N225WN
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
PASSENGER CABIN SEAT ROW 27ABC AND 27DEF PHOTOLUMINESCENT STRIPS HAS MOISTURE UNDER LENS. REMOVED AND REPLACED IAW AMM 33-51-15-400-802.
AFT UPPER FIXED T/E SEAL RETAINER IS CRACKED JUST INBD OF FLAP PROGRAMING BEAM. REMOVED AND REPLACED SEAL RETAINER FITTING IAW SRM 51-40-02.;[02] C/W INSPECTION
FOUR EMERGENCY LIGHT BATTERY PACK FAILED THE CAPACITY TEST FWD AND AFT ENTRY DOORS AND SERVICE DOORS. REMOVED AND REPLACED BATTERY PACKS FWD LT AND RT BATTERY PACKS AND AFT LT AND RT IAW AMM 33-51-06.
AFT FIXED T/E L ANGLE THAT ATTACHES TO THE FLAP PROGRAMING BEAM IS CRACKED. REMOVED AND REPLACED 1 EACH AFT FIXED T/E L ANGLE THAT ATTACHES TO THE FLAP PROGRAMMING BEAM PER SRM 51-40-02.
AFT F/A PANEL EMERGENCY LIGHT SWITCH GUARD MISSING. R & R SWITCH PANEL ASSY REF SWPM 20-71-03 OPS CHECK NORMAL IAW AMM 33-51-00.
OVERHEAD EXIT SIGN MID CABIN FALLING OFF CEILING. RESECURED OVERHEAD EXIT SIGN MID CABIN AS REQUIRED PER M/M 33-51-01. OPS NORMAL.
CRACK ACCESS PANEL 341B LEADING EDGE RIB LOCATED LE STA 105.26 RT HORIZONTAL STAB. REPLACED RIB LOCATED LEADING EDGE LE STA 105.26 ON RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG:186A1001 SHEET: 11 AND SHEET: 13 REV A ; DWG:186A1304 SHEET: 1 REV A.
BROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA). REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA IAW AMM 33-51-01-960-802 STEP 3.C. ITEM (10).
BROKEN EMERGENCY EXIT LENS LAVATORY A AT FWD GALLEY AREA (1 EA). REPLACED EMERGENCY EXIT LENS LAVATORY A AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-801 STEP 3. C. (5) (D).
BROKEN HOUSING ASSY EMERGENCY LIGHT OVERHEAD STOWAGE BIN 3 LH SIDE AT PASSENGER CABIN. REPLACED HOUSING ASSY EMERGENCY LIGHT OVERHEAD STOWAGE BIN 3 LH SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-03-960-802 TEST IS OK.
BROKEN EMERGENCY EXIT LENS LAVATORY B AT AFT GALLEY AREA (1 EA). REPLACED EMERGENCY EXIT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) IAW AMM 33-51-01-960-801 PROCEDURE 2.C. STEP (4).
CRACK STRINGER 25L LOCATED BS540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 25L LOCATED BS540 FWD CARGO COMPARTMENT IAW SRM 53-00-03-2R-1 REPAIR 1.
CRACK SUPPORT ANGLE LOCATED BS 259.5 AND S-8L PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 259.5 AND S-8L PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0;SRM 51-10-02-0G-0, ITEM 9 AND DWG 141A0720 SHEET 46 REV -.
CORROSION ON STRINGER 25L LOCATED BS947.5 TO BS967 AND WL156 AT AFT CARGO COMPARTMENT. SRM SUPPLEMENT WAS NOT CONSULTED FOR REPAIR INSTRUCTIONS STEP 15 ITEM 2;[04] VERIFIED SUPPLEMENT ARM90-7023-01 REV B PARAGRAPH 3.A TABLE 1002; PAGE 1002; AND THE REPAIR DOES NOT FALL ON AFFECTED STC MODIFICATION. INSPECT COMPLETED. VERIFIED SUPPLEMENT ARM90-7023-01 REV B PARAGRAPH 3.A TABLE 1002; PAGE 1002; AND THE REPAIR DOES NOT FALL ON AFFECTED STC MODIFICATION. REPAIRED STRINGER 25L LOCATED BS 947.5 TO BS 987.5 AND WL156 AT AFT CARGO COMPARTMENT IAW SRM 53-00-03-2R-1.
CORROSION O/B FIXED LEADING EDGE FUEL QUANTITY INDICATOR HOUSING AT RT WING . REPAIRED FUEL SYSTEM PANEL LEADING EDGE BTW SS150.81 & SS163.95 RT WING IAW EA# 25-157-01687 WIP1 AND EA# 25-157-01687.
CORROSION SUPPORT BRACKET LOCATED BS986.5 TO BS1006 AND WL156 AT AFT CARGO COMPARTMEN. REPLACED SUPPORT BRACKET (DRAIN MAST SUPPORT) LOCATED BS 986.5 TO BS 1006 AND WL156 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING#147A7443 SHEET:4 REV:B.
CORROSION ON SUPPORT STRUCTURE LOCATED BS947.5 AT LEVEL STR25L TO STR25R AT AFT CARGO COMPARTMENT. REPLACED SUPPORT STRUCTURE LOCATED BS947.5 AT LEVEL STR25L TO STR25R AT AFT CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9 AND DRAWING 149A8117 SHEET 6 REV: AND DWG 149A8110 SHEET 13 REV: B.
CRACK ON STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. REPLACED STUB FRAME LOCATED BS 294.5 AT LEVEL STR 14R TO 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING# 141A8370 SHEET: 10 REV: D.
CRACK ON CARGO LINER SUPPORT ANGLE CEILING AREA LOCATED BS727C AT LEVEL LBL 45 AT AFT CARGO COMPARTMENT. REPAIRED CARGO LINER SUPPORT ANGLE CEILING AREA LOCATED BS 727C AT LEVEL LBL 45 AT AFT CARGO COMPARTMENT IAW SRM 51-70-11-2R-0.
CRACK ON SUPPORT ANGLE LOCATED BS 695 AND BL0 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 695 AND BL0 AT PASSENGER CABIN AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 273A9110 SHEET: 6 REV: A.
CRACK INDICATION ON STUB FRAME LOCATED BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FWD GALLEY DOOR AREA(1EA). CRACK LENGTH APPROX 0.312 INCH AT PASSENGER CABIN. REPLACED STUB FRAME LOCATED BTW BS 294.5 TO BS 296 AND BTW STR-7R TO STR-11R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40-02 AND DRAWING# 141A8370 SHEET: 9 REV: D.
CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA. REPAIRED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA IAW EA-25-153-01693-WIP1 AND EA-25-153-01693.
CRACK ON SUPPORT BRACKET BULKHEAD AREA LOCATED BS727 AT LEVEL BL 0 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT BRACKET BULKHEAD AREA LOCATED BS727 AT LEVEL BL 0 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 144A2600 SHEET: 566 REV: - .
CORROSION WEB - INTERCOSTAL LOCATED BS767 TO BS787 AND STR25R AT AFT CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL LOCATED BS767 TO BS787 AND STR25R AT AFT CARGO COMPARTMENT IAW B737-700 51-10-02 ITEM 9 AND DRAWING 146A0081 SHEET: 25 REV:.
CRACK ON SUPPORT WEB CEILING AREA LOCATED BS847 TO BS867 AT LEVEL LBL24 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT WEB CEILING AREA AND FASTENER LOCATED BS847 TO BS867 AT LEVEL LBL24 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02 SRM 51-10-02 AND DWG 149A8100 SHEET:1 REV -, LENGHT OF CRACK: 0.574.
CRACK BLADE ACCESS PANEL 343AB AT RT HORIZONTAL STAB. REPLACED ON BLADE ACCESS PANEL 343AB AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9.
CRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. REPAIRED FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW B737-700 EA M-22-153-01244.
CRACK ON SUPPORT ANGLE LOCATED FRONT SPAR BOOST PUMP IFSS 116 TO IFSS 126 AT RT WING. REPLACED SUPPORT ANGLE LOCATED FRONT SPAR BOOST PUMP IFSS 116 TO IFSS 126 AT RT WING I.A.W.B737-700 SRM 51-10-01 AND SRM 51-40-05 AND DRAWING 116A3939 SHEET 1 REV B.
CRACK ON SUPPORT ANGLE LOCATED BS 294.5 BTW STR 13L TO STR 14L AT FWD GALLEY AREA. REPLACED SUPPORT ANGLE LOCATED BS 294.5 BTW STR 13L TO STR 14L AT FWD GALLEY AREA IAW B737-700 51-10-02 ITEM 9 AND DWG 141A1311 SHEET:1 REV:C
CORROSION ON FLOOR STRUCTURE SUPPORT ZEE LOCATED BTW BS500 TO BS500B AT LEVEL S-26L WL156 AT FWD CARGO COMPARTMENT. REMOVED DAMAGE AND EVALUATED REWORK AREAS ON SUPPORT ZEE LOCATED BTW BS500 TO BS500B AT LEVEL S-26L WL 156 AT FWD CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 PARAGRAPH 4.A(2)(A) FIGURE 103 DETAIL D SEE INDIVIDUAL SIGNS OFF BELOW.
CORROSION ANGLE - SUPPORT LOCATED BS 500D AND BTW STR26R TO STR26L WL 156 FWD CARGO COMPARTMENT. EVALUATED ANGLE - SUPPORT LOCATED BS 500D AND BTW STR26R TO STR26L WL 156 FWD CARGO COMPARTMENT AND TOOK MEASURES AFTER REWORK MEASURES AREA L=2.205 W=1.178 D=0.052. NOMINAL THICKNESS IS 0.070? IAW SRM 53-30-08-0I-1 FIGURE 2 TABLE 2 AND BAC1517-2818 AND FOUND OUT LIMITS IAW SRM 53-30-08-1A-1. STEP 4.A (2) (A) FIGURE D. ANGLE - SUPPORT WAS REPLACED IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 143A7902 SHEET: 174 REV: - .
CRACK WEB FRAME LOCATED BS 259.5 BETWEEN S-8R TO S-9R AT PASSENGER CABIN. REPAIRED WEB FRAME LOCATED BS 259.5 BTW WL240 AND WL280 AND BTW RBL20 TO RBL50 AT PASSENGER CABIN IAW-EA-25-153-01592-WIP1 AND EA-25-153-0159.
CORROSION UPPER SILL WEB LOCATED BTW BS440 TO BS494 AT LEVEL STR18R WL196 AT FWD CARGO COMPARTMENT. REPLACED UPPER SILL WEB LOCATED BTW BS440 TO BS494 AT LEVEL STR18R WL196 AT FWD CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-40-02-0G-0 DWG 143A8111 SHEET:12 REV:A.
CRACK ANGLE - SUPPORT LOCATED BS440 AND STR26L FWD CARGO COMPARTMENT. REPLACED ANGLE - SUPPORT LOCATED BS440 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND EVALUATED DAMAGE IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 AND NOT FOUND ALLOWABLE.
CRACK STIFFENER ASSY FLOOR STRUCTURE LOCATED BS540 AND BTW BL 0 TO RBL24.75 PASSENGER CABIN. REPLACED STIFFENER ASSY FLOOR STRUCTURE LOCATED BS540 AND BTW BL 0 TO RBL24.75 PASSENGER CABIN IAW SRM 51-40-02-0G-0 AND DWG 143A0060 SHEET 44 REV A.
CRACK SUPPORT ANGLE LOCATED BS 695 AND BL 0 PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 695 AND BL 0 PASSENGER CABIN IAW SRM 51-10-02 ITEM 9 AND DWG 273A9110 SHEET: 6 REV: A.
CRACK ANGLE - SUPPORT LOCATED BS 500B FWD SIDE AND S-26L FWD CARGO COMPARTMENT 2025-371389<[01] REMPLACED ANGLE - SUPPORT LOCATED AND FASTENERS LOCATED BS 500B FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG: 143A7505 SHEET: 5 REV: B <BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1 <BR>REMPLACED ANGLE - SUPPORT LOCATED BS 500B FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG: 143A7505 SHEET: 5 REV: B<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2 <BR>REPLACED ANGLE - SUPPORT LOCATED BS 500B FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG: 143A7505 SHEET: 5 REV: B<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[04] CORRECTIVE ACTION STEP 3 CERTIFIED
CRACK GUSSET LOCATED BS 500D AND S-21L FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED BS 500D AND S-21L FWD CARGO COMPARTMEN IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING# 143A7902 SHEET 174 REV: .
CRACK GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING# 143A7902 SHEET 174 REV: .
BROKEN FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA). REPLACED FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802.
DELAMINATED TRAILING EDGE SPOILER 7 AT RT WING. REPAIRED TRAILING EDGE SPOILER 7 AT RT WING IAW B737-700 SRM 51-70-10-2R-4 REPAIR 4.
CRACK SUPPORT ANGLE LOCATED BS 695 AND RBL 24.75 PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 695 AND RBL 24.75 PASSENGER CABIN IAW B737-700 51-10-02 ITEM 9 AND DWG 111A6000 SHEET:246 REV .
CRACK STIFFENER ASSY FLOOR STRUCTURE LOCATED BS540 AND BTW BL0 TO LBL 24.75 PASSENGER CABIN. REPLACED STIFFENER ASSY FLOOR STRUCTURE LOCATED BS540 AND BTW BL0 TO LBL 24.75 PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A0060 SHEET 44 REV A.
INOP BATTERY PACK EMERGENCY EXIT DOOR RT SIDE PASSENGER CABIN (1EA). REPLACED BATTERY PACK EMERGENCY EXIT DOOR RT SIDE PASSENGER CABIN IAW AMM 33-51-06-960-805. TEST IS OK..
INOP BATTERY PACK EMERGENCY EXIT DOOR LT SIDE PASSENGER CABIN (1EA). REPLACED BATTERY PACK EMERGENCY EXIT DOOR LT SIDE PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805. TEST IS OK.;
CORROSION HINGE WASTE SERVICE DOOR 145AL AT LOWER FUSELAGE 1 EA, REPLACED HINGE WASTE SERVICE DOOR 145AL AT LOWER FUSELAGE (1 EA) IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG 146A7610 SHEET: 6 REV: -.
RT EMERGENCY EXIT DOOR PASSENGER LIGHT INOP. <[01] RELAMPED PER AMM 33-51-01; [02] C/W INSP. RELAMPED PER AMM 33-51-01.
DOOR HANDLE AFT ENTRY DOOR BROKE OFF<[01] R&R'D AFT ENTRY DOOR HANDLE PER 52-41-31;[02] R&R'D AFT ENTRY DOOR ASSIST HANDLE PER 52-13-31
#3 FLAP FAIRING RUB STRIP RIVETS PULLED THROUGH WIDTH MEASUREMENTS FOR HOLES FROM LEFT TO RIGHT 0.259 0.228 0.255 0.204 0.209<[01] PERFORMED REPAIR 2 ALTERNATIVE 1 IN REF TO SRM 57-53-70-2R-2, WIDTH MEASUREMENTS FOR HOLES: 0.259, 0.228, 0.255, 0.204, AND 0.209; [02] PERFORMED REPAIR 2 ALTERNATIVE 1 IN REF TO SRM 57-53-70-2R-2, WIDTH MEASUREMENTS FOR HOLES: 0.259, 0.228, 0.255, 0.204, AND 0.209. REINSPECT EVERY 500 CYCLES; [03] CW; [04] ENGINEERING CONCURS WITH THE SUBJECT SRM DEFERRAL FOR TTG8Q00YCRDE; 57-53-70-2R-2 ALTERNATE 2.
L1 ESCAPE SLIDE IS IN THE RED<[01] REMOVED AND REPLACED L1 DOOR SLIDE PER AMM 25-66-01 AND MT 725-61-06-FE.
FORWARD SERICE DOOR GRIT BAR PLASTIC HOLDER BROKEN.<[01] REPLACED GIRT BAR IAW AMM 25-66-01. OPS CHECK GOOD
L/H SIDE SLIDE OVERWING EMERGENCY LIGHT INOP<[01] RELAMPED L/H SIDE SLIDE OVERWING EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD
FWD ENTRY DOOR ASSIST HANDLE FELL OFF<[01] REMOVE AND REPLACE FWD ENTRY DOOR ASSIST HANDLE PER AMM 52-11-00. OPS CHECK GOOD.
PHOTO LUMINESCENT LIGHT STRIP ON FLOOR BURNT OUT. FRONT RIGHT<[01] R&R PHOTO LUMINESCENT STRIP (36 IN. ) AT ROW 1DEF PER AMM 33-51-15
FORWARD SERVICE DOOR AFT GIRT BAR STOWAGE BRACKET MISSING ONE RIVET.<[01] INSTALLED BRACKET WITH NEW HARDWARE IAW SRM 51-40-02.
GIRT BAR WILL NOT SEAT IN THE AFT BRACKET OF THE FWD SERVICE DOOR<[01] ACCOMPLISHED TEMP REPAIR PER EA M-23-125-01839
FWD MEGAPHONE WONT TEST<[01] R&R FWD MEGAPHONE IAW AMM 25-64-00.
ROW 1 DEF EMERGENCY EXIT LIGHT INOP<[01] CYCLED COCKPIT EMERGENCY LIGHT SWITCH. ROW 1 DEF EMERGENCY EXIT LIGHT WORKS. REF AMM 33-51-00.
WING TO BODY PANEL 193AL HAS DELAMINATION ON TRAILING EDGE.<[01] ACCOMPLISHED PERMANENT REPAIR IAW SRM 51-70-05-2R-10.
WING TO BODY FAIRING PANEL 193AL HAS EDGE DAMAGE AT UPPER AFT TRAILING EDGE THAT IS DELAMINATED APPROXIMATELY 2 AFT OF TE TO 4 DOWN FROM UPPER END (AFT UPPER CORNER OF PANEL).<[01] DELAM IS 6 INCHES FROM TOP OF TRAILING EDGE OF PANEL 193AL AND 2 1/2 INCHES IN WIDTH. DAMAGE IS OUT OF LIMITS REF SRM 53-40-70-1A-1 ITEM (6).;[02] COMPLIED WITH TSR 2023008594 REF TTG8Q00P6ENS.;[03] COMPLETED TEMP REPAIR IAW EA 23-153-03152
AFT ENTRY DOOR SLIDE HAS TWO CRACKED ISOLATORS .<[01] R&R AFT ENTRY DOOR SLIDE ISOLATORS IAW SRM 51-40-02.
CRACK ON HOLE OF LIP INLET COWL LOC. 1 OCLOCK LT ENGINE 2023-490779<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[02] TOOL USED: MICROMETER P/N: 293-344-30; S/N: 71735394; DUE DATE: 23-NOV-23 AND SMALL HOLE GAUGES P/N: 154-901; S/N: AE-411355; DUE DATE: 27-JAN-24;[03] TOOL USED MICROMETER PN: 500-196-30 ; SN: A21126170 DUE DATE 09-NOV-23;[04] TOOL USED MICROMETER PN: 293-344-30 SN: 71735394 DUE DATE 23-NOV-23;[05] REPAIRED HOLE ON INLET COWL LOC 1 O CLOCK LT ENGINE I.A.W EA 23-171-02672-WIP1 AND EA SUMMARY 23-171-02672.SEE INDIVIDUAL STEP SIGN OFS BELOW;[06] CORRECTED STEP #5 REPAIRED HOLE ON INLET COWL LOC 1 O CLOCK LT ENGINE I.A.W EA 23-171-02672-WIP1 AND EA SUMMARY 23-171-02672.SEE INDIVIDUAL SIGN OF BELOW;[07] CORRECTED STEP 5 <BR>REPAIRED HOLE ON INLET COWL LOC 1 O CLOCK LT ENGINE I.A.W EA 23-171-02672-WIP1 AND EA SUMMARY 23-171-02672.SEE INDIVIDUAL SIGN OF BELOW
BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2023-490767<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802
CRACK INSPAR RIB 129.50 LOWER FLANGE REAR SPAR AT LT HORIZONTAL STABILIZER 2023-490754<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 25-JAN-24. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE: 01-FEB-24.;[02] TOOL USED: RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1753759; CAL DUE DATE: 14-OCT-23;[03] PERFORMED PERMANENT REPAIR ON INSPAR RIB 129.50 LOWER FLANGE REAR SPAR AT LT HORIZONTAL STABILIZERI.A.W. B737-700 SRM 55-10-09-2R-5 REPAIR 5 AND EA 23-155-02645-WIP1 AND EA COVER 23-155-02645<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[04] PERFORMED PERMANENT REPAIR ON INSPAR RIB 129.50 LOWER FLANGE REAR SPAR AT LT HORIZONTAL STABILIZERI.A.W. B737-700 SRM 55-10-09-2R-5 REPAIR 5 AND EA 23-155-02645-WIP1 AND EA COVER 23-155-02645 RII CRETIFIED
CRACK INSPAR RIB 129.50 UPPER FLANGE FRONT SPAR AT LT HORIZONTAL STABILIZER 2023-490753<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 25-JAN-24. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE: 01-FEB-24.;[02] PERFORMED REPAIR ON INSPAR RIB 129.50 UPPER FLANGE FRONT SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5; STEP 4. N TO S; AND 23-155-02568-WIP1; SEE INDIVIDUAL SIGN-OFF BELOW.;[03] CORRECTED ACTION 2<BR>PERFORMED REPAIR ON INSPAR RIB 129.50 UPPER FLANGE FRONT SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5; STEP 4.(N) TO 4.(S); AND 23-155-02568-WIP1; SEE INDIVIDUAL SIGN-OFF BELOW.;[04] CORRECTED ACTION 2<BR>PERFORMED REPAIR ON INSPAR RIB 129.50 UPPER FLANGE FRONT SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5; STEP 4.(N) TO 4.(S); AND 23-155-02568-WIP1;RII SEE INDIVIDUAL SIGN-OFF BELOW.;[05] CORRECTED STEP 3<BR>PERFORMED REPAIR ON INSPAR RIB 129.50 UPPER FLANGE FRONT SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 AND EA-23-155-02568-WIP1 AND EA COVER EA-23-155-02568 <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[06] RII ITEM <BR>PERFORMED REPAIR ON INSPAR RIB 129.50 UPPER FLANGE FRONT SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 AND EA-23-155-02568-WIP1 AND EA COVER EA-23-155-02568 <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.
CORROSION DOOR 315A SUPPORT BRAKETS ON APU COMPARTMENT (4 EA) 2023-490756<[01] REPLACED SUPPORT BRACKETS LOCATED ON APU COMPARTMENT (4 E/A) IAW B737-700 SRM 51-40-02 AND AND DWG 148A6350 REV: C; SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED SUPPORT BRACKETS LOCATED ON APU COMPARTMENT (4 E/A) IAW B737-700 SRM 51-40-02 AND AND DWG 148A6350 REV: C; SEE INDIVIDUAL SIGN-OFF BELOW
CRACK INDICATION FOUND AT FLOOR BEAM ATTACH HOLE INNER CHORD LAYER LOC BS 294 5 RBL 58 FWD GALLEY AREA 2023-490743<[01] REPLACED INNER CHORD LOC BS 259.50 TO BS 360 RBL 58 FWD GALLEY AREA PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 141A8310 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INNER CHORD LOC BS 259.50 TO BS 360 RBL 58 FWD GALLEY AREA PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 141A8310 REV:-.RII; SEE INDIVIDUAL SIGN OFF BELOW.
ELONGATED HOLE ON LEADING EDGE ACCESS PANEL 621LB RT WING (1 EA) 2023-490744<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189416; DUE DATE: 19/DEC/23;[02] TOOL USED: SCALE P/N:CR5200 S/N:8342514510 DUE DATE: 13-FEB-24;[03] TOOL USED: HOT BONDER PN: HCS9200B- AV SN:18196127 DUE DATE: 22-JAN-24;[04] TOOL USED: SCALE P/N:CR5200 S/N:8342514510 DUE DATE: 13-FEB-24;[05] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18196119; DUE DATE: 23-MAY-24.;[06] TOOL USED: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 650; S/N: 190984811; DUE DATE: 24-JAN-24;[07] TOOL USED: SCALE P/N: SPX621 S/N: 8340225469 DUE DATE: 20-JUL-24.;[08] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18196021 DUE DATE 24-JAN-24;[09] TOOL USED: MULTIMETER PN: FLUKE-289; S/N: 61180120; DUE DATE: 30-MAY-24;[10] REPAIRED ACCESS PANEL 621LB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGN OFFS BELOW.;[11] JOB TASK COMPLETED.
ELONGATED HOLE CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING 2023-490733<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING I.A.W. B737-700 DWG 115A2001 SHEET 32 REV- AND SRM: 51-10-02 ITEM 9.;[02] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING I.A.W. B737-700 DWG 115A2001 SHEET 32 REV- AND SRM: 51-10-02 ITEM 9
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING 2023-490734<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING I.A.W. B737-700 DWG 115A2001 SHEET 30 REV. A AND SRM: 51-10-02 ITEM 9.;[02] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING I.A.W. B737-700 DWG 115A2001 SHEET 30 REV. A AND SRM: 51-10-02 ITEM 9.
CRACK BODY STATION 540 SUPPORT BRACKET LH SIDE AT AIR CONDITIONING BAY 2023-490735<[01] REPLACED SUPPORT BRACKET IN 540 BODY STATION AT LH AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02-0G;[02] REPLACED SUPPORT BRACKET IN 540 BODY STATION AT LH AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02-0G
CRACK BODY STATION 540 SUPPORT BRACKET RH SIDE AT AIR CONDITIONING BAY 2023-490736<[01] REPLACED SUPPORT BRACKET IN 540 BODY STATION AT RH AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02-0G;[02] REPLACED SUPPORT BRACKET IN 540 BODY STATION AT RH AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02-0G
CRACK EXTERNAL SKIN SLAT 8 LOWER SURFACE AT SLAT STATION 451.97 AT RT WING 2023-490709<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: 00X11290U021704; CAL DUE DATE: 12-MAR-24;[02] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: 00X11290U021704; CAL DUE DATE: 12-MAR-24;[03] TOOL USED DIGITAL CALIPER PN: 500-197-30; SN: B20189523 DUE DATE 21-FEB-24;[04] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[05] TOOL USED DIGITAL CALIPER PN: 500-197-30; SN: B20189523 DUE DATE 21-FEB-24;[06] PERFORMED REPAIR ON EXTERNAL SKIN SLAT 8 LOWER SURFACE AT SLAT STATION 451.97 AT RT WING IAW SRM B737-700 57-42-01-2R-8 REPAIR 8. SEE INDIVIDUAL SIGN OFF BELOW.;[07] PERFORMED REPAIR ON EXTERNAL SKIN SLAT 8 LOWER SURFACE AT SLAT STATION 451.97 AT RT WING IAW SRM B737-700 57-42-01-2R-8 REPAIR 8. SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ANGLE TRAILING EDGE SUPPORT LOCATED ORSS 261 PLUS 11 INCHES ON DEFLECTION CONTROL RIB AREA AT LT WING 2023-490672<[01] REPLACE SUPPORT ANGLE ON TRAILING EDGE LOCATED ORSS 261 PLUS 11 INCHES ON DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 1A5A2930 SHEET 7 REV. - <BR><BR>TOOL USED P/N 500-196-30 S/N A21125526 DUE 05-NOV-23;[02] CORRECTED STEP 1 REPLACE SUPPORT ANGLE ON TRAILING EDGE LOCATED ORSS 261 PLUS 11 INCHES ON DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2930 SHEET 7 REV. - <BR><BR>TOOL USED P/N 500-196-30 S/N A21125526 DUE 05-NOV-23;[03] CORRECTED STEP 1 REPLACE SUPPORT ANGLE ON TRAILING EDGE LOCATED ORSS 261 PLUS 11 INCHES ON DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2930 SHEET 7 REV. - <BR><BR>TOOL USED P/N 500-196-30 S/N A21125526 DUE 05-NOV-23
BROKEN GALLEY 1 EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY AREA 2023-490637<[01] REPLACED GALLEY 1 EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-802 AND OPERATIONAL TEST IS OK;[02] COMPLETED
DELAMINATED ACCESS PANEL 193AL AT LOWER FUSELAGE 2023-490660<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: B20189416 DUE DATE: 19-DEC-23.;[02] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18196126; DUE DATE: 26/MAR/24;[03] TOOL USED SCALE PN: CR5200; SN: 8342514541; DUE DATE: 15/FEB/24.;[04] TOOL USED: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 650; S/N: 190984811; DUE DATE: 24-JAN-24.;[05] REPAIRED ACCESS PANEL 193AL AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-6 REPAIR 6. SEE INDIVIDUAL SIGNOFFS BELOW;[06] TASK COMPLETED.
CRACK OUTBOARD TRAILING EDGE SUPPORT ANGLE LOCATED ORSS279 AT RT WING 2023-490657<[01] REPLACED SUPPORT ANGLE LOCATED OUTBOARD TRAILING EDGE ORSS279 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A6200 REV. -; MEASURE OF CRACK IS: L= 0.812? TOOL USED CALIPER P/N 500-196-30; S/N A26231842; DUE DATE 21/FEB/24;[02] REPLACED SUPPORT ANGLE LOCATED OUTBOARD TRAILING EDGE ORSS279 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A6200 REV. -; MEASURE OF CRACK IS: L= 0.812? TOOL USED CALIPER P/N 500-196-30; S/N A26231842; DUE DATE 21/FEB/24
CRACK SUPPORT ANGLE LOWER SURFACE REAR SPAR LOCATED TRAILING EDGE ORSS 261 PLUS 20 INCHES LT WING 2023-490679<[01] REPLACED SUPPORT ANGLE LOWER SURFACE REAR SPAR LOCATED TRAILING EDGE ORSS 261 PLUS 20 INCHES LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A7112 REV:-. LENGTH OF CRACK:1.070?. TOOL USED CALIPER P/N: 500-196-30 S/N:A21126170 DUE DATE: 09-NOV-23;[02] TASK COMPLETED
CRACK ACCESS PANEL 551FB TRAILING EDGE SUPPORT BRAKET LT WING 2023-490612<[01] REPLACED SUPPORT BRACKET LOC. ON ACCESS PANEL 551FB TRAILING EDGE LT WING IAW B737-700 SRM 51-40-02-0G-0 ; SRM 51-40-05-0G-0 AND DWG 115A2710. SHEET 6 REV B;[02] REPLACED SUPPORT BRACKET LOC. ON ACCESS PANEL 551FB TRAILING EDGE LT WING IAW B737-700 SRM 51-40-02-0G-0 ; SRM 51-40-05-0G-0 AND DWG 115A2710. SHEET 6 REV B
CRACK CARGO TRACK LOCATED BS727E LBL17.24 AND WL156 AT AFT CARGO COMPARTMENT 2023-490578<[01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138003; CAL DUE DATE: 27-MAR-24;[02] PERFORMED REPAIR ON CARGO TRACK LOCATED BS727D TO 727E LBL17.24 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4 ITEM ?O AND P? SRM 51-40-02 AND DWG 146A7500 REV: A. SEE INDIVIDUAL SIGN-OFF BELOW;[03] CORRECTED ACTION STEP 2<BR>PERFORMED REPAIR ON CARGO TRACK LOCATED BS727D TO 767 LBL17.24 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4 ITEM ?O AND P? SRM 51-40-02 AND DWG 146A7500 REV: A. SEE INDIVIDUAL SIGN-OFF BELOW;[04] PERFORMED REPAIR ON CARGO TRACK LOCATED BS727D TO 767 LBL17.24 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4 ITEM ?O AND P? SRM 51-40-02 AND DWG 146A7500 REV: A. <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGN-OFF BELOW
CRACK WEB - INTERCOSTAL LOCATED BS947 RBL21 AND WL179 AT AFT CARGO COMPARTMENT 2023-490605<[01] REPLACED WEB - INTERCOSTAL LOCATED BS927 TO BS947 RBL21 AND WL179 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7500 REV. - SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTED STEP 1:<BR>REPLACED WEB - INTERCOSTAL LOCATED BS927 TO BS947 RBL21 AND WL179 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7500 REV. - SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 1: <BR>REPLACED WEB - INTERCOSTAL LOCATED BS927 TO BS947 RBL21 AND WL179 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7500 REV. - RII; SEE INDIVIDUAL SIGN OFF BELOW.
CRACK CARGO TRACK LOCATED BS767 RBL13.84 AND WL156 AT AFT CARGO COMPARTMENT 2023-490581<[01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138003; CAL DUE DATE: 27-MAR-24;[02] PERFORMED REPAIR ON CARGO TRACK LOCATED BETWEEN BS747 TO 787 RBL13.84 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4 ITEM ?O AND P? SRM 51-40-02 AND DWG 146A7500 REV: A. SEE INDIVIDUAL SIGN-OFF BELOW.;[03] PERFORMED REPAIR ON CARGO TRACK LOCATED BETWEEN BS747 TO 787 RBL13.84 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4 ITEM ?O AND P? SRM 51-40-02 AND DWG 146A7500 REV: A. <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGN-OFF BELOW.
CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 11INCH AND RBL12 AFT CARGO COMPARTMENT 2023-490602<[01] REPLACED ANGLE - SUPPORT LOCATED BS907 PLUS 11INCH AND RBL12 AFT CARGO COMPARTMENT IAW B737-700 SRM-51-40-02 AND DWG-147A7221 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] COMPLETE TASK CERTIFIED
CRACK CARGO TRACK LOCATED BS767 LBL17.24 AND WL156 AT AFT CARGO COMPARTMENT 2023-490579<[01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138003; CAL DUE DATE: 27-MAR-24;[02] PERFORMED REPAIR ON CARGO TRACK LOCATED BETWEEN BS767 TO BS787 LBL17.24 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4 ITEM ?O AND P? SRM 51-40-02 AND DWG 146A7500 REV: A. SEE INDIVIDUAL SIGN-OFF BELOW.;[03] PERFORMED REPAIR ON CARGO TRACK LOCATED BETWEEN BS767 TO BS787 LBL17.24 AND WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4 ITEM ?O AND P? SRM 51-40-02 AND DWG 146A7500 REV: A. <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGN-OFF BELOW.
CORROSION SUPPORT ZEE LOCATED BETWEEN BS727E TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT 2023-490559<[01] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BSU67 RBL21 AND WL156 AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 146A7500 SHEET 85 REV. A AND DWG 146A7502 SHEET 26 REV. -<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 RBL21 AND WL156 AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 146A7500 SHEET 85 REV. A AND DWG 146A7502 SHEET 26 REV. -<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 RBL21 AND WL156 AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 146A7500 SHEET 85 REV. A AND DWG 146A7502 SHEET 26 REV. - <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW<BR>AS RII
CORROSION WEB - INTERCOSTAL LOCATED BS492 TO BS500A RBL21 AND WL156 AT FWD CARGO COMPARTMENT 2023-490506<[01] REPLACED WEB - INTERCOSTAL LOCATED BS492 TO BS500A RBL21 AND WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM-51-40-02 AND DWG-143A0080 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED WEB - INTERCOSTAL LOCATED BS492 TO BS500A RBL21 AND WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM-51-40-02 AND DWG-143A0080 REV: - SEE INDIVIDUAL SIGN-OFF BELOW<BR>AS RII
CRACK ANGLE LOCATED STA 294.5 AND RBL54 WL 208.1 AT FWD GALLEY AREA 2023-490509<[01] REPLACED ANGLE LOCATED STA 294.5 AND RBL54 WL 208.1 AT FWD GALLEY AREA AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 141A8310 SHEET: 25 REV: B SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK TIE CLIP LOCATED STA 277 AND STR 10R AT PASSENGER CABIN 2023-490549<[01] REPLACED TIE CLIP LOCATED STA 277 AND STR 10R AT PASSENGER CABIN B737-700 SRM 51-40-02 AND DWG 141A1110 REV- SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETED <BR>REPLACED TIE CLIP LOCATED STA 277 AND STR 10R AT PASSENGER CABIN B737-700 SRM 51-40-02 AND DWG 141A1110 REV- SEE INDIVIDUAL SIGN OFF BELOW<BR>RII
CRACK FLOOR BEAM LOCATED STA 294.5 AND RBL52 WL 208.1 AT FWD GALLEY AREA 2023-490507<[01] TOOL USED EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220273012; DUE DATE: 17-DEC-23.;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 210138103; CAL DUE DATE: 02-MAY-24;[03] TOOL USED RADIOMETER/PHOTOMETER KIT PN: XRP-3000; SN: 199872; DUE DATE: 15-OCT-23;[04] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[05] TOOL USED: RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1753759; CAL DUE DATE: 14-OCT-23;[06] PERFORMED PERMANENT REPAIR ON FLOOR BEAM LOCATED STA294.5 AND RBL17 TO RBL 58 ; WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16 AND DWG # 141A5502 REV: -. SEE INDIVIDUAL SIGN OFF BELOW<BR>SEE INDIVIDUAL SIGNOFFS BELOW.;[07] RII COMPLETED JOB
CRACK INNER CHORD LOCATED STA 303.9 AND LBL 55 WL 208.1 AT FWD GALLEY AREA 2023-490510<[01] REPLACED INNER CHORD LOCATED BS270 TO BS360 WL208.1 AND LBL56 AT FWD GALLEY AREA AND FASTENERS I.A.W B737-700 SRM 51-40-02 DWG: 141A8310 SHEET: 25 REV: B SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED STA344 TO STA360 AND BL0 WL208.1 FWD GALLEY AND LAV 2023-490514<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED STA344 TO STA360 AND BL0 WL208.1 FWD GALLEY AND LAV IAW B737-700 SRM-51-40-02 AND DWG-141A5400 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED STA344 TO STA360 AND BL0 WL208.1 FWD GALLEY AND LAV IAW B737-700 SRM-51-40-02 AND DWG-141A5400 REV: - SEE INDIVIDUAL SIGN-OFF BELOW RII CERTIFIED
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED STA344 TO STA360 AND LBL11 WL208.1 FWD GALLEY AND LAV 2023-490515<[01] REPLACED WEB- INTERCOSTAL AND FASTENERS LOCATED ON FLOOR STRUCTURE BETWEEN STA344 TO STA360 AND LBL11 WL208.1 FWD GALLEY IAW B737-700 SRM 51-40-02 AND DWG 141A5400 REV:A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB- INTERCOSTAL AND FASTENERS LOCATED ON FLOOR STRUCTURE BETWEEN STA344 TO STA360 AND LBL11 WL208.1 FWD GALLEY IAW B737-700 SRM 51-40-02 AND DWG 141A5400 REV:A. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII
CRACK ACCESS PANEL 561CB TRAILING EDGE AROUND HOLES LT WING 2023-490520<[01] TOOL USED CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 17-OCT-23.;[02] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18196126; DUE DATE: 26/MAR/24.;[03] TOOL USED SCALE PN: CR5200; SN: 8342514541; DUE DATE: 15/FEB/24.;[04] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196127 DUE DATE:22-JAN-24.;[05] TOOL USED: SCALE P/N: CR5200 S/N: 8342514510 DUE DATE: 13-FEB-24.;[06] TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18196119 DUE DATE: 23-MAY-24;[07] ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190984811; DUE DATE: 24-JAN-24.;[08] TOOL USED: MULTIMETER P/N: FLUKE 87 S/N: 90160155 DUE DATE: 14-DEC-23.;[09] REPAIRED ACCESS PANEL 561CB AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[10] JOB COMPLETED.
CRACK FLOOR PANEL 241AEF AT AFT GALLEY AND LAV 2023-490491<[01] TOOL USED CALIPER P/N: 500-197-30 S/N/ B20189527 DUE DATE 26/DEC/23.;[02] TOOL USED: HOT BONDER P/N:HCS9000B-AV S/N:18164925 DUE DATE:22-JAN-24;[03] TOOL USED: CR5200 S/N:8342514510 DUE DATE:13-FEB-24;[04] TOOL USED HOT BONDER P/N: HCS9000B-AV; S/N: 18164925; DUE DATE: 22-JAN-24.;[05] TOOL USED: CR5200 S/N:8343110765 DUE DATE:20-FEB-24.;[06] REPAIRED FLOOR PANEL 241AEF AT AFT GALLEY AND LAV IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFFS BELOW.;[07] JOB TASK COMPLETED. RII INSPECTION COMPLETED .
CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2023-490497<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A18229508;DUE DATE:30-OCT-23.;[02] TOOL USED: RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1753759; CAL DUE DATE: 14-OCT-23;[03] REPAIRED AFT CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B. STEPS ( 2 ) TO ( 7 ) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] JOB TASK COMPLETED.
CRACK INSPAR RIB LOCATED STAB STA129.50 AND 26.5 INCHES FROM FRONT SPAR LT HORIZONTAL STAB 2023-490344<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022237; DUE DATE: 26-JAN-24;[04] PERFORMED PERMANENT REPAIR ON INSPAR RIB STA129.50 AND 26.5 INCHES FROM FRONT SPAR LT HORIZONTAL STAB I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED PERMANENT REPAIR ON INSPAR RIB STA129.50 AND 26.5 INCHES FROM FRONT SPAR LT HORIZONTAL STAB I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN OFF BELOW.<BR>AS RII
INOP EMERGENCY LIGHT ON BIN 5LH AND 6LH AT PASSENGER CABIN (2 EA) 2023-490174<[01] REPLACE EMERGENCY LIGHT ON BIN 5LH AND 6LH AT PASSENGER CABIN (2 EA) IAW AMM 33-51-03-960-802 SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACE EMERGENCY LIGHT ON BIN 5LH AND 6LH AT PASSENGER CABIN (2 EA) IAW AMM 33-51-03-960-802 SEE INDIVIDUAL SIGN OFF BELOW
CRACK SLAT 2 AT LOWER SURFACE SLAT STATION 322.71 AT LT WING 2023-490243<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512 AND DUE DATE: 17-DEC-23.;[02] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101V022237 DUE DATE 26-JAN-24;[03] PERFORMED PERMANENT REPAIR BTW SLAT STATION 312 TO SLAT STATION 336 ON SLAT 2 AT LOWER SURFACE I.A.W. B737-700 SRM 57-42-01-2R-8 REPAIR 8 <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[04] INSTALLED REPAIR LOCATED BTW SLAT STATION 312 TO SLAT STATION 336 ON SLAT 2 AT LOWER SURFACE I.A.W. B737-700 SRM 57-42-01-2R-8 REPAIR 8 STEP 4.F.(10) AND FIGURE202 SHEET 2 ALTERNATIVE 1 AND SRM 51-40-02 SEE INDIVIDUAL SING OFF BELOW;[05] INSTALLED REPAIR LOCATED BTW SLAT STATION 312 TO SLAT STATION 336 ON SLAT 2 AT LOWER SURFACE I.A.W. B737-700 SRM 57-42-01-2R-8 REPAIR 8 STEP 4.F.(10) AND FIGURE202 SHEET 2 ALTERNATIVE 1 AND SRM 51-40-02 SEE INDIVIDUAL SING OFF BELOW
AFT RIGHT EMERGENCY LIGHTING CHARGER INOP. REMOVED AND REPLACED CHARGER PER AMM 33-51-06. RESEALED GALLEY CEILING ACCESS PANEL.
UPPER VAPOR BARRIER ANGLE IN ECS BAY IS CRACKED AT STA 663; WL 167; RBL 41.<[01] VERIFIED ACTION STEP 1 OF STEPS 1; 2 AND 3;[02] VERIFIED ITEM 1 OF STEPS 4; 6; AND 7;[03] VERIFIED ITEM 5 OF STEP 7 AND ITEM 1 OF STEP 8;[04] VERIFIED ITEM 3 OF STEP 8;[05] VERIFIED ITEM 7 OF STEP 4;[06] AUDIT CW
UPPER VAPOR BARRIER ANGLE IN ECS BAY IS CRACKED AT STA 663; WL 167; LBL 41.<[01] REMOVED VERTICAL STIFFENER AT LBL 39 AND HORIZONTAL U-CHANNEL IAW SRM 51-40-02-0G-0.;[02] VERIFIED ITEM 1 OF STEPS 3; 4; 6 AND 7;[03] VERIFIED ITEM 5 OF STEP 7 AND ITEM 1 OF STEP 8;[04] VERIFIED ITEM 3 OF STEP 8;[05] VERIFIED ITEM 2 OF STEP 10;[06] AUDIT CW
CABIN FLOOR PANEL 232SF UPPER SURFACE HAS PULLED FIBERS. FOUND WITHIN REPAIRABLE LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1. PREPPED FLOOR PANEL 232SF FOR WET LAY-UP REPAIR IAW SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (A-J). BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 232SF IAW SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (K-O).
CABIN FLOOR PANEL 231YF UPPER SURFACE HAS PULLED FIBERS. FOUND WITHIN REPAIRABLE LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1. BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 231YF IAW SRM 53-00-50-2R-1, REPAIR 1 STEPS 3, (K-O).
CABIN FLOOR PANEL 231ZF UPPER SURFACE HAS PULLED FIBERS. FOUND WITHIN REPAIRABLE LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1. BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 231ZF IAW SRM 53-00-50-2R-1, REPAIR 1, STEPS 3, (K-O).
CABIN FLOOR PANEL 231XF UPPER SURFACE HAS PULLED FIBERS. FOUND WITHIN REPAIRABLE LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1. BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 231XF IAW SRM 53-00-50-2R-1, REPAIR 1 STEPS 3, (K-O).
CABIN FLOOR PANEL 241AF UPPER SURFACE HAS PULLED FIBERS. FOUND OUT OF LIMITS OF SRM 53-00-50-2R-0. FABRICATED A NEW FLOOR PANEL 241AF IAW DWG 1445810 AND SRM 53-00-50-2R-0, REPAIR GENERAL.
PASSENGER SEAT 11D RECLINES INTO EMERGENCY ROW / [01] ADJUSTED HYDROLOCK COLLAR ON SEAT 11D PER CMM 25-21-42;[02] C/W
FWD GIRT BAR HANDLE DOES NOT SECURE IN PLACE WHEN STOWED CREW VERBALLY STATED IT WAS FWD SERVICE DOOR. / [01] SECURED FWD SERVICE DOOR GIRT BAR HANDLE PER SIP.
AFT LAV SMOKE ALARM AT 8K ON APPROACH FA NOTICED ELECTRICAL SMELL. WATER HEATER AFT LAV FLASHING YELLOW. NO EVIDENCE OF FIRE. / [01] PERFORMED CONDITIONAL INSPECTION AMM 05-51-56. SEE LOG PAGE 1883562 FOR INOP WATER HEATER. AC OK FOR SERVICE
AFT LAV ALARM ALERTED;FAINT ELECTRIC SMELL AFTER AHUTDOWN / [01] REMOVED AND REPLACED AFT LAV SMOKE DETECTOR IAW M.M 26-14-01 ;AND PREFORMED CONDITIONAL INSP IAW M.M 05-51-56. NO DEFECTS NOTED
AREA LIGHT NEAR RH OVER WING EXIT IS INOP. ; / [01] RELAMPED AREA LIGHT NEAR RH OVER WING EXIT PER AMM 33-51-03
ASSOCIATED EMERGENCY LIGHTS WITH BATTERY PACK M1674 ARE INOP. ; ASSOCIATED EMERGENCY LIGHTS WITH ATTERY PACK M1674 ARE INOP. / [01] REMOVED AND REPLACED BATTERY PACK M1674 PER AMM 33-51-06-960-805. GND TEST NORMAL<BR>AAR TAG WN8585; [02] REMOVED AND REPLACED BATTERY PACK M1674 PER AMM 33-51-06-960-805. OPS TEST NORMAL<BR>AAR TAG WN8585; [03] REMOVED AND REPLACED BATTERY PACK M1674 PER AMM 33-51-06-960-805. OPS TEST NORMAL <BR>AAR TAG WN8585; [04] VERIFIED 3
FUSELAGE FAIRING PANEL 193AR HAS A DENT AND AREA DELAMINATED ; / [01] REMOVED DAMAGED PLIES AT PANEL 193AR AS PER B737-700 SRM 51-70-04 GENERAL ; PARAGRAPH 4.B. NO WATER FOUND; [02] PREPARED DAMAGED AREA FOR REPAIRAS PER B737-700 SRM 51-70-04-2R-1; [03] LATE ENTRY. STEP 1. PERFORMED TAP TEST INSPECTION AT DAMAGED AREA AT PANEL 193AR AS PER B737-700 SRM 51-70-04-2R-0 PARAGRAPH 4.A; AND B737 NDT PART 1; 51-05-01. CONFIRMED FAULT; FOUND AREA DELAMINATED.; [04] MEASUREMENTS; [05] APPLIED PRIMER AT REPAIRED AREA PANEL #193AR AS PER B737 AMM 51-21-99-300-802. MATERIALS USED P/O# 1723513; [06] LATE ENTRY: STEP 4: REPAIRED DAMAGED PANEL 193AR AS PER B737 SRM 51-70-04-2R-1; PARAGRAPH 4.B. MATERIALS USED P/O#1731939 AND P/O#1690463; [07] VERIFIED STEPS 4: 5 & 6; [08] PENDING RESTORATION FINISH; [09] APPLIED TOP COAT TO REPAIR AREA PER B737-700 AMM 51-21-73-370-804.; [10] VERIFIED 9
PANEL 191AR DELAMINATED AT 4 SCREWS ATTACHMENTS POINT AREA ; / [01] REMOVED PANEL#191AR FOR ACCESS TO REPAIR AT R/H FORWARD WING TO BODY FAIRING PANEL PER B737-700 AMM 53-51-21-000-803.; [02] MEASUREMENTS; [03] CLEANED AREA AND PREPARED AREA FOR REPAIR ON DAMAGE SCREW HOLE OF PANEL 191AR AS PER B737 SRM 51-70-04-2R-9; [04] VERIFIED 2 & 3<BR>OK TO INSTALL REPAIR; [05] REPAIRED DAMAGE SCREW HOLE ON WING TO BODY FAIRING 191AR AS PER B737 51-70-04-2R-9 MATERIAL USED PO#1731939 AND PO#1690463; [06] PERFORMED TAP TEST ON REPAIRED AREA ON PANEL 191AR FOUND NO DELAMINATION AS PER B737 NDTM 51-05-1 SECTION 5; [07] VERIFIED 5 & 6.<BR>OK TO INSTALL REPAIR; [08] OK TO INSTALL PANEL; [09] CORRECTION: <BR>STEP 7 VERIFIED REPAIR INSTALLATION AND STEPS 5 & 6; [10] INSTALLED PANEL 191AR IAW B737 AMM 53-51-21-400-803<BR><BR>BONDING METER-B/C:168696; [11] VERIFIED STEP 10; [12] REPAIR WAS PERFORMED ON PANEL 191AR AT 4 ATTACHMENT POINT AREA AS PER B737-700 SRM 51-70-04-2R-9; [13] VERIFIED STEP 12
AFT CARGO FLOOR STRUCTURE R/H SIDE REVEAL AT S-25R BETWEEN STA 767-787 WITH CORROSION ; / [01] REMOVED CORROSION ON AFT CARGO FLOOR STRUCTURE R/H SIDE REVEAL STA 767-787 AS PER B737-700 SRM 51-10-02-0G-0; [02] VERIFIED STEP 1; [03] PERFORMED UT THICKNESS INSP ON REWORKED AREA AFT CARGO FLOOR STRUCTURE R/H SIDE REVEAL STA 767-787 IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THICKNESS NOTED 0.030' <BR>TOOL USED : MX-3 B/C 17049 CALDUE: 15-JUN-22; [04] ORIGINAL MATERIAL .05' MATERIAL LOSS .02' MATERIAL REMAINING .03' FOUND OUT OF LIMITS AS PER B737-700 SRM 25-52-01-201-801.; [05] LOCATED AND DRILLED NEW SHIELD P/N:146A8127U12 AS PER B737-700 SRM 51-40-05-0G-0.; [06] ORIGINAL MATERIAL .05' MATERIAL LOSS .02' MATERIAL REMAINING .03' FOUND OUT OF LIMITS AS PER B737-700 SRM 53-60-15-1A-1 AND SRM 53-60-15-1I-1; [07] REFERENCE TASK CARD TTG8Q004BYMK FOR SHIELD INSTALLATION.; [08] VERIFIED STEPS 4; 5; 6; AND 7
STA 663 VAPOR BARRIER UPPER FWD SIDE ATTACH ANGLE CRACKED AT RBL 10 ; / REMOVED FASTENERS FOR REPAIR IAW B737-700 RM 51-40-02-0G-0 AND 57-10-10-2R-5<BR> REPAIR 5;TRIM DAMABED AREA IAW B737-700 SRM 57-10-10-2R-5; [07] VERIFIED STEP 4 AND 6.ACCOMPLISHED DVI ; NO OTHERS DAMAGE NOTED IAW SRM 57-10-2R-5 STEP 4D. STARTED FABRICATING REPAIR ANGLE AS PER SRM 57-10-10-2R-5-A01754 (REPAIR 5 - WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR - PERMANENT)FABRICATED REPAIR PARTS AT WING CENTER SECTION REAR SPAR AS PER REF..B737-700 SRM 57-10-10-2R-5; [10] VERIFIED 9; [11] OK TO TREAT AND PRIME REPAIR PARTS; [12] TREATED AND REPAIR PARTS AS REQUIRED REFERENCE B737-700 SRM 51-20-01-0G-0 AND SOPM 20-41-02; [13] VERIFIED STEP 12. OK TO INSTALL FABRICATED PARTS; [14] INSTALLED FASTENERS INSIDE FUEL TANK REF B737-700 SRM 57-10-10-2R5; [15] PARTIALLY INSTALLED REPAIR PER SRM 57-10-10-2R-5; [16] APPLIED CAP SEAL TO CENTER FUEL TANK FASTENERS AS PER B737-700 SRM 51-80-01; [17] INSTALLED REPAIR PARTS AS PER B737-700 SRM 51-40-02-0G-0; [18] VERIFIED STEPS 15 AND 16; [19] REMOVED EWIS PROTECTION PER AMM 20-60-07-913-801; [20] COMPLETED REPAIR INSTALLATION RBL 10 SAT 663 VAPOR BARRIER FED ATTACH ANGLE PER SRM 57-10-10-2R-5
STA 663 VAPOR BARRIER UPPER FWD SIDE ATTACH ANGLE CRACKED AT LBL 10 ; / REMOVED FASTENERS LOWER SIDE ANGLE VAPOR STA. 663 LBL 10 AS PER SRM 51-40-02-0G-0; [04] VERIFIED 2 & 3; [05] REMOVED FASTENERS FOR REPAIR IAWB737-700 SRM 51-40-02-0G-0 AND 57-10-10-2R-5 REPAIR 5 TRIM DAMAGED AREA IAW B737-700 SR 57-10-10-2R-5;STARTED FABRICATING REPAIR ANGLE AS PER SRM 57-10-10-2R-5-A01754 (REPAIR 5 - WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR - PERMANENT); [10] FABRICATED REPAIR PARTS AT WING CENTER SECTION REAR SPAR AS PER REF. B737-700 SRM 57-10-10-2R-5; [11] VERIFIED 10; [12] OK TO TREAT AND PRIME REPAIR PARTS; [13] TREATED AND PRIMED REPAIR PARTS AS REQUIRED REFERENCE B737-700 SRM 51-20-01-0G-0 AND SOPM 20-41-02; [14] VERIFIED STEP 13. OK TO INSTALL FABRICATED PARTS; [15] INSTALLED FASTENERS INSIDE FUEL TANK REF. B737-700 SRM 57-10-10-2R5; [16] PARTIALLY INSTALLED REPAIR PER SRM 57-10-10-2R-5; [17] APPLIED CAP SEAL TO CENTER FUEL TANK FASTENERS AS PER B737-700 SRM 51-80-01; [18] INSTALLED REPAIR PARTS AS PER B737-700 SRM 51-40-02-0G-0; [19] VERIFIED STEPS 16 AND 17; [20] REMOVED EWIS PROTECTION PER AMM 20-60-07-913-801; [21] COMPLETED REPAIR INSTALLATION AT LBL 10 STA 663 VAPOR BARRIER FWD ATTACH ANGLE PER SRM 57-10-10-2R-5;
AFT CARGO COMPARTMENT STA 727 TO STA 747 LBL 24 STR 25R Z-CHANNEL SPOTS OF CORROSION ; / [01] REMOVED CORROSION ON AFT CARGO ZEE CHANNEL AT STA 727 THROUGH STA 747 LBL 24 AS PER B737-700 SRM 51-10-02-0G-0.; [02] VERIFIED STEP 1; [03] PERFORMED UT THICKNESS INSP ON REWORKED AREA AFT CARGO COMPT STA 727 - 747 LBL24 Z CHANNEL IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THICKNESS NOTED 0.030'<BR>TOOL USED : MX-3 B/C 17049 CALDUE: 15-JUN-22; [04] ORIGINAL MATERIAL .04'; MATERIAL LOSS .01' MATERIAL REMAINING .03' FOUND OUT OF LIMITS AS PER B737-700 SRM 53-00-53-1A-2 AND BAC 1496-377; [05] PERFORMED LAYOUT AND CUTOUT DMG SECTION OF THE Z-CHANNEL AS PER B737-700 SRM 53-00-53-2R-5 REPAIR 5 AND SRM 51-10-02-0G-0.; [06] LOCATED AND DRILLED NEW Z-CHANNEL SECTION AND SPLICE AS PER B737-700 SRM 51-40-05-0G-0 AND SRM 53-00-53-2R-5 REPAIR 5 FIG 202.; [07] VERIFIED STEPS 4/5/6.<BR>OK TO TREAT/PRIME; [08] TREATED AND PRIMED REPAIR PARTS AND NEW Z-CHANNEL AS PER B737-700 AMM 51-21-72-370-804 AND AMM 51-21-41-370-803.; [09] VERIFIED STEP 8; [10] OK TO INSTALL REPAIR SPLICE; [11] REPAIR SPLICE AND NEW Z-CHANNEL INSTALLED AS PER B737-700 SRM 53-00-53-2R-5; [12] VERIFIED ZEE CHANNEL SPLICE REPAIR ON STEP 11. TASK COMPLETE.
EXIT SIGN AT FWD L1 BASE IS CRACKED ; / [01] REMOVED AND REPLACED EXIT SIGN AT FWD L1 AS PER B737-700 AMM 33-51-01-960-802.; [02] PARTS VERIFIED; [03] VERIFIED 1 & 2
EXIT SIGN AT FWD GALLEY G1 BASE IS CRACKED ; / [01] REMOVED AND REPLACED EXIT SIGN AT FWD GALLEY G1 AS PER B737-700 AMM 33-51-01-960-802; [02] VERIFIED
EXIT SIGN AT AFT GALLEY 4 BASE IS CRACKED ; / [01] REMOVED AND REPLACED EXIT SIGN AT AFT GALLEY 4 AS PER B737-700 AMM 33-51-01-960-802.; [02] VERIFIED
FWD CARGO GUSSET AT STA 500D AND S-19R INNER CURVATURE CRACKED ; / [01] REMIOVED GUSSET FROM FWD CARGO AS PER SRM 51-40-02; [02] LOCATED AND DRILLED NEW GUSSET PER SRM 51-40-05-OG-0; [03] VERIFIED 1 & 2; [04] OK TO INSTALL NEW GUSSET; [05] INSTALLED GUSSET PER SRM 51-40-02-0G-0; [06] VERIFIED 5
FWD CARGO COMPARTMENT CLIP CRACKED AT STA 400 AND S-25L (UNDER ZEE ANGLE) ; / [01] REMOVED CLIP AND INTERCOSTAL CRACKER AT FWD. CARGO COMPARTMENT STA. 400 TO STA. 420 AND S-25L IAW B-737-700 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW BAFFLE AND CLIP PER SRM 51-40-05-0G-0; [03] VERIFIED 1 & 2. OK TO INSTALL NEW BAFFLE; [04] INSTALLED NEW BAFFLE AND CLIP PER SRM 51-40-02-0G-0; [05] VERIFIED 4
FWD CARGO GUSSET AT STA 500D AND S-19L INNER CURVATURE CRACKED ; / [01] REMOVED GUSSET AT STA. 500D AND S-19L FWD CARGO AS PER SRM 51-40-02-0G-0; [02] LOCATED AND DRILL NEW GUSSET AS PER SRM 51-40-05-0G-0; [03] OK TO INSTALL NEW GUSSET; [04] INSTALLED FWD CARGO NEW GUSSET AT STA 500D AND S-19L LINER; AS PER REF B737-700 SRM 51-40-02-0G-0.; [05] VERIFIED 4
FWD CARGO COMPARTMENT CLIP CRACKED AT STA 400 AND S-25L (UNDER ZEE ANGLE) ; / [01] REMOVED CLIP AND INTERCOSTAL CRACKER AT FWD. CARGO COMPARTMENT STA. 400 TO STA. 420 AND S-25L IAW B-737-700 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW BAFFLE AND CLIP PER SRM 51-40-05-0G-0; [03] VERIFIED 1 & 2. OK TO INSTALL NEW BAFFLE; [04] INSTALLED NEW BAFFLE AND CLIP PER SRM 51-40-02-0G-0; [05] VERIFIED 4
INSPAR RIB ASSY 4 (STAB STA 120.30); STIFFENER 2 CRACKED ; / [01] PERFORMED HFEC INSP. ON INSPAR RIB ASSY 4 (STAB STA 120.30) STIFFENER 2 IAW B737 NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED. EQUIP: NORTEC 600 B/C 166317 CAL DUE: 10/21; [02] PERFORMED LAYOUT AND CUTOUT DMG ON VERTICAL STIFFENER 2 AS PER B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIG 202.; [03] VERIFIED STEP 2; [04] PERFORMED HFEC INSP ON CUT OUT AREA IAW B737 NDT P6 51-00-00 PROC.23 ; NO CRACKS<BR>TOOL USED : NORTEC 600 B/C 172389; [05] ACCOMPLISHED GVI OF ALL AREAS WITHIN THE REPAIR; NO DISCREPANCIES NOTED. REF B737-700 SRM 55-10-09-2R-4 STEP 4.E; [06] LOCATED AND DRILLED NO.4 RIB AND REPAIR PARTS AS PER SRM 55-10-09-2R-4 REPAIR 4 FIG 202 AND SRM 51-40-05-0G-0.; [07] VERIFIED STEP 6; OK TO TREAT AND PRIME; [08] ACCOMPLISHED TREAT AND PRIME OF REPAIR PARTS PER B737-700 AMM 51-20-01 AND SOPM 20-41-02.; [09] VERIFIED STEP 8; AND OK TO INSTALL REPAIR PARTS; [10] MIXED SEALANT BMS 5-95 AT 19:00 09-10-2021; SQUEEZE OUT AND FASTENER INSTALLATION VERFICATION DUE BY 21:00 09-10-2021.; [11] INSTALLED REPAIR PARTS AS PER B737-700 SRM 51-40-02-0G-0; SRM 55-10-09-2R-4 REPAIR 4 FIG 202 AND DWG NO. 55100003 REV B; [12] SEALANT SQUEEZE OUT VERIFICATION AND 100% PERMANENT FASTENER INSTALLATION ACCOMPLISHED PRIOR TO SQUEEZE OUT LIFE PER SOPM 20-50-19; [13] VERIFIED STEPS 10; 11; AND 12; [14] APPLIED FILLET SEAL TO REPAIR PARTS AS PER B737-700 AMM 51-31-00-390-804.; [15] VERIFIED STEP 14
INSPAR RIB ASSY 4 (STAB STA 120.30); STIFFENER 3 CRACKED ; / [01] PERFORMED HFEC INSP. ON INSPAR RIB ASSY 4 (STAB. STA 120.30) STIFFENER 3 IAW B737 NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED. EQUIP: NORTEC 600 CAL DUE: 10/21 B/C 166317; [02] PERFORMED LAYOUT AND TRIMMED OUT DMG ON VERTICAL STIFFENER 3 AS PER B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIG 202.; [03] VERIFIED STEP 2; [04] PERFORMED HFEC INSP ON CUT OUT AREA IAW B737 NDT P6 51-00-00 PROC.23 ; NO CRACKS<BR>TOOL USED : NORTEC 600 B/C 172389; [05] ACCOMPLISHED GVI OF ALL AREAS WITHIN THE REPAIR; NO DISCREPANCIES NOTED. REF B737-700 SRM 55-10-09-2R-4 STEP 4.E; [06] LOCATED AND DRILLED NO.4 RIB AND REPAIR PARTS AS PER SRM 55-10-09-2R-4 REPAIR 4 FIG 202 AND SRM 51-40-05-0G-0.; [07] VERIFIED STEP 1; OK TREAT AND PRIME; [08] ACCOMPLISHED TREAT AND PRIME OF REPAIR PARTS PER B737-700 AMM 51-20-01 AND SOPM 20-41-02.; [09] VERIFIED STEP 8; AND OK TO INSTALL REPAIR PARTS; [10] MIXED SEALANT BMS 5-95 AT 19:00 09-10-2021; SQUEEZE OUT AND FASTENER INSTALLATION VERFICATION DUE BY 21:00 09-10-2021.; [11] INSTALLED REPAIR PARTS AS PER B737-700 SRM 51-40-02-0G-0; SRM 55-10-09-2R-4 REPAIR 4 FIG 202 AND DWG NO. 55100003 REV B; [12] SEALANT SQUEEZE OUT VERIFICATION AND 100% PERMANENT FASTENER INSTALLATION ACCOMPLISHED PRIOR TO SQUEEZE OUT LIFE PER SOPM 20-50-19; [13] VERIFIED STEPS 10; 11; 12; [14] APPLIED FILLET SEAL TO REPAIR PARTS AS PER B737-700 AMM 51-31-00-390-804.; [15] VERIFIED STEP 14
EMERGENCY LIGHT BATTERY'S FAILED CAPACITY CHECK AT LOCATIONS M1669; M1672; M1673; M1675; M1668 / REMOVED AND REPLACED EMERGENCY LIGHT BATTERY'S AT LOCATIONS M1669; M1672; M1673; M1675; M1668 PER AMM. 33-51-06 REFERENCING DWG-33500005
CABIN RT OVER WING EXIT LIGHT INOPERABLE UNDER SIGN. R & R CABIN RT OVER WING EXIT LIGHT BALLAST, PER MM 33-21-00.
FWD CABIN FWD SERVICE DOOR ESCAPE SLIDE COVER FWD GIRT BAR HANGER LOOSE (SHEARED RIVET) / REMOVED AND REPLACED RIVET IAW SRM 51-40-02
DURING DESCENT FLIGHT ATTENDANTS AND PASSENGERS REPORTED BURNING SMELL IN AFT CABIN/GALLEY AREA. LASTED APPROXIMATELY 5 MINUTES, THEN WENT AWAY. FOUND BULB NOT SECURED IN LIGHT ASSEMBLY. CORRECTLY SECURED BULB PER AMM.
AFT CARGO COMPARTMENT R/H MIDDLE FLOOR TO SIDEWALL CAP STRIP SHOWS SIGNS OF CORROSION. / R&R'D R/H MIDDLE FLOOR SIDEWALL CAP STRIP PER AMM 25-52-06.
AFT RIGHT CAP STRIP IN AFT CARGO PIT IS CORRODED BEYOND LIMITS. / REMOVED AND REPLACED RIGHT AFT CAP STRIP IAW SRM 51-10-02.
AFT CARGO COMPARTMENT L/H AFT FLOOR TO SIDEWALL CAP STRIP SHOWS SIGNS OF CORROSION. / R&R'D L/H AFT FLOOR SIDEWALL CAP STRIP PER AMM 25-52-06.
AFT CARGO COMPARTMENT L/H MIDDLE FLOOR TO SIDEWALL CAP STRIP SHOWS SIGNS OF CORROSION. / R&R'D L/H MIDDLE FLOOR SIDEWALL CAP STRIP PER AMM 25-52-06.
AFT CARGO FWD R/H FLOOR TO SIDEWALL CAP STRIP SHOWS SIGNS OF CORROSION. / R&R'D R/H FLOOR TO SIDEWALL CAP STRIP PER AMM 25-52-06.
AFT CARGO COMPARTMENT FWD L/H FLOOR TO SIDEWALL CAP STRIP SHOWS SIGNS OF CORROSION. / R&R'D L/H FWD FLOOR SIDEWALL CAP STRIP PER AMM 25-52-06.
LT WING #7 HOLE ON VERTICAL ROW FROM TOP INBOARD OF PYLON CRACKED IN THE HORIZONTAL STIFFENER. REPAIRED STRINGER PER SRM.
SUPPORT CHANNEL (1)141A5211 UNDER FLIGHT DECK FLOORBOARD 211AF HAS SEVERAL SURFACE CORRODED AREAS. / REMOVED AND REPLACED SUPPORT CHANNEL 141A5211-1 IAW SRM 51-40-02 AND EA#1-753-35563.
FLOOR SUPPORT CORRODED AT BS 270, BL 0 SEVERAL AREAS. (ENTRY TO THE FLIGHT DECK) REPAIRED FLOOR SUPPORT PER EA.
#1 ENG. I/B T/R SLEEVE; KRUGER FLAP AFT DEFLECTOR FAIRING CRACKED. / REMOVED AND REPLACED FAIRING PER REF SRM51-40-02. SEE TASKS FOR ADDITIONAL SIGN OFFS.
L/H WING OUTBOARD TRAILING EDGE FLAP HAS SMALL AREA OF DELAM ON INBOARD AFT CORNER. / REMOVED DAMAGE AND ACCOMPLISHED REPAIR TO FLAP REF SRM 57-53-01-2R-4. RESTORED FINISH TO AREA REF AMM 51-21-99.
#1 SEAT TRACK CORRODED IN CHANNEL AT BS 727A+11. R&R SEAT TRACK PER SRM.
RIGHT WING PANEL 621LB HAS CORNER DELAMINATION. / REPAIRED PER SRM 51-70-04.
LT WING WIGGLE PLATE CRACKED AT RSS 273. R&R WIGGLE PLATE PER SRM.
AIR RETURN/EMERGENCY DECLARED, L1 COCKPIT WINDOW PANE ARCED AND CRACKED. R&R L1 WINDOW ASSY PER MM.
R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
L1 DOOR EMERGENCY EVAC SLIDE LT RETENTION CLIP LOOSE. R&R GIRT BAR CLIP ASSEMBLY IAW SRM.
DIVERSION, DURING CLIMB ENGINE 1 A HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. COMPLIED WITH QRH A QUANTITY DROPPED TO 35%. R&R NR 1 EDMP PER MM.
LT EMERGENCY EXIT LIGHT INOP BETWEEN ROW 9 TO ROW 12. R&R BATTERY PACK IAW AMM.
EMERGENCY LIGHTS BATTERY PACK M1670 INOP. R&R BATTERY PACK IAW MM.
FWD CARGO COMP FWD CORNER SCUFF PLATE CRACKED / SCUFF PLATE FWD OF FWD CARGO WAS REPAIRED IN THE BACK SHOP W/O 36297-8100-0001 P/N 143A8333-1 E.A 1-A53-2076 REV: 11
FORWARD LAV EMERGENCY LIGHT BROKEN. R&R LIGHT IAW AMM.
PASSENGER CABIN SIDEWALL 232YHW EMERGENCY EXIT SIGN HOUSING DAMAGED. R&R SIGN HOUSING IAW AMM.
RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT HSS 95.96. R & R THE RIB IAW SRM AND DWG.
RT HORIZONTAL STABILIZER AFT VERTICAL STIFFENER CRACKED AT STAB STATION 129.50, FORWARD OF AFT SPAR. REPAIRED STIFFENER IAW SRM.
RT HORIZONTAL STABILIZER 3RD VERTICAL STIFFENER CRACKED AT STAB STATION 92.70, AFT OF FRONT SPAR. REPAIRED STIFFENER IAW SRM.
RT HORIZONTAL STABILIZER 2ND VERTICAL STIFFENER CRACKED AT STAB STATION 92.70, AFT OF FRONT SPAR. REPAIRED STIFFENER IAW SRM.
RT HORIZONTAL STABILIZER 1ST VERTICAL STIFFENER CRACKED AT STAB STATION 92.70 AFT OF FRONT SPAR. REPAIRED STIFFENER IAW SRM.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.70, 10 INCHES AFT OF FRONT SPAR. REPAIRED THE RIB IAW SRM.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.70, 20 INCHES AFT OF FRONT SPAR. REPAIRED RIB IAW SRM.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.70, 26 INCHES AFT OF FRONT SPAR. REPAIRED THE RIB IAW SRM.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.70, 38 INCHES AFT OF THE FRONT SPAR. REPAIRED THE RIB IAW SRM.
LT SIDE OUTER FUSELAGE SUPPORT STRUCTURE FOR WING TO BODY ACCESS PANEL FAIRINGS 191AL AND 195AL SUPPORT BRACKET CRACKED AT BS 500D, BETWEEN STR 18L TO STR 19L. R&R BRACKET IAW SRM & DWG.
FLOORBEAM CORRODED AT BS 328, BETWEEN BL 0 TO RBL 64. REPAIRED T-CHORD PER SRM.
SUPPLEMENTAL INFORMATION: PASS CABIN FLOOR; 3 CRACKS AT FASTENER HOLES ON UPPE R FLANGE OF INTERCOSTAL BETWEEN BS 5OOD AND BS 520. AT BL0. / REMOVED; LOCATED AND CRILLED AND INSTALLED NEW ANLGE AT PASS CABIN FLOOR STA: 500D AND 520 BL-O; AND APP LIED CIC AREA IAW B737-700 SRM 51-40-02-0G-0; SRM 51 -40-05-0G-0; AMM 51-00-59.201 DWG: 143A5400 REV D. T AG: A09419
PASSENGER CABIN INTERCOSTAL CRACKED AT STA 328-12' RBL 31. / REMOVED CRACKED INTERCOSTAL AT STA 328-12'; DRILLED AND INSTALLED NEW NACHINED INTERCOSTAL I/A/W BOEING DRAWING 141A5410; REVA AND B737 SRM 51-40-02; PARA 7.D. INSTALLED 2 EA NUTPLATES FOR FLOORBOARD ATTACH I/A/W B737 SOPM 20-50-12.
CABIN FLOORBOARD 221 DF HAS TOP PLY DE-LAM (MISSING FIBER STRANDS) / REPAIRED FRAYED FIBERS IAW SRM 53-00-50-2R-11
SUPPLEMENTAL INFORMATION: RUDDER BALANCE ARM WEIGHT IS CORRODED. / REMOVED AND INSTALLED NEW RUDDER BALANCE ARM WEIGHT IAW BOEING CMM CHAPTER 55-40-09 STEP (3) WEIGHT WN49 06
PASSENGER CABIN FLOOR BOARD 221FF TOP LAYER DELAMED / REPAIRED FRAYED TOP LAYER ON PANEL 221FF IAW SRM 53-00-50-2R-11 REPAIR 11 A83844
PASSENGER CABIN FLOOR BOARD 221CF TOP LAYER DELAMED / REPAIRED TOP LAYER ON FLOOR PANEL 221CF IAW SRM 53-00-50-2R-11 REPAIRIII
PASSENGER CABIN FLOOR BOARD 221BF TOP LAYER DELAMED / REPAIR CABIN FLOORBOARD 221BF TOP LAYER IAWSRM53-00-50 REPAIR 11; PG 1.
LT AFT CREASE BEAM CORRODED BETWEEN BS 947 TO BS 987. R&R CREASE BEAM IAW SRM AND DWG.
PASSENGER CABIN FLOOR BOARD 221EF TOP LAYER DELAMED / REPAIRED UPPER FACE SHEET ON FLOORBOARD 221EF IAW SRM 53-00-50
FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 38 TO RBL 48. REPAIRED FLOOR BEAM IAW SRM AND EA.
PASSENGER CABIN FLOOR BOARD 221GF TOP LAYER DELAMED / REPAIRED TOP LAYERS ON FLOORPANEL 221GF IAW SRM 53- 00-50-2R-11 REPAIR 11
FUSELAGE LOWER LOBE KEEL BEAM SUPPORT BRACKET CRACKED AT BS 546, LBL 5. R&R BRACKET IAW SRM.
RUDDER BALANCE ARM WEIGHT IS CORRODED. / REMOVED AND INSTALLED NEW RUDDER BALANCE ARM WEIGHT IAW BOEING CMM CHAPTER 55-40-09 STEP (3) WEIGHT WN49 06
AFT GALLEY DOOR CREASE BEAM CORRODED ON UPPER AND LOWER SURFACE. R&R CREASE BEAM IAW DWG AND SRM.
FWD CARGO COMPARTMENT BETWEEN STA 500B AND 500C HAS A CRACKED BAFFLE / REMOVED; LOVACTED; DRILLED AND INSTALLED NEW BAFFLE IN FORWARD CARGO PIT BETWEEN STA 500B AND 500C ON L/H SIDE UNDER '2' MEMBER;IAW BOEING 737 SRM 51-40-02-0G-0 STEP 4B; 51-40-05-0G-0 FIG 3 SHEET 1 ; AND BOEING DRAWING 143A7505 SHEET 5 REVISION B
A/C RAM INLET PANEL 191BR DELAMINATED / REPAIRED 191BR DELAM IAW B737 SRM 51-20-04-2R-1 REV 62
AFT CARGO FLOORBEAM ANGLE CORRODED AT BS 772, RBL 7. REPAIRED THE FLOORBEAM IAW EA & SRM.
FORWARD CARGO BAY BAFFLE ANGLE CRACKED AT BS 500C, LBL 25. R & R THE ANGLE IAW SRM AND DWG.
AFT CARGO PIT STA 887; LATERAL FLOOR SUPPORT STRAP H AS CORROSION. / REMOVED AND REPLACED THE AFT PIT STA 887 FLOOR SUPPO RT STRAP IAW B737-700 SRM 51-40-02-0G-0; STEP 7 AND DWG# 146A7500; REV.A.
AFT PIT STA 772; LATERAL FLOOR PANEL SUPPORT STRAP/STRIP; HAS CORROSION ON UPPER AND LOWER SURFACES. / EVALUATED CORROSION PER B737-700 SRM 53-00-53. ORIGINAL THICKNESS= .070'. 100% MATERIAL LOSS NOTED.PART OUT OF LIMITS PER B737-700 SRM 53-00-53-1A-2 PARA 4A DETAIL D. CORRODED STRAP REPLACED WITH NEW STRAP PN:146A9401-4 ATAG WN4832. STRAP TO BE INSTALLED WITH FLOORPANEL ON ROUTINE JPANEL-141- CLOSE.
AFT PIT RH Z ANGLE BETWEEN STA 727E AND 767 HAS CORROSION. / BLENDED OUT DAMAGE-ORIG MAT'L: .040'; MAT'L REMOVED: .012'; MAT'L REMAINING: .028'. BLENDOUT IS OUT OF LIMITS I/A/W B737 ARM 53-00-53-1A-2. REMOVED DAMAGED Z-ANGLE IN AFT PIT; R/H STA 727 TO STA 737; LOCATED AND DRILLED NEW Z-ANGLE AND SPLICE; ALODINED AND PRIMED AND INSTALLED NEW Z-ANGLE I/A/W SRM 53-00-53-2R-5; REPAIR 5. CIC APPLIED I/A/W SRM 51-10-02.
AFT PIT FLOOR SUPPORT ANGLE CORRODED AT BS 772, LBL 12. R&R CHANNEL PER SRM AND EA.
AFT PIT FLOOR SUPPORT CORRODED ANGLE AT BS 772, RBL 13. REPAIRED ANGLE IAW SRM AND EA.
AFT PIT FLOOR SUPPORT ANGLE CORRODED AT BS 772, LBL 8. R&R CHANNEL PER EA.
AFT PIT STA 772 AT FLOOR SUPPORT ANGLE CORRODED AT BS 772, LBL 3. R&R ANGLE IAW SRM.
AFT PIT FLOOR SUPPORT ANGLE CORRODED AT BS 772, RBL 2. REPAIRED ANGLE IAW SRM.
SUPPLEMENTAL INFORMATION: AFT PIT TIE DOWN TRACK/FLOOR SUPPORT ANGLE; FROM STA 786 TO 867 RH SIDE; HAS MULTIPLE AREAS OF CORROSION. / EVALUATED CORROSION DEEPEST BLEND .022' FROM ORIGINAL .070' WITH .098' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED CARGO TRACK STA 779 TO 887 RBL 14. SI#7530360 IAW SRM 53-00-53-2 REPAIR 3 AND EA 1-A53-8210 REV 2
FUSELAGE LOWER LOBE KEEL BEAM STA 546 RBL 5 SUPPORT BRACKET FOR LOWER LOBE ACCESS PNL# 192 E IS BROKEN AS MARKED / REMOVED AND REPLACED SUPPORT BRACKET AT STA 546 5 IAW SRM 51-40-05; SRM 51-40-02-0G-0; AND SRM 51-40-0G-0
LH WING FIXED TRAILING EDGE PANEL HAS CRACKED SEAL RETAINER BRACKET 11' INBD OF DEFLECTOR RIB. MARKED. / REMOVED CRACKED SEAL RETAINER BRACKET ON L/H WING FIXED TRAILING EDGE PANEL; 11' INBD OF DEFECTER RIB I/A/W SRM 51-40-02. LOCATED AND DRILLED FASTNER HOLES AND INSTALLED SEAL RETAINER ONTO NEW BRACKET I/A/W SRM 51-40-02. INSTALLED BRACKET ONTO L/H WING FIXED TRAILING EDGE PANEL I/A/W SRM 51-40-02; PARA 7.
LT WING WIGGLE PLATE CRACKED AT SHEARED FASTENER UNDER 551 GB. R&R PLATE ASSEMBLY PER SRM.
R/H SIDE OUTER FUSELAGE SUPPORT STRUCTURE FOR WING TO BODY ACCESS PNL FAIRINGS 191AR AND 195AR STA 500D BETWEEN STR 18R AND 19R SUPPORT BRACKET IS CRACKED AS MARKED / REMOVED RH OUTER FUSELAGE SUPPORT STRUCTURE (FROME) IAW B737-700 SRM 51-40-02; VERIFIED FRAME P/N 116A3118-10 ATAG QR1241 IAW BOEING DWG#116A3110. LOCATED & DRILLED NEW FRAME IAW B737-700 SRM 51-40-05 & BOEING DWG# 116A3010 REV A. INSTALLED NEW FRAME P/N 116A3118-10 IAW BOEING DWG# 116A3010 REV A & 149A7101 AND APPLIED C.I.C IAW B737-700 AMM 51-21-91-620-802
LEFT WING LWR LE PNL 521TB IS DELAMINATED AT CORNER. MARKED. / REPAIRED LEFT WING LOWER PANEL 321TB IAW B737-700 SRM 51-70-08-0G-0 PARA 3 RESTORED IAW B737 AMM 51-21-99-300-801 PARA E (6) TABLE 701 REV 63
FWD CARGO BAFFLE CLIP CRACKED AT BS 500C RBL 25' MARKED / REMOVED AND REPLACED BAFFLE CLIP BS500C RBL25 PER B737-700 SRM 51-40-02 PARA B; SRM 51-40-05 FIG 3 TABLE A; AND BOEING DRW #143A7505 SH 5 REV B.
FORWARD CARGO BULKHEAD SUPPORT GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET PER SRM AND DWG.
AFT CARGO COMPARTMENT DOOR AFT SURROUND CORNER RETAINER IS CORRODED. / EVALUATED CORROSION ON AFT CARGO; AFT SURROUND CORNER. FOUND 100% MATERIAL LOSS. REMOVED AND REPLACED REVEAL RETAINER ON SHELF I/A/W S/W 53-00-53-1A-1
AFT CARGO COMPARTMENT DOOR FWD SURROUND CORNER RETAINER IS CORRODED. / REMOVED AND REPLACED AFT CARGO DOOR FWD SURROUND PLATE IAW B737 DRAWING 453A2611 REV C AND IPC 25-52-10-02 P/N 453A2611-1 ATAG A02753
FORWARD CARGO BULKHEAD SUPPORT GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM.
LEFT WING LWR LE PNL 521DB IS DELAMINATED AT 2 CORNERS. MARKED. / REPAIRED LEFT WING LOWER L/E PANEL #521DB IAW B737-700 SRM 51-70-080G-0 PARA 3 REV 62; RESTORED FINISH IAW B737 AMM 51-21-99-300-801 PARA E (6) TABLE REV 63
FORWARD CARGO BAFFLE ANGLE CRACKED AT BS 500C, LBL 25. R & R THE ANGLE IAW SRM AND DWG.
SWA PRODUCTION REP. GENERATED. C2 CENTER THRESHOLD CRACKED FWD END. / REPAIRED C2 CENTER THRESHOLD FOD END I.A.W EA# 1-A53-2076 REV 11
L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER AMM & MT.
RT WING-FIXED UPPER TRAILING EDGE PANEL (BETWEEN INBOARD GROUND SPOILER CUTOUT AND FLIGHT SPOILER PANEL CUTOUT) HAS AFT WEB SEAL ASSY BRACKET CRACKED AT FASTENER HOLE. / REMOVED AND REPLACED AFT WEB SEAL BRACKET ASSY PER SRM 51-40-02.
R1 DOOR CRACKED AT THE RADIUS OF THE VERTICAL INBOARD FLANGE OF NR 4 FRAME. R&R DOOR AS PER AMM.
LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.
L1 LOWER EXIT SIGN MISSING DIRECTIONAL ARROWS. R&R SIGN IAW AMM.
R1 LOWER EXIT SIGN MISSING DIRECTIONAL ARROWS. R & R THE SIGN IAW AMM.
FORWARD UPPER EMERGENCY FLASHLIGHT TAMPER STRAP BROKEN. R & R THE STRAP IAW SIP.
R2 DOOR EMERGENCY EXIT SIGN BROKEN. R & R THE SIGN IAW MM.
R1 DOOR GIRT BAR LOOSE. SECURED GIRT BAR SKIRT IAW SIP.
RIGHT AFT EMER LIGHTS BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW MM.
LEFT CTR EMER LIGHTS BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW MM.
FLIGHT DECK LT NR 1 WINDOW FRAME CRACKED AFT UPPER CORNER. REPAIRED FRAME IAW ACO.
MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB IAW SRM.
MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 33. REPAIRED WEB IAW SRM.
MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 33. REPAIRED WEB IAW SRM.
MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 43. REPAIRED WEB IAW SRM.
MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 33. REPAIRED WEB IAW SRM.
RIGHT AFT GALLEY M1675 EMER BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.
RIGHT FWD GALLEY M1673 EMER BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.
INTERCOSTAL CRACKED BETWEEN STATION 312 TO STATION 294.5, RBL 15. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED BETWEEN STATION 312 TO STATION 294.5, RBL 15. R & R INTERCOSTAL IAW SRM.
RT SKIN PANEL FWD ROW 2ND HOLE FROM TOP CRACKED AT STATION 540, BETWEEN STRINGER 22R TO STRINGER 23R. REPAIRED SKIN IAW ACO & EA.
SKIN PANEL FWD ROW, BOTTOM HOLE CRACKED AT STATION 540, BETWEEN STRINGER 22L TO STRINGER 23L. REPAIRED SKIN IAW ACO & EA.
RT SKIN PANEL FWD ROW, MOST UPPER HOLE CRACKED AT STATION 540, BETWEEN STRINGER 22R TO STRINGER 23R. REPAIRED SKIN IAW EA.
SKIN PANEL FWD ROW, 2ND HOLE FROM TOP CRACKED AT STATION 540, BETWEEN STRINGER 22L TO STRINGER 23L. REPAIRED SKIN IAW ACO & EA.
SEAT TRACK CRACKED AT STATION 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.
INTERCOSTAL CRACKED AT STATION 335, LBL 45. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED BETWEEN STATION 344 TO STATION 360 LBL 11. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED AT STATION 284, 0 BL. R & R INTERCOSTAL IAW SRM.
AFT CARGO FLOOR SUPPORT CORRODED BETWEEN STATION 793 TO STATION 818, RBL 15. R & R TRACK IAW EA & SRM.
AFT CARGO DOOR THRESHOLD WEB CORRODED BETWEEN STATION 800 TO STATION 847. R & R WEB IAW SRM.
SEAT TRACK FASTENER HOLES CRACKED AT STATION 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.
SEAT TRACK FASTENER HOLES CRACKED AT STATION 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.
SEAT TRACK FASTENER HOLES CRACKED AT STATION 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.
SEAT TRACK FASTENER HOLES CRACKED AT STATION 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.
INTERCOSTAL CRACKED BETWEEN STATION 344 TO STATION 360, BL 0. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED AT STATION 320, LBL 45. R & R INTERCOSTAL IAW SRM.
NR 3 LT WINDOW FRAME CRACKED AT 3 O'CLOCK POSITION, NR 2 HOLE FROM BOTTOM. REPAIRED FRAME IAW ACO.
NR 3 RT WINDOW FRAME CRACKED AT 9 O'CLOCK POSITION, NR 2 HOLE FROM BOTTOM. REPAIRED FRAME IAW ACO.
LT HORIZONTAL STABILIZER LOWER SKIN PANEL CRACKED AT STATION 97.4, 1.75' FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.
RT HORIZONTAL STABILIZER LOWER SKIN PANEL CRACKED AT STATION 147.9, INBD SIDE OF RIB 17" FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.
FWD UPPER EMERGENCY FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.
R2 AFT SERVICE DOOR SLIDE GIRT FOLD TOO LONG. ADJUSTED SLIDE GIRT FOLD AS REQUIRED PER AMM.
EMERGENCY EXIT LIGHT CRACKED AT ROW 11. REMOVED AND REPLACED LIGHT PER AMM.
LEFT EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
RIGHT EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 772, LBL 12. REPAIRED BEAM IAW EA.
DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 772, LBL 8. REPAIRED BEAM IAW EA.
DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 772, LBL 3. REPAIRED BEAM IAW EA.
DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BS 772, RBL 2. REPAIRED BEAM IAW EA.
DURING SCHEDULED MV1 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM.
DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 20 TO ROW 21. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY EXIT LIGHT COVER BROKEN BETWEEN ROW 10 TO ROW 21. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.
DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY EXIT LIGHT COVER BROKEN BETWEEN ROW 1 TO ROW 10. REMOVED AND REPLACED COVER PER MM.
EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.
DURING GO-AROUND NOSE LANDING GEAR RED LIGHT REMAINED WITH GEAR HANDLE UP. NOSE GEAR FREE FELL TO GREEN INDICATION (RED LIGHT STILL ON) WITH GEAR HANDLE OFF RECYCLED GEAR DOWN-UP-OFF TO SAME INDICATION. LANDED WITH 3 GREEN, NO RED. REMOVED AND REPLACED SCHRADER VALVE PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK COVERS CRACKED BETWEEN ROW 15 TO ROW 23. REMOVED AND REPLACED COVERS PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK COVERS CRACKED BETWEEN ROW 1 TO ROW 11. REMOVED AND REPLACED COVERS PER MM.
DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM.
DURING SCHEDULED MV3 CHECK, FOUND FWD EEPLS LENS MISSING. INSTALLED LENS PER MM.
EEPLS LOOSE AT ROW 6. SECURED EEPLS PER MM.
FOUND R1 EMERGENCY EXIT DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.
DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
DURING SCHEDULED HC2 CHECK, LT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.
EEPLS LENS LOOSE AT ROW 1 ABC. INSTALLED LENS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 4 ABC. INSTALLED LENS PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 3 ABC. FOUND BROKEN WIRE. REPAIRED WIRE PER MM.
EEPLS LENS CRACKED AT ROW 3 ABC. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED MV1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 9 ABC AND ROW 11 ABC. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED MV2 CHECK, FOUND RIGHT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM.
FOUND EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM.
EEPLS END CAP LOOSE AT LEFT FWD CABIN. SECURED END CAP PER MM.
EEPLS LIGHT COVER LOOSE AT ROW 1 ABC. SECURED LIGHT COVER PER MM.
EEPLS LIGHT LENS LOOSE AT ROW 1 ABC. SECURED LIGHT LENS PER MM.
EEPLS COVER LOOSE AT ROW 1 ABC. SECURED EEPLS COVER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 12 ABC. INSTALLED EEPLS COVER PER MM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.