N473WN
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 | 2010-04-19 – 2010-04-19 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2010-04-19 – 2010-04-19 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
FOWARD ENTRY DOOR GIRT BAR HOOK NOT SECURED. REMOVED AND REINSTALLED FE DOOR SLIDE TO FOM IAW MT# 725-61-06. RESECURED HOOK IAW SRM 51-40-02.
G1 GALLEY DOOR ASSIST HANDLE DAMAGED. REMOVED AND REPLACED NEW ASSIST HANDLE IAW AMM 52-41-31-000-802 STEP E ;4) (A;B); AND AMM 52-41-31-400-802 STEP F 2) (C;D);[02].
DURING DVI AT MAIN CABIN SEAT TRACK AREA, LBL 24.75 & BS 727B FOUND ELONGATED HOLE AT THE BOTTOM OF THE STRUCTURE. REAMED ELONGATED HOLE UP TO 0.312'. REMOVED AND REPLACED DAMAGE SEAT TRACK BS 727B - 887, LBL 25, WL 208, IAW EA 26-153-00796-WIP2, SEAT TRACK FASTENER REPLACEMENT. LOCATION B OF LBL 24.75, CCN TTG8Q01BBGPZ; SRM 51-10-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A5300, REV A.
PASSENGER CABIN SEAT TRACK LBL 25 WL 208 FWD FASTNER AT BS 727B IS SHEARED. ATS QC HAS VERIFIED THAT THE FASTENER AT POSITION B AT 727B FLOORBEAM HAS BEEN INSTALLED CORRECTLY ON CENTERLINE OF TRACK AND SEAT TRACK TEETH.
CRACKED CROSSBEAM AT BS 540, BL 0 - RBL 25, WL 208. REMOVED CROSSBEAM IAW SRM 51-40-02. LOCATED AND DRILLED THE NEW CROSSBEAM IAW SRM 51-40-05, DWG 143A0060, REV-; INSTALLED THE CROSSBEAM IAW SRM 51-40-02, DWG 143A0060 REV-.
CRACKED CROSSBEAM, BS 540, BL 0 - LBL 25, WL 208. REMOVED THE CRACKED CROSSBEAM IAW SRM 51-40-02, INSTALLED A NEW CROSSBEAM IAW SRM 51-40-02, DWG 143A0060, REV A.
ONE CRACK NOTED ON LT HORIZONTAL STABILIZER LOWER SKIN BS 193.90, 10.5' FROM FWD EDGE; L: 0.3'. CRACKED WAS FOUND TO BE OUT OF LIMITS; REMOVED DAMAGE AND REPAIRED IAW SRM 55-10-01-2R-11.
FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 231XF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.
A CRACK NOTED ON THE RADIUS OF FWD SERVICE DOOR NUMBER 4 BEAM; LOCATED TWO INCHES FROM THE INBOARD EDGE; 0.3' IN LENGTH.<[01] FSD #4 BEAM REMOVED AND REPLACED ON ATS COMPONENTS WORK ORDER; JOB NUMBER 590825; SWA RO NUMBER P0083LDM-1;[02] VERIFIED CORRECTIVE ACTION 1
A CRACK NOTED ON THE RADIUS OF FWD SERVICE DOOR NR 5 BEAM, LOCATED HALF AN INCH FROM THE INBOARD EDGE, 0.5' IN LENGTH. FSD NR 5 BEAM, REMOVED AND REPLACED ON ATS COMPONENTS WORK ORDER, JOB NUMBER 590825; SWA RO NUMBER P0083LDM-1.
FWD SERVICE DOOR BOTH GIRT BAR RETAINERS ON SLIDE ARE LOOSE. REMOVED AND REPLACED FASTENERS ON FWD SERVICE DOOR BOTH GIRT BAR RETAINERS IAW SRM 51-40-02-0G-0; AND AIPC 25-66-00-14.
FO SIDE OVERWING EXIT DOOR LIGHT COVER LOOSE. OK TO CONTINUE IAW MEL 25-10-01. R & R THE OVERWING EXIT DOOR LIGHT LENS ASSY IAW AMM 25-21-20.
RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED. R & R RT HORIZONTAL STAB UPPER FWD SLIDING SEAL IAW AMM 53-31-31.
SEAT 11F RECLINES INTO EXIT ROW. ADJUSTED SEAT RECLINE LOCK IN REF TO AMM 25-22-00.
FWD GALLEY SERVICE DOOR UPPER ASSIST HANDLE IS LOOSE.<[01] RE SECURED FWD GALLEY SERVICE DOOR ASSIST HANDLE REF AMM 20-50-11.
FWD ENTRY DOOR UPPER ASSIST HANDLE IS LOOSE.<[01] RE SECURED FWD ENTRY DOOR UPPER ASSIST HANDLE REF AMM 20-50-11.
A/C GROUND AIR ACCESS DOOR WILL NOT OPEN OR CLOSE. <[01] 01 - REMOVED AND REPLACED PER [AMM 52-49-01-401-NG (FORWARD FAIRING ACCESS DOOR - REMOVAL/INSTALLATION - PERMANENT)].
AFT LH EMERGENCY SLIDE FELL OUT OF HOUSING<[01] CW REPACK OF L2 DOOR SLIDE PER MT 725-61-06
AFT MEGAPHONE INOP<[01] REMOVED AND REPLACED AFT GAL MEGAPHONE IAW AMM 25-64-00. NO FURTHER DEFECTS NOTED AT THIS TIME
R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER B737 AMM 33-51-04-960-801. TEST PASSED.;[02] VERIFIED STEP 1.
L/W O/B AFT FLAP; I/B AFT CORNER DISBONDED<[01] FINAL STATEMENT: REMOVED DAMAGE DELAMINATED UPPER AND LOWER SKINS ON L/W O/B AFT FLAP WEDGE I/B CORNER AS PER B737 SWRM 51-70-10-2R-4. PARAG. (7-A-1). INSTALLED HOT BONDER PERMANENT REPAIR AT L\W O\B AFT FLAP ON I\B CORNER UPPER AND LOWER SURFACE PER B737 SRM 57-53-01-2R-14 AND B737 SRM 51-70-10-2R-0PARAGRAPH (20.B) MATERIAL USED FIM ADHES AF 163-2K-06 PO#2053056 AND TOOL USED TEMPERATURE CONTROL ID:170006 DUE DATE 6/1/24.;[02] VERIFIED STEP 1;[03] CORRECTION: UPDATE MEASUREMENT TABLE
PANEL # 192F CORRODED WHERE DME#1 ATTACHES.<[01] REMOVED AND REPLACED PANEL #192F AS PER REFS B737 AMM 53-51-21-000-802 & AMM 53-51-21-400-802.
RIGHT HORIZONTAL STABILIZER I/B BALANCE LWR T/E ACCESS PANEL 343AB 2 AFT ANGLE METAL SEALS WITH BROW COVERS DETERIORATED..<[01] REMOVED AND REPLACED FWD AND AFT ANGLE METAL SEAL (PART#186A3004-4 AND 186A3004-18) FROM PANEL 343AB RIGHT HORIZONTAL STABILIZER I/B BALANCE LWR T/E PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED AND INSPECTED STEP#1.
LT IB FLAP UPPER SURFACE OF TRAILING EDGE WEDGE HAS DELAMINATION 33' FROM OB END AND ON LOWER SURFACE 4' FROM OB END. 8-58<[01] FINAL STATEMENT: REMOVED AND REPLACED WEDGE AT LT WING I/B FLAP T/E REF B737-700 SRM 51-40-02-0G-0 AND DWG# 113A2100.;[02] VERIFIED STEP 1
CORROSION ON LWR SURFACE OF CAPT FWD OB SEAT TRACK. 8-62<[01] REPLACED CAPT FWD OB SEAT TRACK. REF AMM 25-11-11-400-801. FIXTURE TRACK BC 170026.;[02] CORRECTION STEP 1: REMOVE AND REPLACE CAPT FWD OB SEAT TRACK REF SRM 51-40-02-0G-0 AND REF AMM 25-11-11-400-801.;[03] CORRECTION STEP 2: REMOVED AND REPLACED CAPT FWD OB SEAT TRACK REF SRM 51-40-02-0G-0 AND REF AMM 25-11-11-400-801.;[04] VERIFIED STEP 3
CORROSION ON LWR SURFACE OF F/O SEAT TRACK FWD OB. 8-66<[01] FINAL STATEMENT: REMOVED AND REPLACED F/O'S FWD O/B SEAT TRACK REF AMM 25-11-11-400-801 AND SRM 51-40-02-0G-0;[02] VERIFIED STEP 1
CORROSION ON LWR SURFACE OF CAPT SEAT TRACK AFT OB. 8-67<[01] CAPT SEAT TRACK AFT OB WILL BE REPLACED IN TC TTG8Q00SYP7V;[02] VERIFIED STEP 1
CORROSION ON LWR SURFACE OF CAPT SEAT TRACK AFT IB. 8-63<[01] REPLACED AFT IB CAPT SEAT TRACK REF SRM 51-40-02-0G-0 AND AMM 25-11-11-400-801.;[02] CORRECTION STEP #1. REMOVED AND REPLACED AFT IB CAPT SEAT TRACK REF SRM 51-40-02-0G-0 AND AMM 25-11-11-400-801.;[03] VERIFIED STEP 2; SEAT TRACK REPLACED.
CORROSION ON LWR SURFACE OF CAPT SEAT TRACK FWD IB. 8-64<[01] REPLACED FWD CAPT SEAT TRACK. REF AMM 25-11-11-400-801. FIXTURE TRACK BC 170026.;[02] CORRECTION STEP#1. REMOVED AND REPLACED FWD CAPT SEAT TRACK. REF AMM 25-11-11-400-801. REF SRM 51-40-02-0G-0.;[03] VERIFIED STEP 2
CORROSION ON LWR SURFACE OF CAPT SEAT TRACK FWD IB. 8-68<[01] CAPT SEAT TRACK FWD IB WILL BE REPLACED TC TTG8Q00SYP7C.;[02] VERIFIED STEP 1
CRACK FOUND AT I/B LOWER FASTENER HOLE OF S-18A WEB AT STA 727 RIGHT SIDE. CRACK FOUND AT I/B LOWER FASTENER HOLE OF S-18A WEB FITTING AT STA 727 RIGHT SIDE. ( NOTE: CRACK INDICATION FOUND AT WEB FITTING LOCATED AT LOWER SECTION OF THE WEB)<[01] REMOVED AND REPLACED CRACKED SPLICE FITTING AT S-18A AT STA 727 RIGHT SIDE AS PER SRM 51-40-02-0G-0 AND DWG#146A0062. TOOL USED: B/C 175290. CALIBRATION DUE DATE: 03-20-2025.;[02] RII---VERIFIED STEP#1.
ACCESS PANEL 193B HAS AN ELONGATED HOLE R/H SIDE ALF DOT 068<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #193B AS PER B737 SRM 51-70-04-2R-9 PARAG 4-D-M; MATERIAL USED: PO#2061896; PO#1690463; TOOL USED: HOT BONDER ID170006; DUE DATE 06-07-24.APPLIED TOPCOAT ON ACCESS PANEL 193B REF B-737 AMM 51-21-73-370-803;[02] VERIFIED STEP 1
FWD CEILING PANEL HAS EXIT LIGHT LENS BASE CRACKED AND LENS ATTACH BUTTON BROKED. 8-47<[01] REMOVED AND REPLACED HOUSING ASSY - EXIT SIGN AT CEILING ASSY - FWD CLOSE OUT LOWERED PER B737 AMM 33-51-01-960-801;[02] CORRECTION : REMOVED AND REPLACED HOUSING ASSY - EXIT SIGN AT CEILING ASSY - FWD CLOSE OUT LOWERED PER B737 AMM 33-51-01-960-802;[03] VERIFIED 1. AND 2.
GAP COVER 333AT SLIDING PANEL HAS ATTACH ANGLE CRACKED. 8-51<[01] REMOVED AND REPLACED BLADE ASSY AT GAP COVER PANEL 333AT REF B737-700 SRM 51-40-02-0G-0;[02] VERIFIED AND INSPECTED STEP#1.
AFT CARGO COMP. L/H Z CHANNEL BETWEEN ST 767 TO ST 787; LBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLE (18'). (228-004)<[01] REMOVED AND REPLACED NEW Z CHANNEL AT AFT CARGO COMP. BETWEEN STA 767 TO STA 787 LBL 21.PER B 737-700 DWG#146A7500 AND SRM 51-40-02-0G-0.;[02] VERIFIED AND INSPECTED STEP#1.
FASTENER HOLES CRACKED ON LEFT VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 19; 25 & 33 POSITION. FASTENER HOLES CRACKED ON LEFT VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 19 25 & 33 POSITION.<[01] REMOVED AND INSTALLED NEW LT VAPOR BARRIER UPPER SUPPORT ANGLE P/N # 111A1322U5 IN REF B 737-700 SRM 51-40-02-0G-0; 51-80-01-0G-0 AND DWG # 111A1322U5;[02] VERIFIED REPLACEMENT OF ANGLE STEP ONE.
AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 727E TO ST 747; LBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLE (10). (228-007) AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 727E TO ST 747 RBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLE (1'2'5'6'8'10 AND 14'). (228-007)<[01] FAULT TO BE ACCOMPLISHED ON TTG8Q00SV07E.;[02] VERIFIED STEP#1.
AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 727D TO ST 727E; LBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLES (6';7';8';16' AND 18). (228-006) AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 727D TO ST 727E RBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLES (6'7'8'16' AND 18). (228-006)<[01] FAULT TO BE ACCOMPLISHED ON TTG8Q00SV07E.;[02] VERIFIED STEP#1.
AFT CARGO COMP. L/H Z CHANNEL BETWEEN ST 727C TO ST 727D; LBL 21 HAVE LIGHT CORROSION AROUND 2 NUTPLATE HOLES (14' AND 18'). (228-001)<[01] FAULT TO BE ACCOMPLISHED ON TTG8Q00SUZCR.;[02] VERIFIED STEP#1.
AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 727C TO ST 727D; LBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLE (10). (228-005) AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 727C TO ST 727D RBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLE (10). (228-005)<[01] FAULT TO BE ACCOMPLISHED ON TTG8Q00SV07E.;[02] VERIFIED STEP#1.
AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 747 TO ST 767; RBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLES (6';10' AND 14'). (228-008)<[01] REMOVED AND REPLACED NEW Z CHANNEL AT AFT CARGO COMPARTMENT BETWEEN STA 727 TO STA 767 RBL 21. PER B737-700 SRM 51-40-02-0G-0 AND DWG#: 146A7500.;[02] VERIFIED AND INSPECTED STEP#1.
AFT CARGO COMP. L/H Z CHANNEL BETWEEN ST 727E TO ST 747; LBL 21 HAS LIGHT CORROSION AROUND NUTPLATE HOLE (10'). (228-003)<[01] FAULT TO BE ACCOMPLISHED ON TTG8Q00SUZCR.;[02] VERIFIED STEP#1.
CABIN FLOOR STRUCTURE; PANEL BREAK UPPER STRAP CRACKED AT STA. 540 LBL46<[01] REMOVED AND REPLACED PANEL BREAK ASSEMBLY AT STA 540. LBL 46 AS PER REF B737 SRM 51-40-02-0G-0.;[02] CORRECTING PREVIOUS STEP: REMOVED AND REPLACED PANEL BREAK ASSEMBLY UPPER PLATE AT STA 540. LBL 46 AS PER REF B737 SRM 51-40-02-0G-0 AND DWG 143A5240.;[03] VERIFIED 2 REPLACEMENT OF PANEL BREAK UPPER PLATE (STRAP).
SEAT TRACK AT LBL 24.75; STA 360+11 FOUND EXFOLIATED.<[01] REMOVED AND REPLACED EXFOLIATED SEAT TRACK BETWEEN STA 360+11 AND STA 480 LBL 24.75 AS PER B737-700 SRM 51-40-02-0G-0; DWG#: 141A5300 AND DWG#: 143A5300.;[02] VERIFIED AND INSPECTED STEP#1.
FOUND ELONGATED HOLES ON PANEL 551GB<[01] APPLIED REPAIR AT PANEL#551GB PER B737SRM 57-51-01-2R-1 51-70-04-2R-0PARAGRAPH(4.N.2) MATERIAL USED RESIN 3804 PO#2066364 FIBER GLASS PO#1690463. TOOL USED<BR>TEMPERATURE CONTROL ID:160354 DUE DATE:03/07/25 VACUMM GAGE ID:173240 DUE DATE:05/30/24.APPLIED TOP COAT AT PANEL#551GBON REPAIR AREA PER B737 AMM 51-21-99-300-802 PAINT USED PO#2055785.;[02] VERIFIED PANEL REPAIRED
CORROSION ON FLIGHT DECK FLOOR INTERCOSTAL UPPER SURFACE B.S. 268.25 B.L. 0 W.L. 208. (DOT 51-001)<[01] REMOVED AND REPLACED INTERCOSTAL (SUPPORT CHANNEL) AT FLIGHT DECK FLOOR BETWEEN STA 260 AND STA 270 BL 0 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A5210.;[02] VERIFIED INTERCOSTAL REPLACED; (SUPPORT CHANNEL).
LEFT RAM AIR DOOR LINKAGES ARE WORN. THE LINKAGE PIVOT FITTING IS CRACKED THROUGH.<[01] REMOVED AND REPLACED LT RAM AIR DOOR LINKAGES AND HARDWARE REF SRM 51-40-20-0G-0.;[02] VERIFIED STEP 1
FUSELAGE SUPPORT STRUCTURE CRACKED UNDER WTB PANEL #191AR<[01] REMOVED AND REPLACED SUPPORT STRUCTURE (FRAME) UNDER WTB PANEL# 191AR REF B737-700 SRM 51-40-02-0G-0 AND DWG# 116A3110 AND 116A3010.;[02] VERIFIED CORRECTIVE ACTION STEP 1
CABIN FLOOR PANEL #241DF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL# 241 DF; THIS PANEL WILL BE INSTALL ON TTG8Q00SBTUH.;[02] VERIFIED TTG8Q00SBTUH
CABIN FLOOR PANEL #241AF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL 241AF ; THIS PANEL WILL BE INSTALL ON TTG8Q00SBTUP;[02] VERIFIED STEP 1
FWD CARGO CUTOUT FWD SCUFF PLATE CRACKED<[01] RECEIVED WELDED FWD CARGO FWD SCUFF PLATE FOR OUTSIDE VENDOR J.L WELDIND INC PO#2059779 ; THIS SCUFF PLATE WILL BE INSTALL ON TTG8Q0037XG5;[02] ADD STEP #1 SRM 53-30-15-2R-1FOR WENDING;[03] VERIFIED SCUFF PLATE RECIEVED AND INSTALL TO BE ACCOMPLISHED ON TTG8Q0037XG5
CABIN FLOOR PANEL #231XF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL#231XF; THIS PANEL WILL BE INSTALL ON TTG8Q00SBTX5.;[02] VERIFIED TTG8Q00SBTX5.
# 1 ENGINE INLET COWL OUTER BARREL LOWER SKIN ANTI-ICE AIR GRILL OUTLET CRACKED AT 6 O'CLOCK. MARKED DOT 251-006<[01] ENG 1 INLET COWL WILL BE REPLACE USING TASK CARD 7111-E-17062-NG (REP - INLET COWL AND CRUSHABLE WEAR SPACERS) [TTG8Q00S71ZL];[02] VERIFIED STEP 1
LH HORIZONTAL FRONT UPPER SLIDING SEAL IS CRACKED.<[01] REMOVED LH HORIZONTAL FRONT UPPER SLIDING SEAL. REF AMM 53-31-31. INSTALLATION STILL REQUIRED.;[02] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-401 CONFIG 1-NG (STABILIZER TO BODY FRONT SPAR SLIDING SEAL - REMOVAL/INSTALLATION - PERMANENT)]
EXIT SIGN OVER FWD GALLEY DOOR FELL OFF<[01] 04 - REPAIRED PER [EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT)] OK TO CONTINUE PER EA -21-133-00720 MUST BE REPAIRED IN 30 FLT CYCLES
FORWARD SERVICE DOOR GIRT BAR BRACKET IS LOOSE<[01] RESECURED FORWARD SERVICE DOOR GIRTBAR BRACKET PER S.I.P
L1 SLIDE LOOSE; DID NOT DEPLOY<[01] RESECURED SLIDE FOR L1 DOOR IAW MT 725-61-06. A/C OK FOR SERVICE.
EMERGENCY EXIT ROW SIDEWALL LIGHT FO SIDE INOP<[01] R&R RH SIDE ROW EMERGENCY EXIT LAMP &FUSE REF A.M.M 33-51-01;OPS CHECK GOOD AT THIS TIME
FORWARD GALLEY EMERGENCY FLASHLIGHT-BLINKING POWER LIGHT INOP<[01] REMOVED AND REPLACED FWD GALLEY UPPER EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00; OPS CHECK GOOD.
FORWARD ENTRY DOOR. RIGHT GIRT BAR; REPORTED LOOSE. PERFORMED A VISUAL AND OPS CHECK OF FORWARD ENTRY DOOR GIRT BAR PER AMM 25-66-01 OPS CHECKS GOOD.<[01] PERFORMED A VISUAL AND OPS CHECK OF FORWARD ENTRY DOOR GIRT BAR PER AMM 25-66-01; OPS CHECKS GOOD.
FWD SVC DOOR GIRT BAR STOWAGE HOOK LOOSE<[01] RESECURED FWD SVC DOOR GIRT BAR STOWAGE HOOK RIVETS PER <BR>MM 25-66-00
EMER LIGHTS 9/ 12 CBA AND RH AFT OF WING GROUND ILLUMINATION LTS INOP<[01] R/R STA727C+13 EMER LIGHT POWER SUPPLY PER AMM 33-51 -06 OPS CHECK GOOD.
ROW 18 DEF EMERGENCY LIGHT LENS MISSING. / [01] REPLACED MISSING EMERGENCY LIGHT LENS IAM AMM 33-51-03
CRACK ANGLE FLOOR STRUCTURE AT BS 291.5 TO BS 294.5 AT LEVEL STR17R AT PASSENGER CABIN 2022-257561 / [01] REPLACED ANGLE FLOOR STRUCTURE AT BS 291.5 TO BS 294.5 AT LEVEL STR17R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG #141A8310 REV. -. SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED ANGLE FLOOR STRUCTURE AT BS 291.5 TO BS 294.5 AT LEVEL STR17R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG #141A8310 REV. -. RII ; SEE INDIVIDUAL SIGN OFFS BELOW.
MISSING MATERIAL FLOOR PANEL 221BF ON CORNER AREA AT FWD GALLEY AREA 2022-207360 / [01] REPLACED FLOOR PANEL 221BF AT FWD GALLEY AREA IAW B737-700 AMM 53-21-00-400-801;[02] REPLACED FLOOR PANEL 221BF AT FWD GALLEY AREA IAW B737-700 AMM 53-21-00-400-801
DELAMINATED FLOOR PANEL 231AF AT PASSENGER CABIN 2022-207399 REPAIRED FLOOR PANEL 231AF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1.
CORROSION FLOOR PANEL 221BF SLEEVE AT FWD GALLEY AREA (20 EA) 2022-207359 / [01] REPLACED FLOOR PANEL 221BF AT FWD GALLEY AREA IAW B737-700 AMM 53-21-00-400-801;[02] REPLACED FLOOR PANEL 221BF AT FWD GALLEY AREA IAW B737-700 AMM 53-21-00-400-801
PERFORATION FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2022-207311 / [01] FABRICATED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING: 453A2610 SHEET 9 REV E. MATERIAL USED P/N: 2024T3-071 P.O: 2021 210316.;[02] FABRICATED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING: 453A2610 SHEET 9 REV E. MATERIAL USED P/N: 2024T3-071 P.O: 2021 210316.
BROKEN SPAR LOWER BRAKET LOC ON OUTBOARD SIDE STRUT BOX AREA AT RT PYLON 2022-207304 / [01] REPLACED BRACKET AND FASTENERS LOCATED ON OUTBOARD SIDE STRUT BOX AREA AT RT PYLON IAW B737-700 SRM 52-40-02;[02] CORRECTED STEP 1<BR>REPLACED BRACKET AND FASTENERS LOCATED ON OUTBOARD SIDE STRUT BOX AREA AT RT PYLON IAW B737-700 SRM 51-40-02;[03] REPLACED BRACKET AND FASTENERS LOCATED ON OUTBOARD SIDE STRUT BOX AREA AT RT PYLON IAW B737-700 SRM 51-40-02
DETERIORATED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT 2022-207293 / [01] FABRICATED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING: 453A1610 SHEET 7 REV C MATERIAL USED P/N: 2024T3-071 P.O: 2021 210316.;[02] FABRICATED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING: 453A1610 SHEET 7 REV C MATERIAL USED P/N: 2024T3-071 P.O: 2021 210316.
DETERIORATED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT 2022-207314 / [01] FABRICATED FLOOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING 453A2610 SHEET 4 REV C MATERIAL USED: P/N: A90RG1W 48144 P.O: 2021 237448;[02] FABRICATED FLOOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING 453A2610 SHEET 4 REV C MATERIAL USED: P/N: A90RG1W 48144 P.O: 2021 237448
CRACK ON FLOOR PANEL 242XF OF AFT GALLEY AREA 2022-207323 / [01] REPLACED FLOOR PANEL 242XF OF AFT GALLEY AREA I.A.W B737-700 AMM 53-21-00-400-891 STEP 3.F ITEM 10 AND FLOOR PANEL 242XF WILL BE INSTALLED ON CARD: TTG8Q00B8SWC;[02] CERTIFIED WORK PERFORMED.
CRACK FUEL TANK INDICATOR HOUSING ACCESS PANEL 532CB AT LT WING 2022-207272 / [01] REMOVED AND REPLACED MEASURING STICK 3 AND HOUSING IAW B737-700 AMM:28-44-11-400-801 TOOL USED:TORQUE P/N:QD1R50 S/N:0416041420 D/D:22/FEB/23;[02] REMOVED AND REPLACED MEASURING STICK 3 AND HOUSING IAW B737-700 AMM:28-44-11-400-801 TOOL USED:TORQUE P/N:QD1R50 S/N:0416041420 D/D:22/FEB/23<BR>NO LEAK WAS FOUND;[03] CORRECTED STEP 1 AND 2 <BR>REMOVED AND REPLACED MEASURING STICK 3 AND HOUSING IAW B737-700 AMM:28-44-11-400-801 TOOL USED:TORQUE P/N:QD1R50 S/N:0416041420 D/D:22/FEB/23 <BR>NO LEAK WAS FOUND <BR>SEE INDIVIDUAL SIGN OFF BELOW;[04] CERTIFIED STEP 3 COMPLETE <BR>LEAK NOT FOUND
CRACK PLATE ASSY TRAILING EDGE ACCESS PANEL 542 BB LT WING 2022-207265 / [01] REPLACED PLATE ASSY TRAILING EDGE ACCESS PANEL 542 BB LT WING IAW B737-700 SRM 51-40-02-0G-0;[02] REPLACED PLATE ASSY TRAILING EDGE ACCESS PANEL 542 BB LT WING IAW B737-700 SRM 51-40-02-0G-0
CRACK PLATE ASSY TRAILING EDGE OUTBOARD CENTER EDGE ACCESS PANEL 642BB RT WING 2022-207270 / [01] REPLACED PLATE ASSY AND FASTENERSON TRAILING EDGE OUTBOARD CENTER EDGE ACCESS PANEL 642BB RT WING IAW B737-700 SRM 51-40-02-0G-0;[02] REPLACED PLATE ASSY AND FASTENERSON TRAILING EDGE OUTBOARD CENTER EDGE ACCESS PANEL 642BB RT WING IAW B737-700 SRM 51-40-02-0G-0
CRACK PLATE ASSY TRAILING EDGE OUTBARD EDGE ACCESS PANEL 542BB LT WING 2022-207267 / [01] REPLACED PLATE ASSY TRAILING EDGE OUTBARD EDGE ACCESS PANEL 542BB LT WING IAW B737-700 SRM 51-40-02-0G-0;[02] REPLACED PLATE ASSY TRAILING EDGE OUTBARD EDGE ACCESS PANEL 542BB LT WING IAW B737-700 SRM 51-40-02-0G-0
ELONGATED HOLE BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT 2022-207268 / [01] FABRICATED BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING #453A2510 SHEET: 5 REV: -; MATERIAL USED P/N: A60SG4W PO: 2022-104980;[02] TASK COMPLETED
CRACK PLATE ASSY TRAILING EDGE OUTBOARD FWD EDGE ACCESS PANEL 642BB RT WING 2022-207269 / [01] REPLACED PLATE ASSY TRAILING EDGE OUTBOARD FWD EDGE ACCESS PANEL 642BB RT WING IAW B737-700 SRM 51-40-02-0G-0;[02] REPLACED PLATE ASSY TRAILING EDGE OUTBOARD FWD EDGE ACCESS PANEL 642BB RT WING IAW B737-700 SRM 51-40-02-0G-0
ELONGATED HOLE BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT 2022-207266 / [01] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING 453A2510 SHEET 12 REV - MATERIAL USED: A60SG4W 60144 P.O: 2022 104980;[02] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING 453A2510 SHEET 12 REV - MATERIAL USED: A60SG4W 60144 P.O: 2022 104980
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AT BL0 FWD GALLEY AND LAV 2022-207232 / [01] REPLACED NEW WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AT BL0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV - AND SRM 51-10-02 PARAGRAPH 9;[02] CORRECTIVE STEP 1<BR>REPLACED NEW WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AT BL0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV - AND SRM 51-10-02 PARAGRAPH 9. SEE INDIVIDUAL SIGNSOFF BELOW.;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 243 LOWER SURFACE AT RT WING 2022-207218 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 243 LOWER SURFACE AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2001; SHEET 30; REV. A.;[02] TASK COMPLETED
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 243 LOWER SURFACE AT LT WING 2022-207199 / [01] REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE LOCATED AT LEVEL ORSS 243 LOWER SURFACE AT LT WING IAW B737-700 SRM 51-40-02 AD DRAWING 115A2001 SHEET 30 REV. A. PURCHASE ORDER 2022-144386. TOOL USED CALIPER P/N 500-197-30; S/N A21043164; DUE DATE: 01/SEP/22;[02] CORRECTED STEP 1<BR>REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE LOCATED AT LEVEL ORSS 243 LOWER SURFACE AT LT WING IAW B737-700 SRM 51-40-02; SRM B737-700 51-10-02 AND DRAWING 115A2001 SHEET 30 REV. A. PURCHASE ORDER 2022-144386. TOOL USED CALIPER P/N 500-197-30; S/N A21043164; DUE DATE: 01/SEP/22;[03] TASK COMPLETED
CRACK SUPPORT ANGLE LOWER SURFACE REAR SPAR LOCATED AT LEVEL ORSS 281 AND ORSS 329 LT WING 2022-207190 / [01] REPLACED SUPPORT ANGLE ( BEAM ASSY ) P/N : 115A3758-9 PO: 2022 143854 LOC. LOWER SURFACE REAR SPAR AT LEVEL ORSS 281 AND ORSS 329 LT WING IAW B737-700 SRM 51-10-02 ; 51-40-02 AND DWG # 115A3700 REV :- DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM AND CRACK MEASURE IS: 0.700? TOOL USED; DIGITAL CALIPER P/N: 500-197-30 S/N:A21143429 DUE DATE: 11-OCT-22;[02] REPLACED SUPPORT ANGLE ( BEAM ASSY ) P/N : 115A3758-9 PO: 2022 143854 LOC. LOWER SURFACE REAR SPAR AT LEVEL ORSS 281 AND ORSS 329 LT WING IAW B737-700 SRM 51-10-02 ; 51-40-02 AND DWG # 115A3700 REV.
CRACK ACCESS PANEL 661AB HOLES AT RT WING 2022-207241 / [01] TOOL USED: CALIPER P/N:500-464 S/N:15331926 DUE DATE 28-SEP-22;[02] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18175478 DUE DATE:05-AUG-22.;[03] TOOL USED:SCALE P/N: SCA-301 S/N:AE-412127 DUE DATE:14-MAR-23.;[04] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 38200035 ; DUE DATE: 08-SEP-22;[05] REPAIRED ACCESS PANEL 661AB AT RT WING IAW B737-700 SRM 51-70-04-2R-09 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] TASK COMPLETED
CRACK ACCESS PANEL 661BB AT RT WING 2022-207240 / [01] TOOL USED:CALIPER P/N:500-464 S/N:15331926 DUE DATE 28-SEP-22;[02] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18175478 DUE DATE:05-AUG-22;[03] TOOL USED:SCALE P/N: SCA-301 S/N:AE-412127 DUE DATE:14-MAR-23.;[04] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18196127 DUE DATE:16-JAN-23.;[05] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 38200035 ; DUE DATE: 08-SEP-22;[06] REPAIRED ACCESS PANEL 661BB AT RT WING IAW B737-700 SRM 51-70-04-2R-09 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] TASK COMPLETED
CRACK ACCESS PANEL HOLES 561AB AT LT WING 2022-207242 / [01] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18175478 DUE DATE:05-AUG-22.;[02] TOOL USED:SCALE P/N: SCA-301 S/N:AE-412127 DUE DATE:14-MAR-23.;[03] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 38200035 ; DUE DATE: 08-SEP-22;[04] REPAIRED ACCESS PANEL 561AB AT LT WING IAW B737-700 SRM 51-70-04-2R-09 REPAIR 9 TOOL USED: CALIPER P/N: 500-464; S/N: 15331932; DUE DATE: 26-OCT-22. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] TASK COMPLETED
CRACK ACCESS PANEL HOLES 561BB AT LT WING 2022-207243 / [01] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18175478 DUE DATE:05-AUG-22.;[02] TOOL USED:SCALE P/N: SCA-301 S/N:AE-412127 DUE DATE:14-MAR-23.;[03] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18196127 DUE DATE:16-JAN-23.;[04] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 38200035 ; DUE DATE: 08-SEP-22;[05] REPAIRED ACCESS PANEL 561BB AT LT WING IAW B737-700 SRM 51-70-04-2R-09 REPAIR 09. TOOL USED: CALIPER P/N 500-464; S/N: 15331932; DUE DATE: 26-OCT-22. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] JOB COMPLETED
CORROSION ON FLOOR BEAM 986.5 RBL 5 AND WL 208. AFT GALLEY AREA 2022-207214 / [01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN:45MG; SN: 130064101; DUE DATE: 11-MAY-22;[02] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022235; DUE DATE: 03-JUN-22.;[03] TOOL USED P/N FPK-PRO-104 S/N PRO-3384 DUE DATE: 24 MAY 22;[04] REPAIRED FLOOR BEAM BS 986.5 LOC. AT THE RBL 1 TO RBL 9 AND WL 208.1 AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 ALTERNATIVE 1; PARAGRAPH 4; TABLE 201 FIGURE 202; SEE INDIVIDUAL SIGN OFFS BELLOW.;[05] JOB COMPLETE
CORROSION FLOOR BEAM LOCATED BS344 AT LBL9 AND WL208.1 AT FWD GALLEY AREA 2022-207215. [05] REPAIRED FLOOR BEAM BTW BS 328 TO BS 360 LBL 11.10 WL208.1 AT FWD GALLEY AREA I.A.W B737-700 SRM 53-10-51-2R-9 REPAIR 9 REPAIR IS CATEGORY: A DOES NOT REQUIRE INSPECTIONS SEE INDIVIDUAL SING OFF BELOW.;[06] REPAIRED FLOOR BEAM BTW BS 328 TO BS 360 LBL 11.10 WL208.1 AT FWD GALLEY AREA I.A.W B737-700 SRM 53-10-51-2R-9 REPAIR 9 REPAIR IS CATEGORY: A DOES NOT REQUIRE INSPECTIONS;
CORROSION ON FLOOR BEAM 986.5 BTW RBL 39 TO RBL 44 AND WL 208.1 AFT GALLEY AREA 2022-207216 / [01] TOOL USED PN:35DL; SN:091419910; DUE DATE:26-JAN-23.;[02] ET TOOL USED: PN: PHASEC 3D; SN: 587435 /03; DUE DATE: 22 -DEC -22;[03] REPAIRED FLOOR BEAM 986.5 BTW RBL 30.00 TO RBL 50.00 AND AT WL 208.1 AFT GALLEY AREA IAW EA 22-153-01411-WIP1 BARCODE (TTG8Q00CEYZ4) AND EA 22-153-01411 BARCODE (TTG8Q00CL5RG) SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED FLOOR BEAM 986.5 BTW RBL 30.00 TO RBL 50.00 AND AT WL 208.1 AFT GALLEY AREA IAW EA 22-153-01411-WIP1 BARCODE (TTG8Q00CEYZ4) AND EA 22-153-01411 BARCODE (TTG8Q00CL5RG) RII. SEE INDIVIDUAL SIGN OFF BELOW.
CORROSION FLOOR BEAM LOCATED BS328 AT RBL19 TO RBL22 AND WL208.1 AT FWD GALLEY AREA 2022-207225. REPAIRED FLOOR BEAM LOCATED BS328 AT LBL6 TO RBL60 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 ALTERNATIVE 2. THIS REPAIR IS CATEGORY A.
CORROSION FLOOR BEAM LOCATED BS328 AT RBL42 AND WL208.1 AT FWD GALLEY AREA 2022-207223 ; REPAIRED FLOOR BEAM LOCATED BS328 AT LBL 6 TO RBL 60 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 ALTERNATIVE 2 THIS REPAIR IS CATEGORY A.THIS REPAIR IS DOCUMENTED ON FAULT TTG8Q00C3N3L.
CORROSION FLOOR BEAM LOCATED BS294.5 AT RBL9 TO RBL13 AND WL208.1 AT FWD GALLEY AREA 2022-207229 REPAIRED FLOOR BEAM LOC. BS294.5 AT RBL9 TO RBL13 AND WL208.1 AT FWD GALLEY AREA; IAW SRM 53-10-51-2R-16 THIS REPAIR IS CATEGORY A. REPAIRED FLOOR BEAM LOC. BS294.5 BTW RBL41 TO LBL40 AND WL208.1 AT FWD GALLEY AREA; IAW SRM 53-10-51-2R-16 ALTERNATIVE A; THIS REPAIR IS CATEGORY A;
CORROSION INNER CHORD LOCATED BS328 AT RBL58 AND WL208.1 AT FWD GALLEY AREA 2022-207221 / [01] TOOL USED PN. 35DL; SN. 091419910; DUE DATE. 26-JAN-23;[02] REPLACED INNER CHORD LOC. BS328 AT RBL58 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 25 REV: B. SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED INNER CHORD LOC. BS328 AT RBL58 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 25 REV: B. SEE INDIVIDUAL SIGN-OFF BELOW. COMPLETED RII
CORROSION ANGLE - SUPPORT LOCATED BS312 TO BS328 AT RBL59 AND WL208.1 AT FWD GALLEY AREA 2022-207238. REPLACED ANGLE - SUPPORT LOCATED AT INNER CHORD BTW BS294.5 TO BS328 AT RBL59 AND WL208.1 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8310 REV:- SHEET 23.
CORROSION FLOOR BEAM LOCATED BS312 AT LBL16 AND WL208.1 AT FWD GALLEY AREA 2022-207236 / [01] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 60009161631 AND DUE DATE: 03-DEC-22.;[02] REPAIRED FLOOR BEAM LOCATED BS312 AT LBL16 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-17; REPAIR 17. THIS REPAIR IS CATEGORY A. SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPAIRED FLOOR BEAM LOCATED BS312 AT LBL16 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-17; REPAIR 17. THIS REPAIR IS CATEGORY A. SEE INDIVIDUAL SIGNOFF BELOW... RII ITEM
CORROSION ON FLOOR BEAM 986.5 LBL 44 AND WL 208.1 AFT GALLEY AREA 2022-207220 / [04] REPAIRED FLOOR BEAM 986.5 LBL 55.8 BTW LBL 64 AND WL 208.1 AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6 TABLE 204 FIGURE: 205. THIS REPAIR IS CATEGORY AND NOT REQUIRED ANY INSPECTIONS SEE INDIVIDUAL SING OFF BELOW.;[05] CORRECTED STEP 4 REPAIRED FLOOR BEAM 986.5 LBL 55.8 BTW LBL 64 AND WL 208.1 AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6 TABLE 204 FIGURE: 205. THIS REPAIR IS CATEGORY A AND NOT REQUIRED ANY INSPECTIONS
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS294.5 TO BS312 AT RBL15 FWD GALLEY AND LAV 2022-207227 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS294.5 TO BS312 AT RBL15 FWD GALLEY IAW B737-700 SRM 51-10-02 AND B737-700 SRM 51-40-02 AND DRAWING DRAWING 141A5400 REV A AND DRAWING 141A5410 REV A;[02] CORRECTED STEP <BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS294.5 TO BS312 AT RBL15 FWD GALLEY IAW B737-700 SRM 51-10-02 AND B737-700 SRM 51-40-02 AND DRAWING DRAWING 141A5400 REV A AND DRAWING 141A5410 REV A .SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS344 TO BS360 AT RBL32 FWD GALLEY AND LAV 2022-207219 REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS344 TO BS360 AT RBL32 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 39 AND SRM 51-10-02 PARAGRAPH 9.REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS344 TO BS360 AT RBL32 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 33 AND SRM 51-10-02 PARAGRAPH 9.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS312 TO BS328 AT LBL46 FWD GALLEY AND LAV 2022-207233 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS312 TO BS328 AT LBL46 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 141A5400 REV:-;[02] CORRECTIVE STEP 1<BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS312 TO BS328 AT LBL46 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 141A5400 REV:-. SEE INDIVIDUAL SIGNSOFF BELOW.;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW
CRACK INNER CHORD LOCATED BS303.9 AT LBL55 AT FWD GALLEY AREA 2022-207235 / [01] REPLACED INNER CHORD LOCATED BTW BS 360 AND BS 270 AT LBL55 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02 DWG:141A8110 SHEET:9 REV:A P/N: 654A0004-1073 P.O: 2023000639 SEE INDIVIDUAL SING OFFS BELOW;[02] JOB CERTIFIED AS RII.
CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS312 TO BS328 AT RBL30 FWD GALLEY AND LAV 2022-207226 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS312 TO BS328 AT RBL30 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 141A5400 REV:-;[02] CORRECTIVE STEP 1<BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS312 TO BS328 AT RBL30 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 141A5400 REV:-. SEE INDIVIDUAL SIGNSOFF BELOW.;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW
CRACK FRAME ON BS 312 AT LEVEL STR6L FWD GALLEY AND LAV 2022-207130 / [01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138203; DUE: 11-APR-23;[02] INSPECTION REJECT IN STEP 12 SEE TTG8Q00CDDUS;[03] REPAIRED FRAME LOC. ON BS 312 AND BTW STR 5L TO STR 6L FWD GALLEY AND LAVATORY IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 PARAGRAPH 4; FIGURE 203. MATERIAL USED P/N: 7075T0-0.063?; P/O: 2022-124059 1. SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED FRAME LOC. ON BS 312 AND BTW STR 5L TO STR 6L FWD GALLEY AND LAVATORY IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 PARAGRAPH 4; FIGURE 203. MATERIAL USED P/N: 7075T0-0.063?; P/O: 2022-124059 1. RII .SEE INDIVIDUAL SIGN OFF BELOW.
BROKEN LAVATORY B ASSY EMERGENCY EXIT LIGHT AT AFT GALLEY AREA 2022-207125 / [01] REPLACED LAVATORY B ASSY EMERGENCY EXIT LIGHT AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 P/N 702409DME1007;[02] REPLACED LAVATORY B ASSY EMERGENCY EXIT LIGHT AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 P/N 702409DME1007
INOP EMERGENCY EXIT LIGHT BATTERY BTW BS 597 TO BS 616 LT SIDE AT PASSENGER CABIN (1EA) 2022-207119 / [01] REPLACED EMERGENCY EXIT LIGHT BATTERY BTW BS 597 TO BS 616 LT SIDE AT PASSENGER CABIN; TEST IS OK IAW AMM 33-51-06-960-805.;[02] TASK COMPLETED <BR><BR>TEST OK
INOP LOWERED CEILING PANEL BATTERY EMERGENCY EXIT LIGHT AT AFT GALLEY AREA (2EA) 2022-207118 / [01] REPLACED BATTERY EMERGENCY EXIT LIGHT AT AFT GALLEY AREA (2EA); TEST IS OK IAW AMM 33-51-06-960-805.;[02] TASK COMPLETED<BR><BR>TEST OK
CRACK LEADING EDGE SUPPORT ANGLE LOC BTW STR 2RT AND STR 2LT BS 1016 AT VERTICAL STABILIZER 2022-207126 / [01] REPLACED SUPPORT ANGLE (SPRING) LOC. BTW STR 2R AND STR 2L BS 1016 AT VERTICAL STABILIZER IAW: B737-700 SRM 51-40-02 AND DWG 176A3101; SHEET: 4; REV: - AND DWG: 176A3001; SHEET: 23; REV: D. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ANGLE (SPRING) LOC. BTW STR 2R AND STR 2L BS 1016 AT VERTICAL STABILIZER IAW: B737-700 SRM 51-40-02 AND DWG 176A3101; SHEET: 4; REV: - AND DWG: 176A3001; SHEET: 23; REV: D.RII . SEE INDIVIDUAL SIGN OFF BELOW
CRACK FRAME STUB LOCATED BS 294.5 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN 2022-207148 / [01] REPLACED FRAME STUB LOCATED BS 294.5 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED FRAME STUB LOCATED BS 294.5 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGNOFF BELOW.. RII ITEM
CRACK STUB FRAME LOCATED 294.5 AT LEVEL STR17R AT PASSENGER CABIN 2022-207142 / [01] REPLACED STUB FRAME LOC. BS 294.5 AT LEVEL STR 15R TO STR 17R AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM:9 AND DWG:141A8370 SHEET:9 REV:D AND DWG:141A8430 SHEET:4 REV:B;[02] CORRECTED STEP 1: REPLACED STUB FRAME LOC. BS 294.5 AT LEVEL STR 15R TO STR 17R AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM:9 AND DWG:141A8370 SHEET:9 REV:D AND DWG:141A8430 SHEET:4 REV:B;[03] REPLACED STUB FRAME LOC. BS 294.5 AT LEVEL STR 15R TO STR 17R AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM:9 AND DWG:141A8370 SHEET:9 REV:D AND DWG:141A8430 SHEET:4 REV:B
CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2022-207141 / [01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV: -. ;[02] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV: -. SEE INDIVIDUAL SING-OFF BELOW.<BR>RII;[03] CORRECTED STEP 1.REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW SRM B737-700 51-10-02; SRM B737-700 51-40-02 AND DWG 141A1110 SHEET 18 REV: -. ;[04] CORRECTED STEP 2. REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW SRM B737-700 51-10-02; SRM B737-700 51-40-02 AND DWG 141A1110 SHEET 18 REV: -.
CRACK WEB INTERCOSTAL LOCATED BETWEEN BS294.5 TO BS303.9 STR16L AT FWD GALLEY AREA 2022-207128 / [01] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101U102020 DUE DATE 01-JUN-22;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 190023010 DUE DATE: 14-FEB-23;[03] REPLACED WEB INTERCOSTAL LOCATED BETWEEN BS294.5 TO BS303.9 STR16L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A8180 SHEET 27 REV C. SEE INDIVIDUAL SING-OFFS BELOW.;[04] REPLACED WEB INTERCOSTAL LOCATED BETWEEN BS294.5 TO BS303.9 STR16L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A8180 SHEET 27 REV C. SEE INDIVIDUAL SING-OFFS BELOW.<BR>RII
CRACK STRINGER BETWEEN BS294.5 TO BS303.9 STR15L AT PASSENGER CABIN 2022-207139 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN:210136503; DUE DATE: 11-APR-23;[02] TOOL MEASUREMENT ULTRASONIC THICKNESS USED P/N: 45MG S/N: 130060401 DUE DATE: 26-JAN-23.;[03] REPAIRED STRINGER BETWEEN BS294.5 TO BS303.9 STR15L AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; THIS REPAIR IS CATEGORY A. NO FURTHER ACTION OR INSPECTION REQUIRED. SEE INDIVIDUAL SIGNOFF BELOW;[04] REPAIRED STRINGER BETWEEN BS294.5 TO BS303.9 STR15L AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; THIS REPAIR IS CATEGORY A. NO FURTHER ACTION OR INSPECTION REQUIRED. SEE INDIVIDUAL SIGNOFF BELOW AS RII
CRACK STRINGER 16L BETWEEN BS294.5 TO BS303.9 AT PASSENGER CABIN 2022-207127 / REPAIRED STRINGER 16L BETWEEN BS294.5 TO BS303.9 AT PASSENGER CABIN B737-700 SRM 53-00-03-2R-1 REPAIR 1; THIS REPAIR IS CATEGORY A. NO FURTHER ACTION OR INSPECTION REQUIRED. REPAIRED STRINGER 16L BETWEEN BS277 TO BS303.9 AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; THIS REPAIR IS CATEGORY A. NO FURTHER ACTION OR INSPECTION REQUIRED.
RUST ON AFT SERVICE DOOR GIRT BAR FITTING BRACKET AT PASSENGER CABIN (1EA) 2022-207120 / [01] REPLACED ON AFT SERVICE DOOR GIRT BAR FITTING BRACKET AT PASSENGER CABIN (1EA) IAW B737-700 AMM 25-66-02-400-801;[02] REPLACED ON AFT SERVICE DOOR GIRT BAR FITTING BRACKET AT PASSENGER CABIN (1EA) IAW B737-700 AMM 25-66-02-400-801
CRACK ANGLE LOCATED TRAILING EDGE AT LEVEL ORSS 276 AT LT WING 2022-207038 / [01] REPLACED ANGLE LOCATED TRAILING EDGE AT LEVEL ORSS 276 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9;[02] TASK COMPLETED
CRACK WEB LOCATED BETWEEN ORSS 261 AND ORSS 280 TRAILING EDGE AT RT WING 2022-207020 / [01] INSTALLED NEW WEB WITH FASTENERS LOCATED BETWEEN ORSS 261 AND ORSS 280 TRAILING EDGE AT RT WING I.A.W B737-700 SRM 51-40-02 AND DWG 115A2512 REV: A.;[02] CORRECTED STEP 1<BR>REPLACED WEB LOCATED BETWEEN ORSS 261 AND ORSS 280 TRAILING EDGE AT RT WING I.A.W B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 115A2512 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED WEB LOCATED BETWEEN ORSS 261 AND ORSS 280 TRAILING EDGE AT RT WING I.A.W B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 115A2512 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.
CRACK ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 RT WING 2022-207017 / [01] REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 RT WING IAW: B737-700; SRM 51-40-02 AND SRM 51-10-02; ITEM 9; SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 RT WING IAW: B737-700; SRM 51-40-02 AND SRM 51-10-02; ITEM 9; SEE INDIVIDUAL SIGN OFF BELOW.
CRACK INDICATION ON FWD SERVICE DOOR BEAR STRAP BTW BS 291.5 TO BS 294.5 AT LEVEL S-8R TO S-9R PASSENGER CABIN 2022-207062 PERFORMED REOAIR IWA EA 22-153-01299;[06] PERFORMED PERMANENT REPAIR ON FWD SERVICE DOOR BEAR STRAP BTW BS 291.5 TO BS 294.5 AT LEVEL S-8R TO S-9R PASSENGER CABIN IAW EA 22-153-01299. SEE INDIVIDUAL SIGNS OFF BELOW. RII;[07] PERFORMED PERMANENT REPAIR ON FWD SERVICE DOOR BEAR STRAP BTW BS 291.5 TO BS 294.5 AT LEVEL S-8R TO S-9R PASSENGER CABIN IAW EA 22-153-01299.
CRACK CORRUGATED PLATE LOCATED AT LEVEL ORSS261 TRAILING EDGE AT LT WING 2022-207040 / [01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS261 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-20-01 AND DWG 115A2001-59 SHEET 29 REV -;[02] REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS261 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-20-01 AND DWG 115A2001-59 SHEET 29 REV -
CRACK ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 UPPER SURFACE LT WING 2022-207037 / [01] REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 UPPER SURFACE LT WING IAW SRM B737-700 51-10-02 ITEM 9 AND 51-40-02;[02] REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 UPPER SURFACE LT WING IAW SRM B737-700 51-10-02 ITEM 9 AND 51-40-02
CRACK ANGLE LOCATED TRAILING EDGE AT ORSS 271 APPROX LOWER SURFACE AT LT WING 2022-207039 / [01] REPLACED ANGLE AND FASTENERS LOCATED ON TRAILING EDGE AT ORSS 271 APPROX LOWER SURFACE AT LT 2WING IAW B737-700 SRM 51-40-02;[02] CORRECTED STEP 1: REPLACED ANGLE AND FASTENERS LOCATED ON TRAILING EDGE AT ORSS 271 APPROX LOWER SURFACE AT LT WING IAW B737-700 SRM 51-40-02 SRM 51-10-02;[03] CERTIFIED WORK PERFORMED.
CRACK CORRUGATED PLATE LOCATED AT LEVEL ORSS 261 TRAILING LOWER EDGE AT RT WING 2022-207023 / [01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS 261 TRAILING LOWER EDGE AT RT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 115A2001; SHEET 29; REV -.;[02] TASK COMPLETED
CRACK LEADING EDGE SKIN SLAT ACTUATOR 2 AT LT WING 2022-206875 / [01] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 190023010 AND DUE DATE: 14-FEB-23.;[02] TOOL USED RADIUS GAUG P/N: 2204A3 S/N: AE-408652 DUE DATE: 29-JAN-23;[03] REPAIRED LEADING EDGE SKIN SLAT ACTUATOR 2 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1 FIGURE 202. SEE INDIVIDUAL SIGNOFF BELOW.;[04] REPAIRED LEADING EDGE SKIN SLAT ACTUATOR 2 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1 FIGURE 202. SEE INDIVIDUAL SIGNOFF BELOW. COMPLETED RII
CRACK INDICATIONS FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 10.0 INCH FROM REAR SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.200 INCH 2022-206920 REPAIRED RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 10.0 INCH FROM REAR SPAR; INBD SIDE OF RIB IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11 FIGURE 204 SHEET 2 DETAIL:B AND SRM 51-40-02.THIS REPAIR IS CATEGORY B. CRACK LENGTH IS 1.200 INCH. [03] REPAIRED RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 10.0 INCH FROM REAR SPAR; INBD SIDE OF RIB IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11 FIGURE 204 SHEET 2 DETAIL:B AND SRM 51-40-02.THIS REPAIR IS CATEGORY B. CRACK LENGTH IS 1.200 INCH.
CRACK INDICATIONS FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 18.0 INCH FROM REAR SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.250 INCH 2022-206921 REPAIRED HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 18.0 INCH FROM REAR SPAR; INBD SIDE OF RIB. IAW B37-700 SRM 55-10-01-2R-11 REPAIR 11. THIS REPAIR IS CATEGORY B. SEE INDIVIDUAL SIGNOFF BELOW.;[04] REPAIRED HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 18.0 INCH FROM REAR SPAR; INBD SIDE OF RIB. IAW B37-700 SRM 55-10-01-2R-11 REPAIR 11. THIS REPAIR IS CATEGORY B.
CRACK ON STRAP LOCATE BTW BS767 TO BS787 AND STR25L TO STR25R AT AFT CARGO COMPARTMENT 2022-206781 REPLACED STRAP LOCATE BTW BS767 TO BS787 AND STR25L TO STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 146A7500-16. P/N: 146A9401-4ATSMRO PO:2022 142949.REPLACED STRAP LOCATE BTW BS767 TO BS787 AND STR25L TO STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 146A7500-16. P/N: 146A9401-4ATSMRO PO:2022 142949.REPLACED STRAP LOCATE BTW BS767 TO BS787 AND STR25L TO STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 146A7500-16. P/N: 146A9401-4ATSMRO PO:2022 142949.
CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2022-206730 / [01] TOOL USED DIGITAL CALIPER P/N 500-196-30; S/N A21033522; DUE DATE 01-NOV-22.;[02] REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.
WING TO BODY PANEL 193D HAD FRETTING DAMAGE ; / [01] R AND R PANEL 193D PER AMM 53-51-21
PASSENGER CABIN SEAT TRACK LBL 24 STA 685+41' WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION ON UPPER AND LOWER SURFACES OF SEAT TRACK STA 685+41 LBL24 AND PERFORMED 10X MAGNIFYING GLASS I/A/W SRM 51-10-02-0G-0 VERIFIED MATERIAL LOSS AT SEAT TRACK STA 685+41 LBL 24 ON BOTTOM OF SEAT TRACK LOSS OF .015 MAXIMUM LOSS IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED MATERIAL ON UPPER SURFACE OF SEAT TRACK LOSS OF .012 MAXIMUM CLEANUP IS .020 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE VERIFIED STEPS 1. THRU 3. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.
PASSENGER CABIN SEAT TRACK LBL 45 STA 727C+4' WL 208 HAS CORROSION ON LOWER SURFACE<REMOVED CORROSION FROM SEAT TRACK STA 727C + 4' LOWER SURFACE IAW SRM 51-40-02-0G-0. USED 10X MAGNIFICATION GLASS. VERIFIED MATERIAL LOSS ON SEAT TRACK STA 727C + 4' LBL 45 ON LOWER SURFACE IAW SRM 53-00-52-1A-1. DEPTH .02' MAX ALLOWWED .040'. AAR TOOL 36307 CAL DATE DUE 06/14/22. VERIFIED STEPS 1. AND 2. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.
PASSENGER CABIN SEAT TRACK LBL 24 STA 616+17' WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION AT SEAT TRACK STA 616+17 LBL 24 UPPER AND LOWER SURFACE AND PERFORMED 10X MAGNIFYING GLASS I/A/W SRM 51-10-02-0G-0 VERIFIED MATERIAL LOSS AT STA 616+17 LBL24 ON UPPER SURFACES OF SEAT TRACK LOSS OF .011 MAXIMUM IS .020 IS WITHIN LIMITS IAW SRM 53-00-52-1A-1. VERIFIED MATERIAL LOSS ON SEAT TRACK SEA 616+17 LBL24 LOSS OF .015 MAXIMUM. IS .040 ON BOTTOM OF SEAT TRACK IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED STEPS 1. THRU 3. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.
PASSENGER CABIN SEAT TRACK LBL 24 STA 639+23' WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION AT SEAT TRACK STA 639+23 LBL24 ON UPPER AND LOWER SURFACES AND PERFORMED 10X MAGNIFYING GLASS I/A/W SRM 51-10-02-0G-0 VERIFIED MATERIAL LOSS AT SEAT TRACK AT STA 639+23 LBL 24 ON UPPER SURFACES LOSS OF .010 MAXIMUM IS .020 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED MATERIAL LOSS AT LOWER SURFACES OF SEAT TRACK LOSS OF .015 MAXIMUM LOSS IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED STEPS 1. THRU 3. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.
PASSENGER CABIN SEAT TRACK LBL 45 STA 616+19' WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION. AT SEAT TRACK STA 616+19 LBL45 UPPER AND LOWER SURFACES AND PERFORMED 10X MAGNIFYING GLASS I/A/W SRM 51-10-02-OG-0 VERIFIED MATERIALS LOSS AT SEAT TRACK 616+19 LBL 45 LOSS OF .018 ON BOTTOM OF SEAT TRACK MAXIMUM LOSS IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED MATERIAL LOSS ON SEAT TRACK STA 616 +19 LBL 45 ON UPPER SURFACES LOSS OF .011 MAXIMUM IS .020 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED STEPS 1. THRU 3. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.
PASSENGER CABIN SEAT TRACK LBL 45 STA 663 WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION AT SEATTRACK LBL45 STA 663 WL208 AND PERFORMED 10X MAGNIFYING GLASS I/A/W ARM 51-10-02-0G-0 0N UPPER AND LOWER SURFACE VERIFIED MATERIAL LOSS ON SEAT TRACK STA 663 LBL 45 UPPER SURFACE OF TRACK LOSS OF .008 MAXIMUM CLEAN UP IS .020 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 VERIFIED MATERIAL LOSS AT STA 663 LBL45 ON LOWER SURFACE OF SEAT TRACK LOSS OF MATERIAL IS .012 MAXIMUM CLEAN UP IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED STEPS 1. THRU 3. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.
PASSENGER CABIN SEAT TRACK LBL 45 STA 727A+12'' WL 208 HAS CORROSION ON LOWER SURFACE<REMOVED CORROSION AT SEAT TRACK STA 727A+12 UPPER AND LOWER SURFACES AND PERFORMED 10X MAGNIFYING GLASS I/A/W SRM 51-10-02-0G-0 VERIFIED MATERIAL LOSS AT SEAT TRACK AT STA 727A+12 LBL 45 ON BOTTOM OF SEAT TRACK LOSS OF .023 MAXIMUM LOSS IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED MATERIAL AT SEAT TRACK STA 727A+12 LBL45 LOSS OF .010 ON UPPER SURFACES MAXIMUM IS .020 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED STEPS 1. THRU 3. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.
PASSENGER CABIN SEAT TRACK LBL 24 STA 685 WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION AT LBL24 STA 685 WL 208 AT UPPER AND LOWER SURFACE AND CHECKED WITH 10X MAG IAW SRM 51-10-02-0G-0 MATERIAL. LOSS AT LBL 24 STA 685 WL 208 AT CROWN IS.014 AND LOWER BOTTOM IS .024 WITHIN LIMITS IAW SRM 53-00-52-1A-1 LOSS AT LBL 24 STA 685 WL 208 AT CROWN IS .014 MAX ALLOWABLE IS .020 WITHIN LIMITS IAW SRM 53-00-52-1A-1. LOSS AT LBL 24 STA685 WL 208 AT SEAT TRACK BOTTOM IS .024 MAX ALLOWABLE IS .040 WITHIN LIMITS IAW SRM 53-00-52-1A-1 TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.
PASSENGER CABIN SEAT TRACK LBL 45 STA 727A+16.5'' WL 208 HAS CORROSION ON UPPER SURFACE ; / [01] REMOVED CORROSION FROM SEAT TRACJ STA 727A + 16.5' LBL 45. UPPER SURFACE IAW 51-10-02-0G-0; USED 10X MAGNIFYING GLASS.; [02] VERIFIED MATERIAL LOSS STA 727A + 16.5' LBL 45 UPPER SURFACE IAW SRM 53-00-52-1A-1. FOUND TO BE WITHIN LIMITS. DEPTH .016' MAX ALLOWED .020'. AAR TOOL 36307 CAL DUE DATE 06/14/22.; [03] VERIFIED STEPS 1. AND 2.; [04] OK TO RESTORE FINISH.; [05] TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1. COMPLETED ALL STEPS 1-5.; [06] INSPECTION CW.
PASSENGER CABIN SEAT TRACK LBL 24 STA 727A+13' WL 208 HAS CORROSION ON LOWER SURFACE ; / [01] REMOVED CORROSION AT SEAT TRACK LBL24 STA 727A+ 13 WL208 AND PERFORM 10 X MAGNIFYING GLASS I/A/W SRM 51-10-02-0G-0; [02] VERIFIED MATERIAL LOSS AT SEAT TRACK STA 727A +13 LOSS ON .018 MAXIMUM CLEANUP IS .040 ON BOTTOM OF SEAT TRACK IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22; [03] VERIFIED STEPS 1. AND 2.; [04] OK TO RESTORE FINISH.; [05] TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1. COMPLETED ALL STEPS 1-6.; [06] INSPECTION CW.
PASSENGER CABIN SEAT TRACK LBL 45 STA 685+41' WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE ; / [01] REMOVED CORROSION AT SEAT TRACK 685+41 LBL45 AND PERFORMED 10X MAGNIFYING GLASS I/A/W SRM 51-10-02-0G-0; [02] VERIFIED MATERIAL AT SEAT TRACK STA 685+41 LBL45 <BR>ON BOTTOM OF TRACK LOSS OF .024 MAXIMUM IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06\14\22; [03] VERIFIED MATERIAL AT SEAT TRACK STA 685+41 ON UPPER SURFACES LBL45 LOSS OF .008 MAXIMUM IS .020 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22; [04] VERIFIED STEPS 1. THRU 3.; [05] OK TO RESTORE FINISH.; [06] TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.
PASSENGER CABIN SEAT TRACK LBL 45 STA 685 WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION AT SEAT TRACK LBL45 STA 685 AND PERFORMED 10X MAGNIFYING. GLASS I/A/W SRM 51-10-02-0G-0 VERIFIED MATERIALS LOSS AT SEAT TRACK STA 685 LBL45 ON BOTTOM OF SEAT TRACK LOSS OF .017 MAXIMUM CLEAN UP IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED MATERIAL LOSS AT SEAT TRACK 685 LBL 45 UPPER SEAT TRACK LOSS OF .018 MAXIMUM CLEANUP IS .020 IS WITH IN LIMITS I/A/W SRM 53-00-52-1A-1. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.
FOUND CRACK INDICATION IN A/C BAY AT STA 663 VAPOR BARRIER ATTACH ANGLE LBL 10<CUT AND REMOVED ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5 FIG 202. PERFORMED DVI OF REPAIR AREA & UNDERLYING STRUCTURE. NO DEFECTS IAW SRM 57-10-10-2R-5, REPAIR 5. HFEC IAW NDT PART 6 51-00-00 PROC 16. NO DEFECTS. FABRICATED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. TREATED & PRIMED REPAIR PARTS & CUT EDGE IAW SRM 57-10-10-2R-5 REPAIR 5. INSTALLED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. BONDING CHECKS GOOD. APPLIED CIC TO REPAIR AREA IAW SRM 57-10-10-2R-5 REPAIR 5. LEAK CHECK IAW 28-11-00-400-801 NO LEAKS.
BS 663 LOWER CHORD COMMON TO FUEL TANK CRACKED AT RBL 8, CUT & REMOVED ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5. PERFORMED DVI OF REPAIR AREA & UNDERLYING STRUCTURE. NO DEFECTS IAW SRM 57-10-10-2R-5. HFEC IAW NDT PART 6 51-00-00 PROC 16. NO DEFECTS. FABRICATED REPAIR PARTS IAW SRM 57-10-10-2R-5, REPAIR 5. TREATED AND PRIMED REPAIR PARTS & CUT EDGE IAW SRM 57-10-10-2R-5 REPAIR 5. INSTALLED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. BONDING CHECKED GOOD. APPLIED CIC TO REPAIR AREA IAW SRM 57-10-10-2R-5 REPAIR 5. PERFORMED LEAK CHECK IAW AMM 28-11-00-400-801. NO LEAKS.
NUMBER 2 ENG .N-1 4% LOWER THAN #1 .WOULD NOT ATTAIN FULL CLIMB POWER ; NUMBER 2 ENG. N-1 ;4% LOWER THAN #1 WOULD NOT ATTAIN FULL CLIMB POWER / [01] REF W/O 13684334 LINE #11 TASK CARD 773-11-00 HAS BEEN C/W FUEL PUMP AND HMU WERE REPLACED WITH THIS TASK CARD. RAN END TO T/O POWER NO DEFECTS NOTED
NUMBER 2 ENG .N-1 4% LOWER THAN #1 .WOULD NOT ATTAIN FULL CLIMB POWER ; NUMBER 2 ENG. N-1 ;4% LOWER THAN #1 WOULD NOT ATTAIN FULL CLIMB POWER / [01] REF W/O 13684334 LINE #11 TASK CARD 773-11-00 HAS BEEN C/W FUEL PUMP AND HMU WERE REPLACED WITH THIS TASK CARD. RAN END TO T/O POWER NO DEFECTS NOTED
ON TAKEOFF REJECTED TO @ 92 KNTS DUE TO VERY STRONG INTENSITY BURNING ELECTRICAL SMELL. F/A'S SAID THEY SMELLED IT FROM ROW 3 FWD TORNADO FLT DECK / PERFORMED CONDITIONAL INSPECTION AS PER AMM 05-51-56 AND FIM 21-00 TASK 806 R/R BPCU PRECAUTIONARY L/P 0567667 R/R FWD GALLEY COFFEE MAKER PRECAUTIONARY AS PER AMM 25-30-01 IN FWD GALLEY NO OTHER ISSUES OR DEFECTS WERE FOUND AT THIS TIME RAR 93185
ON TAKEOFF REJECTED TO @ 92 KNTS DUE TO VERY STRONG INTENSITY BURNING ELECTRICAL SMELL. F/A'S SAID THEY SMELLED IT FROM ROW 3 FWD TORNADO FLT DECK / PERFORMED CONDITIONAL INSPECTION AS PER AMM 05-51-56 AND FIM 21-00 TASK 806 R/R BPCU PRECAUTIONARY L/P 0567667 R/R FWD GALLEY COFFEE MAKER PRECAUTIONARY AS PER AMM 25-30-01 IN FWD GALLEY NO OTHER ISSUES OR DEFECTS WERE FOUND AT THIS TIME RAR 93185
RT OW EMERGENCY EXIT LOWER LENSE INCORRECT. INSTALLED CURRENT RT OW EMERGENCY EXIT LOWER LENSE COVER PER 33-51-01.
RIGHT OW EXIT LOWER EMER EXIT SIGN LENSE IS MISSING. INSTALLED EMERG LIGHT LAMP PER AMM 33-51-01. OPS CHECK NORMAL.
'EXIT/SALIDA' LIGHT COVER NEAR FWD GALLEY DOOR POPPED OFF, WILL NOT STAY ON. INSTALLED NEW EXIT LIGHT COVER, PER AMM 33-51-02.
CRACK LEADING EDGE RIB AT LE STA 105.26 RT HORIZONTAL STAB / REPLACED LEADING EDGE RIB AT LE STA 105.26 RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 186A1001 REV B
BROKEN PRESSURE ACCESS DOOR 192DR LATCH BOLT AT AIR CONDITIONING BAY (1 EA) / REPLACED LATCH PRESSURE ACCESS DOOR 192DR AT AIR CONDITIONING BAY (1E/A) I.A.W B737-700 51-40-02 AND SRM B737-700 51-10-02 PARAGRAPH 9
INOP EMERGENCY LIGHT BATERRY PACKS M1672 AND M1668 AT PASSENGER CABIN (2 EA) / REPLACED EMERGENCY LIGHT BATTERY PACKS M1672 AND M1668 AT PASSENGER CABIN (2EA) IAW B737-700 AMM 33-51-06-960-805 (U008)
CRACK ON EXIT LIGHT LENS ON HEADER PANEL RH AT AFT GALLEY AREA (1 EA) / REPLACED EXIT LIGHT ON HEADER PANEL RH AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801
CRACK TRAILING EDGE SUPPORT STRUCTURE AT LEVEL ORSS 297 AT LT WING (1EA) / REPLACED SUPPORT STRUCTURE AT LEVEL ORSS 297 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG #115A3712 REV.A
CORROSION SUPPORT ZEE LOCATED BTW BS 727D TO BS 767 AT LEVEL STR 25R AND RBL 22 AT AFT CARGO COMPARTMENT WL 152.8 / REPLACED SUPPORT ZEE SECTION LOCATED BETWEEN BS 727 TO BSJ767 AT LEVEL STR 25RH RBC 22 AND WL 152.8 AFT CARGO COMPARTMENT IAW SRM 737-700 51-10-02 PARAGRAPH 9 AND DRAWING # 146A7500 REV
CRACK ANGLE - SUPPORT LOCATED AT BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT / REPLACED ANGLE SUPPORT LOCATED AT BS867 AT LEVEL STR.26L AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9; 51-40-02 AND DWG #149A8102 REV.-
CRACK BRACKET LOCATED AT BS 727 BTW STR 27R TO STR 27L AT AFT CARGO COMPARTMENT / REPLACED BRACKET LOCATED AT BS727 BTW STR 27R TO STR 27L AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG #144A2600 SHEET 486 REV A AND SRM 51-10-02
CORROSION SUPPORT ZEE LOCATED BTW BS 727C TO BS 787 AT LEVEL STR 25L AND LBL 22 AT AFT CARGO COMPARTMENT WL 152.8 / PERFORMED REPAIR ON SUPPER ZEE LOCATED FROM BS 727 TO BS 807 AT LEVEL STR 25L LBL 22 AND WL 152.8 AFT CARGO COMPARMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DRAWING #146A1500
CORROSION INTERNAL STRUCTURE WEB LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 27R AND RBL 5 AT AFT CARGO COMPARTMENT WL 152.8 / REPLACED INTERNAL STRUCTURE WEB LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 27R AND RBL 5 AT AFT CARGO COMPARTMENT WL 152.8 IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A8130 REV B.
CORROSION INTERNAL STRUCTURE STRAP AT BS 887 BTW STR 25R TO STR 27L BT W RBL 21 TO LBL 9 AT AFT CARGO COMPARTMENT / REPLACED INTERNAL STRUCTURE STRAP AT BS 887 BTW STR 25R TO STR 27L BTW RBL 21 TO LBL 9 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02; SRM 51-10-02 PARAGRAPH DRAWING # 146A7500- SHEET 61; REV -
ELONGATED HOLE INTERNAL STRUCTURE VERTICAL STIFFENER AT BS 907 AT AFT CARGO COMPARTMENT / REPLACED VERTICAL STIFFENER AT BS 907 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 PARAGRAPH 9.
CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACKET BS 747 BTW STR 8R AND STR 9R AT PASSENGER CABIN / REPAIRED FRAME BST 747 BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACK ET BS 787 BTW STR 8R AND STR 9R AT PASSENGER CABIN / REPAIRED FRAME BST 787 BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACK ET BS 827 BTW STR 8R STR 9R AT PASSENGER CABIN / REPAIRED FRAME BST 827 BETWEEN STR 8 AND STR 9 RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACK ET BS 400 BTW STR 8R AND STR 9R AT PASSENGER CABIN (1 EA) / REPAIRED FRAME BST 400 BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4
CRACK ANGLE - CLIP LOCATED ON BS 400 AND STRINGER 26L FWD CARGO COMPARTMENT / REPLACED ANGLE-CLIP LOC ON BS 400 AND STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM '9' AND DWG 143A7505 SHEET 2 REV B (U131)
CRACK ANGLE - CLIP LOCATED FWD FACE OF BS 500B AND STRINGER 26L AT FWD CARGO COMPARTMENT / REPLACED ANGLE-CLIP LOCATED FWD FACE OF BS 500B AND STRINGER 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 REV 'B' (U031)
CRACK ANGLE - CLIP LOCATED BS 400 AND STRINGER 26R FWD CARGO COMPARTMENT / REPLACED ANGLE - CLIP LOCATED BS400 AND STRINGER 26R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7505 REV 'B'
CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACKET BS 360 BTW STR 8R AND STR 9R AT PASSENGER CABIN (1 EA) / REPAIRED FRAME BST 360 BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4
CRACK SUPPORT ANGLE LOCATED AT BS693 AT BL0 FLOOR STRUCTURE (2E/A) AT PASSENGER CABIN / REPLACED SUPPORT ANGLE (2E/A) LOCATED AT BS 693 AT BL0 FLOOR STRUCTURE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9111 REV. 'B'
CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACKET BS 500C BTW STR 8R AND STR 9R AT PASSENGER CABIN / REPAIRED FRAME LOCATED AT BS 500C BTW STR8R AND STR9R AT PASSENGER CABIN IAW EA N.1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACK ET BS 480 BTW STR 8R AND STR 9R AT PASSENGER CABIN / REPAIRED FRAME BST 480 BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACKET BS 727D BTW STR 8R AND STR 9R AT PASSENGER CABIN / REPAIRED FRAME BST 727D BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND INBOARD FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 480 BTW STR 8L AND STR 9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME BS 480 BTW STR 8L TO STR 9L IAW EA #1-A53-12-114 REV 4
CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACK ET BS 440 BTW STR 8R AND STR 9R AT PASSENGER CABIN (1 EA) / REPAIRED FRAME BST 440 BETWEEN STR 8 AND STR 9 RH SIDE AT PASSENGER CABIN IAW EA #1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACK ET BS 500A BTW STR 8R AND STR 9R AT PASSENGER CABIN / REPAIRED FRAME BST 500A BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND INBOARD FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 520 BTW STR 8L AND STR 9L AT PASSENGER CABIN / REPAIRED FRAME LOCATED AT BS 520 BTW STR8L AND STR9L AT PASSENGER CABIN IAW EA N. 1-A53-12114 REV 4
CRACK SUPPORT ANGLE LOCATED AT BS540 BETWEEN RBL24.5 TO LBL24.5 (2E/A) CENTER SECTION / REPLACED SUPPORT ANGLE LOCATED AT BS 540 BETWEEN RBL 24.5 TO LBL 24.5 (2EA) IAW B737-700 SRM 51-40-02 AND DWG 143A0060 REV 'B'
CRACK GUSSET LOCATED ON BS 500D AND STRINGER 19R FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED ON BS 500D AND STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DRAWING 143A7902 REV -
CRACK INDICATION ON FRAME AROUND FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 500C BTW STR 8L AND STR 9L AT PASSENGER CABIN / REPAIRED FRAME LOCATED AT BS500C BETWEEN STR 8L AND STR9L AT PASSENGER CABIN IAW EA N. 1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND INBOARD FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 440 BTW STR 8L AND STR 9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME BS 440 BTW S-8L TO S-9L IAW EA # 1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 500A BTW STR 8L AND STR 9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME BS 500A BTW S-8L AND S-9L IAW EA # 1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMON TO SUPPORT BRACKET AT BS 400 BTW STR8L AND STR9L AT PASSENGER CABIN ( / PERFORMED PERMANENT REPAIR ON FRAME BS 400 BTW STR 8L AND STR 9L IAW EA #1-A53-12114 RVE 4
CRACK INDICATION ON FRAME AROUND FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 727B BTW STR 8L AND STR 9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME LOC ON BS 727B BTW STR 8L TO STR 9L AT PASSENGER CABIN IAW EA #1-A53-12114 REV #4
CRACK INDICATION ON FRAME AROUND INBOARD FASTENER HOLE COMMON TO SUPORT BRACKET AT BS 727D BTW STR8L AND STR9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME BS 7270 BTW STR 8L TO STR 9L IAW EA #1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND INBOARD FASTENER HOLE COMMON TO SUPORT BRACKET AT BS 747 BTW STR8L AND STR9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME BS 747 BTW S-8L TO S-9L IAW EA #1-A53-12114 REV.4
CRACK INDICATION ON FRAME AROUND INBOARD FASTENER HOLE COMMON TO SUPORT BRACKET AT BS 787 BTW STR8L AND STR9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME BS 787 BTW S-8L TO S-9L IAW EA # 1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND INBOARD FASTENER HOLE COMMON TO SUPORT BRACKET AT BS 827 BTW STR8L AND STR9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME LOC ON BS 827 BTW STR 8L TO STR 9L AT PASSENGER CABIN IAW EA #1-A53-12114 REV 4
CRACK INDICATION ON FRAME AROUND INBOARD FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 867 BTW STR 8L AND STR 9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME LOC ON BS 867 BTW STR 8L TO STR 9L AT PASSENGER CABIN IAW EA #1-A53-12114 REV 4
CORROSION FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT / REPLACED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 453A2610 REV E
CORROSION ACCESS DOOR 311BL INTERNAL LOCATED ON 4 INCH LOWER EDGE; 9 INCH AFT EDGE AND 13 INCH UPPER EDGE AT LOWER FUSELAGE / REPLACED ACCESS DOOR 311BL AFT LOWER FUSELAGE IAW AMM B737-700 52-49-11-400-802 AND SRM B737-700 51-10-02 ITEM 9
CRACK FRONT SPAR INSPAR RIB LOCATED STA 120.30 STIFFENER 3 RT HORIZONTAL STAB / PERFORMED PERMANENT REPAIR LOCATED FRONT SPAR INSPAR RIB LOCATED STA 120.30 STIFFENER 3 RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5. THIS REPAIR IS CATEGORY A
CRACK LEADING EDGE SKIN SLAT 5 AT THE ACTUATOR RIB AT RT WING (1 EA) / REMOVED AND REPLACED SLAT 5 RT WING DUE TO CRACKS ON REPAIR AREA ARE NOT PERMITED. I.A.W B737-700 AMM 27-81-21-400-801 AND AMM 27-81-00-820-803 POS:5 TAG/GRB: 619101 P/N OFF:114A5040-A S/N OFF:001553 P/N ON: 114A5040-A S/N ON:001531
CRACK LEADING EDGE SKIN SLAT 3 AT THE ACTUATOR RIB AT LT WING (1 EA) / PERFORMED PERMANENT REPAIR ON SKIN SLAT 3 IAW EA #20-157-00416 REV IR EA #57-0376-20 REV #0
CRACK INSPAR RIB STAB STA 120.30 AND 15.5 INCH FROM FRONT SPAR LT HORIZONTAL STAB / PERFORMED PERMANENT REPAIR ON INSPAR RIB STAB STA 120.30 AND 15.5 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4.
ELONGATED HOLE FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT / REPLACED FLOOR PANEL #120CF AT FWD CARGO COMPARTMENT I.A.W. AMM B737-700 25-52-01-201-801 AND DRAWING #453A1610 REV. D DUE TO ALLOWABLE DAMAGE NOT FOUND FOR ELONGATED HOLE NEW PANEL FABRICATED FROM 0.090' CANOLITE P.O. #2020-138497
CRACK INSPAR RIB STAB STA 120.30 AND 26 INCH FROM FRONT SPAR LT HORIZONTAL STAB / REPAIRED INSPAR RIB STAB STA 120.30 AND 26 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R REPAIR 5. THIS REPAIR IS CATEGORY A
CRACK SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB / REPLACED SEAL PLATE ON ACCESS PANEL 333AB AT LT HORIZONTAL STAB. I.A.W B737-700 SRM 51-10-02- 0G-0 ITEM 9 AND SRM 51-40-02
CORROSION BILGE AREA PLATE BS 787 RBL 25 FWD CARGO COMPARTMENT (1 EA) / REPLACED PLATE LOCATED BILGE AREA BS 787 RBL 25 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 REV C DRAWING 453A2611
UPPER CARGO DOOR SILL CLIP CORRODED AT BS. 460, RBL 66. / REPAIRED CLIP PER EA & ER.
FORWARD CARGO DOOR UPPER DOOR FRAME WEB CORRODED AT BS. 460, STR. 19R. / REPAIRED WEB PER EA & ER.
OVERHEAD EMERGENCY EXIT SIGN BROKEN. / R&R EXIT SIGN HOUSING PER MM.
FORWARD GALLEY EMERGENCY FLASH LIGHT POS #1 SAFETY STRAP BROKEN. / R&R STRAP IAW AMM.
193B PANEL HOLES OUT OF LIMITS / REMOVED AND REPLACED 193B PANEL REF AMM 53-51-21.
R1 DOOR EMERGENCY ESCAPE SLIDE CAME LOOSE. R&R SLIDE PER MT.
CAPTAIN'S ESCAPE ROPE DOOR OUT OF ADJUST. ADJUSTED ROPE DOOR PER SIP.
FOUND COCKPIT FLOOR SKIN CREASED ALONG CHANNEL AT STA 258; LBL 15.33'. DAMAGE MEASURES L = 9; W = 3'; AND D = 0.078'. MOD / REPAIRED COCKPIT FLOOR STA 258 LBL 15.33 IAW SWA EA 1-A53-33179
L1 DOOR EMERGENCY LIGHTS INOP IN GALLEY AREA. R&R BATTERY PACK PER MM.
LT WING OUTBOARD AFT FLAP INBOARD AFT CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM AND AMM.
LT WING FIXED LEADING EDGE PANEL STRINGER CRACKED BETWEEN KRAS 206.32 TO KRAS 224. R&R STRINGER IAW SRM AND DWG.
LT WING TRAILING EDGE INBOARD OF SAIL TAIL WAFFLE PLATE CRACKED AT FASTENER HOLE. R&R WAFFLE PLATE IAW SRM.
RT WING FIXED TRAILING EDGE PANEL SUPPORT RIB CRACKED LOCATED. R&R RIB IAW SRM AND DWG.
LT WING TRAILING EDGE AT SAIL TAIL UPPER AFT BULB SEAL SUPPORT ANGLE CRACKED. R&R ANGLE IAW SRM.
FORWARD CARGO DOOR SURROUND FORWARD CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.
RT WING NR 5 LEADING EDGE SLAT SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED NR 5 SLAT SKIN PER SRM.
RIGHT MAIN WHEEL WELL STA 663 RBL 26 STIFFENER CRACKED OUTBD OF TURBINE EXHAUST DUCT / REPLACED STIFFENER AT 663 RBL 26 REF SRM 51-40-02
RADOME DELAMINATED. / R&R NOSE RADOME IAW AMM 53-52-00. SAM 115 ROBBED PARTS TAG - P/N OFF: 1001002-2 P/N ON: 1001001-1 S/N OFF: 9307205-C S/N ON: 0107103C (ROBBED FROM A/C 968)
CRACK IN LEFT W/W MOISTURE BARRIER MOD. / APPLIED INTERIM REPAIR PER SRM 57-10-10-2R-2. FWD SIDE OF BULKHEAD
RIGHT EMERGENCY EXIT ROW VERTICAL EXIT SIGN COVER MISSING AT ROW 12. R & R THE LIGHT ASSEMBLY IAW MM.
L1 DOOR ESCAPE SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.
FORWARD GALLEY EMERGENCY EXIT LIGHT COVER BROKEN. R&R LIGHT ASSEMBLY IAW AMM.
R2 DOOR EXIT SIGN LOOSE. R&R SIGN ASSEMBLY IAW MM.
L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER TC.
L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW AMM & MAINTENANCE.
M1670 LOWER EMER EXIT LIGHT ASSEMBLY INOPERATIVE BETWEEN ROW 9 - 12. R & R LIGHT ASSEMBLY IAW AMM.
TIE CLIP CORRODED AT BS 867, STRINGER 25L. R & R TIE CLIP IAW SRM & DWG.
AFT LAVATORY SERVICE PANEL SKIN CORRODED AT AFT & LOWER EDGES UNDER PAN. REPAIRED SKIN IAW EA.
INTERCOSTAL CORRODED AT BS 312, RBL 11. R & R INTERCOSTAL IAW SRM & DWG.
R2 DOOR CHORD CORRODED AT THRESHOLD. R & R CHORD IAW SRM & DWG.
AFT CARGO FLOOR STRAP CORRODED AT BS 887. REPAIRED STRAP IAW SRM & DWG.
STRINGER CLIP CRACKED AT BS 500D, STRINGER 19L. REPAIRED CLIP IAW SRM.
FORWARD CARGO THRESHOLD WEB CORRODED. R & R WEB IAW SRM & DWG.
FLOOR STRUCTURE CORRODED AT BS 772, LBL 3. R & R SUPPORT IAW SRM.
STRINGER CLIP CRACKED AT BS 500C, STRINGER 19L. R & R CLIP IAW SRM & DWG.
STRINGER CLIP CRACKED AT BS 500D, STRINGER 19R. R & R CLIP IAW SRM & DWG.
STRINGER CLIP CRACKED AT BS 500C, STRINGER 19L. R & R CLIP IAW SRM & DWG.
LOWER BULKHEAD CHORD FASTENER HOLE CRACKED AT BS 540, BETWEEN STRINGER 22R - 23R. REPAIRED CHORD IAW EA.
FORWARD EMER EXIT SIGN COVER LENS MISSING. INSTALLED LENS IAW SIP.
L1 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR BRACKET IAW MT.
RIGHT OVERWING EMER EXIT LIGHT COVER LOOSE. SECURED COVER IAW MM.
R2 DOOR EMER EXIT SIGN, LENS COVER CRACKED. R & R COVER IAW MM.
L1 DOOR EXIT SIGN LOOSE. R & R SIGN ASSEMBLY IAW MM.
L2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.
M01672 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW WDM.
M01670 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW WDM.
M01669 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW WDM.
RIGHT WING WIGGLE PLATE CRACKED. R & R WIGGLE PLATE IAW SRM.
M01673 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW WDM.
RIGHT OVERWING EXIT SIGN BROKEN. R & R SIGN IAW MM.
R2 DOOR EXIT SIGN LENS MISSING. INSTALLED LENS IAW SIP.
R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM & MT.
LEFT HORIZONTAL STABILIZER STAB STATION 92.70 APPROXIMATELY 20 INCHES FROM FRONT SPAR CRACKED ON LOWER VERTICAL STIFFENER. REMOVED STABILIZER IAW SRM.
SEAT TRACK CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.
SEAT TRACK CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.
SEAT TRACK CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.
SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.
RIGHT WING TE RIB AT REAR SPAR ORSS 275 BULB SEAL FITTING ATTACH BRACKET UPPER FLANGE BROKEN. R & R FITTING IAW SRM & DWG 2.
FLOOR SUPPORT STRUCTURE CRACKED AT BS 540, LBL 0. R & R SUPPORT IAW SRM.
R2 DOOR EMER EVAC SLIDE FWD FLOOR FITTING LOOSE. SECURED FITTING IAW AMM.
R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
L1 DOOR EXIT SIGN LENS DAMAGED. REPAIRED COVER IAW SWA EA.
L2 DOOR EMERGENCY EXIT EXTERNAL LIGHT INOPERATIVE. R&R BULB IAW AMM.
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED CLIP IAW MM.
RT MAIN WHEEL WELL FWD VERTICLE PRESSURE WEB CRACKED 1" AT BS 663.75, RBL 32.83 FWD OF SPOILER CONTROL VALVE. REPAIRED PER SRM 57-10-10-2R-3 REPAIR 3 FIG 204. REFER TO SAM 326 FRO SIGN OFFS. FACT AS A RESULT OF POST REPAIR INSPECTION
LEFT MAIN WHEEL WELL FWD VERTICLE PRESSURE WEB HAS 1" CRACK AT BS 663.75, LBL 38.00 JUST BELOW CEILING. REPAIRED PER SRM 57-10-10-2R-3, REPAIR 3 FIG 204, REFER TO SAM 326 FOR SIGN OFFS.
RIGHT MAIN WHEEL WELL FWD VERTICLE PRESSURE WEB CRACKED 3" AT BS 663.75, RBL 43.80 JUST BELOW CEILING. REPAIRED PER SRM 57-10-10-2R-3 REPAIR 3 FIG 204, REFER TO SAM 326 FOR SIGN OFFS. FACT AS A RESULT OF POST REPAIR INSPECTION
EXIT LIGHT ON ROW 10, CAPT SIDE SIDEWALL, BROKEN. REMOVED AND REPLACED EMERGENCY LIGHTT LENS SECURED C/W EA 1-A33-0130 OK TO CONTINUE ON MX NOTE # 81192 REPAIR/REPLACE/ON BEFORE 30 CYCLES.
EXIT LIGHT ON ROW 10, CAPT SIDE SIDEWALL, BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM OPS GOOD CLEARING # 81636 MEL CLEARED ON L/P 8612346.
FWD KEEL BEAM PANEL HAS A FWD OUTBOARD BRACKET CRACKED. REMOVED AND REPLACED PER AMM.
EMERGENCY EXIT LIGHT ON AFT GALLEY AREA WALL AT AFT ENTRY DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AT AFT ENTRY DOOR PER M/M. OPS CHECK GOOD.
FORWARD RIGHT JUST AFT OF THE FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
RIGHT EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM.
R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RECONNECTED CONNECTOR PER SWPM & AMM.
RIGHT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 8 TO ROW 13. REMOVED AND REPLACED BATTERY PACK PER AMM.
RIGHT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STA 129.50. REMOVED AND REPLACED RIB IAW SRM.
RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.70. REPAIRED RIB IAW SRM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 175.5. REPAIRED SKIN PER SRM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147.9. REPAIRED SKIN PER SRM.
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM.
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.
EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES PER MM.
EMERGENCY LIGHT TRACK COVER CRACKED AT ROW 9. REMOVED AND REPLACED COVER PER MM.
L2 DOOR EMERGENCY EVAC SLIDE BRACKET LOOSE. SECURED BRACKET PER MM.
DURING SCHEDULED HC1 CHECK, FOUND LT EMERGENCY EXIT LIGHT COVER BROKEN AT ROW 11. REMOVED AND REPLACED COVER PER MM.
L2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1. RELAMPED EEPLS PER MM.
DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.
DIVERSION - R1 COCKPIT WINDOW ARCED DURING FLIGHT. REMOVED AND REPLACED R1 WINDOW SHIELD AND HEAT CONTROLLER PER MM.
EEPLS COVER MISSING AT ROW 1. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.
EMERGENCY EXIT LIGHT COVER MISSING AT ROW 1. INSTALLED COVER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 1. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVERS WORN BETWEEN ROW 1 TO ROW 20. REMOVED AND REPLACED COVER PER MM.
AFT GALLEY EMERGENCY FLASHLIGHT BATTERY VOLT LOW. REMOVED AND REPLACED BATTERY PER MM.
EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.
EEPLS LENS MISSING AT ROW 2. INSTALLED LENS PER MM.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS MISSING AT ROW 1. INSTALLED EEPLS PER MM.
DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 3. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY LIGHT COVERS CRACKED BETWEEN ROW 3 TO ROW 14. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY LIGHT COVERS CRACKED BETWEEN ROW 15 TO ROW 23. REMOVED AND REPLACED COVER PER MM.
L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP. RELAMPED PER MM.
DURING SCHEDULED HC1 CHECK, FOUND EEPLS TRACK COVER CRACKED. REMOVED AND REPLACED COVER PER MM.
DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.
DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 2L. REMOVED AND REPLACED EEPLS PER MM.
FWD EEPLS WIRE EXPOSED AT ROW 1. REMOVED AND REPLACED LIGHT ASSY PER MM.
EEPLS LIGHT STRIP LOOSE AT ROW 1. SECURED EEPLS PER MM.
FOUND FWD EEPLS LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 4 ABC. REMOVED AND REPLACED LENS PER MM.
L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.
L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MT.
DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 5 ABC. REMOVED AND REPLACED LENS PER MM.
R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM.
EEPLS TRACK LOOSE AT FWD END. REMOVED AND REPLACED EEPLS PER MM.
EEPLS TRACK COVER MISSING AT ROW 23. INSTALLED COVER PER MM.
DIVERSION, ACRID ELECTRICAL ODOR IN CABIN. GASPER FAN & RECIRCULATION FAN SWITCHES TURNED OFF, ODOR DISSIPATED. REMOVED AND REPLACED EQUIPMENT COOLING FAN PER MM.
DURING SPV, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES PER MM.
R2 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM.