N7827A
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2023-02-04 – 2023-02-04 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2023-02-04 – 2023-02-04 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
RH OVER WING EMERGENCY EXIT LIGHTS ARE INOP(SIDEWALL; ABOVE WINDOW) RH OVER WING EMERGENCY EXIT LIGHTS ARE INOP(SIDEWALL ABOVE WINDOW). REMOVED AND REPLACED RH OVER WING EMERGENCY EXIT LIGHT FUSE PER [AMM 33-21-00-960-803-NG (WINDOW LIGHT - FUSE REPLACEMENT - PERMANENT)] OPS CHECK GOOD.
DURING PROVO; L-2 EMER SLIDE PACK BECAME DISLODGED FROM DOOR HARNESS -NOT SLIDE DID NOT DEPLOY. REINSTALLED L2 DOOR SLIDE PER MT 725-61-06 AND AMM 25-66-01. OPS CHKD GOOD.
NR 3 MLG TIRE BURST ON TAKEOFF<[01] ACCOMPLSIHED CONDITIONAL INSPECTION IAW AMM 05-51-54; FOUND MULTIPLE AREAS WITH DAMAGE. REF. TTG8Q01BVDGT; TTG8Q01BVEQE AND TTG8Q01BVETW FOR DAMAGES. PANEL 651BB & R/H INBD AFT FLA AND PUSH ROD DAMAGED. REF. ORIGINAL LOGPAGE/ TTG8Q01BV9T9 FOR PICTURES.
POSSIBLE TIRE TREAD LOSS ON TAKEOFF OUT OF DEN.
LIGHT ON OVERWING EMERGENCY EXIT DOOR IS NOT WORKING FO SIDE, REPLACED TWO LAMPS, NO HELP. OK CONTINUE IAW MEL 33-2-03. FOUND ROW 15 DEF WINDOW LIGHT INOP WITH BAD FUSE. R & R ROW 15 DEF WINDOW LIGHT FUSE AND REPLACED THE LAMPS IAW AMM 33-21-00. OPS CHECKED GOOD.
NR 2 ENGINE DID NOT MAKE TAKEOFF POWER. PERFORMED FUEL PUMP IMPELLER SHAFT INSPECTION IAW M-26-173-00258. FOUND A SHEARED SHAFT. REMOVED AND REPLACED THE NR 2 ENGINE FUEL PUMP & HMU IAW MT 73-11-00. OPS & LEAK CHECKED GOOD. ACFT OK FOR SERVICE.
NR 2 ENGINE DID NOT MAKE TAKEOFF POWER. PERFORMED THE FUEL PUMP IMPELLER SHAFT INSPECTION IAW M-26-173-00258. FOUND SHEARED SHAFT, REMOVED AND REPLACED NR 2 ENGINE FUEL PUMP AND HMU IAW MT 73-11-00. OPS & LEAK CHECKED GOOD. ACFT OK FOR SERVICE.
LEFT WING OTBD AFT FLAP HAS 3' X 8' AREA DELAMINATION AT AFT INBOARD CORNER. REMOVED FLAP IAW MM 27-51-22, C/W RII REQUIREMENT FOR REMOVED FLAP IAW MM 27-51-22. REMOVED AND REPLACED LT OTBD AFT FLAP IAW AMM 27-51-22. OPS AND RIG CHECKED GOOD.
EMERGENCY EXIT SIGN ON BULKHEAD NEAR FWD ENTRY DOOR FOUND MISSING. REPLACED COVER IAW AMM 33-51-01.
LEFT FUSELAGE EMERGENCY LIGHT INOP RIGHT BEHIND LEFT WING TRAILING EDGE FLAPS. RELAMPED LEFT FUSELAGE EMERGENCY LIGHT PER AMM 33-51-04.
INTERIOR EMERGENCY EXIT LIGHT AT FWD ENTRY DOOR INOP. REMOVED AND REPLACED THE FWD LEFT POWER SUPPLY BATTERY PACK AND OPS TESTED GOOD IAW AMM 33-51-06.
EMERGENCY LIGHT AT ROW 4 A, B, C INOPERATIVE. REMOVED AND REPLACED BULB FOR EMERGENCY LIGHT IAW SIP AND OPS CHECKED GOOD IAW AMM 33-51-00.
FWD GALLEY AREA FWD SERVICE DOOR ASSISTANCE HANDLE LOOSE. 2025-349145<[01] TIGHTENED ASSISTANCE HANDLE FWD SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 SOPM 20-50-01;[02] CORRECTED STEP 1<BR>TIGHTENED ASSISTANCE HANDLE FWD SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 SOPM 20-50-01 REV. NO.39;[03] CERTIFIED ACTION 2; COMPLETED
L2 DOOR EMERGENCY LIGHT INOP. REPLACED L2 DOOR EMERGENCY LIGHT IAW AMM 33-51-04-960-801 TEST IS OK.
DETERIORATED ENTRY DOOR LINING PANEL ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA). REPLACED ENTRY DOOR LINING PANEL ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA) IAW B737-700 AMM 52-13-31-400-802 STEP 3. G.(2).
INOP EMERGENCY EXIT BATTERY PACK RT SIDE ON LOWERED CEILING AT AFT GALLEY AREA. REPLACED EMERGENCY EXIT (BATTERY PACK) RT SIDE ON LOWERED CEILING AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06-960-805, PERFORMED OPERATIONAL TEST, TESTED OK.
INOP EMERGENCY EXIT BATTERY PACK LT SIDE ON LOWERED CEILING AT AFT GALLEY AREA. REPLACED EMERGENCY EXIT BATTERY PACK LT SIDE ON LOWERED CEILING AT AFT GALLEY AREA IAW AMM 33-51-06-960-805. PERFORMED OPERATIONAL TEST, TESTED OK.
ELONGATED HOLE ACCESS PANEL 651FB TRAILING EDGE SUPPORT ANGLE RT WING. REPLACED SUPPORT ANGLE LOCATED ON ACCESS PANEL 651FB TRAILING EDGE RT WING IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A2710; SHEET 6; REV B.
CRACK BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND LBL1 AT PASSENGER CABIN. NOT FOUND ALLOWABLE DAMAGE FOR BRAKE PANEL ON SRM 53-30-51-1A-1 MEASURES ARE:L= 1.429 INCH. REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA540 AND BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DWG 143A0060 SHEET 36 REV A.
CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.601 INCH. PERFORMED REPAIR CATEGORY B LOC BTW LBL 25 TO LBL 60 BS 663 TO 675 AT PASSENGER CABIN IAW SRM 53-40-51-2R-2 REPAIR 2 ; EA #25-153-01480 AND #25-153-01480-WIP1.
ELONGATED HOLE ACCESS PANEL 651FB TRAILING EDGE TEE ANGLE RT WING. REPLACED TEE ANGLE LOCATED ON ACCESS PANEL 651FB TRAILING EDGE RT WING IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 115A2710; SHEET 4; REV B.
CRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND BL0 PASSENGER CABIN. REPLACED ANGLE FLOOR STRUCTURE LOCATED STA695 AND BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV A.
DETERIORATED ENTRY DOOR LINING PANEL ASSIST HANDLE NUT AT FWD GALLEY AREA (4 EA). REPLACED ENTRY DOOR LINING PANEL ASSIST HANDLE NUT AT FWD GALLEY AREA (4 EA) IAW B737-700 AMM 52-11-31-400-802 STEP 3. G. ITEM (2).
CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1; AND BAC 5975.
CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT. REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1; AND BAC 5975.
CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1; AND BAC 5975.
CRACK CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED THE CENTER (MIDDLE) SCUFF PALTE AT AFT CARGO COMPARTMENT IN ACCORDING WITH B737-700 SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4. C; STEPS (2 AND 4 TO 7); FIGURE 203. REFER TO BAC 5975.
RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. R&R RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL REF. AMM 53-31-31.
L2 DOOR SLIDE GIRT DRAGS<[01] REPACKED L2 DOOR SLIDE GIRT PER AMM 25-66-01.
SUPPLEMENTAL INFORMATION: L2 DOORWAY ASSIST HANDLE LOOSE (GALLEY SIDE)<[01] TIGHTENED L2 DOORWAY ASSIST HANDLE PER AMM 25-21-25.
L1 DOOR ESCAPE SLIDE GIRT REPACK REQUIRED.<[01] RE-PACKED L1 DOOR ESCAPE SLIDE GIRT REF AMM 25-66-01.
LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. REMOVED AND REPLACED L/H HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW AMM 53-31-31.
R2 DOOR SLIDE GIRT DRAGS<[01] REPACKED R2 DOOR SLIDE GIRT PER AMM 25-66-01.
PERFORMED A HIGH SPEED REJECTED TAKE OFF AT +- 110KTS DUE TO VISUAL AND AURAL FIRE INDICATIONS OF BOTH ENGINES; APU; AND WHEEL WELL. OVHT INDICATIONS AS WELL FOR BOTH ENGINES. TMNT#4118030049 SUBMITTED FOR FIRE CRT MODULE INSTALLED SER#1200 NOT #1370. ATTACH PICTURE OF PART TAG<[01] R/R ENG.& APU FIRE DETECTION CONTROL MODULE PER AMM 26-10-01; R/R ENG. & APU FIRE CONTROL PANEL PER AMM 26-18-01 OPS CK GOOD
AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR FWD SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.
LOSS OF A HYDRAULICS FLUID. DROPPED TO 20%.<[01] INSPECTED; FOUND HYDRAULIC LEAK COMING FROM A SYSTEM HYDRAULIC PUMP ACOUSTIC FILTER INLET UNION (SWIVEL ELBOW). REMOVED AND REPLACED THE SWIVEL ELBOW PACKING. OPERATION & LEAK CHECKS GOOD. REF. AMM 29-11-27. REPLENISHED ?A? HYD SYSTEM.
FORWARD ENTRY LOWER EXIT SIGN PLASTIC LENS NOT SECURE<[01] SECURED LENS PER AMM 20-50-11
FORWARD GALLEY SERVICE DOOR GIRT BAR DOES NOT STAY LOCKED IN PLACE AND IS LOOSE<[01] INSPECTED AND ADJUSTED GIRT BAR RETAINING CLIPS . OPS CHECK GOOD REF AMM 25.66.01. NO OTHER FAULTS FOUND.
EXTERNAL GROUND POWER RECEPTACLE DOOR SURROUND DOUBLER CRACKED AT LOWER TAB REF ORIGINAL FAULT # TTG8Q00QXA44<[01] REPAIRED PER SRM 53-10-15-2R-4.
ON AFT ENTRY DOOR; RIGHT SIDE ESCAPE SLIDE GIRT BAR MAKES CONTACT WITH EDGE OF AFT GALLEY STORAGE DOOR WHEN DOOR IS OPENED OR CLOSED<[01] FOUND LOWER MOUNTING SUPPORT PIN NOT ALIGNED CORRECTLY CAUSING SLIDE ASSY TO PROTRUDE TOO FAR FROM DOOR. REMOVED AND REINSTALLED SLIDE PER AMM 25-66-01. PROBLEM RESOLVED.<BR>NOTE: LEFT (ENTRY) DOOR WAS AFFECTED; NOT RIGHT DOOR.
AFT ENTRY DOOR SLIDE FELL OUT OF CONTAINER<[01] RESECURED AFT ENTRY DOOR SLIDE IN CONTAINER PER MT 725-61-06. A/C OK FOR SERVICE.
EMERGENCY LIGHT SWITCH IN COCKPIT FAULTY<[01] REPLACED COCKPIT EMERGENCY LIGHT SWITCH REF SWPM 20-83-00. OPS CHECK GOOD AT THIS TIME
EMERGENCY EXIT LIGHT HOUSING OVER FWD SERVICE DOOR IS BROKEN AND WILL NOT HOLD EXIT LENS REF M-21-133-00720-TLD.<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT HOUSING OVER FWD SVC DOOR REF AMM 33-51-01. OPS CHECK GOOD
FORWARD SERVICE DOOR EXIT SIGN FELL OFF.<[01] OK TO CONTINUE ON TLD PER EA M-21-133-00720. SIGN SECURED WITH TRANSPARENT TAPE.
CRACK ANGLE AT BS 747 CELING PANEL STRUCTURE AT AFT CARGO COMPARTMENT 2023-365739<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N:210138003 AND DUE DATE: 27-MAR-24.;[02] REPAIRED ANGLE LOCATED AT BS 747 CELING PANEL STRUCTURE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-70-11-2R-0.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[03] REPAIRED ANGLE LOCATED AT BS 747 CELING PANEL STRUCTURE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-70-11-2R-0. SEE INDIVIDUAL SIGN-OFF BELOW.
DETERIORATED STRIP PHOTOLUMINESCENT FLOOR AT PASSENGER CABIN (6 EA) 2023-365687<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR AT PASSENGER CABIN (6 EA) IAW SOPM 20-50-12 REV. 56 AND DWG-33500007 REV. 2;[02] CERTIFIED WORK PERFORMED. <BR>INVOLVED FAULT TTG8Q00LCS68; MT 733-50-01.
CRACK ON STR28R LOCATED BTW BS312 TO BS328 AT EQUIPMENT ELECTRONIC COMP 2023-365685<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 221860711; DUE DATE: 07 NOV 23.;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112811019; DUE DATE: 25-JAN-24.;[03] REPLACED STRINGER SECTION 28R AND FASTENERS LOCATED BTW STR 27R TO STR28R BTW BS294.5 TO BS 328 AT EQUIPMENT ELECTRONIC COMP IAW B737-700 SRM 53-10-03-01-1 AND SRM 51-10-02 STEP 9. SEE SEE INDIVIDUAL SING-OFFS BELOW;[04] TASK CARD COMPLETED <BR>REPLACED STRINGER SECTION 28R AND FASTENERS LOCATED BTW STR 27R TO STR28R BTW BS294.5 TO BS 328 AT EQUIPMENT ELECTRONIC COMP IAW B737-700 SRM 53-10-03-01-1 AND SRM 51-10-02 STEP 9. SEE SEE INDIVIDUAL SING-OFFS BELOW<BR>RII
CRACK ANGLE - SUPPORT LOCATED BS727B TO BS767 AND LBL51 CEILING STRUCTURE AREA AFT CARGO COMPARTMENT 2023-365591<[01] REPLACED ANGLE - SUPPORT LOCATED BS727 TO BS747 AND LBL51 STR-18L CEILING STRUCTURE AREA AFT CARGO COMPARTMENT IAW B737-700 SRM-51-40-02 AND DWG-149A9490 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE - SUPPORT LOCATED BS727 TO BS747 AND LBL51 STR-18L CEILING STRUCTURE AREA AFT CARGO COMPARTMENT IAW B737-700 SRM-51-40-02 AND DWG-149A9490 REV: - SEE INDIVIDUAL SIGN-OFF BELOW
CRACK FRAME ON BS 907 LOCATED BTW STR 25R TO STR 26R AFT CARGO COMPARTMENT 2023-365595<[01] REPLACED FRAME ON BS 907 LOCATED BTW STR 25R TO STR 26R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG# 147A1007; SHEET 42; REV.D. AND DWG# 147A1007; SHEET 55; REV.-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED FRAME ON BS 907 LOCATED BTW STR 25R TO STR 26R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG# 147A1007; SHEET 42; REV.D. AND DWG# 147A1007; SHEET 55; REV.-. SEE INDIVIDUAL SIGN OFF BELOW.<BR>CERTIFIED AS RII
CORROSION TRAILING EDGE FITTING LOC BTW FIN STA 132.2 AT FIN STA 150.6 AT VERTICAL STABILIZER 2023-365589<[01] REPLACED HOUSING ASSY -BEARING OF STANDBY RUDDER POWER CONTROL UNIT IAW B737-700 SRM 51-40-02-0G-0 AND AMM 20-50-11-910-801.SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1<BR>REPLACED HOUSING ASSY -BEARING OF STANDBY RUDDER POWER CONTROL UNIT IAW B737-700 SRM 51-40-02-0G-0 AND AMM 20-50-11-910-801;AMM 27-21-24-400-801.SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED HOUSING ASSY -BEARING OF STANDBY RUDDER POWER CONTROL UNIT IAW B737-700 SRM 51-40-02-0G-0 AND AMM 20-50-11-910-801;AMM 27-21-24-400-801.SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII
CRACK ANGLE BRACKET LOCATED BS947.5 AT LEVEL STR26L AFT CARGO COMPARTMENT 2023-365592<[01] REPLACED ANGLE BRACKET LOCATED BS947.5 AT LEVEL STR26L AFT CARGO COMPARTMENT. IAW B737-700 SRM: 51-10-02 ITEM 9 AND DWG:149A8103 SHEET 6 REV- SEE INDIVIDUAL SIGN-OFF BELOW.;[02] TASK CARD COMPLETED <BR>REPLACED ANGLE BRACKET LOCATED BS947.5 AT LEVEL STR26L AFT CARGO COMPARTMENT. IAW B737-700 SRM: 51-10-02 ITEM 9 AND DWG:149A8103 SHEET 6 REV- SEE INDIVIDUAL SIGN-OFF BELOW.<BR>RII
CRACK LEADING EDGE SKIN SLAT 6 AT RT WING 2023-365555<[01] TOOL USED: EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 220272512; DUE DATE: 17-DEC-23;[02] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 15-FEB-24 WAS USED;[03] TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[04] PERFORMED PERMANENT REPAIR ON LEADING EDGE SKIN SLAT 6 AT RT WING IAW IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8. SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED PERMANENT REPAIR ON LEADING EDGE SKIN SLAT 6 AT RT WING IAW IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8. SEE INDIVIDUAL SIGN OFF BELOW.
CORROSION SUPPORT ZEE LOCATED BTW BS727D TO BS727E RBL 23 WL 155.5 AT AFT CARGO COMPARTMENT 2023-365566<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N: 221859911 DUE DATE: 07-NOV-23;[02] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 RBL 23 WL 155.5 AT AFT CARGO COMPARTMENT AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG 146A7500 SHEET 61 REV - SEE INDIVIDUAL SIGN OFF BELOW;[03] TASK CARD COMPLETED <BR>REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 RBL 23 WL 155.5 AT AFT CARGO COMPARTMENT AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG 146A7500 SHEET 61 REV - SEE INDIVIDUAL SIGN OFF BELOW<BR>RII
CORROSION SUPPORT ZEE LOCATED BTW BS727A TO BS727D LBL 21 WL 155.5 AT AFT CARGO COMPARTMENT 2023-365567<[01] ULTRASONIC EQUIPMENT USED: P/N:45MG; S/N:130064101; DUE DATE: 12-OCT-23;[02] REPLACED SUPPORT ZEE AND FASTENERS LOC.BS 727 TO BS 847 AND FASTENERS LBL 21 WL 155.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DWG#146A7500 SHEET:61 REV:-;[03] CORRECTED STEP 2.<BR>REPLACED SUPPORT ZEE AND FASTENERS LOC.BS 727 TO BS 847 AND FASTENERS LBL 21 WL 155.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DWG#146A7500 SHEET:61 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[04] REPLACED SUPPORT ZEE AND FASTENERS LOC.BS 727 TO BS 847 AND FASTENERS LBL 21 WL 155.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DWG#146A7500 SHEET:61 REV:- RII;SEE INDIVIDUAL SIGN OFF BELOW.
CORROSION ANGLE LOCATED BTW BS767 TO BS787; WL156.1 AND RBL21 AT AFT CARGO COMPARTMENT 2023-365523<[01] REPLACED NEW ANGLE; NUT PLATES AND FASTENERS LOCATED BTW BS767 TO BS787; WL156.1 AND RBL21 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND 51-40-02 AND DWG 146A8123 SHEET 16 REV: -. SEE INDIVIDUAL SING-OFFS BELOW;[02] REPLACED NEW ANGLE; NUT PLATES AND FASTENERS LOCATED BTW BS767 TO BS787; WL156.1 AND RBL21 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND 51-40-02 AND DWG 146A8123 SHEET 16 REV: -. SEE INDIVIDUAL SING-OFFS BELOW RII CERTIFIED
CRACK ANGLE LOCATED BTW BS907 TO BS927 STR25R/STR27R AFT CARGO COMPARTMENT 2023-365525<[01] REPLACED ANGLE LOCATED BTW BS907 TO BS927 STR25R/STR27R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG NUMBER: 147A7221 SHEET: 17 REV: D: SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE LOCATED BTW BS907 TO BS927 STR25R/STR27R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG NUMBER: 147A7221 SHEET: 17 REV: D: <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGN OFF BELOW.<BR><BR>RII ACCOMPLISHED
CRACK TRACK RBBL 13.84 LOCATED BS727D AFT CARGO COMPARTMENT 2023-365524<[01] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; CAL DUE DATE: 30/AUG/23;[02] REPAIRED CARGO TRACK SECTION LOCATED FROM BS727B TO BS767 RBL 13.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM: 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4 STEP (P) FIG. 203. SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 2: REPAIRED CARGO TRACK SECTION LOCATED FROM BS727B TO BS767 RBL 13.84 AT AFT CARGO COMPARTMENT IAW B737-700 WIP1 AND SRM: 53-00-53-2R-3 REPAIR 3 PARAGRAPH 4 STEP (P) FIG. 203. SEE INDIVIDUAL SIGN OFF BELOW;[04] CORRECTED STEP 3<BR>: REPAIRED CARGO TRACK SECTION LOCATED FROM BS727B TO BS767 RBL 13.84 AT AFT CARGO COMPARTMENT I.A.W EA 23-153-01900-WIP1 AND 23-153-01900 SUMMARY . SEE INDIVIDUAL SIGN OFF BELOW;[05] TASK CARD COMPLETED <BR>REPAIRED CARGO TRACK SECTION LOCATED FROM BS727B TO BS767 RBL 13.84 AT AFT CARGO COMPARTMENT I.A.W EA 23-153-01900-WIP1 AND 23-153-01900 SUMMARY . SEE INDIVIDUAL SIGN OFF BELOW<BR>RII
CRACK ON ANGLE LOCATED BS 663.75 AND RBL 7 UPPER POSITION AT AIR CONDITIONING BAY 2023-365521<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24;[02] REPLACED ANGLE LOCATED BS 663.75 AND RBL 6.15 TO RBL 54.21 UPPER POSITION AT AIR CONDITIONING BAY IAW SRM B737-700 51-40-02 AND DRAWING 111A1000 REV:A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED ANGLE LOCATED BS 663.75 AND RBL 6.15 TO RBL 54.21 UPPER POSITION AT AIR CONDITIONING BAY IAW SRM B737-700 51-40-02 AND DRAWING 111A1000 REV:A. SEE INDIVIDUAL SIGN OFF BELOW. AS RII
CRACK ON ANGLE LOCATED BS 663.75 AND LBL 7 UPPER POSITION AT AIR CONDITIONING BAY 2023-365522<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24.;[02] REPLACED ANGLE AND FASTENERS LOCATED BS 663.75 AND LBL 6.15 TO LBL 54.21 UPPER POSITION AT AIR CONDITIONING BAY COMMON TO THE CENTER FUEL TANK IAW B737-700 SRM 51-40-02 AND DWG 111A1000 SHEET 130 REV . SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED ANGLE AND FASTENERS LOCATED BS 663.75 AND LBL 6.15 TO LBL 54.21 UPPER POSITION AT AIR CONDITIONING BAY COMMON TO THE CENTER FUEL TANK IAW B737-700 SRM 51-40-02 AND DWG 111A1000 SHEET 130 REV . SEE INDIVIDUAL SIGN OFF BELOW. AS RII
CRACK ON SUPPORT ANGLE LOCATED BS 867 CEILING AREA BTW STR 2R TO STR 3R AT PASSENGER CABIN 2023-365515<[01] REPLACED SUPPORT ANGLE LOCATED BS 867 CEILING AREA BTW STR 2R TO STR 3R AT PASSENGER CABIN I.A.W SRM B737-700 51-40-02 AND DRWING #146A7901 : REV:B;[02] CERTIFIED WORK PERFORMED.
CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 36 INCHES FROM FRONT SPAR AT RT HORIZONTAL STABILIZER 2023-365502<[01] TOOL USED: EDDY CURRENT EQUIPMENT P/N NORTEC500D S/N 00X12101V022237 DUE DATE : 26-JAN-24.;[02] TOOL USED: EDDY CURRENT EQUIPMENT P/N NORTEC500D S/N 00X12101V022237 DUE DATE: 26- JAN-24.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[04] REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AND 36 INCHES FROM FRONT SPAR AT RT HORIZONTAL IAW SRM B737-700 55-10-09-2R-5 REPAIR 5; SEE INDIVIDUAL SIGNOFF BELOW.;[05] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNOFF BELOW.
BROKEN SEAL BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER (1 EA) 2023-365516<[01] REPLACED SEAL BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER (1 EA) I.A.W SRM B737-700 51-40-02;[02] JOB COMPLETED
CRACK ANGLE - CLIP LOCATED BS BS500 AND STR26L AFT SIDE POSITION FWD CARGO COMPARTMENT 2023-365480<[01] REPLACED ANGLE AND FASTENER ON BS500 AND S-26L I.A.W SRM B737-700 51-40-02 AND DRAWING #143A7505 REV:-.SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] TASK CARD COMPLETED <BR>REPLACED ANGLE AND FASTENER ON BS500 AND S-26L I.A.W SRM B737-700 51-40-02 AND DRAWING #143A7505 REV:-.SEE INDIVIDUAL STEP SIGN OFFS BELOW<BR>RII
CRACK ANGLE - CLIP LOCATED BS500B AND STR26L FWD POSITION FWD CARGO COMPARTMENT 2023-365482<[01] REPLACED ANGLE AND FASTENER ON BS500B AND S-26L I.A.W SRM B737-700 51-40-02 AND DRAWING #143A7505 REV:B.SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] TASK CARD COMPLETED <BR>REPLACED ANGLE AND FASTENER ON BS500B AND S-26L I.A.W SRM B737-700 51-40-02 AND DRAWING #143A7505 REV:B.SEE INDIVIDUAL STEP SIGN OFFS BELOW<BR>RII
CRACK BILGE AREA CARGO TRACK RBL13.84 AND BS460 AT FWD CARGO COMPARTMENT 2023-365479<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138103 AND DUE DATE: 02-MAY-24.;[02] REPLACED CARGO TRACK SECTION LOCATED RBL 13. 84 BTW BS 400 TO BS 500A FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7500 SHEET:17 REV:A SEE INDIVIDUAL SIGN OFFS BELOW;[03] CORRECTED ITEM 2: REPAIRED CARGO TRACK SECTION LOCATED RBL 13. 84 BTW BS 400 TO BS 500A FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7500 SHEET:17 REV:A SEE INDIVIDUAL SIGN OFFS BELOW;[04] REPAIRED CARGO TRACK SECTION LOCATED RBL 13. 84 BTW BS 400 TO BS 500A FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7500 SHEET:17 REV:A SEE INDIVIDUAL SIGN OFFS BELOW AS RII
CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2023-365488<[01] TOOL USED DIGITAL CALIPER P/N:500-193-30;S/N:0000291;DUE DATE:12-OCT-23.;[02] TOOL USED: RADIOMETER PHOTOMETER PN: XRP-3000; SN: 1753759; DUE DATE: 14-OCT-23;[03] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-30-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-30-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) TO (7) AND BAC 5975. TASK COMPLETED.
CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2023-365487<[01] TOOL USED DIGITAL CALIPER P/N:500-193-30;S/N:0000291;DUE DATE:12-OCT-23.;[02] TOOL USED: RADIOMETER PHOTOMETER PN: XRP-3000; SN: 1753759; DUE DATE: 14-OCT-23;[03] REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-30-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-30-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) TO (7) AND BAC 5975. TASK COMPLETED.
CRACK ANGLE - CLIP LOCATED BS500A AND STR26L FWD POSITION FWD CARGO COMPARTMENT 2023-365481<[01] REPLACED ANGLE AND FASTENER ON BS500A AND S-26L I.A.W SRM B737-700 51-40-02 AND DRAWING #143A7505 REV:B .SEE INDIVIDUAL STEP SIGN OFFS BELOW;[02] TASK CARD COMPLETED <BR>REPLACED ANGLE AND FASTENER ON BS500A AND S-26L I.A.W SRM B737-700 51-40-02 AND DRAWING #143A7505 REV:B .SEE INDIVIDUAL STEP SIGN OFFS BELOW<BR>RII
CRACK FRAME ON BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA 2023-365458<[01] REPAIRED FRAME ON BS 312 AND BETWEEN STR5L TO STR6L FWD GALLEY AND LAV IAW EA M-22-153-01244 SEE SUB TASK BAR CODE TTG8Q00LEMH8;[02] CORRECTED STEP 1. REPAIRED FRAME ON BS 312 AND BETWEEN STR5L TO STR6L FWD GALLEY AND LAV IAW EA M-22-153-01244 SEE SUB TASK BAR CODE TTG8Q00LFQ59;[03] REPAIRED FRAME ON BS 312 AND BETWEEN STR5L TO STR6L FWD GALLEY AND LAV IAW EA M-22-153-01244 SEE SUB TASK BAR CODE TTG8Q00LFQ59; SEE INDIVIDUAL SIGN OFF BELOW.;[04] NOTE: STEP 1 SIGN OFF BELOW WAS SELECTED N/A BY ERROR BUT THIS STEP IS APPLICABLE AND HAS TO BE SELECTED AS COMPLETED
CRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.00 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.800 INCHES. 2023-365475<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220272712; CAL DUE DATE: 17-DEC-23;[02] REPAIRED ON EXTERNAL SKIN LOWER INSPAR AT STAB STA 184.70 TO STA. 203.10 AT RH HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11 AND SRM 51-40-05.SEE INDIVIDUAL SING OFF BELOW;[03] REPAIRED ON EXTERNAL SKIN LOWER INSPAR AT STAB STA 184.70 TO STA. 203.10 AT RH HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11 AND SRM 51-40-05.SEE INDIVIDUAL SING OFF BELOW<BR>RII
CRACK EXTERNAL SKIN LOWER INSPAR AT STAB STA 193.90 AT LT HORIZONTAL STABILIZER 2023-365420<[01] TOOL USED: EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 220272512; DUE DATE: 17-DEC-23;[02] TOOL USED ET EQUIPMENT: P/N: NORTEC 500D; S/N: N500X12101V022233; CAL DU DATE: 30-AUG-23;[03] PERFORMED REPAIR ON EXTERNAL SKIN LOWER INSPAR AT STAB STA 193.90 AT LT HORIZONTAL STABILIZER I.A.W. B737-700 SRM 55-10-01-2R-11 REPAIR 11. SEE INDIVIDUAL SIGN OFF BELOW.;[04] CERTIFIED STEP 3 COMPLETED <BR>RII
OUT OF LIMIT HANGER LINK ASSEMBLY ON RT MAIN LANDING GEAR 2023-365431<[01] REPLACED NEW HANGER LINK ASSEMBLY AND NEW PIN ON RT MAIN LANDING GEAR P/N:115A1500-14; S/N: BN 160003 AND NEW PIN (4) P/N:115A1610-601; S/N: STR33405 THE INSTALL IS DOCUMENTED ON TTG8Q0036KY AND REMOVED AND RE-INSTALLED LANDING GEAR SUPPORT BEAM IAW B737-700 AMM 57-15-00-000-801 AND AMM 57-15-00-400-801;[02] STEP 1 WAS CORRECTED <BR>REPLACED NEW HANGER LINK ASSEMBLY AND NEW PIN ON RT MAIN LANDING GEAR P/N:115A1500-14; S/N: BN 160003 AND NEW PIN (4) P/N:115A1610-601; S/N: STR33405 THE INSTALL IS DOCUMENTED ON TTG8Q0036KYR AND REMOVED AND RE-INSTALLED LANDING GEAR SUPPORT BEAM IAW B737-700 AMM 57-15-00-000-801 AND AMM 57-15-00-400-801.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED NEW HANGER LINK ASSEMBLY AND NEW PIN ON RT MAIN LANDING GEAR P/N:115A1500-14; S/N: BN 160003 AND NEW PIN (4) P/N:115A1610-601; S/N: STR33405 THE INSTALL IS DOCUMENTED ON TTG8Q0036KYR AND REMOVED AND RE-INSTALLED LANDING GEAR SUPPORT BEAM IAW B737-700 AMM 57-15-00-000-801 AND AMM 57-15-00-400-801. <BR>SEE INDIVIDUAL SIGN OFFS BELOW.<BR>RII
ELONGATED HOLE ACCESS PANEL 191HR AT LOWER FUSELAGE 2023-365410<[01] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 221859911; DUE DATE: 07-NOV-23.;[02] TOOL USED MICROMETER PN: 293-344-30 ; SN: 71735394 DUE DATE 23-NOV-23;[03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 25-JAN-24. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 25-JAN-24.;[04] TOOL USED RADIOMETER P/N: XRP-3000; S/N: 1753759; DUE DATE: 14-OCT-23.;[05] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24.;[06] REPAIRED ACCESS PANEL 191HR AT LOWER FUSELAGE IAW EA-23-153-02015 SEE INDIVIDUAL SIGN OFFS BELOW.;[07] REPAIRED ACCESS PANEL 191HR AT LOWER FUSELAGE IAW EA-23-153-02015 SEE INDIVIDUAL SIGN OFFS BELOW
ONE AFT EMERGENCY FLASHLIGHT RED LIGHT NOT BLINKING. R & R THE FLASHLIGHT BATTERY IAW AMM 25-64-00, OPS CHECKED GOOD.
#1 ENGINE NACELLE SUPPORT INBOARD FITTING I/B SIDE HOLE ELONGATED. COMPLIED WITH 22-157-03484-WIP1, COMPLIED WITH 22-157-03484-WIP2, COMPLIED WITH 2-157-03484-WIP1, COMPLIED WITH 22-157-03484-WIP2.
LIGHT OVER WING DOOR F/O SIDE INOP SIDEWALL LIGHT / [01] RELAMPED PER AMM 33-21-00; NO HELP. SIDEWALL LIGHT OK TO CONTINUE PER MEL 33-2-03; SP1B ;AUTH 90401;[02] REMOVED AND REPLACED BALLAST ON R/H OVERWING LIGHT ASSY AS PER AMM 33-51-04.
SMOKE FROM PACKS ON APU. APU TRIPPED OFF BUSSES. FIRE HANDLE PULLED; BOTTLE DISCHARGED. ACRID SMELL IN COCKPIT + THROUGHOUT CABIN. HAZE VISIBLE FROM FORWARD. CABIN. / [01] PERFORMED APU GENERATOR OPS AND LEAK CHECK PER AMM 49-41-21. OPS CHECK GOOD.
SMOKE FROM PACKS ON APU. APU TRIPPED OFF BUSSES. FIRE HANDLE PULLED; BOTTLE DISCHARGED. ACRID SMELL IN COCKPIT + THROUGHOUT CABIN. HAZE VISIBLE FROM FORWARD. CABIN. / [01] PERFORMED APU GENERATOR OPS AND LEAK CHECK PER AMM 49-41-21. OPS CHECK GOOD.
SMOKE FROM PACKS ON APU. APU TRIPPED OFF BUSSES. FIRE HANDLE PULLED; BOTTLE DISCHARGED. ACRID SMELL IN COCKPIT + THROUGHOUT CABIN. HAZE VISIBLE FROM FORWARD. CABIN. / [01] PERFORMED APU GENERATOR OPS AND LEAK CHECK PER AMM 49-41-21. OPS CHECK GOOD.
SMOKE FROM PACKS ON APU. APU TRIPPED OFF BUSSES. FIRE HANDLE PULLED; BOTTLE DISCHARGED. ACRID SMELL IN COCKPIT + THROUGHOUT CABIN. HAZE VISIBLE FROM FORWARD. CABIN. / [01] PERFORMED APU GENERATOR OPS AND LEAK CHECK PER AMM 49-41-21. OPS CHECK GOOD.
SUPPLEMENTAL INFORMATION: FWD HORSESHOE PANEL EMERGENCY LIGHT INOP ; / [01] RELAMPED FWD EMERGENCY BULB IAW AMM 33-51-03 OPS CHECK GOOD
EMERGENCY EXIT LIGHT COVER MISSING AT EXIT ROW; FOS SIDE ; / [01] INSTALLED EMERGENCY EXIT LIGHT COVER IN REF TO AMM 33-51-01
CUSTOMER REQUEST; SW. DURING AAI INSPECTION OF REPAIR 6; STA 727 INTERCOSTAL BETWEEN STRINGERS 27L AND 27R HAS EVIDENCE OF CORROSION FWD SIDE. ; *CORRECTION TO LOCATION* STATION 727+4' INTERCOSTAL BETWEEN STRINGERS 27L AND 27R / [01] REMOVED INTERCOSTAL AT AFT CARGO AT STA 727 BETWEEN STR 28L AND 28R IAW SRM 51 40 02 0G-0; [02] VERIFIED NEW INTERCOSTAL WEB AS P/N 146A3426-7 'A' TAG A49451 IAW BOEING DWG 146A0061 REV :A; [03] INSPECTION VERIFIED STEPS 1 AND 2; [04] LOCATED AND DRILLED NEW WEB IAW SRM 51-40-05-0G-0 AND DWG 146A3426 SHT 7 REV-; [05] VERIFIED STEP 4. OK TO INSTALL; [06] -OUT OF SEQUENCE- REMOVED DAMAGE. ORIGINAL'T' .032' REMAINING .020' LOSS OF .012'. OUT OF LIMITS IAW SRM 53-00-12-1A-1; [07] INSTALLED INTERCOSTAL IAW SRM 51-40-02-0G-0 & DWG 146A0061 SHT 34 REV A; [08] STEP 6&7 C/W; [09] OK TO CIC; [10] APPLIED CIC TO INTERCOSTAL AREA IAW AMM 51-21-91-620-802; [11] STEP 10 C/W; [12] VERIFIED ALL STEPS COMPLETE; [13] C/W
BROKEN FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT ; 2021-288151 / [01] REPAIRED BY WELD CRACK ON FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4.B AND BAC 5975 TOOL USED DIGITAL CALIPER P/N 500-197-30 S/N B20189443 DUE DATE 22-NOV-21; [02] REPAIRED BY WELD CRACK ON FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4.B AND BAC 5975 TOOL USED DIGITAL CALIPER P/N 500-197-30 S/N B20189443 DUE DATE 22-NOV-21
CRACK SCUFF PLATE ON FWD SERVICE DOOR AT FWD GALLEY AREA ; 2021-288149 / [01] REPAIRED SCUFF PLATE ON FWD SERVICE DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B AND BAC 5975.; [02] REPAIRED SCUFF PLATE ON FWD SERVICE DOOR AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B AND BAC 5975.
CORROSION ON KEEL BEAM RH LOWER FLANGE INBOARD SIDE LOCATED BTW BS 727B AND BS 727B PLUS 10 AT AFT CARGO COMPARTMENT ; 2021-288124 / [01] TOOL USED: DIGITAL CALIPER P/N: 700-113-10; S/N: 0033158; DUE DATE: 14/JUL/21; [02] TOOL USED P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 01-DEC-21; [03] SUMMARY EA 21-153-01870 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO THE FAULT BARCODE TTG8Q005LDN3.; [04] REPAIRED KEEL BEAM RH LOWER FLANGE INBOARD SIDE LOCATED BTW BS 727B AND BS 727B PLUS 10 AT AFT CARGO COMPARTMENT IAW EA 21-153-01870; 21-153- 01870-WIP1 AND 21-153-01870-WIP2. NOT FURTHER ACTION AND REINSPECTION REQUIRED.; [05] TASK CARD COMPLETE AND CERTIFIED AS RII.
ELONGATED HOLE FORWARD FAIRING 542AB DRAIN LT WING ; 2021-288131 / [01] TOOL USED: CALIPER P/N: DIGITAL 150 S/N:AE-412610 DUE DATE: 21-MAY-22; [02] HOT BONDER P/N: HCS9000B-AV S/N: 18164925 DUE DATE: 19-NOV-21; [03] SCALE P/N: SCA-301 S/N: AE-412134 DUE DATE 24/FEB/22; [04] TOOL USED: HOT BONDER P/N:HCS9200B S/N:15102320 DUE DATE:19-NOV-21; [05] TOOL USED: FLUKE 1587; S/N: 38200034; DUE DATE: 20-MAR-22.; [06] REPAIRED FORWARD FAIRING 542AB LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.; [07] REPAIRED FORWARD FAIRING 542AB LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.
TORN GIRT BAR FITTING SHIM ON ENTRY DOOR AT AFT GALLEY AREA (2 EA) ; 2021-288087 / [01] REPLACED GIRT BAR FITTING SHIM ON ENTRY DOOR AT AFT GALLEY AREA (2 EA) I.A.W B737-700 AMM 25-66-02-400-801 PART USED:69-64426-1; [02] REPLACED GIRT BAR FITTING SHIM ON ENTRY DOOR AT AFT GALLEY AREA (2 EA) I.A.W B737-700 AMM 25-66-02-400-801 PART USED:69-64426-1.
CORROSION FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT ; 2021-288108 / [01] REPLACED FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 TEM 9; SRM 51-40-05 AND DWG 453A1610 REV C.; [02] REPLACED FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 TEM 9; SRM 51-40-05 AND DWG 453A1610 REV C.
RUST ON SERVICE DOOR HARDWARE GIRT BAR FITTING AT FWD GALLEY AREA ; 2021-288089 / [01] REPLACED ON SERVICE DOOR HARDWARE GIRT BAR FITTING AT FWD GALLEY AREA IAW SOPM 20-50-01 AND P/N USED:BACB30NN4K15; MS35338-43; NAS623-3-5.; [02] REPLACED ON SERVICE DOOR HARDWARE GIRT BAR FITTING AT FWD GALLEY AREA IAW SOPM 20-50-01
RUST ON ENTRY DOOR HARDWARE GIRT BAR FITTING AT FWD GALLEY AREA ; 2021-288088 / [01] REPLACED ENTRY DOOR HARDWARE GIRT BAR FITTING AT FWD GALLEY AREA I.A.W B737-700 25-66-02-400-801 PART USED:NAS23623-3-5;MS35338-43;BACB30NN4K15; [02] REPLACED ENTRY DOOR HARDWARE GIRT BAR FITTING AT FWD GALLEY AREA I.A.W B737-700 25-66-02-400-801; [03] REPLACED ENTRY DOOR HARDWARE GIRT BAR FITTING AT FWD GALLEY AREA I.A.W B737-700 25-66-02-400-801
CORROSION FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT ; 2021-288106 / [01] REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DRAWING 453A1610 SHEET 29 REV B; [02] REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND SRM 51-40-02; SRM 51-10-02 AND DRAWING 453A1610 SHEET 29 REV B.; [03] REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND SRM 51-40-02; SRM 51-10-02 AND DRAWING 453A1610 SHEET 29 REV B.
TORN GIRT BAR FITTING SHIM ON SERVICE DOOR AT AFT GALLEY AREA (2 EA) ; 2021-288086 / [01] REPLACED GIRT BAR FITTING SHIM ON SERVICE DOOR AT AFT GALLEY AREA (2 EA) I.A.W B737-700 AMM 25-66-02-400-801 PART USED:69-64426-1; [02] REPLACED GIRT BAR FITTING SHIM ON SERVICE DOOR AT AFT GALLEY AREA (2 EA) I.A.W B737-700 AMM 25-66-02-400-801 PART USED:69-64426-1.
TORN ENTRY DOOR SHIM GIRT BAR FITTING AT FWD GALLEY AREA (2 EA) ; 2021-288084 / [01] REPLACED ENTRY DOOR SHIM GIRT BAR FITTING AT FWD GALLEY AREA (2 EA) I.A.W B737-700 AMM 25-66-02-400-801 PART USED:69-64426-1; [02] REPLACED ENTRY DOOR SHIM GIRT BAR FITTING AT FWD GALLEY AREA (2 EA) I.A.W B737-700 AMM 25-66-02-400-801 PART USED:69-64426-1.
TORN SERVICE DOOR SHIM GIRT BAR FITTING AT FWD GALLEY AREA (2 EA) ; 2021-288085 / [01] REPLACED SERVICE DOOR SHIM GIRT BAR FITTING AT FWD GALLEY AREA (2 EA) IAW AMM-25-66-02-400-801; [02] REPLACED SERVICE DOOR SHIM GIRT BAR FITTING AT FWD GALLEY AREA (2 EA) IAW AMM-25-66-02-400-801.
RUST ON ENTRY DOOR HARDWARE GIRT BAR FITTING AT AFT GALLEY AREA ; 2021-288091 / [01] REPLACED ENTRY DOOR HARDWARE GIRT BAR FITTING AT AFT GALLEY AREA I.A.W B737-700 25-66-02-400-801 PART USED:BACB30LR-18;BACB30LU4-15;MS35338-43;NAS623-3-5; [02] REPLACED ENTRY DOOR HARDWARE GIRT BAR FITTING AT AFT GALLEY AREA I.A.W B737-700 25-66-02-400-801
RUST ON SERVICE DOOR HARDWARE GIRT BAR FITTING AT AFT GALLEY AREA ; 2021-288090 / [01] REPLACED SERVICE DOOR HARDWARE GIRT BAR FITTING AT AFT GALLEY AREA IAW AMM-25-66-02-400-801; PART USED:NAS623-3-5;MS35338-43;BACB30LU4-15;BACB30LR4-18; [02] REPLACED SERVICE DOOR HARDWARE GIRT BAR FITTING AT AFT GALLEY AREA IAW AMM-25-66-02-400-801
CORROSION ANGLE LOCATED BETWEEN STR 26L TO STR 27L AND BS 807 WL 148.5 AT AFT CARGO COMPARTMENT ; 2021-288076 / [01] TOOL USED DIGITAL CALIPER PN 500-197-30; SN: B20189571; DUE DATE: 22-NOV-21.; [02] CALIPER PN: 500-197-30; SN: A18229497; DUE DATE: 27-JUL-21; [03] TOOL USED: POWER PACK PN: FMK0003223; SN: PE0412/63335; DUE DATE: 23 AUG 21. THERMOMETER PN: FLUKE63; SN: 31330088; DUE DATE 18 MAY 22. MULTIMETER; PN: 2217-20; SN: B83B914290479; DUE DATE: 14 APR 22.; [04] REPLACED ANGLE (SHEAR TIE) LOCATED BETWEEN STRINGER 26L TO STR 27L AND BS 807 WL 148.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02; DWG # 146A3230 REV B. AND DWG-146A1263 REV. A; [05] REPLACED ANGLE (SHEAR TIE) LOCATED BETWEEN STRINGER 26L TO STR 27L AND BS 807 WL 148.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02; DWG # 146A3230 REV B. AND DWG-146A1263 REV. A. RII
CORROSION KEEL BEAM L/H SIDE LOCATED BETWEEN BS 727D TO BS 787 WL 148.5 AT AFT CARGO COMPARTMENT ; 2021-288061 / [01] TOOL USED DIGITAL CALIPER P/N: 700-113-10; S/N: 0033158; DUE DATE: 14/JUL/2172; [02] TOOL USED P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22.; [03] TOOL USED: P/N: NORTEC 600D S/N: 210138103 DUE DATE: 05-MAR-22; [04] REPAIRED KEEL BEAM L/H SIDE LOCATED BETWEEN BS 727D TO BS 787 WL 148.5 AT AFT CARGO COMPARTMENT IAW 21-153-01867;EA# 21-153-01867-WIP1; EA# 21-153-01867-WIP2. THIS REPAIR IS CLASSIFIED MINOR AND CATEGORY A. NO FURTHER ACTION OR INSPECTION REQUIRED.; [05] REPAIRED KEEL BEAM L/H SIDE LOCATED BETWEEN BS 727D TO BS 787 WL 148.5 AT AFT CARGO COMPARTMENT IAW 21-153-01867;EA# 21-153-01867-WIP1; EA# 21-153-01867-WIP2. THIS REPAIR IS CLASSIFIED MINOR AND CATEGORY A. NO FURTHER ACTION OR INSPECTION REQUIRED.
ELONGATED HOLE TRACK SUPPORT LOCATED BETWEEN BS 727A TO BS 727B AND RBL 13.84 AT AFT CARGO COMPARTMENT ; 2021-288036 / [01] TOOL USED: CALIPER 500-197-30 SN A18229497 DUE DATE 27 JUL 21.; [02] TOOL USED P/N:NORTEC 500D; S/N: N500X1693P030457; CAL DUE DATE: 02-JUN-22; [03] REPAIRED CARGO TRACK LOC BS727+4 INCH TO BS727B+8 INCH RBL 13.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3; [04] REPAIRED CARGO TRACK LOC BS727+4 INCH TO BS727B+8 INCH RBL 13.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3.. RII ITEM
GOUGE FRAME ON BS 727C AT LEVEL STRINGER 22L AT AFT CARGO COMPARTMENT ; 2021-288037 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N 112031023 DUE DATE: 22-JAN-22.; [02] REPAIRED FRAME AT BSTA 727C BTW S-21L & S-24L IAW EA# 21-153-01819; EA# 21-153-01819-WIP1; EA# 21-153-01819-WIP2; EA# 21-153-01819-WIP3. THIS REPAIR IS CLASSIFIED AS MAJOR AND CATEGORY B WITH AN INSPECTION THRESHOLD OF 75;000 TOTAL FLIGHT CYCLES.; [03] REPAIRED FRAME AT BSTA 727C BTW S-21L & S-24L IAW EA# 21-153-01819; EA# 21-153-01819-WIP1; EA# 21-153-01819-WIP2; EA# 21-153-01819-WIP3 REV 2. THIS REPAIR IS CLASSIFIED AS MAJOR AND CATEGORY B WITH AN INSPECTION THRESHOLD OF 75;000 TOTAL FLIGHT CYCLES.; [04] CERTIFIED RII MAJOR REPAIR WORK PERFORMED.
CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 727A TO BS 727B AT LEVEL STRINGER 25R AT AFT CARGO COMPARTMENT ; 2021-288038 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22. TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [02] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS 727A TO BS 727B AT LEVEL STRINGER 25R AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 STEP 9 AND SRM 51-40-02 AND DWG 146A7500 REV:-; [03] VERIFIED TASK COMPLETE. TASK RII
CORROSION ANGLE LOCATED BETWEEN STRINGER 26L TO STR 27L AND BS 787 WL 148.5 AT AFT CARGO COMPARTMENT ; 2021-288054 / [01] TOOL USED :DIGITAL CALIPER PN: 500-197-30; SN: B20189571; DUE DATE: 22-NOV-21.; [02] REPLACED SHEAR TIE LOCATED BETWEEN STRINGER 26L TO STR 27L AND BS 787 WL 148.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02; DWG # 146A3230 REV B AND 146A1262 REV -; [03] REPLACED SHEAR TIE LOCATED BETWEEN STRINGER 26L TO STR 27L AND BS 787 WL 148.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02; DWG # 146A3230 REV B AND 146A1262 REV -. VERIFIED AS RII .
CORROSION ANGLE LOCATED BETWEEN STR 25L TO STR 26L AND BS 787 WL 148.5 AT AFT CARGO COMPARTMENT ; 2021-288057 / [01] TOOL USED DIGITAL CALIPER PN: 500-197-30; SN: B20189571; DUE DATE: 22-NOV-21; [02] TOOL USED CALIPER PN 500-197-30 SN A18229497 DUE DATE 27 JUL 21.; [03] TOOL USED: POWER PACK PN. FMK0003223 SN. PE0412/63335 DUE DATE 23 AUG 21. THERMOMETER PN. FLUKE63 SN. 31330088 DUE DATE 18 MAY 22. MULTIMETER PN 2217-20 SN B83B914290479 DUE DATE 14 APR 22.; [04] TOOL USED: POWER PACK PN. FMK0003223 SN. PE0412/63335 DUE DATE 23 AUG 21. THERMOMETER PN. FLUKE63 SN. 31330088 DUE DATE 18 MAY 22. MULTIMETER PN 2217-20 SN B83B914290479 DUE DATE 14 APR 22.; [05] REPLACED ANGLE (SHEAR TIE) LOCATED BETWEEN STRINGER 26L TO STR 25L AND BS 787 WL 148.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02; DWG # 146A3230 REV B AND 146A1262 REV -; [06] REPLACED ANGLE (SHEAR TIE) LOCATED BETWEEN STRINGER 26L TO STR 25L AND BS 787 WL 148.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02; DWG # 146A3230 REV B AND 146A1262 REV -
CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN ; 2021-288019 / [01] REPLACED TIE CLIP LOCATED BS277 AND STR 10R AT PASSENGER CABIN (1 EA) I.A.W B737-700 SRM 51-10-02 AND DWG 141A1110 REV:-; [02] REPLACED TIE CLIP LOCATED BS277 AND STR 10R AT PASSENGER CABIN (1 EA) I.A.W B737-700 SRM 51-10-02 AND DWG 141A1110 REV:-<BR>RII
CRACK INNER CHORD LOCATED BS 303.9 AND STR 17L AT FWD GALLEY AREA ; 2021-288022 / [01] REPLACED INNER CHORD LOCATED BS 303.9 AND STR 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02 AND DWG #141A8110 SHEET 10 REV A AND 140A9810 SHEET 48 REV -.; [02] REPLACED INNER CHORD LOCATED BS259.50 TO BS351.20 AND STR 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02 AND DWG #141A8110 SHEET 10 REV A AND 140A9810 SHEET 48 REV -.; [03] REPLACED INNER CHORD LOCATED BS259.50 TO BS351.20 AND STR 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02 AND DWG #141A8110 SHEET 10 REV A AND 140A9810 SHEET 48 REV -.
CRACK ANGLE - SUPPORT LOCATED BS 380 TO BS 400 AND LBL 13 AT FWD GALLEY AREA ; 2021-288016 / [01] TOOL USED RADIUS GAUGE PN 2204A3; SN AE-408653 CAL DUE DATE 17 DEC 21.; [02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22. TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [03] REPLACED ANGLE AND FASTENERS LOCATED BS 380 TO BS 400 AND LBL 13 AT FWD GALLEY AREA I.A.W B 737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A5300 SHEET: 38 REV: A; [04] REPLACED ANGLE AND FASTENERS LOCATED BS 380 TO BS 400 AND LBL 13 AT FWD GALLEY AREA I.A.W B 737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A5300 SHEET: 38 REV: A COMPLETE RII INSPECTION
CRACK ANGLE - SUPPORT LOCATED BS 380 TO BS 400 AND BL 0 AT FWD GALLEY AREA ; 2021-288014 / [01] REPLACED ANGLE - SUPPORT AND FASTENERS 1(EA) LOCATED BS 380 TO BS 400 AND BL 0 AT FWD GALLEY AREA I.A.W B 737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A5400 SHEET 2 REV: D.; [02] REPLACED ANGLE - SUPPORT AND FASTENERS 1(EA) LOCATED BS 380 TO BS 400 AND BL 0 AT FWD GALLEY AREA I.A.W B 737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A5400 SHEET 2 REV: D.<BR>RII ITEM.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS312 TO BS328 AND RBL33 FWD GALLEY AND LAV ; 2021-288025 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-20 S/N:11094443 DUE DATE:10-SEP-21; [02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE 1 (EA) AND FASTENERS LOCATED BTW BS312 TO BS328 AND RBL 33 FWD GALLEY AND LAV I.A.W B 737-700; SRM 51-10-02 TEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -.; [03] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE 1 (EA) AND FASTENERS LOCATED BTW BS312 TO BS328 AND RBL 33 FWD GALLEY AND LAV I.A.W B 737-700; SRM 51-10-02 TEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -.<BR>RII ITEM.
CRACK ANGLE - SUPPORT LOCATED BS 380 TO BS 400 AND RBL 10 AT FWD GALLEY AREA ; 2021-288018 / [01] REPLACED ANGLE - SUPPORT LOCATED BS 380 TO BS 400 AND RBL 10 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #143A5400 REV -.; [02] REPLACED ANGLE - SUPPORT LOCATED BS 380 TO BS 400 AND RBL 10 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9;SRM 51-40-02 AND DWG #143A5400 REV -. TOOL USED FOR MEASURE; CALIPER P/N: DIGITAL 150 S/N: AE-412608 DUE DATE: 25 MAY 22; [03] REPLACED ANGLE - SUPPORT LOCATED BS 380 TO BS 400 AND RBL 10 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9;SRM 51-40-02 AND DWG #143A5400 REV -. TOOL USED FOR MEASURE; CALIPER P/N: DIGITAL 150 S/N: AE-412608 DUE DATE: 25 MAY 22.<BR>RII ITEM.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AND BL 0 FWD GALLEY AND LAV ; 2021-288024 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AND BL 0 FWD GALLEY AND LAV IAW SRM B737-700 51-10-02 AND DWG 141A5400 REV: -; [02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AND BL 0 FWD GALLEY AND LAV IAW SRM B737-700 51-10-02 AND DWG 141A5400 REV: -<BR>RII
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS312 TO BS328 AND LBL47 FWD GALLEY AND LAV. REPLACED WEB INTERCOSTAL FLOOR STRUCTURE 1 (EA) LOCATED BTW BS312 TO BS328 AND LBL47 FWD GALLEY AND LAV I.A.W B 737-700 SRM 51-10-02 TEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -. REPLACED WEB INTERCOSTAL FLOOR STRUCTURE 1 (EA) LOCATED BTW BS312 TO BS328 AND LBL47 FWD GALLEY AND LAV I.A.W B 737-700 SRM 51-10-02 TEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -.
CRACK BS 294.5 ANGLE - SUPPORT LOCATED AT LEVEL STR17R FWD GALLEY AND LAV ; 2021-288017 / [01] REPLACED NEW ANGLE - SUPPORT 1 (EA) LOCATED AT LEVEL STR 17R FWD GALLEY AND LAV I.A.W B 737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 25 REV-; [02] REPLACED NEW ANGLE - SUPPORT 1 (EA) LOCATED AT LEVEL STR 17R FWD GALLEY AND LAV I.A.W B 737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 25 REV- RII
CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT ; 2021-287929 / [01] DIGITAL CALIPER P/N: 500-197-30 S/N:B20189526 DUE DATE 22-NOV-21; [02] REPAIRED BY WELD CRACK ON AFT CORNER AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B AND BAC 5975 TOOL USED DIGITAL CALIPER P/N 500-197-30 S/N B20189526 DUE DATE 22-NOV-21; [03] REPAIRED BY WELD CRACK ON AFT CORNER AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B AND BAC 5975 TOOL USED DIGITAL CALIPER P/N 500-197-30 S/N B20189526 DUE DATE 22-NOV-21.
CRACK SUPPORT ANGLE LOCATED AT BS 690 AT LEVEL BL 0 CENTER SECTION ; 2021-287862 / [01] TOOL USED PN: NORTEC 600D; SN: 200048001; DUE DATE: 24FEB22; [02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22. TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [03] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [04] REPLACED SUPPORT ANGLE LOCATED AT BS 690 AT LEVEL BL 0 CENTER SECTION; MATERIAL USED ALUMINUM SHEET 7075T6/0.050 P.O: 2021-139514. IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 AND DWG# 273A9112 SHEET 5 REV B; [05] JOB COMPLETED.<BR>CERTIFIED AS RII.
BROKEN WINDSCREEN LT SIDE STRAP EMERGENCY FLASH LIGHT AT FWD GALLEY AREA (4 EA) ; 2021-287863 / [01] REPLACED WINDSCREEN LT SIDE STRAP EMERGENCY FLASH LIGHT AT FWD GALLEY AREA (4 EA) IAW B737-700 AMM 25-64-00-900-806; [02] REPLACED WINDSCREEN LT SIDE STRAP EMERGENCY FLASH LIGHT AT FWD GALLEY AREA (4 EA) IAW B737-700 AMM 25-64-00-900-806
CRACK LEADING EDGE SUPPORT WEB LOCATED AT BS 1016 AT LEVEL S-2R AND 2L AT VERTICAL STABILIZER ; 2021-287875 / [01] REPLACED LEADING EDGE SUPPORT WEB LOCATED AT BS 1016 AT LEVEL S-2R AND 2L AT VERTICAL STABILIZER IAW B737-700 SRM51-10-2 TEM 9; SRM 51-40-02 AND DRAWING 176A3101 SHEET 4; REV -.; [02] REPLACED LEADING EDGE SUPPORT WEB LOCATED AT BS 1016 AT LEVEL S-2R AND 2L AT VERTICAL STABILIZER IAW B737-700 SRM51-10-02 TEM 9; SRM 51-40-02 AND DRAWING 176A3101 SHEET 4; REV -. LENGHT OF CRACK IS: 0.750 INCH TOOL USED DIGITAL CALIPER P/N: DIGITAL150; S/N: AE-412608; DUE DATE: 25-MAY-22.; [03] JOB COMPLETE AND CERTIFIED.
CRACK LEADING EDGE RIB AT LE STA 105.26 AT RT HORIZONTAL STABILIZER ; 2021-287839 / [01] REPLACED RIB LOCATED ON LEADING EDGE AT LE STA 105.26 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02 AND DWG # 186A1001 REV A; [02] REPLACED RIB LOCATED ON LEADING EDGE AT LE STA 105.26 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02 AND DWG # 186A1001 REV A.RII
CRACK LEADING EDGE RIB AT LE STA 78.29 AT LT HORIZONTAL STABILIZER ; 2021-287838 / [01] REPLACED LEADING EDGE RIB AT LE STA 78.29 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9;51-40-02 AND DRAWING 176A3101; [02] REPLACED LEADING EDGE RIB AT LE STA 78.29 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9;51-40-02 AND DRAWING 176A3101 RII; [03] REPLACED LEADING EDGE RIB AT LE STA 78.29 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9;51-40-02 AND DRAWING 176A3101 RII
MISSING OVERHEAD STOWAGE BIN EM. EXIT LIGHT LENS ON BIN 4 LT SIDE AT PASSENGER CABIN (1 EA) ; 2021-287717 / [01] INSTALLED OVERHEAD STOWAGE BIN EM. EXIT LIGHT LENS ON BIN 4 LT SIDE AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-03-960-802; [02] INSTALLED OVERHEAD STOWAGE BIN EM. EXIT LIGHT LENS ON BIN 4 LT SIDE AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-03-960-802
DELAMINATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) ; 2021-287729 / [01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-14-960-802; [02] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-14-960-802 COMPLETED
R/H MLG FORWARD TRUNNION SUPPORT FITTING; UPPER OUTBOARD LUG FACE HAS EVIDENCE OF CORROSION. ; / C/W JIC; EA 1-A57-3246 REV 12 COMPLETED; EA 1-A57-3246 REV 12 COMPLETED
L/H MLG FORWARD TRUNNION SUPPORT FITTING; UPPER OUTBOARD LUG FACE HAS EVIDENCE OF CORROSION. ; / C/W JIC; COMPLETED IAW 1-A57-3246 REV 12; COMPLETED IAW 1-A57-3246 REV 12
FORWARD ENTRY RAFT HANGING BELOW CARRIER AND NOT ALLOWING GIRT BAR TO LOCK FOR ARMING ; / REPOSITIONED FORWARD ENTRY SLIDE IN THE SLIDE COMPARTMENT PER MT 725-61-06
EMERGENCY EXIT LIGHT (BETWEEN FORWARD FLIGHT ATTEND AND JUMPSEAT AND FORWARD ENTRY DOOR) COVER HAS FALLEN OFF. R&R FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT COVER PER MM 335103 & REPAIRED BROKEN WIRE AT LIGHT ASSY PER SWPM 203012.
CEILING OVERWING EXIT SIGN HAD LAMPS OUT. RELAMPED SIGN IAW AMM.
AFT ENTRY EMERGENCY EXIT LIGHT MODULE INOP. R&R LIGHT IAW WDM & AMM.
L1 DOOR LOWER FORWARD RETAINER STRIP ON DOOR FRAME IS CRACKED. / REMOVED AND REPLACED L1 DOOR LOWER FORWARD RETAINER STRIP ON DOOR FRAME IAW SRM 51-40-05-0G-0; BOEING DWG: 141A6240 REV:C
FORWARD CARGO COMPARTMENT FOUND R/H INTERCOSTAL CRACKED BETWEEN BS. 500A TO BS. 500B, RBL 25. / R&R BAFFLE IAW EA & DWG.
FORWARD CARGO BAFFLE FOUND CRACKED BETWEEN BS. 500C TO BS. 500D, RBL 26. / R&R BAFFLE IAW SRM AND DWG.
FORWARD CARGO AFT LOWER BULKHEAD SUPPORT ANGLE FOUND L/H Z ANGLE CORRODED AT BS. 500D, STR. 26L. / R&R ZEE-CHANNEL IAW SRM AND DWG.
CUSTOMER REQUEST SWA-ENG REQUIRES REPLACEMENT OF EXISTING REPAIR DOUBLER AT STA 807 + 5 RBL 13.84 WITH NEW REPAIR PER SRM / REMOVED AND REPLACE CARGO RAIL IAW SRM 53-00-53-2R-3 AT STA 747+8 - 887 RBL 13.84 AFT CARGO.
FORWARD CARGO L/H Z ANGLE CORRODED FOUND BETWEEN BS. 480+10 TO BS. 500D, LBL 25. R&R ZEE CHANNEL IAW SRM.
AFT CARGO INTERCOSTAL CORRODED ON OUTBOARD SIDE BETWEEN BS. 847 TO BS. 847+12, STR. 26L. / R&R INTERCOSTAL IAW SRM AND DWG.
AFT CARGO STRINGER SPLICE CORRODED AT BS. 887, STR 24L, ON OUTBOARD SIDE AT FASTENERS. / REPAIRED STRINGER PER SRM.
FWD CARGO COMPARTMENT FWD CARGO DOOR AFT SKATE ANGLE STA. 500 RBL 24 WL 155 HAS CORROSION IN SEVERAL AREAS. / FWD CARGO COMPARTMENT FWD CARGO DOOR AFT SKATE ANGLE REMOVED AND REPLACED MPN 143A8126U31 SI 753-1855 A TAG XM0847 BOEING DWG 143A8126 REV A AND SRM 51-40-02-0G-0 INSTALLED ON STA 500 RBL 24 WL 155
AFT CARGO COMP BS 727D RT SIDEWALL ANGLE CORROSION AROUND BOTTOM FASTNER HOLE ABOVE STR 25R. REMOVED 4EA NUT PLATES FROM R/H Z ANGLE AT BS 727D R/H (TO BE INSTALLED ON W/O X987523) ; REMOVED CORROSION UNDER NUT PLATES AT BS 727D R/H ZEE ANGLE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; FIG103, SRM 51-10-02-0G-0 PAR 6. REMOVED CORROSION FROM ATTACH ANGLE, FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW PART; INSTALLED NEW SIDEWALL ATTACH ANGLE BS 727D RT; IAW SRM 51-10-02-0G-0; B737 NDT PT4 51-00-00 PROC 2; SRM 53-00-53-1A-2; BOEING DWG#146A1220ID0053 REV-; SRM 51-40-02-0G-0; PAR4; DWG #146A9403 ID0003 REVD; SRM 51-40-05-0G-0 FIG 3 SHT 1 .
AFT CARGO COMP.STA 727 RH BULKHEAD ANGLE CORODED AROUND FASTNER HOLES BOTTOM 3' / REMOVED AND REPLACED ANGLE STA 727 R/H BULKHEAD IAW SRM 51-40-02-0G-0. AND DWG NO. 144A2600 REV:- REMOVED DAMAGED ON STA 727 IAW SRM 51-10-02-0G-0. EVAL MATERIAL LOSS ORIGINAL MATERIAL .040' REMAINING .033' LOSS .007' ALLOWED 10% OUT OF LIMITS IAW SRM 53-00-52-1A-2 FIG 103
AFT CARGO COMPARTMENT R/H Z-ANGLE CORRODED AROUND FASTENER HOLES BETWEEN BS. 727C TO BS. 767. R&R Z-CHANNEL IAW SRM AND DWG.
AFT CARGO COMP.STA 887 FLOOR PANEL ATTACHMENT STRAP CORRODED AROUND FASTNER HOLES / EVALUATED LIMITS OF AFT CARGO STA-887 FLR PNL ATTACHMENT STRAP TO FIND NO PUBLISHED LIMITS PER SRM REF- 53-00-53-1A-2 REMOVED AND REPLACED PART NO-146A9401439 IAW BOEING DWG- NO-146A7500 ID: 0061 REV:- AND BOEING SRM REF-51-40-05-0G-0 AND 51-40-01-0G-0
LEFT WING NR 6 SPOILER LOWER SURFACE DELAMINATED. R & R NR 6 SPOILER PER AMM.
AFT CARGO COMPARTMENT R/H FLOOR SHIELD CORRODED AT BS. 767, AROUND FASTENER HOLES. / R&R SHIELD IAW SRM AND DWG.
MAIN CABIN FLOORBOARD 241EF AFT CORNER CRUSHED. MARKED / REPAIRED MAIN CABIN FLOOR BOARD 241 EF AFT CORNER IAW B 737-700 SRM 53-00-50-2R-1 REV 68 53-00-50-2R-1 REV 68 AND NDT 51-00-05 (A36551) (A42411) (A09236)
AFT CARGO COMP.LAV TANK ACCESS BOTTOM SUPPORT BRACKET CRACKED LH STA 867 / REMOVED AND REPLACED SUPPORT BRACKET PN 149A8109U 114 ATAG A68260 FOR LAV. TANK ACCESS PANEL AFT CARGO L/H STA 867. IAW B-737 SRM 51-40-02-0G-0 AND DRAWING 149A8102 REV:-
MAIN CABIN FLOORBOARD 242DF CORNER CRUSHED. MARKED. / REPAIRED DAMAGE ON FAIRING 193CL. APPLIED RESIN SWEEP TO REPAIR AREA AND CURED. TAP TEST GOOD. RESTORED DECROTIVE FINISH. IAW B737-700 SRM 53-40-70-1A-1 REV 68; SRM 51-70-08-06-0 REV 68; SRM 53-40-70-1A-1 REV 68; SRM 51-70-08-0G-0 REV 68; SRM 51-30-10-06-0 REV 68; B737 AMM 51-21-99-300-801 REV 68
MAIN CABIN FLOORBOARD 242CF CORNER CRUSHED. MARKED. / REPAIRED DAMAGE ON FLOOR PANEL 242 CF. APPLIED POTTING COMPOUND AND WIRE. BONDED REPAIR PLIES AND CURED TAP TEST GOOD. IAW B737-700 SRM 53-00-50-2R-1 REV 68 SRM 53-00-50-2R-0 REV 68 A12438 A09236 A42411
AFT CARGO COMP.LH Z-ANGLE STA 727E+10-817 CORRODED AROUND FASTNER HOLES / REMOVED AND REPLACED L/H Z-ANGLE STA 727-847 IAW SRM 53-00-53-2R-5 AND DWG NO. 146A7500 REV: B. REMOVED DAMAGE ON Z-ANGLE IAW SRM 51-10-02-0G-0. EVALUATED DAMAGE IAW SRM 53-00-53-1A-2 FIG 103 DETAIL D REMOVED .022' ALLOWED .004 FOUND TO BE OUT OF LIMITS. PART NO. BAC 1496-377 707516
FWD CARGO. STA 500A; 2' BELOW STR 24L; ATTACH ANGLE HAS CORROSION / REMOVED CORRODED ATTACH ANGLE FWD CARGO STA. 500A 2' BELOW 24L AND INSTALLED NEW ATTACH ANGLE AS PER B737-700 SRM 51-40-02-0G-0 STEP 4B AND BAC DWG 417A2106 REV -
FORWARD CARGO Z-ANGLE BAFFLE CRACKED IN FORWARD UPPER CORNER AT BS. 500A+2, STR. 26L. / R&R BAFFLE IAW SRM & EA.
FORWARD CARGO LOWER BULKHEAD SUPPORT ANGLE CRACKED ON OUTBOARD EDGE, 1" FROM FORWARD EDGE AT BS. 500D, STR. 26L. / R&R ANGLE IAW SRM & DWG.
PASSENGER CABIN FLOOR STRUCTURE FLOOR BOARD HAT CHANNEL SUPPORT CRACKED AT BS. 520+16, BETWEEN LBL 0 TO LBL 4. / R&R SUPPORT IAW SRM AND DWG.
PASSENGER CABIN FLOOR STRUCTURE FLOOR BOARD HAT CHANNEL SUPPORT CRACKED AT BS. 520+16, BETWEEN RBL 0 TO RBL 4. / R&R SUPPORT IAW SRM AND DWG.
FORWARD CARGO Z-ANGLE BAFFLE CRACKED BETWEEN BS. 500 TO BS. 500A, STR. 26L, IN FORWARD UPPER CORNER. / R&R BAFFLE IAW SRM & DWG.
FORWARD CARGO ATTACH ANGLE ON FORWARD SIDE OF FRAME CRACKED COMMON TO Z-ANGLE BAFFLE BETWEEN BS. 500B TO BS. 500C, STR 26L. R&R BAFFLE IAW SRM & DWG.
FORWARD CARGO STRINGER CLIP GUSSET CRACKED IN UPPER RADIUS AT BS. 500D, STR. 19R. / R&R GUSSET IAW SRM AND DWG.
FORWARD CARGO ATTACH ANGLE ON FORWARD SIDE OF FRAME CRACKED COMMON TO Z-ANGLE BAFFLE BETWEEN BS. 500B TO BS. 500C, STR 26L. / R&R ANGLE IAW SRM & DWG.
FORWARD CARGO STRINGER CLIP GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET IAW DWG & SRM.
AFT CARGO COMP.FLOOR PANEL 140AF CORRODED AROUND PERIMETER SEVERAL LOCATIONS / REMOVED CORROSION FROM AFT CARGO FLOOR PANEL 140AF ORG MATERIAL .070 MATERIAL LOSS .010 REMAINING MATERIAL .060 FOUND TO BE OUT OF LIMITS IAW B737SRM 53-00-53-1A-1; 51-10-02-0G-0 PANEL REPLACED IAW B737-IPC 25-52-10-02 PANEL 140AF TO BE INSTALLED ON CARD JPANEL-141-CLOSE
AFT CARGO COMP.SIDEWALL TO FLOOR STRIPS CORRODED ON BACK SIDE / LOCATED AND DRILLED / COUNTERSUNK NEW CAP STRIP PN# 453A2611-3 IAW BOEING 737-700 ENGINEERING DRAWING # 453A2611 IN THE AFT CARGO COMPARTMENT PART REPLACED TAG#WN0704
AFT CARGO COMP.SIDEALL AND FLOOR STRIP STA.887-947 CORRODED ON BACK SIDE / REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR CAP STRIP FROM STA 887 TO STA 947 RBL I.A.W B-737-700 SRM 51-40-02-0G-0. P/N:7252699; VERFIED PART AS PER B-737-700 IPC 25-52-10-02; CAP STRIP P/N: ISSUE TAG:WN704
AFT CARGO COMP.THRESHOLD WEB TOP FWD PLATE CORRODED BACK SIDE / REPLACED SCUFF PLATE WITH NEW PART # 453A2611-2 IAW BOEING 737-700 SRM 53-60-53-01-1 REV 68 TAG A82985
FWD CARGO. STA 500D; 1' O/B OF STR 26L; CURVED BULKHEAD SUPPORT ANTLE HAS CORROSION ON TOP SIDE AND EVIDENCE OF CORROSION BETWEEN ANGLE AND Z-ANGLE / REMOVED DAMAGED CURVED BULKHEAD SUPPORT ANGLE; FWD CARGO STA 500D 'L/H SIDE.' INSTALLED NEW=30 CURVED BULKHEAD SUPPORT ANGLE IAW DRAWING 143A4981 REV:- GBB05
FWD CARGO. STA 500D; 3' O/B OF STR 26R; CURVED BULKHED SUPPORT ANGLE HAS CORROSION ON FWD VERTICAL FLANGE AND LOWER SIDE OF HORIZONTAL FLANGE / REMOVED DAMAGED CURVED BULKHEAD SUPPORT ANGLE FWD CARGO; STA 500D. IAW B-737 SRM 51-40-02-0G-0. INSTALLED NEW SUPPORT ANGLE PN 143A9485-34 ATAG GS1291. IAW DRAWING PN 143A9481 REV:-. 'RIGHT HAND SIDE'
FWD CARGO; STA 500A; 1' ABOVE STR 24L; ATTACH ANGLE HAS CORROSION ON UPPER SURFACE / REMOVED CORRODED ATTACH ANGLE FWD CARGO STA. 500A 1' ABOVE $-24L AND INSTALLED NEW ATTACHED ANGLE AS PER B737-700 SRM 51-40-02-0G-0 STEP 4B BAC DWG 417A2106 REV -.
FWD CARGO; STA 440 STR 22L; TIE DOWN PLATE HAS CORROSION AROUND NUT PLATE HOLES / BLENDED DAMAGED TIE DOWN PLATE STA 440; STR 22L IAW B737 SRM 51-10-02-0G-0 PAR 15 LIMITS FOR TIE DOWN PLATE WERE NOT FOUND ON B737 SRM 53-00-53-1A-2 AD 2. REMOVED; FABRICATED AND INSTALLED TIE DOWN PLATE IAW BOEING DRAWING 143A9403 REV- AND B737 SRM 51-40-02-0G-0 PAR 4 AND 7.
FWD CARGO; STA 440; STR 23L; TIE DOWN PLATE HAS CORROSION AT NUT PLATE HOLES / BLENDED DAMAGED TIE DOWN PLATE STA 440; STR 23L IAW B737 SRM 51-10-02-0G-0 PAR 15. LIMITS FOR TIE DOWN PLATE WERE NOT FOUND ON B737 SRM 53-00-53-1A-2 AD2. REMOVED; FABRICATED AND INSTALLED TIE DOWN PLATE IAW BOEING DRAWING: 143A9403 REV A. AND B737 SRM
FWD CARGO; STA 440; STR 25L; TIE DOWN PLATE HAS CORROSION AT NUT PLATE HOLES / REPLACED CORRODED TIE DOWN PLATE ON FWD CARGO STA 440; STR 25L I.A.W B737-700 SRM 51-40-05 & BOEING DWG # 143A7550 TY: DWG; ID: 0001 & REV:E.
PASSENGER CABIN COMP.L1 DOOR WAY THRESHOLD MIDDLE ANGLE CORRODED AT AFT FASTNER HOLES / REMOVED CORROSION AT MAIN CABIN L1 DOOR WAY THRESHOLD MIDDLE ANGLE I-A-W SRM 53-10-15-1A-1. VERIFIED MATERIAL LOSS ORIGINAL.063 REMOVED .013 REMAIN .050 ALLOWABLE 10% MAX FOUND OUT OF LIMITS USED AAR TOOL #36646 DUE 02OCT19 I-A-W SRM 53-10-15-1A-1 AND 53-10-15-01-1 REMOVED ZEE ANGLE CHORD I-A-W SRM 51-40-02-0G-00. DRILLED NEW ANGLEI-A-W 51-40-05-0G-00 AND BOEING DWG 141A8110; INSTALLED NEW ZEE ANGLE CHORD I-A-W SRM 51-40-02-0G-00 AND BOEING DRAWING 141A8110
UPPER ANGLE OF LONGITUDINAL FLOOR SUPPORT CRACKED AT BS. 927+9, BL 0. R&R ANGLE IAW SRM AND DWG.
R2 DOOR INNER CREASE BEAM ANGLE CORRODED BETWEEN BS. 947 TO BS. 986, ON UPPER SURFACE. / R&R CREASE BEAM IAW SRM AND DWG.
PASSENGER CABIN FLOOR PANEL 241ABF; UPPER FACE SHEET IS MISSING FIBERS; MARKED IN BLACK. / REPAIRED UPPER FACESHEET MISSING FIBERS ON FLOORBOARD PANEL (241 ABF) I/A/W B737-700 SRM 53-00-50-R2-1 (3) A-N-(REV 68)
PASSENGER CABIN FLOOR PANEL 241AAF; UPPER FACE SHEET HAS MISSING FIBERS / REPAIRED UPPER FACE SHEET MISSING FIBERS TO FLOOR BOARD PANEL (241 AAF) WITH WET LAY UP REPAIR IAW B 737-700 SRM 53-00-50-+2R-1 (3) A-N (REV 68)
PASSENGER CABIN FLOOR PANEL 241XF; UPPER FACE SHEET IS MISSING FIBERS; MARKED IN BLACK. / REPAIRED FLOORBOARD 241XE UPPER FACE SHEET IAW SRM 53-00-50-2R-1; PG'S 1; 2; STEPS 3(A-M)
PASSENGER CABIN FLOOR PANEL 241ABF, FORWARD OUTBOARD SIDE CRACKED 8" FROM OUTBOARD EDGE, BETWEEN BS. 887 TO BS. 1016. / REPAIRED FLOOR BOARD PANEL 241ABF IAW SRM.
UPPER AND LOWER SURFACE OF FLOOR BEAM UPPER T-CAP CORRODED AROUND NUTPLATE HOLES AT BS. 986, BETWEEN RBL 30 TO RBL 45. REPAIRED FLOOR BEAM IAW EA.
PASSENGER CABIN FLOOR PANEL 242UF; UPPER FACE SHEET IS MISSING FIBERS; MARKED IN BLACK. / REPAIRED FLOOR BOARD PANEL 242 UF UPPER FACE IAW SRM 53-00-50-2R-1 PGS 1 2 STEPS 3 (A-M)
FWD CARGO COMP.SCUFF PLATE FWD CORNER CRACKED / REMOVED CORNER ROUTED CORNER TO BACKSHOPFOR REPAIR. BACKSHOP WELDED FWD CARGO SCUFF PLATE FWD CORNER I/A/W EA 1-A53-2076 REV. II REINSTALLED FWD CORNER SCUFF PLATE I/A/W EA 1-A53-2076 REV. II AND 737 AMM 53-11-02-420-801
FWD CARGO COMP.PANEL RH CAP STRIPS CORRODED BACK SIDE AROUND FASTNER HOLES / RECEIVED AND VERIFIED NEW FWD CARGO PANEL CAP STRIPS P/N 453A1611-7 IAW 737 IPC 25-52-10-01 ITEM 365 AND P/N 453A1611-12 IAW 737 IPC 25-52-10-01 ITEM 360; INSTALL IAW 737 AMM 25-52-10-400-801 A-TAG #GS1304 FOR 453A1611-7 A TAG # WN7374 FOR 453A1611-12
AFT CARGO DOOR INTERIOR SKIN CORRODED AT LWR FWD CORNER / REMOVED CORROSION FROM AFT CARGO DOOR INTERIOR SKIN AT FWD LWR CORNER IAW B 737 SRM 51-10-02-0G-0 FOUND DAMAGE OUT OF LIMITS DUE TO PROXIMITY TO HOLE IAW B 737 SRM 52-30-01-1A-1 REPAIRED IAW EA 190542 REV P1 & IR & SWA EA 1-752-2596 REV IR
RT HORIZONTAL STABILIZER 2ND FROM FRONT VERTICAL STIFFENER CRACKED ON RIB AT STAB. STA. 120.3. REPAIRED STABILIZER IAW SRM.
AFT CARGO DOOR INTERIOR SKIN CORRODED AT LOWER AFT CORNER. REPAIRED SKIN IAW SRM AND EA.
L/H HORIZONTAL STABILIZER, 4TH FROM FRONT VERTICAL STIFFENER CRACKED ON RIB AT STAB. STA. 120.3. / REPAIRED STIFFENER IAW SRM.
L/H HORIZONTAL STABILIZER, 3RD FROM FRONT VERTICAL STIFFENER CRACKED ON RIB AT STAB. STA. 120.3. / REPAIRED STIFFENER IAW SRM.
L/H HORIZONTAL STABILIZER, 2ND FROM FRONT VERTICAL STIFFENER CRACKED ON RIB AT STAB. STA. 120.3. / REPAIRED VERTICAL STIFFENER IAW SRM.
RT HORIZONTAL STABILIZER, 3RD FROM FRONT VERTICAL STIFFENER CRACKED ON RIB AT STAB. STA. 120.3. REPAIRED STABILIZER IAW SRM.
R1 DOOR SLIDE GIRT BAR HOLDER LOOSE. / SECURED GIRT BAR HOLDER PER SRM.
AFT GALLEY LT SIDE EXIT SIGN LENS BROKEN. R&R LENS PER AMM.
EMERGENCY LIGHT LENS CRACKED FORWARD GALLEY LT SIDE ATTACHED TO LAVATORY BULKHEAD. R&R LENS IAW AMM.
RT PHOTOLUMINESCENT STRIP DAMAGED AT 1ST SECTION. R&R STRIP PER AMM.
L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER (DID NOT DEPLOY). REINSTALLED SLIDE ASSY PER MT.
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PER AMM.
R1 DOOR SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED SLIDE PER SIP.
R1 DOOR SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED SLIDE PER MM.
LEFT EXTERNAL EMERGENCY LIGHT AFT OF NR 1 ENGINE INOPERATIVE. REPLACED THE LAMP IAW AMM.
L1 DOOR SLIDE OUT OF POSITION. ADJUSTED THE SLIDE IAW MM.
L2 EXIT SIGN COVER LENS MISSING. INSTALLED COVER IAW AMM.
#6 FLAP TRACK MID FAIRING; HAS A CRACK AT THE LOWER AFT END NEAR THE NUTPLATE COMMON TO FAIRING TAILCONE. / REMOVED #6 CRACKED MID FAIRING AND REPLACED WITH A SERVICEABLE #6 FAIRING I.A.W. B737 AMM 27-51-18-000-801 AND 27-51-18-000-802 AND 27-51-18-400-802 AND 27-51-18-400-801 AND ADJUSTED I.A.W. AMM 27-51-18-820-801 POS #6 TAG/GRB/NO. P/N OFF 113A9350-2 S/N OFF 1695 P/N ON 113A 9350-2 S/N ON K1560
LT WING NR 2 SLAT ACTUATOR ATTACH POINT SKIN CRACKED. REPAIRED SKIN IAW SRM.
RT WING NR 7 SLAT LOWER SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED SKIN IAW SRM.
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT M1674. R & R BATTERY PACK IAW DWG.
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT M1675. R & R BATTERY PACK IAW DWG.
R2 DOOR SLIDE COVER LOOSE. R & R COVER ASSEMBLY IAW MM.
L2 DOOR SLIDE COVER LOOSE. R & R COVER ASSEMBLY IAW MM.
R1 DOOR SLIDE INADVERTENTLY FELL OUT OF CASE, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED SLIDE IAW MT.
LEFT WING TO BODY FAIRING EMER EXIT LIGHT LENS AFT DIRTY. CLEANED LENS IAW AMM.
EMERGENCY LIGHT IN AFT DROP DOWN CEILING PANEL INOPERATIVE. R & R LIGHT IAW AMM.
EXTERIOR EMER EXIT LIGHT AFT OF LT WING TO BODY FAIRING INOPERATIVE. RELAMPED LIGHT IAW AMM.
R2 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
LEFT EMER EXIT LIGHT INOPERATIVE AT ROW 6. RELAMPED LIGHT IAW AMM.
RIGHT EMER EXIT LIGHT INOPERATIVE BETWEEN ROW 8 - 9. RELAMPED LIGHT IAW AMM.
RIGHT OVERWING EMER EXIT DOOR INTERIOR HANDLE PULL COVER BROKEN. R & R HANDLE IAW SRM.
FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 847, STRINGER 25L. R & R SUPPORT IAW SRM.
SHEAR TIE CORRODED AT BS 767, BETWEEN STRINGER 26L TO 27L. R & R SHEAR TIE IAW SRM.
INTERCOSTAL CORRODED BETWEEN BS 767 TO BS 787, BETWEEN STRINGER 25R TO 26R. R & R INTERCOSTAL IAW SRM.
AFT CARGO INTERCOSTAL CORRODED BETWEEN BS 847 TO 855.5, RBL 19 UPPER & LOWER SURFACE OF INNER CHORD. R & R INTERCOSTAL IAW DWG & SRM.
AFT CARGO NUTPLATE STRIP CORRODED BETWEEN BS 841 TO 847, RBL 19, UPPER & LOWER SURFACE. R & R STRIP IAW SRM & DWG.
AFT CARGO INTERCOSTAL CORRODED BETWEEN BS 785 TO 789, STRINGER 25R. R & R INTERCOSTAL IAW DWG & SRM.
AFT CARGO INTERCOSTAL CORRODED BETWEEN BS 847 TO 855.5, RBL 24, UPPER & LOWER SURFACE OF INNER CHORD. R & R INTERCOSTAL IAW DWG & SRM.
AFT CARGO INTERCOSTAL CORRODED BETWEEN BS 789 TO 795, RBL 19. R & R INTERCOSTAL IAW DWG.
STRINGER CLIP CORRODED AT BS 747, STRINGER 26R. R & R STRINGER CLIP IAW DWG.
STRINGER CLIP CORRODED AT BS 767, STRINGER 26R. R & R STRINGER CLIP IAW DWG.
AFT CARGO COMPARTMENT SUPPORT BRACKET CORRODED AT BS 727E, STRINGER 27L. REPAIRED BRACKET IAW DWG & SRM. REPAIRED BRACKET IAW DWG & SRM.
AFT CARGO COMPARTMENT CORRODED FLOOR TO SIDEWALL SUPPORT BETWEEN BS 727E TO 727D, RIGHT SIDE. R & R SUPPORT IAW SRM.
AFT CARGO COMPARTMENT INTERCOSTAL CORRODED AT BS 727B, BETWEEN STRINGER 26L TO 25L. R & R INTERCOSTAL IAW DWG & SRM.
AFT CARGO COMPARTMENT SUPPORT BRACKET CLIP CORRODED AT BS 767, STRINGER 27L. R & R CLIP IAW DWG & SRM.
AFT CARGO COMPARTMENT SIDEWALL MOUNT BRACKET CORRODED AT BS 887, BETWEEN STRINGER 27L TO 26L. R & R BRACKET ASSEMBLY IAW SRM.
SUPPORT BRACKET CORRODED AT BS 727, STRINGER 27L. R & R STRINGER CLIP IAW SRM & DWG.
AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 887, BETWEEN STRINGER 25R - 24R. REPAIRED SUPPORT IAW SRM.
AFT CARGO COMPARTMENT FLOOR TO SIDEWALL MOUNT BRACKET CORRODED BETWEEN BS 867 TO 887, STRINGER 25R. REMOVED SUPPORT IAW SRM.
AFT CARGO COMPARTMENT SUPPORT BRACKET CORRODED AT BS 807, STRINGER 27R. REPAIRED BRACKET IAW SRM & DWG.
AFT CARGO COMPARTMENT SUPPORT BRACKET CORRODED AT BS 787, STRINGER 27L. R & R STRINGER CLIP IAW SRM & DWG.
AFT CARGO COMPARTMENT CORRODED SUPPORT BRACKET AT BS 747, STRINGER 27L. R & R STRINGER CLIP IAW SRM & DWG.
AFT CARGO COMPARTMENT FORWARD SUPPORT BRACKET CORRODED BETWEEN BS 727E TO 727D, STRINGER 27L. R & R STRINGER CLIP IAW SRM & DWG.
AFT CARGO COMPARTMENT CORRODED BETWEEN BS 727E TO BS 727D, STRINGER 27L. R & R STRINGER CLIP IAW SRM & DWG.
AFT CARGO COMPARTMENT SUPPORT BRACKET CORRODED AT BS 727D, STRINGER 27L. R & R STRINGER CLIP IAW SRM & DWG.
AFT CARGO COMPARTMENT FLOOR TO SIDEWALL BRACKET CORRODED BETWEEN BS 727C TO 727B. R & R SUPPORT IAW SRM.
AFT CARGO COMPARTMENT SUPPORT BRACKET CORRODED AT BS 727C, STRINGER 27L. R & R CLIP IAW SRM & DWG.
AFT CARGO BAY INTERCOSTAL CORRODED AT BS 747, BETWEEN STRINGER 25 - 26R. R & R THE INTERCOSTAL IAW SRM.
STRINGER CLIP CORRODED AT BS 847, STRINGER 27L. R & R THE STRINGER CLIP IAW SRM & DWG.
AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS 847 TO 867, BETWEEN STRINGER 25 - 26L. R & R INTERCOSTAL IAW SRM.
AFT CARGO COMPARTMENT SPLICE STRAP CORRODED BETWEEN BS 887 TO 890, BETWEEN STRINGER 26 - 27L. REPAIRED STRAP IAW EA & ER.
INTERCOSTAL CORRODED AT BS 727B, BETWEEN STRINGER 26 - 27R. R & R INTERCOSTAL IAW SRM.
FUSELAGE INTERCOSTAL CORRODED AT BS 867 - 887, STRINGER 25-26L. R & R THE INTERCOSTAL IAW SRM.
STRINGER CLIP CORRODED AT BS 827, STRINGER 27L. R & R THE STRINGER CLIP IAW SRM.
AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 907, BETWEEN STRINGER 27L - 26L. R & R SHEAR TIE IAW SRM & DWG.
AFT CARGO COMPARTMENT FLOOR TO SIDEWALL BRACKET CORRODED BETWEEN BS 787 TO 767, BETWEEN STRINGER 25R TO 26R. R & R BRACKET IAW SRM.
AFT CARGO COMPARTMENT SEAL STRAP CORRODED BETWEEN BS 847 TO 787R. R & R SEAL STRAP IAW SRM & DWG.
EXTERNAL FUSELAGE LOWER LOBE BILGE DRAIN SUPPORT PLATE CORRODED AT BS 727+4, RBL 10. REPAIRED PLATE IAW SRM & DWG.
AFT CARGO BAY RT SIDEWALL SUPPORT CORRODED AT BS 727D BETWEEN STRINGER 23R - 24R. R & R SUPPORT IAW SRM & DWG.
AFT CARGO BAY SIDEWALL SUPPORT CORRODED AT BS 787, BETWEEN STRINGER 23L - 25L. REPAIRED SUPPORT IAW SRM & DWG.
EXTERNAL FUSELAGE LOWER LOBE BILGE DRAIN SUPPORT PLATE CORRODED AT BS 727+4, BL 0. R & R PLATE IAW SRM & DWG.
EXTERNAL FUSELAGE LOWER LOBE BILGE DRAIN SUPPORT PLATE CORRODED AT BS 727+4, LBL 10. REPAIRED PLATE IAW SRM & DWG.
FORWARD CARGO BAY, LEFT FLOOR TO SIDEWALL SUPPORT, CRACKED AT BS 420, LBL 24. REPAIRED SUPPORT IAW SRM.
LEFT HORIZONTAL STABILIZER RIB 2ND STIFFENER CRACKED AT BS 92.70 AT LOWER END. REPAIRED RIB IAW SRM.
FUSELAGE FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 360, STRINGER 8L. REPAIRED FRAME IAW EA.
FLOORBEAM CRACKED AT BS 727B, RBL 25.75. REPAIRED BEAM IAW EA.
FLOORBEAM CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM IAW EA.
FLOORBEAM CRACKED AT BS 727B, LBL 25.5. REPAIRED BEAM IAW EA.
FORWARD SEAT TRACK HOLES CRACKED AT BS 727B, LBL 45.5. OTBD AFT & INBD AFT. REPAIRED SEAT TRACK IAW ER & EA.