N8608N
Registered owner: UMB BANK NA TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2019-06-17 – 2019-06-17 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2019-06-17 – 2019-06-17 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
EMERGENCY LIGHTS BY ROW 12 ARE NOT SECURED TO THE FLOOR. REATTACTED STRIP AT ROW 12 PER SIP.
F/A REPORTS 12C FLOOR LIGHT COMING UP. ATTACHED FLOOR PHOTOLUMINESCENT LIGHT AT 12C PER AMM 33-51-15.
F/A REPORTS THAT R1 DOOR SLIDE IS OUT OF POSITION IN BUSTLE. ADJUSTED R1 SLIDE PACK WITHIN BUSTLE PER SIP
L1 DOOR SLIDE FLAP SHOWING. SECURED L1 DOOR SLIDE CAUTION FLAP IAW AMM 25-66-00. OK FOR SERVICE
FORWARD SERVICE DOOR LIGHT ASSEMBLY L1186 DOES NOT ILLUMINATE DURING EMERGENCY LIGHTING TEST.<[01] TROUBLESHOT TO FAULTY FUSE IN M2816 POWER SUPPLY; REPLACED FUSE CONNECTED TO D14812; PIN 15 PER WDM 33-51-21; WDM 33-51-11; AND AMM 33-51-06-960-804. RELAMPED L1186 AND TESTED PER AMM 33-51-01-960-801; TEST NOW PASSES.<BR><BR>FLUKE 77IV<BR>CAL ID: PER1502; DUE: 10/26;[02] VERIFIED ACTION 1.
FORWARD SERVICE DOOR LIGHT ASSEMBLY L1186 DOES NOT ILLUMINATE DURING EMERGENCY LIGHTING TEST. TROUBLESHOT TO FAULTY FUSE IN M2816 POWER SUPPLY. REPLACED FUSE CONNECTED TO D14812; PIN 15 PER WDM 33-51-21, WDM 33-51-11, AND AMM 33-51-06-960-804. REPLACED THE LAMPS L1186 AND TESTED IAW AMM 33-51-01-960-801, TEST NOW PASSES.
FWD GALLEY ASSIST HANDLE IS BROKEN<[01] REMOVED AND REPLACED BROKEN G1 ASSIST HANDLE IAW SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
NOSE RADOME HAS A DELAMINATION AT 4 O`CLOCK, 4 INCHES FROM AFT EDGE, MEASURES 9 INCHES BY 14 INCHES. R & R NOSE RADOME IAW AMM 53-52-00.
LEFT WING OTBD ANGLE UNDER UPPER INBD FIXED TRAILING EDGE PANEL CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-0G-0-B00069.
L1 DOOR EMERGENCY EXIT LIGHT LENS DOESNT MATCH<[01] R&R L1 DOOR EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01
R1 DOOR EMERGENCY EXIT LIGHT LENS DOESNT MATCH<[01] R&R R1 DOOR EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01
CR RR R2 DOOR ASSIST HANDLE AIRFRAME SIDE NEEDS SECURED. <[01] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 25-21-420-801; [02] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 25-21-420-801; [03] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 25-21-420-801.
FORWARD RIGHT-HAND EMERGENCY LIGHTS INOP <[01]. REMOVED AND REPLACED FORWARD R/H BATTERY PACK M02816 AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-805.; [02] REMOVED AND REPLACED FORWARD R/H BATTERY PACK M02816 AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-80.
FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H CRACKED P/N#143A7502-158<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL CLIPS STA 500H R/H WITH NEW PN: 143A7502U158 PO: 1112667.1 AND PN:143A7502U154 PO: 1112648.1 IAW DWG 143A7505 REV - AND B737-800 SRM 51-40-02;[02] VERIFEID REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL CLIPS STA 500H R/H WITH NEW PN: 143A7502U158 PO: 1112667.1 AND PN:143A7502U154 PO: 1112648.1 IAW DWG 143A7505 REV - AND B737-800 SRM 51-40-02
FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H CRACKED P/N 143A7502-154<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H P/N 143A7502-154 PO: 1112648.1 IAW DWG 143A7505 REV - AND B737-800 SRM 51-40-02;[02] VERIFIED REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H P/N 143A7502-154 PO: 1112648.1 IAW DWG 143A7505 REV - AND B737-800 SRM 51-40-02
FWD CARGO COMPARTMENT R/H TRANSITION PANEL CORRODED AT FASTENER HOLES THROUGHOUT FROM STA 500C TO STA 500I<[01] EVALUATED FWD CARGO COMPARTMENT R/H TRANSITION PANEL FROM STA 500C TO STA 500I; ORIG. MAT. THK. 0.040'; MATERIAL REMOVED 100% AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 REMOVED AND FABRICATED NEW TRANSITION PANEL IAW B 737-800 SRM 53-00-53-2R-REPAIR 5 AND INSTALLED IAW B737-800 SRM 51-40-02; SRM 53-00-53-2R REPAIR 5.;[02] VERIFIED EVALUATED FWD CARGO COMPARTMENT R/H TRANSITION PANEL FROM STA 500C TO STA 500I; ORIG. MAT. THK. 0.040'; MATERIAL REMOVED 100% AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 REMOVED AND FABRICATED NEW TRANSITION PANEL IAW B 737-800 SRM 53-00-53-2R-REPAIR 5 AND INSTALLED IAW B737-800 SRM 51-40-02; SRM 53-00-53-2R REPAIR 5.;[03] VERIFIED EVALUATED FWD CARGO COMPARTMENT R/H TRANSITION PANEL FROM STA 500C TO STA 500I; ORIG. MAT. THK. 0.040'; MATERIAL REMOVED 100% AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 REMOVED AND FABRICATED NEW TRANSITION PANEL IAW B 737-800 SRM 53-00-53-2R-REPAIR 5 AND INSTALLED IAW B737-800 SRM 51-40-02; SRM 53-00-53-2R REPAIR 5.
FWD CARGO COMPARTMENT INTERCOSTAL/BAFFLE STA 500F - STA 500G R/H CRACKED (DOT K570) <[01]. REMOVED AND REPLACED BAFFLE STA 500F IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A7510 REV: B AND REPAIRED IAW 51-70-13-2R-1.; [02] VERIFIED: REMOVED AND REPLACED BAFFLE STA 500F IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A7510 REV: B AND REPAIRED IAW 51-70-13-2R-1.; [03] VERIFIED: REMOVED AND REPLACED BAFFLE STA 500F IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A7510 REV: B AND REPAIRED IAW 51-70-13-2R-1.
FWD CARGO COMPARTMENT INTERCOSTAL STA 500D - STA 500E R/H CRACKED (DOT K569)<[01] REMOVED FWD CARGO COMPARTMENT INTERCOSTAL AT STA 500D - STA 500E R/H IAW B737-800 SRM 51-40-02; RECEIVED NEW PART P/N: 143A7510-22 BAFFLE ASSEMBLY; P.O: 1112649.1 IAW BAC DWG 143A7510 REV. B; LOCATED & DRILLED IAW B737-800 SRM 51-40-05 AND BAC DWG 143A7510 REV. B AND INSTALLED IAW B737-800 SRM 51-40-02 & BAC DWG 143A7510 REV. B.;[02] COMPLIED WITH FWD CARGO COMPARTMENT INTERCOSTAL STA 500D - STA 500E R/H CRACKED
(CR - VERNON) FOUND FRAME CRACK AT STA 312 BETWEEN S-5L AND S-6L ABOVE L-1 DOOR<[01] REMOVED DAMAGE; FORMED; LOCATED; DRILLED; HFEC CUT OUT; OPEN HOLES AND FPI FORMED ANGLE; NO DEFECTS NOTED; ALODINED; PRIMED; INSTALLED REPAIR ANGLE; AND CIC REF B737-NG SRM 53-10-07-2R-1; THIS IS A CAT B REPAIR - THRESHOLD 50;000 CYC INSPECTION THRESHOLD; 12;000 CYC REPEAT HFEC FROM MANUFACTURED DATE.; [02] VERIFIED REMOVED DAMAGE; FORMED; LOCATED; DRILLED ANGLE; HFEC CUT OUT; OPEN HOLES AND FPI FORMED ANGLE; NO DEFECTS NOTED; ALODINE; PRIMED; INSTALLED REPAIR ANGLE; AND CIC REF B737-NG SRM 53-10-07-2R-1; THIS IS A CAT B REPAIR - THRESHOLD 50;000 CYC INSPECTION THRESHOLD; 12;000 CYC REPEAT HFEC FROM MANUFACTURED DATE; [03] VERIFIED REMOVED DAMAGE; FORMED; LOCATED; DRILLED ANGLE; HFEC CUT OUT; OPEN HOLES AND FPI FORMED ANGLE; NO DEFECTS NOTED; ALODINE; PRIMED; INSTALLED REPAIR ANGLE; AND CIC REF B737-NG SRM 53-10-07-2R-1; THIS IS A CAT B REPAIR - THRESHOLD 50;000 CYC INSPECTION THRESHOLD; 12;000 CYC REPEAT HFEC FROM MANUFACTURED DATE.
[DOT: Z042] AFT CARGO FLOOR FROM FWD BULKHEAD TO STA 767; RIGHT TRANSITION PANEL CORRODED NUMEROUS PLACES AS MARKED. <[01] REMOVED CORROSION FROM R/H TRANSITION PANEL AT STA 727-STA767 ORIGINAL MATERIAL THICK .040 IAW BAC 1496-377. MATERIAL LOST FROM SAT 727-STA 727+10 .003 AND REMAINS THICK. .037 FOUND TO BE WITHIN LIMITS. ALODINED AND PRIMED IAW B737-800 SRM 51-20-01. FROM 727E+10-STA 767 MATERIAL LOST .020 AND REMAINING THICK. .020 FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 ; REMOVED TRANSITION PANEL FROM STA 727E+10 - STA767 AND REPAIRED IAW B737-800 SRM 53-00-53-2R-REPAIR 5 AND INSTALLED IAW B737-800 SRM 51-40-02 AND VBAC DWG 146A7500 REV:B.[03] VERIFIED REMOVED CORROSION FROM R/H TRANSITION PANEL AT STA 727-STA767 ORIGINAL MATERIAL THICK .040 IAW BAC 1496-377. MATERIAL LOST FROM SAT 727-STA 727+10 .003 AND REMAINS THICK. .037 FOUND TO BE WITHIN LIMITS. ALODINED AND PRIMED IAW B737-800 SRM 51-20-01. FROM 727E+10-STA 767 MATERIAL LOST .020 AND REMAINING THICK. .020 FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 ; REMOVED TRANSITION PANEL FROM STA 727E+10 - STA767 AND REPAIRED IAW B737-800 SRM 53-00-53-2R-REPAIR 5 AND INSTALLED IAW B737-800 SRM 51-40-02 AND VBAC DWG 146A7500 REV:B.
[DOT: B726] AFT CARGO FLOOR BETWEEN STA 767 AND STA 793; RIGHT SUPPORT Z-ANGLE CORRODED AS MARKED.<[01] REMOVED AND REPLACED &NBSP;&NBSP;&NBSP;&NBSP;&NBSP;AFT CARGO FLOOR BETWEEN STA 767 AND STA 793; RIGHT SUPPORT Z-ANGLE REQUIRES INSTALLATION WITH NEW PN:1468127U12 IAW B737-800 SRM 51-40-02 AND DWG 146A0081 REV: A;[02] VERIFIED REMOVED AND REPLACED AFT CARGO FLOOR BETWEEN STA 767 AND STA 793; RIGHT SUPPORT Z-ANGLE REQUIRES INSTALLATION WITH NEW PN:1468127U12 IAW B737-800 SRM 51-40-02 AND DWG 146A0081 REV: A;[03] VERIFIED REMOVED AND REPLACED AFT CARGO FLOOR BETWEEN STA 767 AND STA 793; RIGHT SUPPORT Z-ANGLE REQUIRES INSTALLATION WITH NEW PN:1468127U12 IAW B737-800 SRM 51-40-02 AND DWG 146A0081 REV: A
[DOT: B727] AFT CARGO FLOOR AT STA 847; RBL 19 HAS RAIL SPLICE STRAP CORRODED AS MARKED.<[01] REMOVED AND REPLACED NEW STRAP IAE B737-800 SRM 51-40-02 AAND BAC DWG 146A8120 REV A.;[02] VERIFIED REMOVED AND REPLACED NEW STRAP IAE B737-800 SRM 51-40-02 AAND BAC DWG 146A8120 REV A.;[03] VERIFIED REMOVED AND REPLACED NEW STRAP IAE B737-800 SRM 51-40-02 AAND BAC DWG 146A8120 REV A.
[DOT: Z041] AFT CARGO FLOOR BETWEEN STA 727C AND STA 807; LEFT TRANSITION PANEL CORRODED NUMEROUS PLACES AS MARKED. <FOUND TO BE OUT OF LIMITS ORGINAL MATERIAL IS 0.040IN AND THE MATERIAL REMOVED IS 0.007IN; THE NEW MATERIAL THICKNESS IS 0.033IN. FROM STA 737 TO STA 807 THE TRANSITION PANEL IS FOUND TO BE WITHIN LIMITS. THE ORGINAL MATERIAL IS 0.040IN; THE MATERIAL REMOVED IS 0.003IN AND THE NEW MATERIAL THICKNESS IS 0.037 IAW B737-800 SRM 53-00-53-1A-2. TOOL NUM: T8224L CAL DUE DATE: 02 DEC 25. REMOVED DAMAGED PART OF LEFT TRANSITION PANEL STA 727A TO STA 737 IAW B737-800 SRM 53-00-53-2R-5 AND SRM 51-40-02. APPLIED ALODINE IN LEFT TRANSITION PANEL STA 737 TO STA 807 IAW B737-800 SRM 51-20-01. APPLIED PRIMER IN LEFT TRANSITION PANEL STA 737 TO STA 807 IAW B737-800 SRM 51-20-01. RECEIVED NEW PART # BAC 1496-377 7075-T62 P.O # 1108010.1 PER B737-800 SRM 53-00-53-2R-5. FARBRICATED NEW L/H TRANSITION PANEL IAW B737-800 SRM 53-00-53-2R-5. PRIMED L/H TRANSITION PANEL IAW B737-800 SRM 53-00-53-2R-5. INSTALLED NEW L/H TRANSITION PANEL IAW B737-800 SRM 53-00-53-2R-5.
MAIN CABIN FWD WET AREA INTERCOSTA AT STA.294.5-312 BL0 IS CORR0DED <[01]. REMOVED DAMAGE; ORIG. .063; MATERIAL LOSS .063; REMAINING 0.0; FOUND TO BE OUT OF LIMITS REF B737-NG SRM 53-10-51-1A-1 FIG 105 DETAIL A; REMOVED ALL FASTENERS COMMON TO INTERCOSTAL IAW B737-800 SRM 51-40-02; LOCATED AND DRILLED NEW INTERCOSTAL IAW B737-800 SRM 51-40-06 AND BOEING DWG 141A5600 REV: N. ; INSTALLED NEW INTERCOSTAL P/N 141A5690U1 P.O#0; AT STA.294.5-312 BL0; REF. B737-800 SRM 51-40-02; BOEING DWG 141A5600 REV: N.; [02] VERIFIED REMOVED DAMAGE; ORIG. .063; MATERIAL LOSS .063; REMAINING 0.0; FOUND TO BE OUT OF LIMITS REF B737-NG SRM 53-10-51-1A-1 FIG 105 DETAIL A; REMOVED ALL FASTENERS COMMON TO INTERCOSTAL IAW B737-800 SRM 51-40-02; LOCATED AND DRILLED NEW INTERCOSTAL IAW B737-800 SRM 51-40-06 AND BOEING DWG 141A5600 REV: N. ; INSTALLED NEW INTERCOSTAL P/N 141A5690U1 P.O#0; AT STA.294.5-312 BL0; REF. B737-800 SRM 51-40-02; BOEING DWG 141A5600 REV: N.;[03] VERIFIED REMOVED DAMAGE; ORIG. .063; MATERIAL LOSS .063; REMAINING 0.0; FOUND TO BE OUT OF LIMITS REF B737-NG SRM 53-10-51-1A-1 FIG 105 DETAIL A; REMOVED ALL FASTENERS COMMON TO INTERCOSTAL IAW B737-800 SRM 51-40-02; LOCATED AND DRILLED NEW INTERCOSTAL IAW B737-800 SRM 51-40-06 AND BOEING DWG 141A5600 REV: N. ; INSTALLED NEW INTERCOSTAL P/N 141A5690U1 P.O#0; AT STA.294.5-312 BL0; REF. B737-800 SRM 51-40-02; BOEING DWG 141A5600 REV: N.
FWD PIT TRANSITON PANELS CORRODED AT FASTENER HOLES FROM STA 500C TO 500I <[01]. L/H TRANSITION PANEL FROM STA 500C TO STA 500I EVALUATED ORIG. MAT. THK. = 0.040'; RMV. MAT. = 0.040'; REM. MAT. THK.= 0.00' AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2; TOOL I.D T8224L; CAL. DUE DATE: 02/DEC/25. REMOVED; FABRICATED REPAIR PARTS USING BAC1496-444 7075-T6; PO: 1107340.1; APPLIED ALODINE; PRIMER; CIC; INSTALLED NUTPLATES AND INSTALLED TO AIRCRAFT IAW B737-800 SRM 53-00-53-2R-5. & BAC DWG 1496-444.;[02] VERIFIED L/H TRANSITION PANEL FROM STA 500C TO STA 500I EVALUATED ORIG. MAT. THK. = 0.040'; RMV. MAT. = 0.040'; REM. MAT. THK.= 0.00' AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2; TOOL I.D T8224L; CAL. DUE DATE: 02/DEC/25. REMOVED; FABRICATED REPAIR PARTS USING BAC1496-444 7075-T6; PO: 1107340.1; APPLIED ALODINE; PRIMER; CIC; INSTALLED NUTPLATES AND INSTALLED TO AIRCRAFT IAW B737-800 SRM 53-00-53-2R-5. & BAC DWG 1496-444.;[03] VERIFIED L/H TRANSITION PANEL FROM STA 500C TO STA 500I EVALUATED ORIG. MAT. THK. = 0.040'; RMV. MAT. = 0.040'; REM. MAT. THK.= 0.00' AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2; TOOL I.D T8224L; CAL. DUE DATE: 02/DEC/25. REMOVED; FABRICATED REPAIR PARTS USING BAC1496-444 7075-T6; PO: 1107340.1; APPLIED ALODINE; PRIMER; CIC; INSTALLED NUTPLATES AND INSTALLED TO AIRCRAFT IAW B737-800 SRM 53-00-53-2R-5. & BAC DWG 1496-444.
R-HORIZONTAL UPPER SLIDING SEAL CRACKED DOT# J149 <[01] REMOVED; LOCATED; DRILLED; AND INSTALLED NEW R/H HORIZONTAL UPPER SLIDING SEAL REF B737-NG AMM 53-31-31-400-802; [02] REMOVED; LOCATED; DRILLED; AND INSTALLED NEW R/H HORIZONTAL UPPER SLIDING SEAL REF B737-NG AMM 53-31-31-400-802.
L/H HORIZ. STAB TRAILING EDGE; UPPER BLADE SEAL DELAMINATED APPROX. EL STA. 155. <[01] REMOVED AND REPLACED BLADE SEAL P/N 185A1621-115 PO 1111955.1 REF BAC DWG 180A1659 REV A TOOL SCREW GUN T03835-203 DUE 03 JUN 25; [02] REMOVED AND REPLACED BLADE SEAL P/N 185A1621-115 PO 1111955.1 REF BAC DWG 180A1659 REV A TOOL SCREW GUN T03835-203 DUE 03 JUN 25.
R-WING FLAP FAIRING #6 AT TAILCONE IS CRACKED AND HAS A HOLE DOT# J148 <[01]. REPAIRED RH WING TAILCONE ON FLAP FAIRING #6 IAW 737-800 SRM 51-70-04-2R-1 REPAIR 1 AND APPLIED TOUCH UP PAINT IAW 737-800 AMM 51-21-99-300-802; [02] REPAIRED RH WING TAILCONE ON FLAP FAIRING #6 IAW 737-800 SRM 51-70-04-2R-1 REPAIR 1 AND APPLIED TOUCH UP PAINT IAW 737-800 AMM 51-21-99-300-802.
AFT WET AREA; BS 947 RBL 52 TO LBL 5 +/- FLOORBEAM T CAP CORRODED. WIDE SPREAD AND AS MARKED.<[01] REMOVED DAMAGE; ORIG. .180; MATERIAL LOSS .090. REMAINING .090; FOUND TO BE OUT OF LIMITS REF B737-NG SRM 53-70-51-1A-1 FIG 104 DETAIL C; ACCOMP. HFEC TRIMMED EDGES & ALL HOLES COMMON TO UPPER CHORD IN WEB. PER MX REQUEST; IAW B737 NDT MAN. 51-00-00 PROC 23 & 16; PT6.NO CRACK INDICATIONS FOUND. #T8257F . DUE 13 MAY 25.; MATERIAL I'D FOR -1 T-CHORD 53700002-001 PO 1111889.1; -2 ANGLES BAC1490-2885 7075-T62 CLAD PO 1099692.2; AND -3 STRAPS 7075-T6 .125 ALUMINUM SHEET CLAD PO 1106304.1 REF B737-NG SRM 53-70-51-2R-5 TABLE 201 AND SWA DWG 53700002 REV A; APPLIED ALODINE ON REPAIR PARTS -1 T-CHORD; -2 ANGLES; -3 STRAPS REF B737-NG SRM 53-70-51-2R-5; SRM 51-20-01. OK TO INSTALL REPAIR PARTS -1 T-CHORD; -2 ANGLES; -3 STRAPS; INSTALLED REPAIR PARTS -1 T-CHORD; -2 ANGLES; -3 STRAPS REF B737-NG SRM 53-70-51-2R-5; REMOVED AND INSTALLED INTERCOSTAL AND FLOOR SUPPORTS REQUIRED FOR REPAIR REF B737-NG SRM 51-40-02;[02] APPLIED PRIMER ON REPAIR PARTS -1 T-CHORD; -2 ANGLES; -3 STRAPS REF B737-NG SRM 53-70-51-2R-5; SOPM20-41-02. OK TO INSTALL REPAIR PARTS -1 T-CHORD; -2 ANGLES; -3 STRAPS; INSTALLED REPAIR PARTS -1 T-CHORD; -2 ANGLES; -3 STRAPS REF B737-NG SRM 53-70-51-2R-5; REMOVED AND INSTALLED INTERCOSTAL AND FLOOR SUPPORTS REQUIRED FOR REPAIR REF B737-NG SRM 51-40-02. VERIFIED WORK AND WORK STEPS.
MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-24. MARKED <[01]. MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-24; EVALUATED DAMAGE AND FOUND OUT OF LIMITS IAW B737-800 SRM 53-10-51-1A-1 AND BOEING DWG 141A5770 REV:A; DAMAGE DEPTH: 0.044' ORIGINAL THICKNESS: 0.080'; REMOVED FLOOR SUPPORT IAW B737-800 SRM 51-40-02; RECEIVED NEW PART P/N: 141A5770U3 INTERCOSTAL; PO: 1112018.1 IAW B737-800 IPC 53-42-11-44; LOCATED & DRILLED IAW B737-800 SRM 51-40-05 & BAC DWG 141A5730 REV. A. AND INSTALLED IAW B737-800 SRM 51-40-02 & BAC DWG 141A5730 REV. A. [04] VERIFIED MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-24; EVALUATED DAMAGE AND FOUND OUT OF LIMITS IAW B737-800 SRM 53-10-51-1A-1 AND BOEING DWG 141A5770 REV:A; DAMAGE DEPTH: 0.044' ORIGINAL THICKNESS: 0.080'; REMOVED FLOOR SUPPORT IAW B737-800 SRM 51-40-02; RECEIVED NEW PART P/N: 141A5770U3 INTERCOSTAL; PO: 1112018.1 IAW B737-800 IPC 53-42-11-44; LOCATED & DRILLED IAW B737-800 SRM 51-40-05 & BAC DWG 141A5730 REV. A. AND INSTALLED IAW B737-800 SRM 51-40-02 & BAC DWG 141A5730 REV. A & REV C.
MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-45. <[01] MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-45. EVALUATED DAMAGE AND FOUND OUT OF LIMITS IAW B737-800 SRM 53-10-51-1A-1 AND BOEING DWG 141A5770 REV:A; DAMAGE DEPTH: 0.044' ORIGINAL THICKNESS: 0.080'; REMOVED FLOOR SUPPORT IAW B737-800 SRM 51-40-02; RECEIVED NEW PART P/N: 141A5770U3 INTERCOSTAL; PO: 0 IAW B737-800 IPC 53-42-11-44; LOCATED & DRILLED IAW B737-800 SRM 51-40-05 & BAC DWG 141A5730 REV. A. AND INSTALLED IAW B737-800 SRM 51-40-02 & BAC DWG 141A5730 REV. A; [04] VERIFIED MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-45. EVALU
AFT WET AREA; BS 987 LBL 47 +/- FLOORBEAM T CAP CORRODED AT DOME NUT FASTENER. AS MARKED. <[01] REMOVED CORROSION FROM AFT WET AREA; BS 987 LBL 47 +/- FLOOR BEAM T CAP AT DOME NUT FASTENER IAW B 737-800 SRM 51-10-02; ORIGINAL MATERIAL THICK. 0.150 IAW BAC 1518-1211 MAXIMUM MATERIAL REMOVED .021 MATERIAL REMAINING 0.129 FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. ; CUT OUT DAMAGED IAW B737-NG SRM 53-70-51-2R-6.; ACCOMP. HFEC AREA & TRIM OUT IAW B737 NDT MAN. 51-00-00 PROC. 23; PT6. NO CRACK INDICATIONS FOUND. ; PERFORMED DVI AT THE REPAIR AREA IAW B737-NG SRM 53-70-51-2R-6; NO DEFECTS NOTED.; SHOT PEENED AREA IAW B737-NG SRM 53-70-51-2R-6 AND SRM 51-20-06-0G-0; FABRICATED; LOCATED; DRILLED AND INSTALLED REPAIR PARTS -1 STRAP; -2 ANGLE; AND -3 FILLER REF B737-NG SRM 53-70-51-2R-6.;;[02PERFORMED DVI AT THE REPAIR AREA IAW B737-NG SRM 53-70-51-2R-6; NO DEFECTS NOTED.;; SHOT PEENED AREA IAW B737-NG SRM 53-70-51-2R-6 AND SRM 51-20-06-0G-0; FABRICATED; LOCATED; DRILLED AND INSTALLED REPAIR PARTS -1 STRAP; -2 ANGLE; AND -3 FILLER REF B737-NG SRM 53-70-51-2R-6.
AFT WET AREA BS 967 TO 987 LBL 15 +/- INTERCOSTAL CORRODED AS MARKED. <[01] REMOVED DAMGED ON LBL 15 +/- INTERCOSTAL STA 967-987 FOUND TO BE OUT OF LIMITS IAW B737-800 53-70-51-1A-1; BOEING DWG 147A5676 REV:M ORGINAL THICKNESS:.075 REMAINING THICKNESS .064 MATERIAL REMOVED: .11 MAXIUM ALLOWED MATERIAL REMOVED: 10% (.0075). REMOVED AND INSTALLED NEW INTERCOSTAL IAW B 737-800 SRM 51-40-02 AND BAC DWG 140A9872 REV: K.; [02] VERIFIED REMOVED DAMGED ON LBL 15 +/- INTERCOSTAL STA 967-987 FOUND TO BE OUT OF LIMITS IAW B737-800 53-70-51-1A-1; BOEING DWG 147A5676 REV:M ORGINAL THICKNESS:.075 REMAINING THICKNESS .064 MATERIAL REMOVED: .11 MAXIUM ALLOWED MATERIAL REMOVED: 10% (.0075). REMOVED AND INSTALLED NEW INTERCOSTAL IAW B 737-800 SRM 51-40-02 AND BAC DWG 140A9872 REV: K.
AFT WET AREA; BS 995 LBL 38 +/- WEB CORRODED AT FASTENER. AS MARKED. <[01] REMOVED AND REPLACED FLOOR SUPPORT PN:147A5710U1 AT STA. 995 LBL 38. IAW B737-800 SRM 51-40-02 AND BOEING DWG. NO. 147A5700 REV:A; [02] REMOVED AND REPLACED FLOOR SUPPORT PN:147A5710U1 AT STA. 995 LBL 38. IAW B737-800 SRM 51-40-02 AND BOEING DWG. NO. 147A5700 REV:A.
STA540 R/H FLOORBOARD SUPPORT STRUCTURE CRACKED 2EA AREAS DOT T743 <[01]. REMOVED AND REPLACED PANEL BREAK#143A5240-64 PO#1111708.1 AT STA540 R/H IAW B737-800 SRM 51-40-02 AND BAC DWG#143A0060 REV.A; [02] REMOVED AND REPLACED PANEL BREAK#143A5240-64 PO#1111708.1 AT STA540 R/H IAW B737-800 SRM 51-40-02 AND BAC DWG#143A0060 REV.A. VERIFIED WORK AND WORK ENTRIES.
R/H AFT EMERGENCY LIGHTS ON R2 DOOR INOP <[01]. REMOVED AND REPLACED R/H AFT EMERGENCY BATTERY AND OPS CHECK GOOD IAW B737-800 AMM 33-51-00-710-801; [02] REMOVED AND REPLACED R/H AFT EMERGENCY BATTERY AND OPS CHECK GOOD IAW B737-800 AMM 33-51-00-710-801. VERIFIED WORK AND WORK ENTRIES.
RIGHT WING OUTBOARD AFT FLAP INBOARD LOWER CORNER IS DELAMINATED <[01]. REMOVED AND REPLACED RIGHT WING OUTBOARD AFT FLAP IAW B737-800 AMM 27-51-22-401-NG.; [02] VERIFIED REMOVED AND REPLACED RIGHT WING OUTBOARD AFT FLAP IAW B737-800 AMM 27-51-22-401-NG.; [03] VERIFIED REMOVED AND REPLACED RIGHT WING OUTBOARD AFT FLAP IAW B737-800 AMM 27-51-22-401-NG.
L/H WING FIXED L/E; 3 EACH STIAND OFFS FOR OVER HEAT DETECTOR CORRODED BETWEEN RIB #3 AND RIB #4. <[01] REMOVED AND REPLACED 3 EACH STAND OFFS # BACN10TL3A12 PO # 1111371.1 AT L/H WING FIXED L/E IAW B737-800 SRM 51-40-02 AND BAC DWG #116A2130 REV.- TOOL # T8866U. CAL.DUE.07/APR/25 (TORQUE WRENCH);[02] REMOVED AND REPLACED 3 EACH STAND OFFS # BACN10TL3A12 PO # 1111371.1 AT L/H WING FIXED L/E IAW B737-800 SRM 51-40-02 AND BAC DWG #116A2130 REV.- TOOL # T8866U CAL.DUE. 07/APR/25 (TORQUE WRENCH).
#2 ENGINE I/B FAN COWL IS CRACKED 17' LONG AT FWD LOWER FWD END.<[01] REMOVED AND REPLACED #2 ENGINE INBOARD FAN COWL REF. AMM 71-11-02. INSTALLED VORTEX CONTROL DEVICE REF. AMM 71-11-08.
ON APPROACH LDG GEAR WAS LOWERED AND LT MAIN DISAGREED WITH HANDLE POSITION. NOSE & RT MAIN GREEN/ LEFT MAIN RED AND NO GREEN GEAR LT ON OVERHEAD FOR LT MAIN. RAN QRH FOR LANDING GEAR DISAGREE; PULLED MANUAL EXTENSION AND GOT GREEN LT ON LT MAIN AND OVERHEAD.<[01] OK TO CONTINUE PER MEL 32-16-01 SP#1;[02] REMOVED AND REPLACED L/H MLG UPLOCK ACTUATOR AS PER AMM 32-32-41. OPS CHECK GOOD!
FWD BULLHORN INOP<[01] R & R?D FWD GALLEY MEGAPHONE PER AMM 25-64-00.
RIGHT SIDE PASSENGER EMERGENCY LIGHTS INOP<[01] T/S PER FIM 33-50 TASK 801; RR?D BATTER PACK AT ASSY# M1695 PER AMM 33-51-06. NO HELP. RETURNED BACK TO ORIGINAL CONFIGURATION. R/R EMERGENCY LIGHT BATTERY PACKS AT POS M1676 AND M1671 REF AMM 33-51-06. OPS CHECK NORMAL REF AMM 33-51-00. THIS CLEARS MEL.
R/H AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP<[01] REMOVED AND REPLACED 2EA EMERGENCY LIGHT BATTERY PACKS PER AMM 33-51-06. OPERATIONAL CHECK NORMAL OF EMERGENCY LIGHTS PER AMM 33-51-00. REFERENCE CARD TTG8Q00HCN6F FOR PARTS INSTALLED.;[02] INSPECTED
R/H EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED 2EA EMERGENCY LIGHT BATTERY PACKS PER AMM 33-51-06. OPERATIONAL CHECK NORMAL OF EMERGENCY LIGHTS PER AMM 33-51-00.;[02] INSPECTED
R/T HORIZONTAL PANEL 343AT FWD TRACK IS CRACKED<[01] R&R TRACK PER SOPM 20-50-01;[02] INSPECTED WORK PERFORMED.
EVIDENCE OF CORROSION ON THE RUDDER BALANCE WEIGHT.<[01] REMOVED RUDDER WEIGHT PER CMM 55-40-09;[02] INSTALLED RUDDER WEIGHT PER CMM 55-40-09;[03] C/W INSPECTION.;[04] INSTALLED RUDDER WEIGHT PER CMM 55-40-09
L/H WING FIXED TRAILING EDGE SUPPORT BEAM FWD FASTENER HOLE ADJACENT TO L/H DEFLECTION RIB HAS AN HFEC INDICATION OF A CRACK AT THE FWD SIDE OF THE HOLE SEE ATTACHED PICTURE<[01] REPAIR PER EA #23-157-00063 (N8608N - SWA - REPAIR - L/H WING TRAILING EDGE SUPPORT BEAM FASTENER HOLE CRACK ON PN 115A2179);[02] C/W INSPECTION.
CENTER CABIN STA. 540 LBL 1 FLOOR PANEL SUPPORT ANGLE IS CRACKED AT FASTENER HOLE. MRKD<[01] REMOVED AND REPLACED CABIN FLOOR SUPPORT PER SRM 51-40-02.
CENTER CABIN STA. 540 RBL 1 FLOOR PANEL SUPPORT ANGLE IS CRACKED. MRKD<[01] REMOVED AND REPLACED SUPPORT PART SRM 51-40-02
FASTENER HOLE CRACKED ON PANEL 561CB<[01] REMOVED DAMAGE AND APPLIED REPAIR PER SRM 51-70-04-2R-9;[02] C/W INSPECTION.;[03] RESIN SWEEPED AND SANDED TO AERODYNAMIC SMOOTHNESS PER SRM 51-70-08;[04] C/W INSPECTION.;[05] PRIMED PER AMM 51-21-72 APPLIED TOPCOAT PER AMM 51-21-73;[06] C/W INSPECTION.
L/H WING T/E WAFFLE PLATE IS CRACK AT APPROX. IRSS 220. MRKD<[01] REMOVED AND REPLACED WAFFLE PLATE IAW SRM 51-40-02.;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR: 1. JOSHUA PHIPPS (TECHNICIAN); 08-JAN-2023 04:43 UTC<BR>REMOVED AND REPLACED WAFFLE PLATE IAW SRM 51-40-02.
L2 EXTERIOR EMERGENCY LIGHT INOP ; / [01] RELAMPED L2 EXTERIOR EMERGENCY LIGHT PER AMM 33-51-04
EMERGENCY LIGHTS INOP AFT OF 2ND OVER WING EXIT LT SIDE AND AFT OF WING TO BODY PNL'S LT SIDE / REMOVED AND REPLACED PACK CHARGER ASSY AND BATTERY PACK AT M1670 OPS CK'S GOOD REF AMM 33-51-06REF SA-M 326 A1073571P/N OFF/ON D717-02-030 S/N OFF 103651 S/N ON 25511P/N OFF/ON D717-01-100 S/N OFF 218913 S/N ON 220350
EMERGENCY LIGHTS INOP AFT OF 2ND OVER WING EXIT LT SIDE AND AFT OF WING TO BODY PNL'S LT SIDE / REMOVED AND REPLACED PACK CHARGER ASSY AND BATTERY PACK AT M1670 OPS CK'S GOOD REF AMM 33-51-06REF SA-M 326 A1073571P/N OFF/ON D717-02-030 S/N OFF 103651 S/N ON 25511P/N OFF/ON D717-01-100 S/N OFF 218913 S/N ON 220350
AFT RIGHT HAND (FO SIDE) LAV HAS INTERMITTENT SMOKE ALARM WITH NO PASSENGER IN LAV OR EVIDENCE OF SMOKE SEE AIRCRAFT LOGBOOK / REMOVED AND REPLACED AFT RIGHT LAV SMOKE DETECTOR IN REFERENCE TO AMM 26-14-01 OPS CHECK IS OK CLOSING # 87917
FWD CARGO PANEL 120ZAC HAS A CRACK 4.5' LONG 25' FROM LH EDGE OF PANEL PERFORMED INTERIM REPAIR ON PANEL 120ZAC PER EA 1-A25-3722 REV. 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED.
FWD CABIN L/H AISLE EMERGENCY LIGHTS INOP / REMOVED AND REPLACED THE BATTERY PACK FOR THE POWER SUPPLY AT BS 500 C & 7; OPS CHECK GOOD PER AMM 33-51-06 (D62)
FWD CARGO COMPARTMENT ; AFT CORNER SCUFF PLATE IS CRACKED. / R/R FWD CARGO AFT CORNER SCUFF PLATE IAW AMM 53-11-02SEE SA-M 326: A1304062
FWD CARGO COMPARTMENT ; FWD CORNER SCUFF PLATE IS CRACKED. / R/R FWD CARGO FWD CORNER SCUFF PLATE IAW AMM 53-11-02 SEE SA-M 326: A1304063
CABIN FLOORBOARDS 241 ZF; 242D;242E;242F DAMAGED BEYOND LIMITS / REPLACED AFT CABIN FLOORBOARDS 241ZF; 242D. 242E AND 242F. FLOORBOARD INSTALL ON SWA SAM 565S
FWD GALLEY FLOOR STRUCTURE STA. 274 TO 294 RBL. 1; INTERCOSTAL CRACKED AT FASTENER HOLE / REMOVED DAMAGED INETCOASTAL AND INSTALLED NEW INTERCOASTAL I/A/W SRM 51-40-02.
CORROSION ON TOP OF FLOOR BEAM @ STA 947 FROM RBL 49.5 TO LBL 52 IS OUT OF LIMITS / REMOVED AND REPLACED DAMAGED FLOOR BEA; UPPER HORIZONTAL LEG PER E.A. 21-153-0093 AND SRM 53-70-51-2R-5 SEE SA-M 326'S : A1304014;A1304015;A1304016;A1304017
FWD ENTRY DOOR CUT-OUT Z-ANGLE AND NUT-PLATE SUPPORT CORRODED FROM BS 303-348 / REMOVED + REPLACED FWD ENTRY DOOR CUTOOUT Z ANGLE IAW SRM 51-40-02 AND SRM 51-10-02SA-M 326 S/N A1304019
CORROSION ON TOP SURFACE OF INTERCOSTAL @ STA 947+2 AND LBL 25. / R/R INTERCOSTAL STA 947+2 LBL 25 IAW SRM 51-40-02 AND SRM 51-10-02. PART# REPALCED 147A5660V3.
CORROSION ON TOP SURFACE OF INTERCOSTAL @ STA 947+2 AND LBL 50. / REMOVED AND REPLACED INTERCOSTAL FROM STA 947 TO STA 967; LBL 50' PER SRM 51-40-02 AND EA 21-153-00093 PART 2. INTER COSTAL P/N 147A5660-21.SA-M 326 A1304011
CORROSION ON TOP SURFACE OF INTERCOSTAL @ STA 947+2 AND RBL 50. / REMOVED AND REPLACED DAMAGED INTERCOSTAL 947 TO 967 RBL 50 PER SRM 51-40-02.
RT STAB FWD UPPER SLIDING SEAL CRACKED. / R&R STAB FWD UPPER SLIDING SEAL ASSY IAW AMM 53-31-31SEE S-AM 326: A1304089
LT. HORIZ. STAB FWD UPPER SLIDING SEAL CRACKED. / R&R SLIDING SEAL ASSY IAW AMM 53-31-31SEE SA-M 326: A1304050
FWD WET AREA FLOOR BOARDS DAMAGED FROM STA 2700-420 / FWD WET AREA FLOOR BOARDS (ZZ1AF-ZZICE-ZZ1DF-ZZ1EF-ZZ1FF; ZZ1GF; ZZZ AF - ZZZBF - ZZZCF - ZZZ DF) WERE R&R ON SA-M 565S TASK CARD PANEL SIGN OFF SHEET AND PER AMM 53-21-00; PANEL WERE ALL REPLACED WITH NEW PANELS
BIN EMERGENCY EXIT LIGHT & BEZEL / LENS CRACKED AT 27 ABC / REPLACED LIGHT BEZEL/LENS PER AMM 33-51-03
FWD ENTRY DOOR SLIDE APPEARS TO BE IMPROPERLY RIGGED. REATTACHED THE HOOK AND LOOP ON THE SLIDE LOWER FLAP IAW MT 725-61-06. NO FAULTS NOTED.
FWD. CARGO DOOR HANDLE RETURN SPRING BROKEN (RAMP REPORTS) ( FWD CARGO DOOR EXTERIOR HANDLE RECESS/HINGE SPRINGASSEMBLIES ) / CLEARING DMA LOG PAGE# 0428221REMOVED & REPLACED FWD CARGO DOOR HANDLE RETURN SPRING AS PER M/M 52-31-14 CL# 76792
L/H EMERGENCY EXIT OVERWING FORWARD BROKEN OFF. R&R LIGHT LENS IAW AMM.
FORWARD CABIN EMERGENCY LIGHTS INOP AT LOCATION M2816. R&R BATTERY PACK IAW AMM.
FORWARD CABIN EMERGENCY LIGHTS INOP AT LOCATION M1475. R&R BATTERY PACK IAW AMM.
STRINGER CLIP MISSING AT BS. 727H, STR. 19L. R&R STRINGER CLIP PER SRM & DWG.
WING TO BODY PANEL 193CL FORWARD EDGE HAS SEVERAL LAYERS ERODED WITH DELAM / REPAIRED AND APPLIED RESTORATIVE FINISH ON WING TO BODY PANEL 193CL OF DAMAGE AT FORWARD EDGE OF ONE PLY OR LESS IAW B737-800 SRM 51-70-08-0G-0 REV 67 AND B737 AMM 51-21-99-300-801 REV 68. A38760; A86296; A56952
SHEAR TIE CRACKED AT STA 847 BELOW S-23L / REMOVED DAMAGED SHEAR TIE; LOCATED; DRILLED; AND INSTALLED NEW SHEAR TIE REF B737 SRM 51-40-02; 51-40-03; DWG 146A3230 ID 0184 REV A. AT STA 847 BELOW S23L
STRINGER CLIP DAMAGED AT BS. 727I, STR. 24L. / REPAIR CLIP PER EA.
SKIN DAMAGED BETWEEN BS. 727H-1.5 TO BS. 727J+6, BETWEEN STR. 23L TO STR. 25L. / REPAIR SKIN PER EA.
STRINGER DAMAGED BETWEEN BS. 727H TO BS. 727I, STR. 20L. REPAIRED STRINGER PER EA.
STRINGER DAMAGED AT BS. 727H+6, STR. 18L. REPAIRED STRINGER PER EA.
STRINGER DAMAGED AT BS. 727I, STR. 25L. REPAIRED STRINGER PER EA.
STRINGER CLIP DAMAGED AT BS. 727H, STR. 24L. / REPAIRED CLIP IAW EA.
STRINGER CLIP DAMAGED AT BS. 727I, STR. 18L. REPAIRED CLIP PER EA.
STRINGER CLIP DAMAGED AT BS. 72I, STR. 25L. REPAIR CLIP IAW EA.
STRINGER CLIP DAMAGED AT BS. 727J, STR. 25L. / REPAIRED CLIP IAW EA.
STRINGER CLIP DAMAGED AT BS. 727J, STR. 23L. / REPAIRED CLIP PER EA.
SKIN DAMAGED BETWEEN BS. 727H+5 TO BS. 727I+4, BETWEEN STR. 17L TO STR. 28L. / REPAIRED SKIN PER EA.
SHEAR TIE DAMAGED AT BS. 867, BETWEEN STR. 25L TO STR. 26L. R&R SHEAR TIE PER SRM & DWG.
REF LP 1138480 - FGUESLAGE SKIN REPAIR FROM BS 727H - 727J AND BETWEEN STR23L-25L. REPAIR-53EA-07003 ( MX NOTE ) / REF NR X979661; R/R LEFTHAND SKIN PANEL 146A3201-32 ATAG # ZP0119 IAW SRM 51-40-05-0G-1; SRM 51-40-02-06-0 AND DRWG 146A3200 REV A
SHEAR TIE CRACKED AT BS. 847, STR 23L. R&R SHEAR TIE PER SRM & DWG.
R2 DOOR SAFETY STRAP PULLED OUT OF SIDEWALL. / INSTALLED PULLED SNAP IAW CMM.
EMERGENCY EXIT LIGHTS AT OVERWING EXITS INOP AT M1694. R&R BATTERY PACK IAW AMM.
EMERGENCY EXIT LIGHTS AT OVERWING EXITS INOP AT M1695. R&R BATTERY PACK IAW AMM.
FWD CARGO COMPARTMENT LH BAFFLE BS 500C-500D IS CRACKED / FWD CARGO L/H BAFFLE IS CRACKED AT B.S. 500C TO 500D. DRILLED AND REMOVED CRACKED BAFFLE I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW L/H BAFFLE I/A/W SRM 51-40-05-0G-0. INSTALLED NEW L/H BAFFLE AT STA 500C TO 500D I/A/W SRM 51-40-02-0G-0 ALSO BOEING DWG 143A7505 REV: . APPLIE C.I.C TO AREA I/A/W AMM 51-21-91-620-802.
AFT CARGO ATTACH ANGLE CRACKED AT BS 727+6, BETWEEN LBL 20 TO RBL 20. R&R ANGLE IAW SRM & DWG.
AFT CARGO FLOOR PANEL SPLICE PLATE CORRODED STA 767+5; RBL 18 TO LBL 18 / REMOVED AND INSTALLED AFT CARGO FLOOR PANEL SLICE PLATE AT STA 767 +5 RBL 18 TO LBL 18 P/N 146A9401-4 TAG # WN8493 IAW B737 DWG 146A7500 REV. - SRM 51-40-02-0G-0 AND APPLIED CIC IN PANEL AMM 51-21-91-620-802.
AFT CARGO; STA 887; RBL 18 TO LBL 9; FLOOR PANEL SPLICE HAS CORROSION AROUND NUT PLATE HOLES / REPLACED AFT CARGO STA 887 FLOOR PANEL SPLICE P/N 146A9401-39 IAW B737 SRM 51-40-02; SRM 51-40-05 AND DWG 146A7500 REV:- ATAG: WN7408
CUSTOMER REQUEST-VB R/H STA 663 VAPOR WEB HAS 2 EACH PREVIOUS REPAIRS WITH CRACK EXTENDING BETWEEN REPAIRS. PERM. REPAIR REQUIRED. / REPAIRED R/H STA 663 VAPOR WEB IAW B737 SRM 57-10-10-2R-2 AND SRM 51-70-04-2R-10 PARA 4
AFT CARGO; STA 867; LBL9; JUST BELOW CARGO FLOOR; ATTACH ANGLE CRACKED; COMMON TO VERTICAL BULKHEAD SUPPORT. / REMOVED AND REPLACED CRACKED ATTACH ANGLE; AFT CARGO; STA 867 LBL 8 WITH NEW PART P/N 149A8109U114 IAW SRM 51-40-02 AND DWG 149A8102 REV - ATAG ZP0073
AFT CARGO; STA 727+6; LBL 20 TO RBL 20; FLOOR TO BULKHEAD SUPPORT ANGLE IS CRACKED. / REPLACED AFT CARGO; CRACKED SUPPORT ANGLE AT STA 727 +6 LBL 20 TO RBL 20 WITH NEW PART P/N 453A2611-25 IAW IPC 25-52-10-19 PART TO BE INSTALLED WITH FLOOR BOARD 140AF W/O 38868/1000/0016 ATAG # WN3970
RT VAPOR WEB CRACKED AT BS 663. REPAIRED WEB IAW SRM.
AFT CARGO ATTACH ANGLE CRACKED AT BS 867, LBL 9. R&R ANGLE IAW SRM & DWG.
AFT CARGO FLOOR PANEL 140CF HAS CORROSION ON O/B PERIMETER OF PANEL / PANEL 140CF WAS OUT OF LIMITS IAW SRM 53-00-53-1A-1 CORROSION THE LENGTH OF PANEL RECEIVED NEW PANEL TO REPLACE PANEL 140CF MATERIAL ID IS 453A2610-18 IAW IPC 25-52-10-19 ATAG WN0558 SI 7253512
FWD CARGO COMP FLOOR STRUCTURE;AFT BULKHEAD BOTTOM ANGLE CORROSION AROUND FASTNER HOLES STA.520 / THE FORWARD CARGO AFT BULKHEAD BOTTOM ANGLE 'RAIL ASSY' FOUND TO HAVE ALLOWABLE LIMITS ON SRM IAW B737 SRM 51-10-02-0G-0 PARAGRAPH 9. REMOVED AND INSTALLED A NEW FORWARD CARGO COMPARTMENT FLOOR STRUCTURE AFT BULKHEAD BOTTOM ANGLE 'RAIL ASSY' IAW B737 SRM 51-40-02-0G-0 AND BOEING DRAWING 143A9481 ATAG WN3051 P/N:143A9485-35
AFT CARGO FLOOR PANEL 140EF HAS 1' CRACK 10' FROM FWD SIDE. / AFT CARGO FLOOR PANEL 140EF; HAS CRACK; OUT OF LIMITS IAW SRM 53-00-53-1A-1. REPLACED PANEL 140EF P/N 453A2610-58; 'A'TAG WN4173 ON NRC X888952
FWD CARGO COMP FLOOR STRUCTURE;LH Z-ANGLE CORROSION AROUND FASTNER HOLES STA.500B+14'-500F / FWD CARGO L/H Z-ANGKE STA 500B+14-500F CORROSION FASTENER HOLES. BLENDED AND REMOVED CORROSION IAW AMM 51-00-53-201. 'OUT OF LIMITS' IAW SRM 53-00-53-1A-2 MAT THICKNESS .40 MAT REMOVED .012 REMAINING .028. REMOVED Z-ANGLE STA 500B TO STA 500I IAW SRM 51-40-02-0G-0. FABRICATED; TRIMMED; ALODINED PRIMED NEW SECTION OF Z-ANGLE STA 500B TO STA 500I IAW SRM 51-40-05-0G-0; BOEING DWG 143A7500 REV:-; AMM 51-21-41-370-802; AMM 51-21-72-370-804; INSTALLED NEW SECTION OF Z-ANGLE IAW SRM 51-40-02-0G-0 ALSO BOEING DWG 143A7500. APPLIED C.I.C IAW AMM 51-21-91-620-802 P/N 143A7501-81
AFT CARGO; FWD OF DOOR FLOOR PLATE IS CORRODED (FWD TIE DOWN PLATE) / REPLACED AFT CARGO; FWD OF DOOR FLOOR PLATE P/N 453A2611-1 ATAG 'A89367' IAW B737 AIPC 25-52-10-04. THE NEW PLATE WILL BE INSTALLED ON W/O TASK CARD PANEL SIGN OFF SHEET # 422715; THE REPLACEMENT OF THE PART WAS IAW B737 SRM 51-10-02-0G-0; PARAGRAPH 9. ATAG: A89367
AFT CARGO; AFT OF DOOR FLOOR PLATE IS CORRODED (AFT TIEDOWN PLATE) / RECEIVED NEW AFT CARGO DOOR FLOOR PLATE TIEDOWN REQ MATERIAL ID MATERIAL ID IS 453A2611-2 AIW IPC 25-52-10-04 TAG # A69675 PART TO BE INSTALLED ON CARD WO 422715
AFT CARGO FLOOR PANEL 140EF HAS CORROSION ON O/B PERIMETER OF PANEL / AFT CARGO PANEL 140EF WAS OUT OF LIMITS RECEIVED NEW PANEL 453A2610-58. TO BE INSTALLED ON WORK CARD 422715 OUT OF LIMITS IAW SRM 53-00-53-1A-1 PANEL IAW IAW IPC 25-52-16-19 ATAG # WN4173
AFT CARGO FLOOR PANEL 140DF HAS CORROSION ON O/B AND AFT PERIMETER OF PANEL. / PANEL FOR AFT CARGO 140DF IS OUT OF LIMIT HAS CORROSION THE LENGTH OF PANEL OUT OG LIMITS IAW SRM 53-00-53-1A-1 MATERIAL ID FOR RECEIVED NEW IS 453A2610-20IAW IPC 25-52-10-19 PANEL INSTALLED ON CARD DOC SA-M 565S PG. 32 ITEM 1. ATAG NW9922
FORWARD CARGO COMP FLOOR STRUCTURE RT Z ANGLE CORRODED BETWEEN BS 500+14 TO BS 500E. REPAIRED Z ANGLE IAW SRM.
FWD CARGO COMP FLOOR STRUCTURE;RH Z-ANGLE CORROSION AROUND FASTNER HOLES STA.500+14'-500E / REMOVED Z ANGLE A500 TO 500E AND REPAIRED Z ANGLE IAW BOEING 737 SRM 53-00-53-2R-6 AND SPLICE IAW SRM 53-00-53-2R-5. P/N: 143A7501-158 TOOL AAR 36647 DUE 10 JUN 19
AFT CARGO FLOOR PANEL 140BF HAS CORROSION ON O/B PERIMETER OF PANEL / AFT CARGO FLOOR PANEL # 140BF A-TAG # WN1365 PN # 453A2610-32 PN # 7253513 IAW IPC 25-52-10-19 ORIGINAL PANEL FOUND TO BE OUT OF LIMITS WITH MORE THAN 10 INCHES OF DAMAGE IAW SRM 53-00-53-1A-1 FIG 102. NEW PANEL TO BE INSTALLED ON W/O 422715
LH WING L/E PANEL 521JB IS CRACKED / REPAIRED AND APPLIED DECORATIVE FINISH TO L/H WING L/E PANEL 521JB OF LIGHT DISBOND OF EDGE STRIP (AS MARKED) IAW B737-800 SRM 57-41-01-2R-6 REV 65 AND B737 AMM 51-21-99-300-801 REV 67. A22088; A74378
FWD CARGO FLOOR PANEL 120BF HAS CORROSION AROUND PERIMETER OF PANEL / DAMAGED AREA EXCEEDS LIMITS REPLACED PANEL 120BF P/N 453A1610-16 AS REQUIRED I.A.W. SRM 53-00-53-1A-1 I.P.C. 25-52-10-17
FWD CARGO FLOOR PANEL 120AF HAS CORROSION ON LH O/B SIDE. / DAMAGED AREA EXCEEDS LIMITS REPLACED PANEL 120AF P/N 453A1610-14 AS REQUIRED. I.A.W. SRM 53-00-53-1A-1 I.P.C. 25-52-10-17
FWD CARGO FLOOR PANEL 120DF HAS CORROSION AROUND PERIMETER OF PANEL / DAMAGED AREA EXCEEDS LIMITS REPLACED PANEL 120DF P/N 453A1610-20 AS REQUIRED I.A.W. SRM 53-00-53-1A-1 I.P.PC. 25-52-10-17
FWD CARGO FLOOR PANEL 120CF HAS CORROSION AROUND PERIMETER OF PANEL / VERIFIED NEW FWD CARGO FLOOR PANEL 120CF IAW IPC 25-52-10-17 FOUND FLOOR PANEL 120CF TO BE OUT OF LIMITS DUE TO CORROSION LENGTH OF OVER 10' IAW SRM 53-00-53-1A-1
LH WING T/E PANEL 551FB HAS BROKEN OFF BRACKET / REMOVED AND REPLACED BROKEN BRACKET ON L/H WING PANEL 551FB IAW BOEING 737 SRM 51-40-02
FORWARD CARGO COMP FLOOR STRUCTURE LT Z-ANGLE CORRODED BETWEEN BS 500B+14 TO BS 500F. R&R LT Z ANGLE IAW SRM AND DWG.
SEAL RETAINER AT THE TRAILING EDGE OF TJE L/H LOWER FIXED TRAILING EDGE PANEL 441GB IS CRACKED APPROX FIVE INCHES / REMOVED AND REPLACED THE TRAILING EDGE OF THE L/H LOWER TRAILING EDGE PANEL SEAL RETAINER. REF SRM 51-40-02 AND SIP
RT OVERHEAD BIN EMERGENCY LIGHT LENS CRACKED AT ROW 10. R&R COVER PER AMM.
LT OVERHEAD BIN EMERGENCY LIGHT LENS CRACKED AT ROW 19. R&R COVER PER AMM.
L/H WING #1 SLAT T/E WEDGE LOWER SKIN O/B END DELAMINSTED 1.2' X 3.5' / REMOVED & REPLACED L/H WING #1 SLAT PER AMM 27-81-21. P/N OFF/ON 114A5010-207; S/N OFF 004404; S/N ON 005741
#2 ENG STRUT PNL 441BR CORNERS HAVE DELAMINATION. LOWER AFT CORNER DAMAGE MEASURES 1.3 IN X 1.4 IN UPPER AFT CORNER MEASURES 2.9 IN X 2.3 IN. / REMOVED AND REPLACED PNL 441BR PER AMM 54-53-01 ROBBED FROM AIRCRAFT 283
R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM & SIP.
RIGHT WHEEL WELL VAPOR BARRIER CRACKED RBL 31.83. REPAIRED THE VAPOR BARRIER IAW EA.
LEFT EMERGENCY EXIT LIGHT LENS COVER MISSING AT ROW 27. INSTALLED THE COVER IAW AMM.
LEFT EMER AISLE LIGHT LENS COVER MISSING AT ROW 12. INSTALLED COVER IAW AMM.
LEFT OVERHEAD BIN, EMER LIGHT LENS CRACKED AT ROW 23. R & R LENS IAW AMM.
LEFT CABIN OVERHEAD BIN, EMER LIGHT LENS CRACKED AT ROW 18. R & R LENS IAW AMM.
LEFT CABIN OVERHEAD BIN, EMER LIGHT LENS CRACKED, BETWEEN ROWS 15 - 23. R & R LENS IAW AMM.
LEFT EMER ESCAPE LIGHT LENS, CRACKED BETWEEN ROWS 5 - 16. R & R LENS IAW AMM.
R1 DOOR EMER EVAC SLIDE LATCH BROKEN. REPAIRED LATCH IAW SIP.
R1 DOOR EMER EXIT SIGN FELL OFF. R & R LENS IAW SIP.
R1 DOOR EMER EXIT LIGHT THRESHOLD ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW SIP.
R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. INSTALLED COVER IAW SIP.
R1 DOOR LOWER LIGHT EXIT LIGHT COVER LOOSE. R & R LENS IAW SIP.