N8302F
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
RIGHT MID CABIN AISLE EMERGENCY LIGHTS AND RT OVERWING EXIT EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. EMERGENCY LIGHT BATTERY PACK M1671 REQUIRES REPLACEMENT.
PAX CABIN AFT ENTRY DOOR AREA FWD ASSISTANT HANDLE LOOSE. INSTALLED CORRECTLY PAX CABIN AFT ENTRY DOOR AREA FWD ASSISTANT HANDLE IAW SOPM 20-50-01, REV 40.
INOPERATIVE EMERGENCY LIGHT OVER WING FWD ON FUSELAGE AT RT SIDE. REPLACED LAMP OF THE OVERWING EMERGENCY LIGHT FWD ON FUSELAGE AT RT SIDE IAW AMM 33-51-04-960-801 AND PERFORMED OPERATIONAL TEST EMERGENCY LIGHTS IAW AMM 33-51-00-710-801. OPS TESTED OK.
BROKEN LENS EMERGENCY EXIT LIGHT SIDEWALL PANEL 231ZKW AND SIDEWALL PANEL 232ZKW AT PASSENGER CABIN (2EA). REPLACED LENS EMERGENCY EXIT LIGHT SIDEWALL PANEL 231ZKW AND SIDEWALL PANEL 232ZKW AT PASSENGER CABIN (2EA) IAW AMM 33-51-01-960-802 STEP 3.C.(10).
BROKEN HOUSING ASSY EXIT SIGN AT PASSENGER CABIN. REPLACED HOUSING ASSY EXIT SIGN AT CENTER PASSENGER CABIN IAW AMM 33-51-01-960-802 TESTED OK.
BROKEN HOUSING EXIT SIGN SIDEWALL 232ZKW AT PASSENGER CABIN (1EA). REPLACED HOUSING EXIT SIGN SIDEWALL 232ZKW AT PASSENGER CABIN IAW AMM 33-51-01-960-802. TESTED OK.
CRACK CORRUGATED PLATE, ORSS 404 +18, RT WING T/E. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02-0G-0, AND DWG 115A3700, SHEET 70, REV-.
BROKEN LENS EMERGENCY EXIT LIGTH (WITH ARROW) AT GALLEY 1 FWD GALLEY AREA (1EA). REPLACED LENS EMERGENCY EXIT LIGTH (WITH ARROW) AT GALLEY 1 FWD GALLEY AREA (1EA) IAW AMM 33-51-01-960-802 STEP 3.C.(10).
CRACKED SUPPORT WEB, INBD FAN COWL NR 1 NACELLE. REPLACED THE SUPPORT WEB IAW SRM 51-10-02-0G-0, ITEM 9, AND SRM 51-40-02.
DETERIORATED PHOTOLUMINESCENT STRIP ALONG PASSENGER CABIN. REPLACED PHOTOLUMINESCENT STRIP ALONG PASSENGER CABIN IAW AMM 33-51-15-960-801 AND PHOTOLUMINESCENT STRIP WILL BE INSTALLED ON TTG8Q00LRPSR MT 733-50-01. JOB COMPLETED.
CORROSION HINGE TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE. REPLACED HINGE TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE IAW SRM 51-40-02-0G-0, AND SRM 51-10-02-0G-0, ITEM 9.
CORROSION ON PLATE HINGE TOILET SERVICE DOOR 145AL CUTOUT AT LOWER FUSELAGE. REPLACED PLATE HINGE TOILET SERVICE DOOR 145AL CUTOUT AT LOWER FUSELAGE IAW SRM 51-10-02 ITEM 9 AND DWG 146A7401 SHEET 5 REV-.
CRACKED SEAL BLADE ACCESS PANEL 333AB ON THE LT HORIZONTAL STAB. REPLACED SEAL BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW SRM 51-40-02, AND DWG 186A3101, SHEET 20, REV-.& SRM 51-10-02, STEP 9, ITEM A.
INSTALL CORRECTLY GIRT SLIDE ON FWD SERVICE AT FWD GALLEY AREA. INSTALLED CORRECTLY GIRT SLIDE ON FWD SERVICE AT FWD GALLEY AREA IAW AMM 25-66-01-200-802; STEP 3.B.(1).(D).
ELONGATED HOLE ON ACCESS PANEL 193D BODY FAIRING. REPAIRED ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.
ELONGATED HOLE ON ACCESS PANEL 661CB TRAILING EDGE, RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
ELONGATED HOLE ON ACCESS PANEL 661BB TRAILING EDGE AT RT WINGREPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.
CRACK BS 663.75 VAPOR BARRIER, RBL 48. REPLACED VAPOR BARRIER AND REMOVE AND RE- INSTALL VAPOR BARRIER WILL BE COMPLETED SEE TTG8Q01BACSV .
CRACK SUPPORT ANGLE ON INBD AUXILIARY TRACK SLAT 6 AT RT WING. REPLACED THE SUPPORT ANGLE IAW CMM 57-43-03, REV 41 ASSEMBLY PROCEDURES STEP 2.C(9) PAGE 702.
CRACKED SUPPORT ANGLE ON OTBD AUXILIARY TRACK SLAT 8, RT WING. REPLACED THE SUPPORT ANGLE IAW CMM 57-43-03, REV 41. ASSEMBLY PROCEDURES STEP 2.C(9) PAGE 702.
RIGHT HORIZONTAL UPPER SLIDER CRACKED. R & R THE RIGHT HORIZONTAL UPPER SLIDER IAW SRM 51-40-02-0G-0-B00069.
LEFT WING OTBD TRAILING EDGE FLAP HAS DISBONDING ON UPPER SKIN INBD CORNER 12 AT LONGEST AND 8 AT WIDEST HAVING DISBONDING FROM ZONE 1 TO 5. MORE THAN 2 DIAMETER IN ZONE. SPLIT T/E 1 1/2<. REPLACED LT OTBD AFT FLAP IAW AMM 27-51-22.
FWD ENTRY GIRT BAR SLIDE FWD HOOK LOOSE. INSTALLED FASTENER ON FWD ENTRY GIRT BAR HOOK IAW SRM 51-40-02.
FLASHLIGHT AFT GALLEY F/O SIDE INBOARD INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT IAW AMM 25-64-00.
RIGHT FMC INOPERATIVE, VTK FLAG. REMOVED AND REPLACED IAW AMM 34-61-02-401-NG, SYSTEM OPS TEST PASSED.
FWD OUTBOARD EMER FLASHLIGHT INOP<[01] R AND R BATTERY AS PER AMM 25-64-00
FWD CABIN CENTER AISLE ROWS 1DEF-2DEF PHOTOLUMINESCENT STRIP HAS EVIDENCE OF MOISTURE IN IT.<[01] R&R FWD CABIN CENTER AISLE ROWS 1DEF-2DEF PHOTOLUMINESCENT STRIP IAW AMM 25-00-00. PARTS SOURCED FROM SHIP-SET PREVIOUSLY ORDERED.
RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD HAS SURFACE CORROSION AT STAB STATION 71.5; ALONG AFT EDGE 1.625' LONG BY .375' WIDE. REPAIRED IAW 25-155-00571.
LEFT OVERWING EXIT CNTER LOWER LIGHT IS INOP <[01]. JOB COMPLETED ON CARD TTG8Q00Y2TLW; [02] VERIFIED ITEM 1. AUDIT C/W.
RIGHT OVERWING EXIT BOTH EXIT SIGNS ARE INOP<[01] REMOVED AND REPLACED M1695 EMERGENCY BATTERY PACK FOR RIGHT OVERWING EXIT BOTH EXIT SIGNS INOP IAW AMM 33-51-06-960-805 OPS CHECK GOOD<BR><BR>WN49680;[02] VERIFIED ITEM 1<BR><BR>AUDIT C/W
AFT RIGHT WET AREA EMERG LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACK M1672 FOR AFT RIGHT WET AREA EMERGENCY LIGHTS BEING INOP IAW AMM 33-51-06-960-805 OPS CHECK GOOD.
STR 23 SECOND HOLE AFT OF STA 360 SPLICE ON BEAR-STRAP HAS CRACK INDICATION. CW EA 24-153-03536-WIP5 PERFORMED NDT PART 6 51-00-00 PROC 16. DAMAGED REMOVED. NO FURTHER CRACK INDICATIONS NOTED.
ON LANDING WE GOT A TOO LOW FLAPS WARNING & PERFORMED A GO-AROUND; RETRACTED FLAP ON SCHEDULE BUT FLAP STUCK AT 2 DEGREES. WE RAN THE TRAILING EDGE FLAP DISAGREE QRH AND LANDED FLAPS 15 DEGREES.<[01] FOUND FAULT CODE 27-51351 ON FSEU. PERFORMED FIM TASK 27-51 TASK 830 RESULT/FAULT WAS INTERMITTENT. PERFORMED FLAP SKEW DETECTION SYSTEM FUNCTIONAL TEST IAW AMM 27-59-00; ALL SENSORS ARE WITHIN LIMITS. INSPECTED TRANSMISSION TORQUE TRIP INDICATORS AND NONE WERE EXTENDED.;[02] (REF TTG8Q00X0RQT FOR ACCOMPLISHMENT OF T/S FIM 27-51 TASK 830 FOR FAULT CODE 27-51351 ON FSEU. FOUND TO BE INTERMITTENT. FLAP SKEW DETECTION SYSTEM FUNCTIONAL TEST PER MM 27-59-00. ALL SENSER W/IN LIMITS. FLAP TRANSMISSION TORQUE TRIP INDICATORS WERE INSPECTED. NON EXTENDED) <BR>PERFORMED FSEU BITE IAW FIM 27-51 TASK 801. NO EXISTING FAULTS. PERFORMED OPS CHECK OF TRAILING EDG FLAPS IAW MM 27-51-00. NO DEFECTS NOTED AT THIS TIME.
L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS CAME OFF<[01] REMOVED & REPLACED EMERGENCY EXIT INDICATOR ASSY IAW AMM 33-51-01 OPS CHECK GOOD
PASSENGER ASSIST HANDLE ON FWD ENTRY DOOR IS BROKEN<[01] REPLACED HANDLE NUT PER CMM 25-31-67
RIGHT HORIZONTAL STAB UPPER FWD SLIDER CRACKED.<[01] REMOVED AND REPLACED RIGHT UPPER STAB FWD SLIDER REF SRM 51-40-02
ON THE NOSE CONE IF FACING THE AIRCRAFT FROM THE FRONT AT THE 11 OCLOCK POSITION THERE APPEARS TO BE SUBSTANTIAL DELAMINATING WHERE THE LIGHTNING STRIP ATTACHES TO THE NOSE CONE. THE WEAR AND TEAR IS SIGNIFICANTLY MORE THAN THE PAINT FADING IN THE SURROUNDING PART OF THE NOSE.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-52-00-401-NG (NOSE RADOME - REMOVAL/INSTALLATION - PERMANENT)]
*CUSTOMER WALK* EMERGENCY EXIT SIGN LIGHT BULBS OUT OVER L1 DOOR; R2 DOOR; AND BOTH FORWARD OVER WING EXISTS; JUST A FEW BULBS IN EACH.<[01] REPLACED EMERGENCY EXIT LIGHT BULBS OVER L1 DOOR; R2 DOOR AND BOTH FORWARD OVER WING EXISTS AS PER B737 AMM 33-51-01-960-801. PERFORM OPERATIONAL TEST AS PER B737 AMM 33-51-01-960-801. TEST PASSED.;[02] VERIFIED REPLACED EMERGENCY EXIT LIGHT BULBS OVER L1 DOOR; R2 DOOR AND BOTH FORWARD OVER WING EXISTS AS PER B737 AMM 33-51-01-960-801. PERFORM OPERATIONAL TEST AS PER B737 AMM 33-51-01-960-801. TEST PASSED.
FOUND BATTERY PACK AT POSITION M02816 DEFECTIVE.<[01] REMOVED AND REPLACED BATTERY PACK AT POSITION M02816 AND PERFORMED INSTALLATION TEST AS PER B737 AMM TASK 33-51-06-960-805. TEST OK.;[02] VERIFIED REMOVED AND REPLACED BATTERY PACK AT POSITION M02816 AND PERFORMED INSTALLATION TEST OK.
L2 DOOR LOWER ACCESS PANEL 841DZ AFT SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED AFT SUPPORT BRACKET ASSY AT L-2 DOOR LOWER ACCESS PANEL PER B737-800 SRM 51-40-02-0G-0;[02] VERIFIED REPLACEMENT
R/H ELEVATOR PANEL 344GT HAS A CRACK<[01] ACCOMPLISHED REPAIR IN DAMAGED AREA AT PANEL 344GT AS PER B737 SRM 51-70-06-2R-11. MATERIAL USED PO#1776837; PO# 2012656 AND PO#1755421.;[02] VERIFIED ALL STEPS
LOWER FUSELAGE CENTER WING BOX VERTICAL BULKHEAD VAPOR BARRIER STIFFENER CRACKED @ LOWER RADIUS O/B OF A/C AIR EXIT EXHAUST DUCT STA 663.75 MKD DOT CORRECTION AT L/H SIDE<[01] REMOVED AND REPLACED STIFFENER @ LOWER FUSELAGE CENTER WING BOX VERTICAL BULKHEAD VAPOR BARRIER O/B OF A/C EXIT EXHAUST DUCT STA. 663.75 PER B737-800 SRM 51-40-05-0G-0 AND BOEING DRAWING NO. 111A1000;[02] VERIFIED STIFFENER REPLACEMENT B.S. 663.75 O/B OF A/C EXHAUST DUCT LEFT SIDE.
LOWER AFT CENTER WHEEL WELL ACCESS PANEL # 193D BULGING/CRACKED FASTENER HOLES<[01] VERIFIED;[02] REPAIRED DAMAGED AREA (CRACKED FASTENER HOLES) AT PANEL# 193D AS PER B737 SRM 51-70-04-2R-9; MATERIAL USED PO#1776837; PO#2012656AND PO#1738579. TOUCHED UP PAINT ON LOWER AFT CENTER WHEEL WELL ACCESS PANEL # 193D REF B737 AMM 51-21-73-370-803;[03] VERIFIED STEPS 2
FWD LOWER CENTER WHEEL WELL ACCESS 193B HAS BULGING/CRACKED FASTENER HOLES<[01] VERIFIED AND INSPECTED APPLIED TOP COAT TO FWD LOWER CENTER WHEEL WELL ACCESS 193B HAS BULGING/CRACKED FASTENER HOLES.
FWD SERVICE DOOR NEED ADJUSTMENT<[01] ACCOMPLISHED FWD SERVICE DOOR ADJUSTMENT PER B737 AMM 52-41-00-820-801-NG;[02] VERIFIED ADJUSTMENT
CORROSION AT AFT CARGO COMPARTMENT FLOOR SUPPORT Z CHANNEL S-26R FROM STA 727I TO STA 767 WL 151<[01] FOUND EXFOLIATED CORROSION THROUGH OUT OF LIMITS PER SRM 53-00-53-1A-2<BR>REMOVED AFT CARGO R/H Z CHANNEL FROM SECTION 727F - 767 PER SRM 51-40-02-0G-0<BR>LOCATED AND DRILLED NEW Z-CHANNEL AT AFT CARGO COMPARTMENT FLOOR SUPPORT S-26R STA 727I TO STA767 WL151 PER SRM 51-40-05-0G-0<BR>MAT USE:BAC1496-377 7075 T6<BR>TREATED AND PRIMED NEW Z-CHANNEL SECTION AT AFT CARGO COMPARTMENT FLOOR SUPPORT S-26R FROM STA 727I TO STA 767 PER AMM 51-21-41-370-803 AND AMM 51-21-72-370-804<BR>INSTALLED NEW Z-CHANNEL SECTION AT AFT CARGO COMPARTMENT FLOOR SUPPORT AT STR 26R STA 727I TO STA 767 WL 151 PER SRM 51-40-02-0G-0<BR>DWG# 146A7502;[02] RII- VERIFIED REPLACEMENT
AFT OF AFT CARGO COMPARTMENT BILGE SUPPORT BRACKET CRACKED @ RADIUS AREA S-26L STA 947.5 MKD DOT<[01] SUMMARY.<BR>REMOVED CRACKED SUPPORT BRACKET AT AFT CARGO BILGE AREA STA 947.5 S-26L AS PER B 737 SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED NEW AFT CARGO SUPPORT BRACKET AS PER B 737 SRM 51-40-05-0G-0 AND DWG 149A8113 REV A FRAME 1 OF 1.<BR>INSTALLED NEW AFT CARGO BILGE AREA SUPPORT BRACKET AS PER B 737 SRM 51-40-02-0G-0 AND DWG 149A8113 REV A FRAME 1 OF 1.;[02] VERIFIED STEP 1.
FWD CARGO BULKHEAD POST STANDOFF BROKEN AT STA 500I; LBL 23; WL 158<[01] REMOVE AND REPLACED FWD CARGO BULKHEAD POST STANDOFF AT STA 500I LBL 23 WL 158 PER SRM 51-40-02-0G-0<BR>PN:BACN10TL3A14;[02] VERIFIED
MAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED AT LBL 1 STA 540 MKD DOT<[01] INSTALLED NEW MAIN CABIN CENTER WING FLOOR SUPPORT BREAK AT LBL 1 STA 540 AS PER SRM 51-40-02-0G-0/ DRW 143A0060.;[02] VERIFIED ALL STEPS
FWD CARGO COMPARTMENT FLOOR Z CHANNEL SUPPORT CLIP CRACKED @ S-26L STA 500H WL 151<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT FLOOR Z CHANNEL SUPPORT CLIP S-26L STA 500H PER SRM 51-40-02-0G-0;[02] VERIFIED REPLACEMENT
R/W REAR SPAR LOWER FIXED T/E WIGGLE FITTING CRACKED @ FASTENER'S HEAD I/B FLAP TRACK BEAM NO-6 FWD MKD DOT<[01] REMOVED AND REPLACED R/W REAR SPAR LOWER FIXED T/E WIGGLE FITTING I/B FLAP TRACK BEAM N0 -6 FWD AS PER REF B/737 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1;[03] REMOVED AND REPLACED R/W REAR SPAR LOWER FIXED T/E WIGGLE FITTING I/B FLAP TRACK BEAM N0 -6 FWD AS PER REF B/737 SRM 51-40-02-0G-0.;[04] VERIFIED ALL STEPS
FWD CARGO COMPARTMENT Z CHANNEL LOWER SUPPORT CLIP CRACKED @ S-26R STA 500H MKD DOT<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT Z CHANNEL LOWER SUPPORT CLIP AT S-26R STA 500H PER SRM 51-40-02-0G-0.;[02] VERIFIED INSTALLATION. FOUND ONE COLLAR NOT SNAPED;[03] FINISHED INSTALLATION; INSTALLED 1 MISSING COLLAR PER SRM 51-40-02-0G-0.;[04] VERIFIED RESTORATION OF REJECT
FWD CARGO COMPARTMENT L/H SIDE WALL GUSSET CRACKED @ S-21L STA 500I MKD DOT<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT L/H SIDE WALL GUSSET S-21L STA 500I PER SRM 51-40-02-0G-0;[02] VERIFIED ALL STEPS
FWD CARGO COMPARTMENT R/H SIDE WALL AFT GUSSET CRACKED @ S-19R STA 500I MKD DOT<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT R/H SIDE WALL AFT GUSSET S-19R STA 500I PER SRM 51-40-02-0G-0;[02] VERIFIED ALL STEPS
GALLEY-1 EMERGENCY EXIT LIGHT CONNECTOR WIRE IS BROKEN.<[01] REMOVED AND REPLACED GALLEY #1 EMERGENCY EXIT LIGHT CONNECTOR D03658 AS PER B737 SWPM 20-30-12; SWPM 20-60-11; AND WDM 33-51-21. PERFORMED EMERGENCY LIGHTS - OPERATIONAL TEST; TASK 33-51-00-710-801. TEST OK.;[02] VERIFIED REMOVED AND REPLACED GALLEY #1 EMERGENCY EXIT LIGHT CONNECTOR AND TESTED
FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED AT FASTENER HOLE BETWEEN STA 380 & 400 BL-0 WL 208.1 MKD DOT C<[01] REMOVED DAMAGE FLOOR SUPPORT BET STA 380 TO STA 400 BL-0 WL 208.1 REF B 737-800 SRM 51-40-02;[02] 1. VARGAS; MANUEL (COMPLETE)<BR>06-JUN-2023 19:01:35<BR>INSTALLED ANGLE SUPPORT REF B 737 SRM 51-40-02<BR><BR>VERIFIED ALL STEPS;[03] CORRECTION FOR STEP#2 TO READ INSTALLED ANGLE SUPPORT AS PER REF B 737 SRM 51-40-02 AND DWG #143A5400 REV:A
CORROSION AFT CABIN R-2 DOOR LOWER SILL INNER CHORD FROM STA 947.75 TO STA 992.8 WL 208.1<[01] REMOVED AND REPLACED AT CABIN R-2 DOOR LOWER SILL NEW INNER CHORD FROM STA 947 TO STA 992.8 WL 208.1 AS PER REF B/737 SRM 51-40-02-0G.;[02] SUMMARY :REMOVED AND REPLACED AT CABIN R-2 DOOR LOWER SILL NEW INNER CHORD FROM STA 947 TO STA 992.8 WL 208.1 AS PER REF B/737 SRM 51-40-02-0G.;[03] SUMMARY :REMOVED AND REPLACED AT CABIN R-2 DOOR LOWER SILL NEW INNER CHORD FROM STA 947 TO STA 992.8 WL 208.1 AS PER REF B/737 SRM 51-40-02-0G.
FWD CABIN WET AREA INTERCOSTAL CRACKED @ UPPER CAP HOLE BETWEEN STA 277AND 294.5 BL0 WL 208.1 MKD DOT<[01] INSTALLED NEW FWD CABIN WET AREA INTERCOSTAL BETWEEN STA 277AND 294.5 BL0 WL 208.1 AS PER SRM 51-40-02-0G-0; DWG 141A5410.;[02] RII VERIFIED
FWD CABIN WET AREA INTERCOSTAL CRACKED @ UPPER CAP HOLE BETWEEN STA 312 AND 328 LBL 46 WL 208.1 MKD DOT<[01] REMOVED AND REPLACED NEW INTERCOSTAL AT FWD CABIN WET AREA BETWEEN STA 312 TO STA 328 LBL-46 WL-208 REF USED B737-7 SRM 51-40-02-0G-0 AND DWG#141A5400;[02] VERIFIED STEP 1.
FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED AROUND FASTENETS HOLES @ LBL 13 BETWEEN STA 380 AND 400 WL 208.1 MKD DOT<[01] REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL AT FWD CABIN WET AREA @ LBL 13'; WATER LINE 208.1 BETWEEN STA 380 AND STA 400 PER B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 143A5400;[02] ** CORRECTION **<BR>REMOVED AND REPLACED FLOOR SUPPORT UPPER CHORD AT FWD CABIN WET AREA @ LBL 13'; WATER LINE 208.1 BETWEEN STA 380 AND STA 400 PER B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING 143A5400;[03] VERIFIED STEP 2.
FWD CABIN WET AREA FLOOR PANEL 221BF AFT EDGE 2EA CRACKS AND MISSING INSERTS MKD DOTS<[01] REPLACED NEW FLOOR PANEL#221BF P.N# 141A5810-729 P.O#2012626. THIS PANEL WILL BE INSTALLED IN CUSTUMER CARD N.R# TTG8Q00L1NB1 PER SRM REF 53-00-50-2R-0 PARA 4.;[02] VERIFIED REPLACEMENT
PANEL 242UF SHOWS UPPER SURFACE LOOSE FIBERS<[01] REPLACED NEW FLOOR PANEL #242UF P.N#147A5810-136 P.O #2012626. THIS PANEL WILL BE INSTALLED IN CUSTUMER CARD N.R# TTG8Q00L1N8Y PER SRM 53-00-50-2R-0.;[02] VERIFIED REPLACED
PANEL 222BF HAS SURFACE FIBERS LOOSE<[01] RECEIVED NEW FLOOR PANEL #222BF. PANEL TO BE INSTALLED ON ITEM #TTG8Q00L1MF8. AS PER B 737 AMM 53-21-00-400-801;[02] VERIFIED RECEIVED NEW FLOOR PANEL #222BF. AND VERIFIED #TTG8Q00L1MF8.
PANEL 241DF SHOWS UPPER SURFACE LOOSE FIBERS<[01] APPLIED REPAIR ON FLOOR PANEL 241 DF; AS PER B737 SRM 53-00-50-2R-1 MATERIAL USED PO 1473815 AND PO.1783720;[02] VERIFIED AND INSPECTED APPLIED REPAIR ON FLOOR PANEL 241 DF; AS PER B737 SRM 53-00-50-2R-1 MATERIAL USED PO 1473815 AND PO.1783720
L/E HORIZONTAL STABILIZER HAS EVIDENCE OF A CRACK AT RIB # 4 FROM I/B LH LEADING EDGE PANEL<[01] SUMMARY=REMOVED CRACKED RIB (#4 FROM I/B) AT L/H HORIZONTAL STABILIZER LEADING EDGE PER B737-800 SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED NEW RIB (#4 FROM I/B) AT L/H HORIZONTAL STABILIZER LEADING EDGE PER B737-800 SRM 51-40-05-0G-0.<BR>INSTALLED NEW #4 RIB AT LEFT HAND HORIZONTAL STABILIZER LEADING EDGE AS PER B 737 SRM 51-40-02-OG-0;[02] VERIFIED REMOVED CRACKED RIB (#4 FROM I/B) AT L/H HORIZONTAL STABILIZER LEADING EDGE PER B737-800 SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED NEW RIB (#4 FROM I/B) AT L/H HORIZONTAL STABILIZER LEADING EDGE PER B737-800 SRM 51-40-05-0G-0.<BR>INSTALLED NEW #4 RIB AT LEFT HAND HORIZONTAL STABILIZER LEADING EDGE AS PER B 737 SRM 51-40-02-OG-0;[03] CORRECTION FOR SUMMARY TO READ.<BR>REMOVED CRACKED RIB (#4 FROM I/B) AT L/H HORIZONTAL STABILIZER LEADING EDGE PER B737-800 SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED NEW RIB (#4 FROM I/B) AT L/H HORIZONTAL STABILIZER LEADING EDGE PER B737-800 SRM 51-40-05-0G-0.<BR>INSTALLED NEW #4 RIB AT LEFT HAND HORIZONTAL STABILIZER LEADING EDGE AS PER B 737 SRM 51-40-02-OG-0 AND DWG# 186A1304 FRAME 1 OF 1.;[04] NEW NR GENERATED TO CAPTURE MISSING MEASUREMENT TABLE REF: TTG8Q00LMBSA;[05] VERIFIED CORRECTION ON STEP 3 AND VERIFIED STEP 4
PANEL 241XF HAS LOOSE FIBERS ON TOP SURFACE<[01] REPLACED NEW FLOOR PANEL # 241XF; P.N#147A5810-18 PO#2012626. THIS PANEL WILL BE INSTALLED IN COSTUMER CARD N.R# TTG8Q00L 1MP9 PER SRM REF 53-00-50-2R-0 PARA 4.;[02] VERIFIED REPLACED
PANEL 242D SHOWS UPPER SURFACE LOOSE FIBERS<[01] RECEIVED NEW FLOOR PANEL (242D) P/N: 147A5810-345; PO# 2012626. REF TASK CARD: TTG8Q00L1MP3 FOR PANEL INSTALLATION.;[02] VERIFIED RECEIVED NEW FLOOR PANEL (242D)
RIGHT HORIZONTAL STAB-FWD UPPER-SLIDING SEAL CRACKED ADJACENT TO AFT HINGE.<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STAB-FWD UPPER-SLIDING SEAL REF AMM 53-31-31.
EXIT INDICATOR LIGHTS INOP AT LH AND RH OVERWING EXIT DOORS<[01] R&RED BATTERY PACK M1694 AND CHARGER FUSE PER AMM 33-51-06.
EXIT INDICATOR LIGHTS INOP AT LH AND RH OVERWING EXIT DOORS<[01] R&RED BATTERY PACK M1694 AND CHARGER FUSE PER AMM 33-51-06.
OVERHEAD EMERGENCY EXIT SIGN COVER MISSING. LIGHTS WORK. FOUND AND REINSTALLED MISSING SIGN COVER IAW AMM 33-51-01. EMERGENCY LIGHTS TEST GOOD.
OVERWING EMERGENCY EXIT SIGN FELL OFF / [01] RESECURED OVERWING EMERGENCY EXIT SIGN LENS PER AMM 33-51-03
RIGHT MLG FWD TRUNNION SUPPORT FITTING LOWER O/B LUG OUTER FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA NO: 1-A57-3246 REV 12
LT & RT FWD OVERWING EMERGENCY EXIT FLOOR IDENTIFIERS INOP / REMOVED AND REPLACED BATTERY PACK M1694 PER AMM 33-51-06. OPS CK GOOD. POS OVERWING: P/N OFF/ON: D717-01-100S/N OFF: 208601 S/N ON: 108537
LH WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD END LOWER SURFACE / REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22. RIG AND OPS CHECK GOOD.(SA-M 326 ATTACHED: A1303810)POS: L/HPN OFF/ON: 113A3700-25 SN OFF: 003991 SN ON: 004420
RH WING OUTBOARD AFT FLAP LOWER SURFACE INBOARD END DELAMINATED / REMOVED & REPLACED R/H O/B AFT FLAP PER AMM 27-51-22(SA-M 326 ATTACHED: A1303821)POS: RH TAG: 261998PN OFF: 113A3700-26 SN OFF: 003993PN ON: 113A3700-26 SN ON: S1310-12
FWD SERVICE DOOR HANDLE LOOSE / TIGHTENED FWD SERVICE DOOR HANDLE PER AMM 20-50-11 & MT 725-61-06AMT 117477INSP 52251
EMERGENCY LIGHT COVER MISSING BETWEEN ROWS 3ABC + 4ABC ( NEFITEMS LISTED IN MEL APPENDIX 25-10 NON-ESSENTIAL EQUIPMENT & FURNISHINGS (NEF) ) ( NEF ITEMS LISTED IN MEL APPENDIX 25-10 NON-ESSENTIAL EQUIPMENT & FURNISHINGS (NEF) ) / INSTALLED LIGHT COVER ON EMERGENCY LIGHT BETWEEN ROWS 3ABC & 4ABC PER AMM 33-51-03CL# 84994
EMERGENC EXTI LIGHT ABOVE L1 DOOR; INOP / REMOVED AND REPLACED FWD LEFT EMERGENCY BATTERY PACK AND CHARGER PER AMM 33-51-06INSP 44444
F/O'S AFT INBE SEAT TRACK WORN / REMOVED AND REPLACED F/O'S AFT INBD. SEAT TRACK PER AMM 25-11-00INSP 44444
FORWARD GALLEY EMERGENCY EXIT SIGN LOOSE. / REINSTALLED FORWARD ENTRY DOOR EMERGENCY EXIT SIGN PER AMM.
EVIDENCE OF DENT ON AFT CARGO DOOR SKIN 34" FROM AFT EDGE AND 22" FROM TOP TRANSFERRED FROM NRC Y120008 FOR RE-EVALUATION. / AFTER EVALUATING DENT FOUND DENT TO BE 1.1" WIDE AND .054 DEEP. W/Y=20. THIS FOUND TO BE LARGER THAN THE LIMITS ALLOWED PER SRM 52-30-01. FOUND NO LOOSE OR MISSING FASTNER, AND NO CREASES GOUGES OR CRACKS. A INSPECTION OF THE DENT FOR CORROSION AND CRACKS AFTER EACH 1500 FLIGHT HOUR INTERVAL OR MORE FREQUENTLY, APPLIED DENT DOT PER MM 52-03-01 TRANSFERRED TO LOG PAGE 0096038E.
FLIGHT ATTENDANT REPORTS 2 FLASHLIGHTS INOP. / R&R BATTERYS ON 2 EA FLASHLIGHTS FOR AFT GALLEY PER AMM 25-64-00.
FORWARD CARGO COMPARTMENT FLOOR PANEL 120AF IS CORRODED / REPLACED FORWARD CARGO COMPARTMENT FLOOR PANEL 120AF IAW IPC 25-52-10-17 P/N 453A1610-14. OUT OF LIMITS IAW SRM 53-00-53-1A-1 DAMAGE MORE THAN 2' DIAMETER
R1 CREASE BEAM CORRODED FROM STA 312 TO 328 RBL 59 WL208 / REMOVED CORROSION ON R1 DOOR SURROUND CREASE BEAM ATTACH ANGLE STA 312 TO STA 328 RB 59 W 20; 100% MATERIAL LOSS; OUT OF LIMITS IAW SRM 53-10-15-1A-2. REMOVED AD REPLACED CREASE BEAM ATTACH ANGLE IAW SRM 51-40-02-0G--0 AND BOEING DWG 141A8310 REV -
R1 CREASE BEAM ATTACHING ANGLE CORRODED FROM STA 312 TO 328 RBL 59 WL208 / REMOVED CORROSION ON R1 DOOR SURROUND CREASE BEAM ATTACH ANGLE STA 312 TO STA 328 RB 59 W 20; 100% MATERIAL LOSS; OUT OF LIMITS IAW SRM 53-10-15-1A-2. REMOVED AD REPLACED CREASE BEAM ATTACH ANGLE IAW SRM 51-40-02-0G--0 AND BOEING DWG 141A8310 REV -
R1 CREASE BEAM ATTACHING ANGLE CORRODED BETWEEN BS. 312 TO BS. 328, RBL 59. R & R THE CREASE BEAM ATTACH ANGLE IAW SRM AND DWG.
R1 CREASE BEAM CORRODED BETWEEN BS. 312 TO BS. 328, RBL 59. R & R CREASE BEAM ATTACH ANGLE IAW SRM AND DWG.
FWD CARGO RBL 24 STA 500I SIDE WALL ATTACH POINT HAS CORROSION AS MARKED. / REMOVED AND REPLACED FWD CARGO RBL 24 STA 500I SIDEWALL ATTACH POINT IAW SRM 51-40-02-0G-0; DWG 143A9481 ID: 0017 REV - . OUT OF LIMITS NO WRITTEN LIMITS FOUND IN SRM
AFT CARGO COMPARTMENT FORWARD SHIELD CORRODED BETWEEN BS. 767 TO BS. 787. REPAIRED SHIELD IAW SRM AND DWG.
AFT CARGO COMPARTMENT FLOOR BOARD SUPPORT CORRODED BETWEEN BS. 790 TO BS. 810, RBL 14. / R&R FLOOR BOARD SUPPORT IAW SRM.
AFT CARGO COMPARTMENT FLOORBOARD SUPPORT RBL 20 TO LBL 10 STA 947 HAS CORROSION. / REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOORBOARD SUPPORT RBL 20 - LBL 10 STA 947 IAW SRM 51-40-02-0G-0, DWG 149A8110 ID 6007 REV A. FOUND TO BE OUT OF LIMITS NO WRITTEN LIMITS IN SRM.
AFT CARGO COMPARTMENT FLOOR BOARD SUPPORT RBL 14 STA 790 TO STA 810 HAS CORROSION AS MARKED. / AFT CARGO COMPARTMENT FLOOR BOARD SUPPORT RBL 14 STA 790 TO STA 810 CORROSION BLENDED AND FOUND TO BE 'OUT OF LIMITS' AT ORIGINAL =.080' REMOVED=.040' REMAINING=.040' IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED FLOOR BOARD SUPPORT WITH SPLICE AT STA 747+11 IAW SRM 53-00-53-2R-3
AFT CARGO COMPARTMENT FWD SHIELD STA 767 TO STA 787 HAS CORROSION AS MARKED. / REMOVED CORROSION FROM AFT CARGO COMPARTMENT FWD SHIELD STA 767 TO 787 AND CHECKED LIMIT FOUND TO BE OUT OF LIMIT ORIG 'T' .050 REMAIN .027' LOSS .023'; LOCATED AND DRILLED NEW PARTS INSTALLED SHIELD IAW SRM 51-40-02-0G; SRM 53-00-53-1A-2 SRM 51-10-02-0G; SRM 51-40-05; AND DWG 146A8127 REV - ATAG #WN7041
FWD CARGO R/H Z ANGLE HAS CORROSION AT FASTENER HOLES FROM STA 500B + 10 TO STA 500I AS MARKED.; WL 161 RBL 21. / REMOVED AND REPLACED FWD CARGO R/H Z ANGLE STA 500B + 10' TO 500I IAW SRM 51-40-02-0G-0; DWG 143A7500 ID: 0075 REV - REMOVED CORROSION IAW SRM 51-10-02-0G-0 VERIFIED 10X GLASS; OUT OF LIMITS IAW SRM 53-00-53-1A-2 ORIGINAL 'T' .040 LOSS OF .013 REMAINING .027 TOOL 36647 DUE 6/7/20. APPLIED CIC IAW AMM 51-21-91-620-802
AFT CARGO COMPARTMENT FLOOR PANEL# 140CF UPPER SURFACE CORRODED. / REPLACED AFT CARGO COMPARTMENT FLOOR PANEL 140CF IAW IPC 25-52-10-19 P/N 143A2610-18. OUT OF LIMITS IAW SRM 53-00-53-1A-1 MORE THAN 2' DIAMETER OF DAMAGE.
AFT CARGO COMPARTMENT STA 790-847 RBL 29 WL 158; THRESHOLD WEB IS CORRODED. / REMOVED & REPLACED CORRODED AFT CARGO COMPARTMENT THRESHOLD WEB WITH NEW REF B737 SRM 51-40-02; DWG 146A8123 REV C. BLEND OUT FOUND OUT OF LIMITS ON OLD WEB WITH .045' ORIGINAL 'T'; .036 REMAINING 'T' AND .10T MAX ALLLOWABLE LOSS.
AFT CARGO COMPARTMENT FLOOR PANEL# 140BF UPPER SURFACE CORRODED. / REPLACED AFT CARGO COMPARTMENT FLOOR PNL 140BF IAW IPC 25-52-10-19 P/N 453A2610-32. OUT OF LIMITS IAW SRM 53-00-53-1A-1 DAMAGE MORE THAN 20' IN LENGTH.
AFT CARGO COMPARTMENT THRESHOLD WEB CORRODED BETWEEN BS. 790 TO BS. 847, RBL 29. R & R THE WEB IAW SRM & DWG.
FWD. CARGO DOOR; FWD. CORNER SCUFF PLATE CRACKED. / RECEIVED NEW FWD CARGO DOOR; FWD CORNER SCUFF PLATE PN 143A8331-3 (WN3634); REMOVED AND REPLACED FWD CAROGO FWD CORNER SCUFF PLATE IAW 737 AMM 53-11-02-420
FWD. CARGO DOOR AFT CORNER SCUFF PLATE CRACKED. / REMOVED AND REPLACED FWD CARGO DOOR AFT CORNER SCUFF PLATE IAW 737 AMM 53-1-02-420
AFT R2 EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.
ON CLIMBOUT OBSERVED AN N1 RPM SPLIT OF APPROX. 5% #2 ENGINE WAS LOW. COULD NOT MANUALLY INCREASE THRUST ON NR 2. R&R MAIN FUEL PUMP PER MT.
ON CLIMBOUT OBSERVED AN N1 RPM SPLIT OF APPROX. 5% #2 ENGINE WAS LOW. COULD NOT MANUALLY INCREASE THRUST ON #2. / R&R HYDRO MECHANICAL UNIT PER MT.
SUPPLEMENTAL INFORMATION, RT SIDE EMERGENCY LIGHT AT ROW 25 INOP. R&R BATTERY PACK PER AMM.
CENTER OVERHEAD EXIT SIGN (FACING AFT) MISSING. INSTALLED LENS PER MM.
AIR RETURN, WHEEL WELL FIRE AND FIRE BELL ACTIVATED, LIGHT EXTINGUISHED WHILE RETURNING TO BWI. WHEEL WELL FIRE AND FIRE BELL AGAIN AFTER LANDING DURING TAXI IN. R&R WHEEL WELL OVERHEAT DETECTOR PER MM.
AIR RETURN, WHEEL WELL FIRE AND FIRE BELL ACTIVATED, LIGHT EXTINGUISHED WHILE RETURNING TO BWI. WHEEL WELL FIRE AND FIRE BELL AGAIN AFTER LANDING DURING TAXI IN. R&R OVERHEAT DETECTOR CONTROL UNIT PER MM.
R1 DOOR EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.
R2 DOOR SLIDE ASSEMBLY OUT OF POSITION. R&R SLIDE PER MT.
RT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED / R AND R RT HORIZONTAL STAB UPPER FWD SLIDING SEAL PER AMM 53-31-31AMT 114417INSP 43511
LT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / REMOVED AND REPLACED LT HORIZ STAB UPPER FWD SLIDING SEAL PER AMM 53-31-31AMT 124025INSP 43511
R1 DOOR SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.
BAFFLE CRACKED BETWEEN BS 500F TO 500G, RBL 25. REPAIRED THE BAFFLE IAW EA AND ER.
BAFFLE CRACKED RBL25 BS 500F-500G / REPAIRED CRACKED BAFFLE AT BS 500F-500G RBL 25 PER REPAIR - 53EA -004337 AND ER 17-04470 REV IR
BAFFLE CRACKED RBL25 BS 500G-500H / REMOVED AND REPLACED BAFFLE AT STA 500G-500H RBL25 IAW SRM 51-40-02-0G-0 AND BEOING DWG 143A7505 SH108 REV -
CRACK IN STANCHION CLIP AT STA867;LBL10; WL167 / REMOVED AND REPLACED STANCHION CLIP AT STA 867; LBL10; WL167 WITH NEW CLIP IAW SRM 51-40-02-0G-0 AND DWG #149A8102.
***CORROSION*** ON FLOOR/SIDEWALL FWD CAP AT STA 792;RBL14-20 WL165 / REMOVED CORROSION ON FWD CAP AT STA 792 I.A.W. SRM 51-10-02-0G-0. STEPS 15A-1 THRU 6A. MECHANICALLY MEASURED AREA TO BE 6.3' X 2.0' X .022' FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS I.A.W. SRM 51-10-02-0G-0; STEP 9C. REMOVED CAP I.A.W. AMM 25-52-10-000-801 INSTALLED NEW CAP P/N 453A2611-1 LOT #5061264 I.A.W. AMM 25-52-10-400-801.
***CORROSION*** ON FLOOR/SIDEWALL FWD CAP AT STA 847;RBL14-20 WL165 / REMOVED CORROSION ON FWC CAP AT STA847 I.A.W. SRM 51-10-02-0G-0 STEP 15.A.0 THRU 6A. MECHANICALLY MEASURED AREA TO BE 5.0' X 1.5' X .007. FOUND TO BE OUT OF LIMITS DO TO NO LIMITS I.A.W. SRM 51-10-02-0G-0 STEP 9C. REMOVED CAP I.A.W. AMM 25-52-10-000-801. INSTALLED NEW CAP P/N 452A2611-2 LOT #5061264 I.A.W. AMM 25-52-10-400-801.
FLOOR/SIDEWALL FORWARD CAP CORRODED AT BS 847, BETWEEN RBL14 TO RBL 20. R&R CAP IAW SRM.
FLOOR SIDEWALL FORWARD CAP CORRODED AT BS 792, BETWEEN RBL 14 TO RBL 20. R&R CAP IAW SRM.
***CORROSION*** AFT CARGO; L/H FLOOR TO SIDEWALL SUPPORT CORRODED BS 727I TO 78O LBL25 / REMOVED CORROSION L/H FLOOR SIDEWALL SUPPORT IAW SRM 51-10-02-0G-0; FOUND TO BE OUT OF LIMITS AT 100% IAW SRM 53-00-53-1A-2; REMOVED DAMAGED AREA OF SIDEWALL SUPPORT BS 727I TO 780 LBL25 PER SRM 53-00-53-2R-5; AND SRM 51-40-02-0G-0; FABRICATED REPAIR PARTS IAW SRM 53-00-53-2R-5; TREATED & PRIMED REPAIR PARTS IAW AMM-51-21-41-370-802 & 51-21-72-370-804; INSTALLED REPAIR PARTS IAW SRM 53-00-53-2R-5 & SRM 51-40-02-0G-0; USING MAT BAC1496-377 LOT# 5051578
***CORROSION*** AFT CARGO; R/H FLOOR TO SIDEWALL SUPPORT CORRODED BS 727F TO 76O RBL25 / REMOVED R.H ZEE CHANNEL FROM STA. 727F+10' TO 760. REPLACED DAMAGED SECTION WITH BAC1496-377 7075-T6 LOT# 5051578 IAW SRM 53-00-53-2R-5; BOEING DWG 146A7502; IPC 53-42-11-26. SRM 51-40-02-0G-0;4 AND 7 ALODINED AND PRIMED IAW AMM 51-21-41-370-802;3. AMM 51-21-72-370-804;5 IN ANI AREA 1'X1'X.010 ORIG. T=.040 FOUND TO BE OUT
L/H MLG WHEEL WELL FWD WALL VAPOR BARRIER CRACKED / L/H MLG WHEEL WELL FWD WALL VAPOR BARRIER CRACK REPAIRED IAW SRM 57-10-10-2R-2 AND IAW SRM 51-70-04-2R-10.
***CORROSION*** FORWARD CARGO ; LOWER BULKHEAD RAIL CORRODED BS 500I RBL 9 TO RBL21 / REMOVED AND REPLACED FWD CARGO AFT BULK HEAD LOWER RAIL DUE TO CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS BLENDED DAMAGE AN AREA OF 11.0'W X 1.5'L X .015'D INSTALLED NEW LOWER RAIL PER SRM 51-40-02-0G-0 AND BOEING DWG #143A9481; REV A; 143A7902 REV -. 72385U 10/08/2017
***CORROSION*** FWD CARGO. LH FLOOR TO SIDEWALL SUPPORT CORRODED BS 500C+12 TO 520 / REMOVED CORROSION IN AREA OF .75' X .75' GROUND MULTIPLE FASTENER HOLES. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. RMOVED CORRODED SECTION OF LH FLOOR TO SIDEWALL SUPPORT BS000C412 TO 520 & INSTALLED REPLACEMENT SECTION AND SPLICE IAW SRM 53-00-53-2R-6 AND SRM 51-40-02
***CORROSION*** FWD CARGO. RH FLOOR TO SIDEWALL SUPPORT CORRODED BS 500A+8 TO 520 / REMOVED AND REPLACED R/H FWD CARGO FLOOR TO SIDEWALL SUPPORT FROM STA 500A-520 IAW SRM 51-40-02-0G-0; SRM 53-00-53-2R-5; AND BOEING DWG 143A7500 5H34 REV-
FORWARD CARGO RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A+8 TO BS 520. R&R SUPPORT IAW SRM AND DWG.
FORWARD CARGO LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500C+12 TO BS 520. R&R SUPPORT IAW SRM.
FORWARD CARGO LOWER BULKHEAD RAIL CORRODED AT BS 500I, BETWEEN RBL 9 TO RBL 21. R&R BULKHEAD RAIL PER SRM AND DWG.
RT MAIN LANDING GEAR WHEEL WELL FORWARD WALL VAPOR BARRIER CRACKED. REPAIRED BARRIER PER SRM.
AFT CARGO LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727I TO BS 780, LBL 25. R&R SUPPORT IAW SRM.
AFT CARGO RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727F TO BS 760, RBL 25. R&R ZEE CHANNEL IAW SRM & DWG.
LT MAIN LANDING GEAR WHEEL WELL FORWARD WALL VAPOR BARRIER CRACKED. REPAIRED BARRIER IAW SRM.
R/H MLG WHEEL WELL FWD WALL VAPOR BARRIER CRACKED IN TWO PLACES / REPAIRED CRACKS IN TWO PLACES ON R/H MLG WHEEL WELL FWD WALL VAPOR BARRIER PER SRM 57-10-10-2R-2 AND SRM 51-70-04-2R-10
FORWARD CARGO GUSSET CRACKED AT BS 500I, STR 19R. R&R GUSSET IAW SRM AND DWG.
LT WING FIXED TRAILING EDGE CRACKED ANGLE BRACKET ON OUTBOARD EDGE. R&R BRACKET IAW SRM.
CEILING PANEL EMERGENCY EXIT LIGHT IDENTIFIER SIGN WIRING OUT OF POSITION. REPOSITIONED WIRE PER SIP IAW AMM.
R/H WING #8 SLAT O/B END LOWER SKIN OF T/E WEDGE DELAMINATED. DELAM 3' X 2' 2 1/4 INCH FROM L/E 3 1/2' FROM T/E AND .300 FROM O/B END OF T/E WEDGE / C/W TIME LIMITED ACTION REF REPAIR-57EA-04007- PER ENGINEERING-REINSPECTION ARE REF INSP-57EA-04007 & PERMANENT REPAIR ACCOMPLSHED ON REPAIRE-57EA-04009AMT 20231
RIGHT WING NR 8 SLAT OUTBOARD END LOWER SKIN OF TRAILING EDGE WEDGE DELAMINATED. REPAIRED THE SKIN IAW EA.
LT ENGINE TE ASSY IN LOWER PYLON AFT FAIRING ASSY OB HALF IS CRACKED EXTENDING INTO THE OB FLANGE RADIUS. / REPAIRED PER 51-40-02 (INSP 11803) SEE ATTACHED SAM 326 A787986
R1 DOOR EMERGENCY EVAC SLIDE COVER PLASTIC LENS LOOSE. SECURED COVER IAW AMM.
LT EMERGENCY LIGHT LENS CRACKED BETWEEN ROW 8 TO ROW 12. R&R LENS IAW AMM.
LT EMERGENCY LIGHT LENS CRACKED BETWEEN ROW 15 TO ROW 27. R&R LENS IAW AMM.
RIGHT FORWARD OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY CHARGER IAW AMM.
RIGHT FORWARD OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE LIGHT IAW MM.
RIGHT OVERHEAD EMER LIGHT LENS MISSING AT ROW 25. R & R LIGHT ASSEMBLY IAW AMM.
OVERHEAD EXIT LIGHT LENS MISSING NEXT TO SEAT 25D. INSTALLED LENS IAW MM.
OVERHEAD EXIT LIGHT LENS MISSING NEXT TO SEAT 11D. INSTALLED LENS IAW MM.
RIGHT OVERHEAD EMER LIGHT COVER MISSING AT ROW 14. R & R COVER ASSEMBLY IAW AMM.
RIGHT EMER LIGHT COVER MISSING AT ROW 14. INSTALLED COVER ASSEMBLY IAW AMM.
R1 DOOR EMER EXIT LIGHT COVER BROKEN. R & R LIGHT ASSEMBLY IAW AMM.
R2 DOOR EMERGENCY EVAC SLIDE GIRT OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MM.
FORWARD RIGHT PHOTO LUMINESCENT STRIPS CRACKED. R & R STRIP IAW AMM.
FORWARD LEFT PHOTO LUMINESCENT STRIPS CRACKED. R & R STRIP IAW AMM.
EMERGENCY LIGHT LENS MISSING AT 27 ABC. INSTALLED LENS IAW MM.
FORWARD ENTRY DOOR FWD BULKHEAD EXIT LIGHT COVER FELL OFF. R & R COVER IAW SIP.
AFT LT LAVATORY EEPLS CRACKED. R & R EEPLS IAW AMM.
RIGHT EEPLS CRACKED AT ROW 18. R & R EEPLS IAW MM.
RIGHT EEPLS CRACKED AT ROW 1. R & R EEPLS IAW MM.
LEFT EEPLS CRACKED AT ROW 1. R & R EEPLS IAW MM.
AFT RT LAVATORY EEPLS CRACKED. R & R EEPLS IAW AMM.
R1 DOOR EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.
MID CABIN OVERHEAD EXIT SIGN LENS MISSING. INSTALLED LENS IAW MM.
FWD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS IAW MM.
DECLARED EMERGENCY - THE GLARE SHIELD FIRE WARNING LIGHT CAME ON TWICE WITH NO OTHER ASSOC FIRE LIGHTS. REMOVED AND REPLACED LAMPS PER MM.
R1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.
DECLARED EMERGENCY -- 20 MINS INTO FLIGHT SMELLED ELECTRICAL ODOR IN COCKPIT AND CABIN. REMOVED AND REPLACED RECIRC HEPA FILTER AND RECIRC FAN PER MM.