N915WN
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 | 2012-02-23 – 2012-02-23 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2012-02-23 – 2012-02-23 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
EMERGENCY EXIT LIGHTS IN THE CABIN ARE INOPERATIVE DURING NIGHT MODE. REPLACED THE LAMPS IN THE NIGHT LIGHT AT BS 727E+10 IAW AMM 33-22-00. EMERGENCY EXIT LIGHTS OPS NORMAL IAW AMM 33-51-00.
RT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL HAS VERTICAL CRACKS PARALLEL TO BOTH THE FORWARD AND AFT EDGES. REMOVED AND REPLACED THE STABILIZER TO BODY UPPER FRONT R/H SLIDING SEAL PER AMM 53-31-31.
L/H HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL HAS VERTICAL CRACKS PARALLEL TO BOTH THE FORWARD AND AFT EDGES. REMOVED AND REPLACED L/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL PER AMM 53-31-31.
FWD FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS TEST PASS.
LEFT EMERGENCY EXIT LATCH; EMERGENCY EXIT LIGHT BURNED OUT. REPLACED EMERGENCY EXIT LIGHT, LT EMERGENCY EXIT LATCH IAW AMM 33-51-04-960-801 STEP 2.F.(1)(2)(3)(A)(B)(D).
INOPERATIVE EXTERNAL EMERGENCY LIGHT AFT SERVICE DOOR AT UPPER FUSELAGE. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-04-960-801, STEP 2.F. 1, 2, 3, A, B, D, 4. TESTED OK.
CRACK SUPPORT ZEE LOCATED BETWEEN BS 727D - 727E, S25L, WL 156. REPLACED SUPPORT ZEE IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 146A7500 SHEET 113 REV- DWG 146A7502 SHEET 27 REV-.
CRACK CARGO TRACK RBBL 13.84, BS 767 IN THE AFT CARGO COMPARTMENT. REPAIRED THE CARGO TRACK SECTION BS 727D - 787 IAW SRM 53-00-53-2R-3, REPAIR 3, ALTERNATIVE 1 AND ALTERNATIVE 2.
CRACK ANGLE LOCATED BS 867, LBL 10 IN THE AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BS 867, LBL 10 IAW SRM 51-10-02, ITEM 9, AND INSTALLED FASTENERS IAW SRM 51-40-02, AND DRAWING 149A8102, SHEET 17, REV-. MEASUREMENT OF CRACK IS 0.550 INCH.
CORROSION SUPPORT ZEE BETWEEN BS 727 - 767, S25R, WL 156. REPLACED THE SUPPORT ZEE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 146A7500, SHEET 113, REV-, AND DWG 146A7502, SHEET 49, REV-.
CORROSION SUPPORT ZEE BETWEEN BS 727 - 767, S25R, WL 156. REPLACED SUPPORT ZEE AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 146A7500, SHEET 113, REV-, AND DWG 146A7502, SHEET 49, REV-.
CRACK WEB CEILING AREA, BS 847 TO 867, LBL 19, AFT CARGO BAY. REPLACED WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 149A8100, SHEET 1 REV -.
CORROSION SHIELD WEB FLOOR STRUCTURE BS 767 TO 794.5, S25R, WL156, AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS IAW SRM 51-10-02, ITEM 9, AND INSTALLED FASTENERS IAW SRM 51-40-02, AND DRAWING 146A0081, SHEET 37, REV -.
CRACKED SUPPORT BRACKET, BS 947.5, LBL 10 IN THE AFT CARGO COMPARTMENT. REPLACED SUPPORT BRACKET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 149A8103, SHEET 7, REV A.
CRACK CARGO TRACK RBBL 13.84 FRAME 747 AFT CARGO COMPARTMENT. REPAIRED CARGO TRACK RBL 13.84 BTW SECTION BS 727D - 787 IAW SRM 53-00-53-2R-3, REPAIR 3, ALTERNATIVE 1, AND ALTERNATIVE 2.
CRACK CARGO TRACK RBBL 13.84 BS 727 IN THE AFT CARGO COMPARTMENT. REPAIRED THE CARGO TRACK BTW BS 727D- 787 IAW SRM 53-00-53-2R-3, REPAIR 3, ALTERNATIVE 1 AND 2.
CORRODED WEB, BS 492.4 - 500A, S26R, WL 156 IN THE FWD CARGO BAY. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A0080, SHEET 23, REV-.
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING IAW SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 115A3712 SHEET 7REV A AND DWG 115A3700 SHEET 41 REV - .
CRACKED FLOOR SUPPORT LOCATED BETWEEN BS 312 - 328, LBL 46. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, SRM 51-10-02, AND DWG 141A5400, SHEET 26, REV-.
CORRODED STRAP, FLOOR STRUCTURE LOCATED BETWEEN BS 1016 TO 1040, LBL 4, WL 208.1. REPLACED THE STRAP IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 147A5600, SHEET 32, REV B.
CRACK ON RAIL NUT-PLATE LOCATED ORSS 286 INTERNAL CAVITY TRAILING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 286 INTERNAL CAVITY TRAILING EDGE AT LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9.
CRACK ON ANGLE WING TO BODY FARING STRUCTURE BS 500D AT LEVEL STR19L AT LOWER FUSELAGE. REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 116A3010, SHEET 39, REV-.
CORROSION FLOOR BEAM, BS 986.5, LBL 42, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.
CORROED FLOORBEAM, BS 986.5, RBL 42, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.
CRACK WEB INTERCOSTAL LOCATED BETWEEN BS 294.5 - 303.9, S16L. PERFORMED A MAJOR REPAIR ON WEB INTERCOSTAL IAW EA 25-153-02714-WIP1, TTG8Q015JTW1 AND EA 25-153-02714, TTG8Q015TCU5.
CRACK TIE CLIP LOCATED BS 277, STR 10R. REPLACED THE TIE CLIP AND FASTENERS AT BS 277, S10R IAW SRM 51-40-02-0G-0 AND DWG 141A1110 SHEET 18 REV-.
CRACKED FLOOR SUPPORT BS 328 - 344, LBL 46 REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02, DRAWING 141A5400, SHEET 44, REV-.
CORROSION STRAP FLOOR STRUCTURE LOCATED BETWEEN STA1016 TO STA1040 AND RBL18 WL208.1. REPLACED STRAP FLOOR STRUCTURE IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A5730 SHEET 23 REV C.
DETERIORATED HANDLE ON FWD ENTRY DOOR AT FWD GALLEY AREA (2 E/A). REPLACED HANDLE ON FWD ENTRY DOOR AT FWD GALLEY AREA (2 E/A) IAW AMM 52-11-31-400-802 STEP 3.G.(2).
CRACKED ANGLE FLOOR STRUCTURE LOCATED STA695 AND LBL24.75. REPLACED ANGLE LOCATED STA695 AND LBL24.75 CENTER SECTION IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 273A9110 REV A.
CRACKED ANGLE, FLOOR STRUCTURE. BS 695, RBL 24.75. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 273A9110, REV A, & DWG 111A6000, SHEET 302, REV-.
CRACKED ANGLE, BS 695, BL 0. REPLACED ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, AND DWG 273A9110, SHEET 6, REV A.
CRACKED ANGLE, FLOOR STRUCTURE, BS 695, BL 0. REPLACED ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0 SRM 51-10-02 ITEM 9 AND DWG 273A9110, SHEET 6, REV.A.
CRACK ON RAIL NUT-PLATE, OFSS 509 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 509 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-10-02 ITEM 9 SRM 51-40-02, AND DWG 112A4402, REV -, SHEET 13. MEASUREMENT OF CRACK IS L: 0.240.
CRACK ON RAIL NUT-PLATE LOCATED OFSS 484 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 484 INTERNAL CAVITY LEADING EDGE AT LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 112A4402, SHEET 13, AND SHEET 14 REV-. MEASURE OF CRACK: L=0.410.
CRACK INDICATION ON STUB FRAME BETWEEN BS 294.5 - 296.5, S-8 & 9R AT FWD GALLEY DOOR AREA. CRACK LENGTH 1.375 IN. REPLACED STUB FRAME IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 141A8370, SHEET 9, REV -, SHEET 10, REV D.
CRACK ON RAIL NUT-PLATE LOCATED OFSS 469 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT PLATE LOCATED OFSS 469 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 112A4402, SHEET 13, REV -. CRACK MEASUREMENT IS: 0.257.
CRACK ON RAIL NUT-PLATE LOCATED OFSS 369 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 369 INTERNAL CAVITY LEADING EDGE AT LT WING IAW SRM 51-10-02 ITEM 9 AND DWG 112A4402 SHEET:13 REV-.
CRACK ON ANGLE AUXILIARY TRACK SLAT 8 AT RT WING. REPLACED ANGLE AUXILIARY TRACK SLAT 8 AT RT WING IAW SRM 51-10-02 ITEM 9 & INSTALLED FASTENERS IAW SRM 51-40-02 AND DWG 114A5010; SHEET 16; REV A . AND MEASURE OF CRACK IS 0.750.
CRACK ON ANGLE AUXILIARY TRACK SLAT 7 AT RT WING (TWO EACH). REPLACED ANGLE AUXILIARY TRACK LOCATED ON SLAT 7 AT RT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9. LENGTH OF CRACK 0.250 INCH.
CRACKED ANGLE AUXILIARY TRACK SLAT 6, RT WING. REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, AND SRM 51-40-02. DUE TO EVALUATED CRACK ON ANGLE AND NOT FOUND ALLOWABLE DAMAGE IAW SRM-57-42-02-1A-1, ALLOWABLE DAMAGE 1. MEASUREMENT OF CRACK IS L= 2.057.
CRACK ON RAIL NUT-PLATE LOCATED OFSS 591 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 591 INTERNAL CAVITY LEADING EDGE AT RT WING IAW SRM 51-10-02 ITEM 9 AND DWG: 112A4402 SHEET: 14 REV: -.
INOPERATIVE BATTERY PACK BS 603 RT SIDE AT PASSENGER CABIN. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805, OPS CHECKED OK.
DELAMINATED ACCESS PANEL 193AL AT FUSELAGE EXTERIOR, REPAIRED THE ACCESS PANEL 193AL IAW SRM 51-70-05-2R-6, REPAIR 6.
DETERIORATED HARDWARE GALLEY GIRT BAR FLOOR BRACKETS. REPLACED HARDWARE GALLEY GIRT BAR BRACKETS IAW AMM 25-66-02-400-801.
DETERIORATED HARDWARE AFT ENTRY GIRT BAR FLOOR BRACKETS. REPLACED HARDWARE AFT ENTRY GIRT BAR BRACKETS IAW AMM 25-66-02-400-801.
BURNED EMERGENCY EXIT LIGHT LEFT SIDE IN PASSENGER CABIN. REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-01-960-801, STEP 2.C, 1, C THRU 2. TESTED OK.
DURING F/O ROLL EXPERIENCED RANCID ODOR FOLLOWED BY EXTREMELY HOT AIR COMING THROUGH THE VENTS, COULD BARELY CONTROL TEMP IN CABIN ON LANDING AND TAXI IN WENT TO PACKS HIGH -CONTINE TO DESCRIPTION AND APU BLEED AND KEPT GETTING LEFT PACK TRIP OFF LIGHT. ACM REMOVED AND PARTIALLY ACM INSTALLED PER AMM 21-51-04; JOB STOPPED BECAUSE BUSHING IS NIS IN LAS. FINISHED INSTALLING LH ACM PER AMM 21-51-04. OPS AND LEACH CHECK GOOD.
AFT CARGO COMPARTMENT 2ND FLOOR BACK CRACKED THROUGH. R/R AFT CARGO FLOOR PANEL REF AMM 25-52-10.
OVERHEAD PLACARD EMERGENCY EXIT SIGN MISSING FROM FRONT FWD ENTRY DOOR. INSTALLED LENS PER M/M 33-51-01 OK TO CONT SERVICE
EMERGENCY LIGHTING BATTERY PACK AT L/H OVERWING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
WHILE CLIMBING THROUGH FL210 EXPERIENCED A LOUD POP FROM ENGINE #2 ACCOMPANIED BY A MOMENTARY EGT EXCEEDANCE; OPERATED ENGINE AT REDUCED THRUST SETTING FR THE REMINDER OF THE FLIGHT WITH AIR RETURN TO SJC. OVERWEIGHT LANDING WAS NOT ACCOMPLISHED REFERENCE ORIGINAL WRITE-UP TTG8Q00X0QZX. SINCE ORIGINAL WRITE-UP WAS ASSIGNED TO ENGINE SN IN ERROR WHEN ENGINE WAS REMOVED IT UNASSIGNED THE CARD AND INITIATED A REPAIR ORDER TIED TO THE ENGINE. THAT CARD WAS CHANGED FROM LOG PAGE TO NON-ROUTINE SO THAT THIS CARD CAN REPRESENT THE ORIGINAL FAULT/LOG PAGE SIGN OFF.<[01] REMOVED AND REPLACED #2 ENGINE PER MT 771-00-01.<BR>C/W CONDITIONAL INSP 05-51-59 AMM.
AFT EMERGENCY FLASHLIGHTS BATTERIES NEED REPLACEMENT<[01] REMOVED AND REPLACED BOTH AFT EMERGENCY FLASHLIGHT BATTERIES IAW AMM 25-64-00.
ACCESS DOOR 311AL HAS CORROSION ON LEADING EDGE OF DOOR. ACCESS DOOR 311AL HAS CORROSION ON LEADING EDGE OF DOOR. PICTURES ATTACHED AND SUBMITTED TSR#2024001099.<[01] REPLACED THE ACCESS DOOR 311AL IAW AMM 52-49-11.
FWD SERVICE DOOR GIRT BAR LOOSE<[01] REPLACED RIVET ON GIRT BAR BRACKET ON THE FWD SERVICE DOOR REF SRM 51-40-02 AND MT 725-61-06 FOR REMOVAL AND INSTALLATION OF FWD SERVICE DOOR SLIDE.
FORWARD SERVICE DOOR ASSIST HANDLE LOOSE<[01] REPLACED HANDLE NUT REF AMM 52-41-00
FWD EMERGENCY WARNING LIGHT LENS BAR WON'T LOCK ON. FALLS OFF<[01] RESECURED R1 FWD EMERGENCY WARNING LIGHT IN REF AMM-33-51-01-960-802;[02] VERIFIED STEP 1
R2 DOOR SLIDE SKIRT NEEDS REPOSITIONED CATCHES ON DOOR CUTOUT<[01] FAULT WILL BE ADDRESSED ON BARCODE TTG8Q00P25L7;[02] VERIFIED STEP 1
FORWARD ENTRY DOOR CUTOUT STA 312 BETWEEN STR 5L-6L FRAME END CRACK<[01] FAULT WAS RESOLVED ON ANOTHER FAULT SEE EA M-22-153-01244 TASK CARD # TTG8Q00NPPLX FOR WORK ACCOMPLISHED;[02] VERIFIED STEP 1
FOUND DENT WITH A CRACK OUT OF LIMITS ON UPPER SURFACE R/H WING I/B AFT FLAP AT 32' FROM I/B EDGE AND 10.5' T/E; LENGTH OF DENT CRACK =1.5'.<[01] APPLIED REPAIR AT UPPER SURFACE R/H WING I/B AFT FLAP PER B737 SRM<BR> 57-53-01-2R-4; SRM 51-70-10-2R-4 AND SRM 51-70-10-2R-0 PARAGRAPH 20.B SIZE OF REPAIR IS 3.5'X4.5' MATERIAL USED FILM ADHES AF163-2K-06 PO#1798840 AND TOOLS USED TEMPERATURE CONTROL ID:160354 DUE DATE:02/23/24 AND VACUM GAGE ID:173239 DUE DATE:02-24-23 APPLIED TOP COAT AT UPPER SURFACE R/H WING I/B AFT FLA ON REPAIR AREA PER <BR>B737 AMM 51-21-99-300-802 MATERIAL USED PAINT PO#1750514.;[02] VERIFIED STEP 1
FOUND DENT WITH A CRACK OUT OF LIMITS ON UPPER SURFACE L/H WING I/B AFT FLAP AT 21.5' I/B EDGE AND 12.5' T/E; LENGTH OF DENT CRACK = 1'.<[01] APPLIED REPAIR AT UPPER SURFACE L/H WING I/B AFT FLAP PER B737 SRM<BR> 57-53-01-2R-4; SRM 51-70-10-2R-4 AND SRM 51-70-10-2R-0 PARAGRAPH 20.B SIZE OF REPAIR IS 2.5'X3.5' MATERIAL USED FILM ADHES AF163-2K-06 PO#1798840 AND TOOLS USED TEMPERATURE CONTROL ID:160354 DUE DATE:02/23/24 AND VACUM GAGE ID:173239 DUE DATE:02-24-23 AND APPLIED TOP COAT AT UPPER SURFACE L/H WING I/B AFT FLA ON REPAIR AREA PER <BR>B737 AMM 51-21-99-300-802 MATERIAL USED PAINT PO#1750514.;[02] VERIFIED STEP 1
RIGHT HORIZONTAL STAB RIB # 4 HAS A CRACK AT FIRST HOLE FWD OF LOWER STIFFENER #4<[01] REMOVED CRACK AT FIRST HOLE FWD OF LOWER SECTION COMMON TO STIFFENER #4 REF SRM 51-10-02-0G-0 AND INSTALLED REPAIR PARTS AT RIGHT HORIZONTAL STAB RIB # 4 COMMON TO STIFFENER #4 REF SRM 55-10-09-2R-5.;[02] CORRECTION TO STEP 1. REMOVED CRACK AT FIRST HOLE FWD OF LOWER SECTION COMMON TO STIFFENER #4 REF SRM 51-10-02-0G-0 AND INSTALLED REPAIR PARTS AT RIGHT HORIZONTAL STAB RIB # 4 COMMON TO STIFFENER #4 REF SRM 55-10-09-2R-5. THIS WORK WAS ACCOMPLISHED IN CONJUCTION WITH TTG8Q00NJPDK;[03] RII /VERIFIED ENTRY #2 AS A CORRECT ENTRY FOR WORK ACCOMPLISHED AS A CORRECTIVE ACTION TAKEN & ALSO APPLYS TO ENTRY #1 AS A CORRECTION OF INFO. ENTERD. RII/VERIFIED TT# ENTERD WAS WORKED IN CONJUCTION WITH THIS N/R CARD.
AFT CARGO DOOR CUTOUT AFT SCUFF PLATE CRACKED<[01] RECEIVED REPAIRED PART FROM OUTSIDE VENDOR. PN: 146A8343-7 PO: 2028887. WILL BE INSTALLED PER TASK CARD TTG8Q002ED5A.;[02] VERIFIED STEP 1
AFT CARGO COMP CAP STRIP BETWEEN STA 767-847 LBL 21' CORRODED<[01] RECEIVED NEW AFT CARGO COMPT CAP STRIP STA 767 TO STA 847 LBL 21. PN: 453A2611-4 PO: 2012626. INSTALLATION WILL BE ACCOMPLISHED PER TASK CARD TTG8Q00NKCXJ.
AFT CARGO COMP CAP STRIP BETWEEN STA 727-727D LBL 21' CORRODED<[01] RECEIVED NEW AFT CARGO COMPT CAP STRIP STA 727 TO STA 727D LBL 21. PN: 453A2611-8 PO: 2012626. INSTALLATION WILL BE ACCOMPLISHED PER TASK CARD TTG8Q00NKCXJ.
AFT CARGO COMP CAP STRIP BETWEEN STA 767-727D LBL 21' CORRODED<[01] RECEIVED NEW AFT CARGO COMPT CAP STRIP STA 727D TO STA 767 LBL 21. PN: 453A2611-10 PO: 2012626. INSTALLATION WILL BE ACCOMPLISHED PER TASK CARD TTG8Q00NKCXJ.
AFT CARGO COMP CAP STRIP BETWEEN STA 767-727D RBL 21' CORRODED<[01] RECEIVED NEW AFT CARGO COMPT CAP STRIP STA 727D TO STA 767 RBL 21; PN: 453A2611-11 PO: 2028887. WILL BE INSTALLED PER TASK CARD TTG8Q00NKCXJ.;[02] VERIFIED STEP 1
AFT CARGO COMP CAP STRIP BETWEEN STA 867-947.5 RBL 21' CORRODED<[01] RECEIVED NEW AFT CARGO COMPT CAP STRIP STA 867 TO STA 947.5 RBL 21; PN: 453A2611Y3 PO:1728471. WILL BE INSTALLED PER TASK CARD TTG8Q00NKCXJ.;[02] VERIFIED STEP 1
AFT CARGO COMP CAP STRIP BETWEEN STA 727-727D RBL 21' CORRODED<[01] RECEIVED NEW AFT CARGO COMPT CAP STRIP STA 727 TO STA 727D RBL 21. PN: 453A2611-9 PO: 2012626. INSTALLATION WILL BE ACCOMPLISHED PER TASK CARD TTG8Q00NKCXJ.
AFT CARGO FWD BULKHEAD BRACKET CRACK AT RBL 6'<[01] REMOVED AND REPLACED BRACKET (PN: 144A9401-20) AT AFT CARGO COMPT FWD BULKHEAD STA 727 RBL 6 PER REF SRM 51-41-02-0G-0;[02] CORRECTION TO STEP #1: REMOVED AND REPLACED BRACKET (PN: 144A9401-20) AT AFT CARGO COMPT FWD BULKHEAD STA 727 RBL 6 PER REF SRM 51-41-02-0G-0 AND DWG #144A2600;[03] VERIFIED STEP 2
AFT CARGO FLOOR SUPPORT AT B/S 771 22 INCHES RIGHT OF CENTER LINE IS CORRODED AT NUT PLATE HOLE<[01] WORK WAS ACCOMPLISHED PER TASK CARD TTG8Q00NM3MM;[02] VERIFIED STEP 1
MAIN CABIN STA. 540 HORIZONTAL SPAR CHORD BETWEEN LBL 0.07 AND LBL 24.82 IS CRACKED NEAR EDGE<[01] REMOVED AND REPLACED PANEL BREAK AT MAIN CABIN STA 540 LBL 0.07 AND LBL 24.82 AS PER SRM 51-40-02-0G-0 AND DWG 143A5240.;[02] VERIFIED STEP 1
MAIN CABIN INTERCOSTAL CRACK AT BL 0' BETWEEN STA 380-400<[01] REMOVED AND INSTALLED NEW INTERCOSTAL ANGLE AT MAIN CABIN BL 0' BETWEEN STA 380-400 AS PER SRM 51-40-02.;[02] CORRECTION: REMOVED AND INSTALLED NEW INTERCOSTAL ANGLE AT MAIN CABIN BL 0' BETWEEN STA 380-400 AS PER SRM 51-40-02. & DWG. 143A5400.;[03] VERIFIED STEP 2
MAIN CABIN INTERCOSTAL CRACK AT LBL 13' BETWEEN STA 380-400<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN LBL 13' BETWEEN STA 380-400 AS PER SRM 51-40-02-0G-0 AND DWG 143A5400.;[02] VERIFIED STEP 1
MAIN CABIN INTERCOSTAL CRACK AT RBL 10' BETWEEN STA 380-400<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN RBL 10' BETWEEN STA 380-400 AS PER SRM 51-40-02-0G-0 AND DWG 143A5400.;[02] VERIFIED INSTALLATION
ACCESS PANEL 241AF IS DAMAGED/ DELAMINATED<[01] RECEIVED MAIN CABIN FLOOR PANEL 241AF AND WILL BE INSTALLED ON T/C &NBSP;&NBSP;&NBSP;&NBSP;&NBSP;TTG8Q00MWWZR;[02] VERIFIED STEP 1
MAIN CABIN STA. 540 HORIZONTAL SPAR CHORD BETWEEN RBL 24.82 AND RBL 45.57 HAS CRACKS AROUND FASTENERS<[01] REMOVED AND REPLACED PANEL BREAK AT STA 540 RBL 24.82 AND RBL 45.57 AS PER SRM 51-40-02-0G-0 AND DWG-143A5240.;[02] VERIFIED STEP 1
MAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM FASTENER HOLE STA 986.5 LBL 45'<[01] REMOVED CORROSION AT MAIN CABIN AFT WET AREA STA 986.5 AND LBL 45' REF SRM 51-10-02-0G-0;PERFORMED UT THICKNESS INSP AT REWORKED AREA; IAW B 737 NDT PART 4 51-00-00 PROC 3. MINI THICK 0.122'. TOOL 27MG. BC 172139. CALIB DUE 3-30-24.ORIGINAL MATERIAL 0.150'; REMOVED MATERIAL 0.028'; REMAINING MATERIAL 0.122'; REWORKED AREA IS OUT OF LIMITS REF 53-70-51-1A-1<BR> AND IT WAS REPAIRED PER EA M-21-153-00612 INSTRUCTIONS ON TASK CARD TTG8Q00NMAE9;[02] RII/VERIFIED ENTRY #1 AS WORK ACCOMPLISHED & FOUND OUT OF LIMITS ; AND REPAIRED AS STATED ON ( REPAIRED PER EA M-21-153-00612 INSTRUCTIONS ON TASK CARD #TTG8Q00NMAE9.
MAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM FASTENER HOLE STA 986.5 RBL 45'<[01] REMOVED CORROSION AT MAIN CABIN AFT WET AREA STA 986.5 AND RBL 45' REF SRM 51-10-02-0G-0PERFORMED UT THICKNESS INSP AT REWORKED AREA; IAW B 737 NDT PART 4 51-00-00 PROC 3. MINI THICK 0.126'. TOOL 27MG. BC 172139. CALIB DUE 3-30-24.ORIGINAL MATERIAL 0.150'; REMOVED MATERIAL 0.024'; REMAINING MATERIAL 0.126'; REWORKED AREA IS OUT OF LIMITS REF 53-70-51-1A-1 AND IT WAS REPAIRED PER EA M-21-153-00612 INSTRUCTIONS ON TASK CARD #TTG8Q00NM8E2;[02] RII/VERIFIED ENTRY #1 AS WORK ACCOMPLISHED & FOUND OUT OF LIMITS ; AND REPAIRED AS STATED ON ( REPAIRED PER EA M-21-153-00612 INSTRUCTIONS ON TASK CARD #TTG8Q00NM8E2.
MAIN CABIN FLOOR PANEL 242TF UPPER SURFACE FRAYING<[01] RECEIVED NEW FLOOR PANEL 242TF. ISSUE TAG #E199903 PO#2039032.;[02] VERIFIED STEP 1
MAIN CABIN FLOOR PANEL 241ABF UPPER SURFACE FRAYING<[01] RECEIVED FLOOR PANEL NEW 241 ABF FLOOR.<BR>PANEL WILL BE INSTALLED ON TASK CARD TTG8Q00MWWZZ.;[02] VERIFIED STEP 1
MAIN CABIN FLOOR PANEL 241XF UPPER SURFACE FRAYING<[01] RECEIVED FLOOR PANEL NEW 241XF FLOOR PANEL.<BR>PANEL WILL BE INSTALLED ON TASK CARD TTG8Q00MWX5D.;[02] RECEIVED MAIN CABIN FLOOR PANEL 241XF AND WILL BE INSTALLED ON T/C TTG8Q00MWWZ7;[03] VERIFIED STEP 2
MAIN CABIN FLOOR PANEL 241YF UPPER SURFACE FRAYING<[01] RECEIVED NEW FLOOR PANEL 241YF. ISSUE TAG #E199910 PO#2039038.;[02] VERIFIED STEP 1
MAIN CABIN AFT WET AREA CORROSION AT FLOOR SUPPORT STRAP BETWEEN STA 1016-1040 LBL 3'<[01] CLEAN AREA AT FLOOR SUPPORT STRAP BETWEEN STA 1016-1040 AND LBL 3' REF SOPM 20-30-03; TREAD AND PRIMER REF AMM 51-21-41-370-803 & AMM 51-21-72-370-804;[02] VERIFIED STEP # 1
MAIN CABIN FLOOR PANEL 241ADF SEVERAL INSERT CORRODED<[01] REMOVED AND REPLACED SEVERAL INSERTS AT MAIN CABIN FLOOR PANEL 241ADF IN REF SRM-53-00-50-2R-0-A00938;[02] VERIFIED STEP 1
MAIN CABIN FLOOR PANEL 241ACF SEVERAL INSERT CORRODED<[01] REMOVED AND REPLACED SEVERAL INSERTS AT MAIN CABIN FLOOR PANEL 241ACF IN REF SRM-53-00-50-2R-0-A00938;[02] VERIFIED STEP 1
MAIN CABIN FLOOR PANEL 221CF SEVERAL INSERT CORRODED<[01] RECEIVED NEW FLOOR PANEL 221CF. ISSUE TAG E199911 PO#2039277;[02] VERIFIED STEP 1
MAIN CABIN FLOOR PANEL 221BF SEVERAL INSERT CORRODED<[01] RECEIVED NEW FLOOR PANEL 221BF. ISSUE TAG WN35867 PO#2028887;[02] VERIFIED STEP 1
MAIN CABIN FLOOR PANEL 221EF ONE EACH INSERT CORRODED<[01] REMOVED AND REPLACED INSERT AT MAIN CABIN FLOOR PANEL 221EF IN REF SRM-53-00-50-SR-0;[02] VERIFIED STEP 1
MAIN CABIN FWD WET AREA CORROSION AT INTERCOSTAL UPPER SURFACE STA 294.5+11' LBL 12'<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 294.5 TO STA 312 LBL 11.6 SRM 51-40-02-0G-0 AND DWG 141A5600;[02] VERIFIED STEP 1
MAIN CABIN FLOOR PANEL 241ZF UPPER SURFACE FRAYING<[01] RECEIVED FLOOR PANEL NEW 241ZF FLOOR.<BR>PANEL WIL BE INSTALLED ON TASK CARD TTGQOOMWX03.;[02] CORRECTION: RECEIVED MAIN CABIN FLOOR PANEL 241ZF AND WILL BE INSTALLED ON T/C TTG8Q00MWX03;[03] VERIFIED STEP 2
CRACK FOUND AT AREA AFT OF FWD. CARGO COMPARMENT; LOCATED AT STA. 540 WL 208 RBL 1; SEE DOT # 31<[01] REMOVED AND REPLACE PANEL BREAK AT STA 540 WL 208 RBL 1. AS PER; SRM 51-40-02-0G-0 AND DWG 143A5240.;[02] CORRECTION ON STEP # 1: REMOVED AND REPLACED PANEL BREAK AT STA 540 WL 208 RBL 1. AS PER; SRM 51-40-02-0G-0 AND DWG 143A5240.;[03] VERIFIED STEP 2
MAIN CABIN INTERCOSTAL CRACK AT BL 0' BETWEEN STA 277-294.5<[01] REMOVED AND REINSTALLED NEW INTERCOSTAL AT MAIN CABIN BL 0' BETWEEN STA 277-294.5 AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED STEP 1
MAIN CABIN INTERCOSTAL CRACK AT LBL 12' BETWEEN STA 344-360<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWWEEN STA 344 TO STA 360 AND LBL 12' IN REF B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING #141A5400.;[02] VERIFIED STEP 1
MAIN CABIN FLOOR PANEL 242VF UPPER SURFACE FRAYING<[01] RECEIVED FLOOR PANEL NEW 242 VF FLOOR.<BR>PANEL WILL BE INSTALLED ON TTGQ00MWX5H.;[02] CORRECTION: RECEIVED MAIN CABIN FLOOR PANEL 242VF AND WILL BE INSTALLED AND T/C TTG8Q00MWX5H;[03] VERIFIED STEP 2
MAIN CABIN FLOOR PANEL 242UF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 242UF AND WILL BE INSTALLED ON T/C TTG8Q00MWX5K;[02] VERIFIED STEP 1
RH WING DEFLECTOR PANEL ATTACH SERRATED PLATE HOLES ELONGATED<[01] ACCOMPLISHED REPAIR AT RIGHT WING DEFLECTION CONTRL RIB IN REF B737-700 SRM 57-51-02-2R-1; REPAIR 1.;[02] VERIFIED STEP 1
MAIN CABIN CORROSION AT SEAT TRACK CROWN BOTTOM STA 663.75+12' RBL 24.75<[01] REMOVED DAMAGE FROM SEAT TRACK AT STA 663.75 RBL 24.75 FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1; FIG.103;DETAIL: 'A'. TOOL USED: BC: WN0012; DUE DATE: 4/18/24; PERFORMED SEAT TRACK REPAIR AS PER SRM 53-00-52-2R-3.;[02] VERIFIED STEP 1
RT HORIZONTAL STABILIZER RIB #4 STIFFENER #4 CRACK AT LOWER SECTION<[01] REMOVED CRACK AT RT HORIZONTAL STABILIZER RIB #4 STIFFENER #4 AND FIRST HOLE FWD OF LOWER SECTION COMMON TO STIFFENER #4 REF SRM 51-10-02-0G-0 AND INSTALLED REPAIR PARTS AT RIGHT HORIZONTAL STAB RIB # 4 COMMON TO STIFFENER #4 REF SRM 55-10-09-2R-5.;[02] CORRECTION TO STEP 1. REMOVED CRACK AT RT HORIZONTAL STABILIZER RIB #4 STIFFENER #4 AND FIRST HOLE FWD OF LOWER SECTION COMMON TO STIFFENER #4 REF SRM 51-10-02-0G-0 AND INSTALLED REPAIR PARTS AT RIGHT HORIZONTAL STAB RIB # 4 COMMON TO STIFFENER #4 REF SRM 55-10-09-2R-5. THIS WORK WAS ACCOMPLIOSHED IN CONJUCTION WITH TTG8Q00NMWM0;[03] RII /VERIFIED ENTRY #2 AS A CORRECT ENTRY FOR WORK ACCOMPLISHED AS A CORRECTIVE ACTION TAKEN & ALSO APPLYS TO ENTRY #1 AS A CORRECTION OF INFO. ENTERD. RII/VERIFIED TT# ENTERD WAS WORKED IN CONJUCTION WITH THIS N/R CARD.
LEADING EDGE SLAT #5 STA 85.19 NOSE SKIN ACTUATOR RIB CRACK AT O/B SECOND FASTENER HOLE FROM AFT EDGE<[01] PERFORMED REPAIR ON LEADING EDGE SLAT #5 STA 85.19 NOSE SKIN ACTUATOR RIB IAW SRM 57-42-01-2R-8 REPAIR 8 FIG 202 SHEET 4.;[02] VERIFIED STEP 1
EXTERNAL GROUND POWER RECEPTACLE AFT CUTOUT LOWER AREA HAS MISSING SHIM OF PREVIOUS REPAIR & CRACKED SKIN DOUBLER.<[01] REMOVED AND REPLACED EXTERNAL GROUND POWER RECEPTACLE (EGPR) INNER DOUBLER AT STA 219.8 - STA 244 STR 19R - STR 24R REF SRM 51-40-02-0G-0 AND DWG 141A3702. TREATED; PRIMED ; AND TOP COAT AS REQUIRED REF AMM 51-21-73-370-803; AMM 51-21-72-370-801;[02] VERIFIED STEP 1
FORWARD SERVICE CABIN DOOR (R1). AFT SLIDE MOUNT BRACKET UPPER ISOLATOR IS CRACKED.<[01] R&R FORWARD SERVICE CABIN DOOR (R1). AFT SLIDE MOUNT BRACKET UPPER ISOLATOR IAW SRM 51-40-02.;[02] C/W INSPECTION PER SRM 51-40-02.
RH AFT EMERGENCY BATTERY PACK IS INOP.<[01] R&RR/H AFT EMER BATTERY PER AMM 33-51-06; OPSC HECKK GOOD AT THIS TIME.
RAMP REPORTS CRACK IN AFT CARGO COMP FLOOR<[01] MADE PERM REPAIR AFT CARGO COMP FLOOR AMM 25-52-01
SLIDE ON DOOR R1 STUCK IN THE DISARMED POSITION<[01] POSITIONED GRIT BAR INTO PROPER STOW POSITION PER S.I.P.
TAIL L/H UPPER AFT SLIDING SEAL TRACK IS CRACKED<[01] R+R UPPER AFT L/H STAB SLIDING SEAL TRACK IAW AMM 20-50-11.
TAIL R/H UPPER AFT SLIDING SEAL TRACK IS CRACKED<[01] R+R UPPER AFT R/H STAB SLIDING SEAL TRACK IAW AMM 20-50-11.
TAIL LEFT UPPER AFT SLIDING SEAL HAS LOOSE RUB STRIP. REMOVED AND REPLACED 333AT SLIDING SEAL REF SRM 51-40-02.
AFT ONE THIRD OF CABIN EMERGENCY LIGHTS FAILED A CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK M01673 IAW AMM 33-51-06. ALL CHECKED GOOD.
FWD KEEL BEAM PANEL 192E FWD LEFT SUPPORT BRACKET BROKEN. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02
FWD SERVICE AND ENTRY DOOR EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW / [01] R&R LIGHT LENS COVERS WITH ARROW COVERS IAW AMM 33-51-01.;[02] INSPECTED
AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP / [01] R&R AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT LAMP PER AMM 33-51-04. OPS CHECK GOOD
EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST AT POSITIONS M1675; M1669; AND M1672 / [01] REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACKS AT POSITIONS M1675; M1669; AND M1672 PER ENG DWG 33500005 AND AMM 33-51-06
EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST AT POSITIONS M1675; M1669; AND M1672 / [01] REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACKS AT POSITIONS M1675; M1669; AND M1672 PER ENG DWG 33500005 AND AMM 33-51-06
EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST AT POSITIONS M1675; M1669; AND M1672 / [01] REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACKS AT POSITIONS M1675; M1669; AND M1672 PER ENG DWG 33500005 AND AMM 33-51-06
ASD ESCAPE SLIDE GIRT CATCHES ON THRESHOLD WHILE OPENING DOOR ; / [01] REPACKED ASD GIRT PER AMM 25-66-01-400-804 STEP 6.D(1(C-H); [02] CORRECTION FOR ITEM 1:<BR>REPACKED ASD ESCAPE SLIDE GIRT PER AMM 25-66-01-400-804 STEP 6.D(1(C-H); [03] VERIFIED CORRECTIVE ACTION 1-2.<BR><BR>VERIFIED GIRT NO LONGER CATCHES WHILE OPENING.
FORWARD TWO FLASHLIGHT ARE DEAD. ; / [01] REMOVED AND REPLACED BATTERIES ON FORWARD ATTENDANT 2 EA. FLASHLIGHTS PER AMM 25-64-00-900-806.; [02] VERIFIED CORRECTIVE ACTION 1.
B.S. 663 BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8; W.L. 164. ; / [01] TRIMED OUT ATTACH ANGLE AT VAPOR BARRIER BS 663 RBL 15 WL 164 PER SRM 57-10-10-2R-5 STEP 4 B<BR><BR>PERFORMED DETAIL INSPECTION OF THE REPAIR AREA AND UNDERLYING STRUCTURE TO MAKE SURE THAT THERE IS NO DAMAGE WITHIN THE REPAIR AREA; [02] PERFORM AN OPEN HOLE HFEC INSPECTION FOR ALL INITIAL FASTENERS HOLES IN THE REPAIR AREA TO MAKE SURE THERE IS NO DAMAGE; [13] REPAIRED CRACKED VAPOR BARRIER BULKHEAD UPPER ATTACH ANGLE BS 663 RBL 15 WL 164 PER SRM 57-10-10-2R-5; [14] VERIFIED CORRECTIVE ACTION 13
ACB FWD CORNER SCUFF PLATE CRACKED ; / [01] RECEIVED NEW AFT FWD SCUFF PLATE P/N 654A0004-97; LOCATED AND DRILLED SCUFF PLATE IAW SRM 51-40-05 AND DWG 143A8341 ID:007; REV:A<BR><BR>INSTALL SCUFF PLATE WILL BE ACCOMPLISHED ON C.C. TTG8Q002EGBV.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.; [03] CLARIFICATION TO STEP 1: RECEIVED NEW AFT CARGO BAY FORWARD SCUFF PLATE P/N 654A0004-97; LOCATED AND DRILLED SCUFF PLATE IAW SRM 51-40-05 AND DWG 143A8341 ID:007; REV:A
FCB GUSSET IS CRACKED AT BS500D S-19R WL190 ; / [01] REMOVED FCB GUSSET AT BS 500D STR19R WL 190 IAW SRM 51-40-02; [02] LOCATED AND DRILLED NEW FCB GUSSET AT BS 500D STR 19R; PN#143A9481-5 IAW SRM 51-40-05 AND IAW DWG# 143A7902... OK TO INSTALL; [03] VERIFIED LOCATED AND DRILLED NEW GUSSET PER SRM 51-40-05 AND DWG 143A7902. OK TO INSTALL; [04] INSTALLED NEW GUSSET AT BS500D S-19R WL190; IAW SRM 51-40-02-0G-0 AND DWG#143A7902; [05] VERIFIED CORRECTIVE ACTION 4.; [06] VERIFIED ALL WORK ACCOMPLISHED.
FCB GUSSET IS CRACKED AT BS500D S-19L WL190 ; / [01] REMOVED FCB GUSSET AT BS 500D STR 19L WL 190 IAW SRM 51-40-02; [02] LOCATED AND DRILLED NEW FCB GUSSET AT BS 500D STR 19L; PN#143A9481-6 IAW SRM 51-40-05 AND IAW DWG# 143A7902... OK TO INSTALL; [03] VERIFIED LOCATED AND DRILLED NEW GUSSET PER SRM 51-40-05 AND DWG 143A7902. OK TO INSTALL; [04] INSTALLED NEW FCB GUSSET AT BS500D S-19L WL 190; IAW SRM 51-40-02-0G-0 AND DWG#143A7902; [05] VERIFIED CORRECTIVE ACTION 4.; [06] VERIFIED ALL WORK ACCOMPLISHED.
PANEL 561CB HAS SEVERAL PULLED FASTENER HOLES (MARKED) ; / [01] IDENTIFIED PANEL 561CB MATERIAL IAW SRM 57-51-01-0I-1 FIGURE 3. SHEET 1;ITEM [10] AND TABLE 3. ITEM [10].<BR><BR>CLEANED PANEL AND REMOVED FINISH AS NEEDED TO EVALUATE DAMAGE IAW AMM 51-21-11-150-815 PARA. 17. C. AND D<BR><BR>VISUAL INSPECTION FOUND DAMAGE TO GLASS FIBER PLIES TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4. B. (2)<BR><BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-05-2R-9 AS GIVEN IN SRM 57-51-01-2R-1 PARA 2.E.<BR><BR> REMOVED FULL DEPTH EDGEBAND PLY DAMAGE FROM 29 EA FASTENER HOLES ON THE AFT EDGE; WITH NO MOISTURE OR CONTAMINATION NOTED THEN CLEANED REPAIR AREA. AREA OF REMOVED DAMAGE IS LESS THAN 0.5' DIA. ALL IAW SRM 51-70-05-2R-9 PARA 4. A-C.;[10] FABRICATED REPAIR PLIES FROM BMS9-3 TYH2 LOT 1458851-1; INSTALLED PLIES WITH BMS8-301 CLASS 1 LOT JH1CAA0868.<BR><BR> ASSEMBLED VACUUM BAG AND LEAK CHECKED GOOD USING VACUUM GAGE ID: ATS2584 S/N: 5432766772.<BR><BR>SET PLIES TO CURE USING HOTBONDER I/D: NCX000523 S/N: 11051262. ALL IAW SRM 51-70-04-2R-9 PARA 4. J. - M.; [11] CURED REPAIR PLIES REMOVED BAGGING MATERIAL AND LIGHTLY SANDED IAW SRM 51-70-04-2R-9 PARA 4.M.REQUEST POST CURE NDI TO VERIFY NO DISBONDS IAW SRM 51-70-04-2R-9 PARA 4.O.; [12] VERIFIED CORRECTIVE ACTION ITEMS 10 AND 11.<BR><BR>UT INSPECTED REPAIR PER NDTM PART 4; 51-00-02. NO DISBONDS NOTED.<BR><BR>CAL ID: ATS2341 S/N: 190848104; [13] REFINISHED INNER AND OUTER SURFACE OF PANEL IAW SRM 51-70-04-2R-9 PARA 4 P.
CORROSION FOUND ON INTERCOSTAL AT RBL 20; WL153; STA767+5 AND STA767+6 ; / [01] REMOVED INTERCOSTAL FROM BS 767 TO BS 867; RBL 20; WL 153 IAW SRM 51-40-02-0G-0; [02] VERIFIED COMPLETE STEPS 1; 2.; [03] REMOVED CORROSION FROM INTERCOSTAL AFT CARGO BAY BS767+5'' RBL20 WL153; P/N 146A8123U19; IN AREA .7''X.3''X0.020'' DEEP; ORIGINAL THICKNESS 0.063''; REMAINING MAT. THICKNESS 0.043' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1 STEP 4.B. (2) FIGURE 102. TOOL USED: DEPTH GAGE ID:ATS2472; DUE DATE: 06/2022; [04] VERIFIED CORRECTIVE ACTION ENTRY 3.; [05] RECEIVED NEW INTERCOSTAL LOCATED AND DRILLED MAT. ITEM#146A8123U19; LOT#1470503-2 FROM BS767 TO BS787 RBL 20 WL 153 IAW.SRM 51-40-05-0G-0; DWG 146A8123; [06] VERIFIED DRILLED MAT. ITEM#146A8123U19; LOT#1470503-2 FROM BS767 TO BS787 RBL 20 WL 153 IAW.SRM 51-40-05-0G-0; DWG 146A8123.; [07] OK TO INSTALL NEW INTERCOSTAL.; [08] VERIFIED OK TO INSTALL.; [09] INSTALLED NEW INTERCOSTAL AFT CARGO BAY AT BS 767 TO BS 787 RBL 20 WL 153 IAW SRM 51-40-02-0G-0 DWG 146A0081; [10] VERIFIED INSTALLATION OF NEW INTERCOSTAL AFT CARGO BAY AT BS 767 TO BS 787 RBL 20 WL 153 IAW SRM 51-40-02-0G-0 DWG 146A0081; [11] TASK COMPLETE
CORROSION ON ANGLE P/N 146A8125-53 ATTACHED TO INTERCOSTAL BS 767+5 WL 153 ; / [01] REMOVED DAMAGE ON ANGLE ATTACHED TO INTERCOSTAL AT BS 767 +5 WL 153; RBL 20 AREA .9' X 2' X .010' IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE FOUND IN SRM ; IT'LL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9.C.; [02] VERIFIED REMOVED DAMAGE ON ANGLE ATTACHED TO INTERCOSTAL AT BS 767 +5 WL 153; RBL 20 AREA .9' X 2' X .010' IAW SRM 51-10-02-0G-0. FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE FOUND IN SRM ; IT'LL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9.C.; [03] RECEIVED NEW ANGLE ITEM:146A8125-53 LOT:1463430-1. <BR>LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05-0G-0 AND DRAWING:146A8123.<BR>OK TO INSTALL; [04] VERIFIED LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05-0G-0 AND DRAWING:146A8123. <BR>VERIFIED OK TO INSTALL.; [05] INSTALLED NEW ANGLE ATTACHED TO INTERCOSTAL AFT CARGO BAY AT BS 767 TO BS 787 RBL 20 WL 153 IAW SRM 51-40-02-0G-0 DWG 146A8123; [06] VERIFIED INSTALLATION OF NEW ANGLE ATTACHED TO INTERCOSTAL AFT CARGO BAY AT BS 767 TO BS 787 RBL 20 WL 153 IAW SRM 51-40-02-0G-0 DWG 146A8123; [07] CORRECTED ON PART REQUIREMENT; [08] CORRECTED ON PART REQUIREMENT; [09] VERIFIED JOB IS COMPLETE
PANEL 193B HAS SEVERAL PULLED THROUGH CRACKED FASTENER HOLES ; / [01] IDENTIFIED PANEL / MATERIAL 193B IAW SRM 53-40-70-0I-1 FIG. 2. TABLE 2. ITEM (13).<BR><BR>FOUND 3EA. CRACKED FASTENER HOLE DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PARA 4. B. (2) (A). <BR><BR>REPAIR WILL BE ACCOMPLISHED IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1.<BR><BR>REMOVED CRACKED DAMAGE AT 3EA. FASTENER HOLES ON L/E EDGE BAND & CLEANED REPAIR AREAS. NO CONTAMINATION OR WATER NOTED IAW SRM 51-70-05-2R-6. PARA 4. A. - D.; [02] VALIDATED APPLICABILITY OF REPAIR TO BE COMPLETED IAW SRM 51-70-05-2R-6 AS GIVEN IAW SRM 53-40-70-2R-1.; [11] PANEL 193B WITH SEVERAL PULLED THROUGH CRACKED FASTENER HOLES WERE REPAIRED IAW SRM 51-70-05-2R-6; [12] VERIFIED CORRECTIVE ACTIONS 10 AND 11
CORROSION ON ACB FLOORBOARD SPLICE STRAP TOP SURFACE AT BS 767+5.5; WL 153; LBL 2.5; LBL 10; LBL 15; LBL 16; RBL 3; RBL 4.2; RBL 8; RBL 10.5 & RBL 14.3 ; / [01] VERIFIED COMPLETE STEPS 1 - 9.; [02] RECEIVED NEW ACB FLOORBOARD SPLICE STRAP BS 767 +5.5; WL 153 ; FROM RBL 21 TO LBL 21 P/N 146A9401-4 LOT# 1467541.<BR><BR>INSTALL PART WILL BE ACCOMPLISHED ON C.C. TTG8Q004E68F.; [03] VERIFIED RECEIVED NEW ACB FLOORBOARD SPLICE STRAP BS 767 +5.5; WL 153 ; FROM RBL 21 TO LBL 21 P/N 146A9401-4 LOT# 1467541.<BR>VERIFIED INSTALL PART WILL BE ACCOMPLISHED ON C.C. TTG8Q004E68F.
RT WING T/E PANEL 661AB AFT ROW OS FASTENER HOLES HAS MULTIPLE HOLE WHERE FASTENER HAS PULLED THROUGH ; / [01] IDENTIFIED PANEL 661CB IAW SRM 57-51-01-0I-1 FIGURE 3 ITEM [5] AND TABLE 3 ITEM [5]. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B.(2) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-9 PER SRM 57-51-01-2R-1 PARA 2.E. REMOVED FULL DEPTH EDGEBAND PLY DAMAGE FROM ALL THE FASTENER HOLES ON THE AFT EDGE; MAX AREA OF REMOVED DAMAGE IS 0.5' ALSO CLEANED REPAIR AREA. WORK ACCOMPLISHED IAW SRM 51-70-05-2R-9 PARA 4.A-C.; [02] CORRECTION TO ITEM 1: CORRECT PANEL IS 661AB NOT 661CB.VALIDATED APPLICABILITY OF SRM 51-70-05-2R-9.; [03] INSPECTED DAMAGE REMOVAL AND VERIFIED CORRECTIVE ACTIONS 1 AND 2. OKAY TO PROCEED PER SRM 51-70-05-2R-9.; [04] APPLIED SLURRY MIXTURE OF BMS 8-301 CL1 LOT# JH1CAA0868 AND CHOPPED FIBERS TO FASTENER LOCATIONS. <BR>SET TO CURE WITH HEAT LAMP MONITORED WITH THERMOMETER ID: ATS2209 S/N: 43300739WS <BR>IAW SRM 51-70-05-2R-9 PARA 4D-F.; [05] CURED SLURRY; SANDED FLUSH; CLEANED REPAIR AREA; FABRICATED REPAIR PLIES FROM BMS9-3 TYH2 LOT 1458851-1; INSTALLED PLIES WITH BMS8-301 CLASS 1 LOT JH1CAA0868; VACUUM BAGGED; VERIFIED 5X5 AND SET PLIES TO CURE USING HOTBONDER I/D: NCX000523 S/N: 11051262. WORK ACCOMPLISHED IAW SRM 51-70-05-2R-9 PARA 4.F AND H-M.;[10] REFINISHED PANEL IAW SRM 51-70-05-2R-9 PAR 4O AND AMM 51-21-99-300-802 PAR 3C(1)(D-E).
PANEL 661BB HAS MULTIPLE PULLED THROUGH CRACKED FASTENER HOLES ON AFT EDGE ; / [01] IDENTIFIED PANEL 661CB IAW SRM 57-51-01-0I-1 FIGURE 3 ITEM [9] AND TABLE 3 ITEM [9]. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B.(2) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-9 PER SRM 57-51-01-2R-1 PARA 2.E. REMOVED FULL DEPTH EDGEBAND PLY DAMAGE FROM ALL THE FASTENER HOLES ON THE AFT EDGE; MAX AREA OF REMOVED DAMAGE IS 0.5' ALSO CLEANED REPAIR AREA. WORK ACCOMPLISHED IAW SRM 51-70-05-2R-9 PARA 4.A-C.; [02] CORRECTION TO ITEM 1: CORRECT PANEL IS 661BB NOT 661CB.VALIDATED APPLICABILITY OF SRM 51-70-05-2R-9.;
RT WING T/E PANEL 661CB AFT ROW OF FASTENERS HOLES HAS MULTIPLE HOLES WHERE FASTENERS HAVE PULLED THROUGH ; / [01] IDENTIFIED PANEL 661CB IAW SRM 57-51-01-0I-1 FIGURE 3 ITEM [10] AND TABLE 3 ITEM [10]. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1 PARA 4.B.(2) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-9 PER SRM 57-51-01-2R-1 PARA 2.E. REMOVED FULL DEPTH EDGEBAND PLY DAMAGE FROM NUMEROUS FASTENER HOLES ON THE AFT EDGE; MAX AREA OF REMOVED DAMAGE IS 0.5' ALSO CLEANED REPAIR AREA. WORK ACCOMPLISHED IAW SRM 51-70-05-2R-9 PARA 4/A-C.; 05] APPLIED SLURRY MIXTURE OF BMS 8-301 CL1 LOT# JH1CAA0868 AND CHOPPED FIBERS TO FASTENER LOCATIONS. <BR>SET TO CURE WITH HEAT LAMP MONITORED WITH THERMOMETER ID: ATS2209 S/N: 43300739WS <BR>IAW SRM 51-70-05-2R-9 PARA 4D-F.; [06] CURED SLURRY; SANDED FLUSH; CLEANED REPAIR AREA; FABRICATED REPAIR PLIES FROM BMS9-3 TYH2 LOT 1458851-1; INSTALLED PLIES WITH BMS8-301 CLASS 1 LOT JH1CAA0868; VACUUM BAGGED; VERIFIED 5X5 AND SET PLIES TO CURE USING HOTBONDER I/D: NCX000526 S/N: 12051216. WORK ACCOMPLISHED IAW SRM 51-70-05-2R-9 PARA 4.F AND H-M. 11] REFINISHED PANEL IAW SRM 51-70-05-2R-9 PAR 4O AND AMM 51-21-99-300-802 PAR 3C(1)(D-E).; [12] VERIFIED CORRECTIVE ACTIONS 9 AND 10
CORROSION ON PASSENGER CABIN SEAT TRACK AT B.S. 706+5 AND 727+16-727A+11; R.B.L. 24.75; W.L. 208.1 ; / [01] COMPLETED STEPS.; [02] VERIFIED COMPLETION OF ALL CORROSION REMOVAL STEPS; [03] APPLIED CHEMICAL CONVERSION COATING AND ONE LAYER OF ALUMINIZED EPOXY PRIMER TO REWORKED AREA IAW SRM 51-20-01 AND SOPM 20-41-04; [04] VERIFIED CORRECTIVE ACTIONS 3
CORROSION ON FWD CARGO DOOR CUTOUT AFT SHIELD AT WL 153; STA 480+18; RBL 25; STA 500+2; RBL 24; STA 500+6; RBL 24; STA 500+6; RBL 25; STA 500+11; RBL 25; STA 500+12; RBL24; STA 500+14; RBL 24; ; STA 500+14; RBL 25; STA 500+18; RBL 25. / [01] REMOVED AFT; SHIELD ON FWD CARGO DOOR CUTOUT; WL153; RBL24;NO FOUND ALLOWABLE DAMAGE IN THE SRM. IAW. SRM 51-10-02-0G-0;STEP 9.; AND SRM 51-40-02-0G-0.; [02] CORRECTED MEASUREMENTS FIELD TABLE.; [03] VERIFIED CORRECTIVE ACTION 1; FOR REMOVAL OF FCB DOOR CUTOUT AFT SHIELD AND THAT DAMAGED SHIELD WILL BE REPAIRED BY REPLACEMENT DUE TO NO SRM LIMITS.; [04] LOCATED AND DRILLED NEW SHIELD P/N 143A8126U31; LOT 1472167-1 IAW SRM 51-40-05 AND DWG 143A0080; [05] VERIFIED CORRECTIVE ACTION ENTRY 4.; [06] INSTALLATION OF FCD CUTOUT AFT SHIELD WILL BE PERFORMED ON MOC 5330-E-16461-NG; [07] VERIFIED INSTALLATION OF FCD CUTOUT AFT SHIELD WILL BE PERFORMED ON MOC 5330-E-16461-NG.
RIGHT HAND HORIZONTAL STAIBILIZER INSPAR RIB; 120.30; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] TRIMMED OUT THE DAMAGED PART OF THE RIB AT R/H HORIZ. STAB INSPAR RIB 120.3 3RD VERTICAL STIFFENER; CUT OUT DIMENSIONS 0.5' X 0.250' IAW SRM 55-10-09-2R-4.; [02] TRIMMED OUT THE DAMAGED PART OF THE RIB AT R/H HORIZ. STAB INSPAR RIB 120.3 3RD VERTICAL STIFFENER; CUT OUT DIMENSIONS 0.5' X 0.250' IAW SRM 55-10-09-2R-4. STEP 4B; [10] INSTALLED REPAIR PARTS AT RH HORIZONTAL STABILIZER STA 120.3 RIB 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4; [11] VERIFIED INSTALLATION OF REPAIR PARTS PER SRM 55-10-09-2R-4; [12] CHANGED REPAIR TYPE TO MAJOR; [13] TASK COMPLETE
CORROSION ON FORWARD CARGO BAY AFT BULKHEAD SUPPORT STRAP AT STA 500D; WL 153; RBL 14; RBL 10; LBL 1; LBL 4; LBL 14; LBL 17; LBL 22; LBL 23. ; / [01] REMOVED CORROSION ON SUPPORT STRAP; FWD CARGO BAY AFT BULKHEAD AT STA 500D; WL 153; RBL 14;RBL10;LBL4;LBL14;LBL17;LBL22 AND LBL23. MEASURES RBL14: L=2.550'; W=1.100'; D=0.030'. ORIGINAL THICNESS 0.071'; MATERIAL REMOVED 0.030'; REMAINING MATERIAL THICKNESS 0.041'. THE SUPPORT STRAP IS OUT OF LIMITS. IAW. SRM 53-30-08-1A-1 ALLOWABLE DAMAGE 1; STEP 4.A(2)A. TOOL USED DEPTH GAGE ID: ATS1737; DUE DATE:07/2022.; [02] VERIFIED CORRECTIVE ACTION 1 (OUT OF LIMITS); [03] RECEIVED NEW SUPPORT STRAP; ITEM 143A9485Y35; LOT#1468693. LOCATED AND DRILLED NEW SUPPORT STRAP LOC AT STA 500D. IAW. SRM 51-40-05. OK TO INSTALL.; [04] VERIFIED CORRECTIVE ACTIONS 3; [05] INSTALLATION OF FCB AFT BULKHEAD SUPPORT STRAP STA 500D WL 153 WILL BE PERFORMED ON MOC 5330-E-16461-NG; [06] VERIFIED INSTALLATION OF FCB AFT BULKHEAD SUPPORT STRAP STA 500D WL 153 WILL BE PERFORMED ON MOC 5330-E-16461-NG.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT WL 153; STA500A+2; RBL24; STA500A+6; RBL 25; STA500B+2; RBL 24; STA500B+2; RBL 24; STA500B+6; RBL 25; STA500B+18; RBL 25; STA500C+2; RBL 24; ; STA 500C+2; RBL25; STA500C+7; RBL 24; STA 500C+10; RBL 25. / [01] REMOVED CORROSION TO SIDEWALL SUPPORT BS 500A+2;RBL24; BS500A+6;RBL25; BS 500B+2; RBL24; BS 500+6; RBL25; BS 500B+18; RBL 25; 500C+2 RBL 24; . BS 500B+2 MATERIAL REMOVED L=1''XW=.05''XD.010'' TICKNIES IS .040'' IS OUT LIMITS IAW SRM 53-00-53-1A-2 STEP 4 (2); [02] CORRECTIVE #1 USED TOOL DEPH GAUGE ID: ATS400 DUE 08/2022; [03] VERIFIED CORRECTIVE ACTION ITEM 1 & 2.; [04] REMOVED SIDEWALL SUPPORT PER REF SRM 51-40-02<BR><BR>FABRICATED NEW SIDEWALL SUPPORT RBL24 WL 153 PER REF DWG NBR 143A7501 AND SRM 51-40-05; [05] FABRICATED FLOOR TO SIDEWALL SUPPORT AND SPLICE IAW REF DWG 143A7501 OK TO TREAT AND PRIME <BR>USING LOT NUMBER 5098100-1; [06] JUST SIDEWALL SUPPORT SPLICE WAS FABRICATED ON DIFFERENT NRC; [07] VERIFIED FABRICATED FLOOR TO SIDEWALL SUPPORT AND SPLICE IAW REF DWG 143A7501.<BR>VERIFIED OK TO TREAT AND PRIME.; [08] APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 51-21-72-370-801 AND SRM 51-21-41-370-802; [09] INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG; [10] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 51-21-72-370-801 AND SRM 51-21-41-370-802.<BR>VERIFIED INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG.
CORROSION ON FWD CARGO DOOR CUTOUT FWD SHIELD AT W.L. 153; RBL 24; STA 420 + 6 & STA 420 + 17. ; / [01] REMOVED FWD SHIELD ON FWD CARGO DOOR CUTOUT; WL153; RBL24;DONT HAVE ALLOWABLE DAMAGE IN THE SRM. IAW. SRM 51-10-02-0G-0;STEP 9.; AND SRM 51-40-02-0G-0.; [02] UPDATED PART NUMBER IN MEASUREMENTS SECTION; [03] VERIFIED CORRECTIVE ACTION 1; FOR REMOVAL OF FCB DOOR CUTOUT FWD SHIELD AND THAT DAMAGED SHIELD WILL BE REPAIRED BY REPLACEMENT DUE TO NO SRM LIMITS.; [04] LOCATED AND DRILLED NEW SHIELD P/N 143A8126U21; LOT 1466561-1 IAW SRM 51-40-05 AND DWG 143A0080; [05] VERIFIED CORRECTIVE ACTION ENTRY 4.; [06] INSTALLATION OF FCD CUTOUT FWD SHIELD WILL BE PERFORMED ON MOC 5330-E-16461-NG; [07] VERIFIED INSTALLATION OF FCD CUTOUT FWD SHIELD WILL BE PERFORMED ON MOC 5330-E-16461-NG.
CORROSION ON FWD CARGO L/H FLOOR TO SIDEWALL SUPPORT STRUCTURE AT WL 153 LBL 24 STA 420+10; LBL 25 STA 500A+6; LBL 25 STA 500A+14; LBL 25 STA 500B+2;LBL 24 STA 500B+6; LBL 24 STA 500C+1; ; LBL 25 STA 500C+1; LBL 24 STA 500C+4; LBL 25 STA 500C+6; LBL 24 STA 500C+7. / [01] REMOVED CORROSION AT FCB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-10-02-0G-0; MEASURES L=1.1'' X W=1.0'' X D=0.014 TOOL USED DIGITAL CALIPER ID:ATS2501 S/N:A19335647; MICROMETER ID:ATS1672 S/N:65092939; AND EVALUATED BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PART 4A;; [02] REMOVED FLOOR TO SIDEWALL SUPPORT AT FCB BS400-500D LBL25 WL 153 IAW SRM 51-40-02-0G-0; [03] VERIFIED CORRECTIVE ACTION ITEM 1.; [04] VERIFIED ACCOMPLISHMENT OF STEPS 1-6.; [05] FABRICATED FLOOR TO SIDEWALL SUPPORT AND SPLICE IAW REF DWG 143A7501 AND SRM 53-00-53-2R-6 OK TO TREAT AND PRIME<BR>USING LOT NUMBER 5098100-1; [06] VERIFIED FABRICATED FLOOR TO SIDEWALL SUPPORT AND SPLICE IAW REF DWG 143A7501 AND SRM 53-00-53-2R-6.<BR>VERIFIED OK TO TREAT AND PRIME.; [07] APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 51-21-72-370-801 AND SRM 51-21-41-370-802; [08] INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG; [09] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 51-21-72-370-801 AND SRM 51-21-41-370-802. <BR>VERIFIED INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG.
CORROSION ON FWD CARGO L/H FLOOR TO SIDEWALL SUPPORT STRUCTURE AT WL 153 LBL 25 STA 500C+10; LBL 25 STA 500C+14. ; / [01] REMOVED CORROSION AT FCB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-10-02-0G-0; MEASURES L=1.2'' X W=1.0'' X D=0.010 TOOL USED DIGITAL CALIPER ID:ATS2501 S/N:A19335647; MICROMETER ID:ATS1672 S/N:65092939; AND EVALUATED BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PART 4A;; [02] REMOVED FCB FLOOR TO SIDEWALL SUPPORT BS400-500D LBL25 WL153 IAW SRM 51-40-02-0G-0; [03] VERIFIED CORRECTIVE ACTION ITEM 1.; [04] VERIFIED ACCOMPLISHMENT OF STEPS 1 & 2.; [05] INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG; [06] VERIFIED INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT STA 500C+13; RBL 24; WL 153. ; / [01] REMOVED CORROSION TO SIDEWALL SUPPORT BS 500C+13 RBL 24 REMOVED MATERIAL AREA L=1''XW=.05''XD=.012'' THICKNIE .040'' OUT OF LIMITS PER SRM 53-0053-1A-2 TOOL USED DEPTH GAUGE ID:ATS400 DUE08/2022; [02] REMOVED SIDEWALL SUPPORT PER REF SRM 51-40-02<BR><BR>FABRICATED NEW SIDEWALL SUPPORT RBL24 WL 153 PER REF DWG NBR 143A7501 AND SRM 51-40-05; [03] INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG; [04] VERIFIED INSTALLATION OF FLOOR TO SIDEWALL SUPPORT WILL BE PERFORMED ON MOC 5330-E-16461-NG.
CORROSION ON AFT CARGO R/H FLOOR TO SIDEWALL SUPPORT STRUCTURE AT WL 153 RBL 22 STA 727+10; RBL 22 STA 727A+6; RBL 22 STA 727A+10; RBL 22 STA 727B+2; RBL 22 STA 727B+6; RBL 22 STA 727B+10; ; RBL 22 STA 727B+14; RBL 22 STA 727B+18; RBL 22 STA 727C+2; RBL 22 STA 727C+6. / [01] VERIFIED ACCOMPLISHMENT OF STEPS 1-6.; [02] DAMAGE FOUND AT ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 727+10 TO BS 727B+10 RBL 22 WL 153 FOUND TO BE OUT OFF LIMIT AND WILL BE REPAIRED WITH CUSTOMER CARD #TTG8Q00718SS; [03] VERIFIED DAMAGE FOUND AT ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 727+10 TO BS 727B+10 RBL 22 WL 153 FOUND TO BE OUT OFF LIMIT AND WILL BE REPAIRED WITH CUSTOMER CARD #TTG8Q00718SS.
CORROSION ON AFT CARGO R/H FLOOR TO SIDEWALL SUPPORT STRUCTURE AT WL 153 RBL 22 STA 727C+10; RBL 22 STA 727C+14; RBL 22 STA 727C+18; RBL 22 STA 727D+3; RBL 22 STA 727D+5; RBL 22 STA 727D+6; ; RBL 22 STA 727D+7; RBL 22 STA 727D+10; RBL 20 STA 727D+10; RBL 22 STA 727D+14. / [01] VERIFIED ACCOMPLISHMENT OF STEPS 1-6.; [02] DAMAGE FOUND AT ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 727C+10 TO BS 727D+6 RBL 22 WL 153 FOUND TO BE OUT OFF LIMIT AND WILL BE REPAIRED WITH CUSTOMER CARD #TTG8Q00718SS; [03] VERIFIED DAMAGE FOUND AT ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 727C+10 TO BS 727D+6 RBL 22 WL 153 FOUND TO BE OUT OFF LIMIT AND WILL BE REPAIRED WITH CUSTOMER CARD #TTG8Q00718SS.
CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT STA 727C+8; LBL 20; STA 727C+10; LBL 22; STA 727C+18; LBL 22; STA 727D+6; LBL 22; STA 727D+10; LBL 22; STA 727E+2; LBL 22; STA 727E+8; LBL 20; ; STA 727E+10; LBL 22; STA 727E+14; LBL 22. / [01] VERIFIED ACCOMPLISHMENT OF STEPS 1-9.; [02] DAMAGE FOUND ON ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727C+8 TO BS 727E+8 LBL 22 FOUND TO BE OUT OFF LIMIT AND WILL BE REPLACED WITH CUSTOMER CARD # TTG8Q00718NX; [03] VERIFIED DAMAGE FOUND ON ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727C+8 TO BS 727E+8 LBL 22 FOUND TO BE OUT OFF LIMIT AND WILL BE REPLACED WITH CUSTOMER CARD # TTG8Q00718NX.
CORROSION ON AFT CARGO R/H FLOOR TO SIDEWALL SUPPORT STRUCTURE AT WL 153 RBL 20 STA 727E+2; RBL 22 STA 727E+3; RBL 22 STA 727E+6; RBL 20 STA 727E+8; RBL 22 STA 727E+10; RBL 20 STA 727E+12; ; RBL 22 STA 727E+14; RBL 22 STA 727E+18; RBL 22 STA 747+5. / [01] VERIFIED ACCOMPLISHMENT OF STEPS 1-6.; [02] LOCATED AND DRILLED NEW ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 767; RBL 22; WL 153; MADE FROM EXTRUSION BAC1496-377#7075T62 LOT#5093799-1 IAW SRM 51-40-05-0G-0 AND DWG#146A7502 OK TO TREAT AND PRIME; [03] VERIFIED LOCATED AND DRILLED NEW ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 767; RBL 22; WL 153; MADE FROM EXTRUSION BAC1496-377#7075T62 LOT#5093799-1 IAW SRM 51-40-05-0G-0 AND DWG#146A7502.<BR>VERIFIED OK TO TREAT AND PRIME.; [04] APPLIED CHEMICAL CONVERSION COATING AND PRIMED ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 767 RBL 22 WL 153 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02; [05] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIMED ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 767 RBL 22 WL 153 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02.; [06] INSTALLATION OF ACB FLOOR TO SIDE WALL SUPPORT BS 727 TO BS 767 RBL 22 WL 153 WILL BE ACCOMPLISHED WITH CUSTOMER MOC CARD# TTG8Q004E68F; [07] VERIFIED INSTALLATION OF ACB FLOOR TO SIDE WALL SUPPORT BS 727 TO BS 767 RBL 22 WL 153 WILL BE ACCOMPLISHED WITH CUSTOMER MOC CARD# TTG8Q004E68F.
CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT STA 727E+18; LBL 20; STA 727E+18; LBL 22; STA 747+2; LBL 22; STA 747+5; LBL 20; STA 747+7; LBL 22; STA 747+9; LBL 20; STA 747+14; LBL 22; STA 747+18; ; LBL 22; STA 747+19; LBL 20; STA 767+3; LBL 22. / [01] VERIFIED ACCOMPLISHMENT OF STEPS 1-10.; [02] DAMAGE FOUND ON ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727E+18 TO BS 747+18 LBL 22 FOUND TO BE OUT OFF LIMIT AND WILL BE REPLACED WITH CUSTOMER CARD #TTG8Q00718NX; [03] VERIFIED DAMAGE FOUND ON ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727E+18 TO BS 747+18 LBL 22 FOUND TO BE OUT OFF LIMIT AND WILL BE REPLACED WITH CUSTOMER CARD #TTG8Q00718NX.
CORROSION ON AFT CARGO BAY AFT BULKHEAD SUPPORT STRAP AT STA 947; WL 153; RBL 4 & RBL 6. ; / [01] EVALUATED CORROSION DAMAGE ON AFT BULKHEAD SUPPORT STRAP AT ACB STA 947 WL 153 RBL 4 AND 6 FOUND TO BE OUT OF LIMITS DUE NO LIMITS IN SRM PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTION 1; [11] INSTALLED NEW BULKHEAD SUPPORT STRAP AT AFT CARGO BAY; BS947; RBL4; WL153. IAW SRM 51-40-02-0G-0 AND DWG#149A8117; [12] VERIFIED CORRECTIVE ACTION 11; [13] VERIFIED JOB COMPLETE
CORROSION ON PASSENGER CABIN SEAT TRACK AT B.S. 787+10-807; 827+3-827+15 AND 847+11-847+15; R.B.L. 45.5; W.L. 208.1. ; / [01] COMPLETED STEPS 1;2;3; [02] VERIFIED COMPLETION OF ALL CORROSION REMOVAL STEPS; [03] APPLIED CHEMICAL CONVERSION COATING AND ONE LAYER OF ALUMINIZED EPOXY PRIMER TO REWORKED AREA IAW SRM 51-20-01 AND SOPM 20-41-04; [04] VERIFIED CORRECTIVE ACTIONS 3
CORROSION ON ACB FLOOR SUPPORT AT WL 153; WL 7; STA 767+6 AND STA 767+14. ; CORROSION IS LOCATED AT LBL 7; NOT WL 7. / [01] VERIFIED PARTIAL UPDATES STEP 1; 2.; [02] VERIFIED UPDATED STEPS 1 AND 2 COMPLETE; [03] ALL ITEMS ARE COMPLETE; [04] CORRECTION FOR STEP 2 DAMAGE EVALUATION: LOCATION IS BS 767+14; WL 153; LBL 7; [05] ALL WORK STEPS COMPLETE; REQUESTING FINAL BUYOFF; [06] VERIFIED ALL WORK COMPLETE. VERIFIED CORRECTIVE ACTION 4.
CORROSION ON AFT CARGO R/H FLOOR TO SIDEWALL SUPPORT STRUCTURE AT WL 153 RBL 20 STA 747+8; RBL 22 STA 747+8; RBL 20 STA 747+10; RBL 20 STA 747+12; RBL 22 STA 747+14; RBL 22 STA 747+16. ; / [01] VERIFIED ACCOMPLISHMENT OF STEPS 1-6.; [02] DAMAGE FOUND AT ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 747+8 TO BS 747+14 RBL 22 WL 153 FOUND TO BE OUT OFF LIMIT AND WILL BE REPAIRED WITH CUSTOMER CARD #TTG8Q00718SS; [03] VERIFIED DAMAGE FOUND AT ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 747+8 TO BS 747+14 RBL 22 WL 153 FOUND TO BE OUT OFF LIMIT AND WILL BE REPAIRED WITH CUSTOMER CARD #TTG8Q00718SS.
CORROSION ON AFT CARGO DOOR CUTOUT FWD SHIELD AT STA 767+3; RBL 22; AND STA 767+5; RBL 21. ; / [01] VERIFIED COMPLETE STEPS 1; 2.; [02] RECEIVED NEW SHIELD ITEM:146A8127U12ATSMRO LOT:1467562.<BR>LOCATED AND DRILLED NEW ACB FWD SHIELD IAW SRM 51-40-05-0G-0 AND DRAWING:146A8127.; [03] INSTALLATION OF ACB FWD SHIELD IS DOCUMENTED ON CUSTOMER CARD: CPCP/AD MOC 5360-E-16462-NG CUSTOMER SYSTEM ID:TTG8Q004E68F; [04] ADDED PART NUMBER; [05] VERIFIED LOCATED AND DRILLED NEW ACB FWD SHIELD IAW SRM 51-40-05-0G-0 AND DRAWING:146A8127. <BR>VERIFIED INSTALLATION OF ACB FWD SHIELD IS DOCUMENTED ON CUSTOMER CARD: CPCP/AD MOC 5360-E-16462-NG CUSTOMER SYSTEM ID:TTG8Q004E68F.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 22; WL 153; STA 887+7; AND STA 907+2. ; / [01] VERIFIED COMPLETE STEPS 1; 2.; [02] CORRECTION : DAMAGE IS ON FLOOR TO SIDEWALL SUPPORT AT RBL 22; STA 887 +7 AND STA 907 +2; INSTEAD OF SHIELD.; [03] FABRICATED ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 867 TO BS 947 RBL 22 WL 153 MADE FROM EXTRUSION BAC1496-377#7075T62 LOT#5095753-1 IAW SRM 51-40-05-0G-0 ; DWG#147A7501 AND DWG#146A7502 OK TO TREAT AND PRIME; [04] VERIFIED FABRICATED ACB RH FLOOR TO SIDE WALL SUPPORT ANGLE BS 867 TO BS 947 RBL 22 WL 153 MADE FROM EXTRUSION BAC1496-377#7075T62 LOT#5095753-1 IAW SRM 51-40-05-0G-0 ; DWG#147A7501 AND DWG#146A7502.<BR>VERIFIED OK TO TREAT AND PRIME.; [05] APPLIED CHEMICAL CONVERSION COATING AND PRIMED ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 867 TO BS947 RBL 22 WL 153 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02 ; INSTALLATION WILL BE ACCOMPLISHED WITH CUSTOMER MOC CARD # TTG8Q004E68F; [06] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIMED ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 867 TO BS947 RBL 22 WL 153 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02. <BR>VERIFIED INSTALLATION WILL BE ACCOMPLISHED WITH CUSTOMER MOC CARD # TTG8Q004E68F.
CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT WL 153; STA 767+10; LBL 22; STA 767+14; LBL 22; STA 787+10; LBL 22; STA 787+14; LBL 22. ; / [01] CORRECTED MEASUREMENTS; [02] VERIFIED ACCOMPLISHMENT OF STEPS 1-4.; [03] FABRICATED ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 847 LBL 22 WL 153 WITH SPLICER ANGLE AT BS 727E+10 MADE FROM EXTRUSION BAC1496-377#7075T62 LOT#5095753-1 IAW SRM 51-40-05-0G-0 AND DWG# 146A7502 OK TO TREAT AND PRIME; [04] VERIFIED FABRICATED ACB FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 847 LBL 22 WL 153 WITH SPLICER ANGLE AT BS 727E+10 MADE FROM EXTRUSION BAC1496-377#7075T62 LOT#5095753-1 IAW SRM 51-40-05-0G-0 AND DWG# 146A7502.<BR>VERIFIED OK TO TREAT AND PRIME.; [05] APPLIED CHEMICAL CONVERSION COATING AND PRIMED ACB FLOOR TO SIDE WALL SUPPORT AND SPLICE ANGLE BS 727 TO BS 847 LBL 22 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02 AND WILL BE INSTALLED WITH CUSTOMER MOC CARD# TTG8Q004E68F; [06] VERIFIED APPLIED CHEMICAL CONVERSION COATING AND PRIMED ACB FLOOR TO SIDE WALL SUPPORT AND SPLICE ANGLE BS 727 TO BS 847 LBL 22 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02. <BR>VERIFIED WILL BE INSTALLED WITH CUSTOMER MOC CARD# TTG8Q004E68F.
CORROSION ON PASSENGER CABIN SEAT TRACK AT B.S. 639+9; 663+16 AND 727A+2-727A+10; R.B.L. 45.5; W.L. 208.1 ; / [01] COMPLETED STEPS; [02] VERIFIED COMPLETION OF ALL CORROSION REMOVAL STEPS; [03] APPLIED CHEMICAL CONVERSION COATING AND ONE LAYER OF ALUMINIZED EPOXY PRIMER TO REWORKED AREA IAW SRM 51-20-01 AND SOPM 20-41-04; [04] VERIFIED CORRECTIVE ACTIONS 3
CORROSION ON PASSENGER CABIN SEAT TRACK AT B.S. 578 AND 663.75; L.B.L. 45.5; W.L. 208.1. ; / [01] COMPLETED STEPS 1;2; [02] VERIFIED COMPLETION OF ALL CORROSION REMOVAL STEPS; [03] APPLIED CHEMICAL CONVERSION COATING AND ONE LAYER OF ALUMINIZED EPOXY PRIMER TO REWORKED AREA IAW SRM 51-20-01 AND SOPM 20-41-04; [04] VERIFIED CORRECTIVE ACTIONS 3
LOCK OUT TAG OUT BOX RETAINING BAR BROKEN ; / [01] INSTALLED SLIDE BAR RETAINER PER SIP
AFT CARGO SCUFF PLATE CENTER THRESHOLD OUT OF LIMITS ; / [01] R/R AFTER CARGO DOOR SCUFF PLATE CENTER PER AMM 53-11-02
PASSENGER CABIN ROW 24 ISLE PHOTO LUMINOUS STRIPS RIGHT AND LEFT HAS MOISTURE UNDER COVER / R&R PHOT LUMINOUS STRIPS PER AMM 33-51-15
EMERGENCY SLIDE FWD ENTRY DOOR PRESSURE IN RED. REPLACED FWD ENTRY DOOR SLIDE, PER MT 725-61-06. R & R 74893 P/N OFF/ON:5A3307-7 S/N OFF: BNG12262 S/N ON: BNG11742.
PASSENGER CABIN EVACUATION STRIP MISSING AT AFT WHEEL CHAIR CLOSET AFT OF SEAT 24ABC. / INSTALLED STRIP PER AMM 33-51-15
L/H O/W EMERGENCY LIGHTS INOP / R+R L/H O/W EMERGENCY LIGHTS BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD
EMERGENCY LIGHT WAS OUT FORWARD OF THE AFT CARGO DOOR. / RELAMPED LIGHT PER AMM.
L/H OVERWING EMERGENCY LIGHT INOPERATIVE. / RELAMPED LIGHT IAW AMM.
L/H EMERGENCY LIGHT TEST FAILED BETWEEN SEAT ROW 9 TO ROW 11. / R&R BATTERY PACK PER AMM.
L/H HORIZONTAL STABILIZER RIB #4 CRACK INDICATION AT LOWER FLANGE #10 HOLE FROM AFT ON STIFFENER 4 SIDE. / REPAIRED #4 RIB IAW SRM.
AFT CARGO COMPARTMENT FLOOR SUPPORT STRAP TOP SURFACE CORRODED AT FASTENER HOLES BS. 767. / R&R STRAP IAW SRM.
AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT STRAP HAS EXFOLIATING CORROSION AT STA 887 MKD DOT 60-009 / REMOVED AND REPLACED STRAP AT AFT CARGO COMPARTMENT PER REF 51-40-02-0G-0 AND 51-40-05-0G-0 AND DRAWING 146A9401 (STA 887).
COCKPIT SEAT TRACKS CORRODED PN 226-0202; & 226-0218. / RECEIVED NEW COCKPIT SEAT TRACK WITH PART #226-0204 AND 226-0218 WILL BE INSTALL WITH WORK ORDER #2015322 - 2000-0047 J753-330-00-01Y WITH REFERENCE AS PER AMM 25-11-11-400-801
GALLEY # 1 EMERGENCY EXIT LIGHT LENS WORN. / R&R LIGHT LENS PER AMM.
AFT CARGO COMPARTMENT R/H FLOOR SUPPORT ZEE CHANNEL CORRODED AND CRACKED AT FLANGE FROM STA 727C TO STA 767 / AT AFT CARGO COMPT R/H FLOOR SUPPORT ZEE CHANNEL CRACKED AT FLANGE REMOVED FROM STA 727 TO 767 IAW B737-700 SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW ZEE CHANNEL SECTION IAW B737-700 SRM 51-40-05-0G-0 MAT USED PO #1619098; TREATED AND APPLIED PRIMER PER REF B737-700 SRM 51-20-01-0G-0; INSTALLED NEW ZEE CHANNEL SECTION FROM STA 727 TO 767 IAW B737 SRM 51-40-02-0G-0
R2 LOWER SILL INNER CHORD CORRODED BETWEEN BS. 951 TO BS. 992.8. / R&R INNER CHORD PER SRM & DWG.
R1 DOOR INTERNAL BEAM #4 CRACKED, AT INBOARD MOST HOLE AND BELOW FILLET RADIUS. / R&R #4 BEAM PER SRM & DWG.
LEFT HORIZ STAB RIB 4 STA 120.30 STIFFENER 3 APPEARS TO BE CRACKED AT LWR AREA. 8-46 / PERFORMED HFEC AT LEFT HORIZONTAL STAB RIB #4 STA 120.30 STIFFENER 3; FOUND CRACKED. CUT OUT DAMAGED AREA; PERFORMED HFEC AT CUT OUT (STIFFENER 3) NO CRACK NOTED. LOCATED AND DRILLED REPAIR PARTS (KIT PD:7551022). INSTALLED REPAIR PARTS AT LEFT HORIZONTAL STAB RIB #4 STA 120.30 STIFFENER 3 PER REF B737-700 SRM 55-10-09-2R-5; NDTM PART 6 51-00-00 PROCEDURE 23 AND PROCEDURE 16; B737-700 SRM 51-20-01-0G-0
FORWARD CARGO COMPARTMENT LOWER SILL WEB EXPANDED CORRODED BETWEEN BS. 440 TO S. 492. R&R WEB PER SRM AND DWG.
R/H SIDE VAPOR BARRIER WEB CRACKED AT BS. 663. / REPAIRED WEB PER SRM.
OVERHEAD EXIT LIGHT WAS HANGING DOWN. R&R LIGHT ASSEMBLY IAW AMM.
L1 DOOR SURROUND EMERGENCY LIGHTS INOP. R&R BATTERY IAW AMM.
R1 DOOR SLIDE EMERGENCY LIGHTS INOP. R&R BATTERY IAW AMM.
R1 DOOR SLIDE EMERGENCY LIGHTS INOP. R&R BATTERY CHARGER IAW AMM.
RT STOWBINS EMERGENCY LIGHTS INOP BETWEEN ROW 1 AND ROW 2. R&R BATTERY IAW AMM.
RT STOWBINS EMERGENCY LIGHTS INOP BETWEEN ROW 1 AND ROW 2. R&R BATTERY CHARGER IAW AMM.
L1 DOOR SURROUND EMERGENCY LIGHTS INOP. R&R BATTERY CHARGER IAW AMM.
RT WHEEL WELL FORWARD BULKHEAD VAPOR BARRIER CRACKED BETWEEN RBL 31.83 TO RBL 45.64. REPAIRED BARRIER IAW EA AND SRM.
COMTINUED FROM LOG 0763478 REF. LOG 0763478 RT. WHEEL WELL FWD BULK HEAD UPPER BARRIER HAS 7.5' CRACK BETWEEN RBL 31.83 & RBL 45.64. / CONTINUED FROM LOG 0763478; ALLOWABLE DAMAGE LIMIT. APPLY THE INTERIM SEAL OVER THE CRACK THAT IS LEFT AS GIVEN IN 737-700 SRM 57-10-10 PARAGRAPH 2.C.(4) ALLOWABLE DAMAGED; PERMANENT REPAIR TIME LIMIT 600 FLIGHT CYCLES.
R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER EA.
L2 DOOR ESCAPE SLIDE BLOCK ASSEMBLY LATCH BROKEN. R&R SLIDE PER MT.
LT OVERHEAD OVERWING EXIT SIGN MISSING. INSTALLED COVER PER SIP.
L2 DOOR EMERGENCY LIGHT SEGMENT INOP. R&R LIGHT PER AMM.
LT OVER WING EMERGENCY EXIT LIGHT SEGMENT INOP. R&R LIGHT PER AMM.
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.
LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.
RUDDER BALANCE ARM WEIGHT CORRODED / REPLACED RUDDER BALANCE WEIGHT IAW CMM 55-40-09 STEP 3A 1&2
L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.
R1 DOOR EXTERIOR SLIDE LIGHT INOP. R&R LIGHT IAW AMM.
LT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663. REPAIRED WEB IAW SRM.
MID CABIN EMERGENCY EXIT LIGHT LOOSE. SECURED THE LIGHT ASSY IAW MM.
MID CABIN OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER SIP.
AIR TURNBACK, NR 1 ELECTRIC OVERHEAT LIGHT ILLUMINATED INFLIGHT. R&R NR 1 ELECTRIC HYDRAULIC PUMP IAW AMM.
FORWARD ENTRY LOWER EMERGENCY EXIT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.
LEFT FORWARD CABIN BATTERY PACK FAILED THE TIME TEST FOR BATTERY PACK CAPACITY. R & R THE BATTERY PACK IAW AMM.
LEFT MID CABIN BATTERY PACK FAILED THE TIME TEST FOR BATTERY PACK CAPACITY. R & R BATTERY PACK IAW AMM.
SKIN CORRODED IN AFT CARGO THRESHOLD SCUFF PLATE DOME NUT HOLES. REPAIRED SKIN EA.
OVERWING EMER EXIT LIGHT CONNECTOR DAMAGED. R & R CONNECTOR IAW SWPM.
LEFT HORIZONTAL STABILIZER SECOND VERTICAL RIB FRONT CRACKED AT STATION 92.70. REPAIRED RIB IAW SRM.
LEFT HORIZONTAL STABILIZER CRACKED, BETWEEN SECOND & THIRD VERTICAL RIB FRONT SPAR AT STATION 92.70. REPAIRED RIB IAW SRM.
LEFT HORIZONTAL STABILIZER THIRD VERTICAL RIB FRONT CRACKED AT STATION 92.70. REPAIRED RIB IAW SRM.
INTERCOSTAL CRACKED, BETWEEN BS 328 - 344, LBL 45. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, LBL 45. R & R INTERCOSTAL IAW SRM.
CABIN RT AFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.
LEFT FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW MM.
CABIN LT AFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW MM.
MID CABIN OVERHEAD EMER EXIT SIGN LOOSE. SECURED SIGN IAW MM.
R2 DOOR EMER EVAC SLIDE GIRT BAR HOOK BROKEN. REPAIRED HOOK IAW SRM & MT.
MOST FWD BULLNOSE EMER LIGHT INOPERATIVE. RELAMPED IAW MM.
MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, RBL 42. REPAIRED WEB IAW SRM.
AFT CARGO FLOOR SUPPORT ANGLE CORRODED AFT END OF AFT FLOOR BOARD AT STATION 947. R & R ANGLE IAW SRM.
LT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 184.70, 10 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.
LT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 157.10, 16 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.
LT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 157.10, 10 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.
LT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 101.90, 20 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.
RT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 157.10, 17 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.
RT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 157.10, 10 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.
RT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 129.50, 27 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.
RT HORIZONTAL STABILIZER SKIN LOWER SIDE CRACKED AT STATION 184.70, 10 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.
LT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.
RT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.
RT EMERGENCY EXIT LENS MISSING. R&R LENS IAW AMM.
R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW SIP.
FLOOR PANEL SUPPORT CRACKED AT BS 540, BL0. R & R SUPPORT IAW SRM.
LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED 0.75" INBD OF RIB AT STAB STA 101.90. REPAIRED SKIN IAW SRM.
LOWER RIGHT OVERWING EXIT SIGN BROKEN. REPLACED EXIT SIGN COVER IAW MM.
L1 DOOR EMERGENCY EXIT SIGN COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER M/M.
L2 DOOR EMERGENCY EXIT LIGHT WIRE OUT OF POSITION BEHIND L2 DOOR. REPOSITIONED WIRE IAW M/M.
LT EMERGENCY LIGHT COVER CRACKED AT ROW 23. REMOVED AND REPLACED COVER PER M/M.
EMERGENCY LIGHT INOP AT ROW 1ABC. RELAMPED LIGHT PER M/M.
LT EMERGENCY LIGHT COVER CRACKED BETWEEN ROW 4 TO ROW 7. REMOVED AND REPLACED COVER PER M/M.
COVER LOOSE FROM ESCAPE LIGHT SYSTEM ON FLOOR STRIP AT ROW 1. REMOVED AND REPLACED COVER PER M/M.
LT EEPLS COVER MISSING AT ROW 1. INSTALLED LENS IAW MM.
EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER BROKEN AT ROW 11. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC1 CHECK, FOUND LT EMERGENCY EXIT LIGHT BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED HC1 CHECK, FOUND RT EMERGENCY EXIT LIGHT BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PER MM.
LT EEPLS COVER MISSING AT ROW 11. REMOVED AND REPLACED COVER PER MM.
EEPLS COVER MISSING AT ROW 2. INSTALLED COVER PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER LOOSE. REMOVED AND REPLACED COVER PER MM.
LOOSE WIRE ON EEPLS. SECURED WIRE PER MM.
LT EEPLS OUT OF POSITION AT ROW 1. REPOSITIONED EEPLS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.
DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
ROW 1 EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.
LT EEPLS COVER BROKEN AT ROW 12. REMOVED AND REPLACED COVER PER MM.
LEFT EEPLS LENS LOOSE AT ROW 1. REMOVED AND REPLACED LENS PER MM.
FWD EEPLS LENS MISSING. INSTALLED LENS PER MM.
RT AFT GALLEY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.
R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.
DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP INOP. REMOVED AND REPLACED SLIDE PER MT.
THIRTY MINUTES PRIOR TO ARRIVAL IN FLL, FLT ATTENDANTS SMELLED OILY/RUBBER ODOR WITH VIBRATION CENTERED OVER ROW 9, RT SIDE. FOUND RT PACK ACM SEIZED. REMOVED AND REPLACED RT ACM PER MM.
DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.