N953WN
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
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.
221 reports on file, 2011-02-16 – 2026-08-19.
Part: ISOLATOR — CRACKED (ZONE 800 SLIDE) · airframe 49,662 hrs · 30,638 cycles
AFT ENTRY DOOR UPPER FWD SLIDE MOUNT ISOLATOR CRACKED. R & R AFT ENTRY DOOR UPPER FWD SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.
Part: ISOLATOR — CRACKED (ZONE 800 SLIDE) · airframe 49,662 hrs · 30,638 cycles
FWD SERVICE DOOR FWD LOWER SLIDE ISOLATOR IS CRACKED. R & R FWD SERVICE DOOR FWD LOWER SLIDE ISOLATOR IAW SRM 51-40-02.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 49,517 hrs · 30,550 cycles
THE R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED THE R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT AND PERFORMED TEST IAW AMM 33-51-04-960-801. TESTED OK. TASK CARD COMPLETE.
Part: WEB — CORRODED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CORROSION WEB BTW BS 747 TO 767, RBL 21, AND WL 156 AT AFT CARGO COMPARTMENT. REPLACED WEB BTW BS 747 TO 767 RBL 21 AND WL 156 AT AFT CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9 AND DWG 146A7502 SHEET: 49 REV -.
Part: SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 49,520 hrs · 30,551 cycles
CRACKED SUPPORT ZEE, BS 887 - 907, RBL 21 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ZEE AND FASTENERS IAW SRM 51-40-02, & DWG 147A7500, SHEET 37, REV-.
Part: WEB — CORRODED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CORRODED SHIELD WEB, BS 767 - 794.3, WL 156, RBL 22 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02, AND DWG 146A0081, SHEET 43, REV -.
Part: WEB — CORRODED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CORROSION SHIELD WEB BTWN BS 490 - 500A, STR 26R, WL 156.5 IN THE FWD CARGO BAY. REPLACED SHIELD WEB IAW SRM 51-40-02-0G-0, AND DWG 143A0080, SHT 41, REV-.
Part: WEB — CORRODED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CORRODED SHIELD WEB, BTW BS 847 TO 867, WL156, AND RBL 22 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DRAWING 146A0081, SHEET 43, REV- .
Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CORROSION SUPPORT ANGLE, BS 500D, STR 26R - 26L AND WL 156.5 IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02, ITEM 9, & DWG 143A7902, SHT 259, REV -.
Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CORROSION TRACK RBBL 13.84 BTW STA 787 TO STA 847 AND WL 155 (5 POINTS) AT AFT CARGO COMPARTMENT. REPLACED TRACK AND FASTENERS, RBL 13.84 BTW BS 767 - 887 AND WL 155 AT AFT CARGO BAY IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, AND DRAWING 146A7500, SHEET 173, REV-.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CORRODED SUPPORT ZEE, BS 500A - 500D, STR 26R, WL 156.5 IN THE FWD CARGO BAY. REPLACED THE SUPPORT ZEE & FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 143A7500 SHEET: 71 AND REV-.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CORRODED SUPPORT ZEE, BTW BS 727A - 767, RBL 21, WL 156 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ZEE AND FASTENERS IAW SRM 51-40-02-0G-0, DWG 146A7500, SHEET 13, REV-, & DRAWING 146A7500, SHT 174, REV-.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CORROSION SUPPORT ZEE BTWN BS 727B - 827, LBL 21, WL 156. ( 10 POINTS ) IN THE AFT CARGO BAY. INSTALLED SUPPORT ZEE AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 146A7500, SHT 137, REV-.
Part: ANGLE — CRACKED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CRACKED ANGLE BTWN BS 907 - 927, S25R - 27R IN THE AFT OF AFT CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, AND DWG 147A7221, SHEET 28, REV -.
Part: STRINGER CLIP — CORRODED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CORRODED STRINGER CLIP BS 787, STR 26R, WL 152 IN THE AFT CARGO BAY. REPLACED THE STRINGER CLIP IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG 146A1262, SHT 116, REV- .
Part: ISOLATOR — DETERIORATED (ZONE 800) · airframe 49,520 hrs · 30,551 cycles
DETERIORATED MOUNT ISOLATOR UPPER POSITION AT EMERGENCY EXIT LT SIDE (2EA). REPLACED MOUNT ISOLATOR UPPER POSITION AT EMERGENCY EXIT LT SIDE (2EA) IAW SRM-51-10-02, ITEM 9, AND DWG 144A8111, SHEET 61, REV -.
Part: ISOLATION MOUNT — DETERIORATED (ZONE 800) · airframe 49,520 hrs · 30,551 cycles
DETERIORATE ISOLATION MOUNTS, UPPER POSITION ON THE RT EMERGENCY EXIT, (2EA). REPLACED THE ISOLATION MOUNTS IAW SRM-51-10-02, ITEM 9, AND DWG:144A8111, SHT 61, REV-.
Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CRACKED FLOOR PANEL 120BF IN THE FWD CARGO BAY. REPLACED FLOOR PANEL 120BF IAW SRM 51-10-02-0G-0, PARA 9, AND DWG 453A1610, SHT 7, REV C.
Part: STRINGER — CRACKED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CRACKED STRINGER 25R, BS 540, FWD CARGO BAY, REPAIRED THE STRINGER 25R, BETWEEN BS 500C - 540 IAW SRM 53-00-03-2R-1, REPAIR 1.
Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 49,520 hrs · 30,551 cycles
CRACKED BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW RBL24.82 TO BL0 AT PASSENGER CABIN. REPLACED BRAKE PANEL FLOOR STRUCTURE BS540 AND BTW RBL24.82 TO BL0 AT PASSENGER CABIN IAW SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 ITEM 9 AND DWG:143A0060 SHEET:64 REV:- .
Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 49,520 hrs · 30,551 cycles
CRACKED BRAKE PANEL FLOOR STRUCTURE BS 540 BTW LBL 24.82 TO BL 0. REPLACED THE BRAKE PANEL AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, STEP 9, & DWG 143A0060, SHT 58, REV A.
Part: ANGLE — CRACKED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CRACKED ANGLE, BS 867, S26L, AFT CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, AND DRAWING 149A8102, REV A, SHT 19.
Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 49,520 hrs · 30,551 cycles
CRACKED LEADING EDGE RIB, ACCESS PANEL 331B HSS 114.55 LT HORIZONTAL STAB. REPLACED THE LEADING EDGE RIB ACCESS PANEL 331B IAW SRM 51-40-02-0G-0, AND DWG 186A1001, SHT 19, REV-.
Part: FRAME — CRACKED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CRACKED FRAME, BS 312, S5L & 6L IN THE FWD GALLEY AREA. REPAIRED FRAME IAW M-22-153-01244, SEE TTG8Q01D738K. COMPLETED TASK.
Part: WEB — CRACKED (ZONE 400) · airframe 49,520 hrs · 30,551 cycles
CRACKED SUPPORT WEB, OTBD FAN COWL UPPER POSITION ON NR 2 ENGINE. REPLACED THE SUPPORT WEB AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & 71-13-30.
Part: ANGLE — CRACKED (ZONE 100) · airframe 49,520 hrs · 30,551 cycles
CRACKED ANGLE BS 400, STR 26L IN THE FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 143A7505, SHEET 117, REV- .
Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 49,520 hrs · 30,551 cycles
ELONGATED HOLE ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-9, REPAIR 9.
Part: GLOWSTRIP — DETERIORATED (ZONE 200) · airframe 49,520 hrs · 30,551 cycles
DETERIORATED PHOTOLUMINESCENT STRIP ALONG PAX CABIN. REPLACED AND PHOTOLUMINESCENT STRIP ALONG PAX CABIN IAW AMM 33-51-15-400-802, STEP 1.E (1) (3) (5), & DWG 33500007, REV 2.
Part: ACCESS PANEL — ELONGATED (ZONE 500) · airframe 49,520 hrs · 30,551 cycles
ELONGATED HOLE ON ACCESS PANEL 561BB, LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-9, REPAIR 9.
Part: SKIN — CRACKED (RT NR 6 SLAT) · airframe 49,520 hrs · 30,551 cycles
CRACKED LOWER SURFACE OF LEADING EDGE SLAT 6 NOSE SKIN AT THE ACTUATOR LOCATION. AROUND FASTENER. PERFORMED A REPAIR ON THE LOWER SURFACE OF LEADING EDGE SLAT 6 NOSE SKIN IAW SRM 51-40-02, AND SRM 57-42-01-2R-8, REPAIR 8, AND DWG 114A5030, REV A, SHEET 2.
Part: SKIN — CRACKED (RT NR 7 SLAT) · airframe 49,520 hrs · 30,551 cycles
CRACK LOWER SURFACE OF RT WING LEADING EDGE SLAT 7 NOSE SKIN AT ACTUATOR LOCATION AROUND THE FASTENER. PERFORMED A REPAIR ON LOWER SURFACE OF LEADING EDGE SLAT 7 NOSE SKIN IAW SRM 57-42-01-2R, REPAIR 8, & DWG 114A5020, REV A, SHEET 38.
Earlier reports · 2011–2025 · 190 reports
2025
Part: SUPPORT FITTING — CORRODED (ZONE 700) · airframe 47,745 hrs · 29,362 cycles
LEFT MAIN LANDING GEAR FWD TRUNNION SUPPORT FITTING, LOWER INBOARD LUG NR 4. OUTER FACE HAS EVIDENCE OF CORROSION. R & R LT MLG FWD TRUNNION SUPPORT FITTING; LOWER INBD LUG NR 4 PER EA. 1-A57-3246.
Part: SEAL — CRACKED (ZONE 300) · airframe 47,555 hrs · 29,238 cycles
R/H HORIZONTAL UPPER SLIDER IS CRACKED. R & R STABILIZER-TO-BODY FRONT SPAR UPPER SLIDING SEAL PER M/M 53-31-31.
Part: LENS — BROKEN (ZONE 200) · airframe 46,570 hrs · 28,607 cycles
EXIT LIGHT COVER LENS BY L1 DOOR BROKEN. R&R EXIT LIGHT COVER LENS IAW AMM 33-51-02
Part: SLIDE — DISLODGED (ZONE 800) · airframe 45,170 hrs · 27,717 cycles
FWD ENTRY DOOR SLIDE FELL OUT OF SLIDE COMPARTMENT<[01] 01 - REMOVED AND REPLACED PER [AMM 25-66-01-400-804-NG (ESCAPE SLIDE PACK INSTALLATION (UNSCHEDULED) - PERMANENT)]
Part: MEGAPHONE — LOOSE (ZN 200 FUS TOP) · airframe 44,956 hrs · 27,581 cycles
AFT MEGAPHONE HANDLE LOOSE.<[01] REMOVED AND REPLACED AFT MEGAPHONE PER AMM25-64-00.
2024
Part: FAIRING — CRACKED (ZONE 600) · airframe 44,345 hrs · 27,209 cycles
THE #8 FLAP TRACK FWD FAIRING (644AB) HAS A CRACK ON LOWER SURFACE<[01] REPAIRED CRACK ON #8 FWD FAIRING 644AB IAW SRM 51-70-05-2R-2;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-7
Part: STIFFENER — CRACKED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
VERTICAL STIFFENER IS CRACKED BS 663 LBL 26 WL 145<[01] CRACKED STIFFENER FOUND AT BS 663 LBL 26 WL 145; REMOVED AND INSTALLED NEW VERTICAL STIFFENER AT BS 663 LBL 26 WL 145 PER SRM 51-40-02-0G-0 AND DWG 111A1000 REV: A. FASTENERS COMMON TO VAPOR BARRIER WEB WILL BE INSTALLED IN CUSTOMER CARD # TTG8Q00WEF8N.;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE
Part: ATTACH BRACKET — CRACKED (ZONE 600) · airframe 44,345 hrs · 27,209 cycles
651FB ATTACHING BRACKET (MARKED) IS CRACKED<[01] REMOVED AND REPLACED 651FB ATTACHING BRACKET; PER SRM 51-40-02-0G-0 AND BOEING DWG 115A2710 SHEET 2 REV.B;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE
Part: WEB — CRACKED (ZONE 500) · airframe 44,345 hrs · 27,209 cycles
LT WING FIXED T/E PANEL LOWER WEB HAS CRACK JUST IB OF DEFLECTION RIB ORSS 279. MARKED<[01] REMOVED; REPLACED; AND INSTALLED A NEW LT WING FIXED T/E PANEL LOWER WEB ORSS 279 IAW SRM 51-40-02 AND BOEING DWG 115A2512 SH 4.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
Part: SKATE ANGLE — CHAFED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
CHAFED LH CROWN SKATE ANGLE AT BS1058 LBL11. WL308.5.<[01] REPAIRED LH CROWN SKATE ANGLE AT BS1058 LBL11. WL308.5 IAW SRM 53-80-71-2R-6.;[02] VERIFIED CORRECTIVE ACTION
Part: RIB — CRACKED (ZONE 300) · airframe 44,345 hrs · 27,209 cycles
R/H HORIZONTAL STABILIZER L/E 341B FIRST I/B RIB IS CRACKED (PANEL MARKED)<[01] REMOVED & REPLACED R/H HORIZONTAL STABILIZER L/E 341B FIRST I/B RIB I.A. W SRM 51-40-02 AND DWG 186A1301 LE STA 78.29;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
CABIN FLOOR PANEL 231GF TOP SURFACE IS DELAMINATED.<[01] INSTALLED CABIN FLOOR PANEL 231GF PER AMM 53-21-00-400-801;[02] REMOVED AND REPLACED FLOOR PANEL 231GF PER AMM 53-21-00-000-801; AMM 53-21-00-400-801
Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 44,345 hrs · 27,209 cycles
B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 28 W.L. 164.<[01] CRACK FOUND TO BE OUT OF LIMITS AS PER SRM 57-10-10-1A-2. PART WILL BE REMOVED AND REPLACED ON FAULT TTG8Q00WF8Z9;[02] VERIFIED CORRECTIVE ACTION
Part: STUB FRAME — CRACKED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
2EA CRACKS ON R1 DOOR STUB FRAME INNER SURFACE; ONE ABOVE SEAL DEPRESSOR BS295+4 WL266 L: 0.8'; ONE EXTENDING FROM AFT EDGE BS295+5 WL266 L: 0.2'<[01] DO NOT INSTALL NEW PART; SEE INCOMPLETE SUB-STEP 4 FOR 'FINISH COAT' APPLICATION.;[02] PARTIAL SUB-STEP 4 VERIFIED; OK TO INSTALL PAINTED FRAME.;[03] REMOVED DAMAGED STUB FRAME AND INSTALLED NEW UPPER STUB FRAME ON R1 DOOR P/N 141A8370U13 I.A.W. SRM 51-40-02-0G-0; DWG# 141A8370 REV. D;[04] VERIFIED RII CORRECTIVE ACTION ITEM 3; CARD COMPLETE
Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 44,345 hrs · 27,209 cycles
B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8 W.L. 164.<[01] REMOVED; REPLACED; AND INSTALLED NEW B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE PER SRM 51-40-02-0G-0; AND DWG 111A1000 REV:-.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
CABIN FLOOR PANEL 241AF TOP SURFACE IS DELAMINATED.<[01] COMPLETE STEP 1;[02] FABRICATED NEW 241AF FLOOR PANEL USING BMS4-17 TY6 LOT # 1569956-1; LIGHTLY SANDED EDGES; LOCATED; DRILLED AND UPSIZED ALL (44EA) THROUGH INSERT LOCATIONS IAW SRM 53-00-50-2R-0 PAR. 4. A. (1). TABLE 204. 5. S. AND BOEING DWG: 144A5810 ID: 0127
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
CABIN FLOOR PANEL 241DF TOP SURFACE IS DELAMINATED.<[01] COMPLETED STEP 1;[02] REMOVED AND REPLACED FLOOR PANEL 241DF PER AMM 53-21-00-000-801 AND AMM 53-21-00-400-801
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
CABIN FLOOR PANEL 231DF TOP SURFACE IS DELAMINATED.<[01] UPDATED STEP 1;[02] REMOVED FLOOR PANEL 231DF IAW AMM TASK 53-21-00-000-801 PAR. 2. E. RECEIVED NEW FLOOR PANEL DUE TO EXTENSIVE TOP SURFACE DELAMINATION. CLOSED FLOOR PANEL 231DF IAW AMM 53-21-00-400-801 TOOLING ID:PER1631<BR>DUE DATE: 02/2025;[03] VERIFIED COMPLETION CORRECTIVE ACTION 2 AND MEASUREMENT TABLE.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
CABIN FLOOR PANEL 231XF TOP SURFACE IS DELAMINATED.<[01] UPDATED STEP 1;[02] REINSTALLED NEW SERVICEABLE CABIN FLOOR PANEL 231XF PER AMM 53-21-00-400-801;[03] REMOVED & REPLACED NEW SERVICEABLE CABIN FLOOR PANEL 231XF PER AMM 53-21-00-400-801 & AMM 53-21-00-000-801 PAR. 2. E.;[04] CORRECTIVE ACTION COMPLETED.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
CABIN FLOOR PANEL 231KF TOP SURFACE IS DELAMINATED.<[01] REMOVED AND REPLACED CABIN FLOOR PANEL 231KF PER AMM 53-21-00-000-801 AND PER AMM 53-21-00-400-801;[02] VERIFIED CORRECTIVE ACTION 1
Part: SKIN — DEBONDED (ZONE 100) · airframe 44,345 hrs · 27,209 cycles
PANEL 191D INNER SKIN HAS MULTIPLE DISBONDS. (MARKED)<[01] PANEL 191D WITH MULTIPLE DISBONDS ON INNER SKIN WAS REPAIRED IAW SRM 51-70-05-2R-2.
Part: SKIN — DEBONDED (ZONE 100) · airframe 44,345 hrs · 27,209 cycles
PANEL 194CR OUTER SKIN IS DISBONDED. (MARKED)<[01] PANEL 194CR OUTER SKIN WAS DISBONDED AND REPAIRED IAW SRM 53-60-70-2R-1;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
Part: SKIN — DEBONDED (ZONE 100) · airframe 44,345 hrs · 27,209 cycles
PANEL 191HL OUTER SKIN IS DISBONDED. (MARKED)<[01] DISBOND ON OUTER SKIN OF PANEL 191HL WAS REPAIRED IAW SRM 51-70-05-2R-2.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
CABIN FLOOR PANEL 241NF TOP SURFACE IS DELAMINATED.<[01] UPDATED STEP 1;[02] UPDATED STEP 1;[03] REMOVED FLOOR PANEL 241NF IAW AMM TASK 53-21-00-000-801 PAR. 2. E. RECEIVED NEW FLOOR PANEL DUE TO EXCESSIVE DELAMINATION. CLOSED FLOOR PANEL 241NF IAW AMM 53-21-00-400-801 TOOLING ID:PER1631<BR>DUE DATE: 02/2025;[04] VERIFIED COMPLETION CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
CABIN FLOOR PANEL 241RF TOP SURFACE IS DELAMINATED.<[01] UPDATED STEP 1;[02] UPDATED STEP 1;[03] REMOVED FLOOR PANEL 241RF IAW AMM TASK 53-21-00-000-801 PAR. 2. E. RECEIVED NEW FLOOR PANELDUE TO EXTENSIVE TOP SURFACE DELAMINATION. CLOSED FLOOR PANEL 241RF IAW AMM 53-21-00-400-801 TOOLING ID:PER1631<BR>DUE DATE: 02/2025;[04] VERIFIED COMPLETION CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
CABIN FLOOR PANEL 241KF TOP SURFACE IS DELAMINATED.<[01] COMPLETE STEP 1;[02] FABRICATED NEW 241KF FLOOR PANEL USING BMS4-17 TY6 LOT # 1569956-1; LIGHTLY SANDED EDGES; LOCATED; DRILLED AND UPSIZED ALL (32EA) THROUGH INSERT LOCATIONS IAW SRM 53-00-50-2R-0 PAR. 4. A. (2). TABLE 204. 5. S. (1) (A) - (D). AND BOEING DWG: 146A5810 ID: 0505.;[03] COMPLETED STEP 1;[04] STEP 1 COMPLETE
Part: VAPOR BARRIER — DETERIORATED (ZONE 100) · airframe 44,345 hrs · 27,209 cycles
LOWER R/H BS663 VAPOR BARRIER PREVIOUS REPAIR IS DISBONDED 'MARKED'<[01] LOWER R/H BS663 VAPOR BARRIER PREVIOUS REPAIR DAMAGE HAS BEEN REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED JOB COMPLETE
Part: VAPOR BARRIER — DEBONDED (ZONE 100) · airframe 44,345 hrs · 27,209 cycles
LOWER L/H BS663 VAPOR BARRIER PREVIOUS REPAIR IS DISBONDED 'MARKED'<[01] LOWER L/H BS663 VAPOR BARRIER PREVIOUS REPAIR DAMAGE HAS BEEN REPAIRED PER [SRM 51-70-04-2R-10-A00755 (REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES - AIRFRAME - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED JOB COMPLETE
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
PASSENGER CABIN FLOOR PANEL 241BF IS DELAMINATED AND HAS PLACARDS MISSING<[01] PASSENGER CABIN FLOOR PANEL 241BF; WITH DELAMINATION AND MISSING PLACARDS; WAS REPLACED WITH A NEWLY FABRICATED PANEL THAT INCLUDES ALL OF THE APPLICABLE PLACARDS; ALL OF THE WORK WAS PERFORMED IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810 SHEET 189.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
Part: LIGHT — DAMAGED (ZONE 200) · airframe 44,345 hrs · 27,209 cycles
G1 GALLEY EMERGENCY EXIT INDICATOR LIGHT ASSY DAMAGED<[01] REMOVED AND REPLACED G1 GALLEY EMERGENCY EXIT INDICATOR LIGHT PER AMM 33-51-01-960-802.;[02] REMOVED AND REPLACED G1 GALLEY EMERGENCY EXIT INDICATOR LIGHT ASSY PER AMM 33-51-01-960-802 STEP 3.C.(5); (10);[03] VERIFIED CORRECTIVE ACTIN STEP 2. TASK CARD COMPLETE.
Part: HOUSING — BROKEN (ZONE 200) · airframe 43,825 hrs · 26,880 cycles
ROW 6 ABC EMERGENCY LIGHT HOUSING ASSY BROKEN.<[01] REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-51-03. OPS CHECK GOOD.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 43,822 hrs · 26,879 cycles
EXT AFT L/H AND R/H EMERGENCY SLIDE LIGHT INOP.<[01] REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY IAW AMM 33-51-06. OPS CHECK GOOD.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 43,822 hrs · 26,879 cycles
ROW 6 ABC AND 9 ABC EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY IAW AMM 33-51-06. OPS CHECK GOOD.
Part: GIRT BAR — WORN (ZONE 200) · airframe 34,715 hrs · 17,185 cycles
GIRT WORN<[01] REMOVED AND REPLACED GIRT PER CMM 25-60-37.;[02] C/W INSPECTION
Part: FASTENER — MISSING (GIRT BAR) · airframe 43,684 hrs · 26,790 cycles
L2 DOOR GIRT BAR CLIP RIVET MISSING<[01] RR'D FASTENER PER SRM 51-40-02
Part: RIVET — MISSING (L2 GIRT BAR) · airframe 43,583 hrs · 26,731 cycles
L2 DOOR GIRT BAR CLIP RIVET MISSING<[01] OK TO CONTINUE PER EA M-23-125-01839.
Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 43,388 hrs · 26,617 cycles
AFT CARGO PIT FLOOR PANEL FORWARD OF ENTRY WAY HAS A CRACK / TEAR COMPLETELY THROUGH THE FIGER GLASS PANEL<[01] OK TO CONTINUE PER MEL 25-16-01 SP1B PLACARD INSTALLED;[02] REMOVED AND REPLACED AFT CARGO FLOOR PANEL FORWARD OF ENTRY WAY PER AMM 25-52-10
Part: COVER — BROKEN (LIGHT SWITCH) · airframe 43,053 hrs · 26,421 cycles
THE PLASTIC COVER ON THE EMERGENCY LIGHTS SWITCH IN AFT GALLEY IS BROKEN.<[01] READJUST SPRING COVER PER SIP
2023
Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 40,914 hrs · 25,050 cycles
EMERGENCY LIGHT POWER SUPPLY FAILED TEST AT LOCATION M1669<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK; POWER SUPPLY AT LOCATION M1669 OPS CHECK GOOD PER AMM 33-51-06
Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 40,914 hrs · 25,050 cycles
EMERGENCY LIGHT BATTERIE PACKS FAILED CAPACITY TEST AT LOCATIONS M1674; M1669; M1673 EMERGENCY LIGHT BATTERIE PACKS FAILED CAPACITY TEST AT LOCATIONS M1674 M1669 M1673<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS M1674 M1669; M1673 OPS CHECK GOOD; PER AMM 33-51-06
Part: SIGN — MISSING (ZN 200 FUS TOP) · airframe 40,556 hrs · 24,816 cycles
OVERWING EXIT SIGN MISSING<[01] REINSTALLED LENS IAW M/M 33-51-01
Part: SIGN — BROKEN (ZN 200 FUS TOP) · airframe 40,512 hrs · 24,786 cycles
OVERWING EMERGENCY EXIT SIGN MOUNTING BRACKET BROKEN.<[01] REMOVED AND REPLACED OVERWING EMERGENCY EXIT SIGN HOUSING IAW AMM 33-51-01-960-802. OPS CHECK GOOD.
Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 40,332 hrs · 24,664 cycles
PERFORMING EA M-23-157-02273; FOUND 3 INCH CRACK ON VAPOR BARRIER AT B.S 663; RBL 40; W.L.228<[01] C/W EA M-21-157-00675
Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 40,332 hrs · 24,664 cycles
PERFORMING EA M-23-157-02273; FOUND 7 INCH CRACK ON VAPOR BARRIER AT B.S 663; BETWEEN RBL 45.64-54.21; W.L.228<[01] C/W EA M-21-157-00675
Part: SIGN — BROKEN (ZN 200 FUS TOP) · airframe 40,110 hrs · 24,511 cycles
FA REPORTS EXIT SIGN IN EXIT ROW BROKE<[01] R&R'D OVERWING EMER EXIT SIGN PER 33-51-01
Part: BRACKET — LOOSE (ZN 200 FUS TOP) · airframe 39,792 hrs · 24,310 cycles
FORWARD SERVICE DOOR RIGHT GIRT BAR BRACKET IS LOOSE AND MISSING A RIVET<[01] REINSTALLED GIRT BAR BRACKET IAW SRM 51-40-02.
Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 39,737 hrs · 24,270 cycles
EMERGENCY EXIT SIDEWALL LIGHT INOP AT 12F<[01] RELAMPED WINDOW LIGHT AT 12F IAW AMM 33-21-00. OPS CHECK GOOD
Part: COVER — LOOSE (ZN 200 FUS TOP) · airframe 39,073 hrs · 23,841 cycles
FO SIDE OVER WING WINDOW EXIT SIGN COVER FOR THE HANDLE WILL NOT STAY IN PLACE.<[01] INSTALLED OVERWING EXIT COVER PER STANDARD INDUSTRY PRACTICES. OPS CK GOOD.
2022
Part: HANDLE — LOOSE (L1 DOOR ASSIST) · airframe 38,362 hrs · 23,373 cycles
CUSTOMER WALK.....L1 DOOR AFT LWR ASSIST HANDLE IS LOOSE. / [01] SECURED LOWER ASSIST HANDLE ON L1 DOOR PER REF AMM 52-11-31-400-802;[02] VERIFIED STEP 1.
Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 38,362 hrs · 23,373 cycles
CUSTOMER WALK....L2 DOOR GRIT BAR SKIRT IS DRAGGING NEEDS STOWED. / [01] REMOVED AND REINSTALLED L2 DOOR SLIDE ;STOWED L2 DOOR GRIT BAR SKIRT AS PER MT 725-61-06(REM/INSTL-SLIDE REMOVAL AND INSTALLATION) (AFT ENTRY) TTG8Q00G0A4D;[02] VERIFIED STEP 1
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,362 hrs · 23,373 cycles
EMERGENCY LIGHT BATTERY/POWER SUPPLY (M1672) INOP. REMOVED AND REPLACED EMERGENCY BATTERY CHARGER ASSY AND BATTERY PACK AS PER REF B737 AMM 33-51-06-960-806 AND AMM 33-51-06-960-805. PERFORMED OP TEST IAW AMM 33-51-06-960-806 STEP (5) (B), FOUND NORMAL. PERFORMED OP TEST IAW AMM 33-51-06-960-806, FOUND NORMAL.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,362 hrs · 23,373 cycles
EMERGENCY AISLE LIGHT INOP AT LEFT SIDE ROW 9. REMOVED AND REPLACED BATTERY PACK FUSE FROM BATTERY PACK (M1670) IAW AMM 33-51-06-960-804.<BR>PERFROM FUSE TEST. TEST PASSED.
Part: ACCESS PANEL — CRACKED (BULHEAD) · airframe 38,362 hrs · 23,373 cycles
FWD CARGO COMPARTMENT FWD BULKHEAD PANEL 122HW EXTERNAL SURFACE HAS CRACK. REMOVED THE DAMAGED PLIES AN PREPARED AREA TO APPLY THE CARBON FABRIC REPAIR PLIES. NO WATER NOTE AT REPAIR AREA ON ACCESS PANEL 122 HW EXTERNAL SURFACE IAW SRM 51-70-04-2R-1, PARAGRAPH 4. REPAIRED DAMAGED AREA AT ACCESS PANEL 122 HW EXTERNAL SURFACE IAW SRM 51-70-04-2R-1 PARAGRAPH 4. PAINTED REPAIR AREA AT ACCESS PANEL 122 HW EXTERNAL SURFACE IAW SRM 51-70-04-2R-1 PARAGRAPH 4.
Part: CAP — ELONGATED (ZONE 100) · airframe 38,362 hrs · 23,373 cycles
SEVERAL CAPSTRIPS IN FWD CARGO HAVE ELONGATED HOLES. INSTALLED NEW CAPSTIPS IAW SRM 51-40-02-0G-0.
Part: PLATE — DAMAGED (AFT CARGO) · airframe 38,362 hrs · 23,373 cycles
AFT CARGO FWD AND AFT CAP STRIPS PLATES WITH HOLES ELONGATED. RECEIVED NEW CAP STRIPS PLATES ON AFT CARGO FWD. AND AFT SIDE. NEW PLATES TO BE INSTALLED ON CUSTOMER CARD TTG8Q004BV37.
Part: SUPPORT BRACKET — CRACKED (BS 540) · airframe 38,362 hrs · 23,373 cycles
R/H AIR CONDITIONING BAY BS 540 INB CROSSOVER AIR DUCT SUPPORT BRACKET CRACKED. REMOVED L/H A/C BAY STA 540 INB CROSS-OVER AIR DUCT SUPPORT BRACKET IAW SRM 51-40-02-0G-0. REMOVED RT A/C BAY BS 540 INB CROSSOVER AIR DUCT SUPPORT BRACKET IAW SRM 51-40-02-0G-0. REPLACED RT A/C BAY INBD CROSSOVER AIR DUCT SUPPORT BRACKET IAW SRM 51-40-02-0G-0.
Part: GUSSET — CRACKED (BS 500D S19L) · airframe 38,362 hrs · 23,373 cycles
FWD CARGO COMPARTMENT. L/H SIDE WALL GUSSET CRACKED AT S19L, BS 500D. REMOVED THE GUSSET IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW GUSSET IAW SRM 51-40-05-0G-0. TREATED AND PRIMED HOLES IAW SRM 51-40-02-0G-0. INSTALLED THE NEW GUSSET IAW SRM 51-40-02-0G-0 & DWG 143A7902.
Part: SUPPORT BRACKET — CRACKED (BS 540) · airframe 38,362 hrs · 23,373 cycles
LEFT AIR CONDITIONING BAY BS 540 INBD CROSSOVER AIR DUCT SUPPORT BRACKET CRACKED. REMOVED THE SUPPORT BRACKET IAW SRM 51-40-02-0G-0. REPLACED THE LT A/C BAY BS 540 INBD CROSSOVER AIR DUCT SUPPORT BRACKET IAW SRM 51-40-02-0G-0.
Part: SUPPORT ANGLE — CRACKED (BS 312 S5L) · airframe 38,362 hrs · 23,373 cycles
L1 DOOR CUT OUT UPPER STRUCTURE STA312 STR5 SUPPORT ANGLE CRACKED. ACCOMPLISHED TRIM REPAIR ON L1 DOOR CUT OUT UPPER STRUCTURE FRAME IAW EA. M-22-153-01244.
Part: CARGO TRACK — CORRODED (ZN 100 FUS LOWER) · airframe 38,362 hrs · 23,373 cycles
AFT CARGO TRACK BETWEEN BS 767+12 AND 867 RBL 14 S-26R WL 156 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02-0G-0, REMOVED MORE THAN 10%. FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED THE CARGO TRACK BS 779.5-887 IAW SRM 51-40-02-0G-0. LOCATED & DRILLED NEW CARGO TRACK IAW SRM 51-40-05-0G-0. TREATED AND PRIMED IAW AMM 51-21-41-370-802, & AMM 51-21-72-370-804, INSTALLED THE NEW TRACK IAW SRM 53-00-53-2R-3.
Part: GUSSET — CRACKED (BS 500D S19R) · airframe 38,362 hrs · 23,373 cycles
FWD CARGO COMPARTMENT GUSSET AT BS 500D, S19R FOUND CRACKED. REMOVED THE GUSSET IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW GUSSET IAW SRM 51-40-05-0G-0. TREATED AND PRIMED THE NEW GUSSET IAW SRM 51-20-01-0G-0. INSTALLED AND SEALED THE NEW GUSSET IAW SRM 51-40-02-0G-0.
Part: SUPPORT BRACKET — CRACKED (AFT CARGO) · airframe 38,362 hrs · 23,373 cycles
AFT CARGO FWD BULKHEAD LOWER RT SIDE OF CENTER PANEL SUPPORT BRACKET IS BROKEN. PANEL SUPPORT BRACKET REMOVED IAW SRM 51-40-02-0G-0-A00729. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G-0 AND DRAWING 144A9401.
Part: FLOOR SUPPORT — CRACKED (BS 400 BL 0) · airframe 38,362 hrs · 23,373 cycles
FWD WET AREA BETWEEN STA380 TO STA400 BL0 FLOOR STIFENER CRACK DOT EV43 / [01] REMOVED AND REPLACED FWD WET AREA BETWEEN STA380 TO STA400; BL'0'; WL208; FLOOR ANGLE/STIFFENER REF. SRM 51-40-02-0G-0 AND DRAWING 143A5400;[02] VERIFIED STEP 1
Part: FLOOR PANEL — DAMAGED (BS 540) · airframe 38,362 hrs · 23,373 cycles
CABIN FLOOR CENTER AREA BS 540, LBL 0-20 PANEL BRAKE ASSY HOLES ENLONGATED. REMOVED AND REPLACED PANEL BREAK IAW SRM 51-40-02-0G-0.
Part: FLOOR SUPPORT — CRACKED (BS 277-292 BL 0) · airframe 38,362 hrs · 23,373 cycles
FWD WET AREA BET STA277 TO STA292 BL0 WL208 FLOOR STIFENER HAS CRACK DOT EV41 / [01] REMOVED AND REPLACED FWD WET AREA FLOOR INTERCOSTAL BET. STA.277 & STA.292; BL 'O'; WL 208; REF. SRM 51-40-02-0G-0;[02] VERIFIED STEP 1
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 38,362 hrs · 23,373 cycles
CABIN FLOOR PANEL 241PF UPPER SKIN SURFACE HAS FRAYING. (18-041) / [01] RECEIVED NEW CABIN FLOOR PANEL P/N 146A5810-462; (241 PF) NEW PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00E0Z9A;[02] VERIFIED STEP 1.
Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 38,362 hrs · 23,373 cycles
MLG LEFT SIDE STA.663; VAPOR BARRIER WEB HAS CRACK. CLEANED THE VAPOR BARRIER, STOP DRILLED THE CRACKS. PREPARED DAMAGE AREAS FOR REPAIR; PERFORMED DRY OUT, FOUND NO WATER IAW SRM 51-70-04-2R-10, REPAIRED THE DAMAGE WITH A PERMANENT REPAIR ON THE VAPOR BARRIER WEB IAW SRM 51-70-04-2R-10. PERFORMED TAP TEST ON REPAIRED AREA, FOUND NO DELAMINATION IAW SRM 51-05-01 SECTION 5.
Part: FLOOR PANEL — FRAYED (CABIN) · airframe 38,362 hrs · 23,373 cycles
CABIN FLOOR PANEL 241NF UPPER SKIN SURFACE FRAYING. RECEIVED NEW CABIN FLOOR PANEL 241NF. WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00E0Z9C.
Part: FLOOR PANEL — FRAYED (CABIN) · airframe 38,362 hrs · 23,373 cycles
RIGHT CABIN FLOOR PANEL 242MF UPPER SKIN SURFACE HAS FRAYING. NEW FLOOR PANEL INSTALLED ON CUSTOMER CARD TTG8Q00E10NJ.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 38,362 hrs · 23,373 cycles
CABIN FLOOR PANEL 241UF UPPER SKIN SURFACE FRAYING. RECEIVED NEW CABIN FLOOR PANEL 241UF. ISSUE TAG AL7130.
Part: SUPPORT ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 38,362 hrs · 23,373 cycles
MLG A/C BAY AFT SECTION STA663 VAPOR BARRIER ANGLE SUPPORT HAS CRACK DOT EV34 / [01] REMOVED FASTENERS AT RT UPPER WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE FROM RBL-5 TO RBL-60 STA 663 REF USED SRM 51-40-02-0G-0;[02] REMOVED RT SIDE UPPER VAPOR BARRIER ANGLE AT STA 663 BETWEEN RBL-5 TO RBL-60 REF USED SRM 51-40-02-0G-0;[04] FABRICATED REAR SPAR WING CENTER SECTION RT SIDE UPPER VAPOR BARRIER ANGLE MATERIAL USED 2024-0.063' REF USED DWG#111A1322;[05] CORRECTION STEP#4:FABRICATED REAR SPAR WING CENTER SECTION RT SIDE UPPER VAPOR BARRIER ANGLE MATERIAL USED 2024-0.063' PO#1748073 LOT#362761B9 REF USED DWG#111A1322;13] INSTALLED VAPOR BARRIER WEB RT SIDE ANGLE AND PARTIALLY INSTALLED FASTENERS FROM RBL-5 TO RBL-60 REF USED SEM 51-40-02-0G-0;[14] VERIFIED STEP 13 PARTIALLY FASTENERS INSTALLATION;[15] INSTALLED 100% FASTENERS AT RT VAPOR BARRIER WEB ANGLE REF USED SRM 51-40-02-0G-0AND DWG#111A1000;[16] REM0VED AND REPLACE MLG BAY AFT SECTION STA 663 BETWEEN RBL-5 TO RBL-60 UPPER ANGLE REF USED SRM 51-40-02-0G-0 AND DWG#111A1000;[17] VERIFIED STEPS 15 AND 16<BR><BR>PENDING LEAK CHECK;[18] LEAK CHECK WILL BE ACCOMPLISHED ON CARD # TTG8Q00FL81H;[19] STEP 17 IS RII; VERIFIED INSTALLATION;[20] VERIFIED STEP 18 LEAK CHECK WILL BE ACCOMPLISHED ON CARD # TTG8Q00FL81H
Part: FLOOR PANEL — FRAYED (CABIN) · airframe 38,362 hrs · 23,373 cycles
CABIN FLOOR PANEL 241XF UPPER SKIN SURFACE FRAYING. REPAIRED THE FLOOR PANEL 241XF IAW SRM 53-00-50-2R-1, PARA 3.M.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 38,362 hrs · 23,373 cycles
CABIN FLOOR PANEL 241RF UPPER SKIN SURFACE HAS FRAYING. (18-045) / [01] RECEIVED NEW CABIN FLOOR PANEL P/N 146A5810-466; (241RF) ; NEW FLOOR PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00E0Z96;[02] VERIFIED STEP 1.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 38,362 hrs · 23,373 cycles
RIGHT HORIZONTAL STAB, STA. 120.30 RIB STIFFENER NR 2 CRACKED AT LOWER RADIUS. REMOVED DAMAGE ON STIFFENER IAW SRM 55-10-09-2R-4. PERFORMED HFEC INSP ON CUTOUT AREA IAW NDT P6 51-00-00 PROC.23, NO CRACKS. PERFORMED ROTO INSP ON 8 EXISTING HOLES IAW NDT P6 51-00-00, PROC 16, NO CRACKS. PERFORMED GVI OF ALL AREAS WITHIN THE REPAIR AREA IAW SRM 55-10-09-2R-4. NO DEFECTS NOTED. LOCATED AND DRILLED REPAIR IAW SRM 51-40-05-0G-0. TREATED AND PRIMED REPAIR & RIB IAW AMM 51-21-41-370-802 & AMM 51-21-72-370-804. INSTALLED THE STIFFENER REPAIR IAW SRM 55-10-09-2R-4 & APPLIED FILLET SEAL IAW SRM 51-20-05-0G-0.
Part: STIFFENER — CRACKED (HORIZONAL STAB) · airframe 38,362 hrs · 23,373 cycles
RIGHT HORIZONTAL STABILIZER STAB. STA. 120.30 RIB STIFFENER # 2 HAS A CRACK AT LOWER RADIUS. REPAIRED STIFFENER 2 ON R/H HORIZONTAL.
Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 38,362 hrs · 23,373 cycles
AFT CARGO COMPARTMENT FLOOR PANEL 140DF CRACKED. FABRICATED AFT CARGO FLOOR PANEL 140 DF IAW AMM 25-52-01-201-801.
Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 38,362 hrs · 23,373 cycles
MLG RIGHT SIDE STA.663; VAPOR BARRIER WEB HAS 2EA CRACKS / [01] MEASUREMENTS;[02] CLEANED AND PREPARED CRACK DAMAGE AREA AS MARKED FOR REPAIR ON RIGHT SIDE VAPOR BARRIER; STOP DRILL CRACK; PERFORMED DRY OUT; FOUND NO WATER AS PER B737 SRM 51-70-04-2R-10;[03] VERIFIED STEP 1;[04] VERIFIED STEP 2. OK TO APPLY REPAIR.;[05] REPAIRED CRACK DAMAGE ON MLG RIGHT SIDE VAPOR BARRIER STA 663 WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-10; MATERIALS USED PO#1690463 AND PO#1774613;[06] PERFORMED TAP TEST ON REPAIRED AREA; FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION 5;[07] VERIFIED STEP 5 AND 6;[08] LATE ENTRY.APPLIED TEFLON PAINT ON MLG RIGHT SIDE (VAPOR BARRIER WEB) REF: B 737 AMM 51-21-81-370-802;[09] VERIFIED STEP #8; TEFLON PAINT APPLIED.;[10] REPAIRED MLG R/H SIDE VAPOR BARRIER STA 663 WITH PERMANENT REPAIR REF SRM 51-70-04-2R-10; MATERIAL USED PO#1690463 AND PO#1774613; AND APPLIED TEFLON PAINT REF: AMM 51-21-81-370-802;[11] FINAL INSPECTION; R/H MLG VAPOR BARRIER REPAIRED; WORK ACCOMPLISHED.
Part: BRACKET — CRACKED (ACCESS PANEL) · airframe 38,362 hrs · 23,373 cycles
L/H WING T/E ACCESS PANEL 551GB INTERNAL SURFACE HAS (1 EACH) BRACKET CRACKED. REMOVED AND REPLACED BRACKET ON L/H WING T/E ACCESS PANEL #551GB REF. SRM 51-40-02-0G-0.
Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 38,362 hrs · 23,373 cycles
AFT CARGO COMPARTMENT FLOOR PANEL 140BF CRACKED. FABRICATED NEW AFT CARGO FLOOR PANEL 140 BF PER REF AMM 25-52-01-201-801.
Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 38,362 hrs · 23,373 cycles
AFT CARGO COMPARTMENT FLOOR PANEL 140AF CRACKED. FABRICATED NEW AFT CARGO FLOOR PANEL 140AF PER REF AMM 25-52-01-201-801.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 38,362 hrs · 23,373 cycles
LEFT HORIZONTAL STAB INSPAR RIB NR 5, STA 129.50 STIFFENER CRACKED. PERFORMED HFEC INSP ON RIB 5 STIFFENER 3 IAW NDT P6 51-00-00, PROC 23. CRACK NOTED. LOCATED & DRILLED REPAIR IAW SRM 51-40-05-0G-0. TREATED AND PRIMED REPAIR AND RIB IAW AMM 51-21-41-370-802 & AMM 51-21-72-370-804. INSTALLED RIB STIFFENER REPAIR IAW SRM 55-10-09-2R-4 & APPLIED FILLET SEAL IAW SRM 51-20-05-0G-0.
Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 38,362 hrs · 23,373 cycles
ACCESS PANEL 661BB CORNER HOLES ENLONGATED / [01] PREPARED AREA FOR REPAIR AT ACCESS PANEL 661BB AS PER BOEING 737 SRM 51-70-04-2R-9.;[02] REPAIRED DAMAGE HOLE AT ACCESS PANEL 661BB AS PER BOEING 737 SRM 51-70-04-2R-9. MATERIAL USED EY 3804 PO#1779804 PLUS BMS9-3-120TYD CL7;[03] ACCOMPLISHED TAP TEST ON ACCESS PANEL 661BB FOUND NO DELAMINATION AS PER BOEING 737 NTM 51-05-01.;[04] RESTORED ORIGINAL FINISHED AT PANEL 661BB AS PER BOEING 737 AMM 51-21-99-300-801.;[05] (LATE ENTRY) VERIFIED STEP #1; AREA PREPARED FOR REPAIR.;[06] VERIFIED STEPS #2; #3 AND #4.;[07] FINAL INSPECTION; SCREW HOLE REPAIRED.
Part: PANEL — ELONGATED (FUSELAGE) · airframe 37,504 hrs · 22,798 cycles
PANEL 193B HAS NUMEROUS ELONGATED COUNTERSINK FASTENER HOLES. / [01] REPLACED PANEL 193B PER SRM 51-40-02;[02] VERIFIED REPLACE PANEL 193B PER SRM 51-40-02
Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 37,160 hrs · 22,570 cycles
FWD CARGO COMPARTMENT FLOOR PANEL 120CF HAS MULTIPLE CRACKS. ONE CRACK IS 11 INCHES AND THE OTHER TWO ARE 5 INCHES. / [01] R&R?D FWD CARGO COMPARTMENT FLOOR REF AMM 25-52-10
2021
Part: ANGLE — CRACKED (R2 DOOR) · airframe 35,693 hrs · 21,636 cycles
SUPPLEMENTAL INFORMATION: AFT GALLEY SERVICE DOOR-LOWER DOOR LINER WEB SUPPORT ANGLE CRACKED (RT.SIDE) ; / [01] R&R AFT GALLEY SERVICE DOOR-LOWER DOOR LINER WEB SUPPORT ANGLE. REF AMM 52-41-31
Part: PUMP — FAULTED (FUEL SYSTEM) · airframe 33,321 hrs · 20,230 cycles
CENTER TANK FUEL PUMPS WOULD NOT PUMP FUEL IN LEVEL FLT. CENTER TANK HAD 950# AND LOW PRESSURE LIGHTS ILLUMINATED FOR CENTER TANK. / C/W FUEL QTY COMPARISON CHECK PER M/M 28-41-00. NO FAULTS NOTED ON FQIS. FUWL PUMPS AND INDICATION NORMAL AT THIS TIME.
2020
Part: ANGLE — CORRODED (FWD CARGO) · airframe 33,003 hrs · 20,050 cycles
FWD. CARGO COMP. L/H TRANSITION ANGLE HAS CORROSION AROUND 4 EA. FASTENER HOLES BETWEEN STA. 500 AND 500D. / REMOVED AND REPLACED FWD CARGO L/H TRANSITION ANGLE 480+9 TO 500D IAW SRM 51-40-02
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,003 hrs · 20,050 cycles
CABIN CENTER SECTION STRUCTURE HAS A CRACKED INTERCOSTAL AT STA 540 RBL 4. REMOVED AND REPLACED, PER SRM 51-40-02.
Part: FLOORBOARD — DAMAGED (CABIN) · airframe 33,003 hrs · 20,050 cycles
CABIN FLOOR BOARD 231XF HAS FIBER DAMAGE ON UPPER SURFACE. / REMOVED AND REPLACED FLOOR BOARD PER AMM 53-21-00
Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 33,003 hrs · 20,050 cycles
CABIN FLOOR SUPPORT CRACKED STA 540 AT LBL-1 / REMOVED AND REPLACED PER SRM 51-40-02
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 33,003 hrs · 20,050 cycles
RT STAB INSPAR RIB AT STAB STA 120.30 HAS A CRACK AT THE NR 4 STIFFNER LOWER END (HFEC VERIFIED). REPAIRED IAW SRM 55-10-09-2R-4. SEE WIPS FOR INDIVIDUAL SIGN-OFFS.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 33,003 hrs · 20,050 cycles
RT STAB INSPAR RIB AT STAB STA 120.30 HAS A CRACK AT THE NR 3 STIFFENER LOWER END (HFEC VERIFIED). REPAIRED IAW SRM 55-10-09-2R-4. SEE WIPS FOR INDIVIDUAL SIGN-OFFS.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 33,003 hrs · 20,050 cycles
RT STAB INSPAR RIB AT STAB STA 137.70 HAS A CRACK AT THE NR 4 STIFFENER LOWER END (HFEC VERIFIED). INSTALLED RIB STIFFENER REPAIR, PER SRM 55-10-09-2R-4.
Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 33,003 hrs · 20,050 cycles
FLIGHT COMPARTMENT FLOOR HAS LARGE CREASE IN FLOOR SKIN WHICH IS DENTED OVER FRAME AT STA 257 LBL14. INSTALLED FLIGHT DECK REPAIR WEB, IAW SRM 51-40-02 & EA1-753-33612. PAINTED FLIGHT DECK REPAIR WEB, IAW SOPM 20-41-04. SEE TASK AND WIPS FOR INDIVIDUAL SIGN-OFFS.
Part: PANEL — CORRODED (RT WING) · airframe 33,003 hrs · 20,050 cycles
RH WING REFUELING GAUGE MOUNT PANEL HAS CORROSION AROUND GAUGE CUT-OUTS (MARKED) / REMOVED AND REPLACED REFUELING MOUNT PANEL PER MM 28-41-61
Part: SEAL — CHAFED (HORIZONTAL STAB) · airframe 33,003 hrs · 20,050 cycles
LH HORIZONTAL PANEL 333AT SLIDING SEAL CHAFED/WORN (MARKED) / REPLACED SEAL PER SRM 51-40-02
Part: PANEL — CORRODED (DRAIN MAST) · airframe 33,003 hrs · 20,050 cycles
PANEL 192CR HAS CORROSION ON DRAIN MAST BASE. / REMOVED AND REPLACED FWD DRAIN MAST BASE; PANEL 192CR; PER SOPM 20-50-19.
Part: PANEL — CORRODED (NLG WW) · airframe 33,003 hrs · 20,050 cycles
NWW PANEL 113AC LIGHT SURFACE CORROSION ON LANDINGS / REMOVED AND REPLACED PANEL PER M/M 53-14-01; PANEL WILL BE INSTALLED ON ROUTINE CARD J PANEL 115 CLOSE
Part: PANEL — CORRODED (NLG WW) · airframe 33,003 hrs · 20,050 cycles
NWW PANEL 113BW LIGHT SURFACE CORROSION ON LANDINGS / REMOVED AND REPLACED PANEL PER M/M 53-14-01; PANEL WILL BE INSTALLED ON ROUTINE CARD J PANEL 115 CLOSE
Part: PLATE — CRACKED (RT WING) · airframe 33,003 hrs · 20,050 cycles
RH WING REAR SPAR LOWER CHORD WAFFLE PLATE CRACKED JUST IB OF #6 FLAP TRACK (MARKED) / R&R'D WAFFLE PLATE PER SRM 51-40-02.
Part: SEAL — CHAFED (HORIZONTAL STAB) · airframe 33,003 hrs · 20,050 cycles
RH HORIZONTAL PANEL 343AT SLIDING SEAL CHAFED/WORN (MARKED) / REPLACED SEAL PER SRM 51-40-02
Part: PANEL — CORRODED (NLT WW) · airframe 33,003 hrs · 20,050 cycles
NWW PANEL 114AC LIGHT SURFACE CORROSION ON LANDINGS / REMOVED AND REPLACED PANEL PER M/M 53-14-01; PANEL WILL BE INSTALLED ON ROUTINE CARD JPANEL 115 CLOSE
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,829 hrs · 19,947 cycles
EXTERIOR EMERGENCY LIGHT NEAR AFT ENTRY DOOR INOPERABLE. RELAMPED IAW AMM 33-51-04. OPERATIONS CHECK GOOD AT THIS TIME.
2019
Part: PANEL — CRACKED (L/H ELEVATOR) · airframe 30,751 hrs · 18,639 cycles
L/H ELEVATOR HINGE COVER PANEL# 334GB FOUND CRACKED AT CUTAWAY. / REMOVED AND REPLACED PER SIP
Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 29,764 hrs · 18,009 cycles
OVERWING EXIT SIGN LOOSE. / INSTALLED SIGN IAW AMM.
Part: LENS — UNSECURE (EXIT SIGN) · airframe 28,731 hrs · 17,345 cycles
EXIT SIGN OVER EMERGENCY EXIT ROWS FELL OFF. R&R LENS PER AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,249 hrs · 17,042 cycles
LT OVERWING EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.
2018
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 27,271 hrs · 16,375 cycles
FORWARD CARGO DOOR CUTOUT SEVERAL NUTPLATE HOLES CORRODED BETWEEN BS 800 TO BS 807. REPAIRED CUTOUT PER EA.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,271 hrs · 16,375 cycles
FORWARD CARGO INTERCOSTAL CRACKED BETWEEN BS 500A TO BS 500B, RBL 25. REPAIRED INTERCOSTAL PER SRM.
Part: RETAINER — CRACKED (LEFT WING) · airframe 27,271 hrs · 16,375 cycles
#3 FLAP TRACK AFT SUPPORT FAIRING I/B & O/B SEALS ARE WORN & O/B CENTER SEAL RETAINER IS CRACKED. / REMOVED & REPLACED #3 FLAP TRACK SUPPORT FAIRING O/B FWD. & AFT SEALS AND I/B SEAL PER SOPM 20-50-01 & M/M 27-51-18. R&R CENTER SEAL PER SRM 51-40-02. SEAL COMPRESSION CHECK GOOD PER AMM 27-51-18
Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 27,271 hrs · 16,375 cycles
FORWARD CARGO R/H TRANSITION ANGLE HAS CORROSION FROM STA 500A TO STA 500D / REMOVED AND REPLACED FORWARD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500D PER SRM 51-40-02
Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,271 hrs · 16,375 cycles
FORWARD CARGO FLOOR STRUCTURE L ANGLE CORRODED AT BS 500D, BETWEEN LBL 24 TO RBL 24. REPAIRED L ANGLE PER SRM.
Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 27,271 hrs · 16,375 cycles
SUPPLEMENTAL INFORMATION: FWD CARGO; AFT CORNER THRESHOLD CRACKED. / R&R FWD CARGO; AFT CORNER SCUFF PLATE PER AMM 53-11-02.
Part: NONE — CRACKED (LWR FUSELAGE) · airframe 27,271 hrs · 16,375 cycles
SUPPLEMENTAL INFORMATION: PANEL 195CL HAS CRACK ON AFT END IN THE RADIUS OF THE BEND. / APPLIED REPAIR PLIES AND BONDED PER SRM 51-70-05 REPAIR 6.
Part: STRAP — CORRODED (FUSELAGE) · airframe 27,271 hrs · 16,375 cycles
AFT CARGO COMPARTMENT THRESHOLD STRAP CORRODED AT BS 809, RBL 20. REPAIRED STRAP PER SRM.
Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 27,271 hrs · 16,375 cycles
SUPPLEMENTAL INFORMATION: 222CF FIBERGLASS STRANDS PULLED FROM SURFACE; AND EXCESS SEALANT AROUND EDGES. / PASSENGER CABIN FLOOR PANEL REMOVED PER AMM 53-21-00. NEW PANEL IS GOING TO BE INSTALL ON ROUTINE CARD JPANEL-222 -CLOSE.
Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 27,271 hrs · 16,375 cycles
THE FORWARD CARGO R/H TRANSITION ANGLE HAS CORROSION FROM STA 495 TO STA 500A. / FABRICATED TRANSITION ANGLE PER DRAWING 143A8126. INSTALLED PER SRM. 51-40-02; AND DRAWING 143A0080.
Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 27,271 hrs · 16,375 cycles
SUPPLEMENTAL INFORMATION: 221CF FLOORBOARD FIBERGLASS STRANDS PULLED FROM SURFACE; AND EXCESS SEALANT AROUND EDGES. / PASSENGER CABIN FLOOR PANEL REMOVED PER AMM 53-21-00. NEW PANEL IS GOING TO BE INSTALL ON ROUTINE CARD JPANEL-221 -CLOSE.
Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 27,271 hrs · 16,375 cycles
SUPPLEMENTAL INFORMATION: 221GF FIBERGLASS STRANDS PULLED FROM SURFACE; AND EXCESS SEALANT AROUND EDGES. / PASSENGER CABIN FLOOR PANEL REMOVED PER AMM 53-21-00. NEW PANEL IS GOING TO BE INSTALL ON ROUTINE CARD JPANEL-221 -CLOSE.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,271 hrs · 16,375 cycles
FORWARD CARGO FLOOR STRUCTURE L ANGLE CORRODED AT BS 540, BETWEEN LBL 24 TO RBL 24. REPAIRED L ANGLE PER SRM.
Part: RETAINER — CORRODED (LT HORIZ. STAB.) · airframe 27,271 hrs · 16,375 cycles
L/H HORIZONTAL STABILIZER PIVOT HINGE BUSHING IS WORN INTO BUSHING RETAINER WITH EVIDENCE OF FRETTING. REF AMM 27-41-31 FIG 402 ITEMS [1] AND [17] / FACT AS A RESULT OF POST REPAIR INSPECTION. REF. AMM 27-41-31 FIG 402 ITEMS 1 & 17. REPAIRED PER EA 1-753-33635, SRM 51-20-01 & SOPM 20-41-02.
Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 27,271 hrs · 16,375 cycles
THE FORWARD CARGO R/H TRANSITION ANGLE HAS CORROSION FROM STA 500A TO STA 540. / REMOVED AND REPLACED FORWARD CARGO R/H TRANSITION ANGLE FROM STA 500A TO STA 500D ACCOMPLISHED ON NR#G607659
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 27,271 hrs · 16,375 cycles
221BF FLOORBOARD PANEL POTTED INSERTS MISSING; AND PANEL DELAMINATED AT EDGE OUTBOARD AFT CORNER. (MARKED)ALSO NEEDS SEALANT REMOVED FROM EDGES. / PASSENGER CABIN FLOOR PANEL REMOVED PER AMM 53-21-00. NEW PANEL IS GOING TO BE INSTALL ON ROUTINE CARD JPANEL-221 -CLOSE.
Part: SEAL — CRACKED (R/H HORIZ. STAB.) · airframe 27,271 hrs · 16,375 cycles
R/H HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL CRACKED / REMOVED; AND REPLACED SLIDING SEAL. FUNCTIONAL CHECK GOOD. REF. AMM. 53-31-31
Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 27,271 hrs · 16,375 cycles
SUPPLEMENTAL INFORMATION: 222BF FLOORBOARD PANEL DALRON CORRODED; DRAINS DIRTY; AND EXCESS SEALANT AROUND EDGES. / PASSENGER CABIN FLOOR PANEL REMOVED PER AMM 53-21-00. NEW PANEL IS GOING TO BE INSTALL ON ROUTINE CARD JPANEL-222 -CLOSE.
Part: SEAL PLATE — CRACKED (L/H HORIZ. STAB.) · airframe 27,271 hrs · 16,375 cycles
L/H HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL CRACKED / REMOVED AND REPLACED L/H HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL; OPS CK GOOD PER SRM 53-31-31.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 27,271 hrs · 16,375 cycles
AFT CARGO ON TOP OF THRESHOLD WEB CORRODED BETWEEN BS 807-10 TO BS 847-7. REPAIRED WEB PER SRM.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,271 hrs · 16,375 cycles
AFT CARGO FLOOR ANGLE CORRODED BETWEEN BS 792+4 TO BS 792+6, RBL 13.84. REPAIRED ANGLE PER SRM.
Part: ANGLE — CRACKED (AFT CARGO BAY) · airframe 27,271 hrs · 16,375 cycles
AFT CARGO FLOOR TO LAV VAC TANK CORNER POST ANGLE HAS A CRACK BACK SIDE OF FITTING STA 876 LEFT HAND / REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE AT STATION 876; AFT CARGO FLOOR TO LAV VAC TANK CORNER POST I/A/W SRM 51-40-02.
Part: COVER — UNSECURE (EXIT SIGN) · airframe 25,389 hrs · 15,155 cycles
R1 DOOR LOWER EMERGENCY EXIT SIGN COVER FELL OFF. R&R SIGN ASSEMBLY PER MM.
Part: NONE — BENT (FWD FUSELAGE) · airframe 24,864 hrs · 14,824 cycles
STRINGER CLIP BENT BS480 STR24L / STRINGER CLIP BENT AT B.S 480 STR 24L 'THE DAMAGE IS REPAIRED BY ATS ER 18-01598 REV IR AND SWA EA1-753-32324 REV IR'
Part: SHEAR TIE — CRACKED (FWD FUSELAGE) · airframe 24,864 hrs · 14,824 cycles
SHEAR TIE CRACKED BS480 STR 21 TO 22L / REMOVED DAMAGED SHEARTIC AT B.S 480 STR 21L TO STR 22L PER SRM 51-40-02 LOCATED; DRILLED AND INSTALLED NEW SHEARTIC AT B.S 480 STR 22L AND STR 21L PER DRAWING 143A1220
Part: SHEAR TIE — CRACKED (FWD FUSELAGE) · airframe 24,864 hrs · 14,824 cycles
SHEAR TIE CRACKED BS480 STR23 TO 24L / REMOVED SHEARTIC AT B.S 480 STR 23L TO STR 24L PER SRM 51-40-02 LOCATED; DRILLED AND INSTALLED NEW SHEARTIC AT B.S 480 STR 23L TO STR 24L PER DRAWING 143A1220
Part: NONE — BENT (FWD FUSELAGE) · airframe 24,864 hrs · 14,824 cycles
STRINGER CLIP BENT BS 480 STR 22L / STRINGER CLIP BENT AT B.S480 STR 22L'THE DAMAGE IS REPAIRED BY ATS ER 18-01598 REV IR AND SWA EA1-753-32324 REV IR'
Part: FRAME — BENT (FWD FUSELAGE) · airframe 24,864 hrs · 14,824 cycles
FRAME BENT BS480 BETWEEN STR 20L AND FLOOR TO SIDEWA LL SUPPORT FRAME LH MOD / FRAME BENT BS480 BETWEEN STR 20L AND FLOOR TO SIDE WALL SUPPORT LH SIDE WAS REPAIRED PER ATS ER18-01680 REV IR; SWA EA #1-753-32332 REV IR; ATS ER 18-01599 REV IR AND SWA EA 1-753-32352 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION
Part: DOUBLER — BENT (FWD FUSELAGE) · airframe 24,864 hrs · 14,824 cycles
BS 480 FRAME DOUBLER BENT STR19 TP 24L / B.S 480 FRAME DOUBLER IS BENT BETWEEN STR19 TO STR24L 'THE DAMAGE IS REPAIRED BY ATS ER 18-01599 REV IR AND SWA EA1-753-32532 REV IR'
Part: NONE — BENT (FWD FUSELAGE) · airframe 24,864 hrs · 14,824 cycles
STRINGER CLIP BENT AT BS480 STR 21L / STRINGER CLIP BENT AT B.S 480 STR21L 'THE DAMAGE IS REPAIRED BY ATS ER 18-01598 REV IR AND SWA EA1-753-32324 REVIR'
Part: NONE — BENT (FWD FUSELAGE) · airframe 24,864 hrs · 14,824 cycles
FRAME FAIL SAFE BENT BS480 STR 20 TO 24L / FRAME FAIL SAFE IS BENT B.S 480 STR 20L TO STR 24L' THE DAMAGE IS REPAIRED BY ATS ER 18-01599 REV IR AND SWA EA1-753-32352 REV IR'
Part: STRINGER — BENT (FWD FUSELAGE) · airframe 24,864 hrs · 14,824 cycles
STRINGER 21L BENT BETWEEN BS460 TO 500 / STRINGER 21L BENT BETWEEN B.S 460 TO B.S 500 'THE DAMAGE IS REPAIRED BY ATS ER 18-01598 REV IR AND SWA EA1-753-32324 REV IR'
Part: STRINGER — BENT (FWD FUSELAGE) · airframe 24,864 hrs · 14,824 cycles
STR 22L BENT BETWEEN BS460 TO 500 / STR 22L BENT BETWEEN B.S 460 TO B.S 500 'THE DAMAGE IS REPAIRED BY ATS ER 18-01598 REV IR AND SWA EA1-753-32324 REV IR'
Part: STRINGER — BENT (FWD FUSELAGE) · airframe 24,864 hrs · 14,824 cycles
STR 23L BENT BETWEEN BS460 TO 500 / STR 23L BENT BETWEEN B.S 460 TO 500 'THE DAMAGE IS REPAIRED BY ATS ER 18-01598 REV IR AND SWA EA1-753-32324 REV IR'
Part: SHEAR TIE — CRACKED (FWD FUSELAGE) · airframe 24,864 hrs · 14,824 cycles
SHEAR TIE CRACKED BS480 STR 22 TO 23L / REMOVED SHEARTIC AT B.S 480 STR 22L TO STR 23L PER SRM 51-40-02 LOCATED; DRILLED AND INSTALLED NEW SHEARTIC AT B.S 480 STR 22L AND STR 23L PER DRAWING 143A1220
Part: SKIN — DAMAGED (BS 460-500) · airframe 24,864 hrs · 14,824 cycles
FUSELAGE SKIN DAMAGED BETWEEN BS 460 TO 500, STRINGERS 21L TO 23L. REPAIRED THE SKIN IAW ER AND EA.
Part: NONE — BENT (FWD FUSELAGE) · airframe 24,864 hrs · 14,824 cycles
STRINGER CLIP BENT BS480 STR 23L / STRINGER CLIP BENT AT B.S480 STR 23L'THE DAMAGE IS REPAIRED BY ATS ER 18-01598 REV IR AND SWA EA1-753-32324 REV IR'
Part: BATTERY PACK — FAILED (CABIN) · airframe 24,518 hrs · 14,605 cycles
EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01675. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 24,518 hrs · 14,605 cycles
EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01673. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 24,518 hrs · 14,605 cycles
EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01670. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 24,518 hrs · 14,605 cycles
EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01668. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 24,518 hrs · 14,605 cycles
EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01672. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 24,518 hrs · 14,605 cycles
EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01674. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 24,518 hrs · 14,605 cycles
EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01669. R&R BATTERY PACK PER AMM.
2017
Part: LANYARD — LOOSE (R1 DOOR SLIDE) · airframe 22,946 hrs · 13,576 cycles
R1 DOOR SLIDE COVER LANYARD LOOSE. SECURED THE LANYARD PER MT.
Part: LENS — LOOSE (R2 DOOR) · airframe 22,282 hrs · 13,157 cycles
R2 DOOR EMERGENCY EVAC SLIDE COVER LENS LOOSE. SECURED LENS PER AMM AND MT.
Part: SKIN — GOUGED (BS 381) · airframe 22,015 hrs · 13,008 cycles
FUSELAGE SKIN GOUGED AT BS 381, ABOVE STRINGER 7L. REPAIRED THE SKIN IAW EA.
2016
Part: GLOWSTRIP — CRACKED (CABIN) · airframe 20,803 hrs · 12,272 cycles
FORWARD AISLE PHOTO LUMINESCENT STRIP CRACKED. R&R STRIP PER AMM.
Part: SKIN — DAMAGED (LT WING) · airframe 20,803 hrs · 12,272 cycles
LT WING FIXED LEADING EDGE SKIN DAMAGED BETWEEN NR 2 AND NR 3 RIB AT APPROXIMATELY STA 180. REPAIRED SKIN IAW EA.
Part: PANEL — DAMAGED (FUSELAGE) · airframe 20,803 hrs · 12,272 cycles
AFT CENTER WHEEL WELL SUPPORT STRUCTURE DAMAGED AT AREA COMMON TO PANEL 193D AT BS 727. REPAIRED PANEL ASSEMBLY PER ACO.
Part: RIB — CORRODED (HORIZONTAL STAB) · airframe 20,803 hrs · 12,272 cycles
RIGHT HORIZONTAL STABILIZER FORWARD RIB CRACKED AT HSS 92.70. REPAIRED THE RIB IAW SRM.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 20,803 hrs · 12,272 cycles
RIGHT HORIZONTAL STABILIZER MIDDLE AFT RIB CRACKED AT HSS 92.70. REPAIRED THE RIB IAW SRM.
Part: STRAP — CORRODED (BS 772) · airframe 20,803 hrs · 12,272 cycles
AFT CARGO BIN FLOOR STRAP CORRODED AT BS 772. R & R THE STRAP IAW SRM.
Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 20,163 hrs · 11,868 cycles
RIGHT HORIZONTAL STAB CRACKED AT HSS 101.90, 10 INCHES FORWARD OF REAR SPAR. REPAIRED THE STABILIZER IAW SRM.
Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 20,163 hrs · 11,868 cycles
RIGHT HORIZONTAL STAB CRACKED AT HSS 147.96, 9 INCHES FORWARD OF REAR SPAR. REPAIRED STABILIZER IAW SRM.
2015
Part: BATTERY — INOPERATIVE (CABIN) · airframe 15,980 hrs · 9,427 cycles
RIGHT OVERWING EXIT LIGHT BATTERY PACK INOPERATIVE. R & R BATTERY IAW MM.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 15,071 hrs · 8,926 cycles
LEFT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STATION 157.10, 15 INCHES AFT OF FRONT SPAR. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 15,071 hrs · 8,926 cycles
LEFT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 157.10, 8 INCHES AFT OF FRONT SPAR. REPAIRED SKIN IAW SRM.
Part: GLOWSTRIP — CRACKED (CABIN) · airframe 14,808 hrs · 8,765 cycles
FORWARD RT PHOTO LUMINESCENT STRIP CRACKED AT ROW 1. R & R STRIP IAW AMM.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 14,347 hrs · 8,499 cycles
BRACKET CRACKED AT BS 277, STRINGER 25R. R & R BRACKET IAW SRM & EA.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 14,347 hrs · 8,499 cycles
BRACKET CRACKED AT BS 268.25, STRINGER 25R. R & R BRACKET IAW SRM.
2014
Part: BATTERY PACK — FAILED (CABIN) · airframe 13,699 hrs · 8,126 cycles
M01675 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 13,699 hrs · 8,126 cycles
M01669 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 13,699 hrs · 8,126 cycles
M01673 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.
Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 13,699 hrs · 8,126 cycles
CENTER WING REAR SPAR VAPOR WEB CRACKED AT BS 663.75 RBL 49.0. REPAIRED WEB IAW EA.
Part: BATTERY PACK — FAILED (CABIN) · airframe 13,699 hrs · 8,126 cycles
M01672 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.
Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 13,699 hrs · 8,126 cycles
CENTER WING REAR SPAR VAPOR WEB CRACKED AT BS 663.75 RBL 44.0. REPAIRED WEB IAW EA.
Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 13,699 hrs · 8,126 cycles
LEFT WW FWD BULKHEAD VAPOR WEB CRACKED AT BS 663, LBL 40.00. REPAIRED WEB IAW EA.
Part: COVER — LOOSE (CABIN) · airframe 13,647 hrs · 8,093 cycles
RIGHT OVERWING EMER EXIT LOOSE. SECURED COVER IAW SIP.
Part: LENS — BROKEN (CABIN) · airframe 10,810 hrs · 6,409 cycles
RT OVERWING LOWER EMERGENCY EXIT SIGN LENS BROKEN. R & R LENS IAW SIP.
2013
Part: LIGHT — BROKEN (CABIN) · airframe 10,467 hrs · 6,212 cycles
EMERGENCY EXIT LIGHTING ASSEMBLY BROKEN AT MID CABIN. R & R LIGHT ASSEMBLY IAW MM.
Part: LENS — UNSECURE (EXIT SIGN) · airframe 10,274 hrs · 6,099 cycles
R1 DOOR LOWER EMERGENCY EXIT SIGN COVER FELL OFF. R & R LENS IAW MM.
Part: LENS — BROKEN (CABIN) · airframe 9,286 hrs · 5,501 cycles
RT FORWARD EMERGENCY EXIT LIGHT COVER BROKEN. SECURED LENS IAW SIP.
Part: SIGN — BROKEN (CABIN) · airframe 8,967 hrs · 5,309 cycles
L1 DOOR EMERGENCY EXIT SIGN BROKEN. R&R SIGN ASSEMBLY IAW MM.
2012
Part: COVER — LOOSE (CABIN) · airframe 6,891 hrs · 4,025 cycles
ROW 1 EGRESS LIGHTING COVER LOOSE. OK TO CONTINUE MEL 25-10-01 SP1B TR# 78670. INSTALLED EGRESS LIGHT COVER IAW M/M. OPS CHECK NORMAL. CLEARING # 78761
Part: LENS — MISSING (CABIN) · airframe 6,366 hrs · 3,697 cycles
L1 DOOR EEPLS LENS MISSING. INSTALLED LENS PER M/M.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,752 hrs · 2,745 cycles
RED PASSENGER EGRESS LIGHT INOP. RELAMPED PER MM.
Part: LIGHT — MISSING (CABIN) · airframe 3,852 hrs · 2,222 cycles
EEPLS MISSING. INSTALLED EEPLS PER MM.
2011
Part: LIGHT — LOOSE (CABIN) · airframe 3,459 hrs · 1,994 cycles
EEPLS LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.
Part: COVER — LOOSE (CABIN) · airframe 3,400 hrs · 1,961 cycles
FWD ENTRY EEPLS COVER LOOSE. SECURED COVER PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,387 hrs · 1,953 cycles
R2 DOOR EMERGENCY EXIT LIGHT COVER INOP. REMOVED AND REPLACED LIGHT PER MM.
Part: COVER — LOOSE (CABIN) · airframe 2,618 hrs · 1,511 cycles
EEPLS COVER LOOSE AT ROW 1. SECURED COVER PER MM.
Part: SIGN — LOOSE (CABIN) · airframe 456 hrs · 269 cycles
OVERHEAD EMERGENCY EXIT SIGN LOOSE. RE-INSTALLED SIGN PER MM.