N8697C
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 | 2019-05-25 – 2019-05-25 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2019-05-25 – 2019-05-25 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
L1 DOOR FWD GIRT BAR FITTING MISSING. INSTALLED L1 DOOR FWD FLOOR-MOUNTED ESCAPE SLIDE BRACKET IAW AMM 25-66-02-400-801. VERIFIED INSTALLED SERVICEABLE L1 DOOR FWD FLOOR-MOUNTED ESCAPE SLIDE BRACKET IAW AMM 25-66-02-400-801.
AFT COVE CEILING PANEL EMERGENCY LIGHT LENS MISSING. INSTALLED LENS IAW B737-NG AMM 33-51-03-960-803-NG; NO OPS CHECK REQUIRED. INSTALLED LENS IAW AMM 33-51-03-960-803-NG; NO OPS CHECK REQUIRED.
FORWARD GALLEY FLASHLIGHT WILL NOT TEST. R & R THE FWD GALLEY FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.
LIGHT COVER BROKEN AT ROW 10 CABIN AISLE EMERGENCY LIGHT HOUSING MOUNTED IN THE OVERHEAD BIN BULLNOSE. OK TO CONTINUE IAW MEL 33-15-02 SP1. REMOVED AND REPLACED ROW 10 DEF EMERGENCY LIGHT LENS COVER REFERENCING AMM 33-51-03. OPS CHECK GOOD.
AFT SERVICE DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED AFT SERVICE DOOR EMERGENCY EXIT SIGN LENS PER AMM 33-51-01.
LT AND RT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED PER AMM 33-51-06-960-805-NG.
ESCAPE HATCH; RIGHT SIDE PANEL 843 ESCAPE STRAP RED VELCRO COVER NOT ATTACHED TO DOOR SURROUND FRAME STRUCTURE.<[01] SECURED ESCAPE STRAP RED VELCRO COVER TO DOOR SURROUND FRAME STRUCTURE PER SOPM 20-50-12.;[02] VERIFIED SECURED ESCAPE STRAP RED VELCRO COVER TO DOOR SURROUND FRAME STRUCTURE PER SOPM 20-50-12.
ESCAPE HATCH; LEFT SIDE PANEL 833 CLOSING STRAP BEZEL ATTACHED TO DOOR LINER IS BROKEN. SECURED CLOSING STRAP BEZEL TO THE LEFT OVERWING EXIT DOOR 833 PANEL PER SOPM 20-50-12.
ESCAPE HATCH; LEFT SIDE PANEL 833 ESCAPE STRAP RED VELCRO COVER NOT ATTACHED TO DOOR SURROUND FRAME STRUCTURE. SECURED ESCAPE STRAP RED VELCRO COVER TO DOOR SURROUND FRAME STRUCTURE PER SOPM 20-50-12.
CRACK FOUND AT BS 663, RBL 34, ON VAPOR BARRIER ATTACH ANGLE. REMOVED VERTICAL ATTACHED FASTENERS ON RT 663 CHORD IAW SRM 51-40-02. REMOVED FUEL TANK FASTENERS AT BS 663 ON VAPOR BARRIER ATTACH ANGLE RBL 6 TO RBL 43 IAW SRM 51-40-02. REMOVED AND REPLACED VAPOR BARRIER ATTACH ANGLE IAW SRM 51-40-02 AND EA 25-157-02319 AND EA 25-157-02305. REF DWG 111A1000. FUEL TANK FASTENERS IN CONJUNCTION WITH VAPOR BARRIER ATTACH ANGLE LEAK CHECKED IAW AMM 28-11-00. NO LEAKS NOTED.
NUMBER 1 ENGINE INBD FAN COWL ANGLE AT AFT SIDE OF OIL SERVICE DOOR OPENING CRACKED AT UPPER CORNER. REMOVED AND REPLACED THE NR 1 ENGINE INBD FAN COWL WEB AT OIL SERVICE DOOR IAW AMM 51-40-02.
HFEC SHOWS EVIDENCE OF CRACK IN WIGGLE PLATE ON FWD INBD CORNER OF PANEL 551EB ATTACH POINT.<[01] HFEC WIGGLE PLATE PER NDT MANUAL 51-00-00 PROCEDURE 23;[02] REMOVED DAMAGED WIGGLE PLATE PER SRM 51-40-02.;[03] REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02.;[04] INSPECTED WORK PERFORMED REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02.
LEFT WING OTBD AFT FLAP HAS LARGE AREA OF DELAMINATION ON UPPER SURFACE ON INBD CORNER. REMOVED LT WING OTBD AFT FLAP IAW AMM 27-51-22. INSTALLED LT WING OTBD AFT FLAP IAW AMM 27-51-22.
BOTH AFT GALLEY EXIT SIGN LENSES MISSING<[01] REINSTALLED GALLEY EXIT SIGN LENSES IAW AMM 33-51-01
L1 DOOR SLIDE IS COMING OUT OF ITS CASE<[01] REPOSITION L1 DOOR ESCAPE SLIDE IAW MT 725-61-06
AFT LEFT EMERGENCY LIGHTS BATTERY PACK INOP. R&R BATTERY PACK PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.
AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C L/H IS INOP. REMOVED AND REPLACED AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C L/H PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.
FWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 500C L/H IS INOP. REMOVED AND REPLACED FWD CABIN EMERGENCY LIGHT POWER PACK AT STA 500C L/H PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.
FWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 500C R/H IS INOP. REMOVED AND. REPLACED FWD CABIN EMERGENCY LIGHT BATTERY PACK AT STA 500 R/H PER AMM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.
AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C RT IS INOP. REMOVED AND REPLACED AFT CABIN EMERGENCY LIGHT BATTERY PACK AT STA 727C R/H PER AMM 3-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06. EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.
PASSENGER CABIN FLOOR PANEL SUPPORT CRACKED ATTACH FASTENER STA. 540; LBL 2.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
PASSENGER CABIN FLOOR PANEL SUPPORT CRACKED ATTACH FASTENER STA. 540; RBL 2.<[01] REMOVED AND REPLACED PER SRM 51-40-02.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1
FLOOR STRUCTURE INTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 25 HAS CORROSION ON FWD/RH EDGE<[01] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; RBL 25. ORIGINAL THICKNESS OF 0.084; MATERIAL REMOVED .024; REMAINING THICKNESS IS 0.060. INTERCOSTAL FOUND TO BE OUT OF LIMITED PER SRM 53-70-51-1A-1.;REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL (P/N 147A5660U3) IAW SRM 51-40-02.
FWD ENTRY DOOR: THRESHOLD SUPPORT ANGLE LBL 61 FROM STA 312-348; HAS CORROSION AT SEVERAL NUTPLATES. (M) (M)<[01] REMOVED CORROSION PER SRM 51-10-02.;[02] INSPECTED DAMAGE REMOVAL;[03] TREATED AND PRIMED PER SRM 51-20-02.;[04] TREATED AND PRIMED PER SRM 51-20-01.
FWD ENTRY DOOR: THRESHOLD SUPPORT ANGLE LBL 58 FROM STA 312-348; HAS CORROSION AT SEVERAL NUTPLATES AND RADIUS AREA. (M)<[01] REMOVED CORROSION PER SRM 51-10-02.;[02] INSPECTED DAMAGE REMOVAL;[03] TREATED AND PRIMED PER SRM 51-20-02.;[04] TREATED AND PRIMED PER SRM 51-20-02.;[05] TREATED AND PRIMED PER SRM 51-20-01.
FLOOR SUPPORT MACHINED INTERCOSTAL LOCATED BETWEEN STAS 927-947; LBL 51 HAS CORROSION AT STA 946.<[01] REMOVED FLOOR SUPPORT MACHINED INTERCOSTAL LOCATED BETWEEN STA?S 927-947; LBL 51 PER SRM 51-40-02;[02] REMOVED LIGHT SURFACE CORROSION ON FLOOR SUPPORT MACHINED INTERCOSTAL LOCATED BETWEEN STA?S 927-947; LBL 51. ORIGINAL THICKNESS OF 0.074; MATERIAL REMOVED .001; REMAINING THICKNESS IS 0.073. INTERCOSTAL FOUND TO BE WITHIN LIMITED PER SRM 53-70-51-1A-1.;[03] DISREGARD STEP 2.<BR><BR>REMOVED LIGHT SURFACE CORROSION ON FLOOR SUPPORT MACHINED INTERCOSTAL LOCATED BETWEEN STA?S 927-947; LBL 51. ORIGINAL THICKNESS OF 0.70; MATERIAL REMOVED .023; REMAINING THICKNESS IS 0.047. INTERCOSTAL FOUND TO BE OUT LIMITED PER SRM 53-70-51-1A-1.;[04] LOCATED AND DRILLED FASTENER HOLES ON NEW INTERCOSTAL PER SRM<BR>51-40-05. EXCEPT FASTENER HOLES ATTACHING TO FLOOR STRUCTURAL 947 .;[05] INSTALLED INTERCOSTAL PER SRM 51-40-02.;[06] VERIFIED. LOCATED AND DRILLED FASTENER HOLES ON NEW INTERCOSTAL PER SRM<BR>51-40-05. EXCEPT FASTENER HOLES ATTACHING TO FLOOR STRUCTURAL 947.;[07] RII. VERIFIED INSTALLATION OF INTERCOSTAL LOCATED BETWEEN STA?S 927-947; LBL 51 PER SRM 51-40-02.
CORROSION ON AFT CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA 747-767 (MARKED)<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 747-767 ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005; MAX ALLOWED IS 0.004 ?; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] TOOL T010008 S/N 503011WAS NOT USED;[03] SEE WORK CAPTURE # TTG8Q00UALJZ FOR REPLACEMENT OF LH SIDE PLATE;[04] INSPECTED WORK ABOVE
CORROSION ON AFT CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA 727J-747 (MARKED)<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727J-747 ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005; MAX ALLOWED IS 0.004 ?; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] TOOL T010008 S/N 503011WAS NOT USED;[03] SEE WORK CAPTURE # TTG8Q00UALJZ FOR REPLACEMENT OF LH SIDE PLATE;[04] CW
CORROSION ON AFT CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA 727I-727J (MARKED)<[01] REMOVED CORROSION FROM AFT CARGO LEFT SIDE PLATE FROM STA 727I-727J ORIGINAL MATERIAL THICKNESS IS 0.040?; MAX MATERIAL LOSS IS 0.005; MAX ALLOWED IS 0.004 ?; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] TOOL T010008 S/N 503011WAS NOT USED;[03] CUT OUT DAMAGED SECTION OF THE LH SIDE PLATE FROM STA 727F+10 TO STA 787+10 FOR REPAIR PER SRM 53-00-53-1A-2;[04] LOCATED AND DRILLED NEW LH SIDE PLATE PER SRM 51-40-02;[05] COUNTERSUNK LH SIDE PLATE PER SRM 51-40-08.;[06] LOCATED AND DRILLED NEW LH SIDE PLATE FROM STA.727 - STA.847 PER SRM 51-40-02.;[07] RII. VERIFIED. LOCATED AND DRILLED NEW LH SIDE PLATE FROM STA.727 - STA.847 PER SRM 51-40-02. SIGN OFF FOR CORRECTIVE ACTION #6 ONLY.;[08] RII. VERIFIED COUNTERSUNK LH SIDE PLATE PER SRM 51-40-08. NEW LH SIDE PLATE FROM STA.727 - STA.847. SIGN OFF FOR CORRECTIVE ACTION #5 ONLY.;[09] RII. OK TO INSTALL NEW LH SIDE PLATE FROM STA 727 - STA 847.;[10] INSTALLED NEW LH SIDE PLATE FROM STA 727-847 PER SRM 51-40-02;[11] CW
FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 51 HAS CORROSION ON TOP/FWD SURFACE.<[01] REMOVED FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; RBL 51 PER SRM 51-40-02;[02] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; RBL 51. ORIGINAL THICKNESS OF 0.210; MATERIAL REMOVED .009; REMAINING THICKNESS IS 0.201. INTERCOSTAL FOUND TO BE WITHIN LIMITED PER SRM 53-70-51-1A-1.;[03] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; RBL 51. ORIGINAL THICKNESS OF 0.201; MATERIAL REMOVED .063; REMAINING THICKNESS IS 0.138. INTERCOSTAL FOUND TO BE OUT OF LIMITED PER SRM 53-70-51-1A-1.;[04] DISREGARD STEP 2;[05] LOCATED AND DRILLED FASTENER HOLES ON NEW INTERCOSTAL PER SRM<BR>51-40-05. EXCEPT FASTENER HOLES ATTACHING TO FLOOR STRUCTURAL 947 AND LAV MOUNT.;[06] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02;[07] INSPECTED AS REQUIRED. CORRECTIVE ACTION #5 AND #6
UPPER WEB ATTACH ANGLE LOCATED BETWEEN STAS 927-947; RBL 25 HAS CORROSION AT STA 946.<[01] REMOVED CORROSION UPPER WEB ATTACH ANGLE LOCATED BETWEEN STA?S 927-947; RBL 25 . ORIGINAL THICKNESS OF 0.070; MATERIAL REMOVED .019; REMAINING THICKNESS IS 0.051. ANGLE FOUND TO BE OUT OF LIMITED PER SRM 53-70-51-1A-1.;[02] LOCATED AND DRILLED NEW UPPER WEB ATTACH ANGLE (CHORD) BETWEEN STA 927 - 947 RBL 25 PER SRM 51-40-05; TREATED. AND PRIMED BARE METAL PER SRM 51-20-01;[03] INSPECTED C/A #2 LOCATING & DRILLING OF NEW UPPER WEB ATTACH ANGLE (CHORD) BETWEEN STA 927 - 947 RBL 25 PER SRM 51-40-05 & PRIMING OF BARE METAL PER SRM 51-20-01 (RII);[04] INSPECTED C/A #2 LOCATING & DRILLING OF NEW UPPER WEB ATTACH ANGLE (CHORD) BETWEEN STA 927 - 947 RBL 25 PER SRM 51-40-05 & PRIMING OF BARE METAL PER SRM 51-20-01;[05] REMOVED AND REPLACED ANGLE (CHORD) PER SRM 51-40-02;[06] INSPECTED AS REQUIRED. CORRECTIVE ACTION #5
LH OUTBD AFT FLAP LOWER INBD CORNER HAS DELAMINATION ON UPPER AND LOWER SURFACES.<[01] OK TO INSTALL L/H OUTBD AFT FLAP.;[02] OK TO INSTALL AFT OUTBD FLAP;[03] INSTALLED NEW SERVICEABLE L/H O/B AFT FLAP PER AMM 27-51-22.;[04] INSTALLED NEW SERVICEABLE L/H O/B AFT FLAP PER AMM 27-51-22. RII INSPECTION C/W.
FLOOR STRUCTURE INTERCOSTAL LOCATED BETWEEN STAS 947-967; LBL 25 HAS CORROSION ON FWD/LH EDGE<[01] REMOVED FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; LBL 51 PER SRM 51-40-02;[02] REMOVED CORROSION ON FLOOR SUPPORT INTERCOSTAL LOCATED BETWEEN STA?S 947-967; LBL 25. ORIGINAL THICKNESS OF 0.210; MATERIAL REMOVED .048; REMAINING THICKNESS IS 0.162. INTERCOSTAL FOUND TO BE OUT OF LIMITED PER SRM 53-70-51-1A-1.;[03] LOCATED AND DRILLED FASTENER HOLES ON NEW INTERCOSTAL PER SRM<BR>51-40-05. EXCEPT FASTENER HOLE ATTACHING TO FLOOR STRUCTURAL 947 AND LAV MOUNT.;[04] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02. REFERENCE TASK (TTG8Q00U9UHV);[05] INSPECTED AS REQUIRED. CORRECTIVE ACTION #3; #4
CORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500A-500B.(MARKED)<[01] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] LOCATED AND DRILLED NEW TRANSITION ANGLE P/N #143A7501U188 PER SRM 51-40-05 ;OK TO INSTALL;[03] VERIFIED C/A # 1 : ROBERT DENSFORD (TECHNICIAN); 03-JUL-2024 12:01 UTC<BR>BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[04] VERIFIED C/A 2 : TONY NGUYEN (TECHNICIAN); 03-JUL-2024 14:10 UTC<BR>LOCATED AND DRILLED NEW TRANSITION ANGLE P/N #143A7501U188 PER SRM 51-40-05 ;OK TO INSTALL;[05] GRANTED OK TO INSTALL REPLACE SECTION FROM STA 500A TO STA 500 I;[06] REMOVED AND REPLACED RH SIDE PLATE FROM STA 500A TO STA 500I PER SRM 53-00-53-1A-2;AND SRM 51-40-02.;[07] 02 - INSPECTED PER [SRM 53-00-53-1A-2-B00297 (PERMANENT (NON-DENT DAMAGE TYPES))]
CORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500H-500I.(MARKED)<[01] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.;[02] VERIFIED : ROBERT DENSFORD (TECHNICIAN); 03-JUL-2024 14:32 UTC<BR>BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.
CORROSION ON FWD CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA. 500D-500E.(MARKED)<[01] BLENDED AREAS REMOVED .009' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] VERIFIED OUT OF LIMITS;[03] FABRICATED REPAIR PARTS PER SRM 53-00-53-2R-5 AND EA M-22-153-01550.;[04] 02 - INSPECTED PER [SRM 53-00-53-2R-5-B00308 (REPAIR 5 - CARGO COMPARTMENT SIDEPLATE REPAIR BETWEEN FLOOR PANEL SPLICES - PERMANENT)];[05] OK TO INSTALL ALL REPAIR PARTS PER SRM 53-00-53;[06] REPLACED SECTION OF SIDE PLATE FROM STA. 500B+10 TO 500E+10 PER SRM 53-00-53-2R-5 AND EA M-22-153-01550.;[07] 02 - INSPECTED PER [SRM 53-00-53-2R-5-B00308 (REPAIR 5 - CARGO COMPARTMENT SIDEPLATE REPAIR BETWEEN FLOOR PANEL SPLICES - PERMANENT)]
CORROSION ON FWD CARGO COMPARTMENT LH SIDE PLATE BETWEEN STA. 500E-500F.(MARKED)<[01] BLENDED AREAS; REMOVED .010 ' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION REPLACED ON NR# TTG8Q00UA2SG.;[02] BLENDED AREAS; REMOVED .010 ' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION REPLACED ON NR# TTG8Q00UA2SG.;[03] 02 - INSPECTED PER [SRM 53-00-53-1A-2-B00297 (PERMANENT (NON-DENT DAMAGE TYPES))];[04] 02 - INSPECTED PER [SRM 53-00-53-1A-2-B00297 (PERMANENT (NON-DENT DAMAGE TYPES))]
CORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500F-500G.(MARKED)<[01] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.;[02] VERIFIED : ROBERT DENSFORD (TECHNICIAN); 03-JUL-2024 14:17 UTC<BR>BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.
CORROSION ON FWD CARGO COMPARTMENT RH SIDE PLATE BETWEEN STA. 500C-500D.(MARKED)<[01] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.;[03] VERIFIED : ROBERT DENSFORD (TECHNICIAN); 03-JUL-2024 12:31 UTC<BR>BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[04] VERIFIED : ROBERT DENSFORD (TECHNICIAN); 03-JUL-2024 13:46 UTC<BR>BLENDED AREAS REMOVED .005' MATERIAL; FOUND TO BE OUT OF LIMITS LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00UA2QH.
PASSENGER CABIN FLOOR BEAM AT APPROX. BS987 LBL 43 HAS CORROSION AROUND HOLE.<[01] REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] CUT AND REMOVED DAMAGED PART OF FLOOR BEAM IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4.;[03] C/W INSPECTION<BR>CUT AND REMOVED DAMAGED PART OF FLOOR BEAM IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4.<BR>C/W NDT INSPECTION PER 737 NDT PART 6;51-00-00 PROCEDURE 23<BR> 737 NDT PART 6;51-00-00 PROCEDURE 16;[04] FABRICATED/DRILLED ANGLE AND STRAP PER SRM 53-70-51-2R-6.;[05] FLAP PEENED AREA PER SRM 53-70-51-2R-6 AND SOPM 20-10-03.;[06] FABRICATED FILLER PER SRM 53-70-51-2R-6.;[07] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #4; #5 AND #6.;[08] TREATED AND PRIMED PER SRM 51-20-01. OK TO INSTALL.;[09] VERIFIED TREATED AND PRIMED PER SRM 51-20-01. SIGN OFF FOR CORRECTIVE ACTION #8.;[10] RII. OK TO INSTALL REPAIR PARTS. SIGN OFF FOR CORRECTIVE ACTION #8.;[11] INSTALLED REPAIR PARTS AT PASSENGER CABIN FLOOR BEAM AT APPROX. BS987 LBL 43 PER SRM 53-70-51-2R-6.;[12] RII INSPECTED WORK ABOVE;[13] REPAIR COMPLEAT
PASSENGER CABIN FLOOR BEAM BS947 RBL28 HAS SURFACE CORROSION ON TOP SIDE .<[01] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.052IN MATERIAL; REMAINING 0.128IN; FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1..;[02] ENTIRE LENGTH OF FLOOR BEAM UPPER FLANGE FROM LBL 60 - RBL 60 TO BE REMOVED AND REPAIRED PER SRM 53-70-51-2R-5; ALTERNATIVE 1 ON FAULT #TTG8Q00U9S43.;[03] LOCATED; MATCH DRILLED AND DEBURRED NEW FLOOR BEAM PER SRM 51-10-02.;[04] 01 - REMOVED AND REPLACED PER [REFERENCE] 51-10-02 OK TO INSTALL NEW FLOOR BEAM.;[05] INSTALLED FLOOR BEAM STA.947; LBL 60-RBL 60. PER SRM 51-10-02;[06] REMOVED AND REPLACED FLOOR BEAM STA. 947 LBL 60- RBL 60 PER SRM 51-10-02. ALSO; REFERENCE TASK (TTG8Q00U9S43);[07] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #5. REMOVE AND REPLACE OF STA. 947 FLOOR BEAM. REF.#TTG8Q00U9S43 FOR ALL WORK ACCOMPLISHED.
PASSENGER CABIN BS952 LBL25 SCREW HOLE HAS POSSIBLE CORROSION.<[01] REMOVED LIGHT SURFACE CORROSION ON PASSENGER CABIN BS952 LBL25 SCREW HOLE. ORIGINAL THICKNESS OF 0.083; MATERIAL REMOVED .003; REMAINING THICKNESS IS 0.080. INTERCOSTAL FOUND TO BE WITHIN LIMITED PER SRM 53-70-51-1A-1.;[02] SEE WORK CAPTURE # TTG8Q00UA9P8 FOR INTERCOSTAL REPLACEMENT.;[03] INTERCOSTAL REPLACED ON TASK CARD (TTG8Q00UA9P8);[04] INTERCOSTAL REPLACED PER SRM 51-40-02 ON TASK CARD (TTG8Q00UA9P8);[05] INSPECTED AS REQUIRED. CORRECTIVE ACTION #4
PASSENGER CABIN FLOOR BEAM BS947 RBL25 UNDER AND AROUND LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 RBL 25 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.052IN MATERIAL; REMAINING THICKNESS IS 0.128IN. OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] CORRECTIVE ACTION #2 WRITTEN IN ERROR. WRONG N/R CARD.;[04] INSTALLATION OF LAV TIE DOWN FITTING AT STA 947; RBL 25 TO BE ACCOMPLISHED ON FAULT #TTG8Q00U9S43.;[05] FURTHER INSPECTION REVEALED NO CORROSION ON FLOOR BEAM AT STA 947; RBL 25 UNDER OR AROUND LAV TIE DOWN FITTING PER SRM 51-10-02.;[06] ENTIRE LENGTH OF FLOOR BEAM UPPER FLANGE FROM LBL 60-RBL 60 TO BE REMOVED AND REPAIRED PER SRM 53-70-51-2R-5; ALTERNATIVE 1 ON FAULT. #TTG8Q00U9S43.;[07] 02 - INSPECTED PER [SRM 51-10-02-0G-0-B00070 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)]
PASSENGER CABIN FLOOR BEAM BS947 LBL51 UNDER LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 LBL 51 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.100IN MATERIAL; REMAINING THICKNESS IS 0.080IN. OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] REMOVED AND REPLACED FLOOR BEAM STA. 947 LBL 60- RBL 60 PER SRM 51-10-02. ALSO; REFERENCE TASK (TTG8Q00U9S5C);[04] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #3. REMOVE AND REPLACE OF STA. 947 FLOOR BEAM.
PASSENGER CABIN FLOOR BEAM AT APPROX. BS987 LBL 43 HAS CORROSION AROUND HOLE. REMOVED DAMAGE. FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. CUT AND REMOVED DAMAGED PART OF FLOORBEAM IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4. NDT PART 6;51-00-00 PROCEDURE 16. FABRICATED/DRILLED ANGLE AND STRAP PER SRM 53-70-51-2R-6. FLAP PEENED AREA PER SRM 53-70-51-2R-6 AND SOPM 20-10-03. FABRICATED FILLER IAW SRM 53-70-51-2R-6. TREATED & PRIMED PER SRM 51-20-01. INSTALLED REPAIR PARTS ON FLOORBEAM IAW SRM 53-70-51-2R-6.
PASSENGER CABIN FLOOR BEAM BS947 RBL50 UNDER AND AROUND LAV TIE DOWN FITTING HAS POSSIBLE CORROSION.<[01] REMOVED LAV TIE DOWN FITTING FROM STA 947 RBL 50 PER SRM 51-40-02;[02] REMOVED CORROSION. ORIGINAL THICKNESS OF 0.180IN; REMOVED 0.075IN MATERIAL; REMAINING THICKNESS IS 0.105IN. OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] ENTIRE LENGTH OF FLOOR BEAM UPPER FLANGE FROM LBL 60 - RBL 60 TO BE REMOVED AND REPAIRED PER SRM 53-70-51-2R-5; ALTERNATIVE 1 ON FAULT #TTG8Q00U9S43.;[04] 01 - REMOVED AND REPLACED 947 FLOOR BEAM SEE TASK CARD TTG8Q00U9S5C.;[05] VERIFIED
RH WING LEADING EDGE FUEL GAUGE BRACKET HAS CORROSION MARKED<[01] REMOVED AND REPLACED WING REFUEL PANEL PER SOPM 20-50-01 AND MM 28-41-61.REFUELING PANELS OPS CHECKED GOOD PER MM 28-41-61;MM 28-21-81 AND MM 28-21-00;[02] C/W INSPECTION
RIGHT WING O/B AFT FLAP I/B TE DELAMINATED 14 BY 9 INCH. REMEASURE RIGHT WING O/B AFT FLAP FOUND FLAP DELAMINATED 20.6BY 9.5 INCH.<[01] R AND R RIGHT WING O/B AFT FLAP PER AMM 27-51-22.
CENTER FWD EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
AFT GALLEY EMERGENCY FLASHLIGHT WILL NOT TEST. R/H #1 POS. / [01] REMOVED AND REPLACED AFT GALLEY EMERGENCY FLASHLIGHT. PER AMM 25-64-00. OPS CK GOOD.;[02] (CORRECTION TO MATCH LOGPAGE)REMOVED AND REPLACED AFT GALLEY EMERGENCY FLASHLIGHT. RH #1 POS PER AMM 25-64-00. OPS CK GOOD.
R/H AFT EMERGENCY LIGHTING BATTERY PACK WILL NOT CHARGE.<[01] REMOVED AND REPLACED BATTERY PER M/M 33-51-06.
FWD GIRT BAR CAP. SIDE LOOSE<[01] ADJUSTED L-1 DOOR GIRT BAR IAW SIP. NO FURTHER DEFECTS NOTED AT THIS TIME.
F.O. SEAT WILL NOT MOVE FOUND DEFORMATION ON AFT OUTBOARD F/O SEAT TRACK WHICH MAKES MOVEMENT DIFFICULT<[01] R&R FO'S AFT O/B SEAT TRACK IAW AMM 25-11-11
2 AFT CABIN FLASHLIGHTS INOP<[01] R&R SECURITY SEAL PER S.I.P;[02] PERFORMED OPS CHECK OF FLASH LIGHT; OPS CHECK GOOD PER AMM 25-64-00
EXIT SIGN IN MID CABIN BY EMERGENCY EXIT ROW IS MISSING; CEILING / [01] REMOVED AND REPLACED MID-CABIN OVERHEAD EMERGENCY EXIT SIGN HOUSING AND LENS. OPS CHECK GOOD. REF AMM 33-51-01.
ALL EMERGENCY EXIT LIGHTS CONNECTED TO BATTERY PACK M1672 ARE INOP. / [01] REMOVED AND REPLACED BATTERY PACK M1672 AND TEST GOOD IAW AMM 33-51-06-960-805.;[02] REMOVED AND REPLACED BATTERY PACK M1672 AS PER AMM 33-51-06-960-805;[03] VERIFIED CORRECTIVE ACTIONS STEP 1.
ALL EMERGENCY EXIT LIGHTS CONNECTED TO BATTERY PACK M1673 ARE INOP. / [01] REMOVED AND REPLACED BATTERY PACK M1673 AND TEST GOOD IAW AMM 33-51-06-960-805.;[02] CERTIFIED REMOVED AND REPLACED BATTERY PACK M1673 AND PERFORMED GOOD INSTALL TEST AS PER AMM 33-51-06-960-805;[03] VERIFIED CORRECTIVE ACTIONS STEP 1.
ALL EMERGENCY EXIT LIGHTS CONNECTED TO BATTERY PACK M1675 ARE INOP. / [01] REMOVED AND REPLACED BATTERY PACK AND TEST GOOD IAW AMM 33-51-06-960-805.;[02] REMOVED AND REPLACED BATTERY PACK M1675 AND TEST GOOD IAW AMM 33-51-06-960-805.;[03] CERTIFIED ALL WORK AND GOOD INSTALL TEST AS PER AMM 33-51-06-960-805;[04] VERIFIED CORRECTIVE ACTIONS STEP 2.
BREAK PANEL IS CRACKED AT STA 540; BL 0-LBL 25; WL 208. / [01] UPDATED TABLE;[02] REMOVED FLOOR PANEL 231UF PER AMM 53-21-00-000-801;[03] REMOVED BRAKE PANEL AT STA 540 BL0 - LBL 25 WL 208 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW BREAK PANEL AT STA 540 BL0 LBL 25 WL 208 PER SRM 51-40-05-0G-0. OK TO INSTALL;[05] CERTIFIED REMOVAL OF FLOOR PANEL #231UF AND REMOVAL OF BRAKE PANEL AND LOCATED AND DRILLED NEW BREAK PANEL;[06] VERIFIED CORRECTIVE ACTION #4;[07] INSTALLED BREAK PANEL AT STA 540; BL0 LBL 25;WL 208 I.A.W SRM 51-40-02-0G-0. OK TO INSTALL FLOOR PANEL 231UF.;[08] CERTIFIED INSTALLATION OF BREAK PANEL AT STA540 BLO-LBL25 WL 208;[09] VERIFIED CORRECTIVE ACTION #7;[10] INSTALLED FLOOR PANEL 231UF I.A.W AMM 53-21-00-400-801.<BR>TOOL ID: ATS2266 S/N 1703449 DATE: 02/2022 DUE: 02/2023;[11] CERTIFIED INSTALLATION OF FLOOR PANEL #231UF;[12] VERIFIED CORRECTIVE ACTION #10<BR>VERIFIED MEASUREMENTS
AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION BS727F TO BS767 RBL21 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 727I +10 RBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN NUMEROUS 1'X1' AREAS; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2678 DUE 04/2023;[02] VERIFIED ACTION #1;[03] VALIDATED APPLICABILITY OF SRM 53-00-53-2R-5;[04] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E + 10 - BS767; RBL21; WL156 PER SRM 53-00-53-2R-5 STEP 4.B. SRM 51-40-02-0G-0;[05] FABRICATED; LOCATED AND APPLIED CHEMICAL CONVERSION COATING TO ACB FLOOR TO SIDEWALL SUPPORT AT BS727E+10' - BS767; RBL21; WL156 AND SPLICE REPAIR AT BS727E+8' - BS727E+18' USING BAC1496-77#7075T62 LOT # 1477731-1 PER SRM 51-40-05-0G AND DWG 146A7500; SRM 53-00-53-2R-5 STEP 4. I. AMM 51-21-41-370-802;[06] CORRECTION TO STEP 5; MATERIAL USED IS BAC1496-377#7075T62;[07] VERIFIED CORRECTIVE ACTION #4-6; OK TO PRIME;[08] APPLIED PRIMER TO ACB FLOOR TO SIDEWALL SUPPORT PER SRM 53-00-53-2R-5 STEP 4. J.;[09] OK TO INSTALL REPAIR PARTS.;[10] VERIFIED CORRECTIVE ACTION #9 OK TO INSTALL;[11] INSTALLED NEW ACB FLOOR TO SIDEWALL SUPPORT AT BS727E+10' - BS767; RBL21; WL156 AND SPLICE REPAIR AT BS727E+8' - BS727E+18' PER SRM 53-00-53-2R-5 AND DWG 146A7500;;[12] VERIFIED CORRECTIVE ACTION #11 AND MEASUREMENT FIELD;[13] VERIFIED CORRECTIVE ACTION #11 AND MEASUREMENT FIELD
AFT CARGO BAY LAV TANK BULKHEAD LOWER BRACKET IS BROKEN BS867 LBL10 WL166 / [01] REMOVED DAMAGED LAV TANK LOWER BRACKET; BS867 LBL10; WL 166; LOCATED AND DRILLED AND INSTALLED NEW BRACKET; IAW SRM 51-40-02-0G-0; 51-40-05-0G-0; DWG 149A8104; DWG; 149A8102. IPC 53-42-51-06.;[02] VERIFIED CORRECTIVE ACTION #1
AFT CARGO BAY SHIELD FWD OF THE CARGO DOOR HAS AREAS OF CORROSION 767 TO 787 RBL21 WL156 / [01] EVALUATED CORROSION ON SHIELD BS 767 TO 787 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED ACTION #1;[03] REMOVED ACB FWD SHIELD BS 767 TO BS 792; RBL 21; WL 156 PER SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW ACB FWD SHIELD BS 767 TO BS 792; RBL 21; WL 156 PER DWG 146A0081 AND SRM 51-40-05-0G-0;[05] VERIFIED CORRECTIVE ACTION #4;[06] OK TO INSTALL;[07] OK TO CLOSE GIVEN;[08] INSTALLED NEW ACB FWD SHIELD BS 767 TO BS 792; RBL 21; WL 156 PER DWG 146A0081 AND SRM 51-40-02-0G-0;[09] VERIFIED CORRECTIVE ACTION ITEM 8.;[10] VERIFIED MEASUREMENTS.<BR>VERIFIED FAULT COMPLETE.
FWD CARGO BAY AFT BULKHEAD LOWER SUPPORT HAS AREAS OF CORROSION BS500I LBL15 TO RBL15 WL156 / [01] EVALUATED CORROSION AT ALL LOCATIONS OF BULKHEAD SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 500I RBL 14 WL 156; FOUND 0.020 REMOVED FROM ORIG 0.071 IN NUMEROUS 1'X1' AREAS; FOUND TO BE OUT OF LIMITS PER SRM 53-30-08-1A-1 USING DIAL DEPTH GAUGE ATS 2678 DUE 04/2023;[02] VERIFIED ACTION #1;[03] REMOVED FCB AFT BULKHEAD LOWER SUPPORT BS500I; LBL15 TO RBL15; WL156 PER SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW FCB AFT BULKHEAD LOWER SUPPORT BS500I; LBL15 TO RBL15; WL156 PER DWG 143A7902 AND SRM 51-40-05-0G-0. OK TO INSTALL.;[05] VERIFIED ACTION #3-4; OK TO INSTALL GIVEN;[06] INSTALLED NEW FCB AFT BULKHEAD LOWER SUPPORT BS500I; LBL15 TO RBL15; WL156 PER DWG 143A7902 AND SRM 51-40-02-0G-0.;[07] VERIFIED CORRECTIVE ACTION #6 AND MEASUREMENT FIELD;[08] VERIFIED CORRECTIVE ACTION #6 AND MEASUREMENT FIELD
AFT CARGO BAY ATTACH ANGLE COMMON TO SHIELD HAS AREAS OF CORROSION BS767 TO 787 RBL21 WL156 / [01] EVALUATED CORROSION ON ATTACH ANGLE BS 767 TO 787 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED ACTION #1;[03] REMOVED ACB ATTACH ANGLE COMMON TO SHIELD BS 767 TO BS 787; RBL 21; WL 156 PER SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW ACB ATTACH ANGLE COMMON TO SHIELD BS 767 TO BS 787; RBL 21; WL 156 PER DWG 146A8123 AND SRM 51-40-05-0G-0.;[05] VERIFIED CORRECTIVE ACTION #4;[06] OK TO INSTALL NEW ANGLE;[07] OK TO INSTALL GIVEN;[08] INSTALLED NEW ACB ATTACH ANGLE COMMON TO SHIELD BS 767 TO BS 787; RBL 21; WL 156 PER DWG 146A8123 AND SRM 51-40-02-0G-0.;[09] VERIFIED CORRECTIVE ACTION 8;[10] VERIFIED JOB COMPLETE AND MEASUREMENT TABLE
R/H BS663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED RBL 8 WL 167.68 / [01] VALIDATED APPLICABILITY OF SRM 57-10-10-2R-5;[[08] RECEIVED REPAIR PARTS FOR RH BS663 VAPOR BARRIER UPPER ATTACH ANGLE. RECEIVED SPLICE ANGLE RO#877067-SWA AND REPLACEMENT ANGLE RO#87066-SWA.;[09] CORRECTION: REPLACEMENT ANGLE RO#877066-SWA.;[10] VERIFIED ACTION #8-9;[11] LOCATED; DRILLED; TRIMMED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING AND PRIMERED REPAIR PARTS @ RH BS663 VAPOR BARRIER UPPER ATTACH ANGLE RBL8-RBL20 WL167.68 IAW SRM 57-10-10-2R-5. OK TO INSTALL.;[12] VERIFIED CORRECTIVE ACTION STEP 11. VERIFIED OK TO INSTALL.;[13] INSTALLED RH BS663 VAPOR BARRIER UPPER ATTACH ANGLE REPAIR PARTS RBL8-RBL20 WL167.68 IAW SRM 57-10-10-2R-5. BOND CHECK GOOD. BONDING METER ID:ATS758 S/N:1971 DUE:08/2022.;
L/H BS663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED RBL 8 WL 167.68 / [01] VALIDATED APPLICABILITY OF SRM 57-10-10-2R-5;[11] LOCATED; DRILLED; TRIMMED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING AND PRIMERED REPAIR PARTS @ LH BS663 VAPOR BARRIER UPPER ATTACH ANGLE LBL8-LBL20 WL167.68 IAW SRM 57-10-10-2R-5. OK TO INSTALL.;[12] VERIFIED CORRECTIVE ACTION STEP 11. VERIFIED OK TO INSTALL.;[13] INSTALLED LH BS663 VAPOR BARRIER UPPER ATTACH ANGLE REPAIR PARTS LBL8-LBL20 WL167.68 IAW SRM 57-10-10-2R-5. BOND CHECK GOOD. BONDING METER ID:ATS758 S/N:1971 DUE:08/2022.;
CEILING EXIT SALIDA SIGN OVER CENTER AISLE LENS DETACHED / [01] SECURED CENTER AISLE EXIT SIGN LENS PER SIP
OVERWING CEILING EXIT SIGNS CAME OFF / [01] SECURED LENS PER SIP
SMELL/FUMES IN CABIN ON CLIMB OUT. AFTER APPROX. 10 MIN; THE SMELL DISSIPATED / [01] FOUND RIGHT RECIRC FAN C/B POPPED REPLACED RIGHT RECIRC FAN PER AMM 21-25-02 OPS CHECKS OK<BR>REPLACED RIGHT CABIN RECIRCULATION FILTER PER MM 21-25-01
OVERWING CEILING EMERGENCY LENS M.I.A. ; / [01] FOUND LEN?S RESECURRED PER S.I.P.
EMERGENCY EXIT CEILING SIGN DAMAGED. / [01] RESECURED LIGHT COVER PANEL PER SIP;NO DAMAGE NOTICE
AFT GALLEY FLIGHT ATTENDANT EMERGENCY FLASHLIGHT LOCATED INBOARD. CAPTAIN'S SIDE WILL NOT TEST PROPERLY. OK TO CONTINUE, PER MEL 25-12-01; SP-1B; TRACKING NUMBER 99807. R & R BATTERY AND FLASHLIGHT ASSEMBLY, PER AMM 25-64-00 CL NR 80816.
AFT GALLEY FLIGHT ATTENDANT EMERGENCY FLASHLIGHT LOCATED INBOARD. CAPTAIN'S SIDE WILL NOT TEST PROPERLY. OK TO CONTINUE, PER MEL 25-12-01; SP-1B; TRACKING NUMBER 99807. R & R BATTERY AND FLASHLIGHT ASSEMBLY, PER AMM 25-64-00 CL NR 80816.
REMOVED WTB FAIRING 192BL DUE TO DELAMINATION ON LE OF PNL / ACCOMPLISHED PERMANENT REPAIR IAW SRM 51-70-05 INSTALLED FAIRING 192BL IAW AMM 47-31-02. (SEE SA-M 326 ATTACHED: A755268)
"1" AFT GALLEY EMERGENCY FLASHLIGHT WOULD NOT TEST. / R&R BATTERY IAW AMM.
LT REAR EMERGENCY EXIT SIGN LENS FELL OFF AT ROW 16. REINSTALLED LENS PER MM.
RT AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPOSITIONED FLASHLIGHT AT MOUNT BASE IAW MM.