOOR. / R&R AFT ENTRY SLIDE ASSEMBLY PER MT.

Part: BALANCE WEIGHT — CORRODED (TAIL) · airframe 54,825 hrs · 32,503 cycles

RUDDER WEIGHT HAS EVIDENCE OF CORROSION / REMOVED AND REPLACED RUDDER BALANCE WEIGHT PER CMM 55-40-09 AND AMM 20-50-11.

Part: SEAT TRACK — CORRODED (BS 663) · airframe 54,824 hrs · 325,003 cycles

L/H CABIN #1 SEAT TRACK UPPER AND LOWER FLANGE HAD EVIDENCE OF CORROSION DAMAGE ON SEAT TRACK BETWEEN BS. 663 THROUGH BS. 663+18. / R&R #1 SEAT TRACK PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,824 hrs · 32,503 cycles

L/H HORIZONTAL STABILIZER #4 STA. 120.30 INSPAR RIB #3 VERTICAL STIFFENER HAD A CRACK APPROXIMATELY 1" FROM LOWER SKIN. / REPAIRED RIB PER SRM.

Part: SEAT TRACK — CORRODED (BS 727) · airframe 54,824 hrs · 325,003 cycles

L/H CABIN #1 SEAT TRACK UPPER AND LOWER FLANGE HAD EVIDENCE OF CORROSION DAMAGE ON SEAT TRACK BETWEEN BS. 727 THROUGH BS. 727+15. / R&R #1 SEAT TRACK PER SRM.

Part: SEAT TRACK — CORRODED (BS 648-649) · airframe 54,824 hrs · 325,003 cycles

PASSENGER CABIN SEAT TRACK CORRODED BETWEEN BS. 648 TO BS. 649, RBL 45, LOWER SURFACE. / R&R #4 SEAT TRACK PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,824 hrs · 32,503 cycles

L/H HORIZONTAL STABILIZER #4 STA. 120.30 INSPAR RIB #2 VERTICAL STIFFENER CRACKED APPROXIMATELY 1" FROM LOWER SKIN. / REPAIRED RIB PER SRM.

Part: SEAT TRACK — CORRODED (BS 685-706) · airframe 54,824 hrs · 325,003 cycles

L/H CABIN #1 SEAT TRACK UPPER AND LOWER FLANGE HAD EVIDENCE OF CORROSION DAMAGE ON SEAT TRACK BETWEEN BS. 685 THROUGH BS. 706. / R&R #1 SEAT TRACK PER SRM.

Part: SEAT TRACK — CORRODED (BS 727A-727B) · airframe 54,824 hrs · 325,003 cycles

L/H CABIN #1 SEAT TRACK UPPER AND LOWER FLANGE HAD EVIDENCE OF CORROSION DAMAGE ON SEAT TRACK BETWEEN BS. 727A+10 THROUGH BS. 727B. / R&R #1 SEAT TRACK PER SRM.

Part: SEAT TRACK — CORRODED (BS 597-616) · airframe 54,824 hrs · 325,003 cycles

L/H CABIN #1 SEAT TRACK UPPER AND LOWER FLANGE HAD EVIDENCE OF CORROSION DAMAGE ON SEAT TRACK BETWEEN BS. 597 THROUGH BS. 616. / R&R #1 SEAT TRACK PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,824 hrs · 32,503 cycles

L/H HORIZONTAL STABILIZER #4 STA. 120.30 INSPAR RIB #4 VERTICAL STIFFENER HAD A CRACKED APPROXIMATELY 1" FROM LOWER SKIN. / REPAIRED RIB PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,824 hrs · 32,503 cycles

R/H HORIZONTAL STABILIZER #4 STA. 120.30 INSPAR RIB #3 VERTICAL STIFFENER HAD A CRACKED APPROXIMATELY 1" FROM LOWER SKIN. / REPAIRED RIB PER SRM.

Part: SEAT TRACK — CORRODED (BS 639) · airframe 54,824 hrs · 325,003 cycles

L/H CABIN #1 SEAT TRACK UPPER AND LOWER FLANGE HAD EVIDENCE OF CORROSION DAMAGE ON SEAT TRACK BETWEEN BS. 639 THROUGH BS. 639+10. / R&R #1 SEAT TRACK PER SRM.

Part: SEAT TRACK — CORRODED (BS 616-639) · airframe 54,824 hrs · 325,003 cycles

L/H CABIN #1 SEAT TRACK UPPER AND LOWER FLANGE HAD EVIDENCE OF CORROSION DAMAGE ON SEAT TRACK BETWEEN BS. 616 THROUGH BS. 639. / R&R #1 SEAT TRACK PER SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 54,824 hrs · 32,503 cycles

R/H HORIZONTAL STABILIZER #4 STA. 120.30 INSPAR RIB #2 VERTICAL STIFFENER CRACKED APPROXIMATELY 1" FROM LOWER SKIN. / REPAIRED RIB PER SRM.

Part: SEAT TRACK — CORRODED (BS 630-631) · airframe 54,824 hrs · 325,003 cycles

PASSENGER CABIN SEAT TRACK CORRODED BETWEEN BS. 630 TO BS. 631, RBL 45, LOWER SURFACE. / R&R #4 SEAT TRACK PER SRM.

Part: SEAT TRACK — CORRODED (BS 706) · airframe 54,824 hrs · 325,003 cycles

L/H CABIN #1 SEAT TRACK UPPER AND LOWER FLANGE HAD EVIDENCE OF CORROSION DAMAGE ON SEAT TRACK BETWEEN BS. 706 THROUGH BS. 706+5. / R&R #1 SEAT TRACK PER SRM.

Part: SEAT TRACK — CORRODED (BS 612-616) · airframe 54,824 hrs · 325,003 cycles

PASSENGER CABIN SEAT TRACK CORRODED BETWEEN BS. 612 TO BS. 616, RBL 45, LOWER SURFACE. / R&R #4 SEAT TRACK PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,824 hrs · 32,503 cycles

R/H HORIZONTAL STABILIZER #4 STA. 120.30 INSPAR RIB #4 VERTICAL STIFFENER HAD A CRACKED APPROXIMATELY 1" FROM LOWER SKIN. / REPAIRED RIB PER SRM.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 53,616 hrs · 31,759 cycles

AFT CARGO FLOOR PANEL 140BF FOUND CRACKED. / REMOVED/FABRICATED INSTALLED AFT CARGO FLOOR PANEL 140BF I.A.W. AMM 25-52-10.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 53,521 hrs · 31,691 cycles

L1 DOOR SLIDE FELL OUT OF HOUSING, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,536 hrs · 31,063 cycles

CENTER AISLE OVERHEAD EMERGENCY LIGHT EXIT SIGN FOR OVERWING EXIT INOP. / R&R SIGN IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,010 hrs · 30,755 cycles

AIRCRAFT CENTER OVERHEAD EMERGENCY EXIT SIGN INOP. R+R AIRCRAFT CENTER OVERHEAD EMERGENCY EXIT SIGN POWER SUPPLY IAW AMM 33-51-06. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,590 hrs · 30,498 cycles

LT EMERGENCY LIGHTS INOP BETWEEN SEAT 9 TO SEAT 12. R&R LIGHT ASSEMBLY PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,590 hrs · 30,498 cycles

LT EMERGENCY LIGHTS INOP BETWEEN SEAT 9 TO SEAT 12. R&R BATTERY PACK AT M1670 PER AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 51,590 hrs · 30,498 cycles

LT EMERGENCY LIGHTS INOP BETWEEN SEAT 9 TO SEAT 12. R&R POWER SUPPLY M1670 PER AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 51,089 hrs · 30,175 cycles

LT FORWARD CABIN CEILING AISLE EXIT LOCATOR SIGN INOP. R&R BATTERY PACK CHARGER ASSEMBLY PER AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 49,952 hrs · 29,446 cycles

CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN INOP. R&R POWER SUPPLY PER AMM.

Part: RIVET — LOOSE (R1 DOOR) · airframe 49,722 hrs · 29,292 cycles

R1 DOOR SLIDE COVER AFT GIRT BAR RETAINER LOOSE. R&R RIVET PER SRM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 49,722 hrs · 29,292 cycles

R1 DOOR BEAM CRACKED. R&R R1 DOOR PER AMM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,687 hrs · 28,617 cycles

MID CABIN EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE POWER SUPPLY IAW MM.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 48,102 hrs · 28,269 cycles

REAR SPAR VERTICAL WEB ATTACH ANGLE DRAIN VALVE CUTOUT CRACKED AT BS 663, LBL 35. REPAIRED ANGLE IAW EA.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 48,102 hrs · 28,269 cycles

AFT CARGO COMPARTMENT BETWEEN STA 727D AND 767 L/H CAP STRIP HAS MULTIPLE AREAS OF CORROSION ON BOTTOM SKIN SURFACES AS MARKED / REPLACED DAMAGED AFT CARGO COMPARTMENT STA 727-D 767 L/H CAPSTRIP WITH A NEW P/N 453A2611-10; ATAG # A138BS CAPSTRIP I/A/W DWG# 453A2600 REV D-

Part: CAP — CORRODED (AFT CARGO BAY) · airframe 48,102 hrs · 28,269 cycles

AFT CARGO COMPARTMENT BETWEEN STA 727 AND 727 D L/H CAP STRIP HAS MULTIPLE AREAS OF CORROSION ON BOTTOM SKIN SURFACES NOTE: 1 EA CAP STRIPS AS MARKED / REPLACED CAPSTRIP (P/N# 453A2611-8 ATAG WN1222) AFT CARGO COMPARTMENT STA 727-727D L/H IAW AMM 25-52-06-400-801.

Part: FRAME — CRACKED (BS 727D) · airframe 48,102 hrs · 28,269 cycles

FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: BRACKET — CRACKED (LT WING) · airframe 48,102 hrs · 28,269 cycles

LH WING INTERNAL WING INSPECTION FOUND SEAL MOUNT BRACKET CRACKED 24' INBD OF STA. ORSS 297. CRACK IS ON THE BACKSIDE UPPER CORNER. MARKED WITH A DOT. / REMVOED FITTING L/H WING IAW SRM 51-40-02-0G-0 VERFIED NEW PART NO 115A2953-1 IAW BOEING DWG 115A2930 DRILLED NEW PART IAW SRM 51-40-02-0G-0 INSTALLED NEW FITTING FOR SEAL MOUNT L/H WING IAW BOEING DWG 115A2930

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 48,102 hrs · 28,269 cycles

RIGHT MAIN WHEEL WELL PRESSURE BULKHEAD WEB CRACKED AT BS 663, RBL 35. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: SHROUD — CRACKED (FWD FUSELAGE) · airframe 47,394 hrs · 27,840 cycles

SUPPLEMENTAL INFORMATION: EXTERNAL GROUND POWER RECEPTACLE SHROUD IS CRACKED ON AFT END IN THE RADIUS / REMOVED & REPLACED GROUND POWER RECEPTACLE SHROUD PER SRM 51-40-02-0G-0 AND DWG 141A0640

Part: FLAP — DELAMINATED (LEFT WING) · airframe 45,685 hrs · 26,797 cycles

L/H O/B AFT FLAP; I/B AFT CORNER IS DELAMINATED. DELAM MEASURES APROX. 3.250' X 3.00' / EVALUATED; PREPPED; CLEANED AND REPAIRED DELAM DAMAGE TO L/H O/B AFT FLAP; I/B AFT CORNER IAW B737 SRM 51-70-10-2R-0; PER SRM 51-70-10-2R-4. PAR 3(A&D); PER SRM 57-53-01-2R-4 PAR 3(A&B) REV 63.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 45,685 hrs · 26,797 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 45,685 hrs · 26,797 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 45,685 hrs · 26,797 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 45,685 hrs · 26,797 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 44,444 hrs · 26,070 cycles

FORWARD FLASHLIGHT INOP. R&R BATTERY PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,058 hrs · 24,674 cycles

RIGHT INTERIOR EMER EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

AFT CARGO BAY THRESH HOLD SUB WEB CORRODED, BETWEEN BS 802 - 837. R & R WEB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 500A - 500D, RBL 25. REPAIRED SUPPORT IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,058 hrs · 24,674 cycles

AFT CARGO BAY CARGO TRACK CORRODED AT BS 942, RBL 10. R & R TRACK IAW SRM.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

AFT CARGO BAY PANEL SUPPORT CORRODED AT BS 887, BETWEEN LBL 13 TO RBL 13. R & R SUPPORT IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,058 hrs · 24,674 cycles

AFT CARGO BAY CARGO TRACK CORRODED, BETWEEN BS 887 - 947, BETWEEN LBL 10 - RBL 10. R & R TRACK IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 848, RBL 22. R & R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 767 - 792, RBL 22. R & R SUPPORT IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,058 hrs · 24,674 cycles

AFT CARGO BAY CARGO TRACK CORRODED AT BS 934, RBL 10. R & R TRACK IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 470 - 500D, LBL 25. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727 - 767, RBL 20. R & R SUPPORT IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

THRESHOLD WEB CORRODED, BETWEEN BS 445 - 485, RBL 29. R & R WEB IAW SRM & DWG.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 42,058 hrs · 24,674 cycles

RIGHT HORIZONTAL STABILIZER, 2ND FROM FRONT SPAR, VERTICAL STIFFENER CRACKED AT STATION 138.70. REPAIRED STIFFENER IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT BS 500B, STRINGER 26L. R & R CLIP IAW DWG & SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FLOOR TO SIDE WALL SUPPORT SHIELD CORRODED, BETWEEN BS 500 - 500A, RBL 27. R & R SHIELD IAW SRM & DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,058 hrs · 24,674 cycles

LEFT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT STATION 92.70, 2ND FROM FWD SPAR CHORD. REPAIRED RIB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727 - 847, LBL 20. REPAIRED SUPPORT IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT BS 500C, STRINGER 26L. R & R CLIP IAW DWG & SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,058 hrs · 24,674 cycles

LEFT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT STATION 92.70, 3RD FROM FWD SPAR CHORD. REPAIRED RIB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME AT CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 42,058 hrs · 24,674 cycles

RIGHT WING UPPER TE PANEL, CTR SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT, ABOVE NR 2 PYLON AFT TIP. R & R ANGLE IAW SRM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 42,058 hrs · 24,674 cycles

AFT CARGO BAY DOOR CUT OUT AFT CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 41,785 hrs · 24,501 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE IAW MT.

Part: LENS — OUT OF POSITION (CABIN) · airframe 38,217 hrs · 22,400 cycles

AFT GALLEY EMER EXIT LIGHT LENS OUT OF POSITION. REPOSITIONED LENS IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,052 hrs · 21,747 cycles

EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST AT POSITION M1672. R & R BATTERY PACK IAW MM & DWG.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 35,478 hrs · 20,816 cycles

INTERCOSTAL DAMAGED AT BS 540, BETWEEN BL 0 TO LBL 24. R & R INTERCOSTAL IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 35,478 hrs · 20,816 cycles

LEFT WING OTBD AFT FLAP DELAMINATED ON LOWER SKIN AT INBD LOWER AFT CORNER. REPAIRED AFT FLAP IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 35,478 hrs · 20,816 cycles

FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727B, LBL 45, INBD FWD HOLE & OTBD FWD HOLE. REPAIRED BEAM IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,478 hrs · 20,816 cycles

SEAT TRACK FLANGE CRACKED FWD OF FLOORBEAM AT BS 727B, RBL 24. REPAIRED FLANGE IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 35,478 hrs · 20,816 cycles

FLOORBEAM VERTICAL WEB CRACKED AT BS 727B, LBL 45, 3RD HOLE FROM THE BOTTOM. REPAIRED WEB IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,478 hrs · 20,816 cycles

SEAT TRACK FLANGE CRACKED FWD OF FLOORBEAM AT BS 727B, RBL 45. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,478 hrs · 20,816 cycles

SEAT TRACK FLANGE FWD CRACKED AT BS 727B, LBL 24, INBD FWD HOLE & OTBD AFT HOLE. REPAIRED BEAM IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,478 hrs · 20,816 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 147.9, 9.5 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,478 hrs · 20,816 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 101.9, 19.75 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,478 hrs · 20,816 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 138.7, 17.5 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,478 hrs · 20,816 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 138.7, 16.5 INCHES FROM FRONT SPAR. REPAIRED SKIN IAW SRM.

Part: HOLDER — LOOSE (L1 DOOR) · airframe 35,460 hrs · 20,805 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR HOLDER LOOSE. R & R HOLDER IAW SIP.

Part: SIGN — BROKEN (CABIN) · airframe 35,450 hrs · 20,798 cycles

R2 DOOR EMER EXIT SIGN BROKEN. R & R SIGN ASSEMBLY IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 35,049 hrs · 20,569 cycles

OVERWING CTR AISLE EMERGENCY EXIT SIGN LOOSE. R & R SIGN IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 34,880 hrs · 20,476 cycles

R1 COCKPIT WINDOW FRAME CRACKED IN THE UPPER OTBD CORNER. REPAIRED FRAME IAW EA.

Part: BRACKET — CRACKED (RT WING) · airframe 32,647 hrs · 19,161 cycles

RT WING AFT SPAR LOWER BULB SEAL BRACKET CRACKED ABOVE PANEL 651GB. REPAIRED BRACKET IAW SRM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 31,700 hrs · 18,588 cycles

R2 DOOR EMERGENCY EXIT SIGN COVER LOOSE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER M/M.

Part: SLIDER — CRACKED (LT HORIZ STAB) · airframe 30,324 hrs · 17,783 cycles

LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDER CRACKED. REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDER PER SRM 51-40-02.

Part: SLIDER — CRACKED (RT HORIZ STAB) · airframe 30,324 hrs · 17,783 cycles

RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDER CRACKED. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDER PER SRM 51-40-02.

Part: SIGN — BROKEN (CABIN) · airframe 30,210 hrs · 17,719 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,936 hrs · 17,550 cycles

FORWARD FLOOR PATH EMERGENCY LIGHT INOP. RECONNECTED LIGHT ASSY IAW M/M.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 29,226 hrs · 17,107 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: LIGHT — DAMAGED (CABIN) · airframe 28,688 hrs · 16,791 cycles

R2 DOOR EMERGENCY EXIT LIGHT AFT OF DOOR INTERIOR DAMAGED. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 28,618 hrs · 16,742 cycles

RIGHT FLOOR TO SIDEWALL AFT CARGO BAY CRACKED AT I/B FRAME BS 747. REMOVED AND REPLACED SUPPORT PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,618 hrs · 16,742 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED STA 101.90. REPAIRED SKIN IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 28,618 hrs · 16,742 cycles

RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 783. REMOVED & REPLACED SUPPORT IAW DWG & SRM.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 27,566 hrs · 16,115 cycles

DURING SCHEDULED OTS CHECK, FOUND BUTT STRAP CRACKED AT BS 1088, STR 18L. REMOVED AND REPLACED STRAP IAW SRM AND DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 27,482 hrs · 16,074 cycles

R2 DOOR EMERGENCY EXIT LIGHTS BROKEN. R&R LIGHT ASSY. PER MM.

Part: COVER — MISSING (CABIN) · airframe 27,040 hrs · 15,824 cycles

EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 26,112 hrs · 15,275 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 25,955 hrs · 15,181 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EMERGENCY EXIT DOOR SIDEWALL LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: COVER — LOOSE (CABIN) · airframe 25,263 hrs · 14,775 cycles

DURING SCHEDULED MV1 CHECK FOUND, EEPLS COVER LOOSE AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,114 hrs · 14,688 cycles

FWD EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — LOOSE (L1 DOOR) · airframe 25,027 hrs · 14,636 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 24,905 hrs · 14,559 cycles

FWD EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,705 hrs · 14,443 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,654 hrs · 14,418 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1. REMOVED AND REPLACED BULB PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 23,915 hrs · 14,004 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT BATTERY PACK FAILED TEST AT ROW 16. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — CRACKED (CABIN) · airframe 23,915 hrs · 14,004 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: CAP — MISSING (CABIN) · airframe 23,915 hrs · 14,004 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD EEPLS END CAP MISSING. INSTALLED END CAP PER MM.

Part: COVER — BROKEN (CABIN) · airframe 23,826 hrs · 13,948 cycles

LEFT WD EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,246 hrs · 13,630 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 2. RELAMPED PER MM.

Part: LENS — LOOSE (CABIN) · airframe 22,108 hrs · 12,959 cycles

LOWER L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REPAIRED LENS PER EA.

Part: LIGHT — FAULTY (CABIN) · airframe 22,068 hrs · 12,933 cycles

DURING SCHEDULED 6Y CHECK, FOUND EMERGENCY EXIT LIGHT FAULTY BETWEEN ROW 9 TO ROW 12. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 22,068 hrs · 12,932 cycles

DURING SCHEDULED 6Y CHECK, FOUND EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 22,068 hrs · 12,932 cycles

DURING SCHEDULED 6Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 22,068 hrs · 12,932 cycles

DURING SCHEDULED 6Y CHECK, FOUND EEPLS CRACKED AT BS 358. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 22,068 hrs · 12,932 cycles

DURING SCHEDULED 6Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.70. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,688 hrs · 12,698 cycles

DURING SCHEDULED HC1 CHECK, FOUND AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 21,339 hrs · 12,494 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS BROKEN AT ROW 9. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 20,809 hrs · 12,168 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,175 hrs · 11,148 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 17,992 hrs · 10,427 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS STRIP LIGHT BROKEN. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,707 hrs · 10,253 cycles

FWD EEPLS LIGHT INOP. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,303 hrs · 10,016 cycles

DURING SCHEDULED HC1 CHECK, RT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 17,303 hrs · 10,016 cycles

DURING SCHEDULED HC1 CHECK, LT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 17,091 hrs · 9,903 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. RE-INSTALLED SLIDE PER MT.

Part: SLIDE — LOOSE (CABIN) · airframe 16,346 hrs · 9,470 cycles

FOUND L2 DOOR SLIDE FLAPPER HANGING. SECURED SLIDE PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 14,816 hrs · 8,559 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 15,387 hrs · 8,847 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 14,149 hrs · 8,128 cycles

EEPLS LENS LOOSE AT ROW 23 ABC. SECURED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 12,891 hrs · 7,370 cycles

EEPLS LIGHT ASSY LOOSE AT ROW 5 ABC. SECURED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (ROW 1 ABC) · airframe 12,891 hrs · 7,370 cycles

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

Part: LENS — MISSING (CABIN) · airframe 12,881 hrs · 7,362 cycles

EEPLS LIGHT LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 11,299 hrs · 6,404 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 10,560 hrs · 5,952 cycles

EEPLS SECTION OUT OF RECEPTACLE AT FWD END. REINSTALLED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 10,547 hrs · 5,944 cycles

EEPLS LOOSE AT FWD END. SECURED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 2,019 hrs · 1,164 cycles

FOUND LT FWD CABIN EEPLS TRACK LOOSE. SECURED EEPLS IAW MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 3,808 hrs · 2,147 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.