N940WN
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
FOUND RH OVERWING EXTERIOR AND INTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR RH OVERWING EMERGENCY LIGHTS IAW AMM 33-51-06. PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-06.
RIGHT SIDE OVERWING LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED POWER SUPPLY FUSE AND REMOVED AND REPLACED RIGHT SIDE LOWER EMERGENCY LIGHT IN REF TO AMM 33-51-06. AND AMM 33-51-01 OPS. CHECK GOOD NO FAULTS NOTED
RIGHT SIDE OVER WING LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED POWER SUPPLY FUSE AND REMOVED AND REPLACED RIGHT SIDE LOWER EMERGENCY LIGHT IN REF TO AMM 33-51-06. AND AMM 33-51-01 OPS. CHECKED GOOD, NO FAULTS NOTED
BOTH ENGINES ONLY ACHIEVED 94.6 PERCENT N1 WHEN 95.5 PERCENT WAS REQUIRED-THRUST LEVERS WERE IN FULL FORWARD POSITION. NO FAULTS ON ADIRUS OR DEUS. R & R TAT PROBE IAW AMM 34-21-06 AND PERFORMED POWER ASSURANCE TEST IAW AMM 71-00-00. OP CHKD GOOD. OK FOR SERVICE.
BIRD STRIKE, NO ABNORMAL ENGINE INDICATIONS. ODOR OF HOT OR SOMETHING COOKING IN COCKPIT & CABIN. C/W BIRDSTRIKE CONDITIONAL INSP IAW AMM 05-51-18. REF DEFECT LGPG 3025472. INSPECTED PER AMM 05-51-18-210-801-NG-01.
FWD ENTRY DOOR EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THELAMPS IN L1 DOOR EXTERIOR EMERGENCY LIGHT; OPS CHECKED GOOD IAW AMM 33-51-03.
AFT LEFT ENTRY DOOR ESCAPE SLIDE GIRT BAR CLIP LOOSE. REPLACED FASTNERS AT LT ENTRY DOOR ESCAPE SLIDE GIRT BAR CLIP IAW SRM 51-40-02, AMM 25-66-01 AND MT 725-61-06.
PASSENGER SEAT 10A RECLINES INTO AN EXIT ROW. ADJUSTED HYDRO-LOCK TO THE LOCKED POSITION PER AMM 25-22-00.
PASSENGER SEAT 10B RECLINES INTO AN EXIT ROW. ADJUSTED HYDRO-LOCK TO THE LOCKED POSITION PER AMM 25-22-00.
PASSENGER SEAT 10C RECLINES INTO AN EXIT ROW. ADJUSTED HYDRO-LOCK TO THE LOCKED POSITION PER AMM 25-22-00.
CRACK OUTBOARD FAN COWL HOLD OPEN ROD SUPPORT BRACKET AFT POSITION ON ENGINE 1. REPLACED OUTBOARD FAN COWL HOLD OPEN ROD SUPPORT BRACKET AFT POSITION ON ENGINE 1 IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND CMM 71-13-30 DETAIL F PAGE 10056.
CRACK ACCESS PANEL 321A LOCATED ON RIB #8 ASSY AT VERTICAL STABILIZER. REPLACED RIB #8 LOCATED ON ACCESS PANEL 321A AT VERTICAL STABILIZER I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 174A1008 SHEET 2 REV. C AND DWG 174A0103 SHEET 7 REV. -. DUE TO NOT FUND ALLOWABLE DAMAGE ON SRM B737-700 55-30-01-1A-5. CRACK LENGTH: 0.420'.
CRACK INBOARD FAN COWL SUPPORT WEB ON ENGINE 1. REPLACED SUPPORT WEB INBOARD FAN COWL ON ENGINE 1 IAW B737-700 SRM 51-40-02 AND CMM 71-13-30 SHEET 5.
CRACK INSPAR RIB 92.70 LOCATED ON WEB BTW UPPER CHORD AND FRONT SPAR FITTING AT LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB 92.70 LOCATED ON WEB BTW UPPER CORD AND FRONT SPAR FITTING AT LT HORIZONTAL STABILIZER I.A.W. EA 25-155-01500-WIP1 AND EA 25-155-01500-WIP2 AND EA COVER 25-155-01500.
CRACK ON FITTING LOCATED BS 947.5 AT LEVEL STR 26L WL 156.1 AT AFT CARGO COMPARTMENT 2025-340260<[01] REPLACED FITTING LOCATED BS 947.5 AT LEVEL STR 26L WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 149A8103 SHEET 7 REV A SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED FITTING LOCATED BS 947.5 AT LEVEL STR 26L WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 149A8103 SHEET 7 REV A SEE INDIVIDUAL SIGN OFF BELOW
CRACK ON WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT. REPLACED WEB AND FASTENERS LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 AND DWG: 147A7500 SHEET 29 REV-.
CORROSION SUPPORT ZEE LOCATED BTW BS 727E TO BS 767 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. REMOVED AND REPLACED SUPPORT ZEE BTW BS727 TO BS767 RBL22 AND WL153.1 AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02 AND DWG 146A7500 SHEET 157 REV - AND DWG 146A7502 SHEET 49 REV-.
CORROSION SUPPORT ZEE LOCATED BTW BS 727C TO BS 727E RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. REMOVED AND REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 RBL 22 WL 156.1 AT AFT CARGO COMAPRTMENT REFER TO FAULT TTG8Q010Z364 WHERE WORK IS DOCUMENTED.
CORROSION SUPPORT ZEE LOCATED BTW BS 727C TO BS 727E LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. REMOVED AND PERFORMED REPAIR ZEE CHANNEL SIDEPLATE LOCATED BTW BS 727 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT REFER TO FAULT TTG8Q010YF93 WHERE WORK IS DOCUMENTED.
CORROSION SUPPORT ZEE LOCATED BTW BS 727E TO BS 767 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. REMOVED AND PERFORMED REPAIR ZEE CHANNEL SIDEPLATE LOCATED BTW BS 727 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT REFER TO FAULT TTG8Q010YF93 WHERE WORK IS DOCUMENTED.
CORROSION SUPPORT ZEE LOCATED BTW BS 767 TO BS 807 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. REMOVED AND PERFORMED REPAIR ZEE CHANNEL SIDEPLATE LOCATED BTW BS 727 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6, SRM 51-40-02, & DWG 146A7500. SHEET: 157 REV:-.
CORROSION ON SHIELD WEB LOCATED BTW BS 787 TO BS 794.3 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-340259. REPLACED SHIELD WEB LOCATED BTW BS 787 TO BS 794.3 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 146A0081; SHEET: 37 AND REV:-.
CRACK ON SUPPORT BRACKET LOCATED BTW BS 907 TO BS 927 AFT POSITION AT AFT CARGO COMPARTMENT 2025-340262<[01] REPLACED AFT SUPPORT BRACKET (STIFFENER) BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AT AFT CARGO COMPARTMENT IAW B373-700 SRM 51-40-02 AND DGW 147A7221 SHEET: 24 REV: - SEE INDIVIDUAL SIGN OFF BELLOW.;[02] REPLACED AFT SUPPORT BRACKET (STIFFENER) BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AT AFT CARGO COMPARTMENT IAW B373-700 SRM 51-40-02 AND DGW 147A7221 SHEET: 24 REV: - SEE INDIVIDUAL SIGN OFF BELLOW.
CORROSION WEB LOWER SILL LOCATED BTW BS 440 TO BS 492.4 RBL 25 WL 156.1 AT FWD CARGO COMPARTMENT 2025-340248<[01] THE MINIMUM REMAINING THICKNESS OM REWORKED AREA TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN:130066401; DUE DATE: 21-OCT-25;[02] REPLACED WEB LOWER SILL LOCATED BTW BS 440 TO BS 492.4 RBL 25 WL 156.1 AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 DWG 143A8330 SHEET 42 REV. A <BR><BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] TASK COMPLETED; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW
CORROSION ON SUPPORT ANGLE LOCATED BS 500D BTW STR 26L TO STR 26R WL 156.1 AT FWD CARGO COMPARTMENT 2025-340247<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS 500D BTW STR 26L TO STR 26R IAW B737-700 SRM 51-40-02 AND DRAWING 143A7902 SHEET 209 REV .SEE INDIVIDUAL STEP SIGNOFF BELOW;[02] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ON ANGLE LOCATED BS 867 BTW STR 26L TO STR 27L WL 156.1 AT AFT CARGO COMPARTMENT 2025-340255<[01] REPLACED ANGLE LOCATED BS 867 BTW STR 26L TO STR 27L WL 156.1 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02; SRM B737-700 51-40-02 AND DRAWING #149A8102; SHEET 18; REV.- ; DRAWING# 149A8104; SHEET 1; REV. B. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE LOCATED BS 867 BTW STR 26L TO STR 27L WL 156.1 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02; SRM B737-700 51-40-02 AND DRAWING #149A8102; SHEET 18; REV.- ; DRAWING# 149A8104; SHEET 1; REV. B. SEE INDIVIDUAL SIGN OFF BELOW.
CRACK INSPAR RIB 92.70 LOCATED AT 30 INCH OF FRONT SPAR LT HORIZONTAL STAB 2025-340238<[01] TOOL USED ON STEP 3 AND 4: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 210136503 ; DUE DATE: 24-JUL-25;[02] PERFORMED PERMANENT REPAIR ON INSPAR RIB 92.70 LOCATED AT 30 INCH OF FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM-55-10-09-2R-4 REPAIR 4 PARAGRAPH 4.M TO R. FIGURE: 202 SHEET: 1 AND FIGURE: 202 SHEET: 4 AND B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW.;[03] PERFORMED PERMANENT REPAIR ON INSPAR RIB 92.70 LOCATED AT 30 INCH OF FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM-55-10-09-2R-4 REPAIR 4 PARAGRAPH 4.M TO R. FIGURE: 202 SHEET: 1 AND FIGURE: 202 SHEET: 4 AND B737-700 SRM 51-40-02. <BR>SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII.
CRACK ON TIE CLIP LOCATED FWD FACE 500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2025-340237<[01] REPLACED TIE CLIP AND FASTENERS LOCATED FWD FACE 500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG: 143A1213 SHEET: 57 REV: . SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP <BR>INSTALLED NEW TIE CLIP AND FASTENERS LOCATED FWD FACE 500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG: 143A1213 SHEET: 58 REV: - SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2<BR>REPLACED TIE CLIP AND FASTENERS LOCATED FWD FACE 500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG: 143A1213 SHEET: 58 REV: . SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPLACED TIE CLIP AND FASTENERS LOCATED FWD FACE 500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG: 143A1213 SHEET: 58 REV: . SEE INDIVIDUAL SIGN OFF BELOW.
CORROSION ON SHIELD WEB LOCATED BTW BS 492.4 TO BS 500A RBL23 WL 156.1 AT FWD CARGO COMPARTMENT 2025-340235<[01] REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS 492.4 TO BS 500A RBL23 WL 156.1 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ÿ½TEM 9; SRM 51-40-02 AND DWG 143A0080 SHEET 23 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED RII
CORROSION ON SHIELD WEB LOCATED BTW BS 420 TO BS 440 RBL23 WL 156.1 AT FWD CARGO COMPARTMENT 2025-340236<[01] TOOL USED P/N: 38 DL PLUS; S/N: 120398603; CAL DUE: 23-DEC-25.;[02] REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS 420 TO BS 440 RBL23 WL 156.1 AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A0080 SHEET 33 REV. - <BR><BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS 420 TO BS 440 RBL23 WL 156.1 AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A0080 SHEET 33 REV. -
CORROSION ON SUPPORT ZEE LOCATED BTW BS 500B TO BS 500D RBL 23 WL 156.1 AT FWD CARGO COMPARTMENT 2025-340242<[01] REPLACED SUPPORT AND FASTENERS ZEE LOCATED BTW BS 500A TO BS 500D RBL 23 WL 156.1 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-05 ITEM 9 SRM 51-40-02 AND DWG 143A7500; SHEET: 71 AND REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED SUPPORT AND FASTENERS ZEE LOCATED BTW BS 500A TO BS 500D RBL 23 WL 156.1 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 143A7500; SHEET: 71 AND REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2 <BR>REPLACED SUPPORT ZEE AND FASTENERS LOCATED BTW BS 500A TO BS 500D RBL 23 WL 156.1 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 143A7500; SHEET: 71 AND REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[04] COMPLETED JOB
CORROSION ON STRAP LOCATED BS 887 BTW STR 25L TO STR 25R WL 156.1 AT AFT CARGO COMPARTMENT 2025-340254<[01] REPLACED STRAP LOCATED BS 887 BTW STR 25L TO STR 25R WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;[02] TASK COMPLETED
CORROSION ON STRAP LOCATED BS 767 PLUS 5 INCHES BTW STR 25L TO STR 25R WL 156.1 AT AFT CARGO COMPARTMENT 2025-340253<[01] REPLACED STRAP LOCATED ON BS767 MORE 5' BTW STR25L TO STR25R AND WL156.1 AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A7500 SHEET 157 REV. - ; DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM B737-700 53-00-53-1A-2<BR><BR>CORROSION MEASURES ARE: L: 41.650' W: 1.041' REPLACED STRAP LOCATED ON BS767 MORE 5' BTW STR25L TO STR25R AND WL156.1 AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A7500 SHEET 157 REV. - ; DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM B737-700 53-00-53-1A-2<BR><BR>CORROSION MEASURES ARE: L: 41.650' W: 1.041'.
BROKEN EMERGENCY LIGHT LENS GALLEY 1 AT FWD GALLEY 2025-340228<[01] REPLACED EMERGENCY LIGHT LENS GALLEY 1 AT FWD GALLEY IAW B737-700 AMM 33-51-01-960-801 STEP 2.C (4);[02] REPLACED EMERGENCY LIGHT LENS GALLEY 1 AT FWD GALLEY IAW B737-700 AMM 33-51-01-960-801 STEP 2.C (4)
CRACK ON CARGO TRACK LOCATED BS 747 RBL 13.84 WL 156.1 AT AFT CARGO COMPARTMENT 2025-340199<[01] EQUIPMENT P/N PHASEC 3D; S/N 800YBRK; DUE DATE 16-JUL-25 WAS USED ON STEP 6;[02] TOOL USED : EDDY CURRENT EQUIPMENT P/N NORTEC 600D S/N 210138103 DUE DATE : 10-JUN-25.;[03] PERFORMED PERMANENT REPAIR LOC. ON CARGO TRACK SECTION BETWEEN BS 727D TO BS 767 MORE 10? RBL 13.84 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR 3; SEE INDIVIDUAL SIGN OFF BELOW;[04] PERFORMED PERMANENT REPAIR LOC. ON CARGO TRACK SECTION BETWEEN BS 727D TO BS 767 MORE 10? RBL 13.84 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR 3;
BROKEN EMERGENCY LIGHT LENS SIDEWALL 231YHW AT PASSENGER CABIN 2025-340229<[01] REPLACED EMERGENCY LIGHT LENS SIDEWALL 231YHW AT PASSENGER CABIN I.A.W. B737-700 AMM 33-51-01-960-801 STEP 2. C. ITEM (1) AND (4).;[02] REPLACED EMERGENCY LIGHT LENS SIDEWALL 231YHW AT PASSENGER CABIN I.A.W. B737-700 AMM 33-51-01-960-801 STEP 2. C. ITEM (1) AND (4).
CRACK ON CARGO LINER SUPPORT ANGLE LOCATED BS 727B LBL 51 WL 201 AT AFT CARGO COMPARTMENT 2025-340192<[01] PERFORMED REPAIR ON CARGO LINER SUPPORT ANGLE LOCATED BS 727B LBL 51 WL 201 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-70-11-2R-0. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED
CRACK ACCESS PANEL 194GR BODY FAIRING AT LOWER FUSELAGE 2025-340197<[01] REJECT STEP 10. BECAUSE THE REPAIR PLIES INSTALLED DO NOT MEET THE OVERLAP REQUIREMENTS IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2>CURED THE REPAIR PLIES AND PERFORMED POST REPAIR INSPECTION (TAP TEST) ON REPAIRED AREA AND FOUND IN GOOD CONDITIONS IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2 PARAGRAPH 4.I;J AND B737-700 SRM 51-70-04-2R-0 REPAIR GENERAL PARAGRAPH 4.N AND O.(1); B737-700 NDT MANUAL PART1 51-05-01. TOOL USED: HOT BONDER P/N:HCS9200B-AV S/N:18196021 DUE DATE: 22-FEB-26. CURED TIME: 220 MINUTES AT 200 DEGREES FAHRENHEIT.;[03] VERIFIED CORRECTION IN C/A # 2 HUGO TEJADA ( TECHNICIAN). REMOVE AND INSTALL NEW REPAIR PLIES. THE PROCESS IS DOCUMENTED IN PARTIAL WORK STEPS 11 TO 14.<BR> <BR>CURED THE REPAIR PLIES AND PERFORMED POST REPAIR INSPECTION (TAP TEST) ON REPAIRED AREA AND FOUND IN GOOD CONDITIONS IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2 PARAGRAPH 4.I;J AND B737-700 SRM 51-70-04-2R-0 REPAIR GENERAL PARAGRAPH 4.N AND O.(1); B737-700 NDT MANUAL PART1 51-05-01. TOOL USED: HOT BONDER P/N:HCS9200B-AV S/N:18196021 DUE DATE: 22-FEB-26. CURED TIME: 220 MINUTES AT 200 DEGREES FAHRENHEIT.;[04] REPAIRED ACCESS PANEL 194GR BODY FAIRING AT LOWER FUSELAGE IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] REPAIRED ACCESS PANEL 194GR BODY FAIRING AT LOWER FUSELAGE IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2025-340205<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 146A7901; SHEET: 66; REV A:. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 146A7901; SHEET: 66; REV A:. SEE INDIVIDUAL SIGN OFF BELOW
CRACK ON CARGO TRACK LOCATED BS 727E RBL 13.84 WL 156.1 AT AFT CARGO COMPARTMENT 2025-340201<[01] PERFORMED PERMANENT REPAIR ON CARGO TRACK SECTION BETWEEN BS 727D TO BS 767 MORE 10? RBL 13.84 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR 3; TASK CARD COMPLETED IN TTG8Q010SMEX. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1:<BR>REFER TO FAULT TTG8Q010SMEX WHERE PERMANENT REPAIR WAS PERFORMED;[03] REFER TO FAULT TTG8Q010SMEX WHERE PERMANENT REPAIR WAS PERFORMED
BROKEN EMERGENCY LIGHT LENS LAV A AT FWD GALLEY AREA 2025-340227<[01] REPLACED EMERGENCY LIGHT LENS LAV A AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 STEP 2.C (4);[02] REPLACED EMERGENCY LIGHT LENS LAV A AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 STEP 2.C (4)
CRACK ON SUPPORT ANGLE LOCATED AFT FACE BS 500D AT LEVEL STR 28L AT FWD CARGO COMPARTMENT 2025-340160<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AFT FACE BS 500D AT LEVEL STR 28L AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9AND DWG 14347902 SHEET 126 REV. A <BR><BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED AFT FACE BS 500D AT LEVEL STR 28L AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9AND DWG 14347902 SHEET 126 REV. A <BR><BR>SEE INDIVIDUAL SIGN OFF BELOW
CRACK GUSSET LOCATED BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT 2025-340143<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7902; SHEET: 209; REV: -. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED GUSSET AND FASTENERS LOCATED BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7902; SHEET: 209; REV: -. SEE INDIVIDUAL SIGN OFF BELOW
CRACK ON ANGLE FWD FACE LOCATED BS 500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2025-340144<[01] REPLACED ANGLE FWD FACE LOCATED BS 500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 SRM 51-40-05; SRM 51-20-01 AND DWG 143A7505 SHEET 118 REV ?-? <BR>MATERIAL USED: P/N: 594418 (BONDERITE) PO: 2025 140606; P/N: 10P4-2+EC-117S (PRIMER) PO: 2025 148089.<BR><BR>MEASURE OF CRACK IS L: 0.667 IN.
CRACK ON SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN 2025-340131<[01] REPLACED SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 273A9110 SHEET: 6 REV: A<BR>SEE INDIVIDUAL SIGN OF BELOW;[02] REPLACED SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 273A9110 SHEET: 6 REV: A<BR>SEE INDIVIDUAL SIGN OF BELOW AS RII
WEAR NUT IN ASSIST HANDLE AT FWD ENTRY DOOR (4EA) 2025-340117<[01] REPLACED NUT IN ASSIST HANDLE AT FWD ENTRY DOOR IAW B737-700 AMM 52-41-31-400-802 STEP 3.F.(2).;[02] CORRECTED STEP 1<BR>REPLACED NUT IN ASSIST HANDLE AT FWD ENTRY DOOR IAW B737-700 AMM 52-11-31-400-802 STEP 3.G.(2).;[03] REPLACED NUT IN ASSIST HANDLE AT FWD ENTRY DOOR (4EA) IAW B737-700 AMM 52-11-31-400-802 STEP 3.G.(2).
WEAR NUT IN ASSIST HANDLE AT AFT ENTRY DOOR 2025-340119<[01] REPLACED NUT IN ASSIST HANDLE AT AFT ENTRY DOOR IAW B737-700 AMM 52-41-31-400-802 STEP 3.F.(2).;[02] COREE STEP 1 <BR>REPLACED NUT IN ASSIST HANDLE AT AFT ENTRY DOOR IAW B737-700 AMM 52-13-31-400-802 STEP 3.G.(2).;[03] REPLACED NUT IN ASSIST HANDLE AT AFT ENTRY DOOR IAW B737-700 AMM 52-13-31-400-802 STEP 3.G.(2).
WEAR NUT IN ASSIST HANDLE AT FWD SERVICE DOOR (2EA) 2025-340118<[01] REPLACED NUT IN ASSIST HANDLE AT FWD SERVICE DOOR IAW B737-700 AMM 52-41-31-400-802 STEP 3.F.(2).;[02] REPLACED NUT IN ASSIST HANDLE AT FWD SERVICE DOOR IAW B737-700 AMM 52-41-31-400-802 STEP 3.F.(2).
WEAR NUT IN ASSIST HANDLE AT AFT SERVICE DOOR (2EA) 2025-340120<[01] REPLACED NUT IN ASSIST HANDLE AT AFT SERVICE DOOR IAW B737-700 AMM 52-41-31-400-802 STEP 3.F.(2).;[02] REPLACED NUT IN ASSIST HANDLE AT AFT SERVICE DOOR IAW B737-700 AMM 52-41-31-400-802 STEP 3.F.(2).
CRACK GUSSET LOCATED BS 500D AT LEVEL STR 19R AT FWD CARGO COMPARTMENT 2025-340139<[01] REPLACED GUSSET LOCATED BS 500D AT LEVEL STR 19R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 DWG: 143A7902 SHEET: 209 REV: -. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED GUSSET LOCATED BS 500D AT LEVEL STR 19R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 DWG: 143A7902 SHEET: 209 REV: -. SEE INDIVIDUAL SIGN OFF BELOW
BROKEN PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN (6 EA) 2025-340077<[01] REPLACED PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN (6 EA) I.A.W BOENG SOPM 20-50-12 REV. 57 AND DWG 33500007 REV. 2 SHEET 2;[02] REPLACED PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN (6 EA) I.A.W BOENG SOPM 20-50-12 REV. 57 AND DWG 33500007 REV. 2 SHEET 2;[03] CORRECTED STEP 1 <BR>REPLACED PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN (6 EA) I.A.W B737-AMM 33-51-15-400-802 STEP 1.E.(1) AND 1.E.(5); SOPM 20-50-12 REV. 57;[04] CORRECTED STEP 2<BR><BR>REPLACED PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN (6 EA) I.A.W B737-AMM 33-51-15-400-802 STEP 1.E.(1) AND 1.E.(5); SOPM 20-50-12 REV. 57
CUSTOMER REQUEST CRACK ON EXTERNAL POWER LOWER CUT OUT AT LOWER FUSELAGE 2025-340087<[01] EQUIPMENT P/N PHASEC 3D; S/N 800YBRK; DUE DATE 16-JUL-25 WAS USED ON STEP 4;[02] PERFORMED REPAIR LOCATED EXTERNAL POWER LOWER CUT OUT AT LOWER FUSELAGE IAW B737-700 SRM 53-10-15-2R-4 REPAIR 4. <BR><BR>SEE INDIVIDUAL SING-OFF BELOW.;[03] PERFORMED REPAIR LOCATED EXTERNAL POWER LOWER CUT OUT AT LOWER FUSELAGE IAW B737-700 SRM 53-10-15-2R-4 REPAIR 4.AS RII
BROKEN PHOTOLUMINESCENT STRIP LH SIDE AT PASSENGER CABIN (5 EA) 2025-340078<[01] REPLACED PHOTOLUMINESCENT STRIP LH SIDE AT PASSENGER CABIN (5 EA) I.A.W BOENG SOPM 20-50-12 REV. 57 AND DWG 33500007 REV. 2 SHEET 2;[02] CORRECTED STEP 1<BR>REPLACED PHOTOLUMINESCENT STRIP LH SIDE AT PASSENGER CABIN (5 EA) I.A.W B737-700 AMM 33-51-15-400-802 STEP 1.E.(1) AND 1.E.(5);[03] REPLACED PHOTOLUMINESCENT STRIP LH SIDE AT PASSENGER CABIN (5 EA) I.A.W B737-700 AMM 33-51-15-400-802 STEP 1.E.(1) AND 1.E.(5)
CRACK ON BREAK PANEL (INTERCOSTAL) LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN 2025-340108<[01] REPLACED BREAK PANEL (INTERCOSTAL) AND FASTENERS LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-40-05 ITEM 9; SRM 51-40-02 AND DWG 143A0060 SHEET 46 REV. -;LENGTH OF CRACK IS:1.208 TOOL USED: 500-197-30; S/N: A23334861; DUE DATE: 03-SEP-25. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED BREAK PANEL (INTERCOSTAL) AND FASTENERS LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-40-05 ITEM 9; SRM 51-40-02 AND DWG 143A0060 SHEET 46 REV. -;LENGTH OF CRACK IS:1.208 TOOL USED: 500-197-30; S/N: A23334861; DUE DATE: 03-SEP-25. SEE INDIVIDUAL SIGN OFF BELOW.
CRACK STUB FRAME LOCATED ON BS 296.5 BTW STR 8R TO STR 9R UPPER POSITION AT FWD GALLEY AREA 2025-340106<[01] REPLACED STUB FRAME LOCATED ON BS 296.5 BTW STR 8R TO STR 9R UPPER POSITION AT FWD GALLEY AREA IAW. B737-700 SRM 51-40-02 AND DWG 141A8370 SHEET 9 REV:D AND 141A8380. SHEET 20 REV:-. <BR><BR>SEE INDIVIDUAL SING-OFF BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED STUB FRAME LOCATED ON BS 296.5 BTW STR 8R TO STR 9R UPPER POSITION AT FWD GALLEY AREA IAW. B737-700 SRM 51-40-02 AND DWG 141A8370 SHEET 9 REV:D AND 141A8380. SHEET 20 REV:-. <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[03] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.
#6 AFT FAIRING TAIL CONE IS CRACKED AND DELAMED<[01] REMOVED AND REPLACED TAIL CONE ON #6 AFT FAIRING REF AMM 27-51-18.
RH OVERWING EXIT EMERGENCY LIGHT INOP<[01] RELAMPED PER AMM 33-51-01
RIGHT WING FAIRING SUPPORT FRAME CRACKED AT PANEL 191AR AND WING LEADING EDGE.<[01] REMOVED WING TO BODY PANELS 191AR AND 195AR TO FOM.;[02] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[03] INSPECTED REMOVAL AND REPLACEMENT OF RIGHT WING FAIRING SUPPORT FRAME PER [SRM 51-40-02);[04] REINSTALLED BODY PANELS 191AR & 195AR PER AMM 53-51-21.
R1 DOOR HANDLE INSERT STUD IS BROKEN OFF<[01] REMOVED AND REPLACED R1 DOOR HANDLE INSERT PER AMM 52-31-41
FWD CARGO COMPARTMENT FLOOR BOARD CRACKED APPROX 6.5IN<[01] REMOVED CARGO PANEL PER AMM 25-52-10. INSTALLATION STILL REQUIRED.;[02] INSTALLED FWD CARGO FLOOR PANEL IAW AMM 25-52-10.
BULL NOSE EMERGENCY LIGHT LOOSE @ SEAT 14ABC<[01] REPLACED BULL NOSE EMERGENCY LIGHT LENS AT 14CBA. REF. AMM 33-51-03.
#2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMB OUT. RAN QRH CHECKLIST; LIGHT EXTINGUISHED WHEN THROTTLE WAS RETARDED TO IDLE. RETURNED TO DAL<[01] REMOVED AND REPLACED #2 ENGINE R/H CORE FIRE DETECTOR PER AMM 26-11-01. OPS CHECK GOOD.
L1 DOOR SLIDE DISLODGED<[01] RESECURED L1 DOOR SLIDE IRW MT 725-61-06
R2 DOOR EMERGENCY ESCAPE SLIDE AFT GIRT BAR HOLD BRACKET BOLT BROKEN.<[01] REPLACED BROKEN BOLT PER SRM 51-40-02
AFT GALLEY SERVICE DOOR HANDLE CAM LOOSE<[01] 04 - REPAIRED PER [AMM 20-50-11-910-801-NG (STANDARD TORQUE VALUES - PERMANENT)]AFT GALLEY DOOR HANDLE
LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-400-802-NG (STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL INSTALLATION - PERMANENT)] LEFT HORIZONTAL STABILIZER
RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] R&R RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL. IAW AMM 53-31-31
EMX BATT PACK M01673 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATT M01673 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
AFT GALLEY SERVICE DOOR LOWER GATE BRACKET CRACKED<[01] 01 - REMOVED AND REPLACED PER [AMM 52-41-31-400-802-NG (GALLEY SERVICE DOOR LINING INSTALLATION - PERMANENT)]AFT GALLEY SERVICE DOOR LOWER GATE BRACKET
FWD AREA EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED FWD LH EMERGENCY LIGHT BATTERY PACK IAW B737 AMM 33-51-06. OPS CHECK GOOD
FWD ENTRY DOOR SLIDE SLID OUT OF BUSSEL AT GATE<[01] REMOVED AND REPLACED FWD ENTRY ESCAPE SLIDE ASSY. PER T/C 725-61-06-FE AND AMM 25-66-01.
ROW #6 R/H AISLE EMERGENCY LIGHTS IS OUT<[01] R&R R/H ROW #6 AISLE EMERGENCY LIGHT IAW AMM 33-51-03. OPS CHECK GOOD.
NOSE GEAR DIAGREE LIGHT WHEN LANDING GEAR LEVER PLACED IN OFF. NOSE GEAR FELL BACK DOWN. PER RH RAISING GEAR LEVER CAUSED NOSE GEAR TO RETRACT. PER QRH LEFT LEVER IN THE UP POSITION; NO FURTHER ISSUES<[01] TROUBLE SHOT PER FIM 32-30 TASK 809. JACKED AIRCRAFT AND SWUNG GEAR SEVERAL TIMES. GEAR OPERATED CORRECTLY PER AMM 32-32-00 AND 32-33-00.
EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1668 ARE INOP<[01] UPDATED PAPERWORK;[02] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1668 AND TEST GOOD IAW AMM 33-51-06-960-805.;[03] VERIFIED REMOVAL AND REPLACEMENT OF EMERGENCY EXIT LIGHT BATTERY PACK M1668 AND TEST GOOD IAW AMM 33-51-06-960-805.;[04] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2. TASK CARD COMPLETE.
FOUND EMERGENCY EXIT LIGHT LENS LOCATED AT FED LAV A AFT FACE TO BE ILLEGIBLE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENS LOCATED AT FED LAV A AFT FACE IAW AMM 33-51-14-960-802. OPS CHECK GOOD;[02] VERIFIED CORRECTIVE ACTION 1.
R/W T/E PANEL 651FB FWD SIDE 3RD BRACKET FROM O/B END IS BROKEN<[01] REMOVED R/W T/E PANEL 651FB FWD SIDE 3RD BRACKET FROM O/B END PER SRM 51-40-02-0G-0. STEP 4.;[02] INSTALLED R/W T/E PANEL 651FB FWD SIDE 3RD BRACKET FROM O/B END IAW SRM 51-40-02-0G-0 STEP 4.;[03] VERIFIED CORRECTIVE ACTION 1.
CABIN SEAT TRACK IS CORRODED AT BS 685+9; 727; 727+10; 727A+7; LBL 25; WL 208<[01] VERIFIED APPLICABILITY FOR SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1- SEAT TRACKS11] INSTALLED NEW SEAT TRACK AT BS540 - BS727B; LBL25; WL208; PER SRM 51-40-02-0G-0 AND BOEING DWG 144A5300. USED TOOL ID: ATS2470 DUE DATE: 02/29/24.;[12] VERIFIED CORRECTIVE ACTION #11;[13] FLOOR PANELS #231YF; 231XF; 241BF; 241AF; 241EF; 241DF IAW SRM 51-40-02-0G-0 TO BE INSTALLED ON CARD # TTG8Q00LXSKA;[14] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 13
CABIN SEAT TRACK IS CORRODED AT BS 827+15; 847+8; LBL 25; WL 208<[01] VERIFIED APPLICABILITY FOR SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 - SEAT TRACKS.;[11] LOCATE DAN DRILLED NEW SETA TRACK AT LBL 25 BS 727B TO BS767 PER SRM 51-40-05-0G-0 AND DWG 146A5300. OK TO INSTALL;[12] RECEIVED ATSHFAB-100-316 SEAT TRACK. FABRICATED IAW BOEING DRAWING ATSHFAB-100-316. JOB # 531818;[13] ACCOMPLISHED CONFORMITY INSPECTION ON ATS HFAB 100-316; TRACK CONFORMS TO ATS DRAWING ATS HFAB 100-316.;[14] VERIFIED CORRECTIVE ACTION STEP 11. VERIFIED OK TO INSTALL.;[15] INSTALLED SEAT TRACK AT LBL 25 FROM BS 727C TO BS887 PER SRM 51-40-02-0G-0 AND BOEING DWG 146A5300. USED TOOL ID: ATS1299 DUE DATE: 12/31/23.;[16] VERIFIED CORRECTION ACTION ITEM 15 SEAT TRACK INSTALLATION.;[17] REMOVED FOD PROTECTION FROM LBL 10 TO LBL 45 BS 727B TO BS 887 PER AMM 20-60-07-913-801.;[18] OK TO INSTALL FLOOR PANELS 241LF;241KF;241PF;241NF;241SF;241RF241VF;241UF;[19] PANELS TO BE INSTALLED ON CARD #TTG8Q00LXRWN;[20] CERTIFY CORRECTIVE ACTION #19;[21] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 17-19
PANEL 621YB I/B CORNER IS CRACKED.<[01] PERFORMED PARTIAL WORK ON STEPS 3 AND 4.;[02] COMPLETED STEPS 1; 4; 5;[03] COMPLETED STEPS 6 AND 8; PARTIAL UPDATE STEPS 7 AND 9;[04] CORRECTION TO STEP 12 ITEM 1.;[05] CORRECTION TO STEP 12 ITEM 2.;[06] PANEL 621YB WITH I/B CORNER IS CRACKED WAS REPAIR IAW SRM 51-70-05-2R-6.;[07] FINAL INSPECTION. PANEL REPAIRED PER SRM 51-70-05.
B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 45; W.L. 165.<[01] UPDATED STEP 1 AND 2;[17] FABRICATED SPLICE REPAIR FROM 2024 T3 0.071' LOT. 1508358-1 IAW SRM 57-10-10-2R-5; APPLIED CHEMICAL CONVERSION IAW SOPM 20-43-03; REQ. OR TO PRIME;[23] INSTALLED ALL FASTENERS COMMON TO FUER TANK IAW SRM 57-10-10-2R-5 AND DWG 111A1000 REV:A;[24] VERIFIED CORRECTIVE ACTION ITEM 23.;[25] PARTIAL ENTRY STEPS 3;5;6.;[26] REQUEST OK TO INSTALL FASTENERS AT REPAIR ANGLE BETWEEN LBL 25 TO LBL 55 ; BS 663 ; WL 167.;[27] OK TO INSTALL FASTENERS AT REPAIR ANGLE BETWEEN LBL 25 TO LBL 55 ; BS 663 ; WL 167 GIVEN; AND PARTIAL UPDATED STEPS 3;5;6.;[28] UPDATE STEPS 3;5 AND 6.;[29] INSTALLED NEW FASTENERS AT REPAIR ANGLE BETWEEN LBL 25 TO LBL 55 ; BS 663 ; WL 167 IAW SRM 57-10-1--2R-5 REPAIR 5 AND DWG:111A1000;[30] OK TO APPLY CAP SEAL AT FASTENERS AFT SIDE L/H VAPOR BARRIER BS 663
FWD CARGO; FWD CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON RADIUS OF FWD CARGO FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARAGRAPH 4.B. (2) AND (4)<BR>EQUIP USED: WELDING MACHINE E10583; CAL DUE DATE 01/2024;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] PENETRANT INSPECTED WELD PER SOPM 20-20-02. NO DEFECTS FOUND.;[04] FWD CARGO; FWD CORNER SCUFF PLATE WAS REMOVED AND WILL BE INSTALLED ON FAULT TTG8Q002KE0U<BR>FAULT TTG8QOOLW7K6 COMPLETED;[05] VERIFIED CORRECTIVE ACTION 4.
#1 SLAT BULL NOSE IS CRACKED AT FASTENER ATTACH POINT.<[01] COMPLETED STEP 1.;[12] INSTALLED REPAIR PARTS [1] DOUBLER [2] FILLER PER SRM 57-42-01-2R-8 FIG 202 ALTERNATIVE 1 - SHEET 1 AND SRM 51-40-02-0G-0.;[13] UPDATED STEPS 2 TO 6. (REQUEST OK TO INSTALL);[14] VERIFIED CORRECTIVE ACTION #13;[15] VERIFIED CORRECTIVE ACTION #12;[16] UPDATED STEPS 2 TO 6.;[17] COMPLETED STEPS 2-6;[18] UPDATED NEASUREMENT TABLE.;[19] VERIFIED MEASUREMENTS;[20] CARD COMPLETED.
LOSS OF HYDRAULIC B ON FINAL; EMERGENCY DECLARED.<[01] REMOVED AND REPLACED #5 FLIGHT SPOILER DUE TO LEAKING IAW AMM 27-61-51; ALSO R&R #2 ENGINE HYDRAULIC PUMP; B ELECTRIC HYDRAULIC PUMP; AND HYDRAULIC FILTERS CHANGED PRECAUTIONARY IAW AMM 29-11-21;AMM 29-11-11; AMM 29-11-51 AMM 29-11-41;[02] VERIFIED #5 FLIGHT SPOILER ACTUATOR REMOVAL AND INSTALLATION
LOSS OF HYDRAULIC B ON FINAL; EMERGENCY DECLARED.<[01] REMOVED AND REPLACED #5 FLIGHT SPOILER DUE TO LEAKING IAW AMM 27-61-51; ALSO R&R #2 ENGINE HYDRAULIC PUMP; B ELECTRIC HYDRAULIC PUMP; AND HYDRAULIC FILTERS CHANGED PRECAUTIONARY IAW AMM 29-11-21;AMM 29-11-11; AMM 29-11-51 AMM 29-11-41;[02] VERIFIED #5 FLIGHT SPOILER ACTUATOR REMOVAL AND INSTALLATION
LOSS OF HYDRAULIC B ON FINAL; EMERGENCY DECLARED.<[01] REMOVED AND REPLACED #5 FLIGHT SPOILER DUE TO LEAKING IAW AMM 27-61-51; ALSO R&R #2 ENGINE HYDRAULIC PUMP; B ELECTRIC HYDRAULIC PUMP; AND HYDRAULIC FILTERS CHANGED PRECAUTIONARY IAW AMM 29-11-21;AMM 29-11-11; AMM 29-11-51 AMM 29-11-41;[02] VERIFIED #5 FLIGHT SPOILER ACTUATOR REMOVAL AND INSTALLATION
LOSS OF HYDRAULIC B ON FINAL; EMERGENCY DECLARED.<[01] REMOVED AND REPLACED #5 FLIGHT SPOILER DUE TO LEAKING IAW AMM 27-61-51; ALSO R&R #2 ENGINE HYDRAULIC PUMP; B ELECTRIC HYDRAULIC PUMP; AND HYDRAULIC FILTERS CHANGED PRECAUTIONARY IAW AMM 29-11-21;AMM 29-11-11; AMM 29-11-51 AMM 29-11-41;[02] VERIFIED #5 FLIGHT SPOILER ACTUATOR REMOVAL AND INSTALLATION
R/H ENGINE PYLON AFT TRAILING WEDGE PANEL CRACKED. / [01] REMOVED AND REPLACED R/H ENGINE PYLON AFT TRAILING WEDGE PANEL ASSY. IAW SRM. 51-40-02.
MID CABIN CEILING EXIT ROW SIGN COVER LENS POPPED OFF / [01] RESECURED SIGN LENS PER AMM 33-51-01
AFT SERVICE DOOR EVACUATION SLIDE IS COMING OUT OF STOWAGE CONTAINER / [01] RESECURED VELCRO PER AMM 25-66-01
HFEC CRACK INDICATION FOUND ON 2 EACH HOLES ON LOWER FLANGE OF L/H STAB #5 INSPAR RIB. ; / [01] CUT OUT THE DAMAGED AREA PER SRM 55-10-09-2R-5 REPAIR 5.; [02] FABRICATED REPAIR PARTS PER SRM 55-10-09-2R-5 REPAIR 5.; [03] C/W HFEC OF DAMAGE CUTOUT PER NDT PART 6; 51-00-00 PROC 23. NO DEFECTS FOUND.<BR><BR>C/W HFEC OF EXISTING HOLES PER NDT PART 6; 51-00-00 PROC 16. NO DEFECTS NOTED.; [04] PERFORMED GENERAL VISUAL INSPECTION OF REPAIR AREA PER SRM 55-10-09-2R R5. NO DEFECTS FOUND.<BR>OK TO PRIME AND INSTALL REPAIR PARTS.; [05] SEE TTG8Q006PR6N FOR INSTALLATION OF REPAIR PARTS AND OK TO RE-INSTALL STAB RIB; [06] REINSTALLED RIB PER SRM 51-0-02. SEE TTG8Q006PR6N .; [07] VERIFIED RIB INSTALLATION PER SRM 51-00-02 ON NON ROUTINE TTG8Q006PR6N
L/H STAB; #5 INSPAR RIB (STAB STA. 129.5); HAS CRACK ON THIRD VERTICAL STIFFENER APPROX. 1 INCH FROM BOTTOM OF RIB. ; / [01] REMOVED L/H STAB RIB AT (STB STA. 1295) PER SRM 55-10-09-2R-4 AND SRM 51-40-02.; [02] REMOVED DAMAGED PER SRM 55-10-09-2R-4 REPAIR 4.; [03] C/W HFEC INSPECTION OF CUT EDGES OF THE STIFFENER AND WEB IAW NDT PART 6; 51-00-00 PROC 23. NO DEFECTS FOUND.<BR><BR>C/W HFEC HOLE PROBE INSPECTION OF EXISTING FASTENER HOLES IAW NDT PART 6; 51-00-00 PROC 16. FOUND CRACK INDICATION ON 2 EA HOLES ON LOWER FLANGE. REF NRC TTG8Q006Q83P.; [04] PERFORMED GENERAL VISUAL INSPECTION OF ALL AREAS WITHIN REPAIR AREA PER SRM 55-10-09-2R-4. NO DEFECTS FOUND.; [05] REPAIR REF. CHANGE TO SRM 55-10-09-2R-5 SEE FAULT TTG8Q006Q83P.; [06] FABRICATED REPAIR PARTS PER SRM 55-10-09-2R-5 REPAIR 5. ON FAULT TTG8Q006Q83P.; [07] OK TO PRIME AND INSTALL REPAIR PARTS.; [08] INSTALLED REPAIR (WET WITH BMS 5-95 SEALANT) PER SRM 55-10-09-2R-5 REPAIR 5; [09] INSTALLED REPAIR (WET WITH BMS 5-95 SEALANT) PER SRM 55-10-09-2R-5 REPAIR 5. VERIFIED; [10] OK TO REINSTALL RIB; [11] INSTALLED RIB PER SRM 51-40-02; [12] VERIFIED RIB INSTALLATION PER SRM 51-40-02; [13] VERIFIED L/H STAB RIB REPLACEMENT AT STAB STA 129.5 PER SRM 51-40-02
L/H AFT ESCAPE SLIDE LIGHT L732 IS INOP ; / [01] RELAMPED L/H AFT ESCAPE SLIDE LIGHT L732 AND PERFORMED SATISFACTORY OPERATIONAL TEST PER AMM 33-51-04-960-801.; [02] VERIFIED RELAMPED L/H AFT ESCAPE SLIDE LIGHT L732 AND PERFORMED SATISFACTORY OPERATIONAL TEST PER AMM 33-51-04-960-801.
BULKHEAD SUPPORT BRACKET IS CRACKED BS 727+4'; RBL 3; WL 160 ; / [01] UPDATED MEASUREMENTS TAB; [02] REMOVED CRACKED BULKHEAD SUPPORT BRACKET; BS 727+4; RBL3; IAW SRM 51-40-02-0G-0; LOCATED; DRILLED AND INSTALLED NEW BULKHEAD BRACKET ; IAW SRM 51-40-02-0G-0;SRM 51-40-05-0G-0; DWG144A2600;.; [03] VERIFIED REMOVED CRACKED BULKHEAD SUPPORT BRACKET; BS 727+4; RBL3; IAW SRM 51-40-02-0G-0; LOCATED; DRILLED AND INSTALLED NEW BULKHEAD BRACKET ; IAW SRM 51-40-02-0G-0;SRM 51-40-05-0G-0; DWG144A2600;.
CRACK ON DOUBLER ON FWD SIDE OF L/H BS663 VAPOR BARRIER AT LBL25 WL146 ; / [01] REMOVED DOUBLER ON FWD SIDE OF VAPOR BARRIER BS 663 LBL6-31 IAW SRM 51-40-02-0G-0.; [02] INSTALLED 100% TEMPORARY FASTENERS ON AFT SIDE OF DOUBLER REPAIR AREA (VERTICAL STIFFENERS BS 663 LBL6;25-31)BEFORE SQUEEZE OUT TIME EXPIRED APPLIED BMS5-95 C-20 JUL-05-2021 UTC 14:00 HRS EXPIRATION TIME JUL-06-2021 UTC 10:HRS. IAW SOPM 20-50-19.; [03] VERIFIED INSTALLED 100% TEMPORARY FASTENERS ON AFT SIDE OF DOUBLER REPAIR AREA (VERTICAL STIFFENERS BS 663 LBL6;25-31)BEFORE SQUEEZE OUT TIME EXPIRED APPLIED BMS5-95 C-20 JUL-05-2021 UTC 14:00 HRS EXPIRATION TIME JUL-06-2021 UTC 10:HRS. IAW SOPM 20-50-19.; [04] COMFORMED NEW DOUBLER AND VERIFIED HEAT TREATMENT FABRICATION MAT. USED 2024 T42 CLAD 0.040' LOT#1391616-1 R.O 829384-SWA; LOCATED;DRILLED APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW .BAC 5602;DWG 111A1511;111A1000;11A1001 AND SRM 51-40-05-0G-0. OK TO INSTALL.; [05] INSTALLED NEW DOUBLER AT VAPOR BARRIER BS663 LBL6-31 IAW DWG 111A1511;111A1000;11A1001 AND SRM 51-40-02-0G-0.; [06] VERIFIED FABRICATION; LOCATE-AND-DRILL AND CHEM CONVERSION COATING AND PRIMER; VERIFIED INSTALLATION OF NEW DOUBLER AT VAPOR BARRIER BS663 LBL6-31 IAW DWG 111A1511;111A1000;11A1001 AND SRM 51-40-02-0G-0; [07] VERIFIED ALL WORK COMPLETED THIS TASK
FWD SIDE OF BS 663 VAPOR BARRIER RH SIDE UPPER ATTACH ANGLE UPPER END CRACKED BS663; RBL8; WL167. / [01] UPDATED MEASUREMENT TABLE; [02] CONFORMED -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE PER SRM 57-10-10-2R-5 THE -1 REPLACEMENT ANGLE FABRICATED IN ACCORDANCE WITH SRM 57-10-10-2R REPAIR 5 REFER TO ATS BUILD RECORD ATSHFAB-101-354 JOB # 539510 THE -2 SPLICE ANGLE FABRICATED IN ACCORDANCE WITH SRM57-10-10-2R-5 REFER TO ATS BUILD RECORD ATSHFAB-101-355 JOB # 539866; [03] CONFORMED -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE PER SRM 57-10-10-2R-5 THE -1 REPLACEMENT ANGLE FABRICATED IN ACCORDANCE WITH SRM 57-10-10-2R-5 REFER TO ATS BUILD RECORD ATSHFAB-101-354 JOB # 539510 THE -2 SPLICE ANGLE FABRICATED IN ACCORDANCE WITH SRM 57-10-10-2R-5 REFER TO ATS BUILD RECORD ATSHFAB-101-355 JOB # 539866; [04] REMOVED DAMAGED AREA AND PREPARED REPAIR AREA FOR INSPECTION BS 663 RBL6-14 WL 167 IAW SRM 57-10-10-2R-5.; [05] VERIFIED REMOVED DAMAGED AREA AND PREPARED REPAIR AREA FOR INSPECTION BS 663 RBL6-14 WL 167 IAW SRM 57-10-10-2R-5.;
CRACK ON DOUBLER ON FWD SIDE OF R/H BS 663 VAPOR BARRIER AT RBL 25 WL 146 ; / [01] RECEIVED FROM OSS NEW DOUBLER VERIFIED HEAT TREATMENT AND FABRICATION IAW DWG 111A1511-28 AND BAC 5602 MAT. USED 2024 T42 0.040' LOT#1453744-1; LOCATED AND DRILLED;APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-40-05-0G-0 AND DWG 111A1000.; [02] OK TO INSTALL.; [03] VERIFIED CORRECTIVE ACTION ITEM 1. SEE PO NO. 828953-SWA FOR FABRICATION AND HEAT TREAT.<BR><BR>OK TO INSTALL; [04] INSTALLED 100% OF TEMPORARY FASTENERS ON DOUBLER REPLACEMENT AREA BEFORE SQUEEZE OUT TIME EXPIRE SEALANT BMS 5-95 C-20 MIXED 17:50 HRS 02/JUL/21; TIME EXPIRE 03/JUL/21 13:50 HRS. IAW SOPM 20-50-19.; [05] VERIFIED DOUBLER AREA FASTENERS BEFORE SQUEEZE OUT; [06] INSTALLED DOUBLER AT BS 663 RBL 6-25 IAW SRM 51-40-02-0G-0 AND DWG 111A1001;111A1000.; [07] RII VERIFIED INSTALLED; [08] ALL STEPS COMPLETED FOR DOUBLER ON FWD SIDE RH BS 663 VAPOR BARRIER RBL25 WL146.; [09] VERIFIED RII STEPS COMPLETE; [10] VERIFIED ALL STEPS COMPLETE.
REJECT- PANEL 193AR INCORRECT REPAIR PERFORMED DUE TO DAMAGE THROUGH BOTH SKINS AND CORE; REPAIR FOR DAMAGE THROUGH ONE SKIN AND CORE WAS PERFORMED ; / [01] IDENTIFIED PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 2. TABLE 2. ITEM 18. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.A.(5). <BR><BR>REPAIR IS TO BE ACCOMPLISHED IAW SRM 51-70-05-2R-4 PER SRM 53-40-70-2R-1 PARA 4.B.(1). AND TABLE 201. <BR><BR>REMOVED REJECTED REPAIR ACCOMPLISHED ON TTG8Q005K90D THEN CLEANED REPAIR AREA IAW SRM 51-70-05-2R-4 PARA 4.A.-B.; [02] CERTIFIED STEP 1 AND VALIDATED REPAIR PER SRM 51-70-05-2R-4; [03] VERIFIED; IDENTIFIED PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 2. TABLE 2. ITEM 18. [04] FABRICATED OUTER SURFACE REPAIR PLIES USING BMS8-79 CL3 ST.120 LOT# 1457859-1 AND INSTALLED USING BMS5-129 TY2 GR5 LOT# 1457270-4. FABRICATED CORE PLUG USING BMS8-124 CL4 TY5 GR3 LOT# 1153313 AND INSTALLED USING BMS5-90 TY3 CL1 GR50 LOT# 1461508-1. VACUUM BAGGED; CHECKED FOR LEAKS; CURED; UNBAGGED; LIGHTLY SANDED REPAIR AREA TO CONTOUR AND CLEANED IAW SRM 51-70-05-2R-4 PARA 4. C-H<BR><BR>HOT BONDER: ID- ATS532 S/N- 15092117<BR>VACUUM GAGE: ID- ATS2438 S/N- UNKNON; [12] PANEL 193AR WITH DAMAGE THROUGH BOTH SKINS AND CORE WAS REPAIRED IAW SRM 51-70-05-2R-4; [13] CERTIFIED STEPS 11 AND 12.; [14] VERIFIED WORK PERFORMED IN STEP 11 AND 12 PER SRM.
CRACK ON F.S.D. FWD BEAR STRAP; BS 294.5 +4; BETWEEN S-7R AND S-8R; WL 266 (MARKED) ; / [01] REMOVED STUB FRAME REVEAL FOR ACCESS PER SRM 51-40-02-0G-0; [02] ET INSPECTED IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR><BR>CAL ID ATS1465 N600; [03] UPON FURTHER INVESTIGATION CRACK FOUND ON STUB FRAME REVEAL DOOR SUPPRESSOR SEAL ONLY PART TO BE REPLACED PER SRM 51-10-02-0G-0 DUE TO NO ENTRIES FOUND ON SRM FOR CRACKS; [04] LOCATED AND DRILLED NEW REVEAL DOOR SEAL SUPPRESSOR PER SRM 51-40-05-0G-0 AND BOEING DWG 141A8370 OK TO INSTALL; [05] VERIFIED CRACK IS LIMITED TO SEAL SUPPRESSOR; VERIFIED LOCATE AND DRILL OF NEW SEAL SUPPRESSOR PER SRM 51-40-05 AND DWG 141A8370; OK TO INSTALL; [06] INSTALLED REVEAL DOOR SEAL SUPPRESSOR ON STUB FRAME BS294.5+4 BETWEEN STR7R-8R PER SRM 51-40-02-0G-0 AND BOEING DWG 141A8370; [07] VERIFIED INSTALLED REVEAL DOOR SEAL SUPPRESSOR ON STUB FRAME BS294.5+4 BETWEEN STR7R-8R PER SRM 51-40-02-0G-0 AND BOEING DWG 141A8370; [08] CRACK ON FSD FWD BEAR STRAP BS294.5+4 BETWEEN STR 7R-STR 8R WL266 FOUND TO BE ON STUB FRAME REVEAL DOOR SUPPRESSOR SEAL ONLY ; REMOVED REVEAL DOOR SEAL SUPPRESSOR AND INSTALLED A NEW I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8370; [09] VERIFIED CRACK ON FSD FWD BEAR STRAP BS294.5+4 BETWEEN STR 7R-STR 8R WL266 FOUND TO BE ON STUB FRAME REVEAL DOOR SUPPRESSOR SEAL ONLY ; REMOVED REVEAL DOOR SEAL SUPPRESSOR AND INSTALLED A NEW I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A8370
CORROSION ON SEAT TRACK CROWN IN WELL STA 465; LBL 45; WL 208 ; / [01] REMOVED CORROSION ON SEAT TRACK CROWN IN WELL STA 465; LBL 45; WL 208. MAX MATERIAL REMOVED IN WELL WAS; .006' 1' BY 1'. IN LIMITS PER SRM 53-00-52-1A-1; SRM 51-10-02-0G-0. MEASURED DEPTH WITH DIAL DEPTH GAUGE ID# ATS400; S/N UNKNOWN; EXPIRES 04/2022; [02] VERIFIED DAMAGE REMOVAL IN LIMITS PER SRM 53-00-52-1A-1; [03] TREATED AND PRIMED ON SEAT TRACK ON TOP AND WELL BS 465 LBL 45;WL 208 PER SRM 53-00-52-1A-1 STEP 2.B; [04] TREATED AND PRIMED ON SEAT TRACK ON TOP AND WELL BS 465 LBL 45;WL 208 PER SRM 53-00-52-1A-1 STEP 2.B; SRM 51-20-01-0G-0; SOPM 20-43-03; SOPM 20-41-04.; [05] VERIFIED TREATED AND PRIMED SEAT TRACK ON TOP AND WELL BS 465 LBL 45;WL 208 PER SRM 53-00-52-1A-1 STEP 2.B; SRM 51-20-01-0G-0; SOPM 20-43-03; SOPM 20-41-04.; [06] VERIFIED TREATED AND PRIMED SEAT TRACK ON TOP AND WELL BS 465 LBL 45;WL 208 PER SRM 53-00-52-1A-1 STEP 2.B; SRM 51-20-01-0G-0; SOPM 20-43-03; SOPM 20-41-04
CORROSION ON SEAT TRACK CROWN ON TOP AND IN WELL STA 492-520; LBL 25; WL 208 ; / [01] REMOVED CORROSION ON SEAT TRACK CROWN ON TOP AND IN WELL STA 492-520; LBL 25; WL 208. MAX MATERIAL REMOVED ON TOP WAS .025' .5' BY 2'; .003' 1' BY 1' IN WELL. OUT OF LIMITS PER SRM 53-00-52-1A-1; SRM 51-10-02-0G-0. MEASURED DEPTH WITH DIAL DEPTH GAUGE ID# ATS400; S/N UNKNOWN; EXPIRES 04/2022; [02] VERIFIED DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-00-52-1A-1; [03] REMOVED DAMAGED SEAT TRACK BS 480-520; LBL 25; WL 208 PER SRM 51-40-02-0G-0.; [04] SENT OSS REQUEST TO MACHINE AND ANODIZE REPLACEMENT SEAT TRACK BS 480-520; LBL 25; WL 208.; [05] LOCATED DRILLED AND COUNTERSUNK NEW SEAT TRACK FOR BS 480-520- LBL 25 WL 208 IAW SRM 51-40-05-0G-0 AND SRM 51-40-08-0G-0 OK TO PRIME; [06] RECEIVED NEW SEAT TRACK FROM OSS FABRICATED ON SWA #PO 829344 AND SULFURIC ACID ANODIZED ON SWA #PO 829392 ALL DATED 09 JUL 21; [10] INSTALLED NEW SEAT TRACK AT BS 480-520- LBL 25 WL 208 IAW SRM 51-40-02-0G-0 SOPM 20-50-01 AND BOEING DWG 143A5300;
CRACKED FLOOR SUPPORT UPPER ANGLE BS 380-400 LBL 13 WL 208. ; / [01] REMOVED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL1; WL 208 PER SRM 51-40-02-0G-0; [02] LOCATED/DRILLED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL13; WL 208 PER SRM 51-40-05-0G-0 AND DWG 143A5400. OK TO INSTALL; [03] REMOVED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL13; WL 208 PER SRM 51-40-02-0G-0; [04] CERTIFIED REMOVED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL13; WL 208 PER SRM 51-40-02-0G-0 AND LOCATED/DRILLED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL13; WL 208 PER SRM 51-40-05-0G-0 AND DWG 143A5400. OK TO INSTALL.; [05] UPDATED MEASUREMENT TABLE.; [06] VERIFIED LOCATE & DRILL OF FLOOR SUPPORT UPPER ANGLE BS380-400; LBL13; WL 208 PER SRM 51-40-05-0G-0 AND DWG 143A5400. OK TO INSTALL GIVEN.; [07] INSTALLED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL13; WL 208 PER SRM 51-40-05-0G-0 AND DWG 143A5400.; [08] CERTIFIED INSTALLED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL13; WL 208 PER SRM 51-40-05-0G-0 AND DWG 143A5400.; [09] VERIFIED REPLACEMENT OF FLOOR SUPPORT UPPER ANGLE; BS 380-400; LBL 13; WL 208 PER SRM 51-40-02 AND DWG 143A5400; [10] VERIFIED COMPLETION OF ALL STEPS.
CRACKED FLOOR SUPPORT UPPER ANGLE BS 380-400 LBL 1 WL 208. ; / [01] REMOVED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL1; WL 208 PER SRM 51-40-02-0G-0; [02] LOCATED/DRILLED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL1; WL 208 PER SRM 51-40-05-0G-0 AND DWG 143A5400. OK TO INSTALL; [03] CERTIFIED REMOVED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL1; WL 208 PER SRM 51-40-02-0G-0 AND REMOVED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL1; WL 208 PER SRM 51-40-02-0G-0.; [04] UPDATED MEASUREMENT TABLE.; [05] VERIFIED LOCATE & DRILL OF FLOOR SUPPORT UPPER ANGLE BS380-400; LBL1; WL 208 PER SRM 51-40-05-0G-0 AND DWG 143A5400. OK TO INSTALL GIVEN.; [06] INSTALLED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL1; WL 208 PER SRM 51-40-05-0G-0 AND DWG 143A5400.; [07] CERTIFIED INSTALLED FLOOR SUPPORT UPPER ANGLE BS380-400 LBL1; WL 208 PER SRM 51-40-05-0G-0 AND DWG 143A5400.; [08] VERIFIED REPLACEMENT OF FLOOR SUPPORT UPPER ANGLE; BS 380-400; LBL 1; WL 208 PER SRM 51-40-02 AND DWG 143A5400; [09] VERIFIED ALL WORK COMPLETE THIS TASK
CORROSION ON AFT SERVICE DOOR MOP SILL BS 960-986 RBL 52 WL 208. ; / [01] REMOVED CORROSION ON AFT SERVICE DOOR MOPSILL STA 960-986; RBL 52; WL 208. MAX MATERIAL REMOVED WAS .012' 1' BY 1' FROM .080'. OUT OF LIMITS PER SRM 53-70-15-01-1; SRM 53-70-15-1A-1; SRM 51-10-02-0G-0.; [02] VERIFIED REMOVED CORROSION ON AFT SERVICE DOOR MOPSILL STA 960-986; RBL 52; WL 208. MAX MATERIAL REMOVED WAS .012' 1' BY 1' FROM .080'. OUT OF LIMITS PER SRM 53-70-15-01-1; SRM 53-70-15-1A-1; SRM 51-10-02-0G-0.; [03] REMOVED DAMAGED AFT SERVICE DOOR MOP SILL PER SRM 51-40-02-0G-0.; [04] VERIFIED REMOVED DAMAGED AFT SERVICE DOOR MOP SILL PER SRM 51-40-02-0G-0.; [05] LOCATED AND DRILLED AND COUNTERSUNK NEW AFT SERVICE DOOR MOPSILL PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; DWG# 147A8501; REV A. OK TO INSTALL.; [06] VERIFIED CORRECTIVE ACTION ITEMS 3-5. OK TO INSTALL.; [07] ACCOMPLISHED PARTIAL INSTALLATION OF AFT SERVICE DOOR MOPSIL 100% TEMP OR PERMANENT FASTENERS INSTALLED WITHIN SEALANT SQUEEZE OUT TIME; [08] VERIFIED 100% TEMP OR PERMANENT FASTENERS INSTALLED WITHIN SEALANT SQUEEZE OUT TIME; [09] COMPLETED INSTALLATION OF NEW AFT SERVICE DOOR MOPSILL PER SRM 51-40-02-0G-0 AND BOEING DWG# 147A8501.; [10] VERIFIED INSTALLATION OF NEW ASD MOPSILL PER SRM 51-40-02-0G-0 AND BOEING DWG# 147A8501; VERIFIED REJECTION ISSUE CORRECTED ON OTHER TASK; [11] VERIFIED ALL WORK COMPLETE THIS TASK
CORROSION ON AFT ENTRY DOOR MOP SILL BS 964-986 LBL 52 WL 208. ; / [01] REMOVED CORROSION ON AFT ENTRY DOOR MOPSILL STA 964-986; LBL 52; WL 208. MAX MATERIAL REMOVED WAS .015' 1' BY 1' FROM .080'. OUT OF LIMITS PER SRM 53-70-15-01-1; SRM 53-70-15-1A-1; SRM 51-10-02-0G-0.; [02] VERIFIED REMOVED CORROSION ON AFT ENTRY DOOR MOPSILL STA 964-986; LBL 52; WL 208. MAX MATERIAL REMOVED WAS .015' 1' BY 1' FROM .080'. OUT OF LIMITS PER SRM 53-70-15-01-1; SRM 53-70-15-1A-1; SRM 51-10-02-0G-0.; [03] REMOVED AFT ENTRY DOOR MOP SILL IAW SRM 51-40-02-0G-0.; [04] LOCATED AND DRILLED AND COUNTERSUNK NEW AFT ENTRY DOOR MOPSILL PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; DWG#147A8501; REV B. OK TO INSTALL.; [05] VERIFIED CORRECTIVE ACTION ITEMS 3 AND 4; OK TO INSTALL; [06] ACCOMPLISHED PARTIAL INSTALLATION OF AFT ENTRY DOOR MOPSIL 100% TEMP OR PERMANENT FASTENERS INSTALLED WITHIN SEALANT SQUEEZE OUT TIME; [07] VERIFIED 100% TEMP OR PERMANENT FASTENERS INSTALLED WITHIN SEALANT SQUEEZE OUT TIME; [08] COMPLETED INSTALLATION OF NEW AFT ENTRY DOOR MOPSILL PER SRM 51-40-02-0G-0 AND BOEING DWG 147A8501.; [09] VERIFIED INSTALLATION OF THE AED MOP SILL PER DWG 147A8501; [10] COMPLETE
BS 494-500A RBL24.5 WL157 FLOOR TO SIDEWALL SHIELD IS CORRODED. / [01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORROSION TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE IN THE SRM. REPLACE PER SRM 51-10-02-0G-0; [03] REMOVED FCB AFT SHIELD AT BS494-BS500A; RBL24.5; WL 157 PER SRM 51-40-02-0G-0; [04] LOCATED; DRILLED; AND INSTALLED NUTPLATES ON FCB AFT SHIELD BS494-BS500A; RBL24.5; WL157. PER DWG 143A0080; AND SRM 51-40-05-0G-0; [05] VERIFIED;LOCATED; DRILLED; AND INSTALLED NUTPLATES ON FCB AFT SHIELD BS494-BS500A; RBL24.5; WL157. PER DWG 143A0080; AND SRM 51-40-05-0G-0.; [06] INSTALLATION DOCUMENTED ON TTG8Q005PPLQ; [07] VERIFIED INSTALLED ON TTG8Q005PPLQ; [08] VERIFIED INSTALLATION DOCUMENTED ON TTG8Q005PPLQ. FAULT COMPLETE.
FWD ENTRY DOOR MAIN FRAME DAMAGED IN 3 EA PLACES ALONG AFT UPPER EDGES (ALL MARKED) ; / [01] REMOVED DAMAGE ON FED MAIN FRAME BS344 LBL56 WL283 0.750'X0.500';BS344 LBL58 WL280 0.500'X0.0500' AND BS344 LBL60 WL270 1.250'X0.250' I.A.W SRM 51-10-02-0G-0 AND SRM 52-10-02-1A-1 PAR 4.B(2) FIG 103 ALLOWABLE DAMAGE 1; [02] VERIFIED DAMAGE REMOVAL.; [03] ET INSPECTED BLENDS AND HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23 AND PROCEDURE 16; NO CRACKS NOTED.<BR>UT INSPECTED BLENDS IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.058'<BR><BR>CAL ID ATS1465 N600<BR>CAL ID ATS2031 E650; [04] LIMIT STATEMENT; DAMAGE ON FED MAIN FRAME BS344 LBL56 WL283 FOUND TO BE OUT LIMITS ORIGINAL MATERIAL THICKNESS IS 0.071' REMAINING MATERIAL THICKNESS IS 0.058' PER SRM 51-10-02-0G-0 AND SRM 52-10-02-1A-1 PAR 4.B(2) FIG 103 ALLOWABLE DAMAGE 1 DETAILS A;B;C;D AND F; [05] REQUESTED ENGINEERING FOR REPAIR INSTRUCTIONS; [06] COMPLETED STEPS 1-13 EA 21-152-1862 TTG8Q005QH7V; [07] COMPLETED REPAIR PER EA 21-152-01862; [08] VERIFIED CORRECTIVE ACTION #7
CRACKED FLOOR SUPPORT BS 344-360 LBL 11 WL 208. ; / [01] REMOVED CRACKED FLOOR SUPPORT BS344-360 LBL11 WL208 PER SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW FLOOR SUPPORT PER SRM 51-40-05-0G-0 AND DWG 141A5410.; [03] UPDATED MEASUREMENT TABLE AND REQUEST OK TO INSTALL; [04] VERIFIED LOCATED AND DRILLED NEW FLOOR SUPPORT PER SRM 51-40-05-0G-0 AND DWG 141A5410. AND OK TO INSTALL.; [05] INSTALLED NEW FLOOR SUPPORT BS344-360 LBL11 WL208 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5410; [06] REMOVED AND REPLACED FLOOR SUPPORT BS344-360 LBL11 WL208 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5410; [07] SIGNED PART REQUIREMENT; [08] CORRECTED DWG NUMBER REMOVED AND REPLACED FLOOR SUPPORT BS344-360 LBL11 WL208 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5400; [09] CORRECTED DWG NUMBER REMOVED AND REPLACED FLOOR SUPPORT BS344-360 LBL11 WL208 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 PARTS REMOVED / INSTALLED; [10] VERIFIED REPLACEMENT OF FLOOR SUPPORT AT BS344-360 LBL11 WL208 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5400; [11] CORRECTED DWG NUMBER REMOVED AND REPLACED FLOOR SUPPORT BS344-360 LBL11 WL208 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5400; [12] FIXED ACTION STATEMENT; [13] VERIFIED TECHNICIAN CORRECTED STATEMENTS.<BR><BR>PART REPLACEMENT ACCOMPLISHED PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 <BR><BR>NO FURTHER ACTIONS REQUIRED.
BS 500B-500C RBL24.5 WL157 FLOOR TO SIDEWALL SUPPORT IS CORRODED. / [01] EVALUATED CORROSION FROM BS 500B-500C FOUND DEEPEST LOCATION AT BS 500B+10 FOUND 0.015 REMOVED FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566A S/N UNKNOWN; [02] VERIFIED CORROSION TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [03] REMOVED FCB FLOOR TO SIDEWALL SUPPORT AT BS500A-BS500D; RBL24.5; WL 157 PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW FCB RH FLOOR TO SIDEWALL SUPPORT BS500A-500D; RBL24 IAW SRM 51-40-02-0G-0; DWG143A7500; [05] VERIFIED CORRECTIVE ACTION ITEM 3 AND 4; [06] OK TO INSTALL; [07] INSPECTED; OK TO INSTALL; [08] INSTALLED FLOOR TO SIDEWALL SUPPORT BS500D-500A RBL25 WL 157 IAW SRM 51-40-02-0G-0; DWG 143A7505 AND 143A7500.; [09] VERIFIED FLOOR TO SIDEWALL SUPPORT BS500D-500A RBL25 WL 157 INSTALLED IAW SRM 51-40-02-0G-0; DWG 143A7505 AND 143A7500.; [10] COMPLETE
CORROSION ON FLOOR TO SIDE WALL SUPPORT BS 727+4-767 RBL 21; WL 156 ; / [01] EVALUATED CORROSION FROM BS 727+4 TO 767 FOUND DEEPEST LOCATION AT BS 747 FOUND 0.015 REMOVED FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566A S/N UNKNOWN; [02] VERIFIED CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; [03] REMOVED FLOOR TO SIDEWALL SUPPORT BS727+4-BS767; RBL 21; WL 156. PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED FLOOR TO SIDE WALL SUPPORT BS 727+4-767 RBL 21; WL 156 PER SRM 51-40-020G-0 AND DWG 146A7500; [05] VERIFIED STEP 3 AND 4. REMOVED FLOOR TO SIDEWALL SUPPORT BS727+4-BS767; RBL 21; WL 156. PER SRM 51-40-02-0G-0 AND LOCATED AND DRILLED FLOOR TO SIDE WALL SUPPORT BS 727+4-767 RBL 21; WL 156 PER SRM 51-40-020G-0 AND DWG 146A7500; [06] VERIFIED CORRECTIVE ACTION ITEMS 3; 4; AND 5.; [07] OK TO INSTALL ACB FLOOR TO SIDEWALL SUPPORT BS727+4TO BS767; RBL21; WL 156.; [08] OK TO INSTALL ACB FLOOR TO SIDEWALL ANGLE BS 727+4 TO BS 767; RBL 21; WL 156 GIVEN.; [09] SEALED AND INSTALLED ACB FLOOR TO SIDEWALL SUPPORT BS727+4-767; RBL 21; WL 156. PER DWG 146A7500; SRM 51-40-02-0G-0; AND AMM 51-31-00-390-801;
BS500-500C LBL24.5 WL157 FLOOR TO SIDEWALL SUPPORT IS CORRODED. / [01] EVALUATED CORROSION FROM BS 500-500C FOUND DEEPEST LOCATION AT BS 500B FOUND 0.015 REMOVED FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566A S/N UNKNOWN; [02] VERIFIED CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; [03] REMOVED FCB L/H FLOOR TO SIDEWALL SUPPORT BS400-BS500D; RBL24.5; WL157 PER SRM 51-40-02-0G-0; [04] * CORRECTION * L/H FLOOR TO SIDEWALL SUPPORT BS 400 TO BS500D L/B 24.5 WAS NOT REMOVED; [05] CERTIFIED STEP 3; [06] REMOVED FCB L/H FLOOR TO SIDEWALL SUPPORT BS400-BS500D; LBL24.5; WL157 PER SRM 51-40-02-0G-0; [07] VERIFIED STEP 6 REMOVED FCB L/H FLOOR TO SIDEWALL SUPPORT BS400-BS500D; LBL24.5; WL157 PER SRM 51-40-02-0G-0; [08] LOCATED AND DRILLED FCB NEW FLOOR TO SIDEWALL SUPPORT BS396-500D LBL24 IAW SRM 51-40-02-0G-0; DWG143A7500; [09] VERIFIED CORRECTIVE ACTION ITEMS 3-8; [10] OK TO INSTALL; [11] OK TO INSTALL; [12] INSTALLED FLOOR TO SIDEWALL SUPPORT BS500D-396 LBL25 WL 157 IAW SRM 51-40-02-0G-0; DWG 143A7505 AND 143A7500.; [13] VERIFIED FLOOR TO SIDEWALL SUPPORT BS500D-396 LBL25 WL 157 INSTALLED IAW SRM 51-40-02-0G-0; DWG 143A7505 AND 143A7500; [14] COMPLETE
FORWARD CARGO BAY BS440-494 RBL 25 WL157 SUBWEB THRESHOLD IS CORRODED. / [01] EVALUATED CORROSION FROM BS 440-494 FOUND DEEPEST LOCATION AT BS 460 FOUND 0.015 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING DEPTH GAUGE P/N ATS400 S/N UNKNOWN; [02] VERIFIED CORROSION TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1; [03] REMOVED FCB SUB THRESHOLD WEB BS440 - BS494; RBL25; WL157 PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED FCB SUBWEB THRESHOLD BS440 - BS494; RBL25; WL157 PER SRM 51-40-050G-0 AND DWG 143A8330; [05] VERIFIED LOCATED AND DRILLED FCB SUBWEB THRESHOLD BS440 - BS494; RBL25; WL157 PER SRM 51-40-050G-0 AND DWG 143A8330; [06] OK TO INSTALL.; [07] INSPECTED; OK TO INSTALL; [08] INSTALLED FCB SUBWEB THRESHOLD BS440 - BS494; RBL25-29; WL157 PER SRM 51-40-02-0G-0 AND DWG 143A8330; [09] VERIFIED FCB SUBWEB THRESHOLD INSTALLED BS440 - BS494; RBL25-29; WL157 PER SRM 51-40-02-0G-0 AND DWG 143A8330; [10] COMPLETE
CORROSION ON FLOOR TO SIDE WALL SUPPORT BS 727+4-847; LBL21; WL 156 ; / EVALUATED CORROSION FROM BS 727+4 TO 847 FOUND DEEPEST LOCATION AT BS 787 FOUND 0.015 REMOVED FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER P/N 4566A S/N UNKNOWN; VERIFIED CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; REMOVED ACB L/H FLOOR TO SIDEWALL SUPPORT BS727+4-BS847; LBL 21; WL 156. PER SRM 51-40-02-0G-0; [04] STARTED DRILLING REPAIR PARTS IAW SRM 53-00-53-2R-5 REPAIR5.LOCATED AND DRILLED REPAIR PARTS FOR ACB LH FLOOR TO SIDEWALL SUPPORT; BS 727+4--847 LBL21; IAW SRM53-00-53-2R-5; REPAIR 5. SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01-0G-0; AND OK TO PRIME REPAIR PARTS. LOCATE AND DRILL REPAIR PARTS ALSO DWG146A7500FABRICATED AND ASSEMBLED REPAIR PARTS; SPLICE AT BS727E+10; AND INSTALLED BS727 BOLT BRACKET; AND FLOOR T-STRAP PLATES; IAW SRM 51-40-02-0G-0; SRM53-00-53-2R-5; REPAIR5; DWG 146A7500; AND INSTALLED NUT PLATES IAW SRM51-40-10-2R-0. REPAIR PARTS FABRICATED FROM MATERIAL; BAC1496-377#7075 T62; LOT#1459405-1 VERIFIED REPAIR PARTS FABRICATION; BAC1496-377#7075T62; LOT# 1459405-1. PER SRM 53-00-53-2R-5<BR><BR>VERIFIED ASSEMBLY OF FLOOR TO SIDEWALL SUPPORT AND SPLICE PER SRM 51-40-02; SRM 53-00-53-2R-5<BR><BR>OK TO INSTALL INSTALLED ACB L/H FLOOR TO SIDEWALL SUPPORT BS727+4-BS847; LBL 21; WL 156. PER SRM 51-40-02-0G-0 AND DWG 146A7500
CORROSION ON ACB DOOR SUB THRESHOLD WEB BS 793-847; RBL 15-23 WL 156 ; / [01] EVALUATED CORROSION FROM BS 793-847 FOUND DEEPEST LOCATION AT BS 827 FOUND 0.015 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING DEPTH GAUGE P/N ATS400 S/N UNKNOWN; [02] VERIFIED CORROSION OUT OF LIMITS IAW SRM 53-60-15-1A-1; [03] REMOVED ACB SUB-THRESHOLD WEB BS793-BS847; RBL 15-23; WL 156. PER SRM 51-40-02-0G-0; [04] LOCATED; DRILLED; AND INSTALLED NUTPLATES ON NEW ACB SUB-THRESHOLD WEB BS793-BS847; RBL 15-23. PER DWGS 146A8340; 146A8120; SRM 51-40-05-0G-0; AND SRM 51-40-02-0G-0; [05] VERIFIED CORRECTIVE ACTION ITEM 3 AND 4; [06] UPDATED PARTS INSTALLED TAB; [07] OK TO INSTALL ACB SUB THRESHOLD WEB BS793-847; RBL 15-23; WL 156; [08] CERTIFIED OK TO INSTALL ACB SUB THRESHOLD WEB BS793-847; RBL 15-23; WL 156; [09] INSPECTED; OK TO INSTALL; [10] SEALED AND INSTALLED ACB SUB THRESHOLD WEB BS793-847; RBL 15-23; WL 156. PER DWG 147A8340; SRM 51-40-02-0G-0; AND AMM 51-31-00-390-801; [11] CORRECTION TO ITEM 10 CHANGE DWG TO 146A8340; [12] VERIFIED INSTALLATION OF ACB SUB THRESHOLD WEB BS793-847; RBL 15-23; WL 156. PER DWG 146A8340 ; SRM 51-40-02-0G-0; AND AMM 51-31-00-390-801; [13] VERIFIED REPLACEMENT AND INSTALLATION OF ACB SUB THRESHOLD WEB BS793-847; RBL 15-23; WL 156. PER DWG 146A8340 ; SRM 51-40-02-0G-0; AND AMM 51-31-00-390-801
CORROSION ON ACB FLOOR PANEL SPLICE AT BS 727D+6 LBL 20 - RBL 20; WL156 ; / [01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORROSION TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM. REPLACE PER SRM 51-10-02-0G-0; [03] RECEIVED NEW ACB FLOOR PANEL SPLICE BS727D+6; LBL20-RBL20; WL156 FROM STORES ON PO# 827575 /1; [04] VERIFIED RECEIVED NEW ACB FLOOR PANEL SPLICE BS727D+6; LBL20-RBL20; WL156 FROM STORES ON PO# 827575 /1; [05] ACB FLOOR PANEL SPLICE @BS 727+6 LBL20-RBL20 WL156 WILL BE INSTALLED ON CUSTOMER CARD #TTG8Q00599T3.; [06] VERIFIED ACB FLOOR PANEL SPLICE @BS 727+6 LBL20-RBL20 WL156 WILL BE INSTALLED ON CUSTOMER CARD #TTG8Q00599T3.
FWD ENTRY DOOR TARGET ANGLE CRACKED (MARKED) ; / [01] REMOVED AND REPLACED CRACKED FED TARGET ANGLE IAW SRM 51-40-02-0G-0 DWG 141A6124; [02] PERFORMED FORWARD ENTRY DOOR INDICATION SENSOR ADJUSTMENT TEST PER AMM 52-71-11-820-801. OPS CHECK TEST GOOD; [03] VERIFIED TARGET INSTALLATION SRM 51-40-02-0G-0 DWG 141A6124; AND RETEST AMM 52-71-11-820-801
CRACK ON FRAME BS 312 ABOVE FWD ENTRY DOOR UPPER SILL WEB. ; / [01] ET INSPECTED CRACK IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; VERIFIED CRACK AND MARKED ENDS.<BR><BR>CAL ID ATS1465 N600; [02] REMOVED CRACK ON FRAME STA 312 ABOVE FWD ENTRY DOOR UPPER SILL WEB. AREA REMOVED WAS .300' BY 1' JUST ABOVE STR 6L PER SRM 51-10-02-0G-0.; [03] VERIFIED REMOVAL OF CRACK ON FRAME STA 312 ABOVE FWD ENTRY DOOR UPPER SILL WEB PER SRM 51-10-02-0G-0; [04] ET INSPECTED CUT OUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; VERIFIED CRACK AND MARKED ENDS. <BR><BR>CAL ID ATS1465 N600; [05] EDIT ITEM 4:<BR>REMOVE 'VERIFIED CRACK AND MARKED ENDS'; CUT OUT IS CRACK FREE.; [06] REMOVED CRACK ON FRAME STA 312 ABOVE FWD ENTRY DOOR UPPER SILL WEB. AREA REMOVED WAS .300' BY .300' JUST ABOVE STR 6L PER SRM 51-10-02-0G-0; [10] COMPLETED PER EA 21-153-1861; [11] VERIFIED CORRECTIVE ACTION #10
CORROSION ON FWD ENTRY DOOR I/B THRESHOLD SUPPORT ANGLE BS 316 -338 LBL 60 WL 208. ; / [01] REMOVED CORROSION ON FWD ENTRY DOOR I/B SUPPORT ANGLE STA 316-338; LBL 60; WL 208. MAX MATERIAL REMOVED WAS .014'; 22' BY 1' FROM .080' OUT OF LIMITS PER SRM 51-10-02-0G-0; SRM 53-10-15-1A-1.; [02] UPDATED MEASUREMENTS; [03] VERIFIED CORROSION REMOVAL OUT OF LIMITS PER SRM 51-10-02 AND SRM 53-10-15-1A-1; [04] REMOVED DAMAGED FWD ENTRY DOOR I/B THRESHOLD SUPPORT ANGLE STA 316-338; LBL 60; WL 208 PER SRM 51-40-02-0G-0.; [05] LOCATED AND DRILLED NEW FWD ENTRY DOOR I/B THRESHOLD SUPPORT ANGLE FOR STA 316-338 LBL 60 WL 208 IAW SRM 51-40-05-0G-0 OK TO INSTALL; [06] VERIFIED CORRECTIVE ACTION ITEMS 4 AND 5. 0K TO INSTALL; [07] INSTALLED FWD ENTRY DOOR I/B THRESHOLD SUPPORT ANGLE AT STA 316-338 LBL 60 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8110; [08] VERIFIED INSTALLATION OF FWD ENTRY DOOR I/B THRESHOLD SUPPORT ANGLE AT STA 316-338 LBL 60 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8110; [09] APPLIED FILLET SEAL TO FWD ENTRY DOOR I/B THRESHOLD SUPPORT ANGLE AT BS 316-338 LBL 60 WL 208 IAW AMM 51-31-00-390-804; [10] VERIFIED CORRECTIVE ACTION ITEM 9; [11] VERIFIED REMOVAL AND INSTALLATION OF FWD ENTRY DOOR I/B THRESHOLD SUPPORT ANGLE AT STA 316-338 LBL 60 WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8110 IS COMPLETE
BS 420-440 RBL24.5 WL157 FLOOR TO SIDEWALL SHIELD IS CORRODED. / [01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORROSION TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE PER SRM. REPLACE PER SRM 51-10-02-0G-0; [03] REMOVED FCB FORWARD SHIELD AT BS420-BS440; RBL24.5; WL 157 PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED FCB SHIELD BS420 -BS440; RBL24.5; WL157 PER SRM 51-40-050G-0 AND DWG 143A0080; [05] VERIFIED LOCATED AND DRILLED FCB SHIELD BS420 -BS440; RBL24.5; WL157 PER SRM 51-40-050G-0 AND DWG 143A0080; [06] INSPECTED; OK TO INSTALL; [07] INSTALLED FCB SHIELD BS420 -BS440; RBL24.5; WL157 PER SRM 51-40-02-0G-0 AND DWG 143A0080; [08] RII INSPECTED SHIELD INSTALLATION; [09] COMPLETE
BS500D LBL24.5-RBL24.5 WL157 AFT BULKHEAD PANEL SUPPORT IS CORRODED. / [01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORROSION TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE IN THE SRM. REPLACE PER SRM 51-10-02-0G-0; [03] REMOVED FCB LOWER AFT CENTER BULKHEAD SUPPORT BS500D; LBL24.5 - RBL24.5; WL157 PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW FCB LOWER AFT CENTER BULKHEAD SUPPORT BS500D; LBL24.5 - RBL24.5 PER DWG 143A9481; 143A7902; AND SRM 51-40-05-0G-0; [05] VERIFIED CORRECTIVE ACTION ITEMS 3 AND 4; [06] OK TO INSTALL; [07] INSPECTED; OK TO INSTALL; [08] INSTALLED NEW FCB LOWER AFT CENTER BULKHEAD SUPPORT BS500D; LBL24.5 - RBL24.5 PER DWG 143A9481; 143A7902; AND SRM 51-40-02-0G-0; [09] VERIFIED NEW FCB LOWER AFT CENTER BULKHEAD SUPPORT BS500D; LBL24.5 - RBL24.5 INSTALLED PER DWG 143A9481; 143A7902; AND SRM 51-40-02-0G-0; [10] UPDATED PARTS TABLE; [11] COMPLETE
CORROSION ON FLOOR TO SIDE WALL SUPPORT BS 767-793; RBL 21; WL 156 ; / [01] EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORROSION TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE PER THE SRM. REPLACE PER SRM 51-10-02-0G-0; [03] REMOVED ACB FWD SHIELD BS767-BS793; RBL 21; WL 156. PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW ACB FWD SHIELD BS767-793; RBL21; WL156. PER DWG 146A0081 AND SRM 51-40-05-0G-0; [05] VERIFIED CORRECTIVE ACTION ITEMS 3 AND 4; [06] OK TO INSTALL SHIELD BS 767-793 RBL 21L; WL 156.; [07] OK TO RE-INSTALL ACB FLOOR TO SIDEWALL ANGLE AT BS 767-BS 793; RBL 21; WL 156 GIVEN.; [08] INSTALLED SHIELD BS 767-793 RBL 21; WL 156 PER SRM 51-40-02-0G-0; DWG 146A0081.; [09] VERIFIED INSTALLATION OF FWD SHIELD/ FLOOR TO SIDEWALL SUPPORT BS767-793 RBL21; WL156 PER SRM 51-40-02-0G-0; DWG 146A0081.; [10] VERIFIED REPLACEMENT AND INSTALLATION OF FWD SHIELD/ FLOOR TO SIDEWALL SUPPORT BS767-793 RBL21; WL156 PER SRM 51-40-02-0G-0; DWG 146A0081.
FWD FLOOR PANEL 221BF HAS DAMAGED INSERTS ON O/B EDGE ; / [01] IDENTIFIED FORWARD FLOOR PANEL 221 BF<BR>IAW SRM 53-00-50-0I-1 FIGURE 2; TABLE 2<BR>FOUND DAMAGE TO ENTIRE UPPER SURFACE AND BROKEN TANG TO<BR>EXCEED ALLOWABLE DAMAGE LIMITS.<BR>IAW SRM 53-00-50-1A-1 PARA 4 F.<BR><BR>REPAIR TO BE EFFECTED IAW SRM 53-00-50-2R-1 AND<BR>SRM 53-00-50-2R-6<BR><BR>REMOVED ALL INSERTS TO FACILITATE REPAIR.<BR>IAW SRM 53-00-50-2R-1 PARA 3 B.<BR><BR>REMOVED DAMAGE ON ENTIRE UPPER SURFACE AND TANG; CLEANED<BR>REPAIR AREA. NO CONTAMINATION NOTED.<BR>IAW SRM 53-00-50-2R-1 PARA 3 A; C; D; & F; AND <BR>SRM 53-00-50-2R-6 PARA 3 A; C; & E.; [02] VALIDATED APPLICABILITY OF REPAIR SRM 53-00-50-2R-1 AND <BR>SRM 53-00-50-2R-6[21] VERIFIED; COMPLETED CURE WITH THERMOMETER ID:ATS2208 S/N: 43300740WS; UNBAGGED AND TRIMMED. <BR>INSTALLED 1EA BLIND INSERT USING BMS 5-28TY19 LOT#AK0DP4131K USED SCALE ID:ATS2275 S/N:P1662216 <BR>IAW SRM 53-00-50-2R-1 PARA 3M;N AND SRM 53-00-50-2R-6 PARA 3M AND DWG 141A5810-729.<BR>INSTALLED ALL NEW THROUGH INSERTS INTO FLOOR PANEL USING BMS5-107 CL1 LOT# AK0DP4051K; AND CURED THROUGH INSERTS AND POTTED INSERT. IAW SRM 53-00-50-2R-1 PAR. 3.N AND BOEING DWG 141A5810 ID: 0729. USED THERMOMETER ID: ATS2208 S/N: 433007740WS.; [22] F
FWD FLOOR PANEL 221DF HAS DAMAGED UPPER SURFACE PLIES ; / [01] IDENTIFIED FORWARD FLOOR PANEL 221DF<BR>IAW SRM 53-00-50-0I-1 FIGURE 2; TABLE 2<BR>FOUND DAMAGE TO UPPER SURFACE TO EXCEED ALLOWABLE LIMITS<BR>IAW SRM 53-00-50-1A-1 PARA 4 F.<BR><BR>REPAIR TO BE EFFECTED IAW SRM 53-00-50-2R-1<BR><BR>REMOVED 16 EA INSERTS TO FACILITATE REPAIR.<BR>IAW SRM 53-00-50-2R-1 PARA 3 B.<BR><BR>REMOVED DAMAGE FROM UPPER SURFACE AND CLEANED REPAIR AREA.<BR>NO CONTAMINATION NOTED.<BR>IAW SRM 53-00-50-2R-1 PARA 3 A; C; & F.; [02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.; [03] VERIFIED MATERIAL ID PER SRM 53-00-50-0I-1<BR>VERIFIED DAMAGE IS OUT OF LIMITS PER SRM 53-00-50-1A-1<BR>VALIDATED REPAIR PER SRM 53-00-50-2R-1 <BR>VERIFIED WORK PERFORMED PER SRM 53-00-50-2R-1; [04] FABRICATED REPAIR PLIES FROM BMS 9-3 TY H2 LOT#1458851-1<BR>OK TO INATALL.<BR>IAW SRM 53-00-50-2R-1 PARA 3 K(1); [05] CORRECTED STEP 4; LINE 2 TO READ 'OK TO INSTALL'; [06] VERIFIED PER SRM 53-00-50-2R-1<BR>OK TO INSTALL REPAIR PLIES; [07] INSTALLED REPAIR PLIES USING RESIN BMS8-201 TY3 LOT#AK0GP9267K; AND VACUUM BAGGED; LEAK CHECKED GOOD WITH VACUUM GAUGE ID: ATS2438 S/N: UNKNOWN; AND SET REPAIR TO CURE IAW SRM 53-00-50-2R-1 PAR. 3K(1)L(1).
FWD FLOOR PANEL 221CF HAS DAMAGED INSERTS ; / [01] DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 221CF; REPLACED WITH NEW.<BR>IAW SRM 51-10-02-0G-0 PARA 9 A(1) AND<BR>AIPC 53-21-51-21L ITEM 175; [02] FLOOR PANEL REPLACED. JOB COMPLETE.
FWD FLOOR PANEL 222BF HAS UPPER SURFACE PLY DAMAGE ; / [01] DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 222BF; REPLACED WITH<BR>NEW PANEL.<BR>IAW SRM 51-10-02-0G-0 PARA 9 A. (1) AND<BR>AIPC 52-21-51-21L ITEM 135; [02] VERIFIED PANEL REPLACEMENT
LT HORIZONTAL STAB. LWR SKIN STAB STA 193.90-1; CRACK NOTED 16' AFT OF FRONT SPAR LE. CRACK LENGTH 1.3' / [01] -CUT OUT DAMAGED AREA ON LT HORIZONTAL STABILIZER LOWER SKIN IAW SRM 55-10-01-2R-11 STEP 4 B;C. CUT OUT DIMENSIONS: L=1.70'; W=1.60'; [02] VERIFIED CUT OUT DAMAGED AREA ON LT HORIZONTAL STABILIZER LOWER SKIN IAW SRM 55-10-01-2R-11 STEP 4 B;C. CUT OUT DIMENSIONS: L=1.70'; W=1.60; [03] -HFEC INSPECTION OF CUT EDGES REQUIRED PER SRM 55-10-01-2R-11 STEP 4 D(1); [04] ET INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR><BR>CAL ID ATS1465 N600; [05] -FABRICATED REPAIR PARTS IAW SRM 55-10-01-2R-11 STEP 4. G THRU L AND TABLE 201 AND 202. PARTS MADE FROM: DOUBLER 2024T3 #0.080' LOT# 1447577-1; FILLER 2024T3#0.063' LOT # 1446328-1; [06] -APPLIED CHEMICAL CONVERSION COATING TO REPAIR PARTS AND SKIN CUT EDGES IAW SRM 55-10-01-2R-11 STEP 4. M; [15] REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 16' AFT OF FRONT SPAR L/E IAW SRM 55-10-01-2R-11.
FWD FLOOR PANEL 221EF HAS DAMAGED UPPER SURFACE PLIES ; / [01] DUE TO THE EXTENT OF DAMAGE; REPLACED FWD FLOOR PANEL 221EF WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 295.; [02] PANEL REPLACED. JOB COMPLETE.
CORROSION FOUND ON FLIGHT DECK FLOOR UPPER FLANGE OF BS 259.5; LBL 11 - RBL 11; WL 208 ; / [01] REMOVED FASTENER ON DAMAGED AREA FOR ACCESS I.A.W SRM 51-40-02-0G-0; [02] NO APPLICABILITY ENTRIES FOUND ON SRM <BR>DAMAGE TO BE REMOVE PER SRM 51-10-02-0G-0; [03] REMOVED DAMAGE ON BS 259.5 FLIGHT DECK FLOOR UPPER AFT FLANGE LBL11-RBL11 WL 208.5;22'X1.2' I.A.W SRM 51-10-02-0G-0; [04] VERIFIED CORROSION REMOVED; [05] ET INSPECTED BLEND AND HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23 AND 16; NO CRACKS NOTED.<BR>UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.092'<BR><BR>CAL ID ATS1465 N600<BR>CAL ID ATS2031 E650; [06] NO ALLOWABLE LIMITS FOUND ON SRM FOR BS 259.5 FLIGHT DECK FLOOR UPPER AFT FLANGE LBL11-RBL11 WL 208.5 ORIGINAL MAT. THICKNESS IS 0.094' REMAINING MAT. THICKNESS IS 0.092'I.A.W.SRM 53-10-08-0I-3 CONTACTED ENGINEERING FOR REPAIR INSTRUCTIONS. ACCOMPLISHED REPAIR OF UPPER FLANGE OF CHORD AT BS 259.5 LBL 11 TO RBL 11 WL 208 IAW EA# 21-153-01901 AND EA# 21-153-01901-WIP1
CORROSION FOUND ON FLIGHT DECK FLOOR INTERCOSTAL SUPPORT CHANNEL BETWEEN BS 259.5 AND BS 270; BL 0; WL 208 ; / [01] VERIFIED APPLICABILITY PER SRM 53-10-51-1A-1 PAR 4.B(2)(A) FIGURE 105/ALLOWABLE DAMAGE 1 DETAIL E; [02] REMOVED CORROSION ON SUPPORT CHANNEL BS262-BS268 LBL3-RBL3 WL207.5;6'X3'AREA I.A.W SRM 51-10-02-0G-0 AND SRM 53-10-51-1A-1 PAR 4.B(2)(A) FIGURE 105/ALLOWABLE DAMAGE 1 DETAIL E; [03] VERIFIED CORROSION REMOVED; [04] ET INSPECTED BLEND AND HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23 AND 16; NO CRACKS NOTED.<BR>UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.035'<BR><BR>CAL ID ATS1465 N600<BR>CAL ID ATS2031 E650; [05] REMOVED FLOOR INTERCOSTAL SUPPORT CHANNEL BS 259.5 TO BS 270 LBL3-RBL3 WL 208 PER SRM 51-40-02-0G-0; [06] CORROSION ON SUPPORT CHANNEL BS262-BS268 LBL3-RBL3 WL207.5;6'X3'AREA FOUND TO BE OUT LIMITS ORIGINAL MAT. THICKNESS IS 0.040 REMAINING MAT. THICKNESS IS 0.035 I.A.W SRM 51-10-02-0G-0 ;SRM 53-10-51-1A-1 PAR 4.B(2)([14] REMOVED AND REPLACED SUPPORT CHANNEL BS259.5-BS270 LBL3-RBL3 WL207.5 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5210;
CORROSION FOUND ON LATERAL BEAM UPPER FLANGE AT BS 270; LBL 11 - RBL 11; WL 208 ; / REMOVED FASTENER ON DAMAGED AREA FOR ACCESS I.A.W SRM 51-40-02-0G-0; VERIFIED APPLICABILITY PER SRM 53-10-51-1A-1 PAR 4.C(2)(A) FIGURE 105/ALLOWABLE DAMAGE 1 DETAIL E; [03] REMOVED CORROSION ON LATERAL BEAM UPPER FWD FLANGE BS270 LBL11-RBL11 WL207.5;22'X1' AREA I.A.W SRM 51-10-02-0G-0 AND SRM 53-10-51-1A-1 PAR 4.C(2)(A) FIGURE 105/ALLOWABLE DAMAGE 1 DETAIL E; VERIFIED CORROSION REMOVED; ET INSPECTED BLEND AND HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23 AND 16; NO CRACKS NOTED.<BR>UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.092'<BR><BR>CAL ID ATS1465 N600<BR>CAL ID ATS2031 E650; [06] EDIT ACTION 5:<BR><BR>LOWEST THICKNESS IS ACTUALLY = 0.040'; CORROSION ON LATERAL BEAM UPPER FWD FLANGE BS270 LBL11-RBL11 WL207.5;22'X1' AREA FOUND TO BE OUT LIMITS ORIG. MAT. THICKNESS IS 0.050';REMAINING MAT. THICKNESS IS 0.040' I.A.W SRM 53-10-51-1A-1 PAR 4.C(2)(A) FIGURE 105/ALLOWABLE DAMAGE 1 DETAIL E AND SRM 53-10-51-0I-2 TABLE 2 ITEM 4 CONTACTED ENGINEERING FOR REPAIR INSTRUCTION; VERIFIED CORROSION OUT OF LIMITS; REFER TO EA 21-153-01911 SUMMARY REQUIREMENT; BARCODE: TTG8Q005V48S AND MULTI EFFECTIVITY EA M-21-153-00277; BARCODE: TTG8Q005PK28.; ACCOMPLISHED REPAIR PER EA 21-153-01911/TTG8Q005V48S<BR>AND EA 21-153-01911-WIP1/TTG8Q005QZ1F
AFT FLOOR PANEL 241AEF HAS PLY DAMAGE ON THE AFT EDGE UPPER SURFACE SKIN ; / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 6 TABLE 6.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>REMOVED 2EA THROUGH INSERTS TO FACILITATE REPAIR IAW SRM 53-00-50-2R-9 PARA 4B.<BR>REMOVED DAMAGED PLIES AND LOOSE PIECES OF CORE; CLEANED REPAIR AREA IAW SRM 53-00-50-2R-1 PARA 3C-F.; [02] CORRECTION TO STEP 1: INSERT REMOVAL ACCOMPLISHED IAW SRM 53-00-50-2R-1 PARA 3B.; [03] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.; [04] VERIFIED DAMAGE OUT OF LIMITS AND DAMAGE REMOVAL PER SRM 53-00-50-1A-1 AND 53-00-50-2R-1. OKAY TO PROCEED.; [05] APPLIED BMS 5-28 TY 19 LOT#1455162-1; CURED & SANDED FLUSH.<BR>USED SCALE ID:ATS2275 S/N P1662216 AND THERMOMETER<BR>ID: ATS2208 S/N 43300740WS<BR>IAW SRM 53-00-50-2R-1 PARA 3 G-J; [06] VERIFIED ITEM 5; [07] FABRICATED REPAIR PLIES USING BMS 9-3ST1581 LOT#1458851-1;<BR>OK TO INSTALL IAW SRM 53-00-50-2R-1 PARA 3K.; [08] VERIFIED FABRICATED REPAIR PLIES USING BMS 9-3ST1581 LOT#1458851-1; <BR>OK TO INSTALL IAW SRM 53-00-50-2R-1 PARA 3K.
B.S. 663 LOWER COMPOSITE BULKHEAD VERTICAL 'L' ANGLE SUPPORT IS CRACKED AT L.B.L. 27; W.L. 150. ; / [01] UPDATED MEASUREMENT TABLE; [02] REMOVED BS 663 LWR VAPOR BARRIER VERTICAL 'L' ANGLE SUPPORT LBL27 WL150 IAW SRM 51-40-02.; [03] LOCATED AND DRILLED NEW VERTICAL ANGLE SUPPORT LBL27 WL150 PO# 796986/1 PER SRM 51-40-05-0G-0 AND DWG 111A1000; [04] VERIFIED LOCATED AND DRILLED NEW VERTICAL ANGLE SUPPORT LBL27 WL150 PO# 796986/1 PER SRM 51-40-05-0G-0 AND DWG 111A1000; [05] VERIFIED LOCATE AND DRILL OF NEW VERTICAL ANGLE SUPPORT AT LBL27 WL150 PO# 796986/1 PER SRM 51-40-05-0G-0 AND DWG 111A1000.; [06] OK TO INSTALL VERTICAL ANGLE SUPPORT; [07] OK TO INSTALL VERTICAL ANGLE SUPPORT; BS 663; LBL 27; WL 150; [08] INSTALLED 'L'ANGLE ON VAPOR BARRIER BS663 LBL27 IAW SRM 51-40-02-0G-0;DWG 111A1000 AND 111A1001.; [09] VERIFIED INSTALLATION OF 'L' ANGLE ON VAPOR BARRIER BS663; LBL27; IAW SRM 51-40-02-0G-0; DWG 111A1000 AND 111A1001; [10] VERIFIED STEPS COMPLETE.
R/H B.S 663 VAPOR BARRIER IS CRACKED ; / [01] REMOVED 6 EACH VERTICAL STIFFENERS TO ACCESS CRACKED AREA AT RBL 25 TO RBL 40 IAW SRM 51-40-02 PAR.7 D (6);DAMAGE WILL BE REPAIRED IAW SRM 51-70-04-2R-10<BR>PER SRM 57-10-10-2R-2 PARA 1C(NOTE).
L/H B.S 663 VAPOR BARRIER IS CRACKED ; / [01] REMOVED CHORD AND 3 EA BRACKETS TO FACILITATE REPAIR.<BR>IAW SRM 51-40-02-0G-0 PARA 4 E. & FIGURE 8; [02] REMOVED 5 EA. DOUBLERS AND 2 EA. STIFFENERS IAW SRM 51-40-02-0G-0 PARA 4 STEP E; PARA 7 STEP D AND AMM 51-31-00-100-802 PARA 17 STEP E.; [03] REMOVED LARGE BRACKET TO FACILITATE REPAIR PER SRM 51-40-02-0G-0 PAR.7D AND AMM 51-31-00-100-802 PAR.17 STEP E.; [04] IDENTIFIED MATERIAL ID PER SRM 57-10-10-0I-2 FIG.2; SHT.1; TABLE 2; AND ITEM 4. FOUND CRACK TO BE OUT OF ALLOWABLE DAMAGE LIMITS PER SRM 57-10-10-1A-2 PAR.4D1. A REPAIR WILL BE ACCOMPLISHED PER SRM 51-70-04 REPAIR 10 AS DIRECTED PER SRM 57-10-10-2R-2 PAR.1C AND NOTE.; [05] REMOVED DAMAGE ON FWD. SIDE APPROX. 4.0' X 22.0' AND ON AFT. SIDE APPROX. 2.0' X 22' WITH NO MOISTURE CONTAMINATION NOTED PER SRM 51-70-04 2R-10 PAR.4 STEPS A-C.; [06] VERIFIED ITEM 4 AND 5 ONLY; MATERIAL ID; OUT OF LIMITS; DAMAGE REMOVED; NO MOISTURE CONTAMINATION; OK TO PROCEED; [07] FABRICATED REPAIR PLIES FORM BMS9-3 STYLE 1581 TYPE H2 LOT#1458851-1 IAW SRM 51-70-04-2R-10 PARA 4 STEP D OK TO INSTALL REPAIR PLIES.; [26] REPAIRED CRACK IN B.S. 663 VAPOR BARRIER IAW SRM 51-70-04-2R-10 JOB COMPLETE; [27] VERIFIED BS 663 VAPOR BARRIER WAS REPAIRED PER SRM 51-70-04-2R-10; [28] VERIFIED BS 663 VAPOR BARRIER WAS REPAIRED PER SRM 51-70-04-2R-10
CRACK IN 3RD VERTICAL STIFFENER ON RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 129.50. ; / [01] -ACCESSED RT HORIZONTAL STABILIZER FRONT SPAR WEB FROM STAB STATION 111.10 TO STAB STATION 147.90 IAW SRM 51-40-02-0G-0<BR><BR>-REMOVED RT HORIZONTAL STABILIZER INSPAR RIB LOCATED AT STAB STATION 129.50 IAW SRM 51-40-02-0G-0; [02] CUT AND REMOVED CRACK DAMAGE ON STIFFENER L=0.75'X W=0.35' IAW SRM 55-10-09-2R-4.; [03] VERIFIED DAMAGE REMOVAL AND DIMENSIONS PER SRM 55-10-09-2R-4; [04] HFEC INSP OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071 EQUIP ID#: ATS2407 S/N: MM1591DD064104; [05] HFEC INSP CUTOUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071; [06] FABRICATED REPAIR PARTS IAW SRM 55-10-09-2R-4 STEP 4F THROUGH 4J.REPAIR PARTS MADE FROM T-SECTION 60-5872#7075T76511 LOT # 1449876-1; ANGLE BAC1490-2793#7075762 LOT # 1412885-2; SHIMS 2 707576#0.016' LOT # 1439717-1. APPLIED CHEMICAL CONVERSION COATING TO REPAIR PARTS AND RIB BARE SURFACES IAW SRM 55-10-09-2R-4 STEP 4K.; [07] VERIFIED FABRICATION OF REPAIR PARTS IAW SRM 55-10-09-2R-4; VERIFIED APPLICATION OF CHEMICAL CONVERSION COATING IAW SRM 55-10-09-2R-4;[17] REPAIRED 3RD VERTICAL ON RT HORIZONTAL STAB INSPAR RIB AT STAB STA 129.50 IAW SRM 55-10-09-2R-4; COMPLETION VERIFIED.
BS 663+4 LBL30 WL140 WING TO BODY (193D) FAIRING PANEL SUPPORT STRUCTURE HAS CHAFED DAMAGE. / [01] REMOVED BS 663+4 LBL30 WL140 WING TO BODY (193D)FAIRING PANEL SUPPORT STRUCTURE IAW SRM 51-40-02.; [02] LOCATED AND DRILLED NEW FAIRING PANEL SUPPORT STRUCTURE BS 663+4 LBL30 WL140 PO# 820084/7; [03] LOCATED AND DRILLED NEW FAIRING PANEL SUPPORT STRUCTURE BS 663+4 LBL30 WL140 PO# 820084/7 PER SRM 51-40-05-0G-0 AND DWG 149A7216; [04] VERIFIED LOCATED AND DRILLED NEW FAIRING PANEL SUPPORT STRUCTURE BS 663+4 LBL30 WL140 PO# 820084/7 PER SRM 51-40-05-0G-0 AND DWG 149A7216; [05] VERIFIED LOCATE AND DRILL OF NEW FAIRING PANEL SUPPORT STRUCTURE BS 663+4 LBL30 WL140 PO# 820084/7 PER SRM 51-40-05-0G-0 AND DWG 149A7216.; [06] OK TO INSTALL FAIRING SUPPORT STRUCTURE; [07] OK TO INSTALL FAIRING SUPPORT; BS 663; LBL 30; WL 140; [08] INSTALLED FAIRING FORMER SUPPORT ASSY BS 6663+4 LBL30 IAW SRM 51-40-02-0G-0;DWG 149A7216;111A1000 AND 111A1001.; [09] RII INSPECTED INSTALLED FAIRING FORMER SUPPORT ASSY BS 6663+4 LBL30 IAW SRM 51-40-02-0G-0;DWG 149A7216;111A1000 AND 111A1001.; [10] INSPECTION COMPLETE
BS 663+4 RBL30 WL140 WING TO BODY (193D) FAIRING PANEL SUPPORT STRUCTURE HAS CHAFFED DAMAGE. / [01] LOCATED AND DRILLED NEW FAIRING SUPPORT P/N 146A7214-20 IAW SRM 51-40-02-0G-0 AND DWG 149A7216. REMOVAL AND INSTALLATION TO BE DOCUMENTED ON TTG8Q005KR5K.; [02] VERIFIED LOCATED AND DRILLED NEW FAIRING SUPPORT P/N 146A7214-20 IAW SRM 51-40-02-0G-0 AND DWG 149A7216.; [03] UPDATED INSTALLED PARTS CHART; [04] VERIFIED REMOVAL AND INSTALLATION OF WTB FAIRING PANEL (193D) SUPPORT AT BS 663+4 RBL30 WL140 WILL BE ACCOMPLISHED AND DOCUMENTED ON TTG8Q005KR5K. CARD IS COMPLETE.
PANEL 193AR MATING SURFACE IS CHAFED. / [01] IDENTIFIED PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 2. TABLE 2. ITEM 9.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.B.(2).<BR><BR>REPAIR IS TO BE ACCOMPLISHED IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1 PARA 4.B.(2). AND TABLE 202.<BR><BR>REMOVED 3EA BRACKETS TO FACILITATE REPAIR IAW SRM 51-40-02-0G-0 PARA 9.<BR><BR>REMOVED DAMAGE FROM INNER SURFACE EDGE BAND; CLEANED; AND NO MOISTURE OR CONTAMINATION NOTED IAW SRM 51-70-05-2R-6 PARA 4.A.-D.; [02] CERTIFIED IDENTIFIED PANEL 193AR IAW SRM 53-40-70-0I-1 FIGURE 2. TABLE 2. ITEM 9.FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.B.(2).REPAIR IS TO BE ACCOMPLISHED IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1 PARA 4.B.(2). AND TABLE 202.REMOVED 3EA BRACKETS TO FACILITATE REPAIR IAW SRM 51-40-02-0G-0 PARA 9.REMOVED DAMAGE FROM INNER SURFACE EDGE BAND; CLEANED; AND NO MOISTURE OR CONTAMINATION NOTED IAW SRM 51-70-05-2R-6 PARA 4.A.-D.;[07] FABRICATED REPAIR PLIES FROM BMS8-79 CL3 ST 1581 LOT# 1455461-1 AND BMS8-79 CL3 ST 120 LOT#1457269-3 AND INSTALLED USING BMS5-129 TY2 GR5 LOT# 1457270-4 IAW SRM 51-70-05-2R-6 PARA 4.E.; [08] CERTIFIED FABRICATED REPAIR PLIES FROM BMS8-79 CL3 ST 1581 LOT# 1455461-1 AND BMS8-79 CL3 ST 120 LOT#1457269-3 AND INSTALLED USING BMS5-129 TY2 GR5 LOT# 1457270-4 IAW SRM 51-70-05-2R-6 PARA 4.EING SURFACE WITH CHAFING WAS REPAIRED IAW SRM 51-70-05-2R-6;
PANEL 193AL MATING SURFACE IS CHAFED. / [01] IDENTIFIED PANEL 193AL IAW SRM 53-40-70-0I-1.FIG2; ITEM[7]. FOUND DAMAGE ALONG I/B EDGE ON INNER SURFACE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1.PARA 4.B.(6). REQUIRES REPAIR PER SRM 51-70-05-2R-6 IAW SRM 53-40-70-2R-1.TABLE 202.<BR>REMOVED DAMAGED PLIES FROM APPROX. 28'X18' DAMAGED AREA IAW SRM 51-70-05-2R-6.PARA 4.A-D.; [02] VALIDATED APPLICABILITY OF SRM 51-70-05-2R-6 IAW SRM 53-40-70-2R-1.; [03] INSPECTED AND VERIFIED DAMAGE IS BEYOND LIMITS AND DAMAGE REMOVAL PER SRM 53-40-70-1A-1 AND SRM 51-70-05-2R-6; [04] FABRICATED REPAIR PLIES FROM BMS8-139 ST120 LOT#1460986-1; BMS8-139 ST1581 LOT#1457262-2; BMS5-154 TY2 GR05 LOT#1448775-8. INSTALLED; VACUUM BAGGED; CHECKED FOR LEAKS. LEAK CHECK GOOD. SET TO CURE USING HEATCON ID:ATS532 S/N:15092117 IAW SRM 51-70-05-2R-6.PARA 4.E-G; [05] CURED REPAIR PLIES; UNBAGGED; LIGHTLY SANDED. REQUEST NDI FOR POST CURE IAW SRM 51-70-05-2R-6.PARA 4.G-I.; [06] VERIFIED REPAIR CURED AND PREPPED FOR NDI INSPECTION PER SRM 51-70-05-2R-6.PARA 4.G-I.; [07] VERIFIED CORRECTIVE ACTION #4; [08] UT INSPECTED REPAIR PER NDTM PART 4; 51-00-02. NO DISBONDS NOTED.<BR>CAL ID: ATS2031 S/N: 170515011; [09] REFINISHED IAW SRM 51-70-05-2R-6.PARA 4.I.; [10] FINAL INSPECTED PANEL. JOB COMPLETE.
AFT ENTRY DOOR SLIDE AND GIRT REQUIRE REPOSITIONING. ; / [01] REMOVED AFT ENTRY DOOR ESCAPE SLIDE AND COVER FROM AFT ENTRY DOO FOR ACCESS PER AMM 25-66-01-000-801; [02] REPOSITIONED SLIDE IN PACK; REINSTALLED SLIDE; AND PEFORMED GOOD OPS CHECK PER CUSTOMER CARD NBR: 725-61-06 EA (CUST SYSTEM ID: TTG8Q005WNGR.; [03] VERIFIED SLIDE PACK WAS REINSTALLED PER MT# 725-61-06 EA. STILL REQUIRES GIRT BAR CHECK WHEN GIRT FLOOR FITTINGS ARE REINSTALLED.; [04] VERIFIED PROPER OPERATION OF AED GIRT BAR LOCKING INTO FLOOR FITTINGS PER AMM 25-66-01-400-804; STEP 6.E.(U); [05] VERIFIED CORRECTIVE ACTION #4
FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. ; / [01] EVALUATED DENTS ON FLIGHT DECK FLOOR AT BS 255; RBL 4 - LBL 14; WL 207.54. DENTS FOUND TO BE GOUGED; THEREFORE; DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1; FIG. 105; DEIAL D.; [02] VERIFIED EVALUATED DENTS ON FLIGHT DECK FLOOR AT BS 255; RBL 4 - LBL 14; WL 207.54. DENTS FOUND TO BE GOUGED; THEREFORE; DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1; FIG. 105; DEIAL D.; [03] INSTALLED EWIS PROTECTION ON DAMAGE AREA I.A.W AMM 20-60-07; [04] REMOVED EWIS PROTECTION ON REPAIR AREA I.A.W AMM 20-60-07; [05] VERIFIED REMOVAL OF EWIS PROTECTION PER AMM 20-60-07; [06] REMOVED DAMAGE PART OF THE WEB AND REPAIRED PER M-21-153-00734; [07] RII VERIFIED COMPLETION OF REPAIR PER EA M-21-153-00734; [08] VERIFIED COMPLETION OF REPAIR PER EA M-21-153-00734
LH MLG WHEEL WELL VAPOR BARRIER HAS A CRACK MEASURING 15.5' AT LBL 30. ACCOMPLISHED INTERIM REPAIR IAW SRM 5710101A2.
AFT SERVICE DOOR SLIDE RUBBING ON THRESHOLD. SECURED THE SLIDE IN ITS HOUSING IAW MM 25-66-01, AND MT 725-61-06.
FLIGHT DECK; FO'S SEAT TRACK AFT INBOARD IS WORN. / R & R FLIGHT DECK; FO'S SEAT TRACK AFT INBOARD; PER AMM 25-11-11.
OVERWING EMERGENCY EXIT CABIN CEILING SIGN IS LOOSE / RESECURED OVERWING EMERGENCY EXIT CABIN CEILING SIGN PER MM 33-51-00
FWD SERVICE DOOR SLIDE GIRT REQUIRES ADJUSTMENT / PERFORM ADJUSTMENT OF FWD SERVICE DOOR SLIDE GIRT IN REF TO MT 725-61-06
L1 DOOR SLIDE GIRT REQUIRES ADJUSTMENT / PERFORMED ADJUSTMENT OF L1 DOOR SLIDE GIRT PER MT 725-61-06
PASSENGER CABIN; TWO EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST. / R & R TWO EMERGENCY LIGHTING BATTERY PACKS (M01672 & M01673) PER DWG# 33500005 AND AMM 33-51-06.
R1 DOOR FUSELAGE EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.
RT EMERGENCY EXIT AISLE LIGHT INOP AT ROW 3. R&R BATTERY PACK PER AMM.
FASTENER HOLE DAMAGED AT STA 265 LBL 10. (FLIGHT DECK FLOOR. UNDER PANEL 211AF ) / REPAIRED PER EA 1-753-35133.
VERTICAL STIFFENER CRACKED AT BS. 663, RBL 25 JUST OUTBOARD OF EXHAUST DUCT FOR PACKS. R&R VERTICAL STIFFENER PER SRM.
2 EACH FASTENERS R/H AFT ON CANOE FAIRING 542BB PULLED THROUGH COMPOSITE MATERIAL. MARKED. / SEE NR G65912; FOR REMOVAL AND REPLACEMENT OF FLAP TRACK FAIRING 542BB
LH FLAP TRACK FAIRING 542BB O/B FWD BULB SEAL RETAINER IS BROKEN. / SEE NR G65912; FOR REMOVAL AND REPLACEMENT OF FLAP TRACK FAIRING 542BB
PASSENGER CABIN FLOOR SUPPORT CRACKED AT BS. 540. LBL 1. R & R THE FLOOR SUPPORT IAW SRM.
THE RUDDER BALANCE WEIGHT IS CORRODED / REMOVED AND REPLACED RUDDER BALANCE WEIGHT PER CMM 55-40-09
R/H OVERWING EXIT DOOR ASSIST STRAP FRAYED. / R&R STRAP PER CMM.
R/H OVERWING EXIT DOOR ASSIST STRAP FRAYED. / R&R STRAP PER CMM.
FLOOR PANEL 241DF HAD UPPER SURFACE DELAMINATED, BETWEEN BS. 537.45 TO BS. 727B. R&R FLOOR PANEL PER AMM.
FLOOR PANEL 231XF HAD UPPER SURFACE DELAMINATED, BETWEEN BS. 537.45 TO BS. 727B. / R&R FLOOR PANEL PER AMM.
R1 DOOR CRACKED IN THE #4 BEAM ADJACENT TO THE FASTENER HOLE CLOSEST TO THE INBOARD SKIN. R&R DOOR PER AMM.
FLOOR PANEL 241AF HAS UPPER SURFACE DELAMINATION. / REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.
#1 ENG O/B T/R LARGE ANGLE NEAR TOP AFT SIDE CRACKED. / :REPLACED BRACKET REF SRM 51-40-02
L/H WING WAFFLE PLATE TRAILING EDGE CRACKED JUST INBOARD OF #3 FLAP TRACK. / R&R WAFFLE PLATE PER SRM.
LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.
LT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.
LT MAIN LANDING GEAR FORWARD TRUNION FITTING UPPER OUTBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.
RT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.
RT WING MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD LUG OUTER FACE CORRODED. REPAIRED FITTING PER EA.
RT MLG UPPER TRAILING EDGE PNL 'Z' CLIP CRACKED / R/R'ED RT MLG UPPER TRAILING EDGE 'Z' CLIP PER SRM 51-10-02 AND 51-40-02
BULKHEAD CRACKED AT BS 663, RBL 42.5. REPAIRED BULKHEAD IAW SRM.
L1 DOOR EMERGENCY SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REPOSITIONED SLIDE IAW MT.
FORWARD FLASHLIGHT SHIELD BROKEN. R&R SHIELD PER AMM.
AFT GALLEY EMERGENCY FLASHLIGHT INOP. R&R BATTERY ASSEMBLY PER MM.
L1 DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW. R&R LENS AMM.
R1 DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW. R&R LENS IAW AMM.
L1 DOOR ESCAPE SLIDE LOOSE. SECURED SLIDE IAW AMM.
LT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT BS 99.31, 3 STIFFENERS. REPAIRED RIB IAW SRM AND DWG.
LT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT STA 71.31, 1 STIFFENER. REPAIRED RIB IAW SRM AND DWG.
LT HORIZONTAL STABILIZER LEADING EDGE RIB STIFFENER CRACKED AT STA 71.3. REPAIRED STIFFENER IAW SRM AND DWG.
LT HORIZONTAL STABILIZER LEADING EDGE RIB STIFFENER CRACKED AT STA 99.31. REPAIRED STIFFENER IAW SRM AND DWG.
FRAME SHEAR TIE DELAMINATED AT BS 907, STR 20L. R&R FRAME ASSEMBLY PER EA.
FRAME SHEAR TIE DELAMINATED AT BS 907, STR 19L. R&R FRAME ASSEMBLY PER EA AND SRM.
SKIN DAMAGE AT AFT FUSELAGE AREA AT STA 896 TO STA 945 BETWEEN STR 19 AND 20 LEFT / REPAIRED PER EA 1-753-33126. REF TO EA FOR SIGNOFFS.
FRAME BENT AT BS 907, BETWEEN STR 17L TO STR 20L. R&R FRAME ASSEMBLY PER EA AND SRM.
1 EA SHEAR TIE HAS ELONGATED HOLES AT STA 927 STR 20L -21L / OVERSIZED FASTENER HOLE 1/32 OVER AND INSTALLED FASTENER PE SRM 51-40-02
STR 20L IS BROKEN AT STA 927 / REPAIRED STR. 20L FROM STA. 917 TP 937 PER SRM 53-00-03 AND E.A. 1-753-33103
L1 DOOR SLIDE LOOSE FROM COVER. SECURED SLIDE IAW AMM.
R2 DOOR EMERGENCY EVAC SLIDE LOOSE. REINSTALLED SLIDE IAW MT.
L2 DOOR EMERGENCY EVAC SLIDE LOOSE. REINSTALLED SLIDE IAW MT.
RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31
ONE EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M01675. R&R BATTERY PACK PER AMM AND DWG.
LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31
AFT CARGO ; ANGLE BELOW THE LAV TANK POST AT APPROX. STA.867 LBL 20 IS CRACKED. / REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-10-02.
#3 CANOE FAIRING HAS A CRACK ON THE INTERIOR SURFACE. / REPAIRED #3 CANOE FAIRING INTERIOR SURFACE PER SRM 57-53-70-2R-4 AND 51-70-04-2R-11 AND M.M. 51-21-81 SEE WIP'S AND SUB TASKS FOR INDIVIDUAL SIGN OFFS
AFT CARGO THRESHOLD WEB CORRODED. R&R WEB IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294.5, LBL0. R&R INTERCOSTAL PER SRM.
CRACKED FLOOR SUPPORT INTERCOSTAL AROUND FLOOR BOARD FASTENER HOLE AT BL 0 BETWEEN STA 344 AND 360. / REMOVED AND REPLACED DAMAGED INTERCOSTAL PER SRM 51-10-02 PT.9 AND 51-40-02.
FWD SERVICE DOOR ATTACH ANGLE TO 'Z' ANGLE CORRODED STA 300-320 / REMOVED & REPLACED ANGLE PER SRM 51-10-02/ SRM 51-40-02.
AFT CARGO BIN FLOOR BOARD SPLICE STRAP CORRODED AT BS 887. R&R STRAP PER SRM.
AFT CARGO BIN LT TRANS ANGLE CORRODED STA 767 TO 807. / INSTALLED REPAIR PART OF THE LT TRANS ANGLE FROM STA 758 TO 797 PER SRM 53-00-53-2R-5.
AFT CARGO BIN THRESHOLD WEB CORRODED UNDER DOOR. R&R WEB IAW SRM.
AFT CARGO BIN STRAP CORRODED STA 807 TO 827 RBL19. / REMOVED AND REPLACED STRAP PER SRM 51-10-02 AND SRM 51-40-02
FORWARD CARGO AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED BY A/C DUCTING ON W.O. 7530065-AAR. TO BE INSTALLED ON 753-140-00-01Y
AFT CARGO FORWARD CORNER SCUFF PLATE IS CRACKED / REPAIRED BY VENDOR AIRCRAFT DUCTING REPAIR INC ON 08JUN17 UNDER RO# 7530220-A7R. SCUFF PLATE TO BE REINSTALLED ON TASKCARD 753-140-00-02Y.
AFT CARGO AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED BY A.C. DUCTING ON W.O.7530220-A7R TO BE INSTALLED ON 753-140-00-02Y
FORWARD CARGO FORWARD CORNER SCUFF PLATE IS CRACKED / REPAIRED BY VENDOR AIRCRAFT DUCTING REPAIR INC ON 09JUN17 UNDER RO# 7530028-A7R. SCUFF PLATE TO BE REINSTALLED ON TASKCARD 753-140-00-01Y.
AFT RT CABIN EMER LIGHTING, BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
FORWARD RT CABIN EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
AFT LT CABIN EMER LIGHTING, BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
AFT CABIN EMER LIGHTING, BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
L1 DOOR EMER EVAC SLIDE GIRT BAR FWD RETAINER CLIP LOOSE. SECURED CLIP IAW SRM.
SEAT TRACK CRACKED AT STATION 727B, LBL 45.5. REPAIRED TRACK IAW EA.
EMERGENCY EXIT SIGN MID CABIN LOOSE. R & R SIGN IAW MM.
DECLARED EMERGENCY, FUMES IN CABIN. LT CABIN BULLNOSE AISLE EMERGENCY LIGHTS FAULTY BETWEEN ROW 17 TO ROW 20. R&R BATTERY PACK PER AMM.
DECLARED EMERGENCY, FUMES IN CABIN. RT CABIN BULLNOSE AISLE EMERGENCY LIGHTS FAULTY BETWEEN ROW 16 TO ROW 19. R&R BATTERY PACK PER AMM.
CEILING AFT ENTRY EMER EXIT LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW AMM.
BRACKET CRACKED AT BS 540 RT OF CTR. R & R BRACKET IAW SRM.
MID CABIN EMER EXIT LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW AMM.
BRACKET CRACKED AT BS 540 LT OF CTR. R & R BRACKET IAW SRM.
L1 EXTERIOR EGRESS LIGHTS INOPERATIVE. RELAMPED EGRESS IAW MM.
RT AFT BODY EXTERIOR FAIRING EGRESS LIGHTS INOPERATIVE. RELAMPED EGRESS IAW MM.
RT OVERWING EMERGENCY EXIT LIGHT FAILED BATTERY CAPACITY TEST. R & R BATTERY IAW AMM.
AT ROW 23ABC FLOOR EMERGENCY LIGHTING CLEAR LENS MISSING. INSTALLED CLEAR LENS PER M/M.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
FORWARD EEPLS ENDCAP MISSING. INSTALLED ENDCAP PER M/M.
LEFT EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 7. REMOVED AND REPLACED COVER PER M/M.
L2 DOOR EMERENCY EVAC SLIDE COVER AFT GIRT BAR STOW HOOK LOOSE. SECURED HOOK PER SRM.
LEFT EEPLS LENS CRACKED AT ROW 13. REMOVED AND REPLACED LENS PER MM.
L2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MM.
RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW AMM.
EEPLS LENS MISSING 1C. INSTALLED NEW LENS ASSY AT 1C PER MM.
RIGHT EMERGENCY BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. (SUBMITTED AS A SUPPLEMENT, COULDN`T FIND ORIGINAL CONTROL NUMBER.)
RT EMERGENCY BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER AMM.
AFT CABIN MID LEFT EMERGENCY LIGHTS FAILED AT ROW 16. REMOVED AND REPLACED BATTERY CHARGER IAW MM.
LT EMERGENCY BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER AMM.
CABIN FLOOR EMERGENCY LIGHT LENS IS DIRTY AT 13C. REMOVED AND REPLACED LIGHT LENS PER MM.
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
LT EEPLS COVER LOOSE AT ROW 1. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.
EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.