N7874B
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
PASSENGER CABIN SEAT 15D (EMERGENCY EXIT ROW) IS NOT SUPPOSED TO RECLINE. READJUSTED PASSENGER CABIN SEAT RECLINE 15D (EMERGENCY EXIT ROW) PER CMM 25-21-45.
FO SIDE OVER WING EXIT DOOR PULL HANDLE CAME LOOSE. OK TO CONTINUE PER MEL 25-10-01 SP1B AUTH 305955, INSTALLED NEW HARDWARE IN RELEASE HANDLE PAN IAW MM 52-22-51.
FWD LAVATORY SMOKE DETECTOR ACTIVATED IN CLIMB & DESCENT. RESET BOTH TIMES. NO EVIDENE OF SMOKE OR ODOR. OK TO CONT PER MEL 26-16-01, SP1B, AND SP3. R & R THE SMOKE DETECTOR IAW AMM 26-14-01, OPS CHECKED GOOD.
CRACK FRAME, BS 727D BTW S8 - 9R. PERFORMED A REPAIR ON THE FRAME IAW EA 1-A53-12114.
CRACKED CORRUGATED PLATE TRAILING EDGE IRSS 215 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 215 AT LT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 115A2001 SHEET 30 REV A AND DWG 115A2713 SHEET 3 REV A.
CRACK TRAILING EDGE FIXED PANEL SUPPORT BRACKET AT LEVEL ORSS 271 AT LT WING. REPLACED SUPPORT BRACKET LOC. TRAILING EDGE FIXED PANEL AT LEVEL ORSS 271 AT LT WING IAW SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 ITEM 9. MEASURE OF CRACK IS: L: 0.646 INCHES.
CRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE, ORSS 261 LT WING IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, & DWG 115A2001, SHEET 29, REV-.
CRACKED CORRUGATED PLATE, TRAILING EDGE IRSS 215 RT WING. REPLACED CORRUGATED PLATE, TRAILING EDGE, IRSS 215 RT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 115A2001, SHEET 30, REV A, AND DWG 115A2713, SHEET 3, REV A.
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING. PERFORMED VISUAL INSPECTION ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING AND NOT FOUND CRACK PAINT MARKET ONLY; PERFORMED CLEAN IAW SRM 51-10-04.
ELONGATED HOLE ACCESS PANEL 661BB AT RT WING 2025-759490<[01] TOOL USED ON STEP 11 ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 20-JUN-26;[02] TOOL USED: HUMIDITY/TEMPERATURE CHART RECORDER P/N: RH550 ; S/N: 240709411 ; DUE DATE: 29-SEP-26;[03] TOOL USED MULTIMETER P/N: FLUKE 1587 FC ; S/N: 65570063 ; DUE DATE: 22-NOV-26 ; POSITECTOR P/N: NS2 ; S/N: 110098 ; DUE DATE: 09-SEP-26 ; HUMIDITY/TEMPERATURE CHART RECORDER P/N: RH550 ; S/N: 240709411 ; DUE DATE: 29-SEP-26;[04] REPAIRED ACCESS PANEL 661BB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] REPAIRED ACCESS PANEL 661BB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.
ELONGATED HOLES ON ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.
DEBONDED OB AFT FLAP INBOARD EDGE AT RT WING. PERFORMED INTERIM REPAIR AT OB AFT FLAP IB SIDE AT RT WING IAW SRM 57-53-01-2R-16, REPAIR 16, AND THE REPAIR REQUIRED TAP TEST INSPECTION EVERY 6;875 CYCLES OR 30 MONTHS.
CRACKED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB. REPLACED BLADE ON ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW SRM 51-40-02-0G-0, AND DWG 186A3101, SHEET 13, REV C.
CRACKED BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW RBL24.82 TO BL0 AT PASSENGER CABIN. REPLACED BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW RBL24.82 TO BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 STEP 9 AND DWG 143A0060 SHEET 36 REV.A MEASURE OF CRACK IS: 1.680 INCHES.
CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB, RBL 41, BS 663. CRACK LENGTH 0.375 INCH. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LOCATED BTW RBL 30 TO RBL 60 BTW BS 663.75 TO BS 675 AT PASSENGER CABIN IAW SRM 53-40-51-2R-2, REPAIR 2.
CRACK BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW LBL24.82 TO BL0 AT PASSENGER CABIN. REPLACED BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW LBL24.82 TO BL0 AT PASSENGER CABIN IAW SRM 51-40-02-0G-0 AND DWG 143A0060 SHEET 36 REV.A
CRACKED SUPPORT ANGLE, FLOOR STRUCTURE, BS 695, BL 0 IN PAX CABIN. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.
ELONGATED HOLE ON ACCESS PANEL 561CB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-9 .REPAIR 9.
#1 ENG FAIL WITH UNCOMMANDED SHUT DOWN DURING TAXI IN.<[01] PERFORMED FIM 73-05 TASK 805; FOUND EEC 1 CODE FAULT 73-20811; CHIPS DETECTORS FOUND OK; FUEL FILTER FOUND OK; BLEED CHECK VALVE FOUND OK; VSV FOUND OK AND ACTUATOR TEST PASSED; ENGINE AND DEU DISCRETES FOUND GOOD. FUEL PUMP IMPELLER FOUND IN GOOD CONDITION BUT MAKING NOISE WHEN TURNED HAND CRANK. PERFORMED ENGINE RUN; NO ABNORMALITIES ENGINE STABLE.;[02] R&R FUEL PUMP PACKAGE PER MT 773-11-00. OPS CK GOOD
PASSENGER CABIN SEAT 11D RECLINES AND IS NOT SUPPOSED TO RECLINE AS IT IS IN AN EMERGENCY EXIT ROW. <[01] ADJUSTED 11D RECLINE CABLE HDROLCOK TO BE LOCKED OUT PER CMM 25-21-45.
R2 DOOR SLIDE GIRT DRAGGING<[01] REPACKED R2 DOOR SLIDE GIRT PER AMM 25-66-01.
PASSENGER CABIN FORWARD GALLEY MEGAPHONE IS NOT SECURE.<[01] ADJUSTED FWD GALLEY MEGAPHONE CLAMP PER AMM SIP.
L2 DOOR SLIDE GIRT DRAGGING<[01]. REPACKED L2 DOOR SLIDE GIRT PER AMM 25-66-01.
AFT ENTRY SLIDE FELL OUT OF CASE<[01] REINSTALLED AFT ENTRY DOOR ESCAPE SLIDE PER MT 725-61-06.
FWD ENTRY DOOR ESCAPE SLIDE PRESSURE LOW.<[01] C/W MT 725-61-06
R2 SLIDE GAUGE INDICATING IN THE RED<[01] REMOVED AND REPLACED AFT SERVICE EMERGENCY ESCAPE SLIDE PER AMM 25-66-01.
RH OVERWING EXIT DOOR EMERGENCY EXIT SIGNS. INOPERATIVE.<[01] RESECURED LOOSE CONNECTOR OF THE OVERWING EXIT DOOR EMERGENCY SIGN PER REF. AMM 33-51-04-960-801.PERFORMED EMERGENCY LIGHT OPERATIONAL TEST PER REF. AMM 33-51-00-710-801. TEST PASSED;[02] VERIFIED AND INSPECTED STEP#1.
EMERGENCY BATTERY PACK M1674 DEFECTIVE; ALL LIGHT ASSOCIATED WITH THIS BATTERY PACK; OFF.<[01] REPLACED BATTEY PACK M1674 AS PER REFERENCE AMM 33-51-06-960-805.<BR>PERFORMED EMERGENCY LIGHTS- OPERATIONAL TEST AS PER REFERENCE AMM 33-51-00-710-801.TEST NORMAL;[02] VERIFIED AND INSPECTED STEP#1.
LEFT WING LOWER LEADING-EDGE PANEL#521DB HAS DELAMINATION AT ONE CORNER. APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #521DB IAW SRM 51-70-04-2R-13 PARAG 4-D-G.
AFT CARGO COMPARTMENT LEFT SIDE. FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 767 & 727E, WL155.5, LBL 21. THE Z CHANNEL IS GOING TO BE REPLACED IN THE TTG8Q00S1KQK.
AFT CARGO COMPARTMENT LEFT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 807 & 767 WL155.5 LBL21. THE Z CHANNEL IS GOING TO BE REPLACED IN THE TTG8Q00S1KQK.
AFT CARGO COMPARTMENT RIGHT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 787 AND 767, WL155.5, RBL21. R & R THE SHIELD IAW SRM 51-40-02-0G-0 AND DWG 146A0081.
AFT CARGO COMPARTMENT RIGHT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 767 & 727E, WL155.5, RBL 21. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G-0, & DWG 146A7500.
AFT CARGO COMPARTMENT LEFT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 727B & 727, WL155.5, LBL 21. THE CHANNEL IS GOING TO BE REPLACED ON TTG8Q00S1KQK.
AFT CARGO COMPARTMENT RIGHT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 737B & 727, WL155.5, RBL 21. FAULT RESOLVED ON TTG8Q00S1KR6.
AFT CARGO COMPARTMENT LEFT SIDE, FLOOR STRUCTURE Z CHANNEL HAD EVIDENCE OF CORROSION BETWEEN BS 727C & 727B, WL155.5, LBL 21. THE CHANNEL IS GOING TO BE REPLACED IN TTG8Q00S1KQK.
AFT CARGO COMPARTMENT RIGHT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 727C & 727B, WL155.5, RBL 21. FAULT RESOLVED ON TTG8Q00S1KR6.
AFT CARGO COMPARTMENT LEFT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 727D & 727C, WL155.5, LBL 21. THE CHANNEL IS GOING TO BE REPLACED IN THE TTG8Q00S1KQK.
AFT CARGO COMPARTMENT RIGHT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 727D & 727C, WL155.5, RBL 21. FAULT RESOLVED ON TTG8Q00S1KR6.
AFT CARGO COMPARTMENT LEFT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 727E - 727D, WL155.5, LBL21. R & R THE CHANNEL IAW SRM 51-40-02-0G-0, & DWG 146A7500.
AFT CARGO COMPARTMENT RIGHT SIDE, FLOOR STRUCTURE Z CHANNEL HAS EVIDENCE OF CORROSION BETWEEN BS 727E & 727D, WL155.5, RBL21. FAULT RESOLVED ON TTG8Q00S1KR6.
FWD CARGO AFT BULKHEAD SUPPORT STRUCTURE, BS 500D, STR 19R HAS AFT ATTACHED ANGLE MISSING. INSTALLED A NEW AFT ATTACHED ANGLE AT FWD CARGO AFT BULKHEAD SUPPORT IAW SRM 51-40-02-0G-0, & DWG 143A7902. INSPECTED IAW SRM 51-40-02-0G-0-A00729.
CABIN FLOOR PANEL #241DF DELAMINATED.<[01] RECEIVED NEW PANEL 241DF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00RFYUK;[02] VERIFIED STEP 1.
CABIN FLOOR PANEL #241AF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL 241AF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00RFYUT;[02] VERIFIED STEP 1.
CABIN FLOOR PANEL #231XF DELAMINATED<[01] RECEIVED NEW PANEL 231XF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00RFZ04;[02] VERIFIED STEP 1
CABIN FLOOR PANEL #231ZF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL 231ZF ; THIS PANEL WILL BE INSTALL ON FAULT TTG8Q00RFYXX
R/W MOVEABLE SLAT NO-7 L/E NOSE SKIN ACTUATOR ATTACHED RIB APPEAR CRACKED @ FASTENER HEADS MKD DOT<[01] ACCOMPLISHED PERMANENT REPAIR OF DAMAGE FOUND AT RT WING SLAT #7 NOSE SKIN AT ACTUATOR ATTACHING AREA PER REF B737 SRM 57-42-01-2R-8;[02] VERIFIED STEP 1; REPAIR ACCOMPLISHED
FORWARD GALLEY R1 DOOR GIRT BAR COVER TORN. REMOVED AND INSTALLED THE R1 SLIDE WILL BE ACCOMPLISHED ON T/C REF SA-M/MT 725-61-06.
AFT CARGO COMPARTMENT FLOOR PANEL 140CF HAD A SMALL CRACK. CUT & REMOVED THE DAMAGED AREA IAW SRM 53-00-53-2R-1 & SRM 51-10-02-0G-0. COMPLETED FABRICATION OF NEW REPAIR PARTS IAW SRM 53-00-53-2R-1. INSTALLED NEW REPAIR IAW SRM 53-00-53-2R-1 & SRM 51-40-02-0G-0.
FWD ENTRY DOOR GIRT BAR RETAINER CLIP MISSING RETAINER PIN<[01] REPLACED FWD ENTRY DOOR GIRT BAR REF AMM 25-66-01
#1 SPOILER UPPER SURFACE HAS A REPAIR THAT HAS BECOME DISBONDED.<[01] REMOVED AND REPLACED #1 GROUND SPOILER IAW AMM 29-62-91. OPS CHECKED GOOD.
EXIT SIGN AFT GALLEY CRACKED<[01] REMOVED AND REPLACED AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN HOUSING ASSEMBLY PER AMM 33-51-01; OPS CHK GOOD
B SYS HYD FAILURE FOUND PRESSURE DECK FLOW LIMITER ASSEMBLY LEAKING FROM UNION PACKING. CREW REPORTS IMMEDIATELY TURNED BOTH EDP & EMDP TO OFF POSITION. DUE TO HYDRAULIC QUANTITY DEPLETING.<[01] FOUND CRACKED FITTING; REMOVED AND REPLACED T/E FLAP FLOW LIMITER; AMM IAW 27-51-67. RAN ENGINES AND ALL FLIGHT CONTROLS; PER AMM 71-00-00; SERVICED HYDRAULIC QUANITY PER AMM 12-12-00; ALL SYSTEMS RESTORED.
WITH FLAPS INDICATING 15; SELECTED FLAPS 30. DURRING TRANSIT TO 30; L&E FLAPS POSITION INDICATORSDEVELOPED A SPLIT. APPROCHING FLAPS 25 FLAP INDICATORS COME BACK TO AN UNSKEWED POSITION AND ACHIEVED WITH FLAPS INDICATING 15 SELECTED FLAPS 30. DURRING TRANSIT TO 30 L&E FLAPS POSITION INDICATORSDEVELOPED A SPLIT. APPROCHING FLAPS 25 FLAP INDICATORS COME BACK TO AN UNSKEWED POSITION AND ACHIEVED A NORMAL 30 INDICATION.<[01] R AND R LH FLAP TRANSMITTER PER MM 27-58-01.
2 EA EMERGENCY EXIT LIGHTS AFT OF RT OVERWING EXIT INOP ALSO EXTERNAL GROUND EVACUATION LIGHT INOP<[01] R&R?D BATTERY PACK 33-51-06
ON TAKE OFF DURING ROTATION AIRCRAFT BEGAN TO EXPERIENCE MODERATE VIBRATION. REF TTG8Q00KL7SJ FOR #1 AND #2 MLG TIRE CHANGE.
ROW 15 DEF AND ROW 20 ABC SIDEWALL LIGHT LENS DETACHED<[01] SECURED WITH TAPE. OK TO CONTINUE PER MEL 25-10-01 SP1 B<BR>AUTH 125699;[02] SECURED SIDEWALL LIGHT LENS AT 15DEF AND 20ABC. REFERENCE M/M 33-51-04
BOTH MEGAPHONES REQUIRE NEW BATTERIES.<[01] R&R'D BATTERIES AND INSPECTION TAG PER AMM 25-64-00
FWD ENTRY DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW. REMOVED AND REPLACED THE COVER IAW AMM 33-51-01.
FWD SERVICE DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW. REMOVED AND REPLACED THE COVER IAW AMM 33-51-01.
AFT SERVICE EXTERIOR EMERGENCY LIGHT INOP. / [01] RELAMPED AFT SRV DOOR SLIDE LIGHT PER AMM 33-51-04; OPS CHECK GOOD.
LEFT WING O/B AFT FLAP DELAMINATED ON I/B LOWER SURFACE. / [01] PERFORMED SRM 57-53-01-1A-4. NUMBER 4; (8)(A) 1) A-H)
EXTERNAL FUSELAGE AFT ENTRY AND AFT SERVICE EMERGENCY LIGHTS INOP 2022-131886 / [01] REPLACED SLIDE LAMP EXTERIOR EMERGENCY LIGHTS AFT ENTRY AND GALLEY AT AFT AREA GALLEY IAW B737-700 AMM 33-51?04-960-801; TEST IS OK. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SLIDE LAMP EXTERIOR EMERGENCY LIGHTS AFT ENTRY AND GALLEY AT AFT AREA GALLEY IAW B737-700 AMM 33-51?04-960-801; TEST IS OK. SEE INDIVIDUAL SIGN OFF BELOW.
ELONGATED HOLE BRACKET ON ACCESS PANEL 651GB AT RT WING 2022-131837 / [01] REPLACED BRACKET ON ACCESS PANEL 651GB AT RT WING IAW B737-700 SRM 51-10-02 AND SRM 51-40-02;[02] REPLACED BRACKET ON ACCESS PANEL 651GB AT RT WING IAW B737-700 SRM 51-10-02 AND SRM 51-40-02
CRACK FLOOR PANEL 241ADF AT AFT GALLEY AREA. 2022-131832 / [01] REPAIRED FLOOR PANEL 241ADF AT AFT GALLEY AREA IAW B737-700 AMM 25-00-00-300-801S; STEP 2F;[02] COMPLETE TASK CERTIFIED;[03] CORRECTED STEP 1: REPAIRED FLOOR PANEL 241ADF AT AFT GALLEY AREA IAW B737-700 AMM 25-00-00-300-801; STEP 2F MEASURE OF CRACK IS 0.0635' TOOL USED CALIPER P/N: 500-197-30; S/N: A21041998; DUA DATE 11-AUG-22;[04] COMPLETE CERTIFIED TASK
CRACK FLOOR PANEL 242RF AT AFT GALLEY AREA 2022-131833 / [01] REPAIRED FLOOR PANEL 242RF AT AFT GALLEY AREA IAW B737-700 AMM 25-00-00-300-801S; STEP 2F;[02] COMPLETE TASK CERTIFIED;[03] CORRECTED STEP 1: REPAIRED FLOOR PANEL 242RF AT AFT GALLEY AREA IAW B737-700 AMM 25-00-00-300-801S; STEP 2F MEASURE OF CRACK IS 0.096' TOOL USED CALIPER P/N: 500-197-30; S/N: A21041998; DUA DATE 11-AUG-22;[04] COMPLETE CERTIFIED
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING 2022-131823 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING IAW B737-700 DWG # 115A2001 REV.- SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OFFS BELOW;[02] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING IAW B737-700 DWG # 115A2001 REV.- SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OFFS BELOW
CRACK TRACK RBBL 13.84 LOCATED BS 727E AFT CARGO COMPARTMENT 2022-131819 / [01] TOOL USED : EDDY CURRENT TOOL; P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 02 JUN 22.;[02] TOOL USED CALIPER P/N 500-197-30 S/N A18135101 DUE DATE 06-AUG-22;[03] REPAIRED TRACK RBBL 13.84 LOCATED BS 727E AFT CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-3. SEE INDIVIDUAL SIGN-OFF BELOW;[04] TASK CARD COMPLETED <BR>RII<BR>SEE INDIVIDUAL SIGN OFFS BELOW
CORROSION STRINGER 26L BS 907 LBL 31 AND WL 165 AT AFT CARGO COMPARTMENT 2022-131820 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG; S/N: 130064101; DUE DATE: 11-MAY-22;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[03] REPAIRED STRINGER 26L BS 907 LBL 31 AND WL 165 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; AND DWG 147A0060; SHEET 26 AND REV -.SEE INDIVIDUAL SIGN-OFFS BELOW;[04] REPAIRED STRINGER 26L BS 907 LBL 31 AND WL 165 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; AND DWG 147A0060; SHEET 26 AND REV -.RII .SEE INDIVIDUAL SIGN-OFFS BELOW;[05] CORRECTED STEP 3.<BR>REPAIRED STRINGER 26L BS 907 LBL 31 AND WL 165 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; AND DWG 147A0060; SHEET 26 AND REV -. AND REMOVED EWIS PROTECTION ON WIRE BUNDLES LOC BTW BS 907 TO BS 927 AND BTW STR 23L TO STR 27R IAW B-737-700 AMM 20-60-07-913-801. SEE INDIVIDUAL SIGN-OFFS BELOW;[06] REPAIRED STRINGER 26L BS 907 LBL 31 AND WL 165 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; AND DWG 147A0060; SHEET 26 AND REV -. AND REMOVED EWIS PROTECTION ON WIRE BUNDLES LOC BTW BS 907 TO BS 927 AND BTW STR 23L TO STR 27R IAW B-737-700 AMM 20-60-07-913-801.RII. SEE INDIVIDUAL SIGN-OFFS BELOW
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 AND BL0 FWD GALLEY AND LAV 2022-131745 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 AND BL0 FWD GALLEY I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG # 141A5400 REV -.;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 AND BL0 FWD GALLEY I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG # 141A5400 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 AND BL0 FWD GALLEY I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG # 141A5400 REV -. RII .SEE INDIVIDUAL SIGN OFF BELOW.
ELONGATED HOLE UPPER FITTING LOCATED BS1016 AND BL0 AT PASSENGER CABIN 2022-131780 / [01] REPLACED UPPER FITTING LOCATED BS1016 AND BL0 AT PASSENGER CABIN IAW. B737-700 SRM 51-40-02; DWG # 148A2230 REV. C. SRM 51-10-02 ITEM 9.;[02] STED 1 CORRECTED. <BR>REPLACED UPPER FITTING LOCATED BS1016 AND BL0 AT PASSENGER CABIN IAW. B737-700 SRM 51-40-02; DWG # 148A2230 REV. C. SRM 51-10-02 ITEM 9.<BR>SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] JOB COMPLETE
BROKEN EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AND LAV 2022-131758 / [01] REMOVED AND REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AND LAV IAW B737-700 AMM 33-51-01-960-802 TEST IS OK;[02] REMOVED AND REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AND LAV IAW B737-700 AMM 33-51-01-960-802 TEST IS OK<BR>TASK COMPLETED
CORROSION FLOOR STRUCTURE BEAM LOCATED BS986.5 LBL43 AND WL208.1 AT AFT GALLEY AREA 2022-131775 / [01] TOOL USED P/N: 45MG; S/N: 130063701; DUE DATE: 11-MAY-22;[02] TOOL USED. EDDY CURRENT EQUIPMENT. P/N: NORTEC 500D. S/N: N500X12101V022233. DUE DATE: 02-JUN-22.;[03] TOOL USED CALIPER P/N 500-197-30; S/N: A18135088; DUE DATE: 01-AUG-22;[04] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 LBL43 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 3 FIGURE 204 SEE INDIVIDUAL SIGN-OFFS BELOW.;[05] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 LBL43 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 3 FIGURE 204 SEE INDIVIDUAL SIGN-OFFS BELOW... RII ITEM
CORROSION FLOOR STRUCTURE BEAM LOCATED BS986.5 RBL43 AND WL208.1 AT AFT GALLEY AREA 2022-131772 / [01] TOOL USED ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 11-MAY-22;[02] TOOL USED. EDDY CURRENT EQUIPMENT. P/N: NORTEC 500D. S/N: N500X12101V022233. DUE DATE: 02-JUN-22.;[03] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 RBL43 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 3 FIGURE 204 SEE INDIVIDUAL SIGN-OFFS BELOW.;[04] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 RBL43 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 3 FIGURE 204 SEE INDIVIDUAL SIGN-OFFS BELOW... RII ITEM
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS328 TO BS344 AND LBL47 FWD GALLEY AND LAV 2022-131755 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS328 TO BS344 AND LBL47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; 51-10-02 ÿ½TEM 9 AND DWG 141A5400; REV:- SHEET: 44.;[02] CORRECTED STEP 1.<BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS328 TO BS344 AND LBL47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; 51-10-02 ÿ½TEM 9 AND DWG 141A5400; REV:- SHEET: 44. SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] JOB COMPLETE <BR>RII.
CRACK FLOOR STRUCTURE BEAM LOCATED BS294.5 AND RBL55 AT FWD GALLEY AREA 2022-131749 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 60007161486 DUE DATE 06-DEC-22.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[03] REPAIRED STRUCTURE FLOOR BEAM LOCATED BS 294.5 AND RBL 55 AT FWD GALLEY AREA. IAW B737-700 SRM 53-10-51-2R-16 ALTERNATIVE 2 PARAGRAPH.4D TABLE 201 REPAIR 16 FIGURE 202. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[04] TASK CARD COMPLETED <BR>RII<BR>SEE INDIVIDUAL SIGN OFFS BELOW
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 AND LBL47 FWD GALLEY AND LAV 2022-131752 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 AND LBL47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; 51-10-02 ÿ½TEM 9 AND DWG 141A5400; REV:-; SHEET 26;[02] JOB COMPLETE <BR>RII.;[03] CORRECTED STEP 1.<BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 AND LBL47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; 51-10-02 ÿ½TEM 9 AND DWG 141A5400; REV:-; SHEET 26. SEE INDIVIDUAL SIGN-OFFS BELOW;[04] CERTIFIED STEP 3 OF CORRECTIVE ACTION JOB COMPLETE <BR>RII.
CRACK SUPPORT ANGLE LOCATED BS 291.5 TO BS 294.5 AND STRINGER 17R AT PASSENGER CABIN 2022-131716 / [01] REPLACED SUPPORT ANGLE LOCATED BS 291.5 TO BS 294.5 AND STRINGER 17R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A8310 REV B<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED SUPPORT ANGLE LOCATED BS 291.5 TO BS 294.5 AND STRINGER 17R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A8310 REV B <BR>SEE INDIVIDUAL SIGNOFF BELOW RII
DONT WORK CORRECTLY EMERGENCY LIGHT BATTERY PACK AFT LT AT PASSENGER CABIN (1 EA) 2022-131722 / [01] REPLACED EMERGENCY LIGHT BATTERY PACK AFT LT AT PASSENGER CABIN (1 EA) IAW AMM 33-51-06-960-805. TEST IS OK.<BR>SEE INDIVIDUAL SIGNOFF STEP BELOW;[02] REPLACED EMERGENCY LIGHT BATTERY PACK AFT LT AT PASSENGER CABIN (1 EA) IAW AMM 33-51-06-960-805. TEST IS OK. <BR>SEE INDIVIDUAL SIGNOFF STEP BELOW
CRACK SUPPORT BRACKET LOCATED AT WS 253.00 TRAILING EGE AT LT WING 2022-131705 / [01] REPLACED SUPPORT BRACKET LOCATED AT WS 253.00 TRAILING EGE AT LT WING IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 P/N USED 115A2982-9 PO 2021-235986 1;[02] CORRECTED STEP 1: REPLACED SUPPORT BRACKET LOCATED AT WS 253.00 TRAILING EGE AT LT WING IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 P/N USED 115A2982-9 PO 2021-235986 1. SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED SUPPORT BRACKET LOCATED AT WS 253.00 TRAILING EGE AT LT WING IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 P/N USED 115A2982-9 PO 2021-235986 1. SEE INDIVIDUAL SIGN OFF BELOW
DONT WORK CORRECTLY EMERGENCY LIGHT BATTERY PACK MID LT SIDE AT PASSENGER CABIN (1 EA) 2022-131720 / [01] REPLACED EMERGENCY LIGHT BATTERY PACK MID LT SIDE AT PASSENGER CABIN (1 EA) IAW AMM 33-51-06-960-805 TEST IS OK<BR>SEE INDIVIDUAL SIGNOFF STEP BELOW;[02] REPLACED EMERGENCY LIGHT BATTERY PACK MID LT SIDE AT PASSENGER CABIN (1 EA) IAW AMM 33-51-06-960-805 TEST IS OK<BR>SEE INDIVIDUAL SIGNOFF STEP BELOW
CRACK FRAME LOCATED BS 312 AND BETWEEN STRINGER 5L TO STR 6L AT PASSENGER CABIN 2022-131707 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022236 ; DUE DATE: 02-JUN-22;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23;[03] PERFORMED REPAIR FRAME LOCATED BS 312 AND BETWEEN STRINGER 5L TO STR 6L AT PASSENGER CABIN IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1.<BR>?SEE INDIVIDUAL SING-OFF BELLOW?;[04] CORRECTED STEP 3<BR>PERFORMED REPAIR FRAME LOCATED BS 312 AND BETWEEN STRINGER 5L TO STR 6L AT PASSENGER CABIN IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1.<BR>?SEE INDIVIDUAL SING-OFF BELOW?;[05] CORRECTED STEP 3 AND 4<BR>PERFORMED REPAIR FRAME LOCATED BS 312 AND BETWEEN STRINGER 5L TO STR 6L AT PASSENGER CABIN IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1.<BR>?SEE INDIVIDUAL SIGN-OFFS BELOW?;[06] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101V022237 DUE DATE 06-OCT-22;[07] PERFORMED REPAIR FRAME LOCATED BS 312 AND BETWEEN STRINGER 5L TO STR 6L AT PASSENGER CABIN IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1. RII <BR>?SEE INDIVIDUAL SIGN-OFFS BELOW?
CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.000 INCH 2022-131724 / [01] TOOL USED. EDDY CURRENT EQUIPMENT. P/N: NORTEC 500D. S/N: N500X12101V022233. DUE DATE: 02-JUN-22.;[02] PERFORMED REPAIRED ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. IAW. B737-700 SRM 51-40-02 AND SRM 55-10-01-2R-11 REPAIR 11. FIG 204 ITEM B SHEET 2. SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW
CRACK TIE CLIP LOCATED BS 277 AND STRINGER 10R AT PASSENGER CABIN (1 EA) 2022-131714 / [01] REPLACED TIE CLIP LOCATED BS 277 AND STRINGER 10R AT PASSENGER CABIN (1 EA) IAW B737-700 SRM 51-40-02 DWG 141A1110; SHEET 18; REV -<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED TIE CLIP LOCATED BS 277 AND STRINGER 10R AT PASSENGER CABIN (1 EA) IAW B737-700 SRM 51-40-02 DWG 141A1110; SHEET 18; REV - <BR>SEE INDIVIDUAL SIGNOFF BELOW RII
DELAMINATED ACCESS PANEL 521DB AT LT WING 2022-131697 / [01] TOOL USED: CALIPER P/N 500-464 S/N 15331926 DUE DATE 28-SEP-22.;[02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18196119 DUE DATE 24 FEB 23;[03] TOOL USED SCALE P/N:CL5000 S/N:AE-408758 DUE DATE 09-FEB-23;[04] TOOL USED: HOT BONDER: P/N: HCS9200B; S/N: 1622983; DUE DATE: 16-JAN-23.;[05] TOOL USED SCALE P/N 1863T62 S/N AE-40571 DUE DATE 19 MAY 22;[06] REPAIRED ACCESS PANEL 521DB AT LT WING AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGN OFFS BELOW.;[07] TASK COMPLETED
CRACK ACCESS PANEL COVER CUT OUT ENTRY DOOR LOCATED BS 303.9 AND BTW STRINGER 7L TO STR 9L AT PASSENGER CABIN 2022-131708 / [01] REPLACED ACCESS PANEL COVER CUT OUT ENTRY DOOR LOCATED BS 303.9 AND BTW STRINGER 7L TO STR 9L AT PASSENGER CABIN IAW B737-700 SRM 51-10-02. TOOL USED CALIPER P/N: 500-197-30 S/N: A18135101 DUE DATE 06-AUG-22;[02] TASK COMPLETED
DONT WORK CORRECTLY EMERGENCY LIGHT BATTERY PACK FWD LT AT PASSENGER CABIN (1 EA) 2022-131719 / [01] REPLACED EMERGENCY LIGHT BATTERY PACK FWD LT AT PASSENGERS CABIN AND PERFORMED FUNCTIONAL TEST OF THE EMERGENCY LIGHT BATTERY IAW B737-700 AMM 33-51-06-960-805. TEST IS OK. SEE INDIVIDUAL SIGN-OFFS BELOW;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN-OFFS BELOW
DONT WORK CORRECTLY EMERGENCY LIGHT BATTERY PACK MID RT SIDE AT PASSENGER CABIN (1 EA) 2022-131721 / [01] REPLACED EMERGENCY LIGHT BATTERY PACK MID RT SIDE AT PASSENGER CABIN (1 EA) IAW AMM 33-51-06-960-805. TEST IS OK.<BR>SEE INDIVIDUAL SIGNOFF STEP BELOW;[02] REPLACED EMERGENCY LIGHT BATTERY PACK MID RT SIDE AT PASSENGER CABIN (1 EA) IAW AMM 33-51-06-960-805. TEST IS OK. <BR>SEE INDIVIDUAL SIGNOFF STEP BELOW
CRACK TRAILING EDGE SUPPORT BRACKET LOCATED AT LEVEL IRSS140 AT LT WING 2022-131679 / [01] REPLACED TRAILING EDGE SUPPORT BRACKET LOCATED AT LEVEL IRSS140 AT LT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9; 51-40-02;[02] REPLACED TRAILING EDGE SUPPORT BRACKET LOCATED AT LEVEL IRSS140 AT LT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9; 51-40-02
CRACK SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN 2022-131622 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[02] REPLACED SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ÿ½TEM 9 DWG# 111A6000 REV : ?;[03] REPLACED SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ÿ½TEM 9 DWG# 111A6000 REV : ? SEE INDIVIDUAL SING-OFF BELOW.;[04] REPLACED SUPPORT ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ÿ½TEM 9 DWG# 111A6000 REV : ? SEE INDIVIDUAL SING-OFF BELOW. RII
BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE (3EA) AND LH SIDE (2EA) AT PASSENGER CABIN (5 EA) 2022-131632 / [01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE (3EA) AND LH SIDE (2EA) AT PASSENGER CABIN (5 EA) I.A.W SOPM 20-50-19 AND DWG 33500007.;[02] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE (3EA) AND LH SIDE (2EA) AT PASSENGER CABIN (5 EA) I.A.W SOPM 20-50-19 AND DWG 33500007.
CRACK BELLY FAIRING HOLES ON FWD FACE OF ACCESS PANEL 194E AT LOWER FUSELAGE 2022-131657 / [01] TOOL USED: HOT BONDER P/N HCS9200B S/N 16122983 DUE DATE 16-JAN-23;[02] TOOL USED: HOT BONDER P/N: HCS9200B; SN: 16122983; D/D: 16/JAN/23.;[03] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 16122983 DUE DATE: 16/JAN/23.;[04] REPAIRED ACCESS PANEL 194E AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 REPAIR 8 SEE INDIVIDUAL SIGNOFFS BELOW.;[05] ENTRY BY ERROR CORRECTIVE ACTIONS 4.<BR>THE CORRECT CORRECTIVE ACTIONS IS: <BR>REPAIRED ACCESS PANEL 194E AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 REPAIR 8 SEE INDIVIDUAL SIGNOFFS BELOW. TOOL USED CALIPER PN:500-464 ; SN:15331926 DUE DATE 28/SEP/22.;[06] JOB TASK COMPLETED.
CRACK ON ANGLE LOCATED BS 663.75 AND BTW LBL 6.01 TO LBL 15.04 UPPER POSITION AT AIR CONDITIONING BAY 2022-131653 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23;[02] TOOL USED COMBINATION GAGE P/N CBG-12-0-N-1 S/N AE-39357 DUE DATE 07-DEC-22; CALIPER P/N 500-196-30 S/N A21029144 DUE DATE 07-OCT-22;[03] REPLACED ANGLE LOCATED BS 663.75 AND BTW LBL 6.01 TO LBL 15.04 UPPER POSITION AT AIR CONDITIONING BAY AREA AT LOWER FUSELAG IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02. AND DWG: 111A1000; REV -. SEE INDIVIDUAL SIGN-OFF ENTRIES BELOW.;[04] TASK CARD COMPLETED <BR>RII<BR>SEE INDIVIDUAL SIGN OFFS BELOW
CRACK BELLY FAIRING HOLES ON AFT POSITION OF ACCESS PANEL 193D AT LOWER FUSELAGE 2022-131658 / [01] TOOL USED: HOT BONDER P/N HCS9200B S/N 16122983 DUE DATE 16-JAN-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; SN: 16122983; D/D: 16/JAN/23.;[03] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 16122983 DUE DATE: 16/JAN/23.;[04] REPAIRED ACCESS PANEL 193D AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 SEE INDIVIDUAL SIGNOFFS BELOW;[05] ENTRY BY ERROR CORRECTIVE ACTIONS 4.<BR>THE CORRECT CORRECTIVE ACTIONS IS: <BR>REPAIRED ACCESS PANEL 193D AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 SEE INDIVIDUAL SIGNOFFS BELOW. TOOL USED CALIPER PN:500-464 ; SN:15331926 DUE DATE 28/SEP/22.;[06] ENTRY BY ERROR CORRECTIVE ACTIONS 5.<BR>THE CORRECT CORRECTIVE ACTIONS IS: <BR>REPAIRED ACCESS PANEL 193D AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 SEE INDIVIDUAL SIGNOFFS BELOW. TOOL USED CALIPER PN:500-464 ; SN:15331926 DUE DATE 28/SEP/22 MULTIMETER P/N: FLUKE 87 ; S/N: 43050123 ; DUE DATE: 03-FEB-23.;[07] JOB TASK COMPLETED.
CRACK ACCESS PANEL 621FB AT RT WING 2022-131656 / [01] TOOL USED P/N 500-464 S/N 15331926 DUE DATE 28-SEP-22.;[02] TOOL USED SCALE P/N:CL5000 S/N:AE-408758 DUE DATE 09-FEB-23;[03] TOOL USED: HOT BONDER: P/N: HCS9200B; S/N: 1622983; DUE DATE: 16-JAN-23.;[04] TOOL USED SCALE P/N 1863T62 S/N AE-40571 DUE DATE 19 MAY 22;[05] TOOL USED: HOT BONDER:P/N; HCS9000B S/N:18175469 DUE DATE: 5-AUG-22.<BR>POSITECTOR 200 C ADV P/N: DF-631235 S/N: AE-406428 DUE DATE:6-JUL-22;[06] TOOL USED SCALE P/N: CL5000 S/N: AE-409561 DUE DATE: 24-MAR-22.;[07] CORRECTIVE ACTION 6. ENTRY BY ERROR <BR>CORRECT CORRECTIVE ACTION IS: <BR>TOOL USED SCALE P/N: CL5000 S/N: AE-409561 DUE DATE: 24-MAY-22.;[08] TOOL USED HOTBONDER P/N: HCS9000B; S/N: 18175469 DUE DATE: 05-AUG-22.;[09] CORRECTIVE ACTION 3. ENTRY BY ERROR <BR>CORRECT CORRECTIVE ACTION IS: <BR>TOOL USED: HOT BONDER: P/N: HCS9200B; S/N: 16122983; DUE DATE: 16-JAN-23;[10] REPAIRED ACCESS PANEL 621FB AT RT WING AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[11] REPAIRED ACCESS PANEL 621FB AT RT WING AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[12] TASK COMPLETED
CRACK ON ANGLE LOCATED BS 663.75 AND BTW RBL 6.01 TO RBL 15.04 UPPER POSITION AT AIR CONDITIONING BAY 2022-131652 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23;[02] TOOL USED COMBINATION GAGE P/N CBG-12-0-N-1 S/N AE-39357 DUE DATE 07-DEC-22; CALIPER P/N 500-196-30 S/N A21029144 DUE DATE 07-OCT-22;[03] REPLACED ANGLE LOCATED BS 663.75 AND BTW RBL 6.01 TO RBL 15.04 UPPER POSITION AT AIR CONDITIONING BAY AREA AT LOWER FUSELAG IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02. AND DWG: 111A1000; REV -. SEE INDIVIDUAL SIGN-OFF ENTRIES BELOW.;[04] TASK CARD COMPLETED <BR>RII<BR>SEE INDIVIDUAL SIGN OFFS BELOW
CRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT 2022-131416 / [01] REPLACED FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG 453A2610 REV: E.;[02] CORRECTED STEP 1.<BR>REPLACED FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG 453A2610 REV: E. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[03] REPLACED FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG 453A2610 REV: E. ?SEE INDIVIDUAL SIGNOFFS BELOW?.
BROKEN EMERGENCY DOOR LOWER STRAP COVER ASSY LH SIDE AT PASSENGER CABIN (1 EA) 2022-131468 / [01] REPLACED EMERGENCY DOOR LOWER STRAP COVER ASSY LH SIDE AT PASSENGER CABIN (1 EA) IAW B737-700-AMM 52-22-51-400-801 STEP 3.D.(2 ) (D);[02] REPLACED EMERGENCY DOOR LOWER STRAP COVER ASSY LH SIDE AT PASSENGER CABIN (1 EA) IAW B737-700-AMM 52-22-51-400-801 STEP 3.D.(2 ) (D)
EMERGENCY LIGHT BATTERIES FAILED @ STATION M1675 ; EMERGENCY LIGHT ATTERIES FAILED @ STATION M1675 / [01] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06
R-1 DOOR SLIDE GIRT TO LONG NEEDS REINSTALLED IN PACK. ; / [01] REMOVED/REPACKED/REINSTALLED R1 DOOR SLIDE IAW AMM 25-66-01-401 AND TASK CARD TTG8Q00AC2RD
L-2 DOOR SLIDE GIRT TO LONG; NEEDS REINSTALLED IN PACK. ; / [01] REMOVED/REPACKED/REINSTALLED L2 SLIDE IAW AMM 25-66-01 AND TASK CARD TTG8Q00AC2RE; [02] C/W
SUPPLEMENTAL INFORMATION: L2 DOOR EMERGENCY EVACUATION SLIDE PSI LOW ; / [01] REMOVED AND REPLACED L2 DOOR SLIDE IAW MT 725-61-06
AFT FO SIDE (RIGHT) GIRT BAR HANGING LOW NEEDS ADJUSTING ; / [01] REPOSITIONED AFT SERVICE SLIDE IAW 725-61-06 ASSIST 60704
RIGHT EMERGENCY EXIT DOOR LIGHT IS INOP ; / [01] RELAMPED RIGHT EMERGENCY EXIT DOOR LIGHT IN REFERENCE TO AIRCRAFT MAINTENANCE MANUAL 33 - 21 - 00 - 960 - 801 - NG
RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-51-04 OPS CHECK GOOD.
PEELED PAINT ON ELEVATOR AND ELEVATOR TAB AT LT HORIZONTAL STABILIZER PAINTED ELEVATOR AND ELEVATOR TAB AT LT HORIZONTAL STABILIZER IAW B737 AMM 51-21-99-300-801 AND AMM 27-31-11-400-801, TOOL USED TRAMMEL BAR PIN F80055-1 SIN 105320 DUE DATE 15/APR/20 PIN C27628-11.S/N MS757-1 DUE LOTE 15/APR/20 AND FCF IS DOCUMENTED ON LOG PAGE 392745
PEELED PAINT ON ELEVATOR AND ELEVATOR TAB AT RT HORIZONTAL STABILIZER PAINTED ELEVATOR AND ELEVATOR TAB AT TH HORIZONTAL STABILIZER IAW B737 AMM 51-21-99-300-801 AND AMM 24-31-11-400-801 TOOL USED TRAMMEL BAR PIN F80055-1 SIN 105310 DUE DATE 15/APR/20 PIN C27628-1 SIN M5757-1 DUE DATE 15/APR/20 AND FCF IS DOCUMENTED ON LOG PAGE 1392475
CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT (1 EA) / REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW EA # 1-A53-2076 REV 11
AFT CARGO COMPARTMENT ANGLE CORRODED BETWEEN BS. 767 TO BS. 787, AT LEVEL STR. 25R, LOWER AREA COMMON TO SUPPORT CHANNEL. / R&R ANGLE IAW SRM AND DWG.
CRACK ON SUPPORT BRACKET APU BLEED DUCT LOCATED BS540+4 INCH LT SIDE / REPLACED SUPPORT BRACKET APU BLEED DUCT LOC. BS 540+4 INCH LT SIDE IAW B737-700 SRM 51-10-02; ITEM 9 AND 51-40-02 AND DRAWING 212A1101 REV-
ELONGATED HOLE FRAME BS857 AT LEVEL STR 21R AT AFT CARGO COMPARTMENT REPAIRED FRAME BSTA 855.95 AT S-21R LEVEL AT AFT CARGO COMPARTMENT IAW EA # 53-0175-20 REV#0 AND EA N. 1-753-36667 REV IR FOR FURTHER INSPECTION SEE TLD FACT AS A RESULT OF POST REPAIR INSPECTION
INOP EMERGENCY LIGHT BATTERY PACKS M1672 AND M1673 AT PASSENGER CABIN REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS M1672 AND M1673 AT PASSENGER CABIN IAW AMM 33-51-06-960-805. PERFORMED TEST OF THE NEW BATTERY PACK IAW AMM 33-51-06-960-805 TEST IS OK
CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT / REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW EA# 1-A53-2076 REV 11
INOP EMERGENCY LIGHT BATTERY PACKS M1670 AT PASSENGER CABIN REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS M1668 AND M1670 AT PASSENGER CABIN IAW AMM 33-51-06 -960-805 AND PERFORMED TEST OF THE NEW BATTERY PACK IAW AMM 33-51-06-960-805 TEST IS GOOD
INOP EMERGENCY LIGHT BATTERY PACKS M1668 AT PASSENGER CABIN. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS M1668 AND M1670 AT PASSENGER CABIN IAW AMM 33-51-06 -960-805 AND PERFORMED TEST OF THE NEW BATTERY PACK IAW AMM 33-51-06-960-805 TEST IS GOOD
BROKEN LAVATORY A EMERGENCY LIGHT ASSEMBLY AT FORWARD GALLEY AREA. / R&R LIGHT ASSEMBLY IAW AMM.
AFT GALLEY AREA WEB CRACKED BETWEEN BS. 927 TO BS. 947.5, BL 0. / R&R WEB IAW SRM AND DWG.
AFT CARGO COMPARTMENT SUPPORT ZEE CORRODED BETWEEN BS. 727 TO BS. 767, BETWEEN STR. 25R TO STR. 26R. / R&R SUPPORT ZEE IAW SRM AND DWG.
AFT CARGO COMPARTMENT SUPPORT ZEE CORRODED BETWEEN BS. 727 TO BS. 847, BETWEEN STR. 25L TO STR. 26L. / R&R SUPPORT ZEE IAW SRM AND DWG.
FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS. 400, STR. 26L. / R&R ANGLE IAW SRM AND DWG.
FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS. 500B, STR. 26L. / R&R ANGLE IAW SRM & DWG.
FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS. 500C, STR. 26L. / R&R ANGLE IAW SRM & DWG.
FORWARD CARGO COMPARTMENT CHANNEL SUPPORT CORRODED BETWEEN BS. 492 TO BS. 500A, STR. 26R. / R&R CHANNEL SUPPORT (SHIELD ASSEMBLY) IAW SRM AND DWG.
FLOOR STRUCTURE SUPPORT ANGLE CRACKED AT BS. 540, BETWEEN LBL 24.5 TO RBL 24.5. / R&R SUPPORT ANGLE IAW SRM.
FLOOR STRUCTURE ANGLE CRACKED AT BS. 685, BL 0, PASSENGER CABIN CENTER SECTION. / R&R ANGLE IAW DWG AND SRM.
CRACK ANGLE LOCATED BS 500C AND STR 26L AFT SIDE FLOOR STRUCTURE AT F WD CARGO COMPARTMENT / REPLACED ANGLE LOC BS 500C AND STR26L AFT SIDE FLOOR STRUCTURE AT FWD CARGO COMAPRTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 8 SRM; 51-40-02 AND DRAWING 143A7505 REV B
FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS. 440, STR. 26L. / R&R ANGLE IAW SRM & DWG.
AFT CARGO COMPARTMENT ANGLE SUPPORT CRACKED AT BS. 727, BETWEEN RBL 3 TO RBL 8. / R&R SUPPORT ANGLE IAW SRM AND DWG.
CRACK FWD CORNER SCUFF PLATE AND AFT CORNER SCUFF PLATE AFT CARGO COMPARTMENT / PERFORMED REPAIR FWD CORNER SCUFF PLATE AND AFT CORNER SCUFF PLATE LOC. ON AFT CATGO COMPARTMENT IAW EA # 1-A53-2076 REV.II
AFT CARGO COMPARTMENT CHANNEL SUPPORT CORRODED BETWEEN BS. 767 TO BS. 787, STR. 25R. / R&R CHANNEL SUPPORT IAW SRM & DWG.
FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET IAW SRM AND DWG.
FORWARD GALLEY AREA EMERGENCY EXIT LENS CRACKED. / R&R LENS IAW AMM.
R1 DOOR AT FORWARD GALLEY AREA LOWER BEAM CRACKED. / R&R LOWER BEAM IAW SRM AND DWG.
FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET IAW SRM AND DWG.
L/H HORIZONTAL STABILIZER INSPAR RIB LOCATED AT STAB. STA. 120.30 AND 9 INCHES FROM REAR SPAR. / REPAIRED INSPAR RIB IAW SRM.
L/H HORIZONTAL STABILIZER INSPAR RIB CRACKED LOCATED AT STAB. STA. 120.30, 19 INCHES FROM REAR SPAR. / REPAIRED RIB IAW SRM.
L/H HORIZONTAL STABILIZER INSPAR RIB CRACKED LOCATED AT STAB. STA. 120.30, 18 INCHES FROM FRONT SPAR. / REPAIRED RIB IAW SRM.
R/H HORIZONTAL STABILIZER INSPAR RIB CRACKED STAB. STA. 120.30 AT 28 INCH. / REPAIRED INSPAR RIB IAW SRM.
AFT CARGO COMPARTMENT ANGLE SUPPORT CRACKED AT BS. 867, STR. 26L. / R&R ANGLE SUPPORT IAW SRM AND DWG.
DUE TO MULTIPLE DENTS ON FORWARD CARGO DOOR RE SKIN IS REQUIRED BY CUSTOMER REQUEST AT FWD CARGO COMPARTMENT REPAIRED FORWARD CARGO DOOR SKIN IAW SRM 52-30-01-2R REPAIR 3 B737-700
EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M01670. R&R BATTERY PACK PER AMM AND DWG.
RT OVERWING EXIT LIGHT INOP. SECURED LIGHT PER SRM.
RT EMERGENCY EXIT HANDLE COVER FELL OFF. R&R COVER IAW SIP.
R2 DOOR EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. R&R BATTERY PER AMM.
L1 DOOR EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. R&R BATTERY PER AMM.
L1 DOOR EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. R&R BATTERY CHARGER PER AMM.
L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
RT EMERGENCY LIGHTS INOP. CHARGED BATTERY PER AMM.
LT EMERGENCY LIGHTS INOP. CHARGED BATTERY PER AMM.
LT BIN BULLNOSE EMERGENCY LIGHT INOP BETWEEN ROW 1 TO ROW 9. R&R BATTERY PACK PER AMM.
FORWARD EMERGENCY LIGHTS INOP AT LOCATION M1675. R&R BATTERY PACK PER AMM.
LT BIN BULLNOSE EMERGENCY LIGHT INOP AT ROW 12. R&R BATTERY PACK PER AMM.
RT BIN BULLNOSE EMERGENCY LIGHT INOP BETWEEN ROW 8 TO ROW 18. R&R BATTERY PACK PER AMM.
LT WING UPPER T/E PANEL JUST AFT OF #1 PYLON AFT HORIZ. BULB SEAL RETAINER IS CRACKED. / REMOVED AND REPLACED LT WING T/E BULB SEAL RETAINER AFT OF #1 PYLON; AFT LOCATION IAW SRM 51-40-02-0G-0 STEP 4; SRM 51-40-04-0G-0
AFT CARGO BAY FORWARD CORNER THRESHOLD IS CRACKED / REPAIRED AFT CARGO BAY FORWARD CORNER THRESHOLD IAW EA 1-A53-2076 REV 11
RIGHT WING LOWER T/E PANEL (651GB) I/B WIGGLE PLATE BROKEN / REMOVED AND REPLACED R/H WING LWR T/E PANEL (651GB) I/B WIGGLE PLATE IAW SRM 51-40-02-0G-0 PARA 4.
AFT CARGO BAY AFT CORNER THRESHOLD IS CRACKED / REPAIRED AFT CARGO BAY AFT CORNER THRESHOLD IAW EA 1-A53-2076 REV 11
RT WING NR 8 SLAT LOWER SURFACE OF THE SLAT NOSE SKIN AT ACTUATOR RIB CRACKED. REPAIRED SKIN PER SRM.
FORWARD ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP. R&R BATTERY CHARGER IAW AMM.
#1 ENG OUTBD T/R SLEEVE TRAILING EDGE 7 O'CLOCK POSITION DELAMINATED/DAMAGED / REPAIRED #1 ENG OUTBD T/R SLEEVE TRAILING EDGE 7 O'CLOCK POSITION PER SRM 54-30-01 AND SRM 51-70-05
L/H WHEEL WELL VERTICAL STIFFENER CRACKED. / REMOVED AND REPLACED L/H VERTICAL STIFFENER PER SRM 51-40-02.
AFT FLOOR PHOTO ILLUMINESCENT STRIP INOP. R&R STRIP PER AMM.
R2 DOOR SLIDE GIRT BAR RETAINER OUT OF ADJUST. ADJUSTED RETAINER IAW SIP.
L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR STOWAGE HOOK LOOSE. R&R HOOK IAW SRM & MT.
RT OVERWING EXTERNAL EMERGENCY LIGHT INOP. R&R LIGHT ASSEMBLY IAW AMM.
RT OVERWING EMERGENCY LIGHT INOP. R&R BATTERY PER AMM.
L2 DOOR SLIDE INADVERTENTLY FELL OUT OF IT`S CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED THE SLIDE IAW MT.
RIGHT OVERWING EXIT SIGN LOOSE. R & R THE SIGN IAW MM.
FUEL CROSSFEED VALVE INOPERATIVE. R & R FUEL CROSSFEED VALVE ACTUATOR IAW MM.
LT AFT FUSELAGE EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.
L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT LENS LOOSE. R & R LENS IAW SIP.
R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FORWARD NYLON SPACER BROKEN. R & R GIRT BAR ASSY IAW AMM.
COCKPIT EMERGENCY EXIT SWITCH DOME LIGHT INOPERATIVE. RECONNECTED LAMP IAW AMM.
RIGHT LOWER FORWARD OVERWING EMERGENCY EXIT LIGHT PARTIALLY INOPERATIVE. RELAMPED LIGHT IAW AMM.
LEFT FORWARD LOWER OVERWING EMERGENCY EXIT LIGHT PARTIALLY INOPERATIVE. RELAMPED LIGHT IAW AMM.
R2 DOOR INTERIOR EMERGENCY EXIT AREA LIGHT BELOW EXIT SIGN PARTIALLY INOPERATIVE. RELAMPED LIGHT IAW AMM.
LEFT EMERGENCY EXIT AREA LIGHT INOPERATIVE AT ROW 14. R & R LIGHT IAW AMM.
L2 DOOR ESCAPE SLIDE CONTAINER FORWARD END CAP MISSING. INSTALLED END CAP IAW SRM.
EXTERIOR EMERGENCY EXIT LIGHT LENS DIRTY. CLEANED LENS IAW AMM.
LEFT BULLNOSE BIN EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 11. R & R LIGHT IAW AMM.
STRINGER CORRODED AT BS 962, STRINGER 25L. REPAIRED STRINGER IAW ER & EA.
LEFT OVERWING EMERGENCY EXIT ESCAPE STRAP ANCHOR FITTING ASSEMBLY CORRODED. R & R FITTING ASSEMBLY IAW MM.
RIGHT OVERWING EMERGENCY EXIT ESCAPE STRAP ANCHOR FITTING ASSEMBLY CORRODED. R & R FITTING ASSEMBLY IAW MM.
L2 DOOR SLIDE GIRT BAR AFT QUICK DISCONNECT RETAINER RING BROKEN. R & R RING IAW AMM.
FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW EA.
RIGHT FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED BETWEEN BS 767 - 727. R & R SUPPORT IAW SRM.
RIGHT WING TRANSVERSE WEB CRACKED JUST INBD OF MAIN FLAP PROGRAM ROLLER SUPPORT ARM. R & R WEB IAW SRM.
RIGHT SIDE LOWER BULKHEAD CHORD SKIN CRACKED AT BS 540, 2ND LOWER AFT HOLE. REPAIRED SKIN IAW ER AND EA.
LOWER BULKHEAD CHORD CRACKED AT BS 540, STR 22L, 2ND LOWER AFT HOLE. REPAIRED SKIN IAW ER AND EA.
RIGHT WING UPPER T/E PANEL SUPPORT BEAM FORWARD SPAR ATTACHMENT ANGLE CRACKED AT RSS. 70.5. R & R ANGLE IAW SRM.
RIGHT WING UPPER T/E PANEL SUPPORT ANGLE CRACKED ABOVE NR 2 PYLON AFT TIP. R & R ANGLE IAW SOPM.
RIGHT WING LOWER TE WAFFLE PLATE CRACKED JUST INBD OF NR 2 PYLON AFT TIP. R & R PLATE ASSEMBLY IAW SRM.
FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 380, STRINGER 8R. REPAIRED FRAME IAW EA.
INTERCOSTAL CRACKED BETWEEN BS 328 - 344, LBL 47. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 312 - 328, LBL 47. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 312 - 328, RBL 34. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 277 - 294, RBL 2. R & R INTERCOSTAL IAW SRM.
INTERCOSTAL CRACKED BETWEEN BS 344 - 360, LBL 1. R & R INTERCOSTAL IAW SRM.
LOWER STUB FRAME CRACKED AT BS 294.5, RBL 54. R & R FRAME IAW SRM & DWG.
INTERCOSTAL CRACKED BETWEEN BS 344 - 360, LBL 7. R & R INTERCOSTAL IAW SRM.
FRAME CRACKED AT BS 360, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.
FORWARD CARGO BAY THRESHOLD WEB CORRODED BETWEEN BS 440 - 492, BETWEEN RBL 23 - 30.5. REPAIRED WEB IAW SRM.
AFT CARGO BAY FRAME ATTACH BRACKET CRACKED AT BS 727D, STRINGER 24R. R & R BRACKET IAW SRM & DWG.
FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 441, LBL 23. R & R SUPPORT IAW SRM.
RIGHT NR 1 WINDOW FRAME UPPER AFT CORNER, INTERIOR SURFACE CRACKED. REPAIRED CORNER IAW ACO.