N278WN
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
L1 FWD ENTRY EMERGENCY SLIDE CAME OUT OF CONTAINER. REPACKED L1 DOOR EMERGENCY SLIDE PER MT 725-SWA-105. REF AMM 25-66-00
LEFT MLG CENTER DOOR WEB CRACKED LOWER FWD CORNER. REMOVED CENTER AND INNER LT GEAR DOOR IAW MM 32-13-11 & OK TO CONT IAW CDL 32-10-3X. INSTALLED LT MLG CENTER & INNER DOORS IAW AMM 32-13-11. OPS CHKD GOOD.
FWD ENTRY LT EMERGENCY BATTERY PACK FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
RIGHT WING TRAILING EDGE FLAP DELAMINATION<[01] REMOVED DAMAGED WEDGE PER SRM 51-40-02; LOCATED AND DRILLED NEW WEDGE PER SRM 51-40-06;[02] INSTALLED NEW WEDGE PER SRM 51-40-02;[03] ALL TASKS C/W
CAPTAIN`S SIDE EMERGENCY EXIT LIGHT IS INOPERATIVE. PERFORMED AN OPS TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS TESTED GOOD.
AFT R2 DOOR EMERGENCY EXIT DOOR SLIDE GIRT BAR RETAINER CLIP BROKE. REPLACED R2 ESCAPE SLIDE GIRT BAR RETAINER (STOP ASSY) IAW AMM25-66-01
RIGHT OVER WING EXIT DOOR ASSIST PANEL LOOSE. PANEL SECURED - OK TO CONTINUE PER MEL 25-10-01 SP#1B. INSTALLED MISSING HARDWARE ON EXIT DOOR LINING REF AMM 52-22-51
EMERGENCY LIGHT OVER RT WING INOPERATIVE. REMOVED AND REPLACED PER AMM 33-51-04-960-801-NG.
FWD GALLEY DOOR SLIDE NEEDS TO BE REPOSITIONED. REPOSITIONED FWD SERVICE DOOR SLIDE PER MM 25-66-01 AND MT 725-61-06. OK FOR SERVICE.
RIGHT OVERWING EXIT LIGHT MISSING PLASTIC EXIT COVER<[01] INSTALLED OVER WING EXIT LIGHT COVER PER AMM 33-51-01
(CUSTOMER REQUEST) MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75. 2025-94369<[01] REPLACED MAIN CABIN FLOOR STRUCTURE SUPPORT LOCATED AT STA540 BL 0 TO RBL 24.75 IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG# 143A0060 SHEET 46 REV. - SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED MAIN CABIN FLOOR STRUCTURE SUPPORT LOCATED AT STA540 BL 0 TO RBL 24.75 IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG# 143A0060 SHEET 46 REV. - SEE INDIVIDUAL SIGN OFF BELOW
DETERIORATE PLATE (2EA) AND SHIM (2EA) OF ENTRY DOOR GIRT BAR FITTING AT AFT GALLEY AREA 2025-94357<[01] REPLACED PLATE (2EA) AND SHIM (2EA) OF ENTRY DOOR GIRT BAR FITTING AT AFT GALLEY AREA I.A.W SOPM 20-50-01 REV.38;[02] REPLACED PLATE (2EA) AND SHIM (2EA) OF ENTRY DOOR GIRT BAR FITTING AT AFT GALLEY AREA I.A.W SOPM 20-50-01 REV.38.
DETERIORATE PLATE (2EA) AND SHIM (2EA) OF SERVICE DOOR GIRT BAR FITTING AT AFT GALLEY AREA 2025-94358<[01] REPLACED PLATE (2EA) AND SHIM (2EA) OF SERVICE DOOR GIRT BAR FITTING AT AFT GALLEY AREA I.A.W SOPM 20-50-01 REV.38;[02] REPLACED PLATE (2EA) AND SHIM (2EA) OF SERVICE DOOR GIRT BAR FITTING AT AFT GALLEY AREA I.A.W SOPM 20-50-01 REV.38.
DETERIORATE HARDWARE OF ENTRY DOOR GIRT BAR FITTING AT AFT GALLEY AREA 2025-94359<[01] REPLACED HARDWARE OF ENTRY DOOR GIRT BAR FITTING AT AFT GALLEY AREA I.A.W SOPM 20-50-01 REV.38;[02] REPLACED HARDWARE OF ENTRY DOOR GIRT BAR FITTING AT AFT GALLEY AREA I.A.W SOPM 20-50-01 REV.38.
DETERIORATE HARDWARE OF SERVICE DOOR GIRT BAR FITTING AT AFT GALLEY AREA 2025-94360<[01] REPLACED HARDWARE OF SERVICE DOOR GIRT BAR FITTING AT AFT GALLEY AREA I.A.W SOPM 20-50-01 REV.38;[02] REPLACED HARDWARE OF SERVICE DOOR GIRT BAR FITTING AT AFT GALLEY AREA I.A.W SOPM 20-50-01 REV.38.
DETERIORATE HARDWARE OF SERVICE DOOR GIRT BAR FITTING AT FWD GALLEY AREA 2025-94350<[01] REPLACED HARDWARE OF SERVICE DOOR GIRT BAR FITTING AT FWD GALLEY AREA I.A.W SOPM 20-50-01 REV.38;[02] REPLACED HARDWARE OF SERVICE DOOR GIRT BAR FITTING AT FWD GALLEY AREA I.A.W SOPM 20-50-01 REV.38
DETERIORATE PLATE (2EA) AND SHIM (2EA) OF SERVICE DOOR GIRT BAR FITTING AT AFT GALLEY AREA 2025-94358<[01] REPLACED PLATE (2EA) AND SHIM (2EA) OF SERVICE DOOR GIRT BAR FITTING AT AFT GALLEY AREA I.A.W SOPM 20-50-01 REV.38;[02] REPLACED PLATE (2EA) AND SHIM (2EA) OF SERVICE DOOR GIRT BAR FITTING AT AFT GALLEY AREA I.A.W SOPM 20-50-01 REV.38.
DETERIORATE PLATE (2EA) AND SHIM (2EA) OF ENTRY DOOR GIRT BAR FITTING AT FWD GALLEY AREA 2025-94347<[01] REPLACED PLATE (2EA) AND SHIM (2EA) OF ENTRY DOOR GIRT BAR FITTING AT FWD GALLEY AREA I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D (1)(B);[02] REPLACED PLATE (2EA) AND SHIM (2EA) OF ENTRY DOOR GIRT BAR FITTING AT FWD GALLEY AREA I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D (1)(B)
DETERIORATE PLATE (2EA) AND SHIM (2EA) OF SERVICE DOOR GIRT BAR FITTING AT FWD GALLEY AREA 2025-94348<[01] REPLACED PLATE (2EA) AND SHIM (2EA) OF SERVICE DOOR GIRT BAR FITTING AT FWD GALLEY AREA I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D (1)(B);[02] REPLACED PLATE (2EA) AND SHIM (2EA) OF SERVICE DOOR GIRT BAR FITTING AT FWD GALLEY AREA I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D (1)(B)
DETERIORATE HARDWARE OF ENTRY DOOR GIRT BAR FITTING AT FWD GALLEY AREA 2025-94349<[01] REPLACED HARDWARE OF ENTRY DOOR GIRT BAR FITTING AT FWD GALLEY AREA I.A.W SOPM 20-50-01 REV.38;[02] REPLACED HARDWARE OF ENTRY DOOR GIRT BAR FITTING AT FWD GALLEY AREA I.A.W SOPM 20-50-01 REV.38
CRACK BRACKET LOCATED BS544 AND RBL7 AT AIR CONDITIONING BAY 2025-94314<[01] REPLACED BRACKET LOCATED BS544 AND RBL7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] REPLACED BRACKET LOCATED BS544 AND RBL7 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9
CRACK ANGLE LOCATED BS663.75 AND LBL8 AT WING CENTER SECTION 2025-94310<[01] TOOL USED IN STEP 3: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631 DUE DATE: 11-MAR-25;[02] REPAIRED ANGLE LOCATED STA663.75 AND BTW LBL5 TO LBL25 AT CENTER WING BOX IAW B737-700 SRM 57-10-10-2R-5 REPAIR 5; SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPAIRED ANGLE LOCATED STA663.75 AND BTW LBL5 TO LBL25 AT CENTER WING BOX IAW B737-700 SRM 57-10-10-2R-5 REPAIR 5; SEE INDIVIDUAL SIGN OFF BELOW.
BROKEN EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA 2025-94286<[01] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(10);[02] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(10)
CORROSION BILGE AREA STRAP BS 887 BTW STR 25R TO STR 26L AND WL 156 AT AFT CARGO COMPARTMENT 2025-94298<[01] REPLACED BILGE AREA STRAP BS 887 BTW STR 25R TO STR 26L AND WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.;[02] REPLACED BILGE AREA STRAP BS 887 BTW STR 25R TO STR 26L AND WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.
CRACK TRACK LBBL 17.24 ON BS 767 AT AFT CARGO COMPARTMENT 2025-94301<[01] ON STEP 4: TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101V022235; DUE DATE: 07 OCT 25;[02] REPAIR TRACK LBBL 17.24 ON BS 767 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1.<BR>SEE INDIVIDUAL SIGNOFF BELOW;[03] CORRECTED STEP 2<BR>REPAIR TRACK LBBL 17.24 ON BS 767 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 AND 2<BR>SEE INDIVIDUAL SIGNOFF BELOW;[04] CORRECTED STEP 2 AND 3<BR>REPAIRED TRACK LBBL 17.24 BTW BS 747 TO BS 787 AT AFT CARGO COMPARTMENT IAW B737 700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL SIGN OFF BELOW;[05] CERTIFIED RII MAJOR REPAIR WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.
CRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 215 AT RT WING 2025-94294<[01] REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 215 AT RT WING AND FASTENER IAW B737-700 #DWG:115A2781 SHEET: 2 REV: B AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNS OFF BELOW;[02] REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 215 AT RT WING AND FASTENER IAW B737-700 #DWG:115A2781 SHEET: 2 REV: B AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNS OFF BELOW.JOB COMPLETE.
CRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 215 AT LT WING 2025-94291<[01] REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 215 AT LT WING AND FASTENER IAW B737-700 #DWG:115A2781 SHEET: 2 REV: B AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNS OFF BELOW;[02] REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 215 AT LT WING AND FASTENER IAW B737-700 #DWG:115A2781 SHEET: 2 REV: B AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNS OFF BELOW.JOB COMPLETE.
CRACK FLOOR STRUCTURE ANGLE LOCATED ON BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2025-94299<[01] REPLACED ANGLE LOCATED ON BS 867 AT LEVEL STR 26L IAW B737-700 SRM 51-40-02 AND DWG# 149A8102; SHEET 17; REV: - AND DWG# 149A8104; SHEET 1; REV B. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE LOCATED ON BS 867 AT LEVEL STR 26L IAW B737-700 SRM 51-40-02 AND DWG# 149A8102; SHEET 17; REV: - AND DWG# 149A8104; SHEET 1; REV B. SEE INDIVIDUAL SIGN OFF BELOW.JOB COMPLETE.
CORROSION SUPPORT ZEE BTW BS 727D TO BS 747 AT STR 25L AND WL 154 AT AFT CARGO COMPARTMENT 2025-94300<[01] REPAIRED SUPORT ZEE LOC BTW 727C TO 747 AT STR 25L AND WL 154 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DWG: 146A7500; SHEET:85; REV: A.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGN OFF BELOW<BR>REPAIRED SUPORT ZEE LOC BTW 727C TO 747 AT STR 25L AND WL 154 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DWG: 146A7500; SHEET:85; REV: A.
CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS400 TO BS420 AND STR26L FWD CARGO COMPARTMENT 2025-94237<[01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS400 TO BS420 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #143A7505 SHEET 81 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS400 TO BS420 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #143A7505 SHEET 81 REV.- SEE INDIVIDUAL SIGN OFF BELOW
CRACK STUB FRAME BS 294.5 AT LEVEL STRINGER 17R PASS CABIN 2025-94239<[01] REPLACED FASTENER (2E/A) LOC. ON INNER CHORD BS 294.5 AT LEVEL STRINGER 17R PASS CABIN IAW B737-700 #DWG: 141A8310 SHEET: 25 REV:- AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNS OFF BELOW.;[02] REPLACED FASTENER (2E/A) LOC. ON INNER CHORD BS 294.5 AT LEVEL STRINGER 17R PASS CABIN IAW B737-700 #DWG: 141A8310 SHEET: 25 REV:- AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNS OFF BELOW.JOB COMPLETE.
CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500B TO BS500C AND STR26L FWD CARGO COMPARTMENT 2025-94234<[01] REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS500B TO BS500C AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #143A7505 SHEET 81 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS500B TO BS500C AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #143A7505 SHEET 81 REV.- SEE INDIVIDUAL SIGN OFF BELOW
DETERIORATED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA 2025-94218<[01] REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C (10);[02] REJECT LENS WITH ARROW INDICATE TO INSIDE;[03] INSTALLED CORRECTLY EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C (10);[04] CERTIFIED CORRECTIVE ACTION 3;[05] INSTALLED CORRECTLY EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C (10)
DETERIORATE EMERGENCY LIGHT LENS IN THE WALL FROM LAVATORY A AT FWD GALLEY AREA 2025-94230<[01] REPLACED EMERGENCY LIGHT LENS IN THE WALL FROM LAVATORY A AT FWD GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-802 STEP 3.C (5)(D) AND 3.C(10);[02] REPLACED EMERGENCY LIGHT LENS IN THE WALL FROM LAVATORY A AT FWD GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-802 STEP 3.C (5)(D) AND 3.C(10)
CRACK GUSSET LOCATED BETWEEN BS500D AND STR19R FWD CARGO COMPARTMENT 2025-94232<[01] REPLACED GUSSET LOCATED BETWEEN BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 209 REV: -.;[02] REPLACED GUSSET LOCATED BETWEEN BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 209 REV: -.
CRACK SUPPORT ANGLE BS 294.5 AND STRINGER 13L PASSENGER CABIN 2025-94233<[01] REPLACED SUPPORT ANGLE BS 294.5 AND STRINGER 13L PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG: 141A1311; SHEET:1; REV:C<BR>SEE INDIVIDUAL SIGN OF BELOW;[02] REPLACED SUPPORT ANGLE BS 294.5 AND STRINGER 13L PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG: 141A1311; SHEET:1; REV:C<BR>SEE INDIVIDUAL SIGN OF BELOW
CRACK TIE CLIP LOCATED BS277 AT LEVEL STR10R AT PASSENGER CABIN 2025-94188<[01] REPLACED TIE CLIP LOCATED BS277 AT LEVEL STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED TIE CLIP LOCATED BS277 AT LEVEL STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW JOB COMPLETE AS RII.
CRACK WEB LOCATED BTW BS294.5 TO BS303.9 AT LEVEL STR16L AT PASSENGER CABIN 2025-94185<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 29-JAN-26.;[02] REPLACED WEB LOCATED BTW BS294.5 TO BS303.9 AT LEVEL STR16L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED 2 <BR>REPLACED WEB LOCATED BTW BS294.5 TO BS303.9 AT LEVEL STR16L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A8180; SHEET 27; REV. C. SEE INDIVIDUAL SIGN OFF BELOW DWG 141A8180; SHEET 27; REV. C.;[04] CORRECTED STEP 3<BR>REPLACED WEB LOCATED BTW BS294.5 TO BS303.9 AT LEVEL STR16L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A8180; SHEET 27; REV. C. SEE INDIVIDUAL SIGN OFF BELOW;[05] REPLACED WEB LOCATED BTW BS294.5 TO BS303.9 AT LEVEL STR16L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A8180; SHEET 27; REV. C. SEE INDIVIDUAL SIGN OFF BELOW
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS312 TO BS328 LBL47 FWD GALLEY AND LAV 2025-94182<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS312 TO BS328 LBL47 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #141A5400 SHEET 26 REV.-. REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS312 TO BS328 LBL47 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #141A5400 SHEET 26 REV.-
CRACK INNER CHORD LOCATED BS303.9 LBL55 AT FWD GALLEY AREA 2025-94180<[01] REPLACED INNER CHORD LOCATED AT BS 277 TO BS360 LBL55 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG:141A8110 SHEET: 9 REV:A. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED INNER CHORD LOCATED AT BS 277 TO BS360 LBL55 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG:141A8110 SHEET: 9 REV:A. SEE INDIVIDUAL SIGN OFF BELOW.JOB COMPLETE AS RII.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS328 TO BS344 LBL47 AT FWD GALLEY AND LAV 2025-94183<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS328 TO BS344 LBL47 AT FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 44 REV -. SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS328 TO BS344 LBL47 AT FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 44 REV -. SEE INDIVIDUAL SIGNOFF BELOW
CRACK ON SCUFF PLATE FWD ENTRY DOOR ON POSITION FWD CORNER AT FWD GALLEY AREA 2025-94164<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23399190; DUE DATE: 04/MAR/25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N: 1859843 ; DUE DATE: 10-MAR-25;[03] REPAIRED THE SCUFF PLATE FWD ENTRY DOOR ON POSITION FWD CORNER AT FWD GALLEY AREA I.A.W. BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2; PARAGRAPH 4.B. STEPS (3 TO 6 AND 8); FIGURE 203; BAC 5975. SEE INDIVIDUAL SIGNOFF BELOW.;[04] REPAIRED THE SCUFF PLATE FWD ENTRY DOOR ON POSITION FWD CORNER AT FWD GALLEY AREA I.A.W. BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2; PARAGRAPH 4.B. STEPS (3 TO 6 AND 8); FIGURE 203; BAC 5975.
CRACK INDICATION IN LOWER FASTENER HOLE LOCATED AT BS 727 FRAME INNER CHORD AT S-18A RIGHT SIDE.CRACK DIRECTION 9 O CLOCK.AFT CARGO COMPARTMENT 2025-94144<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 240525411; DUE DATE: 13-NOV-25.;[02] STEP 4. TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 200048001; DUE DATE: 28-MAY-25;[03] 'REFER TO FAULT TTG8Q00YED9N WHERE EA 25-153-00424 WAS ADDED AS A SUBTASK.';[04] CORRECTED STEP 3<BR>REPAIRED LOWER FASTENER HOLE LOCATED AT BS 727 FRAME INNER CHORD AT S-18A RIGHT SIDE.CRACK DIRECTION 9 O CLOCK.AFT CARGO COMPARTMENT IAW EA 25-153-00424;[05] CORRECTED STEP 3 AND 4<BR>'REFER TO FAULT TTG8Q00YED9N WHERE EA 25-153-00424 WAS ADDED AS A SUBTASK.';[06] REPAIRED LOWER FASTENER HOLE LOCATED AT BS 727 FRAME INNER CHORD AT S-18A RIGHT SIDE.CRACK DIRECTION 9 O CLOCK.AFT CARGO COMPARTMENT IAW EA 25-153-00424<BR>5. 'REFER TO FAULT TTG8Q00YED9N WHERE EA 25-153-00424 WAS ADDED AS A SUBTASK.'<BR>TASK RII CERTIFIED
CRACK INDICATION IN UPPER FASTENER HOLE LOCATED AT BS 727 FRAME INNER CHORD AT S-18A RIGHT SIDE.CRACK DIRECTION 11 O CLOCK.AFT CARGO COMPARTMENT 2025-94143<[01] TOOL USED ON STEP 1: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N:240525011; DUE DATE:13-NOV-25.[07] REPAIRED UPPER FASTENER HOLE LOCATED AT BS 727 FRAME INNER CHORD AT S-18A RIGHT SIDE.CRACK DIRECTION 11 O CLOCK.AFT CARGO COMPARTMENT IAW EA 25-153-00424 (AD - N278WN - AEM - REPAIR - FUSELAGE - WHEEL WELL BULKHEAD - AT BSTA 727 AND AT S-18A RHS - WEB & AFT LOWER FITTING - FASTENER HOLE - CRACK.)<BR>TASK CERTIFIED;[08] REPAIRED UPPER FASTENER HOLE LOCATED AT BS 727 FRAME INNER CHORD AT S-18A RIGHT SIDE.CRACK DIRECTION 11 O CLOCK.AFT CARGO COMPARTMENT IAW EA 25-153-00424 (AD - N278WN - AEM - REPAIR - FUSELAGE - WHEEL WELL BULKHEAD - AT BSTA 727 AND AT S-18A RHS - WEB & AFT LOWER FITTING - FASTENER HOLE - CRACK.)<BR>TASK RII CERTIFIED
CRACK INDICATION ON STUB FRAME LOCATED BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FWD GALLEY DOOR AREA(1EA). CRACK LENGTH APPROX 1.250 INCH AT PASSENGER CABIN. 2025-94080<[01] REPLACED STUB FRAME AND FASTENER LOCATE BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FWD GALLEY DOOR AT PASSENGER CABIN IAW B737-700 SRM 51-40-02;#DWG: 141A8370 SHEET: 9 REV: D AND #DWG: 141A8370 SHEET: 11 REV:D.;[02] CORRECTED ACTION 1.<BR><BR>REPLACED STUB FRAME AND FASTENER LOCATE BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FWD GALLEY DOOR AT PASSENGER CABIN IAW B737-700 SRM 51-40-02;#DWG: 141A8370 SHEET: 9 REV: D AND #DWG: 141A8370 SHEET: 11 REV:D.<BR><BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED STUB FRAME AND FASTENER LOCATE BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FWD GALLEY DOOR AT PASSENGER CABIN IAW B737-700 SRM 51-40-02;#DWG: 141A8370 SHEET: 9 REV: D AND #DWG: 141A8370 SHEET: 11 REV:D.<BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.JOB COMPLETE AS RII.
CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2025-94034<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N:A23046221; DUE DATE: 25-MAY-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1859843 ; DUE DATE : 10/MAR/25;[03] REPAIRED FWD CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1; AND BAC 5975. SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED FWD CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1; AND BAC 5975. SEE INDIVIDUAL SIGN OFF BELOW. COMPLETED STEP
BROKEN PHOTOLUMINESCENT STRIP AT PASSENGER CABIN 10EA 2025-93934<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN 10EA IAW SOPM 20-50-12 REV. 56;[02] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN 10EA IAW SOPM 20-50-12 REV. 56
CRACK BODY STATION 663.75 VAPOR BARRIER LBL41 AT MAIN WHEEL WELL COMPARTME 2025-93866<[01] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 15-FEB-25;[02] TOOL USED: SCALE PN: SPX621 SN: 8340225489 DUE DATE: 22-FEB-25.;[03] TOOL USED: SCALE PN: 91847 SN: AE-409320 DUE DATE:29-JUN-25.;[04] TOOL USED: HOT BONDER PN: HCS9200B SN: 18165044 DUE DATE: 11-APR-25.;[05] EQUIPMENT P/N EPOCH 600; S/N 120357005; DUE DATE 10-JUN-25 WAS USED ON STEP 11;[06] REPAIRED BODY STATION 663.75 VAPOR BARRIER LBL41 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNSOFF BELOW;[07] CORRECTIVE ACTION 6 ENTER BY ERROR; CORRECTED CORRECTIVE ACTION IS: REPAIRED BODY STATION 663.75 VAPOR BARRIER LBL41 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] TASK COMPLETED.
RH HORIZONTAL STAB UPPER FWD SLIDER CRACKED<[01] R AND R SLIDER PER SRM 51-40-02.
PASSENGER SEAT 11F SHOULD NOT RECLINE INTO EXIT ROW.<[01] ADJUSTED SEAT AT 11F IAW AMM 25-22-00-201-AR-NG
EMERGENCY LIGHTS AT LEFT ISLE STATIONS 716; 727; 787 GO OUT AFTER A COUPLE OF MINUTES<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]
FWD. SERVICE DOOR COVER PLATE UNDER HANDLE CRACKED.<[01] R&R FWD SERVICE DOOR COVER PLATE PER AMM 52-41-31
AFT CABIN CENTER AISLE TO AFT GALLEY L/H AND R/H EGRESS STRIPS DELAMINATED.<[01] R&R PHOTOLUMINESCENT STRIPS PER AMM 33-51-15
PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES.<[01] REPLACED PANEL PER SRM 51-40-02;[02] INSPECTION C/W REPLACED PANEL PER SRM 51-40-02
SEVERAL AREAS AROUND INTERIOR OF #2 NOSE COWL INLET HAS ABRADABLE SHROUD CRACKED AND DELAMINATED<[01] C/W LOCAL RECONDITION ON #2 ENGINE ABRADABLE SHROUD IAW MT 772-21-05. SEE TTG8Q00RJMKC FOR WORK PERFORMED.
#6 FLAP CANOE IS DELAMINATED ON O/B SIDE<[01] REMOVED AND REPLACED #6 FLAP CANOE AFT CONE IAW SRM 51-40-02.;[02] COMPLIED WITH INSPECTION OF THE REMOVED AND REPLACED #6 FLAP CANOE AFT CONE IAW SRM 51-40-02.
RIGHT AFT EMERGENCY LIGHT BATTERY NOT TESTING<[01] REPLACED RT AFT BATERY PACK. EMERGENCY LT OPS TEST PASS. NO DEFECTS NOTED REF AMM 33-51-06
GIRT BAR HOLDER LOOSE AT FWD ENTRY DOOR [TTG8Q00P6MTB]<[01] R&R GIRT BAR HOLDER RIVETS AS REQUIRED IAW SRM 51-40-02.
GIRT BAR HOLDER LOOSE AT FWD ENTRY DOOR<[01] COMPLIED WITH EA M-23-125-0189 OK TO CONTINUE ON TLD.
GIRT BAR MAIN ENTRY DOOR IS LOOSE<[01] SECURED LOOSE SCREW ON FLOOR BRACKET REF AMM 25-66-02
AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS CRACKED<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT LENDS PER 33-51-01
AFT SERVICE DOOR OUTSIDE EMERGENCY LIGHT NOT WORKING<[01] INSTALLED NEW LIGHT BULB ON THE AFT SERVICE DOOR OUTSIDE EMERGENCY LIGHT REF AMM 33-51-04. OPS CHECK GOOD
CENTER AISLE OVERWING EXIT SIGN BROKEN<[01] R/R OVERWING EXIT LIGHT. OPS CHECK GOOD. REF AMM 33-51-01
SLIDE ON AFT SERVICE DOOR PARTIALLY OUT OF ENCLOSURE<[01] ADJUSTED AFT SERVICE DOOR ESCAPE SLIDE PER AMM 245-66-01.
FLOOR PHOTOLUMINESENT STRIP LIGHTING COVER LOOSE NEAR BACK GALLEY<[01] REINSTALLED PHOTOLUMINESENT STRIP PER AMM 33-51-15 OPS CHECKS GOOD
MISSING GIRT BAR SHIM (2 EA) FWD ENTRY DOOR AT FWD GALLEY AREA (2 EA) 2023-127714<[01] REPLACED GIRT BAR SHIM (2 EA) FWD ENTRY DOOR AT FWD GALLEY AREA (2 EA) I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D.(1).(H).;[02] REPLACED GIRT BAR SHIM (2 EA) FWD ENTRY DOOR AT FWD GALLEY AREA (2 EA) I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D.(1).(H).
MISSING GIRT BAR BOLT AND SHIME AT FWD GALLEY AREA 2023-127614 MISSING GIRT BAR BOLT AND SHIM ON FWD SERVICE DOOR AT FWD GALLEY AREA (1EA)<[01] INSTALLED GIRT BAR BOLT AND SHIM AT FWD GALLEY AREA I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D.(1).(E) THRU 3.D.(1).(H);[02] CORRECTED STEP 1 INSTALLED GIRT BAR BOLT AND SHIM AT FWD GALLEY AREA I.A.W B737-700 AMM 25-66-02-400-801 STEP 3.D.(1).(E) THRU 3.D.(1).(H) SEE INDIVIDUAL SIGN OFF BELLOW;[03] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CORROSION FLOOR STRUCTURE STRAP COMMON NUTPLATE AT BS 790 PLUS 8 IN RBL 18 AT AFT CARGO COMPARTMENT 2023-127702<[01] REPLACED STRAP LOC. BS 790 PLUS 8 IN BTW STR 25R TO STR 26R RBL 18 AT AFT CARGO COMPARTMENT IAW B737-700 SRM: 51-40-02 AND DWG:146A8340 REV. A.;[02] REPLACED STRAP LOC. BS 790 PLUS 8 IN BTW STR 25R TO STR 26R RBL 18 AT AFT CARGO COMPARTMENT IAW B737-700 SRM: 51-40-02 AND DWG:146A8340 REV. A.
CRACK ON INSPAR RIB 120.30 LOWER CHORD AT 7 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER. 2023-127697<[01] ET TOOL USED: PN: MIZ-21C ; SN: 769680; DUE DATE: 07-JUL-23;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[03] PERFORMED PERMANENT REPAIR LOCATED INSPAR RIB 120.30 LOWER CHORD AT 7 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5. REPAIR 5. THIS REPAIR IS CATEGORY A AND NOT FURTHER ACTION REQUIRED. SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR LOCATED INSPAR RIB 120.30 LOWER CHORD AT 7 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5. REPAIR 5. THIS REPAIR IS CATEGORY A AND NOT FURTHER ACTION REQUIRED. RII;SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ON INSPAR RIB 120.30 AT 34 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER. 2023-127698<[01] ET TOOL USED: PN: MIZ-21C ; SN: 769680; DUE DATE: 07-JUL-23;[02] ACCOMPLISHED PERMANENT REPAIR HORIZONTAL STABILIZER - INSPAR RIB SSTA 120.3 - LOWER CHORD IAW EA-23-155-00790-WP1 ; EA 23-155-00790-WIP2 AND EA SUMMARY 23-155-00790. SEE INDIVIDUAL SIGN OFF BELLOW.;[03] ACCOMPLISHED PERMANENT REPAIR HORIZONTAL STABILIZER - INSPAR RIB SSTA 120.3 - LOWER CHORD IAW EA-23-155-00790-WP1 ; EA 23-155-00790-WIP2 AND EA SUMMARY 23-155-00790. RII; SEE INDIVIDUAL SIGN OFF BELLOW.
CRACK ANGLE - SUPPORT BS 380 TO BS400 BL0 WL 208 AT FWD GALLEY AREA 2023-127694<[01] REPLACED NEW ANGLE SUPPORT BS 380 TO BS400 BL0 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 143A5400 SHEET:92 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW
CRACK WEB COMMON TO AFT PRESSURE BULKHEAD BS 1016 BTW BL 0 TO RBL 8 WL 208 2023-127681<[01] REPLACED WEB COMMON TO AFT PRESSURE BULKHEAD BS 1016 BTW BL 0 TO RBL 8 WL 208 IAW B737-700 SRM 51-10-02 AND 51-40-02 DWG 148A0922 REV - SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CORROSION FLOOR STRUCTURE PLATE BTW BS 787 TO BS 790 BTW S 25R TO S 26R AT RBL 18 AT AFT CARGO COMPARTMENT 2023-127664<[01] REPLACED PLATE BTW BS 787 TO BS 790 BTW STR 25R TO STR 26R AT RBL 18 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG:146A8340 REV. A.;[02] REPLACED PLATE BTW BS 787 TO BS 790 BTW STR 25R TO STR 26R AT RBL 18 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG:146A8340 REV. A.
CRACK FLOOR STRUCTURE SUPPORT ANGLE LOCATED ON BS 807 AT LEVEL RBL 18 AT AFT CARGO COMPARTMENT 2023_127661<[01] REPLACED SUPPORT ANGLE LOCATED ON BS 807 AT LEVEL RBL 18 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 51-40-02 AND DWG 146A8120 REV-.SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT ANGLE LOCATED ON BS 807 AT LEVEL RBL 18 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-9;51-40-02 AND DWG 146A8120 REV-.SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 1 AND 2.<BR>REPLACED SUPPORT ANGLE LOCATED ON BS 807 AT LEVEL RBL 18 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DWG 146A8120 REV-.SEE INDIVIDUAL SIGN OFF BELOW;[04] REPLACED SUPPORT ANGLE LOCATED ON BS 807 AT LEVEL RBL 18 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DWG 146A8120 REV-.ITEM RII SEE INDIVIDUAL SIGN OFF BELOW
CORROSION FLOOR STRUCTURE PLATE BTW BS 847 TO BS 850 AT LEVEL RBL 18 BTW S 25R TO S 26R AT AFT CARGO COMPARTMENT 2023-127666<[01] REPLACED STRAP AND FASTENER LOCATED BTW BS 847 TO BS 850 AT LEVEL RBL 18 BTW S 25R TO S 26R AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02 AND DRAWING 146A0081 REV - SEE INDIVIDUAL SING-OFFS BELOW.;[02] REMOVED STRAP FLOOR STRUCTURE LOCATED BTW BS 847 TO BS 850 AT LEVEL RBL 18 BTW S 25R TO S 26R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 RII
CORROSION STRAP ON BS 887 BTW S 25R TO S 26L AT WL 153 AT AFT CARGO COMPARTMENT 2023-127667<[01] REPLACED STRAP ON BS 887 BTW S 25R TO S 26L AT WL 153 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETED <BR>REPLACED STRAP ON BS 887 BTW S 25R TO S 26L AT WL 153 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 SEE INDIVIDUAL SIGN OFF BELOW<BR>RII
CORROSION FLOOR STRUCTURE SHIELD PLATE BTW BS 767 TO BS 790 AT LEVEL S 25R AND RBL 21 AT AFT CARGO COMPARTMENT 2023-127665<[01] REPLACED PLATE LOCATED BTW BS 767 TO BS 790 AT LEVEL S 25R AND RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02;SRM 51-40-02.AND DWG 146A0081 SHEET 28 REV A . SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED PLATE LOCATED BTW BS 767 TO BS 790 AT LEVEL S 25R AND RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02;SRM 51-40-02.AND DWG 146A0081 SHEET 28 REV A . SEE INDIVIDUAL SIGN OFF BELOW... RII ITEM
CORROSION SUPPORT ZEE BTW BS 727E TO BS 807 AT LEVEL S 25L AT LBL 21 AT AFT CARGO COMPARTMENT 2023-127668<[01] UT EQUIPMENT P/N: 45MG; S/N: 221859911; DUE DATE: 07-NOV-23;[02] REPLACED SUPPORT ZEE AND FASTENERS BTW BS 727E TO BS 807 AT LEVEL S 25L AT LBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9;51-40-02 AND DWG 146A7500 REV A.SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED SUPPORT ZEE AND FASTENERS BTW BS 727E TO BS 807 AT LEVEL S 25L AT LBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9;51-40-02 AND DWG 146A7500 REV A.SEE INDIVIDUAL SIGN OFF BELOW
CRACK BILGE AREA ANGLE BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT 2023-127660<[01] REPLACED ANGLE LOCATED ON BILGE AREA BTW BS907 TO 927 AND BTW STR25R TO STR27R AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 146A7221 SHEET 24 REV.-<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTIVE ACTION CERTIFIED RII <BR><BR>REPLACED ANGLE LOCATED ON BILGE AREA BTW BS907 TO 927 AND BTW STR25R TO STR27R AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 146A7221 SHEET 24 REV.- <BR>SEE INDIVIDUAL SIGN-OFF BELOW
CORROSION WEB - INTERCOSTAL BTW BS 747 TO BS 767 AT LEVEL S 25R AND RBL 21 AT AFT CARGO COMPARTMENT 2023-127670<[01] REPLACED WEB - INTERCOSTAL BTW BS 747 TO BS 767 AT LEVEL S 25R AND RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A7500; SHEET 88 AND REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CORROSION FLOOR STRUCTURE PLATE BTW BS 790 TO BS 807 BTW STR 25R AND STR 26R AT LEVEL RBL 18 AT AFT CARGO COMPARTMENT 2023-127663<[01] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 38 DL PLUS; S/N: 120398603; DUE DATE: 07-NOV-23.;[02] UT TOOL USED PN: 38DLPLUS ; SN: 120398603. DUE DATE: 07-NOV-23;[03] REPLACED NEW FLOOR STRUCTURE PLATE BTW BS 790 TO BS 807 BTW STR 25R AND STR 26R AT LEVEL RBL 18 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081 SHEET:31 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[04] REPLACED NEW FLOOR STRUCTURE PLATE BTW BS 790 TO BS 807 BTW STR 25R AND STR 26R AT LEVEL RBL 18 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081 SHEET:31 REV:-RII; SEE INDIVIDUAL SIGN OFF BELOW.
CORROSION SUPPORT ZEE BTW BS 727C TO BS 767 AT LEVEL S 25R AT LBL 21 AT AFT CARGO COMPARTMENT 2023-127669<[01] TOOL USED P/N: 45MG; S/N: 130066401; CAL DUE: 21-SEP-23.;[02] REPLACED SUPPORT ZEE AND FASTENERS BTW BS 727C TO BS 767 AT LEVEL S 25R AT LBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ÿ½TEM 9;51-40-02 AND DWG 146A7500 REV A.SEE INDIVIDUAL SIGN OFF BELOW;[03] JOB COMPLETED CERTIFIED RII
CORROSION LOWER SILL BTW BS 790 TO BS 847 AT LEVEL STR 25R AND RBL 21 AT AFT CARGO COMPARTMENT 2023-127662<[01] REPLACED LOWER SILL AND FASTENERS LOCATED BTW BS 807 TO BS 847 AT LEVEL STR 25R AND RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SRM 51-10-02 ITEM 9 AND DWG 146A8340 REV: A;[02] REPLACED LOWER SILL AND FASTENERS LOCATED BTW BS 807 TO BS 847 AT LEVEL STR 25R AND RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SRM 51-10-02 ITEM 9 AND DWG 146A8340 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED LOWER SILL AND FASTENERS LOCATED BTW BS 807 TO BS 847 AT LEVEL STR 25R AND RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SRM 51-10-02 ITEM 9 AND DWG 146A8340 REV: A. RII; SEE INDIVIDUAL SIGN OFF BELOW.
CRACK GUSSET LOCATED BS 500D STRINGER 21L FWD CARGO COMPARTMENT 2023-127581<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 21L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 143A7902 REV -;[02] REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 21L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 143A7902 REV -.SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED AS RII <BR>REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 21L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 143A7902 REV -.SEE INDIVIDUAL SIGN OFF BELOW
CRACK GUSSET LOCATED BS 500D STRINGER 19R FWD CARGO COMPARTMENT 2023-127582<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 143A7902 REV -;[02] CORRECTED STEP 1.REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 143A7902 REV -.SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED AS RII <BR>REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 143A7902 REV -.SEE INDIVIDUAL SIGN OFF BELOW
CRACK GUSSET LOCATED BS 500D STRINGER 19L FWD CARGO COMPARTMENT 2023-127580<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 143A7902 REV -;[02] REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 143A7902 REV -.SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED AS RII <BR>REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 143A7902 REV -.SEE INDIVIDUAL SIGN OFF BELOW
CORROSION ON FLOOR BEAM 986.5 LBL 46.5 WL 208 AT AFT GALLEY AREA 2023-127571<[01] TOOL USED PN NORTEC 600D SN 220272712 DUE DATE 17-DEC-23;[02] TOOL USED: FLAPSPEED; PN: FPK-PRO-104; SN: PRO-3448; DUE DATE: 27-JUN-23;[03] PERFORMED PERMANENT REPAIR AT FLOOR BEAM BS 986.5 UPPER FLANGE BTW LBL 35 TO LBL 47 WL 208. AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6. REPAIR 6. ALTERNATIVE 4. SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR AT FLOOR BEAM BS 986.5 UPPER FLANGE BTW LBL 35 TO LBL 47 WL 208. AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6. REPAIR 6. ALTERNATIVE 4. SEE INDIVIDUAL SIGN OFF BELOW... RII ITEM
CORROSION ON STRAP BTW BS 1006 TO BS 1016 RBL 2 AND WL 208 AFT GALLEY AREA 2023-127570<[01] REPLACED NEW STRAP BTW BS 1006 TO BS 1016 RBL 2 AND WL 208 AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 147A5730 SHEET:23 REV:C SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1.<BR>REPLACED STRAP BTW BS 1006 TO BS 1016 RBL 2 AND WL 208 AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 147A5730 SHEET:23 REV:C SEE INDIVIDUAL SIGN OFF BELOW;[03] JOB COMPLETED RII.
CORROSION ON FLOOR BEAM 986.5 RBL 46.5 WL 208 AT AFT GALLEY AREA 2023-127569<[01] TOOL USED PN NORTEC 600D SN 220272712 DUE DATE 17-DEC-23;[02] TOOL USED: FLAPSPEED; PN: FPK-PRO-104; SN: PRO-3448; DUE DATE: 27-JUN-23;[03] PERFORMED PERMANENT REPAIR AT FLOOR BEAM BS 986.5 UPPER FLANGE BTW RBL 35 TO RBL 47 WL 208. AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6. REPAIR 6. ALTERNATIVE 4. SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR AT FLOOR BEAM BS 986.5 UPPER FLANGE BTW RBL 35 TO RBL 47 WL 208. AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6. REPAIR 6. ALTERNATIVE 4. SEE INDIVIDUAL SIGN OFF BELOW... RII ITEM
CRACK ON WEB-INTERCOSTAL BTW BS 312 TO BS 328 RBL 35 WL 208 FWD GALLEY AREA 2023-127568<[01] REPLACED WEB INTERCOSTAL BTW BS 312 TO BS 328 RBL 35 WL 208 FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET:39 REV:- SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED WEB INTERCOSTAL BTW BS 312 TO BS 328 RBL 35 WL 208 FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET:39 REV:- SEE INDIVIDUAL SIGN-OFF BELOW<BR>CERTIFIED AS RII
CRACK WEB -INTERCOSTAL BTW BS 280 TO BS 294.5 RBL 5 WL 208 AT FWD GALLEY AREA 2023-127563<[01] REPLACED WEB -INTERCOSTAL BTW BS 280 TO BS 294.5 RBL 5 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET:20 REV:-SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED WEB -INTERCOSTAL BTW BS 280 TO BS 294.5 RBL 5 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET:20 REV:- RII; SEE INDIVIDUAL SIGN-OFF BELOW
CRACK ON WEB-INTERCOSTAL BTW BS 328 TO BS 344 LBL 46 WL 208 FWD GALLEY AREA 2023-127561<[01] REPLACED NEW WEB-INTERCOSTAL BTW BS 328 TO BS 344 LBL 46 WL 208 FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET:44 REV:- SEE INDIVIDUAL SIGN-OFF BELOW;[02] CERTIFIED STEP 1 COMPLETED <BR>ITEM RII
CRACK STRINGER 27L LACATED STA 540 FWD CARGO COMPARTMENT 2023-127548<[01] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 45 MG; S/N: 130063701; DUE DATE: 16-JUN-23.;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[03] REPAIRED STRINGER 27L LOCATED BTW BS 500D AND BS 540 FWD CARGO COMPARTMENT IAW SRM B737-700 B737-700 53-00-03-2R-1 REPAIR 1 SEE INDIVIDUAL SIGNOFFS BELOW.;[04] TASK CARD COMPLETED <BR><BR>REPAIRED STRINGER 27L LOCATED BTW BS 500D AND BS 540 FWD CARGO COMPARTMENT IAW SRM B737-700 B737-700 53-00-03-2R-1 REPAIR 1 SEE INDIVIDUAL SIGNOFFS BELOW.<BR>RII
CORROSION ON PLATE COMMON THRESHOLD PANEL AT BS 767 2023-127535<[01] REPLACED PLATE COMMON THRESHOLD PANEL AT BS 807 RBL 18 IAW B737-700 SRM 51-40-02 VERIFIED EXACTLY LOCATION;[02] CORRECTED STEP 1.<BR>REPLACED PLATE COMMON THRESHOLD PANEL AT BS 807 RBL 18 IAW B737-700 SRB 51-10-02 ITEM 9 SRM 51-40-02 VERIFIED EXACTLY LOCATION;[03] CORRECTED STEP 1.<BR>REPLACED PLATE COMMON THRESHOLD PANEL AT BS 797 RBL 18 IAW B737-700 SRB 51-10-02 ITEM 9 VERIFIED EXACTLY LOCATION REFER TO TTG8Q00498U0 FOR PLATE INSTALLATION;[04] JOB COMPLETED.<BR>ACCOMPLISHED VISUAL INSPECTION ON AREA AND NO ADDITIONAL DAMAGES FOUND.
CRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 690 AT RBL 24.75 AT PASSENGER CABIN 2023-127528<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE PID CTRL P/N: 48VFL11; S/N: AE-31448; DUE DATE: 14-JUN-23.;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATED ON BS 690 AT RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG273A9110 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED ANGLE FLOOR STRUCTURE LOCATED ON BS 690 AT RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG273A9110 REV:-. SEE INDIVIDUAL SIGN OFF BELOW. AS RII
CRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 540 BTW BL 0 TO RBL 24.75 AT PASSENGER CABIN 2023-127522<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED ON BS 540 BTW BL 0 TO RBL 24.75 AT PASSENGER CABINIAW B737-700 SRM 51-40-02 AND DWG 143A0060 REV-. SEE INDIVIDUAL STEP BELOW;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATED ON BS 540 BTW BL 0 TO RBL 24.75 AT PASSENGER CABINIAW B737-700 SRM 51-40-02 AND DWG 143A0060 REV-. SEE INDIVIDUAL STEP BELOW. COMPLETED
CORROSION ON PLATE COMMON THRESHOLD PANEL AT BS 847.5 2023-127536<[01] REPLACED PLATE COMMON THRESHOLD PANEL AT BS 847.5 IAW B737-700 SRM 51-40-02;[02] CORRECTED STEP 1.<BR>REPLACED PLATE COMMON THRESHOLD PANEL AT BS 847.5 IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[03] REPLACED PLATE COMMON THRESHOLD PANEL AT BS 847.5 IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02
CRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 690 AT BL 0 AT PASSENGER CABIN 2023-127527<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE PID CTRL P/N: 48VFL11; S/N: AE-31448; DUE DATE: 14-JUN-23.;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATED ON BS 690 AT BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 273A9110 REV:A SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPLACED ANGLE FLOOR STRUCTURE LOCATED ON BS 690 AT BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 273A9110 REV:A SEE INDIVIDUAL SIGNOFFS BELOW. AS RII
CRACK FLOOR STRUCTURE ANGLE LOCATED ON BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN 2023-127521<[01] REPLACED FLOOR STRUCTURE ANGLE LOCATED ON BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A0060 REV-. SEE INDIVIDUAL STEP BELOW;[02] REPLACED FLOOR STRUCTURE ANGLE LOCATED ON BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A0060 REV-. SEE INDIVIDUAL STEP BELOW. COMPLETED
DELAMINATED FLOR PANEL 242AF AT PASSENGER CABIN 2023-127483CORRECT FAULT DESCRIPTION:DELAMINATED FLOOR PANEL 242AF AT PASSENGER CABIN<[01] TOOL USED: HOT BONDER PN: HCS9200B-AV;SN: 18185733;DUE DATE: 23-JAN-24.;[02] TOOL USED SCALE P/N: SPX621; S/N: 8340225441; DUE DATE: 20-JUL-2;[03] TOOL USED: HOT BONDER PN: HCS9000B-AV; SN:18164925 DUE DATE: 22-JAN-24;[04] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N:18185781 DUE DATE: 24 JAN 24.;[05] REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189526; 20-DEC-23. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189526; 20-DEC-23 RII COMPLETED
CRACK DOOR CUTOUT SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2023-127493<[01] TOOL USED: BLACK LIGHT METER : P/N XDS- 1000 S/N 1998072 DUE DATE : 03-MAY-23.;[02] REPAIRED BY WELD SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A21143279; DUE DATE 31-DEC-23 SEE INDIVIDUAL SIGNOFFS BELOW;[03] JOB COMPLETED
DELAMINATED FLOR PANEL 241BF AT PASSENGER CABIN 2023-127485CORRECT FAULT DESCRIPTION:DELAMINATED FLOOR PANEL 241BF AT PASSENGER CABIN<[01] TOOL USED: HOT BONDER PN: HCS9200B-AV;SN: 18185733;DUE DATE: 23-JAN-24;[02] TOOL USED SCALE P/N: SPX621; S/N: 8340225441; DUE DATE: 20-JUL-23.;[03] TOOL USED: HOT BONDER PN: HCS9000B-AV; SN:18164925 DUE DATE: 22-JAN-24;[04] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N:18185781 DUE DATE: 24 JAN 24.;[05] REPAIRED FLOOR PANEL 241BF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189526; 20-DEC-23. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] REPAIRED FLOOR PANEL 241BF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189526; 20-DEC-23 RII COMPLETED
DELAMINATED FLOR PANEL 231ZF AT PASSENGER CABIN 2023-127481CORRECT FAULT DESCRIPTION:DELAMINATED FLOOR PANEL 231F AT PASSENGER CABIN<[01] TOOL USED: HOT BONDER PN: HCS9200B-AV;SN: 18185733;DUE DATE: 23-JAN-24;[02] TOOL USED SCALE P/N: SPX621; S/N: 8340225441; DUE DATE: 20-JUL-23.;[03] TOOL USED: HOT BONDER PN: HCS9000B-AV; SN:18164925 DUE DATE: 22-JAN-24;[04] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N:18185781 DUE DATE: 24 JAN 24.;[05] REPAIRED FLOOR PANEL 231ZF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189526; 20-DEC-23. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] REPAIRED FLOOR PANEL 231ZF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189526; 20-DEC-23.RII COMPLETED
DELAMINATED FLOR PANEL 232SF AT PASSENGER CABIN 2023-127487CORRECT FAULT DESCRIPTION:DELAMINATED FLOOR PANEL 232SF AT PASSENGER CABIN<[01] TOOL USED SCALE P/N: SPX621; S/N: 8340225441; DUE DATE: 20-JUL-23.;[02] TOOL USED: HOT BONDER PN: HCS9000B-AV; SN:18164925 DUE DATE: 22-JAN-24;[03] TOOL USED HOT BONDER P/N: HCS9200B-AV S/N:18185781 DUE DATE: 24 JAN 24.;[04] REPAIRED FLOOR PANEL 232SF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189526; 20-DEC-23; HOT BONDER PN: HCS9200B-AV; SN: 18185733;DUE DATE: 23-JAN-24. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] REPAIRED FLOOR PANEL 232SF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. TOOL USED: CALIPER P/N: 500-197-30; S/N: B20189526; 20-DEC-23; HOT BONDER PN: HCS9200B-AV; SN: 18185733;DUE DATE: 23-JAN-24.RII COMPLETED
CRACK INSPAR RIB 120.30 AT 18 INCHES FROM FRONT SPAR AT LT HORIZONTAL STABILIZER 2023-127441<[01] ET TOOL USED: PN: MIZ-21C ; SN: 769680; DUE DATE: 07-JUL-23;[02] TOOL USED PN:NORTEC 600D;PN:200053402;DUE DATE:13-MAY-23;[03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[04] TOOL USED: Bÿ½SCULA; PN: SCA-301; SN: AE-412136; DUE DATE: 14-MAR-23;[05] 'REFER TO FAULT TTG8Q00J4TZ0 WHERE EA 23-155-00790 WAS ADDED AS A SUBTASK.'; SEE INDIVIDUAL STEP SIGN OFFS BELOW;[06] 'REFER TO FAULT TTG8Q00J4TZ0 WHERE EA 23-155-00790 WAS ADDED AS A SUBTASK.'; RII; SEE INDIVIDUAL STEP SIGN OFFS BELOW
BROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2023-127410<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) I.A.W B737-700 AMM 33-51-15-400-802 AND DWG 33500007 REV .2;[02] COMPLETED
CUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT RT WING 2023-127406<[01] TOOL USED CALIPER P/N 500-197-30 S/N A21147765 DUE DATE 08/NOV/23.;[02] TOOL USED BOND TESTER PN S-3 SN 064 DUE DATE 19-JUL-23;[03] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18185847 DUE DATE: 24-SEP-23;[04] TOOL USED: POSITECTOR P/N:NS2 S/N:138341 DUE DATE: 06-JUL-23;[05] TOOL USED CALIPER P/N: 500-193-30 S/N: 0000288 DUE DATE: 27-DEC-23.;[06] REPAIRED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT RT WING IAW B737-700 SRM 57-53-01-2R-18 REPAIR 18. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] TASK COMPLETED. RII COMPLETED.
L1 DOOR SLIDE GIRT BAR STOWAGE BRACKET HAD ONE RIVET SHEARED. INSTALLED A RIVET IAW SRM 51-40-02.
FORWARD SERVICE DOOR GIRT BAR HOLDER ON LEFT SIDE<[01] ADJUSTED FWD SERVICE DOOR SLIDE COVER BRACKET PER SIP
FWD ENTRY DOOR AND FWD SERVICE DOOR EXTERIOR EMERGENCY LIGHTS INOP / [01] RELAMPED PER 33-51-04
RUDDER COUNTERBALANCE WEIGHT IS ERODED; LOOSE AND SEALANT IS MISSING FROM THE SEAMS. RUDDER COUNTERBALANCE WEIGHT IS ERODED LOOSE AND MISSING SEALANT FROM THE SEAMS. / [01] REPLACED RUDDER COUNTERBALANCE WEIGHT PER CMM 55-40-09;[02] C/W INSPECTION PER CMM 55-40-09.
FLT ATT REPORTS; RIGHT HAND OVERWING EXIT SIGN LOOSE / [01] SECURED LENS PER M/M 33-51-01
LENS AFT OF RH EMERGENCY EXIT MISSING / [01] REF AMM 33-51-01 SECURED LENS. OK FOR SERVICE
FLIGHT ATTENDANT REPORTS A FWD GALLEY FLASHLIGHT INOP / [01] R&R EMERGENCY FLASHLIGHT BATTERY PER AMM 25-64-00
NR 1 ENGINE OVERHEAT LIGHT DURING CLIMBOUT PASSING 20;000' 300KTS 97 N1EGT APPROX830 BOTH ENGINES& ALL ENGINE INDICATIONS NORMAL. NO ENGINE SURGING; TEMPS; FUEL FLOW ALL NORMAL BOTH ENGINES. OVHT LIGHT ; #1 ENGINE OVERHEAT LIGHT DURING CLIMBOUT PASSING 20;000' 300KTS 97 N1EGT APPROX830 BOTH ENGINES& ALL ENGINE INDICATIONS NORMAL. NO ENGINE SURGING; TEMPS; FUEL FLOW ALL NORMAL BOTH ENGINES. OVHT LIGHT EXTINGUISED WHEN THRUST LEVER WAS CLOSED RTB BNA ALL CHECK LIST COMPLETED. NOTE #1 OVERHEAT LIGHT WAS ON FIRE CONTROL PANEL. 'A' LOOP MEL'D. / [01] INSPECTED #1 ENG A&B FIRE LOOPS CLEANED & RESEATED LOOP CONNECTORS DP1501 &DP1601 NO VISUAL DEFECTS NOTED PREFORMED OPERATIONAL TEST AS PER MM 26-11-00
L1 DOOR ASSIST HANDLE LOOSE / RESECURED L1 DOOR ASSIST HANDLE PER B737-700 AMM 52-11-31-400-801 SUB TASK 52-11-31-020-011
EMERGENCY LIGHTS OPS TEST FAILED AT LEFT EMERGENCY EXIT DOOR. / REMOVED AND REPLACED BATTERY PACK POS M1668 AND PERFORMED OPS TEST FOUND NORMAL AS PER REF B737 AMM 33-51-06-960-805; WDM 33-51-13.
MAIN CABIN FLOOR PANEL # 241AF TOP SURFACE FIBER LAYERS DAMAGED. / CLEANED AND REPAIRED WITH A PERMANENT REPAIR ON TOP SURFACE OF MAIN CABIN FLOOR. PANEL #241AF AS PER B737 SRM 53-00-50-2R-1 MATERIALS USED PO# 169458
CUSTOMER REQUEST: R/H VAPOR BARRIER CRACKED / CLEANED AND REPAIRED DAMAGE R/H VAPOR BARRIER AN STA 663 RBL 44' SIZE OF CRACK 8'. STOP DRILL CRACK PERFORMED DRY-OUT; AND INSTALLED A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-10. PERFORMED TAP-TEST ON REPAIRED AREA FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 (SEC5) PRIMED AND TOP COAT VAPOR BARRIER AS PER B737 AMM 51-21-72-370-801.MATERIAL USED PO#1694548; PO#1709723; PO#1693633; PO#1704546; PO#1705870
RIGHT WING DEFLECTION CONTROL RIB PANEL VERTICAL BULB SEAL FITTING CRACKED MKD / REMOVED AND REPLACED WEB AT R/W DEFLECTION CONTROL RIB PANEL VERTICAL AS PER B737-7 SRM 51-40-02-0G-0
RIGHT WING DEFLECTION CONTROL RIB PANEL T/ E BULB SEAL RETAINER CRACKED MKD DOT 60-010 / REMOVED AND REPLACED FITTING AT R/W DEFLECTION CONTROL RIB PANEL T/E AS PER B737-7 SRM 51-40-02-0G-0
AFT E & E DOOR WILL NOT CLOSE. R & R AFT EE DOOR BOTH ROLLER TRUCK ASSYS. OPS OKAY AMM 52-48-41.
FWD RT EMERGENCY LIGHT NOT WORKING. R & R RT BATTERY PACK, PER AMM 33-51-06. OPERATIONS CHECK GOOD.
GIRT BAR GOT WEDGED IN DOOR FRAME / 'PLASTIC/CLOTH' PIECE THAT HOLDS GIRT BAR IN PLACE WAS STICKING OUT TO FAR. POPPED GIRT BAR OUT OF HOLDER RE-SECURED SLIDE GIRT BAR PER SIP. OPS CHECK GOOD & AMM 25-66-01
FWD LEFT SIDE CABIN EMERGENCY LIGHTS INOP. / R & R FWD LEFT EMERGENCY BATTERY PACK IN FWD GALLEY CEILING IAW AMM 33-51-06; OPS CHK GD.
#2 FIRE WARNING DOES NOT TEST IN 'NML' / R & R #2 ENG 'B' LOOP CORE FIRE DETECTION HARNESS IAW AMM 26-11-02; OPS CHK GD. CLOSING #37386 (CLOSING DMA #0151548).
FWD LOWER EMERGENCY FLASHLIGHT BATTERY WEAK R/R EMERGENCY BATTERY ON FWD LWER EMERGENCY FLASHLIGHT PER M/M 25-64-00
DECLARED EMERGENCY------------------------------------------------------TRAILING EDGE FLAPS REMAINED BETWEEN 265 WITH FLAP HANDLE AT 15. MOVED THE FLAPS TO 15 ELECTRICALLY. / R&R FLAP POSITION INDICATOR PER AMM.
R/H FORWARD BULKHEADS CRACKED IN WHEEL WELL AT BS. 663.75, BETWEEN LBL 31.83 TO LBL 40. REPAIRED BULKHEAD IAW SRM.
L/H FORWARD BULKHEADS CRACKED IN WHEEL WELL AT BS. 663.75, BETWEEN LBL 40 TO LBL 31.83. / REPAIRED BULKHEAD IAW SRM.
DIVERSION/DECLARED EMERGENCY, ON CLIMBOUT WE GOT A RAPID 1500 LB IMBALANCE - LEFT TANK SHOWED LESS FUEL WITH FULL AVAILABLE IN CENTER TANK - CROSSFEED OPERATED NORMALLY - FF NORMAL LANDED WITH 16.0 FUEL - WE COULD FEEL THE IMBALANCE ON LANDING. R&R L/H STR FUEL BOOST PUMP AS A PRECAUTIONARY PER AMM.
SUPPLEMENTAL INFORMATION, RIGHT CENTER PUMP STOPPER FEEDING NIGHT ENGINE CLIMBING THROUGH FC 180 CAUSING WING FUEL IMBALANCED. 1200 CBS SMOOTH AIR NO TURBULENCE NO CENTER PUMP LIGHT ILLUMINATED. R&R CIR RIGHT BOOST PUMP PER AMM.
EMERGENCY LIGHTS BATTERY PACK M1670 INOP. R&R BATTERY PACK PER AMM.
FORWARD CARGO BAY AFT SCUFF PLATE IS CRACKED / REMOVED AND REPLACED FCB AFT SCUFF PLATE I.A.W. AMM 53-11-02-020-801 AND AMM 53-11-02-420-801
FORWARD CARGO BAY FWD SCUFF PLATE IS CRACKED / REMOVED AND REPLACED FCB FWD SCUFF PLATE I.A.W AMM 53-11-02-020-801 AND AMM 53-11-02-420-801
INTERCOSTAL ATTACH ANGLE CORRODED BETWEEN BS. 767 TO BS. 787, RBL 21. R&R ANGLE PER SRM & DWG.
RH HORIZONTAL STAB RIB AT 120.30 IS CRACKED AT LOWER END OF 4TH VERTICAL STIFFENER FROM THE FRONT / REPAIRED RH HORIZONTAL RIB 120.30 AT LOWER END OF 4TH VERTICAL STIFFENER FROM THE FRON PER SRM 55-10-09-2R-4
RH HORIZONTAL STAB RIB AT 120.30 IS CRACKED AT LOWER END OF 3RD VERTICAL STIFFENER FROM THE FRONT. REPAIRED RH HORIZONTAL RIB 120.30 AT LOWER END OF 3RD VERTICAL STIFFENER FWD THE FRONT PER SRM 55-10-09-2R-4.
AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 22. R&R SHIELD PER SRM.
AFT CARGO BAY BULKHEAD FITTING CRACKED AT BS. 947, LBL 10. R&R FITTING PER SRM AND DWG.
RH HORIZONTAL STAB RIB 129.5 HAS A CRACK ON FWD CHORD (STIFFENER) TO FRONT SPAR REMOVED AND REPLACED RH HORIZONTAL STAB RIB 129.5 IAW. SRM AND DWG
R1 DOOR CUTOUT FITTING CRACKED AT FORWARD EDGE OF WL 222. R&R DEPRESSOR PER SRM AND DWG.
RT HORIZONTAL STABILIZER RIB CRACKED AT STA. 129.5 CRACKED AT AFT CHORD STIFFENER TO REAR SPAR. R&R STIFFENER IAW ER, EA, AND SRM.
***CORROSION*** ON EXTERNAL DOUBLER AT ROW 44 BS747+ 7.5' BL0 - RBL2.5. / CORROSION ON ROW 44 DOUBLER AT BS747+7.5' BL0-RBL2.5 WAS REPAIRED IAW ATS ER 19-02804 REV IR DATED 07MAY19 AND EA 1-753-34778 REV IR
PANEL 193B HAS DELAMINATION ON EDGE BAND / REPAIRED DELAMINATION DAMAGE ON EDGE BAND ON PANEL 193B IAW SRM 51-70-05-2R-6.
EXTERNAL POWER DOOR CUTOUT BARE STRAP ALONG FORWARD EDGE DEFORMED. REPAIRED STRAP IAW ER AND EA.
EXTERNAL POWER DOOR CUTOUT PREVIOUS REPAIR AT AFT CENTER LATCH DAMAGED. REPAIRED CUTOUT IAW ER AND EA.
L/H WING UPPER OUTBOARD FIXED TRAILING EDGE PANEL VERTICAL CURVED BULB SEAL SUPPORT CRACKED. / R&R SUPPORT IAW SRM.
FLOOR TO SIDEWALL SUPPORT CRACKED AT BS. 767, LBL 22. R&R SUPPORT IAW SRM AND DWG.
AFT CARGO BAY FLOOR TRACK AROUND FASTENER HOLE CORRODED BETWEEN BS. 727 TO BS. 887, RBL 14. R&R FLOOR TRACK PER SRM & DWG.
LFET WING LOWER TE WIGGLE PLATE CRACKED AT FASTENER PANEL 651GB REJECTION: LOWER WING SURFACE DECORATIVE FINISH NOT RESTORED / REJECTED INSP 390 4-12-19 RESTORED LOWER WING SURFACE DECORATIVE FINISH IAW. AMM 51-21-99-300-801; REMOVED AND REPLACED LEFT WING LOWER TE WIGGLE PLATE AT PANEL 651GB P/N 115A2781-3 IAW.SRM 51-40-02 AND AIPC.57-50-00-22A 88920U 12APR19
FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 500 TO BS. 500A, RBL 22. R&R FLOOR SUPPORT IAW SRM.
FWD CARGO COMPARTMENT L/H FLOOR TO SIDEWALL SUPPORT CRACKED AROUND FASTENER STA 500A. R&R SUPPORT PER SRM AND DRAWING.
FWD CARGO BAY BS500D STGR 19 LT. CORNER SUPPORT BRACKET CRACKED. / REMOVED AND REPLACED ON FWD CARGO BAY STGR 19 LT. CORNER SUPPORT BRACKET P/N 143A9481-6. P/O 735540/11; IAW SRM 51-40-02 DWG # 143A7902 59202U 12APR19
FWD CARGO BAY BS500D STGR 19 RT. CORNER SUPPORT BRACKET CRACKED. / REMOVED AND REPLACED IN FWD CARGO BAY BS 500D STR 19 RT. CORNER SUPPORT BRACKET P/N 143A9481-5; P/O 730969/1 IAW SRM 51-40-02; DWG #143A7902 59202U 12APR19
CRACK ON FLOOR TO SIDEWALL SUPPORT STA 727E, WL 156, RBL 20 / REMOVED AND REPLACED SUPPORT PER SRM 51-40-02 59202U 15APR19
AFT CARGO BAY ON R/H FLOOR TO SIDEWALL SUPPORT CORRODED BS. 867 TO BS. 947, RBL 22. R&R SUPPORT IAW SRM AND DWG.
GIRT BAR FITTING ATTACH POINT CORRODED AT BS. 344, LBL 59. R&R FITTING ATTACH POINT PER SRM.
FLOOR PANEL SUPPORT CRACKED AT BS. 540, RBL 26. / R&R FLOOR PANEL SUPPORT IAW SRM AND DWG.
PASSENGER CABIN CRACKED FLOOR PANEL SUPPORT CRACKED AT BS. 540, LBL 1. R&R SUPPORT IAW SRM AND DWG.
R1 DOOR SURROUND LOWER STUB FRAME CRACKED AT BS. 294, RBL 55. R&R STUB FRAME PER SRM AND DWG.
FORWARD OF AFT CARGO BAY DOOR SIDEWALL SHIELD CORRODED BETWEEN BS. 767 TO BS. 787 +7, RBL 23. REPAIRED SHIELD IAW SRM AND DWG.
AFT CARGO BAY FRAME CORRODED AT BS. 947, LBL 10. R&R FRAME PER SRM AND DWG.
ABOVE ENTRY DOOR FRAME CRACKED AT BS. 312, STR. 5L. REPAIRED FRAME IAW ER AND EA.
FRAME TO FLOOR CLIP CORRODED AT BS. 947, LBL 10. R&R FLOOR CLIP IAW SRM.
CRACKED SUPPORT TAB FOR BODY FAIRING PANEL 192E B.S.540+12 RBL5. MARKED / REMOVED AND REPLACED SUPPORT TAB FOR BODY FAIRING PANEL 192E B.S. 540+12 RBL 5 PER SOPM 20-50-01. 57006U 09APR19 AND IPC 53-12-11-25. 57006U 09APR19
CRACK IN BULKHEAD SUPPORT ANGLE BRACKET STA 847+18 LBL 10 WL 165 (MARKED) / REMOVED AND REPLACED IN BULKHEAD SUPPORT ANGLE BRACKET STA 847 +18 LBL10 WL165 WITH P/N 149A81 PER SRM 51-40-02; DWG 6# 149A8102 59202U 26APR19
R2 DOOR MOP SILL CORRODED BETWEEN BS. 947 TO BS. 986+10, RBL 49. / R&R MOPSILL IAW SRM AND DWG.
***CORROSION*** ON TENSION STRAP AT STA 1016+13 RBL 18 WL 208 / REMOVED AND REPLACED TENSION STRAP FROM BS 1016 TO BS 1028.5 WL 208 RBL 18 IAW SRM 51-40-02 AND DWG 147A5730.
L/H HORIZONTAL STABILIZER RIB AT STA 120.30 NEAR BOTTOM IN RADIUS OF CURVE IS CRACKED. REPAIRED IAW SRM
RT HORIZONTAL STABILIZER RIB CRACKED STAB. STA. 129.50 NEAR BOTTOM IN RADIUS OF CURVE. REPAIRED RIB PER SRM.
CRACKS ON R/H HORIZONTAL STABILIZER RIB STAB STA 120.30 NEAR BOTTOM IN RADIUS OF CURVE (MARKED) / REPAIRED IAW SRM 55-10-09-2R-4,
RH ELEVATOR HINGE COVER 344GT IS CRACKED / REMOVED AND REPLACED RH ELEVATOR HINGE COVER 344GT PER SOPM 20-50-01 AND IPC 55-20-00-03.
VAPOR BARRIER PREVIOUS REPAIR DETERIORATED AT BS. 663, LBL 30. / REPAIRED BARRIER IAW SRM.
PREVIOUS REPAIR VAPOR BARRIER DETERIORATED AT BS. 663, RBL 47. R&R BARRIER IAW SRM.
FORWARD FLOOR PANEL 221BF UPPER SKIN PUNCTURED NEAR AFT INBOARD CORNER WITH DAMAGED INSERTS NOTED. REPAIRED FLOOR PANEL IAW SRM AND DWG. (BETWEEN BS. 270 TO BS. 420)
FWD FLOOR PANEL 222DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD FLOOR PANEL 222DF WITH UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A.(1)
AFT FLOOR PANEL 241ADF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / AFT FLOOR PANEL 241 ADF WITH UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-G-0. PARA 9.A.(1)
AFT FLOOR PANEL 241YF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / DAMAGED FLOOR PANEL 241YF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G 0 PAR. 9
FORWARD FLOOR PANEL 221GF FORWARD OUTBOARD TANG CRACKED, (BETWEEN BS. 270 TO BS. 420). REPAIRED FLOOR PANEL IAW SRM AND DWG.
FORWARD FLOOR PANEL 221FF LOWER SKIN INBOARD EDGE PUNCTURED APPROX 6" FROM AFT EDGE. REPAIRED FLOOR PANEL IAW SRM AND DWG.
FWD FLOOR PANEL 222CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / FWD FLOOR PANEL 222CF WITH UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-40-02-0G-0 PARA 9.A.(1)
EXTERIOR EMERGENCY EXIT LIGHTS INOP. R&R LT STA 952 BATTERY PACK PER MM.
SEVERAL INTERIOR EMERGENCY EXIT LIGHTS INOP. R&R RT STA 952 BATTERY PACK PER MM.
EXTERIOR EMERGENCY EXIT LIGHTS INOP. R&R RT STA 952 BATTERY PACK PER MM.
SEVERAL INTERIOR EMERGENCY EXIT LIGHTS INOP. R&R LT STA 952 BATTERY PACK PER MM.
R1 DOOR CRACKED ABOVE AND BELOW DOOR HANDLE TORQUE BOX. R&R DOOR PER AMM.
DURING L/E SLAT LUB FOUND WING PANEL 521ZB 1 HOLE CRACKED OUT / REMOVED & REPLACED PANEL 521ZB REF J727-220-01-01
RIGHT AFT OVERWING FUSELAGE EMERGENCY LIGHT BULB INOPERATIVE. R & R THE BULB IAW AMM.
L1 DOOR UPPER HINGE SKIN CRACKED AT BS 311, BETWEEN STRINGERS 8L. REPAIRED THE STRAP IAW EA.
LT TRAILING EDGE EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT IAW AMM.
LT INTERCOSTAL CRACKED AT BS 540, LBL 0. R&R INTERCOSTAL PER SRM.
RT INTERCOSTAL CRACKED AT BS 540, RBL 0. R&R INTERCOSTAL PER SRM.
L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED SLIDE PER MT.
MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS. 663, RBL 42. REPAIRED THE BULKHEAD WEB IAW SRM.
MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 35. REPAIRED THE BULKHEAD WEB IAW SRM.
RT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED JUST INBOARD OF STAB STA 184.7, 26" FROM FRONT SPAR. REPAIRED SKIN PER EA.
CENTER TANK WILL NOT FEED BOTH CENTER TANK LOW PRESSURE LIGHTS ILLUMINATED WITH PUMP SWITCHES ON 1220 FUEL IN CENTER TANK. REPAIRED PRIMARY CENTER BOOST PUMP IAW AMM.
CENTER TANK WILL NOT FEED BOTH CENTER TANK LOW PRESSURE LIGHTS ILLUMINATED WITH PUMP SWITCHES ON 1220 FUEL IN CENTER TANK. REPAIRED SECONDARY CENTER BOOST PUMP IAW AMM.
L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.
RIGHT WING FIXED TE PANEL LOWER FORE FLAP BULB SEAL BRACKET CRACKED. R & R BRACKET IAW SRM.
AFT FLASHLIGHT CHARGING INDICATION INOPERATIVE. R & R BATTERY IAW MM.
NUMBER 1 FWD EMER FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERY.
NUMBER 2 FWD EMER FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BATTERY.
RIGHT OVERWING EMER EXIT LIGHT INOPERATIVE. R & R LAMP IAW MM.
RIGHT HORIZONTAL STABILIZER 2ND VERTICAL STIFFENER OF RIB CRACKED AT STABILIZER STATION 92.70. REPAIRED STIFFENER IAW SRM.
RIGHT HORIZONTAL STABILIZER 3RD VERTICAL STIFFENER OF RIB CRACKED AT STAB STATION 92.70. REPAIRED STIFFENER IAW SRM.
R1 DOOR THRESHOLD Z ANGLE CORRODED ON THE INBD SIDE OF THE INNER ANGLE. R & R Z ANGLE IAW EA.
FLOOR INTERCOSTAL CRACKED BETWEEN BS 328 - 344, LBL 47. REPAIRED INTERCOSTAL IAW SRM.
FLOOR INTERCOSTAL CRACKED BETWEEN BS 344 - 360, BL 0. REPAIRED INTERCOSTAL IAW SRM.
FLOOR INTERCOSTAL CRACKED BETWEEN BS 270 - 294.5, BL. REPAIRED INTERCOSTAL IAW SRM.
FLOOR INTERCOSTAL CRACKED BETWEEN BS 312 - 328, LBL 47. REPAIRED INTERCOSTAL IAW SRM.
FLOOR INTERCOSTAL CRACKED BETWEEN BS 312 - 328, RBL 31. REPAIRED INTERCOSTAL IAW SRM.
FLOORBEAM FWD AFT SEAT TRACK FLANGE CRACKED AT BS 727B, RBL 23, HOLE C. REPAIRED FLANGE IAW ACO.
FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+19, LBL 44, HOLE D. REPAIRED FLANGE IAW ACO.
FLOORBEAM FWD AFT SEAT TRACK FLANGE CRACKED AT BS 727B, LBL 46.5, HOLE C. REPAIRED FLANGE IAW ACO.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+19, LBL 23.25, HOLE D. REPAIRED FLANGE IAW ACO.
MAIN CABIN FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, LBL 47, HOLE D. REPAIRED FLANGE IAW ACO.
FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+19, LBL 47, HOLE D. REPAIRED FLANGE IAW ACO.
FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, LBL 23.25, HOLE D. REPAIRED FLANGE IAW ACO.
FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, RBL 26.25, HOLE D. REPAIRED FLANGE IAW ACO.
FLOORBEAM FWD SEAT TRACK FLANGE CRACKED AT BS 727A+18, RBL 23.25, HOLE D. REPAIRED FLANGE IAW ACO.
LEFT NR 3 FLIGHT DECK WINDOW FRAME SECOND HOLE FROM THE BOTTOM CRACKED AT 3 O'CLOCK POSITION. REPAIRED FRAME IAW ACO.
FLIGHT DECK LT NR 1 WINDOW FRAME CRACKED IN UPPER LT RADIUS. REPAIRED FRAME IAW SRM.
CABIN EMER EXIT CEILING SIGN COVER LENS MISSING. INSTALLED LENS IAW SIP.
RIGHT MLG CTR GEAR DOOR CRACKED. R & R DOOR IAW AMM.
L2 LOWER EMERGENCY EXIT LIGHT COVER LOOSE. R & R COVER IAW AMM.
AFT GALLEY EMERGENCY EXIT SIGN LENS LOOSE. R & R LIGHT ASSEMBLY IAW MM.
LEFT EMERGENCY EXIT LIGHT POWER SUPPLIES FASTENERS BROKEN. REMOVED AND REPLACED BATTERY PACK PER MM.
RIGHT EMERGENCY EXIT LIGHT POWER SUPPLIES FASTENERS BROKEN. REMOVED AND REPLACED BATTERY PACK PER MM.
LEFT HORIZONTAL STABILIZER RIB AT STA 92.70 2ND VERT STIFFENER CRACKED. REPAIRED RIB PER SRM.
RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM.
AFT CARGO BAY, ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 847 TO 867, RBL 22. REMOVED AND REPLACED PLATE IAW SRM AND DWG.
LEFT WING TRAILING EDGE BULB SEAL SUPPORT BRACKET JUST ABOVE NR 1 PYLON AFT FAIRING CRACKED AT LOWER FASTENER HOLE. REMOVED AND REPLACED BRACKET PER SRM.
RIGHT WING UPPER T/E PANEL AFT SUPPORT ANGLE CRACKED ABOVE NR 2 ENGINE PYLON. REMOVED AND REPLACED ANGLE IAW SRM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STA 138.7. REPAIRED SKIN IAW SRM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STA 101.9. REPAIRED SKIN IAW SRM.
RIGHT WING BULB SEAL RETAINER SUPPORT ANGLE CRACKED ABOVE NR 2 ENGINE PYLON. REMOVED & REPLACED RETAINER IAW SRM.
LEFT WING TRAILING EDGE BULB SEAL RETAINER ATTACH ANGLE JUST ABOVE NR 1 PYLON AFT FAIRING CRACKED. REMOVED AND REPLACED ANGLE IAW SRM.
FLOOR PANEL 140CF CORRODED. REMOVED AND REPLACED PANEL IAW SRM.
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STABILIZER STA 147.9. REPAIRED SKIN IAW SRM.
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STABILIZER STA 101.9. REPAIRED SKIN IAW SRM.
AFT CARGO BAY CARGO FLOOR SUPPORT BEAM CORRODED AT BS 771, RBL 14. REPAIRED BEAM IAW SRM.
AFT CARGO BAY CARGO FLOOR SUPPORT BEAM CORRODED AT BS 771, RBL 9. REPAIRED BEAM IAW SRM.
LEFT HORIZONTAL STAB LOWER SKIN CRACKED AT STA 147.9. REPAIRED SKIN PER SRM.
LT WING INBD T/E FLAP HAD DELAMINATED AREA. R & R FLAP IAW MM.
OVERHEAD OVERWING EMERGENCY EXIT LIGHT HOUSING BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M.
L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED & REPLACED COVER PER M/M.
RIGHT EXTERIOR OVERWING EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW M/M.
DURING SCHEDULED HC1 CHECK, FOUND FLOOR LIGHTING TRACK COVER CRACKED AT ROW 22. REMOVED AND REPLACED COVER.
DURING SCHEDULED HC1 CHECK, FOUND FLOOR LIGHTING TRACK COVER CRACKED. REMOVED AND REPLACED COVER.
DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SLIDE FWD GIRT BAR BRACKET LOOSE. REMOVED AND REPLACED FASTENER.
LT EEPLS LENS INOP AT ROW 1. RELAMPED LENS IAW MM.
LT EEPLS EEPLS INOP AT ROW 18. RELAMPED LENS IAW MM.
AFT SVC DOOR LWR EXIT SIGN LOOSE. RE-SECURED AFT SERVICE DOOR LOWER EXIT LIGHT LENS PER MM.
DURING SCHEDULED OTS CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GAUGE WINDOW MISSING. INSTALLED WINDOW PER MT.
DURING SCHEDULED MV3 CHECK, FOUND AFT EEPLS LENS MISSING. INSTALLED LENS PER MM.
DURING SCHEDULED CV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.
DURING SCHEDULED MV3 CHECK, FOUND EEPLS COVER MISSING AT ROW 1. INSTALLED COVER PER MM.
L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT PER MM.
DURING SCHEDULED HC1 CHECK, FOUND EMERGENCY LIGHTS STRIP CRACKED BETWEEN ROW 1 TO ROW 15. REMOVED AND REPLACED EEPLS PER MM.
ELEVATOR FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED IN FLIGHT WITH APPEARANT SLOW LEAK IN A-HYDRAULIC SYSTEM. FOUND LOOSE FITTING AT ELEVATOR FEEL COMPUTER. SECURED PNEUMATIC FITTING PER MM.
EEPLS COVER LOOSE AT ROW 2 ABC. REMOVED AND REPLACED COVER PER MM.
EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM.