N466WN

Part: NONE — CRACKED (FUSELAGE) · airframe 58,901 hrs · 34,794 cycles

CRACK INNER CHORD LOCATED AT BS 294.5 AT RBL 50 AND WL 208.1 AT FWD GALLEY AREA ; 2021-577502 / [01] TOOL USED CALIPER P/N:500-197-30 S/N:A21143464 DUE DATE:16-OCT-22.; [02] REPLACED INNER CHORD LOC AT BS 294.5 AT RBL 50 AND WL 208.1 AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02 AND DWG #141A8310; SHEET 25 REV .; [03] CORRECTED STEP 2.<BR>REPLACED INNER CHORD LOC AT BS 294.5 AT RBL 50 AND WL 208.1 AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02 AND DWG #141A8310; SHEET 25 REV . ?SEE INDIVIDUAL SIGNOFF BELOW?.; [04] REPLACED INNER CHORD LOC AT BS 294.5 AT RBL 50 AND WL 208.1 AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02 AND DWG #141A8310; SHEET 25 REV .

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 58,898 hrs · 34,793 cycles

CUSTOMER REQUEST - DEBONDED EXISTING REPAIR ON OB AFT FLAP UPPER SURFACE IB END AT LT WING ; 2021-577481 / [01] TOOL USED; CALIPER PN: 500-197-30; SN: A18229508; DUE DATE: 29/SEP/22.; [02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18196119 DUE DATE 27/JAN/22.; [03] TOOL USED HOT BONDER P/N HCS9200B -AV S/N 18196126 DUE DATE 27 JAN 22; [04] REPAIRED OB AFT FLAP UPPER SURFACE IB END AT LT WING AS PER B737-700 SRM 57-53-01-2R-16 REPAIR 16 AND AND B737-700 SRM 51-70-10-2R-0 REPAIR GENERAL.SEE INDIVIDUAL SIGNOFFS BELOW.; [05] TASCK COMPLETED. RII COMPLETED.

Part: ANGLE — CRACKED (R/H WING) · airframe 58,901 hrs · 34,794 cycles

CRACK TRAILING EDGE SUPPORT ANGLE LOCATED ON ORSS 273 AT RT WING ; 2021-577400 / [01] REPLACED TRAILING EDGE SUPPORT ANGLE LOCATED ON ORSS 273 AT RT WING IAW SRM B737-700 51-10-02 ITEM 9 AND SRM B737-700 51-40-02; [02] TASK CARD COMPLETED

Part: WEB — CORRODED (R/H WING) · airframe 58,901 hrs · 34,794 cycles

CORROSION WEB LOCATED ON FUELING STATION INTERNAL AREA OF PANEL 621GB AT RT WING ; 2021-577424 / [01] REPLACED WEB LOCATED ON FUELING STATION INTERNAL AREA OF PANEL 621GB AT RT WING IAW B737-700 SRM 51-10-02 AND B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGNOFFS BELOW; [02] REPLACED WEB LOCATED ON FUELING STATION INTERNAL AREA OF PANEL 621GB AT RT WING IAW B737-700 SRM 51-10-02 AND B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGNOFFS BELOW

Part: PLATE — CRACKED (R/H WING) · airframe 58,901 hrs · 34,794 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 273 AT RT WING ; 2021-577402 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 273 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND DWG 115A2001; SH 29; REV -. SEE INDIVIDUAL SIGN-OFF BELOW.; [02] TASK CARD COMPLETE.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: BULKHEAD — CRACKED (AFT CARGO BAY) · airframe 58,901 hrs · 34,794 cycles

CUSTOMER REQUEST CRACK ON BULKHEAD ACCESS PANEL 142NWB AT AFT CARGO COMPARTMENT ; 2021-577432 / [01] EVALUATED BULKHEAD ACCESS PANEL 142NWB AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS TO REPAIR IAW B737-700 AMM 25- 52-00-200-806 PARA 6.D(3)(D); (4)(B). DAMAGE SIZE IS:1.50? IN DIAMETER; AND REPAIRED IAW B737-700 AMM 25-52-01-300-805 PARA 4.F TOOL USED CALIPER P/N: 700-113-10; S/N: 0019289; DUE DATE: 30-SEP-22.; [02] EVALUATED BULKHEAD ACCESS PANEL 142NWB AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS TO REPAIR IAW B737-700 AMM 25- 52-00-200-806 PARA 6.D(3)(D); (4)(B). DAMAGE SIZE IS:1.50? IN DIAMETER; AND REPAIRED IAW B737-700 AMM 25-52-01-300-805 PARA 4.F TOOL USED CALIPER P/N: 700-113-10; S/N: 0019289;

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 58,901 hrs · 34,794 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS 400 AND BS 420 STRINGER 25L FWD CARGO COMPARTMENT ; 2021-577407. REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS 400 AND BS 420 STRINGER 25L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM B737-700 51-40-02 AND DWG 143A7505 SHEET 2 REV: B.

Part: SUPPORT — CRACKED (AFT CARGO BAY) · airframe 58,901 hrs · 34,794 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS907 TO BS927 AND STR25R TO STR27R AFT CARGO COMPARTMENT (FWD POSITION). REPLACED ANGLE-SUPPORT LOCATED BETWEEN BS907 TO BS927 AND STR25R TO STR27R AFT CARGO COMPARTMENT (FWD POSITION) IAW SRM 51-40-02. SRM 51-10-02 ITEM 9. DWG 147A7221 REV:D.

Part: ACCESS PANEL — ELONGATED (R/H WING) · airframe 58,901 hrs · 34,794 cycles

ELONGATED HOLE FRONT SPAR BRACKET INTERNAL CAVITY OF ACCESS PANEL 611AT AT RT WING ; 2021-577345 / [01] REPLACED FRONT SPAR BRACKET INTERNAL CAVITY OF ACCESS PANEL 611AT AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM B737-700 51-40-02 AND DWG 212A1901 SHEET 2 REV: A; [02] REPLACED FRONT SPAR BRACKET INTERNAL CAVITY OF ACCESS PANEL 611AT AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM B737-700 51-40-02 AND DWG 212A1901 SHEET 2 REV: A

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 58,901 hrs · 34,794 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS747 TO BS787 AND LBL21; WL156 AFT CARGO COMPARTMENT ; 2021-577349 / [01] TOOL USED: DIGITAL CALIPER P/N= 500-196-30; S/N= A20231842; DUE DATE= AUG-12-2022; [02] REPLACED SUPPORT ZEE LOCATED BETWEEN BS747 TO BS787 AND LBL21; WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; B737-700 SRM 53-00-53-2R-6 REPAIR 6. FIG 203; TABLE 201 AND DRAWING 146A7500 SHEET 61 REV.- SEE INDIVIDUAL SIGNOFFS BELOW; [03] TASK COMPLETED ; RII ; SEE INDIVIDUAL SIGNOFFS BELOW

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 58,901 hrs · 34,794 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS727D TO BS747 AND RBL21; WL156 AFT CARGO COMPARTMENT ; 2021-577346 / [01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 AND RBL 21 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 DWG# 146A7500 SHEET 61 REV - SEE INDIVIDUAL SIGN-OFFS BELOW; [02] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 AND RBL 21 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 DWG# 146A7500 SHEET 61 REV - RII ;SEE INDIVIDUAL SIGNOFFS BELOW

Part: ANGLE — CRACKED (AFT CARGO BAY) · airframe 58,901 hrs · 34,794 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS907 TO BS927 AND STR25R TO STR27R AFT CARGO COMPARTMENT (AFT POSITION) ; 2021-577338 / [01] REPLACED ANGLE-SUPPORT LOCATED BETWEEN BS907 TO BS927 AND STR25R TO STR27R AFT CARGO COMPARTMENT (AFT POSITION) IAW B737-700 SRM 51-40-02. SRM 51-10-02 ITEM 9 DWG 147A7221 REV:D. SEE INDIVIDUAL SING-OFF BELOW.; [02] REPLACED ANGLE-SUPPORT LOCATED BETWEEN BS907 TO BS927 AND STR25R TO STR27R AFT CARGO COMPARTMENT (AFT POSITION) IAW B737-700 SRM 51-40-02. SRM 51-10-02 ITEM 9 DWG 147A7221 REV:D. SEE INDIVIDUAL SING-OFF BELOW.

Part: ACCESS PANEL — ELONGATED (L/H WING) · airframe 58,901 hrs · 34,794 cycles

ELONGATED HOLE FRONT SPAR BRACKET INTERNAL CAVITY OF ACCESS PANEL 511AT AT LT WING ; 2021-577343 / [01] REPLACED FRONT SPAR BRACKET INTERNAL CAVITY OF ACCESS PANEL 511AT AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM B737-700 51-40-02 AND DWG 212A1901 SHEET 2 REV: A; [02] REPLACED FRONT SPAR BRACKET INTERNAL CAVITY OF ACCESS PANEL 511AT AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM B737-700 51-40-02 AND DWG 212A1901 SHEET 2 REV: A

Part: FLOORBEAM — CORRODED (BS 986 LBL43) · airframe 58,901 hrs · 34,794 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BS986.5 LBL43 AND WL208.1 AT AFT GALLEY AREA ; 2021-577226 / [01] TOOL USED: P/N: 45MG; S/N: 130060401; DUE DATE: 22-APR-22; [02] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101U102020; CAL DUE DATE: 01-JUN-22; [03] TOOL USED FLAPSPEED P/N FPK-PRO-104 S/N PRO-3384 DUE DATE: 24 MAY 22; [04] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 LBL43 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 1 FIGURE 205 SEE INDIVIDUAL SIGN-OFFS BELOW; [05] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 LBL43 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 1 FIGURE 205 SEE INDIVIDUAL SIGN-OFFS BELOW<BR>RII ACCOMPLISHED

Part: PLATE — CRACKED (L/H WING) · airframe 58,901 hrs · 34,794 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED ORSS 261 LT WING ; 2021-577243 / [01] REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS 261 LT WING IAW B737-700 SRM 51-40-02. SRM 51-10-02 ITEM 9 DWG 115A2001 REV:-. SEE INDIVIDUAL SING-OFF BELOW.; [02] REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS 261 LT WING IAW B737-700 SRM 51-40-02. SRM 51-10-02 ITEM 9 DWG 115A2001 REV:-. SEE INDIVIDUAL SING-OFF BELOW.

Part: WEB — CRACKED (FWD GALLEY) · airframe 58,901 hrs · 34,794 cycles

CRACK WEB LOCATED BETWEEN STA 328 TO STA 344 LBL 47 AND WL 208.1 AT FWD GALLEY AREA ; 2021-577254 / [01] REPLACED WEB LOCATED BETWEEN STA 328 TO STA 344 LBL 47 AND WL 208.1 AT FWD GALLEY ARE IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02 AND DRAWING 141A5400 REV.- SEE INDIVIDUAL SIGNOFFS BELOW; [02] REPLACED WEB LOCATED BETWEEN STA 328 TO STA 344 LBL 47 AND WL 208.1 AT FWD GALLEY ARE IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02 AND DRAWING 141A5400 REV.- <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: FLOORBEAM — CRACKED (FWD GALLEY) · airframe 58,901 hrs · 34,794 cycles

CRACK FLOOR BEAM 328 RBL 20 AND WL 208.1 AT FWD GALLEY AREA ; 2021-577242 / [01] TOOL USED DIGITAL CALIPER P/N:500-196-30 S/N:A20231842 DUE DATE: 12-AUG-22; [02] FOR PERMANENT REPAIR OF FLOOR BEAM 328 BTW BL0 TO RBL 60 AND WL 208.1 AT FWD GALLEY AREA SEE FAULT TTG8Q009Y2ZD; [03] FOR PERMANENT REPAIR OF FLOOR BEAM 328 BTW BL0 TO RBL 60 AND WL 208.1 AT FWD GALLEY AREA SEE FAULT TTG8Q009Y2ZD

Part: WEB — CRACKED (FWD GALLEY) · airframe 58,901 hrs · 34,794 cycles

CRACK WEB LOCTED BETWEEN STA 294.5 TO STA 312 RBL 15 AND WL 208.1 AT FWD GALLEY AREA ; 2021-577249 / [01] REPLACED WEB LOCTED BETWEEN STA 294.5 TO STA 312 RBL 15 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG 141A5400 REV: A P/N USED 141A5410U146 PO 2021 245669 1 SEE INDIVIDUAL SIGN-OFFS BELOW.; [02] JOB COMPLETE <BR>RII

Part: FLOORBEAM — CRACKED (FWD GALLEY) · airframe 58,901 hrs · 34,794 cycles

CRACK FLOOR BEAM 294.5 RBL 52 AND WL 208.1 AT FWD GALLEY AREA. PERFORMED PERMANENT REPAIR LOCATED AT FLOOR BEAM 294.5 BETWEEN RBL 25 AND RBL 52 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16; FIGURE 202; ALTERNATIVE 2.

Part: FLOORBEAM — CORRODED (BS 986 RBL 43) · airframe 58,901 hrs · 34,794 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BS986.5 RBL43 AND WL208.1 AT AFT GALLEY AREA ; 2021-577225 / [01] TOOL USED P/N 45 MG S/N 130064101 DUE DATE 11/MAR/2022; [02] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101U102020; CAL DUE DATE: 01-JUN-22; [03] TOOL USED FLAPSPEED P/N FPK-PRO-104 S/N PRO-3384 DUE DATE: 24 MAY 22; [04] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 RBL43 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 1 FIGURE 205 SEE INDIVIDUAL SIGN-OFFS BELOW; [05] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 RBL43 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 1 FIGURE 205 SEE INDIVIDUAL SIGN-OFFS BELOW<BR>RII ACCOMPLISHED

Part: PLATE — CRACKED (L/H WING) · airframe 58,901 hrs · 34,794 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED BETWEEN WS204.25 TO WS228.25 LT WING ; 2021-577252 / [01] REPLACED PLATE ASSY TRAILING EDGE LOCATED BETWEEN WS204.25 TO WS228.25 LT WING IAW B737-700 SRM 51-10-02 ITEM 9. AND DWG 115A2001 SHEET: 30 REV: A. P/N USED 115A2781-201 PO 2021 246225 1 SEE INDIVIDUAL SING-OFFS BELOW; [02] REPLACED PLATE ASSY TRAILING EDGE LOCATED BETWEEN WS204.25 TO WS228.25 LT WING IAW B737-700 SRM 51-10-02 ITEM 9. AND DWG 115A2001 SHEET: 30 REV: A. P/N USED 115A2781-201 PO 2021 246225 1 SEE INDIVIDUAL SING-OFFS BELOW.

Part: WEB — CRACKED (FWD GALLEY) · airframe 58,901 hrs · 34,794 cycles

CRACK WEB LOCATED BETWEEN STA 277 TONSTA 294.5 BL 0 AND WL 208.1 AT FWD GALLEY AREA ; 2021-577251 / [01] REPLACED WEB LOCATED BETWEEN STA 277 TO STA 294.5 BL 0 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9;B737-700 SRM 51-40-02 AND DRAWING 141A5400 REV.- SEE INDIVIDUAL SIGNOFFS BELOW; [02] REPLACED WEB LOCATED BETWEEN STA 277 TO STA 294.5 BL 0 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9;B737-700 SRM 51-40-02 AND DRAWING 141A5400 REV.- SEE INDIVIDUAL SIGNOFFS BELOW; RII

Part: ANGLE — CRACKED (L/H WING) · airframe 58,901 hrs · 34,794 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS 273 LT WING ; 2021-577248 / [01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 273 LT WING IAW B7E7-700 SRM 51-10-02 ITEM 9;SRM 51-40-02 AND DWG 115A2930 REV.-SEE INDIVIDUAL SIGN-OFFS BELOW; [02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 273 LT WING IAW B7E7-700 SRM 51-10-02 ITEM 9;SRM 51-40-02 AND DWG 115A2930 REV.-SEE INDIVIDUAL SIGN-OFFS BELOW

Part: NONE — BROKEN (CABIN) · airframe 58,901 hrs · 34,794 cycles

SUPPLEMENTAL INFORMATION: BROKEN EMERGENCY EXIT LENS GALLEY 1 AND ASSY FWD GALLEY AND LAV ; 2021-577233 / [01] REPLACED EMERGENCY EXIT LENS GALLEY 1 AND ASSY FWD GALLEY AND LAV IAW B737-700 AMM 33-51-01-960-802; TEST IS OK; [02] REPLACED EMERGENCY EXIT LENS GALLEY 1 AND ASSY FWD GALLEY AND LAV IAW B737-700 AMM 33-51-01-960-802; TEST IS OK

Part: FLOORBEAM — CRACKED (FWD GALLEY) · airframe 58,901 hrs · 34,794 cycles

CRACK FLOOR BEAM 328 RBL 27.5 AND WL 208.1 AT FWD GALLEY AREA ; 2021-577246 / [01] TOOL USED DIGITAL CALIPER P/N:500-196-30 S/N:A20231842 DUE DATE: 12-AUG-22; [02] PERFORMED PERMANENT REPAIR ON FLOOR BEAM 328 BTW BL0 TO RBL 60 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 FIG 205 ALTERNATIVE 2. SEE INDIVIDUAL SIGNOFFS BELOW; [03] PERFORMED PERMANENT REPAIR ON FLOOR BEAM 328 BTW BL0 TO RBL 60 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 FIG 205 ALTERNATIVE 2. RII;SEE INDIVIDUAL SIGNOFFS BELOW

Part: NONE — CORRODED (FUSELAGE) · airframe 58,901 hrs · 34,794 cycles

CORROSION FLOOR STRUCTURE INNER CHORD LOCATED BS951 TO BS992.8 RBL46 AND WL208.1 AFT GALLEY AND LAV ; 2021-577224 / [01] REPLACED INNER CHORD LOCATED AT FLOOR STRUCTURE BS951 TO BS992.8 RBL46 AND WL208.1 AFT GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 147A8501 SHEET 5 REV B SEE INDIVIDUAL SIGN-OFFS BELOW; [02] CORRECTED STEP 1 REPLACED INNER CHORD LOCATED AT FLOOR STRUCTURE BS951 TO BS992.8 RBL46 AND WL208.1 AFT GALLEY AND LAV P/N USED 147A8540U8ATSMR0 BATCH SW 2021002534 IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 147A8501 SHEET 5 REV B SEE INDIVIDUAL SIGN-OFFS BELOW; [03] CERTIFIED WORK PERFORMED RII.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 58,901 hrs · 34,794 cycles

SUPPLEMENTAL INFORMATION: CRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT ; 2021-577113 / [01] TOOL USED;DIGITAL CALIPER P/N:500-196-30 S/N:B21141569; DUE DATE:02-NOV-22.; [02] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW; [03] TASK COMPLETED.

Part: TIE CLIP — CRACKED (STRINGER 10 RH) · airframe 58,901 hrs · 34,794 cycles

CRACK TIE CLIP LOCATED BS 277 STRINGER 10 R/H AT PASSENG ; 2021-577215 / [01] REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 STRINGER 10 R/H AT PASSENGER IAW B737-700 SRM 51-40-02 AND DWG: 141A1110 REV: -<BR>P/N: 141A1250-92; P/O: 2021-169997.<BR>SEE INDIVIDUAL SIGNOFFS BELOW.; [02] REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 STRINGER 10 R/H AT PASSENGER IAW B737-700 SRM 51-40-02 AND DWG: 141A1110 REV: - <BR>P/N: 141A1250-92; P/O: 2021-169997. <BR>SEE INDIVIDUAL SIGNOFFS BELOW. RII

Part: FITTING — ELONGATED (FUSELAGE) · airframe 58,901 hrs · 34,794 cycles

ELONGATED HOLE UPPER FITTING LOCATED BS1016 AND BL0 AT PASSENGER CABIN ; 2021-577143 / [01] REPLACED UPPER FITTING LOCATED BS 1016 AND BL0 AT PASSENGER CABIN. IAW B737-700 SRM 51-40-02 DWG 148A2230 SHEET 8 REV C.; [02] COMPLETE TASK CERTIFIED RII

Part: BRACKET — CRACKED (CENTER WING BOX) · airframe 58,901 hrs · 34,794 cycles

CRACK BODY STATION 540 SUPPORT BRACKET OF THE BLEED DUCT ON INTERNAL AREA OF ACCESS PANEL 192CL AT LOWER FUSELAGE ; 2021-577193 / [01] REPLACED FRONT BRACKET OF THE BLEED DUCT ON INTERNAL AREA OF ACCESS PANEL 192CL IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM B737-700 51-40-02.; [02] REPLACED FRONT BRACKET OF THE BLEED DUCT ON INTERNAL AREA OF ACCESS PANEL 192CL IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM B737-700 51-40-02.

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 58,901 hrs · 34,794 cycles

CRACK ON ANGLE LOCATED BS663 AND RBL 10 APPROX AIR CONDITIONING COMPARTMENT AREA AT LOWER FUSELAGE ; 2021-577198 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 21-JAN-22; [02] REPLACED ANGLE LOCATED BS663. BTW RBL 65.00 AND RBL 5.00. AIR CONDITIONING COMPARTMENT AREA AT LOWER FUSELAG IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02. AND DWG: 111A1000; REV -. SEE INDIVIDUAL SIGN-OFF ENTRIES BELOW.; [03] REPLACED ANGLE LOCATED BS663. BTW RBL 65.00 AND RBL 5.00. AIR CONDITIONING COMPARTMENT AREA AT LOWER FUSELAG IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02. AND DWG: 111A1000; REV -. SEE INDIVIDUAL SIGN-OFF ENTRIES BELOW. AS RII

Part: FRAME — CRACKED (PAX CABIN) · airframe 58,901 hrs · 34,794 cycles

CRACK FRAME LOCATED 312 AT LEVEL STRINGER 5 L/H AT PASSENGER CABIN ; 2021-577216 / [01] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N: 210138203; DUE DATE: 05-MAR-22.; [02] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 21-JAN-22; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 21-JAN-22.; [03] PERFORMED REPAIR OF FRAME LOC BS 312 AT LEVEL STRINGER 5 L/H AT PASSENGER CABIN. IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1. ?SEE INDIVIDUAL SIGNOFF BELOW?.; [04] PERFORMED REPAIR FRAME (UPPER CHORD) LOC. BS 312; BETWEEN STRINGER 5L AND 6L AT PASSENGER CABIN. IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1.

Part: BRACKET — BROKEN (#1 ENGINE) · airframe 58,901 hrs · 34,794 cycles

BROKEN OUTBOARD FAN COWL HOLD OPEN ROD SUPPORT BRACKET; AFT POSITION ON ENGINE 1 ; 2021-577042 / [01] REPLACED OUTBOARD FAN COWL HOLD OPEN ROD SUPPORT BRACKET AFT POSITION ON ENGINE 1. IAW B737 SRM 51-10-02 ITEM 9. SRM 51-40-02. CMM 71-13-30.; [02] CORRECTED STEP 1.<BR>REPLACED OUTBOARD FAN COWL HOLD OPEN ROD SUPPORT BRACKET AFT POSITION ON ENGINE 1. IAW B737-700. SRM 51-10-02 ITEM 9. SRM 51-40-02. CMM 71-13-30.GOODRICH AEROSTRUCTURES; [03] REPLACED OUTBOARD FAN COWL HOLD OPEN ROD SUPPORT BRACKET AFT POSITION ON ENGINE 1. IAW B737-700. SRM 51-10-02 ITEM 9. SRM 51-40-02. CMM 71-13-30.

Part: FLASHLIGHT — MISSING (AFT CABIN) · airframe 58,901 hrs · 34,794 cycles

MISSING WINDSCREEN LT SIDE STRAP FLASHLIGHT AT AFT GALLEY AREA (1 EA) ; 2021-576911 / [01] INSTALLED WINDSCREEN LT SIDE STRAP FLASHLIGHT AT AFT GALLEY AREA (1 EA) I.A.W CMM ASTRONICS PAG 10006 AND PAG 10009 REV.10; [02] CORRECTED STEP 1 INSTALLED WINDSCREEN LT SIDE STRAP FLASHLIGHT AT AFT GALLEY AREA (1 EA) I.A.W CMM ASTRONICS 25-60-02 PAG 10006 AND PAG 10009 REV.10; [03] TASK CARD COMPLETED

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 58,901 hrs · 34,794 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT ; 2021-576971 / [01] TOOL USED;DIGITAL CALIPER P/N:500-196-30 S/N:B21141569; DUE DATE:02-NOV-22.; [02] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW; [03] TASK COMPLETED.

Part: ACCESS PANEL — CRACKED (CENTER WING BOX) · airframe 58,901 hrs · 34,794 cycles

CRACK BODY STATION 540 SUPPORT BRACKET OF THE BLEED DUCT ON INTERNAL AREA OF ACCESS PANEL 192CR AT LOWER FUSELAGE (1 EA) ; 2021-576955 / [01] REPLACED BODY STATION 540 SUPPORT BRACKET OF THE BLEED DUCT ON INTERNAL AREA OF ACCESS PANEL 192CR AT LOWER FUSELAGE (1 EA) IAW SRM B737-700 51-40-02 AND SRM B737-700 51-10-02 ITEM 9; [02] TASK CARD COMPLETE.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 58,388 hrs · 34,476 cycles

SUPPLEMENTAL INFORMATION: L1 DOOR SLIDE GRIT DRAGGING ON THE DOOR OPENING ; / [01] ADJUSTED DOOR SLIDE GIRT PER TASK CARD 725-61-06 AND AMM25-66-01

Part: SLIDE — LOOSE (L2 DOOR) · airframe 58,388 hrs · 34,476 cycles

SUPPLEMENTAL INFORMATION: L2 DOOR SLIDE GRIT DRAGGING ON THE DOOR OPENING ; / [01] RE SECURED AND REPACKED SLIDE GIRT PER AMM 25-66-01 AND TASK CARD 725-61-06.

Part: HANDLE — LOOSE (R1 DOOR ASSIST) · airframe 57,122 hrs · 33,726 cycles

FORWARD SERVICE DOOR ASSIST HANDLE LOOSE ; / TIGHTENED FWD SERVICE DOOR ASSIST HANDLE PER AMM 20-00-00-201-NG

Part: REVEAL — CRACKED (L2 DOOR) · airframe 56,526 hrs · 33,373 cycles

AFT ENTRY DOOR LINER WINDOW REVEAL IS CRACKED / R&R AFT ENTRY DOOR LINER WINDOW REVEAL IAW AMM 52-13-31.

Part: SHIELD — BROKEN (AFT FLASHLIGHT) · airframe 56,264 hrs · 33,220 cycles

AFT EMERGENCY FLASH LITE SHIELD BROKEN. R & R AFT F/A EMERGENCY FLASHLIGHT SHIELD, IAW MM 25-64-00.

Part: LIGHT — LOOSE (CABIN) · airframe 55,484 hrs · 32,758 cycles

BULL NOSE EMERGENCY LIGHT LENS AND ASSY LOOSE AT ROW 1 ABC / OK TO CONTINUE PER MEL 33-15-02 SP1 TRACKING #49411

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,078 hrs · 32,511 cycles

LH OVERWING EMERGENCY LIGHT INOP / RELAMPED LH OVERWING EMERGENCY LIGHT IAW AMM 33-51-05

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 54,049 hrs · 31,898 cycles

LH CABIN EMERGENCY LIGHTS LOCATED AT BS 560 AND 628 / IS INOP. / R&R THE EMERGENCY LIGHT POWER SUPPLY AT BS 727C+13. / OPS CHECK GOOD PER AMM 33-51-06.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 54,049 hrs · 31,898 cycles

CABIN FLOOR PANEL (#222AF ) HAS FIBERS DAMAGED ON UPPER SURFACE AND 1' CRACK ON AFT INBD. CORNER. / DAMAGED REMOVED IAW SRM 53-00-50; REPAIR #1. APPLIED REPAIR PLIES IAW SRM 53-00-50 REPAIR #1. INSTALLED INSERTS THAT WERE REMOVED TO FOM PER SRM 53-00-50.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

AFT CARGO FLOOR BEAM JOGGLED AREA CORRODED AT BS. 767+5, RBL 3.0 AT NUTPLATE HOLE. / REPAIRED FLOOR BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

AFT CARGO FLOOR BEAM JOGGLED AREA CORRODED AT BS. 767+5, RBL 8.1 AT NUTPLATE HOLE. / REPAIRED FLOOR BEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

AFT CARGO STRINGER CLIP CRACKED AT BS. 807, STR. 26R, AT LOWER END. / REPAIRED CLIP PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

FORWARD CARGO COMPARTMENT INTERCOSTAL CRACKED BETWEEN BS. 500B TO BS. 500C, LBL 25. / R&R INTERCOSTAL PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

FORWARD CARGO COMPARTMENT FRAME FASTENER HOLE DAMAGED AND CRACKED AT BS. 500D, WHERE LOWER STEP OF L/H TRANSITION ANGLE ATTACHES TO FRAME. / REPAIRED FRAME PER EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

AFT CARGO WEB CORRODED AT BS. 787, RBL 6. / R&R WEB PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

R1 DOOR FORWARD UPPER STUB FRAME CRACKED AT LATCH PLATE. / R&R STUB FRAME PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

FORWARD CARGO COMPARTMENT INTERCOSTAL CRACKED BETWEEN BS. 500B TO BS. 500C, LBL 25. / R&R INTERCOSTAL PER SRM.

Part: BEAR STRAP — CRACKED (FWD FUSELAGE) · airframe 54,049 hrs · 31,898 cycles

FWD SERVICE DOOR BEAR STRAP IS CRACKED ABOVE THE UPPER HINGE CUT OUT. STA 303 MINUS 5 INCHES; BETWEEN STRINGERS 8R AND 10R. / REPAIRED PER SRM 53-10-01-2R-6.

Part: STRINGER — CRACKED (LEFT WING) · airframe 54,048 hrs · 31,898 cycles

LEFT WING INBOARD FIXED LEADING EDGE STRINGER CRACKED WS. 210. R&R THE WING STRINGER IAW SRM.

Part: STRUCTURE — CORRODED (BS 663) · airframe 54,048 hrs · 31,898 cycles

FASTENER HOLE CORRODED AT BS. 663, LBL 64. REPAIRED HOLE PER EA.

Part: FLOOR SUPPORT — CORRODED (BS 500B-500C) · airframe 54,048 hrs · 31,898 cycles

INTERCOSTAL WEB CORRODED AROUND FASTENER HOLES BETWEEN BS. 500B TO BS. 500C, RBL 25, WHERE IT ATTACHES TO BOTTOM OF TRANSITION ANGLE. / R&R INTERCOSTAL PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

CABIN FLOOR BEAM UPPER SURFACE CORRODED AT BS. 312, LBL 14.5. / REPAIRED FLOOR BEAM PER EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

FORWARD ENTRY DOOR Z ANGLE CORRODED AT BS. 340. / R&R Z ANGLE PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

CRACK IN CABIN FLOOR SUPPORT STRUCTURE BETWEEN BS. 312 TO BS. 328, RBL 30, FLOOR PANEL ATTACH HOLE. / R&R INTERCOSTAL PER SRM.

Part: FLOORBEAM — CORRODED · airframe 54,049 hrs · 31,898 cycles

CORROSION UPPER SURFACE FLOOR BEAM STA. 344 LBL 11 / PERFORMED A T CAP REPAIR PER EA 1-753-36215 AND S.R.M. 51-40-02. SEE SUB TASK AND WIPS FOR INDIVIDUAL TASKS AND SIGN OFFS.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

CABIN FLOOR STRUCTURE CORRODED BETWEEN BS. 312 TO BS. 328, RBL 10.5. / R&R FLOOR STRUCTURE PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

CABIN FLOOR STRUCTURE CORRODED BETWEEN BS. 312 TO BS. 328, LBL 11. / R&R FLOOR STRUCTURE PER SRM.

Part: ANGLE — CORRODED (FWD SERVICE DOOR) · airframe 54,049 hrs · 31,898 cycles

FWD SERVICE DOOR Z-ANGLE CORROSION STA. 312 TO STA. 343;(MARKED) / REPLACED SUPPORT ANGLE PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

CRACK IN CABIN FLOOR SUPPORT STRUCTURE BETWEEN BS. 312 TO BS. 328, LBL 46, FLOOR PANEL ATTACH HOLE. / R&R INTERCOSTAL PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 54,049 hrs · 31,898 cycles

FLOOR ANGLE SUPPORT CRACKED AT APPROX. STA 540 LBL1 / REPLACED FLOOR PANEL BREAK ASSEMBLY PER SRM 51-40-02.

Part: ANGLE — CORRODED (AFT CARGO) · airframe 54,049 hrs · 31,898 cycles

AFT CARGO R/H TRANSITION ANGLE HAS CORROSION STA.767 TO STA.795. (RBL21). MARKED / REMOVED AND REPLACED TRANSITION ANGLE FROM STA. 727+5 TO 767 PER SRM. 51-10-02 (PART REPLACED #146A8127U12 )

Part: ANGLE — CORRODED (FWD CARGO) · airframe 54,049 hrs · 31,898 cycles

FWD CARGO COMPARTMENT TRANSITION ANGLE AT 25.2RBL HAS CORROSION AROUND FASTENER HOLES BETWEEN STAS 420-440. / R & R TRANSITION ANGLE IN FWD CARGO COMPARTMENT AT 25.2RBL AT STAS 420-440. PER SRM 51-40-02-0G01 ASSY P/N 143A8126-21

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

TRIANGULAR SUPPORT ANGLE CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

FORWARD CARGO COMPARTMENT BULKHEAD ANGLE CORRODED AROUND FASTENER HOLES AT BS. 500D, BETWEEN LBL 25.2 TO RBL 25.2. / R&R ANGLE PER SRM.

Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 54,049 hrs · 31,898 cycles

FWD CARGO COMPARTMENT TRANSITION ANGLE AT 25.2RBL HAS CORROSION AROUND FASTENER HOLES BETWEEN STAS 500-500A. / REMOVED AND REPLACED TRANSITION ANGLE PER SRM 51-40-02. P/N 143A8126-31.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

TRIANGULAR SUPPORT ANGLE CRACKED AT BS. 500D, STR. 19L. / R&R ANGLE PER SRM.

Part: ANGLE — CORRODED (FWD CARGO) · airframe 54,049 hrs · 31,898 cycles

FWD CARGO COMPARTMENT TRANSITION ANGLE AT 25.2LBL HAS CORROSION AROUND FASTENER HOLES BETWEEN STAS 460-500. / REMOVED AND REPLACED FWD CARGO LH TRANSITION ANGLE AT 25.2LBL FROM STA. 400 TO 500D PER SRM 51-40-02.

Part: ANGLE — CORRODED (FWD CARGO) · airframe 54,049 hrs · 31,898 cycles

FWD CARGO COMPARTMENT TRANSITION ANGLE AT 25.2RBL HAS CORROSION AROUND FASTENER HOLES BETWEEN STAS 500A-500D. / REMOVED AND REPLACED TRANSITION ANGLE PER SRM 51-40-02; SEE SUBTASK AND WIPS FOR DETAILED DESCRIPTION OF WORK.

Part: ANGLE — CORRODED (AFT CARGO) · airframe 54,049 hrs · 31,898 cycles

AFT CARGO R/H TRANSITION ANGLE HAS LIGHT CORROSION AROUND FASTENER HOLES STA.727B +2 TO 727C +11 (RBL21). MARKED / REMOVED AND REPLACED R/H TRANSITION ANGLE FROM STA. 727+5 TO 767 PER SRM. 51-40-02. SEE WIP'S AND TASKS FOR ADDITIONAL INFORMATION. CORROSION QUESTIONS CORRECTED AND ANSWERED ACCORDINGLY

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 54,048 hrs · 31,898 cycles

AFT CARGO FLOOR TRACK CORRODED AROUND TIE DOWN AND FASTENER HOLES AT BS. 847+5, RBL 14. / R&R FLOOR TRACK PER SRM.

Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 54,049 hrs · 31,898 cycles

FWD CARGO COMPARTMENT TRANSITION ANGLE AT 25.2RBL HAS CORROSION AROUND FASTENER HOLES BETWEEN STAS 400-420. / INSTALLED R/H TRANSITION ANGLE FROM STA 400 TO STA 420; RBL 25.2 IAW SRM 51-40-02 AND REFERENCE BOEING DRAWING 143A7501-14.REFER ALL WIP'S FOR WORK ACCOMPLISHED.

Part: ANGLE — CORRODED (FWD CARGO) · airframe 54,049 hrs · 31,898 cycles

FWD CARGO COMPARTMENT TRANSITION ANGLE AT 25.2LBL HAS CORROSION AROUND FASTENER HOLES BETWEEN STAS 500-500D. / REMOVED AND REPLACED RH TRANSITION ANGLE PN 143A7501-187 AT STA 500-500D IAW SRM 51-40-02

Part: ANGLE — CORRODED (AFT CARGO) · airframe 54,049 hrs · 31,898 cycles

AFT CARGO R/H TRANSITION ANGLE HAS CORROSION STA.727C +11 TO STA.767. (RBL21). MARKED / REMOVED AND REPLACED R/H TRANSITION ANGLE FROM STA. 727+5 TO 767 PER SRM. 51-40-02. SEE WIP'S AND TASKS FOR ADDITIONAL INFORMATION. CORRECTED CORROSION QUESTIONS AND ANSWERED ACCORDINGLY.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 54,048 hrs · 31,898 cycles

AFT CARGO FLOOR TRACK CORRODED AROUND FASTENER HOLES BETWEEN BS. 795+8 TO BS. 827, RBL 14. / R&R FLOOR TRACK PER SRM.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 54,049 hrs · 31,898 cycles

AFT CARGO L/H TRANSITION ANGLE HAS LIGHT CORROSION AROUND FASTENER HOLES STA.727E +9 TO 807 (LBL21). MARKED / REMOVED AND REPLACED TRANSITION ANGLE PER SRM 51-40-02; SEE SUBTASK AND WIPS FOR DETAILED DESCRIPTION OF WORK.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 54,049 hrs · 31,898 cycles

AFT CARGO L/H TRANSITION ANGLE HAS HEAVY CORROSION STA.727C +10 TO 727E +9 (LBL21). MARKED / REMOVED AND REPLACED TRANSITION ANGLE PER SRM 51-40-02; SEE SUBTASK AND WIPS FOR DETAILED DESCRIPTION OF WORK.

Part: SUPPORT BRACKET — CRACKED (AFT CARGO BAY) · airframe 54,049 hrs · 31,898 cycles

AFT CARGO FWD BULKHEAD SUPPORT BRACKET CRACKED. STA.727 RBL 6. MARKED / BRACKET REPLACED PER SRM 51-40-02.

Part: STRAP — CORRODED (FUSELAGE) · airframe 54,048 hrs · 31,898 cycles

AFT CARGO COMPARTMENT FLOOR BEAM STRAP CORRODED AT BS. 887, BETWEEN LBL 9 TO RBL 21. / R&R STRAP PER SRM.

Part: TRACK — CORRODED (AFT CARGO BAY) · airframe 54,049 hrs · 31,898 cycles

AFT CARGO COMPARTMENT STRUCTURE HAS CORROSION AT STA 927 LBL 3. / REMOVED AND REPLACED AFT CARGO FLOOR TRACK AT STA 887-947 LBL 3. PART #147A7501-13 PER SRM. 51-10-02

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 54,048 hrs · 31,898 cycles

AFT CARGO COMPARTMENT STRUCTURE CORRODED BETWEEN BS. 887 TO BS. 947, RBL 15. / R&R FLOOR TRACK PER SRM.

Part: ATTACH ANGLE — CRACKED (AFT CARGO BAY) · airframe 54,049 hrs · 31,898 cycles

AFT CARGO COMPARTMENT LOWER ATTACH ANGLE ON SUPPORT POST FOR WASTE TANK AREA IS CRACKED; STA 867 LBL 10. / REPLACED ATTACH ANGLE PER SRM 51-40-02. LOWER BULKHEAD SUPPORT ANGLE TO BE REINSTALLED ON N/R G701182.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 54,048 hrs · 31,898 cycles

AFT CARGO COMPARTMENT STRUCTURE CORRODED BETWEEN BS. 887 TO BS. 947, LBL 3. / R&R FLOOR TRACK PER SRM.

Part: ATTACH ANGLE — CRACKED (AFT CARGO BAY) · airframe 54,049 hrs · 31,898 cycles

AFT CARGO COMPARTMENT ATTACH ANGLE FOR FWD LEFT WATER TANK MOUNT IS CRACKED AT STA 947 LBL 15. / REMOVED AND REPLACED ATTACH ANGLE AFT CARGO COMPARTMENT FWD LEFT WATER TANK MOUNT STA 947 LBL 15. PER SRM.51-10-02

Part: SKIN — CANNING (LT HORIZ STAB) · airframe 54,048 hrs · 31,898 cycles

L/H HORIZONTAL STABILIZER LOWER SKIN HAD LARGE AREA OF OIL CANNING OUTBOARD OF AFT OUTBOARD DOUBLER OF SKIN REPLACEMENT REPAIR. / REPAIRED SKIN PER EA.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 54,049 hrs · 31,898 cycles

FWD CARGO COMPARTMENT; FWD SCUFF PLATE CRACKED/BLOKEN / REMOVED AND REPLACED FWD CARGO COMPARTMENT; FWD SCUFF PLATE IAW AMM 53-11-02

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 54,049 hrs · 31,898 cycles

FWD CARGO COMPARTMENT; AFT SCUFF PLATE CRACKED/BLOKEN / REMOVED AND REPLACED FWD CARGO COMPARTMENT; AFT SCUFF PLATE IAW AMM 53-11-02

Part: BEAM — CRACKED (R1 DOOR) · airframe 54,049 hrs · 31,898 cycles

FWD SERVICE DOOR LOWER #4 BEAM 141A6536-14 HAS MULTIPLE CRACKS.VERIFIED BY HFEC PER 737 NDT MANUAL PSRT6; 51-00-00 PROC.23 / REMOVED DOOR AND REPAIRED DOOR FRAME PER REPAIR ORDER # 0520055-G5R. REINSTALLED DOOR PER M/M REF 52-41-00. DOOR ADJUSTMENT ACCOMPLISHED ON N/R G704263 TAG NO: 646468 PN ON: 141A6516-18M SN ON: BN001524 PN OFF: SN OFF: BN001524

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 54,049 hrs · 31,898 cycles

AFT CARGO DOOR CUTOUT; AFT CORNER SCUFF PLATE IS CRACKED. / REPLACED SCUFF PLATE PER AMM 53-11-02.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 54,049 hrs · 31,898 cycles

AFT CARGO DOOR CUTOUT; FWD CORNER SCUFF PLATE IS CRACKED. / REPLACED SCUFF PLATE PER AMM 53-11-02.

Part: LENS — CRACKED (CABIN) · airframe 54,048 hrs · 31,898 cycles

L/H CABIN OVERHEAD EMERGENCY LIGHT LENS CRACKED AT ROW 1. / R&R LENS PER AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,005 hrs · 31,868 cycles

AFT OF L2 DOOR EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.

Part: GUIDE — UNSECURE (GIRT BAR) · airframe 52,094 hrs · 30,617 cycles

AFT GALLEY GIRT BAR GUIDE CAME OFF. INSTALLED NEW GIRT BAR PER AMM.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 51,885 hrs · 30,473 cycles

LH HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL CRACKED. / R&R LH HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL PER AMM 53-31-31

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,885 hrs · 30,473 cycles

L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. / RELAMPED LIGHT PER AMM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 51,885 hrs · 30,473 cycles

RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED. / R/R R/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL REF AMM 53-31-31.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,885 hrs · 30,473 cycles

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

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 51,885 hrs · 30,473 cycles

L/H AFT BATTERY PACK (M01673) FOUND TO HAVE HAD LOW OUT PUT. / R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,169 hrs · 30,012 cycles

R1 FORWARD EMERGENCY LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: FITTING — ELONGATED (LT WING) · airframe 48,134 hrs · 28,070 cycles

ON OK TO INSTALL LT WING T/E PANEL 551GB FOUND FWD I/B SUPPORT ROD FITTING HAS ELONGATED FASTENER HOLE / REMOVED AND REPLACED LT WING T/E PANEL 551GB FWD I/B SUPPORT ROD FITTING PN 115A2350-1 ATAG SB1134 IAW SRM 51-40-02-OG AND DWG 115A5300.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 48,134 hrs · 28,070 cycles

RIGHT WING TRAILING EDGE ABOVE PYLON SAIL TAIL, LOWER SEAL SUPPORT BRACKET CRACKED. R & R THE SUPPORT BRACKET IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 48,134 hrs · 28,070 cycles

RIGHT WING T/E ABOVE PYLON SAIL TAIL; UPPER SEAL SUPPORT BRACKET IS CRACKED. / REMOVED AND REPLACED BRACKET ON RIGHT WING ABOVE SAIL TAIL IAW SRM 51-40-02-OG-0. A TAG. A65808

Part: PLATE — CRACKED (RT WING) · airframe 48,134 hrs · 28,070 cycles

RT WING TRAILING EDGE ABOVE AND INBOARD OF PYLON SAIL TAIL WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM AND DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 48,134 hrs · 28,070 cycles

FWD CARGO FWD THRESHOLD CASTING CRACKED / REPAIRED FWD CARGO FWD THRESHOLD CASTING IAW SWA EA# 1A53-2076 REV. 11.

Part: ANGLE — CRACKED (LT WING) · airframe 48,134 hrs · 28,070 cycles

LEFT WING BULKHEAD SEAL RETAINER INBOARD OF INBOARD DEFLECTION RIB, ANGLE CRACKED. R & R THE ANGLE IAW MM.

Part: SKIN — DELAMINATED (LT WING) · airframe 48,134 hrs · 28,070 cycles

LEFT WING OUTBOARD AFT FLAP INBOARD LOWER EDGE SKIN SEPARATING. / REPAIRED LH WING OB AFT FLAP IB LOWER EDGE IAW 737-700 SRM 51-70-10-2R-0 REV 63 PER SRM 51-70-10-2R-4 REV 63 PER SRM 57-53-01-2R-4 REV 63. CLASSIFIED AS SECONDARY FLIGHT CONTROL PER 737-700 SRM 51-00-04-0G-0 PAR 9;TABLE 5; FIG 2 REV 63.

Part: SUPPORT FRAME — CRACKED (RT WING) · airframe 48,134 hrs · 28,070 cycles

#2 SAIL TAIL AFT O/B FAIRING SUPPORT FRAME IS CRACKED. (TAIL ASSY. P/N 313A2752-1) / REMOVED AND REPLACED #2 SAIL TAIL AFT FAIRING SUPPORT ASSEMBLY I/A/W SRM 51-40-02-0G-0 AND BOEING DRAWING 313A2752 REV. A.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 48,689 hrs · 28,111 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 45,749 hrs · 26,567 cycles

R1 DOOR EMERGENCY EXIT FLOOR LENS COVER LOOSE. / SECURED COVER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 44,166 hrs · 25,668 cycles

L1 DOOR EMERGENCY SLIDE OUT OF POSITON. REPOSITIONED THE SLIDE IAW MT.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

RIGHT DOUBLER CRACKED AT BS 235.8. REPAIRED DOUBLER IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

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

Part: ANGLE — CRACKED (LT MLG WW) · airframe 42,242 hrs · 24,538 cycles

BULKHEAD WEB ANGLE CRACKED AT STATION 663.75, LBL 28. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED · airframe 42,242 hrs · 24,538 cycles

NUMBER 1 ENG SUPPORT ANGLE CRACKED, ON LOWER SPAR ON STRUT BOX LT SIDE. R & R ANGLE IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

STRINGER CRACKED AT BS 540, STRINGER 23L. REPAIRED STRINGER IAW SRM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 42,242 hrs · 24,538 cycles

LEFT WING TE SUPPORT BRACKET CRACKED ON AT LEVEL RSS 138.79,. UPPER CHORD. R & R BRACKET IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

INTERCOSTAL CRACKED AT STATION 500D, STRINGER 28L. REPAIRED INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

INTERCOSTAL CRACKED AT STATION 927 - 948, STRINGER 25R. REPAIRED INTERCOSTAL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

TIE CLIP CRACKED AT BS 60, STRINGER 8R. R & R TIE CLIP IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

WEB CRACKED, BETWEEN BS 312 - 328, LBL 46. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

FUSELAGE FRAME CRACKED AT STATION 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

FRAME WEB CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

FUSELAGE FRAME CRACKED AT STATION 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

FRAME WEB CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

WEB CRACKED, BETWEEN BS 312 - 328, RBL 31. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

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

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 42,242 hrs · 24,538 cycles

BULKHEAD WEB CRACKED AT BS 663.75, LBL 19. REPAIRED WEB IAW EA.

Part: FAIRING — CRACKED (FLAP TRACK) · airframe 42,242 hrs · 24,538 cycles

RIGHT WING FLAP TRACK FAIRING 642BB INTERNAL CAVITY CRACKED. REPAIRED FAIRING IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

FORWARD CARGO COMPARTMENT WEB INTERCOSTAL CRACKED, BETWEEN BS 500 - 500A, STRINGER 26L. R & R INTERCOSTAL IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

WING TO BODY FAIRING ANGLE CRACKED AT BS 540, RBL 41. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

FORWARD CARGO COMPARTMENT WEB INTERCOSTAL CRACKED, BETWEEN BS 500A - 500B, STRINGER 26L. R & R INTERCOSTAL IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 500B, STRINGER 26R. R & R ANGLE IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,242 hrs · 24,538 cycles

AFT CARGO SEAT TRACK CORRODED AT STATION 787 - 847, RBL 13.84. R & R SEAT TRACK SECTION IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 42,242 hrs · 24,538 cycles

AFT CARGO SUPPORT ANGLE CORRODED AT STATION 727B+9 - 847, LBL 21. REPAIRED ANGLE IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,242 hrs · 24,538 cycles

LEFT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STATION 92.70, 39" FROM FRONT SPAR. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,242 hrs · 24,538 cycles

LEFT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STATION 92.70, 29" FROM FRONT SPAR. REPAIRED RIB IAW SRM.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 42,242 hrs · 24,538 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,194 hrs · 24,506 cycles

RIGHT AFT WING TO BODY EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,067 hrs · 24,439 cycles

EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M1675. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,067 hrs · 24,439 cycles

EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M1672. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,067 hrs · 24,439 cycles

EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M1673. R & R BATTERY PACK IAW MM.

Part: LIGHT — BROKEN (EXIT SIGN) · airframe 38,489 hrs · 22,408 cycles

RIGHT SIDE OVERWING EMER EXIT SIGN LIGHT BROKEN. R & R SIGN IAW MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,606 hrs · 20,791 cycles

RIGHT TRANS ANGLE CORRODED BETWEEN BS 727C+10 TO BS 767. REPAIRED ANGLE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,606 hrs · 20,791 cycles

SEAT TRACK FLANGE ON OTBD SIDE FWD OF FLOORBEAM CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,606 hrs · 20,791 cycles

SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,606 hrs · 20,791 cycles

INTERCOSTAL CRACKED AT BS 540, LBL 1. R & R INTERCOSTAL IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 35,606 hrs · 20,791 cycles

RIGHT WING WIGGLE PLATE CRACKED ABOVE RT AFT STRUT FAIRING AT ORSS 265. R & R WIGGLE PLATE IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 35,606 hrs · 20,791 cycles

RIGHT FLIGHT DECK NR 3 WINDOW E F POST CRACKED FROM NR 8 FASTENER HOLE. REPAIRED POST IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,606 hrs · 20,791 cycles

LEFT FLIGHT DECK NR 1 WINDOW FRAME CRACKED ON UPPER OTBD EDGE. REPAIRED FRAME IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 35,606 hrs · 20,791 cycles

LEFT FLIGHT DECK NR 3 WINDOW E F POST CRACKED FROM NR 8 FASTENER HOLE. REPAIRED POST IAW ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,606 hrs · 20,791 cycles

SKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED SKIN IAW EA.

Part: BRACKET — CRACKED (RT WING) · airframe 35,606 hrs · 20,791 cycles

RIGHT WING INBD DEFLECTION RIB CRACKED ANGLE BRACKET AT UPPER SHELF PANEL. R & R BRACKET IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,606 hrs · 20,791 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 138.70, APPROXIMATELY 33 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,606 hrs · 20,791 cycles

LEFT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 184.70 APPROXIMATELY 10 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,606 hrs · 20,791 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 129.50, APPROXIMATELY 17.5 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,606 hrs · 20,791 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 103.7. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,606 hrs · 20,791 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 101.90, APPROXIMATELY 28 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,606 hrs · 20,791 cycles

LEFT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT REAR SPAR, STAB STATION 98.0. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,606 hrs · 20,791 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 138.70, APPROXIMATELY 17.5 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 34,009 hrs · 19,843 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED 1.25". REPAIRED SKIN IAW SRM.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 33,277 hrs · 19,398 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT CONTAINER RING LOOSE. R&R GIRT BAR IAW MM & SIP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,903 hrs · 19,192 cycles

LT AFT LOWER FUSELAGE EMERGENCY EXIT LIGHT INOPERATIVE. R&R BULB IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 31,883 hrs · 18,609 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,514 hrs · 18,390 cycles

LEFT OVERWING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 31,128 hrs · 18,167 cycles

DIVERSION / DECLARED EMERGENCY - FUEL CROSS FEED VALVE C/B TRIPPED. REMOVED AND REPLACED FUEL CROSS FEED VALVE PER MM.

Part: GIRT BAR — OUT OF ADJUST (R2 DOOR) · airframe 30,776 hrs · 17,959 cycles

R2 DOOR SLIDE GIRT BAR NEEDS RE-INSTALLED, TOO LONG. RE-INSTALLED PER M/M R-2 DOOR SLIDE GIRT C/W T/C 725-61-06.

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR) · airframe 30,776 hrs · 17,959 cycles

L2 DOOR SLIDE GIRT NEEDS REINSTALLED, TOO LONG. RE-INSTALLED PER M/M L-2 DOOR SLIDE GIRT C/W T/C 725-61-06.

Part: RING — BROKEN (GIRT BAR) · airframe 30,776 hrs · 17,959 cycles

R2 DOOR SLIDE GIRT BAR AFT RETAINING RING BROKEN. REMOVED AND REPLACED R-2 DOOR SLIDE GIRT BAR AFT RETAINING RING PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 30,007 hrs · 17,514 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 29,722 hrs · 17,337 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE FROM CASE. REMOVED AND REPLACED SLIDE PER AMM AND MT.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 29,722 hrs · 17,337 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE FROM CASE. SECURED SLIDE PER AMM AND MT.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 29,722 hrs · 17,337 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE AMM AND MT.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 29,722 hrs · 17,337 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER AMM AND MT.

Part: LENS — LOOSE (CABIN) · airframe 29,599 hrs · 17,254 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER AMM.

Part: REGULATOR — FAULTY (BLEED AIR SYS) · airframe 29,565 hrs · 17,235 cycles

DIVERSION/DECLARED EMERGENCY. ALTITUDE WARNING HORN AT CRUISE FL 390 CABIN ALT CLIMBED TO 14K PRESSURIZATION VERY ERRATIC AND SLOW TO COME BACK DOWN BELOW 10K. NO OR VERY LITTLE CONTROL IN AUTO. MANUAL PRESS WITH NR 1 BLEED CLOSED, PRESS RESPONDED NORMALLY. REMOVED AND REPLACED NR 1 ENGINE HIGH STAGE REGULATOR, BLEED AIR REGULATOR, PRSOV, AND 35 DEGREE CONTROLLER PER MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,901 hrs · 17,443 cycles

RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 133. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,972 hrs · 16,884 cycles

RIGHT STABILIZER LOWER INSPAR SKIN CRACKED AT LE STA 133.15+57. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,972 hrs · 16,884 cycles

LEFT STABILIZER, LOWER INSPAR SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,834 hrs · 16,805 cycles

R1 DOOR FUSELAGE SKIN CUTOUT CRACKED AT BS 296, WL 208. REPAIRED SKIN IAW ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,834 hrs · 16,805 cycles

FLOORBEAM CORRODED AT BS 344, BETWEEN RBL 8 TO LBL 11. REPAIRED BEAM IAW EA AND ER.

Part: WEB — CORRODED (FUSELAGE) · airframe 28,834 hrs · 16,805 cycles

FLOOR WEB CORRODED BETWEEN BS 1006 TO BS 1013, LBL 3. REMOVED AND REPLACED WEB ASSY IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,834 hrs · 16,805 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.70. REPAIRED RIB IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,834 hrs · 16,805 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB 129.50. REPAIRED SKIN IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 28,834 hrs · 16,805 cycles

LT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.0. REPAIRED RIB IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 28,834 hrs · 16,805 cycles

BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, LBL 22. REMOVED AND REPLACED ANGLE PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,834 hrs · 16,805 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,834 hrs · 16,805 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.30. REPAIRED SKIN IAW SRM.

Part: HEAT EXCHANGER — FAULTY (AC BAY) · airframe 28,482 hrs · 16,595 cycles

FLT ATT REPORTS ELECTRICAL ODOR AT VICINITY OF ROW 13 A/C RIGHT NO VISIBLE SMOKE NOTED. REMOVED AND REPLACED RT SECONDARY HEAT EXCHANGER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,943 hrs · 16,254 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT EEPLS INOP. RELAMPED PER MM.

Part: COVER — LOOSE (CABIN) · airframe 27,748 hrs · 16,142 cycles

FWD EEPLS COVER LOOSE. SECURED COVER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 27,708 hrs · 16,123 cycles

EEPLS BROKEN AT ROW 1. R&R EEPLS PER MM.

Part: CAP — BROKEN (CABIN) · airframe 27,580 hrs · 16,035 cycles

DURING SCHEDULED CV CHECK, FOUND FWD EMERGENCY EXIT LIGHT END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM.

Part: COVER — CRACKED (CABIN) · airframe 27,580 hrs · 16,035 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 16 TO ROW 22. REMOVED AND REPLACED COVER IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 27,580 hrs · 16,035 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 3. REMOVED AND REPLACED COVER IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 27,580 hrs · 16,035 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 23. REMOVED AND REPLACED COVER IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 26,425 hrs · 15,351 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1 TO ROW 12. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 26,425 hrs · 15,351 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 23. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 22,217 hrs · 12,934 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,304 hrs · 12,991 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLAT — DAMAGED (RT WING) · airframe 21,991 hrs · 12,806 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING NR 4 SLAT O/B OF NR 1 ENG DAMAGED. REMOVED AND REPLACED SLAT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 21,943 hrs · 12,777 cycles

DURING SCHEDULED 6Y CHECK, FOUND EEPLS LOOSE. SECURED EEPLS PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 21,856 hrs · 12,733 cycles

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

Part: CAP — MISSING (CABIN) · airframe 21,856 hrs · 12,733 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS END CAP MISSING AT 1 ABC. INSTALLED END CAP PER MM.

Part: COVER — LOOSE (CABIN) · airframe 18,666 hrs · 10,833 cycles

R1 DOOR EMERGENCY EXIT DOOR LIGHT COVER LOOSE. R&R LIGHT PER MM.

Part: CAP — MISSING (CABIN) · airframe 18,028 hrs · 10,449 cycles

FWD EEPLS END CAP MISSING. INSTALLED END CAP PER MM.

Part: CAP — MISSING (CABIN) · airframe 17,350 hrs · 10,039 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS END CAP MISSING AT ROW 1. INSTALLED END CAP PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,273 hrs · 9,991 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EMERGENCY LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHTS) · airframe 12,480 hrs · 7,079 cycles

EEPLS COVER LOOSE AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 12,445 hrs · 7,061 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 12,415 hrs · 7,039 cycles

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

Part: CAP — LOOSE (CABIN) · airframe 12,381 hrs · 7,022 cycles

EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 12,370 hrs · 7,015 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 12,370 hrs · 7,015 cycles

DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 12,314 hrs · 6,981 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 12,314 hrs · 6,981 cycles

EEPLS ASSY LOOSE AT ROW 3 ABC. SECURED EEPLS ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 12,280 hrs · 6,959 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: ENGINE — FAILED (RH WING) · airframe 11,465 hrs · 6,481 cycles

INFLIGHT SHUTDOWN / DECLARED EMERGENCY. AT 24,000 FT NR 2 ENGINE OIL BYPASS LIGHT ILLUMINATED. OIL PRESSURE LIGHT ALSO ILLUMINATED AND NR 2 ENGINE FAILED. REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 11,131 hrs · 6,288 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 11,131 hrs · 6,288 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: FITTING — BROKEN (GIRT BAR) · airframe 9,728 hrs · 5,480 cycles

R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING BROKEN. REMOVED AND REPLACED AFT GIRT BAR FITTING PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 9,107 hrs · 5,120 cycles

EEPLS COVER LOOSE AT LT FWD CABIN. SECURED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 8,368 hrs · 4,699 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CONTROLLER — INOPERATIVE (E/E BAY) · airframe 8,350 hrs · 4,686 cycles

AIR TURNBACK, AIRCRAFT FAILED TO PRESSURIZE AT LIFT-OFF. REMOVED AND REPLACED NR 2 CABIN PRESSURE CONTROLLER PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHTS) · airframe 7,248 hrs · 4,029 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1 TO ROW 23. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56 hrs · 35 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.