N7886A
Registered owner: BANK OF UTAH TRUSTEE, UT (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
Maintenance disclosures
FWD ENTRY DOOR SLIDE GIRT FLAP IS LOOSE. SECURED FWD ENTRY DOOR SLIDE GIRT FLAP IAW MT725-61-06.
EMERGENCY EXIT ROW LIGHT LENS COVER FELL OFF. SECURED LIGHT LENS PER 33-51-01.
LH AFT FUSELAGE EMERGENCY EXIT LIGHT INOP. REPLACED LH AFT FUSELAGE EMERGENCY EXIT LIGHT IAW AMM 33-51-04-960-801 TEST IS OK.
ACCOMPLISH REPAIR ON FLOOR STRUCTURE SEAT TRACK LOC BTW BS 727C TO BS 727D AND AT LBL 24.75 2025-417409<[01] PERFORMED REPAIR ON FLOOR STRUCTURE SEAT TRACK LOC BTW BS 727C TO BS 727D AND AT LBL 24.75 I.A.W EA 25-153-02012;[02] PERFORMED REPAIR ON FLOOR STRUCTURE SEAT TRACK LOC BTW BS 727C TO BS 727D AND AT LBL 24.75 I.A.W EA 25-153-02012<BR>SEE INDIVIDUAL SIGN OFF BELOW<BR>RII
FWD CARGO COMPARTMENT 540 BULKHEAD VERTICAL STRUCTURE STIFFENER HAS CRACK STA 540 LBL 24.97. REPLACED FWD CARGO COMPARTMENT BULKHEAD VERTICAL STRUCTURE STIFFENER ON STA 540 LBL 24.97 IAW-B737-700 SRM 51-40-02-0G-0; SRM- 51-10-02-0G-0; DWG# 111A2001 SHEET 77 REV - AND DWG# 111A6000 SHEET 283 REV -.
ELONGATED HOLES ON ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-9 REPAIR 9. S
CRACK SUPPORT BRACKET ON BODY STATION 540 LOCATED RBL5 AT AIR CONDITIONING BAY REPLACED SUPPORT BRACKET ON BODY STATION 540 LOCATED RBL5 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.
BROKEN EMERGENCY EXIT LIGHT SWITCH GUARD ON LAVATORY B AFT GALLEY AREA. REPLACED EMERGENCY EXIT LIGHT SWITCH GUARD ON LAVATORY B AFT GALLEY AREA I.A.W CMM BAE SYSTEM 33-11-05 REV.16 FIG.2 ITEM (15) PAGE 10028.
ELONGATED HOLES ON ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.
ELONGATED HOLES ON ACCESS PANEL 561BB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.
ELONGATED HOLES ON ACCESS PANEL 661AB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661AB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-9 REPAIR 9.
CRACK ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA927 TO STA947.5 AND BL0 AT AFT GALLEY AREA. REPLACED ANGLE LOCATED ON FLOOR STRUCTURE BETWEEN STA927 TO STA947.5 AND BL0 AT AFT GALLEY AREA IAW SRM 51-10-02-0G STEP 9 AND DWG 147A5400 SHEET 22 REV -.
CRACK ON INBOARD AND OUTBOARD ANGLE LOCATED INBOARD AUXILIARY TRACK SLAT 1 AT LT WING (2E/A). REPLACED INBOARD AND OUTBOARD ANGLE LOCATED INBOARD AUXILIARY TRACK SLAT 1 AT LT WING (2E/A) IAW B737-700 CMM-57-43-01 PAGE 702 STEP 3 C ITEM (9).
DEBONDED SEAL LOCATED ACCESS PANELS 632KB 632JB AT RT WING. INSTALLED SEAL LOCATED ACCESS PANELS 632KB 632JB AT RT WING IAW B737-700 AMM 28-11-11-900-801.
CRACK KEEL BEAM LOCATED BS 727 TO 727A AND S-28R AT AFT CARGO COMPARTMENT 2025-417115<[01] TOOL USED ON ITEM 5 AND 6: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210136503; DUE DATE: 24-JUL-25;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP -3000 ; S/N : 1859843 ; DUE DATE: 07/OCT/25;[03] TOOL USED: POWER PACK: P/N: PE1068; S/N: PE0318-95852; DUE DATE: 12-OCT-25; THERMOMETER P/N: FLUKE 566; S/N: 65060015WS; DUE DATE: 23-OCT-25.;[04] PERFORMED REPAIR ON KEEL BEAM LOCATED BS 727 TO BS 727A AND S-28R AT AFT CARGO COMPARTMENT INSTALLED IAW EA 25-153-01836. SEE INDIVIDUAL SIGN OFFS BELOW.;[05] RII COMPLETED JOB
CRACK TIE CLIP LOCATED BS 277 AND S10R PASSENGER CABIN. REPLACED TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN IAW SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV-.
BURNED EXIT LIGHT ASSY AT G4 (1EA) AFT GALLEY AREA. REPLACED EXIT LIGHT ASSY AT G4 (1EA) AFT GALLEY ARE IAW AMM 33-51-01-960-801 STEP 2.C.(1)(3) AND (4) FOR OPERATIONAL TEST SEE TTG8Q00CWKNC STEP 60 AND TTG8Q013GD1U.
CRACK WEB INTERCOSTAL LOCATED BETWEEN STA294.5 TO STA303.9 AND STR16L AT FWD GALLEY AREA. REPLACED WEB-INTERCOSTAL LOCATED BETWEEN STA294.5 TO STA303.9 AND STR16L AT FWD GALLEY AREA IAW SRM 51-40-02; SRM 51-10-02 AND DWG 141A8180 SHEET 27 AND 28 REV C.
CRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 264 DEFLECTION CONTROL RIB AREA AT RT WING. REPLACED SUPPORT ANGLE LOCATED AT LEVEL ORSS 264 DEFLECTION CONTROL RIB AREA AT RT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 8 REV -.
CRACK ON WEB LOCATED AT LEVEL ORSS 268 DEFLECTION CONTROL RIB AREA AT LT WING. REPLACED WEB LOCATED AT LEVEL ORSS 268 DEFLECTION CONTROL RIB AREA AT LT WING IAW SRM- 51-40-02-0G-0 AND DWG # 115A2512 SHEET 14 REV A.
CRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 265 DEFLECTION CONTROL RIB AREA AT LT WING. REPLACED SUPPORT ANGLE LOCATED AT LEVEL ORSS 265 DEFLECTION CONTROL RIB AREA AT LT WING IAW SRM-51-40-02 AND DWG 115A2930 SHEET 7 REV-.
CRACK ACCESS PANEL 341B RIB 151.75 AT RT HORIZONTAL STABILIZER. REPLACED ACCESS PANEL 341B RIB 151.75 AT RT HORIZONTAL STABILIZER IAW SRM 51-40-02; SRM 51-10-05 ITEM 9 AND DWG 186A1001; SHEET 19; REV -.
INOP EMERGENCY EXIT LIGHT BATTERY PACK LOCATED BETWEEN STA727B AND STA727C STR16L AND STR17L AT PASSENGER CABIN (1 EA). REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK LOCATED BETWEEN STA 727B AND STA 727C STR 16L AND STR 17L AT PASSENGER CABIN (1 EA) IAW AMM 33-51-06-960-805 AND PERFORMED A TEST OF THE NEW BATTERY PACK IAW B737-700 AMM 33-51-06-960-805 TEST IS OK.
INOP PACK BATTERY EMERGENCY EXIT LIGHT ON ENTRY CEILING AT AFT GALLEY AREA (1 EA). REPLACED EMERGENCY LIGHT POWER SUPPLY-BATTERY PACK ON ENTRY CEILING AT AFT GALLEY AREA (1 EA) I.A W B737-700 AMM 33-51-06-960-805. TEST IS OK.
INOP EMERGENCY EXIT LIGHT BATTERY PACK CEILING ENTRY AT FWD GALLEY AREA (2 EA). REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK CEILING ENTRY AT FWD GALLEY AREA (2 EA) IAW B737-700 AMM 33-51-06-960-805 AND PERFORMED A TEST OF THE NEW BATTERY PACKS IAW B737-700 AMM 33-51-06-960-805 TEST IS OK.
ELONGATED HOLES ON FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT 2025-417087<[01] FABRICATED NEW FLOOR PANEL 120CF ON FWD CARGO COMPARTMENT IAW-B737-700-SRM 51-40-02-0G-0; SRM-51-20-01 AND DWG# 453A1610 SHEET 23 REV C. SEE INDIVIDUAL SIGN OFF BELOW;[02] FABRICATED NEW FLOOR PANEL 120CF ON FWD CARGO COMPARTMENT IAW-B737-700-SRM 51-40-02-0G-0; SRM-51-20-01 AND DWG# 453A1610 SHEET 23 REV C. SEE INDIVIDUAL SIGN OFF BELOW
ELONGATED HOLES ON FLOOR PANEL 120AF AT FWD CARGO COMPARTMENT 2025-417085<[01] FABRICATED NEW FLOOR PANEL 120AF ON FWD CARGO COMPARTMENT IAW-B737-700-SRM 51-40-02-0G-0; SRM-51-20-01 AND DWG#143A1610 SHEET 9 REV F. SEE INDIVIDUAL SIGN OFF BELOW;[02] FABRICATED NEW FLOOR PANEL 120AF ON FWD CARGO COMPARTMENT IAW-B737-700-SRM 51-40-02-0G-0; SRM-51-20-01 AND DWG#143A1610 SHEET 9 REV F. SEE INDIVIDUAL SIGN OFF BELOW
ELONGATED HOLES ON FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT 2025-417086<[01] FABRICATED NEW FLOOR PANEL 120BF ON FWD CARGO COMPARTMENT IAW-B737-700-SRM 51-40-02-0G-0; SRM-51-20-01 AND DWG# 453A1610 SHEET 29 REV B. SEE INDIVIDUAL SIGN OFF BELOW;[02] FABRICATED NEW FLOOR PANEL 120BF ON FWD CARGO COMPARTMENT IAW-B737-700-SRM 51-40-02-0G-0; SRM-51-20-01 AND DWG# 453A1610 SHEET 29 REV B. SEE INDIVIDUAL SIGN OFF BELOW
CRACK GUSSET STA 500D STR 19L FWD CARGO COMPARTMENT. REPLACED GUSSET LOC. STA 500D STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G STEP 9; SRM 51-40-02-0G-0 AND DWG 143A7902 SHEET 209 REV -.
CRACK BULKHEAD PANEL 121EW AT FWD CARGO COMPARTMENT 2025-417078<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: B23304029; DUE DATE: 10- NOV-25.;[02] PREPARED REPAIR AREA AND APPLIED REPAIR PATCH ON BULKHEAD PANEL 121EW AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-300-804 SEE INDIVIDUAL<BR>SIGNOFF BELOW.;[03] CORRECTED STEP 2. REPARED BULKHEAD PANEL 121EW AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-300-804 SEE INDIVIDUAL<BR>SIGNOFF BELOW.;[04] REPAIRED BULKHEAD PANEL 121EW AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-300-804 SEE INDIVIDUAL<BR>SIGNOFF BELOW.
CRACK INDICATION ON STUB FRAME LOCATED BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FWD GALLEY DOOR AREA. REPLACED STUB FRAME LOCATED BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FWD GALLEY DOOR AREA IAW SRM 51-10-02 ITEM. 9 AND 51-40-02 AND DWG 141A8370 SHEET 9 REV D;SHEET 10 REV D; SHEET 10 REV D.
CRACKED GUSSET STA 500D AND STR 19R FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED ON STA 500D AND STR 19R FWD CARGO COMPARTMENT IAW B737 700 SRM 51-10-02-0G STEP 9; SRM 51-40-02-0G AND DWG 143A7902 SHEET REV -.
CRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT 2025-417042<[01] FABRICATED NEW FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT IAW-B737-700-SRM 51-40-02-0G-0; SRM-51-20-01 AND DWG#143A2610 SHEET 20 REV E. SEE INDIVIDUAL SIGN OFF BELOW;[02] FABRICATED NEW FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT IAW-B737-700-SRM 51-40-02-0G-0; SRM-51-20-01 AND DWG#143A2610 SHEET 20 REV E. SEE INDIVIDUAL SIGN OFF BELOW
BOLT MISSING FROM FWD ENTRY DOOR ESCAPE SLIDE.<[01] INSTALLED BOLT ON FWD ENTRY DOOR ESCAPE SLIDE REF AMM 25-66-01.
AFT ENTRY DOOR GIRT BAR HOLD DOWN TRIM PLATE SCREW MISSING PLATE IS STICKING UP FA SAYS ITS A TRIP HAZZARD <[01]. REPLACED SCREW PER AMM 25-27-21.
PASSENGER CABIN FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS NOT ATTACHED.<[01] REATTACHED PASSENGER CABIN FWD ENTRY DOOR EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01.
DURING CLIMBOUT THERE WAS A CLICK SOUND AND THEN THE LOWER DU BLANKED; THE LEFT FWD;RIGHT AFT AND LEFT CTR FUEL LOW PRESSURE LIGHTS ILLUMINATED; THE FORWARD WINDOW HEAT LIGHTS ILLUMINATED;ALL AMPS AND VOLTS APPEARED TO BE NORMAL<[01] FOUND C/B XFER BUS 1 SECTION 2 POPPED BEHIND P-91 PANEL. INSPECTED WIRING FOR OBVIOUS DEFECTS ON FUEL BOOST PUMPS; VISIBLE WIRING FROM P-91 PANEL FWD IN E&E TO COCKPIT AND WIRING FROM FLOOR TO ASSOCIATED SYSTEMS BEHIND P-6 PANEL REF WDM 24-51-11;[02] REMOVED P91 PANEL PER AMM 24-21-21. INSPECTED P91 PANEL CHECK CONTINUITY FROM A2 TO J2A; B2 TO J2B; C2 TO J2C AND FOR SHORTS. NO FAULTS FOUND. REPLACED C3002 AND C0801 PER AMM 24-61-01 AND SWPM 20-30-00.;[03] OPS NORMAL AT THIS TIME.
FWD LOWER FA FLASHLIGHT INOP<[01] REPLACED FLASHLIGHT BATTERY IRT AMM 25-64-00. OPS CHECK OK.
L1 DOOR SLIDE PARTIALLY DEPLOYED<[01] REPLACED SLIDE PER MT 725-61-06
SWA - REPAIR - NG DOOR SLIDE COVER GIRT BAR RETAINER CLIP MISSING FASTENERS - PERMANENT<[01] REPLACED MISSING FASTENER ON NG DOOR SLIDE COVER GIRT BAR RETAINER CLIP PER SRM 51-40-02
FWD GIRT BAR ASSEMBLY BRACKET LOOSE.<[01] INSTALLED TEMPORARY REPAIR FASTENER IAW EA M-23-125-01839.
WHILE WORKING CUSTOMER CARD TTG8Q00MWAWZ FOUND CORROSION ON NUTPLATE STRAP P/N 146A8128-18 BS 794-801 RBL 19 W/L 155<[01] UPDATED STEPS 1 AND 2;[02] UPDATED STEPS 1 AND 2;[03] UPDATED STEP 2.;[04] REMOVED DAMAGE NUT PLATE STRIP AND INSTALLED NEW NUT PLATE STRIP IAW SRM 51-40-02-0G-0; DWG 146A8340 ID:0022 REV:A;[05] VERIFIED CORRECTIVE ACTION #4<BR>VERIFIED MEASUREMENTS
PANEL 195CL HAS A CRACK IN THE AFT EDGE LOWER RADIUS<[01] REPAIRED CRACK DAMAGE IN THE AFT EDGE LOWER RADIUS OF PANEL 195CL IAW SRM 51-70-05-2R-6.;[02] FINAL INSPECTION. JOB COMPLETE.
CORROSION ON 727D SIDEWALL SUPPORT ON FWD SIDE OF FRAME BETWEEN STR 24L AND 25L<[01] UPDATE STEP 1;[02] STEPS 2 & 3 COMPLETE.;[03] STEP 4 COMPLETE.;[04] REMOVED AND REPLACED NEW CHANNEL SIDEWALL SUPPORT AT BS 727D BETWEEN STR 19 TO STR 25 LH IAW SRM 51-40-02-0G-0 AND DWG 146A1220; ID: 0052; REV:-;[05] VERIFIED CORRECTIVE ACTION ITEM 4. <BR>VERIFIED MEASUREMENT TABLE COMPLETE.
FWD CABIN SERVICE DOOR SURROUND LOWER STUB FRAME CRACKED BS294 RBL55 WL209.<[01] INSTALLED NEW FSD LOWER SURROUND LOWER FRAME AT BS294 RBL55 WL209 PER SRM 51-40-05-0G-0 AND DWG 141A8370.;[02] UPDATED PART;[03] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.;[04] JOB CARD COMPLETED
CRACKED INTERCOSTAL AT FWD CABIN BS344+6 BL0 WL208.<[01] REMOVED CRACKED INTERCOSTAL AT FWD CABIN BS344+6 BL0 WL208 <BR>PER <BR>SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT);[02] VERIFIED ACTION 1.;[03] UPDATE STEPS 2-4;[04] VERIFIED ACTION 3.;[05] VERIFIED STEPS 1;2;3;4 OK TO INSTALL GIVEN.;[06] COMPLETED STEP 3;[07] VERIFIED ACTION 6;[08] FOUND NO LIMITATIONS FOR CRACKS IN SRM; REMOVED AND REPLACED INTERCOSTAL BL0; BS 340-360 PER SRM 51-40-02.;[09] VERIFIED ACTION 8.;[10] CORRECTED MEASUREMENT FIELD.;[11] COMPLETE;;[12] EDITIED MEASUREMENT TABLE;[13] VERIFIED;[14] VERIFIED CORRECTIVE ACTION 8. INTERCOSTAL REPLACED PER SRM 51-40-02 AND DWG 141A5400
CORROSION ON FWD SERVICE DOOR THRESHOLD SUPPORT ANGLE BS311 RBL57 WL208.<[01] UPDATED STEP 1;[02] UPDATED STEP 2;[03] UPDATED STEP 2;[04] UPDATED MEASUREMENT TABLE;[05] CERTIFY EDIT;[06] CORRECTED ENTRY 17 ON MEASUREMENT TABLE;[07] CERTIFIED EDIT TO MEASUREMENT TABLE;[08] UPDATED STEP 4.;[09] UPDATED PARTS USED;[10] FINAL SUMMARY; FOUND CORROSION ON FWD SERVICE DOOR THRESHOLD SUPPORT BS 311 RBL 57; WL208 TO BE OUT OF LIMITS PER SRM 53-10-15-1A-2; REMOVED AND REPLACED PART.
CRACKED ATTACH ANGLE AT FWD PASSENGER CABIN BS294 RBL54 WL208.<[01] INSTALLED NEW ATTACH ANGLE AT FWD PASSENGER CABIN BS294 RBL54 WL208 PER SRM 51-40-05-0G-0 AND DWG 141A8310.;[02] VERIFIED CORRECTIVE ACTION #1
CORROSION ON SIDEWALL SUPPORT AT ACB BS727D S-25L LBL25. MARKED.<[01] EVALUATED DAMAGE ON SIDEWALL SUPPORT AT ACB BS727D S-25L LBL25 FOUND TO BE OUT OF LIMITS FOR NO ALLOWABLE DAMAGE PER SRM. PART IS TO BE REPLACED ON CUSTOMER CARD NUMBER TTG8Q00N0UTL.;[02] VERIFIED CORRECTION ACTION ITEM 1; REPLACED ON CUSTOMER CARD NUMBER TTG8Q00N0UTL; CARD COMPLETE.;[03] VERIFIED CORRECTION ACTION ITEM 1; MEASUREMENT TABLE; REPLACED ON CUSTOMER CARD NUMBER TTG8Q00N0UTL; CARD COMPLETE.
CRACKED ATTACH ANGLE AT ACB BEHIND WATER SERVICE PANEL BS918 RBL12 WL171.<[01] UPDATED STEP 1.;[02] UPDATED STEPS 1-3.;[03] UPDATED STEP 2.;[04] CORRECTION ON STEP 2 RBL TO RBL POSITION.;[05] DWG 147A7221;[06] REMOVED AND REPLACED NEW STIFFENER(ATTACH ANGLE) PN 147A7221-32 IAW SRM 51-40-02 AND DWG 147A7221;[07] VERIFIED CORRECTIVE ACTION ITEM 6.
CORROSION ON WEB AT ACB BS786 RBL20 WL157.<[01] UPDATED STEP 1;[02] UPDATED MEASUREMENTS.;[03] UODATED STEP 2;[04] FIXED PART# IN MEASUREMENTS.;[05] PARTIAL UPDATE TO STEP 3;[06] PARTIAL UPDATE STEP 5;[07] UPDATED STEP 7;[08] FIXED PART NUMBER ON MEASUREMENT TABLE;[09] DISCREPANCY BS NUMBERS DO NOT MATCH MEASUREMENT TABLE NUMBERS;[10] UPDATED STEP 8;[11] UPDATED STEP 8 AND 9;[12] UPDATED 1;2;6; AND 8;[13] REMOVED DAMAGE FROM WEB IN A 1.0LX2.0W AREA IAW SRM 51-10-02.<BR><BR>ORIGINAL MATERIAL THICKNESS : 0.055' DAMAGE REMOVED : 0.006' REMAINING THICKNESS : 0.049' DAMAGE EXCEED 10% OF ORIGINAL THICKNESS; FOUND TO BE OUT OF LIMIT IAW SRM 53-60-15-1A-1<BR><BR>REMOVED WEB BETWEEN BS 767 TO 787 RBL20 IAW SRM 51-40-02-0G-0<BR><BR>LOCATED AND DRILLED ACB WEB IAW SRM 51-40-05-0G-0 AND DWG 146A8123 ID: 0017 REV:-<BR><BR>INSTALLED ACB WEB AT RLB20 BS767-787 IAW SRM 51-40-02-0G-0 AND DWG 146A0081 ID:0031 REV:-
CORROSION ON WEB AT ACB BS767+15 RBL20 WL157.<[01] UPDATED MEASUREMENTS.;[02] PARTIAL UPDATE TO STEP 1 AND 2;[03] CORRECTED STEP 3 TO INCLUDE EQUIPMENT USED.;[04] THIS WORK TO BE COMPLETED BY CUST SYSTEM ID : TTG8Q00MWC6J;[05] THIS FAULT BEING REFERENCED TO TTG8Q00MWC6J. PART NUMBERS ON THE MEASUREMENT TABLES DO NOT MATCH EACH OTHER. IF THIS IS NOT THE SAME PART NUMBER THEN THE ITEM MAY NOT BE REFERRED.;[06] UPDATED STEP 4
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS927+6 RBL21 WL177.<[01] UPDATED STEP 1 AND 2;[02] UPDATED STEP 3;[03] UPDATED STEP 4;[04] VERIFIED STEP 4 IN PARTIAL.;[05] UPDATED STEP 3;[06] VERIFIED STEP 3 IN PARTIAL.;[07] UPDATED STEP 5<BR><BR>THERE IS NO SRM ALLOWABLE DAMAGE FOR ACB INTERCOSTAL AT ACB BS927+6 RBL21 WL177. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0<BR><BR>REMOVED INTERCOSTAL IAW SRM 51-40-02-0G-0<BR><BR>LOCATED AND DRILLED NEW INTERCOSTAL IAW SRM 51-40-05-0G-0 AND DWG 147A7500 ID:0028 REV:-<BR><BR>INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02-0G-0 AND DWG 147A7500 ID:0028 REV:-<BR><BR>APPLIED BMS10-11 TYPE2 ENAMEL (WHITE PAINT) IAW SOPM 20-41-02;[08] VERIFIED CORRECTIVE ACTION #7;[09] UPDATED MEASUREMENTS FIELDS;[10] INSTILLATION OF THIS PRIMARY STRUCTURE IS RII AND MUST BE REVERIFIED.;[11] VERIFIED CORRECTIVE ACTIONS STEP 7.
CORROSION ON TRACK TIEDOWN AT ACB BS787+4 LBL17 WL158.<[01] UPON FURTHER INVESTIGATION THERE IS A CRACKED AT ACB TRACK AT LBL 17 WL 158 P/N: 146A7501-1. TRACK WILL BE REPAIRED BY REPLACEMENT ON CUST CARD # TTG8Q00MWAXE;[02] UPON FURTHER INVESTIGATION THERE IS A CRACKED AT ACB TRACK BS 767 LBL 17 WL 158 P/N: 146A7501-1. TRACK WILL BE REPAIRED BY REPLACEMENT ON CUST CARD # TTG8Q00MWAXE;[03] VERIFIED CORRECTIVE ACTION ITEM 2 AND MEASUREMENT TABLE; CARD COMPLETE.
CORROSION ON FWD SHIELD ATTACH ANGLE BS767+1 RBL21 WL157.<[01] UPDATED STEPS 1-4; 6.;[02] UPDATED STEP 5;[03] UPDATED STEP 7;[04] UPDATED STEP 3 AND 7;[05] UPDATED STEP 3 AND 7;[06] ALL STEPS COMPLETE. REMOVED AND INSTALLED NEW REPLACEMENT ANGLE. IAW SRM 51-40-02; DWG 146A8123 ID:0016 REV:-; DWG 146A0081 ID:0031 REV:-; SRM 51-40-05; SRM 51-40-06; SRM 51-10-02.;[07] VERIFIED CORRECTIVE ACTION #6
CRACKED TRACK AT ACB BS767 RBL13 WL157.<[01] PARTIAL STEP 1-3;[02] COMPLETED STEP 2;[03] COMPLETED STEP 4-5-6 AND 8;[04] PARTIAL STEP 9-11;[05] UPDATE STEPS 9-11.;[06] REMOVED AND REPLACED CARGO TRACK FROM B/S 727 TO B/S 787 RBL 13 WL 157 IAW SRM 51-40-02; AND SRM 51-10-02 PARAGRAPH 9 AND DWG 146A7500 REV:- DUE TO FOUND OUT LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 AND PERFORMED REPAIR SPLICE BTW B/S 767 TO 747 IAW SRM 53-00-53-2R-3 REPAIR 3;[07] VERIFIED CORRECTIVE ACTION COMPLETE.
CORROSION ON STRAP AROUND NUT PLATES AT ACB BS787+3 RBL20 WL151.<[01] UPDATED MEASUREMENTS;[02] PARTIAL UPDATE TO STEPS 1; 2.;[03] UPDATED STEP 2;[04] CORRECTION TO LINE 1: FIXED MEASUREMENT #19 TO MINOR;[05] STEP 1 REQ. OK TO INSTALL NEW STRAP.;[06] STEP 1; OK TO INSTALL.;[07] UPDATED STEP 1.;[08] REMOVED DAMAGE NUT PLATE AND INSTALLED NEW NUT PLATE IAW SRM 51-10-02; SRM 51-40-02-0G-0; AND DWG. 146A0081.;[09] VERIFIED COMPLETE. <BR>VERIFIED MEASUREMENTS.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727A - BS727D; BS747 - BS807 LBL21 WL157.<[01] VERIFIED STEPS 4;5 IN PARTIAL.;[02] VERIFIED STEPS 4;5 IN PARTIAL.;[03] VERIFIED STEP 6 IN PARTIAL.;[04] OK TO INSTALL<BR>STEP 3;[05] UPDATED STEP 3;[06] COMPLETED STEP 3.;[07] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY.;[08] EDIT TO CORRECTIVE ACTION 7; REFERENCES USED: DWG 146A7502; DWG 146A7500; SRM 53-00-53-2R-6; AND SRM 51-40-02.;[09] VERIFIED CORRECTIVE ACTION STEP 7. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
CORROSION ON STRAP AT ACB BS787+5; BS787+13; BS787+17. BS827+15; RBL19 WL156.<[01] ENTERED MEASUREMENTS;[02] PARTIAL ON STEPS 1-5;[03] STEP 5 PARTIAL;[04] UPDATED STEP 2.;[05] REMOVED DAMAGE; EVALUATED; FOUND PART (IN-LIMTS) THEN TREATED AND PRIMED IAW SRM 53-60-15-1A-1; SRM 53-60-151A-1; 4G; (3)(B) FIGURE 103; DETAIL G; SRM 51-10-02; SRM 51-40-02;[06] VERIFIED COMPLETE.
CRACKED TRACK AT ACB BS767 LBL17 WL157.<[01] UPDATED STEP 1 AND 2;[02] UPDATED STEP 3;[03] PARTIAL ON STEP 3;[04] UPDATED STEP 3;[05] CHANGED STEP 4 TO PARTIAL;[06] SIGNED FOR PART;[07] CRACK ON AFT BAY CARGO TIEDOWN TRACK BS 767 LBL 17 WL 157; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; REMOVED TRACK BS 727-867; LOCATED; DRILLED AND INSTALLED TIEDOWN TRACK IAW SRM 51-40-02-0G AND DWG 146A7500;[08] VERIFIED CORRECTIVE ACTION #7
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE AT STA: 500A+2; 500A+6; 500A+10; & 500B+18; WL 156; RBL 24.5< FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2<REMOVED AND REPLACED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0G AND DWG 143A7500 ID:0071 REV:-;[14] REMOVED DAMAGE AT<BR>STA 500A+2 0.006 (OUT OF LIMIT)<BR>STA 500A+6 0.008 (OUT OF LIMIT)<BR>STA 500A+10 0.010 (OUT OF LIMIT)<BR>STA 500B+18 0.007 (OUT OF LIMIT)<BR><BR>ORIGINAL MATERIAL THICKNESS : 0.040; THE DEEPEST DAMAGE : 0.010 (AT STA 500A+10); REMAINING THICKNESS : 0.030. ALL DAMAGE EXCEED 10% OF ORIGINAL THICKNESS. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 FABRICATED NEW FLOOR TO SIDEWALL SUPPORT MATERIAL USING BAC1496-444#7075T662 .040 LOT#:1509343-1 IAW SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 143A7501 ID:0114 REV:-<BR><BR>APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02<BR><BR>APPLIED BMS 10-11 TYPE 2 ENAMEL COATING (WHITE PAINT) IAW SOPM 20-41-02<BR><BR>REMOVED AND REPLACED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0G AND DWG 143A7500 ID:0071 REV:-;[
APU COMPESSOR SCROLL HOUSING HAS INTERSECTING CRACKS NEAR THE EXIT DUCT.<[01] FOUND TO BE OUT OF LIMITS PER AMM 49-11-00 PART REPLACEMENT REQUIRED PER AMM 49-11-00 STEP 2 E. (F) 1);[02] UPDATED MEASUREMENTS VERIFIED;[03] VERIFIED FOUND TO BE OUT OF LIMITS PER AMM 49-11-00 PART REPLACEMENT REQUIRED PER AMM 49-11-00 STEP 2 E. (F) 1) UPDATED MEASUREMENTS VERIFIED;[04] REMOVAL AND REPLACEMENT OF APU DOCUMENTED ON TASK CARD 749-11-01; ID# TTG8Q00MV159.;[05] VERIFIED;[06] CORRECTION STEP 4. REMOVAL AND REPLACEMENT OF APU DOCUMENTED ON TASK CARD 749-11-01; ID# TTG8Q00J0080;[07] VERIFIED CORRECTIVE ACTION STEP 4. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
INTERCOSTAL CRACKED BS380-400; WL208; RBL10<[01] UPDATED STEP #1;[02] UPDATED STEP #2;[03] UPDATED STEP #3;[04] UPDATED STEP #3;[05] COMPLETED REMAINING AMT STEPS;[06] COMPLETED STEPS;[07] UPDATED PART REQUIREMENT;[08] OPENED STEP 5 FROM COMPLETE TO PARTIAL.;[09] REMOVED AND REPLACED UPPER ANGLE ON INTERCOSTAL B.S. 380-400 PER SRM 51-40-02.
CORROSION ON FWD CARGO BAY DOOR CUT-OUT AFT SHIELD AT STA: 500+6 & 500+10; WL 156; RBL 24.5.<[01] COMPLETED STEP 1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] UPDATED MEASUREMENT TABLE.;[04] UPDATED STEPS 2 AND 3.;[05] EDIT TO STEP 3; NOW HAS CORRECT REFERENCE.;[06] UPDATED STEP 2;4;5;AND 6;[07] NO SRM ALLOWABLE DAMAGE WAS FOUND TO BE APPLICABLE. REPAIR BY REMOVAL AND REPLACEMENT OF PART IAW SRM 51-10-02-0G-0 9.C.<BR><BR>REMOVED FWD CARGO BAY DOOR CUT-OUT SHIELD IAW SRM 51-40-02-0G-0.<BR><BR>LOCATE AND DRILLED NEW FWD CARGO BAY DOOR CUT-OUT SHIELD IAW SRM 51-40-05-0G-0 AND DWG 143A0080.<BR><BR>APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02<BR><BR>APPLIED BMS 10-11 TYPE 2 ENAMEL COATING IAW SOPM 20-41-02<BR><BR>INSTALLED NEW FCB DOOR CUTOUT SHIELD IAW SRM 51-40-02-0G-0 AND DWG 143A0080 ID:0023 REV:-;[08] VERIFIED CORRECTIVE ACTION #7<BR>VERIFIED MEASUREMENTS
CORROSION; AFT WET AREA; BS1016; WL208;LBL12; AROUND FASTENER HEAD<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02. <BR>REMOVED CORROSION FROM WEB AT AFT WET AREA; BS1016; WL208;LBL12 IN AN AREA OF L: 3' X W: 1' PER SRM 51-10-02-0G-0. THE SRM DOESN'T HAVE ALLOWABLE DAMAGE FOR THE WEB. WEB ORIGINAL THICKNESS .040';[02] CERTIFIED CORRECTIVE ACTION 1;[03] UPDATED MEASURMENT TABLE;[04] CORROSION AT BS 1016 WL 208 LBL 12 WAS REPAIRED ON EA 23-153-02627; AND SRM 51-10-02;[05] VERIFIED ALL STEPS COMPLETE AND MEASUREMENT TABLE; CARD COMPLETE.
FWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREA OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222DF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED JOB COMPLETE AND MEASUREMENT TABLE
FWD FLOOR PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] I UPDATED THE MEASUREMENTS TABLE.;[02] FWD FLOOR PANEL 221FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[03] VERIFIED RII STEPS COMPLETE;[04] VERIFIED JOB COMPLETE AND MEASUREMENT TABLE
FWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221EF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED JOB COMPLETE
FWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] UPDATED THE MEASUREMENT TABLE.;[02] FWD FLOOR PANEL 221CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[03] VERIFIED RII STEPS COMPLETE;[04] VERIFIED JOB COMPLETE
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL156.<[01] COMPLETED STEP 1.;[02] VERIFIED STEP 1 COMPLETE.;[03] PARTIAL STEP 2.;[04] COMPLETED STEP 2.;[05] COMPLETED STEP 3.;[06] UPDATED MEASUREMENT TABLE.;[07] COMPLETED STEP 4.;[08] PARTIAL STEP 5.;[09] COMPLETED STEP 5.;[10] VERIFIED STEP 5 COMPLETE.;[11] COMPLETED STEP 7.;[12] COMPLETED STEPS 8 AND 9.;[13] OK TO INSTALL<BR>STEP 6;[14] COMPLETED INSTALLATION-STEP 6
INTERCOSTAL CRACKED; BS380-400; WL208; LBL13<[01] UPDATED STEPS 1 & 2.;[02] UPDATED STEPS 3;4;[03] UPDATE STEP 5;[04] REMOVED AND REPLACED THE UPPER CHORD ANGLE ON THE INTERCOSTAL AT BS380-400 LBL13; WL 208 DUE TO NO REPAIR LIMITS IN THE SRM. INSTALLED IAW SRM 51-40-02-0G-0; DWG 143A5400
AFT FLOOR PANEL 242VF UPPER SKIN HAS PULLED STRANDS<[01] PULLED STRANDS ON UPPER SURFACE SKIN OF AFT PANEL 242VF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED JOB COMPLETE AND CURE SHEETS;[03] EDITED STEPS TO INCLUDE RII INSPECTION ITEMS.;[04] FINAL INSPECTION. JOB COMPLETE.
AFT FLOOR PANEL 241ACF UPPER SKIN HAS PULLED STRANDS<[01] FLOOR PANEL 241ACF UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED ALL CURE SHEETS TO THIS FAULT.;[02] FINAL INSPECTION. JOB COMPLETE.;[03] FINAL INSPECTION. JOB COMPLETE.
AFT FLOOR PANEL 241AAF UPPER SKIN HAS PULLED STRANDS<[01] FABRICATED REPLACEMENT FLOOR PANEL 241AAF IAW SRM 53-00-50-2R-0 AND BOEING DWG: 147A5810 ID: 0008.;[02] FINAL INSPECTION. JOB COMPLETE.
AFT FLOOR PANEL 241ZF UPPER SKIN HAS PULLED STRANDS.<[01] PULLED STRANDS ON UPPER SURFACE SKIN OF AFT PANEL 241ZF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED JOB COMPLETE AND MEASUREMENT TABLE
FLOOR PANEL 232SF IS MISSING AN INSERT ALONG THE O/B EDGE. (MARKED)<[01] FOUND DAMAGE AT MISSING INSERT LOCATION ON O/B EDGE OF FLOOR PANEL 232SF; DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 232SF FROM BMS 4-23TY2 LOT#1534174-1; INSTALLED INSERTS USING BMS 5-107 LOT#1534504-1; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2023 APPLIED TAPE TO LOWER SURFACE AND PART MARKED IAW SRM 53-00-50-2R-0 PARA 1.A(NOTE); 5.S AND BOEING DWG 144A5810-161.;[02] INSPECTED AND VERIFIED CORRECTIVE ACTION 1.;[03] ATTACHED CURE SHEET;[04] FINAL INSPECTION. JOB COMPLETE.
WING CENTER SECTION BREAK PANEL IS CRACKED BS 540; RBL 1; WL 207<[01] UPDATED STEPS;[02] CERTIFIED STEPS;[03] UPDATED MEASUREMENT TABLE;[04] CERTIFIED CORRECTIVE ACTION; MEASUREMENT TABLE;[05] REMOVED AND REPLACED PANEL BREAK AT BS BL0 TO RBL25; WL 207 DUE TO NO SRM DAMAGE LIMITS. REPLACED IAW SRM 51-10-02-0G-0 STEP 9; SRM 51-40-02-0G-0; DWG 143A5240;[06] VERIFIED CORRECTIVE ACTION #5
WING CENTER SECTION BREAK PANEL IS CRACKED BS 540; LBL 1; WL 207<[01] UPDATED STEPS;[02] EDIT UPDATE TO STEP #1;[03] CERTIFY STEP #1;[04] UPDATED MEASUREMENT TABLE;[05] STEPS 1;4 COMPLETE;[06] STEP 4 COMPLETE;[07] REMOVED AND REPLACED PANEL BREAK AT BS BL0 TO LBL25; WL 207 DUE TO NO SRM DAMAGE LIMITS. REPLACED IAW SRM 51-10-02-0G-0 STEP 9; SRM 51-40-02-0G-0; DWG 143A5240;[08] VERIFIED CORRECTIVE ACTION #7
FWD CARGO DOOR SUB THRESHOLD HAS CORROSION AT BS 440+11 - 480+3 RBL 28 WL 157<[01] UPDATED STEP 1 AND 2;[02] VERIFIED STEP 1 & 2 COMPLETE.;[03] UPDATED STEP 3;[04] MEASUREMENT TABLE INCORRECT. SEE STEP 6;[05] UPDATED MEASUREMENTS TABLE;[06] UPDATED STEP 5 AND 7;[07] UPDATED STEP 7 AND 8.;[08] STEP 6 UPDATED.;[09] UPDATED STEP 3;[10] REMOVED CORROSION SEVERAL PLACE BETWEEN BS440+11 AND 480+3. THE DEEPEST DAMAGE AT STA 460+9 : 0.012; ORIGINAL MATERIAL THICKNESS : 0.045; REMAINING THICKNESS : 0.033. DAMAGE EXCEED 10% OF ORIGINAL THICKNESS. FOUND TO BE OUT OF LIMIT IAW SRM 53-30-15-1A-1<BR><BR>CALIBRATION TOOL DEPTH GAUGE<BR>ID : ATS2666<BR>DUE : 05/2024<BR><BR>REMOVED FCB SUB THRESHOLD WEB IAW SRM 51-40-02-0G-0<BR><BR>LOCATED AND DRILLED NEW FWD CARGO DOOR SUB THRESHOLD IAW SRM 51-40-05-0G-0 AND DWG 143A8330;ID: 0042; REV:A<BR><BR>INSTALLED NUTPLATES ON NEW FWD CARGO DOOR SUB THRESHOLD IAW SRM 51-40-02-0G-0 AND DWG 143A8330;ID: 0040; REV:A<BR><BR>INSTALLED FCB SUB THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND DWG 143A8330 ID:0042 REV:A
312 FRAME IS CRACKED IN RADIUS JUST ABOVE FWD ENTRY DOOR HEADER<[01] B.S. 312 FRAME JUST ABOVE FWD ENTRY DOOR HEADER WAS REPAIRED PER M-22-153-012 (TTG8Q00MV151) IN SUBTASK ATTACHED.;[02] VERIFIED CORRECTIVE ACTIONS 1.
FLOOR BEAM AT BS 986 LBL 25-45 HAS MULTIPLE AREAS OF CORROSION< REMOVED CORROSION FROM FLOOR BEAM AT BS 986.5 WL 208 BLEND OUT AREAS MEASURE: LBL 44: L: 2.5' W: 1.2' REMAINING THICKNESS: .104' ORIGINAL THICKNESS .150'; FOUND FLOOR BEAM TO BE OUT LIMITS PER SRM 53-70-51-1A-1 PAR. 4. H. (2)(B) FIGURE 103. DETAILS A; B; C; E; F; G; H AND N. USED TOOL ID: IS000459 DUE DATE: 02/29/24.<BR>FABRICATED AND INSTALLED REPAIR PARTS [1] 1EA T-CHORD MADE FROM BAC1505-101474 7050-T76511 LOT: 1505572-11; [2] ANGLE 2EA MADE FROM BAC1490-2887 7075-T6 LOT: 1505568-1; [3] ANGLE 2EA MADE FROM BAC1490-2887 7075-T6 LOT: 1523264-1 AND [4] STRAP 2EA MADE FROM 7075-T6#0.080 LOT: 1492623-1 IAW EA 23-153-02524 AND SRM 53-70-51-2R-4 PAR. 4. G. H. I. J. AND K.;[35] VERIFIED REPAIR PERFORMED PER CORRECTIVE ACTION ITEM 34. FAULT COMPLETE. MEASUREMENT TABLE COMPLETE.
FLOOR BEAM AT BS 986 RBL 25-45 HAS MULTIPLE AREAS OF CORROSION<[01] VERIFIED APPLICABILITY FOR BOEING 737-700 SRM 53-70-51-1A-1.;[02] CERTIFIED STEP 2;[03] STEP 3 COMPLETE.;[04] VERIFIED STEP 3 COMPLETE.;[05] VERIFIED STEP 3 COMPLETE AND MEASUREMENT TABLE
FWD SERVICE DOOR SCUFF PLATE CRACKED (MARKED)<[01] WELDED CRACK ON RADIUS OF FWD SERVICE DOOR SCUFF PLATE USING AMS 4954 .045' FILLER ROD LOT NUMBER M798431 PER SRM 53-10-15-2R-2 PARAGRAPH 4.B. (3) AND (4). REPAIR WELD STILL REQUIRES A DYE PENETRANT INSPECTION.<BR>EQUIPMENT USED; WELDING MACHINE E10583 CALIBRATION DUE DATE 01/2024;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1.<BR>REPAIR WELD STILL REQUIRES A DYE PENETRANT INSPECTION.;[03] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-RADIOMETER ID: ATS2561-1; 2; 3 CAL DUE: 08/23;[04] SANDED WELD REPAIR AREA PER SRM 53-10-15-2R-2 PARAGRAPH 4.B. (6).;[05] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 4.;[06] APPLIED PRIMER TO SCUFF PLATE INNER SURFACE PER SOPM 20-41-02;[07] APPLIED PRIMER TO SCUFF PLATE INNER SURFACE PER SRM 53-10-15-2R-2 PARAGRAPH 4.B. (8).;[08] VERIFIED ACTIONS 6 AND 7.;[09] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 7.;[10] INSTALLED FWD SERVICE DOOR SCUFF PLATE IAW AMM 53-11-01-420-801;[11] VERIFIED CORRECTIVE ACTION #10
CRACKED LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL40 WL160.<[01] PART/MATERIAL IDENTIFIED PER SRM 57-10-10-0I-2 FIGURE 2 TABLE 2 ITEM 4.<BR>CUMULATIVE CRACK LENGTHS 30' EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 57-10-10-1A-2 PARA 4. D. (1).<BR>REPAIR TO BE PERFORMED IAW SRM 51-70-04-2R-10 AS GIVEN IN SRM 57-10-10-2R-2 PARA 1. C. NOTE: ALTERNATIVE PATCH REPAIR.;[02] VERIFIED CORRECTIVE ACTION 1;[03] CRACK IN THE LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL40 WL160 WAS REPAIRED IAW SRM 51-70-04-2R-10.;[04] VERIFIED CORRECTIVE ACTION 3;[05] VERIFIED CORRECTIVE ACTION 3
CRACKED LOWER R/H COMPOSITE BULKHEAD AT BS663 RBL32 WL151.<[01] EDITED STEPS 2 AND 4.;[02] CRACKED LOWER R/H VAPOR BARRIER BS633 RBL32 WL151 WAS REPAIRED IAW SRM 51-70-04-2R-10.;[03] UPDATED MEASUREMENTS;[04] VERIFIED CORRECTIVE ACTIONS 1-3<BR><BR>VERIFIED MEASUREMENTS TABLE;[05] VERIFIED CORRECTIVE ACTIONS 1-3<BR><BR>VERIFIED MEASUREMENTS TABLE
FWD SERVICE DOOR SLIDE PACK NEEDS REPOSITIONING.<[01] REPOSITIONED FWD SERVICE (R1) DOOR SLIDE REF AMM 25-66-01.;[02] ADDED REFERENCE TO SIG-OFF: AND MT 725-61-06
MULTIPLE EMERGENCY LIGHTS OUT IN FWD CABIN / [01] REMOVED AND REPLACED FWD LH BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.
MULTIPLE EMERGENCY LIGHTS ARE OUT IN AFT CABIN. / [01] R+R BATTERY PACK FOR INOP EMERGENCY LIGHTS IN AFT CABIN PER AMM 33-51-06; OPS CHECK GOOD.
ALL EMERGENCY LIGHTS IN CABIN DO NOT ILLUMINATE & THEY WILL ILLUMINATE WHEN EMERGENCY EXIT LIGHT SWITCH PUSHED IN CABIN / [01] EMERGANCY EXIT LIGHTS OPS CHECKS NORMAL PER AMM 33-51-00
SIDEWALL WINDOW LIGHTING INOP ROW 9 10 CAPTAINS SIDE; ROW 13 FO SIDE SIDEWALL WINDOW LIGHTING INOP ROW 9 10 CAPTAINS SIDE ROW 13 FO SIDE / [01] R/R SIDEWALL LIGHTS BULBS AT ROW 9-10 LEFT HAND . R/H ROW 13 PER M/M 33-21-00
L-2 DOOR SLIDE GIRT BAR GIRT TOO LONG NEEDS REINSTALLED IN CONTAINER. / [01] READJUSTED L2 DOOR SLIDE IN COMPARTMENT PER MT725-66-01
AFT SERVICE DOOR SLIDE NEED TO BE REPOSITIONED IN SLIDE CASE / [01] REPOSITIONED SLIDE IN SLIDE CASE PER AMM 25-66-01 AND MT 725 61-06
L/H EMERGENCY EXIT DOOR LIGHT INOP.(RELAMP NO HELP). ; / [01] R&R'D BALLAST IAW M/M 33-21-00.; [02] PARTS
FWD AND AFT ISLE AREA MISSING CARPET END CAPS AND PHOTOLUMINESCENT STRIPS. ; / [01] INSTALLED PHOTOLUMINESCENT STRIPS AND END-CAPS ON CABIN FLOOR FROM STA. 360-927 PER AMM 33-51-15; [02] INSPECTED.
CAP STRIP FOR PANELS 122DW AND 122EW HAS ELONGATED HOLES . ; / [01] REMOVED AND REPLACED CAP STRIP IN REF TO AMM 25-52-06
FITTING CRACKED FOR THE AFT CARGO VACUUM WASTE TANK ENCLOSURE SUPPORT INSTL STA 947.5 LBL 10 ; / [01] REMOVED AND INSTALLED NEW FITTING IAW SRM 51-40-02.; [02] INSPECTED
ENTIRE SHIPSET OF PHOTOLUMINESCENT STRIPS SHOW SIGNS OF CRAZING AND STAINING. ; / [01] REMOVED ALL OLD PHOTOLUMINESCENT STRIPS FROM CABIN FLOOR PER AMM 33-51-15 AND TASK CARD 733-080-00-01.; [02] INSTALLED PHOTOLUMINESCENT STRIPS ON CABIN FLOOR FROM STA. 360-927 PER AMM 33-51-15 AND TASK CARD 733-080-00-01.; [03] INSTALLED PHOTOLUMINESCENT STRIPS ON CABIN FLOOR FROM STA. 360-927 PER AMM 33-51-15; [04] INSPECTED
FWD ENTRY DOOR CUT-OUT UPPER HINGE FOLLOW UP DOOR CRACKED. ; / [01] REMOVED AND REPLACED DOOR PER SRM 51-40-02
FWD ENTRY DOOR MAKES A POPPING NOISE WHILE CLOSING. ; / [01] ADJUSTED FORWARD ENTRY DOOR PER AMM 52-11-00 FOR CLEARANCE
UPPER SURFACE OF RIGHT TRANSITION ANGLE HAS SMALL AREA OF CORROSION AT STATION 432 IN FORWARD BAG BIN.(MARKED) ; / [01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [02] TO BE REMOVED AND REPLACED DAMAGED PART ON EA 5330-E-16461-NG AND TTG8Q004DOV4; [03] TO BE REMOVED AND REPLACED DAMAGED PART ON EA 5330-E-16461-NG AND TTG8Q004DOV4.
AFT CARGO SIDE TRANSITION ANGLE RIGHT SIDE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 747-767 ; AFT CARGO SIDE TRANSITION ANGLE RIGHT SIDE HAS CORROSION AROND NTPLATE HOLES FROM STA 747-767 / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED.010; OUT OF LIMITS PER SRM 53-00-53-1A-1. REPLACING R/H TRANSITION ANGLE FROM BS 727-767 ON TTG8Q006TA4X.
AFT CARGO SIDE TRANSITION ANGLE RIGHT SIDE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 727-727A ; AFT CARGO SIDE TRANSITION ANGLE RIGHT SIDE HAS CORROSION AROND NTPLATE HOLES FROM STA 727-727A / [01] REMOVED DAMAGE PER SRM 53-00-53-1A-2 AND FOUND TO BE OUT-OF-LIMITS PER SRM 53-00-53-1A-2.; [02] REMOVED R/H TRANSITION ANGLE BS 727-767 FOR REPLACEMENT PER SRM 51-40-02.; [03] REMOVED AND REPLACED TRANSITION ANGLE PER SRM 51-40-02.; [04] STRAP REPLACED ON CARD TTG8Q00483WX.; [05] LINE 4 WRITTEN IN ERROR; [06] ANGLE REPLACED ON CARD TTG8Q00483WX.
AFT CARGO SIDE TRANSITION ANGLE RIGHT SIDE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 767-787 ; AFT CARGO SIDE TRANSITION ANGLE RIGHT SIDE HAS CORROSION AROND NTPLATE HOLES FROM STA 767-787 / [01] REMOVED AFT CARGO DOOR CUTOUT SHIELD; STA 767 TO STA 787 PER SRM 51-40-02.; [02] REMOVED DAMAGE PER SRM 53-60-15-1A-1 AND FOUND TO BE OUT-OF-LIMITS PER SRM 53-60-15-1A-1.; [03] LOCATED; DRILLED AND DE-BURRED REPLACEMENT SHIELD PER SRM 51-40-05.; [04] C/W INSPECTION OF STEP #3; [05] INSTALLED AFT CARGO R/H SHIELD STA. 767-792 IAW SRM 51-40-02.
AFT CARGO SIDE TRANSITION ANGLE LEFT SIDE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 727B-727C ; AFT CARGO SIDE TRANSITION ANGLE LEFT SIDE HAS CORROSION AROND NTPLATE HOLES FROM STA 727-727C / [01] CORROSION REMOVAL FOUND TO BE OUT OF LIMITS; REMOVAL WAS .010 DEEP; OUT OF LIMITS PER SRM 53-00-53-1A-1. REMOVAL FOR REPLACEMENT FROM BS 727- 847 WILL BE ACCOMPLISHED ON [TTG8Q006TAFU; [02] CORROSION REMOVAL FOUND TO BE OUT OF LIMITS; REMOVAL WAS .010 DEEP; OUT OF LIMITS PER SRM 53-00-53-1A-1. REMOVAL FOR REPLACEMENT FROM BS 727- 847 WILL BE ACCOMPLISHED ON [TTG8Q006TAFU
AFT CARGO SIDE TRANSITION ANGLE LEFT SIDE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 787-807 ; AFT CARGO SIDE TRANSITION ANGLE LEFT SIDE HAS CORROSION AROND NTPLATE HOLES FROM STA 787-807 / [01] REMOVED DAMAGE PER SRM 53-00-53-1A-2 AND FOUND TO BE OUT OF LIMITS.; [02] CORROSION REMOVAL FOUND TO BE OUT OF LIMITS; REMOVAL WAS OUT OF LIMITS PER SRM 53-00-53-1A-1. REMOVAL FOR REPLACEMENT FROM BS 727- 847 WILL BE ACCOMPLISHED ON [TTG8Q006TAFU
AFT CARGO SIDE TRANSITION ANGLE LEFT SIDE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 727A-727B ; AFT CARGO SIDE TRANSITION ANGLE LEFT SIDE HAS CORROSION AROND NTPLATE HOLES FROM STA 727A-727 / [01] CORROSION REMOVAL FOUND TO BE OUT OF LIMITS; REMOVAL WAS .010 DEEP; OUT OF LIMITS PER SRM 53-00-53-1A-1. REMOVAL FOR REPLACEMENT FROM BS 727- 847 WILL BE ACCOMPLISHED ON [TTG8Q006TAFU]; [02] CORROSION REMOVAL FOUND TO BE OUT OF LIMITS; REMOVAL WAS .010 DEEP; OUT OF LIMITS PER SRM 53-00-53-1A-1. REMOVAL FOR REPLACEMENT FROM BS 727- 847 WILL BE ACCOMPLISHED ON [TTG8Q006TAFU
AFT CARGO SIDE TRANSITION ANGLE RIGHT SIDE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 727D-727E ; AFT CARGO SIDE TRANSITION ANGLE RIGHT SIDE HAS CORROSION AROND NTPLATE HOLES FROM STA 727D- / [01] CORROSION REMOVAL FOUND TO BE OUT OF LIMITS; REMOVAL WAS .010 DEEP; OUT OF LIMITS PER SRM 53-00-53-1A-1.; [02] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED.010; OUT OF LIMITS PER SRM 53-00-53-1A-1. REPLACING R/H TRANSITION ANGLE FROM BS 727-767 ON TTG8Q006TA4X.
AFT CARGO SIDE TRANSITION ANGLE LEFT SIDE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 747-767 ; AFT CARGO SIDE TRANSITION ANGLE LEFT SIDE HAS CORROSION AROND NTPLATE HOLES FROM STA 747-767 / [01] CORROSION REMOVAL FOUND TO BE OUT OF LIMITS; REMOVAL WAS .010 DEEP; OUT OF LIMITS PER SRM 53-00-53-1A-1. REMOVAL FOR REPLACEMENT FROM BS 727- 847 WILL BE ACCOMPLISHED ON [TTG8Q006TAFU; [02] ANGLE REPLACED ON CARD TTG8Q00483WX.
AFT CARGO SIDE TRANSITION ANGLE RIGHT SIDE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 727E-747 ; AFT CARGO SIDE TRANSITION ANGLE RIGHT SIDE HAS CORROSION AROND NTPLATE HOLES FROM STA 727E-747 / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED.010; OUT OF LIMITS PER SRM 53-00-53-1A-1. REPLACING R/H TRANSITION ANGLE FROM BS 727-767 ON TTG8Q006TA4X.
SUPPLEMENTAL INFORMATION: LEFT TRANSITION ANGLE IN AFT CARGO PIT HAS CORROSION STA. 727 - 727+11 / CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-1. REMOVED L/H TRANSITION ANGLE FROM BS 727-849 FOR REPLACEMENT PER SRM 51-40-02. REMOVED AND REPLACED TRANSITION ANGLE PER SRM 51-40-02. STRAP REPLACED ON CARD TTG8Q00483WX. LINE 3 WRITTREN IN ERROR ANGLE REPLACED ON CARD TTG8Q00483WX.
FLOOR PANEL ABUTMENT STRAP HAS ELONGATED HOLE ON L/H SIDE (STA 772.6) ; FLOOR PANEL ATMENT STRAP HAS ELONGATED HOLE ON LH SIDE / [01] REMOVED AND REPLACED STRAP PER SRM 51-40-02.; [02] STRAP REPLACED ON CARD TTG8Q00483WX.
AFT CARGO SIDE TRANSITION ANGLE RIGHT SIDE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 787-807 ; AFT CARGO SIDE TRANSITION ANGLE RIGHT SIDE HAS CORROSION AROND NTPLATE HOLES FROM STA 787-807 / [01] FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED PER SRM 51-40-02 AND CARD TTG8Q00483WX
AFT CARGO SIDE TRANSITION ANGLE LEFT SIDE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 727E-747 ; AFT CARGO SIDE TRANSITION ANGLE LEFT SIDE HAS CORROSION AROND NTPLATE HOLES FROM STA 727E-747 / [01] CORROSION REMOVAL FOUND TO BE OUT OF LIMITS; REMOVAL WAS .010 DEEP; OUT OF LIMITS PER SRM 53-00-53-1A-1. REMOVAL FOR REPLACEMENT FROM BS 727- 847 WILL BE ACCOMPLISHED ON [TTG8Q006TAFU
AFT CARGO SIDE TRANSITION ANGLE LEFT SIDE HAS CORROSION AROUND NUTPLATE HOLES FROM STA 727C-727D ; AFT CARGO SIDE TRANSITION ANGLE LEFT SIDE HAS CORROSION AROND NTPLATE HOLES FROM STA 727C-727D / [01] CORROSION REMOVAL FOUND TO BE OUT OF LIMITS; REMOVAL WAS .010 DEEP; OUT OF LIMITS PER SRM 53-00-53-1A-1. REMOVAL FOR REPLACEMENT FROM BS 727- 847 WILL BE ACCOMPLISHED ON [TTG8Q006TAFU
211AF IS WARPED / [01] REPLACED FLOOR PANEL 211AF IAW SOPM 20-50-02. PANEL WILL BE CLOSED ON SWA CARD # TTG8Q006L19G.; [02] FLOOR PANEL REPLACEMENT IS C/W
521 TB PANEL L/H WING HAS CORNER DELAMINATION. ; / [01] REMOVED DAMAGE PER ARM 51-70-05-2R-6; [02] C/W INSPECTION; [03] REPAIRED PER SRM 51-70-05-2R-6; [04] WITNESS REPAIR ON STEP 3 IAW SRM 51-70-05-2R-1; [05] RESTORED FINISH ON PANEL PER AMM 51-21-99.; [06] INSPECTED
SUPPLEMENTAL INFORMATION: R/H WING FUELING STATION AT PANEL 621GB LIGHT CORROSION ON BRACKET FOR #1 TANK QUANTITY GAUGE. MRKD / R&R'D REFUELING PANEL PER MM 28-41-61 STILL REQUIRES OPS CHECK. OPS CHECK GOOD IAW M/M 28-41-61.
SEAT TRACK; LBL24; BS727E-5; BOTTOM SURFACE INSIDE TRACK HAS LIGHT SURFACE CORROSION.<BLENDED OUT CORROSION MATERIAL REMOVED .018' FOUND TO BE WITHIN LIMITS TREATED AND PRIMED AREA ALL WORK DONE IAW SRM 53-00-52-1A-1. VERIFIED DAMAGE REMOVAL C/W HFEC SURFACE INSPECTION OF REWORKED AREA PER NDTM PART 6 51-00-00 PROCEDURE 23 WITH NO DEFECT NOTED.
#3 SEAT TRACK HAS EVIDENCE OF CORROSION ON CROWN BASE AT STATION 578. REMOVED DAMAGE MATERIAL REMOVED .015' FOUND TO BE WITHIN LIMITS TREATED AND PRIMED AREA. ALL WORK DONE IAW SRM 53-00-52-1A-1. VERIFIED DAMAGE REMOVAL C/W HFEC SURFACE INSPECTION OF REWORKED AREA PER NDTM PART 6 51-00-00 PROCEDURE 23 WITH NO DEFECT NOTED.
EMERGENCY LT BATTERY PACK M1675 DEAD. R & R EMERGENCY LT BATTERY PACK MT 1675, PER M/M 33-51-06. OPS CHECK GOOD.
EXTERNAL GROUND POWER DOOR AFT LATCH RUBBING BLOCK DOUBLER HAS 2 EA CRACKS AT LOWER RIVET. MOD / INSTALLED TIME LIMITED REPAIR PER EA 20-153-01603. SEE ATTACHED SA-M 326 FOR WORK IN PROGRESS DETAILS PERMANENT ACTION REQUIRED: PERMANENT REPAIR OF THIS ITEM WILL BE INCORPORATED WITH THE PERMANENT REPAIR OF EA 20-153-0150. PERMANENT REPAIR TIME LIMIT 55 DAYS OR 420 CYCLES; WHICHEVER COMES FIRST
LEFT EXTERIOR OVERWING EXIT LIGHT LENS LOOSE. R&R NUTPLATE RING ASSEMBLY ON LIGHT ASSEMBLY IAW SIP.
R1 DOOR SLIDE BONDING CLIP CAME OFF. / REATTACHED BONDING JUMPER IAW MT.
PASSENGER CABIN FLOOR BOARD PANEL 231XF FACE PLY SHEET IS PULLED OFF / DISPLACED SEAT ROWS 9ABC; 10ABC; 11ABC; 12ABC; 13ABC; 14ABC; AND 9DEF. DISPLACED CARPET TO FOM REMOVED FLOORBOARD; REMOVED FLOORBOART 231XF; BY FABRICATION; INSTALLED NEW FLOORBOARD 231XF; REINSTALLED DISPLACED CARPET AND REINSTALLED DISPLACED SEATS IAW AMM 53-21-00-000-801; AMM 53-21-00-400-801; AMM 25-22-00-000-801; AMM 25-22-00-400-802; AMM 25-27-15-000-801; AMM 25-27-15-400-801; SRM 53-00-50-2R-0 TABLE 204; DRAWING 144A5810 REV-; AND SWA MT 725-22-03
PASSENGER CABIN FLOOR BOARD PANEL 231YF FACE PLY SHEET IS PULLED OFF / DISPLACED SEAT ROWS 9ABC; 10ABC; 11ABC; 12ABC; 13ABC; 14ABC; AND 9DEF; DISPLACED CARPET TO FOM REMOVE FLOORBOARDS; REMOVED FLOORBOARD 231YF; REPLACED FLOORBOARD 231YF BY FABRICATION; INSTALLED NEW FLOORBOARD 231YF; REINSTALLED DISPLACED CARPET AND REINSTALLED DISPLACED SEATS IAW AMM 53-21-00-000-801; AMM 53-21-00-400-801; AMM 25-22-00-000-801; AMM 25-22-00-400-802; AMM 25-27-15-000-801; AMM 25-27-15-400-801; SRM 53-00-50-2R-0 TABLE 204; DRAWING 144A5810 REV-; AND SWA MT 725-22-03
EMERGENCY LIGHT DAMAGED. R&R LIGHT IAW AMM.
PASSENGER CABIN FLOOR BOARD PANEL 241MF BOTTOM SIDE HAS FIBER PULLED OFF. / REPAIRED FLOOR BOARD 241MF BOTTOM SIDE I.A.W. B737-700 SRM'S 53-00-50-2R-1 REV. 68 & 53-00-50-2R-0 REV 68 (A13438) (A09236) (A05429) (A08637)
UPON OK TO CLOSE; R/H FWD CORNER OF LOWER SURFACE R/H WING PANEL 621YB; FOUND CRACKED / REPAIRED CRACK AND REPLACED ALUMINUM FOIL ON R/H FWD CORNER OF R/H WING PANEL 621 YB I/A/W SRM51-70-04-2R-9 REV 68; SRM 51-70-04-2R-0 REV 68; SRM 51-70-14-2R-3 REV 68.
DURING OK TO INSTALL FOUND LEFT WING LEADING EDGE PANEL 521ZB CRACKED AT THE OUTBOARD FORWARD FASTENER HOLE / REPAIRED CRACK AT FASTNER HOLE AND REPAIRED ALUMINUM FOIL I/A/W SRM 51-70-04-2R-9 REV 68; SRM 51-70-04-2R-0 GENERAL; SRM 57-41-01-2R-6 REV 68;SRM 51-70-14-2R-3 REV 68.
ATTACHING ANGLE FOR THE PRESSURE SEAL AT STA 1016 LH BL-2 IS CRACKED / REMOVED CRACKED ANGLE FROM BS 1016 RH BL-2 IAW SRM 51-40-02-0G-0 VERIFIED MATERIAL .020' 7075+6 IAW DWG 65-54862 FABRICATED ANGLE IAW SRM 51-40-05-0G-0 AND DWG 148A0922 REV. A TREATED AND PRIMER PART IAW SRM 51-20-01-0G-0 AND AMM 51-21-72-370-801 ACCOMPLISHED COMFIRMITY INSPECTION AND VERIFIED ATTACH ANGLE P/N 65-54862-20 CONFORMS TO THE SPECIFICATION FOUND IN BOEING DWG 148A0922 REV. A INSTALLED NEW PART AT BS 1016 RH BL-2 IAW SRM 51-40-02-0G-0 AND DWG 148A0922 REV. A APPLIED CIC TO AREA REWORK IAW AMM 51-21-91-620-802
CORROSION ON AFT CARGO FLOOR STRAP STA 767 TO STA 847 RH SIDE / REMOVED CORROSION FROM STRAP IAW SRM 51-10-02-0G-0 MEASURED MATERIAL ORIGINAL T .100' MAT LOSS 'T' .021' REMAINING 'T' .079' FOUND OUT OF LIMIT IAW SRM 53-00-53-1A-2 REMOVED STRAP FROM FLOOR IAW SRM 51-40-02-0G-0. VERIFIED NEW STRAP P/N 146A8128U14 IAW DWG 146A8120 REV. B LOCATED AND DRILLED NEW STRAP IAW DWG 146A8120 REV B INSTALLED NEW STRAP AT AFT CARGO FLOOR IAW DWG 146A8120 REV. B AND SRM 51-40-02-0G-0 P/N 146A8128-14
LT OVERWING EMERGENCY EXIT DOOR HANDLE ASSEMBLY BROKEN. R&R DOOR HANDLE IAW AMM.
STRINGER CLIP CRACKED AT BS. 259.5, STR. 8L. R&R CLIP IAW SRM AND DWG.
STRINGER CLIP CRACKED AT BS. 259.5, STR. 10L. R&R STRINGER CLIP IAW DWG & SRM.
AFT CARGO PIT; LAV TANK AREA; VERTICAL PANEL STRUCTURE; ATTACH CLIP IS CRACKED; STA:867; LBL: 15.5; WL 208 - 42' / REMOVED VERTICAL PANEL STRUCTURE ATTATCH CLIP STA 867 LBL 15.5 WL 208-42' IAW SRM 51-70-02-0G-0; VERIFIED NEW PART IAW BOEING DRAWING 149A8102 REV A PN:149A8109-114. LOCATED AND DRILLED NEW ATTACH CLIP IAW 51-40-05-0G-0. INSTALLED NEW ATTACH CLIP IAW SRM 51-40-02-0G-. ATAG A98635
PASSENGER CABIN FLOOR BOARD PANEL 231BF FACE PLY SHEET IS PULLED OFF / REPAIRED PASSENGER CABIN FLOORBOARD PANEL 231BF OF UPPER SURFACE FACE PLY SHEET PULLED OFF (AS MARKED) IAW B737-700 SRM 53-00-5-2R-0 REV 68 AND B737-700 SRM 53-00-50-2R-1 REV 66. A09236; A13438.
PASSENGER CABIN FLOOR BOARD PANEL 231DF FACE PLY SHEET IS PULLED OFF / EVALUATED; PREPPED; CLEANED AMD REPAIRED EXPOSED / FRAYED FIBERS ALONG UPPER FACESHEET ON FLOORBOARD 231 DF IAW B737 SRM 53-00-50-2R-1; PAR 3 (A;C;E&F; K1;L1;M1). - REV 68.
PASSENGER CABIN FLOOR BOARD PANEL 241BF FACE PLY SHEET IS PULLED OFF / REPAIRED DAMAGE TO FACE PLY ON FLOOR BOARD 241 BF I/A/W SRM 53-00-50-2R-0 REV. 68 AND SRM 53-00-50-2R-1 REV. 68
PASSENGER CABIN FLOOR BOARD PANEL 241UF FACE PLY SHEET IS PULLED OFF / REPAIRED PASSENGER CABIN FLOOR BOARD PANEL 241 UF IAW B737 SRM 53-00-50-2R-1 PARA 3 AND 53-00-50-2R-0 PARA 5.
PASSENGER CABIN FLOORBOARD PANEL 242AF FORWARD RT CORNER BROKEN BETWEEN BS 537.45 TO BS 727B. REPAIRED FLOORBOARD 242AF IAW SRM.
PASSENGER CABIN FLOOR BOARD PANEL 232RF FACE PLY SHEET IS PULLED OFF / REPAIRED PASSENGER CABIN FLOOR BOARD PANEL 232RF OF UPPER SURFACE FACE PLY SHEET PULLING OFF ENTIRE LENGTH OF BOARD IAW B737-700 SRM 53-00-50-2R-1 REV 68 AND B737-700 SRM 53-00-50-2R-0 REV 68. A93557; A13438
PASSENGER CABIN FLOOR BOARD PANEL 231UF FACE PLY SHEET IS PULLED OFF / EVALUATED; PREPPED; CLEANED AND REPAIRED MULTIPLE AREA OF UPPER FACESHEET DAMAGE ON FLOORBOARD 231 UF IAW B737 SRM 53-00-50-2R-1; PAR 3 (A;C;E&F; K1;L1; M1) REV 68.
PASSENGER CABIN FLOOR BOARD PANEL 231KF FACE PLY SHEET IS PULLED OFF / REPAIRED UPPER SKIN AS MARKED ON PASSENGER CABIN FLOOR BOARD PANEL 231 KF AS REQ IAW B73 SRM 53-00-50-2R-1 REP 1 REV 68: SRM 53-00-502R-0 REF. GEN REV 68.
PASSENGER CABIN FLOOR BOARD PANEL 232FF FACE PLY SHEET IS PULLED OFF / REPAIRED PNL 232FF PULLED AND FRAYED UPPER FACE PLY. TAP TEST GOOD IAW B737-700 SRM 53-00-50-2R-1 REV 68; SRM 53-00-50-2R-0 REV 68. A13438; A87145.
PASSENGER CABIN FLOOR BOARD PANEL 232DF FACE PLY SHEET IS PULLED OFF / REPAIRED PASSENGER CABIN FLOORBOARD 232DF UPPER SIDE IAW B737 SRM 53-00-50-2R-1 REV 68 AND B737 SRM 53-00-50-2R-0 REV 68. A13438;; A09236.
PASSENGER CABIN FLOOR BOARD PANEL 231CF FACE PLY SHEET IS PULLED OFF / REPAIRED PASSENGER CABIN FLOOR BOARD PANEL 231CF OF UPPER SURFACE FACE PLY SHEET PULLED OFF (AS MARKED) IAW B737-700 SRM 53-00-50-2R-0 REV 68 AND B737 -700 SRM 53-00-50-2R-1 REV 68. A36551; A09236.
PASSENGER CABIN FLOOR BOARD PANEL 241KF FACE PLY SHEET IS PULLED OFF / EVALUATED; PREPPED; CLEANED AND REPAIRED AREA OF FRAYED/ EXPOSED COMPOSITES ALONG UPPER SURFACE ON FLOORBOARD 241KF IAW B737 SRM 53-00-50-2R-1 PAR 3 (A;C;E&E;K1;L1;M1)- REV 68.
PASSENGER CABIN FLOOR BOARD PANEL 242CF FACE PLY SHEET IS PULLED OFF / EVALUATED; PREPPED; CLEANED AND REPAIRED EXPOSED FIBERS AT UPPER SURFACE ON FLOORBOARD 242CF IAW B737 SRM 53-00-50-2R-1; PAR 3 (A;C;E&F; K1; L1; M1) - REV 68.
PASSENGER CABIN FLOOR BOARD PANEL 242DF FACE PLY SHEET IS PULLED OFF / EVALUATED; PREPPED; CLEANED AND REPAIRED EXPOSED FIBERS AT UPPER SURFACE ON FLOORBOARD 242DF IAW B737 SRM 53-00-50-2R-1; PAR 3 (A;C;E&F; K1; L1; M1) - REV 68.
PASSENGER CABIN FLOOR BOARD PANEL 241DF FACE PLY SHEET IS PULLED OFF / EVALUATED; PREPPED; CLEANED AND REPAIRED EXPOSED / FRAYED FIBER ALONG UPPER FACESHEET ON FLOORBOARD 241 DF IAW B737 SRM 53-00-50-2R-1; PAR 3 (A;C;E&F; K1;L1;M1) - REV 68.
PASSENGER CABIN FLOOR BOARD PANEL 241FF FACE PLY SHEET IS PULLED OFF / REPAIRED PASSENGER CABIN FLOOR BOARD PANEL 241FF UPPER SIDE IAW B737 SRM 53-00-50-2R-1 REV 68 AND B737 SRM 53-00-50-2R-0 REV 68. A13438.
PASSENGER CABIN FLOOR BOARD PANEL 241EF FACE PLY SHEET IS PULLED OFF / REPAIRED PASSENGER CABIN FLOOR PANEL 241 EF UPPER SIDE IAW B 737 SRM 53-00-50-2R-1 REV 68 AND B 737 SRM 53-00-50-2R-0 REV 68 A09236 A13438
PASSENGER CABIN FLOOR BOARD PANEL 241CF FACE PLY SHEET IS PULLED OFF / REPAIRED PASSENGER CABIN FLOOR BOARD PANEL 241CF UPPER SIDE IAW B737 SRM 53-00-50-2R-1 REV 8 AND B737-SRM 53-00-50-2R-0 REV 68. A13438;A09236.
PASSENGER CABIN FLOOR BOARD PANEL 232SF FACE PLY SHEET IS PULLED OFF / REPAIRED PASSENGER CABIN FLOOR BOARD PANEL 232 SF FACE PLY I.A.W B737-700 SRM'S 53-00-50-2R-1 REV 68 & 53-00-50-2R-0 REV 68. (A09236) (A13438).
PASSENGER CABIN FLOOR BOARD PANEL 242AF FACE PLY SHEET IS PULLED OFF / REPAIRED CABIN FLOORBOARD PANEL 242AF FACESHEET UPPER AS MARKED I/A/W SRM 53-00-50-2R-1 REV 68; SRM 53-00-50-2R-0 GENERAL REV 68.
PASSENGER CABIN FLOOR BOARD PANEL 231WF FACE PLY SHEET IS PULLED OFF / REPAIRED PASENGER CABIN FLOOR BOARD PANEL 231 WF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 REV 68 AND B737 SRM 53-00-50-2R-0 REV 68.
CABIN STA 295; RBL53; OTBD SIDE OF CREASE BEAM INNER CHORD ANGLE; SUPPORT ANGLE CRACKED IN RADIUS. / REMOVED AND REPLACED SUPPORT ANGLE @ STA 295 RBL 53; OUT/BD SIDE OF CREASE BEAM INNER CHORD IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8310 SHT 1 REV:D ATAG #13847
PASSENGER CABIN FLOOR SUPPORT AT STA 540 LBL 1AND W/L 208 IS CRACKED / REMOVED FLOOR SUPPORT @ F.S. 540 LBL-1. RECIEVED NEW FLOOR SUPPORT P/N # 143A5240-35. LOCATED; DRILLED; DEBURRED; & INSTALLED NEW FLOOR SUPPORT. ALL ACTIONS AREA IAW B737 SRM'S 51-40-02-0G-0; 51-40-05-0G-0; 51-40-06-0; & BOEING DWG # 143A0060 REV-A ATAG # EM1774
PASSENGER CABIN FLOOR BOARD PANEL 231ZF FACE PLY SHEET IS PULLED OFF / REPLACED CABIN FLOOR PANEL 231 ZF BY FABRICATION AND SAMPLE IAW DWG 144A5810-162 REV B AND BAC 5085 8.4.2.2. REV E; AND B737 SRM 53-00-50-2R-0 REV 68. A83992 A05429 MP1345
PASSENGER CABIN FLOOR BOARD PANEL 241AF FACE PLY SHEET IS PULLED OFF / REPLACED BY FABRICATION PASSENGER CABIN FLOOR BOARD PANEL 241AF IAW B737 SRM 53-00-50-2R-0 REV 68; BAC. 5085 AND DWG 144A5810-127. A75020; WN2679; D22108.
PASSENGER CABIN FLOOR BOARD PANEL 231GF FACE PLY SHEET IS PULLED OFF / FABRICATED NEW FLOOR PANEL FOR PASSENGER CABIN PANEL 231 GF PER ORIGINAL SAMPLE; FOR FACEPLY SHEET DAMAGE. IAW B737-700 SRM 53-00-50-2R-0 REV 68; BOE. DRAWING 143A5810 ID:0010 REV:- BAC 5085 REV (E) 21-FEB-2018. CURED IN OVEN EO-01 10-14-19 FOR 1 HR @ 140 DEGREES F IN @ 2:00PM OUT @ 3:00PM. MP1345; A75020; A84941.
PASSENGER CABIN FLOOR BOARD PANEL 241RF FACE PLY SHEET IS PULLED OFF / REPLACED CABIN FLOOR BOARD 241RF BY FABRICATION I/A/W SRM 53-00-50-2R-0 REV. 68 PAR 4; BAC 58085 AND DRAWING 146A5810-11 (A05429); (WN2679);(A08637).
PASSENGER CABIN FLOOR BOARD PANEL 241MF FACE PLY SHEET IS PULLED OFF / REPAIRED FLOOR BOARD 241MF UPPER SURFACE I.A.W. B737-700 SRM'S 53-00-50-2R-1 REV. 68 & 53-00-50-2R-0 REV 68 (A13438) (A09236)
PASSENGER CABIN FLOOR BOARD PANEL 242GF FACE PLY SHEET IS PULLED OFF / REPAIRED FLOOR BOARD PANEL 242GF I.A.W. B737-700 SRM 53-00-50-2R-1 REV. 68 & 53-00-50-2R-0 REV 68 (A13438) (A09236)
INTERNAL; RT CABIN STA 5OOC FRAME; 1.5 INCHES ABOVE FLOOR STRUCTURE; I/B LIP OF FRAME; HAS CHAFFE MARK. / ACCOMPLISHED FUSELAGE FRAME REPAIR AT STA 500C ABOVE S-17R ON INNER CHORD I.A.W. E.A 190687 IR AND SWA E.A. 1-753-35486 REV IR.
FORWARD CABIN FLOORBOARD 222BF, FORWARD OUTBOARD CORNER CRACKED BETWEEN BS 270 TO BS 420. REPAIRED FLOORBOARD 222BF IAW SRM.
FORWARD WET AREA FLOOR INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, RBL 31. R&R INTERCOSTAL IAW SRM & DWG.
PASSENGER CABIN FORWARD WET AREA FLOOR INTERCOSTAL STA 277-294 BL 0 UPPER FLANGE IS CRACKED AT BOTH FLOOR BOARD HOLES / REMOVED AND REPLACED WET AREA FLOOR INTERCOSTAL AT STA 277 TO STA 294 BLO IAW B737 SRM 51-40-02-0G-0 AND BOEING DWG 141A5400 IDI0020; REV I-
PASSENGER CABIN FORWARD WET AREA FLOOR INTERCOSTAL STA 312-328 LBL 46 IS CRACKED AT FLOOR BOARD HOLE / REMOVED AND REPLACED INTERCOSTAL AT STA 312-328 LBL 46 IAW BOEING DWG 141A5400; ID0001; REV:-
FORWARD CARGO PIT FLOOR BEAM STA 400+7' LBL 9 HAS ELONGATED NUTPLATE HOLE / INSTALLED REPAIR TO FWD CARGO FLOOR BEAM STA 400 TO 400+10' IAW SRM 53-00-53-2R-4. LBL9 ATAG WN5120 / ATAG A86735
AFT CARGO COMPARTMENT RIGHT SIDE PLATE AT STA 727+ 12 TO STA 767 RBL 25 TO RBL 26 WL 155 HAS AREAS OF CORROSION ON TOP SURFACE. / REMOVED CORROSION SIDE PLATE 727+10' TO 767 RBL 25 IAW SRM 51-10-02-0G-0; MAT ORIGINAL T .040' MAT LOSS T .030' MAT REMAINING T .010 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DETAIL FA REMOVED SIDE PLATE FROM BS 727 TO BS 767 RBL 25 IAW SRM 51-40-02-0G-0 IDENTIFIED NEW PART IAW SRM 53-00-53-2R-5 P/N BAC 1496-377 7075T62 NEW PART IAW SRM 51-20-01-0G-0 AND AMM 51-21-72-370-801 INSTALLED NEW PART IAW SRM 51-40-02-0G-0 & DWG 146A7500 P/N 146A7502-30
PASSENER CABIN FLOOR PANEL 221DF HAS DAMAGE / DISBONDED REPAIR ALONG UPPER INBOARD SURFACE. / REPAIRED AND INSTALLED 11 EA NEW INSERTS ON PASSENGER CABIN FLOOR PANEL 221DF UPPER SIDE IAW B737 SRM 52-00-50-2R-1 REV 68 AND B737 SRM 53-00-50-2R-0 REV 68. A69236; RB3829; A13438; A62785.
AFT CARGO COMPARTMENT LEFT SIDE PLATE AT STA 727C+ 6 TO SPLICE STA 747+10 LBL 25 TO LBL 26 WL 155 HAS AREAS OF CORROSION ON TOP SURFACE. / REMOVED CORROSION ON L/H SIDE PLATE STA 727C+6 TO 747_10 LBL 25 WL 155 IAW SRM 51-10-02-0G-0; VISIUAL INSPECTION WITH A 10X MAG GLASS; NO DEFECTS ORIGINAL .040' REMAIN .033 LOSS .007'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED L/H DIFR PLSYR DYS 737 TO 847 LBL 25 IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A7502 SHT 27 REV:- P/N 146A7502-27 TOOL 36647 CAL 6-7-20.
FORWARD CARGO PIT LEFT SIDEPLATE STA 500+10' TO 500C+8' LBL 24 WL 157 HAS CORROSION ON UPPER SURFACE AROUND FASTENER HOLES / REMOVED CORROSION ON FWD CARGO LEFT SIDE-PLATE STA 500+ 10' LBL 24 IAW SRM 51-10-02-0G-0; VISUAL INSPECTION WITH A 10X MAG GLASS; NO DEFECTS; ORIGINAL .040' REMAIN .031' LOSS .009' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED LEFT SIDE PLATE STA 400 TO 500 D IAW SRM 53-00-53-2R-4 AND SRM 51-40-02-0G-0 ATAG A79982 P/N 143A7501-25 TOOL 36644 CAL 19SEP19
FORWARD CARGO PIT L/H BAFFLE CLIP CRACKED AT BS. 500B, FORWARD SIDE OF FRAME. / R&R BAFFLE CLIP IAW SRM AND DWG.
FORWARD CARGO PIT AFT BULKHEAD STRUCTURE STA 500D LOWER RAIL ASSY HAS CORROSION LBL 25-33 WL 158 / REMOVED CORROSION LOWER RAIL ASSY IAW SRM 51-10-02-0G-0 NO ALLOWABLE DAMAGE LIMITS PART REPAIRABLE BY REPLACEMENT; REMOVED LH RAIL ASSY IAW SRM 51-40-02-0G-0; VARIFIED NEW PAET IAW IPC 53-11-01-43 P/N 143A9485-30. LOCATED AND DRILLED NEW PART IAW SRM 51-40-05-0G-0. INSTALLED NEW PART AT FWD CARGO BS 5OOD LH IAW SRM 51-40-02-0G-0 P/N 143A9485-30 ATAG - BN2481
FORWARD CARGO PIT LEFT FRAME STA 500B BRACKET ASSY (P/N 417A2106-29) BETWEEN STR 24L-25L WL 162 HAS CORROSION AROUND FASTENER HOLES / EVALUATED MATERIAL LOSS FOR ATTACH BRACKET IN FWD PIT FRAME STA 500B BETWEEN STR 24L - 25L 100% LOSS. SRM 53-00-07-1A-1. FABRICATED NEW CLIP I.A.W DWG 417A2150 REV AF AND E.A 1907 17 IR AND SWA E.A. 1-753-35534 REV IR. P/N 417A2106-29.
FORWARD CARGO PIT LEFT FRAME STA 480 BRACKET ASSY (P/N 417A2106-23) BETWEEN STR 23L-24L WL 165 HAS CORROSION AROUND FASTENER HOLES / REMOVED BRACKET @ F.S. 480 BETWEEN STR 23L - 24L. DUE TO 100% MATERIAL LOSS OF CORROSION REMOVAL. RECEIVED NEW BRACKET P/N 417A2106-23. LOCATED & DRILLED NEW BRACKET. INSTALLED NEW BRACKET. ALL ACTIONS ARE IAW B737 SRM'S 53-00-07-1A-1; 51-40-02-0G-0; 51-40-05-06-0; 51-40-06-0G-0 & AIPC 38-51-31-11. ATAG#A14737
FORWARD CARGO PIT LEFT FRAME STA 460 BRACKET ASSY (P/N 417A2106-21) BETWEEN STR 23L-24L WL 165 HAS CORROSION AROUND FASTENER HOLES / FABRICATED NEW ATTACH CLIP IN FWD CARGO AT FRAME STA 460 BETWEEN STR 23L - 24L. ORIGINAL T=.040'; REMAINING .030'; LOSS=.010' OUT OF LIMITS. I.A.W SRM 53-00-07-1A-1 I.A.W. E.A. 190717 IR AND SWA E.A 1-753-35534 REV IR.
AFT CARGO COMPARTMENT DOOR CUTOUT SILL WEB HAS CORROSION. / REMOVED CORROSION FROM WEB IAW SRM 51-10-02-0G-0 ORIGINAL 'T' .045' LOSS 'T' .007 REMAINING 'T' .039' FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-; VERFIED NEW PART P/N 146A8123-25 IAW DWG 146A8123 REV- REMOVED WEB IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW WEB IAW SRM 51-20-05-0G-0 AND 51-40-06-0G-0. INSTALLED NEW PART SRM 51-40-02-0G-0 AND DWG 146A8340 REV A. APPLIED CIC AREA REWORK IAW AMM 31-00-59-201 P/N 146A8123-24 ATAG EM1768
FORWARD CARGO PIT AFT BULKHEAD STRUCTURE STA 500D LOWER RAIL ASSY HAS CORROSION RBL 26-30 WL 158 / REMOVED CORROSION. NO ALLOWABLE DAMAGE LIMITS. REMOVED AND REPLACED RAIL ASSY IAW B737 SRM 51-10-02-0G-0 AND 51-40-02-0G-0
AFT PIT FLOOR PANEL 140DF HAS CORROSION AROUND EDGES / REMOVED AFT PIT FLOOR PANEL #140DF FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-53-1A-1 FIG 102. RECEIVED NEW FLOOR PANEL #140DF; PART NO. 453A2610-20; SI #7253767 IAW AIPC 25-52-10-18; PG 4 ITEM 65. REPLACED ON SHELF. ATAG WN4460
AFT PIT FLOOR PANEL 140BF HAS CORROSION AROUND EDGES / RECEIVED NEW FLOOR PANEL 140BR IAW B737-700 AIPC 25-52-10-18 PAR NO. 453A2610-32; SI#2753513; ORIGINAL PART FOUND OUT OF LIMITS REPLACED ON SHELF. ATAG WN2341
AFT PIT FLOOR PANEL 140AF HAS CORROSION AROUND EDGES / REMOVED CORROSION FROM AFT PIT PANEL 140 A-F (FLOOR) AROUND EDGES; BLEND IS GREATER THAN 20 INCHES FOUND TO BE OUT OF LIMITS IAW B-737 SRM 53-00-53-1A-1 FABRICATED NEW FLOOR PANEL IAW DWG 453A2610 REV B AND IDENTIFIED NEW PANEL WITH P/N 953A2610-34AAR-AST-I. ATAG A09127 P/N 453A2610-34
AFT PIT LH CAP STRIPS FROM STA 727+4' TO 847 CORRODED / VERIFIED NEW AFT CARGO PIT R/H CAP STRIP P/N 453A2611-10; 453A2611-8; 453A2611-4 IAW IPC 25-52-10-02. REPLACED PART ON SHELF. A TAG:A11539; WN0840; WN0767.
AFT CARGO COMPARTMENT FLOOR PANEL STA 727 HORSESHOE SUPPORT HAS CORROSION. / REMOVED FLOOR PANEL SUPPORT AT STA 727 NO LIMITS FOUND REPLACED IAW SRM 51-10-02-00-0 PARA 9.C. RECIVED NEW PART; P/N 453A2611-25; SI #7253171 REPLACE ON SHELF.
AFT CARGO COMPARTMENT SIDEWALL R\H CAP STRIPS STA 727 TO 847 HAS CORROSION. / VERIFIED NEW AFT CARGO R/H CAP STRIP P/N 453A2611-9 AND 453A2611-11 I.A.W. IPC 25-52-10-02 REPLACED PART ON SHELF. A-TAG A11525 A11529.
FWD CARGO DOOR AFT CORNER SCUFF PLATE BROKEN / WELDED FWD CARGO DOOR AFT CORNER SCUFF PLATE AT BACKSHOP IAW EA 1-A53-2076 REV 11. NO DEFECTS NOTED. PN: 143A8331-4.
FORWARD CARGO PIT GUSSET CRACKED AT BS. 500D, STR. 19L. R&R GUSSET IAW SRM AND DWG.
FORWARD CARGO PIT GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET IAW SRM AND DWG.
L1 DOOR SURROUND STRUCTURE CREASE BEAM INNER CHORD CRACKED AT BS. 303 ON VERTICAL FLANGE. R&R L1 DOOR CREASE BEAM IAW SRM AND DWG.
LEFT WING TRAILING EDGE PANEL 551FB FORWARD SUPPORT BRACKET 27' FROM OUTBOARD END IS BENT WITH EVIDENCE OF CRACK / REMOVED AND REPLACED LEFT WING TRAILING EDGE PANEL 551FB FORWARD SUPPORT BRACKET 27' FROM OUTBOARD END IAW B737 SRM 51-40-02-0G-0 STEP 4.B+E AND DWG 115A2710 REV C ATAG A10527
R/H HORIZONTAL STABILIZER LEADING EDGE PANEL 341B RIB CHORD CRACKED AT LEADING EDGE STA. 105.26. / R&R CHORD IAW SRM AND DWG.
RIGHT WING TRAILING EDGE PANEL 651FB FORWARD EDGE SUPPORT BRACKET 27' FROM OUTBOARD EDGE IS BROKEN / REMOVED AND REPLACED DAMAGED BRACKET ON TRAILIN EDGE PANEL 651 FB I/A/W SRM51-40-02-0G-0 PAR 4 AND DWG 115A2741 REV C. A-TAG# A10523 P/N 287A9152-24 ____X _____X
L/H WING REAR SPAR IRSS. 140 UPPER CLIP ON VERTICAL STIFFENER CRACKED. R&R STIFFENER IAW SRM.
L/H WING TRAILING EDGE MID SPAN BULKHEAD WBL 201.90 SEAL RETAINER WEB AFT OF LATERAL WEB CRACKED. R&R WEB IAW SRM AND DWG.
LEFT WING LOWER TRAILING EDGE SKIN WIGGLE PLATE ASSY IS CRACKED JUST INBOARD OF #3 FLAP TRACK / REMOVED AND REPLACED WIGGLE PLATE INBOARD OF #3 FLAP TRACK IAW SRM 51-40-02. P/N 115A2781-3 A TAG #WN3797
R/H REAR SPAR IRSS. 140 UPPER CLIP ON VERTICAL STIFFENER CRACKED. R&R CLIP ON VERTICAL STIFFENER IAW SRM.
LT WING LOWER TRAILING EDGE SKIN WIGGLE PLATE ASSEMBLY CRACKED BETWEEN IRSS 140 TO 162. R&R WIGGLE PLATE IAW SRM AND DWG.
LH WING LEADING EDGE PANEL 521TB IS CRACKED / REPAIRED CRACK TO L/H WING LEADINGE EDGE PANEL 521TB I/A/W SRM 57-41-01-2A-1 REV.68; SRM 51-70-04-2R-9 REV. 6 AND AMM 51-21-99-500-801 REV. 69. A13438; A09199; A20068
EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK IAW AMM.
EMERGENCY EXIT LIGHT IS INOP. R&R BATTERY PACK IAW AMM.
AIR TURNBACK, CLIMBING THROUGH 19,000' CABIN ALTITUDE WARNING HORN AND LIGHT CAME ON. RIGHT RAM AIR DOOR FULL OPEN LIGHT WAS ILLUMINATED FULL BRIGHT. CABIN WAS CLIMBING THROUGH 10,000' AND REACHED A MAX OF 13,000'. MANUAL CONTROLLER STOPPED THE CLIMB (MAYBE WE WERE DESCENDING AT THE SAME TIME). / R&R PRESSURE RELIEF VALVE IAW MM.
RT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. R&R LIGHT BALLAST PER AMM.
EMERGENCY LIGHT BATTERY PACK OVERRIDE PANEL AT LOCATION M1669 INOP. R&R BATTERY PACK PER AMM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER MM.
LT PHOTOLUMINESCENCE STRIP DELAMINATED AT ROW 1. R&R STRIP PER AMM.
RT PHOTOLUMINESCENCE STRIP DELAMINATED AT ROW 1. R&R STRIP PER AMM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PER MM.
L2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED THE LENS IAW MM.
DURING CLIMB OUT. LOST LNAV, VNAV AND SOME FMC FUNCTIONS INCLUDING ROUTE WHICH WENT INACTIVE. LOST SPEED BANDS AND SOME MCP FUNCTIONS. FLT DIRECTORS LOST. AFTER TROUBLESHOOTING SYSTEM CAME BACK AFTER 10-15 MINS. DIVERTED. R & R THE NR 1 AIR DATA INTERIAL REFERENCE DATA UNIT IAW MM.
DURING CLIMB OUT, LOST LNAV, VNAV AND SOME FMC FUNCTIONS INCLUDING ROUTE WHICH WENT INACTIVE. LOST SPEED BANDS AND SOME MCP FUNCTIONS. FLT DIRECTORS LOST. DIVERTED. AFTER TROUBLESHOOTING THE SYSTEM CAME BACK AFTER 10-15 MINS. R & R THE NR 2 AIR DATA INTERIAL REFERENCE DATA UNIT IAW MM.
FORWARD ENTRY HORSESHOE PANEL EMERGENCY LIGHT LENS BROKEN. R&R LENS PER MM.
RT OVERWING EXIT HATCH EXTERIOR EMERGENCY LIGHT NUTPLATE BROKEN. R&R LIGHT ASSEMBLY IAW MM.
RT EXTERNAL EMERGENCY EXIT LIGHT AT THE OVER WING EXIT INOP. R&R POWER SUPPLY IAW B737 AMM.
FORWARD SERVICE DOOR THRESHOLD CRACKED. REPAIRED THE THRESHOLD IAW EA.
AFT CARGO BAY BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 747 TO BS. 767, RT SIDE. R & R THE SIDEWALL SUPPORT IAW SRM.
ACB FWD NET TIE DOWN PLATE IS CRACKED / REMOVED ACB NET TIE DOWN PLATE IAW SRM 51-40-02-0G. 88952U 12/5/17 LEAD 59 05DEC17. INSTALLED NEW ACB FWD NET TIE DOWN IAW DWG #453A2611; SRM 51-40-02-0G-0; AIPC 25-52-10-02. 88952U 12/27/17
***CORROSION*** FORWARD CARGO COMPARTMENT PANEL 120AF HAS CORROSION ALONG FORWARD EDGE ON UPPER SURFACE / F.C.B. FLOOR PANEL 120AF. REMOVED AND EVALUATED DAMAGE 1.0' X 8.0' X .010'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 STEP 5(B) FABRICATED; LOCATED AND DRILLED NEW FLOOR PANEL; MADE OF 2024T3 X .071' IAW DWG #453A1610. MATERIAL LOT #1301996-1
***CORROSION*** AFT CARGO COMPARTMENT PANEL 140CF HAS CORROSION AT FORWARD EDGE OF THRESHOLD CUTOUT ON BOTTOM SIDE OF PANEL. / PANEL 140 CF FROM AFT CARGO COMPARTMENT FOUND TO BE OUT OF LIMITS DUE CORROSION AND ADITIONAL GOUGES EXCEED 50% OF PANEL AREA IAW SRM 53-00-53-1A-1 AD1 PAR 5; A (1). LOCATED; DRILLED AND FABRICATED FLOOR PANEL FROM 2024T3 CLAD .071' LOT # 1310914-1 IAW DWG # 453A2610 AND AMM 51-21-72-370-804
RW TE WIGGLE PLATE COMMON TO IB FWD ATTACH POINT OF PANEL 651EB CRACKED / REMOVED AND REPLACED RW TE WIGGLE PLATE COMMON TO IB FWD ATTACH POINT OF PANEL 651EB. P/N 115A2781-4 PO# 661472 IAW SRM 51-40-02. AND AIDE 57-50-00-22A
AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 747. R&R SUPPORT IAW SRM & DWG.
AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 747, TO FORWARD BULKHEAD. R & R THE SIDEWALL SUPPORT IAW SRM.
AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 747 TO FORWARD BULKHEAD. REPAIRED THE SIDEWALL SUPPORT IAW SRM.
***CORROSION*** AFT CARGO BAY FLOOR SUPPORT UPPER CHORD BS887 RBL4-LBL4 / REMOVED AND REPLACED AFT CARGO BAY FLOOR SUPPORT SPLICE TEE ITEM 146A9401U21 IAW DWG 146A9401 AND SRM 51-40-02 88324U 15DEC17
***CORROSION*** AT AFT CARGO BAY BS 727 O/B R/H BULKHEAD SUPPORT #2 FASTENER HOLE (MARKED) / NO ALLOWABLE DAMAGE FOUND ON SRM FOR ACB BS 727 O/B R/H BULKHEAD SUPPORT; PART IS REPAIRABLE BY REPLACEMENT IAW. SRM 51-10-02. REMOVED AND REPLACED BULKHEAD SUPPORT MADE FROM BAC1490-2596 7075 TO LOT # 1316020 HEAT TREATED TO T6 CONDITION. ITEM HFAB53-AN-011 PO # 61385; INSTALLED IAW. SRM 51-40-02; DWG 144A2600
AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 847 TO BS 867. R&R SUPPORT IAW SRM AND DWG.
L/W ORSS 271 SEAL RETAINER IS CRACKED.(MARKED) / REMOVED AND REPLACED L/W ORSS 271 SEAL RETAINER P/N 115A2953-1 IAW. SRM 51-40-02.
LOWER BULKHEAD SKIN CRACKED AT BS 540, BETWEEN STR 22L TO STR 23L. REPAIRED SKIN IAW EA AND ER.
FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 480 TO BS 500. R&R SUPPORT IAW SR & DWG.
RT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 92.70, 2ND STIFFENER FROM THE FRONT OF THE RIB, LOWER INBOARD FLANGE. REPAIRED RIB IAW SRM.
LOWER BULKHEAD SKIN CRACKED AT BS 540, BETWEEN STR 22R TO STR 23R. REPAIRED SKIN IAW EA AND ER.
RT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 92.70, 3RD STIFFENER FROM THE FRONT OF THE RIB, LOWER INBOARD FLANGE. REPAIRED RIB IAW SRM.
FORWARD CARGO BAY AFT BULKHEAD LOWER SUPPORT CORRODED AT BS 500D, RBL 12. R & R THE SUPPORT ANGLE IAW SRM AND DWG.
FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 495 TO 500A. R & R THE SIDEWALL SUPPORT IAW SRM AND DWG.
FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 420 TO 440. R & R THE SIDEWALL SUPPORT IAW DWG & SRM.
LT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 92.70, 3RD STIFFENER FROM FORWARD SPAR. REPAIRED RIB IAW SRM.
AFT SERVICE DOOR MOPSILL CORRODED BETWEEN BS 947 TO 987. R & R THE MOPSILL IAW SRM AND DWG.
AFT ENTRY DOOR MOPSILL CORRODED BETWEEN BS 947 TO BS 987. R & R THE MOPSILL IAW SRM AND DWG.
LT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 92.70, 2ND STIFFENER FROM FORWARD SPAR. REPAIRED RIB IAW SRM.
AFT CARGO BAY; AFT CORNER SCUFF PLATE CRACKED. / A.C.B; AFT CORNER. LOCATED AND DRILLED NEW SCUFF PLATE. ITEM 7530337 IAW SRM 51-40-05-0G-0. 89021C 06DEC17 INSP # 357 12/6/17
AFT CARGO BAY; FORWARD CORNER SCUFF PLATE CRACKED. / A.C.B; FWD CORNER. LOCATED AND DRILLED NEW SCUFF PLATE ITEM 7530659 IAW SRM 51-40-05-0G-0 89021C 06DEC17 INSP # 357 12/6/17
INTERCOSTAL AT BS 312- BS 328 LBL 46 WL 208 IS CRACKED. / REMOVED AND REPLACED INTERCOSTAL AT BS312-328 LBL 46 WL 208 IAW SRM 51-40-02 AND DWG # 141A5400 84632U 28NOV17
INTERCOSTAL AT BS 312- BS 328 RBL 31 WL 208 IS CRACKED. / REMOVED AND REPLACED INTERCOSTAL A + BS 312-328 RBL 31 WL 208 IAW SRM 51-40-02 AND DWG # 141A5400 84632U 28NOV17
R1 DOOR HANDLE HOUSING LOWER FITTING CRACKED AT FORWARD LOWER INBOARD BOLT HOLE AREA. R&R FITTING PER WO.
FLIGHT DECK, L3 WINDOW FRAME E-F POST FOUND TO BE CRACKED IN THE SECOND LOWER FASTENER HOLE. REPAIRED THE WINDOW POST IAW ACO.
FLIGHT DECK R1 WINDOW FRAME FOUND TO BE CRACKED THROUGH AT UPPER OUTBOARD CORNER. REPAIRED THE WINDOW FRAME IAW ACO.
FWD GALLEY DOOR LOWER BEAM COMMON TO HANDLE MECHANISM IS CRACKED NEAR FWD ATTACH BOLT / FSD LOWER BEAM; COMMON TO HANDLE MECHANISM. WAS REPLACED ON CARD T708464 & WO 502052
PANEL 192E FWD LH AND RH SUPPORT FITTING ARE BROKEN / REMOVED & REPLACED PANEL 192 E; FWD. L/H & R/H FUSELAGE SUPPORT FITTINGS IAW 737-700 SRM 51-40-02-0G-0 & AIPC 53-12-11-25.
RT NR 3 WINDOW FRAME E-F POST CRACKED IN THE 2ND AND 4TH LOWER FASTENER HOLES. REPAIRED POST IAW ACO.