N500WR
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 | 2017-09-25 – 2017-09-25 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2017-09-25 – 2017-09-25 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-06, OPS CHECKED OK. R & R BATTERY PACK IAW AMM 33-51-06. OPS CHECKED OK.
CREW REPORTS EMERGENCY EXIT LIGHTS ABOVE FWD GALLEY ON INTERMITTENT. PERFORMED OPS CHK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHKD GOOD.
EMERGENCY EXIT LIGHT ABOVE FWD GALLEY DOOR ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED FWD ENTRY EMERGENCY LIGHT CHARGER.
AFT GALLEY RIGHT HAND INBD FLASHLIGHT INOPERATIVE. FOUND BATTERY DISCONNECTED; RECONNECTED EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.
CRACKED SUPPORT BRACKET, BS 867, STR 2R - STR 3R IN THE PAX CABIN. FAULT RESOLVED ON OTHER FAULT SEE TTG8Q01C79F8.
CRACKED FRAME, BS 312 BTW STR 5L - STR 6L IN THE FWD GALLEY AREA. FAULT RESOLVED ON OTHER FAULT IAW SWA MPM 52.2.5 SEE TTG8Q01C77VD.
DELAMINATED FLOOR PANEL 241ABF AT AFT GALLEY AREA. REPAIRED FLOOR PANEL 241ABF AT AFT GALLEY AREA IAW SRM 53-00-50-2R-7 REPAIR 7 AND B737-800 SRM 53-00-50-2R-0 REPAIR GENERAL.
CRACKED ANGLE FLOOR STRUCTURE, BS 380 TO 400, LBL 50 IN PASSENGER CABIN. REPLACED ANGLE FLOOR STRUCTURE IAW DWG 143A5400, SHEET 140, REV- AND SRM 51-40-02-0G-0.
CRACKED FLOOR SUPPORT LOCATED BETWEEN BS 380 - 400, LBL 13. REPLACED FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 184, REV -.
DELAMINATED FLOOR PANEL 231KF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 231KF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.
CRACKED SUPPORT ANGLE, BS 867, S26L IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE LOCATED BS 867 AND S-26L AFT CARGO COMPARTMENT IAW SRM 51-10-02; SRM 51-40-02 AND DWG 149A8102 SHEET 19 REV A.
DELAMINATED ACCESS PANEL 232 RF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 232RF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.
CRACKED LEADING EDGE RIB ACCESS PANEL 331B LE STA 105.26 AT LT HORIZONTAL STABILIZER. REPLACED RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 186A1001 SHEET 19 REV -.
CRACKED LEADING EDGE RIB ACCESS PANEL 331B LE STA 114.55 AT LT HORIZONTAL STABILIZER. REPLACED RIB LOCATED LE STA 114.55 AT LT HORIZONTAL STABILIZER IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 186A1001 SHEET 19 REV-.
CRACKED SUPPORT BRACKET ON ACCESS PANEL 834DZ ON THE AFT ENTRY DOOR. REPLACED SUPPORT BRACKET LOCATED ON ACCESS PANEL 834DZ AT AFT ENTRY DOOR IAW SRM 51-10-02-0G ITEM 9, SRM 51-40-02-0G, AND DWG 411A2119, SHEET 72, REV -. EVALUATED CRACK ON SUPPORT BRACKET AND NOT FOUND ALLOWABLE DAMAGE IN B737-800 SRM.<BR>MEASURE OF CRACK: 0.287? INCH.
DELAMINATED FLOOR PANEL 241EF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 241EF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.
DELAMINATED FLOOR PANEL 241KF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 241KF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.
DELAMINATED FLOOR PANEL 242HF AT PASSENGER CABIN. REPAIRED FLOOR PANEL 242HF AT PASSENGER CABIN IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.
CRACK WEB - INTERCOSTAL LOCATED BS 927 TO BS 947 AND S-25R AFT CARGO BAY. REPLACED WEB - INTERCOSTAL LOCATED BS 927 TO BS 947 AND S-25R AFT CARGO BAY IAW SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG: 147A7500 SHEET 36 AND SHEET 37 REV-.
CORRODED WEB - INTERCOSTAL LOCATED BS 767 TO BS 794 S-25R WL 156 AFT CARGO COMPARTMENT. REPLACED SHIELD PLATE LOCATED BS 767 TO BS 794 S-25R WL 156 AFT CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 146A0081 SHEET 49 REV A.
CORRODED SUPPORT ANGLE, BS 767 TO BS 787 S-25R WL 156 AFT CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED BS 767 TO BS 787 S-25R WL 156 AFT CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG: 146A8123 SHEET: 16 REV: - AND DWG: 146A0081 SHEET: 49 REV: A.
CORROSION FRAME LOCATED BS 303.9, WL 203, AND LBL 56 AT PASSENGER CABIN. PERFORMED REPAIR CATEGORY B ON FRAME LOCATED BS 303.9, WL 203, AND LBL 56 IN THE PASSENGER CABIN IAW E/A 26-153-01439.
CRACKED LEADING EDGE RIB LOC LE STA 105.26 AT RT HORIZONTAL STAB. REPLACED RIB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 186A1001, SHEET 19, REV -.
CORROSION SUPPORT ZEE BTW BS 500C - 500I, LBL 25, WL 156, IN THE FWD CARGO BAY. THE DAMAGE WAS REPAIRED IAW SRM 53-00-53-2R-5, REPAIR 5, AND EA M-22-153-01550.
CORROSION SHIELD WEB LOCATED BTW BS492.4 TO BS500A RBL25 AND WL156 AT FWD CARGO BAY. REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS 492.4 TO BS 500A RBL25 AND WL156 AT FWD CARGO BAY IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A0080 SHEET: 39 REV -.
CRACK ON SUPPORT ANGLE, FWD FACE BS 695, BL 0, WL 208.1 RT SIDE OF PAX CABIN. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 273A9110, SHEET 6, REV A.
CORROSION SUPPORT ZEE LOCATED BTW BS500A TO BS500I RBL25 AND WL156 AT FWD CARGO COMPARTMENT. THE DAMAGE WAS REPAIRED IAW SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550. S
CRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. REPLACED SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A8310; SHEET 33; REV-.
CRACKED ANGLE TRAILING EDGE LOCATED ORSS 280 RT WING. REPLACED ANGLE TRAILING EDGE LOCATED ORSS 280 RT WING IAW ALLOWABLE DAMAGE 57-51-02-1A-1 ALLOWABLE DAMAGE 1, NOT FOUND ALLOWABLE DAMAGE, SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 115A6200, SHEET 17, REV A.
CRACKED ANGLE AT BS 663.75 RBL34 UPPER POSITION. REPLACED ANGLE BS 663.75 BTW RBL 5 TO RBL 65 UPPER POSITION IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 111A1000, SHEET 349, REV-.
CRACKED SUPPORT BRACKET, BS 867 BTW STR 2R - 3R IN THE PAX CABIN. REPLACED SUPPORT BRACKET IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 146A7901, SHEET 66, REV A.
CRACKED FRAME, BS 312 BTW STR 5L - 6L. PERFORMED PERMANENT REPAIR ON FRAME IAW EA M-22-153-01244.
DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR LT FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1 E/A) ON BAY 2; P/N: 183A0210-14 (1 E/A) AND P/N: 69-53211-2 (2 E/A) ON BAY 3;P/N: 183A0210-15 ON BAY 4 . TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-03766 SEE TASK TTG8Q01CASHB, TASK CARD ACCOMPLISHED ON MULTI EA M-22-155-03766 TASK TTG8Q01CASHB
DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR RT FOUND BALANCE WEIGHTS P/N: 183A0210-14 (1 E/A) ON BAY 2; P/N: 183A0210-14 (1 E/A) AND P/N: 69-53211-2 (2 E/A) ON BAY 3;P/N: 183A0210-15 ON BAY 4 FAULT RESOLVED ON OTHER FAULT TTG8Q01CCTK7.
CRACKED ANGLE LOCATED FWD FACE BS 500E AT LEVEL STR 26R AT FWD CARGO BAY. REPLACED ANGLE LOCATED FWD FACE BS 500E AT LEVEL STR 26R AT FWD CARGO BAY IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505, SHEET 137, REV-.
CRACKED ANGLE FWD FACE BS 500G, STR 26L AT FWD CARGO BAY. REPLACED ANGLE IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 137 REV-.
CRACK ON CARGO LINER SUPPORT LOCATED BS727F AT LEVEL STR18L AT AFT CARGO BAY. REPAIRED CARGO LINER SUPPORT LOCATED BS 727F STR 18L AT AFT CARGO BAY IAW SRM 51-70-11-2R-0 REPAIR GENERAL.
DELAMINATED FLOOR PANEL 221BF AT FWD GALLEY AREA. REPLACED FLOOR PANEL 221BF AT FWD GALLEY AREA IAW DWG-142A5810-729 REV. A. INSTALLATION WILL BE ACCOMPLISHED ON TASK TTG8Q01BUVFQ
CRACKED ANGLE LOCATED FWD FACE BS 500F AT LEVEL STR 26R AT FWD CARGO BAY. REPLACED ANGLE LOCATED FWD FACE BS 500F AT LEVEL STR 26R AT FWD CARGO BAY IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 137 REV-.
CRACKED ANGLE, LOCATED FWD FACE BS 500H AT LEVEL STR 26L AT FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 143A7505 SHEET 137 REV-.
CRACKED INTERCOSTAL LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 AT FWD GALLEY AREA. INSTALLED A NEW INTERCOSTAL LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 AT FWD GALLEY AREA AND FASTENER IAW SRM 51-10-02-0G-0 SRM 51-40-02-0G AND DWG 141A5400 SHEET 46 REV A.
CRACKED ANGLE FWD FACE BS 500H AT LEVEL STR 26R AT FWD CARGO BAY. REPLACED ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 137, REV-.
CRACK ANGLE - CLIP LOCATED AFT FACE BS 500H AT LEVEL STR 26L AT FWD CARGO BAY. REPLACED CLIP LOCATED AFT FACE BS 500H AT LEVEL STR 26L AT FWD CARGO BAY IAW SRM 51-10-02, ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 137 REV-.
CRACK CARGO LINER SUPPORT ANGLE LOCATED STA 727B AT LEVEL STR 18L AT AFT CARGO BAY. REPAIRED CARGO LINER SUPPORT ANGLE LOCATED BS 727B, STR 18L AT AFT CARGO BAY IAW SRM 51-70-11-2R-0 REPAIR GENERAL.
CRACKED OTBD FIXED LEADING EDGE RAIL NUTPLATE RETAINER LOCATED BETWEEN OSS 90.49 AND OSS 109.69 AT LT WING. REPLACED RAIL NUTPLATE RETAINER AND FASTENERS LOCATED BETWEEN OSS 90.49 AND OSS 109.69 AT LT WING IAW SRM 51-40-02.
CRACKED GUSSET ANGLE, BS 500I, STR 19R IN THE FWD CARGO BAY. REPLACED GUSSET ANGLE AND FASTENERS IAW SRM 51-40-02 AND DWG 143A7902 SHEET 256 REV B.
CRACKED GUSSET ANGLE. BS 500I, STR 21L, IN THE FWD CARGO BAY. REPLACED THE GUSSET ANGLE AND FASTENERS IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET: 256 REV: B.
CRACKED FLOOR PANEL 222DF. REPAIRED THE FLOOR PANEL 222DF IAW SRM 53-00-50-2R-7, REPAIR 7.
CRACKED ANGLE, FWD FACE BS 500D, STR 26R IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 137, REV-.
CRACKED WEB BTW BS 277 TO 294.5, RBL 1, WL 208.1 IN THE FWD GALLEY AREA. REPLACED WEB LOCATED BTW BS 277 TO BS 294.5 RBL 1 WL 208.1 IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A5400, SHEET 20, REV -.
CRACKED WEB BTW BS 344 - 360, RBL 51, WL 208.1 IN THE FWD GALLEY AREA. INTERCOSTAL REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS FOR CRACKED ON FASTENER HOLE IN SRM 53-10-51-1A-1, ALLOWABLE DAMAGE 1, SECTION 41 FLOOR STRUCTURE.
CRACK INNER CHORD LOCATED BS 303.9, STR 17L IN FWD GALLEY AND LAV. REPLACED INNER CHORD AND FASTENERS LOCATED FROM BS 270 - 360, STR 17L FWD GALLEY AND LAV IAW SRM 51-40-02, AND DWG 141A8110, SHEET 9, REV A, & DWG 141A8110, SHEET 11 REV-.
DELAMINATED FLOOR PANEL 222BF. REPAIRED FLOOR PANEL 222BF AT FWD GALLEY AREA IAW SRM 53-00-50-2R-7, REPAIR 7.
CRACKED WEB BTW BS 344 - 360, BL 0, WL 208.1. REPLACED WEB IAW SRM 51-10-02, ITEM 9, AND DWG 141A5400, SHEET 13, REV- DUE TO NOT FOUND ALLOWABLE DAMAGE FOR CRACK IAW SRM 53-10-51-1A-1.
CORRODED WEB, BS 986.5 + 4.5 INCHES, LBL 34, WL 208.1. REPLACED THE WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 147A5700, SHEET 121, REV A.
CORROSION ON FLOORBEAM BS 344, RBL 7, WL 208.1 IN THE FWD GALLEY AREA. PERFORMED REPAIR CATEGORY A LOCATED ON FLOORBEAM BS 344 AND BTW LBL10 TO RBL 20 IAW SRM 53-10-51-2R-10, REPAIR 10, AND EA 26-153-01400.
CRACKED ANGLE AFT FACE BS 500G, STR 26L AT FWD CARGO BAY. REPLACED ANGLE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 137, REV-.
CRACKED WEB, BTW BS 312 - 328, RBL 31, WL 208.1 IN THE FWD GALLEY AREA. REPLACED WEB AND FASTENERS LOCATED BTW BS 312 - 328, RBL 31, WL 208.1 IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A5400, SHEET 39, REV -.
CRACKED WEB, BTW BS 312 - 328, LBL 47, WL 208.1. REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS 312 TO BS 328 LBL 47 WL 208.1 AT FWD GALLEY AREA IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 141A5400, SHEET 26, REV -.
CRACKED ANGLE, AFT FACE BS 500G, STR 26R IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 137, REV-.
CRACKED ANGLE, FWD FACE BS 500G, STR 26R IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A7505, SHEET 137, REV-.
CRACKED ANGLE LOCATED AFT FACE BS 500H AT LEVEL STR 26R AT FWD CARGO COMPARTMENT. REPLACED ANGLE - CLIP LOCATED AFT FACE BS 500H AT LEVEL STR 26R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 137 REV-.
DELAMINATED WING TO BODY FAIRING ACCESS PANEL 191CR INTERNAL AREA AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 191CR INTERNAL AREA AT LOWER FUSELAGE IAW SRM 51-70-04-2R-6, REPAIR 6.
CORROSION INTERCOSTAL BTW BS 947.5 - BS 967, RBL 52, WL 208.1 IN THE AFT GALLEY AREA. REPLACED INTERCOSTAL IAW SRM 51-10-02 ITEM 9 AND DWG 147A5650 SHEET 71 REV A:
CORRODED WEB, BS 986.5 + 4 INCHES, LBL 43, WL 208.1 IN THE AFT GALLEY AREA. FAULT RESOLVED ON OTHER FAULT TTG8Q01C650B.
CORRODED FLOORBEAM, BS 947.5, LBL 53, WL 208.1 IN THE AFT GALLEY AREA. REPAIRED THE UPPER TEE FLOORBEAM WILL BE INSTALLED ON FAULT TTG8Q01C5CAC IAW SRM 53-70-51-2R-5, REPAIR 5.
CORRODED FLOORBEAM, BS 986.5, LBL 43, WL 208.1 IN THE AFT GALLEY AREA. PERFORMED REPAIR ON FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.
CORROSION FLOORBEAM, BS 986.5, RBL43, WL 208.1 IN THE AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.
CORRODED FLOORBEAM BS 947.5, LBL 25, WL 208.1 AT AFT GALLEY AREA. THIS REPAIR HAS BEEN ACCOMPLISHED IAW SRM 53-70-51-2R-5 ALTERNATIVE 2 WITH A MINOR DEVIATION CONSIDERED ACCEPTABLE AS PER EA 26-153-01390.
CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW SRM 53-30-15-2R-1, REPAIR 1, AND BAC 5975.
CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED FWD CORNER SCUFF PLATE OF FWD CARGO COMPARTMENT I.A.W. B737-800 S.R.M 53-30-15-2R-1 REPAIR 1 AND BAC 5975 SEE INDIVIDUAL SIGN OFF BELOW. RII COMPLETED.
CORROSION INTERCOSTAL LOCATED BTW BS947.5 TO BS967 LBL53 AND WL208.1 AT AFT GALLEY AREA. REPLACED INTERCOSTAL LOCATED BTW BS947.5 TO BS967 LBL53 AND WL 208.1 AT AFT GALLEY IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02. AND DWG 147A5650 SHEET 54 REV A.
CRACKED AFT SERVICE SCUFF PLATE (POSITION CENTER)AT AFT GALLEY AREA. REPAIRED AFT SERVICE, CENTER SCUFF PLATE AT AFT GALLEY AREA IAW SRM 53-70-15-2R-1; REPAIR 1; PARAGRAPH 4. B; FIGURE 203. REFER TO BAC 5975.
BROKEN EMERGENCY VALANCE LENS BIN POSITION 3 LT AND 5 LT SIDE AT PASSENGER CABIN. REPLACED EMERGENCY VALANCE LENS BIN POSITION 3 LT AND 5 LT SIDE AT PASSENGER CABIN IAW AMM 33-51-03-960-803. REPLACED EMERGENCY VALANCE LENS BIN POSITION 3 LT AND 5 LT SIDE AT PASSENGER CABIN IAW AMM 33-51-03-960-803.
DETERIORATED HARDWARE ENTRY AND SERVICE GIRT BAR FITTING AT AFT GALLEY AREA. REPLACED HARDWARE ENTRY AND SERVICE GIRT BAR FITTING AT AFT GALLEY AREA IAW AMM 25-66-02-400-801 THE INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8R007DGB8 STEP 13.
RIGHT AFT ATTENDANT SEAT ACCESS DOOR FOR EMERGENCY FLASHLIGHT WILL NOT OPEN. REPLACED ACCESS DOOR LATCH IAW CMM 25-25-12. OPS OK.
FOUND THE NR 3 LEFT FWD AISLE EMERGENCY LIGHTS AND LT FWD OVERWING ESCAPE LIGHT INOPERATIVE. R & R. BATTERY PACK IAW AMM 33-51-06. CHKD GOOD.
TRAILING EDGE FLAPS DISAGREE; INDICATOR SHOWED FLAPS 25 WITH FLAP HANDLE SELECTED AT FLAPS 30 <[01]. PERFORMED TRAILING EDGE FLAP SYSTEM OPS CK PER AMM 27-51-00. FLAPS OPERATE NORMALLY. PERFORMED FLAP OVERSPEED PHASE 1 CONDITIONAL INSPECTION AS A PRECAUTION IAW AMM 05-51-08. AHM DATA INDICATED NO FLAP DISAGREE ANOMALIES FOR THIS FLIGHT. NO 30 DAY HISTORY.
EMERGENCY LIGHTS INOP AT LH OVERWING EXITS. REMOVED, REPLACED AND OPS CHECKED BATTERY PACK IAW AMM 33-51-06
LH AFT CABIN BULLNOSE EMERGENCY LIGHTS INOP. REMOVED REPLACED AND OPS CHECKED BATTERY PER AMM 33-51-06.
CABIN FLOOR PANEL 231KF HAS DELAMINATION.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)];[02] INSPECTION C/W FOR CORRECTIVE ACTION #1 PER AMM 53-21-00.
RH AFT CABIN BULLNOSE EMERGENCY LIGHTS INOP. REMOVED REPLACED AND OPS CHECKED BATTERY ACK PER AMM 33-51-06.
PANEL 242HF IS DELAMINATED. PANEL 242FH IS DELAMINATED.<[01] INSTALLED FLOOR PANEL IAW AMM 53-21-00.
PANEL 242GF IS DELAMINATED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)];[02] INSPECTION C/W FOR 1. DOUGLAS GILLASPY (TECHNICIAN); 05-JUN-2024 09:00 UTC<BR>01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)
PANEL 242FF IS DELAMINATED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)];[02] INSPECTION C/W.
PANEL 242EF IS DELAMINATED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)];[02] INSPECTION C/W.
PANEL 242JF IS DELAMINATED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)];[02] INSPECTION C/W FOR 1. DOUGLAS GILLASPY (TECHNICIAN); 05-JUN-2024 09:01 UTC<BR>01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)].
PANEL 242LF IS DELAMINATED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)];[02] INSPECTION C/W FOR 1. DOUGLAS GILLASPY (TECHNICIAN); 05-JUN-2024 09:04 UTC<BR>01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT
PANEL 242KF IS DELAMINATED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)];[02] INSPECTION C/W FOR 1. DOUGLAS GILLASPY (TECHNICIAN); 05-JUN-2024 09:06 UTC<BR>01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)]
PANEL 242MF IS DELAMINATED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)];[02] INSPECTION C/W FOR 1. DOUGLAS GILLASPY (TECHNICIAN); 05-JUN-2024 09:07 UTC<BR>01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)]
PANEL 242NF IS DELAMINATED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)];[02] INSPECTION C/W FOR 1. DOUGLAS GILLASPY (TECHNICIAN); 05-JUN-2024 09:09 UTC<BR>01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT.
PANEL 242PF IS DELAMINATED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)];[02] INSPECTION C/W FOR C/A 1. DOUGLAS GILLASPY (TECHNICIAN); 05-JUN-2024 09:10 UTC<BR>01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)]
PANEL 242QF IS DELAMINATED.<[01] INSTALLED FLOOR PANEL IAW AMM 53-21-00.;[02] INSTALLED FLOOR PANEL IAW AMM 53-21-00.
THE #4 SEAT TRACK LOWER SURFACE HAS AREA OF CORROSION FROM STATION 727F TO 867.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO OUT OF LIMITS PER SRM 53-00-52-1A-1. REMOVED 0.060 MATERIAL AT STA 847 RBL 45.5;[02] VERIFIED OUT OF LIMITS;[03] REMOVED # 4 SEAT TRACK FOR STA 727B TO 887 PER SRM 51-40-02.;[04] FINISHED DRILLING UP NEW SEAT TRACK IAW. SRM. 51-40-02.;[05] VERIFIED WORK ACCOMPLISHED IN C/A #4. OK TO INSTALL.;[06] REMOVED AND REPLACED PER SRM 51-40-02.;[07] C/W INSPECTION.
FWD CARGO FWD BULKHEAD PANEL 121LW HAS FOAM DETERIORATION ON BACKSIDE OF PANEL.. REMOVED AND REPLACED FWD CARGO FWD BULKHEAD PANEL 121LW FOAM ON BACKSIDE OF PANEL PER AMM 25-52-16. INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR FOAM REPLACEMENT.
CABIN FLOOR STRUCTURE INTERCOSTAL IS CRACKED AT FASTENER AT STA 540 LBL 1.<[01] REPLACED INTERCOSTAL PER SRM 51-40-02.
CABIN FLOOR STRUCTURE INTERCOSTAL IS CRACKED AT FASTENER AT STA 540 RBL 1.<[01] REPLACED INTERCOSTAL PER SRM 51-40-02.
231YF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] REMOVED AND REPLACED FLOORBOARD IAW AMM 53-21-00.
231ZF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] REMOVED AND REPLACED FLOORBOARD IAW AMM 53-21-00.
232RF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]
232SF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]
241AF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)];[02] TOOL INPUT;[03] C/W INSPECTION OF C/A 1 AND 2.
241BF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] REMOVED AND REPLACED FLOORBOARD IAW AMM 53-21-00.
241FF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] REMOVED AND REPLACED FLOORBOARD IAW AMM 53-21-00.
241EF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] REMOVED AND REPLACED FLOORBOARD IAW AMM 53-21-00.
242EF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] CARD GENERATED IN ERROR DUE TO INCORRECT PANEL IDENTIFIER
242FF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] FAULT RAISED IN ERROR DUE TO INCORRECT PANEL IDENTIFIER
242BF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]
242CF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]
242DF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]
241CF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] REMOVED AND REPLACED FLOORBOARD IAW AMM 53-21-00.
241DF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)];[02] TOOL INPUT;[03] C/W INSPECTION OF C/A 1 AND 2.
242AF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)];[02] 02 - INSPECTED PER [AMM 53-21-00-400-801-NG (PASSENGER CABIN FLOOR PANEL INSTALLATION - PERMANENT)]
231XF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] 01 - REMOVED AND REPLACED PER [AMM 53-21-00-401-NG (PASSENGER CABIN FLOORS - REMOVAL/INSTALLATION - PERMANENT)];[02] TOOL INPUT;[03] C/W INSPECTION OF C/A 1 AND 2.
RH AFT EMERG LIGHTS INOP<[01] REPLACED RH AFT EMERG LIGHT POWER SUPPLY BATTERY REF AMM 33-51-06. OPS CHECK GOOD.
ENGINE FAILURE AT FL190; COMPRESSOR STALL SUSPECTED. NR 2 ENG REPLACED.
GIRT DRAGS THE FLOOR WHEN OPENING AFT ENTRY DOOR.<[01] RE-SECURED GIRT AFT ENTRY DOOR REF AMM 25-66-01.
AFT RIGHT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED AFT RIGHT SERVICE DOOR EXTERIOR EMERGENCY LIGHT PER AMM 33-51-04. CHECK GOOD.
FWD ENTRY DOOR SLIDE FELL OUT OF COMPARTMENT; SLIDE DID NOT DEPLOY.<[01] REINSTALLED FWD ENTRY DOOR SLIDE IAW MT 725-61-06. A/C OK FOR SERVICE.
FOUND FWD ENTRY AREA EMERGENCY LIGHTS INOP<[01] REPLACED BATTERY PACK AND CHARGER ASSY PER AMM 33-51-06. OPS CHK GOOD AT THIS TIME.
FWD CABIN MEGAPHONE BROKEN<[01] R/R FWD CABIN MEGAPHONE IAW AMM 25-64-00.
LEFT WING FIXED TRAILING EDGE PANEL; IN BETWEEN SPOILERS 5 AND 6; OUTBOARD RIB ASSEMBLY CRACKED AT SERRATED PLATE BRACKET.<[01] COMPLIED WITH REPAIR IAW SRM 57-51-02-2R-3 REPAIR #3
#1 ENGINE I/B FAN COWL ; AFT UPPER CORNER HAS A CRACK 2.7 IN. LENGTH.<[01] PERFORMED HFEC INSPECTION OF THE REPAIR AREA PER NDT MANUAL PART 6; 51-00-00 PROCEDURE 23. NO DEFECTS NOTED. COMPLIED WITH SRM 54-20-01-2R-13 STEP 4E.;[02] PERFORMED HFEC (ROTARY SCANNER) INSPECTION OF THE REMOVED FASTENER HOLES PER NDT MANUAL PART 6; 51-00-00 PROCEDURE 16. NO DEFECTS NOTED. COMPLIED WITH SRM 54-20-01-2R-13 STEP 4F.;[03] REPAIRED PER EA 23-171-03496
AFT ENTRY DOOR SLIDE HANGING<[01] INSPECTED AND ADJUSTED AFT LH SLIDE FLAP IRW AMM 25-66-01 OPS TEST GOOD
FWD. SERVICE DOOR SLIDE DRAGS THE FLOOR WHERE IT ATTACHES TO GURT BAR.<[01] REPOSITIONED SLIDE REF MT 725-61-06.
ON APPROACH INTO SAN EXPERIENCED FLAP ASYMMETRY WHILE CONFIGURING FOR APPROACH. THE RIGHT FLAP INDICATION DID NOT MOVE AND LEFT INDICATION SPLIT. WE PERFORMED A TRAILING EDGE FLAPS UP LANDING IN LAX.<[01] ON FSCU BITE FOUND FLAP 5 SCEW FAULTED. R&R NO.5 INBOARD FLAP INBOARD SKEW SENSOR PER AMM 27-59-01. OPS OK AT THIS TIME. PERF FSCU BITE PER FIM 27-51 TASK 801. NO FAULTS AT THIS TIME.
L2 EXTERNAL EMERGENCY EXIT LIGHT INOP<[01] RELAMPED L2 SLIDE LIGHT IAW MM 33-51-04. NO HELP. R/R?D BATTERY PACK M1673 IAW MM 33-51-06. OPS CHECK NORMAL.
R2 EMERGENCY EXIT LIGHT INOP<[01] ENTERED IN ERROR
STRINGER S-18L SEVERED AT BS460 - SPLICE REPAIR PER SRM 53-00-03 REPAIR 1 REQUIRED AT BS 487.<[01] 'PERFORMED A SPLICE REPAIR PER SRM 53-00-03 REPAIR 1 WITH HI-LOKS IN LIEU OF RIVETS AS ALLOWED IN EA 23-153-01112. REF FAULT TTG8Q00K8WAD;[02] REF ORIGINAL FAULT TTG8Q00K8WAD & TTGQ00K9WB7. CW RII INSP OF SPLICE REPAIR ON STRINGER 18L PER SRM 53-00-03 & EA 23-153-01112
STRINGER S-18L SEVERED AT BS460 - SPLICE REPAIR PER SRM 53-00-03 REPAIR 1 REQUIRED AT BS 447.5.<[01] 'PERFORMED A SPLICE REPAIR PER SRM 53-00-03 REPAIR 1 WITH HI-LOKS IN LIEU OF RIVETS AS ALLOWED IN EA 23-153-01112. REF FAULT TTG8Q00K8WAD.;[02] REF ORIGINAL FAULT TTG8Q00K8WAD & TTGQ00K9WB7. CW RII INSP OF SPLICE REPAIR ON STRINGER 18L PER SRM 53-00-03 & EA 23-153-01112
STRINGER S-19L SEVERED AT BS460 - SPLICE REPAIR PER SRM 53-00-03 REPAIR 1 REQUIRED AT BS 447.5.<[01] 'PERFORMED A SPLICE REPAIR PER SRM 53-00-03 REPAIR 1 WITH HI-LOKS IN LIEU OF RIVETS AS ALLOWED IN EA 23-153-01112. REF FAULT TTG8Q00K8WAD;[02] REF ORIGINAL FAULT TTG8Q00K8WAD & TTGQ00K9WBB. CW RII INSP OF SPLICE REPAIR ON STRINGER 18L PER SRM 53-00-03 & EA 23-153-01112
#1 ENGINE FAILURE IN FLIGHT #1 ENGINE FAILURE (CATASTROPHIC). SEE PICTURES ATTACHED<[01] REMOVED ENGINE IN MXI AND INSTALLED ENGINE SN963439;[02] C/W;[03] C/W;[04] PERFORMED OPS C.K FOR #1 ENG PER MT 771-00-01 OPS C.K GOOD
QC WALK- EMERGENCY LIGHT ON RIGHT AFT HATCH DOOR; WHEN YOU TURN ON THE WHITE BRIGHT LIGHT IT START TO FLASH. / [01] REMOVED AND REPLACED RH AFT OVER WING EMERGENCY LIGHT PER AMM 33-21-00-960-805; 25-21-20-000/400-801. TEST NORMAL PER AMM 33-21-00-960-805 AND 21-45-00-700-801.;[02] VERIFIED STEP 1
R/H EXTERIOR OVER-WING EMERGENCY LIGHT INOP. / [01] PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST AS PER B737 AMM 33-51-00-710-801. TEST OK;[02] VERIFIED STEP 1.
OVERHEAD BIN EMERGENCY LIGHTS AT ROWS 6R/H; 10R/H AND 13R/H INOP. / [01] PERFORMED TROUBLESHOOTING AS PER REFERENCE B737 WDM 33-51-12-13. FOUND POWER SUPPLY AND BATTERY PACK M1676 DEFECTIVE.;[02] REMOVED AND REPLACED POWER SUPPLY M1676 AS PER REFERENCE B737 AMM 33-51-06-960-806.;[03] VERIFIED STEP 1;2;[04] REMOVED AND REPLACED BATTERY PACK ON M1676 FOR OVERHEAD BIN EMERGENCY LIGHTS AT ROWS 6R/H; 10R/H AND 13R/H AS PER B737 AMM 33-51-06-960-805. TEST OK;[05] VERIFIED STEP 4.
R1 DOOR EMERGENCY EXIT SIGN AND EXTERIOR LIGHT INOP. / [01] PERFORMED T/S AS PER B737 WDM 33-51-11 AND WDM 33-51-12 AND FOUND CONNECTOR D14812 ON POWER SUPLLY M2816 NO PROPERLY SEATED; RECONNECTED CONNECTOR D14812 AND PERFORMED EMERGENCY LIGHT OPERATIONAL TEST AS PER B737 AMM 33-51-00-710-801. TEST OK.;[02] VERIFIED STEP 1
FWD CARGO COMPARTMENT DOOR CUTOUT LOWER SILL WEB PLATE SKIN CRACKED MKD DOTS / [01] RECEIVED NEW WEB PLATE ; WEB PLATE WILL BE INSTALLED ON WORK CARD TTG8R007DQTA;[02] VERIFIED STEP 1.
AFT CARGO LWR DOOR CUT-OUT;SHOWS AFT SCUFF PLATE CRACKED AT UPPER FWD EDGE.MKD. / [01] RECEIVED REPAIRED AFT CARGO LOWER DOOR CUTOUT AFT SCUFF PLATE PER REF SRM53-60-15-2R-1;AND INSTALLATION TO BE ACCOMPLISHED ON JOB CARD TTG8R007DQSB.;[02] VERIFIED STEP 1.
ROW 23 THRU 30 DEF SIDEWALL LIGHTS AND AFT GALLEY COVE LIGHTS ARE DELAYED WHEN T 03/28- OP'S CHECKED GOOD / [01] RELAMPED SIDEWALL LIGHT ASSY @ ROW 22DEF IAW AMM 33-22-00. OPS CHECK GOOD. MEL CLEARED.
LEFT WING TRAILING EDGE DEFLECTION RIB/PANEL SUPPORT WEB CRACKED AT OUTBOARD FASTENER. ; / [01] REMOVED AND REPLACED SUPPORT WEB REF SRM 51-40-02.
RH WING TRAILING EDGE DEFLECTION RIB/PANEL SUPPORT WEB CRACKED AT OUTBOARD FASTENER. ; / [01] REMOVED AND REPLACED SUPPORT WEB REF SRM 51-40-02.
EMERGENCY EXIT LIGHTS BY R1 DOOR INSIDE CABIN AND EXTERIOR ARE INOP / REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK FOR R1 DOOR PER AMM 33-51-06; OPS CHECK GOOD
AFT GALLEY SERVICE DOOR LOWER PAN ASSEMBLY CRACKED / REMOVED AND REPLACED AFT GALLEY SERVICE DOOR LOWER PAN ASSEMBLY PER AMM 52-41-31.INSPECTOR: E74102
ANTI SKID-INOP LIGHT ILLUMINATED, TROUBLESHOT REF. FIM 32-42-TASK 803. FAULT CODE: BOX 1-4. CASE DETERMINED TO BE AACU. REPLACED AACU, REF AMM 32-45-21. TAG NR 373175ONLY PN OFF/ON: 142-147 SN OFF/ON: 890/1638.
ON APPROACH INTO MDW THE FLAPS STOPPED AT 8 DEGREE WHEN SELECTED TO 15 ON THE LEVER. DIVERTED TO MKE AND FLAPS WORKED USING ALTERNATE FLAP SELECTOR TO 15 DEGREE. REMOVED AND REPLACED FLAP POSITION SENSOR, PER AMM 27-58-01. OPERATIONS CHECK GOOD ISSUE NR 3078754 POS/LT TAG/701440 P/N OFF/ON 18-1738-12 S/N OFF 5619 S/N ON 2235.
R/H WING TRAILING EDGE PANEL 651FB FWD BRACKET IS BROKEN / REMOVED AND REPLACED R/H WING TRAILING EDGE PANEL 651FB FWD BRACKET IAW SRM 51-40-02-0G-0 AND DWG 115A2710 REV- SHEET 9.
APU DOOR IS BENT IN FWD. L/H CORNER / REPAIRED APU ACCESS DOOR SKIN; FWD FRAME & L/H ZEE FRAME PER ATS ER 20-02730 REV IR AND SWA CARD NUMBER 20-152-00794 REV IR
L/H WING FWD FLAP TRACK FAIRING 544AB (#1) HAS DISBOND AREA BETWEEN FWD AND AFT MOUNT HOLES. / REMOVED AND REPLACED L/H WING FWD FLAP TRACK FAIRING 544AB (#1) IAW AMM 27-51-28-000-801 AND AMM 27-51-28-400-801. VERIFIED ADJUSTMENT IAW AMM 27-51-28-820-801. NO ADJUSTMENT IS REQUIRED. 59083U 6-14-20 (POS:#1; TAG NO:693480; P/N OFF:113A9110-1; S/N OFF:K4709; P/N ON:113A9110-1; S/N ON:K5911)
RH CABIN FLOOR PANEL 232QF HAS DAMAGE ON AFT EDGE. (MARKED) / REPAIRED DAMAGE ON AFT EDGE OF RH CABIN FLOOR PANEL 232QF IAW SRM 53-00-50-2R-1. DAMAGE WAS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.E.(2)(B) DAMAGE WAS WITHIN 3.0' FROM THE EDGE OF THE PANEL.
**CORROSION** AFT CARGO COMPARTMENT BAFFLE STA. 747-767; RBL30;WL165 HAS CORROSION / REMOVED AND REPLACED R/H BAFFLE FS 747-767 WL 165 DUE TO OUT OF LIMITS CORRISION IAW SRM 51-40-02-0G-0; SRM 53-00-04-1A-1 AND DWG 146A7505; DWG 146A7500
*** CORROSION *** AFT CARGO COMPARTMENT AFT SHIELD HAS CORROSION FROM STA 847+9 TO 847+12; RBL 21; WL 167. / DUE TO NO ALLOWABLE LIMITS IN THE SRM; REMOVED AND REPLACED AFT CARGO; AFT SHIELD P.O. 765476 IAW SRM 51-40-02-0G-0; BOEING DWG 146A0081 REV A
AFT CARGO COMPARTMENT AFT BULKHEAD TO FLOOR SUPPORT HAS AREA'S OF CORROSION AT STA 947.5; RBL 6-20; WL183. (MARKED) / AFT CARGO COMPARTMENT AFT BULKHEAD TO FLOOR SUPPORT STA 947.5 WL 183 FOUND TO BE OUT OF LIMITS DUE TO NO STATEMENT IN SRM; REMOVED DAMAGED BULKHEAD SUPPORT & INSTALLED NEW BULKHEAD TO FLOOR SUPPORT P/N 7530182 IAW SRM 51-40-02-0G-0; DWG 149A8117.
RIGHT HAND BS 663 LOWER VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT RBL8 / REPAIRED RIGHT HAND BS 663 LOWER VAPOR BARRIER UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5
AFT CARGO COMPARTMENT RH Z CHANNEL HAS AREA'S OF CORROSION FROM STA 727+13 TO 767; RBL 21; WL 157. (MARKED) / CORROSION ON AFT CARGO RH Z CHANNEL FOUND TO BE OUT OF LIMITS I.A.W. SRM 53-00-53-1A-2. REMOVED Z CHANNEL FROM STA 727 TO 767 IAW. SRM 51-40-02-0G-0. FABRICATED Z CHANNEL FROM BAC 1496-377 7075 T62 IAW SRM 53-00-53-2R-5; SPLICE LOCATED AT STA 727F+11.40'. INSTALLED Z CHANNEL IAW SRM 57-40-02-0G-0 AND BOEING DWG 146A7500 REV:-.
*** CORROSION *** AFT CARGO COMPARTMENT FWD SHIELD HAS CORROSION FROM STA 767-787; RBL 21; WL 159. / REMOVED AND REPLACED AFT CARGO COMPARTMENT FWD SHIELD WITH NEW SHIELD AT STA 767-787; RBL 21; WL 159 PO# 771818 IAW SRM 51-40-02 SRM 51-40-05 AND DWG 146A0081
AFT CARGO COMPARTMENT RT Z CHANNEL HAS AREA'S OF CORROSION AT BS 927+17, RBL 20, WL 182. FOUND TO BE OUT OF LIMITS DUE TO DAMAGE LOCATION TO FASTNER HOLE IAW SRM 53-00-53-1A-2 DETAIL D. REMOVED DAMAGED SECTION FROM 887-947.5 AND FABRICATED & INSTALLED NEW SECTION IAW SRM 53-60-53-0I-2 TABLE 2, SRM 51-40-02-0G-0, AND DWG 147A7500.
AFT CARGO COMPARTMENT LH Z CHANNEL HAS AREA'S OF CORROSION FROM STA 727F+13 TO 807+9; LBL 21; WL 157. (MARKED) / CORROSION ON AFT CARGO L/H Z CHANNEL FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES IAW SRM 53-00-53-1A-2 FIG 103 DETAIL 'D'. FABRICATED REPLACEMENT CHANNEL IAW SRM 53-00-53-2R-5. INSTALLED WITH SPLICES IAW SRM 51-40-02-0G-0, AND DWG 146A7502 REV-
LEFT HAND BS 663 LOWER VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT LBL8 / REPAIRED LEFT HAND BS 663 LOWER VAPOR BARRIER UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5
***CORROSION*** FWD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT HAS CORROSION AT STA 500I LBL 23 TO RBL 23 WL 157 / REMOVED DAMAGED FWD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT AT BS 500I LBL 23 TO RBL 23 WL 152. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 FIG 103 DETAIL D. INSTALLED REPLACEMET PART PO# 778494 FROM STA 500I LBL 23 TO RBL 23 WL 157 IAW SRM 51-40-02 AND BOEING DWG# 143A9481 + 143A7902. 57828U 6/5/2020
***CORROSION*** FWD CARGO BAY FWD SHIELD HAS CORROSION FROM STA 420 - 440 RBL 23 WL 157 / REMOVED FWD CARGO BAY FWD SHIELD FROM STA 420 - 440 RBL 23 WL 157 DUE TO CORROSION BEING OUT OF LIMITS IAW SRM 53-00-53 FIG 103; INSTALLED NEW SHIELD PO # 772092 FORM STA 420 - 440 RBL 23 WL 157 IAW SRM 51-40-02-0G-0 AND BOEING DWG # 143A0080. 57828U 6/4/2020
***CORROSION*** FWD CARGO BAY AFT SHIELD HAS CORROSION FROM STA 492 - 500A RBL 23 WL 157 / REMOVED AND REPLACED FWD CARGO BAY AFT SHIELD P.O.NO: 794584 FROM STA 492 TO STA 500A RBL 23 WL 157 I.A.W SRM 51-40-02-0G-0 AND DWG 143A0080; 59600U 04-JUN-20
FWD CARGO BAY R/H Z-CHANNEL HAS CORROSION FROM STA 500A - 500I RBL 23 WL 157 / REMOVED DAMAGED Z CHANNEL R/H STA 500A - 500I RBL 23 WL 157 IAW SRM 51-40-02-0G-0; FABRICATED & INSTALLED NEW Z CHANNEL AT STA 500A - 500I WITH SPLICE LOCATION AT 500E+10 IAW SRM 53-00-53-2R-5; SRM 51-40-02-0G-0; DWG 143A7501
FWD CARGO BAY L/H Z-CHANNEL HAS CORROSION FROM STA500B - 500I LBL 23 WL 157 FOUND CORROSION ON FWD CARGO BAY LH ZEE CHANNEL TO BE OUT OF LIMITS IAW SRM 53-00-53 FIG 103 - DETAIL D REMOVED DAMAGED PORTION OF ZEE CHANNEL PER SRM 51-40-02-0G-0 FABRICATED AND INSTALLED NEW ZEE CHANNEL AND REPAIR SPLICE FROM BAC1496-444 7075+6 LOT 5090717-1 IAW SRM 51-40-05-0G-0 SRM 53-00-53-2R-5 AND BOEING DWG 143A7500 REPAIR SPLICE LOCATED AT STA 500B+10' LBL 23 WL 157
DENT FOUND ON EXTERIOR FUSELAGE SKIN @STA. 927+5.8; 2.9' BELOW STR. 18L / ACCOMPLISHED SKIN REPAIR BS 927+5.8 2.9' BELOW STR 18L IAW ATS ER 20-02685 REV IR & SWA WORK INSTRUCTION NO. 20-153-00799 REV IR
DENT FOUND ON EXTERIOR AFT CARGO DOOR SKIN 19.5' AFT OF FWD. EDGE; 23.0' BELOW UPPER EDGE / REPAIRED AFT CARGO DOOR SKIN (P/N 146A6110-33 S/N PMC-00222 PER ATS ER 20-02692 REV IR AND SWA WORK CARD 20-152-00785 REV IR.
EXTERIOR FUSELAGE EMRGCY. LT. INOP.; AFT OF LEFT WING TRAILING EDGE / RELAMPED PER AMM 33-51-04 OPS-OK
FORWARD FLIGHT ATTENDANT FLASHLIGHT RED LIGHT DID NOT FLASH. / R&R FLASHLIGHT PER AMM.
PHOTOLUMINESCENT STRIP FIRST OFFICER FORWARD SIDE INOP. / R&R PHOTOLUMINESCENT STRIP IAW AMM.
L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED LIGHT PER AMM.
R1 DOOR EMERGENCY ESCAPE SLIDE INADVERTENTLY CAME OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. / R&R SLIDE PER MT.
MID CABIN CEILING EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM.
DIVERSION, B SYSTEM HYDRAULIC LOSS WITH LOW PRESSURE LIGHT ILLUMINATED. R&R NR 2 ENGINE DRIVEN PUMP PER MM.
A SYSTEM HYDRAULIC QUANTITY LOSS IN FLIGHT. R & R NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM.
PILOT REPORTED PRESSURIZATION SYSTEM REVERTED TO UNCOMMANDED EMERGENCY PRESSURIZATION MODE.