N765SW
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 | 2017-06-03 – 2017-06-03 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2017-06-03 – 2017-06-03 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
EMERGENCY LIGHT BATTERY PACK AT LOCATION M1674 FAILED CAPACITY TEST<[01] R/R M1674 EMERGENCY BATTER PACK PER AMM 33-51-06;[02] ADD PART REMOVAL TO S/O
PANEL 193D CRACKED . CRACK MEASURED 3 IN LENGTH.<[01] REMOVED AND REPLACED FAIRING PANEL 193D PER AMM. 53-51-21.
L/H AFT LOWER FUSELAGE EMER LIGHT INOP<[01] R&R L/H AFT LOWER FUSELAGE EMER LIGHT BULB PER AMM 33-51-04.OPS CHECK GOOD
INOPERTIVE BULLNOSE EMERGENCY LIGHT 18DEF. RELAMPED PER AMM 33-51-03
FWD GALLEY FLASHLIGHT INOP / [01] REMOVED AND REPLACED FLUSH LIGHT IAW AMM 25-64-00;[02] REMOVED AND REPLACED FLASH LIGHT IAW AMM 25-64-00;[03] REMOVED AN REPLACED FLIS=H LIGHT IAW AMM 25-64-00
MULTIPLE EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED FWD RH (M1674) BATTERY AND BATTERY CHARGER PACK ASSEMBLY IN REFERENCE TO AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.
FWD SERVICE SIDE EMERGENCY EXIT LENSE FELL OFF / [01] OK TO CONT PER MEL 25-10-01 SP1B<BR>AUTH#86171;[02] RE-SECURED FWD SERVICE DOOR EMERGENCY EXIT LENSE PER SIP
PANEL 193 B HAS WORN/DELAMINATED AREAS AT FASTENER HOLE LOCATIONS 6; 8; 10; 11; 13; 14; 17; 22; 33; AND 34. PANEL 193 B HAS WORN/DELAMINATED AREAS AT FASTENER HOLE LOCATIONS 6 8 10 11 13 14 17 22 33 AND 34. / [01] R/R 193B PANEL IAW AMM 53-51-21.
DURING FLIGHT AT 29K FEET WE LOST HYDRAULIC SYS B FLUID WENT TO ZERO AND TOTAL LOSS OF PRESSURE / [01] REF TTG8Q00DVGLL ALT BRAKE SELECTOR VALVE LEAKING. MT 729-PPRD-01-01 HYDRO SYSTEM FLUSH / FILTER R/R B SYSTEM. NO METAL OR DEBRIS NOTED. TTG8Q00DVGR3 ' B ' EMDP R/R; TTG8Q00VGR5 #2 EDP R/R; SYSTEM RESTORED NO LEAKS NOTED.
DURING FLIGHT AT 29K FEET WE LOST HYDRAULIC SYS B FLUID WENT TO ZERO AND TOTAL LOSS OF PRESSURE / [01] REF TTG8Q00DVGLL ALT BRAKE SELECTOR VALVE LEAKING. MT 729-PPRD-01-01 HYDRO SYSTEM FLUSH / FILTER R/R B SYSTEM. NO METAL OR DEBRIS NOTED. TTG8Q00DVGR3 ' B ' EMDP R/R; TTG8Q00VGR5 #2 EDP R/R; SYSTEM RESTORED NO LEAKS NOTED.
DURING FLIGHT AT 29K FEET WE LOST HYDRAULIC SYS B FLUID WENT TO ZERO AND TOTAL LOSS OF PRESSURE / [01] REF TTG8Q00DVGLL ALT BRAKE SELECTOR VALVE LEAKING. MT 729-PPRD-01-01 HYDRO SYSTEM FLUSH / FILTER R/R B SYSTEM. NO METAL OR DEBRIS NOTED. TTG8Q00DVGR3 ' B ' EMDP R/R; TTG8Q00VGR5 #2 EDP R/R; SYSTEM RESTORED NO LEAKS NOTED.
EXIT LIGHT COVER FELL OFF ON TAKEOFF (MIDDLE OF AIRCRAFT). WILL NOT STAY SECURED. / [01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW MM 33-51-01. OPS A CHECK GOOD.
FWD OVERHEAD EXIT SIGN FELL OFF / [01] SECURED LENS PER SIP/AMM 33-51-01. OK FOR SERVICE
INOP BATTERY EMERGENCY LIGHT AFT GALLEY AREA RH ; 2021-549938 / [01] REPLACED BATTERY PACK ON AFT GALLEY AREA ON RH SIDE P/N OFF: D717-01-100SWA S/N OFF: 19023 P/N ON: D717-01-100SWA S/N ON: 310687 AND PERFORMED OPERATIONAL TEST OF THE NEW BATTERY PACK IAW B737-700 AMM 33-51-06-960-805 TEST IS OK; [02] COMPLETE TASK CERTIFIED
BROKEN FWD SERVICE DOOR SLIDE SHOCK MOUNT AT PASSENGER CABIN (1 EA) ; 2021-549919 / [01] REPLACED SLIDE SHOCK MOUNT LOC. FWD SERVICE DOOR AT PASSENGER CABIN (1 EA) I.A.W B737-700 SRM 51-40-02 AND 51-10-02 PARAGRAPH 9; [02] CERTIFIED WORK PERFORMED
CRACK GUSSET LOCATED BS 500D STR 19R FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED BS 500D STR 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. DGW: 143A7902 REV: E.
CRACK GUSSET LOCATED BS 500D STR 19L FWD CARGO COMPARTMENT ; 2021-549916 / [01] REPLACED GUSSET LOCATED BS 500D STR 19L FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02-0G-0 STEP9 AND DWG 143A7902 REV:E. PART USED P/N: 143A9481-6. P/0: 2021-118586. SEE INDIVIDUAL SIGN OFFS BELOW.
CORROSION WEB LOCATED BS196.5 TO BS203.8 AND LBL 9; WL148.5 AT LOWER FUSELAGE ; 2021-549878 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 21-JAN-22; TEMPERATURE CHART RECORD P/N: KT8P2; S/N: 19021963; DUE DATE: 14-MAY-22.; [02] REPLACED WEB AND FASTENERS LOCATED BS196.5 TO BS203.8 AND LBL 9; WL148.5 AT LOWER FUSELAGE I.A.W B737-700 SRM 51-40-02 AND DWG 141A3501 REV D; 141A1502 REV F.; [03] CORRECTED STEP 2. REPLACED WEB AND FASTENERS LOCATED BS196.5 TO BS203.8 AND LBL 9; WL148.5 AT LOWER FUSELAGE I.A.W B737-700 SRM 51-40-02 AND DWG 141A3501 REV D; 141A1502 REV F.
SUPPLEMENTAL INFORMATION: CRACK INTERNAL CAVITY STRINGER U-8 UPPER SURFACE BETWEEN RIB 19 TO RIB 20 AT LT WING ; 2021-549843 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020. DUE DATE: 21-JAN-22.; [02] PERFORMED REPAIR UPPER STRINGER U8 BETWEEN RIB 19 TO RIB 20 (WSTA 564.5 AND WSTA 591.5) LT WING IAW EA 21-157-03716 WIP 1 BARCODE TTG8Q009T67U AND EA 21-157-03716 BARCODE TTG8Q009YPH6 SEE INDIVIDUAL SIGN OFF BELOW.; [03] PERFORMED REPAIR UPPER STRINGER U8 BETWEEN RIB 19 TO RIB 20 (WSTA 564.5 AND WSTA 591.5) LT WING IAW EA 21-157-03716 WIP 1 BARCODE TTG8Q009T67U AND EA 21-157-03716 BARCODE TTG8Q009YPH6 SEE INDIVIDUAL SIGN OFF BELOW.
SUPPLEMENTAL INFORMATION: CRACK INSPAR RIB LOC STAB STA 129.50 AT 35 INCH FROM FRONT SPART LT HORIZONTAL STAB (1 E/A) ; 2021-549836 / [01] TOOL USED. EDDY CURRENT EQUIPMENT. P/N: NORTEC 500D. S/N: N500X12101V022233. DUE DATE: 02-JUN-22.; [02] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN:200048001;DUE DATE: 24-FEB-22; [03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 21-JAN-22. TEMPERATURE CONTROLLER P/N 142811019 DUE DATE: 21-JAN-22.; [04] PERFORMED REPAIR INSPAR RIB LOC STAB STA 129.50 AT 35 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW EA 21-155-03744-WIP1 BARCODE TTG8Q009V2WC AND EA 21-155-03744 BARCODE TTG8Q00A22Y3<BR><BR>SEE INDIVIDUAL SIGNOFF BELOW; [05] PERFORMED REPAIR INSPAR RIB LOC STAB STA 129.50 AT 35 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW EA 21-155-03744-WIP1 BARCODE TTG8Q009V2WC AND EA 21-155-03744 BARCODE TTG8Q00A22Y3 AS RII
SUPPLEMENTAL INFORMATION: CRACK ACCESS PANEL 651GB CORRUGATED PLATE AT RT WING ; 2021-549847 / [01] REPLACED CORRUGATED PLATE ON ACCESS PANEL 651GB AT RT WING. I.A.W B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A2001 REV:A SHEET 7; [02] INSTALLED CORRUGATED PLATE ON ACCESS PANEL 651GB AT RT WING. I.A.W B737-700 SRM 51-40-02 AND DWG 115A2001 REV:A SHEET 7
CRACK ANGLE - CLIP LOC ON BS 400 AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT ; 2021-549819 / [01] REPLACED CLIP AND FASTENERS LOC ON BS 400 AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. DWG: 143A7505 REV: B; [02] REPLACED CLIP AND FASTENERS LOC ON BS 400 AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. DWG: 143A7505 REV: B. COMPLETED
SUPPLEMENTAL INFORMATION: CRACK ACCESS PANEL 532NB FUEL TANK FLOAT AT LT WING ; 2021-549811 / [01] FAULT RESOLVED ON OTHER FAULT REPLACED FUEL TANK FLOAT ON ACCESS PANEL 532NB AT LT WING ON TTG8Q009MYPM; [02] TASK CARD COMPLETED
CRACK ANGLE - CLIP LOCATED ON BS 500C AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT ; 2021-549817 / [01] REPLACED CLIP AND FASTENERS LOCATED ON BS 500C AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02. DGW: 143A7505 REV: A.; [02] CORRECTED STEP 1 <BR>REPLACED CLIP AND FASTENERS LOCATED ON BS 500C AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02. DWG: 143A7505 REV: A.<BR>SEE INDIVIDUAL SIGNOFFS BELOW.; [03] REPLACED CLIP AND FASTENERS LOCATED ON BS 500C AFT FACE AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02. DWG: 143A7505 REV: A. COMPLETED
CRACK DORSAL FIN RIB 8 AT VERTICAL STABILIZER ; 2021-549833 / [01] REPLACED RIB 8 AND FASTENERS LOC. DORSAL FIN AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A1008 SHEET 2 REV.C. REPLACED RIB 8 AND FASTENERS LOC. DORSAL FIN AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A1008 SHEET 2 REV.C. SEE INDIVIDUAL SIGN OFF BELOW.
CORROSION SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL STR 25R RBL 21 AT AFT CARGO COMPARTMENT ; 2021-549830 / [01] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL STR 25R RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A7500 REV:- SEE INDIVIDUAL SIGNOFFS BELOW.; [02] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW
CRACK FLOOR STRUCTURE PLATE LOCATED ON BS 540 BTW BL 0 TO RBL 25 AT PASSENGER CABIN ; 2021-549792 / [01] REPLACED FLOOR STRUCTURE PLATE LOCATED ON BS 540 BTW BL 0 TO RBL 25 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-40-02 ;SRM 51-10-02 ITEM 9 AND DWG 143A0060; SHEET 2; REV B; [02] VERIFIED TASK COMPLETE.<BR>TASK RII.
CORROSION STRINGER 26L LOCATED ON BS 540 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 26L BETWEEN BS500D TO BS540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.
CORROSION STRINGER 23L BS 540 AT WL 164 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 23L BETWEEN BS500D TO BS540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1; REPAIR 1 FIG 206.
SUPPLEMENTAL INFORMATION: CRACK FLOOR STRUCTURE PLATE LOCATED ON BS 540 BTW BL 0 TO LBL 25 AT PASSENGER CABIN ; 2021-549793 / [01] REPLACED FLOOR STRUCTURE PLATE LOCATED ON BS 540 BTW BL 0 TO LBL 25 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-40-02 ;SRM 51-10-02 ITEM 9 AND DWG 143A0060; SHEET 2; REV B; [02] VERIFIED TASK COMPLETE.<BR>TASK RII.
CRACKED STRINGER 26R, AT BS 540 IN FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 26R LOCATED BTW BS500D TO BS540 IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.
CORROSION STRINGER 25R AT BS 540 AND WL 156 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR LOCATED STRINGER 25R BETWEEN BS500C TO BS540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.
CORROSION STRINGER 23R LOCATED AT BS 540. WL164 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 23R BETWEEN BS500D TO BS540 WL154 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.
BROKEN TRAILING EDGE CORRUGATED PLATE LOCATED WS180.00 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING ; 2021-549676 / [01] REPLACED CORRUGATED PLATE LOCATED WS180.00 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING. I.A.W B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A2001 REV: B SHEET 1.; [02] REPLACED CORRUGATED PLATE LOCATED WS180.00 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING. I.A.W B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A2001 REV: B SHEET 1.
BROKEN TRAILING EDGE CORRUGATED PLATE LOCATED WS204.25 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING ; 2021-549674 / [01] REPLACED CORRUGATED PLATE LOCATED WS204.25 INTERNAL AREA OF ACCESS PANEL 651EB AT RT WING. IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A2001 REV: B SHEET 1; [02] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW
BROKEN SUPPORT BRACKET LOCATED IRSS140 REAR SPAR UPPER AREA AT LT WING ; 2021-549710 / [01] REPLACED SUPPORT BRACKET LOCATED IRSS140 REAR SPAR UPPER AREA AT LT WING IAW B737-700 SRM 51-10-02-0G-0 STEP 9; [02] TASK COMPLETED
BROKEN ANGLE TRAILING EDGE LOCATED ORSS174 REAR SPAR UPPER AREA AT RT WING ; 2021-549722 / [01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS174 REAR SPAR UPPER AREA AT RT WING I.A.W B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 SEE INDIVIDUAL SIGNOFFS BELOW.; [02] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW
CORROSION STRINGER 22R LOCATED AT BS 540 AND WL 168 AT FWD CARGO COMPARTMENT ; 2021-549688. PERFORMED PERMANENT REPAIR LOCATED STRINGER 22R BETWEEN BS500C TO BS540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.
CORROSION STRINGER 24R LOCATED AT BS 540 AND WL 160 AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR STRINGER 24R BETWEEN BS500D TO BS540 AND WL 160 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.
CRACK ACCESS PANEL 561AB HOLES AT LT WING ; 2021-549546 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 15331932; DUE DATE: 26-OCT-22; [02] HOT BONDER PN: HCS9200B-AV; SN: 18196021; DUE DATE: 14/DEC/21.; [03] SCALE P/N: 1863T62; S/N: AE-40571; DUE DATE: 19-MAY-22; [04] TOOL USED SCALE P/N:SCA-301 S/N:AE-412125 DUE DATE: 24 FEB 22.; [05] HOT BONDER PN: HCS9200B; SN: 16122983; DUE DATE: 16/DEC/21.; [06] REPAIRED ACCESS PANEL 561AB AT LT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9. TOOL USED: MULTIMETER P/N:FLUKE 1587 S/N:19370078 DUE DATE: 10-OCT-22. SEE INDIVIDUAL SIGNOFFS BELOW.; [07] JOB COMPLETED.
CRACK ACCESS PANEL 561BB HOLES AT LT WING ; 2021-549549 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 15331932; DUE DATE: 26-OCT-22; [02] HOT BONDER PN: HCS9200B-AV; SN: 18196021; DUE DATE: 14/DEC/21.; [03] SCALE P/N: 1863T62; S/N: AE-40571; DUE DATE: 19-MAY-22; [04] TOOL USED SCALE P/N:SCA-301 S/N:AE-412125 DUE DATE: 24 FEB 22.; [05] HOT BONDER PN: HCS9200B; SN: 16122983; DUE DATE: 16/DEC/21.; [06] TOOL USED: DIGITAL MEGOMETHER P/N: 3454-10 S/N: 071012680 DUE DATE: 28-DEC-22; [07] CORRECTIVE ACTION 6 ENTRY BY ERROR: <BR>THE CORRECT ACTION IS: TOOL USED: DIGITAL MEGOMETHER P/N: 3454-10 S/N: 071012680 DUE DATE: 28-AUG-22; [08] REPAIRED ACCESS PANEL 561BB AT LT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9.
CRACK SUPPORT ANGLE LOCATED BS695 AND LBL24.75 LOWER POSITION CENTER SECTION ; 2021-549500 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE 22 JAN 22; P/N P3015GOES00000 S/N 112820025 DUE DATE 22 JAN 22.; [02] REPLACED SUPPORT ANGLE LOCATED BS695 AND LBL24.75 LOWER POSITION CENTER SECTION I.A.W B737-700 SRM 51-40-02 AND DWG 111A6000; SHEET 4; REV A; [03] VERIFIED TASK COMPLETE
CRACK ON FWD CORNER SCUFF PLATE LOCATED BS 792 AT AFT CARGO BAY. REPAIRED BY WELDING FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1.
CRACK ON FWD CORNER SCUFF PLATE LOCATED BS 440 AT FWD CARGO COMPARTMENT ; 2021-549494 / [01] TOOL USED; DIGITAL CALIPER; P/N:500-197-30 S/N:A21142022 DUE DATE:02-OCT-22.; [02] REPAIRED BY WELDING FWD CORNER SCUFF PLATE LOCATED BS 440 AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.<BR>TOOL USED; DIGITAL CALIPER; P/N:500-197-30 S/N:A21142022 DUE DATE:02-OCT-22. SEE INDIVIDUAL SIGNOFFS BELOW.; [03] REPAIRED BY WELDING FWD CORNER SCUFF PLATE LOCATED BS 440 AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.
CRACK SUPPORT ANGLE LOCATED BS695 AND BL0 LH SIDE CENTER SECTION ; 2021-549495 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22 TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [02] REPLACED SUPPORT ANGLE LOCATED BS695 AND BL0 LH SIDE CENTER SECTION I.A.W B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 5; REV A; [03] VERIFIED TASK COMPLETE. TASK RII.
CRACK SUPPORT ANGLE LOCATED BS695 AND BL0 RH SIDE CENTER SECTION ; 2021-549493. REPLACED SUPPORT ANGLE LOCATED BS695 AND BL0 RH SIDE CENTER SECTION I.A.W B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 5; REV A; [03] VERIFIED TASK COMPLETE. TASK RII.
CRACK SUPPORT ANGLE LOCATED BS695 AND RBL24.75 VERTICAL POSITION CENTER SECTION ; 2021-549502. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS695 AND RBL24.75 VERTICAL POSITION CENTER SECTION I.A.W. B737-700 SRM 51-10-02 AND DWG 111A6002; SHEET 10; REV. A.; REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS695 AND RBL24.75 VERTICAL POSITION CENTER SECTION IAW SRM 51-10-02 AND DWG 111A6002; SHEET 10; REV. A. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS695 AND RBL24.75 VERTICAL POSITION CENTER SECTION IAW SRM 51-10-02 AND DWG 111A6002; SHEET 10, REV A.
CRACK ON AFT CORNER SCUFF PLATE LOCATED BS 847 AT AFT CARGO BAY. REPAIRED BY WELDING AFT CORNER SCUFF PLATE LOCATED BS 847 AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1.
CRACK ON AFT CORNER SCUFF PLATE LOCATED BS 492 AT FWD CARGO COMPARTMENT ; 2021-549491 / [01] TOOL USED; DIGITAL CALIPER P/N:500-197-30 S/N:A21142022 DUE DATE: 02-OCT-22.; [02] REPAIRED BY WELDING AFT CORNER SCUFF PLATE LOCATED BS 492 AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.<BR>TOOL USED; DIGITAL CALIPER; P/N:500-197-30 S/N:A21142022 DUE DATE:02-OCT-22. SEE INDIVIDUAL SIGNOFFS BELOW; [03] REPAIRED BY WELDING AFT CORNER SCUFF PLATE LOCATED BS 492 AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.
CRACK SUPPORT ANGLE LOCATED BS695 AND RBL24.75 LOWER POSITION CENTER SECTION ; 2021-549498 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22 TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [02] REPLACED SUPPORT ANGLE LOCATED BS695 AND RBL24.75 LOWER POSITION CENTER SECTION I.A.W B737-700 SRM 51-40-02 AND DWG 111A6000; SHEET 4; REV A; [03] VERIFIED TASK COMPLETE
DELAMINATED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT ; 2021-549424 / FABRICATED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT I.A.W. B737-700 AMM 25-52-01-201-801 STEP 1(A) AND DRAWING 453A2610 REV C. CORRECTED STEP 1 FABRICATED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW AMM 25-52-01-201-801 AND DRAWING 453A2610 REV C. FABRICATED AFT CARGO PANEL 142MW IAW AMM B737-700 25-52-01-201-801 ITEM 1F AND DWG 453A2510 REV :. FABRICATED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW AMM 25-52-01-201-801 AND DRAWING 453A2610 REV C.
CUSTOMER REQUEST CRACK ON VAPOR BARRIER LOCATED BS 663.75 RBL 17 APPROX. RT MAIN WHEEL WELL COMPARTMENT ; 2021-549467 / [01] TOOL USED= CALIPER P/N: 500-196-30; S/N: A21126170; DUE DATE: 15-OCT-22; [02] REPAIRED VAPOR BARRIER LOCATED BS 663.75 RBL 17 APPROX. RT MAIN WHEEL WELL COMPARTMENT AS PER B737-700 SRM 57-10-10-2R-2 REPAIR 2 PARAGRAPH 6. SEE INDIVIDUAL SIGNOFFS BELOW; [03] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW
CRACK INSPAR RIB LOC. STAB STA 129.50 AT 27 INCH FROM FRONT SPART LT HORIZONTAL STAB (1 EA). PERFORMED REPAIR INSPAR RIB LOC. STAB STA 129.50 AT 27 INCH FROM FRONT SPART LT HORIZONTAL STAB I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4.
CRACK INSPAR RIB LOC. STAB STA 129.50 AT 19 INCH FROM FRONT SPART LT HORIZONTAL STAB (1 EA). PERFORMED REPAIR INSPAR RIB LOC. STAB STA 129.50 AT 19 INCH FROM FRONT SPART LT HORIZONTAL STAB I.A.W B737-700 SRM 55-10-09-2R-5 ;REPAIR 5; PARAGRAPH 4; N;O;P;Q;R;S.
DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (4 EA) ; 2021-549406 / [01] GENERAL FAULT RESOLVED ON OTHER SEE TTG8Q0030UQQ; [02] GENERAL FAULT RESOLVED ON OTHER SEE TTG8Q0030UQQ
FUEL CROSSFEED VALVE CB POPPED IN FLIGHT. NO HARD LANDING. NO EXCESSIVE BRAKING. FUEL IMBALANCE 2300# UPON LANDING. FUEL IMBALANCE LT ILLUMINATED. ; / [01] FOUND C/B POPPED WITH CROSS FEED VALVE IN THE OPEN POSITION. C/B WOULD NOT RESET. REPLACED CROSS FEED VALVE REF AMM 28-22-21. VALVE OPS CHECKS NORMAL.
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01670 ; / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK AND CHARGING BASE AT LOCATION M01670 PER AMM 33-51-06
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01670 ; / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK AND CHARGING BASE AT LOCATION M01670 PER AMM 33-51-06
RIGHT WING TO BODY PANELS 191AR; 191FR SUPPORT ASSEMBLY CRACKED ; / [01] REMOVED AND REPLACED RIGHT WING TO BODY PANELS 191AR; 191FR SUPPORT ASSEMBLY IAW SRM 51-40-02
AFT SERVICE DOOR SLIDE LOOSE. ; / [01] REPACKED AFT SERVICE DOOR ESCAPE SLIDE IAW MT 725-61-06. A/C OK FOR SERVICE.
AFT GALLEY INBD FLASHLIGHT STRAP BROKEN / REMOVED AND REPLACED 'FOR EMERGENCY USE ONLY' STRAP ON AFT GALLEY I/B FLASHLIGHT. REF AMM 25-64-00
APPEARANCE TECHS REPORT L1 DOOR SLIDE HAS COME OUT OF ITS HOLDER. REPACKED L1 DOOR SLIDE PER MT 725-61-06.
AFT ENTRY DOOR ESCAPE SLIDE IS NOT PACKED CORRECTLY. / REPACKED AFT ENTRY DOOR ESCAPE SLIDE PER MT 725-61-06
L1 DOOR EMERGENCY EXIT LIGHT LENS WOULD NOT STAY ON. INSTALLED NEW LENS IAW SIP AND AMM.
FORWARD SERVICE DOOR UPPER EMERGENCY LIGHT ASSEMBLY WOULD NOT ILLUMINATED. R&R M1675 EMERGENCY LIGHT POWER SUPPLY PER AMM.
FWD CARGO DOOR CENTER SCUFF PLATE IS DAMAGED. / REMOVED AND REPLACED REF AMM 53-11-02.
EMERGENCY LIGHT BATTERY PACK AT POSITION M1668 FAILED OPERATIONAL TEST. / R&R BATTERY PACK IAW AMM.
INTERCOSTAL CRACKED BETWEEN BS. 328 TO BS. 344, LBL 45. / R&R INTERCOSTAL PER SRM AND DWG.
INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, LBL 45. / R&R INTERCOSTAL PER SRM AND DWG.
FLOOR BEAM UPPER CHORD CRACKED AT BS. 328, RBL 23. / REPAIRED CHORD IAW SRM.
FLOOR BEAM LOWER CHORD STABILIZER STRAP CRACKED BETWEEN BS. 312 TO BS. 328, RBL 30. / REPAIRED STRAP PER SRM.
INTERCOSTAL CRACKED BETWEEN BS. 294.5+5 TO BS. 312, RBL 15. / R&R INTERCOSTAL PER SRM AND DWG.
CRACK INTERCOSTAL STA 312+5'; RBL 30; WL 207.54 / REMOVED AND REPLACED INTERCOSTAL AT STA 312 TO STA 328 RBL 30 WL 207.54 IRW 737-700 SRM 51-40-02-0-0G
AFT PRESSURE BULKHEAD BOLT 9R HOLE OUT OF TOLERANCE AT BS. 1016, STR. 3R. / REPAIRED BULKHEAD IAW SOUTHWEST SPECIAL ITEM.
AFT PRESSURE BULKHEAD HOLE BOLT 9L OUT OF TOLERANCE AT BS. 1016, STR. 3L. / REPAIRED BULKHEAD IAW SOUTHWEST SPECIAL ITEM.
AFT PRESSURE BULKHEAD BOLT 8R HOLE OUT OF TOLERANCE AT BS. 1016, STR. 3R. / REPAIRED BULKHEAD IAW SOUTHWEST SPECIAL ITEM.
AFT PRESSURE BULKHEAD BOLT 7R HOLE OUT OF TOLERANCE AT BS. 1016, STR. 3R. / REPAIRED BULKHEAD IAW SOUTHWEST SPECIAL ITEM.
CRACK AT FWD CARGO CENTER SCUFF PLATE 7' FROM AFT EDGE; STA 460+10'; STR 24R. / ACCOMPLISHED WELDING REPAIR AS REQUIRED AT FWD CARGO CENTER SCUFF PLATE P/N 143A833-5 B4 VENDOR J.L. WELDING INC. UNDER OUR W.O 15793 AND SWA EA NO: 1-A53-2076 REV 11
R/H PRESSURE WEB LIGHT CORRODED 7 INCHES FROM INBOARD FORWARD SIDE AND 10 INCHES AFT SIDE AT BS. 1016. / R&R WEB PER SRM.
L/H EMERGENCY LIGHT FAILED TEST AT SEAT ROW 11. / R&R LIGHT ASSEMBLY IAW AMM.
FRAME BOLT HOLE 7L OUT OF TOLERANCE AT BS. 1016, STR 3L. / REPAIRED FRAME IAW SOUTHWEST SPECIAL ITEM.
FRAME BOLT HOLE 8L OUT OF TOLERANCE AT BS. 1016, STR. 3L. / REPAIRED FRAME IAW SOUTHWEST SPECIAL ITEM.
WHEEL WELL VAPOR BARRIER FORWARD SIDE SUPPORT ANGLE CRACKED AT BS. 663, RBL 6. / R&R ANGLE IAW SRM.
PRESSURE BULKHEAD WEB CORRODED BETWEEN BS. 1016 TO BS. 1040, BETWEEN STR. 24L TO STR. 25R, LOWER AREA. / REPAIRED SKIN PER EA.
AFT CARGO RIGHT SIDE 'Z' CHANNEL IS CORRODED AT BS 727A TO 767. / REMOVED CORROSION AT AFT CARGO RIGHT SIDE ZEE CHANNEL AT BS 727A TO BS 767 PER REF B737-700 SRM 51-10-02-0G-0. FOUND OUT OF LIMITS. REMOVED AND REPLACED ZEE CHANNEL AT AFT CARGO RIGHT SIDE BS 727A TO BS767 PER REF B737-700 SRM 51-40-02-0G-0 AND DWG#146A7502.
ANGLE CORRODED BETWEEN BS. 350 TO BS. 360, STR. 27L. / R&R ANGLE PER DWG AND SRM.
AFT CARGO LEFT SIDE "Z" CHANNEL CORRODED BETWEEN BS. 727C TO BS. 807. / R&R "Z" CHANNEL PER SRM AND DWG.
AFT CARGO FLOOR SUPPORT AT BS 887 IS CORRODED AT 11 INCHES LEFT OF CENTER LINE TO 20' RIGHT OF CENTER LINE. / ACCOMPLISHED INSPECTION AT AFT CARGO FLOOR SUPPORT AT STA 887.FOUND DEEP CORROSION AT FASTENER HOLE.FOUND OUT OF LIMITS.REMOVED AND REPLACED FLOOR SUPPORT IAW B737 SRM 53-00-53-1A-2; SRM 51-40-05-0G-0 AND 51-40-02-0G-0. (AR 20492 11/01/19)
AFT PRESSURE WEB WAS HEAVILY CORRODED AT BS. 1016, BETWEEN LBL 7 TO RBL 7. / REPAIRED WEB PER EA.
INTERCOSTAL WEB CORRODED AT BETWEEN BS. 807 TO BS. 827, STR. 27R. / R&R WEB PER SRM AND DWG.
R/H HORIZONTAL STABILIZER INSPAR #4 RIB #4 STIFFENER CRACKED. / REPAIRED STIFFENER IAW SRM.
R/H HORIZONTAL STABILIZER INSPAR #4 RIB #4 STIFFENER CRACKED. / REPAIRED RIB IAW SRM.
AFT PRESSURE BULKHEAD BOLT 5R HOLE OUT OF TOLERANCE AT BS. 1016, STR. 2R. / REPAIRED PRESSURE BULKHEAD IAW SI.
AFT PRESSURE BULKHEAD BOLT HOLE 6R OUT OF TOLERANCE AT BS. 1016, STR. 2R. / REPAIRED BULKHEAD IAW SI.
R/H HORIZONTAL STABILIZER INSPAR #4 RIB ASSEMBLY, #3 STIFFENER CRACKED. / REPAIRED #4 RIB IAW SRM.
R/H HORIZONTAL STABILIZER INSPAR #4 RIB ASSEMBLY, #3 STIFFENER CRACKED. / REPAIRED #3 STIFFENER IAW SRM.
AFT PRESSURE BULKHEAD BOLT HOLE 5L OUT OF TOLERANCE AT BS. 1016, STR. 2L. / REPAIRED BULKHEAD IAW SI.
LH CREASE BEAM INNER CORD UPPER SURFACE HAS LIGHT CORROSION SPOTS BETWEEN STA 616 AND 727 / BLENDED OUT CORROSION AT L/H CREASE BEAM INNER CORD UPPER SURFACE STA 663; 75+9' TO STA 727 ORIG MAT .071' MAT LOST .003' MAT REMAINING .068' FOUND TO BE IN LIMIT IAW B737 SRM 53-40-13-1A-A FIG 103 DET C TREATED AND PRIMED AREA SRM 51-20-01-0G-0. STA 616 TO STA 663.75+9' ORIG MAT .050' MAT LOST .018' MAT REMAINING .032' FOUND TO BE OUT OF LIMIT SRM 53-40-13-1A-1 FIG 103 DET C REMOVED AND REPLACED L/H CREASE BEAM FROM STA 520+11' TO STA 663.75+9' IAW B737 SRM 51-40-02-0G-0 AND DWG # 144A5901 DA 18533 11-7-19
AFT PRESSURE BULKHEAD BOLT 6L HOLE OUT OF TOLERANCE AT STA 1016, STR. 2L. / REPAIRED FASTENER HOLE IAW SI.
324QL VERT STAB T/E LH PANEL CRACKED. (200-034) / REMOVED AND REPLACED VERTICAL STAB T/E L/H PANEL 324QL IAW B737 SRM 51-40-02-0G-0
LH WING #2 KRUGGER FLAP UPPER I/B CORNER CRACKED 2'X2' PIECE. / REMOVED; REPAIRED; AND REINSTALLED L/H WING #2 KRUGER FLAP; AS PER B737 AMM 27-81-11-400-801. ACCOMPLISH OPS CHECK AS PER B737 AMM 27-81-11-400-801 FOUND NORMAL
DENT ON FLIGHT DECK FLOOR APPROXIMATELY BS 260, LBL12. / REMOVED DAMAGE AND PERFORMED REPAIR IAW EA # 1-A53-33179.
VAPOR WEB FORWARD FACE ANGLE CRACKED AT BS. 633, LBL 15. / R&R ANGLE PER SRM AND DWG.
L/H MLG FWD TRUNNION SUPPORT FITTING LOWER OUTBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 REPAIR 2 SEE WO P26883
L/H MLG FWD TRUNNION SUPPORT FITTING UPPER OUTBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 REPAIR 2 SEE W/O P26883
L/H MLG FWD TRUNNION SUPPORT FITTING UPPER INBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 REPAIR 2 SEE W/O 26883
R/H MLG FWD TRUNNION SUPPORT FITTING UPPER INBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 REPAIR 2 SEE WO# 26883
R/H MLG FWD TRUNNION SUPPORT FITTING UPPER OUTBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 R-2 REPAIR 2 SEE WO# P26883
L/H MLG FWD TRUNNION SUPPORT FITTING LOWER INBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 REPAIR 2 SEE W/O P26883
R/H MLG FWD TRUNNION SUPPORT FITTING LOWER OUTBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 REPAIR 2 SEE WO P26883
L/H EMERGENCY EXIT DOOR LIGHT INOP. R&R LIGHT PER MM.
L/H AFT FLASHLIGHT STRAP BROKEN. R&R STRAP PER MM.
R/H MIDDLE FORWARD OF R/H EMERGENCY EXIT DOOR, EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. / R&R BATTERY PER AMM.
L/H FORWARD EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. / R&R BATTERY PER AMM.
L/H AFT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. / R&R BATTERY PER AMM.
R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.
RT EMERGENCY EXIT LIGHT INOP. R&R BATTERY CRADLE PER AMM.
RT EMERGENCY EXIT LIGHT INOP. R&R BATTERY CRADLE PER AMM.
LT EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER AMM.
RT VERTICAL STABILIZER ATTACH SKATE ANGLE WORN ON THE VERTICAL FLANGE, AT STA 1119, BELOW ACCESS PANEL 323CR. REPAIRED ANGLE PER SRM.
RH HORIZONTAL LEADING EDGE HAS CRACKED RIB AT STA 86.66 / REMOVED AND REPLACED RH HORIZONTAL LEADING EDGE RIB AT STA 86.66 NDT OPEN HOLES. INSTALLED RIB AIW BOEING DWG 186A 1001 REV B AND SRM 51-40-02-0G-0
LEFT HORIZONTAL STABILIZER LEADING EDGE RIB UPPER AFT FASTENER HOLE CRACKED AT BS 95.96. R & R RIB IAW DWG AND SRM.
PASSENGER CABIN FLOORBOARD 231JF HAS PUNTURE AT CENTER FWD END TOP SIDE / REPAIRED PASSENGER CABIN FLOORBOARD 231JF OF PUNCTURE AT CENTER FORWARD END TOP SIDE IAW B737 SRM 53-00-50-2R-4 REV 63 AND B737 SRM 53-00-560-2R-0 REPAIR GENERAL REV 63. A26592; A26386; A51273
RT OUTBOARD SEAT TRACK CROWN CORRODED BETWEEN BS 701 TO BS 724. R&R SEAT TRACK IAW SRM.
AFT CARGO COMPARTMENT FLOOR AFT TIE DOWN TRANSITION STRAP IS CORRODED / AFTER FURTHER INVESTIGATION THE CORROSION HAS NO LIMIT AND THE PART REQUIRED REPLACEMENT IAW B737-700 SRM 51-10-02-0G-0
AFT WET AREA FLOOR PANEL 242RF UPPER FACESHEET HAS FIBER DAMAGE / PREPPED VERIFIED MATERIALS AND BONDED REPAIR TO F/B # 242 RF IAW 737 SRM 53-00-50-2R-1 REV 63 53-00-50-2R-0 REV 63
AFT WET AREA FLOOR PANEL 241ZF HAS DAMAGE ON EDGES / REPAIRED AFT WET AREA FLOOR PANEL 241ZF OF ONE PLY DAMAGE ONLY IAW B737 SRM 53-00-50-2R-4 REV 63 AND B737 SRM 53-00-50-2R-0 REPAIR GENERAL. ALONG PANEL EDGES A26592; A51273; A26386; A44008; A06044; A31296
FWD WET AREA FLOOR PANEL 221DF LOWER FACESHEET IS DAMAGED AT INSERT HOLES / PREPPED; VERIFIED MATERIALS; AND BONDED F/B # N765SW IAW 737 SRM 53-00-50-2R-0 REV 63 737 SRM 53-00-50-2R-2 REV 63
FWD WET AREA FLOOR PANEL 221FF UPPER FACESHEET IS DAMAGED ON INBOARD SIDE / REPAIRED FWD WET AREA FLOOR PANEL 221FF OF INBOARD SIDE UPPER FACE SHEET DAMAGE IAW B737 SRM 53-00-50-2R-6 REV 63 AND B737 SRM 53-00-50-2R-0 REV 63.
AFT WET AREA FLOOR PANEL 241AEF UPPER FACESHEET IS DELAMINATED ON AFT END / REPAIRED AFT WET AREA FLOOR PANEL 241AEF UPPER FACESHEET ON AFT END IAW B737 SRM 53-00-50-2R-4 REV 63. A26386 A28460 A26592
FWD WET AREA FLOOR PANEL 221BF AFT OUTBOARD END IS DAMAGED AND DELAMINATED / REPAIRED FWD WET AREA FLOOR PANEL 221 BF AFT OUT BOARD END IAW B737 SRM 53-00-50-2R-G
AFT CARGO COMPARTMENT FLOOR PANEL 140CF IS CORRODED ON EDGES / AFT CARGO COMPARMENT FLOOR 140CF REMOVED CORROSION FOUND AREA TO BE MORE THAN 3.0' IN LENGTH. OUT OF LIMITS IAW SRM 53-00-53-1A-1. REPLACED PANEL 140CF P/N 453A2610-2. ATAG WN6466. IAW AMM 25-52-10-400-801. PANEL INSTALLED ON J-PANEL -141-CLOSE.
AFT CARGO COMPARTMENT R/H SIDE FLOOR TO SIDEWALL CAPSTRIPS ARE CORRODED / AFT CARGO COMPARTMENT R/H SIDEWALL PANEL CAPSTRIPS. REMOVED OLD CAPSTRIPS 3 EACH AND REPLACED WITH NEW CAPSTRIPS IAW AMM 25-52-10-400-801. AND BOEING DWG 453A2611 REV D.
AFT CARGO COMPARTMENT L/H SIDE FLOOR TO SIDEWALL PANEL CAP STRIPS ARE CORRODED / AFT CARGO COMPARTMENT L/H SIDEWALL PANEL CAPSTRIPS. REMOVED OLD CAPSTRIPS 3 EACH. AND REPLACED WITH NEW CAPSTRIPS. IAW AMM 25-52-10-400-801. AND BOEING 453A2611 REV D.
PASSENGER CABIN R/H INBD SEAT TRACK CROWN FROM STA 698 TO 727 HAS CORROSION. / BLENDED OUT CORROSION ON RH INBD SEAT TRACK CROWN FROM STA 698 TO STA 727 AND FOUND MATERIAL LOSS OUT OF LIMITS IAW B737 SRM 53-00-52-1A-1. MAT. LOSS = .047' ON BOTTOM SIDE OF CROWN; MAT. ALLOWED = .040'. REPAIR AREAS ACCOMPLISHED ON NRC # X666058.
PASSENGER CABIN FWD WET AREA FLOOR PNL # 222BF AFT C CORNER EDGE OF BOARD IS BROKEN AS MARKED ON BOTTOM SIDE / BONDED REPAIR ON FLOOR PANEL 222BF AFT CORNER EDGE IAW B737-200 SRM 53-00-50-1A-1 REV 63; SRM -32 REV 53-00-50-2R-6 REV 63; SRM 53-00-2R-0 REV 63
AFT CARGO COMPARTMENT FLOOR FWD TIE DOWN TRANSITION STRAP IS CORRODED / THE DAMAGE EVALUATED AS CORROSION WITHOUT ALLOWABLE LIMIT; THE PART BEEN REPLACED IAW B737-700 SRM 51-10-02-0G-0
AFT CARGO BAY FLOOR PANEL SPLICE CORRODED AT BS 767. R & R PANEL SPLICE IAW SRM & DWG.
AFT CARGO COMPARTMENT FLOOR PANEL SPLICE CORRODED AT BS 727D. / R&R PANEL SPLICE IAW BOEING DWG.
AFT WET AREA RT CREASE BEAM INNER CHORD CORRODED BETWEEN BS 945 TO BS 992.8. R&R CREASE BEAM IAW SRM AND DWG.
T-CAP CORRODED AT BS 986.5, BETWEEN LBL 21 TO LBL 45. REPAIRED T-CAP IAW SRM.
CABIN L1 ENTRANCE DOOR SILL I/B STIFFNER HAS CORROSION. / REMOVED AND REPLACED L-1 DOOR SILL STIFFNER IAW BOEING 737 DWG 141A8110 ID 0011 REV-
INTERCOSTAL CRACKED BETWEEN BS 308 TO BS 328, RBL 32. R&R INTERCOSTAL IAW SRM & DWG.
CABIN FORWARD WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL IAW SRM AND DWG.
INTERCOSTAL STRUCTURE CORRODED BETWEEN BS 986.5 TO BS 1006, RBL 38. R&R INTERCOSTAL IAW DWG AND SRM.
L1 ENTRANCE INBOARD CREASE BEAM CORRODED BETWEEN BS 308 TO BS 328. R&R CREASE BEAM IAW SRM AND DWG.
LT INBOARD SEAT TRACK CROWN CORRODED BETWEEN BS 500D+16 TO BS 520. REPAIRED SEAT TRACK IAW SRM.
LT OUTBOARD SEAT TRACK CROWN CORRODED BETWEEN BS 500D+10 TO BS 520. REPAIRED SEAT TRACK IAW SRM AND EA.
CABIN L1 DOOR ENTRANCE UPPER SILL WEB MIDDLE STIFFNER HAS CORROSION. / REMOVED AND REPLACED CABIN L-1 DOOR UPPER SILL WEB MIDDLE STIFFNER IAW BOEING 737 SRM 51-40-02 AND BOEING DWG 141A8110 CIC IAW AMM 51-21-91 PAGES 2 AND 6
AFT CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 794 TO BS 810, RBL 14. REPAIRED FLOOR TRACK IAW SRM, EA, & DWG.
AFT CARGO BAY ZEE ANGLE CORRODED AT BS 777, LT SIDE. REPAIRED THE ANGLE IAW SRM.
AFT CARGO BAY ZEE ANGLE CORRODED BETWEEN BS 867 TO 902, RBL 21. R & R THE ANGLE IAW SRM.
FORWARD CARGO COMPARTMENT RT ZEE ANGLE CORRODED BETWEEN BS 500A TO BS 500D. REPAIRED ZEE ANGLE IAW SRM.
L2 DOOR THRESHOLD SUPPORT BRACKET BROKEN AT STA 970 LBL 50....T. VU 22288. / REMOVED L-2 DOOR THRESHOLD SUPPORT BRACKET @ STA 970 LBL 50 IAW SRM 51-40-02-0G-0 AND INSTALLLED NEW THRESHOLD SUPPORT BRACKET @ STA 970 LBL 50 IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A8501 REV:-
AFT CARGO COMP.DOOR SURROUND; THRESHOLD WEB CORRODED AROUND SEVERAL FASTNER HOLES / REMOVED DAMAGE ON WEB MATERIAL LOSS IS .007 ORIGINAL WAS 0.45 REMAINING IS .038 WEB IS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 LOCATED & DRILLED INSTALLED NEW WEB IAW BOEING DWG 146A8340 REV A
AFT CARGO BAY; AT STA. 947.5; LBL 13; AFT OF LEFT CORNER OF STANCHION IS A FLOOR FITTING THAT IS CRACKED. / REMOVED CRACKED FLOOR FITTING AT STA 947 AFT CARGO LBL 13 IAW B737-700 SRM 51-40-02 AND LOCATED AND DRILLED NEW FITTING P/N 149A8113-6 IAW DWG 149A.8113 REV. A. INSTALLED THE NEW FITTING IAW DWG 149A8103 REV:- A 64422
AFT CARGO COMPARTMENT RH SIDE STA. 787 TO STA. 793 SIDE FILLER PANEL HAS CORROSION. SPOTS MARKED WITH DOTS. / REMOVED CORROSION ON SHIELD R/H SIDE STA 787-93 ORIGINAL MATERIAL WAS .050 MATERIAL LOSS IS 0.20 REMAINING 0.30 SHIELD IS FOUND TO BE OUT OF IIMITS IAW BOEING 737-700 SRM 53-60-15-1A-1 LOCATED & DRILLED & INSTALLED NEW SHIELD IAW BOEING DWG 146A0081 REV: A
AFT CARGO BAY; STA 887 FLOOR PANEL SUPPORT HAVE SEVERAL AREAS OF CORROSION. / AFT CARGO BAY; STA 887 FLOOR PANEL SUPPORT CORRODED. 100% MATERIAL LOSS. LOCATED AND DRILLED NEW FLOOR PANEL SUPPORT P/N 146A9401-35 SI#7530863 ATAG WN 6228 IAW BOEING DWG.146A9401 REVA AND SRM 51-40-05
AFT CARGO COMPARTMENT ZEE ANGLE CORRODED BETWEEN BS 761 TO 765, LT SIDE. REPAIRED THE ANGLE IAW SRM.
AFT CARGO COMPARTMENT ZEE ANGLE CORRODED BETWEEN BS 727E & 727E +5, LT SIDE. REPAIRED THE ANGLE IAW SRM.
AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS. 727C+6, STR. 3R. R & R THE FLOOR SUPPORT IAW SRM.
AFT CARGO COMPARTMENT FLOOR PANEL NUT PLATES CORRODED AT BS 727D +5, BETWEEN LBL 12 TO RBL 12. REPAIRED FLOORBEAM IAW EA AND AMM.
RT WING TRAILING EDGE CAVITY 2" INBOARD OF SAILTAIL WAFFLE PLATE CRACKED. R&R WAFFLE PLATE IAW SRM.
PASSENGER CABIN FLOOR PANEL 231FF FORWARD OUTBOARD IS DELAMED / REPAIRED PASSENGER FLOOR PANEL 231FF FORWARD OUTBOARD CORNER IAW SRM 53-00-50-2R-0 REV 63 AND SRM 53-00-2R-10 REV 63
PASSENGER CABIN FLOOR BOARD 241FF MULTIPLE IAW SRM LOCATIOS OF DELAMINATION ON EDGE OF PANEL (MAKRED / REPAIRED PASSENGER CABIN FLOOR BOARD 241FF IAW SRM 53-00-50-SR-0 AND SRM 53-00-50-SR-10. A 26592
PASSENGER CABIN FLOOR PANEL 231FF FORWARD INBOARD CORNER IS CRUSHED/DELAMED / REPAIRED PASSENGER FLOOR PANEL 231FF FORWARD INBOARD CORNERS IAW SRM 53-00-50-2R-0 REV 63 AND SRM 53-00-50-SR-10 REV 63
PASSENGER CABIN FLOOR BOARD 241EF MULTIPLE LOCATIONS OF DELAMINATION AT EDGE OF PANEL (MARKED) / REMOVED PASSENGER CABIN FLOOR BOARD 241EF DELAMINATION ON EDGE OF PANEL (5 EA AREAS) IAW B737 SRM 53-00-50-2R-10 REV 63. A26592
LT WING TRAILING EDGE WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM.
RT MAIN WHEEL WELL HORIZONTAL PRESSURE DECK CRACKED AT BS 663, RBL 41. REPAIRED WEB IAW EA.
LT MAIN WHEEL WELL HORIZONTAL PRESSURE DECK CRACKED AT BS 663, LBL 32. REPAIRED DECK IAW EA.
L2 DOOR EMERGENCY EVAC SLIDE PULL HANDLE COVER LOOSE. SECURED COVER IAW AMM.
L1 DOOR EMERGENCY EVAC SLIDE PULL HANDLE COVER LOOSE. SECURED COVER IAW AMM.
R2 DOOR EMERGENCY EVAC SLIDE PULL HANDLE COVER LOOSE. SECURED COVER IAW AMM.
DIVERSION, INFLIGHT SHUTDOWN, DECLARED EMERGENCY. NR 2 ENGINE FAILURE AT FL 410 CRUISE INCAPABLE OF RESTART. R&R NR 2 ENGINE IAW MT.
L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED HOOKS PER SIP.
L1 DOOR EMERGENCY EVAC SLIDE GIRT OUT OF ADJUST. ADJUSTED SLIDE PER MT.
L2 DOOR EMERGENCY EVACUATION SLIDE FOUND LOOSE. SECURED THE SLIDE IAW MM AND MT.
RIGHT WING OVERWING EMERGENCY EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.
AFT GALLEY AREA, EMER EXIT LIGHT ASSEMBLY BROKEN ON GALLEY 4. R & R LIGHT ASSEMBLY IAW AMM.
RIGHT WING SKIN, CRACKED AT FASTENER HOLE INBD OF RIB 10. REPAIRED SKIN IAW SRM & DWG.
UPPER SUPPORT ON ANGLE CRACKED AT BS 663.75, LBL 8. REPLACED ANGLE IAW SRM.
FORWARD BULKHEAD WEB CRACKED AT BS 663.75 OF LT AT AIR CONDITIONING BAY. REPAIRED WEB IAW EA.
FLOORBEAM CRACKED AT BS 727A+17.5, RBL 45.5, INBD FLANGE, FWD FASTENER HOLE NR 9, HOLE UPPER CHORD HORIZONTAL FLANGES. REPAIRED FLOORBEAM IAW EA.
FLOORBEAM CRACKED AT BS 727A+18.5, LBL 24.75, INBD FLANGE AFT FASTENER HOLE NR 8, HOLE UPPER CHORD HORIZONTAL FLANGES. REPAIRED FLOORBEAM IAW EA.
FLOORBEAM CRACKED AT BS 727A+17.5, LBL 24.75, INBD FLANGE FWD FASTENER HOLE NR 7, HOLE UPPER CHORD HORIZONTAL FLANGES. REPAIRED FLOORBEAM IAW EA.
FLOORBEAM CRACKED AT BS 727A+18.5, LBL 24.75, OTBD FLANGE AFT FASTENER HOLE NR 10, HOLE UPPER CHORD HORIZONTAL FLANGES. REPAIRED FLOORBEAM IAW EA.
SEAT TRACK FLOORBEAM, CRACKED AT BS 727A+17.5, LBL 24.75, OTBD FLANGE FWD FASTENER HOLE NR 9 HOLE UPPER CHORD HORIZONTAL FLANGES. REPAIRED FLOORBEAM IAW EA.
SEAT TRACK FLOORBEAM CRACKED AT BS 727A+18.5, LBL 45.5, INBD FLANGE AFT FASTENER HOLE NR 8, HOLE UPPER CHORD HORIZONTAL FLANGES.
SEAT TRACK FLOORBEAM CRACKED AT BS 727A+17.5, LBL 45, INBD FLANGE FWD FASTENER HOLE NR 7, HOLE UPPER CHORD HORIZONTAL FLANGES. REPAIRED FLOORBEAM IAW EA.
SEAT TRACK FLOORBEAM CRACKED AT BS 727A+18.5, LBL 45.5, OTBD FLANGE, AFT FASTENER HOLE NR 10 HOLE. REPAIRED FLOORBEAM IAW EA.
SEAT TRACK CROSSBEAM FLANGE CRACKED AT BS 727B, LBL 45.5, FASTENER HOLE NR 3. REPAIRED FLOORBEAM IAW EA.
UPPER CHORD HORIZONTAL FLANGE CRACKED AT BS 727A+17.5, RBL 24.75, AT FASTENER HOLE NR 8, OTBD FLANGE AFT HOLE. REPAIRED CHORD IAW EA.
UPPER CHORD HORIZONTAL FLANGE CRACKED AT BS 727A+17.5, RBL 24.75, AT FASTENER HOLE NR 10, INBD FLANGE AFT HOLE. REPAIRED CHORD IAW EA.
UPPER CHORD HORIZONTAL FLANGE CRACKED AT BS 727A+17.5, RBL 24.75, AT FASTENER HOLE NR 9, INBD FLANGE FWD HOLE. REPAIRED CHORD IAW EA.
FRAME CRACKED AT BS 787, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 727B, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 907, STRINGER 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 907, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
SEAT TRACK CRACKED AT BS 727B, LBL 22.75 FASTENER HOLE NR 1 ON CROSSBEAM FLANGE. REPAIRED FLANGE IAW EA.
SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, RBL 45.57 FASTENER HOLE NR 2. REPAIRED SEAT TRACK IAW EA.
FLOORBEAM CRACKED AT BS 727A+18.5, RBL 45.5, OTBD FLANGE AFT FASTENER HOLE NR 8, HOLE UPPER CHORD HORIZONTAL FLANGES. REPAIRED FLOORBEAM IAW EA.
FLOORBEAM CRACKED AT BS 727A+17.5, RBL 45.5, OTBD FLANGE FWD FASTENER HOLE NR 7, HOLE UPPER CHORD HORIZONTAL FLANGES. REPAIRED FLOORBEAM IAW EA.
FLOORBEAM CRACKED AT BS 727A+18.5, RBL 45.5, INBD FLANGE AFT FASTENER HOLE NR 10, HOLE UPPER CHORD HORIZONTAL FLANGES. REPAIRED FLOORBEAM IAW EA.
FRAME CRACKED AT BS 907, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 827, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 500C, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 520, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 500C, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
AFT GALLEY EMER EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.
FRAME CRACKED AT BS 520, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 787, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 480, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 440, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 400, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 500A, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 480, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
LEFT WING NR 3 FLAP TRACK INTERNAL SURFACE DELAMINATED. REPAIRED FLAP TRACK IAW EA & SRM.
RIGHT WING NR 6 FLAP TRACK FAIRING INTERNAL SURFACE DELAMINATED. REPAIRED FAIRING IAW EA & SRM.
VERTICAL PRESS WEB CRACKED AT BS 663, RBL 35. REPAIRED WEB IAW SRM.
RIGHT WING NR 6 SLAT SKIN CRACKED ON LOWER SURFACE. REPAIRED SKIN IAW SRM.
FORWARD LOWER SIDE LIP, EXTERNAL POWER DOOR CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATIONS M1673. R & R BATTERY IAW AMM.
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATIONS M1672. R & R BATTERY IAW AMM.
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATIONS M1670. R & R BATTERY IAW AMM.
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATIONS M1675. R & R BATTERY IAW AMM.
RIGHT LOWER OVERWING EXIT SIGN LENS MISSING. INSTALLED LENS IAW AMM.
EMERGENCY EXIT LIGHT BATTERY FAILED TEST AT ROW 17. R & R BATTERY IAW AMM.
RT HORIZONTAL STABILIZER RIB STATION 120.3, 10" AFT OF FWD SPAR, 1" ABOVE LOWER RIB FLANGE, VERTICAL STIFFENER, CRACKED. REPAIRED STIFFENER ASSEMBLY IAW SRM.
LT WING LOWER LE NR 3 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.
FRAME WEB CRACKED AT BS 727D, STRINGER 8R. REPAIRED WEB IAW EA.
FRAME WEB CRACKED AT BS 747, STRINGER 8R. REPAIRED WEB IAW EA.
LT WING NR 1 SLAT LOWER LE SLAT NOSE SKIN AT ACTUATOR, INBD SKIN CRACKED AT FASTENER. REPAIRED SKIN IAW SRM.
FLIGHT DECK LT NR 1 WINDOW FRAME SKIN CUTOUT CRACKED. REPAIRED FRAME IAW ACO. CORRECTED ATA, DESCRIPTION, PART NAME & PART DEFECT LOCAL.
FLIGHT DECK LT NR 3 WINDOW FRAME CRACKED IN 2ND & 3RD FASTENER HOLES FROM BOTTOM ON FWD SIDE OF FRAME. REPAIRED FRAME IAW SWA EA.
FLIGHT DECK RT NR 3 WINDOW FRAME CRACKED IN 2ND FROM BOTTOM FASTENER HOLE ON FWD SIDE OF FRAME. REPAIRED FRAME IAW SWA EA.
EMERGENCY EXIT LENS BROKEN AFT ENTRY DOOR. REMOVED AND REPLACED AFT ENTRY DOOR EMERGENCY EXIT LIGHTT ASSY PER M/M.
RIGHT FWD LOWER HORIZONTAL STAB SLIDER CRACKED. REPLACED RIGHT FWD LOWER STAB SLIDER REF AMM.
R1 DOOR EMERGENCY EVAC SLIDE LOCK MECHANISM DAMAGED. REMOVED AND REPLACED SLIDE PER M/M.
R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF LIMIT. REMOVED AND REPLACED SLIDE PER MT.
DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BETWEEN LBL 47 TO RBL 47. REPAIRED BEAM IAW EA.
DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 47. REPAIRED BEAM IAW EA.
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME IAW EA.
DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 706 TO BS 727, RBL 63. REPAIRED BEAM IAW ER.
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME IAW EA.
DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA.
DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 47. REPAIRED BEAM IAW SRM.
DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA.
DURING SCHEDULED 12Y CHECK, FOUND STUB FRAME CRACKED AT BS 296, STR 17R. REMOVED AND REPLACED FRAME PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, BL 11. REPAIRED BEAM IAW SRM.
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.
DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. SECURED RETAINER PER MM.
DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED SIGN HOUSING PER MM.
DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
LT OVERHEAD EMERGENCY EXIT SIDEWALL LIGHT INOP. REPAIRED LIGHT PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED 10Y CHECK, FOUND RT WING O/B AFT FLAP I/B TRAILING EDGE DELAMINATED. REPAIRED AFT FLAP PER SRM.
DURING SCHEDULED 10Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 4. REMOVED AND REPLACED BULB PER MM.
DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR CORRODED AT BS 270. REPAIRED FLOOR PER SRM & EA.
DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767, LBL 7.5. REPAIRED BEAM PER EA.
DURING SCHEDULED 10Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 22. RELAMPED LIGHT PER MM.
DURING SCHEDULED 10Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 6. RELAMPED LIGHT PER MM.
DURING SCHEDULED HC2, LT FWD BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER SWA EA.
DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER SWA EA.
DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.
DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
R1 EMERGENCY EXIT DOOR SLIDE LOOSE. REMOVED AND REPLACED SLIDE PER MM.
FOUND R1 DOOR EMERGENCY ESCAPE SLIDE LOOSE. REMOVED AND REPLACED SLIDE PER MM.
DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM.
R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 53. REPAIRED FLOORBEAM PER SWA EA.
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 35 TO RBL 45. REPAIRED FLOORBEAM PER SWA EA.
DIVERSION, HYDRAULIC B-SYSTEM FAILURE. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP PER MM.
L1 DOOR EMERGENCY EVAC SLIDE VIEWING LENS LOOSE. SECURED SLIDE LENS PER MM.
NR 1 TIRE REPORTED FLAT BY ANOTHER AIRCRAFT. INSPECTED LEFT MLG, FOUND AXLE DAMAGE DUE TO NR 1 WHEEL BEARING FAILED. REMOVED AND REPLACED NR 1 MLG INNER CYLINDER PER MM.
R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED HC1 CHECK, OVERWING RT EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, OVERWING LT EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, SEAT ROW 16 EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, ROW AFT LT EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, ROW AFT RT EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, FWD LT EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED 5Y CHECK, FOUND 2 EA LONGITUDINAL FLOORBEAM CRACKS AT BS 773, LBL 12 & RBL 3. REPAIRED BEAMS PER SRM.
L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. RE-INSTALLED SLIDE PER MM.
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REINSTALLED SLIDE PER MM.
FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.
LEFT FWD EEPLS HAS WIRES EXPOSED. REMOVED AND REPLACED EEPLS COVER PER MM.
L1 DOOR EVAC SLIDE DEPLOYED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.
DURING SCHEDULED RON CHECK, (DUE TO SWA SDR SWAA03-2584) FOUND PAX O2 SYS SWEDGED BALLS PULLED AT PSU'S 13 ABC AND 10 DEF. REATTACHED BALLS PER MM.
DURING SCHEDULED RON CHECK, (DUE TO SWA SDR SWAA03-2584) FOUND PAX O2 SYS MASKS TORN AT PSU'S 12 DEF, 19 ABC, 20 ABC, 23 ABC AND 9 DEF. REMOVED AND REPLACED O2 MASKS PER MM.
DURING SCHEDULED A1 CHECK, SWA SI 11038-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS ON NR 2, NR 3 AND NR 4 TAB HINGES PER MM.
DURING SCHEDULED A1 CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED HARDWARE AND BUSHINGS ON NR 1, NR 3 AND NR 4 TAB HINGES PER MM.
DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.
AIR TURNBACK, A-SYSTEM, ELECTRIC HYD PUMP FAILURE. REMOVED AND REPLACED A-SYSTEM HYD PUMP AND CASE DRAIN FILTER PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT LT SIDEWALL. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT SEVERAL LOCATIONS IN CABIN. R & R TRACK COVERS PER MM.
DURING CLIMB, NR 2 ENG VIB BEGAN INCREASING WITH NOTICEABLE AIRFRAME VIBRATION. AT FULL PWR, VIB INCREASED PAST 4. REDUCED PWR PER QRH TO MAINTAIN 4. PRIOR TO TURNBACK COULD MAINTAIN ONLY 92 PERCENT N1 WITH 4.0 VIB. REMOVED NR 2 ENG FAN BLADES, CHECKED BLADE WEIGHT. TRIM WEIGHT ARE IN CORRECT POSITION, ALL FOUND OK. REINSTALLED FAN BLADE SET PER MM. PERFORMED FAN TRIM BALANCE PER MM AND ADJUSTED WEIGHTS PER AVM.
AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND LT WING INBD T/E FLAP HAS A CRACK .75 LONG, 20 OTBD OF FLAP, 6 UP FROM T/E. REPAIRED FLAP PER RA 1-757-0926
DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED GIRT ASSY PER MM.
FWD SERVICE DOOR EVACUATION SLIDE NOT STOWED PROPERLY. REINSTALLED SLIDE ASSY PER MM.