N946WN

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

BAFFLE SUPPORTING ANGLE AFT SIDE BS 500B RBL 25 IS CRACKED. REMOVED AND REPLACED FCB BAFFLE ANGLE FROM BS 500B FRAME RBL 25R AFT SIDE IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV -.

Part: COVER PLATE — MISSING (ZONE 800) · airframe 50,632 hrs · 31,066 cycles

MISSING COVER PLATE ON FORWARD SERVICE DOOR HANDLE. INSTALLED MISSING COVER PLATE ON FORWARD SERVICE DOOR HANDLE IAW AMM 52-41-31-400-802 3. F. (5) (D).

Part: WEB — CORRODED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

VERTIFCAL WEB HAS CORROSION AT RBL +20 BS 767 - 787. REMOVED AND REPLACED VERTICAL WEB AT BS 767 TO 787 RBL 20 IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 146A0081, REV-

Part: WEB — CORRODED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

CORROSION ON ACD SUB THRESHOLD WEB BETWEEN BS 794- 847, RBL 26. REMOVED AND REPLACED ACB SUB THRESHOLD WEB IAW SRM 51-40-02 AND DWG 146A8340 REV-.

Part: SUPPORT CHANNEL — CORRODED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

CORROSION ON ACB AFT BULKHEAD R/H LOWER SUPPORT CHANNEL AT BS 947, RBL 25, WL 156. REMOVED AND REPLACED NEW SUPPORT CHANNEL AT BS 947 RT SIDE IAW SRM 51-40-05 AND DWG 149A8117 REV -.

Part: BAFFLE — CRACKED (ZN 100 FUS LOWER) · airframe 50,632 hrs · 31,066 cycles

FORWARD CARGO BAY BAFFLE FROM BS 500A - 500B, RBL 25 FOUND CRACKED. REMOVED AND REPLACED FWD CARGO BAY BAFFLE IAW 51-40-02-0G-0, AND DWG 143A7505, REV -.

Part: BAFFLE — CRACKED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

FORWARD CARGO BAY BAFFLE FROM BS 500B - 500C, RBL 25 FOUND CRACKED. REMOVED AND REPLACED FWD CARGO BAY BAFFLE BS 500B TO BS 500C, RBL 25 IAW SRM 51-40-02-0G-0, AND DWG 143A7505, REV -.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

FCB; INTERCOSTAL ANGLE CRACKED AT BS 500C+1 LBL 24, WL 156. REMOVED AND INSTALLED A NEW INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02, AND DWG 143A7505, REV -.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 887 - 947, RBL 21, WL 155. REMOVED AND REPLACED AFT CARGO BAY SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 147A7500, REV -, DWG 146A7502, REV -.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

FORWARD CARGO BAY SIDEPLATE, BS 500A - 500D, RBL 22 HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED THE FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02, AND DWG 143A7500, REV A.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

CORROSION ON AFT CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT BS 947, LBL 15, RBL 15, WL 155. REMOVED AND REPLACED THE AFT CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT IAW SRM 51-40-02, AND DWG 149A8117, REV-.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727B - BS 767, RBL 21, WL 155. REMOVED AND REPLACED ACB SIDEWALL SUPPORT BS 727 - BS 767, RBL 21, WL 155 IAW SRM 51-40-02, DWG 146A7500 REV -, & DWG 146A0061, REV A.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

FCB; AFT LOWER BULKHEAD SUPPORT BS 500D, RBL 22 TO LBL 22 HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED FCB LOWER AFT BULKHEAD SUPPORT RAIL IAW SRM 51-10-02 PAR 9 AND SRM 51-40-02.

Part: WEB — CORRODED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

CORROSION ON AFT CARGO BAY SUB WEB THRESHOLD AT BS794 847; RBL 24; WL 155.<[01] TASK CARD WAS ACCOMPLISHED ON CUSTOMER CARD TTG8Q019KHBF.;[02] INSPECTION VERIFIED TASK ACCOMPLISHED ON CUSTOMER CARD TTG8Q019KHBF.;[03] INSPECTION VERIFIED TASK ACCOMPLISHED ON CUSTOMER CARD TTG8Q019KHBF.;[04] TASK CARD ACCOMPLISHED IN FAULT TTG8Q019KHBF

Part: SIDEWALL SUPPORT — CORRODED (ZONE 200) · airframe 50,632 hrs · 31,066 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 730 - 847, LBL 21, WL 155. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02, AND DWG 146A7500, REV -.

Part: SHIELD — CORRODED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

CORROSION ON AFT CARGO BAY SHEILD SUPPORT AT BS 767 - 794, RBL 24, WL 155. REMOVED AND REPLACED AFT CARGO BAY FWD SHIELD IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 146A0081, REV-.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

FCB; SIDE PLATE BS 396 TO 420 RBL 22 HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED NEW FLOOR TO SIDEWALL SUPPORT BS396 TO BS420 RBL22 IAW SRM 51-40-02 AND DWG 143A7500 REV-A.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

FWD CARGO BAY, INTERCOSTAL ANGLE CRACK AT BS 400, LBL 24. REMOVED AND REPLACED FWD CARGO BAY INTERCOSTAL ATTACH ANGLE AT BS 400 LBL 24 IAW SRM 51-40-02, AND DWG 143A7505, REV-.

Part: WEB — CORRODED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

FCD SURROUND STRUCTURE; SUB THRESHOLD BS 440 TO 490, RBL 22, WL 156 HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED SUB THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND DWG 143A8330 REV G.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 200) · airframe 50,632 hrs · 31,066 cycles

FORWARD CARGO BAY SIDEPLATE BS 396 - 500D, LBL 22 HAS SEVERAL SPOTS OF CORROSION. R & R THE FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02, AND DWG 143A7500, REV -.

Part: SHIELD — CORRODED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

FWD CARGO DOOR SURROUND STRUCTURE, AFT SHIELD BS 490 - 500A, RBL 22 HAS SEVERAL SPOTS OF CORROSION. REMOVED AND REPLACED FWD CARGO BAY AFT SHIELD BS 492 - 500A, RBL22 IAW SRM 51-40-02 AND DWG 143A0080 REV -.

Part: SUPPORT FRAME — CRACKED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

LEFT FWD WING-TO-BODY FAIRING SUPPORT STRUCTURE FRAME AT BS 500A CRACKED. REMOVED AND REPLACED THE LT FWD WING-TO-BODY FAIRING SUPPORT STRUCTURE FRAME AT BS 500A IAW SRM 51-40-02 AND DWG 116A3118, REV A.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

FCB; INTERCOSTAL ANGLE CRACKED AT BS 440 LBL 24, WL 156. REMOVED AND INSTALLED NEW INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02 AND DWG 143A7505, REV -.

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 50,632 hrs · 31,066 cycles

FWD CARGO BAY INTERCOSTAL ATTACH ANGLE CRACKED, BS 500B, LBL 24. REMOVED AND INSTALLED A NEW ATTACH ANGLE IAW SRM 51-40-02 AND DWG 143A7505, REV -.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

FCB; INTERCOSTAL ANGLE CRACK AT BS 500B+19, LBL 24. REMOVED AND INSTALLED NEW INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02 AND DWG 143A7505, REV B.

Part: FASTENER — MISSING (ZONE 100) · airframe 50,632 hrs · 31,066 cycles

FWD CARGO COMPARTMENT SUPPORT BRACKET MISSING A FASTENER BS 500D, S-20L. INSTALLED A NEW FASTENER AT FCB SUPPORT BRACKET BS 500D S-21L IAW SRM 51-40-02-0G-0 AND DWG: 143A7902, REV E VIEW 2C10.

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 50,632 hrs · 31,066 cycles

CRACKED PANEL BREAK AT PASSENGER COMPARTMENT BS540; LBL44; WL 208. THIS TASK CARD WAS PERFORMED WHIT THE CARD TTG8Q019HCS5. WORK PERFORMED ON CC TTG8Q019HCS5

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 50,632 hrs · 31,066 cycles

CRACKED PANEL BREAK AT PASSENGER COMPARTMENT BS 540; RBL 27; WL 208. REMOVED AND REPLACED PANEL BREAK AT BS 540, RBL 27, WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A0060 REV-.

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 50,632 hrs · 31,066 cycles

CRACKED PANEL BREAK AT PASSENGER COMPARTMENT BS 540,; LBL 27, WL 208. REMOVED AND REPLACED PANEL BREAK BS 540, LBL 24 TO LBL 45, WL 208 IAW SRM 51-40-02 AND DWG 143A0060, REV -.

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 50,632 hrs · 31,066 cycles

CRACKED PANEL BREAK AT PASSENGER COMPARTMENT BS540; LBL23; WL 208. REMOVED AND REPLACED PANEL BREAK IAW SRM 51-40-02 AND DWG 143A0060 REV -.

Part: SIGN — DETACHED (ZONE 200) · airframe 50,125 hrs · 30,713 cycles

CENTER AISLE OVER WING EXIT SIGN FELL OFF. REMOVED AND REPLACED CENTER AISLE OVERHEAD EXIT SIGN PER AMM 33-51-02. OPS CHECK GOOD.

Part: PANEL — DELAMINATED (ZONE 300 RUDDER) · airframe 49,540 hrs · 30,342 cycles

RIGHT SIDE RUDDER SEAL IS DELAMINATED AT STATION STA 288. INSTALLED NEW PANEL IAW AMM 55-33-31.

Part: PANEL — DELAMINATED (ZONE 300 RUDDER) · airframe 49,540 hrs · 30,342 cycles

RIGHT SIDE RUDDER SEAL IS DELAMINATED AT STATION STA 269. INSTALLED NEW PANEL IAW AMM 55-33-31.

Part: PANEL — DELAMINATED (ZONE 300 RUDDER) · airframe 49,540 hrs · 30,342 cycles

RIGHT SIDE RUDDER SEAL IS DELAMINATED AT STATION STA 194. INSTALLED NEW PANEL IAW AMM 55-33-31.

Part: PANEL — DELAMINATED (ZONE 300 RUDDER) · airframe 49,540 hrs · 30,342 cycles

RIGHT SIDE RUDDER SEAL IS DELAMINATED AT RS 288. INSTALLED NEW PANEL REF AMM 55-33-31.

Part: PANEL — DELAMINATED (ZONE 300 RUDDER) · airframe 49,540 hrs · 30,342 cycles

RIGHT SIDE RUDDER SEAL IS DELAMINATED AT STATION STA 269. INSTALLED NEW PANEL REF AMM 55-33-31.

Part: PANEL — DELAMINATED (ZONE 300 RUDDER) · airframe 49,540 hrs · 30,342 cycles

RIGHT SIDE RUDDER SEAL IS DELAMINATED AT STATION STA 194. INSTALLED NEW PANEL REF AMM 55-33-31.

Part: LENS — DETACHED (ZONE 200) · airframe 47,917 hrs · 29,333 cycles

EXIT SIGN OVERWING EXIT FELL OFF RE ATTACHED OVERWING EXIT SIGN LENS PER MM 33-51-11<[01] INSTALLED OVERWING EXIT SIGN LENS PER MM 33-51-03

Part: GIRT BAR — BENT (ZONE 800) · airframe 47,061 hrs · 28,806 cycles

CONTROL CABIN GIRT BAR ON GEAR PIN COMPARTMENT BENT.<[01] R&R CONTROL CABIN GIRT BAR ON GEAR PIN COMPARTMENT IAW AMM SIP.

Part: HOOK AND LOOP — LOOSE (ZONE 800) · airframe 46,971 hrs · 28,755 cycles

FWD SERVICE DOOR EMERGENCY ESCAPE SLIDE VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF.<[01] REATTACHED ESCAPE SLIDE VELCRO STRIPS ON GIRT ON FS DOOR EMERGENCY ESCAPE SLIDE ASSY IAW MT 725-61-06

Part: HOOK AND LOOP — LOOSE (ZONE 800) · airframe 46,971 hrs · 28,755 cycles

AFT SERVICE EMERGENCY ESCAPE SLIDE VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF.<[01] REATTACHED ESCAPE SLIDE VELCRO STRIPS ON GIRT ON AS DOOR EMERGENCY ESCAPE SLIDE ASSY IAW MT 725-61-06

Part: HOOK AND LOOP — LOOSE (ZONE 800) · airframe 46,971 hrs · 28,755 cycles

FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF.<[01] REATTACHED ESCAPE SLIDE VELCRO STRIPS ON GIRT ON FE DOOR EMERGENCY ESCAPE SLIDE ASSY IAW MT 725-61-06

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 46,655 hrs · 28,567 cycles

17 ABC EMERGENCY FLOOD LIGHT INOP<[01] RELAMPED EMERGENCY AREA FLOOD LIGHT AT 17 ABC PER AMM 33-51-03. OPS CHECK GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 46,346 hrs · 28,377 cycles

AFT LH EXTERIOR OVERWING EMERGENCY LIGHT INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801-NG (AFT LH OVERWING LIGHT - LAMP REPLACEMENT - PERMANENT)]

Part: HANDLE — BROKEN (FWD SERV DOOR) · airframe 44,915 hrs · 27,506 cycles

FORWARD SERVICE DOOR INTERIOR DOOR PULL BROKEN.<[01] REMOVED AND REPLACED FWD SERVICE DOOR ASSIST HANDLE IAW M/M 52-41-00

Part: LOCK — LOOSE (SEAT 10A) · airframe 44,527 hrs · 27,268 cycles

SEAT 10A RECLINES INTO THE EMERGENCY EXIT ROW.<[01] SECURED HYDROLOCK AT 10A PER CMM 25-22-46.

Part: MEGAPHONE — INOPERATIVE (ZN 200 FUS TOP) · airframe 44,434 hrs · 27,214 cycles

FWD L/H WINDSCREEN MEGA PHONE MIC NOT WORKING<[01] REMOVED AND REPLACED FWD L/H WINDSCREEN MEGA PHONE IAW AMM 25-64-00-710-801 FUNCTIONAL CHECK GOOD.;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.

Part: BEAM — CRACKED (R4 DOOR) · airframe 44,434 hrs · 27,214 cycles

CRACK FOUND DURING HFEC INSPECTION OF FSD #4 BEAM (141A6536-14) AT MOST I/B HOLE MEASURED APPROX L: 0.5' MARKED<[01] REMOVED FWD SERVICE DOOR ASSY PER AMM 52-41-00-000-801; ACCOMPLISHED ON TASK TTG8Q00QYJHM;[02] REPAIR TO FWD SERVICE DOOR #4 BEAM ACCOMPLISHED ON FAA FORM 8130-3 TRACKING# N-186938 CUSTOMER RO# P7987704-1.;[03] >DIT ACTION 1: REMOVED AND REOINSTALLED FWD SERVICE DOOR ASSY PER AMM 52-41-00-401; ACCOMPLISHED ON TASK TTG8Q00QYJHM;[04] VERIFIED CORRECTIVE ACTIONS 1-3 AND MEASUREMENT TABLE

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 44,434 hrs · 27,214 cycles

UPPER T/E PANEL 651AT; U CHANNEL PANEL SUPPORT ANGLE CRACKED AT UPPER REAR SPAR ATTACH POINT JUST O/B OF WING STATION 70.5 (MARKED)<[01] REMOVED AND REPLACED CRACKED UPPER TRAILING EDGE PANEL 651AT; U CHANNEL PANEL SUPPORT ANGLE CRACKED AT UPPER REAR SPAR ATTACH POINT JUST OUTBOARD OF WING STATION 70.5 IAW AIPC 57-50-00-34 & SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION1 AND MEASUREMENT TABLE

Part: LINER — DAMAGED (FWD GALLEY DOOR) · airframe 44,434 hrs · 27,214 cycles

FWD GALLEY DOOR LINER IS DAMAGED AROUND ASSIST HANDLE<[01] REPAIRED SURFACE DAMAGE AROUND UPPER HOLE ON THE FWD. GALLEY DOOR LINER AROUND UPPER ASSIST HANDLE IAW CMM 25-00-66. REPAIR 2-1 PG 603 SEC 4 SEPT A; B. (1-6);[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.

Part: SEAT BACK — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 44,357 hrs · 27,165 cycles

SEAT 10A RECLINES INTO EMERGENCY EXIT ROW.<[01] RESECURED HYDROLOCK IAW M/M 25-22-00

Part: SIGN — LOOSE (ZN 200 FUS TOP) · airframe 44,061 hrs · 26,989 cycles

RT SIDE AFT EMERGENCY LOCATOR SIGN WILL NOT STAY INSTALL (ABOVE R2 DOOR)<[01] C/W EA M-21-133-00720. A/C OK FOR SERVICE.

Part: SEAT BACK — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 43,561 hrs · 26,679 cycles

PASSENGER SEAT 10A EMERGENCY EXIT ROW RECLINES AND SHOULD NOT<[01] ADJUSTED HYDRO-LOCK TO THE STOP POSITION PER AMM 25-22-00

Part: GIRT BAR — LOOSE (ZN 800 DOOR) · airframe 43,551 hrs · 26,673 cycles

GIRT BAR STORAGE CLIP LOOSE. FWD SERVICE DOOR<[01] REPLACED MISSING FASTENER IN CLIP REF SRM 51-40-01.

Part: GIRT BAR — LOCKED (ZN 800 DOOR) · airframe 43,515 hrs · 26,647 cycles

R1 SERVICE DOOR GIRT BAR RETAINER LOOSE<[01] ADJUSTED AND RESECURED DOOR MOUNTED GIRT BAR STOW CLIP REF AMM 25-66-01

Part: FUSE — INOPERATIVE (ZN 200 FUS TOP) · airframe 43,049 hrs · 26,334 cycles

RIGHT SIDE AFT OF WING EMERGENCY LIGHT INOP<[01] FOUND RIGHT SIDE AFT OF WING EMERGENCY LIGHT FUSE ON POWER SUPPLY M1670 BLOWN. R&R FUSE PER AMM 33-51-06.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 42,389 hrs · 25,911 cycles

R2 DOOR EMERGENCY SLIDE LIGHT<[01] RELAMPED PER AMM 33-51-04

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 42,073 hrs · 25,711 cycles

FOUND CRACK ON FWD CARGO PIT FLOOR PANEL 120CF APPROX 10 LONG<[01] APPLIED WITH PERMANENT REPAIR OF FWD CARGO PIT PANEL 120CF PER AMM 23-52-01

Part: SLIDE — LOW PRESSURE (SERVICE DOOR) · airframe 41,401 hrs · 25,246 cycles

RT AFT SERVICE SLIDE LOW PRESSURE<[01] REMOVED AND REPLACED SLIDE PER MT 725-66-01

Part: LIGHT — INOPERATIVE (ZN 900 LAV/GALLE) · airframe 40,754 hrs · 24,812 cycles

SUPPLEMENTAL INFORMATION: EMERGENCY EXIT ROM LIGHT FO SIDE INOP RELAMPED NO HELP / [01] OK TO CONTINUE PER MEL 33-2-03; SP1B; AUTH 100919<BR><BR>(SIDEWALL LIGHT; NOT EMERGENCY LIGHT INOP);[02] REMOVED AND REPLACED BALLAST PER MM 33-21-00

Part: SLIDE — DISPLACED (L1 DOOR) · airframe 39,830 hrs · 24,167 cycles

L1 DOOR SLIDE BECAME DISPLACED FROM DOOR / [01] INSTALLED L1 DOOR SLIDE ONTO DOOR PER AMM 25-66-01.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 38,769 hrs · 23,511 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. / [01] RELAMPED R1 DOOR EXTERIOR EMERGENCY LIGHT AS PER B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 38,769 hrs · 23,511 cycles

L1 DOOR SLIDE GAGE NOT CENTERED / [01] REPOSITIONED L1 DOOR SLIDE GAGE IN REF B737 AMM 25-66-01-400-801. STEP C.;[02] FINAL INSPECTION; REPOSITIONED SLIDE GAGE.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 38,769 hrs · 23,511 cycles

EMERGENCY BATTERY PACKS (M1674 AND M1675) AT STA 322 INOP. / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACKS (M1674) & (M1675) AT STA:322. AND PERFORMED OPS CHECK EMERGENCY LIGHT TEST PASS AS PER B737 AMM 33-51-06-960-805;[02] VERIFIED 1.

Part: BATTERY PACK — INOPERATIVE (L/H CABIN) · airframe 38,769 hrs · 23,511 cycles

EMERGENCY POWER SUPPLY ( M1673) AT STA 952 L/H INOP. / [01] REMOVED & REPLACED EMERGENCY POWER SUPPLY & BATTERY PACK (M1673) AT STA. 952 AND PERFORMED OPS CHECK EMERGENCY LIGHT TEST PASS AS PER B737 AMM 33-51-06-960-806 ;AMM 33-51-06-960-805;[02] VERIFIED 1.

Part: POWER SUPPLY — INOPERATIVE (L/H CABIN) · airframe 38,769 hrs · 23,511 cycles

EMERGENCY POWER SUPPLY ( M1673) AT STA 952 L/H INOP. / [01] REMOVED & REPLACED EMERGENCY POWER SUPPLY & BATTERY PACK (M1673) AT STA. 952 AND PERFORMED OPS CHECK EMERGENCY LIGHT TEST PASS AS PER B737 AMM 33-51-06-960-806 ;AMM 33-51-06-960-805;[02] VERIFIED 1.

Part: PANEL — CRACKED (ELEVATOR) · airframe 38,769 hrs · 23,511 cycles

ELEVATOR HINGE COVER ACCESS (L/H LOWER)PANEL #334GB; FASTENER HOLE CRACK. / [01] REMOVED THE DAMAGED PLIES AND PREPARED AREA TO APPLY THE FABRIC REPAIR PLIES; NO WATER NOTE AT REPAIR AREA ON ACCESS PANEL 334 GB REF B737-700 SRM 51-70-04-2R-10 PARAGRAPH 4 AND SRM 51-70-04-2R-0 PARAGRAPH 4.;[02] VERIFIED STEP1. OK TO APPLY REPAIR.;[03] APPLIED FABRIC REPAIR PLIES AT DAMAGED AREA. REF B737-700 SRM 51-70-04-2R-10 PARAGRAPH 4 AND SRM 51-70-04-2R-0 PARAGRAPH 4.;[04] VERIFIED STEP 3. OK TO PAINT PNL.;[05] PAINTED REPAIR AREA AT ACCESS PANEL 334GB. REF B737-700 AMM 51-21-99-300-802.;[06] FINAL INSPECTION; REPAIRED DAMAGE AREA.

Part: STIFFENER — CARBONED (R/H HORIZ. STAB.) · airframe 38,769 hrs · 23,511 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB ASSY. #4 (STAB STA 120.30) STIFFENER #4 LOWER AREA CRACK NOTED. / [01] REMOVED DAMAGE OF RIB #4 AS PER B737-700 SRM 55-10-09-2R-417] INSTALLED REPAIR PARTS AT RT HORIZONTAL STAB INSPAR RIB #4 REF B737-700 SRM 55-10-09-2R-5 FIG 203 TABLE 201.;[18] VERIFIED STEP #16;[19] (RII) VERIFIED STEP #18; REPAIRED PARTS INSTALLED.;[20] APPLIED FILLET SEAL TO REPAIR PARTS IAW AMM 51-31-00-390-804.;[21] (FINAL) REMOVED DAMAGE OF RIB #4 AS PER B737-700 SRM 55-10-09-2R-4. REMOVED THE DAMAGE FROM THE LOWER CHORD OF THE RIB AS PER REF B737-700 SRM 55-10-09-2R-5. FABRICATED ANGLE [2] MATERIAL USED BAC1490 7075-T6 CLAD 0.063 IN. (6.5 X 2.4) AND SHIM[4] MATERIAL USED 7075-T6 CLAD 0.016 (3.1 X 1.0) AND FILLER [3] MATERIAL USED 7075-T6 CLAD 0.063 IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5. LOCATED AND DRILLED REPAIR PARTS AT RIGHT HORIZONTAL STABILIZER INSPAR RIB ASSY #4 STIFFENER #4 IAW SRM 55-10-09-2R-5 REPAIR 5. INSTALLED REPAIR PARTS AT RT HORIZONTAL STAB INSPAR RIB #4 REF B737-700 SRM 55-10-09-2R-5 FIG 203 TABLE 201.;[22] VERIFIED STEP 20.;[23] FINAL INSPECTION; DAMAGE REMOVAL AND INSTALLED NEW FABRICATED PARTS AND REPAIR DAMAGE AREAS.;[24] CORRECTION ON STEP #19.<BR> (RII) VERIFIED STEP #17; REPAIR PARTS INSTALLED.

Part: STRUCTURE — DETERIORATED (FWD FUSELAGE) · airframe 38,769 hrs · 23,511 cycles

FED WET AREA CABIN FLOOR STRUCTURE HAS DETERIORATED CIC STA 270_380 / [01] THIS ITEM WILL BE ACCOMPLISHED ON FAULT TTG8Q002JXKJ;[02] VERIFIED 1.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 38,769 hrs · 23,511 cycles

CABIN FLOOR PNL 241WF HAS 3 CRACKS. 8-87 / [01] CLEANER AND PREPARED AREAS FOR REPAIR AT FLOOR PANEL#241WF AS PER BOEING 737 SRM 53-00-50-2R-1;[02] REPAIRED DAMAGE AREAS AT CABIN FLOOR PANEL #241WF AS PER BOEING 737 SRM 53-00-50-2R-1. MATERIAL USED EPOCAST 50-A/946 PO#1714421 PLUS BMS9-3-120TYD CL7 PO#1690463.;[03] VERIFIED 1-2.

Part: SEAT TRACK — CORRODED · airframe 38,769 hrs · 23,511 cycles

CAPT FWD O/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-79 / [01] PARTS RECEIVED; INSTALLATION WILL BE COMPLETED ON TTG8Q002JXV4.;[02] VERIFIED 1.

Part: SEAT TRACK — CORRODED · airframe 38,769 hrs · 23,511 cycles

F/O FWD I/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-82 / [01] PARTS RECEIVED; INSTALLATION WILL BE COMPLETED ON TTG8Q002JXV4.;[02] VERIFIED 1.

Part: SEAT TRACK — CORRODED · airframe 38,769 hrs · 23,511 cycles

F/O AFT I/B SEAT TRACK HAS CORROSION AND CRACK ON LWR SURFACE. 8-85 / [01] PARTS RECEIVED; INSTALLATION WILL BE COMPLETED ON TTG8Q002JXV4.;[02] VERIFIED 1.

Part: SEAT TRACK — CORRODED · airframe 38,769 hrs · 23,511 cycles

CAPT FWD I/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-81 / [01] RECEIVED CAPTAIN FWD IB SEAT TRACK. WILL BE INSTALLED ON TC TTG8Q002JXV4.;[02] FINAL INSPECTION; RECEIVED CAPTAIN FWD IB SEAT TRACK. WILL BE INSTALLED ON TC TTG8Q002JXV4.

Part: SEAT TRACK — CORRODED · airframe 38,769 hrs · 23,511 cycles

F/O FWD O/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-83 / [01] PARTS RECEIVED; INSTALLATION WILL BE COMPLETED ON TTG8Q002JXV4.;[02] VERIFIED 1.

Part: SEAT TRACK — CORRODED · airframe 38,769 hrs · 23,511 cycles

F/O AFT O/B SEAT TRACK HAS CORROSION ON LWR SURFACE. 8-84 / [01] PARTS RECEIVED; INSTALLATION WILL BE COMPLETED ON TTG8Q002JXV4.;[02] VERIFIED 1.

Part: NONE — BROKEN (R/H ELEVATOR) · airframe 38,769 hrs · 23,511 cycles

RT ELEVATOR AT HINGE 3 UPPER CUTOUT BOTH CORNERS BROKEN. 8-66 / [01] MEASURE;[02] APPLIED DRY PROCESS AT R\T ELEVATOR AN HINGE #3 UPPER SURFACE CUT OUT PER B737SRM 51-70-04 2R-0 PARAGRAPH (4.D.9);[03] PREPARED DAMAGED AREA TO APPLY REPAIR TA R\T ELEVATOR PER B737SRM 51-70-04-2R-0 PARAGRAPH (4.E);[04] VERIFIED 1-3. OK TO INSTALL REPAIR.;[05] REPAIRED DAMAGED AREA AT ELEVATOR ON HINGE #3 UPPER SURFACE PER B737 SRM 55-20-01-2R-1 AND B737 SRM 51-70-04-2R-0 MATERIAL USED RESIN EY-3804 PO# 1753536 AND CARBON FIBER PO# 1160897;[06] VERIFIED 5.

Part: ANGLE — CORRODED (AFT CARGO) · airframe 38,769 hrs · 23,511 cycles

AFT CARGO COMP STA 947.5 FLOOR SUPPORT ANGLE CORRODED BETWEEN LBL 11' AND RBL 20' / [01] REMOVED CORROSION FROM AFT CARGO COMPARTMENT STA 947.5 FLOOR SUPPORT ANGLE IAW B 737-700 SRM 51-10-02-0G-0.;;[13] (FINAL) REMOVED CORROSION FROM AFT CARGO COMPARTMENT STA 947.5 FLOOR SUPPORT ANGLE IAW B 737-700 SRM 51-10-02-0G-0. EVALUATED AREA: ORIGINAL THICKNESS IS 0.080'. MATERIAL REMOVED IS 0.014'. MATERIAL REMAINING 0.066' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; FIG. 103; A-A. LOCATED; DRILLED; AND INSTALLED NEW AFT CARGO COMPARTMENT STA 947.5 FLOOR SUPPORT ANGLE IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0.;[14] VERIFIED STEP #12;[15] FINAL INSPECTION; REPLACED FLOOR SUPPORT ANGLE.

Part: CHANNEL — CORRODED (AFT CARGO) · airframe 38,769 hrs · 23,511 cycles

AFT CARGO COMPARTMENT - L/H ZEE CHANEL - STA 727 TO 847 - LBL 21 - WL 156.5 - SURFACE CORROSION IN SEVERAL AREAS / [01] AFT CARGO COMPARTMENT L/H ZEE CHANNEL BETWEEN STA 727 AND STA 847 LBL 21 FOUND EXFOLIATED AND OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] LOCATED AND DRILLED NEW R/H AFT CARGO ZEE CHANNEL IAW B737-700 SRM 51-40-05-0G-0. ZEE CHANNEL WILL BE INSTALLED ON T/C: TTG8Q004BM58;[03] VERIFIED STEPS #1 AND #2;[04] OK TO TREAT AND PRIME;[05] TREATED AND PRIMED DRILLED HOLES IAW SRM 51-20-01-0G-0.;[06] (FINAL) AFT CARGO COMPARTMENT L/H ZEE CHANNEL BETWEEN STA 727 AND STA 847 LBL 21 FOUND EXFOLIATED AND OUT OF LIMITS IAW SRM 53-00-53-1A-2. LOCATED AND DRILLED NEW R/H AFT CARGO ZEE CHANNEL IAW B737-700 SRM 51-40-05-0G-0. ZEE CHANNEL WILL BE INSTALLED ON T/C: TTG8Q004BM58;[07] VERIFIED STEP #5;[08] FINAL INSPECTION; REPLACED ZEE CHANNEL.

Part: ANGLE — CORRODED (AFT CARGO) · airframe 38,769 hrs · 23,511 cycles

AFT CARGO COMP R/H BETWEEN STA 727B AND STA 767 RBL 21' ZEE CHANNEL SURFACE CORROSION / [01] LOCATED AND DRILLED NEW FASTENER HOLES ONTO R/H AFT CARGO ZEE CHANNEL STA 727 - STA 767. ZEE CHANNEL WILL BE INSTALLED ON T/C: TTG8Q004BM58.;[02] (LATE ENTRY) AFT CARGO COMPARTMENT R/H ZEE CHANNEL BETWEEN STA 727B AND STA 767 RBL 21 FOUND EXFOLIATED AND OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[03] AMENDED TO STEP #1 LOCATED AND DRILLED NEW FASTENER HOLES ONTO R/H AFT CARGO ZEE CHANNEL STA 727 - STA 767. REF B737-700 SRM 51-40-05-0G-0. ZEE CHANNEL WILL BE INSTALLED ON T/C: TTG8Q004BM58.;[04] VERIFIED STEPS #1; #2 AND #3;[05] OK TO TREAT AND PRIME.;[06] TREATED AND PRIMED DRILLED HOLES IAW SRM 51-20-01-0G-0.;[07] (FINAL) AFT CARGO COMPARTMENT R/H ZEE CHANNEL BETWEEN STA 727B AND STA 767 RBL 21 FOUND EXFOLIATED AND OUT OF LIMITS IAW SRM 53-00-53-1A-2. LOCATED AND DRILLED NEW FASTENER HOLES ONTO R/H AFT CARGO ZEE CHANNEL STA 727 - STA 767. REF B737-700 SRM 51-40-05-0G-0. ZEE CHANNEL WILL BE INSTALLED ON T/C: TTG8Q004BM58.;[08] VERIFIED STEP #6;[09] FINAL INSPECTION; REPLACED ZEE CHANNEL.

Part: PANEL — ELONGATED (L/H HORIZ. STAB.) · airframe 38,769 hrs · 23,511 cycles

L/T HORIZONTAL STAB. LOWER T/E ACCESS PANEL # 333AB HAS RUBBER SEAL WITH ELONGATED HOLES; BLADE AND AFT METAL SEALS WORN / [01] REMOVED AND REPLACED RUBBER SEAL; BLADE AND AFT METAL SEALS AT L/T HORIZONTAL STAB. LOWER T/E ACCESS PANEL # 333AB IAW B737-700 SRM 51-40-02-0G-0.;[02] FINAL INSPECTED; SEAL REPLACED.

Part: SKIN — CRACKED (R/H HORIZ. STAB.) · airframe 38,769 hrs · 23,511 cycles

R/H HOR. STAB L/E SKIN RIB AT ABOUT LE STA 283 CRACKED FOUND CRACKED RIB AT R/H HORZ STAB L/E CORRECT LOCATION FOR DAMAGE RIB IS AT L/E STA 281.91 / [01] REMOVED DAMAGE PART FROM R/H HOR. STAB. L/E. SKIN RIB AT ABOUT L/E. STA. 283 IAW. B-737-700 SRM.51-40-02-0G-0;[02] VERIFIED REMOVAL;[03] MACH DRILL NEW R/H. HORIZONTAL L/E. SKIN RIB AT STA. 281.91 IAW. B-737-700 SRM.51-40-05-0G-0;[04] CORRECTION STEP #1. STA. 281.91;[05] VERIFIED 3 AND 4. OK TO INSTALL SKIN RIB AT R/H HORIZONTAL STAB L/E AT STA 281.91;[06] REMOVED AND REPLACE R/H. HORIZONTAL STAB. L/E. SKIN RIB AT L/E. STA. 281.91 IAW. B-737-700 SRM.51-40-02-0G-0;[07] VERIFIED STEP 6

Part: GUSSET — CRACKED (FWD CARGO) · airframe 38,769 hrs · 23,511 cycles

FWD CARGO COMPT GUSSET CRACKED AT BS 500D S19L / [01] REMOVED GUSSET AT FWD CARGO STA 500D; STG 19L AS PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW GUSSET AT FWD CARGO; STA 500D; STG 19LAS PER B737-700 SRM 51-40-05-0G-0;[03] VERIFIED 1-2. OK TO INSTALL NEW GUSSET.;[04] INSTALLED NEW GUSSET AT BS. 500D STR.19L IAW. B-737-700 SRM. 51-40-02-0G-0 AND DWG. #143A7902;[05] REMOVED AND REPLACE DAMAGE GUSSET AT BS.500D; STR.19L IAW. B-737-700 SRM.51-40-02-0G-0 AND DWG.#143A7902;[06] VERIFIED 4-5.

Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 38,769 hrs · 23,511 cycles

PAX CABIN FLOOR PANEL 241RF LOWER FWD SECTION DELAMINATED PAX CABIN FLOOR PANEL 241RF LOWER AFT SECTION DELAMINATED. / [01] REMOVED PAX CABIN FLOOR PANEL 241RF IAW B737-AMM-53-21-00-000-801.;[02] VERIFIED STEP #1.;[03] OK TO INSTALL NEW PANEL.;[04] INSTALLED NEW PAX CABIN FLOOR PANEL 241RF IAW B737-AMM-53-21-00-400-801. TORQUE WRENCH USED BC 164615; DUE DATE 02-AUG-2022;[05] FINAL INSPECTION; NEW FLOOR PANEL INSTALLED.

Part: GUSSET — CRACKED (FWD CARGO) · airframe 38,769 hrs · 23,511 cycles

FWD CARGO COMPT GUSSET CRACKED AT BS 500D S19R / [01] REMOVED DAMAGE GUSSET AT FWD CARGO R/H SIDE STA 550D S-19R REF B 737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW GUSSET AT FWD CARGO R/H SIDE STA 550D S-19R REF B 737-700 SRM 51-40-05-0G-0 AND DWG# 143A9481.;[03] VERIFIED STEPS.<BR>OK TO INSTALL NEW GUSSET .;[04] INSTALLED NEW GUSSET AT FWD CARGO R/H SIDE STA 550D S-19R REF B 737-700 SRM 51-40-02-0G-0 AND DWG# 143A9481.;[05] REMOVED AND REPLACED GUSSET AT FWD CARGO R/H SIDE STA 550D S-19R REF B 737-700 SRM 51-40-02-0G-0 AND DWG# 143A9481.;[06] VERIFIED STEPS 4;5.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,769 hrs · 23,511 cycles

MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 344 AND STA 360 BL 0 APPEARED CRACK AT AFT FASTENER HOLE / [01] REMOVED MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 344 AND STA 360 BL 0 IAW SRM 51-40-02-0G-0.;[02] VERIFIED STEP #1;[03] LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-05-0G-0;[04] VERIFIED STEP # 3;[05] OK TO INSTALL NEW INTERCOSTAL;[06] INSTALLED NEW INTERCOSTAL AT MAIN CABIN BETWEEN STA 360 TO STA 344 BL 0 REF B 737-700 SRM 51-40-02-0G-0 AND DWG# 141A5400.;[07] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 360 TO STA 344 BL 0 REF B 737-700 SRM 51-40-02-0G-0 AND DWG# 141A5400.;[08] VERIFIED STEPS 6 AND 7.

Part: ANGLE — CRACKED (FWD FUSELAGE) · airframe 38,769 hrs · 23,511 cycles

MAIN CABIN L/H STA 312 JUST ABOVE DOOR CUTOUT UPPER STRUCTURE FLANGE CRACKED / [01] TRIMMED OUT DAMAGED AREA AT MAIN CABIN UPPER CHORD OF FRAME STA 312 BETWEEN S-5L AND S-6L AND EVALUATED SURFACE ROUGHNESS FOUND TO BE SMOOTHER THAN 63 MICROINCHES RA AT CUT EDGE REF B737-700 SRM 51-10-02-0G-0 AND SRM 53-10-07-2R-1 FIG 202. TOOL USED B/C#171854;[21] INSTALLED NEW REPAIR ANGLE AT MAIN CABIN L/H STA 312 JUST ABOVE DOOR CUTOUT UPPER STRUCTURE IAW SRM 53-10-07-2R-1 REPAIR 1 AND SRM 51-40-02-0G-0;[22] (FINAL) TRIMMED OUT DAMAGED AREA AT MAIN CABIN UPPER CHORD OF FRAME STA 312 BETWEEN S-5L AND S-6L AND EVALUATED SURFACE ROUGHNESS FOUND TO BE SMOOTHER THAN 63 MICROINCHES RA AT CUT EDGE REF B737-700 SRM 51-10-02-0G-0 AND SRM 53-10-07-2R-1 FIG 202. TOOL USED B/C#171854. FABRICATED REPAIR ANGLE; MATERIAL USED 7075-O .O63 P.O. # 1557906 IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1. LOCATED AND DRILLED REPAIR ANGLE IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1. INSTALLED NEW REPAIR ANGLE AT MAIN CABIN L/H STA 312 JUST ABOVE DOOR CUTOUT UPPER STRUCTURE IAW SRM 53-10-07-2R-1 REPAIR 1 AND SRM 51-40-02-0G-0.;[23] (RII) VERIFIED STEPS #20 AND #21; INSTALLATION OF NEW REPAIR.;[24] OK TO APPLY CIC ON REPAIR AREA.;[25] APPLIED CIC ON REPAIR AREA IAW SRM 53-10-07-2R-1 REPAIR 1 AND AMM 51-21-91-620-802.;[26] VERIFIED STEP #25.;[27] (RII) FINAL INSPECTION; TRIMMED AND INSTALLED NEW FABRICATED REPAIRED ANGLE AT STA 312 BETWEEN S-5L AND S-6L.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,769 hrs · 23,511 cycles

MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 277 AND STA 294.5 BL 0 CRACKED / [01] REMOVED MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 277 AND STA 294.5 BL 0;[02] REMOVED MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 277 AND STA 294.5 BL 0 IAW SRM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-05-0G-0;[04] VERIFIED 2-3. OK TO INSTALL NEW INTERCOSTAL.;[05] INSTALLED NEW INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN STA 277 AND STA 294.5 BL 0 IAW DRAWING 141A5400 AND SRM 51-40-02-0G-0;[06] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN STA 277 AND STA 294.5 BL 0 IAW DRAWING 141A5400 AND SRM 51-40-02-0G-0;[07] VERIFIED 5-6.

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 38,769 hrs · 23,511 cycles

LEFT A/C BAY VAPOR BARRIER UPPER ATTACH ANGLE AT WING CENTER SECTION HAS A CRACK FROM FASTENER HOLE AT B.S. 663.75 L.BL 8'. / [01] REMOVED FASTENERS ON L/H SIDE VAPOR BARRIER UPPER ATTACH ANGLE AT STA 663.75 FOR ACCESS TO REPAIR .REF B737-700 SRM 51-40-02-0G-0.;[02] CUT AND REMOVED VAPOR BARRIER UPPER ATTACH ANGLE SECTION AT L/H SIDE STA 663.75 REF B737-700 SRM 51-10-02-0G-0 AND SRM 57-10-10-2R-5 FIG 202 SHEET 4.;[03] VERIFIED 1-2.;[04] PERFORMED HFEC AT CUT OUT AT UPPER ATTACH ANGLE AT L/H SIDE STA 663.75 IAW NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS;[05] PERFORMED HFEC HOLE PROBE INSPECTION ON ALL REMOVED FASTENER LOCATIONS WITHIN REPAIR AREA IAW NDTM PART 6; 51-00-00; PROCEDURE 16. NO CRACKS.;[06] FABRICATED REPAIR PARTS; REPLACEMENT ANGLE AND SPLICE ANGLE MATERIAL USED 2024-T3 0.063' PO# 1742537 AND 2024-T3 0.071' PO#1749426 REF B737-700 SM 57-10-102R-5 FIG 202 TABLE 201.;[07] VERIFIED STEPS #5 AND #6.<BR> OK TO TREAT AND PRIME FABRICATED PARTS.;[08] TREATED AND PRIMED FABRICATED PARTS IAW SRM 51-20-01-0G-0.;[09] VERIFIED STEP 8..O.K. TO INSTALL FABRICATED PARTS.;[10] MIXED 0870C020BM654SKN40 SEALANT AT 19:30; 2/25/22. SQUEEZE OUT TIME BY 15:30; 2/26/22.;[11] INSTALLED REPAIR PARTS AT LEFT A/C BAY VAPOR BARRIER WING CENTER SECTION BS 663.75 LBL 8 IAW SRM 57-10-10-2R-5 AND SRM 51-40-02-0G-0.;[12] VERIFIED STEPS 10 AND 11..;[13] RII NOT USED

Part: FLOOR PANEL — PEELING (CABIN) · airframe 38,769 hrs · 23,511 cycles

CABIN FLOOR PANEL 222BF HAS PEELED UPPER SURFACE FIBERS. 124-004 / [01] RECEIVED NEW FLOOR 222BF. PANEL WILL BE INSTALLED ON CUSTOMER CARD #TTG8Q009XWZK;[02] VERIFIED STEP 1

Part: BULKHEAD — CORRODED · airframe 38,769 hrs · 23,511 cycles

CORROSION SPOTS ON THE AFT END OF THE UPPER FLANGE OF BS 259.5 BULKHEAD (WL 208.1; FROM LBL 11 TO RBL 11) 8-41. INSTALLED EWIS PROTECTION UNDER FLOOR STRUCTURE WHERE PANEL 211 AF FROM BS 259 TO 270 ; RBL 11 TO LBL 11 IAW 20-60-07-913-801. REMOVED FASTENER FOR ACCESS TO REMOVE CORROSION AT AFT END OF UPPER FLANGE OF BS 259 LBL 11 TO RBL 11 IAW SRM 51-40-02-0G-0. REMOVED LIGHT CORROSION ON AREAS IAW SRM 51-10-02-0G-0. REMOVED LIGHT CORROSION ON AREAS IAW SRM 51-10-02-0G-0. FOUND IN LIMITS IAW SRM 53-10-51-1A-1 FIG 105. APPLIED ALODINE & PRIMER ON AREA.

Part: BULKHEAD — DISTORTED (AFT CARGO) · airframe 38,769 hrs · 23,511 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD UPPER LH #141LW SURFACE WAVY/DISTORTED. / [01] FABRICATED AFT CARGO COMPARTMENT FWD BULKHEAD UPPER LH#141JW IAW B737-700 AMM 25-52-01-201-801-NG MATERIALS USED A60SG4W;[02] (CORRECTING STEP 1) FABRICATED AFT CARGO COMPARTMENT FWD BULKHEAD UPPER LH#141LW IAW B737-700 AMM 25-52-01-201-801-NG MATERIALS USED A60SG4W;[03] FINAL INSPECTION; PANEL FABRICATED.

Part: BRACKET — CRACKED (L/H FUSELAGE) · airframe 38,769 hrs · 23,511 cycles

L/H STA 540 UNDER ACCESS DOOR 192CL ANTIC ICE DUCT SUPPORT BRACKET CRACKED / [01] REMOVED AND REPLACED ANTIC ICE SUPPORT BRACKET AT L/H STA 540; INSIDE ABOVE ACCESS DOOR 192CL AS PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED 1.

Part: STIFFENER — CRACKED (L/H FUSELAGE) · airframe 38,769 hrs · 23,511 cycles

FWD OF L/H MAIN WHEEL WELL VERTICAL BULKHEAD STA 663.75 O/B OF A/C AIR EXIT EXHAUST HAS STEFFINER CRACKED @ LOWER END MKD DOT / [01] REMOVED DAMAGE STEFFINER AT FWD OF L/H MAIN WHEEL WELL VERTICAL BULKHEAD STA 663.75 O/B OF A/C AIR EXIT EXHAUST AS PER B737-700 REF SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW STEFFINER AT FWD OF L/H MAI N WHEEL WELL VERTICAL BULKHEAD STA 663.75 O/B OF A/C AIR EXIT EXHAUST AS PER B737-700 REF SRM 51-40-05-0G-0;[03] VERIFIED 1-2.;[04] VERIFIED 1-2. OK TO INSTALL NEW STIFFENER.;[05] INSTALLED NEW STEFFINER AT FWD OF L/H MAI N WHEEL WELL VERTICAL BULKHEAD STA 663.75 O/B OF A/C AIR EXIT EXHAUST AS PER B737-700 REF SRM 51-40-02-0G-0;DWG # 111A1000;[06] VERIFIED STEP #5; NEW STIFFENER INSTALLED.;[07] REMOVED AND REPLACED STEFFINER AT FWD OF L/H MAI N WHEEL WELL VERTICAL BULKHEAD STA 663.75 O/B OF A/C AIR EXIT EXHAUST AS PER B737-700 REF SRM 51-40-02-0G-0.;[08] FINAL INSPECTION; REPLACED STIFFENER.

Part: BULKHEAD — DELAMINATED (FWD CARGO BAY) · airframe 38,769 hrs · 23,511 cycles

FWD CARGO B/H PNL 121JW HAS DELAMATION AND GOUGES. 8-1 / PREPARED AREA FOR REAPAIR DELAMINATION AND GOUGES AT FWD CARGO B/H PANEL # 121JW AS PER B737 AMM 25-52-01-300-804 REPAIRED DELAMINATED AREA AND GOUGES AT FWD CARGO B/H PANEL#121JW AS PER B737 AMM 25-52-01-300-804 .

Part: BULKHEAD — DELAMINATED (FWD CARGO BAY) · airframe 38,769 hrs · 23,511 cycles

FWD CARGO B/H PNL 122HW HAS DELAMINATION AND GOUGES. 8-2 / PREPARED AREA FOR REPAIR DELAMINATIONAN GOUGES AT FWD CARGO B/H PNL # 122HW AS PER B737 AMM 25-52-01-300-804 REPAIRED DELAMINATION AND GOUGES AREA AT FWD CARGO B/H PNL #122HW AS PER B737 AMM 25-52-01-300-804 PREPARED FOR REPAIR AND REAPAIRED DELAMINATION AREA AT FWD CARGO B/H PANEL# 122HW AS PER B737 AMM 25-52-01-300-804.

Part: SHROUD — CRACKED (AFT CARGO) · airframe 38,769 hrs · 23,511 cycles

AFT CARGO FWD B/H SHROUD CRACKED 142NWB. 8-17 / [01] RECEIVED NEW AFT CARGO PANEL 142NWB. PANEL WILL BE INSTALLED ON CUSTOMER CARD #TTG8Q009XUNE.;[02] VERIFIED STEP 1

Part: VAPOR BARRIER — DEBONDED (WHEEL WELL) · airframe 38,769 hrs · 23,511 cycles

LOWER FUSELAGE L/H WHEEL WELL VAPOR BARRIER LBL 35' AND 9' FROM BOTTOM PREVIOUS REPAIR SEALANT DISBONDING / [01] PREPARED DAMAGEAREA FOR DRY-OUT AT VAPOR BARRIER B737-700 51-70-2R-0;[02] VERIFIED STEP #1.;[03] PERFORMED DRY OUT ON L/H VAPOR BARRIER AS PER B737 SRM 51-70-04-2R-10;[04] CORRECTING REF ON STEP 1: PREPARED DAMAGE AREA FOR DRY-OUT AT VAPOR BARRIER PER REF B737-700 SRM 51-70-04-2R-0;[05] VERIFIED 2-3. OK TO INSTALL REPAIR.;[06] VERIFIED STEP #4.;[07] REPAIRED CRACK DAMAGE SIZE 15' ON L/H VAPOR BARRIER LBL. 35' AS PER B737-700 SRM 51-70-04-2R-10 MATERIALS USED PO# 1746221 AND PO# 1690463;[08] VERIFIED STEP #7; CRACKED REPAIRED.;[09] RESTORED FINISHED ON REPAIR AREA PER REF B737 AMM 51-21-73-370-803;[10] REPAIRED CRACK DAMAGE SIZE 15' ON L/H VAPOR BARRIER LBL. 35' AS PER B737-700 SRM 51-70-04-2R-10;[11] STEP #8 CHANGE TO (RII) VERIFIED STEP #7; CRACKED REPAIRED.;[12] NOTE: (RII) FINAL INSPECTION; VERIFIED STEPS #9 AND #10.

Part: SERVICE DOOR — CORRODED · airframe 38,769 hrs · 23,511 cycles

CORROSION. AT LOWER FUSELAGE. EXTERNAL AFT TOILET COMPARTMENT ACCESS DOOR 145AL INTERNAL SKIN AND BONDING LEAD ATTACHED POINT . / [01] REMOVED CORROSION AT LOWER FUSELAGE. EXTERNAL AFT TOILET COMPARTMENT ACCESS DOOR 145AL INTERNAL SKIN AND BONDING LEAD ATTACHED POINT. AS PER B737 SRM 51-10-02-0G-0;[02] VERIFIED STEP 1;[03] PERFORMED UT THICKNESS INSP ON REWORKED AREA. IAW B 737 NDT PART 4 51-00-00 PROCE 3. TOOL 27MG. BC 172139. CALIB DUE 4-1-22. MINNI THICK 0.016'.;[04] ORIGINAL MAT. 0.060' MAT. REMOVED 0.044' MAT. REMAINING 0.016' FOUND TO BE OUT OF LIMITS AS PER B737 SRM 52-40-01-1A-4;[05] VERIFIED 4.;[06] REMOVED AND REPLACED LOWER FUSELAGE EXTERNAL AFT TOILET COMPARTMENT ACCESS DOOR 145AL IAW AMM 52-49-07-400-801;[07] PERFORMED BONDING RESISTANCE CHECK FOUND BETWEEN THE PARAMETERS AS PER REF B737-700 AMM 52-49-07-400-801 <BR>TOOL USED :168692 DUE:16-SEP-22;[08] VERIFIED 6-7.

Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 38,769 hrs · 23,511 cycles

CRACK FOUND AT LH HORIZONTAL LOWER SKIN STAB STA 193.90; 17' FROM REAR SPAR I/B ROW; LENGTH APPROX .875'. CRACK FOUND AT LH HORIONTAL LOWER SKIN STAB STA 193.90 17' FROM REAR SPAR I/B ROW LENGTH APPROX .875'. / [01] APPLIED STRIPPING ON SKIN SURFACE OF REPAIR AREA IN IAW AMM 51-21-11-150-801[18] INSTALLED REPAIR PART AT L/H. HORIZONTAL STABILIZER LOWER SKIN STA. 193.90. 17' FROM REAR SPAR; IAW. B-737-700 SRM.55-10-01-2R-11 FIGURE 204;[19] VERIFIED 18.;[20] APPLIED TOP-COAT TO REPAIR AREA IAW. B-737-700 AMM. 51-21-73-370-803;[21] ACCOMPLISHED PERMANENT REPAIR OF CRACK AT L/H. STAB. LOWER SKIN STA. 193.90 PER B-737-700 SRM. 55-10-01-2R-11.;[22] REMOVED THE DAMAGE AREA OF L/H HORIZONTAL STABILIZER LOWER SKIN STA 193.90 17' FROM REAR SPAR IN IAW SRM 51-10-02-0G-0 AND 55-10-01-2R-11 FIG 204 ; COMPLETED FABRICATIONS OF REPAIR PARTS; DOUBLER AND FILLER. MAT. USED FOR DOUBLER 2024-T3 0.090'. MAT. USED FOR FILLER 2024-T3 0.071' IAW. B-737-700 SRM.51-10-01-2R-11 FIGURE 204 ; INSTALLED REPAIR PART AT L/H. HORIZONTAL STABILIZER LOWER SKIN STA. 193.90. 17' FROM REAR SPAR; IAW. B-737-700 SRM.55-10-01-2R-11 FIGURE 204;[23] VERIFIED 20-22.

Part: SLIDE — FAILED · airframe 38,753 hrs · 23,501 cycles

FOWARD ENTRY ESCAPE SLIDE PRESSURE OUT OF LIMITS ; / [01] R&R FWD ENTRY SLIDE PER MT 725-61-06

Part: BRACKET — LOOSE (FWD SERVICE DOOR) · airframe 38,697 hrs · 23,465 cycles

BRACKET THAT HOLDS FWD SERVICE GIRT BAR LOOSE ; / [01] COMPLIED WITH EA 22-125-00248

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,025 hrs · 23,080 cycles

AFT LT GALLEY (MO 1673) RT OVER WING (MO 1679) BATTERY PACKS /POWER SUPPLIES FAILED TEST. ; / [01] R&R BATTERY PACKS AT AFT LT GALLEY (MO 1673) RT OVER WING (MO 1679) PER AMM 33-51-06.

Part: ACCESS PANEL — STUCK (AFT CARGO DOOR) · airframe 37,735 hrs · 22,911 cycles

AFT CARGO DOOR HANDLE STUCK IN STOW POSITION ; / [01] R&R ACCESS PANELS TO OPEN AFT CARGO DOOR LUBE DOOR HANDLE OPS CK GOOD IAW MM REF. 52-31-14; [02] R&R ACCESS PANELS TO OPEN AFT CARGO DOOR LUBE DOOR HANDLE OPS CK GOOD IAW MM REF 52-31-14

Part: TRUNNION — CORRODED (LT MLG) · airframe 33,784 hrs · 20,459 cycles

L/H MAIN LANDING GEAR, FORWARD TRUNNION SUPPORT FITTING, LOWER OUTBOARD LUG FACE HAD EVIDENCE OF CORROSION. / REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 33,784 hrs · 20,459 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG, OUTER LUG FACE HAD EVIDENCE OF CORROSION. / REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 33,784 hrs · 20,459 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG, OUTER LUG FACE HAD EVIDENCE OF CORROSION. / REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 33,784 hrs · 20,459 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING, UPPER INBOARD LUG, OUTER FACE HAD EVIDENCE OF CORROSION. / REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 33,784 hrs · 20,459 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG, OUTER LUG FACE HAD EVIDENCE OF CORROSION. / REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 33,784 hrs · 20,459 cycles

R/H MAIN LANDING GEAR - FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD LUG OUTER LUG FACE HAD EVIDENCE OF CORROSION. / REPAIRED LUG PER EA.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 33,738 hrs · 20,418 cycles

MAIN CABIN LOWER FLOOR SUPPORT ANGLE CRACKED AT BS. 540, LBL 1. / R&R ANGLE PER SRM.

Part: ANGLE — CRACKED (BS 540) · airframe 33,738 hrs · 20,418 cycles

MAIN CABIN LOWER FLOOR SUPPORT ANGLE CRACKED AT BS. 540, RBL 1. / R&R ANGLE PER SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 33,739 hrs · 20,418 cycles

L/H HORIZONTAL STABILIZER RIB #6 STAB STA 138.70 THE #3 STIFFENER IS CRACKED. VERIFIED CRACK AT L/H HORIZONTIAL STAB RIB #6; STAB STA.138.70 STIFFNER #3. PER BOEING NDT MANUAL PART 6; 51-00-00 PROC.23 / REPAIRED #3 STIFFENER PER SRM 55-10-09-2R-4.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 33,739 hrs · 20,418 cycles

L/H HORIZONTAL STABILIZER RIB #6 STAB STA 138.70 THE #2 STIFFENER IS CRACKED. VERIFIED CRACK AT L/H HORIZONTIAL STAB RIB #6; STAB STA.138.70 STIFFNER #2. PER BOEING NDT MANUAL PART 6; 51-00-00 PROC.23 / INSTALLED REPAIR PER SRM 55-10-09-2R-4.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 33,738 hrs · 20,418 cycles

LT HORIZONTAL STABILIZER RIB NR 5 STAB STA 129.50 THE NR 4 STIFFENER CRACKED. R&R STIFFENER PER SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 33,738 hrs · 20,418 cycles

LT HORIZONTAL STABILIZER RIB NR 5 STAB STA 129.50 THE NR 2 STIFFENER CRACKED. R&R STIFFENER PER SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 33,738 hrs · 20,418 cycles

LT HORIZONTAL STABILIZER RIB NR 5 STAB STA 129.50 THE NR 3 STIFFENER CRACKED. R&R STIFFENER PER SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 33,738 hrs · 20,418 cycles

LEFT HORIZONTAL STABILIZER RIB NR 4 AT STAB. STA. 120.30 WAS FOUND CRACKED AT THE NR 3 STIFFENER. REPAIRED THE STIFFENER PER SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 33,738 hrs · 20,418 cycles

LT HORIZONTAL STABILIZER FRONT SPAR STIFFENER AT STAB STA 120.30 CRACKED. R&R STIFFENER PER SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 33,738 hrs · 20,418 cycles

LEFT HORIZONTAL STABILIZER RIB 4 HSS 120.30, THE NR 4 STIFFENER MOST AFT STIFFENER CRACKED. REPAIRED THE STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 33,738 hrs · 20,418 cycles

L/H HORIZONTAL STABILIZER RIB 6, HSS 138.70, THE NR 3 STIFFENER WAS CRACKED. REPAIRED THE STIFFENER PER SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 33,738 hrs · 20,418 cycles

LT HORIZONTAL STABILIZER RIB 6 HSS 138.70, THE NR 2 STIFFENER WAS CRACKED. REPAIRED THE STIFFENER IAW SRM.

Part: HOOK — CORRODED (EMERGENCY EXIT) · airframe 33,738 hrs · 20,418 cycles

L/H EMERGENCY EXIT HATCH ESCAPE STRAP HOOK HAD LIGHT SURFACE CORROSION. / R&R HOOK PER AMM.

Part: PLATE — CRACKED (RT TE FLAP TRACK) · airframe 33,738 hrs · 20,418 cycles

RIGHT WING WIGGLE PLATE INBOARD OF NR 6 FLAP TRACK CRACKED. R & R WIGGLE PLATE IAW SRM.

Part: SEAT TRACK — OUT OF LIMITS (COCKPIT) · airframe 33,122 hrs · 20,033 cycles

CAPTAIN'S AFT INBOARD SEAT TRACK OUT OF LIMITS IN FLIGHT DECK. / R&R SEAT TRACK PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 33,122 hrs · 20,033 cycles

EMERGENCY LIGHTING BATTERY PACK AT LOCATION M1672 FAILED TEST. / R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 33,122 hrs · 20,033 cycles

EMERGENCY LIGHTING BATTERY PACK AT LOCATION M1674 FAILED TEST. / R&R BATTERY PACK PER AMM.

Part: SEAL — CRACKED (LH HOR STAB) · airframe 33,122 hrs · 20,033 cycles

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

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 33,122 hrs · 20,033 cycles

EMERGENCY LIGHTING BATTERY PACK AT LOCATION M1675 FAILED TEST. / R&R BATTERY PACK PER AMM.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 32,708 hrs · 19,758 cycles

FORWARD GALLEY FA FLASHLIGHT LOWER NOT BLINKING. R&R FLASHLIGHT BATTERY IAW AMM.

Part: SUPPORT ANGLE — CRACKED (RT WING PANEL) · airframe 30,993 hrs · 18,669 cycles

R/H WING TRAILING EDGE PANEL SUPPORT ANGLE CRACKED OUTBOARD END ANGLE JUST INBOARD OF DEFLECTION RIB. / R&R ANGLE PER SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 30,758 hrs · 18,517 cycles

RT HORIZONTAL STABILIZER STA 129.5 RIB CRACKED AT 2ND VERTICAL STIFFENER FROM FORWARD END. REPAIRED STIFFENER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 30,758 hrs · 18,517 cycles

RT HORIZONTAL STAB VERTICAL RIB AT STA 126.50,THIRD STIFFENER CRACKED. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 30,758 hrs · 18,517 cycles

RT HORIZONTAL STAB VERTICAL RIB AT STA 120.30,THIRD STIFFENER CRACKED. REPAIRED RIB PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,870 hrs · 17,950 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 29,246 hrs · 17,541 cycles

R2 DOOR EVAC SLIDE FAILED INSPECTION. R&R SLIDE IAW MT.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,518 hrs · 17,057 cycles

RT WING TRAILING EDGE EXTERNAL EMERGENCY LIGHT INOP. R&R POWER SUPPLY PER AMM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 27,528 hrs · 16,422 cycles

RIGHT EXTERIOR EMERGENCY LIGHT LENS CRACKED AFT WING POSITION. R & R THE LENS IAW AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 27,388 hrs · 16,340 cycles

AFT CARGO FWD CORNER THRESHOLD IS CRACKED. / REMOVED AND REPLACED AFT CARGO CORNER THRESHOLD PER AMM 53-11-02. LEAK CHECK TO BE COMPLIED ON TASK 721-000-00-01.

Part: FLOOR SUPPORT — CRACKED (BS 294-312) · airframe 27,388 hrs · 16,340 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 294.5 TO 312, LBL 11.16. R & R THE FLOOR SUPPORT IAW SRM.

Part: ANGLE — CRACKED (BS 303) · airframe 27,388 hrs · 16,340 cycles

FORWARD ENTRY ZEE ANGLE CRACKED AT BS 303.9. REPAIRED THE ANGLE IAW EA.

Part: FAIRING — CRACKED (LT WING) · airframe 27,388 hrs · 16,340 cycles

# 3 FLAP CANOE FAIRING 542BB FWD LIP IS CRACKED. / REPAIRED PER E/A 1-757-14866 PART 1; E/A 1-757-14866 PART 2; AND E/A 1-A57-6168.

Part: STRAP — CORRODED (BS 1030) · airframe 27,388 hrs · 16,340 cycles

AFT PASSENGER FLOOR STRUCTURE BONDED STRAP CORRODED ON FLOOR PAN AT BS 1030, LBL 4. R & R THE STRAP IAW SRM.

Part: CAP — CORRODED (FWD CARGO BAY) · airframe 27,388 hrs · 16,340 cycles

SMALL SPOT OF CORROSION AROUND FASTENER HOLE IN TRANSITION ANGLE AFT OF FORWARD CARGO DOOR CUTOUT AT STATION 500A +6 INCHES RBL24. / REF NRC# G530976; REMOVED AND REPLACED R/H TRANSITION ANGLE FROM STA 500A TO 500D PER SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 27,388 hrs · 16,340 cycles

FLOOR SUPPORT CRACKED IN THE FORWARD WET AREA BETWEEN BS 312 TO 328, LBL 46. R & R THE FLOOR SUPPORT IAW SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 27,388 hrs · 16,340 cycles

AFT CORNER SCUFF PLATE IN AFT CARGO COMPARTMENT CRACKED . / REPAIRED BY VENDOR AIRCRAFT DUCTING REPAIR INC ON 15FEB18 UNDER RO# 7530220-AHR. SCUFF PLATE TO BE REINSTALLED ON TASKCARD 753-140-00-02Y.

Part: STRIP — CRACKED (RT HORIZ STAB) · airframe 27,388 hrs · 16,340 cycles

RT HORIZ STAB PANEL 343CB T/E HAS NUMEROUS CRACKS AT FASTENERS [MARKED]. / REMOVED OLD AND INSTALLED NEW FAIRING STRIP THAT WAS CRACKED REF SRM 51-40-02.

Part: FAIRING — CRACKED (RT WING) · airframe 27,388 hrs · 16,340 cycles

#6 FLAP TRACK CANOE FAIRING HAS A SMALL CRACK ON THE INTERIOR SURFACE. / REPAIRED PER E/A 1-A57-6168.

Part: FAIRING — CRACKED (LT HORIZ STAB) · airframe 27,388 hrs · 16,340 cycles

LT HORIZ STAB PANEL 333DB T/E HAS NUMEROUS CRACKS AT FASTENERS [MARKED]. / REMOVED OLD AND INSTALLED NEW FAIRING STRIP THAT WAS CRACKED REF SRM 51-40-02.

Part: FAIRING — CRACKED (RT HORIZ STAB) · airframe 27,388 hrs · 16,340 cycles

RT HORIZ STAB PANEL 343DB T/E HAS NUMEROUS CRACKS AT FASTENERS [MARKED]. / REMOVED OLD AND INSTALLED NEW FAIRING STRIP THAT WAS CRACKED REF SRM 51-40-02.

Part: FAIRING — CRACKED (LT HORIZ STAB) · airframe 27,388 hrs · 16,340 cycles

LT HORIZ STAB PANEL 333CB T/E HAS NUMEROUS CRACKS AT FASTENERS [MARKED]. / REMOVED OLD AND INSTALLED NEW FAIRING STRIP REF SRM 51-40-02.

Part: FAIRING — CRACKED (LT WING) · airframe 27,388 hrs · 16,340 cycles

#3 FLAP TRACK CANOE FAIRING HAS A SMALL CRACK ON THE INTERIOR SURFACE. / REPAIRED #3 FLAP TRACK CANOE FAIRING ON THE INTERIOR SURFACE PER EA# 1-A57-6168 REV 2SEE THIS CARD FOR INDIVIDUAL SIGN OFFS

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 27,128 hrs · 16,176 cycles

FORWARD UPPER EMERGENCY FLASHLIGHT INOPERATIVE. R & R THE BATTERY IAW MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 25,534 hrs · 15,147 cycles

L1 DOOR EMERGENCY LIGHT LENS MOUNT BROKEN. R & R THE LENS ASSY IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 24,694 hrs · 14,608 cycles

EMERGENCY LIGHTING BATTERY PACK FAIL CAPACITY TEST AT LOCATION M01670. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 24,694 hrs · 14,608 cycles

EMERGENCY LIGHTING BATTERY PACK FAIL CAPACITY TEST AT LOCATION M01675. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 24,694 hrs · 14,608 cycles

EMERGENCY LIGHTING BATTERY PACK FAIL CAPACITY TEST AT LOCATION M01672. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 24,694 hrs · 14,608 cycles

EMERGENCY LIGHTING BATTERY PACK FAIL CAPACITY TEST AT LOCATION M01669. R&R BATTERY PACK PER AMM AND DWG .

Part: WEB — CORRODED (BS 781-829) · airframe 24,655 hrs · 14,583 cycles

AFT CARGO BAY THRESHOLD WEB CORRODED BETWEEN BS 781 TO 829, RBL 29. R & R THE THRESHOLD WEB IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,655 hrs · 14,583 cycles

RT FORWARD EXTERNAL EMERGENCY EXIT LIGHT INOP. R&R BULB PER AMM.

Part: MEGAPHONE — INOPERATIVE (AFT CABIN) · airframe 23,468 hrs · 13,860 cycles

AFT MEGAPHONE INOPERATIVE. R & R THE MEGAPHONE IAW AMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 20,859 hrs · 12,272 cycles

LEFT CREASE BEAM CORRODED AT STATION 727. REPAIRED BEAM IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 20,859 hrs · 12,272 cycles

CENTER WING REAR SPAR, VAPOR WEB CRACKED, AT BS 663, LBL 34. REPAIRED WEB IAW EA.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 20,859 hrs · 12,272 cycles

MAIN LANDING GEAR WW BULKHEAD WEB CRACKED AT STA 663, RBL42, WL 199. REPAIRED WEB IAW SR.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 20,859 hrs · 12,272 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT SHIELD CORRODED, BETWEEN BS 767 - 792, RT SIDE. R & R SHIELD IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,859 hrs · 12,272 cycles

FORWARD CARGO BAY, AFT CTR BULKHEAD SUPPORT CORRODED, AT BS 500D, BETWEEN LBL 25 TO RBL 25. R & R SUPPORT IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 20,859 hrs · 12,272 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED, BETWEEN BS 500 - 500A, RT SIDE. R & R SHIELD IAW SRM.

Part: BRACKET — LOOSE (L1 DOOR) · airframe 20,091 hrs · 11,836 cycles

L1 DOOR SLIDE GIRT BAR BRACKET LT LOOSE. SECURED BRACKET IAW MM.

Part: PANEL — CRACKED (LT MLG WW) · airframe 15,950 hrs · 9,417 cycles

LEFT WW FWD BULKHEAD FIBERGLASS PANEL CRACKED. REPAIRED PANEL IAW EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 13,506 hrs · 8,014 cycles

LT BATTERY PACK FAILED CAPACITY TEST AT ROW 1. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 13,506 hrs · 8,014 cycles

LT AFT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 10,232 hrs · 6,044 cycles

PASSENGER CABIN EMERGENCY FLOOR LIGHTING LENS CRACKED BETWEEN ROW 11 TO ROW 20. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 10,232 hrs · 6,044 cycles

FLOOR EMERGENCY EXIT LIGHT LENS AT 4C IS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 9,456 hrs · 5,555 cycles

EMERGENCY EGRESS LIGHT AT EMERGENCY EXIT HAS 2ND RED LENS FROM FWD IS BROKEN. REMOVED AND REPLACED RED LENS 2ND FROM FWD AT THE EMERGENCY EXIT IAW MM 33-51-12-960-801, LIGHT OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,456 hrs · 5,555 cycles

EMERGENCY EGRESS LIGHT AT EMERGENCY EXIT HAS 2ND LIGHT FROM FWD IS INOP. RELAMPED 2ND LIGHT FROM FWD AT EMERGENCY EXIT AND OPERATIONAL CHECKED IAW AMM 33-51-12-960-801, OPS CHECK GOOD.

Part: LENS — LOOSE (R2 DOOR) · airframe 9,456 hrs · 5,555 cycles

R2 DOOR SLIDE LENS LOOSE. SECURED R2 DOOR SLIDE INSPECTION IAW BOEING SOPM 20-50-12 PARA AX

Part: LENS — MISSING (CABIN) · airframe 9,456 hrs · 5,555 cycles

EGRESS LIGHT LENS MISSING AT SEAT ROWS 6 9 AND 18ABC. REPLACED MISSING 3EA CLEAR EGRESS LIGHT LENS AT SEAT ROWS 6 9 AND 18ABC IAW DRAWING 33500006 AND AMM 25-27-31-400-801-001 STEP 3D 10.

Part: BATTERY PACK — FAILED (CABIN) · airframe 9,220 hrs · 5,419 cycles

RIGHT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER MM & SSM.

Part: LENS — CRACKED (CABIN) · airframe 9,220 hrs · 5,419 cycles

LEFT EEPLS LENS CRACKED BETWEEN ROW 1 TO ROW 12. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 9,220 hrs · 5,419 cycles

LEFT EEPLS LENS CRACKED BETWEEN ROW 14 TO ROW 23. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 9,220 hrs · 5,419 cycles

LEFT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER MM & SSM.

Part: FAN — FAULTY (AC BAY) · airframe 7,577 hrs · 4,437 cycles

FLIGHT ATTENDANTS REPORTED SMELL OF SMOKE IN CABIN ON FINAL APPROACH. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: COVER — MISSING (CABIN) · airframe 7,489 hrs · 4,398 cycles

LEFT EEPLS COVER MISSING AT ROW 12. REMOVED AND REPLACED EEPLS PER M/M.

Part: LENS — MISSING (CABIN) · airframe 6,602 hrs · 3,880 cycles

LT EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 5,926 hrs · 3,487 cycles

EMERGENCY EXIT LIGHT BULB BROKEN AT ROW 15. REMOVED AND REPLACED BULB PER MM.

Part: LENS — BROKEN (CABIN) · airframe 5,926 hrs · 3,487 cycles

EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 15. R&R LENS PER MM.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 5,867 hrs · 3,451 cycles

DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: REGULATOR — FAULTY (AC BAY) · airframe 1,957 hrs · 1,164 cycles

DECLARED EMERGENCY. ON ARRIVAL OUT OF 32000FT "CABIN AH" HORN - CABIN WENT TO 10,500FT. REMOVED AND REPLACED HIGH PRESSURE REGULATOR AND HIGH PRESSURE BLEED VAVLE PER MM.