N939WN
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2025-02-13 – 2025-02-13 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2025-02-13 – 2025-02-13 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AFT FA MEGAPHONE INOPERATIVE. CLEANED BATTERY CONTACTS AND ACCOMPLISHED MEGAPHONE OPS CHECK IAW AMM 25-64-00, CHECKED NORMAL.
PASSENGER CABIN EMERGENCY EXIT ROW SEAT 14B RECLINES. LOCKED OUT 14B SEAT RECLINE IAW CMM 25-21-42
RIB FITTING IS CRACKED AT STAB BL 281.81 RH SIDE. PERFOMED REPAIR IAW SRM 55-10-90-2R-1-A01330, REPAIR 1.
LH HORIZONTAL STAB UPPER FWD SLIDER SEAL IS CRACKED. REMOVED AND REPLACED SEAL PER AMM 53-31-31.
RH HORIZONTAL STAB UPPER FWD SLIDER SEAL CRACKED. REMOVED AND REPLACED SEAL PER AMM 53-31-31.;[02] C/W INSPECTION
CRACK ON WEB LOCATED BTW BS440 TO BS BS460 AT LEVEL S-25L FWD CARGO COMPARTMENT 2025-203869<[01] FABRICATED WEB LOCATED BTW BS440 TO BS BS460 AT LEVEL S-25L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-05; SRM 51-20-01; SRM 51-30-01 AND DWG 143A7510 REV C. SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED CORRECTIVE ACTION 1; COMPLETED
ELONGATED HOLE ANGLE LOCATE BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT 2025-203852<[01] REPLACED ANGLE AND LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG: 146A0081 SHEET: 37 REV: - AND DWG: 146A8123 SHEET: 16 REV: -. <BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1<BR>REPLACED ANGLE LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG: 146A0081 SHEET: 37 REV: - AND DWG: 146A8123 SHEET: 16 REV: -. <BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED ANGLE LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; AND SRM 51-10-02 ITEM 9 AND DWG: 146A0081 SHEET: 37 REV: - AND DWG: 146A8123 SHEET: 16 REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED
INCORRECTLY EMERGENCY LIGHT LENS GALLEY 1 AT FWD GALLEY AREA 2025-203843<[01] REPLACED EMERGENCY LIGHT LENS GALLEY AREA 1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 STEP 2.C.(1).(A)(2) AND (3).(4);[02] JOB COMPLETED
INCORRECTLY EMERGENCY LIGHT LENS GALLEY 4 AT AFT GALLEY AREA 2025-203844<[01] REPLACED EMERGENCY LIGHT LENS GALLEY 4 AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 STEP 2.C.(1).(A)(2) AND (3).(4);[02] JOB COMPLETED
CRACK LOWER ANGLE FLOOR STRUCTURE BS 695 AND RBL 24.75 CENTER SECTION 2025-203648<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 29-JAN-26.;[02] REPLACED LOWER ANGLE FLOOR STRUCTURE BS 695 AND RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02 AND 51-10-02 PARAGRAPH 9; DWG: 273A9112 SHEET: 6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2<BR>REPLACED LOWER ANGLE FLOOR STRUCTURE BS 695 AND RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02 AND 51-10-02 PARAGRAPH 9; DWG: 273A9110 SHEET: 6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[04] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.
CRACK RIB 8 ON ACCESS PANEL 321A AT VERTICAL STABILIZER 2025-203809<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26.;[02] REPLACED RIB 8 AND FASTENERS LOCATED ON PANEL 312A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DRAWING 174A1008 SHEET 2 REV C.SEE INDIVIDUAL STEP SIGNOFF BELOW;[03] REPLACED RIB 8 AND FASTENERS LOCATED ON PANEL 312A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DRAWING 174A1008 SHEET 2 REV C.SEE INDIVIDUAL STEP SIGNOFF BELOW
CRACK CARGO TRACK RBBL 13.84 LOCTAED BS727E AFT CARGO COMPARTMENT 2025-203785 <[01]. STEP 5 AND 6 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATE: 27-AUG-25; [02] INSTALLED PERMANENT REPAIR PARTS [1] TRACK EXTRUSION [2] TRACK SPLICE (1 E/A) AND FASTENERS LOCATED ON CARGO TRACK LOCATED BS 727D + 12? TO BS 727E + 10? RBBL 13.84. AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL STEP SIGNOFF BELOW .; [03] INSTALLED PERMANENT REPAIR PARTS [1] TRACK EXTRUSION [2] TRACK SPLICE (1 E/A) AND FASTENERS LOCATED ON CARGO TRACK LOCATED BS 727D + 12? TO BS 727E + 10? RBBL 13.84. AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL STEP SIGNOFF BELOW .; [04] CORRECTED STEP 3. INSTALLED PERMANENT REPAIR PARTS [1] TRACK EXTRUSION [2] TRACK SPLICE (1 E/A) AND FASTENERS LOCATED ON CARGO TRACK LOCATED BS 727D + 12? TO BS 727E + 10? RBBL 13.84. AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL STEP SIGNOFF BELOW . RII.
CORROSION ANGLE FLOOR STRUCTURE LOCATED STA947.5 AND RBL4 WL156 AT AFT CARGO COMPARTMENT 2025-203796<[01] REPLACED ANGLE FLOOR STRUCTURE AND FASTENERS LOCATED STA947.5 AND RBL4 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG # 149A8117 SHEET 6 REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED
CORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203782<
CRACK ANGLE - SUPPORT LOCATED STA947.5 AND LBL11 AT AFT CARGO COMPARTMENT 2025-203797<[01] REPLACED ANGLE - SUPPORT LOCATED STA947.5 AND LBL11 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02 AND DWG # 149A8103 SHEET 7 REV: A.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1<BR>REPLACED ANGLE - SUPPORT FITTING LOCATED STA947.5 AND LBL11 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02 AND DWG # 149A8103 SHEET 7 REV: A.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] COMPLETED JOB
CRACK CARGO TRACK LBBL 17.24 LOCATED BS727E AFT CARGO COMPARTMENT 2025-203789<[01] STEP 4 AND 5 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATE: 27-AUG-25;[02] REPAIRED CARGO TRACK LOCATED BS 727D + 13? TO BS 727E + 11? LBL 17.24 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 53-00-53-2R-3 REPAIR AND BOEING 737-700 SRM 51-40-02.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[03] REPAIRED CARGO TRACK LOCATED BS 727D + 13? TO BS 727E + 11? LBL 17.24 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 53-00-53-2R-3 REPAIR AND BOEING 737-700 SRM 51-40-02.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.<BR>RII;[04] CORRECTED STEP 3 <BR>REPAIRED CARGO TRACK LOCATED BS 727D + 13? TO BS 727E + 11? LBL 17.24 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 53-00-53-2R-3 REPAIR AND BOEING 737-700 SRM 51-40-02.
CRACK CARGO TRACK RBBL 13.84 LOCATED BS727C AFT CARGO COMPARTMENT 2025-203786<[01] STEP 4 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATE: 27-AUG-25;[02] STEP 5 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 240497907; DUE DATE: 27-AUG-25;[03] MAR-2025 15:11:20<BR>INSTALLED PERMANENT REPAIR PARTS [1] TRACK EXTRUSION [2] TRACK SPLICE (2 E/A) AND FASTENERS LOCATED ON CARGO TRACK LOCATED BS 727B + 8? TO BS 727C +9? RBBL 13.84. AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3;[04] CORRECTED STEP 3: INSTALLED PERMANENT REPAIR PARTS [1] TRACK EXTRUSION [2] TRACK SPLICE (2 E/A) AND FASTENERS LOCATED ON CARGO TRACK LOCATED BS 727B + 8? TO BS 727C +9? RBBL 13.84. AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3.SEE INDIVIDUAL STEP SIGNOFF BELOW;[05] INSTALLED PERMANENT REPAIR PARTS [1] TRACK EXTRUSION [2] TRACK SPLICE (2 E/A) AND FASTENERS LOCATED ON CARGO TRACK LOCATED BS 727B + 8? TO BS 727C +9? RBBL 13.84. AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3.SEE INDIVIDUAL STEP SIGNOFF BELOW<BR><BR>RII
CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 41 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH 0.312 INCH APPROXIMATELY. ) 2025-203751<[01] ON STEP 6 AND 7: TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101V022240; DUE DATE: 28 MAR 25;[02] REJECTED INSTALLATION STEP BECAUSE THE FASTENERS ON THE OUTERS ROW ARE INCORRECTLY INSTALLED AND THE AREA ALREADY HAS PRIMER APPLIED; APPROXIMATELY AT RBL 60 PRESSURE DECK;[03] REPLACED FASTENERS ON THE OUTERS ROW APPROXIMATELY AT RBL 60 PRESSURE DECK IAW B737-700 SRM 51-40-02 AND IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 PARAGRAPH 4.L;[04] REPLACED FASTENERS ON THE OUTERS ROW APPROXIMATELY AT RBL 60 PRESSURE DECK IAW B737-700 SRM 51-40-02 AND IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 PARAGRAPH 4.L<BR>RII;[05] PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LOC. BS 663.75 TO BS 675 BTW RBL 30 TO RBL 38 AT PASSENGER CABIN IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2; SEE INDIVIDUAL SIGN OFF BELOW.;[06] CORRECTED STEP 5<BR>PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LOC. BS 663.75 TO BS 675 BTW RBL 30 TO RBL 60 AT PASSENGER CABIN IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2; SEE INDIVIDUAL SIGN OFF BELOW.;[07] PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LOC. BS 663.75 TO BS 675 BTW RBL 30 TO RBL 60 AT PASSENGER CABIN IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2; SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII
CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 30 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH 0.250 INCH APPROXIMATELY. ) 2025-203749<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138103; DUE DATE: 10-JUN-25.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138103; DUE DATE: 10-JUN-25.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138103; DUE DATE: 10-JUN-25.;[04] PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LOC. BS 663.75 TO BS 675 BTW LBL 30 TO LBL 60 AT PASSENGER CABIN IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2; SEE INDIVIDUAL SIGN OFF BELOW.;[05] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW
CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 30 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH 0.250 INCH APPROXIMATELY. ) 2025-203749<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138103; DUE DATE: 10-JUN-25.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138103; DUE DATE: 10-JUN-25.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138103; DUE DATE: 10-JUN-25.;[04] PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LOC. BS 663.75 TO BS 675 BTW LBL 30 TO LBL 60 AT PASSENGER CABIN IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2; SEE INDIVIDUAL SIGN OFF BELOW.;[05] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW
CORROSION ANGLE FLOOR STRUCTURE LOCATED STA947.5 AND RBL4 WL156 AT AFT CARGO COMPARTMENT 2025-203796<
CRACK LOWER ANGLE FLOOR STRUCTURE BS 695 AND RBL 24.75 CENTER SECTION 2025-203648<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 29-JAN-26.;[02] REPLACED LOWER ANGLE FLOOR STRUCTURE BS 695 AND RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02 AND 51-10-02 PARAGRAPH 9; DWG: 273A9112 SHEET: 6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2<BR>REPLACED LOWER ANGLE FLOOR STRUCTURE BS 695 AND RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02 AND 51-10-02 PARAGRAPH 9; DWG: 273A9110 SHEET: 6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[04] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.
CORROSION SHIELD WEB LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT 2025-203783<[01] REPLACED SHIELD WEB AND FASTENERS LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9. AND DWG 146A0081 SHEET: 37; REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED CORRECTIVE ACTION STEP 1<BR>RII ACCOMPLISHED
CORROSION SUPPORT ZEE LOCATED BETWEEN BS727C TO BS807 LBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203784<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 LBL 21 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 146A7502 SHEET 27 REV:-<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK COMPLETED <BR>RII
CORROSION SHIELD WEB LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT 2025-203783<
CORROSION SUPPORT ZEE LOCATED BETWEEN BS727C TO BS807 LBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203784<
CORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203782<[01] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BETWEEN BS727 TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02 AND DWG # 146A7500 SHEET 113 REV: -<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BETWEEN BS727 TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02 AND DWG # 146A7500 SHEET 113 REV: -<BR>SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ANGLE - CLIP LOCATED STA440 AND STR26L FWD CARGO COMPARTMENT 2025-203694<[01] REPLACED ANGLE CLIP LOCATED BS 440 STRINGER 26L AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG # 143A7505 SHEET 118. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED ANGLE CLIP LOCATED BS 440 STRINGER 26L AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG # 143A7505 SHEET 118. SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK STRINGER 23L LOCATED STA540 FWD CARGO COMPARTMENT 2025-203705<[01] TOOL USED ON STEP 6. ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] REPAIRED STRINGER 23L LOCATED BS 500D PLUS 10 INCHES TO BS 540 IAW BOEING 737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG 143A3210 SHEET 74 REV. B<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[03] TASK COMPLETED <BR>RII
ELONGATED HOLE ON SHIELD WEB LOCATED BETWEEN STA492.4 TO STA500A AND RBL21 AT FWD CARGO COMPARTMENT 2025-203697<[01] REPLACED SHIELD WEB LOCATED BTW BS 492.4 TO BS 500A AND RBL 21 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG # 143A0080; SHEET 33; REV -.
INOP WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) 2025-203706<[01] REPLACED WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-SWA-807 AND DWG 25600001 REV K;[02] CORRECTED ITEM 1 <BR><BR>REPLACED WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-SWA-807 AND DWG 25600001 REV K<BR><BR>NEXT INSPECTION RECORD VALUE: JUL-27;[03] CORRECTED ITEM 2<BR>REPLACED WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-SWA-807 AND DWG 25600001 REV K TEST IS OK<BR><BR>NEXT INSPECTION RECORD VALUE: JUL-27;[04] REPLACED WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-SWA-807 AND DWG 25600001 REV K TEST IS OK<BR><BR>NEXT INSPECTION RECORD VALUE: JUL-27
CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2025-203695<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D AND STRINGER 19L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG # 143A7902; SHEET 209; REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK CARD COMPLETED <BR>REPLACED GUSSET AND FASTENERS LOCATED BS 500D AND STRINGER 19L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG # 143A7902; SHEET 209; REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ANGLE - CLIP LOCATED STA440 AND STR26L FWD CARGO COMPARTMENT 2025-203694<
CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2025-203695<
INOP WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) 2025-203706 <[01]. REPLACED WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-SWA-807 AND DWG 25600001 REV K; [02] CORRECTED ITEM 1. REPLACED WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-SWA-807 AND DWG 25600001 REV K. NEXT INSPECTION RECORD VALUE: JUL-27; [03] CORRECTED ITEM 2. REPLACED WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-SWA-807 AND DWG 25600001 REV K TEST IS OK. NEXT INSPECTION RECORD VALUE: JUL-27; [04] REPLACED WINDSCREEN LT SIDE FLASH LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-SWA-807 AND DWG 25600001 REV K TEST IS OK. NEXT INSPECTION RECORD VALUE: JUL-27.
CRACK STRINGER 23L LOCATED STA540 FWD CARGO COMPARTMENT 2025-203705<[01] TOOL USED ON STEP 6. ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] REPAIRED STRINGER 23L LOCATED BS 500D PLUS 10 INCHES TO BS 540 IAW BOEING 737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG 143A3210 SHEET 74 REV. B<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[03] TASK COMPLETED <BR>RII
CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN RBL 24.75 TO RBL 45.5 AT PASSENGER CABIN 2025-203647<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN RBL 24.75 TO RBL 45.5 AT PASSENGER CABIN. B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG 143A0060 SHEET 46 REV -;[02] TASK COMPLETED
CRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.375 IN. APROX.AT PASSENGER CABIN 2025-203649<[01] REPLACED STUB FRAME AND FASTENERS LOC. BETWEEN STR7R TO STR11R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG DWG 141A8370 SHEET 9; REV. ; AND DWG 141A8370 SHEET 10; REV. .<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTED ITEM 1 <BR>REPLACED STUB FRAME AND FASTENERS LOC. BS296.5 BETWEEN STR7R TO STR11R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG DWG 141A8370 SHEET 9; REV. ; AND DWG 141A8370 SHEET 10; REV. .<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[03] REPLACED STUB FRAME AND FASTENERS LOC. BS296.5 BETWEEN STR7R TO STR11R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG DWG 141A8370 SHEET 9; REV. ; AND DWG 141A8370 SHEET 10; REV. .<BR>SEE INDIVIDUAL SIGN OFFS BELOW. CERTIFIED AS RII.
CRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.375 IN. APROX.AT PASSENGER CABIN 2025-203649<[01] REPLACED STUB FRAME AND FASTENERS LOC. BETWEEN STR7R TO STR11R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG DWG 141A8370 SHEET 9; REV. ; AND DWG 141A8370 SHEET 10; REV. .<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTED ITEM 1 <BR>REPLACED STUB FRAME AND FASTENERS LOC. BS296.5 BETWEEN STR7R TO STR11R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG DWG 141A8370 SHEET 9; REV. ; AND DWG 141A8370 SHEET 10; REV. .<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[03] REPLACED STUB FRAME AND FASTENERS LOC. BS296.5 BETWEEN STR7R TO STR11R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG DWG 141A8370 SHEET 9; REV. ; AND DWG 141A8370 SHEET 10; REV. .<BR>SEE INDIVIDUAL SIGN OFFS BELOW. CERTIFIED AS RII.
CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN LBL 24.75 TO LBL 45.5 AT PASSENGER CABIN 2025-203646<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN LBL 24.75 TO LBL 45.5 AT PASSENGER CABIN B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG 143A0060 SHEET 46 REV -;[02] CORRECTED ITEM 1<BR>REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN LBL 24.75 TO LBL 45.5 AT PASSENGER CABIN B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG 143A0060 SHEET 46 REV - SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN LBL 24.75 TO LBL 45.5 AT PASSENGER CABIN B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG 143A0060 SHEET 46 REV - SEE INDIVIDUAL SIGN OFF BELOW
CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN RBL 24.75 TO RBL 45.5 AT PASSENGER CABIN 2025-203647<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN RBL 24.75 TO RBL 45.5 AT PASSENGER CABIN. B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG 143A0060 SHEET 46 REV -;[02] TASK COMPLETED
CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN 2025-203644<[01] REPLACED FLOOR STRUCTURE BRAKE PANEL AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM-51-40-02-0G; B737-700 SRM-51-10-02-0G ITEM 9 AND DWG:143A0060 SHEET:46 REV:-.<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED FLOOR STRUCTURE BRAKE PANEL AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM-51-40-02-0G; B737-700 SRM-51-10-02-0G ITEM 9 AND DWG:143A0060 SHEET:46 REV:-.<BR>SEE INDIVIDUAL SIGN OFFS BELOW
CRACK BLADE SUPPORT STRUCTURE OF THE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER 2025-203656<[01] REPLEACED BLADE SUPPORT STRUCTURE OF THE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] CORREDTED STEP 1 REPLEACED BLADE SUPPORT STRUCTURE OF THE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. TOOL USED CALIPER P/N: 500-197-30 S/N: A23272233 DUE DATE: JAN-07-2026;[03] CORREDTED STEP 2 REPLEACED BLADE SUPPORT STRUCTURE OF THE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. TOOL USED CALIPER P/N: 500-197-30 S/N: A23272233 DUE DATE: 07-JAN-26;[04] COMPLETED TASK CERTIFIED
CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN 2025-203644 <[01]. REPLACED FLOOR STRUCTURE BRAKE PANEL AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM-51-40-02-0G; B737-700 SRM-51-10-02-0G ITEM 9 AND DWG:143A0060 SHEET:46 REV:-. SEE INDIVIDUAL SIGN OFFS BELOW; [02] REPLACED FLOOR STRUCTURE BRAKE PANEL AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM-51-40-02-0G; B737-700 SRM-51-10-02-0G ITEM 9 AND DWG:143A0060 SHEET: 46 REV:-. SEE INDIVIDUAL SIGN OFFS BELOW.
CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN 2025-203645 <[01]. REPLACED FLOOR STRUCTURE BRAKE PANEL AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM-51-40-02-0G; B737-700 SRM-51-10-02-0G ITEM 9 AND DWG:143A0060 SHEET:46 REV:-. SEE INDIVIDUAL SIGN OFFS BELOW;[02] TASK COMPLETED. SEE INDIVIDUAL SIGN OFFS BELOW; [03] SIGNING FOR MISSING STEPS IN MEASUREMENTS SECTION; 3;4 AND 9.
CRACK ACCESS PANEL 191D AT LOWER FUSELAGE 2025-203626<[01] TOOL USED CALIPER PN: 8647A43; SN: B22440130; DUE DATE: 20/SEP/25.;[02] TOOL USED; HOT BONDER PN: HCS9200B; SN: 16122983; DUE DATE: 22-FEB-26.;[03] TOOL USED; SCALE PN: SCA-301; SN: AE-412135; DUE DATE: 11-APR-25.;[04] REPAIRED ACCESS PANEL 191D AT LOWER FUSELAGE IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. REFER TO INDIVIDUALS SIGNOFFS BELOW.;[05] REPAIRED ACCESS PANEL 191D AT LOWER FUSELAGE IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. REFER TO INDIVIDUALS SIGNOFFS BELOW.
CRACK ACCESS PANEL 191D AT LOWER FUSELAGE 2025-203626<[01] TOOL USED CALIPER PN: 8647A43; SN: B22440130; DUE DATE: 20/SEP/25.;[02] TOOL USED; HOT BONDER PN: HCS9200B; SN: 16122983; DUE DATE: 22-FEB-26.;[03] TOOL USED; SCALE PN: SCA-301; SN: AE-412135; DUE DATE: 11-APR-25.;[04] REPAIRED ACCESS PANEL 191D AT LOWER FUSELAGE IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. REFER TO INDIVIDUALS SIGNOFFS BELOW.;[05] REPAIRED ACCESS PANEL 191D AT LOWER FUSELAGE IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. REFER TO INDIVIDUALS SIGNOFFS BELOW.
CRACK BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB 2025-203624<[01] REPLACED BLADE ON ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02. TOOL USED CALIPER P/N: 500-197-30 S/N: A23272233 DUE DATE: 07-JAN-26;[02] REPLACED BLADE ON ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02. TOOL USED CALIPER P/N: 500-197-30 S/N: A23272233 DUE DATE: 07-JAN-26
CRACK ACCESS PANEL 334GB AT AT LT HORIZONTAL STABILIZER 2025-203633<
CRACK ACCESS PANEL 334GB AT AT LT HORIZONTAL STABILIZER 2025-203633<[01] REPLACED ACCESS PANEL 334GB AT AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 183A3010 SHEET: 2 REV E; FOR INSTALLATION SEE FAULT TTG8Q00YMRX1;[02] COMPLETED TASK CERTIFIED
DETERIORATED PHOTOLUMINISCENT STRIP LIGHTING AT PAX CABIN (10EA) 2025-203584<[01] REPLACED PHOTOLUMINISCENT STRIP LIGHTING AT PAX CABIN (10EA) IAW B737-700 AMM 33-51-15-400-802;[02] COMPLETED TASK CERTIFIED
CRACK SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING 2025-203583<[01] STEP 3. EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 240525411 AND DUE DATE: 13-NOV-25.;[02] STEP 7 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 240525411; CAL DUE DATE: 13-NOV- 25;[03] INSTALLED PERMANENT REPAIR PARTS [1] DOUBLER ; [2] FILLER AND FASTENERS ON SLAT #4 LOCATED SLAT STATION 85.19 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 ;FIGURE 202 ALTERNATIVE 1 SHEET 4 .SEE INDIVIDUAL STEP SIGNOFF BELOW;[04] CERTIFIED WORK PERFORMED; SEE INDIVIDUAL SIGNOFF BELOW
CRACK SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING 2025-203583<[01] STEP 3. EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 240525411 AND DUE DATE: 13-NOV-25.;[02] STEP 7 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 240525411; CAL DUE DATE: 13-NOV- 25
CRACK FWD CORNER SCUFF PLATE LOCATED AT AFT CARGO COMPARTMENT 2025-203590<[01] TOOL USED DIGITAL CALIPER P/N: 500-193-30; S/N: 0000293; DUE DATE: 01-NOV-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1753759 ; DUE DATE : 30/JUN/25;[03] REPAIRED BY WELD FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I. A.W. B737-700 SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4 TO 7); FIGURE 203 REFER TO BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPAIRED BY WELD FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I. A.W. B737-700 SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4 TO 7); FIGURE 203 REFER TO BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.
DETERIORATED PHOTOLUMINISCENT STRIP LIGHTING AT PAX CABIN (10EA) 2025-203584<
CRACK FWD CORNER SCUFF PLATE LOCATED AT AFT CARGO COMPARTMENT 2025-203590<[01] TOOL USED DIGITAL CALIPER P/N: 500-193-30; S/N: 0000293; DUE DATE: 01-NOV-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1753759 ; DUE DATE : 30/JUN/25;[03] REPAIRED BY WELD FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I. A.W. B737-700 SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4 TO 7); FIGURE 203 REFER TO BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPAIRED BY WELD FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I. A.W. B737-700 SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4 TO 7); FIGURE 203 REFER TO BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.
LEFT WING OUTBOARD TRAILING EDGE FLAP HAS A 6' X 6' DELAMINATION ON THE UPPER INBOARD SURFACE.<[01] ACCOMPLISHED TEMP REPAIR TO LW OTBD AFT FLAP DELAMINATION PER EA 24-127-03237 REF TASK ID # TTG8Q00X68ZX.;[02] CORRECTION; ACCOMPLISHED INTEREM REPAIR AS DESCRIBED; NOT TEMP.
FWD CARGO DOOR THRESHOLD BULLNOSE HAS A CRACK AT THE ORIGINAL DENT DAMAGE LOCATION. SEE ATTACHED IMAGE.<[01] REMOVED BULLNOSE THRESHOLD CHORD PER SRM 51-40-02;[02] REMOVED DAMAGE BY BLENDING PER SRM 51-10-02.;[03] PERFORMED NDT HFEC SURFACE INSPECTION PER NDT PART 6; 51-00-00-00 PROCEDURE 23 AND VERIFIED DAMAGE IS COMPLETELY REMOVED.;[04] MACH DRILLED REPLACEMENT COURT BULLNOSE AT FWD CARGO DOOR THRESHOLD PER SRM 51-40-05.;[05] INSPECTION VERIFIED CORRECTIVE ACTION TAKEN IN STEP 4. OK TO INSTALL FORWARD CARGO BULLNOSE CHORD.;[06] REMOVED; DEBURRED; CLEANED; PREPPED; INSTALLED WET WITH SEALANT AND WET INSTALLED FASTENERS PER SRM 51-40-02.;[07] VERIFIED CORRECTIVE ACTION TAKEN IN STEP 6. OK TO CIC FORWARD CARGO BULLNOSE CHORD.
WHEEL WELL FIRE ALARM SOUNDED OFF IN DECENT INTO KMCI MULT TIMES. WHEEL WELL FIRE ALARM SOUNDED OFF IN DESCENT INTO KMCI MULT TIMES.<[01] INSPECTED WHEEL WELL AND FOUND INDICATION ISSUE ONLY. 05 - OK TO CONTINUE PER [MEL 26-4-01;WHEEL WELL FIRE DETECTION SYSTEM]. WITH SP1 & SP3 AND AUTHORIZATION NUMBER 207224. PERFORMED 'OPTION 2;' DISCONNECTED CONNECTORS ON M270 DETECTION ELEMENT.;[02] REMOVED MAIN WHEEL WELL FIRE DETECTION LOOP IAW AMM 26-18-02;[03] R&R WHEEL WELL FIRE LOOP M270 IAW AMM 26-18-02
AFT SERVICE DOOR HANDLE LOOSE<[01] TIGHTENED AFT SERVICE DOOR HANDLE IAW AMM 52-41-31
L1 SLIDE PACK NEEDS TO BE RESECURED.<[01] RE-POSITIONED L1 DOOR SLIDE; CK?S GOOD; REF MT 725-61-06.
FWD ENTRY DOOR EVAC SLIDE PRESS LOW.<[01] R&R FWD ENTRY DOOR SLIDE PER MT 725-61-06-FE.
#1 ENGINE FAILED AT ROUGHLY 7000 FT AFTER DEPARTING KATL NOTICED N1 ON #1 ENGINE ROLLED BACK AND RED ARC ON GAUGE RAN QRC AND QRH PULLED #1 FIRE HANDLE.<
R2 SLIDE HITTING THESHOLD<[01] REPOSITION GIRT ON SLIDE R2 DURING USING MT <BR>725-61-06 (REM/INSTL - SLIDE REMOVAL AND INSTALLATION)&NBSP;&NBSP;&NBSP;&NBSP;&NBSP;TTG8Q00KT3GN;[02] VERIIFIED STEP 1
LH VAPOR BARRIER FWD WEB AT LBL 20 FOUND CRACKED<[01] REMOVED; FABRICATED AND REPLACED CRACKED LH VAPOR BARRIER FWD WEB AT LBL 20 AS PER SRM 51-40-02-0G-0 AND DWG#111A1000.;[02] CARD COMPLETED
CUSTOMER REQUEST : LEFT VAPOR BARRIER - HAS REPAIR APPEARS TO BE LIFTING AT HE EDGE.<[01] APPLIED A PERMANENT REPAIR ON DAMAGED AREA AT L/H VAPOR BARRIER AS PER B737 SRM 51-70-04-2R-10. MATERIALS USED PO#1800550 AND PO#1690463;[02] VERIFIED 1 PERMANENT REPAIR INSTALLED ON LT VAPOR BARRIER.
LEFT WING FWD UNDER WING PANEL 191FL; FASTENER HOLES ELONGATED/DELAMINATED DOT 223-LWP191FL.<[01] (FINAL) REPAIRED DAMAGED AREA AT PANEL 191FL PER B737 SRM 51-70-04-2R-0 MATERIAL USED RESIN 3804 PO#1800550; FIBERGLASS PO#1738579 CABOSIL PO#1775890;[02] C/W
CENTER WHEEL WELL FWD PANEL #193B; ELONGATED FASTENERS HOLES DOT 223-CWP193B.<[01] APPLIED REPAIRED AT PANEL #193B PER B737 SRM 51-70-04-2R-0; LOCATED AND DRILLED REPAIRED FASTENERS HOLES ON CENTER WHEEL WELL FWD PANEL #193B AS PER B737-700 SRM 51-40-05-0G-0; PAINTED CENTER WHEEL WELL FWD PANEL #193B AS PER REF AMM 51-21-73-370-803.;[02] VERIFIED REPAIR.
PANEL 192BL AT FWD EDGE HAS EVIDENCE OF LAYER COMPOSITE LOSS.<[01] REPAIRED DAMAGED AREA AT PANEL 192BL AS PER B737 SRM 51-70-04-2R-6 MATERIAL USED RESIN PO#1800550 AND FABRIC PO#1153636.;[02] FINAL INSPECTION; ALL WORK PERFORMED.
AFT CARGO DOOR CUTOUT AFT CORNER PLATE CRACKED. 8-22<[01] RECEIVED AFT CARGO SCUFF PLATE(WELDED) AFT CORNER FOR OUTSIDE VENDOR JL.WELDING INC ; PART# 146A8341-9 ; PO#413988 ; PART TAG 427115; REPAIR USED SRM 53-60-15-2R-1;BAC5975.;[02] SCUFF PLATE WILL BE INSTALL ON FAULT TTG8Q002HM5X;[03] VERIFIED 1-2.
FWD CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE CRACKED. 8-23<[01] RECEIVED FWD CARGO DOOR FWD CORNER SCUFF PLATE WELDING FROM OUTSIDE VENDOR J.L. WELDING INC. PO# 413985; PN# 143A8331-4; TAG# 427113. SCUFF PLATE WILL BE INSTALLED ON FAULT # TTG8Q002HM50.;[02] FINAL INSPECTION; SCUFF PLATE CRACKED REPAIRED. SCUFF PLATE WILL BE INSTALLED ON FAULT # TTG8Q002HM50.
RIGHT WING LOWER MID SPAN T/E ACCESS PANEL # 661AB HAS SEVERAL FASTENERS HOLES BULGING/CRACKED<[01] REPAIRED AT PANEL # 661AB PER B737 SRM 51-70-04-2R-9 MATERIAL USED RESIN EY3804 PO#1800550 AND FIBERGLASS PO#1690463;[02] VERIFIED 1.
RIGHT WING LOWER MID SPAN T/E ACCESS PANEL # 661CB HAS SEVERAL FASTENERS HOLES BULGING/CRACKED<[01] APPLIED REPAIRED AT PANEL # 661CB PER B737 SRM 51-70-04-2R-0 (4.L.6.7). LOCATED AND DRILLED REPAIRED AREAS ON ACCESS PANEL #661CB AS PER B737-700 SRM 51-40-05-0G-0. APPLIED TOPCOAT ON REPAIRED AREAS AT ACCESS PANEL #661CB AS PER B737-700 AMM 51-21-73-370-803.;[02] FINAL INSPECTION; ALL WORK PERFORMED.
RIGHT WING LOWER MID SPAN T/E ACCESS PANEL # 661BB HAS SEVERAL FASTENERS HOLES BULGING/CRACKED<[01] REPAIRED RIGHT WING LOWER MID SPAN T/E ACCESS PANEL # 661BB AT DAMAGED AREA PER B737 SRM 51-70-04-2R-9 PARA 4.D. LOCATED AND DRILLED REPAIRED AREAS ON ACCESS PANEL #661BB AS PER B737-700 SRM 51-40-05-0G-0 AND APPLIED TOPCOAT ON REPAIRED AREAS AT ACCESS PANEL #661BB AS PER B737-700 AMM 51-21-73-370-803.;[02] FINAL INSPECTION; WORK PERFORMED.
EMERGENCY BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED FIVE BATTERY PACKS AT M01668, M01669, M01670, M01672, AND M01673 IAW AMM 33-51-06.
LEFT A/C BAY DIAGONAL SUPPORT BRACKET JUST O/B OF THE PACK EXHAUST DUCT IS CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02.
MULTIPLE EMERGENCY LIGHTS INOP. FWD GALLEY RH BATTERY CHARGER ASSY KEEPS BLOWING LOWER FUSE. JUST ORDER FWD RIGHT M1674 PACK AND ALL ASSOCIATED LIGHTS JUST A PRECAUTION. FOUND EMER AREA LIGHT ASSY SHORTED AT 6DEF & 6ABC; R&R REF AMM 33-51-03. FOUND EMER BATTERY PACK DISCHARGED AT FWD GALLEY RH; R&R REF AMM 33-51-06. FOUND BATT POWER SUPPLY ASSY INOP AT 17ABC; R&R REF AMM 33-51-06. PERFORMED OPS CHK REF AMM 33-51-00; OPS CHK GOOD.
FLOOR DEGRADED IN FWD CARGO BIN / [01] REPAIRED FLOOR PER AMM 25-52-01
RAMP REPORTS NO2 ENG TAIL PIPE FIRE AFTER SHUTDOWN / [01] INSP MOTOR FOUND OIL ACCMULATION IN CENTER PLUG CAVITY. DRY MOTORED AND RAN ENGINE NO ABNORMAL ANOMALIES NOTED. ALL ENG PARAMETERS NORMAL. A/C OKAY FOR CONTINUED SERVICE IAW FIM 71-05 TASK 811 AUTHORIZATION 72849
-LEFT WING O\B AFT FLAP I\B AFT CORNER DELAMINATED LOWER SURFACE APPROX 11X11; AND UPPER SURFACE APPROX 9X6. / [01] ADDED EA 22-157-01446 TO FAULT.;[02] CW EA-22-157-01446.
AFT MEGAPHONE BROKEN ; / [01] R&R?D AFT MEGAPHONE & OPS NML IAW AMM 25-64-00
DONT WORK CORRECTLY LOWERED CEILING PANEL EMERGENCY POWER SUPPLY LH SIDE AT FWD GALLEY AREA (1 EA) / REPLACED LOWERED CEILING PANEL EMERGENCY POWER SUPPLY LH SIDE AT FWD GALLEY AREA (1EA) IAW B737-700 AMM 33-51-06-960-806 TEST IS OK
MISSING GALLEY 4 LENS EMERGENCY EXIT AT AFT GALLEY AREA (1 EA) / INSTALLED GALLEY 4 LENS EMERGENCY EXIT AT AFT GALLEY AREA (1EA) IAW B737-700 AMM 33-51-01-960-802 ITEM 3C(10)
CORROSION FLOOR BEAM UPPER AREA LOCATED BS 986.5 BTW RBL 44 AND LBL 44 AT AFT GALLEY AREA / REPAIRED FLOOR BEAM UPPER AREA LOC BS986.5 BTW LBL40 TO LBL50 IAW SWA EA #21-153-01264 REV IR AND AEROMAN EA #53-0216-21 REV 0 AND PAGE 1-2 PART 1
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 277 TO BS 294 AND BL 0 FWD GALLEY AND LAV / REPLACED WEB-INTERCOSTAL AND FASTENERS FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294 AND BL0 FWD GALLEY AND LAV IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING #141A5400 REV O PART NUMBER 141A5410U139
CRACK SUPPORT BRACKET LOCATED BS 540 BETWEEN BL 0 TO LBL 24 AT PASSENGER CABIN / REMOVED AND REPLACED SUPPORT BRACKET LOCATED BS540 BTW BL 0 TO LBL 24 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02
CORROSION Z ANGLE LOCATED BETWEEN BS 294.5 TO BS 332.1 WL 207.54 RBL 6 4 AT FWD GALLEY AREA / REPLACED Z ANGLE LOCATED BETWEEN BS 294.5 TO 332.1 WL 207.54 RBL 64 AT FWD GALLEY AREA IAW SRM B737- 700 51-10-02 ITEM 9 AND DRAWING #141A8310 REV: B PART NUMBER USED P/N:141A8312Y5
CORROSION Z ANGLE LOCATED BETWEEN BS 312 TO BS 344 WL 207.54 LBL 64 AT FWD GALLEY AREA / REPLACED Z ANGLE LOCATED BETWEEN BS312 TO BS 344WL 207.54 LBL 64 AT FWD GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-10-02 AND DRAWING 141A8110-13 REV.-
CRACK STRINGER 19R LOCATED ON BS 500D FWD CARGO COMPARTMENT / REPAIRED STRINGER 19R LOCATED BETWEEN BS500B TO BS520 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1 MATERIAL USED BAC1498-157- 7075 TO PO #2020-189930 PN BAC1498-117 PO #2021-
CRACK SUPPORT ANGLE LOCATED BETWEEN BS 380 TO BS 400 BL 0 AT PASSENGER CABIN / REPLACED SUPPORT ANGLE AND FASTENER LOC BTW BS 380 AND BS 400 BL0 FWD PASSENGER CABIN IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 143A5400 REV - MATERIAL USED ALLUMINIUM SHEET 7075 TO 10.071' PO 2021-146858
CRACK SERVICE DOOR CUT OUT ON TIE CLIP LOCATED BS 277 AND STRINGER 10R AT FWD GALLEY AREA / REPLACED TIE CLIP AND FASTENERS LOCATED SERCICE DOOR CUT OUT BS 277 AND STRINGER 10 R AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING $141A1110 REV . 0 AND DRAWING #141A8380 REV . 0.
CRACK ENTRY DOOR CUT OUT INTERCOSTAL WEB LOCATED BEETWEN BS 294.5 TO BS 303.9 AND STRINGER 16L AT FWD GALLEY AREA / REPLACED ENTRY DOOR CUT OUT INTERCOSTAL WEB LOCATED BETWEEN BS 294.5 TO BS303-9 AND STRINGER 16L AT FWD GALLEY AREA UAW B737-700 SRM 51-40-02 AND DWG
CRACK ENTRY DOOR CUT OUT INNER CHORD LOCATED ON BS 303.9 AND STRINGER 17L AT FWD GALLEY AREA / REPLACED INNER CHORD LOCATED ON BS 360 TO BS 270 AT LEVEL STRINGER 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG # 142A0050 REV - .
CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 787 AND BS 767 S-25R WL154.5 AT AFT CARGO COMPARTMENT / REPLACED WEB INTERCOSTAL AND FASTENER LOC BTW BS747 AND BS767 S-25R WL 154.5 AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 146A7502 MATERIAL USED 7075-TO 0.032" BATCH NUMBER:
CORROSION SUPPORT ZEE LOCATED BETWEEN BS 847 AND BS 727 S-25L WL 154.5 AT AFT CARGO COMPARTMENT / REPAIRED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 S-25L WL 154.5 AT AFT CARGO COMPARTMENT IAW SRM B737-700 53-00-53-2R-6 REPAIR 6 AND DRAWING #146A7500 REV:-MATERIAL USED P/N:BAC1496-377
CORROSION SUPPORT ZEE LOCATED BETWEEN BS 767 AND BS 727 S-25R WL 154.5 AT AFT CARGO COMPARTMENT / REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 S-25R WL 154.5 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING #146A7500 REV:-MATERIAL USED P/N:BAC1496-377
CRACK TRACK RBBL 13.84 AT BS 747 AND BS 767 AFT CARGO COMPARTMENT / REPAIRED CARGO TRACK RBBL 13.84 AT BS 727E TO BS 787 AFT CARGO COMPARTMENT IAW SRM B737-700 53-00-53-2R-3 REPAIR 3 FIG. 203 ALTERNATIVE 1 AND ALTERNATIVE 2, MATERIAL USED P/N:BAC1520-1397.
CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS 847 AND BS 867 CEILING PANEL LBL 15 APPROX AFT CARGO COMPARTMENT / REPAIR WEB-INTERCOSTAL LOCATED BETWEEN BS 847 AND BS 867 CEILING PANEL LBL 15 APPROX AFT CARGO COMPARTMENT IAW SWA EA # 21-153-01307 REV IR AND AEROMAN EA # 53-0215-21 REV 0 PART #1
CRACK ANGLE LOCATED BS 867 S-26L AFT CARGO COMPARTMENT / REPLACED ANGLE AND FASTENRS LOCATED BS 867 AND STRINGER 26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9;SRM 51-40-02 DRAWING #149A8402. REV
CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS494 TO BS500A AT LEVEL STR26R AND RBL21.80 AT FWD CARGO COMPARTMENT / REPLACED WEB-INTERCOSTAL LOC BTW BS494 TO BS500A AT LEVEL STR 26R AND RBL 21.80 AT FWD CARGO COMPARTMEN PART NUMBER USED 143A8126-31 PO:0 IAW B737-700
CRACK SUPPORT BRACKET BODY STATION LOCATED AT BS 545 LBL 6 KEEL BEAM. REPLACED SUPPORT BRACKET BODY STATION LOC AT BS 545 LBL 6 KEEL BEAM IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02
CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30 -15-2R-1 REPAIR 1 PARAGRAPH 4B STEP (4) AND BAC 5975.
CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT. REPLACED NEW GUSSET AND FASTERNER LOCATED BS500D AND STR 19L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 PARAG 9 AND DWG 143A1225 REV.A.
CRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT.
CRACK ANGLE - CLIP LOCATED BS400 AFT FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE-CLIP LOC. BS400 AFT FACE AND STR26L FWD CARGO COMPARTMENT PART NUMBER USED 143A7502U155 PO 2020-212944 IAW B737-700 SRM 51-10-02 ITEM 9 51-40-02 AND DWG 143A7505 REV.-
CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED BY WELD FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4B AND BAC 5975 STEP (4).
CRACK ANGLE - CLIP LOCATED BS500C AFT FACE AND STR26L FWD CARGO COMPARTMENT / REPLACED ANGLE CLIP LOC. BS500C AFT FACE AND STR26L FWD CARGO COMPARTMENT PART NUMBER USED 143A7502U155 PO 2020-212944 IAW B737-700 SRM 51-10-02 ITEM 9 51-40-02 AND DWG 143A7505 REV.-
CRACK SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB (3 EA) / REPLACED SEAL-PLATE ACCESS PANEL 333AB AT LH HORIZONTAL STAB (3E/A) IAW B737-700 SRM 51-10-02 ITEM 9
CRACK INSPAR RIB LOCATED STAB STA 147.90 AND 18 INCH FROM REAR SPAR AT RT HORIZONTAL STABILIZER / EVALUATED ALLOWABLE DAMAGE ON INSPAR RIB AND NO FOUND ON SRM B737-700 REPAIR IAW SRM B737-700 55-10-09-2R-4 REPAIR 4.
BROKEN LOWERED CEILING PANEL EMERGENCY EXIT LIGHT AND LENS ASSY AT AFT GALLEY AREA /
BROKEN LOWERED CEILING PANEL EMERGENCY EXIT LIGHT AND LENS ASSY AT AFT GALLEY AREA / REPLACED LOWERED CEILING PANEL EMERGENCY EXIT LIGHT AND LENS ASSY AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-802
CRACK INSPAR RIB LOCATED STAB STA 92.70 AND 18 INCH APPROX FROM REAR SPAR AT RT HORIZONTAL STABILIZER / REPAIRED INSPAR RIB LOCATED STAB STA 92.70 AND 18' APPROX FROM REAR SPAR AT RT HORIZONTAL STABILIZER IAW SRM B737-700 55-10-09-2R-4 REPAIR 4 REPAIRED DUE TO NOT CRACK PERMITTED ON INSPAR RIB IAW SRM B737-700 55-10-09-1A-1 MATERIAL USED. KIT T-SECTION PN 55100003-01 BATH #SW2021000555
CRACK VAPOR VARRIER LH SIDE AT MAIN WHEEL WELL COMPARTME / REPAIRED VAPOR BARRIER LH SIDE AT MAIN WHEEL WELL COMPARTMENT AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10
FLIGHT ATTENDANT NOTICED PRESSURE BELOW GREEN INDICATION OF FORWARD SERVICE DOOR SLIDE. / R&R FWD SERVICE DOOR SLIDE ASSY IAW MT 725-61-06 RAR # 93881 P/N OFF/ON 5A3307-7 S/NOFF BNG20987 S/NON BNG30268
LEFT SIDE EMERGENCY EXIT OVERHEAD LIGHT INOPERABLE. CLOSING DMA PAGE: 0412223. RELAMPED SIDEWALL LIGHT AT SEAT 11A, IAW AMM 33-51-01 CL 57515.
L/H HORIZONTAL STAB RIB 120.33 FWD ATTACH FITTING CRACKED / REMOVED AND REPLACED LH HORIZONTAL STAB RIB 120.33 FWD ATTACH FITTING (RIB STIFFENER) PER DWG #182A5304 REV C; 182A2401 REV:F AND SRM 51-40-05; 51-40-02.
SUPPLEMENTAL INFORMATION: L/H STABILIZER RIB AT STA 120.33 3RD VERTICAL STIFFENER IS CRACKED / REMOVED DAMAGED AND REPAIRED LH STABILIZER RIB AT STA 120.33; 3RD VERTICAL STIFFENER - CATEGOARY A REPAIR INSTALLED PER SRM 55-10-09-2R-4 REPAIR 4.
L/H STABILIZER RIB AT STA 120.33 2ND VERTICAL STIFFENER IS CRACKED / REPAIRED L/H STABILIZER RIB AT 120.33 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4
SUPPLEMENTAL INFORMATION: R/H UPPER ATTACH ANGLE CRACKED BS 663 RBL 41 WL 164 / REMOVED DAMAGE ON R/H UPPER ATTACH ANGLE AND REPAIRED PER SRM 57-10-10-2R-5 BS1.63 RBL 36-63
SUPPLEMENTAL INFORMATION: L/H STABILIZER RIB AT STA 120.33 4TH VERTICAL STIFFENER IS CRACKED / REMOVED DAMAGED AND REPAIRED LH STABILIZER RIB AT STA120.33; 4TH VERTICAL STIFFENER-CATEGORY A REPAIR PER SRM 55-10-09-2R-5. REPAIR 5.
DEFECT TRANSFERRED FROM LOG PAGE 1313904. DEFECT: RIGHT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT STAB STA 193.9; 17' FWD SPAR; CRACK IS 1.5' LONG. / REPAIRED RIGHT HORIZONTAL STABILIZER LWR SKIN AT STAB STA 193.9 IAW SRM 55-10-01-2R-11
DEFECT TRANSFERRED FROM LOG PAGE 1313903. DEFECT: FUSELAGE STA 662 LEFT VAPOR BARRIER SUPPORT T FITTING AT LBL 6.25 CRACKED IN THE RADIUS 2.5' AT THE KEEL BEAM. / REPLACED BS662 L/H VAPOR BARRIER SUPPORT T FITTING IAW DWG 144A7100 AND SRM 51-40-02
LEFT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED AT STAB STA 193.9; 17' FWD SPAR; CRACK IS 1' LONG. REPAIRED LT HORIZONTAL STABILIZER LWR SKIN STAB STA 193.9 IAW SRM 55-10-01-2R-11
DEFECT TRANSFERRED FROM LOG PAGE 1313902. DEFECT: FUSELAGE STA 662 RIGHT VAPOR BARRIER SUPPORT T FITTING AT RBL 6.25 CRACKED IN THE RADIUS 2.5' AT THE KEEL BEAM. / REPLACED R/H BS662 VAPOR BARRIER SUPPORT T FITTING RBL 6.25 IAW DWG 144A7100 AND SRM 51-40-02
KEEL BEAM PANEL 192E FORWARD LEFT AND RIGHT SUPPORT BRACKETS CRACKED / REMOVED AND REPLACED KEEL BEAM PANEL 192E FORWARD LEFT AND RIGHT SUPPORT BRACKETS PER SRM 51-40-02.
LEFT HORIZONTAL STABILIZER REAR UPPER CHORD OUTER SKIN HAS EVIDENCE OF SURFACE CORROSION / REPAIRE L/H HORIZ STAB REAR CHORD SKIN PER EA 20-155-00380 REV IR. THIS IS A PERMANENT REPAIR
RIGHT HORIZONTAL STABILIZER UPPER SLIDING SEAL IS CRACKED / REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER UPPER SLIDING SEAL PER AMM 53-31-31.
LEFT HORIZONTAL FWD UPPER SLIDING SEAL IS CRACKED / REMOVED AND REPLACED LEFT HORIZONTAL FWD UPPER SLIDING SEAL PER AMM 53-31-31
LEFT FWD EMERGENCY LIGHTS FAILED. R&R BATTERY PACK PER AMM.
OVERHEAD OVERWING EMERGENCY EXIT SIGN LOOSE FROM THE CEILING. R&R SIGN HOUSING SIP.
ELECTRICAL SMELL IN THE CABIN. R&R RECIRC FAN AMM.
CABIN FLOOR CHANNEL AT STA 540 RBL 3 CRACKED / REMOVED AND REPLACED CABIN FLOOR CHANNEL AT STA 540 RBL3; IAW B737-700 SRM 51-40-02-0G-0
LEFT WING LEADING EDGE CAVITY UNDER ACCESS WING TO BODY FAIRING 191AL GUSSET ATTACHED TO FRAME STANTION FOR FAIRING IS CRACKED AS MARKED ON AFT SIDE / REMOVED GUSSET ATTACHED TO FRAME AT LEAK WING LEADING EDGE CAVITY ACCESS WING TO BODY RAINING 191AL I.A.W B737-700 SRM 51-40-02-0G-0. VERFIED NEW FRAME P/N 116 A31118-9 ATAG WN6760 I.A.W B737-700 DWG 116A3010 INSTALLED I.A.W B737-700 DWG 116A3010 AND SRM 51-40-02-0G-0
STA 663 L/H VAPOR WEB HAS CRACK 5.5' LONG BETWEEN LBL 31 AND LBL 40 / EVALUATED DAMAGE ON L/H VAPOR WEB STA 663 LBL31 + LBL 40 FOUND TO BE REPAIRABLE CLEANED + PREPPED REPAIR BONDED REPAIR + RESTORED FINISH IAW SRM 57-10-10-2R-2 + 51-70-04-2R-10 + 51-70-04-2R-0 + AMM 51-21-99-300-802
L1 DOOR SLIDE GIRT BAR OFF OF THE SLIDE SHELF. (OUT OF POSITION) / REPOSITIONED GIRT BAR IAW AMM.
RT WING WIGGLE PLATE CRACKED AT OUTBOARD RIVET JUST INBOARD OF #6 FLAP TRACK. R&R WIGGLE PLATE IAW SRM & DWG.
LT WING TRAILING EDGE CAVITY ABOUT 10" OUTBOARD OF LOWER ACCESS PANEL DOOR 551DB WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM & DWG.
R1 DOOR #4 BEAM WHERE HANDLE BOX HOUSING ATTACHES WAS CRACKED. / R&R #4 BEAM IAW SRM & DWG.
FWD SERVICE DOOR #5 BEAM WHERE HANDLE BOX HOUSING ATTACHES IS CRACKED. / REPLACED FWD SERVICE DOOR #5 BEAM WHERE HANDLE BOX HOUSING ATTACHES IAW B737 SRM 51-40-02-0G-0 AND BOEING DRAWINGS 141A6535 REV. D AND 141A6516 REV. D
CENTER WING REAR SPAR VAPOR WEB CRACKED BETWEEN LBL 31.83 TO LBL 40.00. / REPAIRED WEB PER SRM.
CEILING MOUNTED "EXIT" SIGN AT EMERGENCY EXIT ROW LOOSE. SECURED COVER PER MM.
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG FACE CORRODED. REPAIRED FITTING PER EA.
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG FACE CORRODED. REPAIRED FITTING PER EA.
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG FACE CORRODED. REPAIRED FITTING PER EA.
FORWARD GALLEY FLASHLIGHT SECURITY STRAP BROKEN. INSTALLED STRAP IAW AMM.
L1 DOOR EMERGENCY EVAC SLIDE HANGER OUT OF ADJUST. ADJUSTED HANGER PER SIP.
LEFT BULLNOSE EMERGENCY LIGHT INOPERATIVE AT ROW 20. REPLACED THE LAMPS IAW AMM.
WHEEL WELL STA. 663 LBL 26 STIFFENER CRACKED. / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02
LH HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL IS CRACKED / R&R LH HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL PER AMM 53-31-31.
RH HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL IS CRACKED / R&R RH HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL PER AMM 53-31-31.
R1 DOOR SLIDE COMPARTMENT WIRE MISROUTED. REROUTED THE SLIDE WIRE IAW AMM.
RIGHT HORIZONTAL STABILIZER INTERNAL RIB AT STA. 120.30 HAS A CRACK AT THIRD VERTICAL STIFFENER(COUNTING FROM THE FRONT). / REPAIRED THIRD VERTICAL STIFFENER PER SRM 55-10-09-2R
RIGHT HORIZONTAL STABILIZER INTERNAL RIB AT STA. 120.30 HAS A CRACK AT NUMBER FOUR VERTICAL STIFFENER(COUNTING FROM THE FRONT). / REPAIRED PER SRM 55-10-09-2R-4 AND EA 1-755-3534
RIGHT HORIZONTAL STABILIZER INTERNAL RIB AT STA. 120.30 HAS A CRACK AT SECOND VERTICAL STIFFENER(COUNTING FROM THE FRONT). / REPAIRED SECOND VERTICAL STIFFENER PER SRM 55-10-09-2R
CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, BL 0. R&R INTERCOSTAL PER SRM.
CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL PER SRM.
CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL PER SRM.
RT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 43.5. REPAIRED WEB PER SRM.
R2 DOOR SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED THE SLIDE IAW MT.
LEFT MLG WW REAR SPAR VAPOR BARRIER WEB CRACKED BETWEEN LBL 45 TO 55. REPAIRED THE WEB IAW SRM.
LT WING OUTBOARD AFT FLAP TRAILING EDGE SEPARATED, 14" OUTBOARD OF THE INBOARD MOST EDGE. REPAIRED AFT FLAP PER SRM.
EMERGENCY EXIT SIGN LOOSE AT ROW 11 ABC. SECURED THE SIGN IAW MM.
LT OVERWING EXIT LIGHT LENS CRACKED. R&R LENS IAW AMM.
L2 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER IAW SIP.
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1669. R & R BATTERY PACK IAW DWG & AMM.
EMERGENCY LIGHT POWER SUPPLY M01673 INOPERATIVE. R & R POWER SUPPLY IAW AMM.
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1675. R & R BATTERY PACK IAW DWG & AMM.
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1673. R & R BATTERY PACK IAW DWG & AMM.
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1672. R & R BATTERY PACK IAW DWG & AMM.
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1670. R & R BATTERY PACK IAW DWG & AMM.
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1668. R & R BATTERY PACK IAW DWG & AMM.
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1674. R & R BATTERY PACK IAW DWG & AMM.
FORWARD GALLEY EXIT SIGN LENS COVER ON HEADER PANEL CRACKED. R & R COVER IAW AMM.
AFT CARGO DOOR THRESHOLD WEB CORRODED. REPAIRED WEB IAW SRM.
CABIN SEAT TRACK CRACKED AT STATION 727B, RBL 45.5. REPAIRED TRACK IAW EA.
CABIN SEAT TRACK CRACKED AT STATION 727B, LBL 45.5. REPAIRED TRACK IAW EA.
RIGHT OVERWING EXIT SIGN LOOSE. R & R EXIT SIGN IAW MM.
RIGHT OVERWING EXIT SIGN COVER MISSING. INSTALLED COVER IAW SIP.
R1 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.
INFLIGHT SHUT DOWN DIVERSION DECLARED EMERGENCY IN CRUISE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. WE FOLLOWED QRH & SHUTDOWN THE ENGINE. R&R NR 1 ENGINE IAW MT.
FORWARD CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY IAW MM.
AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY IAW MM.
MID CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY IAW MM.
EXIT LENS FELL OFF AT RIGHT OVERWING EXT. RE-INSTALLED EMERGENCY EXIT LIGHT LENS AT RIGHT EMERGENCY EXIT ROW PER AMM.
LEFT EEPLS CRACKED AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.
FORWARD EEPLS BROKEN. REMOVED AND REPLACED EEPLS PER MM.
FORWARD EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
LEFT EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS PER AMM.
LEFT EEPLS LENS BROKEN AT ROW 5. REMOVED AND REPLACED LENS PER AMM.
DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.
LT EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.
R1 DOOR EMERGENCY EXIT SIGN ASSY BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.
DURING SCHEDULED MV2 CHECK, FOUND RT LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED CV CHECK, FOUND EEPLS COVER DAMAGED AT ROW 11. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.