N8642E

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CRACKED SUPPORT ANGLE, BS 500I, STR 28L REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A7902, SHEET 320, REV-.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CRACK SUPPORT ANGLE, BS 500I, STR 28R IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE, AND FASTENERS IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET 320, REV-.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 38,126 hrs · 18,579 cycles

CRACKED ACCESS PANEL 551GB T/E LT WING. REPAIRED THE ACCESS PANEL 551GB IAW SRM 51-70-05-2R-10, REPAIR 10.

Part: LENS — BROKEN (ZONE 200) · airframe 38,126 hrs · 18,579 cycles

BROKEN LENS OF EMERGENCY LIGHT, STRONGHBACK ROW 24-25 RT SIDE. REPLACED THE LENS IAW AMM 33-51-03-960-803, STEP 4.D, ITEM (1) & (2).

Part: WEB — CRACKED (ZONE 600) · airframe 38,126 hrs · 18,579 cycles

CRACKED WEB, ORSS 271 RT WING T/E. REPLACED THE WEB IAW SRM 51-10-02, STEP 9, SRM 51-40-02-0G-0, & DWG 115A2512, SHEET 16, REV-.

Part: SUPPORT — DAMAGED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

ELONGATED HOLES ON SUPPORT ZEE BTW BS 727C - 747, RBL 21 IN THE AFT CARGO BAY. TOOK INITIAL MEASUREMENTS OF HOLES ON THE SUPPORT ZEE, HOLE NR 1: D=0.246, HOLE NR 2: D=0.247, HOLE NR 3: D=0.246. REAMED HOLE NR 1: D=250, HOLE NR 2: D=0.250, HOLE NR 3: D=0.250. FOUND WITHIN TOLERANCE IAW SRM 51-40-05-0G-0, TABLE A, FIGURE 4, SHEET 2, & DWG 146A7502, SHEET 54, REV -.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CORRODED WEB - INTERCOSTAL BS 747 - 767, RBL 21, WL 155 IN THE AFT CARGO BAY. REPLACED THE WEB - INTERCOSTAL IAW SRM 51-10-02, ITEM 9, AND DWG 146A7500, SHEET 236, REV-.

Part: SHIELD — CORRODED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CORRODED SHIELD WEB, BTW BS 767 - 794.3, RBL 21, WL 155 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB IAW SRM 51-40-02, & DWG 146A0081, SHEET 49, REV A.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CRACKED SUPPORT ANGLE, BS 867, S26 - 27L. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 149A8102, SHEET 19, REV A.

Part: CROSSBEAM — CRACKED (ZN 200 FUS TOP) · airframe 38,126 hrs · 18,579 cycles

CRACKED CROSSBEAM, BS 540, BL 0 - LBL 24.75. REPLACED CROSSBEAM IAW SRM 51-40-02, AND DWG 143A0060, SHEET 64, REV-.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 38,126 hrs · 18,579 cycles

CRACKED PAX CABIN FLOOR SUPPORT BTW BS 380 - 400, LBL 51. REPLACED THE FLOOR SUPPORT & FASTENERS IAW SRM 51-40-02-0G, SRM 51-10-02 PARAGRAPH 9, & DWG 143A5400, SHEET 183, REV -.

Part: ANGLE — CORRODED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CORRODED ANGLE, BS 986.5 + 10, RBL 42, WL 208.1. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02, DWG 147A5700, SHEET 123, REV A, SRM 51-10-02, STEP 9 ITEM A.

Part: ANGLE — CRACKED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CRACKED ANGLE, BS 500G, RBL 21 AFT SIDE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02-0G-0, ITEM 9, & DWG 143A7505, SHEET 137, 138, & 139, REV-.

Part: ANGLE — CRACKED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CRACKED ANGLE, BS 500G, RBL 21, IN THE CARGO BAY. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 137, REV-.

Part: ANGLE — CRACKED (ZONE 200) · airframe 38,126 hrs · 18,579 cycles

CRACKED ANGLE, BS 500H, LBL 21 IN THE FWD CARGO BAY. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02, DWG 143A7505, SHEET 138, REV -.

Part: ANGLE — CRACKED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CRACKED ANGLE, BS 400, LBL 21, IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 143A7505,SHEET 137, REV-.

Part: GUSSET ANGLE — CRACKED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CRACKED GUSSET ANGLE, BS 500I, S19R. REPLACED THE GUSSET & FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 143A7902, SHEET 256, REV B.

Part: ANGLE — CRACKED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CRACKED ANGLE, BS 440, LBL 21. IN THE CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 138, REV -.

Part: ANGLE — CRACKED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CRACKED ANGLE, BS 500H, RBL 21 AFT SIDE IN THEFWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02-0G, SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 137, REV-.

Part: ANGLE — CRACKED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CRACKED ANGLE, BS 500H, RBL 21 FWD SIDE IN THE FWD CARGO BAY. REPLACED THE ANGLE & FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 137, REV-.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CRACKED SCUFF PLATE AFT CORNER IN THE FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS 2 & 4 - 7.

Part: STRAP — CORRODED (ZONE 100) · airframe 38,126 hrs · 18,579 cycles

CORRODED FLOOR STRAP, AFT POSITION BULKHEAD IN THE FWD CARGO BAY. REPLACED THE FLOOR STRAP IAW SRM 51-40-02-0G-0.

Part: SLIDE — OUT OF POSITION (ZONE 800) · airframe 36,424 hrs · 17,705 cycles

PULL HANDLE EXPOSED ON AFT SERVICE DOOR SLIDE<[01] FOUND VELCRO PULL HANDLE COVER TUCKED UP IN SLIDE COVER ;PULLED DOWN AND PUT INTO PLACE PER SIP

Part: SLIDE — DISLODGED (ZONE 800) · airframe 35,784 hrs · 17,358 cycles

R2 DOOR SLIDE FELL OUT OF COVER. REINSTALLED SLIDE IAW AMM 25-66-00 AND TASK CARD 725-61-06

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 35,699 hrs · 17,315 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1673 FAILS TO CHARGE<[01] REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR>WN50318;[02] VERIFIED C/W

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 35,699 hrs · 17,315 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1694 FAILS TO CHARGE<[01] REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR><BR>WN50316;[02] VERIFIED C/W

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 35,699 hrs · 17,315 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1671 FAILS TO CHARGE<[01] REMOVED & REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.<BR><BR>WN50317;[02] VERIFIED C/W

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 35,699 hrs · 17,315 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1695 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY IAW AMM 33-51-06-960-805.<BR>OPS CHECK GOOD.;[02] WN50315;[03] VERIFIED C/W

Part: BRACKET — CRACKED (ZONE 400) · airframe 35,699 hrs · 17,315 cycles

040-001 BRACKET ON AFT SIDE OF # 1 ENGINE O/B COWL IS WORN AND CRACKED. HAS STREAMER ATTACHED.<[01] REMOVED WORN AND CRACKED BRACKET ON AFT SIDE OF #1 ENG O/B COWL AND REPLACED WITH NEW BRACKET; PN 314-2264-7 ATAG A307566; IAW SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED ITEM 1<BR>C/W

Part: HANDLE — LOOSE (ZONE 800) · airframe 35,699 hrs · 17,315 cycles

R2 DOOR LINER ASSIST HANDLE IS LOOSE<[01] RESECURED R2 DOOR LINER ASSIST HANDLE IAW AMM-52-41-31-400-802 PG 3 STEP F ITEM 2;[02] VERIFIED ITEM 1<BR>C/W

Part: HANDLE — LOOSE (ZONE 800) · airframe 35,699 hrs · 17,315 cycles

R1 DOOR LINER ASSIST HANDLE IS LOOSE<[01] RESECURED R1 DOOR LINER ASSIST HANDLE IAW AMM-52-41-31-400-802 PG 3 STEP F ITEM 2;[02] VERIFIED ITEM 1<BR>C/W

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 35,630 hrs · 17,281 cycles

L1 DOOR EMERGENCY SLIDE AFT GIRL BAR HOLDER LOOSE <[01]. REPLACED FWD L1 DOOR SLIDE AFT GIRT BAR HOLDER FWD RIVET PER SIP. REF AMM 25-66-01. OK FOR SVC.

Part: LENS — BROKEN (ZONE 200) · airframe 34,131 hrs · 16,448 cycles

OVERHEAD EMERGENCY LIGHT LENS COVER 4-5 ABC BROKE<[01] 05 - OK TO CONTINUE PER [MEL 33-15-02;INTERIOR EMERGENCY EXIT LIGHTING SYSTEM - EMERGENCY AISLE LIGHTS]. REPLACED LENS ON OVERHEAD EMERGENCY LIGHT 4-5 ABC. OP CHECKS GOOD IAW SIP

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 34,119 hrs · 16,441 cycles

LEFT AFT OVER WING EXIT EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED M1670 EMERGENCY LIGHT BATTERY PER AMM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 33,548 hrs · 16,123 cycles

THE FOLLOWING EXTERNAL EMERGENCY EXIT LIGHTS ARE INOP: LH OWE AFT; RH OWE AFT; L2 DOOR; RH AFT FUSELAGE; LH AFT FUSELAGE.<[01] REMOVED BATTERY PACKS M1670; M1671 AND M1673 BATTERY PACKS; REPLACED WITH SERVICEABLE UNITS AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805.;[02] JOB COMPLETE.

Part: SKIN — DELAMINATED (ZONE 600) · airframe 33,548 hrs · 16,124 cycles

R/H O/B AFT FLAP DELAMINATED ON I/B END<[01] REMOVED; REPLACED; AND ADJUSTED R/H O/B AFT FLAP PER AMM 27-51-22.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-5.

Part: RIB — CRACKED (ZN 100 FUS LOWER) · airframe 33,548 hrs · 16,124 cycles

BODY RIB CRACKED ON RH A/C BAY AT BS 540+18; RBL37.WL136(APPROX.)<[01] 'REPAIRED PER EA 24-157-01843 WITH AN INSPECTION THRESHOLD DEFINED IN 24-157-01843-DTI1 AND 24-157-01843-DTI2.';[02] VERIFIED CORRECTIVE ACTION #1

Part: SHIELD — CRACKED (ZONE 400) · airframe 33,548 hrs · 16,124 cycles

#1 ENGINE I/B FAN COWL OIL TANK ACCESS DOOR SHIELD CRACKED<[01] REMOVED AND REPLACED ACCESS DOOR SHIELD IAW SRM 51-40-02.;[02] PARTS REMOVED / INSTALLED;[03] REJECTION OF CORRECTIVE ACTION 1 AND STEP 1: 1EA BAD RIVET AT LOWER END OF #1 ENGINE I/B FAN COWL OIL TANK ACCESS DOOR SHIELD. SEE TTG8Q00UH35J

Part: SUPPORT — CRACKED (ZONE 100) · airframe 33,548 hrs · 16,124 cycles

PANEL BREAK AT BS 540 LBL 2 IS CRACKED<[01] REMOVED CRACKED PANEL BREAK AT BS 540 LBL 2 IAW SRM 51-40-02-0G-0.<BR>OBTAINED AND INSTALLED NEW PANEL BREAK AT BS 540 LBL 2 IAW SRM 51-40-02-0G-0 AND DRW 143A0060;[02] UPDATED MEASUREMENTS;[03] VERIFIED CORRECTIVE ACTION #1

Part: SUPPORT — CRACKED (ZONE 100) · airframe 33,548 hrs · 16,124 cycles

PANEL BREAK AT BS 540 RBL 2 IS CRACKED<[01] REMOVED AND REPLACED PANEL BREAK PER SRM 51-40-02-0G-0 AND DWG 143A0060;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] CARD COMPLETE

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 32,145 hrs · 15,343 cycles

LEFT OUTBOARD AFT FLAP INBOARD SIDE UPPER AND LOWER SURFACE DELAMINATED.<[01] REMOVED AND REPLACED LEFT OUTBOARD AFT FLAP REF AMM 27-51-11. REQUIRES OPS CHECK.;[02] REMOVED AND REPLACED LEFT OB AFT FLAP REF AMM 27-51-22-400-801; THRU STEP F.(5)(G). OB AFT FLAP ADJUSTMENT REQUIRED.;[03] COMPLIED WITH FLAP ADJUSTMENT IAW AMM 27-51-26

Part: LIGHT — DAMAGED (ZN 200 FUS TOP) · airframe 31,697 hrs · 15,091 cycles

PHOTO ILLUMINATION STRIP AT ROW 1 FED DAMAGED<[01] OK TO CONTINUE PER MEL 33-19-01; SP #1;[02] REPLACED PHOTO ILLUMINATION STRIP AT ROW 1DEF PER AMM 33-51-15. MEL CLEARED.

Part: MEGAPHONE — INOPERATIVE (ZN 200 FUS TOP) · airframe 31,595 hrs · 15,035 cycles

FWD MEGAPHONE IS INOP.<[01] REMOVED AND REPLACED FWD MEGAPHONE PER AMM 25-64-00. OPS CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 31,074 hrs · 14,735 cycles

L/H FWD EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY AT L/H FWD CEILING AND BATTERY PACK AT 8 ABC AIR GRILLE LOCATIONS; PER AMM 33-51-06. EMERGENCY EXIT LIGHTS OP?S CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (ZN 200 FUS TOP) · airframe 31,074 hrs · 14,735 cycles

L/H FWD EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY AT L/H FWD CEILING AND BATTERY PACK AT 8 ABC AIR GRILLE LOCATIONS; PER AMM 33-51-06. EMERGENCY EXIT LIGHTS OP?S CHECK GOOD.

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 30,651 hrs · 14,485 cycles

CREW REPORTS FWD SLIDE L1 DOOR FELL OUT OF CONTAINER<[01] REINSTALLED L1 DOOR SLIDE PER MT 725-61-06

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 30,470 hrs · 14,377 cycles

RIGHT FWD ISLE EMERGENCY LIGHTS IN-OP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT M2335 LOCATION PER AMM 33-51-06. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 30,382 hrs · 14,327 cycles

RH OVER WING EMERGENCY LIGHT INOP<[01] RELAMPED RH OVER WING EMERGENCY LIGHT PER AMM 33-51-04

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 29,758 hrs · 13,971 cycles

ALL INTERIOR AND EXTERIOR EMERGENCY LIGHTS AT R2 DOOR INOP<[01] R/R AFT R/H BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.

Part: ACM — DEFECTIVE (LEFT) · airframe 28,527 hrs · 13,284 cycles

AT CRUISE F/A HEARD A BANG NOISE MID CABIN. COCKPIT AND CABIN THEN SMELLED FAINT SMELL OF SMOKE. RUN QRH; SMELL IMMEDIATELY CLEARED OUT.<[01] PERFORMED CONDITIONAL INSPECTION FOR SMOKE IN CABIN PER AMM 05-51-56. DETERMINED CAUSE OF SMOKE & ODOR TO BE A DEFECTIVE LT PACK ACM. ACM REPLACED PER AMM 21-51-04. REFER TO LOGPAGE #2101069 FOR CORRECTIVE ACTION & PARTS REPLACEMENT.

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 27,092 hrs · 12,498 cycles

EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M2816 ARE INOP. / [01] REMOVED NON-OPERATIONAL BATTERY PACK; INSTALLED AND PERFORMED GOOD INSTALLATION TEST OF NEW BATTERY PACK PER AMM 33-51-06-960-805.;[02] VERIFIED WORK ACCOMPLISHED AS NOTED IN ACTION ITEM 1.;[03] VERIFIED CORRECTIVE ACTIONS #1 AND #2

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 27,092 hrs · 12,498 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1675 ATE INOP<[01] REMOVED AND REPLACED M675 BATTERY PACK PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1;[03] PERFORMED GOOD TEST OF NEW BATTERY PACK PER AMM 33-51-06-960-805 STEPS 4.E.6.A-C.;[04] VERIFIED WORK ACCOMPLISHED AS NOTED IN ACTION ITEM 3

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 27,092 hrs · 12,498 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1672 ARE INOP<[01] REMOVED AND REPLACED M1672 BATTERY PACK PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1;[03] PERFORMED GOOD TEST OF NEW BATTER PACK PER AMM 33-51-06-960-805 STEPS 4.E.6.A-C.;[04] VERIFIED WORK ACCOMPLISHED AS NOTED IN ACTION ITEM 3.;[05] VERIFIED CORRECTIVE ACTION #3

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 27,092 hrs · 12,498 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATYERY PACK M1676 ARE INOP<[01] REMOVED AND REPLACED M1676 BATTERY PACK PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION #1;[03] PERFORMED GOOD TEST OF NEW BATTER PACK PER AMM 33-51-06-960-805 STEPS 4.E.6.A-C.;[04] VERIFIED WORK ACCOMPLISHED AS NOTED IN ACTION ITEM 3;[05] VERIFIED CORRECTIVE ACTION #3

Part: FLASHLIGHT ASSY — BROKEN (AFT CABIN) · airframe 27,092 hrs · 12,498 cycles

FLASHLIGHT BRACKET BROKEN AT AFT R/H ATTENDANCE SEAT OUTBOARD POSITION / [01] REPLACED FLASHLIGHT ASSY PER AMM 25-64-00-200-802 STEPS (4); (6); (7);[02] REPLACED FLASHLIGHT BRACKET ASSY PER AMM 25-64-00-200-802 SEC 10 B STEPS (3); (4); (6); (7) & AMM SWAD633A101-SWA SEC 2;[03] EDIT ITEM 1 AMM REFERENCE TO READ AMM 25-64-00-200-802; STEP 10. B.(4); (6); AND (7).

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,092 hrs · 12,498 cycles

CRACKED INTERCOSTAL STA 344-360; RBL 13; WL 208. / [01] REMOVED INTERCOSTAL STA 344-360; BL0; WL 200-208 FOR ACCESS PER SRM 51-40-02-0G-0.;[02] REMOVED DAMAGED INTERCOSTAL STA 344-360; RBL 13; WL 208 PER SRM 51-40-02-0G-0.;[03] LOCATED AND DRILLED AND DEBURRED NEW INTERCOSTAL STA 344-360; RBL 13; WL 200-208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0. OK TO INSTALL BOTH INTERCOSTALS; AT 344-360 AT BL0; RBL 13.;[04] VERIFIED CORRECTIVE ACTION 3.;[05] VERIFIED MEASUREMENT TABLE;[06] INSTALLED A NEW INTERCOSTAL AT BS 344-360 RBL13 WL208 IAW SRM 51-40-02; AND BOEING DWG 141A5400. ALSO; REINSTALLED INTERCOSTAL FOR ACCESS AT BS 344-360 BL0 WL208 IAW SRM 51-40-02 AND BOEING DWG 141A5400.;[07] VERIFIED CORRECTIVE ACTION #6;[08] VERIFIED CORRECTIVE ACTION #6

Part: INTERCOSTAL — CRACKED · airframe 27,092 hrs · 12,498 cycles

CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 50; WL 208. / [01] UPON FURTHER INVESTIGATION PART WILL BE REPLACEMENT IAW SRM 51-10-02 STEP 9. REMOVED CRACKED UPPER ATTACH ANGLE AT BS 380-400 LBL50 WL208 IAW SRM 51-40-02. RECEIVED A NEW UPPER ATTACH ANGLE PO# 876805 LOCATED FASTENERS HOLES; DRILLED; DEBURRED; AND INSTALLED AT BS 380-400 LBL50 WL208 IAW SRM 51-40-05; SRM 51-40-02; AND BOEING DWG 143A5400.;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE;[03] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE

Part: FLOOR SKIN — CRACKED (L1 DOOR) · airframe 27,092 hrs · 12,498 cycles

FWD ENTRY MOPSILL IS CRACKED COMMON TO 303 FRAME ON VERTICAL FLANGE LBL 54; WL 209. / [01] NOT ALLOWABLE LIMITS FOUND ON SRM FOR CRACK ON BS303 FED MOPSILL LBL54 WL209 REPLACEMENT OF THE PART IS APPLICABLE PER SRM 51-10-02-0G-0 PAR. 9.C;[02] REMOVE FED MOPSILL I.A.W SRM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW FED MOPSILL I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 140A9810 OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION 3. OK TO INSTALL THE FED MOP SILL.;[05] VERIFIED MEASUREMENT TABLE.;[06] INSTALLED NEW FED MOPSILL BS270-BS356 WL209 LBL54 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 140A9810 COMPLETED ALL REMOVED AND REPLACED TASK;[07] VERIFIED ITEM 6 CORRECTIVE ACTIONS.;[08] VERIFIED MEASUREMENTS

Part: INTERCOSTAL — CRACKED · airframe 27,092 hrs · 12,498 cycles

CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; RBL 9; WL 208. / [01] UPON FURTHER INVESTIGATION PART WILL BE REPLACEMENT IAW SRM 51-10-02 STEP 9. REMOVED CRACKED UPPER ATTACH ANGLE AT BS 380-400 LBL1 WL208 IAW SRM 51-40-02. RECEIVED A NEW UPPER ATTACH ANGEL PO#876312; LOCATED FASTENERS HOLES; DRILLED; DEBURRED; AND INSTALLED AT BS 380-400 LBL1 WL208 IAW SRM 51-40-05; SRM 51-40-02; AND BOEING DWG 143A5400;[02] VERIFIED CORRECTIVE ACTION #1; MEASUREMENT FIELD VERIFIED;[03] VERIFIED CORRECTIVE ACTION #1; MEASUREMENT FIELD VERIFIED

Part: INTERCOSTAL — CRACKED · airframe 27,092 hrs · 12,498 cycles

CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 1; WL 208. / [01] UPON FURTHER INVESTIGATION PART WILL BE REPLACEMENT IAW SRM 51-10-02 STEP 9. REMOVED CRACKED UPPER ATTACH ANGLE AT BS 380-400 LBL1 WL208 IAW SRM 51-40-02. RECEIVED A NEW UPPER ATTACH ANGEL PO#876312; LOCATED FASTENERS HOLES; DRILLED; DEBURRED; AND INSTALLED AT BS 380-400 LBL1 WL208 IAW SRM 51-40-05; SRM 51-40-02; AND BOEING DWG 143A5400;[02] VERIFIED CORRECTIVE ACTION #1; MEASUREMENT FIELD VERIFIED;[03] VERIFIED CORRECTIVE ACTION #1; MEASUREMENT FIELD VERIFIED

Part: INTERCOSTAL — CRACKED · airframe 27,092 hrs · 12,498 cycles

CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; RBL 41; WL 208. / [01] UPON FURTHER INVESTIGATION PART WILL BE REPLACEMENT IAW SRM 51-10-02 STEP 9. REMOVED CRACKED UPPER ATTACH ANGLE AT BS 380-400 RBL41 WL208 IAW SRM 51-40-02. RECEIVED A NEW UPPER ATTACH ANGLE PO# 876805 LOCATED FASTENERS HOLES; DRILLED; DEBURRED; AND INSTALLED AT BS 380-400 RBL41 WL208 IAW SRM 51-40-05; SRM 51-40-02; AND BOEING DWG 143A5400.;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE;[03] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,092 hrs · 12,498 cycles

CORROSION ON FWD SERVICE DOOR MOPSILL SCUFFPLATE ATTACH ANGLE STA 302-326; RBL 57- RBL 59; WL 209. / [01] REMOVED NUT PLATES COMMON TO FWD SERVICE DOOR MOP SILL SCUFF PLATE ATTACH ANGLE IAW SRM 51-40-02-0G-0 BLENDED CORROSION FROM ATTACH ANGLE IN SEVERAL SPOTS BS 302 TO 326 RBL 57 -59 WL 209 1' X 1' MAX REMOVED .012 FROM ORIGINAL .090 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-2 STEP 4.A FIG 102 USING DIAL INDICATOR ATS2678 S/N UNKNOWN CAL DUE 04/2023;[02] VERIFIED CORRECTIVE ACTION ITEM 1;[03] REMOVED CORRODED FWD SERVICE DOOR MOP SILL SCUFF PLATE ATTACH ANGLE AT BS 302-326 RBL 57 WL 209 IAW SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED AND COUNTERSUNK AND DEBURRED NEW FWD SERVICE DOOR MOPSILL SCUFFPLATE ATTACH ANGLE STA 302-326; RBL 57-RBL 59; WL 209 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0. OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION 4.;[06] VERIFIED MEASUREMENT TABLE.;[07] INSTALLED NEW FWD SERVICE DOOR MOPSILL SCUFFPLATE ATTACH ANGLE STA 302-326; RBL 57-RBL 59; WL 209 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A8310 COMPLETED ALL REMOVED AND REPLACED TASK;[08] VERIFIED ITEM 7 CORRECTIVE ACTIONS.;[09] VERIFIED MEASUREMENTS.;[10] CHANGED MAJOR TO MINOR IN TABLE;[11] CHANGED MAJOR TO MINOR IN TABLE

Part: INTERCOSTAL — CRACKED · airframe 27,092 hrs · 12,498 cycles

CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 13; WL 208. / [01] UPON FURTHER INVESTIGATION PART WILL BE REPLACEMENT IAW SRM 51-10-02 STEP 9. REMOVED CRACKED UPPER ATTACH ANGLE AT BS 380-400 LBL13 WL208 IAW SRM 51-40-02. RECEIVED A NEW UPPER ATTACH ANGLE PO# 876805 LOCATED FASTENERS HOLES; DRILLED; DEBURRED; AND INSTALLED AT BS 380-400 LBL13 WL208 IAW SRM 51-40-05; SRM 51-40-02; AND BOEING DWG 143A5400.;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE;[03] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT TABLE

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,092 hrs · 12,498 cycles

FWD PASSENGER CABIN CRACKED FRAME AT BS312 11' BELOW S-4L WL283. MARKED. / [01] NDT HFEC SURFACE INSPECTED AREA PER 737 NDTM PART 6 51-00-00 PROC 23; CRACK NOTED AND MARKED ENDS.<BR>EQUIP ID. NORTEC 500D S/N IS000681 DUE 02/23;[02] REMOVED CRACK IN FRAME IN FWD CABIN STA 312; 11' BELOW STR 4L; WL 283. AREA REMOVED IS .300' BY .200' ON ENDV OF FRAME PER SRM 51-10-02-0G-0.;[03] VISUALLY INSPECTED BLEND AREA- NO CRACK NOTED VISUALLY.;[04] CORRECTED DIMENSION IN TABLE;[05] NDT HFEC SURFACE INSPECTED AREA PER 737 NDTM PART 6 51-00-00 PROC 23; NO CRACK NOTED.<BR>EQUIP ID. NORTEC 500D IS000681 DUE 02/23;[06] PERFORMED .040' INSURANCE CUT ON 312 FRAME CUTOUT PER SRM 51-10-02-0G-0.;[07] PERFORMED .040' INSURANCE CUT ON 312 FRAME CUTOUT TRIMMED EDGES PER SRM 51-10-02-0G-0.;[08] EDITED TABLE;[09] ADDED TRIMMED EDGES TO STATEMENT;[10] VERIFIED CORRECTIVE ACTION 7 AND MEASUREMENT TABLE.;[11] REPAIRED DAMAGE ON FWD PASSENGER CABIN CRACKED FRAME AT BS312 11' BELOW S-4L WL283 PER EA 22-153-02216.;[12] VERIFIED CORRECTIVE ACTION #11

Part: SUPPORT — CORRODED (AFT FUSELAGE) · airframe 27,092 hrs · 12,498 cycles

CORROSION ON FLOOR SUPPORT STA 949; LBL 52; WL 208; UPPER SURFACE. / [01] NO LIMITS FOUND ON SRM FOR SPECIFIC DAMAGE SRM 51-10-02-0G-0 PAR 9.C REPLACEMENT OF THE PART IS APPLICABLE;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT FIELD;[03] REMOVED DAMAGED FLOOR SUPPORT STA 947-986; LBL 52; WL 208 PER SRM 51-40-02-0G-0.;[04] REMOVED FLOOR SUPPROT STA 950; LBL 25-LBL 52; WL 208 FOR ACCESS PER SRM 51-40-02-0G-0.;[05] REMOVED DAMAGED FLOOR SUPPORT STA 947-967; LBL 52; WL 208 PER SRM 51-40-02-0G-0.;[06] CORRECTED BODY STATION 947-967.;[07] LOCATED AND DRILLED NEW FLOOR SUPPORT BS947-BS967 LBL52 WL208 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 147A5650. OK TO INSTALL;[08] VERIFIED CORRECTIVE ACTION 7. OK TO INSTALL FLOOR UPPORT.;[09] INSTALLED FLOOR SUPPORT BS947-BS967 LBL52 WL208 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 147A5650.;[10] VERIFIED CORRECTIVE ACTION #9 AND STEP 1;[11] UPDATED PARTS USED INFO.;[12] VERIFIED CORRECTIVE ACTION #9 AND STEP 1

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 27,092 hrs · 12,498 cycles

CORROSION ON FLOOR SUPPORT STA 949; RBL 23.5; WL 208; UPPER SURFACE. / [01] NO LIMITS FOUND ON SRM FOR SPECIFIC DAMAGE SRM 51-10-02-0G-0 PAR 9.C REPLACEMENT OF THE PART IS APPLICABLE;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT FIELD;[03] REMOVED FLOOR SUPPORT BS947-BS967 RBL24 WL208 I.A.W SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW FLOOR SUPPORT BS947-BS967 RBL24 WL208 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 147A5650. OK TO INSTALL;[05] VERIFIED CORRECTIVE BACTION 4 AND MEASUREMENT TABLE.;[06] INSTALLED FLOOR SUPPORT BS947-BS967 RBL24 WL208 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 147A5650.;[07] VERIFIED CORRECTIVE ACTION #6 AND STEP 1;[08] VERIFIED CORRECTIVE ACTION #6 AND STEP 1

Part: ANGLE — CORRODED · airframe 27,092 hrs · 12,498 cycles

G4B R/H STRAP BACKSIDE BOTTOM HAS CORROSION / [01] G4B R/H STRAP CONNECTOR ANGLE HAS NO LIMITS ON CORROSION; OUT OF LIMITS AND SRM 51-10-02-0G-0 IS APPLICABLE REPLACEMENT OF PART.;[02] REMOVED AND REPLACED G4B R/H STRAP CONNECTOR ANGLE PER SOPM 20-50-01.;[03] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 2. VERIFIED MEASUREMENT FIELDS ARE ACCURATE & COMPLETE.

Part: SUPPORT — CORRODED (AFT FUSELAGE) · airframe 27,092 hrs · 12,498 cycles

CORROSION ON FLOOR SUPPORT STA 949; LBL 25; WL 208; UPPER SURFACE. / [01] NO LIMITS FOUND ON SRM FOR SPECIFIC DAMAGE SRM 51-10-02-0G-0 PAR 9.C REPLACEMENT OF THE PART IS APPLICABLE;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT FIELD;[03] REMOVED FLOOR SUPPORT BS947-BS967 LBL25 WL208 I.A.W SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW FLOOR SUPPORT BS947-BS967 LBL25 WL208 I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 147A5650. OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 4. OK TO INSTALL FLOOR SUPPORT.;[06] INSTALLED NEW FLOOR SUPPORT BS 947-967 LBL25 WL 208 PER SRM 51-40-02-0G-0;[07] CORRECTED STEP 1;[08] CERTIFIED CORRECTION;[09] VERIFIED CORRECTIVE ACTION #6 AND STEP 1;[10] VERIFIED CORRECTIVE ACTION #6 AND STEP 1

Part: SPLICE STRAP — CORRODED (AFT CARGO) · airframe 27,092 hrs · 12,498 cycles

AFT CARGO BAY CARGO FLOOR SPLICE STRAP HAS CORROSION BS727I +6 RBL20 WL156 / [01] EVALUATED CORROSION ON FLOOR SPLICE STRAP BS 727I+6 RBL 20 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 ACTION #1;[03] RECEIVED NEW AFT CARGO BAY CARGO FLOOR SPLICE STRAP BS727I +6 RBL20 WL156 ON PO # 833679 INSTALL WELL BE ON CARD # TTG8Q00CX314;[04] VERIFIED CORRECTIVE ACTION #3

Part: SPLICE STRAP — CORRODED (AFT CARGO) · airframe 27,092 hrs · 12,498 cycles

AFT CARGO BAY CARGO FLOOR SPLICE STRAP HAS CORROSION BS767+6 RBL20 WL156 / [01] EVALUATED CORROSION ON FLOOR SPLICE STRAP BS 767+6 RBL 20 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 ACTION #1;[03] RECEIVED NEW AFT CARGO BAY CARGO FLOOR SPLICE STRAP BS767+6 RBL20 WL156 ON PO # 835775 INSTALL WELL BE ON CARD # TTG8Q00CX310;[04] VERIFIED CORRECTIVE ACTION #3

Part: BRACKET — BROKEN (AFT CARGO) · airframe 27,092 hrs · 12,498 cycles

AFT CARGO BAY LAV TANK BULKHEAD LOWER BRACKET BROKEN BS867 LBL10 WL166 / [01] REMOVED AND REPLACED ACB LAV TANK BULKHEAD LOWER BRACKET BS 867; LBL 10; WL 166 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG# 149A8104; DWG#149A8102.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] VERIFIED COMPLETE

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 27,092 hrs · 12,498 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION BS727F TO BS767 RBL21 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS ON FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 727I+10 RBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN NUMEROUS 1'X1' AREAS; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATD 2678 DUE 04/2023;[02] VERIFIED ACTION #1;[03] VALIDATED APPLICABILITY OF SRM 53-00-53-2R-5;[04] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS727E +12' - BS767; RBL21; WL156 PER SRM 51-40-02-0G-0; SRM 53-00-53-2R-5;[05] FABRICATED; LOCATED AND APPLIED CHEMICAL CONVERSION COATING TO ACB FLOOR TO SIDEWALL SUPPORT AT BS727E +12' - BS767; RBL21; WL156 AND SPLICE REPAIR AT BS727E+7' - BS727E+17' USING BAC1496-377#7075T62 LOT # 1494598-1 PER SRM 51-40-05-0G AND DWG 146A7500; SRM 53-00-53-2R-5; AMM 51-21-41-370-802;[06] VERIFIED CORRECTIVE ACTION #5<BR>VERIFIED MEASUREMENTS;[07] APPLIED PRIMER TO FLOOR TO SIDEWALL SUPPORT PER SRM 53-00-53-2R-5; AMM 51-21-72-370-804;[08] OK TO INSTALL REPAIR PARTS;[09] VERIFIED CORRECTIVE ACTION 7 AND 8; OK TO INSTALL;[10] INSTALLED NEW ACB FLOOR TO SIDEWALL SUPPORT AT BS727E +12' - BS767; RBL21; WL156 AND SPLICE REPAIR AT BS727E+7' - BS727E+17' PER SRM 51-40-02-0G AND DWG 146A7500; SRM 53-00-53-2R-5;[11] VERIFIED CORRECTIVE ACTION #10;[12] VERIFIED CORRECTIVE ACTION #10

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 27,092 hrs · 12,498 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION BS747 TO BS847 LBL21 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS ON FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 747+10 LBL 21 WL 21; FOUND 0.015 REMOVED FROM ORIG 0.040 IN NUMEROUS 1'X1' AREAS; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATD 2678 DUE 04/2023;[02] CORRECTION TO STEP 1; WL IS 156;[03] VERIFIED ACTION #1;2;[04] VALIDATED APPLICABILITY OF SRM 53-00-53-2R-5;[05] REMOVED DAMAGED PART OF THE ACB L/H FLOOR TO SIDEWALL SUPPORT BS727J+10 TO BS847; LBL21; WL156. PER SRM 53-00-53-2R-5 STEP 4. B & C.;[06] FABRICATED ACB L/H FLOOR TO SIDEWALL SUPPORT AND ALL REPAIR PARTS BS727J+10 TO BS847; LBL21; WL156. PER DWG 146A7500 AND SRM 53-00-53-2R-5 STEPS 4. D. THRU H. FROM BAC1496-377#7075T62 EXT. CLAD LOT#1494598-1. SLICE LOCATION BS727J+10.;[07] VERIFIED CORRECTIVE ACTION #5; 6<BR>VERIFIED MEASUREMENTS;[08] APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO ACB FABRICATED L/H FLOOR TO SIDEWALL SUPPORT AND ALL REPAIR PARTS PER SRM 53-00-53-2R-5 STEP 4. I. AND J. OK TO INSTALL.;[09] VERIFIED CORRECTIVE ACTION #8;[10] INSTALLED FABRICATED ACB L/H FLOOR TO SIDEWALL SUPPORT AND ALL REPAIR PARTS BS727J+10 TO BS847; LBL21; WL156. PER DWG 146A7500 AND SRM 53-00-53-2R-5 STEPS 4. K THRU N.;[11] VERIFIED CORRECTIVE ACTION #10

Part: SHIELD — CORRODED (AFT CARGO) · airframe 27,092 hrs · 12,498 cycles

AFT CARGO BAY SHIELD FWD OF CARGO DOOR HAS AREAS OF CORROSION BS767 TO BS787 RBL21 WL156 / [01] EVALUATED CORROSION ON SHIELD BS 767 TO BS 787 RBL 21 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 ACTION #1;[03] REMOVED ACB SHIELD BS767 TO BS793 RBL21 WL156 PER SRM 51-40-02-0G-0.;[04] LOCATED; DRILLED AND DEBURRED NEW SHIELD BS767 TO BS793 RBL21 WL156 PER SRM 51-40-05-0G-0. AND DWG 146A0081.;[05] VERIFIED CORRECTIVE ACTION 4;[06] OK TO INSTALL NEW SHIELD.;[07] OK TO INSTALL NEW SHIELD.;[08] INSTALLED NEW SHIELD BS767 TO BS793 RBL21 WL156 PER SRM 51-40-02-0G-0. AND DWG 146A0081.;[09] VERIFIED CORRECTIVE ACTOIN 8;[10] ADDED PARTS;[11] VERIFIED MEASUREMENTS

Part: ANGLE — VAPOR LOCK (AFT CARGO) · airframe 27,092 hrs · 12,498 cycles

AFT CARGO BAY ATTACH ANGLE UNDER SHIELD BS767 TO BS787 RBL21 WL156 HAS AREAS OF CORROSION / [01] EVALUATED CORROSION ON ATTACH ANGLE UNDER SHIELD BS 767 TO BS 787 RBL 21 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 ACTION #1;[03] REMOVED ACB ANGLE UNDER SHIELD BS767 TO BS787 RBL21 WL156 PER SRM 51-40-02-0G-0.;[04] LOCATED; DRILLED AND DEBURRED NEW ANGLE UNDER SHIELD BS767 TO BS787 RBL21 WL156 PER SRM 51-40-05-0G-0 AND DWG 146A8123.;[05] VERIFIED CORRECTIVE ACTION 4;[06] OK TO INSTALL NEW ANGLE UNDER SHIELD.;[07] OK TO INSTALL NEW ANGLE UNDER SHIELD.;[08] INSTALLED NEW ANGLE UNDER SHIELD BS767 TO BS787 RBL21 WL156 PER SRM 51-40-02-0G-0 AND DWG 146A8123.;[09] VERIFIED CORRECTIVE ACTION 8;[10] ADDED PARTS;[11] VERIFIED MEASUREMENTS

Part: WEB — CORRODED (AFT CARGO) · airframe 27,092 hrs · 12,498 cycles

AFT CARGO BAY SUBTHRESHOLD WEB HAS CORROSION AT BS807 RBL26 WL156 / [01] EVALUATED CORROSION ON SUBTHRESHOLD WEB BS 807 RBL 26 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.045 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DIAL DEPTH GAUGE ATS 2678 DUE 04/2023;[02] VERIFIED ACTION #1;[03] REMOVED ACB SUBTHRESHOLD WEB BS. 794-847 RBL 26 WL 156 PER SRM 51-40-02.;[04] LOCATED; DRILLED; DEBURRED; AND INSTALLED NUT PLATES ON NEW ACB SUB THRESHOLD WEB BS 794 TO BS847; RBL 26; WL 156 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG#146A8120; DWG#146A8340.;[05] VERIFIED CORRECTIVE ACTION #4; MEASUREMENT FIELD VERIFIED;[06] OK TO INSTALL.;[07] VERIFIED CORRECTIVE ACTION 6 OK TO INSTALL;[08] INSTALLED NEW ACB SUB THRESHOLD WEB BS 794 TO BS 847; WL 156 PER DWG 146A8340 AND SRM 51-40-02-0G-0.;[09] VERIFIED CORRECTIVE ACTION #8;[10] VERIFIED CORRECTIVE ACTION #8

Part: WEB — CORRODED (FWD CARGO) · airframe 27,092 hrs · 12,498 cycles

FWD CARGO BAY CENTER THRESHOLD WEB HAS CORROSION BS462 RBL28 WL156 / [01] EVALUATED CORROSION ON SUBTHRESHOLD WEB BS 462 RBL 28 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.045 IN 1'X1' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DIAL DEPTH GAUGE ATS 2678 DUE 04/2023;[02] VERIFIED ACTION #1;[03] REMOVED FCB SUBTHRESHOLD WEB BS 440-492 RBL 28; WL 156 PER SRM 51-40-02.;[04] LOCATED; DRILLED; AND DEBURRED NEW FCB CENTER SUB THRESHOLD WEB BS 440 TO BS 492; RBL 28; WL 156 IAW SRM 51-40-05-0G-0; DWG#143A8330; DWG#143A8120.;[05] VERIFIED CORRECTIVE ACTION 4 AND MEQSUREMENT TABLE.;[06] OK TO INSTALL;[07] INSTALLED FWD CARGO BAY CENTER THRESHOLD WEB HAS CORROSION BS462 RBL28 WL156 IAW SRM 51-40-02-0G-0 AND DWG 143A8330;[08] CORRECTION: INSTALLED NEW FWD CARGO BAY CENTER SUB THRESHOLD WEB BS 440 TO BS 492; RBL 28 WL 156 IAW SRM 51-40-02-0G-0 AND 143A8330;[09] VERIFIED CORRECTIVE ACTION 6.<BR>OK TO INSTALL.;[10] UPDATED PARTS TABLE;[11] VERIFIED CORRECTIVE ACTION 8;[12] VERIFIED MEASUREMENT TABLE

Part: STAB CHANNEL — CRACKED (L/H HORIZ. STAB.) · airframe 27,092 hrs · 12,498 cycles

LEFT HORIZONTAL STAB FRONT SPAR UPPER SLIDE SEAL CRACKED / [01] REMOVED LH UPPER SLIDE SEAL IAW AMM 53-31-31-000-802<BR>ASSEMBLED SEAL PLATE; TIE BAR; AND CORNER PLATES IAW AMM 53-31-31-400-802 STEPS 3.F (1-18);[02] VERIFIED CORRECTIVE ACTION #1;[03] INSTALLED SEAL PLATE IN TRACKS PER AMM 53-31-31-400-802 STEPS 3.F(19)-(21)<BR>TOOL ID ATS392 DUE 01-2023;[04] VERIFIED CORRECTIVE ACTION #3;[05] INSTALLED SLIDING SEAL IAW AMM 53-31-31-400-802 STEPS 3.F(22)-(28);G;[06] VERIFIED CORRECTIVE ACTION #5

Part: FAIRING — DELAMINATED (R/H WING) · airframe 27,092 hrs · 12,498 cycles

#6 FLAP TRACK AFT FAIRING HAS DELAMINATED AREA AT O/B SIDE / [01] IDENTIFIED #6 AFT FLAP TRACK FAIRING PANEL 642BB IAW SRM 57-53-70-0I-3 FIGURE 1-2; 4 AND 14; ITEM 1; TABLE 3 AND 12<BR><BR>DAMAGE IS OUT OF ALLOWABLE LIMITS IAW SRM 57-53-70-1A-1 FIGURE 101 AND 104; ZONE 1; PARA 4.A(5)<BR><BR>ENGINEERING IS REQUIRED DUE TO THE SIZE OF THE DAMAGE IS MORE THAN 3' DIA PER SRM 57-53-70-2R-1 PARA 4.A(1) AND 4.B(1); FIGURE 204; ZONE 1 AND TABLE 201<BR><BR>VISUALLY EXAMINED EXTENT OF DAMAGE; TAP TESTED - MULTIPLE DISBONDS NOTED; REMOVE 2EA AREAS OF DISBONDS; AREA #1; REMOVED 4.5' X 8.8' OF OUTER OB SURFACE PLY (1 PLY); AREA #2; [07] DUE TO DAMAGE IS OUT OF REPAIRABLE LIMITS ON #6 AFT FLAP TRACK FAIRING THE PART WAS REPLACED WITH A SERVICEABLE UNIT. IAW SRM 57-53-70-1A-1 AND AIPC 27-51-18-01 ITEM 425 AFT TAIL CONE AND AFT MOUNT STRUCTURE WILL BE TRANSFERRED TO NEW UNIT FROM OFF UNIT ON FAULT TTG8Q00DRFYY.

Part: ATTACH ANGLE — CRACKED (CENTER WING) · airframe 27,092 hrs · 12,498 cycles

L/H BS663 UPPER ATTACH ANGLE CRACKED ON VAPOR BARRIER LBL8 WL167.68 / [01] VERIFIED APPLICABILITY OF SRM 57-10-10-2R-5 REPAIR 5 AND UPDATED MEASUREMENT TABLE [12] INSTALLED LH BS663 UPPER ATTACH ANGLE REPAIR PARTS LBL8-LBL20 WL167.68 IAW SRM 57-10-10-2R-5. BOND CHECK GOOD. TOOL ID:ATS1751 S/N:DC004716 DUE:10/2022. CAP SEALING AND LEAK CHECK ON INTERNAL SIDE FUEL TANK FASTENERS WILL BE ACCOMPLISHED ON CC#TTG8Q00DLKRU.;[13] VERIFIED CORRECTIVE ACTION 12;[14] FILLET SEALED; CAP SEALED EXTERNAL SIDE OF REPAIR AND APPLIED CIC TO BS663 LH UPPER ATTACH ANGLE REPAIR PARTS LBL8-LBL20 WL167.68 IAW SRM 57-10-10-2R-5.;[15] REMOVED PROTECTION OF EWIS @ LH BS 663 UPPER ATTACH ANGLE ON FWD AND AFT SIDE OF VAPOR BARRIER IAW AMM 20-60-07-913-801.;[16] VERIFIED CORRECTIVE ACTIONS 14 AND 15

Part: PANEL — CRACKED (FUSELAGE) · airframe 25,116 hrs · 11,429 cycles

FWD CARGO AC DISTRIBUTION BAY RIGHT FLOOR BREAK PNL ASSEMBLY CRACKED ; / [01] REMOVED AND REPLACED R/H BREAK PANEL ASSEMBLY IN FWD CARGO AC DISTRIBUTION BAY AS PER SRM 51-40-02

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,819 hrs · 9,736 cycles

LEFT WING FORWARD EMERGENCY EXTERIOR LIGHT INOPERABLE. REMOVED AND REPLACED LEFT WING FORWARD EMERGENCY EXTERIOR LIGHT BULB, IN REF TO AMM 33-51-04. OPERATIONS CHECKS GOOD.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,824 hrs · 9,207 cycles

AFT CARGO BAY FLOOR PANEL 140EF CORRODED / EVALUATED CORROSION ON AFT CARGO BAY FLOOR PANEL 140EF; LENGTH OF TOTAL ACCUMULATED DAMAGE EXCEEDED 20' MAXIMUM ALLOWEABLE LENGTH - OUT OF LIMITS IAW SRM 53-00-53-1A-1; REPLACED WITH NEW/FABRICATED PANEL 140EF IAW AMM 25-52-01-201-801; TO BE INSTALLED ON SA-M 565S PANEL SIGN OFF SHEET; AND BOEING DWG 453A2610-SHT 38 REV. C. P/N 453A2610-58 ATAG A68668

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,824 hrs · 9,207 cycles

AFT CARGO BAY FLOOR PANEL 140AF CORRODED / EVALUATED CORROSION ON AFT CARGO PIT FLOOR PANEL 140AF CORROSION EXCEEDED THE 20 INCH ALLOWABLE LIMITS; OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102. FABRICATED NEW FLOOR PANEL IAW AMM 25-52-01-201-801 AND BOEING DRAWING 453A2610 SHEET 26 REV. E; TREATED AND PRIMED IAW AMM 51-21-41-370-802 AND AMM 51-21-72-370-804

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,824 hrs · 9,207 cycles

AFT CARGO BAY FLOOR PANEL 140DF CORRODED / EVALUATED CORROSION ON AFT CARGO BAY FLOOR PANEL 140DF AND FOUND ACCUMULATED LENGTH OF DAMAGE TO BE MORE THAN 20' MAXIMUM ALLOWED - OUT OF LIMITS IAW SRM 53-00-53-1A-1; FABRICATED NEW PANEL 140DF IAW AMM 25-52-01-201-801 AND BOEING DWG 453A2610 REV B; TO BE INSTALLED ON SA-M 565S TASK CARD PANEL SIGN OFF SHEET ATAG A11784

Part: SKIN — DEBONDED (LT WING SPOILER) · airframe 20,824 hrs · 9,207 cycles

LH WING #6 SPOILER LOWER SURFACE DENT #8 DISBONDED / REPAIRED #8 DENT WITH DISBOND ON LOWER SKIN OF #6 SPOILER. IAW B737800 SRM 5770010I1; SRM 5770012R2; SRM 5170102R2; SRM 5170102R0; AMM 512199300801.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,824 hrs · 9,207 cycles

AFT CARGO BAY FLOOR PANEL 140CF CORRODED / EVALUATED CORROSION ON AFT CARGO PANEL 140CF CORROSION EXCEEDS THE 20 INCH ALLOWABLE LIMITS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102 FABRICATED NEW FLOOR PANEL IAW AMM 25-52-01-201-801 AND BOEING DRAWING 453A2610 SHEET 11 REV C TREATED AND PRIMED IAW AMM 51-21-41-370-802 AND AMM 51-21-72-370-804

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,824 hrs · 9,207 cycles

AFT CARGO BAY FLOOR PANEL 140BF CORRODED / FOUND CORROSION TO BE MORE THAN 20' IN LENGTH WHICH IS OUT OF LIMITS. FABRICATED NEW PANEL 140BF I/A/W AMM 25-52-01-201; SRM 53-00-53-1A AND DRAWING 453A2610 REV. K

Part: SHIELD — CORRODED (FWD CARGO) · airframe 20,824 hrs · 9,207 cycles

FWD PIT STA 500+6' FLOOR SHIELD UPPER SURFACE CORRODED AT RBL 23 AND WL157. / REMOVED CORROSION FROM PIT STA 500+6' FLOOR SHEILD UPPER SURFACE AT RBL 23 AND WL 157; ORIGINAL THICKNESS .050' REMAINING .045' LOSS .005' NO ALLOWABLE LIMITS ON PART OUT OF LIMITS. BACK SHOP FORMED AND HEAT TREATED PART ON WORK ORDER # 41323-1400-0001 I/A/W BOEING DWG 143A8126 REV - FABRICATED NEW FLOOR SHEILD I/A/W BOEING 143A8125- REV.- REPLACED FLOOR SHEILD I/A/W 737-800 SRM 51-40-02-0G-0 AND BOEING DWG REV. -143A0080- REV - P/N 143A8126-38

Part: CHANNEL — CORRODED (BS 500A-500I) · airframe 20,824 hrs · 9,207 cycles

FWD PIT STA 500A TO STA 500I RIGHT Z ANGLE UPPER SURFACE CORRODED AT RBL 23 AND WL157 / REMOVED CORROSION FROM FWD CARGO BAY RH ZEE ANGLE STA 500A TO STA 500I RBL 23 WL157 IAW SRM 51-10-02-0G-0 AND USED 10X MAG GLASS NO DEFECTS NOTED EVALUATED MATERIAL LOSS TO BE .020' ORIGINAL T = .040' LIMIT = .004' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FABRICATED NEW ZEE ANGLE IAW SRM 53-00-53-2R-5 INSTALLED NEW ZEE ANGLE IAW SRM 51-40-02-0G-0 AND DWG 143A7500 REV - APPLIED CIC TO BOTTOM AND TOP SURFACES IAW AMM 51-21-91-620-802 P/N 143A7501-88

Part: ANGLE — CORRODED (BS 727E-727F) · airframe 20,824 hrs · 9,207 cycles

AFT CARGO COMPARTMENT; Z-ANGLE; WL156; LBL20; BS727E +15' - 727F +15'; CORRODED MULTIPLE LOCATIONS / AFT CARGO Z-ANGLE L/H SIDE STA 727E TO 727F+15' CORRODED BLENDED AND REMOVED CORROSION ON Z-ANGLE AND CHECKED WITH 10X MAG I/A/W SRM 51-10-02-0G-0 THICKNESS IS .040; MAT LOSS IS .014; MAT REMINING IS .026 'OUT OF LIMITS' I/A/W SRM 53-00-53-2R-5 REPAIR 5. CUT AND REMOVED DAMAGED SECTION 727E TO 727J+10; FABRICATED NEW SECTION; DRILLED; DEBURRED; TRIMMED I/A/W SRM 53-00-563-2R-5. TREATED AND PRIMED AND INSTALLED NUT-PLATES I/A/W SRM 53-00-53-2R-5 STEP I;J;K;M. INSTALLED I/A/W SRM 53-00-53-2R-5 REPAIR 5 STEPS L. APPLIED C.I.C I/A/W SRM 53-00-53-2R-5 STEP N. P/N 146A7502-31

Part: DOUBLER — CORRODED (AFT CARGO BS 747) · airframe 20,824 hrs · 9,207 cycles

AFT CARGO COMPARTMENT; FRAME; WL157; LBL21; BS747; CORRODED / AFT CARGO FRAME 747 LBL 21 CORRODED. BLENDED AND REMOVED CORROSION AND CHECKED WITH 10X MAG I/A/W 51-10-02-0G-0 SRM. 'OUT OF LIMITS' THICKNESS IS .063 MAT LOSS .010 REMAINING .053 I/A/W SRM 53-00-07-1A-1 FIG 102 DETAIL C. FABRICATED REPAIR DOUBLER TRIMMED; DEBURRED; DRILLED ALL FASTENER HOLES I/A/W SRM 53-60-07-2R-2 REPAIR 2. TREATED AND PRIMED NEW DOUBLER I/A/W SRM 51-21-72-370-804; SRM 51-21-07-06-0. INSTALLED NEW DOUBLER I/A/W SRM 51-40-02-0G-0 ALSO SRM 51-40-05-0G-0. APPLIED C.I.C TO REPAIR I/A/W AMM 51-21-91-620-802 (P/N 146A1265-61)

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 20,824 hrs · 9,207 cycles

CABIN FLOOR PANEL 241AF FWD R/H CORNER IS MISSING CORE MATERIAL. REPAIRED CABIN FLOOR PANEL 241AF FWD R/H CORNER MISSING CORE IAW B737 SRM 53-00-50-2R-4 REV 69 ABD B737 SRM 53-00-50-2R-0 REV 69. A64736 A94414 A03261

Part: SUPPORT ANGLE — CORRODED (BS 500I) · airframe 20,824 hrs · 9,207 cycles

FWD PIT STA 500I BULKHEAD PANEL LWR SUPPORT ANGLE UPPER SURFACE CORRODED FROM LBL 20 TO RBL 23 / FWD PIT STA 500I BULKHEAD PANEL LOWER SUPPORT ANGLE UPPER SURFACE CORRODED FROM LBL 20 TO RBL 23 REMOVED AND REPLACED WITH NEW ANGLE P/N 143A9485Y35 IAW SRM 51-40-05-0G-0 AND BOEING DWG'S 143A9485 (PL) REV F AND 143A9481 REV - REMOVED CORROSION; VISUALLY INSPECTED AREA WITH 10X MAG NO DEFECTS NOTED IAW 51-1-02-0G-0 ORIG 'T' .071' LOSS OF .005' REMAINING .066' NO SRM ALLOWABLE LIMITS ATAG WN2583

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 20,824 hrs · 9,207 cycles

FWD PIT FLOOR PNL 120AF HAS CORROSION ON UPPER SURFACE ALONG FWD AND RH EDGES / EVALUATED CORROSION ON UPPER SURFACE ALONG FWD AND RH EDGES OF FWD PIT FLOOR PNL 120AF; TOTAL ACCUMLATED CORROSION DAMAGE FOUND TO EXCEED 20' MAXIMUM LENGTH ALLOWED - OUT OF LIMITS; IAW SRM 53-00-53-1A-1; FABRICATED NEW FLOOR PANEL 120AF IAW AMM 25-52-01-201-801; TO BE INSTALLED ON SA-M 565S CARD PANEL SIGN OFF SHEET ATAG A63683

Part: ANGLE — CORRODED (BS 500B-500C) · airframe 20,824 hrs · 9,207 cycles

FWD PIT STA 500B TO 500G LEFT Z ANGLE CORRODED AT LBL 23 AND WL157 / REMOVED CORROSION AND EVALUATED MATERIAL LOSS ON FWD CARGO LH Z ANGLE FROM STA 500B TO 500G ORIGINAL 'T' .040' LOSS .010' REMAINING 'T' .030' FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 REPAIRED LH Z ANGLE FROM STA 500B TO STA 500G IAW SRM 53-00-53-2R-5 P/N 143A7501-187

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 20,824 hrs · 9,207 cycles

FWD PIT FLOOR PNL 120CF HAS CORROSION ON UPPER SURFACE ALONG LH AND RH EDGES / FWD PIT FLOOR PNL 120CF HAS CORROSION ON UPPER SURFACE ALONG LH AND RH EDGES EVALUATED CORROSION FOUND IT EXCEEDS 20' OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102 VERIFIED NEW MATERIAL P# 2024-T3-071 A TAG # A68671 IAW SRM 51-20-01-0G-0 PRIMED IAW AMM 51-21-72-370-804

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 20,824 hrs · 9,207 cycles

FWD PIT FLOOR PANEL 120DF CORRODED IN MANY LOCATIONS ON TOP SIDE OF AFT AND RH EDGES. / EVALUATED FWD PIT FLOOR PANEL 120DF CORROSION EXCEEDED LIMITS IAW SRM 53-00-53-1A-1 FABRICATED NEW FLOOR PANEL IAW AMM 25-52-01-201-801

Part: ANGLE — CRACKED (BS 663) · airframe 20,824 hrs · 9,207 cycles

RH A/C PACK BAY. HORIZONTAL ANGLE COMMON TO LOWER CENTER FUEL TANK AT STATION 663 IS CRACKED 3RD FASTENER OUTBOARD OF KEEL BEAM VERTICAL ANGLE. / REPIARED R/H STA 663 HORIZONTIAL ATTACH ANGLE 3RD FASTENER O/B OF KEEL BEAM VERTICAL ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5.

Part: FAN — BURNED (CABIN) · airframe 20,057 hrs · 8,828 cycles

DIVERSION------------------------------FUMES & SMOKE IN CABIN. / INSPECTED A/C PER AMM 05-5156 & FIM 21-00-806. THE ONLY ISSUE FOUND IS LH RECIRE FAN BURNT UP & CAUSING SMOKEY SMELL (REF) LP# 1371078 FOR RECIRE FAN MEL A/C OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 19,763 hrs · 8,692 cycles

FLASHLIGHT IN FWD GALLEY INOP. / REPLACED BATTERY ON FWD GALLEY FLASHLIGHT PER SIP.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 19,383 hrs · 8,523 cycles

L1 DOOR LATCH LEFT ON DOOR BELOW SLIDE LOOSE. / R&R SLIDE PER MT.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 16,296 hrs · 7,134 cycles

ROW 15 OVERWING EXIT ROW LIGHT FLUTTERED. R&R LIGHT IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,298 hrs · 6,706 cycles

RT EMERGENCY LIGHTS INOP BETWEEN ROW 6 TO ROW 14. R&R BATTERY PACK PER AMM AND WDM.

Part: GIRT BAR — OUT OF POSITION (R2 DOOR) · airframe 12,577 hrs · 5,545 cycles

R2 DOOR EMERGENCY EVAC SLIDE FLOOR GIRT BAR OUT OF POSITION. REPOSITIONED GIRT BAR PER MT.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 10,673 hrs · 4,693 cycles

AFT MEGAPHONE INOP. R&R MEGAPHONE PER MM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 9,858 hrs · 4,342 cycles

LT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED / R&R'D LT HORIZ STAB UPPER FWD SLIDING SEAL REF AMM 53-31-31.AMT 67660 INSP P44

Part: LENS — CRACKED (CABIN) · airframe 8,015 hrs · 3,558 cycles

R1 DOOR EMERGENCY EXIT LIGHTED SIGN LENS CRACKED. R & R THE LENS IAW MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 746 hrs · 354 cycles

AFT RT OTBD FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT ASSEMBLY IAW CMM.