N958WN
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
L2 DOOR SLIDE ZEE FOLD HANGING DOWN. REINSTALLED L2 DOOR SLIDE IAW AMM 25-66-01 AND MT 725-61-01.
FWD CARGO BAY FLOOR PANEL 120CF WAS CRACKED AT THE CENTER FLOOR BEAM 9 INCHES. REMOVED AND REPLACED THE FLOOR PANEL 120CF IAW AMM 25-52-10, AND EA M-25-125-02432.
AFT CARGO FLOOR PANEL 140BF IS CRACKED THRU AT SEVERAL FLOORBEAMS. REMOVED & REPLACED THE FLOOR PANEL 140BF IAW AMM 25-52-10, AND EA M-25-125-02433.
EMERGENCY BATTERY PACK AT FWD ENTRY DOOR LEFT M1675 FAILED A CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06.
PASSENGER CABIN AFT SERVICE DOOR ESCAPE SLIDE SKIRT RUBBER DISBONDED AND FRAYED<[01] R&R PASSENGER CABIN AFT SERVICE DOOR ESCAPE SLIDE IAW AMM 25-66-01. REF.#TTG8Q00PLDJQ FOR PARTS INFO.;[02] INSPECTION C/W R&R PASSENGER CABIN AFT SERVICE DOOR ESCAPE SLIDE IAW AMM 25-66-01. REF.#TTG8Q00PLDJQ FOR PARTS INFO.
EXIT LIGHT LENS OVER FWD GALLEY SVC DOOR FELL OFF<[01] PERFORMED INTERIM REPAIR PER EA M-21-133-00720. SECURED WITH TAPE.
EMERGENCY LIGHTS INOP STA. 727C; STA. 952; AND STA. 322.<[01] REMOVED AND REPLACED 3 EA BATTERY PACKS M1670; M1673; AND M1674 AND OPS CHECK GOOD IAW SWA B737-700 AMM 33-51-06-960-805.;[02] REMOVED AND REPLACED 3 EA BATTERY PACKS M1670; M1673; AND M1674 AND OPS CHECK GOOD IAW SWA B737-700 AMM 33-51-06-960-805.
CRACK FOUND R-1 DOOR UPPER FWD CUTOUT INTERNAL SURFACE JUST ABOVE SEAL DEPRESSOR MARKED AT .750' L TO END OF CUTOUT.<[01] REMOVED AND REPLACED 141A8371U7 STUB FRAME IAW B737-700 SRM 51-40-02 AND BAC DWG 141A8370;[02] VERIFIED REMOVED AND REPLACED 141A8371U7 STUB FRAME IAW B737-700 SRM 51-40-02 AND BAC DWG 141A8370
ASSIST HANDLE LOOSE AT R2 DOOR LINER<[01] SECURED ASSIST HANDLE AT R2 DOOR LINER IAW B737-700 AMM 52-13-31-400-802 SUBTASK 52-13-31-020-008;[02] SECURED ASSIST HANDLE AT R2 DOOR LINER IAW B737-700 AMM 52-13-31-400-802 SUBTASK 52-13-31-020-008
CR VB LAV SERVICE DOOR HAS SPOT OF CORROSION ON INNER SURFACE<[01] CR VB LAV SERVICE DOOR HAS SPOT OF CORROSION ON INNER SURFACE [TTG8Q00ZYZ5U];[02] REMOVED AND REPLACED LAV SERVICE DOOR IAW B737-700 AMM 52-49-07-400-801; 20-50-11-910-801; & AIPC 52-49-07-01;[03] REMOVED AND REPLACED LAV SERVICE DOOR IAW B737-700 AMM 52-49-07-400-801; 20-50-11-910-801; & AIPC 52-49-07-01
LEFT MAIN LANDING GEAR TIRE FAILED ON DEPARTURE ROLL REJECTED TAKEOFF AT 130 KNOTS. 31.7M FT-LBS <[01] PREFORMED CONDITIONAL INSPECTIONS; HIGH ENERGY STOP; BRAKE SEIZURE INSPECTION AND TIRE TREAD LOSS/ TIRE BURST INSPECTION SEE TTG8Q00ZE4FT FOR WORK PREFORMED.
FWD PASSENGER DOOR ESCAPE SLIDE SKIRT RUBBER COVER WORN AND DELAMINATED<[01] R&R FWD ENTRY ESCAPE SLIDE IAW MT 725-61-06 FE REF:TTG8Q0F8KDU.;[02] INSPECTION C/W R&R FWD ENTRY ESCAPE SLIDE IAW MT 725-61-06 FE REF:TTG8Q0F8KDU
WHITE COVER FOR EXIT/SALIDA BROKEN OFF FROM ROW 11 ABC<[01] R&R OVER WING EXIT LIGHT COVER IAW AMM 33-51-01
#2 ENGINE OVERHEAT ON CLIMB OUT. ENGINE OVERHEAT LIGHT EXTINGUISHED WITH THRUST LEVER AT IDLE AFTER TWO MINUTES.<[01] FOUND START VALVE LEAKING EXCESSIVELY R+R #2 ENG START VALVE PER AMM 80-11-03
CAPT SIDE AFT EMERGENCY SLIDE BUNCHED UP ON BOTTOM OF DOOR WHEN GIRT BAR ARMED<[01] ADJUSTED PER M.M 25-66-01; NO DEFECTS FOUND
ROW 11 ABC WINDOW LIGHT INOPERATIVE. RELAMPED 11ABC WINDOW LIGHT IN REF. TO AMM 33-21-00. OPS CHECK GOOD.
SEAT ROW 1 BULLNOSE BIN EMERGENCY LIGHT INOP<[01] REPLACED SEAT ROW 1 BULLNOSE BIN EMERGENCY LIGHT LAMP IAW AMM 33-51-03-960-801. LIGHT STILL INOP.;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED ACTION 1 IS COMPLETE;[04] REPARED WIRE W0130-001-20 IN CONNECTOR D11344 PER WDM 35-51-12 AND SWPM 20-61-28.<BR>GOOD PERMORMANCE TEST EMERGENCY LIGHT SEAT ROW 1 BULLNOSE BIN <BR><BR>CRIMP TOOL:<BR>ID: E3380<BR>S/N: 668539<BR>DUE: 11/2023;[05] CERTIFIED ITEM 4;[06] VERIFIED CORRECTIVE ACTION 4.
L/H OWE LOWER EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED BULB AND PERFORMED A GOOD OPERATIONAL TEST IAW AMM 33-51-04-960-801.;[02] CERTIFIED ACTION 1;[03] JOB COMPLETE.
F.E.D MOPSILL FOUND TO BE CRACKED AT FWD ATTACH FASTENER COMMON TO BS 303.9 FRAME<[01] REMOVED GIRT BAR BRACKET FLOOR ATTACHMENTS AT BS 312 AND BS 344 FOR ACCESS TO MOPSILL PER SRM 51-40-02-0G-0<BR><BR>BEGAN REMOVING FASTENERS IN MOPSILL PER SRM 51-40-02-0G-0;[02] VERIFIED SRM 53-10-15-1A-1 IS APPLICABLE FOR ALLOWABLE DAMAGE TO FED DOOR SURROUND STRUCTURE.<BR><BR>FED MOPSILL FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1 PARA. 4C(1) FIG. 108 DETAIL C;[03] UPDATED MEASUREMENT TABLE.;[04] VERIFIED CORRECTIVE ACTION #2;[05] VERIFIED FED MOP SILL FOUND TO BE OUT OF LIMITS<BR>MEASUREMENT TABLE VERIFIED;[06] REMOVED MOPSILL FED LBL BS 270 TO BS 360 IAW SRM 51-40-02-0G-0 AND INSTALL FOD PROTECTION BS 277-360 LBL IAW AMM 20-60-07;[07] CERTIFY;[08] RECEIVED FROM TOOL ROOM NEW FED CHORD (MOPSILL) P/N 654A0004-1073; LOT# 1520563-1.<BR>LOCATED AN DRILLED NEW FED CHORD (MOPSILL) PER SRM 51-40-05-0G-0 AND BOEING DWG# 141A8110.;[09] CERTIFIED CORRECTIVE ACTION 8;[10] VERIFIED CORRECTIVE ACTION #8;[11] OK TO INSTALL NEW FED CHORD (MOPSILL).;[12] VERIFIED CORRECTIVE ACTION #11; OK TO INSTALL;[13] INSTALLED ON MOPSILL 100% OF TEMPORARY AND PERMANENT FASTENERS WITH SEALANT C-20 AT 21-APR-23 05:30 UTC PER SRM 51-4-02-0G-0 AND BOEING DWG 141A8110.;[14] INSTALLED MOPSILL BS270 - BS360; WL208 PER SRM 51-4-02-0G-0 AND BOEING DWG 141A8110.;[15] VERIFIED CORRECTIVE ACTION #13; #14.
L/H VAPOR BARRIER DOUBLER IS CRACKED BS 663; LBL 25 W/L 148<[01] UPDATED STEP 1-9;[02] UPDATED STEP 10;[03] UPDATED MEASUREMENTS TABLE;[04] FABRICATED DOUBLER IAW SRM 51-30-01-0G-0 AND DWG 111A1511-27 REV:A FROM 2024 T0 0.040' LOT. 1510004-1;[05] VERIFIED CORRECTIVE ACTION 4 AND MEASUREMENT TABLE .;[06] REQ. OK TO INSTALL ITEMS ON STEPS 4-10;[07] VERIFIED CORRECTION ITEM 6 STEPS 4-10; OK TO INSTALL.;[08] REQ. OK TO INSTALL ITEMS ON STEPS 1-3;[09] VERIFIED CORRECTION ITEM 8; OK TO INSTALL GIVEN.;[10] INSTALLED ITEMS ON STEPS 1-10;[11] VERIFIED CORRECTION ACTION ITEMS 1-10.;[12] RECEIVED NEW DOUBLER P/N:HFAB53-DB-002; LOT:1524548-1;PO/N:014661/1; LOCATED AND DRILLED AND APPLIED CHEMICAL CONVERSION COATING IAW SOPM 20-43-03 ;SRM 51-40-05 AND DWG: 111A1001; REQUEST OK TO PRIME;[13] VERIFIED CORRECTIVE ACTION #12.<BR>VERIFIED OK TO PRIME NEW DOUBLER.;[14] APPLIED PRIMER ON DOUBLER IAW SOPM 20-41-02 DOUBLER WIIL BE INSTALLED ON JOB CARD TTG8Q00K8Y6L.;[15] VERIFIED CORRECTIVE ACTION #14.
FOUND CRACK ON INTERCOSTAL COMMON TO FASTENER HOLE AT BS 321 WL 208 LBL 44<[01] UPDATED MEASUREMENT FIELD;[02] UPDATED MEASUREMENT TABLE;[03] CERTIFY;[04] REMOVED INTERCOSTAL AT WL208 LBL44 BS 312-328; LOCATED AND DRILLED NEW INTERCOSTAL PN:141A5410U12. NEED OK TO INSTALL.;[05] CERTIFY;[06] VERIFIED CORRECTION ACTIONS 2;3;4 AND 5 AND OK TO INSTALL.;[07] INSTALLED NEW INTERCOSTAL BS312-328 LBL44 IAW SRM 51-40-02-0G-0 AND DWG #141A5400 REV:-;[08] CERTIFY;[09] VERIFIED CORRECTIVE ACTION 7 AND MEASUREMENT TABLE
FOUND CRACK ON INTERCOSTAL COMMON TO FASTENER HOLE AT BS 353.5 WL 208 LBL 11<[01] UPDATED MEASUREMENT TABLE;[02] REMOVED INTERCOSTAL FOR ACCESS AT BS344-360 WL208.5 RBL2 PER SRM 51-40-02-0G-0;[03] REMOVED INTERCOSTAL AT BS 344-360 WL208 LBL11 PER SRM 51-40-02-0G-0;[04] LOCATED HOLES IN INTERCOSTAL AT BS 344-360 WL208 LBL11 PER SRM 51-40-06-0G-0 AND DRAWING # 141A5400 SHT 46 REV A;[05] OK TO INSTALL INTERCOSTALS AT BS 344-360 WL208 LBL11 AND BS344-360 WL208.5 RBL2;[06] CORRECTION TO STEP 4 PRIER TO LOCATING HOLES RECIEVED NEW INTERCOSTAL PO # 914766;[07] VERIFIED CORRECTIVE ACTIONS #4; #5 AND #6<BR>OK TO INSTALL INTERCOSTALS AT BS 344-360 WL208 LBL11 AND BS344-360 WL208.5 RBL2 GIVEN<BR>MEASUREMENT TABLE VERIFIED;[08] CORRECTION TO STEP 2; SHOULD HAVE READ BL0 NOT RBL2;[09] CORRECTION ALSO TO STEP 5 SHOULD HAVE READ BL0 NOT RBL2. INSTALLED INTERCOSTALS AT BS 344-360 WL208 LBL11 AND BS344-360 WL208.5 BL0 PER SRM 51-40-02-0G-0 AND DRAWINGS 141A5400 SHT 32 REV-;141A5400 SHT 46 REV A;[10] VERIFIED CORRECTIVE ACTION #9;[11] THE TASK CANNOT BE COMPLETED BECAUSE THERE IS AT LEAST ONE PART INSTALLATION THAT HAS NOT BEEN COMPLETED.;[12] UPDATED PARTS JOB COMPLETE;[13] VERIFIED PARTS REQUIREMENTS
FOUND CORROSION ON L/H GIRT BAR FITTING AFT MOUNTING BRACKET FASTENER HOLE BS 986 WL 208 LBL 43<OUT OF LIMITS PER B737-700 SRM 53-70-51-2R-6 REPAIR 6.REMOVED CORROSION DAMAGE AREA PER B737-700 SRM 53-70-51-2R-6 REPAIR 6; FIGURE 6. REQUIRE DETAIL INSPECTION ON TOP AND BOTTON SURFACE OF THE UPPER CHORD IN THE DAMEGE AREA.;[06] REQUIRE HFEC ON THE CUTOUT EDGES TO MAKE SURE IS FREE OF CRACKS AND DO A OPEN HOLE INSPECTION (HFEC) OF ALL INITIAL FASTENERS HOLES IN THE REPAIR AREA MAKE SURE NO DAMAGE. CERTIFY; DAMAGE REMOVAL. ACCOMPLISHED <BR>EQUIPMENT USED N600 ATS1465 DUE 09/2023. VERIFY MATERIAL ID FOR FLOOR BEAM REPAIR FELLER BAC1505-101474 7075-T6 LOT# 1505572-1; L-ANGLE BAC1490-2887 7075-T6-C LOT# 1501184-1 AND STRAP 7075T6#0.100 LOT# 1517301-2. FABRICATED REPAIR PARTS FILLER; L-ANGLE; STRAP AND LOCATED AND DRILLED NEW REPAIR PARTS; APPLIED A CHEMICAL CONVERSION COATING ON REPAIR PARTS PER B737-700 SRM 53-70-51-2R-6 REPAIR 6FLAPPED PEEN THE CUTOUT EDGE AND BLEND OUT AREA PER B737-700 SRM 52-70-51-2R-6 REPAIR 6. PRIMED REPAIR PARTS FILLER; STRAP AND L-ANGLE PER B737-700 SRM 53-70-51-2R-6 REPAIR 6. FROM STEP 4.L. TREATED AND PRIMED CUTOUT AREA AND BLEND OUT AREA PER B737-700 SRM 53-70-51-2R-6 REPAIR 6. INSTALLED REPAIR PARTS AT BS 986 WL 208 LBL43 PER B737-700 SRM 52-70-51-2R-6 REPAIR 6.CARD COMPLETE
AFT OF CARGO COMPARTMENT - STRINGER CLIP HAS CORROSION BS 947 STR 26L<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS AFT CARGO COMPARTMENT STRINGER CLIP BS 947 STR 26 IAW SRM 51-10-02;[02] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPACEMENT IAW SRM 51-10-02-0G-0 PARAGRAPH # 9;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2.;[04] RECEIVED FROM TOOL ROOM NEW ANGLE P/N HFAB53-AN-011 HEAT TREATED TO T62 CONDITION; PO# 914699-SWA.<BR>LOCATED; DRILLED AND CHEMICAL CONVERSION COATED ANGLE PER SRM 51-40-05-0G; BOEING DWG# 147A1047 AND SOPM 20-43-03.<BR>OK TO APPLY PRIMER.;[05] CORRECTIVE ACTION FOR STEP 4; (COMPLETING INFORMATION) STRINGER CLIP FABRICATED IN ACCORDANCE WITH BOEING DWG# 147A7580; REFER TO ATS BUILD RECORD 914699-SWA.;[06] VERIFIED CORRECTIVE ACTIONS 4 AND 5. OK TO PRIME.;[07] APPLIED PRIMER TO NEW ANGLE PER SOPM 20-41-02. OK TO INSTALL NEW PART.;[08] VERIFIED CORRECTIVE ACTION 7; OK TO INSTALL;[09] INSTALLED STRINGER CLIP AT ACB BEHIND BS 947 STR 26L PER SRM 51-40-02-0G-0 AND BOEING DWG. 147A1047.;[10] VERIFIED CORRECTIVE ACTION #9<BR>VERIFIED MEASUREMENT TABLE; ITEM 20 IS INCORRECT;[11] EDITED MEASUREMENT TABLE;[12] MEASUREMENT TABLE VERIFIED<BR>TASK COMPLETE
AFT CARGO BAY - RAIL HAS A MECHANICAL DAMAGE BS 747+6 RBL 3.<OUT OF LIMITS IAW SRM 51-10-02 AND 53-00-53-1A-2 FIG 103;DETAIL D.<BR>USED TOOL:<BR>ID:ATS2827<BR>DATE:01/13/23<BR>DUE:01/31/24;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] CORRECTIVE ACTION FOR STEP 1; RIGHT REFERENCE IAW SRM 53-00-53-1A-2 FIG 103;DETAIL D.;[04] VERIFIED CORRECTION ITEM 3.;[05] SRM 53-00-53-2R-3 REPAIR 3 IS FOUND TO BE APPLICABLE.;[06] CUTOUT AND REMOVED RAIL SECTION BETWEEN BS 747+5' TO BS 747+8' IAW SRM 53-00-53-2R-3 REPAIR 3 PAR 4. STEP C.;[07] CUTOUT AND REMOVED RAIL SECTION BETWEEN BS 747+5' TO BS 747+8' IAW SRM 53-00-53-2R-3 REPAIR 3 PAR 4. STEP C. ALTERNATIVE 1 ; FIG 203; RECEIVED NEW CHANNEL P/N: HFAB53-CN-017; LOT:1507930-1; PO/N:889513/1 AND TRACK EXTRUSION P/N:BAC1509-100146#7050T76511;LOT:1481054-1;PO/N:854563/1.;[13] LOCATED; DRILLED AND TRIMMED NEW CHANNEL AND NEW EXTRUSION IAW SRM 53-00-53-2R-3 REPAIR 3 PAR 4. STEP C. ALTERNATIVE 1; FIG 203;[17] TREATED AND PRIMED NEW CHANNEL AND EXTRUSION IAW SRM 51-20-01 & SOPM 20-42-01. OK TO INSTALL.;[18] VERIFIED CORRECTIVE ACTION 17.<BR>OK TO INSTALL;[19] INSTALLED NEW CHANNEL AND EXTRUSION ON AFT CARGO BAY RAIL BS 747+6 RBL 3 IAW SRM 53-00-53-2R-3 REPAIR 3 PAR 4. PERMANENT) WILL BE COMPLIED WITH ON TTG8Q00KFZ0T.
FOUND CRACK ON INTERCOSTAL COMMON TO FASTENER HOLE AT BS 284.5 WL 208 BL 0<[01] UPDATED MEASUREMENT TABLE;[02] REMOVED INTERCOSTAL AT 208 BL 0 BS 277-294.5 AND LOCATED AND DRILLED NEW INTERCOSTAL PN:141A5410U3AAR; NEED OK TO INSTALL;[03] CERTIFY;[04] VERIFIED CORRECTION ACTIONS 1;2;3; AND OK TO INSTALL.;[05] INSTALLED NEW INTERCOSTAL BS277-294.5 BL0 IAW SRM 51-40-02-0G-0 AND DWG #141A5400 REV:-;[06] CERTIFY;[07] VERIFIED CORRECTIVE ACTION 5 AND MEASUREMENT TABLE
AFT FLOOR PANEL 242UF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4. F.REMOVED DAMAGED PLIES ON UPPER FACESHEET IN NUMEROUS LOCATIONS WITH THE LARGEST MEASURING 6' X 5.5'; THEN CLEANED IAW SRM 53-00-50-2R-1 PARA 3. A. AND C. - E. WITH NO MOISTURE OR CONTAMINATION NOTED.;APPLIED BMS5-28 TY19 LOT#AK2JP8366K POTTING COMPOUND TO EXPOSED CORE CELLS THEN SET TO CURE USING HEAT LAMP AND THERMOMETER ID: ATS2209 CAL DUE: 10/2023 IAW SRM 53-00-50-2R-1 PAR.3. G. - H.;CURED POTTING; SANDED FLUSH; CLEANED REPAIR AREA AND FABRICATED REPAIR PLIES FROM BMS9-3 STYLE 1581 H2 LOT NUMBER 1522395-2 INSTALLED PLIES WITH BMS8-201 TYPE III LOT NUMBER 1522301-1; VACUUM BAGGEDVERIFIED CURE COMPLETE; UNBAGGED; TRIMMED PLY EDGES AND RE-DRILLED INSERT HOLES AS NEEDED. ALL IAW SRM 53-00-50-2R-1 PARA 3. M. (1) AND 3. N. <BR> <BR>INSTALLED ALL PREVIOUSLY REMOVED THROUGH INSERTS WITH ADHESIVE BMS 5-107 CLASS 1 LOT# AK2KP8383K AND CURED UNDER HEAT LAMP USING THERMOMETER ID: ATS2209; CAL DUE: 10/2023 TO MONITOR THE TEMPERATURE.<BR><BR>INSTALLED ALL PREVIOUSLY REMOVED BLIND INSERTS WITH ADHESIVE BMS5-28 TY19 LOT#AK2JP8366K AND SET TO CURE UNDER HEAT LAMP USING THERMOMETER ID: ATS2209; CAL DUE: 10/2023 ; TO MONITOR THE TEMPERATURE.<BR><BR> ALL WORK ACCOMPLISHED IAW SRM 53-00-50-2R-1 PARA 3. N. AND BOEING DRAWING 147A5810 SHEET 95. CURED POTTING FOR BLIND INSERTS IAW SRM 53-00-50-2R-1 PARAGRAPH 3.N.
AFT CARGO BAY - RAIL HAS CORROSION RBL 3 BS 767+5.<OUT OF LIMITS IAW SRM 51-10-02 AND 53-00-53-1A-2 FIG 103;DETAIL E.<BR>USED TOOL:<BR>ID:NCX000336<BR>S/N:UNKNOWN<BR>DATE:06/2022<BR>DUE:06/2023;[02] VERIFIED CORRECTIVE ACTION 2.;[03] SRM 53-00-53-2R-3 IS FOUND TO BE APPLICABLE.;[04] PERFORMED DAMAGE CUTOUT OF DAMAGE AREA BETWEEN BS 767+3' TO BS 767+6.5' AT ACB RAIL RBL 3 IAW SRM 53-00-53-2R-3 AND 51-10-02.;[05] PERFORM HFEC INSPECTION CUTOUT AREA.;[06] VERIFIED CORRECTIVE ACTIONS 3 AND 4;[07] HFEC INSPECTED TRIMMED EDGE OOF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. TOOL N600 ATS2353 DUE 01/2024.;[08] CORRECTIVE ACTION FOR STEP 3 AND 4 RIGHT REFERENCE IAW SRM 53-00-53-2R-2;[09] RECEIVED NEW CHANNEL P/N:HFAB53-CN-017;LOT:1524583-1;PO/N:914733/1. FABRICATED AND LOCATED AND DRILLED AT RAIL BETWEEN BS 767 TO 767+11' ;RBL3 IAW SRM 51-40-05 AND SRM 53-00-53-2R-2. REQUEST OK TO TREAT AND PRIME;[10] VERIFIED CORRECTIVE ACTION 8. APPLICABLE REFERENCE IS 53-00-53-2R-2.;APPLIED CHEMICAL CONVERSION COATING AND PRIME ON NEW CHANNEL IAW SRM 51-20-01 AND SOPM 20-41-02; REQUEST OK TO INTALL NEW CHANNEL.;[13] APPLIED CHEMICAL CONVERSION COATING AND PRIME ON DAMAGE CUTOUT IAW SRM 51-20-01 AND SOPM 20-41-02;[14] VERIFIED CORRECTIVE ACTIONS 12 AND 13. OK TO INSTALL CHANNEL.;[15] INSTALLED NEW CHANNEL AT ACB RAIL BETWEEN BS 767 TO 767+11' ;RBL3 IAW SRM 53-00-53-2R-2 ALTERNATIVE 5.
FOUND CORROSION ON R/H GIRT BAR FITTING AFT MOUNTING BRACKET FASTENER HOLE BS 986 WL 208 RBL 43<[01] UPDATED MEASUREMENT TABLE;[02] SRM 53-70-51-2R-6 FOUND TO BE APPLICABLER FOR 986 FLOOR BEAM REPAIR;[03] REMOVED DAMAGE ON 986 FLOOR BEAM AT RBL 43 WL208 GIRT BAR FITTING AFT MOUNTING BRACKET FASTENER HOLE PER SRM 53-70-51-2R-6 STEP 4 C-2;[04] REQUEST HFEC ALONG CUT EDGES OF CUT OUT PER SRM 53-70-51-2R-6 STEP 4 C-2;[05] REQUEST HFEC ON OPEN HOLE IN REPAIR AREA SRM 53-70-51-2R-6 STEP 4 D-2;[06] REMOVED DAMAGE AT R/H GIRT BAR FITTING AFT MOUNTING BRACKET FASTENER HOLE BS 986 WL 208 RBL 43 IN A 1'X.9'X.065 AREA FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-2R-6;[07] DAMAGE CUT OUT 1.2'X1' PER SRM 53-70-51-2R-6 ON ITEM 3;[08] COMPLETED MEASUREMENT TABLE;[09] VERIFIED CORRECTION ITEM 6; 7 AND 8; MEASUREMENT TABLE IS CORRECT.;[10] ACCOMPLISHED HFEC SURFACE SCAN IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. NO CRACKS NOTED. PERFORMED DETAILED INSPECTION OF ADJACENT STRUCTURE.IN REPAIR AREA NO FURTHER DAMAGE FOUND PER SRM 53-70-51-2R-6 STEP 4 D-3;FLAP PEENED CUT EDGE PER PER SRM 53-70-51-2R-6 STEP 4 2-C AND SOPM 20-10-03;[15] UPDATE CORRECTION ACTION ITEM 3.;[16] APPLIED CHEMICAL CONVERSION COATING AND PRIMED AT CUT OUT ON 986 FLOOR BEAM PER SRM 53-70-51-2R-6;[17] APPLIED PRIMER TO ALL REPAIR PARTS PER SRM 53-70-51-2R-6 STEP 4 -L INSTALLED REPAIR PARTS ON BS 986; WL 208; RBL 43; PER SRM 53-70-51-2R-6 FIG. 205; SRM 51-40-02-0G-0 AND BOEING DWG. 147A5730.
CORROSION ON PASSENGER CABIN SEAT TRACK RBL45 BS727C+16; 766;787+10; 807; 827; 827+14; 847+11; 867+3 WL208.< OUT OF LIMITS PER SRM 53-00-52-1A-1. FIGURE 103; PG.11. SEAT TRACK TO BE REPLACED.;[02] VERIFIED CORRECTIVE ACTION 1<BR>VERIFIED MEASUREMENTS TABLE.;[03] REMOVED FASTENER FROM PASSENGER CABIN SEAT TRACK LOCATED AT B.S. 727B - B.S. 887; RBL 45 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW SEAT TRACK FROM RBL 45 PART# ATSHFAB-100-316 LOT# 545484 PER B737-700 DWG 146A5300 REV B. OK TO INSTALL NEW SEAT TRACK.;[05] VERIFIED CORRECTION ACTION ITEM 4; OK TO INSTALL GIVEN.;[06] NEW PART MARKED PER ATS QCM 4.35.26.<BR>INSTALLED PASSENGER CABIN SEAT TRACK RBL45; FROM BS727B - BS887; WL208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A5300.<BR>LOCATED AND DRILLED CABIN FLOOR BOARD HOLES COMMON TO SEAT TRACK RBL45 BS727B - BS887 PER SRM 51-40-05-0G-0.;[07] CERTIFIED CORRECTIVE ACTION 6;[08] VERIFIED CORRECTIVE ACTIONS STEP 6.
FOUND 3EA AREAS OF CORROSION ALONG MOPSILL THRESHOLD ATTACH PLATE FSD AT BS 310-312.5 WL 208 RBL 56.5; BS 316-317.5 WL 208 RBL 58 AND BS 319.5-320.5 WL 208 RBL 58.75<[01] VERIFIED APPLICABILITY FOR SRM 53-10-15-1A-2.<BR>REMOVED CORROSION FROM FSD MOPSILL THRESHOLD ATTACH PLATE L=10.0' X W=1.0' X D=.010'. ORIGINAL MATERIAL THICKNESS 0.090'; MECHANICALLY MEASURED WITH ID: ATS2827; S/N: UNKNOWN; D.D.: 01/31/24. FOUND TO BE OUT OF LIMITS PER SRM 53-10-15-1A-2; PAR. 4.C.(2).(A).;[02] LOCATED AND DRILLED NEW FSD MOPSILL ATTACH ANGLE IAW SRM 51-40-05-0G-0.;[03] OK TO INSTALL MOPSILL ATTACH ANGLE/PLATE.;[04] UPDATE TO PARTS LIST;[05] UPDATED MEASUREMENT TABLE;[06] CORRECTED MEASUREMENT TABLE UPDATE.;[07] CERTIFY;[08] VERIFED FSD MOPSILL THRESHOLD ATTACH PLATE OUT OF LIMITS;[09] VERIFIED CORRECTIVE ACTIONS #2 AND #3<BR>OK TO INSTALL MOPSILL ATTACH ANGLE/PLATE GIVEN<BR>MEASUREMENT TABLE VERIFIED FOUND ITEM 20 TO BE MARKED INCORRECTLY;[10] CORRECTIVE #20 MEASUREMENT TABLE UPDATE;[11] CERTIFY;[12] VERIFIED CORRECTIVE ACTION #10<BR>MEASUREMENT TABLE VERIFIED;[13] INSTALLED NEW MOPSILL THRESHOLD ATTACH ANGLE PLATE IN FSD WL 208 RBL 58.75 IAW SRM 51-40-02-0G-0 AND DWG #141A8310 REV:-;[14] CERTIFY;[15] VERIFIED CORRECTIVE ACTION #13;[16] TASK COMPLETE
FCB SUB THRESHOLD CORROSION; BS460 +4; +5; +7; +10; +13; +16 2EA; +18; BS480+1; +11 MARKED;<[01] VERIFIED APPLICABILITY OF SRM 53-30-15-1A-1 ALLOWABLE DAMAGE 1 AND SRM 53-30-15-01-1 IDENTIFICATION 1.;[02] UPDATED MEASUREMENT TABLE.<BR>REMOVED CORROSION FROM BS 460 +4; +5; +7; +10; +13; +16 2EA; +18; BS 480+1; +11. AFTER BLENDOUT BOTH SURFACES AT BS 460 + 13' MEASUREMENTS: L = 1.80'; W = 1.00'; D = 0.009'; ORIGINAL THIKNESS IS 0.045'; REMAINING MATERIAL IS 0.036' AND IS FOUND OUT OF LIMITS IAW SRM 53-30-15-1A-1 ALLOWABLE DAMAGE 1; PARR. 4G.(2); FIG 103; DETAIL G.<BR>USED TOOL MICROMETER ID ATS2827; S/N: UNKNOW; DUE DATE: 01/31/24.;[03] VERIFIED CORRECTION ITEM 1 AND 2; MEASUREMENT TABLE.;[04] RECEIVED NEW PART. LOCATED AND DRILLED/ COUNTERSINKED AND INSTALLED NEW NUT PLATES. IAW DWG 143A8330 ID:0021 REV:-; SRM 51-40-05; SRM 51-40-06; SRM 51-40-08. SRM 51-40-02.;[05] VERIFIED CORRECTIVE ACTION 4 AND MEASUREMENT TABLE
R/H FLOOR TO SIDEWALL SUPPORT ANGLE CORROSION; BS500A +2; 6; 10; BS500B+10; +14; BS500C +7; +10; RBL24; WL156<[01] VERIFIED APPLICABILITY IAW SRM 53-30-53-01-2 AND SRM 53-00-53-1A-2;[02] REMOVED CORRSION AT<BR><BR>BS 500A+2 0.005'(OUT OF LIMIT) - THE DEEPEST DAMAGE<BR>BS 500A+6 0.002'(WITHIN LIMIT)<BR>BS 500A+10 0.004'(WITHIN LIMIT)<BR>BS 500B+10 0.003'(WITHIN LIMIT)<BR>BS 500B+14 0.001'(WITHIN LIMIT)<BR>BS 500C+7 0.005'(OUT OF LIMIT) - THE DEEPEST DAMAGE<BR>BS 500C+10 0.002'(WITHIN LIMIT)<BR><BR>ORIGINAL MATERIAL THICKNESS : 0.040' DEEPEST DAMAGE REMOVED : 0.005' REMAINING THICKNESS : 0.035' DAMAGE EXCEED 10% OF ORIGINAL THICKNESS AT BS 500A+2 AND BS 500C+7. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2<BR><BR>CALIBRATION TOOL DEPTH GAUGE<BR>ID : ATS2678<BR>DUE : 02/29/24;[03] VERIFIED CORRECTION ITEM1 AND 2.;[04] FABRICATED REPLACMENT FLOOR TO SIDEWALL SUPPORT BS500A-500D RBL 24 PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0 AND DWG 143A7501 OUT OF BAC1496-444#7075T62 LOT#1520195-1<BR><BR>OKAY TO APPLY CHEMICAL CONVERSION COATING AND PRIMER;[05] VERIFIED CORRECTIVE ACTIONS STEP 4; OKAY TO APPLY CHEMICAL CONVERSION COATING AND PRIMER GIVEN.;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER PER AMM 51-21-41-370-802 AND AMM 51-21-72-370-804;[07] VERIFIED CORRECTIVE ACTIONS STEP 6.;[08] INSTALLED CLICKBOND NUTPLATES IAW SRM 51-40-10-2R-0 AND DWG. 143A7501-186.;[09] VERIFIED CORRECTIVE ACTION 8 AND MEASUREMENT TABLE
FOUND 2 EA AREAS OF CORROSION ALONG MOP SEAL THRESHOLD I/B ATTACH PLATE FED AT BS 313.4-316 WL 208 LBL 59 AND BS 334-336.5 WL 208 LBL 62.5<[01] VERIFIED APPLICABILITY FOR SRM 53-10-15-1A-1;[02] REMOVED CORROSION ALONG MOP SEAL THRESHOLD I/B ATTACH PLATE FED AT <BR>BS 313.4-316 WL 208 LBL 59 LENGTH: 4.5' X WIDTH: 0.9' <BR>BS 334-336.5 WL 208 LBL 62.5 LENGTH: 3' X WIDTH: 0.9' PER SRM 53-10-15-1A-1 FIG. 103 DETAIL H;[03] REQUEST NDI FOR MATERIAL REMAINING THICKNESS; [06] REMOVED CORROSION ALONG MOP SEAL THRESHOLD I/B ATTACH PLATE FED AT<BR>BS 334-336.5 WL 208 LBL 62.5 LENGTH: 3' X WIDTH: 0.9' D:0.066' FROM ORIGINAL THICKNESS 0.080' FOUND TO BE OUT OF LIMITS PER SRM 53-10-15-1A-1 FIG. 103 DETAIL H<BR>3;[07] REMOVED MOP SEAL THRESHOLD I/B ATTACH PLATE FED AT BS 312-344 WL 208 LBL 60 PER SRM 51-40-02-0G-0;[08] VERIFIED CORRECTIVE ACTIONS STEP 6.;[09] RECEIVED FROM TOOL ROOM NEW FED MOP SEAL THRESHOLD I/B ATTACH PLATE P/N 141A8112U20; LOT# 1524424-1.<BR>LOCATED AND DRILLED PER SRM 51-40-05-0G-0 AND BOEING DWG# 141A8110. OK TO INSTALL.;[10] VERIFIED CORRECTIVE ACTION #9; OK TO INSTALL
CORROSION ON PASSENGER CABIN SEAT TRACK LBL45 BS727B+3; BS727B+20; BS727D+13; 747+2; 747+13; 767+14;787+6; 807+5; 827+16; 867+7. WL208.< OUT OF LIMITS PER SRM 53-00-52-1A-1. SEAT TRACK TO BE REPLACED.;[02] VERIFIED CORRECTIVE ACTIONS STEP 1;[03] REMOVED CABIN SEAT TRACK LBL45 BS727B-887 PER SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW SEAT TRACK FROM LBL 45 PART# ATSHFAB-100-316 LOT# 545484 PER B737-700 DWG 146A5300 REV B. OK TO INSTALL NEW SEAT TRACK.;[05] VERIFIED CORRECTION ACTION ITEM 3; OK TO INSTALL GIVEN.;[06] VERIFIED CORRECTION ACTION ITEM 4; OK TO INSTALL GIVEN.;[07] INSTALLED PASSENGER CABIN SEAT TRACK LBL45; FROM BS727B - BS887; WL208; PER SRM 51-40-02-0G-0 AND BOEING DWG 146A5300.;[08] CERTIFIED CORRECTIVE ACTION 7;[09] VERIFIED CORRECTIVE ACTIONS STEP 7.;[10] LOCATED AND DRILLED FLOOR PANEL HOLES IN SEAT TRACK BS 727B-887; LBL 45; WL 208 PER SRM 51-40-05;[11] VERIFIED CORRECTIVE ACTION #10<BR>MEASUREMENT TABLE VERIFIED
FRAME BS 312 CRACKED IN RADIUS; AT UPPER DOOR THRESHOLD STR 5 LH<[01] REMOVED DAMAGE IAW SRM51-10-02-OG.;[02] VERIFIED CORRECTION ITEM 1.;[03] REQUEST NDI FOR HFEC SERVICE SCAN TO VERIFY CRACK FREE CONDITION AT CUT OUT.;[04] HFEC INSPECTED CUTOUT AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS1465 CAL DUE: 09/23;[05] OK TO APPLY CHEMICAL CONVERSION AND PRIMER;[06] VERIFIED CORRECTION ITEM 5; OK TO APPLY CHEMICAL CONVERSION AND PRIMER.;[07] APPLIED CHEMICAL CONVERSION AND PRIMER IAW SRM 51-20-01-0G-0 & AMM 51-21-72-370-804;[08] VERIFIED CORRECTION ACTION ITEM 7; MEASURENT TABLE; COMPLETE.
R/H FLOOR TO SIDEWALL SHIELD CORROSION; BS500+2; +6; +10; +14; RBL24; WL156; R/H FLOOR TO SIDEWALL SHIELD CORROSION BS500+2 +6 +10 +14 RBL24 WL156<[01] REMOVED CORROSION FROM 6 SPOTS ON PART 143A8126Y36. THE DEEPEST SPOT IS 1.00 X 1.50 DEPTH 0.015. ORDINAL THICKNESS IS .040. PART HAS NO LIMITS FOR DAMAGE(OUT OF LIMITS). REPAIR BY REPLACEMENT. IAW SRM 51-10-02.<BR>CAL TOOL ATS2592 SER F01852 EXP 02/29/2024;[02] RECEIVED NEW PART. LOCATED AND DRILLED/ COUNTERSINKED AND INSTALLED NEW NUT PLATES. IAW DWG 143A0080 ID:0041 REV:-; SRM 51-40-05; SRM 51-40-06; SRM 51-40-08. SRM 51-40-02.;[03] VERIFIED CORRECTIVE ACTION 1-2 AND MEASUREMENT TABLE
CORROSION ON PASSENGER CABIN SEAT TRACK LBL45 BS497; BS500A+4; WL208.<[01] SEAT TRACK TO BE REPLACED ON FAULT ID: TTG8Q00KCSLD;[02] VERIFIED CORRECTIVE ACTIONS 1.
FWD CABIN FLOOR PANEL 222CF HAS A RIPPED OUT INSERT 3RD BACK FROM THE FWD EDGE ON L/H SIDE<OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.FABRICATED AND CLEANED HONEYCOMB CORE PLUGS USING BMS 8-124; C4; T05; G09 LOT: 1287137 IAW SRM 53-00-50-2R-6 PARA 3.F ALONG WITH DWG: 141A5810 SHEET: 750<BR><BR>OKAY TO INSTALL.<BR><BR>UPPER SURFACE REPAIR PLIES TO BE FABRICATED AND INSTALLED ON FAULT TTG8Q00KBJVC; INSTALLED CORE PLUG USING BMS 5-28 TY19 LOT: AK2IP3152K USING VACUUM AND A CAUL PLATE TO SUPPORT THE REPAIR. IAW SRM 53-00-50-2R-6 PARA 3.F;H.;USED VACUUM GAUGE ATS2798 DUE: 10/2023CURED UPPER SURFACE PLIES THAT WERE INSTALLED ON FAULT TTG8Q00KBJVC USING THERMOMETER ID: ATS2209 CAL DUE: 10/2023 AND REMOVED VACUUM BAG AND TRIMMED REPAIR EDGES. FABRICATED REPAIR PLIES FOR THE LOWER SURFACE FROM BMS9-3 ST1581 LOT# 1522395-2. OKAY TO INSTALL REPAIR PLIES ON THE LOWER SURFACE IAW SRM 53-00-50-2R-6 PARAGRAPH 3.H.(1); I(1); J.K(1)(A). INSTALLED LOWER SURFACE REPAIR PLIES USING BMS8-201 LOT#1522301-1; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD USING VACUUM GAUGE ATS2798 CAL DUE DATE 10/2023 AND SET FOR CURE USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023 IAW SRM 53-00-50-2R-6 PARA 3K(1)-L(1)-M(1).CURED USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023; UNBAGGED AND LIGHTLY SANDED REPAIR IAW SRM 53-00-50-2R-6 PARA 3M(1).;INSERTS WERE INSTALLED AND CURED ON FAULT: TTG8Q00KBJVC
LEFT HORIZONTAL FRONT SPAR ATTACH LUG UPPER SLIDE SEAL IS CRACKED<[01] REMOVED L/H HORIZ STAB FWD SPAR ATTACH LUG UPPER SLIDE SEAL IAW AMM 53-31-31-000-801. STEP 2.;[02] INSTALLED L/H HORIZ STAB FWD SPAR ATTACH LUG UPPER SLIDE SEAL IAW AMM 53-31-31-400-802. STEP 3. F.;[03] EDITED ITEM 2. INSTALLED L/H HORIZ STAB FWD SPAR ATTACH LUG UPPER SLIDE SEAL IAW AMM 53-31-31-400-801. STEP 3. D.;[04] VERIFIED CORRECTIVE ACTION 3
FWD PANEL 221CF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIG 2 TABLE 2 SECTION 41<BR>UPPER SURFACE STRAND DAMAGE EXCEEDS THE ALLOWABLE DAMAGE LIMITS PER SRM 53-00-50-1A-1 PARA 4. B.<BR>REPAIR TO BE PERFORMED IAW SRM 53-00-50-2R-1 .;[02] PERFORMED DAMAGE REMOVAL & SURFACE PREPARATION IAW SRM 53-00-50-2R-1 PARA 4 STEPS A-F.;[03] UPDATED MEASUREMENTS;[04] VALIDATED REPAIR PER SRM 53-00-50-2R-1; USING BMS9-3 STYLE 1581 GLASS LOT 1522395-2 & BMS8-301/50A RESIN LOT 1523449-1 FABRICATED REPAIR PLIES IAW SRM 53-00-50-2R-1 PARA 3 STEPS K & J (1) OK TO LAY UP THE REPAIR.;LAID UP THE REPAIR VACUUM BAGGED THEN LEAK CHECKED IAW SRM 53-00-50-2R-1 PARA 3. L. STEPS (1) (A)-(C) CAL TOOL VACUUM GAGE ID E11543 CAL DUE 09/2023 & SET TO CURE; CURED REPAIR USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023; UNBAGGED; AND LIGHTLY SANDED THEN INSTALLED ALL THROUGH INSERTS USING BMS5-107 LOT#AK2KP8383K IAW SRM 53-00-50-2R-1 PARA 3M(1)-N NSERTS REMOVED IN CORRECTIVE ACTION LINE 5 WERE REPLACED & CURED IAW SRM 53-00-50-2R-0 PARA 5 S. TABLE 203-PAGE 2 REF CAL TOOL THERMOMETER ID ATS2208 CAL DUE 10/2023;[14] VERIFIED CORRECTIVE ACTIONS 11-13;[15] CABIN FLOOR PANEL 221CF UPPER FACE SHEET WAS REPAIRED IAW SRM 53-00-50-2R-1
AFT FLOOR PANEL 242TF UPPER FACESHEET HAS AREAS OF PULLED STRANDS.<[01] NEW FLOOR PANEL WAS FABRICATED IAW EA 23-153-01187-WIP1 & EA 23-153-01187. VERIFIED ALL STEPS COMPLETED WITH NO DEVIATIONS.<BR><BR>JOB COMPLETE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 COMPLETE.
MULTIPLE AREA OF CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727E+9 TO BS 7847.<OUT OF LIMITS IAW SRM 53-00-53-1A-2. REPAIR BY REPLACEMENT<BR><BR>TOOL USED<BR>DEPTH GAUGE ID:ATS2678 CAL.DUE:02/29/2024 LOCATED AND DRILLED NEW AFT CARGO COMPARTMENT LH FLOOR TO SIDEWALL SUPPORT FROM BS 727 - BS 847 AND SPLICE AT BS 727E- BS 747 IAW SRM 51-40-05-0G-0; SRM 53-00-53-2R-6; DWG 146A7500 AND DWG 146A7502.MATERIAL USED: BAC1496-377. LOT#1521599-1<BR><BR>REQUEST TO TREAT AND PRIME;[05] VERIFIED CORRECTIVE ACTIONS STEP 4 AND MEASUREMENTS TABLE.;[06] APPLIED CHEMICAL CONVERSION COATING PER AMM 51-21-41-370-802 AND APPLIED PRIMER PER AMM 51-21-72-370-804;[07] OKAY TO INSTALL SPLICE PLATE;[08] VERIFIED CORRECTIVE ACTIONS STEPS 6;7 OK TO INSTALL SPLICE PLATE GIVEN.;[09] PARTIALLY INSTALLED SPLICE PLATE PER SRM 53-00-53-2R-6;[10] INSTALLED REPAIR PARTS OF NEW AFT CARGO COMPARTMENT LH FLOOR TO SIDEWALL SUPPORT FROM BS 727 - BS 847 AND SPLICE AT BS 727E- BS 747 IAW SRM 51-40-05-0G-0; SRM 53-00-53-2R-6; DWG 146A7500 AND DWG 146A7502.
AFT CARGO BAY - TRACK-TIE DOWN HAS CORROSION RBL 13.75 BS 727D+8; BS 747; BS 767+5; BS 787+5; BS 787+8; BS 787+11; BS 787+15; BS 787+18.5<OUT OF LIMITS IAW SRM 51-10-02 AND SRM 53-00-53-1A-2.;[02] CORROSION ON TRACK IT'S OUT OF LIMITS WIIL BE REPAIRED BY REPLACEMENT OF PART IAW SRM 51-10-02 PAR 9.;[03] CORRECTIVE ACTION FOR STEP 1.<BR>USED TOOL:<BR>ID:NCX000697<BR>S/N:UNKNOWN<BR>DATE:09/2022<BR>DUE:09/2023;[04] VERIFIED CORRECTIVE ACTIONS STEPS 1;2.;[05] REMOVED DAMAGED ACB TRACK FROM BS 727 TO BS 887 RBL 13.75 IAW SRM 51-40-02-0G-0;[06] RECEIVED NEW TRACK ASSY. (2 PIECE KIT) P/N 654A0004-1350 LOT: 1524880-1 PO: 915408/1. PARTIALLY LOCATED AND DRILLED IAW DWG: 146A7500 ID: 0173 REV:- AND SRM 51-30-01-0G-0.;[07] LOCATED AND DRILLED BOTH PIECES OF P/N 654A0004-1350 ASSY. IAW DWG: 146A7500 ID:0173 REV:- AND SRM 51-30-01-0G-0.;[08] VERIFIED CORRECTIVE ACTION STEPS 6 AND 7.;[09] PARTIALLY INSTALLED NEW TRACK ASSY. IAW DWG: 146A7500 ID: 0173 REV:- AND SRM 51-40-02-0G-0.;[10] RECEIVED SPLICE P/N 146A7506-20 PO: 900397/1 <BR>LOT: 1514807-1.;[11] LOCATED AND DRILLED NEW TRACK SPLICE AT BS 747+8' IAW SRM 53-00-53-2R-3. INSTALLED NEW ACB CARGO TIE-DOWN TRACK AND TRACK SPICE AT RBL 13.75 IAW SRM 51-40-02-0G-0; SRM 53-00-53-2R-3; AND DWG 146A7500 ID:0174 REV:
MULTIPLE AREA OF CORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847-867<[01] REMOVED CORROSION FROM 6 SPOTS ON PART 146A8172Y10. THE DEEPEST SPOT IS 0.50 X 0.50 DEPTH 0.005. ORDINAL THICKNESS IS .040. PART HAS NO LIMITS FOR DAMAGE(OUT OF LIMITS). REPAIR BY REPLACEMENT. IAW SRM 51-10-02.<BR>CAL TOOL ATS2592 SER F01852 EXP 02/29/2024;[02] RECEIVED NEW PART. LOCATED AND DRILLED/ COUNTERSINKED IAW DWG 146A8127 ID:0008 REV:-; SRM 51-40-05; SRM 51-40-06; SRM 51-40-08.;[03] CORRECTION TO LINE 1: REMOVED CORROSION FROM 6 SPOTS ON PART 146A8172Y10. THE DEEPEST SPOT IS 0.50 X 0.50 DEPTH 0.005. ORDINAL THICKNESS IS .035. PART HAS NO LIMITS FOR DAMAGE(OUT OF LIMITS). REPAIR BY REPLACEMENT. IAW SRM 51-10-02.<BR>CAL TOOL ATS2592 SER F01852 EXP 02/29/2024;[04] VERIFIED CORRECTIVE ACTION 1; 2; 3 AND MEASUREMENT TABLE
FWD PANEL 221DF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<EXCEEDS THE ALLOWABLE DAMAGE LIMITS PER SRM 53-00-50-1A-1 PARA 4. B. PERFORMED DAMAGE REMOVAL & SURFACE PREPARATION IAW SRM 53-00-50-2R-1 PARA 4 STEPS A-F.;[03] UPDATED MEASUREMENTS;[04] VALIDATED REPAIR PER SRM 53-00-50-2R-1;[05] REMOVED 26EA THROUGH INSERTS & 6EA BLIND INSERTS USING BMS9-3 STYLE 1581 GLASS LOT 1522395-2 & BMS8-301/50A RESIN LOT 1523449-1 FABRICATED REPAIR PLIES IAW SRM 53-00-50-2R-1 PARA 3 STEPS K & LAID UP THE REPAIR VACUUM BAGGED THEN LEAK CHECKED IAW SRM 53-00-50-2R-1 PARA 3. L. STEPS (1) (A)-(C) CAL TOOL VACUUM GAGE ID ATS2798 CAL DUE 10/2023 & SET TO CURE;CURED REPAIR USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023; UNBAGGED; AND LIGHTLY SANDED THEN INSTALLED ALL THROUGH INSERTS USING BMS5-107 LOT#AK2KP8383K; REMOVED 3EA DAMAGED BLIND INSERTS THEN INSTALLED ALL NEW BLIND INSERTS USING POTTING BMS5-28 TYPE 19 LOT#AK2LP8414K IAW SRM 53-00-50-2R-1 PARA 3M(1)-N<BR><BR>INSERTS NEED CURE.;INSERTS REMOVED IN CORRECTIVE ACTION LINES 5 & 11 WERE REPLACED & CURED IAW SRM 53-00-50-2R-0 PARA 5 S. TABLE 203-PAGE 2 REF CAL TOOL THERMOMETER ID ATS2208 CAL DUE 10/2023;CABIN FLOOR PANEL 221DF UPPER SURFACE FACE SHEET WAS REPAIRED IAW SRM 53-00-50-2R-1;
FWD PANEL 221EF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<EXCEEDS THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-50-1A-1 PARA 4 F.REMOVED 32EA THROUGH INSERTS THEN PERFORMED DAMAGE REMOVAL & SURFACE PREPARATION STEPS USING BMS5-28 TYPE 19 POTTING COMPOUND LOT AK21P3152K-1 FILLED THE EXPOSED HONEYCOMB CORE CELLS & SET TO CURE IAW SRM 53-00-50-2R-1 PARA 3. STEP G .;[06] CURED THE POTTING COMPOUND AT THE EXPOSED CORE CELLS; SANDED THEN FABRICATED REPAIR PLIES. IAW SRM 53-00-50-2R-1 PARA 3 STEP K OK TO LAY UP THE REPAIR;[07] LINE 6 CORRECTION: SHOULD READ SANDED THEN PREPARED THE SURFACE IAW SRM 53-00-50-2R-1 .;[08] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 5; 6 AND 7. OKAY TO INSTALL REPAIR PLIES.;[09] INSTALLED REPAIR PLIES USING BMS 8-201TY4 LOT#1523449-1; VACUUM BAGGED; LEAK CHECK GOOD WITH VACUUM GAUGE ID:E11543 CAL DUE 09/2023 IAW SRM 53-00-50-2R-1 PARA 3.K(1)-L(1).;[10] INSPECTED AND VERIFIED CORRECTIVE ACTION 9.;[11] CURED REPAIR PLIES WITH THERMOMETER ID:ATS2208 CAL DUE 10/2023 AND UNBAGGED IAW SRM 53-00-50-2R-1 PARA 3.M(1).;[12] SANDED EDGES AND DRILLED HOLES FOR INSERTS IAW SRM 53-00-50-2R-1 PARAGRAPH 3. N. AND BOEING DWG 144A5810 SHEET 249.;[13] CORRECTION TO ITEM 12: SHOULD READ 'AND BOEING DWG 141A5810'.<BR><BR>INSTALLED ALL INSERTS USING BMS 5-107 LOT#AK2KP8383K-1 IAW SRM 53-00-50-2R-1 PARA 3.N AND BOEING DWG 141A5810 SHEET 249<BR>USED THERMOMETER ID:ATS2208 CAL DUE 10/2023;
FWD PANEL 222AF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>REMOVED ALL INSERTS ON PANEL TO FACILITATE REPAIR; REMOVED ALL DAMAGED PLIES ON UPPER AND LOWER SURFACE; REMOVED LOOSE PIECES OF CORE; CLEANED REPAIR AREA IAW SRM 53-00-50-2R-1 PARA 3.B-F;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.;[03] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 1 AND 2.<BR><BR>VERIFIED MEASUREMENTS TABLE.;[04] APPLIED POTTING BMS 5-28TY19 LOT#AK2IP3152K AND CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2023 IAW SRM 53-00-50-2R-1 PARA 3.G-H.;[05] SANDED POTTING SMOOTH TO SURFACE; CLEANED REPAIR AREA AND FABRICATED REPAIR PLIES USING BMS 9-3H2 LOT#1522395-2 IAW SRM 53-00-50-2R-1 PARA 3.I-K(1).<BR>OK TO INSTALL.;[06] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 4 AND 5. OKAY TO INSTALL REPAIR PLIES.;[07] INSTALLED REPAIR PLIES USING BMS 8-201 LOT#1523449-1; VACUUM BAGGED REPAIR; LEAK CHECK GOOD USING VACUUM GAUGE ID: ATS2441 CAL DUE:10/2023 IAW SRM 53-00-50-2R-1 PARA 3.K-L.;[08] VERIFIED CORRECTIVE ACTION 7;[09] CURED REPAIR USING THERMOMETER ID:ATS2208 CAL DUE 10/2023; UNBAGGED AND TRIMMED EXCESS MATERIAL IAW SRM 53-00-50-2R-1 PARA 3.M(1).;[10] INSTALLED ALL INSERTS USING BMS 5-107 LOT#AK2KP8383K-1 IAW SRM 53-00-50-2R-1 PARA 3.N AND BOEING DWG 141A5810 ID 769
FWD PANEL 222BF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL MATERIAL IAW 53-00-50-0I-1 SHEET 1; FIGURE 2; TABLE 2;<BR>AND DWG DOC: 141A5810 ID: 0464<BR><BR>DAMAGE TO UPPER FACESHEET AREAS IS OUT OF ALLOWABLE LIMITS IAW SRM<BR>53-00-50-1A-1 PAR. 4.F.DAMAGE TO PANEL FACESHEET IS REPAIRABLE IAW SRM 53-00-50-2R-1 AS <BR>DIRECTED BY SRM 53-00-50-2R-0 PAR. 2. A. TABLE 201REMOVED (36EA) INSERTS FROM AREAS (P1 - P36) IAW SRM 53-00-50-2R-0 <BR>PAR. 5. S. (1)(A) & 5. S. (1)(B)<BR><BR>REMOVED DAMAGED PLIES AND CLEANED REPAIR AREA WITH FABRICATED REPAIR PLIES USING BMS9-3 TYH2 CL7 ST1581 LOT#<BR>1522395-2 IAW SRM 53-00-50-2R-1 PAR. 3. J. & 3. K.FOUND AND REMOVED (7EA) DAMAGED ADDITIONAL INSERTS FROM <BR>AREAS (P37 - P40; P53 - P55) IAW SRM 53-00-50-2R-0<BR>PAR. 5. S. (1)(A) & 5. S. (1)(B);INSTALLED REPAIR PLIES CURED REPAIR USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023 AND UNBAGGED PANEL IAW SRM 53-00-50-2R-1 PARA 3M(1).;[10] SANDED REPAIR EDGES; LOCATED AND CLEANED (43EA) INSERT AREAS IAW SRM <BR>53-00-50-2R-1 PAR. 3. M. (1) & 3. N REMOVED 3EA ADDITIONAL DAMAGED BLIND INSERTS; CLEANED AREA; INSTALLED 7EA BLIND INSERTS USING BMS5-28 TYPE 19 LOT#AK2IP3152K AND CURED USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023 IAW SRM 53-00-50-2R-1 PARA 3B AND 3N.
FWD PANEL 222CF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR><BR>WILL PERFORM REPAIRS IAW SRM 53-00-50-2R-1 REMOVED 40EA INSERTS TO FACILITATE REPAIR. REMOVED DAMAGED PLIES; CLEANED AND PREPARED PANEL IAW SRM 53-00-50-2R-1 PARA 3.A-C; J.;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.; FABRICATED REPAIR PLIES USING BMS 9-3 TYH2 CL7 ST1581 LOT: 1522395-2 IAW SRM 53-00-50-2R-1 PARA 3.K. <BR><BR>OK TO INSTALL;[05] INSPECTED AND VERIFIED CORRECTIVE ACTION 4. OKAY TO INSTALL REPAIR PLIES.;[06] INSTALLED REPAIR PLIES USING BMS 8-201 TY3 LOT: 1522301-1<BR>ASSEMBLED VACUUM BAG AND PERFORMED 5X5 TEST USING VACUUM GAUGE ATS2798. PASSED. IAW SRM 53-00-50-2R-1 PARA 3.K-L.;[07] CORRECTION TO ACTION 6: USED GAUGE ATS2798 DUE: 10/2023;[08] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 6 AND 7.;[09] CURED REPAIR PLIES USING THERMOMETER ID: ATS2209 CAL DUE: 10/2023. REMOVED VACUUM BAG; AND TRIMMED REPAIR EDGES IAW SRM 53-00-50-2R-1 PARAGRAPH 3.M(1).;[10] VERIFIED CORRECTIVE ACTION 9;[11] DRILLED HOLES FOR INSERTS IAW SRM 53-00-50-2R-1 PARAGRAPH 3. N. AND BOEING DWG 144A5810 SHEET 750.;[12] INSTALLED 40EA INSERTS USING BMS 5-107 LOT: AK2KP8383K-1<BR>CURED USING THERMOMETER ATS2209 DUE: 10/2023 IAW SRM 53-00-50-2R-1 PARA 3.N ALONG WITH DWG 141A5810 SHEET 750;[13] VERIFIED CURE TAPE<BR>VERIFIED CORRECTIVE ACTION #11; 12
FWD PANEL 222DF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR><BR>WILL PERFORM REPAIRS IAW SRM 53-00-50-2R-1<BR><BR>REMOVED 41EA INSERTS TO FACILITATE REPAIR. REMOVED DAMAGED PLIES; CLEANED AND PREPARED PANEL IAW SRM 53-00-50-2R-1 PARA 3.A-C; J.;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1.;[03] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 1 AND 2.<BR><BR>VERIFIED MEASUREMENTS TABLE.;[04] FABRICATED REPAIR PLIES USING BMS 9-3 TYH2 CL7 STYLE 1581 LOT# 1522395-2 IAW SRM 53-00-50-2R-1 PARA 3.K(1).<BR><BR>OKAY TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION 4;[06] OK TO INSTALL REPAIR PLIES;[07] INSTALLED REPAIR PLIES USING BMS 8-201 TY3 LOT: 1522301-1<BR>ASSEMBLED VACUUM BAG AND PERFORMED 5X5 TEST USING VACUUM GAUGE ATS2798. PASSED. IAW SRM 53-00-50-2R-1 PARA 3.K-L.;[08] CORRECTION TO ACTION 7: USED VACUUM GAUGE ATS2798 DUE: 10/2023;[09] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 7 AND 8.;[10] CURED REPAIR USING THERMOMETER ID: ATS2209 CAL DUE: 10/2023. UNBAGGED; TRIMMED AND SANDED IAW SRM 53-00-50-2R-1 PARA 3.M.;[11] VERIFIED CORRECTIVE ACTION 10;[12] DRILLED HOLES FOR INSERTS IAW SRM 53-00-50-2R-1 PARAGRAPH 3. N. AND BOEING DWG 144A5810 SHEET 749.;[13] INSTALLED 41EA INSERTS USING BMS 5-107 LOT: AK2KP8383K-1<BR>CURED USING THERMOMETER ATS2209 DUE: 10/2023 IAW SRM 53-00-50-2R-1 PARA 3.N. ALONG WITH DWG 141A5810 SHEET 749.;[14] VERIFIED CORRECTIVE ACTION #12; 13<BR>VERIFIED CURE TAPE
FWD PANEL 222DF HAS A RIPPED OUT INSERT ALONG THE O/B EDGE. (MARKED)<OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F. FOUND ADDITIONAL DAMAGE ON THE INBOARD EDGE. FABRICATED AND CLEANED 2E HONEYCOMB CORE PLUGS USING BMS 8-124; TYPE V; GRADE 9.0; CLASS 4 LOT# 1287137 IAW SRM 53-00-50-2R-6 PARA 3.F AND TABLE 201; BWG DWG #: 141A5810 SHEET: 749] INSTALLED CORE PLUGS USING BMS 5-28 TY19 LOT: AK2IP3152K USING VACUUM AND CAUL PLATES TO SUPPORT THE REPAIRS IAW SRM 53-00-50-2R-6 PARA 3.F;H.;[09] CORRECTION TO ACTION 8: USED VACUUM GAUGE ATS2798 DUE: 10/2023;[10] INSPECTED AND VERIFIED CORRECTIVE ACTION 9.<BR>.;[11] 5067<BR><BR>UPPER SURFACE PLIES CURED AND UNBAGGED ON FAULT TTG8Q00KBKR7<BR><BR>SANDED 2EA HONEYCOMB CORE PLUGS TO BE LEVEL WITH THE ADJACENT SURFACES IAW SRM 53-00-50-2R-6 PARA 3.J. <BR><BR>FABRICATED REPAIR PLIES FROM BMS 9-3 TY H2 CL7 STYLE 1581 LOT#1522395-2-1 IAW SRM 53-00-50-2R-6 PARA 3.K(1) INSTALLED LOWER SURFACE REPAIR PLIES USING BMS8-201 LOT#1522301-1; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD USING VACUUM GAUGE ATS2798 CAL DUE DATE 10/2023 AND SET FOR CURE USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023 IAW SRM 53-00-50-2R-6 PARA 3K(1)-L(1)-M(1).;[15] INSPECTED AND VERIFIED CORRECTIVE ACTION 14.;[16] CURED USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023; UNBAGGED AND LIGHTLY SANDED REPAIR IAW SRM 53-00-50-2R-6 PARA 3M(1).;[17] INSERTS WERE INSTALLED AND CURED ON FAULT TTG8Q00KBKR7\\
MULTIPLE AREA OF CORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 22 BS 767-787<[01] REMOVED CORROSION FROM 8 SPOTS ON PART 146A8172U12. THE DEEPEST SPOT IS 0.75 X 0.75 DEPTH 0.010. ORDINAL THICKNESS IS .040. PART HAS NO LIMITS FOR DAMAGE(OUT OF LIMITS). REPAIR BY REPLACEMENT. IAW SRM 51-10-02. <BR>CAL TOOL ATS2592 SER F01852 EXP 02/29/2024;[02] RECEIVED NEW PART. LOCATED AND DRILLED/ COUNTERSINKED IAW DWG 146A8127 ID:0007 REV:-; SRM 51-40-05; SRM 51-40-06; SRM 51-40-08.;[03] VERIFIED CORRECTIVE ACTION 1; 2 AND MEASUREMENT TABLE
AFT FLOOR PANEL 242SF UPPER FACESHEET HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 242SF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6. PULLED STRANDS OF FIBERGLASS AT DISCREPANT LOCATION EXCEED ALLOWABLE DAMAGE LIMITS AND REQUIRE REPAIR IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. DAMAGED AREAS ARE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>REMOVED INSERTS TO FACILITATE REPAIR IAW SRM 53-00-50-2R-1 PARAGRAPH 3.B<BR><BR>REMOVED DAMAGED PLIES (STRANDS) AT DISCREPANT LOCATION AND CLEANED AREAS IAW SRM 53-00-50-2R-1 PARAGRAPH 3.A;C;E-F.;[02] VALIDATED REPAIR PER SRM 53-00-50-2R-1;[03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.;[04] FABRICATED REPAIR PLIES FROM BMS9-3 ST1581 LOT# 1522395-2. OKAY TO INSTALL REPAIR PLIES IAW SRM 53-00-50-2R-1 PARAGRAPH 3.K(1)(A).;[05] VERIFIED CORRECTIVE ACTION 4<BR><BR>OK TO INSTALL REPAIR PLIES;[06] INSTALLED REPAIR PLIES USING BMS8-201 TY4 LOT# 1523449-1. VACUUM BAGGED AND LEAK CHECKED GOOD USING VACUUM GAUGE ID: ATS2441 CAL DUE: 08/2023 IAW SRM 53-00-50-2R-1 PARAGRAPH 3.K(1)(B-C)L(1) CURED REPAIR PLIES USING THERMOMETER ID: ATS2209 CAL DUE: 10/2023. REMOVED VACUUM BAG AND TRIMMED REPAIR EDGES AND CLEANED IAW SRM 53-00-50-2R-1 PARAGRAPH 3.L(1); M(1);INSTALLED ALL INSERTS WITH ADHESIVE BMS5-107 LOT# AK2KP8383K-1; AND CURED USING THERMOMETER ATS2209 CAL DUE: 10/2023 IAW SRM 53-00-50-2R-1 PARAGRAPH 3.N AND BAC DWG 147A5810 ID:0099; ATTACHED CURE SHEETS.;[14] FINAL INSPECTION. JOB COMPLETE
AFT PANEL 242XF LOWER SKIN IS BROKEN. (MARKED)<[01] IDENTIFIED FLOOR PANEL 242XF MATERIAL IAW SRM 53-00-50-0I-1 FIG 6; TABLE 6 AND BOING DWG 147A5810-11.<BR><BR>FOUND DAMAGE AT 2EA LOCATIONS ON LOWER SURFACE; BOTH AREAS ARE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F. <BR><BR>REPAIRS TO BE ACCOMPLISHED PER SRM 53-00-50-2R-1.<BR><BR>REMOVED DAMAGE AT BOTH LOCATIONS AND CLEANED AREAS; OK TO POT EXPOSED CORE IAW SRM 53-00-50-2R-1 PARA 3C-F;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-1; APPLIED POTTING BMS5-28 TYPE 19 LOT#AK2LP8414K TO EXPOSED CORE AND CURED USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023 IAW SRM 53-00-50-2R-1 PARA 3G-H.;[05] SANDED POTTING SMOOTH WITH SURFACE; CLEANED REPAIR AREA AND FABRICATED REPAIR PLIES FROM BMS 9-3 TY H2 LOT#1522395-2 IAW SRM 53-00-50-2R-1.PARA 3. I.- K. (1) (A). INSTALLED REPAIR PLIES USING BMS8-201 LOT#1522301-1; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD USING VACUUM GAUGE ATS2441 CAL DUE DATE 08/2023 AND SET FOR CURE USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023. IAW SRM 53-00-50-2R-1 PARA 3K(1)-L(1)-M(1).;[08] INSPECTED AND VERIFIED CORRECTIVE ACTION 7.;[09] VERIFIED CURE WAS COMPLETE AND REMOVED PANEL FROM VACUUM BAG IAW SRM 53-00-50-2R-1 PARA 3. M. (1) TRIMMED EXCESS MATERIAL IAW SRM 53-00-50-2R-1 PARA 3.M(1).;[12] FINAL INSPECTION. JOB COMPLETE.
AFT PANEL 241XF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] NEW FLOOR PANEL WAS FABRICATED IAW EA 23-153-01174-WIP1 AND EA 23-153-01174. VERIFIED ALL STEPS COMPLETE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 COMPLETE.
AFT PANEL 241ABF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] VERIFIED COMPLETION OF PANEL 241ABF FABRICATION IAW EA 23-153-01175;[02] VERIFIED CORRECTIVE ACTION 1
AFT PANEL 241ADF UPPER FACESHEET HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] NEW PANEL WAS FABRICATED IAW EA 23-153-01177-WIP1 AND EA 23-153-01177. ALL STEPS COMPLETED WITH NO DEVIATIONS. <BR><BR> JOB COMPLETE.;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED CURE TAPE
FWD PANEL 221BF UPPER FACESHEET HAS AN AREA OF PULLED STRANDS.<[01] FLOOR PANEL 221BF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL ON FAULT TTG8Q00KBJAJ.;[02] PANEL REPLACED. JOB COMPLETE
FWD. R/H BRACKET BROKEN AT LWR. FAIRING WING CENTER SECTION PANEL 192E<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE IAW SRM 51-10-02;[02] FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9.;[03] REMOVED FWD R/H BRACKET BROKEN AT LWR FAIRING WING CENTER SECTION PANEL 192E IAW SRM 51-40-02.;[04] LOCATED AND DRILLED FWD R/H NEW BRACKET AT LWR P/N149A7712-42 LOT#1524352-1 PO#914652/1;FAIRING WING CENTER SECTION PANEL 192E IAW SRM 51-40-05 AND DWG 149A7712 REV:-;[05] VERIFIED CORRECTION ACTION ITEM 4.;[06] INSTALLED FWD R/H NEW BRACKET AT LWR FAIRING WING CENTER SECTION PANEL 192E IAW SRM 51-40-02 AND DWG 149A7701 REV:-A;[07] VERIFIED CORRECTIVE ACTIONS STEP 6.
MULTIPLES AREA OF CORROSION ON AFT CARGO BAY THRESHOLD AT BS 787+8-847 RBL 27.5.<[01] VERIFY APPLICABILITY OF SRM 53-60-15-1A-1<BR><BR>MEASURMENT UPDATE;[02] FIXED REMAINING THICKNES FROM 0.035 TO 0.033;[03] REMOVED CORROSION FROM AFT CARGO THRESHOLD WEB BS787+8 TO BS847 DEEPEST AREA AT BS807+2 MEASURED 16.3'L X 1'W AND 0.017'DEEP; ORIGINAL THICKNESS OF 0.050' FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1<BR><BR>CAL ID DIAL DEPTH GAUGE <BR>ATS2678<BR>DUE 02/29/24;[04] VERIFIED CORRECTIVE ACTIONS STEPS 1;2;3.;[05] LOCATED AND DRILLED NEW ACB THRESHOLD WEB P/N 146A8123-25; LOT. 1522932-1; IAW SRM 51-40-05-0G-0 AND DWG. 146A8340.<BR>INSTALLED NUT PLATES IAW SRM 51-40-02-0G-0.;[06] COUNTERSINKED SUB THRESHOLD IAW DWG 146A8340 ID 026 REV-; SRM 51-40-08.;[07] VERIFIED CORRECTIVE ACTIONS STEPS 5;6 AND MEASUREMENTS TABLE.
MULTIPLE AREA OF CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727+4 TO BS 767.<[01] VERIFIED SRM 53-00-53-1A-2 TO BE APPLICABLE;[02] REMOVED CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 727+4 TO BS 767; DEEPEST AREA OF DAMAGE L=1.9' W=1.3' DEPTH = 0.015'; BEYOND 10% OF ORIGINAL MATERIAL THICKNESS OF 0.040'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2.;[03] CALIBRATED TOOL USED; DIAL DEPTH GAUGE 643JZ(ATS2678) DUE: 02/29/24;[04] VERIFIED CORRECTION ITEM 1; 2 AND 3.;[05] FABRICATED; LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT FROM BAC1496-377 7075-T62 LOT: 1521599-1 IAW SRM 51-30-01-0G-0 & DWG 146A7502 ID: 0002 REV: A.;[06] COUNTERSANK FASTENER LOCATIONS ON REPLACEMENT FLOOR TO SIDEWALL SUPPORT PER SRM 51-40-08-0G-0 AND DWG 146A7502<BR><BR>OKAY TO APPLY CHEMICAL CONVERSION COATING AND PRIMER;[07] VERIFIED CORRECTIVE ACTION STEP 6 OK GIVEN;[08] APPLIED CHEMICAL CONVERSION COATING AND PRIMER PER AMM 51-21-41-370-802 AND AMM 51-21-72-370-804;[09] VERIFIED CORRECTIVE ACTIONS STEP 8.;[10] UPDATED MEASUREMENTS PARAMETERS ITEM 7 AND 8.;[11] TASK CARD COMPLETE;[12] VERIFIED CORRECTIVE ACTIONS 10;11 AND MEASUREMENT TABLE
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 22.5 BS 867+11.75; BS 867+15.<[01] VERIFIED APPLICABILITY OF SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 AND UPDATED MEASUREMENT TABLE.;[02] TOOL USED DEPTH GAGE ID ATS2472; S/N: UNKNOW; DUE DATE: 12/31/23.;[03] REMOVED CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT AT RBL 22.5 BS 867+11.75 AND BS 867+15: AFTER BLENDOUT AREA: L= 1.5'; W= 0.800'; D= 0.017'; ORIGINAL THIKNESS IS 0.040'; REMAINING MATERIAL : 0.023'; AND IS FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2; ALLOWABLE DAMAGE 2; PARR. 4A;FIG. 103; DETAIL D.;[04] VERIFIED CORRECTION ACTION ITEM 1; 2 AND 3.;[05] LOCATED AND DRILLED NEW ACB FLOOR TO SIDEWALL SUPPORT P/N 146A7502-57 IAW SRM 51-40-05-0G-0. AND DWG. 146A7502; MATERIAL BAC1496-377#7075T62 CLAD. LOT. # 1515191-1.<BR>APPLIED CHEMICAL CONVERSION COATING IAW AMM 51-21-41-370-802.<BR>REQ. OK TO PRIMER.;[06] VERIFIED CORRECTION ITEM 5; OK TO APPLIED CHEMICAL CONVERSION COATING AND PRIMER.;[07] UPDATED MEASUREMENT TABLE.;[08] APPLIED CHEMICAL CONVERSION COATING IAW AMM 51-21-41-370-802 AND PRIMER IAW AMM 51-21-72-370-804.;[09] VERIFIED CORRECTIVE ACTION 8 AND MEASUREMENT TABLE
MULTIPLE AREA OF CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727B TO BS 727E+9.<[01] SRM 53-00-53-1A-2 FOUND TO BE APPLICABLE<BR>UPDATED MEASUREMENT TABLE;[02] SRM 53-00-53-1A-2 FOUND TO BE APPLICABLE<BR>UPDATED MEASUREMENT TABLE;[03] REMOVED CORROSION AT MULTIPLE AREAS ON ACB FLOOR TO SIDEWALL SUPPORT LBL 21 BS 727B TO BS 727E+9.<BR>DEEPEST BLEND L=1.8' W=1.4 D=0.008' REMAINING THICKNESS=0.032' ORIGINAL THICKNESS=0.040' <BR>DAMAGED FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REPAIR BY REPLACEMENT<BR><BR>TOOL USED<BR>DEPTH GAUGE ID:ATS2678 CAL.DUE:02/29/2024;[04] VERIFIED CORRECTION ITEM 3.;[05] TASK WILL BE ACCOMPLISHED AT CUST CARD # TTG800KBW3K;[06] VERIFIED CORRECTIVE ACTIONS STEP 5.;[07] VERIFIED MEASUREMENTS TABLE.;[08] CERTIFY
AFT CARGO BAY - TRACK-TIE DOWN HAS A CORROSION BS 867 RBL 13.5<[01] REMOVED CORROSION AT ACB TRACK-TIE DOWN RBL 13.75; BS 867 IN L=2' X W=1' X D=0.030'' FROM ORIGINAL TICKNESS OF 0.080' FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02 AND SRM 53-00-53-1A-2.<BR>USED TOOL:<BR>ID:NCX000697<BR>S/N:UNKNOWN<BR>DATE:09/2022<BR>DUE:09/2023;[02] CORROSION ON TRACK TIE DOWN IT'S OUT LIMITS WILL BE REPAIRED ON JOB CARD: TTG8Q00KBVA2.;[03] VERIFIED CORRECTION ITEM 1 AND 2 AND MEASUREMENT TABLE; CARD COMPLETE.;[04] VERIFIED CORRECTION ITEM 1;2 ;3 AND MEASUREMENT TABLE; CARD COMPLETE
AFT FLOOR PANEL 241YF UPPER FACESHEET HAS AN AREA OF PULLED STRANDS.<OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR. 4. E. & 4. F.PANEL UPPER SURFACE IS REPAIRABLE IAW SRM 53-00-50-2R-1 AS DIRECTED <BR>BY SRM 53-00-50-2R-0 PAR. 2. A. TABLE 201.REMOVED (15EA) INSERTS FROM AREAS (P1; P13 - P23; P10) IAW SRM <BR>53-00-50-2R-0 PAR. 5. S. (1)(A) & 5. S. (1)(B) REMOVED DAMAGED PLIES AND CORE BY 1IN NEAR (P19) AREA AND CLEANED WITH NO CONTAMINATES NOTED IAW SRM 53-00-50-2R-1 PAR. 3. C. - F.REMOVED DAMAGED UPPER FACESHEET PLIES AND CLEANED WITH NO CONTAMINATES NOTED IAW SRM 53-00-50-2R-1 PAR. 3. A. - F.UPDATED MEASUREMENTS TABLE.;PREPARED POTTING COMPOUND USING BMS5-28 TY19 EPOCAST 1619 LOT#<BR>AK2LP8414K AND FILLED OPEN CORE REPAIR AREA IAW SRM 53-00-50-2R-1 <BR>PAR. 3. G.;SET POTTING COMPOUND FOR HEATLAMP CURE MONITORED BY THERMOMETER ID: ATS2209 CAL/DUE: 10/2023; CURED POTTING AND SANDED SMOOTH AND CLEANED IAW SRM<BR>53-00-50-2R-1 PAR. 3. H. - J. FABRICATED REPAIR PLIES USING BMS9-3 TYH2 CL7 ST1581 LOT#1522395-2 IAW SRM 53-00-50-2R-1 PAR. 3. K. INSTALLED REPAIR PLIES USING BMS8-201 LOT#1522301-1; 53-00-50-2R-1 PAR. 3. M. (1);SRM 53-00-50-2R-1 PAR. 3. M. (1). INSTALLED ALL THROUGH INSERTS USING BMS5-107 LOT#AK2KP8383K AND CURED USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023 IAW SRM 53-00-50-2R-1 PARA 3N.
AFT PANEL 241ZF UPPER FACESHEET HAS AREAS OF PLLED STRANDS.<OUT OF ALLOWABLE DAMAGE LIMITS IAW <BR>SRM 53-00-50-1A-1 PAR. 4. F.PANEL UPPER FACESHEET IS REPAIRABLE IAW SRM 53-00-50-2R-1 AS <BR>DIRECTED BY SRM 53-00-50-2R-0 PAR. 2. A. TABLE 201.<BR><BR>REMOVED (26EA) INSERTS FROM AREAS (P6 - P11; P17 - P26; P31 - P40)<BR>FOLLOWING DWG: 147A5810 ID: 0098 IAW SRM 53-00-50-2R-0 PAR.<BR>5. S. (1)(A) & 5. S. (1)(B REMOVED DAMAGED PLIES AND CLEANED REPAIR AREA WITH NO CONTAMINATES NOTED IAW SRM 53-00-50-2R-1 PAR. 3. A. - C. & 3. E. & 3. F. VALIDATED REPAIR PER SRM 53-00-50-2R-1PREPARED POTTING COMPOUND USING BMS5-28 TY19 EPOCAST 1619 LOT#<BR>AK2LP8414K AND FILLED OPEN CORE REPAIR AREA IAW SRM 53-00-50-2R-1 PAR. 3. G.;[06] SET POTTING COMPOUND FOR HEATLAMP CURE MONITORED BY<BR>THERMOMETER ID: ATS2209 CAL/DUE: 10/2023; CURED POTTING AND SANDED SMOOTH AND CLEANED IAW SRM<BR>53-00-50-2R-1 PAR. 3. H. - J. FABRICATED REPAIR PLIES FROM BMS9-3H2ST1581 LOT#1522395-2; OK TO INSTALL IAW SRM 53-00-50-2R-1 PARA 3K(1).;INSTALLED REPAIR PLIES USING BMS8-201 LOT#1522301-1; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD USING VACUUM GAUGE ATS2441 CAL DUE DATE 08/2023 AND SET FOR CURE USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023. IAW SRM 53-00-50-2R-1 PARA 3K(1)-L(1)-M(1)] INSTALLED ALL THROUGH INSERTS USING BMS5-107 LOT#AK2KP8383K AND CURED USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023 IAW SRM 53-00-50-2R-1 PARA 3N
CORROSION ON PASSENGER CABIN UPPER CHORD AT BS 706 WL 208 RBL 63.<OUT OF LIMITS PER SRM 53-40-13-1A-1 FIG. 103 DETAIL F.;[08] DURING MAINTENANCE; CORROSION WAS FOUND COMMON TO EXISTING PASSENGER CABIN UPPER CHORD AND REMOVED CORROSION AT RBL63; WL 208<BR>BS685+13' L:1' X W:1'<BR>BS685+15' L:1' X W:1'<BR>BS685+18' L:1' X W:1'<BR>BS706+1' L:1' X W:1'<BR>BS706+4' L:1' X W:1'<BR>I.A.W SRM 53-40-13-1A-1 FIG. 103 DETAIL F;[09] VERIFIED CORRECTIVE ACTIONS 7 AND 8.;[10] REQUEST NDI FOR MATERIAL REMAINING THICKNESS ON REWORKED AREAS>REWORKED AREAS FOUND WITHIN LIMITS I.A.W SRM 53-40-13-1A-1 FIG. 103 DETAIL F. APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO REWORKED AREAS PER AMM 51-21-41-370-802; AMM 51-21-72-370-804; FABRICATED; LOCATED AND DRILLED STRAP AND TAPERED FILLERS USING 7075T6 0.080' ALUMINUM SHEET LOT# 1492623-1 AND FILLER USING 7075T6 0.020' ALUMINUM SHEET LOT# 1353253-2 AT BS685+10' - 706+7'; RBL63; WL208 PER SRM 53-40-13-1A-1 4. H APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO REPAIR PARTS PER SRM 53-40-13-1A-1 4. J. INSTALLED STRAP; TAPERED FILLERS; AT BS685+10' - BS706+7'; RBL63; WL208 PER SRM 53-40-13-1A-1 ALTERNATIVE 1 ; SRM 51-40-02-0G-0
CRACK ON PASSENGER CABIN FLOOR SUPPORT AT BS 540 LBL 2 WL 208.<[01] REMOVED PANEL BREAK ASSY LOCATED AT B.S. 540; LBL 2; WL 208 PER SRM 51-10-02-0G-0 PARA: 4.C.(3) AND SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED PANEL BREAK ASSY PER SRM 51-40-05-0G-0; SRM 51-40-06-0G-0 AND DWG #143A5240; REV. B.<BR><BR>REQUESTING OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTIONS STEP 2; OK TO INSTALL GIVEN.;[04] VERIFIED MEASUREMENTS TABLE.;[05] INSTALLED PANEL BREAK ASSY AND LOCATED AND DRILLED FLOOR PANEL FASTENER HOLES LOCATED AT B.S. 540; LBL 2; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-06-0G-0 AND DWG # 1435240 REV. B;[06] VERIFIED CORRECTIVE ACTIONS 5 AND MEASUREMENT TABLE
FWD CARGO BAY FWD SCUFF PLATE CRACKED<[01] WELDED CRACKS ON FWD CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARA 4.B. (2) AND (4).<BR>EQUIP USED: WELDING MACHINE E10583 DUE 01/2024;[02] VERIFIED CORRECTIVE ACTION #1<BR>MEASUREMENT TABLE VERIFIED;[03] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-RADIOMETER ID: ATS2504-A; B; C CAL DUE: 05/23;[04] SANDED WELD REPAIR AREAS SMOOTH PER SRM 53-30-15-2R-1 PARA (5);[05] VERIFIED CORRECTIVE ACTION STEP 4.;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SOPM 20-43-03 AND SOPM 20-41-02;[07] VERIFIED CORRECTIVE ACTION 6.
PASSENGER CABIN FLOOR PANEL 241BF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL FROM BMS4-17 TYPE VI LOT NUMBER 1522265-1 USING BMS5-107 CLASS 1 RESIN LOT NUMBER AK2KP8383K-1 WITH THE INSERTS; CURED RESIN WITH A HEAT LAMP USING THE THERMOMETER ID: ATS2208 DUE: 10/2023 ; TO MONITOR THE TEMPERATURE. WORK PERFORMED IAW DRAWING 144A5810 SHEET 189 AND SRM 53-00-50-2R-0 PARAGRAPH 4.A.(2) AND TABLE 204.;[02] INSPECTED AND VERIFIED CORRECTIVE ACTION 1.;[03] ATTACHED CURE SHEET TO THIS FAULT RECORD.;[04] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 241AF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIGURE 4 TABLE 4 SECTION 44. <BR>CABIN FLOOR UPPER SURFACE EXCEEDS ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-50-1A-1 PARA 4 CONDITIONS A-F REQUIRES REPLACEMENT.<BR>FABRICATE REPLACEMENT FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE:;[02] BEGAN FABRICATING NEW FLOOR PANEL 241AF USING BMS 4-23 LOT#1508290-1 IAW SRM 53-00-50-2R-0 PARA 1.A(NOTE).;[03] COMPLETED FABRICATION OF NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1.A(NOTE).<BR><BR>INSTALLED INSERTS AND CURED USING HEAT LAMP WITH BMS 5-107 LOT#AK2KP8383K-1 IAW SRM 53-00-50-2R-0 PAR. 5.S(1) (D-G) AND BAC DWG 144A5810 ID:0127<BR><BR>PROTECTIVE TAPE TO LOWER SURFACE STILL REQUIRES INSTALL.;[04] CORRECTED MEASUREMENTS TABLE WITH UPDATED INFORMATION.;[05] ADDING TO LINE 3; 'THERMOMETER ID: ATS2209 / CAL DUE DATE: 10/2023';[06] CORRECTION TO LINE 3; 'SRM 53-00-50-2R-0 PAR. 5.S(1) (D-G)' SHOULD READ ' SRM 53-00-50-2R-0 PAR. 5.S(1) (D-H)'.;[07] VERIFIED CORRECTIVE ACTION ITEMS 1-6 AND MEASUREMENTS TABLE.;[08] INSTALLED PROTECTIVE TAPE; AND PART MARKED PANEL IAW BOEING DWG 146A5810-127<BR><BR>JOB COMPLETE;[09] VERIFIED CORRECTIVE ACTION ITEM 8. JOB COMPLETE
PASSENGER CABIN FLOOR PANEL 242DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 242DF IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 B<BR><BR>DUE TO EXTENT OF DAMAGE NEW FLOOR PANEL WILL BE FABRICATED FROM RAW STOCK IAW SRM 53-00-50-2R-0 PAR.1 A(NOTE)<BR><BR>FABRICATED FLOOR PANEL FROM BMS 4-23 TY 2 LOT#1508290-1; INSTALLED (42EA) THROUGH INSERTS USING BMS5-107 CL1 LOT#AK2KP838K-1; CURED INSERTS UNDER HEAT LAMP USING THERMOMETER ID:ATS2208 DUE:10/2023; INSTALLED PROTECTIVE TAPE; AND PART MARKED ALL IAW BOEING DWG 144A5810-123;[02] CORRECTED MEASUREMENTS TABLE; 'REPAIR TYPE' FROM 'MAJOR' TO 'N/A';[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2<BR><BR>VERIFIED MEASUREMENTS TABLE;[04] ATTACHED CURE SHEET TO THIS FAULT RECORD.;[05] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 242AF UPPER SKIN OF AFT O/B CORNER IS DELAMINATED FROM CORE.<[01] DUE TO THE EXTENT OF ALL THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL FROM BMS4-17 TYPE VI LOT NUMBER 1522265-1 USING BMS5-107 CLASS 1 RESIN LOT NUMBER AK2KP8383K-1 WITH THE INSERTS; CURED RESIN WITH A HEAT LAMP USING THE THERMOMETER; ID: ATS2208 DUE: 10/2023; TO MONITOR THE TEMPERATURE. WORK PERFORMED IAW DRAWING 144A5810 SHEET 189 AND SRM 53-00-50-2R-0 PARAGRAPH 4.A.(2) AND TABLE 204.;[02] INSPECTED AND VERIFIED CORRECTIVE ACTION 1.<BR><BR>VERIFIED MEASUREMENTS TABLE.;[03] ATTACHED CURE SHEET TO THIS FAULT RECORD.;[04] JOB COMPLETE.
PASSENGER CABIN FLOOR PANEL 231XF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED 231XF PANEL IAW SRM 53-00-50-0I-1 PARA FIGURE 4; TABLE 4<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F<BR><BR>WILL PERFORM REPAIRS IAW SRM 53-00-50-2R-0<BR><BR>FABRICATED NEW PANEL USING BMS 4-17 TY6 LOT: 1522265-1 IAW SRM 53-00-50-2R-0 PARA 1.A.NOTE. ALONG WITH DWG 144A5819 SHEET: 126<BR><BR>INSTALLED 42EA INSERTS USING BMS 5-107 LOT: AK2KP8383K<BR>CURED RESIN USING THERMOMETER ATS2208 DUE: 10/2023 IAW SRM 53-00-50-2R-0 PARA 5.S.(1) ALONG WITH DWG 144A5810 SHEET: 126<BR><BR>STILL NEEDS FOAM TAPE TO BE INSTALLED;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-0.;[03] VERIFIED CORRECTIVE ACTION ITEMS 1-2.;[04] INSTALLED PROTECTIVE TAPE (BMS8-283TY1 LOT# OCN056291) TO LOWER SURFACE AND VERIFIED PANEL WAS PARTMARKED IAW DRAWING 144A5810 SHT 126.<BR><BR>JOB COMPLETE.;[05] VERIFIED CORRECTIVE ACTION ITEM 4; JOB COMPLETE.
RT WING L/E PANEL 621CB FWD O/B CORNER IS CRACKED<OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A(5).REMOVED INNER SURFACE DAMAGED PLIES AND CLEANED REPAIR AREA FABRICATED REPAIR PLIES FROM BMS 5-129 TY2 GR05 LOT#1521552-3; BMS 8-79 CL3 ST120 LOT#1520138-1; AND BMS 8-79 CL3 ST1581 LOT#1513773-1. INSTALLED REPAIR PLIES; VACUUM BAGGED; LEAK CHECK GOOD USING VACUUM GAUGE ID:ATS2798 DUE:10/23 ;FABRICATED FOIL REPAIR PLY FROM BMS 8-289 LOT#1511321-1 AND INSTALLED FOIL PLY USING BMS 5-128 LOT#1521411-1; VACUUM BAGGED; LEAK CHECK GOOD USING VACUUM GAUGE ID:E11543 DUE:09/23 AND CURED FOIL UNDER HEAT LAMP USING THERMOMETER ID:ATS2209 DUE:10/23. UNBAGGED FOIL AND TRIMMED EXCESS MATERIAL IAW SRM 51-70-14-2R-3 PARA 4.A(3;4); (5(A)) AND (11(A-L)).<BR>INSTALLED 2EA BACKUP PLATES IAW SRM 51-40-02-0G-0 PARA 4.A-C AND BDWG 116A9110 SHEET 31.<BR><BR>PREPARED DAMAGED SURFACE AND INSTALLED ALUMINUM STRIP USING BMS 5-109 LOT#1522019-1; APPLIED PRESSURE AND CURED UNDER HEAT LAMP USING THERMOMETER ID:ATS2209 DUE:10/23 IAW SRM 57-41-01-2R-6 PARA 4.F-M.;[10] REFINISHED PANEL'S TOOLSIDE IAW SRM 51-70-05-2R-6 PARA 4.I.;[
CRACKED LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL34 WL149.<OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR 4.D (1).<BR>A PERMANENT REPAIR WILL BE ACCOMPLISHED IAW SRM 51-70-04-2R-10 AS DIRECTED PER SRM 57-10-10-2R-2 PAR 1.C.;[02] DETERMINED EXTENT OF DAMAGE VIA VISUAL METHOD.<BR>REMOVED DAMAGED AND CONTAMINATED FIBERGLASS PLIES FROM DISCREPANT AREA. PREPARED AREA FOR REPAIR AND CLEANED. <BR>WORKED ACCOMPLISHED IAW SRM 51-70-04-2R-10 PAR 4.A-C.;[03] VALIDATED REPAIR PER SRM 51-70-04-2R-10;[04] VERIFIED CORRECTIVE ACTIONS 1-3 VALIDATED REPAIR PER SRM 51-70-04-2R-10;FABRICATED REPAIR PLIES USING FIBERGLASS BMS 9-3 STYLE 1581; LOT# 1512777-1. <BR>WORK ACCOMPLISHED IAW SRM 51-70-04-2R-10 PAR 4.D.] INSTALLED REPAIR PLIES USING RESIN BMS 8-301; CLASS 1. LOT# JH2EAA8895.<BR>VACUUM BAGGED REPAIR; CHECKED VACUUM BAG FOR LEAKS; VACUUM BAG CHECKED GOOD AND SET REPAIR TO CURE.CALIBRATED TOOLS USED:<BR>VACUUM GAUGE: ATS2798; CAL DUE DATE: 10/2023<BR>HOT BONDER MACHINE: ID: NCX000523; CAL DUE DATE: 06/2023; CURED REPAIR; UNBAGGED REAPIR AND LIGHTLY SANDED REPAIR IAW SRM 51-70-04-2R-10 PARAGRAPH 4.F AND H. PERFORM POST CURE NDI IAW SRM 51-70-04-2R-10 PARAGRAPH 4.G. INSPECTED AND VERIFIED CORRECTIVE ACTION 10.<BR><BR>POST REPAIR UT INSPECTED PER 737NDT PART 4 51-00-02. NO DEFECTS FOUND. TOOL E650 ATS2341 DUE 06/2023.;REFINISHED REPAIR AREA IAW SRM 51-70-04-2R-10 PARAGRAPH 4.H.;[13] FINAL INSPECTION. JOB COMPLETE.
RH EMERGENCY EXIT LIGHT COVER IS LOOSE.(MARKED).<[01] TTGTENED RH EMERGENCY EXIT LIGHT COVER PER MM 33-51-01-960-802;[02] VERIFIED CORRECTIVE ACTION 1
EMERGENCY EXIT LIGHT BATTERY PACK (M1673) FAILS TO TAKE CHARGE / [01] SIGNING AND CERTIFYING FOR AAR EMPLOYEE #28971. REPLACE EMERGENCY LIGHT BATTERY PACK (M1673) EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-51-06-960-805;[02] SIGNING AND CERTIFYING FOR AAR EMPLOYEE #28971. REPLACED EMERGENCY LIGHT BATTERY PACK (M1673) EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-51-06-960-805;[03] ALL WORK C/W<BR>AUDIT C/W
PHOTOLUMINESCENT FLOOR LIGHT STRIP AT SEAT ROW 8ABC IS DISBONDED / [01] REMOVED AND REINSTALLED PHOTOLUMINESCENT STRIP CORRECTLY AT SEAT ROW 8ABC I/A/W AMM 33-51-15-000-802 AND 33-51-15-400-802.
FOUND TWO EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST. / [01] REMOVED & REPLACED TWO EMERGENCY LIGHTING BATTERY PACKS (M01668 & M01669) PER AMM 33-51-06 AND DWG # 33500005.
-RIGHT WTB PNL 191AR TO 191FR VERTICAL SUPPORT CRACKED JUST I\B OF LANDING LIGHT. / [01] REMOVED AND REPLACED VERTICAL SUPPORT AT RIGHT WTB PNL 191AR TO 191FR JUST I/B OF LANDING LIGHT PER SRM 51-40-02
FOUND TWO EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST. / [01] REMOVED & REPLACED TWO EMERGENCY LIGHTING BATTERY PACKS (M01668 & M01669) PER AMM 33-51-06 AND DWG # 33500005.
ELECTRICAL AND ELECTRONICS COMPARTMENT CENTER INTERCOSTAL BETWEEN BS344 AND BS360 IS CRACKED AT THE FASTENER HOLES / [01] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-02.
RIGHT WING LEADING EDGE PANEL 621YB CRACKED ; PANEL CRACKED 2.2 INCHES ALONG THE INBD FWD LEADING EDGE / [01] REMOVED AND REPLACED RIGHT WING L/E ACCESS PANEL 621YB REF AMM 57-41-02
CRACKED FLOOR SUPPORT AT B.S. 540; B.L. 0 - L.B.L. 24.5; W.L. 208.1. / REMOVED & REPLACED FLOOR SUPPORT AT B.S. 540; B.L 0 - L.B.L 24.5; W.L. 208.1. PER SRM 51-40-02 AND DWG # 143A5240 57600U 14APR21
CRACKED FLOOR SUPPORT AT B.S. 540; B.L. 0 - R.B.L. 24.5; W.L. 208.1. / REMOVED & REPLACED FLOOR SUPPORT AT B.S. 540; B.L. 0 - R.B.L. 24.5; W.L. 208.1; PER SRM 51-40-02 AND DWG # 143A5240 57600U 14APR21
L/H SKATE ANGLE CHAFED BS 1016-1132 / REMOVED AND REPLACED L/H SKATE ANGLE LOT# 7550174 AT B/S 1016-1132 DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS ON SRM IAW SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 148A3590 REV: A. 59900U 10APR21
R/H SKATE ANGLE CHAFED BS 1016-1132 / REMOVED AND REPLACED R/H SKATE ANGLE AT BS 1016 TO BS 1132 IAW SRM 51-40-02 AND DWG 148A3590 REV 'A' 57049U 12APR21
CORROSSION AND ABRASION ON SEAT TRACK BS 540-727B; LBL 45; WL 208 / REMOVED CORROSION ON SEAT TRACK BS 540-727B LBL 45 WL 208. AT BS 697 1' X .5' X .026 (CROWN) FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1 REPLACED SEAT TRACK WITH NEW TRACK FROM B.S. 540-727B LBL 45 WL 208 IAW SRM 51-40-02-0G-0 & DRAWING 144A5300 3364C 13APR21
MECHANICAL DAMAGE ON TOP OF SEAT TRACK BS 500B+2 RBL 45 WL208 / REMOVED MECHANICAL DAMAGE ON TOP OF SEAT TRACK BS 500B+2 RBL 45 WL 208 1' X .6 X .004; IS WITHIN LIMITS; APPLIED FINISH TO BARE METAL IAW SRM 53-00-52-1A-1
AFT ENTRY DOOR SLIDE GIRT BINDS IN DOOR WHEN CLOSING DOOR / READJUSTED THE GIRT Z-FOLD TO LIFT GIRT TO PREVENT INTERFERENCE PER AMM 25-61-06-SWA-001 STEP 3.K(3) & TASK CARD 725-61-06
R/H BS 663 GFRP VAPOR BARRIER CRACKED JUST ABOVE HYDRAULIC SERVICE HANDLE / REPAIRED CRACK DAMAGE JUST ABOVE HYDRAULIC SERVICE HANDLE ON R/H BS 663 GFRP VAPOR BARRIER IAW SRM 51-70-04-2R-10 7062U 4-10-21
DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 (LOWER) BEAM TO BE CRACKED IN THEA RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / FORWARD SERVICE DOOR #4 LOWER BEAM REPAIRED PER CUSTOMER RO NO. 0520055-HHR JOB NO. 538720
TRANSVERSE WEB ON LEFT WING T/E UPPER SURFACE PANEL JUST AFT OF AFT PYLON TIP IS CRACKED / REMOVED TRANSVERSE WEB ON LEFT WING; T/E UPPER SURFACE PANEL JUST AFT OF PYLON AND REPLACED WITH NEW TRANSVERSE WEB IAW SRM 51-40-02; SRM 51-40-05. AIPC 57-50-00-36A 59042U 16APR21
FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / FOUND FLIGHT DECK FLOOR DENTS AT B.S. 255 RBL 4 - LBL 14 WL 207.54 TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1 FIG 105 DETAIL D; REPAIRED ON CUSTOMER CARD # 1-A53-33179 REV 1
ACCESS AND RESTORE AFT CARGO BAY FOR CARGO BAY PNL REPLACEMENT / REMOVED AND REPLACED FLOOR PANEL 140BF; SIDEWALL PANEL 141BW; 141FW; 141HW; 142BW; 142FW IAW AMM 25-52-10-400-801 AMM 25-52-06-400-801 AND SRM 51-10-02 PARAGRAPH 9. 59900U 15APR21
FWD CARGO BAY FLOOR PNL 120CF DAMAGED / FABRICATED NEW FCB FLOOR PANEL 120CF FROM 090 CONOLITE; LOT# 1454533-1 PER AMM 25-52-01-201-801 AND DWG 453A1610
AFT CARGO BAY FLOOR PNL 140BF DAMAGED / FABRICATD NEW ACB FLOOR PANEL 140BF FROM 090 CONOLITE; LOT # 1454533-1 PER AMM 25-52-01-201-801 AND DWG 453A2610
RT AFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED, PER AMM 33-51-06.
LT FWD EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED, PER AMM.33-51-06.
EMERGENCY LIGHTS AT ROW 11 & 13 DEF INOPERABLE. REMOVED & REPLACED BATTERY PA (CHARGER). OPS CHECK GOOD, IAW AMM 33-51-06.
SMALL SURFACE CRACK IN RADOME MOD / REMOVED & REPLACED RADOME IAW AMM 53-52-00. P/N OFF 1001002-2; P/N ON 1001002-7B S/N OFF 03103046; S/N ON C186555-17
FLOOR PANEL 120 120CF / REMOVED AND REPLACED PANEL 120 CF IAW AMM 25-52-10
PHOTO ILLUMINATE STRIP LOOSE AT ROW 8. SECURED STRIP IAW SIP.
LT EMERGENCY BATTERY PACK AT ROW 17 FAIL CAPACITY CHECK. R&R BATTERY PACK PER MM.
R1 DOOR GIRT BAR STUCK IN HOLDER. ADJUSTED GIRT BAR HOOKS IAW SIP.
RH FWD EXTERIOR EMERGENCY LIGHT INOP. / REMOVED & REPLACED EMERGENCY BATTERY PACK PER MM.
EMERGENCY ISLE LIGHTS INOP BETWEEN SEAT ROWS 3 FED AND 6 FED. / REMOVED, REPLACED AND PERFORMED INSTALLATION TEST FOR EMERGENCY BATTERY PACK IAW AMM
FWD CARGO AFT LWR BULKHEAD SUPPORT WL 156 STA 500D CORRODED. / REMOVED AND REPLACED FWD CARGO AFT LWR BULKHEAD SUPPORT I-A-W SRM 51-40-02-0G-0. AND BDWG# 143A9481 PO# 731180
FWD CARGO DOOR THRESHOLD WEB RBL28 WL156 STA 458 LOCATED, DRILLED AND INSTALLED WEB IAW SRM'S 51-40-05-0G-0, 51-40-02-0G-0 AND DWG 143A8120 AND 143A8330. 92058U 04/16/19
AFT CARGO DOOR THRESHOLD WEB HAS CORROSION AT RBL 28 WL 156 STATION 794 TO 847 REMOVED THRESHOLD WEB IAW SRM 51-40-02-0G-0, LOCATED AND DRILLED IAW SRM 51-40-05-0G-0 AND BAC DWG 146A8123, REV C, AND INSTALLED IAW SRM 51-40-02-0G-0
FORWARD CARGO L/H FLOOR TO SIDEWALL CORRODED BETWEEN BS. 510 TO BS. 500A+10, LBL 25. / R&R ANGLE IAW SRM AND DWG.
AFT CARGO FLOOR SHIELD CORRODED BETWEEN BS. 767 TO BS. 787, RBL 22. / R&R SHIELD PER SRM & DWG.
L/H FLOOR TO SIDEWALL SUPPORT ANGLE HAS CORROSIOIN FROM STA 747 - 767 WL 156, LBL 25 REMOVED AND REPLACED, IAW SRM 51-40-02-06-0, SRM 53-00-53-2R-5, AND BOEING DWG 146A7500.
FORWARD CARGO DOOR CUTOUT LOWER AFT CORNER SCUFF PLATE CRACKED. / REPAIRED SCUFF PLATE IAW SRM AND DWG.
FORWARD CARGO DOOR CUTOUT LOWER FORWARD CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW SRM AND DWG.
AFT CARGO COMPARTMENT AFT CORNER SCUFF PLATE IS CRACKED / LOCATED AND DRILLED NEW SCUFF PLATE ITEM NUMBER 7530337 PO NO 717935 PER S.R.M. 51-40-05-0G-0 PARA 4(2) AFT CORNER SCUFF PLATE TO BE INSTALLED IN CUSTOMER CARD NO 753-140-00-02Y
R/H FLOOR TO SIDEWALL SUPPORT ANGLE HAS CORROSIOIN FROM STA 727D - 767 WL 156, LBL 25 / REMOVED AND REPLACED IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A7500 57649U 4/11/19
AFT CARGO COMPARTMENT FWD CORNER SCUFF PLATE IS CRACKED / LOCATED AND DRILLED NEW SCUFF PLATE ITEM NUMBER 7530063 PO NO 714262 PER S.R.M. 51-40-05-0G-0 PARA 4(2) FWD CORNER SCUFF PLATE TO BE INSTALLED IN CUSTOMER CARD NO 753-140-00-027
R/H LOWER VAPOR BARRIER CRACKED AT BS. 663. REPAIRED VAPOR BARRIER PER SRM.
***CORROSION*** R2 DOOR INNER CHORD BS 967 - 986; RBL 50; WL 208 / REMOVED + REPLACED R2 DOOR INNER CHORD MOP SILL BS 967 - BS 986 RBL 50 WL 208 IAW SRM 51-40-02-0G-0; SRM 51-40-05; + DWG 147A8501. 56379U 12APR19
***CORROSION*** FLOOR WEB BS 1029; RBL 2; WL 208 / REPAIRED BS 1029 FLOOR WEB RBL 2 WL 208; IAW ATS ER # 19-02792 REV IR DATED 17APR2019 AND SWA EA # 1-753-34639 REV IR DATED 17APR2019.
FLOOR STRAP CORRODED AT BS 1028, LBL 3, WL 208 / REMOVED AND REPLACED FLOOR STRAP IAW SRM 51-40-02-0G-0 AND BOEING DRAWING NUMBER
FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET IAW SRM AND DWG.
PASSENGER CABIN FLOOR BOARD 241AEF HONEYCOMB CORE CREACKED / REPAIRED CRACKED HONEYCOMB CORE ON PASSENGER CABIN FLOOR BOARD 241AEF PER SRM 53-00-50-2R-6. DAMAGE WAS BEYOND ALLOWABLE LIMITS PER SRM 53-00-50-1A-1 PARA 4F
FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19L. R&R GUSSET IAW SRM AND DWG.
AIR TURNBACK/DECLARED EMERGENCY, AFTER TAKEOFF AND LANDING GEAR LEVER RAISED THE GEAR INDICATION LIGHTS SHOWED 3 RED IN BOTH THE UP & OFF POSITION. R&R LANDING GEAR CONTROL LEVER MODULE PER MM.
R1 DOOR EVAC SLIDE OUT OF POSITION. R&R SLIDE PER MT AND AMM.
SUPPLEMENTAL INFORMATION: RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM. 53-31-31
R2 DOOR THRESHOLD EMERGENCY EXIT LIGHT LENS CRACKED. R&R LENS IAW AMM.
L1 DOOR EMERGENCY EXIT SIGN MISSING RED ARROW. R & R SIGN IAW AMM.
R1 DOOR EMERGENCY EXIT SIGN MISSING RED ARROW. R & R SIGN PER AMM.
RIGHT MAIN WHEEL WELL FORWARD BULKHEAD CRACKED BETWEEN RBL 30 TO 35, APPROXIMATELY 12 INCHES FROM OUTBOARD EDGE ON LOWER END. REPAIRED THE BULKHEAD IAW SRM.
RIGHT WHEEL WELL FORWARD BULKHEAD VAPOR BARRIER WEB CRACKED. REPAIRED THE BULKHEAD WEB IAW EA.
RT WHEEL WELL FORWARD BULKHEAD CRACKED. REPAIRED BULKHEAD IAW EA.
EMERGENCY BATTERY PACK M1669 AT BS 603 FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
EMERGENCY BATTERY PACK M1673 AT BS 952 FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
EMERGENCY BATTERY PACK M1668 AT BS 603 FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
EMERGENCY BATTERY PACK M1672 AT BS 952 FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
R1 DOOR EMERGENCY EVAC SLIDE LATCH BRACKET ASSEMBLY BROKEN. R & R SLIDE IAW MAINTENANCE.
RIGHT FWD EMER SLIDE LIGHT INOPERATIVE. R & R FWD EMER LIGHT BATTERY CHARGER IAW MM.
AFT CABIN, LT EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.
AFT CABIN RT EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.
FORWARD CABIN, LT EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.
R1 DOOR LOWER EMER EXIT SIGN LENS BROKEN. R & R LENS IAW MM.
FIRST OFFICERS NR 2 WINDOW FAILED EXTERNAL EMER EXIT RELEASE OPERATIONAL CHECK. ADJUSTED WINDOW IAW AMM.
RIGHT LOWER EMER EXIT OVERWING LIGHT MISSING. INSTALLED LIGHT IAW MM.
FORWARD GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.
LEFT EMERGENCY EXIT LIGHT LENS LOOSE. R & R LIGHT IAW MM.
FLOOR TRACK LIGHTING COVERS CRACKED. REMOVED AND REPLACED FLOOR TRACK LIGHTING COVERS PER MM.
LEFT LANDING GEAR UNSAFE LIGHT ON LANDING. REPAIRED DOWN LOCK ASSY PER MM.
LEFT FORWARD EMERGENCY EXIT LIGHT WIRING LOOSE. SECURED WIRE PER M/M.
EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 18. REMOVED AND REPLACED COVER IAW M/M.
EMERGENCY EXIT FLOOR LIGHTING END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM.
LT EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED LENS PER MM.
R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM.
GEAR DISAGREED, RED LIGHTS ILLUMINATED WHEN GEAR HANDLE IN "OFF" POSITION. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER MODULE PER MM.