N968WN
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 | 2014-06-17 – 2014-06-17 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2014-06-17 – 2014-06-17 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
L1 DOOR ESCAPE SLIDE GIRT, REPACK REQUIRED. REPACKED L1 DOOR ESCAPE SLIDE GIRT IAW AMM 25-66-01.
R1 DOOR ESCAPE SLIDE GIRT UNPACKED. REPACKED R1 DOOR ESCAPE SLIDE GIRT IAW AMM 25-66-01.
ASSIST HANDLE AFT OF L1 DOOR IS LOOSE. TIGHTEN ASSIST HANDLE AFT OF L1 DOOR PER AMM 25-21-31-420-802.
EMERGENCY EXIT SIGN ON FWD LAV HAS ONE LAMP INOPERATIVE. REMOVED; REPLACED AND PERFORMED GOOD OPS CHECK OF THE EMERGENCY EXIT SIGN ON FWD LAV IAW AMM 33-51-01-960-801<BR><BR>COMPLETED TASK CARD.
DURING OK TO CLOSE FOUND CRACK ON RH WING TO BODY FAIRING SUPPORT AROUND THE FASTENER. REMOVED DAMAGED RIB/FAIRING SUPPORT AND INSTALLED NEW RIB/FAIRING SUPPORT PER DWGS 149A7101; 116A31100; 116A3010 AND SRM 51-40-02-0G-0.
RIGHT WING T/E WIGGLE PLATE JUST I/B OF THE #8 FLAP TRACK CRACKED. UPON FURTHER INVESTIGATION; SUSPECTED CRACK ON RIGHT WING T/E WIGGLE PLATE OF # 8 FLAP TRACK WAS LIMITED TO SURFACE FINISH (PRIMER) ONLY. REPRIMED AREA IAW AMM 51-21-99-300-801.
LEFT WING T/E WIGGLE PLATE COMMON TO PANEL 551EB ON THE I/B SIDE IS CRACKED. REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE COMMON TO PANEL 551EB ON THE I/B SIDE IAW SRM 51-40-02 AIPC 57-50-00-22A.
2 EA CRACKS FOUND ON FSD STUB FRAME ABOVE SEAL DEPRESSOR WL 206 + 57.5 L 1' W .01'; WL 206 + 58.5 L .06' W .01'. REMOVED AND REPLACED FSD STUB FRAME IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8370 REV D.
MID CABIN OVERHEAD EXIT LIGHT COVER MISSING<[01] R&R CABIN OVHD EMERGENCY EXIT SIGN ASSY PER AMM 33-51-01.
A/C HAS FIBER VAPOR BARRIER CRACK BETWEEN RBL 31.83 & RBL 40 APPRX 11.5 IN LENGTH AND 11 FROM BOTTOM OF VAPOR BARRIER. ZONE 1 <[01]. PERFORMED STOP DRILL OF CRACKED AREA AND APPLIED SPEED TAPE. REF SRM. 57-10-10-1A-2 STEP 2(C)(4). DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY.
CREW REPORTS : BLUE FLOOR ILLUMINATION PROXIMITY PHOTOLUMINESCENT STRIP MOST AFT. LEFT SIDE IS MISSING<[01] REPLACED STRIP. ALL GOOD. REF AMM 33-51-15.
AFT SERVICE DOOR HANDLE AIRCRAFT RIGHT LOOSE<[01] INSTALLED NEW DOOR ASSIST HANDLE LOWER BASE ON DOOR PER M/M 52-13-31.OPS NORMAL.
L/H HORIZONTAL STABILIZER FWD UPPER SLIDER SEAL CRACKED<[01] REMOVED AND REPLACED L/H HORIZONTAL FWD UPPER SLIDER SEAL IAW AMM 53-31-31.
FWD GALLEY MEGAPHONE MISSING ATTACHMENT BOLT<[01] REMOVED AND REPLACED FWD GALLEY MEGAPHONE PER AMM 25-64-00
R2/L2 ENTRY DOORS ASSIST HANDLES LOOSE 2023-661655<[01] TIGHTENED R2/L2 ENTRY DOORS ASSIST HANDLES I.A.W. SOPM 20-50-01 REV 38;[02] TASK CARD COMPLETED
R2/L2 ENTRY DOORS ASSIST HANDLES LOOSE 2023-661655<[01] TIGHTENED R2/L2 ENTRY DOORS ASSIST HANDLES I.A.W. SOPM 20-50-01 REV 38;[02] TASK CARD COMPLETED
ELONGATED HOLE FITTING ACCESS PANEL 551GB TRAILING EDGE AT LT WING 2023-661623<[01] REMOVED AND REPLACED FITTING ON TRAILING EDGE ACCESS PANEL 551GB AT LT WING IAW B737-700 SRM 51-40-02-0G-0;[02] COMPLETED
CRACK ANGLE TRAILING EDGE LOCATED IRSS 140 UPPER POSITION RT WING 2023-661609<[01] REPLACED ANGLE TRAILING EDGE LOCATED IRSS 140 UPPER POSITION RT WING IAW. B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG: 115A2000 SHEET: 22 REV: A TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N: A21042057 DUE DATE: 04-APR-24;[02] REPLACED ANGLE TRAILING EDGE LOCATED IRSS 140 UPPER POSITION RT WING IAW. B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG: 115A2000 SHEET: 22 REV: A TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N: A21042057 DUE DATE: 04-APR-24
CRACK ANGLE ON INBOARD AUXILIARY SLAT TRACK SLAT 8 AT RT WING 2023-661597<[01] REMOVED AND REPLACED ANGLE INBOARD AUXILIARY TRACK ON SLAT 8 AT RT WING IAW B737-700 CMM 57-43-01 STEP 2C(10) PAGE 702 FIG. 701.<BR>TOOL USED: CALIPER; PN: 500-196-30; SN: A22348307; DUE DATE: 23-AUG-24; THICKNESS GAGE; PN: 17-1803; SN: AE-407089; DUE DATE: 02-MAY-24.;[02] REMOVED AND REPLACED ANGLE INBOARD AUXILIARY TRACK ON SLAT 8 AT RT WING IAW B737-700 CMM 57-43-01 STEP 2C(10) PAGE 702 FIG. 701.<BR>TOOL USED: CALIPER; PN: 500-196-30; SN: A22348307; DUE DATE: 23-AUG-24; THICKNESS GAGE; PN: 17-1803; SN: AE-407089; DUE DATE: 02-MAY-24.JOB COMPLETED.
CRACK WEB - INTERCOSTAL LOCTED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R WL 156 AFT CARGO COMPARTMENT 2023-661594<[01] REPLACED WEB - INTERCOSTAL LOCTED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R WL 156 AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-10-02 PAR. 9; SRM 51-40-02 AND DRAWING 147A7500 SHEET 36 REV. -;[02] REPLACED WEB - INTERCOSTAL LOCTED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R WL 156 AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-10-02 PAR. 9; SRM 51-40-02 AND DRAWING 147A7500 SHEET 36 REV. -
CORROSION EXTERNAL SKIN DOUBLER LOCATED BETWEEN BS 727B AND 727C; STR 1 AND STR 2R AT UPPER FUSELAGE 2023-661591<[01] REPLACED FASTENERS EXTERNAL SKIN DOUBLER LOCATED BETWEEN BS 727B AND 727C; STR 1 AND STR 2R AT UPPER FUSELAGE IAW B737-700 SRM 51-40-02 AND DRAWING DG234-7023-20 REV. D. SEE INDIVIDUAL SIGNOFFS BELOW;[02] CERTIFIED STEP 1 COMPLETED
CRACK ANGLE - SUPPORT BS 867 BETWEEN STRINGER 26L AND STRINGER 27L AFT CARGO COMPARTMENT 2023-661583<[01] REPLACED ANGLE - SUPPORT BS 867 BETWEEN STRINGER 26L AND STRINGER 27L AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 ITEM 9.;[02] REPLACED ANGLE - SUPPORT BS 867 BETWEEN STRINGER 26L AND STRINGER 27L AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 ITEM 9.
CORROSION EXTERNAL SKIN DOUBLER LOCATED BETWEEN BS 747 AND BS 767; STR 1 AND STR 2R AT UPPER FUSELAGE 2023-661592<[01] REPLACED FASTENERS EXTERNAL SKIN DOUBLER LOCATED BETWEEN BS 747 AND BS 767; STR 1 AND STR 2R AT UPPER FUSELAGE IAW B737-700 SRM 51-40-02 AND DRAWING DG234-7023-20 REV. D. SEE INDIVIDUAL SIGNOFFS BELOW;[02] CERTIFIED STEP 1 COMPLETED
DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (5EA) 2023-661585<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (5EA) IAW B737-700 AMM 33-51-15-400-802;[02] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (5EA) IAW B737-700 AMM 33-51-15-400-802
BROKEN BODY STATION 663.75 SUPPORT ANGLE LOCATED AT RBL 25.00 AT MAIN WHEEL WELL COMPARTME 2023-661580<[01] REPLACED SUPPORT ANGLE LOCATED ON BODY STATION 663.75 & RBL 25.0 AT MAIN WHEEL WELL COMPARTMENT. IAW B737-700 SRM 51-10-02.;[02] CORRECTED STEP 1.<BR>REPLACED SUPPORT ANGLE LOCATED ON BODY STATION 663.75 & RBL 25.0 AT MAIN WHEEL WELL COMPARTMENT. IAW B737-700 SRM 51-10-02. 'SEE INDIVIDUAL SIGNOFFS BELOW'.;[03] COMPLETE TASK CERTIFIED
CRACK BRACKET BS 947.5 AND STRINGER 26L AT AFT CARGO COMPARTMENT 2023-661586<[01] REPLACED BRACKET LOCATED BS 947.5 & STRINGER 26L AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 & DWG 149A8103 SHEET 7; REV A.;[02] CORRECTED STEP 1.<BR>REPLACED BRACKET LOCATED BS 947.5 & STRINGER 26L AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 & DWG 149A8103 SHEET 7; REV A. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[03] REPLACED BRACKET LOCATED BS 947.5 & STRINGER 26L AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 & DWG 149A8103 SHEET 7; REV A. ?SEE INDIVIDUAL SIGNOFFS BELOW?
CORROSION SUPPORT ZEE BETWEEN BS 727C TO BS 767 RBL 21 AND WL 156 AFT CARGO COMPARTMENT 2023-661590<[01] TOOL USED ULTRASONIC EQUIPMENT PN: 45MG; SN: 232019809; DUE DATE: 22-SEP-24.;[02] EVALUATED DAMAGE ON SUPPORT ZEE LOCATED BTW BS 727C TO BS 767 RBL 21 & WL 156 AT AFT CARGO COMPARTMENT & FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2. 'SEE INDIVIDUALS SIGNOFFS BELOW'.;[03] EVALUATED DAMAGE ON SUPPORT ZEE LOCATED BTW BS 727C TO BS 767 RBL 21 & WL 156 AT AFT CARGO COMPARTMENT & FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2. 'SEE INDIVIDUALS SIGNOFFS BELOW'.
CRACK ON SUPPORT ANGLE LOCATED BTW BS 500D TO BS 520 RBL 4 AT PASSENGER CABIN 2023-661573<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 500D TO BS 520 RBL 4 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND B737-700 DWG:153A5400 SHEET 122 REV:-SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED SUPPORT ANGLE LOCATED BTW BS 500D TO BS 520 RBL 4 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND B737-700 DWG:143A5400 SHEET 122 REV:-SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED SUPPORT ANGLE LOCATED BTW BS 500D TO BS 520 RBL 4 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND B737-700 DWG:143A5400 SHEET 122 REV:-SEE INDIVIDUAL SIGN OFFS BELOW.
CRACK ANGLE INBOARD AUXILIARY SLAT TRACK ON SLAT1 AT LT WING 2023-661534<[01] REMOVED AND REPLACED ANGLE INBOARD AUXILIARY TRACK ON SLAT 1 AT LT WING IAW B737-700 CMM 57-43-01 STEP 2C(10) PAGE 702 FIG. 701.<BR>TOOL USED: CALIPER; PN: 500-196-30; SN: A22348307; DUE DATE: 23-AUG-24; THICKNESS GAGE; PN: 17-1803; SN: AE-407089; DUE DATE: 02-MAY-24.;[02] REMOVED AND REPLACED ANGLE INBOARD AUXILIARY TRACK ON SLAT 1 AT LT WING IAW B737-700 CMM 57-43-01 STEP 2C(10) PAGE 702 FIG. 701.<BR>TOOL USED: CALIPER; PN: 500-196-30; SN: A22348307; DUE DATE: 23-AUG-24; THICKNESS GAGE; PN: 17-1803; SN: AE-407089; DUE DATE: 02-MAY-24..JOB COMPLETED.
CRACK SUPPORT ANGLE LOCATED BS867 AT LEVEL STR3R PASSENGER CABIN 2023-661511<[01] REPLACED SUPPORT ANGLE LOCATED BS 867 AT LEVEL STR 3R PASSENGER CABIN SUPPORT ANGLE MUST BE REPLACED IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 146A7901 SHEET: 66 REV: A . SEE INDIVIDUAL SIGN-OFF BELOW.;[02] CORRECTED STEP 1<BR>REPLACED SUPPORT ANGLE LOCATED BS 867 AT LEVEL STR 3R PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 146A7901 SHEET: 66 REV: A . SEE INDIVIDUAL SIGN-OFF BELOW.;[03] REPLACED SUPPORT ANGLE LOCATED BS 867 AT LEVEL STR 3R PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 146A7901 SHEET: 66 REV: A . SEE INDIVIDUAL SIGN-OFF BELOW.<BR>CERTIFIED AS RII
CRACK LEADING EDGE RIB LOC. LE STA 114.55 AT LT HORIZONTAL STABILIZER 2023-661510<[01] REPLACED LEADING EDGE RIB (CHORD) LOC. LE STA 114.55 AT LT HORIZONTAL STABILIZER IAW SRM B737-700 51-10-02 ITEM 9 AND DWG# 186A1001 REV- ; DWG# 186A1305 REV-. SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED LEADING EDGE RIB (CHORD) LOC. LE STA 114.55 AT LT HORIZONTAL STABILIZER IAW SRM B737-700 51-10-02 ITEM 9 AND DWG# 186A1001 REV- ; DWG# 186A1305 REV-. SEE INDIVIDUAL SIGNOFF BELOW.
CORROSION STRINGER 23R LOCATED BS540 AT FWD CARGO COMPARTMENT 2023-661505<[01] TOOL USED:ULTRASONIC EQUIPMENT P/N 45MG S/N 221860711 DUE DATE: 07-NOV-23 .;[02] TOOL P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 12-MAR-24.;[03] TOOL USED TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24;[04] PERFORMED PERMANENT REPAIR STRINGER 23R LOCATED BS540 AT FWD CARGO COMPARTMENT; IAW BOEING 737-700 SRM 53-00-03-2R-1 REPAIR 1; SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED PERMANENT REPAIR STRINGER 23R LOCATED BS540 AT FWD CARGO COMPARTMENT; IAW BOEING 737-700 SRM 53-00-03-2R-1 REPAIR 1; SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED
CORROSION STRINGER 23L LOCATED BS540 AT FWD CARGO COMPARTMENT 2023-661506<[01] TOOL P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 12-MAR-24.;[02] TOOL USED TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24;[03] PERFORMED PERMANENT REPAIR STRINGER 23L LOCATED BS540 AT FWD CARGO COMPARTMENT; IAW BOEING 737-700 SRM 53-00-03-2R-1 REPAIR 1; SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR STRINGER 23L LOCATED BS540 AT FWD CARGO COMPARTMENT; IAW BOEING 737-700 SRM 53-00-03-2R-1 REPAIR 1; SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED
BROKEN STRINGER CLIP ON STR 3 BTW BS986.5 AND BS1006 RH SIDE 2023-661469<[01] REPLACED STRINGER CLIP ON STR 3 BTW BS986.5 AND BS1006 RH SIDE I.A.W SOPM 20-50-01 REV. 38;[02] REPLACED STRINGER CLIP ON STR 3 BTW BS986.5 AND BS1006 RH SIDE I.A.W SOPM 20-50-01 REV. 38
CORROSION ON PLATE LOCATED FLOOR STRUCTURE BS 1016 PLUS 13 INCHES AT AFT GALLEY AREA 2023-661470<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN: 221861811; DUE DATE: 08-NOV-23;[02] EVALUATED PLATE LOCATED FLOOR STRUCTURE BS 1016 PLUS 13 INCHES AT AFT GALLEY AREA AND FOUND WHITIN LIMITS IAW B737-700 SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH 4.G(2) FIGURE 103 DETAIL L. SEE INDIVIDUAL SIGN OFFS BELOW;[03] EVALUATED PLATE LOCATED FLOOR STRUCTURE BS 1016 PLUS 13 INCHES AT AFT GALLEY AREA AND FOUND WHITIN LIMITS IAW B737-700 SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH 4.G(2) FIGURE 103 DETAIL L. SEE INDIVIDUAL SIGN OFFS BELOW
DETERIORATED GIRT BAR FITTING HARDWARE ON FWD ENTRY/SERVICE AT AFT GAL LEY AREA 2023-661394<[01] REPLACED GIRT BAR FITTING HARDWARE ON FWD ENTRY/SERVICE AT AFT GALLEY AREA I.A.W. B737-700 AMM 25-66-02-201;[02] REPLACED GIRT BAR FITTING HARDWARE ON FWD ENTRY/SERVICE AT AFT GALLEY AREA I.A.W. B737-700 AMM 25-66-02-201
CORROSION INLET COWL LIP-SKIN INBOARD AREA ON ENGINE 1 2023-661449<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 130063701 AND DUE DATE: 24-JUL-24.;[02] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[03] REPAIRED INLET COWL LIP-SKIN INBOARD AREA ON ENGINE 1 IAW EA 23-171-03332-WIP1 AND EA 23-171-03332 SEE INDIVIDUAL SIGNOFFS BELOW;[04] REPAIRED INLET COWL LIP-SKIN INBOARD AREA ON ENGINE 1 IAW EA 23-171-03332-WIP1 AND EA 23-171-03332 SEE INDIVIDUAL SIGNOFFS BELOW
CORROSION INLET COWL LIP-SKIN INBOARD AREA ON ENGINE 2 2023-661450<[01] TOOL USED: ULTRASONIC THICKNESS GAGE. PN: 45MG; SN: 232019809; DUE DATE: 22-SEP-24;[02] TOOL USED ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 130063701; CAL DUE DATE: 24-JUL-24;[03] REPAIRED INLET COWL LIP-SKIN INBOARD AREA ON ENGINE 2 IAW EA 23-171-03333-WIP1 AND EA 23-171-03333 SEE INDIVIDUAL SIGNOFFS BELOW;[04] REPAIRED INLET COWL LIP-SKIN INBOARD AREA ON ENGINE 2 IAW EA 23-171-03333-WIP1 AND EA 23-171-03333 SEE INDIVIDUAL SIGNOFFS BELOW
ELONGATED HOLE ON FITTING LOCATED BS 1016 UPPER AREA AT AFT GALLEY AREA 2023-661434<[01] REPLACED FITTING LOCATED BS 1016 UPPER AREA AT AFT GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9. AND DWG 148A2230 SHEET: 8 REV: C. SEE INDIVIDUALS SIGN-OFF BELOW;[02] REPLACED FITTING LOCATED BS 1016 UPPER AREA AT AFT GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9. AND DWG 148A2230 SHEET: 8 REV: C. SEE INDIVIDUALS SIGN-OFF BELOW<BR>CERTIFIED AS RII
CORROSION ON FLOOR BEAM LOCATED BS 986.5 LBL 42 WL 208.1 AT AFT GALLEY AREA 2023-661415<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 130060401 DUE DATE: 20-MAR-24;[02] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 200053402 AND DUE DATE: 24-AUG-24.;[03] REPAIRED FLOOR BEAM LOCATED BS 986.5 LBL 39 TO LBL 47 WL 208.1 AT AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4; SEE INDIVIDUAL SIGN-OFF BELOW;[04] REPAIRED FLOOR BEAM LOCATED BS 986.5 LBL 39 TO LBL 47 WL 208.1 AT AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4; SEE INDIVIDUAL SIGN-OFF BELOW<BR>CERTIFIED AS RII
ELONGATED HOLE SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2023-661417<[01] REPLACED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02; SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1.<BR>REPLACED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02; INSTALLATION IS DOCUMENTED ON TTG8Q0020G67; SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02; INSTALLATION IS DOCUMENTED ON TTG8Q0020G67; SEE INDIVIDUAL SIGN-OFF BELOW
CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-661411<[01] REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. IAW DWG 141A1110 SHEET 18 REV - SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. IAW DWG 141A1110 SHEET 18 REV -; RII; SEE INDIVIDUAL SIGNOFFS BELOW.
INOP BATTERY PACK ON FWD PASSENGER CABIN (2 EA) AFT PASSENGER CABIN (2 EA) AND OVER-WING ESCAPE HATCH (1 EA) 2023-661407<[01] REPLACED BATTERY PACK ON FWD PASSENGER CABIN (2 EA) AFT PASSENGER CABIN (2 EA) AND OVER-WING ESCAPE HATCH LT (1 EA) I.A.W B737-700 AMM 33-51-06-960-805.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED BATTERY PACK ON FWD PASSENGER CABIN (2 EA) AFT PASSENGER CABIN (2 EA) AND OVER-WING ESCAPE HATCH LT (1 EA) I.A.W B737-700 AMM 33-51-06-960-805.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.
CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-661411<[01] REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. IAW DWG 141A1110 SHEET 18 REV - SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. IAW DWG 141A1110 SHEET 18 REV -; RII; SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK SUPPORT BRACKET ASSY LOCATED BTW BS 540 TO BS 559 RT SIDE AT AIR CONDITIONING BAY 2023-661413<[01] REPLACED SUPPORT BRACKET ASSY LOCATED BTW BS540 TO BS559 RT SIDE AT AIR CONDITIONING BAY IAW SRM B737-700 51-10-02-0G ITEM 9 AND SRM B737-700 51-40-02-0G-0;[02] REPLACED SUPPORT BRACKET ASSY LOCATED BTW BS540 TO BS559 RT SIDE AT AIR CONDITIONING BAY IAW SRM B737-700 51-10-02-0G ITEM 9 AND SRM B737-700 51-40-02-0G-0
INOP BATTERY PACK LOCATED BS 603 WL 212 RBL 67 AT PASSENGER CABIN 2023-661361<[01] REPLACED BATTERY PACK LOCATED BS 603 WL 212 RBL 67 AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-06-960-805. SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] REPLACED BATTERY PACK LOCATED BS 603 WL 212 RBL 67 AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-06-960-805. SEE INDIVIDUAL SIGN-OFFS BELOW.
CRACK ON SUPPORT ANGLE LOCATED BS 695 RBL 0 AT PASSENGER CABIN 2023-661370<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:112820025; DUE DATE: 01-FEB-24.;[02] REPLACED SUPPORT ANGLE LOCATED BS 695 RBL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG: 273A9110 SHEET: 6 REV: A . SEE INDIVIDUAL SIGN-OFF BELOW.;[03] TASK CARD COMPLETED
CRACK ON SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN 2023-661371<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N:112820025; DUE DATE: 01-FEB-24.;[02] REPLACED SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 273A9110 SHEET: 6 REV: A. SEE INDIVIDUAL SIGN-OFF BELOW.;[03] TASK CARD COMPLETED
CRACK ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER 2023-661369<[01] TOOL USED CALIPER P/N: 500-197-30; S/N 15120589; DUE DATE: 13-FEB-24.;[02] TOOL USED HOT BONDER P/N HCS9200B; S/N 15102320; DUE DATE: 22-JAN-24.;[03] TOOL USED SCALE P/N CL5000; S/N AE-408751; DUE DATE:12-APR-24;[04] TOOL USED SCALE P/N 91847 S/N AE-409313; DUE DATE:13-JUN-24;[05] TOOL USED HOT BONDER P/N HCS9200B; S/N 15102320; DUE DATE: 22-JAN-24.;[06] TOOL USED: UT EQUIPMENT P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 24-JAN-24;[07] REPAIRED ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-20-01-2R-4 REPAIR 4 PARAGRAPH 4.C(2); TABLE 201; B737-700 SRM 51-70-04-2R-10 REPAIR 10 . SEE INDIVIDUAL SIGN OFFS BELOW.;[08] REPAIRED ACCESS PANEL 334GB AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-20-01-2R-4 REPAIR 4 PARAGRAPH 4.C(2); TABLE 201; B737-700 SRM 51-70-04-2R-10 REPAIR 10 . SEE INDIVIDUAL SIGN OFFS BELOW.
CRACK VAPOR VARRIER RH SIDE BS663 RBL 48 AT MAIN WHEEL WELL COMPARTME (CUSTOMER REQUEST ) 2023-661346<[01] TOOL USED; CALIPER P/N: 500-197-30; S/N: 15120589; DUE DATE: 13-FEB-23.;[02] TOOL USED HOT BONDER P/N: HCS9000B-AV; S/N: 18164925; DUE DATE: 22-JAN-24.;[03] TOOL USED SCALE P/N: SPX621; S/N: 8340225451; DUE DATE: 16-AUG-24.;[04] TOOL USED HOT BONDER P/N: HCS9200B; S/N: 16122983; DUE DATE: 24-JAN-24.;[05] TOOL USED : ULTRASONIC EQUIPMENT P/N EPOCH 600 S/N 120357005 DUE DATE: 24-JAN-24.;[06] REPAIRED VAPOR VARRIER RH SIDE BS663 RBL 48 AT MAIN WHEEL WELL COMPARTMET IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] REPAIRED VAPOR VARRIER RH SIDE BS663 RBL 48 AT MAIN WHEEL WELL COMPARTMET IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW. RII ACCOMPLISHED
CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2023-661293<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189443;DUE DATE:27-DEC-23.;[02] TOOL USED RADIOMETER P/N XRP-3000 S/N 1859843 DUE DATE 05-DEC-24;[03] REPAIRED THE AFT CORNER SCUFF PLATE OF FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4.B. STEPS ( 2 ) TO ( 7 ) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[04] JOB COMPLETED.
MULTIPLE EMERGENCY LIGHTS OUT IN AFT CABIN AND AT AFT SVC AND AFT ENTRY DOOR.<[01] REMOVED AND REPLACED R/H AFT EMERGENCY BATTERY PACK M1672 REF AMM 33-51-06. OPS CHECK GOOD.
LH EMERGENCY ESCAPE HATCH EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK FOR LEFT ESCAPE HATCH AND OVER WING EMERGENCY EXIT LIGHTS (M1670) PER AMM 33-51-06.
EMERGENCY EXIT LIGHT LENS AT L/H OVERWING EXIT FELL OFF.<[01] INSTALLED NEW EXIT LIGHT LENS AT L/H OVERWING EXIT IAW AMM 33-51-01.
LEFT OVERWING EMERGENCY LIGHT INOP<[01] RELAMPED LEFT OVERWING EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.
L1 DOLE EXT EMERGENCY LIGHT INOP.<[01] RNR FWD ENTRY BATTERY PACK IAW AMM 33-51-06. OPC GOOD.
FWD CARGO AFT CORNER THRESHOLD CRACKED AT RADIUS.<[01] R+R FWD CARGO AFT THRESHOLD PER AMM 53-11-02.;[02] R+R FWD CARGO AFT THRESHOLD PER AMM 53-11-02.
FWD SERVICE DOOR EMERG EXIT LIGHT COVER BROKEN / [01] REMOVED AND REPLACED FWD SERVICE DOOR EMERG LIGHT ASSY PER AMM 33-51-01.
PLASTIC EXIT ROW SIGN OF CAPTAINS AFT ENTRY LOOSE / [01] R/R THE EMERGENCY EXIT LIGHT ASSY. AT THE L2 DOOR; OP?S CHECK IAW AMM 33-51-01.
AFT SERVICE DOOR SLIDE PRESS IS LOW / [01] R&R AFT SERVICE DOOR SLIDE PER MT 725-61-06
SUPPLEMENTAL INFORMATION: SUSPECTED FUEL LEAK ON #2 ENGINE. IMBALNCE OF 500# WITHIN 20 MINUTES. FUEL FLOW ON #2 ENGINE SHOWED 60 POUNDS MORE FLOW. HANGAR REQUEST RECORD #1499PLANNED HOU 02/08 / [01] FOUND TANK UNITS F4; F5; F6; F8; F9; F11; F12 DRY AND WET CAPACITANCE OUT OF AMM 28-41-21 LIMITS. NEEDS TANK DIVE.<BR>OK TO CONTINUE PER MEL 28-6-02 SP1; SP3; SP28<BR>AUTH# 46275;[02] R&R?D #2 FUEL TANK PROBES F4; F5; F6; F8; F9; F11 & F12. ALL WORK ACCOMPLISHED ON TANK TIGERS W/O# 12234R150. OPS AND LEAK CHECK GOOD.
R/H OVER WING EXIT SIGN (LOWER FWD DOOR) AS INOP BULBS ; RH OVER WING EXIT SIGN (LOWER FWD DOOR) AS INOP LS / [01] REMOVED; REPLACED AND PERFORMED GOOD OPERATIONAL CHECK OF R/H OVER WING EXIT SIGN (LOWER AND FWD OF DOOR) LAMPS PER AMM 33-51-01-960-801.
R/H OVER WING EXIT SIGN (LOWER FWD DOOR) AS INOP BULBS ; RH OVER WING EXIT SIGN (LOWER FWD DOOR) AS INOP LS / [01] REMOVED; REPLACED AND PERFORMED GOOD OPERATIONAL CHECK OF R/H OVER WING EXIT SIGN (LOWER AND FWD OF DOOR) LAMPS PER AMM 33-51-01-960-801; [02] VERIFIED CORRECTIVE ACTION ENTRY 1. CARD COMPLETE.
EMERGENCY EXIT SLIDE LIGHT AT LEFT OVERWING AND LEFT GROUND ILLUMINATION POSITION INOP. ; / [01] REPLACED LAMPS FOR EMERGENCY EXIT SLIDE LIGHT AT LEFT OVERWING EXIT AND LEFT GROUND ILLUMINATION POSITION AND PERCORMED GOOD TEST PER AMM 33-51-04-960-801.; [02] VERIFIED CORRECTIVE ACTION #1
LT WING L/E PANEL 521TB FWD I/B CORNER IS DELAMINATED ; / [01] IDENTIFIED MATERIAL OF PANEL 521TB IAW SRM 57-41-01-0I-4 FIGURE 1; 3 AND 10; ITEM #1; TABLE 3 AND 10<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 TABLE 101; PARA 4.A(5)<BR><BR>REPAIR TO BE ACCOMPLISHED IAW SRM 51-70-05 PER SRM 57-41-01-2R-1 PARA 4.B(2) AND 4.E; TABLE 202; [02] VALIDATED APPLICABILITY OF REPAIR TO BE COMPLETED IAW SRM 51-70-05 (250 PREPREG) AS GIVEN IAW SRM 57-41-01-2R-1.; [03] REMOVED 2EA BACKING PLATES IAW SRM 51-40-02-0G-0 PARA 4.E<BR><BR>REMOVED INNER SURFACE ALUMINUM FOIL PLY IAW SRM 51-70-14-2R-3 PARA 4.A(2)(B & E)<BR><BR>VISUALLY EXAMINED EXTENT OF DAMAGE; TAP TESTED - DISBONDS NOTED; REMOVED DAMAGE AT FWD IB CORNER AND DAMAGE AT AFT 3RD HOLE ALONG IB EDGED; REMOVED 2.5' X 7' OF DAMAGE ON INNER SURFACE AND REMOVED 2' X 6' OF DAMAGE ON OUTER SURFACE; PREPPED AND CLEANED REPAIR AREAS IAW SRM 51-70-05-2R-6 PARA 4.A-C; [04] VERIFIED CORRECTIVE ACTIONS 1-3<BR><BR>VALIDATED REPAIR PER SRM 51-70-05; [05] FABRICATED REPAIR PLIES FROM BMS 8-79 (120) LOT# 1466500-1 AND (1581) LOT# 1469966-1; BMS 5-129 (GR5) LOT# 1470655-1; INSTALLED REPAIR PLIES; VACUUM BAGGED AND SET FOR CURE IAW SRM 51-70-05-2R-6 PARA 4.E-F<BR><BR>HOT BONDER ID NCX000523 SN 11051262;
FWD CARGO AFT CORNER SCUFF PLATE IS CRACKED ; FWD CARGO AFT CORNER SCFF PLATE IS CRACKED / [01] WELDED CRACKED RADIUS OF FCB; AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-30-15-2R-1 PARA 4.B. (2) AND (4)<BR>WELDING MACHINE CALIBRATION I.D. E10583; S/N; KJ256554 12-2021; [02] INSPECTED ACTION 1; [03] PT INSPECTED SCUFF PLATE IAW SOPM 20-20-02. NO CRACKS NOTED.; [04] EQUIP. USED; ID: ATS2561-1;2;3 S/N: 191424A/B/C; [05] SANDED WELD REPAIR AREA PER SRM 53-30-15-2R-1 PARA 4.B.(5); [06] VERIFIED CORRECTIVE ACTION 5; [07] REQUEST OK TO INSTALL AFT CORNER SCUFF PLATE.; [08] VERIFIED OK TO INSTALL; [09] INSTALLED THE FWD CARGO DOOR CUTOUT SCUFF PLATES IAW AMM 53-11-02; [10] INSTALLED THE FWD CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE IAW AMM 53-11-02; [11] CORRECTED LOCATION.; [12] TOOL USED ID: ATS2620 S/N: 1703016; [13] ADDED TOOL USED; [14] INSTALLED THE FWD CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE IAW AMM 53-11-02 AND SRM 53-30-15-2R-1 STEP 4.B. (6-13).<BR><BR>TOOL USED ID: ATS2620 S/N: 1703016; [15] VERIFIED CORRECTIVE ACTIONS 9-14; [16] ALL WORK ACCOMPLISHED.
FWD CARGO FWD CORNER SCUFF PLATE IS CRACKED ; FWD CARGO FWD CORNER SCFF PLATE IS CRACKED / [01] WELDED CRACK ON FCB; FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-30-15-2R-1 PARA 4.B. (2) AND (4)<BR>WELDING MACHINE CALIBRATION I.D. E10583; S/N; KJ256554; [02] INSPECTED ACTION 1; [03] PT INSPECTED SCUFF PLATE IAW SOPM 20-20-02. FOUND CRACK AT CENTER LINE OF SCUFF PLATE CREST IN THE RADIUS; [04] EQUIP. ID: ATS2561-1;2;3 S/N: 191424A/B/C; [05] WELDED CRACK AS NOTED BY NDT INSPECTION ON FCB; FWD CORNER SCUFF PLATE RADIUS USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-30-15-2R-1 PARA 4.B. (2) AND (4) <BR>WELDING MACHINE CALIBRATION I.D. E10583; S/N; KJ256554; [06] VERIFIED CORRECTIVE ACTION 5 (RE-WELD); [07] PT INSPECTED WELD AT RADIUS IAW SOPM 20-20-02. NO CRACKS NOTED. EQUIP. ID: ATS2561-1;2;3 S/N: 191424A/B/C; [08] SANDED REPAIR WELDS SMOOTH PER SRM 53-30-15-2R-1 PARA 4.B (5); [09] VERIFIED CORRECTIVE ACTION 8; [10] REQUEST OK TO INSTALL FWD CORNER SCUFF PLATE.; [11] VERIFIED OK TO INSTALL; [12] INSTALLED THE FWD CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE IAW AMM 53-11-02.; [13] TOOL USED ID: ATS2620 S/N: 1703016; [14] ADDED TOOL USED; [15] INSTALLED THE FWD CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE IAW AMM 53-11-02 AND SRM 53-30-15-2R-1 STEP 4.B. (6-13).<BR><BR>TOOL USED ID: ATS2620 S/N: 1703016; [16] VERIFIED CORRECTIVE ACTIONS 12-15.; [17] ALL WORK ACCOMPLISHED.
RT WING UPPER T/E PANEL I/B OF #8 SPOILER THE LOWER WEB O/B ATTACH ANGLE IS CRACKED AT FLAP LOAD RIB ; / [01] REMOVED AND REPLACED RT WING UPPER T/E PANEL I/B OF #8 SPOILER THE LOWER WEB O/B ATTACH ANGLE P/N 115A6260-2 IAW SRM 51-40-02 AND AIPC 57-42-51-03; [02] VERIFIED REPLACEMENT OF RT WING UPPER T/E PANEL; I/B OF #8 SPOILER; LOWER WEB O/B ATTACH ANGLE PER SRM 51-40-02 AND AIPC 57-42-51-03
FWD CARGO BAY GUSSET CRACKED BS 500D STR 19R ; / [01] REMOVED FWD CARGO BAY GUSSET BS 500D STR 19R IAW SRM 51-40-02.; [02] RECEIVED NEW GUSSET P/N 143A9481-5; LOCATED AND DRILLED NEW GUSSET AT FWD CARGO BAY BS 500D STR 19R IAW SRM 51-40-05-OG-0 DWG#143A7902.; [03] VERIFIED CORRECTIVE ACTION STEP 2.; [04] OK TO INSTALL.; [05] OK TO INSTALL NEW GUSSET AT BS 500D; STR-19R; [06] INSTALLED NEW GUSSET FWD CARGO BAY BS500D STG 19R IAW SRM 51-40-02-0G-0; DWG#143A7902; [07] VERIFIED INSTALLATION OF NEW FCB GUSSET; BS 500D; STR-19R; PER SRM 51-40-02-0G-0 AND DWG 143A7902; [08] VERIFIED INSTALLATION COMPLETE; ALL WORK ACCOMPLISHED THIS TASK; [09] VERIFIED ALL WORK COMPLETE THIS TASK
FWD CARGO BAY GUSSET CRACKED BS 500D STR 19L ; / [01] REMOVED FWD CARGO BAY GUSSET BS 500D STR 19L IAW SRM 51-50-02.; [02] RECEIVED NEW GUSSET P/N 143A9481-6; LOCATED AND DRILLED NEW GUSSET AT FWD<BR>CARGO BAY BS 500D STR 19L IAW SRM 51-40-05-OG-0 DWG#143A7902; [03] VERIFIED CORRECTIVE CTION STEP 2.; [04] OK TO INSTALL.; [05] OK TO INSTALL NEW GUSSET AT BS 500D; STR-19L; [06] INSTALLED NEW GUSSET FWD CARGO BAY BS500D STG 19L IAW SRM 51-40-02-0G-0; DWG#143A7902; [07] VERIFIED INSTALLATION OF NEW FCB GUSSET; BS 500D; STR-19L; PER SRM 51-40-02-0G-0 AND DWG 143A7902; [08] VERIFIED ALL WORK COMPLETE THIS TASK
CRACKED DUCT SUPPORT BRACKET AT STA 540+7; WL 168; RBL 6 ; / [01] REMOVED DUCT SUPPORT BRACKET AT STA 540+7 WL 168 RBL 6 IAW SRM 51-40-02.; [02] INSTALLED NEW DUCT SUPPORT BRACKET P/N 212A1116-1 AT BS 540+7 RBL 6 WL 168 . IAW 737-700 SRM 51-40-02-0G-0; DWG 212A1110 . ALL REQUIRED MAINTENANCE ACTIONS ARE COMPLETE=REQUEST FINAL BUYOFF; [03] RECEIVED AND INSTALLED NEW DUCT SUPPORT BRACKET P/N 212A1116-1 LOT WO-45631100 AT BS 540+7 RBL 6 WL 168 . IAW 737-700 PER SRM 51-40-02 AND SOPM 20-50-00;SATANDAR TORQUE FOR CLAMPS FIG 4; DWG 212A1110 . USED TOOL ID ATS597 DUE09/2022 ALL REQUIRED MAINTENANCE ACTIONS ARE COMPLETE=REQUEST FINAL BUYOFF; [04] VERIFIED CORRECTIVE ACTION STEPS 2 AND 3.
CRACKED DUCT SUPPORT BRACKET AT STA 540+7; WL 168; LBL 6 ; / [01] REMOVED SUPPORT BRACKET AT STA 540+7;WL;168 LBL 6 IAW SRM 51-40-02.; [02] INSTALLED NEW DUCT SUPPORT BRACKET P/N 212A1116-1 AT BS 540+7 LBL 6 WL 168 . IAW 737-700 SRM 51-40-02-0G-0; DWG 212A1110 . ALL REQUIRED MAINTENANCE ACTIONS ARE COMPLETE=REQUEST FINAL BUYOFF; [03] RECEIVED AND INSTALLED NEW DUCT SUPPORT BRACKET P/N 212A1116-1 LOT WO-45631100 AT BS 540+7 LBL 6 WL 168 . IAW 737-700 PER SRM 51-40-02 AND SOPM 20-50-00;SATANDAR TORQUE FOR CLAMPS FIG 4; DWG 212A1110 . USED TOOL ID ATS597 DUE09/2022 ALL REQUIRED MAINTENANCE ACTIONS ARE COMPLETE=REQUEST FINAL BUYOFF; [04] VERIFIED CORRECTIVE ACTION STEPS 2 AND 3.
CORROSION FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 500B +10; +14; +18; BS 500C +2; +6; +10-14 LBL 24 WL 156 ; / [01] REMOVED AND EVALUATED DAMAGE; [02] VERIFIED STEPS 1-6 COMPLETE. OUT OF LIMITS.; [03] FABRICATED NEW SIDEWALL SUPPORT IAW SRM 51-40-05-0G-0 AND DRAWING#143A7501 LOT#1467644-1 BAC1496-444 7075-T6.<BR>FABRICATED SPLICE REPAIR IAW SRM 53-00-53-2R-6 REPAIR 6 PART 4D-4I; SRM 51-40-05-0G-0 LOT#1467644-1 BAC1496-444 7075-T6 <BR>OK TO TREAT AND PRIME; [04] VERIFIED CORRECTIVE ACTION ENTRY 3. OK TO TREAT AND PRIME GIVEN.; [05] THIS CARD WILL BE ACCOMPLISHED WITH THE CUSTOMER CARD #TTG8Q0092ZPC.; [06] VERIFIED APPLICATION OF CONVERSION COATING AND PRIMER AND PART INSTALLATION TO BE ACCOMPLISHED ON FAULT # TTG8Q0092ZPC
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT WL 153; LBL 23; STATIONS: 727B+10; 727C+2; 727C+6; 727C+14; 727C+18; 727C+6; 727C+19; 727D+6; 727D+18; 727E+2. ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT DISCREPANCY AREA FOUND TO BE OUT OF LIMITS L=1.800' W=1.000' D=0.018' ORIGINAL THICKNEES 0.040 IAW SRM 53-00-53-1A-2 FIG 103 DETAIL C USED TOOL ID ATS 1671 DATE DUE 01/2022; [02] VERIFIED DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; [03] FABRICATED; LOCATED AND DRILLED NEW SIDEWALL SUPPORT IAW SRM 53-00-53-2R-6 REPAIR 6; SRM 51-40-05-0G-0 AND DRAWING#146A7501 LOT#5095753-1.<BR>OK TO TREAT AND PRIME; [04] REPAIR TYPE=MAJOR; [05] MATERIAL USED TO FABRICATED SIDEWALL SUPPORT P/N BAC1496-377 7075-T62.; [06] VERIFIED FABRICATED; LOCATED AND DRILLED NEW SIDEWALL SUPPORT IAW SRM 53-00-53-2R-6 PARA 4 D-I REPAIR 6; SRM 51-40-05-0G-0 AND DRAWING#146A7501 MATERIAL USED TO FABRICATED SIDEWALL SUPPORT P/N BAC1496-377 7075-T62 LOT#5095753-1. <BR>OK TO TREAT AND PRIME; [07] FABRICATED -2 SPLICE REPAIR FROM MATERIAL BAC1496-377 7075-T62 LOT# 5095753-1 AT BS 727E+10 AND LOCATED AND DRILLED IAW SRM 53-00-53-2R-6 REPAIR 6 OK TREAT AND PRIMER;
FWD CARGO BAY INTERCOASTAL ATTACH ANGLE CRACKED BS 400 RBL 24 WL154 ; / [01] FWD CARGO BAY INTERCOSTAL ATTACH ANGLE NO HAVE ALLOWABLE DAMAGE IN SRM MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-2 PARAG. 9.C; [02] REMOVED AT FWD CARGO BAY INTERCOASTAL ATTACH ANGLE BS 400 RBL 24 WL154 IAW SRM 51-40-02; [03] LOCATED AND DRILLED NEW INTERCOSTAL ATTACH ANGLE AT B/S 400 RBL 24 WL154 P/N 143A7502U154; PO # 837570/2 LOT# 1469069-2 IAW SRM 51-40-05 AND DWG 143A7505 REV:-; [04] OK TO INSTALL; [05] INSPECTED ACTION 1-4; OK TO INSTALL; [06] INSTALLED AT FWD CARGO BAY INTERCOASTAL ATTACH ANGLE BS 400 RBL 24 WL154 IAW SRM 51-40-02 AND DWG #143A7505; [07] RII INSPECTED ACTION 6; [08] PART REQUIRED; [09] VERIFIED CARD COMPLETE; [10] VERIFIED CARD COMPLETE
CRACKED FLOOR SUPPORT AT STA 540; WL 207; RBL 4 & 23. ; / [01] REMOVED AN REPLACE FLOOR SUPPORT BS 540 WL 207 RBL 4-23 PER SRM 51-40-02-0G-0 AND 51-40-05-; [02] PART USAGE INFO; [03] CORECTION TO ITEM #1 DWG # 143A0060; [04] VERIFIED REPLACEMENT OF CABIN FLOOR SUPPORT AT BS 540; RBL 4 - RBL 23; WL 207; PER SRM 51-40-02 AND DWG #143A0060; [05] VERIFIED ALL WORK COMPLETE THIS TASK
CRACKED FLOOR SUPPORT AT STA 540; WL 207; LBL 2. ; / [01] REMOVED AND REPLACED FLOOR SUPPORT BS 54- WL 207 LBL 2 PER SRM 51-40-02-0G-0 AND 51-40-05; [02] CORRECTION TO ITEM # 1 BS 540; [03] CORRECTION TO ITEM #1 - ADDED DWG #143A0060; [04] VERIFIED REPLACEMENT OF CABIN FLOOR SUPPORT AT BS 540; LBL 2; WL 207; PER SRM 51-40-02 AND DWG #143A0060; [05] VERIFIED ALL WORK COMPLETE THIS TASK
CORROSION FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 480 +14; +18; BS 500 + 10; +14; +18; BS 500A +2; +6; +10; BS 500B +2; +6 LBL 24 WL 156 ; / [01] REMOVED AND EVALUATED DAMAGE; [02] VERIFIED STEPS 1-10 COMPLETE. OUT OF LIMITS.; [03] FABRICATED NEW SIDEWALL SUPPORT IAW SRM 51-40-05-0G-0 AND DRAWING#143A7501 LOT#1467644-1 BAC1496-444 7075-T6.<BR>FABRICATED SPLICE REPAIR IAW SRM 53-00-53-2R-6 REPAIR 6 PART 4D-4I; SRM 51-40-05-0G-0 LOT#1467644-1 BAC1496-444 7075-T6 <BR>OK TO TREAT AND PRIME; [04] VERIFIED CORRECTIVE ACTION ENTRY 3. OK TO TREAT AND PRIME GIVEN.; [05] THIS CARD WILL BE ACCOMPLISHED WITH THE CUSTOMER CARD #TTG8Q0092ZPC.; [06] VERIFIED APPLICATION OF CONVERSION COATING AND PRIMER AND PART INSTALLATION TO BE ACCOMPLISHED ON FAULT # TTG8Q0092ZPC
CORROSION FWD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS 500D LBL 2; 9;13; 14-18; 20; 23; RBL 5; 8-11; 14-15; 23 WL 156 ; / [01] REMOVED AND EVALUATED DAMAGE.; [02] VERIFIED STEPS 1-10 OUT OF LIMITS.; [03] LOCATED AND DRILLED NEW FCB AFT BULKHEAD TO FLOOR SUPPORT ANGLE ITEM# 143A9485Y35 LOT#1468774-1 IAW 51-40-05-0G-0 OK TO INSTALL; [04] LOCATED AND DRILLED NEW FCB AFT BULKHEAD TO FLOOR SUPPORT ANGLE ITEM# 143A9485Y35 LOT#1468774-1 IAW SRM<BR> 51-40-05-0G-0 OK TO INSTALL; [05] VERIFIED LOCATE AND DRILL OF NEW FCB AFT BULKHEAD-TO-FLOOR SUPPORT PER SRM 51-40-05-0G-0; OK TO INSTALL; [06] FCB AFT BULKHEAD TO FLOOR SUPPORT ANGLE WILL BE INSTALLED ON CUSTOMER CARD # TTG8Q004EMB3; [07] UPDATED PARTS REMOVED / INSTALLED.; [08] INSPECTION COMPLETE
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT WL 153; LBL 23; STA 747+14. ; / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORTAT DISCREPANCY AREA .FOUND TO BE OUT LIMITS L=1.000 W=0.600' D=0.015' ORIGINAL THICKNESS O.O40' IAW SRM 53-00-53-1A-2 FIG103 DETAIL C USED TOOL ID ATS 1671 DATE DUE 01/2022; [02] VERIFIED DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; [03] THIS DISCREPANCY WILL ACCOMPLISED ON CARD TTG8Q0092YBD; [04] VERIFIED WORK TO BE ACCOMPLISHED ON FAULT TTG8Q0092YBD
CORROSION FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 500C +2; +6; +10; +14; BS 500B +7; 10-14; +18; BS 500A +6; +12; +14 RBL 24; WL 156 ; / [01] REMOVED AND EVALUATED DAMAGE; [02] VERIFIED STEPS 1-10. OUT OF LIMITS; [03] FABRICATED LOCATED AND DRILLED NEW FCB FLOOR TO SIDE WALL SUPPORT ANGLE BS 500A TO BS 500D RBL 24 WL 156 MADE FROM EXTRUSION BAC1496-777#7075T62 LOT#1466509-1 IAW SRM 51-40-05-0G-0 AND DWG# 143A7501 OK NTO TREAT AND PRIME; [04] VERIFIED CORRECTIVE ACTION ENTRY 3. OK TO TREAT AND PRIME GIVEN.; [05] APPLIED CHEMICAL CONVERSION COATING AND PRIMED FCB FLOOR TO SIDE WALL SUPPORT ANGLE BS 500A TO BS 500D RBL 24 WL 156 IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02 AND WILL BE INSTALLED WITH CUSTOMER MOC CARD# TTG8Q004EMB3; [06] VERIFIED CORRECTIVE ACTION ENTRY 5. CARD COMPLETE.
CORROSION FWD CARGO BAY AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE BS 500D LBL 25 WL 156 ; / [01] REMOVED DAMAGE ON FCB AFT BULKHEAD SUPPORT ANGLE P/N 143A9485-35 AT BS 500D; LBL 25; WL 156; AREA 1.2' X 1.2' X .026'. ORIGINAL MAT. THICKNESS .071' . FOUND TO BE OUT OF LIMITS IAW SRM 53-30-08-1A-1 STEP. 4.A.(2).<BR><BR>TOOL USED ID: ATS601 S/N: 87172291; [02] FCB AFT BULKHEAD SUPPORT ANGLE P/N 143A9485-35 AT BS 500D; LBL 25; WL 156 WILL BE ACCOMPLISHED ON C.C.TTG8Q0092WE0.; [03] VERIFIED CORRECTIVE ACTION ENTRIES 1 & 2. CARD COMPLETE.
CORROSION FWD CARGO BAY AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE BS 500D RBL 25 WL156 ; / [01] REMOVED DAMAGE ON FCB AFT BULKHEAD SUPPORT ANGLE P/N 143A9485-35 AT BS 500D; RBL 25; WL 156; AREA 1.2' X 1' X .026'. ORIGINAL MAT. THICKNESS .071' . FOUND TO BE OUT OF LIMITS IAW SRM 53-30-08-1A-1 STEP. 4.A.(2).; [02] FCB AFT BULKHEAD SUPPORT ANGLE P/N 143A9485-35 AT BS 500D; RBL 25; WL 156 WILL BE ACCOMPLISHED ON C.C.TTG8Q0092WE0.; [03] TOOL USED ID: ATS601 S/N: 87172291; [04] ADDED TOOL USED.; [05] VERIFIED CORRECTIVE ACTION ENTRIES 1-4. CARD COMPLETE.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT WL 153; RBL 23; STATIONS: 727+1; 727+14; 727A+6; 727A+10; 727B+2; 727B+6; 727C+6; 727C+10; 727C+14; AND 727D+2. ; / [01] REMOVED CORROSION ON FLOOR SIDEWALL SUPPORT AT WL153; STA 727+1; 727+14; 727A+6;727A+10;727B+2;727B+6;727C+10;727C+14; RBL 23 AND STA 727D+2; . STATION 727+14'; MEASURES: L= 1'; W=0.500'; D=0.012'.ORIGINAL THICKNESS= 0.040'; MATERIAL REMOVED=0.012'; REMAINING MATERIAL THICKNESS=0.028'. THE SIDEWALL SUPPORT IS OUT OF LIMITS.IAW. SRM 51-10-02; SRM53-00-53-1A-2 ALLOWABLE DAMAGE 2; STEP 4.A(2) (A). TOOL USED:MICROMETER. ID:ATS1671; DUE DATE:01/2022.; [02] VERIFIED CORROSION REMOVAL OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q0092WDW.; [04] VERIFIED WORK TO BE ACCOMPLISHED ON FAULT TTG8Q0092WDW
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT WL 153; LBL 23; STATIONS: 727E+14; 727E+18; 747+10; 767+1; 767+11; 767+14 AND WL 153; STA 727C+14 LBL 21; STA 727D+15 LBL 21; STA 747+3 LBL 21; ; AND STA 747+18 LBL 21. / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT DISCREPANCY AREA FOUND TO BE OUT LIMITS L=1.000' W=0.600' D=0.015 ORIGINAL THICKNESS 0.040' IAW SRM 53-00-53-1A-2 FIG 103 DATAIL C USED TOOL ID ATS 1671 DATE DUE 01/2022; [02] VERIFIED DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG.103; [03] THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q0092YBD; [04] VERIFIED WORK TO BE ACCOMPLISHED ON FAULT TTG8Q0092YBD
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT WL 153; RBL 23; STATIONS: 727D+4; 727D+6; 727D+14; 727D+16; 727D+18; 727E+2; 727E+6; 727E+10; 727E+14; AND AT WL 153; RBL 22; STATION 727E+2. ; / [01] REMOVED CORROSION ON FLOOR SIDEWALL SUPPORT AT WL153; STA 727D+4; 727D+6; 727D+14; 727D+16;727D+18;727E+2;727E+6;727E+10;727E+14; RBL 23 AND STA 727E+2; RBL 22. STATION 727E+10';RBL23; MEASURES: L= 1.300'; W=0.600'; D=0.011'.ORIGINAL THICKNESS= 0.040'; MATERIAL REMOVED=0.011'; REMAINING MATERIAL THICKNESS=0.029'. THE SIDEWALL SUPPORT IS OUT OF LIMITS.IAW. SRM 51-10-02; SRM53-00-53-1A-2 ALLOWABLE DAMAGE 2; STEP 4.A(2) (A). TOOL USED:MICROMETER. ID:ATS1671; DUE DATE:01/2022.; [02] VERIFIED CORROSION REMOVAL OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] THIS DISCREPANCY WILL ACCOMPLISHED ON CARD TTG8Q0092WDW.; [04] VERIFIED WORK TO BE ACCOMPLISHED ON FAULT TTG8Q0092WDW
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT WL 153; STA 727E+16 RBL 23; STA 727E+18 RBL 23; STA747+1 RBL 21; STA747+6 RBL 23; STA747+10 RBL 23. ; / [01] REMOVED CORROSION ON FLOOR SIDEWALL SUPPORT AT WL153; STA 727E+16; 727E+18; 747+6; 747+10; RBL 23 AND STA 747+1; RBL 21. STATION 747+10';RBL23; MEASURES: L= 1.400'; W=0.700'; D=0.014'.ORIGINAL THICKNESS= 0.040'; MATERIAL REMOVED=0.014'; REMAINING MATERIAL THICKNESS=0.026'. THE SIDEWALL SUPPORT IS OUT OF LIMITS.IAW. SRM 51-10-02; SRM53-00-53-1A-2 ALLOWABLE DAMAGE 2; STEP 4.A(2) (A). TOOL USED:MICROMETER. ID:ATS1671; DUE DATE:01/2022.; [02] VERIFIED CORROSION REMOVAL OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] REMOVED AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT WL153; BETWEEN BS727 TO BS767 RBL21; IAW SRM 51-40-02-0G-0.; [04] FABRICATED LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT FROM EXTRUSION ITEM:BAC1496-377#7075T62; LOT#5093799-1; AT BS727 TO BS767; RBL 21; WL153; IAW SRM 51-40-05-0G-0 AND DWG# 146A7500; OK TO CHEMICAL CONVERSION COATING AND PRIME.;
CORROSION ON AFT CARGO DOOR CUTOUT FWD SHIELD AT WL 153; STA 747+3 RBL 24; STA 747+9 RBL 22; STA 747+11 RBL 24; STA 747+15 RBL 24; STA 747+19 RBL 24. ; / [01] REMOVED CORROSION ON AFT CARGO DOOR CUTOUT FWD SHIELD AT WL 153 RBL 25 AND 747+3 TO 747+19 .<BR>PER REF SRM 51-10-02<BR><BR>THE STRUCTURAL ITEM DOES NOT HAVE ENTRIES IN ALLLOWABLE DAMAGE. THEREFORE ;THAT WILL BE REPAIRABLE BY REPLACEMENT PER REF SRM 51-10-02-0G STEP 9; [02] VERIFIED NO SRM LIMITS SPECIFIED FOR ACB DOOR CUTOUT FWD SHIELD; AND PART TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02; [03] REMOVED A.C.D CUTOUT FWD SHIELD PER SRM 51-40-02; [04] LOCATED AND DRILLED NEW A.C.D. CUTOUT FWD SHIELD P/N: 146A8127U12 PER SRM 51-40-05 AND DWG#146A0081 SH25 REV A. OK TO INSTALL; [05] INSPECTED ACTION 4; [06] INSTALLATION COMPLETED ON FAULT TTG8Q004EKJ7 STEP 62; [07] ITEM 6 STEP 62 ENTRY AN ERROR HAS TO BE 39; [08] VERIFIED THAT BOTH REMOVAL AND INSTALLATION OF ACB CUTOUT FWD SHIELD WAS ACCOMPLISHED ON FAULT TTG8Q004EKJ7
CORROSION ON AFT CARGO BAY DOOR SUB-THRESHOLD WEB AT WL 153; STA 787+12 RBL 25; STA 787+13 RBL 26; STA 787+17 TO 807+6 RBL 26; STA 807+7 TO STA 807+14 RBL 26; STA 827+2 TO STA 827+6 RBL 26. ; / [01] REMOVED CORROSION ON AFT CARGO BAY DOOR SUB-THRESHOLD WEB AT WL 153 FROM STA 787+12 TO 827+6 AND RBL 25 L=10 W=1.5. MATERIAL LOST IS MORE THAN 20% THEREFORE FOUND TO BE OUT OF LIMITS ORIGINAL MATERIAL THICKNESS IS .050'' REMAINING THICKNESS IS .030 PER REF SRM 53-60-15-1A-1; [02] REMOVED AFT CARGO BAY DOOR SUB-THRESHOLD WEB AT WL 153 PER REF SRM 51-40-02-0G; [03] VERIFIED CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1; [04] LOCATED AND DRILLED NEW SUB-THRESHOLD WEB ACB AT BS 797 TO BS 847 RBL 25 WL 153 IAW SRM 51-40-05-0G-0; [05] VERIFIED LOCATION AND DRILL UP OF SUB-THRESHOLD WEB PER SRM 51-40-05; [06] OK TO INSTALL NEW PART; [07] VERIFIED OK TO INSTALL NEW PART (STEP 6).; [08] INSTALLED NEW AFT CARGO BAY DOOR SUB-THRESHOLD WEB AT WL153; RBL26; BS707-BS847; IAW SRM 51-40-02-0G-0 AND DWG#146A8120; [09] VERIFIED INSTALLED NEW AFT CARGO BAY DOOR SUB-THRESHOLD WEB AT WL153; RBL26; BS707-BS847; IAW SRM 51-40-02-0G-0 AND DWG#146A8120.; [10] VERIFIED ALL STEPS COMPLETE.
CORROSION FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 400+6; +10; +14; +18 RBL 24 WL 156 ; / [01] REMOVED AND EVALUATED DAMAGE; [02] VERIFIED STEPS 1-4 COMPLETE. OUT OF LIMITS.; [03] FABRICATED LOCATED AND DRILLED NEW FCB FLOOR TO SIDEWALL SUPPORT BS 396 TO BS 420 RBL 24 WL 156 IAW SRM 51-40-05-0G-0 ; APPLIED A CHEMICAL CONVERSION COATING IAW SOPM 20-43-03 ; OK TO PRIME; [04] FABRICATED LOCATED AND DRILLED NEW FCB FLOOR TO SIDEWALL SUPPORT ; BS 396 TO BS 420 RBL 24 WL 156 ;MATERIAL USE BAC1496-444#7075T62 EXTRUSION LOT # 1466509-1 IAW SRM 51-40-05-0G-0 ; APPLIED A CHEMICAL CONVERSION COATING IAW SOPM 20-43-03 ; OK TO PRIME; [05] VERIFIED CORRECTIVE ACTION ENTRY 4. OK TO PRIME GIVEN; [06] PRIMED FCB FLOOR TO SIDE WALL SUPPORT ANGLE BS 396 TO BS 420 RBL 24 WL 156 IAW SOPM 20-41-02 AND WILL BE INSTALLED WITH CUSTOMER MOC CARD# TTG8Q004EMB3; [07] VERIFIED CORRECTIVE ACTION ENTRY 6. CARD COMPLETE.
CORROSION FWD CARGO BAY SUBTRESHOLD WEB BS 440 +8; +16; BS 460 +5; +7; +10; +15;+17; BS 480 +4 RBL 28 WL 156 ; / [01] REMOVED SUBTRESHOLD WEB LOCATED BTW BS 420 - BS 492.4 IAW SRM 51-40-02. REMOVED CORROSION ON FWD CARGO BAY SUBTRESHOLD WEB BS 460+5. MAX. MATERIAL LOSS L=1.' X W=0.5' X D=0.008' ORIGINAL THICKNESS IS 0.045'; FOUND OUT OF LIMITS REWORKED AREA IAW SRM 53-30-15-1A-1 PARAG 4.G.2(B) DETAIL G ; USED TOOL: ID=ATS1672; S/N:65092939; DUE DATE:03/2022; [02] VERIFIED CORROSION REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1; [03] RECEIVED SUBTHRESHOLD WEB ITEM 654A0003-58; LOT. 1471116. LOCATED AND DRILLED SUBTHRESHOLD WEB BTW BS 420 - BS 492; RBL 28 WL 156 . IAW SRM 51-40-05 DWG# 143A8330.; [04] INSPECTED ACTION 3; [05] FCB SUBTHRESHOLD WEB WILL BE INSTALLED WITH CUSTOMER MOC CARD # TTG8Q004EMB3; [06] VERIFIED CORRECTIVE ACTION ENTRY 5. CARD COMPLETE.
CORROSION FWD CARGO BAY AFT SHIELD BS 480 +17; BS 500 +14; +18 RBL 24 WL 156 ; / [01] REMOVED FWD CARGO BAY AFT SHIELD BS 492-500A RBL24 WL 156. IAW 51-40-02.NO FOUND ALOWABLE DAMAGE PART MUST BE REPLACED. IAW 51-10-02.; [02] VERIFIED FCB AFT SHIELD TO BE REPAIRED BY REPLACEMENT DUE TO NO SRM ALLOWABLE LIMITS; [03] LOCATED AND DRILLED NEW FCB AFT SHIELD BS 480 TO BS 500A RBL 24 WL 156 IAW SRM 51-40-05-0G-0; [04] FCB AFT SHIELD WILL BE INSTALLED ON CUSTOMER CARD #5330-E-16461-NG; [05] VERIFIED CORRECTIVE ACTION ITEMS 3 & 4. VERIFIED NEW FCB AFT SHIELD WILL BE INSTALLED ON FAULT TTG8Q004EMB3; JOB CARD STEP 44.
CORROSION FWD CARGO BAY FWD SHIELD BS 420 +5; +9; +12; +15 RBL 24 WL 156 ; / [01] REMOVED FWD CARGO BAY FWD SHIELD BS 420-440 RBL24 WL 156. IAW 51-40-02.NO FOUND ALOWABLE DAMAGE PART MUST BE REPLACED. IAW 51-10-02.; [02] VERIFIED FCB FWD SHIELD TO BE REPAIRED BY REPLACEMENT DUE TO NO SRM LIMITS; [03] LOCATED AND DRILLED NEW FCB FWD SHIELD IAW SRM 51-40-05 ;; [04] FCB NEW FWD SHIELD WILL BE INSTALLED ON CUSTOMER CARD #TTG8Q004EMB3; [05] UPDATED PARTS REMOVED / INSTALLED.; [06] ADDED P/N.; [07] VERIFIED LOCATED AND DRILLED NEW FCB FWD SHIELD IAW SRM 51-40-05 ;; [08] INSPECTION COMPLETE
CORROSION FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 420 +13; BS 440+2; +6; +10; +14 BS 460+ 6; +10;+14; BS 480 +6; +10 LBL 24 WL 156 ; / [01] REMOVED AND EVALUATED DAMAGE; [02] VERIFIED STEPS 1 -10 COMPLETE. OUT OF LIMITS.; [03] FABRICATED NEW SIDEWALL SUPPORT IAW SRM 51-40-05-0G-0 AND DRAWING#143A7501 LOT#1467644-1 BAC1496-444 7075-T6.<BR>FABRICATED SPLICE REPAIR IAW SRM 53-00-53-2R-6 REPAIR 6 PART 4D-4I; SRM 51-40-05-0G-0 LOT#1467644-1 BAC1496-444 7075-T6 <BR>OK TO TREAT AND PRIME; [04] VERIFIED CORRECTIVE ACTION ENTRY 3. OK TO TREAT AND PRIME GIVEN.; [05] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON REPAIR PARTS IAW SRM 51-20-1; SOPM 20-41-02.; [06] VERIFIED APPLICATION OF CONVERSION COATING AND PRIMER PER SRM 51-20-1; SOPM 20-41-02; [07] FCB L/H FLOOR TO SIDEWALL SUPPORT BS 395 TO BS 500D WILL BE INSTALLED ON FAULT TTG8Q004EMB3; [08] VERIFIED CORRECTIVE ACTION ITEM 7. NEW FCB L/H FLOOR TO SIDEWALL ANGLE WILL BE INTALLED ON FAULT TTG8Q004EMB3; JOB CARD STEP 42.
LEFT HAND VAPOR BARRIER IS CRACKED AT BS 663; LBL 40 TO 48. ; / [01] REMOVED 1EA PLACARD FROM FWD OB SURFACE (BAC27DHY0286)<BR><BR>IDENTIFIED MATERIAL OF LEFT HAND VAPOR BARRIER IAW SRM 57-10-10-0I-2 FIGURE 1-2; ITEM #4; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PARA 4.D(1)<BR><BR>14] CURED REPAIR; UNBAGGED AND LIGHTLY SANDED IAW SRM 51-70-04-2R-10 PARA 4.F&H; [REPAIRED CRACK IN LEFT HAND VAPOR BARRIER AT BS 663 LBL 40 TO LBL 48 IAW SRM 51-70-04-2R-10; [18] VERIFIED STEP 14 RII; [19] VERIFIED CORRECTIVE ACTION 17 REPAIR COMPLETE; [20] VERIFIED RII STEPS REPAIR COMPLETE
EMERGENCY EXIT LTS INOP AT ROWS 9 & 11 ABC & GROUND ILLUMINTION. / REMOVED & REPLACED EMERGENCY EXIT & GROUND ILLUMINATION LTS. BATT PACK AT STATION 727 L/H IAW AMM 33-51-06 OPS CHECK GOOD
LEFT ENGINE AFT STRUT FAIRING STIFFENER I/B BOLTS LOOSE WITH ELONGATED HOLES IN STIFFENER. STIFFENER LOCATED UNDER FWD END OF PANEL 434BL. / COMPLIED WITH EA 1-754-2497
L/H WING EMERGENCY EXIT EXTERIOR LIGHT INOP. / R&R LIGHT IAW AMM.
R2 DOOR EMERGENCY SLIDE LIGHT INOP. / R&R LAMP IAW AMM.
R1 DOOR EMERGENCY SLIDE LIGHT INOP. / R&R LAMP IAW AMM.
AFT CARGO BAY AT STA 867 BILGE AREA BETWEEN STR 26L AND 27L LOWER ANGLE FOR REMOVABLE BULKHEAD FRAME WORK IS CRACKED / REMOVED CRACKED ANGLE STA 867 BILGE ARA BETWEEN STR. 26 L/H AND 27 L/H AND INSTALLED NEW ANGLE ALL IAW SRM 51-40-02-0G-0 AND DWG:149A8012 REV A. A TG # A39458
AFT CARGO BAY BETWEEN STA 727D AND 727E BL 0 WL 148.8 TOP SIDE OF ANTENA IN CARGO BILGE IS COROODED AS MARKED / REMOVED CORROSION IN AFT CARGO BAY BETWEEN STA 727D AND 727E BLO TOP SIDE OF VHF ANTENNA DOUBLER IAW SRM 51-10-02-0G-0. VERIFIED MATERIAL LOSS; NO ALLOWABLE LIMITS IN THE SRM. INSTALLED NEW ANTENNA DOUBLER IAW SRM 51-40-02-0G-0 AND BOEING DRAWING 143A3280 REV - . INSTALLED VHF ANTENNA IAW AMM 23-12-11-400-802 AND AMM 23-12-00-730-801. BOND CHECK AND OPS CHECK GOOD. A66200; A98645; WN0494.
AFT CARGO DOOR AFT CORNER SCUFFPLATE P/N 146A8341-7 IS CRACKED / AFT CARGO DOOR AFT CORNER SCUFF PLATE P/N 146A8341-7 REPAIRED ON BACKSHOP W/O 40149-1600-0001. INSTALLED ON CUSTOMER CARD J753-140-00-02Y.
FORWARD WET AREA BETWEEN BS. 294.5 TO BS. 287, BL 0, AREA FLOOR STRUCTURE INTERCOSTAL CRACKED AT FORWARD FLOOR BOARD FASTENER HOLE. / R&R INTERCOSTAL IAW SRM AND DWG.
FWD CARGO COMP.FLOOR PANEL STRAP STA.500D CORRODED BOTTOM SIDE / NO LIMITS PUBLISHED FOR FLOOR PANEL STRAP STA 500D; THERE FOR PART IS OUT OF LIMITS. VERIFIED OF NEW PART AS PART NO 3 453A1611-9 A TG # WN0969 IAW DWG # 453A1600 REV -. STRAP INSTALLED WITH FLOOR PANEL 120CF ON CARD # JPANEL-121-CLOSE.
PASSENGER CABIN FORWARD WET AREA BETWEEN BS. 312 TO BS. 328, LBL 46 FLOOR SUPPORT INTERCOSTAL CRACKED AT FLOOR BOARD FASTENER HOLE. / R&R INTERCOSTAL IAW SRM AND DWG.
PASSENGER CABIN FORWARD WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS. 344 TO BS. 360, BL 0 AREA FORWARD FASTENER HOLE FOR FLOOR BOARD. / R&R INTERCOSTAL IAW SRM AND DWG.
L2 DOOR CREASE BEAM SILL CORRODED BETWEEN BS. 950 TO BS. 985, LBL 53. / REPAIRED CREASE BEAM IAW SRM.
PASSENGER COMPARTMENT SEAT TRACK CORRODED ON BASE BETWEEN BS. 810 TO BS. 827, LBL 45. / R&R SEAT TRACK IAW DWG & SRM.
AFT CARGO COMPARTMENT LABLED R/H INBD OF DOOR CAP STRIP ON AAR ID TAG; BOTTOM SKIN SURFACE IN SEVERAL AREAS THE LENGTH OF STRIP IS CORRODED / REMOVED CORROSION AT AFT CARGO CAP STRIP R/H I/B OF DOOR I.A.W SRM 51-10-02-0G-0. VERIFIED MATERIAL LOSS NO ALLOWABLE LIMITS FOUND IN THE SRM PART FOUND OUT OF LIMITS. REPLACED CAP STRIP I.A.W BOEING DWG 453A2600 ATAG # A50265
AFT CARGO COMPARTMENT FWD CAP STRIP ATTACHED TO FWD SIDE OF FLOOR PNL 140AF PART # (UNREADABLE) IS CORRODED IN SEVERAL AREAS AS MARKED BOTTOM SIDE / BLENDED & EVALUATED AFT CARGO COMPARTMENT FWD SIDE OF FLOOR PANEL 140 AF FWD CAP STRIP NO ALLOWABLE SRM LIMITS TO BE FOUND IN SRM 51-10-02-0G REPLACED CAPSTRIP & INSTALLED ON JPANEL 40146/1600/0015 ATAG# A66496 PN#453A2611-12
FWD CARGO COMPARTMENT; FWD CARGO DOOR CUTOUT SCUFF PLATE ASSY IS CRACKED AS MARKED / FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE WAS REPAIRED ON BACK SHOP W/O 40149/1400/0002 S/N 7451126 IAW B737 SRM 53.30.15.2R.1.
FWD CARGO DOOR; FWD CORNER SCUFF PLATE IS CRACKED / FWD CARGO COMPARTMENT FWD CORNER SUCFF PLATE WAS REPAIRED ON BACK SHOP W/O 40149/1400/0001 S/N 7451126 IAW B737 SRM 53.30.25.2R.1.
PASSENGER COMPARTMENT LBL 45 STA 841 TO STA 853 SEAT TRACK HAS CORROSION ON BASE. / REMOVED CORROSION FROM SEAT TRACK STA 841 TO 853 LBL LBL 45 IAW B737 SRM 51-10-02-0G-0. FOUND OUT OF LIMITS WITH .041' LOSS MAX ALLOWED .040' IAW B737 SRM 53-00-52-1A-1. REMOVED & REPLACED SEAT TRACK ON NRC Y131587. 146A5350-35
AFT CARGO COMPARTMENT L/H CENTER CAP STRIP BOTTOM SKIN SURFACE IN SEVERAL AREAS THE LENGTH OF STRIP IS CORRODED / REMOVED DAMAGE ON CAP STRIP LH CENTER IAW SRM 51-10-02-0G-0 NO PUBLISHED SRM LIMIT. (REPLACE CAP STRIP). RECIEVED NEW CAP STRIP P/N 453A2611-4 AND VERIFIED PER IPC 25-52-10-02 B737-700 SRM 51-10-02-0G-0 STEP 9.C. WN8950
AFT CARGO COMPARTMENT L/H AFT CAP STRIP BOTTOM SKIN SEVERAL AREAS LENGTH OF STRIP IS CORRODED AS MARKED / REMOVED CORROSION AT AFT CARGO L/H AFT CAP STRIP I.A.W 51-10-02-0F-0. VERIFIED MATERIAL LOSS. NO ALLOWABLE DAMAGE REMOVEL FOUND IN SRM. PART OUT OF LIMITS. REPLACED CAP STRIP I.A..W BOEING DWG 453A2600 REV:A ATAG# WN3012 AND 13T3171
AFT CARGO COMPARTMENT L/H MIDDLE CAP STRIP AND TRANSITION BOTTOM SKIN SURFACES IN SEVERAL AREAS THE LENGTH OF STRIP IS CORRODED AS MARKED / REMOVED CORROSION AT AFT CARGO L/H MIDDLE CAP STRIP I.A.W SRM 51-10-02-0G-0. VERIFIED MATERIAL LOSS NO ALLOWABLE LIMITS FOUND IN SRM PART OUT OF LIMITS REPLACED CAP STRIP IA.W BOEING DWG 453A2600 A-TAG # A7954106
AFT CARGO COMPARTMENT R/H FWD CAP STRIP BOTTOM SKIN SURFACE IN SEVERAL AREAS THE LENGTH OF STRIP IS CORRODED / EVALUATED CORROSION ON AFT CARGO COMPARTMENT R/H FWD CAP STRIP BOTTOM SURFACE. SRM HAS NO ALLOWABLE LIMITS IN THIS AREA. VERIFIED NEW CAP STRIP IAW IPC 25-52-10-02 AND BOEING DRAWING 453A2611 REV D.
R/H MAIN LANDING GEAR VAPOR BARRIER WEB HAD REPAIR DELAMINATED AT BS. 663. / REPAIRED WEB IAW SRM.
FORWARD UPPER EMERGENCY FLASHLIGHT INOP. R & R THE FLASHLIGHT IAW AMM.
L/H VAPOR BARRIER HAS A CRACK 14' LONG APPROX. AT LBL 30. (REF TO NRC 639575/001). AN INTERIM REPAIR WAS COMPLETED IAW SRM 57-10-10-1A-Z. THIS AICRAFT HAS SPLIT SCIMITAR CONFIGURATION. / USING 737 NG SRM 57-10-10 ALLOWABLE DAMAGE 2 IS APPLICABLE AND ACCEPATABLE FOR USE ON AIRCRAFT N 968 WN WITH THE SPLIT SCIMITAR CONFIGURATION. PER EA # 1-757-15791.
RT AFT FLOOR EGRESS STRIP DELAMINATED. R&R STRIP PER DWG.
R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE LIGHT IAW AMM.
L1 DOOR EMERGENCY EVAC SLIDE ASPIRATOR OUT OF POSITION. R&R SLIDE PER MT.
L2 DOOR EXIT SIGN MISSING RED ARROW. R&R SIGN IAW AMM.
LT PHOTOLUMINESCENT STRIP CRAZED BETWEEN BS 342 TO BS 955. R&R STRIP PER MM.
LT PHOTOLUMINESCENT STRIP CRAZED BETWEEN BS 328 TO BS 953. R&R STRIP PER MM.
RT MAIN LANDING GEAR WHEEL WELL VAPOR PANEL CRACKED AT BS 663, LBL 34. REPAIRED PANEL PER SRM.
AFT CARGO DOOR THRESHOLD AFT CORNER SCUFF PLATE HAS CORROSION ON LOWER SURFACE / AFT CARGO DOOR THRESHOLD AFT CORNER SCUFF PLATE WAS REPLACED ON NRC #G501366
AFT CARGO DOOR THRESHOLD FWD CORNER SCUFF PLATE HAS CORROSION ON LOWER SURFACE / AFT CARGO DOOR THRESHOLD FWD CORNER SCUFF PLATE WAS REPLACED ON NRC #G501367
AFT CARGO L/H TRANSITION ANGLE STA 727-827 HAS NUMEROUS AREAS OF CORROSION / REMOVED AND REPLACED AFT CARGO L/H TRANSITION ANGLE FROM STA 727-847 PER SRM 51-40-02.
AFT CARGO FLOOR PANEL ATTACH STRIP CORRODED AT BS 767, AROUND NUT PLATE HOLES. R&R STRIP PER SOPM.
SEAT TRACK CORRODED BETWEEN BS 725 TO 729, LBL 45.5. R & R THE SEAT TRACK IAW SRM.
CABIN FLOOR PANEL 241EF DELAMINATED / REMOVED AND REPLACED PER AMM. 53-21-00.
CABIN FLOOR PANEL 242 DF DENTED AND DELAMINATED / REMOVED AND REPLACED PANEL IAW M/M 53-21-00.
SEAT TRACK CORRODED BETWEEN BS 684 TO 687, LBL 45.5. R & R SEAT TRACK IAW SRM.
SEAT TRACK CORRODED BETWEEN BS 727A+7 - 727A+11, LBL 45.5. R & R THE SEAT TRACK IAW SRM.
CABIN FLOOR PANEL 241DF DELAMINATED / REMOVED AND REPLACED PER AMM. 53-21-00.
WAFFLE PLATE SEEN UNDER PANEL #551EB CRACKED. / REMOVED AND REPLACED WAFFLE PANEL PER SRM 51-40-02; REAPPLIED PROTECTIVE FINISH PER SRM 51-20-01.
L WING FLAP DEFLECTION CONTROL BEAM; UPPER FIXED PANEL ATTACH FASTENER HOLES ELONGATED.(MARKED) / REPAIRED IAW SRM 57-51-02-2R-1 AND EA1757-14498.
FORWARD BATTERY FAILED A TIME TEST. R & R THE BATTERY IAW AMM.
RIGHT MAIN LANDING GEAR WHEEL WELL BULKHEAD WEB CRACKED. REPAIRED THE BULKHEAD WEB IAW EA.
RIGHT CENTER BATTERY FAILED A TIME TEST. R & R THE BATTERY IAW AMM.
LT ENGINE LOWER PYLON AFT STRUT FAIRING AFT TE FAIRING ASSY. FWD WEB IS CRACKED. / REPLACED WEB PER AMM 51-40-02 IN CONNECTION WITH AMM 54-52-04
AFT BATTERY FAILED A TIME TEST. R & R THE BATTERY IAW AMM.
L1 DOOR EXIT SIGN MISSING RED ARROW. R & R SIGN ASSEMBLY IAW AMM.
R1 DOOR EXIT SIGN MISSING RED ARROW. R & R SIGN IAW AMM.
R2 DOOR EXIT LIGHT LENS BROKEN. R & R THE LIGHT IAW AMM.
OVERWING CEILING EMERGENCY EXIT SIGN DAMAGED. R&R LIGHT ASSEMBLY PER MM.
CEILING OVERWING EMERGENCY EXIT SIGN DAMAGED. R & R THE EMERGENCY LIGHT ASSEMBLY IAW MM.
OVERHEAD EMER EXIT SIGN LENS LOOSE. R & R LENS IAW MM.
RIGHT OVERWING EMER EXIT LIGHT COVER BROKEN. R & R LIGHT ASSEMBLY IAW MM.
RIGHT WW FWD SIDE FIBERGLASS PANEL CRACKED, BETWEEN WW & ACFT CARGO BAY. REPAIRED PANEL IAW EA.
RIGHT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER IAW MM.
LEFT PASSENGER COMPARTMENT FLOOR EGRESS LIGHT TRACK COVERS CRACKED BETWEEN ROW 1 TO ROW 23. REMOVED AND REPLACED COVERS PER AMM.
L1 DOOR EMERGENCY ESCAPE SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER M/M.