N219WN

Part: HANDLE — CRACKED (ZONE 800) · airframe 66,160 hrs · 39,809 cycles

THE RIGHT WING EMERGENCY EXIT DOOR HANDLE MOLDING IS CRACKED. REMOVED AND REPLACED THE RT WING EMERGENCY EXIT DOOR HANDLE MOLDING IAW AMM 52-22-51.

Part: FITTING — LOOSE (ZONE 800) · airframe 64,915 hrs · 39,066 cycles

R1 FWD SERVICE DOOR; GIRT BAR FITTINGS; FWD AND AFT; LOOSE.<[01] TIGHTENED R1 FWD SERVICE DOOR GIRT BAR FITTINGS FWD AND AFT PER AMM 25-66-02-400-801; OPS CHECK CHECK GOOD.;[02] REJECT - BOTH FWD AND AFT GIRT BAR FITTINGS REMAIN LOOSE.;[03] TIGHTENED R1 FWD SERVICE DOOR GIRT BAR FITTINGS FWD AND AFT IAW AMM 25-66-02-400-801; OPS CHECK CHECK GOOD.;[04] VERIFIED

Part: FUSE — INOPERATIVE (ZONE 200) · airframe 64,915 hrs · 39,067 cycles

FSD HEADER PANEL AND FWD LAV 'A' EMERGENCY EXIT LIGHT IN-OP<[01] REPLACED FUSE AT POWER SUPPLY OF BATTERY PACK M1675 AND PERFORMED GOOD EMERGENCY EXIT LIGHT TEST OF FWD HEADER PANEL AND FWD LAV 'A' IAW AMM 33-51-06-960-804.;[02] COMPLETE

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,915 hrs · 39,067 cycles

CABIN FLOOR PANEL 222BF HAS TOP SURFACE DELAMINATION.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED CABIN FLOOR PANEL 222BF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-50D ITEM96.;[02] VERIFIED JOB COMPLETE

Part: FITTING — OUT OF ROUND (ZONE 100) · airframe 64,915 hrs · 39,067 cycles

OUT OF ROUND HOLE FOUND ON BS727 INNER CHORD RH STR-18A UPPER FASTENER; MOST OUTBOARD LAYER OF STACK-UP. UNABLE TO COMPLETE NDI INSPECTION OF HOLE. <[01] REMOVED AND REPLACED UPPER FITTING BS 727 STR 18A IAW SRM 51-40-05; SRM 51-40-02; DWG #146A0062 REV-; DWG #144A7321 REV A.; [02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,915 hrs · 39,067 cycles

CABIN FLOOR PANEL 221GF HAS TOP SURFACE DELAMINATION.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED CABIN FLOOR PANEL 221GF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-50D ITEM 295.;[02] VERIFIED JOB COMPLETE

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,915 hrs · 39,067 cycles

CABIN FLOOR PANEL 221EF HAS TOP SURFACE DELAMINATION.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 221EF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,915 hrs · 39,067 cycles

CABIN FLOOR PANEL 222CF HAS TOP SURFACE DELAMINATION.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 222CF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: PANEL — DEBONDED (ZONE 600) · airframe 64,915 hrs · 39,067 cycles

PANEL 621ZB FWD. CORNER DISBONDED.<[01] PANEL 621ZB WITH FWD CORNER DISBONDED WAS REPAIRED IAW SRM 57-41-01-2R-6.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FORMER — CRACKED (ZONE 100) · airframe 64,915 hrs · 39,067 cycles

WING TO BODY FAIRING FORMER IS CRACKED BS 500D BETWEEN STRINGER 19 AND 20 R/H<[01] REMOVED AND INSTALLED NEW FAIRING FORMER BS 500D BETWEEN STRINGER 19 AND 20 R/H IAW SRM 51-40-02-0G-0 AND DWG 116A3010 REV: A; 149A7101 REV: -.

Part: SKIN — CRACKED (ZONE 300) · airframe 64,915 hrs · 39,067 cycles

CRACK ON RH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 11.75' FROM FWD EDGE; .25' IN LENGTH (MARKED)<[01] 'REPAIRED PER EA 25-155-00704 WITH REPETITIVE INSPECTION PROGRAM DEFINED IN EA 25-155-00704-INSP.';[02] COMPLETE

Part: STIFFENER — CRACKED (ZONE 300) · airframe 64,915 hrs · 39,067 cycles

LH STAB RIB #4 STA 120.30 STIFFENER #2 AND #4 SHOWN CRACK<[01] REPAIRED LH STAB RIB #4 STA 120.30 STIFFENER #2 AND #4 IAW SRM 55-10-09-2R-4 REPAIR 4 AND SRM 55-10-09-2R-5 REPAIR 5 RESPECTIVELY.;[02] VERIFIED CORRECTIVE ACTION;[03] ALL RII STEPS COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 64,915 hrs · 39,067 cycles

FLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 242DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 64,915 hrs · 39,067 cycles

FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241DF USING BMS 4-17 TY6 LOT#1594495-1; INSTALLED INSERTS USING BMS 5-107 LOT#AK4FA2417A/A; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2025; PART MARKED AND APPLIED TAPE IAW SRM 53-00-50-2R-0 PARA 1.A(NOTE); 5.S AND BOEING DWG 144A5810 ID:0128;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.

Part: PANEL — CRACKED (ZONE 100) · airframe 64,915 hrs · 39,067 cycles

STA 540 BREAK PANEL IS CRACKED AT LBL 1; WL 208. <[01] REMOVED AND REPLACED WITH NEW BREAK PANEL AT 540 LBL 1; WL 208. REMOVE AND REINSTALL FLOOR PANEL 231UF TO ACCESS BREAK PANEL AT STA 540 LBL 1 WL 208. FLOOR PANEL 231UF WILL BE INSTALLED ON CARD#TTG8Q00Z5EM LOCATED AND DRILLED REPLACEMENT BREAK PANEL IAW SRM 51-40-02-0G-0. REMOVED PANEL BREAK ASSY AT BS 540; BL0-24L PER SRM 51-40-02-0G-0 OK TO INSTALL NEW PART. INSTALLED NEW BREAK PANEL AT STA 540 LBL 1 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A5240 SHEET 14; REV -; DATE: 04/11/02 AND DWG 143A0063 SHEET 44 REV A DATE: 01/25/05. VERIFIED APPLICABILITY OF SRM 51-40-02-0G-0. NO ALLOWABLE DAMAGE FOUND FOR PART.; [02] VERIFIED ALL STEPS; CORRECTION ACTION ITEM 1; MEASUREMENT FIELD COMPLETE; CARD COMPLETE.

Part: RIB — CRACKED (ZONE 300) · airframe 64,915 hrs · 39,067 cycles

RT HORIZ STAB L/E (341B) RIB AT LE STA 95.96 IS CRACKED AT UPPER AFT EDGE<[01] REMOVED AND REPLACED RIB AT R/H LE STAB STA 95.96 IAW SRM 51-40-02-0G-0 AND DWG. 186A1001-16; REV. A.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 64,915 hrs · 39,067 cycles

FLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241EF USING BMS 4-17 TY6 LOT#1594495-1; INSTALLED INSERTS USING BMS 5-107 LOT#AK4FA2417A/A; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2025; PART MARKED AND APPLIED TAPE IAW SRM 53-00-50-2R-0 PARA 1.A(NOTE); 5.S AND BOEING DWG 144A5810 ID:0129;[02] VERIFIED CORRECTIVE ACTION STEP 1. TASK CARD COMPLETE.;[03] TASK CARD COMPLETE.

Part: RIB — CRACKED (ZONE 300) · airframe 64,915 hrs · 39,067 cycles

LT HORIZ STAB L/E (331B) RIB AT LE STA 95.96 IS CRACKED AT LOWER AFT EDGE<[01] REPLACED A NEW RIB L/H HORIZONTAL STAB L/E (331B) AT L/E STA 95.96 IAW SRM 51-40-02 AND BOEING DWG 186A1001 SH 10

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 64,915 hrs · 39,067 cycles

LEFT HAND BS 663 COMPOSITE VAPOR BARRIER HAS MULTIPLE CRACKS AT LBL 28; WL 164. <[01] L/H VAPOR BARRIER BS663 MULTIPLE CRACKS AT LBL 28 WL 164 WERE REPAIRED IAW SRM 51-70-04-2R-10.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,086 hrs · 38,557 cycles

L1; R1; AND FWD GALLEY EMERGENCY EXIT LIGHTS INOP.<[01] REMOVED AND REPLACED LH FWD BATTERY PACK IAW AMM 33-51-06. OP CHECK GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 63,803 hrs · 38,388 cycles

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

Part: TAILPIPE — FIRE (NR 2 ENGINE) · airframe 62,956 hrs · 37,847 cycles

#2 ENGINE TAIL PIPE FIRE AT GATE<[01] LP 2602505 AP 3395119 INSPECTED INLET AND EXHAUST FOUND OIL ACCUMULATION IN THE CENTER EXHAUST PLUG CAVITY NO OTHER DEFECTS NOTED. OIL CONSUMPTION AND PRESSURE ARE WITHIN NORMAL LIMITS. REF FIM 71-05 TASK 811. POWERPLANT ENGINEERING WILL MONITOR. AC OKAY FOR SERVICE.

Part: IDG — FAULTED (NR 2 GENERATOR) · airframe 62,541 hrs · 37,605 cycles

DURING CRUISE FLIGHT @FL370 #2 IDG SHOWED SOURCE OFF LIGHT AND TRANSFER BUS OFF LIGHT ILLUMINATED.<[01] R & R #2 ENG IDG IAW AMM 24-11-11. NO DEFECTS NOTED.

Part: SIGN — WRONG PART (ZN 200 FUS TOP) · airframe 61,713 hrs · 37,057 cycles

LOWER RT OVER WING EMERGENCY EXIT SIGN DOESN'T HAVE A DIRECTION ARROW.<[01] REMOVED AND REPLACED SIGN IAW AMM 33-51-01

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 61,713 hrs · 37,057 cycles

EMERGENCY EXIT LIGHT LENS IS MISSING AT 4ABC.<[01] INSTALLED NEW COVER IAW AMM 25-24-31

Part: SLIDE — OUT OF ADJUST (AFT SERVICE DOOR) · airframe 61,539 hrs · 36,964 cycles

AFT SERVICE DOOR SLIDE LOOSE<[01] REMOVED SLIDE WITH COMPARTMENT FROM DOOR AND ADJUSTED. SLIDE SECURE AND GAUGE VISIBLE. REINSTALLED SLIDE IAW MT#725-61-06.

Part: LENS — LOOSE (ZN 200 FUS TOP) · airframe 60,896 hrs · 36,568 cycles

CABIN AISLE LIGHT ROW 11 DEF COVER CAME OFF<[01] OK TO CONTINUE PER MEL 33-15-02 SP1;[02] INSTALLED LENS IAW AMM 33-51-03

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 60,642 hrs · 36,414 cycles

RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL PER AMM 53-31-31.

Part: FASTENER — BROKEN (ZN 800 DOOR) · airframe 60,490 hrs · 36,324 cycles

FORWARD SERVICE DOOR FIRST BAR HOLDER BROKEN<[01] REMOVED AND REPLACED FASTENERS ON FWD SERVICE DOOR SLIDE GIRT BAR AFT HOOK PER SRM 51-40-02

Part: LIGHT — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 60,184 hrs · 36,120 cycles

FWD SERVICE DOOR EMERGENCY LIGHT EXIT LIGHT COVER FALLS OFF.<[01] R&R FWD SERVICE DOOR EMERGENCY EXIT LIGHT ASSEMBLY REF AMM 33-1-01.

Part: STRAP — LOOSE (ZN 200 FUS TOP) · airframe 59,759 hrs · 35,844 cycles

RH EMERGENCY EXIT ASSIST STRAP COMPARTMENT NOT SECURE<[01] RE-SECURED RH EMERGENCY EXIT ASSIST STRAP COMPARTMENT; PER AMM 52-22-51

Part: TRACK — CORRODED (ZN 100 FUS LOWER) · airframe 58,693 hrs · 35,154 cycles

CORROSION TRACK RBBL 13.84 LOCATED BTW STA 787 TO STA 807 PLUS 3 INCHES WL 157.5 AT AFT CARGO COMPARTMENT 2023-<[01] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00HU0PW;[02] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00HU0PW

Part: BRACKET — BROKEN (ZN 500 LEFT WING) · airframe 58,693 hrs · 35,154 cycles

BROKEN SUPPORT BRACKET ON ACCESS PANEL 551FB LT WING 2023-113098<[01] REPLACED SUPPORT BRACKET ON ACCESS PANEL 551FB LT WING IAW B737-700 SRM 51-40-02 AND DRAWING # 115A2710 REV: B. TOOK MEASURE OF CRACK IS : L= 0.950?. TOOL USED CALIPER P/N: 500-752-20; S/N:B20317422; DUE DATE:29-AUG-23. EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 57-51-02-1A-1 ALLOWABLE DAMAGE 1.;[02] REPLACED SUPPORT BRACKET ON ACCESS PANEL 551FB LT WING IAW B737-700 SRM 51-40-02 AND DRAWING # 115A2710 REV: B. TOOK MEASURE OF CRACK IS : L= 0.950?. TOOL USED CALIPER P/N: 500-752-20; S/N:B20317422; DUE DATE:29-AUG-23. EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 57-51-02-1A-1 ALLOWABLE DAMAGE 1.

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 58,690 hrs · 35,153 cycles

CUSTOMER REQUEST AAI CRACK ON ANGLE LOCATED RACEWAY PANEL AREA CAPTAIN SIDE AT COCKPIT 2023-113089<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: 48VFL11; S/N: AE-31448; DUE DATE: 14-JUN-23.;[02] REPLACED ANGLE LOC. RACEWAY PANEL AREA CAPTAIN SIDE AT COCKPIT IAW B737-700 SRM-51-10-02; ITEM 9 SEE INDIVIDUAL SIGN-OFF BELOW;[03] TASK CARD COMPLETED

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,693 hrs · 35,154 cycles

CRACK ANGLE LOCATED BTW STA 907 TO STA 927 STR 25R TO STR 27R FWD POSITION AFT CARGO COMPARTMENT 2023-113080<[01] REPLACED ANGLE LOCATED BTW STA 907 TO STA 927 STR 25R TO STR 27R FWD POSITION AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A7221 REV. - SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: TRACK — CORRODED (ZN 100 FUS LOWER) · airframe 58,693 hrs · 35,154 cycles

CORROSION TRACK RBBL 13.84 LOCATED BTW STA 787 TO STA 807 PLU 3 INCHES WL 157.5 AT AFT CARGO COMPARTMENT 2023-113084<[01] PERFORMED REPAIR ON CARGO TRACK SECTION RBBL 13.84 LOCATED BTW BS747 MORE 7? TO BS887 I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR 3 FIGURE 203 ALTERNATIVE 3. SEE INDIVIDUAL SIGN OFF BELLOW;[02] TASK CARD COMPLETED <BR>PERFORMED REPAIR ON CARGO TRACK SECTION RBBL 13.84 LOCATED BTW BS747 MORE 7? TO BS887 I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR 3 FIGURE 203 ALTERNATIVE 3. SEE INDIVIDUAL SIGN OFF BELLOW<BR>RII

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 58,693 hrs · 35,154 cycles

CORROSION SUPPORT ZEE LOCATED BTW 737D TO STA 767 AT LEVEL STR 25R WL 156.5 AT AFT CARGO COMPARTMENT 2023-113083<[01] REPLACED SUPPORT ZEE LOCATED BTW 727 TO STA 767 AT LEVEL STR 25R WL 156.5 AT AFT CARGO COMPARTMENT AND FASTENERS I.A.W B737-700 SRM 51-40-02 AMD DWG 146A7500 REV. A SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTIVE ACTION 1 COMPLETE RII <BR><BR>REPLACED SUPPORT ZEE LOCATED BTW 727 TO STA 767 AT LEVEL STR 25R WL 156.5 AT AFT CARGO COMPARTMENT AND FASTENERS I.A.W B737-700 SRM 51-40-02 AMD DWG 146A7500 REV. A SEE INDIVIDUAL SIGN OFF BELOW

Part: TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 58,693 hrs · 35,154 cycles

CRACK CARGO TRACK LOCATED BS747 RBL13 AND WL156 AT AFT CARGO COMPARTMENT 2023-113064<[01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: B20189511 DUE DATE: 12-OCT-23.;[02] PERFORMED REPAIR ON CARGO TRACK LOCATED BTW BS727E MORE 7.5? TO BS747 MORE 11? RBL13 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 3 SEE INDIVIDUAL SIGNOFFS BELOW;[03] TASK CARD COMPLETED <BR>PERFORMED REPAIR ON CARGO TRACK LOCATED BTW BS727E MORE 7.5? TO BS747 MORE 11? RBL13 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 3 SEE INDIVIDUAL SIGNOFFS BELOW<BR>RII

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 58,693 hrs · 35,154 cycles

CRACK REAR SPAR CORRUGATED PLATE LOCATED AT IRSS 216 AT LT WING 2023-113071<[01] REPLACED REAR SPAR CORRUGATE PLATE LOCATED AT IRSS 216 AT LT WING I.A.W. B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG 115A2001 SHEET 30 REV.A. DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700 57-20-10 CRACK LENGTH: 0.670? TOOL USED CALIPER P/N:500-196-30 S/N: B21141563 DUE DATE: 30/NOV/23;[02] COMPLETED STEP 1

Part: SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 58,693 hrs · 35,154 cycles

CRACK ANGLE - SUPPORT LOCATED STA 867 AT LEVEL STR 26L AFT CARGO COMPARTMENT 2023-113074<[01] REPLACED ANGLE - SUPPORT LOCATED STA 867 AT LEVEL STR 26L AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG #149A8102 REV:-;[02] REPLACED ANGLE - SUPPORT LOCATED STA 867 AT LEVEL STR 26L AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG #149A8102 REV:-

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,693 hrs · 35,154 cycles

CRACK ANGLE LOCATED BTW STA 907 TO STA 927 STS 25L TO STR 27L AFT CARGO COMPARTMENT 2023-113072<[01] REPLACED ANGLE LOCATED BTW STA 907 TO STA 927 STS 25L TO STR 27L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-20-02 ITEM 9 AND DWG 147A7221 REV. -. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 58,693 hrs · 35,154 cycles

CRACK CARGO TRACK LOCATED BS767 LBL17 AND WL156 AT AFT CARGO COMPARTMENT 2023-113063<[01] TOOL USED: DIGITAL CALIPER; P/N: 500-193-30; S/N:0000293; DUE DATE:12-OCT-23.;[02] PERFORMED PERMANENT REPAIR CARGO TRACK LOCATED BS747 TO BS 787 LBL17 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3.;[03] CORRECTED STEP 2.PERFORMED PERMANENT REPAIR CARGO TRACK LOCATED BS747 TO BS 787 LBL17 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3. SEE INDIVIDUAL SIGN-OFF BELOW.;[04] PERFORMED PERMANENT REPAIR CARGO TRACK LOCATED BS747 TO BS 787 LBL17 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3. SEE INDIVIDUAL SIGN-OFF BELOW.

Part: PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 58,693 hrs · 35,154 cycles

DELAMINATED ACCESS PANEL 193AR AT LOWER FUSELAGE 2023-113052<[01] TOOL USED: CALIPER PN: 500-197-30 B20189526 DUE DATE: 20/DEC/23.;[02] TOOL USED HOT BONDER P/N: HCS9200B P/N: 18165044; DUE DATE: 28-FEB-23;[03] TOOL USED: SCALE PN: SPX621; SN: 8340225441; DUE DATE: 20-JUL-23;[04] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 16122983 DUE DATE: 24-JAN-24.;[05] REPAIRED ACCESS PANEL 193AR AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-2 REPAIR 2. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] JOB COMPLETED

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 58,692 hrs · 35,153 cycles

CORROSION SUPPORT ZEE LOCATED BS500A TO BS500D RBL21 AND WL156 AT FWD CARGO COMPARTMENT 2023-113045<[01] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 45 MG; S/N: 130063701; DUE DATE: 16-JUN-23.;[02] REPLACED SUPPORT ZEE LOCATED BS500A TO BS500D RBL21 AND WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM-51-40-02 AND DWG-143A7500 REV:- SEE INDIVIDUAL SIGN-OFF BELOW;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 58,692 hrs · 35,153 cycles

CRACK CARGO TRACK LOCATED BS500 RBL13.84 AND WL156 AT FWD CARGO COMPARTMENT 2023-113043<[01] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[02] INSPECTION REJECT IN STEP 7<BR>SEE TTG8Q00J8N87;[03] PERFORMED PERMANENT REPAIR CARGO TRACK LOCATED BS 396 TO 500A RBL13.84 AND WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM B737-700 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL SIGN OFF BELOW;[04] PERFORMED PERMANENT REPAIR CARGO TRACK LOCATED BS 396 TO 500A RBL13.84 AND WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM B737-700 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL SIGN OFF BELOW AS RII

Part: WEB — CRACKED (ZN 600 RIGHT WIN) · airframe 58,692 hrs · 35,153 cycles

CRACK WEB TRAILING EDGE LOCATED BTW ORSS261 TO ORSS279 AT RT WING 2023-113028<[01] REPLACED WEB TRAILING EDGE LOCATED BTW ORSS261 TO ORSS271 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A2512 SHEET 11 REV.- DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700 57-51-02. CRACK LENGTH: 1.398? TOOL USED CALIPER P/N: 500-197-30 S/N: A21043202 DUE DATE: 12/OCT/23;[02] CORRECTED STEP 1<BR>REPLACED WEB TRAILING EDGE LOCATED BTW ORSS261 TO ORSS271 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND SRM 51-40-05 AND SRM 51-20-01 AND DWG 115A2512 SHEET 11 REV.- DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700 57-51-02-1A-1. CRACK LENGTH: 1.398? TOOL USED CALIPER P/N: 500-197-30 S/N: A21043202 DUE DATE: 12/OCT/23;[03] REPLACED WEB TRAILING EDGE LOCATED BTW ORSS261 TO ORSS271 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND SRM 51-40-05 AND SRM 51-20-01 AND DWG 115A2512 SHEET 11 REV.- DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700 57-51-02-1A-1. CRACK LENGTH: 1.398? TOOL USED CALIPER P/N: 500-197-30 S/N: A21043202 DUE DATE: 12/OCT/23.RII

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 58,692 hrs · 35,153 cycles

CORROSION ANGLE LOCATED BS500D BETWEEN LBL21 TO RBL21 AND WL156 AT FWD CARGO COMPARTMENT 2023-113046<[01] REPLACED ANGLE LOCATED BS500D BETWEEN LBL21 TO RBL21 AND WL156 AT FWD CARGO COMPARTMEN IAW B737-700 SRM 51-10-02 Ï¿½TEM 9. PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND MORE DAMAGE.;[02] REPLACED ANGLE LOCATED BS500D BETWEEN LBL21 TO RBL21 AND WL156 AT FWD CARGO COMPARTMEN IAW B737-700 SRM 51-10-02 Ï¿½TEM 9. PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND MORE DAMAGE.

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 58,692 hrs · 35,153 cycles

CRACK OUTBOARD TRAILING EDGE CORRUGATED PLATE LOCATED AT ORSS 261 AT RT WING 2023-113010<[01] REPLACED OUTBOARD TRAILING EDGE CORRUGATE PLATE LOCATED AT ORSS 261 AT RT WING I.A.W. B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG 115A2001 SHEET 32 REV.-. DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700 57-20-10 CRACK LENGTH: 1.044? TOOL USED CALIPER P/N:500-196-30 S/N: B21141563 DUE DATE: 30/NOV/23;[02] COMPLETED STEP 1

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 58,692 hrs · 35,153 cycles

CRACK INTERNAL CAVITY CORRUGATE PLATE LOCATED AT LEVEL IRSS 248 TRAILING EDGE AT LT WING 2023-112990<[01] REPLACED CORRUGATE PLATE LOCATED AT LEVEL IRSS 248 TRAILING EDGE AT LT WING AND FASTENERS IAW<BR>B737-700 SRM-51-40-02; SRM 51-10-02 AND DWG 115A2001 REV:A;[02] REPLACED CORRUGATE PLATE LOCATED AT LEVEL IRSS 248 TRAILING EDGE AT LT WING AND FASTENERS IAW<BR>B737-700 SRM-51-40-02; SRM 51-10-02 AND DWG 115A2001 REV:A SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTIVE ACTION STEP 2 CERTIFIED

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 58,692 hrs · 35,153 cycles

CRACK INTERNAL CAVITY CORRUGATE PLATE LOCATED ORSS261 TRAILING EDGE AT LT WING 2023-112989<[01] REPLACED CORRUGATE PLATE AND FASTENERS LOCATED ORSS261 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02.;[02] CORRECTED STEP 1.<BR>REPLACED CORRUGATE PLATE AND FASTENERS LOCATED ORSS261 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02.SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED CORRUGATE PLATE AND FASTENERS LOCATED ORSS261 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02.SEE INDIVIDUAL SIGN OFF BELOW.

Part: PANEL — CRACKED (ZN 500 LEFT WING) · airframe 58,692 hrs · 35,153 cycles

CRACK INTERNAL CAVITY PHENOLIC STRAP LOCATED AT LEVEL ORSS 273 TRAILING EDGE AT LT WING 2023-112987<[01] REPLACED OUTBOARD TRAILING EDGE CORRUGATE PLATE (ASSY) LOCATED AT ORSS 273 AT LT WING I.A.W. B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG 115A2001 SHEET 32 REV.-. DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700 57-20-10 CRACK LENGTH: 0.352? TOOL USED CALIPER P/N:500-196-30 S/N: B21141563 DUE DATE: 30/NOV/23;[02] COMPLETED STEP 1

Part: COVER — CRACKED (ZN 200 FUS TOP) · airframe 58,692 hrs · 35,153 cycles

CRACK COVER LOCATED BS992.8 AT LEVEL STR10R AT PASSENGER CABIN 2023-112949<[01] REPLACED COVER LOCATED BS992.8 AT LEVEL STR10R AT PASSENGER CABIN I.A.W B737-700 AMM 52-71-11-400-801 STEP 3. F. (5).;[02] CERTIFIED WORK PERFORMED.

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 58,692 hrs · 35,153 cycles

CRACK WEB LOCATED BS294.5 TO BS303.9 AT LEVEL STR16L AT PASSENGER CABIN 2023-112925<[01] REPLACED WEB INTERCOSTAL LOCATED BS294.5 TO BS303.9 AT LEVEL STR16L AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A8180 REV;C. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: COVER — CRACKED (ZN 200 FUS TOP) · airframe 58,692 hrs · 35,153 cycles

CRACK COVER LOCATED BS992.8 AT LEVEL STR10L AT PASSENGER CABIN 2023-112950<[01] REPLACED COVER LOCATED BS992.8 AT LEVEL STR10L AT PASSENGER CABIN I.A.W B737-700 AMM 52-71-11-400-801 STEP 3F ITEM (5);[02] REPLACED COVER LOCATED BS992.8 AT LEVEL STR10L AT PASSENGER CABIN I.A.W B737-700 AMM 52-71-11-400-801 STEP 3F ITEM (5)

Part: FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 58,692 hrs · 35,153 cycles

CRACK FRAME ON BS 312 BETWEEN STR5L TO STR6L FWD GALLEY AND LAV 2023-112926<[01] PERFORMED REPAIR ON FRAME BS 312 BETWEEN STR 5L TO STR 6L FWD GALLEY AND LAV I.A.W EA M-22-153-01244;[02] CERTIFIED STEP 1; COMPLETED <BR>ITEM RII

Part: TIE CLIP — CRACKED (ZN 200 FUS TOP) · airframe 58,692 hrs · 35,153 cycles

CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2023-112927<[01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN AND FASTENERS I.A.W B737-700 SRM 51-40-02 DWG:141A1110 SHEET:18 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,692 hrs · 35,153 cycles

CRACK ANGLE LOCATED BS291.5 TO BS294.5 AT LEVEL STR17R AT FWD GALLEY AREA 2023-112929<[01] REPLACED ANGLE LOCATED BS291.5 TO BS294.5 AT LEVEL STR17R AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02 AND DWG 141A8310- 33 REV B. <BR>SEE INDIVIDUAL SIGN OFF BELLOW;[02] REPLACED ANGLE LOCATED BS291.5 TO BS294.5 AT LEVEL STR17R AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8310- 33 REV B. <BR>SEE INDIVIDUAL SIGN OFF BELLOW;[03] CORRECTED STEP 1 AND 2:<BR>REPLACED ANGLE LOCATED BS291.5 TO BS294.5 AT LEVEL STR17R AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A8310- 33 REV B. <BR>SEE INDIVIDUAL SIGN OFF BELLOW;[04] CERTIFIED STEP 3; COMPLETED <BR>ITEM RII

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 58,692 hrs · 35,153 cycles

CRACK ON AFT CORNER SCUFF PLATE OF FWD CARGO COMPARTMENT 2023-112901<[01] TOOL USED DIGITAL CALIPER P/N:2340A11;S/N:B17119057;DUE DATE:05-DEC-23.;[02] TOOL USED: BLACK LIGHT METER : P/N XDS- 1000 S/N 1998072 DUE DATE : 03-MAY-23.;[03] REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-30-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2); (4)TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[04] JOB TASK COMPLETED.

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 58,692 hrs · 35,153 cycles

CRACK INSPAR RIB 120.30 AT 28 INCHES OF FRONT SPAR LT HORIZONTAL STAB 2023-112863<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138203; DUE DATE: 11-APR-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138203; DUE DATE: 11-APR-23.;[03] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101V022233; DUE DATE: 30 AUG 23.;[04] PERFORMED REPAIR INSPAR RIB 120.30 LOCATED AT 28 INCHES OF FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED REPAIR INSPAR RIB 120.30 LOCATED AT 28 INCHES OF FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN OFF BELOW. RII ITEM

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 58,692 hrs · 35,153 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS847 TO BS867; LBL20 CEILING AREA AFT CARGO COMPARTMENT 2023-112884<[01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS847 TO BS867; LBL20 CEILING AREA AFT CARGO COMPARTMENT IAW B737-700 SRM-51-40-02 AND DWG-149A8100 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 58,692 hrs · 35,153 cycles

CRACK SUPPORT BRACKET BS540 LT SIDE AT AIR CONDITIONING BAY 2023-112867<[01] REPLACED SUPPORT BRACKET BS540 LT SIDE AT AIR CONDITIONING BAY IAW B737-700 51-40-02;[02] REPLACED SUPPORT BRACKET BS540 LT SIDE AT AIR CONDITIONING BAY IAW B737-700 51-40-02

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 58,692 hrs · 35,153 cycles

CRACK ON FWD CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT 2023-112904<[01] TOOL USED: BLACK LIGHT METER : P/N XDS- 1000 S/N 1998072 DUE DATE : 03-MAY-23.;[02] REPAIRED BY WELD CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A21143279; DUE DATE 31-DEC-23 SEE INDIVIDUAL SIGNOFFS BELOW;[03] JOB COMPLETED

Part: BEAM — CORRODED (ZN 100 FUS LOWER) · airframe 58,692 hrs · 35,153 cycles

CORROSION FLOOR STRUCTURE BEAM LOC STA 986.5 BTW RBL 40 TO RBL 45 AND WL 208.1 AT AFT GALLEY AREA 2023-112824<[01] TOOL USED: CALIPER; PN: 500-752-20; SN: B20317422; DUE DATE: 29-AUG-23.;[02] RADIUS GAUGE; PN: 2204A3; SN: AE-408657; DUE DATE: 14-FEB-23.;[03] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[04] TOOL USED: FLAPSPEED; PN: FPK-PRO-104; SN: PRO-3384; DUE DATE: 27-JUN-23.;[05] PERFORMED REPAIR ON FLOOR BEAM 986.5 BTW RBL 40 TO RBL 45 AND WL 208.1 AT AFT GALLY AREA IAW SRM B737-700 53-70-51-2R-6 REPAIR 6 SEE INDIVIDUAL SIGN OFF BELOW;[06] PERFORMED REPAIR ON FLOOR BEAM 986.5 BTW RBL 40 TO RBL 45 AND WL 208.1 AT AFT GALLY AREA IAW SRM B737-700 53-70-51-2R-6 REPAIR 6 SEE INDIVIDUAL SIGN OFF BELOW AS RII

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,692 hrs · 35,153 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV 2023-112817<[01] REPLACED INTERCOSTAL WEB LOCATED ON FLOOR STRUCTURE BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV I.A.W. B737-700 SRM 51-40-02 AND DWG 141A5400 REV. -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INTERCOSTAL WEB LOCATED ON FLOOR STRUCTURE BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV I.A.W. B737-700 SRM 51-40-02 AND DWG 141A5400 REV. -. SEE INDIVIDUAL SIGN OFF BELOW. RII

Part: PANEL — ELONGATED (ZN 100 FUS LOWER) · airframe 58,692 hrs · 35,153 cycles

ELONGATED HOLE BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT 2023-112859<[01] FABRICATED BULKHEAD 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWIN 453A2510 SHEET 4 REV- A MATERIAL USED PN CONOLITE #A60SG4W; PO# 2022-003394;[02] FABRICATED BULKHEAD 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING 453A2510 SHEET 4 REV- A MATERIAL USED PN CONOLITE #A60SG4W; PO# 2022-003394

Part: STRUCTURE — CRACKED (ZN 100 FUS LOWER) · airframe 58,692 hrs · 35,153 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOC. STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV 2023-112818<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOC. STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-40-02 AND DGW: 141A5400 REV: - SHEET: 26. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED ESTEP 1 <BR>REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOC. STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-40-02 AND DWG: 141A5400 REV: - SHEET: 26. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOC. STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-40-02 AND DWG: 141A5400 REV: - SHEET: 26. SEE INDIVIDUAL SIGN OFF BELOW. RII

Part: PANEL — CRACKED (ZN 300 STABILIZE) · airframe 58,692 hrs · 35,153 cycles

CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.700 INCH. APPROX. 2023-112752<[01] TOOL USED: CALIPER; PN: 500-752-20; SN: B20317422; DUE DATE: 29-AUG-23.;[02] RADIUS GAUGE; PN: 2204A3; SN: AE-408651; DUE DATE: 24-FEB-23;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138203; DUE DATE: 11-APR-23.;[04] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138203; DUE DATE: 11-APR-23.;[05] PERFORMED REPAIR ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL LOCATED AT STAB STA 193.9 RIB AND 16 INCH FROM FRONT SPAR IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11. SEE INDIVIDUAL SIGN OFF BELOW.;[06] PERFORMED REPAIR ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL LOCATED AT STAB STA 193.9 RIB AND 16 INCH FROM FRONT SPAR IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11. RII;SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 58,692 hrs · 35,153 cycles

CRACK TRAILING EDGE SUPPORT ANGLE INTERNAL CAVITY ORSS 271 AT LT WING 2023-112628<[01] REPLACED SUPPORT ANGLE LOCATED TRAILING EDGE INTERNAL CAVITY ORSS 271 AT LT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2930 SHEET 7 REV - . SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED SUPPORT ANGLE LOCATED TRAILING EDGE INTERNAL CAVITY ORSS 271 AT LT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2930 SHEET 7 REV - . SEE INDIVIDUAL SIGN-OFF BELOW.

Part: PANEL — DEBONDED (ZN 500 LEFT WING) · airframe 58,689 hrs · 35,152 cycles

CUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING 2023-112679<[01] TOOL USED; CALIPER PN: 500-197-30; SN: B20189526; DUE DATE: 20/DEC/23.;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 24-JAN-24; PROSITECTOR 6000 NS3 S/N: 767584 DUE DATE: 02-AUG-23.;[03] TOOL USED PN: BONDMASTER 600M; SN: 220052310; DUE DATE: 31-OCT-23.;[04] PERFORMED INTERIM REPAIR ON IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING IAW B737-700 SRM 57-53-01-2R-18 REPAIR 18. SEE INDIVIDUAL SIGNOFFS BELOW;[05] JOB COMPLETED RII.

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 58,692 hrs · 35,153 cycles

CRACK TRAILING EDGE SUPPORT ANGLE INTERNAL CAVITY ORSS 271 AT RT WING 2023-112631<[01] REPLACED TRAILING EDGE SUPPORT ANGLE INTERNAL CAVITY ORSS271 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A2930 SHEET 8 REV.- DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700 57-51-02. CRACK LENGTH: 0.501? TOOL USED CALIPER P/N: 500-197-30 S/N: A21043202 DUE DATE: 12/OCT/23;[02] CORRECTED STEP 1<BR>REPLACED TRAILING EDGE SUPPORT ANGLE INTERNAL CAVITY ORSS271 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND SRM 51-40-05 AND SRM 51-20-01 AND DWG 115A2930 SHEET 8 REV.- DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700 57-51-02-1A-1. CRACK LENGTH: 0.501? TOOL USED CALIPER P/N: 500-197-30 S/N: A21043202 DUE DATE: 12/OCT/23;[03] REPLACED TRAILING EDGE SUPPORT ANGLE INTERNAL CAVITY ORSS271 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND SRM 51-40-05 AND SRM 51-20-01 AND DWG 115A2930 SHEET 8 REV.- DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700 57-51-02-1A-1. CRACK LENGTH: 0.501? TOOL USED CALIPER P/N: 500-197-30 S/N: A21043202 DUE DATE: 12/OCT/23 RII

Part: WEB — CRACKED (ZN 600 RIGHT WIN) · airframe 58,692 hrs · 35,153 cycles

CRACK WEB TRAILING EDGE LOCATED ORSS 271 AT RT WING 2023-112634<[01] REPLACED WEB AT TRAILING EDGE LOCATED ORSS271 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A2930 SHEET 6 REV.-.<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] COMPLETED STEP 1; RII

Part: FLAP — DEBONDED (ZN 500 LEFT WING) · airframe 58,689 hrs · 35,152 cycles

CUSTOMER REQUEST - DEBONDED OB AFT FLAP LOWER SURFACE LOCATED INBOARD SIDE AT LT WING 2023-112680<[01] TOOL USED; CALIPER PN: 500-197-30; SN: B20189526; DUE DATE: 20/DEC/23.;[02] TOOL USED CALIPER PN: 500-464 S/N: B17030933 DUE DATE: 17/OCT/23;[03] TOOL USED: AUDIBLE BOND TESTER; PN: S-3; SN: 064; DUE DATE: 19-JUL-23;[04] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 24-JAN-24; PROSITECTOR 6000 NS3 S/N: 767584 DUE DATE: 02-AUG-23.;[05] TOOL USED: BOND TESTING UNIT; PN:BONDMASTER 600M; SN: 220052310; DUE DATE: 31-OCT-23;[06] REPAIRED OB AFT FLAP LOWER SURFACE LOCATED INBOARD SIDE AT LT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. SEE INDIVIDUAL SIGNOFFS BELOW. TOOL USED SCALE P/N: SPX621; S/N: 8340225441; DUE DATE: 20-JUL-23.;[07] TASK COMPLETED. RII COMPLETED.

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 58,692 hrs · 35,153 cycles

CRACK ANGLE TRAILING EDGE LOCATED INTERNAL CAVITY ORSS 275 AT LT WING 2023-112629<[01] REPLACED ANGLE TRAILING EDGE LOCATED INTERNAL CAVITY ORSS 275 AT LT WING I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG #115A6200 REV:-;[02] REPLACED ANGLE TRAILING EDGE LOCATED INTERNAL CAVITY ORSS 275 AT LT WING I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG #115A6200 REV:- <BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED ANGLE TRAILING EDGE LOCATED INTERNAL CAVITY ORSS 275 AT LT WING I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG #115A6200 REV:- <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 58,072 hrs · 34,753 cycles

OVERHEAD BIN EMERGENCY LIGHT COVER CRACKED AT 4ABC AND 11DEF. R & R THE LENS IAW AMM 33-51-03.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 57,986 hrs · 34,691 cycles

CRACK FOUND ON UPPER ATTACH ANGLE STA 663 (WL 167) AT LBL 40 / [01] STARTED REMOVING FASTENERS FROM UPPER ATTACH ANGLE STA 663 IAW SRM 51-40-02-0G-0;[02] DOCUMENTED STARTED INSTALL OF ATTACH ANGLE ENTERED AS CORRECTIVE ACTION 1;[03] ACTION 2 SHOULD STATE REMOVAL NOT INSTALL;[04] VERIFIED ACTION 2 IN STEP 1; ACTION 1 IN STEP 2; AND ACTION 1 IN STEP 3;[05] VERIFIED STEP 1 ITEM 4 AND STEP 4 ITEM 1;[06] VERIFIED STEP 4 AND 5;[07] VERIFIED ITEM 2 OF STEP 8;[08] OK TO INSTALL REMOVED STRUCTURE FOR REPAIR;[09] AUDIT C/W

Part: PANEL — PULLED (ZN 100 FUS LOWER) · airframe 57,986 hrs · 34,691 cycles

DOT A24-65 MID CABIN FLOOR BOARD PANEL 242BF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1. TAP TEST GOOD;[02] CLEANED AND PREPARED IAW SRM 53-00-50-2R-1 STEP 3A;C;E-F;[03] VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201 RESIN (A150261) FABRIC (A10269).;[04] VERIFIED STEPS AND OK TO BOND;[05] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 150 DEGREES (AAR B0-06 EXP 11-8-22). TAP TEST GOOD.;[06] REPAIRED MID CABIN FLOOR BOARD PANEL 242BF UPPER SIDE IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1.;[07] VERIFIED STEPS 5-6

Part: PANEL — PULLED (ZN 100 FUS LOWER) · airframe 57,986 hrs · 34,691 cycles

DOT A24-57 MID CABIN FLOOR BOARD PANEL 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED AND FOUND MISSING PLIES THE LENGTH OF BOARD. TAP TEST GOOD. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. FABRIC (10269); RESIN (A150262).<BR><BR>REQUEST OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. TAP TEST GOOD. CURED AT 150 DEGREES (AAR 30347 EXP 4-30-23).;[04] REPAIRED CABIN FLOOR BOARD PANEL 241AF UPPER SIDE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3-4

Part: PANEL — PULLED (ZN 100 FUS LOWER) · airframe 57,986 hrs · 34,691 cycles

DOT A24-58 MID CABIN FLOOR BOARD PANEL 232RF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED PANEL 232RF AND FOUND DAMAGE TO BE B.E.R. MANUFACTURED NEW PANEL PER SAMPLE. IAW B737-700 SRM 53-00-50-2R-0 PAR 1A & NOTE AND TABLE 204. (A1409978);(A147545);(WN13845).;[02] MANUFACTURED NEW PANEL 232RF USING OLD PANEL AS SAMPLE. IAW B737-700 SRM 53-00-50-2R-0.;[03] VERIFIED STEPS

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 57,986 hrs · 34,691 cycles

DOT A24-52 MID CABIN FLOOR BOARD PANEL 231ZF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] MID CABIN FLOOR BOARD 231ZF REPLACED BY FABRICATION OF NEW PANEL ON NON-ROUTINE #TTG8Q000FS2GY.;[02] VERIFIED STEPS

Part: PANEL — PULLED (ZN 100 FUS LOWER) · airframe 57,986 hrs · 34,691 cycles

DOT A24-52 MID CABIN FLOOR BOARD PANEL 241BF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED AND FOUND BOARD TO BE BER AND TO REPLACE BY FABRICATION PER SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL STEP 4 AND TABLE 204<BR>VERIFIED MATERIALS AS FLOOR BOARD STOCK (WN13845); INSERTS (A147545); INSERT GLUE (A140998); DECAL (A145274) IAW BOEING DRAWING 144A5810 AND SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204<BR>FABRICATED NEW BOARD PER SAMPLE AND INSTALLED INSERTS IAW SRM 53-00-50-2R-0 REPAIR GENERAL STEP 4; BOEING DRAWING 144A5810 AND BAC5085;[02] REPLACED FLOOR BOARD BY FABRICATION OF NEW BOARD PER SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL; BOEING DRAWING 144A5810 AND BAC5085;[03] VERIFIED STEPS

Part: PANEL — PULLED (ZN 100 FUS LOWER) · airframe 57,986 hrs · 34,691 cycles

DOT A24-56 MID CABIN FLOOR BOARD PANEL 231XF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>CLEANED; PREPPED AREAS IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;C;D;E;F;G;H;I; AND J. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; RESIN EPOCAST50A(A150262)); FIBERGLASS CLOTH BMS9-3(A10269); <BR><BR>REQUIRES OKAY TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS K;L;AND M. TAP TEST GOOD. OVEN B0-06 CAL DUE 11/8/22.;[04] REPAIRED CABIN FLOOR BOARD PANEL 231XF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1.;[05] VERIFIED STEPS 3-4

Part: PANEL — PULLED (ZN 100 FUS LOWER) · airframe 57,986 hrs · 34,691 cycles

DOT A24-60 MID CABIN FLOOR BOARD PANEL 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED AND FOUND BOARD TO BE BER AND TO REPLACE BY FABRICATION PER SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL STEP 4 AND TABLE 204<BR>VERIFIED MATERIALS AS FLOOR BOARD STOCK (WN13845); INSERTS (A147545); INSERT GLUE (A140998); DECAL (A145274) IAW BOEING DRAWING 144A5810 AND SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204<BR>FABRICATED NEW BOARD PER SAMPLE AND INSTALLED INSERTS IAW SRM 53-00-50-2R-0 REPAIR GENERAL STEP 4; BOEING DRAWING 144A5810 AND BAC5085;[02] REPLACED FLOOR BOARD BY FABRICATION OF NEW BOARD PER SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL; BOEING DRAWING 144A5810 AND BAC5085;[03] VERIFIED STEPS

Part: PANEL — PULLED (ZN 100 FUS LOWER) · airframe 57,986 hrs · 34,691 cycles

DOT A24-64 MID CABIN FLOOR BOARD PANEL 232SF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED AND FOUND PANEL 232SF DAMAGED B.E.R.. FABRICATE NEW FLOOR BOARD PER SAMPLE AND DWG 144A5810-159 IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204.<BR><BR>FABRICATED NEW FLOOR BOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL PER SAMPLE AND DWG 144A5810-159. FLOOR BOARD (WN13845); INSERTS (A147545); EPIBOND420 (A140998).;[02] REPLACED BY FABRICATION MID CABIN FLOOR BOARD PANEL 232SF IAW SRM 53-00-50-2R-0 REPAIR GENERAL; DWG 144A5810-159 AND SAMPLE.;[03] VERIFIED STEPS

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 57,986 hrs · 34,691 cycles

DOT A24-53 MID CABIN FLOOR BOARD PANEL 241CF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED AND FOUND BOARD TO BE BER AND TO REPLACE BY FABRICATION PER SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL STEP 4 AND TABLE 204 <BR>VERIFIED MATERIALS AS FLOOR BOARD STOCK (WN13845); INSERTS (A147545); INSERT GLUE (A140998) IAW BOEING DRAWING 144A5810 AND SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204 <BR>FABRICATED NEW BOARD PER SAMPLE AND INSTALLED INSERTS IAW SRM 53-00-50-2R-0 REPAIR GENERAL STEP 4; BOEING DRAWING 144A5810 AND BAC5085;[02] REPLACED FLOOR BOARD BY FABRICATION OF NEW BOARD PER SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL; BOEING DRAWING 144A5810 AND BAC5085;[03] VERIFIED STEPS

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,749 hrs · 34,530 cycles

EXTERIOR LH OVERWING EMERGENCY LT INOP. OK TO CONTINUE PER MEL 33-14-01; SP1. REPLACED CABIN LH OVERWING EMERGENCY LIGHTING POWER SUPPLY IAW AMM 33-51-06. OPERATIONAL CHECK GOOD.

Part: NONE — INOPERATIVE (OVERWING EXIT) · airframe 57,549 hrs · 34,395 cycles

LH OVERWING EXIT LIGHT OVER DOOR INOP / [01] R&R?D LH EMERGENCY EXIT OVERWING BATTERY PACK AT BS 603 REF AMM 33-51-06. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 57,308 hrs · 34,235 cycles

EMERGENCY BATTERY PACK (M1668) INOP. / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK (M1668) AND PERFORMED INSTALLATION TEST AS PER B737 AMM 33-51-06-960-805. TEST OK.;[02] VERIFIED STEP 1

Part: SHEAR TIE — CORRODED (AFT CARGO) · airframe 57,308 hrs · 34,235 cycles

AFT CARGO COMPARTMENT; FRAME SHEAR TIE AT BS 847; S-23L WL165 CORROSION NOTED.<[01] REMOVED DAMAGE SHEAR TIE AT AFT CARGO COMP BS 847 S-23L TO S-24L PER REF B737 SRM 51-40-02-0G-0.;[11] (RII) FINAL INSPECTED; SHEAR TIE EXFOLIATION FOUND OUT OF LIMITS; ACCOMPLISHED ALL REPAIRS AND PROCEDURES AS PER EA 22-153-02349-WIP1; #TTG8Q00DZWET.

Part: SKIN — CORRODED (AFT CARGO) · airframe 57,308 hrs · 34,235 cycles

FUSELAGE SKIN BELOW TOILET SERVICE DOOR HAS EVIDENCE OF CORROSION.<[01] INSTALLED EWIS PROTECTION AT AFT CARGO COMPARTMENT BETWEEN STA 847 AND STA 867 LBL 25 LOWER SECTION AS PER B737-700 AMM 20-60-07-913.;[02] REMOVED INSULATION BLANKETS AT AFT CARGO COMPARTMENT BETWEEN STRINGER 24LT AND STRINGER 26LT ; STA 847 AND STA 867 AS PER B737-700 AMM 25-80-00-000.;FUSELAGE SKIN BELOW TOILET SERVICE DOOR FOUND OUT OF LIMITS SRM 53-00-01-1A-5. ACCOMPLISHED REPAIRS AS PER EA#22-153-02310.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,303 hrs · 34,234 cycles

FUSELAGE SKIN BELOW TOILET SERVICE DOOR HAS EVIDENCE OF CORROSION / [01] TRANSFERRED TO SA-M 663 LP# 2039647 DUE TO FERRY FLIGHT.;[02] TRANSFERRED TO SA-M 663 LP# 2039647 DUE TO FERRY FLIGHT.

Part: LIGHT — BROKEN (PAX CABIN) · airframe 56,757 hrs · 33,875 cycles

EMERGENCY EXIT SIGN/PLACARD (LOWER) IS EVIDENCED AS BROKEN AT AIRCRAFT LEFT / [01] FOUND L/H OVERWING EXIT SIGN LOOSE. REINSTALLED L/H OVERWING EXIT SIGN PER AMM33-51-01

Part: SIGN — BROKEN · airframe 56,763 hrs · 33,881 cycles

EMERGENCY EXIT SIGN/PLACARD (LOWER) IS EVIDENCED AS BROKEN AT AIRCRAFT LEFT / [01] FOUND L/H OVERWING EXIT SIGN LOOSE. REINSTALLED L/H OVERWING EXIT SIGN PER AMM33-51-01

Part: LIGHT — INOPERATIVE · airframe 55,635 hrs · 33,137 cycles

LEFT OVER WING EXIT LIGHT IS DIM ; / [01] RELAMPED EMER EXIT LIGHT REF AMM 33-51-04 OPS CK GOOD

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 55,352 hrs · 32,973 cycles

RIGHT WING-OTBD TRAILING EDGE -AFT FLAP-DELAMINATED AT INBD END. REMOVED AND REPLACED R/H OUTBOARD AFT FLAP PER MM 27-51-12

Part: COVER — LOOSE (SIGN) · airframe 53,876 hrs · 32,097 cycles

EMERGENCY EXIT SIGN#2OVERWING FELL OFF ; / [01] RE-INSTALLED EMERGENCY EXIT SIGN COVER IAW AMM 33-51-01

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

INTERCOSTAL AT CRACKED AT BS 344-BS 360; BL 0; WL 207.5 / REMOVED AND REPLACED INTERCOSTAL AT B.S344- B.S360; BL0 WL207.5 IAW SRM 51-40-02-0G-0 AND DWG 141A5400

Part: LAMP — INOPERATIVE (CABIN) · airframe 53,274 hrs · 31,733 cycles

OVERWING INTERIOR EMERGENCY LIGHTS HAVE BURNED OUT BULBS / REMOVED; REPLACED AND PERFORMED GOOD OPS CHECK OF ALL INOP OVERWING INTERIOR EMERGENCY EXIT SIGN LIGHT LAMPS PER AMM 33-51-01-960-801 STEP 2.B.(1)(A) AND 2.B.(1)(C) AND 2.B.(2).

Part: LAMP — INOPERATIVE (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

AFT L/H ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT IS INOP / REMOVED; REPLACED AND PERFORMED GOOD OPS CHECK OF AFT L/H ENTRY EXTERIOR EMERGENCY EXIT (SLIDE) LIGHT LAMP PER AMM 33-51-04-960-801.

Part: LAMP — INOPERATIVE (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

R/H OVERWING EXTERIOR EMERGENCY EXIT LIGHT IS INOP / REMOVED; REPLACED; AND PERFORMED GOOD OPS CHECK OF R/H OVERWING EXTERIOR EMERGENCY EXIT (SLIDE) LIGHT LAMP PER AMM 33-51-04-960-801.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 53,274 hrs · 31,733 cycles

EMERGENCY LIGHT COMMON TO FUSELAGE SKIN AT BS 757 JUST BELOW STR 21L CONNECTOR IS DAMAGED / REMOVED AND REPLACED CONNECTOR D11082 AT BS 757 PER SWPM 20-61-28. PERFORMED GOOD OPERATIONAL CHECK PER AMM 33-51-04-960-801 STEP 2.F(2)

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

ACB BS 947 RBL 45 WL 196 SIDEWALL UPPER ATTACH ANGLE CRACKED / REMOVED CRACKED ACB SIDEWALL ATTACH ANGLE BS 887-947 RBL 45 RECIEVED SERVICABLE PART. LOCATED DRILLED & INSTALLED PER SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 & DWG 149A9490

Part: FORMER — CHAFED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

FAIRING FORMER HAS CHAFE DAMAGE BS657 TO BS667 WL150 RBL28 / REMOVED AND REPLACED FAIRING FORMER BS657-BS667; WL150; RBL28 IAW SRM 51-40-05-0G-0 FIG 3+4; AND DWG 149A7216. WILL BE INSTALLED ON NRC U287789

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

REINFORCEMENT DOUBLER IS CRACKED ON FWD SIDE OF LOWER VAPOR BARRIER BS663 RBL26 WL154 / REMOVED REINFORCEMENT DOUBLER DAMAGED AND INSTALLED NEW REINFORMENT DOUBLER AT BS 663 RBL 6-25 WL 154 IAW SRM 51-40-02-0G-0 AND DWG 111A1001.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB FLOOR TO SIDEWALL SUPPORT BS 88 7' TO 947 RBL 21 WL 156 / REMOVED FLOOR TO SIDEWALL SUPPORT DAMAGED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT ANGLE AT BS 887-947 RBL 21 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 147A7500

Part: STIFFENER — CRACKED (L/H HORIZ. STAB.) · airframe 53,274 hrs · 31,733 cycles

LT HORIZ. STAB RIB AT STAB STA 129.50 2ND VERT STIFFENER IS CRACKED. / REPAIRED LT HORIZ STAB RIB AT STAB STA 129.50 2ND VERTICAL STIFFENER IAW SRM 55-10-06-2R-4. 59796C 15MAR21

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

FORWARD CARGO BAY CRACKED INTERCOSTAL BS500C TO BS500D STR26L WL158 / REPLACED FCB INTERCOSTAL BS 500C TO 500D STR 26L WL 158 PER SRM 51-40-02-0G-0 AND DWG 143A7505

Part: ANGLE — CRACKED (FWD CARGO) · airframe 53,274 hrs · 31,733 cycles

FORWARD CARGO BAY CRACKED CLIP AFT SIDE OF THE FRAME BS400 LBL21 WL158 / REPLACED FCB CLIP AFT SIDE OF THE FRAME BS 400 LBL 21 WL 158 PER SRM 51-10-02-0G-0 AND DWG 143A7505

Part: STRAP — CORRODED (AFT CARGO) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB FLOOR STRAP BS 767+7' LBL 22 WL 156 / RECEIVED NEW SERVICEABLE FLOOR STRAP ON SWA P.O. # 813290/1; NEW STRAP WILL BE INSTALLED ON SWA CARD # JPANEL-141-CLOSE

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB FLOOR TO BULKHEAD SUPPORT BS 947 RLB 20-LBL 8 WL 156 / REMOVED DAMAGED FLOOR TO BKD SUPPORT AND INSTALLED NEW FLOOR TO BKD SUPPORT BS 947 RBL 20 - LBL 10 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 149A8110; 147A7500

Part: INTERCOSTAL — CORRODED (AFT CARGO) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB INTERCOSTAL BS 767787 RBL 22 W L 156 CORROSION DAMAGE EVALUATION PN 146A812320 ACB INTERCOSTAL ASSY BS767787; RBL 22; WL 156; WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO HOLES PER SRM 530004. REMOVED AND INSTALLED NEW ACB INTERCOSTAL ASSY PN 146A812320 BS 767787; RBL 22; WL 156. PER DWG 146A0081; AND SRM 514002 87713U 17MAR21

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 53,274 hrs · 31,733 cycles

RT HORIZ. STAB RIB AT STAB STA 129.50 4TH VERT STIFFENER IS CRACKED. REPAIRED RT HORIZ. STABILIZER RIB AT STAB STA 129.50 4TH VERT STIFFENER IAW SRM 5510092R4. 59796C 15MAR21.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** FORWARD CARGO BAY L/H FLOOR TO SIDE WALL SUPPORT BS400 TO BS500D LBL 21 WL156 / REMOVED DAMAGED FLOOR TO SIDEWALL SUPPORT AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT BS 396 - 500D LBL 21 WL 156 IAW SRM 51-40-02-0G-0 & DWG 284A0603

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

ACB CRACKED ANGLE BS 947 LBL 10 WL 156 / REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE AT BS 947 LBL 10 WL 156 IAW SRM 51-40-02-0G-0 AND IPC 53-42-51-03

Part: WEB — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB SUBTHRESHOLD WEB BS 792-847 RBL 25 WL 156 / REPLACED ACB SUBTHRESHOLD WEB BS 792-847 RBL 25 WL 156 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A8340

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

FORWARD CARGO BAY CRACKED INTERCOSTAL BS500 TO BS500A STR26L WL158 / REPLACED FCB INTERCOSTAL BS 500 TO BS 500A STR 26L WL 158 PO # 812273/6 PER DWG 143A7505 AND SRM 51-40-02-0G-0

Part: FLOOR SPLICE — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB EXISTING FLOOR SPLICE BS 767+5' LBL 17 WL 156 /

Part: STRAP — CORRODED (AFT CARGO) · airframe 53,274 hrs · 31,733 cycles

***CORROSION***ACB FLOOR STRAP BS 887 LBL 7 WL 156 / RECEIVED NEW SERVICEABLE FLOOR STRAP ON SWA P.O.# 814641/1. NEW STRAP WILL BE INSTALLED ON SWA CARD # JPANEL-141-CLOSE

Part: ANGLE — CRACKED (AFT CARGO) · airframe 53,274 hrs · 31,733 cycles

ACB CLIP CRACKED BS 827 RBL 19 WL 156 REPLACED ACB CLIP BS 827 RBL 19 WL 156 PO# 817763 PER SRM 5140020G0 AND DWG 146A8120

Part: FLOOR SPLICE — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB EXISTING FLOOR SPLICE BS 767+5' RBL 8 WL 156 / FOUND OUT OF LIMITS DUE TO NO SRM LIMITS. REMOVED AND REPLACED DAMAGE REPAIR PARTS AS PER SRM 51-40-02 (737-700) AS SHOWN IN 1-A53-4982 REV 3.

Part: WEB — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** FORWARD CARGO BAY SUB THRESHOLD WEB BS449 TO BS480 RBL 25 WL156 / CORROSION ON FWD CARGO BAY SUB THRESHOLD WEB BS 449-480; RBL 25; WL 156 FOUND OUT OF LIMITS DUE TO PROXIMITY TO HOLES PER SRM 53-30-15-1A-1 FIG 103 DETAIL D. REMOVED WEB; LOCATED & DRILLED; COUNTERSUNK AND INSTALLED NUT PLATES IN NEW WEB AND INSTALLED NEW WEB PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0 AND DWG 143A8330.

Part: STIFFENER — CRACKED (L/H HORIZ. STAB.) · airframe 53,274 hrs · 31,733 cycles

LT HORIZ. STAB RIB AT STAB STA 92.70 1ST VERT STIFFENER IS CRACKED. / REPAIRED LT HORIZ. STAB RIB AT STAB STA 92.70 1ST VERT. STIFFENER IAW SRM 55-10-09-2R-4.

Part: SHIELD — CORRODED (FWD CARGO) · airframe 53,274 hrs · 31,733 cycles

CORROSION FORWARD CARGO BAY SHIELD BS420TO BS 440 RBL 23 WL156 REMOVED AND REPLACED FORWARD CARGO BAY SHIELD ASSY BS 420 BS 440 RBL 23; WL 156 PER SRM 514005; 514002 AND DWG # 143A0080 REV

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** FORWARD CARGO BAY BULKHEAD SUPPORT ANGLE BS 500D RBL18 TO LBL18 WL156 / REPLACED FWD CARGO BAY BULKHEAD SUPPORT ANGLE BS 500D RBL 8 TO LBL 18 WL 156 PO # 818035 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 143A9485-35 AND DWG 143A9481

Part: FLOOR SPLICE — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB EXISTING FLOOR SPLICE BS 767+5' LBL 3 WL 156 / FOUND OUT OF LIMITS DUE TO NO SRM LIMITS. REMOVED AND REPLACED DAMAGE REPAIR PARTS AS PER 737-700 SRM 51-40-02 AS SHOWN IN 1-A53-4982 REV 3.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** FORWARD CARGO BAY SHIELD BS492 TO B500A RBL 23 WL156 / REMOVED AND REPLACED FCB SHIELD BS 492 TO BS 500A RBL 23 WL 156 I.A.W SRM 51-40-02-0G-0 AND DWG 143A0080 REV:-

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB INTERCOSTAL BS 747-767 RBL 22 WL 156 / CORROSION ON INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER: SRM 53-00-04-1A-1. INTERCOSTAL IS A PART OF THE 146A7502-51 ASSY AND WAS REPLACED ON NRC U287962

Part: STIFFENER — CRACKED (L/H HORIZ. STAB.) · airframe 53,274 hrs · 31,733 cycles

LT HORIZ. STAB RIB AT STAB STA 92.70 3RD VERT STIFFENER IS CRACKED. / REPAIRED LT HORIZONTAL STAB RIB AT STAB STA 92.70 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4. 59796C 15MAR21

Part: SUPPORT ANGLE — CRACKED (AFT BULKHEAD) · airframe 53,274 hrs · 31,733 cycles

ACB BULKHEAD SUPPORT ANGLE BS 727+4' RBL 4 WL 162 IS CRACKED REMOVED AND REPLACED ACB BULKHEAD SUPPORT ANGLE BS 727+4; WL 162; RBL 4 IAW SRM 5140020G0; DWG# 144A2600

Part: STRIP — CORRODED (AFT CARGO) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB NUTPLATE STRIP BS 787-792 RBL 2 0 WL 156 / REPLACED ACB NUTPLATE STRIP BS 787-792 RBL 20 WL 156 PER SRM 51-40-02-0G-0 AND DWG 146A0081

Part: SHIELD — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB SHIELD BS 767-792 RBL 22 WL 156 / CORROSION DAMAGE EVALUATION ON ACB SHIELD P/N 146A8127-12 WAS FOUND TO BE OUT OF LIMITS. DUE TO NO LIMITS GIVEN IN SRM. REMOVED AND INSTALLED NEW ACB SHIELD BS 767-792; RBL 22; WL 156. PER DWG 146A0081. AND SRM 51-40-02 87713U 18MAR21

Part: FRAME ANGLE — CORRODED (AFT CARGO) · airframe 53,274 hrs · 31,733 cycles

CORROSION ACB BS947 FRAME CLIP LBL8; WL175. REMOVED DAMAGED FRAME CLIP AT BS 947 LBL 8 WL 175 AND INSTALLED NEW FRAME CLIP IAW SRM 5140020G0 AND DWG 147A1047.

Part: FLOOR SPLICE — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB EXISTING FLOOR SPLICE BS 767+5' RBL 3 WL 156 / FOUND OUT OF LIMITS DUE TO NO LIMITS (SRM.) REMOVED AND REPLACED DAMAGE REPAIR PARTS AS PER 737-700 SRM 51-40-02 AS SHOWN IN 1-A53-4982 REV 3

Part: FLOOR SPLICE — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB EXISTING FLOOR SPLICE BS 767+5' LBL 8 WL 156 / FOUND OUT OF LIMITS DUE TO NO LIMITS. (SRM) REMOVED AND REPLACED DAMAGE REPAIR PARTS AS PER 737-700 SRM 51-40-02 AS SHOWN IN 1-A53-4982 REV 3

Part: WEB — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB WEB BS 767-787 RBL 6 WL 156 / REPLACED ACB WEB BS 767-787 RBL 6 WL 156 PO# 818018 PER SRM 51-40-02 AND DWG 146A8130 REV: B 59899U 17MAR21

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB SHIELD SUPPORT ANGLE BS 767-787 RBL 22 WL 156 / CORROSION DAMAGE EVALUATION ON ACB SHIELD SUPPORT ANGLE BS 767-787; RBL 22; WL 156 WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN IN SRM. NEW ACB SHIELD SUPPORT ANGLE WILL BE REPLACED AS PART ASSY 146A8123-20 ON CARD U287967.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

FORWARD CARGO BAY CRACKED INTERCOSTAL BS400 TO BS420 STR26L WL158 / REPLACED FCB INTERCOSTAL BS 400 TO BS 420 STR 26L WL 158 PO # 764707 PER DWG 143A7505 AND SRM 51-40-02-0G-0

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

ACB CRACKED INTERCOSTAL BS 927-947 RBL 21 WL 156 / REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL AT BS 927-947 RBL 21 WL 156 IAW SRM 51-40-02-0G-0 AND DWG

Part: WEB — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB VERTICAL WEB UNDER NUTPLATES BS 792-847 RBL21 WL 156 / REPLACED ACB VERTICAL WEB UNDER NUTPLATES BS 792-847 RBL WL 156 PO# 767063/1 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 146A8120; DWG 146A8121 DWG 146A8340; DWG 146A0081

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB FLOOR TO SIDEWALL SUPPORT BS 727+4' TO 767 RBL 21 WL 156 / CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE PRIXCIMITY TO FASTENER HOLES PER: SRM 53-00-53-1A-2. REMOVED AND REPLACED SUPPORT PER SRM 51-40-02 AND DRAWING 146A7500

Part: FLOOR SPLICE — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB EXISTING FLOOR SPLICE BS 767+5' LBL 13 WL 156 / FOUND OUT OF LIMITS DUE TO NO SRM LIMITS REMOVED AND REPLACED DAMAGE REPAIR PARTS AS PER 737-700 SRM 51-40-02 AS SHOWN IN 1-A53-4982 REV 3.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB FLOOR TO SIDEWALL SUPPORT BS 727+4' TO 847 LBL 21 WL 156 / REMOVED DAMAGED FLOOR TO SIDEWALL SUPPORT AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT BS 847-927 LBL 21 WL 156 IAW SRM 51-40-02-0G & DWG 146A7500 AND 149A8102

Part: WEB — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** ACB WEB BS 787-807 RBL 6 WL 156 / CORROSION ON WEB FOUND OUT OF LIMITS DUE TO PROXIMTY TO FASTENER HOLES RECIEVED SERVICABLE WEB CUSTOMER P.O.# 81825C. LOCATED DRILLED & INSTALLED 787-807 RBL 6 WEB PER SRM 51-46-02-0G-0; SRM 51-40-05-0G-0; DWG 146A8130

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** SIDEWALL TO BULKHEAD SUPPORT BS 947 RBL 21 WL 156 / REMOVED DAMAGED SIDEWALL TO BKD AND INSTALLED NEW SIDEWALL TO BKD SUPPORT BS 947 RBL 21-45 WL 156 IAW SRM 51-40-02-0G-0 & DWG 149A8110; 147A7500

Part: STIFFENER — CRACKED (L/H HORIZ. STAB.) · airframe 53,274 hrs · 31,733 cycles

LT HORIZ. STAB RIB AT STAB STA 129.50 4TH VERT STIFFENER IS CRACKED. / INSTALLED REPAIR LEFT HORIZONTAL STABILIZER RIB STAB STA 129.50 4TH VERTICAL STIFFENER IAW SRM 55-10-09-2R-4

Part: WEB — WORN (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

AT THE EBAY DOOR CUTOUT WEB AT BS 336 STR 28R IS WORN ABOVE DOOR LATCH FITTING / AERA OF 1' X 1.5' X .020' OUT OF .040' ORIGINAL THICKNESS - OUT OF LIMITS PER SRM 53-10-15-1A-3; REPLACED WEB PER SRM 51-40-02; 51-40-05 AND DWG # 141A8511.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** BETWEEN BS 259.5-BS 270 LBL11.20 WL209; SUPPORT CHANNEL TOP FLANGE I/B SIDE HAS CORROSION. / DAMAGE REPAIRED PER EA 21-153-00837 REV IR (ATS ER 21-01495 REV IR). REFER TO NRC 287947 FOR TRACKING.

Part: SKIN — CRACKED (R/H HORIZ. STAB.) · airframe 53,274 hrs · 31,733 cycles

DURING HFEC INSP. FOUND CRACK IN LWR SKIN OF RH HORIZONTAL STAB STA 193.90 RIB. 18 IN. FWD OF REAR SPAR; APPROXIMATELY 2 IN. IN LENGTH. AREA MARKED / REPAIRED RH HORIZ. STAB LWR SKIN AT STAB STA 193.90 RIB; 18' FWD OF REAR SPAR IAW SRM 55-10-01-2R-11. REMOVABLE COMPONENT: P/N 186A2000-41; S/N SAIC0599

Part: FLANGE — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** FWD SIDE TOP FLANGE OF BS 270; BETWEEN LBL11 -RBL11 WL208 HAS CORROSION. / DAMAGE REPAIRED PER EA 21-153-00837 REV IR (ATS ER 21-01495 REV IR). REFER TO NRC U287947 FOR TRACKING. EA 1-A53-13812 REV 3

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** BETWEEN BS 259.5-BS 270 RBL11.20 WL209; SUPPORT CHANNEL TOP FLANGE I/B SIDE HAS CORRO SION. / DAMAGE REPAIRED PER EA 21-153-00837 REV IR (ATS ER 21-01495 REV IR). REFER TO NRC U287947 FOR TRACKING

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

FLOOR SUPPORT IS CRACKED AT BS 540 BL0-LBL25 WL 208 / REMOVED FLOOR SUPPORT AT BS 540 BL0 - LBL25 WL208 PER SRM 51-40-02-0G-0 AND INSTALLED NEW PER SRM 51-40-02-0G-0 AND DWG 143A0060.

Part: FLANGE — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** AFT END OF THE TOP FLANGE OF BS 259.5; BETWEEN LBL11-RBL11 WL 209 HAS CORROSION. / REPAIRED DAMAGE PER EA 21-153-00837 REV IR AND ATS ER 21-01495 REV IR.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

***CORROSION*** BETWEEN BS 259.5- BS270 BL0 WL 209; INTERCOSTAL SUPPORT CHANNEL HAS CORROSION. / DAMAGE REPAIRED PER EA 21-153-00837 REV IR (ATS ER 21-01495 REV IR). REFER TO NRC U287947 FOR TRACKING.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT R.B.L. 29; W.L. 150. / REMOVED AND REPLACED BS 663 LOWER COMPOSITE BULKHEAD @ RBL 29 WL 150 IAW SRM 51-40-02 AND DWG 111A1000.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

FLOOR PANEL 231YF INSERT IS DAMAGED AT FWD L/H UPPER CORNER (MARKED) / IDENTIFIED FLOOR PANEL 231YF IAW SRM 53-00-50-0I-1 FIGURE 4; SHEET 1; TABLE 4. UPON INSPECTION OF PANEL FOUND MULTIPLE AREAS OF DAMAGE TO UPPER AND LOWER SURFACES. DAMAGED INSERT AT FWD L/H UPPER CORNER; AS MARKED; AND DAMAGE FOUND ON FLOOR PANEL 231YF ARE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR 4E(2B). DUE TO THE EXTENT OF DAMAGE OPTED TO FABRICATE NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 PAR 1A(NOTE); 4A(2). FABRICATED NEW FLOOR PANEL OUT OF BMS 4-17 TYVI LOT # 420733-1; LOCATED; DRILLED; UPSIZED; AND INSTALLED ALL INSERTS USING BMS 5-107 LOT # AK0HP5746K; CURED; AND PART MARKED PANEL IAW DWG 144A5810-124; BAC5085 PAR 8.4.2.2 A-F; AND SRM 53-00-50-2R-0 PAR4A(2).56563U 14MAR21

Part: SKATE ANGLE — CRACKED (FUSELAGE) · airframe 53,274 hrs · 31,733 cycles

LT FWD FIN TO BODY SKATE ANGLE IS CRACKED / REMOVED & REPLACED LT FWD FIN TO BODY SKATE ANGLE IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; DWG #S 147A0070; 147A0030 & AMM 51-21-99-300-802 56304U 10MAR21

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 53,274 hrs · 31,733 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. THE DAMAGE IS REPAIRED PER EA 1A5333179 REV 1.

Part: STIFFENER — CRACKED (R/H HORIZ. STAB.) · airframe 53,274 hrs · 31,733 cycles

R/H HORIZONTAL STABILIZER RIB 5 STA 129.50; 2ND VERTICAL STIFFENER IS CRACK. / REPAIRED L/H HORIZONTAL STABILIZER RIB 5 AT STAB STA 129.50 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-5; SRM 51-40-02-0G-0; - AND DWG #'S 182A1500; 182A3001; 0020001; 182A2401. 59796C 18MAR21

Part: STIFFENER — CRACKED (R/H HORIZ. STAB.) · airframe 53,274 hrs · 31,733 cycles

R/H HORIZONTAL STABILIZER RIB 5 STA 129.50; 3RD VERTICAL STIFFENER IS CRACK. / REPAIRED RT HORIZONTAL STABILIZER RIB 5 STAB STA 129.50 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4. 59796C 15MAR21

Part: STIFFENER — CRACKED (L/H HORIZ. STAB.) · airframe 53,274 hrs · 31,733 cycles

L/H HORIZONTAL STABILIZER RIB 5 STA 129.50; 3RD VERTICAL STIFFENER IS CRACK. / REPAIRED L/H HORIZONTAL STABILIZER RIB 5 STAB STA 129.50 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-5; SRM 51-40-02-0G-0; DWG #'S: 182A1500; 182A3001; 002A0001; 182A2401 59796C 18MAR21

Part: STIFFENER — CRACKED (L/H HORIZ. STAB.) · airframe 53,274 hrs · 31,733 cycles

L/H HORIZONTAL STABILIZER RIB 1 STA 92.70; 2ND VERTICAL STIFFENER POSSIBLE CRACK. / REPAIRED L/H HORIZONTAL STABILIZER RIB 1 STAB STA 92.70; 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4; 51-40-02-0G-0; DWG #'S: 182A1500; 132A3001; 002A0001. 59796C 16MAR21

Part: SIGN — CRACKED (AFT GALLEY) · airframe 53,106 hrs · 31,634 cycles

REF: SA-M H24954-1_AFT GALLEY R/H EME EXIT SIGN OVER DOOR CRACKED / R&R EXIT SIGN REF 33-51-01

Part: STRAP — BROKEN (AFT FLASHLIGHT) · airframe 52,588 hrs · 31,326 cycles

AFT F/A FLASHLIGHT SEAL/STRAP BROKEN. REPLACED AFT F/A FLASHLIGHT SEAL/STRAP, REF 25-61-00.

Part: SKIN — WORN (BS 888) · airframe 52,228 hrs · 31,101 cycles

FUSELAGE SKIN WEAR FWD OF BS888; BETWEEN STR 1L AND STR 2L. / AREA REPAIRED PER EA 20-153-01468

Part: LAMP — INOPERATIVE (EXTERIOR) · airframe 52,177 hrs · 31,067 cycles

LH WING/SLIDE EMERGENCY LIGHT INOP. RELAMPED LH WING/SLIDE EMERGENCY LIHGT IAW AMM 33-51-04

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,735 hrs · 30,782 cycles

FWD ESCAPE SLIDE EMERGENCY LIGHT RT INOP. R&R'D BATTERY PACK M1674 PER MM 33-51-06; OPS CHECK GOOD.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 51,456 hrs · 30,612 cycles

REF. G717376 R/H MLG WHEEL WELL WING CENTER SECTION FWD BULKHEAD (REAR SPAR BS 663) LOWER WEB VAPOR BARRIER HAS 10" CRACK BETWEEN RBL 25-RBL 31.83 ACCOMPLISHED A PERMANENT REPAIR PER SRM 57-10-10 PARAGRAPH 2.C(4A)/ALLOWABLE DAMAGE 2. REPAIR REQUIRES A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLES INTERVALS OR MORE FREQUENTLY.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 51,227 hrs · 30,468 cycles

RH MAIN LANDING GEAR WHEEL WELL WING CENTER SECTION FORWARD BULKHEAD REAR SPAR LOWER WEB VAPOR BARRIER CRACKED AT BS. 663, BETWEEN RBL 25 TO RBL 31.83. / REPAIRED BARRIER PER EA. *

Part: PAN — CRACKED (R2 DOOR) · airframe 51,227 hrs · 30,468 cycles

AFT SERVICE DOOR LOWER DOOR PAN IS CRACKED ON BOTTOM RIGHT CORNER. / R&R AFT SERVICE DOOR LOWER PAN PER AMM 52-41-31.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 51,227 hrs · 30,468 cycles

RH MLG WHEEL WELL WING CENTER SECTION FWD BULKHEAD (REAR SPAR BS663) LOWER WEB VAPOR BARRIER HAS 6' CRACK BETWEEN RBL 25 - RBL 31.83 / CRACK NOW FOUND TO BE 10'. ACCOMPLISHED A INTERIM REPAIR PER SRM 57-10-10 PAR 2.C(4A) ALLOWABLE DAMAGE 2 REPAIR REQUIRES REINSPECT. SEE LOG PAGE #1260482

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 50,871 hrs · 30,232 cycles

L1 DOOR SLIDE FELL OUT. / REPOSITIONED SLIDE PER MT.

Part: BATTERY — FAILED (CABIN) · airframe 49,284 hrs · 29,210 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,357 hrs · 28,618 cycles

L/H OVERWING EMERGENCY EXIT IDENTIFIER BULBS BURNED OUT. / R&R EXIT SIGN LIGHT ASSEMBLY PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,357 hrs · 28,618 cycles

L/H OVERWING EMERGENCY EXIT IDENTIFIER BULBS BURNED OUT. / R&R LAMP PER AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 48,357 hrs · 28,618 cycles

AFT CARGO DOOR AFT CORNER SCUFF PLATE IS BROKEN / REMOVED AFT CORNER SCUFF PLATE ACB CARGO DOOR IAW SRM 51-40-02-0G-0 AND LOCATED AND DRILLED NEW SCUFF PLATE IAW SRM 51-40-05-0G-0 OK TO INSTALL. LEAD 113 09APR19 INSP 35 9APR19 INSTALLED ACD CORNER SCUFF PLATE IAW AMM 53-11-02-420-801 56334U 09APR19

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 48,357 hrs · 28,618 cycles

FWD CARGO BAY FWD CORNER SCUFF PLATE IS BROKEN / REMOVED FWD CORNER SCUFF PLATE FCB IAW SRM 51-40-02 AND LOCATED AND DRILLED NEW SCUFF PLATE IAW SRM 51-40-05-0G-0 OK TO INSTALL. LEAD 113 09APR19 INSP 35 9APR19 INSTALLED FWD CARGO BAY FWD CORNER SCUFF PLATE IAW AMM TASK 53-11-02-420-801. 59351U 09APR19

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 48,357 hrs · 28,618 cycles

FWD CARGO BAY AFT CORNER SCUFF PLATE IS BROKEN / REMOVED AFT CORNER SCUFF PLATE FCB; LOCATED AND DRILLED NEW SCUFF PLATE IAW SRM 51-40-05-0G-0 AND OK TO INSTALL. LEAD 113 09APR19 INSP 35 9APR19 INSTALLED FWD CARGO BAY AFT CORNER SCUFF PLATE IAW AMM TASK 53-11-02-420-801. 59351U 09APR19

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 48,357 hrs · 28,618 cycles

FSD #4 LOWER BEAM CRACKED. / REPAIRED FSD #4 LOWER BEAM ON WORK ORDER 522541 59803U 11APR19 (POS:FSD; TAG NO:544896; P/N OFF:141A6516-20M; S/N OFF:002476; P/N ON:141A6516-20M; S/N ON:002476)

Part: SEAT TRACK — DAMAGED (BS 480) · airframe 48,357 hrs · 28,618 cycles

SEAT TRACK MECHANICAL DAMAGED BETWEEN BS. 480 TO BS. 520, LBL 45. R&R SEAT TRACK IAW SRM.

Part: SEAT TRACK — DAMAGED (BS 480-520) · airframe 48,357 hrs · 28,618 cycles

SEAT TRACK MECHANICALLY DAMAGED BETWEEN BS. 480 TO BS. 520, LBL 24.5. / R&R SEAT TRACK IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WHEEL WELL) · airframe 48,357 hrs · 28,618 cycles

LEFT HAND LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT B.S. 663; L.B.L.10 . W.L. 164. / REPAIRED LEFT HAND LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE AT BS 663 LBL 10 WL 164 IAW ATS ER 19-02703 REV IR AND EA 1-757-16160 REV IR

Part: ATTACH ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 48,357 hrs · 28,618 cycles

R/H LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE CRACKED AT BS. 663, LBL10. / REPAIRED ANGLE PER ER AND EA.

Part: BRACKET — LOOSE (L1 DOOR) · airframe 48,021 hrs · 28,416 cycles

L1 DOOR GIRT BAR SUPPORTS LOOSE. SECURED BRACKETS PER SIP.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 48,021 hrs · 28,416 cycles

R1 DOOR GIRT BAR SUPPORTS LOOSE. SECURED BRACKETS PER SIP.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 47,731 hrs · 28,229 cycles

R1 DOOR SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,068 hrs · 27,788 cycles

LT EMERGENCY LIGHT INOP AT SEAT 9. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,531 hrs · 27,437 cycles

LT EMERGENCY EXIT DOOR LIGHT INOP. R&R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,345 hrs · 26,671 cycles

L2 DOOR INTERIOR EMERGENCY EXIT LIGHT BULBS INOP. R&R BULBS PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 45,339 hrs · 26,667 cycles

BATTERY PACK FAILED CAPACITY CHECK AT M1672. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 45,339 hrs · 26,667 cycles

BATTERY PACK FAILED CAPACITY CHECK AT M1669. R&R BATTERY PACK PER AMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 45,339 hrs · 26,667 cycles

EPGR DOOR DOUBLER FILLER CRACKED / REMOVED EXISTING CRACKED FILLER FOR EPGR DOOR DOUBLER FROM 7075T6 .050 M#1300812-1 LOCATED; DRILLED; APPLIED CHEMICAL CONVERSION COATINGS PRIMED & INSTALLED PER SRM 53-10-15-2R-4

Part: BATTERY PACK — FAILED (CABIN) · airframe 45,339 hrs · 26,667 cycles

BATTERY PACK FAILED CAPACITY CHECK AT M1675. R&R BATTERY PACK PER AMM.

Part: SWITCH — FAULTED (CABIN PRESSURE) · airframe 41,617 hrs · 24,313 cycles

PASSING THROUGH FL 360 DURING CLIMB OUT, CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE WAS 5500 FT, CABIN DIFFERENTIAL PRESSURE APPROACHED 9. DIVERTED. R & R THE NR 2 CABIN PRESSURE SWITCH IAW MM.

Part: SKIN — DELAMINATED (L/H WING) · airframe 41,604 hrs · 24,304 cycles

LEFT WING LOWER SKIN INBD EDGE OF OTBD FLAP DELAMINATED. REPAIRED SKIN IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,604 hrs · 24,304 cycles

INTERCOSTAL WEB CRACKED BETWEEN BS 500C TO BS 500D, STR 26L. R&R WEB IAW SRM AND DWG.

Part: CARGO TRACK — CRACKED (BS 727E) · airframe 41,604 hrs · 24,304 cycles

AFT CARGO TRACK CRACKED AT BS 727E, RBL 13.84. REPAIRED THE CARGO TRACK IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,604 hrs · 24,304 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 500C, STR 26L. R&R ANGLE IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,604 hrs · 24,304 cycles

FORWARD CARGO COMPARTMENT ANGLE CLIP CRACKED AT BS 500C, STR 26L. R&R CLIP IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (BS 500A-500B) · airframe 41,604 hrs · 24,304 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500A TO 500B, STRINGER 26L. R & R INTERCOSTAL IAW SRM AND DWG.

Part: ANGLE — CRACKED (BS 500B) · airframe 41,604 hrs · 24,304 cycles

FORWARD CARGO BAY ANGLE CRACKED AT BS 500B, STRINGER 26L. R & R THE ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (BS 500C) · airframe 41,604 hrs · 24,304 cycles

FORWARD CARGO BAY ANGLE CRACKED AT BS 500C, STRINGER 26R. R & R THE ANGLE IAW SRM AND DWG.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 41,604 hrs · 24,304 cycles

LEFT WING OUTBOARD AFT FLAP DELAMINATED. REPAIRED THE FLAP IAW SRM.

Part: SKIN — DELAMINATED (TAILCONE) · airframe 41,604 hrs · 24,304 cycles

TAIL CONE SKIN DELAMINATED AT BS1156 +27", LBL 12. REPAIRED SKIN IAW SRM.

Part: SKIN — DELAMINATED (TAILCONE) · airframe 41,604 hrs · 24,304 cycles

RIGHT TAILCONE SKIN DELAMINATED AT BS 1156 +6.5. REPAIRED THE SKIN IAW SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 41,604 hrs · 24,304 cycles

FUSELAGE GUSSET CRACKED AT BS 500D, STRINGER 19L. R & R THE GUSSET IAW SRM.

Part: CHANNEL — CRACKED (BS 540 FLOORBEAM) · airframe 41,604 hrs · 24,304 cycles

FLOORBEAM CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24.5. R&R FLOORBEAM CHANNEL IAW SRM AND DWG.

Part: ANGLE — CRACKED (BS 663) · airframe 41,604 hrs · 24,304 cycles

ANGLE CRACKED AT BS 663.75+29, BL 0. R&R ANGLE IAW SRM AND DWG.

Part: LIGHT — DETACHED (CABIN) · airframe 39,798 hrs · 23,258 cycles

CEILING OVERWING EXIT AISLE LIGHT FELL OFF. R & R THE LIGHT ASSEMBLY IAW SIP.

Part: HOLDER — LOOSE (L1 DOOR) · airframe 39,177 hrs · 22,903 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOLDER LOOSE. R & R HOLDER IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,177 hrs · 22,903 cycles

EMERGENCY LIGHTS BATTERY PACK AT LOCATION M1668 FAILED CAPACITY CHECK. R & R BATTERY PACK IAW DWG.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 38,730 hrs · 22,634 cycles

L1 DOOR SLIDE INADVERTENTLY FELL OUT OF COMPARTMENT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: SIGN — UNSECURE (CABIN) · airframe 37,689 hrs · 220,264 cycles

R1 DOOR EMER EXIT SIGN FELL OFF. R & R LIGHT ASSEMBLY IAW MM.

Part: WEB — CRACKED (R1 DOOR) · airframe 36,923 hrs · 21,585 cycles

R1 DOOR BOTTOM LT DOOR MECHANISM HARDWARE ATTACH POINT TO DOOR, WEB STRUCTURE CRACKED. R & R DOOR IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 36,923 hrs · 21,585 cycles

M1668 EMER LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,805 hrs · 20,919 cycles

FLIGHT DECK, RT NR 1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER. REPAIRED FRAME IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 35,805 hrs · 20,919 cycles

NUMBER 3 LT COCKPIT WINDOW POST CRACKED. REPAIRED POST IAW SI.

Part: POST — CRACKED (FUSELAGE) · airframe 35,805 hrs · 20,919 cycles

NUMBER 3 RT COCKPIT WINDOW POST CRACKED. REPAIRED POST IAW SI.

Part: FAIRING — CRACKED (TE FLAP) · airframe 35,805 hrs · 20,919 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING 642BB, AFT END, AT APPROX. 8 O CLOCK POSITION LOOKING FORWARD, CRACKED. REPAIRED FAIRING IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,805 hrs · 20,919 cycles

FORWARD CABIN SEAT TRACK FLANGE CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,805 hrs · 20,919 cycles

FORWARD CABIN SEAT TRACK FLANGE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,805 hrs · 20,919 cycles

SEAT TRACK CRACKED AT STATION 727B, RBL 45.5. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,805 hrs · 20,919 cycles

FORWARD CABIN SEAT TRACK FLANGE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,805 hrs · 20,919 cycles

FORWARD CABIN SEAT TRACK FLANGE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 35,805 hrs · 20,919 cycles

AFT SIDE LT WW CRACKED AT BS 663, BETWEEN LBL 25 TO 45. REPAIRED WW IAW SRM.

Part: LENS — UNSECURE (CABIN) · airframe 35,252 hrs · 20,605 cycles

LEFT EMER EXIT LIGHT LENS FELL OFF. R & R LENS IAW SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,808 hrs · 20,348 cycles

RIGHT OVERWING EMER LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,598 hrs · 19,086 cycles

MID CABIN EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,598 hrs · 19,086 cycles

CEILING AFT ENTRY EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,598 hrs · 19,086 cycles

FORWARD ENTRY EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 32,598 hrs · 19,086 cycles

FUSELAGE WW FWD BULKHEAD CRACKED AT BS 663 RBL 43. REPAIRED BULKHEAD IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 32,598 hrs · 19,086 cycles

FLOORBOARD SUPPORT BRACKET CRACKED AT BS 540 RT OF CTR. R & R BRACKET IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 32,598 hrs · 19,086 cycles

FLOORBOARD SUPPORT BRACKET CRACKED AT BS 540, LT OF CTR. R & R BRACKET IAW SRM.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 32,501 hrs · 19,027 cycles

AIR TURN BACK & DECLARED EMER. NR 2 ENG EGT SPIKE 950 DEG C, VIBRATION 4.8. KEPT ENG AT IDLE FOR REMAINDER OF FLIGHT. R & R NR 2 ENG IAW MT.

Part: POST — CRACKED (FUSELAGE) · airframe 32,087 hrs · 18,800 cycles

L1 WINDOW OTBD POST AFT UPPER CORNER JUST BELOW RADIUS CRACKED IN SKIN. REPAIRED POST IAW EA.

Part: LENS — MISSING (CABIN) · airframe 29,087 hrs · 17,023 cycles

R2 DOOR EMERGENCY EXIT LIGHT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 28,761 hrs · 16,846 cycles

FLOOR BOARD PANEL 221BF AFT OUTBOARD EDGED BROKEN. REPAIRED PANEL IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 28,761 hrs · 16,846 cycles

GROUND POWER INTERNAL DOUBLER CRACKED. REPAIRED DOUBLER IAW EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 28,761 hrs · 16,846 cycles

FLOOR SUPPORT STRAP CORRODED BETWEEN STA 1016 TO STA 1030, RBL 2. R & R FLOOR STRAP IAW SRM AND DWG.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 28,761 hrs · 16,846 cycles

AFT WET AREA, PRESSURE DECK FLOORBOARD 241AEF, INBD AFT EDGE DELAMINATED. REPAIRED FLOORBOARD IAW SRM.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 28,761 hrs · 16,846 cycles

AFT WET AREA, PRESSURE DECK FLOORBOARD 241AEF, OTBD AFT EDGE DELAMINATED. REPAIRED FLOORBOARD IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 28,761 hrs · 16,846 cycles

AFT WET AREA, RT SIDE AFT GALLEY DOOR SCUFF PLATE INBD SUPPORT CORRODED. R & R SUPPORT IAW SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 28,761 hrs · 16,846 cycles

AFT WET AREA, STA 1016 TO STA 1030, LBL 2 FLOOR SUPPORT STRAP CORRODED. R & R STRAP IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,761 hrs · 16,846 cycles

INTERCOSTAL CRACKED BETWEEN STA 312 TO STA 328, LBL 48. R & R INTERCOSTAL IAW DWG AND SRM.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 28,761 hrs · 16,846 cycles

FLOORBEAM CORRODED AT STA 344, BL 0. R & R FASTENER IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,761 hrs · 16,846 cycles

LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED IN SKIN ON INBD SIDE OF STAB. STA 101.9, RIB, 19.750" TO 20.500" FROM AFT EDGE OF AFT SPAR. R & R SKIN IAW CCO.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,761 hrs · 16,846 cycles

LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED IN SKIN ON INBD SIDE OF STABILIZER STA 157.10, RIB, 9.125" TO 9.500" FROM AFT EDGE OF AFT SPAR. R & R SKIN IAW CCO.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,761 hrs · 16,846 cycles

LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED IN SKIN ON INBD SIDE OF STABILIZER STA 101.9, RIB, 10.625" TO 11.625" FROM AFT EDGE OF AFT SPAR. R & R SKIN IAW CCO.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,761 hrs · 16,846 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. R & R SKIN IAW CCO.

Part: SEAL — MISSING (FLAP FAIRING) · airframe 28,078 hrs · 16,440 cycles

NR 3 FLAP CANOE OTBD SIDE CENTER BULB-SEAL AND RUBSTRIP MISSING. R & R FAIRING IAW AMM.

Part: SLIDE — OUT OF LIMITS (L2 DOOR) · airframe 27,875 hrs · 16,316 cycles

L2 DOOR SLIDE PRESS INDICATOR OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 27,713 hrs · 16,208 cycles

REAR ENTRY SLIDE HARD TO READ SLIDE PRESSURE. REPOSITIONED SLIDE PER M/M.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,666 hrs · 15,596 cycles

RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: SIGN — UNSECURE (CABIN) · airframe 26,264 hrs · 15,377 cycles

FRONT GALLEY EMERGENCY EXIT SIGN FELL OFF. REMOVED AND REPLACED SIGN PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 25,862 hrs · 15,169 cycles

OVERWING EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: FASTENER — LOOSE (GIRT BAR) · airframe 24,796 hrs · 14,585 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED FASTENERS PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 24,690 hrs · 14,524 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,659 hrs · 14,508 cycles

LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,009 hrs · 14,132 cycles

AFT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT PER M/M.

Part: LENS — LOOSE (CABIN) · airframe 23,691 hrs · 13,959 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 7. REMOVED AND REPLACED LENS IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 22,643 hrs · 13,340 cycles

DURING SCHEDULED CV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REMOVED AND REPLACED SLIDE IAW MT.

Part: LIGHT — LOOSE (CABIN) · airframe 22,133 hrs · 13,043 cycles

EMERGENCY EXIT LIGHT STRIP LOOSE. REMOVED AND REPLACED ENDCAP PER MM.

Part: LENS — MISSING (CABIN) · airframe 22,073 hrs · 13,006 cycles

LT EEPLS MISSING AT ROW 7. REMOVED AND REPLACED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 21,927 hrs · 12,921 cycles

EEPLS LENS MISSING. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 21,917 hrs · 12,913 cycles

AFT EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,760 hrs · 12,806 cycles

DURING SCHEDULED 6Y CHECK FOUND, AFT CARGO FLOORBEAM JOGGLE HOLES CORRODED AT BS 772, LBL 8. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,760 hrs · 12,806 cycles

DURING SCHEDULED 6Y CHECK FOUND, AFT CARGO FLOORBEAM JOGGLE HOLES CORRODED AT BS 772, RBL 8. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,760 hrs · 12,806 cycles

DURING SCHEDULED 6Y CHECK FOUND, AFT CARGO FLOORBEAM JOGGLE HOLES CORRODED AT BS 772, LBL 3. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,760 hrs · 12,806 cycles

DURING SCHEDULED 6Y CHECK FOUND, AFT CARGO FLOORBEAM JOGGLE HOLES CORRODED AT BS 772, LBL 18. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,760 hrs · 12,806 cycles

DURING SCHEDULED 6Y CHECK FOUND, AFT CARGO FLOORBEAM JOGGLE HOLES CORRODED AT BS 772, LBL 13. REPAIRED BEAM PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,584 hrs · 12,704 cycles

DURING SCHEDULED HC1 CHECK FOUND, LT OVERWING EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 17,784 hrs · 10,443 cycles

DURING SCHEDULED SPV CHECK, FOUND LOWER FUSELAGE SKIN CORRODED AT BS 354, BL 0. REPAIRED SKIN PER AAR EA.

Part: LIGHT — CRACKED (CABIN) · airframe 17,029 hrs · 9,973 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.

Part: SIGN — MISSING (CABIN) · airframe 16,526 hrs · 9,669 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED SIGN PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 15,972 hrs · 9,339 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CASE, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 14,840 hrs · 8,633 cycles

DURING SCHEDULED HC2 CHECK, BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COFFEEMAKER — FAULTY (AFT GALLEY) · airframe 13,390 hrs · 7,768 cycles

30 MIN FROM LAS F/A REPORTED SMOKE FROM AFT COFFEE MAKER. SECURED GALLEY POWER AND SMOKE STOPPED, LANDED IN LAS. REMOVED AND REPLACED NR 1 AFT GALLEY COFFEE MAKER PER MM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 12,106 hrs · 6,959 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 10,905 hrs · 6,228 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT ASSY BROKEN AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 10,842 hrs · 6,193 cycles

FWD CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: LENS — LOOSE (CABIN) · airframe 10,647 hrs · 6,068 cycles

EEPLS LIGHT LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 10,528 hrs · 5,994 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — LOOSE (CABIN) · airframe 10,456 hrs · 5,948 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 10,387 hrs · 5,908 cycles

EEPLS LOOSE AT ROW 3 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 10,378 hrs · 5,902 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS LENS MISSING AT ROW 5 ABC. INSTALLED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 8,354 hrs · 4,698 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 8,130 hrs · 4,567 cycles

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

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 7,913 hrs · 4,430 cycles

FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 7,817 hrs · 4,378 cycles

FWD EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 5,212 hrs · 2,865 cycles

EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED EEPLS COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 5,190 hrs · 2,853 cycles

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

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 5,168 hrs · 2,840 cycles

EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED EEPLS COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 3,869 hrs · 2,121 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — MISSING (CABIN) · airframe 3,558 hrs · 1,964 cycles

EEPLS COVER MISSING AT RT FWD CABIN. INSTALLED EEPLS COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,561 hrs · 1,382 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT FWD END. RECONNECTED EEPLS WIRE TO LIGHT SOCKET PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 1,203 hrs · 663 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 8 ABC. INSTALLED COVER PER MM.