N461WN
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 | 2025-04-20 – 2025-04-20 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2025-04-20 – 2025-04-20 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
L1 DOOR SLIDE PRESSURE IN THE RED BAND. R & R L1 DOOR SLIDE IAW MT 725-61-06-FE
FIRST OFFICER SIDE OVERWING EXIT SIDEWALL LIGHT INOPERATIVE. R & R RT OVERWING EXIT LIGHT LAMP IAW AMM 33-21-00, OPS CHECKED GOOD.
FA SMELLED SOME ELECTRICAL ODOR CENTER CABIN ROW 7. C/W FUMES IN THE CABIN, NO DEFECTS NOTED IAW FIM 21-00 TASK 806. ACFT OK FOR SERVICE.
ELONGATED HOLE IN ACCESS PANEL 661BB AT TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB AT TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.
DELAMINATED TAIL CONE RIGHT SIDE ON EXTERNAL SKIN. REPAIRED TAIL CONE RIGHT SIDE ON EXTERNAL SKIN IAW SRM 51-70-04-2R-1, REPAIR 1.
CRACK SUPPORT ANGLE, TRAILING EDGE ORSS 280 AT RT WING. EVALUATED SUPPORT ANGLE AND NOT FOUND ON ALLOWABLE DAMAGE ON SRM IAW SRM-57-51-02-1A-1 ALLOWABLE DAMAGE 1. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02 AND DWG 115A6200 SHEET 10 REV - MEASUREMENT OF CRACK: 0.300".
CRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 AT RT WING. REPLACED CORRUGATED PLATE LOCATED ON TRAILING EDGE ORSS 261 AT RT WING IAW SRM 51-10-02-0G-O, PARAGRAPH 9; DRAWING 115A2001 SHEET 29, REV- AND SRM 51-40-02-0G-0. MEASUREMENT OF CRACK, REMOVED: L: 0.44F INCH.
CRACKED ANGLE, TRAILING EDGE ORSS 271 LT WING. REPLACED THE ANGLE IAW SRM 51-40-02, AND DRAWING 115A2930, SHEET 7, REV -.
CRACK CORRUGATED PLATE TRAILING EDGE IRSS 215 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 215 AT RT WING IAW SRM 51-40-02 AND DWG 115A2001, SHEET 30; REV A.
CRACKED SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-O2, & SRM 51-10-02, ITEM 9. MEASUREMENT OF CRACK IS 0.200".
CRACK ON AFT CORNER SCUFF PLATE IN FWD CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS 2 TO 7, FIGURE 203.
CRACKED CORRUGATED PLATE TRAILING EDGE IRSS 215 AT LT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02-0G-0, PARAGRAPH 9, DRAWING 115A2001, SHEET 30, REV A, & SRM 51-40-02-0G-0. MEASUREMENT OF CRACK: REMOVED: L: 0.519 INCH.
DELAMINATED ACCESS PANEL 431AT AT RT PYLON. PERFORMED VISUAL INSPECTION ON ACCESS PANEL 431AT AT RT PYLON AND NOT FOUND DAMAGE ON FIBER SKIN ONLY WAS FOUND SURFACE PROTECTION DETERIORATED IAW B737-700 NDT PART 1. 51-05-01 PARAGRAPH 3 AND RESTORED SURFACE PROTECTION IAW AMM 51-21-99-300-801.
CRACK SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND RBL 1 PASSENGER CABIN. INSTALLED SUPPORT ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE BS 695 AND RBL 1 PASSENGER CABIN IAW SRM 51-40-0G AND DRAWING 273A9110 SHEET 6 REV A.
CRACKED ACCESS PANEL 661BB AT TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB AT TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.
BROKEN PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA). REPLACED PHOTOLUMINESCENT STRIPS IAW DWG 33500007, REV 2, & SOPM 20-50-12, REV 58.
CRACK HOLE ACCESS PANEL 561BB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.
CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT RBL 43 BETWEEN STA 663 TO STA 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.312 IN. APPROX. PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK WEB AT RBL 43 BETWEEN BS 663 - 675 AT MAIN WHEEL WELL COMPARTMENT IAW SRM 53-40-51-2R-2 REPAIR 2.
CORROSION ON BRACKET FUEL BOOST PUMP REA LOCATED IRSS147 AT RT WING (2 E/A). REPLACED BRACKET FUEL BOOST PUMP AREA LOCATED IRSS147 AT RT WING IAW AMM 28-22-41-000-801 AND AMM 28-22-41-400-801.
DELAMINATED FLOOR PANEL 241EF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 241EF AT PASSENGER CABIN IAW SRM 53-00-50-2R-1 REPAIR 1.
AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-03.
FWD SERVICE DOOR GIRT BAR HOOKS ARE REPORTED LOOSE. ADJUSTED FORWARD SERVICE DOOR GIRT BAR HOOKS IN REFERENCE TO AIRCRAFT MAINTENANCE MANUAL 25-66-00-201-NG
#1 ENG AFT STRUT FAIRING O/B SIDE FWD STIFFENER HAS PULLED THRU HILOCS <[01]. REPLACED FRAME SECTION AS REQUIRED REF SRM 51-40-05 AND DWG313A2700.
LEFT AFT ENTRY DOOR SLIDE FELL OUT OF CONTAINER<[01] INSTALLED SLIDE PER M/M 25-66-01;AND MT#725-61-06-AE.NO DEFECTS NOTED.
L/H OUTBOARD AFT FLAP IS DELAMINATED ON INBD SIDE.<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22.;[02] C/W INSP. REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22.
SEAT 12F EMERGENCY EXIT LIGHT COVER DISPLACED<[01] RE SECURED EMERGENCY EXIT LIGHT COVER AT SEAT 12F; REF STANDARD INDUSTRY PRACTICES.
FORWARD CARGO BIN HAS A CRACK IN BIN FLOOR<[01] OK TO CONTINUE PER MEL 25-16-01 SP1<BR>FWD BAG PIT UNUSABLE;[02] R&R FWD CGO COMPARTMENT FLOOR PANEL PER AMM 25-52-10.
FSD UPPER EMERGENCY EXIT FWD BULB IS BURNT OUT 2023-652354<[01] REPLACED UPPER EMERGENCY EXIT FWD BULB IAW: B737-700 SWPM 20-84-13 AND PERFORMED OPERATIONAL TEST AMM 33-51-00-720-801 TEST IS OK.;[02] REPLACED UPPER EMERGENCY EXIT FWD BULB IAW: B737-700 SWPM 20-84-13 AND PERFORMED OPERATIONAL TEST AMM 33-51-00-720-801 TEST IS OK.
AFT SERVICE DOOR UPPER EMERGENCY EXIT LIGHT HAS BURNT OUT BULB 2023-652353<[01] REPLACED AFT SERVICE DOOR UPPER EMERGENCY EXIT LIGHT IAW: B737-700 SWPM 20-84-13 AND PERFORMED OPERATIONAL TEST AMM 33-51-00-720-801 TEST IS OK.;[02] REPLACED AFT SERVICE DOOR UPPER EMERGENCY EXIT LIGHT IAW: B737-700 SWPM 20-84-13 AND PERFORMED OPERATIONAL TEST AMM 33-51-00-720-801 TEST IS OK.
CORROSION RAIL NUT INTERNAL CAVITY LEADING EDGE OFSS 292 AT RT WING 2023-652286<[01] REPLACED RAIL NUT INTERNAL CAVITY LEADING EDGE OFSS 292 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 112A4402 SHEET 8 REV.B;[02] REPLACED RAIL NUT INTERNAL CAVITY LEADING EDGE OFSS 292 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 112A4402 SHEET 8 REV.B
CRACK ANGLE SLAT 1 INBOARD AUXILIARY SLAT TRACK AT LT WING 2023-652285<[01] REPLACED ANGLE SLAT 1 INBOARD AUXILIARY SLAT TRACK AT LT WING IAW B737-700 SRM 51-40-02;[02] REPLACED ANGLE SLAT 1 INBOARD AUXILIARY SLAT TRACK AT LT WING IAW B737-700 SRM 51-40-02
CRACK ON STRINGER 15L LOCATED AT BS 294.5 MORE 4 INCH AT FWD GALLEY AREA 2023-652267<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE: 15-FEB-24 WAS USED.;[02] REPAIRED STRINGER 15L LOCATED AT BS 294.5 MORE 4 INCH AT FWD GALLEY AREA IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 STEP 4.K THROUGH L AND TABLE 201 FIGURE 206 SHEETS 1 AND 2;[03] CORRECTED STEP 2: REPAIRED STRINGER 15L LOCATED AT BS 294.5 MORE 4 INCH AT FWD GALLEY AREA IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 STEP 4.K THROUGH L AND TABLE 201 FIGURE 206 SHEETS 1 AND 2. SEE INDIVIDUAL SIGN-OFFS BELOW.;[04] REPAIRED STRINGER 15L LOCATED AT BS 294.5 MORE 4 INCH AT FWD GALLEY AREA IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 STEP 4.K THROUGH L AND TABLE 201 FIGURE 206 SHEETS 1 AND 2. SEE INDIVIDUAL SIGN-OFFS BELOW.
CRACK SUPPORT ANGLE LOCATED BS867 AND BETWEEN STR2R/STR3R AT PASSENGER CABIN 2023-652137<[01] REPLACED SUPPORT ANGLE LOCATED BS867 AND BETWEEN STR2R/STR3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND #DWG:146A7901 SHEET: 58 REV:-.;[02] TASK COMPLETED
CRACK STRINGER 26L BS 540 FWD CARGO COMPARTMENT 2023-652104<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] TOOLS 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] REPAIRED STRINGER 26L BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND SRM 51-10-02 ITEM 9 . <BR>SEE INDIVIDUAL SIGN OFF BELOW;[05] CORRECTED STEP 4<BR>REPAIRED STRINGER 26L BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[06] CORRECTED STEP 4<BR>REPAIRED STRINGER 26L BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. RII SEE INDIVIDUAL SIGN OFF BELOW.
CRACK STRINGER 23R BS 540 FWD CARGO COMPARTMENT 2023-652105<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] TOOLS 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] REPAIRED STRINGER 23R LOCATED BS500D TO BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[05] CERTIFIED RII MAJOR REPAIR PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK STRINGER 25R BS 540 FWD CARGO COMPARTMENT 2023-652106<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] TOOLS 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] REPAIRED STRINGER 25R BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[05] CORRECTED STEP 4<BR>REPAIRED STRINGER 25R 500C BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[06] REPAIRED STRINGER 25R BETWEEN STA 500C AND <BR> BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.<BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGN OFF BELOW
CRACK FRAME BS 259.5 AND STRINGER 8R AT PASSENGER CABIN 2023-652122<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC600D; S/N: 220273012; DUE DATE: 17-DEC-23.;[02] REPAIRED FRAME BS 259.5 AND BTW STR 8R TO STR 12R AT PASSENGER CABIN IAW EA 23-153-03257 AND 23-153-03257-WIP1. SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] REPAIRED FRAME BS 259.5 AND BTW STR 8R TO STR 12R AT PASSENGER CABIN IAW EA 23-153-03257 AND 23-153-03257-WIP1. RII. SEE INDIVIDUAL SIGN-OFFS BELOW.
CRACK STIFFENER FLOOR STRUCTURE LOCATED BS947.5 AND STR26L AT AFT CARGO COMPARTMENT 2023-652097<[01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS947.5 AND STR26L AT AFT CARGO IWA B737-700 #DWG:186A8103 SHEET: 9 REV:- AND SRM 51-40-02 AND 51-10-02 ÿ½TEM 9.<BR>SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS947.5 AND STR26L AT AFT CARGO IWA B737-700 #DWG:149A8103 SHEET: 9 REV:- AND SRM 51-40-02 AND 51-10-02 ÿ½TEM 9.<BR>SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS947.5 AND STR26L AT AFT CARGO IWA B737-700 #DWG:149A8103 SHEET: 9 REV:- AND SRM 51-40-02 AND 51-10-02 ÿ½TEM 9.<BR>SEE INDIVIDUAL SIGNOFF BELOW
CORROSION WEB LOCATED BTW BS727A TO BS727B AND RBL3.0 WL148.5 AT AFT CARGO COMPARTMENT 2023-652092<[01] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 221859911; DUE DATE: 07-NOV-23.;[02] EVALUATED REWORK AREA WEB LOCATED BTW BS727A TO BS727B AND RBL3.0 WL148.5 AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2; ITEM 4.C(B)(1); FIGURE 103 DETAIL E.. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] EVALUATED REWORK AREA WEB LOCATED BTW BS727A TO BS727B AND RBL3.0 WL148.5 AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2; ITEM 4.C(B)(1); FIGURE 103 DETAIL E.. SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK STRINGER 26R BS 540 FWD CARGO COMPARTMENT 2023-652107<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] TOOLS 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] REPAIRED STRINGER 26R LOCATED BS500D TO BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPAIRED STRINGER 26R LOCATED BS500D TO BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.<BR>CERTIFIED AS RII
CRACK STRINGER 23L BS 540 FWD CARGO COMPARTMENT 2023-652103<[01] TOOL USED P/N: 45MG; S/N: 221861811; CAL DUE: 08-NOV-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] TOOLS 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] REPAIRED STRINGER 23L LOCATED BS500D TO BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPAIRED STRINGER 23L LOCATED BS500D TO BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII
CRACK STUB FRAME ON BS 294.5 UPPER POSITION RH SIDE AT FWD GALLEY AND LAV 2023-652064 CRACK STUB FRAME RH SIDE ON BS 294.5 UPPER POSITION FWD GALLEY AND LAV<[01] REPLACED STUB FRAME LOC BS 294.5 UPPER POSITION RH SIDE AT FWD GALLEY AND LAV. IAW B737-700 51-40-02 AND DWG 141A8370 SHEET 9 REV D .SEE INDIVIDUAL SING OFF BELOW;[02] REPLACED STUB FRAME LOC BS 294.5 UPPER POSITION RH SIDE AT FWD GALLEY AND LAV. IAW B737-700 51-40-02 AND DWG 141A8370 SHEET 9 REV D .SEE INDIVIDUAL SING OFF BELOW;[03] CORRECTED STEP 2 (MISSING RII)<BR>REPLACED STUB FRAME LOC BS 294.5 UPPER POSITION RH SIDE AT FWD GALLEY AND LAV. IAW B737-700 51-40-02 AND DWG 141A8370 SHEET 9 REV D .SEE INDIVIDUAL SING OFF BELOW<BR>RII
CRACK FRAME LOCATED BS 727D BTW STRINGER 8L TO STRINGER 9L AT PASSENGER CABIN 2023-652063<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23.;[02] PERFORMED VISUAL INSPECTION ON AREA AND FOUND ONLY DIRTY AND PERFORMED CLEAN IAW SOPM 20-30-03 HFEC WAS DONE AND NOT FOUND CRACK INDICATION IAW B737-700 SRM 51-10-02.;[03] CORRECTED STEP 2: PERFORMED VISUAL INSPECTION ON AREA AND FOUND ONLY DIRTY AND PERFORMED CLEAN IAW SOPM 20-30-03 HFEC WAS DONE AND NOT FOUND CRACK INDICATION IAW B737-700 SRM 51-10-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[04] TASK CARD COMPLETE.
CORROSION WEB LOCATED BTW BS727A TO BS727B AND LBL3.0 WL148.5 AT AFT CARGO COMPARTMENT 2023-652091<[01] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 221859911; DUE DATE: 07-NOV-23.;[02] EVALUATED REWORK AREA WEB LOCATED BTW BS727A TO BS727B AND LBL3.0 WL148.5 AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2; ITEM 4.C(B)(1); FIGURE 103 DETAIL E.. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] EVALUATED REWORK AREA WEB LOCATED BTW BS727A TO BS727B AND LBL3.0 WL148.5 AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2; ITEM 4.C(B)(1); FIGURE 103 DETAIL E.. SEE INDIVIDUAL SIGNOFFS BELOW.
INOP LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA (2 EA) 2023-651813<[01] REPLACED LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA (2 EA) IAW: B737-700 AMM 33-51-06-960-805 TEST IS OK;[02] REPLACED LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA (2 EA) IAW: B737-700 AMM 33-51-06-960-805 TEST IS OK
CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 7 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT 2023-652085<[01] REPLACED ANGLE LOCATED BS907 PLUS 7 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 17 REV D. PART USED: 147A7221Y32ATSMRO P.O: 2023 248205; SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE LOCATED BS907 PLUS 7 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 17 REV D. PART USED: 147A7221Y32ATSMRO P.O: 2023 248205; SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 11 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT 2023-652086<[01] REPLACED ANGLE LOCATED BS907 PLUS 11 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 17 REV D. PART USED: 147A7221Y32ATSMRO P.O: 2023 248209; SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE LOCATED BS907 PLUS 11 INCHES AND BTW STR25R TO STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 17 REV D. PART USED: 147A7221Y32ATSMRO P.O: 2023 248209; SEE INDIVIDUAL SIGN OFF BELOW.
CRACK FRAME ON BS 907 BTW STR25R AND STR26R AFT CARGO COMPARTMENT 2023-652087<[01] REPLACED FRAME LOC. ON BS 907 BTW STR25R AND STR25L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A1007 SHEET 55 REV.-; 147A1007 SHEET 42 REV.D; 147A7500 SHEET 19 REV.-; 147A0002 SHEET 85 REV.-; 147A7500 SHEET 1 REV.B. SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED FRAME LOC. ON BS 907 BTW STR24R AND STR24L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A1007 SHEET 55 REV.-; 147A1007 SHEET 42 REV.D; 147A7500 SHEET 19 REV.-; 147A0002 SHEET 85 REV.-; 147A7500 SHEET 1 REV.B. SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED STEP 2 COMPLETED<BR>RII
CRACK ANGLE - SUPPORT LOCATED BS867 AND BTW STR26L / STR27L AFT CARGO COMPARTMENT 2023-652088<[01] REPLACED ANGLE - SUPPORT LOCATED BS867 AND BTW STR26L / STR27L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 <BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK TRACK RBBL 13.84 LOCATED BS727E AFT CARGO COMPARTMENT 2023-652089<[01] REPAIRED CARGO TRACK RBBL 13.84 LOCATED BS727E AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4. SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED ACTION 1<BR> REPAIRED CARGO TRACK RBBL 13.84 LOCATED BS727D TO BS 767 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4. SEE INDIVIDUAL SIGN OFF BELOW;[03] JOB COMPLETED AND CERTIFIED RII.
CRACK ON TRACK LBL 17.24 LOCATED BS727E AT AFT CARGO COMPARTMENT 2023-652090<[01] REPAIRED CARGO TRACK LOCATED AT LBL 17.24 BETWEEN STA 727D TO STA 767 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPAIRED CARGO TRACK LOCATED AT LBL 17.24 BETWEEN STA 727D TO STA 767 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4. RII;SEE INDIVIDUAL SIGN OFF BELOW.
CRACK WEB INTERCOSTAL LOCATED BTW 294.5 TO BS303.9 AND STR15L AT PASSENGER CABIN 2023-652065<[01] REPAIRED WEB INTERCOSTAL LOCATED BTW 294.5 TO BS303.9 AND STR15L AT PASSENGER CABIN IAW EA 23-153-03218-WIP1.;[02] REPAIRED WEB INTERCOSTAL LOCATED BTW 294.5 TO BS303.9 AND STR15L AT PASSENGER CABIN IAW EA 23-153-03218-WIP1.RII CERTIFIED
CRACK TIE CLIP LOCATED BS 277 STRINGER 10R CENTER SECTION 2023-652066<[01] REPLACED NEW TIE CLIP LOCATED BS 277 STRINGER 10R CENTER SECTION I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ÿ½TEM 9 AND #DWG: 141A1110 SHEET: 17 REV:-.<BR>SEE INDIVIDUAL SIGNOFF BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNOFF BELOW.
CRACK ON BEAR STRAP LOCATED BTW BS291.5 TO 294.5 STR8R AND STR9R PASSENGER CABIN 2023-652067<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] REPAIRED BY 737-700 SRM 53-10-01-2R-6 AND EA M-21-153-03542. SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] REPAIRED BY 737-700 SRM 53-10-01-2R-6 AND EA M-21-153-03542. SEE INDIVIDUAL SIGN-OFFS BELOW.<BR>AS RII
CRACK BS 294.5 ANGLE - SUPPORT AND STR13L FWD GALLEY AND LAV 2023-652068<[01] REPLACED ANGLE-SUPPORT LOC BS 294.5 STR 13L FWD GALLEY IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A1311 REV C SHEET 1 <BR>SEE INDIVIDUAL SIGNS OFF BELOW;[02] CERTIFIED AS RII <BR>REPLACED ANGLE-SUPPORT LOC BS 294.5 STR 13L FWD GALLEY IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A1311 REV C SHEET 1 <BR>SEE INDIVIDUAL SIGNS OFF BELOW
CRACK INNER CHORD LOCATED BS303.9 AT LEVEL STR 17L AT PASSENGER CABIN 2023-652071<[01] REPLACED NEW INNER CHORD LOCATED BS303.9 AT LEVEL STR 17L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 7 REV - SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1.<BR>REPLACED INNER CHORD LOCATED BS303.9 AT LEVEL STR 17L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 7 REV - SEE INDIVIDUAL SIGN-OFF BELOW;[03] CORRECTED STEP 1.<BR>REPLACED INNER CHORD LOCATED BS303.9 AT LEVEL STR 17L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 7 REV - RII SEE INDIVIDUAL SIGN-OFF BELOW
CRACK ANGLE LOCATED BTW BS291.5 TO BS294.5 AT LEVEL STR17R AT PASSENGER CABIN 2023-652072<[01] REPLACED ANGLE LOCATED BTW BS291.5 TO BS294.5 AT LEVEL STR17R AT PASSENGER CABIN I.A.W B737-700 #DWG: 141A8310 SHEET: 25 REV:- AND SRM 51-10-02 AND 51-10-02 ITEM 9.<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.
DETERIORATED ENTRY DOOR COVER PLASTIC GIRTBAR FITTING AT FWD GALLEY AREA (2 EA) 2023-652058<[01] REPLACED ENTRY DOOR COVER PLASTIC GIRTBAR FITTING AT FWD GALLEY AREA (2 EA) IAW B737-700 AMM 25-66-02-400-801 STEP 3.A THRU 3.D ITEM (1) (H);[02] CERTIFIED WORK PERFORMED.
WEAR ON ENTRY DOOR BASE GIRT BART FITTING AT FWD GALLEY AREA (2 EA) 2023-652057<[01] REPLACED ON ENTRY DOOR BASE GIRT BART FITTING AT FWD GALLEY AREA (2 EA) IAW B737-700 AMM 25-66-02-400-801 STEP 3A THRU 3.D ITEM (1) (G).;[02] CERTIFIED WORK PERFORMED.
DELAMINATED ACCESS PANEL 193B WING TO BODY FAIRING EXTERNAL SKIN AFT LEFT CORNER AT LOWER FUSELAGE 2023-652045<[01] TOOL USED CALIPER P/N: 700-113-10; S/N 0033174; DUE DATE: 12-MAR-24.;[02] HOT BONDER P/N HCS9200B-AV; S/N 18196127; DUE DATE: 22-JAN-24.;[03] TOOL USED SCALE P/N 91847 S/N AE-409316 DUE DATE: 12-JUN-24.;[04] TOOL USED HOT BONDER P/N HCS9200B-AV; S/N 18196127; DUE DATE: 22-JAN-24.;[05] TOOL USED: UT EQUIPMENT P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 24-JAN-24;[06] REPAIRED ACCESS PANEL 193B WING TO BODY FAIRING EXTERNAL SKIN AFT LEFT CORNER AT LOWER FUSELAGE I.A.W. B737-700 SRM 53-40-70-2R-1 REPAIR 1 PARAGRAPH 4.B(2) TABLE 202. AND B737-700 SRM 51-70-04-2R-6 REPAIR 6 SEE INDIVIDUAL SIGN OFFS BELOW.;[07] JOB COMPLETED.
CORROSION CREASE BEAM LOCATED BS 639 LBL 64 WL 208.1 AT PASSENGER CABIN 2023-652027<[01] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 45 MG; S/N: 232017609; DUE DATE: 22-SEP-24.;[02] REPLACED CREASE BEAM SECTION LOC BTW BS616 + 12? TO BS 639 +9 ? LBL 64 WL 208.1 AT PASSENGER CABIN I.A.W. B737-700 DWG 144A5901 SHEET 36 REV '-' AND B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] REJECT STEP 8. TOOL MARK ON CREASE BEAM WEB RIVETS LOC BTW BS 639 LBL 64 WL 208.1 AT PASSENGER CABIN (3 EA. FAULT RAISED TTG8Q00PDDYL.;[04] CORRECTED STEP 2<BR>REPLACED CREASE BEAM SECTION LOC BTW BS616 + 12? TO BS 639 +9 ? LBL 64 WL 208.1 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 144A5901 SHEET 36 REV '-'. SEE INDIVIDUAL SIGN-OFFS BELOW.;[05] TASK CARD COMPLETED <BR>REPLACED CREASE BEAM SECTION LOC BTW BS616 + 12? TO BS 639 +9 ? LBL 64 WL 208.1 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 144A5901 SHEET 36 REV '-'. SEE INDIVIDUAL SIGN-OFFS BELOW.<BR>RII
CRACK ANGLE - CLIP LOCATED BS400 AND STR26R FWD CARGO COMPARTMENT 2023-652013<[01] REPLACED ANGLE - CLIP AND LOCATED BS400 AND STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 REV: B SHEET 2. SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED ANGLE - CLIP AND LOCATED BS400 AND STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 REV: B SHEET 2. <BR>SEE INDIVIDUAL SIGNOFFS BELOW
CRACK ANGLE - CLIP LOCATED BS500A AND STR26L FWD CARGO COMPARTMENT 2023-652015<[01] REPLACED ANGLE - CLIP LOCATED BS500A AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 207 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED STEP 1 COMPLETED
CRACK ANGLE - CLIP LOCATED BS500C AND STR26L FWD CARGO COMPARTMENT 2023-652016<[01] REPLACED ANGLE - CLIP LOCATED BS500C AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 207 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED STEP 1 COMPLETED
CRACK ANGLE LOCATED BS 695 LBL 24.75 AT CENTER WING BOX 2023-652022<[01] 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.;[02] REPLACED ANGLE LOCATED BS 695 LBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 273A9110 SHEET 6; REV. A<BR>SEE INDIVIDUAL SIGNSOFF BELOW;[03] REPLACED ANGLE LOCATED BS 695 LBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 273A9110 SHEET 6; REV. A<BR>SEE INDIVIDUAL SIGNSOFF BELOW
CRACK ON ANGLE LOCATED BS727B AREA CEILING PANEL LH SIDE AFT CARGO COMPARTMENT 2023-652023<[01] REPLACED ANGLE LOCATED LOCATED AT CEILING UPPER POSITION LH SIDE BETWEEN BS727A TO BS747 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 149A9490 REV- .SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED ANGLE LOCATED LOCATED AT CEILING UPPER POSITION LH SIDE BETWEEN BS727A TO BS747 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 149A9490 REV- .FOR OVERHEAT SENSING ELEMENT INSTALATION AND OPERATIONAL SEE TTG8Q00PLF80.SEE INDIVIDUAL SIGNOFF BELOW
CRACK ANGLE LOCATED BS 695 RBL 24.75 AT CENTER WING BOX 2023-652025<[01] 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.;[02] REPLACED ANGLE LOCATED BS 695 RBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-05; SRM 51-10-02 IITEM 9 AND DWG 273A9110 REV A SHEET 6 <BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[03] REPLACED ANGLE LOCATED BS 695 RBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-05; SRM 51-10-02 IITEM 9 AND DWG 273A9110 REV A SHEET 6 <BR>SEE INDIVIDUAL SIGNSOFF BELOW.
CRACK ANGLE LOCATED BS 695 BL0 LH SIDE AT CENTER WING BOX 2023-652024<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER: P/N: 38615K71; S/N: AE-40585; DUE DATE: 22-DEC-23.;[02] REPLACED ANGLE LOCATED BS 695 BLO LH SIDE AT CENTER<BR>WING BOX IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND<BR>DWG DWG 273A9110 SHEFT 6. REV. A;[03] CORRECTED STEP 2<BR>REPLACED ANGLE LOCATED BS 695 BL0 LH SIDE AT CENTER<BR>WING BOX IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND<BR>DWG DWG 273A9110 SHEFT 6. REV. A<BR>SEE INDIVIDUAL SIGNSOFF BELOW;[04] REPLACED ANGLE LOCATED BS 695 BL0 LH SIDE AT CENTER<BR>WING BOX IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND<BR>DWG DWG 273A9110 SHEFT 6. REV. A<BR>SEE INDIVIDUAL SIGNSOFF BELOW
CRACK ANGLE - CLIP LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT 2023-652014<[01] REPLACED ANGLE - CLIP LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 143A7505 SHEET 9 REV. A;[02] CORRECTED STEP 1<BR>REPLACED ANGLE - CLIP LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 143A7505 SHEET 9 REV. A SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED STEP 2 COMPLETED
CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2023-651997<[01] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ÿ½TEM 9 AND DWG: 143A9481 SHEET 2 REV A;[02] CORRECTED STEP 1<BR>REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ÿ½TEM 9 AND DWG: 143A9481 SHEET 2 REV A. SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 2<BR>REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ÿ½TEM 9 AND DWG: 143A7902 SHEET 174 REV -SEE INDIVIDUAL SIGN OFF BELOW;[04] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ÿ½TEM 9 AND DWG: 143A7902 SHEET 174 REV -SEE INDIVIDUAL SIGN OFF BELOW<BR>AS RII
CRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023-651921<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30;S/N:B22394220;DUE DATE:22-AUG-24.;[02] TOOL USED RADIOMETER PN. XRP-3000; SN. 1753759; DUE DATE. 12-APR-24;[03] REPAIRED THE AFT CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B. STEPS ( 2 ) TO ( 7 ) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[04] TASK COMPLETED.
CRACK ANGLE LOCATED BS663.75 AND RBL6.14 WL 173.5 AT CENTER WING BOX 2023-651802<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24.;[02] REPLACED REPAIR ANGLE LOCATED BS663.75 AND RBL6.14 WL 173.5 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #111A1000 SHEET 139 REV - .SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED STEP 2 COMPLETED <BR>RII
CRACK SLAT 8 LOWER SKIN LOCATED SLAT STATION 451.97 AT RT WING 2023-651791<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138003; DUE DATE: 27-MAR-24;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X1693P030456; DUE DATE: 12 MAR 24.;[03] PERFORMED PERMANENT REPAIR ON SLAT 8 LOWER SKIN LOCATED SLAT STATION 451.97 AT RT WING IAW B737-700 SRM 57-42-01-2R-8. REPAIR 8 AND SRM 51-40-02.SEE INDIVIDUAL SIGN OFF BELLOW.;[04] PERFORMED PERMANENT REPAIR ON SLAT 8 LOWER SKIN LOCATED SLAT STATION 451.97 AT RT WING IAW B737-700 SRM 57-42-01-2R-8. REPAIR 8 AND SRM 51-40-02.SEE INDIVIDUAL SIGN OFF BELLOW. COMPLETE TASK CERTIFIED
CORROSION FLOOR STRAP LOC BS 787 PLUS 6 INCHES AND BTW STR 25R TO STR 26R AT AFT CARGO COMPARTMENT 2023-651778<[01] REPLACED STRAP LOC BS 787 PLUS 6 INCHES AND BTW STR 25R TO STR 26R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9.;[02] COMPLETE TASK CERTIFIED
R1 DOOR SLIDE BRACKET LOOSE<[01] RESECURED R1 DOOR GIRT BAR BRACKET; OPERATES NORMAL PER AMM 25-66-01.
FWD SERVICE DOOR GIRT BAR CLIP INOP.<[01] REPLACED DAMAGED FASTENER PER SRM 51-40-02.
AFT ENTRY DOOR (L2) EXTERIOR EMERGENCY LIGHT INOP<[01] DISCONNECTED WIRING FROM LIGHT ASSY ON AFT ENTRY DOOR EXTERIOR REF AMM 33-51-04.;[02] REPLACED L2 DOOR SLIDE EMERGENCY LIGHT SOCKET AND CONTACT PER AMM SIP. OPS CHECK GOOD AT THIS TIME.
AFT ENTRY DOOR (L2) EXTERIOR EMERGENCY LIGHT INOP<[01] DISCONNECTED WIRING FROM LIGHT ASSY ON AFT ENTRY DOOR EXTERIOR REF AMM 33-51-04.;[02] REPLACED L2 DOOR SLIDE EMERGENCY LIGHT SOCKET AND CONTACT PER AMM SIP. OPS CHECK GOOD AT THIS TIME.
FORWARD MEGAPHONE INOP. / [01] R/R BATTERIES IAW AMM 25-64-00. MEGAPHONE OPS NORMAL. A/C OK FOR SERVICE.
#1 WINDSHIELD (FWD CAPT.) CRACKED / [01] R&R'D L1 WINDOW; C/W OP'S CKS; LEAK CK; NO DEFECTS NOTED IAW MM 56-11-11 REF LG #2048731 FOR HGS UPGRADE
ROW 12 R EXIT LT LENS FELL OFF / [01] RE INSTALLED LENS PER AMM 33-51-01
R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. ; / [01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF. B737 AMM 33-51-04-960-801. TEST OK; [02] VERIFIED STEP 1.
L2 DOOR EMERGENCY EXIT SIGN LIGHT INOP. ; / [01] FOUND CONNECTORS LOOSED AND RECONNECTED AT L2 DOOR EMERGENCY EXIT SIGN LIGHT ; OPERATIONAL CHECK FOUND NORMAL AMM 33-51-01-960-802.; [02] C/W
PANEL 242VF DELAMINATED ; / [01] CLEANED AND PREPARED FOR REPAIR FIBERGLASS AT ;FLOOR PANEL 242VF AS PER B737-700 SRM 53-00-50-2R-7; [02] VERIFIED CLEANING AND OK TO INSTALL REPAIR.; [03] REPAIRED DELAMINATION ; AT FLOOR PANEL 242VF AS PER B737-700 SRM 53-00-50-2R-7; [04] VERIFIED COMPLETED; [05] CLEANED; PREPARED FOR REPAIR THE FIBERGLASS; REPAIRED AT FLOOR PANEL 242VF AS PER B737-700 SRM 53-00-50-2R-7 MATERIAL USED PO;1711677PO;1150387 PO;1713932
CRACKED INTERCOSTAL AT STR 25R AND BETWEEN BS927 AND 947.5. AFT CARGO. ; CRACKED INTERCOSTAL AT STR 25R AND ETWEEN BS927 AND 947.5. AFT CARGO. / [01] REMOVED CRACKED INTERCOSTAL AT AFT CARGO STR 25-R BETWEEN STA 927 TO STA 947.5 IAW B 737-7 SRM 51-40-02-0G-0; [02] VERIFIED REMOVAL OF INTERCOSTAL.; [03] INSTALLED NEW INTERCOSTAL AT AFT CARGO R/H FROM STA 927 TO STA 947.5 STR 25R AS PER B737-700 SRM 51-40-02-0G-0; [04] REMOVED AND REPLACED AFT CARGO INTERCOSTAL FROM STA 927 TO STA 947.5 STR 25R AS PER B737-700 SRM 51-40-02-0G-0; [05] VERIFIED STEPS 3 AND 4...; [06] LATE ENTRY RII<BR>RII OK TO INSTALL.<BR>RII VERIFIED INSTALLATION.
CORROSION SPOTS ON AFT CARGO AFT LKHEAD LOWER ANGLE PNL SPPORT. CORROSION IS OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AFT CARGO AFT BULK HEAD SUPPORT ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW AFT CARGO AFT BULKHEAD LOWER ANGLE IAW SRM 51-40-05-0G-0. INSTALLED NEW AFT CARGO AFT BULKHEAD LOWER ANGLE IAW SRM 51-40-02-0G-0.
CORROSION AT FWD CABIN WET AREA FLOOR SUPPORT BEAM = @ LBL14 AND STA 312 ; / [01] REMOVED CORROSION AT MAIN CABIN FWD WET AREA STA 312 & LBL 14 AS PER SRM 51-10-02-0G-0.; [02] PERFORMED UT THICKNESS ON REWORKED AREA IAW NDTM PART 4; 51-00-00 PROCEDURE 3. MINIMUM FOUND :0.067'.<BR>[27MG ; B/C 172139 ; CALIB.DUE-04/22]; [03] CHECK LIMITS ORIGINAL MATERIAL 0.125' MATERIAL LOST 0.058' MATERIAL REMAINING 0.067' FOUND OUT OF LIMITS AS PER SRM 53-10-51-1A-1 FIGURE 105 DETAIL B.; [04] LATE ENTRY INSTALLED PROTECTION OF EWIS AT MAIN CABIN FROM STA 294.5 TO 328 BETWEEN LBL 40 AND RBL 20 AS PER AMM 20-60-07-913-801.; [05] VERIFIED STEP 3; 4; [06] LATE ENTRY VERIFIED STEP 1; [07] VERIFIED ALL WORK ACCOMPLISHED ON REPLACEME
SUPPLEMENTAL INFORMATION: CORROSION ** FWD CABIN WT AREA FLOOR SUPPORT ANGLE LBL 12 BETWEEN STA 312 AND 328 MKD DOT ; / [01] REMOVED FLOOR SUPPORT ANGLE AT FWD CABIN LBL 12 BETWEEN STA 312 AND STA 328 PER BOEING 737-700 SRM 51-40-02-0G-0.; [02] FLOOR SUPPORT ANGLE FOUND OUT OF LIMITS AS PER B737-700 SRM 53-10-51-1A-1; [03] INSTALLED NEW FLOOR SUPPORT ANGLE AT LBL 12 BETWEEN STA 312 AND STA 328 AS PER B737-700 SRM 51-40-02-0G-0 / DRWG # 141A5400 .; [04] VERIFIED INSTALLED NEW FLOOR SUPPORT ANGLE AT LBL 12 BETWEEN STA 312 AND STA 328 <BR>LATE ENTRY: OK TO INSTALL
SUPPLEMENTAL INFORMATION: CORROSION ** AT FWD WET AREA FLOOR SUPPORT ANGLE LBL12 BETWEEN STA 291.5 AND 312 ; / [01] PARTIALLY REMOVED FLOOR SUPPORT AT FWD CABIN WET AREA LBL 12 BETWEEN STA 294 AND STA 312 PER BOEING 737-700 SRM 51-40-02-0G-0.; [02] COMPLETED REMOVAL OF FLOOR SUPPORT ANGLE LBL 12 BETWEEN STA 291.5 AND 312 AS PER SRM 51-40-02-0G-0.; [03] LOCATED AND DRILLED FLOOR SUPPORT ANGLE REF B-737-700 SRM 51-40-05-0G-0; [04] VERIFIED REMOVAL OF FLOOR SUPPORT AND LOCATION AND DRILL OF NEW ONE.<BR>OK TO INSTALL; [05] INSTALLED FLOOR SUPPORT AT FWD WET ARE STA 291.5 TO STA 312 LBL 12 REFB-737-700-SRM 51-40-02; LATE ENTRY TREATED & PRIMER REF 51-20-01-0G-0; [06] VERIFIED INSTALLATION; [07] PARTS VERIFICATION; [08] LATE ENTRY TREATED & PRIMER VERIFIED
CORROSION AFT CABIN WET AREA FLOOR SUPPORT BEAM UPPER FWD FLANGE FASTENERS HOLES RBL 23 TO RBL45 STA 986.5. REMOVED CORROSION AFT WET AREA FLOOR SUPPORT BEAM UPPER FLANGE HOLES. FOUND OUT LIMITS. REPAIR PARTS TRIM AND DRILLED HOLES. TREAT AND PRIMED CUTOUT FLANGE, REPAIR PARTS AND ALL DRILLED HOLES IAW SRM 51-20-01-0G-0. PERFORMED DETAIL VISUAL INSPECTIONS OF CUTOUT FLANGE, ADJACENT STRUCTURE AND INTERCOSTAL, NO OTHER DAMAGE FOUND. TRIMMED OUT MACHINED INTERCOSTALS IAW SRM 53-70-51-2R-4 REPAIR 4 STEP 4.E 9(3). PERFORMED HFEC INSP ON CUTOUTS IAW NDT P6 51-00-00 PROC.23, NO CRACKS. ACCOMPLISHED FLAP PEENING ON CUT EDGES OF INTERCOSTALS AND CORNER FITTINGS IAW SRM 53-70-51-2R-4, SOPM 20-10-03.
AFT CABIN WET AREA FLOOR PANEL # 241ABF EDGE DELAMINATED AND SEVERAL DAMAGED INSERTS MKD ; / [01] REPAIRED DELAMINATED AREA AND REMOVED & REPLACED DAMAGED INSERTS AT FLOOR PANEL 241ABF. REF B737-700 SRM 53-00-50-2R-0; SRM 53-00-50-2R-9 PARAGRAPH 4 AND SRM 53-00-50-2R-0 PARAGRAPH 5 S.; [02] VERIFIED REPAIR
FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED @ FWD FASTENER HOLE RBL 33 BETWEEN STA 312 AND 328 ; / [01] REMOVED FLOOR SUPPORT INTERCOSTAL RBL 33 BETWEEN STA 312 AND 328 INREF. B-737 700 SRM 51-40-02-0G; [02] LOCATED AND DRILLED NEW INTERCOSTAL P/N 141A5410U12 AS PER SRM 51-40-05-0G-0.; [03] VERIFIED. STEPS 1 AND 2; [04] RII OK TO INSTALL NEW INTERCOSTAL; [05] REMOVED AND REPLACED INTERCOSTAL P/N 141A5410U12 AT MAIN CABIN RBL 33 BETWEEN STA 312 AND 328 AS PER SRM 51-40-02-0G-0 AND DWG 141A5400; [06] VERIFIED STEP # 5.
FWD LT FUSELAGE FRAME SMALL CRACK AT FLANGE ABOVE L1 DOOR CUTOUT BS 312. REMOVED CRACK IAW SRM 53-10-07-2R-1 REPAIR 1. PERFORMED HFEC INSP. ALONG EDGE OF CUTOUT IAW NDT PART 6; 51-00-00, PROCEDURE 23. NO CRACKS NOTED. LOCATED & DRILLED NEW HOLES ON LAY OUT REPAIR AND FABRICATED NEW PART. HEAT TREATED ANGLE IAW BAC 5602 PAGES 22- 28. TRIM OUT REPAIR ANGLE IAW SRM 53-10-07-2R-1 REPAIR 1. LOCATED & DRILLED REPAIR PART IAW SRM 53-10-07-2R-1. PERFORMED ROTO INSP ON EXISTING HOLES IAW NDT P6 51-00-00 PROC.16; NO CRACKS. PERFORMED PENETRANT INSP ON ANGLE IAW SOPM 20-20-02, NO CRACKS NOTED. TREATED & PRIMED PART IAW AMM 51-21-41 -370-801 & AMM 5121-72-370-80. INSTALLED REPAIR IAW SRM 51-40-02-0G-0.
FWD WET AREA FLOOR PANEL 221CF EDGES DELAMINATED MKD ; / [01] RECEIVED AND REPLACED PANEL 221CF AS PER AMM 53-21-00-300-801.; [02] VERIFIED REPLACEMENT. CLOSING WILL BE ACCOMPLISHED ON CARD TTG8Q006Q1SK
CORROSION ** AT L- 1-DOOR FWD GIRT BAR FITTING MKD ; / [01] REMOVED AND REPLACED GIRT BAR FITTING AT L-1 DOOR FWD REF B-737-700 SRM 51-40-02; [02] VERIFIED INSTALLATION PER B-737-700 SRM 51-40-02-0G-0; [03] ADDED REFERENCE MANUALLY
CORROSION AT AFT CABIN WET AREA GALLEY FLOOR SUPPORT WEB STA 1016 LBL 10. OUT OF LIMITS IAW SRM 53-70-51-1A-1. REMOVED AFT CABIN WET AREA GALLEY FLOOR SUPPORT WEB IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW AFT WET AREA FLOOR SUPPORT WEB IAW SRM=51-40-05-0G-0. PARTIALLY INSTALLED SHEAR WEB IAW SRM=51-40-05-0G-0. INSTALLED AFT CABIN WET AREA GALLEY FLOOR SUPPORT WEB IAW SRM 51-40-02-0G-0 AND DWG 147A5600 SHEET 32 REV B.
CORROSION ON AFT CABIN WET AREA FLOORBEAM UPPER FLANGE FASTENER HOLE, LBL43 BS 986.5 REMOVED CORROSION FROM AFT CABIN WET AREA FLOOR SUPPORT BEAM UPPER FLANGE FASTENERS HOLE IAW SRM 51-10-02-0G-0. PERFORMED SHOT PEENED PROCEDURE ALONG THE CUT EDGES OF THE REPAIR AREA PER SOPM 20-10-03. INSTALLED FASTENERS TEE ANGLE IAW SRM 53-70-51-2R-4, REPAIR 4,
SUPPLEMENTAL INFORMATION: CORROSION. ** AT L- 2 DOOR LOWER FLOOR ENTRY CUTOUT SILL INNER CHORD FROM STA 947.5 TO STA 986.5 MKD ; / [01] REMOVED CORROSION AT L-2 DOOR LOWER ENTRY CUT OUT SILL INNER CHORD FROM STA 947.5 TO STA 986.5 .FOUND OUT LIMITS AREA [EXFOLIATED]IAW B737 SRM 51-10-02-0G-0.; [31] REMOVED AND REPLACED L-2 DOOR LOWER FLOOR ENTRY SILL INNER CHORD BETWEEN STA 893 TO STA 1007 LBL-60 REF B737-7 SRM 51-40-02-0G-0 AND DWG#147A8501; [32] VERIFIED REMOVED AND REPLACED L-2 DOOR LOWER FLOOR ENTRY SILL INNER CHORD BETWEEN STA 893 TO STA 1007 LBL-60 REF B737-7 SRM 51-40-02-0G-0 AND DWG#147A8501; [33] VERIFIED LATE ENTRY: INSTALLED AND REMOVED EWIS PROTECTION AT L-2 DOOR LOWER FLOOR ENTRY SILL INNER CHORD AREA REF B7370-7 AMM 20-60-07-913-801
FWD CABIN WET AREA FLOORBEAM, LBL23 AND BS 312. REMOVED CORROSION IAW SRM 51-10-92-0G-0. COMPLETED FABRICATION OF REPAIR PARTS FOR THE FLOORBEAM IAW SRM 53-10-51-2R-17, REPAIR 17. TREATED AND PRIMED ALL REPAIR PARTS IAW AMM=51-00-58-201 AND AMM 51-21-72-370-802, STEP 29. INSTALLED REPAIR IAW SRM 51-40-02-0G-0, AND SRM 53-10-51-2R-17, REPAIR 17.
CORROSION. ** AFT CABIN R-2 DOOR FLOOR ENTRY LOWER SILL INNER CHORD FROM STA 947.5 TO STA 986.5 MKD ; / [01] REMOVED CORROSION AFT R-2 DOOR FLOOR ENTRY LOWER SILL CHORD FROM STA 947.5 TO STA 986.FOUND OUT LIMITS AREA [EXFOLIATED ] IAW SRM 51-10-02-0G-0. [20] ACCOMPLISHED REPLACED RT INNER CHORD AND INSTALLED RT AFT WEB REF B737-7 SRM 51-40-02-0G-0 AND DWG #147A8501; [21] REMOVED EWISN PROTECTION AT RT REPAIR AREAS REF 737-7 AMM 20-60-07-913-801; [22] CORRECTION STEP. 21 REMOVED EWIS; [23] CHANGED FROM MAJOR TO MINOR REPAIR TYPE; [24] VERIFIED R2 DOOR FLOOR ENTRY LOWER SILL INNER CHORD INSTALLATION & EWIS PROTECTION REMOVAL; [25] C/W; [26] VERIFIED REPLACED RT INNER CHORD STA 947 T0 STA 1007.<BR>VERIFIED INSTALLED RT AFT WEB FROM STA 986.5 TO STA 1016 BETWEEN RBL 45 TO RBL 60.
SUPPLEMENTAL INFORMATION: FWD CABIN FLOOR WET AREA INTERCOSTAL CRACKED AT BL-0 BETWEEN STA 270 AND 294.5 MKD DOT ; / [01] REMOVED INTERCOSTAL AT FWD CABIN WET AREA BL-0 BETWEEN STA 270 & 294.5 AS PER SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW INTERCOSTAL AS PER SRM 51-40-05-0G-0.; [03] VERIFIED STEPS 1; 2.<BR><BR>OK TO INSTALL NEW INTERCOSTAL; [04] INSTALLED NEW INTERCOSTAL AT MAIN CABIN FORWARD WET AREA BL-0 BETWEEN STA 270 AND 294.5 AS PER SRM 51-40-02-0G-0 AND DWG 141A5400.; [05] VERIFIED; [06] PART CERTIFICATION.; [07] C/W
SUPPLEMENTAL INFORMATION: CORROSION ** AT FWD CABIN WET AREA R-1 DOOR ENTRY LOWER SILL INNER CHORD BETWEEN STA312 AND 328 ; / [01] REMOVED 2 FASTENERS FOR ACCESS AT R-1 DOOR LOWER SILL INNER CHORD AT STA 312+9' PER BOEING 737-700 SRM 51-40-02-0G-0;[15] COMPLETED INSTALLATION OF NEW INNER CORD P/N 654A0004-134 AS PER SRM 51-40-02-0G-0 AND DWG 141A8310.; [16] REMOVED EWIS PROTECTION MENTIONED ON STEP 6 .; [17] VERIFIED INSTALLATION OF NEW R1 DOOR LOWER SILL INNER CHORD BETWEEN STA 277- STA 360; [18] RE-INSTALLED 2 FASTENERS REMOVED ON STEP 1.; [19] CORRECTION ADDED TO STEP 18: PER BOEING 737-700 SRM 51-40-02-0G-0.<BR>VERIFIED INSTALLATION OF FASTENERS
SUPPLEMENTAL INFORMATION: AFT CABIN FLOOR PANEL # 241ZF TOP LAYERS DELAMINATED MKD ; / [01] MEASUARES; [02] RECEIVED AND REPLACED FLOOR PANEL 241ZF AS PER B737-700 AMM 53-21-00-300-801.; [03] PANEL WILL BE INSTALLED ON TTG8Q006Q134
SUPPLEMENTAL INFORMATION: AFT CABIN WET AREA FLOOR PANEL # 242DF TOP SURFACE LAYERS DELAMINATED AND SEVERAL INERTS MISSING ; / [01] REMOVED CABIN FLOOR PANEL #242DF AS PER BOEING 737-700 AMM 53-21-00-000-801.; [02] OK TO INSTALL NEW FLOOR PANEL 242DF; [03] INSTALLED NEW PASSENGER CABIN FLOOR PANEL #242DF AS PER BOEING 737-700 AMM 53-21-00-400-801; [04] MEASURES; [05] VERIFIED FLOOR PANEL INSTALLATION 242DF
SUPPLEMENTAL INFORMATION: AFT WET AREA CABIN FLOOR PANEL 241ADF TOP LAYERS DELAMINATED ; / [01] CLEANED AND PREPARED FOR REPAIR FIBERGLASS AT CABIN FLOOR PANEL 241 ADF AS PER B737- 700 SRM 53-00-50-2R-2; [02] VERIFIED STEP #1; [03] (RII) OK TO APPLY FIBERGLASS REPAIR.; [04] REPAIRED FIBERGLASS AT CABIN FLOOR PANEL 241ADF AS PER B737-700 SRM 53-00-50-2R-2; [05] (RII) VERIFIED STEP #4; [06] CLEANED ; PREPARED FOR REPAIR THE FIBERGLASS ;REPAIRED AT FLOOR PANEL 241ADF AS PER B737-700 SRM 53-00-50-2R-2 MATERIAL USED PO;1711677 PO;1150387 PO; 1713932; [07] (RII) FINAL INSPECTION; FIBERGLASS FLOOR REPAIRED.
SUPPLEMENTAL INFORMATION: FWD CABIN WET AREA FLOOR INTERCOSTAL CRACKED @ LBL 45 BETWEEN STA 328 AND 344 ; / [01] REMOVED INTERCOSTAL DAMAGED IN REFERENCE. B-737 SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED HOLES IN THE NEW INTERCOSTAL IN REFERENCE B-737 SRM 51-40-02-0G-0 AT STA 328-344 LBL 45.; [03] VERIFIED NEW PART DRILL.<BR>OK TO INSTALL; [04] STAR INSTALLING HI LOCK IN REFERENCE. B737 SRM 51-40-02-0G-0.; [05] INSTALLED NEW INTERCOSTAL AT FWD WET AREA BETWEEN STA 328 AND STA 344 LBL 45 AS PER B737-700 SRM 51-40-02-0G-0 / 51-40-05-0G-0 AND DRWG # 141A5400 .; [06] VERIFIED PARTS AND MEASUREMENTS; [07] VERIFIED INSTALLATION
AFT CABIN WET AREA L/H GALLEY FLOOR SUPPORT WEB 2EA FASTENER HOLES ELONGATED AND MISSING NUT PLATES LBL 45 BETWEEN BS 986.5 AND 1016. REMOVED AFT WET AREA L/H FLOOR WEB AT STA 986.5 BETWEEN LBL 45 AND STA 986.5 IAW B 737-7 SRM 51-40-02-0G-01 LOCATED AND DRILLED NEW AFT WET AREA LT FLOOR SUPPORT WEB AT STA 986.5 IAW SRM 51-40-05-0G-0-A00745. START TO INSTALL FASTENERS AT AFT CABIN WET AREA LT GALLEY FLOOR SUPPORT WEB IAW SRM -40-05-0G-0-A00745. COMPLETED INSTALLED GALLEY FLOOR SUPPORT WEB AT MAIN CABIN AFT WET AREA IAW SRM 51-40-05-0G-01, AND 51-40-0G-0-A00745.
SUPPLEMENTAL INFORMATION: FWD CABIN WET AREA INTERCOSTAL SUPPORT CRACKED @ LBL45 BETWEEN STA 312 AND 328 MKD ; / [01] REMOVED DAMAGED INTERCOSTAL IN REFERENCE B-737 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED HOLES IN NEW INTERCOSTAL AT STA 312-328 LBL 45; IN REFERENCE B-737 SRM 51-40-02-0G-0; [03] VERIFIED NEW PART DRILL.<BR>OK TO INSTALL; [04] STAR INSTALLING HI LOCKS IN REFERENCE B-737 SRM 51-40-02-0G-0.; [05] INSTALLED NEW INTERCOSTAL AT FWD. WET AREA LBL 45 BETWEEN STA 312 AND STA 328 AS PER B737-700 SRM 51-40-02-0G-0 / 51-40-05-0G-0 AND DRWG # 141A5400.; [06] VERIFIED MEASUREMENTS; [07] VERIFIED INSTALLATION
ACCESS PANEL 192F AT FWD AND AFT ANTENNA INTERFACE WITH CORROSION ; / [01] CLEANED AREA IN REFERENCE B-737 SRM 51-10-02- 0G-0AND FOUND OUT LIMITS IN REFENCES B-737 SRM 53-40-70-1A-1; [02] PAINTED ON ACCESS PANEL 192AT AS REQUURED REF B-737 AMM 51-21-73-370-803; [03] VERIFIED PAINT; [04] CORRECTION: PANEL 192F; [05] REPLACED PANEL 192F IN REFERENCE. B737 SRM 51-42-02-0G-0; [06] CORRECTION<BR>PANEL 192F WAS REPLACED AND PAINTED; [07] PANEL 192F WILL BE INSTALLED ON CARD TTG8Q006Q1F3
L-2 DOOR INNER WEB STRUCTURE UNDER SCUFF PLATE CORRODED. REMOVED CORROSION UNDER SCUFF PLATE. FOUND OUT OF LIMITS IAW SRM 51-010-02-0G-0. REMOVED STRUCTURE UNDER SCUFF PLATE IAW SRM 51-40-02-0G-0. WEB STRUCTURE UNDER SCUFF PLATE INSTALLED WEB, INSTALLED FASTENERS IAW SRM 51-40-02-0G-0. ] FINALIZED INSTALLATION OF L-2 DOOR INNER WEB UNDER SCUFF PLATE IAW SRM 51-40-02-0G-0.
L/H FWD WING TO BODY FAIRING AFT SUPPORT FOR PANEL 191AL CRACKED. ; / [01] REMOVED WTB FAIRING PANEL 195 AL FOR ACCESS AS PER B737-700 AMM 53-51-21-000-802.; [02] REMOVED FRAME SUPPORT ANGLE FOR WTB FAIRING PANEL 191AL AS PER B737-700 SRM 51-40-02-0G-0.; [03] LOCATED AND DRILLED NEW SUPPORT ANGLE FOR WTB FAIRING PANEL 191AL AS PER B737-700 SRM 51-40-05-0G-0.; [04] VERIFIED REMOVED WTB FAIRING PANEL 195 AL AND REMOVED FRAME SUPPORT ANGLE FOR WTB FAIRING PANEL 191AL; [05] VERIFIED LOCATION AND DRILL OF NEW SUPPORT ANGLE.<BR>OK TO INSTALL; [06] INSTALLED NEW SUPPORT ANGLE FOR WTB FAIRING PANEL 191AL AS PER B737-700 SRM 51-40-02-0G-0 / DRWG # 116A3110; [07] VERIFIED STEP # 6; [08] OK TO INSTALL 195AL; [09] CLOSED P
SUPPLEMENTAL INFORMATION: RIGHT WING REAR SPAR UPPER PANEL SUPPORT BRACKET CRACKED ABOVE # 2 FUEL PUMP ; / [01] REMOVED AND REPLACED BRACKET AT RIGHT WING REAR SPAR UPPER PANEL SUPPORT;ABOVE # 2 FUEL PUMP PER SRM 51-40-02-0G-0.; [02] ACCOMPLISHED PARTS TRANSACTION.; [03] C/W
SUPPLEMENTAL INFORMATION: DME#2 BASE ON PANEL 192F CORRODED ; / [01] CLEANED AREA AND FOUND OUT LIMITS IN REFERENCE B-737 SRM 53-40-70-1A-1; [02] ADD REFERENCE 51-10-02-0G-0; [03] ADD B-737 SRM; [04] WILL BE ACCOMPLISHED. IN ITEM # TTG8Q009DQ95; [05] VERIFIED ACCOMPLISHED. IN ITEM # TTG8Q009DQ95
DME#1 BASE ON PANEL 192F CORRODED ; / [01] CLEANED AREA AND FOUND OUT LIMITS IN REFERENCE B-737 SRM 53-40-70-1-A-1; [02] ADD REFERENCE B-737 SRM 51-10-02-0G-0; [03] WILL BE ACCOMPLISHED IN ITEM #TTG8Q009DQ95; [04] VERIFIED ACCOMPLISHED IN ITEM #TTG8Q009DQ95
CRACK FOUND AT LT HORIZONTAL STAB HSS 184.70 LOWER SKIN, I/B OF DRAIN HOLE, 10' FROM AFT SPAR. REMOVED PAINT IAW AMM 51-21-11-150-801. PERFORMED HFEC INSP IAW NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED. CRACK LENGTH .625'. REMOVED PANEL 331BZ IAW SRM 55-10-01-2R REPAIR 8. INSTALLED PANEL #331BZ IAW SRM51-40-02-0G-0. RESTORED PAINT IAW AMM 51-21 -73-370-801.
F/O GLARESHIELD GRAB HANDLE BROKEN ; / [01] REMOVED AND REPLACED F/O GRAB ASSIST HANDLE PER AMM 20-00-00 S.I.P.
CABIN FLOOR PANEL 242AF AFT UPPER SURFACE HAS PEELED FIBERS. EVALUATED FLOORBOARD 242AF AND FOUND PULLED FIBERS TO UPPER FACE SHEET, REPAIRABLE IAW SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL TABLE 201 REPAIR 1. CLEANED & PREPPED FLOORBOARD IAW SRM 53-00-50-2R-1 REV. 73 STEPS 3 A C E F AND SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL. BONDED REPAIR PLIES IAW SRM 53-00-50-2R-1 REV. 73 STEPS 3 J-M AND SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL. TAP TESTED GOOD. REPAIRED DAMAGE TO FLOORBOARD 242AF AFT UPPER SURFACE IAW SRM 53-00-50-2R-1 REV. 73 AND SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL.
FUSELAGE SKIN BAS CORROSION AROUND WATER SERVIVE DOOR CUTOUT. BLENDED CORROSION. EVALUATED MATERIAL LOSS TO BE .004' ORIG .063' REMAINING .059' WITHIN LIMITS IAW SRM 53-00-01-1A-1. APPLIED ALODINE IAW AMM 51-21-41-370-803 & PRIMER IAW AMM 51-21-72-370-804. RESTORED TOP COAT AT WATER SERVICE DOOR CUTOUT IAW AMM 51-21-73-804.
CABIN FLOOR PANEL 231ZF UPPER SURFACE HAS 3 PUNCTURES INBD SIDE DOT A-21-13 ; / BONDED REPAIR . IAW B737-700 SRM 53-00-50-2R-2 PAR3J-L. AAR DIGITAL THERMOMETER 30347 D.D.4-29-22 150DEG 3HRS.;EVALUATED PANEL 231ZF. FOUND 3EA PUNCTURES TO UPPER FACE SKIN. FOUND TO BE REPAIRABLE IAW B737-700 SRM 53-00-50-2R-2 PAR 1A. CLEAN AND PREP AREA'S FOR REPAIR. B737-700 SRM 53-00-50-2R-2 PAR3A;C-E. APPLIED POTTING COMPOUND TO 3EA AREA'S. IAW B737-700 SRM 53-00-50-2R-2 PAR3 F-I. VERIFIED MATERIALS AS BMS 5-28 TY 19 (15911); BMS 9-3 (A72547); BMS 8-201 (A51765).;REPAIRED 3EA PUNCTURES TO UPPER FACE SKIN. IAW B737-700 SRM 53-00-50-2R-2; SRM 53-00-50-2R-O.;STEP 1 OK. OK TO BOND;STEP 3 AND 4 OK. AUDITED
CABIN FLOOR PANEL 241CF UPPER SURFACE HAS PEELED FIBERS DOT A-21-19 ; / BONDED REPAIR IAW SRM 53-00-50-2R-1 REV. 73 STEPS 3 J-M AND SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL. TAP TEST GOOD. CURED 3 HOURS AT 150 DEGREES OVEN--BO-O6 DUE 8-25-21;EVALUATED FLOOR BOARD AND FOUND PULLED FIBERS TO UPPER FACE SHEET AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REV. 73 TABLE 201 REPAIR 1.<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 REV. 73 REPAIR 1 STEPS 3 A;C;E;F AND SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL<BR>VERIFIED REPAIR MATERIALS AS GLASS (A94414); RESIN (A51765) IAW SRM 53-00-50-2R-1 REV. 73 REPAIR 1 TABLE 201;REPAIRED DAMAGE TO UPPER SURFACE OF FLOOR BOARD 241CF IAW SRM 53-00-50-2R-1 REV. 73; SRM 53-00-50-2R-0 REV. 73 REPAIR GENERAL. TAP TEST GOOD.;STEP 1 OK. OK TO BOND;STEP 3 AND 4 OK. AUDITED
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675 IN CABIN. / REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT LOCATION M1675 IN CABIN PER AMM 33-51-06
FLIGHT DECK #1 FIRST OFFICER WINDOW FRAME CRACKED AT C AND D POST UPPER CORNER. / REPAIRED FRAME IAW EA.
FWD CARGO BAY BS 500D STR 21 R/H GUSSET IS CRACKED / REMOVED & REPLACED GUSSET AT FCB BS 500D STR 21 R/H IAW SRM 51-40-02 & DWG 113A7902 REV.- E 59191U 14NOV19
FWD CARGO BAY BS 500D STR 21 L/H GUSSET IS CRACKED / REMOVED & REPLACED GUSSET AT FCB BS 500D STR 21 L/H IAW SRM 51-40-02 & DWG 143A7902 REV.-E 59191U 14NOV19
WHILE WORKING CUSTOMER CARD T995135 FOUND BAFFLE AT BS 500A-500B; RBL 21; WL 156 IS DAMAGED. / REPAIRED BAFFLE AT BS 500A - 500B RBL 21; WL 156 IAW EA 1-753-36067 REV IR AND ATS REPAIR # 19-05640 REV IR.
***CORROSION*** WHILE WORKING CUSTOMER CARD T995118/ FUSE 5044; FOUND CORROSION ON BAFFLE AT BS 747-767; RBL 21; WL 156 / CORRODED BAFFLE AT BS747-767; RBL21; WL156 REMOVED AND REPLACED IAW DWG 146A7500 AND B737 SRM 51-40-02
AFT CARGO BAY SHIELD ATTACH ANGLE CRACKED BETWEEN BS. 767 TO BS. 787, RBL 22, AT FASTENER HOLE. / R&R ANGLE IAW SRM & DWG.
AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 767 TO BS. 787+7, RBL 22. / R&R SHIELD IAW SRM & DWG.
AFT CARGO BAY ON R/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 767, RBL 22. / R&R SUPPORT IAW DWG AND SRM.
AFT CARGO BAY BILGE INTERCOSTAL CORRODED AT BS. 787+8, RBL 7. / R&R INTERCOSTAL IAW SRM AND DWG.
FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 400 TO BS. 500D, LBL 24. / R&R SUPPORT IAW SRM AND DWG.
***CORROSION*** IN MULTIPLE AREAS OF ACB FLOOR T STRAP STA 767 LBL 20 RBL 20 WL 159 / REMOVED AND INSTALLED NEW 'T' STRAP AT ACB BS 767 LBL 20 TO RBL 20 WL 159 IAW SRM 51-40-02. 59807U 11/16/19
***CORROSION*** IN MULTIPLE AREAS OF ACB FLOOR T STRAP STA 887 LBL 10 RBL 22 WL 159 / REMOVED AND REPLACED FLOOR STRAP LOCATED STA 887 LBL 10 - RBL 22 W.L 159 IAW SRM 51-40-02; 51-10-02 PARAGRAPH 9 AND DWG 146A9401.
***CORROSION*** ON FORWARD CARGO BAY SHIELD FROM B.S. 420-440; R.B.L. 24; W.L. 155 / REMOVED AND INSTALLED NEW FCB SHIELD FROM BS420-440; RBL24; WL155 IAW SRM 51-40-02 AND DWG #143A8126. 59565U 09NOV19
***CORROSION*** IN MULTIPLE LOCATIONS IN ACB ON L/H FLOOR TO SIDEWALL SUPPORT STA 727-847 LBL 22 WL 175 / REMOVED & REPLACED L/H FLOOR TO SIDEWALL SUPPORT BS-727 - 847 LBL 22 WL 175 IAW SRM 51-40-02 & DWG 146A7500 59191U 11-13-19
AFT CARGO BAY FLOOR TRACK CORRODED BETWEEN BS. 759 TO BS. 867, BETWEEN RBL 13 TO RBL 15. / R&R TRACK IAW SRM.
FORWARD CARGO BAY SHIELD CORRODED BETWEEN BS. 494 TO BS. 500A, RBL 24. / R&R SHIELD PER SRM AND DWG.
CORROSION IN WELL AND TOP OF TRACK BS 480 - 520 LBL25 WL 208 / REMOVED CORROSION ON SEAT TRACK B.S 480-520 LBL 25; FOUND TO BE OUT OF LIMITS AT B.S 520; LBL 25 IN AN AREA OF 1.2' X 1' X .022' I.A.W SRM 53-00-52-1A-1 SETP 4A(2)(A) FIG 103. REMOVED AND REPLACED SEAT TRACK BS 480-520 LBL 25 I.A.W DWG 143A5300 SHT 42; SRM 51-40-02-0G-0 STEP 7D & 9B
***CORROSION*** AROUND MAJORITY OF FASTENERS THROUGH FUSELAGE SKIN EXTERNALLY; COVERED BY DORSAL FIN FROM STA 867 TO STA 1006; APPROXIMATELY STR 2R TO STR 2L. / REPAIRED FUSELAGE SKIN B.S 867-1006 STR 2R-2L IAW EA 1-753-36041 REV IR AND ATS ER 19-05567 REV IR
FWD SERVICE DOOR IS CRACKED AT #5 BEAM / REPAIRED FWD SERVICE DOOR #5 BEAM ON CUSTOMER R.O. #0520055-FWR; JOB #528263
L/H HORIZONTAL STABILIZER #5 RIB CRACKED AT LOWER END OF #2 STIFFENER STAB. STA. 129.50. / REPAIRED #5 RIB PER SRM.
L/H HORIZONTAL STABILIZER #5 RIB CRACKED, LOWER END OF #3 STIFFENER STAB. STA. 129.50. / REPAIRED #5 RIB IAW SRM.
FWD SERVICE DOOR IS CRACKED AT #4 BEAM / REPAIRED FWD SERVICE DOOR #4 BEAM ON CUSTOMER R.O. #0520055-FWR; JOB #528263
R1 DOOR EVAC SLIDE GRIT BAR STOWAGE CLIP LOOSE. SECURED CLIP PER SIP.
RT OVERWING EMERGENCY EXIT LOWER LIGHT MISSING DIRECTIONAL ARROW. R&R SIGN IAW MM.
CENTER CABIN CEILING EMERGENCY EXIT LIGHT MISSING. R&R LIGHT HOUSING IAW AMM.
R1 DOOR EMERGENCY SLIDE BAR VERY HARD TO ARM. FOUND DEBRIS IN FORWARD DOOR BRACKET. CLEANED DEBRIS FROM BRACKET IAW AMM.
R1 DOOR ESCAPE SLIDE ANCHOR (FLOOR) PLATE MISSING A SCREW. R&R PLATE SCREW PER AMM.
EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PACK PER AMM.
LT EMERGENCY EXIT SIDEWALL LIGHT INOP. R&R LIGHT BALLAST PER AMM.
EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PACK PER AMM.
EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1674. R&R BATTERY PACK PER AMM.
RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM. 53-31-31
EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PACK PER AMM.
EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PACK PER AMM.
EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PACK PER AMM.
VERTICAL STIFFENER CRACKED IN LEFT WHEEL WELL AT LBL 27; LOWER WING TO BODY SUPPORT. / REMOVED AND REPLACED PER SRM 51-40-02.
AFT ATTENDANT PANEL EMERGENCY LIGHT SWITCH COVER BROKEN. R&R COVER IAW CMM.
R/H INBD FIXED LEADING EDGE AFT STRINGER AT WS 204.25 CRACKED AT FASTENER HOLE. 7TH HOLE FWD OF FWD SPAR / REMOVED AND REPLACED STRINGER I.A.W SRM 51-40-02.
INBOARD FASTENER HOLE FOR DRAIN FITTING CRACKED AT APPROXIMATELY 7 O'CLOCK POSITION, RBL 33.5". REPAIRED FITTING PER EA.
FLOOR PANEL 241CF HAS PULLED AND TORN FIBERS ON UPPER FACE SHEET. / R&R'D FLOOR PANEL PER AMM 53-21-00
FLOOR PANEL 241DF HAS PULLED AND TORN FIBERS ON UPPER FACE SHEET. / R&R'D FLOOR PANEL PER AMM 53-21-00
FLOOR PANEL 232EF HAS PULLED AND TORN FIBERS ON UPPER FACE SHEET. / R&R'D FLOOR PANEL PER AMM 53-21-00
FLOOR PANEL 231KF HAS PULLED AND TORN FIBERS ON UPPER FACE SHEET. / R&R'D FLOOR PANEL PER AMM 53-21-00
FLOOR PANEL 231XF HAS PULLED AND TORN FIBERS ON UPPER FACE SHEET. / INSTALLED CABIN FLOOR PANEL 231XF PER AMM 53-21-00
FLOOR PANEL 241AF HAS PULLED AND TORN FIBERS ON UPPER FACE SHEET. / R&R'D FLOOR PANEL PER AMM 53-21-00
EXTERIOR LAV SERVICE DOOR HAS CORROSION ON INSIDE SURFACE / R&R LAV DOOR ASSY PER AMM 52-49-07
RIGHT WING OBRSS 273;17 INCHES AFT R/S;1 INCH BELOW UPPER PNL SEAL RETAINER BRACKET IS CRACKED. / REPLACED SEAL RETAINER BRACKET PER SRM 51-40-02
AFT CARGO FWD CORNER THRESHOLD CRACKED IN 3 LOCATIONS (MARKED) / THRESHOLD PLATE REPAIRED ON REPAIR ORDER # 7530063-ANR. PLATE TO BE INSTALLED ON ROUTINE TASK CARD 753-721-00-01.
LT WING OUTBOARD AFT FLAP LOWER SKIN DELAMINATED AT INBOARD TRAILING EDGE. REPAIRED AFT FLAP PER SRM.
RT WING NR 7 SLAT SKIN CRACKED AT LOWER NOSE ATTACH RIB ATTACHING FASTENER. R&R NR 7 SLAT PER SRM.
LT WING NR 1 SLAT SKIN CRACKED AT SLAT ACTUATOR OUTBOARD ATTACH RIB 2ND FROM AFT FASTENER. R&R NR 1 SLAT PER SRM.
AFT CARGO FWD FLOOR PANEL 140AF CRACKED/WORN / REMOVED AND REPLACED PER AMM 25-52-10.
AFT CARGO FWD CENTER FLOOR PANEL 140BF CRACKED/WORN / REMOVED AND REPAIRED PER AMM 25-52-10
L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.
R1 DOOR SLIDE GIRT BAR LOOSE. SECURED THE GIRT BAR IAW MM.
R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. (DID NOT DEPLOY) R&R SLIDE ASSY PER MM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R & R THE BATTERY PACK IAW AMM AND DWG.
HIGH VIBRATION INDICATION ON NR 1 ENGINE. DECLARED EMERGENCY AND AIR TURNBACK. R & R THE NR 1 ENGINE IAW MM.
FORWARD ENTRY DOOR EMER LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW AMM.
R1 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
R1 DOOR EXTERIOR EMER LIGHT IN OPERATIVE. R & R LIGHT IAW AMM.
L2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
R1 DOOR CUTOUT UPPER HINGE RECESS CRACKED, AT BS 303, RBL 64. R & R HINGE BOX IAW SRM & DWG.
R1 DOOR CUT OUT LOWER FWD CORNER ON THE INTERNAL SIDE CRACKED, AT BS 303, RBL 64. R & R CUT OUT IAW SRM & DWG.
RIGHT HORIZONTAL STABILIZER LE PANEL 341BZ, 5TH RIB OTBD FROM INBD END, RIB ATTACH ANGLE CRACKED AT UPPER AFT END. R & R RIB IAW SRM & DWG.
FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.
LEFT CREASE BEAM INNER CORD CORRODED, BETWEEN BS 695 - 711. REPAIRED INNER CHORD IAW ER & EA.
RIGHT CREASE BEAM INNER CHORD CORRODED, BETWEEN BS 695 - 729. REPAIRED INNER CHORD IAW ER & EA.
STRAP CORRODED AT BS 1016, BETWEEN LBL 6 - 10. R & R STRAP IAW SRM & DWG.
R1 DOOR INNER CHORD CORRODED, BETWEEN BS 294 - 332. R & R INNER CHORD IAW SRM.
FORWARD ENTRY DOOR INNER CHORD CORRODED, BETWEEN BS 313 - 348. R & R CHORD IAW SRM & DWG.
AFT CARGO FLOORBEAM TRACK TOP SURFACE CORRODED, BETWEEN BS 793 - 807, RBL 14. R & R TRACK IAW SRM & EA.
LEFT CARGO FLOOR TO SIDEWALL TRANSITION SUPPORT CORRODED AT BS 770.5, LBL 24. R & R SUPPORT IAW SRM.
STRINGER CLIP CORRODED, AT BS 967, STRINGER 23R. R & R CLIP IAW SRM & DWG.
RIGHT FLOOR TO SIDEWALL TRANSITION SUPPORT CORRODED, BETWEEN BS 767 - 727E. R & R SUPPORT IAW SRM.
STRINGER CLIP CORRODED AT BS 847, STRINGER 23L. R & R CLIP IAW SRM & DWG.
CARGO DOOR WEB CORRODED, BETWEEN BS 795 - 830. REMOVED WEB IAW SRM.
FORWARD CARGO BIN DOOR WEB CORRODED, BETWEEN BS 460 - 490. R & R WEB IAW SRM.
AIR RETURN, NR 1 BLEED TRIP OFF LIGHT ILLUMINATED DURING CLIMB & WOULD NOT RESET. R & R NR 1 ENG PRE-COOLER CONTROL VLV IAW MM.
FLOORBEAM SPLICE STRAP CRACKED AT BS 727B RBL 45.5. REPAIRED FLOORBEAM IAW EA.
L2 DOOR EMER EVAC SLIDE BOTTLE PRESS LOW. R & R SLIDE IAW MT.
RIGHT OVERWING EMER EXIT SIGN COVER MISSING. INSTALLED COVER IAW AMM.
RIGHT OVER WING DOOR ESCAPE STRAP FRAYED. R & R STRAP IAW MM.
LEFT EMERGENCY EXIT HATCH ESCAPE STRAP FRAYED. R & R STRAP IAW AMM.
RIGHT HORIZONTAL STABILIZER STAB STATION 101.90 RIB FWD END OTBD SIDE CRACKED. REPAIRED RIB IAW EA.
LT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW MM.
RT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW MM.
R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW AMM.
AFT GALLEY EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT ROW 16. R & R BATTERY IAW AMM.
L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER FELL OFF. R & R LENS ASSY IAW MM.
LEFT HORIZ STAB LOWER IN SPAR SKIN CRACKED AT STA 138.70. REPAIRED SKIN IAW SRM.
LEFT HORIZ STAB LOWER IN SPAR SKIN CRACKED AT STA 129.50. REPAIRED SKIN IAW SRM.
RIGHT STAB LOWER IN SPAR SKIN CRACKED AT STA 101.90. REPAIRED SKIN IAW SRM.
DIVERT/DECLARED EMERGENCY/ENGINE SHUT DOWN. ON CLIMBOUT NR 2 ENGINE LOUD BAND AND SHUTDOWN. REMOVED AND REPLACED NR 2 ENGINE PER MT.
R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.
LT FRAME CRACKED AT BS 312, STR 4L. REPAIRED FRAME IAW EA.
AFT CARGO FLOOR SUPPORT CHANNEL CORRODED AT BS 770, LBL 3. REPAIRED CHANNEL PER EA.
AFT CARGO FLOOR SUPPORT CHANNEL CORRODED AT BS 770, LBL 12. REPAIRED CHANNEL PER EA.
FWD RT EMERGENCY BATTERIES FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACKS PER MM.
FWD LT EMERGENCY BATTERIES FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.
AIR TURNBACK, LEFT FORWARD WINDSHIELD ARCED AND THEN CRACKED. REMOVED AND REPLACED L1 WINDOW AND WINDOW HEAT CONTROLLER PER MM.
MID CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 19 TO ROW 23. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC1 CHECK, FOUND FWD EEPLS END CAP MISSING. INSTALLED END CAP PER MM.
DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE TRACK LOOSE. SECURED SLIDE PER MM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS WIRING INOP BETWEEN ROW 18 TO ROW 20. REPAIRED WIRE PER MM.
R1 DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
R1 DOOR EMERGENCY EXIT LIGHT BASE BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED HC1 CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED MV2 CHECK FOUND EEPLS INOP AT ROW 1. RELAMPED PER MM.
DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 807, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER MISSING AT ROW 7. INSTALLED COVER PER MM.
DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED PER MM.
DURING SCHEDULED HC1 CHECK, FOUND LT OVERWING EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, FOUND RT AFT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, FOUND LT AFT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
FOUND RT OVERWING EMEGENCY EXIT DOOR SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS STRIP CRACKED. REMOVED AND REPLACED STRIP PER MM.
EEPLS LENS AFT COVER MISSING. INSTALLED COVER ASSY PER MM.
R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM.
DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED EVAC SLIDE PER MM.
DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.