N8541W
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT NOT TESTING CORRECTLY. R & R FWD F/A FLASHLIGHT BATTERY PER SIP. CKS OK.
FWD LEFT EMERGENCY ISLE LIGHTS WILL NOT TURN ON. REMOVED AND REPLACE EMERGENCY BATTERY PACK AND PERFORMED GOOD OPS CHECK IAW AMM 33-51-06-960-805.
FWD RIGHT HAND EMERGENCY ISLE LIGHTS WILL NOT TURN ON. REMOVED AND REPLACE EMERGENCY BATTERY PACK AND PERFORMED GOOD OPS CHECK IAW AMM 33-51-06-960-805.
AFT LEFT HAND EMERGENCY ISLE LIGHTS WILL NOT TURN ON. REMOVED AND REPLACED BATTERY PACK AND PERFORMED GOOD OPS CHECK IAW B737-800 AMM 33-51-06-960-805.
RIGHT WING T/E BEAM 115A2759-14 HAS ELONGATED HOLES. REMOVED AND REPLACED RT WING T/E BEAM ASSY IAW DWG 115A2714, REV -, AND SRM 51-40-02. C/W MT.
AFT CARGO FLOOR PANEL 140EF IS CRACKED. REMOVED AND REPLACED AFT CARGO FLOOR PNL 140EF IAW B737-800 AMM 25-52-01-201-801 AND BOEING DWG. # 453A2610 REV. D.
RIGHT WING LEADING EDGE AT OFSS STATION 308 WING LEADING EDGE SUPPORT RIB CORRODED. REMOVED AND REPLACED STATION 308 WING LEADING EDGE SUPPORT RIB IAW BOEING DWG 116A5300 REV. A. AND SRM 51-40-02.
LEFT VAPOR BARRIER ATTACH ANGLE BS 663 CRACKED AT LBL9 AND 34. REMOVED VAPOR BARRIER LT ANGLE AT BS 663 IAW SRM 51-40-02 AND INSTALLED NEW ATTACH ANGLE L/H VAPOR BARRIER STA.663; IAW B737-800 SRM 51-40-02-0G-O; BOEING DRW 111A1000 REV B AND BOEING DRW 111A1000 REV -.
RIGHT VAPOR BARRIER ATTACH ANGLE STA.663 CRACKED AT RBL9 AND 34. REMOVED THE VAPOR BARRIER RT ANGLE AT STA.663 IAW SRM 51-40-02 AND INSTALLED NEW ATTACH ANGLE RT VAPOR BARRIER STA.663; IAW SRM 51-40-02-0G-O; BOEING DWG 111A1000 REV B AND BOEING DRW 111A1000 REV -.
APU SHUTDOWN IN FLIGHT. R & R APU LUBE MODULE IAW AMM 49-91-11.
AFT FLIGHT ATT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT AND FLASHLIGHT BATTERY AFT F/A CA?S SIDE INBD IN REF TO AMM 25-64-00. OPS CHECK GOOD MEL CLEARED.
EMERGENCY LIGHTS ON ROW 6 - 14 OVERHEAD BINS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK M1676 AND PERFORMED GOOD OPS CHECK IAW AMM 33-51-06. REMOVED AND REPLACED BATTERY PACK M1676 AND PERFORMED GOOD OPS CHECK IAW AMM 33-51-06.
LEFT & RIGHT OVERWING FWD DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT).
EGPR DOOR CUT OUT DOUBLER CRACKED AT LOWER SIDE. ACCOMPLISHED REPAIR ON EGPR DOOR SURROUND DOUBLER AT BS 224.8+7' AND 8' ABOVE S24R IAW B737-800 SRM 53-10-15-2R-4.
L2 AIRFRAMEDOOR ASSIST HANDLES NEED SECURED. SECURED L2 DOOR ASSIST HANDLES IAW AMM 25-21-25-420-801
CR RR R1 DOOR ASSIST HANDLE NEEDS SECURED. SECURED R1 DOOR ASSIST HANDLE IAW B737-800 AMM 52-41-31.
CR RR L1 DOOR ASSIST HANDLE NEEDS SECURED. SECURED L1 DOOR ASSIST HANDLES IAW AMM TASK 25-21-31-420-802.
FLT ATT REPORTS; EXIT SIGN @ MID CABIN CIELING LOOSE.<[01] SECURED EXIT SIGN PER M/M 33-51-01.
AFT OF R/H SECOND EMERGENCY EXIT HATCH EMERGENCY LIGHTS INOP. <[01] R&R BATTERY PACK AT SEAT ROW 20DEF AND AFT GALLEY IAW AMM 33-51-00. OPS CHK GOOD.
M1673 EMERGENCY LIGHT NOT POWERING LIGHTS AFTER DEEP CYCLE<[01] REMOVED AND REPLACED M1673 CHARGER ASSY AND BATTERY PACK REF AMM 33-51-06.
M1673 EMERGENCY LIGHT NOT POWERING LIGHTS AFTER DEEP CYCLE<[01] REMOVED AND REPLACED M1673 CHARGER ASSY AND BATTERY PACK REF AMM 33-51-06.
AFT FA MEGA PHONE PIECE MISSING<[01] REMOVED AND REPLACED AFT MEGA PHONE REF AMM 25-64-00
EMERGENCY EXIT SIGN AT AFT LAV CAPT. SIDE MISSING<[01] REPLACED EMERGENCY EXIT SIGN LENS AT AFT LAV CAPT. SIDE PER AMM 33-51-01. OPS CHECK GOOD.
ONE FORWARD FLIGHT ATTENDANT FLASHLIGHT INOP<[01] REPLACED BATTERY REF AMM 25-64-00
SEAT BACK AT 12D IS STUCK IN RECLINE<[01] SECURED UPRIGHT; SEAT 12D RECLINE INOP; ASSIGNED TO MEL 25-6-02<BR><BR>SP1B;[02] R&R SEAT 12D RECLINE LOCK. REF. CMM 25-23-67. OPS CHECK GOOD.
1 AFT EMERGENCY FLASHLIGHT IS INOP<[01] R/R EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00.OPS. CHECK GOOD.
L1 DOOR SLIDE LOWER FLAP REQUIRES REPOSITION.<[01] READJUSTED L1 DOOR LOWER FLAP PER SIP
SPEED TRIM FAIL ILLUMINATED ON CLIMBOUT FOLLOWED BY INOPERATIVE ELECTRIC L TRIM; NO OVERWEIGHT LANDING<[01] TROUBLESHOT PER FIM 27-41 TASK 804; RESET DTM INTERNAL LOGIC; REMOVED; INSPECTED AND CLEANED STAB TRIM MOTOR CONNECTOR; STAB TRIM OPERATES NORMALLY
FLT ATTENDANT REPORTS THAT MEGA - PHONE IS INOP<[01] REMOVED AND REPLACED FWD MEGA-PHONE PER AMM 25-64-00
OUTBOARD FLAP OUTBOARD SUPPORT FAIRING ADJUSTMENT; TASK 27-51-28-820-801 REQUIRED ON L/H WING #1.<[01] ACCOMPLISHED L/H WING OUTBOARD FLAP OUTBOARD SUPPORT FAIRING #1 ADJUSTMENT CHECK IAW AMM TASK 27-51-28-820-801;[02] INSPECTED WORK PERFORMED.
AFT CARGO AFT THRESHOLD CORNER CRACKED<[01] REMOVED AND REPLACED AFT CARGO AFT SCUFF PLATE PER AMM 53-11-02-420-801;[02] PARTS;[03] 1. JOHN RABOZZI (TECHNICIAN); 20-JUL-2023 16:46 UTC<BR>REMOVED AND REPLACED AFT CARGO AFT SCUFF PLATE PER AMM 53-11-02-420-801<BR>2. JASON MILLER (TECHNICIAN); 22-JUL-2023 11:10 UTC<BR>PARTS;[04] COMPLETE;[05] C/W PER AMM 53-11-02-420-801
FOWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP<[01] R&R POWER SUPPLY BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD IAW AMM TASK CARD 33-51-00-710-801.;[02] C/W INSPECTION
RIGHT HORIZONTAL STAB FWD UPPER SLIDER SEAL CRACKED.<[01] REMOVED AND REPLACED SLIDER SEAL IAW AMM 53-31-31.;[02] C/W INSPECTION
LEFT HORIZONTAL STAB FWD UPPER SLIDER SEAL CRACKED.<[01] REMOVED AND REPLACED L/H FORWARD UPPER HORIZONTAL STABILIZER SLIDING SEAL PER AMM 53-53-31-400-801;[02] REMOVED AND REPLACED L/H FORWARD UPPER HORIZONTAL STABILIZER SLIDING SEAL PER AMM 53-31-31-400-801
L/H FORWARD UPPER HORIZONTAL STABILIZER SLIDING SEAL REQUIRES ADJUSTMENT.<[01] REMOVED AND REPLACED L/H FORWARD UPPER HORIZONTAL STABILIZER SLIDING SEAL PER AMM 53-53-31-400-801;[02] REMOVED AND REPLACED L/H FORWARD UPPER HORIZONTAL STABILIZER SLIDING SEAL PER AMM 53-31-31-400-801
AFT CARGO FLOOR STRUCTURE RH BAFFLE STA 747 TO 767; RBL 22; HAS CORROSION. AFT CARGO STRUCTURE RH BAFFLE STA 747 TO 767 RBL 22 HAS CORROSION.<[01] REMOVED AFT CARGO FLOOR STRUCTURE RH BAFFLE STA 747 TO 767 PER SRM 51-40-02.;[02] DRILLED NEW RH BAFFLE 146A7505-12 PER SRM 51-10-02 AND 51-40-02. OK TO INSTALL.;[03] C/W INSPECTION OF CORRECTIVE ACTION STEP #2;[04] REMOVED AND REPLACED BAFFLE PER SRM 51-40-02.;[05] REMOVED CORROSION FROM AREA PER SRM 51-10-02 (0.025' REMAINING THICKNESS). BAFFLE IS OUT OF LIMITS PER SRM 51-10-02. REMOVED AND REPLACED BAFFLE PER SRM 51-40-02.
FLOORBOARD PANEL 222BF (P/N 141A5810-464) DELAMINATED AT UNDERSIDE OF AFT DRAIN HOLE. FLOORBOARD PANEL 22BF (P/N 141A5810-464) DELAMINATED AT UNDERSIDE OF AFT DRAIN HOLE.<[01] INSTALLED NEW SERVICEABLE FLOORBOARD PANEL 222BF (P/N 141A5810-464) ON CARD NO. TTG8Q00L4JU7.;[02] C/W INSPECTION
#1 ENG. I/B FAN COWL; OIL SERVICE DOOR WEB CRACKED<[01] REMOVED AND REPLACED I/B FAN COWL OIL SERVICE DOOR WEB IAW SRM 51-40-02;[02] VERIFIED C/A # 1 : . JAMES LYNCH (TECHNICIAN); 06-JUL-2023 00:29 UTC<BR>REMOVED AND REPLACED I/B FAN COWL OIL SERVICE DOOR WEB IAW SRM 51-40-02
FWD CARGO; STA 500I BULKHEAD LOWER ANGLE HAS CORROSION IN SEVERAL AREAS RBL 24 TO LBL 24<[01] REMOVED CORROSION; REMAINING STRUCTURE THICKNESS IS OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[02] REMOVED CORROSION; REMAINING STRUCTURE THICKNESS IS OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[03] REMOVED AND REPLACED ANGLE IAW SRM 51-40-02.;[04] REMOVED AND REPLACED ANGLE IAW SRM 51-40-02
AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDEPLATE HAS SURFACE CORROSION FROM STA 727J TO 747 RBL 23<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.036' REMAINING THICKNESS). SIDEPLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] SIDE PLATE IS REPAIRED FROM STA 727G TO STA 767 ON FAULT ID # TTG8Q00LUT3R;[03] RII: SIDEPLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2. SIDE PLATE IS REPAIRED FROM STA 727G TO STA 767 ON FAULT ID # TTG8Q00LUT3R.
AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDEPLATE HAS SURFACE CORROSION FROM STA 747 TO 767 RBL 23<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.035' REMAINING THICKNESS). SIDEPLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] SIDE PLATE IS REPAIRED FROM STA 727G TO STA 767 ON FAULT ID # TTG8Q00LUT3R;[03] RII: SIDE PLATE IS REPAIRED FROM STA 727G TO STA 767 ON FAULT ID # TTG8Q00LUT3R
AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDEPLATE HAS SURFACE CORROSION FROM STA 767 TO 787 RBL 23<[01] REMOVED CORROSION FROM AREA PER SRM 53-60-15-1A-1 (0.030' REMAINING THICKNESS). SHIELD (SIDEPLATE) IS OUT OF LIMITS PER SRM 53-60-15-1A-1.;[02] REMOVED SHIELD (SIDEPLATE) PER SRM 51-40-02.;[03] LOCATED HOLES ON NEW SHIELD (SIDEPLATE) PER SRM 51-40-02.;[04] INSTALLED NEW SHIELD PER SRM 51-40-02;[05] INSPECTION VERIFIED CORRECTIVE ACTION STEP 4.;[06] COMPLETED CARD
AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDEPLATE HAS SURFACE CORROSION FROM STA 727I TO 727J RBL 23<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). SIDEPLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] SIDE PLATE IS REPAIRED FROM STA 727G TO STA 767 ON FAULT ID # TTG8Q00LUT3R;[03] RII: SIDE PLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2. SIDE PLATE IS REPAIRED FROM STA 727G TO STA 767 ON FAULT ID # TTG8Q00LUT3R.
AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDEPLATE HAS SURFACE CORROSION FROM STA 727H TO 727I RBL 23<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.036' REMAINING THICKNESS). SIDEPLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] SIDE PLATE IS REPAIRED FROM STA 727G TO STA 767 ON FAULT ID # TTG8Q00LUT3R;[03] RII: SIDE PLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2. SIDE PLATE IS REPAIRED FROM STA 727G TO STA 767 ON FAULT ID # TTG8Q00LUT3R.
AFT CARGO COMPARTMENT DOOR THRESHOLD WEB HAS SURFACE CORROSION FROM STA 787+7 TO STA 847 RBL 27.<[01] REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-60-15;[02] REMOVED WEB FOR REPLACMANT PER SRM 51-40-02;[03] LOCATED AND DRILLED HOLES FOR NEW WEB PER SRM 51-40-05.INSTALLED NUTPLATES PER SRM 51-40-02;[04] INSPECTED C/A #3 LOCATION & DRILLED HOLES & NUTPLATE INSTALL;[05] OK TO INSTALL WEB;[06] OK TO INSTALL WEB;[07] REMOVED AND REPLACED WEB PER SRM 51-40-02;[08] REMOVED AND REPLACED WEB PER SRM 51-40-02
AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDEPLATE HAS SURFACE CORROSION FROM STA 727G TO 727H RBL 23<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). SIDEPLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] CUT OUT AND REMOVED DAMAGED SECTION OF RH SIDEPLATE FROM STA 727F+10' TO STA 767 PER SRM 53-00-53-2R-5.;[03] DRILLED REPLACEMENT SECTION AND SPLICE OF RH SIDEPLATE FROM STA 727F+10' TO STA 767 PER SRM 53-00-53-2R-5. OK TO TREAT AND PAINT.;[04] TREATED AND PAINTED REPLACEMENT SECTION AND SPLICE OF RH SIDEPLATE FROM STA 727F+10' TO STA 767 PER SRM 51-20-01 AND AMM 51-21-72. OK TO INSTALL NUTPLATES AND ATTACH SPLICE TO REPLACEMENT SECTION.;[05] C/W INSPECTION OF CORRECTIVE ACTION STEP #4;[06] INSTALLED SPLICE TO REPLACEMENT SECTION PER SRM 51-40-02. INSTALLED ADHESIVE BOND NUTPLATES PER SRM 51-40-10 AT 1300 3JUL2023.;[07] INSTALLED SIDEPLATE REPAIR FROM STA 727F+10? TO STA 767 PER SRM 53-00-53-2R-510] REPAIRED RH SIDEPLATE FROM STA 727F+10? TO STA 767; RBL 23 PER SRM 53-00-53-2R-5.;[11] INSPECTED WORK PERFORMED
AFT CARGO COMPARTMENT FLOOR STRUCTURE LEFT SIDEPLATE HAS SURFACE CORROSION FROM STA 767 TO 787 LBL 23<[01] COMPLIED WITH MEASUREMENT REQUIREMENTS.;[02] COMPLIED WITH TOOL REQUIREMENT.;[03] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 ( 0.036' REMAINING THICKNESS). SIDEPLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2;[04] EDITED MEASUREMENTS.;[05] CERTIFIED.;[06] SIDE PLATE IS REPAIRED FROM STA 727I TO STA 787+10? ON FAULT ID # TTG8Q00LUT14;[07] C/W INSPECTION
AFT CARGO COMPARTMENT FLOOR STRUCTURE LEFT SIDEPLATE HAS SURFACE CORROSION FROM STA 747 TO 767 LBL 23<[01] COMPLIED WITH TOOL REQUIREMENT.;[02] COMPLIED WITH MEASUREMENT REQUIREMENTS.;[03] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 ( 0.035' REMAINING THICKNESS). SIDEPLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2;[04] EDITED MEASUREMENTS.;[05] CERTIFIED.;[06] SIDE PLATE IS REPAIRED FROM STA 727I TO STA 787+10? ON FAULT ID # TTG8Q00LUT14;[07] C/W INSPECTION
AFT CARGO COMPARTMENT FLOOR STRUCTURE LEFT SIDEPLATE HAS SURFACE CORROSION FROM STA 727J TO 747 LBL 23<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.037' REMAINING THICKNESS). SIDEPLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] EDITED MEASUREMENTS.;[03] CERTIFIED.;[04] SIDE PLATE IS REPAIRED FROM STA 727I TO STA 787+10? ON FAULT ID # TTG8Q00LUT14;[05] C/W INSPECTION
AFT CARGO COMPARTMENT FLOOR STRUCTURE LEFT SIDEPLATE HAS SURFACE CORROSION FROM STA 727I TO 727J LBL 23<[01] REMOVED CORROSION FROM AREA PER SRM 53-00-53-1A-2 (0.034' REMAINING THICKNESS). SIDEPLATE IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] CUT AND REMOVED DAMAGED SECTION OF LEFT SIDEPLATE FROM STA 727H+10 TO STA 787+10 I.A.W SRM 53-00-53-2R-5.;[03] DRILLED REPLACEMENT SECTION AND SPLICES OF LH SIDEPLATE FROM STA 727H+10' TO STA 787+10? PER SRM 53-00-53-2R-5. TREATED AND APPLIED PRIMER TO REPAIR PARTS PER SRM 51-20-01 AND AMM 51-21-72. OK TO INSTALL NUTPLATES AND ATTACH SPLICE TO REPLACEMENT SECTION.;[04] INSPECTION VERIFIED CORRECTIVE ACTION STEP 3.;[05] INSTALLED SPLICES TO REPLACEMENT SECTION PER SRM 51-40-02. INSTALLED ADHESIVE BOND NUTPLATES PER SRM 51-40-10 AT 0430 7JUL2023.09] INSTALLED FWD REPAIR SPLICE ON LH SIDEPLATE AT STA 727H+10'; LBL 23 PER SRM 53-00-53-2R-5.;[10] INSPECTED WORK PERFORMED ON C/A #9;[11] COMPLETED INSTALLATION OF REPAIR SECTION AND SPLICES OF LH SIDEPLATE FROM STA 727H+10' TO STA 787+10? PER SRM 53-00-53-2R-5.;[12] C/W INSPECTION OF STEP #11;[13] REPAIRED PER SRM 53-00-53-2R-5.;[14] C/W INSPECTION
AFT GALLEY FLOOR STRUCTURE STA. 947.5 LBL 56; AFT ENTRY 'Z' ANGLE HAS CORROSION AROUND NUT PLATE HOLES. AREA MARKED IS ADJACENT TO 2 HI LOCKS AND NOT AROUND NUTPLATE HOLES<[01] CORRECTED LOCATION TO STA 947.5 ON MEASUREMENTS.;[02] REMOVED CORROSION WITHIN LIMITS PER SRM53-70-51-1A-1. OK TO TREAT AND PAINT.;[03] REMOVED CORROSION WITHIN LIMITS PER SRM 51-10-02 AND 53-70-51-1A-1. OK TO TREAT AND PAINT.;[04] REMOVED CORROSION WITHIN LIMITS PER SRM 51-10-02 AND 53-70-51-1A-1. OK TO TREAT AND PAINT. C/W INSPECTION;[05] REMOVED CORROSION WITHIN LIMITS PER SRM 51-10-02 AND 53-70-51-1A-1. TREATED AND PRIMED AREA PER SRM 51-20-01 AND AMM 51-21-72.;[06] REMOVED CORROSION WITHIN LIMITS PER SRM 51-10-02 AND 53-70-51-1A-1. TREATED AND PRIMED AREA PER SRM 51-20-01 AND AMM 51-21-72 C/W INSPECTION;[07] REMOVED CORROSION WITHIN LIMITS PER SRM 51-10-02 AND 53-70-51-1A-1. TREATED AND PRIMED AREA PER SRM 51-20-01 AND AMM 51-21-72 C/W INSPECTION
AFT GALLEY FLOOR STRUCTURE INTERCOSTAL STA. 951 RBL 54 (ADJACENT TO R/H O/B LAV MOUNT) HAS CORROSION. (MARKED)<[01] REMOVED CORROSION WITHIN LIMITS PER SRM53-70-51-1A-1. OK TO TREAT AND PAINT.;[02] REMOVED CORROSION WITHIN LIMITS PER SRM 51-10-02 AND 53-70-51-1A-1. OK TO TREAT AND PAINT.;[03] REMOVED CORROSION WITHIN LIMITS PER SRM 51-10-02 AND 53-70-51-1A-1. OK TO TREAT AND PAINT. C/W INSPECTION;[04] PREVIOUSLY REMOVED AFT GALLEY MOUNT AT STA 947.5 PER SRM 51-40-02. TREATED AND PRIMED AREA PER SRM 51-20-01 AND AMM 51-21-72. OK TO INSTALL MOUNT AT STA 947.5.;[05] PREVIOUSLY REMOVED AFT GALLEY MOUNT AT STA 947.5 PER SRM 51-40-02. TREATED AND PRIMED AREA PER SRM 51-20-01 AND AMM 51-21-72. OK TO INSTALL MOUNT AT STA 947.5. C/W INSPECTION;[06] INSTALLED AFT GALLEY MOUNT AT STA 947.5 RBL54 PER SRM 51-40-02. COMPLETED PERMANENT REPAIR OF AREA PER SRM 51-10-02 AND 53-70-51-1A-1.
AFT GALLEY DOOR CUTOUT Z ANGLE STA. 967-987 RBL 47; HAS CORROSION. (MARKED)<[01] REMOVED CORROSION WITHIN LIMITS PER SRM53-70-51-1A-1. OK TO TREAT AND PAINT.;[02] REMOVED CORROSION WITHIN LIMITS PER SRM 51-10-02 AND 53-70-51-1A-1. OK TO TREAT AND PAINT.;[03] REMOVED CORROSION WITHIN LIMITS PER SRM 51-10-02 AND 53-70-51-1A-1. OK TO TREAT AND PAINT. C/W INSPECTION;[04] REMOVED CORROSION WITHIN LIMITS PER SRM 51-10-02 AND 53-70-51-1A-1. TREATED AND PRIMED AREA PER SRM 51-20-01 AND AMM 51-21-72.;[05] REMOVED CORROSION WITHIN LIMITS PER SRM 51-10-02 AND 53-70-51-1A-1. TREATED AND PRIMED AREA PER SRM 51-20-01 AND AMM 51-21-72 C/W INSPECTION;[06] REMOVED CORROSION WITHIN LIMITS PER SRM 51-10-02 AND 53-70-51-1A-1. TREATED AND PRIMED AREA PER SRM 51-20-01 AND AMM 51-21-72 C/W INSPECTION
RH ELEVATOR HINGE COVER PANEL 344AB IS CRACKED. (MARKED)<[01] NEW PANEL TO BE INSTALLED PER AMM 20-50-11 ON FAULT # TTG8Q00L4K6X (344AB CLOSE CARD).
AFT GALLEY FLOOR STRUCTURE STA. 947.5 LBL 25 HAS CORROSION ON FLOOR BEAM.<[01] REMOVED CORROSION PER SRM 51-10-02. BLENDED AREA OUT OF LIMITS PER SRM 53-70-51-1A-1. REMANING THICKNESS IS .084?.[10] FABRICATED ALL REPAIR PARTS I.A.W SRM 53-70-51-2R-5;[11] VERIFIED FABRICATED ALL REPAIR PARTS I.A.W SRM 53-70-51-2R-5. OK TO TREAT PRIME AND INSTALL REPAIR PARTS.;[12] INSTALLED PART [1] T-CHORD; ALL PART [2] ANGLES; AND ALL PART [3] STRAPS I.A.W SRM 53-70-51-2R-5.;[13] INSTALLED PART [1] T-CHORD; ALL PART [2] ANGLES; AND ALL PART [3] STRAPS I.A.W SRM 53-70-51-2R-5.;[14] INSTALLED PART [1] T-CHORD; ALL PART [2] ANGLES; AND ALL PART [3] STRAPS I.A.W SRM 53-70-51-2R-5.;[15] RII: INSPECTED WORK PERFORMED IN STEPS 1 THRU 8.;[16] COMPLETED REPAIR OF STA 947.5 FLOOR BEAM AND ATTACHMENT OF ADJACENT STRUCTURE IAW SRM 53-70-51-2R-5 AND 51-40-02.;[17] RII: INSPECTION COMPLIED WITH. SEE STEPS AND CORRECTIVE ACTIONS FOR ALL WORK PERFORMED. COMPLETED REPAIR OF STA 947.5 FLOOR BEAM AND ATTACHMENT OF ADJACENT STRUCTURE IAW SRM 53-70-51-2R-5 AND 51-40-02.
LEFT WING; WINGLET SPLIT SCIMITAR UPPER END HAS POSSIBLE CRACK 8' BELOW UPPER CAP. (MARKED)<[01] REMOVED DAMAGED STRAKLET FROM A/C INVENTORY AND REPLACED WITH NEW SERVICEABLE STRAKLET. STRAKLET TO BE INSTALLED ON MT# &NBSP;&NBSP;&NBSP;&NBSP;&NBSP;757-31-01 (INSP - INTERNAL - LEFT WINGLET -700 AND -800 WITH BLENDED WINGLET AND SPLIT SCIMITAR) [TTG8Q00D2KT4];[02] VERIFIED C/A #1.
FWD ENTRY DOOR GIRT BAR HARD TO ARM/DISARM / [01] INSPECTED FWD ENTRY GIRT BAR AND FLOOR MOUNTED BRACKETS. NO DEFECTS NOTED. CLEANED FLOOR BRACKETS AND INSTALLED GIRT BAR INTO FLOOR BRACKETS. NO INTERFERENCE. OPS CHECK GOOD. REF AMM 25-66-01
LEFT INBD AFT FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT NOT BLINKING; RIGHT OUTBD AFT LEFT INBD AFT FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT NOT BLINKING RIGHT OUTBD AFT FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT NOT BLINKING. / [01] REPLACE BATTERY OF L INBOARD AFT AND R OUTBOARD AFT FA FLASHLIGHTS PER AMM 25-64-00. OPS CHECK GOOD.
AFT FLASHLIGHT HAS NO CHARGE. / [01] OK TO CONTINUE PER MEL 25-12-01. C/W SP-1B; AUTH# 66372.;[02] REPLACED AFT LEFT HAND HANDSET PER M/M 25-64-00. OPS CHECKS OK;[03] CORRECTION: REPLACED AFT RIGHT FLIGHT ATTENDANT FLASHLIGHT PER M/M 25-64-00. OPS CHECKS OK
L/H BREAK PANEL CRACKED IN THE AIR CONDITIONING DISTRIBUTION BAY IN FORWARD CARGO COMPARTMENT AT B.S. 540. / [01] REMOVED CABIN FLOOR PANEL TO ACCESS L/H BREAK PANEL PER AMM 53-21-00;[02] INSTALLED BREAK ANGLE PER SRM 51-40-02;[03] INSTALLED FLOOR PANEL PER AMM 53-21-00<BR>REINSTALLED CARPET PER AMM 25-27-15
3 EMERGENCY FLASHLIGHTS WILL NOT TEST; CAPTS SIDE CABIN FORE AND AFT AND F/O SID 3 EMERGENCY FLASHLIGHTS WILL NOT TEST CAPTS SIDE CABIN FORE AND AFT AND F/O SIDE AFT GALLEY OTBD / [01] REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERIES; OPS NORMAL AT THIS TIME. 33-55-00. THIS CLEARS MEL 25-12-01. L/P-1730155.
L/H WING # 3 CANUE FWD FAIRING IS CRACKED ; LH WING # 3 CANE FWD FAIRING IS CRACKED / [01] REMOVED AND REPLACED L/H WING # 3 FLAP SUPPORT FAIRING IAW AMM 27-51-18
R/H O/B AFT FLASHLIGHT INOP AT AFT FLIGHT ATTENDANT STATION. ; RH IB AFT FLASHLIGHT INOP AT AFT FLIGHT ATTENDANT STATION. / [01] PERFORMED OPS CK OF BOTH AFT F/A R/H INBD AND OTBD EMERGENCY FLASH LIGHTS IAW AMM 25-64-00. OPS CK GOOD AT THIS TIME. BOTH AFT F/A R/H INBD AND OTBD FLASHLIGHTS REQUIRE WHITE TAMPER STRIPS.; [02] OPS CHECK GOOD & INSTALLED WHITE TAMPER STRIPS PER AMM 25-64-00. THIS CLEARS MEL 25-12-01.
EXIT SIGN LOOSE CENTER OF AIRCRAFT / SECURED EXIT SIGN PER SIP
FWD F/A MEGAPHONE INOP / REPLACED FWD MEGAPHONE AND PERFROMED OPS TEST PER AMM 25-64-00. A/C OK FOR SERVICE
THE MEGAPHONE IN THE AFT GALLEY DOES NTO SHOW THE GREEN GLASHING LIGHT. / R&R AFT GALLEY MEGAPHONE BATTERIES AS PER AMM 25-64-00 MEGAPHONE OP'S CHECKS NORMAL AT THIS TIME
L-1 DOOR SLIDE GRIT BAR BINDS IN FLOOR ATTACH POINTS WHEN ATEMPTING TO DISARM RESTORED SLIDE RIBBON TO GIRT BAR IN SLIDE CASE PER AMM 25-66-00. GIRT OPERATION CHECK FREELY ARMS & DISARMS.
MID CABIN EMERGENCY "EXIT" SIGN FELL OUT. / SECURED LENS PER AMM.
R1 DOOR SLIDE GIRT BAR STORAGE LATCH, LT SIDE INOPERATIVE. REPOSITIONED THE LATCH IAW SIP.
LT OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM.