N8655D
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 | 2018-05-07 – 2018-05-07 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2018-05-07 – 2018-05-07 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
LOWER EXIT SIGN MISSING FROM ROW 14AC. INSTALLED LOWER EXIT SIGN IAW AMM REF 33-51-01.
LOWER PLACARD AT ROW 14A EMERGENCY EXIT MISSING. RESECURED LOWER PLACARD AT ROW 14A EXIT PER SIP.
PHOTOLUMINESCENT FLOOR PROXIMITY LIGHT STRIP LIFTING AT 12C. SECURED WITH DOUBLE SIDED TAPE IAW AMM 33-51-15.
MID CABIN EXIT SIGN ON CEILING LOOSE. SECURED EXIT SIGN PER MM 33-51-01
AFTER TAKEOFF RAISED GEAR HANDLE TO UP POSITION, GEAR CAME UP UPON MOVING GEAR HANDLE TO OFF POSITION RECEIVED A RED NOSE GEAR LIGHT AND COULD HEAR THAT THE GEAR EXTENDED. OK CONTINUE PER MEL 32-16-01, SP1. ADJUSTED RT NLG DOOR AFT STOP IAW AMM 32-22-11-000-802. PERFORMED OPS TEST OF NLG IAW AMM 32-33-00-710-801. OP CHKD OK. INSPECTED IAW AMM 32-22-11-000-802-NG.
L2 DOOR SLIDE COVER WINDOW NOT SECURE. SECURED L2 DOOR SLIDE COVER IAW SOPM 20-50-12.
L1 DOOR ASSIST HANDLES (BOTH) LOOSE. SECURED BOTH L1 DOOR ASSIST HANDLES IAW AMM 52-11-31.
R1 DOOR ASSIST HANDLE LOOSE DOOR SIDE. SECURED R1 DOOR ASSIST HANDLE IAW B737-800 AMM 52-41-31.
R2 DOOR ASSIST HANDLE LOOSE. SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 52-41-31.
FWD FA FLASHLIGHT INOP<[01] R & R FWD F.A. FLASHLIGHT BATTERY. OPS CK GOOD PER AMM 25-64-00
FWD L/H ENTRY EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED FWD L/H EMERGENCY POWER SUPPLY AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-805;[02] REMOVED AND REPLACED FWD L/H EMERGENCY POWER SUPPLY AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-805
R/H O/B AFT FLAP HAS SIGN OF DELAMINATION AT THE I/B AFT CORNER AREA. R/H O/B AFT FLAP HAS SIGNS OF DEMLAMINTION AT THE I/B AFT CORNER AREA.<[01] R/H O/B AFT FLAP REMOVED AND REPLACED IAW B737-800 AMM 27-51-22;[02] VERIFIED R/H O/B AFT FLAP REMOVED AND REPLACED IAW B737-800 AMM 27-51-22
CR: (MH) FLOOR PANEL 231LF DELAM/ PUNCTURE REQ. REMOVE AND REPLACE<[01] REMOVED AND REINSTALLED FLOOR PANEL 231LF IAW B737 AMM 53-21-00<BR>TOOL: T03830-22<BR>DUE: 23/JAN/25;[02] REMOVED AND REINSTALLED FLOOR PANEL 231LF IAW B737 AMM 53-21-00<BR>TOOL: T03830-22<BR>DUE: 23/JAN/25<BR> VERIFIED
CR: (MH) FLOOR PANEL 241RF DELAM REQ. REMOVE AND REPLACE<[01] REMOVED AND REPLACED PANEL 241RF IAW B737NG AMM 53-21-00-401;[02] REMOVED AND REPLACED PANEL 241RF IAW B737NG AMM 53-21-00-401
RIGHT WING TRAILING EDGE WEB AT AFT PYLON AREA HAS A CRACKED BRACKET. STREAMERED<[01] REMOVED AND REPLACED BRACKET 115A6260-2 PO#1084100.3 IAW B737-800 SRM 51-40-02 AND BAC DWG#115A6200 REV.A;[02] REMOVED AND REPLACED BRACKET 115A6260-2 PO#1084100.3 IAW B737-800 SRM 51-40-02 AND BAC DWG#115A6200 REV.A
LEFT WING TRAILING EDGE WEB AT AFT PYLON AREA HAS A CRACKED BRACKET OUTBOARD END OF WEB.<[01] REMOVED AND REPLACED BRACKET 115A6260-1 PO#110490.1 IAW B737-800 SRM 51-40-02 AND BAC DWG#115A6200 REV.A;[02] REMOVED AND REPLACED BRACKET 115A6260-1 PO#110490.1 IAW B737-800 SRM 51-40-02 AND BAC DWG#115A6200 REV.A
CR: (MH) FLOOR PANEL 232JF DELAM REQ. REMOVE AND REPLACE<[01] C/W T/C REMOVED AND REPLACED FLOOR PANEL 232JF;[02] REMOVED AND REPLACED NEW FLOOR PNL 232JF IAW B737-800 AMM 53-21-00-401;[03] VERIFIED REMOVED AND REPLACED NEW FLOOR PNL 232JF IAW B737-800 AMM 53-21-00-401
EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER CRACKED<[01] ACCOMPLISHED REPAIR OF EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER IAW B737-800 SRM 53-10-15-2R-4;[02] VERIFIED ACCOMPLISHED REPAIR OF EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER IAW B737-800 SRM 53-10-15-2R-4;[03] VERIFIED ACCOMPLISHED REPAIR OF EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER IAW B737-800 SRM 53-10-15-2R-4;[04] VERIFIED ACCOMPLISHED REPAIR OF EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER IAW B737-800 SRM 53-10-15-2R-4
FWD CARGO COMPARTMENT AFT BULKHEAD PANEL 121HW HAS 2EA DELAMINATED MARKS (DOT K049)<[01] REPAIRED PANEL 121HW OF 2 PUNCTURES IAW B737-800 AMM 25-00-00-300-801;[02] 02 - INSPECTED PER [AMM 25-00-00-300-801-NG (CRUSHED-CORE AND SANDWICH PANEL REPAIR - PERMANENT)]
L/H VAPOR BARRIER ANGLE CRACKED AT APPROX LBL 8.<[01] REMOVED DAMAGE; FORMED PARTS; ALODINED; PRIMED AND INSTALLED REPAIR PARTS AT VAPOR BARRIER ATTACH ANGLE L/H. STA LBL 5 TO LBL20 APROX. IAW B737-800 SRM 57-10-10-5-2R. ACCOMP. HFEC CUT EDGES; IAW B737 NDT MAN. 51-00-00 PROC.23; PT6. NO CRACK INDICATIONS FOUND. CAP SEALED TANK FASTENERS IAW B737 AMM 51-31-00-390-805.;[02] 02 - INSPECTED PER [SRM 57-10-10-2R-5-B01456 (REPAIR 5 - WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR - PERMANENT)]
R/H VAPOR BARRIER ANGLE CRACKED AT APPROX RBL 8<[01] REMOVED; LOCATED; DRILLED; AND INSTALLED NEW VAPOR BARRIER ATTACH ANGLE; CHANNEL; STIFENER AND FITTING AT WING SECTION REAR SPART R/H FROM STA RBL 5 TO RBL 65 IAW B737-800 SRM 57-10-10-2R-5 ACCOMPLISHED A OPEN HOLE HFEC INSPECTION OF ALL OPEN HOLES ON THE R/H VAPOR BARRIER REPLACEMENT AREA IAW 737 NDT MAN. PT. 6; 51-00-00 PROC. 16. USING T8257I DUE 03 OCT. 25. NO INDICATIONS WERE NOTED AT THIS TIME. CAP SEALED TANK FASTENERS IAW B737 AMM 51-31-00-390-805.;[02] REMOVED; LOCATED; DRILLED; AND INSTALLED NEW VAPOR BARRIER ATTACH ANGLE; CHANNEL; STIFENER AND FITTING AT WING SECTION REAR SPART R/H FROM STA RBL 5 TO RBL 65 IAW B737-800 SRM 57-10-10-2R-5 ACCOMPLISHED A OPEN HOLE HFEC INSPECTION OF ALL OPEN HOLES ON THE R/H VAPOR BARRIER REPLACEMENT AREA IAW 737 NDT MAN. PT. 6; 51-00-00 PROC. 16. USING T8257I DUE 03 OCT. 25. NO INDICATIONS WERE NOTED AT THIS TIME. CAP SEALED TANK FASTENERS IAW B737 AMM 51-31-00-390-805.
CABIN SEAT ROW LOOSE IN FLOOR TRACK 12DEF; 2DEF; 3DEF<[01] RE-SECURED PASSENGER SEAT ROWS AT 3DEF; 12DEF; AND 2DEF PER AMM 25-22-00.
LEFT AFT EMERGENCY EXIT SIDEWALL; EMERGENCY EXIT LIGHT LENS MISSING.(PHOTO ATTACHED.)<[01] INSTALLED REPLACEMENT EMERGENCY EXIT LIGHT LENS COVER PER SIP.
L1 DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] REVAMPED L1 EMERGENCY DOOR LIGHT IAW AMM 33-51-04 OPS CHECK GOOD
CABIN FLOOR BOARD PANEL BREAK ASSEMBLY AT STA. 540 CRACKED AT INBOARD END RIGHT OF CENTER IN A/C DISTRIBUTION BAY.<[01] REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240.;[02] IS: REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240.<BR><BR>SHOULD BE: REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240 SHEET 3 AND SHEET 11.
AFT ENTRY DOOR INBOARD DOOR HANDLE CAM HOUSING SAFETY WIRE BROKEN.<[01] RE-SECURED AFT ENTRY DOOR INBOARD DOOR HANDLE CAM HOUSING W SAFETY WIRE REF AMM 52-13-00.
CABIN FLOOR BOARD PANEL BREAK ASSEMBLY AT STA. 540 CRACKED AT INBOARD END L/H OF CENTER IN A/C DISTRIBUTION BAY.<[01] REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240.;[02] IS: REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240.<BR><BR>SHOULD BE: REMOVED AND REPLACED PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND DRAWING 143A5240 SHEET 3 AND SHEET 11.
ANTI-SKID INOP LIGHT ILLUMINATED ON TAKEOFF.<[01] FOUND #3 WHEEL SPIN TRANSDUCER CONNECTOR NOT INSTALLED. SECURED PER AMM 20-61-13. OPS CK GOOD PER AMM 32-42-00
OVERWING EXIT CEILING EMERGENCY EXIT SIGN INOP<[01] REMOVED AND REPLACED OVERWING AISLE CEILING EMERGENCY EXIT SIGN. OPS CHECK GOOD. REF AMM 33-51-03
AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP.<[01] RELAMPED AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK NORMAL.
EMERGENCY EXIT SIGN CAME OFF.<[01] RESECURED EXIT ROW SIGN. OPS CHECK GOOD. REF AMM 11-32-01.
OVERWING EXIT SIGN LENS MISSING<[01] INSTALLED EMERGENCY EXIT SIGN LENS AS PER REF AMM 33-51-01
14D SEAT RECLINES INTO EXIT ROW<[01] SECURED SEAT RECLINE AT 14D PER CMM 25-22-46
AFT ENTRY DOOR SLIDE PRESSURE IN RED<[01] REMOVED AND INSTALLED SLIDE PER AMM 25-66-01
EMERGENCY 'EXIT' LIGHT; R/H LOWER SIDE FWD GALLEY LENS IS CRACKED. / [01] REMOVED AND REPLACED EXIT SIGN - LIGHT ASSEMBLY ON R/H LOWER FWD GALLEY PER AMM 33-51-01. EXIT SIGN OPS CHECKED GOOD PER AMM 33-51-00.;[02] VERIFIED DANIEL LEBLANC (TECHNICIAN); 03-NOV-2022 02:34 UTC<BR>REMOVED AND REPLACED EXIT SIGN - LIGHT ASSEMBLY ON R/H LOWER FWD GALLEY PER AMM 33-51-01. EXIT SIGN OPS CHECKED GOOD PER AMM 33-51-00.
FWD CARGO COMPARTMENT LH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 490 TO 500 (MARKED) (REF. TTG8Q00FFPCA) / [01] DUE TO OTHER DAMAGE THAT IS OUT OF LIMITS PER SRM 53-00-53-1A-2; THIS SECTION OF TRANSITION ANGLE FROM STA 480+10' TO STA 500I WILL BE REMOVED AND REPLACED REF FAULT #S TTG8Q00FH1JY AND TTG8Q00FH8OJ.;[02] DUE TO OTHER DAMAGE THAT IS OUT OF LIMITS PER SRM 53-00-53-1A-2; THIS SECTION OF TRANSITION ANGLE FROM STA 480+10' TO STA 500I WILL BE REMOVED AND REPLACED REF FAULT #S TTG8Q00FH1JY AND TTG8Q00FH8OJ.
DOME NUT HAS CORROSION INSIDE OF HOLE AT AFT WET AREA STA. 986.5 RBL 43. / [01] REMOVED DOME NUT AT RBL 43 TO FOM PER SRM 51-40-02. ATTEMPTED TO REMOVE CORROSION FROM HOLE PER SRM 51-10-02. CORROSION IS STILL PRESENT IN HOLE. CONTACTED ENGINEERING FOR FURTHER INSTRUCTION.;[02] REAMED HOLE UP TO .360IN TO REMOVE CORROSION PER SRM 51-10-02. ALTHOUGH REMAINING CORROSION ON UNDER SIDE REMOVAL IS OUT OF LIMITS. THIS DAMAGE WILL CUT OUT AND REPAIRED PER SRM 53-70-51-2R-6 ALTERNATIVE 4.;[03] CUT OUT DAMAGE IAW SRM 53-70-51-2R-6; ALTERNATIVE 4.;[04] ACCOMPLISHED A HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION ALONG THE CUT EDGES TO MAKE SURE THERE ARE NO CRACKS. REFER TO 737 NDT PART 6; 51-00-00; PROCEDURE 4 OR 737 NDT PART 6; 51-00-00; PROCEDURE 23. (NO DEFECTS NOTED)<BR><BR>ACCOMPLISHED AN OPEN HOLE AND COUNTERSUNK HFEC INSPECTION OF (1) INITIAL FASTENER HOLE IN THE REPAIR AREA. REFER TO 737 NDT PART 6; 51-00-00; PROCEDURE 16 AND 737 NDT PART 6 53-00-00 PROCEDURE 3. NO DEFECTS NOTED<BR><BR>ACCOMPLISHED A DETAILED INSPECTION OF THE ADJACENT STRUCTURE IN THE REPAIR AREA. NO DEFECT NOTED;[05] FABRICATED REPAIR PARTS IAW SRM 53-70-51-2R-6; ALTERNATIVE 4. OK TO INSTALL.[07] REPAIRED PER SRM 53-70-51-2R-6; ALTERNATIVE 4 .;[08] C/W INSPECTION.
FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500E-500F REFERENCE [TTG8Q00FFPBL] / [01] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT OF LIMITS DAMAGE AT OTHER LOCATIONS.;[02] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT LIMITS DAMAGE AT OTHER LOCATIONS ON ANGLE.
FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500G-500H REFERENCE [TTG8Q00FFPBL] / [01] SECTION OF TRANSITION ANGLE UP TO STATION 500G+9 WILL BE REPLACED AS NOTED ON CARD TTG8Q00FGJJX DUE TO OUT OF LIMITS DAMAGE AT OTHER LOCATIONS. REMOVED DAMAGE AT STATIONS 500G+11 AND 500G+19 PER SRM 51-10-02. REMOVED .001 INCH OF MATERIAL AT THOSE LOCATIONS. REMAINING MATERIAL THICKNESS IS .039 INCH AND IS WITHIN LIMITS PER SRM 53-00-53-1A-2. OKAY TO TREAT AND PRIME.;[02] INSPECTED AS REQUIRED. OK TO TREAT AND PRIME STA. 500G+11' AND STA. 500G+19. VERIFIED SECTION OF TRANSITION ANGLE UP TO STATION 500G+9 WILL BE REPLACED AS NOTED ON CARD TTG8Q00FGJJX DUE TO OUT OF LIMITS DAMAGE AT OTHER LOCATIONS.;[03] TREATED AND RESTORED PRIMER AT STATIONS 500G+11 AND 500G+19 PER SRM 51-20-01.;[04] TREATED AND RESTORED PRIMER AT STATIONS 500G+11 AND 500G+19 PER SRM 51-20-01. SEE ADDITIONAL SIGNOFFS. C/W INSPECTION;[05] TREATED AND RESTORED PRIMER AT STATIONS 500G+11 AND 500G+19 PER SRM 51-20-01. SEE ADDITIONAL SIGNOFFS. C/W INSPECTION
FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500F-500G REFERENCE [TTG8Q00FFPBL] / [01] REMOVED DAMAGE AT STATION 500F+11. REMOVED .023 INCH OR MATERIAL. REMAINING MATERIAL THICKNESS IS .017 INCH AND IS OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX.;[02] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT LIMITS DAMAGE AT OTHER LOCATIONS ON ANGLE.
AFT CARGO PIT R/H TRANSITION ANGLE HAS NUMEROUS AREAS OF CORROSION FROM STA 727H+12 TO 767 / [01] REMOVED CORROSION PER SRM. 51-10-02 MATERIAL FOUNDED OUT OF LIMITS PER SRM. 53-00-53-1A-02 ;;[02] REMOVE EXITING TRANSITION ANGLE FROM STA.727 H +10 TO STA. 767 LOCATED AND DRILLED TRANSITION ANGLE PART # BAC1496-377 ; PER SRM. 53-00-53-2R-5 TREATED AND PRIMED REPAIR PART PER SRM 51-20-02 ;INSTALLED BONDING NUT PLACES PER SRM 51-40-10;[03] C/W INSPECTION.;[04] INSTALLED NEW SECTION TRANSITION ANGLE FROM STA.727 H +10 TO STA. 767 PER SRM 53-00-53-2R 5;[05] C/W INSPECTION.
AFT WET AREA INTERCOSTAL LOCATED BETWEEN STA 947.5-967; RBL 50 HAS CORROSION ON UPPER SURFACE AT LAV MOUNT BASE. / [01] BLENDED CORROSION ON MACHINED INTERCOSTAL P/N 147A5660-22 PER SRM 51-10-02. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ORIGINAL THICKNESS = .200?; REMAINING THICKNESS = .174?.;[02] VERIFIED CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] REMOVED AND REPLACED INTERCOSTAL BETWEEN STA. 947.5 TO STA. 967 AT RBL 50 PER SRM 51-40-02.;[04] VERIFIED INTERCOSTAL BETWEEN STA. 947.5 TO STA. 967 AT RBL 50 WAS REMOVED AND REPLACED.
FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500C-500D REFERENCE [TTG8Q00FFPBL] / [01] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT LIMITS DAMAGE AT OTHER LOCATIONS ON ANGLE.;[02] INSPECTED AS REQUIRED. THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT LIMITS DAMAGE AT OTHER LOCATIONS ON ANGLE.
FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500B-500C REFERENCE [TTG8Q00FFPBL] / [01] REMOVED DAMAGE PER SRM 51-10-02. REMOVED .001 INCH OF MATERIAL AT STATIONS 500B+2 AND 500B+7. REMAINING MATERIAL AT THOSE LOCATIONS IS .039 INCH AND IS WITHIN LIMITS PER SRM 53-00-53-1A-2. OKAY TO TREAT AND PRIME REWORKED AREAS AT THE TWO GIVEN LOCATIONS.;[02] REMOVED DAMAGE PER SRM 51-10-02 AT STATION 500B+15. REMOVED .013 INCH OF MATERIAL. REMAINING THICKNESS AT THIS LOCATION IS .027 INCH AND IS OUT OF LIMITS PER SRM 53-00-53-1A-2. REPLACE DAMAGED SECTION OF TRANSITION ANGLE AS NOTED IN STEP 1.;[10] CHANGED REPAIR TYPE FROM MINOR TO MAJOR AS PER INSTRUCTIONS IN EA M-22-153-01550.;[11] INSTALLED NEW R/H TRANSITION ANGLE FROM STATION 500B+10 TO 500G+9. ALL WORK REFERENCE TO SRM 53-00-53-2R-5; AND EA M-22-153-01550.;[12] 11. CAO TRAN (TECHNICIAN); 29-OCT-2022 03:14 UTC<BR>INSTALLED NEW R/H TRANSITION ANGLE FROM STATION 500B+10 TO 500G+9. ALL WORK REFERENCE TO SRM 53-00-53-2R-5; AND EA M-22-153-01550.<BR>C/W RII INSPECTION.;[13] C.W. ALL TASKS.
FWD CARGO COMPARTMENT RH FLOOR TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLES STA. 500D-500E REFERENCE [TTG8Q00FFPBL] / [01] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT OF LIMITS DAMAGE AT OTHER LOCATIONS ON ANGLE.;[02] THIS SECTION OF TRANSITION ANGLE TO BE REPLACED ON CARD NUMBER TTG8Q00FGJJX DUE TO OUT LIMITS DAMAGE AT OTHER LOCATIONS ON ANGLE.
AFT LAV. LH; AFT RH MOUNT (INBD); MOUNT HAS CORROSION. AROUND BASE. / [01] BLENDED CORROSION ON MACHINED INTERCOSTAL P/N 147A5660-3 PER SRM 51-10-02. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ORIGINAL THICKNESS = .200?; REMAINING THICKNESS = .175?.;[02] VERIFIED CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] INTERCOSTAL REPLACED ON FAULT TTG8Q00FFYWH.;[04] CORRECTION FOR CA #3 - REPLACED INTERCOSTAL P/N 147A5660-3 UNDER L/H AFT LAV; INBD MOUNT PER SRM 51-40-02.;[05] VERIFIED C/A # 4 : BRIAN PENCE (TECHNICIAN); 25-OCT-2022 21:22 UTC<BR>CORRECTION FOR CA #3 - REPLACED INTERCOSTAL P/N 147A5660-3 UNDER L/H AFT LAV; INBD MOUNT PER SRM 51-40-02.
AFT WET AREA; RH LAV. AFT MOUNT OUTBD; HAS CORROSION AROUND BASE. / [01] BLENDED CORRODED AREA PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ORIGINAL PART THICKNESS = .180?; REMAINING THICKNESS AFTER BLEND OUT = .089?. CORRODED PART #147A5504-8.05] FLAP PEEN THE CUT EDGE OF THE STA-947 FLOOR BEAM FROM APPROXIMATELY RBL 9' TO RBL 59' PER SRM 53-70-51-2R-5;[06] VERIFIED FLAP PEEN ALONG CUT EDGE OF STA.947 FLOOR BEAM REPAIR;[07] OBTAINED PREFABRICATED T-CHORD FROM STORES MPN 53700002-001. LOCATED AND PILOTED VERTICAL FLANGE OF -1 REPLACEMENT T-CHORD PER SRM 53-70-51-2R-5; ALTERNATIVE 2. LOCATED AND PILOTED -2 REPAIR SPLICE ANGLES PER SRM 53-70-51-2R-5; ALTERNATIVE 2 AND EA 22-153-03130-WIP1 (TTG8Q00FKR7P).;[08] ACCOMPLISHED FLAP PEEN OF CUT EDGE OF PART [1] T-CHORD IAW SRM 53-70-51-2R-5 AND SOPM 20-10-03.;[09] INSPECTED FLAP PEEN OF CUT EDGE OF PART [1] T-CHORD;[10] FABRICATED REPAIR PARTS PER SRM 53-70-51-2R-5.14] TREATED AND PRIMED REPAIR PARTS PER SRM 53-70-51-2R-5. OK TO INSTALL REPAIR PARTS.;[[16] INSTALLED REPAIR PARTS PER SRM 53-70-51-2R-5; ALTERNATIVE 2.;[18] REPAIR ACCOMPLISHED IAW SRM 53-70-51-2R-5; ALTERNATIVE 2 AND EA 22-153-03130.;
R/H HORIZONTAL STAB. AFT UPPER SLIDING SEAL FWD TRACK CRACKED / [01] R&R'D TRACK PER SOPM 20-50-01;[02] VERIFIED C/A #1.
WITH THE EMERGENCY LIGHTS IN TEST MODE; NONE OF THE EMERGENCY LIGHTING IN THE FWD GALLEY AREA OPERATE. / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT STA 310;317L;500CL;500CR;565L;565R;727R AND STA 952R PER MM 33-51-06;[02] VERIFIED 1. CHRISTOPHER KENNEDY (TECHNICIAN); 22-OCT-2022 15:31 UTC <BR>REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT STA 310;317L;500CL;500CR;565L;565R;727R AND STA 952R PER MM 33-51-06;[03] OPS CHECKS GOOD PER AMM 33-51-00.;[04] INSPECTED AS REQUIRED. CORRECTIVE ACTION #3
AFT CARGO FLOOR PANEL 140BF HAS MULTIPLE DENTS AND WAVINESS BETWEEN FLOOR SUPPORTS. / [01] FABRICATED FLOOR PANEL AFT. CARGO #140BF PER BOEING DRAWING #453A2610;[02] C/W INSPECTION.
CEILING EXIT SIGN AT EMERGENCY EXIT ROW MISSING FORWARD COVER / [01] INSTALLED NEW COVER ON THE EMERGENCY EXIT SIGN IN THE CEILING. NO OTHER DEFECTS NOTED AT THIS TIME. REF AMM 33-51-00
OVERHEAD EXIT SALIDAS CEILING SIGN BY OVER WING EXIT CAME OFF / [01] SECURED OVERHEAD EMERGENCY EXIT SIGN COVER IAW AMM 33-51-01
AIRCRAFT FORWARD OVERWING EXIT SIGN ON CABIN CEILING HAS COME OFF / [01] RESECURED OVERWING EXIT LIGHT COVER IAW M/M 33-51-01
MID CABIN OVERHEAD EMERGENCY EXIT PLASTIC LENS MISSING [FACING FORWARD] / [01] SNAPPED EMERGENCY EXIT LENS BACK ON PER AMM 33-51-01
R2 SLIDE BECAME DISLODGED / [01] REPACKED R2 SLIDE PER MT 725-61-06.
AISLE OVER WING EXIT SIGN MISSING LENS ; / [01] INSTALLED AISLE OVER-WING EXIT SIGN LENS REF AMM 33-51-01
EMERGENCY EXIT SIGN AFT OF LEFT OVERWING EXIT DOOR AND EMERGENCY LIGHTS AT 16ABC TO 23ABC INOP ; / [01] REMOVED & REPLACED BATTERY PACK CHARGER (M1670) IAW AMM 33-51-06. NO HELP; REQUIRES BATTERY PACK; PLACED BATTERY PACK ON ORDER.; [02] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06
AFT CARGO FLOOR FWD BULKHEAD FLOOR ANGLE BENT / REMOVED AND REPLACED PER SRM 51-40-02.
AFT CARGO RAIL ASSEMBLY HAS CORROSION AT BS 867 +12 RBL 8 / ACCOMPLISHED SRM 53-00-53-2R-3 REPAIR ALT 1 STA 867 + 7 - 887 (S/N A1314370)
AFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT MULTIPLE AREAS BOTH UPPER + LOWER SURFACE B5 767- B5 787 / REMOVED AND REPLACED PER SRM 51-40-02
AFT CARGO FLOOR PANEL SUPPORT STRIP AT B5 767+5 HAS CORROSION AT MULTIPLE SCREW HOLES / REMOVED AND REPLACED WITH NEW FLOOR STRIP PER SRM 51-40-02 (PN # 146A9401-4)
FWD CARGO; AFT BULKHEAD LOWER ANGLE HAS SEVERAL AREAS OF CORROSION STA 500I RBL24 TO LBL24 / REMOVED AND REPLACED FWD CARGO AFT BULKHEAD LOWER ANGLE AT ATA. 500I PER SRM 51-40-02. P/N 143A9485-35 (SA-M 326 ATTACHED: A1314355)
CORROSION ON NUTPLATE STRIP B5 787+3 + B5787+5 UNDERSIDE OF R/H TRANSITION ANGLE / REMOVED AND REPLACED PER SRM 51-40-02 ( PN # 146A8128-G)
AFT CARGO ANGLE BELOW + ATTACH TO R/H TRANSITION ANGLE HAS CORROSION AROUND SEVERAL NUTPLATES (MARKED) B5767-B5787 / REMOVED AND REPLACED PER SRM 51-40-02
AFT CARGO R/H TRANSITION ANGLE HAS MULTIPLE AREAS OF CORROSION B5 727H- 727I / REMOVED AND REPLACED R/H TRANSITION FROM BS 727H+10 THRU 767 PER SRM 53-00-53-2R-5 (S/N A1314364)
FWD CARGO; R/H TRANSITION ANGLE HAS CORROSION AROUND SEVERAL NUTPLATE HOLES STA 500A TO 500I / REPAIRED PER SRM 53-00-53-2R-5 AND EA 20-153-02159 (PN # 146A7502-340) (SA-M 326 ATTACHED: A1314343)
FWD CARGO; L/H TRANSITION ANGLE HAS CORROSION AROUND SEVERAL NUTPLATE HOLES STA 500 TO 500C / REMOVED + REPLACED TRANSITION ANGLE. REF. SRM. 53-00-53-2R-5; AND E.A. 20-153-02159.
FWD CARGO; L/H TRANSITION ANGLE HAS CORROSION AROUND SEVERAL NUTPLATE HOLES STA 500C TO 500I / REMOVED + REPLACED TRANSITION ANGLE. REF. SRM. 53-00-53-2R-5; E.A. 20-153-02159.P/N 146A7502-33
AFT CARGO R/H TRANSITION ANGLE HAS LARGE AREAS OF CORROSION BOTH UPPER + LOWER SURFACE B5 727I-767 / R/H TRANSITION ANGLE WAS REPLACED FROM 727H +10 THRU BS 767 ON NR# D469439
FWD CARGO FLOOR PNL 121ZBC IS DAMAGED. / REMOVED AND REPLACED FLOOR PANEL PER AMM 25-52-10.
PANEL 532 EB HAS EVIDENCE OF CORROSION / REPLACED PANEL WITH SERVICABLE PANEL T0 BE INSTALLED ON W/O 698428
PANEL 532 GB HAS EVIDENCE OF CORROSION / REPLACED PANEL WITH SERVICEABLE PANEL TO BE INSTALLED ON W/O 698428
ON THE RIGHT WING; JUST INBD OF THE DELECTION RIB. THE ATTACH ANGLE IS CRACKED. (OTBD END OF LOWER BULB SEAL.) / REMOVED AND DAMAGED ANGLE PER SRM 51-40-02; 104029. INSTALLED NEW ATTACH ANGLE PER SRM 51-40-02.
FOUND DAMAGE ON RH WINGLET LOWER STRAKE TRAILING EDGE. / R+R R/H WINGLET STRAKE PER A.I.P FINALL INSTALL WILL BE ACCOMPLISHED ON TASK CARD 757-31-02POS P/H P/N OFF/ON 737-2510-4 S/N OFF 12225406/001 S/N ON 1254031/001
RADOME HAS MANY LARGE HOLES IN BOOT / REPLACED RADOME ROFM/M 53-52-00POS ONLY TAG 97797 P/N OFF/ON 1001002-7B S/N OFF NRD-0268 S/N ON C205766-02
CEILING MOUNTED EXIT SIGN AT THE OVERWING EXIT OUT OF POSITION. / REPOSITIONED EXIT SIGN PER SIP.
PANEL 193AL HAS DELAMINATION ON LEADING EDGE 7' FROM TOP OF PANEL 13' LONG 3/4' WIDE 5 PLYS DEEP.ACCOMPLISHED EA TASKS AS REQUIRED PER REPAIR-53EA-06466; SEE ALSO SA-M 943T V009237 FOR FURTHER ACTION.PERMANENT ACTION REQUIRED:PERFORM A PERMANENT REPAIR PER SRM 51-70-04; OTHER APPLICABLE PERMANENT REPAIR; OR REMOVE AND REPLACE THE P/N 149A7655-21 PANEL. / ACCOMPLISHED PERMANENT REPAIR PER 51-70-05.
PANEL 193AL HAS DELAMINATION ON LEADING EDGE 7' FROM TOP OF PANEL 13' LONG 3/4' WIDE 5 PLYS DEEP. / ACCOMPLISHED EA TASKS AS REQUIRED PER REPAIR-53EA-06466; SEE ALSO SA-M 943T V009237 FOR FURTHER ACTION.PERMANENT ACTION REQUIRED:PERFORM A PERMANENT REPAIR PER SRM 51-70-04; OTHER APPLICABLE PERMANENT REPAIR; OR REMOVE AND REPLACE THE P/N 149A7655-21 PANEL.
FORWARD AFT EMERGENCY FLASHLIGHT BATTERIES DIM. R&R BATTERIES AMM.
R2 DOOR GIRT BAR HOLDERS WAS STIFF AND DIFFICULT TO OPERATE. LUBED GIRT BAR HOLDER PER SIP.
NLG WHEEL WELL R/H SEAL RETAINER CRACKED. (P/N 141A7514-6) / REMOVED AND REPLACED NLG W/W R/H SEAL RETAINER I/A/W SRM 51-40-02 AND BOEING DWG 141A0611
NLG WHEEL WELL FWD R/H CORNER SEAL RETAINER CRACKED. (P/N 141A6910-20) / VERIFIED; LOCATED AND DRILLED NEW P/N:141A6910U20 IAW B737-800 SRM 51-40-05-0G-0 DWG:141A7500 REV: F TAG A67793
STRINGER 24L CRACKED BETWEEN BS 277 TO 285. REPAIRED THE STRINGER IAW EA.
SUPPLEMENTAL INFORMATION: STRINGER CLIP AT STA 277; STR 26L IS CRACKED/ DAMAGED/ BUCKLED / COMPLIED WITH INTERIM REPAIR PER EA# REPAIR-53EA-05164 PERMANENT REPAIRS REQUIRED WIHTIN ONE NON-REVENUE FLIGHT CYCLE PER EA# REPAIR-53EA-05164 REFERENCE MX NOTE ON LOG PAGE 0704209
STRINGER CLIP CRACKED AT BS 277, STRINGER 26L. REPAIRED THE STRINGER CLIP EA.
SUPPLEMENTAL INFORMATION: STRINGER 24L BETWEEN STA 277 AND 285 IS CRACKED AND BENT / COMPLIED WITH INTERIM REPAIR PER EA# REPAIR-53EA-05164. PERMANENT REPAIRS REQUIRED WITHIN ONE FLIGHT CYCLE NON REVENUE PER EA# REPAIR-53EA-05164 REFERENCE MX NOTE ON LOG PAGE # 0704209
SUPPLEMENTAL INFORMATION: STRINGER 25L BETWEEN BS 277 AND 285 IS CRACKED AND BENT / COMPLIED WITH INTERIM REPAIR PER EA# REPAIR-53EA-05164. PERMANENT REPAIRS REQUIRED WITHIN ONE FLIGHT CYCLE NON REVENUE PER EA# REPAIR-53EA-05164 REFERENCE MX NOTE ON LOG PAGE # 0704209
STRINGER CRACKED BETWEEN BS 277 TO BS 285, STR 25L. REPAIRED STRINGER IAW EA.
LEFT HORIZONAL STABILIZER UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED LEFT HORIZONTAL STAB UPPER SLIDING SEAL PER AMM CH 53-31-31
L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED GIRT BAR PER AMM.
OVERHEAD OVERWING EMER LIGHT LENS MISSING. INSTALLED LENS IAW MM.
R1 DOOR EGRESS LIGHT LENS BROKEN. R & R LENS IAW SIP.
R1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
R1 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
LEFT AFT EMER EXIT LIGHT LENS FELL OFF. REINSTALLED LENS IAW SIP.
LEFT EMER EXIT COVER LENS MISSING AT ROW 16. INSTALLED LENS IAW SIP.
R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM & MT.
RIGHT EMER EXIT SIGN LOOSE AT ROW 13. SECURED SIGN IAW SIP.