N8530W
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
AFT ENTRY DOOR SLIDE IS OUT OF CASE. REINSTALLED L2 DOOR SLIDE IAW MT 72561-06. NO DEFECTS NOTED.
AFT FA FLASHLIGHT WOULD NOT TEST. REPLACED AFT FLASHLIGHT BATTERY REF AMM 25-64-00. OPS CHECK GOOD
EMERGENCY LIGHTS ON COVE PANELS ABOVE OVERHEAD BINS LOCATED AT SEAT ROW 14DEF AND 15 ABC ARE INOP. REMOVED AND REPLACED IAW AMM 33-51-03-960-802-NG. OPS CHECKED GOOD.
CENTER CABIN FLOORBOARD 231XF HAD FIBERS FRAYING. REMOVED AND INSTALLED THE FLOORBOARD 231XF IAW AMM 53-21-00.
CENTER CABIN FLOORBOARD 241AF, FIBERS FRAYING. REMOVED AND INSTALLED THE FLOORBOARD 241AF IAW AMM 53-21-00.
RIGHT WING UPPER TE SHELF PANEL SUPPORT ANGLE, SEAL RETAINER UPPER AFT OTBD CORNER CRACKED JUST INBD OF DEFLECTION RIB. REMOVED RT WING UPPER TE SHELF PANEL SUPPORT ANGLE/SEAL RETAINER PER SRM 51-40-02. DRILLED NEW INTERCOSTAL PER SRM 51-40-05 AND INSTALLED NEW INTERCOSTAL PER SRM 41-40-02. REMOVED RW UPPER TE SHELF PANEL SUPPORT ANGLE/SEAL RETAINER PER SRM 51-40-02. DRILLED NEW INTERCOSTAL PER SRM 51-40-05 AND INSTALLED NEW INTERCOSTAL PER SRM 41-40-02. CLEANED AND RESTORED FINISHED PER AMM 51-21-95 RW UPPER TE SHELF PANEL; REF FOR RESTORED FINISHED AMM 51-21-99. CW INSPECTION OF RESTORED FINISH.
BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT LBL 34. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02 AND DWG 111A1000. WORK ACCOMPLISHED AND EA M-24-157-02340.
BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT RBL 9. REPAIRED I.A.W. SRM 57-10-10-2R-5 AND EA-M-24-157-02340. REMOVED AND REPLACED ANGLE IAW SRM 57-10-10-2R-5 AND DWG 111A1000.
BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT LBL 9. SEE ATTACHED PICTURE.<LOCATED; DRILLED; AND DEBURRED NEW SERVICEABLE BS 663 LH VAPOR BARRIER ATTACH ANGLE IAW SRM 51-40-05. REMOVED AND REPLACED VAPOR ATTACH ANGLE PER SRM 51-40-02; BOEING DRAWING 111A1000; AND EA M-24-157-02340 (TTG8Q01B5908).
BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT RBL 34. REMOVED BS 663 VAPOR BARRIER ATTACH ANGLE SECTION FROM APROX. RBL 5 TO RBL 65 PER SRM 51-40-02. LOCATED; DRILLED AND DEBURRED NEW REPLACEMENT ANGLE IAW SRM 51-40-05. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02 AND DWG 111A1000.
LEFT WING DEFLECTION RIB INTERCOSTAL CRACKED AT O/B UPPER FASTENER HOLE<[01] REMOVED DEFLECTION RIB INTERCOSTAL PER SRM 51-40-02;[02] DRILLED NEW INTERCOSTAL PER SRM 51-40-05 AND INSTALLED NEW INTERCOSTAL PER SRM 41-40-02;[03] INSPECTED C/A 1. LANCE BEARD (TECHNICIAN); REMOVED DEFLECTION RIB INTERCOSTAL PER SRM 51-40-02. C/A 2. STEVEN POULIN (TECHNICIAN); DRILLED NEW INTERCOSTAL PER SRM 51-40-05 AND INSTALLED NEW INTERCOSTAL PER SRM 41-40-02;[04] CLEANED AND RESTORED FINISHED PER AMM 51-21-95;[05] REF FOR RESTORED FINISHED AMM 51-21-99;[06] CW INSP OF RESTORED FINISHED;[07] VERIFIED C/A 1-6 ARE COMPLIED WITH.
LEFT WING DEFLECTION RIB INTERCOSTAL OTBD ATTACH ANGLE CRACKED.<[01] REMOVED ATTACH ANGLE PER SRM 51-40-02;[02] DRILLED NEW ATTACH ANGLE PER SRM 51-40-05 AND INSTALLED NEW RIB PER SRM 41-40-02;[03] DRILLED NEW ATTACH ANGLE PER SRM 51-40-05 AND INSTALLED NEW ANGEL PER SRM 41-40-02;[04] VERIFIED C/A 1-3 ARE COMPLIED WITH..
GIRT BAR LOOSE ON FWD ENTRY DOOR. FOUND SHEARED RIVET ON FWD ENTRY DOOR SLIDE J HOOK. INSTALLED A NEW RIVET IAW SRM 51-40-02-0G-0, PARA 4B.
EMERGENCY LIGHT AFT OF THE RT FLAP INOPERATIVE. REMOVED AND REPLACED THE LAMP ON THE EMERGENCY EXIT LIGHT AFT OF THE RT FLAP IAW AMM 33-51-04. OPS GOOD.
RIGHT OVERWING HEADER EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED M1671 AND OWE BATTERY PACK PER AMM 33-51-06-960-805-NG, POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT. OPS CHECK GOOD.
L2 DOOR BOTH ASSIST HANDLES LOOSE. SECURED BOTH L2 DOOR ASSIST HANDLES IAW B737NG AMM 52-13-31-400-802 SUBTASK 52-13-31-020-008.
L2 DOOR LINER ASSIST HANDLE NUT BROKEN<[01] REMOVED AND REPLACED ASSIST HANDLE NUT AND SECURED ASSIST HANDLE IAW B737NG AMM 52-13-31-400-802 SUBTASK 52-13-31-020-008 PO:1128177.1;[02] VERIFIED REMOVED AND REPLACED ASSIST HANDLE NUT AND SECURED ASSIST HANDLE IAW B737NG AMM 52-13-31-400-802 SUBTASK 52-13-31-020-008 PO:1128177.1
OVER WING CENTER ISLE EMER EXIT LIGHT LENSE FELL OFF<[01] REPLACED OVER WING CENTER ISLE; EMER EXIT SIGN PER M/M33-51-01
EXIT ROW COVER NEEDS REATTACHED.<[01] REATTACHED EXIT ROW COVER PER SIP
CABIN OVERHEAD EMERGENCY EXIT SIGN DETACHED<[01] RESECURED CABIN OVERHEAD EMERGENCY EXIT SIGN LENS COVER AS PER AMM 33-51-01
CABIN EMERGENCY EXIT ROW SIGN BROKEN <[01]. RE-ATTACHED CABIN OVERHEAD EMERGENCY EXIT LENS PER AMM REF 33-51-01.
CREW REPORTS 1 FWD FA EMERGENCY FLASHLIGHT WILL NOT TEST.<[01] RE-SEATED FWD FA EMERGENCY FLASHLIGHT REF. 25-64-00. TEST LIGHT WORKS NORMAL.
EXIT SIGN OVER EMERGENCY EXIT ROW FELL OFF. <[01] RE-ATTACHED SIGN COVER REF. SIP.
OVERWING OVERHEAD EXIT ROW SIGN FELL OFF<[01] REATTACHED EMER EXIT SIGN AMM 33-51-01
LEFT AFT EMERGENCY EXIT LIGHT INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
AFT LAV EMERGENCY EXIT LIGHT COVER MISSING.<[01] REPLACED AFT LAV EMERGENCY EXIT LIGHT COVER PER SIP
LH INDOOR EMERGENCY WINDOW LIGHT INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-960-802-NG (EXIT SIGN - LIGHT ASSEMBLY REPLACEMENT - PERMANENT)]
AFT FA FLASHLIGHT INOP<[01] REPLACED AFT FA FLASHLIGHT BATTERY PER AMM 25-64-00
LH SIDE FWD MOST POSTION FLOOR PATH LIGHTING HAS MOISTURE INSIDE TRACK<[01] REMOVED AND REPLACED PHOTOLUMINESCENCE STRIP AT 2ABC (L/H FWD) PER [AMM 33-51-15-960-801-NG (FLOOR PROXIMITY LIGHT - PHOTOLUMINESCENT STRIP REPLACEMENT - PERMANENT)].
F/A REPORTS FWD GALLEY OB EMERGENCY FLASHLIGHT HOLDER TEST LIGHT DOESN'T BLINK<[01] R & R FLASHLIGHT BATTERY PER AMM 25-64-00.
FWD GALLEY FLASHLIGHT GREEN LIGHT DOES NOT COME ON: AND THE RED LIGHT IS DIM<[01] R&R FWD LH FLASHLIGHT PER AMM 25-64-00
MID AFT OVHD EMER EXIT LENS COVER MISSING<[01] REPLACED MID AFT OVHD EMER EXIT LENS COVER PER AMM 33-51-01
L/H WING PANEL 521CB HAS ELONGATED FASTNER HOLE.<[01] REPAIRED L/H WING PANEL 521CB IAW SRM 51-70-04;[02] INSPECTION C/W.
FWD CABIN R/H EMERGENCY LIGHTS BATTERY PACK FAILED OPS CHECK<[01] REMOVED AND REPLACED FWD CABIN EMERGENCY LIGHT BATTERY PACK PER MM 33-51-06.FWD CABIN EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] COMPLIED WITH INSPECTION; REMOVED AND REPLACED FWD CABIN EMERGENCY LIGHT BATTERY PACK PER MM 33-51-06.FWD CABIN EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06
FWD CABIN R/H EMERGENCY LIGHTS BATTERY PACK FAILED OPS CHECK<[01] REMOVED AND REPLACED FWD CABIN EMERGENCY LIGHT BATTERY PACK PER MM 33-51-06.FWD CABIN EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[02] COMPLIED WITH INSPECTION; REMOVED AND REPLACED FWD CABIN EMERGENCY LIGHT BATTERY PACK PER MM 33-51-06.FWD CABIN EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06
AFT GALLEY EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACKS AT STA 952L AND STA 952R PER MM 33-51-06;[02] C/W INSPECTION;[03] AFT GALLEY EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[04] REMOVED AND REPLACED BATTERY PACKS AT STA 952L AND STA 952R PER MM 33-51-06; AFT GALLEY EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06
FWD CABIN LEFT EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACE BATTERY PACK AT STA 565L PER MM 33-51-06;[02] C/W INSPECTION;[03] FWD CABIN EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[04] COMPLIED WITH INSPECTION; REMOVED AND REPLACE BATTERY PACK AT STA 565L PER MM 33-51-06; FWD CABIN EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.
FWD GALLEY L/H EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK AT STA 317L PER MM 33-51-06;[02] C/W INSPECTION;[03] FWD GALLEY EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06
FWD CABIN LEFT EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACE BATTERY PACK AT STA 565L PER MM 33-51-06;[02] C/W INSPECTION;[03] FWD CABIN EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[04] COMPLIED WITH INSPECTION; REMOVED AND REPLACE BATTERY PACK AT STA 565L PER MM 33-51-06; FWD CABIN EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.
#8 LEADING EDGE SLAT HAS A LARGE AREA OF DELAMINATION ON THE BOTTOM OUTBOARD END OF THE AFT WEDGE.<[01] ACCOMPLISHED INSTALLATION OF INBOARD AND OUTBOARD MAIN TRACKS AT SLAT ATTACH POINT PER MM 27-81-21;[02] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #1;[03] RII INSPECTED AS REQUIRED. PERFORMED VISUAL INSPECTION OF INBOARD SLAT TRACK CAN AND OUTBOARD SLAT TRACK DRY BAY AREA FOR FOREIGN DEBRIS PRIOR TO INSTALL OF #8 SLAT. NO DISCREPANCIES NOTED. OK TO INSTALL #8 SLAT.;[04] RII INSPECTED AS REQUIRED; #8 SLAT INSTALLATION IN STEP 1. SLAT ACTUATOR TO SLAT CONNECTION TO BE ACCOMPLISHED ON TASK CARD TTG8R007UPWG;[05] ADDED PART NUMBER AND SERIAL NUMBER TO SUB INVENTORY;[06] REMOVED AND REPLACED #8 SLAT PER AMM 27-81-21. PERFORMED LEADING EDGE SLAT ADJUSTMENT PER AMM 27-81-00.;[07] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #6
PANEL 193CL HAVE A DENT AND DELAMINATION ON THE MIDDLE TOPSIDE OF PANEL.<[01] REPAIRED PANEL 193CL PER SRM 51-70-05-2R-1;[02] VERIFIED REPAIR COMPLETED PER SRM 51-70-05-2R-1.;[03] RESTORED FINISH PER SRM 51-70-05-2R-1.
L/H TRANSITION ANGLE HAS CORROSION AT STATION 787-10.<[01] REMOVED DAMAGE. MATERIAL REMOVED IS .015IN. REMAINING THICKNESS OF .035IN. ORIGINAL THICKNESS OF .050IN. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] NEW L/H TRANSITION ANGLE AND REPAIR SPLICES TO BE INSTALLED FROM 727+4 TO 847 PER SRM 53-00-53-2R-5. ALL INSTALLATION WORK TO BE ACCOMPLISHED ON NR # (TTG8Q00JWK6V).;[03] VERIFIED CA-#1. MICHAEL PETERSON (TECHNICIAN); 18-MAR-2023 16:45 UTC<BR>REMOVED DAMAGE. MATERIAL REMOVED IS .015IN. REMAINING THICKNESS OF .035IN. ORIGINAL THICKNESS OF .050IN. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[04] VERIFIED LONNIE HERMANN (TECHNICIAN); 29-MAR-2023 05:42 UTC<BR>NEW L/H TRANSITION ANGLE AND REPAIR SPLICES TO BE INSTALLED FROM 727+4 TO 847 PER SRM 53-00-53-2R-5. ALL INSTALLATION WORK TO BE ACCOMPLISHED ON NR # (TTG8Q00JWK6V).;[05] VERIFIED LONNIE HERMANN (TECHNICIAN); 29-MAR-2023 05:42 UTC<BR>NEW L/H TRANSITION ANGLE AND REPAIR SPLICES TO BE INSTALLED FROM 727+4 TO 847 PER SRM 53-00-53-2R-5. ALL INSTALLATION WORK TO BE ACCOMPLISHED ON NR # (TTG8Q00JWK6V).
FLIGHT COMPARTMENT FLOOR PANEL 211AF HAS MULTIPLE DENTS AND DISFORMED.<[01] LOCATED/DRILLED FASTENER HOLES IN REPLACEMENT PANEL IAW SRM 51-10-02. PAINTED PANEL IAW AMM 25-00-00. PANEL TO BE INSTALLED ON FAULT #TTG8Q00HCAKE.;[02] COMPLIED WITH INSPECTION OF THE LOCATED/DRILLED FASTENER HOLES IN REPLACEMENT PANEL IAW SRM 51-10-02. PAINTED PANEL IAW AMM 25-00-00. PANEL TO BE INSTALLED ON FAULT #TTG8Q00HCAKE.
AFT CARGO FLOOR BOARD STRIP CORROSION STA 727D+6<[01] REPLACED WITH NEW TEE STRIP ASSY P/N 146A9401-8 PER AMM 25-52-10.;[02] REPLACED WITH NEW PART.;[03] INSPECTION C/W.
AFT CARGO ANGLE CRACKED STA 867 LBL 14 JUST BELOW LAV TANK ENCLOSURE VERTICAL SUPPORT ANGLE.<[01] REMOVED AND REPLACED AFT CARGO ANGLE CRACKED STA 867 LBL 14 ENCLOSURE VERTICAL SUPPORT ANGLE PER SRM 51-40-02;[02] REMOVED AND REPLACED AFT CARGO ANGLE CRACKED STA 867 LBL 14 ENCLOSURE VERTICAL SUPPORT ANGLE PER SRM 51-40-02
AFT CARGO WATER TANK SUPPORT BRACKET CRACKED STA 947 LBL 10. (MARKED)<[01] REMOVED AFT CARGO WATER TANK SUPPORT BRACKET PER SRM 51-40-02.;[02] INSTALLED NEW AFT CARGO FITTING PART #149A8113U6 IAW SRM 51-40-02;[03] VERIFIED C/A #2.
AFT CARGO R/H TRANSITION ANGLE JUST AFT OF CARGO DOOR CUTOUT HAS CORROSION.<[01] REMOVED DAMAGE. MATERIAL REMOVED IS .015IN. REMAINING THICKNESS OF .035IN. ORIGINAL THICKNESS OF .050IN. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] LOCATED AND DRILLED NEW SHIELD PLATE PER SRM 51-40-02.;[03] RII. VERIFIED LOCATED AND DRILLED NEW SHIELD PLATE PER SRM 51-40-02. SIGN OFF FOR CORRECTIVE ACTION #2.;[04] INSTALLED NEW R/H SHIELD(TRANSITION ANGLE) JUST AFT OF CARGO DOOR CUTOUT FROM STA. 847 TO STA. 867; RBL 22? PER SRM 51-40-02.;[05] INSTALLED WORK ABOVE
AFT CARGO R/H TRANSITION ANGLE CORROSION FROM STA 727F THRU STA767.<[01] REMOVED TRANSITION ANGLE PER SRM 51-40-02.;[02] REMOVED L/H TRANSITION ANGLE PER SRM 51-40-02 TO FOM;[13] INSTALLED R/H TRANSITION ANGLE PER SRM 51-40-02;[14] CORRECTION FOR LINE 13; INSTALLED REPLACEMENT R/H TRANSITION ANGLE FROM STA 727 TO STA 767. PER SRM 51-40-02 AND SRM REPAIR 53-00-3-2R-5;[15] VERIFIED INSTALLATION OF NEW R/H TRANSITION ANGLE FROM STA 727 TO STA 767 PER SRM 51-40-02 WITH REPAIR SPLICE INSTALLED AT STA 727F+10 PER SRM 53-00-53-2R-5.;[16] FOR INFORMATIONAL PURPOSES: CORROSION DISCREPANCIES LOCATED BETWEEN STA. 727F AND STA. 727F+10? ARE REPAIRED ON FAULT TTG8Q00JWGJM. SEE FAULT FOR ALL WORK ACCOMPLISHED.;[17] INSPECTED WORK ABOVE;[18] CERTIFIED EDIT
AFT CARGO L/H TRANSITION ANGLE CORROSION FROM STA 727F THRU STA 847.<[01] REMOVED L/H TRANSITION ANGLE PER SRM 51-40-02 TO FOM;[02] REMOVED DAMAGE OF .010IN OF MATERIAL. REMAINING THICKNESS OF .040IN. ORIGINAL THICKNESS OF .050IN. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[03] TRANSITION ANGLE CUT AT 727J+13? AND 727F+10?. FABRICATED NEW TRANSITION ANGLE SECTION FROM 727+4? TO 727F+10?; FABRICATED NEW TRANSITION ANGLE SECTION FROM 727F+10? TO 727J+13?; AND FABRICATED NEW TRANSITION ANGLE SECTION FROM 727J+13? TO 847. FABRICATED REPAIR SPLICE PLATES FOR 727F+10? AND FOR 727J+13? ALL PER SRM 53-00-53-2R-5.;[04] VERIFIED STEP#3. LONNIE HERMANN (TECHNICIAN); 29-MAR-2023 06:05 UTC TRANSITION ANGLE CUT AT 727J+13? AND 727F+10?. FABRICATED NEW TRANSITION ANGLE SECTION FROM 727+4? TO 727F+10?; FABRICATED NEW TRANSITION ANGLE SECTION FROM 727F+10? TO 727J+13?; AND FABRICATED NEW TRANSITION ANGLE SECTION FROM 727J+13? TO 847. FABRICATED REPAIR SPLICE PLATES FOR 727F+10? AND FOR 727J+13? ALL PER SRM 53-00-53-2R-5.;[05] INSTALLED ADHESIVELY BONDED NUTPLATES ON NEW TRANSITION ANGLE FROM STA 727+4? TO 847 PER SRM 51-40-10.;[06] INSPECTED WORK ABOVE;[07] RII OK TO INSTALL L/H TRANSITION ANGLE REPAIR SECTIONS STA. 727+4 TO STA. 847.;[08] INSTALLED REPAIR PARTS PER SRM 53-00-53-2R-5.;[09] RII. VERIFIED INSTALLATION OF L/H TRANSITION ANGLE 727+4 TO STA. 847 ONLY. SIGN OFF FOR CORRECTIVE ACTION #8.;[10] FAULT C/W
AFT CARGO L/H TRANSITION ANGLE CORROSION AROUND FASTENER HOLE STA 727D +4<[01] DID NOT REWORK THIS CORROSION DUE TO THIS SECTION IS BEING REPAIRED ON NR # (TTG8Q00JWK6V).;[02] NEW L/H TRANSITION ANGLE FROM 727+4? TO 847 AND REPAIR SPLICE PLATES TO BE FABRICATED AND INSTALLED PER SRM 53-00-53-2R-5 ON NR # (TTG8Q00JWK6V).;[03] VERIFIED LONNIE HERMANN (TECHNICIAN); 29-MAR-2023 05:53 UTC<BR>NEW L/H TRANSITION ANGLE FROM 727+4? TO 847 AND REPAIR SPLICE PLATES TO BE FABRICATED AND INSTALLED PER SRM 53-00-53-2R-5 ON NR # (TTG8Q00JWK6V).
AFT CARGO R/H TRANSITION ANGLE HAS FASTENER PULLED THROUGH STA 727E AT FRAME.< REMOVED TRANSITION ANGLE PER SRM 51-40-02.;[02] REMOVED RIVET. RIVET WAS PULLED THROUGH DUE TO CORROSION AROUND FASTENER. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;CUT AND REMOVED DAMAGED SECTION OF R/H TRANSITION ANGLE(SIDEPLATE) FROM STA. 727 TO STA. 727F+10? OBTAINED BAC1496-377 SIDEPLATE FROM STORES. LOCATED AND DRILLED NEW SIDEPLATE FROM STA. 727 TO STA. 727F+10? AND THE REPAIR SPLICE AT STA. 727F+10? PER SRM 53-00-53-2R-5 RII;[06] ALODINED AND PRIMED REPAIR PARTS PER SRM 51-20-01 AND SOPM 20-41-02. OK TO INSTALL REPAIR PARTS PER SRM 53-00-53-2R-5 FROM STA. 727 TO STA. 727F+10?;[07] ALODINED AND PRIMED REPAIR PARTS PER SRM 51-20-01 AND SOPM 20-41-02. OK TO INSTALL REPAIR PARTS PER SRM 53-00-53-2R-5 FROM STA. 727 TO STA. 727F+10?;INSTALLED BONDED NUTPLATES TO R/H SIDEPLATE FROM STA. 727 TO STA. 727F+10? AT 0200HRS ON 24-MAR-2023 PER SRM 51-40-10.;INSTALLED BONDED NUTPLATES TO R/H SIDEPLATE FROM STA. 727 TO STA. 727F+10? AT 0200HRS ON 24-MAR-2023 PER SRM 51-40-10.INSPECTED;INSTALLED REPAIR PARTS FROM STA. 727 TO STA 727F+10? PER SRM 53-00-53-2R-5.
AFT CARGO R/H TRANSITION ANGLE STA 867+6 ON SMALL TRANSITION ANGLE HA CORROSION.<[01] REMOVED AFT CARGO R/H TRANSITION ANGLE STA 867 + 6 TO FOM;[02] REMOVED DAMAGE. MATERIAL REMOVED IS .006IN. REMAINING MATERIAL IS .044IN. ORIGINAL THICKNESS OF .050IN. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[03] REMOVED AND REPLACED AFT CARGO R/H TRANSITION ANGLE BETWEEN STA. 867 TO STA. 887 PER SRM 51-40-02.;[04] C/W REMOVED AND REPLACED AFT CARGO R/H TRANSITION ANGLE BETWEEN STA. 867 TO STA. 887 PER SRM 51-40-02.
AFT CARGO R/H TRANSITION ANGLE JUST FWD OF CARGO DOOR OPENING HAS CORROSION.<[01] REMOVED DAMAGE. MATERIAL REMOVED WAS .012IN. REMAINING IS .038IN. ORIGINAL THICKNESS WAS .050IN. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED AFT CARGO R/H TRANSITION ANGLE JUST FWD OF CARGO DOOR OPENING (SHIELD) PER SRM 51-40-02;[03] LOCATED AND DRILLED AFT CARGO R/H TRANSITION ANGLE JUST FWD OF CARGO DOOR OPENING (SHIELD) PER SRM 51-40-05;[04] REPLACED TRANSITION ANGLE (SHIELD) PER SRM 51-40-02.;[05] COMPLIED WITH INSPECTION OF REPLACED TRANSITION ANGLE (SHIELD) PER SRM 51-40-02.
AFT CARGO DOOR CUTOUT LOWER THRESHOLD WEB HAS CORROSION.<[01] REMOVED DAMAGE OF .012IN OF MATERIAL. REMAINING THICKNESS OF .038IN. ORIGINAL THICKNESS OF .050IN. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. SO REQUIRES REPLACEMENT.;[02] REMOVED AFT CARGO DOOR CUTOUT LOWER THRESHOLD WEB. ALL WORK REFERENCE SRM 51-40-02.;[03] INSTALLED NEW AFT CARGO CUTOUT LOWER THRESHOLD WEB IAW SRM 51-40-02;[04] VERIFIED C/A #3.
AFT GALLEY TIE DOWN INTERCOSTAL AT STA. 947+2'; RBL 53 HAS CORROSION. THIS IS THE CORRECTED FAULT FROM TTG8Q00JUV4M BECAUSE OF INCORRECT STATION LOCATION.<[01] REMOVED DAMAGED INTERCOSTAL BETWEEN STA. 947 TO STA. 967; AT RBL 53. CORROSION DAMAGE IS .040' DEEP AND IS OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] VERIFIED CORRECTIVE ACTION #1; CORROSION REMOVAL IS OUT OF LIMITS.;[03] DRILLED UP INTERCOSTAL PER SRM 51-40-06.;[04] OK TO INSTALL INTERCOSTAL;[05] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.
AFT CARGO FLOOR BOARD STRIP HAS CORROSION STA 767+6.<[01] REPLACED WITH NEW TEE STRIP PER AMM 25-52-10.;[02] REPLACED WITH NEW PART.;[03] INSPECTION C/W.
AFT CARGO ANGLE CRACKED STA 867 LBL 14 JUST BELOW LAV TANK ENCLOSURE VERTICAL SUPPORT ANGLE.<[01] REMOVED AND REPLACED AFT CARGO ANGLE CRACKED STA 867 LBL 14 ENCLOSURE VERTICAL SUPPORT ANGLE PER SRM 51-40-02;[02] REMOVED AND REPLACED AFT CARGO ANGLE CRACKED STA 867 LBL 14 ENCLOSURE VERTICAL SUPPORT ANGLE PER SRM 51-40-02
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 241WF<[01] INSTALLED FLOOR BOARD PANEL 241WF I.A.W. AMM 53-21-00;[02] VERIFIED C/A #1.
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 241UF<[01] REMOVED AND REPLACED PASSENGER CABIN FLOOR PANEL 241UF PER AMM 53-21-00.;[02] INSPECTION C/W
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 241F<[01] REMOVED AND REPLACED FLOOR PANEL 241F PER AMM 53-21-00. REFERRED TO TASK # TTG8Q00HC98Z FOR WORK ACCOMPLISHED. TORQUE WRENCH # T000023 S/N 920183.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 242SF<[01] REPLACED WITH NEW PANEL; INSTALLATION TO BE ACCOMPLISHED ON TTG8Q00HCAGR.;[02] PER AMM 53-21-00.;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 242RF<[01] REPLACED WITH NEW PANEL; INSTALLATION ACCOMPLISHED ON TTG800HCAGT.;[02] PER AMM 53-21-00;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 241XF<[01] REPLACED WITH NEW PANEL; INSTALLATION ACCOMPLISHED ON TTG800HC98P.;[02] PER AMM 53-21-00;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 222AF.<[01] FLOOR PANEL 222AF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 222AF CLOSE CARD ON LINE 422.;[02] VERIFIED.
PASSENGER CABIN FLOOR BEAM STRUCTURE HAS CORROSION IN AND AROUND NUT PLATE HOLE BS328 RBL 21.<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1. DAMAGED PART P/N 141A5504-26 ORIGINAL THICKNESS = .125?; REMAINING THICKNESS AFTER INITIAL BLEND = .110?. CORROSION STILL REMAINING AROUND EDGE OF HOLE.;[02] VERIFIED DAMAGE IS OUT OF LIMITS .BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1. DAMAGED PART P/N 141A5504-26 ORIGINAL THICKNESS = .125?; REMAINING THICKNESS AFTER INITIAL BLEND = .110?. CORROSION STILL REMAINING AROUND EDGE OF HOLE.;[03] ACCOMPLISHED ULTRA SOUND THICKNESS OF BLENDED AREA PER NDT PART 4 51-00-00 PROC. 3;[04] CORRECTION TO NDT REF. ACCOMPLISHED ULTRA SOUND THICKNESS OF BLENDED AREA PER NDT PART 4 51-00-00 PROC. 2;[05] UPDATED PARTS AND MEASUREMENTS INFORMATION.;[06] FLOORBEAM REPAIRED PER EA 23-153-00902.;[07] C/W INSPECTION.;[08] C/W INSPECTION.
AFT GALLEY TIE DOWN AT STATION 947 RBL 25 HAS CORROSION (MARKED)<[01] REMOVED CORROSION AROUND AFT GALLEY TIE DOWN AT STA 947 RBL 25 PER SRM 51-10-02. MAX MATERIAL REMOVED WAS 0.036?.;[02] VERIFIED REMOVED CORROSION AROUND AFT GALLEY TIE DOWN AT STA 947 RBL 25 PER SRM 51-10-02. MAX MATERIAL REMOVED WAS 0.036?.;[03] BLENDED OUT DAMAGED AREA; FABRICATED SHIM AND APPLIED ALODINE AND PRIMER TO BLENDED AREA AND SHIM ALL PER EA 23-153-00895 AND SRM 53-70-51-2R-8 ALTERNATIVE 3.;[04] VERIFIED BLENDOUT OF DAMAGE; SHIM FABRICATION; TREATING AND PRIMING OF REPAIR PARTS.;[05] OK TO INSTALL.;[06] INSTALLED REPAIR SHIM AND LAV MOUNT AT STA. 947 RBL 25 PER EA 23-153-00895 AND SRM 53-70-51-2R-8 ALTERNATIVE 3.;[07] INSPECTED INSTALLATION OF REPAIR SHIM AND AFT MOUNT AT STA 947 RBL 25 PER EA 23-153-00895 AND SRM 53-70-51-2R-8 ALTERNATIVE 3.;[08] C/W;[09] REPAIRED PER EA 23-153-00895;[10] UPDATED PARTS INFO;[11] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #9
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 242UF<[01] REFERRED TO CARD NO. TTG8Q00HCAGP FOR WORK ACCOMPLISHED. REMOVED AND REPLACED CABIN FLOOR BOARD 242UF PER AMM 53-21-00. TORQUE WRENCH # T000023 S/N NO. 920183.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 241YF<[01] REPLACED WITH NEW PANEL; INSTALLATION ACCOMPLISHED ON TTG800HCA69.;[02] PER AMM 53-21-00;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 231BF<[01] FLOOR PANEL 231BF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 231BF CLOSE CARD ON LINE 1114.;[02] VERIFIED.
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 222CF<[01] FLOOR PANEL 222CF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 222CF CLOSE CARD ON LINE 1124.;[02] VERIFIED.
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 222DF<[01] FLOOR PANEL 222DF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 222DF CLOSE CARD ON LINE 1122.;[02] VERIFIED.
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 242D<[01] REPLACED WITH NEW PANEL; INSTALLATION TO BE ACCOMPLISHED ON TTG8Q00HC98H.;[02] PER AMM 53-21-00;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 241AAF<[01] REPLACED WITH NEW PANEL; INSTALLATION TO BE ACCOMPLISHED ON TTG8Q00HC99H.;[02] PER AMM 53-21-00;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 242F<[01] REMOVED AND REPLACED CABIN FLOOR PANEL 242F PER AMM 53-21-00. REFERRED TO ROUTINE CARD TTG8Q00HC98B FOR WORK ACCOMPLISHED. TORQUE WRENCH # T000023 S/N 920183.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 242E<[01] REMOVED AND REPLACED FLOOR PANEL 242E PER AMM 53-21-00. REFERRED TO TASK # TTG8Q00HC98D FOR WORK ACCOMPLISHED. TORQUE WRENCH # T000023 S/N 920183.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
AFT SERVICE DOOR Z ANGLE HAS CORROSION AT STATION 986 +5 (MARKED)<[01] AFT SERVICE DOOR Z ANGLE HAS CORROSION AT STATION 986 +5 ; STATION LOCATION WAS WRITTEN IN ERROR SEE FAULT TTG8Q00JVCK1 FOR CORRECTED LOCATION.;[02] VERIFIED NEW FAULT GENERATED WITH CORRECT STA. LOCATION.
AFT GALLEY TIE DOWN AT STATION 967 +18 RBL 53 HAS CORROSION (MARKED)<[01] AFT GALLEY TIE DOWN AT STATION 967 +18 RBL 53 HAS CORROSION; STATION LOCATION WAS WRITTEN IN ERROR SEE FAULT TTG8Q00JV91U FOR CORRECTED LOCATION.;[02] VERIFIED NEW FAULT GENERATED WITH CORRECT STA. LOCATION.
AFT SERVICE DOOR Z ANGLE HAS CORROSION AT STATION 967 +9 (MARKED)<[01] AFT SERVICE DOOR Z ANGLE HAS CORROSION AT STATION 967 +9 ; STATION LOCATION WAS WRITTEN IN ERROR SEE FAULT TTG8Q00JVC1T FOR CORRECTED LOCATION.;[02] VERIFIED NEW FAULT GENERATED WITH CORRECT STA. LOCATION.
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 221DF<[01] FLOOR PANEL 221DF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 221DF CLOSE CARD ON LINE 1132.;[02] VERIFIED.
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 242QF<[01] INSTALLED FLOOR PANEL 242QF I.A.W. AMM 53-21-00;[02] VERIFIED C/A #1.
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 241E<[01] REMOVED AND REPLACED FLOOR PANEL 241E PER AMM 53-21-00. REFERRED TO TASK # TTG8Q00HC993 FOR WORK ACCOMPLISHED. TORQUE WRENCH # T000023 S/N 920183.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 241UF<[01] REMOVED AND REPLACED PASSENGER CABIN FLOOR PANEL 241UF PER AMM 53-21-00.;[02] INSPECTION C/W
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 241VF<[01] INSTALLED FLOOR PANEL 241VF I.A.W. AMM 53-21-00.;[02] VERIFIED C/A #1.
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 242QF<[01] INSTALLED FLOOR PANEL 242QF I.A.W. AMM 53-21-00;[02] VERIFIED C/A #1.
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 242PF<[01] INSTALLED FLOOR PANEL 242PF I.A.W. AMM 53-21-00.;[02] VERIFIED C/A #1.
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 241F<[01] REMOVED AND REPLACED FLOOR PANEL 241F PER AMM 53-21-00. REFERRED TO TASK # TTG8Q00HC98Z FOR WORK ACCOMPLISHED. TORQUE WRENCH # T000023 S/N 920183.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 241E<[01] REMOVED AND REPLACED FLOOR PANEL 241E PER AMM 53-21-00. REFERRED TO TASK # TTG8Q00HC993 FOR WORK ACCOMPLISHED. TORQUE WRENCH # T000023 S/N 920183.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 241YF<[01] REPLACED WITH NEW PANEL; INSTALLATION ACCOMPLISHED ON TTG800HCA69.;[02] PER AMM 53-21-00;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 241XF<[01] REPLACED WITH NEW PANEL; INSTALLATION ACCOMPLISHED ON TTG800HC98P.;[02] PER AMM 53-21-00;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 221AF<[01] FLOOR PANEL 221AF IS BEING REPLACED WITH A NEW FLOOR PANEL AND IS BEING INSTALLED ON THE 221AF CLOSE CARD ON LINE 2013.;[02] THE LINE NUMBER FOR PANEL 221AF CLOSE ON THE PREVIOUS SIGNOFF IS INCORRECT. THE PANEL 221AF CLOSE CARD IS ON LINE 1138.;[03] INSPECTION C/W
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 221BF<[01] FLOOR PANEL 221BF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 221BF CLOSE CARD ON LINE 1136.;[02] VERIFIED.
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 222BF.<[01] FLOOR PANEL 222BF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 222BF CLOSE CARD ON LINE 420.;[02] VERIFIED.
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 241ABF<[01] REMOVED AND REPLACED FLOOR PANEL 241ABF PER AMM 53-21-00. REFERRED TO TASK # TTG8Q00HC99F FOR WORK ACCOMPLISHED. TORQUE WRENCH # T000023 S/N 920183.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 221CF<[01] FLOOR PANEL 221CF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 221CF CLOSE CARD ON LINE 1134.;[02] VERIFIED.
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 221EF<[01] FLOOR PANEL 221EF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 221EF CLOSE CARD ON LINE 1130.;[02] VERIFIED.
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 241ZF<[01] REPLACED WITH NEW PANEL; INSTALLATION ACCOMPLISHED ON TTG800HCASM.;[02] PER AMM 53-21-00;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 221EF<[01] FLOOR PANEL 221EF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 221EF CLOSE CARD ON LINE 1130.;[02] VERIFIED.
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 241D<[01] REPLACED WITH NEW PANEL; INSTALLATION TO BE ACCOMPLISHED ON TTG8Q00HC997.;[02] PER AMM 53-21-00;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 221F<[01] FLOOR PANEL 221FF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 221FF CLOSE CARD ON LINE 1128.;[02] VERIFIED. PANEL 221FF.
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 232BF<[01] FLOOR PANEL 232BF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 232BF CLOSE CARD ON LINE 798.;[02] VERIFIED.
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 232AF<[01] FLOOR PANEL 232AF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 232AF CLOSE CARD ON LINE 800.;[02] VERIFIED.
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 231AF<[01] FLOOR PANEL 231AF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 231AF CLOSE CARD ON LINE 1116.;[02] VERIFIED.
PASSENGER CABIN FWD WET AREA FLOOR PANEL HAS DELAMINATION 231CF<[01] FLOOR PANEL 231CF IS BEING REPLACED WITH A NEW PANEL AND IS BEING INSTALLED ON THE 231CF CLOSE CARD ON LINE 1112.;[02] VERIFIED.
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 241VF<[01] INSTALLED FLOOR PANEL 241VF I.A.W. AMM 53-21-00.;[02] VERIFIED C/A #1.
PASSENGER CABIN AFT WET AREA FLOOR PANEL HAS DELAMINATION 242PF<[01] INSTALLED FLOOR PANEL 242PF I.A.W. AMM 53-21-00.;[02] VERIFIED C/A #1.
RIGHT WING DEFLECTION RIB HAS ELONGATED HOLES AT SHELF PANEL ATTACH POINT.<[01] REMOVED DAMAGE FROM FIXED UPPER RIB PER SRM 57-51-02-2R-1.[05] FABRICATED AND LOCATED REPAIR PARTS PER SRM 57-51-02-2R-4 TABLE 102; ITEMS 1 THRU 4 AND VENDOR PO# P6895661 AND P6895665.;[06] FABRICATED AND LOCATED REPAIR PARTS PER SRM 57-51-02-2R-4 TABLE 102; ITEMS 1 THRU 4; SRM 57-51-02-2R-1 AND VENDOR PO# P6895661 AND P6895665.;[07] VERIFIED C/A # 6 : RICHARD BLACKBURN (TECHNICIAN); 30-MAR-2023 01:40 UTC<BR>FABRICATED AND LOCATED REPAIR PARTS PER SRM 57-51-02-2R-4 TABLE 102; ITEMS 1 THRU 4; SRM 57-51-02-2R-1 AND VENDOR PO# P6895661 AND P6895665.;10] ACCOMPLISHED R/H WING DEFLECTION RIB AND UPPER SUPPORT BEAM REPAIR PER SRM 57-51-02-2R-1; SRM 57-51-02-2R-4; AND EA 23-157-01051-WIP1.;[11] RII: INSPECTED WORK PERFORMED. 10. RICHARD BLACKBURN (TECHNICIAN); 31-MAR-2023 05:48 UTC ACCOMPLISHED R/H WING DEFLECTION RIB AND UPPER SUPPORT BEAM REPAIR PER SRM 57-51-02-2R-1; SRM 57-51-02-2R-4; AND EA 23-157-01051-WIP1.;[12] ADDED TOOLING;[13] REPAIRED IAW SRM 57-51-02-2R-1 AND SRM 57-51-02-2R-4. SEE ATTACHED CORRECTIVE ACTIONS/STEPS FOR INDIVIDUAL SIGN OFFS.;[14] COMPLIED WITH INSPECTION; REPAIRED IAW SRM 57-51-02-2R-1 AND SRM 57-51-02-2R-4. SEE ATTACHED CORRECTIVE ACTIONS/STEPS FOR INDIVIDUAL SIGN OFFS.
RIGHT SIDE EXTERNAL EMERGENCY LIGHTS INOP<[01] FOUND FWD SERVICE DOOR BATTERY PACK FOR BATTERY POWER SUPPLY M02816 INOP.;[02] REMOVED AND REPLACED FWD BATTERY PACK M02816 PER AMM 33-51-06;[03] PN OFF. D717-01-100<BR>SN OFF 433245
FWD SERVICE DOOR GIRT BAR STUCK IN HANGAR. / [01] FREE?D GIRT BAR FROM HANGAR AND OPS CHECKED GOOD REF <BR>MM 25-66-01
EMERGENCY FLASHLIGHTS IN AFT GALLEY ON B SIDE WILL NOT TEST. / [01] RESEATED FLASH LIGHTS IN CRADLE OPS CHECKS GOOD IAW MM 25-64-00
MID CABIN EXIT SIGN LENSE FELL OFF / [01] REINSTALL LENS PER AMM 33-51-01
AFT ENTRY SLIDE PRESSURE LOW ; / [01] REPLACED AFT ENTRY DOOR SLIDE IAW MT 725-61-06-AC
OVERWING EMERGENCY EXIT SIGN AFT LENS IS MISSING. / REPLACED LENS PER SIP
AFT SERVICE DOOR SLIDE BLINALE HAS CORD HANGING. SECURED THE SLIDE IAW SIP.
AFT SLIDE OUT OF POSITION REPACKED R2 SLIDE PER MT 725-61-06
R/H OVERWING EXIT SIGN COVER BROKEN. / R&R COVER IAW AMM.
FORWARD JUMP SEAT EMERGENCY FLASHLIGHT FLASHED RED. / R&R BATTERY PER SIP.