N8575Z
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
35 reports on file, 2018-06-14 – 2026-08-21.
Part: FIRE LOOP — INOPERATIVE (ZONE 400) · airframe 27,256 hrs · 14,085 cycles
NR 1 ENGINE, FIRE DETECTOR LOOP B INOPERATIVE. OK TO CONTINUE IAW MEL 26-2-01 XB. NR 1 ENGINE 34B& 34 LOOPS, ENGINE OVERHEAT & FIRE DETECTION SYS . PERFORMED AN OPS TEST OF NR1 ENGINE FIRE DETECTOR LOOP B IAW AMM 26-11-00. OPS CHECKED GOOD.
Part: BUSHING — MISSING (GIRT BAR) · airframe 27,080 hrs · 13,991 cycles
FWD SERVICE DOOR GIRT BAR BUSHING FELL OFF. REINSTALLED BUSHING IAW AMM 25-66-01. A/C OK FOR SERVICE.
Part: TABLE — OUT OF LIMITS (ZONE 200) · airframe 26,798 hrs · 13,845 cycles
TRAY TABLES ON SEAT BACKS OF PAX SEATS 14C; 14B; 14D; 14E DO NOT EXTEND ENOUGH FOR EXIT ROW. ADJUSTED TRAY TABLES AT SEAT BACKS OF PASSENGER SEATS 14C; 14B; 14D; AND 14E IAW CMM 25-23-67;[02] READJUSTED TRAY TABLE OF PASSENGER SEATS 14C; 14B; 14D; AND 14E TO 3IN EXTENSIONS PER CMM EFFECTIVETY IAW CMM 25-23-67.
Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 26,319 hrs · 13,593 cycles
CHECKED R1 SLIDE PRESSURE, SHOWING IN RED. REMOVED AND REPLACED IAW AMM 25-66-01-401-NG, MT 725-61-06
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 24,935 hrs · 12,906 cycles
FLASHLIGHT BELOW AFT RIGHT SIDE JUMPSEAT INOPERATIVE. AFT EMERGENCY FLASHLIGHT OP CHECK GOOD PER AMM 25-64-00.
Earlier reports · 2018–2025 · 30 reports
2025
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 23,364 hrs · 12,111 cycles
AFT FLIGHT ATTENDANT FLASHLIGHT FO SIDE NOT CHARGING. REPLACED FLASHLIGHT BATTERY AND SEAL IAW AMM 25-64-00.
2024
Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 20,369 hrs · 10,511 cycles
FWD MEGAPHONE INOP<[01] REMOVED AND REPLACED FWD MEGAPHONE AND PERFORMED OPERATIONAL CHECK REF AMM 25-64-00
Part: BATTERY PACK — INOPERATIVE (FWD FLASHLIGHT) · airframe 19,789 hrs · 10,212 cycles
FWD FA FLASHLIGHT INOP<[01] REMOVED AND REPLACED OUTBD FWD FA FLASHLIGHT AND BATT PER AMM 25-64-00 OPS CHECK OK.
Part: SUPPORT BRACKET — DAMAGED (LT WING LE) · airframe 19,583 hrs · 10,104 cycles
ELONGATED HOLE SUPPORT BRACKET LOCATED IB LEADING EDGE AT LEVEL IFSS 151 AT LT WING 2024-318209<[01] REPLACED SUPPORT BRACKET LOCATED IB LEADING EDGE AT LEVEL IFSS 151 AT LT WING IAW B737-800 SRM 51-40-02 AND SRM 51-40-04.;[02] REPLACED SUPPORT BRACKET LOCATED IB LEADING EDGE AT LEVEL IFSS 151 AT LT WING IAW B737-800 SRM 51-40-02 AND SRM 51-40-04.TOOL USED TORQUE WRENCH 40-200 P/N QD1R200A S/N 0821900898 DUE DATE 14-SEP-24 TORQUE APPLIED 65 IN-LB.;[03] REPLACED SUPPORT BRACKET LOCATED IB LEADING EDGE AT LEVEL IFSS 151 AT LT WING IAW B737-800 SRM 51-40-02 AND SRM 51-40-04.TOOL USED TORQUE WRENCH 40-200 P/N QD1R200A S/N 0821900898 DUE DATE 14-SEP-24 TORQUE APPLIED 65 IN-LB.
Part: WEB — CRACKED (FAN COWL) · airframe 19,583 hrs · 10,104 cycles
CRACK WEB OUTBOARD FAN COWL ON ENGINE 2 2024-318208<[01] REPLACED WEB OUTBOARD FAN COWL ON ENGINE 2 IAW B737-800 SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] REPLACED WEB OUTBOARD FAN COWL ON ENGINE 2 IAW B737-800 SRM 51-40-02-0G-0 AND CMM 71-13-30 TOOL USED CALIPER PN:500-196-30 SN:A21033522 DUE DATE :22/DEC/24;[03] CERTIFIED WORK PERFORMED.
Part: WEB — CRACKED (FAN COWL) · airframe 19,583 hrs · 10,104 cycles
CRACK WEB INBOARD FAN COWL INTERNAL AREA ON ENGINE 1 2024-318200<[01] REPLACED WEB LOCATED ON INBOARD FAN COWL INTERNAL AREA ON ENGINE 1 IAW B737-800 SRM 51-10-02 ITEM 9 AND GOODRICH AEROSTRUCTURES CMM 71-13-30. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB LOCATED ON INBOARD FAN COWL INTERNAL AREA ON ENGINE 1 IAW B737-800 SRM 51-10-02 ITEM 9 AND GOODRICH AEROSTRUCTURES CMM 71-13-30. SEE INDIVIDUAL SIGN OFF BELOW.
Part: SUPPORT ANGLE — CORRODED (BS 500I S26L/R) · airframe 19,583 hrs · 10,104 cycles
CORROSION ON SUPPORT ANGLE LOCATED BS500I WL156 AND BTW STR26L TO STR26R AT FWD CARGO COMPARTMENT 2024-318190<[01] REPLACED SUPPORT ANGLE LOCATED BS500I WL156 AND BTW STR26L TO STR26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DRAWING 143A9481 SHEET 17 REV- AND 143A9485 SHEET 11 REV B. SEE INDIVIDUAL SIGN-OFF BELLOW.;[02] REPLACED SUPPORT ANGLE LOCATED BS500I WL156 AND BTW STR26L TO STR26R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DRAWING 143A9481 SHEET 17 REV- AND 143A9485 SHEET 11 REV B. SEE INDIVIDUAL SIGN-OFF BELLOW.
Part: ANGLE — CRACKED (BS 500H S26L) · airframe 19,583 hrs · 10,104 cycles
CRACK ANGLE - CLIP LOCATED BS500H STR26L FWD FACE FWD CARGO COMPARTMENT 2024-318189<[01] REPLACED ANGLE - CLIP LOCATED BS500H STR26L FWD FACE FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET 175 REV -.;[02] CORRECTED STEP 1. REPLACED ANGLE - CLIP LOCATED BS500H STR26L FWD FACE FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET 175 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] STEP 2 COMPLETED <BR>TASK CARD COMPLETED
Part: ANGLE — CRACKED (BS 867 LBL 11) · airframe 19,583 hrs · 10,104 cycles
CRACK ANGLE LOCATED BS867 AND LBL11 AFT CARGO COMPARTMENT 2024-318172<[01] REPLACED ANGLE LOCATED BS867 AND LBL11 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-05-0G-0; DWG 149A8102 SHEET 19 REV A. AND DWG 149A8104 SHEET 1 REV B.;[02] CORRECTED STEP 1. REPLACED ANGLE LOCATED BS867 AND LBL11 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0; DWG 149A8102 SHEET 19 REV A. AND DWG 149A8104 SHEET 1 REV B.;[03] COMPLETED CORRECTIVE ACTION 2
Part: FLOORBEAM — CORRODED (BS 947 LBL38-60) · airframe 19,583 hrs · 10,104 cycles
CORROSION FLOOR STRUCTURE BEAM LOCATED BS 947; LBL50; WL 208.1 AT AFT GALLEY AREA. REPAIRED FLOOR STRUCTURE BEAM LOCATED BS 947; LBL38 TO LBL 60; WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM-53-70-51-2R-5 REPAIR 5; THIS IS REPAIR CATEGORY A .
Part: FLOORBEAM — CORRODED (BS 947 RBL 50) · airframe 19,583 hrs · 10,104 cycles
CORROSION FLOORBEAM LOCATED BS 947; RBL 50; WL 208.1 AT AFT GALLEY AREA. REPAIRED FLOOR STRUCTURE BEAM LOCATED BS 947; RBL 50; WL 208.1 AT AFT GALLEY AREA THE REPAIR WAS ACCOMPLISHED IAW SRM 53-70-51-2R-5 WITH MINOR DEVIATIONS DOCUMENTED IN EA 24-153-01398. THIS IS REPAIR CATEGORY A.
Part: FLOOR SUPPORT — CORRODED (BS 947 LBL 49) · airframe 19,583 hrs · 10,104 cycles
CORROSION FLOOR STRUCTURE FITTING LOCATED BS 947; LBL 49; WL 208.1 AT AFT GALLEY AREA 2024-318126<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45 MG; S/N: 130066701; DUE DATE: 09-JUN-24.;[02] REPLACED INTERCOSTAL LOCATED BS 947 T0 967; LBL 49; WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM 51-40-02 AND DWG 147A5650 SHETTS 55 REV A;[03] REPLACED INTERCOSTAL LOCATED BS 947 T0 967; LBL 49; WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM 51-40-02 AND DWG 147A5650 SHETTS 55 REV A;[04] CORRECTED CORRECTIVE ACTION 3 <BR><BR>REPLACED INTERCOSTAL LOCATED BS 947 T0 967; LBL 49; WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM 51-40-02 AND DWG 147A5650 SHETTS 55 REV A<BR><BR>ITEM RII
Part: ANGLE — CRACKED (LT WING TE) · airframe 19,583 hrs · 10,104 cycles
CRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING 2024-318123<[01] REPLACED ANGLE LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02-0G-0 AND DWG 115A2930 SHEET 17 REV -. MEASURES OF THE CRACK ARE: L= 0.303? TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A23329368 DUE DATE 06-MAR-2025.;[02] REPLACED ANGLE LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02-0G-0 AND DWG 115A2930 SHEET 17 REV -. MEASURES OF THE CRACK ARE: L= 0.303? TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A23329368 DUE DATE 06-MAR-2025.
Part: ANGLE — CRACKED (LT WING TE) · airframe 19,583 hrs · 10,104 cycles
CRACK ANGLE TRAILING EDGE ORSS 280 DEFLECTION CONTROL RIB AREA LT WING 2024-318124<[01] REPLACED ANGLE ON TRAILING EDGE ORSS 280 DEFLECTION CONTROL RIB AREA LT WING IAW B737-800 SRM 51-40-02-0G AND DWG 115A6200 SHEET 24 REV A;[02] COMPLETED TASK CERTIFIED
Part: ACCESS PANEL — CRACKED (BODY FAIRING) · airframe 19,583 hrs · 10,104 cycles
CRACK ACCESS PANEL 191D BODY FAIRING AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 191D BODY FAIRING AT LOWER FUSELAGE IAW B737-800 SRM 51-70-04-2R-2 REPAIR 2.
Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 19,583 hrs · 10,104 cycles
CRACK ON FWD CORNER SCUFF PLATE OF AFT CARGO DOOR CUT OUT 2024-318055<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23272782; DUE DATE: 06-MAR-25.;[02] TOOL USED IN STEP 4: RADIOMETER PHOTOMETER KIT P/N: XRP-3000 S/N: 1859843 DUE DATE: 24-JUL-24;[03] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDING WITH BOEING 737-800 SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4) TO (7); BAC 5975. SEE INDIVIDUAL SIGNOFF BELOW.;[04] JOB TASK COMPLETED.
Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 19,583 hrs · 10,104 cycles
CRACK FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT 2024-318104<[01] REPLACED FLOOR PANEL 120CF FWD CARGO COMPARTMENT IAW B737-800 AMM 25-52-01-201-801 AND DWG 453A1610 SHEET 65 REV-<BR>MATERIAL USED ALUMINUM SHEET : P/N: 2024-T3 0.071. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED FLOOR PANEL 120CF FWD CARGO COMPARTMENT IAW B737-800 AMM 25-52-01-201-801 AND DWG 453A1610 SHEET 65 REV-<BR>MATERIAL USED ALUMINUM SHEET : P/N: 2024-T3 0.071 PO: 2022 195554. SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 1 AND 2. REPLACED FLOOR PANEL 120CF FWD CARGO COMPARTMENT IAW B737-800 AMM 25-52-01-201-801 AND DWG 453A1610 SHEET 65 REV-<BR>MATERIAL USED ALUMINUM SHEET : P/N: 2024-T3 0.071 PO: 2022 195554. SEE INDIVIDUAL SIGN OFF BELOW;[04] REPLACED FLOOR PANEL 120CF FWD CARGO COMPARTMENT IAW B737-800 AMM 25-52-01-201-801 AND DWG 453A1610 SHEET 65 REV-<BR>MATERIAL USED ALUMINUM SHEET : P/N: 2024-T3 0.071 PO: 2022 195554. SEE INDIVIDUAL SIGN OFF BELOW
Part: FITTING — CORRODED (ZONE 200) · airframe 19,583 hrs · 10,104 cycles
CORROSION LOWER FITTING LOCATED G1 AT FWD GALLEY AREA (2 EA) 2024-318079<[01] REPLACED LOWER FITTING LOCATED G1 AT FWD GALLEY AREA (2 EA) IAW B737-800 SOPM 20-50-01 REV. 38;[02] CORRECTED STEP 2. REPLACED LOWER FITTING LOCATED G1 AT FWD GALLEY AREA (2 EA) IAW B737-800 SOPM 20-50-01 REV. 38 AND ENCORE CMM 25-31-71 REV. B.;[03] REPLACED LOWER FITTING LOCATED G1 AT FWD GALLEY AREA (2 EA) IAW B737-800 SOPM 20-50-01 REV. 38 AND ENCORE CMM 25-31-71 REV. B.
Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 19,583 hrs · 10,104 cycles
CRACK ON AFT CORNER SCUFF PLATE OF AFT CARGO DOOR CUTOUT 2024-318054<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23399190; DUE DATE: 04-MAR-25.;[02] ON STEP 4 ; TOOL USED: RADIOMETER/PHOTOMETER KIT. P/N:XRP-3000. S/N:1859843. DUE DATE:24-JUL-24.;[03] REPAIRED AFT CORNER SCUFF PLATE OF AFT CARGO DOOR CUTOUT IAW BOEING 737-800 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED AFT CORNER SCUFF PLATE OF AFT CARGO DOOR CUTOUT IAW BOEING 737-800 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.
Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 19,583 hrs · 10,104 cycles
CRACK FLOOR PANEL 140EF AT AFT CARGO COMPARTMENT 2024-317742<[01] REPLACED FLOOR PANEL 140EF AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-20-01-0G-0 AND DWG 453A2610 SHEET 38 REV C.;[02] CORRECTED STEP 1. REPLACED FLOOR PANEL 140EF AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-20-01-0G-0 AND DWG 453A2610 SHEET 38 REV C. SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 1 AND 2. REPLACED FLOOR PANEL 140EF AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0 AND DWG 453A2610 SHEET 38 REV C. SEE INDIVIDUAL SIGN OFF BELOW;[04] CORRECTED STEP 1 AND 2. REPLACED FLOOR PANEL 140EF AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G-0 AND DWG 453A2610 SHEET 38 REV C. SEE INDIVIDUAL SIGN OFF BELOW
2023
Part: MEGAPHONE — FAILED (ZN 200 FUS TOP) · airframe 18,168 hrs · 9,318 cycles
FWD MEGAPHONE WILL NOT TEST<
Part: FLASHLIGHT — NO TEST (AFT CABIN) · airframe 17,487 hrs · 8,905 cycles
RIGHT SIDE OTBD AFT EMERGENCY FLASHLIGHT WONT TEST. OK TO CONT PER MEL 25-12-01 SP#1B. R & R FLASHLIGHT ASSY PER SIP.
Part: SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 15,796 hrs · 7,932 cycles
FLOOR BOARD SUPPORT L/H PANEL BRAKE ASSY. CRACKED - LOCATED AT STA 540<[01] REMOVED AND REPLACED BREAKER PANEL L/H PER SRM 51-40-02 AT STA. 540.
Part: SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 15,796 hrs · 7,932 cycles
FLOOR BOARD SUPPORT R/H PANEL BRAKE ASSY. CRACKED - LOCATED AT STA 540<[01] REMOVED AND REPLACED BREAKER PANEL R/H AT STA. 540 PER SRM 51-40-02.
2021
Part: SLIDE — LOW (L2 DOOR) · airframe 11,540 hrs · 5,503 cycles
AFT ENTRY DOOR SLIDE PRESSURE GAUGE READING EXACTLY ON THE LINE BETWEEN RED AND GREEN ; / [01] AFT ENTRY DOOR SLIDE REPLACED PER MT 725-61-06
Part: INDICATOR — OUT OF TOLERANCE (TE FLAP SYS) · airframe 11,438 hrs · 5,451 cycles
FLAPS WOULD NOT EXTEND BEYOND FLAPS 10 PREFORMED ALTERNATE FLAPS EXTENSION + FLAPS 15 FOR LANDING ; / [01] PREFORMED FSEU BITE IAW FIM 27-51 TASK 801 AND PSEU BITE IAW FIM 32-09 TASK 801 NO FAULTS OR FAULT HISTORY FOUND. PREFORMED TRAILING EDGE LOAD RELIEF TEST IAW FIM 27-51 TASK 803 AND FLAP TRAILING EDGE PRIMARY CONTROL OPERATION/LOCKOUT IAW FIM 27-51 TASK 836 NO FAULTS FOUND <BR>PREFORMED FLAP SKEW DETECT SYSTEM FUNCTION TEST IAW AMM 27-59-00. FUND SKEW SENSOR #1 AND #8 OUT OF RANGE IN POS 15. ADJUSTED #1 SENSOR PER AMM 27-59-00. OPS CHECK GOOD. CHECKED FLAP TRANSMISSION FLUID ON ALL FLAPS IWA AMM 12-22-51. ALL LEVELS GOOD.; [02] PREFORMED FLAP TRAILING EDGE DRIVE SYSTEM INSPECTION IAW AMM 27-51-00 NO DEFECTS FOUND. REPLACED FLAP POS INDICATOR IAW AMM 27-58-02. OPS CHECK GOOD.
2020
Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 7,514 hrs · 3,379 cycles
LEFT AFT INBOARD FLASHLIGHT WILL NOT TEST. R&R LEFT AFT INBOARD FLASHLIGHT, PER AMM 25-64-00. OPS CHECK GOOD.
Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 7,421 hrs · 3,327 cycles
AFT LEFT FLIGHT ATTENDANT FLASHLIGHT INOP. OK TO COTNINUE PER MEL 25-12-01 SP1B TRACKING # 97915( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ) / REMOVED AND RECREDLED BOTH AFT FLASH LIGHTS; OPS CK NORMAL REF 25-64-00.
Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 5,997 hrs · 2,642 cycles
AFT JUMPSEAT AIRCRAFT RIGHT OUTBD FLASHLIGHT DEAD. ( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ). / R/R AFT O/B EMERG FLASHLIGHT PER MM 25-64-00. CLEARING #74318
2018
Part: HOLDER — OUT OF ADJUST (R1 DOOR) · airframe 53 hrs · 24 cycles
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED HOLDER IAW SIP.