N8538V
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
FORWARD ENTRY DOOR GIRT BAR CLIPS NEED TO BE TIGHTENED. SECURED FWD ENTRY DOOR GIRT BAR CLIPS IAW AMM 25-66-02.
FWD ENTRY DOOR EVAC SLIDE PRESSURE LOW<[01] R&R FWD ENTRY DOOR MOUNTED ESCAPE SLIDE AS PER AMM 25-66-01. OPS CHECK GOOD. REMOVAL/ INSTALLATION OF SLIDE PART DONE ON SUB TASK # TTG8Q01C7F9J.;
RIGHT WING UPPER SURFACE EMERGENCY ESCAPE PATHWAY PAINT WORN CHIPPED AND MISSING IN MULTIPLE AREAS. REAPPLIED WING WALK WHITE COATING IAW AMM 51-21-97. BLACK COATING WILL BE APPLIED ON TTG8Q01C3920.
LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED RIGHT OVER WING EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-51-06. OPS CHECKS GOOD IAW MM 33-51-00
LEFT WING UPPER SURFACE EMERGENCY ESCAPE PATHWAY PAINT WORN CHIPPED AND MISSING IN MULTIPLE AREAS. RESTORED LT WING UPPER SURFACE EMERGENCY ESCAPE PATHWAY PAINT IAW AMM 51-21-97-701-NG.
EMERGENCY LIGHTS ON LEFT FRONT OVERHEAD BINS INOPERATIVE. REMOVED AND REPLACED LEFT FRONT EMERGENCY BATTERY PACK IAW MM 33-51-06. OPS CHECKS GOOD PER MM 33-51-00.
SIGNS OF CORROSION AT FWD CARGO RT SIDE FLOOR TO SIDE WALL TRANSITION ANGLE FROM STA 500 TO STA 500I. REMOVED CORROSION AT FWD CARGO RT TRANSITION ZEE ANGLE IAW SRM 51-10-02. MEASURED OUT OF LIMITS PER SRM 53-00-53-1A-2. MATERIAL NOMINAL THICKNESS 0.050, REMOVED 0.017, MAX ALLOWED 0.005. REMOVED DAMAGED TRANSITION ZEE ANGLE AT FWD CARGO RT BS 500A TO 500I IAW SRM 51-40-02.
LEFT WING OUTBOARD AFT FLAP UPPER SURFACE IS DELAMINATED AT I/B END. REMOVED LEFT WING OTBD AFT FLAP IAW AMM 27-51-22. SET INBD AND OTBD ROLLERS ON NEW LT WING OTBD AFT FLAP TO NOMINAL POSITION IAW AMM 27-51-22. INSTALLED LEFT WING OUTBOARD AFT FLAP PER AMM 27-51-22. REQUIRES OUTBOARD AFT FLAP ADJUSTMENT TO BE PERFORMED.
PANEL 661AB TRAILING EDGE SUPPORT BRACKET CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-10-02 AND SRM 51-40-02. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-10-02 AND SRM 51-40-02.
CRACK FOUND ON LT VAPOR BARRIER ATTACH ANGLE AT BS 663, LBL 9 AND LBL 34. PERFORMED NDT INSPECTION PER NDT PART 6; 51-00-00 PROCEDURE 16 OF HOLES COMMON TO REPAIR; IN TANK HOLES AND WEB HOLES. NO DEFECTS NOTED. REMOVED AND REPLACED LT VAPOR BARRIER ATTACH ANGLE AT BS 663 IAW SRM 51-40-02, AND EA M-24-157-02340.
CRACK FOUND ON RT VAPOR BARRIER ATTACH ANGLE AT BS 663, RBL 9 AND RBL 34. PERFORMED NDT INSPECTION PER NDT PART 6; 51-00-00 PROCEDURE 16 OF HOLES COMMON TO REPAIR; IN TANK HOLES AND WEB HOLES. NO DEFECTS NOTED. FABRICATED REPAIR PARTS. REMOVED AND REPLACED RT VAPOR BARRIER ATTACH ANGLE AT BS 663 IAW SRM 51-40-02 AND EA M-24-157-02340.
RIGHT HORIZONTAL STAB FWD UPPER SLIDER SEAL CRACKED. REMOVED AND REPLACED RT UPPER SLIDER SEAL IAW AMM 53-31-31.
LEFT HORIZONTAL STAB FWD UPPER SLIDER SEAL IS CRACKED. REMOVED AND REPLACED LT UPPER SLIDER SEAL IAW AMM 53-31-31.
ON THE LEFT HORIZONTAL STAB, THE FWD UPPER SLIDER SEAL HAS EVIDENCE OF CORROSION ON THE LOWER ATTACH POINTS. CLEANED ATTACH POINT PER SOPM 20-30-03; NO CORROSION FOUND.
RIGHT STABILIZER, UPPER BODY-TO-HORIZONTAL STABILIZER SLIDING SEAL CRACKED. REMOVED AND REPLACED RT UPPER SLIDER SEAL IAW AMM 53-31-31.
CREW REPORTS CEILING EMERGENCY EXIT SIGN BROKEN. REMOVED & REPLACED CEILING EMERGENCY EXIT SIGN ASSY IAW AMM 33-51-01.
MID-CABIN EMERGENCY EXIT SIGN BROKEN BY PAX. REINSTALLED THE EMERGENCY EXIT LENS IAW AMM 33-51-01.
EMERGENCY EXIT SIGN MID CABIN IS LOOSE. SECURED EMERGENCY EXIT SIGN MID CABIN IAW AMM 33-51-01.
EXIT SIGN MISSING. REPLACED THE SIGN IAW SIP.
SEVERAL AFT RIGHT EMERGENCY LIGHTS WOULD NOT TEST. REMOVED AND REPLACED M1671 BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.
FORWARD RT SIDE FA FLASHLIGHT LOW POWER. R & R FWD FLASHLIGHT BATTERY PER AMM 33-55-00.
CEILING MOUNTED EXIT SIGN BETWEEN OVERWING EXIT ROWS HAS DETATCHED. INSTALLED EXIT SIGN LENS PER AMM#33-1-01.
FWD OUTBOARD EMERGENCY FLASHLIGHT DOES NOT TEST ( CREW REPORTS )<[01] R/R FWD OUTBOARD EMERGENCY FLASHLIGHT BATTERY REF AMM 5-64-00;[02] R/R FWD OUTBOARD EMERGENCY FLASHLIGHT BATTERY REF AMM 25-64-00<BR><BR>CORRECTED AMM REFERENCE. APPROVED BY 66543;[03] CORRECTED AMM REFERENCE PER 66543
FA REPORTED POSSIBLE ODOR THAT RESEMBLED ELECTRICAL<[01] PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-56. NOTICED FOUL SMELL FROM TRASH AREA. NO OTHER DEFECTS NOTED.
SWA-REPAIR- CRACK; #2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY RIGHT ENGINE AFT PYLON AFT A-FRAME CRACKED<[01] REMOVED AND REPLACED #2 ENGINE PYLON AFT STRUT SUPPORT ASSEMBLY P/N 313A2752-1 PER SRM 51-40-02.
RIGHT ENGINE AFT PYLON AFT A-FRAME IS CRACKED. CRACK ORIGINATES AT FRAME DOUBLER AND CONTINUES THROUGH RADIUS FOR OVERALL LENGTH OF 1.2 INCHES. VERIFIED WITH NDT PART 6 PROCEDURE 23.<[01] 04 - REPAIRED PER [EA M-23-154-01884-REPREF (737-700/-800 - SWA-REPAIR- CRACK; #1/#2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY- REPAIR REFERENCE)]
#2 ENGINE AFT PYLON HAS A CRACK IN THE AFT A-FRAME THAT STARTS AT A PREVIOUSLY DOCUMENTED CRACK. IT BEGINS IN THE FRAME RADIUS AND ENDS IN THE SAME RADIUS. CRACK IS .150 LONG. SEE PREVIOUS WRITE UP. SEE ORIGINAL WRITE UP TTG8Q00VK0GY.<[01] 04 - REPAIRED PER [EA M-23-154-01884-REPREF (737-700/-800 - SWA-REPAIR- CRACK; #1/#2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY- REPAIR REFERENCE)] REF/ TTG8Q00VK0GY
CENTER AISLEWAY EXIT SIGN COVER (NEAR OVERWING) CAME OFF<[01] RESECURED CENTER AISLE EXIT SIGN LENS IN REFERENCE TO AIRCRAFT MAINTENANCE MANUAL 33 - 51 - 01 - 960 - 802
AFT GALLEY FLIGHT ATTENDANT FLASHLIGHT INOP.<[01] RESEATED FLASHLIGHT IN HOLDER IAW AMM 25-64-00.
EMX BATT PACK M02816 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M02816 PER AMM 33-51-06
EMX BATT PACK M01670 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01670 PER AMM 33-51-06
PASSENGER CABIN - L1 DOOR SLIDE GIRT BAR AFT HOLDER BRACKET LOOSE<[01] ADJUSTED PASSENGER CABIN - L1 DOOR SLIDE GIRT BAR AFT HOLDER BRACKET PER SRM 51-40-02
FORWARD SERVICE DOOR SLIDE APPEARS VERY LOW IN DOOR<[01] REPACKED R1 DOOR SLIDE PER MT 725-61-06
GIRT BAR FOR THE FWD SERVICE DOOR LOOSELY HELD BY THE FWD GIRT BAR RETAINER CLIP WHEN STOWED<[01] ADJUSTED TENSION OF THE FWD GIRT BAR RETAINER CLIP ON THE FWD SERVICE DOOR AS PER AMM SIP. GIRT BAR NOW SECURELY RETAINED WHEN STOWED
L1 DOOR SLIDE PROTRUDING EXCESSIVELY<[01] REPOSITIONED L1 DOOR ESCAPE SLIDE PER MT#725-61-06.
FWD MEGAPHONE BATTERY BAD<[01] REMOVED AND REPLACED FWD MEGAPHONE REF AMM 25-64-00
EMER. EXIT SIGN AT OVERWING EXIT FELL OFF.<[01] RE INSTALLED EMER. EXIT SIGN AT OVERWING EXIT PER SIP<BR>OPS CHK GOOD.
R1 SERVICE DOOR GIRT BAR FLOOR LATCH DOES NOT HOLD BAR<[01] RI DOOR GIRT BAT SLIDE BRACKET OPS NORMAL PER M/M 25-66-02
PER CUSTOMER REQUEST- L2 DOOR ASSIST HANDLE LOOSE<[01] RESECURED L2 DOOR ASSIST HANDLE AS PER AMM 52-13-31-400-802;[02] VERIFIED AND INSPECTED STEP #1; RESECURED L2 DOOR ASSIST HANDLE AS PER AMM 52-13-31-400-802
EMERGENCY BATTERY PACK (M1672) AT LEFT SIDE DEFECTIVE.<[01] EMERGENCY BATTERY PACK (M1672) WILL BE REPLACED ON N/R TTG8Q00KRZPJ.;[02] VERIFIED STEP 1.
EMERGENCY BATTERY PACK (M1673) AT LEFT SIDE DEFECTIVE.<[01] EMERGENCY BATTERY PACK (M1673) WILL BE REPLACED ON N/R TTG8Q00KRZPJ.;[02] VERIFIED STEP 1.
PASSENGER COMPARTMENT SEVERAL EMERGENCY LIGHTS INOPERATIVE.<[01] REMOVED AND REPLACED; M1672;1673;1676;AND 1675;BATTERY PACKS;PERFORMED OPEARATIONAL TEST; TEST PASS. REF. TO AMM 33-51-06-960-805.;[02] VERIFIED STEP 1
AFT CARGO TEE SUPPORT P/N 146A9410-16 HAS CORROSION AROUND 1 FASTENER HOLE AFT CARGO TEE SUPPORT ASSY P/N 146A9401-4 HAS CORROSION AROUND 1 FASTENER HOLE<[01] ACCOMPLISHED PART TRANSACTION;[02] REMOVED CORROSION TO AFT CARGO TEE SUPPORT ASSY PER SRM 51-10-02-0G-0. EVALUATED AREA ORIGINAL MAT. 0.070'; MAT. REMOVED 0.018; MAT. REMAINING 0.052' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2. RECEIVED NEW AFT CARGO TEE SUPPORT PART 146A9401-4 AND INSTALLED AT STA 772.6 PER SRM 51-40-02-0G-0.
RIGHT HORIZONTAL STAB ACCESS PANEL 343AT HAS BLADE SEAL CRACKED<[01] REMOVED AND REPLACED BLADE SEAL ON RIGHT HORIZONTAL STAB ACCESS PANEL 343AT AS PER SRM 51-40-02-0G-0. WORK WAS ACCOMPLISHED BY NOE M. ORTEGA.;[02] VERIFIED STEP 1
LEFT HORIZONTAL STAB ACCESS PANEL 333AB HAS BLADE SEAL CRACKED<[01] REMOVED AND REPLACED BLADE SEAL AT LEFT HORIZONTAL STAB ACCESS PANEL 333AB IRW SRM 51-40-02;[02] VERIFIED STEP 1.
LT WING T/E STRUCTURE;SHOWS INB FIXED UPPER PANEL SUPPORT ANGLE BRACKET WITH INB ATTACH BRACKET CRACKED.MKD<[01] REMOVED AND REPLACED DAMAGED LT WING T/E STRUCTURE I/B FIXED UPPER PANEL SUPPORT ANGLE BRACKET I/B ATTACH BRACKET IN REF WITH SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1; COMPLETE
AFT OF AFT CARGO COMPARTMENT SUPPORT BRACKET CRACKED BELOW WASTE TANK CENTER POST S-27L STA 867 MKD DOT<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT SUPPORT BRACKET BELOW WASTE TANK CENTER POST S-27L STA 867 PER SRM 51-40-05-0G-0 AND SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.
FWD CARGO COMPARTMENT SIDE WALL AFT R/H GUSSET CRACKED AT S-19R STA 500I<[01] REMOVED AND REPALCED FWD CARGO COMPARTMENT SIDE WALL AFT R/H GUSSET AT S-19R STA 500I IRW SRM 51-40-02 DWG 143A7902;[02] VERIFIED STEP 1; COMPLETE
CORROSION AT FWD CARGO COMPARTMENT BILGE AFT FLOOR SUPPORT ANGLE FROM S-26L TO S-26R STA 500I<[01] REMOVE AND REPLACE FWD CARGO COMPARTMENT BILGE AFT FLOOR SUPPORT ANGLE FROM S-26L TO S-26R STA 500I IRW SRM 51-40-02 DWG 143A9481;[02] VERIFIED STEP 1
FOUND CORROSION AROUND THE FASTENER HOLE IN FLOOR STRUCTURE AFT WET AREA AT STA 951 ; LBL 19' (228-001)<[01] REMOVED AND INSTALLED NEW T ANGLE SUPPORT IN FLOOR STRUCTURE AFT WET AREA AT STA 951 LBL 19 AS PER SRM 51-40-02-0G-0 AND DWG # 147A5650 SHEET 54 REV A.;[02] REMOVED AND INSTALLED NEW T ANGLE SUPPORT IN FLOOR STRUCTURE AFT WET AREA AT STA 951 LBL 19 AS PER SRM 51-40-02-0G-0 AND DWG # 147A5650 SHEET 54 REV A.;[03] VERIFIED STEP #1. REMOVED AND INSTALLED NEW T ANGLE SUPPORT IN FLOOR STRUCTURE AFT WET AREA AT STA 951 LBL 19 AS PER SRM 51-40-02-0G-0 AND DWG # 147A5650 SHEET 54 REV A;[04] VERIFIED STEP 3. REMOVED AND INSTALLED NEW T ANGLE SUPPORT IN FLOOR STRUCTURE AFT WET AREA AT STA 951 LBL 19 AS PER SRM 51-40-02-0G-0 AND DWG # 147A5650 SHEET 54 REV A.
FLIGHT DECK ENTRY FLOOR SKIN PANEL AREAS WORN BETWEEN STA 259 & 270 ;LBL-5 AND RBL-3<[01] ACCOMPLISHED EA M-21-153-00734;[02] VERIFIED STEP 1;[03] ADDED FAILURE TYPE AND MAJOR REPAIR VALUE UNDER REPAIR TYPE MEASUREMENT AT THE REQUEST OF REGULATORY AFFAIRS.;[04] CERTIFIED
MAIN CABIN CENTER AISLE FLOOR SUPPORT BREAK CRACKED @ LBL-1 STA 540 MKD DOT<[01] REMOVED AND REPLACED PANEL BREAK ASSY AT STA 540 LBL-1 IRW SRM 51-40-02 DWG 143A0060;[02] VERIFIED STEP 1
MAIN CABIN CENTER AISLE FLOOR SUPPORT BREAK CRACKED @ RBL-1 STA 540 MKD DOT<[01] REMOVED AND REPLACED PANEL BREAK ASSY AT STA 540 RBL-1 IRW SRM 51-40-02 DWG 143A0060;[02] VERIFIED STEP 1
NO-1 ENG INB FAN COWL INTERNAL INTERCOSTAL CRACKED AT UPPERVEDGE I/B OF ENG OIL SERVICE ACCESS DOOR MKD DOT CORRECTION TO FAULT DETAI :NO-1 ENG INB FAN COWL INTERNAL SHEILD CRACKED AT UPPER EDGE I/B OF ENG OIL SERVICE ACCESS DOOR<[01] REMOVED AND REPLACE NO-1 ENG INB FAN COWL INTERNAL INTERCOSTAL IRW SRM 51-40-02 AND CMM 71-13-30;[02] CORRECTION TO STEP 1:REMOVED AND REPLACE NO-1 ENG INB FAN COWL SHIELD IRW SRM 51-40-02 AND CMM 71-13-30;[03] VERIFIED STEP 2<BR>AKNOWLEGED STEP 1
LEFT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL LOWER CENTER ANGLE O/B EDGE CRACKED<[01] REMOVED AND REPLACED DAMAGED L/W T/E DEFLECTION CONTROL RIB PANEL LOWER CENTER ANGLE IN REF WITH SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1; COMPLETE
LEFT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL LOWER O/B ANGLE CRACKED<[01] REMOVED AND REPLACED DAMAGED L/W T/E DEFLECTION CONTROL RIB PANEL LOWER O/B ANGLE IN REF WITH SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1; COMPLETE
EXTERNAL POWER RECEPTACLE CUTOUT CRACKED AT LOWER CENTER AREA<[01] ACCOMPLISHED REPAIR OF EXTERNAL POWER RECEPTACLE CUTOUT DAMAGE AT LOWER CENTER AREA IN REF WITH SRM 53-10-15-2R-4.;[02] CORRECTION TO STEP 1: ACCOMPLISHED REPAIR OF EXTERNAL POWER RECEPTACLE CUTOUT DAMAGE AT LOWER CENTER AREA IN REF WITH SRM 53-10-15-2R-4 DWG 141A8701;[03] AKNOWLEDGED STEP 1<BR>VERIFIED STEP 2
FO SIDE AFT FA JUMPSEAT FLASHLIGHT INOP / [01] REMOVED AND REPLACED F.O SIDE FLIGHT ATTENDANT FLASHLIGHT BRACKET ASSY REF AMM 25-64-00
EXIT SIGN MID CABIN FELL OFF / REINSTALLED LENS PER M/M 33-51-02.
EMERGENCY EXIT COVER PLATE FELL OFF FROM OVERHEAD SIGN ON CEILING / RESECURED LENS ON EMERGENCY EXIT SIGN PER SIP AC OK FOR SERVICE
AFT INBD EMERGENCY FLASHLIGHT WILL NOT TEST ( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ) / AFT IB EMERGENCY FLASHLIGHT TESTS NORMAL
CABIN EMERGENCY LIGHTS CB P6-11 A9 BROKEN OFF. / R&R C/B IAW SWPM 20-30-00
FWD MEGAPHONE BATTERIES DEAD. R & R MEGAPHONE IAW AMM 25-64-00.
AFT FIRST OFFICERS SIDE FLASHLIGHTS NOT CHARGING. RERACKED INBOARD AFT FLASHLIGHTS IAW MM.
AFT FIRST OFFICERS SIDE FLASHLIGHTS NOT CHARGING. RERACKED OUTBOARD AFT FLASHLIGHTS PER MM.
R/H FLOOR PATH LIGHTING AT ROW 1, FIRST 2 INCHES LIGHT UP BUT REST WERE DARK UNTIL ROW 2. / R&R LIGHT STRIP PER AMM.
DECLARED EMERGENCY, ELECTRICAL ODOR IN FWD GALLEY AREA. C/W INSPECTION. R&R FWD GALLEY COFFEE MAKER AS PRECUATION PER MM.