N777QC

Part: CONNECTOR — INOPERATIVE (L/H FUSELAGE) · airframe 70,958 hrs · 42,186 cycles

EXTERIOR EMER. EXT. LIGHT LEFT FWD DOOR INOP / [01] FOUND PUSHED PIN AT CONNECTOR D11074. SECURED PIN. OPS CK GOOD. REF SWPM 20-61-28; AMM 33-51-04

Part: PANEL — ELONGATED · airframe 70,395 hrs · 41,823 cycles

193B PANEL HAS SEVERAL HOLES ELONGATED / [01] REMOVED AND REPLACED WITH NEW PANEL PER SRM 51-40-02.;[02] C/W INSP

Part: HANDLE — LOOSE (FWD ENTRY DOOR) · airframe 70,260 hrs · 41,732 cycles

FWD ENTRY DOOR ASSIST HANDLE LOOSE / [01] RESECURED FWD ENTRY DOOR ASSIST HANDLE IAW AMM 52-11-31 AC OKAY FOR SERVICE

Part: HANDLE — OUT OF POSITION (R2 DOOR) · airframe 70,111 hrs · 41,630 cycles

R2 DOOR ESCAPE SLIDE PULL TO INFLATE HANDLE COVER NOT EXPOSED. / [01] RE-ATTACHED VELCRO COVER PER AMM 25-66-01.

Part: HANDLE — OUT OF POSITION (R1 DOOR) · airframe 70,111 hrs · 41,630 cycles

R1 DOOR ESCAPE SLIDE PULL TO INFLATE HANDLE COVER NOT EXPOSED. / [01] RE-ATTACHED VELCRO COVER PER AMM 25-66-01.

Part: HANDLE — OUT OF POSITION (L2 DOOR) · airframe 70,111 hrs · 41,630 cycles

L2 DOOR ESCAPE SLIDE PULL TO INFLATE HANDLE COVER NOT EXPOSED. / [01] RE-ATTACHED VELCRO COVER PER AMM 25-66-01.

Part: FLOOR PANEL — DAMAGED (CABIN FLOOR) · airframe 69,839 hrs · 41,432 cycles

PANEL 211AF OIL CANNED AND DENTED / [01] VERIFY APPLICABILITY OF SRM 53-10-51-1A-1 TO THIS ALLOWABLE DAMAGE ON THE FLIGHT DECK FLOOR PANEL. FLIGHT DECK FLOOR PANEL 211AF DENTED AT BS 262 LBL4 WL207.54 DUE TO SHARP CREASE ARE NOT PERMITTED FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1;[02] LOCATED AND DRILLED NEW FLIGHT DECK PANEL 211AF PART#141A5133U15 PER SRM 51-40-05 AND DWG141A0631;[03] PAINTED ON THE TOP SURFACE OF THE FLIGHT DECK 211AF PER AMM 51-21-73-370-803;[04] CERTIFY;[05] VERIFIED CORRECTIVE ACTION 1-3

Part: SIGN — INOPERATIVE (CABIN) · airframe 68,673 hrs · 40,726 cycles

SUPPLEMENTAL INFORMATION: MID PASSENGER CABIN CEILING EMERGENCY EXIT SIGN INOP. ; / [01] REMOVED MID PASSENGER CABIN CEILING EMERGENCY EXIT SIGN PER B737 REF. 33-51-01-960-802.; [02] VERIFIED STEP 1.; [03] REPLACED MID PASSENGER CABIN EXIT SIGN LIGHT ASSEMBLY AS PER REFERENCE B737 AMM 33-51-01-960-802; PERFORMED OPERATIONAL TEST; TEST NORMAL.; [04] VERIFIED STEP 3

Part: STRIP — CORRODED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

FOR CORROSION MEASUREMENTS ONLY: REF TTG8Q006V6JC AFT CAROGO COMPARTMENT FLOOR STRUCTURE LT SIDE CAP STRIP STA 767 HAS EVIDENCE OF CORROSION ; / [01] CORROSION MEASURMENT ONLY; [02] STEP 1 VERIFIED

Part: STIFFENER — CRACKED (R/H HORIZ. STAB.)

WHILE PERFORMING HFEC ON STIFFENER CUT EDGES FOUND ADDITIONAL CRACK ON WEB AT R/H HORIZ. STAB. RIB#4 STIFFENER 3. ; WHILE PERFORMING HFEC ON STIFFENER CUT EDGES FOUND ADDITIONAL CRACK ON WEB AT RH HORIZ. STAB. RIB#4 STIFFENER 3. / [01] REMOVED ADDITIONAL DAMAGED FROM WEB AT R/H HORIZONTAL STAB #4 RIB #3 STIFFENERS IAW B737 SRM 55-10-09-2R REPAIR#4.; 14] (RII) VERIFIED STEP #10; HEAT TREATED FABRICATED #2 AND #4 REPAIR ANGLES PER EA 21-155-03221 AND BAC 5602.

Part: NONE — CRACKED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

FWD CARGO COMPT R/H STA 500A STR 25 SUPPORT BRACKET CRACKED ; / [01] REMOVED SUPPORT BRACKET AT FWD CARGO COMPT R/H STA 500A STR 25 IAW B 737-700 SRM 51-40-02; [02] FABRICATED CLIP. PART# 143A8124-15 MATERIAL USED EXTRUSION PART# BAC1503-100179 PO# 1746001 IAW B737-700 DGW 143A8124; [03] VERIFIED STEPS 1 AND 2 OK TREAT AND PRIME; [04] TREATED AND PRIME SUPPORT CLIP IAW B737-700 SRM 51-20-01-0G-0; [05] VERIFIED STEP 4 OK TO INSTALL NEW CLIP; [06] INSTALLED NEW CLLP AT FWD CARGO COMPT R/H STA 500A STAR 25 IAW B637-700 SRM 51-40-02; [07] STEP #6; ADD REF. DWG. 143A8124.; [08] VERIFIED STEPS 6 AND 7

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

FWD CARGO COMPT L/H STR 25 BETWEEN STA 500B AND STA 500C BAFFLE CRACKED ; / [01] REMOVED AND INSTALLED BAFFLE PLATE AT FWD CARGO STA 500B AND STA 500C IAW B 737-700 SRM 51-40-02; [02] CORRECTION FOR STEP 1 REMOVED BAFFLE AT FWD CARGO COMPT L/H STR 25 BETWEEN STA 500B AND STA 500C REF B737-700 SRM 51-40-02; [03] LOCATED AND DRILLED HOLES ON NEW BAFFLE REF B737-700 SRM 51-40-05; [04] VERIFIED STEPS 1-3 OK TO INSTALL NEW BAFFLE; [05] INSTALLED NEW BAFFLE AT STA. 500B - 500C; S-25L; AS PER B737-7 SRM 51-40-02-0G-0 & DWG. 143A7510.; [06] VERIFIED STEP 5

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

FWD CARGO COMPT L/H STR 25 BETWEEN STA 500A AND 500B BAFFLE CRACKED ; / [01] REMOVED BAFFLE PLATE AT FWD CARGO STA 500A AND 500B IAW B 737-700 SRM 51-40-02; [16] INSTALLED REPAIR ANGLE AT BAFFLE STA. 500A - 500B;S-25L. AS PER B737-7 SRM 53-30-53-2R-1;FIG.202 SHEET 2.; [17] VERIFIED STEP 16 OK TO INSTALL NEW BAFFLE; [18] INSTALLED NEW BAFFLE AT STA. 500A - 500B; S-25L. AS PER B737-7 SRM 51-40-02-0G-0 & DWG. 143A7510.; [19] VERIFIED STEP 18; [20] CORRECTION TO SELECTED REFERENCE.

Part: STUB FRAME — CRACKED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

AFTER PERFORMED DVI OF R-1 DOOR UPPER FWD CUTOUT FOUND CRACKED INTERNAL STUB FRAME STA 296. ; / [01] REMOVED DAMAGE STUB FRAME AT R-1 DOOR UPPER FWD. CUTOUT STA. 296; AS PER B737-7 SRM 51-40-02-0G-0.; [02] LOCATED & DRILLED NEW STUB FRAME R-1 DOOR FWD UPPER CUTOUT STA 296; AS PER B737-7 SRM 51-40-05-0G-0 & DWG. # 141A8370.; [03] VERIFIED STEPS 1 AND 2; [04] OK TO INSTALL NEW STUB FRAME; [05] MIXED BMS 5-95 SEALANT AT 09.00 AM 11-4-21 SQUEEZE OUT TIME BY 05.00 PM 11-7-21; [06] INSTALLED NEW STUB FRAME AT R-1 DOOR FWD UPPER CUTOUT STA 296; AS PER B737-7 SRM 51-40-02-0G-0 & DWG. # 141A8370.

Part: PANEL — CRACKED (R/H WING) · airframe 68,673 hrs · 40,726 cycles

R/W LOWER LEADING EDGE; PANEL 621FB; CRACKED AND DELAMINATED ON CORNER ; / [01] PREPARED DAMAGED AREA; REPAIR AREA IS FULLY DRY NO WATER NOTE AT ACCESS PANEL 621FB. REF B737-700 SRM 51-70-04-2R-13 PARAGRAPH 4 B AND C.; [02] VERIFIED STEP 1; [03] OK TO APPLY REPAIR; [04] APPLIED REPAIR AT DAMAGED AREA ON ACCESS PANEL 621FB. REF B737-700 SRM 51-70-04-2R-13 PARAGRAPH 4 D; E; F; G; H AND I.; [05] VERIFIED STEP 4; [06] OK TO APPLY FINISH; [07] APPLIED FINISH AT REPAIR AREA ON ACCESS PANEL 621FB. REF B737-700 SRM 51-70-04-2R-13 PARAGRAPH 4 I.; [08] VERIFIED STEP 7

Part: STRIP — CORRODED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

REF TTG8Q006V6JC AFT CAROGO COMPARTMENT FLOOR STRUCTURE LT SIDE CAP STRIP STA 767 HAS EVIDENCE OF CORROSION. COMPLIANCE FINDING MISSING MEASUREMENTS ; / [01] ADDED MEASUREMENTS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

REF TTG8Q006UTC1 FLOOR BEAM AT 294.5 11' RIGHT OF CENTER LINE HAS CORROSION AROUND 2 HI-LOCKS. COMPLIANCE FINDING MISSING MEASUREMENTS ; / [01] ADDED MEASUREMENTS.

Part: NONE — CRACKED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

FOUND INTERCOSTAL UPPER CHORD BELOW PANEL 231AF BETWEEN STA 380 AND 400 BL 0 CRACKED ; / [01] REMOVED INTERCOSTAL UPPER CHORD BELOW PANEL 231AF BETWEEN STA 380 AND 400 BL REF B-737-700 SRM-51-40-02-0G-A00729; [02] VERIFIED STEP 1 .<BR>OK TO INSTALL PART.; [03] LATE ENTRY: APPLIED EWIS PROTECTION AT WORK AREA UNDER FLOOR PANEL 231AF; AS PER B737-7 AMM 20-60-07-913-801.; [04] INSTALLED NEW CHORD ANGLE AT INTERCOSTAL STA. 380 - 400; BL 0; AS PER B737-7 SRM 51-40-02-0G-0; & DWG. 143A5400.; [05] REMOVED EWIS PROTECTION AT WORKED AREA; AS PER B737-7 AMM 20-60-07-913-801.; [06] VERIFIED STEPS 3-5; [07] VERIFIED STEPS 3-5

Part: BRACKET — ELONGATED (CENTER WING) · airframe 68,673 hrs · 40,726 cycles

LEFT MAIN WHEEL WELL FWD BULKHEAD VAPOR BARRIER UPPER SUPPORT BRACKET HOLE ELONGATED JUST O/B OF LBL 40.87 ; / [01] PERFORMED HFEC ROTO ON OPEN FASTENER HOLES ON UPPER SUPPORT BRACKET AT BS 663.75 LBL 40.85 (LEFT MAIN WHEEL WELL FWD BULKHEAD) EXCEPT ELONGATED HOLE; IAW NDTM PART 6;51-00-00 PROCEDURE 16. NO CRACKS.<BR>[NORTEC 600 ;B/C 166316; CALIB DUE-10/22]; [14] REPAIRED LH WW VAPOR BARRIER BRACKET HOLE PER EA 21-157-03204; [15] VERIFIED STEPS 12-14. TASK C/W; [16] VERIFIED STEPS 12-14. TASK C/W

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

CABIN FLOOR PANEL 221GF FWD O/B TIP BROKEN ; / [01] REPLACED FLOOR PANEL 221GF INSTALLATION WILL BE ACCOMPLISHED ON T/C TTG8Q006A9GZ; [02] VERIFIED STEP #1

Part: MEGAPHONE — BROKEN (FWD CABIN) · airframe 68,673 hrs · 40,726 cycles

SUPPLEMENTAL INFORMATION: MEGAPHONE LOCATED AT L1 WINDSCREEN HAS HANDLE BROKEN ; / [01] REMOVED AND REPLACED MEGAPHONE LOCATED AT L1 WINDSCREEN AS PER DWG: 25600001.; [02] VERIFIED STEP 1

Part: BUSHING — CORRODED (L/H HORIZ. STAB.) · airframe 68,673 hrs · 40,726 cycles

LT HORIZONTAL STABILIZER AFT LOWER BUSHING SHOWS SIGNS OF PITTING CORROSION ; / [01] ISSUED SUMMARY EA 21-155-03095; [02] ALL WORK REPLATED TO THIS DISCREPANCY WAS ACCOMPLISHED ON EA 21-155-03095 WIP 1; 21-155-03095 WIP 2 AND EA 21-155-03095 WIP 3; [03] 21-155-03095-WIP1; 21-155-03095-WIP2 AND 21-155-03095-WIP3 ARE COMPLETED AND SIGNED OFF.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 68,673 hrs · 40,726 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPARTMENT DOOR CUTOUT LOWER SILL FWD SCUFF PLATE CRACKED @ EDGE MKD DOT ; / [01] LOCATED AND DRILLED NEW FWD CARGO COMPARTMENT DOOR CUTOUT LOWER DOOR SILL FWD SCUFF PLATE PER B737-700 SRM 51-40-05-0G-0 AND SRM 51-40-08-0G-0; [02] VERIFIED STEP 1

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 68,673 hrs · 40,726 cycles

L/H HORIZ STAB L/E PANEL 331B 4 RIB FROM I/B CRACKED. PERFORMED HFEC INSP ON LH HORIZ STAB L/E PANEL 331B 4 RIB IAW NDT P6 51-00-00 PROC.23. CRACK CONFIRMED. REMOVED DAMAGE RIB IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW RIB IAW SRM 51-40-05-0G-0. INSTALLED THE NEW RIB IAW SRM 51-40-02-0G-0.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPT R/H STR 18 STA 500D GUSSET CRACKED ; / [01] FWD CARGO COMP REMOVED GUSSET R/H STR 18 STA 500D REF 51-40-02-0G-0-A00729; [02] REMOVED AND REPLACED GUSSET.AS PER B-737-700 DRAWING 143A9481-5 AT R/H STR 18 STA 500D; [03] REPLACED GUSSET AT FWD CARGO COMP STR 18R STA 500D PER DWG 143A9481; [04] VERIFIED STEPS # 1;2 AND 3.

Part: NONE — CRACKED (CENTER WING) · airframe 68,673 hrs · 40,726 cycles

SUPPLEMENTAL INFORMATION: MAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED @ LBL-1 STA 540 MKD DOT ; / [01] REMOVED MAIN CABIN CENTER WING FLOOR SUPPORT BRACKET LBL-1 STA 540. IAW B 737-7 SRM 51-40-02.; [02] LOCATED AND DRILLED NEW FLOOR SUPPORT . IAW B 737-7 SRM 51-40-05.; [03] VERIFIED STEPS 1 AND 2.; [04] OK TO INSTALL BREAK ASSY; [05] REMOVED AND INSTALLED NEW BREAK ASSY AT MAIN CABIN CENTER WING LBL-1 STA 540 REF B 737-7 SRM 51-40-02 AND DWG #134A5240; [06] VERIFIED STEP 5; [07] VERIFIED STEP 5

Part: SHIELD — CORRODED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPT R/H STR 25 BETWEEN STA 480 AND STA 500 SHIELD UPPER SURFACE CORROSION ; / [01] REMOVED CORROSION AT FWD CARGO COMPT R/H STR 25 BETWEEN STA 480 AND STA 500 SHIELD UPPER SURFACE FOUND OUT OF LIMITS (EXFOLIATION) I.A.W B737-700 SRM 51-10-02 AND SRM 53-30-53; [02] SHIELD P/N: 143A8126-31 WAS REMOVED & WILL BE INSTALLED ON FWD. CARGO COMPT. CPCP MOC CARD #5330-E-16461-NG. BARCODE: TTG8Q004EBR4.; [03] RECEIVED NEW SHIELD P/N: 143A8126-31; PO#1728471.ISSUED TAG WN7103.; [04] VERIFIED STEPS 1-3

Part: NONE — CORRODED (R1 DOOR) · airframe 68,673 hrs · 40,726 cycles

SUPPLEMENTAL INFORMATION: MAIN CABIN RIGHT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK ASSEMBLY CORRODED ; / [01] REMOVED AND REPLACED MAIN CABIN RT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK ASSEMBLY DUE TP CORROSION AS PER B737-700 AMM 25-61-10-400-802.; [02] THIS CORROSION IS NOT AT A STRUCTURAL ITEM. THE PART WAS REPLACED.; [03] VERIFIED STEPS 1 AND 2

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 68,673 hrs · 40,726 cycles

L/H HORIZ STAB L/E PANEL 331B #3 RIB FROM I/B CRACKED (AS MARKED) ; / [01] PERFORMED HFEC INSP ON LH HORIZ STAB L/E PANEL 331B #3 RIB IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 07/22; [02] REMOVED AND REPLACED L/H HORIZONTAL STAB L/E PANEL 331B #3 RIB REF B 737 SRM 51-40-02. WORK WAS ACCOMPLISHED BY TECHNICIAN RAFAEL MERLANO EMPL # 15961; [03] STEP 2 VERIFIED; [04] STEP 2 VERIFIED

Part: ANGLE — CRACKED (R/H HORIZ. STAB.) · airframe 68,673 hrs · 40,726 cycles

RT HORIZONTAL STAB STA 120.30 INSPAR RIB 4 #3 STIFFNER CRACKED AT LOWER EDGE ; / [01] REMOVED EXISTING REPAIR;ACCOMPLISH .040 INSURANCE CUT;FINAL DIMENSIONS OF CUTOUT 2.8 ' PER .600 '.<BR>WORKED PERFORMED BY EMP # 16894; [20] INSTALLED REPAIR PARTS; # 2 AND # 4 ANGLES;# 3 FILLER;# 5 AND # 6 SHIMS PER EA 21-155-03221 AND 737-700 SRM 51-20-05;51-40-02 AND SOPM 20-50-19; [21] STEP 20 VERIFIED; [22] ISSUED SUMMARY EA 21-155-03221.; [23] REPAIR ACCOMPLISHED PER EA 21-155-03221; [24] MEASUREMENTS ONLY; [25] VERIFIED STEP 23 & 24

Part: STRIP — CORRODED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

AFT CAROGO COMPARTMENT FLOOR LT SIDE CAP STRIP BS 767 HAS EVIDENCE OF CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREAS IAW NDT P4 51-00-00 PROC.3; MIN THK. NOTED 0.052'. INSTALLATION ACCOMPLISHED ON TASK CARD TTG8Q004GEP8.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPT L/H UNDER ZEE CHANNEL STA 500B BRACKET CRACKED ; / [01] FWD CARGO COMPT L/H UNDER ZEE CHANNEL STA 500 B REMOVED BRAKET REF 51-40-02-0G-A00729; [02] VERIFIED STEP 1; [03] OK TO INSTALL SERVICEABLE CLIP.; [04] INSTALLED NEW CLIP P/N 143A7502-13;PO# 1740025;AT FWD. CARGO COMPT. STA. 500B; LBL 21; AS PER B737-7 SRM 51-40-02-0G-0; & DWG. 143A7505.; [05] VERIFIED STEP 4

Part: NONE — CORRODED (L1 DOOR) · airframe 68,673 hrs · 40,726 cycles

SUPPLEMENTAL INFORMATION: MAIN CABIN LEFT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK ASSY CORRODED ; / [01] REMOVED AND REPLACED MAIN CABIN LEFT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK ASSY AS PER B737-700 AMM 25-61-10-000-802/25-61-10-400-802.; [02] PARTS REQUIREMENTS ONLY; [03] VERIFIED STEPS 1 AND 2

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

FWD CARGO COMPT L/H STR 25 BETWEEN STA 500 AND STA 500A INTERCOSTAL CRACKED ; / [01] FWD CARGO COMPT REMOVED INTERCOSTAL L/H STR 25 BETWEEN STA 500 AND 500A REF SRM-51-40-02-0G-A00729; [02] VERIFIED STEP 1; [03] OK TO INSTALL SERVICEABLE CLIP.; [04] INSTALLED NEW INTERCOSTAL/BAFFLE P/N:143A7510-15;PO#1684224;AT FWD CARGO COMPT. BETWEEN STA. 500 & 500A;LBL 21;AS PER B737-7 SRM 51-40-02-0G-0 & DWG. 143A775100.; [05] VERIFIED STEP 4

Part: STRIP — CORRODED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE RT CAP STRIP BETWEEN BS 727D-747 HAS EVIDENCE OF CORROSION. REMOVED CORROSION IAW SRM51-10-02-0G-0. PERFORMED UT THICKNESS INSP ON REWORKED AREAS IAW NDT P4 51-00-00 PROC.3; MIN THK. NOTED 0.051'. CAPSTRIP FOUND TO BE OUT OF LIMITS IAW SRM 51-40-02-0G-0. INSTALLATION ACCOMPLISHED ON TASK CARD TTG8Q004GEP8.

Part: NONE — CRACKED (CENTER WING) · airframe 68,673 hrs · 40,726 cycles

MAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED @ FASTENER TAIL RBL-1 ; STA 540 MKD DOT ; / [01] REMOVED MAIN CABIN CENTER WING FLOOR SUPPORT BRACKET RBL-1 STA 540. IAW B 737-7 SRM 51-40-02.; [02] LOCATED AND DRILLED NEW FLOOR SUPPORT. IAW B 737-7 SRM 51-40-05.; [03] VERIFIED STEPS 1 AND 2.; [04] OK TO INSTALL BREAK ASSY; [05] REMOVED AND INSTALLED NEW BREAK ASSY AT MAIN CABIN CENTER WING RBL-1 STA 540 REF B 737-7 SRM 51-40-02 AND DWG #143A5240; [06] VERIFIED STEP 5; [07] VERIFIED STEP 5

Part: BRACKET — CRACKED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPT R/H UNDER ZEE CHANNEL STA 500C BRACKET CRACKED ; / [01] FWD CARGO COMPT REMOVED BRAKET R/H UNDER ZEE CHANEL STA 500C REF 51-40-02-0G-A00729; [02] VERIFIED STEP 1; [03] OK TO INSTALL SERVICEABLE CLIP.; [04] INSTALLED NEW CLIP P/N : 143A7502-13; AT FWD CARGO COMPT. STA. 500C;RBL 21;AS PER B737-7 SRM 51-40-02-0G-0; & DWG. 143A7505.; [05] VERIFIED STEP 4

Part: GUSSET — CRACKED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPT L/H STR 18 STA 500D GUSSET CRACKED ; / [01] FWD CARGO COMP REMOVED GUSSET L/H STR 18 STA 500D REF SRM 51-40-02-0G-0-A00729; [02] REMOVED AND REPLACED GUSSET. AS PER B737-700 DRAWING 143A9481-6 AT L/H STR 18 STA 500 D.; [03] REPLACED GUSSET AT FWD CARGO COMP STA 500D STR 18L PER DWG 143A9481; [04] VERIFIED STEPS # 1;2 AND 3.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO COMPT L/H STA 500A UNDER ZEE CHANNEL BRACKET APPEARED CRACKED ; / [01] FWD CARGO COMPT REMOVED L/H STA 500 A UNDER ZEE CHANNEL BRACKET REF 51-40-02-0G-0-A00729; [02] VERIFIED STEP 1; [03] OK TO INSTALL SERVICEABLE BRACKET.; [04] INSTALLED NEW CLIP P/N:143A7502-13;PO#1740025;AT FWD. CARGO COMPT. L/H STA. 500A;LBL 21. AS PER B737-7 SRM 51-40-02-0G-0 & DWG.143A7505.; [05] VERIFIED STEP 4

Part: BEAM — CRACKED (R1 DOOR) · airframe 68,673 hrs · 40,726 cycles

CRACK FOUND AT PERIMETER OF I/B FASTENER HOLE OF 141A6536-14 BEAM #4 OF FWD SERVICE DOOR.CRACK LENGTH : 0.866'. REMOVED BRACKETS ASSEMBLY FWD AND AFT; BACKPLATES FWD & AFT, PARTIALLY REMOVED (LOWER INTERNAL SKIN) FOR ACCESS IAW SRM 51-40-02-0G-0, & DWG 141A6535. REMOVED BEAM #4 AT FORWARD GALLEY DOOR IAW SRM 51-40-02-0G-0 & DWG 141A6535. LOCATED & DRILLED NEW BEAM #4 AT R1 DOOR IAW SRM 51-40-02-0G-0 & DWG 141A6535. INSTALLED BEAM IAW SRM 51-40-02-0G-0 AND DWG 141A6516 REV B. REINSTALLED BRACKETS ASSEMBLY FWD AND AFT; BACKPLATES FWD AND AFT; AND (LOWER INTERNAL SKIN) IAW SRM 51-40-02-0G-0;AND DWG 141A6535. REPLACEMENT OF R-1 FWD SERVICE DOOR #4 BEAM WAS ACCOMPLISHED AT CARD : 5241-C-14093-NG.

Part: CHANNEL — CORRODED · airframe 68,673 hrs · 40,726 cycles

LEFT SIDE ZEE CHANNEL IS CORRODED AT 727B - 847. REMOVED CORROSION IAW SRM 51-10-020G-0. FOUND OUT OF LIMITS IAW SRM 53-00-53. FABRICATED A NEW CHANNEL IAW DWG 146A7502 AND SRM 53-00-53-2R-6. TREATED AND PRIMED IAW AMM 51-21-41-370-803, & 51-21-72-370-804. PAINTED AND INSTALLED.

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

R1 DOOR BEAR STRAP BS 290 - 296, S8 - 9R, FOUND A CRACK INDICATION FROM FASTENER HOLE FWD OF FITTING LATCH. CRACK LENGTH=1.772'. STARTED REMOVING FASTENERS COMMON TO REPAIR. PERFORMED HFEC ON CUTOUT AREA. IAW NDT PART 6 51-00-00 PROCE 23. NO CRACKS FOUND. HFEC ROTO ON FASTENERS OPEN HOLES IAW NDT PART 651-00-00 PROCE 16. NO CRACKS FOUND. HFEC COUNTERSINKS OPEN HOLES IAW NDT PART 6 53-30-00 PROCE 3. NO CRACKS FOUND. COMPLETED REMOVAL OF FASTENERS COMMON TO REPAIR IAW SRM 51-40-02-0G-0 & 53-10-01-2R-6. CUT-OUT DAMAGED IAW SRM 53-10-01-2R-6. REMOVED SEAL DEPRESSOR 51-40-02-0G-0, COMPLETED FABRICATION OF REPAIRDOUBLER, TRIPLER FILLER AND TAPER SHIMS PER B737SRM53-10-01-2R-6.

Part: NONE — CRACKED (L/H WING) · airframe 68,673 hrs · 40,726 cycles

L/W T/E UNDER DEFLECTION PANEL O/B BRACKET CRACKED ; / [01] REMOVED AND REPLACED BRACKET CLIP AT L/W T/E O/B UNDER DEFLECTION PANEL REF B737-700 SRM 51-40-02; [02] VERIFIED STEP # 1.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

CORROSION LOCATED AT APPROX. 6 O'CLOCK POS. STA. 1016 JUST FWD OF DRAINS. 1] CLEANED AREA IAW SRM 51-10-02-0G-0. FOUND UPPER SPLICE ANGLE WITH EXFOLIATING CORROSION OUT OF LIMITS. REMOVED FWD SPLICE ANGLE IAW SRM 51-40-02, FABRICATED SPLICE ANGLE IAW DWG 148A2216. LOCATED AND DRILLED NEW SPLICE ANGLE IAW SRM 51-40-05-0G-0.

Part: WEB — CRACKED (CENTER WING) · airframe 68,673 hrs · 40,726 cycles

CTR. WING REAR SPAR STA. 663; BWL 160;L/H LWR. GFRP WEB IS CRACKED BETWEEN LBL45.64 & LBL54.21. ; / [01] PREPARED PANEL (VAPOR BARRIER) FOR DRY PROCESS AS PER BOEING 737 SRM 51-70-04-2R-10; [02] VERIFIED STEP 1; [03] ACOMPLISHED DRY PROCESS (24 HRS) ON VAPOR BARRIER L/H AS PER BOEING 737 SRM 51-70-04-2R-0; [04] VERIFIED STEP 3; [05] OK TO INSTALL REPAIR; [06] REPAIRED DAMAGE AREA AT VAPOR BARRIER L/H AS PER BOEING 737 SRM 51-70-04-2R-10 REPAIR 10. MATERIAL USED EY3804 PO#1731939 PLUS HCS2410-030 PO#1150387.; [07] VERIFIED STEP 6; [08] MEASUREMENTS; [09] PREPPED AND APPLIED TPCOAT ON L/H GFRP WEB REF B 737-700 AMM 51-21-72-370-804 .

Part: WEB — CRACKED (CENTER WING) · airframe 68,673 hrs · 40,726 cycles

SUPPLEMENTAL INFORMATION: CTR. WING REAR SPAR STA. 663; BWL 160;R/H LWR. GFRP WEB IS CRACKED BETWEEN RBL25.00 & RBL31.83. / FOUND PERMANENT METAL REPAIR AT FWD. FACE OF CTR. WING REAR SPER STA. 663 BWL 160 - 168R/H LWR. GFRP WEBRBL 25 & RBL 31.83. APPLIED SEALANT & ALUMINUM FOIL AT THE AFT FACE OF R/H LOWER GFRP WEB TO PROTECT AREA AS PER B737-7 SRM 57-10-10-1A-2PARA. 2C(3). VERIFIED STEPS 1 AND 2 VERIFIED STEPS 1 AND 2

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 68,673 hrs · 40,726 cycles

FWD FUSELAGE R/H EXTERNAL POWER COMPARTMENT CUTOUT AFT EDGE REPAIR DOUBLER CRACKED. REMOVED EXISTING DOUBLER FILLER REPAIR AT EGPR DOOR CUTOUT IAW SRM 53-10-15-2R-5. FABRICATED NEW DOUBLER FILLER AT EGPR IAW SRM 51-10-15-2R-5. TREATED AND PRIMED NEW DOUBLER FILLER IAW AMM 51-21-41-370-802, AND AMM 51-21-72-370-804. INSTALLED NEW DOUBLER FILLER ON EGPR DOOR CUTOUT IAW SRM 53-10-15-2R-5. THIS REPAIR IS A CATEGORY 'B' REPAIR IAW SRM 53-10-15-2R-5 REPAIR 5 PARA. 5.A.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 68,301 hrs · 40,504 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. / R&R BATTERY PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 68,301 hrs · 40,504 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. / R&R BATTERY PER MM.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG BORE CORRODED. / REPAIRED LUG PER SRM.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG BORE CORRODED. / REPAIRED LUG PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG BORE CORRODED. / REPAIRED LUG PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,131 hrs · 39,739 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD BUSHING HAT FACE CORRODED. / REPAIRED FACE PER SRM.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG BORE CORRODED. / REPAIRED LUG PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD LUG BORE CORRODED. / REPAIRED LUG PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 67,131 hrs · 39,739 cycles

R/H OUTBOARD AFT FLAP UPPER SKIN DELAMINATED ON INBOARD END. R&R R/H OUTBOARD AFT FLAP PER MM.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,131 hrs · 39,739 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD BUSHING HAT FACE CORRODED. / REPAIRED LUG BORE PER SRM.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG BORE CORRODED. / REPAIRED LUG PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG BORE CORRODED. / REPAIRED LUG PER EA.

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG BORE CORRODED. / REPAIRED LUG PER EA.

Part: FITTING — CORRODED (WHEEL WELL RH) · airframe 67,131 hrs · 39,739 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING LOWER I/B BUSHING HAT FACE CORRODED / REPAIRED PER SRM 57-20-90-2R-2

Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,131 hrs · 39,739 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER OUTBOARD LUG FACE CORRODED. / REPAIRED LUG FACE PER EA.

Part: MOUNT — BROKEN (EXIT LIGHT) · airframe 66,292 hrs · 39,199 cycles

EXIT LIGHT LENS MOUNT BROKEN. R&R EMERGENCY EXIT LIGHT IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 66,257 hrs · 39,174 cycles

LT WING OUTBOARD AFT FLAP LOWER SURFACE DELAMINATED AREAS AT THE INBOARD END OF FLAP. R&R AFT FLAP PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 66,257 hrs · 39,174 cycles

L/H WING OUTBOARD AFT FLAP UPPER SURFACE HAD DELAMINATED AREAS AT THE INBOARD END OF THE FLAP. / REPAIRED AFT FLAP PER EA.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 66,250 hrs · 39,169 cycles

L/H WING OUTBOARD AFT FLAP UPPER SURFACE HAD TWO DELAMINATED AREAS AT THE INBOARD END OF FLAP. REPAIRED AFT FLAP PER EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,223 hrs · 39,149 cycles

R/H AISLE EMERGENCY LIGHTS INOP OVER ROWS 3 TO ROW 5. R&R BATTERY PACK M1674 AMM.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 65,821 hrs · 38,901 cycles

193 B. PANEL EROSION OF CORNER LOCATION (8) (MARKED). ALOO HAS HOLE IN PANEL SURFACE NOT CONTINUING THRU JUST FWD OF FASTENER 34. HOLE IS APPROX .125 IN DIAMETER AND HAS LOCALIZED DELAMINATION ASSOCIATED WITH HOLE APPROX .250 INDIAMETER / REMOVED AND REPLACED PANEL 193B PER AMM 53-51-21

Part: WINDOW — ARCED (L1) · airframe 65,641 hrs · 38,785 cycles

COCKPIT L1 WINDOW ARCED. R&R L1 WINDOW IAW AMM.

Part: WINDOW — ARCED (L1) · airframe 65,641 hrs · 38,785 cycles

COCKPIT L1 WINDOW ARCED. R&R HEAT CONTROLLER IAW AMM.

Part: FLAP — DELAMINATED (RH OUTBD AFT FLA) · airframe 65,293 hrs · 38,555 cycles

R/H O/B TRAILING AFT FLAP DELAMINATED ON THE I/B TRAILING EDGE CORNER. 1.4 LENGTH INCH BY .7 UPPER AND LOWER SKIN. (ZONE 1) / SI 0270249 SN S0306 WAS REMOVED FROM AIRCRAFT AND REPLACED WITH SI 0270249 SN 000206. SN0306 IS CURRENTLY IN HOU SHOP RO# 0270249-BIR JOB ORDER J10625606. (SA-M 735/LELAND SYKES)

Part: LENS — MISSING (CABIN) · airframe 64,980 hrs · 38,349 cycles

AFT OVER WING EXIT LENS COVER MISSING. INSTALLED LENS IAW SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,466 hrs · 37,367 cycles

FORWARD EMERGENCY EXIT LIGHTS INOP AT LOCATION M1674. R&R BATTERY PACK PER AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED ACB FWD CORNER SCUFF PLATE PER EA 1-A53-2076 REV. 11.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 63,466 hrs · 37,367 cycles

FWD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED FWD CARGO BAY AFT CORNER SCUFF PLATE PER EA NO. 1-A53-8076 REV 11

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

VAPOR BARRIER SUPPORT ATTACH ANGLE CRACKED AT BS 663, LBL 54.21. R&R ANGLE IAW SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

SPLICE CORRODED AT BS 360, STR 28L. R&R SPLICE PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

LOWER FASTENER HOLE OF VERTICAL SUPPORT ANGLE CRACKED AT BS 662, RBL 27.5. R&R ANGLE IAW SRM AND DWG.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

BULKHEAD AROUND THE APU DUCT DOUBLER ASSEMBLY CRACKED AT BS 663. R&R DOUBLER ASSEMBLY IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (MLG WW) · airframe 63,466 hrs · 37,367 cycles

BS 663 VAPOR BARRIER ATTACHED ANGLE CRACKED LBL 6 TO LBL 31 / REMOVED ANGLE PER SRM 51-40-02. LOCATED AND DRILLED NEW ANGLE ITEM 7530146 PER SRM 51-40-05 AND DWG 111A1000. INSTALLED PER SRM 51-40-02 AND DWG 111A1000 88324U 13JUL18

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

FUSELAGE SHEAR TIE CRACKED AT STA 727D, STR 26L TO STR 27L. R&R SHEAR TIE PER SRM.

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

PANEL 193AR HAS A DELAMINATED AREA ON THE EXTERNAL SURFACE / REPAIRED DELAMINATED AREA ON EXTERNAL SURFACE OF PANEL 193AR IAW SRM 53-40-70-2R-1 AND SRM 51-70-05-2R-2

Part: BRACKET — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY ON LOWER VHF BRACKET CORRODED AT BS 727D+4, RBL 0. R&R BRACKET IAW SRM & DWG.

Part: FRAME — CORRODED (AFT CARGO BAY) · airframe 63,466 hrs · 37,367 cycles

***CORROSION*** ACB STA 947 FRAME HAS CORROSION AT LBL 9 / REMOVED CORROSION ON ACB BS 947 FRAME LBL 9; 5' X 1.2'; .005' MAX DEPTH; ORIGINAL THICKNESS .063'. OUT OF LIMITS PER SRM 53-00-07; ALLOWABLE DAMAGE 1; FIG 102; DETAIL C. REWORKED AREA PER ER 18-03331 REV IR AND EA 1-753-33002 REV IR

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY BULKHEAD TO FLOOR SUPPORT CORRODED AT BS 947, RBL 9. R&R ANGLE IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

STRINGER CLIP CORRODED AT STA 727E, STR 26L. R&R CLIP PER SRM.

Part: SUPPORT ANGLE — CORRODED (AFT CARGO BAY) · airframe 63,466 hrs · 37,367 cycles

***CORROSION*** R/H SIDEWALL BULKHEAD SUPPORT ANGLE 947 CORROSION AT RBL22. / REMOVED AND REPLACED RH SIDEWALL BULKHEAD SUPPORT ANGLE AT 947 STR 21R TO STR 25R PER SRM 51-40-02-0G- 0 AND DWG 149A817

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY ON 927 FRAME CORRODED AT BS 927, BETWEEN LBL 8 TO LBL 11. REPAIRED FRAME PER ER AND EA.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

PRESSURE BULKHEAD VAPOR BARRIER TEE CHORD CRACKED AT BS 663, RBL 27. REPAIRED TEE CHORD IAW EA AND ER.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

VAPOR BARRIER WING CENTER SECTION ATTACH ANGLE CRACKED AT BS 663, LBL 45. R&R ATTACH ANGLE PER SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

RT FLOORBEAM CRACKED AT BS 294. REPAIRED FLOORBEAM IAW ER AND EA.

Part: PANEL — DELAMINATED (LH PYLON) · airframe 63,466 hrs · 37,367 cycles

LT ENG ACCESS PANEL 431ER BURNT AND DISBONDED ON CORNER (MARKED) / INSTALLED SERVICEABLE PANEL 431 ER IAW AMM 54-53-01-400-801 STEP 3.H. AND 3.H.(7) 57315U 18JUL18

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

FUSELAGE SHEAR TIE CORRODED AT STA 807, STR 56L. R&R SHEAR TIE PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 26. R&R SUPPORT IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

FASTENER HOLE ON FLOORBEAM UPPER CHORD CRACKED AT BS 328, RBL 21.5. REPAIRED FLOOR BEAM PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

TAPERED STRAP CORRODED AT BS 793, RBL 20. R&R STRAP IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 480+10 TO BS 500D, LBL 26. R&R SUPPORT IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 440-1, RBL 26. R&R SUPPORT IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

STRINGER CLIP CORRODED AT STA 787, STR 26L. R&R CLIP PER SRM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

SHEAR WEB CORRODED BETWEEN BS 1006 TO BS 1016, LBL 45. R&R SHEAR WEB PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 47. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

FUSELAGE SHEAR TIE CORRODED AT STA 807, STR 26L TO STR 27L. R&R SHEAR TIE PER SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

FUSELAGE INTERCOSTAL CORRODED AT STA 727A TO STA 727B, LBL 3. R&R INTERCOSTAL PER SRM.

Part: NONE — CORRODED (AFT CARGO COMPT) · airframe 63,466 hrs · 37,367 cycles

***CORROSION*** AFT CARGO BAY 727D+4 INBOARD CLIP COMMON TO STR 27L (KEEL BEAM) HAS CORROSION / CORROSION ON ACB KEEL BEAM CLIP IB BS727+4 STR27L FOUND TO BE OUT OF LIMIT DUE TO NO SRM COVERAGE PARTS WILL BE REPAIRED AND REPLACED IAW SRM 51-10-02-0G-0 FABRICATED CLIP MADE FROM EXTRUSION 1988228 LOT# 1340111 IAW DOC #146A7730 SURFACE TREATED AND PRIMED IAW SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804 AND INSTALLED IAW SRM 51-40-02-0G-0 AND DOC# 146A7730

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

R1 DOOR MOP SILL UPPER SURFACE CORRODED BETWEEN BS 294 TO BS 335. R&R MOPSILL IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

STRINGER CLIP CORRODED AT STA 727D, STR 26L. R&R CLIP PER SRM.

Part: STRAP — CORRODED (CABIN) · airframe 63,466 hrs · 37,367 cycles

***CORROSION*** ON TENSION STRAP; UPPER SURFACE; B.S. 1016-1026; L.B.L. 3. / REMOVED AND REPLACED STRAP PN 147A5620U3 IAW SRM 51-40-02 AND DWG 174A5600 88324U 03JUL18

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 12. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

STRINGER CLIP CORRODED AT STA 767, STR 26L. R&R CLIP PER SRM.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,466 hrs · 37,367 cycles

CRACKED INTERCOSTAL AT B.S. 277-294; B.L. 0 W.L. 208.1. / REMOVED AND INSTALLED NEW INSTERCOSTAL ITEM# 141A5410U3AAR AT B.S 277-294; RLO WL 208.1 IAW SRM 51-40-02-0G-0; AND DWG# 141A5410

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

FORWARD ENTRY DOOR MOP SILL CORRODED BETWEEN BS 294 TO BS 344. R&R MOPSILL IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

STRINGER CLIP CORRODED AT STA 727E, STR 26R. R&R CLIP PER SRM.

Part: BEAM — CRACKED (RIGHT WING) · airframe 63,466 hrs · 37,367 cycles

RT WING LOWER T/E AFT PANEL SUPPORT BEAM COMMON TO PANEL 661AB IS CRACKED ON I/B END / REMOVED AND REPLACED RT WING LOWER T/E AFT PANEL SUPPORT BEAM COMMON TO PANEL 661AB IAW SRM 51-40-02-0G-0; BOEING DWG 115A3700 AND BOEING DWG 115A3758. 57865U 10JULY18

Part: FITTING — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY INBOARD AND OUTBOARD CLIPS CORRODED AT BS 727D, STR 27L. R&R CLIPS IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

STRINGER CLIP CORRODED AT STA 727D, STR 26R. R&R CLIP PER SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 63,466 hrs · 37,367 cycles

CORROSION ON B.S. 328 FLOOR BEAM (UPPER SURFACE) R.B.L. 37; BY FASTENER HOLE. / BS 328 FLOOR BEAM UPPER SURFACE RBL 37. REMOVED CORROSION 1.2' X 1.0' X 0.008'. IAW SRM 51-10-02. ORIGINAL THICKNESS 0.925'; REMAINING THICKNESS 0.117'. FOUND TO BE WITHIN LIMITS IAW SRM 53-10-51-1A-1. UPON INVESTIGATION. CRACK FOND AT FLOOR FLOOR BEAM BS 328 UPPER CHORD RBL 21.5. ACCOMPLISHED; FLOOR BEAM REPAIR UPPER CHORD BETWEEN RB 1.1 AND RBL 60 ON CC# T799656

Part: NONE — CORRODED (AFT CARGO COMPT) · airframe 63,466 hrs · 37,367 cycles

***CORROSION*** AFT CARGO BAY INBOARD AND OUTBOARD CLIPS COMMON TO STR 27L (KEEL BEAM) BS 727C HAVE CORROSION / CORROSION ON ACB FEEL BEAM CLIPS IB 4OB BS727 STR 27L FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR-9 FABRICATED NEW CLIPS 2(EA) LOCATED AND DRILLED MADE FROM BAC 1490-2815 LOT# 1205280 IAW DOC# 146A1320 APPLIED CHEMICAL CONVERSATION COATION AND PRIMED IAW AMM 51-21-41-370-802 AND 51-21-72-320-804 AND INSTALLED IAW DOC# 146A1320 AND SRM 51-40-02-0G-0

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

STRINGER CLIP CORRODED AT STA 747, STR 26L. R&R CLIP PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 47. R&R INTERCOSTAL IAW SRM & DWG.

Part: NONE — CORRODED (ASD THRESHOLD) · airframe 63,466 hrs · 37,367 cycles

***CORROSION*** ON AFT SERVICE DOOR MOP SILL; UPPER SURFACE; B.S. 947-997. / REMOVED AND REPLACED AFT SERVICE DOOR MOP SILL IAW SRM 51-40-02 AND DWG 147A8540 88324U 03JUL18

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

SHEAR WEB CORRODED BETWEEN BS 986 TO BS 1006, RBL 45. R&R SHEAR WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FWD CARGO LH) · airframe 63,466 hrs · 37,367 cycles

***CORROSION*** ON FWD CARGO AFT BULKHEAD LWR SUPPORT STA 500D; LBL 0 TO LBL 26; WL 158. / REMOVED AND REPLACED FWD CARGO AFT BULKHEAD LWR SUPPORT STA 500D WITH ITEM #7530142 IAW SRM 51-40-02-0G-0 AND AIPC 53-11-01-43

Part: BEAM — CORRODED (CABIN) · airframe 63,466 hrs · 37,367 cycles

***CORROSION*** ON B.S. 986 FLOOR BEAM; UPPER SURFACE; L.B.L. 50 - R.B.L. 50; W.L. 208.1. / REPAIRED FLOOR BEAM BS 986 PER SRM 53-70-51-2R-4 REPAIR 4

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 35. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FITTING — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY INBOARD AND OUTBOARD CLIPS CORRODED AT BS 727E, STR 27L. R&R CLIPS IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

STRINGER CLIP CORRODED AT STA 727C, STR 26L. R&R CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

FUSELAGE RT STUB FRAME CRACKED AT STA 294, WL 209. REPAIRED FRAME PER EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY OUTBOARD CLIP CORRODED AT BS 787, STR 27L. R&R CLIP IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 1. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

FUSELAGE INTERCOSTAL CORRODED AT STA 727A TO STA 727B, LBL 17. R&R INTERCOSTAL PER SRM.

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

FWD CABIN FLOOR PANEL 221BF AFT O/B CORNER IS BROKEN AND HAS DAMAGED INSERTS / REMOVED AND REPLACED ALL DAMAGED INSERTS AND REPAIRED AFT O/B CORNER ON FWD CABIN FLOOR PANEL 221BF IAW SRM 53-00-50-2R-6. 57066U 7/2/18

Part: STRAP — CORRODED (CABIN) · airframe 63,466 hrs · 37,367 cycles

***CORROSION*** ON TENSION STRAP; UPPER SURFACE; B.S. 1016-1026; R.B.L. 3. / REMOVED AND REPLACED STRAP PN 147A5744-1 IAW SRM 51-40-02 AND DWG 147A5730 88324U 03JUL18

Part: WEB — CORRODED (FWD CARGO THRESH) · airframe 63,466 hrs · 37,367 cycles

***CORROSION*** ON FWD CARGO BAY DOOR SURROUND SUB THRESHOLD; NUMEROUS AREAS; STA 440 TO 500;RBL 28 TO RBL 35; WL 158. / FWD CARGO BAY DOOR SURROUND SUB THRESHOLD WEB CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1; BLEND WAS 2' X 1' X .020'; ORIGINAL THICKNESS WAS .45' IAW SRM 53-30-15-1A-1. REMOVED AND REPLACED SUB THRESHOLD WEB IAW DRAWING 143A8330 & SRM 51-40-2

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY SHIELD AFT OF CARGO DOOR CORRODED ON UPPER SURFACE, BETWEEN BS 847 TO BS 867. R&R SHIELD IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 20. R&R SUPPORT IAW SRM AND DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY FLOOR SPLICE CORRODED AT BS 887. R&R SPLICE IAW SRM AND DWG.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 63,466 hrs · 37,367 cycles

***CORROSION*** AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT HAS CORROSION ON UPPER SURFACE BS 920-947 / REMOVED DAMAGE FROM ACB R/H FLOOR TO SIDEWALL SUPPORT BETWEEN B920-BS947 AREA L=2'; W=1.1' REMAINING THICKNESS 0.033' ORIGINAL THICKNESS 0.040'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED; FABRICATED AND INSTALLED NEW R/H FLOOR SIDEWALL SUPPORT AT ACB BS867-BS947 IAW SRM 51-40-02-0G-0 DWG 146A7500; DWG 147A7500 AND DWG 147A9409

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY FLOOR SUPPORT TRACK CORRODED AT BS 934, RBL 14. R&R TRACK IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

INTERCOSTAL CORRODED AT STA 847 TO STA867, STR 25L TO STR 26L. R&R INTERCOSTAL PER SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

STRINGER CLIP CORRODED AT STA 827, STR 27L. R&R CLIP PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LT ON UPPER SURFACE. R&R SUPPORT IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

FUSELAGE SHEAR TIE CORRODED AT STA 907, STR 26L TO STR 27L. R&R SHEAR TIE PER SRM.

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 63,466 hrs · 37,367 cycles

CRACK LOCATED ON PANEL 195CR AFT CORNER. / REPAIRED CRACK ON PANEL 195CR AT AFT CORNER IAW SRM 53-40-70-2R-1 SRM 53-40-70; SRM 51-70-05-2R-6 AND AMM 51-21-71

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY BUTT SPLICE INTERNAL DOUBLER CORRODED AT BS 887, STR 27L. REPAIRED DOUBLER IAW EA AND ER.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

STRINGER CLIP CORRODED AT STA 807, STR 26L. R&R CLIP PER SRM.

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 63,466 hrs · 37,367 cycles

***CORROSION*** ACB FLOOR PANEL 140CF IS CORRODED AROUND FASTENER HOLES / FABRICATED NEW ACB PANEL 140CF USING 2024T3 .071 LOT# 1348622-1 AND TREATED IAW BOEING DWG# 453A12610 AND AMM 25-52-01-201-801 OK TO PRIME 56333C 29JUN18 INSP 86 29JUN18 APPLIED PRIMER PER AMM # 51-21-72-370-804. 57609U 12JUL18

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 63,466 hrs · 37,367 cycles

VAPOR BARRIER CRACKED AT BS 663, LBL 10. REPAIRED BARRIER IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY FLOOR SUPPORT TRACK CORRODED AT BS 793, RBL 14. R&R TRACK IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY FRAME CORRODED AT BS 907, STR 27L. REPAIRED FRAME IAW EA AND ER.

Part: VAPOR BARRIER — CRACKED (WHEEL WELL RH) · airframe 63,466 hrs · 37,367 cycles

VAPOR BARRIER IS CRACKED AT B.S. 663; R.B.L. 25. / REPAIRED B.S. 663 VAPOR BARRIER IAW SRM 57-10-10-2R-2

Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 63,466 hrs · 37,367 cycles

***CORROSION*** AFT CARGO BAY SUB THRESHOLD WEB HAS CORROSION / REMOVED AND REPLACED AFT CARGO BAY SUB THRESHOLD WEB IAW SRM 51-40-02 AND BOEING DWG 146A8340 SH. 9.

Part: FITTING — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY CLIP CORRODED AT BS 807, STR 27L. R&R CLIP PER SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY FORWARD OF CARGO DOOR SHIELD CORRODED BETWEEN BS 768 TO BS 794. R&R SHIELD IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY FRAME CORRODED AT BS 787, BETWEEN RBL 14 TO RBL 17. REPAIRED FRAME IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

AFT CARGO BAY FRAME CORRODED AT BS 807, STR 27L. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 63,466 hrs · 37,367 cycles

STRINGER CLIP CORRODED AT STA 847, STR 27L. R&R CLIP PER SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,466 hrs · 37,367 cycles

LT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED ON THE INTERIOR SIDE AT BS 663, LBL 27. REPAIRED WEB PER ER AND EA.

Part: FAIRING — DAMAGED (RT WING FLAP) · airframe 62,413 hrs · 36,707 cycles

SUPPLEMENTAL INFORMATION: #6 FLAP FAIRING SEAL FASTENER HOLE ELONGATED / PERFORMED INTERIM REPAIR PER SRM 57-53-70-2R-2 ALTERNATIVE 1; REQUIRES DVI OF INTERIM REPAIR EVERY 500 FLIGHT CYCLES. IF DAMAGED IS FOUND REPAIR MUST BE PERMANENTLY REPAIRED

Part: PLATE — CRACKED (LT WING) · airframe 62,325 hrs · 36,650 cycles

LEFT WING LOWER TRAILING EDGE SHELF PANEL 551GB FORWARD SUPPORT BRACKET WIGGLE PLATE CRACKED. R & R THE WIGGLE PLATE IAW SRM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 62,325 hrs · 36,650 cycles

LEFT WING OUTBOARD AFT FLAP DELAMINATED. R & R THE AFT FLAP IAW AMM.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 61,947 hrs · 36,408 cycles

RIGHT WING OUTBOARD NR 12 GROUND SPOILER ACTUATOR LEAKING. R & R THE ACTUATOR IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 60,290 hrs · 35,357 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 60,290 hrs · 35,357 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 60,290 hrs · 35,357 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R & R THE BATTERY IAW AMM.

Part: BRACKET — LOOSE (R1 GIRT BAR) · airframe 60,290 hrs · 35,357 cycles

R1 DOOR SLIDE GIRT BAR BRACKET LOOSE ON LT SIDE. SECURED THE BRACKET IAW SRM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 60,290 hrs · 35,357 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 60,290 hrs · 35,357 cycles

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

Part: RETAINER — CRACKED (VERTICAL STABILI) · airframe 60,290 hrs · 35,357 cycles

PANEL 323CL SKATE ANGLE RETAINER IS CRACKED / R&R PANEL 323CL SKATE ANGLE RETAINER PER SRM.51-40-02

Part: FLAP — DELAMINATED (LT WING) · airframe 58,578 hrs · 34,332 cycles

LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD AFT CORNER. REPAIRED AFT FLAP PER SRM.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 58,567 hrs · 34,326 cycles

L1 DOOR PHOTOLUMINESCENT LIGHT STRIP INOP. R&R STRIP PER AMM.

Part: FRAME — CRACKED (BS 907) · airframe 56,906 hrs · 33,372 cycles

FRAME CRACKED AT BS 907, BETWEEN STRINGERS 8 - 9L. REPAIRED THE FRAME IAW EA.

Part: WEB — CRACKED (FAIRING) · airframe 56,906 hrs · 33,372 cycles

LT WHEEL WELL AFT OUTBOARD WING TO BODY FILLET FAIRING UPPER AND LOWER CHORD WEB CRACKED. R&R WEB IAW DWG AND SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 56,906 hrs · 33,372 cycles

RIGHT HORIZONTAL STABILIZER RIB LOWER FLANGE CRACKED ON OTBD SIDE AT RIB STA 120.30, 27.5" AFT FROM FWD SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 56,906 hrs · 33,372 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT BS 138.70, 17.5" AFT FROM FORWARD SPAR. REPAIRED THE RIB IAW EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 56,906 hrs · 33,372 cycles

RIGHT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT RIB STA 111.10, 37.0" AFT FROM FORWARD SPAR. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 56,906 hrs · 33,372 cycles

LEFT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT RIB STA 120.30, 26.5" AFT FROM FORWARD SPAR. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 56,906 hrs · 33,372 cycles

RIGHT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT RIB STA 111.10, 28.5" AFT FROM FORWARD SPAR. REPAIRED STIFFENER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,906 hrs · 33,372 cycles

FRAME CRACKED AT BS 400, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,906 hrs · 33,372 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,906 hrs · 33,372 cycles

FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,906 hrs · 33,372 cycles

FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,906 hrs · 33,372 cycles

FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,906 hrs · 33,372 cycles

FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,906 hrs · 33,372 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,906 hrs · 33,372 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,906 hrs · 33,372 cycles

FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,906 hrs · 33,372 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,906 hrs · 33,372 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,906 hrs · 33,372 cycles

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

Part: FRAME — CRACKED (BS 907) · airframe 56,906 hrs · 33,372 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,906 hrs · 33,372 cycles

FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (BS 540) · airframe 56,906 hrs · 33,372 cycles

FUSELAGE SKIN CRACKED AT BS 540, BETWEEN STRINGERS 22 - 23R. REPAIRED SKIN IAW EA.

Part: FAIRING — CRACKED (RT WING) · airframe 56,906 hrs · 33,372 cycles

RT WING TO BODY FAIRING 195CR T/E CRACKED. REPAIRED FAIRING IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,906 hrs · 33,372 cycles

RT WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 42. REPAIRED WEB IAW SRM.

Part: COVER — LOOSE (CABIN) · airframe 56,415 hrs · 33,083 cycles

LEFT EMER LIGHT COVER LOOSE AT ROW 1. SECURED COVER IAW SIP.

Part: LENS — LOOSE (CABIN) · airframe 55,377 hrs · 32,492 cycles

LEFT OVERWING EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: POST — CRACKED (FUSELAGE) · airframe 55,321 hrs · 32,459 cycles

R1 COCKPIT WINDOW FRAME POST CRACKED. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 55,321 hrs · 32,459 cycles

RIGHT NR 1 COCKPIT WINDOW POST FRAME CRACKED. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 55,321 hrs · 32,459 cycles

LEFT NR 3 COCKPIT WINDOW POST FRAME CRACKED. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 55,321 hrs · 32,459 cycles

LEFT NR 1 COCKPIT WINDOW POST FRAME CRACKED. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 55,321 hrs · 32,459 cycles

RIGHT NR 3 COCKPIT WINDOW POST FRAME CRACKED. REPAIRED POST IAW ACO.

Part: LENS — MISSING (EXIT SIGN) · airframe 53,919 hrs · 31,631 cycles

LEFT OVERWING LOWER EXIT SIGN COVER LENS MISSING. INSTALLED LENS IAW MM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 52,845 hrs · 31,013 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED SLIDE IAW MT.

Part: SIGN — LOOSE (CABIN) · airframe 51,856 hrs · 30,440 cycles

MID CABIN EMER EXIT S.

Part: SIGN — DETACHED (CABIN) · airframe 51,585 hrs · 30,289 cycles

CENTER AISLE EXIT SIGN ON DETACHED. SECURED SIGN IAW MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 51,554 hrs · 30,268 cycles

L2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 51,476 hrs · 30,226 cycles

L2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,424 hrs · 29,604 cycles

RIGHT WING NR 6 LE SLAT SKIN CRACKED AT STATION 202.45. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,424 hrs · 29,604 cycles

RIGHT WING NR 7 LE SLAT STATION 322.7, LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 49,924 hrs · 29,309 cycles

RIGHT OVERWING INTERIOR LOWER EMERGENCY LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 49,428 hrs · 29,022 cycles

LEFT OVERWING EMERGENCY EXIT SIGN BROKEN. R & R SIGN ASSEMBLY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 49,273 hrs · 28,933 cycles

FORWARD GALLEY EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,097 hrs · 27,623 cycles

LT EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY CHECK. R&R BATTERY PACK IAW MM & SSM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,097 hrs · 27,623 cycles

RT EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY CHECK. R&R BATTERY PACK IAW MM & SSM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 43,543 hrs · 25,435 cycles

RIGHT OVERWING FWD LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FUSE CHARGER IAW MM.

Part: STRINGER — CRACKED (LT WING) · airframe 43,543 hrs · 25,435 cycles

LEFT WING INBOARD LEADING EDGE, OUTBOARD AFT STRINGER CRACKED AT BS 222. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 43,543 hrs · 25,435 cycles

FLOORBEAM CRACKED AT BS 767+ 7, RBL 13.84. REPAIRED BEAM IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,543 hrs · 25,435 cycles

FRAME CRACKED AT BS 380, BETWEEN STR 8L AND STR 7L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,543 hrs · 25,435 cycles

FRAME WEB CRACKED AT STA 727, LBL 60. REPAIRED WEB IAW EA AND AAR EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,543 hrs · 25,435 cycles

FRAME CRACKED AT BS 480, BETWEEN STR 8L AND STR 9L. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,543 hrs · 25,435 cycles

STRINGER CLIP CRACKED AT BS 1006, STR 14R. REMOVED AND REPLACED CLIP IAW BOEING DWG & SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,543 hrs · 25,435 cycles

RIGHT HORIZONTAL STABILIZER, LOWER SIDE SKIN, INBOARD SIDE STA 129.50 CRACKED. REPAIRED SKIN IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,543 hrs · 25,435 cycles

L1 DOOR SURROUND CREASE BEAM BENEATH THRESHOLD CORRODED BETWEEN BS 315 TO BS 330. REMOVED AND REPLACED ANGLE IAW SRM & BOEING DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,543 hrs · 25,435 cycles

FRAME ANGLE CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,543 hrs · 25,435 cycles

AFT CARGO PIT RIGHT Z-ANGLE CORRODED BETWEEN BS 727D+5 TO BS 747. REMOVED AND REPLACED Z- ANGLE IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,543 hrs · 25,435 cycles

L2 DOOR CREASE BEAM CORRODED BETWEEN BS 986 TO 967. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,543 hrs · 25,435 cycles

R2 DOOR CREASE BEAM CORRODED BETWEEN BS 947 TO BS 993. REMOVED AND REPLACED BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,543 hrs · 25,435 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 46 TO LBL 46. REPAIRED "T" CAP PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,543 hrs · 25,435 cycles

RIGHT HORIZONTAL STABILIZER, LOWER SIDE SKIN, INBOARD SIDE STA 120.30 CRACKED. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 43,402 hrs · 25,353 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALL SLIDE IAW MT.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 42,870 hrs · 25,048 cycles

LT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT L/E STA 138.70. REPAIRED SKIN IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,250 hrs · 24,676 cycles

FORWARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FWD BATTERY PER M/M.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 40,115 hrs · 23,373 cycles

INFLIGHT SHUTDOWN / DECLARED EMERGENCY. NR 2 ENGINE QUIT AT FL 280 CLR AIR SHUDDER AND ROLL BACK. SECURED ENGINE AND EMERGENCY DECLARED. NO OIL PRESSURE EGT DECREASE N1 & N2 SPARKS VISIBLE AT TAIL PIPE. REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 39,581 hrs · 23,059 cycles

DURING SCHEDULED CV CHECK FOUND, L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 39,581 hrs · 23,059 cycles

DURING SCHEDULED CV CHECK FOUND, R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 39,581 hrs · 23,059 cycles

DURING SCHEDULED CV CHECK FOUND, L2 ESCAPE SLIDE HAS LOW PRESSURE, OUT OF GREEN BAND. REMOVED AND REPLACED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,004 hrs · 22,735 cycles

DURING SCHEDULED SPV CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHTS INOP. RELAMPED PER MM.

Part: LENS — DAMAGED (CABIN) · airframe 39,004 hrs · 22,735 cycles

DURING SCHEDULED SPV CHECK, FOUND ENTRY DOOR SLIDE EMERGENCY EXIT LIGHT LENS DAMAGED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,234 hrs · 25,253 cycles

SKIN CRACKED AT BS 1020, STR 16R. REPAIRED SKIN PER EA AND ER.

Part: LIGHT — MISSING (CABIN) · airframe 38,541 hrs · 22,440 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS MISSING AT ROW 9. INSTALLED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,435 hrs · 21,809 cycles

DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 36,817 hrs · 21,452 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT COCKPIT OUTBOARD AFT SEAT TRACK CORRODED ON LOWER SURFACE. REMOVED AND REPLACED SEAT TRACK PER MM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 36,817 hrs · 21,452 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT COCKPIT OUTBOARD FWD SEAT TRACK CORRODED ON LOWER SURFACE. REMOVED AND REPLACED SEAT TRACK PER MM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,817 hrs · 21,452 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 10. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,817 hrs · 21,452 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,817 hrs · 21,452 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 42. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,817 hrs · 21,452 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 33. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,817 hrs · 21,452 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 16. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,817 hrs · 21,452 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 16. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 36,817 hrs · 21,452 cycles

DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 33. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 34,789 hrs · 20,259 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 34,789 hrs · 20,259 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING CORRODED. REPAIRED FITTING PER EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 33,301 hrs · 19,317 cycles

L1 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: TRACK — WORN (CABIN) · airframe 31,834 hrs · 18,447 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK WORN AT ROW 9. REMOVED AND REPLACED EEPLS PER MM.

Part: TRACK — MISSING (CABIN) · airframe 31,834 hrs · 18,447 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK MISSING AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,834 hrs · 18,447 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP BETWEEN ROW 11 TO ROW 13. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 30,123 hrs · 17,370 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM ZEE ANGLE CORRODED AT BS 294 TO BS 338, RBL 56. REPAIRED ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,123 hrs · 17,370 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,123 hrs · 17,370 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 8 TO LBL 17. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,123 hrs · 17,370 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 43 TO RBL 36. REPAIRED UPPER CHORD PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,123 hrs · 17,370 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727D, RBL 8 TO LBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: CREASE BEAM — CORRODED (BS 294-338) · airframe 30,123 hrs · 17,370 cycles

DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CHORD CORRODED BETWEEN BS 294 AND BS 338, RBL 56. R&R CHORD PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 27,259 hrs · 15,612 cycles

DURING SCHEDULED HC2 CHECK, LEFT OVERWING CABIN EMERGENCY EXIT BATTERY PACK FAILS LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 27,259 hrs · 15,612 cycles

DURING SCHEDULED HC2 CHECK, LEFT FWD CABIN EMERGENCY EXIT BATTERY PACK FAILS LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 27,259 hrs · 15,612 cycles

DURING SCHEDULED HC2 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.50. REPAIRED SKIN PER SRM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 26,524 hrs · 15,158 cycles

DURING SCHEDULED MV1 CHECK, R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — BINDING (R1 DOOR) · airframe 22,602 hrs · 12,885 cycles

R1 DOOR EMERGECNY EVAC SLIDE BAR CATCHES WHEN OPENING. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,804 hrs · 10,706 cycles

DURING SCHEDULED 5Y CHECK, FOUND FUSELAGE SKIN CREASED AT BS 812, BETWEEN STR 27L AND STR 26R. REPAIRED SKIN PER SRM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,797 hrs · 10,700 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY LIGHT INOP AT ROW 13 DEF. RELAMPED LIGHT PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,797 hrs · 10,700 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 14,964 hrs · 8,550 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,240 hrs · 8,139 cycles

CREW REPORTS EEPLS FWD RED LIGHT INOP. REPAIRED EEPLS LIGHT PER MM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 13,847 hrs · 7,930 cycles

DURING SCHEDULED C4 CHECK, FOUND BS 1016 PRESS BULKHEAD BETWEEN STRINGERS 3L AND 4L, OIL CANNED. REPAIRED BULKHEAD WEB PER SRM.

Part: CLAMP — LOOSE (APU) · airframe 9,971 hrs · 5,788 cycles

CABIN WOULD ONLY DESCEND WITH BOTH A/C PACKS IN HIGH POSITION. FOUND CLAMP LOOSE OF APU DUCT AT BS 1016 PRESS BULKHEAD. SECURED CLAMP, NO LEAKS NOTED PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 9,039 hrs · 5,278 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11075-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB HARDWARE AND BUSHING AT NR 1 HINGE ATTACH POINT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,022 hrs · 5,267 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS FWD LIGHT INOP. RELAMPED PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 8,732 hrs · 5,107 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: LENS — MISSING (CABIN) · airframe 7,114 hrs · 4,197 cycles

DURING SCHEDULED A1 CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT MISSING LENS AND BULB. INSTALLED LENS AND BULB PER MM.