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. (SWAA) | Operator | on 2017-06-03 | 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.
303 reports on file, 2000-05-22 – 2023-08-18.
Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 78,477 hrs · 46,364 cycles
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
Part: PANEL — CRACKED (ZN 400 NACELLE/P) · airframe 78,247 hrs · 46,216 cycles
PANEL 193D CRACKED . CRACK MEASURED 3 IN LENGTH.<[01] REMOVED AND REPLACED FAIRING PANEL 193D PER AMM. 53-51-21.
Part: BULB — INOPERATIVE (ZN 200 FUS TOP) · airframe 78,068 hrs · 46,100 cycles
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
Earlier reports · 2000–2022 · 300 reports
2022
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,538 hrs · 45,134 cycles
INOPERTIVE BULLNOSE EMERGENCY LIGHT 18DEF. RELAMPED PER AMM 33-51-03
Part: FLASHLIGHT — INOPERATIVE (FWD GALLEY) · airframe 76,058 hrs · 44,808 cycles
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
Part: NONE — INOPERATIVE (PAX CABIN) · airframe 75,955 hrs · 44,746 cycles
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.
Part: NONE — OUT OF POSITION (FWD SERVICE DOOR) · airframe 75,629 hrs · 44,528 cycles
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
Part: PANEL — DELAMINATED (FUSELAGE) · airframe 75,476 hrs · 44,418 cycles
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.
Part: O-RING — LEAKING (#2 ENGINE) · airframe 75,310 hrs · 44,297 cycles
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.
Part: SELECTOR VALVE — LEAKING (#2 ENGINE) · airframe 75,310 hrs · 44,297 cycles
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.
Part: SELECTOR VALVE — LEAKING (#2 ENGINE) · airframe 75,310 hrs · 44,297 cycles
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.
Part: LIGHT — LOOSE (CABIN) · airframe 75,053 hrs · 44,128 cycles
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.
Part: LIGHT — FAILED · airframe 74,339 hrs · 43,670 cycles
FWD OVERHEAD EXIT SIGN FELL OFF / [01] SECURED LENS PER SIP/AMM 33-51-01. OK FOR SERVICE
2021
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 73,634 hrs · 43,227 cycles
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
Part: SHOCK MOUNT — BROKEN (R1 DOOR) · airframe 73,634 hrs · 43,227 cycles
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
Part: GUSSET — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: GUSSET — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: WEB — CORRODED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 73,634 hrs · 43,227 cycles
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
Part: ACCESS PANEL — CRACKED (R/H WING) · airframe 73,634 hrs · 43,227 cycles
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
Part: STRINGER — CRACKED (L/H WING) · airframe 73,634 hrs · 43,227 cycles
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.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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
Part: NONE — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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
Part: ACCESS PANEL — CRACKED (L/H WING) · airframe 73,634 hrs · 43,227 cycles
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
Part: RIB — CRACKED (VERTICAL STAB) · airframe 73,634 hrs · 43,227 cycles
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.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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
Part: NONE — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: PLATE — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: PLATE — BROKEN (R/H WING) · airframe 73,634 hrs · 43,227 cycles
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
Part: PLATE — BROKEN (R/H WING) · airframe 73,634 hrs · 43,227 cycles
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.
Part: BRACKET — BROKEN (L/H WING) · airframe 73,634 hrs · 43,227 cycles
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
Part: ANGLE — BROKEN (R/H WING) · airframe 73,634 hrs · 43,227 cycles
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
Part: ACCESS PANEL — CRACKED (L/H WING) · airframe 73,634 hrs · 43,227 cycles
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.
Part: ACCESS PANEL — CRACKED (L/H WING) · airframe 73,634 hrs · 43,227 cycles
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.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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
Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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
Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 73,634 hrs · 43,227 cycles
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.
Part: VAPOR BARRIER — CRACKED (CENTER WING) · airframe 73,634 hrs · 43,227 cycles
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
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 73,634 hrs · 43,227 cycles
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.
Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 73,634 hrs · 43,227 cycles
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.
Part: LIGHT — DETERIORATED (CABIN) · airframe 73,634 hrs · 43,227 cycles
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
Part: CIRCUIT BREAKER — POPPED (FUSELAGE) · airframe 73,559 hrs · 43,186 cycles
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.
Part: BATTERY PACK — FAILED (CABIN)
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
Part: NONE — FAILED (CABIN) · airframe 73,552 hrs · 43,181 cycles
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
Part: SUPPORT — CRACKED (R/H WING)
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
Part: SLIDE — LOOSE (R2 DOOR) · airframe 72,557 hrs · 42,556 cycles
AFT SERVICE DOOR SLIDE LOOSE. ; / [01] REPACKED AFT SERVICE DOOR ESCAPE SLIDE IAW MT 725-61-06. A/C OK FOR SERVICE.
Part: STRAP — BROKEN (FLASHLIGHT ASSY) · airframe 72,136 hrs · 42,322 cycles
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
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 71,323 hrs · 41,859 cycles
APPEARANCE TECHS REPORT L1 DOOR SLIDE HAS COME OUT OF ITS HOLDER. REPACKED L1 DOOR SLIDE PER MT 725-61-06.
2020
Part: SLIDE — MISINSTALLED (L2 DOOR) · airframe 70,353 hrs · 41,281 cycles
AFT ENTRY DOOR ESCAPE SLIDE IS NOT PACKED CORRECTLY. / REPACKED AFT ENTRY DOOR ESCAPE SLIDE PER MT 725-61-06
2019
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 69,189 hrs · 40,548 cycles
L1 DOOR EMERGENCY EXIT LIGHT LENS WOULD NOT STAY ON. INSTALLED NEW LENS IAW SIP AND AMM.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,182 hrs · 40,542 cycles
FORWARD SERVICE DOOR UPPER EMERGENCY LIGHT ASSEMBLY WOULD NOT ILLUMINATED. R&R M1675 EMERGENCY LIGHT POWER SUPPLY PER AMM.
Part: DOOR SILL — DAMAGED (FWD CARGO BAY) · airframe 69,092 hrs · 40,476 cycles
FWD CARGO DOOR CENTER SCUFF PLATE IS DAMAGED. / REMOVED AND REPLACED REF AMM 53-11-02.
Part: BATTERY PACK — FAILED (CABIN) · airframe 69,042 hrs · 40,446 cycles
EMERGENCY LIGHT BATTERY PACK AT POSITION M1668 FAILED OPERATIONAL TEST. / R&R BATTERY PACK IAW AMM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,042 hrs · 40,446 cycles
INTERCOSTAL CRACKED BETWEEN BS. 328 TO BS. 344, LBL 45. / R&R INTERCOSTAL PER SRM AND DWG.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 69,042 hrs · 40,446 cycles
FLOOR BEAM UPPER CHORD CRACKED AT BS. 328, RBL 23. / REPAIRED CHORD IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,042 hrs · 40,446 cycles
INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, LBL 45. / R&R INTERCOSTAL PER SRM AND DWG.
Part: STRAP — CRACKED (FUSELAGE) · airframe 69,042 hrs · 40,446 cycles
FLOOR BEAM LOWER CHORD STABILIZER STRAP CRACKED BETWEEN BS. 312 TO BS. 328, RBL 30. / REPAIRED STRAP PER SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,042 hrs · 40,446 cycles
INTERCOSTAL CRACKED BETWEEN BS. 294.5+5 TO BS. 312, RBL 15. / R&R INTERCOSTAL PER SRM AND DWG.
Part: INTERCOSTAL — CRACKED (CABIN) · airframe 69,042 hrs · 40,446 cycles
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
Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,042 hrs · 40,446 cycles
AFT PRESSURE BULKHEAD HOLE BOLT 9L OUT OF TOLERANCE AT BS. 1016, STR. 3L. / REPAIRED BULKHEAD IAW SOUTHWEST SPECIAL ITEM.
Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,042 hrs · 40,446 cycles
AFT PRESSURE BULKHEAD BOLT 9R HOLE OUT OF TOLERANCE AT BS. 1016, STR. 3R. / REPAIRED BULKHEAD IAW SOUTHWEST SPECIAL ITEM.
Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,042 hrs · 40,446 cycles
AFT PRESSURE BULKHEAD BOLT 8R HOLE OUT OF TOLERANCE AT BS. 1016, STR. 3R. / REPAIRED BULKHEAD IAW SOUTHWEST SPECIAL ITEM.
Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,042 hrs · 40,446 cycles
AFT PRESSURE BULKHEAD BOLT 7R HOLE OUT OF TOLERANCE AT BS. 1016, STR. 3R. / REPAIRED BULKHEAD IAW SOUTHWEST SPECIAL ITEM.
Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 69,042 hrs · 40,446 cycles
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
Part: BULKHEAD WEB — CORRODED (BS 1016) · airframe 69,042 hrs · 40,446 cycles
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.
Part: LIGHT — NO TEST (SEAT ROW 11) · airframe 69,042 hrs · 40,446 cycles
L/H EMERGENCY LIGHT FAILED TEST AT SEAT ROW 11. / R&R LIGHT ASSEMBLY IAW AMM.
Part: FRAME — CRACKED (BS 1016 BULKHEAD) · airframe 69,042 hrs · 40,446 cycles
FRAME BOLT HOLE 8L OUT OF TOLERANCE AT BS. 1016, STR. 3L. / REPAIRED FRAME IAW SOUTHWEST SPECIAL ITEM.
Part: FRAME — OUT OF TOLERANCE (BS 1016 BULKHEAD) · airframe 69,042 hrs · 40,446 cycles
FRAME BOLT HOLE 7L OUT OF TOLERANCE AT BS. 1016, STR 3L. / REPAIRED FRAME IAW SOUTHWEST SPECIAL ITEM.
Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 69,042 hrs · 40,446 cycles
WHEEL WELL VAPOR BARRIER FORWARD SIDE SUPPORT ANGLE CRACKED AT BS. 663, RBL 6. / R&R ANGLE IAW SRM.
Part: SKIN — CORRODED (BS 1016-1040) · airframe 69,042 hrs · 40,446 cycles
PRESSURE BULKHEAD WEB CORRODED BETWEEN BS. 1016 TO BS. 1040, BETWEEN STR. 24L TO STR. 25R, LOWER AREA. / REPAIRED SKIN PER EA.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,042 hrs · 40,446 cycles
R/H HORIZONTAL STABILIZER INSPAR #4 RIB #4 STIFFENER CRACKED. / REPAIRED RIB IAW SRM.
Part: CHANNEL — CORRODED (AFT CARGO COMPT) · airframe 69,042 hrs · 40,446 cycles
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.
Part: ANGLE — CORRODED (BS 350-360) · airframe 69,042 hrs · 40,446 cycles
ANGLE CORRODED BETWEEN BS. 350 TO BS. 360, STR. 27L. / R&R ANGLE PER DWG AND SRM.
Part: WEB — CORRODED (BS 807-827) · airframe 69,042 hrs · 40,446 cycles
INTERCOSTAL WEB CORRODED AT BETWEEN BS. 807 TO BS. 827, STR. 27R. / R&R WEB PER SRM AND DWG.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 69,042 hrs · 40,446 cycles
R/H HORIZONTAL STABILIZER INSPAR #4 RIB #4 STIFFENER CRACKED. / REPAIRED STIFFENER IAW SRM.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 69,042 hrs · 40,446 cycles
AFT CARGO LEFT SIDE "Z" CHANNEL CORRODED BETWEEN BS. 727C TO BS. 807. / R&R "Z" CHANNEL PER SRM AND DWG.
Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 69,042 hrs · 40,446 cycles
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)
Part: BULKHEAD WEB — CORRODED (BS 1016) · airframe 69,042 hrs · 40,446 cycles
AFT PRESSURE WEB WAS HEAVILY CORRODED AT BS. 1016, BETWEEN LBL 7 TO RBL 7. / REPAIRED WEB PER EA.
Part: BULKHEAD — DAMAGED (BS 1016) · airframe 69,042 hrs · 40,446 cycles
AFT PRESSURE BULKHEAD BOLT HOLE 6R OUT OF TOLERANCE AT BS. 1016, STR. 2R. / REPAIRED BULKHEAD IAW SI.
Part: BULKHEAD — DAMAGED (BS 1016) · airframe 69,042 hrs · 40,446 cycles
AFT PRESSURE BULKHEAD BOLT 5R HOLE OUT OF TOLERANCE AT BS. 1016, STR. 2R. / REPAIRED PRESSURE BULKHEAD IAW SI.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 69,042 hrs · 40,446 cycles
R/H HORIZONTAL STABILIZER INSPAR #4 RIB ASSEMBLY, #3 STIFFENER CRACKED. / REPAIRED #3 STIFFENER IAW SRM.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,042 hrs · 40,446 cycles
R/H HORIZONTAL STABILIZER INSPAR #4 RIB ASSEMBLY, #3 STIFFENER CRACKED. / REPAIRED #4 RIB IAW SRM.
Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,042 hrs · 40,446 cycles
AFT PRESSURE BULKHEAD BOLT HOLE 5L OUT OF TOLERANCE AT BS. 1016, STR. 2L. / REPAIRED BULKHEAD IAW SI.
Part: NONE — CORRODED (CABIN) · airframe 69,042 hrs · 40,446 cycles
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
Part: BULKHEAD — OUT OF TOLERANCE (BS 1016) · airframe 69,042 hrs · 40,446 cycles
AFT PRESSURE BULKHEAD BOLT 6L HOLE OUT OF TOLERANCE AT STA 1016, STR. 2L. / REPAIRED FASTENER HOLE IAW SI.
Part: PANEL — CRACKED (VERTICAL STABILI) · airframe 69,042 hrs · 40,446 cycles
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
Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 69,042 hrs · 40,446 cycles
DENT ON FLIGHT DECK FLOOR APPROXIMATELY BS 260, LBL12. / REMOVED DAMAGE AND PERFORMED REPAIR IAW EA # 1-A53-33179.
Part: FLAP — CRACKED (LEFT WING) · airframe 69,042 hrs · 40,446 cycles
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
Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 69,042 hrs · 40,446 cycles
VAPOR WEB FORWARD FACE ANGLE CRACKED AT BS. 633, LBL 15. / R&R ANGLE PER SRM AND DWG.
Part: TRUNNION — CORRODED (RIGHT WING) · airframe 68,571 hrs · 40,141 cycles
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
Part: TRUNNION — CORRODED (LEFT WING) · airframe 68,571 hrs · 40,141 cycles
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
Part: TRUNNION — CORRODED (RIGHT WING) · airframe 68,571 hrs · 40,141 cycles
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
Part: TRUNNION — CORRODED (RIGHT WING) · airframe 68,571 hrs · 40,141 cycles
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
Part: TRUNNION — CORRODED (LEFT WING) · airframe 68,571 hrs · 40,141 cycles
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
Part: TRUNNION — CORRODED (LEFT WING) · airframe 68,571 hrs · 40,141 cycles
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
Part: TRUNNION — CORRODED (LEFT WING) · airframe 68,571 hrs · 40,141 cycles
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
Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,502 hrs · 40,096 cycles
L/H EMERGENCY EXIT DOOR LIGHT INOP. R&R LIGHT PER MM.
Part: STRAP — BROKEN (AFT FLASHLIGHT) · airframe 67,862 hrs · 39,693 cycles
L/H AFT FLASHLIGHT STRAP BROKEN. R&R STRAP PER MM.
Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 67,241 hrs · 39,298 cycles
R/H MIDDLE FORWARD OF R/H EMERGENCY EXIT DOOR, EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. / R&R BATTERY PER AMM.
Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 67,241 hrs · 39,298 cycles
L/H AFT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. / R&R BATTERY PER AMM.
Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 67,241 hrs · 39,298 cycles
L/H FORWARD EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. / R&R BATTERY PER AMM.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,241 hrs · 39,298 cycles
R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.
2018
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 66,376 hrs · 38,740 cycles
LT EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER AMM.
Part: CRADLE — DEFECTIVE (CABIN) · airframe 66,376 hrs · 38,740 cycles
RT EMERGENCY EXIT LIGHT INOP. R&R BATTERY CRADLE PER AMM.
Part: CRADLE — DEFECTIVE (CABIN) · airframe 66,376 hrs · 38,740 cycles
RT EMERGENCY EXIT LIGHT INOP. R&R BATTERY CRADLE PER AMM.
Part: ANGLE — WORN (VERTICAL STAB) · airframe 63,041 hrs · 36,603 cycles
RT VERTICAL STABILIZER ATTACH SKATE ANGLE WORN ON THE VERTICAL FLANGE, AT STA 1119, BELOW ACCESS PANEL 323CR. REPAIRED ANGLE PER SRM.
2017
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 62,871 hrs · 36,499 cycles
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
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 62,871 hrs · 36,499 cycles
LEFT HORIZONTAL STABILIZER LEADING EDGE RIB UPPER AFT FASTENER HOLE CRACKED AT BS 95.96. R & R RIB IAW DWG AND SRM.
Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 62,871 hrs · 36,499 cycles
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
Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 62,871 hrs · 36,499 cycles
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
Part: NONE — CORRODED (AFT CARGO COMPT) · airframe 62,871 hrs · 36,499 cycles
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.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,871 hrs · 36,499 cycles
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
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
RT OUTBOARD SEAT TRACK CROWN CORRODED BETWEEN BS 701 TO BS 724. R&R SEAT TRACK IAW SRM.
Part: SPLICE — CORRODED (AFT CARGO) · airframe 62,871 hrs · 36,499 cycles
AFT CARGO BAY FLOOR PANEL SPLICE CORRODED AT BS 767. R & R PANEL SPLICE IAW SRM & DWG.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
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
Part: TRACK — CORRODED (CABIN) · airframe 62,871 hrs · 36,499 cycles
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.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,871 hrs · 36,499 cycles
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
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
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.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,871 hrs · 36,499 cycles
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.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 62,871 hrs · 36,499 cycles
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
Part: NONE — CORRODED (AFT CARGO COMPT) · airframe 62,871 hrs · 36,499 cycles
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.
Part: FLOOR PANEL — BROKEN (CABIN) · airframe 62,871 hrs · 36,499 cycles
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
Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 62,871 hrs · 36,499 cycles
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
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
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
Part: FLOOR PANEL — CORRODED (BS 727D) · airframe 62,871 hrs · 36,499 cycles
AFT CARGO COMPARTMENT FLOOR PANEL SPLICE CORRODED AT BS 727D. / R&R PANEL SPLICE IAW BOEING DWG.
Part: STIFFENER — CORRODED (FED THRESHOLD) · airframe 62,871 hrs · 36,499 cycles
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
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
T-CAP CORRODED AT BS 986.5, BETWEEN LBL 21 TO LBL 45. REPAIRED T-CAP IAW SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
LT OUTBOARD SEAT TRACK CROWN CORRODED BETWEEN BS 500D+10 TO BS 520. REPAIRED SEAT TRACK IAW SRM AND EA.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
INTERCOSTAL CRACKED BETWEEN BS 308 TO BS 328, RBL 32. R&R INTERCOSTAL IAW SRM & DWG.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
L1 ENTRANCE INBOARD CREASE BEAM CORRODED BETWEEN BS 308 TO BS 328. R&R CREASE BEAM IAW SRM AND DWG.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
AFT WET AREA RT CREASE BEAM INNER CHORD CORRODED BETWEEN BS 945 TO BS 992.8. R&R CREASE BEAM IAW SRM AND DWG.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
LT INBOARD SEAT TRACK CROWN CORRODED BETWEEN BS 500D+16 TO BS 520. REPAIRED SEAT TRACK IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
CABIN FORWARD WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL IAW SRM AND DWG.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
INTERCOSTAL STRUCTURE CORRODED BETWEEN BS 986.5 TO BS 1006, RBL 38. R&R INTERCOSTAL IAW DWG AND SRM.
Part: STIFFENER — CORRODED (FED THRESHOLD) · airframe 62,871 hrs · 36,499 cycles
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-
Part: ANGLE — CORRODED (BS 777) · airframe 62,871 hrs · 36,499 cycles
AFT CARGO BAY ZEE ANGLE CORRODED AT BS 777, LT SIDE. REPAIRED THE ANGLE IAW SRM.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
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
Part: ANGLE — CORRODED (BS 727E) · airframe 62,871 hrs · 36,499 cycles
AFT CARGO COMPARTMENT ZEE ANGLE CORRODED BETWEEN BS 727E & 727E +5, LT SIDE. REPAIRED THE ANGLE IAW SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
AFT CARGO COMPARTMENT FLOOR PANEL NUT PLATES CORRODED AT BS 727D +5, BETWEEN LBL 12 TO RBL 12. REPAIRED FLOORBEAM IAW EA AND AMM.
Part: PANEL — CORRODED (AFT CARGO COMPT) · airframe 62,871 hrs · 36,499 cycles
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
Part: FLOOR SUPPORT — CORRODED (BS 727C) · airframe 62,871 hrs · 36,499 cycles
AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS. 727C+6, STR. 3R. R & R THE FLOOR SUPPORT IAW SRM.
Part: BRACKET — BROKEN (AED THRESHOLD) · airframe 62,871 hrs · 36,499 cycles
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:-
Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 62,871 hrs · 36,499 cycles
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
Part: ANGLE — CORRODED (BS 761-765) · airframe 62,871 hrs · 36,499 cycles
AFT CARGO COMPARTMENT ZEE ANGLE CORRODED BETWEEN BS 761 TO 765, LT SIDE. REPAIRED THE ANGLE IAW SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
AFT CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 794 TO BS 810, RBL 14. REPAIRED FLOOR TRACK IAW SRM, EA, & DWG.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 62,871 hrs · 36,499 cycles
FORWARD CARGO COMPARTMENT RT ZEE ANGLE CORRODED BETWEEN BS 500A TO BS 500D. REPAIRED ZEE ANGLE IAW SRM.
Part: FITTING — CRACKED (AFT CARGO COMPT) · airframe 62,871 hrs · 36,499 cycles
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
Part: ANGLE — CORRODED (BS 867-902) · airframe 62,871 hrs · 36,499 cycles
AFT CARGO BAY ZEE ANGLE CORRODED BETWEEN BS 867 TO 902, RBL 21. R & R THE ANGLE IAW SRM.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,871 hrs · 36,499 cycles
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
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,871 hrs · 36,499 cycles
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
Part: PLATE — CRACKED (LT WING) · airframe 62,871 hrs · 36,499 cycles
LT WING TRAILING EDGE WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,871 hrs · 36,499 cycles
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
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 62,871 hrs · 36,499 cycles
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
Part: PLATE — CRACKED (RT WING) · airframe 62,871 hrs · 36,499 cycles
RT WING TRAILING EDGE CAVITY 2" INBOARD OF SAILTAIL WAFFLE PLATE CRACKED. R&R WAFFLE PLATE IAW SRM.
Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 62,871 hrs · 36,499 cycles
LT MAIN WHEEL WELL HORIZONTAL PRESSURE DECK CRACKED AT BS 663, LBL 32. REPAIRED DECK IAW EA.
Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 62,871 hrs · 36,499 cycles
RT MAIN WHEEL WELL HORIZONTAL PRESSURE DECK CRACKED AT BS 663, RBL 41. REPAIRED WEB IAW EA.
Part: COVER — LOOSE (L1 DOOR) · airframe 622,357 hrs · 36,181 cycles
L1 DOOR EMERGENCY EVAC SLIDE PULL HANDLE COVER LOOSE. SECURED COVER IAW AMM.
Part: COVER — LOOSE (R2 DOOR) · airframe 622,357 hrs · 36,181 cycles
R2 DOOR EMERGENCY EVAC SLIDE PULL HANDLE COVER LOOSE. SECURED COVER IAW AMM.
Part: COVER — LOOSE (L2 DOOR) · airframe 622,357 hrs · 36,181 cycles
L2 DOOR EMERGENCY EVAC SLIDE PULL HANDLE COVER LOOSE. SECURED COVER IAW AMM.
Part: ENGINE — FAILED (LEFT) · airframe 61,380 hrs · 35,593 cycles
DIVERSION, INFLIGHT SHUTDOWN, DECLARED EMERGENCY. NR 2 ENGINE FAILURE AT FL 410 CRUISE INCAPABLE OF RESTART. R&R NR 2 ENGINE IAW MT.
2016
Part: HOOK — LOOSE (L2 DOOR) · airframe 59,676 hrs · 34,592 cycles
L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED HOOKS PER SIP.
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 59,228 hrs · 34,308 cycles
L1 DOOR EMERGENCY EVAC SLIDE GIRT OUT OF ADJUST. ADJUSTED SLIDE PER MT.
Part: SLIDE — LOOSE (L2 DOOR) · airframe 58,618 hrs · 33,955 cycles
L2 DOOR EMERGENCY EVACUATION SLIDE FOUND LOOSE. SECURED THE SLIDE IAW MM AND MT.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,103 hrs · 33,660 cycles
RIGHT WING OVERWING EMERGENCY EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.
2015
Part: LIGHT — BROKEN (CABIN) · airframe 56,373 hrs · 32,661 cycles
AFT GALLEY AREA, EMER EXIT LIGHT ASSEMBLY BROKEN ON GALLEY 4. R & R LIGHT ASSEMBLY IAW AMM.
Part: SKIN — CRACKED (RT WING) · airframe 56,373 hrs · 32,661 cycles
RIGHT WING SKIN, CRACKED AT FASTENER HOLE INBD OF RIB 10. REPAIRED SKIN IAW SRM & DWG.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FORWARD BULKHEAD WEB CRACKED AT BS 663.75 OF LT AT AIR CONDITIONING BAY. REPAIRED WEB IAW EA.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
UPPER SUPPORT ON ANGLE CRACKED AT BS 663.75, LBL 8. REPLACED ANGLE IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 907, STRINGER 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 727B, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 907, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
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.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 787, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
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.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
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.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
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.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
SEAT TRACK FLOORBEAM CRACKED AT BS 727A+18.5, LBL 45.5, OTBD FLANGE, AFT FASTENER HOLE NR 10 HOLE. REPAIRED FLOORBEAM IAW EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
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.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
SEAT TRACK FLOORBEAM CRACKED AT BS 727A+18.5, LBL 45.5, INBD FLANGE AFT FASTENER HOLE NR 8, HOLE UPPER CHORD HORIZONTAL FLANGES.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
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.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
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.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
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.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
SEAT TRACK CRACKED AT BS 727B, LBL 22.75 FASTENER HOLE NR 1 ON CROSSBEAM FLANGE. REPAIRED FLANGE IAW EA.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
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.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
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.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B, RBL 45.57 FASTENER HOLE NR 2. REPAIRED SEAT TRACK IAW EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
SEAT TRACK CROSSBEAM FLANGE CRACKED AT BS 727B, LBL 45.5, FASTENER HOLE NR 3. REPAIRED FLOORBEAM IAW EA.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
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.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
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.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 907, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 520, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 520, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 787, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 500C, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 500A, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 440, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 400, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 500C, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 480, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 480, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: LENS — BROKEN (CABIN) · airframe 56,373 hrs · 32,661 cycles
AFT GALLEY EMER EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FRAME CRACKED AT BS 827, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,373 hrs · 32,661 cycles
VERTICAL PRESS WEB CRACKED AT BS 663, RBL 35. REPAIRED WEB IAW SRM.
Part: FLAP TRACK — DELAMINATED (TE FLAP) · airframe 56,373 hrs · 32,661 cycles
LEFT WING NR 3 FLAP TRACK INTERNAL SURFACE DELAMINATED. REPAIRED FLAP TRACK IAW EA & SRM.
Part: SKIN — DELAMINATED (FLAP FAIRING) · airframe 56,373 hrs · 32,661 cycles
RIGHT WING NR 6 FLAP TRACK FAIRING INTERNAL SURFACE DELAMINATED. REPAIRED FAIRING IAW EA & SRM.
Part: SKIN — CRACKED (LE SLAT) · airframe 56,373 hrs · 32,661 cycles
RIGHT WING NR 6 SLAT SKIN CRACKED ON LOWER SURFACE. REPAIRED SKIN IAW SRM.
Part: BATTERY — FAILED (CABIN) · airframe 55,256 hrs · 32,003 cycles
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATIONS M1673. R & R BATTERY IAW AMM.
Part: BATTERY — FAILED (CABIN) · airframe 55,256 hrs · 32,003 cycles
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATIONS M1670. R & R BATTERY IAW AMM.
Part: BATTERY — FAILED (CABIN) · airframe 55,256 hrs · 32,003 cycles
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATIONS M1672. R & R BATTERY IAW AMM.
Part: BATTERY — FAILED (CABIN) · airframe 55,256 hrs · 32,003 cycles
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATIONS M1675. R & R BATTERY IAW AMM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 56,373 hrs · 32,661 cycles
FORWARD LOWER SIDE LIP, EXTERNAL POWER DOOR CUT OUT CRACKED. REPAIRED CUT OUT IAW EA.
Part: LENS — MISSING (EXIT SIGN) · airframe 55,208 hrs · 31,978 cycles
RIGHT LOWER OVERWING EXIT SIGN LENS MISSING. INSTALLED LENS IAW AMM.
2014
Part: BATTERY — FAILED (CABIN) · airframe 50,639 hrs · 29,425 cycles
EMERGENCY EXIT LIGHT BATTERY FAILED TEST AT ROW 17. R & R BATTERY IAW AMM.
2013
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 49,958 hrs · 29,028 cycles
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.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,958 hrs · 29,028 cycles
FRAME WEB CRACKED AT BS 747, STRINGER 8R. REPAIRED WEB IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,958 hrs · 29,028 cycles
FRAME WEB CRACKED AT BS 727D, STRINGER 8R. REPAIRED WEB IAW EA.
Part: SKIN — CRACKED (LE SLAT) · airframe 49,958 hrs · 29,028 cycles
LT WING NR 1 SLAT LOWER LE SLAT NOSE SKIN AT ACTUATOR, INBD SKIN CRACKED AT FASTENER. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (LE SLAT) · airframe 49,958 hrs · 29,028 cycles
LT WING LOWER LE NR 3 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,958 hrs · 29,028 cycles
FLIGHT DECK LT NR 1 WINDOW FRAME SKIN CUTOUT CRACKED. REPAIRED FRAME IAW ACO. CORRECTED ATA, DESCRIPTION, PART NAME & PART DEFECT LOCAL.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,958 hrs · 29,028 cycles
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.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 49,865 hrs · 28,980 cycles
FLIGHT DECK RT NR 3 WINDOW FRAME CRACKED IN 2ND FROM BOTTOM FASTENER HOLE ON FWD SIDE OF FRAME. REPAIRED FRAME IAW SWA EA.
Part: LENS — BROKEN (L1 DOOR) · airframe 46,809 hrs · 27,170 cycles
EMERGENCY EXIT LENS BROKEN AFT ENTRY DOOR. REMOVED AND REPLACED AFT ENTRY DOOR EMERGENCY EXIT LIGHTT ASSY PER M/M.
2012
Part: SLIDER — CRACKED (RT HORIZ STAB) · airframe 46,216 hrs · 26,784 cycles
RIGHT FWD LOWER HORIZONTAL STAB SLIDER CRACKED. REPLACED RIGHT FWD LOWER STAB SLIDER REF AMM.
Part: MECHANISM — DAMAGED (EVAC SLIDE) · airframe 45,039 hrs · 26,023 cycles
R1 DOOR EMERGENCY EVAC SLIDE LOCK MECHANISM DAMAGED. REMOVED AND REPLACED SLIDE PER M/M.
Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 43,730 hrs · 25,273 cycles
R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE OUT OF LIMIT. REMOVED AND REPLACED SLIDE PER MT.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,192 hrs · 24,962 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,192 hrs · 24,962 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME IAW EA.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,192 hrs · 24,962 cycles
DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 47. REPAIRED BEAM IAW EA.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,192 hrs · 24,962 cycles
DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BETWEEN LBL 47 TO RBL 47. REPAIRED BEAM IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,192 hrs · 24,952 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME IAW EA.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,192 hrs · 24,962 cycles
DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 706 TO BS 727, RBL 63. REPAIRED BEAM IAW ER.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,192 hrs · 24,962 cycles
DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,192 hrs · 24,962 cycles
DURING SCHEDULED 12Y CHECK, FOUND STUB FRAME CRACKED AT BS 296, STR 17R. REMOVED AND REPLACED FRAME PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,192 hrs · 24,962 cycles
DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 47. REPAIRED BEAM IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,192 hrs · 24,962 cycles
DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,192 hrs · 24,962 cycles
DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, BL 11. REPAIRED BEAM IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,192 hrs · 24,962 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.
2011
Part: RETAINER — LOOSE (GIRT BAR) · airframe 40,511 hrs · 23,365 cycles
DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER LOOSE. SECURED RETAINER PER MM.
Part: HOUSING — FAULTY (CABIN) · airframe 39,746 hrs · 22,938 cycles
DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED SIGN HOUSING PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 39,625 hrs · 22,863 cycles
DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,697 hrs · 22,905 cycles
LT OVERHEAD EMERGENCY EXIT SIDEWALL LIGHT INOP. REPAIRED LIGHT PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,470 hrs · 22,197 cycles
DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,045 hrs · 21,381 cycles
DURING SCHEDULED 10Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 4. REMOVED AND REPLACED BULB PER MM.
Part: FLAP — DELAMINATED (RT WING) · airframe 37,045 hrs · 21,381 cycles
DURING SCHEDULED 10Y CHECK, FOUND RT WING O/B AFT FLAP I/B TRAILING EDGE DELAMINATED. REPAIRED AFT FLAP PER SRM.
Part: STRUCTURE — CORRODED (COCKPIT) · airframe 37,045 hrs · 21,381 cycles
DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR CORRODED AT BS 270. REPAIRED FLOOR PER SRM & EA.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,045 hrs · 21,381 cycles
DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767, LBL 7.5. REPAIRED BEAM PER EA.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,045 hrs · 21,381 cycles
DURING SCHEDULED 10Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 22. RELAMPED LIGHT PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,045 hrs · 21,381 cycles
DURING SCHEDULED 10Y CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 6. RELAMPED LIGHT PER MM.
2009
Part: BATTERY PACK — FAILED (CABIN) · airframe 35,316 hrs · 20,303 cycles
DURING SCHEDULED HC2, LT FWD BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: FITTING — CORRODED (LT WING) · airframe 35,232 hrs · 20,251 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER SWA EA.
Part: FITTING — CORRODED (RT WING) · airframe 35,232 hrs · 20,251 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER SWA EA.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,971 hrs · 18,879 cycles
DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.
2008
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,447 hrs · 18,570 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
Part: SLIDE — LOOSE (DOOR) · airframe 31,776 hrs · 18,155 cycles
FOUND R1 DOOR EMERGENCY ESCAPE SLIDE LOOSE. REMOVED AND REPLACED SLIDE PER MM.
Part: SLIDE — LOOSE (DOOR) · airframe 31,749 hrs · 18,137 cycles
R1 EMERGENCY EXIT DOOR SLIDE LOOSE. REMOVED AND REPLACED SLIDE PER MM.
Part: SKIN — CRACKED (HORIZ STAB) · airframe 30,518 hrs · 17,391 cycles
DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM.
Part: LIGHT — BROKEN (CABIN) · airframe 29,782 hrs · 16,960 cycles
R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,565 hrs · 16,822 cycles
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 35 TO RBL 45. REPAIRED FLOORBEAM PER SWA EA.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,565 hrs · 16,822 cycles
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 53. REPAIRED FLOORBEAM PER SWA EA.
2007
Part: PUMP — FAILED (NR 2 ENGINE) · airframe 28,027 hrs · 15,896 cycles
DIVERSION, HYDRAULIC B-SYSTEM FAILURE. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP PER MM.
Part: LENS — LOOSE (L1 DOOR) · airframe 27,294 hrs · 15,480 cycles
L1 DOOR EMERGENCY EVAC SLIDE VIEWING LENS LOOSE. SECURED SLIDE LENS PER MM.
Part: BEARING — FAILED (LT MLG) · airframe 26,471 hrs · 15,032 cycles
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.
Part: COVER — BROKEN (CABIN) · airframe 26,075 hrs · 14,815 cycles
R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
2006
Part: BATTERY — FAILED (CABIN) · airframe 23,237 hrs · 13,192 cycles
DURING SCHEDULED HC1 CHECK, OVERWING LT EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 23,237 hrs · 13,192 cycles
DURING SCHEDULED HC1 CHECK, SEAT ROW 16 EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 23,237 hrs · 13,192 cycles
DURING SCHEDULED HC1 CHECK, ROW AFT LT EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 23,237 hrs · 13,192 cycles
DURING SCHEDULED HC1 CHECK, OVERWING RT EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 23,237 hrs · 13,192 cycles
DURING SCHEDULED HC1 CHECK, FWD LT EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 23,237 hrs · 13,192 cycles
DURING SCHEDULED HC1 CHECK, ROW AFT RT EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
2005
Part: FLOOR SUPPORT — CRACKED (AFT CARGO BAY) · airframe 18,831 hrs · 10,695 cycles
DURING SCHEDULED 5Y CHECK, FOUND 2 EA LONGITUDINAL FLOORBEAM CRACKS AT BS 773, LBL 12 & RBL 3. REPAIRED BEAMS PER SRM.
Part: SLIDE — DISLODGED (L1 DOOR) · airframe 18,561 hrs · 10,539 cycles
L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. RE-INSTALLED SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 18,465 hrs · 10,488 cycles
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REINSTALLED SLIDE PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,281 hrs · 10,383 cycles
FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.
2004
Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 16,734 hrs · 9,502 cycles
LEFT FWD EEPLS HAS WIRES EXPOSED. REMOVED AND REPLACED EEPLS COVER PER MM.
Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 15,622 hrs · 8,885 cycles
L1 DOOR EVAC SLIDE DEPLOYED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE PER MM.
2003
Part: BALL — LOOSE (CABIN) · airframe 13,573 hrs · 7,696 cycles
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.
Part: MASK — TORN (CABIN) · airframe 13,573 hrs · 7,696 cycles
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.
2002
Part: BUSHING — WORN (LT ELEVATOR) · airframe 9,118 hrs · 5,179 cycles
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.
Part: BUSHING — WORN (RT ELEVATOR) · airframe 9,118 hrs · 5,179 cycles
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.
Part: COVER — CRACKED (CABIN) · airframe 8,950 hrs · 5,073 cycles
DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED THROUGH OUT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.
Part: PUMP — FAILED (HYD SYSTEM) · airframe 7,272 hrs · 4,157 cycles
AIR TURNBACK, A-SYSTEM, ELECTRIC HYD PUMP FAILURE. REMOVED AND REPLACED A-SYSTEM HYD PUMP AND CASE DRAIN FILTER PER MM.
2001
Part: BATTERY — DISCHARGED (CABIN) · airframe 5,675 hrs · 3,285 cycles
DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT LT SIDEWALL. REMOVED AND REPLACED BATTERY PER MM.
Part: COVER — CRACKED (CABIN) · airframe 5,409 hrs · 3,136 cycles
DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT SEVERAL LOCATIONS IN CABIN. R & R TRACK COVERS PER MM.
Part: FAN BLADE — OUT OF TOLERANCE (NR 2 ENGINE) · airframe 4,140 hrs · 2,418 cycles
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.
Part: SLIDE — DETACHED (AFT SERVICE DOOR) · airframe 2,724 hrs · 1,622 cycles
AFT SVC DOOR EMERGENCY EVAC SLIDE ASSY FELL OUT OF CONTAINER. REINSTALLED EVAC SLIDE ASSY PER MM.
2000
Part: FLAP — CRACKED (LT WING) · airframe 2,358 hrs · 1,416 cycles
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
Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 2,032 hrs · 1,232 cycles
DURING SCHEDULED C2 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED GIRT ASSY PER MM.
Part: SLIDE — MISINSTALLED (SERVICE DOOR) · airframe 285 hrs · 188 cycles
FWD SERVICE DOOR EVACUATION SLIDE NOT STOWED PROPERLY. REINSTALLED SLIDE ASSY PER MM.