N261WN
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 | 2011-12-01 – 2011-12-01 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2011-12-01 – 2011-12-01 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AFT CARGO BIN FLOOR CRACKED. PANEL 140CF 15. OK TO CONTINUE IAW MEL 25-16-01 SP1B AUTH 314501. R & R AFT FLOOR PANEL 140CF IAW AMM25-52-10.
SEAT 11D OVER RECLINES INTO EXIT ROW. SECURED RECLINE LOCK IAW CMM 25-21-42. NO FURTHER DEFECTS NOTED FOR SEAT 11D.
L/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06
R2 SLIDE OUT OF LIMITS. REMOVED AND REPLACED THE R2 SLIDE IAW AMM 25-60 6-01.
AT ROTATION AIRCRAFT YAWED TO THE LEFT WITH A VIBRATION FELT; AFTER ABEING AIRBORNE NO FLIGHT CONTROL DISCREPANCIES NOTICED; NO ABNORMAL ENGINE PERAMETERS NOTED; RETURNED TO AIRFIELD NORMAL SMOOTH LANDING WITH NO ABNORMAL VIBRATIONS FELT NO OVERWEIGHT LANDING OCCURED<[01] REMOVED AND REPLACED LEFT MAIN SHIMMY DAMPER IAW M/M 32-11-81. PERFORMED LANDING GEAR SHIMMY/VIBRATION PHASE 1 INSPECTION IAW M/M 05-51-68. SEE ATTACHED NON ROUTINE FOR FDR DOWNLOAD.
FO SIDE 1ST ROW PHOTOLUMINESCENT STRIP DAMAGED<[01] OK TO CONTINUE PER MEL 33-19-01 SP1<BR>AUTH# 248928;[02] REMOVED AND REPLACED FO SIDE 1ST ROW PHOTOLUMINESCENT STRIP PER SIP
LEADING EDGE FLAPS + SLATS AND TRAILING EDGE FLAPS DID NOT EXTEND WHEN FLAPS LEVER PLACED TO FIVE. FLAP ASYMMETRY INDICATED WHEN ALT FLAP SWITCHED DOWN. LEADING EDGE FLAPS+SLATS EXTENDED<[01] R & R LH FLAP POS TRANSMITTER PER AMM 27-58-01(E148386) <BR>R/R CONNECTOR D275 IAW SWPM 20-61 (E146121)<BR>REF TSR 2025001644 & BOEING SERVICE LETTER 737-SL-27-196-D FOR PART EFFECTIVITY. OPS CHECK GOOD
LEADING EDGE FLAPS + SLATS AND TRAILING EDGE FLAPS DID NOT EXTEND WHEN FLAPS LEVER PLACED TO FIVE. FLAP ASYMMETRY INDICATED WHEN ALT FLAP SWITCHED DOWN. LEADING EDGE FLAPS+SLATS EXTENDED<[01] R & R LH FLAP POS TRANSMITTER PER AMM 27-58-01(E148386) <BR>R/R CONNECTOR D275 IAW SWPM 20-61 (E146121)<BR>REF TSR 2025001644 & BOEING SERVICE LETTER 737-SL-27-196-D FOR PART EFFECTIVITY. OPS CHECK GOOD
FLOOR LIGHTING STRIP SEGMENT INOP. FRONT; FO SIDE ROW 1.<[01] R&R FLOOR LIGHTING STRIP AT ROW 1; FO?S SIDE PER AMM 25-27-31.
PAX CABIN AFT LEFT ENTRY DOOR SLIDE LOWER COVER IS CHAFFING AGAINST WITH SCUFF PLATE WHEN TO CLOSE THE DOOR 2024-361966<[01] PERFORMED REPOSITION OF SLIDE IN THE SLIDE COMPARTMENT AT AFT ENTRY DOOR I.A.W. B737-700 AMM 25-66-01-400-803 AND MT 725-61-06 (TTG8Q00UDMF9) SLIDE LOWER COVER NO MAKE CONTACT WITH DOOR FRAME.;[02] PERFORMED REPOSITION OF SLIDE IN THE SLIDE COMPARTMENT AT AFT ENTRY DOOR I.A.W. B737-700 AMM 25-66-01-400-803 AND MT 725-61-06 (TTG8Q00UDMF9) SLIDE LOWER COVER NO MAKE CONTACT WITH DOOR FRAME.
POPPED OUT C/B LIGHTING EMER CHGR WHEN TURN THE EMER EXIT LIGHT SWITCH TO OFF POSITION<[01] REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY M1673 IAW B737-700 AMM 33-51-06-960-805; TEST IS OK.
CRACK ON SERVICE DOOR SCUFF PLATE CENTER SIDE AT FWD GALLEY AREA 2024-361946<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A23217720;DUE DATE:14-FEB-25.;[02] . TOOL USED; RADIOMETER/PHOTOMETER KIT; P/N: XRP-3000; S/N: 1859843; DUE DATE: 24/JUL/24;[03] REPAIRED SERVICE DOOR SCUFF PLATE CENTER SIDE AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED SERVICE DOOR SCUFF PLATE CENTER SIDE AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.
CRACK BODY STATION 540 SUPPORT BRACKET LOCATED AT LT SIDE AT KEEL BEAM 2024-361808<[01] REPLACED BODY STATION 540 SUPPORT BRACKET LOCATED AT LT SIDE AT KEEL BEAM IAW BOEING 737-700 SRM 51-10-02-0G-0 STEP 9 AND BOEING 737-700 SRM 51-40-02-0G-0 STEP 9;[02] REPLACED BODY STATION 540 SUPPORT BRACKET LOCATED AT LT SIDE AT KEEL BEAM IAW BOEING 737-700 SRM 51-10-02-0G-0 STEP 9 AND BOEING 737-700 SRM 51-40-02-0G-0 STEP 9
CRACK SLAT 1 AUXILIARY TRACK ON SUPPORT BRACKET LOCATED LEADING EDGE AREA INTERNAL CAVITY AT LT WING 2024-361803<[01] REPLACED SUPPORT BRACKET LOCATED SLAT 1 AUXILIARY TRACK ON LEADING EDGE AREA INTERNAL CAVITY AT LT WING I.A.W. B737-700 SRM 51-40-02-0G-0 AND CMM 57-43-01 FIGURE 1 (SHEET 12 ) AND TOOK MEASURE OF CRACK IS L: 2.024 INCH TOOL USED DIGITAL CALIPER P/N 500-197-30 S/N B23316910 DUE DATE 04-FEB-25;[02] COMPLETED TASK CERTIFIED
DETERIORATED HARDWARE GIRT BAR FITTING ON FWD SERVICE AND ENTRY DOOR AT FWD GALLEY AREA 2024-361788<[01] REPLACED HARDWARE GIRT BAR FITTING ON FWD SERVICE AND ENTRY DOOR AT FWD GALLEY AREA IAW B737-700- AMM 25-66-02-400-801;[02] JOB COMPLETED
DETERIORATED HARDWARE GRIT BAR FITTING ON AFT SERVICE AND ENTRY DOOR AT AFT GALLEY AREA 2024-361792<[01] REPLACED HARDWARE GRIT BAR FITTING ON AFT SERVICE AND ENTRY DOOR AT AFT GALLEY ARE I.A.W B737-700 SOPM-20-50-01;[02] REPLACED HARDWARE GRIT BAR FITTING ON AFT SERVICE AND ENTRY DOOR AT AFT GALLEY ARE I.A.W B737-700 SOPM-20-50-01.
CRACK BLADE ACCESS PANEL 343AB AT RT HORIZONTAL STAB 2024-361769<[01] REPLACED BLADE ASSY LOC. ACCESS PANEL 343AB AT RT HORIZONTAL STAB I.A.W. B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND TOOK MEASURE OF CRACK IS L: 0.437 INCH TOOL USED DIGITAL CALIPER P/N 500-196-30 S/N A21033526 DUE DATE 06-DEC-24;[02] CORRECTED STEP 1<BR>REPLACED BLADE ASSY LOC. ACCESS PANEL 343AB AT RT HORIZONTAL STAB I.A.W. B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 186A3005 SHEET: 2 REV: B AND TOOK MEASURE OF CRACK IS L: 0.437 INCH TOOL USED DIGITAL CALIPER P/N 500-196-30 S/N A21033526 DUE DATE 06-DEC-24.;[03] CLOSED
CORROSION SUPPORT ZEE LOCATED BTW BS727 TO BS787 WL156 LBL21 AT AFT CARGO COMPARTMENT 2024-361772<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130064101; CAL DUE DATE: 13-DEC-24;[02] REPAIRED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 WL156 LBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM B737-700 53-00-53-2R-6 REPAIR 6 AND DWG 146A7500 SHEET 85 REV A ;DWG 140N4500 SHEET 17 REV J.;[03] CORRECTED STEP 2.<BR>REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 WL156 LBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DWG 146A7500 SHEET 85 REV A; DWG 140N4500 SHEET 17 REV J. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] CERTIFICATED AS RII <BR>REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 WL156 LBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DWG 146A7500 SHEET 85 REV A; DWG 140N4500 SHEET 17 REV J. SEE INDIVIDUAL SIGNOFFS BELOW.
CORROSION SUPPORT ZEE LOCATED BTW BS727 TO BS767 WL156 AND RBL21 AT AFT CARGO COMPARTMENT 2024-361770<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130064101; CAL DUE DATE: 13-DEC-24;[02] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 WL156 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 DWG: 146A7502 SHEET: 26 REV -;[03] CORRECTED STEP 2<BR>REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 WL156 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 DWG: 146A7502 SHEET: 26 REV - SEE INDIVIDUAL SIGNOFFS BELOW;[04] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 WL156 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 DWG: 146A7502 SHEET: 26 REV - SEE INDIVIDUAL SIGNOFFS BELOW
CRACK TRACK RBBL 13.84 AT LEVEL OF BS 767 AFT CARGO COMPARTMENT 2024-361768<[01] TOOL USED ON STEP 4 AND 5: EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030457 DUE DATE: 15 OCT 24.;[02] REPAIRED CARGO TRACK RBBL 13.84 LOCATED BS767 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPAIRED CARGO TRACK RBBL 13.84 LOCATED BS767 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL SIGNOFFS BELOW.<BR>CERTIFIED AS RII
CRACK TRACK RBBL 13.84 AT LEVEL OF BS 727E AFT CARGO COMPARTMENT 2024-361771<[01] FAULT WAS RESOLVED ON ANOTHER FAULT DUE TO REPAIR WAS PERFORMED FROM BS 727D PLUS 12 INCHES TO BS 767 PLUS 12 INCHES SEE TTG8Q00TT1W8;[02] FAULT WAS RESOLVED ON ANOTHER FAULT DUE TO REPAIR WAS PERFORMED FROM BS 727D PLUS 12 INCHES TO BS 767 PLUS 12 INCHES SEE TTG8Q00TT1W8<BR>CERTIFIED AS RII
CRACK FWD SERVICE DOOR CUT OUT TIE-CLIP AT S-10R AND STA 277 AT PASSENGER CABIN 2024-361697<[01] REPLACED TIE-CLIP AND FASTENERS AT FWD SERVICE DOOR CUT OUT S-10R AND STA 277 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; DWG-141A1110 SHEET: 18 REV: - AND DWG-141A8380 SHEET: 21 REV: - .;[02] REPLACED TIE-CLIP AND FASTENERS AT FWD SERVICE DOOR CUT OUT S-10R AND STA 277 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; DWG-141A1110 SHEET: 18 REV: - AND DWG-141A8380 SHEET: 21 REV: - .<BR>CERTIFIED AS RII
CRACK FWD SERVICE DOOR CUT OUT TIE-CLIP AT S-10R AND STA 277 AT PASSENGER CABIN 2024-361697<[01] REPLACED TIE-CLIP AND FASTENERS AT FWD SERVICE DOOR CUT OUT S-10R AND STA 277 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; DWG-141A1110 SHEET: 18 REV: - AND DWG-141A8380 SHEET: 21 REV: - .;[02] REPLACED TIE-CLIP AND FASTENERS AT FWD SERVICE DOOR CUT OUT S-10R AND STA 277 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; DWG-141A1110 SHEET: 18 REV: - AND DWG-141A8380 SHEET: 21 REV: - .<BR>CERTIFIED AS RII
CRACK ON STIFFENER LOCATED BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN 2024-361678<[01] REPLACED STIFFENER AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02.;[02] CORRECTED STEP 1.<BR>REPLACED STIFFENER AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED STIFFENER AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02.<BR>SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ENTRY DOOR CUT OUT SUPPORT ANGLE LOCATED AT FWD FACE THE STA294.5 AND S-13L AT FWD GALLEY AREA 2024-361700<[01] REPLACED SUPPORT ANGLE LOCATED ENTRY DOOR CUT OUT AT FWD FACE THE STA294.5 AND S-13L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 141A1311 SHEET: 1 REV C SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED SUPPORT ANGLE LOCATED ENTRY DOOR CUT OUT AT FWD FACE THE STA294.5 AND S-13L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 141A1311 SHEET: 1 REV C SEE INDIVIDUAL SIGNOFFS BELOW<BR>RII CERTIFIED
CRACK ENTRY DOOR CUT OUT WEB INTERCOSTAL AT S-16L AND BETWEEN STA294.5 TO STA 303.9 AT FWD GALLEY AREA 2024-361693<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BSTA 294.5 TO BSTA 303.9 AT STR 16L. AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02. PARAGRAPH 9. DWG# 141A8180 SHEET 27 REV. ?C?. AND SHEET 28. REV. ?C?. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BSTA 294.5 TO BSTA 303.9 AT STR 16L. AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02. PARAGRAPH 9. DWG# 141A8180 SHEET 27 REV. ?C?. AND SHEET 28. REV. ?C?. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED
DETERIORATED GIRT BAR FITTING SLEEVE ON ACCESS FLOOR PANEL 242UF (2EA) AND 241ABF (2EA) AT AFT GALLEY AREA (4EA) 2024-361723<[01] REPLACED GIRT BAR FITTING SLEEVE ON ACCESS FLOOR PANEL 242UF (2EA) AND 241ABF (2EA) AT AFT GALLEY AREA IAW B737-700 SRM 53-00-50-2R-0 REPAIR GENERAL PARA. 5 S(1). TOOL USED: SCALE P/N: CR5200; S/N: 8343110878; DUE DATE: 05-MAR-25. HOT BONDER P/N: HCS9200B; S/N:18185761; DUE DATE: 24-JAN-25;[02] CERTIFIED WORK PERFORMED.
CRACK ENTRY DOOR CUT OUT WEB INTERCOSTAL AT S-16L AND BETWEEN STA294.5 TO STA 303.9 AT FWD GALLEY AREA 2024-361693<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BSTA 294.5 TO BSTA 303.9 AT STR 16L. AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02. PARAGRAPH 9. DWG# 141A8180 SHEET 27 REV. ?C?. AND SHEET 28. REV. ?C?. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BSTA 294.5 TO BSTA 303.9 AT STR 16L. AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02. PARAGRAPH 9. DWG# 141A8180 SHEET 27 REV. ?C?. AND SHEET 28. REV. ?C?. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED
CRACK BILGE AREA SUPPORT ZEE LOCATED BETWEEN STA 500B TO STA 500C RH SIDE AT FWD CARGO COMPARTMENT 2024-361692<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN STA 500A TO STA 500D RH SIDE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 AND DWG 141A7500 SHEET 58 REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ZEE LOCATED BETWEEN STA 500A TO STA 500D RH SIDE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 AND DWG 141A7500 SHEET 58 REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.
CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2024-361725<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189516;DUE DATE:17-JAN-25.;[02] TOOL USED IN STEP 4: RADIOMETER/PHOTOMETER; P/N: XRP-3000; S/N: 1859843; DUE DATE: 24-JUL-24.;[03] REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.
CRACK INNER CHORD AT STA 312 AND AT LEVEL S-17L AT FWD GALLEY AREA 2024-361648<[01] REPLACED INNER CHORD; BS 270 TO BS 360 AND LBL 55 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 141A8110 SHEET: 11 REV:-. AND DWG 141A5220 SHEET: 1 REV: -. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED INNER CHORD; BS 270 TO BS 360 AND LBL 55 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 141A8110 SHEET: 11 REV:-. AND DWG 141A5220 SHEET: 1 REV: -; RII . SEE INDIVIDUAL SIGN-OFF BELOW.
CORROSION FLOOR BEAM LOCATED STA 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2024-361606<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 24-JUL-24;[02] ON STEP 10 TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 21-JUL-24.;[03] TOOL USED ON STEP 11 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 60009161631 DUE DATE: 11-MAR-25;[04] PERFORMED REPAIR FLOOR BEAM LOCATED STA 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED REPAIR FLOOR BEAM LOCATED STA 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 328 TO BS 344 AND LBL 45 FWD GALLEY AND LAV 2024-361603<[01] REPLACED WEB - INTERCOSTAL LOCATED FLOOR STRUCTURE BETWEEN BS 328 TO BS 344 AND LBL 45 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 44 REV -. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN-OFF BELOW
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-361597<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9 AND BOEING 737-700 DRAWING 141A5400 SHEET 20 REV -.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9 AND BOEING 737-700 DRAWING 141A5400 SHEET 20 REV -.SEE INDIVIDUAL SIGN OFF BELOW.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-361597<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9 AND BOEING 737-700 DRAWING 141A5400 SHEET 20 REV -.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9 AND BOEING 737-700 DRAWING 141A5400 SHEET 20 REV -.SEE INDIVIDUAL SIGN OFF BELOW.
CRACK FLOOR BEAM LOCATED STA 328 RBL 20 AT FWD GALLEY AREA 2024-361601<[01] TOOL USED EDDY CURRENT HIGH FREQUENCY INSPECTION P/N: NORTEC600D; S/N: 60009161631; DUE DATE: 11-MAR-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT ; P/N: XRP-3000; S/N: 1859843; DUE DATE : 24/JUL/24;[03] PERFORMED PERMANENT REPAIR ON FLOOR BEAM UPPER CHORD LOCATED AT BSTA 328 AND BETWEEN BL0 TO RBL 65. AT FWD GALLEY AREA. IAW B737-700 SRM 53-10-51-2R-7. REPAIR 7. SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR ON FLOOR BEAM UPPER CHORD LOCATED AT BSTA 328 AND BETWEEN BL0 TO RBL 65. AT FWD GALLEY AREA. IAW B737-700 SRM 53-10-51-2R-7. REPAIR 7. SEE INDIVIDUAL SIGN OFF BELOW.<BR>AS RII
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 312 TO BS 328 AND LBL 45 FWD GALLEY AND LAV 2024-361600<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 312 TO BS 328 LBL 45 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND BOEING 737-700 DRAWING 141A5400 SHEET 26 REV -.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 312 TO BS 328 LBL 45 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND BOEING 737-700 DRAWING 141A5400 SHEET 26 REV -.SEE INDIVIDUAL SIGN OFF BELOW.
CORROSION FLOOR BEAM LOCATED STA 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2024-361607<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 24-JUL-24;[02] ON STEP 10 TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 21-JUL-24.;[03] TOOL USED ON STEP 11 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 60009161631 DUE DATE: 11-MAR-25;[04] PERFORMED REPAIR FLOOR BEAM LOCATED STA 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED REPAIR FLOOR BEAM LOCATED STA 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED
WEAR ON DEFLECTION CONTROL RIB SUPPORTS BEAM O/B TRAILING EDGE AT LT WING 2024-361557. POWER PACK P/N: PE1068; S/N: PE0318-95852; DUE DATE: 16-SEP-25. REPAIRED DEFLECTION CONTROL RIB SUPPORTS BEAM O/B TRAILING EDGE AT LT WING IAW B737-700 SRM 57-51-02-2R-1 AND 57-52-01-2R-4. REPAIRED DEFLECTION CONTROL RIB SUPPORTS BEAM O/B TRAILING EDGE AT LT WING IAW B737-700 SRM 57-51-02-2R-1 AND 57-52-01-2R-4.
(CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOCATED ON BS 663 LH SIDE AT WING CENTER SECTION. 2024- 361522<[01] CALIPER P/N: 8647A42; S/N: B22058354; DUE DATE: 07-SEP-24.;[02] TOOL USED CALIPER P/N: 500-752-20 S/N: B16101265; DUE DATE: 06-DEC-24.;[03] TOOL USED. HOT BONDER P/N:HCS9200B; S/N: 18185733; DUE DATE: 25-JAN-25.;[04] TOOL USED SCALE P/N; CR5200 S/N; 8343110878 DUE DATE; 05-MAR-25;[05] TOOL USED HOT BONDER P/N:HCS9200B; S/N: 18185733; DUE DATE: 25-JAN-25.;[06] TOOL USED SCALE P/N; CR5200 S/N; 8342514499 DUE DATE; 17-FEB-25;[07] TOOL USED HOT BONDER P/N:HCS9200B; S/N: 18185733; DUE DATE: 25-JAN-25.;[08] TOOL USED ON STEP 12 UT EQUIPMENT P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 04-OCT-24;[09] REPAIRED WEB VAPOR BARRIER LOCATED BS 663 CENTER SECTION AS PER B737-700 SRM 57-10-10-2R-2 REPAIR 2 AND B737-700 SRM 51-70-04-2R-10 REPAIR 10 . SEE INDIVIDUAL SIGN OFFS BELOW;[10] CERTIFIED RII MAJOR REPAIR WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.
CRACK SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AT PASSENGER CABIN 2024-361562<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE 23-JAN-25.;[02] REPLACED SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AND FASTENERS AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 AND DWG 273A9110 SHEET: 6 REV: A; SEE INDIVIDUALS SIGN-OFF BELOW;[03] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW
CRACK SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AT PASSENGER CABIN 2024-361562<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE 23-JAN-25.;[02] REPLACED SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AND FASTENERS AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 AND DWG 273A9110 SHEET: 6 REV: A; SEE INDIVIDUALS SIGN-OFF BELOW;[03] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW
CRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING 2024-361560<[01] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-10-02 ITEM 9.<BR>TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N:A22257522 DUE DATE: 20-AUG-2024.;[02] CORRECTED STEP 1.<BR>REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-10-02 ITEM 9. CRACK IS L: 0.752 TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N:A22257522 DUE DATE: 20-AUG-2024.;[03] CORRECTED STEP 2.<BR>REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02. CRACK IS L: 0.752 TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N:A22257522 DUE DATE: 20-AUG-2024.;[04] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02. CRACK IS L: 0.752 TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N:A22257522 DUE DATE: 20-AUG-2024.
CRACK ANGLE TRAILING EDGE ORSS 271 LT WING 2024-361555<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 271 LT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEET: 7 REV: -.;[02] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 271 LT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEET: 7 REV: -.
DETERIORATED PLASTIC NUT OF ASSIST HANDLES AT FWD ENTRY DOOR (4 EA) 2024-361511<[01] REPLACED PLASTIC NUT OF ASSIST HANDLES AT FWD ENTRY DOOR I.A.W B737-700 AMM 52-11-31-400-802 STEP 3.G(2);[02] REPLACED PLASTIC NUT OF ASSIST HANDLES AT FWD ENTRY DOOR I.A.W B737-700 AMM 52-11-31-400-802 STEP 3.G(2)
DELAMINATED ACCESS PANEL 193AL BODY FAIRING AT LOWER FUSELAGE 2024-361518<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189521; DUE DATE: 26/JAN/25.;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 25-JAN-25.;[03] TOOL USED: SCALE P/N: CR5200 S/N: 8342514510 DUE DATE: 24/FEB/25.;[04] TOOL USED: HOT BONDER P/N:HCS9200B-AV S/N: 18196021 DUE DATE: 15/FEB/25.;[05] TOOL USED: HOT BONDER P/N:HCS9200B-AV S/N: 18196126 DUE DATE: 03/APR/25.;[06] TOOL USED: HOT BONDER PN:HCS9200B-AV SN:18175478 DUE DATE: 25-JAN-25;[07] UT EQUIPMENT USED P/N: EPOCH 650; S/N: 190984811; DUE DATE: 11-JAN-25;[08] REPAIRED ACCESS PANEL 193AL BODY FAIRING AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFFS BELOW.;[09] REPAIRED ACCESS PANEL 193AL BODY FAIRING AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFFS BELOW.
R2 GIRT BAR DOES NOT STAY SECURE WHEN DOOR IS OPENED<[01] INCREASE CLIP PRESSURE PER SIP
FWD ENTRY DOOR ESCAPE SLIDE GIRT BAR SKIRT FLAP RUBBER DISBONDED. R&R FWD ENTRY DOOR ESCAPE SLIDE IAW MT 725-61-06. INSPECTION C/W R&R FWD ENTRY DOOR ESCAPE SLIDE IAW MT 725-61-06.
AFT SERVICE DOOR EMERGENCY SLIDE AFT LOWER ISOLATOR CRACKED. R & R AFT SERVICE DOOR EMERGENCY SLIDE AFT LOWER ISOLATOR IAW SRM 51-40-02.
INTERIOR EMERGENCY LIGHTS AT ROWS 3 AND 6 INOP<[01] REMOVED AND REPLACED FWD SERVICE DOOR EMERGENCY EXIT LIGHT BATTERY PACK REF AMM 33-51-06. OPS CHECK NORMAL.
L2 DOOR ESCAPE SLIDE UPPER FWD MOUNT UPPER ISOLATOR CRACKED.<[01] REMOVED AND REPLACED L2 DOOR ESCAPE SLIDE UPPER FWD MOUNT UPPER ISOLATOR PER SRM 51-40-02
REF PREVIOUS LP#2119565 - FORWARD SERVICE DOOR SLIDE NEEDS REPACKED<[01] REMOVED FWD SVC DOOR SLIDE ASSY REF MT 725-61-06 FOUND SLIDE COVER CLASP BROKEN SEE LP#2119565 FOR FINAL CORRECTIVE ACTION
FWD SERVICE DOOR NEEDS REPACKED<[01] R&R FS DOOR ESCAPE SLIDE PER MT 725-61-06.
R-1 DOOR HEADER PANEL EXIT SIGN ASSY BROKEN / [01] REPLACED AT R1 DOOR HEADER PANEL EMERGENCY EXIT SIGH AND PERFORMED EXIT SIGH INSTALLATION TEST AS PER B737 AMM 33-51-01-960-802. TEST OK.;[02] PERFORMED EMERGENCY LIGHTS - OPERATIONAL TEST AS PER B737 AMM 33-51-00-710-801 AND EMERGENCY LIGHTS - OPERATIONAL CHECK AS PER B737 AMM 33-51-00-720-801. BOTH TEST FOUND OK.;[03] VERIFIED REPLACEMENT AND TEST
EMERGENCY LIGHTS AT L/H AND R/H O/W ESCAPE GROUND ILUMINATION LIGHT; AND 9ABC & 11ABC SEAT ROWS INOPERATIVE. / [01] T/S AND FOUND DEFECTIVE BATTERY PACK AT POSITION M1670 AS PER WDM 33-51-13.;[02] VERIFIED STEP 1;[03] REPLACED BATTERY PACK AT POSITION M1670 AND PERFORMED INSTALLATION TEST AS PER B737 AMM 33-51-06-960-805. TEST OK.;[04] VERIFIED REPLACEMENT
R/W INBD ACCESS PANEL 651AT LOWER BRACKET CRACK. / [01] INSTALLED PROTECTION OF EWIS AT WORK AREA AS PER AMM 20-60-07-913-801.;[02] REMOVED BRAKED AT R/WING I/B ACCESS PANEL 651AT LOWER AS PER REF SRM 51-40-02-0G-0.;[03] LOCATED AND DRILLED NEW BRACKET AT R/W ACCESS PANEL 651AT AS PER REF SRM 51-40-05-0G-0.;[04] VERIFIED STEPS #1; #2 AND #3; OK TO INSTALL NEW BRACKET.;[05] INSTALLED BRACKET AT R/W I/B ACCESS PANEL 651AT LOWER AS PER REF SRM 51-40-02-0G-0.;[06] REMOVED PROTECTION OF EWIS AT AREA AS PER REF AMM 20-60-07-913-801;[07] SUMMARY: INSTALLED PROTECTION OF EWIS AT WORK AREA AS PER AMM 20-60-07-913-801.REMOVED BRAKED AT R/WING I/B ACCESS PANEL 651AT LOWER AS PER REF SRM 51-40-02-0G-0.LOCATED AND DRILLED NEW BRACKET AT R/W ACCESS PANEL 651AT AS PER REF SRM 51-40-05-0G-0.INSTALLED BRACKET AT R/W I/B ACCESS PANEL 651AT LOWER AS PER REF SRM 51-40-02-0G-0.REMOVED PROTECTION OF EWIS AT AREA AS PER REF AMM 20-60-07-913-801;[08] VERIFIED STEPS #5 ; #6 AND #7.
FOUND CRACK AT R/H INBOARD FIXED LEADING EDGE STRAKELET SKIN. / [01] TRIM OUT AND NDT PERFORMED ON CARD TTG8Q00E06UM;[02] C/W 22-157-02433-WIP1; 22-157-02433-WIP2; 22-157-02433-WIP3; 22-157-02433-WIP4; 22-157-02433-WIP5;[03] PERFORMED EA 22-157-02433. REFERENCE FAULT TTG8Q00E06UM.;[04] PERFORMED EA 22-157-02433. REFERENCE FAULT TTG8Q00E06UM.
RT WING - INBD FIXED LEADING EDGE WEB AT LIGHT HOUSING CRACK AT INBD SIDE P/N 116A3410-2. / [01] REMOVED RT WING I/B FIXED L/E WEB ATVLIGHT HOUSING REF USED SRM 51-40-02-0G-0;[02] VERIFIED REMOVAL OF WEB;[03] OK TO INSTALL;[04] INSTALLED NEW RIGHT WING I/B FIXED L/E WEB AT LIGHT HOUSING AS PER B 737-7 SRM 51-40-02-0G AND DWG # 116A3410 DWG 1;[05] VERIFIED REPLACEMENT
FWD CABIN L/H FUS SUPPORT FRAME FLANGE CUTOUT SMALL CRACK ABOVE L-1 DOOR CUTOUT STA 312 / [01] ACCOMPLISHED EA M-22-153-01244 REV A ON TASK CARD TTG8Q00E2HR9;[02] C/W
L/H WING REMOVABLE WING TIP LOWER ELECTRICAL CONNECTOR ON WING IS CRACKED / [01] REMOVED ACCESS PANEL 521ABB AS PER B737 AMM 57-41-02-000-801.;[02] REPLACER AT L/H WING REMOVABLE WING TIP LOWER ELECTRICAL CONNECTOR (J3) AS PER B737 SWPM 20-61-00; WDM 33-44-12; AND WDMS 33-44-12.<BR><BR><BR>PENDING ANTI-COLLISION WHITE OPERATIONAL TEST.;[03] VERIFIED 2<BR>OK TO REINSTALL PANEL 521ABB;[04] REINSTALLED ACCESS PANEL 521ABB AS PER B737 AMM 57-41-02-400-801.;[05] VERIFIED 4;[06] PERFORMED L/H WING TIP ANTI-COLLISION LIGHTS (WHITE) OPERATIONAL TEST AS PER B737 AMM 33-44-00-710-801. TEST OK.;[07] VERIFIED 6
AFT OF AFT CARGO COMPARTMENT FLOOR. SUPPORT ANGLE CRACKED FWD OF POTABLE WATER TANK L/H SUPPORT S-25L AND STA 947.5 MKD DOT / [01] REMOVED AND REPLACED AFT CARGO FLOOR SUPPORT ANGLE FORWARD OF POTABLE WATER TANK AT L/H SUPPORT AT STR 25-L AND STA 947.5 AS PER B 737-7 SRM 51-40-02-0G-0;[02] VERIFIED STEP #1
CORROSION. AFT CARGO COMPARTMENT L/H FLOOR SUPPORT ZEE CHANNEL @ S-25L FROM STA 727 TO STA 847 / [01] REMOVED CORROSION AT L/H ZEE CHANNEL S-25L FROM STA 727 TO STA 847 AS PER B 737-7 SRM51-10-02-0G-0;[09] LOCATED AND DRILLED NEW L/H ZEE CHANNEL AS PER B737-700-SRM 51-40-05-0G-0;[10] VERIFIED AND INSPECTED STEP#9.;[11] 'STEP 8 CORRECTION' START FABRICATING L/H ZEE CHANNEL AS PER B 737-700 SRM51-40-05-0G-0;[12] VERIFIED STEP#11. OK TO TREAT AND PRIME L/H ZEE CHANNEL.;[13] TREATED AND PRIMED NEW L/H ZEE CHANNEL AS PER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[14] VERIFIED AND INSPECTED STEP#13.;[15] OK TO INSTALL NUTPLATES;[16] INSTALLED NEW NUT PLATES AS PER B737-7 SRM=51-40-10-2R-0;[17] SUMMARY=REMOVED CORROSION AT L/H ZEE CHANNEL S-25L FROM STA 727 TO STA 847 AS PER B 737-7 SRM51-10-02-0G-0 EVALUATED REWORKED AREA ORG. MAT. .040 MAT. REMAINING .025 MAT. REMOVED.015 FOUND TO BE OUT OF LIMITS AS PER B737-7 SRM 53-00-53-1A-2 REMOVED AFT CARGO COMP L/H FLOOR SUPPORT ZEE CHANEL S-25 STA 727 TO STA847 IAW B737 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW L/H ZEE CHANNEL AS PER B737-700-SRM 51-40-05-0G-0TREATED AND PRIMED NEW L/H ZEE CHANNEL AS PER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804 INSTALLED NEW NUT PLATES AS PER B737-7 SRM=51-40-10-2R-0;[18] ZEE-CHANNEL REMOVED IN STEP #5 TO BE FABRICATED WILL BE INSTALLED ON ITEM 2019610 1000/0007 BAR CODE TTG8Q004EU16;[19] VERIFIED STEPS 16; 17 AND 18.
CORROSION AFT CARGO COMPARTMENT R/H FLOOR SUPPORT ZEE CHANNEL S-25R FROM STA 727 TO 767 / [01] REMOVED CORROSION AT R/H ZEE CHANNEL S-25R FROM STA 727 TO STA 767 AS PER B 737-7 SRM51-10-02-0G-007] LOCATED AND DRILLED NEW AFT CARGO R/H Z-CHANNEL AS PER B 737-7 SRM =51-40-05-0G-0;[08] VERIFIED STEP 7. OK TO TREAT AND PRIME.;[09] TREATED AND PRIMED NEW Z-CHANNEL AS PER B 737-7 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[10] VERIFIED AMT STEP 9. OK TO INSTALL NUT PLATES.;[11] CORRECTED MEASUREMENT TABLE;[12] INSTALLED NUT PLATES ON NEW R/H ZEE CHANNEL AS PER B737-700 SRM 51-40-10-2R-0;[13] REMOVED CORROSION AT R/H ZEE CHANNEL S-25R FROM STA 727 TO STA 767 AS PER B 737-7 SRM51-10-02-0G-0. EVALUATED REWORKED AREA ORG. MAT. .040 MAT REMAINING .015 MAT REMOVED .025 FOUND TO BE OUT OF LIMITS AS PER B 737-7 SRM 53-00-53-1A-2. REMOVED AT AFT CARGO COMP R/H SUPPORT ZEE CHANNEL S-25 STA 727 TO STA767IAW B737 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW AFT CARGO R/H Z-CHANNEL AS PER B 737-7 SRM =51-40-05-0G-0. TREATED AND PRIMED NEW Z-CHANNEL AS PER B 737-7 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804. INSTALLED NUT PLATES ON NEW R/H ZEE CHANNEL AS PER B737-700 SRM 51-40-10-2R-0.;[14] VERIFIED AND INSPECTED STEP #11; #12; AND #13. FINAL.
CORROSION SPOTS AROUND FASTENERS HEADS AT FWD CARGO COMPARTMENT AFT BULKHEAD LOWER BILGE FLOOR SUPPORT ANGLE STA 500D FROM S-25L TO S-25R MKD DOT / [01] BLENDED OUT AREA IN ACCORDANCE B-737-700 SRM 51-10-02-0G-0.;[02] AFTER REMOVING CORROSION THE DEEPEST POINT WAS FOUND IN LBL 3 WITH A REMAINING THICKNESS OF 0.050 IN; ORIGINAL THICKNESS WAS 0.071 IN; MATERIAL LOST 0.021. FOUND OUT OF LIMITS IN ACCORDANCE TO B-737-700 SRM 53-00-53-1A-2.;[03] VERIFIED BLEND & EVALUATION;[04] LOCATED AND DRILLED NEW PART AS PER B-737-700 SRM 51-40-05-0G-0; DRAWING #: 143A9481.;[05] NEW PART INSTALLATION WOULD BE ACCOMPLISHED IN WORK CARD: TTG8Q004DCHM.;[06] VERIFIED STEPS 4; 5
L/H GUSSET CRACKED AT S-19L STA 500D WL198 MKD DOT / [01] REMOVED CRACKED L/H GUSSET AT STA 500D AS PER B-737-700 SRM 51-40-02-0G-0.;[02] NEW GUSSET LOCATED AND DRILLED IN REF B-737-700 SRM 51-40-05-0G-0.;[03] OK TO INSTALL GUSSET;[04] NEW GUSSET INSTALLED IN REF B-737-700 SRM 51-40-02-0G-0.;[05] VERIFIED 4
AFT CARGO SCUFF PLATE FWD CORNER CRACKED / [01] RECEIVED NEW AFT CARGO FORWARD SCUFF PLATE PART #146A8341-7 SCUFF PLATE TO BE INSTALLED ON ITEM# 2019606 1000/0023 BARCODE #TTG8Q003LV8P STEP #17;[02] VERIFIED AMT STEP 1.
MAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED @. STA 540 LBL 1 MKD DOT / [01] OPENED FLOOR CABIN 231UF FOR ACCESS IN REF B-737-700 SRM 53-21-00-000-801.;[02] REMOVED MAIN CABIN CENTER WING FLOOR SUPPORT AT STA 540 LBL 1 AS PER B-737-700 SRM 51-40-02-0G-0.;[03] NEW PART LOCATED AND DRILLED AS PER B-737-700 SRM 51-40-05-0G-0.;[04] OK TO INSTALL;[05] VERIFIED STEPS 1; 2 & 3;[06] NEW PART INSTALLED AS PER B-737-700 SRM 51-40-02-0G-0.;[07] ADDING DRAWING #143A5240.;[08] VERIFIED 6; 7<BR>OK TO REINSTALL FLOOR PANEL;[09] CLOSED FLOOR CABIN PANEL 231UF IN REF B-737-700 SRM 53-21-00-400-801.;[10] ACCOMPLISHED REMOVAL PARTS TRANSACTION IN MXI;[11] VERIFIED 9; 10
R/H HORIZONTAL STABILIZER FRONT SPAR REMOVEABLE FAIRING CRACKED @ RIB 5 INTERNAL MKD DOT / [01] REMOVED #5 RIB AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW RIB #5 AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-05-0G-0.;[03] OK TO INSTALL RIB #5;[04] INSTALLED #5 RIB AT R/H HORIZONTAL STAB L/E ASPER REF SRM 51-40-02-0G-0.;[05] SUMMARY :REMOVED #5 RIB AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0<BR>LOCATED AND DRILLED NEW RIB #5 AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-05-0G-0.INSTALLED #5 RIB AT R/H HORIZONTAL STAB L/E ASPER REF SRM 51-40-02-0G-0.;[06] VERIFIED STEP #4 AND #5;[07] VERIFIED STEPS #4; #5 AND #6
MAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED @. STA 540 RBL 1 MKD DOT / [01] REMOVED MAIN CABIN CENTER WING FLOOR SUPPORT AT STA 540 RBL 1 AS PER B-737-700 SRM 51-40-02-0G-0.;[02] NEW PART LOCATED AND DRILLED AS PER B-737-700 SRM 51-40-05-0G-0.;[03] OK TO INSTALL<BR>VERIFIED STEPS 1 & 2;[04] NEW PART INSTALLED AS PER B-737-700 SRM 51-40-02-0G-0.;[05] ADDING DRWG # 143A5240.;[06] VERIFIED 4; 5<BR>C/W;[07] COMPLETED.;[08] ACCOMPLISHED REMOVAL PARTS TRANSACTION IN MXI.;[09] COMPLETED
R/H HORIZONTAL STABILIZER FRONT SPAR REMOVEABLE FAIRING CRACKED @ RIB 3 INTERNAL MKD DOT / [01] REMOVED #3 RIB AT R/H HORIZONTAL STAB FROM L/E AS PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW# 3 RIB R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-05-0G-0.;[03] VERIFIED STEP #2;[04] OK TO INSTALL RIB #3;[05] INSTALLED NEW RIB#3 AT R/H HORIZONTAL STABILIZER L/E AS PER B 737-7 SRM 51-40-02-0G-0;[06] VERIFIED STEP #5
FWD CARGO FWD CORNER SCUFF PLATE CRACKED / [01] LOCATED AND DRILLED NEW FWD CARGO FWD CORNER SCUFF PLATE IN REFERENCE. B-737 SRM51-40-05-0G-0;[02] VERIFIED LOCATED AND DRILLED.<BR>OK TO INSTALL;[03] INSTALLATION WILL BE COMPLETED ON CARD TTG8Q003LV9R;[04] LOCATED AND DRILLED NEW FWD CARGO FWD CORNER SCUFF PLATE IN REFERENCE. B-737 SRM51-40-05-0G-0
R/H HORIZONTAL STABILIZER FRONT SPAR REMOVEABLE FAIRING CRACKED @ RIB 4 INTERNAL MKD DOT / [01] REMOVED #4 RIB AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-020-0G-0.;[02] LOCATED AND DRILLED NEW RIB # 4 AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-5-0G-0.;[03] OK TO INSTALL #4 RIB ON R/H STAB L/E;[04] INSTALLED NEW RIB#4 AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G;[05] SUMMARY : REMOVED #4 RIB AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-020-0G-0.LOCATED AND DRILLED NEW RIB # 4 AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-5-0G-0.INSTALLED NEW RIB#4 AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G.;[06] VERIFIED STEP 4 AND 5;[07] RII VERIFIED STEP 4 AND 5;[08] VERIFIED
CENTER WING LEFT SIDE VAPOR WEB FIBERGLASS PANEL HAS SMALL CRACK INBOARD OF HYDRAULIC MODULE / [01] MEASUREMENTS[13] SUMMARY=PERFORMED VISUAL INSPECTION AND PERFORMED TAP TEST; FOUND SMALL 5' CRACK AT LBL 45' AND CONTAMINATION ON SURFACE OF VAPOR BARRIER ; NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION 3 AND 5 CLEANED AND PREPARED DAMAGE AREAS FOR DRY OUT; STOP DRILL CRACKS AS PER B737 SRM 51-70-04-2R-10 PERFORMED DRY OUT ON L/H VAPOR BARRIER; FOUND NO WATER AS PER B737 SRM 51-70-04-2R-10 REPAIRED SMALL CRACK DAMAGE ON L/H VAPOR BARRIER WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-10; MATERIALS USED PO#1690463 AND PO#1778994 PERFORMED TAP TEST ON REPAIRED AREA OF VAPOR BARRIER; FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION 5 LOCATED AND DRILLED HOLES THAT WERE COVERED BY REPAIR AT VAPOR WEB AS PER B 737-7 SRM51-40-05-0G-0 APPLIED TOPCOAT ON LEFT SIDE VAPOR WEB FIBERGALSS PANEL REF B 737 AMM 51-21-81-370-801;[14] VERIFIED AMT STEP 13.;[15] VERIFIED AMT STEP 13.;[16] VERIFIED AMT STEP 13. RII
CRACK FOUND AT L/H HORIZONTAL STAB LOWER SKIN STAB STA 193.90; 17' FROM FWD. SPAR; I/B ROW. CRACK LENGTH: 1.25' CRACK FOUND AT L/H HORIONTAL STAB LOWER SKIN STAB STA 193.90 17" FROM FWD. SPAR I/B ROW. CRACK LENGTH: 1.25" / [01] REMOVED PAINT FOR ACCESS FASTENER FOR REPAIR AT L/H STA 193.90 IAW B737 AMM51-21-11-150-801.[25] REMOVED PAINT FOR ACCESS FASTENER FOR REPAIR AT L/H STA 193.90 IAW B737 AMM51-21-11-150-801.<BR>REMOVED FASTENERS LOWER SKIN STA 193.90 FOR ACCESS REPAIR IAW B737 SRM 51-40-02-0G-0.<BR>REMOVED DAMAGED ON AREA LOWER OF SKIN [CRACK ] AT L/H HORIZONTAL STAB STA 193.90 17' FROM FWD SPAR I/B ROW IAW B737 SRM 55-10-01-2R-11 REPAIR 11.PERFORMED HFEC INSP ON CUTOUT AREA IAW B737 NDT P6 51-00-00 PROC.23; NO CRACKS<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23.PERFORMED ROTO INSP ON ALL EXISTING HOLES IAW B737 NDT P6 51-00-00 PROC.16; NO CRACKS<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23.<BR>PERFORMED COUNTERSINK INSP ON ALL EXISTING COUNTERSUNK HOLES IAW B737 NDT P6 53-30-00 PROC.3; NO CRACKS<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23.<BR>FABRICATED FILLER AT L/H HORIZONTAL STAB LOWER SKIN STA 193.90 MATERIAL USED 2024 T3 .071 ALUMINUM CLAP PO # 1749426 IAW B737 SRM 5510-01-2R-11 REPAIR 11.<BR>FABRICATED DOUBLER AT L/H HORIZONTAL STAB LOWER SKIN STA 193.90 .MATERIAL USED 2024 T3 -0.090 ALUMINUM CLAP .PO#1727238 IAW B737 SRM 55-10-01-2R-11 REPAIR 11
VERTICAL ANGLE (CLIP) @STA 727 PNL 193 HAS CRACK APPROX .75? LONG ; ANGLE CLIP IS ON LH SIDE OF WHEELWELL WING-TO-BODY FAIRING. / [01] FABRICATED AND INSTALLED NEW VERTICAL ANGLE PER<BR> SRM 51-40-02
CLIP @STA 727 PANEL 193 HAS CRACK APPROX .75? LONG. ; / [01] CLIP WAS REMOVED AND REPLACED WITH ONE FABRICATED PER EA INSTRUCTIONS
OVERHEAD EMERGENCY DOOR EXIT SIGN BASE IS BROKEN ; / R&R OVERHEAD HOUSING & LENES PER AMM 33-51-01
OVERHEAD EMERGENCY DOOR EXIT SIGN BASE IS BROKEN ; / R&R OVERHEAD HOUSING & LENES PER AMM 33-51-01
CENTER ISLE EXIT SIGN COVER FELL OFF. INSTALLED EMERGENCY EXIT FWD LENS PER SIP.
LT STA 475, 1.25 ABOVE S25L. DAMAGE OR BLEND OUT IS L .90 X W .70 AND .013 MATERIAL WAS REMOVED. DUE TO LIGHTNING STRIKE DAMAGE. MOD/REPAIRED PER SRM 53-00-01-2R-4 PERMANENT ACTION REQUIRED. PERMANENT REPAIR WITH SOLID FASTENERS MUST BE INSTALLED NO LATER THAN 20;000 CYCLES, IAW SRM 53-00-01-2R-4 REPAIR 4.
CARGO FLOOR STRAP DAMAGED IN AFT CARGO PIT FWD SIDE OF DOOR OPENLY / R&R FWD LOWER CARGO PLATE ON FLOOR ON 453A2611-1 RDW SRM 51-40-02 & 53-00-05
SEAT TRACK HAS MECHANICAL DAMAGE/WORN AT BS 520 LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK BS 480-520 LBL 45 WL 208, PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 BOEING DWG 143A5300; AND BOEING DWG 143A5034.
FORWARD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED 'MARKED' / REPAIRED SCUFF PLATE PER: SRM 53-30-15-2R-1
FORWARD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED 'MARKED' / REPAIRED SCUFF PLATE PER: SRM 53-30-15-2R-1
LEFT WING TRAILING EDGE PANEL (551GB) I/B EDGE SUPPORT BRACKET FWD BEARING DAMAGED / REMOVED AND REPLACED LEFT WING TRAILING EDGE PANEL (551GB) DAMAGED I/B EDGE SUPPORT BRACKET IAW SRM 51-40-02-0G-0 STEP 4 AND IPC 57-50-00-30A
LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 129.50 3RD VERTICAL STIFFENER IS CRACKED. REPAIRED LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 129.50 3RD VERTICAL STIFFENER, IAW SRM 55-10-09-2R-4; DWG'S: 182A3001; 182A1500; 002A0001 182A2401; SRM 51-40-02-0G-0. 59796C 4SEP'20.
LEFT AND RIGHT OVERWING EXIT LOCATORS HAVE BURNT OUT BULBS. REPLACED BURNT OUT LAMPS FOR LEFT AND RIGHT OVERWING EXIT LOCATORS AND PERFORMED GOOD OPERATIONAL TEST, PER AMM 33-51-01-960-801.
ON OPENING FWD ENTRY FOOR GIRT BAR BECAME DETACHED FROM SLIDE CASE. REINSTALLED FORWARD ENTRY DOOR SLIDE PER MT 725-61-06
RAMP REPORTS AFT CARGO PER FLOOR CRACKED AT STATION 768 MEASURES L= 10 3/4' 1 7/8' FROM EDGE OF PANEL / R&R'D FLOOR PANEL PER AMM 25-52-10.
'GROUND CREW FOUND A CRACK IN THE FIBERGLASS FLOOR ATTEND FORWARD CARGO BIN' / R&R FWD CARGO AFT FLOOR PANEL PER MM 25-52-10
LH WING T/E BULB SEAL RETAINER BRACKET CRACKED BETWEEN #5 AND #6 SPOILERS (MARKED) / R&R LH WING T/E BULB SEAL RETAINER BRACKET BETWEEN #5 AND #6 SPOILERS IAW SRM 51-40-02.
L2 DOOR SLIDE WAS PULLED OUT TOO FAR, HARD TO ARM DOOR. / REPOSITIONED SLIDE PER AMM.
GROUND POWER RECEPTACLE CUT-OUT CRACKED COMING FROM A FASTENER AT THE BOTTOM OF CUT-OUT FORWARD FASTENER. REPAIR GROUND POWER RECEPTACLE CUT OUT PER SRM.
DURING DESCENT REPORTED ELECTRIC BURNING SMELL IN AFT GALLEY. FOUND RECIRC FAN INOP. R&R RECIRC FAN PER MM.
OVERWING EXIT LIGHT COVER FELL OFF. SECURED COVER PER AMM.
***CORROSION*** AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT BS727D+10 REPAIR SPLICE / REMOVED AND REPLACED ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT SPLICE LOCATE AT BS 727D+10; LBL 21 IAW. SRM 51-40-02 53-00-53-2R-6 REPAIR 6
AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 727D+10 TO BS 727, LBL 21. R&R SUPPORT IAW SRM & DWG.
GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET IAW SRM & DWG.
AFT CARGO BAY ANGLE CORRODED BETWEEN BS 767 TO BS 787, STR 26R. R&R ANGLE IAW DWG AND SRM.
AFT CARGO BAY STRAP CORRODED BETWEEN BS 787 TO BS 794, RBL 19.5. R&R STRAP IAW ER AND EA.
R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727D+8 TO BS 767. R&R SUPPORT IAW SRM & DWG.
AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 777 TO BS 787. R&R SUPPORT IAW SRM & DWG.
AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 912. R&R SUPPORT IAW SRM AND DWG.
AFT CARGO FLOOR TRACK CORRODED BETWEEN BS 794 TO BS 810, RBL 14. R&R FLOOR TRACK PER DWG.
AFT CARGO BAY INTERIOR, CARGO FLOOR TRACK CORRODED AT BS 771, LBL 2. R&R ANGLE IAW SRM AND EA.
AFT CARGO BAY INTERIOR, AFT BULKHEAD LOWER CHORD CORRODED AT BS 947, RBL 17. R&R CHORD IAW DWG AND SRM.
AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 789 TO BS 797, LBL 21. R&R SUPPORT IAW SRM & DWG.
FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED. R&R SUPPORT IAW SRM & DWG.
FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 494 TO BS 500A. R&R SUPPORT IAW SRM & DWG.
AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 827 TO BS 847, BETWEEN STR 25L TO STR 26L. R&R INTERCOSTAL IAW SRM AND DWG.
***CORROSION*** NOTED ON ACB INTERCOSTAL (BS 747 - BS 767 / BETWEEN S-25R AND S-26R). / MULTIPLE CORROSION AREAS UNDER THE NUTPLATES ON THE INTERCOSTAL (BAFFLE) FROM BS 747 - BS 767 RBL 21 BETWEEN STR 25R - 26R FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM NEED TO BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 PAR 9.C. REMOVED AND REPLACED INTERCOSTAL (BAFFLE) FROM BS 747 - BS 767 RBL 21 BETWEEN STR 25R - 26R; P/N # 146A7505-8; PO# 698532 IAW DWG# 146A7502.
AFT CARGO DOOR CUTOUT LOWER MAIN SILL THRESHOLD WEB CORRODED BETWEEN BS 794.5 TO BS 847, RBL 25. R&R WEB IAW SRM AND DWG.
AFT CARGO BAY STRAP ASSEMBLY CORRODED BETWEEN BS 794.5 TO BS 800, RBL 19.5. R&R STRAP ASSEMBLY IAW ER AND EA.
CREASE BEAM WEB CORRODED AT BS 907+5, STR 17L. R&R WEB IAW SRM & DWG.
FORWARD CARGO BAY, RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D. R&R SUPPORT IAW SRM & DWG.
FORWARD CARGO BAY AFT BULKHEAD LOWER RT CHORD CORRODED AT BS 500D. R&R CHORD IAW SRM & DWG.
FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D. R&R SUPPORT IAW SRM AND DWG.
RT HORIZONTAL STABILIZER STA 120.30 INSPAR RIB CRACKED AT 3RD VERTICAL STIFFENER. REPAIRED RIB PER SRM.
INTERCOSTAL CRACKED BETWEEN BS 294.5 TO BS 312, RBL 15. R&R INTERCOSTAL IAW SRM & DWG.
INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R&R INTERCOSTAL IAW SRM & DWG.
INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 47. R&R INTERCOSTAL IAW SRM & DWG.
L1 DOOR GIRT BAR ATTACH POINT FITTING CORRODED AT BS 312, WL 208.1. R&R FITTING IAW DWG AND SOPM.
L1 DOOR GIRT BAR ATTACH POINT FITTING CORRODED AT BS 344, WL 208.1. R&R FITTING IAW DWG AND SOPM.
SUPPLEMENTAL INFORMATION: FAIRING FORMER UNDER L/H ACCESS PANEL 191AL; BS 500D; WL 191 CRACKED AT FASTENER HOLE (MARKED) / REMOVED & REPLACED NEW FAIRING FORMER P/N 116A3118U9 IAW DRW 116A3010 & SRM 51-40-02-0G-0 88924U 10OCT18
INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL IAW SRM & DWG.
INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL IAW SRM & DWG.
SUPPLEMENTAL INFORMATION: PANEL 194BR HAS AN ELONGATED HOLE / PANEL 194BR ELONGATED HOLE REPAIRED IAW SRM 51-70-05-2R-8 PER SRM 53-60-70-2R-1 59298U 10/04/18
R2 DOOR MOP SILL CORRODED BETWEEN BS 897 TO BS 1006. R&R MOPSILL IAW DWG AND SRM.
R1 DOOR MOP SILL CORRODED BETWEEN BS 320 TO BS 330. R&R MOPSILL IAW DWG.
SUPPLEMENTAL INFORMATION: ***CORROSION*** UNDER R/H WING PANEL 621EB BONDING JUMPER / FOUND CORROSION LIMITED TO SEAL RETAINER ONLY AT BONDING JUMPER. REMOVED AND REPLACED SEAL RETAINER ON R/H WING PANEL 621EB IAW SOPM 20-50-01 STEPS 1-9; AND SWPM 20-20-10 TABLE 31; 41. STEP 4.D.;4.G. RESISTANCE CHECK GOOD.
INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, BL 0. R&R INTERCOSTAL IAW DWG & SRM.
FORWARD CABIN FLOOR SUPPORT BROKEN AT BS 540, RBL 2. R&R SUPPORT IAW SRM & DWG.
FORWARD CABIN INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520, BL 0. R&R INTERCOSTAL IAW DWG & SRM.
SUPPLEMENTAL INFORMATION: DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 BEAM TO BE CRACKED COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY AT THE RADIUS ON THE INBD SIDE. / SF DOOR #4 BEAM WAS REMOVED & REPLACED ON WORK ORDER: 509948. REMOVAL & INSTALLATION OF SF DOOR WAS ACCOMPLISHED ON CUSTOMER CARD: 14079. LINER REMOVED & INSTALLED PER AMM 52-41-31-000-802 & 52-41-31-400-802. ADJUSTMENT ACCOMPLISHED PER AMM 52-41-00-820-801. SF DOOR SYSTEM TEST WAS PERFORMED PER AMM 52-41-00-700-801. SYSTEM TEST GOOD! (POS: FSD; TAG NO.: 469508; P/N OFF: 141A6516-18; S/N OFF: 002138; P/N ON: 141A6516-18M; S/N ON: 002138)
SUPPLEMENTAL INFORMATION: AFT CABIN FLOOR PANEL 242WF O/B EDGE IS BROKEN / AFT CABIN FLOOR PANEL 242WF WITH O/B EDGE THAT IS BROKEN WAS REPLACED WITH A SERVICABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE 57852U 09/27/18
SUPPLEMENTAL INFORMATION: PREVIOUS REPAIR WITH PROPAGATING DAMAGE AT BS663 VAPOR BARRIER LBL45 (MARKED) / REPAIRED DAMAGE AT BS 663 VAPOR BARRIER LBL 45 IAW SRM 51-70-04-2R-10. 56749U 10/05/2018
SUPPLEMENTAL INFORMATION: PREVIOUS REPAIR WITH PROPAGATING DAMAGE AT BS663 VAPOR BARRIER RBL35 (MARKED) / PREVIOUS REPAIR WITH PROPAGATING DAMAGE AT BS 663 VAPOR BARRIER RBL 35 AND 2 OTHER LOCATIONS WERE REPAIRED IAW SRM 51-70-04-2R-10.
FLOOR SUPPORT BROKEN AT BS 540, BETWEEN BL 0 TO LBL 25. R&R SUPPORT IAW SRM & DWG.
RT FWD EMERGENCY LIGHT BATTERY FAILED TEST. R&R BATTERY PACK PER MM.
LT FWD CABIN EMERGENCY LIGHT BATTERY FAILED TEST. R&R BATTERY PACK PER MM.
RT MID CABIN EMERGENCY LIGHT BATTERY FAILED TEST. R&R BATTERY PACK PER MM.
LT HATCH EXTERIOR OVERWING EMERGENCY LIGHT INOP. R&R BATTERY PACK IAW AMM.
LT HATCH LOWER EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK IAW AMM.
LT EMERGENCY BULLNOSE LIGHTS INOP AT ROW 6. R&R BATTERY PACK IAW AMM.
#6 FLAP TRACK FAIRING HAS 2 FASTENERS PULLED THROUGH ON OUTBOARD SEAL ATTACHMENT / PERFORMED INTERIM REPAIR PER SRM 57-53-70-2R-2 DVI OF REPAIR REQUIRES EVERY 500 CYCLES
LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.
WING TO BODY FAIRING PANEL-193B-LOWER FORWARD EDGE LH CORNER HAS 2 1/8' X 2' DELAMINATION WITH LAYERS MISSING. / CLOSING DMA 0204568 R&R'D PANEL 143B PER AMM 53-51-21 CLEARING # 20164
L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY PARTIALLY FELL OUT OF CONTAINER, SLIDE DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.
EMERGENCY EXIT ROW HOOK AND LOOP LOOSE. R & R HOOK AND LOOP IAW SIP.
LEFT EMERGENCY EXIT HATCH ESCAPE STRAP CORRODED AT ATTACH POINTS. R & R THE STRAP IAW MM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R & R BATTERY PACK IAW MM AND DWG.
L2 DOOR ESCAPE SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
L2 DOOR EMER SLIDE LOOSE. SECURED SLIDE IAW AMM.
LEFT AFT ENTRY OUTSIDE EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.
EMERGENCY EXIT LIGHTS ACTIVATED IN CABIN CB P-18-3-A-11 POPPED. FOUND WIRE SHORTED. REPAIRED WIRE IAW SWOM.
PASSENGER CABIN LIGHTING EMER CHARGER FWD CB POPPED. RESET CHARGER IAW AMM.
M1670 EMER LIGHTING BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW MM.
M1675 EMER LIGHTING BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW MM.
M1673 EMER LIGHTING BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW MM.
M1672 EMER LIGHTING BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW MM.
R1 DOOR EMER EVAC SLIDE CABLE LOOSE. SECURED CABLE IAW AMM.
OVERHEAD EMER EXIT AISLE LIGHT ASSEMBLY BROKEN. REPAIRED LIGHT ASSEMBLY IAW EA.
SKIN CREASED BETWEEN BS 424 TO 436 STRINGER 15L. REPAIRED SKIN IAW EA.
SKIN CREASED BETWEEN BS 448 TO 453 STRINGER 15L. REPAIRED SKIN IAW EA.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT STATION 157.10 FWD OTBD HOLE. REPAIRED RIB IAW EA.
SKIN CREASED BETWEEN BS 448 TO 453 STRINGER 15L. REPAIRED SKIN IAW EA.
STRINGER CLIP CRACKED AT BS STRINGER 16L. R & R CLIP IAW SRM.
RIGHT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED ON RIB AT STATION 92.70, 38.25 INCHES AFT OF FWD SPAR. REPAIRED STIFFENER IAW SRM.
FLOOR SUPPORT CORRODED BETWEEN BS 747 TO 846 RBL 14. R & R SUPPORT IAW SRM.
RIGHT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED ON RIB AT STATION 92.70, 29.00 INCHES AFT OF FWD SPAR. REPAIRED STIFFENER IAW SRM.
RIGHT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED ON RIB AT STATION 92.70, 10.50 INCHES AFT OF FWD SPAR. REPAIRED STIFFENER IAW SRM.
FLOOR SUPPORT CORRODED BETWEEN BS 772 LBL 3. R & R SUPPORT IAW SRM.
AFT FLOOR SUPPORT CORRODED AT BS 799 RBL 14. R & R SUPPORT IAW SRM.
AFT THRESHOLD WEB CORRODED BETWEEN BS 793 TO 847. R & R WEB IAW SRM.
RIGHT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED ON RIB AT STATION 92.70, 19.75 INCHES AFT OF FWD SPAR. REPAIRED STIFFENER IAW SRM.
LEFT HORIZONTAL STABILIZER RIB CRACKED STATION 129.50 AT BOTH FWD ATTACH HOLES. REPAIRED RIB IAW EA.
R1 DOOR L ANGLE CORRODED AT BS 312 RBL 65.5. REPAIRED L ANGLE IAW SRM.
FORWARD CARGO COMPARTMENT CORRODED AROUND FASTENER HOLE ON RT SUPPORT FITTING AT BS 500+15 RBL 21.80. R & R FITTING IAW SRM.
FLOORBEAM INTERCOSTAL CRACKED BETWEEN BS 312 TO 320, RBL 31. R & R INTERCOSTAL IAW SRM.
AFT BACK BEAM FLOOR SUPPORT CORRODED AT BS 772, LBL 3. REPAIRED SUPPORT IAW EA.
FLOORBEAM INTERCOSTAL CRACKED BETWEEN BS 328 TO 344, LBL 46. R & R INTERCOSTAL IAW SRM.
FORWARD SEAT TRACK UPPER CHORD CRACKED AT BS 727B RBL 45 INBD FWD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.
FORWARD SEAT TRACK UPPER CHORD CRACKED AT BS 727B RBL 45 OTBD FWD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.
FORWARD SEAT TRACK UPPER CHORD CRACKED AT BS 727B LBL 24 INBD AFT FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.
FORWARD SEAT TRACK UPPER CHORD CRACKED AT BS 727B LBL 45 INBD AFT FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.
FORWARD SEAT TRACK UPPER CHORD CRACKED AT BS 727B LBL 45 OTBD AFT FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.
FORWARD SEAT TRACK UPPER CHORD CRACKED AT BS 727B LBL 24 OTBD AFT FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.
AFT SEAT TRACK UPPER CHORD CRACKED AT BS 727B LBL 24 FASTENER HOLE C. REPAIRED CHORD IAW SRM.
AFT SEAT TRACK UPPER CHORD CRACKED AT BS 727B LBL 45 FASTENER HOLE E. REPAIRED CHORD IAW SRM.
MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663 BETWEEN LBL 40 TO 42. REPAIRED WEB IAW SRM.
MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663 RBL 32. REPAIRED WEB IAW SRM.
MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663 LBL 41. REPAIRED WEB IAW SRM.
RIGHT NR 3 CONTROL CABIN WINDOW FRAME E - F POST NR 8 CRACKED. REPAIRED POST IAW ACO.
LEFT NR 3 CONTROL CABIN WINDOW FRAME E - F POST NR 8 CRACKED. REPAIRED POST IAW ACO.
LEFT WING NR 1 SLAT LOWER SURFACE SKIN CRACKED AT SLAT STATION 451.97. R & R NR 1 SLAT ASSEMBLY IAW AMM.
LEFT FWD EEPLS CRACKED. R & R EEPLS IAW AMM.
L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.
RIGHT WING INBD T/E FLAP OTBD END SHELF VERTICAL BULB SEAL RETAINER CRACKED. R & R RETAINER IAW SRM.
L2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.
FORWARD ENTRY SLIDE FELL OUT OF CONTAINER. RE-INSTALLED SLIDE IAW SWMT 325-61-06.
AFT LEFT GALLEY SERVICE DOOR AREA EXTERNAL EMERGENCY EVAC SLIDE LIGHT LENS DIRTY. CLEANED LENS IAW MM.
PASSENGER CABIN FLOOR PANEL BREAK AT BS 540 LBL '0' - LBL 24.75 IS CRACKED. REMOVED AND REPLACED PANEL IAW AMM.
PASSENGER CABIN FLOOR PANEL BREAK AT BS 540 RBL '0' - RBL 24.75 IS CRACKED. REMOVED AND REPLACED PANEL IAW AMM.
AFT CARGO COMPARTMENT LEFT Z-ANGLE CORRODED BETWEEN STA 727D TO STA 840. REMOVED AND REPLACED Z-ANGLE IAW SRM.
RIGHT WING, LEADING EDGE PANEL 621CB, FWD INBD CORNER, FASTENER HOLE CRACKED. REPAIRED FASTENER HOLE IAW SRM.
AFT CARGO COMPARTMENT RIGHT Z-ANGLE CORRODED. REPAIRED Z-ANGLE IAW SRM AND DWG.
RIGHT HORIZONTAL STABILIZER CRACKED AT STA 101.90. REPAIRED STABILIZER IAW SRM.
RIGHT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER AMM.
LEFT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER AMM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT AND MM.
L1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER AMM.
R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
EMERGENCY FLOOR TRACK LIGHT INOP AT ROW 10. RELAMPED LIGHT PER M/M.
DIVERSION -- CROSSFEED VALVE CIRCUIT BREAKER POPPED AND WOULD NOT RESET. REMOVED AND REPLACED FUEL CROSSFEED VALVE ACTUATOR PER MM.
FWD EMERGENCY EXIT SLIDE CAME OUT WHEN DOOR OPENED. RE-INSTALLED SLIDE PER MX TASK.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER MM.
FWD ENTRY EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP AT ROW 11. REMOVED AND REPLACED EEPLS PER MM.
L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT PER MM.
LT EEPLS COVER CRACKED AT ROW 2. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.
DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKETS LOOSE. SECURED BRACKETS PER MM.
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS CRACKED AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LENS CRACKED AT ROW 7. REMOVED AND REPLACED LENS PER MM.
EEPLS LIGHT COVER MISSING. INSTALLED COVER PER MM.
L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.
DECLARED EMERGENCY. NR 2 ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. DURING DESCENT, B-SYSTEM HYDRAULIC FLUID QUANTITY DECREASED FLUID QUANTITY DECREASED TO ZERO WITH SUBSEQUENT LOSS OF B-SYSTEM PRESSURE. REMOVED AND REPLACED HYDRAULIC PUMP PER MM.
DECLARED EMERGENCY, NR 2 ENG DRIVEN HYDRAULIC PRESSURE LOW PRESSURE LIGHT EN ROUTE SUBSEQUENT SLOW LOSS OF QUANTITY. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP PER MM.
R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS END CAP BROKEN AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM.
FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
EEPLS INOP ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.
DURING SCHEDULED MV1 CHECK, FOUND AFT RIGHT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
FWD CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.
EEPLS COVER LOOSE AT ROW 3 DEF. SECURED COVER PER MM.
LEFT FWD CABIN EMERGENCY BATTERY INOP. REMOVED AND REPLACED BATTERY PACK PER MM.