N8706W
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
Maintenance disclosures
FA REPORTS RT AFT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERY IAW AMM 25-64-00.
INSPECTED CABIN AREA, & FOUND ONE CEILING EMERGENCY LIGHT COVER MISSING IN FRONT OF THE LIFE RAFT AT SEAT ROW 21D. COMPLIED WITH EMERGENCY LIGHTS OPS TEST IAW AMM 33-51-00. LIGHTS WORKS NORMAL. DEFERRED LENS COVER. OKAY TO CONTINUE IAW MEL 25-10-014. INSTALLED THE EMERGENCY AISLE LIGHT LENS IAW AMM 33-51-03. OPS CHECKED GOOD.
CAPTS SIDE AFT GALLEY I BE FLASHLIGHT WILL NOT TEST. OK TO CONTINUE PER MEL 25-64-02A;EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS. WITH SP 1B & AUTHORIZATION NUMBER 302197. REMOVED AND REPLACED BATTERY PER AMM 25-64-00. OPS CHECK GOOD.
APU OVERSPEED FAULT CODE 49-31014. OK TO CONT PER MEL 49-11-01. R & R APU SPEED SENSOR REF AMM 49-61-21.
FIRST 12-14 OF FLOOR STRIP LIGHTING LEFT SIDE NOT WORKING AIRCRAFT LEFT.<[01] REPLACED PHOTOLUMINESCENT FLOOR STRIP LEFT SIDE REF AMM 33-51-15.
PANEL 192BL IS DELAMINATED<[01] R&R PANEL 192BL PER AMM 53-51-21. REFERENCE TTG8Q00W949J
GIRT BAR DROOP ON AFT ENTRY EMERGENCY SLIDE<[01] SECURED GIRT BAR IAW AMM 25-66-01. OK FOR SERVICE.
EMERGENCY EXIT SLIDE COMING OUT OF HOUSING L2 DOOR<[01] ADJUSTED L2 DOOR SLIDE PER AMM 25-66-01 AND MT 825-PRD-01-01. A/C OK FOR SERVICE.
AFT SLIDE CAPTAINS SIDE DIFFICULT TO DISARM<[01] REMOVED DEBRIS FROM AFT ENTRY DOOR SLIDE GIRTH BAR AS REQUIRED. NO FURTHER DEFECTS NOTED REFERENCE AMM 25?66-01.
4 ABC EMERGENCY CEILING LIGHT AND LEFT FWD EXTERNAL OVERWING EMERGENCY LIGHT INOP DURING EMERGENCY LIGHTS TEST<[01] REMOVED AND REPLACED M2335EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK PER AMM 33-51-06
4 ABC EMERGENCY CEILING LIGHT AND LEFT FWD EXTERNAL OVERWING EMERGENCY LIGHT INOP DURING EMERGENCY LIGHTS TEST<[01] REMOVED AND REPLACED M2335EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK PER AMM 33-51-06
FLOOR RETURN PANEL COVERS MISSING AT 16DEF; 19ABC AND 20DEF<[01] REPLACED SEAT TRACK AT 16DEF 19ABC AND 20DEF AS PER SA-M1023
EXTERIOR EMERGENCY LIGHT AFT OF R2 DOOR IS INOP.<[01] RELAMPED EXTERIOR EMERGENCY LIGHT AFT OF R2 DOOR. IAW AMM 33-51-04. OPS CHECK GOOD.
WHILE TROUBLE SHOOTING EMERGENCY EXIT LIGHTS FOUND EMERGENCY EXIT ISLE LIGHTS OUT AT SEAT ROW 10 AND 14 DEF<[01] REPLACED EMERG LIGHT BATTERY PACK AT STA 500C +7 RIGHT SIDE CABIN BEHIND DADO PANEL IAW 33-51-06-960-802. TESTS GOOD;[02] VERIFIED ITEM 1<BR>C/W
AFT GALLEY AREA EMERGENCY EXIT LIGHTS ARE INOP AT M1673<[01] REPLACED EMERGENCY BATTERY PACK IAW AMM 33-51-06-960-802 OPS TEST GOOD FOR BATTERY PACK;[02] VERIFIED STEP 1.<BR>AUDIT C/W.
AFT GALLEY AREA EMERGENCY EXIT LIGHTS ARE INOP AT M1672<[01] REPLACED EMERGENCY BATTERY PACK IAW AMM 33-51-06-960-802 OPS TEST GOOD FOR BATTERY PACK;[02] VERIFIED STEP 1.<BR>AUDIT C/W.
FWD LH ENTRY AREA EMERGENCY EXIT LIGHTS ARE INOP AT M1675<[01] REMOVED AND REPLACED BATTERY ON POWER SUPPLY M1675 IAW AMM 33-51-06-960-802. EMERGENCY LIGHTS FOR POWER SUPPLY M1675 CHECK GOOD.;[02] VERIFIED STEP 1.<BR>AUDIT C/W.
AFT CARGO COMPARTMENT; FWD L/H #3 CAPSTRIP HAS CORROSION ON LOWER SURFACE AFT CARGO COMPARTMENT FWD L/H #3 CAPSTRIP HAS CORROSION ON LOWER SURFACE<[01] REMOVED AND INSTALLED NEW CAP STRIP P/N 453A2611-10 A TAG A194733 IAW SRM 51-40-02;[02] VERIFIED ITEM 1<BR>C/W
(A204 DOT 81) AFT CARGO FLOOR PANEL 140DF HAS CORROSION ON UPPER SURFACE AROUND PERIMITER OF FLOOR PANEL<[01] EVALUATED CORROSION AREA FOUND LENGTH OF CORRODED AREA IS MORE THAN 3' MAX ALLOWABLE LIMIT IS 3' FOUND OUT OF LIMITS I.A.W BOEING SRM 53-00-53-1A-1;[02] VERIFIED MATERIAL FOR NEW FLOOR PANEL 2024-T3 IAW SRM 53-60-53-0L-1 IDENTIFICATION 1 TABLE 2 ITEM 6 SIGNING FOR JORDAN LOYOLA 36874;[03] STEP 2 VERIFIED MATERIAL FOR NEW FLOOR PANEL 2024-T3 IAW SRM 53-60-53-0L-1 IDENTIFICATION 1 TABLE 2 ITEM 6 SIGNING FOR JORDAN LOYOLA 36874.<BR><BR>A-TAG :A132705;[04] MATERIAL VERIFIED; STEPS 1-3 COMPLETE;[05] LOCATED AND DRILLED HOLES ON AFT CARGO FLOOR PANEL 140DF IAW 737-8-SRM 51-40-05-0G-0 FIGURE 6 AND AMM 50-10-04-400-801 SIGNING FOR JORDAN LOYOLA 36874;[06] VERIFIED STEP 5;[07] FABRICATED AFT CARGO FLOOR PANEL 140DF IAW 737-8 AMM 50-10-04-400-801;[08] VERIFIED STEP 7;[09] OK TO TREAT AND PRIME;[10] TREATED AND PRIME AFT CARGO FLOOR PANEL 140DF IAW AMM 51-21-41-370-802; AND AMM 51-21-72-370-804;[11] VERIFIED STEP 10<BR>AUDIT CW
(A204 DOT 18) AFT CARGO; STA 867; LBL 10; JUST BELOW CARGO FLOOR LINE. ATTACHE ANGLE CRACKED FROM LONGITUDINAL FLOOR SUPPORT TO ANGLED FLOOR SUPPORT (LAV VACUUM COMPARTMENT STRUCTURE)<[01] REMOVED ANGLE ON AFT CARGO; STA 867; LBL 10; JUST BELOW CARGO FLOOR LINE (LAV VACUUM COMPARTMENT STRUCTURE) I.A.W SRM 51-40-02-0G-0;[02] VERIFIED NEW ANGLE WITH PART NUMBER:149A8109U114 AND A192984 I.A.W DWG 149A8102;[03] VERIFIED ITEM 2<BR>OK TO INSTALL;[04] INSTALLED NEW ANGLE ON AFT CARGO; STA 867; LBL 10; JUST BELOW CARGO FLOOR LINE (LAV VACUUM COMPARTMENT STRUCTURE) I.A.W SRM 51-40-02-0G-0;[05] VERIFIED ITEM 4<BR>OK TO CIC;[06] APPLIED CIC ON ANGLE AT AFT CARGO; STA 867; LBL 10; JUST BELOW CARGO FLOOR LINE (LAV VACUUM COMPARTMENT STRUCTURE) I.A.W AMM 51-21-91-620-802;[07] VERIFIED ALL STEPS ARE COMPLETE;[08] VERIFIED ITEMS 6 AND 7<BR>AUDIT C/W
(A204; DOT 13) AFT CARGO STA 727H TO 847; LBL 23; WL 161; Z-ANGLE HAS CORROSION AROUND FASTNER HOLES.<[01] REMOVED CORROSION Z ANGLE AND CHECK WITH 10X MAGNIFYING GLASS IAW SRM 51-10-02-0G-0 ITEM 14;[02] EVALUATED DAMAGE : ORIG;'T' .040 REMAINING .031 LOSS .009 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 TOOL USED AAR #36649 DUE 08/02/23;[03] VERIFIED ITEMS 1&2;[04] OK TO INSTALL NUT PLATES;[05] INSTALLED NUT PLATES IAW B737 SRM 53-00-53-2R-5 STEP 4.K.;[06] VERIFIED STEP 5<BR>OK TO CIC;[07] APPLIED CIC IAW B737 SRM 53-00-53-2R-5 STEP 4.N.;[08] VERIFIED STEP 7 C/W;[09] OK TO INSTALL REPAIR PARTS;[10] INSTALLED ZEE CHANEL REPAIR PARTS BETWEEN STA 727H + 14.0 IN AND 787 + 9.0 IN AT LBL 21.00 IAW B737 SRM 53-00-53-2R-5 STEP 4.L.;[11] VERIFIED STEP 10 C/W;[12] OK TO CIC;[13] APPLIED CIC REPAIR AREA IAW AMM51-21-91-620-802;[14] VERIFIED ITEM 13<BR>AUDIT C/W
LH HORIZONTAL STAB ELEVATOR BALANCE BY SEAL PANEL 334CB BULB SEAL IS CRACKED AT ELEVATOR STA. 149.12 P/N 183A2433-3<[01] REPLACED L/H HORIZONTAL STAB ELEVATOR BALANCE SEAL PANEL 334CB PLATE I/A/W SRM 51-40-02-0G-0 AND BOEING DWG 183A0300 REV A;[02] C/W;[03] VERIFIED STEP 1<BR>AUDIT CW
(A204 DOT 20) AFT CARGO STA 847+6; RBL 23; WL 162; SPLASH SHIELD HAS CORROSION AROUND NUT PLATE HOLE.<[01] EVALUATED CORRODED SHIELD NO ALLOWABLE LIMIT FOUND IN SRM 53-00-53-1A-2;[02] VERIFIED STEP 1;[03] REMOVED SHIELD IAW SRM 51-40-02-0G-0;[04] VERIFIED REPLACEMENT SHIELD TO BE THE CORRECT PN 146A8127Y10 A TAG WN32589 IAW BOEING DWG 146A0081 REV-A;[05] VERIFIED ITEM 4;[06] LOCATED AND DRILLED PN: 146A8127Y10 IAW SRM 51-40-05;[07] VERIFIED ITEM 6;[08] OK TO CIC AREA UNDER SHIELD;[09] APPLIED CIC TO AREA IAW AMM 51-21-91-620-802 APPLICATION TIME IS 8:15AM 11/JUL/23;[10] VERIFIED ITEM 9<BR>OK TO INSTALL SHIELD;[11] OK TO INSTALL IN RII ROLE;[12] INSTALLED SHIELD IAW SRM 51-40-02-0G-0 AND IAW BOEING DWG #146A0081 REV-A;[13] VERIFIED ITEM 12<BR>OK TO CIC;[14] APPLIED CIC IAW AMM TASK 51-21-91-620-802 APPLICATION TIME 12:15PM 11/JUL/2023;[15] VERIFIED STEP 14.<BR>AUDIT C/W.
(A204 DOT 19) AFT CARGO. STA 887; BL0 TO RBL 16; WL 165; FLOOR PANEL SPLICE PLATE HAS CORROSION ON UPPER SURFACE.<[01] EVALUATED SPLICE PLATE NO ALLOWABLE LIMITS FOUND IN SRM;[02] VERIFIED STEP 1;[03] SPLICED REMOVED FROM STA 887 BL 0 WL 165 IAW SRM 51-40-05;[04] VERIFIED P/N WITH IPC 53-42-11-27 TAG A192979;[05] FABRICATED PART IAW SRM 51-40-02;[06] VERIFIED STEPS 4 & 5<BR><BR>OK TO INSTALL;[07] INSTALLED NEW (TEE) FLOOR SPLICE PLATE AT STA 887 BL 0 WL 165 IAW SRM 51-40-02-0G;[08] VERIFIED STEP 7<BR>AUDIT CW
(A204 DOT 17) AFT CARGO STA 767 TO 787; RBL 23; WL 161; SPLACE SHIELD ATTACH ANGLE HAS CORROSION ON LOWER SURFACE COMMON TO NUT PLATES.<[01] EVALUATED ANGLE FOUND MATERIAL LOSE IS MORE THAN 90% OF MATERIAL THICKNESS OUT OF LIMITS I.A.W SRM 51-10-02-0G-0;[02] REMOVED ANGLE I.A.W SRM 51-40-02-0G-0;[03] VERIFIED ITEM 1;2;[04] VERIFIED PN 146A8125U53ATSMRO ATAG WN32393 TO BE CORRECT IAW BOEING DWG # 146A8123 REV-;[05] CERTIFYING STEP 4;[06] VERIFIED ITEM 4;[07] LOCATED AND DRILLED PN 146A8125U53ATSMRO IAW SRM 51-40-05 AND IAW BOEING DWG # 146A8123 REV-;[08] VERIFIED ITEM 7;[09] OK TO INSTALL TO SHIELD;[10] STARTED TO INSTALL SHIELD IAW SRM 51-40-02-0G-0 AND IAW BOEING DWG # 146A8123 REV-;[11] ITEM 9 SHOULD READ OK TO INSTALL SHIELD ANGLE TO AIRCRAFT STRUCTURE.<BR>VERIFIED ITEM 10;[12] COMPLETED INSTALLATION OF SHIELD ATTACH ANGLE IAW SRM 51-40-02-0G-0 AND DWG 146A8123 REV-;[13] VERIFIED STEP 12<BR>JOB COMPLETE<BR>AUDIT C/W;[14] COMPLETE
(A204 DOT 16) AFT CARGO STA 767 TO 787+6; RBL 23; WL 161; SPLASH SHIELD HAS CORROSION ON UPPER AND LOWER SURFACE.<[01] EVALUATED SHOELD NO ALLOAWBLE LIMITS FOUND IN SRM 53-60-15-1A-1;[02] REMOVED SHIELD I.A.W SRM 51-40-02-0G-0;[03] VERIFIED ITEMS 1;2;[04] VERIFIED REPLACEMENT SPLASH SHIELD TO BE CORRECT PN 146A8127-12 A TAG WN32591 IAW BOEING DWG NUMBER 146A0081 REV A;[05] VERIFIED STEP 4.;[06] LOCATED AND DRILLED PN 146A8127-12 IAW BOEING DWG #146A0081 REV-A;[07] VERIFIED STEP 4 AS RII.;[08] VERIFIED ITEM 6;[09] OK TO CIC AREA UNDER SHIELD;[10] APPLIED CIC IAW AMM TASK 51-21-91-620-802 APPLICATION TIME IS 2:00PM 11/JUL/2023;[11] VERIFIED ITEM 10;[12] OK TO INSTALL SHIELD;[13] BEGAN INSTALLATION OF FWD SHIELD IAW SRM 51-40-02-0G-0; DWG 146A0081 REV A <BR>WORK PERFORMED BY NATHAN JAMES 36937;[14] VERIFIED STEP 13;[15] COMPLETED INSTALLING FWD SHIELD IAW SRM 51-40-02-0G-0 BOEING DWG 146A0081 REV A;[16] VERIFIED STEP 15. (RII);[17] JOB COMPLETED;[18] AUDIT C/W.
(A204 DOT 15) AFT ARGO STA 727I+4; RBL 23; WL 161; Z-ANGLE DOUBLER PLATE HAS CORROSION ON LOWER SURFACE.<[01] Z ANGLE DOUBLER PLATE BEEN REPLACED ON N/R TTG8Q00LZ34E I.A.W SRM 53-00-53-2R-5;[02] AUDIT C/W
(A204 DOT 14) AFT CARGO STA 727I+4 RBL 23; WL 161; Z-ANGLE HAS CORROSION AROUND FASTNER HOLE.<[01] REMOVED CORROSION OF Z- ANGLE AND CHECK WITH MAGNIFYING GLASS IAW SRM 51-10-02-0G-0 ITEM 14;[02] EVALUATED DAMAGE ;ORIG.'T' .040 MATERIAL REMAINING.032 LOSS.008 FOUND OUT OF LIMITS IWA SRM 53-00-53-1A-2 TOOL USED UT AAR#36644 DUE 08/02/23;[03] ENTER IN ERROR : TOOL USED AAR#36649 DUE 08/02-23;[04] REMOVED DAMAGED PART OF THE SIDEPLATE I.A.W. SRM 53-00-53-2R-5;[05] C/W;[06] VERIFIED MATERIAL FOR -1 ZEE CHANNEL SIDEPLATE AND -2 SPLICE SIDEPLATE MATERIAL BAC1496-377 7075-T62 ATAG A120480 IAW SRM 53-00-53-2R-5 TABLE 201;[07] VERIFIED ITEM 6;[08] STARTED FABRICATING NEW -1 ZEE CHANNEL SIDEPLATE IAW SRM 53-00-53-2R-5;[09] VERIFIED ITEM 8;[10] COMPLETED FABRICATION OF Z-ANGLE AND SPLICE IAW SRM 53-00-53-2R-5 FIGURE 202.;[11] VERIFIED STEP 10 C/W<BR>OK TO TREAT AND PRIME;[12] APPLIED CHEMICAL CONVERSION AND PRIMER IAW SRM 53-00-53-2R-5 SECTION 4. I; J.;[13] STEP 12 C/W;[14] OK TO INSTALL SPLICE PARTS AND NUT PLATES;[15] INSTALLED NUTPLATES ON NEW Z-ANGLE SECTION IAW SRM 53-00-53-2R-5 SECTION 4. K.;[16] STEP 15 C/W;[17. Z ANGLE HAS BEEN CUT AT STA 727H+12' TO STA 767 R/H <BR>OK TO INSTALL;[21] INSTALLED ALL REPAIR PARTS IAW SRM 53-00-53-2R-5 FIG 202;[22] NEED OK TO APPLY CIC REPAIR AREA;[23] VERIFIED ITEM 21;[24] OK TO CIC;[25] CICED AREA I.A.W SRM 53-00-53-2R-5;[26] STEP 25 C/W AUDIT C/W
A221 DOT 04 FWD CARGO BAY AT STA 520 AND BETWEEN STR 25L AND 25R LOWER L BRACKET SUPPORT STRUCTURE FOR CENTER BULKHEAD PNL HAS SEVERAL AREAS OF CORROSION AS MARKED<[01] FOUND TO BE OUT OF LIMITS. NO PUBLISHED LIMITS IN SRM;[02] REMOVED ANGLE IAW SRM 51-40-02;[03] VERIFIED STEPS 1;2;[04] REPLACEMENT ANGLE VERIFIED TO BE PN 143A9485Y35 A TAG WN12803 TO BE CORRECT PART IAW BOEING DWG NUMBER 143A9481 REV A;[05] VERIFIED ITEM 4;[06] LOCATED AND DRILLED IAW SRM 51-40-05 AND IAW BOEING DWG NUMBER 143A9481 REV A;[07] VERIFIED ITEM 6;[08] OK TO INSTALL;[09] INSTALLED PN 143A9485Y35 IAW SRM 51-40-02-0G-0 AND IAW BOEING DWG # 143A9481 REV A;[10] VERIFIED ITEM 9;[11] OK TO CIC ITEM 9;[12] APPLIED CIC IAW AMM TASK 51-21-91-620-802 APPLICATION TIME 11:30 AM ON 06-JUL-2023;[13] VERIFIED ITEM 12;[14] AUDIT C/W.
DOT 114-020. CARGO COMPARTMENT PANEL #140AF HAS MULTIPLE AREAS OF CORROSION ON INBOARD AND OUTBOARD SIDES.<[01] FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. DAMAGE BEYOND 3' IN LENGTH.;[02] VERIFIED MATERIAL TO BE .071' 2024 T-3 IAW SRM 53-60-53-0I-1 <BR>A129384;[03] VERIFIED STEPS 1;2;[04] FABRICATED NEW PNL IAW AMM 50-10-04-400-801;[05] OK TO TREAT AND PRIME;[06] TREATED PRIMED FLOOR PANEL IAW AMM 50-10-04-400-801;[07] ALL STEPS C/W<BR>AUDIT C/W
A225 001 FORWARD CARGO FLOOR PANEL 120 DF HAS CORROSION AT EDGE OF PANEL UPPER SURFACE.<[01] OK TO TREAT AND PRIME;[02] APPLIED PROTECTIVE TREATMENT AND PRIMER IAW B737 SRM <BR>51-20-01-0G-0. TABLE 3.;[03] VERIFIED STEP 2<BR>AUDIT CW
SEVERAL LH INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1670 IAW AMM 33-51-06. OPS CK GOOD.
LH OVER WING EMERGENCY EXIT SIGNS DONT ILLUMINATED.<[01] REMOVED AND REPLACED THE LH OVER WING EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06. LH OVER WING EMERGENCY LIGHTS OPS CHECK GOOD.
FWD GALLEY LH EMERGENCY FLASHLIGHT WILL NOT TEST<[01] REMOVED AND REPLACED FWD GALLEY LH EMERGENCY FLASHLIGHT ASSY IAW AMM 25-64-00. OPS CHECK GOOD.
L1 DOOR EMERGENCY SLIDE DISPLACED<[01] INSTALLED FWD ENTRY SLIDE PER AMM 25-66-01.<BR><BR>WORK C/W BY E115571
RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT RIGHT BATTERY PACK IAW AMM 33-51-06
FWD SERVICE DOOR HANDLE ASSIST BROKEN. R & R THE FWD SERVICE DOOR HANDLE ASSIST PER MM 52-41-31.
AFT GALLEY FLASHLIGHT INOP / [01] REMOVED AND REPLACED AFT GALLEY L/H INBD FLASHLIGHT BATTERY IAW AMM 25-64-00
L/H AFT FLASHLIGHT INOP / [01] REMOVED & REPLACED LEFT AFT FLASH LIGHT PER AMM 25-64-00-900-805
L1 DOOR EXTERNAL EMERGENCY LIGHT INOP. R&R BULB PER MM.
FORWARD ENTRY EMERGENCY EXIT SLIDE LIGHT INOP. RELAMPED LIGHT IAW AMM.
OVERHEAD OVERWING AISLE EMERGENCY EXIT SIGN LIGHT LOOSE FROM CEILING. REINSTALLED SIGN PER AMM.
MID CABIN OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED THE SIGN IAW AMM.