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. (SWAA) | Operator | on 2025-02-13 | Operator named in NTSB report |
Accident & incident history
Operated by SOUTHWEST AIRLINES CO (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
200 reports on file, 2009-10-14 – 2026-08-06.
Part: GIRT BAR — UNPACKED (ZONE 800) · airframe 55,471 hrs · 33,890 cycles
FA REPORTS L1 GIRT BAR HARD TO RELEASE. REPACKED EXCESS GIRT MATERIAL AT BOTTOM OF SLIDE AMM 25-66-01. OP CHECK GOOD
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 55,316 hrs · 33,787 cycles
FWD ENTRY NR 1 EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD ENTRY NR 1 EMERGENCY FLASHLIGHT REF AMM 25-64-00.
Part: SEAT — OUT OF ADJUST (ZONE 200) · airframe 54,985 hrs · 33,569 cycles
PASSENGER CABIN SEAT 14B, WHICH IS IN AN EMERGENCY EXIT ROW, RECLINES AND SHOULDN`T. LOCKED OUT SEAT 14B RECLINE IAW CMM 25-21-45.
Part: CONTACT — DIRTY (MEGAPHONE) · airframe 53,916 hrs · 32,838 cycles
AFT FA MEGAPHONE INOPERATIVE. CLEANED BATTERY CONTACTS AND ACCOMPLISHED MEGAPHONE OPS CHECK IAW AMM 25-64-00, CHECKED NORMAL.
Part: SEAT — OUT OF ADJUST (ZONE 200) · airframe 53,803 hrs · 32,756 cycles
PASSENGER CABIN EMERGENCY EXIT ROW SEAT 14B RECLINES. LOCKED OUT 14B SEAT RECLINE IAW CMM 25-21-42
Earlier reports · 2009–2025 · 195 reports
2025
Part: FITTING — CRACKED (ZONE 300) · airframe 53,395 hrs · 32,488 cycles
RIB FITTING IS CRACKED AT STAB BL 281.81 RH SIDE. PERFOMED REPAIR IAW SRM 55-10-90-2R-1-A01330, REPAIR 1.
Part: SEAL — CRACKED (ZONE 300) · airframe 52,835 hrs · 32,124 cycles
RH HORIZONTAL STAB UPPER FWD SLIDER SEAL CRACKED. REMOVED AND REPLACED SEAL PER AMM 53-31-31.;[02] C/W INSPECTION
Part: SEAL — CRACKED (ZONE 300) · airframe 52,835 hrs · 32,124 cycles
LH HORIZONTAL STAB UPPER FWD SLIDER SEAL IS CRACKED. REMOVED AND REPLACED SEAL PER AMM 53-31-31.
Part: WEB — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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
Part: ANGLE — DAMAGED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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
Part: LENS — MISINSTALLED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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
Part: LENS — WRONG PART (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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
Part: SUPPORT — CORRODED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
CORROSION SUPPORT ZEE LOCATED BETWEEN BS727C TO BS807 LBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203784<
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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
Part: RIB — CRACKED (ZONE 300) · airframe 51,518 hrs · 31,311 cycles
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
Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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
Part: TRACK — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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.
Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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
Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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
Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
CORROSION ANGLE FLOOR STRUCTURE LOCATED STA947.5 AND RBL4 WL156 AT AFT CARGO COMPARTMENT 2025-203796<
Part: SUPPORT — CORRODED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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
Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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
Part: ANGLE — CRACKED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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.
Part: SHIELD — CORRODED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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
Part: SUPPORT — CORRODED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
CORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT 2025-203782<
Part: SHIELD — CORRODED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
CORROSION SHIELD WEB LOCATED BETWEEN BS767 TO BS794.3 RBL21 AND WL156 AT AFT CARGO COMPARTMENT 2025-203783<
Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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.
Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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
Part: FLOORBEAM — CRACKED (ZONE 2000) · airframe 51,518 hrs · 31,311 cycles
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.
Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2025-203695<
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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.
Part: ANGLE — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
CRACK ANGLE - CLIP LOCATED STA440 AND STR26L FWD CARGO COMPARTMENT 2025-203694<
Part: STRINGER — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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
Part: SHIELD — DAMAGED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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 -.
Part: ANGLE — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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.
Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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.
Part: STRINGER — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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
Part: STUB FRAME — CRACKED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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.
Part: STUB FRAME — CRACKED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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.
Part: PANEL — CRACKED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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
Part: SUPPORT — CRACKED (ZONE 300) · airframe 51,518 hrs · 31,311 cycles
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
Part: PANEL — CRACKED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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.
Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 51,518 hrs · 31,311 cycles
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
Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 51,518 hrs · 31,311 cycles
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
Part: ACCESS PANEL — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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.
Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 51,518 hrs · 31,311 cycles
CRACK ACCESS PANEL 334GB AT AT LT HORIZONTAL STABILIZER 2025-203633<
Part: ACCESS PANEL — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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.
Part: SCUFF PLATE — CRACKED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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.
Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 51,518 hrs · 31,311 cycles
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.
Part: SKIN — CRACKED (ZONE 500 SLAT) · airframe 51,518 hrs · 31,311 cycles
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
Part: LIGHT — DETERIORATED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
DETERIORATED PHOTOLUMINISCENT STRIP LIGHTING AT PAX CABIN (10EA) 2025-203584<
Part: LIGHT — DETERIORATED (ZONE 200) · airframe 51,518 hrs · 31,311 cycles
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
Part: SKIN — CRACKED (ZONE 500 SLAT) · airframe 51,518 hrs · 31,311 cycles
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
2024
Part: SKIN — DELAMINATED (ZONE 500 FLAP) · airframe 50,529 hrs · 30,720 cycles
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.
Part: THRESHOLD — CRACKED (ZONE 100) · airframe 49,642 hrs · 30,155 cycles
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.
Part: FIRE LOOP — DISCONNECTED (ZN 200 FUS TOP) · airframe 49,605 hrs · 30,128 cycles
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
Part: HANDLE — LOOSE (AFT SERVICE DOOR) · airframe 48,543 hrs · 29,450 cycles
AFT SERVICE DOOR HANDLE LOOSE<[01] TIGHTENED AFT SERVICE DOOR HANDLE IAW AMM 52-41-31
2023
Part: SLIDE — LOOSE (ZN 800 DOOR) · airframe 46,986 hrs · 28,478 cycles
L1 SLIDE PACK NEEDS TO BE RESECURED.<[01] RE-POSITIONED L1 DOOR SLIDE; CK?S GOOD; REF MT 725-61-06.
Part: SLIDE — LOW (ZN 800 DOOR) · airframe 46,613 hrs · 28,236 cycles
FWD ENTRY DOOR EVAC SLIDE PRESS LOW.<[01] R&R FWD ENTRY DOOR SLIDE PER MT 725-61-06-FE.
Part: ENGINE — FAILED (NR 1) · airframe 66,343 hrs · 39,114 cycles
#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.<
Part: GIRT BAR — OUT OF POSITION (ZN 800 DOOR) · airframe 45,563 hrs · 27,572 cycles
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
Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 45,563 hrs · 27,572 cycles
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
Part: BARRIER — DELAMINATED (ZN 100 FUS LOWER) · airframe 45,563 hrs · 27,572 cycles
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.
Part: PANEL — DAMAGED (ZN 500 LEFT WING) · airframe 45,563 hrs · 27,572 cycles
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
Part: PANEL — DAMAGED (ZN 100 FUS LOWER) · airframe 45,563 hrs · 27,572 cycles
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.
Part: PANEL — ELONGATED (ZN 100 FUS LOWER) · airframe 45,563 hrs · 27,572 cycles
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.
Part: PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 45,563 hrs · 27,572 cycles
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.
Part: PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 45,563 hrs · 27,572 cycles
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.
Part: PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 45,563 hrs · 27,572 cycles
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.
Part: PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 45,563 hrs · 27,572 cycles
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.
Part: PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 45,563 hrs · 27,572 cycles
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.
2022
Part: SUPPORT BRACKET — CRACKED (LT A/C BAY) · airframe 44,592 hrs · 26,929 cycles
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.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 44,592 hrs · 26,929 cycles
EMERGENCY BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED FIVE BATTERY PACKS AT M01668, M01669, M01670, M01672, AND M01673 IAW AMM 33-51-06.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,350 hrs · 26,761 cycles
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.
Part: NONE — DELAMINATED (FWD CARGO) · airframe 43,731 hrs · 26,339 cycles
FLOOR DEGRADED IN FWD CARGO BIN / [01] REPAIRED FLOOR PER AMM 25-52-01
Part: TAILPIPE — FAULTY (#2 ENGINE) · airframe 43,169 hrs · 25,967 cycles
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
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 42,799 hrs · 25,720 cycles
-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.
Part: MEGAPHONE — BROKEN · airframe 41,861 hrs · 25,133 cycles
AFT MEGAPHONE BROKEN ; / [01] R&R?D AFT MEGAPHONE & OPS NML IAW AMM 25-64-00
2021
Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 39,769 hrs · 23,903 cycles
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
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 39,769 hrs · 23,903 cycles
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)
Part: FLOORBEAM — CORRODED (BS 986 R/RBL 44) · airframe 39,769 hrs · 23,903 cycles
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
Part: ANGLE — CORRODED (BS 344 LBL 64) · airframe 39,769 hrs · 23,903 cycles
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.-
Part: WEB — CRACKED (BS 277-294 BL0) · airframe 39,769 hrs · 23,903 cycles
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
Part: SUPPORT ANGLE — CRACKED (BS 380-400 BL 0) · airframe 39,769 hrs · 23,903 cycles
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
Part: STRINGER — CRACKED (BS 500B-520 S19R) · airframe 39,769 hrs · 23,903 cycles
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-
Part: SUPPORT BRACKET — CRACKED (BS 540 BL0-LBL24) · airframe 39,769 hrs · 23,903 cycles
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
Part: ANGLE — CORRODED (BS 294-332 RBL64) · airframe 39,769 hrs · 23,903 cycles
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
Part: STRINGER CLIP — CRACKED (BS 277 S10R) · airframe 39,769 hrs · 23,903 cycles
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.
Part: INTERCOSTAL — CRACKED (BS 294-303) · airframe 39,769 hrs · 23,903 cycles
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
Part: STRUCTURE — CRACKED (BS 303 S17L) · airframe 39,769 hrs · 23,903 cycles
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 - .
Part: INTERCOSTAL — CORRODED (BS 767-787 S25R) · airframe 39,769 hrs · 23,903 cycles
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:
Part: CARGO TRACK — CRACKED (BS 747-767) · airframe 39,769 hrs · 23,903 cycles
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.
Part: SUPPORT — CORRODED (BS 727-847 S25L) · airframe 39,769 hrs · 23,903 cycles
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
Part: ANGLE — CRACKED (BS 867-S26L) · airframe 39,769 hrs · 23,903 cycles
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
Part: INTERCOSTAL — CORRODED (BS 494-500A S26R) · airframe 39,769 hrs · 23,903 cycles
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
Part: SUPPORT — CORRODED (BS 727-767 S25R) · airframe 39,769 hrs · 23,903 cycles
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
Part: INTERCOSTAL — CRACKED (BS 847-867) · airframe 39,769 hrs · 23,903 cycles
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
Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 39,769 hrs · 23,903 cycles
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).
Part: GUSSET — CRACKED (BS 500D S19L) · airframe 39,769 hrs · 23,903 cycles
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.
Part: GUSSET — CRACKED (BS 500D S19D) · airframe 39,769 hrs · 23,903 cycles
CRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT.
Part: BRACKET — CRACKED (BS 545 LBL 6) · airframe 39,769 hrs · 23,903 cycles
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
Part: ANGLE — CRACKED (BS 400 S26L) · airframe 39,769 hrs · 23,903 cycles
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.-
Part: ANGLE — CRACKED (BS 500C S26L) · airframe 39,769 hrs · 23,903 cycles
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.-
Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 39,769 hrs · 23,903 cycles
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.
Part: PLATE — CRACKED (HORIZONTAL STAB) · airframe 39,769 hrs · 23,903 cycles
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
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 39,769 hrs · 23,903 cycles
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.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 39,769 hrs · 23,903 cycles
BROKEN LOWERED CEILING PANEL EMERGENCY EXIT LIGHT AND LENS ASSY AT AFT GALLEY AREA /
Part: LIGHT — BROKEN (CABIN) · airframe 39,769 hrs · 23,903 cycles
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
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 39,769 hrs · 23,903 cycles
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
Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 39,769 hrs · 23,903 cycles
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
Part: SLIDE — LOW PRESSURE (FWD SERVICE DOOR) · airframe 39,693 hrs · 23,858 cycles
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
2020
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,734 hrs · 23,261 cycles
LEFT SIDE EMERGENCY EXIT OVERHEAD LIGHT INOPERABLE. CLOSING DMA PAGE: 0412223. RELAMPED SIDEWALL LIGHT AT SEAT 11A, IAW AMM 33-51-01 CL 57515.
Part: ATTACH FITTING — CRACKED (LT HORIZ STAB) · airframe 37,705 hrs · 22,596 cycles
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.
Part: STIFFENER — CRACKED (L/H HORIZ. STAB.) · airframe 37,705 hrs · 22,596 cycles
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.
Part: STIFFENER — CRACKED (L/H HORIZ. STAB.) · airframe 37,705 hrs · 22,596 cycles
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.
Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 37,705 hrs · 22,596 cycles
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
Part: ANGLE — CRACKED (FUSELAGE) · airframe 37,705 hrs · 22,596 cycles
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
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 37,705 hrs · 22,596 cycles
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
Part: SUPPORT FITTING — CRACKED (BS 663) · airframe 37,705 hrs · 22,596 cycles
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
Part: SKIN — CRACKED (HORIZONAL STAB) · airframe 37,705 hrs · 22,596 cycles
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
Part: SUPPORT FITTING — CRACKED (BS 662) · airframe 37,705 hrs · 22,596 cycles
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
Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 37,702 hrs · 22,595 cycles
LEFT HORIZONTAL FWD UPPER SLIDING SEAL IS CRACKED / REMOVED AND REPLACED LEFT HORIZONTAL FWD UPPER SLIDING SEAL PER AMM 53-31-31
Part: SUPPORT BRACKET — CRACKED (KEEL BEAM) · airframe 37,702 hrs · 22,595 cycles
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.
Part: SKIN — CORRODED (LT HORIZ STAB) · airframe 37,702 hrs · 22,595 cycles
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
Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 37,702 hrs · 22,595 cycles
RIGHT HORIZONTAL STABILIZER UPPER SLIDING SEAL IS CRACKED / REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER UPPER SLIDING SEAL PER AMM 53-31-31.
2019
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,747 hrs · 21,364 cycles
LEFT FWD EMERGENCY LIGHTS FAILED. R&R BATTERY PACK PER AMM.
Part: HOUSING — LOOSE (EXIT SIGN) · airframe 35,655 hrs · 21,303 cycles
OVERHEAD OVERWING EMERGENCY EXIT SIGN LOOSE FROM THE CEILING. R&R SIGN HOUSING SIP.
Part: FAN — FAULTY (CABIN) · airframe 35,102 hrs · 20,931 cycles
ELECTRICAL SMELL IN THE CABIN. R&R RECIRC FAN AMM.
Part: FRAME — CRACKED (LEFT WING) · airframe 34,762 hrs · 20,712 cycles
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
Part: WEB — CRACKED (WHEEL WELL LH) · airframe 34,762 hrs · 20,712 cycles
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
Part: CHANNEL — CRACKED (CABIN) · airframe 34,762 hrs · 20,712 cycles
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
Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 34,762 hrs · 20,712 cycles
L1 DOOR SLIDE GIRT BAR OFF OF THE SLIDE SHELF. (OUT OF POSITION) / REPOSITIONED GIRT BAR IAW AMM.
Part: PLATE — CRACKED (LT WING) · airframe 34,762 hrs · 20,712 cycles
LT WING TRAILING EDGE CAVITY ABOUT 10" OUTBOARD OF LOWER ACCESS PANEL DOOR 551DB WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM & DWG.
Part: PLATE — CRACKED (RT WING) · airframe 34,762 hrs · 20,712 cycles
RT WING WIGGLE PLATE CRACKED AT OUTBOARD RIVET JUST INBOARD OF #6 FLAP TRACK. R&R WIGGLE PLATE IAW SRM & DWG.
Part: BEAM — CRACKED (R1 DOOR) · airframe 34,762 hrs · 20,712 cycles
R1 DOOR #4 BEAM WHERE HANDLE BOX HOUSING ATTACHES WAS CRACKED. / R&R #4 BEAM IAW SRM & DWG.
Part: BEAM — CRACKED (FSD) · airframe 34,762 hrs · 20,712 cycles
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
Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 34,015 hrs · 20,229 cycles
CENTER WING REAR SPAR VAPOR WEB CRACKED BETWEEN LBL 31.83 TO LBL 40.00. / REPAIRED WEB PER SRM.
Part: COVER — LOOSE (EXIT SIGN) · airframe 33,827 hrs · 20,105 cycles
CEILING MOUNTED "EXIT" SIGN AT EMERGENCY EXIT ROW LOOSE. SECURED COVER PER MM.
Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 33,767 hrs · 20,064 cycles
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LOWER INBOARD LUG FACE CORRODED. REPAIRED FITTING PER EA.
Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 33,767 hrs · 20,064 cycles
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER OUTBOARD LUG FACE CORRODED. REPAIRED FITTING PER EA.
Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 33,767 hrs · 20,064 cycles
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING UPPER INBOARD LUG FACE CORRODED. REPAIRED FITTING PER EA.
2018
Part: STRAP — BROKEN (FLASHLIGHT) · airframe 31,673 hrs · 18,685 cycles
FORWARD GALLEY FLASHLIGHT SECURITY STRAP BROKEN. INSTALLED STRAP IAW AMM.
Part: HANGER ASSY — OUT OF ADJUST (L1 DOOR) · airframe 31,435 hrs · 18,530 cycles
L1 DOOR EMERGENCY EVAC SLIDE HANGER OUT OF ADJUST. ADJUSTED HANGER PER SIP.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,344 hrs · 18,467 cycles
LEFT BULLNOSE EMERGENCY LIGHT INOPERATIVE AT ROW 20. REPLACED THE LAMPS IAW AMM.
Part: STIFFENER — CRACKED (LT WHEEL WELL) · airframe 31,344 hrs · 18,467 cycles
WHEEL WELL STA. 663 LBL 26 STIFFENER CRACKED. / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02
2017
Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 29,344 hrs · 17,187 cycles
LH HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL IS CRACKED / R&R LH HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL PER AMM 53-31-31.
Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 29,344 hrs · 17,187 cycles
RH HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL IS CRACKED / R&R RH HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL PER AMM 53-31-31.
Part: WIRE — MISROUTED (R1 DOOR SLIDE) · airframe 28,202 hrs · 16,469 cycles
R1 DOOR SLIDE COMPARTMENT WIRE MISROUTED. REROUTED THE SLIDE WIRE IAW AMM.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,946 hrs · 16,324 cycles
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
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,946 hrs · 16,324 cycles
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
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,946 hrs · 16,324 cycles
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
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,945 hrs · 16,324 cycles
CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL PER SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,945 hrs · 16,324 cycles
CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL PER SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,945 hrs · 16,324 cycles
CABIN FLOOR INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, BL 0. R&R INTERCOSTAL PER SRM.
Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 27,945 hrs · 16,324 cycles
RT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 43.5. REPAIRED WEB PER SRM.
Part: SLIDE — DISLODGED (R2 DOOR) · airframe 27,537 hrs · 16,068 cycles
R2 DOOR SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED THE SLIDE IAW MT.
Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 27,360 hrs · 15,952 cycles
LEFT MLG WW REAR SPAR VAPOR BARRIER WEB CRACKED BETWEEN LBL 45 TO 55. REPAIRED THE WEB IAW SRM.
Part: FLAP — SEPARATED (LT WING) · airframe 27,945 hrs · 16,324 cycles
LT WING OUTBOARD AFT FLAP TRAILING EDGE SEPARATED, 14" OUTBOARD OF THE INBOARD MOST EDGE. REPAIRED AFT FLAP PER SRM.
Part: SIGN — LOOSE (ROW 11ABC) · airframe 27,356 hrs · 15,950 cycles
EMERGENCY EXIT SIGN LOOSE AT ROW 11 ABC. SECURED THE SIGN IAW MM.
2016
Part: LENS — CRACKED (CABIN) · airframe 26,284 hrs · 15,316 cycles
LT OVERWING EXIT LIGHT LENS CRACKED. R&R LENS IAW AMM.
Part: COVER — LOOSE (L2 DOOR) · airframe 25,510 hrs · 14,855 cycles
L2 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER IAW SIP.
2015
Part: BATTERY PACK — FAILED (CABIN) · airframe 22,856 hrs · 13,286 cycles
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1672. R & R BATTERY PACK IAW DWG & AMM.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 22,856 hrs · 13,286 cycles
EMERGENCY LIGHT POWER SUPPLY M01673 INOPERATIVE. R & R POWER SUPPLY IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 22,856 hrs · 13,286 cycles
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1673. R & R BATTERY PACK IAW DWG & AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 22,856 hrs · 13,286 cycles
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1669. R & R BATTERY PACK IAW DWG & AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 22,856 hrs · 13,286 cycles
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1675. R & R BATTERY PACK IAW DWG & AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 22,856 hrs · 13,286 cycles
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1670. R & R BATTERY PACK IAW DWG & AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 22,856 hrs · 13,286 cycles
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1668. R & R BATTERY PACK IAW DWG & AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 22,856 hrs · 13,286 cycles
EMERGENCY LIGHT BATTERY PACK FAIL CAPACITY TEST AT M1674. R & R BATTERY PACK IAW DWG & AMM.
Part: COVER — CRACKED (CABIN) · airframe 21,284 hrs · 12,361 cycles
FORWARD GALLEY EXIT SIGN LENS COVER ON HEADER PANEL CRACKED. R & R COVER IAW AMM.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 21,284 hrs · 12,361 cycles
AFT CARGO DOOR THRESHOLD WEB CORRODED. REPAIRED WEB IAW SRM.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 21,284 hrs · 12,361 cycles
CABIN SEAT TRACK CRACKED AT STATION 727B, LBL 45.5. REPAIRED TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 21,284 hrs · 12,361 cycles
CABIN SEAT TRACK CRACKED AT STATION 727B, RBL 45.5. REPAIRED TRACK IAW EA.
Part: SIGN — LOOSE (CABIN) · airframe 21,257 hrs · 12,343 cycles
RIGHT OVERWING EXIT SIGN LOOSE. R & R EXIT SIGN IAW MM.
Part: COVER — MISSING (EXIT SIGN) · airframe 21,184 hrs · 12,303 cycles
RIGHT OVERWING EXIT SIGN COVER MISSING. INSTALLED COVER IAW SIP.
Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 20,781 hrs · 12,066 cycles
R1 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.
2013
Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 14,881 hrs · 8,613 cycles
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.
Part: BATTERY — DISCHARGED (CABIN) · airframe 14,025 hrs · 8,128 cycles
FORWARD CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY IAW MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 14,025 hrs · 8,128 cycles
AFT CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY IAW MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 14,025 hrs · 8,128 cycles
MID CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY IAW MM.
Part: LENS — DETACHED (CABIN) · airframe 12,889 hrs · 7,484 cycles
EXIT LENS FELL OFF AT RIGHT OVERWING EXT. RE-INSTALLED EMERGENCY EXIT LIGHT LENS AT RIGHT EMERGENCY EXIT ROW PER AMM.
2012
Part: LIGHT — CRACKED (CABIN) · airframe 11,136 hrs · 6,486 cycles
LEFT EEPLS CRACKED AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.
Part: LIGHT — BROKEN (CABIN) · airframe 11,136 hrs · 6,486 cycles
FORWARD EEPLS BROKEN. REMOVED AND REPLACED EEPLS PER MM.
Part: LENS — BROKEN (CABIN) · airframe 11,136 hrs · 6,486 cycles
FORWARD EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,538 hrs · 6,140 cycles
LEFT EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS PER AMM.
Part: LENS — BROKEN (CABIN) · airframe 10,538 hrs · 6,140 cycles
LEFT EEPLS LENS BROKEN AT ROW 5. REMOVED AND REPLACED LENS PER AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 93,307 hrs · 5,444 cycles
DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 9,307 hrs · 5,444 cycles
DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.
2011
Part: COVER — BROKEN (CABIN) · airframe 6,411 hrs · 3,785 cycles
LT EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.
2010
Part: SIGN — BROKEN (CABIN) · airframe 4,589 hrs · 2,718 cycles
R1 DOOR EMERGENCY EXIT SIGN ASSY BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,513 hrs · 2,668 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 4,178 hrs · 2,460 cycles
DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: COVER — DAMAGED (CABIN) · airframe 3,455 hrs · 2,041 cycles
DURING SCHEDULED CV CHECK, FOUND EEPLS COVER DAMAGED AT ROW 11. REMOVED AND REPLACED COVER PER MM.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 1,193 hrs · 691 cycles
DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.