N476WN
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
POSSIBLE CRACK INDICATION ON LT OTBD AFT FLAP INBOARD CLOSURE RIB UPPER HOLE AT 7 O'CLOCK POSITION. R & R T/E AFT FLAP LT OTBD IAW AMM 27-51-22, NO DEFECTS NOTED.
INOPERATIVE EMERGENCY LIGHTS 2 (EA) OVERHEAD BINS 5 AND 6. REPLACED FUSES ON BOTH POWER SUPPLIES M1668 AND M1670 IAW AMM 33-51-06-960-804. TESTED OK;
TWO INOPERATIVE EMERGENCY LIGHTS OVERHEAD BINS 5 AND 6. REPLACED FUSES ON BOTH POWER SUPPLIES M1668 AND M1670 IAW AMM 33-51-06-960-804. TESTED OK.
DELAMINATION ON INBOARD CORNER ON AFT FLAP OUTBOARD LT WING. EVALUATED DAMAGE ON INBOARD CORNER OF OUTBOARD AFT FLAP AT LT WING IAW SRM 57-53-01-2R-16. FOR REMOVE AND INSTALL AFT FLAP OUTBOARD LT WING PROCEDURE SEE TTG8Q01CRW1P
CRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 250 AT LT WING. PERFORMED VISUAL INSPECTION IAW SRM 51-10-04-0G-0 ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 250 AT LT WING AND NOT FOUND CRACK ONLY BROKEN FASTENER HEAD (2/EA) REMOVED AND INSTALLED FASTENER IAW SRM 51-40-02-0G-0, AND DWG 115A2001, SHEET 29, REV-.
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 219 AT LT WING. REPLACED CORRUGATED PLATE LOC. ON TRAILING EDGE IRSS 219 AT LT WING IAW SRM 51-40-02-0G-0 AND 51-10-02-0G-0, ITEM 9.
CRACKED ANGLE TRAILING EDGE LOCATED ORSS 271 RT WING. REPLACED ANGLE T/E LOCATED ORSS 271 RT WING IAW SRM 51-40-02-0G-0, DWG 115A2930, SHEET 6, REV-.
CRACKED CORRUGATED PLATE T/E LOCATED ORSS 261 AT RT WING. PERFORMED VISUAL INSPECTION IAW SRM 51-10-04 ON CORRUGATED PLATE T/E LOCATED ORSS 261 AT RT WING AND NOT FOUND CRACK ONLY BROKEN FASTENER HEAD (1 E/A). REMOVED AND INSTALLED FASTENER IAW SRM 51-40-02, AND DWG 115A2001, SHEET 29, REV-.
CRACK LEADING EDGE RIB LOCATED LE STA 86.66 RT HORIZONTAL STAB. REPLACED LEADING EDGE RIB LOCATED ON LE BS 86.66 RT HORIZONTAL STAB IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 186A1001, SHEET 10, REV A.
ELONGATED HOLE ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
CRACKED SUPPORT ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R PASSENGER CABIN. REPLACED SUPPORT ANGLE BS 867 BETWEEN S2R TO S3R PASSENGER CABIN IAW SRM 51-40-02-0G-0, & DWG 146A7901, SHEET 58, REV-.
DETERIORATED PHOTOLUMINESCENT STRIP (5EA) RH SIDE. REPLACED PHOTOLUMINESCENT STRIP (5EA) RT SIDE IAW AMM 33-51-15-400-802.
DETERIORATED PHOTOLUMINESCENT STRIP (5EA) LT SIDE. REPLACED PHOTOLUMINESCENT STRIP (5EA) LT SIDE IAW AMM 33-51-15-400-802.
CRACKED ANGLE ACCESS PANEL 551FB AT LT WING. REPLACED ANGLE ON ACCESS PANEL 551FB AT LT WING IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 115A2710, SHEET 6, REV B.
BROKEN EMERGENCY LENS OVERHEAD STOWAGE BIN ON POSITION (2) (3) (4) (5) (6) (7) (8) (10) RT SIDE IN PASSENGER CABIN. REPLACED EMERGENCY LENS OVERHEAD STOWAGE BIN ON POSITION (2); (3); (4); (5); (6); (7); (8); (10) IAW AMM 33-51-03-960-801, STEP 2.D (3) (A), & (C).
CRACKED AFT CORNER SCUFF PLATE AT AFT CARGO BAY. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.
BROKEN EMERGENCY LENS OVERHEAD STOWAGE BIN ON POSITION (1) (3) (4) (5) (6) (7) (8) (9) (11) LT SIDE AT PASSENGER CABIN. REPLACED EMERGENCY LENS OVERHEAD STOWAGE BIN ON POSITION (1) (3) (4) (5) (6) (7) (8) (9) & (11) LT SIDE AT PASSENGER CABIN IAW AMM 33-51-03-960-801, STEP 2.D (3) (A) & (C).
CRACK INDICATION FOUND ON LT HORIZONTAL STAB LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 8 INCH. FROM REAR SPAR. INBD SIDE OF RIB. ON STEP 7 AND 8. PERFORMED REPAIR ON LT HORIZONTAL STAB LOWER SKIN PANEL IAW SRM 55-10-01-2R-11, REPAIR 11.
CRACK ANGLE FLOOR STRUCTURE LOCATED BS 694 AND RBL 24.82 AT PASSENGER CABIN. REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 694 TO RBL 24.82 AT PASSENGER CABIN IAW SRM 51-40-02-0G-0, AND DRAWING 111A6000, SHEET 208, REV-, AND SRM 51-10-02-0G-0, ITEM 9.
CRACKED ANGLE FLOOR STRUCTURE LOCATED BS 694 LBL 0.07 IN THE PASSENGER CABIN. REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 694 BTW LBL 24.82 TO LBL 0.07 IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0, PARAGRAPH 9, AND DWG 273A9110, SHEET 6, REV A.
CRACK FLOOR STRUCTURE BREAK PANEL ON BS 540 BTW LBL 0.07 TO RBL 24.82. REPLACED BREAK PANEL LOCATED ON FLOOR STRUCTURE BS 540 AND BTW LBL0 TO RBL 24.82 IAW DWG 143A0060, SHEET 36, REV A, SRM 51-40-02-0G-0, & SRM 51-10-02-0G-0, PARAGRAPH 9.
CRACKED VAPOR BARRIER WEB RT SIDE AT BS 663.75 MAIN WHEEL WELL. REPAIRED VAPOR BARRIER WEB RT SIDE AT BS 663.75 MAIN WHEEL WELL COMPARTMENT IAW SRM 57-10-10-2R-2, REPAIR 2.
CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT LBL 31 BETWEEN BS 663 TO BS 675 IN THE MAIN WHEEL WELL. PERFORMED A PERMANENT REPAIR LOC ON HORIZONTAL PRESSURE DECK WEB IAW SRM 53-40-51-2R-2, REPAIR 2.
CRACK AROUND FASTENER LOWER SURFACE LEADING EDGE SLAT NOSE SKIN AT THE ACTUATOR FITTING SLAT 6 AT RT WING. EVALUATED LOWER SURFACE LEADING EDGE SLAT NOSE SKIN AT THE ACTUATOR FITTING SLAT 6 (SLAT STATION 202.45) AT RT WING AND FOUND OUT LIMITS DUE TO CRACK IS LOCATED IN THE AREA NOSE BEAM. IAW SRM 57-42-01-1A-1 ALLOWABLE DAMAGE 1. STEP 4.A(1); FIGURE 105; DETAIL A. SLAT 6. REPLACEMENT AND PART REQUIREMENT TRANSACTION OF THE SLAT 6 IS ACCOMPLISEHED ON FAULT [TTG8Q01CFLAH].
CRACKED LOWER SURFACE OF LEADING EDGE SLAT 5 NOSE SKIN AT ACTUATOR LOC. AROUND FASTENER AT RT WING. PERFORMED PERMANENT REPAIR ON LOWER SURFACE LEADING EDGE SLAT NOSE SKIN AT THE ACTUATOR FITTING SLAT 5 BTW SS 75 TO SS 95 RT WING IAW SRM 57-42-01-2R-8, REPAIR 8, ALTERNATIVE 1, FIGURE 202, SHEET 4.
AFT FLIGHT ATTENDANT OVERHEAD CALL LIGHT INOPERATIVE. REMOVED AND REPLACED AFT EXIT SIGN ASSY IAW AMM 33-51-01. OPS CHECKED GOOD.
FA REPORTED AFTER ENTRY DOOR HANDLE LOOSE. TORQUED AND SAFETIED AFT ENTRY DOOR INTERIOR HANDLE IAW AMM 52-13-00.
TRAILING EDGE FLAP SPLIT ON LANDING CONFIGURATION. REMOVED AND REPLACED THE NR 3 FLAP TRANSMISSION INBD COUPLING SLEEVE & HALF IAW AMM 27-51-31 & LT POSITION TRANSMITTER IAW AMM 27-58-01. OP CHECKED GOOD.
TRAILING EDGE FLAP SPLIT ON LANDING CONFIGURATION. REMOVED LT FLAP POSITION TRANSMITTER IAW AMM 27-58-01. REMOVED AND REPLACED THE NR 3 FLAP TRANSMISSION INBD COUPLING SLEEVE & HALF IAW AMM 27-51-31, & LT POSITION TRANSMITTER IAW AMM 27-58-01. OP CHECK GOOD.
GIRT BAR FWD SERVICE DOOR NOT SECURE IN PLACE ON LEFT SIDE. REPACKED SLIDE AND GIRT BAR PER AMM 25-66-01. OPS CHECK GOOD.
GIRT BAR FWD SERVICE DOOR NOT SECURE IN PLACE ON LEFT SIDE. REPACKED SLIDE AND GIRT BAR PER AMM 25-66-01. OPS CHECK GOOD
CRACKED SHEETMETAL AT LOWER CUTOUT OF EXTERNAL ACCESS POWER DOOR. REPAIRED DAMAGED LOCATION PER SRM 53-10-15-2R-4. PERFORMED HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE TRIM OUT EDGE IAW NDT PART 6; 51-00-00; PROCEDURE 23. NO DEFECTS NOTED.
AFT MEGAPHONE HAS BROKEN HANDLE. REMOVED AND REPLACED AFT MEGAPHONE PER AMM 25-64-00.
FWD MEGAPHONE INOPERATIVE.
FWD ENTRY DOOR ESCAPE SLIDE FELLOUT OF POSITION<[01] C/W MT-725-61-06<BR>RESECURED SLIDE PACK
MID-CABIN OVERHEAD EXIT SIGN COVER DETACHED <[01]. RESECURRED OVERWING EMERGENCY EXIT SIGN PER AMM 33-51-00.
#1 PYLON FARING FORWARD CASTING INBD HILOK FASTENER HOLES COMMON TO INTERCOSTAL PULLED THROUGH.<[01] REMOVED AND REPLACED STRUCT FAIRING FWD FITTING PER SRM 51-10-02 AND SRM 51-40-02;[02] INSPECTED WORK ABOVE;[03] C/W RII INSPECTION. OF INSTALLED FAIRING FWD T SUPPORT ANGLE.
FWD ENTRY DOOR SLIDE RETENTION CLIP MISSING ON LEFT SIDE.<[01] REPOSITIONED GIRT BAR RETAINER AND REPLACED MISSING FASTENER REF IPC 25-66-00-14 AND SIP.
FOUND CRACK ON TRF PN 340-166-210-0 SN PA179695 STRUT 16 AREA C2 THAT MEASURES .375' IN LENGTH.<[01] C/W EA M-21-172-00810 TRIGGERING TRF MOUNT INSPECTION 7256-I-14340 FOR LARGEST CUMULATED CRACK FINDINGS FROM 0.28 INCH TO LESS THAN 0.39 INCH IN LENGTH
R2 DOOR GIRT LOW; CATCHES DOOR JAM WHEN CLOSING<[01] REPACKED R2 SLIDE PER MT 725-61-06
CUSTOMER WALK: R2 DOOR SLIDE SKIRT HITS HARD ON DOOR THRESHOLD WHEN DOOR OPEN/CLOSED<[01] RE-ADJUSTED VELCRO STRIPS AT R2 DOOR SLIDE AS PER AMM 26-66-01-200-802;[02] CORRECTION STEP #1<BR>RE-ADJUSTED VELCRO STRIPS AT R2 DOOR SLIDE AS PER AMM 25-66-01-200-802;[03] VERIFIED STEP 2.
SEVERAL EXTERIOR AND INTERIOR EMERGENCY LIGHTS INOPERATIVE.<[01] PERFORMED TROUBLESHOOTING OF EMERGENCY EXIT LIGHTS - MID CIRCUIT AND FOUND BATTERY PACK DEFECTIVE. FOUND ALSO OPEN CIRCUIT FROM CONNECTOR D10716 POSITION 15 AND POSITION 16 TO GROUND THROUGH L1065 AISLE LIGHT. REFERENCE B737 SSM 33-51-13 PAGE 101 SHEET 1. WIRING CHECK AND OPERATIONAL TEST AT LIGHT L548 PASSED. CONTINUE T/S. REPLACED BATTERY PACK AT M1670 POWER SUPPLY ASSEMBLY. REFERENCE B737 AMM 33-51-06-960-805. CONTINUED TROUBLESHOOTING OF EMERGENCY EXIT LIGHTS - MID CIRCUIT AND FOUND CONNECTOR D11100 AND CONNECTOR D11326 DISCONNECTED. RECONNECTED AND RESECURED BOTH CONNECTORS PER REF. WDM 33-51-13. PERFORMED INSTALLATION TEST PER REF. AMM. 33-51-06-960-805. TEST FOUND NORMAL. PERFORMED BATTERY PACK INSTALLATION TEST PER REF. AMM. 33-51-06-960-805. TEST FOUND NORMAL.;[02] VERIFIED STEP 1.
LAVATORY B EMERGENCY EXIT LIGHT ASSY. IS DAMAGED.<[01] REMOVED AND REPLACED LAVATORY B EMERGENCY EXIT LIGHT ASSY; REF B737-700 AMM 33-51-01-960-802.;[02] VERIFIED STEP 1 <BR>AUDIT C/W FER MPM 52-02-02
RH HORIZONTAL LEADING EDGE PANEL 341B RIB #10 FOUND CRACKED.<[01] SUMMARY=<BR>APPLIED STRIPPER TO RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB #10 FOR NDT TEST AS PER B 737 AMM 51-21-11-150-801.<BR>PERFORMED HFEC INSP. ON RH HORIZONTAL L/E PANEL 341B RIB #10 IAW B737 NDT PART 6 51-00-00 PROC. 23. NO CRACKS NOTED; EQUIP: NORTEC 600 B/C 166317 CAL DUE: 10/24.<BR>TREATED AND PRIMED RIB #10 AS REQUIRED AS PER B 737 AMM 51-21-41-370-80 & AMM 51-21-72-370-804.;[02] CORRECTION FOR SUMMARY TO ALSO READ AMM 51-21-41-370-803.;[03] VERIFIED STEP 1. <BR><BR>VERIFIED CORRECTION MADE TO AMM REF. IN STEP 2.
RH HORIZONTAL LEADING EDGE PANEL 341B RIB #6 FOUND CRACKED.<[01] ***SUMMARY**<BR>REMOVED RIGHT HORIZONTAL STABILIZER L/E #6 RIB AS PER B 737 SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED NEW RIB AS PER B 737 SRM 51-40-05-0G-0.<BR>INSTALLED RH HORIZONTAL LEADING EDGE RIB #6 AS PER B-737 SRM 51-40-02-0G-0 & DWG 186A1306.<BR>MIXED SEALANT 0870B002BM<BR>10:00 PM 06/25/24<BR>SQUEEZE OUT TIME 12:00 AM @ 06/26/24;[02] VOID ENTRY STEP #1. SUMMARY STEP WAS WRITTEN IN ERROR.;[03] VERIFIED STEP 2. VOID STEP.;[04] ***SUMMARY**<BR>REMOVED RIGHT HORIZONTAL STABILIZER L/E #6 RIB AS PER B 737 SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED NEW RIB AS PER B 737 SRM 51-40-05-0G-0.<BR>INSTALLED FIRST OVER SIZE FASTENER AT 4TH EXISTING HOLE FROM TOP.<BR>INSTALLED RH HORIZONTAL LEADING-EDGE RIB #6 AS PER B-737 SRM 51-40-02-0G-0 & DWG 186A1306 & DWG 186A101.<BR>MIXED SEALANT 0870B002BM<BR>10:00 PM 06/25/24<BR>SQUEEZE OUT TIME 12:00 AM @ 06/26/24;[05] CORRECTION FOR SUMMARY TO READ REMOVED RIGHT HORIZONTAL STABILIZER L/E #6 RIB AS PER B 737 SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED NEW RIB AS PER B 737 SRM 51-40-05-0G-0.<BR>INSTALLED FIRST OVER SIZE FASTENER AT 4TH EXISTING HOLE FROM TOP PER SRM 51-40-05-0G-0.SRM 51-40-02-0G-0.<BR>INSTALLED RH HORIZONTAL LEADING-EDGE RIB #6 AS PER B-737 SRM 51-40-02-0G-0 & DWG 186A1306 & DWG 186A1001<BR>MIXED SEALANT 0870B002BM<BR>10:00 PM 06/25/24;[06] RII--VERIFIED STEP 5.
CORROSION R/H LOWER FWD WING TO BODY FAIRING PANEL # 191CR HAS CORROSION AT INNER DOUBLER DRAING MAST.<[01] EVALUATED DAMAGE AT R/H LOWER FWD WING TO BODY FAIRING PANEL # 191CR INNER DOUBLER DRAING MAST FOUND OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED AND REPLACED INNER DOUBLER DRAING MAST AMM 51-31-00-390-804;[02] VERIFIED REPLACEMENT;[03] C/W AUDIT PER MPM 52.02.02
CRACK FOUND AT RH BS 727 STRINGER 18A AFT UPPER FITTING LOWER FASTENER HOLE; CRACK DIRECTION 3 O'CLOCK; CRACK DEPTH 0.030 CRACK FOUND AT RH BS 727 STRINGER 18A AFT UPPER FITTING LOWER FASTENER HOLE CRACK DIRECTION 3 O'CLOCK CRACK DEPTH 0.030'.<[01] ***SUMMARY***<BR>REMOVE CORNER UPPER FITTING AT STA 727 STR 18A AS PER B 737 SRM 51-40-02-0G-0.<BR>REMOVED PANEL 242DF FOR ACCESS AS PER B-737 SRM 51-40-02-0G-0<BR>LOCATED AND DRILLED RH BS 727 STRINGER 18A NEW FITTING AS PER B-737 SRM 51-40-05-0G & DWG 144A7321<BR>TREATED AND PRIMED RH BS 727 STRINGER 18A NEW FITTING AS PER B-737 AMM 51-21-41-370-803 & AMM 51-21-72-370-804INSTALLED NEW FITTING AT RIGHT HAND STA 727 STR 18 AS PER SRM 51-40-04-0G-0 DWG 146A0062 TORQUED TO 180'-POUND TOOL USED B/C # 176329 DUE DATE ON 2/14/2025. MIXED SEALANT 0870C080BM654SKN40 AT 5:00 PM ON 06/29/24 SQUEEZ OUT TIME 1:00 AM ON 07/01/24<BR>REINSTALLED FLOOR PANEL 242DF BOEING 737-700 SRM 51-40-02-0G-0 .SCREW GUN USED ID:176025<BR>DUE DATE:04-DEC-24;[03] VERIFIED STEP 2.
AFT CARGO COMPARTMENT FLOOR SUPPORT BRACKET CRACKED UNDER WASTE TANK POST @ S-26L STA 867 MKD DOT<[01] REMOVED AND REPLACED NEW BRACKET AT AFT CARGO COMPARTMENT FLOOR SUPPORT UNDER WASTE TANK S-26L STA 867 PER REF 51-40-02-0G-0 AND DWG# 149A8102.;[02] VERIFIED REPLACEMENT
FLAP TRACK # 8 FAIRING 644BB CRACKED AT INTERNAL SKIN AFT MKD DOT<[01] PREPARED FOR REPAIR ON FLAP TRACK # 8 FAIRING 644BB; AS PER SRM 51-70-04-2R-1;INSTALLED REPAIR ON FLAP TRACK # 8 FAIRING 644BB; AS PER SRM 51-70-04-2R-1- MATERIAL USED PO.2061896 AND PO.1738579; INSTALLED TOPCOAT ON FLAP TRACK # 8 FAIRING 644BB; AS PER AMM 51-21-73-370-803;[02] VERIFIED REPAIR
FLAP TRACK # 2 FWD FAIRING 543AB HAS SOLID DELAMINATION @ EXTERIOR SKIN FASTENERS HOLES MKD DOT<[01] SUMMARY :PERFORMED PULSE-ECHO UT INSP FOR DELAMINATION.<BR>IAW B737 NDT PART 4; 51-00-01 & PART 1; 51-01-02.<BR>TOOL: EPOCH 600; B/C 19498 CAL. DUE: 03-25-2025.<BR>NO ADDITIONAL DAMAGE FOUND OTHER THAN FAULT DETAIL.PERFORMED DRY OUT ON FLAP TRACK # 2 FWD FAIRING 543AB AS PER B737 SRM 51-70-04-2R-9 PARAG 4-B TOOL USED: TEMP CONTROLLER ID160354 AND CALIBRATION DUE 03-07-25.PREPARED DAMAGE AREA FOR REPAIR ON FLAP TRACK # 2 FWD FAIRING 543AB AS PER B737 SRM 51-70-04-2R-9 PARAG 4-C.APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON FLAP TRACK # 2 FWD FAIRING 543AB AS PER B737 SRM 51-70-04-2R-9 PARAG 4-D-M; MATERIAL USED PO#2061896; PO#1738579 AND TOOL USED: TEMP CONTROLLER ID160354; CALIBRATION DUE 03-07-25.PERFORMED ULTRASOUND INSPECTION OF REPAIRED AREA AND MINIMUM OF 6 INCHES ALL AROUND USING CONTACT THROUGH TRANSMISSION ULTRASONIC REF B737 NDT PT 1; 51-01-01; NDT PT4 51-00-02.
AFT OF AFT CARGO COMPARTMENT FLOOR SUPPORT BRACKET CRACKED AFT END @ S-25L STA 947.75 MKD DOT<[01] SUMMARY: REMOVED AFT CARGO FLOOR SUPPORT BRACKET AT STA 947.75 S-25L AS PER B 737 SRM 51-40-02-0G-0.LOCATED AND DRILLED NEW BRACKET AT S-25 STA 947.75 AS PER REF B/737 SRM 51-40-05-0G-0.INSTALLED NEW BRACKET AT STA 947.75 S-25L AS PER REF B/737 SRM 51-40-02-0G-0.;[02] VERIFIED REMOVED AND REPLACED FLOOR SUPPORT BRACKET AT AFT CARGO STA 947.75 S-25L.
CRACK FOUND AT LOWER FASTENER OPEN HOLE OF BS 727 INNER CHORD AT STRIMGER 18A R/S.<[01] FAULT TO BE RESOLVED ON ITEM # TTG8Q00U011U.;[02] CORRECTION TO READ FAULT TO BE RESOLVED ON ITEM # TTG8Q00U1GHG.;[03] VERIFIED STEP 2 FAULT WILL BE RESOLVED ON TTG8Q00U1GHG
AFT OF FWD CARGO COMPARTMENT DRAG ANGLE AFT END CRACKED @ S-25R BETWEEN STA 500D AND STA 520 MKD DOT<[01] REMOVED; FABRICATED AND INSTALLED DRAG ANGLE FROM AFT OF FWD CARGO COMPARTMENT AT S-25R BETWEEN STA 500D AND STA 520 IN REF SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG #: 143A9803; 143A7902; 143A9801. MATERIAL USED: 7075-O 0.032'; PO# 1734421.;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52-02-02
MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED @ RBL 1 STA 540<[01] REMOVED AND REPLACED MAIN CABIN CENTER SECTION FLOOR SUPPORT @ RBL 1 STA 540 REF SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG#: 143A5240.;[02] RII VERIFIED REMOVED AND REPLACED FLOOR PANEL SUPPORT.;[03] AUDIT C/W MPM 52-0202
MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED @ LBL 1 STA 540<[01] OPENED CABIN FLOOR PANEL 231UF FOR ACCESS PER AMM 53-21-00-000-801.REMOVED AND REPLACED FLOOR SUPPORT BREAK AT MAIN CABIN CENTER SECTION @ LBL 1 STA 540 PER B737 737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING 143A5240..REINSTALLED FLOOR PANEL 231UF REF BOEING 737-700 AMM 53-21-00-400-801.;[02] VERIFIED REPLACED
R/H FWD WING TO BODY FAIRING SUPPORT ANGLE ATTACHED TO FIXED L/E I/B END CRACKED MKD DOT<[01] REMOVED AND REPLACED ANGLE AT R/WING FWD WING TO BODY FAIRING SUPPORT ATTACHED TO FIXED L/E AT I/B END PER B737-700 SRM 51-40-02-0G AND BOEING DRAWING 116A3118.;[02] VERIFIED REPLACEMENT
L/H FWD WING TO BODY FAIRING SUPPORT ANGLE ATTACHED TO FIXED L/E I/B END CRACKED MKD DOT<[01] REMOVED; LOCATED; DRILLED AND INSTALLED L/H FWD WING TO BODY FAIRING SUPPORT ANGLE ATTACHED TO FIXED L/E IAW SRM 51-40-02-0G-0 AND DWGS 116A3118 /116A3110 AND SRM 51-40-05-0G-0.;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52-02-02
G1 GALLEY EMERGENCY EXIT LIGHT ASSY IS DAMAGED.<[01] REMOVED AND REPLACED G1 GALLEY EMERGENCY EXIT LIGHT ASSY; REF B737-700 AMM 33-51-01-960-802.;[02] VERIFIED STEP 1<BR>AUDIT C/W REF MPM 52-02-02
RIGHT A/C BAY PNEUMATIC CROSSOVER DUCT ATTACH BRACKET ON KEEL BEAM CRACKED B.S. 540+5' RBL' 6'. (DOT 51-002)<[01] REMOVED AND REPLACED RIGHT A/C BAY PNEUMATIC CROSSOVER DUCT ATTACH BRACKET ON KEEL BEAM REF B-737 SRM 51-40-02-0G-0;[02] VERIFIED REPLACED
RH DEFLECTOR PANEL OUTBOARD SUPPORT ANGLE CRACKED<[01] REMOVED AND REPLACED SUPPORT ANGLE P/N 115A6260-2 AS PER SRM 51-40-02-0G-0 AND DRAWING 115A6200.;[02] VERIFIED REPLACEMENT
CRACK FOUND ON RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 ; 16' FROM FRONT SPAR; I/B ROW. CRACK LENGTH : O.343' CRACK FOUND ON RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 16' FROM FRONT SPAR I/B ROW. CRACK LENGTH : O.343'<SUMMARY=REMOVED PAINT FOR ACCESS FASTENER ON REPAIR AREA LOWER SKIN STA 193.90 16' AS PER REF B/737 AMM 51-21-11-150-801.<BR>REMOVED FASTENERS ON LOWER SKIN ON R/H HORIZONTAL STAB STA 193.90 16' AS PER REF B/737 SRM 51-40-02-0G-0.<BR>REMOVED DAMAGE AT LOWER STABILIZER SKIN AT STABILIZER STA 193.90 16' FROM FRONT SPAR I/B ROW AS PER SRM 55-10-01-2R-11 REPAIR 11 PERFORMED ROUGHNESS TEST TOOL USED B/C# 172331 NO CALIBRATION DUE DATE.<BR>FABRICATED REPAIR FILLER. MATERIAL USED 2024 T-3 0.080 PO#2072607 AND DOUBLER AS PER REF B/737 SRM 55-10-01-2R-11 REPAIR 11. MATERIAL USED 2024 T-3 0.080 PO#2071143.PERFORMED ROUGHNESS TEST. USED TOOL B/C 172331 NO DUE DATE.<BR>TREATED AND PRIMED LOWER SKIN AREA OF REPAIR AND FILLER AND DOUBLER AS PER REF B/737 SRM 55-10-01-2R-11 REPAIR 11.<BR>INSTALLED COUNTERSINK REPAIR WASCHES AS PER REF B/737 SRM 55-10-01-2R-11 REPAIR 11.<BR>INSTALLED REPAIR PARTS R/H HORIZONTAL STAB LOWER SKIN AT STA 193.90' 16' FRONT SPAR AS PER REF B/737 SRM 55-10-01-2R-11 REPAIR 11.<BR>MIXED SEALANT 0870B002BM 06/018/24 7:00PM. SQUEEZE OUT TIME 06/18/24 10: PM.<BR>APPLIED SEALANT AROUND THE EDGE OF THE DOUBLER AS PER REF B/737 SRM 55-10-01-2R-11 REPAIR 11.
LEFT A/C BAY PNEUMATIC CROSSOVER DUCT ATTACH BRACKET ON KEEL BEAM CRACKED B.S.540+5' LBL. 6'. (DOT 51-001)<[01] REMOVED LEFT A/C BAY PNEUMATIC CROSSOVER DUCT ATTACH BRACKET ON KEEL BEAM REF B-737 SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED LEFT A/C BAY PNEUMATIC CROSSOVER DUCT ATTACH BRACKET ON KEEL BEAM REF B-737 SRM 51-40-02-0G-0;[03] VERIFIED REPLACED
EMERGENCY LIGHT AT 12ABC INOP<[01] RELAMPED EMERGENCY LIGHT AT 12ABC REF AMM 33-51-03 OPS CHECK GOOD
EMERGENCY LIGHT AT 9ABC INOP<[01] RELAMPED EMERGENCY LIGHT AT 9ABC REF AMM 33-51-03 OPS CHECK GOOD
FWD MEGAPHONE HANDLE LOOSE/MISSING SCREW<[01] 01 - REMOVED AND REPLACED PER [AMM 25-64-00-710-801-NG (MEGAPHONE OPERATIONAL TEST - PERMANENT)]
L2 DOOR SLIDE LOOSE.<[01] REPOSITIONED GIRT BAR Z-FOLD IAW MT 725-61-06-AE.<BR>01 - REMOVED AND REPLACED PER [AMM 25-66-01(DOOR-MOUNTED ESCAPE SYSTEM - REMOVAL/INSTALLATION - PERMANENT)]
EMERGENCY EXIT NOT ARMED LIGHT DOES NOT EXTINGUISH WHEN ARMED.<[01] R&R?D SWITCH PER SWPM 20-83-11.
AFT GALLEY MEGAPHONE INOP<[01] OPS CHECK AFT GALLEY MEGAPHONE IAW MM 25-64-00 OPS CHECK GOOD
AFT CABIN MEGAPHONE INOP.<[01] R/R MEGAPHONE BATTERIES IAW AMM 25-64-00. MEGAPHONE CHECKS NORMAL.
CABIN - EMERGENCY LIGHT BATTERY PACKS M1675 AND M1672 FAILED CAPACITY CHECK<[01] R&R EMERGENCY LIGHT BATTERY PACKS M1675 AND M1672 OPS CHK GOOD; CAPACITY CHK PASSED REF AMM 33-51-06
CABIN - EMERGENCY EXIT LIGHT INOP AT RH OVERWING EXIT DOOR FWD LOWER POSITION<[01] RELAMPED RH OVERHAND EMERGENCY EXIT DOOR FWD LOWER LAMPS PER AMM 33-51-14
AFT GALLEY SERVICE DOOR LOWER LINER PAN CRACKED.<[01] REMOVED AND REPLACED AFT GALLEY SERVICE DOOR LINING LOWER BRACKET PER AMM 52-41-31
GROUND CREW REPORTS THAT THE AIR CONDITIONING PANEL ACCESS DOOR WIL NOT CLOSE / [01] REMOVED AND REPLACED AIR CONDITIONING ACCESS DOOR IAW B737 AMM 52-49-01.
AFT GALLEY EMERGENCY LIGHT STRIP LOOSE. / [01] RESECURED EMERGENCY LIGHT STRIP IAW AMM 33-51-15
L2 DOOR ESCAPE SLIDE PRESSURE LOW / [01] REMOVED SLIDE PER AMM25-66-01; AWAITING PARTS;[02] REMOVED SLIDE PER AMM25-66-01; AWAITING PARTS;[03] R&R L2 DOOR SLIDE ASSY PER AMM25-66-01 AND MT 725-61-01AE
*CUSTOMER WALK*L1 DOOR EMERGENCY EXIT SIGN HAS 1 BULB NOT ILLUMINATING / [01] RELAMPED L1 DOOR EMERGENCY EXIT SIGN AS PER B737 AMM 33-51-01-960-801. TEST OK;[02] VERIFIED STEP 1
EMERGENCY LIGHT BATTERY PACK M1669 INOP / [01] REPLACED BATTERY PACK AT M1669; S/N ON: BN200883 AS PER B737 AMM 33-51-06-960-805; OPS-CHECK FOUND NORMAL.;[02] VERIFIED STEP 1
EMERGENCY BATTERY PACK M1674 INOP. / [01] REPLACED BATTERY PACK AT M1674; S/N ON: BN200852 AS PER B737 AMM 33-51-06-960-805; OPS-CHECK FOUND NORMAL.;[02] VERIFIED STEP 1
R1 DOOR INTERIOR EXIT SIGN INOP. / [01] FOUND FORWARD RIGHT DOORWAY LINING CONNECTOR D40042P DISCONNECTED. RE-SECURED CONNECTOR AND PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST; AS PER B737 AMM 33-51-00-710-801; WDM 33-51-12. TEST FOUND NORMAL.;[02] VERIFIED STEP 1
FOUND L-1 DOOR LOWER HINGE COVER PLATE CRACKED AT FASTENER HOLE. / [01] REMOVED; REPLACED AND ADJUSTED L-1 DOOR LOWER HINGE COVER PLATE IN REF AMM 52-11-00-820-801;[02] VERIFIED STEP 1
L-1 DOOR CUTOUT FWD SIDE INNER SURFACE WITH A CRACK AT UPPER SECTION OF UPPER HINGE CUTOUT / [01] REMOVED L1 DOOR CUTOUT ANGLE AS PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED THE NEW L1 DOOR CUTOUT ANGLE AS PER SRM 51-40-05-0G-0;[03] VERIFIED STEPS 1 AND 2. OK TO TREAT AND PRIMER THE HOLES.;[04] TREATED AND PRIMED HOLES AS PER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[05] OK TO INSTALL L-1 DOOR CUTOUT ANGLE.;[06] INSTALLED NEW REVEAL ANGLE AT L-1 DOOR CUT OUT FWD SIDE IAW B737-700 SRM 51-40-02-0G-0;[07] VERIFIED STEP 6;[08] APPLIED WHITE TOPCOAT PAINT TO NEW REVEAL ANGLE AT L1 DOOR CUTOUT AS PER B737-700 AMM 51-21-73-370-804;[09] VERIFIED STEP 8;CARD COMPLETED.
FLOOR PANEL 221GF MISSING PIECE O/B FWD EDGE / [01] MEASUREMENTS;[02] REPAIRED DAMAGE AREA ON FLOOR PANEL #221GF O/B FWD EDGE ASPER B737 SRM 53-00-50-2R-9;[03] VERIFIED 1 & 2
R1 FWD UPPER STUB FRAME CRACKED / [01] LOCATED AND DRILLED NEW R1 FWD UPPER STUB FRAME P/N 141A8371U7 PER B737-700 SRM 51-10-02-0G-0.;[02] VERIFIED 1. OK TO TREAT AND PRIME;[03] TREATED AND PRIMER UPPER STUB FRAME AT R1 DOOR CUT OUT AREA PER SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804;[04] FRAME INSTALLATION WILL BE ACCOMPLISH ON TTG8Q00CHF4K;[05] VERIFIED 4
'CORROSION' AFT CARGO COMPARTMENT FLOOR STRUCTURE STRAP STA 867+4 CORROSION / [01] REMOVED CORROSION AS PER B737-700 SRM 51-10-02-0G-0;[02] VERIFIED STEP 1;[03] ORIGNAL THICKNESS 0.08'. MATERIAL REMOVED 0.0284'. REMAINING THICKNESS 0.0516' FOUND TO BE OUT OF LIMITS AS PER B737-700 SRM 53-60-53-0I-2 FIG. 2 SHEET 1. TOOL USED B/C# 165543; DUE 01SEP2022.;[04] VERIFIED STEP 3;[05] NEW PART TO BE INSTALLED ON TASK CARD # TTG8Q004G6DZ;[06] VERIFIED STEP 5
RH PASSENGER CABIN FLOOR ACCESS PANEL 242UF HAS SEVERAL INSERTS CORRODED. / [01] REMOVED AND REPLACED DAMAGED INSERTS ON MAIN CABIN FLOOR PANEL 242UF AS PER B737-700 SRM 53-00-50-2R-0;[02] VERIFIED STEP 1
MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 312 AND STA 328 RBL 29' CRACKED FLOOR INTERCOSTAL LOCATED BETWEEN STA 312-STA 328 RBL 31.6 AND WL 208.1 / [01] REMOVED MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 312 AND STA 328 RBL 29' AS PER B737-700 SRM 51-10-02-0G-0;[02] LOCATED AND DRILLED INTERCOSTAL AS PER B737-700 SRM 51-40-05-0G-0;[03] CORRECTION TO STEP 1: CORRECT REFERENCE USED B737-700 SRM 51-40-02-0G-0;[04] CORRECT LOCATION TO MAIN CABIN FLOOR INTERCOSTAL IS BETWEEN STA 312 AND 328 RBL 31.6 AND WL 208.1;[05] VERIFIED STEPS 2;3 AND 4 OK TO TREAT AND PRIME DRILLED HOLES.;[06] TREATED AND PRIMED HOLES AS PER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[07] VERIFIED AMT STEP 6 ; OK TO INSTALL CABIN FLOOR INTERCOSTAL IS BETWEEN STA 312 AND 328 RBL 31.6 AND WL 208.1;[08] INSTALLED CABIN FLOOR INTERCOSTAL BETWEEN STA 312 AND STA 328 RBL 31.6 AND WL 208.1 AS PER B737-700 SRM 51-40-05-0G-0;[09] CORRECTION TO STEP 2: LOCATED AND DRILLED NEW INTERCOSTAL AS PER B737-700 SRM 51-40-05-0G-0;[10] VERIFIED STEPS 8 AND 9
MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 344 AND STA 360 BL 0' CRACKED / [01] REMOVED INTERCOSTAL AT MAIN CABIN BL 0 STA 344.0 TO STA 360.0 PER SRM 51-40-02-0G-0;[02] CUT OUT ON THE TOP FORWARD CORNER OF THE INTERCOSTAL IAW B 737-700 SRM 53-10-51-2R-10 SECTION 41;[03] FLAP PEEN AREA ON THE EDGE OF CUT OUT AT FWD CORNER OF THE INTERCOSTAL IAW B 737-700 SOPM 20-10-03 FLAP PEEN KIT USED B/C 19433;[04] LOCATED AND DRILL NEW INTERCOSTAL IAW B737-700 SRM 51-40-05-;[05] VERIFIED 1 TO 4. OK TO TRAT AND PRIME REWORKED INTERCOSTAL;[06] TREATED AND PRIMER AREA INTERCOSTAL IAW B 737-700 AMM 51-21-72-370-804 AND 51-21-41-370-803;[07] VERIFIED 6;[08] LATE ENTRY: ACCOMPLISHED DVI THE TRIM AREA. NO DAMAGE NOTED;[09] LATE ENTRY REMOVED ANGLE FITTING REPAIR FOR ACCESS REPAIR AT NEW INTERCOSTAL IAW B737-700 SRM 51-40-02-0G-0;[10] OK TO INSTALL INTERCOSTAL AND REMOVED PART;[11] INSTALLED NEW INTERCOSTAL AND ANGLE FITTING AT MAIN CABIN FWD WET AREA BETWEEN STA 344 TO 360 BL 0 IAW B 737-700 SRM 53-10-51-2R-10 AND 51-10-40-0G-0;[12] APPLIED FILLET SEAL AND PRIMER AT FASTENERS HEAD IAW B737-700 AMM 51-21-72-370-804;[13] VERIFIED 11 & 12
MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 344 AND STA 360 RBL 12' CRACKED / [01] REMOVED INTERCOSTAL AT MAIN CABIN STA 344 TO STA 360 PER SRM 51-40-02-0G-0;[02] DRILLED HOLES IN NEW INTERCOSTAL AT MAIN CABIN STA.344 TO STA. 360 IAW B737-700 SRM 51-40-05-OG-O;[03] VERIFIED 1;[04] VERIFIED HOLES'S DRILL NEW INTERCSTAL;[05] OK TO TREAT AND PRIME DRILLED HOLES;[06] TREATED AND PRIMED HOLES IN NEW INTERCOSTAL IAW B737-700 SRM 51-20-01-OG-O AND AMM 51-21-72-370-804.;[07] VERIFIED 6. OK TO INSTALL;[08] INSTALLED NEW INTERCOSTAL AT MAIN CABIN BETWEEN STA 344 TO STA 360 RBL 12 AS PER B737-700 SRM 51-40-02-0G-0 AND DWG # 141A5400;[09] VERIFIED STEP 8
MAIN CABIN FWD WET AREA INTERCOSTAL BETWEEN STA 312 AND STA 328 LBL 46' CRACKED / [01] REMOVED AND REPLACED NEW INTERCOSTAL MAIN CABIN FWD WET AREA BTW STA 312 AND 328 AND LBL 46 AS PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1;[03] ADDON TO STEP 1: DWG 141A5400;[04] STEP 2 IS RII INSPECTION BUYBACK
PASSENGER CABIN FLOOR ACCESS PANEL 241ACF HAS SEVERAL INSERTS CORRODED. / [01] REMOVED AND REPLACED INSERTS AT MAIN CABIN FLOOR PANEL 241ACF AS PER B737-700 SRM 53-00-50-2R-0.;[02] VERIFIED 1
MAIN CABIN FWD WET AREA FLOOR PANEL 221BF HAS MISSING AND DAMAGED INSERTS / [01] PANEL REPLACED WITH NEW PANEL PER B737-700 SRM 51-10-02-0G-0 INSTALLATION WILL BE ACCOMPLISH ON TTG8Q00BPAMT;[02] VERIFIED 1
MAIN CABIN FWD WET AREA FLOOR PANEL 221CF MISSING SEVERAL INSERT / [01] PANEL REPLACED WITH NEW PANEL PER B737-700 SRM 51-10-02-0G-0 INSTALLATION WILL BE ACCOMPLISH ON T/C TTG8Q00BPAMR;[02] VERIFIED 1
MAIN CABIN FWD WET AREA FLOOR SUPPORT BETWEEN STA 294.5 AND STA 312 LBL 12' CORROSION / [01] REMOVED FASTENERS ON FWD WET AREA FLOOR SUPPORT BETWEEN STA 277 AND STA 294.5 LBL 12 AND ON LEFT ELEVATOR 'EA' AND 'EB' CONTROL CABLE PULLEYS AT (STA 294.5) AS PER B737-700 SRM 51-40-02-0G-0;[02] REMOVED ON FWD WET AREA FLOOR SUPPORT BETWEEN STA 294.5 AND STA 312 LBL 12 AS PER B737-700 SRM 51-40-02-0G-0;[03] LOCATED AND DRILLED HOLES AT NEW FLOOR SUPPORT AS PER B737-700 SRM 51-40-05-0G-0;[04] VERIFIED STEP #3 AND OK TO INSTALL NEW INTERCOASTAL;[05] MIXED SEALANT BMS 5-95 AT 23:00 EST 05/26/2022; SQUEEZE OUT AND FASTENER INSTALLATION VERIFICATION DUE BY 7:00 EST 05/30/2022.;[06] INSTALLED INTERCOSTAL AT FWD WET AREA FLOOR BETWEEN STA 294.5 AND STA 312 LBL 12 AS PER B737-700 SRM 51-40-02-0G-0 AND DWG 141A5600;[07] INSTALLED ALL REMOVED FASTENERS ON FWD WET AREA SUPPORT BETWEEN STA 277 AND STA 294.5 LBL 12 AND ON LEFT ELEVATOR 'EA' AND 'EB' CONTROL CABLE PULLEYS AT (STA 294.5) AS PER B737-700 SRM 51-40-02-0G-0;[08] VERIFIED STEPS 6 AND 7; FASTENER INSTALLATION VERIFIED ON 28MAY2022 3:53 UTC
MAIN CABIN L/H STA 312 STR 4 FRAME CRACKED / [01] PERFORMED HFEC INSP ON MAIN CABIN L/H STA 312 STR 4. IAW B 737 NDT PART 6 51-00-00 PROCE 23. TOOL NORTEC 600. BC 166316. CALIB DUE 10-8-22. CONFIRMED CRACK; LENGTH 0.313'.;[02] CUTOUT DAMAGED AREA AT FRAME STA 312 STR 4 MAIN CABIN L/H SIDE AS PER B737-7 SRM 53-10-07 2R-1 REPAIR 1 FIG 202 VIEW A .;[03] VERIFIED 2;[04] PERFORMED HFEC INSP. ALONG THE EDGES OF THE CUTOUT OF THE REPAIR AREA IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. NO CRACKS NOTED <BR>TOOL: NORTEC 600 B/C: 166316 DUE: 10/08/22;[05] PERFORMED HFEC ROTO INSP. OF ALL INITIAL FASTENER HOLES WITHIN THE REPAIR AREA ON IAW B737 NDT PART 6; 51-00-00; PROCEDURE 16. NO CRACKS NOTED <BR>TOOL: NORTEC 600 B/C: 166316 DUE: 10/08/22<BR>TOOL: OLYMPUS MINIMITE B/C: 160006 DUE: 01/18/22;[06] FABRICATED AND OPENED NEW FASTENER HOLES AT REPAIR ANGLE AS PER B737-7 SRM 53-10-07-2R-1 REPAIR 1 MAT. USED 7075-0 .063'.[16] INSTALLED ANGLE REPAIR AT MAIN CABIN L/H STA 312 STR 4 FRAME IAW B 737-700- SRM 53-10-07-2R-1;[17] VERIFIED 16;[18] APPLIED FILLET SEAL AROUND THE EDGE OF ANGLE AND CIC AT SURFACES OF THE REPAIR IAW B 737-700-AMM 51-21-91-620-802;[19] VERIFIED 18;[20] C/W
CABIN SEAT TRACK AT BS 727B RBL-45.5 FWD FASTENER (FASTENER B) FOUND LOOSE / [01] REMOVED AND REPLACED (FASTENER B) AT STA 727B RBL 45.5; WORK ACCOMPLISHED ON TTG8Q00CKRJW.;[02] VERIFIED 1
L1 DOOR TARGET ATTACH ANGLE ON AFT UPPER SIDE OF DOOR IS RUBBING AGAINST THE BOLT HEAD ON THE LATCH RECEIVER. / [01] REMOVED ATTACH ANGLE ON AFT UPPER SIDE OF L1 DOOR IAW B737-700 SRM 51-40-02-OG-0;[02] OK TO INSTALL RECEIVED NEW ANGLE;[03] INSTALLED NEW ATTACH ON AFT UPPER SIDE OF L1 DOOR IAW B737-700 SRM 51-40-O2-OG-O;[04] VERIFIED 3
CRACK FOUND AT FWD GALLEY DOOR (R1) BEAR STRAP, BS 290-296, BETWEEN S-8R & S-9R, AFT OF FASTENER OPPOSITE FITTING LATCH. INSTALLED EWIS AND FOD PROTECTION AROUND R1 DOOR FOR BEARSTRAP REPAIR IAW AMM 20-60-07-913-801. REMOVED RAIN GUTTER FROM R1 DOOR IAW SRM 51-40-02-0G-0. APPLIED AND REMOVED PAINT STRIPPING ON OUTER SKIN IAW AMM 51-21-11-150-810. REMOVED ALL FASTENERS AT R1 DOOR REPAIR AREA IAW SRM-53-10-01-2R-6. STEP 4-A & B. REMOVED STUB FRAME IAW SRM-53-10-01-2R-6. STEP 4-A. PERFORMED CUT OUT OF AREA IAW FIGURE 202, REPAIR 6 IAW SRM-53-10-01-2R-6. STEP 4-C. FABRICATED REPAIR DOUBLER. TRIPLER, FLAT SHIM IAW SRM -53-10-01-2R-6. STEP:4-E/F/G/H/I. REPAIR ACCOMPLISHED IAW EA 22-153-01504.
L2 DOOR EXTERIOR EMERGENCY LIGHT INOP . L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. / [01] RELAMPED ; OPS CHECK?S GOOD REF B737 AMM 33-51-04 .
ROW 17DEF AND ROW 18ABC SIDEWALL LIGHTS INOP. REMOVED AND REPLACED WINDOW LIGHTS AT ROW 17DEF AND ROW 18ABC. REF AMM 33-21-00. OPS NORMAL.
FORWARD ENTRY DOOR BOTTOM EMERGENCY EXIT SIGN COVER BROKEN / [01] R/R FWD ENTRY DOOR BOTTOM EMERGENCY EXIT SIGN ASSEMBLY PER M/M 3A 3-51-01 OPS CHI?S GOOD
SUPPLEMENTAL INFORMATION: 192E PANEL FWD MOUNT BRACKETS (2) CRACKED OFF ; / [01] REMOVED AND REPLACED BRACKETS PER MM 20-50-11
STA 663 O/B OF RBL 45 WL 200 UPPER CHORD CRACKED. REPAIRED STA 663 UPPER CHORD O/B OF RBL 45 AT WL 200 I/A/W EA 21-157-02567.
RIGHT OVER WING EXIT SIDEWALL LIGHT INOP. ; RIGHT OVER WING EXIT SIDEWALL LIGHT INOP. / RELAMPED
PREVIOUS LOG PG 1864701 EMERGENCY EXIT ROW FO SIDE SIDEWALL LIGHT INOP / RELAMP EMERGENCY EXIT ROW 12A LIGHT SIDEWALL PER AMM 33-51-21 CL # 77836
EMERGENCY EXIT ROW; FO SIDE; SIDEWALL LIGHT OUT / OK TO CONTINUE PER MEL 33-2-03 SP1B
BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT CRACKED; BS 400-420 L/H SIDE; LBL 25 / REMOVED AND REPLACED BAFLE UNDER FLOOR TO SIDEWALL SUPPORT BS400-420 LBL25 P/N 143A7510-33 IAW SRM 51-40-02 REF DWG 143A7505 89004U 11JUN20
***CORROSION*** ON FWD SHIELD AT FCB BS420 - BS440 R BL23 WL157. / CORROSION ON FCB FWD SHIELD BS420-440 RBL-23 WL157 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS REPAIRED BY REPLACMENT IAW SRM 51-10-02-0G-0 PAR-9C LOCATED AND DRILLED NEW SHIELD ITEM# 7530143 IAW SRM 51-40-05-0G-0 AND DWG# 143A8126 REV-A AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG# 143A0080
***CORROSION*** ON FLOOR SUPPORT SPLICE AT ACB BS887 LBL8 - RBL20 WL168. / REMOVED AND REPLACED ON FLOOR SUPPORT SPLICE AT ACB BS887 FROM LBL8 - RBL20 WL168 IAW SRM 51-40-02 AND DWG 146A9401
***CORROSION*** ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FCB BS500D LBL22 TO RBL22 WL157. / REMOVED AND INSTALLED NEW ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FCB BS500D LBL22 TO RBL22 ITEM 7530142 PO#792417 IAW SRM 51-40-02 SRM 51-40-05 AND DWG 143A9481; DWG 143A7902 80641U 12JUN20
CRACKED SUPPORT ANGLES BEHIND WATER SERVICE PANEL AT ACB BS907 - BS927 RBL12 WL171. / REMOVED; & REPLACED 2EA NEW SUPPORT ANGLES BEHIND WATER SERVICE PANEL OF ACB BS907-BS927 RBL12 PART# 147A7221-32 IAW SRM 51-40-02-0G-0 & DWG 147A7221
FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / REMOVED AND REPLACED ON FCB AFT BULKHEAD SUPPORT GUSSET BS500D S-19R P/N 143A9481-5 IAW SRM 51-40-02; SRM 51-40-05 AND DWG 143A7902 80641U 11JUN20
FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / REMOVED AND REPLACED FCB AFT BULKHEAD SUPPORT GUSSET BS500D STR 19L WL193 IAW SRM 51-40-02 AND DWG #143A7902
BENT STRINGER CLIP AT ACB BS727C S-23R WL163. REMOVED AND REPLACED STRINGER CLIP AT ACB BS727C S-23R WL167 IAW SRM 51-40-02 AND DWG 146A1202.
CORROSION ON RAIL AT ACB BS767+6 RBL8 WL157. REPLACED SPLICE ANGLE C63 ON RAIL AT ACB B/S 76716 RBL8 WL157 IAW SRM 53-00-53-2R-2 REPAIR 2.
CORROSION ON RAIL AT ACB BS767+6 RBL13 WL157. ACCOMPLISHED CARGO TRACK REPAIR AT ACB BS 767+6 RBL13 WL157 IAW SRM 53-00-53-2R-3 REPAIR 3.
***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT ACB BS887 - BS947 RBL21 WL171. / REMOVED; AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT ACB BS887-947 RBL21 IAW SRM 51-40-02; SRM 53-70-53-01-2; SRM 51-20-01; DWG 147A7500 AND DWG 147A9409 80641U 13JUN20 (CORROSION OUT OF LIMITS)
***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FCB BS400 - BS420 RBL22 WL157. / REMOVED; FABRICATED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT FCB BS. 400-BS 420 RBL 22; W.L. 157 ITEM # BAC 1496-444 #7075T62 LOT #1435481-1 IAW SRM 53-00-53-1A-2; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG #143A7501; SRM 51-20-01-0G-0 STEP 5; SOPM 20-41-02 STEP 3.; DWG #143A7500 57319U 05-10-20
***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FCB BS500A - BS500D RBL23 WL157. / REMOVED; FABRICATED; AND INSTALLED NEW FCB FLOOR TO SIDEWALL SUPPORT AT BS500A-500D RBL23; WL157 ITEM# BAC1496-444 #7075T62 LOT#1435481-1 IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0; SRM 53-00-53-1A-2; STEP 4.A(2) FIG 103; SRM 51-40-05-0G-0; SRM 51-20-01-0G-0; STEP 5; SOPM; 20-41-02-STEP3; DWG# 143A7501; DWG#143A7500 57319U 05-10-20
***CORROSION*** ON AFT SHIELD AT ACB BS847 - BS867 RBL21 WL159. MARKED / REMOVED INSTALLED NEW AFT SHIELD AT ACB BS847-867 RBL21 IAW SRM 51-40-02; SRM 51-40-05 AND DWG 146A0081 REV A 80641U 14JUN20; NO SRM ALLOWABLE DAMAGE.
***CORROSION*** ON AFT SHIELD AT FCB BS500 - BS500A RBL23 WL157. / REMOVED AND INSTALLED NEW AFT SHIELD AT FCB B.S.500- BS500A RBL23 WL157 ITEM# 7531855 IAW SRM 51-10-02-0G-0 PAR 9.C; SRM 51-40-02-0G-0 AND DWG# 143A0080
***CORROSION*** ON FWD SHIELD AT ACB BS767 - BS787 RBL21 WL156. MARKED / REMOVED & REPLACED NEW SHIELD AT ACB BS767-BS787 RBL 21 WL 156 IAW SRM 51-40-02-0G-0 & DWG 146A0081 88929R 12JUN20 INSP 357 JUN 12 2020
***CORROSION*** ON TRACK AROUND FASTENER HOLE AT ACB BS942 RBL12 WL179. MARKED / REMOVED AND REPLACED TRACK AT ACB BS887 TO BS947 RBL12 WL179 IAW SRM 51-40-02-0G-0 AND DWG 147A7500 CORROSION OUT OF LIMITS.
***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727B - BS767 RBL21 WL156. / REMOVED AND REPLACED FLOOR SIDEWALL SUPPORT AT ACB BS727 TO BS767 RBL21 WL156 IAW SRM 51-40-02-0G-0 DWG 146A7500
***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS827 LBL17 WL156. / REMOVED AND REPLACED SIDEWALL SUPPORT AT ACB B/S727 TO B/S847 LBL17 WL156 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9. AND DWG 146A7502 REV A 59900U 11JUN20
CORROSION ON BULKHEAD TO FLOOR SUPPORT ANGLE AT BS 947, LBL 8 TO RBL 19, WL180. REMOVED & REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, & DWG 149A8117. NO SRM ALLOWABLE DAMAGE.
CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500A FWD SIDE LBL24 WL156. / REMOVED AND REPLACED FCB INTERCOSTAL ATTACH ANGLE AT BS500A FWD SIDE LBL24 WL156 IAW SRM 51-40-02 AND DWG #143A7505
CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500B FWD SIDE LBL24 WL156. REMOVED AND REPLACED FCB INTERCOSTAL ATTACH ANGLE AT BS500B FWD SIDE LBL24 LBL156 IAW SRM 51-40-02 AND DWG 143A7505
CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500C FWD SIDE LBL24 WL156. / REMOVED AND REPLACED FCB INTERCOSTAL ATTACH ANGLE AT BS500C FWD SIDE LBL24 WL156 IAW SRM 51-40-02 AND DWG #143A7505
CRACKED INTERCOSTAL ATTACH ANGLE AT BS 500C FWD SIDE RBL 24, WL 156. REMOVED AND REPLACED THE INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02-OG-0, AND DWG 143A7505 REV D.
CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS400 LBL25 WL156. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02, AND DWG 143A7505.
SUB THRESHOLD WEB AT BS 794 - 847, RBL23, WL157 CORRODED. REMOVED CORROSION ON THE ACB SUB THRESHOLD WEB IN AREA OF 2' X 1' X 0.02'DEEP ORIGINAL MATERIAL THICKNESS 0.050' FOUND TO BE OUT OF LIMIT IAW SRM 53-60-15-1A-1. LOCATED AND DRILLED NEW SUB THRESHOLD WEB IAW SRM 51-40-05-0G-0, AND DWG 146A8123 AND INSTALLED IAW SRM 51-40-02-0G-0, AND DWG 146A8340.
CORROSION ON RAIL AT ACB BS727D+5 RBL3 WL155. ACB RAIL AT BS727D+5 RBL3 WL155 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM FOR THIS PART; THEREFORE; REPAIRED ACB RAIL BETWEEN BS727 TO 727D+10 RBL3 WL155 IAW SRM 53-00-53-2R-2 REPAIR 2.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS400 - BS500D LBL23 WL157. REMOVED CORROSION FROM FCB FLOOR TO SIDEWALL SUPPORT BS396-400D LBL-23 IN AREA OF 180' X 1' X 0.012' DEEP FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 STEP 4A FIG 103. FABRICATED NEW FLOOR TO SIDEWALL SUPPORT AND SPLICE ANGLE MADE FROM BAC1496-444 7075T62 LOT 1435481 IAW SRM 53-00-53-2R-5 AND DWG 143A7501. APPLIED CHEMICAL CONVERSION COATING AND PRIMED IAW SRM 53-00-53-2R-5 STEP 4I-J AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG 143A7500 SPLICE AT BS492 LBL23.
CORROSION ON RAIL AT ACB BS767+6 LBL3 WL157. REPLACED SPLICE ANGLE C63 ON RAIL AT ACB B/S 767+6 LBL3 WL157 IAW SRM 53-00-53-2R-2 REPAIR 2.
CORROSION ON RAIL AT ACB BS767+6 RBL3 WL157. REMOVED AND REPLACED RAIL SPLICE AT ACB BS767+6 RBL3 WL157; FABRICATED FROM CHANNEL P/N 7530199 IAW SRM 53-00-53-2R-2.
CRACKED FLOOR PANEL SUPPORT AT B.S. 540; R.B.L. 24.5 - 45; W.L. 208.1. / REMOVED AND INSTALLED NEW FLOOR PANEL SUPPORT AT BS 540; R.B.L. 24.5- 45; W.L. 208.1 ITEM # 7531404 IAW SRM 51-40-02-0G-0; AIPC 53-42-11-66.
***CORROSION*** AT AREA AFT OF ACB AROUND FASTENER BS991 LBL19 WL184. MARKED / REMOVED AND REPLACED AFT DRAIN MAST FITTING PER SRM 51-40-02 AND SRM 51-40-05
FUSELAGE SKIN HAS A DENT AT BS 312+2'; 2' BELOW S-2L. DENT MEASURES AT L=1.1'; W=0.9'; Y=.015'; W/Y=60. FUSELAGE SKIN DENT AT BS 312+2' BELOW STR 2L WAS REPAIRED IAW EA 20-153-00851 REV IR DATED 06/19/2020 & ATS ER 20-02734 REV IR DATED 06/19/2020.
UPPER FUSELAGE SKIN EXTERIOR HAS AREAS OF CORROSION AROUND FASTENERS AND BETWEEN BAYS APPROXIMATELY BS 887- BS 1006 STR 3L TO STR 3R. CORROSION ON UPPER FUSELAGE EXTERIOR SKIN AROUND FASTENERS AND BETWEEN BAY APPROXIMATELY BS 887-1006 STR 3L TO STR 3R REPAIRED IAW ATS ER 20-02696; REV IR, AND PER EA 20-153-00768 REV IR. 55981U.
CRACKED FLOOR PANEL SUPPORT AT B.S. 540; B.L. 0 - L.B.L. 24.5 ; W.L. 208.1. REMOVED AND INSTALLED NEW FLOOR PANEL SUPPORT AT B.S. 540 B.L. 0 - L.B.L. 24.5; W.L. 208.1 ITEM # 753090 IAW SRM 51-40-02-0G-0; AIPC 53-42-11-66 57319U 06-05-20
CHAFED RH CROWN SKATE ANGLE AT EXTERNAL FUSELAGE BS1009 RBL14. REMOVED AND REPLACED RH CROWN SKATE ANGLE BS 10061016 RBL 14 IAW SRM 514002; DWG 147A0070 & DWG 147A0030 83802U 03JUN20
CHAFED RH CROWN SKATE ANGLE AT EXTERNAL FUSELAGE BS1016 TO BS1121 RBL14. REMOVED & REPLACED RH CROWN SKATE ANKLE AT EXTERNAL FUSELAGE BS1016 TO BS1121 RBL14 IAW SRM 5140020G0 & DWG 147A0030 PN 147A3200 U12 APPLIED DECORATIVE EXTERIOR PAINT IAW AMM 512199 AND INSTALLED SKATE ANGLE IAW DWG 148A8300
CHAFED LH CROWN SKATE ANGLE AT EXTERNAL FUSELAGE BS1009 LBL14. REMOVED AND REPLACED LH CROWN SKATE ANGLE BS 10061016 LBL14 IAW SRM 5140-02; DWG 147A0070 & DWG 147A0030 83802U 03JUN20
CHAFED LH CROWN SKATE ANGLE AT EXTERNAL FUSELAGE BS1016 TO BS1121 LBL14. REMOVED & REPLACED LH CROWN SKATE ANGLE AT EXTERNAL FUSELAGE BS 1016 TO BS 1121 LBL 14 PN 147A3200U11 IAW SRM 5140020G0 & APPLIED DECORATIVE EXTERIOR PAINT IAW AMM 512199 DWG 148A3590 DWG 148A8300
CRACKED FLOOR PANEL SUPPORT AT B.S. 540; B.L. 0 - R.B.L. 24.5 ; W.L. 208.1. / REMOVED AND INSTALLED NEW FLOOR PANEL SUPPORT AT B.S. 540; B.L. 0 - R.B.L. 24.5; W.L. 208.1. ITEM # 7530909 IAW SRM 51-40-02-0G-0; IAPC 53-42-11-66 57319U 06-05-20
BS 663 LOWER COMPOSITE BULKHEAD RIGHT HAND UPPER ATTACH ANGLE IS CRACKED AT RBL 10; WL 164. ACCOMPLISHED BS663 LOWER COMPOSITE BULKHEAD RIGHT HAND UPPER ATTACH ANGLE REPAIR IAW SRM 57-10-10-2R-5 REPAIR 5.
LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STATION 129.50 IS CRACKED AT THE 3RD VERTICAL STIFFENER. REPAIRED LT HORIZONTAL STABILIZER INSPAR RIB AT STATION 129.50 THE 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4.
AFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED / REPAIRED AND INSTALLED ACB AFT CORNER SCUFF PLATE IAW BAC 5975 USING ER 4043 WITH .063 FILLER ROD LOT # 1131216 AND AMM 53-11-02-420-801
FLIGHT DECK FLOOR IS DENTED AT BS 255; BL O TO LBL 14; WL 207.54. FLIGHT DECK FLOOR DENT AT BS 255 BL0 TO LBL 14 REPAIRED IAW EA NO:1-A53-33179 REV 1.
RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STATION 120.30 IS CRACKED AT THE 3RD VERTICAL STIFFENER. TRIMMED OUT THE DAMAGE PART AT RT HORIZONTAL STABILIZER INSPAR RIB AT STATION 120.30 AT THE 3RD VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4.
DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #5 (UPPER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / FORWARD SERVICE DOOR #5 UPPER BEAM WAS REMOVED & REPLACED ON WORK ORDER:533502. (POS:SF; TAG NO:708511; P/N OFF:141A6516-18; S/N OFF:BN001553; P/N ON:141A6516-18M; S/N ON:BN001553.)
RT SIDE HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 665 RBL 42 WL 200. REPAIRED RT SIDE HORIZONTAL PRESSURE DECK WEB AT BS 663-675 BETWEEN RBL30 RBL60 IAW SRM 53-40-51-2R-2 REPAIR 2.
EMERGENCY EXIT ROW LIGHT COVER BROKEN OFF. / R&R LENS COVER PER AMM.
FORWARD ENTRY EMERGENCY EXIT LIGHT LOWER LENS MISSING DIRECTIONAL ARROW. R&R COVER PER SIP.
193 B PANEL DELAMINATED FWD RT I/B CORNER / R&R 193B PANEL IAW AMM 53-51-21 REF SA-M 326 A1073930
AFT GALLEY FLASHLIGHT RETAINING STRAP DETACHED ON INBOARD FLASHLIGHT. INSTALLED STRAP PER AMM.
LT OVER WING INTERIOR FORWARD EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.
AFT PANEL EMERGENCY EXIT LIGHT BUTTON CLEAR LIGHT LENS COVER BROKEN. R&R COVER PER MM.
AFT PANEL EMERGENCY EXIT LIGHT COVER BROKEN. R&R COVER PER AMM.
TAIL CONE DELAMINATED ON EXTERIOR SURFACE ON LOWER FWD R/H SIDE BELOW ACCESS PANEL OPENING / REPAIRED DAMAGE PER SRM 51-70-04 REPAIR 1
CABIN FLOOR INTERCOSTAL CRACKED AT STA-540 FROM BL-0 TO LBL-24.75 / REMOVED AND REPLACED CABIN FLOOR INTERCOSTAL PER SRM 51-40-02.
RT WING INBOARD FIXED LEADING EDGE SKIN STIFFENER CRACKED INBOARD OF PYLON AT STA 208.32. R&R STIFFENER PER SRM.
LT WING LEADING EDGE UPPER SKIN INBOARD OF PYLON FASTENER HOLE CRACKED N COUNTERSINK LOCATED IN ZONE 2, 11TH FASTENER FROM OUTBOARD EDGE OF ZONE 2. R&R SKIN PER SRM.
L/H TRANSITION ANGLE HAS CORROSION ON AND AROUND NUT PLATE HOLES FROM STA. 727B +10 TO STA. 817. / REMOVED AND REPLACED LH TRANSITION ANGLE FROM STATION 727-847PER SRM 51-10-02 AND SRM 51-40-02. CORRECTED ATA CODE.
R/H TRANSITION ANGLE HAS CORROSION ON AND AROUND NUT PLATE HOLES FROM STA. 767 TO STA. 787. / REMOVED AND REPLACED TRANSITION ANGLE FROM STA 767 TO STA 793 PER SRM 51-10-02;AND SRM 51-40-02. ATA CORRECTED AND CORROSION QUESTIONS ARE ANSWERED.
R/H TRANSITION ANGLE HAS CORROSION ON AND AROUND NUT PLATE HOLES FROM STA. 727A +15 TO STA. 767. / REMOVED AND REPLACED TRANSITION ANGLE PER SRM 51-10-02 AND SRM 51-40-02. ATA CODE CORRECTED.
RH WING UPPER TE PANEL HAS SEAL RETAINER CRACKED 10INCHES OB OF #7 GROUND SPOILER / REMOVED AND REPLACED SEAL RETAINER PER SRM 51-40-02.
RH WING TE FLAPWELL RIB HAS SEAL RETAINER CRACKED AT APPROX. RSS-273 / REMOVED AND REPLACED SEAL RETAINER PER SRM 51-40-02.
AFT CARGO DOOR FWD CORNER SCUFF PLATE IS CRACKED ON BULL NOSE. / REPLACED ON ROUTINE CARD 753-721-00-01
AFT CARGO DOOR CENTER SCUFF PLATE HAS A .5' CRACK ON BULL NOSE 4' AFT OF FWD EDGE. / REPLACED ON ROUTINE CARD 753-721-00-01
ACCESS PANEL 194BL LOWER CENTER SCREW HOLE ELONGATED / REMOVED DAMAGE PER SRM 51-70-05. REPAIRED FASTENER HOLE PER SRM 51-70-05. SEALED AND APPLIED PROTECTIVE COATING IAW SRM 51-70-08-0G-0. DRILLED AND COUNTERSUNK HOLE PER SRM 51-70-05-2R-8.
RUDDER BALANCE WEIGHT CORRODED MID SPAN / REMOVED AND REPAIRED PER CMM 55-40-09
MAIN LANDING GEAR WHEEL WELL REAR SPAR VERTICAL STIFFENER AT RBL25 CRACKED 2' AT THE BOTTOM. / REMOVED AND REPLACED STIFFENER REF SRM 51-40-02.
LOWER SUPPORT FOR THE CORNER POST OF AFT CARGO PANEL 141PW IS CRACKED. / REMOVED AND REPLACED SUPPORT PLATE REF SRM 51-40-02.
RIGHT EMERGENCY EXIT LOWER LIGHT LENS MISSING. R & R THE LENS ASSEMBLY IAW MM.
FUEL TRANSFER FEED VALVE WILL NOT OPEN. BLUE LIGHT NEVER DIMS. CLEANED THE CONNECTER IAW AMM.
RT WING AFT FLAP DEFLECTION ROLLER SUPPORT FITTING AT ORSS 281 CRACKED. REPAIRED FITTING PER SRM.
R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MM.
EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M01670. R&R BATTERY PACK PER DWG.
EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M01675. R&R BATTERY PACK PER DWG.
EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M01669. R&R BATTERY PACK PER DWG.
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R THE BATTERY PACK IAW DWG.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT AND AMM.
EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M01672. R&R BATTERY PACK PER DWG.
EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M01673. R&R BATTERY PACK PER DWG.
RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT HSS 105.26. R & R THE RIB IAW SRM.
FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM.
FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STRINGER 19L. R & R GUSSET IAW SRM.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.7, SECOND STIFFENER AFT AT LOWER END. REPAIRED THE RIB IAW SRM.
FORWARD CABIN FLOOR SUPPORT CRACKED BETWEEN BS 328 - 344, LBL 46. R & R THE FLOOR SUPPORT IAW DWG AND SRM.
FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 727B, STRINGER 8L. REPAIRED THE FRAME IAW EA.
L1 DOOR AFT GIRT BAR MOUNT FITTING CORRODED AT BS 344, LBL 59. R & R THE GIRT BAR FITTING IAW SRM.
FORWARD CABIN FLOOR SUPPORT CRACKED BETWEEN BS 312 - 328, LBL 46. R & R THE FLOOR SUPPORT IAW DWG AND SRM.
FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 727D STRINGER 8R. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED THE FRAME IAW EA.
AFT FLOOR SUPPORT UPPER SURFACE CORRODED AT BS 947.5+13, LBL 49. R & R THE FLOOR SUPPORT IAW SRM.
AFT FLOOR WEB CORRODED AT BS 1016+12, BETWEEN LBL 4 TO 9. R & R THE WEB IAW SRM.
AFT FLOORBEAM UPPER SURFACE CORRODED AT BS 986.5, LBL 46. REPAIRED THE FLOORBEAM IAW EA AND ER.
AFT FLOORBEAM CORRODED AT BS 986.5, RBL 42. REPAIRED FLOORBEAM IAW EA.
MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 42. R & R THE BULKHEAD WEB IAW SRM & DWG.
AFT CARGO BAY BULKHEAD FITTING CRACKED AT BS 948, LBL 10. R & R THE FITTING IAW SRM.
AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727C+10 - 797, LBL 22. REPAIRED THE SUPPORT IAW SRM.
AFT CARGO BAY L ANGLE UNDER INTERCOSTAL CORRODED BETWEEN BS 767 - 787, RBL 22. R & R THE ANGLE IAW SRM.
AFT CARGO BAY THRESHOLD WEB CORRODED BETWEEN BS 807 - 827, RBL 26. R & R WEB IAW SRM.
AFT CARGO BAY SHIELD CORRODED BETWEEN BS 767 TO 792, RT AREA. R & R THE SHIELD IAW SRM.
AFT CARGO BAY BULKHEAD SUPPORT SHROUD ANGLE CRACKED AT BS 727, RBL 6. R & R THE ANGLE IAW SRM.
AFT CARGO BAY RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727C - 767, RBL 22. R & R THE SUPPORT IAW SRM.
LEFT WING NR 1 SLAT BULLNOSE SKIN CRACKED. REPAIRED THE SKIN IAW SRM.
BULKHEAD CRACKED AT BS 663, LBL 33. R & R BULKHEAD IAW SRM AND DWG.
AFT CARGO BAY FLOORBEAM SPLICE TEE STRAP CORRODED AT BS 727D+5, BETWEEN LBL 20 TO RBL 20. R & R FLOORBEAM TEE SPLICE IAW SRM.
AFT CARGO BAY FLOORBEAM SPLICE TEE STRAP CORRODED AT BS 772, BETWEEN LBL 23 TO RBL 23. R & R FLOORBEAM STRAP IAW SRM.
AFT CARGO BAY FLOORBEAM TEE STRAP CORRODED AT BS 887, BETWEEN LBL 22 TO RBL 22. R & R THE FLOORBEAM TEE SPLICE IAW SRM.
SKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED THE SKIN PER ER AND EA.
RIGHT WING TRANSVERSE WEB TO MAIN FLAP ROLLER SUPPORT ARM ATTACH ANGLE CRACKED. R & R THE ROLLER ATTACH ANGLE IAW SRM AND DWG.
RIGHT WING TRANSVERSE WEB CRACKED INBOARD OF MAIN FLAP ROLLER SUPPORT ARM. R & R THE SUPPORT ARM IAW SRM.
SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED THE SKIN IAW ER AND EA.
RIGHT WING NR 8 SLAT NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED THE SKIN IAW SRM.
LT WING NR 3 SLAT NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED SKIN PER SRM.
MID CABIN CEILING EXIT SIGN FELL OFF. INSTALLED & SECURED LENS IAW MM.
OVERWING EXIT SIGN COVER MISSING. REINSTALLED COVER IAW MM.
AT CRUISE FLIGHT, DECK BURNING ODOR AT COCKPIT DOOR LOCK MODULE. R & R DOOR LOCK MODULE IAW MM.
R1 DOOR EMER EVAC SLIDE GIRT BAR DOES MISALIGNED. REALIGNED SLIDE IAW SIP.
LEFT WING UPPER TE FIXED PANEL ABOVE DEFLECTION RIB BETWEEN INBD & OTBD FLAPS AFT HORIZONTAL ANGLE CRACKED. REPAIRED ANGLE IAW SRM.
STRINGER CRACKED AT BS 540 STRINGER 22R. REPAIRED STRINGER IAW EA.
AFT ENTRY DOOR CUT OUT CRACKED AT BS 737B LBL 24.75 ON FWD INBD HOLE ON FLANGE. REPAIRED CUT OUT IAW EA.
AFT ENTRY DOOR CUT OUT CRACKED AT BS 737B RBL 24.75 ON FWD INBD HOLE ON FLANGE. REPAIRED CUT OUT IAW EA.
FLOORBOARD SUPPORT CRACKED AT BS 540 LBL 1. R & R SUPPORT IAW SRM.
AFT ENTRY DOOR CUT OUT CRACKED AT BS 737B LBL 45.75 ON AFT OTBD HOLE ON FLANGE. REPAIRED CUT OUT IAW EA.
STRINGER CRACKED AT BS 540 STRINGER 22L. REPAIRED STRINGER IAW EA.
RIGHT NR 1 WINDOW FRAME CRACKED IN THE UPPER OTBD CORNER. REPAIRED FRAME IAW ACO.
RIGHT WING UPPER SHELF PANEL AT FLAP DEFLECTION RIB CRACKED BRACKET AT UPPER STIFFENER FWD SIDE. R & R BRACKET IAW SRM.
RIGHT WING UPPER SHELF PANEL AT FLAP DEFLECTION RIB CRACKED BRACKET AT UPPER STIFFENER AFT SIDE. R & R BRACKET IAW SRM.
CABIN FLOOR SUPPORT CRACKED AT BS 540 LBL 1. R & R SUPPORT IAW SRM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 111.10 RIB 9.5 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW EA.
R1 DOOR EMERGENCY EXIT SIGN LIGHT ASSEMBLY COVER MISSING. R & R LIGHT ASSEMBLY IAW MM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
SKIN CRACKED AT UPPER FWD CORNER OF BLEND OUT JUST BELOW EXT POWER DOOR LOWER HINGE. REPAIRED SKIN IAW EA.
LEFT EEPLS LENS MISSING AT ROW 5. INSTALLED LENS PER AMM.
RIGHT OVERWING EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.
STRINGER CRACKED BETWEEN BS 328 TO BS 344, STR 5R. REPAIRED STRINGER PER SRM.
FLOORBEAM CORRODED AT BS 344, BL 0. REPAIRED BEAM PER SRM.
FLOORBEAM CORRODED AT BS 344, LBL 4. REPAIRED BEAM PER SRM.
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.
FWD EEPLS LENS LOOSE. SECURED LENS PER M/M.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.
R1 DOOR EMERGENCY EVAC SLIDE LOCKING LATCH RIVET BROKEN. REMOVED AND REPLACED SLIDE ASSY PER MT.
FIRST OFFICERS WINDOW DID NOT OPEN FROM OUTSIDE. REMOVED AND REPLACED WINDOW PER MM.
FLOOR EMERGENCY LIGHT TRACK COVER CRACKED BETWEEN 11C AND 21C. REMOVED AND REPLACED TRACK COVER PER MM.
OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.
DURING SCHEDULED CV CHECK, FOUND EEPLS STRIP SPACERS CRACKED BETWEEN OVERWING EXIT ROW AND AFT ROW. REMOVED AND REPLACED SPACERS PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 5 TO ROW 6. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 11. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED MV1 CHECK, FOUND RT LOWER HORIZONTAL STABILIZER CRACKED AT STA 101.90. REPAIRED STABILIZER PER SRM.
DURING SCHEDULED HC1 CHECK, R2 DOOR EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED MV2 CHECK FOUND, FWD EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS COVER BROKEN AT ROW 17. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT MID CABIN. RELAMPED PER MM.
FWD EEPLS LENS LOOSE. REMOVED AND REPLACED EEPLS PER MM.
EEPLS COVER MISSING AT ROW 1. INSTALLED COVER PER MM.
LT EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767, RBL 3. REPAIRED BEAM PER EA.
DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 767, LBL 8. REPAIRED CHANNEL PER EA.
DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767, RBL 8. REPAIRED BEAM PER EA.
DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 731D, TO BS 807, RBL 8. REPAIRED BEAM PER EA.
DURING SCHEDULED 6Y CHECK, FOUND CENTER BOX WING SHEAR FITTING CRACKED AT BS 540, LBL 15.04. REMOVED AND REPLACED FITTING PER MM AND SRM.
DURING SCHEDULED 6Y CHECK, FOUND CENTER BOX WING SHEAR FITTING CRACKED AT BS 540, LBL 6.14. REMOVED AND REPLACED FITTING PER MM AND SRM.
DURING SCHEDULED 6Y CHECK, FOUND R2 DOOR EMERGENCY EXIT SIGN AFT WALL COVER FADED. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED 6Y CHECK, FOUND FWD CARGO COMPARTMENT LT Z ANGLE CORRODED BETWEEN BS 400 TO BS 500D, LBL 24. REPAIRED ANGLE PER SRM.
DURING SCHEDULED 6Y CHECK, FOUND AFT EMERGENCY EXIT LIGHT LENS FOGGY. CLEANED LENS PER MM.
DURING SCHEDULED 6Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.
DURING SCHEDULED HC2 CHECK, FWD EMERGENCY BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT AFT EEPLS LENS BROKEN AT ROW 23. REMOVED AND REPLACED LENS PER MM.
AFT O/B EMERGENCY EXIT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW 5 TO ROW 21. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED EVAC SLIDE PER MM.
L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.
DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT INOP AT ROW 1 ABC. SECURED CONNECTOR PER MM.
DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 6 ABC TO ROW 11 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.
DURING SCHEDULED MV3 CHECK, FOUND EVAC SLIDE LIGHT INOP AT L1 DOOR. REMOVED AND REPLACED LIGHT BULB PER MM.
FOUND FWD CABIN EMERGENCY EXIT FLOOR LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
FWD CABIN EMERGENCY EXIT LIGHT AND LENS MISSING. INSTALLED LIGHT AND LENS PER MM.
EEPLS TRACK LOOSE AT FWD END. REMOVED AND REPLACED EEPLS END CAP PER MM.
EEPLS TRACK LENS LOOSE AT FWD END. RESECURED LENS PER MM.
DURING SCHEDULED RON, FOUND R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.