N930WN
Registered owner: WILMINGTON TRUST COMPANY TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2017-10-02 – 2017-10-02 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2017-10-02 – 2017-10-02 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
DELAMINATED FLOOR PANEL 241AEF AT AFT GALLEY AREA. REPAIRED FLOOR PANEL 241AEF AT AFT GALLEY AREA IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.
L1 DOOR SLIDE SECONDARY RELEASE FLAP FOLDED UP IN CONTAINER AND NOT SECURED DOWN. UNFOLDED AND SECURED FLAP WHERE IT BELONGS AS DESCRIBED IN MT 725-61-06. CONTAINER NOT OPENED OR REMOVED.
PASSENGER CABIN, RIGHT OVERWING UPPER AND LOWER FWD EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY POWER SUPPLY M1669 IAW AMM 33-51-06-960-806.
EXIT SIGN COVER AT RIGHT OVER WING EXIT FELL OFF. REINSTALLED EMERGENCY EXIT SIGN AT RIGHT OVER WING EXIT IAW AMM 33-51-01.
FWD CARGO COMPARTMENT AFT FIBERGLASS FLOOR PANEL HAS 3 SEPARATE CRACKS MEASURING 6.5'; 3.5 '; AND 5' LONG. REMOVED AND REPLACED FWD CARGO COMPARTMENT AFT FIBERGLASS FLOOR PANEL REF AMM 25-52-10 WITH FABRICATED PANEL REF AMM 25-52-01.
FIRST OFFICER`S SIDE OVERWING EXIT LOWER SIGN BROKEN OFF. REMOVED AND REPLACED EXIT ROW LOWER EXIT SIGN RT COVER IAW AMM 33-51-01.
F/A REPORTED FWD ENTRY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED THE FWD ENTRY DOOR EXIT ASSY SIGN IAW AMM 33-51-01-960.
SIDEWALL LIGHT AT SEAT ROW 11 ABC IS INOPERATIVE. OK TO CONTINUE PER MEL 33-2-03 SP1B. REPLACED THE LAMP IN SIDEWALL LIGHT AT 11ABC IAW AMM 33-51-04.
L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
EMERGENCY LIGHTING BATTERY PACK AT THE R/H OVERWING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
LOWER EXIT EMERGENCY SIGN @ ROW 12FED HAS 3 BULB INOP.<[01] REMOVED AND REPLACED PER [AMM 33-51-01-960-801-NG (EXIT SIGN - LAMP REPLACEMENT - PERMANENT)]
UPPER EXIT EMERGENCY SIGN @ ROW 12FED HAS 3 BULBS INOP.<[01] REMOVED AND REPLACED PER [AMM 33-51-01-960-801-NG (EXIT SIGN - LAMP REPLACEMENT - PERMANENT)]
LOWER EXIT EMERGENCY SIGN @ ROW 11CB HAS 1 BULB INOP.<[01] REMOVED AND REPLACED PER [AMM 33-51-01-960-801-NG (EXIT SIGN - LAMP REPLACEMENT - PERMANENT)]
AIRCRAFT LH AFT ESCAPE SLIDE SLIPPED OUT OF RECEPTACLE<[01] C/W MT 725-66-06 TO REPLACE SLIDE ON AFT ENTRY DOOR.
FOUND FORWARD SERVICE DOOR THRESHOLD PLATE CRACKED<[01] R&R'D FORWARD SERVICE DOOR SCUFF PLATE IAW AMM 53-11-01;[02] VERIFIED: R&R'D FORWARD SERVICE DOOR SCUFF PLATE IAW AMM 53-11-01
FWD FLIGHT ATT. FLASHLIGHTS MISSING<[01] REPLACED FWD FLIGHT ATT. FLASHLIGHTS PER AMM 26-64-00. OPS CHECK GOOD. A/C OK FOR SERVICE.
FAS REPORT EXIT SIGN MISSING IN AFT GALLEY FO SIDE<[01] REMOVED AND REPLACED EXIT SIGN ASSEMBLY PER AMM 33-51-01<BR>OP CHK OK
G2 UPPER INBD CUBBY SLIDE STRIP NOT SECURED TO FLOOR OF COMPARTMENT.<[01] SECURED G2 INBD CUBBY SLIDE STRIP TO FLOOR OF COMPARTMENT AS PER B737 SOPM 20-50-12.;[02] VERIFIED STEP 1
L2 DOOR SLIDE HITS DOOR THRESHOLD WHEN DOOR OPERATED. REPOSITION L2 DOOR ESCAPE SLIDE SKIRT AS PER WORK INSTRUCTIONS 725-61-06;[02] VERIFIED STEP 1
R2 DOOR SLIDE HITS DOOR THRESHOLD WHEN DOOR OPERATED.<[01] READJUSTED GIRT Z FOLD AS PER MT 725-61-06 STEP 3.K.(3).;[02] VERIFIED STEP 1
PAX EMERGENCY LIGHTS L1; R2 AND L/H R/D MID CABIN INOP<[01] REPLACED BATTERY PACK AT POSITION M1672 AND M1674 AS PER REF AMM 33-51-06-960-805.<BR>PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST TASK 33-51-00-710-801. TEST PASS.;[02] REPLACED BATTERY PACK AT POSITION M1672 AND M1674 AS PER REF AMM 33-51-06-960-805.<BR>PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST AS PER REF AMM 33-51-00-710-801. TEST PASS.;[03] VERIFIED STEP 2.
MAIN CABIN AFT LOWERED CELLING PANEL EXIT SING HOUSING BROKEN<[01] REMOVED AND REPLACED MAIN CABIN AFT LOWERED CELLING PANEL EXIT SING HOUSING;<BR>AS PER B737 AMM 33-51-02-020-801 AS FOR REMOVAL REFERENCE AND<BR>33-51-02-400-801 AS FOR INSTALLATION REFERENCE.;[02] VERIFIED STEP 1
CAP STRIP WITH ELONGATED HOLE AT STA 847 L/H<[01] RECEIVED NEW CAP STRIP. FOR INSTALLATION REF. TTG8Q00V3GGE;[02] VERIFIED STEP 1
PANEL 142KW CRACKED<[01] RECEIVED PANEL 142KW PART;WILL BE INSTALLED ON ITEM TTG8Q00TU02H;[02] VERIFIED STEP 1.
L2 DOOR PNL. 834DZ HAS A CRACKED BRACKET<[01] REMOVE AND REPLACED L2 DOOR PANEL 834DZ REF: SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.
AFT CARGO COMP;STA 827-STA 847 LBL 21 WL155.6 INTERCOASTALHAS ELONGATED HOLE<[01] REMOVED AND REPLACED INTERCOASTAL AT AFT CARGO COMP;STA 827-STA 847 LBL 21 WL155.6 REF:SRM 51-40-02-0G-0AND SRM 51-40-05-0G-0;[02] CORRECTION STEP 1 OF STEP 4 REMOVED AND REPLACED INTERCOASTAL AT AFT CARGO COMP;STA 827-STA 847 LBL 21 WL155.6 REF:SRM 51-40-02-0G-0AND SRM 51-40-05-0G-0 AND DRW 146A7502;[03] CORRECTION : STEP 2 ENTER IN ERROR<BR>CORRECT STATEMENT IS: <BR>REMOVED AND REPLACED INTERCOASTAL AT AFT CARGO COMP;STA 827-STA 847 LBL 21 WL155.6 REF:SRM 51-40-02-0G-0AND SRM 51-40-05-0G-0 AND DRW 146A7502;[04] VERIFIED STEP 3.
DORSAL FIM MOST FWD RIB IS CRACKED<[01] REMOVED DAMAGED FWD RIB FROM DORSAL FIN REF. SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED NEW FWD RIB AT DORSAL FIN REF.SRM 51-40-05-0G-0.<BR>INSTALLED NEW FWD RIB ON DORSAL FIN REF. SRM 51-40-02-0G-0 AND BOEING DRAWING:174A1008.;[02] VERIFIED STEP 1.
FOUND 3 EACH ELONGATED HOLES AT FLIGHT DECK FLOOR DENTED (PREVIOUS REPAIR) STA 252 RBL 10.<[01] ACCCOMPLISHED EA 24-153-02293. REF TTG8Q00U7A5.;[02] CORRECTING STEP 1: ACCCOMPLISHED 3 EACH ELONGATED HOLES AT FLIGHT DECK FLOOR REPAIR PER EA 24-153-02293. REF TTG8Q00U7A5.;[03] CORRECTION STEP 1 AND 2. ACCOMPLISHED EA 24-153-02293. REF FAULT TTG8Q00UZ7A5.;[04] RII -- VERIFIED STEP 3.
FOUND 3 EACH ELONGATED HOLES AT FLIGHT DECK FLOOR DENTED (PREVIOUS REPAIR) STA 252 LBL 22.<[01] ACCCOMPLISHED EA 24-153-02293. REF TTG8Q00U7A5.;[02] CORRECTING STEP 1: ACCCOMPLISHED 3 EACH ELONGATED HOLES AT FLIGHT DECK FLOOR REPAIR PER EA 24-153-02293. REF TTG8Q00U7A5.;[03] CORRECTING STEP 2: ACCOMPLISHED EA 24-153-02293. REF FAULT TTG8Q00UZ7A5.;[04] RII -- VERIFIED STEP 3.
FWD CABIN WET AREA INTERCOSTAL BETWEEN STA 344 AND STA 360 BL 0 HAS A CRACK AROUND FASTENER HOLE.<[01] REMOVED AND INSTALLED NEW INTERCOSTAL AT FWD CABIN WET AREA BETWEEN STA 344 AND STA 360 BL 0 AS PER SRM 51-40-02-0G-0 AND DWG#141A5400.;[02] VERIFIED STEP 1
FWD CABIN WET AREA INTERCOSTAL BETWEEN STA 294.5 AND STA 285.62 BL 0 HAS A CRACK AROUND FASTENER HOLE. FWD CABIN WET AREA INTERCOSTAL BETWEEN STA 294.5 AND STA 277 BL 0 HAS A CRACK AROUND FASTENER HOLE.<[01] REMOVED AND INSTALLED NEW INTERCOSTAL AT FWD CABIN WET AREA BETWEEN STA 294.5 AND STA 277 BL 0 AS PER AS PER SRM-51-40-02-0G-0 AND DWG#141A5400;[02] VERIFIED STEP 1
FWD CABIN WET AREA INTERCOSTAL BETWEEN STA 344 AND STA 360 LBL 13 HAS A CRACK AROUND FASTENER HOLE.<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 344 AND STA 360 LBL 13 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A5400;[02] VERIFIED REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 344 AND STA 360 LBL 13
PASSENGER CABIN FLOOR SUPPORT CRACKED B.S. 540 LBL 2' W.L. 208. (DOT 51-015) PASSENGER CABIN FLOOR SUPPORT CRACKED B.S. 540 RBL 2' W.L. 208. (DOT 51-015)<[01] REMOVED FLOOR PANEL 231UF FOR ACCES REF AMM 53-21-00-000-801; REMOVED PASSENGER CABIN FLOOR SUPPORT B.S. 540 RBL 2' W.L. 208. REF SRM 51-40-02-0G-0; CORRCTION STEP 1 OF STEP 3LOCATED AND DRILLED PANEL AND BREAK ASSY FLOOR SUPPORT B.S.540 RBL2' W.L. 208; REF : SRM 51-40-05-0G-0 AND DRW #143A5240;PERFORMED HFEC ROTO INSP ON EXISTING FASTENER OPEN HOLES;<BR>IAW B737 NDT PART 6; 51-00-00 PROC. 16<BR>TOOLS: NORTEC 600; B/C 166317; CAL. DUE: 20-NOV-2024.<BR>NO CRACKS FOUND;OK TO INSTALL PASSENGER CABIN FLOOR SUPPORT B.S. 540 RBL 2' W.L. 208; INSTALLED FLOOR SUPPORT AT PASSENGER CABIN AT B.S 540 RBL 2' W.L 208 AS PER REF: BOEING 737-700 SRM 51-40-02-0G-0 AND DWG # 143A5240;[02] RII -- VERIFIED STEP 1.
PASSENGER CABIN FLOOR SUPPORT CRACKED AT F.S. 540 RBL 25' W.L. 208. (DOT 51-014) PASSENGER CABIN FLOOR SUPPORT CRACKED AT F.S. 540 LBL 25' W.L. 208. (DOT 51-014)<[01] REMOVED FLOOR PANEL 231VF FOR ACESS REF AMM 53-21-00-000-801<BR>LOCATED AND DRILLED MAIN CABIN FLOOR SUPPORT BREAK ASSY AT<BR>FS 540 LBL 25' W.L. 208. REF SRM 51-40-02-0G-0<BR>AND DRW #143A5240<BR>PERFORMED COUNTERSINK INSP AND ROTO INSP. ON EXISTING HOLES IAW B737 NDT P. 6; 53-30-00 PROC. 3. NO CRACKS. EQUIP: NORTEC 600 B/C 166317 CAL DUE: 11/24<BR>LOCATED AND DRILLED AND INSTALLED MAIN CABIN FLOOR SUPPORT BREAK ASSY AT<BR>FS 540 LBL 25' W.L. 208. REF SRM 51-40-05-0G-01<BR>AND DRW #143A5240<BR>INSTALLED FLOOR PANEL 231VF FOR ACESS REF AMM 53-21-00-000-801<BR>TOOL USED I/D: 176021; S/N :15880; DUE :04-DEC-2024;[02] VERIFIED STEP1.
FWD CARGO COMPT L/H Z CHANNEL FASTENER HOLE ELONGATED AT STA 480+6.<[01] REMOVED FWD CARGO COMPARTMENT L/H Z CHANNEL FROM STA 400 TO STA 480+8 PER SRM 51-40-02-0G-0; REMOVED Z CHANNEL SPLICE AT FWD CARGO COMPARTMENT L/H BETWEEN STA 480 AND 500 PER SRM 51-40-02-0G-0; FABRICATED NEW SPLICE PER SRM 53-00-53-2R-5 MATERIAL USED BAC 1496-444 PO:2072494; FABRICATED; LOCATED AND DRILLED Z CHANNEL SECTION L/H FROM STA 396 TO STA 490 PER SRM 51-40-05-0G-0; TREATED AND PRIMED PER SRM 51-20-01-0G-0; INSTALLED SPLICE AND Z CHANNEL PER SRM 53-00-53-2R-5 AND SRM 51-40-02-0G-0; DWG 143A7500.;[02] VERIFIED STEP 1
CRACK FOUND ON THE 141A6536-14 BEAM IAW B737 NDT P. 6; 51-00-00 PROC. 23. CRACKED IN RADIUS. CRACK FOUND ON THE 141A6536-14 BEAM 4 IAW B737 NDT P. 6 51-00-00 PROC. 23. CRACKED IN RADIUS EO 5241-C-14093 OR 5241-C-14344 WILL BE ADDED TO REPAIR ORDER FOR REPAIR.<[01] SUMMARY :REMOVED BEAM FOUND CRACK P/N 141A6536-14 AND INSTALLED NEW BEAM AS PER RE B/737 SRM 51-40-02-0G-0.AND DWG # 141A06535 AND 141A6516.;[02] RII -- VERIFIED STEP 1.;[03] COMPLETED SME INSPECTION OF WORKMANSHIP AND PAPERWORK AUDIT.;[04] RII -- VERIFIED STEP 1.
CRACK FOUND AT STA 294.5 +4 AT S-15L WL 230 LBL 64. CRACK FOUND AT STA 294.5 +4 AT S-14L WL 230 LBL 64<[01] REPAIR WAS ACCOMPLISHED PER EA 24-153-02286 AT STA 294.5 +4 AT S-15L WL 230 LBL 64;[02] CORRECTED STEP 1. REPAIR WAS ACCOMPLISHED PER EA 24-153-02286 AT STA 294.5 +4 AT S-14L WL 230 LBL 64;[03] RII -- VERIFIED STEP 2.
CRACK FOUND ON THE 141A6536-15 BEAM IAW B737 NDT P. 6; 51-00-00 PROC. 23. CRACKED IN RADIUS. CRACK FOUND ON THE 141A6536-15 BEAM 5 IAW B737 NDT P. 6 51-00-00 PROC. 23. CRACKED IN RADIUS. EO 5241-C-14093 OR 5241-C-14344 WILL BE ADDED TO REPAIR ORDER FOR REPAIR.<[01] REMOVED BEAM #5 FOR DAMAGE AT R1 DOOR IN REF B 737-700 SRM 51-40-02-0G-0. INSTALLED NEW BEAM #5 AT R1 DOOR IN REF B 737-700 SRM 51-40-02-0G-0 AND DWG # 141A6535; 141A6516;[02] RII -- VERIFIED STEP 1.
CABIN RT SIDE CUSP WEB BETWEEN ST 420 AND 440 WL 208.1 - STAND-OFF HAS A PULLED RIVET AS MARKED. 124-002<[01] REPLACEMENT OF CABIN RT SIDE WEB BETWEEN ST 420 AND 440 WL 208.1 WILL BE ACCOMPLISHED ON TTG8Q00V1YXU.;[02] VERIFIED STEP 1
STA 312 L/H SIDE HAS A CRACK JUST ON TOP OF L-1 DOOR CUTOUT.<[01] THIS TASK CARD WAS ACCOMPLISHED ON EA NO:M-22-153-01244;[02] CORRECTION TO STEP 1: WORK WAS ACCOMPLISHED ON TASK CARD TTG8Q00V38DR; EA NO:M-22-153-01244.;[03] VERIFIED STEP 2
RH HORIZONTAL STABILIZER RIB #3 STIFFENER 3 CRACK.<[01] REMOVED DAMAGED AND INSTALLED NEW REPAIR KIT AT RH HORIZONTAL STABILIZER RIB #3; AND STIFFENER #3 PER SRM 55-10-09-2R-4 REPAIR 4 AND DWG 55100003;[02] STEP 1 ENTERED IN ERROR;[03] REMOVED DAMAGE AND INSTALLED NEW REPAIR KIT AT HORIZONTAL STABILIZER RIB#3; STIFFENER #3 PER SRM 55-10-09-2R-4 REPAIR 4 AND DWG= 55100003;[04] VERIFIED STEP 3
CABIN RT SIDE CUSP WEB BETWEEN ST 420 AND 440 WL 208.1 CRACKED AS MARKED. 124-001<[01] REMOVED ; FABRICATED AND INSTALLED RT SIDE CUSP WEB BETWEEN STA 420 TO STA 440 PER 51-40-02-0G-0 AND DWG: 143A5913;[02] VERIFIED STEP 1
FLOOR STRUCTURE AFT O/B FITTING OF LAV A HAS CORROSION EDIT FAULT DESCRIPTION: L-1 DOOR FWD GIRT BAR FITTING HAS CORROSION<[01] REMOVED AND REPLACED L-1 DOOR FWD GIRT BAR FITTING PER SRM 51-40-02-0G-0.;[02] VERIFIED REPLACEMENT
FWD WET AREA FLOOR PANEL 221BF HAS INSERTS WITH CORROSION.<[01] FAULT RESOLVED ON OTHER FAULT. PANEL WILL BE REPLACED . REF. TTG8Q00V0RKR;[02] CORRECTION: FAULT RESOLVED ON OTHER FAULT. PANEL WILL BE REPLACED REF. TTG8Q00V0RL0;[03] VERIFIED T/C: ON TTG8Q00V0RL0
FWD WET AREA FLOOR PANEL 221BF AFT O/B CORNER IS CRACKED<[01] RECEIVED NEW FLOORPANEL #141A5810-729 (221BF) WILL BE INSTALLED ON TTG8Q00U3WRV.;[02] VERIFIED STEP 1
P15 REFUEL PANEL FACEPLATE HAS MULTIPLE CORROSION SPOTS<[01] REMOVED AND REPLACED P15 REFUEL PANEL FACE PLATE I/A/W BOEING AMM 28-21-00-000-801 & 28-21-00-400-801; OPS CHECK FOUND NORMAL;[02] VERIFIED STEP 1
CORROSION FOUND ACCESS DOOR 311BL FWD EDGE HAS EVIDENCE OF CORROSION.<[01] REMOVED AND REPLACED ACCESS DOOR 311BL AS PER AMM 52-49-11-000-802 AND AMM 52-49-11-400-802.;[02] VERIFIED STEP 1
PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES AND COUNTERSINKS.<[01] REMOVED AND REPLACED PANEL PER SRM 51-40-02.
FWD GALLEY SERVICE DOOR HANDLE COVER CRACKED<[01] R&R FWD GALLEY SERVICE DOOR HANDLE COVER PER SIP.
CAPT SIDE EMER. EXIT SIDE WALL LIGHT INOP ( WINDOW)<[01] AC OK TO CONTINUE PER MEL 33-2-03 SP1B AUTH#128268;[02] RELAMPED EMERGENCY. EXIT SIDEWALL LIGHT PER AMM 33-51-01
CREW REPORTS FWD ENTRY GIRT BAR HARD TO ENGAGE / [01] REMOVED DEBRIS FROM GIRT BAR LATCHES PER SIP
R/H OVERWING EXIT LENS MISSING / [01] REPLACED THE MISSING OVERWING EXIT LENS REF AMM 33-51-01;[02] CREATED IN ERROR. FAULT FOR A/C 730 REF BARCODE TTG8Q00E9GBE
RUDDER COUNTER BALANCE WEIGHT RH SIDE FWD CORNER; SPOT OF CORROSION. REMOVED RUDDER COUNTER BALANCE WEIGHT AT BALANCE ARM IAW CMM 55-40-09. INSPECTED AREA OF INSTALLATION, BOLTS & NEW BALANCE WEIGHT. INSTALLED NEW BALANCED WEIGHT IAW CMM 55-40-09, FOUND WEIGHT BALANCE WITHIN LIMITS IAW SRM: 55-40-02-1A-3.
AFT CARGO DOOR FWD CORNER SCUFF PLATE CRACK. ACCOMPLISH AFT CARGO DOOR FWD CORNER SCUFF PLATE WELD REPAIR IAW SRM 53-60-15-2R-1.
AFT CARGO COMP. AFT CORNER SCUFF PLATE WITH EVIDENCE OF CRACK AT FWD END. / [01] PERFORMED HFEC INSP ON AFT CARGO SCUFF PLATE; IAW B 737 NDT PART 6 51-00-00 PROCE 23. TOOL NORTEC 600. BC 166316. CALIB DUE 10-8-22. CRACK INDICATION ON FWD END.;[02] ACCOMPLISHED WELDING REPAIR BY OUTSIDE VENDOR WITH P.O NO.413588 AT AFT CARGO COMP. AFT CORNER SCUFF PLATE FWD END PER B737-700 SRM 53-60-15-2R-1 STEP B (4) PAGE. #2;[03] VERIFIED STEP #2 CERTIFICATION; OK.;[04] FWD CARGO COMP. SCUFF PLATES WAS REMOVED AND WILL BE INSTALL ON FWD CARGO MOC #TTG8Q004BG3S STEP 5 AND 55;[05] VERIFIED STEP #4 TTG8Q004BG3S
L/H EXTERIOR EMERGENCY OVERWING LIGHT INOP. / [01] REMOVED AND REPLACED LAMP AT L/H EXTERIOR EMERGENCY OVERWING LT AND PERFORMED OPS TEST FOUND NORMAL AS PER REF B737-AMM-33-51-04-960-801;[02] VERIFIED STEP 1
EMERGENCY BATTERY PACK AT POSITION M1673 AND M1668 FAILED OPS TEST. / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT POSITION M1668 REF B737 AMM 33-51-06-960-805;[02] VERIFIED STEP 1;[03] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT POSITION M1673 REF B737 AMM 33-51-06-960-805;[04] EMERGENCY LIGHTING SYSTEM OPS CHECKED NORMAL REF B737 AMM 33-51-06-960-805;[05] VERIFIED 3; 4
EMERGENCY BATTERY PACK AT POSITION M1673 AND M1668 FAILED OPS TEST. / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT POSITION M1668 REF B737 AMM 33-51-06-960-805;[02] VERIFIED STEP 1;[03] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT POSITION M1673 REF B737 AMM 33-51-06-960-805;[04] EMERGENCY LIGHTING SYSTEM OPS CHECKED NORMAL REF B737 AMM 33-51-06-960-805;[05] VERIFIED 3; 4
CORROSION FOUND AFT CARGO DOOR CUTOUT LOWER SILL STRAP AT STA 787 +16 RBL 20 W.L. 155.5 / [01] REMOVED CORROSION AT AFT CARGO DOOR CUTOUT LOWER SILL STRAP STA 787+16 RBL 20 WL 155.5 AS PER REF B737-700 SRM 51-10-02-0G-0;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THK. NOTED 0.050'<BR>TOOL USED : OLYMPUS 27MG B/C 172139 04/22;[04] EVALUATED REWORKED AREA. ORIGINAL THICKNESS 0.100'; MATERIAL LOST 0.050'; MATERIAL REMAINING 0.050'. FOUND OUT OF LIMITS AS PER REF B737-700 SRM 53-60-15-1A-1;[05] REMOVED AFT CARGO DOOR CUTOUT LOWER SILL STRAP STA 787+16 RBL 20 WL 155.5 AS PER REF B737-700 SRM 51-40-02-0G-0;[06] LOCATED AND DRILLED NEW AFT CARGO DOOR CUTOUT LOWER SILL STRAP AS PER REFERENCE B737-700 SRM 51-40-05-0G-0.;[07] VERIFIED STEPS 4; 5 AND 6. OK TO INSTALL NEW STRAP.;[08] STARTED INSTALLATION OF THE NEW AFT CARGO DOOR CUTOUT LOWER SILL STRAP AS PER REFERENCE B737-700 SRM 51-40-02-0G-0 AND DWG #146A8120.;[09] INSTALLED NEW AFT CARGO DOOR CUTOUT LOWER SILL STRAP AS PER REFERENCE B737-700 SRM 51-40-02-0G-0 AND DWG #146A8120.;[10] VERIFIED STEPS 8 AND 9.
CORROSION FOUND AT AFT CARGO FLOOR STRIP AT STA 767 +5 BETWEEN RBL 21 AND LBL 21 W.L. 155.5 AROUND FASTENER HOLES. / [01] FOUND EXFOLIATION AT AFT CARGO FLOOR STRIP AROUND THE FASTENERS OUT OF LIMITS AS PER REF B737-700 SRM 53-00-53-1A-2;[02] RECEIVED AND VERIFIED NEW FLOORBOARD SPLICE P/N 146A9401-4 AS PER REFERENCE B737-700 SRM 53-60-53-0L-2 AND DWG #146A9401.<BR>FLOORBOARD SPLICE WILL BE INSTALL IN TASK CARD # TTG8Q004BZAN.;[03] VERIFIED STEP#2 ABOVE.
WEB LOCATED AND ATTACHED TO INBOARD SIDE LEFT DEFLECTION CONTROL RIB SUPPORT BEAM IS CRACKED / [01] REMOVE L/H DEFLECTION CONTROL RIB SUPPORT BEAM REF SRM 51-40-02;[02] CORRECTION OF STEP 1. REMOVE WEB FROM L/H DEFLECTION CONTROL RIB SUPPORT BEAM REF SRM 51-40-02;[03] VERIFIED STEP #2.;[04] OK TO INSTALL NEW WEB ANGLE.;[05] INSTALLED NEW ANGLE TO L/H DEFLECTION CONTROL RIB SUPPORT BEAM; REF SRM<BR>51-40-02;[06] CERTIFIED;[07] VERIFIED ALL STEPS
RH STA 663 VAPOR BARRIER CRACKED AT RBL 25. / [01] MEASUREMENTS;[02] CLEANED R/H VAPOR BARRIER ;PREPARED DAMAGE AREA FOR REPAIR; STOP DRILL ALL CRACKS AS PER B737 SRM 51-70-04-2R-10;[03] PERFORMED DRY OUT ON VAPOR BARRIER; FOUND NO WATER AS PER B737 SRM 51-70-04-2R-10;[04] VERIFIED STEPS 1 ;2 & 3 AND OK TO INSTALL REPAIR;[05] REPAIRED CRACK DAMAGE ON R/H VAPOR BARRIER WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-10;[06] PERFORMED TAP TEST ON REPAIRED AREA ;FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION 5;[07] VERIFIED STEPS #5 AND #6.;[08] OK TO APPLY PRIMER AND TOP COAT.;[09] APPLIED TREAT AND PRIMER AT VAPOR BARRIER REPAIR AS PER REF B737-700 AMM 51-21-73-370-803;[10] APPLIED TOP COAT AT VAPOR BARRIER REPAIR AS PER REF B737-700 AMM 51-21-73-370-803;[11] VERIFIED STEPS 9 AND 10.
FLAPS WOULD NOT EXTEND BEYOND 2. USED ALT FLAP EXTENSION TO EXTEND TO 15 / [01] C/W FIM 27-51 TASK 813; FLAPS OP'S NORMAL; NO DEFECTS NOTED. INSPECTED FLAPS NO DEFECTS NOTED. FURTHER TROUBLESHOOT REQUESTED BY MX CONT.;[02] R+R L/H FLAP POSITION TRANSMITTER REF AMM 27-58-01 OPS GOOD
SIDEWALL LIGHT ON L/H EMERGENCY EXIT DOOR INOP. / [01] REPLACED BALLAST L/H EMERGENCY EXIT REF. AMM 33-21-00.
L1 DOOR PLASTIC ASSIST HANDLE BROKEN ; / [01] ROBBED HANDLE FROM FWD AND INSTALLED ON L1 DOOR IAW AMM 52-11-31
193D PN TRAILING EDGE HAS 6 DIMPLED; CRACKED AND OVERSIZED FASTENER HOLES. ; / [01] REMOVED AND PLACED PANEL PER AMM 53-51-21
AT BEGINNING OF DSECENT; NO 2 ENGINE HYDRAULIC PUMP PRESSURE FLICKERED; THEN EVENTUALLY CAME ON STEADY. HYDRAULIC B-SYSTEM QTY WAS 0. DID QRH PROCEDURE TO SECURE ENG DRIVEN PUMP; THEN ELECTRIC PUMP ; LOW PRESSURE LIGHT ILLUMINATED. RAN QRH FOR B-SYSTEM HYDRAULIC SYSTEM FAILURE. / [01] PERFORMED EXTERNAL LEAK CHECK REF AMM 29-00-00-790-801.FOUND HYDRAULIC B PRESS RUDDER TUBE LINE LEAKING.INSPECTED CASE DRAIN FILTERS; NO CONTAMINATION NOTED; REPLACED BOTH FILTERS AS PER REF AMM 29-11-51.INSTALLED TEMP LINE HYDRAULIC B RUDDER PRESS TUBE REF. MPM 53.05.08.02 & REF AMM 20-10-52.SERVICED SYSTEM B HYDRAULICS AS PER REF AMM 12-12-00.
FORWARD SERVICE DOOR OUTSIDE EMERGENCY LIGHT INOP ; / RELAMPED IAW AMM 33-51-04
AFT GALLEY EXIT LIGHT COVER OFF / RESECURED AFT GALLEY EXIT LIGHT COVER AT R2 DOOR PER S.I.P.
FWD SERVICE DOOR FLOOR EXIT SIGN COVER MISSING. REPLACED FWD SERVICE DOOR FLOOR EXIT SIGN COVER, PER SIP.
AFT GALLEY LT BATTERY FAILED CHECK. REMOVED AND REPLACED, PER AMM.33-51-06.
RT OVERWING EMERGENCY EXIT BATTERY FAILED CHECK. REMOVED AND REPLACED, PER AMM 33-51-06.
CRACK ANGLE - SUPPORT LOCATED BS 867 AT LEVEL FLOOR STRUCTURE BETWEEN STR 26L TO STR27L AFT CARGO COMPARTMENT (1 EA) / REPLACED ANGLE SUPPORT LOCATED BS 867 AT LEVEL FLOOR STRUCTURE BTW STR R26L TO 27L AFT CARGO COMPARTMENT IAW 737-700 SRM 51-40-02 DWG 149A8103 SHEET 1 REV D. SRM B737-700 51-10-02 ITEM 9
CRACK SUPPORT STRUCTURE WING TO BODY FAIRING AT LEVEL BS 540 STR 24R AT LOWER FUSELAGE / REPLACED BRACKET ON SUPPORT STRUCTURE WING TO BODY FAIRING AT LEVEL BS 540 STR 24R AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A0060 REV.A
CORROSION CHANNEL SUPPORT BETWEEN BS 767 TO BS 787 AT LEVEL FLOOR STRUCTURE RBL 22 AND WL 155.5 APPROX. AFT CARGO COMPARTMENT / REPLACED CHANNEL SUPPORT BTW BS 767 TO BS 787 AT LEVEL FLOOR STRUCTURE RBL 22 AND WL 154 APPROX. AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG:146A0081 REV A
CRACK FLOOR STRUCTURE SUPPORT PLATE BS540 BETWEEN RBL 24 TO RBL45 AT PASSENGER CABIN (1 EA) / REPLACED FLOOR STRUCTURE SUPPORT PLATE BS 540 BETWEEN RBL 24 TO RBL 45 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02
CRACK FLOOR STRUCTURE SUPPORT PLATE BS540 BETWEEN BL0 TO LBL24 AT PASSENGER CABIN (1 EA) / REPLACED FLOOR STRUCTURE SUPPORT PLATE BS 540 BETWEEN BL0 TO LBL24 PASSENGER CABIN IAW B737-700 SRM 51-40-02
CORROSION LOWER SILL LOCATED BETWEEN BS 794 TO BS 847; RBL 25 AT LEVEL FLOOR STRUCTURE WL 154 APPROX. AFT CARGO COMPARTMENT / REPLACED LOWER SILL LOCATED BETWEEN BS 794 TO BS 847; RBL 25 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG #146A8340 REV-
CRACK INTERCOSTAL, WEB FLOOR STRUCTURE LOCATED BETWEEN BS 344 TO BS 360 AT BL 0 AT PASSENGER CABIN. REPLACED INTERCOSTAL WEB, FLOOR STRUCTURE LOCATED BETWEEN BS 344 TO BS 360 AT BL 0 AT PASSENGER CABIN, IAW B737-700 SRM 51-10-02 STEP 9 AND DRAWING 141A5400 REV.
CORROSION FLOOR STRUCTURE INNER CHORD LOCATED BETWEEN BS 967 TO BS 1006 AT LEVEL STR 17R AND RBL 51 AFT GALLEY AND LAV AND WL 208.1. REPLACED INNER CHORD FLOOR STRUCTURE LOCATED BETWEEN BS 907 TO BS 1006 AT LEVEL STR 17R AND RBL 51 AND WL 208.1 AFT GALLEY, IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 147A8501 REV B.
CRACK TRACK RBBL 13.84 LOCATED BETWEEN BS 727E TO BS 767 AT AFT CARGO COMPARTMENT (3 EA). REPAIRED TRACK LOCATED BETWEEN BS 727D AND BS 787 TO RBL 13.84 AT AFT CARGO COMPARTMENT, IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3.
GOUGE CLOSURE ANGLE FWD POSITION LOCATED BETWEEN BS 1006 TO BS 1016 LT SIDE AT UPPER FUSELAGE (1 EA). REPLACED CLOSURE ANGLE FWD POSITION LOCATED BETWEEN BS 1006 TO BS 1016 LT SIDE AT UPPER FUSELAGE, IAW B737-700 SRM 51-40-02 DRAWING 147A0030 REV B.
CORROSION BILGE AREA AT SUPPORT ZEE LOCATED BS 500A AT LEVEL STR 26L AND WL 156.5 AT FWD CARGO COMPARTMENT. REPAIRED SUPPORT ZEE BILGE AREA LOCATED BS 500A AT LEVEL STR 26L AND WL 156.5 AT FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DWG 143A7501 REV B.
CRACK WEB INTERCOSTAL BETWEEN BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA. REPLACED WEB INTERCOSTAL BETWEEN BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA, IAW B737-700 SRM 51-10-02 ITEM 9 B737-700 SRM 1-40-02 AND DRAWING 141A8180 REV C.
GOUGE CLOSURE ANGLE FWD POSITION LOCATED BETWEEN BS 1006 TO BS 1016 RT SIDE AT UPPER FUSELAGE (1 EA). REPLACED CLOSURE ANGLE FWD POSITION LOCATED BETWEEN BS 1006 TO BS 1016 RT SIDE UPPER FUSELAGE, IAW B737-700 SRM 51-40-02 AND DRAWING 147A0030 REV B.
CRACK TIE CLIP AT LEVEL BS 277 ON STR 10R AT PASSENGER CABIN. REPLACED TIE CLIP AT LEVEL BS 277 ON STR 10R AT PASSENGER CABIN, IAW B737-700 SRM 51-10-02 STEP 9 AND DRAWING 141A1110 REV.
CORROSION CHANNEL SIDEPLATE LOCATED BS500 TO BS500A AT LEVEL STR26R AND WL156.5 FWD CARGO COMPARTMENT / REPLACED CHANNEL SIDEPLATE LOCATED BS 500 TO BS 500A AT LEVEL STR 26R FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG # 143A0080 REV-
CRACK STRINGER 25R AT BS 540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 25R LOCATED BETWEEN BS 500C TO BS 540 FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.
CRACK STRINGER 24R AT BS540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 24R LOCATED BETWEEN BS 500D TO BS 540 FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03- 2R-1 REPAIR 1.
CRACK STRINGER 26R AT BS 540 AT FWD CARGO COMPARTMENT. REPAIRED STRINGER 26R AT BS 540 AT FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.
CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT / REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1; BHC 5975.
BROKEN ESCAPE SLIDE VISOR SERVICE DOOR AT FWD GALLEY AND LAVATORY. REPLACED VISOR ON ESCAPE SLIDE COVER SERVICE DOOR AT FWD GALLEY, IAW BOEING 737-700 DRAWING 416A2204 REV R.
DETERIORATED FLOOR MAT GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA. REPLACED FLOOR MAT GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA, IAW B737-700 AMM 25-66-02-400-801 STEP 3.D(I).
CRACK CHANNEL SUPPORT AFT SIDE OF STA 727 BULKHEAD AFT CARGO COMPARTMENT (1 EA) / REPLACED CHANNEL SUPPORT AFT SIDE OF STA 727 BULKHEAD AFT CARGO COMPARTMENT (1EA) I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 144A2600 REV. A
CRACK GUSSET BS500D AT LEVEL STR 19 L FWD CARGO COMPARTMENT (1 EA) / REPLACED NEW GUSSET LOC BS 500D AT LEVEL STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 STEP 9 AND DRAWING # 143A7902 REV -.
SEVERAL DENTS ON INBOARD MAIN FLAP LOWER SURFACE LOCATED AT 4.5IN FROM TRAILING EDGE AND 6.25 IN FROM OUTBOARD EDGE WEDGE PANEL AT RT WING. PERFORMED PERMANENT REPAIR ON INBOARD MAIN FLAP WEDGE PANEL AT RT WING, AS PER B737-700 SRM 57-53-01-2R-7 REP 7. TOOL USED CALIPER P/N 500-197-30 S/N 15272055 DUE DATE 04AUG21; HOTBONDER P/N HCS9200B S/N 13061394 DUE DATE 09JUL21; NDT TOOL P/N 5-3 S/N 064 DUE DATE 08JUN21.
DENT INBOARD MAIN FLAP LOWER SURFACE LOC AT 3.75 IN FROM TRAILING EDGE AND 4.25 IN FROM OUTBOARD EDGE AT RT WING. PERFORMED PERMANENT REPAIR ON INBOARD MAIN FLAP WEDGE PANEL AT RT WING AND IS DOCUMENTED ON DEFECT NO L177042.
DENT INBOARD MAIN FLAP UPPER SURFACE LOC AT 2.5 IN FROM TRAILING EDGE AND 43.5 IN FROM OUTBOARD EDGE AT RT WING. PERFORMED PERMANENT REPAIR ON INBOARD MAIN FLAP WEDGE PANEL AT RT WING AND IS DOCUMENTED ON DEFECT NO L177042.
CRACK GUSSET BS 500D AT LEVEL STR 19 R FWD CARGO COMPARTMENT (1 EA) / REPLACED GUSSET BS 500D AT LEVEL STR 19R FWD CARGO COMPARTMENT (1EA) I.A.W B737-700 SRM 51-10-02-OG-0 ITEM 9 AND DWG 143A7902 REV-.
DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (8EA). REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN(8EA) AND STEPS ARE DOCUMENTED ON SWA CARD 733-080-00-01.
ROW 16 DEF AND 19DEF AISLE EMERGENCY LIGHTS INOP. / R7R BATTERY PACK FOR EMERGENCY LIGHTS AT APROX. PAX ROW 16 & 19DEF I/A/W AMM 33-21-06. OPS CHECK NORMAL
ROW 3 DEF;6DEF;9ABC AND 12ABC AISLE EMERGENCY LIGHTS INOP. / R&R POWER SUPPLY BATTERY PACKS AT STA322 AND STA 727 + 13 AND OPS CHECK GOOD PER AMM 33-51-06
CARGO FIRE DISCHARGE L7 CAME ON IN CRUISE / R/R CARGO FIRE CONTROL PANEL AS PER REF AMM 26-00-02 RAR# 54790 P/N OFF/ON 47355-1 S/N OFF 4499 S/N ON 1664
CARGO FIRE DISCHARGE LIGHT ILL INFLIGHT WITH NO FIRE INDICATIONS. FLIGHT CREW REPORTS LIGHT WENT OUT DURING FLIGHT. PERFORMED CARGO FIRE OPERATIONAL TEST IAW AMM 26-16-00 OPS TEST GOODD NO HISTORY WITHIN 30 DAYS
FORWARD GALLEY OVER DOOR EXIT SIGN INOP. R&R BATTERY PACK PER AMM.
LT EXIT LOCATOR SIGN INOP. R&R BATTERY PACK PER AMM.
L1 DOOR ESCAPE SLIDE LIGHT INOP. R&R BATTERY PACK PER AMM.
L1 DOOR ESCAPE SLIDE LIGHT INOP. R&R CHARGER PER AMM.
LT EXIT LOCATOR SIGN INOP. R&R CHARGER PER AMM.
FORWARD GALLEY OVER DOOR EXIT SIGN INOP. R&R CHARGER PER AMM.
LH WING #3 CANOE OUTBD SIDE SEAL RETAINER HAS 3 RIVETS PULLED THROUGH / (CLOSING DMA 0061824) CL # 56047 PERMANENT REPAIR ACCOMPLISHED ON ACTION LOG PAGE # 0661043
L2 DOOR EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.
LT HORIZONTAL STABILIZER RIB CRACKED AT 120.30, 4TH STIFFENERS FROM FORWARD END. REPAIRED RIB PER SRM.
LT HORIZONTAL STABILIZER RIB CRACKED AT 120.30, 3RD STIFFENERS FROM FORWARD END. REPAIRED RIB PER SRM.
LT HORIZONTAL STABILIZER RIB CRACKED AT 120.30, 2ND STIFFENERS FROM FORWARD END. REPAIRED RIB PER SRM.
RT HORIZONTAL STABILIZER RIB CRACKED 120.30 3RD STIFFENERS FROM FORWARD END. REPAIRED RIB PER SRM.
RT HORIZONTAL STABILIZER RIB CRACKED 120.30 2ND STIFFENERS FROM FORWARD END. REPAIRED RIB PER SRM.
RT HORIZONTAL STABILIZER RIB CRACKED 120.30 4TH STIFFENERS FROM FORWARD END. REPAIRED RIB PER SRM.
LT WING FIXED LEADING EDGE AFT STRINGER CRACKED AT OUTBOARD FLANGE FASTENER HOLE COMMON TO SEAL RIB. R&R STRINGER IAW SRM AND DWG.
WHILE WORKING FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 767-794 R/H SIDE / REMOVED FLOOR TO SIDEWALL SUPPORT BS 767-794 IAW SRM 51-40-02. RECEIVED FLOOR TO SIDEWALL ITEM 7531132 PO #700102. LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 146A0081. INSTALLED FLOOR TO SIDEWALL SUPPORT BS 7670794 IDW DWG 146A0081 AND SRM 51-40-02 80641U 12/14/18
LOWER CENTER VAPOR BARRIER WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB PER SRM AND EA.
RT MAIN LANDING GEAR FORWARD TRUNNION LUG FITTING CORRODED. REPAIRED FITTING PER EA.
LT MAIN LANDING GEAR FORWARD TRUNNION LUG FITTING CORRODED. REPAIRED FITTING PER EA.
L1 DOOR EVAC SLIDE EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
L1 DOOR ESCAPE SLIDE INADVERTENTLY FELL OUT OF COVER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER AMM AND MT.
ON PREFLIGHT INSPECTION LT MAIN WHEEL WELL MOISTURE BARRIER CRACKED AT LBL 40. REPAIRED BARRIER PER SRM.
DURING CLIMB, RECEIVED OIL FILTER BYPASS LIGHT FOR THE NR 2 ENGINE 2. RAN QRH AND LIGHT DID NOT EXTINGUISH. INFLIGHT SHUTDOWN, AIR TURNBACK, DECLARED AN EMERGENCY. R & R THE NR 2 ENGINE IAW MT.
LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.
INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294.5, BL 0. R&R INTERCOSTAL PER SRM.
L1 DOOR FLOOR STRUCTURE ANGLE CRACKED AT BS 303. REPAIRED ANGLE PER EA.
FORWARD CARGO THRESHOLD WEB CORRODED. REPAIRED WEB PER SRM.
LT OVERWING EMERGENCY EXIT LIGHT INOP. R&R LIGHT PER AMM.
ELECTRICAL BURNING ODOR AND SLIGHT SMOKY HAZE REPORTED IN THE CABIN AROUND ROW 17. SMOKE ODOR WENT AWAY AFTER TURNING OFF GALLEY POWER AND SEAT BELT SIGN. R & R CABIN RECIRCULATION FAN IAW AMM.
R1 DOOR EXIT SIGN FELL OFF. R&R LIGHT ASSEMBLY COVER PER MM.
RIGHT OVERWING EXIT DOOR LIGHT LENS BROKEN. R & R LENS IAW MM.
OVERWING CEILING EMER EXIT SIGN LOOSE. R & R SIGN IAW AMM.
EMER BATTERY FAILED CAPACITY CHECK AT LOCATION M1674. R & R BATTERY IAW AMM.
RIGHT WING NR 6 GND SPOILER, UPPER TE SHELF PANEL SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATION M1670. R & R BATTERY IAW AMM.
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATION M1673. R & R BATTERY IAW AMM.
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATION M1672. R & R BATTERY IAW AMM.
R1 DOOR EMER LIGHT MISSING ON WALL. INSTALLED LIGHT ASSEMBLY IAW SIP.
FLOOR SUPPORT INTERCOSTAL BROKEN AT BS 540, BETWEEN BL 0 TO LBL 24. R & R INTERCOSTAL IAW SRM.
LEFT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER AT STAB STATION 129.5, 27 INCHES FROM THE FRONT SPAR CRACKED. REPAIRED RIB IAW EA.
LEFT FLIGHT DECK WINDOW FRAME CRACKED AT OTBD UPPER SURFACE. REPAIRED FRAME IAW EA.
LEFT MLG WW CTR WING SECTION, LOWER LT VAPOR BARRIER CRACKED AT LBL 40.00 6 INCHES FROM BOTTOM. REPAIRED BARRIER IAW SRM.
RIGHT FWD EEPLS WORN. R & R EEPLS IAW MM.
L1 DOOR EMER EXIT SIGN LENS MOUNT BROKEN. R & R MOUNT ASSEMBLY IAW AMM.
MID CABIN CEILING EMER LIGHT LENS LOOSE. SECURED LENS IAW SIP.
R1 DOOR EMER EXIT LIGHT COVER LOOSE. R & R COVER IAW MM.
OVERWING EMERGENCY EXIT SIGN BROKEN OFF. R&R EXIT SIGN IAW M/M.
LEFT HORIZ STAB LOWER IN-SPAR SKIN CRACKED AT L/E STA 138.7. REPAIRED SKIN PER SRM.
RIGHT HORIZ STAB LOWER IN-SPAR SKIN CRACKED AT L/E STA 101.9. REPAIRED SKIN PER SRM.
LEFT MLG W/W CENTER WING REAR SPAR VAPOR WEB IS CRACKED 15" LONG. REPAIRED VAPOR BARRIER LEFT MLG WHEEL WELL PER EA 1-A53-3376.
LEFT CENTER CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY, OP CHECK GOOD PER AMM.
RIGHT CENTER CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY, OP CHECK GOOD PER AMM.
LEFT EEPLS INOP AT ROW 21. REMOVED AND REPLACED BULB IAW AMM.
AFT EEPLS INOP. RELAMPED EEPLS PER M/M.
L/G EEPLS COVERS CRACKED BETWEEN ROW 1 TO ROW 11. REMOVED AND REPLACED COVERS PER M/M.
FWD GALLEY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M.
AFT EMERGENCY EXIT SIGN FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER AMM.
EEPLS STRIP CRACKED AT 1C. REMOVED AND REPLACED STRIP PER AMM.
LT EMERGENCY EXIT LIGHT COVER IN FLOOR ROW MISSING. INSTALLED COVER IAW M/M.
AFT SERVICE DOOR EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.
R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
DURING SCHEDULED HC2 CHECK, FOUND LT FWD EEPLS LENS CRACKED. REMOVED AND REPLACED LENS PER MM.
R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.
L1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
RT EMERGENCY EXIT SIGN BROKEN AT AFT CABIN. REMOVED AND REPLACED SIGN ASSY PER MM.
OVERWING EMERGENCY EXIT LIGHT LENS COVER LOOSE. SECURED COVER PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS LOOSE AT ROW 1. INSTALLED LENS PER MM.
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW BRACKET OUT OF ADJUST. ADJUSTED BRACKET PER MM.
FWD EEPLS END CAP MISSING. REMOVED AND REPLACED EEPLS PER MM.
AIR TURNBACK, A HYDRAULIC ELECTRIC PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED A SYSTEM HYDRAULIC PUMP PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVERS LOOSE AT ROW 1. INSTALLED COVERS MM.
DURING SCHEDULED MV1 CHECK, FOUND AFT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
EEPLS COVER MISSING AT ROW 1. INSTALLED COVER PER MM.
FWD EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM.
EEPLS INOP AT ROW 1. REPAIRED EEPLS WIRING PER MM.
R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT PER MM.