N232WN
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 | 2015-08-23 – 2015-08-23 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2015-08-23 – 2015-08-23 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AFTER ENTRY GIRT BAR DOES NOT SEAT FIRMLY IN CLIPS. INSPECTED AND CLEANED AFT ENTRY GIRT BAR. OPS CHKD GOOD IAW SIP.
FWD SERVICE SLIDE CONTAINER AFT BRACKET IS LOOSE THAT HOLDS GIRT BAR FWD SERVICE DOOR SLIDE CONTAINER AFT BRACKET IS LOOSE THAT HOLDS GIRT BAR. R&R FASTENERS ON BRAKET IAW SRM 51-40-02.
RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R RT OVERWING EMERGENCY EXIT LIGHT BULB AND LENS IAW AMM 33-51-04. OPS CHECKED GOOD.
CRACKED STRINGER CLIP AT PAX CABIN BS 727B, S7L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1102 REV -.
CORROSION ON STRAP AT MID CABIN, BS 709, LBL 63, WL 203. REFER TO FAULT TTG8Q013SLHA WHERE EA 25-153-01977 WAS ADDED AS A SUBTASK.
CORROSION ON STRAP AT MID CABIN, BS 713, LBL 64 - LBL 67, WL 203. REFER TO FAULT TTG8Q013SLHA WHERE EA 25-153-01977 WAS ADDED AS A SUBTASK.
CORROSION ON STRAP AT MID CABIN BS 703, LBL 68, WL 203. REFER TO FAULT TTG8Q013SLHA. EA 25-153-01977.
CORROSION ON STRAP AT MID CABIN BS718 RBL62 WL203. CORROSION ON STRAP AT MID CABIN BS718 RBL62 WL203 REPAIRED PER EA 25-153-01971-WIP1.
CRACKED PANEL BREAK AT PASSENGER CABIN BS 540, LBL 26, WL 208. REPLACED PANEL BREAK IAW SRM 51-40-02, AND BOEING DWG 143A0060 REV:-;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
CRACKED PANEL BREAK AT PASSENGER CABIN BS 540, LBL 1, WL 208. REPLACED PANEL BREAK PASSENGER CABIN BS540 LBL1 IAW SRM 51-40-02 AND DWG 143A0060 REV-.
CORROSION ON STRAP AT MID CABIN BS692 LBL68 WL203. REMOVED CORROSION ON STRAP BS 692, LBL 68, WL 203 AND ACCOMPLISHED REWORK OF STRAP IAW EA 25-153-01977.
CORROSION ON AFT BULKHEAD SUPPORT BS 947; RBL 20; WL 160. REMOVED AND REPLACED AFT BULKHEAD SUPPORT STA 947. STR 25L-STR 25R IAW SRM 51-40-02; DWG 149A8117 REV:- AND DWG 149A8110 REV:A.
CORROSION ON AFT CARGO COMPARTMENT FWD SHIELD BS 767-787, RBL 22, WL 156-157. INSTALLED NEW SHIELD IAW SRM 51-40-02, 51-40-05, AND DWG 146A8127 REV -.
CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT STA 727+4-767 RBL 22; WL 156. REMOVED OLD AND INSTALLED NEW AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT BS A 727+4 - 767 RBL 22; WL 156 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; BOEING DWG 146A7500 REV:A; BOEING DWG 146A7502 REV:-.
MAIN CABIN SEAT TRACK LBL 45 AT STA 540 AND STA 727+12 APPROX. WAS FOUND MECHANICAL DAMAGE ON CROWN. AND AT STA 559+10 APPROX. WAS FOUND CORROSION ON WELL. SEAT TRACK FOUND TO BE OUT OF LIMITS ON FAULT TTG8Q013QT63 AND WILL BE REPLACED ON TTG8Q013QT63.
MAIN CABIN SEAT TRACK LBL 45 AT STA 616+18 APPROX.; BS 663; BS 663+12 APPROX.; STA 685+12 APPROX. AND AT STA 727A+10 APPROX. WAS FOUND CORRODED ON CROWN. REMOVED CORROSION ON SEAT TRACK BS 540-727 LBL 45 FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02-0G-0 AND DWG 144A5300 REV E.
CORROSION ON AFT CARGO COMPARTMENT FLOOR TIEDOWN STRAP STA 887; BETWEEN FLOOR PANELS 140CF-140DF. REMOVED AND REPLACED SPLICE / TEE ASSY IAW SRM 51-40-05 AND DWG 146A7500 REV A.
CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT STA 887+4-887+12; 907+2; RBL 22; WL 159. REMOVED AND REPLACED ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT STA 867 TO 887 PER SRM 51-40-02; 51-40-05 AND BOEING DWG 147A7500REV -.
CORROSION ON AFT CARGO COMPARTMENT L/H FLOOR TO SIDEWALL SUPPORT BS 727+4 - 787+1-10, LBL 22, WL 156. REMOVED AND REPLACED AFT CARGO COMPARTMENT LT FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, DWG 146A7500 REV:B, DWG 146A7502 REV-, AND SRM 51-40-05-0G-0.
CORROSION ON FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BS 500A-500D; RBL 22; WL 157. REMOVED AND REPLACED SIDEWALL SUPPORT IAW SRM 51-4-02 AND DWG 143A7500 REV-.
CORROSION ON FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BS 400-500D, LBL 22, WL 157. SUPPORT HAS MISSING FASTENER AND IS NOT DRILLED AT BS 396, LBL 22, WL 157. DRILLED HOLE AND INSTALLED FASTENER IAW SRM 51-40-05, SRM 51-40-02, AND DWG 143A7500 REV-. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS 400-500D, LBL 22; WL 157 IAW SRM 51-40-02 AND DWG :143A7500 REV-.
CORROSION ON FWD CARGO COMPARTMENT SHIELD BS 500+6, 500+10, RBL 22, WL 156. CORROSION FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2. REPAIR BY REPLACEMENT IAW SRM 51-10-02<BR>REMOVED DAMAGED SHIELD IAW SRM 51-40-02. INSTALLED A NEW SHIELD IAW SRM 51-40-02 AND DWG 143A0080 REV-.
CORROSION ON AFT CARGO COMPARTMENT AFT SHIELD BS 847-867, RBL 22, WL 157. NO ALLOWABLE DAMAGE GIVEN FOR THIS PART IN SRM 53-00-53-1A-2. REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0, STEP 9. REMOVED DAMAGED SHIELD AND INSTALLED A NEW SHIELD IAW SRM 51-40-02 AND DWG 146A0081 REV -.
CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT BS 867+10, 867+15-16, RBL 22, WL 158. REMOVED AND REPLACED ON AFT CARGO COMPARTMENT R/H FLOOR SIDEWALL SUPPORT BS 867 TO 887 IAW SRM 51-40-02, AND 51-40-05 AND DWG 146A7500 REV A.
CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. REMOVED DAMAGED STRINGER S-26L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT STRINGER 26L BS 540-BS 500D+10 IAW SRM 53-00-03-2R-1; SRM 51-40-02 DWG143A3230 REV A.
CRACKED STRINGER AT AREA AFT OF FCB BS 535, S-23L, WL164. REMOVED DAMAGED STRINGER S-23L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT STRINGER 23L BS 540-BS 500D+10 IAW SRM 53-00-03-2R-1; SRM 51-40-02 DWG143A3210 REV B.
CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. REMOVED DAMAGED STRINGER S-26L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT STRINGER 26L BS 540-BS 500D+10 IAW SRM 53-00-03-2R-1; SRM 51-40-02 DWG143A3230 REV A.
RIGHT WING T/E WIGGLE PLATE AT ORSS 261 IS CRACKED.
CRACKED STRINGER AT AREA AFT OF FCB BS535 S-23L WL164. REMOVED DAMAGED STRINGER S-23L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT STRINGER 23L BS 540-BS 500D+10 IAW SRM 53-00-03-2R-1; SRM 51-40-02 DWG143A3210 REV B.
CRACK FOUND ON STUB FRAME BS 294.5 +8.5'; ABOVE SEAL DEPRESSOR, BETWEEN S8R AND S9R; LENGTH 1.4'. REMOVED OLD FWD SERVICE DOOR STUB FRAME BS 294 +8.5' IAW SRM 51-40-02-0G-0 AND INSTALLED NEW FWD SERVICE DOOR STUB FRAME IAW SRM 51-40-02-0G-0 AND DWG 141A8370 REV. D.
FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE PER SRM 53-30-15-2R-1, SOPM 20-43-03, SOPM 20-41-02;
AFT SERVICE DOOR SURROUND ASSIST HANDLE IS BROKEN.
L/H HORIZONTAL STAB REMOVABLE L/E; 4TH RIB FROM I/B END IS CRACKED. REMOVED AND REPLACED 4TH RIB FROM I/B END OF L/H HORIZONTAL STAB. L/E IAW SRM 51-40-02-0G-0 PARA. 4.
L/H HORIZONTAL STAB REMOVABLE L/E; 3RD RIB FROM I/B END IS CRACKED. REMOVED AND REPLACED 3RD RIB FROM I/B END OF L/H HORIZONTAL STAB. L/E IAW SRM 51-40-02-0G-0 PARA. 4.
L/H HORIZONTAL STAB REMOVABLE L/E; 5TH RIB FROM I/B END IS CRACKED. REMOVED AND REPLACED 5TH RIB FROM I/B END OF L/H HORIZONTAL STAB. L/E IAW SRM 51-40-02-0G-0 PARA. 4.
PASSENGER CABIN FLOOR PANEL 242CF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 242CF WITH AREAS OF UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0125.
PASSENGER CABIN FLOOR PANEL 231YF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 231YF IAW SRM 53-00-50-2R-0 AND BOEING DRAWING 144A5810 SHEET 124..
PASSENGER CABIN FLOOR PANEL 231XF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 231XF IAW SRM 53-00-50-2R-0 AND BOEING DRAWING 144A5810 SHEET 126.
PASSENGER CABIN FLOOR PANEL 242AF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATION OF NEW 242AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0-A00938, REPAIR GENERAL.
PASSENGER CABIN FLOOR PANEL 242BF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 242BF IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0122.
PASSENGER CABIN FLOOR PANEL 241EF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241EF WITH AREAS OF DELAMINATION ON UPPER SKIN WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810-129.
PASSENGER CABIN FLOOR PANEL 241FF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241FF WITH AREAS OF UPPER SKIN DELAMINATION WAS REPLACED BY FABRICATING A NEW BOARD IAW SRM 53-00-50-2R-0 AND DWG 144A5810-131.
RIGHT HORIZONTAL STAB RIB 5 STIFFENER HAS CRACK ON LOWER RADIUS. REPAIRED RT HORIZONTAL STAB RIB 5, STAB STA 129.5 IAW SRM 51-40-2-0G-0 AND SRM 55-10-09-2R-4 REPAIR 4; FIG. 202; DETAIL.
PASSENGER CABIN FLOOR PANEL 232SF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 232SF IAW SRM 53-00-50-2R-0 AND DWG 144A5810 SHEET 159.
PASSENGER CABIN FLOOR PANEL 241AF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241AF WITH AREAS OF UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810-127.
PASSENGER CABIN FLOOR PANEL 241BF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241BF WITH AREAS OF UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810-189.
L/H ENGINE INLET COWL BARREL SKIN HAS A PULLED THROUGH FASTENER AT 10:00 O'CLOCK POSITION.NR 1 ENGINE INLET COWL WAS REMOVED AND REPLACED ON CARD 7111-E-17062-NG. FAULT WAS ATTACHED TO R/O AND WILL BE CORRECTED WHEN INLET COWL GETS MODIFIED.
RAMP REPORTS. EMERGENCY LIGHT LENSE DISPLACED AIRCRAFT LEFT AFT<[01] SECURED EMERGENCY LIGHT LENSE REF SIP
EMERGENCY AREA LIGHT AMS AT 9ABC AND 18DEF INOP <[01]. 01 - REMOVED AND REPLACED EMERGENCY AREA LAMPS AT 9ABC AND 18DEF PER [AMM 33-51-03-960-801-NG (AREA LIGHT - LAMP REPLACEMENT - PERMANENT)].
#2 ENGINE FAILED ON APPROACH TO RUNWAY 22@ HOU.<[01] PERFORMED FIM TASK 73-06 TASK 812 DUE TO LOSS OF THRUST ON #2 ENGINE FOUND INTERNAL EEC FAULT AND R/R #2 ENGINE EEC REF MM 73-21-60 OPS CHECK GOOD. ALSO VISUALLY INSPECTED FUEL PUMP DRIVE SHAFT REF MM 73-11-01 NO DEFCETS NOTED AND CHECKED WIRING BETWEEN #2 TRA RESOLVER AND #2 EEC REF WD 73-21-21 NO DEFECTS NOTED
M1668 AND M1669 FAILED CAPACITY CHECK<[01] R/R M1668 AND M1669 BATTERY PACK PER AMM 33-51-06
M1675 AND. M1674 FAILED CAPACITY CHECK<[01] R/R M1675 AND M1674 BATTERY. PACK PER AMM 33-51-06
M1673 AND M1672 FAILED CAPACITY CHECK<[01] R/R M1673 AND M1672 BATTERY PACKS PER AMM 33-51-06
M1670 FAILED CAPACITY CHECK<[01] R/R M1670 BATTERY PACK PER AMM 33-51-06
FWD MEGAPHONE CRACKED<[01] R/R FWD MEGAPHONE IAW AMM 25-64-00.
EMERGENCY LIGHT AT ROW 11DEF AND 22DEF INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BULBS AT ROWS 11DEF AND 22DEF IAW AMM 33-51-03. OPS CHECKED GOOD
R/H AFT O/B TRAILING EDGE FLAP DISBONDED<[01] APPLIED PERMANENT REPAIR PER SRM 51-70-10.
AFT ENTRY DOOR ESCAPE SLIDE DISLODGED (CAPT SIDE)<[01] ADJUSTED AND REINSTALLED AFT ENTRY DOOR SLIDE PER MM25-66-01.
LEFT OVERWING EXIT DOOR SIGN LENS BROKEN<[01] REPLACED EXIT SIGN ASSY BASE PER MM 33-51-01
CORROSION ACCESS PANEL 193AL BODY FAIRING STRUCURE AT LOWER FUSELAGE 2023-447822<[01] REPLACED FRAME LOC ON BODY FAIRING STRUCTURE AT LOWER FUSELAGE AND FASTENERS IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 149A7216 SHEET 7 REV-A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] COMPLETED JOB
CORROSION ACCESS PANEL 193AR BODY FAIRING STRUCTURE AT LOWER FUSELAGE 2023-447823<[01] REPLACED FRAME LOC ON BODY FAIRING STRUCTURE AT LOWER FUSELAGE AND FASTENERS IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 149A7216 SHEET 7 REV-A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFF BELOW
CRACK ON BRACKET ASSY OF ACCESS PANEL I/B FIXED TRAILING<BR>EGDE AT LT WING 2023-447819<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 25-JAN-24;[02] REPLACED FASTENERS AND BRACKET ASSY OF ACCESS PANEL I/B FIXED TRAILING EGDE AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2511 SHEET 9 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED FASTENERS AND BRACKET ASSY OF ACCESS PANEL I/B FIXED TRAILING EGDE AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2511 SHEET 9 REV-. SEE INDIVIDUAL SIGN OFF BELOW
BROKEN ACCESS PANEL I/B FIXED TRAILING EGDE AT LT WING 2023-447802<[01] TOOL USED CALIPER PN: 500-197-30; SN: 15120589; DUE DATE: 13/FEB/24.;[02] TOOL USED HOT BONDER PN: HCS9000B; SN: 18175469; DUE DATE: 24/SEP/23.;[03] TOOL USED SCALE PN: CR5200; SN: 8343110765; DUE DATE: 20/FEB/24.;[04] TOOL USED: SCALE: P/N:CR5200 S/N:8343110809 DUE DATE:21-FEB-24.;[05] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 24-JAN-24.;[06] TOOL USED: HOT BONDER PN: HCS9000B-AV SN: 18185761 DUE DATE: 24/SEP/23.;[07] TOOL USED BONDMASTER EQUIPMENT PN: BONDMASTER 600M; SN:220052310; DUE DATE:31-OCT-23;[08] TOOL USED MULTIMETER PN: FLUKE 87; S/N: 37640208; DUE DATE: 24-FEB-24;[09] REPAIRED ACCESS PANEL I/B FIXED TRAILING EGDE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGN OFF BELOW.;[10] JOB TASK COMPLETED.
WEAR ON EMERGENCY DOOR BOLT(1EA) AND NUT(1EA) THAT ATTACH INTERIOR HANDLE RH SIDE AT PASSENGER CABIN 2023-447794<[01] REPLACED ON EMERGENCY DOOR BOLT(1EA) AND NUT(1EA) THAT ATTACH INTERIOR HANDLE RH SIDE AT PASSENGER CABIN IAW SOPM 20-50-01 REV.38;[02] TASK CARD COMPLETED
BROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2023-447744<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) I.A.W AMM 33-51-15-400-802.;[02] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) I.A.W AMM 33-51-15-400-802
DELAMINATED WING TO BODY FAIRING ACCESS PANEL 193B INTERNAL AREA AT MAIN WHEEL WELL COMPARTMENT 2023-447751<[01] TOOL USED= CALIPER P/N: 500-196-30; S/N:A20231600; DUE DATE: 12-SEP-23;[02] TOOL USED= HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 26-MAR-24;[03] TOOL USED= SCALE P/N: CR5200; S/N: 8342514563; DUE DATE. 20-FEB-24;[04] REPAIRED WING TO BODY FAIRING ACCESS PANEL 193B INTERNAL AREA AT MAIN WHEEL WELL COMPARTMENT AS PER B737-700 SRM 53-40-70-2R-1 REPAIR 1 . AND B737-700 SRM 51-70-04-2R-2 REPAIR 2. TOOL USED .CALIPER P/N: 500-196-30; S/N:A20231600; DUE DATE: 12-SEP-23. HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 26-MAR-24. SCALE P/N: CR5200; S/N: 8342514563; DUE DATE. 20-FEB-24. SEE INDIVIDUAL SIGN OFFS BELOW.;[05] REPAIRED WING TO BODY FAIRING ACCESS PANEL 193B INTERNAL AREA AT MAIN WHEEL WELL COMPARTMENT AS PER B737-700 SRM 53-40-70-2R-1 REPAIR 1 . AND B737-700 SRM 51-70-04-2R-2 REPAIR 2. TOOL USED .CALIPER P/N: 500-196-30; S/N:A20231600; DUE DATE: 12-SEP-23. HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 26-MAR-24. SCALE P/N: CR5200; S/N: 8342514563; DUE DATE. 20-FEB-24. SEE INDIVIDUAL SIGN OFFS BELOW.
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 289 AT LT WING 2023-447715<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 289 AT LT WING I.A.W. B737-700 SRM 51-40-02;[02] TASK CARD COMPLETED
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 212 AT LT WING TASK CARD 2023-447712<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 212 AT LT WING I.A.W. B737-700 SRM 51-40-02;[02] TASK CARD COMPLETED
CRACK FRAME ON BS 947.5 LBL 8.10 AFT CARGO COMPARTMENT 2023-447661<[01] REPLACED FRAME LOCATED ON BS 947.5 BTW STR 23L TO STR 23R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING: 147A1047 REV: -. SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK CARD COMPLETED <BR>REPLACED FRAME LOCATED ON BS 947.5 BTW STR 23L TO STR 23R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING: 147A1047 REV: -. SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII
CRACK ON ANGLE LOCATED 12 INCHES OF AFT EDGE AND 17 INCHES OF LOWER EDGE AT OUTBOARD FAN COWL 2023-447695<[01] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[02] PERFORMED HFEC AND CONFIRMED NO CRACK ON ANGLE LOCATED 12 INCHES OF AFT EDGE AND 17 INCHES OF LOWER EDGE AT OUTBOARD FAN COWL; RESTORED PROTECTIVE FINISH IAW B737-700 SRM 51-20-01. SEE INDIVIDUAL SIGN OFF BELOW.;[03] TASK CARD COMPLETED <BR>PERFORMED HFEC AND CONFIRMED NO CRACK ON ANGLE LOCATED 12 INCHES OF AFT EDGE AND 17 INCHES OF LOWER EDGE AT OUTBOARD FAN COWL; RESTORED PROTECTIVE FINISH IAW B737-700 SRM 51-20-01. SEE INDIVIDUAL SIGN OFF BELOW.
CRACK TRAILING EDGE BEAM ASSY LOCATED ORSS 275 AT RT WING 2023-447667<[01] REPLACED BEAM ASSY LOCATED ON TRAILING EDGE ORSS 275 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 115A3712; SHEET: 7; REV: A. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED BEAM ASSY LOCATED ON TRAILING EDGE ORSS 275 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 115A3712; SHEET: 7; REV: A. SEE INDIVIDUAL SIGN OFF BELOW
CRACK TRAILING EDGE TEE ANGLE LOCATED ORSS 273 AT RT WING 2023-447668<[01] REPLACED TRAILING EDGE TEE ANGLE LOCATED ON ORSS273 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A3700 REV.- SHEET 41 DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B7377-700 57-51-02 <BR><BR>CRACK LENGTH: 1.956? <BR><BR>TOOL USED CALIPERP/N: 500-752-20 S/N: B21014901 DUE DATE: 20/SEP/23;[02] REPLACED TRAILING EDGE TEE ANGLE LOCATED ON ORSS273 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A3700 REV.- SHEET 41 DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B7377-700 57-51-02 <BR><BR>CRACK LENGTH: 1.956? <BR><BR>TOOL USED CALIPERP/N: 500-752-20 S/N: B21014901 DUE DATE: 20/SEP/23
CRACK FLAP TRACK FAIRING 7 INTERNAL AND EXTERNAL SKIN LOCATED AT 44IN FROM AFT EDGE AT RT WING (REFER TO FAULT TTG8Q00BE1UM) 2023-447704<[01] TOOL USED; CALIPER PN: 500-464; S/N: B17030933; DUE DATE: 17/OCT/2023.;[02] REPAIRED FLAP TRACK FAIRING 7 (643BB) INTERNAL AND EXTERNAL SKIN IAW EA # 23-157-02310. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] STEPS 1 AND 2 ENTERED IN ERROR; <BR><BR>CORRECT STEP: REPAIRED FLAP TRACK FAIRING 7 (643BB) INTERNAL AND EXTERNAL SKIN IAW EA # 23-157-02310. TOOL USED; CALIPER PN: 500-464; S/N: B17030933; DUE DATE: 17/OCT/23. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] CORRECTIVE ACTION COMPLETED: REPAIRED FLAP TRACK FAIRING 7 (643BB) INTERNAL AND EXTERNAL SKIN IAW EA # 23-157-02310. TOOL USED; CALIPER PN: 500-464; S/N: B17030933; DUE DATE: 17/OCT/23. SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK ANGLE BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R AFT POSITION AFT CARGO COMPARTMENT 2023-447605<[01] REPLACED ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R AFT POSITION AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV.-<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R AFT POSITION AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV.- RII CERTIFIED
CORROSION LOWER SILL BTW BS 787 TO BS 847 RBL 24 WL 159 AFT CARGO COMPARTMENT 2023-447612<[01] EQUIPMENT P/N 45MG; S/N 221859911; DUE DATE 07-NOV-23 WAS USED;[02] REMOVED CORROSION AND EVALUATE REWORK LOWER SILL BTW BS 787 TO BS 847 RBL 24 WL 159 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-60-15-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH 4(G)(2)(B) FIGURE 103 DETAIL G AND FOUND WITHIN LIMITS SEE INDIVIDUAL SIGN OFF BELOW;[03] JOB COMPLETED
CRACK ANGLE BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R FWD POSITION AFT CARGO COMPARTMENT 2023-447604<[01] REPLACED ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R FWD POSITION AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV.- <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R FWD POSITION AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV.- RII CERTIFIED
CRACK ANGLE BS 867 LBL 12.5 WL 164 AFT CARGO COMPARTMENT 2023-447603<[01] REPLACED ANGLE LOCATED BS 867 LBL 12.5 WL 164 AFT CARGO COMPARTMENT. IAW. B737-700 SRM 51-40-02; DWG: 149A8102 SHEET:17 REV:- MEASURE OF CRACK L:1.000?. TOOL USED CALIPER P/N:700-113-10 SN:0023244 DUE DATE: 05-DEC-2023.;[02] REPLACED ANGLE LOCATED BS 867 LBL 12.5 WL 164 AFT CARGO COMPARTMENT. IAW. B737-700 SRM 51-40-02; DWG: 149A8102 SHEET:17 REV:- MEASURE OF CRACK L:1.000?. TOOL USED CALIPER P/N:700-113-10 SN:0023244 DUE DATE: 05-DEC-2023.
CRACK TRACK RBBL 13.84 BS 767 AFT CARGO COMPARTMENT 2023-447614<[01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN 220272712; DUE DATE 17-DEC-23;[02] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 220273012; CAL DUE DATE: 17-DEC-23.;[03] REPAIRED TRACK LOCATED ON RBBL 13.84 BS 767 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 AND B737-700 SRM 51-10-02.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[04] CORRECTED ITEM 3: REPAIRED TRACK LOCATED ON RBBL 13.84 BS 767 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ITEM 4 (P) FIGURE 203 SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPAIRED TRACK LOCATED ON RBBL 13.84 BS 767 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ITEM 4 (P) FIGURE 203 SEE INDIVIDUAL SIGN OFF BELOW.ITEM RII
BROKEN EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA 2023-447522<[01] REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(7)(10);[02] REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(7)(10). JOB COMPLETED.
CRACK ON FRAME LOCATED BS 787 BTW STR 8R TO 9R AT PASSENGER CABIN 2023-447565<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512 AND DUE DATE: 17-DEC-23.;[02] PERFORMED HFEC ON AREA AND NOT FOUNS CRACK INDICATION; INSTALLED BRACKET AND FASTENER ON FRAME LOCATED BS787 BETWEEN STR 8R TO STR 9R I.A.W B737-700 SRM 51-40-02. AND DRAWING #146A1133REV: - .SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] CORRECTED STEP 2<BR>CORRECTED ITEM 1 PERFORMED HFEC INSPECTION ON AREA AND NOT FOUND CRACK INDICATION; INSTALLED BRACKET AND FASTENER ON FRAME LOCATED BS787 BETWEEN STR 8R TO STR 9R I.A.W B737-700 SRM 51-40-02. AND DRAWING #146A1133REV:- .SEE INDIVIDUAL STEP SIGN OFFS BELOW;[04] PERFORMED HFEC INSPECTION ON AREA AND NOT FOUND CRACK INDICATION; INSTALLED BRACKET AND FASTENER ON FRAME LOCATED BS787 BETWEEN STR 8R TO STR 9R I.A.W B737-700 SRM 51-40-02. AND DRAWING #146A1133REV:- .SEE INDIVIDUAL STEP SIGN OFFS BELOW ITEM RII
CRACK ON SUPPORT ANGLE LOCATED CEILING AREA BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2023-447553<[01] REPLACED SUPPORT ANGLE LOCATED CEILING AREA BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM-51-40-02 AND DWG-146A7901 REV: -;[02] REPLACED SUPPORT ANGLE LOCATED CEILING AREA BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM-51-40-02 AND DWG-146A7901 REV: -
CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA 2023-447483<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[03] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA I.A.W SRM B737-700 51-40-02 AND DRAWING 141A5400 REV:-;SEE INDIVIDUAL STEP SIGN OFFS BELOW;[04] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA I.A.W SRM B737-700 51-40-02 AND DRAWING 141A5400 REV:-;SEE INDIVIDUAL STEP SIGN OFFS BELOW<BR>RII CERTIFIED
CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA 2023-447482<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA IAW B 737-700 51-40-02 AND DWG 141A5400 SHEET 44 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2.<BR>REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA IAW B 737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA IAW B 737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV - SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED
CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 LBL 27 AT FWD GALLEY AREA 2023-447485<[01] REPLACED WEB-INTERCOSTAL LOCATED FLOOR STRUCTURE BETWEEN BS294.5 TO BS312 AND LBL27 FWD GALLEY AREA IAW B737-700 SRM:51-40-02 AND DWG: 141A5400 REV.A. SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] CORRECTED STEP 1: REPLACED WEB-INTERCOSTAL LOCATED ON FLOOR STRUCTURE BETWEEN BS294.5 TO BS312 AND LBL27 FWD GALLEY AREA IAW B737-700 SRM:51-40-02 AND DWG: 141A5400 SHEET: 22; REV: A. SEE INDIVIDUAL SIGN-OFF BELOW.;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN-OFF BELOW
CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 RBL 15 AT FWD GALLEY AREA 2023-447486<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022237; DUE DATE: 26-JAN-24.;[02] PERFORMED PERMANENT REPAIR ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 RBL 15 AT FWD I.A.W B737-700 SRM 53-10-51-2R-6 REPAIR 6; FIGURE 203; SHEET 5; AND SRM 51-40-02-0G-0. SEE INDIVIDUAL SIGN OFF BELOW.;[03] PERFORMED PERMANENT REPAIR ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 RBL 15 AT FWD I.A.W B737-700 SRM 53-10-51-2R-6 REPAIR 6; FIGURE 203; SHEET 5; AND SRM 51-40-02-0G-0. SEE INDIVIDUAL SIGN OFF BELOW.<BR>TASK COMPLETED RII
CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 RBL 32 AT FWD GALLEY AREA 2023-447487<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 RBL 32 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -;[03] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 RBL 32 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -<BR>RII CERTIFIED
CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA 2023-447488<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED WEB AND FASTENER LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA I.A.W SRM B737-700 51-40-02 AND DRAWING 141A5400 REV:-;SEE INDIVIDUAL SIGN OFFS BELOW;[03] REPLACED WEB AND FASTENER LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA I.A.W SRM B737-700 51-40-02 AND DRAWING 141A5400 REV:-;SEE INDIVIDUAL SIGN OFFS BELOW<BR>RII CERTIFIED
CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 LBL 32 AT FWD GALLEY AREA 2023-447491<[01] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 LBL 32 AT FWD GALLEY AREA. IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET: 24 REV: A. SEE INDIVIDUAL SIGNOFF BELOW.;[02] TASK CARD COMPLETED <BR>REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 LBL 32 AT FWD GALLEY AREA. IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET: 24 REV: A. SEE INDIVIDUAL SIGNOFF BELOW.<BR>RII
CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 LBL 12 AT FWD GALLEY AREA 2023-447497<[01] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23;[02] PERFORMED PERMANENT REPAIR ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 LBL 12 AT FWD GALLEY AREA I.A.W B737-700 SRM 53-10-51-2R-20 REPAIR 20; FIGURE 206; ALTERNATIVE 2; SHEET 1; AND INSTALLED WEB INTERCOSTAL I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG#141A5400; SHEET 94; REV.-. SEE INDIVIDUAL SIGN OFF BELOW.;[03] RII JOB COMPLETED
CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA 2023-447498<[01] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23;[02] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23;[03] REPAIRED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW SRM B737-700 53-10-51-2R-19 REPAIR 19 SEE INDIVIDUAL SIGNOFF BELOW.;[04] REPAIRED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-19 REPAIR 19 SEE INDIVIDUAL SIGN OFF BELOW.;[05] TASK CARD COMPLETED <BR>REPAIRED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-19 REPAIR 19 SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII
CRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2023-447516<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 25 REV : SEE INDIVIDUAL SIGNOFF BELOW;[02] CORRECTIVE ACTION CERTIFIED RII
CRACK ANGLE - SUPPORT LOCATED BS727A TO BS727E AT LBL51 AFT CARGO COMPARTMENT 2023-447481<[01] REMOVED FASTENER COMMON TO ANGLE - SUPPORT LOCATED BS727A TO BS727E AT LBL51 AFT CARGO COMPARTMENT IAW B737-700 51-40-02 AND PERFORMED VISUAL INSPECCIÿ½N IAW B737-700 51-10-02 AND DAMAGE IS ONLY ON FASTENER; REPLACED FASTENERS IAW B737-700 51-40-02;[02] CORRECTED STEP 1.<BR>REMOVED FASTENER COMMON TO ANGLE - SUPPORT LOCATED BS727A TO BS727E AT LBL51 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECCIÿ½N IAW B737-700 SRM 51-10-02 AND DAMAGE IS ONLY ON FASTENER; FASTENER WAS REPLACED IAW B737-700 SRM 51-40-02;[03] CORRECTED STEP 1. <BR>REMOVED FASTENER COMMON TO ANGLE - SUPPORT LOCATED BS727A TO BS727E AT LBL51 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECCIÿ½N IAW B737-700 SRM 51-10-02 AND DAMAGE IS ONLY ON FASTENER AND WAS REPLACED IAW B737-700 SRM 51-40-02
CORROSION ON SUPPORT BRACKET LOCATED BS 312 RBL 54 AT LEVEL STR 17L AT FWD GALLEY AREA 2023-447504<[01] REPLACED SUPPORT BRACKET LOCATED BS 312 RBL 54 AT LEVEL STR 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM B737-700 SRM 51-10-02. TOOK MEASURE OF CORROSION ARE: L= 0.625?; W= 0.550?; D= 0.035?. TOOL USED CALIPER P/N: 500-752-20; S/N:B21038258; DUE DATE: 20-SEP-23. EVALUATED CORROSION AND NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 53-10-15-1A-1. ALLOWABLE DAMAGE 1.;[02] CORRECTED STEP 1. REPLACED SUPPORT BRACKET LOCATED BS 312 LBL 54 AT LEVEL STR 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM B737-700 SRM 51-10-02. TOOK MEASURE OF CORROSION ARE: L= 0.625?; W= 0.550?; D= 0.035?. TOOL USED CALIPER P/N: 500-752-20; S/N:B21038258; DUE DATE: 20-SEP-23. EVALUATED CORROSION AND NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 53-10-15-1A-1. ALLOWABLE DAMAGE 1.;[03] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW
CORROSION ON SUPPORT ANGLE LOCATED BTW BS 312 TO BS 344 AT LEVEL STR 17R RBL57 WL 208.1 AT FWD GALLEY AREA 2023-447502<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N:221861811 AND DUE DATE: 08-NOV-23.;[02] REPLACED NEW SUPPORT ANGLE LOCATED BTW BS 312 TO BS 344 AT LEVEL STR 17R RBL57 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET:23 SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED NEW SUPPORT ANGLE LOCATED BTW BS 312 TO BS 344 AT LEVEL STR 17R RBL57 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET:23 SEE INDIVIDUAL SIGN OFF BELOW
CRACK ACCESS PANEL 561AB TRAILING EDGE AT LT WING 2023-447443<[01] TOOL USED: CALIPER P/N: 500-193-30 S/N: 0000288 DUE DATE: 27/DEC/23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N:18185733 DUE DATE:23-JAN-24.;[03] TOOL USED: SCALE P/N: CR5200; S/N: 8343110809; DUE DATE:21-FEB-24.;[04] TOOL USED ULTRASONIC EQUIPMENT P/N: EPOCH 650; S/N: 201036102; CAL DUE DATE: 16/SEP/23;[05] TOOL USED: MULTIMETER P/N: FLUKE 179 S/N: 97220166 DUE DATE: 24-FEB-24.;[06] REPAIRED ACCESS PANEL 561AB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] STEP 6 VERIFIED AND CORRECTIVE ACTION COMPLETED : REPAIRED ACCESS PANEL 561AB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS273 AT LT WING 2023-447423<[01] REPLACED SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS273 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2930; REV: ?.;[02] REPLACED SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS273 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2930; REV
CORROSION ON EXISTING REPAIR LOCATED BS 986.5 BTW RBL 35 TO RBL 44 WL 208.1 AT AFT GALLEY AREA 2023-447444<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 130060401 AND DUE DATE: 20-MAR-24.;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[03] PERFORMED REPAIR ON FLOOR BEAM LOCATED BS 986.5 BTW RBL 35 TO RBL 44 WL 208.1 AT AFT GALLEY AREA I.A.W EA 23-153-02337-WIP1 AND EA 23-153-02337 SUMMARY. SEE INDIVIDUAL STEP SIGN OFFS BELOW;[04] PERFORMED REPAIR ON FLOOR BEAM LOCATED BS 986.5 BTW RBL 35 TO RBL 44 WL 208.1 AT AFT GALLEY AREA I.A.W EA 23-153-02337-WIP1 AND EA 23-153-02337 SUMMARY. SEE INDIVIDUAL STEP SIGN OFFS BELOW
CRACK ON FRAME LOCATED BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA 2023-447419<[01] MEASURE OF CRACK IS L:0.125 INCHES TOOL USED CALIPER P/N: 500-752-20 S/N:B21014945 DUE DATE: 08-NOV-23 AND EVALUATE CRACK IS NOT PERMITTED I.A.W SRM B737-700 53-00-07-1A-1 STEP 4.A(1); FRAME MUST BE REPAIRED.<BR>REPAIRED FRAME ON BS 312 AND BETWEEN STR5L TO STR6L FWD GALLEY AND LAV IAW EA M-22-153-01244 SEE SUB TASK BAR CODE TTG8Q00M70VK;[02] STEP 1 CORRECTED.<BR>REPAIRED FRAME ON BS 312 AND BETWEEN STR5L TO STR6L FWD GALLEY AREA IAW EA M-22-153-01244 SEE SUB TASK BAR CODE TTG8Q00M70VK SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPAIRED FRAME ON BS 312 AND BETWEEN STR5L TO STR6L FWD GALLEY AREA IAW EA M-22-153-01244 SEE SUB TASK BAR CODE TTG8Q00M70VK; SEE INDIVIDUAL SIGNOFFS BELOW. RII.
CORROSION ON FLOOR BEAM BS 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2023-447441<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 130060401 AND DUE DATE: 20-MAR-24.;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101U102020 DUE DATE: 30 AUG 23.;[03] PERFORMED PERMANENT REPAIR LOCATED FLOOR BEAM BS 986.5 AT LBL 43 AND WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 4 AND FIGURE 205. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[04] PERFORMED PERMANENT REPAIR LOCATED FLOOR BEAM BS 986.5 AT LBL 43 AND WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 4 AND FIGURE 205. RII SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2023-447425<[01] REPLACED NEW INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-40-02 AND DWG # 141A8180 REV ?C? SEE INDIVIDUAL SING OFF BELLOW;[02] RII ITEM <BR>REPLACED NEW INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-40-02 AND DWG # 141A8180 REV ?C? SEE INDIVIDUAL SING OFF BELLOW
CRACK ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2023-447440<[01] TOOL USED: CALIPER P/N: 500-193-30 S/N: 0000288 DUE DATE: 27/DEC/23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N:18196021 DUE DATE:24-JAN-24.;[03] TOOL USED: SCALE P/N: CR5200; S/N: 8343110809; DUE DATE:21-FEB-24.;[04] TOOL USED SCALE P/N:CR5200 S/N:8343110809 DUE DATE: 21-FEB-24.;[05] TOOL USED ULTRASONIC EQUIPMENT P/N: EPOCH 650; S/N: 201036102; CAL DUE DATE: 16/SEP/23;[06] REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2023-447442<[01] TOOL USED: CALIPER P/N: 500-193-30 S/N: 0000288 DUE DATE: 27/DEC/23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N:18185733 DUE DATE:23-JAN-24.;[03] TOOL USED SCALE P/N:CR5200 S/N:8343110809 DUE DATE: 21-FEB-24.;[04] TOOL USED ULTRASONIC EQUIPMENT P/N: EPOCH 650; S/N: 201036102; CAL DUE DATE: 16/SEP/23;[05] TOOL USED: MULTIMETER P/N: FLUKE 179 S/N: 97220166 DUE DATE: 24-FEB-24.;[06] REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196127 DUE DATE: 22-JAN-24. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.
CRACK INSPAR RIB LOCATED STAB STA111.10 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL STAB 2023-447369<[01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138203; CAL DUE DATE: 09-JUN-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN -24.;[03] REPAIRED INSPAR RIB LOCATED STAB STA111.10 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4;[04] CORRECTED STEP 3.<BR>REPAIRED INSPAR RIB LOCATED STAB STA111.10 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN OFF BELOW;[05] CORRECTED STEP 3. <BR>REPAIRED INSPAR RIB LOCATED STAB STA111.10 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. RII; SEE INDIVIDUAL SIGN OFF BELOW.
CRACK SUPPORT ANGLE ON FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN 2023-447360<[01] REPLACED ANGLE - SUPPORT ANGLE ON FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN IAW B737 700 SRM 51-40-02 ; SRM 51-10-02 AND DWG 273A9110-6 REV:A AND MEASURES OF CRACK IS L: 1.593 INCH TOOK MECHANICALLY TOOL USED CALIPER P/N: 500-196-30 S/N:A20231707 DUE DATE: 06-SEP-23.SEE INDIVIDUAL SIGN OFF STEP BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED ANGLE - SUPPORT ANGLE ON FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN IAW B737 700 SRM 51-40-02 ; SRM 51-10-02 AND DWG 273A9110 REV:A AND MEASURES OF CRACK IS L: 1.593 INCH TOOK MECHANICALLY TOOL USED CALIPER P/N: 500-196-30 S/N:A20231707 DUE DATE: 06-SEP-23.SEE INDIVIDUAL SIGN OFF STEP BELOW.;[03] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK SUPPORT BRACKET BS 540 AND LBL 6 AT AIR CONDITIONING BAY 2023-447326<[01] REPLACED SUPPORT BRACKET LOCATED BS 540 AND LBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] COMPLETED
CORROSION COVER PLATE LOCATED BS400 TO BS420 AND BETWEEN STR27L TO STR28L AND WL149.5 LOWER FUSELAGE 2023-447319<[01] REPLACED COVER PLATE LOCATED BS400 TO BS420 AND BETWEEN STR27L TO STR28L AND WL149.5 LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SING-OFF BELOW;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CORROSION COVER PLATE LOCATED BS440 TO BS460 AND BETWEEN STR27L TO STR28L AND WL149.5 LOWER FUSELAGE 2023-447320<[01] REPLACED COVER PLATE LOCATED BS440 TO BS460 AND BETWEEN STR27L TO STR28L AND WL149.5 LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SING-OFFS BELOW;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.
RT WING I/B MAIN FLAP DELAMINATED APPROX 11 FOR O/B EDGE. DAMAGE IS APPROX 11.5X5.7. PERFORMED TEMPORARY REPAIR OF RT WING INBD MAIN FLAP PER SRM 57-53-01-1A-1. PERFORMED INTERIM REPAIR OF RH WING INBD MAIN FLAP PER SRM 57-53-01-1A-1.
INSIDE L1 DOOR ASSIST CLOSE HANDLE UPPER ATTACHMENT LOOSE. / [01] TIGHTENED INSIDE L1 DOOR ASSIST CLOSE HANDLE UPPER ATTACHMENT PER AMM-52-11-00;[02] INSPECTED
20 ABC EMER LIGHT INOP / [01] RELAMPED 20ABC EMERGENCY LIGHT PER AMM 33-51-03. OPS CHECK NORMAL.
POSITIONED FLAP HANDLE TO 5; FLAPS FAILED TO EXTEND BEYOND 1; SPLIT NEEDLE INDICATION INDICATED. TRAILING EDGE FLAP LOCKOUT / [01] PERFORMED FSEU BITE FOUND MAINT MSG 27-52260; PER FIM 27-51 TASK 820; R&R?D R/H FLAP POSITION TRANSMITTER PER AMM 27-58-01; AND FLAP POSITION INDICATOR PER AMM 27-58-02; ALL OPS CHECKS NORMAL.
FLAP ASSEMETRY; RIGHT SIDE LOCKED OUT. F185 ATL-LGA DIVERTED INTO EWR._PERFORMED FSEU BITE FOUND MAINT MSG 27-52260; PER FIM 27-51 TASK 820; / R&RD R/H FLAP POSITION TRANSMITTER PER AMM 27-58-01; AND FLAP POSITION INDICATOR PER AMM 27-58-02; ALL OPS CHECKS NORMAL._BWI MX DROVE;
DURING TAXI OUT ATC AND FLIGHT ATTENDANTS REPORTED FLAMES OUT OF THE BACK OF THE #1 ENGINE / [01] PERFORMED GVI OF #1 ENGINE INLET AND EXHAUST AREA; NO DEFECTS NOTED. PERFORMED #1 ENGINE START PROCEDURE; NO DEFECTS NOTED IAW AMM 71-00-00. A/C OK FOR SERVICE.
LEFT NR 3 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS. OPS CHECK GOOD.
SUPPLEMENTAL INFORMATION: R1 DOOR SLIDE NEEDS REPACK / [01] REPACKED R1 DOOR SLIDE PER AMM 25-66-01 MT 725-61-06
SUPPLEMENTAL INFORMATION: R2 DOOR SLIDE NEEDS REPACK / [01] REPACKED R2 DOOR SLIDE PER AMM 25-66-01 AND MT 725-61-06
LEFT HAND LOWER EMERGENCY SLIDE LIGHT IS INOP. / [01] RE-LAMPED AND PERFORMED GOOD OPS TEST OF LEFT HAND LOWER EMERGENCY SLIDE LIGHT PER AMM 33-51-04-960-801.; [02] VERIFIED CORRECTIVE ACTIONS STEP 1.
AFT CARGO BAY FLOOR PNL 140CF CRACKED. CRACK FOUND L=1' X W=1 X D=.080'; NO CRACKS ALLOWED IAW SRM REPAIR BY REPLACEMENT. FABRICATED NEW ACB FLOOR PANEL 140CF IAW DWG 435A2610 AND SRM 51-40-05.
AFT CARGO BAY R/H SIDEWALL CAP STRIP CRACKED BS 790 STR 18 - STR 25 ; / [01] REPLACED CRACKED AFT CARGO BAY R/H SIDEWALL CAP STRIP AT BS 790; STR 18R - 25R WITH NEW PART S/N / LOT# 1421820-3 IAW AMM 25-52-06-400-801 PAR. 3.D. (9)<BR><BR>ATS SCREW GUN ATS2246 S/N 1703310 07/2022; [02] VERIFIED AFT CARGO BAY CAP STRIP AT BS 790 STR 18R - 25R INSTALLED PER AMM 25-52-06-400-801 PARA. 3.D.(9).
FWD CARGO BAY AFT BULHEAD GUSSET CRACKED AT BS 500D STR 21L REMOVED FCB AFT BULKHEAD GUSSED IAW SRM 51-40-02. LOCATED AND DRILLED NEW GUSSET IAW SRM 51-40-02 AND DWG 143A481 ID:0003 REV -. INSTALLED FCB AFT BULKHEAD GUSSET IAW SRM 51-40-02 AND DWG 143A7902.
FWD CARGO BAY AFT BULKHEAD GUSSET CRACKED AT BS 500D, S19R. REMOVED FWD CARGO BAY AFT BULKHEAD GUSSET IAW SRM 51-40-02-0G-0. REMOVED FWD CARGO BAY AFT BULKHEAD GUSSET IAW SRM 51-40-02-0G-0. LOCATED & DRILLED NEW PART IAW SRM 51-40-05-0G-0 & DWG 143A7902. INSTALLED FWD CARGO BAY AFT BULKHEAD GUSSET IAW 737 SRM51-40-02-0G-0 AND DWG 143A7902.
FWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED, WELDED CRACKS ON FCB; FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1 PARA. 4.B. (2) & (4). FLUORESCENT DYE PENETRANT INSPECTED REPAIR AREA IAW SOPM 20-20-02 METHOD C. NO CRACKS FOUND. SANDED WELD REPAIR AREA PER SRM 53-30-15-2R-1 PARA. 4.B. (5). APPLIED CHEMICAL CONVERSION COATING AND BMS-10 PRIMER TO BARE METAL IAW SRM 53-30-15-2R-1, SOPM 20-43-03, SPOM 20-41-02. INSTALLED FWD BAY FWD CORNER SUFF PLATE IAW SRM 53-30-15-2R-1.
FWD CARGO BAY AFT CORNER SCUFF PLATE CRACKED. WELDED CRACKS ON FCB; AFT CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1 PARA. 4.B. (2) & (4). FLUORESCENT DYE PENETRANT INSPECTED REPAIRED AREA IAW SOPM 20-20-02 METHOD C. NO CRACKS FOUND. SANDED WELD REPAIR AREA PER SRM 53-30-15-2R-1 PARA. 4.B. (5). APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO BARE METAL IAW SRM 53-30-15-2R-1, SOPM 20-43-03, & SPOM 20-41-02. INSTALLED FWD BAY AFT CORNER SUFF PLATE IAW SRM 53-30-15-2R-1.
AFT CARGO RH FLOOR INTERCOSTAL HAS AN ELONGATED HOLE; BS 727A + 5; RBL 21; WL 156. REMOVED INTERCOSTAL IAW SRM 51-40-02. DID NOT FIND ALLOWABLE DAMAGE IN SRM. REPLACED PART FOR REPAIR IAW SRM 51-10-02. LOCATED AND DRILLED NEW PART IAW SRM 51-40-05-0G-0 AND DWG 146A7502. INSTALLED AFT CARGO R/H FLOOR INTERCOSTAL AT BS 727A TO BS 727B; RBL 21; WL 156 IAW SRM 51-40-02-0G-0 AND DWG 146A7500 ; ID 88; [07] VERIFIED AFT CARGO BAY R/H FLOOR INTERCOSTAL AT BS 727A TO BS 727B; RBL 21; WL 156 INSTALLED PER SRM 51-40-02-0G-0 AND DWG 146A7500 .
UPON ACCOMPLISHING HFEC INSPECTION; FOUND 1 (EA) CRACK IN SEAT TRACK FASTENER HOLE AT BS 727B RBL 24.75 COMMON TO THE LWR STRAP. ; / [01] REMOVED AND REPLACED LWR SPLICE STRAP AT BS727B RBL 24.75 IAW SB 737-53-1296 FIG.7 & FIG11.; [02] REJECTION: INCORRECT ORIENTATION ON RADIUS FILLER; RAISED FAULT TTG8Q006UCGQ.; [03] UPDATED MEASUREMENT CHART.; [04] UPDATED PARTS.; [05] VERIFIED SPLICE STRAP REPLACED AT BS 727 RBL 24.75 PER 51-40-02 AND SB 737-53-1296.
SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S..727E+10; 727E+14; 727E+15; 727E+18; 727E+19; 747; 747+2; 747+5; 747+6 AND 747+10; R.B.L. 22; W.L. 154. ; / [01] REMOVED AND EVALUATED MULTIPLE AREAS OF CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT R/H FROM BS 727E+10 TO BS 747+10 RBL 22 WL 154. LARGEST AREA OF MATERIAL REMOVED MEASURES 2.4' L; 0.98' W; 0.18' D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMAINDER OF WORK TO BE ACCOMPLISHED ON TASK TTG8Q006S5CK.; [02] VERIFIED CORRECTIVE ACTION STEP 1; [03] REMOVED AND EVALUATED MULTIPLE AREAS OF CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT R/H FROM BS 727E+10 TO BS 747+10 RBL 22 WL 154. LARGEST AREA OF MATERIAL REMOVED MEASURES 2.4' L; 0.98' W; 0.18' D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMAINDER OF WORK TO BE ACCOMPLISHED ON TASK TTG8Q006S5CK; [04] VERIFIED ACTION 3
CORROSION ON AFT CARGO BAY DOOR THRESHOLD SUBWEB AT B.S..794+3; R.B.L. 22; W.L. 154. ; / [01] REMOVED ACB DOOR THRESHOLD SUBWED AT B.S. 807-847 RBL 22 WL 154 IAW 51-40-02; [02] REMOVED ACB DOOR THRESHOLD SUBWED AT B.S. 807-847 RBL 22 WL 154 IAW 51-40-02; [03] REMOVED CORROSION FROM ACB DOOR THRESHOLD WEB AT BS 794+3 RBL 22 MEASURED 3'L X 2'W AND 0.020' DEEP ORIGINAL THICKNESS OF 0.045' FOUND OUT OF LIMITS PER SRM 53-60-15-1A-1; [04] REMOVED CORROSION FROM ACB DOOR THRESHOLD WEB AT BS 794+3 RBL 22 MEASURED 3'L X 2'W AND 0.020' DEEP ORIGINAL THICKNESS OF 0.045' FOUND OUT OF LIMITS PER SRM 53-60-15-1A-1; [05] VERIFIED DAMAGE OUT OF LIMITS PER SRM 53-60-15-1A-1; [06] UPDATED MEASUREMENTS; [07] LOCATED AND DRILLED NEW ACB SUBTHRESHOLD WEB PER SRM 51-40-05; SRM 51-40-08; DWG# 146A8123.; [08] VERIFIED CORRECTIVE ACTION 7.; [09] REQUEST OK TO INSTALL.; [10] CERTIFIED ACTION 9; [11] OK TO INSTALL GIVEN.; [12] APPLIED SEALANT AT 06:27 UTC 13OCT21 AND INSTALLED ALL TEMP AND PERMANENT FASTENERS IAW SRM 51-31-00-390-801 ; SRM 51-40-02; DWG 146A8340 ID 28 REV-; [13] VERIFIED CORRECTIVE ACTION ENTRY 12.; [14] INSTALLED REMAINING PERMANENT FASTENERS IN ACB CARGO BAY DOOR THRESHOLD SUBWED AT BS 794+3 RBL 22 WL 154 IAW SRM 51-40-02 0G-0 AND DWG 146A8340 REV:-; [15] RII INSPECTED ACTION 14; [16] INSPECTION COMPLETE
SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S..727B+14; 727C+5; 727C+10; 727D+3; 727D+7; 727D+10; 727D+14; 727D+19; 727E+2 AND 727E+6; R.B.L. 22; W.L. 154. ; / [18] INSTALLED FLOOR TO SIDEWALL SUPPORT AT ACB B.S 727 TO B.S 767; R.B.L. 22 W.L. 154 PER SRM 51-40-02-0G-0 AND DWG 146A7500; 146A7502; AND 146A0061; [19] VERIFIED CORRECTIVE ACTION ENTRY 17.; [20] VERIFIED CARD COMPLETE
SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 767+3; 767+7; 767+10; 767+14; 787+6 AND 787+10; L.B.L. 22; W.L. 154. ; / [01] REMOVED AND EVALUATED MULTIPLE AREAS OF CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT L/H FROM BS 767+3 TO BS 787+10. LARGEST AREA OF MATERIAL REMOVED MEASURED 1.32' L; 1.15' W; 0.004' D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMAINDER OF WORK TO BE ACCOMPLISHED ON TASK TTG8Q006S5AU.; [02] VERIFIED CORRECTIVE ACTION STEP 1; [03] REMOVED AND EVALUATED MULTIPLE AREAS OF CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT L/H FROM BS 767+3 TO BS 787+10. LARGEST AREA OF MATERIAL REMOVED MEASURED 1.32' L; 1.15' W; 0.004' D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMAINDER OF WORK TO BE ACCOMPLISHED ON TASK TTG8Q006S5AU; [04] VERIFIED CORRECTIVE ACTION 3.; [05] VERIFIED FLOOR TO SIDEWALL SUPPORT WILL BE REPLACED ON TASK TTG8Q006S5AU
SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S..727A+10; 727B+5; 727B+8; 727C+14; 727D+2; 727D+4; 727D+5; 727D+7; 727D+10 AND 727D+15; L.B.L. 22; W.L. 154. ; / [23] INSTALLED NEW FLOOR TO SIDEWALL SUPPORT LOCATED BTW B/S 727 TO B/S 847 LBL 22 WL 154 IAW SRM 51-40-02 AND DWG 146A7502 REV:-. AND 146A7500 REV:A; [24] VERIFIED CORRECTIVE ACTION ENTRY 23.; [25] VERIFIED CARD COMPLETE
SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY SHIELD AT B.S. 767+3; 767+7; 767+11; 767+12; 767+15; 767+16 AND 767+19; R.B.L. 22; W.L. 154. ; / [01] CORROSION ON SHIELD ACB IT'S OUT OF LIMITS DUE TO NO ARE LIMITS GIVEN IN SRM. REPLACEMENT PAR PER SRM 51-10-02-0G-0 STEP 9.C. REMOVED ACB SHIELD AT BS794-787 RBL22. WL154 IAW SRM 51-40-02; [02] UPDATED MEASUREMENTS; [03] VERIFIED CORRECTIVE ACTION 1.; [04] LOCATED AND DRILLED NEW SHIELD SUPPORT AT BS 767+3;RBL 22; WL 154 IAW SRM 51-40-05-0G-0 AND DWG 146A0081; ID 31; [05] VERIFIED CORRECTIVE ACTION 4.; [06] REQUEST OK TO INSTALL.; [07] OKAY TO INSTALL NEW SHIELD SUPPORT IN THE AFT CARGO BAY AT BS 767-787 RBL 22 WL 154.; [08] INSTALLED NEW ACB SHIELD AT BS 767-787 RBL 22 WL 154 IAW DWG 146A0081 SHEET 34 AND SRM 51-40-02-0G; [09] VERIFIED INSTALLED NEW ACB SHIELD AT BS 767-787 RBL 22 WL 154 IAW DWG 146A0081 SHEET 34 AND SRM 51-40-02-0G.; [10] VERIFIED ALL STEPS COMPLETE.
SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY INTERCOSTAL AT B.S..767+5; R.B.L. 20; W.L. 154. ; / [01] REMOVED DAMAGE FROM ACB INTERCOSTAL BS 767+5 RBL 20; MATERIAL LOSS MORE THAN 20% FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1.; [02] REMOVED INTERCOSTAL AT RBL 20 WL 154 BS 767 TO BS 787 IAW ARM 51-40-02-0G-0; LOCATED AND DRILLED NEW INTERCOSTAL P/N 146A8123U19 PO# 1466078 IAW SRM 51-40-05-0G-0; [03] VERIFIED CORRECTIVE ACTION 2.; [04] REQ. OK TO INSTALL INTERCOSTAL AT AFT CARGO BAY INTERCOSTAL AT B.S..767-787 R.B.L. 20; W.L. 154; [05] VERIFIED CORRECTIVE ACTION 4.; [06] INSTALLED INTERCOSTAL AT AFT CARGO BAY AT B.S..767-787 R.B.L. 20; W.L. 154 IAW SRM 51-40-020G-0 AND DWG 164A0081 REV.-; [07] VERIFIED CORRECTIVE ACTION ITEM 6.; [08] APPLIED CORROSION INHIBITING COMPOUND AT AFT CARGO BAY INTERCOSTAL AT B.S..767-787 R.B.L. 20; AND REWORK AREA IAW SOPM 20-41-05; [09] VERIFIED CORRECTIVE ACTION 8.
SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY TENSION STRAP AT B.S..794 - 807+14; 827+7 AND 827+14; R.B.L. 20; W.L. 154. ; / [01] REMOVED CORROSION FROM ACB TENSION STRAP BS 827+14; RBL 20 IN AN AREA OF L=2.5 X W=2 X DEPTH= 0.025 FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 4(G).3 FIG103 DETAIL G.; [02] USED TOOL DEPTH GAUGE ID# ATS400 DUE 08/2022.; [03] PROCURED ; LOCATED AND DRILLED NEW TENSION STRAP ; BTW B/S 767+10' TO B/S 847+14' RBL 20 WL 154 LOT#1468918 IAW SRM 51-40-05 AND DWG 146A8120 REV:-. AND 146A 8130 REV:B AND OK TO INSTALL; [04] VERIFIED CORRECTIVE ACTION 1 AND 3.; [05] REMOVED TENSION STRAP ; BTW B/S 767+10' TO B/S 847+14' IAW SRM 51-40-02; [06] INSTALLED NEW TENSION STRAP BS 767+10' TO BS 847+14' RBL 20 WL 154 IAW DWG: 146A8120 ID:0034 REV:- ; DWG:146A0081 ID:0031 REV:- AND SRM 51-40-02; [07] INSTALLED NEW TENSION STRAP BS 767+10' TO BS 847+14' RBL 20 WL 154 IAW DWG: 146A8120 ID:0034 REV:- ; DWG:146A0081 ID:0031 REV:- AND SRM 51-40-02; [08] RII VERIFIED NEW STRAP INSTALLED IAW DWG: 146A8120 ID:0034 REV:- ; DWG:146A0081 ID:0031 REV:- AND SRM 51-40-02.; [09] VERIFIED ALL STEPS COMPLETE; JOB COMPLETE.
SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY SHIELD SUPPORT AT B.S. 847+1 AND 847+2; R.B.L. 22; W.L. 154. ; / [01] REMOVED AFT CARGO BAY AFT SHIELD IAW SRM 51-40-02-0G-0; [02] THERE ARE NO SRM ALLOWABLE DAMAGE FOR AFT CARGO BAY SHIELD. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9.C; [03] VERIFIED CORRECTIVE ACTION 1 AND 2.; [04] LOCATED AND DRILLED NEW SHIELD SUPPORT AT BS 847+1;RBL 22; WL 154 IAW SRM 51-40-05-0G-0 AND DWG 146A0081; ID 31; [05] VERIFIED CORRECTIVE ACTION 4.; [06] REQUESTING OK TO INSTALL NEW SHIELD SUPPORT AT BS 847-BS 867;RBL 22; WL 154; [07] OKAY TO INSTALL SHIELD SUPPORT AT BS 847 - BS 867 AND RBL 22; WL 154.; [08] INSTALLED SHIELD SUPPORT AT BS 847 - BS 867 AND RBL 22; WL 154. IAW SRM 51-40-02 AND DWG 146A0081 REV:-; [09] VERIFIED CORRECTIVE ACTION ENTRY 8.; [10] VERIFIED CARD COMPLETE.
SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 747+16 AND 747+19; R.B.L. 22; W.L. 154. ; / [01] REMOVED AND EVALUATED MULTIPLE AREAS OF CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT R/H FROM BS 747+16 TO BS 747+19. LARGEST AREA OF MATERIAL REMOVED MEASURED 1.84' L; 1.25' W; 0.005' D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMAINDER OF WORK TO BE ACCOMPLISHED ON TASK TTG8Q006S5CK.; [02] VERIFIED CORRECTIVE ACTION STEP 1; [03] REMOVED AND EVALUATED MULTIPLE AREAS OF CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT R/H FROM BS 747+16 TO BS 747+19. LARGEST AREA OF MATERIAL REMOVED MEASURED 1.84' L; 1.25' W; 0.005' D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMAINDER OF WORK TO BE ACCOMPLISHED ON TASK TTG8Q006S5CK; [04] VERIFIED ACTION 3
SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT B.S. 947; R.B.L. 23; W.L. 157. ; / [01] REMOVED CORRODED AFT CARGO BAY BULKHEAD CENTER PANEL LOWER SUPPORT AT BS 947.5 RBL 23 WL157. NO LIMITS FOUND IN SRM; REPAIR BY REPLACEMENT. IAW SRM 51-10-02-0G-0 PARAGRAPH 9 STEP C; SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW BRACKET ASSY SUPPORT PO#812692 IAW SRM 51-40-05-0G-0; DWG 149A8118 REV B <BR><BR>OK TO INSTALL; [03] OKAY TO INSTALL AFT CARGO BAY AFT BULKHEAD LOWER SUPPORT BRACKET P/N 149A8118-27 AT BS947; RBL 23.; [04] INSTALLED AFT CARGO BAY SUPPORT BRACKET AT BS 947.5 RBL 23 WL157 IAW SRM 51-40-02-0G-0; DWG 149A8118 REV B; 149A8110 REV B; [05] VERIFIED AFT CARGO BAY SUPPORT BRACKET AT BS 947.5 RBL 23 WL 157 INSTALLED PER SRM 51-40-02-0G-0; DWG 149A8118 REV B AND 149A8110 REV B.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 887+9; 907+2; 907+6 AND 927+10; R.B.L. 22; W.L. 154. REMOVED ACB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02. REMOVED AND EVALUATED DAMAGE, LARGEST AREA OF REMOVED MATERIAL AT BS 947. DAMAGE MEASURES 1.33' L; 0.61' W; 0.006' D. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED ACB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02. DRILLED A NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05; 51-40-08 AND DWG 147A7501 REV A. APPLIED CHEMICAL CONVERSION COATING IAW SOPM 20-41-02. LOCATED AND DRILLED THE NEW FLOOR TO SIDEWALL SUPPORT1 IAW SRM 51-40-05; 51-40-08 AND DWG 147A7501 ID: 0006 REV:A.
AFT CARGO BAY FORWARD BULKHEAD PANEL SUPPORT ATTACH BRACKET IS CRACKED AT BS 727, RBL 3, WL 160. INSTALLED A NEW ATTACH BRACKET IAW SRM 51-40-02 AND DWG 144A2600.
CRACKED STRINGER AT AREA AFT OF FCB BS 540, S25R, WL 156. EVALUATED CRACK AND FOUND OUT OF LIMITS IAW SRM 53-00-03-1A-1 PARAGRAPH 4A(2)(A)1. REMOVED FASTENERS FROM STRINGER 25 RT IAW SRM 51 40-02. REMOVED DAMAGE BY TRIMMING IAW SRM 51-10-02. LOCATED AND DRILLED A NEW SECTION OF STRINGER IAW SRM 51-40-05 AND 53-00-03-2R-1. STRINGER 25R REPAIRED IAW EA 21-153-02986 REV A.
CRACKED STRINGER 26R, BS 540, WL 153. REMOVED FASTENERS FROM STRINGER IAW SRM 51-40-02-0G-0. EVALUATED CRACK AND FOUND OUT OF LIMITS IAW SRM 53-00-03-1A-1, PARA 4A(2)(A)1. FABRICATED, LOCATED & DRILLED A NEW STRINGER SECTION AND SPLICE IAW SRM 53-00-03-2R-1, FIG 205. APPLIED CHEMICAL CONVERSION COATING ON REPAIR PARTS IAW SRM 53-00-03-2R-1, PARA 4.I. APPLIED PRIMER ON REPAIR PARTS IAW SRM 53-00-03-2R-1. PERFORMED VISUAL INSPECTION, NO MORE DAMAGE FOUND IAW SRM 53-00-03-2R-1, REPAIR 1 STEP 4B(1). HFEC INSPECTED CUT EDGES IAW NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. INSTALLED THE NEW STRINGER SECTION AND SPLICE IAW SRM 53-00-03-2R-1, REPAIR 1, SOPM 20-50-19 AND DWG 143A3230 REV A.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A -BS500D RBL24 WL156. ; / [16] INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 500A-500D RBL 24 WL 156;IAW SRM 51-40-02 ;DWG 143A7500 REV:- AND DWG 143A7505 REV:D.; [17] VERIFIED INSTALLATION OF THE FLOOR TO SIDEWALL SUPPORT BS500500D RBL 24 WL156 PER SRM 51-40-02; DWG 143A7500 REV:- AND DWG 143A7505 REV:D.
CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS 454 - 476, RBL 28, WL 156. EVALUATED DAMAGE ON SUBTHRESHOLD WEB. ORIGINAL THICKNESS .045' DAMAGE REMOVED; .009' REMAINING THICKNESS .0036 L= 2' X W=1.2' DEPTH .009 DAMAGE EXCEED 10% OF ORIGINAL THICKNESS, FOUND TO BE OUT LIMITS IAW SRM 53-30-15-1A-1; 4.G.(12). REMOVED SUBTHRESHOLD WEB IAW SRM 51-40-02. LOCATED, DRILLED AND COUNTERSINK NEW SUBTHRESHOLD WEB IAW SRM 51-40-05-0G-0, SRM 51-40-08-0G-0 & DWG 143A8330. INSTALLED FCB SUBTHRESHOLD WEB IAW SRM 51-40-02-0G-0 PAR. 5 AND DWG 143A8330. INSTALLED FCB SUBTHRESHOLD WEB IAW SRM 51-40-02-0G-0 PAR. 5 & DWG 143A8330.
CORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL24 WL156. EVALUATED DAMAGE ON SHIELD AND NO FOUND ALLOWABLE DAMAGE LIMITS IN SRM 51-10-02-0G-0 PARA 9. REMOVED SHIELD IAW SRM 51-40-02. LOCATED & DRILLED IAW SRM 51-40-05-0G-0 & DWG 143A0080. INSTALLED FCB AFT SHIELD IAW SRM 51-40-02-0G-0 AND DWG 143A0080 REV -.
CORROSION ON FWD SHIELD AT FWD CARGO BAY BS420 - 440, RBL 23, WL 156. REMOVED SHIELD IAW SRM 51-40-02. LOCATED AND DRILLED THE SHIELD IAW SRM 51-40-05 AND DWG 143A0080. INSTALLED FWD SHIELD AT FCB BS.420 TO BS.440 RBL 23 WL 156 IAW SRM 51-40-02 AND BOEING DWG 143A0080- REV-.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500 -BS500B LBL24 WL156. ; / [24] INSTALLED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 396-500D LBL24 WL 156 IAW SRM 51-40-02 ;DWG 143A7500 REV:- AND DWG 143A7505 REV:D.; [25] VERIFIED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT INSTALLED AT BS 396-500D LBL 24 WL 156 PER SRM 51-40-02 ;DWG 143A7500 REV:- AND DWG 143A7505 REV:D.
FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED ; / [01] REMOVED FCB AFT BULKHEAD SUPPORT GUSSET AT BS500D S-19L WL 193 PER SRM 51-40-02; [02] REMOVED FCB AFT BULKHEAD SUPPORT GUSSET AT BS500D S-19L WL 193 PER SRM 51-40-02; [03] NO ALLOWABLE DAMAGE FOUND IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0; PARA 9; STEP C; [04] LOCATED AND DRILLED NEW GUSSET IAW SRM 51-40-05; DWG 143A7902 REV-. OKAY TO INSTALL; [05] VERIFIED NEW GUSSET DRILLED; OK TO INSTALL PER SRM 51-40-05 AND DWG 143A7902.; [06] INSTALLED GUSSET AT BS 500D S-19L WL 193 IAW DWG 143A7902 REV -; SRM 51-40-02-0G-0 PARAGRAPH 4.; [07] VERIFIED CORRECTIVE ACTION ITEM 6.; [08] VERIFIED TASK IS COMPLETE.
FWD CARGO INTERCOSTAL ATTACH ANGLE CRACKED BS 400 LBL 25 WL 155. REMOVED INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02 AND DWG 143A7505 REV.-B. LOCATED AND DRILLED NEW ATTACH ANGLE IAW SRM 51-40-02-0G0-0, AND DWG 143A7505 REV- B. INSTALLED FCB INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02 AND DWG 143A7505 ID:0002 REV B.
CORROSION ON PASSENGER CABIN SEAT TRACK BS494; BS500+6; BS500A+7; BS500A+16; BS500B+18; ; / [01] UPON FURTHER INVESTIGATION; FOUND CORROSION TO BE ON SEAT TRACK AT LBL 45.; [02] VERIFIED CORRECTIVE ACTION 1; [03] SEAT TRACK AT BS 480 - BS 520 LBL45 WL208 TO BE REPLACED ON CUSTOMER CARD#TTG8Q006RCWF; [04] VERIFIED CORRECTIVE ACTION 3.; [05] TO BE REPLACED ON CUSTOMER CARD#TTG8Q006RCWF COMPLETE
PANEL 191D HAS SEVERAL DELAMINATIONS TO OUTER SURFACE. IDENTIFIED PANEL IAW SRM 53-30-70-0I-1 FIG 2 TABLE 2 ITM 9. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-30-70-1A-1 PARA 4.A. DAMAGE IS TO BE REPAIRED IAW SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11 AS GIVEN IAW SRM 53-30-70-2R-1 PARA 4.B (2) TABLE 202. REMOVED DAMAGED SKIN AND PARTIAL DEPTH CORE IAW SRM 51-70-05-2R-2 PARA 4.A - 4.C. CLEANED; FABRICATED REPAIR PARTS, INSTALLED IAW SRM 51-70-05-2R-11 PAR 4B-E; SRM 51-70-05-2R-2 PAR 4F-G; AND SRM 51-70-14-2R-4 PAR 6D;H-I.
B.S. 663 LOWER COMPOSITE BULK HEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 42; W.L. 163. ; / [01] REMOVED EXISTING SPLICE AND DAMAGE ANGLE AT R/H VAPOR BARRIER BS 663 WL 163 BNETWEEN RBL 65 TO RBL 18 IAW SRM 51-10-02 0G-0; [02] REMOVED EXISTING REPAIR ANGLE AT R/H VAPOR BARRIER BS 663 WL163 RBL 18 TO RBL 6 IAW SRM 51-40-02-0G-0; [03] VERIFIED CORRECTIVE ACTION 1 AND 2.; [04] FORMED AND HEAT TREATED NEW ANGLE IAW 111A1322 REV:B ON CUSTOMER RO NO 840092-SWA JOB NUMBER 543500; [05] LOCATED AND DRILLED NEW ANGLE AT B/S 663 BTW RBL6 - RBL 65 WL 163 IAW SRM 51 40-05 AND DWG 111A1000 REV:AND DWG 111A1000 REV:-. FORMED AND HEAT TREATED NEW ANGLE IAW 111A1322 REV B.
CRACKED FLOOR SUPPORT AT BODY STATION 540+1; RBL 1; WL 208 ; / [01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 540+1 RBL 1 WL 208 IAW SRM 51-40-02 AND BOEING DWG 143A0060.; [02] MATCH DRILLED FLOOR BOARD HOLES IAW SRM 51-40-05.; [03] VERIFIED; [04] VERIFIED CORRECTIVE ACTION ENTRIES 1. AND 2.
CRACKED FLOOR SUPPORT AT BODY STATION 540+1; LBL 1; WL 208 ; / [01] REMOVED AND BEGAN INSTALLATION OF FLOOR SUPPORT AT BS 540+1 LBL1 WL208 IAW SRM 51-40-02 AND BOEING DWG 143A0060; [02] COMPLETED INSTALLATION OF FLOOR SUPPORT AT BS 540+1 LBL1 WL208 IAW SRM 51-40-02 AND BOEING DWG 143A0060<BR>MATCH DRILLED FLOOR BOARD HOLES IAW SRM 51-40-05; [03] VERIFIED; [04] VERIFIED CORRECTIVE ACTION ENTRIES 1. AND 2.
CRACKED FLOOR SUPPORT AT BODY STATION 540+1; RBL 25; WL 208 ; / [01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 540+1 RBL 25 WL 208 IAW SRM 51-40-02 AND BOEING DWG 143A0060 <BR>MATCH DRILLED FLOOR BOARD HOLES IAW SRM 51-40-05.; [02] VERIFIED; [03] VERIFIED CORRECTIVE ACTION ENTRY 1.
LEFT EMER EXIT SIGNS; LT OVERWING LIGHT AND ISLE LIGHT AT 6ABC DIDN'T PASS CAPACITY TEST. R & R BATTERY PACK AND POWER SUPPLY AT M1668 PER AMM 33-51-06.
LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED / R&R LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL PER MM 53-31-31
AFT ENTRY DOOR SLIDE GIRT NEEDS ADJUSTMENT. INSTALLED AFT ENTRY DOOR SLIDE GIRT PER AMM 25-66-01.
LEFT EMER EXIT SIGNS; LT OVERWING LIGHT AND ISLE LIGHT AT 6ABC DIDN'T PASS CAPACITY TEST. R & R BATTERY PACK AND POWER SUPPLY AT M1668 PER AMM 33-51-06.
EMERGENCY BATTERY PACK AFT LT AND MIDDLE RT INOPERATIVE. REMOVED A DREPLACED AFT LT AND MIDDLE RT EMERGENCY BATTERY PACKS IAW AMM 33-51-06. OPS CHECK GOOD.
SEVERAL LH AFT CABIN EMERGENCY LIGHT'S OUT AND L-2 EXTERNAL EMERGENCY LIGHT OUT. / REMOVED & INSTALLED SERVICEABLE PACK CHARGER ASSY M1673. OPS CK GOOD PER MT 33-51-06
R/H OVERWING EMERGENCY EXIT SIGN LIGHT COVER MISSING. / INSTALLED LENS PER AMM.
L/H FLOOR TRACK LIGHTING AT ROW 8 AREA PULLED UP FROM FLOOR. / SECURED PHOTO LUMINESCENT STRIP IAW AMM.
R/H WING TRAILING EDGE CAVITY INBD WIGGLE PLATE ABOVE SAIL TAIL HAS FASTENERS SHEARED AND PLATE IS CRACKED / REMOVED AND REPLACED RH WING TRAILING EDGE CAVITY I/B WIGGLE PLATE P/N 115A2781-14 (7570259) WN6612 IAW B 737-700 AIPC 57-50-00-30 & SRM 51-40-02-0G-0
R1 DOOR LOWER DOOR BEAM #4 CRACKED BY UPPER FASTNER IN FILLET AREA. R&R #4 BEAM IAW SRM AND DWG.
R1 DOOR UPPER DOOR BEAM #5 CRACKED IN UPPER FILLET AREA.BY FASTNER HOLE. R&R NR 5 BEAM IAW SRM AND DWG.
R/H WING TRAILING EDGE CAVITY INBD WIGGLE PLATE ABOVE SAIL TAIL HAS FASTENERS SHEARED AND PLATE IS CRACKED / R/H TRAILING EDGE ACVITY I/B PLATE ABOVE SAIL TAIL REMOVED IAW B-737-700 SRM 51-40-02-0G-0 AND REPLACED NEW IAW -737-700 SRM 51-40-05-0G-0 & SRM 51-40-06-0G-0 & SRM 51-4-02-0G-0. A-TAG # WN8798
R/H WING TRAILING EDGE CAVITY 10' INBD OF DIFLECTOR RIB ASSY BULB SEAL RETAINER IS CRACKED OUTBD SIDE AT FASTENER HOLE / REMOVED CRACKED R/WING TRAILING EDGE FITTING AND BULB SEAL RETAINER 10' I/B DEFLECTOR RIB. VERIFIED NEW PART. P/N 115A2953-2 (A21612) IAW IPC 57-50-00-25 MATCH DRILLED NEW FITTING IAW 737-700 SRM 51-40-050G-0 AND INSTALLED IAW 737-700 SRM 51-40-02-0G-0
RIGHT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 4 (STAB STA 120.30) IS CRACKED AT 2ND VERTICAL STIFFENER. / REPAIRED STIFFENER IAW SRM.
L/H WING AFT TRAILING EDGE CAVITY WIGGLE PLATE UNDER SAIL TAIL INBOARD SIDE, RIVETS SHEARED AND PLATE CRACKED. R&R WIGGLE PLATE IAW SRM & AMM.
L/H WING PANEL 551FB FWD BRACKET IS BROKEN OFF 27' FROM OTBD EDGE AS MARKED. / REMOVED BRACKET @ L/H WING PANEL 551FB FWD END 27 FROM OUTBOARD EDGE IAW SRM 51-40-02-0G-0 AND INSTALLED NEW BRACKET P/N 287A9152 A-TAG WN5864 AT L/H WING PANEL 551FB FWD END 27' FROM O/B EDGE IAW SRM 51-40-02-0G-0 PG 2 STEP 4B
RIGHT WING TRAILING EDGE PANEL 661CB INTERNAL MATING SURFACE AFT FASTENER ROW HAS SEVERAL CRACKED HOLES / REPAIRED FASTENER HOLES ON PANEL 661CB I/A/W SRM 57-51-01-2R-1 REV. 68; SRM 51-70-04-2R-9 REV.68 AND AMM 51-21-99-300-802 REV. 69; AMM 51-21-81-370-802 REV. 69 A33188; A22759; A72331; A98284; A20068
R/H WING TRAILING EDGE CAVITY ABOVE #6 FLAP TRACK ASSEMBLY WIGGLE PLATE ASSEMBLY CRACKED AT INBOARD FASTENER LOCATION. R&R WIGGLE PLATE ASSEMBLY IAW SRM AND DWG.
RIGHT WING TRAILING EDGE PANEL 661BB INTERNAL MATING SURFACE AFT FASTENER ROW HAS SEVERAL CRACKED HOLES / REPAIRED DAMAGE TO FASTENER HOLES ON PANEL 661BB IAW SRM 57-51-01-2R-1 REV 68; SRM 51-70-04-2R-9 REV. 68; AMM 51-21-99-300-802 REV. 69; AMM 51-21-81-370-802 RE. 69 A33188; A22759; A72331; A20069; A98284
RIGHT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 4 (STAB STA 120.30) IS CRACKED AT 3RD VERTICAL STIFFENER. REPAIRED STIFFENER IAW SRM.
RIGHT WING TRAILING EDGE PANEL 651GB AFT BULB SEAL RETAINER IS CRACKED AT OUTBOARD END / REPLACED CRACKED BULB SEAL RETAINER ON PNL 651GB IAW SRM 51-40-02-0G-0. A TAG #WN8435
SECTION 48 EXTERNAL SKIN HAS A DENT AT STA 1016 +4.5", 2.0" ABOVE S-14L. / REPAIRED SKIN PER ER AND SWA EA.
AFT CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED. / REMOVED AND REPLACED SCUFF PLATE REF AMM 53-11-02.
LEFT FWD EMERGENCY BATTERY PACK DOES NOT LAST THE REQUIRED TEST TIME. R&R LEFT FWD EMERGENCY BATTERY PACK AND CHARGER PER AMM.
RIGHT FWD EMERGENCY BATTERY PACK DOES NOT LAST THE REQUIRED TEST TIME. R&R RIGHT FWD EMERGENCY BATTERY PACK AND CHARGER PER AMM 33-51-06.
R2 DOOR EMERGENCY EXIT LIGHTS INOP. R&R AFT RH BATTERY PACK IAW MM.
FORWARD SERVICE DOOR SLIDE GIRT BAR WILL NOT STAY IN THE DISARMED/STOWED POSIITON. ADJUSTED AFT BAR RETAINER HOOK ON FWD SERVICE DOOR AND VERIFIED SECURITY OF GIRT BAR WITH SLIDE DISARM REF AMM 25-66-01
L/H SIDE EMERGENCY LIGHT BEHIND L2 DOOR INOP. RELAMPED LIGHT PER AMM.
MID CABIN CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN DISLODGED. REINSTALLED COVER PER SIP.
LT PHOTOLUMINESCENT STRIP MISSING AT AISLE 1. INSTALLED STRIP PER DWG.
AFT GALLEY FLASHLIGHT COMPARTMENT DOOR LATCH LOOSE. SECURED LATCH PER SIP.
RIGHT WING SUPPORT ANGLE CRACKED AT DEFLECTOR RIB. R & R THE SUPPORT ANGLE IAW SRM AND DWG.
LEFT WING; LOWER LEADING EDGE PANEL 521ZB; CRACKED AT FOWARD OUTBOARD FASTENER HOLE. / REPAIRED AND RESTORED FINISH ON EDGE PANEL 521ZB OUTBOARD FASTENER HOLE IAW B737-700 AMM 51-21-99-300-801 REV 63; SRM 51-70-14-2R-REV62; SRM 51-70-04-2R-0 REV 62 SRM 57-41-01-2R-1 REV 62
LEFT WING LOWER TRAILING EDGE SKIN WIGGLE PLATE JUST OUTBOARD OF THE NR 3 FLAP TRACK CRACKED. R & R THE WIGGLE PLATE IAW SRM AND DWG.
PASSENGER CABIN FLOOR PANEL BREAK CRACKED AT STA 540 BL 0 TO RBL 25 / STA 540 BETWEEN BL O AND RBL 25'; REMOVED AND REPLACED PANEL BREAK MPN 143A5240-36 SI # 75309009 ATAG VE0043; IAW BOEING DWG 143A0060 AND SRM 51-40-02-0G-0
REF. EA1-A55-3550 STEP 16. HORIZONTAL STAB. RIGHT SIDE LEADING EDGE RIB HAS ONE ELONGATED RIVET HOLE ON LOWER FLANGE. (AT STATION 133.15) / RH STAB HORIZONTAL LEADING EDGE RIB AT STA 133.15 REMOVED ON NON-ROUTINE X637200. RECIVED NEW RIB P/N 186A1307; SI# 7550164 A-TAG WN7783 LOCATED AND DRILLED NEW RIB AND INSTALLED NEW RIN IN RH STAB HORIZONTAL LEADING EDGE AT STA 133.15 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 186A1001 REV A
RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT HSS 216.83, UPPER AFT FASTENER HOLE. R & R THE RIB IAW SRM & DWG.
RIGHT STABILIZER LEADING EDGE RIB CRACKED AT BS 114.55 BETWEEN RADIS AND FASTENER HOLE. R & R THE RIB IAW DWG & SRM.
KEEL BEAM PANEL 192F HAS CORROSION AT BOTH DME ANTENNA MOUNT LOCATIONS / REPAIRE OF KEEL BEAM PANEL WAS ACCOMPLISHED ON BACK SHOP REPAIRE ORDER # 36442 1000 0004 PANEL #192F AND #36440-1000-0036
FLOOR BOARD 241TF IS PUNCTURED [MARKED] / REPAIRED FLOORBOARD 241TF PUNCTURE I-A-W B737-700SRM 53-00-50-2R-4 REV 62 SRM 53-00-50-2R-0 REV 62
SUPPLEMENTAL INFORMATION: PASSENGER CABIN SEAT TRACK LBL 45 BETWEEN STA 500B AND 520 GOUGED WITH MINOR CORROSION IN BASE AND CROWN AS MARKED / BLENDEDGAUGEAT PASSENGER CABIN SEAT TRACK LBL 45 STA 500B-520 AND FOUND DEPTH OF .030' LOSS; .020' ALLOWED FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1. CUT OUT DAMAGED SECTION OF SEAT TRACK AND SPLICED IN NEW IAW WA 1-A53-11779REV. I AND SRM 53-00-52-2R-4
TEE CAP CRACKED AT BS 520, RBL 65. REPAIRED THE TEE CAP IAW EA.
PASSENGER CABIN FWD WET AREA BETWEEN STA 312 AND 328 LBL 47 INTERCOASTAL IS CRACKED AS MARKED / AT PASSENGER CABIN; FWD WET AREA; BETWEEN STA 312 TO 328 LBL 47REMOVED + REPLACED INTERCOSTAL IAW- BOEING DWG 141A5400 REV:- AND B737-700 SRM 51-40-02-0G-0 PAR 7.D. AND FIG 12. PART A TAG # IS A82274
PASSENGER CABIN FWD WET AREA BETWEEN STA 312 AND 328 RBL 31 INTERCOASTAL IS CRACKED AS MARKED / AT PASSENGER CABIN FWD WETAREA BETWEEN B.S.312 TO 328 RBL31 REMOVED AND REPLACED INTERCOSTAL I.A.W. BOEING DWG 141A541OU12;AND B737-700 S.R.M 51-40-02 PAR 7.FIG12; A-TAG # A82274
RT KEEL BEAM WEB ANGLE CRACKED AT BS 663. REPAIRED ANGLE IAW EA.
RIGHT WING INBOARD LEADING EDGE WING TO BODY FAIRING CURVED ANGLE CRACKED AT BS 500D. REPAIRED THE ANGLE IAW SRM.
AFT GALLEY R2 CUTOUT CREASE BEAM INBOARD CORRODED BETWEEN BS 956 TO 992. R & R THE CREASE BEAM IAW SRM AND DWG.
AFT CARGO BAY LONGITUDINAL WEB CORRODED AT BS 787, STRINGER 27R. R & R THE WEB IAW SRM AND DWG.
FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM AND DWG.
FORWARD CARGO BAY, RT BAFFLE ANGLE ON THE FORWARD SIDE OF FRAME CRACKED AT BS 500B. R & R THE ANGLE IAW DWG & SRM.
FORWARD CARGO BAY, LEFT SIDE, AFT OF FRAME ANGLE CRACKED AT BS 500C. R & R THE FRAME ANGLE IAW DWG AND SRM.
FORWARD CARGO BAY LEFT SIDE, FORWARD SIDE OF FRAME ANGLE CRACKED AT BS 500C. R & R THE FRAME ANGLE IAW DWG AND SRM.
FORWARD CARGO BAY LEFT FORWARD SIDE OF FRAME CRACKED AT BS 500B. R & R THE FRAME ANGLE IAW DWG AND SRM.
L1 DOOR CUTOUT LT CREASE BEAM VERTICAL FLANGE WAS CRACKED AT BS 302. R & R THE CREASE BEAM IAW DWG AND SRM.
CARGO TRACK CORRODED AT BS 942, LBL 3. R & R THE CARGO TRACK IAW SRM AND DWG.
AFT CARGO DOOR THRESHOLD WEB CORRODED BETWEEN BS 795 & 835. REPAIRED THE WEB IAW SRM & DWG.
AFT CARGO BAY "Z" ANGLE CORRODED BETWEEN BS 727C TO BS 787, LBL 25. REPAIRED Z ANGLE IAW SRM.
AFT CARGO BAY "Z" ANGLE CORRODED BETWEEN BS 727C TO BS 787, RBL 25. REPAIRED Z ANGLE IAW SRM.
RT WING TRAILING EDGE INBOARD OF INBOARD DEFLECTOR RIB VERTICAL INTERCOSTAL ANGLE COMMON TO RIB CRACKED. R&R ANGLE IAW AMM & DWG.
FORWARD CARGO PIT GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM AND DWG.
FORWARD CARGO PIT LOWER SILL WEB STA 440 - 492 RBL 24 - RBL 29 HAS CORROSION ON UPPER AND LOWER SURFACES / BLEND CORROSION ON FWD PIT SILL WEB IAW SRM 53-30-15-1A-1; ORIGINAL THICKNESS .045; .007 MAT'L LOSS WITH .038 REMAINING OUT OF LIMITS VERIFIED NEW SILL WEB IAW 143A8330 ATAG OW0067 P/N 654A0003-58 LOCATED AND DRILLED NEW WEB IAW SRM 51-40-05-06 & BOEING DWG 143A8330 INSTALLED NEW WEB FWD CARGO IAW BOEING DWG 143A8330
FORWARD CARGO PIT DOOR SURROUND AFT SHIELD STA 492 - 500A RBL 23 HAS CORROSION ON UPPER AND LOWER SURFACES / REMOVED CORROSION. EVALUATED DAMAGE AS OUT OF LIMITS. REMOVED SHIELD IAW SRM 51-40-02; SRM 51-40-05; AND DWG 143A0080 REV-
AFT CARGO COMPARTMENT; STA 947.5; AFT BULKHEAD LOWER ATTACH ANGLE RBL 9-14 HAS CORROSION. / REMOVED AND REPLACED AFT BULKHEAD LOWER ATTACH ANGLE AT RBL 9 - 14 DUE TO CORROSION ORIGINAL THICNKESS .090' MATERIAL REMAINING .060' MATERIAL IS OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED + REPLACED IAW SRM 51-40-02-0G-0 + IPC 53-11-51-01
FORWARD CARGO PIT STA 500D BULKHEAD LOWER ANGLE LBL 24 - RBL 24 HAS CORROSION ON UPPER SURFACE / REMOVED CORROSION AT STA 500D LBL 24 - RBL 24 ON ANGLE ASSY FOUND TO BE 100% OUT OF LIMITS IAW SRM 51-10-02-0G-0 & SRM 53-00-53-1A-2 VERIFIED P/N FOR NEW RAIL ASSY 143A9485-35/7530142 IAW SWA AIPC 53-11-01-43 INSTALLED NEW RAIL ASSY FWD PIT STA 500D LBL 24 - RBL 24 IAW SRM 51-40-02-0G-0 PG 3 STEP B.
AFT CARGO BAY STA767 PLUS 4' FLOOR PANEL SPLICE HAS CORROSION. / REMOVED CORROSION AT AFT CARGO BAY STA 767+4' FLOOR PANEL SPLICE IAW SRM 51-10-02-0G-0 FOUND TO 100% OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED AND REPLACED SPLICE PN: 146A9401-4 IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV A TAG A27911
RIGHT WING TRAILING EDGE INBOARD OF INBOARD DEFLECTOR RIB UPPER FIXED PANEL MID TRIANGLE SHAPED STIFFENER CRACKED. R & R THE STIFFENER IAW SRM.
FORWARD CARGO BAY LT SIDE ANGLE CORRODED BETWEEN BS 500+5 TO 500C+11, LBL 21. REPAIRED THE ANGLE IAW SRM.
FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 36 TO RBL 43. R & R THE FLOORBEAM IAW SRM AND EA.
LEFT WING LEADING EDGE PANEL 521KB FORWARD EDGE MATING SURFACE HAS EROSION/DELAM AT 3 AREAS (MARKED) / REPAIRED LEFT WING L/E PANEL 521 KB FWD EDGE MATING SURFACE AS MARKED AND REPAIRED ALLUMINIUM FOIL I/A/W SRM 51-70-04-2R-6 REV 62 AND SRM 51-70-14-2R-3 REV 62
L2 DOOR EXIT LIGHT LENS LOOSE. R&R LIGHT ASSY PER MM.
LT OVERWING EXIT LIGHT INOP. R&R EXIT LIGHT BATTERY ASSY PER MM.
R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF PACK, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.
AIR TURN BACK, LOUD BANG ON TAKEOFF, FOLLOWED BY LOUD AIR NOISE IN AIR. ALL OTHER INDICATIONS NORMAL. R & R NR 1 ENG ASSEMBLY IAW MT.
CENTER CABIN OVERWING EXIT LIGHT HOUSING BROKEN. R & R LIGHT ASSEMBLY IAW AMM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN, CRACKED AT STAB STATION 184.7, 9" FWD OF STAB REAR SPAR. REPAIRED SKIN IAW ACO & EA.
LEFT HORIZONTAL STABILIZER LOWER INSPAR SKIN, CRACKED AT STAB STATION 184.7 RIB, FROM REAR SPAR. REPAIRED SKIN IAW EA.
RIGHT HORIZONTAL STABILIZER LOWER SKIN, CRACKED AT STAB STATION 184.7, 9" FWD OF STAB REAR SPAR. REPAIRED SKIN IAW CCO & EA.
LEFT HORIZONTAL STABILIZER INSPAR SKIN CRACKED AT STAB STATION 138.70 RIB, 17" FROM REAR SPAR. REPAIRED SKIN IAW ACCO.
RIGHT HORIZONTAL STAB LOWER IN SPAR SKIN CRACKED AT REAR SPAR, BETWEEN STAB STATION 92.7 & 101.9. REPAIRED SKIN IAW CCO.
RIGHT HORIZONTAL STABILIZER, LOWER SKIN CRACKED AT STABILIZER STATION 138.7 24" AFT OF LE. REPAIRED SKIN IAW CCO.
RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 101.9, HORIZONTAL FLANGE AT AFT SPAR, CRACKED ON OUTBOARD SIDE. REPAIRED RIB IAW EA.
RIGHT HORIZONTAL STABILIZER RIB CRACKED AT 2ND VERTICAL STIFFENER FROM AFT SPAR AT STATION 129.5. REPAIRED ANGLE IAW SRM.
LEFT HORIZONTAL STABILIZER STATION 120.30, 3RD RIB AFT CRACKED. REPAIRED RIB IAW SRM.
LONGITUDINAL FLOORBEAM FLOOR SEAT TRACK, CRACKED AT BS 727B, RBL 45. REPAIRED SEAT TRACK IAW EA.
LONGITUDINAL FLOORBEAM FLOOR SEAT TRACK, CRACKED AT BS 727B, RBL 24. REPAIRED SEAT TRACK IAW EA.
LONGITUDINAL FLOORBEAM FLOOR SEAT TRACK, CRACKED AT BS 727B, LBL 24. REPAIRED SEAT TRACK IAW EA.
LONGITUDINAL FLOORBEAM FLOOR SEAT TRACK, CRACKED AT BS 727B, LBL 45. REPAIRED SEAT TRACK IAW EA.
RIGHT OVERWING EXIT LIGHT ASSEMBLY LOOSE. REPAIRED LIGHT ASSEMBLY IAW EA.
RIGHT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LUG FACE CORRODED. REPAIRED FITTING IAW EA.
RT FLIGHT DECK WINDOW FRAME CRACKED. REPAIRED FRAME IAW SWA EA.
RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 184.7, 9" FWD OF STAB REAR SPAR. REPAIRED SKIN IAW SRM.
AFT CARGO FLOOR SUPPORT STRAP CORRODED AT BS 772 BETWEEN LBL 8 TO RBL 21. R & R STRAP IAW SRM.
L1 DOOR FWD GIRT BAR TIE DOWN FITTING CORRODED AT BS 312, LBL 54. R & R FITTING IAW SRM.
RT VERTICAL PRESS DECK WEB CRACKED AT BS 663, RBL 33. REPAIRED WEB IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344 LBL 45. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328 RBL 30. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 294 TO BS 312 RBL 15. R & R INTERCOSTAL IAW SRM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.70 2. REPAIRED SKIN PER SRM.
CENTER EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT IAW AMM.
RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.7. REPAIRED RIB IAW ER & EA.
LEFT HORIZONTAL STABILIZER INSPAR SKIN CRACKED AT STA 184.70. REPAIRED SKIN IAW SRM.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT STA 129.50. REPAIRED RIB IAW SRM.
RIGHT HORIZONTAL STABILIZER INSPAR SKIN CRACKED BETWEEN STA 92.70 TO STA 101.90. REPAIRED SKIN IAW SRM.
LEFT HORIZONTAL STABILIZER INSPAR SKIN CRACKED AT STA 138.70. REPAIRED SKIN IAW SRM.
RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.7 3RD VERT STIFFENER. REPAIRED RIB PER SRM.
LEFT EMERGENCY BATTERY PACK FAILED LONG CHECK. REMOVED AND REPLACED BATTERY PER AMM.
RIGHT EMERGENCY BATTERY PACK FAILED LONG CHECK. REMOVED AND REPLACED BATTERY PER AMM.
L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.
L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.
DURING SCHEDULED MV2 CHECK, FOUND OVERWING EEPLS INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS LENS MISSING AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.
DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS BROKEN AT ROW 2. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.
DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
RIGHT AFT EMERGENCY EXIT SIDEWALL SIGN COVER LOOSE. REMOVED AND REPLACED SIGN ASSY PER MM.
EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM.
EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.
EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.
EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM.
EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM.
EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.
EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STUCK WILL NOT LOCK. CLEANED GIRT BAR PER MM.
DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, FWD LT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
EEPLS ASSY LOOSE AT ROW 3 ABC. SECURED EEPLS ASSY PER MM.
EEPLS ASSY LOOSE AT ROW 1 ABC. SECURED ASSY PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS END CAP MISSING. INSTALLED END CAP PER MM.
EEPLS COVER MISSING ROW 1 ABC. INSTALLED COVER PER MM.
EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM.
R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED EVAC SLIDE FWD GIRT BAR FITTING PER MM.
EEPLS LIGHT COVER LOOSE AT ROW 1 ABC. SECURED EEPLS LIGHT COVER PER MM.
R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.