N8517F
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2025-02-25 – 2025-02-25 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2025-02-25 – 2025-02-25 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
EMERGENCY EXIT SIGN IN THE MID-CABIN FELL OFF CEILING CONNECTION. REINSTALLED EXIT SIGN COVER IAW AMM 33-51-01
FORWARD ENTRY DOOR LINING UPPER AND LOWER ASSIST HANDLE ARE LOOSE. TIGHTENED FORWARD ENTRY DOOR LINING UPPER AND LOWER ASSIST HANDLE IAW AMM 52-11-31-400-802 STEP 3.G.(2).
PANEL 193CL L/E WAS WIND ERODED. REPAIRED IAW SRM 51-70-05-2R-6.
CRACK FOUND AT BS 663 VAPOR BARRIER ATTACH ANGLE APPROXIMATELY LBL 9. REPAIRED THE UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5.
CRACK FOUND AT BS 663 VAPOR BARRIER ATTACH ANGLE APPROXIMATELY RBL 9. REPAIRED THE UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5.
EXIT SIGN MID CABIN FELL OFF DURING DEPLANING. ATTACHED EXIT OVERHEAD SIGN COVER PER AMM 33-51-01 STEP C(4). NO DEFECT FOUND.
FWD FLIGHT ATTENDANT FLASHLIGHT INOP.
EMERGENCY EXIT LIGHT BATTERY PACK M1676 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1676 IAW AMM 33-51-06-960-805; AMM 25-21-46-400-801. OPS CHECK GOOD;[02] COMPLETE<BR>AUDIT C/W
EMERGENCY EXIT LIGHT BATTERY PACK M1670 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1670 IAW AMM 33-51-06-960-805; AMM 25-21-46-400-801. OPS CHECK GOOD;[02] COMPLETE<BR>AUDIT C/W
EMERGENCY EXIT LIGHT BATTERY PACK M1694 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1694 IAW AMM 33-51-06-960-805-NG; AMM 25-21-46-400-801.<BR>OPS CHECK GOOD;[02] COMPLETE<BR>AUDIT C/W
EMERGENCY EXIT LIGHT BATTERY PACK M1695 FAILS TO CHARGE<[01] OPENED DADO PANEL AT BATTERY PACK M1695 IAW AMM 33-51-06-960-805-NG.<BR><BR>REMOVED & REPLACED BATTERY AT BATTERY PACK M1695 IAW AMM 33-51-06-960-805-NG.<BR><BR>CLOSED DADO PANEL IAW AMM 21-23-03-400-802 STEP 6.D(1)<BR><BR>ACCOMPLISHED EMERGENCY LIGHTS OPS CHECK IAW AMM 33-51-06-960-805 STEP 4.E(5) THRU 4.F. TEST GOOD;[02] COMPLETE<BR>AUDIT C/W
EMERGENCY EXIT LIGHT BATTERY PACK M2335 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M2335 IAW AMM 33-51-06-960-805; AMM 25-21-46-400-801. OPS CHECK GOOD;[02] COMPLETE<BR>AUDIT C/W
EMERGENCY EXIT LIGHT BATTERY PACK M1671 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1671 IAW AMM 33-51-06-960-805-NG. OPS CHECK GOOD;[02] COMPLETE<BR>AUDIT C/W
EMERGENCY EXIT LIGHT BATTERY PACK M1672 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1672 IAW AMM 33-51-06-960-805;[02] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1672 IAW AMM 33-51-06-960-805. OPS CHECK GOOD;[03] COMPLETE<BR>AUDIT C/W
CIRCUIT BREAKER 'CABIN EMER LIGHTS' ON P6-11 PANEL INBOARD SIDE; BUTTON POOPED OUT AND WILL NOT RESET<[01] REMOVED & REPLACED CABIN EMER LIGHTS CIRCUIT BREAKER A 9 ON P6-11 PANEL IAW SWPM 20-30-00 & 20-83-11<BR>OPS CHECKED CABIN EMER LIGHTS CIRCUIT BREAKER A 9 ON P6-11 PANEL IAW SWPM 20-83-11 SWPM 20-30-00 <BR>OPS CHECK GOOD;[02] COMPLETE<BR>AUDIT C/W
LAV D; DOOR WILL NOT FULLY CLOSE POSSIBLE CORROSION AT BOTTOM AFT CORNER AT AFT DOOR POST.<[01] REMOVED DOOR POST IAW CMM 25-40-42 REMOVED UPPER FRAME IAW CMM 25-40-42 AND REMOVED TRIM PCS IAW CMM 25-40-42 INSTALLED NEW POST IAW CMM 25-40-42 REINSTALLED ORIGINAL UPPER FRAME IAW CMM 25-40-42 AND INSTALLED TRIM PCS IAW CMM 25-40-42;[02] AUDIT C/W
FLOOR PANEL 241DF HAS PULLED FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK. REPAIRED FLOOR PANEL 241DF IAW B737 SRM 53-00-50-2R-1.;[02] AUDIT C/W
FLOOR PANEL 231XF UPPER SURFACE HAS 2 AREAS OF DELAMINATION.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK. REPAIRED FLOOR PANEL 231XF IAW B737 SRM 53-00-50-2R-1.;[02] AUDIT C/W
A177-012 CABIN FLOOR PANEL 231CF HAS PULLING FIBERS AND A SCRIBE ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK. CABIN FLOOR PANEL 231CF REPAIRED IAW B737 SRM 53-00-50-2R-1.;[02] AUDIT C/W
A177-011 CABIN FLOOR PANEL 231BF HAS MULTIPLE DENTS AND PULLING FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK. REPAIRED CABIN FLOOR PANEL 231BF IAW B737 SRM 53-00-50-2R-1.;[02] AUDIT C/W
DOT A24-70 MID CABIN FLOOR INTERCOSTAL AT STATION 540 IS CRACKED AT RBL 1.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] C/W REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069;[03] VERIFIED ITEMS 1 AND 2<BR>AUDIT C/W;[04] C/W
DOT#09 A-043 CABIN FLOOR STRUCTURE AFT WET AREA CORRODED AROUND LAV MOUNT STA 947 RBL 25 WL 208<[01] 01 - REMOVED AND REPLACED INTERCOSTAL LOCATED AT RBL 25 AND WL 208 BETWEEN BSTA 974 TO BSTA 767 PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] COMPLETE;[03] COMPLETE<BR>AUDIT C/W
DOT A24-71 MID CABIN FLOOR INTERCOSTAL AT STATION 540 IS CRACKED AT LBL 1.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] VERIFIED ITEM 1;[03] C/W REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069;[04] VERIFIED ITEM 3<BR>AUDIT C/W
DOT#13 A-043 CABIN FLOOR STRUCTURE AFT WET AREA ANGLE CORRODED AROUND 2EA NUTPLATE HOLES STA 986+7' RBL 40 WL 208<[01] REMOVED CORROSION ON ANGLE AROUND 2EA NUTPLATE HOLES STA 986+7' RBL 40 WL 208 I.A.W. 51-10-02-0G-0 ITEM 15 VERIFIED WITH 10X MAGNIFYING GLASS<BR><BR>BLEND OUT FOUND TO BE OUT OF LIMITS ALLOWABLE DAMAGE LIMITS FOR THE ANGLE LOCATED ON BS 986+7' AT RBL 40 AND WL 208 NO WERE FOUND ON B737 SRM 53-70-51-1A-1.<BR><BR>UT MEASURED IAW B737 NDT P4 51-00-00 P2 TOOL 36285 DUE 02NOV25<BR><BR>FOUND .050' ORIGINAL; .029' REMAINING; .021' LOSS<BR><BR>FINDINGS MARKED ON PART<BR><BR>REMOVED AND INSTALLED NEW SUPPORT ANGLE I.A.W. SRM 51-40-02-0G-0;[02] REMOVED CORROSION ON ANGLE AROUND 2EA NUTPLATE HOLES STA 986+7' RBL 40 WL 208 I.A.W. 51-10-02-0G-0 ITEM 15 VERIFIED WITH 10X MAGNIFYING GLASS<BR><BR>BLEND OUT FOUND TO BE OUT OF LIMITS ALLOWABLE DAMAGE LIMITS FOR THE ANGLE LOCATED ON BS 986+7' AT RBL 40 AND WL 208 NO WERE FOUND ON B737 SRM 53-70-51-1A-1.<BR><BR>UT MEASURED IAW B737 NDT P4 51-00-00 P2 TOOL 36285 DUE 02NOV25<BR><BR>FOUND .050' ORIGINAL; .029' REMAINING; .021' LOSS<BR><BR>FINDINGS MARKED ON PART<BR><BR>REMOVED AND INSTALLED NEW SUPPORT ANGLE I.A.W. SRM 51-40-02-0G-0 AND I.A.W. B-737 DWG NO. 147A5700 REV.A;[03] COMPLETE <BR> C/W AUDIT
DOT#19 A-043 AFT CARGO COMPARTMENT LEEK ANGLE CRACKED AT STA 867 LBL 11 WL 156<[01] REMOVED CRACKED LEEK ANGLE AT STA 867 LBL 11 WL 156 IN AFT CARGO COMPARTMENT AND REPLACED WITH NEW ANGLE; PN 149A8109-114 ATAG A275021; IAW SRM 51-40-02-0G-0 AND BOEING DWG 149A8102 ID:0019 REV:A;[02] VERIFIED ITEM 1<BR>AUDIT C/W
DOT A24-20 AFT PIT RH INTERCOSTAL BETWEEN STATIONS 747 AND 767; RBL 22; WL 156 IS CORRODED ON LOWER SIDE.<[01] REMOVED CORROSION FROM LOWER SIDE OF AFT PIT RH INTERCOSTAL BETWEEN STATIONS 747 AND 767; RBL 22; WL 156 IAW SRM 51-10-02-0G-0; .032' ORIG 'T' .022' REMAINING LOSS .010' FOUND OUT OF LIMITS IAW SRM 53-00-04-1A-1 FIG 102 <BR>TOOL USED AAR#24508 DUE 02/01/25<BR>REMOVED CORRODED INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL; PN 146A7505-12 ATAG WN49011; IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A7502 ID:0050 REV:-;[02] AUDIT C/W
DOT#17 A-043 CABIN FLOOR STRUCTURE AFT WET AREA; CORROSION AROUND LAV MOUNT STA 947 LBL 25 WL 208<[01] 04 - REPAIRED CABIN FLOOR BEAM AT BSTA 947.5 BETWEEN LBL 8 TROUGH LBL 56 AND WL 208 PER [SRM 53-70-51-2R-5-B00675 (REPAIR 5 - SECTION 47 - LARGE CORROSION DAMAGE ON THE UPPER CHORD OF THE FLOOR BEAM AT STA 947.5 - PERMANENT)]<BR><BR>CABIN FLOOR STRUCTURE AFT WET AREA; FLOOR BEAM BSTA 947.5 AT WL 208 BETWEEN LBL 8 TO LBL 56;[02] VERIFIED STEP 1<BR>AUDIT CW
DOT#15 A-043 CABIN FLOOR STRUCTURE AFT WET AREA; 'T' CAP CORRODED AROUND DOMENUT HOLE STA 986 LBL 42 WL 208<[01] CORROSION AT STA 986 LBL 42T CAP AROUND DOMENUT HOLE WAS REMOVED AND REPAIRED I.A.W. SRM 53-70-51-2R-6; ALTERNATIVE 3.;[02] COMPLETE <BR>AUDIT C/W;[03] COMPLETE <BR>AUDIT C/W
DOT#12 A-043 CABIN FLOOR STRUCTURE AFT WET AREA 'T' CAP CORRODED AROUND DOMENUT HOLE STA 986 RBL 42 WL 208<[01] 04 - REPAIRED FLOOR BEAM UPPER T CHORD AT STA 986; RBL 42 AND WL 208 PER [SRM 53-70-51-2R-6-B00676 (REPAIR 6 - SECTION 47 - SMALL CORROSION DAMAGE ON THE UPPER CHORD OF THE FLOOR BEAM AT STA 986.5 - PERMANENT)];[02] COMPLETE;[03] COMPLETE <BR>AUDIT C/W
A177-003 CABIN FLOOR PANEL 222BF IS GOUGED ON UPPER SURFACE AND HAS FIBERS PULLING.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK. CABIN FLOOR PANEL 222BF REPAIRED IAW SRM 53-00-50-2R-1.;[02] AUDIT C/W
A177-001 CABIN FLOOR PANEL 221BF IS BROKEN ON UPPER SURFACE AND HAS FIBERS PULLING.<[01] REPLACED FLOOR PANEL 221BF WITH NEW PART (PART#141A5810-729 BN#492222) PER STANDARD INDUSTRY PRACTICES. FLOOR PANEL WAS INSTALLED ON FAULT #TTG8Q00WA89R<BR>INFO ONLY: A-TAG#WN49012;[02] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK;[03] ALL STEPS EA 24-153-03220 COMPLETED;[04] AUDIT C/W
A177-010 CABIN FLOOR PANEL 231AF HAS DELAMINATION AND PULLING FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK. REPAIRED CABIN FLOOR PANEL 231AF IAW B737 SRM 53-00-50-2R-1.;[02] AUDIT C/W
A177-009 CABIN FLOOR PANEL 221EF HAS PULLING FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK; REPAIRED CABIN FLOOR PANEL IAW SRM 53-00-50-2R-1;[02] AUDIT C/W
DOT A24-55 AFT PIT RH FORWARD SHIELD I/B SUPPORT WEB CORRODED AROUND NUT PLATES ON LOWER SIDE. STATION 767-787 WL 156 RBL 24.<[01] REMOVE CORROSION ON LOWER SIDE OF AFT PIT RH FORWARD SHIELD I/B SUPPORT WEB STATION 767-787 WL 156 RBL 24 SRM 51-10-02-0G-0; ;050 ORIG 'T' REMAINING .035 LOSS .015 FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1 FIG 103 <BR>TOOL USED MIC :AAR#1714 DUE 10/10/25<BR>INSTALLED NEW SHIELD SUPPORT WEB IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A0081 ID:0049 REV:A;[02] VERIFIED ITEM 1;[03] AUDIT C/W
EGPR DOOR EXISTING REPAIR AT LOWER CUTOUT IS MISSING THE REPAIR FILLER.<[01] FABRICATED AND INSTALLED REPAIR FILLER IAW SRM 53-10-15-2R-4;[02] AUDIT C/W
A24-2 AFT PIT FLOOR STRUCTURE STRAP AT DOOR OPENING CORRODED BS 792-847 WL 156 RBL 18<[01] REMOVE CORROSION IAW SRM 51-10-02-0G-0 ITEM 15 AND CHECK WITH 10X MAGNIFYIN GLASS<BR>EVALUATED ALLOWABLE LIMITS 103 ORIG 'T' .084 REMAINING .019 LOSS FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1 FIG 103<BR>REMOVED DAMAGE STRAP IAW SRM 51-40-02-0G-0<BR>VERIFIED PART USING ATAG WN48987 PART NUMBER 146A8128-14AND 146A8120<BR>REV: A<BR>INSTALLED IAW SRM 51-40-02-0G-0 & BOEING DWG 146A8120 REV: A<BR>APPLIED CIC IAW SRM 53-60-15-2R-1 STEP: 4.B(9);[02] COMPLETE;[03] COMPLETE<BR>AUDIT C/W
DOT A24-77 FWD CARGO COMPARTMENT GUSSET CRACKED AT STA 500I STR 18R<[01] REMOVED AND REPLACED CRACKED GUSSET AT FWD CARGO COMPARTMENT STA 500I 18R IAW RM 51-40-02 BOEING DWG 143A7902 REV B AMM 51-21-91;[02] AUDIT C/W
(A125-7) FORWARD CARGO COMPARTMENT; FLOOR STRUCTURE @ DOOR OPENING CORRODED BS440-490; WL156; RBL18-28<[01] 01 - REMOVED AND REPLACED FWD CARGO LOWER MAIN SILL WEB PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]<BR>AND BOEING DWG 143A8330 REV. B.;[02] C/W<BR>AUDIT C/W
AFT CARGO; FWD TIEDOWN PLATE IS CORRODED<[01] REMOVED DAMAGE IAW SRM 53-00-53-1A-1 STEP: 5.B(1)<BR>EVALUATED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 STEP: 5.B(1)<BR>MATERIAL VERIFICATION IAW SRM 53-00-53-1A-1<BR>ATAG: 274044<BR>P/N: 453A2611-1<BR>INSTALLED TIEDOWN PLATE IAW SRM 51-40-02-0G-0;[02] VERIFIED ITEM 1<BR>AUDIT C/W
AFT CARGO DOOR; AFT CORNER SCUFF PLATE IS CRACKED<[01] CRACK ON AFT CARGO DOOR; AFT CORNER SCUFF PLATE WAS REPAIRED ON BACK SHOP W/O 46221/1600/0001 SERIAL NO: 9482708 IAW SRM 53-60-15-2R-1;[02] VERIFIED ITEM 1<BR>AUDIT C/W
(A125-3) AFT CARGO COMPARTMENT; FLOOR STRUCTURE; DOOR SHIELD CORRODED BS847-867; WL156; RBL24<[01] 01 - REMOVED AND REPLACED FLOOR STRUCTURE SHIELD ON AFT CARGO COMPARTMENT BETWEEN STA 847 TROUGH STA 867 AT RBL 24 AND WL 156 PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] AUDIT C/W
(A125-4) AFT CARGO COMPARTMENT; FLOOR STRUCTURE; Z-ANGLE CORRODED BS727-846; WL156; LBL24<[01] REMOVED; FABRICATED AND REPLACED (INSTALLED) NEW AFT CARGO COMPARTMENT; FLOOR STRUCTURE; Z-ANGLE; WL156; LBL24 WITH EXISTING REPAIR SPLICE AT STA 727J+3' AND 727F-19.250' I.A.W SRM 53-00-53-2R-5 AND SRM 51-40-02-0G-0 AND APPLIED CIC I.A.W AMM 51-21-91-701;[02] VERIFIED ITEM 1<BR>C/W;[03] AUDIT C/W
(A125-6) AFT CARGO COMPARTMENT; FLOOR STRUCTURE; Z-ANGLE CORRODED BS727-767; WL156; RBL24<[01] REMOVED; FABRICATED AND INSTALLED NEW Z-ANGLE FS 727F-3.5' TO 767; NEW SPLICE LOCATED FS 727F-3.5' WL156; RBL24 AND APPLIED CIC; I.A.W. SRM 51-40-02-0G-0; SRM 53-00-53-2R-5 AND AMM 51-21-91-620-802;[02] VERIFIED ITEM 1<BR>C/W
(A125-1) AFT CARGO COMPARTMENT; FLOOR STRUCTURE @ DOOR OPENING CORRODED BS792-847; WL156; RBL19-28<[01] REMOVED CORROSION AND VERIFIED WITH 10X MAGNIFIER ALL REMOVED IAW SRM 51-10-02-0G-0VERIFIED LIMITS; ORIGINAL THICKNESS .050'; REMAINIG THICKNESS .026'; MATERIAL LOSS OF .024'; LOSS OF UP TO .005' ALLOWED-OUT OF LIMITS IAW SRM 53-60-15-1A-1 INSTALLED NEW WEB I/A/W BOEING DWG 146A8120 REVA;[02] C/W<BR>AUDIT C/W
DOT L7-022: R2 DOOR PANEL 844DZ IS BENT ALOG EDGE OF PANEL AND CRACKED AT RIVET HOLE<[01] REPLACED R-2 DOOR PANEL 844DZ I/W/A SRM 51-40-02-0G-0 A TAG WN48921;[02] VERIFIED ITEM 1<BR>AUDIT C/W
CABIN OVERWING EXIT SIGN SCREW MISSING<[01] REINSTALLED EXIT SIGN LENS PER AMM 33-51-01
CA SIDE AFT DOOR FRAME BROKEN<[01] SECURED DOOR FRAME PER SIP
MID CABIN EMERGENCY EXIT LIGHT LENS IS MISSING.<[01] INSTALLED OVERHEAD EMERGENCY EXIT SIGN LENS PER <BR>MM 33-51-01.
MID CABIN EXIT LIGHT COVER MISSING<[01] REINSTALLED EXIT LIGHT COVER PER AMM 33-51-01.
AFT ENTRY EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED AFT ENTRY DOOR EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-6. O CHECK GOOD.;[02] OPS CHECK GOOD.
GIRT BAR HOOK IS LOOSE<[01] RESECURED PER SIP
MIDDLE CABIN EMERGENCY EXIT LIGHT COVER WILL NOT STAY SECURED<[01] RESECURED MID CABIN EMERGENCY EXIT LIGHT COVER <BR>PER AMM 33-51-01
FWD RIGHT EMERGENCY DOOR EXIT LIGHT FLICKERING, SEAT 14 DEF CEILING LIGHT. OK TO CONTINUE IAW MEL 33-2-04. REPLACED THE SEAT 14 DEF OVERWING EXIT LIGHT IAW AMM 33-21-00. OPS CHECKED GOOD.
R2 DOOR EMERGENCY EXTERIOR LIGHT INOP. / [01] RELAMPED R2 DOOR EMERGENCY EXTERIOR LIGHT AS PER REF B737 &NBSP;&NBSP;&NBSP;&NBSP;&NBSP;AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.
SEVERAL PASSENGER CABIN EMERGENCY LIGHTS INOP. / [01] PERFORMED TROUBLESHOOTING AS PER WM 33-51-12; FOUND BATTERY PACK POSITIONS M02816 AND M01675 INOPERATIVE.;[02] REMOVED AND REPLACED BATTERY PACKS POSITIONS M02816 AND M01675 AS PER REFERENCE AMM 33-51-06-960-805; PERFORMED INSTALLATION TEST. TEST NORMAL OPERATION.;[03] VERIFIED STEPS 1 AND 2; TEST NORMAL
SEVERAL PASSENGER CABIN EMERGENCY LIGHTS INOP. / [01] PERFORMED TROUBLESHOOTING AS PER WM 33-51-12; FOUND BATTERY PACK POSITIONS M02816 AND M01675 INOPERATIVE.;[02] REMOVED AND REPLACED BATTERY PACKS POSITIONS M02816 AND M01675 AS PER REFERENCE AMM 33-51-06-960-805; PERFORMED INSTALLATION TEST. TEST NORMAL OPERATION.;[03] VERIFIED STEPS 1 AND 2; TEST NORMAL
L/H FWD OVER-WING EXTERIOR EMERGENCY LIGHT INOP. / [01] RELAMPED L/H FWD OVER-WING EXTERIOR EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.
FOUND SEVERAL SPOTS OF CORROSION WHERE THE SIDE PLATE (Z CHANNEL) ATTACHES TO THE FLOOR STRUCTURE; INTERCOASTALS AND T ANGLES FROM STA 727+4' TO STA 767 AND RBL 22.21 / [01] CLEANED SEVERAL SPOTS OF CORROSION WHERE THE SIDE PLATE (Z CHANNEL) ATTACHES TO THE FLOOR STRUCTURE; INTERCOASTALS AND T ANGLES FROM STA 727+4' TO STA 767 AND RBL 22.21 AS PER SRM 51-10-02-0G-0.[07] RECEIVED; LOCATED AND DRILLED REPAIR ZEE CHANNEL FOR RIGHT SIDE STA 727+4 AND STA 767; RBL 22.21 IN REFERENCE WITH SRM 51-40-05-0G-0 AND SRM 51-40-06-0G-0; ZEE CHANNEL PART ORDERED IN REFERENCE WITH SRM 53-00-53-2R-5.;[08] VERIFIED STEP 6 AND 7;[09] LOCATED AND DRILLED HOLES ONTO SPLICE REPAIR AND FABRICATED RIGHT ZEE CHANNEL AND SPLICE REPAIR AT STA 727F IN REFERENCE WITH SRM 53-00-53-2R-5 REPAIR 5 ; SRM 51-40-05-0G-0 AND SRM 51-40-06-0G-0.;[10] VERIFIED STEP NO 9. OK TO TREAT AND PRIME Z CHANEL AND SPLICE REPAIRS.;[11] TREATED AND PRIMED RIGHT ZEE CHANNEL AND SPLICE REPAIR IN REFERENCE WITH AMM 51-21-41-370-801; AND AMM 51-21-72-370-804.;[12] VERIFIED STEP 11; OK TO ASSEMBLE REPAIR PARTS;[13] INSTALLED SPLICE REPAIR PARTS ON RIGHT 'Z' CHANNEL AS PER SRM 53-00-53-2R-5 REPAIR 5.;[16] INSTALLED 'Z' CHANNEL R/H FROM STA 727+4' TO STA 767 AND RBL 22.21 AS PER SRM 51-40-02-0G-0 WORK WAS ACCOMPLISHED BY JUSTIN MARTINEZ;[17] VERIFIED STEP 16
FOUND SEVERAL SPOTS OF CORROSION WHERE THE SIDE PLATE (Z CHANNEL) ATTACHES TO THE FLOOR STRUCTURE; INTERCOASTALS AND T ANGLES FROM STA 767 TO STA 787 AND RBL 22.21 CORROSION IS AT SHIELD LOCATED AT STA 767-787 AND RBL-22.21 / [01] CLEANED SEVERAL SPOTS OF CORROSION WHERE THE SIDE PLATE (Z CHANNEL) ATTACHES TO THE FLOOR STRUCTURE; INTERCOASTALS AND T ANGLES FROM STA 767 TO STA 787 AND RBL 22.21 AS PER SRM 51-10-02-0G-0.;[02] VERIFIED STEP 1;[03] VERIFIED STEP 1; HOWEVER REJECTED BECAUSE CORROSION STILL PRESENT AT SOME SPOTS (MARKED);[04] REMOVED CORROSION FOUND TO BE OUT OF LIMITS DUE TO CORROSION PASSING THRU THE SIDE PLATE (Z CHANNEL)(SHIELD) ATTACHES TO THE FLOOR STRUCTURE; INTERCOASTALS AND T ANGLES FROM STA 767 TO STA 787 AND RBL 22.21 PER SRM 51-10-02-0G-0.;[05] VERIFIED STEP 4; CORROSION AT SHILED LOCATED AT STA 767-787 AND RBL-22.21 PASSES THROUGH MATERIAL. OUT OF LIMITS.;[06] REMOVED SHIELD LOCATED AT STA 767 TO 787 AND RBL 22.21 PER SRM 51-40-02-0G-0.;[07] VERIFIED STEP 6;[08] RECEIVED NEW SHIELD; LOCATED AND DRILLED TO SIZE PER SRM 51-40-05-0G-0.;[09] VERIFIED NEW SHEILD & VERIFIED DRILLED ON LOCATION ALL FASTENER HOLES & DEBURED.( OK TO TREAT & PRIME ALL BARE METAL AREAS.;[10] TREATED AND PRIMED ALL BARE METAL AREAS PER AMM 51-21-72-370-804 AND 51-21-41-370-804.;[11] VERIFIED STEP #10 ; OK TO PROCEED WITH INSTALLATION PROCESS AS PER SRM/ IN USE.;[12] INSTALLED NEW FWD SHIELD PER SRM 51-40-02-0G-0.;[13] VERIFIED STEP #12 AS COMPLETE ( JOB CLOSED ).
FOUND SEVERAL SPOTS OF CORROSION WHERE THE SIDE PLATE (Z CHANNEL) ATTACHES TO THE FLOOR STRUCTURE; INTERCOASTALS AND T ANGLES FROM STA 727+4' TO STA 847 AND LBL 22.21 / [01] REMOVED CORROSION ON SEVERAL SPOTS TO SIDE PLATE (Z CHANNEL) ATTACHED TO THE FLOOR STRUCTURE; INTERCOASTALS AND T ANGLES FROM STA 727+4' TO STA 847 AND LBL 22.21 AS PER SRM 51-10-02-0G-0 AND FOUND ONE SECTION OF CORROSION PASSING THROUGH 'Z' CHANNEL. 'Z' CHANNEL NEEDS REPLACEMENT.[10] INSTALLED SPLICE REPAIR PARTS AND INSTALLED ALL NUTPLATES ON LEFT 'Z' CHANNEL AS PER SRM 53-00-53-2R-5 REPAIR 5 AND SRM 51-40-10-2R-0.
FWD CARGO BILGE STA 500H FWD SIDE - BAFFLE CLIP IS CRACKED LBL 21 S-26L WL 156 AS MARKED. 124-006 / [01] REMOVED AND REPLACED CLIP AT FWD CARGO BILGE STA 500H FWD SIDE LBL 21 S-26L IRE SRM 51-40-02;[02] VERIFIED STEP 1
FWD CARGO BILGE SIDEPLATE SUPPORT Z STA 500B+15 TO STA 500I RBL 21 S-26R WL 156 HAS CORROSION AS MARKED. 124-003 / [01] REMOVED CORROSION ON Z CHANNEL FROM STA 500B TO STA 500I RBL 21 S-26R WL 156. MATERIAL REMOVED 0.010'; MATERIAL REMAINING 0.030'; ORIGINAL MATERIAL 0.040'; Z CHANNEL AFFECTED AREAS FOUND OUT OF LIMITS. IN REFERENCE WITH SRM 53-00-53-1A-2.;[02] REMOVED CORROSION ON Z CHANNEL FROM STA 500B TO STA 500I RBL 21 S-26R WL 156. MATERIAL REMOVED 0.010'; MATERIAL REMAINING 0.030'; ORIGINAL MATERIAL 0.040'; Z CHANNEL AFFECTED AREAS FOUND OUT OF LIMITS. IN REFERENCE WITH SRM 53-00-53-1A-2. TOOL USED : B/C 171960 ; CAL DUE: 07-MARCH-2023.;[03] LOCATED AND DRILLED NEW Z SIDE PLATE FROM BAC1496-444 7075-T62 PO# 1747909 IRW SRM 51-40-05;[04] VERIFIED STEPS 1; 2 AND 3<BR>OK TO TREAT AND PRIME;[05] TREATED PRIMED NEW Z SIDEPLATE IRW AMM 51-21-41-370-803;AMM 51-21-72-370-804;[06] VERIFIED STEP 5;OK TO INSTALL NEW Z SIDE PLATE FROM STA 500B TO STA 500I RBL 21 S-26R W/L 156;[07] INSTALLED NEW Z SIDE PLATE FROM STA 500A TO STA 500I RBL21 IRW SRM 51-40-02;[08] VERIFIED STEP 7
LT WING T/E STRUCTURE AT DEFLECTION CONTROL RIB;SHOWS FIXED UPPER PANEL ATTACH BRACKET CRACKED AT FWD SIDE;MKD / [01] REMOVED AND REPLACED LT WING T/E STRUCTURE AT DEFLECTION CONTROL RIB FIXED UPPER PANEL ATTACH BRACKET AT FWD SIDE IRW SRM 51-40-02;[02] VERIFIED STEP 1
LH WING ACCESS PANEL FWD O/B SUPPORT CRACKED; UNDER SPOILER NO. 2 / [01] REMOVED AND REPLACED LEFT WING ACCESS PANEL FWD O/B SUPPORT UNDER SPOILER #2 IRW SRM 51-40-02.;[02] VERIFIED STEP 1;COMPLETE
#2 OIL QTY TO 18% IN CRUISE ; / [01] R&R'ED #2 ENG LUBE UNIT PER AMM 79-21-01
1 AFT CABIN FLASHLIGHT INOPERABLE OKAY TO CONTINUE, PER MEL 25-12-01 SP1B TRACKING 100140 (CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS). R & R FLASHLIGHT BATTERY, PER MM 25-64-00. OPERATIONS OK CL NR 81082.
LEFT HORIZONTAL STB FWD UPPER SLIDING SEAL CRACKED / REMOVED & REPLACED LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW AMM 53-31-31.AMT 135306INSP 67932
R1 DOOR SLIDE HARD TO PLACE INTO GIRT BAR HANGER. REPOSITIONED SLIDE PER MT.
R1 DOOR SLIDE GIRT BAR OUT OF ADJUST. R&R SLIDE ASSEMBLY PER AMM.
MID CABIN OVERHEAD EXIT SIGN LENS MISSING. REINSTALLED LENS PER SIP.