N492WN

Part: COVER — BROKEN (ZN 200 FUS TOP) · airframe 63,780 hrs · 37,864 cycles

RIGHT WINDOW WING EXIT LIGHT COVER BROKEN.<[01] REPLACED RIGHT OVERWING EMERGENCY EXIT LOWER LIGHT LENSE REF AMM 33-51-03

Part: POWER SUPPLY — INOPERATIVE (ZN 800 DOOR) · airframe 63,430 hrs · 37,651 cycles

EMERGENCY EXTERNAL LIGHT L2 DOOR INOP.<[01] R/R AFT GALLEY LH EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-06. OPS CHECK GOOD

Part: BATTERY — INOPERATIVE (ZN 200 FUS TOP) · airframe 62,371 hrs · 36,965 cycles

MULTIPLE FWD EMERGENCY LIGHTS INOP. SUSPECT BATTERY PACK M01674.<[01] R & R BATTERY PACK AT MO1674 AND BATTERY AT M01675

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 62,371 hrs · 36,965 cycles

MULTIPLE FWD EMERGENCY LIGHTS INOP. SUSPECT BATTERY PACK M01674.<[01] R & R BATTERY PACK AT MO1674 AND BATTERY AT M01675

Part: SIGN — INOPERATIVE (ZN 200 FUS TOP) · airframe 61,929 hrs · 36,663 cycles

PASSENGER TO ATTENDANT CALL LIGHT ON AFT GALLEY EXIT SIGN INOP<[01] RELAMPED AFT BLUE F/A CALL LIGHT IAW AMM 33-27-00

Part: BATTERY — INOPERATIVE (ZN 200 FUS TOP) · airframe 61,404 hrs · 36,327 cycles

EMERGENCY MEGAPHONE FWD GALLEY INOP<[01] R & R FWD MEGA PHONE BATTERIES PER SIP

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 60,891 hrs · 36,003 cycles

L1 DOOR EMERGENCY SLIDE PRESSURE GAUGE INDICATES RED / [01] R&R L1 SLIDE IAW AMM 25-66-01 AND MT 725-61-06

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 60,891 hrs · 36,003 cycles

L1 DOOR EMERGENCY SLIDE PRESSURE GAUGE INDICATES RED. / [01] INSP FWD SLIDE FOUND TO BE WITHIN MM LIMITS IAW AMM 25-66-01<BR>A/C OKAY FOR CONTINUED SERVICE

Part: BEAM — CORRODED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CORROSION FLOOR STRUCTURE BEAM HORIZONTAL FLANGE BS 986.5 LBL 24 AT AFT GALLEY AREA 2022-441641 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 210138503; DUE DATE: 19-MAY-23;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[03] REPAIRED FLOOR STRUCTURE BEAM HORIZONTAL FLANGE BS 986.5 LBL 24 AT AFT GALLEY AREA IAW EA M-21-153-00612 SEE INDIVIDUALS SIGN OFF BELOW;[04] REPAIRED FLOOR STRUCTURE BEAM HORIZONTAL FLANGE BS 986.5 LBL 24 AT AFT GALLEY AREA IAW EA M-21-153-00612 SEE INDIVIDUALS SIGN OFF BELOW

Part: BEAM — CORRODED (AFT FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BS986.5 WL208.1 AND LBL 43 AT AFT GALLEY AREA 2022-441640 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 22-FEB-23.;[02] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 200048001; DUE DATE: 30-MAR-23;[03] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 WL208.1 AND LBL 43 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 SEE INDIVIDUALS SIGN OFF BELOW;[04] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 WL208.1 AND LBL 43 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; RII ACCOMPLISHED SEE INDIVIDUALS SIGN OFF BELOW

Part: NONE — CRACKED (FWD CARGO) · airframe 60,350 hrs · 35,654 cycles

CRACK ANGLE - CLIP LOCATED BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT 2022-441639 / [01] REPLACED ANGLE - CLIP LOCATED BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 9 REV: A;[02] REPLACED ANGLE - CLIP LOCATED BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 9 REV: A SEE INDIVIDUAL SINGOFFS BELOW <BR>RII

Part: NONE — CRACKED (FWD CARGO) · airframe 60,350 hrs · 35,654 cycles

CRACK ANGLE - CLIP BS 400 AT LEVEL STR 26L FWD CARGO COMPARTMENT 2022-441607. / [01] REPLACED ANGLE - CLIP BS 400 AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 2 REV: B. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETED <BR>RII

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK ANGLE FLOOR STRUCTURE CENTER SECTION LOCATED ON BS 695 BL 0; WL 208.1 AT PASSENGER CABIN 2022-441608 / [01] REPLACED ANGLE FLOOR STRUCTURE CENTER SECTION LOCATED ON BS 695 BL 0; WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 273A9110 SHEET 6 REV: A.;[02] TASK CARD COMPLETED

Part: NONE — CRACKED (FWD CARGO) · airframe 60,350 hrs · 35,654 cycles

CRACK ANGLE - CLIP BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT 2022-441606. / [01] REPLACED ANGLE - CLIP BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 5 REV:B.;[02] REPLACED ANGLE - CLIP BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 5 REV:B. SEE INDIVIDUAL SINGOFFS BELOW<BR>RII

Part: NONE — CRACKED (FWD CARGO) · airframe 60,350 hrs · 35,654 cycles

CRACK ANGLE - CLIP BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT 2022-441606. / [01] REPLACED ANGLE - CLIP BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 5 REV:B.;[02] REPLACED ANGLE - CLIP BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 5 REV:B. SEE INDIVIDUAL SINGOFFS BELOW<BR>RII

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 60,350 hrs · 35,654 cycles

CRACK SCUFF PLATE AFT CORNER AFT CARGO COMPARTMENT 2022-441553 / [01] DIGITAL CALIPER P/N: 500-197-30 S/N: A18229508; DUE DATE: 29-SEP-22.;[02] REPAIR SCUFF PLATE AFT CORNER AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[03] CORRECTED STEP 2: REPAIRED SCUFF PLATE AFT CORNER AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[04] STEP 3 VERIFIED AND CORRECTIVE ACTION COMPLETED : CORRECTED STEP 2: REPAIRED SCUFF PLATE AFT CORNER AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW .

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 60,350 hrs · 35,654 cycles

CRACKS FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2022-441554 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N B20189515; DUE DATE 30-NOV-22.;[02] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1; REPAIR 1 PARAGRAPH 4.B. AND BAC 5975. SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1; REPAIR 1 PARAGRAPH 4.B. AND BAC 5975. SEE INDIVIDUAL SIGNOFF BELOW.

Part: LENS — BROKEN (CABIN) · airframe 60,350 hrs · 35,654 cycles

BROKEN GALLEY 1 EXIT SIGN LENS AT FWD GALLEY AREA (1 EA) 2022-441537 / [01] REPLACED GALLEY 1 EXIT SIGN LENS AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51?01-960?802 STEP 3C(D) AND STEP 3C(10);[02] CORRECTED STEP 1 : REPLACED GALLEY 1 EXIT SIGN LENS AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51?01-960?802 STEP 3.C (5) (D) AND 3.C (10);[03] REPLACED GALLEY 1 EXIT SIGN LENS AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51?01-960?802 STEP 3.C (5) (D) AND 3.C (10)

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 60,350 hrs · 35,654 cycles

CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2022-441555 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A18229508; DUE DATE 29-SEP-22;[02] REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[03] STEP 2 VERIFIED AND CORRECTIVE ACTION COMPLETED: REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 60,350 hrs · 35,654 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2022-441552 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A18229508; DUE DATE 29-SEP-22;[02] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[03] STEP 2 VERIFIED AND CORRECTIVE ACTION COMPLETED: REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PLATE — CRACKED (R/H WING) · airframe 60,350 hrs · 35,654 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT URSS 261 AT RT WING 2022-441508 / [01] REMOVED CORRUGATED PLATE TRAILING EDGE LOCATED AT URSS 261 AT RT WING IAW B737-700 SRM 51-40-02 AND PERFORMED CLEAN ON CORRUGATED PLATE AND TRAILING EDGE LOCATED AT URSS 261 AT RT WING IAW SOPM 20-30-03 AND PERFORMED DETAIL VISUAL INSPECTION ON CORRUGATED PLATE AND NOT FOUND CRACK ONLY DIRTY AND NOT FOUND ADDITIONAL DAMAGE ON AREA INSTALLED CORRUGATED PLATE AND FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING 115A2001 REV -;[02] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: PLATE — CRACKED (L/H WING) · airframe 60,350 hrs · 35,654 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT URSS 261 AT LT WING 2022-441500 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT ORSS 261 AT LT WING I.A.W B737-700 SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT ORSS 261 AT LT WING I.A.W B737-700 SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW

Part: PLATE — CRACKED (RT WING TE) · airframe 60,350 hrs · 35,654 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT URSS 261 AT RT WING 2022-441508 /

Part: SUPPORT ANGLE — CORRODED (LAV FLOOR) · airframe 60,350 hrs · 35,654 cycles

CORROSIN LAVATORY A ON INTERNAL ANGLE FLOOR STRUCTURE AT FORWARD GALLEY AREA 1 EA 2022-441417. PERFORMED CLEAN ON INTERNAL ANGLE LOCATED ON LAVATORY A FLOOR STRUCTURE AT FORWARD GALLEY AREA IAW SOPM 20-30-03 AND PERFORMED VISUAL INSPECTION ANGLE LOC.PERFORMED CLEAN ON INTERNAL ANGLE LOCATED ON LAVATORY A FLOOR STRUCTURE AT FORWARD GALLEY AND NOT FOUND CORROSION ONLY DETERIORATED PROTECTIVE TREATMENT. APPLIED PROTECTIVE TREATMENT ON ANGLE LOCATED PERFORMED CLEAN ON INTERNAL ANGLE LOCATED ON LAVATORY A FLOOR STRUCTURE AT FORWARD GALLEY IAW SRM 51-20-01.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BS695 WL208.1 AND BL0 CENTER SECTION 2022-441392 / [01] REPLACED ANGLE FLOOR STRUCTURE AND FASTENERS LOCATED BS695 WL208.1 AND BL0 CENTER SECTION IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 273A9110 SHEET 6 REV: A. S

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK VERTICAL SUPPORT ANGLE LOCATED BS695 WL208.1 AND BL0 AT PASSENGER CABIN 2022-441393 / [01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: 48VFL11; S/N: AE-31448; DUE DATE: 14-JUN-23;[02] REPLACED VERTICAL SUPPORT ANGLE LOCATED BS695 WL208.1 AND BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 273A9110 SHEET 6 REV: A. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] TASK CARD COMPLETED

Part: NONE — CORRODED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BS986.5 AT RBL43 AND WL208.1 AT AFT GALLEY AREA 2022-441372 / [01] EQUIPMENT P/N 38DLPLUS; S/N 120398603; DUE DATE 18-OCT-22 WAS USED;[02] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 03-DEC-22;[03] TOOL USED FLAPSPEED PN: FPK-PRO-104; SN: PRO-3447; DUE DATE: 27-JUN-23;[04] REPAIRED FLOOR STRUCTURE BEAM UPPER CHORD LOCATED BS986.5 BTW RBL39 TO RBL 46 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4 AND FIGURE 205.;[05] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 03-DEC-22;[06] CORRECTED STEP 4 REPAIRED FLOOR STRUCTURE BEAM UPPER CHORD LOCATED BS986.5 BTW RBL39 TO RBL 46 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4 AND FIGURE 205; SEE INDIVIDUAL SIGN OFF BELOW;[07] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: WEB — CORRODED (AFT FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CORROSION WEB LOCATED BETWEEN BS1016 TO AFT PRESSURE BULKHEAD WL208.1 AND LBL18 AT AFT GALLEY AREA 2022-441367 / [01] REPLACED WEB LOCATED BETWEEN BS1016 TO AFT PRESSURE BULKHEAD WL208.1 AND LBL18 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02; 515-10-02 AND DRAWING 147A5600 SHEET 32 REV B; SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB LOCATED BETWEEN BS1016 TO AFT PRESSURE BULKHEAD WL208.1 AND LBL18 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02; 515-10-02 AND DRAWING 147A5600 SHEET 32 REV B; RII .SEE INDIVIDUAL SIGN OFF BELOW.

Part: BRACKET — CRACKED (L/H WING) · airframe 60,350 hrs · 35,654 cycles

CRACK TRAILING EDGE BRACKET AT LEVEL OF WS 204.25 AND BETWEEN ORSS 261 AND ORSS 297 AT LT WING 2022-441391 / [01] REPLACED BRACKET AT LEVEL OF WS 204.25 AND BETWEEN ORSS 261 AND ORRS 297 AT LT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2900 SHEET 1 REV 3;[02] VERIFIED STEP 1; COMPLETE

Part: STRAP — CORRODED (AFT FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CORROSION STRAP LOCATED BETWEEN BS1006 TO AFT PRESSURE BULKHEAD WL208.1 AND LBL3 AT AFT GALLEY AREA. REPLACED STRAP LOCATED BETWEEN BS1006 TO AFT PRESSURE BULKHEAD WL208.1 AND LBL3 AT AFT GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG# 147A5600 SHEET:32 REV:B.

Part: BEAM — CORRODED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BS986.5 WL208.1 AND BETWEEN LBL28 TO LBL43 AT AFT GALLEY AREA 2022-441373 / [01] TOOL P/N: 35DL; S/N: 091419910; CAL DUE: 26 -JAN-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 22-FEB-23.;[03] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 200048001; DUE DATE: 30-MAR-23;[04] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 200048001; DUE DATE: 30-MAR-23;[05] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 WL208.1 AND LBL28 AT AFT GALLEY AREA IAW EA M-21-153-00612 SEE INDIVIDUALS SIGN OFF BELOW;[06] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 WL208.1 AND LBL28 AT AFT GALLEY AREA IAW EA M-21-153-00612 SEE INDIVIDUALS SIGN OFF BELOW

Part: WEB — PERFORATED (AFT FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

PERFORATION ON WEB LOCATED BS1016 TO AFT PRESSURE BULKHEAD AND BL0 TO RBL38 AT AFT GALLEY AREA 2022-441366 / [01] REPLACED WEB LOCATED BS1016 TO AFT PRESSURE BULKHEAD AND BL0 TO RBL38 AT AFT GALLEY AREA I.A.W. B737-700 DWG# 147A5730 SHETT:23 REV: C AND SRM 51-40-02 AND 51-10-02;[02] CORRECTED STEP 1 REPLACED WEB LOCATED BS1016 TO AFT PRESSURE BULKHEAD AND BL0 TO RBL38 AT AFT GALLEY AREA I.A.W. B737-700 DWG# 147A5730 SHETT:23 REV: C AND SRM 51-40-02 AND 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 1 REPLACED WEB LOCATED BS1016 TO AFT PRESSURE BULKHEAD AND BL0 TO RBL38 AT AFT GALLEY AREA I.A.W. B737-700 DWG# 147A5730 SHETT:23 REV: C ; AND SRM 51-40-02 AND 51-10-02 ; RII .SEE INDIVIDUAL SIGN OFF BELOW .

Part: BRACKET — CRACKED (BS 540) · airframe 60,350 hrs · 35,654 cycles

CRACK BRACKET ASSY LOCATED BS540 BLEED AIR DUCT RH SIDE AT AIR CONDITIONING BAY 2022-441408.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BS695 AND RBL24 CENTER SECTION 2022-441395 / [01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: 48VFL11; S/N: AE-31448; DUE DATE: 14-JUN-23.;[02] REPLACED ANGLE FLOOR STRUCTURE AND FASTENERS LOCATED BS695 AND RBL24 CENTER SECTION IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 273A9110 SHEET 6 REV: A. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] TASK CARD COMPLETED

Part: STRAP — CORRODED (AFT FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CORROSION STRAP LOCATED BS1006 TO AFT PRESSURE BULKHEAD AT RBL3 AND WL208.1 AT AFT GALLEY AREA. REPLACED STRAP LOCATED BS1006 TO AFT PRESSURE BULKHEAD AT RBL3 AND WL208.1 AT AFT GALLEY AREA IAW SRM 51-10-02 AND DWG 147A5730, SHEET 23, REV C.

Part: NONE — CRACKED (CENTER WING) · airframe 60,350 hrs · 35,654 cycles

CRACK BRACKET ASSY LOCATED BS540 BLEED AIR DUCT LH SIDE AT AIR CONDITIONING BAY 2022-441403 / [01] REPLACED BRACKET ASSY LOCATED BS540 BLEED AIR DUCT LH SIDE AT AIR CONDITIONING BAY I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 AND DWG 212A1110 REV C;[02] TASK CARD COMPLETED

Part: NONE — CRACKED (CENTER WING) · airframe 60,350 hrs · 35,654 cycles

CRACK BRACKET ASSY LOCATED BS540 BLEED AIR DUCT RH SIDE AT AIR CONDITIONING BAY 2022-441408 / [01] REPLACED BRACKET ASSY LOCATED BS540 BLEED AIR DUCT RH SIDE AT AIR CONDITIONING BAY I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 AND DWG 212A1110 REV C;[02] TASK CARD COMPLETED

Part: BRACKET — CRACKED (BS 540) · airframe 60,350 hrs · 35,654 cycles

CRACK BRACKET ASSY LOCATED BS540 BLEED AIR DUCT LH SIDE AT AIR CONDITIONING BAY 2022-441403 /

Part: BRACKET — CORRODED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CORROSION SUPPORT BRACKET LOCATED BETWEEN BS312 WL208.1 AND LBL55 AT FWD GALLEY AREA 2022-441308 / [01] REPLACED SUPPORT BRACKET LOCATED BETWEEN BS312 WL208.1 AND LBL55 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELLOW;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELLOW

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK STRINGER 15L AND BS294.5 AT PASSENGER CABIN 2022-441290 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] PERFORMED REPAIR ON STRINGER 15L AND BS294.5 AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 ALTERNATIVE METHOD SEE INDIVIDUALS SIGN OFF BELOW;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS328 TO BS344 AND LBL46 FWD GALLEY AND LAV 2022-441306 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS328 TO BS344 AND LBL46 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400; SHEET 44; REV -.<BR>?SEE INDIVIDUAL SING-OFF BELOW?.;[02] CORRECTED STEP 1 REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS328 TO BS344 AND LBL46 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; 51-10-02 AND DWG 141A5400; SHEET 44; REV -.<BR>?SEE INDIVIDUAL SING-OFF BELOW?.;[03] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS328 TO BS344 AND LBL46 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; 51-10-02 AND DWG 141A5400; SHEET 44; REV -. <BR>?SEE INDIVIDUAL SING-OFF BELOW?. <BR><BR>COMPLETED AS RII

Part: STUB FRAME — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK STUB FRAME LOCATED BS294.5 AND BETWEEN STR7R TO STR9R AT PASSENGER CABIN 2022-441288 / [01] REPLACED STUB FRAME LOCATED BS294.5 AND BETWEEN STR7R TO STR9R AT PASSENGER CABIN IAW B737-700 SRM B737-700 SRM 51-10-02 ; 51-40-02 AND DRAWING 141A8370 REV D;[02] CORRECTED STEP 1 REPLACED STUB FRAME LOCATED BS294.5 AND BETWEEN STR7R TO STR9R AT PASSENGER CABIN IAW B737-700 SRM B737-700 SRM 51-10-02 ; 51-40-02 AND DRAWING 141A8370 REV D; SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED STUB FRAME LOCATED BS294.5 AND BETWEEN STR7R TO STR9R AT PASSENGER CABIN IAW B737-700 SRM B737-700 SRM 51-10-02 ; 51-40-02 AND DRAWING 141A8370 REV D; SEE INDIVIDUAL SIGN OFF BELOW

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK FRAME ON BS 312 AT LEVEL STR 5L FWD GALLEY AND LAV 2022-441285 / [01] PERFORMED PERMANENT REPAIR IAW EA M-22-153-01244 LOC. ON BS 312 AT LEVEL STR 5L FWD GALLEY AND LAV;[02] CERTIFIED WORK PERFORMED.

Part: BEAM — CORRODED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BS312 AT LBL13 TO LBL15 AND WL208.1 AT FWD GALLEY AREA 2022-441307 / [01] TOOL USED ULTRASONIC EQUIPMENT PN: 35DL; SN: 091419910; DUE DATE: 26 JAN 23;[02] TOOL USED CALIPER PN: 500-197-30; SN: 15120589; DUE DATE: 28-NOV-22;[03] TOOL P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 26-JAN-23.;[04] TOOL P/N: NORTEC 500D; S/N: N500X12101V022240; CAL DUE: 27-JAN-23.;[05] TOOL P/N: NORTEC 500D; S/N: N500X12101V022240; CAL DUE: 27-JAN-23.;[06] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[07] PERFORMED REPAIR ON TRANSVERSAL BEAM AT BSTA 312 BTW LBL 30 & RBL 30 IAW EA 22-153-02693 SEE INDIVIDUALS SIGN OFF BELOW;[08] PERFORMED REPAIR ON TRANSVERSAL BEAM AT BSTA 312 BTW LBL 30 & RBL 30 IAW EA 22-153-02693 SEE INDIVIDUALS SIGN OFF BELOW<BR>CERTIFIED AS RII;[09] PERFORMED REPAIR ON TRANSVERSAL BEAM AT BSTA 312 BTW LBL 30 & RBL 30 IAW EA 22-153-02693 SEE INDIVIDUALS SIGN OFF BELOW <BR>CERTIFIED AS RII

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK STRINGER 7L AND BS294.5 AT PASSENGER CABIN 2022-441287 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[03] PERFORMED REPAIR LOC AT STRINGER 7L AND BTW BS294.5 AND BS 277 AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. THIS REPAIR IS CATEGORY ?B?.<BR> SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED REPAIR LOC AT STRINGER 7L AND BTW BS294.5 AND BS 277 AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. THIS REPAIR IS CATEGORY ?B?. <BR> SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: NONE — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK INNER CHORD LOCATED BS294.5 TO BS312 AT LBL55 AT FWD GALLEY AREA 2022-441300 / [01] REPLACED INNER CHORD LOCATED BTW BS277 TO BS360 AT LBL55 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; 51-10-02 AND DRAWING # 141A8110 REV - SEE INDIVIDUALS SIGN OFF BELOW;[02] REPLACED INNER CHORD LOCATED BTW BS277 TO BS360 AT LBL55 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; 51-10-02 AND DRAWING # 141A8110 REV - SEE INDIVIDUALS SIGN OFF BELOW<BR>RII ACCOMPLISHED

Part: NONE — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS312 TO BS328 AND LBL46 FWD GALLEY AND LAV 2022-441305 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS312 TO BS328 AND LBL46 FWD GALLEY AND LAV AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400; SHEET 26; REV -. ?SEE INDIVIDUAL SING-OFF BELOW?.;[02] CORRECTED STEP 1 REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS312 TO BS328 AND LBL46 FWD GALLEY AND LAV AND LAV IAW B737-700 SRM 51-40-02 ; 51-10-02 AND DWG 141A5400; SHEET 26; REV -. ?SEE INDIVIDUAL SING-OFF BELOW?.;[03] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS312 TO BS328 AND LBL46 FWD GALLEY AND LAV AND LAV IAW B737-700 SRM 51-40-02 ; 51-10-02 AND DWG 141A5400; SHEET 26; REV -. ?SEE INDIVIDUAL SING-OFF BELOW?<BR><BR>CERTIFIED AS RII

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK SUPPORT ANGLE LOCATED BS294.5 AND STR13L AT PASSENGER CABIN 2022-441293 / [01] REPLACED SUPPORT ANGLE LOCATED BS294.5 AND STR13L AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; DWG 141A1311 SHEET 1 REV:C AND SRM 51-40-02; SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK STRINGER 16L AND BS294.5 AT PASSENGER CABIN 2022-441292 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] PERFORMED REPAIR ON STRINGER 16L LOCATED BS 294.5 AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1; REPAIR 1 FIGURE 206 SEE INDIVIDUAL SIGN OFFS BELOW;[03] PERFORMED REPAIR ON STRINGER 16L LOCATED BS 294.5 AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1; REPAIR 1 FIGURE 206 SEE INDIVIDUAL SIGN OFFS BELOW RII

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AT BL0 FWD GALLEY AND LAV 2022-441299 / [01] REPLACED WEB - INTERCOSTAL ON FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AT BL0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400; SHEET 20; REV - ?SEE INDIVIDUAL SING-OFF BELOW?.;[02] CORRECTED STEP 1 REPLACED WEB - INTERCOSTAL ON FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AT BL0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40- 02; 51-10-02 AND DWG 141A5400; SHEET 20; REV - ?SEE INDIVIDUAL SING-OFF BELOW?.;[03] REPLACED WEB - INTERCOSTAL ON FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AT BL0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40- 02; 51-10-02 AND DWG 141A5400; SHEET 20; REV - ?SEE INDIVIDUAL SING-OFF BELOW?. <BR><BR>CERTIFIED AS RII

Part: INTERCOSTAL — CORRODED (FWD FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CORROSION FLOOR STRUCTURE INTERCOSTAL LOCATED BS294.5 TO BS312 AT RBL11 AND WL208.1 AT FWD GALLEY AREA 2022-441302 / [01] REPLACED FLOOR STRUCTURE INTERCOSTAL LOCATED BS294.5 TO BS312 AT RBL11 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; DWG 141A5400 SHEET: 8; REV: -. AND SRM 51-40-02; SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED FLOOR STRUCTURE INTERCOSTAL LOCATED BS294.5 TO BS312 AT RBL11 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; DWG 141A5400 SHEET: 8; REV: -. AND SRM 51-40-02; SEE INDIVIDUAL SIGN OFFS BELOW.<BR><BR>RII ACCOMPLISHED

Part: NONE — CORRODED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CORROSION INNER CHORD LOCATED BS294.5 TO BS344 AT RBL57 AND WL208.1 AT FWD GALLEY AREA 2022-441304 / [01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 130066701; CAL DUE DATE: 08-APR-23;[02] REPLACED INNER CHORD AND FASTENERS LOCATED BS259 TO BS360 AT RBL57 AND WL208.1 AT FWD GALLEY ARE IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING # 141A8310 REV 'B';[03] CORRECTED STEP 2. REPLACED INNER CHORD AND FASTENERS LOCATED BS259 TO BS360 AT RBL57 AND WL208.1 AT FWD GALLEY ARE IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING # 141A8310 REV 'B'. SEE INDIVIDUAL SIGN OFF BELOW.;[04] CORRECTED STEP 2. REPLACED INNER CHORD AND FASTENERS LOCATED BS259 TO BS360 AT RBL57 AND WL208.1 AT FWD GALLEY ARE IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING # 141A8310 REV 'B'. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII ACCOMPLISHED

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2022-441286 / [01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV -. SEE INDIVIDUAL SIGN OFFS BELOW;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: BEAM — CORRODED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BS328 AT RBL39 TO RBL42 AND WL208.1 AT FWD GALLEY AREA 2022-441309 / [01] TOOL USED ULTRASONIC EQUIPMENT PN: 35DL; SN: 091419910; DUE DATE: 26 JAN 23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23;[03] PERFORMED REPAIR ON FLOOR STRUCTURE BEAM LOCATED BS328 BTW LBL6 TO RBL64 AND WL208.1 IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 ALTERNATIVE 2 SEE INDIVIDUALS SIGN OFF BELOW;[04] PERFORMED REPAIR ON FLOOR STRUCTURE BEAM LOCATED BS328 BTW LBL6 TO RBL64 AND WL208.1 IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 ALTERNATIVE 2 SEE INDIVIDUALS SIGN OFF BELOW<BR>RII ACCOMPLISHED

Part: WEB — CRACKED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CRACK WEB LOCATED BS294.5 TO BS303.9 AND STR15L AT PASSENGER CABIN 2022-441291 / [01] REPLACED WEB LOCATED BS294.5 TO BS303.9 AND STR15L AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING# 141A8180 SHEET 3 REV: A.;[02] CORRECTED STEP 1. REPLACED WEB LOCATED BS294.5 TO BS303.9 AND STR15L AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING# 141A8180 SHEET 3 REV: A. SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 60,350 hrs · 35,654 cycles

CORROSION SUPPORT BRACKET LOCATED BS344 WL208.1 AND LBL58 AT FWD GALLEY AREA 2022-441310 / [01] REPLACED SUPPORT BRACKET LOCATED BS344 WL208.1 AND LBL58 AT FWD GALLEY AREA IAW B737-700 SM 51-40-02 AND SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELLOW;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELLOW

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 60,350 hrs · 35,654 cycles

CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 26.3 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.125 INCH 2022-441278 / [01] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 03-DEC-22;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030456 DUE DATE: 26 JAN 23;[03] REPAIRED LH HORIZONTAL STABILIZER LOWER SKIN AT SSTA 184.70. IAW EA#22-155-02744-WIP1 AND EA# 22-155-02744;[04] TASK CARD COMPLETED RII CERTIFIED

Part: NONE — CRACKED (AFT CARGO) · airframe 60,350 hrs · 35,654 cycles

CRACK WEB - INTERCOSTAL LOCATED BS947 RBL21 AND WL170 AT AFT CARGO COMPARTMENT 2022-441269 / [01] REPLACED NEW WEB - INTERCOSTAL LOCATED BTW BS 927 TO BS947 RBL21 AND WL170 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG #147A7500 SHEET:19 REV:-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED NEW WEB - INTERCOSTAL LOCATED BTW BS 927 TO BS947 RBL21 AND WL170 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG #147A7500 SHEET:19 REV:-. RII .SEE INDIVIDUAL SIGN OFFS BELOW.

Part: NONE — CORRODED (AFT CARGO) · airframe 60,350 hrs · 35,654 cycles

CORROSION SUPPORT ZEE LOCTAED BS727D LBL21 AND WL156 AFT CARGO COMPARTMENT 2022-441273 / [01] PERFORMED REPAIR ON SUPPORT ZEE LOCATED BS 727E TO BS 747 I.A.W B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND REPLACED SUPPORT ZEE BTW BS 727 TO BS 847 AT LBL 21 IAW B737-700 SRM 51-10-02; 51-40-02 AND DRAWING 146A7500 REV -; SEE INDIVIDUAL SIGN OFF BELOW;[02] PERFORMED REPAIR ON SUPPORT ZEE LOCATED BS 727E TO BS 747 I.A.W B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND REPLACED SUPPORT ZEE BTW BS 727 TO BS 847 AT LBL 21 IAW B737-700 SRM 51-10-02; 51-40-02 AND DRAWING 146A7500 REV -; SEE INDIVIDUAL SIGN OFF BELOW<BR><BR>RII ACCOMPLISHED

Part: NONE — CRACKED (AFT CARGO) · airframe 60,350 hrs · 35,654 cycles

CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 13INCH AND RBL13 AT AFT CARGO COMPARTMENT 2022-441272 / [01] REPLACED ANGLE-SUPPORT AND LOCATED BS907 PLUS 13INCH AND RBL13 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 17. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — CORRODED (AFT CARGO) · airframe 60,350 hrs · 35,654 cycles

CORROSION SUPPORT ZEE LOCATED BS727E PLUS 10INCH RBL 21 AND WL156 AFT CARGO COMPARTMENT 2022-441275 / [01] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 RBL 21 AND WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 AND DRAWING 146A7500 REV -;[02] CORRECTED STEP 1 REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 RBL 21 AND WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 AND DRAWING 146A7500 REV -; SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 RBL 21 AND WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 AND DRAWING 146A7500 REV -; SEE INDIVIDUAL SIGN OFF BELOW<BR>CERTIFIED AS RII

Part: NONE — CORRODED (AFT CARGO) · airframe 60,350 hrs · 35,654 cycles

CORROSION WEB - INTERCOSTAL LOCATED BS727B RBL13 AND WL150 AT AFT CARGO COMPARTMENT 2022-441276 / [01] TOOL USED: P/N 35DL S/N 091419910 DUE DATE: 26-JAN-23.;[02] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED BS727B RBL13 AND WL150 AT AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-40-02; B737-SRM 51-10-02 ITEM 9; AND DWG 146A7505 SHEET 86 REV A; SEE INDIVIDUAL SIGNS-OFF BELOW.;[03] CORRECTED STEP 2:<BR>EVALUATED REWORKED AREA ON WEB-INTERCOSTAL LOCATED BS727B RBL13 AND WL150 AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 PARAGRAPH 4.C.(1)(B) DETAIL D; FIGURE 103; NOMINAL THICKNESS OF WEB-INTERCOSTAL LOCATED BS727B RBL13 AND WL150 AT AFT CARGO COMPARTMENT IS: 0.045' IAW B737-700 SRM 53-60-53-0I-2 TABLE 2; FIGURE 2; MRT ON REWORKED AREA IS =0.042 INCHES. IAW NDT MANUAL 51-00-00 PART 4 PROCEDURE 3 . TOOL USED: P/N 35DL S/N 091419910 DUE DATE: 26-JAN-23.;[04] EVALUATED REWORKED AREA ON WEB-INTERCOSTAL LOCATED BS727B RBL13 AND WL150 AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 PARAGRAPH 4.C.(1)(B) DETAIL D; FIGURE 103; NOMINAL THICKNESS OF WEB-INTERCOSTAL LOCATED BS727B RBL13 AND WL150 AT AFT CARGO COMPARTMENT IS: 0.045' IAW B737-700 SRM 53-60-53-0I-2 TABLE 2; FIGURE 2; MRT ON REWORKED AREA IS =0.042 INCHES. IAW NDT MANUAL 51-00-00 PART 4 PROCEDURE 3 . TOOL USED: P/N 35DL S/N 091419910 DUE DATE: 26-JAN-23. RII

Part: SUPPORT — CRACKED (AFT CARGO) · airframe 60,350 hrs · 35,654 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS907 PLUS 8INCH AND RBL13 AT AFT CARGO COMPARTMENT 2022-441271 / [01] REPLACED ANGLE-SUPPORT LOCATED ON BS907 PLUS 8INCH AND RBL13 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 17 REV. D. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 60,350 hrs · 35,654 cycles

CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 26.3 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.125 INCH 2022-441278 / [01] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 03-DEC-22;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030456 DUE DATE: 26 JAN 23

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 60,350 hrs · 35,654 cycles

CRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 203.10 RIB; 24.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.510 INCH 2022-441277 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN/ NORTEC 600D; SN/ 60009161631; DUE DATE/ 03-DEC-22.;[02] REPAIRED RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 203.10 RIB IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11. THE TOTAL OUTBOARD WIDTH ACROSS THE INSPAR SKIN REPAIR AREA NOT EXCEED 66 INCHES. ELEVATOR POWER-OFF FLIGHT TEST IS NOT NECESSARY.;[03] TASK CARD COMPLETED RII CERTIFIED

Part: NONE — DEBONDED (L/H WING) · airframe 60,350 hrs · 35,654 cycles

DEBONDED O/B AFT FLAP LOWER SURFACE AT LT WING. PERFORMED INTERIM REPAIR ON O/B AFT FLAP LOWER SURFACE AT LT WING IAW SRM SRM 57-53-01-2R-16 REPAIR 16.

Part: FITTING — DETERIORATED (L1 DOOR) · airframe 60,350 hrs · 35,654 cycles

DETERIORATED ENTRY DOOR HARDWARE AND PLATE GIRT BAR FITTING AT AFT GALLEY AREA 2022-441132 / [01] REPLECED ENTRY DOOR HARDWARE AND PLATE GIRT BAR FITTING AT AFT GALLEY AREA IAW BOEING 737-700 AMM 25-66-02-400-801-NG;[02] TASK CARD COMPLETED

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 60,350 hrs · 35,654 cycles

CRACK INSPAR RIB LOCATED STAB STA 111.10 AND 29 INCHES FROM FRONT SPAR LT HORIZONTAL STAB 2022-441142 / [01] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 210138003 AND DUE DATE: 22-FEB-23.;[02] ET TOOL USED: PN: MIZ-21C ; SN: 769680; DUE DATE: 07-JUL-23;[03] PERFORMED REPAIR ON INSPAR RIB LOCATED STAB STA 111.10 AND 29 INCHES FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4 SEE INDIVIDUALS SIGN OFF BELOW;[04] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 60,350 hrs · 35,654 cycles

CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 18.5 INCHES FROM FRONT SPAR AT RT HORIZONTAL STABILIZER 2022-441147 / [01] TOOL P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 26-JAN-23.;[02] TOOL P/N: NORTEC 500D; S/N: N500X12101V022240; CAL DUE: 27-JAN-23.;[03] PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED STAB STA 129.50 AND 18.5 INCHES FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN OFFS BELOW.;[04] PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED STAB STA 129.50 AND 18.5 INCHES FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN OFFS BELOW.<BR>RII

Part: FITTING — DETERIORATED (R2 DOOR) · airframe 60,350 hrs · 35,654 cycles

DETERIORATED SERVICE DOOR HARDWARE AND PLATE GIRT BAR FITTING AT AFT GALLEY AREA 2022-441133 / [01] REPLACED SERVICE DOOR HARDWARE AND PLATE GIRT BAR FITTING AT AFT GALLEY AREA IAW BOEING 737-700 AMM 25-66-02-400-801-NG;[02] TASK CARD COMPLETED

Part: NONE — DETERIORATED (FWD SERVICE DOOR) · airframe 60,350 hrs · 35,654 cycles

DETERIORATED SERVICE DOOR HARDWARE AND PLATE GIRT BAR FITTING AT FWD GALLEY AREA 2022-441130 / [01] REPLACED SERVICE DOOR HARDWARE AND PLATE GIRT BAR FITTING AT FWD GALLEY AREA I.A.W B737-700 AMM-25-66-02-400-801;[02] TASK COMPLETED

Part: NONE — DETERIORATED (FWD ENTRY DOOR) · airframe 60,350 hrs · 35,654 cycles

DETERIORATED ENTRY DOOR HARDWARE AND PLATE GIRT BAR FITTING AT FWD GALLEY AREA 2022-441129 / [01] REPLACED ENTRY DOOR HARDWARE AND PLATE GIRT BAR FITTING AT FWD GALLEY AREA I.A.W B737-700 AMM-25-66-02-400-801;[02] TASK COMPLETED

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 60,350 hrs · 35,654 cycles

CRACK LEADING EDGE SKIN RIB L/E STA 105.26 AT LT HORIZONTAL STABILIZER 2022-441098 / [01] DRILLED NEW RIB I.A.W B373-700 SRM 51-20-07-0G-0 REV.77 10-JU-22 AND APPLIED PROTECTIVE TREATMENT ON NEW HOLE I.A.W. B737-700 SRM 51-20-01-0G-0 REV.77 10-JUL-22 AND OBTAINED OK TO INSTALL OF NEW RIB AND FASTENERS;[02] STEP 1 ENTER ERROR;[03] REPLACED RIB AND FASTENERS ON LEADING EGDE OF LH HORIZONTAL STABILIZER AT LEVEL LE STA 105.26 IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02 AND DRAWING# 186A1001 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[04] TASK CARD COMPLETED RII CERTIFIED

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 60,350 hrs · 35,654 cycles

CRACK LEADING EDGE SKIN RIB ON L/E STA 105.26 AT RT HORIZONTAL STABILIZER 2022-441103 / [01] REPLACED RIB LOC. LEADING EDGE STA 105.26 AT RT HORIZONTAL STABILIZER B737-700 SRM 51-10-02 ITEM:9; SRM 51-40-02 AND DWG 186A1001; SHEET:10 REV:A SHEET 10; SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: BATTERY PACK — INOPERATIVE (FWD CABIN) · airframe 60,350 hrs · 35,654 cycles

INOP CEILING PANEL BATTERY PACK LT SIDE AT FWD GALLEY AREA (1 EA) 2022-441043 / [01] REPLACED CEILING PANEL BATTERY PACK LT SIDE AT FWD GALLEY AREA IAW B737-700 AMM-33-51-06-960-805 TEST IS GOOD;[02] REPLACED CEILING PANEL BATTERY PACK LT SIDE AT FWD GALLEY AREA IAW B737-700 AMM-33-51-06-960-805 TEST IS GOOD

Part: RIB — CRACKED (LMLG DOOR) · airframe 60,228 hrs · 35,576 cycles

LH MLG CENTER DOOR HAS A .5 CRACK ON INNER RIB JUST ABOVE THE BOTTOM FORWARD HINGE CONNECTION BRACKET. HFEC VERIFIED PER NDT 51-00-00 PART 6; PROCEDURE 23. / [01] REMOVED CENTER + INNER L/H MLG DOOR PER AMM 32-13-11

Part: PLATE — CRACKED (FUSELAGE) · airframe 59,931 hrs · 35,370 cycles

DURING ACCOMPLISHMENT OF 22-153-01522-WIP1[TTG8Q00D7FVA]; OVERSIZED REPAIR FASTENER HOLE LOCATED AT BS 922; S-27R FOUND TO HAVE VISIBLE INTERNAL EDGE DAMAGE AND HFEC HOLE PROBE CRACK INDICATION. / [01] REPAIRED FASTENER HOLE PER EA 22-153-01522.;[02] REPAIRED FASTENER HOLE PER EA 22-153-01522

Part: LIGHT — INOPERATIVE (R/H CABIN) · airframe 59,188 hrs · 34,873 cycles

ROW 12 RIGHT SIDE SIDEWALL LIGHT INOP / [01] TROUBLESHOT SIDEWALL LIGHT AT ROW 12 INOP IN REF TO FIM 33-20-00. SUSPECT BAD LIGHT ASSEMBLY. MEL REMAINS ACTIVE.;[02] R&R SIDEWALL LIGHT ASSY AT SEAT ROW 12 RIGHT SIDE PER AMM 33-51-04; OPS CHECK GOOD

Part: ANGLE — CRACKED (CENTER WING) · airframe 58,938 hrs · 34,716 cycles

RIGHT AC BAY; CRACK INDICATION STATION 663 RBL 8 AT FASTENER HOLE. MARKED 234/02 RIGHT AC BAY CRACK INDICATION STATION 663 RBL 8 AT FASTENER HOLE. MARKED 234/02 / [01] CUT AND REMOVED DAMAGED SECTION OF ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5;[02] PERFORMED DVI OF REPAIR AREA. NO DEFECTS NOTED IAW SRM 57-10-10-2R-5 REPAIR 5;[03] VERIFIED STEPS 1-2;[04] PERFORMED NDT IAW B737 NDT PT. 6; 51-00-00 PROC 16. NO DEFECTS NOTED. TOOL # 36303 CAL DUE 13APR22;[05] VERIFIED REPAIR PART AS -1 P/N 43226-6000-0001 REPLACEMENT ANGLE AND -2 P/N 43226-6000-0002 SPLICE ANGLE PER AARFORM 600 IAW ARM 57-10-10-2R-5 REPAIR 5 TABLE 201;[06] INSPECTION VERIFIED ON SHOP WORK ORDER;[07] ACCOMPLISHED HFEC IAW B737 NDT PART 6; 51-00-00 PROCEDURE 23 AT EDGE OF CUTOUT. NO DEFECTS NOTED. TOOL 40083 DUE 14SEP22;[08] STARTED FABRICATING REPAIR PARTS -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE FOR STEP4 E OF SRM 57-10-10-2R-5 REPAIR 5;[09] INSPECTION CW STEP 8;[10] FINISHED FABRICATING REPAIR PARTS -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE IAW SRM 57-10-10-2R-5 PARAGRAPH 4 E. NEED OK TO TREAT AND PRIME FOR REPAIR PARTS.;

Part: ANGLE — CRACKED (CENTER WING) · airframe 58,938 hrs · 34,716 cycles

LEFT AC BAY; CRACK INDICATION STATION 663 LBL 8 AT FASTENER HOLE. MARKED DOT 234/01 LEFT AC BAY CRACK INDICATION STATION 663 LBL 8 AT FASTENER HOLE. MARKED DOT 234/01 / [01] CUT AND REMOVED DAMAGED SECTION OF ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5;[02] PERFORMED DVI OF REPAIR AREA. NO DEFECTS NOTED IAW SRM 57-10-10-2R-5 REPAIR 5;[03] VERIFIED STEPS 1-2;[04] PERFORMED NDT IAW B737 NDT PT. 6; 51-00-00 PROC 16. NO DEFECTS NOTED. TOOL # 36303 CAL DUE 13APR22;[05] VERIFIED NEW MATERIALS OF REPLACEMENT ANGLE AS 43226-5000-0001 AND SPLICE ANGLE 43226-5000-0002 I/A/W SRM 57-10-10-2R-5 REPAIR 5 STEP 4 E;[06] INSPECTION VERIFIED STEP 5; ON SHOP WORK ORDERS;[07] ACCOMPLISHED HFEC IAW B737 NDT PART 6; 51-00-00 PROCEDURE 23 AT EDGE OF CUTOUT; NO DEFECTS NOTED. TOOL 49983 DUE 14SEP22;[08] STARTED FABRICATING -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE I/A/W SRM 57-10-10-2R-5 REPAIR 5 STEP 4E;[09] INSPECTION CW STEP 8;[10] COMPLETED FABRICATION; LOCATING; AND DRILLING OF -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE I/A/W BOEING SRM 57-10-10-2R-5 REPAIR 5 STEP 4.E.;TREATED AND PRIMED REPAIR PARTS I/A/W B737 SRM 57-10-10-2R-5 REPAIR 5.; INSTALLED REPAIR PARTS I/A/W B737 SRM 57-10-10-2R-5 REPAIR 5.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 58,938 hrs · 34,716 cycles

CABIN FLOOR PANEL 232SF AFT I/B CORNER DELAMINATED DOT 5 / [01] EVALUATED PANEL 232SF AND FOUND DAMAGE TO AFT I/B CORNER. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-10 PAR 1A REV 75. CLEAN AND PREP PANEL FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-10 PAR 3 A-D. APPLIED POTTING COMPOUND. IAW B737-700 SRM 53-00-50-2R-10 PAR 3E-G REV 75. (A101798) AAR DIGITAL THERMOMETER 30347 150DEG 3HRS.;[02] REPAIRED DAMAGED EDGE AFT I/B CORNER ON PANEL 232SF. IAW B737-700 SRM 53-00-50-2R-10; SRM 53-00-50-2R-0.

Part: FLAP — DELAMINATED (L/H WING) · airframe 58,938 hrs · 34,716 cycles

LH O/B AFT FLAP INBD CORNER HAS EVIDENCE OF DELAM / [01] EVALUATED L/H O/B AFT FLAP INBD CORNER. FOUND AREA OF LESS THAN .50' IN DEPTH & 1.250' IN LENGTH DELAMINATION. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 57-53-01-2R-4 PAR1A & 3B REV 75. CLEAN AND PREP AREA FOR REPAIR. IAW B737-700 SRM 51-70-10-2R-1 PAR 3 A-C. APPLIED RESIN (A106472). IAW B737-700 SRM 51-70-10-2R-1 PAR 3 D-G. AAR DIGITAL THERMOMETER 30347 140DEG 3HRS. TAP TEST GOOD.;[02] REPAIRED AREA OF DELAMINATION ON L/W O/B AFT FLAP INBD CORNER. IAW B737-700 SRM 57-53-01-2R-4; SRM 51-70-10-2R-1.;[03] VERIFIED STEP 1;2<BR>C/W

Part: PANEL — ELONGATED (FUSELAGE) · airframe 58,361 hrs · 34,369 cycles

SUPPLEMENTAL INFORMATION: 194E PANEL HAS 2 ELONGATED HOLES / [01] INSTALLED PANEL 194E

Part: PANEL — CRACKED (FUSELAGE) · airframe 58,361 hrs · 34,369 cycles

SUPPLEMENTAL INFORMATION: 194E PANEL HAS 3 CRACKED HOLES / [01] REPLACED PANEL 194E

Part: ENGINE — FAILED (NR 2) · airframe 57,612 hrs · 33,905 cycles

IN CRUISE AT FL 330 WE HEARD A LOUD BANG THEN ENGINE NUMBER 2 FAILED. AFTER COMPLETING ENGINE FAILURE QRH AND ENGINE INFLIGHT START QRH WE WERE ABLE TO RESTART ENG #2. ; NO INDICATION OF FIRE OR ABNORMAL ENGINE INDICATIONS. LANDING WEIGHT WAS 124.1 / [01] R&R'D #2 ENGINE PER TASK CARD TTG8Q0064PNJ. OPS. AND LEAK CHECK GOOD. ENGINE OFF: CFM56-7B24 SER.# OFF: 892201 ENGINE ON: CFM56-7B24/3 SER.#ON: 802330; [02] R&R'D #2 ENGINE PER MT# 771-00-01.; [03] CERTIFIED

Part: WARNING MESSAGE — ILLUMINATED (NR 2 ENGINE) · airframe 57,610 hrs · 33,903 cycles

#2 EEC AND CAUTION LIGHT ILLUMINATED ALONG WITH TOWER REPORTED SMOKE/FLAMES FROM #2. NO EXCEEDANCES OR FIRE INDICATIONS IN FLIGHT DECK. ; / [01] R&R'D FRONT AND REAR SPINNER PER AMM 72-21-01FOR F.O.M AND PRIMARY EXHAUST PLUG; TAIL PIPE NOZZLE PER AMM 78-11-02; 78-11-01 FOR GEOWS WORK ORDER #10175395. LEAK CHECK TEST 3A PER AMM 71-00-00 WAS GOOD.

Part: COLLAR — MISSING (L1 DOOR HANDLE) · airframe 55,155 hrs · 32,453 cycles

L1 AND R2 DOORWAY ASSIST HANDLES ARE MISSING THE COLLARS. INSTALLED L1 AND R2 DOOR WAY ASSIST HANDLES COLLARS, AS PER B737-700 AMM 25-21-31-420-801.

Part: COLLAR — MISSING (R2 DOOR HANDLE) · airframe 55,155 hrs · 32,453 cycles

L1 AND R2 DOORWAY ASSIST HANDLES ARE MISSING THE COLLARS. INSTALLED L1 AND R2 DOOR WAY ASSIST HANDLES COLLARS, AS PER B737-700 AMM 25-21-31-420-801.

Part: HOUSING — CORRODED (R1 DOOR HANDLE) · airframe 55,155 hrs · 32,453 cycles

** CORROSION ** R-1 DOOR HANDLE BOX ATTACHING FASTENER HOLE UPPER LOWER MKD DOT 60-035 / REPAIRED CORRODED FASTENER HOLE AT R1 DOOR HANDLE BOX UPPER AREA LOWER POSITION PER CMM 52-41-05 REPAIR 20-2 BY OUTSIDE VENDOR PO#1689056

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 55,155 hrs · 32,453 cycles

RIGHT HORIZONTAL STAB LE RIB CHORD HAS CRACK AT STA 114.55. REMOVED AND REPLACED RT HORIZ STAB L/E RIB CHORD AT STA 114.55, PER B737-700 SRM 51-40-02-0G-0 AND DRWG NR 186A1305.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 55,155 hrs · 32,453 cycles

RIGHT HORIZONTAL STAB LE HAS A CRACKED CHORD AT STA 95.96. PEFORMED REPAIR AT RT HORIZONTAL STAB L/E RIB NR 3 AT STA 95.96, IAW B737 SRM 51-70-11-2R-0. RR 31998 09/10/20.

Part: PANEL — CORRODED (LT MLG WW) · airframe 55,155 hrs · 32,453 cycles

CORROSION ON NLG WW LT AFT PANEL 113BW AN MATING SURFACE HAS FRETTING CORROSION MKD DOT 60-029 / AFTER FURTHER VISUAL INSPECTION ON NLG WHEEL WELL CAVITY AFT PANEL (DOOR) #113BW FOUND FRETTING CORROSION AROUND INSTALLATION HOLES TO DEEP. FOUND OUT OF LIMITS DUE TO PROXIMITY TO THE INSTALLATION HOLES. REPLACED PANEL (DOOR) REF B737-700 SRM 53-10-14-1A-2 AND AMM 53-14-01-420-801. PANEL #113BW WILL BE INSTALLED ON ROUTINE CARD # JPANEL-115-CLOSE

Part: NUT PLATE — BROKEN (R1 DOOR SLIDE) · airframe 55,155 hrs · 32,453 cycles

R-1 DOOR SLIDE PACK AFT MOUNT BRACKET SUPPORT ATTACHED NUT PLATE IS BROKEN MKD DOT 60-025 / REMOVED AND REPLACED NUT PLATE AT R-1 DOOR SLIDE PACK AFT BRACKET SUPPORT AS PER SRM 51-40-02-0G-0

Part: SUPPORT ANGLE — CRACKED (BS 867 S27L) · airframe 55,155 hrs · 32,453 cycles

SUPPORT ANGLE CRACKED AT AFT CARGO COMPMT. WASTE TANK AFT FRAME POST LOWER ATTACHMENT INB. S-27L STA 867 MKD DOT / REMOVED AND REPLACED ANGLE BRACKET AT AFT CARGO COMPT. WASTE TANK AFT FRAME POST LOWER AS PER REF B737-700 SRM 51-40-02-0G-0 AND DWG #149A8102 STA 867 AND S-27L.

Part: SUPPORT BRACKET — CRACKED (BS 727) · airframe 55,155 hrs · 32,453 cycles

SUPPORT BRACKET CRACKED AT AFT CARGO COMPMT .FWD BULKHEAD STA 727 LOWER BL-0 MKD DOT 60-003 / REPLACED SUPPORT BRACKET AT AFT CARGO COMPMT. FWD BULKHEAD STA 727 LOWER AS PER REF B737-700 SRM 51-40-02-0G-0 AND DRAWING 144A2600.

Part: BEAM — CRACKED (R1 DOOR) · airframe 55,155 hrs · 32,453 cycles

FWD SERVICE DOOR NR 4 DOOR MECHANISM BEAM HAS CRACK ON THE UPPER INBOARD RADIUS, MARKED R1 DOOR. REMOVED AND REPLACED FWD SERVICE DOOR (R1) NR 4 BEAM PER DRWG NR 141A6516; 141A6535 AND B737-700 SRM 51-40-02-0G-0. REF WORK INSTRUCTIONS NR 5241-C-14093-NG.

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 55,155 hrs · 32,453 cycles

FWD SERVICE DOOR NR 5 DOOR MECHANISM BEAM HAS CRACK ON THE UPPER INBOARD RADIUS, MARKED (R1 DOOR). REMOVED & REPLACED FWD SERVICE DOOR NR 5 BEAM, PER B737-700 SRM 51-40-02-0G-0 ; 51-40-05-0G-0; DRAW & 141A6516 & 141A6535.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 55,155 hrs · 32,453 cycles

CABIN FLOOR PANELS SUPPORT ANGLES LT AND RT AT B.L. ZERO STATION 540 HAVE CRACKS AT ATTACHMENTS. / REMOVED AND REPLACED FLOOR SUPPORT ANGLES LT AND RT B.L. ZERO STA 540. AS PER SRM : 51-40-02-0G-0 AND REINSTALL FLOOR PANEL # 231UF AS PER SRM 53-21-00-000-801.

Part: FLOORBEAM — CORRODED (BS 270) · airframe 55,155 hrs · 32,453 cycles

CORROSION, FLIGHT DECK FLOOR STRUCTURE AT STA 270 FORWARD SIDE OF LATERAL BEAM BETWEEN LBL 10 TO RBL 10 WL 208.1 HAS SPOTS OF CORROSION, MARKED 78-8. REPAIRED FLIGHT DECK FLOOR STRUCTURE AT STA 270 FWD SIDE OF LATERAL BEAM BETWEEN LBL 10 TO RBL 10 WL 208.1, AS PER REF B737-700 SRM 51-40-02-0G-0 AND EA 1-A53-13812-REV 2. CUSTOMER CARD EA 1-A53-13812/W1501691. MEASURES AFTER REMOVED CORROSION: ORIGINAL THICKNESS .050'; MATERIAL REMOVED .017'; REMAINING MATERIAL .037'. FOUND OUT OF LIMITS, AS PER REF B737-700 SRM 53-10-51-1A-1. CORRECTION ACTION ACCOMPLISHED.

Part: PRESSURE DECK — DAMAGED (FLIGHT DECK) · airframe 55,155 hrs · 32,453 cycles

FLIGHT DECK FLOOR WEB APPROX BS 260 BETWEEN LBL 14 AND RBL 4 WL 208.1 DAMAGED. REPAIRED DAMAGED FLIGHT DECK FLOOR WEB AT APPROX BS 260 LBL 14 AND RBL 4 WL 208.1, PER EA 1-A53-33179 REV 1 FIG 1.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 55,155 hrs · 32,453 cycles

RT HORIZ STAB INSPAR RIB NR 1 STIFFENER NR 2 HAS CRACK INDICATIOIN. REPAIRED RIB NR 1 STIFFENER NR 2 RT STAB VERTICAL, AS PER B/737 SRM 55-10-09-2R-4 R 4 FIG 102A.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 55,155 hrs · 32,453 cycles

LEFT HORIZ STAB APPROX 26 INCHES FROM INBOARD EDGE THE 3RD RIB HAS A CRACK AT LOWER AREA, MKD 78-7, LEADING EDGE. REMOVED & REPLACED RIB ASSY AT LT HORIZ STAB APPROX 26' FROM INBOARD EDGE 3RD RIB, PER B737-700 SRM 51-40-02-0G-0 DRWG NR 186A1001 & 186A1304.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 55,155 hrs · 32,453 cycles

RT HORIZONTAL STAB INSPAR RIB NR 4 STIFFENER NR 4 HAS CRACK INDICATION. REPAIR NR 4 STIFFENER NR 4 RIB RT HORIZONTAL STAB, IN REF B737 SRM 55-10-09-2R-5 AS 22135.

Part: FRAME — CORRODED (BS 887 S25R-27L) · airframe 54,782 hrs · 32,216 cycles

FUSELAGE BS 887 BETWEEN S-25R TO S-27L HAS MULTIPLE SMALL AREAS OF CORROISION ON AFT SIDE OF BS 887 FRAME (AFT CARGO) / REMOVED CORROISION PER SRM 51-10-01; INSTALLED FASTENERS PER REF SRM 53-00-01; TREATED PER SRM 51-20-01 REF SA-M 326: A1131711

Part: POWER SUPPLY — FAILED (CABIN) · airframe 54,459 hrs · 32,022 cycles

EMERGENCY LIGHTS FAILED CAPACITY TEST AT LOCATIONS M1668;M1672;M1673;M1675;M1674. / R&R EMERGENCY LIGHT BATTERY/POWER SUPPLIES AT M1668;M1672;M1673;M1675;M1674 PER AMM 33-51-06.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 54,459 hrs · 32,022 cycles

EMERGENCY LIGHTS FAILED CAPACITY TEST AT LOCATIONS M1668;M1672;M1673;M1675;M1674. / R&R EMERGENCY LIGHT BATTERY/POWER SUPPLIES AT M1668;M1672;M1673;M1675;M1674 PER AMM 33-51-06.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 54,459 hrs · 32,022 cycles

LEFT HORIZ STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED LEFT HORIZ STAB FWD UPPER SLIDING SEAL PER AMM. 53-31-31

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,872 hrs · 30,394 cycles

EMERGENCY EXIT LIGHT INOP. RELAMPED PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,386 hrs · 30,085 cycles

R1 DOOR SLIDE EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: FAIRING — ELONGATED (LWR FUSELAGE) · airframe 51,318 hrs · 30,033 cycles

WING TO BODY FAIRING PANEL 193B HAS ENLONGATED & ENLARGED FASTENER HOLES AT LOCATIONS 1-6;10;12-17; 19;21;22;29-33 & 35-38 MOD / INSTALLED NEW PANEL 193B REF AMM 53-40-70 PERFORMED ELECTRICAL RESISTANCE CHECK REF AMM 53-51-01

Part: COVER — BROKEN (EXIT SIGN) · airframe 50,207 hrs · 29,304 cycles

L2 DOOR EMERGENCY EXIT SIGN PLASTIC COVER BROKEN. R&R SIGN PER AMM.

Part: COVER — MISSING (CABIN) · airframe 49,921 hrs · 29,132 cycles

R2 DOOR EMERGENCY EXIT LIGHTS "EXIT" COVER MISSING. R&R LAV LIGHT ASSEMBLY PER MM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 49,478 hrs · 28,854 cycles

LT HORIZONTAL LEADING EDGE FOUND 3RD STIFFENER AFT CRACKED AT STA 120.30. R&R STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 49,478 hrs · 28,854 cycles

RT HORIZONTAL STABILIZER LEADING EDGE, FOUND 2ND STIFFENER AFT CRACKED AT STA 120.30. R&R STIFFENER IAW SRM.

Part: SUPPORT BRACKET — BROKEN (LT WING) · airframe 49,478 hrs · 28,854 cycles

PANEL 551FB HAS BROKEN BRACKET; OUTBOARD FWD. SUPPORT / REMOVED & REPLACED BROKEN BRACKET ON PANEL 551FB OUTBOARD FWD SUPPORT IAW SRM 51-40-02-0G-0 PAR 7 AND DWG 115A2001 & DWG 115A5552 REV A

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 49,478 hrs · 28,854 cycles

LT HORIZONTAL NR 3 STIFFENER CRACKED AT STAB STA 129. R&R STIFFENER IAW SRM & DWG.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 49,478 hrs · 28,854 cycles

RT HORIZONTAL STABILIZER LEADING EDGE, FOUND 3RD STIFFENER AFT CRACKED AT STA 120.30. R&R STIFFENER IAW SRM & DWG.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 49,478 hrs · 28,854 cycles

LT HORIZONTAL STIFFENER CRACKED A STAB STA 129 NR 2. R&R STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 49,478 hrs · 28,854 cycles

LT HORIZONTAL LEADING EDGE FOUND 2ND STIFFENERS AFT CRACKED AT STA 120.30. R&R STIFFENER IAW SRM.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 49,478 hrs · 28,854 cycles

ACCESS PANEL 343AT L/H HORIZONTAL STABILIZER GAP COVER UPPER BLADE SEAL CRACKED. / REMOVED AND REPLACED ACCESS PANEL 343 AT R/H HORIZONTAL STABILIZER GAP COVER UPPER BLADE SEAL WITH NEW I.A.W. SRM 51-40-02-0G-0.

Part: SKIN — CORRODED (FUSELAGE) · airframe 49,478 hrs · 28,854 cycles

CROWN SKIN CORRODED BETWEEN BS 891 TO BS 929.5, BETWEEN STR 2L TO STR 2R. R&R SKIN IAW SRM AND EA.

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 49,478 hrs · 28,854 cycles

LT WING NR 5 SPOILER UPPER SURFACE DELAMINATED AT ZONE 1. R&R NR 5 SPOILER IAW AMM.

Part: ANGLE — CRACKED (LT WING) · airframe 49,478 hrs · 28,854 cycles

LT WING; REAR SPAR ORSS 297 -30 I/B OF REFLECTION ARM HAS A CRACK ANGLE. / REMOVED & REPLACED SEAL ASSEMBLY ON LT WING; REAR SPAR ORSS 297-30 I/B OF REFLECTION ARM IAW SOPM 20-50-01 AND AMM 20-50-11-910-801 TABLE 204

Part: GUSSET — CRACKED (AFT CARGO BAY) · airframe 49,478 hrs · 28,854 cycles

FWD. CARGO STA.500D STR.18L GUSSET HAS CRACK. (MARKED) / REMOVED AND REPLACED FWD CARGO COMPARTMENT L/H GUSSET AT STA.500D STR.18L PART#143A9481-6 PO#701753 IAW SRM 51-10-02-0G-0 AND BOEING DWG 143A9481

Part: SEAL — CRACKED (RT WING) · airframe 49,478 hrs · 28,854 cycles

RIGHT WING TRAILING EDGE DEFLECTION RIB BULB SEAL RETAINER BRACKET CRACKED AT FASTENER HOLE. APPROX. REAR SPAR STATION 268 / REPLACED RH WING TRAILING EDGE DEFLECTION RIB BULB SEAL RETAINER BRACKET AT APPROX. REAR SPAR STATIUM 268 PER SRM 51-40-02-0G-0 PAR 4 AND FIG 8 AND DRAWING 115A2930

Part: SKIN — CRACKED (LE SLAT) · airframe 49,478 hrs · 28,854 cycles

RT WING NR 5 LEADING EDGE SLAT CRACKED AT ACTUATOR RIB SLAT STATION 85.9. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 49,478 hrs · 28,854 cycles

RT WING NR 7 LEADING EDGE SLAT SKIN CRACKED AT ACTUATOR RIB SLAT STATION 322.71. REPAIRED SKIN IAW SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 49,478 hrs · 28,854 cycles

AFT CARGO DOOR CUTOUT. FWD LOWER CORNER SCUFF PLATE CRACKED / LOCATED & DRILLED NEW AFT CARGO DOOR CUTOUT FWD LOWER CORNER SCUFF PLATE IAW BOEING DWG 146A8341 REV -- DATED 10-12-1999 & SRM 51-40-05-0G-0. REMOVAL AND INSTALLATION OF SCUFF PLATES ACOMPLISHED ON CARD #753-721-10-01 57773U 10-4-18

Part: SKIN — CRACKED (LE SLAT) · airframe 49,478 hrs · 28,854 cycles

RT WING NR 6 LEADING EDGE SLAT CRACKED AT ACTUATOR RIB SLAT STATION 202.45. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,478 hrs · 28,854 cycles

LT STOW BINS EMERGENCY LIGHT INOP BETWEEN ROW 3 TO ROW 4. R&R LIGHT IAW AMM.

Part: LENS — MISSING (L2 DOOR) · airframe 49,452 hrs · 28,839 cycles

L2 DOOR EMERGENCY EXIT LENS COVER MISSING DIRECTIONAL ARROW. R&R LENS IAW MM.

Part: LENS — MISSING (R2 DOOR) · airframe 49,452 hrs · 28,839 cycles

R2 DOOR EMERGENCY EXIT LENS COVER MISSING DIRECTIONAL ARROW. R&R LENS IAW MM.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 49,330 hrs · 28,756 cycles

AFT CARGO FLOOR LINER HAS A CRACK (RAMP REPORT) / R&R AFT CARGO FLOOR PANEL #14013F IAW AMM 25-52-10 CLOSING NO 2559

Part: SLIDE — LOOSE (R2 DOOR) · airframe 48,980 hrs · 28,527 cycles

R2 DOOR SLIDE LOOSE FROM CONTAINER. SECURED SLIDE IAW MT.

Part: FLOOR PANEL — CRACKED (FWD CARGO COMPT) · airframe 48,193 hrs · 28,022 cycles

FWD CARGO FLOOR DAMAGED AT BS 500 ONE CRACK 7' LONG 2ND CRACK 5' LONG. / REF LOG PAGE 0063606 R & R CARGO FLOOR PANEL AT BS SOU IAW AMM 25-52-10. CL# 71112.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 46,214 hrs · 26,790 cycles

RIGHT WING NR 6 SLAT LEADING EDGE SKIN CRACKED. REPAIRED THE SLAT SKIN IAW EA.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 46,214 hrs · 26,790 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 46,016 hrs · 26,660 cycles

FUSELAGE SKIN CORRODED AT BS 355, BL 0, UNDERNEATH LOWER ATC ANTENNA. REPAIRED SKIN PER EA.

Part: RIVET — SHEARED (GIRT BAR ASSY) · airframe 45,200 hrs · 26,142 cycles

R1 DOOR SLIDE COVER FORWARD GIRT RETAINER RIVETS SHEARED. R & R THE GIRT ASSEMBLY IAW AMM AND SRM.

Part: FUSE — FAULTY (LE SLAT) · airframe 45,109 hrs · 26,086 cycles

AIR TURNBACK, LEADING EDGE FLAP TRANSIT WOULD NOT EXTINGUISH. R&R STANDBY FUSES PER AMM.

Part: BATTERY PACK — SMOKE (EMERGENCY LIGHT) · airframe 43,508 hrs · 25,155 cycles

SMOKE CAME FROM CEILING IN FORWARD GALLEY. R & R THE BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,951 hrs · 24,816 cycles

RT OVERWING HATCH INTERIOR EMERGENCY EXIT LIGHT BULB INOP. R&R BULB IAW AMM.

Part: BATTERY — LOW VOLTAGE (CABIN) · airframe 42,951 hrs · 24,816 cycles

FORWARD ENTRY OVERHEAD EMERGENCY BATTERY PACK M01675 LOW VOLTAGE. R&R BATTERY PACK IAW AMM.

Part: SUPPORT ANGLE — CORRODED (BS 767-787) · airframe 42,951 hrs · 24,816 cycles

SHIELD SUPPORT ANGLE CORRODED BETWEEN BS 767 TO 787, RBL 21. R & R THE SUPPORT ANGLE IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 727-727E) · airframe 42,951 hrs · 24,816 cycles

AFT CARGO SUPPORT CORRODED BETWEEN BS 727 TO 727E+10, LBL 21. R & R THE SUPPORT IAW SRM AND DWG.

Part: STRINGER SPLICE — CRACKED (BS 295) · airframe 42,951 hrs · 24,816 cycles

FORWARD ENTRY DOOR FORWARD SURROUND STRUCTURE STRINGER SPLICE CRACKED AT BS. 295.5, STRINGER 14L. REPAIRED THE STRINGER SPLICE IAW ER AND EA.

Part: FRAME — CRACKED (BS 294) · airframe 42,951 hrs · 24,816 cycles

STUB FRAME CRACKED AT BS 294, STRINGER 17R. REPAIRED STUB FRAME IAW EA.

Part: FRAME — CRACKED (BS 500C) · airframe 42,951 hrs · 24,816 cycles

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

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 42,951 hrs · 24,816 cycles

OUTBOARD SURFACE OF CHORD CRACKED AT BS 540, STR 22R. REPAIRED CHORD IAW ER AND EA.

Part: FRAME — CRACKED (BS 559) · airframe 42,951 hrs · 24,816 cycles

FRAME CRACKED AT BS 559, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 500A) · airframe 42,951 hrs · 24,816 cycles

FUSELAGE FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 727D) · airframe 42,951 hrs · 24,816 cycles

FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,951 hrs · 24,816 cycles

FUSELAGE FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED THE FRAME IAW SWA EA.

Part: FRAME — CRACKED (BS 827) · airframe 42,951 hrs · 24,816 cycles

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

Part: FRAME — CRACKED (BS 827) · airframe 42,951 hrs · 24,816 cycles

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

Part: FRAME — CRACKED (BS 440) · airframe 42,951 hrs · 24,816 cycles

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

Part: FRAME — CRACKED (BS 747) · airframe 42,951 hrs · 24,816 cycles

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

Part: FRAME — CRACKED (BS 400) · airframe 42,951 hrs · 24,816 cycles

FUSELAGE FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 42,951 hrs · 24,816 cycles

RIGHT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 40 AND 45.64. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,951 hrs · 24,816 cycles

FUSELAGE SKIN CRACKED AT BS 540, STR 22R. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,951 hrs · 24,816 cycles

BULKHEAD CHORD SKIN CRACKED AT BS 540, STR 22L. REPAIRED SKIN IAW EA.

Part: BULKHEAD WEB — CRACKED (LT MLG WW) · airframe 42,951 hrs · 24,816 cycles

LEFT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN LBL 31.83 - 40. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: SUPPORT — CORRODED (BS 500-500A) · airframe 42,951 hrs · 24,816 cycles

FORWARD CARGO BAY RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500 TO 500A. R & R SUPPORT IAW SRM & DWG.

Part: PLATE — CORRODED (BS 847) · airframe 42,951 hrs · 24,816 cycles

AFT CARGO SIDE PLATE CORRODED AT BS 847, RBL 21.0. R & R THE PLATE IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (BS 727D) · airframe 42,951 hrs · 24,816 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 727D+6, BETWEEN RBL 3 TO RBL 8.1. R & R THE FLOORBEAM IAW SRM & DWG.

Part: WEB — CORRODED (FWD CARGO BAY) · airframe 42,951 hrs · 24,816 cycles

FORWARD CARGO BAY SCUFF PLATE SUB WEB CORRODED. R & R THE WEB IAW SRM & DWG.

Part: SUPPORT BRACKET — CORRODED (BS 500D BULKHEAD) · airframe 42,951 hrs · 24,816 cycles

FORWARD CARGO BAY AFT LOWER BULKHEAD PANEL SUPPORT BRACKET CORRODED AT BS 500D. R & R THE BRACKET IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 767-794) · airframe 42,951 hrs · 24,816 cycles

AFT CARGO SUPPORT CORRODED BETWEEN BS 767 TO 794, RBL 21. REPAIRED THE SUPPORT IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (BS 727-887) · airframe 42,951 hrs · 24,816 cycles

AFT CARGO TRACK CORRODED BETWEEN BS 727 TO 887, RBL 13.8. R & R THE CARGO TRACK IAW DWG AND SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 42,951 hrs · 24,816 cycles

FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 420 TO BS 440. R&R SUPPORT SHIELD IAW DWG AND SRM.

Part: WIRE — BROKEN (CABIN) · airframe 42,951 hrs · 24,816 cycles

FORWARD LAV EXIT LIGHT QUICK DISCONNECT WIRE BROKEN. REPAIRED WIRE PER WDM AND MM.

Part: WEB — CORRODED (BS 804-840) · airframe 42,951 hrs · 24,816 cycles

AFT CARGO DOOR THRESHOLD PLATE UNDER SCUFF PLATE WEB CORRODED BETWEEN BS 804 TO 840. R & R THE WEB IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (BS 887-947) · airframe 42,951 hrs · 24,816 cycles

AFT CARGO BAY, CARGO TRACK CORRODED BETWEEN BS 887 TO 947.5, LBL 3. R & R THE CARGO TRACK IAW SRM & DWG.

Part: DOOR SILL — CORRODED (BS 847-794) · airframe 42,951 hrs · 24,816 cycles

AFT CARGO AFT DOOR CUTOUT LOWER SILL ASSEMBLY CORRODED BETWEEN BS 847 TO 794, RBL 21.0. R & R DOOR SILL IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 771) · airframe 42,951 hrs · 24,816 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 771, LBL 8.10. R&R THE FLOORBEAM IAW SRM & DWG.

Part: CROSSMEMBER — CORRODED (FUSELAGE) · airframe 42,951 hrs · 24,816 cycles

AFT CARGO FLOOR STRUCTURE CROSS MEMBER CORRODED AT BS 887. R&R MEMBER PER SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 727B-767) · airframe 42,951 hrs · 24,816 cycles

AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS 727B +4 TO 767, RBL 21.0. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: STRUCTURE — CORRODED (BS 956-992) · airframe 42,951 hrs · 24,816 cycles

R2 DOOR CUTOUT CORRODED AT BS 956 TO 992, WL 208. REPAIRED IAW SRM.

Part: SUPPORT — CORRODED (BS 753-794) · airframe 42,951 hrs · 24,816 cycles

AFT CARGO SUPPORT CORRODED BETWEEN BS 753 TO 794, LBL 21. R & R THE SUPPORT IAW SRM AND DWG.

Part: SKIN — CRACKED (LT WING LE SLAT) · airframe 42,951 hrs · 24,816 cycles

LEFT WING NR 1 SLAT SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED THE SLAT SKIN IAW SRM.

Part: SPRING — MISSING (AILERON SYS) · airframe 42,299 hrs · 24,427 cycles

AIR TURNBACK AT TAKEOFF, FLIGHT CONTROLS FELT VERY LIGHT AND UNRESPONSIVE. FOUND LOWER SPRING MISSING ON AILERON FEEL AND CENTERING UNIT. REPLACED UNIT IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 42,284 hrs · 24,419 cycles

EMERGENCY LIGHT INOPERATIVE BETWEEN ROW 9 TO ROW 12. R & R POWER SUPPLY IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 41,654 hrs · 24,051 cycles

FORWARD ENTRY DOOR EMER EXIT LIGHT COVER MISSING. R & R LIGHT ASSEMBLY IAW AMM.

Part: RETAINER — OUT OF ADJUST (R1 DOOR) · airframe 40,899 hrs · 23,609 cycles

R1 DOOR EMER EVAC SLIDE, GIRT BAR RETAINER OUT OF ADJUSTMENT. ADJUSTED RETAINER IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,098 hrs · 23,157 cycles

LEFT EMER LIGHT INOPERATIVE AT SEAT ROW 23. RELAMPED LIGHT IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,347 hrs · 21,018 cycles

CENTER CABIN FLOOR BREAK ASSEMBLY PANEL INTERCOSTAL CRACKED AT BS 540 BETWEEN BL 0 TO LBL 25. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,347 hrs · 21,018 cycles

CENTER CABIN FLOOR BREAK ASSEMBLY PANEL INTERCOSTAL CRACKED AT BS 540, BETWEEN RBL 25 TO 45. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,347 hrs · 21,018 cycles

CENTER CABIN FLOOR BREAK ASSEMBLY PANEL INTERCOSTAL CRACKED AT BS 540 BETWEEN BL 0 TO RBL 25. R & R INTERCOSTAL IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 36,347 hrs · 21,018 cycles

LEFT WING WAFFLE PLATE CRACKED AFT OF PYLON INBD OF HYD LINES. R & R WAFFLE PLATE IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 36,347 hrs · 21,018 cycles

LEFT WING WAFFLE PLATE CRACKED ABOVE NR 3 FLAP TRANS. R & R WAFFLE PLATE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,347 hrs · 21,018 cycles

FLANGE IN SEAT TRACK CRACKED AT BS 727B LBL 24.75, FWD LT HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,347 hrs · 21,018 cycles

FLANGE IN SEAT TRACK CRACKED AT BS 727B LBL 24.75, AFT LT HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,347 hrs · 21,018 cycles

FLANGE IN SEAT TRACK CRACKED AT BS 727B RBL 45, FWD LT HOLE. REPAIRED SEAT TRACK IAW EA.

Part: POST — DAMAGED (FUSELAGE) · airframe 36,347 hrs · 21,018 cycles

RIGHT NR 1 COCKPIT WINDOW POST LOWER FASTENER HOLE DAMAGED. REPAIRED POST IAW ACO.

Part: BATTERY — FAILED (CABIN) · airframe 35,410 hrs · 20,470 cycles

CENTER RT EMER BATTERY FAILED TIME TEST. R & R BATTERY PER.

Part: BATTERY — FAILED (CABIN) · airframe 35,410 hrs · 20,470 cycles

AFT LT EMER BATTERY FAILED TIME TEST. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 35,410 hrs · 20,470 cycles

AFT RT EMER BATTERY FAILED TIME TEST. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 35,410 hrs · 20,470 cycles

FORWARD RT EMER BATTERY FAILED TIME TEST. R & R BATTERY IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 33,006 hrs · 19,086 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER MISSING. R & R LIGHT BASE ASSEMBLY IAW MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 31,950 hrs · 18,452 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP LOOSE ON RT SIDE. R&R CLIP IAW SRM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 30,742 hrs · 17,744 cycles

GALLEY NR 1 LOWER OUTBOARD AREA EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED SIGN IAW AMM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 30,742 hrs · 17,744 cycles

LEFT HORIZONTAL STABILIZER RIB AT STATION 101.9 CRACKED FASTENER HOLE 27.0 INCHES AFT OF FORWARD SPAR ON LOWER INBOARD SIDE OF RIB. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 30,742 hrs · 17,744 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT STATION 101.9 FASTENER HOLE 30.5 INCHES AFT OF FORWARD SPAR ON LOWER INBOARD SIDE OF RIB. REPAIRED RIB IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 36,355 hrs · 21,024 cycles

RIGHT FLIGHT DECK NR 1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER INSIDE & OUT. REPAIRED FRAME IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

CORROSION ON SIDEWALL SUPPORT BS 767-794, RBL 21. REMOVED AND REPLACED SIDE SHIELD ACB BS 767-794 RBL 21 IAW SRM 57-40-02 AND DRW

Part: SILL — CORRODED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

CORROSION ON AFT CARGO DOOR LOWER SILL BEAM (BOTTOM OF UPPER FLANGE AT NUT PLATE LOCATIONS); BS 795.5 TO BS 847, RBL 19, WL 161. REMOVED AFT CARGO DOOR LOWER SILL WEB AND REPLACED WITH NEW WEB PER SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,576 hrs · 17,065 cycles

CORROSION AFT CARGO COMPARTMENT CARGO TRACK; BS 907, RBL 13.5 WL 172. REMOVED AND REPLACED TRACK PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT RAIL; BS 772, LBL 3, WL 157. REPAIRED AFT CARGO COMPARTMENT FLOOR SUPPORT RAIL AT BS 772, LBL 3, WL 157 IAW EA 1-A53-4982 REV 3.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,576 hrs · 17,065 cycles

CORROSION AFT CARGO COMPARTMENT CARGO TRACK; BS 887, LBL 3, WL 171. REMOVED CORROSION-.020"X1"X2", ORIGINAL THICKNESS - .063", MATERIAL REMAINING-.043" FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 AND 53-60-53-01-2. REMOVED LOCATED,

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

CORROSION AT CARGO COMPARTMENT FLOOR SUPPORT RAIL; BS 887, RBL 3, WL 171. REMOVED AND REPLACED SUPPORT PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

CORROSION CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT B867 TO BS 887 RBL 21 WL 170. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

CORROSION ON AFT CARGO DOOR LOWER SILL BEAM STRAP (BOTTOM OF UPPER FLANGE AT NUT PLATE LOCATIONS); BS 795 TO BS 802, RBL 19, WL 158. REMOVED & REPLACED NUT PLATE STRAP BS 787-802 RBL 19 WL 158 IAW SRM 51-40-02 AND DWG 146A8128 87529U 17NOV12.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 29,576 hrs · 17,065 cycles

CORROSION ON AFT CARGO COMPARTMENT CARGO TRACK; BS 772, LBL 17, WL 157. REPAIRED CARGO TRACK PER SRM AND EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

CORROSION AFT CARGO COMPARTMENT FLOOR SUPPORT RAIL; BS 772, RBL 3, WL 157. AFT CARGO COMPARTMENT FLOOR SUPPORT RAIL BS 772, RBL 3 WL 157. REPAIRED PER EA 1-A53-4982 87719U 14NOV12.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

CORROSION CARGO TRACK AT BS 787 TO BS 847, RBL 13.5, WL 157-170. REMOVED AND REPLACED TRACK IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

CORROSION ON AFT CARGO DOOR LOWER SILL BEAM UPPER STRAP; BS 791-847, RBL 19, WL 160. REMOVED AND REPLACED AFT CARGO DOOR LOWER SILL UPPER STRAP BS 775-860 RBL 15 WL 160 IAW SRM 51-40-02 AND DWG 146A0081 87529U 17NOV12.

Part: STRAP — CORRODED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

CORROSION ON AFT CARGO DOOR LOWER SILL BEAM STRAP (BOTTOM OF UPPER FLANGE AT NUT PLATE LOCATIONS); BS 841 TO BS 847, RBL 19, WL 161. REMOVED AND REPLACED NUT PLATE STRAP ACB BS 860 RBL 19, WL 161, IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

CORROSION CARGO COMPARTMENT FLOOR SUPPORT RAIL BS 772, LBL 8, WL 157. REPAIRED SUPPORT RAIL PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

CORROSION AFT CARGO COMPARTMENT FLOOR SUPPORT RAIL; BS 887, RBL 8, WL 171. REMOVED AFT CARGO BAY FLOOR SUPPORT RAIL DUE TO CORROSION AT BS 887-947 RBL 8 LW 171 PER SRM 51-40-02-0G-0. INSTALLED NEW FLOOR SUPPORT RAIL BS 887-947 RBL 8 WL

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 29,576 hrs · 17,065 cycles

LEFT HORIZ STAB RIB AT STA 92.7 2ND AND 3RD VERT STIFFENERS ARE CRACKED AT THE LWR END. REPAIRED LEFT HORZ STAB RIB AT STAB STA 92.70 2ND AND 3RD VERT STIFFENERS PER SRM 55-10-09-2R-4 4318U 13NOV12.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

CORROSION BS 500B-500D WL 54 LBL 23 LEFT FLOOR TO SIDEWALL SUPPORT HAS AREAS OF CORROSION. REPAIRED FLOOR TO SIDEWALL SUPPORT BS 488-500D LBL 23 IAW SRM 53-00-53-2R-5.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 29,576 hrs · 17,065 cycles

CABIN FLOOR PANEL 241ADF IS CRACKED IN AFT O/B CORNER. REPAIRED CRACK IN AFT O/B CORNER ON CABIN FLOOR PANEL 241DF IAW SRM 53-00-50-2R-6. 89216U, 11NOV2012.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

FLOOR SUPPORT INTERCOSTAL BETWEEN BS 344-BS 360, BL 0, WL 208 IS CRACKED. REMOVED DAMAGED INTERCOSTAL BS 344-360, BL-0, WL 208 IAW SRM 51-40-02 LOCATED AND DRILLED NEW PART IAW SRM 51-40-05-0G-0 INSTALLED IAW SRM 51-40-02.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 29,576 hrs · 17,065 cycles

RIGHTT HORIZ STAB RIB AT STA 129.50 3RD VERT STIFFENER IS CRACKED. REPAIRED THE RIGHT HORIZ STAB RIB AT STA 129.50, 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4, SOPM 20-50-01, SRM 51-40-02-0G-0 AND MM 27-31-41-400-801. OPS CHECK GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

FLOOR SUPPORT INTERCOSTAL BETWEEN BS 344-BS 360, LBL 11, WL 208 IS CRACKED. REMOVED AND INSTALLED NEW FLOOR SUPPORT INTERCOSTAL BETWEEN BS 344 - BS 360, LBL 11 WL 208 IAW 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 29,576 hrs · 17,065 cycles

FLOOR SUPPORT INTERCOSTAL BS 294.5- BS 312, RBL 15,WL 208 CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,576 hrs · 17,065 cycles

THE RIGHT STAB LOWER SKIN STAB STA 138.70 HAS A 1.0 INCH CRACK 15 INCHES FROM REAR SPAR. REPAIRED RIGHTT STAB LOWER SKIN AT STAB STA 138.70 15 INCHES FORWARD OF REAR SPAR IAW SRM 55-10-01-2R-11.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,576 hrs · 17,065 cycles

THE LEFT STAB LWR SKIN REAR SPAR HAS A 2.5" CRACK 3.4" FROM STAB STA 92.70. REPAIRED LEFT STAB LWR SKIN AT STAB STA 92.70 IAW SRM 55-10-01-2R-11 FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: LIGHT — BROKEN (CABIN) · airframe 29,576 hrs · 17,065 cycles

AFT LAV EXIT LIGHT ASSY BROKEN. REPLACED AFT LAV EXIT LIGHT ASSY IAW SOPM 20-50-01.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,576 hrs · 17,065 cycles

THE LEFT STAB LOWER SKIN STAB STA 147.90 HAS A 1.0 INCH CRACK 15 INCHES FROM THE FORWARD SPAR. REPAIRED LEFT STAB LOWER SKIN STA 147.90 IAW SRM 51-10-01-2R-11 REPAIR 11.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,576 hrs · 17,065 cycles

THE LEFT STAB LOWER SKIN STAB STA 138.70 HAS A 1.0 INCH CRACK 7 INCHES FROM THE REAR SPAR. REPAIRED LEFT STAB LOWER SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,576 hrs · 17,065 cycles

THE RIGHT STAB LOWER SKIN REAR SPAR HAS A 2.0 INCH CRACK 4 INCHES FROM STAB STA 129.50. REPAIRED RIGHT STAB LOWER SKIN AT REAR SPAR STAB STA 129.50 IAW SRM 55-10-01-2R-11.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,576 hrs · 17,065 cycles

THE RIGHT STAB LOWER SKIN STAB STA 129.50 HAS A 1.2 INCH CRACK 8 INCHES FROM FWD SPAR. REPAIRED RIGHT STAB LOWER SKIN STAB STA 129.50 IAW SRM 55-10-01-2R-11.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,576 hrs · 17,065 cycles

THE LEFT STAB LOWER SKIN STAB STA 138.70 HAS A 1.0 INCH CRACK 7 INCHES FROM THE REAR SPAR. REPAIRED LEFT STAB LOWER SKIN STA 138.70 IAW SRM 55010-01-2R-11 REPAIR 11.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,576 hrs · 17,065 cycles

THE RIGHT STAB LWR SKIN REAR SPAR HAS A 2.7" CRACK 2.8" FROM STAB STA 101.90. REPAIRED RIGHT STAB LWR SKIN REAR SPAR HAS A CRACK 2.8" FROM STAB STA 101.90 IAW SRM 55-10-01-2R-11.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 28,307 hrs · 16,391 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 27,757 hrs · 16,105 cycles

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

Part: LATCH — MISSING (R2 DOOR) · airframe 27,757 hrs · 16,105 cycles

R2 DOOR EMERGENCY EVAC SLIDE COVER LATCH MISSING. INSTALLED LATCH PER MT AND MM.

Part: COVER — CRACKED (CABIN) · airframe 27,757 hrs · 16,105 cycles

LEFT EEPLS COVERS CRACKED BETWEEN ROW 1 TO ROW 4. REMOVED AND REPLACED COVERS PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 27,757 hrs · 16,105 cycles

L2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED SLIDE PER MT AND MM.

Part: COVER — CRACKED (CABIN) · airframe 26,566 hrs · 15,423 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 2. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,666 hrs · 14,892 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MM AND MT.

Part: LENS — LOOSE (CABIN) · airframe 25,516 hrs · 14,801 cycles

LT FWD EEPLS LENS LOOSE. SECURED LENS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 24,155 hrs · 14,013 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 24,204 hrs · 14,040 cycles

LT EMERGENCY EXIT SIGN COVER BROKEN. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 22,524 hrs · 13,099 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EEPLS COVER MISSING AT ROW 2. INSTALLED COVER PER MM.

Part: COVER — CRACKED (BS 580) · airframe 22,330 hrs · 12,994 cycles

DURING SCHEDULED 6Y CHECK, FOUND EMERGENCY LIGHT COVER CRACKED AT BS 580. REMOVED AND REPLACED COVER PER MM.

Part: COVER — MISSING (BS 392) · airframe 22,330 hrs · 12,994 cycles

DURING SCHEDULED 6Y CHECK, FOUND EMERGENCY LIGHT COVER MISSING AT BS 392. REPLACED COVER PER MM.

Part: COVER — CRACKED (BS 707) · airframe 22,330 hrs · 12,994 cycles

DURING SCHEDULED 6Y CHECK, FOUND EMERGENCY LIGHT COVER CRACKED AT BS 707. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 21,165 hrs · 12,327 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: COVER — CRACKED (CABIN) · airframe 19,658 hrs · 11,439 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS FWD COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 19,658 hrs · 11,439 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 19,235 hrs · 11,166 cycles

FWD EEPLS LOOSE. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,535 hrs · 9,525 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS TRACK LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 15,939 hrs · 9,168 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY LIGHT LENS MISSING AT ROW 1. REPLACED EMERGENCY LIGHT ASSY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 14,975 hrs · 8,577 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 14,975 hrs · 8,577 cycles

DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 12,424 hrs · 7,026 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 12,061 hrs · 6,804 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 12,038 hrs · 6,791 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM.