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. (SWAA) | Operator | on 2017-09-25 | Operator named in NTSB report |
Accident & incident history
Operated by Southwest Airlines (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
175 reports on file, 2011-11-09 – 2026-06-29.
Part: NUT — MISSING (ZONE 800) · airframe 39,724 hrs · 19,451 cycles
AFTER ENTRY DOOR LINER IS MISSING PLASTIC NUT. INSTALLED MISSING DOOR LINER PLASTIC NUT IAW AMM 52-13-31
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 39,632 hrs · 19,399 cycles
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.
Part: LIGHT — NO DISCREPANCY (ZONE 200) · airframe 39,630 hrs · 19,398 cycles
CREW REPORTS EMERGENCY EXIT LIGHTS ABOVE FWD GALLEY ON INTERMITTENT. PERFORMED OPS CHK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHKD GOOD.
Part: BATTERY — DISCONNECTED (FLASHLIGHT) · airframe 39,628 hrs · 19,397 cycles
AFT GALLEY RIGHT HAND INBD FLASHLIGHT INOPERATIVE. FOUND BATTERY DISCONNECTED; RECONNECTED EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD.
Part: CHARGER — INTERMITTENT (ZONE 200) · airframe 39,632 hrs · 19,399 cycles
EMERGENCY EXIT LIGHT ABOVE FWD GALLEY DOOR ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED FWD ENTRY EMERGENCY LIGHT CHARGER.
Part: FRAME — CRACKED (ZN 200 FUS TOP) · airframe 39,626 hrs · 19,396 cycles
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.
Part: SUPPORT BRACKET — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
CRACKED SUPPORT BRACKET, BS 867, STR 2R - STR 3R IN THE PAX CABIN. FAULT RESOLVED ON OTHER FAULT SEE TTG8Q01C79F8.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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 -.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: RIB — CRACKED (ZONE 300) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: SUPPORT BRACKET — CRACKED (ZONE 800) · airframe 39,626 hrs · 19,396 cycles
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.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: RIB — CRACKED (ZONE 300) · airframe 39,626 hrs · 19,396 cycles
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 -.
Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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.
Part: FRAME — CORRODED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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
Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: WEB — CORRODED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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 -.
Part: RIB — CRACKED (ZONE 300) · airframe 39,626 hrs · 19,396 cycles
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 -.
Part: FRAME — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
CRACKED FRAME, BS 312 BTW STR 5L - 6L. PERFORMED PERMANENT REPAIR ON FRAME IAW EA M-22-153-01244.
Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: SUPPORT BRACKET — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: ANGLE — CRACKED (ZONE 600) · airframe 39,626 hrs · 19,396 cycles
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.
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: BALANCE WEIGHT — OUT OF TOLERANCE (ZONE 300) · airframe 39,626 hrs · 19,396 cycles
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.
Part: BALANCE WEIGHT — OUT OF TOLERANCE (ZONE 300) · airframe 39,626 hrs · 19,396 cycles
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
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: SUPPORT — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: NUT PLATE — CRACKED (ZONE 500) · airframe 39,626 hrs · 19,396 cycles
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.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
DELAMINATED FLOOR PANEL 222BF. REPAIRED FLOOR PANEL 222BF AT FWD GALLEY AREA IAW SRM 53-00-50-2R-7, REPAIR 7.
Part: GUSSET — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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.
Part: GUSSET — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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.
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: WEB — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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 -.
Part: WEB — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: STRUCTURE — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: WEB — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: WEB — CORRODED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: WEB — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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 -.
Part: WEB — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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 -.
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
CRACKED FLOOR PANEL 222DF. REPAIRED THE FLOOR PANEL 222DF IAW SRM 53-00-50-2R-7, REPAIR 7.
Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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-.
Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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.
Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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.
Part: ACCESS PANEL — DELAMINATED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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.
Part: WEB — CORRODED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
CORRODED WEB, BS 986.5 + 4 INCHES, LBL 43, WL 208.1 IN THE AFT GALLEY AREA. FAULT RESOLVED ON OTHER FAULT TTG8Q01C650B.
Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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:
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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.
Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 39,626 hrs · 19,396 cycles
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.
Part: LENS — BROKEN (ZONE 200) · airframe 39,626 hrs · 19,396 cycles
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.
Part: FITTING — DETERIORATED (GIRT BAR) · airframe 39,626 hrs · 19,396 cycles
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.
Earlier reports · 2011–2025 · 99 reports
2025
Part: LATCH — INOPERATIVE (ZONE 200) · airframe 38,339 hrs · 18,752 cycles
RIGHT AFT ATTENDANT SEAT ACCESS DOOR FOR EMERGENCY FLASHLIGHT WILL NOT OPEN. REPLACED ACCESS DOOR LATCH IAW CMM 25-25-12. OPS OK.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 37,663 hrs · 18,410 cycles
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.
Part: FLAP SYSTEM — FALSE INDICATION · airframe 35,842 hrs · 17,451 cycles
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.
2024
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,320 hrs · 16,086 cycles
EMERGENCY LIGHTS INOP AT LH OVERWING EXITS. REMOVED, REPLACED AND OPS CHECKED BATTERY PACK IAW AMM 33-51-06
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,320 hrs · 16,086 cycles
LH AFT CABIN BULLNOSE EMERGENCY LIGHTS INOP. REMOVED REPLACED AND OPS CHECKED BATTERY PER AMM 33-51-06.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,320 hrs · 16,086 cycles
RH AFT CABIN BULLNOSE EMERGENCY LIGHTS INOP. REMOVED REPLACED AND OPS CHECKED BATTERY ACK PER AMM 33-51-06.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,320 hrs · 16,086 cycles
PANEL 242QF IS DELAMINATED.<[01] INSTALLED FLOOR PANEL IAW AMM 53-21-00.;[02] INSTALLED FLOOR PANEL IAW AMM 53-21-00.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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)
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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)]
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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)]
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,320 hrs · 16,086 cycles
PANEL 242HF IS DELAMINATED. PANEL 242FH IS DELAMINATED.<[01] INSTALLED FLOOR PANEL IAW AMM 53-21-00.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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)]
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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)].
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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.
Part: PANEL — DETERIORATED (FWD CARGO) · airframe 33,320 hrs · 16,086 cycles
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.
Part: INTERCOSTAL — CRACKED (BS 540 LBL1) · airframe 33,320 hrs · 16,086 cycles
CABIN FLOOR STRUCTURE INTERCOSTAL IS CRACKED AT FASTENER AT STA 540 LBL 1.<[01] REPLACED INTERCOSTAL PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (BS 540 RBL 1) · airframe 33,320 hrs · 16,086 cycles
CABIN FLOOR STRUCTURE INTERCOSTAL IS CRACKED AT FASTENER AT STA 540 RBL 1.<[01] REPLACED INTERCOSTAL PER SRM 51-40-02.
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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)]
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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)]
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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.
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
242FF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] FAULT RAISED IN ERROR DUE TO INCORRECT PANEL IDENTIFIER
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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)]
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
241BF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] REMOVED AND REPLACED FLOORBOARD IAW AMM 53-21-00.
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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)]
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
231ZF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] REMOVED AND REPLACED FLOORBOARD IAW AMM 53-21-00.
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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.
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
231YF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] REMOVED AND REPLACED FLOORBOARD IAW AMM 53-21-00.
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
241CF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] REMOVED AND REPLACED FLOORBOARD IAW AMM 53-21-00.
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
241EF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] REMOVED AND REPLACED FLOORBOARD IAW AMM 53-21-00.
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
242EF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] CARD GENERATED IN ERROR DUE TO INCORRECT PANEL IDENTIFIER
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
241FF CABIN FLOOR PANEL HAS DENTS AND PULLED FIBERS<[01] REMOVED AND REPLACED FLOORBOARD IAW AMM 53-21-00.
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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)]
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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)]
Part: FLOOR PANEL — PULLED (CABIN) · airframe 33,320 hrs · 16,086 cycles
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.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,835 hrs · 15,818 cycles
RH AFT EMERG LIGHTS INOP<[01] REPLACED RH AFT EMERG LIGHT POWER SUPPLY BATTERY REF AMM 33-51-06. OPS CHECK GOOD.
Part: COMPRESSOR — STALLED (ENGINE) · airframe 32,818 hrs · 15,810 cycles
ENGINE FAILURE AT FL190; COMPRESSOR STALL SUSPECTED. NR 2 ENG REPLACED.
Part: GIRT BAR — LOOSE (DOOR SLIDE) · airframe 32,520 hrs · 15,638 cycles
GIRT DRAGS THE FLOOR WHEN OPENING AFT ENTRY DOOR.<[01] RE-SECURED GIRT AFT ENTRY DOOR REF AMM 25-66-01.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,510 hrs · 15,634 cycles
AFT RIGHT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED AFT RIGHT SERVICE DOOR EXTERIOR EMERGENCY LIGHT PER AMM 33-51-04. CHECK GOOD.
Part: SLIDE — DISLODGED (ZN 800 DOOR) · airframe 32,234 hrs · 15,491 cycles
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.
2023
Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 32,016 hrs · 15,345 cycles
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.
Part: RIB — CRACKED (ZN 500 LEFT WING) · airframe 31,938 hrs · 15,292 cycles
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
Part: MEGAPHONE — BROKEN (ZN 200 FUS TOP) · airframe 31,938 hrs · 15,292 cycles
FWD CABIN MEGAPHONE BROKEN<[01] R/R FWD CABIN MEGAPHONE IAW AMM 25-64-00.
Part: COWLING — CRACKED (ZN 400 NACELLE/P) · airframe 31,938 hrs · 15,292 cycles
#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
Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 31,153 hrs · 14,833 cycles
AFT ENTRY DOOR SLIDE HANGING<[01] INSPECTED AND ADJUSTED AFT LH SLIDE FLAP IRW AMM 25-66-01 OPS TEST GOOD
Part: SLIDE — OUT OF POSITION (ZN 800 DOOR) · airframe 30,625 hrs · 14,518 cycles
FWD. SERVICE DOOR SLIDE DRAGS THE FLOOR WHERE IT ATTACHES TO GURT BAR.<[01] REPOSITIONED SLIDE REF MT 725-61-06.
Part: SENSOR — SPLIT (ZN 100 FUS LOWER) · airframe 30,288 hrs · 14,314 cycles
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.
Part: BATTERY PACK — INACCURATE (ZN 200 FUS TOP) · airframe 30,252 hrs · 14,292 cycles
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.
Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 30,251 hrs · 14,291 cycles
R2 EMERGENCY EXIT LIGHT INOP<[01] ENTERED IN ERROR
Part: SPLICE — SEVERED (ZN 100 FUS LOWER) · airframe 29,851 hrs · 14,063 cycles
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
Part: SPLICE — SEVERED (ZN 100 FUS LOWER) · airframe 29,851 hrs · 14,063 cycles
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
Part: SPLICE — SEVERED (ZN 100 FUS LOWER) · airframe 29,851 hrs · 14,063 cycles
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
Part: ENGINE — FAILED (ZN 400 NACELLE/P) · airframe 29,434 hrs · 13,827 cycles
#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
2022
Part: LIGHT — FAULTY (OVERWING EXIT) · airframe 27,308 hrs · 12,600 cycles
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
Part: CONNECTOR — INOPERATIVE (R1 DOOR) · airframe 27,308 hrs · 12,600 cycles
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
Part: LIGHT — INOPERATIVE (R/H CABIN) · airframe 27,308 hrs · 12,600 cycles
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.
Part: LIGHT — INOPERATIVE (R/H FUSELAGE) · airframe 27,308 hrs · 12,600 cycles
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.
Part: PLATE — CRACKED (FWD CARGO) · airframe 27,308 hrs · 12,600 cycles
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.
Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 27,308 hrs · 12,600 cycles
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.
Part: LIGHT — INOPERATIVE · airframe 26,576 hrs · 12,184 cycles
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.
2021
Part: WEB — CRACKED (RH WING) · airframe 25,731 hrs · 11,705 cycles
RH WING TRAILING EDGE DEFLECTION RIB/PANEL SUPPORT WEB CRACKED AT OUTBOARD FASTENER. ; / [01] REMOVED AND REPLACED SUPPORT WEB REF SRM 51-40-02.
Part: WEB — CRACKED (LH WING) · airframe 25,731 hrs · 11,705 cycles
LEFT WING TRAILING EDGE DEFLECTION RIB/PANEL SUPPORT WEB CRACKED AT OUTBOARD FASTENER. ; / [01] REMOVED AND REPLACED SUPPORT WEB REF SRM 51-40-02.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,893 hrs · 24,187 cycles
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
Part: PAN — CRACKED (R2 DOOR) · airframe 22,957 hrs · 10,214 cycles
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
2020
Part: ANTI-SKID SYS — INOPERATIVE (MLG) · airframe 22,636 hrs · 10,045 cycles
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.
Part: POSITION SENSOR — FAULTED (TE FLAPS) · airframe 22,486 hrs · 9,968 cycles
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.
Part: BRACKET — BROKEN (RT WING TE) · airframe 21,274 hrs · 9,362 cycles
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.
Part: SKIN — BENT (APU DOOR) · airframe 21,274 hrs · 9,362 cycles
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
Part: FAIRING — DEBONDED (LT FLAP TRACK) · airframe 21,274 hrs · 9,362 cycles
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)
Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 21,274 hrs · 9,362 cycles
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.
Part: BAFFLE — CORRODED (BS 747-767) · airframe 21,274 hrs · 9,362 cycles
**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
Part: SUPPORT — CORRODED (BS 947) · airframe 21,274 hrs · 9,362 cycles
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.
Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 21,274 hrs · 9,362 cycles
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
Part: SHIELD — CORRODED (AFT CARGO) · airframe 21,274 hrs · 9,362 cycles
*** 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
Part: CHANNEL — CORRODED (BS 927) · airframe 21,274 hrs · 9,362 cycles
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.
Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 21,274 hrs · 9,362 cycles
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
Part: CHANNEL — CORRODED (BS 727-807) · airframe 21,274 hrs · 9,362 cycles
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-
Part: SHIELD — CORRODED (AFT CARGO) · airframe 21,274 hrs · 9,362 cycles
*** 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
Part: CHANNEL — CORRODED (BS 727-767) · airframe 21,274 hrs · 9,362 cycles
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:-.
Part: SHIELD — CORRODED (FWD CARGO) · airframe 21,274 hrs · 9,362 cycles
***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
Part: CHANNEL — CORRODED (BS 500B-500I) · airframe 21,274 hrs · 9,362 cycles
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
Part: CHANNEL — CORRODED (BS 500A-500I) · airframe 21,274 hrs · 9,362 cycles
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
Part: SHIELD — CORRODED (BS 420-440) · airframe 21,274 hrs · 9,362 cycles
***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
Part: FLOORBEAM — CORRODED (BS 500I) · airframe 21,274 hrs · 9,362 cycles
***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
Part: SKIN — DENTED (BS 927) · airframe 21,274 hrs · 9,362 cycles
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
Part: SKIN — DENTED (CARGO DOOR) · airframe 21,274 hrs · 9,362 cycles
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.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,202 hrs · 9,326 cycles
EXTERIOR FUSELAGE EMRGCY. LT. INOP.; AFT OF LEFT WING TRAILING EDGE / RELAMPED PER AMM 33-51-04 OPS-OK
Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 20,433 hrs · 8,970 cycles
FORWARD FLIGHT ATTENDANT FLASHLIGHT RED LIGHT DID NOT FLASH. / R&R FLASHLIGHT PER AMM.
Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 20,154 hrs · 8,854 cycles
PHOTOLUMINESCENT STRIP FIRST OFFICER FORWARD SIDE INOP. / R&R PHOTOLUMINESCENT STRIP IAW AMM.
2019
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,321 hrs · 8,016 cycles
L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED LIGHT PER AMM.
Part: SLIDE — DISLODGED (R1 DOOR) · airframe 17,948 hrs · 7,852 cycles
R1 DOOR EMERGENCY ESCAPE SLIDE INADVERTENTLY CAME OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. / R&R SLIDE PER MT.
2017
Part: LIGHT — LOOSE (CABIN) · airframe 10,169 hrs · 4,460 cycles
MID CABIN CEILING EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM.
2016
Part: PUMP — LOW PRESSURE (NR 2 ENGINE) · airframe 8,570 hrs · 3,764 cycles
DIVERSION, B SYSTEM HYDRAULIC LOSS WITH LOW PRESSURE LIGHT ILLUMINATED. R&R NR 2 ENGINE DRIVEN PUMP PER MM.
Part: PUMP — LEAKING (HYD SYSTEM) · airframe 8,027 hrs · 3,490 cycles
A SYSTEM HYDRAULIC QUANTITY LOSS IN FLIGHT. R & R NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM.
2011
Part: CONTROL VALVE — FAILED (CABIN PRESSURE) · airframe 6,309 hrs · 6,712 cycles
PILOT REPORTED PRESSURIZATION SYSTEM REVERTED TO UNCOMMANDED EMERGENCY PRESSURIZATION MODE.