N930WN
Registered owner: WILMINGTON TRUST COMPANY TRUSTEE, DE (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 2017-10-02 | 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.
241 reports on file, 2009-05-26 – 2026-06-25.
Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
DELAMINATED LAVATORY A FLOOR PANEL LOWER SURFACE AT FWD GALLEY AREA. REPAIRED LAVATORY A FLOOR PANEL LOWER SURFACE AT FWD GALLEY AREA IAW AMM 25-00-00-300-801.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 55,646 hrs · 33,976 cycles
DELAMINATED LAVATORY A FLOOR PANEL UPPER SURFACE AT FWD GALLEY AREA. EVALUATE DELAMINATED LAVATORY A FLOOR PANEL UPPER SURFACE AT FWD GALLEY AREA AND FOUND WITHIN LIMITS TO REPAIR IAW AMM 25-00-00-300-801, PARAGRAPH 2. DAMAGE SIZE. L: 1.43 IN W:1.24 IN.
Part: TRAY TABLE — BROKEN (ZONE 200) · airframe 55,646 hrs · 33,976 cycles
BROKEN FOOD TRAY PASSENGER SEAT ROWS 2D 2F 3D 3E 3F 4D 5D 5E 5F 6D 6E 7E 8D 8E 8F 9D 9E 9F 15D 15E 15F 16D 16E 16F RH SIDE AT PASSENGER CABIN (24 EA) REPLACED FOODTRAYS IAW CMM- 25-21-42 REV.07 ASSEMBLY STEP 3.Y.(3) PAGE 7014 AND FIGURE 5, PAGE 10102, ITEM 60.
Part: ANGLE — CORRODED (ZONE 200) · airframe 55,646 hrs · 33,976 cycles
CORROSION ON ANGLE UPPER SILL LOCATED BS 827 PLUS 2.5 INCH AT LEVEL S-18R AND WL 200 AFT CARGO BAY. REPLACED ANGLE UPPER SILL AND FASTENERS LOCATED BS 827 PLUS 2.5 INCH AT LEVEL S-18R AND WL 200 AFT CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 146A8310 SHEET 16 REV A.
Part: SEAL BRACKET — CRACKED (ZONE 300) · airframe 55,646 hrs · 33,976 cycles
CRACKED SEAL PLATE, ACCESS PANEL 333AB ON LT HORIZONTAL STAB (2 EA). REPLACED PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CORROSION ON WEB INTERCOSTAL UPPER SILL LOCATED BS 827 PLUS 4 INCH AT LEVEL S-18R AND WL 200 AFT CARGO COMPARTMENT. REPLACED WEB INTERCOSTAL UPPER SILL AND FASTENERS LOCATED BS 827 PLUS 4 INCH AT LEVEL S-18R AND WL 200 AFT CARGO BAY IAW SRM 51-40-02-0G-0, DWG 143A8310 SHEET 16 REV A, & DWG 143A8310 SHEET 15 REV A.
Part: RIB — CRACKED (ZONE 300) · airframe 55,646 hrs · 33,976 cycles
CRACKED RIB, LE STA 105.26 ACCESS PANEL 331B AT LT HORIZONTAL STAB. REPLACED RIB AND FASTENERS LOCATED LE STA 105.26 ACCESS PANEL 331B AT LT HORIZONTAL STAB IAW SRM 51-40-02, DWG 186A1304, SHEET 1, REV A AND DWG 186A1001, SHEET 19, REV-.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CORROSION ON WEB INTERCOSTAL UPPER SILL LOCATED BS 827 PLUS 2.5 INCH AT LEVEL S-18R AND WL 200 AFT CARGO BAY. REPLACED WEB INTERCOSTAL UPPER SILL LOCATED BS 827 PLUS 2.5 INCH AT LEVEL S-18R AND WL 200 AFT CARGO BAY IAW SRM 51-10-02, ITEM 9, AND DWG 146A8310, SHEET 16, REV A, DWG 146A8310, SHEET 15, REV A;
Part: TRAY TABLE — BROKEN (ZONE 200) · airframe 55,646 hrs · 33,976 cycles
BROKEN FOODTRAY PASSENGER SEAT ROW 2B 2C 3B 3C 4A 4B 5A 5B 5C 6B 6C 7C 8A 8B 8C 14B 15A 15B 15C 16A 16B 16C 17A LH SIDE AT PASSENGER CABIN. REPLACED THE FOOD TRAYS IAW CMM 25-21-42 REV. 07 ASSEMBLY STEP 3.Y.(3). PAGE 7014 AND FIGURE 5 PAGE 10102 ITEM 60.
Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 55,646 hrs · 33,976 cycles
ELONGATED HOLE ACCESS PANEL 651CB AT RT WING. REPAIRED ACCESS PANEL 651CB AT RT WING IAW EA-26-157-01738 WIP1 AND EA-26-157-01738.
Part: ANGLE — CRACKED (ZONE 600 FLAP) · airframe 55,646 hrs · 33,976 cycles
CRACKED ANGLE TRAILING EDGE LOCATED IRSS 140 UPPER POSITION AT RT WING. REPLACED ANGLE TRAILING EDGE LOCATED IRSS 140 UPPER POSITION AT RT WING IAW SRM 51-40-02-0G-0 & DWG:115A2000; SHEET 22, REV A. MEASUREMENT OF CRACK IS: 1.495 IN.
Part: FRAME — OUT OF ALIGNMENT (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
DOES NOT MATCH 5311-I-17336-NG WITH FIGURE 15 STEP 20 STA 328 FRAME STRAP CONFIGURATION LOCATED ON S-20R TO S-22R. AS PER EA 26-153-01613; THE CONFIGURATION IS ACCEPTABLE
Part: SUPPORT — CORRODED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CORROSION SUPPORT ZEE RBL 22 BTW BS 727D TO BS 727E WL 156 AFT CARGO BAY. REPLACED SUPPORT ZEE AND FASTENERS LOCATED RBL 22 BTW BS 727 TO BS 767 WL 156 AFT CARGO COMPARTMENT IAW SRM 51-40-02-0G-0 AND DWG 146A7500 SHEE:137; REV:-; DWG 146A7502; SHEET:49;REV:-.
Part: WEB — CORRODED (ZONE 200) · airframe 55,646 hrs · 33,976 cycles
CORROSION SHIELD WEB LOCATED BTW BS 767 TO 794.3, WL 156, RBL 22 IN AFT CARGO BAY. REPLACED NEW SHIELD WEB AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02 ITEM 9, AND DWG 146A0081, SHEET 37, REV-.
Part: WEB — CORRODED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CORROSION ON WEB UPPER SILL DOOR CUT OUT, BS 787 TO 847, STR 18R, WL 200 IN THE AFT CARGO BAY. REPLACED WEB UPPER MAIN SILL AND FASTENERS IAW SRM 51-40-02-0G-0; DWG 146A0080 SHEET 16 REV:A AND DWG 146A8111 SHEET 16 REV-.
Part: RETAINER — CRACKED (ZONE 500) · airframe 55,646 hrs · 33,976 cycles
CRACK RETAINER SEAL ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 472 AT LT WING. INSTALLED SERVICEABLE CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 472 AT LT WING AND FASTENERS IAW B737-700 SRM 51-40-02-0G-0 AND 51-10-02-0G-0 ITEM 9 AND DWG:115A3700 SHEET:51 REV:-.
Part: STRAP — CORRODED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CORROSION LOWER STRAP BTW BS 794.3 TO BS 807 AND RBL 20 CUT OUT DOOR AFT CARGO BAY. REPLACED LOWER STRAP BTW BS 794.3 TO BS 807 AND RBL 20 CUT OUT DOOR AFT CARGO BAY IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0 ITEM 9, AND DWG 146A8340 SHEET:28 REV:-
Part: SUPPORT — CORRODED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CORRODED SUPPORT ANGLE BTW BS 767 - 787, RBL 22, WL 156 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, AND DWG 146A8123, SHEET 16, REV -.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CORRODED SUPPORT ZEE LBL 22 BTW BS 727D TO BS 767, WL 156 IN THE AFT CARGO BAY. REPLACED SUPPORT ZEE IAW SRM 51-10-02 ITEM 9, SRM 51-40-02-0G-0, AND DWG 146A7500, SHEET 85, REV A.
Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACKED SUPPORT ANGLE BTW BS 907 TO BS 927, STR 25R AND STR 27R IN AFT CARGO BAY. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 147A7221, SHEET 24, REV-.
Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACK SUPPORT BRACKET LOCATED BS947.5 AND LBL11 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT BRACKET LOCATED BS947.5 AND LBL11 AT AFT CARGO BAY IAW SRM 51-10-02-0G-0 ITEM 9 AND DWG 149A8103 SHEET 7 REV A.
Part: PLATE — CRACKED (ZONE 500) · airframe 55,646 hrs · 33,976 cycles
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT LT WING IAW SRM 51-10-02-0G-0 STEP 9; SRM 51-42-02-0G-0 AND DWG : 115A2713 SHEET: 5 REV:-.
Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACKED CARGO TRACK RBL 13.84 AND BS 727C AT AFT CARGO BAY. ACCOMPLISHED NDT INSPECTION IAW SRM 53-00-53-2R-3, STEP 4F. STEPS 11 TRHU 14. REPAIRED CARGO TRACK RBL 13.84 AND BS 727B TO 727D AT AFT CARGO BAY IAW SRM 53-00-53-2R-3, REPAIR 3.
Part: PLATE — CRACKED (ZONE 600) · airframe 55,646 hrs · 33,976 cycles
CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 217 AT RT WING IAW SRM 51-10-02-0G-0 ITEM9 AND DWG:115A2713 SHEET:5 REV:-.
Part: FRAME — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACKED FRAME ON BS 947.5 BTW STR 25L TO STR 25R AFT CARGO BAY. REPLACED THE FRAME IAW SRM 51-40-02-0G-0 AND DRAWING 147A0040 SHEET 55 REV B.
Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACKED WEB, INTERCOSTAL BTW BS 400 TO BS 420 AND STR 26L FWD CARGO BAY. REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED BTW BS 400 TO BS 420 AND STR 26L FWD CARGO BAY IAW SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0. I?TEM 9 AND DWG 143A7505, SHEET 81,REV- AND DWG 143A7505,SHEET 82, REV-.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CORROSION SUPPORT ZEE BTW BS 500A TO BS 500D AND RBL 22 WL 156 FWD CARGO BAY. REPLACED THE SUPPORT ZEE BTW BS 500A TO BS 500D AND RBL 22 WL 156 FWD CARGO BAY IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 AND DRAWING 143A7500 REV.-, DRAWING 143A7505, SHEET 81, REV -.
Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACKED FLOOR PANEL 140CF AT AFT CARGO BAY. FABRICATED FLOOR PANEL 140CF IAW SRM 51-40-05, SRM 51-40-08, AND DWG 453A2610, SHEET 9, REV E.
Part: ANGLE — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACKED ANGLE, BS 400 & STR 26L IN FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS BS 400, STR 26L IAW SRM 51-10-02-0G-0, STEP 9, SRM 51-40-02-0G-0, AND DWG 143A7505, SHEET 81, REV -.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 55,646 hrs · 33,976 cycles
DELAMINATED FLOOR PANEL 241AEF AT AFT GALLEY AREA. REPAIRED FLOOR PANEL 241AEF AT AFT GALLEY AREA IAW SRM 53-00-50-2R-7 REPAIR 7 AND SRM 53-00-50-2R-0 REPAIR GENERAL.
Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 55,646 hrs · 33,976 cycles
ELONGATED HOLES ON PLATE ACCESS PANEL 644BB AT RT WING. REPLACED PLATE ON ACCESS PANEL 644BB AT RT WING IAW SRM 51-10-02-0G-0 STEP 9 AND SRM 51-40-02-0G-0.
Part: WEB — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACK ON WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26L AT FWD CARGO BAY. REPLACED WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING# 143A1222 SHEET 58 REV:-.
Part: RIB — CRACKED (ZONE 500 FLAP) · airframe 55,646 hrs · 33,976 cycles
CRACK INDICATION ON LT OTBD AFT FLAP INBD CARTRIDGE RADIUS ZONE.CRACK LENGHT 0.250 IN APPROX. LEFT WING. REPLACED OTBD AFT FLAP INBD CLOSURE RIB LT WING IAW SRM 51-10-02, ITEM 9; FOR CARTRIDGE ASSEMBLY INSTALLATION SEE TTG8Q01BR3XM
Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 55,646 hrs · 33,976 cycles
CRACK INDICATION ON RT OTBD AFT FLAP INBOARD CLOSURE RIB RADIUS ZONE.CRACK LENGHT 0.250 IN APPROX. RIGHT WING. EVALUATED OTBD AFT FLAP INBD CLOSURE RIB (CARTRIDGE) RT WING AND NOT FOUND ALLOWABLE DAMAGE IAW SRM 57-53-02-1A-4 AND REPLACED OTBD AFT FLAP AT RT WING IAW AMM 27-51-26/401, THE INSTALLATION IS DOCUMENTED ON TTG8Q01BR3XM.
Part: ACCESS PANEL — DELAMINATED (ZONE 600) · airframe 55,646 hrs · 33,976 cycles
DELAMINATED ACCESS PANEL 642EB AT RT WING. PERFORMED PERMANENT REPAIR ON ACCESS PANEL 642EB RT WING IAW EA 26-157-01758- WIP 1 AND STEP ARE DOCUMENTED ON FAULT TTG8Q01CZBT5.
Part: FLAP — CRACKED (ZONE 600) · airframe 55,646 hrs · 33,976 cycles
CRACK INDICATION ON RT OTBD AFT FLAP INBD CARTRIDGE RADIUS ZONE. EVALUATED OTBD AFT FLAP INBD CARTRIDGE AND DID NOT FIND ALLOWABLE DAMAGE IAW SRM 57-53-02-1A-4 AND REPLACED OTBD AFT FLAP AT RT WING IAW AMM 27-51-26/401. INSTALLATION IS DOCUMENTED ON TTG8Q01BR3XM.
Part: RAIL — CORRODED (ZONE 500) · airframe 55,646 hrs · 33,976 cycles
CORROSION RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS 449 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS 449 AT LT WING IAW B737-700 SRM 51-10-02-0G-0 STEP 9; SRM 51-40-02-0G AND DWG: 112A4402 SHEET: 13 REV: -.
Part: ANGLE — CRACKED (ZONE 500) · airframe 55,646 hrs · 33,976 cycles
CRACKED ANGLE ON AUXILIARY TRACK LOWER SKIN, SLAT 1, LT WING. REPLACED ANGLE LOCATED AUXILIARY TRACK LOWER SKIN SLAT 1 AT LT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 114A5010 SHEET 2, REV D.
Part: WEB — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACK ON WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 24 AT AFT CARGO BAY. REPLACED ON WEB (SUPPORT) LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 24 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG: 149A8100 SHEET: 1 REV-.
Part: SKIN — CRACKED (ZONE 600) · airframe 55,646 hrs · 33,976 cycles
CORROSION LOWER SKIN INTERNAL CAVITY OF LEADING EDGE AT LEVEL OFSS 575 AT RT WING. REPAIRED RT WING, OUTER WING, LWR SKIN PANEL NR 2, INNER SURFACE, BTW WSTA 537.50 (RIB 18) & WSTA 591.50 (RIB 20) AND FRONT SPAR LEVEL IAW EA 26-157-01701-WIP1, AND EA 26-157-01701.
Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACKED SUPPORT BRACKET, BS 663, LBL 54.21 AT LOWER FUSELAGE. REPLACED SUPPORT BRACKET AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 111A7000, SHT:58, REV-.
Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACK ON CARGO LINER SUPPORT ANGLE LOCATED BS 727B LBL 52 AT AFT CARGO BAY. REPAIRED CARGO LINER ANGLE LOCATED BTW 727B TO 727C LBL 52 AT AFT CARGO BAY LOCATED BETWEEN BS 727A TO BS 727C AT LEVEL LBL 52 IAW SRM 51-70-11-2R-0.
Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 55,646 hrs · 33,976 cycles
CRACKED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN. REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN AND FASTENERS IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 ITEM 9 AND DWG:146A7901 SHEET:66 REV:A
Part: ANGLE — CORRODED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CORROSION ON INNER CHORD LOCATED BTW BS 328 TO BS 344 LBL 57 WL 208.1 AT FWD GALLEY AREA. REPLACED INNER CHORD LOCATED BTW BS 328 TO BS 344 LBL 57 WL 208.1 AT FWD GALLEY AREA IAW SRM 51-40-02-0G-0, AND DWG 141A8310, SHEET 25, REV-.
Part: ANGLE — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACKED ANGLE BTW BS 380 AND BS 400, LBL 13 FLOOR STRUCTURE PASSENGER CABIN. REPLACED ANGLE IAW SRM 51-10-02, ITEM 9, AND DRAWING 143A5400, SHEET 120, REV-, AND DRAWING 143A5400, SHEET 114, REV A.
Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACK ON INTERCOSTAL LOCATED BTW BS 344 TO BS 360 RBL 12 WL 208.1 AT FWD GALLEY AREA. REPLACED INTERCOSTAL LOCATED BTW BS 344 TO BS 360 RBL 12 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING# 141A5400 SHEET 3; REV:-.
Part: TIE CLIP — CRACKED (ZONE 200) · airframe 55,646 hrs · 33,976 cycles
CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA SRM 51-10-02 ITEM 9 AND DRAWING 141A8380 SHEET 21 REV: 21 AND DRAWING# 141A1110 SHEET 39 REV:-.
Part: WEB — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACK ON WEB LOCATED BTW BS 270 TO BS 277 LBL 1 WL 208.1 AT FWD GALLEY AREA . REPLACED WEB LOCATED BTW BS 270 TO BS 277 LBL 1 WL 208.1 AT FWD GALLEY ARE IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 ITEM 9 AND DWG 141A5210 SHEET 19 REV -, DWG 141A5210 REV -.
Part: WEB — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACK ON WEB LOCATED BTW BS 312 TO BS 328 RBL 31 WL 208.1 AT FWD GALLEY AREA. REPLACED WEB AND FASTENERS LOCATED BTW BS 312 TO BS 328 RBL 31 WL 208.1 AT FWD GALLEY AREA IAW SRM 51-40-02-0G-0, AND DWG 141A5400 SHEET 39 REV-.
Part: WEB — CRACKED (ZONE 200) · airframe 55,646 hrs · 33,976 cycles
CRACK ON WEB LOCATED BTW BS 312 TO BS 328 LBL 47 WL 208.1 AT FWD GALLEY AREA. REPLACED WEB (INTERCOSTAL) LOCATED BTW BS 312 TO BS 328 LBL 47 WL 208.1 AT FWD GALLEY AREA IAW SRM 51-10-02 ITEM 9 AND DRAWING 141A5400 SHEET 26 REV:-.
Part: ANGLE — CRACKED (ZONE 200) · airframe 55,646 hrs · 33,976 cycles
CRACKED ANGLE BTW BS 380 AND BS 400, BL 0 FLOOR STRUCTURE PASSENGER CABIN. REPLACED ANGLE AND FASTENERS LOC BTW BS 380 AND BS 400, BL 0 FLOOR STRUCTURE PASSENGER CABIN IAW SRM 51-40-02-0G-0, AND DWG:143A5400, SHEET 120, REV-.
Part: RIB — CRACKED (ZONE 500) · airframe 55,646 hrs · 33,976 cycles
CRACK ANGLE DEFLECTION CONTROL RIB TRAILING EDGE AT LEVEL ORSS 277 LT WING CRACK ANGLE DEFLECTION CONTROL RIB TRAILING EDGE AT LEVEL ORSS 277 LT WING. REPLACED ANGLE (CLIP) LOCATED DEFLECTION CONTROL RIB TRAILING EDGE AT LEVEL ORSS 277 LT WING IAW SRM 51-40-02-0G-0 AND DWG:115A6200; SHEET: 10; REV - .
Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 55,646 hrs · 33,976 cycles
ELONGATED HOLES ACCESS PANEL 661CB AT RT WING. REPAIRED ACCESS PANEL 661CB AT RT WING IAW SRM 51-70-04-2R-9, REPAIR 9.
Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 55,646 hrs · 33,976 cycles
CRACKED SUPPORT ANGLE, BS 695, RBL 24.75 AT PASSENGER CABIN. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND DRAWING 273A9110, SHEET 6, REV A, DWG 111A6000, SHEET 304, REV-.
Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 55,646 hrs · 33,976 cycles
ELONGATED HOLES ON ACCESS PANEL 661AB AT RT WING. REPAIRED ACCESS PANEL 661AB AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 55,646 hrs · 33,976 cycles
CORROSION ON FLOORBEAM LOCATED BS 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA. REPAIRED FLOORBEAM LOCATED BS 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA IAW SRM 53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 55,646 hrs · 33,976 cycles
CORROSION ON FLOOR BEAM LOCATED BS 328 RBL 45.5 WL 208.1 AT FWD GALLEY AREA. REPAIRED FLOORBEAM LOCATED BS 328 WL 208.1 BTW BL 0 TO RBL 60 AT FWD GALLEY AREA IAW SRM 53-10-51-2R-7, REPAIR 7.
Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 55,646 hrs · 33,976 cycles
ELONGATED HOLES ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-9, REPAIR 9.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 55,646 hrs · 33,976 cycles
CORROSION ON FLOORBEAM LOCATED BS 986.5 LBL 42 WL 208.1 AT AFT GALLEY AREA. REPAIRED THE FLOORBEAM LOCATED BS 986.5 LBL 42 WL 208.1 AT AFT GALLEY AREA IAW SRM 53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4.
Part: STIFFENER — CRACKED (ZONE 100) · airframe 55,644 hrs · 33,975 cycles
CRACK ON VERTICAL STIFFENER LOC BS 540 AND LBL 24.97 AT AFT BULKHEAD FWD CARGO COMPARTMENT. REPLACED VERTICAL STIFFENER LOC BS 540 AND LBL 24.97 AT AFT BULKHEAD FWD CARGO BAY IAW SRM 51-10-02, ITEM 9, AND DWG 111A2001, SHEET 114, REV B, DWG 111A2000, SHEET 49, REV - AND DWG 111A2001 SHEET 115 REV A.
Part: LIGHT — DETERIORATED (ZONE 200) · airframe 55,646 hrs · 33,976 cycles
DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN. REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (12 EA) IAW B737-700 SOPM 20-50-12<BR>REV. 58 AND DWG 33500007 REV.2 SHEET 2.
Part: SLIDE — UNPACKED (ZONE 800) · airframe 54,645 hrs · 33,300 cycles
L1 DOOR SLIDE SECONDARY RELEASE FLAP FOLDED UP IN CONTAINER AND NOT SECURED DOWN. UNFOLDED AND SECURED FLAP WHERE IT BELONGS AS DESCRIBED IN MT 725-61-06. CONTAINER NOT OPENED OR REMOVED.
Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 54,589 hrs · 33,258 cycles
PASSENGER CABIN, RIGHT OVERWING UPPER AND LOWER FWD EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY POWER SUPPLY M1669 IAW AMM 33-51-06-960-806.
Earlier reports · 2009–2025 · 178 reports
2025
Part: SIGN — DETACHED (ZONE 200) · airframe 53,935 hrs · 32,812 cycles
EXIT SIGN COVER AT RIGHT OVER WING EXIT FELL OFF. REINSTALLED EMERGENCY EXIT SIGN AT RIGHT OVER WING EXIT IAW AMM 33-51-01.
Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 53,792 hrs · 32,717 cycles
FWD CARGO COMPARTMENT AFT FIBERGLASS FLOOR PANEL HAS 3 SEPARATE CRACKS MEASURING 6.5'; 3.5 '; AND 5' LONG. REMOVED AND REPLACED FWD CARGO COMPARTMENT AFT FIBERGLASS FLOOR PANEL REF AMM 25-52-10 WITH FABRICATED PANEL REF AMM 25-52-01.
Part: COVER — BROKEN (ZONE 200) · airframe 53,760 hrs · 32,697 cycles
FIRST OFFICER`S SIDE OVERWING EXIT LOWER SIGN BROKEN OFF. REMOVED AND REPLACED EXIT ROW LOWER EXIT SIGN RT COVER IAW AMM 33-51-01.
Part: SIGN — BROKEN (ZONE 200) · airframe 53,760 hrs · 32,697 cycles
F/A REPORTED FWD ENTRY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED THE FWD ENTRY DOOR EXIT ASSY SIGN IAW AMM 33-51-01-960.
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 53,528 hrs · 32,536 cycles
SIDEWALL LIGHT AT SEAT ROW 11 ABC IS INOPERATIVE. OK TO CONTINUE PER MEL 33-2-03 SP1B. REPLACED THE LAMP IN SIDEWALL LIGHT AT 11ABC IAW AMM 33-51-04.
Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 52,577 hrs · 31,938 cycles
EMERGENCY LIGHTING BATTERY PACK AT THE R/H OVERWING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 52,577 hrs · 31,938 cycles
L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 52,233 hrs · 31,721 cycles
LOWER EXIT EMERGENCY SIGN @ ROW 11CB HAS 1 BULB INOP.<[01] REMOVED AND REPLACED PER [AMM 33-51-01-960-801-NG (EXIT SIGN - LAMP REPLACEMENT - PERMANENT)]
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 52,233 hrs · 31,721 cycles
LOWER EXIT EMERGENCY SIGN @ ROW 12FED HAS 3 BULB INOP.<[01] REMOVED AND REPLACED PER [AMM 33-51-01-960-801-NG (EXIT SIGN - LAMP REPLACEMENT - PERMANENT)]
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 52,233 hrs · 31,721 cycles
UPPER EXIT EMERGENCY SIGN @ ROW 12FED HAS 3 BULBS INOP.<[01] REMOVED AND REPLACED PER [AMM 33-51-01-960-801-NG (EXIT SIGN - LAMP REPLACEMENT - PERMANENT)]
Part: SLIDE — DISLODGED (ZONE 800) · airframe 51,230 hrs · 31,097 cycles
AIRCRAFT LH AFT ESCAPE SLIDE SLIPPED OUT OF RECEPTACLE<[01] C/W MT 725-66-06 TO REPLACE SLIDE ON AFT ENTRY DOOR.
2024
Part: SCUFF PLATE — CRACKED (ZONE 200) · airframe 51,023 hrs · 30,964 cycles
FOUND FORWARD SERVICE DOOR THRESHOLD PLATE CRACKED<[01] R&R'D FORWARD SERVICE DOOR SCUFF PLATE IAW AMM 53-11-01;[02] VERIFIED: R&R'D FORWARD SERVICE DOOR SCUFF PLATE IAW AMM 53-11-01
Part: FLASHLIGHT — MISSING (ZONE 200) · airframe 50,623 hrs · 30,722 cycles
FWD FLIGHT ATT. FLASHLIGHTS MISSING<[01] REPLACED FWD FLIGHT ATT. FLASHLIGHTS PER AMM 26-64-00. OPS CHECK GOOD. A/C OK FOR SERVICE.
Part: SIGN — MISSING (ZONE 200) · airframe 50,544 hrs · 30,677 cycles
FAS REPORT EXIT SIGN MISSING IN AFT GALLEY FO SIDE<[01] REMOVED AND REPLACED EXIT SIGN ASSEMBLY PER AMM 33-51-01<BR>OP CHK OK
Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 50,251 hrs · 30,483 cycles
R2 DOOR SLIDE HITS DOOR THRESHOLD WHEN DOOR OPERATED.<[01] READJUSTED GIRT Z FOLD AS PER MT 725-61-06 STEP 3.K.(3).;[02] VERIFIED STEP 1
Part: STRIP — LOOSE (ZONE 800) · airframe 50,251 hrs · 30,483 cycles
G2 UPPER INBD CUBBY SLIDE STRIP NOT SECURED TO FLOOR OF COMPARTMENT.<[01] SECURED G2 INBD CUBBY SLIDE STRIP TO FLOOR OF COMPARTMENT AS PER B737 SOPM 20-50-12.;[02] VERIFIED STEP 1
Part: SKIRT — OUT OF ADJUST (ZONE 800) · airframe 50,251 hrs · 30,483 cycles
L2 DOOR SLIDE HITS DOOR THRESHOLD WHEN DOOR OPERATED. REPOSITION L2 DOOR ESCAPE SLIDE SKIRT AS PER WORK INSTRUCTIONS 725-61-06;[02] VERIFIED STEP 1
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
PAX EMERGENCY LIGHTS L1; R2 AND L/H R/D MID CABIN INOP<[01] REPLACED BATTERY PACK AT POSITION M1672 AND M1674 AS PER REF AMM 33-51-06-960-805.<BR>PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST TASK 33-51-00-710-801. TEST PASS.;[02] REPLACED BATTERY PACK AT POSITION M1672 AND M1674 AS PER REF AMM 33-51-06-960-805.<BR>PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST AS PER REF AMM 33-51-00-710-801. TEST PASS.;[03] VERIFIED STEP 2.
Part: SIGN — BROKEN (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
MAIN CABIN AFT LOWERED CELLING PANEL EXIT SING HOUSING BROKEN<[01] REMOVED AND REPLACED MAIN CABIN AFT LOWERED CELLING PANEL EXIT SING HOUSING;<BR>AS PER B737 AMM 33-51-02-020-801 AS FOR REMOVAL REFERENCE AND<BR>33-51-02-400-801 AS FOR INSTALLATION REFERENCE.;[02] VERIFIED STEP 1
Part: STRIP — ELONGATED (ZONE 100) · airframe 50,251 hrs · 30,483 cycles
CAP STRIP WITH ELONGATED HOLE AT STA 847 L/H<[01] RECEIVED NEW CAP STRIP. FOR INSTALLATION REF. TTG8Q00V3GGE;[02] VERIFIED STEP 1
Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 50,251 hrs · 30,483 cycles
PANEL 142KW CRACKED<[01] RECEIVED PANEL 142KW PART;WILL BE INSTALLED ON ITEM TTG8Q00TU02H;[02] VERIFIED STEP 1.
Part: BRACKET — CRACKED (ZONE 800) · airframe 50,251 hrs · 30,483 cycles
L2 DOOR PNL. 834DZ HAS A CRACKED BRACKET<[01] REMOVE AND REPLACED L2 DOOR PANEL 834DZ REF: SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.
Part: FLOOR SUPPORT — ELONGATED (ZONE 100) · airframe 50,251 hrs · 30,483 cycles
AFT CARGO COMP;STA 827-STA 847 LBL 21 WL155.6 INTERCOASTALHAS ELONGATED HOLE<[01] REMOVED AND REPLACED INTERCOASTAL AT AFT CARGO COMP;STA 827-STA 847 LBL 21 WL155.6 REF:SRM 51-40-02-0G-0AND SRM 51-40-05-0G-0;[02] CORRECTION STEP 1 OF STEP 4 REMOVED AND REPLACED INTERCOASTAL AT AFT CARGO COMP;STA 827-STA 847 LBL 21 WL155.6 REF:SRM 51-40-02-0G-0AND SRM 51-40-05-0G-0 AND DRW 146A7502;[03] CORRECTION : STEP 2 ENTER IN ERROR<BR>CORRECT STATEMENT IS: <BR>REMOVED AND REPLACED INTERCOASTAL AT AFT CARGO COMP;STA 827-STA 847 LBL 21 WL155.6 REF:SRM 51-40-02-0G-0AND SRM 51-40-05-0G-0 AND DRW 146A7502;[04] VERIFIED STEP 3.
Part: RIB — CRACKED (ZONE 300) · airframe 50,251 hrs · 30,483 cycles
DORSAL FIM MOST FWD RIB IS CRACKED<[01] REMOVED DAMAGED FWD RIB FROM DORSAL FIN REF. SRM 51-40-02-0G-0.<BR>LOCATED AND DRILLED NEW FWD RIB AT DORSAL FIN REF.SRM 51-40-05-0G-0.<BR>INSTALLED NEW FWD RIB ON DORSAL FIN REF. SRM 51-40-02-0G-0 AND BOEING DRAWING:174A1008.;[02] VERIFIED STEP 1.
Part: PRESSURE DECK — DENTED (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
FOUND 3 EACH ELONGATED HOLES AT FLIGHT DECK FLOOR DENTED (PREVIOUS REPAIR) STA 252 LBL 22.<[01] ACCCOMPLISHED EA 24-153-02293. REF TTG8Q00U7A5.;[02] CORRECTING STEP 1: ACCCOMPLISHED 3 EACH ELONGATED HOLES AT FLIGHT DECK FLOOR REPAIR PER EA 24-153-02293. REF TTG8Q00U7A5.;[03] CORRECTING STEP 2: ACCOMPLISHED EA 24-153-02293. REF FAULT TTG8Q00UZ7A5.;[04] RII -- VERIFIED STEP 3.
Part: PRESSURE DECK — DENTED (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
FOUND 3 EACH ELONGATED HOLES AT FLIGHT DECK FLOOR DENTED (PREVIOUS REPAIR) STA 252 RBL 10.<[01] ACCCOMPLISHED EA 24-153-02293. REF TTG8Q00U7A5.;[02] CORRECTING STEP 1: ACCCOMPLISHED 3 EACH ELONGATED HOLES AT FLIGHT DECK FLOOR REPAIR PER EA 24-153-02293. REF TTG8Q00U7A5.;[03] CORRECTION STEP 1 AND 2. ACCOMPLISHED EA 24-153-02293. REF FAULT TTG8Q00UZ7A5.;[04] RII -- VERIFIED STEP 3.
Part: BEAM — CRACKED (ZONE 100) · airframe 50,251 hrs · 30,483 cycles
CRACK FOUND ON THE 141A6536-14 BEAM IAW B737 NDT P. 6; 51-00-00 PROC. 23. CRACKED IN RADIUS. CRACK FOUND ON THE 141A6536-14 BEAM 4 IAW B737 NDT P. 6 51-00-00 PROC. 23. CRACKED IN RADIUS EO 5241-C-14093 OR 5241-C-14344 WILL BE ADDED TO REPAIR ORDER FOR REPAIR.<[01] SUMMARY :REMOVED BEAM FOUND CRACK P/N 141A6536-14 AND INSTALLED NEW BEAM AS PER RE B/737 SRM 51-40-02-0G-0.AND DWG # 141A06535 AND 141A6516.;[02] RII -- VERIFIED STEP 1.;[03] COMPLETED SME INSPECTION OF WORKMANSHIP AND PAPERWORK AUDIT.;[04] RII -- VERIFIED STEP 1.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
PASSENGER CABIN FLOOR SUPPORT CRACKED B.S. 540 LBL 2' W.L. 208. (DOT 51-015) PASSENGER CABIN FLOOR SUPPORT CRACKED B.S. 540 RBL 2' W.L. 208. (DOT 51-015)<[01] REMOVED FLOOR PANEL 231UF FOR ACCES REF AMM 53-21-00-000-801; REMOVED PASSENGER CABIN FLOOR SUPPORT B.S. 540 RBL 2' W.L. 208. REF SRM 51-40-02-0G-0; CORRCTION STEP 1 OF STEP 3LOCATED AND DRILLED PANEL AND BREAK ASSY FLOOR SUPPORT B.S.540 RBL2' W.L. 208; REF : SRM 51-40-05-0G-0 AND DRW #143A5240;PERFORMED HFEC ROTO INSP ON EXISTING FASTENER OPEN HOLES;<BR>IAW B737 NDT PART 6; 51-00-00 PROC. 16<BR>TOOLS: NORTEC 600; B/C 166317; CAL. DUE: 20-NOV-2024.<BR>NO CRACKS FOUND;OK TO INSTALL PASSENGER CABIN FLOOR SUPPORT B.S. 540 RBL 2' W.L. 208; INSTALLED FLOOR SUPPORT AT PASSENGER CABIN AT B.S 540 RBL 2' W.L 208 AS PER REF: BOEING 737-700 SRM 51-40-02-0G-0 AND DWG # 143A5240;[02] RII -- VERIFIED STEP 1.
Part: CHANNEL — ELONGATED (ZONE 100) · airframe 50,251 hrs · 30,483 cycles
FWD CARGO COMPT L/H Z CHANNEL FASTENER HOLE ELONGATED AT STA 480+6.<[01] REMOVED FWD CARGO COMPARTMENT L/H Z CHANNEL FROM STA 400 TO STA 480+8 PER SRM 51-40-02-0G-0; REMOVED Z CHANNEL SPLICE AT FWD CARGO COMPARTMENT L/H BETWEEN STA 480 AND 500 PER SRM 51-40-02-0G-0; FABRICATED NEW SPLICE PER SRM 53-00-53-2R-5 MATERIAL USED BAC 1496-444 PO:2072494; FABRICATED; LOCATED AND DRILLED Z CHANNEL SECTION L/H FROM STA 396 TO STA 490 PER SRM 51-40-05-0G-0; TREATED AND PRIMED PER SRM 51-20-01-0G-0; INSTALLED SPLICE AND Z CHANNEL PER SRM 53-00-53-2R-5 AND SRM 51-40-02-0G-0; DWG 143A7500.;[02] VERIFIED STEP 1
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
FWD CABIN WET AREA INTERCOSTAL BETWEEN STA 344 AND STA 360 LBL 13 HAS A CRACK AROUND FASTENER HOLE.<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 344 AND STA 360 LBL 13 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A5400;[02] VERIFIED REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 344 AND STA 360 LBL 13
Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 50,251 hrs · 30,483 cycles
FWD CABIN WET AREA INTERCOSTAL BETWEEN STA 344 AND STA 360 BL 0 HAS A CRACK AROUND FASTENER HOLE.<[01] REMOVED AND INSTALLED NEW INTERCOSTAL AT FWD CABIN WET AREA BETWEEN STA 344 AND STA 360 BL 0 AS PER SRM 51-40-02-0G-0 AND DWG#141A5400.;[02] VERIFIED STEP 1
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
PASSENGER CABIN FLOOR SUPPORT CRACKED AT F.S. 540 RBL 25' W.L. 208. (DOT 51-014) PASSENGER CABIN FLOOR SUPPORT CRACKED AT F.S. 540 LBL 25' W.L. 208. (DOT 51-014)<[01] REMOVED FLOOR PANEL 231VF FOR ACESS REF AMM 53-21-00-000-801<BR>LOCATED AND DRILLED MAIN CABIN FLOOR SUPPORT BREAK ASSY AT<BR>FS 540 LBL 25' W.L. 208. REF SRM 51-40-02-0G-0<BR>AND DRW #143A5240<BR>PERFORMED COUNTERSINK INSP AND ROTO INSP. ON EXISTING HOLES IAW B737 NDT P. 6; 53-30-00 PROC. 3. NO CRACKS. EQUIP: NORTEC 600 B/C 166317 CAL DUE: 11/24<BR>LOCATED AND DRILLED AND INSTALLED MAIN CABIN FLOOR SUPPORT BREAK ASSY AT<BR>FS 540 LBL 25' W.L. 208. REF SRM 51-40-05-0G-01<BR>AND DRW #143A5240<BR>INSTALLED FLOOR PANEL 231VF FOR ACESS REF AMM 53-21-00-000-801<BR>TOOL USED I/D: 176021; S/N :15880; DUE :04-DEC-2024;[02] VERIFIED STEP1.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
FWD CABIN WET AREA INTERCOSTAL BETWEEN STA 294.5 AND STA 285.62 BL 0 HAS A CRACK AROUND FASTENER HOLE. FWD CABIN WET AREA INTERCOSTAL BETWEEN STA 294.5 AND STA 277 BL 0 HAS A CRACK AROUND FASTENER HOLE.<[01] REMOVED AND INSTALLED NEW INTERCOSTAL AT FWD CABIN WET AREA BETWEEN STA 294.5 AND STA 277 BL 0 AS PER AS PER SRM-51-40-02-0G-0 AND DWG#141A5400;[02] VERIFIED STEP 1
Part: STRINGER — CRACKED (ZONE 100) · airframe 50,251 hrs · 30,483 cycles
CRACK FOUND AT STA 294.5 +4 AT S-15L WL 230 LBL 64. CRACK FOUND AT STA 294.5 +4 AT S-14L WL 230 LBL 64<[01] REPAIR WAS ACCOMPLISHED PER EA 24-153-02286 AT STA 294.5 +4 AT S-15L WL 230 LBL 64;[02] CORRECTED STEP 1. REPAIR WAS ACCOMPLISHED PER EA 24-153-02286 AT STA 294.5 +4 AT S-14L WL 230 LBL 64;[03] RII -- VERIFIED STEP 2.
Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 50,251 hrs · 30,483 cycles
CRACK FOUND ON THE 141A6536-15 BEAM IAW B737 NDT P. 6; 51-00-00 PROC. 23. CRACKED IN RADIUS. CRACK FOUND ON THE 141A6536-15 BEAM 5 IAW B737 NDT P. 6 51-00-00 PROC. 23. CRACKED IN RADIUS. EO 5241-C-14093 OR 5241-C-14344 WILL BE ADDED TO REPAIR ORDER FOR REPAIR.<[01] REMOVED BEAM #5 FOR DAMAGE AT R1 DOOR IN REF B 737-700 SRM 51-40-02-0G-0. INSTALLED NEW BEAM #5 AT R1 DOOR IN REF B 737-700 SRM 51-40-02-0G-0 AND DWG # 141A6535; 141A6516;[02] RII -- VERIFIED STEP 1.
Part: CUSP WEB — CRACKED (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
CABIN RT SIDE CUSP WEB BETWEEN ST 420 AND 440 WL 208.1 CRACKED AS MARKED. 124-001<[01] REMOVED ; FABRICATED AND INSTALLED RT SIDE CUSP WEB BETWEEN STA 420 TO STA 440 PER 51-40-02-0G-0 AND DWG: 143A5913;[02] VERIFIED STEP 1
Part: SKIN — CRACKED (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
STA 312 L/H SIDE HAS A CRACK JUST ON TOP OF L-1 DOOR CUTOUT.<[01] THIS TASK CARD WAS ACCOMPLISHED ON EA NO:M-22-153-01244;[02] CORRECTION TO STEP 1: WORK WAS ACCOMPLISHED ON TASK CARD TTG8Q00V38DR; EA NO:M-22-153-01244.;[03] VERIFIED STEP 2
Part: CUSP WEB — PULLED (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
CABIN RT SIDE CUSP WEB BETWEEN ST 420 AND 440 WL 208.1 - STAND-OFF HAS A PULLED RIVET AS MARKED. 124-002<[01] REPLACEMENT OF CABIN RT SIDE WEB BETWEEN ST 420 AND 440 WL 208.1 WILL BE ACCOMPLISHED ON TTG8Q00V1YXU.;[02] VERIFIED STEP 1
Part: STIFFENER — CRACKED (ZONE 300) · airframe 50,251 hrs · 30,483 cycles
RH HORIZONTAL STABILIZER RIB #3 STIFFENER 3 CRACK.<[01] REMOVED DAMAGED AND INSTALLED NEW REPAIR KIT AT RH HORIZONTAL STABILIZER RIB #3; AND STIFFENER #3 PER SRM 55-10-09-2R-4 REPAIR 4 AND DWG 55100003;[02] STEP 1 ENTERED IN ERROR;[03] REMOVED DAMAGE AND INSTALLED NEW REPAIR KIT AT HORIZONTAL STABILIZER RIB#3; STIFFENER #3 PER SRM 55-10-09-2R-4 REPAIR 4 AND DWG= 55100003;[04] VERIFIED STEP 3
Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
FWD WET AREA FLOOR PANEL 221BF HAS INSERTS WITH CORROSION.<[01] FAULT RESOLVED ON OTHER FAULT. PANEL WILL BE REPLACED . REF. TTG8Q00V0RKR;[02] CORRECTION: FAULT RESOLVED ON OTHER FAULT. PANEL WILL BE REPLACED REF. TTG8Q00V0RL0;[03] VERIFIED T/C: ON TTG8Q00V0RL0
Part: FITTING — CORRODED (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
FLOOR STRUCTURE AFT O/B FITTING OF LAV A HAS CORROSION EDIT FAULT DESCRIPTION: L-1 DOOR FWD GIRT BAR FITTING HAS CORROSION<[01] REMOVED AND REPLACED L-1 DOOR FWD GIRT BAR FITTING PER SRM 51-40-02-0G-0.;[02] VERIFIED REPLACEMENT
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 50,251 hrs · 30,483 cycles
FWD WET AREA FLOOR PANEL 221BF AFT O/B CORNER IS CRACKED<[01] RECEIVED NEW FLOORPANEL #141A5810-729 (221BF) WILL BE INSTALLED ON TTG8Q00U3WRV.;[02] VERIFIED STEP 1
Part: PANEL — CORRODED (ZONE 100) · airframe 50,251 hrs · 30,483 cycles
P15 REFUEL PANEL FACEPLATE HAS MULTIPLE CORROSION SPOTS<[01] REMOVED AND REPLACED P15 REFUEL PANEL FACE PLATE I/A/W BOEING AMM 28-21-00-000-801 & 28-21-00-400-801; OPS CHECK FOUND NORMAL;[02] VERIFIED STEP 1
Part: ACCESS DOOR — CORRODED (ZONE 800) · airframe 50,251 hrs · 30,483 cycles
CORROSION FOUND ACCESS DOOR 311BL FWD EDGE HAS EVIDENCE OF CORROSION.<[01] REMOVED AND REPLACED ACCESS DOOR 311BL AS PER AMM 52-49-11-000-802 AND AMM 52-49-11-400-802.;[02] VERIFIED STEP 1
2023
Part: PANEL — ELONGATED (ZN 100 FUS LOWER) · airframe 46,199 hrs · 27,916 cycles
PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES AND COUNTERSINKS.<[01] REMOVED AND REPLACED PANEL PER SRM 51-40-02.
Part: COVER — CRACKED (ZN 800 DOOR) · airframe 46,199 hrs · 27,916 cycles
FWD GALLEY SERVICE DOOR HANDLE COVER CRACKED<[01] R&R FWD GALLEY SERVICE DOOR HANDLE COVER PER SIP.
Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 45,930 hrs · 27,739 cycles
CAPT SIDE EMER. EXIT SIDE WALL LIGHT INOP ( WINDOW)<[01] AC OK TO CONTINUE PER MEL 33-2-03 SP1B AUTH#128268;[02] RELAMPED EMERGENCY. EXIT SIDEWALL LIGHT PER AMM 33-51-01
2022
Part: GIRT BAR — OUT OF ADJUST (ZN 900 LAV/GALLE) · airframe 44,850 hrs · 27,043 cycles
CREW REPORTS FWD ENTRY GIRT BAR HARD TO ENGAGE / [01] REMOVED DEBRIS FROM GIRT BAR LATCHES PER SIP
Part: LIGHT — MISSING (PAX CABIN) · airframe 44,063 hrs · 26,516 cycles
R/H OVERWING EXIT LENS MISSING / [01] REPLACED THE MISSING OVERWING EXIT LENS REF AMM 33-51-01;[02] CREATED IN ERROR. FAULT FOR A/C 730 REF BARCODE TTG8Q00E9GBE
Part: COUNTERWEIGHT — CORRODED (RUDDER) · airframe 44,026 hrs · 26,491 cycles
RUDDER COUNTER BALANCE WEIGHT RH SIDE FWD CORNER; SPOT OF CORROSION. REMOVED RUDDER COUNTER BALANCE WEIGHT AT BALANCE ARM IAW CMM 55-40-09. INSPECTED AREA OF INSTALLATION, BOLTS & NEW BALANCE WEIGHT. INSTALLED NEW BALANCED WEIGHT IAW CMM 55-40-09, FOUND WEIGHT BALANCE WITHIN LIMITS IAW SRM: 55-40-02-1A-3.
Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 44,026 hrs · 26,491 cycles
AFT CARGO DOOR FWD CORNER SCUFF PLATE CRACK. ACCOMPLISH AFT CARGO DOOR FWD CORNER SCUFF PLATE WELD REPAIR IAW SRM 53-60-15-2R-1.
Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 44,026 hrs · 26,491 cycles
AFT CARGO COMP. AFT CORNER SCUFF PLATE WITH EVIDENCE OF CRACK AT FWD END. / [01] PERFORMED HFEC INSP ON AFT CARGO SCUFF PLATE; IAW B 737 NDT PART 6 51-00-00 PROCE 23. TOOL NORTEC 600. BC 166316. CALIB DUE 10-8-22. CRACK INDICATION ON FWD END.;[02] ACCOMPLISHED WELDING REPAIR BY OUTSIDE VENDOR WITH P.O NO.413588 AT AFT CARGO COMP. AFT CORNER SCUFF PLATE FWD END PER B737-700 SRM 53-60-15-2R-1 STEP B (4) PAGE. #2;[03] VERIFIED STEP #2 CERTIFICATION; OK.;[04] FWD CARGO COMP. SCUFF PLATES WAS REMOVED AND WILL BE INSTALL ON FWD CARGO MOC #TTG8Q004BG3S STEP 5 AND 55;[05] VERIFIED STEP #4 TTG8Q004BG3S
Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 44,026 hrs · 26,491 cycles
L/H EXTERIOR EMERGENCY OVERWING LIGHT INOP. / [01] REMOVED AND REPLACED LAMP AT L/H EXTERIOR EMERGENCY OVERWING LT AND PERFORMED OPS TEST FOUND NORMAL AS PER REF B737-AMM-33-51-04-960-801;[02] VERIFIED STEP 1
Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 44,026 hrs · 26,491 cycles
EMERGENCY BATTERY PACK AT POSITION M1673 AND M1668 FAILED OPS TEST. / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT POSITION M1668 REF B737 AMM 33-51-06-960-805;[02] VERIFIED STEP 1;[03] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT POSITION M1673 REF B737 AMM 33-51-06-960-805;[04] EMERGENCY LIGHTING SYSTEM OPS CHECKED NORMAL REF B737 AMM 33-51-06-960-805;[05] VERIFIED 3; 4
Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 44,026 hrs · 26,491 cycles
EMERGENCY BATTERY PACK AT POSITION M1673 AND M1668 FAILED OPS TEST. / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT POSITION M1668 REF B737 AMM 33-51-06-960-805;[02] VERIFIED STEP 1;[03] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT POSITION M1673 REF B737 AMM 33-51-06-960-805;[04] EMERGENCY LIGHTING SYSTEM OPS CHECKED NORMAL REF B737 AMM 33-51-06-960-805;[05] VERIFIED 3; 4
Part: STRAP — CORRODED (AFT CARGO) · airframe 44,026 hrs · 26,491 cycles
CORROSION FOUND AFT CARGO DOOR CUTOUT LOWER SILL STRAP AT STA 787 +16 RBL 20 W.L. 155.5 / [01] REMOVED CORROSION AT AFT CARGO DOOR CUTOUT LOWER SILL STRAP STA 787+16 RBL 20 WL 155.5 AS PER REF B737-700 SRM 51-10-02-0G-0;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THK. NOTED 0.050'<BR>TOOL USED : OLYMPUS 27MG B/C 172139 04/22;[04] EVALUATED REWORKED AREA. ORIGINAL THICKNESS 0.100'; MATERIAL LOST 0.050'; MATERIAL REMAINING 0.050'. FOUND OUT OF LIMITS AS PER REF B737-700 SRM 53-60-15-1A-1;[05] REMOVED AFT CARGO DOOR CUTOUT LOWER SILL STRAP STA 787+16 RBL 20 WL 155.5 AS PER REF B737-700 SRM 51-40-02-0G-0;[06] LOCATED AND DRILLED NEW AFT CARGO DOOR CUTOUT LOWER SILL STRAP AS PER REFERENCE B737-700 SRM 51-40-05-0G-0.;[07] VERIFIED STEPS 4; 5 AND 6. OK TO INSTALL NEW STRAP.;[08] STARTED INSTALLATION OF THE NEW AFT CARGO DOOR CUTOUT LOWER SILL STRAP AS PER REFERENCE B737-700 SRM 51-40-02-0G-0 AND DWG #146A8120.;[09] INSTALLED NEW AFT CARGO DOOR CUTOUT LOWER SILL STRAP AS PER REFERENCE B737-700 SRM 51-40-02-0G-0 AND DWG #146A8120.;[10] VERIFIED STEPS 8 AND 9.
Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 44,026 hrs · 26,491 cycles
CORROSION FOUND AT AFT CARGO FLOOR STRIP AT STA 767 +5 BETWEEN RBL 21 AND LBL 21 W.L. 155.5 AROUND FASTENER HOLES. / [01] FOUND EXFOLIATION AT AFT CARGO FLOOR STRIP AROUND THE FASTENERS OUT OF LIMITS AS PER REF B737-700 SRM 53-00-53-1A-2;[02] RECEIVED AND VERIFIED NEW FLOORBOARD SPLICE P/N 146A9401-4 AS PER REFERENCE B737-700 SRM 53-60-53-0L-2 AND DWG #146A9401.<BR>FLOORBOARD SPLICE WILL BE INSTALL IN TASK CARD # TTG8Q004BZAN.;[03] VERIFIED STEP#2 ABOVE.
Part: BARRIER — CRACKED (CENTER WING) · airframe 44,026 hrs · 26,491 cycles
RH STA 663 VAPOR BARRIER CRACKED AT RBL 25. / [01] MEASUREMENTS;[02] CLEANED R/H VAPOR BARRIER ;PREPARED DAMAGE AREA FOR REPAIR; STOP DRILL ALL CRACKS AS PER B737 SRM 51-70-04-2R-10;[03] PERFORMED DRY OUT ON VAPOR BARRIER; FOUND NO WATER AS PER B737 SRM 51-70-04-2R-10;[04] VERIFIED STEPS 1 ;2 & 3 AND OK TO INSTALL REPAIR;[05] REPAIRED CRACK DAMAGE ON R/H VAPOR BARRIER WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-10;[06] PERFORMED TAP TEST ON REPAIRED AREA ;FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION 5;[07] VERIFIED STEPS #5 AND #6.;[08] OK TO APPLY PRIMER AND TOP COAT.;[09] APPLIED TREAT AND PRIMER AT VAPOR BARRIER REPAIR AS PER REF B737-700 AMM 51-21-73-370-803;[10] APPLIED TOP COAT AT VAPOR BARRIER REPAIR AS PER REF B737-700 AMM 51-21-73-370-803;[11] VERIFIED STEPS 9 AND 10.
Part: WEB — CRACKED (L/H WING) · airframe 44,026 hrs · 26,491 cycles
WEB LOCATED AND ATTACHED TO INBOARD SIDE LEFT DEFLECTION CONTROL RIB SUPPORT BEAM IS CRACKED / [01] REMOVE L/H DEFLECTION CONTROL RIB SUPPORT BEAM REF SRM 51-40-02;[02] CORRECTION OF STEP 1. REMOVE WEB FROM L/H DEFLECTION CONTROL RIB SUPPORT BEAM REF SRM 51-40-02;[03] VERIFIED STEP #2.;[04] OK TO INSTALL NEW WEB ANGLE.;[05] INSTALLED NEW ANGLE TO L/H DEFLECTION CONTROL RIB SUPPORT BEAM; REF SRM<BR>51-40-02;[06] CERTIFIED;[07] VERIFIED ALL STEPS
Part: FLAP SYSTEM — FAILED · airframe 43,392 hrs · 26,041 cycles
FLAPS WOULD NOT EXTEND BEYOND 2. USED ALT FLAP EXTENSION TO EXTEND TO 15 / [01] C/W FIM 27-51 TASK 813; FLAPS OP'S NORMAL; NO DEFECTS NOTED. INSPECTED FLAPS NO DEFECTS NOTED. FURTHER TROUBLESHOOT REQUESTED BY MX CONT.;[02] R+R L/H FLAP POSITION TRANSMITTER REF AMM 27-58-01 OPS GOOD
Part: BALLAST — INOPERATIVE (L/H DOOR) · airframe 42,810 hrs · 25,671 cycles
SIDEWALL LIGHT ON L/H EMERGENCY EXIT DOOR INOP. / [01] REPLACED BALLAST L/H EMERGENCY EXIT REF. AMM 33-21-00.
Part: HANDLE — BROKEN (L1 DOOR) · airframe 42,508 hrs · 25,486 cycles
L1 DOOR PLASTIC ASSIST HANDLE BROKEN ; / [01] ROBBED HANDLE FROM FWD AND INSTALLED ON L1 DOOR IAW AMM 52-11-31
Part: PANEL — CRACKED · airframe 42,323 hrs · 25,378 cycles
193D PN TRAILING EDGE HAS 6 DIMPLED; CRACKED AND OVERSIZED FASTENER HOLES. ; / [01] REMOVED AND PLACED PANEL PER AMM 53-51-21
2021
Part: LINE — LEAKING (HYD SYSTEM) · airframe 40,839 hrs · 24,488 cycles
AT BEGINNING OF DSECENT; NO 2 ENGINE HYDRAULIC PUMP PRESSURE FLICKERED; THEN EVENTUALLY CAME ON STEADY. HYDRAULIC B-SYSTEM QTY WAS 0. DID QRH PROCEDURE TO SECURE ENG DRIVEN PUMP; THEN ELECTRIC PUMP ; LOW PRESSURE LIGHT ILLUMINATED. RAN QRH FOR B-SYSTEM HYDRAULIC SYSTEM FAILURE. / [01] PERFORMED EXTERNAL LEAK CHECK REF AMM 29-00-00-790-801.FOUND HYDRAULIC B PRESS RUDDER TUBE LINE LEAKING.INSPECTED CASE DRAIN FILTERS; NO CONTAMINATION NOTED; REPLACED BOTH FILTERS AS PER REF AMM 29-11-51.INSTALLED TEMP LINE HYDRAULIC B RUDDER PRESS TUBE REF. MPM 53.05.08.02 & REF AMM 20-10-52.SERVICED SYSTEM B HYDRAULICS AS PER REF AMM 12-12-00.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,170 hrs · 24,110 cycles
FORWARD SERVICE DOOR OUTSIDE EMERGENCY LIGHT INOP ; / RELAMPED IAW AMM 33-51-04
Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 39,736 hrs · 23,877 cycles
AFT GALLEY EXIT LIGHT COVER OFF / RESECURED AFT GALLEY EXIT LIGHT COVER AT R2 DOOR PER S.I.P.
2020
Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 38,982 hrs · 23,431 cycles
FWD SERVICE DOOR FLOOR EXIT SIGN COVER MISSING. REPLACED FWD SERVICE DOOR FLOOR EXIT SIGN COVER, PER SIP.
Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 38,910 hrs · 23,386 cycles
RT OVERWING EMERGENCY EXIT BATTERY FAILED CHECK. REMOVED AND REPLACED, PER AMM 33-51-06.
Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 38,910 hrs · 23,386 cycles
AFT GALLEY LT BATTERY FAILED CHECK. REMOVED AND REPLACED, PER AMM.33-51-06.
Part: ANGLE — CRACKED (BS 867 S26-27L) · airframe 38,883 hrs · 23,372 cycles
CRACK ANGLE - SUPPORT LOCATED BS 867 AT LEVEL FLOOR STRUCTURE BETWEEN STR 26L TO STR27L AFT CARGO COMPARTMENT (1 EA) / REPLACED ANGLE SUPPORT LOCATED BS 867 AT LEVEL FLOOR STRUCTURE BTW STR R26L TO 27L AFT CARGO COMPARTMENT IAW 737-700 SRM 51-40-02 DWG 149A8103 SHEET 1 REV D. SRM B737-700 51-10-02 ITEM 9
Part: SUPPORT — CRACKED (BS 540 S24R) · airframe 38,883 hrs · 23,372 cycles
CRACK SUPPORT STRUCTURE WING TO BODY FAIRING AT LEVEL BS 540 STR 24R AT LOWER FUSELAGE / REPLACED BRACKET ON SUPPORT STRUCTURE WING TO BODY FAIRING AT LEVEL BS 540 STR 24R AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A0060 REV.A
Part: SUPPORT — CORRODED (BS 794-847) · airframe 38,883 hrs · 23,372 cycles
CORROSION LOWER SILL LOCATED BETWEEN BS 794 TO BS 847; RBL 25 AT LEVEL FLOOR STRUCTURE WL 154 APPROX. AFT CARGO COMPARTMENT / REPLACED LOWER SILL LOCATED BETWEEN BS 794 TO BS 847; RBL 25 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG #146A8340 REV-
Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 38,883 hrs · 23,372 cycles
CRACK INTERCOSTAL, WEB FLOOR STRUCTURE LOCATED BETWEEN BS 344 TO BS 360 AT BL 0 AT PASSENGER CABIN. REPLACED INTERCOSTAL WEB, FLOOR STRUCTURE LOCATED BETWEEN BS 344 TO BS 360 AT BL 0 AT PASSENGER CABIN, IAW B737-700 SRM 51-10-02 STEP 9 AND DRAWING 141A5400 REV.
Part: CARGO TRACK — CRACKED (BS 727E-767) · airframe 38,883 hrs · 23,372 cycles
CRACK TRACK RBBL 13.84 LOCATED BETWEEN BS 727E TO BS 767 AT AFT CARGO COMPARTMENT (3 EA). REPAIRED TRACK LOCATED BETWEEN BS 727D AND BS 787 TO RBL 13.84 AT AFT CARGO COMPARTMENT, IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3.
Part: FLOOR SUPPORT — CORRODED (BS 967-1006) · airframe 38,883 hrs · 23,372 cycles
CORROSION FLOOR STRUCTURE INNER CHORD LOCATED BETWEEN BS 967 TO BS 1006 AT LEVEL STR 17R AND RBL 51 AFT GALLEY AND LAV AND WL 208.1. REPLACED INNER CHORD FLOOR STRUCTURE LOCATED BETWEEN BS 907 TO BS 1006 AT LEVEL STR 17R AND RBL 51 AND WL 208.1 AFT GALLEY, IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 147A8501 REV B.
Part: SUPPORT PLATE — CRACKED (BS 540) · airframe 38,883 hrs · 23,372 cycles
CRACK FLOOR STRUCTURE SUPPORT PLATE BS540 BETWEEN RBL 24 TO RBL45 AT PASSENGER CABIN (1 EA) / REPLACED FLOOR STRUCTURE SUPPORT PLATE BS 540 BETWEEN RBL 24 TO RBL 45 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02
Part: CHANNEL — CORRODED (BS 767-787) · airframe 38,883 hrs · 23,372 cycles
CORROSION CHANNEL SUPPORT BETWEEN BS 767 TO BS 787 AT LEVEL FLOOR STRUCTURE RBL 22 AND WL 155.5 APPROX. AFT CARGO COMPARTMENT / REPLACED CHANNEL SUPPORT BTW BS 767 TO BS 787 AT LEVEL FLOOR STRUCTURE RBL 22 AND WL 154 APPROX. AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG:146A0081 REV A
Part: SUPPORT PLATE — CRACKED (BS 540) · airframe 38,883 hrs · 23,372 cycles
CRACK FLOOR STRUCTURE SUPPORT PLATE BS540 BETWEEN BL0 TO LBL24 AT PASSENGER CABIN (1 EA) / REPLACED FLOOR STRUCTURE SUPPORT PLATE BS 540 BETWEEN BL0 TO LBL24 PASSENGER CABIN IAW B737-700 SRM 51-40-02
Part: SUPPORT — CORRODED (BS 500A) · airframe 38,883 hrs · 23,372 cycles
CORROSION BILGE AREA AT SUPPORT ZEE LOCATED BS 500A AT LEVEL STR 26L AND WL 156.5 AT FWD CARGO COMPARTMENT. REPAIRED SUPPORT ZEE BILGE AREA LOCATED BS 500A AT LEVEL STR 26L AND WL 156.5 AT FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DWG 143A7501 REV B.
Part: CHANNEL — CORRODED (FWD CARGO) · airframe 38,883 hrs · 23,372 cycles
CORROSION CHANNEL SIDEPLATE LOCATED BS500 TO BS500A AT LEVEL STR26R AND WL156.5 FWD CARGO COMPARTMENT / REPLACED CHANNEL SIDEPLATE LOCATED BS 500 TO BS 500A AT LEVEL STR 26R FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG # 143A0080 REV-
Part: ANGLE — GOUGED (BS 1006-1016) · airframe 38,883 hrs · 23,372 cycles
GOUGE CLOSURE ANGLE FWD POSITION LOCATED BETWEEN BS 1006 TO BS 1016 LT SIDE AT UPPER FUSELAGE (1 EA). REPLACED CLOSURE ANGLE FWD POSITION LOCATED BETWEEN BS 1006 TO BS 1016 LT SIDE AT UPPER FUSELAGE, IAW B737-700 SRM 51-40-02 DRAWING 147A0030 REV B.
Part: ANGLE — GOUGED (BS 1006-1016) · airframe 38,883 hrs · 23,372 cycles
GOUGE CLOSURE ANGLE FWD POSITION LOCATED BETWEEN BS 1006 TO BS 1016 RT SIDE AT UPPER FUSELAGE (1 EA). REPLACED CLOSURE ANGLE FWD POSITION LOCATED BETWEEN BS 1006 TO BS 1016 RT SIDE UPPER FUSELAGE, IAW B737-700 SRM 51-40-02 AND DRAWING 147A0030 REV B.
Part: INTERCOSTAL — CRACKED (BS 294-303) · airframe 38,883 hrs · 23,372 cycles
CRACK WEB INTERCOSTAL BETWEEN BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA. REPLACED WEB INTERCOSTAL BETWEEN BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA, IAW B737-700 SRM 51-10-02 ITEM 9 B737-700 SRM 1-40-02 AND DRAWING 141A8180 REV C.
Part: TIE — CRACKED (BS 277) · airframe 38,883 hrs · 23,372 cycles
CRACK TIE CLIP AT LEVEL BS 277 ON STR 10R AT PASSENGER CABIN. REPLACED TIE CLIP AT LEVEL BS 277 ON STR 10R AT PASSENGER CABIN, IAW B737-700 SRM 51-10-02 STEP 9 AND DRAWING 141A1110 REV.
Part: STRINGER — CRACKED (BS 540) · airframe 38,883 hrs · 23,372 cycles
CRACK STRINGER 26R AT BS 540 AT FWD CARGO COMPARTMENT. REPAIRED STRINGER 26R AT BS 540 AT FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.
Part: STRINGER — CRACKED (BS 540) · airframe 38,883 hrs · 23,372 cycles
CRACK STRINGER 24R AT BS540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 24R LOCATED BETWEEN BS 500D TO BS 540 FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03- 2R-1 REPAIR 1.
Part: STRINGER — CRACKED (BS 540) · airframe 38,883 hrs · 23,372 cycles
CRACK STRINGER 25R AT BS 540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 25R LOCATED BETWEEN BS 500C TO BS 540 FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.
Part: VISOR — BROKEN (R1 DOOR) · airframe 38,883 hrs · 23,372 cycles
BROKEN ESCAPE SLIDE VISOR SERVICE DOOR AT FWD GALLEY AND LAVATORY. REPLACED VISOR ON ESCAPE SLIDE COVER SERVICE DOOR AT FWD GALLEY, IAW BOEING 737-700 DRAWING 416A2204 REV R.
Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 40,149 hrs · 24,097 cycles
CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT / REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1; BHC 5975.
Part: SUPPORT — CRACKED (BS 727) · airframe 38,883 hrs · 23,372 cycles
CRACK CHANNEL SUPPORT AFT SIDE OF STA 727 BULKHEAD AFT CARGO COMPARTMENT (1 EA) / REPLACED CHANNEL SUPPORT AFT SIDE OF STA 727 BULKHEAD AFT CARGO COMPARTMENT (1EA) I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 144A2600 REV. A
Part: FITTING — DETERIORATED (R2 GIRT BAR) · airframe 38,884 hrs · 23,372 cycles
DETERIORATED FLOOR MAT GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA. REPLACED FLOOR MAT GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA, IAW B737-700 AMM 25-66-02-400-801 STEP 3.D(I).
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 38,883 hrs · 23,372 cycles
DENT INBOARD MAIN FLAP LOWER SURFACE LOC AT 3.75 IN FROM TRAILING EDGE AND 4.25 IN FROM OUTBOARD EDGE AT RT WING. PERFORMED PERMANENT REPAIR ON INBOARD MAIN FLAP WEDGE PANEL AT RT WING AND IS DOCUMENTED ON DEFECT NO L177042.
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 38,883 hrs · 23,372 cycles
DENT INBOARD MAIN FLAP UPPER SURFACE LOC AT 2.5 IN FROM TRAILING EDGE AND 43.5 IN FROM OUTBOARD EDGE AT RT WING. PERFORMED PERMANENT REPAIR ON INBOARD MAIN FLAP WEDGE PANEL AT RT WING AND IS DOCUMENTED ON DEFECT NO L177042.
Part: GUSSET — CRACKED (BS 500D S19R) · airframe 38,883 hrs · 23,372 cycles
CRACK GUSSET BS 500D AT LEVEL STR 19 R FWD CARGO COMPARTMENT (1 EA) / REPLACED GUSSET BS 500D AT LEVEL STR 19R FWD CARGO COMPARTMENT (1EA) I.A.W B737-700 SRM 51-10-02-OG-0 ITEM 9 AND DWG 143A7902 REV-.
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 38,883 hrs · 23,372 cycles
SEVERAL DENTS ON INBOARD MAIN FLAP LOWER SURFACE LOCATED AT 4.5IN FROM TRAILING EDGE AND 6.25 IN FROM OUTBOARD EDGE WEDGE PANEL AT RT WING. PERFORMED PERMANENT REPAIR ON INBOARD MAIN FLAP WEDGE PANEL AT RT WING, AS PER B737-700 SRM 57-53-01-2R-7 REP 7. TOOL USED CALIPER P/N 500-197-30 S/N 15272055 DUE DATE 04AUG21; HOTBONDER P/N HCS9200B S/N 13061394 DUE DATE 09JUL21; NDT TOOL P/N 5-3 S/N 064 DUE DATE 08JUN21.
Part: GUSSET — CRACKED (BS 500D S19L) · airframe 38,883 hrs · 23,372 cycles
CRACK GUSSET BS500D AT LEVEL STR 19 L FWD CARGO COMPARTMENT (1 EA) / REPLACED NEW GUSSET LOC BS 500D AT LEVEL STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 STEP 9 AND DRAWING # 143A7902 REV -.
Part: LIGHT — DETERIORATED (CABIN) · airframe 38,883 hrs · 23,372 cycles
DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (8EA). REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN(8EA) AND STEPS ARE DOCUMENTED ON SWA CARD 733-080-00-01.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,238 hrs · 22,952 cycles
ROW 3 DEF;6DEF;9ABC AND 12ABC AISLE EMERGENCY LIGHTS INOP. / R&R POWER SUPPLY BATTERY PACKS AT STA322 AND STA 727 + 13 AND OPS CHECK GOOD PER AMM 33-51-06
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,238 hrs · 22,952 cycles
ROW 16 DEF AND 19DEF AISLE EMERGENCY LIGHTS INOP. / R7R BATTERY PACK FOR EMERGENCY LIGHTS AT APROX. PAX ROW 16 & 19DEF I/A/W AMM 33-21-06. OPS CHECK NORMAL
Part: CONTROL PANEL — FAULTY (CARGO BAY) · airframe 38,235 hrs · 22,951 cycles
CARGO FIRE DISCHARGE L7 CAME ON IN CRUISE / R/R CARGO FIRE CONTROL PANEL AS PER REF AMM 26-00-02 RAR# 54790 P/N OFF/ON 47355-1 S/N OFF 4499 S/N ON 1664
Part: WARNING LIGHT — FALSE ACTIVATION (COCKPIT) · airframe 38,007 hrs · 22,806 cycles
CARGO FIRE DISCHARGE LIGHT ILL INFLIGHT WITH NO FIRE INDICATIONS. FLIGHT CREW REPORTS LIGHT WENT OUT DURING FLIGHT. PERFORMED CARGO FIRE OPERATIONAL TEST IAW AMM 26-16-00 OPS TEST GOODD NO HISTORY WITHIN 30 DAYS
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,515 hrs · 22,470 cycles
L1 DOOR ESCAPE SLIDE LIGHT INOP. R&R BATTERY PACK PER AMM.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 37,515 hrs · 22,470 cycles
FORWARD GALLEY OVER DOOR EXIT SIGN INOP. R&R CHARGER PER AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,515 hrs · 22,470 cycles
LT EXIT LOCATOR SIGN INOP. R&R BATTERY PACK PER AMM.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 37,515 hrs · 22,470 cycles
L1 DOOR ESCAPE SLIDE LIGHT INOP. R&R CHARGER PER AMM.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 37,515 hrs · 22,470 cycles
LT EXIT LOCATOR SIGN INOP. R&R CHARGER PER AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,515 hrs · 22,470 cycles
FORWARD GALLEY OVER DOOR EXIT SIGN INOP. R&R BATTERY PACK PER AMM.
2019
Part: RETAINER — PULLED (LEFT WING) · airframe 34,932 hrs · 20,822 cycles
LH WING #3 CANOE OUTBD SIDE SEAL RETAINER HAS 3 RIVETS PULLED THROUGH / (CLOSING DMA 0061824) CL # 56047 PERMANENT REPAIR ACCOMPLISHED ON ACTION LOG PAGE # 0661043
2018
Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 33,866 hrs · 20,138 cycles
L2 DOOR EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 33,866 hrs · 20,138 cycles
RT HORIZONTAL STABILIZER RIB CRACKED 120.30 4TH STIFFENERS FROM FORWARD END. REPAIRED RIB PER SRM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 33,866 hrs · 20,138 cycles
LT HORIZONTAL STABILIZER RIB CRACKED AT 120.30, 4TH STIFFENERS FROM FORWARD END. REPAIRED RIB PER SRM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 33,866 hrs · 20,138 cycles
LT HORIZONTAL STABILIZER RIB CRACKED AT 120.30, 3RD STIFFENERS FROM FORWARD END. REPAIRED RIB PER SRM.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 33,866 hrs · 20,138 cycles
RT HORIZONTAL STABILIZER RIB CRACKED 120.30 2ND STIFFENERS FROM FORWARD END. REPAIRED RIB PER SRM.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 33,866 hrs · 20,138 cycles
RT HORIZONTAL STABILIZER RIB CRACKED 120.30 3RD STIFFENERS FROM FORWARD END. REPAIRED RIB PER SRM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 33,866 hrs · 20,138 cycles
LT HORIZONTAL STABILIZER RIB CRACKED AT 120.30, 2ND STIFFENERS FROM FORWARD END. REPAIRED RIB PER SRM.
Part: STRINGER — CRACKED (LT WING) · airframe 33,866 hrs · 20,138 cycles
LT WING FIXED LEADING EDGE AFT STRINGER CRACKED AT OUTBOARD FLANGE FASTENER HOLE COMMON TO SEAL RIB. R&R STRINGER IAW SRM AND DWG.
Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 33,866 hrs · 20,138 cycles
WHILE WORKING FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 767-794 R/H SIDE / REMOVED FLOOR TO SIDEWALL SUPPORT BS 767-794 IAW SRM 51-40-02. RECEIVED FLOOR TO SIDEWALL ITEM 7531132 PO #700102. LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 146A0081. INSTALLED FLOOR TO SIDEWALL SUPPORT BS 7670794 IDW DWG 146A0081 AND SRM 51-40-02 80641U 12/14/18
Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 33,590 hrs · 19,972 cycles
LOWER CENTER VAPOR BARRIER WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB PER SRM AND EA.
Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 33,180 hrs · 19,722 cycles
RT MAIN LANDING GEAR FORWARD TRUNNION LUG FITTING CORRODED. REPAIRED FITTING PER EA.
Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 33,180 hrs · 19,722 cycles
LT MAIN LANDING GEAR FORWARD TRUNNION LUG FITTING CORRODED. REPAIRED FITTING PER EA.
Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 32,514 hrs · 19,249 cycles
L1 DOOR EVAC SLIDE EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.
Part: SLIDE — UNSECURE (L1 DOOR) · airframe 30,637 hrs · 18,027 cycles
L1 DOOR ESCAPE SLIDE INADVERTENTLY FELL OUT OF COVER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER AMM AND MT.
Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 30,609 hrs · 18,005 cycles
ON PREFLIGHT INSPECTION LT MAIN WHEEL WELL MOISTURE BARRIER CRACKED AT LBL 40. REPAIRED BARRIER PER SRM.
2017
Part: WARNING LIGHT — ILLUMINATED (OIL BYPASS) · airframe 28,219 hrs · 16,473 cycles
DURING CLIMB, RECEIVED OIL FILTER BYPASS LIGHT FOR THE NR 2 ENGINE 2. RAN QRH AND LIGHT DID NOT EXTINGUISH. INFLIGHT SHUTDOWN, AIR TURNBACK, DECLARED AN EMERGENCY. R & R THE NR 2 ENGINE IAW MT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,827 hrs · 16,238 cycles
LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.
2016
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,429 hrs · 15,977 cycles
INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294.5, BL 0. R&R INTERCOSTAL PER SRM.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,429 hrs · 15,977 cycles
L1 DOOR FLOOR STRUCTURE ANGLE CRACKED AT BS 303. REPAIRED ANGLE PER EA.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 27,429 hrs · 15,977 cycles
FORWARD CARGO THRESHOLD WEB CORRODED. REPAIRED WEB PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,138 hrs · 15,801 cycles
LT OVERWING EMERGENCY EXIT LIGHT INOP. R&R LIGHT PER AMM.
Part: FAN — FAILED (RECIRCULATION) · airframe 26,255 hrs · 15,270 cycles
ELECTRICAL BURNING ODOR AND SLIGHT SMOKY HAZE REPORTED IN THE CABIN AROUND ROW 17. SMOKE ODOR WENT AWAY AFTER TURNING OFF GALLEY POWER AND SEAT BELT SIGN. R & R CABIN RECIRCULATION FAN IAW AMM.
Part: COVER — UNSECURE (EXIT SIGN) · airframe 26,189 hrs · 15,234 cycles
R1 DOOR EXIT SIGN FELL OFF. R&R LIGHT ASSEMBLY COVER PER MM.
Part: LENS — BROKEN (CABIN) · airframe 25,867 hrs · 15,048 cycles
RIGHT OVERWING EXIT DOOR LIGHT LENS BROKEN. R & R LENS IAW MM.
Part: SIGN — LOOSE (CABIN) · airframe 24,955 hrs · 14,521 cycles
OVERWING CEILING EMER EXIT SIGN LOOSE. R & R SIGN IAW AMM.
2015
Part: BATTERY — FAILED (CABIN) · airframe 22,763 hrs · 13,255 cycles
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATION M1670. R & R BATTERY IAW AMM.
Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 22,763 hrs · 13,255 cycles
RIGHT WING NR 6 GND SPOILER, UPPER TE SHELF PANEL SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.
Part: BATTERY — FAILED (CABIN) · airframe 22,763 hrs · 13,255 cycles
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATION M1672. R & R BATTERY IAW AMM.
Part: BATTERY — FAILED (CABIN) · airframe 22,763 hrs · 13,255 cycles
EMER BATTERY FAILED CAPACITY CHECK AT LOCATION M1674. R & R BATTERY IAW AMM.
Part: BATTERY — FAILED (CABIN) · airframe 22,763 hrs · 13,255 cycles
EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATION M1673. R & R BATTERY IAW AMM.
Part: LIGHT — MISSING (CABIN) · airframe 22,131 hrs · 12,902 cycles
R1 DOOR EMER LIGHT MISSING ON WALL. INSTALLED LIGHT ASSEMBLY IAW SIP.
Part: INTERCOSTAL — BROKEN (FUSELAGE) · airframe 21,105 hrs · 12,306 cycles
FLOOR SUPPORT INTERCOSTAL BROKEN AT BS 540, BETWEEN BL 0 TO LBL 24. R & R INTERCOSTAL IAW SRM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 21,105 hrs · 12,306 cycles
LEFT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER AT STAB STATION 129.5, 27 INCHES FROM THE FRONT SPAR CRACKED. REPAIRED RIB IAW EA.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 21,105 hrs · 12,306 cycles
LEFT FLIGHT DECK WINDOW FRAME CRACKED AT OTBD UPPER SURFACE. REPAIRED FRAME IAW EA.
2014
Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 20,865 hrs · 12,184 cycles
LEFT MLG WW CTR WING SECTION, LOWER LT VAPOR BARRIER CRACKED AT LBL 40.00 6 INCHES FROM BOTTOM. REPAIRED BARRIER IAW SRM.
Part: LIGHT — WORN (CABIN) · airframe 20,560 hrs · 12,000 cycles
RIGHT FWD EEPLS WORN. R & R EEPLS IAW MM.
Part: MOUNT — BROKEN (EXIT SIGN) · airframe 19,457 hrs · 11,372 cycles
L1 DOOR EMER EXIT SIGN LENS MOUNT BROKEN. R & R MOUNT ASSEMBLY IAW AMM.
Part: LENS — LOOSE (CABIN) · airframe 19,087 hrs · 11,179 cycles
MID CABIN CEILING EMER LIGHT LENS LOOSE. SECURED LENS IAW SIP.
Part: COVER — LOOSE (CABIN) · airframe 19,003 hrs · 11,135 cycles
R1 DOOR EMER EXIT LIGHT COVER LOOSE. R & R COVER IAW MM.
2013
Part: SIGN — BROKEN (CABIN) · airframe 15,506 hrs · 9,100 cycles
OVERWING EMERGENCY EXIT SIGN BROKEN OFF. R&R EXIT SIGN IAW M/M.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 14,802 hrs · 8,681 cycles
LEFT HORIZ STAB LOWER IN-SPAR SKIN CRACKED AT L/E STA 138.7. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 14,802 hrs · 8,681 cycles
RIGHT HORIZ STAB LOWER IN-SPAR SKIN CRACKED AT L/E STA 101.9. REPAIRED SKIN PER SRM.
Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 13,797 hrs · 8,100 cycles
LEFT MLG W/W CENTER WING REAR SPAR VAPOR WEB IS CRACKED 15" LONG. REPAIRED VAPOR BARRIER LEFT MLG WHEEL WELL PER EA 1-A53-3376.
2012
Part: BATTERY — FAILED (CABIN) · airframe 13,523 hrs · 7,953 cycles
LEFT CENTER CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY, OP CHECK GOOD PER AMM.
Part: BATTERY — FAILED (CABIN) · airframe 13,523 hrs · 7,953 cycles
RIGHT CENTER CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY, OP CHECK GOOD PER AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,130 hrs · 7,715 cycles
LEFT EEPLS INOP AT ROW 21. REMOVED AND REPLACED BULB IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,856 hrs · 7,524 cycles
AFT EEPLS INOP. RELAMPED EEPLS PER M/M.
Part: COVER — CRACKED (CABIN) · airframe 12,660 hrs · 7,395 cycles
L/G EEPLS COVERS CRACKED BETWEEN ROW 1 TO ROW 11. REMOVED AND REPLACED COVERS PER M/M.
Part: LIGHT — BROKEN (CABIN) · airframe 11,999 hrs · 7,019 cycles
FWD GALLEY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M/M.
Part: SIGN — OUT OF POSITION (CABIN) · airframe 11,935 hrs · 6,982 cycles
AFT EMERGENCY EXIT SIGN FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER AMM.
Part: STRIP — CRACKED (CABIN) · airframe 11,441 hrs · 6,697 cycles
EEPLS STRIP CRACKED AT 1C. REMOVED AND REPLACED STRIP PER AMM.
Part: COVER — MISSING (CABIN) · airframe 10,848 hrs · 6,355 cycles
LT EMERGENCY EXIT LIGHT COVER IN FLOOR ROW MISSING. INSTALLED COVER IAW M/M.
Part: COVER — MISSING (CABIN) · airframe 10,640 hrs · 6,225 cycles
AFT SERVICE DOOR EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: COVER — MISSING (CABIN) · airframe 10,639 hrs · 6,225 cycles
R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.
2011
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 9,568 hrs · 5,597 cycles
DURING SCHEDULED MV1 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
Part: LENS — CRACKED (CABIN) · airframe 9,213 hrs · 5,391 cycles
DURING SCHEDULED HC2 CHECK, FOUND LT FWD EEPLS LENS CRACKED. REMOVED AND REPLACED LENS PER MM.
Part: LIGHT — BROKEN (CABIN) · airframe 8,759 hrs · 5,132 cycles
R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,660 hrs · 5,079 cycles
L1 DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: SIGN — BROKEN (CABIN) · airframe 7,837 hrs · 4,614 cycles
RT EMERGENCY EXIT SIGN BROKEN AT AFT CABIN. REMOVED AND REPLACED SIGN ASSY PER MM.
2010
Part: COVER — LOOSE (CABIN) · airframe 5,327 hrs · 3,187 cycles
OVERWING EMERGENCY EXIT LIGHT LENS COVER LOOSE. SECURED COVER PER MM.
Part: LENS — LOOSE (CABIN) · airframe 4,085 hrs · 2,473 cycles
DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS LOOSE AT ROW 1. INSTALLED LENS PER MM.
Part: BRACKET — OUT OF ADJUST (GIRT BAR) · airframe 3,875 hrs · 2,351 cycles
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW BRACKET OUT OF ADJUST. ADJUSTED BRACKET PER MM.
2009
Part: CAP — MISSING (CABIN) · airframe 2,292 hrs · 1,381 cycles
FWD EEPLS END CAP MISSING. REMOVED AND REPLACED EEPLS PER MM.
Part: PUMP — FAULTY (NR 1 ENGINE) · airframe 2,207 hrs · 1,328 cycles
AIR TURNBACK, A HYDRAULIC ELECTRIC PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED A SYSTEM HYDRAULIC PUMP PER MM.
Part: COVER — LOOSE (CABIN) · airframe 2,167 hrs · 1,307 cycles
DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVERS LOOSE AT ROW 1. INSTALLED COVERS MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 2,139 hrs · 1,286 cycles
DURING SCHEDULED MV1 CHECK, FOUND AFT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: COVER — MISSING (CABIN) · airframe 1,945 hrs · 1,174 cycles
EEPLS COVER MISSING AT ROW 1. INSTALLED COVER PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 1,904 hrs · 1,152 cycles
FWD EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM.
Part: WIRE — DAMAGED (CABIN) · airframe 659 hrs · 403 cycles
EEPLS INOP AT ROW 1. REPAIRED EEPLS WIRING PER MM.
Part: COVER — BROKEN (CABIN) · airframe 1,177 hrs · 713 cycles
R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT PER MM.