N966WN

Part: ENGINE — SHUTDOWN (NR 1) · airframe 44,979 hrs · 27,828 cycles

NUMBER 1 ENGINE ON SHUTDOWN, ENG FAIL APPEARED ON DISPLAY. DISAPPEARED AFTER AROUND 10 SECONDS. PERFORMED EEC BITE NR 1 ENGINE, MSG 76-31361 SHOWS THE START LEVER DISAGREE ON SHUTDOWN. PERFORMED NR 1 ENGINE RUN PER MM 71-00-00. NO ABNORMAL PARAMETERS SHOWED ON SHUTDOWN. EEC BITE SHOWS NO FAULTS. ACFT OK FOR SERVICE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 44,820 hrs · 27,723 cycles

FORWARD CABIN FLOOR PANEL 231FF UPPER COMPOSITE PLY PULLED AWAY AND DISBONDED AT AFT END. REPAIRED COMPOSITE DAMAGE ON CABIN FLOOR PANEL 231FF IAW B737 SRM 53-00-50-2R-1; REPAIR 1. REPAIRS COMPLETED IAW SRM 53-00-50-2R-1-A AND EA M-25-153-02385.

Part: SEAL — DEBONDED (ZONE 300) · airframe 44,820 hrs · 27,723 cycles

RUDDER BLADE SEAL 324RL DISBONDED. REMOVED AND REPLACED ON SHELF REF IPC 55-30-00-31 ITEM 75.

Part: SEAL — DEBONDED (ZONE 300) · airframe 44,820 hrs · 27,723 cycles

RUDDER BLADE SEAL 324ABL DISBONDED. REPLACED RUDDER BLADE SEAL 324ABL ON SHELF IAW AIPC 55-30-00-21 ITEM 25 PG. 6.

Part: SEAL — DEBONDED (ZONE 300) · airframe 44,820 hrs · 27,723 cycles

DOT A24-16 RUDDER BLADE SEAL 324ZL DISBONDED. REPLACED RUDDER BLADE SEAL 324ZL ON SHELF IAW AIPC 55-30-00-21 ITEM 35 PG. 7.

Part: SEAL — DEBONDED (ZONE 300) · airframe 44,820 hrs · 27,723 cycles

RUDDER BLADE SEAL 324AAL DISBONDED. REPLACED RUDDER BLADE SEAL 324AAL ON SHELF IAW AIPC 55-30-00-21 ITEM 30 PG. 6.

Part: FLOORBOARD — PEELING (ZONE 200) · airframe 44,820 hrs · 27,723 cycles

MAIN CABIN FLOORBOARD 222DF THE FIBER IN TOP SIDE OF PANEL IS PEELING. REFER TO FAULT TTG8Q014XXD0 WHERE EA 25-153-02429 WAS ADDED AS A SUBTASK.

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 44,820 hrs · 27,723 cycles

R1 DOOR; BETWEEN S-8 AND S-9 RIGHT; INTERNAL STUB FRAME CRACKED; NOTED BY HFEC ABOVE SEAL DEPRESSOR<[01] REMOVED CRACKED INTERNAL STUB FRAME AT R1 DOOR; BETWEEN S-8 AND S-9 AND REPLACED WITH NEW STUB FRAME; P/N 141A8370U13 TAG# WN 51731; IAW SRM 51-40-02-0G-0 AND BOEING DGW 141A8370 REV:D ;141A8380 REV: -

Part: ANGLE — DAMAGED (ZONE 600) · airframe 44,820 hrs · 27,723 cycles

RIGHT WING PANEL 651 FB FWD EDGE 26, INBD OF OTBD END LT ATTACH ANGLE HAS 2 EA ELONGATED HOLES. REMOVED RT WING PNL 651FB; 26' IB OF OB END; L ATTACH ANGLE WITH 2 EA ELONGATED HOLES AND REPLACED WITH NEW L ATTACH ANGLE; PN 287A9152-24 IAW SRM 51-40-02-0G-0 AND DWG 115A2710 0007, REV-.

Part: PLATE — CRACKED (ZONE 600) · airframe 44,820 hrs · 27,723 cycles

RIGHT WING OTBD OF ACCESS PANEL 651DB HAS CRACKED WIGGLE PLATE. REMOVED AND REPLACED WIGGLE PLATE OTBD OF PANEL 651DB IAW SRM 51-40-02-0G-0 AND DWG 115A2001, REV-.

Part: PLATE — CRACKED (ZONE 500) · airframe 44,820 hrs · 27,723 cycles

LEFT WING OTBD OF ACCESS PANEL 551DB HAS CRACKED WIGGLE PLATE. REMOVED AND REPLACED WIGGLE PLATE OTBD OF PANEL 551DB IAW SRM 51-40-02-0G-0 AND DWG.115A2001, REV-.

Part: THRESHOLD — CRACKED (ZONE 100) · airframe 44,820 hrs · 27,723 cycles

AFT CARGO DOOR CUTOUT; FWD CORNER THRESHOLD CRACKED. REPAIRED ON BACK SHOP W/O 47165/0000/0001 SERIAL NO. 9720058 SHOP REQUEST BY WELDING IAW SRM 53-60-15-2R-1.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 44,820 hrs · 27,723 cycles

MAIN CABIN SEAT TRACK AT LBL 45 BETWEEN STA 807+17' AND STA 807+19' UPPER CROWN HAS WEAR. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R-5-A00847, AND DWG: 146A5300 REV-, REPAIR 5, SECTION 46.

Part: SEAT TRACK — WORN (ZONE 200) · airframe 44,820 hrs · 27,723 cycles

MAIN CABIN SEAT TRACK AT LBL 45 STA 520 UPPER CROWN HAS WEAR. REMOVED WEAR DAMAGE FROM MAIN CABIN SEAT TRACK AT LBL 45 STA 520 UPPER CROWN IAW SRM 51-10-02-0G-0; DAMAGE CLEAN UP DEPTH .025'; MAX CLEAN UP DEPTH ALLOWED .020'. FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1. CUT AND REPLACED OUT OF LIMITS SEAT TRACK FROM BS 500C+10' - 520 IAW SRM 53-00-52-2R-4.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 44,820 hrs · 27,723 cycles

SEAT TRACK RBL 45 FROM STA. 440+2' IS CORRODED AT THE LOWER CROWN. COUNTERSUNK SEAT TRACK REPAIR STA 380-480 RBL 45' IAW SRM 51-40-08-0G-0. REMOVED CORROSION FROM LOWER CROWN OF SEAT TRACK AT RBL 45 AT STA 440+2' AND VERIFIED WITH 10X MAGNIFIER ALL REMOVED IAW SRM 51-10-02-0G-0, DAMAGE CLEAN UP DEPTH WAS .047'; MAX CLEAN UP DEPTH ALLOWED .040'; OUT OF LIMITS IAW SRM 53-00-52-1A-1. REPLACED THE SEAT TRACK IAW SRM 51-40-02-0G-G AND DWG 143A5300 ID:0055 REV-.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 44,820 hrs · 27,723 cycles

MAIN CABIN SEAT TRACK AT LBL 45 BETWEEN BS 727B -747+5' LOWER CROWN HAS CORROSION IN MULTIPLE AREAS. REPAIRED IAW DWG 146A5300 REV: -, EVALUATED MATERIAL LOSS OF .043 MAX LOSS OF .040 IAW SRM 53-00-52-1A-1, FOUND TO OUT OF LIMITS. CUT AND REMOVED SEAT TRACK AT BS 727B - 727E + 10', LBL 45 IAW SRM 53-00-52-2R-5. COMPLETED INSTALLING SEAT TRACK REPAIR SECTIONS LBL 45 STA 727B - 887 IAW SRM 53-00-52-2R-5 AND DWG 146A5300 REV-.

Part: PUMP — FAULTED (FUEL SYS) · airframe 54,608 hrs · 32,907 cycles

DURING CLIMB THE NUMBER 2 ENGINE WOULD MOT MAKE CLIMB POWER. AT 230 LEVEL IT RETURNED TO NORMAL INDICATIONS. R&R FUEL PUMP IAW MT 773-11-00 AND AMM 73-11-11-401-NG.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 44,389 hrs · 27,463 cycles

RH ROWS 2 THRU 6 EMERGENCY LIGHTS ARE INOP. REMOVED RT FWD BATTERY PACK PER AMM 33-51-06. INSTALLED RH FWD BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD. INSPECTED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 43,703 hrs · 27,046 cycles

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

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 43,703 hrs · 27,046 cycles

THE EMERGENCY LIGHTING BATTERY PACK AT THE R/H OVERWING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.

Part: BATTERY — NO TEST (ZONE 200) · airframe 43,703 hrs · 27,046 cycles

THE EMERGENCY LIGHTING BATTERY PACK AT THE L/H OVERWING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 60,006 hrs · 35,879 cycles

APPROACHING FL35 LEFT ENG BEGAIN TO SURGE & STALL WITH ASSOLIATED POPPING NOISES BEING HEADED IN THE CABIN. N1 WAS MANUALLY REDUCED TO 54% WHERE THE ENG STABILIZED.

Part: FSEU — FAULT MESSAGE (ZONE 500 FLAP) · airframe 42,427 hrs · 26,275 cycles

LE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED IN FLIGHT INTERROGATED FSEU AND PSEU NO CURRENT FAULTS OR FAULT HISTORY FOUND SAME FOR MCO MX.. NO RECENT HISTORY NO FAULTS CHANGED FSEU AS PRECAUTION. C/W FIM TASK 27-88/820; PERFORMED FSEU BITE; NO FAULTS FOUND. OK TO CONTINUE PER MEL 27-4-02 SP1;[02] R & R FSEU REF 27-51-01 OPS CHECK NORMAL.

Part: WARNING LIGHT — FALSE ACTIVATION (LE FLAPS) · airframe 42,090 hrs · 26,061 cycles

LE FLAPS TRANSIT REMAINING ILLUMINATED WITH FLAPS 5 EXTENDED<[01] PERFORMED FSEU BITE NO FAULTS FOUND; OK TO CONTINUE PER MEL 27-4-02 SP1;[02] 02 - INSPECTED PER [AMM 27-88-00-201-NG (LEADING EDGE FLAP AND SLAT POSITION INDICATING SYSTEM - MAINTENANCE PRACTICES - PERMANENT)] INSPECTED AND OPERATED FLAPS LE SYSTEM . NO TRANSIT LIGHT REAINS ON AT FLAPS 5 . FSCU SHOWS NO FAULTS OR FAULT HISTORY. ALL SENSORS SHOW NORMAL NEAR/FAR INDICATIONS . NO DEFECTS NOTED. I/A/W AMM 27-88-00 THIS CLEARS AUTH# 219627 RE-INSTALLED LAMPS IN INDICATOR.

Part: SLIDE — OUT OF POSITION (ZN 800 DOOR) · airframe 41,313 hrs · 25,555 cycles

FWD ENTRY DOOR SLIDE OUT OF DOOR MOUNTED COVER<[01] REMOVED AND REPLACED FWD ENTRY SLIDE IAW AMM 25-66-01

Part: TRANSMITTER — FAULTED (TE FLAPS) · airframe 40,979 hrs · 25,350 cycles

FLAP DISAGREE; FLAP HANDLE AT 15; FLAP INDICATOR AT 10 ALTERNATE FLA[ EXTENSION TO FLAPS 15<[01] FOUND FAULT CODES ?TE FLAP SNSR R? AND ?TE FLAP SNSR L? ON FSEU BITE. REMOVED AND REPLACED LH AND RH FLAP POSITION TRANSMITTERS AND OPS CHECK GOOD PER AMM 27-58-01

Part: MODULE — FAULTY (ZN 200 FUS TOP) · airframe 39,128 hrs · 24,183 cycles

SMELL OF BURNING IN THE COCKPIT ASSOCIATED WITH COCKPIT DOOR LOCK SWITCHING ON AND OFF. DOOR LOCK/CHIME MODULE WAS HOT TO THE TOUCH. MOVE FLIGHT DECK ACCESS SWITCH TO OFF AND THE SMELL WENT AWAY AND DOOR LOCK SWITCHING STOPPED. ONE HOUR LATER THE SMELL RETURNED AND FLIGHT ATTENDANTS REPORTED. THE LIGHT ON THE COCKPIT AND PAD STARTED FLASHING. SMOKE WAS REPORTED COMING FROM THE LOCK AREA.<[01] R&R CHIME MODULE REF. AMM 52-51-06. OPS CHK GOOD.

Part: CONNECTOR — LOOSE (ZN 200 FUS TOP) · airframe 38,345 hrs · 23,699 cycles

L1 DOOR ENTRY UPPER EMERGENCY EXIT SIGN INOPERATIVE.<[01] TROUBLESHOT L1 DOOR UPPER EMERGENCY EXIT SIGN .FOUND CONNECTOR NOT SECURED (D10748).RESECURED CONNECTOR (D10748) IN REF WITH B737 AMM 33-51-06-960-806;33-51-00-710-801 AND WDM 33-51-12.PERFORMED EMERGENCY LIGHT OPERATIONAL TEST NORMAL.;[02] FINAL INSPECTION; VERIFIED STEP #1. RESECURED CONNECTOR.

Part: BATTERY PACK — INOPERATIVE (ZN 800 DOOR) · airframe 38,345 hrs · 23,699 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN INOPERATIVE.<[01] CHARGE BATTERY PACK M1675 IN REF WITH B737 AMM 33-51-06-610-802.PERFORMED EMERGENCY LIGHT OPERATIONAL TEST NORMAL IN REF WITH B737 AMM 33-51-00-710-801.;[02] FINAL INSPECTION; VERIFIED STEP #1. OPS CHECK NORMAL; EXIT SIGN OPERATIONAL.

Part: BATTERY PACK — INOPERATIVE (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

L-2 AND R-2 DOOR EXTERNAL EMERGENCY LIGHT INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1672 IN REF WITH B737 AMM 33-51-06-960-805.INSTALLATION TEST NORMAL.;[02] VERIFIED STEP 1

Part: GIRT BAR — OUT OF POSITION (ZN 800 DOOR) · airframe 38,345 hrs · 23,699 cycles

R2 DOOR SLIDE GIRT BAR FOUND RUBBING DURING DOOR CLOSING.<[01] R2 DOOR SLIDE GIRT BAR FOUND RUBBING DURING DOOR CLOSING. WILL BE ACCOMPLISHED. ON T/C MT-725-61-06 AS TTG8Q00N1N67;[02] VERIFIED STEP #1

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

ACCESS PANEL 193AL IS SHOWING A CRACK AT I/B SURFACE AREA<[01] REPAIRED ACCESS PANEL 193AL I/B SURFACE; PER REF B737 SRM 51-70-04-2R-1; MATERIAL USED PO.1791128 AND PO.1473815;[02] FINAL INSPECTION; VERIFIED STEP #1. CRACKED REPAIRED.

Part: ACCESS PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 38,345 hrs · 23,699 cycles

R/H FWD O/B ACCESS PANEL 193CR IS SHOWING A CRACK SEE DOT<[01] APPLIED PERMANENT REPAIR ON DAMAGED AREA AS MARKED AT PANEL #193CR AS PER B737 SRM 51-70-04-2R-1 AND 51-70-04-2R-0 PARAGRAPH 4-L-M-N ; MATERIAL USED PO#1791128 AND PO#1690463;[02] APPLIED PERMANENT REPAIR ON DAMAGED AREA AS MARKED AT PANEL #193CR AS PER B737 SRM 53-40-70-2R-1; SRM 51-70-04-2R-1 AND 51-70-04-2R-0 PARAGRAPH 4 (B-N); MATERIAL USED PO#1791128 AND PO#1690463;[03] VERIFIED STEP #1 AND 2

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

FWD CARGO COMPARTMENT THRESHOLD WEB CRACK.<[01] RECIEVED NEW FWD CARGO COMPT THRESHOLD WEB 143A8333-8<BR>FOR INSTALLATION REFER TO TASKCARD: TTG8Q002NMHC;[02] VERIFIED STEP #1

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 38,345 hrs · 23,699 cycles

RIGHT WING LOWER TRAILING EDGE PANEL 651EB SUPPORT ATTACH BRACKET CRACKED AT I/B FORWARD CORNER OF PANEL. (51-001)<[01] REMOVED AND REPLACED CRACKED SUPPORT ATTACH ANGLE AT RIGHT WING LOWER TRAILING EDGE PANEL 651EB AT I/B FORWARD CORNER AS PER SRM 51-40-02-0G-0 AND DWG #115A2001.;[02] VERIFIED STEP #1.

Part: DOOR — CORRODED (ZN 800 DOOR) · airframe 38,345 hrs · 23,699 cycles

**CORROSION** EXTERNAL (SECTION 46) LOWER FUSELAGE TOILET SERVICE DOOR; AFT CORNER LOWER FRAME CORROSION SPOT NOTED.<[01] ACCOMPLISHED ALL WORK PROCEDURES PER EA 23-152-02585;[02] ACCOMPLISHED ALL WORK PROCEDURES PER EA 23-152-02585

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

AFT CARGO COMPARTMENT; SCUFF PLATE FWD CORNER CRACK<[01] RECIEVED NEW AFT CARGO SCUFF PLATE FWD CORNER; <BR>PN:146A8341-7.<BR>FOR INSTALLATION REFERENCE TASKCARD: TTG8Q002NKR6;[02] RECIEVED WELDED AFT CARGO SCUFF PLATE FWD CORNER FROM <BR>JL WELDING TAGNO./PO<BR>:426441<BR>PN:146A8341-7.<BR>FOR INSTALLATION REFERENCE TASKCARD: TTG8Q002NKR6;[03] VERIFIED STEP #2

Part: ACCESS PANEL — BULGED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

AFT CENTER LOWER WHEEL WELL ACCESS PANEL # 193D HAS BULGING/CRACKED FASTENER HOLES<[01] FILLED FASTENERS HOLES WITH RESIN AND CHOPPED FIBERS FOR CONTINUATION OF REPAIR; CURED REPAIR AS PER B737 SRM 53-40-70-2R-1; SRM 51-70-042R-9 PARAG. 4(D-I); AND SRM 51-70-04-2R-0 PARAG. 4(E) AND FIGURE 214. EQUIPMENT USED HOT BONDER ID 160354 DUE DATE 02-16-24; VACUUM GAGE ID 173239 DUE DATE 02-23-24.;[02] APPLIED TOPCOAT ON AFT CENTER LOWER WHEEL ACCESS PANEL #193D REF B 737 AMM 51-21-73-370-803;[03] FINAL INSPECTION; VERIFIED STEP #1. FASTENER HOLES REPAIRED.

Part: ACCESS PANEL — BULGED (ZONE 100) · airframe 38,345 hrs · 23,699 cycles

L/H LOWER AFT ACCESS PANEL # 194DL HAS BULGING/CRACKED FASTENER HOLES<[01] FILLED FASTENER HOLES WITH RESIN AND CHOPPED FIBERS FOR CONTINUATION OF REPAIR; CURED REPAIR AS PER B737 SRM 53-60-70-2R-1; SRM 51-70-04-2R-9 PARAG 4-(D-I) AND SRM 51-70-04-2R-0 4(E) AND FIGURE 214.

Part: PANEL — BULGED (ZN 600 RIGHT WIN) · airframe 38,345 hrs · 23,699 cycles

R/H FWD O/B ACCESSPANEL # 193CR HAS BULGING/CRACKED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGED AREA FASTENER HOLES AS MARKED AT PANEL 193CR AS PER B737 SRM 51-70-04-2R-9 AND 51-70-04-2R-0 PARAGRAPH 4-L-M-N ; MATERIAL USED PO#1791128 ANA PO#1690463.;[02] VERIFIED STEP 1

Part: ACCESS PANEL — BULGED (ZN 500 LEFT WING) · airframe 38,345 hrs · 23,699 cycles

L/H WING LOWER MID T/E ACCESS PANEL # 561CB HAS BULGING/CRACKED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGED AREA FASTENER HOLES AS MARKED AT PANEL #561CB AS PER B737 SRM 51-70-04-2R-9 AND 51-70-04-2R-0 PARAGRAPH 4-L-M-N ; MATERIAL USED PO#1791128 ANA PO#1690463.;[02] PAINTED L/H WING LOWER MID T/E ACCESS PANEL #561CB REF B737 AMM 51-21-73-370-803.;[03] APPLIED PERMANENT REPAIR ON DAMAGED AREA FASTENER HOLES AS MARKED AT PANEL #561CB AS PER B737 SRM 57-51-01-2R-1; SRM 51-70-04-2R-9 AND 51-70-04-2R-0 PARAGRAPH 4-L-M-N ; MATERIAL USED PO#1791128 ANA PO#1690463.;[04] VERIFIED

Part: SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

FWD CABIN WET AREA FUS FRAME SUPPORT SMALL CRACKED @ FLANGE CUTOUT S-7L STA 312 ABOVE L-1 DOOR CUTOUT UPPER FWD MKD DOT<[01] ACCOMPLISHED PERMANENT REPAIR AT STA 312 UPPER CHORD PER ATTACHED EA # M-22-153-01244.;[02] VERIFIED; STEP # 1

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

PASSENGER CABIN FLOOR ACCESS PANEL #241ADF; UPPER SURFACE DELAMINATED DOT 223-AW241ADF.<[01] RECEIVED NEW FLOOR PANEL# 241ADF. PANEL WILL BE INSTALL ON FAULT# TTG8Q00M6ZAL.;[02] FINAL INSPECTION. RECEIVED NEW FLOOR PANEL# 241ADF. PANEL WILL BE INSTALL ON FAULT# TTG8Q00M6ZAL.

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

PASSENGER CABIN FLOOR ACCESS PANEL #241ACF; UPPER SURFACE DELAMINATED DOT 223-AW241ACF.<[01] RECEIVED PANEL 241ACF FABRICATED BY OUTSIDE VENDOR AND ATTACHED CERTS IN MAINTENIX. FINAL INSTALLATION OF FLOOR PANEL 241ACF WILL BE COMPLETED ON ROUTINE CARD TTG8Q00M6ZAN.;[02] VERIFIED STEP #1

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

PASSENGER CABIN FLOOR ACCESS PANEL #242RF; UPPER SURFACE DELAMINATED DOT 223-AW242RF.<[01] RECEIVED NEW FLOOR PANEL# 242RF. THIS PANEL WILL BE INSTALL ON FAULT# TTG8Q00M6ZT2.;[02] FINAL INSPECTION. RECEIVED NEW FLOOR PANEL# 242RF. THIS PANEL WILL BE INSTALL ON FAULT# TTG8Q00M6ZT2.

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

PASSENGER CABIN FLOOR PANEL #242WF; UPPER SURFACE DELAMINATED DOT 223-AW242WF.<[01] RECEIVED PANEL 242WF FABRICATED BY OUTSIDE VENDOR AND ATTACHED CERTS IN MAINTENIX. FINAL INSTALLATION OF FLOOR PANEL 242WF WILL BE COMPLETED ON ROUTINE CARD TTG8Q00M6ZSS.;[02] VERIFIED STEP #1

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

PASSENGER CABIN FLOOR ACCESS PANEL #242UF; UPPER SURFACE DELAMINATED UPPER SURFACE DELAMINATED DOT 223-AW242UF.<[01] RECEIVED PANEL 242UF FABRICATED BY OUTSIDE VENDOR AND ATTACHED CERTS IN MAINTENIX. FINAL INSTALLATION OF FLOOR PANEL 242UF WILL BE COMPLETED ON ROUTINE CARD TTG8Q00M6ZSW.;[02] VERIFIED STEP #1

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

FWD CARGO COMPARTMENT RIGHT SIDE; GUSSET HAS CRACK INTERNAL AREA; AT STRINGER 19R STA 500D.<[01] REMOVED AND REPLACED GUSSET AT RIGHT SIDE FWD CARGO COMP STRINGER 19R STA 500D PER REF SRM 51-40-02-0G 0;[02] REMOVED AND REPLACED GUSSET AT RIGHT SIDE FWD CARGO COMP STRINGER 19R STA 500D PER REF SRM 51-40-02 -0G-0 AND DWG 143A9481;[03] CORRECTING STEP # 2 DWG # 143A7902;[04] VERIFIED STEPS COMPLETE.

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

PASSENGER CABIN FLOOR PANEL #231ZF; UPPER SURFACE DELAMINATED DOT 223-CP231ZF.<[01] RECEIVED NEW PANEL 231ZF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZD4;[02] VERIFIED STEP 1. COMPLETE

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

PASSENGER CABIN FLOOR PANEL #232SF; UPPER SURFACE DELAMINATED DOT 223-CP232SF.<[01] RECEIVED MAIN CABIN FLOOR PANEL 232SF (P/N 144A5810-161); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZCA.;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 232SF (P/N 144A5810-161); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZCA.

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

PASSENGER CABIN FLOOR ACCESS PANEL #241AEF; UPPER SURFACE DELAMINATED DOT 223-AW241AEF.<[01] RECEIVED PANEL 241AEF FABRICATED BY OUTSIDE VENDOR AND ATTACHED CERTS IN MAINTENIX. FINAL INSTALLATION OF FLOOR PANEL 241AEF WILL BE COMPLETED ON ROUTINE CARD TTG8Q00M6ZAJ.;[02] VERIFIED STEP #1

Part: ACCESS PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

PASSENGER CABIN FLOOR ACCESS PANEL #241DF; UPPER SURFACE DELAMINATED DOT 223-CP241DF.<[01] RECEIVED NEW PANEL 241DF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZAA;[02] VERIFIED STEP 1. COMPLETE

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

CRACK AT UPPER VAPOR BARRIER ATTACH ANGLE STA 663 LBL 8 SEEN THRU AC BAY. 8-30<[01] REMOVED AND INSTALLED NEW FABRICATED REPAIR PARTS AT UPPER VAPOR BARRIER ATTACH ANGLE AT STA 663; LBL 8 AS PER B737-700 SRM 51-40-02-0G-0; SRM 57-10-10-2R-5.;[02] (RII) FINAL INSPECTION; VERIFIED STEP #1. NEW FABRICATED PARTS INSTALLED.

Part: CHANNEL — CRACKED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

MAIN CABIN CENTER AISLE FLOOR SUPPORT BREAK CRACKED @ LBL- 1 STA 540 MKD DOT<[01] REMOVED AND INSTALLED NEW FLOOR SUPPORT BREAK ASSY CHANNEL AT STA 540 FROM LBL 1 TO LBL 21 AS PER B737-700 SRM 51-40-02-0G-0; DWG# 143A0060.;[02] VERIFIED STEP 1 FINAL

Part: FLOOR PANEL — CORRODED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

FWD CABIN WET AREA FLOOR PANEL NO-221BF UPPER SURFACE SKIN BULGING ;DELAMINATED AREAS MKD DOT<[01] RECEIVED NEW PANEL 221BF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZUS;[02] FINAL INSPECTION; RECEIVED NEW PANEL 221BF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZUS.

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

FWD CABIN WET AREA FLOOR PANEL NO- 221EF UPPER SKIN SURFACE DELAMINATED MKD DOT<[01] RECEIVED MAIN CABIN FLOOR PANEL 221EF (P/N 141A5810-249); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZUJ.;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 221EF (P/N 141A5810-249); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZUJ.

Part: CHANNEL — CRACKED (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

MAIN CABIN CENTER AISLE FLOOR SUPPORT BREAK CRACKED @ RBL- 1 STA 540 MKD DOT<[01] REMOVED AND INSTALLED NEW FLOOR SUPPORT BREAK PANEL (CHANNEL) AT MAIN CABIN CENTER AISLE STA 540; FROM RBL 1 TO RBL 21 AS PER B737-700 SRM 51-40-02-0G-0; DWG# 143A0060.;[02] VERIFIED STEP 1 FINAL

Part: FLOOR PANEL — PEELING (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

CABIN FLOOR PANEL UPPER SURFACE PEELING 231GF. 8-64<[01] RECEIVED NEW FLOOR PANEL 231GF ; THIS PANEL WILL BE INSTALL ON FAULT # &NBSP;&NBSP;&NBSP;&NBSP;&NBSP;TTG8Q00M6ZTU;[02] FINAL INSPECTION; RECEIVED NEW FLOOR PANEL 231GF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZTU

Part: FLOOR PANEL — PEELING (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

CABIN FLOOR PANEL UPPER SURFACE PEELING RF. 8-66 PANEL FLOOR 241RF<[01] RECEIVED NEW PANEL 241RF ; THIS PANEL WILL BE INSTALL ON FAULT #TTG8Q00M6Z9S;[02] VERIFIED STEP 1. COMPLETE

Part: FLOOR PANEL — PEELING (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

CABIN FLOOR PANEL UPPER SURFACE PEELING 231XF. 8-62<[01] RECEIVED NEW FLOOR PANEL PANEL 231XF ; THIS FLOOR WILL BE INSTALL ON FAULT #TTG8Q00M6ZE0;[02] FINAL INSPECTION; RECEIVED NEW FLOOR PANEL PANEL 231XF ; THIS FLOOR WILL BE INSTALL ON FAULT #TTG8Q00M6ZE0.

Part: FLOOR PANEL — PEELING (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

CABIN FLOOR PANEL UPPER SURFACE PEELING 231KF. 8-63<[01] RECEIVED MAIN CABIN FLOOR PANEL 231KF (P/N 143A5810-580); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZTN;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 231KF (P/N 143A5810-580); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZTN.

Part: FLOOR PANEL — PEELING (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

CABIN FLOOR PANEL UPPER SURFACE PEELING 231DF. 8-65<[01] RECEIVED MAIN CABIN FLOOR PANEL 231DF (P/N 143A5810-513); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZU0.;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 231DF (P/N 143A5810-513); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZU0.

Part: FLOOR PANEL — PEELING (ZN 100 FUS LOWER) · airframe 38,345 hrs · 23,699 cycles

CABIN FLOOR PANEL UPPER SURFACE PEELING 241UF. 8-67<[01] RECEIVED MAIN CABIN FLOOR PANEL 241UF (P/N 146A5810-470); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6YE6.;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 241UF (P/N 146A5810-470); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6YE6.

Part: PANEL — CRACKED (ZN 500 LEFT WING) · airframe 38,345 hrs · 23,699 cycles

LEFT WING LOWER MID SPAN T/E PANEL #561BB; INNER/LOWER SURFACE CRACK/DELAMINATED DOT 223-LW561BB.<[01] APPLIED PERMANENT REPAIR ON DAMAGED AREA AT LEFT WING LOWER MID SPAN T/E PANEL #561BB AS PER B737 SRM 57-51-01-2R-1; SRM 51-70-05-2R-4 PARAG 4.E AND SRM 51-70-05-2R-0 PARAG 4.M.3. MATERIAL USED P/0#2033057; P/O#1798840 AND EQUIMENT USED HOT BONDER ID 160354 DUE DATE 02-16-24; VACUUM GAGE ID 173239 DUE DATE 02-23-24. APPLIED TOPCOAT ON LEFT WING LOWER MID SPAN T/E PANEL # 561BB INNER /LOWER SURFACE REF B 737 AMM 51-21-73-370-803

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 38,233 hrs · 23,630 cycles

EMERGENCY LIGHT FWD OF RH AFT CARGO INOP.<[01] RELAMPED AFT R/H SLIDE LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.

Part: FLOORBOARD — CRACKED (ZN 100 FUS LOWER) · airframe 38,116 hrs · 23,553 cycles

AFT CARGO FLOOR BOARD 140BF HAS CRACK 15 INCHES LONG; ALONG CENTER FLOOR FRAME.<[01] REMOVED AND REPLACED AFT CARGO FLOOR BOARD 140BF PER AMM 25-52-10

Part: INDICATOR — FAULTY (ZN 200 FUS TOP) · airframe 38,009 hrs · 23,478 cycles

DUE TO AHM DATA. AIRCRAFT LOGGING L/R FLAP POSITION MARGIN FAULTS. PLEASE T/S USING THE FMS MCDU AND WATCH THE MARGIN NUMBER AS YOU MOVE THE FLAPS. YOU SHOULD NOT SEE THE MARGIN NUMBER DROP BELOW 6. REMOVE INDICATOR AND IF PROBLEM GOES AWAY REPLACE THE INDICATOR. IF NOT, YOU WILL HAVE TO DIG INTO WHICH FLAP POSITION TRANSMITTER IS CAUSING PROBLEM AMM 27-58-01-820-899 TO ADJ THE TRANSMITTER. CODE PARTS TAG AHM OR FAILURE NOT SCHDULED. DLA<T/S PER MX CTL REQUEST - REMOVED AND REPLACED FLAP POS. INDICATOR REF. AMM. 27-58-02. ALL INDICATIONS NML.

Part: SLIDE — LOOSE (ZN 200 FUS TOP) · airframe 37,802 hrs · 23,358 cycles

J HOOK FOR FWD ENTRY DOOR SLIDE LOOSE.<[01] TIGHTENED J HOOK FOR L1 DOOR BY USING HAND PRESSURE TO CLOSE J HOOK PER SIP

Part: WHEEL — BLOWN (ZN 700 LANDING G) · airframe 37,150 hrs · 22,922 cycles

BLOWN #2 TIRE ON TAKEOFF ACCOMPLISHED AN OVERWEIGHT LANDING AT 132.1 K<[01] R/R #1 & #2 MLG WHEEL ASSY REF AMM 32-45-11.

Part: MEGAPHONE — INOPERATIVE (ZN 900 LAV/GALLE) · airframe 36,232 hrs · 22,315 cycles

FA AFT MEGAPHONE DOES NOT WORK / [01] REPLACED MEGAPHONE PER AMM 25-64-00. OPS CHECK GOOD.

Part: SEAL PLATE — CRACKED (L/H HORIZ. STAB.) · airframe 35,547 hrs · 21,846 cycles

-LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / [01] R&R LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL REF AMM 53-31-31.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 35,547 hrs · 21,846 cycles

AFT GALLEY SERVICE DOOR LINER LOWER SUPPORT BRACKETS CRACKED. / [01] R&R AFT GALLEY SERVICE DOOR LINER LOWER SUPPORT BRACKET PER AMM 52-41-31

Part: SLIDING SLEEVE — CRACKED (R/H HORIZ. STAB.) · airframe 35,547 hrs · 21,846 cycles

-RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / [01] REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER MM 53-31-31

Part: SLIDE — LOW PRESSURE (AFT) · airframe 34,729 hrs · 21,274 cycles

AFT ENTRY DOOR SLIDE NEEDLE IN RED (LOW) / [01] REPLACED AFT ENTRY SLIDE PER MT725-61-06

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 34,618 hrs · 21,203 cycles

AFT ENTRY DOOR SLIDE NEEDS TO BE ADJUSTED IN THE SLIDE BUSTLE SO THAT GREEN BAND OF PRESSURE GAUGE IS VISIBLE / [01] READJUSTED AFT ENTRY DOOR SLIDE REF M/M 25-66-01;[02] C/W

Part: NONE — LOOSE (CABIN FLOOR) · airframe 33,424 hrs · 20,451 cycles

SUPPLEMENTAL INFORMATION: PHOTO ILLUM STRIP NEAR ROW 9 LOOSE ; / [01] SECURED PHOTO ILLUMINATION STRIP @ ROW 9 PER SIP.

Part: MEGAPHONE — BROKEN (CABIN) · airframe 33,414 hrs · 20,444 cycles

FORWARD MEGAPHONE IS BROKEN ; / [01] REMOVED AND REPLACED FORWARD MEGAPHONE IN REFERENCE TO AMM 25-64-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,714 hrs · 19,999 cycles

M1675 EMERGENCY LIGHT BATTERY PACK INOP. ; / [01] SWAPPED KNOWN GOOD BATTERY PACK INTO CHARGER ASSEMBLY M1675 TO CONFIRM BATTERY PACK INOP PER AMM 33-51-06-960-805. KNOWN GOOD UNIT TURNS LIGHTS ON AS INTENDED; M1675 REQUIRES REPLACEMENT. RESTORED BATTERY PACKS TO ORIGINAL LOCATIONS PER AMM 33-51-06-960-805.; [02] REMOVED; REPLACED AND PERFORMED GOOD OPERATIONAL CHECK OF M1675 EMERGENCY EXIT LIGHTS BATTERY PACK PER AMM 33-51-06-960-805; [03] VERIFIED CORRECTIVE ACTION ENTRY 1 & 2. CARD COMPLETE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,714 hrs · 19,999 cycles

L/H OVERWING EMERGENCY EXIT DOOR EXIT LOCATOR SIGN HAS 1EA BULBS INOP. ; / [01] REMOVED; REPLACED AND PERFORMED GOOD OPERATIONAL CHECK OF L/H OVERWING EMERGENCY EXIT DOOR LOCATOR SIGN LIGHT LAMP PER AMM 33-51-01-960-801; [02] VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE.

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 32,714 hrs · 19,999 cycles

R/H GUSSET FOUND TO BE CRACKED AT BS500D STR19R WL190 / [01] REMOVED GUSSET AT BS 500D STR 19R WL 190. IAW. SRM 51-40-02; [02] EVALUATED DAMAGE ON GUSSET LOCATED AT B/S 500D STR 19R WL 190 AND NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM MUST BE REPLACED IAW SRM 51 -10-02 PARAGRAPH 9; [03] LOCATED AND DRILLED NEW GUSSET AT B/S 500D STR 19R WL 190 P/N 143A9483-5 LOT# 1461912-2 IAW SRM 51-40-05 AND DWG 143A7902 REV:B; [04] OK TO INSTALL; [05] VERIFIED ITEMS 2 AND 3 CORRECTIVE ACTIONS. OK TO INSTALL.; [06] INSTALLED NEW GUSSET AT B/S 500D STR 19R WL 190 P/N 143A9483-5 IAW SRM 51-40-02 AND DWG 143A7902 REV:B; [07] VERIFIED ITEM 6 CORRECTIVE ACTIONS.; [08] VERIFIED ALL ITEMS COMPLETE.

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 32,714 hrs · 19,999 cycles

L/H GUSSET FOUND TO BE CRACKED AT BS500D STR19L WL190 / [01] REMOVED GUSSET AT BS 500D STR 19L WL 190. IAW. SRM 51-40-02; [02] EVALUATED DAMAGE ON GUSSET LOCATED AT B/S 500D STR 19L WL 190 AND NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM MUST BE REPLACED IAW SRM 51 -10-02 PARAGRAPH 9; [03] LOCATED AND DRILLED NEW GUSSET AT B/S 500D STR 19L WL 190 P/N 143A9483-6 LOT# 1460592-1 IAW SRM 51-40-05 AND DWG 143A7902 REV:B; [04] OK TO INSTALL; [05] VERIFIED ITEMS 2 AND 3 CORRECTIVE ACTIONS. OK TO INSTALL.; [06] INSTALLED NEW GUSSET AT B/S 500D STR 19L WL 190 P/N 143A9483-6 IAW SRM 51-40-02 AND DWG 143A7902 REV:B; [07] VERIFIED ITEM 6 CORRECTIVE ACTIONS.; [08] VERIFIED ALL ITEMS COMPLETE.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

AFT CARGO BAY FLOOR STRAP CORODDED BS 772 RBL 21- LBL 21 WL 156 ; / [01] REMOVED AFT CARGO BAY FLOOR STRAP BS772 RBL21-LBL21 IAW SRM 51-40-02-0G-0; [02] THERE IS NO ALLOWABLE DAMAGE FOR AFT CARGO BAY FLOOR STRAP. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0; [03] RECEIVED NEW STRAP<BR>ITEM 146A9401-4<BR>PO# 829373/1; [04] LOCATED; AND DRILLED NEW STRAP IAW SRM 51-40-05-0G-0 AND DWG 146A9401 REV:C; [05] VERIFIED CORRECTIVE ACTION #4.; [06] OK TO INSTALL; [07] OK TO INSTALL; [08] OK TO INSTALL GIVEN; [09] INSTALLED ACB FLOOR STRAP BS 772 RBL 21 - LBL 21 WL 156 IAW SRM 51-40-02 AND DWG 146A7500 ID: 0157 REV:- 146A9401 ID: 2 REV: C; [10] INSTALLED ACB FLOOR STRAP BS 772 RBL 21 - LBL 21 WL 156 IAW SRM 51-40-02; [11] VERIFIED INSTALLATION OF THE FLOOR STRAP AT BS 772 LBL21-RBL21 PER SRM 51-40-02; DWG 146A7500 ID: 0157 REV:- AND 146A9401 ID: 2 REV:C; [12] WORK SCOPE COMPLETE

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS747+16; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+16'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+16'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: WEB — CORRODED (AFT CARGO THRSHL) · airframe 32,714 hrs · 19,999 cycles

ACB DOOR SURROUND; SUB THRESHOLD WEB CORROSION. BS827+1; RBL27; WL153 ; / [01] REMOVED CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB AT BS 827+1' RBL 27 WL 153 <BR>MEASURED L 1' X W 1' AND 0.003' DEEP. ORIGINAL THICKNESS .050'; REMAINING THICKNESS .047' <BR>FOUND TO BE IN LIMITS IAW SRM 53-60-15-1A-1 ALLOWABLE DAMAGE 1 - AFT CARGO DOOR SURROUND STRUCTURE <BR>TO BE REPAIRED BY REPLACEMENT DUE TO SURROUNDING CORROSION DAMAGE; ON CUSTOMER CARD TTG8Q006A439 <BR><BR>DEPTH GAUGE ATS 2473 S/N UNKNOWN 07/2022; [02] VERIFIED REMOVED CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB AT BS 827+1' RBL 27 WL 153 <BR>MEASURED L 1' X W 1' AND 0.003' DEEP. ORIGINAL THICKNESS .050'; REMAINING THICKNESS .047' <BR>FOUND TO BE IN LIMITS IAW SRM 53-60-15-1A-1 ALLOWABLE DAMAGE 1 - AFT CARGO DOOR SURROUND STRUCTURE <BR>TO BE REPAIRED BY REPLACEMENT DUE TO SURROUNDING CORROSION DAMAGE; ON CUSTOMER CARD TTG8Q006A439.

Part: SUPPORT — CORRODED (BS 737) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS767+13.2; LBL21.6; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767+ LBL22 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIEDREMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767+ LBL22 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FWD SHIELD CORROSIN. BS767+3.5; RBL21; WL151. ; / [01] REMOVED CORROSION ON ACB FWD SHIELD BS767+3.5 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS; [02] VERIFIED REMOVED CORROSION ON ACB FWD SHIELD BS767+3.5 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FWD SHIELD CORROSION. BS767+19.5; RBL22; WL151 ; / [01] NO ALLOWABLE DAMAGE FOUNDED ON SRM; REPLACE PART FOR REPAIR; THE REPAIR WILL BE DONE UNDER CUSTOMER FAULT TTG8Q006A1HS; [02] REMOVED CORROSION ON ACB FWD SHIELD BS767+19.5 RBL21 WL151; L=.500 W=.500 D=.003;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS; [03] VERIFIED REMOVED CORROSION ON ACB FWD SHIELD BS767+19.5 RBL21 WL151; L=.500 W=.500 D=.003;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727C+18.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727D+18.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>CARD TO BE COMPLETED ON:<BR>TTG8Q006A199; [02] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727C+18.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [03] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727C+18.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D+10.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727D+10.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS. <BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>CARD TO BE COMPLETED ON:<BR>FUSE 5127<BR>CUST ID: <BR>TTG8Q006A199; [02] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727D+10.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>CARD TO BE COMPLETED ON:<BR>FUSE 5127<BR>CUST ID: <BR>TTG8Q006A199; [03] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727D+10.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [04] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727D+10.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727C+14; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727C+14 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>CARD TO BE COMPLETED ON:<BR>TTG8Q006A199; [02] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727C+14 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [03] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727C+14 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727D LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>CARD TO BE COMPLETED ON:<BR>TTG8Q006A199; [02] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727D LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [03] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727D LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727C+14; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727C+14 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>CARD TO BE COMPLETED ON<BR>TTG8Q006A199; [02] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727C+14 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [03] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727C+14 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+18.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727E+18.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727E+18.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (BS 767) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS767; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SHIELD — CORRODED (BS 737) · airframe 32,714 hrs · 19,999 cycles

ACB FWD SHIELD CORROSION. BS767+1.75; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FWD SHIELD BS767+1.75 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS; [02] VERIFIED REMOVED CORROSION ON ACB FWD SHIELD BS767+1.75 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS

Part: SHIELD — CORRODED (BS 767) · airframe 32,714 hrs · 19,999 cycles

ACB FWD SHIELD CORROSION. BS767+12.5; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FWD SHIELD BS767+12.5 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS; [02] VERIFIED REMOVED CORROSION ON ACB FWD SHIELD BS767+12.5 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS

Part: SUPPORT — CORRODED (BS 500B-500D) · airframe 32,714 hrs · 19,999 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT B.S. 500B-500D; L.B.L. 24; W.L. 154. ; / REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT B.S. 500B-500D; L.B.L. 24; W.L. 154 IAW SRM 51-10-02-0G-0. CORRODED AREA MEASURES 40'L X 4'W. REMOVED .006' OF MATERIAL. ORIGINAL THICKNESS = .045'CORROSION DAMAGE FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2. REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0] REMOVED FCB L/H FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02; [06] FABRICATED NEW FLOOR TO SIDEWALL SUPPORT AT B.S. 400-500D; L.B.L. 24; W.L. 154 FROM BAC1496-444; LOT#1466509-1 IAW SRM 51-40-05; SRM 53-00-53-2R-5 4. A-H; BOEING DWG 143A7501; AND BOEING DWG 143A7500. OK TO TREAT AND PRIME; [07] FABRICATED NEW FLOOR TO SIDEWALL SUPPORT AND REPAIR SPLICE AT B.S. 400-500D; L.B.L. 24; W.L. 154 FROM BAC1496-444; LOT#1466509-1 IAW SRM 51-40-05; SRM 53-00-53-2R-5 4. A-H; BOEING DWG 143A7501; AND BOEING DWG 143A7500. OK TO TREAT AND PRIME; [08] VERIFIED FABRICATION OF SUPPORT AND SPLICE REPAIR PARTS PER SRM 51-40-05; SRM 53-00-53-2R-5 AND DWG 143A7501 AND DWG 143A7500 INSTALLED SIDEWALL SUPPORT AT BS 396 TO 500D LBL 24 WL 154. IAW DWG:143A7500 AND SRM 51-40-02 INSTALLED SIDEWALL SUPPORT AT BS 396 TO 500D LBL 24 WL 154. IAW DWG:143A7500 AND SRM 51-40-02

Part: SUPPORT — CORRODED (BS 727B) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727B+14.5; RBL20; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727B+14.5'; RBL20; WL151; WORK AREA 1.0' X 1.0' X 0.024' REMAINING THICKNESS IS 0.016. FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID:ATS 2472 S/N UNKNOWN DUE:06/2022. REPAIRED BY REPLACEMENT ON JOB CARD TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727B+14.5'; RBL20; WL151; WORK AREA 1.0' X 1.0' X 0.024' REMAINING THICKNESS IS 0.016. FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID:ATS 2472 S/N UNKNOWN DUE:06/2022. REPAIRED BY REPLACEMENT ON JOB CARD TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727B) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727B+2.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727B+2.5'; RBL22; WL151; WORK AREA 1.0' X 1.0' X 0.006' REMAINING THICKNESS IS 0.034. FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID:ATS 2472 S/N UNKNOWN DUE:06/2022. REPAIRED BY REPLACEMENT ON JOB CARD TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727B+2.5'; RBL22; WL151; WORK AREA 1.0' X 1.0' X 0.006' REMAINING THICKNESS IS 0.034. FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID:ATS 2472 S/N UNKNOWN DUE:06/2022. REPAIRED BY REPLACEMENT ON JOB CARD TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727B) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727B+10.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727B+10.5'; RBL22; WL151; WORK AREA 1.0' X 1.0' X 0.007' REMAINING THICKNESS IS 0.033. FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID:ATS 2472 S/N UNKNOWN DUE:06/2022. REPAIRED BY REPLACEMENT ON JOB CARD TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727B+10.5'; RBL22; WL151; WORK AREA 1.0' X 1.0' X 0.007' REMAINING THICKNESS IS 0.033. FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID:ATS 2472 S/N UNKNOWN DUE:06/2022. REPAIRED BY REPLACEMENT ON JOB CARD TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727D) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727D+15.5; RBL19; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+15.5'; RBL 19; WL 151 ; WORK AREA 1.0'X 1.0' X 0.006' ; REMAINING THICKNESS IS 0.034; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+15.5'; RBL 19; WL 151 ; WORK AREA 1.0'X 1.0' X 0.006' ; REMAINING THICKNESS IS 0.034; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727D) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D+16; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+16'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.022' ; REMAINING THICKNESS IS 0.018 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+16'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.022' ; REMAINING THICKNESS IS 0.018 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+10.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+10.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.035' ; REMAINING THICKNESS IS 0.005 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+10.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.035' ; REMAINING THICKNESS IS 0.005 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+2.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+2.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.007' ; REMAINING THICKNESS IS 0.033; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+2.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.007' ; REMAINING THICKNESS IS 0.033; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [03] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+2.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.007' ; REMAINING THICKNESS IS 0.033; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727E+15.5; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+15.5'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.007' ; REMAINING THICKNESS IS 0.033 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+15.5'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.007' ; REMAINING THICKNESS IS 0.033 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727E+14.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+14.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.007' ; REMAINING THICKNESS IS 0.033 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+14.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.007' ; REMAINING THICKNESS IS 0.033 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+18.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.014' ; REMAINING THICKNESS IS 0.026 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.014' ; REMAINING THICKNESS IS 0.026 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727E+2.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+2.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.009' ; REMAINING THICKNESS IS 0.031; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+2.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.009' ; REMAINING THICKNESS IS 0.031; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+19; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+19'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.014' ; REMAINING THICKNESS IS 0.026 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+19'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.014' ; REMAINING THICKNESS IS 0.026 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+6.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+6.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.023' ; REMAINING THICKNESS IS 0.017 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022; [02] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+6.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.023' ; REMAINING THICKNESS IS 0.017 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [03] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+6.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.023' ; REMAINING THICKNESS IS 0.017 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [04] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+6.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.023' ; REMAINING THICKNESS IS 0.017 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+2; RBL21; WL151 ; / [01] FAULT RESOLVED ON OTHER CUSTOMER CARD NBR:TTG8Q006A3FD; [02] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+2'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [03] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+2'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727E+19; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+19'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.008' ; REMAINING THICKNESS IS 0.032 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+19'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.008' ; REMAINING THICKNESS IS 0.032 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747; RBL19; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747; RBL 19; WL 151 ; WORK AREA 1.0'X 1.0' X 0.017' ; REMAINING THICKNESS IS 0.023 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747; RBL 19; WL 151 ; WORK AREA 1.0'X 1.0' X 0.017' ; REMAINING THICKNESS IS 0.023 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.017' ; REMAINING THICKNESS IS 0.023 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.017' ; REMAINING THICKNESS IS 0.023 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727E+18.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.008' ; REMAINING THICKNESS IS 0.032 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.008' ; REMAINING THICKNESS IS 0.032 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS747+2; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+2'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.006' ; REMAINING THICKNESS IS 0.034 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+2'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.006' ; REMAINING THICKNESS IS 0.034 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+8.5; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+8.5'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.025' ; REMAINING THICKNESS IS 0.015 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+8.5'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.025' ; REMAINING THICKNESS IS 0.015 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+6.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+6.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+6.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+10.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+10.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.013' ; REMAINING THICKNESS IS 0.027 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+10.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.013' ; REMAINING THICKNESS IS 0.027 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+18.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+19; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+19'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+19'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+6.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 747+6.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 747+6.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: CARGO TRACK — CORRODED (BS 767) · airframe 32,714 hrs · 19,999 cycles

ACB RAIL UPPER SURFACE CORROSION BS767+4.5 TO BS767+6.5; RBL3; WL151 ; / REMOVED CORROSION ON AFT CARGO BAY R/H ACB RAIL UPPER SURFACE BS767+4.5 TO BS767+6.5 IN L: 2.150IN W: 0.900IN D: 0.012; FROM ORIGINAL THICKNESS OF 0.075IN. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2<BR>TOOLING ID: ATS1671 S/N 65093024 DATE: 04/2021 DUE: 01/2022 <BR>TOOLING ID: ATS1317; S/N: UNKNOWN; DATE: 06/2021 DUE: 06/2022 REMOVED CORROSION DAMAGE ON UPPER FLANGE IAW SRM 53-00-53-2R-2] HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. CAL ID IS000450 S/N N500D000M120071 LOCATED AND DRILLED REPAIR PARTS IAW SRM 53-00-53-2R-2 AND SRM 51-40-05.; [14] ADD TO ITEM 13. REPAIR SPLICE MARERIAL I.D.: BAC1510-1355 7050 T76511 LOT#1447574-1. REF: CUSTOMER RO # 816177-SWA. ITEM HFAB53-CS-017; [15] VERIFIED CORRECTIVE ACTION 13 AND 14 PER SRM 53-00-53-2R-2 ALTERNATIVE 5 AND SRM 51-40-05. REFERENCE CUSTOMER RO # 816177-SWA. ITEM HFAB53-CS-017; [16] APPLIED CHEMICAL CONVERSION COATING AND PRIMER AT RAIL AND REPAIR PART IAW SRM 53-00-53-2R-2 REPAIR 2 STEP 4(N)(O) INSTALLED REPAIR AT ACB RAIL BS 767 TO BS 767+10' RBL 3. WL15; IAW SRM 53-00-53-2R-2 REPAIR 2 AND SRM 51-4-02

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+18.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 747+18.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 747+18.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (BS 767) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS767; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 767; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 767; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 767) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS767+14.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767 + 14.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767 + 14.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (BS 767) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS767+14.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767+14.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767+14.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (BS 767) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS767+5.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767 + 5.5' LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767 + 5.5' LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (BS 767) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS767+18.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767 +18.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767 +18.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (BS 787) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS787+10.25; LBL22; WL153 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 787 + 10.25 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 787 + 10.25 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: STRAP — CORRODED (BS 807) · airframe 32,714 hrs · 19,999 cycles

ACB DOOR SURROUND STRUCTURE STRAP CORROSION BS807+2; RBL19.25; WL154. ; / [01] REMOVED AND EVALUATED CORROSION AT BS807+2 RBL19 WL154. DAMAGE MEASURES 1.3LX1.1WX0.025D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1. PART TO BE REPAIRED BY REPLACEMENT.; [02] CERTIFIED ACTION 1; [03] VERIFIED REMOVED AND EVALUATED CORROSION AT BS807+2 RBL19 WL154. DAMAGE MEASURES 1.3LX1.1WX0.025D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1. PART TO BE REPAIRED BY REPLACEMENT.; [04] UPDATED PART#; [05] CALIBRATION TOOL DEPTH GAUGE<BR><BR>ID : ATS2472<BR>S/N : UNKNOWN<BR>DUE : 06/2022; [06] LOCATED AND DRILLED NEW ACB DOOR SURROUND STRUCTURE STRAP BS 807 ;RBL 19.25; WL 154 IAW SRM 51-40-05-0G-0 AND DWG 146A8120; [07] VERIFIED LOCATED AND DRILLED PER SRM 51-40-05 AND DWG 146A8120; [08] OK TO INSTALL NEW STRAP ACB DOOR SURROUND STRUCTURE STRAP BS 807 ;RBL 19.25; WL 154; [09] VERIFIED OK TO INSTALL ACB DOOR SURROUND STRUCTURE STRAP.; [10] INSTALLED NEW STRAP ACB DOOR SURROUND STRUCTURE STRAP BS 807 ;RBL 19.25; WL 154 IAW. DWG : 146A8120 AND SRM: 51-40-02; [11] UPDATED DWG REVISION USED ON ITEM 10- REV: A.; [12] VERIFIED CORRECTIVE ACTION #10 & 11.; [13] UPDATED MEASUREMENTS PARAMETERS- REPAIR TYPE N/A PART REPLACED.; [14] JOB COMPLETE

Part: NUT PLATE — CORRODED (BS 787) · airframe 32,714 hrs · 19,999 cycles

NUT PLATE STRIP HAS CORROSION. COMMON TO ACB DOOR SURROUND STRUCTURE. BS787+3.75; RBL20; WL153. ; / [01] REMOVED AND REPLACED NUT PLATE STRIP ACB DOOR SURROUND STRUCTURE BS787+3.75' RBL 20; WL 153. PER DWG#146A0081 REV: A AND SRM 51-40-02.; [02] VERIFIED ACTION 1; [03] VERIFIED ACTION 1

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+14.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+14.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+14.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FWD SHIELD CORROSION. BS767+3.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FWD SHIELD BS767+3.5 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT IAW SRM 51-10-02; [02] REMOVED SHIELD AT ACB BS767+3.5 RBL22 WL151 IAW SRM 51-40-02 LOCATED; DRILLED AND COUNTERSINK NEW SHIELD P/N 146A8127U12 PO# 835530 IAW SRM 51-40-05; 51-50-08 AND DWG 146A8127; [07] VERIFIED ACTION 6; [08] TOPCOAT ENAMEL AND CIC APPLIED PER CUSTOMER CARD# TTG8Q004E21X REQUEST OK TO INSTALL.; [09] VERIFIED ENAMEL & CIC WERE APPLIED ON FAULT TTG8Q004E21X STEPS 24 & 32.<BR>OK TO INSTALL ACB FORWARD SHIELD GIVEN.; [10] INSTALLED ACB FWD SHIELD BS 767-794; RBL 22 PER SRM 51-40-02; DWG# 146A0081

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+4; RBL22; WL151 ; / REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+4'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD LOCATED AND DRILLED ACB NEW SIDEWALL SUPPORT BS 727+4 TO BS 767 ; RBL 22; WL 151; IAW SRM 51-40-05-0G-0 AND DWG 146A7500; [06] VERIFIED LOCATE AND DRILL UP PER SRM 51-40-05 AND DWG 146A7500.; [07] REQUEST OK TO INSTALL; [08] REQUEST OK TO INSTALL; [09] OK TO INSTALL GIVEN.; [10] INSTALLED SIDEWALL SUPPORT AT ACB BS 727+4 TO BS 767 ;RBL 22 ;WL 151 IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A7500 REV.- B

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 32,714 hrs · 19,999 cycles

CORROSION ON FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT B.S. 500D; L.B.L. 24 - R.B.L. 24; W.L. 154. ; / [01] ADDED MEASURMENTS; [02] NO ALLOWABLE DAMAGE FOUND IN B737-700 SRM FOR FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT BS500D LBL24-RBL24 WL154. REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0.; [03] REMOVED FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT BS500D LBL24-RBL24 WL154 IAW SRM 51-40-02-0G-0; [04] VERIFIED NO ALLOWABLE DAMAGE FOUND IN B737-700 SRM FOR FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT BS500D LBL24-RBL24 WL154. REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0.; [05] PROCURED NEW FCB AFT BULKHEAD CENTER PNL LOWER SUPPORT ANGLE 143A9485-35 LOT#1467206-1. LOCATED; DRILLED NEW SUPPORT ANGLE PER SRM 51-40-05 AND DWG# 143A9481 REV: -.; [06] VERIFIED ACTION 5; [07] REQUEST OK TO INSTALL NEW FCB BAY AFT BULKHEAD CENTER PNL LOWER SUPPORT AT BS 500D LBL 24 WL 154; [08] OK TO INSTALL FCB AFT CENTER LOWER BULKHEAD SUPPORT GIVEN.; [09] INSTALLED NEW FCB BAY AFT BULKHEAD CENTER PNL LOWER SUPPORT AT BS 500D LBL 24 WL 154. IAW. DWG: 143A7902 AND 143A9481; [10] UPDATED MEASUREMENTS; [11] VERIFIED INSTALLATION OF FCB AFT CENTER LOWER BULKHEAD SUPPORT; CORRECTIVE ACTION 9.; [12] VERIFIED ALL CORRECTIVE ACTIONS ARE COMPLETE AND VERIFIED

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

CORROSION ON FORWARD BAY SHIELD AT B.S. 494-500A; R.B.L. 24; W.L. 154. ; / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0 RECEIVED NEW BAY SHIELD ITEM HFAB53-SHD-011; LOT:1467549-1; PO NUMBER: 835449. LOCATED AND DRILLED; COUNTERSINKED NEW FWD BAY SHIELD IAW SRM 51-40-05 AND DWG 143A8126. OK TO APPLIED PROTECTIVE FINISHED; [04] VERIFIED CORRECTIVE ACTION #3.<BR>OK TO APPLY ENAMEL.; [05] APPLIED CHEMICAL CONVERSION COATING AND PRIMER AND INSTALLED NUTPLATE IAW SRM 51-40-10 AND DWG 143A8126; SRM 51-20-01 AND SOPM 20-41-02. OK TO APPLY WHITE PAINT.; [06] VERIFIED CORRECTIVE ACTION 5. OK TO APPLY ENAMEL.<BR>CORRECTION TO CORRECTIVE ACTION 4: OK TO APPLY CHEMICAL CONVERSION COATING & PRIMER.; [07] APPLIED ENAMEL AT FORWARD BAY SHIELD B.S. 494-500A; R.B.L. 24; IAW SOPM 20-41-02; [08] VERIFIED ITEM 7 CORRECTIVE ACTIONS.; [09] APPLIED CIC AT FORWARD BAY SHIELD AT B.S. 494-500A; R.B.L. 24 IAW SOPM 20-41-05 UPDATED MEASUREMENTS; [12] VERIFIED CORRECTIVE ACTIONS 9 AND 10; OK TO INSTALL; [13] INSTALLED BAY SHIELD AT B.S. 494-500A; R.B.L. 24; W.L. 154 IAW SRM 51-40-02 AND DWG 143A0080 AND 143A8126; [14] INSTALLED BAY SHIELD AT B.S. 494-500A; R.B.L. 24; W.L. 154 IAW SRM 51-40-02 AND DWG 143A0080 ID;0038 REV:- AND 143A8126 ID:0018 REV

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FWD SHIELD CORROSION. BS767+11.5; RBL22; WL151 ; / [01] NO ALLOWABLE DAMAGE FOUNDED ON SRM; REPLACE PART FOR REPAIR; THE REP AIR WILL BE DONE UNDER CUSTOMER FAULT TTG8Q006A1HS; [02] NO ALLOWABLE DAMAGE FOUNDED ON SRM; REPLACE PART FOR REPAIR; THE REPAIR WILL BE DONE UNDER CUSTOMER FAULT TTG8Q006A1HS; [03] REMOVED CORROSION ON ACB FWD SHIELD BS767+11.5 RBL21 WL151; L=.500 W=.500 D=.003;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS; [04] VERIFIED REMOVED CORROSION ON ACB FWD SHIELD BS767+11.5 RBL21 WL151; L=.500 W=.500 D=.003;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS

Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB WASTE TANK ENCLOSE BULKHEAD SUPPORT ANGLE CRACKED. BS867-1.5; LBL10; WL161 ; / [01] REMOVED BULKHEAD ANGLE SUPPORT AT BS867-1.5' LBL10 WL161 IAW SRM 51-40-02 NO ALLOWABLE LIMITS FOR CRACK; ANGLE IS REPAIRED BY REPLACEMENT IAW SRM 51-10-02; [02] REMOVED BULKHEAD SUPPORT ANGLE FOM BETWEEN BS 847 - 867 LBL 10 - 17;WL 161 PER SRM 51-40-02.; [03] LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-05; DWG# 149A8102; 149A8104. REQUEST OK TO INSTALL.; [04] VERIFIED CORRECTIVE ACTION ENTRY 3. OK TO INSTALL GIVEN.; [05] INSTALLED ACB WASTE TANK ENCLOSURE BULKHEAD SUPPORT BRACKET AT BS 867; LBL 10 IAW SRM 51-40-02; DWG# 149A8102; 149A8104.; [06] VERIFIED CORRECTIVE ACTION ENTRY 5.; [07] VERIFIED CARD COMPLETE

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+15.75; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+15.75'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+15.75'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+16.25; RBL20; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+16.25'; RBL 20; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+16.25'; RBL 20; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB DOOR SURROUND; SUB THRESHOLD WEB CORROSION. BS827+2.2; RBL27; WL153. REMOVED CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB AT BS 827+2.2' RBL 27 WL 153. MEASURED L 1' X W .5' AND 0.006' DEEP. ORIGINAL THICKNESS .050'; REMAINING THICKNESS .049'. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 ALLOWABLE DAMAGE 1 - AFT CARGO DOOR SURROUND STRUCTURE<BR>TO BE REPAIRED BY REPLACEMENT ON CUSTOMER CARD TTG8Q006A439. REMOVED CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB AT BS 827+2.2' RBL 27 WL 153<BR>MEASURED L 1' X W .5' AND 0.006' DEEP. ORIGINAL THICKNESS .050'; REMAINING THICKNESS .044'<BR>FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 ALLOWABLE DAMAGE 1 - AFT CARGO DOOR SURROUND STRUCTURE TO BE REPAIRED BY REPLACEMENT ON CUSTOMER CARD TTG8Q006A439. VERIFIED SUB THRESHOLD TO BE REPLACED ON FAULT #TTG8Q006A439

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+18.2; LBL20; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727E+18.2 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727E+18.2 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (BS 727D) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D+5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727C) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727C+18.5; RBL22; WL151 ; / [01] FAULT RESOLVED ON OTHER CUSTOMER CARD NBR:TTG8Q006A3FD; [02] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727C+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [03] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727C+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SHIELD — CORRODED (BS 767) · airframe 32,714 hrs · 19,999 cycles

ACB FWD SHIELD CORROSION. BS767+15.7; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FWD SHIELD BS767+15.7 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS; [02] VERIFIED REMOVED CORROSION ON ACB FWD SHIELD BS767+15.7 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+2; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+2'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.035' ; REMAINING THICKNESS IS 0.005 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+2'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.035' ; REMAINING THICKNESS IS 0.005 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 767) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS767+10.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767=10.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767=10.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS747+5.5; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+5.5'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+5.5'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E; RBL19; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E; RBL 19; WL 151 ; WORK AREA 1.0'X 1.0' X 0.008' ; REMAINING THICKNESS IS 0.032 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E; RBL 19; WL 151 ; WORK AREA 1.0'X 1.0' X 0.008' ; REMAINING THICKNESS IS 0.032 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727B) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727B+14.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727B+14.5'; RBL22; WL151; WORK AREA 1.0' X 1.0' X 0.022' REMAINING THICKNESS IS 0.018. FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID:ATS 2472 S/N UNKNOWN DUE:06/2022. REPAIRED BY REPLACEMENT ON JOB CARD TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727B+14.5'; RBL22; WL151; WORK AREA 1.0' X 1.0' X 0.022' REMAINING THICKNESS IS 0.018. FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID:ATS 2472 S/N UNKNOWN DUE:06/2022. REPAIRED BY REPLACEMENT ON JOB CARD TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727B) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727B+15.5; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727B+15.5'; RBL21; WL151; WORK AREA 1.0' X 1.0' X 0.007' REMAINING THICKNESS IS 0.033. FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID:ATS 2472 S/N UNKNOWN DUE:06/2022. REPAIRED BY REPLACEMENT ON JOB CARD TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727B+15.5'; RBL21; WL151; WORK AREA 1.0' X 1.0' X 0.007' REMAINING THICKNESS IS 0.033. FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID:ATS 2472 S/N UNKNOWN DUE:06/2022. REPAIRED BY REPLACEMENT ON JOB CARD TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 32,714 hrs · 19,999 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT B.S. 500A-500D; R.B.L. 24; W.L. 154. ; / REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0.; [03] CORROSION DAMAGE WAS REMOVED IAW SRM 53-00-53-1A-2; [04] CORRECTION. CHANGED POTENTIAL CORROSION LEVEL FROM LEVEL 1 TO LEVEL 2. (OUT OF ALLOWABLE DAMAGE LIMITS); [05] VERIFIED CORRECTIVE ACTION ITEMS 1 THRU 4. OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2.; [06] CALIBRATION TOOL DEPTH GAUGE<BR>ID : ATS2472<BR>S/N : UNKNOWN<BR>DUE : 06/2022; [07] LOCATED; DRILLED; AND COUNTERSANK NEW FLOOR TO SIDEWALL SUPPORT MATERIAL USING BAC1496-444#7075T62 LOT# 1466509-1 IAW SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 143A7501 REV:-; [08] APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02; INSTALLED FLOOR TO SIDEWALL SUPPORT AT B.S. 500A-500D; R.B.L. 24 W.L. 154 IAW SRM 51-40-02 AND DWG 143A7500 AND 143A7505

Part: SUPPORT — CORRODED (BS 727D) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D+14.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+14.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+14.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FWD SHIELD CORROSION. BS767+9.2; RBL21; WL151 ; / [01] NO ALLOWABLE DAMAGE FOUNDED ON SRM; REPLACE PART FOR REPAIR; THE REP AIR WILL BE DONE UNDER CUSTOMER FAULT TTG8Q006A1HS; [02] NO ALLOWABLE DAMAGE FOUNDED ON SRM; REPLACE PART FOR REPAIR; THE REPAIR WILL BE DONE UNDER CUSTOMER FAULT TTG8Q006A1HS; [03] REMOVED CORROSION ON ACB FWD SHIELD BS767+9.2 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS; [04] REMOVED CORROSION ON ACB FWD SHIELD BS767+9.2 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS; [05] VERIFIED REMOVED CORROSION ON ACB FWD SHIELD BS767+9.2 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+14.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 747 +14.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 747 +14.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+10.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 747+10.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 747+10.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727C+10.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727C+10.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 5110-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2<BR><BR>TOOL USED:<BR>ATS1671<BR>CAL DUE 01/2022<BR><BR>PART TO BE REPAIRED ON CARD #:<BR>TTG8Q006A199; [02] VERIFIED REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 727C+10.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; SRM 53-60-53-0I-2 <BR><BR>TOOL USED: <BR>ATS1671 <BR>CAL DUE 01/2022 <BR><BR>PART TO BE REPAIRED ON CARD #: <BR>TTG8Q006A199

Part: SUPPORT — CORRODED (BS 727D) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D+10.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+10.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.007' ; REMAINING THICKNESS IS 0.033 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+10.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.007' ; REMAINING THICKNESS IS 0.033 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: ANGLE — CORRODED (BS 727D) · airframe 32,714 hrs · 19,999 cycles

ACB CORROSION ON CLIP. FOWARD SIDE OF BS727D; RBL6; WL144.5 ; / [01] REMOVED CLIP AT BS727D RBL 6 WL 144.5 IAW SRM 51-40-02 NO ALLOWABLE LIMITS FOR CRACK; CLIP IS REPAIRED BY REPLACEMENT IAW SRM 51-10-02; [02] FABRICATED ACB CLIP 146A1320-10 PER DWG 146A1323 PL. PRIMED PER FINISH CODE 17.07 OK TO PRIME; [03] VERIFIED CORRECTIVE ACTION STEP 2 PER DWG. VERIFIED OK TO PRIME.; [04] COMPLETED PRIME AND LOCATED DRILLED -10 CLIP FROM BAC1490-2815 7075T62 LOT #1455934-1 PER DWG 146A1320. TASK 2. DWG CORRECTION TO BE 146A1320; [05] VERIFIED PART MATERIAL; LOCATION; AND DRILL UP PER DWG 146A1320; [06] OK TO INSTALL NEW CLIP; [07] FABRICATED ACB CLIP 146A1320-10 PER DWG 146A1320 PL. APPLIED CHEMICAL CONVERSION COATING PER FINISH CODE 17.07 OK TO PRIME; [08] INSTALLED -10 CLIP PER DWG 146A7810 SHT 3 AND 4; [09] UPDATE MEASUREMENT; [10] VERIFIED INSTALLATION OF CLIP PER DWG 146A1320 AND SRM 51-40-02; [11] TASK COMPLETE; [12] VERIFIED MEASUREMENTS UPDATED.; [13] REMOVED CLIP AT BS727D RBL 6 WL 144.5 IAW SRM 51-40-02 NO ALLOWABLE LIMITS FOR CORROSION; CLIP IS REPAIRED BY REPLACEMENT IAW SRM 51-10-02; [14] EDITED ITEM 1 FROM CRACK TO CORROSION

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FWD SHIELD CORROSION. BS787+2; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FWD SHIELD BS767+2 RBL21 WL151; L=.500 W=.500 D=.010;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS; [02] VERIFIED REMOVED CORROSION ON ACB FWD SHIELD BS767+2 RBL21 WL151; L=.500 W=.500 D=.010;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS

Part: SUPPORT — CORRODED (BS 727C) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727C+18.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727C+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727C+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727D) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D+18.5; RBL22; WL151 ; / [01] FAULT RESOLVED ON OTHER CUSTOMER CARD NBR:TTG8Q006A3FD; [02] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [03] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FWD SHIELD CORROSION. BS767+7.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FWD SHIELD BS767+7.5 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS; [02] VERIFIED REMOVED CORROSION ON ACB FWD SHIELD BS767+7.5 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS

Part: SUPPORT — CORRODED (BS 747) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+12; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+12'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.013' ; REMAINING THICKNESS IS 0.027 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+12'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.013' ; REMAINING THICKNESS IS 0.027 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SUPPORT — CORRODED (BS 727D) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D+6; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+6'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+6'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: WEB — CORRODED (AFT CARGO THSHLD) · airframe 32,714 hrs · 19,999 cycles

ACB DOOR SURROUND; SUB THRESHOLD WEB CORROSION. BS827+2.5; RBL27; WL153 ; / [01] REMOVED CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB AT BS 827+2.5' RBL 27 WL 153<BR>MEASURED L 1' X W 1' AND 0.006' DEEP. ORIGINAL THICKNESS .050'; REMAINING THICKNESS .049'<BR>FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 ALLOWABLE DAMAGE 1 - AFT CARGO DOOR SURROUND STRUCTURE TO BE REPAIRED BY REPLACEMENT. REMOVED CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB AT BS 827+2.5' RBL 27 WL 153, MEASURED L 1' X W 1' AND 0.006' DEEP. ORIGINAL THICKNESS .050'; REMAINING THICKNESS .049'. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 ALLOWABLE DAMAGE 1 - AFT CARGO DOOR SURROUND STRUCTURE LOCATED AND DRILLED ACB SURROUND SUB THRESHOLD WEB IAW DWG 146A8120 SH42 REV A & SRM 51-40-05; [04] LOCATED AND DRILLED ACB SURROUND SUB THRESHOLD WEB IAW DWG 146A8120 SH42 REV A ;DWG 146A8340 SH16 AND SRM 51-40-05; [05] INSPECTED AND VERIFIED CORRECTIVE ACTION ITEMS 1 THRU 4. OKAY TO INSTALL NEW SUB THRESHOLD WEB. REINSTALLED AFT CARGO BAY SUBTHRESHOLD WEB. IAW SRM 51-40-02; DWG 146A8340 ID:0021 REV:-; [07] VERIFIED ACTION 6; [08] VERIFIED ACTION 6.

Part: SUPPORT — CORRODED (BS 727E) · airframe 32,714 hrs · 19,999 cycles

ACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+14.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+14.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.022' ; REMAINING THICKNESS IS 0.018 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD; [02] VERIFIED REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+14.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.022' ; REMAINING THICKNESS IS 0.018 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 USING DEPTH GAGE ID: ATS2472; S/N UNKNOWN ;DUE 06/2022 ; PART TO BE REPAIRED BY REPLACEMENT BY CUSTOMER CARD NBR:TTG8Q006A3FD

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 32,714 hrs · 19,999 cycles

ACB FWD SHIELD CORROSION. BS767+6; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FWD SHIELD BS767+6 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS; [02] VERIFIED REMOVED CORROSION ON ACB FWD SHIELD BS767+6 RBL21 WL151; L=.500 W=.500 D=.005;USED CALIBRATION TOOL ID:ATS1866 SERIAL:UNKNOWN DATE DUE:01/2022; NO ALLOWABLE LIMITS IN SRM; SHIELD IS REPAIRED BY REPLACEMENT ACCOMPLISHED ON CUSTOMER FAULT TTG8Q006A1HS

Part: RETAINER — CRACKED (VERTICAL STAB) · airframe 32,714 hrs · 19,999 cycles

VERTICAL STAB PANEL 324AL RETAINER CRACKED ; / [01] REMOVED AND REPLACED VERTICAL STAB PANEL 324AL RETAINER IAW SRM 51-40-02-0G-0 STEP 4 AND DRAWING 172A6123; [02] VERIFIED REMOVED AND REPLACED VERTICAL STAB PANEL 324AL RETAINER IAW SRM 51-40-02-0G-0 STEP 4 AND DRAWING 172A6123

Part: SEAT TRACK — CORRODED (BS 616) · airframe 32,714 hrs · 19,999 cycles

CORROSION SEAT TRACK WELL BS 616 +16 LBL 45 WL 208 ; / [01] REMOVED CORROSION ON LOWER SURFACE OF SEAT TRACK AT B.S 616 + 16' LBL45 WL208 IAW SRM 51-10-02-OG-0. BLEND AREA IN LOWER WELL WAS 1'X0.7'X.015' . IN LIMITS IAW SRM 53-00-52-1A-1 FIG 103. DEPTH MEASURED BY DIAL DEPTH GAUGE ; ATS 1737; S/N: NSN; DUE 07/2022;; [02] VERIFIED REMOVED CORROSION ON LOWER SURFACE OF SEAT TRACK AT B.S 616 + 16' LBL45 WL208 IAW SRM 51-10-02-OG-0. BLEND AREA IN LOWER WELL WAS 1'X0.7'X.015' . IN LIMITS IAW SRM 53-00-52-1A-1 FIG 103. DEPTH MEASURED BY DIAL DEPTH GAUGE ; ATS 1737; S/N: NSN; DUE 07/2022; [03] ADDITIONAL DAMAGE AREA ON CUST SYSTEM ID:TTG8Q0069GY2 FOUND OUT OF LIMITS AND WILL BE REPLACED FROM BS 540 TO 727B; LBL46; WL208; [04] CERTIFY; [05] VERIFIED ADDITIONAL DAMAGE AREA ON CUST SYSTEM ID:TTG8Q0069GY2 FOUND OUT OF LIMITS AND WILL BE REPLACED FROM BS 540 TO 727B; LBL46; WL208

Part: SEAT TRACK — CORRODED (BS 663) · airframe 32,714 hrs · 19,999 cycles

CORROSION SEAT TRACK WELL BS 663.75 LBL 46 WL 208 ; / [01] REMOVED CORROSION ON LOWER SURFACE OF SEAT TRACK AT B.S 663.75 LBL46 WL208 IAW SRM 51-10-02-OG-0. BLEND AREA IN LOWER WELL WAS 1'X0.7'.017' . IN LIMITS IAW SRM 53-00-52-1A-1 FIG 103. DEPTH MEASURED BY DIAL DEPTH GAUGE ; ATS 1737; S/N: NSN; DUE 07/2022;; [02] VERIFIED REMOVED CORROSION ON LOWER SURFACE OF SEAT TRACK AT B.S 663.75 LBL46 WL208 IAW SRM 51-10-02-OG-0. BLEND AREA IN LOWER WELL WAS 1'X0.7'.017' . IN LIMITS IAW SRM 53-00-52-1A-1 FIG 103. DEPTH MEASURED BY DIAL DEPTH GAUGE ; ATS 1737; S/N: NSN; DUE 07/2022;; [03] ADDITIONAL DAMAGE AREA ON CUST SYSTEM ID:TTG8Q0069GY2 FOUND OUT OF LIMITS AND WILL BE REPLACED FROM BS 540 TO 727B; LBL46; WL208; [04] CERTIFY; [05] VERIFIED ADDITIONAL DAMAGE AREA ON CUST SYSTEM ID:TTG8Q0069GY2 FOUND OUT OF LIMITS AND WILL BE REPLACED FROM BS 540 TO 727B; LBL46; WL208

Part: SEAT TRACK — CORRODED (BS 727A) · airframe 32,714 hrs · 19,999 cycles

CORROSION SEAT TRACK WELL BS 727A +8 TO BS 727A +12 LBL 46 WL 208 ; / [01] ADDITIONAL DAMAGE AREA ON CUST SYSTEM ID:TTG8Q0069GY2 FOUND OUT OF LIMITS AND WILL BE REPLACED FROM BS 540 TO 727B; LBL46; WL208; [02] CERTIFY; [03] VERIFIED SEAT TRACK WILL BE REPLACED BS 540 TO 727B; LBL46; WL208 ON CUSTOMER CARD # TTG8Q0069GY2

Part: SEAT TRACK — CORRODED (BS 787) · airframe 32,714 hrs · 19,999 cycles

CORROSION ON BOTTOM OF SEAT TRACK FROM BODY STA 787 + 7 TO STA 787 + 12; RBL 44; WL 208 ; / [01] REMOVED CORROSION ON BOTTOM OF SEAT TRACK AT BS8787+7 TO 787+12 RBL45 WL208. 8.500'X0.90' MAX. DEPTH: 0.043' IAW SRM 53-00-52-1A-1 AND WAS FOUND OUT LIMITS. MEASUREMENT TOOL ID:ATS1737 S/N: UNKNOWN CAL. DATE 07/2021[03] INSTALLED EWIS AND FOD PROTECTION BS 727A-887 UNDER SEAT TRACK RBL 45 AS REQUIRED PER AMM 20-60-07; [04] REMOVED DAMAGED SEAT TRACK FROM BS 727B-887 RBL 45.5 IAW SRM CH 51-40-02; [05] SEAT TRACK FABRICATED IAW BOEING DWG 146A5350. REFER TO ATS WORK ORDER #W57955 & PO #778043. PART MARKED PER ATS QCM 4.35.26.; [06] LOCATED AND DRILLED SEAT TRACK AT BS 727B-887; RBL 44 ;WL 208 PER DWG 146A5300; [07] INSPECTED AND VERIFIED CORRECTIVE ACTION ITEMS 3 THRU 6. OKAY TO INSTALL SEAT TRACK.; [08] INSTALLED SEAT TRACK AT BS 727B-887; RBL 44; WL 208 IAW DWG 146A5300. TOOL USED ID#ATS1353 S/N 0614803529

Part: SEAT TRACK — CORRODED (BS 639) · airframe 32,714 hrs · 19,999 cycles

CORROSION SEAT TRACK WELL BS 639 +7 LBL 45 WL 208 ; / [01] REMOVED CORROSION ON LOWER SURFACE OF SEAT TRACK AT B.S 639 +7 LBL45 WL208 IAW SRM 51-10-02-OG-0. BLEND AREA IN LOWER WELL WAS 1'X0.7'X.010' . IN LIMITS IAW SRM 53-00-52-1A-1 FIG 103. DEPTH MEASURED BY DIAL DEPTH GAUGE ; ATS 1737; S/N: NSN; DUE 07/2022;; [02] VERIFIED REMOVED CORROSION ON LOWER SURFACE OF SEAT TRACK AT B.S 639 +7 LBL45 WL208 IAW SRM 51-10-02-OG-0. BLEND AREA IN LOWER WELL WAS 1'X0.7'X.010' . IN LIMITS IAW SRM 53-00-52-1A-1 FIG 103. DEPTH MEASURED BY DIAL DEPTH GAUGE ; ATS 1737; S/N: NSN; DUE 07/2022; [03] ADDITIONAL DAMAGE AREA ON CUST SYSTEM ID:TTG8Q0069GY2 FOUND OUT OF LIMITS AND WILL BE REPLACED FROM BS 540 TO 727B; LBL46; WL208; [04] CERTIFY; [05] VERIFIED ADDITIONAL DAMAGE AREA ON CUST SYSTEM ID:TTG8Q0069GY2 FOUND OUT OF LIMITS AND WILL BE REPLACED FROM BS 540 TO 727B; LBL46; WL208

Part: SEAT TRACK — CORRODED (BS 706) · airframe 32,714 hrs · 19,999 cycles

CORROSION SEAT TRACK WELL BS 706 LBL 46 WL 208 ; / [01] ADDITIONAL DAMAGE AREA ON CUST SYSTEM ID:TTG8Q0069GY2 FOUND OUT OF LIMITS AND WILL BE REPLACED FROM BS 540 TO 727B; LBL46; WL208; [02] CERTIFY; [03] VERIFIED SEAT TRACK WILL BE REPLACED BS 540 TO 727B; LBL46; WL208 ON CUSTOMER CARD # TTG8Q0069GY2

Part: SEAT TRACK — CORRODED (BS 663) · airframe 32,714 hrs · 19,999 cycles

CORROSION SEAT TRACK WELL BS 663.75 +7 TO BS 663.75 +14 LBL 46 WL 208 ; / [01] REMOVED CORROSION ON LOWER SURFACE OF SEAT TRACK AT B.S 663.75+7 TO 663.75+14 LBL46 WL208 IAW SRM 51-10-02-OG-0. BLEND AREA IN LOWER WELL WAS 7'X0.7'X.022' . IN LIMITS IAW SRM 53-00-52-1A-1 FIG 103. DEPTH MEASURED BY DIAL DEPTH GAUGE ; ATS 1737; S/N: NSN; DUE 07/2022;; [02] VERIFIED REMOVED CORROSION ON LOWER SURFACE OF SEAT TRACK AT B.S 663.75+7 TO 663.75+14 LBL46 WL208 IAW SRM 51-10-02-OG-0. BLEND AREA IN LOWER WELL WAS 7'X0.7'X.022' . IN LIMITS IAW SRM 53-00-52-1A-1 FIG 103. DEPTH MEASURED BY DIAL DEPTH GAUGE ; ATS 1737; S/N: NSN; DUE 07/2022;; [03] ADDITIONAL DAMAGE AREA ON CUST SYSTEM ID:TTG8Q0069GY2 FOUND OUT OF LIMITS AND WILL BE REPLACED FROM BS 540 TO 727B; LBL46; WL208; [04] CERTIFY; [05] VERIFIED ADDITIONAL DAMAGE AREA ON CUST SYSTEM ID:TTG8Q0069GY2 FOUND OUT OF LIMITS AND WILL BE REPLACED FROM BS 540 TO 727B; LBL46; WL208

Part: SEAT TRACK — CORRODED (BS 706) · airframe 32,714 hrs · 19,999 cycles

CORROSION SEAT TRACK WELL BS 706 +20 LBL 46 WL 208 ; / [01] ADDITIONAL DAMAGE AREA ON CUST SYSTEM ID:TTG8Q0069GY2 FOUND OUT OF LIMITS AND WILL BE REPLACED FROM BS 540 TO 727B; LBL46; WL208; [02] CERTIFY; [03] VERIFIED SEAT TRACK WILL BE REPLACED BS 540 TO 727B; LBL46; WL208 ON CUSTOMER CARD # TTG8Q0069GY2

Part: SEAT TRACK — CORRODED (BS 685) · airframe 32,714 hrs · 19,999 cycles

CORROSION SEAT TRACK WELL BS 685 +9 TO BS 685 +14 LBL 46 WL 208 ; / [01] REMOVED CORROSION ON BOTTOM OF SEAT TRACK AT BS685+9 TO BS 685+14 LBL46 WL208; CORROSION MEASURES REMOVED 5'X.7'X.046' FOUND OUT LIMITS IAW SRM 53-00-52-1A-1 STEP 4.A(2); CALIBRATED TOOL ID:ATS1737; S/N:NSN; DUE:07/2022; [02] VERIFIED REMOVED CORROSION ON BOTTOM OF SEAT TRACK AT BS685+9 TO BS 685+14 LBL46 WL208; CORROSION MEASURES REMOVED 5'X.7'X.046' FOUND OUT LIMITS IAW SRM 53-00-52-1A-1 STEP 4.A(2); CALIBRATED TOOL ID:ATS1737; S/N:NSN; DUE:07/2022; [03] REMOVED SEAT TRACK WELL BS 540 TO 727B IAW SRM 51-40-02-OG-0; [04] CERTIFY REMOVAL; [05] SEAT TRACK FABRICATED IAW DWG 144A5350; REFER TO ATS BUILD RECORD 526789. PART MARKED PER ATS QCM 4.35.26.; [06] LOCATED AND DRILLED SEAT TRACK AT LBL 45.5; BS 540-727B; WL208 PER DWG 144A5300. OK TO INSTALL.; [07] INSPECTED SEAT TRACK LOCATED AND DRILLED. OKAY TO INSTALL PER DWG 144A5300; [08] INSTALLED SEAT TRACK AT LBL 45.5; BS 540-727B; WL 208 PER DWG 144A5300. ALL FASTENERS STILL REQUIRE TORQUE.; [09] TORQUED FASTENERS IAW AMM 20-50-11-901-801.<BR>ID: ATS2328 S/N: 0219095273.; [10] VERIFIED INSTALLED SEAT TRACK AT LBL 45.5; BS 540-727B; WL 208 PER DWG 144A5300; TORQUED FASTENERS IAW AMM 20-50-11-901-801. <BR>CALIBRATED TOOL ID: ATS2328 S/N: 0219095273.

Part: SUPPORT — CRACKED (BS 540) · airframe 32,714 hrs · 19,999 cycles

CRACKED PNEUMATIC DUCT CLAMP SUPPORT AT B.S. 540+5; R.B.L. 7; W.L. 160. ; / [01] REMOVED PNEUMATIC DUCT CLAM SUPPORT P/N 212A1116-1 AT BS 540+5 RBL 7 WL 160 IAW SRM 51-4-02; [02] RECIEVED NEW BRACKET ASSY P/N 212A1116-1AAR LOT: 1462093-1 . REQUEST OK TO INSTALL; [03] VERIFIED OK TO INSTALL; [04] INSTALLED NEW BRACKET ASSY P/N: 212A1116-1AAR LOT: 1462093-1 IAW. DWG: 212A116 AND AMM 36-13-01-401; [05] INSTALLED NEW BRACKET ASSY P/N: 212A1116-1AAR LOT: 1462093-1 IAW DWG# 212A116 AND AMM 36-13-01-401; AIPC 36-13-01-01A.; [06] FINAL INSPECTION. JOB COMPLETE PER AMM 36-13-01-401 AND DWG 212A!16.; [07] NO FOLLOW ON REQUIREMENTS

Part: SUPPORT — CRACKED (BS 540) · airframe 32,714 hrs · 19,999 cycles

CRACKED PNEUMATIC DUCT CLAMP SUPPORT AT B.S. 540+5; L.B.L. 7; W.L. 160. ; / [01] REMOVED PNEUMATIC DUCT CLAM SUPPORT P/N 212A1116-1 AT BS 540+5 LBL 7 WL 160 IAW SRM 51-4-02; [02] REMOVED PNEUMATIC DUCT CLAM SUPPORT P/N 212A1116-1 AT BS 540+5 LBL 7 WL 160 IAW SRM 51-4-02; [03] RECIEVED NEW BRACKET ASSY P/N 212A1116-1AAR LOT: 1454605-1 . OK TO INSTALL; [04] VERIFIED OK TO INSTALL; [05] INSTALLED NEW BRACKET ASSY P/N: 212A1116-1AAR LOT: 1454605-1 IAW. DWG: 212A116 AND AMM 36-13-01-401; [06] INSTALLED NEW BRACKET ASSY P/N: 212A1116-1AAR LOT: 1454605-1 IAW DWG# 212A116 AND AMM 36-13-01-401; AIPC 36-13-01-01A.; [07] FINAL INSPECTION. JOB COMPLETE PER AMM 36-13-01-401 AND DWG 212A116.; [08] NO FOLLOW ON REQUIREMENTS

Part: PANEL — DETERIORATED (RT WING LE) · airframe 32,714 hrs · 19,999 cycles

RIGHT WING L/E PANEL 621JB HAS DISBOND AT CUTOUT FWD I/B AND O/B FWD CORNERS ; / [01] IDENTIFIED MATERIAL OF PANEL 621JB IAW SRM 57-41-01-0I-4 FIGURE 1; 4 & 15; ITEM 2; TABLE 4 & 13<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 TABLE 101; PARA 4.A(5)REMOVED 1EA BACKING PLATE IAW SRM 51-40-02-0G-0 PARA 4.E<BR><BR>VISUALLY EXAMINED EXTENT OF DAMAGE; TAP TESTED - DISBONDS NOTED; REMOVED 2 AREAS OF DISBOND; AREA #1; IB CUTOUT CORNER; REMOVED 2.5' X 2.5' OF DAMAGE; AREA #2; OB CUTOUT CORNER; REMOVED 2.4' X 3' OF DAMAGE; PREPPED AND CLEANED REPAIR AREAS IAW SRM 51-70-05-2R-6 PARA 4.A-C REMOVED INNER SURFACE ALUMINUM FOIL PLY AND CLEANED IAW SRM 51-70-14-2R-3 PARA 4.A(2)(E)<BR><BR>FABRICATED REPAIR PLIES FROM BMS 8-79 FIBERGLASS LOT# 1464915-1 AND 1458373-1 AND BMS 5-129 (GR5) ADHESIVE LOT# 1464324-2; INSTALLED REPAIR PLIES; VACUUM BAGGED AND SET FOR CURE IAW SRM 51-70-05-2R-6 PARA 4.E-G<BR><BR>HOT BONDER ID: IS000678 S/N: 12071586; [05] CURED REPAIR; UNBAGGED AND LIGHTLY SANDED IAW SRM 51-70-05-2R-6 PARA 4.G AND ICLEANED PANEL; FABRICATED ALUMINUM FOIL PLY FROM BMS 8-289 LOT# 1441162-1; INSTALLED FOIL WITH BMS 5-128 (956) LOT# 1466513-1 RESINREINSTALLED 1EA BACKING PLATE IAW SRM 51-40-02-0G-0 PARA 4.B-C; BOEING DWG 116A9110 SHEET 7; [10] VERIFIED CORRECTIVE ACTIONS 8 AND 9; [11] REPAIRED DISBONDS AT CUTOUT FWD IB AND OB CORNERS ON PANEL 621JB IAW SRM 51-70-05-2R-6 AND SRM 51-70-14-2R-3

Part: PUMP — LEAKING (B HYD SYSTEM) · airframe 32,163 hrs · 19,675 cycles

LOSS SYSTEM B HYDRAULIC FLUID INFLT BOTH LOW PRESS LIGHTS ILLUMINATED ELEC 1B ENG 2 ; / FOUND FLAP FLOW LIMITER FUSE LEAKING. R/R EDP AND EDMP CASE DRAIN FILTERS FOR B SYS; REPLACED B SYS RETURN FILTER. FOUND NO EVIDENCE OF DEBRIS OR METALIC PARTICLES; RESERVICED B RESEVOIR AND OPS CHECKED ALL SYSTEMS PER AMM REF 29-00-00 AND FIM 29-11-00-810 TASK 802

Part: FILTER — LEAKING (B HYD SYSTEM) · airframe 32,163 hrs · 19,675 cycles

LOSS SYSTEM B HYDRAULIC FLUID INFLT BOTH LOW PRESS LIGHTS ILLUMINATED ELEC 1B ENG 2 ; / FOUND FLAP FLOW LIMITER FUSE LEAKING. R/R EDP AND EDMP CASE DRAIN FILTERS FOR B SYS; REPLACED B SYS RETURN FILTER. FOUND NO EVIDENCE OF DEBRIS OR METALIC PARTICLES; RESERVICED B RESEVOIR AND OPS CHECKED ALL SYSTEMS PER AMM REF 29-00-00 AND FIM 29-11-00-810 TASK 802

Part: HANDLE — BROKEN (GLLY DOOR ASSIST) · airframe 31,902 hrs · 19,516 cycles

F/O PULL HANDLE BROKEN ; / REMOVE AND REPLACE PULL ASSIST HANDLE. OPS NORMAL; REF 56-11-00 F/O SIDE.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 29,738 hrs · 18,216 cycles

FLOOR TRACK LIGHTS; AREA 8D IS LOOSE. RESECURED PHOTO LUMINECENT TRACK LIGHT TO FLOOR PER SIP.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 28,672 hrs · 17,528 cycles

CAPT'S AFT I/B SEAT TRACK IS OUT OF LIMITS. / REMOVED AND REPLACED CAPT'S AFT I/B SEAT TRACK PER AMM 25-11-11.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 28,672 hrs · 17,528 cycles

F/O'S AFT I/B SEAT TRACK IS OUT OF LIMITS. / REMOVED AND REPLACED F/O'S AFT I/B SEAT TRACK PER AMM 25-11-11.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 28,672 hrs · 17,528 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1668, M1669, M1670 AND M1673 IN CABIN. / R&R EMERGENCY LIGHT BATTERY PACKS PER AMM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 28,672 hrs · 17,528 cycles

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

Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 28,672 hrs · 17,528 cycles

RIGHT KEEL BEAM TO VAPOR BARRIER SUPPORT ANGLE CRACKED AT BS. 662, RBL 6.01 IN THE RADIUS AT THE KEEL BEAM. / R&R SUPPORT ANGLE PER SRM AND DWG.

Part: PIN — NOT SEATED (CONNECTOR) · airframe 27,460 hrs · 16,751 cycles

DOME EMERGENCY LIGHT INOP. RESEATED PIN CONNECTOR IAW AMM.

Part: FLOOR PANEL — MISSING (CABIN FLOOR) · airframe 27,460 hrs · 16,751 cycles

FWD PASSENGER CABIN FLOOR PANEL 221AF HAS EDGE DAMAGE AT MISSING INSERT ON INBOARD EDGE. / REPAIRED FWD PASSENGER CABIN FLOOR PANEL 221AF OF EDGE DAMAGE AT MISSING INSERT ON INBOARD EDGE (AS MARKED) IAW B737-700 SRM 53-00-50-2R-0 REPAIR GENERAL REV 68 AND B737-700 SRM 53-00-50-2R-6 REPAIR 6 REV 68. A07264; A36551; A93557; A40676

Part: FLOORBOARD — BROKEN (FUSELAGE) · airframe 27,460 hrs · 16,751 cycles

PASSENGER CABIN FLOORBOARD 242XF IS BROKEN INTO MULTIPLE PIECES / REPLACED BROKEN FLOOR PANEL 242XF WITH NEW PANEL P/N 147A5810-11 PANEL INSTALLED ON CARD 39896/2400/0034 JPANEL-241-CLOSE. A TAG: WN6472

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 27,460 hrs · 16,751 cycles

LT CREASE BEAM INNER CHORD ANGLE CRACKED AT VERTICAL FASTENER HOLE AT BS. 303, LBL 56. REPAIRED CREASE BEAM INNER CHORD IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 27,460 hrs · 16,751 cycles

FORWARD PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL UPPER FLANGE CRACKED AT FASTENER HOLE, BETWEEN BS. 312 TO BS. 328, LBL46. / R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 27,460 hrs · 16,751 cycles

FORWARD PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL UPPER FLANGE CRACKED BETWEEN BS. 277 TO BS. 294.5, BL 0. / R&R INTERCOSTAL IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,460 hrs · 16,751 cycles

FORWARD PASSENGER CABIN FLOOR STRUCTURE, CREASE BEAM INNER CHORD ANGLE CORRODED, BETWEEN BS 300 TO BS 327, RBL 55. REPAIRED ANGLE IAW SRM & DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,460 hrs · 16,751 cycles

FORWARD PASSENGER CABIN FLOOR PANEL 221GF AFT OUTBOARD CORNER DAMAGED, BETWEEN BS. 270 TO BS. 420. REPAIRED FLOOR BOARD 221GF IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 27,460 hrs · 16,751 cycles

FLOOR STRUCTURE SUPPORT ANGLE OUTBOARD OF CREASE BEAM INNER CHORD CRACKED BETWEEN BS. 291 TO BS. 295, RBL 54. R&R CHORD IAW DWG AND SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 27,460 hrs · 16,751 cycles

FWD PASSENGER CABIN FLOOR PANEL 221BF AFT OUTBOARD CORNER CRACKED. / EVALUATED; PREPPED; CLEANED AND REPAIRED BROKEN/CRACKED AREA AT AFT O/B CORNER ON FLOORBOARD 221BF IAW B737 SRM 53-00-50-2R-4; PAR 3 (A;C-K1; L1; M1) - REV 68.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,460 hrs · 16,751 cycles

FORWARD PASSENGER CABIN FLOOR PANEL 222DF HAD SEVERAL AREAS DAMAGED TO FORWARD UPPER COMPOSITE SURFACE, BETWEEN BS. 270 TO BS. 420. REPAIRED PANEL 222DF IAW SRM.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 27,460 hrs · 16,751 cycles

PASSENGER CABIN FLOORBOARD 242SF FWD INBD CORNER IS DELAMED / REPAIRED PASSENGER CABIN FLOORBOARD 242SF FWD INBD CORNER IAW B737 SRM 53-00-50-2R-5 REPAIR 5 PARA 3

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 27,460 hrs · 16,751 cycles

PASSENGER CABIN FLOORBOARD 242WF FACE SHEET FIBERS LOOSE BETWEEN BS 887 TO BS 1016. REPAIRED FLOORBOARD 242WF IAW SRM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 27,460 hrs · 16,751 cycles

MAIN CABIN COMPARTMENT L/H STOW BIN EMERGENCY LIGHT LENS CRACKED AT 17. R&R LENS IAW AMM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 27,460 hrs · 16,751 cycles

MAIN CABIN COMPARTMENT L/H STOW BIN EMERGENCY LIGHT LENS CRACKED AT ROW 4. / REPAIRED LENS IAW AMM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 27,460 hrs · 16,751 cycles

MAIN CABIN COMPARTMENT L/H STOW BINS EMERGENCY LIGHT LENS CRACKED BETWEEN ROW 6 TO ROW 7. R&R LENS IAW AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 27,460 hrs · 16,751 cycles

FORWARD LAVATORY EMERGENCY EXIT LIGHT DAMAGED. R&R LIGHT IAW AMM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 27,460 hrs · 16,751 cycles

MAIN CABIN COMPARTMENT L/H STOW BIN EMERGENCY LIGHT LENS CRACKED BETWEEN ROW 19 TO ROW 20. / R&R LENS IAW AMM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 27,460 hrs · 16,751 cycles

MAIN CABIN COMPARTMENT L/H STOW BIN EMERGENCY LIGHT LENS CRACKED AT ROW 14. / R&R LENS IAW AMM.

Part: FAIRING — CRACKED (LOWER EXT FUSELA) · airframe 27,460 hrs · 16,751 cycles

LEFT WING TO BODY FAIRING 195CL AFT CORNER RADIUS IS CRACKED / REPAIRED AND RESTORED DECORATIVE TEFLON FINISH TO LEFT WING TO BODY FAIRING 195CL AFT CORNER; IAW B737-700 SRM 51-70-04-2R-6 RREV 68; 53-40-70-2R-1 REV 68; 51-70-04-2R-0 REV 68 GENERAL AND B737-AMM 51-21-81-370-802 REV 69 (A13438) (A73464) (A33874) (A97075)

Part: SKIN — DELAMINATED (LE SLAT) · airframe 26,619 hrs · 16,204 cycles

LT WING #1 SLAT DELAMINATED ON THE LOWER OUTBOARD SURFACE. REPAIRED #1 SLAT PER EA.

Part: SLIDE — FAILED (R1 DOOR) · airframe 22,241 hrs · 13,325 cycles

R1 DOOR EMERGENCY EVAC SLIDE FAILED TEST. R&R SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,047 hrs · 13,189 cycles

RT OVERWING EXIT SIGN LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BATTERY PACK — FAULTY (FLASHLIGHT) · airframe 21,971 hrs · 13,138 cycles

AFT FLASHLIGHT BATTERIES FAULTY. R & R THE BATTERY PACK IAW MM.

Part: LIGHT — LOOSE (MID CABIN) · airframe 21,729 hrs · 12,983 cycles

MID CABIN EMERGENCY EXIT LIGHT LOOSE. R & R THE LIGHT ASSY IAW MM.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 20,624 hrs · 12,286 cycles

AFT CARGO COMPARTMENT FLOOR BOARD SUPPORT STRIP (TEE) AT STA 772.6 IS CORRODED BEYOND LIMITS / REMOVED AND REPLACED AFT CARGO SUPPORT STRIP (TEE) PER SRM 51-10-02. AT STA 772.6

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 20,624 hrs · 12,286 cycles

AFT CARGO TRACK CORRODED AT BS 767+4, RBL 14. R&R TRACK PER SRM.

Part: FAIRING — CRACKED (RIGHT WING) · airframe 20,624 hrs · 12,286 cycles

FLAP FAIRING 642BB CRACKED ON INNER LOWER SURFACE / REMOVED DAMAGE AND ACCOMPLISHED REPAIR REF EA 1-A57-6168 AND SRM 51-70-05. RESTORED FINISH REF AMM 51-21-99.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 20,624 hrs · 12,286 cycles

AFT CARGO THRESHOLD PLATE WEB SKIN CORRODED. R&R WEB PER SRM.

Part: SLIDER — CRACKED (HORIZONTAL STAB) · airframe 20,624 hrs · 12,286 cycles

RIGHT HAND HORIZONTAL STABILIZER LOWER AFT SLIDER SEAL 343AB IS OUT OF TRACK AND UPPER EDGE OF SLIDER IS CRACKED / REPLACED SEAL PER SRM 51-40-02.

Part: PLATE — CRACKED (RT WING) · airframe 20,624 hrs · 12,286 cycles

RIGHT WING; WAFFLE PLATE IS CRACKED INBD OF #6 FLAP TRACK / R&R'D WAFFLE PLATE IAW SRM 51-40-02.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 20,573 hrs · 12,259 cycles

CENTER CABIN EMERGENCY EXIT SIGN COVER BROKEN. SECURED COVER IAW SIP.

Part: GASKET — LEAKING (NR 1 ENGINE) · airframe 20,251 hrs · 12,070 cycles

ON TAKEOFF ROLL AT 85 KNOTS THE NR 1 ENGINE FAILED. ABORTED THE TAKEOFF. ENGINE FAIL ILLUMINATED AND NR 1 ENGINE ROLLED BACK. R & R THE GASKET IAW AMM.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 19,065 hrs · 11,347 cycles

L2 DOOR SLIDE HARDWARE LOOSE. SECURED THE SLIDE ASSEMBLY IAW SIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 18,580 hrs · 11,062 cycles

EXTERIOR POWER DOOR CUTOUT CRACKED. REPAIRED CUTOUT PER SRM AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 18,542 hrs · 11,040 cycles

EXTERNAL POWER DOOR CUTOUT CRACKED. REPAIRED CUTOUT PER EA.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,064 hrs · 10,186 cycles

R2 DOOR EXIT LIGHT LENS MISSING. INSTALLED THE LENS IAW MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 13,999 hrs · 8,392 cycles

L1 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW AMM & MT.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 13,539 hrs · 8,098 cycles

CENTER WING LT WW REAR SPAR VAPOR BARRIER CRACKED JUST FWD OF A SYS RETURN FILTER. REPAIRED VAPOR IAW EA.

Part: LENS — MISSING (CABIN) · airframe 12,920 hrs · 7,742 cycles

RIGHT OVERWING EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: SIGN — UNSECURE (CABIN) · airframe 12,541 hrs · 7,532 cycles

R2 DOOR EMER EXIT SIGN FELL OFF. R & R SIGN IAW MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 12,290 hrs · 7,385 cycles

R1 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: BATTERY — FAILED (CABIN) · airframe 11,205 hrs · 6,719 cycles

AFT RT EMER BATTERY PACK FAILED CAPACITY CHECK. R & R EMER BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 11,205 hrs · 6,719 cycles

RIGHT OVERWING EXIT EMER BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 11,205 hrs · 6,719 cycles

FORWARD LT EMER BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 11,205 hrs · 6,719 cycles

AFT LT EMER BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 10,348 hrs · 6,219 cycles

FORWARD ENTRY DOOR EMER LIGHT LENS LOOSE. SECURED LENS IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 5,610 hrs · 3,413 cycles

L1 DOOR EGRESS LIGHT BROKEN. REMOVED AND REPLACED LIGHT IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 2,567 hrs · 1,513 cycles

LEFT EEPLS COVER MISSING AT ROW 1. INSTALLED COVER PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 1,069 hrs · 661 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP AT ROW 11. REMOVED AND REPLACED LIGHT PER MM.

Part: COVER — LOOSE (CABIN) · airframe 435 hrs · 277 cycles

AFT EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED EEPLS PER MM.

Part: CAP — LOOSE (CABIN) · airframe 85 hrs · 58 cycles

FWD EEPLS END CAP LOOSE. REMOVED AND REPLACED END CAP PER MM.