N481WN
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2014-12-11 – 2014-12-11 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2014-12-11 – 2014-12-11 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
MUTIPLE EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED; INSTALLED SERVICEABLE, AND PERFORMED OPS CHECK OF EMERGENCY LIGHT BATTERY PACKS M1672, M1673, AND M1675 IAW AMM 33-51-06-960-805. OPS CHECK GOOD. PERFOMED OPS CHECK OF EMERGENCY LIGHT BATTERY PACKS IAW AMM 33-51-06-960-805. OPS CHKD GOOD.
RIGHT VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 25. REMOVED AND REPLACED RH VAPOR BARRIER UPPER ATTACH ANGLE AT BS 663 IAW SRM 51-40-02 AND BOEING DWG 111A1000 SHEET 45 REV:A AND BOEING DWG 111A1000 SHEET 153 REV-.
RIGHT WING TRAILING EDGE STRUCTURE; DEFLECTION CONTROL RIB AND SUPPORT BEAM ATTACHMENT. ELONGATED FASTENER HOLES NOTED. REPAIRED RIGHT WING TRAILING EDGE STRUCTURE; DEFLECTION CONTROL RIB AND SUPPORT BEAM ATTACHMENT ELONGATED FASTENER HOLES PER B737 SRM 57-51-02-2R-1 AND SRM SRM 57-51-02-2R-1. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS TO RIGHT WING TE DEFLECTION CONTROL RIB AND SUPPORT BEAM ATTACHMENT IAW SRM 57-51-02-2R-1 & SRM SRM 57-51-02-2R-4.
RIGHT WING TRAILING EDGE STRUCTURE; DEFLECTION CONTROL RIB AND SUPPORT BEAM ATTACHMENT. ELONGATED FASTENER HOLES NOTED. REPAIRED RIGHT WING TRAILING EDGE STRUCTURE; DEFLECTION CONTROL RIB AND SUPPORT BEAM ATTACHMENT ELONGATED FASTENER HOLES IAW SRM 57-51-02-2R-1 AND SRM SRM 57-51-02-2R-1. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS TO RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB AND SUPPORT BEAM ATTACHMENT IAW SRM 57-51-02-2R-1 AND SRM SRM 57-51-02-2R-4.
EXIT SIGN LENS AT EXIT ROW RIGHT MISSING. INSTALLED A NEW EXIT SIGN LENS IAW AMM 33-51-01.
ESCAPE SLIDE FRONT GALLEY DOOR LOOSE. REPACKED FWD SERVICE DOOR SLIDE IAW MT 725-61-06.
RIGHT EMERGENCY EXIT LIGHT IS INOP ABOVE HATCH. R & R OVERWING SIDEWALL LIGHT AND LENS IAW AMM 33-51-03.
LEFT EMERGENCY EXIT LIGHT IS DIM ABOVE HATCH. R & R THE OVERWING SIDEWALL LIGHT AND LENS PER AMM 33-51-03.
LEFT EMERGENCY EXIT LIGHT IS DIM ABOVE HATCH. R & R THE OVERWING SIDEWALL LIGHT AND LENS PER AMM 33-51-03.
RIGHT EMERGENCY EXIT LIGHT IS INOP ABOVE HATCH. R & R THE OVERWING SIDEWALL LIGHT AND LENS IAW AMM 33-51-03.
ELECTRIC STABILIZER TRIM INOPERATIVE. ] R & R STAB TRIM MOTOR PER AMM 27-41-71 OPS CHECK GOOD.
AFT ENTRY DOOR ASSIST HANDLE IS CRACKED.<[01] R&R AFT ENTRY DOOR ASSIST HANDLE ATTACH FITTING IAW AMM 52-13-31.;[02] INSP IAW AMM 52-13-31
LEFT SIDE SLIDING WINDOW HEATING ELEMENT ARC-ED. LASTED A FEW SECONDS WITH A STRONG SMELL. TURNED WINDOW HEAT OFF; NO CBS POPPED.<[01] REPLACED LT. NO. 2 OPENABLE WINDOW IAW AMM 56-12-11 AND MT 756-12-02. REPLACED LT. SIDE WHCU BECAUSE OF ARCING WHICH OCCURRED IAW AMM 30-41-11.
CUSTOMER WALK ITEMS / R2DOOR SLIDE SKIRT HANGS ON THRESHOLD WHEN DOOR OPERATED<[01] REPOSITION R2 DOOR ESCAPE SLIDE SKIRT AS PER WORK INSTRUCTIONS 725-61-06;[02] VERIFIED STEP 1.
CUSTOMER WALK ITEMS / L2 DOOR SLIDE SKIRT HANGS ON THRESHOLD WHEN DOOR OPERATED<[01] REPOSITION L2 DOOR ESCAPE SLIDE SKIRT AS PER WORK INSTRUCTIONS 725-61-06;[02] VERIFIED STEP 1.
CUSTOMER WALK ITEMS/ 1 EA BULB BURNED OUT ON EMER EXIT SIGN ABOVE R2 DOOR<[01] RE-LAMPED 1 LAMP ON EMERGENCY EXIT SIGN ABOVE R2 DOOR AS PER AMM REF 33-51-01-960-801. INSTALLATION TEST FOUND NORMAL.;[02] VERIFIED STEP 1.
R1 DOOR FWD CUTOUT PANEL CRACKED AT LOWER SECTION<[01] REPAIRED R1 DOOR FWD CUTOUT PANEL AT LOWER SECTION AS PER B737 AMM 25-00-00-300-802.;[02] VERIFIED STEP 1<BR>AUDIT C/W REF MPM 52.02.02
L/H AFTER WING EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] TROUBLESHOT INOPERATIVE L/H AFT WING EMERGENCY LIGHT (L547) REF B737 FIM 33-50 TASK 801; REMOVED AND REPLACED CONNECTOR D11082 AT EMERGENCY LIGHT L547 REF B737 SWPM 20-61-28; PERFORMED EMERGENCY LIGHT L547 OPERATIONAL TEST; TEST CHECKED NORMAL REF B737 AMM 33-51-04-960-802.;[02] REMOVED AND REPLACED CONNECTOR D11082 AT EMERGENCY LIGHT L547 REF B737 SWPM 20-61-28; OPS CHECK FOUND NORMAL;[03] VERIFIED STEP 1; 2<BR>AUDIT C/W REF MPM 52.02.02
L2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] REPLACED LAMP AT L2 DOOR EXTERIOR EMERGENCY LIGHT (L732) IN REF WITH B737 AMM 33-51-04-960-801.LAMP TEST NORMAL.;[02] VERIFIED STEP 1
L1 DOOR LINER EMERGENCY EXIT SIGN INOP<[01] FOUND CONNECTOR D2972 FOR EXIT LIGHT NOT PROPERLY SEATED; RESEAT I/A/W BOEING WDM 33-51-12; PERFORMED OPS CHECK OF EMERGENCY LIGHTS I/A/W BOEING AMM 33-51-00-710-801; OPS CHECK NORMAL;[02] VERIFIED STEP 1<BR>AUDIT C/W REF MPM 52.02.02
**REJECTION** DURING OK TO CLOSE FOUND AFT CARGO SCUFF PLATE AFT CORNER CRACKED MKD (107-001)<[01] RECEIVED AFT CARGO SCUFF PLATE AFT CORNER P;O 2074280 WILL BE INSTALL ON THIS CARD TTG80022CD3;[02] RECEIVED AFT CARGO SCUFF PLATE AFT CORNER P;O 2074280 WILL BE INSTALL ON THIS CARD TTG8Q0022CD3;[03] VERIFIED STEP 1<BR>AUDIT C/W REF MPM 52.02.02
RIGHT WING O/B AFT FLAP AT #6 CUT OUT EDGE COVER CRACKED<[01] REMOVED AND REPLACED RIGHT WING O/B AFT FLAP AT #6 CUT OUT EDGE COVER B737 SRM-51-40-02-0G-0 DWG#113A3700 AND AICP-27-51-22-01.;[02] VERIFIED STEP 1<BR>AUDIT C/W REF MPM 52.02.02
FOUND CHANNEL TIE WITH PITTING CORROSION AT E&E COMP INTERNAL SIDE STA 351.2+8 BL0<[01] REMOVED; FABRICATED AND INSTALLED NEW CHANNEL TIE AT SKIN BS 351.2+8 BL 0 PER REF SRM 51-40-02-0G-0 AND DWG 141A1160;[02] VERIFIED STEP 1<BR>AUDIT C/W REF MPM 52.02.02
KEEL BEAM UNDER WING-TO-BODY FAIRING PANEL 192E HAS SUPPORT WITH FRETTING AT STA 600. 8-48<[01] REMOVED AND INSTALLED NEW SUPPORT AT KEEL BEAM UNDER WING-TO-BODY FAIRING PANEL 192E AS PER SRM-51-40-02-0G-0;[02] VERIFIED STEP:1
L/W LOWER LEADING-EDGE PANEL#521XB HAS SCREW HOLE CRACKED. 8-46<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #521XB AS PER B737 SRM 51-70-04-2R-9; MATERIAL USED; PO#1791128; PO#1473815; TOOL USED; TEMP CONTROLLER ID 160354; CALIBRATION DUE 03-07-25.;[02] VERIFIED STEP 1<BR>AUDIT PER MPM 52-02-02
LEFT HORIZONTAL STABILIZER L/E PANEL RIB # 2 CRACK.<[01] REMOVED CRACKED RIB #2 AT LEFT HORIZONTAL STABILIZER L/E PER B737-700 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW RIB #2 AT LEFT HORIZONTAL STABILIZER L/E PANEL PER B737-700 SRM 51-40-05-0G-0 AND DWG#: 186A1302. INSTALLED NEW RIB #2 AT LEFT HORIZONTAL STABILIZER L/E PANEL PER B737-700 SRM 51-40-02-0G-0 AND DWG#:186A1302.;[02] VERIFIED STEP 1.
LEFT HORIZONTAL STABILIZER L/E PANEL RIB # 3 CRACK.<[01] LOCATED AND DRILLED NEW RIB #3 AT LEFT HORIZONTAL STABILIZER L/E PER B737-700 SRM 51-40-05-0G-0 AND DWG#:186A1303.<BR>OK TO INSTALL NEW RIB #3 AT LEFT HORIZONTAL STABILIZER L/E PANEL.<BR>INSTALLED NEW RIB #3 AT LEFT HORIZONTAL STABILIZER L/E PER B737-700 SRM 51-40-05-0G-0 AND DWG#:186A1303.;[02] VERIFIED STEP 1.
RH HORIZONTAL STAB PANEL 343 BLADE SEAL RETAINER CRACK. RH HORIZONTAL STAB PANEL 343AB BLADE SEAL RETAINER CRACK.<[01] REMOVED AND REPLACED RH HORIZONTAL STAB PANEL 343 BLADE SEAL RETAINER ANGLE REF. SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED RH HORIZONTAL STAB PANEL 343 BLADE SEAL RETAINER ANGLE REF. SRM 51-40-02-0G-0;[03] REMOVED AND REPLACED RH HORIZONTAL STAB PANEL 343AB BLADE SEAL RETAINER ANGLE REF. SRM 51-40-02-0G-0;[04] VERIFIED STEP 3.
CORROSION SPOT IN E&E AT SKIN BS 351.2+6 BL O. 8-25<[01] REMOVED; FABRICATED AND INSTALLED NEW CHANNEL AT SKIN BS 351.2+6 BL 0 PER REF SRM 51-40-02-0G-0 AND DWG 141A3502;[02] VERIFIED STEP 1<BR>ATC ANTENNA WILL BE INSTALL ON T/C TTG8Q00UT1KC<BR>AUDIT C/W REF MPM 52.02.02
CENTER CABIN FLOOR PANEL 231YF HAS UPPER SURFACE LAYER FIBERS PEELED. 124-001<[01] RECEIVED NEW PANEL # 231YF INSTALLATION WILL BE ACCOMPLISH ON # TTG8Q00TNY32;[02] CORRECTED STEP 1 . RECEIVED NEW PANEL # 231YF INSTALLATION WILL BE ACCOMPLISH ON #TTG8Q00TNY33;[03] VERIFIED STEP:2<BR>AUDIT C/W REF MPM 52.02.02
AFT OF AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT BRACKET CRACKED @ AFT END FWD OF WATER TANK STA 947.75 S-26L MKD DOT<[01] INSTALLED BRACKETED AT AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT AT AFT END FORWARD OF WATER TANK STA.947.5 S-26L AS PER BOEING 737 SRM 51-40-02-0G-0;[02] REMOVED/INSTALLED BRACKET AT AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT AT AFT END FORWARD OF WATER TANK STA.947.5 S-26L AS PER BOEING 737 SRM 51-40-02-0G-0;[03] REMOVED/INSTALLED BRACKET AT AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT AT AFT END FORWARD OF WATER TANK STA.947.5 S-26L AS PER BOEING 737 SRM 51-40-02-0G-0 AND DRW 149A8113;[04] VERIFIED STEPS 1; 2 AND 3.
CENTER CABIN FLOOR PANEL 241BF HAS UPPER SURFACE LAYER FIBERS PEELED AND 3EA EXISTING REPAIRS. 124-002<[01] RECEIVED NEW PANEL # 241BF ; INSTALLATION WILL BE ACCOMPLISH ON # TTG8Q00TNY15;[02] CORRECTED STEP 1 .RECEIVED NEW PANEL # 241BF ; INSTALLATION WILL BE ACCOMPLISH ON # TTG8Q00TNY16;[03] VERIFIED STEP:2<BR>AUDIT C/W REF MPM 52.02.02
FWD CARGO COMPARTMENT GAUSET CRACKED AT S-21R STA 500D MKD DOT<[01] REMOVED GAUSET AT S-21R STA 500D PER SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW PART PER SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PART PER SRM 51-20-01-0G-0; INSTALLED NEW PART PER SRM 51-40-02-0G-0;[02] VERIFIED STEP:1<BR>AUDIT C/W REF MPM 52.02.02
FWD CABIN L-1 DOOR CUTOUT AFT JAMB LOWER INB COVER PLATE APPEARS CRACKED @ LOWER HOLE STA 348.2 MKD DOT<[01] PERFORMED HFEC INSP. ON SUSPECTED CRACK IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. CRACK CONFIRMED (LENGTH 1') <BR>TOOL: NORTEC 600 B/C: 166316 DUE: 10/27/24;[02] STEP 1 ENTER IN ERROR;[03] REMOVED; FRABRICATED AND INSTALLED NEW FWD CABIN L-1 DOOR CUTOUT AFT JAMB LOWER INB COVER PLATE AS PER SRM-51-40-02-0G-0 ANDDWG#141A890.;[04] CORRECTION TO STEP 3: REMOVED; FRABRICATED AND INSTALLED NEW FWD CABIN L-1 DOOR CUTOUT AFT JAMB LOWER INB COVER PLATE AS PER SRM-51-40-02-0G-0 ANDDWG#141A8190;[05] CORRECTION TO STEP 4: REMOVED; FRABRICATED AND INSTALLED NEW FWD CABIN L-1 DOOR CUTOUT AFT JAMB LOWER INB COVER PLATE AT LOWER HOLE STA 348.2AS PER SRM-51-40-02-0G-0 ANDDWG#141A8190;[06] (RII) VERIFIED STEP:5;[07] CORRECTION STEP:6 (RII) VERIFIED STEP:5.<BR>AUDIT C/W REF MPM52.02.02
CORROSION** FWD CARGO COMPARTMENT FLOOR SUPPORT SHIELD @ S-26R STA 500 TO 500A MKD DOT<[01] REMOVED FWD CARGO COMPARTMENT FLOOR SUPPORT SHIELD AT S-26R FROM STA 500 TO 500A PER SRM 51-40-02-0G-0; RECEIVED NEW PART; LOCATED AND DRILLED NEW PART PER SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PART PER SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804; INSTALLED NEW PART PER SRM 51-40-02-0G-0;[02] CORRECT STEP 1: REMOVED FWD CARGO COMPARTMENT FLOOR SUPPORT SHIELD AT S-26R FROM STA 500 TO 500A PER SRM 51-40-02-0G-0; RECEIVED NEW PART; LOCATED AND DRILLED NEW PART PER SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PART PER SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804; INSTALLED NEW PART PER SRM 51-40-02-0G-0; DWG NO: 143A0080;[03] VERIFIED STEP 2<BR>AUDIT PER MPM 52-02-02
FWD CARGO COMPARTMENT GUSSET CRACKED AT S-19R STA 500D MKD DOT<[01] REMOVED GUSSET AT S-19R STA 500D PER SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW PART PER SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PART PER SRM 51-20-01-0G-0; INSTALLED NEW PART PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP:1<BR>AUDIT C/W REF MPM 52.02.02
FWD CARGO COMPARTMENT GAUSET CRACKED AT S-19L STA 500D MKD DOT<[01] REMOVED GAUSET AT S-19L STA 500D PER SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW PART PER SRM 51-40-05-0G-0; TREATED AND PRIMED NEW PART PER SRM 51-20-01-0G-0; INSTALLED NEW GAUSET PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP:1<BR>AUDIT C/W REF MPM 52.02.02
CORROSION ** AFT CARGO COMPARTMENT BILGE SKIN PREVIOUS DOUBLER REPAIR @ S-26R STA 807+5' MKD DOT<[01] ACCOMPLISHED REPAIR PER EA -24-153-01888 AT AFT CARGO COMPARTMENT BILGE STR 26R STA 807'+5'.;[02] VERIFIED STEP 1; 2<BR>TREAT AND PRIME C/W ON EA 24-153-01880-WIP1<BR>AUDIT C/W REF MPM 52.02.02
RIGHT VERTICAL FIN PANEL#323AR ASSY SUPPORT ANGLE LOWER SURFACE HAS BARE METAL. RIGHT VERTICAL FIN PANEL#323AR ASSY CRACKED AT LOWER CORNER<[01] RECEIVED NEW PART. LOCATED AND DRILLED AND COUNTERSUNK FASTENER HOLES ON NEW VERTICAL PANEL 323AR REF. SRM 51-40-05-0G0 & SRM 51-40-08-0G-0;[02] VERIFIED STEP 1.
CORROSION ** L/H RAM AIR INLET FWD DOOR ACTUATING ROD LOWER LINK MKD DOT<[01] REMOVED AND REPLACED L/H RAM AIR INLET FWD DOOR ACTUATING ROD LOWER LINK AS PER AMM 21-51-22-000-802 AND 21-51-22-400-802.;[02] VERIFIED STEP:1
AFT OF FWD CARGO COMPARTMENT INTERCOSTAL SUPPORT CRACKED @ AFT END BETWEEN STA 500D AND 520 S-25R<[01] REMOVED FWD CARGO COMPARTMENT INTERCOSTAL SUPPORT BETWEEN STA 500D AND 520 S-25R PER SRM 51-40-02-0G-0; ACCOMPLISHED HEAT TREATMENT OF FABRICATED PART PER OP 84; TYPE: PL; 143A9803-58; LOCATED AND DRILLED NEW INTERCOSTAL SUPPORT PER SRM 51-40-05-0G-0; TREATED AND PRIMED NEW INTERCOSTAL SUPPORT PER SRM 51-20-01-0G-0; INSTALLED NEW FWD CARGO COMPARTMENT INTERCOSTAL SUPPORT PER SRM 51-40-02-0G-0; DWG 143A9801.;[02] VERIFIED STEP:1
MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT LBL 1 STA 540<[01] REVOVED AND REPLACED PANEL BREAK AT MAIN CABIN CENTER SECTION; STA 540; LBL 1 AS PER B737-700 SRM 51-40-02-0G-0.;[02] ADDING DWG# 143A5240 O N STEP 1 (FINAL).;[03] VERIFIED STEP:1 AND STEP:2
AFT CARGO COMPARTMENT AFT SCUFF PLATE CRACKED<[01] REPAIRED PART 'AFT CARGO AFT SCUFF PLATE' RECEIVED AND WILL BE INSTALLED ON CARD: TTG8Q00229WY;[02] VERIFIED STEP 1.
L/W REAR SPAR LOWER FIXED T/E PANEL 551GB INB AFT SUPPORT ROD LOWER ATTACHED FITTING ELONGATED HOLE MKD DOT<[01] REMOVED AND REPLACED L/W REAR LSPAR LOWER FIXED T/E PANEL# 551GB AFT SUPPORT ROD PER REF SRM 51-40-02-0G-0;[02] VERIFIED STEP:1
MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT RBL 1 STA 540<[01] REMOVED AND REPLACED PANEL BREAK AT MAIN CABIN CENTER SECTION; STA 540; RBL 1 AS PER B737-700 SRM 51-40-02-0G-0.;[02] ADDING DWG#143A5240 ON STEP 1 (FINAL).;[03] VERIFIED STEP:1 AND STEP:2
LOWER FUS CENTER SECTION ATTACHED ANGLE CRACKED @ RAM AIR EXIT EXHAUST DUCT CUTOUT SEAL O/B LOWER CORNER MKD DOT<[01] REMOVED AND INSTALLED ANGLE AT LOWER FUS CENTER SECTION @ RAM AIR EXIT EXHAUST DUCT CUTOUT SEAL O/B LOWER CORNER AS PER SRM-51-40-02-0G-0 DWG# 111A1000;[02] VERIFIED STEP:1<BR>AUDIT C/W REF MPM 52.02.02
L/W OUB AFT FLAP INB END LOWER SURFACE DELAMINATION AROUND PREVIOUS REPAIR MKD DOT<[01] REMOVE AND REPLACED L/W OUB AFT FLAP AS PER AMM 27-51-22-000-801 AND 27-51-22-400-801.;[02] VERIFIED STEP 1
CAPT FWD OB SEAT TRACK HAS CORROSION.<[01] RECIEVED NEW PART. INSTALATION WILL BE ACCOMPLISHED ON TTG8Q0022A89.;[02] CORRECTION TO STEP 1: RECIEVED NEW CAPT FWD OB SEAT TRACK. INSTALATION WILL BE ACCOMPLISHED ON TTG8Q0022A89.;[03] VERIFIED 2.
F/O FWD OB SEAT TRACK HAS CORROSION.<[01] RECIEVED NEW PART. INSTALATION WILL BE ACCOMPLISHED ON TTG8Q0022A89.;[02] CORRECTION TO STEP 1: RECIEVED NEW F/O FWD OB SEAT TRACK. INSTALATION WILL BE ACCOMPLISHED ON TTG8Q0022A89.;[03] VERIFIED 2.
KEEL BEAM UNDER WING-TO-BODY FAIRING FOUND BRACKET CRACK AT STA 560 UNDER PANEL#192E KEEL BEAM UNDER WING-TO-BODY FAIRING FOUND BRACKET CRACK AT STA 600 UNDER PANEL#192E<[01] BRACKET WAS RECEIVED AND REPLACED ON [TTG8Q00U3VT0];[02] VERIFIED STEP:1
KEEL BEAM UNDER WING-TO-BODY FAIRING FOUND BRACKET CRACK AT STA 600 UNDER PANEL#192E<[01] REMOVED AND INSTALLED NEW BRACKET AT KEEL BEAM UNDER WING-TO-BODY AT STA 600 UNDER PANEL#192E AS PER SRM-51-40-02-0G-0.;[02] VERIFIED 1.
CAPT FWD IB SEAT TRACK HAS CORROSION.<[01] RECIEVED NEW PART. INSTALATION WILL BE ACCOMPLISHED ON TTG8Q0022A89.;[02] VERIFIED 1.
PANEL 192F HAS FLAME SPRAY CORRODED AT ANTENNA MOUNT AREA. 8-22<[01] RECIEVED NEW PANEL. WORK WILL BE ACCOMPLISHED ON TTG8Q00U3UBG;[02] CORRECTION TO STEP 1: <BR>RECIEVED NEW PANEL; PART NUMBER 14A7755-1 192F. WORK WILL BE ACCOMPLISHED ON TTG8Q00TNXXE;[03] VERIFIED STEP 2<BR>AUDIT PER MPM 52-02-02
F/O FWD IB SEAT TRACK HAS CORROSION.<[01] RECIEVED NEW PART. INSTALATION WILL BE ACCOMPLISHED ON TTG8Q0022A89.;[02] CORRECTION TO STEP 1: RECIEVED NEW F/O FWD IB SEAT TRACK. INSTALATION WILL BE ACCOMPLISHED ON TTG8Q0022A89.;[03] VERIFIED 2.
CORROSION ON INNER SURFACE OF LAV SER PNL 145AL. 8-18<[01] REMOVED AND REPLACED NEW DOOR ASSY P/N 146A7410-6 ISSUE TAG JT2322 AS PER B-737-AMM 52-49-07-400-801; TOOL USED BONDING MILLI-OHMMETER C/ID:168696 DUE DATE:21-MAR-25<BR>01 - REMOVED AND REPLACED PER [REFERENCE]<BR>01 - REMOVED AND REPLACED PER [REFERENCE]<BR>01 - REMOVED AND REPLACED PER [REFERENCE];[02] CORRECTED STEP 1. REMOVED AND REPLACED NEW DOOR ASSY P/N 146A7410-6 ISSUE TAG JT2322 AS PER B-737-AMM 52-49-07-400-801; TOOL USED BONDING MILLI-OHMMETER C/ID:168696 DUE DATE:21-MAR-25 IPC 52-49-07-01;[03] VERIFIED STEP 2.
CUSTOMER REQUEST-CORROSION PIT IN FUSELAGE SKIN BY FASTENER HOLE BS 907 S-25L. 8-16<[01] REMOVED CORROSION AT FUSELAGE SKIN BY FASTENER HOLE BS 907 S-25L FOUND TO BE WITHIN LIMITS PER REF SRM 53-00-01-1A-1; REMOVED AND INSTALLED NEW FASTENER; TREATED; PRIMED AND TOPCOAT AREA PER REF SRM 51-40-02-0G-0; AMM 51-21-41-370-803 ;AMM 51-21-72-370-804 AND AMM 51-21-73-370-803;[02] CORRECTINGT STEP 1: REMOVED CORROSION AT FUSELAGE SKIN BY FASTNER HOLE BS 907 S-25L FOUND TO BE WITHIN LIMITS PER REF SRM 53-00-01-1A-1; REMOVED AND INSTALLED NEW FASTENER; TREATED; PRIMED AND TOPCOAT AREA PER REF SRM 51-40-02-0G-0; AMM 51-21-41-370-803 ;AMM 51-21-72-370-804 AND AMM 51-21-73-370-803;[03] VERIFIED STEP 2<BR>AUDIT PER MPM 52-02-02
RWW FWD SIDE OF VAPOR BARRIER CRACKED AT 4 EACH FASTENER HOLES ALONG LWR EDGE ABOVE PACK AIR HEAT EXCHANGR OUTLET RBL 18. 8-19<[01] APPLIED REPAIR ON RWW FWD SIDE VAPOR BARRIER AT 4 EACH FASTNER HOLES AND CURED PER B737 SRM 51-70-04-2R-9 PARAGRAPH 4.K AND 4.M AND B737 SRM 51-70-04-2R-0 PARAGRAPH 4.L AND 4.N. MATERIALS USED RESIN EY3804 P/O#1759622; CLOTH BMS-9-3 P/O#1738579. TOOLS USED TEMP CONTROLLER ID 160354; CALIBRATION DUE: 03-07-25. AND APPLIED TOPCOAT AT RWW FWD SIDE OF VAPOR BARRIER ON REPAIR AREA PER B737 AMM51-21-72-370-802 PRIMER USED 512X310QTKT PO#2059196;[02] VERIFIED COMPOSITE REPAIR ON VAPOR BARRIER.
PANEL 323CL PN 172A6124-1 ENLONGATED HOLES<[01] RECEIVED NEW PANEL 323CL P/N 1726164-1.<BR>LOCATED; DRILLED AND COUNTERSUNK NEW HOLES ON NEW PANEL 323CL P/N 172A6124-1 REF. SRM 51-40-05-0G-0.<BR>NEW PANEL 323CL P/N 1726164-1 WOULD BE PAINTED PER NON ROUTINE ITEM TTG8Q00UE3TW / 2022622-3000/0057.<BR>NEW PANEL 323CL WOULD BE INSTALLED WITH CUSTOMER ORDER CARD TTG8Q00TNZ82 / 2022620-3000/0146;[02] VERIFIED STEP 1.
GIRT WORN<[01] REMOVED AND REPLACED GIRT PER GCMM 25-60-37;[02] C/W INSPECTION
FWD NORTH DOOR EMERGENCY SLIDE FELL OUT FWD ENTRY DOOR EMERGENCY SLIDE FELL OUT<[01] REINSTALLED FWD ENRTY DOOR ESCAPE SLIDE PER MT 725-61-06
LH OVERWING AISLE AND FLAP GROUND CLEARANCE EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED EMERGENCY POWER SUPPLY AND BATTERY PACK M1670 PER AMM 33-51-06. OPS CHECKED GOOD.
L1 DOOR EXIT SIGN WRONG LENS<[01] R/R L1 DOOR EMERGENCY EXIT SIGN LENS IAW AMM 33-51-00.
COCKPIT EMERGENCY LIGHT INOP<[01] RELAMPED COCKPIT EMERGENCY LIGHT IN ACCORDANCE WITH AMM 33-51-03
FWD ENTRY DOOR ASSIST HANDLE BROKEN.<[01] REPLACED FWD ENTRY DOOR ASSIST HANDLE IAW SIP.
LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW SIP. OPS CHECKED GOOD.
DELAMINATED BULKHEAD PANEL 121HW FIBER PLY FWD CARGO COMPARTMENT 2022-268391 / [01] REPAIRED BULKHEAD PANEL 121HW IAW B737-700 AMM 25-52-01-300-804 AND AMM 25-52-00-200-803.;[02] REPAIRED BULKHEAD PANEL 121HW IAW B737-700 AMM 25-52-01-300-804 AND AMM 25-52-00-200-803.
DELAMINATED BULKHEAD PANEL 121EW FIBER PLY FWD CARGO COMPARTMENT 2022-268392 / [01] REPAIRED BULKHEAD PANEL 121EW IAW B737-700 AMM 25-52-01-300-804 AND AMM 25-52-00-200-803.;[02] REPAIRED BULKHEAD PANEL 121EW IAW B737-700 AMM 25-52-01-300-804 AND AMM 25-52-00-200-803.
DELAMINATED BULKHEAD PANEL 122GW FIBER PLY FWD CARGO COMPARTMENT 2022-268390 / [01] REPAIRED BULKHEAD PANEL 122GW IAW B737-700 AMM 25-52-01-300-804 AND AMM 25-52-00-200-803.;[02] REPAIRED BULKHEAD PANEL 122GW IAW B737-700 AMM 25-52-01-300-804 AND AMM 25-52-00-200-803.
(AEROMAN REQUEST) CRACK ON FAIRING PANEL 543EB LH WING 2022-268372 / [01] TOOL USED: CALIPER P/N:500-464 S/N:15331926 DUE DATE: 28-SEP-22;[02] TOOL USED: HOT BONDER P/N: HCS9000B S/N: 18175469 DUE DATE: 05-AUG-22.;[03] TOOL USED: SCALE: P/N: SCA-301 S/N: AE-412123 DUE DATE: 14-MAR-23;[04] TOOL USED: MULTIMETER P/N: FLUKE 87-5 S/N: 32040125 DUE DATE: 21-SEP-22.;[05] REPAIRED FAIRING PANEL 543EB LH WING IAW B737-700 SRM 51-70-05-2R-2 REPAIR 2 AND B737-700 SRM 51-70-05-2R-0 REPAIR GENERAL PARAGRAPH 4;[06] CORRECTED STEP 5: REPAIRED FAIRING PANEL 543EB LH WING IAW B737-700 SRM 51-70-05-2R-2 REPAIR 2 AND B737-700 SRM 51-70-05-2R-0 REPAIR GENERAL PARAGRAPH 4.<BR><BR>SEE INDIVIDUAL SINGOFF BELOW.;[07] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW
CRACK ON VERTICAL WEB FLOORBEAM 727B LOC. LBL 45.5 AT AFT CARGO COMPARTMENT 2022-268342 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[03] REPAIRED VERTICAL WEB FLOORBEAM 727B LOC. LBL 45.5 AT AFT CARGO COMPARTMENT IAW B737-700 EA Nÿ½ 22-153-01843-WIP1 REV 2 AND EA Nÿ½ 2-153-01843 REV 1. SEE INDIVIDUAL SIGNOFF BELOW.;[04] CORRECTED STEP 3<BR>PERFORMED REPAIR IAW EA Nÿ½ 22-153-01843-WIP1 REV 2 AND EA Nÿ½ 2-153-01843 REV1 ON TRANSVERSAL FLOOR BEAM ? AT BSTA 727B ? AND BTW LBL 40 & LBL 50. SEE INDIVIDUAL SIGNOFF BELOW.;[05] PERFORMED REPAIR IAW EA Nÿ½ 22-153-01843-WIP1 REV 2 AND EA Nÿ½ 2-153-01843 REV1 ON TRANSVERSAL FLOOR BEAM ? AT BSTA 727B ? AND BTW LBL 40 & LBL 50. SEE INDIVIDUAL SIGNOFF BELOW.<BR>RII
CRACK ACCESS PANEL 551FB ANGLE AT LT WING (1 EA) 2022-268279 / [01] REPLACED ACCESS PANEL 551FB ANGLE AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; DWG 115A2710 REV: B.;[02] REPLACED ACCESS PANEL 551FB ANGLE AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; DWG 115A2710 REV: B.
CORROSION SEAT TRACK LOCATED ON BOTTOM SURFACE BTW BS 360 TO BS 380 LBL 24.75 WL 208.1 AT PASSENGER CABIN 2022-268233 / [01] TOOL USED: DIGITAL CALIPER; P/N: 500-197-30; S/N: B20189443; DUE DATE: 03-DEC-22.;[02] TOOL USED: POWER PACK P/N FMK0003223 S/N PE0412/63335 DUE DATE: 26-JAN- 23.MULTIMETER P/N FLUKE 87 S/N 44560136 DUE DATE: 21-SEP-22. THERMOMETER P/N FLUKE 566 S/N 36160082WS DUE DATE: 08-JUL-22;[03] REPLACED SEAT TRACK LOC BTW BS 360+10? TO BS 480 LBL 24.75 AND WEB BTW BS 380 TO BS 400 AND FASTENERS IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5300 SHEET 21 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[04] REPLACED SEAT TRACK LOC BTW BS 360+10? TO BS 480 LBL 24.75 AND WEB BTW BS 380 TO BS 400 AND FASTENERS IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5300 SHEET 21 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.<BR><BR>RII ACCOMPLISHED
CRACK ANGLE - SUPPORT LOCATED BS 867 BWT STR 25L TO STR 26L AT AFT CARGO COMPARTMENT 2022-268242 / [01] REPLACED ANGLE - SUPPORT LOCATED BS 867 BWT STR 25L TO STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9.;[02] CORRECTED STEP 1<BR>REPLACED ANGLE - SUPPORT LOCATED BS 867 BWT STR 25L TO STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9.LENGTH OF CRACK: 1.2050 TOOL USED CALIPER P/N:500-197-30 S/N: A21042094 DUE DATE: 01FEB23.;[03] REPLACED ANGLE - SUPPORT LOCATED BS 867 BWT STR 25L TO STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9.LENGTH OF CRACK: 1.2050 TOOL USED CALIPER P/N:500-197-30 S/N: A21042094 DUE DATE: 01FEB23.<BR>CERTIFIED AS RII
CORROSION SEAT TRACK LOCATED ON BOTTOM SURFACE BTW BS 360 TO BS 380 LBL 45.5 WL 208.1 AT PASSENGER CABIN 2022-268232 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-193-30; S/N 0000291; DUE DATE: 16-SEP-22.;[02] TOOL USED POWER PACK P/N: FMK0003223; S/N: PE0412/63335; DUE DATE: 26-JAN-23; THERMOMETER P/N: 42510A; S/N: 200813258; DUE DATE 29-JUN-22; MULTIMETER P/N: FLUKE 87; S/N: 37640185; DUE DATE: 31-OCT-22.;[03] REPLACED SEAT TRACK LOC BTW BS 360+10? TO BS 480 LBL 45.5. I.A.W B737-700 SRM 51-40-02 AND DWG:141A5300 SHEET:2 REV:A AND DWG:143A5300 SHEET:42 REV:A. <BR>SEE INDIVIDUAL SIGNOFF BELOW;[04] REPLACED SEAT TRACK LOC BTW BS 360+10? TO BS 480 LBL 45.5. I.A.W B737-700 SRM 51-40-02 AND DWG:141A5300 SHEET:2 REV:A AND DWG:143A5300 SHEET:42 REV:A. <BR>SEE INDIVIDUAL SIGNOFF BELOW. COMPLETED
CRACK TRACK RBBL 13.84 LOCATED BS 767 AT AFT CARGO COMPARTMENT 2022-268241 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210136503; DUE DATE: 11-APR-23.;[02] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A21303945 DUE DATE: 06-MAY-22.;[03] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 500D; SN: N500X12101V022240; DUE DATE: 27-JAN-23;[04] REPAIRED CARGO TRACK BTW BS 747 TO BS 787 RBBL 13.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 2. SEE INDIVIDUAL STEP SIGNOFF BELOW;[05] CORRECTED STEP 4: REPAIRED CARGO TRACK BTW BS 747 TO BS 787 RBBL 13.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 2. SEE INDIVIDUAL SIGNOFF BELOW;[06] CORRECTED STEP 4: REPAIRED CARGO TRACK BTW BS 747 TO BS 787 RBBL 13.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 2. SEE INDIVIDUAL SIGNOFF BELOW
CRACK SUPPORT BRACKET TRAILING EDGE AT LEVEL WS 236 RT WING 2022-268137 / [01] REPLACED SUPPORT BRACKET TRAILING EDGE AT LEVEL WS 236 RT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02;[02] REPLACED SUPPORT BRACKET TRAILING EDGE AT LEVEL WS 236 RT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02
CRACK SUPPORT BRACKET BODY STATION 540 LBL 6 KEEL BEAM 2022-268140 / [01] REPLACED SUPPORT BRACKET BODY STATION 540 LBL 6 KEEL BEAM IAW B737-700 SRM 51-40-02;[02] REPLACED SUPPORT BRACKET BODY STATION 540 LBL 6 KEEL BEAM IAW B737-700 SRM 51-40-02
CRACK SUPPORT BRACKET BODY STATION 540 RBL6 KEELBEAM 2022-268139 / [01] REPLACED SUPPORT BRACKET BODY STATION 540 RBL6 KEELBEAM IAW B737-700 SRM 51-40-02;[02] REPLACED SUPPORT BRACKET BODY STATION 540 RBL6 KEEL BEAM IAW B737-700 SRM 51-40-02
DETERIORATED LAVATORY A LENS EXIT LIGHT AT FWD GALLEY AREA (1 EA) 2022-268153 / [01] REPLACED LAVATORY A LENS EXIT LIGHT AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-802 P/N 207377-1009;[02] REPLACED LAVATORY A LENS EXIT LIGHT AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-802 P/N 207377-1009
EROSION ACCESS PANEL 193AR AT LOWER FUSELAGE 2022-268150 / [01] TOOL USED CALIPER P/N 500-197-30 S/N 021043156 DUE DATE 20/AUG/22;[02] TOOL USED: HOT BONDER P/N HCS9200B-AV S/N 18185781. DUE DATE 16-JAN-23.;[03] TOOL USED SCALE P/N: SCA-301 S/N: AE-412136 DUE DATE: 14-MAY-23.;[04] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 16-JAN-23;[05] TOOL USED: HOT BONDER P/N:HCS9200B-AV S/N:18196127 DUE DATE:16-JAN-23.;[06] REPAIRED ACCESS PANEL 193AR AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-6 REPAIR 6. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] REPAIRED ACCESS PANEL 193AR AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-6 REPAIR 6. SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK STRINGER 15L BETWEEN BS 294.5 AND BS 303.9 WL223 AT PASSENGER CABIN 2022-268066 / [01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 142811019; DUE DATE: 02-FEB-23.;[02] TOOL EDDY CURRENT USED P/N: NORTEC 600D; S/N: 210138003 AND DUE DATE: 22-FEB-23;[03] REPAIRED STRINGER 15L BETWEEN BS 294.5 AND BS 303.9 WL223 AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIG. 206. THIS REPAIR IS CATEGORY A. SEE INDIVIDUAL SIGNOFF BELOW;[04] REPAIRED STRINGER 15L BETWEEN BS 294.5 AND BS 303.9 WL223 AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIG. 206. THIS REPAIR IS CATEGORY A. SEE INDIVIDUAL SIGNOFF BELOW<BR>RII
CRACK FRAME STA 312 FWD UPPER CUT OUT DOOR LH SIDE WL 288 AT PASSENGER CABIN 2022-268067 / [01] REPAIRED FRAME STA 312 FWD UPPER CUT OUT DOOR LH SIDE WL 288 AT PASSENGER CABIN IAW EA M-22-153-01244.;[02] REPAIRED FRAME STA 312 FWD UPPER CUT OUT DOOR LH SIDE WL 288 AT PASSENGER CABIN IAW EA M-22-153-01244.
CRACK SUPPORT ANGLE LOCATED BETWEEN BS 291.5 AND BS 294.5 S-17R WL 208.1 AT PASSENGER CABIN 2022-268071 / [01] REPLACED SUPPORT ANGLE LOCATED BETWEEN BS 291.5 AND BS 294.5 S-17R WL 208.1 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 DWG:141A8310 SHEET:25 REV: SEE INDIVIDUAL SING OFF BELOW .;[02] REPLACED SUPPORT ANGLE LOCATED BETWEEN BS 291.5 AND BS 294.5 S-17R WL 208.1 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 DWG:141A8310 SHEET:25 REV: SEE INDIVIDUAL SING OFF BELOW .<BR>RII
CRACK WEB LOCATED BETWEEN BS 328 TO BS 344 AT LEVEL STRINGER 5R WL286 AT FWD GALLEY AREA 2022-268077 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[02] REPAIRED WEB WEB LOCATED BETWEEN BS 328 TO BS 344 AT LEVEL STRINGER 5R WL286 AT FWD GALLEY AREA IAW EA 22-153-01811-WIP1 BARCODE TTG8Q00CS0KD EA 22-153-01811 BARCODE TTG8Q00DDDDV; SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED RII MAJOR REPAIR PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK ANGLE - SUPPORT LOCATED BETWEEN BS 927 AND BS 947.5 BL 0 WL208.1 AT AFT GALLEY AREA 2022-268029 / [01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 927 AND BS 947.5 BL 0 WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 147A5400; SHEET 22; REV. -. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW
CORROSION FLOOR STRUCTURE BEAM BS 986.5 AT RBL42 WL208.1 AT AFT GALLEY AREA 2022-268030 / [01] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D S/N: 60009161631; DUE DATE: 03-DEC-22;[02] REPAIRED FLOOR BEAM 986.5 LOC. AT RBL 38 TO RBL 45 WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 SEE INDIVIDUAL SIGN OFF BELOW;[03] REPAIRED FLOOR BEAM 986.5 LOC. AT RBL 38 TO RBL 45 WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6.RII. SEE INDIVIDUAL SIGN OFF BELOW
CORROSION FLOOR STRUCTURE BEAM BS 986.5 AT LBL 42 WL208.1 AT AFT GALLEY AREA 2022-268031 / [01] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101V022240 DUE DATE 27-JAN-23;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[04] REPAIRED FLOOR STRUCTURE BEAM BS 986.5 BTW RBL 2 TO LBL 50 WL208.1 AT AFT GALLEY AREA IAW EA # 22-153-01846-WIP1 AND EA# 22-153-01846 REV. 1;[05] REPAIRED FLOOR STRUCTURE BEAM BS 986.5 BTW RBL 2 TO LBL 50 WL208.1 AT AFT GALLEY AREA IAW EA # 22-153-01846-WIP1 AND EA# 22-153-01846 REV. 1. SEE INDIVIDUAL SIGN OFF BELOW;[06] STEP 5 COMPLETED <BR>REPAIRED FLOOR STRUCTURE BEAM BS 986.5 BTW RBL 2 TO LBL 50 WL208.1 AT AFT GALLEY AREA IAW EA # 22-153-01846-WIP1 AND EA# 22-153-01846 REV. 1. SEE INDIVIDUAL SIGN OFF BELOW
CORROSION WEB LOCATED BETWEEN BS 294 AND BS 312 LBL12 WL208.1 AT FWD GALLEY AREA 2022-268018 / [01] REPLACED WEB LOCATED BETWEEN BS 294 AND BS 312 LBL12 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG # 141A5600 REV. N;[02] REPLACED WEB LOCATED BETWEEN BS 294 AND BS 312 LBL12 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG # 141A5600 REV. N<BR>RII
DELAMINATED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR 2022-268032 / [01] TOOL USED CALIPER P/N 500-197-30 S/N 021043156 DUE DATE 20/AUG/22;[02] TOOL USED: HOT BONDER P/N HCS9200B-AV S/N 18185781 DUE DATE 16-JAN-23;[03] TOOL USED SCALE P/N: SCA-301 S/N: AE-412136 DUE DATE: 14-MAY-23.;[04] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 16-JAN-23;[05] TOOL USED: HOT BONDER P/N:HCS9200B-AV S/N:18196127 DUE DATE:16-JAN-23.;[06] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196127 DUE DATE: 16-JAN-23.;[07] REPAIRED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-05-2R-6 REPAIR 6. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] REPAIRED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-05-2R-6 REPAIR 6. SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 277 AND BS 294.5 BL0 WL208.1 FWD GALLEY AND LAV 2022-268021 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 277 AND BS 294.5 BL0 WL208.1 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV - SEE INDIVIDUAL SIGNS -OFF BELOW;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 277 AND BS 294.5 BL0 WL208.1 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV - <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGNS -OFF BELOW
CRACK INNER CHORD LOCATED AT BS 301 AT LEVEL S-17L WL208.1 AT FWD GALLEY AREA 2022-268020 / [01] REPLACED INNER CHORD LOCATED AT BS 301 AT LEVEL S-17L WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG #141A8110 SHEET 9 REV A AND DWG# 140A9810 SHEET 48 REV -.<BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[02] CORRECTIVE STEP 1<BR>REPLACED INNER CHORD LOCATED AT BS 270 TO BS 360 AT LEVEL S-17L WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG #141A8110 SHEET 9 REV A AND DWG# 140A9810 SHEET 48 REV -.<BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNSOFF BELOW.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL 46 WL208.1 FWD GALLEY AND LAV 2022-268016 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL 46 WL208.1 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV- .SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL 46 WL208.1 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV- . ITEM RII. SEE INDIVIDUAL SIGNS-OFF BELOW.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 RBL 31 WL208.1 FWD GALLEY AND LAV 2022-268015 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 RBL 31 WL208.1 FWD GALLEY AND LAVATORY AREA IAW B737-700 SRM 51-40-02; SRM 41-10-02 AND DWG 141A5410 SHEET 12; REV:A; SEE INDIVIDUAL SIGN OFFS BELOW.;[03] CORRECTED STEP 2 REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 RBL 31 WL208.1 FWD GALLEY AND LAVATORY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 141A5410 SHEET 12; REV:A; SEE INDIVIDUAL SIGN OFFS BELOW.;[04] TASK COMPLETED ; RII <BR> SEE INDIVIDUAL SIGN OFFS BELOW.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 328 AND BS 344 LBL 46 WL208.1 FWD GALLEY AND LAV 2022-268014 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 328 AND BS 344 LBL 46 WL208.1 FWD GALLEY AND LAVATORY AREA IAW SRM 51-40-02; 51-0-02 DWG 141A5410 SHEET 16; REV:B. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRECTED STEP 1 REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 328 AND BS 344 LBL 46 WL208.1 FWD GALLEY AND LAVATORY AREA IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5410 SHEET 16; REV:B. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 AND BS 360 RBL 33 WL208.1 FWD GALLEY AND LAV 2022-268012 / [01] INSTALLED EWIS PROTECTION LOC BTW BS 344 AND BS 360 RBL 33 WL 208.1 FWD GALLEY IAW B737-700 AMM 20-60-07;[02] STEP 1 ENTER BY ERROR.;[03] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 AND BS 360 RBL 33 WL208.1 FWD GALLEY AND LAV. IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 141A5400 REV:-;[04] CORRECTED STEP 3 REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 AND BS 360 RBL 33 WL208.1 FWD GALLEY AND LAV. IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 141A5400 REV:- SEE INDIVIDUAL SIGNOFFS BELOW;[05] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 AND BS 360 BL 0 WL 208.1 FWD GALLEY AND LAV 2022-268013 / [01] REPLACED INSTALLED NEW WEB INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 344 AND BS 360 BL 0 WL 208.1 FWD GALLEY AND LAV. GRANTED IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 32 REV - SEE INDIVIDUAL SIGNS- OFF BELOW;[02] CORRECTED STEP 1: REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 AND BS 360 BL 0 WL 208.1 FWD GALLEY AND LAV. IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DWG 141A5400 SHEET 32 REV - SEE INDIVIDUAL SIGNS- OFF BELOW;[03] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 AND BS 360 BL 0 WL 208.1 FWD GALLEY AND LAV. IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DWG 141A5400 SHEET 32 REV - SEE INDIVIDUAL SIGNS- OFF <BR>BELOW<BR>RII
CRACK FLOORBEAM LOCATED BS 294.5 AT RBL 52 WL 208.1 FWD GALLEY AND LAV 2022-268011 / [01] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 03-DEC-22.;[02] TOOL USED P/N: FPK-PRO-104; S/N: PRO-3344 AND DUE DATE: 06-MAY-23;[03] REPAIRED FLOORBEAM LOCATED BS 294.5 AT RBL 25 TO RBL 60 WL 208.1 FWD GALLEY AND LAVATORY AREA I.A.W B737-700 SRM 53-10-51-2R-16 REPAIR 16 ALTERNATIVE 2 AND DWG:141A5502 SHEET:15 REV:- AND DWG:141A8310 SHEET:7 REV:-. SEE INDIVIDUAL SING OFF BELOW.;[04] JOB COMPLETED AND CERTIFIED AS RII.
CRACK AFT CORNER SCUFF PLATE POSITION LOCATED FWD CARGO COMPARTMENT 2022-267973 / [01] TOOL USED: DIGITAL CALIPER P/N:500-193-30;S/N: 0000291; DUE DATE: 16/SEP/22.;[02] REPAIRED AFT CORNER SCUFF PLATE POSITION LOCATED FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.;[03] TASK COMPLETED.
CRACK SCUFF PLATE AFT CORNER POSITION AT AFT CARGO COMPARTMENT 2022-267974 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A18229508; DUE DATE 29-SEP-22;[02] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW
CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 AND 16 INCH. FROM FRONT SPAR. CRACK LENGTH = 0.500 INCH. APPROX. 2022-267968 / [01] ET TOOL USED: PN: NORTEC 600D; SN:210138203; DUE DATE: 11-APR-23;[02] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X11290U021704 DUE DATE 01-FEB-23.;[03] REPAIRED LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN LOCATED AT STAB STA 193.90 AND 16 INCH. FROM FRONT SPAR. IAW B737 700 SRM 55-10-01-2R-11 REPAIR 11. SEE INDIVIDUAL SING-OFF BELOW;[04] REPAIRED LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN LOCATED AT STAB STA 193.90 AND 16 INCH. FROM FRONT SPAR. IAW B737 700 SRM 55-10-01-2R-11 REPAIR 11.RII. SEE INDIVIDUAL SING-OFF BELOW
INOP LOWERED CEILING PANEL EMERGENCY BATTERY PACK AT FWD GALLEY AREA (1 EA) 2022-267921 / [01] REPLACED BATTERY PACK AT FWD GALLEY AREA IAW: B737-700 AMM 33-51-06-960-805;[02] REPLACED BATTERY PACK AT FWD GALLEY AREA IAW: B737-700 AMM 33-51-06-960-805. COMPLETED
INOP LOWER SIDEWALL PANEL MID CABIN LH SIDE EMERGENCY BATTERY PACK AT PASSENGER CABIN (1 EA) 2022-267922 / [01] REPLACED BATTERY PACK AT PASSENGER MID CABIN LH SIDE IAW: B737-700 AMM 33-51-06-960-805;[02] REPLACED BATTERY PACK AT PASSENGER MID CABIN LH SIDE IAW: B737-700 AMM 33-51-06-960-805. COMPLETED
CRACK BULKHEAD PANEL 142NW B AFT CARGO COMPARTMENT 2022-267902 / [01] REPAIRED BULKHEAD PANEL 141LW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-300-805. PARA 4.F. TOOL USED :CALIPER P/N:500-197-30 ; S/N:A21041924; DUE DATE: 10SEP22. SEE INDIVIDUAL SIGNOFFS BELOW. REPAIRED BULKHEAD PANEL 142NW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-300-805.TOOL USED :CALIPER P/N:500-197-30 ; S/N:A21041924; DUE DATE: 10SEP22. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPAIRED BULKHEAD PANEL 141LW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-300-805. PARA 4.F. TOOL USED :CALIPER P/N:500-197-30 ; S/N:A21041924; DUE DATE: 10SEP22. SEE INDIVIDUAL SIGNOFFS BELOW. REPAIRED BULKHEAD PANEL 142NW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-300-805.TOOL USED :CALIPER P/N:500-197-30 ; S/N:A21041924; DUE DATE: 10SEP22. SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK EXTERNAL GROUND ELECTRICAL POWER LOC AT RECEPTACLE SURROUND CUTOUT AT LOWER FUSELAGE 2022-267900 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: 00X12101V022235; CAL DUE DATE: 03-JUN-22;[02] REPAIRED EXTERNAL GROUND ELECTRICAL POWER LOC AT RECEPTACLE SURROUND CUTOUT AT LOWER FUSELAGE I.A.W B737-700 SRM 53-10-15-1A-4.;[03] REPAIRED EXTERNAL GROUND ELECTRICAL POWER LOC AT RECEPTACLE SURROUND CUTOUT AT LOWER FUSELAGE I.A.W B737-700 SRM 53-10-15-1A-4.
CRACK BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT 2022-267903 / [01] BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801. MATERIAL USED: SH OFFWHITE 48X144X0.06 P/N:A60SG4W 4844; PO: 2022 127802;[02] CORRECTIVE STEP 1<BR>FABRICATED BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801. MATERIAL USED: SH OFFWHITE 48X144X0.06 P/N:A60SG4W 4844; PO: 2022 127802;[03] FABRICATED BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801. MATERIAL USED: SH OFFWHITE 48X144X0.06 P/N:A60SG4W 4844; PO: 2022 127802
CRACK BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT 2022-267904 / [01] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 MATERIAL USED: CONOLITE SHEET OFFWHITE WALL 0.060? PN:A60SG4W 60144 PO: 2021 214612;[02] TASK COMPLETED
LOSS OF HYD 'B' SYS. COMPLIED WITH QRH ; LOSS OF HYD SYSTEM . TRAILING EDGE FLAP FLOW LIMITERCREW REPORTS SMOOTH OVERWEIGHT LANDING OF 133;000 LS / [01] REMOVED AND REPLACED TRAILING EDGE FLAP LIMITER AS REQUIRED. OPS AND LEAK CHECK NORMAL. WORK IAW B737 AMM 27-51-67
EMERGENCY LIGHT IN CABIN CEILING AT OVERWING EXITS BROKEN AND FALLING DOWN. ; / [01] REMOVED AND REPLACED EMERGENCY LIGHT ASSAY AT CABIN CEILING OVERWING EXITS PER AMM33-51-01. OPS CHECKS GOOD.
F.O. ASSIST HANDLE BROKEN ; / [01] REMOVED AND REPLACED FO ASSIST HANDLE IAW M/M 56-11-11
EMERGENCY EXIT ROW FLUORESCENTLIGHT INOP EXIT SIGN WORKS NORMALLY ; RH SIDE / [01] OK TO CONT PER MEL 33-2-03 SP1B AUTH 34746
LIGHT IN EXIT ROW SIGN FO SIDE BURNT OUT. ; / [01] RELAMPED F/O EXIT ROW SIGN PER AMM 33-51-01. OPS CHK GOOD.
A .600' CRACK IN BS 663 BULKHEAD LOWER SKIN PANEL ATTACH ANGLE, RBL 40, WL 164. CUT AND REMOVED DAMAGED SECTION OF ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5. PERFORMED VISUAL INSPECTION OF REPAIR AREA. NO DEFECTS NOTED IAW SRM 57-10-10-2R-5, REPAIR 5. TREATED AND PRIMED REPAIR AND CUT EDGES IAW SRM 57-10-10-2R-5, REPAIR 5, STEP 10. INSTALLED ALL FUEL TANK FASTENERS. SEALED FASTENERS IN TANK IAW SRM 57-10-10-2R-5, REPAIR 5. INSTALLED REPAIR CHANNEL AND STIFFENER IAW SRM 57-10-10-2R-5, REPAIR 5, AND DWG 111A1000, SHT 153, REV -. DAMAGE REPAIRED IAW SRM 57-10-10-2R-5, REPAIR 5, & EA 21-157-03174.
LEFT WING T/E SHELF PANEL VERTICAL BULB SEAL RETAINER CRACKED INBD OF FLAP DEFLECTOR BEAM / R&R VERTICAL BULB SEAL RETAINER PER MM REF 20-50-11
FORWARD SERVICE DOOR SLIDE BECAME DISLODGED UPON OPENING. RESECURED SLIDE F/SERVICE, PER MT 725-61-06.
RIGHT OVERWING EXIT SIGN (1' X 5') COVER IS MISSING. INSTALLED NEW COVER FOR RH OVERWING EXIT SIGN PER S.I.P
FWD CLOSEOUT PANEL LOWER LEFT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED AND TESTED SERVICEABLE IAW AMM 33-51-01-960-802.
FWD SERVICE DOOR EMERGENCY SLIDE LIGHT WAS OUT. REMOVED AND REPLACED THE POWER SUPPLY M1674 IAW AMM 33-51-06-960-805. PERFORMED A GOOD TEST IAW AMM 33-51-06-960-805, STEP 4S.
LEFT BS 663 VAPOR BARRIER UPPER ATTACH ANGLE WAS CRACKED AT LBL 8 WL 167.68. REMOVED THE DAMAGED SECTION OF UPPER ATTACH ANGLE AND INSTALLED NEW SECTION REPAIR PARTSE IAW SRM 57-10-10-2R-5.
AFT CARGO BAY; FWD AND AFT WATER SERVICE PAN STIFFENERS ARE CRACKED BETWEEN BS 907 AND 927. REMOVED AND REPLACED ACB FWD & AFT WATER SERVICE PAN STIFFENERS IAW SRM 51-40-02, SRM 51-40-05, AND AIPC 52-49-00-02.
AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUTPLATE HOLES BS727 TO BS767 RBL23 WL156 / EVALUATED ACB R/H FLOOR TO SIDEWALL SUPPORT; BS727-767; REMOVED .015' FROM ORIG .040'; FOUND TO BE OUT OF LIMITS; IAW SRM 53-00-53-1A-2; REMOVED DAMAGED SECTION; LOCATED DRILLED; AND INSTALLED NEW R/H FLOOR TO SIDEWALL SUPPORT; BS 727-767; IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 146A7500.
FWD CARGO BAY SHIELD BETWEEN BS492 AND BS500A HAS CORROSION AROUND NUT PLATES RBL23 WL156 / EVALUATED CORROSION ON FCB SHIELD; BS492-500A; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM REMOVED DAMAGED SHIELD; LOCATED AND DRILLED; AND INSTALLED; NEW FCB SHIELD; BS 492-500A; IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 143A0080.
AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUTPLATE HOLES BS727D TO BS787 LBL23 WL156 / REMOVED AND REPLACED L/H FLOOR TO SIDEWALL SUPPORT PLATE BS 727-847 LBL23; WL156 IAW SRM 51-40-02; SRM 51-40-05; DWG #146A7500.
AFT CARGO BAY R/H SHIELD HAS CORROSION AROUND NUT PLATE HOLES BS767 TO BS794 RBL23 WL156 / EVALUATED CORROSION ON SHIELD (PART #146A8127-12); FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM; REPLACEMENT OF PARTS REQUIRED; REMOVED AND REPLACED ACB R/H SHIELD BS 767 TO BS 794; RBL23 WL156 IAW SRM 51-10-02-0G-0 PARA 9; SRM 51-40-02-0G-0 PARA 5(B); AND DWG 146A0081
AFT CARGO BAY ANGLE COMMON TO R/H SHIELD HAS CORROSION AROUND NUT PLATE HOLES BS767 TO BS787 RBL23 WL155 / EVALUATED CORROSION AFT CARGO BAY ANGLE (PART #146A8125-53); FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM; REPLACEMENT OF PART REQUIRED IAW SRM 51-10-02-0G-0 PARA 9. REMOVED AND REPLACED AFT CARGO BAY ANGLE COMMON TO R/H SHIELD BS 767-787; RBL23; WL155 IAW SRM 51-40-02-0G-0 PARA 4(B); 7(D) AND DWG 146A8123
FWD CARGO BAY STR19R GUSSET IS CRACKED AT BS500D / REMOVED AND REPLACED FWD CARGO GUSSET. B.S. 500D STR19R PER SRM 51-40-05-0G-0 SRM 51-40-02-0G-0 AND DWG 143A7902
L/H VERTICAL STIFFENER ON THE AFT SIDE OF BS663 LOWER VAPOR BARRIER LBL25 IS CRACKED AT WL145 / REMOVED AND REPLACED L/H VERTICAL STIFFENER ON THE AFT SIDE OF BS663 LOWER VAPOR BARRIER LBL25; WL145 IAW DWG 111A1000 AND DWG 149A7210.
RIGHT PASSENGER CABIN SIDEWALL PANEL 232YHW EXIT LIGHT ASSEMBLY WAS DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-01-960-802; STEP 3, D5, D6, 10. OPS CHECKED IAW MM 33-51-00-720-801, AND MM 33-51-00-710-801, TESTED GOOD.
AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / WELDED SCUFF PLATE PER SRM 53-60-15-2R-1 AND BAC5975 AFT BAY FWD CORNER
AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / WELDED SCUFF PLATE PER SRM 53-60-15-2R-1 AND BAC5975 AFT BAY AFT CORNER
DAMAGED ISOLATOR ON R/H OVERWING EXIT CUTOUT LOWER SILL WEB STA 620 ON VERTICAL FLANGE 15; WL 220 (FWD) (MARKED). / REMOVED AND REPLACED DAMAGED ISOLATOR AT RH OWE CUTOUT LOWER SILL WEB STA 620 ON VERT. FLANGE AT WL 220 (FWD) AS MARKED IAW SRM 51-40-02
RT FWD VERT FIN CLOSURE SKATE ANGLE IS CRACKED. REMOVED & REPLACED RT FWD VERT FIN CLOSURE (SKATE) ANGLE IAW SRM 5140020G0; 5140050G0; 5140080G0; DWGS 147A0030 & 147A0070. RESTORED DECORATIVE FINISH ON NEW SKATE ANGLE IAW AMM 512199300801 56304U 10JUN20 AND SOPM 204401 56304U 10JUN20
LT FWD VERT FIN CLOSURE SKATE ANGLE IS CHAFED / REMOVED & REPLACED LT FWD; VERT FIN CLOSURE (SKATE) ANGLE IAW SRM 51-40-02-0G-0; 51-40-05-0G-0; 51-40-08-0G-0 DWG #'S 147A0030 & 147A0070. RESTORED DECORATIVE FINISH ON NEW SKATE ANGLE IAW AMM 51-21-99-300-801 56304U 10JUN20 AND SOPM 20-44-01 56304U 10JUN20
CORROSION FOUND ON THE EXTERNAL SKIN AROUND FASTENER HEADS, BS 990-1001, STRINGER 2L. REPAIRED THE SKIN IAW EA 20-153-00844, REV IR, AND ER 20-02425, REV IR.
BS 663 LOWER COMPOSITE BULKHEAD WAS CRACKED AT LBL 39, WL 150. REMOVED AND REPLACED THE BULKHEAD LEFT SIDE IAW SRM 51-40-02-0G-0, DWG 111A1000, MM 53-51-21-400-802, AND MM 51-31-00-390-805.
RIGHT FLAP TRACK SUPPORT STIFFENER WAS CHAFED. REMOVED AND REPLACED THE RT FLAP TRACK SUPPORT STIFFENER IAW SRM 51-40-02, SRM 51-40-05, AND DWG 149A7506.
LEFT FLAP TRACK SUPPORT STIFFENER AT BS 727A, STRINGER 20L WAS CHAFED. REMOVED AND REPLACED THE SUPPORT STIFFENER IAW SRM 51-40-05, SRM 51-40-02, AND DWG 149A7506.
CORROSION FOUND ON THE EXTERNAL SKIN AROUND FASTENER HEADS, BS 990 - 998, STRINGER 2R. REPAIRED SKIN IAW EA 20-153-00844, REV IR, AND ER 20-02725, REV IR.
FLIGHT DECK FLOOR WAS DENTED AT BS 255, RBL 4 - LBL 14, WL 207.54. REPAIRED IAW SRM 51-00-10, AND SRM 51-40-02, IAW EA 1-753-33107, REV IR.
NOSE RADOME BOOT IS DAMAGED / REMOVED AND REPLACED DAMAGED RADOME BOOT IAW AMM 53-52-00-400-802
RIGHT WING TO BODY PANEL 191AR AFT VERTICAL SUPPORT FRAME CRACKED. / REMOVED AND REPLACED AFT VERTICAL SUPPORT PER SRM 51-10-02 AND SRM 51-40-02
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669 IN CABIN. / R&R BATTERY PACK PER AMM.
L1 DOOR SLIDE OUT OF CONTAINER ADJUST. / REINSTALLED SLIDE PER MT.
PANEL 193B HAS 1' AREA OF DELAMINATION ASSOCIATED WITH DENT; CRACK ON INTERIOR SURFACE. MARKED ON PANEL. / REMOVED AND REPLACED 193B PANEL PER AMM 53-51-21.
PANEL 193B FASTENER HOLES 38EA. ARE ELONGATED AND WORN AT COUNTER SINK. / REMOVED AND REPLACED 193B PANEL PER AMM 53-51-21.
DECLARED EMERGENCY, STRONG ELECTRICAL SMELL/FUMES IN MID CABIN SECTION. SMELL WENT THROUGHOUT ENTIRE CABIN. FOUND RECIRCULATION FAN FAILED. R&R RECIRCULATION FAN PER AMM.
OVERHEAD CEILING EMERGENCY EXIT SIGN LOOSE. SECURED LIGHT PER SIP.
LT AFT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. R&R BATTERY PER AMM.
LT OVERWING EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY CHECK. R&R BATTERY PER AMM.
LT FORWARD EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. R&R BATTERY PER AMM.
LT HORIZONTAL STABILIZER LEADING EDGE CRACKED AT RIB STA 105. R&R RIB PER SRM.
INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520, BL 0. R&R INTERCOSTAL PER SRM.
RT HORIZONTAL STABILIZER LEADING EDGE CRACKED AT RIB STA 105.26. R&R RIB PER SRM.
LT MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER CRACKED AT LBL 39. REPAIRED BARRIER PER SRM.
PANEL BREAK ASSEMBLY @ STA 540 BETWEEN BL 0 AND RBL33 TOP COVER CRACKED. / R&R PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND SRM 51-40-05.
PANEL BREAK ASSEMBLY @ STA 540 LBL33 TOP COVER CRACKED. / R&R PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND SRM 51-40-05.
PANEL BREAK ASSEMBLY @ STA 540 RBL33 TOP COVER CRACKED. / R&R PANEL BREAK ASSEMBLY IAW SRM 51-40-02 AND SRM 51-40-05.
R/H STAB @ RIB STA 120.3; 3RD VERTICAL STIFFENER FROM THE FRONT SPAR IS CRACKED. / REPAIR ACCOMPLISHED TO RIB IAW SRM 55-10-09-2R-4.
R/H TRANSITION ANGLE HAS CORROSION AROUND NUTPLATE HOLES MARKED FROM STA.792 TO STA.727D. / INSTALLED TRANSITION ANGLE REPLACEMENT FRO STA 727C TO STA 792 ;AND REPAIR SPLICE AT STA 727C PER SRM 53-00-53-2A;AND SRM 51-40-02.
AFT CARGO COMPARTMENT L/H TRANSITION ANGLE HAS CORROSION AROUND NUTPLATE HOLES MARKED AT STA. 792 TO STA.727D / REMOVED AND REPLACED L/H TRANSITION ANGLE STA. 727 TO STA. 792 IAW SRM 51-40-02.
CABIN NR 3 SEAT TRACK CORRODED BETWEEN BS 706 TO BS 727, RBL 25. R&R SEAT TRACK CROWN PER SRM.
LT MAIN LANDING GEAR WHEEL WELL ON REAR SPAR SUPPORT ANGLE CRACKED ABOVE AND INBOARD OF NR 1 TANK AFT BOOST PUMP. R&R ANGLE IAW SRM.
CABIN #1 SEAT TRACK LBL45 WORN FROM STATION 639 TO STATION 673 AND SURFACE CORROSION / WP:E104704-BLANKS; KENNETH - 08/18/2018 19:37 COMPLETE: DUE TO OUT OF LIMITS WEAR IN MULTIPLE AREAS; ALL WORK IS TO BE PERFORMED ON NON-ROUTINE CARD G581061.(REPLACEMENT OF NUMBER 1; LBL 45; SEAT TRACK CROWN FROM STATION 540-727B).
CABIN #1 SEAT TRACK LBL45 WORN FROM STATION 685 TO STATION 706 AND SURFACE CORROSION / WP:E104704-BLANKS; KENNETH - 08/18/2018 19:38 COMPLETE: DUE TO OUT OF LIMITS WEAR IN MULTIPLE AREAS; ALL WORK IS TO BE PERFORMED ON NON-ROUTINE CARD G581061.(REPLACEMENT OF NUMBER 1; LBL 45; SEAT TRACK CROWN FROM STATION 540-727B).
L/H AILERON HAS SEVERAL BALANCE WEIGHTS THAT HAVE SURFACE CORROSION. / WP:E58064-CRONIN; KEVIN - 08/18/2018 10:46 COMPLETE: AILERON IS REPLACED ON NON-ROUTINE G580951 WITH NEW WEIGHTS INSTALLED . NO FURTHER ACTION REQUIRED. CORRECTLY ANSWERED CORROSION QUESTIONS.
L/H WING T/E WIGGLE PLATE IS CRACKED O/B OF #3 CANOE FAIRING UNDER ACCESS PNL 551GB. / REMOVED AND REPLACED WAFFLE PLATE PER SRM 51-40-02.
R2 DOOR OVERHEAD EMERGENCY EXIT SIGN LIGHT INOP. R&R BATTERY PER AMM.
R2 DOOR SLIDE ASPIRATOR ORINTATION OUT OF POSITION. R & R THE SLIDE ASSY IAW MM.
R2 DOOR EMERGENCY LIGHT LENS BROKEN. R & R THE LIGHT ASSEMBLY IAW AMM.
AFT GALLEY AFT ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. R & R THE LIGHT ASSEMBLY IAW AMM.
RIGHT OVERWING EXIT SIGN LENS MISSING. INSTALLED THE LENS IAW AMM
LEFT HORIZONTAL STABILIZER UPPER SLIDER CRACKED. / R AND R SLIDER PER AMM 53-31-31
SUPPLEMENTAL INFORMATION: LW PANEL 521ZB CRACKED @ OB FWD HOLE / REMOVED AND REPLACED PANEL 521ZB REF AMM 57-41-02
FUEL CROSSFEED CIRCUIT BREAKER POPPED INFLIGHT. R&R CROSSFEED VALVE ACTUATOR IAW AMM.
L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE, PRESSURE LOW. R & R SLIDE IAW MAINTENANCE.
L1 DOOR ESCAPE SLIDE GIRT BAR FLOOR ATTACH FITTINGS LOOSE. SECURED THE FITTINGS IAW AMM.
AFT ENTRY CENTER EMERGENCY EXIT SIGN BROKEN. R&R THE SIGN IAW AMM.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 120.3, LOWER END OF 4TH STIFFENER AFT. REPAIRED RIB IAW SRM.
RIGHT HORIZONTAL STAB RIB CRACKED AT HSS 92.7, BOTTOM OF 2 STIFFENER FROM TRAILING EDGE. REPAIRED THE RIB IAW SRM.
RT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.70, LOWER END OF THE 3RD AND 4TH VERTICAL STIFFENERS FROM THE TRAILING EDGE. REPAIRED RIB IAW SRM.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.70, LOWER END OF THE 3RD AND 4TH VERTICAL STIFFENERS FROM THE LEADING EDGE. REPAIRED RIB IAW SRM.
L1 DOOR GIRT BAR AFT RETAINER LOOSE. R & R THE RETAINER ASSEMBLY IAW SRM.
FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 727B STRINGER 8R. REPAIRED FRAME IAW EA.
RIGHT CREASE BEAM WEB CORRODED BETWEEN BS 619 - 639, STRINGER 17R. R & R WEB IAW SRM.
RIGHT UPPER FRAME FORWARD SIDE BULKHEAD CRACKED AT BS 663, RBL 8. REPAIRED THE FRAME IAW EA & ER.
FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED THE FRAME IAW EA
FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED THE FRAME PER EA.
FRAME CRACKED AT BS 480, STR. 8L. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED THE FRAME IAW EA.
FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 520, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.
R2 DOOR MOP SILL UPPER SURFACE INNER ANGLE CORRODED BETWEEN BS 950 - 990, RBL 48. R&R THE ANGLE IAW SRM.
FLOORBEAM CORRODED AT BS 986, LBL 45. REPAIRED THE FLOORBEAM IAW EA.
FRAME CRACKED AT BS 294.5, RBL 54. REPAIRED THE FRAME IAW EA AND ER.
R1 DOOR THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 300 TO 317, RBL 58. R&R ANGLE IAW SRM.
RIGHT FORWARD CARGO BAY SHIELD CORRODED BETWEEN BS 492 - 500A. R & R THE SHIELD IAW SRM.
FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STRINGER 19L. R & R THE GUSSET IAW SRM.
FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM.
AFT CARGO BAY SUB THRESHOLD WEB CORRODED. R & R THE WEB IAW SRM.
AFT CARGO BAY INTERCOSTAL ANGLE UNDER SHIELD CORRODED BETWEEN BS 767 - 787. R & R THE ANGLE IAW SRM.
AFT CARGO BAY RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 - 767. R & R THE SUPPORT IAW SRM AND DWG.
AFT CARGO BAY LEFT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727C+10 - 817. R & R THE SUPPORT IAW SRM.
RIGHT AFT CARGO BAY SHIELD CORRODED BETWEEN BS 847 - 867. R & R THE SHIELD IAW SRM.
RIGHT AFT CARGO BAY SHIELD CORRODED BETWEEN BS 767 - 792. R & R THE SHIELD IAW SRM.
FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED. R & R THE WEB IAW SRM.
FORWARD CARGO BAY BULKHEAD ANGLE CORRODED AT BS 500D, BETWEEN LBL 25 - RBL 25. R & R THE ANGLE IAW SRM.
RIGHT WING NR 7 SLAT LOWER SURFACE CRACKED AT ACTUATOR ATTACH POINT. REPAIRED 7 SLAT IAW SRM.
LEFT WING NR 3 SLAT LOWER SURFACE CRACKED AT ACTUATOR ATTACH POINT. REPAIRED NR 3 SLAT IAW SRM.
RIGHT WING NR 8 SLAT LOWER SURFACE CRACKED AT ACTUATOR ATTACH POINT. REPAIRED NR 8 SLAT IAW SRM.
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR PER AMM.
R2 DOOR EMERGENCY EVAC SLIDE GIRT BRACKET CLIP OUT OF ADJUST. ADJUSTED CLIP IAW SIP.
FORWARD OVERHEAD EMER ESCAPE SIGN LIGHT INOPERATIVE, BETWEEN BS 429 - 500. R & R BATTERY PACK IAW AMM.
LEFT BULKHEAD CHORD SKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED SKIN IAW EA.
BULKHEAD CHORD SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.
SKIN CRACKED AT BS 540, BETWEEN STRINGER 22L - 23L. REPAIRED SKIN IAW EA.
R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
RIGHT EMER EXIT SIDEWALL LIGHT INOPERATIVE. CONNECTED LIGHT IAW AMM.
EMERGENCY LIGHT CONNECTOR ASSEMBLY ABOVE FWD LAVATORY INOPERATIVE. CLEANED LIGHT ASSEMBLY IAW AMM.
RIGHT EMER EXIT DOOR LIGHT INOPERATIVE. R & R LIGHT IAW MM.
OVERHEAD EXIT LIGHT ABOVE FWD LAVATORY LOOSE. SECURED LIGHT IAW MM.
RIGHT MLG EDGE OF WEB ASSEMBLY DAMAGED. R & R WEB IAW DWG.
L2 DOOR AFT FLOOR GIRT BAR BRACKET, AFT ATTACH BOLT, FLOORBOARD INSERT BUSHING MISSING. INSTALLED INSERT IAW SRM.
BEAM CRACKED AT BS 727B LBL 24 OTBD SIDE OF VERTICAL FASTENER 2ND FROM BOTTOM. REPAIRED BEAM IAW SRM.
CENTER WING BOX UPPER SKIN PANEL CRACKED AT BS 540 RBL 32.40 5TH HOLE FOR SHEAR FITTING. REPAIRED SKIN IAW SRM & EA.
CENTER WING BOX UPPER SKIN PANEL SHEAR FITTING CRACKED AT BS 540 LBL 6.14. REPAIRED FITTING IAW SRM & EA.
FORWARD SEAT TRACK CRACKED AT BS 727B RBL 45 OTBD SIDE ON FWD & AFT FASTENER. REPAIRED SEAT TRACK IAW SRM.
FORWARD SEAT TRACK CRACKED AT BS 727B RBL 45 INBD SIDE ON AFT FASTENER. REPAIRED SEAT TRACK IAW SRM.
FLIGHT DECK RT NR 1 WINDOW FRAME CRACKED. REPAIRED FRAME IAW EA.
SEAT TRACK CRACKED AT BS 727B RBL 24 INBD SIDE OF FWD FASTENER. REPAIRED SEAT TRACK IAW EA.
SEAT TRACK CRACKED AT BS 727B RBL 24 OTBD SIDE OF FWD FASTENER. REPAIRED SEAT TRACK IAW EA.
SEAT TRACK CRACKED AT BS 727B LBL 24 INBD SIDE OF AFT FASTENER. REPAIRED SEAT TRACK IAW EA.
SEAT TRACK CRACKED AT BS 727B LBL 24 OTBD SIDE ON FWD & AFT FASTENER. REPAIRED SEAT TRACK IAW EA.
SEAT TRACK CRACKED AT BS 727B LBL 45 INBD SIDE ON FWD FASTENER. REPAIRED SEAT TRACK IAW EA.
CENTER WING BOX UPPER SKIN PANEL CRACKED AT BS 540 LBL 32.40, 3RD HOLE FOR SHEAR FITTING. REPAIRED SKIN IAW SRM & EA.
CENTER WING BOX UPPER SKIN PANEL CRACKED AT BS 540 LBL 40.87, 3RD HOLE FOR SHEAR FITTING. REPAIRED SKIN IAW SRM & EA.
SEAT TRACK WORN AT BS 727A+15 LBL 45.57. REPAIRED SEAT TRACK IAW SRM.
MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663 BETWEEN LBL 25 TO 45. REPAIRED WEB IAW SRM.
RIGHT WING TE WIGGLE PLATE CRACKED ABOVE NR 6 FLAP TRACK. R & R WIGGLE PLATE IAW SRM.
LEFT WING TE WIGGLE PLATE CRACKED FWD INBD END OF PANEL 551GB. R & R WIGGLE PLATE IAW SRM.
LEFT WING TE WIGGLE PLATE CRACKED FWD INBD END OF PANEL 551EB. R & R WIGGLE PLATE IAW SRM.
MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663 BETWEEN RBL 25 TO 45. REPAIRED WEB IAW SRM.
FRAME CRACKED AT BS 727D BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.
RIGHT WING IRSS 220 WAFFLE PLATE CRACKED AT OTBD FASTENER HOLE. R & R WAFFLE PLATE IAW SRM.
LEFT NR 3 WINDOW E - F POST, 2ND LOWER FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW EA.
RIGHT WING TE WAFFLE PLATE CRACKED AT WING STATION 279, OTBD OF NACELLE STRUT AFT END. R & R WAFFLE PLATE IAW SRM.
UPPER SHELF PANEL OTBD OF NR 6 SPOILER SEAL RETAINER ANGLE CRACKED ON BACKSIDE. R & R ANGLE IAW SRM.
FRAME CRACKED AT BS 787 BETWEEN STRINGER 8L TO 9L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 787 BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.
RIGHT WING UPPER FIXED TE PANEL WING STATION 271 CTR RIB BRACKET CRACKED ON FWD SIDE. R & R BRACKET IAW SRM.
INTERCOSTAL CRACKED AT BS 540 INBD MOUNT. R & R INTERCOSTAL IAW SRM.
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN INBD CRACKED AT STATION 147.90 BETWEEN 7.5 TO 8.0 FROM REAR SPAR. REPAIRED SKIN IAW SRM.
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STATION 142.7. REPAIRED SKIN IAW EA.
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 98. REPAIRED SKIN IAW EA.
CAPTAIN`S WINDOW POST CD CRACKED. REPAIRED POST IAW EA.
MID CABIN EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. R & R BATTERIES IAW AMM.
CEILING AFT EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. R & R BATTERIES IAW AMM.
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED .750 INCHES LONG AT STABILIZER STATION 101.9 9INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW SRM & EA.
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED ALONG AFT SPAR 1.5 INCHES LONG AT STAB STATION 98. REPAIRED SKIN IAW SRM & EA.
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AFT SPAR 2 INCHES LONG AT STAB STATION 142.7. REPAIRED SKIN IAW SRM & EA.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. R & R SLIDE IAW MT.
AFT LT EMERGENCY LIGHTING BATTERY PACK FAILED LONG TEST. R & R BATTERY PACK IAW MM.
AFT RT EMERGENCY LIGHTING BATTERY PACK FAILED LONG TEST. R & R BATTERY PACK IAW MM.
LT OVER WING EMERGENCY LIGHTING BATTERY PACK FAILED LONG TEST. R &R BATTERY PACK IAW MM.
LEFT WING MLG FWD TRUNNION BEARING INBD LOWER ATTACH LUG FACE CORRODED. REPAIRED LUG PER EA.
EMERGENCY LIGHT ABOVE L1 DOOR AND LOWER INTERIOR EMERGENCY LIGHT ADJACENT TO R1 DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ON RT SIDE OF FWD ENTRY LIGHT IAW AMM. OPS CHECK GOOD.
PASSENGER OVERHEAD EMERGENCY EXIT AISLE LIGHT ASSY NOT SECURE. SECURED LIGHT ASSY AS PER AMM.
R2 DOOR EMERGENCY EVAC SLIDE LENS LOOSE. REMOVED AND REPLACED LENS PER MT & MM.
L1 DOOR EMERGENCY EVAC SLIDE LENS LOOSE. REMOVED AND REPLACED LENS PER MT AND MM.
AIR TURNBACK/DECLARED EMERGENCY. ENGINE THRUST BECAME UNCONTROLLABLE DURING FLIGHT SHORTLY AFTER LEVEL OFF. THRUST DETERIORATED ON NR 2 THEN WENT NEAR MAX POWER, REDUCED TO IDLE. NR 1 ENGINE DID THE SAME SHORTLY THERE AFTER. REMOVED AND REPLACED NR 1 HMU PER MT.
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 120.30. REPAIRED SKIN PER SRM.
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.
EMERGENCY EXIT FLOOR TRACK COVER CRACKED. REMOVED AND REPLACED TRACK COVER PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS INOP AT ROW 2. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS INOP AT ROW 2. REMOVED AND REPLACED CHARGER PER MM.
DURING SCHEDULED HC1 CHECK, FOUND FWD EEPLS INOP BETWEEN ROW 1 TO ROW 2. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST AT M1668, M1669, AND M1675. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS INOP AT ROW 12. RELAMPED PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS LENS CRACKED AT ROW 1. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.
EEPLS LENS MISSING AT OVERWING EXITS. INSTALLED LENS PER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 8. REPAIRED BEAM PER EA.
DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 17. REPAIRED BEAM PER EA.
DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 12. REPAIRED BEAM PER EA.
DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, RBL 8. REPAIRED BEAM PER EA.
DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED BEAM PER EA.
DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED BEAM PER EA.
DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX NR 5 HORIZONTAL STIFFENER CRACKED AT BS 548, LBL 7. REMOVED AND REPLACED STIFFENER PER SRM.
DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX CENTER WING BOX NR 7 HORIZONTAL STIFFENER CRACKED AT BS 548, RBL 14. REMOVED AND REPLACED STIFFENER PER SRM.
DURING SCHEDULED 6Y CHECK, FOUND NR 4 HORIZONTAL STIFFENER CRACKED AT BS 548, LBL 14. REMOVED AND REPLACED STIFFENER PER SRM.
DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE COVER LENS LOOSE. REMOVED AND REPLACED LENS PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS DAMAGED AT ROW 18 ABC. REMOVED AND REPLACED EEPLS LENS PER MM.
L1 DOOR EMERGENCY EXIT DOOR SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.
DECLARED EMERGENCY, ON APPROACH TO AIRPORT THE LT FLAP INDICATOR INDICATED POSITION ZERO AND RT FLAP INDICATED POSITION 1, SPLIT FLAP INDICATION ON PANEL. REMOVED AND REPLACED LT FLAP POSITION TRANSMITTER & NR 4 SKEW SENSOR PER MM.
DURING SCHEDULED CV CHECK, FOUND EEPLS LENS BROKEN AT ROW 5. REMOVED AND REPLACED LENS PER MM.
EEPLS INOP AND COVER LOOSE. REMOVED AND REPLACED LENS COVER & POWER SUPPLY PER MM.
DURING SCHEDULED HC1 CHECK, FWD LT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, FWD RT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, AFT RT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM.
R2 DOOR EMERGENCY EXIT LIGHT LENS BASE BROKEN. REMOVED AND REPLACED LIGHT PER MM.
R2 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP CRACKED BETWEEN ROWS 7 ABC & 14 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM.
DURING SCHEDULED RON CHECK, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT COVER BROKEN AT ROW 3 ABC. REMOVED AND REPLACED LIGHT COVER PER MM.
DURING SCHEDULED RON CHECK, FOUND EEPLS TRACK LIGHT INOP AT ROW 6. RELAMPED LIGHT PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT AFT CABIN. REINSTALLED EEPLS WIRING PER MM.