N287WN
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 | 2018-10-09 – 2018-10-09 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2018-10-09 – 2018-10-09 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AFT EMERGENCY EXIT BATTERY PACK M1674 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK PER AMM 33-51-06.
COCKPIT FIRE EXTINGUISHER PRESSURE BELOW LIMITS<[01] R/R COCKPIT FIRE EXT. IAW AMM 26-26-01
GIRT BAR ON L1 DOOR HARD TO GET ON AND OFF CLIPS. RESECURED GIRT BAR ON L1 DOOR PER AMM 25-66-01.
FAS REPORT L1 DOOR LEFT SIDE SLIDE GIRT BAR IS LOOSE. SECURED THE GIRT BAR TO CLIP IAW AMM 25-66-01. OPS CHKD GOOD.
FLT ATT ASSIST HANDLE AFT OF L1 DOOR IS LOOSE 2025-168124 <[01]. CORRECTED INSTALL ASSIST HANDLE AFT OF L1 DOOR I.A.W AMM 25-21-25-420-801 STEP 3. B. (5); [02] INSTALL ASSIST HANDLE AFT OF L1 DOOR I.A.W AMM 25-21-25-420-801 STEP 3. B. (5).
FAULT RAISED TO CAPTURE MANDATORY MEASUREMENT OF CORROSION ON SUPPORT ZEE LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT ADDING RII LABOR ROW REMOVED BY ERROR ON FAULT TTG8Q00Z1GCE <[01]. REPLACED SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; [02] REPLACED SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. RII CERTIFIED.
CUSTOMER REQUEST AAI INSPECTION REFERENCE V909529 - PASSENGER CABIN STA 727B LBL 45.5 IB SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED. MISSING EA IDENTIFIER PER STEP 29 OF EA 130808. 2025-168072<[01] REPAIR SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. ON PASSENGER CABIN STA 727B LBL 45.5 IB IAW EA-130808 STEP 29.;[02] CORRECTED STEP 1. REPAIRED SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. ON PASSENGER CABIN STA 727B LBL 45.5 IB IAW EA-130808 REV P1 STEP 29.;[03] REPAIRED SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. ON PASSENGER CABIN STA 727B LBL 45.5 IB IAW EA-130808 REV P1 STEP 29.
CUSTOMER REQUEST AAI INSPECTION REFERENCE V909529 - PASSENGER CABIN STA 727B LBL 45.5 IB SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED. MISSING EA IDENTIFIER PER STEP 29 OF EA 130808. 2025-168072 <[01]. REPAIR SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. ON PASSENGER CABIN STA 727B LBL 45.5 IB IAW EA-130808 STEP 29.; [02] CORRECTED STEP 1. REPAIRED SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. ON PASSENGER CABIN STA 727B LBL 45.5 IB IAW EA-130808 REV P1 STEP 29.; [03] REPAIRED SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. ON PASSENGER CABIN STA 727B LBL 45.5 IB IAW EA-130808 REV P1 STEP 29.
CORROSION ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 2025-168032 <[01]. TOOL USED ON STEP 4: EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.; [02] TOOL USED ON STEP 5: EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.; [03] TOOL USED ON STEP 7:ULTRASONIC THICKNESS GAGE P/N:45 MG; S/N:221860711; DUE DATE:20-DEC-25.; [04] PERFORMED PERMANENT REPAIR ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 EA #25-157-00651-WIP1 AND EA 25-157-00651. SEE INDIVIDUAL SIGN OFF BELOW.; [05] PERFORMED PERMANENT REPAIR ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 EA #25-157-00651-WIP1 AND EA 25-157-00651. SEE INDIVIDUAL SIGN OFF BELOW.
CORROSION ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 2025-168032<[01] TOOL USED ON STEP 4:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.;[02] TOOL USED ON STEP 5:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.;[03] TOOL USED ON STEP 7:ULTRASONIC THICKNESS GAGE P/N:45 MG; S/N:221860711; DUE DATE:20-DEC-25.;[04] PERFORMED PERMANENT REPAIR ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 EA #25-157-00651-WIP1 AND EA 25-157-00651. SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED PERMANENT REPAIR ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 EA #25-157-00651-WIP1 AND EA 25-157-00651. SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ON BRACKET STRUCTURE WING CENTER SECTION LOCATED BS540 AND BS578 AT LEVEL BL6 KEEL BEAM 2025-168021<[01]. REPLACED BRACKET LOCATED ON STRUCTURE WING CENTER SECTION BS540 AT LEVEL BL6 KEEL BEAM IAW B737 700 SRM 51-40-02-0G AND DWG 149A7701 SHEET 3 REV A.; [02] REPLACED BRACKET LOCATED ON STRUCTURE WING CENTER SECTION BS540 AT LEVEL BL6 KEEL BEAM IAW B737 700 SRM 51-40-02-0G AND DWG 149A7701 SHEET 3 REV A.
CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING 2025-168012 <[01]. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 45 REV-; AND EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMAGE IAW B737-700; MUST BE REPLACED; TOOK MEASURE OF CRACK IS L= 0.950? TOOL USED DIGITAL CALIPER P/N: 500-197-30; S/N: B23412298; DUE DATE: 10-NOV-25.; [02] CORRECTED STEP 1. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 45 REV-; AND EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMAGE IAW B737-700-SRM MUST BE REPLACED; TOOK MEASURE OF CRACK IS L= 0.950? TOOL USED DIGITAL CALIPER P/N: 500-197-30; S/N: B23412298; DUE DATE: 10-NOV-25.; [03] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 45 REV-; AND EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMAGE IAW B737-700-SRM MUST BE REPLACED; TOOK MEASURE OF CRACK IS L= 0.950? TOOL USED DIGITAL CALIPER P/N: 500-197-30; S/N: B23412298; DUE DATE: 10-NOV-25.
CORROSION ON SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT 2025-167993<[01] REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31 REV-.;[02] CORRECTED STEP 1. REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31 REV-. SEE INDIVIDUAL SING OFFS BELOW;[03] RII ITEM <BR>REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31 REV-. SEE INDIVIDUAL SING OFFS BELOW
CORROSION ON SUPPORT ZEE LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT 2025-167994<[01] FABRICATED A NEW SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW;[02] FABRICATED A NEW SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW
CORROSION ON SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT 2025-167993<[01] REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31 REV-.;[02] CORRECTED STEP 1. REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31 REV-. SEE INDIVIDUAL SING OFFS BELOW;[03] RII ITEM <BR>REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31 REV-. SEE INDIVIDUAL SING OFFS BELOW
CORROSION ON SUPPORT ZEE LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT 2025-167994<[01] FABRICATED A NEW SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW;[02] FABRICATED A NEW SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW
CRACK TIE CLIP LOCATED BS277 AND STR10R PASSENGER CABIN 2025-167974 <[01]. REPLACED NEW TIE CLIP LOCATED BS277 AND STR10R PASSENGER CABIN IAW B737-700 SRM-51-40-03-0G-O AND DWG-141A1110 SHEET 17 REV - . SEE INDIVIDUAL SIGN OFF BELOW.; [02] CERTIFIED CORRECTIVE ACTION STEP 1.
CRACK ANGLE BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2025-167870<[01] REPLACED ANGLE BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02;[02] REPLACED ANGLE BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02
CRACK ANGLE BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB 2025-167865<[01] REPLACED ANGLE BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02;[02] REPLACED ANGLE BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02
CRACK WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING 2025-167701<[01] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ON HOLES LOCATED ACCESS PANEL 661CB AT RT WING 2025-167784<[01] STEP 12 TOOL USED ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 10-JUN-25;[02] TOOL USED: MULTIMETER P/N: FLUKE 87-V; S/N: 65700125; DUE DATE: 09-JAN-26. TOOL USED HUMIDITY/TEMPERATURE CHART RECORDER P/N: RH550; S/N: 240531238 ; DUE DATE: 10-SEP-25.;[03] REPAIRED ACCESS PANEL 661CB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPAIRED ACCESS PANEL 661CB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK FWD SERVICE DOOR SCUFF PLATE AT PASSENGER CABIN 2025-167749 <[01]. TOOL USED: DIGITAL CALIPER P/N: 8647A42 S/N: B22440130 DUE DATE: 20-SEP-25; [02] STEP 4. TOOL USING RADIOMETER/PHOTOMETER P/N: XRP-3000; S/N: 1753759; DUE DATE: 30-JUN-25.; [03] REPAIRED BY WELDING FWD SERVICE DOOR SCUFF PLATE AT PASSENGER CABIN CENTER SECTION IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.; [04] REPAIRED BY WELDING FWD SERVICE DOOR SCUFF PLATE AT PASSENGER CABIN CENTER SECTION IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975. SEE INDIVIDUAL SIGN OFF BELOW.
CRACK RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING 2025-167738<[01] REPLACED RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV 2025-167675<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV -SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV -SEE INDIVIDUAL SIGN OFF BELOW. JOB COMPLETED
CRACK RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING 2025-167744<[01] REPLACED RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED
CRACK SUPPORT ANGLE FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING 2025-167645<[01] REPLACED FITTING LOCATED FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEET:7 REV: -.;[02] COMPLETED JOB
CORROSION ANGLE - SUPPORT LOCATED BTW STA 294.5 TO STA 312 RBL 56 AND WL 208.1 AT FWD GALLEY AREA 2025-167730 <[01]. REPLACED NEW ANGLE - SUPPORT LOCATED BTW STA 294.5 TO STA 312 RBL 56 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 SEE INDIVIDUAL SIGN OFF BELOW.; [02] REPLACED NEW ANGLE - SUPPORT LOCATED BTW STA 294.5 TO STA 312 RBL 56 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 SEE INDIVIDUAL SIGN OFF BELOW.
CRACK STUB FRAME LOCATED STA 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2025-167697 <[01]. REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02 AND DWG 141A8370 SHEET 16 REV - DWG 141A8370 SHEET 10 REV D SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1. REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02;DWG 141A8370 SHEET 16 REV - ; DWG 141A8370 SHEET 10 REV D AND DWG 141A8430 SHEET 4 REV B.; [03] CORRECTED STEP 1 AND 2. REPLACED STUB FRAME LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-10-2-0G-0 PARRG 9 AND SRM 51-40-02; DWG 141A8370 SHEET 16 REV - ; DWG 141A8370 SHEET 9 REV D AND DWG 141A8430 SHEET 4 REV B.; [04] TASK COMPLETED. CERTIFIED RII.
CRACK RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING 2025-167717<[01] REPLACED RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED
CRACK STUB FRAME LOCATED STA 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2025-167697<[01] REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02 AND DWG 141A8370 SHEET 16 REV - DWG 141A8370 SHEET 10 REV D SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02;DWG 141A8370 SHEET 16 REV - ;DWG 141A8370 SHEET 10 REV D AND DWG 141A8430 SHEET 4 REV B.;[03] CORRECTED STEP 1 AND 2. <BR>REPLACED STUB FRAME LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-10-2-0G-0 PARRG 9 AND SRM 51-40-02;DWG 141A8370 SHEET 16 REV - ;DWG 141A8370 SHEET 9 REV D AND DWG 141A8430 SHEET 4 REV B.;[04] TASK COMPLETED <BR>CERTIFIED RII
CRACK ON HOLES LOCATED ACCESS PANEL 661CB AT RT WING 2025-167784<[01] STEP 12 TOOL USED ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 10-JUN-25;[02] TOOL USED: MULTIMETER P/N: FLUKE 87-V; S/N: 65700125; DUE DATE: 09-JAN-26. TOOL USED HUMIDITY/TEMPERATURE CHART RECORDER P/N: RH550; S/N: 240531238 ; DUE DATE: 10-SEP-25.;[03] REPAIRED ACCESS PANEL 661CB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPAIRED ACCESS PANEL 661CB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING 2025-167701<[01] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING 2025-167685<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING ; MEASURE OF CRACK IS L:0.600 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[02] CORRECTED STEP 1 REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING ; MEASURE OF CRACK IS L:0.600 INCH. REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING ; MEASURE OF CRACK IS L:0.600 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26
CRACK SUPPORT ANGLE FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING 2025-167645<[01] REPLACED FITTING LOCATED FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEET:7 REV: -.;[02] COMPLETED JOB
CRACK RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING 2025-167738<[01] REPLACED RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED
CRACK RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING 2025-167744<[01] REPLACED RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV 2025-167681<[01] REPLACED WEB INTERCOSTAL WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB INTERCOSTAL WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING 2025-167685<REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING ; MEASURE OF CRACK IS L:0.600 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING ; MEASURE OF CRACK IS L:0.600 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26; REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING ; MEASURE OF CRACK IS L:0.600 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND LBL 47 FWD GALLEY AND LAV 2025-167669<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND LBL 47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV -.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND LBL 47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV -.SEE INDIVIDUAL SIGN OFF BELOW. JOB COMPLETED
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 328 TO STA 344 AND LBL 47 FWD GALLEY AND LAV 2025-167671<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 328 TO STA 344 AND LBL 47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 328 TO STA 344 AND LBL 47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW.
CRACK RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING 2025-167717<[01] REPLACED RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED
CRACK INDICATION ON STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-8 TO STR-9 IN FORWARD GALLEY DOOR RH SIDE; CRACK LENGTH 1.272 INCHES APPROX. 2025-167597 <[01]. REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8370 SHEET 9 TO SHEET 11 REV D. SEE INDIVIDUAL SIGN OFF BELOW.; [02] REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8370 SHEET 9 TO SHEET 11 REV D. SEE INDIVIDUAL SIGN OFF BELOW. RII VERIFIED.
CRACK ANGLE ON INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING 2025-167631<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[02] STEP 1 CORRECTED REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK ANGLE OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[03] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK ANGLE OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.
CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2025-167634<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING ; MEASURE OF CRACK IS L:0.450 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[02] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING ; MEASURE OF CRACK IS L:0.450 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[03] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING ; MEASURE OF CRACK IS L:0.450 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.
CRACK INDICATION ON STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-8 TO STR-9 IN FORWARD GALLEY DOOR RH SIDE; CRACK LENGTH 1.272 INCHES APPROX. 2025-167597<[01] REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8370 SHEET 9 TO SHEET 11 REV D. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8370 SHEET 9 TO SHEET 11 REV D. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII VERIFIED
CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2025-167634<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING ; MEASURE OF CRACK IS L:0.450 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[02] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING ; MEASURE OF CRACK IS L:0.450 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[03] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING ; MEASURE OF CRACK IS L:0.450 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.
CRACK ANGLE ON INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING 2025-167631<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[02] STEP 1 CORRECTED REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK ANGLE OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[03] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK ANGLE OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.
CRACK SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN 2025-167579 <[01]. TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26.; [02] REPLACED SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV A AND DWG 111A6000; SHEET 282; REV -. SEE INDIVIDUAL SIGN OFF BELOW.; [03] REPLACED SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV A AND DWG 111A6000; SHEET 282; REV -. SEE INDIVIDUAL SIGN OFF BELOW.
CRACK SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN 2025-167579 <[01]. TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26.; [02] REPLACED SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV A AND DWG 111A6000; SHEET 282; REV -. SEE INDIVIDUAL SIGN OFF BELOW.; [03] REPLACED SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV A AND DWG 111A6000; SHEET 282; REV -. SEE INDIVIDUAL SIGN OFF BELOW.
CRACK VAPOR BARRIER WEB LOCATED BS663.75 AND LBL 40 AT MAIN WHEEL WELL COMPARTMENT 2025-167480 <[01]. TOOL USED CALIPER P/N 500-197-30 S/N A18135086 DUE DATE 21 JUN 25; [02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18175478 DUE DATE 22 FEB 26; [03] ON STEP 12; TOOL USED: ULTRASONIC FLAW DETECTOR; PN: EPOCH 600; SN: 130547106; DUE DATE: 30-SEP-25; [04] REPAIRED VAPOR VARRIER WEB LOCATED BS663.75 AND LBL 40 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW; [05] REPAIRED VAPOR VARRIER WEB LOCATED BS663.75 AND LBL 40 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW; [06] CORRECTED CORRECTIVE ACTION 5. REPAIRED VAPOR VARRIER WEB LOCATED BS663.75 AND LBL 40 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW. RII ACCOMPLISHED.
CRACK SKIN SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING 2025-167451<[01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138203; DUE DATE: 09-SEP-25;[02] PERFORMED REPAIR ON LOWER SKIN SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; SEE INDIVIDUAL SIGN OFFS BELOW;[03] PERFORMED REPAIR ON LOWER SKIN SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; SEE INDIVIDUAL SIGN OFFS BELOW
CRACK SKIN SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING 2025-167451<[01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138203; DUE DATE: 09-SEP-25;[02] PERFORMED REPAIR ON LOWER SKIN SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; SEE INDIVIDUAL SIGN OFFS BELOW;[03] PERFORMED REPAIR ON LOWER SKIN SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; SEE INDIVIDUAL SIGN OFFS BELOW
CAPTAINS SIDE EXIT ROW SEAT 12A STAYS RECLINED.<[01] ADJUSTED PAX SEAT IN 12A PER MM 25-22-00<BR>OPS CHECK GOOD
FA REPORTS FO SIDE AFT GIRT BAR BRACKET NEEDS ADJUSTED.<[01] ADJUSTED RETAINER CLIP IAW SIP.
FWD ENTRY EMERGENCY EXIT LIGHTS INOP.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
FWD GALLEY SERVICE DOOR AFT SLIDE MOUNT ISOLATOR IS CRACKED.<[01] R&R FWD GALLEY SERVICE DOOR AFT SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.
F/OS ASSIST HANDLE BROKEN AT UPPER W/S FRAME<[01] R/R F/O?S ASSIST HANDLE ASSY PER AMM 56-11-11.
CUSTOMER REQUEST BROKEN BODY STA 663.75 ANGLE UPPER POSITION RBL 7 AT AIR CONDITIONING BAY 2023-378136<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 200048001; DUE DATE: 01-MAY-24.;[02] REPAIRED UPPER ANGLE BODY STA 663.75 BTW RBL 7 TO RBL 21 AT AIR CONDITIONING BAY IAW B737-700 SRM 57-10-10-2R-5 REPAIR 5;[03] STEP 2 ENTERED IN ERROR; CORRECT STEP IS:<BR>REPAIRED UPPER ANGLE BODY STA 663.75 BTW RBL 7 TO RBL 21 AT AIR CONDITIONING BAY IAW B737-700 SRM 57-10-10-2R-5 REPAIR 5<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[04] REPAIRED UPPER ANGLE BODY STA 663.75 BTW RBL 7 TO RBL 21 AT AIR CONDITIONING BAY IAW B737-700 SRM 57-10-10-2R-5 REPAIR 5 ; RII SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK FRAME STA 312 UPPER CHORD BETWEEN S-5L AND S-6L LBL 33 AT PASSENGER CABIN 2023-378124<[01] PERFORMED REPAIR ON BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L IAW EA M-22-153-01244<BR>SEE TASK CARD: TTG8Q00LLCPH;[02] PERFORMED REPAIR ON BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L IAW EA M-22-153-01244 <BR>SEE TASK CARD: TTG8Q00LLCPH
CRACK ON RIB 8 LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER 2023-378132<[01] REPLACED RIB 8 LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A0103 SHEET 7 REV.- SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK CARD COMPLETED <BR>REPLACED RIB 8 LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A0103 SHEET 7 REV.- SEE INDIVIDUAL SIGNOFFS BELOW
CRACK INDICATION FOUND ON ANGLE CLIP LOCATED ON FLOOR STRUCTURE BTW BS 291.5 AND BS296.4 STR 17R RBL 52 AT FWD GALLEY AREA. 2023-378121<[01] TOOL USED: CALIPER P/N 500-752-20 S/N B21038528 CAL. DUE DATE 20 SEP 23.;[02] REPLACED NEW ANGLE CLIP LOCATED ON FLOOR STRUCTURE BTW BS 291.5 AND BS296.4 STR 17R RBL 52 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A8310 SHEET 25 REV-.;[03] CORRECTED STEP 2 <BR>REPLACED NEW ANGLE CLIP LOCATED ON FLOOR STRUCTURE BTW BS 291.5 AND BS296.4 STR 17R RBL 52 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A8310 SHEET 25 REV-. SEE INDIVIDUAL SIGN OFF BELOW;[04] CORRECTED STEP 2 <BR>REPLACED NEW ANGLE CLIP LOCATED ON FLOOR STRUCTURE BTW BS 291.5 AND BS296.4 STR 17R RBL 52 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A8310 SHEET 25 REV-. RII. SEE INDIVIDUAL SIGN OFF BELOW.
CORROSION FLOOR STRUCTURE FLOOR BEAM 986.5 AT RBL 43 WL 208.1 AT AFT GALLEY AREA 2023-378096<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022235; DUE DATE: 03-AUG-23.;[02] TOOL USED P/N FPK-PRO-104 S/N PRO-3384 CAL DUE DATE 24 APR 23.;[03] PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE FLOOR BEAM 986.5 AT RBL 43 WL 208.1 AT AFT GALLEY AREA .IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. MATERIAL USED: STRAP 7075-T6 0.100? P.O: 2012 531818; ANGLE BAC1490-2887 P.O: 2023 124527; FILLER 7075-T6 0.150? P.O:2023 109423;[04] CORRECTED STEP 2: TOOL USED P/N: FPK-PRO-104 S/N PRO-3384 CAL DUE DATE: 24 APR 24.;[05] CORRECTED STEP 3:<BR>PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE FLOOR BEAM 986.5 AT RBL 43 WL 208.1 AT AFT GALLEY AREA .IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. MATERIAL USED: STRAP 7075-T6 0.100? P.O: 2012 531818; ANGLE BAC1490-2887 P.O: 2023 124527; FILLER 7075-T6 0.150? P.O:2023 109423. SEE INDIVIDUAL SIGN OFF BELOW;[06] CORRECTED STEP 3: <BR>PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE FLOOR BEAM 986.5 AT RBL 43 WL 208.1 AT AFT GALLEY AREA .IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. MATERIAL USED: STRAP 7075-T6 0.100? P.O: 2012 531818; ANGLE BAC1490-2887 P.O: 2023 124527; FILLER 7075-T6 0.150? P.O:2023 109423. RII SEE INDIVIDUAL SIGN OFF BELOW.
CORROSION FLOOR STRUCTURE FLOOR BEAM 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2023-378097<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022235; DUE DATE: 03-AUG-23.;[02] TOOL USED P/N FPK-PRO-104 S/N PRO-3384 CAL DUE DATE 24 APR 23.;[03] PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE FLOOR BEAM 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA.IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. MATERIAL USED : STRAP 7075-T6 0.100? P.O: 2012 531818; ANGLE BAC1490-2887 P.O: 2023 124527 FILLER 7075-T6 0.150? P.O:2023 109423. SEE INDIVIDUAL SIGN OFF BELOW;[04] CORRECTED STEP 2: <BR>TOOL USED P/N FPK-PRO-104 S/N PRO-3384 CAL DUE DATE 24 APR 24.;[05] PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE FLOOR BEAM 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA.IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. MATERIAL USED : STRAP 7075-T6 0.100? P.O: 2012 531818; ANGLE BAC1490-2887 P.O: 2023 124527 FILLER 7075-T6 0.150? P.O:2023 109423. RII SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ON UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND RBL 1 WL 208 AT FWD GALLEY AREA 2023-378070<[01] REPLACED UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND RBL 1 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A5400;SHEET 92; REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1. REPLACED UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND RBL 1 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A5400;SHEET 38; REV: A.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND RBL 1 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A5400;SHEET 38; REV: A. <BR>SEE INDIVIDUAL SIGN OFF BELOW <BR>CERTIFIED RII
CRACK ON UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND R BL 10 WL 208 AT FWD GALLEY AREA 2023-378069<[01] REPLACED ANGLE OF INTERCOSTAL AND FASTENER LOCATED BTW BS 380 TO BS 400 AND RBL 10 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; DWG 143A5410-170.<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE OF INTERCOSTAL AND FASTENER LOCATED BTW BS 380 TO BS 400 AND RBL 10 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; DWG 143A5410-170. <BR>SEE INDIVIDUAL SIGN-OFF BELOW<BR><BR>ITEM RII
CRACK ON INTERCOSTAL LOCATED BTW BS 312 TO BS 328 AT LBL 45 AND WL 208 AT FWD GALLEY AREA 2023-378068<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW BS 312 TO BS 328 AT LBL 45 AND WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 141A5400; SHEET 26; REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB - INTERCOSTAL LOCATED BTW BS 312 TO BS 328 AT LBL 45 AND WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 141A5400; SHEET 26; REV - <BR>SEE INDIVIDUAL SIGN OFF BELOW. RII
CRACK ON ANGLE LOCATED INTERNAL STRUCTURE BTW 907 TO BS 927 FWD POSITION BTW STR 26R TO STR 27R AFT CARGO COMPARTMENT 2023-378093CRACK ON STIFFENER LOCATED INTERNAL STRUCTURE BTW 907 TO BS 927 FWD POSITION BTW STR 26R TO STR 27R AFT CARGO COMPARTMENT<[01] REPLACED STIFFENER LOCATED INTERNAL STRUCTURE BTW 907 TO BS 927 FWD POSITION BTW STR 26R TO STR 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 24 REV - SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED
CRACK ON ANGLE LOCATED INTERNAL STRUCTURE BTW 907 TO BS 927 AFT POSITION AND BTW STR 26R TO STR 27R AFT CARGO COMPARTMENT 2023-378094CRACK ON STIFFENER LOCATED INTERNAL STRUCTURE BTW 907 TO BS 927 AFT POSITION AND BTW STR 26R TO STR 27R AFT CARGO COMPARTMENT<[01] REPLACED STIFFENER LOCATED INTERNAL STRUCTURE BTW 907 TO BS 927 AFT POSITION BTW STR 26R TO STR 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 24 REV - SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED
CRACK ANGLE - SUPPORT LOCATED BS827 AND RBL19 WL155 AT AFT CARGO COMPARTMENT 2023-378095<[01] REPLACED ANGLE AND FASTENERS LOCATED BS827 AND RBL19 WL155 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG 146A8120 REV - DWG 146A0081 REV - <BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] TASK COMPLETED ; TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNOFF BELOW
CRACK TRACK LBBL 17.24 LOCATED BS727E AFT CARGO COMPARTMENT 2023-378092<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101U102020; CAL DUE DATE: 30-AUG-23;[02] REPAIRED TRACK LBBL 17.24 LOCATED BS727E AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPAIRED TRACK LBBL 17.24 LOCATED BS727E AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 SEE INDIVIDUAL SIGNOFFS BELOW<BR><BR>ITEM RII
CRACK TRACK RBBL 13.84 LOCATED BS767 AFT CARGO COMPARTMENT 2023-378091<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101U102020; CAL DUE DATE: 30-AUG-23;[02] REPAIRED TRACK RBBL 13.84 LOCATED BS767 AFT CARGO COMPARTMENT IAW B373-700 SRM 53-00-53-2R-3 REPAIR 3 SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPAIRED TRACK RBBL 13.84 LOCATED BS767 AFT CARGO COMPARTMENT IAW B373-700 SRM 53-00-53-2R-3 REPAIR 3 SEE INDIVIDUAL SIGNOFFS BELOW<BR><BR>ITEM RII
CRACK ON UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND R BL 13 WL 208 AT FWD GALLEY AREA 2023-378071<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24;[02] REPLACED UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND RBL 13 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A5400;SHEE 38 REV A<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND RBL 13 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A5400;SHEE 38 REV A <BR>SEE INDIVIDUAL SIGN OFF BELOW AS RII
CRACK STRINGER 23R BS 540 FWD CARGO COMPARTMENT 2023-378089<[01] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 45MG; S/N: 221860711; DUE DATE: 07 NOV 23.;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 60009161631; CAL DUE DATE: 31-JAN-24;[03] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER: P/N:P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24;[04] REPAIRED STR 23R LOC. BTW BS 500D TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[05] REPAIRED STR 23R LOC. BTW BS 500D TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 <BR>SEE INDIVIDUAL SIGN OFFS BELOW. AS RII
CRACK FWD SERVICE DOOR SCUFF PLATE AT PASSENGER CABIN 2023-378048<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A21042019;DUE DATE:17-MAR-24.;[02] TOOL USED : LIGHT METER P/N XRP-3000 S/N 1998072 DUE DATE: 15-OCT-23.;[03] REPAIRED FWD SERVICE DOOR SCUFF PLATE AT PASSENGER CABIN I.A.W. BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975 SEE INDIVIDUAL SIGNOFFS BELOW;[04] JOB COMPLETED
CRACK INSPAR RIB 92.70 AT 30 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2023-378014<[01] TOOL USED: EDDY CURRENT EQUIPMENT. P/N: NORTEC 600D. S/N: 210138003. DUE DATE: 27-MAR-24.;[02] REPAIRED INSPAR RIB 92.70 AT 30 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN-OFF BELOW.;[03] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW
CRACK CUT OUT EMERGENCY DOOR PLATE LOC BTW STR 10L TO STR 11L AT PASSENGER CABIN 2023-378013<[01] REPLACED NEW PLATE LOC EMERGENCY DOOR BTW STR 10L TO STR 11L STA 621.73 TO STA 633.26 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 411A2857 SHEET 1 REV.D AND SRM 51-10-02 ÿ½TEM 9 . SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED NEW PLATE LOC EMERGENCY DOOR BTW STR 10L TO STR 11L STA 621.73 TO STA 633.26 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 411A2857 SHEET 1 REV.D AND SRM 51-10-02 ÿ½TEM 9 . SEE INDIVIDUAL SIGN OFF BELOW. RII CERTIFIED
INOP LOWERED CEILING PANEL BATTERY PACK LT SIDE AT AFT GALLEY AREA (1 EA) 2023-378027<[01] REPLACED LOWERED CEILING PANEL BATTERY PACK LT SIDE AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-06-960-805;[02] REPLACED LOWERED CEILING PANEL BATTERY PACK LT SIDE AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-06-960-805
CUSTOMER REQUEST CRACK ON INTERNAL SURFACE OF CENTER MLG DOOR LH SIDE 2023-377973<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022235; DUE DATE: 03-AUG-23.;[02] TOOL USED: P/N; 500-193-30 S/N; 0000291 DUE DATE; 12-OCT-23;[03] REPAIRED CENTER MLG DOOR LH SIDE IAW B737-700 SRM 52-80-02-2R-3 FIG 202 SHEET 5; SHEET 6 AND SHEET 7. SEE INDIVIDUAL SIGNOFFS BELOW;[04] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW
INOP LOWER SIDEWALL PANEL BATTERY PACK ON BS 616 RT SIDE AT PASSENGER CABIN 2023-377921<[01] REPLACED LOWER SIDEWALL PANEL BATTERY PACK ON BS 616 RT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 AND B737-700 WDM 33-51-13. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] JOB COMPLETED
CRACK ANGLE LOCATED BS 500C FWD SIDE AND S-26L FWD CARGO COMPARTMENT 2023-377912<[01] REPLACED ANGLE LOCATED BS 500C FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG 143A7505 SHEET 82;REV-.SEE INDIVIDUAL SIGN OFF BELOW;[02] COORECTED STEP 1:<BR>REPLACED ANGLE LOCATED BS 500C FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 AND DWG 143A7505 SHEET 82 REV-.;[03] REPLACED ANGLE LOCATED BS 500C FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 AND DWG 143A7505 SHEET 82 REV-.<BR>CERTIFIED AS RII
CRACK GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT 2023-377908<[01] REPLACED GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 209 REV-.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 209 REV-.SEE INDIVIDUAL SIGN OFF BELOW.<BR>CERTIFIED AS RII
CRACK GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT 2023-377910<[01] REPLACED GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV-<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV- <BR>SEE INDIVIDUAL SIGN OFF BELOW<BR>CERTIFIED AS RII
CRACK ANGLE FLOOR STRUCTURE BTW STA 685 TO STA 706 AND RBL 24.75 AT PASSENGER CABIN 2023-377867<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24.;[02] REPLACED ANGLE FLOOR STRUCTURE BTW STA 685 TO STA 706 AND RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV: A<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED ANGLE FLOOR STRUCTURE BTW STA 685 TO STA 706 AND RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV: A <BR>SEE INDIVIDUAL SIGN OFF BELOW<BR>CERTIFIED AS RII
R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP<[01] RELUMPED R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT PER AMM 33-51-04. OPS CHECKED GOOD
RH I/B FLAP T/E WEDGE DELAMINATED. REMOVED RH I/B FLAP T/E WEDGE PER SRM 51-40-02. LOCATED AND DRILLED NEW WEDGE ASSY P/N: 113A2550-604 PER SRM 51-40-05.;[04] APPLIED SURFACE FINISH PER AMM 51-21-99;[05] INSPECTION VERIFIED CORRECTIVE ACTION STEPS 1 THRU 4. OK TO INSTALL WEDGE ASSEMBLY.;[06] INSTALLED NEW WEDGE ASSY P/N: 113A2550-604 PER SRM 51-40-02.;[07] INSPECTION VERIFIED CORRECTIVE ACTION STEP 6.;[08] INSTALLED PANEL 653ET REFERENCE SOPM 20-50-01.;[09] C/W OF INSPECTION STEP 8 ABOVE.;[10] C/W
FOUND 10 INCH LONG CRACK IN FWD CARGO COMPOSITE FLOOR PANEL AFT OF CARGO DOOR. REMOVED AND REPLACED THE FLOOR PANEL 120CF IAW AMM 25-52-10.
FLOOR GIVES WAY AND THUMPS BETWEEN ROW 13 AND 14 / [01] REMOVED AND REPLACED PASSENGER CABIN FLOOR PANEL BETWEEN ROW 13 AND 14 IAW AMM 53-21-00 NO DEFECTS NOTED.
RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED / [01] R&R RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL REF AMM 53-31-31.
FLOOR LIGHTING AT ROW 8-9 AC LEFT NEEDS TO BE SECURED. / [01] RESECURED FLOOR EMERGENCY LIGHTING AT 8/9 ABC PER AMM 33-51-12.
FLOOR LIGHT STRIPS AT 9 & 10 DEF DETACHED FROM FLOOR CAUSING A TRIP HAZARD. ; / [01] RESECURED FLOOR PROXIMITY LIGHT AT 9& 10 DEF IN REF. TO AMM 33-51-14.
SUPPLEMENTAL INFORMATION: PHOTO LUMINESCENCE LIGHT STRIPE I FLIGHT AT SEAT 8/9 BOTH SIDES ; / [01] SECURED PHOTO IIIMINESCENCE EXIT LIGHT AT ROW 8/9 PER AMM 33-51-15
FWD LOWERED CEILING L/H EMERGENCY LIGHT BATTERY PACK MO1675 IS BAD ; / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT FWD LH LOCATION MO1675 IAW AMM 33-51-06-960-805. OPS CHECK GOOD.; [02] VERIFIED STEP 1.<BR>AUDIT C/W
PASSENGER CABIN - LH STOWBIN BULLNOSE EMERGENCY LIGHT INOP SEAT ROWS 17-24. ; / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT AFT LH LOCATION IAW AMM 33-51-06-960-805. OPS CHECK GOOD.; [02] VERIFIED STEP 1.<BR>AUDIT C/W
AFT CARGO AFT CORNER SCUFF PLATE CRACKED ; / [01] REPAIRED CRACKED AFT CARGO AFT CORNER SVUFF PLATE IN BACKSHOP ON WO:42436-8300-0001.; [02] VERIFIED ITEM 1.<BR>AUDITED.
AFT CARGO COMPT. Z-ANGLE STA 747+18; RBL 25; WL 156 HAS CORROSION UPPER SURFACE DOT A-21-71 ; AFT CARGO COMPT. Z-ANGLE STA 747+18; RBL 25; WL 156 HAS CORROSION (LOWER) SURFACE DOT A-21-71 / [01] REMOVED CORROSION FROM RH Z-ANGLE IN AFT CARGO COMPARTMENT. IAW SRM 5-10-02-0G-0. PAR 15. VERIFIED WITH 102X MAG GLASS.; [02] VERIFIED MATERIAL LOSS TO BE AS FOLLOWS ORIGINAL THICKNESS .040'; LOSS .009'; REMAINING MATERIAL .031'. OUT OF LIMITS IAW SRM 53-00-53-1A-2. AAR TOOL 36949 CAL DUE DATE 04 AUG 21.; [03] NEW Z ANGLE FABRICATED ON TTG8Q005QK0Z. NEW Z ANGLE INSTALLED ON TTG8Q004E6LY.; [04] VERIFIED STEPS 1;2;3<BR>AUDIT C/W
AFT CARGO COMPT. Z-ANGLE STA 727C+10; RBL 25; WL 156 HAS CORROSION UPPER SURFACE DOT A-21-68 ; / [01] REMOVE CORROSION FROM RH Z-ANGLE IAW SRM 51-10-02-0G-0. PAR 15; AND VERIFIED WITH 10X MAG GLASS.; [02] VERIFIED MATERIAL LOSS. ORIGINAL THICKNESS .040'; LOSS OF .018'; REMAINING MATERIAL .022'. OUT OF LIMITS IAW SRM 53-00-53-1A-0 AAR TOOL 36649; CAL DATE 04 AUG 21.; [03] MATERIAL VERIFIED AS BAC1496-377 7075T6 A23339 IAW SRM 53-00-53-2R-5 REPAIR 5; [04] VERIFIED ITEMS 1 - 3.; [05] FABRICATED NEW Z-ANGLE IAW SRM 53-00-53-2R-5 REPAIR 5; [06] VERIFIED ITEM 5.<BR>OK TO TREAT & PRIME.; [07] TREATED AND PRIMED NEW Z ANGLE IAW SRM 53-00-53-2R-5 REPAIR 5; [08] VERIFIED ITEM 7 ON NEW Z-ANGLE; [09] INSTALLED NUTPLATES ON NEW Z-ANGLE FROM STA 727-767 IAW SRM 51-40-10-2R-0 STEPS 5 A-H; [10] VERIFIED ITEM 9; PUSH TEST NEEDS ACP; [11] REFERENCE ITEM 3; REPAIR Z-ANGLE IS FROM STA: 727 TO 767.; [12] PERFORMED NUTPLATE PUSH TEST. TESTS GOOD IAW SRM 51-40-10-2R-0. TOOL # 42641 DUE 12/14/21; [13] VERIFIED STEP 12; [14] FABRICATED NEW Z ANGEL FROM STA 727-767. NEW Z ANGLE INSTALLED ON TTG8Q004E6LY; [15] VERIFIED STEP 14; [16] AUDIT C/W
AFT CARGO COMPT. Z-ANGLE STA 767+14; LBL 25; WL 156 HAS CORROSION UPPER SURFACE DOT A-21-64 ; / [01] EVALUATED CORROSION ON L/H ZEE ANGLE; ORIGINAL THICKNESS .040'; LOSS .020' REMAINING .020' OUT OF LIMITS IAW SRM 53-00-53-1A-2; [02] VERIFIED MATERIAL FOR ZEE ANGLE REPLACEMENT; BAC1496 7075-T62 ATAG 76442 IAW SRM 53-00-53-2R-5 TABLE 201.; [03] VERIFIED STEP 1.; [04] VERIFIED MATERIAL IN STEP 2.; [05] FABRICATED ZEE ANGLE REPLACEMENT SECTIONS FROM STA 727 TO 847 IAW SRM 53-00-53-2R-5 SECTION 4. D -H.; [06] INSPECTION CW STEP 5; [07] OK TO TREAT AND PRIME; [08] APPLIED CHEMICAL CONVERSION AND PRIMER TO ZEE ANGLE REPLACEMENT SECTION IAW SRM 53-00-53-2R-5 SECTION 4. I AND J.; [09] VERIFIED STEP 8.; [10] APPLIED NUTPLATES IAW SRM 51-40-10-2R-0 STEPS 5 A-H; [11] VERIFIED STEP 10 <BR>PUSH TEST NEEDS ACCOMPLISHED; [12] PERFORMED NUTPLATE PUSH TEST. TESTS GOOD IAW SRM 51-40-10-2R-0. TOOL # 42641 DUE 12/14/21; [13] VERIFIED STEP 12; [14] AFT CARGO COMPARTMENT LH Z-ANGLE; EVALUATED CORROSION VERIFED; ORIGINAL T .040'; LOSS .020'; REMAINING MATERIAL .020'. OUT OF LIMITS IAW SRM 53-00-53-1A-2. FABRICATED NEW Z-ANGLE BS 727-847; LBL 25 WL 156; IAW SRM 53-00-53-2R-5; LH Z-ANGLE INSTALLED ON (5360-E-16462-NG) TTG8Q004E6LY.; [15] C/W; [16] VERIFIED STEPS 14<BR>AUDIT C/W
DOT 045-001; L2 DOOR LOWER AFT ATTACH BRACKET IS CRACKED; COMMON TO DOOR AND SWEEPER SEAL PLATE. ; / [01] REMOVED L/2 SWEEPER SEAL BRACKET I/A/W SRM 51-40-02-0G-0; [02] DISPLACED L/2 DOOR LINER I/A/W SRM 51-40-02-0G-0; [03] REMOVED AND INSTALLED NEW L/2 DOOR LOWER AFT ATTACH BRACKETAT SWEEPER SEAL PLATE I/A/W SRM 51-40-02-0G-0 A TAG A63434; [04] VERIFIED STEP 3.<BR>OK TO INSTALL SWEEPER SEAL BRACKET AND LINER; [05] INSTALLED SWEEPER SEAL BRACKET AND LINER INSTALLED L/2 DOOR LOWER AFT ATTACH BRACKET COMMON TO FOOD AND SWEEPEF SEAL PLATE I/A/W AMM 52-13-31-400-802; [06] VERIFIED STEP 5.<BR>AUDIT C/W
LEFT HORIZONTAL STAB INSPAR RIB 5 (STAB STA 129.50); STIFFENER 3 HAS CRACK NEAR LOWER SKIN DOT A-21-41 ; / [01] CUT AND REMOVED DAMAGE IAW SRM 55-10-09-2R-4 REPAIR 4; [02] PERFORMED GVI OF ALL AREAS WITHIN THE REPAIR AREA. NO DEFECTS NOTED IAW SRM 55-10-09-2R-4 REPAIR 4; [03] VERIFIED STEP 1<BR>COMPLETED STEP 2 GVI REPAIR AREAS; [04] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 23 & PROC 16. NO DEFECTS NOTED. TOOL#31822; DUE 12AUG21; [05] KIT VERIFIED AS P/N 55100003-01 WN5067 IAW SRM 55-10-09-2R-4 REPAIR 4 AND DWG 55100003 REV B; [06] VERIFIED STEP 5; [07] FABRICATED REPAIR PARTS IAW SRM 55-10-09-2R-4 REPAIR 4; [08] VERIFIED ITEM 7; [09] OK TO INSTALL; [10] INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4 REPAIR 4; [11] VERIFIED STEP 10<BR>OK TO CIC; [12] APPLIED CIC TO REPAIR AREA IAW SRM 55-10-09-2R-4 REPAIR 4; [13] VERIFIED STEP 12; [14] C/W; [15] AUDIT C/W
FWD SERVICE DOOR #4 BEAM 141A3536-14 IS CRACKED NEAR INBD HOLE. REMOVED R/1 DOOR LINER I/A/W AMM 52-41-31-000-802 REMOVED R/1 DOOR HANDLE BOX ASSY IAW SRM 51-40-02-0G-0 REMOVED UPPER & LOWER SPICE ANGLE IAW SRM 51-40-02-000-0G. REMOVED R/1 DOOR PNL 841CZ841BZ BEGAN REMOVAL OF #4 BEAM IAW SRM 51-40-02-OG-0. BEGAN LOCATING AND DRILLING #4 BEAM IAW SRM 51-40-05-0G-0 DWG'S 141A6516 AND 141A6535REMOVED AND REPLACED FWD SERVICE DOOR # 4 BEAM P/N 141A3536-14 I/A/W ARM 51-40-02-0G-0 AND BOEING DWG # 141A6516 AND 141A6535.
VERTICAL STAB FIXED L/E SPRING P/N 176A3101-26 R/H SIDE HAS CRACK AT RADIUS DOT A-21-11 ; / [01] REMOVED CRACKED FIXED L/E -26 SPRING IAW SRM 51-40-02-0G.; [02] RECEIVED NEW PART P/N 176A3101U26; A-TAG AK7947; LOCATED AND DRILLED ALL HOLES TO SIZE AND DEBURRED IAW IPC 55-33-11-02A AND SRM 51-40-05-0G; [03] VERIFIED STEP 1;2; [04] OK TO INSTALL P/N 176A3101U26; [05] INSTALLED NEW -26 SPRING IAW SRM 51-40-02-0G.; [06] VERIFIED STEP 5. OK TO CIC; [07] APPLIED CIC IAW AMM 51-21-91-620. ALL WORK COMPLETE.; [08] VERIFIED STEP 7; [09] AUDIT COMPLETE
A-061 DOT 007 WIGGLE PLATE PHENOLIC CRACKER UNDER R/H WING PNL 661AB ; / [01] REMOVED AND REPLACED WIGGLE PLATE(P/N 115A3760Y26 ATAG: A62893) UNDER LOWER WING PANEL 651 AB I/A/W SRM 51-40-02 AND IPC 57-50-00-18; [02] OK TO TREAT AND PRIME LOWER WING SKIN; [03] TREATED AND PRIMED LOWER WING SKIN I/A/W AMM 51-21-41-370-803 AND AMM 51-21-72-370-804; [04] VERIFIED STEPS 1;3<BR>OK TO PAINT; [05] APPLIED TOPCOAT TO LOWER WING SKIN I/A/W AMM 51-21-73-370-804; [06] VERIFIED STEP 5<BR>AUDIT C\W
FWD SERVICE DOOR #5 BEAM 141A6536-15 IS CRACKED IN RADIUS NEAR INBD HOLE. STARTED REMOVAL OF #5 BEAM IASW SRM 51-40-02-OG-0. LOCATED AND DRILLED NEW BEAM IAW EO 5241-C-1493-NG SRM 51-40-05-0G-0 DWG'S 141A6516 REV C. INSTALLED #5 BEAM IAW SRM 51-40-02-0G-0 AND DWG 141A6516 141A6535. REMOVED AND REPLACED #5 BEAM IN FWD SERVICE DOOR IAW SRM 51-40-02-0G-0 AND DWGS 141A6516 141A6535 AND EL 5241-C-1493-NG.
A-061DOT 008 CURVED BULB SEAL RETAINER CRACKER R/H WING 12'' INBD OF DEFLECTOR RIB ; CORRECTION CHANGE CRACKER TO CRACKED / [01] REMOVED WEB AND RETAINER IASW SRM 51-40-02-0G-0.; [02] VERIFIED NEW PART AS P/N 115A2953-2. A-TAG A24928. IAW BOEING DWG 115A2930 REV-.; [03] LOCATED AND DRILLED RETAINER IAW SRM <BR>51-40-05-0G-0.; [04] INSPECTION CW STEPS 1-3. OK TO INSTALL ON AIRCRAFT.; [05] INSTALLED RETAINER IAW SRM 51-40-02-0G-0. BOEING DWG 115A2930 REV-. ALL STEPS 1-5 C/W.; [06] VERIFIED STEP 5.<BR>AUDIT C/W
FWD CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED ; / [01] RECIEVED REPAIRD SCUFF PLATE FROM BACKSHOP ON WORKORDER 42436-1400-0001; [02] VERIFIED STEP 1. AUDIT COMPLETE
CABIN FLOOR PANEL 242BF TOP SURFACE HAS AREAS OF PULLED FIBERS. EVALUATED PANEL 242BF AND DAMAGED FIBERS 1PLY TO UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR1A REV73. CLEAN AND PREP PANEL FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3ACE&F REV73. VERIFIED MATERIALS. (A51753)(A24484). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201 REV73. VERIFIED STEP 1 AND OK TO BOND BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3K-M REV73. AAR DIGITAL THERMOMETER 30347 4-29-22 150DEG 3HRS. REPAIRED DAMAGED AREA ON UPPER FACE SHEET OF PANEL 242BF. IAW B737-700 SRM 53-00-50-2R-1 SRM 53-00-50-2R-0.
FWD CARGO FLOOR PANEL 120BF IS CORRODED ALONG EDGE DOT A-203-006 ; / [01] VERIFIED MATERIAL AS 2024-T3; .071; IAW AMM 25-52-01-201-801. A-TAG # A53465.; [02] VERIFIED MATERIAL STEP 1.; [03] OK TO TREAT AND PRIME; [04] FABRICATED REPLACEMENT FWD CARGO FLOOR PANEL; VERIFIED MATERIAL AS 2024-T3 .071 A-TAG # A53465 IAW AMM 25-52-01-201-801. TREATED BACK OF PANEL IAW AMM 51-21-41-370-803. PRIMED TREATED SIDE IAW AMM 51-21-72-370-804; [05] VERIFIED STEP 4.<BR>AUDIT C/W
LT OVERWING EXIT ASSIST HANDLE HOUSING IS NOT SECURE. REPAIRED, PER AMM 20-60-11 BY INSTALLING MISSING SCREWS.
SF ESCAPE SLIDE GAUGE IN RED. R & R SF ESCAPE SLIDE, PER MT 725-61-00 + MT 25-66-20 RAR 71071 POS SF TAG 714864 P/N OFF/ON 5A3307-7 S/N OFF BNG 7842 S/N ON BNG 15978.
FA'S REPORT GIRT BER FLAG OVER R1 DOOR DIFFICULT TO SECURE IN ARMED POSITION CLEAN SLIDE LATCHES; CHECKS GOOD SIP FLAG
FLOOR BOARD BREAK CRACKED AT STA 540 LEFT OF BUTT LINE 0. / REMOVED AND REPLACED FLOOR BOARD BREAK ASSY AT STA 540 LEFT OF BUTT LINE 0 IAW SRM 51-40-02 AND AMM 53-21-00
1ABC EMERGENCY FLOOR TRACK STRIP DAMAGED. REMOVED AND REPLACED 1ABC EMERGENCY FLOOR TRACK STRIP PER ENG DWG 33500007.
1FED EMERGENCY FLOOR TRACK STRIP DAMAGED. REMOVED & REPLACED 1FED EMERGENCY FLOOR TRACK STRIP; PER DWG 33500007.
FLOOR BOARD BREAK CRACKED AT STA 540 RIGHT OF BUTT LINE 0. / REMOVED AND REPLACED FLOOR BOARD BREAK ASSY AT STA 540 RIGHT OF BUTT LINE 0 IAW AMM 53-21-00 AND SRM 51-40-02
OVERHEAD EXIT SIGN AFT GALLEY BROKEN. / R&R'D AFT OVERHEAD EXIT SIGN PER MM.
OVERHEAD OVERWING EMERG. EXIT SIGN HANGING BY WIRE. / REINSTALLED SEALING EXIT SIGN ASSEMBLY PER AMM 33-51-01 AC OK FOR SERVICE
EMERGENCY BATTERY PACK M1674 DEFECTIVE AT FORWARD ENTRY RIGHT CEILING PANEL. R&R BATTERY PACK M1674 AS PER AMM.
APU DOOR RIB AFT SIDE OF FWD HINGE HAS WHAT APPEARS TO BE 2 OLD CRACKES BY BOLT HOLE. / REMOVED DAMAGE RIB ;FABRICATED AND INSTALED NEW RIB AT RT APU DOOR FWD HINGE AFT SIDE PER REF B737 SRM 51-40-02-0G-0 ANDDWG NO 148A6353
APU DOOR RIB FWD SIDE OF FWD HINGE HAS WHAT APPEARS TO BE 3 OLD CRACKES BY BOLT AND RIVET HOLES / REMOVED DAMAGE RIB; FABRICATED AND INSTALLED NEW RIB AT RT APU DOOR FWD HINGE FWD SIDE PER REF B737 SRM 51-40-02-0G-0 AND DWG NO 148A6353
FUSELAGE SKIN AT APU DOOR FWD HINGE CUTOUT DAMAGED. / CUT OUT DAMAGED AREA AT FUSELAGE SKIN APU DOOR FWD HINGE PERFORMED ROTO INSP AND HFEC INSP NO CRAKCS NOTED; FABRICATED DOUBLER MAT USED 2024T3.125' PO #1354279 FILLER MAT USED 2024T3.100' PO #1596666 TREATED AND PRIMED REPAIR PARTS; INSTALLED REPAIR AND FILLER REF B737-700 SRM 51-40-02-0G-0; 53-80-01-2R-1 REPAIR 1; SOPM 20-41-02 ; NDTM P6 51-00-00 PROC 16 AND PROC 23
R/H HORIZONTAL STABILIZER INTERNAL RIB AT STA. 120.30 CRACKED AT MOST AFT VERTICAL STIFFENER AND LOWER CHORD. / REPAIRED LOWER CHORD PER SRM.
R/H HORIZONTAL STABILIZER LEADING EDGE FAIRING 341B CRACKED AT 4TH RIB FROM INBOARD INTERNAL. R&R RIB IAW SRM & DWG.
FLOOR TRACK AFT CARGO JUST O\B OF S27R HAS 5 NUTPLATE HOLES CORRODED JUST AFT OF STA 921. / REMOVED AND INSTALLED NEW FLOOR TRACK P/N 7530159 AT O/B OF STR 27R. RBL 13.8 FROM STA 887 TO STA 947 REF B737-700 SRM 51-40-02-0G-0 AND DW # 147A7500
INTERCOSTAL JUST OUTBOARD CORRODED AT BS. 921, STR. 27L. R&R TRACK PER SRM AND DWG.
AFT CARGO COMPARTMENT L/H Z CHANNEL CORRODED BETWEEN BS. 727E+8 TO BS. 787+8. / R&R Z CHANNEL IAW SRM AND DWG.
FWD CARGO COMPARTMENT.R/H LOWER SIDE WALL Z CHANNEL SUPPORT FLOOR CORRODED AT STA 500 TO STA 500A ; S-25R MKD DOT 60-005 / REMOVED AND REPLACED DAMAGE Z CHANNEL SUPPORT AT FWD CARGO COMP. R/H SIDEWALL LOWER AREA STR 25 RT FROM STA 500 TO STA 500A PER REF B737 SRM 51-40-02-0G-0; AND DWG 143A8126
FORWARD CABIN WET AREA R1 DOOR ENTRY FLOOR SUPPORT INTERCOSTAL CRACKED AFT END AT BS. 328, RBL 30. / R&R FLOOR SUPPORT INTERCOSTAL PER SRM.
AFT CARGO COMPARTMENT R/H LOWER SIDE WALL Z CHANNEL SUPPORT CORRODED BETWEEN BS. 767 TO BS. 787, STR. 25R. / R&R Z CHANNEL PER SRM AND DWG.
RT HORIZONTAL STAB INTERNAL RIB 4 AT STAB. STA. 120.30 HAD TWO CRACKS AT STIFFENERS LOWER AREA. REPAIRED RIB PER AMM, SRM, AND DWG.
RT HORIZONTAL STABILIZER INTERNAL RIB 5 AT STAB. STA. 129.50 HAD ONE CRACK AT STIFFENER LOWER AREA. REPAIRED RIB PER SRM AND DWG.
FORWARD CABIN WET AREA FORWARD OF L1 DOOR CUTOUT FLOOR SUPPORT SURFACE CRACKED BETWEEN BS. 260 TO BS. 360, LBL 55. R&R FLOOR SUPPORT IAW SRM AND DWG.
LT HORIZONTAL STABILIZER INTERNAL RIB INBOARD SIDE AT STAB. STA. 120.30 CRACKED AT STIFFENER LOWER AREAS. REPAIRED RIB IAW SRM AND DWG.
FORWARD CARGO DOOR CUTOUT AFT SCUFF PLATE SECTION CRACKED. REPAIRED SCUFF PLATE PER EA.
FLOOR SUPPORT CORRODED. R&R FLOOR SUPPORT PER SRM AND DWG.
FORWARD CARGO THRESHOLD HAD SEVERAL AREAS OF CORRODED. R&R WEB IAW SRM AND DWG.
LT MAIN WHEEL WELL VERTICAL PRESURE DECK WEB CRACKED. REPAIRED PER SRM.
AFT CARGO AFT CORNER SCUFF PLATE BROKEN. 8-22 (OFF AIRCRAFT) / AFT CARGO AFT CORNER SCUFF PLATE WELD REPAIRED ACCOMPLISHED ON EA NO: 1-A53-2076 REV 11 REF W/O 2015067 ; 1000 ; 0048
UPPER FORWARD EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT BATTERY PER AMM.
R1 DOOR SLIDE GIRT BAR HUNG UP ON DOOR FRAME, SLIDE INADVERTENTLY PULLED PARTIALLY FROM COVER, DID NOT DEPLOY, STILL OPERATIONAL. R&R SLIDE ASSEMBLY PER MT.
L1 DOOR SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.
SUPPLEMENTAL INFORMATION: FUSELAGE SKIN DISBONDED FROM EGPR STIFFNER AT LOWER RUBBING BLOCK AREA WITH ASSOCIATED SKIN DAMAGE AT ELECTRICAL GROUND POWER RECEPTICLE SURROUND CUTOUT / ACCOMPLISHED PERMANENT REPAIR PER EA #1-753-34233 REF IR
SUPPLEMENTAL INFORMATION: FUSELAGE SKIN DISBONDED AT DAMAGED AREA FROM EGPR STIFFNER AFT SIDE OF ELECTRICAL GROUND POWER RECEPTICLE SURROUND CUTOUT / ACCOMPLISHED PERMANENT REPAIR PER EA #1-753-34233 REV IR
SUPPLEMENTAL INFORMATION: FUSELAGE SKIN AND EGPR STIFFINER BENT OUTWARD AT AFT SIDE OF GROUND POWER RECERTICLE CUTOUT WITH ASSOCIATED DISBONDED SKIN AND PULLED AWAY FROM FASTENERS. AT BS 235.80 AND WL 180. / ACCOMPLISHED PERMANENT REPAIR PER EA #1-753-34233 REV IR
R2 DOOR LOWER EXIT SIGN MISSING. R&R LIGHT ASSEMBLY PER AMM.
RAMP REPORTS CRACK IN BIN D FLOOR / REMOVED FABRICATED REPLACEMENT PANEL; AND INSTALLED NEW PANEL PER M/M 25-52-10. CL # 19522
RT OVERWING EXTERNAL EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.
EMERGENCY LIGHT BATTERY M1670 FAILED TEST. R&R BATTERY PER MM.
PASSENGER CABIN FLOORBOARD INTERCOSTAL STA 328 - STA 344 BL-46'L IS CRACKED 1.75' LONG IN E&E / REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02 AND SRM 51-10-02
PASSENGER CABIN FLOORBOARD INTERCOSTAL STA 344 - STA 360 BL-0 IS CRACKED 1.75' LONG IN E&E / REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02 AND SRM 51-10-02
EMERGENCY LIGHT BATTERY M1672 FAILED TEST. R&R BATTERY PER MM.
FORWARD GALLEY EMERGENCY EXIT LIGHT HOUSING BROKEN. R&R SIGN ASSEMBLY PER MM.
L1 DOOR EVAC SLIDE GIRT BAR HOLDER OUT OF ADJUST. / ADJUSTED GIRT BAR HOLDER PER MM.
R/H AFT ESCAPE PATH LIGHT STRIP BY G3 GALLEY DELAMINATED. / R&R STRIP PER DWG.
R/H OVERWING EXIT SIDEWALL LIGHT DIM. / RELAMPED LIGHT PER AMM.
L1 DOOR EMERGENCY LIGHT INOPERATIVE. R & R POWER SUPPLY FUSE IAW AMM.
AFT CARGO BAY ZEE ANGLE CORRODED BETWEEN BS 727D TO 767, STRINGER 26R. R & R THE ANGLE IAW SRM.
AFT CARGO COMPARTMENT;5' AFT OF STA 767; FLOOR STRAP HAS AREAS OF CORROSION NEAR DOOR SIDE. / REMOVED CORROSION FOUND TO BE 100% MATERIAL LOSS. REMOVED & REPLACED FLOOR STRAP @ APPROX STA 772 IAW SRM 51-40-02-0G-0. ATAG WN2909
RT WING TRAILING EDGE PANEL AFT OF PYLON VERTICAL BULB ATTACH ANGLE CRACKED. R&R ANGLE IAW DWG.
RIGHT WING AT WING ROOT UPPER PANEL INBOARD ATTACH BRACKET CRACKED AT FORWARD ATTACH POINT. R & R THE ATTACH BRACKET IAW SRM AND DWG.
LEFT WING, ABOVE AND INBOARD OF THE NR 1 AFT FUEL BOOST PUMP BRACKET, ATTACHED TO UPPER REAR SPAR CRACKED. R & R THE BRACKET IAW SRM AND DWG.
MAIN WHEEL WELL BULKHEAD WEB CRACKED AT BS 663, RBL 35. REPAIRED THE BULHEAD WEB IAW EA.
PASSENGER CABIN FLOOR STRUCTURE STA 540 PANEL BREAK LBL 24-BL 0 IS CRACKED ON INBOARD END / REMOVED AND REPLACED FLOOR PANEL SPLICE IAW B737 DRAWING 143A0060 REV A LOCATED AND DRILLED SPLICE IAW B737 SRM 51-40-05-0G-0
EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01670. R & R THE BATTERY PACK IAW AMM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01674. R & R THE BATTERY PACK IAW AMM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01673. R & R THE BATTERY PACK IAW AMM.
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01669. R & R THE BATTERY PACK IAW AMM.
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01672. R & R THE BATTERY PACK IAW AMM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01675. R & R THE BATTERY PACK IAW AMM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01668. R & R THE BATTERY PACK IAW AMM.
R2 DOOR SLIDE GRIT BAR ANGLE LOOSE. SECURED THE GIRT BAR HANGER IAW SIP.
VENT OUTLET AFT OF AFT PRESSURE BULKHEAD ON BOTTOM OF PLANE SHEARED AT BS 1016, STRINGER 26R. REPAIRED THE DRAIN TUBE ASSEMBLY IAW EA.
RIGHT AFT EMERGENCY LIGHT BATTERY FAILED TIME TEST. R & R THE BATTERY PACK IAW AMM.
LEFT OVERWING EXIT LIGHT LENS BROKEN. R & R LENS IAW MM.
R2 DOOR EMERGENCY EXIT SIGN COVER MISSING. R&R LIGHT ASSEMBLY PER AMM.
CENTER WING SPAR VAPOR WEB CRACKED AT BS 663, BETWEEN RBL 31 - 38. REPAIRED WEB IAW EA.
AIR TURN BACK, RT LG GREEN LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE UP. RT LG RED DISAGREEMENT LIGHT WAS ILLUMINATED. R & R SENSOR S0073 IAW AMM.
L1 DOOR MOUNT PLATE FOR FWD GIRT BAR FITTING GOUGED. R & R MOUNT PLATE IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 312 TO 328, LBL 45. R & R INTERCOSTAL IAW SRM.
AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS 827 TO 847, RBL 19. R & R SUPPORT IAW SRM.
AFT CARGO AROUND NUTPLATE HOLE CORRODED AT BS 798, RBL 14. REPAIRED NUTPLATE IAW EA.
AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS 794 TO 807, RBL 19. R & R SUPPORT IAW SRM.
AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS 807 TO 827, RBL 19. R & R SUPPORT IAW SRM.
AFT CARGO DOOR THRESHOLD WEB CORRODED. R & R WEB IAW SRM.
LEFT WINGLET LE FRONT SPAR DELAMINATED AT STATION 4 AT UPPER & LOWER RADIUS. R & R LT WINGLET IAW MM.
RIGHT OVERWING EMER EXIT SIGN MISSING. INSTALLED SIGN IAW AMM.
L2 WINDOW UPPER EDGE CRACKED. R & R WINDOW IAW MM.
R2 DOOR AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. RE LAMPED LIGHT IAW MM.
FWD EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY IAW AMM.
AFT EMERGENCY EXIT LIGHT BATTERY PACK FAIL CAPACITY TEST. R & R BATTERY IAW AMM.
R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER, R & R LIGHT ASSEMBLY IAW MM.
LT HORIZONTAL STABILIZER RIB CRACKED AT STABILIZER STATION 147.9. REPAIRED RIB IAW EA.
"Z" ANGLE CORRODED BETWEEN STATION 500 - STATION 500D, LBL 24. REPAIRED Z-ANGLE IAW SRM.
SEAT TRACK FLANGE FORWARD FASTENER HOLE CRACKED AT STATION 727B, LBL 24.75. REPAIRED FLANGE IAW EA.
SEAT TRACK FLANGE FORWARD FASTENER HOLE CRACKED AT STATION 727B, LBL 45.5. REPAIRED FLANGE IAW EA.
AFT CARGO COMPARTMENT AFT FLOOR PANEL 140CF CORRODED AROUND ENTIRE TOP SURFACE TAPED EDGES. REPAIRED PANEL IAW SRM & SWA EA.
SEAT TRACK FLANGE FORWARD FASTENER HOLE CRACKED AT STATION 727B, LBL 45.5. REPAIRED FLANGE IAW EA.
SEAT TRACK FLANGE CRACKED AT STATION 727B, LBL 24.75. REPAIRED FLANGE IAW EA.
SEAT TRACK FLANGE CRACKED AT STATION 727B, LBL 45.5. REPAIRED FLANGE IAW EA.
LT WING INBD FIXED TE UPPER PANEL LOWER MIDDLE BRACKET CRACKED. R&R BRACKET IAW SRM & DRAWING.
RT Z ANGLE UPPER SURFACE CORRODED BETWEEN BS 727E+10 - BS 767. REPAIRED Z ANGLE IAW SRM.
LT FLOOR SUPPORT Z ANGLE UPPER SURFACE CORRODED BETWEEN BS 807 - BS 747. R&R "Z" ANGLE IAW SRM.
FWD LAVATORY EMERGENCY EXIT LIGHTS BROKEN. R&R LIGHTS IAW AMM.
G1 GALLEY EMERGENCY EXIT LIGHTS BROKEN. R&R LIGHTS IAW AMM.
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MT AND AMM.
FUSELAGE EXTERNAL POWER RECEPTACLE DOOR CUTOUT INTERNAL DOUBLER SKIN CRACKED ON AFT EDGE RUB BLOCK AREA. REPAIRED DOUBLER IAW EA.
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINING COLLAR BROKEN. R & R COLLAR ASSY IAW AMM.
L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINING COLLAR BROKEN. R & R COLLAR ASSY IAW AMM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MM AND MT.
L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MT AND MM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW AMM AND MT.
EMERGENCY EXIT LIGHT CENTER CEILING BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW AMM.
RIGHT AFT GALLEY EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW M/M.
AFT GALLEY SERVICE DOOR EMERGENCY EXIT SIGN FELL OFF. RE-INSTALLED SIGN PER M/M.
R2 DOOR EMERGENCY EXIT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER M/M.
AFT RT EMERGENCY EXIT DOOR SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER AMM.
LT HORIZONTAL STAB LOWER IN-SPAR SKIN CRACKED AT STA 129.5. REPAIRED SKIN IAW SRM.
RT HORIZONTAL STAB LOWER IN-SPAR SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM.
EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER AMM.
LT EEPLS LENS BROKEN BETWEEN ROW 1 TO ROW 10. REMOVED AND REPLACED LENS PER AMM.
L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 3. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS LENS BROKEN AT ROW 11. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.
EEPLS LENS MISSING. INSTALLED LENS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP BETWEEN ROW 11 TO ROW 17. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC CHECK, LT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED HC CHECK, RT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.
R2 DOOR EMERGENCY EXIT SIGN LENS MISSING. REMOVED AND REPLACED SIGN ASSY PER MM.
DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT LIGHT ON AFT LAV BY L2 DOOR INOP. CONNECTED LIGHT PER MM.
R1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED LENS PER MM.
L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINTER, DID NOT DEPLOY. REINSTALLED SLIDE PER MT.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.
DURING SCHEDULED RON CHECK, FOUND EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND FWD EEPS END CAP MISSING. INSTALLED ENCAP PER MM.
FOUND FWD ENTRY FLOOR LEVEL EMERGENCY EXT SIGN LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 5 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.
EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.
EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.