N242WN
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 | 2010-04-28 – 2010-04-28 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2010-04-28 – 2010-04-28 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
T/E UPPER FIXED PANEL OTBD OF NR 7 SPOILER HAS A CRACKED ANGLE ON INBD SIDE. MATCH DRILLED SERVICEABLE REPLACEMENT FITTING AND INSTALLED TO WEB IAW SRM 51-40-02. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02.
ELONGATED HOLES ON ACCESS PANEL 661BB, RT WING. REPAIRED THE ACCESS PANEL 661BB IAW SRM 51-70-04-2R-9, REPAIR 9.
ELONGATED HOLES ON ACCESS PANEL 561BB TRAILING EDGE, LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10.
CRACK LEADING EDGE RIB LOCATED LE HSS 105.26, RT HORIZONTAL STAB. REPLACED THE LEADING EDGE RIB AND FASTENERS IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 186A1001, SHEET 10, REV A.
CRACKED SUPPORT ANGLE LOCATED BS360 BTW STR27R TO STR28R AT EQUIPMENT ELECTRONIC COMP. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02. MEASUREMENT OF CRACK 0.210 INCH.
CORROSION WEB INTERNAL CAVITY LEADING EDGE LOCATED OFSS276, RT WING. PERFORMED PERMANENT REPAIR ON WEB IN THE INTERNAL CAVITY LEADING EDGE IAW SRM 51-70-11-2R-0, REPAIR GENERAL, PARAGRAPH 4.
CRACKED ANGLE, BS 663, RBL 8 IN THE AIR CONDITIONING BAY. REPLACED THE REPAIR ANGLE, BS 663, RBL 5 - RBL 30 IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, SRM 57-10-10-2R-5, REPAIR 5, DWG 111A10000, SHEET: 202, REV -, & MPM 52.1.1.1.
CRACK RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS 734, RT WING. REPLACED THE RAIL NUT PLATES AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 112A4402, SHEET 14, REV-.
CRACKED BRACKET, BTWN BS 540 - 560, RBL 7. REPLACED THE BRACKET IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 212A1116, SHEET 1, REV -.
CRACKED RAIL NUT PLATES, INTERNAL CAVITY LEADING EDGE LOCATED OFSS 577, LT WING. REPLACED RAIL NUT PLATES AND FASTENERS IAW SRM 51-40-02, AND DWG 112A4402, SHEET 14, REV -. MEASUREMENT OF CRACK: 0.438 INCH.
CRACK ON THE INBD SIDE, LOWER CHORD INSPAR RIB HSS 120.30 IN THE RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON THE RIB IAW SRM 55-10-09-2R-5, REPAIR 5, FIGURE 205.
CRACKED ANGLE BRACKET, BTW BS 540 - 560, LBL 7. REPLACED THE ANGLE BRACKET IAW SRM 51-10-02-0G, ITEM 9, AND DWG 212A1116, SHEET 1, REV - . MEASUREMENT OF CRACK: L: 0.782 INCH.
CRACKED RAIL NUT PLATES, INTERNAL CAVITY OF THE LEADING EDGE, OFSS449, LT WING. REPLACED THE NUT PLATES & FASTENERS IAW SRM 51-40-02, & DWG 112A4402, SHEET 40, REV A.
CORRODED STRAP, BS 887, RBL 10, WL 156 IN THE AFT CARGO BAY. REPLACED THE STRAP IAW SRM 51-10-02, SRM 51-40-02, AND DWG 14YA7500, SHEET 85, REV A.
CORROSION SUPPORT ZEE, BS 727 - 767, RBL 21, WL 156 IN THE AFT CARGO BAY. MANUFACTURED & DRILLED A NEW SUPPORT ZEE IAW SRM 51-40-05, AND DWG 146A7502, SHEET 26, REV-. REPLACED THE SUPPORT ZEE & FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 146A7500, SHEET 85, REV A, & DWG 146A7502, SHEET 26, REV-.
CORRODED FLOOR SUPPORT, BS 706 - 716, LBL 65, WL 202. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, DWG 144A7700, SHEET 144, REV B, & DWG 144A7730, SHEET 7, REV -.
CORRODED FLOOR SUPPORT BTWN BS 706 - 716, RBL 65, WL 202. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, DWG 144A7700, SHEET 144, REV B, & DWG 144A7730, SHEET 7, REV -.
CORRODED SUPPORT ZEE, BS 727 - 847, LBL 21, WL 156 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ZEE IAW SRM 51-10-02, SRM 51-40-02, DWG 146A7502, SHEET 27, REV -, & DWG 145A7500, SHEET 85, REV A.
CORRODED WASTE SERVICE DOOR 145AL. PERFORMED A PERMANENT REPAIR ON THE WASTE SERVICE DOOR IAW SRM 52-40-01-2R-8, REPAIR 8.
CRACKED ANGLE, BS 294.5, S13L. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 141A1311, SHEET 1, REV C.
CORRODED SHIELD WEB, BTW BS 492.4 - 500A, RBL 21, WL 156 IN THE FWD CARGO BAY. REPLACED THE SHIELD WEB AND FASTENERS IAW SRM 51-10-02 ITEM 9, AND DWG 143A0080, SHEET 23, REV -.
CRACK TIE CLIP, BS 277, S10R. REPLACED THE TIE CLIP, MEASUREMENT OF DAMAGE: 1.650 INCH. REPLACED THE TIE CLIP, MEASURE OF DAMAGE: 1.650 INCH, & NO FOUND ALLOWABLE DAMAGE, IAW 51-40-02 AND DWG 141A1110, SHEET 18, REV-.
DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG PASSENGER CABIN (1KT). REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING IAW AMM 33-51-15-400-802.
CRACKED FLOOR SUPPORT BETWEEN BS 291.5 TO 294.5, S17R. REPLACED THE FLOOR SUPPORT AND & FASTENERS IAW SRM 51-10-02 ITEM 9, AND 141A8310, SHEET 25, REV- .
CRACKED INTERCOSTAL WEB, BS 294.5 - 303.9, S16L. PERFORMED A REPAIR CAT B ON THE INTERCOSTAL WEB IAW EA 26-153-00182-WIP1, & EA 26-153-00182.
CRACKED INSPAR RIB, HSS 111.10 AND 28 INCHES FROM FRONT SPAR IN THE LT HORIZONTAL STAB. REPAIRED THE RIB LOCATED IAW SRM 55-10-09-2R-4, REPAIR 4.
ELONGATED HOLES ON ACCESS PANEL 561BB, LT WING. REPAIRED ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10.
ELONGATED HOLES ON ACCESS PANEL 661BB, RT WING. REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-9, REPAIR 9.
CRACKED FRAME, BS 259.5, S8 - 9R IN THE FLIGHT DECK. PERFORMED A REPAIR, CAT B ON THE FRAME BS 259.5 BTWN STR 6 - 11R IAW EA 26-153-00146-WIP1. & EA 26-153-00146.
CRACKED INSPAR RIB, HSS 120.30 AND 10 INCHES FROM REAR SPAR IN THE RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR OF THE RIB IAW SRM 55-10-09-2R-4, REPAIR 4, FIGURE 202.
DELAMINATED ACCESS PANEL 644BB AT RT WING. REPAIRED THE ACCESS PANEL 644BB IAW SRM 57-53-70-2R-5, REPAIR 5.
A CRACK INDICATION ON THE STUB FRAME, BTWN BS 294.5 - 296.5, S8R - S9R AT THE FWD GALLEY DOOR AREA. REPLACED THE STUB FRAME IAW SRM 51-40-02, SRM 51-10-02, PARAGRAPH 9, & DWG 141A8370, SHEET 9, & SHEET 11, DWG 141A3310, SHEET 43, REV -, & DWG 141A8380, SHEET 20, REV -.
CRACKED GUSSET, BS 500D, S19R IN THE FWD CARGO BAY. REPLACED THE GUSSET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A7902, SHEET 174, REV -.
CRACKED FLOOR SUPPORT, BS 695, BL0. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.
CRACKED CROSSBEAM, BS 540, BL 0 - LBL 24.75. REMOVED PROTECTIVE TREATMENT & PERFORMED GVI AND DID NOT FIND ADDITIONAL DAMAGE ON AREA IAW AMM 51-21-11-150-801, REPLACED THE CROSSBEAM AND FASTENERS IAW SRM 51-10-02, ITEM 9, AND DWG 143A0060, SHEET 46, REV -.
CRACKED CROSSBEAM, BS 540, BL0 - LBL 24.75. REMOVED PROTECTIVE TREATMENT AND PERFORMED GVI & DID NOT FIND ADDITIONAL DAMAGE IN AREA IAW AMM 51-21-11-150-801, REPLACED THE CROSSBEAM AND FASTENERS IAW SRM 51-10-02 ITEM 9, & DWG 143A0060, SHEET 46, REV -.
CRACKED FLOOR SUPPORT, BS 695, RBL24.75. REPLACED THE FLOOR SUPPPORT IAW SRM 51-40-02, & DWG 273A9110, SHEET 6, REV A.
CRACKED CROSSBEAM, BS 540, BL0 - RBL 24.75. REPLACED THE CROSSBEAM & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 143A0060, SHEET 46, REV -.
CRACKED FLOOR SUPPORT, BS 695, LBL24.75. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.
CRACKED AFT CORNER OF THE SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, PARAGRAPH 4.B, & BAC 5975.
CRACKED FWD CORNER OF THE SCUFF PLATE IN THE FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1. PARAGRAPH 4.B, & BAC 5975.
CRACKED AFT CORNER OF THE SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4.B, AND BAC 5975.
FWD MEGAPHONE HANDLE LOOSE. REPLACED FWD MEGAPHONE IAW AMM 25-64-00. OPS OK.
DOOR R1 SLIDE COVER GIRT BAR HOOK HAS A BROKEN RIVET<[01] COMPLIED WITH EA M-23-125-01839
RIGHT OVERWING EXIT LIGHT INOP<[01] REMOVED AND REPLACED RIGHT OVERWING EXIT LAMP PER AMM 33-51-01
EMERGENCY OVER WING EXIT LIGHT COVER MISSING ON CO PILOT SIDE.<[01] REINSTALLED RH OVER WING EXIT EMERGENCY LIGHT LENS PER AMM 33-51-01
R1 DOOR ASSIST HANDLE LOOSE<[01] TIGHTENED R1 DOOR ASSIST HANDLE IAW AMM 25-21-31.
L1 DOOR UPPER DOOR ASSIST HANDLE LOOSE<[01] TIGHTENED L1 DOOR HANDLE IAW AMM 25-21-31.
FORWARD SERVICE DOOR SLIDE MOUNTED FORWARD GIRT BAR RETAINER CLIP FASTENERS ARE LOOSE.<[01] REMOVED AND REPLACED FASTENERS ON FWD GIRT BAR RETAINER CLIP PER SRM 51-40-02
SLIDE FELL FROM CONTAINER. FRONT CAPTAIN SIDE SLIDE FELL FROM CONTAINER. FRONT CAPTAIN SIDE<[01] REINSTALLED FWD ENTRY SIDE PER MT 725-61-06
FWD GALLEY SERVICE DOOR AFT SLIDE MOUNT ISOLATOR CRACKED<[01] REMOVED AND REPLACED ISOLATOR PER SRM 51-40-02;[02] C/W INSP
RIGHT MLG; UPPER I/B SUPPORT PANEL CRACKED AT FWD ATTACHMENT BRACKET.<[01] REMOVED AND REPLACED BRACKET PER. SRM REF. 51-40-02.
BOTH FWD GALLEY EMERGENCY FLASH LIGHT BATTERIES NEED REPLACEMENT.<[01] REMOVED AND REPLACED BOTH FWD GALLEY EMERGENCY FLASHLIGHT BATTERIES REF AMM 25-64-00. NEW EXPIRATION DATE MAR 2026.
EXT. RH O/W EXIT EMERG LIGHT INOP<[01] REPLACED LAMP FOR RH OVERWING/SLIDE LIGHT AND PERFORMED GOOD TEST PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
EMERGENCY EXIT LOCATORS ON LEFT AND RIGHT OWE HAVE INOP BULBS FWD LOCATOR ON L/H OWE HAS 2 INOP AFT LOCATOR ON R/H OWE HAS 2 INOP<[01] RELAMPED EMERGENCY EXIT LOCATORS ON LEFT AND RIGHT OWE; PERFORMED GOOS TEST PER AMM 33-51-01-960-801; TASK CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
ACB AFT CORNER SCUFF PLATE CRACKED<[01] SCUFF PLATE REMOVED IAW AMM 53-11-02-020-801<BR>SCUFF PLATE REPAIRED IAW BAC5975 - REF STEP 2<BR>CORNER SCUFF PLATE INSTALLED ON BAR CODE TTG8Q00RN1RP;[02] VERIFIED.
REJECT - INTERCOSTAL CRACKED AT FASTENER ATTACHMENT WITH SIDEWALL SUPPORT FCB BS 460 LBL23 WL156. MARKED. PIC ATTACHED.<[01] REMOVED AND INSTALLED NEW BAFFLE P/N 143A7510-9 LOT#1555679-1 PO#963418/1 AT LBL 23 WL 156 BS 440- TO BS 460 IAW SRM 51-40-02 AND DWG 143A7505 REV:-;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.
ACB WEB(146A8322-11) HAS CORROSION AT BS 787 - BS794 RBL 25 WL 160<[01] REMOVED AND REPLACED ACB WEB(146A8322-11) AT BS 787 - BS794 RBL 25 WL 160 IAW SRM 51-40-02 AND DWG 146A8320.
ANGLE(146A8125-52) AT BS787 - BS794 HAS CRACK AT FASTENER HOLE RBL 21 WL 157<[01] REMOVED AND REPLACED ANGLE(146A8125-52) AT BS787 - BS794 RBL 21 WL 157 IAW SRM 51-40-02-0G-0. DWG 146A0081. DWG 146A8123.;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1.;[03] MEASUREMENTS TABLE OK; CARD COMPLETE.
ANGLE(146A8125-53) AT BS767+2 - BS787 HAS CRACK AT FASTENER HOLE RBL 21 WL 157<[01] REMOVED AND REPLACED ANGLE(146A8125-53) AT BS767+2 - BS787 RBL 21 WL 157 IAW SRM 51-40-02 AND DWG 146A0081. DWG 146A8123.;[02] VERIFIED CORRECTIVE ACTION ITEM 1;MEASUREMENTS TABLE OK; CARD COMPLETE.
FCB BAFFLE CRACKED AT FASTENER HOLE BS 500 - BS 500A LBL 25 WL 156<[01] VERIFIED INSTALLATION OF BAFFLE.;[02] REMOVED AND INSTALLED NEW BAFFLE P/N 143A7510-15 LOT#1555332-1 PO#962911/1 AT LBL 25 WL 156 BS 500 TO BS 500A IAW SRM 51-40-02;143A7510 REV:B AND DWG 143A7505 REV:-.
FWD CGO DOOR CUTOUT; CORROSION ON SUBTHRESHOLD BS440+31; RBL28; WL156<[01] VERIFIED STEP 1 COMPLETE.;[02] COMPLETED MEASUREMENT TABLE.;[03] REMOVED CORROSION FROM THRESHOLD WEB AND FOUND OUT OF LIMITS; IAW SRM 53-30-15-1A-1; AND INSTALLED NEW WEB P/N 143A8122-10; LOT # 1538599-1; IAW SRM 51-40-02-0G-0 AND DWG. 143A8330.;[04] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
#1 ENGINE I/B FAN COWL OIL ACCESS DOOR CLOSE OUT FRAME IS CRACKED.<[01] REMOVE AND REPLACE #1 ENGINE I/B FAN COWL OIL ACCESS DOOR CLOSE OUT FRAME PER. SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE
FWD CGO DOOR CUTOUT; SUBTHRESHOLD FASTENER NOT SEATED AND WORKING OUT; BS440+30; RBL28; WL156<[01] SUB THRESHOLD WEB TO BE REPLACED ON FAULT TTG8Q00RNSDT<BR>TASK COMPLETE;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED ACB FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1. PART IS TO BE INSTALLED ON CUSTOMER CARD TTG8Q00RN1RP
DURING REMOVAL R/H VAPOR BARRIER FOUND CRACKED ANGLE P/N 276A9183-2 BS 663 BETWEEN RBL 45- RBL 54<[01] REMOVED AND REPLACED BRACKET P/N 276A9183-2 IAW SRM 51-40-092 AND DWG 111A1001 REV.-;[02] REMOVED AND REPLACED BRACKET P/N 276A9183-2 IAW SRM 51-40-02 AND DWG 111A1001 REV.-;[03] VERIFIED CORRECTIVE ACTION ITEM 2; MEASUREMENTS TABLE OK; CARD COMPLETE.
AFT FLOOR PANEL 242VF AFT R/H CORNER TORN<[01] AFT FLOOR PANEL 242VF WITH AFT R/H CORNER TORN WAS REPAIRED IAW SRM 53-00-50-2R-6.;[02] VERIFIED CORRECTIVE ACTION 1
CORROSION ON FUSELAGE CROWN SKIN COMMON TO FASTENER LOCATIONS FROM STA 1016+2; TO STA 1016+23; BUTT LINE 8 TO 13; LEFT AND RIGHT.<[01] CERTIFIED APPLICABILITY OF SRM 53-00-01-1A-1;[02] ' AS PER EA 24-153-00521; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.';[03] VERIFIED CORRECTIVE ACTION 2
MULTIPLES CRACKS ON PANEL 211A (MARKED)<[01] UPON INVESTIGATION FOUND COCKPIT PANEL 211A IS ACTUALLY 212B. FOUND ONE CRACK ON PANEL 212B; REPAIRED PANEL 212B PER CMM 25-00-66 REPAIR 3-1 PARAGRAPH 4 APPLIED FIBERGLASS AT 10:30 AM;[02] VERIFIED 24HR CURE OF FIBERGLASS REPAIR TO PANEL 212B IAW CMM 25-00-66 REPAIR 3-1 PARAGRAPH 4 AND REPLACED RIVET IN REPAIRED AREA IAW SRM 51-40-02-0G-0;[03] VERIFIED ITEMS 1 AND2
CORROSION ON FWD SHIELD AT ACB BS767 - BS787 RBL21 WL157.<[01] REMOVED AND REPLACED FWD SHIELD AT ACB BS767 - BS787 RBL21 WL157 IAW SRM 51-40-02 AND DWG 146A0081;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE
CORROSION ON FWD SHIELD FWD ATTACH TAB AT ACB BS767 RBL23 WL157.<[01] REMOVED AND REPLACED FWD SHIELD FWD ATTACH TAB AT ACB BS767 RBL23 WL157 IAW SRM 51-40-02 AND DWG 146A0081;[02] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE;
CORROSION ON AFT SHIELD AT FCB BS500 RBL23 WL156.<[01] REMOVED AND REPLACED FCB BAY AFT NEW SHIELD P/N 143A8126-31 LOT#1553496-2 PO#960004/2 AT BS 480+15 TO BS 500A RBL 23; WL 156 IAW SRM 51-40-02 AND DWG 143A0080 REV: -;[02] VERIFIED RII CORRECTIVE ACTION ITEM1.;[03] VERIFIED MEASUREMENTS TABLE; CARD COMPLETE.
CORROSION ON TRACK TIEDOWN AT FCB BS436; BS496; BS500 LBL18 WL156.<[01] REMOVED AND REPLACED TIEDOWN TRACK AT FCB BS 396 TO BS 500D LBL 18 WL 156 IAW BOEING DWG 143A7500 AND SRM 51-40-02;[02] 02 - INSPECTED PER [SRM 53-00-53-1A-2-A00028 (PERMANENT (NON-DENT DAMAGE TYPES))];[03] 02 - INSPECTED PER [SRM 53-00-53-1A-2-A00028 (PERMANENT (NON-DENT DAMAGE TYPES))] VERIFIED STEP 4
CORROSION ON NUTPLATES AT ACB BS727D BL0 WL150.<[01] CUMPLETED STEP 1;[02] TASK CARD COMPLETED;[03] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
CRACKED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS914 RBL11 WL170.<[01] REMOVED AND REPLACED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS914 WL170 IAW BOEING DWG 147A7221; SRM 51-40-05 AND SRM 51-40-02.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE
CRACKED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS918 RBL11 WL170.<[01] REMOVED AND REPLACED SUPPORT ANGLE BEHIND WATER SERVICE PANEL BS918 WL 170 IAW BOEING DWG; SRM 51-40-02 AND 51-40-05.;[02] REMOVED AND REPLACED SUPPORT ANGLE BEHIND WATER SERVICE PANEL BS918 WL 170 IAW BOEING DWG 147A7221; SRM 51-40-02 AND 51-40-05.;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLE
FWD WET AREA - CORROSION ON INTERCOSTAL LBL 11 BS 294.5+5; BS 294.5+8; BS 294.5 +14.5 WL 208 (MARKED)<[01] UPDATED STEP 1.;[02] CORRECTED MEASURMENT;[03] STEPS 4;5 COMPLETE;[04] REMOVED AND REPLACED INTERCOSTAL AT LBL 11; BS 294.5 TO BS 312 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5600.;[05] VERIFIED CORRECTIVE ACTION 4.<BR>JOB COMPLETE.
FWD WET AREA - CORROSION ON MOPSILL RBL 61 FROM BS 312+2.5 TO BS 328+14.5 WL 208 (MARKED)<[01] TASK CARD WAS CORRECTED AND WILL BE ACCOMPLISHED ON TTG8Q00RLLMU.;[02] TASK CARD WAS CORRECTED AND WILL BE ACCOMPLISHED ON TTG8Q00RLL1S;[03] VERIFIED ACTION 1.<BR>JOB COMPLETE.
FWD WET AREA - CORROSION ON MOPSILL BS 294.5+10.5 RBL 56; BS 294.5+15 RBL 57; BS 312+3.5 RBL 57.5; BS 328+7 RBL 57.75; BS 312+10 RBL 58; BS 328+11.75 RBL 57.75; WL 208 (MARKED)<[01] UPDATED STEP 1.;[02] CORRECTED MEASUREMENT;[03] REMOVED AND REPLACED FSD MOPSILL PER SRM 51-40-02-0G-0 AND DWG#141A8310;[04] VERIFIED CORRECTION 3.<BR>JOB COMPLETE.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS809 LBL21 WL157.<[01] REMOVED AND REPLACED SIDEWALL SUPPORT LH FROM BS 727+4 TO BS 847; LBL 21; WL 157; IAW SRM 51-40-02-0G-0 AND DWG 146A7500; ID: 0085; REV: A;[02] VERIFIED ALL STEPS; ALL STEPS AND CARD COMPLETE.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL157.<[01] REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BETWEEN BS 727+4' TO BS 767; RBL 21; WL 157 PER 51-40-02 AND DWG:146A7500.;[02] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE;
MULTIPLES CRACKS ON PANEL 211B (MARKED)<[01] REMOVED AND REPLACED PANEL 211B PER SOPM 20-50-01.;[02] UPDATED MEASUREMENT TABLE.;[03] VERIFIED.
FWD WET AREA - CRACK ON INTERCOSTAL BS 344+9 BL 0 WL 208 (MARKED)<[01] UPDATED STEPS;[02] UPDATED MEASUREMENT TABLE;[03] SUMMARY; THE CRACKED INTERCOSTAL AT BS 344 BL0 WAS REMOVED AND REPLACED IAW SRM 51-10-02-0G-0 STEP 9 A (1) (2).;[04] REJECT: IMPROPERLY INSTALLATION 2E/A FASTENERS ON INTERCOSTAL STA-344 TO 360 BL-0 (MARKED WITH RED TAPE) [TTG8Q00RP6L4];[05] 2 EA IMPROPERLY INSTALLED FASTNERES REPLACED ON FAULT TTG8Q00RP6L4.;[06] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
FWD WET AREA - CRACK ON INTERCOSTAL BS 277+7.5 BL 0 WL 208 (MARKED<[01] UPDATED STEPS;[02] UPDATED STEP;[03] UPDATED MEASUREMENT TABLE;[04] VERIFIED STEPS 1;2;3;4; COMPLETE; STEP 5 IN PARTIAL.;[05] STEP #5 COMPLETE;[06] CUSTOMER CARD COMPLETE AND VERIFIED MEASUREMENT TABLE
AFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW AFT FLOOR PANEL 241AAF IAW SRM 53-00-50-2R-0 AND BOEING DWG 147A5810 ID:0008;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
AFT FLOOR PANEL 242WF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED AFT FLOOR PANEL 242WF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 195.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
FWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
FWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
FWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
FWD FLOOR PANEL 231AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 231AF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.
FWD FLOOR PANEL 231BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FLOOR PANEL 231BF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1
AFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PULLED STRANDS ON AFT FLOOR PANEL 241XF UPPER SKIN HAVE BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.
AFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ZF UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED REPAIR OF FLOOR PANEL 241ZF UPPER SKIN IAW SRM 53-00-50-2R-1.;[03] WORKSCOPE IS COMPLETE.
AFT FLOOR PANEL 241ABFF UPPER SKIN HAS AREAS OF PULLED STRANDS. PANEL SHOULD BE 241ABF<[01] AREAS OF PULLED STRANDS ON FLOOR PANEL 241ABF WERE REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>DOWNLOADED CURE SHEETS AND TAPE.;[02] VERIFIED FLOOR PANEL 241ABF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[03] WORKSCOPE IS COMPLETE
AFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ACF UPPER AND LOWER SKIN DAMAGED AREAS HAVE BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED REPAIR OF FLOOR PANEL 241ACF PER SRM 53-00-50-2R-1.;[03] WORKSCOPE IS COMPLETE.
AFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON AFT FLOOR PANEL 241ADF UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.
AFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242TF UPPER SKIN AREAS OF PULLED STRANDS WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED REPAIR OF FLOOR PANEL 242TF UPPER SKIN IAW SRM 53-00-50-2R-1.;[03] WORKSCOPE IS COMPLETE.
AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1
FWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] REPAIRED AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 221CF IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
FWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 221EF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1.
FWD FLOOR PANEL 222AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222AF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.
FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BAC DWG 141A5810 ID: 245.;[02] INFORMATION ENTERED ON ITEM 1 WAS ENTERED IN ERROR. THIS IS AN INSPECTOR BLOCK.;[03] FWD FLOOR PANEL 222CF UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BAC DWG 141A5810 ID: 245.;[04] VERIFIED FLOOR PANEL 222CF UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BAC DWG 141A5810 ID: 245
FWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222DF WITH UPPER SKIN PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BAC DWG 141A5810 ID:185.;[02] VERIFIED CORRECTIVE ACTION 1.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS460 - BS500C LBL23 WL156.<[01] VERIFIED STEP 15 IN PARTIAL.;[02] VERIFIED STEP 16 COMPLETE.;[03] REJECT - INSTALLATION OF SIDEWALL SUPPORT; FOUND CRACK AT INTERCOSTAL FASTENER ATTACHMENT POINT; BS460; WL156; LBL23 TTG8Q00RT568;[04] 02 - INSPECTED PER [SRM 51-10-02-0G-0-A00248 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)];[05] TASK COMPLETE
CORROSION ON FLOOR BEAM AT AFT WET AREA BS986 RBL43 WL208. MARKED<[01] CORROSION ON BS 986 FLOOR BEAM AT RBL 43; WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-6.;[02] CORRECTED MEASUREMENT;[03] CUSTOMER CARD COMPLETE AND VERIFIED MEASUREMENT TABLE
CORROSION ON TENSION STRAP AT AFT WET AREA BS1016; BS1016+11; RBL3 WL208. MARKED<[01] CORROSION ON TENSION STRAP AT AFT WET AREA BS 1016+11 RBL 3 WL 208 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED AFT WET AREA TENSION STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5730 REV: C;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE
PANEL 194CL OUTER SKIN HAS 2 TIGHTLY GROUPED DISBONDS NEAR CENTER OF PANEL. (MARKED)<[01] PANEL 194CL OUTER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 51-70-05-2R-2.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED PANEL 194CL OUTER SKIN HAS BEEN REPAIRED IAW SRM 51-70-05-2R-2.
DURING HFEC INSPECTION OF LH HORIZONTAL STABILIZER LOWER SKIN (TTG8Q00BDWA5); CRACK FOUND AT STA:193.90; 18' FROM FWD EDGE; MEASURED L: 1.0' MARKED<[01] REPAIRED LH HORIZONTAL STABILIZER LOWER INSPAR SKIN AT STA 193.90 18' FROM FWD EDGE IAW SRM 55-10-01-2R-11;[02] VERIFIED TASK COMPLETED
CORROSION ON FLOOR BEAM AT AFT WET AREA BS986 LBL43 WL208. MARKED<[01] COMPLETED STEP 8; PARTIAL STEP 9.;[02] COMPLETED STEP 9.;[03] VERIFIED STEPS 11;13 COMPLETE.;[04] REMOVED CORROSION FROM AFT WET AREA FLOOR BEAM BS 986 LBL 43 WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ACCOMPLISHED REPAIR OF 986 FLOOR BEAM IAW SRM 53-70-51-2R-6;[05] VERIFIED CORRECTIVE ACTION 4.<BR>JOB COMPLETE.
RIGHT WING FIXED T/E PANEL JUST AFT OF THE PYLON ATTACH ANGLE CRACKED JUST IB OF DEFLECTION RIB. MARKED<[01] REMOVED AND REPLACED RIGHT WING FIXED T/E ATTACH ANGLE JUST AFT OF PYLON AND I/B OF DEFLECTION RIB IAW SRM 51 -40-02-0G-0 PARA. 4.;[02] VERIFIED COMPLETE
CORROSION ON 1016 WEB AT AFT WET AREA BS1016+13 LBL7 WL208. MARKED<[01] REMOVED CORROSION ON 1016 WEB AT AFT WET AREA BS 1016+13 LBL 7; WL 208 AND REWORKED PER EA 24-153-00486.;[02] TASK CARD COMPLETE
FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0.;[02] ADDITION TO ITEM 1: IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 SHEET:8.;[03] VERIFIED CORRECTIVE ACTION ITEMS 1 AND 2.
FLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242CF WITH PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0006;[02] JOB COMPLETE.
FLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241FF WITH PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0013;[02] VERIFIED FLOOR PANEL 241FF WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0013
FLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241EF IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION 1.
FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241DF IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION 1.
WHEEL WELL PRESSURE DECK CRACKED; BS665; LBL35; WL200<[01] PRESSURE DECK AT BS 665 LBL 35 WL 200 REPAIRED ON FAULT TTG8Q00RJ619. FAULT COMPLETE.;[02] VERIFIED RII ITEMS WERE COMPLETED ON FAULT TTG8Q00RJ619.;[03] VERIFIED COMPLETION ON FAULT TTG8Q00RJ619. CARD COMPLETE.
CRACK FOUND DURING HFEC INSPECTION OF HORIZONTAL PRESSURE DECK WEB (TTG8Q00BCA3K) AT LBL 34.5 BS663+1.5. L:0.5IN MARKED<[01] REPAIRED HORIZONTAL PRESSURE DECK AT LBL 34.5 BS663+1.5 PER SRM 53-40-51-2R-2 REPAIR 2. FAULT COMPLETE.;[02] VERIFIED ALL RII STEPS ARE COMPETED.
WHEEL WELL PRESSURE DECK CRACKED; BS666; RBL41; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
WHEEL WELL PRESSURE DECK CRACKED; BS666; RBL42; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
WHEEL WELL PRESSURE DECK CRACKED; BS672; RBL41; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
WHEEL WELL PRESSURE DECK CRACKED; BS665; RBL40; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
#2 ENGINE INLET COWL OUTER LIP SKIN HAS A CRACKED RIVET HEAD AT THE 10:00 POSITION SPLICE SECOND ONE IN FROM THE AFT SIDE OF LIP SKIN.<[01] UPDATED PARTS;[02] REMOVED AND REPLACED #2 ENGINE INLET COWL IAW 71-11-01-000-802-F00 AND 71-11-01-400-802-F00 STEP 5.H.(1)(3-8) (10-13) (20-22).<BR>T/W ATS1760 DUE DATE: 09/2024; ID: PER2249 DUE DATE: 09/2024 AND BONDING METER ID: ATS1257 DUE DATE: 11/2024.;[03] VERIFIED CORRECTIVE ACTION 2;[04] PERFORMED GOOD LEAK CHECK OF THE #2 ENGINE INLET TAI DUCT PER AMM 81-11-01-400-801-F00 STEP 5H(15)-(17). ALL WORK ACCOMPLISHED.;[05] VERIFIED CORRECTIVE ACTION ITEM 4 COMPLETE.<BR>VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.
CRACK FOUND DURING HFEC INSPECTION OF HORIZONTAL PRESSURE DECK WEB (TTG8Q00BCA3K) AT RBL 41 BS663+2. L:0.4IN MARKED<[01] REPAIRED BEADED PRESSURE DECK BETWEEN BS 663.5 TO BS 675; RBL 30 TO RBL 60 WL 202 IAW SRM 53-40-51-2R-2 REPAIR 2. FIGURE 202.;[02] VERIFIED CORRECTIVE ACTION 1.<BR>JOB COMPLETE.
FWD CARGO FLOOR AFT OF DOOR HAS CRACK IN IT. REPLACED FWD CARGO FLOOR PANEL REF AMM 25-52-10.
TAIL-CONE RH SIDE HAS A DENT MEASURING 10 LONG 2 WIDE AND .106 DEEP. DENT HAS AREAS THAT ARE DELAMINATED.<[01] APPLIED SPEED TAPE TO TAIL CONE RH SIDE AND COMPLIED WITH EA - 23-153-03378.
TAIL CONE RH SIDE HAS A DENT 12 FWD OF ELEVATOR INDEX PLATE MEASURING 3 LONG 3 WIDE AND .087 DEEP. DENT IS DELAMINATED. DAMAGE IS WITHIN 4 OF PREVIOUS DENT.<[01] C/W EA: 23-153-03381;[02] EDIT STEP 3 TO INDICATE 'YES'
EMERGENCY LIGHT BATTERY PACKS POS M1675 AND M1674 FAILED CAPACITANCE CHECK<[01] R/R EMERGENCY LIGHT BATTERY PACKS AT POSITIONS M1675 AND M1674 REF AMM 33-51-06.
ALL FOUR DOOR LINER ASSIST HANDLES ARE LOOSE.<[01] RESECURED ALL FOUR DOOR LINER ASSIST HANDLE IAW AMM-25-99-99-SWA-001 PAGE 6 STEP B ITEM (C);[02] VERIFIED ITEM 1.<BR>AUDITED.
DURING DVI INSPECTION FOUND L/H VAPOR BARRIER WEB CRACKED AT STA 663 WL 167 LBL47<[01] EVALUATED DAMAGE; CRACKS ARE REPAIRABLE IAW B737 SRM 57-10-10-2R-2. TAP TEST GOOD; NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 51-70-04-2R-10 PAR 4 STEPS A; B; AND C. <BR><BR>VERIFIED REPAIR MATERIAL IAW B737 SRM 51-70-04-2R-0 TABLE 203: RESIN EY3804AB (A171928); FIBERGLASS CLOTH BMS9-3 (A184337). <BR><BR>REQUIRES OKAY TO BOND.;[02] VERIFIED STEP1 AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM SRM 51-70-04-2R-10 PAR 4 STEPS D THRU G; TAP TEST GOOD; OVEN B0-06 CAL DUE 7/27/23.;[04] VERIFIED STEP 3;[05] OK TO PRIME BOTH FWD AND AFT SIDES OF VAPOR BARRIER;[06] APPLIED PRIMER ON FWD AND AFT SIDES OF VAPOR BARRIER WEB IAW B737 SRM 51-70-04-2R-10 PAR 4.P;[07] VERIFIED STEP 6<BR><BR>OK TO PAINT;[08] APPLIED PAINT ON VAPOR BARRIER WEB IAW B737 SRM 51-70-04-2R-10 PAR 4.P;[09] VERIFIED STEP 8;[10] VERIFIED ALL STEPS ARE COMPLETE;[11] AUDIT C/W
DOT A24-07 RH WING I/B L/E WING TO BODY FAIRING / L/E SUPPORT STRUCTURE ANGLE CRACKED AT FASTENER HOLE. MARKED<[01] REMOVED CRACKED ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05-0G-0 AND BOEING DWG# 116A3110 ID:0005 REV:B. WORK PERFORMED BY NATHAN JAMES #36937;[02] VERIFIED STEP 1;[03] STARTED INSTALLING NEW ANGLE IAW SRM 51-40-02-0G-0 AND BOEING DWG# 116A3110 ID:0005 REV:B. WORK PERFORMED BY NATHAN JAMES #36937;[04] FINISHED INSTALLING NEW BRACKET I.A.W SRM 51-40-02-0G-0 AND BOEING DWG# 116A3110 REV: B;[05] VERIFIED STEPS 3-4.<BR>OK TO CIC.;[06] APPLIED CIC TO NEW ANGLE BRACKET AT 2:12 PM ON 11 JULY 2023 I.A.W BOEING AMM 51-21-91-620-802;[07] VERIFIED ITEM 6<BR>AUDIT C/W
DOT A160-46; FLOOR PANEL 241BF HAS DELAMINATION<[01] WORK ACCOMPLISHED ON NON-ROUTINE TTG8Q00M1DKD
DOT A160-44; FLOOR PANEL 231ZF HAS DELAMINATION OF TOP PLYS<[01] WORK ACCOMPLISHED ON NON-ROUTINE TTG8Q00M1D0E
L/H VAPOR BARRIER UPPER ANGLE IS CRACKED AT STA663 WL 167 AT LBL 10 I/B<[01] ACCOMPLISHED HFEC SURFACE AND OPEN HOLE IAW B737 NDT P6 51-00-00 P16 AND P23 TOOL 44291 DUE 03NOV23 NO CRACKS NOTED;[02] AUDIT C/W
R/H VAPOR BARRIER WEB AT STA 663 HAVE CRACK AT RBL 45 AND RBL 37<[01] EVALUATED DAMAGE; CRACK IS REPAIRABLE IAW B737 SRM 57-10-10-2R-2 REPAIR 2. NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 51-70-04-2R-10 PAR 4 STEPS A; B; AND C. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 51-70-04-2R-0 TABLE 203; RESIN EY3804 (A171928); FIBERGLASS CLOTH BMS9-3 (A184337). <BR><BR>REQUIRES OKAY TO BOND.;[02] VERIFIED STEP 1 ;OKAY TO BOND.;[03] BONDED REPAIR PLIES IAW B737 SRM 51-70-04-2R-10 PAR 4 STEPS D THRU G. TAP TEST GOOD. OVEN B0-06 CAL DUE 7/27/2023.;[04] VERIFIED STEP 3 COMPLETE.;[05] COMPLETED RII OF STEP 3.;[06] VERIFIED ALL STEPS ARE COMPLETE;[07] AUDIT C/W
R/H VAPOR BARRIER UPPER ANGLE HAS CRACK AT STA663 WL 167 AT RBL 45<[01] RECEIVED REPAIR ANGLES FROM BACK SHOP 2024-0 .071 W/O 44942-1000-0004 AND 2024-0 .063 W/O 44942-1000-0001;[02] VERIFIED ITEM 1;[03] ACCOMPLISHED HFEC SURFACE AND OPEN HOLE IAW B737 NDT P6 51-00-00 P16 AND P23 TOOL 44291 DUE 03NOV23 NO CRACKS NOTED;[04] OK TO TREAT AND PRIME;[05] APPLIED ALODINE AND PRIMER TO REPAIR PARTS IAW SRM 51-20-01-0G-0 AMM 51-21-72-370-804;[06] STEP 5 C/W;[07] OK TO INSTALL REPAIR PARTS;[08] OK TO INSTALL REPAIR PARTS IN RII ROLE;[09] VERIFIED ITEM 1 IN RII ROLE;[10] OUT OF SEQUENCE: ACCOMPLISHED DETAILED INSPECTION OF THE REPAIR AREA AND UNDERLYING STRUCTURE NO OTHER DAMAGES FOUND IAW SRM 57-10-10-2R-5 ITEM 4;[11] INSTALLED ALL REPAIR PARTS AT STA 663 R/H IAW SRM 57-10-10-2R-5;[12] WROTE IN ERROR STEP 1<BR>SHOULD BE <BR>RECEIVED -1 AND -2 REPAIR ANGLES FROM BACK SHOP<BR>REPAIR ANGLES BEEN FABRICATED ON W/O 44942-1000-0004 AND W/O 44942-1000-0001;[13] VERIFIED ITEM 10.;[14] VERIFIED ITEMS 11;12;[15] C/W
R1 DOOR SLIDE UNSEATED FROM HOLDER<[01] INSPECTED R1 DOOR SLIDE; RE-SECURED GIRT BAR INTO RETAINING CLIPS NO DEFECTS NOTED PER AMM 25-66-01.
PANEL 193B HAS SEVERAL ELONGATED HOLES.<[01] REMOVED AND REPLACED WITH NEW PANEL PER AMM 53-51-01.;[02] INSPECTION VERIFIED CORRECTIVE ACTION STEP 1.
FWD ENTRY SLIDE MORE THAN ONE NEEDLE WIDTH INTO THE RED / [01] R&R FWD ENTRY SLIDE PER AMM 25-66-01
FORWARD ENTRY DOOR SLIDE PRESSURE IN THE RED / [01] INSPECTED SLIDE PRESSURE IAW AMM 25-66-01; FOUND WITHIN LIMITS AT THIS TIME
L2 DOOR SLIDE GIRT BAR NEEDS TO BE REPOSITIONED 2022-129940 / [01] INSTALLED CORRECTLY L2 DOOR SLIDE GIRT BAR IAW B737-700 AMM 25-66-01-000-804;[02] CORRECTED ACTION<BR>INSTALLED CORRECTLY L2 DOOR SLIDE GIRT BAR IAW B737-700 AMM 25-66-01-400-803;[03] INSTALLED CORRECTLY L2 DOOR SLIDE GIRT BAR IAW B737-700 AMM 25-66-01-400-803
CRACK ANGLE - CLIP LOCATED BS 400; STRINGER 26L FWD CARGO COMPARTMENT 2022-129821 / [01] REPLACED ANGLE - CLIP AND FASTENERS LOCATED BS 400; STRINGER 26L FWD CARGO COMPARTMENT IAW SRM B737-700 51-40-02 AND DRAWING 143A7505 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE - CLIP AND FASTENERS LOCATED BS 400; STRINGER 26L FWD CARGO COMPARTMENT IAW SRM B737-700 51-40-02 AND DRAWING 143A7505 REV:- SEE INDIVIDUAL SIGN OFF BELOW RII
CRACK GUSSET LOCATED BS 500D; STRINGER 19R FWD CARGO COMPARTMENT 2022-129813 / [01] REPLACED GUSSET LOCATED BS 500D STRINGER 19R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-0-02 ITEM 9 AND DRAWING 143A7902 REV -; SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED GUSSET LOCATED BS 500D STRINGER 19R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-0-02 ITEM 9 AND DRAWING 143A7902 REV -; SEE INDIVIDUAL SIGNOFF BELOW.<BR>RII ACCOMPLISHED
CRACK ANGLE - SUPPORT LOCATED BS 947.5 AND LBL 8.10 AT AFT CARGO COMPARTMENT 2022-129812 / [01] REPLACED ANGLE-SUPPORT AND FASTENERS; AT BS947.5 AND LBL 8.10 ON AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG 149A8103 REV. ?A? SEE SIGN OFFS BELOW.;[02] REPLACED ANGLE-SUPPORT AND FASTENERS; AT BS947.5 AND LBL 8.10 ON AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG 149A8103 REV. ?A? SEE SIGN OFFS BELOW. RII
CRACK ANGLE SUPPORT LOCATED BS867 AND LBL 12-50 AT AFT CARGO COMPARTMENT 2022-129797 / [01] REPLACED SUPPORT LOCATED BS 867 AND LBL 12.50 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 149A8102 REV:-;SEE INDIVIDUAL SIGNOFF BELOW.;[02] CORRECTED STEP 1.<BR>REPLACED ANGLE SUPPORT LOCATED BS 867 AND LBL 12.50 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 149A8102 REV:-;SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPLACED ANGLE SUPPORT LOCATED BS 867 AND LBL 12.50 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 149A8102 REV:-;SEE INDIVIDUAL SIGNOFF BELOW.
CRACK GUSSET LOCATED BS 500D; STRINGER 19L FWD CARGO COMPARTMENT 2022-129817 / [01] REPLACED GUSSET LOCATED BS 500D STRINGER 19L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7902 REV. -; SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED GUSSET LOCATED BS 500D STRINGER 19L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7902 REV. -; SEE INDIVIDUAL SIGNOFF BELOW.RII ACCOMPLISHED
CRACK ON RIB #8 ON PANEL 321A DORSAL FIN 2022-129776 / [01] REPLACED RIB #8 AND FASTENERS LOCATED ON PANEL 321A DORSAL FIN IAW B737-700 SRM 51-40-02 AND DWG 174A1008 SHEET 2 REV. C. PART NUMBER USED: 174A1108-2 P.O:2022-128747.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW
CRACK ACCESS PANEL 561BB TRAILING EDGE ARAUND HOLES LT WING 2022-129777 / [01] TOOL USED: CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 29-SEP-22.;[02] TOOL USED SCALE P/N: CL5000 S/N: AE-409558 DUE DATE: 19-MAY-22.;[03] TOOL USED HOTBONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 16-JAN-23.;[04] TOOL USED P/N FLUKE -87 S/N 193700733 DUE DATE 22SEP 22;[05] TOOL USED MULTIMETER P/N FLUKE -87 S/N 193700733 DUE DATE 22SEP 22;[06] REPAIRED ACCESS PANEL 561BB; LT WING IAW B737-700 SRM 51-70-05-2R-9 REPAIR 9. SEE INDIVIDUAL SIGN OFFS BELOW.;[07] REPAIRED ACCESS PANEL 561BB; LT WING IAW B737-700 SRM 51-70-05-2R-9 REPAIR 9. SEE INDIVIDUAL SIGN OFFS BELOW.
CRACK ACCESS PANEL 194DL WING TO BODY FAIRING AT FUSELAGE EXTERIOR 2022-129778 / [01] TOOL USED CALIPER P/N: 500-464 S/N: 15331926 DUE DATE: 28-SEP-22.;[02] TOOL USED: HOT BONDER P/N:HCS9200B S/N:15102320 DUE DATE: 16-JAN-23;[03] TOOL USED: SCALE P/N:1863T62 S/N:AE-40571 DUE DATE: 19-MAY-22;[04] REPAIRED ACCESS PANEL 194DL WING TO BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. SEE INDIVIDUAL SIGN OFFS BELOW.;[05] REPAIRED ACCESS PANEL 194DL WING TO BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT 2022-129765 / [01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 2000053402; CAL DUE DATE: 23-APR-22<BR>TOOL USED PN ULTRASONIC EQUIPMENT PN: 45MG; SN: 130063701; DUE DATE: 11-MAY-22;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[03] REPAIRED STRINGER 26L LOCATED BTW BS 500D AND BS 540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1 FIGURE 206. SEE INDIVUDUAL SIGNOFF BELOW.;[04] REPAIRED STRINGER 26L LOCATED BTW BS 500D AND BS 540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1 FIGURE 206. RII ;SEE INDIVUDUAL SIGNOFF BELOW.
CRACK FLOOR STRUCTURE SUPPORT BRACKET LOCATED STA. 540 AND LBL 0.07 TO LBL 24.82 AT PASSENGER CABIN 2022-129736 / [01] REPLACED FLOOR STRUCTURE SUPPORT BRACKET LOCATED STA. 540 AND LBL 0.07 TO LBL 24.82 AT PASSENGER CABIN I.A.W.B737-700 SRM 51-40-02 AND SRM 51-10-02;SEE INDIVIDUAL SING OFF BELOW.;[02] REPLACED FLOOR STRUCTURE SUPPORT BRACKET LOCATED STA. 540 AND LBL 0.07 TO LBL 24.82 AT PASSENGER CABIN I.A.W.B737-700 SRM 51-40-02 AND SRM 51-10-02;SEE INDIVIDUAL SING OFF BELOW. AS RII
ELONGATED HOLE ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR 2022-129653 / [01] TOOL USED SCALE P/N: CL5000 S/N: AE-409558 DUE DATE: 19-MAY-22.;[02] TOOL USED HOTBONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 16-JAN-23.;[03] TOOL USED FLUKE -87 S/N 193700733 DUE DATE 22 SEP 22;[04] TOOL USED MULTIMETER P/N FLUKE -87 S/N 193700733 DUE DATE 22 SEP 22;[05] TOOL USED CALIPER PN:500-464 ; SN:15331926 DUE DATE 28/SEP/22;[06] REPAIRED ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-05-2R-9 REPAIR 9. SEE INDIVIDUAL SIGN OFFS BELOW.;[07] REPAIRED ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-05-2R-9 REPAIR 9. SEE INDIVIDUAL SIGN OFFS BELOW.
ELONGATED HOLE FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT 2022-129549 / [01] FABRICATED PANEL 120CF AT AFT CARGO COMPARTMENT I.A.W AMM 25-52-201-801 AND DRAWING# 453A1610 REV:D ; MATERIAL USED P/N:A90RG1W 0.09' P.O#2021233166;[02] FABRICATED PANEL 120CF AT AFT CARGO COMPARTMENT I.A.W AMM 25-52-201-801 AND DRAWING# 453A1610 REV:D ; MATERIAL USED P/N:A90RG1W 0.09' P.O#2021233166
CRACK BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT 2022-129552 / [01] REPLACED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 DWG #453A2510 REV.- MATERIAL CONOLITE 0.060? P/N A60SG4W P.O. 2021 214612;[02] CORRECTED STEP 1 <BR>FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 DWG #453A2510 REV.- MATERIAL CONOLITE 0.060? P/N A60SG4W P.O. 2021 214612;[03] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 DWG #453A2510 REV.- MATERIAL CONOLITE 0.060? P/N A60SG4W P.O. 2021 214612<BR>TASK COMPLETED
CORROSION PLATE LOCATED 794.5 AND RBL25.2 AT WL158.1 AT AFT CARGO COMPARTMENT 2022-129593 / [01] REPLACED PLATE LOC BS 794.5 AND RBL 25.2 AT WL158.1 AT AFT CARGO COMP I.A.W SRM B737-700 51-40-02 AND SRM B737-700 51-10-02 ITEM 9;[02] REPLACED PLATE LOC BS 794.5 AND RBL 25.2 AT WL158.1 AT AFT CARGO COMP I.A.W SRM B737-700 51-40-02 AND SRM B737-700 51-10-02 ITEM 9
CORROSION TIE DOWN LOCATED BS 794.5 AND BS847 AT RBL25.2 AND WL163.56 AT AFT CARGO COMPARTMENT (2 EA) 2022-129594 / [01] REPLACED TIE DOWN 2 E/A LOC BS794.5 AND 847 AT RBL 25.2 WL163.56 AT AFT CARGO COMP I.A.W SRM 51-40-02 B737-700. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700;[02] REPLACED TIE DOWN 2 E/A LOC BS794.5 AND 847 AT RBL 25.2 WL163.56 AT AFT CARGO COMP I.A.W SRM 51-40-02 B737-700. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700
CRACK LOWER SURFACE SLAT 8 ON SLAT STATION 451.97 RT WING 2022-129548 / [01] TOOL USED : EDDY CURRENT TOOL; P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 02 JUN 22.;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 500D; SN:N500X1693P030457; DUE DATE: 02-JUN-22;[03] REPAIRED LOWER SURFACE SLAT 8 ON SLAT STATION 451.97 RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; SEE INDIVIDUAL SIGNOFF BELOW.;[04] 3. JOSUE MARTINEZ (TECHNICIAN); 22-MAR-2022 02:53 UTC <BR>REPAIRED LOWER SURFACE SLAT 8 ON SLAT STATION 451.97 RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; RII .SEE INDIVIDUAL SIGNOFF BELOW
F/A REPORTS EMERGENCY SLIDE AT L1 DOOR HAS COTTER PIN LOOSE / PERFORMED MT 725-61-06 REINSTALLED COTTER PIN
AFT UPPER CABIN ; CABLE ATTACH CLIP ; AT STA 867 BETWEEN STRINGER 2R AND 3R CRACKED / REMOVED AND REPLACED CLIP AT STA 867 BETWEEN STR 2R AND 3R PER SRM 51-40-02.
L/H WING TRAILING EDGE PANEL 551GB BULB SEAL RETAINING BRACKET CHAFFED AND WORN. / REMOVED AND REPLACED L/H WING T/E PANEL 551GB BULB SEAL RETAINING BRACKET REF SOPM 20-50-01.
RT. HORIZ. STAB SKIN SS176 AND 2.5 INCHES FWD OF REAR SPAR HAS 1 HOLE THAT SHOWS CRACK INDICATION PER HFEC MANUAL PART 6 CH51-00-00 PROC. 16. (MARKED) / FACT AS A RESULT OF POST REPAIR INSPECTION
RT. HORIZ. STAB SKIN SPLICE (INTERNAL) SS181 HAS 5 HOLES THAT SHOWS CRACK INDICATION PER HFEC MANUAL PART 6 CH51-00-00 PROC. 16. (MARKED) / FABRICATED AND INSTALLED NEW STAB SKIN SPLICE (INTERNAL) PER EA 1-755-4672.
RT. HORIZ. STAB RIB SS184.7 HAS 3 HOLES THAT SHOWS CRACK INDICATION PER HFEC MANUAL PART 6 CH51-00-00 PROC. 16. (MARKED) / REPAIRED IAW EA 1-755-4677
R/H ELEVATOR UPPER SURFACE HAS MULTIPLE LARGE AREAS OF CRACKED AND BUBBLED PAINT / REMOVED AND REPLACED R/H ELEVATOR ASSY. IAW AMM 27-31-11. SEE WIPS AND SUBTASKS FOR INDIVIDUAL SIGN OFFS. TAG NO: 683848 PN ON: 183A0107-2 SN ON: 001127 PN OFF: SN OFF: 000953
AFT ENTRY DOOR SKIN DAMAGED AROUND UPPER PLUG FOR GUIDE ARM BOLT. / REMOVED AND REPLACED AFT ENTRY DOOR AND ADJUSTED PER AMM 52-13-00. (SEE SUB TASK FOR WORK ACCOMPLISHED) TAG NO: SAM-11 PN ON: 147A6116-30 SN ON: CYC0052 PN OFF: SN OFF: 001976
R/H HORIZONTAL STABILIZER LOWER SKIN IS WAVY AT FIRST BAY O/B OF SKIN MOD DOUBLERS / FACT AS A RESULT OF POST REPAIR INSPECTION
R/H TRANSITION ANGLE FROM STA. 747-767 HAS HEAVY CORROSION THOUGHT OUT THE ANGLE THAT HAS BEEN PREVIOUSLY REWORK AND IS OUT OF LIMITS. / E104704-BLANKS; KENNETH - 03/19/2020 22:56 COMPLETE: REMOVED AND REPLACED RH TRANSITION FROM STA. 727-767 PER SRM 51-40-02.
L/H TRANSITION ANGLE FROM STA. 747-867 HAS HEAVY CORROSION THOUGHT OUT THE ANGLE THAT HAS BEEN PREVIOUSLY REWORK AND IS OUT OF LIMITS. / INSTALLED NEW TRANSITION ANGLE FROM STOCK PER SRM 51-40-02.
FLIGHT DECK FLOOR DENT STA 260 LBL 10 / REPAIRED IAW EA 1-A53-33179
PASSENGER CABIN FLOORBOARD 242AF DENTED AND MULTIPLE FIBER STRANDS PULLED UP ON UPPER SURFACE / REPLACED PASSENGER CABIN FLOORBOARD 242AF PER AMM 53-21-00.
FWD SERVICE DOOR THRESHOLD INNER CENTER TRIM PLATE BENT AND DEFORMED / REMOVED AND REPLACED FWD SERVICE DOOR THRESHOLD INNER CENTER TRIM PLATE PER AMM 53-11-01.
R/H STAB HAS A CRACKED #3 STIFFENER AT THE #4 RIB LOWER END; STAB STA.120.3.(VERIFIED BY HFEC PART6; 51-00-00 PROC.23) / REPAIRED RIB PER SRM 55-10-09-2R-4. SEE SUB TASKS AND WIPS FOR DETAILS OF WORK ACCOMPLISHED.
PASSENGER CABIN FLOORBOARD 241BF HAS MULTIPLE FIBER STRANDS PULLED UP ON UPPER SURFACE / REMOVED AND REPLACED PASSENGER CABIN FLOORBOARD 241BF PER AMM 53-21-00.
R/H STAB HAS TOOLING DAMAGE AT #1 STIFFENER AT THE #7 RIB LOWER END; STAB STA.147.90.(MARKED) / REPAIRED RH STAB #7 RIB AT #1 STIFFENER PER SRM 55-10-09-2R-4.
L/H AFT CARGO TRANS ANGLE HAS MULTIPLE DAMAGED NUT PLATES. / L/H AFT TRANSITION ANGLE HAD HEAVY CORROSION AND WAS REPLACED WITH NEW FROM STOCK TRANSITION ANGLE ALONG WITH BAD NUTPLATES ON NON ROUTINE #G720829
SEAT TRACK #4 FROM STA 727B TO 887 NEEDS TO BE REPLACED DUE TO DAMAGE OUT OF LIMITS. / REMOVED AND REPLACED SEAT TRACK FROM STATION 727B-887 RBL45 PER SRM 51-10-02 AND SRM 51-40-02
FLIGHT COMPARTMENT FLOOR DENTED UNDER FIRST OBSERVERS SEAT. / DUPLICATE WRITE UP ; REFER TO NRC # G721906 FOR CORRECT NRC.
AFT CARGO DOOR REQUIRES REPLACEMENT DUE TO DAMAGE OUT OF LIMITS. / REMOVED AND REPLACED AFT CARGO DOOR PER AMM 52-31-00. TAG NO: 652420 PN ON: 146A6110-29 SN ON: 001885 PN OFF: SN OFF: 001973
AFT CARGO DOOR CUT-OUT; FWD SIDE STA. 787 RBL23; CLOSEOUT PANEL 142KW; BENT AND DAMAGED. / REMOVED AND REPLACED PANEL PER SRM 51-40-02
#1 SEAT TRACK LOWER LANDING FINISH WORN STA 500C THRU STA 500D. / SEAT TRACK WILL BE REPAIR FROM STA 500C TO STA 520 ON N/R#G720806 DUE TO UPPER CROWN OUT OF LIMITS AT STA520).
#1 SEAT TRACK LOWER LANDING FINISH WORN STA 500D THRU STA 520. / SEAT TRACK WILL BE REPAIR FROM STA 500C +10 TO STA 520 ON N/R#G720806 DUE TO UPPER CROWN OUT OF LIMITS AT STA520).
#1 SEAT TRACK UPPER CROWN GOUGED AND DAMAGED AT STA 520. / ACCOMPLISHED SPLICE REPAIR TO #1 SEAT TRACK FROM STA 500C+10 TO STA 520 IAW SRM 53-00-52-2R-4 REPAIR 4 AND EA 1-A53-11779.
R/H WING WIGGLE PLATE IS SHEARED AWAY. LOCATED INBD, AND ABOVE #2 PYLONG REMOVABLE FAIRING. / REMOVED AND REPLACED WIGGLE LATE PER SRM. 51-10-02 AND SRM 51-40-02.
EXTERNAL POWER DOOR CUTOUT DAMAGED IN THE AFT LOWER CORNER. / REPAIRED ON N/R G720414
EXTERNAL POWER DOOR CUTOUT DAMAGED ON THE AFT SIDE IN THE MIDDLE. / FABRICATED DOUBLER AND FILLER; INSTALLED PARTS REF SRM 53-10-15-2R-4
MOD TYPE: 6 NBR: 28564 REV: POS: DURING SI # 12043-53, FOUND SKIN CRACK INDICATION, BS 540, BELOW STRINGER 22R, / SECOND FASTENER FROM THETOP IN THE AFT ROW. / REPAIRED PER EA.
CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M1674. R&R BATTERY PACK PER AMM AND DWG.
CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M1673. R&R BATTERY PACK PER AMM AND DWG.
CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M1672. R&R BATTERY PACK PER AMM AND DWG.
CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M1669. R&R BATTERY PACK PER AMM AND DWG.
CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M1670. R&R BATTERY PACK PER AMM AND DWG.
R/H EGRESS I LUMINESCENT STRIP IN FRONT OF SEAT 1 CRACKED. R&R STRIP IAW AMM.
R1 DOOR ESCAPE SLIDE FABRIC CAUGHT IN GIRT BAR. R&R GIRT BAR PER AMM.
WING TO BODY PANEL 193B HAS SEVERAL HOLES THAT ARE OVER SIZED/ WORN/ ELONGATED. / REMOVED AND REPLACED 193B PER AMM 53-51-21.
R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.
R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER AMM.
LEFT HORIZONTAL STAB RIB FRONT END THIRD STIFFENER CRACKED AT HSS 92.70. REPAIRED THE STRIFFENER IAW SRM.
LEFT HORIZONTAL STABILIZER, HSS 120.30 RIB WAS FOUND CRACKED AT THE SECOND STIFFENER FROM FRONT. R & R THE RIB IAW SRM.
LEFT HORIZONTAL STAB RIB FRONT END THIRD STIFFENER CRACKED AT HSS 120.30. REPAIRED THE STIFFENER IAW SRM.
LEFT HORIZONTAL STAB RIB FRONT END FOURTH STIFFENER CRACKED AT HSS 120.30. REPAIRED STIFFENER IAW SRM.
CRACK FOUND AT FWD SERVICE DOOR AT #4 BEAM PARALLEL TO I/B RADIUS / REPLACEMEAT OF FWD SERVICE DOOR #4 BEAM ACCOMPLISHED ON WORK ORDER # 0520055-B6R.
FLOOR SUPPORT CRACKED BETWEEN BS 380 TO 400, BL 0. R & R THE FLOOR SUPPORT IAW SRM AND DWG.
FLOOR SUPPORT CRACKED BETWEEN BS 500D TO 520, BL 0. R & R THE FLOOR SUPPORT IAW SRM AND DWG.
CORROSION ON AFT CARGO BAY BS 767+6 FLOOR SPLICE RBL 10 TO LBL10 / CORROSION ON AFT CARGO BAY B.S 767+6 FLOOR SPLICE WAS FOUND OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS RECIEVED NEW PART ON PO# 670176
CORROSION ON AFT CARGO BAY BS 727D FLOOR SPLICE RBL 10 TO LBL10 / CORROSION ON THE 727D CARGO BAY FLOOR SPLICE WAS FOUND OUT OF LIMITS DUE TO NO ALLOWABLE SRM LIMITS RECIEVED NEW FLOOR SLPICE ON PO#682471
CREASE BEAM WEB CORRODED BETWEEN BS 827 TO 847, STRINGER 17R. R & R THE CREASE BEAM WEB IAW SRM AND DWG.
LOWER BULKHEAD CLIP IS CRACKED AT BS 947 LBL 20 / REMOVED AND REPLACED LOWER BULKHEAD CLIP BS 947 LBL20 IAW SRM 51-40-02 AND A1PC 53-42-51-03.
L1 DOOR MOP SILL CRACKED ON VERTICAL FLANGE AT BS 303.9, LBL 58. R&R MOPSILL IAW SRM AND DWG.
CORROSION ON AFT CARGO BAY BS 887 FLOOR SPLICE RBL 10 TO LBL10 / REMOVED AND REPLACED AFT CARGO BAY BS 887 FLOOR SPLICE ROB10 TO LBL10 IAW SRM 51-40-02 AND A1PC 53-42-11-30
FUSELAGE CREASE BEAM CORRODED AT BS 887 TO 907, STRINGER 17L. R & R THE CREASE BEAM SECTION IAW SRM.
CREASE BEAM WEB CORRODED BETWEEN BS 639 TO 663, RBL 66. R & R THE CREASE BEAM WEB IAW AMM AND DWG.
FORWARD CARGO BAY AFT BULKHEAD GUSSET CRACKED AT BS 500D, STRINGER 19L. R & R THE GUSSET IAW SRM & DWG.
FORWARD CARGO BAY AFT BULKHEAD GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM & DWG.
REINFORCEMENT STRAP CORRODED AT BS 1028, RBL 18. R & R THE STRAP IAW SRM AND DWG.
FWD CARGO BAY CENTER SCUFF PLATE IS DENTED AND CRACKED IN MULTIPLE AREAS / REMOVED AND REPLACED FWD CARGO BAY; DENTED AND CRACKED CENTER SCUFF PLATE PER AMM 53-11-02-020-801; AMM 53-11-02-408-801.
CRACKED FLOOR SUPPORT BS 312-328 LBL 47 WL 208. / REMOVED AND INSTALLED NEW FLOOR SUPPORT AT BS 312-328 LBL47 WL208 IAW SRM 51-40-02-OG-0 PAGE 6; SRM 51-40-05-OG-0 AND DWG 141A5400 ID: 0026 REV:-
CRACKED FLOOR SUPPORT BS 344-360 LBL 1-WL 208. / REMOVED AND REPLACED FLOOR SUPPORT AT B.S. 344-360; LBL 1 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 141A5400.
AFT PASSENGER FLOOR PANEL 242UF FWD I/B CORNER IS BROKEN / REPAIRED FWD I/B CORNER PUNCTURE AND DELAMINATION DAMAGE ON AFT PASSENGER FLOOR PANEL 242UF SRM 53-00-50-2R-2 AND SRM 53-00-50-2R-9 (570660)
FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294, BL 0. R & R THE FLOOR SUPPORT IAW SRM AND DWG.
REINFORCEMENT STRAP CORRODED BETWEEN BS 1024 TO 1029, LBL 3. R & R THE STRAP IAW SRM AND DWG.
R2 DOOR MOP SILL CORRODED BETWEEN BS 947 TO 986, RBL 60. R & R THE MOP SILL IAW SRM & DWG.
AFT LEFT SHEAR WEB CORRODED BETWEEN BS 1026 TO 1028, LBL 17 TO LBL 28. R & R THE SHEAR WEB IAW SRM & DWG.
FLOOR SUPPORT CRACKED BETWEEN BS 328 TO BS 344, LBL 47. R&R SUPPORT IAW SRM AND DWG.
MOP SILL CHORD CLIP ANGLE CRACKED AT BS 294.5, RBL 53. R&R ANGLE IAW SRM AND DWG.
MAIN PRESSURE BULKHEAD WEB CRACKED AT BS 663, BETWEEN LBL 25 TO LBL 48. REPAIRED THE BULKHEAD WEB IAW SRM.
LEFT WING LEADING EDGE STRINGER FOUND CRACKED. R & R THE STRINGER IAW SRM.
CABIN FLOORBOARD BREAK PANEL LEFT OF CENTER AT STA. 540 CRACKED. / REMOVED AND REPLACED PANEL REF SRM 51-40-02.
CABIN FLOORBOARD BREAK PANEL RIGHT OF CENTER AT STA. 540 CRACKED. / REMOVED AND REPLACED PANEL REF SRM 51-40-02.
R1 DOOR LOWER EXIT SIGN FELL OFF. R & R THE SIGN IAW MM.
FWD ENTRY EXIT LIGHT LENS MISSING. R & R THE LIGHT ASSY IAW MM.
RIGHT EMERGENCY LIGHT FAILED CAPACITY TEST. R & R THE BATTERY PACK IAW DWG.
R1 DOOR EMERGENCY SLIDE LENS LOOSE. R & R THE LENS IAW MT & AMM.
R1 DOOR EMER EXIT LIGHT WIRE BROKEN. R & R LIGHT ASSEMBLY IAW AMM.
FORWARD LT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.
LEFT OVERWING EXIT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.
LEFT BATTERY PACK FAILED CAPACITY CHECK AT ROW 17. R & R BATTERY PACK IAW MM.
EXTERIOR EMERGENCY LIGHT AFT OF L2 DOOR INOPERATIVE. REPLACED THE LAMP IAW MM.
RIGHT OVERWING FWD EMER EXIT LIGHT LENS CRACKED. REPAIRED LENS IAW EA.
VERTICAL PRESS DECK CRACKED AT BS 663.75, BETWEEN RBL 35 - 43. REPAIRED DECK IAW EA.
SIDEWALL EXIT LIGHT COVER LENS LOOSE AT ROW 11. REPAIRED LENS IAW MM.
AFT RT EMER BATTERY FAILED FUNCTIONAL CHECK. R & R BATTERY IAW AMM.
CENTER RT EMER BATTERY FAILED FUNCTIONAL CHECK. R & R BATTERY IAW AMM.
AFT LT EMER BATTERY FAILED FUNCTIONAL CHECK. R & R BATTERY IAW AMM.
AFT LT BATTERY CHARGER AFT NUTPLATE BROKEN. R & R CHARGER ASSEMBLY IAW AMM.
FORWARD RT EMER BATTERY FAILED FUNCTIONAL CHECK. R & R BATTERY IAW AMM.
OUTBOARD SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.
INBOARD SEAT TRACK FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.
OUTBOARD SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.
INBOARD SEAT TRACK FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.
INTERCOSTAL CRACKED BETWEEN BS 294 TO BS 312, RBL 15. R & R INTERCOSTAL IAW SRM.
LEFT WING REAR SPAR WAFFLE PLATE CRACKED INBD OF NR 3 FLAP FAIRING. R & R WAFFLE PLATE IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 334 TO BS 360, RBL 11. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 33. R & R INTERCOSTAL IAW SRM.
AFT BAGGAGE BIN L ANGLE CRACKED AT BS 867, LBL 12. R & R ANGLE IAW SRM.
OUTBOARD SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.
INBOARD SEAT TRACK FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.
OUTBOARD SEAT TRACK FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW EA.
FORWARD GALLEY Z ANGLE CORRODED BETWEEN BS 294 TO BS 360. R & R ANGLE IAW SRM.
FORWARD CABIN INTERCOSTAL CRACKED AT BS 315, RBL 30. R & R INTERCOSTAL IAW SRM.
FORWARD CABIN INTERCOSTAL CRACKED AT BS 350, CBL 0. R & R INTERCOSTAL IAW SRM.
WEB STIFFENER STEP CORRODED AT BS 1028, RBL 3. R & R STRAP IAW SRM.
WEB STIFFENER STRAP CORRODED AT BS 1028, LBL 3. R & R STRAP IAW SRM.
AFT CARGO COMPARTMENT UNDERSIDE STRAP CORRODED JUST AFT OF THRESHOLD PLATE. R & R STRAP IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R & R INTERCOSTAL IAW SRM.
SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW SRM.
RIGHT HORIZONTAL STABILIZER SKIN 5 INCHES CRACKED ON INBD SIDE OF FRAME AT STATION 184.7, 26 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.
RIGHT HORIZONTAL STABILIZER SKIN CRACKED 5 INCHES ON FWD SIDE OF REAR SPAR AT STAB STATION 123. REPAIRED SKIN IAW SRM.
RIGHT NR 3 FLIGHT DECK WINDOW FRAME E - F CRACKED AT NR 8 FASTENER HOLE. REPAIRED FRAME IAW SI.
LEFT HORIZONTAL STABILIZER SKIN CRACKED ON INBD SIDE OF FRAME AT STAB STATION 129.50, 18 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.
LEFT HORIZONTAL STABILIZER SKIN CRACKED ON INBD SIDE OF FRAME AT STAB STATION 129.50, 10 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.
LEFT HORIZONTAL STABILIZER SKIN 5 INCHES CRACKED ON INBD SIDE OF FRAME AT STATION 175.50, 10.5 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.
AFT EMERGENCY FLASHLIGHTS INOPERATIVE. R & R BATTERIES IAW CMM.
L1 DOOR EXIT LIGHT COVER BROKEN. R & R L1 DOOR EXIT LIGHT ASSEMBLY.
R1 DOOR SLIDE COVER AFT ATTACH NUTPLATE DAMAGED. R & R NUTPLATE IAW MM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY IAW MM.
EXIT LIGHT LENS FWD ENTRY DOOR MISSING. INSTALLED NEW LENS FWD ENTRY EMERGENCY EXIT SIGN AS PER MM.
AFT SERVICE DOOR SLIDE OUT OF CONTAINER. RE-INSTALLED SLIDE ASSY PER 725-61-06.
ONE EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST FWD RIGHT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK FWD RIGHT (M01674) PER M/M AND SSM.
R2 GALLEY DOOR SLIDE COVER LENS CRACKED. REMOVED AND REPLACED R2 GALLEY DOOR SLIDE COVER LENS IAW MT 25-66-01/401.
L2 DOOR SLIDE LOWER FLAP REQUIRES REPOSITION. REPOSITIONED L2 DOOR SLIDE LOWER FLAP IAW M/M.
RIGHTT WING LOWER AFT T/E SHELF PANEL 651GB FWD SUPPORT BRACKET (WIGGLE PLATE) CRACKED AROUND SEVERAL RIVETS. REMOVED AND REPLACED RIGHT WING LOWER AFT T/E SHELF PANEL 651GB FWD SUPPORT BRACKET (WIGGLE PLATE) PER SRM 51-40-02 AND MM
L1 DOOR SLIDE LOWER FLAP REQUIRES REPOSITION. REPOSITIONED PER M/M L1 DOOR SLIDE, C/W T/C 725-61-06.
LEFT EEPLS BROKEN AT ROW 1. REMOVED AND REPLACED EEPLS PER M/M.
RIGHT Z-ANGLE IS CORRODED BETWEEN BS 727D TO BS 767. REPAIRED Z-ANGLE IAW SRM AND DWG.
LEFT FLOOR SUPPORT Z ANGLE UPPER SURFACE CORRODED BETWEEN BS 499 TO 500 + 5, LBL 22. REMOVED AND REPLACED Z ANGLE IAW SRM.
RIGHT ZEE ANGLE CORRODED BETWEEN BS 767 TO BS 794. REMOVED AND REPLACED ZEE ANGLE IAW SRM AND DWG.
RIGHT ZEE ANGLE CORRODED BETWEEN BS 767 TO BS 787. REMOVED AND REPLACED ZEE ANGLE IAW SRM AND DWG.
LEFT WING TRAILING EDGE GROUND SPOILER NR 6 LOWER SKIN PUNCTURED. REMOVED AND REPLACED NR 6 GROUND SPOILER IAW AMM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED STA 101.90. REPAIRED SKIN IAW SRM.
RT HORIZONTAL STAB LOWER IN-SPAR SKIN HAS 2" CRACK AT STAB STA. 139.7. REPAIRED SKIN PER SRM.
LT OVERWING EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED PER AMM.
R2 WINDOW ARCED. REMOVED AND REPLACED NR 3 CONTROLLER, PIGTAIL, AND WINDOW PER MM.
EMERGENCY FLOOR TRACK LENS AT ROW 2 BROKEN. REMOVED AND REPLACED LENS PER AMM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER BROKEN AT ROW 4. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER BROKEN AT ROW 22. REMOVED AND REPLACED COVER PER MM.
RT EMERGENCY EXIT SIDEWALL LIGHT INOP BETWEEN ROW 12 TO ROW 13. REPAIRED LIGHT PER MM.
FWD EEPLS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED SPV CHECK, FOUND LT EEPLS LENS BROKEN AT ROW 11. REMOVED AND REPLACED LENS PER MM.
LT EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.
DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 11. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 19 TO ROW 23. REMOVED AND REPLACED COVER PER MM.
L1 DOOR LOWER EMERGENCY EXIT LENS COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHTS BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED SPV CHECK, FOUND AFT CABIN CENTER CEILING EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.
FWD GALLEY EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM.
DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.
FOUND FIRST EMERGENCY EXIT FLOOR TRACK LIGHT INOP. RECONNECTED WIRES PER MM.
FOUND EMERGENCY EXIT FLOOR TRACK LIGHT INOP. RECONNECTED WIRES PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.
L1 DOOR EMERGECNY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.
EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.