N929WN
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.
267 reports on file, 2009-01-02 – 2026-08-13.
Part: EXTINGUISHER — LOW PRESSURE (ZONE 100) · airframe 58,450 hrs · 35,755 cycles
LEFT ENGINE FIRE BOTTLE IN WHEEL WELL READS 450 PSI. R & R ENGINE FIRE EXTINGUISHING BOTTLE NR 1 IAW AMM 26-21-01. OPS CHKD GOOD.
Part: FUSE — INOPERATIVE (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
EMERGENCY EXIT SIGN MOUNTED ON FDR ACCESS DOOR IS INOPERATIVE. REMOVED AND REPLACED FUSE ON (M1672) AND PERFORMED A GOOD TEST EMERGENCY EXIT SIGN MOUNTED ON FDR ACCESS DOOR PER AMM 33-51-06-960-804.
Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
RIGHT OVER WING EMERGENCY EXIT LIGHT (EXTERNAL) INOPERATIVE. REPLACED M1669 EMERGENCY BATTERY IAW AMM 33-51-06-960-805. RELAMPED RIGHT OVERWING EMERGENCY EXIT SLIDE LIGHT IAW AMM 33-51-04-960-801. PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST PER AMM 33-51-00-710-801, ALL EMERGENCY LIGHTS OPERATE CORRECTLY.
Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
F/O'S NR 1 WINDOW FRAME POST OTBD UPPER CORNER IS CRACKED. F/O'S NR 1 WINDOW FRAME REPAIRED IAW EA 26-153-01462.
Part: STRAP — CRACKED (ZONE 100) · airframe 58,054 hrs · 35,506 cycles
CRACK NOTED IN ONE FASTENER HOLE DURING OHEC INSPECTION (TTG8Q01BLWC6; STEP 22) OF RT STUB BEAM STRAP, BS 639, RBL 45, LOWER AFT HOLE, EXTENDING IN AFT DIRECTION. ENGINEERING REQUIRED FOR REPAIR. REMOVED RT STUB BEAM STRAP DAMAGED AT BS 639, RBL 45, AND REPLACED BY NEW IAW SRM 51-40-02-0G-0, & DWG 144A1715, REV A. REMOVED RT STUB BEAM STRAP BS 639, RBL 45 IAW SRM 51-40-02-0G-0. LOCATED & DRILLED RT STUB BEAM STRAP BS 639, RBL 45 IAW SRM 51-40-05-0G-0, DWG 144A1715, REV A, & DWG 144A1705, REV-. INSTALLED REPLACEMENT RT STUB BEAM STRAP IAW SRM 51-40-02-0G-0 AND DWG 144A1715, REV A. REINSTALLED STUB BEAM ASSY IAW SRM 51-40-02-0G-0, DWG 110A0170, REV-, & DWG 144A1715, REV A. REMOVED STIFFENER BS 639 - 663, RBL 69.5, WL 204 IAW SRM 51-40-02-0G-0. INSTALLED STIFFENER IAW SRM 51-40-02-0G-0 & DWG 144A7301 REV-. CAP SEAL & FILLET SEAL APPLIED AROUND THE FASTENERS OUTSIDE & INSIDE AREA OF STUB BEAM ASSY.
Part: FRAME — CRACKED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
BS 312 FRAME CRACKED WL 283 LBL 35 ABOVE FWD ENTRY UPPER SILL WEB. ACCOMPLISHED REPAIR OF FRAME AT BS 312, WL 283, LBL 35, BTW S5L AND S6L IAW EA M-22-153-01244.
Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
CAPTAINS #1 WINDOW FRAME HAS CRACK IN LOWER INBOARD CORNER<[01] ACCOMPLISHED HFEC SURFACE SCAN OF SUSPECTED CRACKED LOCATION IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. REMOVED SKIN PANEL 141A3816-9 TO F.O.M I.A.W SRM 51-40-02-0G-0. INSTALLED FASTENER PER EA 26-153-01448-WIP2. PERFORMED A HARD ALIGNMENT VERIFICATION PER SMM 34-36-00 AND VERIFIED ALIGNMENT IS WITHIN RANGE LESS THAN 10 (RADIANS) ACTUAL READING IS 8 RADIANS. VERIFIED SERVICEABILITY OF THE HUD MOUNT BRACKET AND THE INSTALLATION PER DRAWING REQUIREMENTS 141A8870 REV-. REPAIR ACCOMPLISHED IAW EA 26-153-01448.;
Part: RIB — CRACKED (ZONE 300) · airframe 58,054 hrs · 35,506 cycles
RIGHT HORIZONTAL STAB REMOVABLE LEADING-EDGE 2ND FROM INBD RIB CRACKED. REMOVED, LOCATED, AND DRILLED. REPLACED NEW RT HORIZONTAL STAB REMOVABLE LEADING-EDGE 2ND FROM INBD RIB IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, AND DWG 186A1001, REV B.
Part: SKIN — CRACKED (ZONE 300) · airframe 58,054 hrs · 35,506 cycles
CRACK NOTED ON RT HORIZONTAL STABILIZER LOWER SKIN, BS 193.90; APPROX 3.6' FWD OF PREVIOUS REPAIR; L: 0.25'. REPAIRED PER EA 26-155-01375 WITH REPETITIVE INSPECTION PROGRAM DEFINED IN EA 26-155-01375-INSP. ALL STEPS ACCOMPLISHED. TASK CARD COMPLETE.
Part: RIB — CRACKED (ZONE 600 FLAP) · airframe 58,054 hrs · 35,506 cycles
CRACK FOUND ON RT OTBD AFT FLAP CLOSURE RIB. PROCURED NEW LT OTBD AFT FLAP. REMOVAL AND INSTALLATION TO BE ACCOMPLISHED ON FAULT TTG8Q01C9QA5. IAW AMM 27-51-22-401.
Part: CARTRIDGE — CRACKED (ZONE 600 FLAP) · airframe 58,054 hrs · 35,506 cycles
CRACKED FOUND ON RT OTBD AFT FLAP CARTRIDGE. RECEIVED A NEW AFT FLAP. NO FURTHER ACTION REQUIRED ON THIS FAULT.
Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 58,054 hrs · 35,506 cycles
CORROSION ON PASSENGER CABIN SEAT TRACKS IN WELL AT BS 480+14 - BS 480+19, BS 500A+4 - BS 500A+16, BS 500D+9 - BS 500D+13. ON CROWN BS 480+8 - BS 480+13, LBL 45, WL 208. THE SEAT TRACK FOUND TO BE OUT OF LIMITS; WILL BE REPLACED ON TASK CARD TTG8Q01C9N0.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
CORROSION IN WELL ON PASSENGER CABIN SEAT TRACKS AT BS 480+15- BS 500+8, BS 500A+6 - BS 500A+18, BS 500D+8 - BS 500D+19. ON CROWN BS 500A+18 AT LBL 25 WL 208. SEAT TRACK FOUND TO BE OUT OF LIMITS, & WILL BE REPLACED ON TASK CARD TTG8Q01C933B.
Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
CORRODED FLOOR SUPPORT AT BS 294 - 312, LBL 11, WL 208. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, DWG 141A5600, SHEET 1, REV N, AND DWG 141A5600, SHEET 2, REV N.
Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
CORROSION ON CREASE BEAM WEB AT BS 727A+16 LBL 69 WL 208. REMOVED AND TREATED CORROSION OF CREASE BEAM WEB AT BS 727A+16 LBL 69 WL 208 PER SRM 51-10-02-0G-0 AND EA 26-153-01357.
Part: STRAP — CORRODED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
CORROSION ON STRAP AT BS 1026-1028, RBL 17, WL 208. REMOVED AND REPLACED STRAP AT BS 1026-1028, RBL 17, WL 208 IAW SRM 51-40-02-0G-0, AND DWG 147A5730, SHEET 23, REV C, DATE: 02/19/08. VERIFIED CORRECTIVE ACTION 1.
Part: STRAP — CORRODED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
CORRODED ON STRAP AT BS 1016-1029, LBL 3, WL 208. REMOVED AND REPLACED STRAP AT BS 1016-1029, LBL 3, WL 208 IAW SRM 51-40-02-0G-0, AND DWG 147A5600, SHEET 32, REV B.
Part: WEB — CORRODED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
CORROSION ON WEB AT BS 1018 LBL 1 WL 208. NO ALLOWABLE ENTRIES FOUND THEREFORE SHEAR WEB DAMAGE TO BE REMOVE IAW SRM 51-10-02-0G-0 AND SENT TO ENGINEERING FOR FURTHER REPAIR INSTRUCTIONS. REMOVED CORROSION ON WEB AT BS 1018 LBL 1 WL 208 1'X1' AREA IAW SRM 51-10-02-0G-0. REMOVED 1EA FASTENER TO FOM BS 1018 LBL 1 WL 208 IAW SRM 51-40-02-0G-0. INSTALLED ONE FASTENER IAW SRM 51-40-02-0G-0 & SRM 147A5600 REV B. ACCOMPLISHED HFEC INSP OF ONE HOLE WITHIN REWORKED AREA IAW NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 16. NO CRACKS NOTED. APPLIED CHEMICAL CONVERSION COAT & PRIMED AREA IAW SRM 51-20-01 AND SOPM 20-41-02. REMOVED & TREATED CORROSION ON WEB IAW SRM 51-10-02-0G-0, AND EA 26-153-01349.
Part: STRAP — CORRODED (ZN 100 FUS LOWER) · airframe 58,054 hrs · 35,506 cycles
CORROSION ON STRAP AT BS 1022-1029, RBL 3, WL 208. REMOVED AND REPLACED STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5730, SHEET 23, REV C.
Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
CRACKED INTERCOSTAL AT BS 380-400, RBL 40, WL 208. REMOVED AND REPLACED INTERCOSTAL FROM BS 380-400 RBL 40 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A5400 ID:0109 REV. A.
Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
CRACKED INTERCOSTAL AT BS 312 - 328, LBL 45, WL 208. REMOVED AND REPLACED THE INTERCOSTAL AT BS 312-328 LBL 45 WL 208 IAW SRM 51-40-02, & DWG 141A5400, REV-.
Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
CRACKED INTERCOSTAL AT BS 312 - 328, RBL 31, WL 208. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, AND DWG 141A5400, REV-.
Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
CRACKED INTERCOSTAL AT BS 380-400, LBL 13, WL 208. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02-0G-0, AND DWG 143A5400, REV A.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
CRACKED FLOOR SUPPORT AT BS 270 - 277, LBL 1, WL 208. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, & DWG 141A5210, SHEET 19, REV -.
Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
AFT FLOOR PANEL 241XF UPPER SURFACE HAS PULLED STRANDS. AFT FLOOR PANEL 241XF UPPER SURFACE WITH PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.
Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
AFT FLOOR PANEL 241YF UPPER SURFACE HAS PULLED STRANDS. REPAIRED PER SRM 53-00-50-2R-1-A00939.
Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
AFT FLOOR PANEL 242TF UPPER SURFACE HAS PULLED STRANDS<[01] 242TF AFT FLOOR PANEL FOUND UPPER AND LOWER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
AFT FLOOR PANEL 242UF UPPER SURFACE HAS PULLED STRANDS. 242UF AFT FLOOR PANEL FOUND UPPER AND LOWER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.
Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
AFT FLOOR PANEL 241AAF UPPER SURFACE HAS PULLED STRANDS. FABRICATION OF NEW 241AAF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.
Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
AFT FLOOR PANEL 241ABF UPPER SURFACE HAS PULLED STRANDS. AFT FLOOR PANEL 241ABF UPPER SURFACE WITH PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.
Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,054 hrs · 35,506 cycles
FWD FLOOR PANEL 222BF UPPER SURFACE HAS PULLED STRANDS. FWD FLOOR PANEL 222BF UPPER SURFACE WITH PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.
Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
FWD FLOOR PANEL 222DF UPPER SURFACE HAS PULLED STRANDS. PULLED STRANDS ON UPPER SURFACE OF FWD FLOOR PANEL 222DF WERE REPAIRED IAW SRM 53-00-50-2R-1.
Part: STUB FRAME — CRACKED (ZONE 100) · airframe 58,054 hrs · 35,506 cycles
CRACK ON FSD STUB FRAME .6' ABOVE SEAL DEPRESSOR AT BS291.5 + 9, REMOVED DAMAGE FSD STUB FRAME, LOCATED, DRILLED, AND INSTALLED NEW FSD STUB FRAME AT BS 291+9 IAW SRM 51-40-02-0G-0, AND DWG 141A8370, REV D.
Part: FORMER — CRACKED (ZONE 100) · airframe 58,054 hrs · 35,506 cycles
WING TO BODY FAIRING FORMER IS CRACKED BS 500D BETWEEN STRINGER 19 AND 20 RT. REMOVED DAMAGED FAIRING FORMER AND INSTALLED NEW WING TO BODY FAIRING FORMER AT BS 500D BETWEEN STRINGER 19 AND 20 RT IAW SRM 51-40-02-0G-0, AND DWG 116A3010, REV -.
Part: SPLICE STRAP — CORRODED (ZONE 100) · airframe 58,054 hrs · 35,506 cycles
CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE, BS 767+6, RBL 11.5, WL 156. CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. NEW STRAP TO BE INSTALLED ON FAULT TTG8Q01BBZ84.
Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
CRACK FOUND ON HORIZONTAL PRESSURE DECK RBL 39, BS 663+2, L: 0.300. REPAIRED HORIZONTAL PRESSURE DECK AT BS 663 - BS 675; RBL 39 - RBL 62 IAW SRM 53-40-51-2R-2, REPAIR 2.
Part: SKIN — DEBONDED (ZONE 100) · airframe 58,054 hrs · 35,506 cycles
PANEL 192AL OUTER SKIN IS DISBONDED. REPAIRED OUTER SKIN DISBOND IAW SRM 51-70-05-2R-2-A00733. (REPAIR 2 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE - AIRFRAME - PERMANENT)
Part: SCUFF PLATE — CRACKED (ZONE 200) · airframe 58,054 hrs · 35,506 cycles
FWD SERVICE DOOR SCUFF PLATE CRACKED AT AFT EDGE. ACCOMPLISHED REPAIR OF CRACKED FSD SCUFF PLATE PER SRM 53-10-15-2R-2. SCUFF PLATE WILL BE INSTALLED BY TASK TTG8Q002E2N5. ] RII N/A DUE TO SRM 53-10-15-2R-2 4.B. NOTE, THIS ITEM IS NOT A STRUCTURAL PART.
Part: BRACKET — CRACKED (ZONE 800) · airframe 57,685 hrs · 35,259 cycles
AFT SERVICE DOOR LINER LOWER ATTACH PLATE FWD BRACKET CRACKED. R & R AFT SERVICE DOOR LINER LOWER PAN IAW AMM 52-41-31.
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 57,685 hrs · 35,259 cycles
FLIGHT DECK EMERGENCY LIGHTS, R1 DOOR SLIDE LIGHT INOPERATIVE. REPLACED THE LAMPS IN THE EMERGENCY LIGHTS R1 DOOR SLIDE LIGHT IAW AMM 33-51-04.
Earlier reports · 2009–2025 · 227 reports
2025
Part: SEAT BACK — NO DISCREPANCY (ZONE 200) · airframe 56,955 hrs · 34,752 cycles
SEAT 11D SEAT RECLINES INTO EXIT ROW. OPS CHECKED SEAT 11D, FOUND SMALL FORWARD MOVEMENT BUT NO RECLINE MOVEMENT IAW SOPM.
Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 56,686 hrs · 34,547 cycles
PASSENGER CABIN EMERGENCY LIGHTS BATTERY PACKS M1675, M1674, M1673, & M1672 FAILED CAPACITY TEST. R & R EMERGENCY LIGHTS BATTERY PACKS IAW AMM 33 51-06.
Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 56,686 hrs · 34,547 cycles
PASSENGER CABIN EMERGENCY LIGHTS BATTERY PACKS M1675, M1674, M1673, & M1672 FAILED CAPACITY TEST. R & R EMERGENCY LIGHTS BATTERY PACKS IAW AMM 33 51-06.
Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 56,686 hrs · 34,547 cycles
PASSENGER CABIN EMERGENCY LIGHTS BATTERY PACKS M1675, M1674, M1673, & M1672 FAILED CAPACITY TEST. R & R THE EMERGENCY LIGHTS BATTERY PACKS IAW AMM 33 51-06.
Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 56,686 hrs · 34,547 cycles
PASSENGER CABIN; EMERGENCY LIGHTS BATTERY PACKS M1675, M1674, M1673, & M1672 FAILED CAPACITY TEST. R & R EMERGENCY LIGHTS BATTERY PACKS IAW AMM 33 51-06.
Part: DOUBLER — CORRODED (ZONE 100) · airframe 55,697 hrs · 33,924 cycles
EVIDENCE OF CORROSION FOUND ON RF CONNECTOR DOUBLER BELOW WIFI RADOME AT CONNECTION D9302<[01] COMPLIED WITH EA 25-153-02026 REF TTG8Q014719L
Part: DOUBLER — CORRODED (ZONE 100) · airframe 55,697 hrs · 33,924 cycles
EVIDENCE OF CORROSION FOUND ON RF CONNECTOR DOUBLER UNDER WIFI RADOME AROUND CONNECTOR D9303 HOLE.<[01] COMPLIED WITH EA 25-153-02026 REF TTG8Q014719L
Part: SIGN — BROKEN (ZONE 200) · airframe 55,659 hrs · 33,899 cycles
OVERWING EXIT OVERHEAD EMERGENCY LT HOUSING BROKEN. R+R EMERGENCY EXIT SIGN PER AMM 33-51-01.
Part: HANDLE — LOOSE (ZONE 800) · airframe 54,561 hrs · 33,228 cycles
AFT SERVICE DOOR ASSIST HANDLE LOOSE <[01]. SECURED ASSIST DOOR HANDLE REF B737 AMM 52-41-31.
2024
Part: COVER — MISSING (ZN 200 FUS TOP) · airframe 53,558 hrs · 32,633 cycles
MID-CABIN OVERHEAD AFT EXIT SALIDA SIGN COVER IS MISSING.<[01] FOUND AND RE-INSTALLED OVERHEAD EMERGENCY EXIT SIGN COVER. REF. AMM 33-51-01.
Part: FLOORBEAM — DEFECTIVE (BS 986) · airframe 52,102 hrs · 31,708 cycles
DURING ACCOMPLISHMENT OF STA 986 FLOOR BEAM REPAIR FAULT TTG8Q00TDFQW REF: SRM 53-70-51-2R-4 DEVIATION IN FASTENERS HOLES LAYOUT AT RBL 22.5' FASTENERS NOT STAGGERED AS PER SRM LAYOUT.<[01] RECEIVED ENGINEERING APPROVAL FOR DEVIATION OF FASTENER HOLES LAYOUT AT STA 986.5 REPAIR REF: EA 24-153-01465 (TTG8Q00TS3Y5);[02] RII- VERIFIED RECEIVED ENGINEERING APPROVAL
Part: SHIELD — CORRODED (FWD CARGO) · airframe 52,102 hrs · 31,708 cycles
**CORROSION** FWD CARGO R/H SIDE PLATE UPPER SURFACE BETWEEN STA 492 TO 500A RBL 21.80 HAS CORROSION AROUND FASTENERS HOLES MKD (107-005)<[01] (FINAL) REMOVED CORROSION AROUND FASTENER HOLES FROM FWD CARGO R/H SIDE PLATE UPPER SURFACE BETWEEN STA 492 TO STA 500A RBL 21.80' PER B737-700 SRM 51-10-02-0G-0. AND; PERFORMED SURFACE ROUGHNESS TEST ON REWORKED AREA; FOUND IT TO BE SMOOTHER THAN 125 MICROINCHES RA.<BR>TOOL USED B/C: 172329. NO CALIBRATION DUE DATE. LOCATED AND DRILLED NEW FWD CARGO COMPARTMENT DOOR AFT SHIELD PER B737-700 PER SRM 51-40-05-0G-0. INSTALLED NEW FWD CARGO COMPARTMENT DOOR AFT SHIELD PER B737-700 DWG# 143A0080 AND SRM 51-40-02-0G-0.;[02] (CORRECTION STEP 1) REMOVED CORROSION AROUND FASTENER HOLES FROM FWD CARGO R/H SIDE PLATE UPPER SURFACE BETWEEN STA 492 TO STA 500A RBL 21.80' PER B737-700 SRM 51-10-02-0G-0. AND; PERFORMED SURFACE ROUGHNESS TEST ON REWORKED AREA; FOUND IT TO BE SMOOTHER THAN 125 MICROINCHES RA.<BR>TOOL USED B/C: 172329. NO CALIBRATION DUE DATE. EVALUATED REWORKED AREA ORG MAT .032' MAT REMAINING .022' MAT REMOVED .010' FOUND TO BE OUT OF LIMITS AS PER B 737 SRM 53-00-53-1A-2. LOCATED AND DRILLED NEW FWD CARGO COMPARTMENT DOOR AFT SHIELD PER B737-700 PER SRM 51-40-05-0G-0. INSTALLED NEW FWD CARGO COMPARTMENT DOOR AFT SHIELD PER B737-700 DWG# 143A0080 AND SRM 51-40-02-0G-0.;[03] VERIFIED STEP 2.
Part: FLOOR SUPPORT — CRACKED (BS 312-328 LBL52) · airframe 52,102 hrs · 31,708 cycles
MAIN CABIN FWD WET AREA UNDER PANEL 221DF BETWEEN STA 312 AND STA 328 APPROX. LBL 52 HAS INTERCOSTAL WITH POSSIBLE CRACK.<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN FWD WET AREA UNDER PANEL 221DF BETWEEN STA 312 AND STA 328 APPROX. LBL 52 PER B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING 141A5400.;[02] VERIFIED STEP 1
Part: SCUFF PLATE — CORRODED (L1 DOOR AREA) · airframe 52,102 hrs · 31,708 cycles
MAIN CABIN FWD WET AREA AT L1 DOOR SCUFF PLATE LOWER STRUCTURE UNDER AFT DRAIN HOLE SHOW SIGNS OF CORROSION<[01] CLEANED AREA UNDER AFT DRAIN HOLE AT MAIN CABIN FWD WET AREA L-1 DOOR SCUFF PLATE LOWER STRUCTURE PER BOEING SOPM 20-30-03. NO COROSION NOTED. ONLY FOUND ACCUMULATION OF CIC.;[02] VERIFIED STEP 1
Part: FLOORBEAM — CRACKED (BS 540 LBL1) · airframe 52,102 hrs · 31,708 cycles
MAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED AT STA 540 LBL 1 MKD DOT<[01] SUMMARY <BR>REMOVED MAIN CABIN FLOOR PANEL 231UF FOR ACCESS PER B737-700 SRM 51-40-02-0G-0.<BR>REMOVED FLOOR SUPPORT BREAK AT STA 540 LBL 1 AS PER B-737 SRM 51-40-02-0G-0LOCATED AND DRILLED NEW FLOOR SUPPORT BREAK AS PER B-737 SRM 51-40-05-0G-0.<BR>INSTALLED NEW FLOOR SUPPORT AS PER B-737 SRM 51-40-02-0G-0. & DWG 143A0060<BR>RE-INSTALLED FLOOR PANEL 231UF AT MAIN CABIN CENTER SECTION AS PER B-737 AMM 53-21-00-400-801 TOOL USED B/C # 176025 DUE DATE ON 07/JUN/2024.;[02] VERIFIED STEP 1.
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 52,102 hrs · 31,708 cycles
MAIN CABIN FWD WET AREA PANEL 221EF WITH SEVERAL AREAS OF DELAMINATION ON TOP OF PANEL PN: 141A5810-249<[01] RECEIVED AND REPLACED PANEL 221EF AS PER SRM 53-00-50-2R-0. PANEL CLOSING WILL ACCOMPLISHED IN TASK CARD TTG8Q00SJK78.;[02] VERIFIED REPLACED;[03] VERIFIED REPLACED.<BR>QUALITY CONTROL PERFORMED A REVIEW OF THIS FAULT.<BR>C/W AUDIT PER MPM 52.02.02
Part: FLOOR SUPPORT — CRACKED (BS 286-295 RBL5) · airframe 52,102 hrs · 31,708 cycles
MAIN CABIN FWD WET AREA UNDER PANEL 221AF BETWEEN STA 285.62 AND STA 294.5 APPROX. RBL 5 HAS INTERCOSTAL WITH POSSIBLE CRACK.<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN FWD WET AREA UNDER FLOOR PANEL 221AF BETWEEN STA 285.62 AND STA 294.5 APPROX. RBL 5 PER B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING 141A5400;[02] VERIFIED REPLACEMENT;[03] QUALITY CONTROL (QC) PERFORMED A REVIEW OF THIS FAULT<BR>C/W AUDIT PER MPM 52-02-02
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 52,102 hrs · 31,708 cycles
MAIN CABIN FWD WET AREA PANEL 221CF WITH SEVERAL AREAS OF DELAMINATION ON TOP OF PANEL PN: 141A5810-9<[01] RECEIVED FLOOR PANEL 221CF P/N 141A5810-9 AND INSTALLED ON TASK CARD TTG8Q00SJK7C;[02] QUALITY CONTROL PERFORMED A REVIEW OF THIS FAULT.<BR>C/W AUDIT PER MPM 52.02.02.
Part: FLOORBEAM — CORRODED (BS 987) · airframe 52,102 hrs · 31,708 cycles
CORROSION ** AFT CABIN WET AREA FLOOR SUPPORT BEAM FASTENER HOLE FWD EDGE RBL 45 STA 986.5 MKD DOT<[01] REMOVED CORROSION ON FLOOR BEAM AT STA 986.5 RBL 45 AT FASTENER HOLE AS PER B 737 SRM 51-10-02-0G-0. EVALUATE DAMAGE: ORIGINAL MATERIAL 150'; MATERIAL LOST 0.056'; MATERIAL REMAINING 0.094' FOUND OUT OF LIMITS AS PER SRM 53-70-51-1A-1. FIG. 103; DETAIL C. ACCOMPLISHED A REPAIR PER SRM 53-70-51-2R -4 REPAIR 4.;[02] RII-VERIFIED REPAIR;[03] ACCOMPLISHED EA 24-153-01465. REF FAULT TTG8Q00TLYED.;[04] VERIFIED ACCOMPLISHED EA 24-153-01465. REF FAULT TTG8Q00TLYED
Part: FLOOR PANEL — DELAMINATED (FWD CABIN) · airframe 52,102 hrs · 31,708 cycles
MAIN CABIN FWD WET AREA PANEL 221GF WITH SEVERAL AREAS OF DELAMINATION ON TOP OF PANEL PN: 141A5810-181<[01] RECEIVED AND REPLACED PANEL 221GF AS PER SRM 53-00-50-2R-0. PANEL CLOSING WILL ACCOMPLISHED IN TASK CARD TTG8Q00SJK74.;[02] VERIFIED REPLACED.<BR>QUALITY CONTROL PERFORMED A REVIEW OF THIS FAULT.<BR>C/W AUDIT PER MPM 52.02.02
Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 52,102 hrs · 31,708 cycles
MAIN CABIN FWD WET AREA PANEL 221CF WITH TWO FASTENER INSERT HOLES WITH SIGNS OF CORROSION PN: 141A5810-9<[01] FLOOR PANEL 221CF REPLACED ON NR TTG8Q00TD1ZK.;[02] QUALITY CONTROL PERFORMED A REVIEW OF THIS FAULT.<BR>C/W AUDIT PER 52.02.02
Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 52,102 hrs · 31,708 cycles
AFT CARGO BAY AFT CARGO DOOR SCUFF PLATE CRACK.DOT 251-0015<[01] RECEIVED NEW SCUFF PLATE P/N 654A0004 PO# 2059779.LOCATED AND DRILL NEW SCUFF PLATE PER 51-40-05-0G-0.;[02] VERIFIED RECEIVED NEW
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 52,102 hrs · 31,708 cycles
CABIN FLOOR PANEL 231XF UPPER SKIN DELAMINATED AND TORN IN SEVERAL AREAS.<[01] RECEIVED AND REPLACED PANEL 231XF IAW SRM 53-00-50-2R-0.<BR>INSTALLATION WILL BE ACCOMPLISHED ON ITEM TTG8Q00SJKID;[02] VERIFIED STEP 1
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 52,102 hrs · 31,708 cycles
CABIN FLOOR PANEL 241UF UPPER SKIN DELAMINATED AND TORN IN SEVERAL AREAS<[01] RECEIVED AND REPLACED PANEL 241UF AS PER SRM 53-00-50-2R-0. PANEL CLOSING WILL ACCOMPLISHED IN TASK CARD TTG8Q00SJJZX.;[02] VERIFIED REPLACED.<BR>QUALITY CONTROL PERFORMED A REVIEW OF THIS FAULT.<BR>C/W AUDIT PER MPM 52.02.02
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 52,102 hrs · 31,708 cycles
RH HORIZONTAL STABILIZER RIB #4 STIFFENER #3 LOWER SECTION CRACK<[01] SUMMARY<BR>REMOVED DAMAGE AT RIB #4 STIFFENER #3 AS PER B-737 SRM 55-10-09-2R-4.<BR>REMOVED CRACK ON #3 STIFFINER; AREA MARKED AS PER B-737 SRM 55-10-09-2R-4.<BR>LOCATED AND DRILLED REPAIR PARTS AS PER B-737 SRM 55-10-09-2R-4<BR> & PERFORMED ROUGHNESS TEST ON REPAIR PARTS FOUND THEM TO BE SMOOTHER THAN 125 MICROINCHES RA & PERFORMED ROUGHNESS TEST ON INITIAL PARTS FOUND THEM TO BE SMOOTHER THAN 36 MICROINCHES RA AS PER B-737 SRM 51-20-13-0G-0<BR>TOOL USED: BC 172331. NO CALIBRATION DUE DATE<BR>TREATED AND PRIME REPAIR PARTS AND INITIAL PARTS AS PER B-737 AMM 51-21-41-370-803 & AMM 51-21-72-370-801.<BR>ACCOMPLISH INSTALLATION OF RIB #4 STIFFENER #3 REPAIR AS PER B-737 SRM<BR>55-10-09-2R-4 & SRM 51-40-02<BR>ACCOMPLISH SEALANT FINISH AS PER B-737 SRM 51-20-05-0G & AMM 51-20-99/701;[02] VERIFIED STEP 1.
Part: BULKHEAD — CRACKED (FWD CARGO) · airframe 52,102 hrs · 31,708 cycles
FWD CARGO FWD BULKHEAD PANEL 121LW HAS CRACK. 8-14<[01] REPAIRED DAMAGE AREA AT FWD BULHEAD PANEL 121LW AS PER SRM 51-70-04-2R-1. MATERIAL EY3804 PO 1759622 PLUS BMS9-3-7781 PO 1738579 .RESTORED ORIGINAL FINISHED AT FWD BULKHEAD PANEL 121LW AS PER AMM 51-21-99-300-802.;[02] VERIFIED STEP 1 <BR>C/W AUDIT PER MPM 52-02-02
Part: BULKHEAD — CRACKED (FWD CARGO) · airframe 52,102 hrs · 31,708 cycles
FWD CARGO FWD BULKHEAD PANEL 121JW HAS CRACK. 8-13<[01] APPLIED REPAIR TO DAMAGED AREA AT FWD CARGO FWD BULKHEAD PANEL 121JW PER B737 AMM 25-00-00-300-801 AND SUBTASK 25-00-00-020-001 MATERIALS USED PO# 1690463 AND PO# 2039827.;[02] VERIFIED CORRECTIVE ACTION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,102 hrs · 31,708 cycles
MULTIPLE PAX EMERGENCY LIGHT BATTERIES INOP<[01] PERFORMED TROUBLESHOOTING AS PER B737 AMM 33-51-00-710-801 AND SSM 33-51-13. FOUND M1670 EMERGENCY EXIT LIGHT BATTERY PACK DEFECTIVE.<BR>PERFORMED POWER SUPPLY - BATTERY PACK REPLACEMENT AT POSITION M1670 AS PER REF AMM 33-51-06-960-805. TEST FOUND NORMAL.;[02] VERIFIED STEP 1.;[03] AUDIT C/W PER MPM 52.02.02.
Part: PANEL — CORRODED (REFUEL) · airframe 52,102 hrs · 31,708 cycles
REFUEL PANEL (P15) FACE PLATE HAS SIGN OF CORROSION AROUND FUEL QTY GAUGES.<[01] REMOVED REFUEL PANEL (P15) AS PER B737 AMM TASK 28-21-00-000-801.<BR>INSTALLED EWIS PROTECTION FOR MAINTENACE AS PER B737 AMM TASK 20-60-07-913-801.<BR>REPLACED FACEPLATE/BRACKET ASSY AS PER B737 WDM 28-44-11 AND SPWM 20-10-11.<BR>REMOVED EWIS PROTECTION FOR MAINTENACE AS PER B737 AMM TASK 20-60-07-913-801.<BR>INSTALLED REFUELING PANEL P15 AS PER B737 AMM TASK 28-21-00-400-801.<BR>PERFORMED P15 REFUEL PANEL INSTALLATION TEST AS PER B737 AMM 28-21-00-400-801. TEST NORMAL<BR>PERFORMED REFUEL QUANTITY INDICATOR OPERATIONAL TEST AS PER B737 AMM 28-41-61-400-801.TEST NORMAL;[02] CORRECTION STEP 1<BR>REMOVED REFUEL PANEL (P15) AS PER B737 AMM TASK 28-21-00-000-801.<BR>INSTALLED EWIS PROTECTION FOR MAINTENACE AS PER B737 AMM TASK 20-60-07-913-801.<BR>REPLACED FACEPLATE/BRACKET ASSY AS PER B737 WDM 28-44-11 AND SPWM 20-10-11.<BR>REMOVED EWIS PROTECTION FOR MAINTENACE AS PER B737 AMM TASK 20-60-07-913-801.<BR>INSTALLED REFUELING PANEL P15 AS PER B737 AMM TASK 28-21-00-400-801.<BR>PERFORMED P15 REFUEL PANEL INSTALLATION TEST AS PER B737 AMM 28-21-00-400-801. TEST NORMAL;[03] VERIFIED STEP 2.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 52,102 hrs · 31,708 cycles
CRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90; 16' FROM FRONT SPAR; I/B ROW. LENGTH OF CRACK: 1'. CRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 16' FROM FRONT SPAR I/B ROW. LENGTH OF CRACK: 1'.<[01] COMPLETED SME INSPECTION OF WORKMANSHIP AND PAPERWORK AUDIT.;[02] SUMMARY<BR>REMOVED PAINT ON AREA FOR ACCESS REPAIR AS PER REF B/737 AMM 51-21-11-150-801.<BR>REMOVED PANEL #341BZ FOR ACCESS REPAIR AS PER REF B/737SRM 51-40-02-0G-0.<BR>REMOVED CRACK AT RIGHT H/STAB LOWER SKIN AT STA 193.90 AS PER REF B/737 SRM 55-10-01-2R-11 REPAIR 11.<BR>LOCATE AND DRILL AREA LOWER SIKIN AND REPAIR PART<BR>FABRICATED PARTS : DOUBLER 2024-T3 CLAD 0.080' PO#1763714 AND FILLER 2024 T-3 0.063 PO#1735552.PERFORMED ON CUT EDGE OF INITIAL PARTS FOUND SURFACE SMOOTHNESS 63 MICROINCHES RA AND MAKE ON CUT OF REPAIR PARTS AND INITIAL PARTS HAVE SURFACE SMOOTHNESS OF 125 MICROINCHES OF 125 RA AS PER REF B/737 SRM55-10-01-2R-11 REPAIR 11.USED TOOL B/C 1718555 NO DUE DATE.<BR>TREATED AND PRIMED AREA LOWER SKIN REPAIR AND REPAIR PARTS AS PER REF B/737 AMM 51-21-41-370-803.<BR>INSTALLED FILLER WASHERS ON REPAIR AREA PER B737-700 SRM 55-10-01-2R-11.<BR>INSTALLED REPAIR PARTS ON REWORKED AREA PER B737-700 SRM 55-10-01-2R-11 AND SRM 51-40-02-0G-0
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 51,960 hrs · 31,630 cycles
MID CABIN OVERHEAD EMERGENCY MID CABIN OVERHEAD EMERGENCY LIGHT AFT LIGHT PANEL CAME OFF<[01] RESECURED MID CABIN OVERHEAD EMERGENCY LIGHT LENS IAN AMM 33-51-01
Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 51,946 hrs · 31,621 cycles
FWD CARGO BIN AFT FLOOR PANEL HAS A CRACK.<[01] REPAIRED CARGO FLOOR PANEL PER AMM 25-52-01
2023
Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 50,391 hrs · 30,659 cycles
R/H OVERWING EMERGENCY EXIT LIGHT INOP / [01] R&R EMERGENCY LIGHT CHARGER ASSEMBLY AT POSITION M01669 PER AMM 33-51-06.
Part: SIGN — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 48,016 hrs · 29,136 cycles
CENTER CEILING EXIT SIGN FELL OFF<[01] LP1878487 AP3230074 REATTACHED LENS REF AMM 33-51-01
Part: GIRT BAR — OUT OF ADJUST · airframe 47,968 hrs · 29,106 cycles
FWD SERVICE DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED FWD SERVICE DOOR SLIDE GIRT IAW SIP
Part: GIRT BAR — OUT OF ADJUST · airframe 47,968 hrs · 29,106 cycles
FWD ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED FWD ENTRY SLIDE GIRT IAW SIP
2022
Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 46,444 hrs · 28,102 cycles
LH OVERWING EXIT DOOR INTERIOR LIGHT INOP / [01] RELAMPED LH OVERWING EXIT DOOR AND OPS CHECKED PER MM 33-21-00
Part: HANDLE — BROKEN (L1 DOOR) · airframe 46,047 hrs · 27,838 cycles
L1 ENTRY DOOR ASSIST HANDLE BROKEN. / [01] REMOVED ASSIST HANDLE FROM FWD LAV AND INSTALLED ON L1 DOOR REF AMM 25-40-11. FWD LAV ASSIST HANDLE OK TO CONTINUE PER MEL 25-10-01. SP1B AUTH 72341;[02] INSTALLED ASSIST HANDLE PER CMM 25-42-60. THIS CLEARS MEL 25-10-01.
Part: COVER — DETACHED (PAX CABIN) · airframe 46,035 hrs · 27,832 cycles
OVERHEAD EMERGENCY EXIT SIGN AT EMERGENCY EXIT ROW COVER CAME OFF / [01] SECURED EMERGENCY EXIT SIGN PER AMM STANDARD INDUSTRY PRACTICES
Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 45,998 hrs · 27,808 cycles
EXTERIOR EMERGENCY LIGHT AT R1 DOOR INOP. / [01] RE-LAMPED EXTERIOR EMERGENCY LIGHT AT R1 DOOR AND PERFORMED LAMP REPLACEMENT TEST AS PER B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED REPLACEMENT
Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 45,998 hrs · 27,808 cycles
R/H OVERWING DOOR WINDOW LIGHT INOP. / [01] RE-LAMPED R/H OVERWING DOOR WINDOW LIGHT AND PERFORMED LAMP REPLACEMENT TEST AS PER B737 AMM 33-21-00-960-801. TEST OK.;[02] VERIFIED REPLACEMENT
Part: LAMP — INOPERATIVE (PAX CABIN) · airframe 45,998 hrs · 27,808 cycles
R/H AFT OVERWING EMERGENCY LIGHT INOP. / [01] RE-LAMPED R/H AFT OVERWING EMERGENCY LIGHT AND PERFORMED LAMP REPLACEMENT TEST AS PER B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED REPLACEMENT
Part: STIFFENER — CRACKED (VAPOR BARRIER) · airframe 45,998 hrs · 27,808 cycles
STA 663.5 VAPOR BARRIER LOWER SECTION FOUND STIFFENER CRACKED AT RBL 25'. / [01] STARTED TO REMOVED STIFFENER AT VAPOR BARRIER STA 663.5 RBL 25' AS PER SRM 51-40-02-0G-0.;[02] REMOVED STIFFENER AT VAPOR BARRIER STA 663.5 RBL 25' AS PER SRM 51-40-02-0G-0.;[03] LOCATED AND DRILLED NEW STIFFENER AS PER SRM 51-40-05-0G-0.;[04] VERIFIED 3<BR>OK TO INSTALL;[05] INSTALLED STIFFENER AT STA 663.5 RBL 25 AS PER B737-700 SRM 51-40-02-OG-0 AND DRWG # 111A1000.;[06] VERIFIED AND INSPECTED STEP#5 STIFFENER INSTALLED AT STA 663.5 RBL 25.;[07] OK TO INSTALL CAP SEAL ON FASTENERS.;[08] CAP SEALED FASTENERS AS PER B737-700 SOPM 20-50-19;[09] REMOVED STIFFENER AT VAPOR BARRIER STA 663.5 RBL 25' AS PER SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW STIFFENER AS PER SRM 51-40-05-0G-0. INSTALLED STIFFENER AT STA 663.5 RBL 25 AS PER B737-700 SRM 51-40-02-OG-0 AND DRWG # 111A1000. CAP SEALED FASTENERS AS PER B737-700 SOPM 20-50-19.;[10] VERIFIED AND INSPECTED STEP#8 AND #9 FINAL: REMOVED STIFFENER AT VAPOR BARRIER STA 663.5 RBL 25' AS PER SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW STIFFENER AS PER SRM 51-40-05-0G-0. INSTALLED STIFFENER AT STA 663.5 RBL 25 AS PER B737-700 SRM 51-40-02-OG-0 AND DRWG # 111A1000. CAP SEALED FASTENERS AS PER B737-700 SOPM 20-50-19.
Part: LENS — MISSING (PAX CABIN) · airframe 45,998 hrs · 27,808 cycles
AFT LAVATORY EXIT SIGN LEN MISSING / [01] INSTALLED AFT LAVATORY EXIT SIGN LENS REF. BOEING 737-700 AMM 33-51-01-960-802;[02] VERIFIED INSTALLATION
Part: VAPOR BARRIER — CRACKED · airframe 45,998 hrs · 27,808 cycles
RH VAPOR BARRIER CRACKED / [01] MEASUREMENTS;[02] CLEANED DAMAGE AREA OF R/H VAPOR BARRIER FOR REPAIR; STOP DRILL CRACK ; PERFORMED DRY OUT ;FOUND NO WATER AS PER B737 SRM 51-70-04-2R-10;[03] VERIFIED STEPS 1 AND 2. OK TO APPLY REPAIR.;[04] REPAIRED CRACK DAMAGE ON R/H VAPOR BARRIER WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-10; MATERIALS USED PO#1690463 AND PO#1753794;[05] PERFORMED TAP TEST ON REPAIRED AREA OF VAPOR BARRIER; FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION (5).;[06] RII VERIFIED STEPS 4 AND 5 OK TO TOP COAT;[07] RESTORED FINISH TO R/H VAPOR BARRIER IAW B737-7 AMM=51-21-72-370-804 AND AMM=51-21-81-370-802 JOB ACCOMPLISHED BY ANASTACIO MENDOZA #2381;[08] SUMMARY=MEASUREMENTS CLEANED DAMAGE AREA OF R/H VAPOR BARRIER FOR REPAIR; STOP DRILL CRACK ; PERFORMED DRY OUT ;FOUND NO WATER AS PER B737 SRM 51-70-04-2R-10 REPAIRED CRACK DAMAGE ON R/H VAPOR BARRIER WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-10; MATERIALS USED PO#1690463 AND PO#1753794 RESTORED FINISH TO R/H VAPOR BARRIER IAW B737-7 AMM=51-21-72-370-804 AND AMM=51-21-81-370-802 JOB ACCOMPLISHED BY ANASTACIO MENDOZA #2381;[09] VERIFIED STEP 7;CARD COMPLETED
Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 45,998 hrs · 27,808 cycles
CRACK FOUND AT LEFT HAND HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90 ; I/B ROW ; 16' FROM REAR SPAR. CRACK LENGTH 0.906' CRACK FOUND AT LEFT HAND HORIONTAL STABILIER LOWER SKIN STAB STA 193.90 I/B ROW 16' FROM REAR SPAR. CRACK LENGTH 0.906' / [01] REMOVED PANEL#331 BZ FOR ACCESS REPAIR CRACK AT LEFT HAND HORIZONTAL STAB LOWER SKIN STAB STA 193.90 I/B ROW 16' FROM SPAR IAW B737 SRM 51-40-02-0G-0.[22] SUMMARY:REMOVED PANEL#331 BZ FOR ACCESS REPAIR CRACK AT LEFT HAND HORIZONTAL STAB LOWER SKIN STAB STA 193.90 I/B ROW 16' FROM SPAR IAW B737 SRM 51-40-02-0G-0. REMOVED PAINT FOR ACCESS FASTENERS LOWER SKIN ON AREA .INSTALLED REPAIR AT LEFT HAND HORIZONTAL STAB LOWER SKIN STA 193.90;I/B ROW 16' FROM SPAR IAW B737 SRM 55-1-0102R-11 REPAIR 11 FIG 204 DETAIL B. REPAIR AT LEFT HAND H/STAB STA 193.90' I/B ROW 16 'FROM REAR SPAR IAW B737 AMM 51-21-11-150-801. . FABRICATED FILLER OF REPAIR .MATERIAL USED 2024 T3 0.063 CLAD PO1735552.AND DRILLED IAW B737 SRM 55-10-01 2R 11 REPAIR 11.INSTALLED REPAIR AT LEFT HAND HORIZONTAL STAB LOWER SKIN STA 193.90;I/B ROW 16' FROM SPAR IAW B737 SRM 55-1-0102R-11 REPAIR 11 FIG 204 DETAIL B. INSTALLED PANEL #331BZ FROM L/H HORIZONTAL
2021
Part: HANDLE — BROKEN (L1 DOOR ASSIST) · airframe 43,885 hrs · 26,520 cycles
L1 DOOR WILL NOT OPEN CORRECTLY ASSIST HANDLE BROKEN ; L1 DOOR WILL NOT OPEN AND ASSIST HANDLE BROKEN / [01] REPLACED GUIDE ARM AND DOOR ASSIST HANDLE PER MM 52-11-21
Part: ROLLER — CRACKED (R2 DOOR) · airframe 42,239 hrs · 25,583 cycles
AFT SERVICE DOOR GUIDE ROLLER CRACKED. / REMOVED AND REPLACED PER AMM 52-41-21.
2020
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 40,823 hrs · 24,698 cycles
FWD SERVICE DOOR EMERGENCY EXIT LOCATOR SIGN HAS SEVERAL LIGHTS OUT. RELAMPED FWD SERVICE DOOR EMERGENCY EXIT LOCATOR SIGN AND PERFORMED GOOD FUNCTIONAL TEST AS PER AMM 33-51-01-960-801.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,823 hrs · 24,698 cycles
EMERGENCY EXIT LIGHT L1189 FORWARD OF LT OWE HAS BULBS OUT. RELAMPED EMERGENCY EXIT LIGHT L1189 AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-01-960-801.
Part: LIGHT — NOT SEATED (CABIN) · airframe 40,823 hrs · 24,698 cycles
RT OVERWING ESCAPE GROUND EMERGENCY EXIT LIGHT L548 BULB IS OUT. RESEATED RT OVERWING ESCAPE GROUND EMERGENCY EXIT LIGHT L548 AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-04-960-801.
Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 40,823 hrs · 24,698 cycles
FWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / LOCATED AND DRILLED NEW FWD CARGO BAY FWD CORNER SCUFF PLATE PO #784955/1 IAW SRM 51-40-05. OK TO INSTALL 88918C 29JUN20 INSP 86 29JUN20. INSTALLED FWD CARGO BAY FWD CORNER SCUFF PLATE IAW AMM 53-11-02-420-801
Part: SCUFF PLATE — BROKEN (AFT CARGO) · airframe 40,823 hrs · 24,698 cycles
AFT CARGO DOOR SCUFF PLATE FWD CORNER HAS BROKEN FLANGE / LOCATED AND DRILLED NEW AFT CARGO DOOR SCUFF PLATE FWD CORNER IAW SRM 51-40-05. OK TO INSTALL 88928C 29JUN20 INSP 86 29JUN20. INSTALLED AFT CARGO DOOR SCUFF PLATE FWD CORNER IAW AMM 53-11-02-420-801
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
CORROSION ON INTERCOSTAL AT PASSENGER CABIN BS 294 - BS312 LBL12 WL208. REMOVED & REPLACED INTERCOSTAL AT BS 294-312 LBL12 WL208 IAW SRM 51-40-02 & REF DWG 141A5600.
Part: SKIN — GOUGED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
FUSELAGE SKIN HAS A GOUGE AT BS 847+4.5' STR 1. FUSELAGE SKIN GOUGE AT BS 847+4; STR 1 WAS REPAIRED IAW ATS ER 20-02766 REV IR RATED 30JUN20 AND EA 20-153-00953 REV IR.
Part: SKIN — GOUGED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
FUSELAGE SKIN HAS A GOUGE AT BS 847+6.5'; .8' BELOW S-1L. DAMAGE REPAIRED PER EA 20-153-00953 REV IR (ATS ER 20-02766 REV IR) REFER TO NRC U181821 FOR TRACKING.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,823 hrs · 24,698 cycles
AFT CABIN FLOOR PANEL 242VF HAS DAMAGED UPPER SURFACE SKIN. REPAIRED DAMAGE TO PANEL 242VF UPPER SURFACE IAW SRM 53-00-50-2R-1.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,823 hrs · 24,698 cycles
FWD CABIN FLOOR PANEL 222DF HAS DAMAGED INSERTS ON THE FWD O/B EDGE. DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 222DF WITH NEW PANEL IAW SRM 51-10-02-0G-0 PAR 9A(1) AND AIPC 53-21-51-21L.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,823 hrs · 24,698 cycles
FWD CABIN FLOOR PANEL 222BF HAS DAMAGED UPPER SURFACE SKIN. FWD CABIN FLOOR PANEL 222BF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9A.(1).
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,823 hrs · 24,698 cycles
FWD CABIN FLOOR PANEL 221AF HAS DAMAGE UPPER SURFACE SKIN. FWD CABIN FLOOR PANEL 221AF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9A.(1).
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,823 hrs · 24,698 cycles
FWD CABIN FLOOR PANEL 221BF HAS DAMAGE UPPER SURFACE SKIN. DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 221BF WITH NEW PANEL IAW SRM 51-10-02-0G-0 PAR 9A(1) AND AIPC 53-21-51-21L.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,823 hrs · 24,698 cycles
FWD CABIN FLOOR PANEL 221DF HAS DAMAGE UPPER SURFACE SKIN. RECEIVED NEW FLOORBOARD P/N 141A5810-235; SI# 7532003. FLOORBOARD WILL BE INSTALLED ON CARD JPANEL-221-CLOSE.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,823 hrs · 24,698 cycles
PASSENGER CABIN FLOOR PANEL 241MF DAMAGED ON BACK SIDE OF PANEL. DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW PASSENGER CABIN FLOOR PANEL 241MF USING BMS 4-23 TY2 LOT 1428456-1; INSTALLED INSERTS USING BMS 5-107 LOT AK9GP5303K; APPLIED TAPE TO LOWER SURFACE AND PART MARKED IAW SRM 53-00-50-2R-0 PARA 1A(NOTE) AND DWG 146A5810-503.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,823 hrs · 24,698 cycles
PASSENGER CABIN FLOOR PANEL 242DF DAMAGED ON EDGE OF PANEL. DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW PASSENGER CABIN FLOOR PANEL 242DF USING BMS 4-23 TY2 LOT 1428456-1; INSTALLED INSERTS USING BMS 5-107 LOT AK9GP5303K; APPLIED TAPE TO LOWER SURFACE AND PART MARKED IAW SRM 53-00-50-2R-0 PARA 1A(NOTE) AND DWG 144A5810-123.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,823 hrs · 24,698 cycles
AFT CABIN FLOOR PANEL 241AEF HAS DAMAGED UPPER SURFACE SKIN. REPAIRED DAMAGE TO UPPER SURFACE OF FLOOR PANEL 241AEF IAW SRM 53-00-50-2R-1.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,823 hrs · 24,698 cycles
AFT CABIN FLOOR PANEL 242RF HAS DAMAGED LOWER SURFACE SKIN. DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 242RF; REPLACED WITH NEW PANEL IAW SRM 51-10-02-0G-0 PARA 9; & AIPC 53-21-00-26 ITEM 35.
Part: BULKHEAD — DELAMINATED (LT MLG WW) · airframe 40,823 hrs · 24,698 cycles
BS 663 LOWER COMPOSITE BULKHEAD IS SEPARATING AT PREVIOUS REPAIR AT LBL 38; WL 150. BS 663 LOWER COMPOSITE BULKHEAD WAS REPAIRED IAW SRM 51-70-04-2R-10.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,823 hrs · 24,698 cycles
FWD CABIN FLOOR PANEL 221FF HAS DAMAGE UPPER SURFACE SKIN. FWD CABIN FLOOR PANEL 221FF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9A.(1).
Part: STRAP — CORRODED (BS 794-810) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB DOOR SURROUND STRUCTURE LWR STRAP CORROSION; BS794 TO BS810; RBL19.5; WL156. / REMOVED AND REPLACED STRAP LOCATED ACB DOOR SURROUND STRUCTURE LWR B/S 767 TO B/S 86 + RBL19.5 WL156 PO: 778979 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 146A8120 REV: A
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
CORROSION ON INNER CHORD AT PASSENGER CABIN BS685 - BS727 RBL63 WL208. CORROSION ON INNER CHORD AT BS 685 - BS 727; RBL 63; WL 208 WAS REPAIRED IAW ATS ER 20-02761 REV IR DATED 02JUN2020 AND EA 20-153-00976 REV IR.
Part: CARGO TRACK — CORRODED (BS 787-790) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB TIE DOWN TRACK CORROSION IN WELL BS787 TO BS790; LBL17. / REMOVED CORROSION ACB TIE DOWN TRACK IN WELL B/S787 TO B/S790; LBL17; IAW SRM 53-00-53-1A-2 AND PROTECTIVE TREATMENT APPLIED IAW SRM 51-20-01 59899U 18/06/20
Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB TRACK RBL13; BS942.5 TO BS935 AT FASTENER HOLES. / REMOVED AND REPLACED ACB TRACK BS 887-947 RBL 13 P/N 7530159 PO #784853 IAW SRM 51-40-02 REF. DWG 147A7500 89004U 22JUN20
Part: STRAP — CORRODED (AFT CARGO) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB FLOOR T STRAP; BS887; LBL9 TO RBL21. WL 156. / REMOVED AND REPLACED NEW/SERVICABLE ACB FLOOR T-STRAP AT BS887 LBL9 TO RBL21; WL156 PER SRM #51-40-02-0G-0 AND AIPC #55-92-11-30 57609U 25JUN20
Part: NUT PLATE — CORRODED (AFT CARGO) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB NUT PLATE STRIP LWR SURFACE; BS 794.5 TO BS807; RBL19.5; WL156. / REMOVED AND REPLACED NUT PLATE STRIP; B/S 794.5 TO B/S 807; RBL 19.5; WL 156 PO: 787531/11 IAW SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9 AND DWG 146A8340 REV: 59900U 19JUN20
Part: CARGO TRACK — CORRODED (BS 867) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB TIE DOWN TRACK CORROSION IN WELL; BS867; LBL3. / REMOVED CORROSION ACB TIE DOWN TRACK IN WELL B/S867; LBL3 IAW SRM 53-00-53-1A-2 AND PROTECTIVE TREATMENT APPLIED IAW SRM 51-20-01 59899U 18/06/20
Part: SUPPORT — CORRODED (AFT CARGO) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB FLOOR TO SIDEWALL SUPPORT RBL21; BS727D TO BS767. / REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT LOCATED RBL21; B/S 727D TO B/S 767 PO: 789433/1 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 146A7500 REV:- 59900U 16JUN20
Part: WEB — CORRODED (BS 794-847) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB DOOR SURROUND STRUCTURE LWR SILL WEB; BS794 TO BS847; RBL24; WL156. / REMOVED AND REPLACED SILL WEB B/S 794 TO B/S 847 RBL24; WL156 IAW SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 AND DWG 146A8340 REV: 59900U 20JUN20
Part: CARGO TRACK — CORRODED (BS 887-947) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB RAIL LBL3; BS942.5 TO BS935. / REMOVED AND REPLACED NEW ACB RAIL LBL3 BS887 TO BS947 ITEM 7530392 PO #779084 IAW SRM 51-40-02 SRM 51-40-03 AND SRM 58-70-53-01-2; DWG 147A7500 80641U 17JUN20
Part: SUPPORT — CORRODED (AFT CARGO) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB FLOOR TO SIDEWALL SUPPORT LBL21; BS727B TO BS787 / REMOVED AND REPLACED ON ACB FLOOR TO SIDEWALL SUPPORT LBL21 BS 727-BS847. ITEM 7532037 PO #795658. IAW SRM 51-40-02; SRM 51-40-05. SRM 53-60-53-01-2; SRM 53-00-53-1A-2 AND DWG 146A7500 80641U 22JUN20
Part: SUPPORT — CORRODED (BS 947 LBL9) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB; AFT LOWER CENTER BULKHEAD SUPPORT. BS947; LBL9 TO RBL23; WL156 / REMOVED AND INSTALLED ACB NEW LOWER CENTER BULKHEAD SUPPORT; B/S 947; LBL 9 TO RBL 23 WL 156 P/N 149A8118-29 PO #792279/1 IAW SRM 51-40-02 AND DWG 149A8117 REV- 59899U 18-06-20
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 40,823 hrs · 24,698 cycles
CORROSION ACB RBL14 TRACK CORROSION; BS794 TO BS847 WL157. REMOVED AND REPLACED ACB TRACK BS727 TO BS887 RBL14 WL157 IAW SRM 51-40-02 REF DWG 146A7500. INSTALLED REPAIR SPLICE AT BS 747+8 RBL14 WL157 IAW SRM 53-00-53-2R-3.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
ACB LWR BULKHEAD SUPPORT ANGLE CRACKED IN RADIUS . BS866.5; LBL10; WL165. / REMOVED AND REPLACED SUPPORT ANGLE LOCATED B/S 866.5 LBL10 WL165 PO:791844/2 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 149A8104 REV:B 59900U 13JUN20
Part: GUSSET — CRACKED (FWD CARGO) · airframe 40,823 hrs · 24,698 cycles
FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / REMOVED DAMAGED GUSSET AND INSTALLED NEW GUSSET AT BS 500D S-19L WL193 IAW SRM 51-40-02-0G-0 AND DWG 142A7902.
Part: GUSSET — CRACKED (FWD CARGO) · airframe 40,823 hrs · 24,698 cycles
FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / REMOVED DAMAGED GUSSET AND INSTALLED NEW GUSSET AT BS 500D S-19R WL 193 IAW SRM 51-40-02-0G-0 AND DWG 143A7902
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
CRACKED PASSENGER CABIN FLOOR PANEL SUPPORT BS540 RBL3 WL208. REMOVED AND INSTALLED NEW PASSENGER CABIN FLOOR PANEL SUPPORT AT BS 540 RBL 3 WL 208 ITEM 7530909 IAW SRM 51-40-02-0G-0; AIPC 53-42-11-66.
Part: WEB — CORRODED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS440 - BS493 RBL28 WL156. REMOVED AND INSTALLED NEW SUBTHRESHOLD WEB AT FWD CARGO BAY BS 440-BS 493 RBL 28 WL 156 ITEM 7530597 IAW SRM 53-30-15-01-1; SRM 53-30-15-1A-1; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 143A8122; DWG 143A8330.
Part: SHIELD — CORRODED (FWD CARGO) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL23 WL156. / REMOVED AND REPLACED NEW ON FWD SHIELD AT FWD CARGO BAY BS 420-BS 440 RBL23 ITEM 7530143 PO #787952 IAW SRM 51-40-03; SRM 51-40-02 AND DWG 143A0080 80641U 19JUN20
Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL156. / REMOVED AND INSTALLED FLOOR TO SIDEWALL SUPPORT AT FCB BS500A-BS500D RBL23 NEW FROM BDE1496-449 & 7075T62 CLAD LOT #1431953-1 IAW SRM 51-40-02; SRM 51-20-01; SRM 53-30-53-01-2; DWG 143A7501 AND DWG 143A7500 80643U 22JUN20
Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
CRACKED INTERCOSTAL ANGLE AT PASSENGER CABIN BS380 - BS400 RBL9 WL208. REMOVED AND REPLACED ANGLE AT INTERCOSTAL PASSENGER CABIN BS 380-BS 400 RBL 9 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A5400.
Part: SHIELD — CORRODED (FWD CARGO) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ON AFT SHIELD AT FWD CARGO BAY BS495 - BS500A RBL23 WL156. / REMOVED AND REPLACED NEW ON AFT SHIELD AT FCB BS 495-BS 500A RBL 23 IAW SRM 51-40-05; SRM 51-40-02 AND DWG 143A0080 80641U 19JUN20
Part: INTERCOSTAL — BENT (BS 480-500 S25L) · airframe 40,823 hrs · 24,698 cycles
BENT INTERCOSTAL AT FWD CARGO BAY BS480- BS500 S-25L WL158. / REMOVED AND REPLACED INTERCOSTAL AT FCB BS 480-BS 500 S-25L WL 158 IAW SRM 51-40-02-0G-0 DWG 143A7550 59205U 20JUN20
Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
CRACKED INTERCOSTAL ANGLE AT PASSENGER CABIN BS380 - BS400 BL0 WL208. REMOVED AND REPLACE ANGLE AT INTERCOSTAL PASSENGER CABIN BS 380-BS 400 BLO WL 208 IAW SRM 51-40-02-0G-0 DWG 143A5400.
Part: SHIELD — CORRODED (AFT CARGO) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB FWD SHIELD; BS767 TO BS787; RBL 21. / REMOVED AND REPLACED SHIELD; B/S 767 TO B/S 787 RBL21 PO: 774635/1 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 146A0081 REV. A 59900U 16JUN20
Part: SUPPORT — CORRODED (BS 767-787) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB INTERCOSTAL ANGLE COMMON TO FWD SHIELD; LWR SURFACE; AT NUTPLATE LOCATIONS. BS767 TO BS787; RBL22; WL156 / REMOVED AND REPLACED INTERCOSTAL ANGLE COMMON TO FWD SHIELD; B/S 767 TO B/S 787 RBL22 WL156 PO: 760495/4 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 146A0081 REV: A 59900U 17JUN20
Part: GUSSET — CRACKED (FWD CARGO) · airframe 40,823 hrs · 24,698 cycles
FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-21L WL193. MARKED / REMOVED DAMAGED GUSSET AND INSTALLED NEW GUSSET AT BS 500D S-21L WL 193 IAW SRM 51-40-02-0G-0 AND DWG 143A7902
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
CRACKED INTERCOSTAL AT PASSENGER CABIN BS500D - BS520 BL0 WL208. REMOVED AND REPLACED PASSENGER CABIN INTERCOSTAL AT BS 500D - BS 520 BLO WL 208 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A5400.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FCB BS500D RBL23 TO LBL23 WL156. MARKED / REMOVED AND REPLACED FCB AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS 500D DUE TO NO ALLOWABLE LIMITS FOUND IN THE SRM FOR THIS ITEM IAW SRM 51-40-02 AND DWG #143A9481
Part: CARGO TRACK — CORRODED (BS 747) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ACB TRACK TIE DOWN CORROSION IN WELL; BS747; LBL17. / REMOVED CORROSION ACB TRACK TIE DOWN IN WELL; B/S747 LBL17 IAW SRM 53-00-53-1A-2 AND PROTECTIVE TREATMENT APPLIED IAW SRM 51-20-01 59899U 18/06/20
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
CRACKED INTERCOSTAL ANGLE AT PASSENGER CABIN BS380 - BS400 LBL13 WL208. REMOVED AND REPLACED ANGLE AT INTERCOSTAL PASSENGER CABIN BS 380-BS 400 LBL 13 WL 208 IAW SRM 51-40-02-0G-0 DWG 143A5400.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS460 - BS500D LBL23 WL156. REMOVED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT FCB BS 400-BS 500D LBL 23 IAW SRM 51-40-02; SRM 53-00-53-2R-5; SRM 51-20-01 AND DWG 143A7500.
Part: BEAM — CRACKED (R1 DOOR) · airframe 40,823 hrs · 24,698 cycles
DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR NR 4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. FORWARD SERVICE DOOR NR 4 (LOWER) BEAM WAS REMOVED & REPLACED ON WORK ORDER: 533613.
Part: BEAM — CRACKED (R1 DOOR) · airframe 40,823 hrs · 24,698 cycles
DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR NR 5 (UPPER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. FORWARD SERVICE DOOR NR 5 (UPPER) BEAM WAS REMOVED & REPLACED ON WORK ORRDER:533613.
Part: SUPPORT ANGLE — CORRODED (BS 620 LBL 60) · airframe 40,823 hrs · 24,698 cycles
***CORROSION*** ON SCUFF PLATE SUPPORT ANGLE AT PASSENGER CABIN BS320 LBL60 WL208. MARKED / REMOVED AND REPLACED SCUFF PLATE SUPPORT ANGLE AT PASSENGER CABIN FROM BS 320 TO BS 344 LBL 60 WL 208 IAW SRM 51-40-02 AND DWG 141A8110
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
CRACKED INTERCOSTAL AT PASSENGER CABIN BS344 - BS360 RBL11 WL208. REMOVED AND REPLACED INTERCOSTAL AT PASSENGER CABIN BS 344-BS 360 RBL 11 WL 208 IAW SRM 51-40-02-0G-0 DWG 141A5400.
Part: BOOT — DAMAGED (RADOME) · airframe 40,823 hrs · 24,698 cycles
NOSE RADOME BOOT IS DAMAGED / REMOVED RADOME BOOT IAW AMM 53-52-00-000-802 TAP TESTED. NO DISBONDS NOTED IAW SRM 51-10-06-0G-0 PARA 5&7 13742C 06-12-20 INSP 357 JUN 12 2020 INSTALLED NEW NOSE RADOME PROTECTIVE BOOT IAW AMM 53-52-00-400-802 PAR 5.E(1)-(14). 6645U 06/17/20
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
CRACKED INTERCOSTAL AT PASSENGER CABIN BS344 - BS360 BL0 WL208. REMOVED AND REPLACED INTERCOSTAL AT PASSENGER CABIN BS 344- BS 360 BLO WL 208 IAW SRM 51-40-02-0G-0 DWG 141A5400.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
CRACKED INTERCOSTAL AT PASSENGER CABIN BS312 - BS328 RBL30 WL208. REMOVED AND REPLACED INTERCOSTAL AT PASSENGER CABIN BS 312-BS 328 RBL 30 WL 208 IAW SRM 51-40-02-0G-0 DWG 141A5400.
Part: SKIN — DENTED (LT HORIZ STAB) · airframe 40,823 hrs · 24,698 cycles
DENT ON LEFT HORIZONTAL STAB UPPER SKIN 9.5' FROM FRONT SPAR; STAB STA226. DENT ON LEFT HORIZONTAL STAB UPPER SKIN 9.5' FROM FRONT SPAR STAB STA 226 REPAIRED IAW ATS ER 20-02742; REV IR; DATED 06-JUL-2020 AND PER EA NO: 20-155-01022 REV IR.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 40,823 hrs · 24,698 cycles
CRACKED SUPPORT ANGLE AT PASSENGER CABIN JUST FWD OF FWD SERVICE DOOR BS293 RBL54 WL208. REMOVED AND REPLACED SUPPORT ANGLE AT PASSENGER CABIN FWD SERVICE DOOR BS 293 RBL 54 WL 208 IAW SRM 51-40-02-09-0 DWG 141A8310.
Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 40,823 hrs · 24,698 cycles
LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STATION 120.30; 2ND VERTICAL STIFFENER IS CRACKED. REMOVED THE DAMAGE PART INSTALLED REPAIR PARTS AT LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.30 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4.
Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 40,823 hrs · 24,698 cycles
BS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT LBL 10 WL 164. REPAIRED LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE PER SRM 57-10-10-2R-5; ACCOMPLISH CAP SEAL AT FASTENER ON W/O 2011M513.
Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 40,823 hrs · 24,698 cycles
LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STATION 120.30; 3RD VERTICAL STIFFENER IS CRACKED. REMOVED THE DAMAGED PART AND INSTALLED REPAIR PARTS AT LEFT HAND HORIZONTAL STABILIZER INSPAR RIB STAB STA 120.30 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-5 88920U 18JUN20.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 40,823 hrs · 24,698 cycles
LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STATION 120.30; 4TH VERTICAL STIFFENER IS CRACKED. REMOVED THE DAMAGE PART AND INSTALLED REPAIR PARTS AT LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.30 4TH VERTICAL STIFFENER IAW SRM 55-10-09-2R-5.
Part: STRUCTURE — DENTED (COCKPIT) · airframe 40,823 hrs · 24,698 cycles
FLIGHT DECK FLOOR IS DENTED AT BS 255 RBL 4 - LBL 14 WL 207.54. ACCOMPLISHED FLIGHT DECK FLOOR REPAIR AT BS 255 RBL-4. LBL 14; WL 207.54 IAW EA 1-A53-33179 REV 1 DATED 28-MAY-19.
Part: SKIN — CRACKED (LE SLAT) · airframe 40,823 hrs · 24,698 cycles
NR 3 SLAT LOWER SKIN CRACKED ACTUATOR RIB ATTACHMENT FASTENER HOLE. TRIMMED OUT THE DAMAGE PART OF NR 3 SLAT LWR SKIN AT ACTUATOR RIB ATTACHMENT AND INSTALLED REPAIR PARTS IAW SRM 57-42-01-2R-8.
2019
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 38,298 hrs · 23,079 cycles
CENTER CABIN OVERHEAD EMERGENCY EXIT SIGN AFT LENS FELL OFF. / SECURED LENS PER SIP.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,186 hrs · 23,014 cycles
L/H EMERGENCY OVERWING ESCAPE GROUND LIGHT INOP. R&R BATTERY PACK IAW AMM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,186 hrs · 23,014 cycles
L/H EMERGENCY OVERWING ESCAPE LIGHT INOPERATIVE. R&R BATTERY PACK IAW AMM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,186 hrs · 23,014 cycles
EMERGENCY OVERWING AISLE LIGHT INOP. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,186 hrs · 23,014 cycles
R/H EMERGENCY OVERWING ESCAPE GROUND LIGHT INOP. R&R BATTERY PACK IAW AMM.
Part: BATTERY — FAILED (CABIN) · airframe 37,969 hrs · 22,877 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1674. R&R BATTERY PER AMM.
Part: BATTERY — FAILED (CABIN) · airframe 37,969 hrs · 22,877 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1675. R&R BATTERY PER AMM.
Part: BATTERY — FAILED (CABIN) · airframe 37,969 hrs · 22,877 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1668. R&R BATTERY PER AMM.
Part: BATTERY — FAILED (CABIN) · airframe 37,969 hrs · 22,877 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1672. R&R BATTERY PER AMM.
Part: BATTERY — FAILED (CABIN) · airframe 37,969 hrs · 22,877 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1669. R&R BATTERY PER AMM.
Part: BATTERY — FAILED (CABIN) · airframe 37,969 hrs · 22,877 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1670. R&R BATTERY PER AMM.
Part: SUPPORT FRAME — CRACKED (LWR FUSELAGE) · airframe 37,969 hrs · 22,877 cycles
LT WING TO BODY PNL 191AL SUPPORT FRAME CRACKED / R/R LT WING TO BODY PNL 191AL SUPPORT FRAME PER SRM 51-40-02
Part: BATTERY — FAILED (CABIN) · airframe 37,969 hrs · 22,877 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1673. R&R BATTERY PER AMM.
Part: LIGHT — LOOSE (CABIN) · airframe 37,356 hrs · 22,485 cycles
RT EMERGENCY EXIT INSIDE OVERHEAD BIN BULB ASSEMBLY LOOSE. SECURED LIGHT IAW AMM.
Part: LENS — MISSING (CABIN) · airframe 37,356 hrs · 22,485 cycles
RT EMERGENCY EXIT LIGHT LENS COVER MISSING AT ROW 6. INSTALLED LENS IAW AMM.
Part: SLIDE — UNSECURE (L1 DOOR) · airframe 36,264 hrs · 21,754 cycles
L1 DOOR EVAC SLIDE PARTIALLY FELL OUT OF CONTAINER, (DID NOT DEPLOY). REINSTALLED SLIDE ASSY PER MM.
2018
Part: HOLDER — OUT OF ADJUST (R1 DOOR) · airframe 35,912 hrs · 21,524 cycles
R1 DOOR GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR HOLDER PER AMM.
Part: COVER — MISSING (EXIT SIGN) · airframe 35,016 hrs · 20,916 cycles
R1 DOOR LOWER EMERGENCY EXIT SIGN MISSING DIRECTIONAL ARROW. R&R SIGN PER AMM.
Part: FLOOR PANEL — BROKEN (CABIN) · airframe 34,892 hrs · 20,833 cycles
FWD WET AREA FLOOR PANEL 221BF IS BROKEN. / REMOVED AND REPLACED FLOOR PANEL # 221 BF PER AMM 53-21-00.
Part: FLAP — DELAMINATED (RH INBD MAIN FLA) · airframe 34,892 hrs · 20,833 cycles
RIGHT WING INBD MAIN FLAP WEDGE IS DELAMINATED. / REMOVED AND REPLACED RT INBD FLAP WEDGE PANEL PER SRM 51-40-02
Part: PANEL — CRACKED (RIGHT WING) · airframe 34,892 hrs · 20,833 cycles
RH WING PANEL 621YB HAS A CRACKED CORNER / REPAIRED PER SRM 51-70-05. REPAIRED FOIL PER SRM 51-70-14. RESTORED FINISH PER MM 51-21-99.
Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 34,892 hrs · 20,833 cycles
AFT CARGO FLOOR SPLICE STRIP HAS CORROSION STA. 767+4. / REPLACED AFT CARGO FLOOR SPLICE STRIP AT STA. 767+4 PER SRM 51-40-02.
Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 34,892 hrs · 20,833 cycles
AFT CARGO FLOOR PANEL SPLICE STRIP AT STA 727D+6 HAS CORROSION. / REPLACED AFT CARGO FLOOR PANEL SPLICE STRIP AT STA 727D+6 PER SRM 51-40-02.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,892 hrs · 20,833 cycles
L1 DOOR Z ANGLE CRACKED ON VERTICAL LEG STA 303.9, AT FASTENER HOLE. REPAIRED Z ANGLE PER EA.
Part: FAIRING — CRACKED (RIGHT WING) · airframe 34,892 hrs · 20,833 cycles
#6 CANOE HAS A CRACK ON INSIDE BOTTOM AREA / ACCOMPLISHED REPAIR TO #6 CANOE REF EA 1-A57-6168. SEE NON-ROUTINE FOR INDIVIDUAL SIGN OFFS
Part: FAIRING — ELONGATED (LEFT WING) · airframe 34,892 hrs · 20,833 cycles
FASTENER HOLES ENLARGED ON #3 CANOE AT INBOARD SIDE MIDDLE BULB SEAL SEGMENT. (REF INBOUND MTSI-6431) / REMOVED DAMAGE TO FASTENER HOLES AND ACCOMPLISHED REPAIR REF SRM 57-53-70-2R-2 ALTERNATIVE 2.
Part: SUPPORT — ELONGATED (FLIGHT DECK) · airframe 34,892 hrs · 20,833 cycles
ELONGATED NUT PLATE HOLE COMMON TO COCKPIT FLOOR ACCESS PLANE # 211AF AT RBL2 SUPPORT STRUCTURE REF. P/N141A5210. / REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL COMMON TO COCKPIT FLOOR ACCESS PANEL #211AF PER SRM 51-40-02.
Part: STIFFENER — ELONGATED (FLIGHT DECK) · airframe 34,892 hrs · 20,833 cycles
ELONGATED NUT PLATE HOLE COMMON TO COCKPIT FLOOR ACCESS PLANE # 211AF AT LBL11 STIFFENER P/N141A5210. / STIFFENER @ STA 270 LBL 11 WAS REPLACED ON N/R G575778. NEW SCREW HOLE AND NUT PLATE WHERE LOCATED AND INSTALLED ON NEW STIFFENER PER SRM 51-40-02
Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 34,892 hrs · 20,833 cycles
CENTER WING SECTION FLOORBOARD NUTPLATE SUPPORT CHANNEL CRACKED AT BS 539, LBL 1. R&R CHANNEL IAW SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,892 hrs · 20,833 cycles
SEAT TRACK LOWER CROWN CORRODED BETWEEN BS 651 TO BS 727A+8, RBL 45.5. R&R SEAT TRACK ASSEMBLY PER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,892 hrs · 20,833 cycles
SEAT TRACK LOWER CROWN CORRODED BETWEEN BS 667 TO BS 727A+8, RBL 24.75. REPAIRED SEAT TRACK PER SRM.
Part: FAIRING — CRACKED (LEFT WING) · airframe 34,892 hrs · 20,833 cycles
#3 CANOE HAS A SMALL CRACK ON THE INSIDE SURFACE / REPAIRD PER E/A 1-A57-6168.
Part: PLATE — CRACKED (RIGHT WING) · airframe 34,892 hrs · 20,833 cycles
RIGHT WING; WIGGLE PLATE I/B OF #6 FLAP TRACK; CRACKED / REPLACED RIGHT WING; WIGGLE PLATE I/B OF #6 FLAP TRACK PER SRM 51-40-02.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,892 hrs · 20,833 cycles
SEAT TRACK LOWER CROWN CORRODED BETWEEN BS 663 TO BS 738, LBL 45.5. REPAIRED SEAT TRACK PER SRM.
Part: PLATE — CRACKED (LEFT WING) · airframe 34,892 hrs · 20,833 cycles
LEFT WING WIGGLE PLATE I/B OF #3 FLAP TRACK CRACKED AT O/B FASTENER / R & R WIGGLE PLATE PER SRM 51-40-02.
Part: FLOOR PANEL — DENTED (FLIGHT DECK FLOO) · airframe 34,892 hrs · 20,833 cycles
FLIGHT COMPARTMENT FLOOR AT STA 256 HAS SEVERAL DENTS AND CREASES FROM LBL16 TO RBL 7 / CUT OUT DAMAGE AREA. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS PER EA#1-753-33009.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,892 hrs · 20,833 cycles
SEAT TRACK LOWER CROWN CORRODED BETWEEN BS 727D+7 TO BS 727E+5, LBL 45.5. R&R SEAT TRACK ASSEMBLY PER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,892 hrs · 20,833 cycles
LOWER CROWN SEAT TRACK CORRODED BETWEEN BS 727B+17 TO BS 727C+14, LBL 45.5. R&R SEAT TRACK ASSEMBLY PER SRM.
Part: ACCESS PANEL — ELONGATED (LT WING) · airframe 34,892 hrs · 20,833 cycles
PANEL 553DT NEEDS TO BE REPLACED FOR ELONGATED HOLE / DRILLED UP NEW PANEL PER SRM 51-40-02. COUNTERSUNK NEW PANEL PER SRM 51-40-080G-0 AND REFINISHED NEW PANEL PER MM 51-21-00. PANEL WILL BE INSTALLED ON SWA ROUTINE CARD PANEL-550-CLOSE.
Part: STIFFENER — ELONGATED (LT WING) · airframe 34,892 hrs · 20,833 cycles
STIFFENER FOR IB MAIN FLAP PANEL 553DT HAS AN ELONGATED BOLT HOLE / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02.
Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 34,751 hrs · 20,738 cycles
R1 DOOR EMERGENCY EVAC SLIDE GAUGE SHOWED LOW PRESSURE. R&R SLIDE PER MT.
Part: BALLAST — FAILED (CABIN) · airframe 34,659 hrs · 20,679 cycles
LT FAINT BURNING PLASTIC SMELL BETWEEN ROW 20 TO ROW 22. FOUND AFT ENTRY LIGHT BALLAST FAILED. R&R BALLAST IAW AMM.
Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 34,636 hrs · 20,666 cycles
RT MAIN LAND GEAR FORWARD TRUNNION LUG FACE SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.
Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 34,636 hrs · 20,666 cycles
LT MAIN LAND GEAR FORWARD TRUNNION LUG FACE SUPPORT FITTING CORRODED. REPAIRED FITTING PER EA.
Part: PANEL — CRACKED (LT WING) · airframe 34,636 hrs · 20,666 cycles
LT MLG UPPER TRAILING EDGE PNL CLIP CRACKED / R&R LT MLG UPPER TRAILING EDGE PNL CLIP IAW SRM 51-40-02.
Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 34,516 hrs · 20,580 cycles
AFT COFFEE MAKER HAD STRONG ELECTRICAL ODOR. R&R AFT GALLEY NR 1 COFFEE MAKER PER AMM.
Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 33,800 hrs · 20,101 cycles
M1672 REAR EMERGENCY LIGHT BATTERY FAILED A CAPACITY CHECK. R & R THE BATTERY IAW SIP.
Part: HOLDER — LOOSE (L2 GIRT BAR) · airframe 33,387 hrs · 19,850 cycles
L2 DOOR SLIDE GIRT BAR HOLDER LOOSE. SECURED THE HOLDER IAW MM.
2017
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,745 hrs · 19,436 cycles
R/H OVERWING EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.
Part: LIGHT — LOOSE (CABIN) · airframe 32,207 hrs · 19,091 cycles
AFT GALLEY EXIT SIGN LOOSE. SECURED LIGHT ASSEMBLY PER SIP.
Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 30,524 hrs · 18,023 cycles
RIGHT OVERWING EXIT ROW SIDEWALL LIGHT COVER FELL OFF. INSTALLED THE COVER IAW MM.
Part: FITTING — LOOSE (R2 DOOR GIRT BAR) · airframe 30,503 hrs · 18,008 cycles
R2 DOOR SLIDE FORWARD FLOOR GIRT BAR FITTING LOOSE. SECURED THE FITTING IAW AMM.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 29,525 hrs · 17,419 cycles
RIGHT OVERWING EMERGENCY EXIT SIGN LIGHT LENS BROKEN. R & R THE LENS IAW AMM.
2016
Part: LIGHT — BROKEN (CABIN) · airframe 28,042 hrs · 16,546 cycles
CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT BROKEN. R & R THE LIGHT IAW AMM.
Part: WEB — CORRODED (BS 1006-1016) · airframe 28,042 hrs · 16,546 cycles
AFT GALLEY WEB CORRODED BETWEEN BS 1006 - 1016, RBL 39. R & R THE WEB IAW SRM.
Part: STRAP — CORRODED (BS 1029) · airframe 28,042 hrs · 16,546 cycles
AFT GALLEY WEB STRAP CORRODED AT BS 1029, RBL 17. R & R THE STRAP IAW SRM.
Part: ANGLE — CORRODED (BS 957-987) · airframe 28,042 hrs · 16,546 cycles
AFT GALLEY RT Z-ANGLE CORRODED BETWEEN BS 957 - 987. R & R THE ANGLE IAW SRM.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 28,042 hrs · 16,546 cycles
RIGHT HORIZONTAL STABILIZER NR 1 STIFFENER CRACKED AT HSS 92.70, LOWER RADIUS. REPAIRED STIFFENER PER SRM.
Part: INTERCOSTAL — CRACKED (BS 344-360) · airframe 28,042 hrs · 16,546 cycles
INTERCOSTAL CRACKED BETWEEN BS 344 - 360, BL 0. R & R INTERCOSTAL IAW AMM.
Part: SUPPORT ANGLE — CRACKED (BS 294) · airframe 28,042 hrs · 16,546 cycles
R1 DOOR CUTOUT FORWARD LOWER CORNER SUPPORT ANGLE CRACKED AT BS 294.5, STRINGER 17R. R & R THE SUPPORT ANGLE IAW SRM.
Part: INTERCOSTAL — CRACKED (BS 344-360) · airframe 28,042 hrs · 16,546 cycles
INTERCOSTAL CRACKED BETWEEN BS 344 - 360, LBL 12. R & R INTERCOSTAL IAW AMM.
Part: ANGLE — CORRODED (DOOR) · airframe 28,042 hrs · 16,546 cycles
AFT GALLEY DOOR Z-ANGLE CORRODED. REPAIRED THE ANGLE IAW SRM.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 28,042 hrs · 16,546 cycles
LEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.70, IN FLANGE RADIUS AT FORWARD LOWER SPAR. REPAIRED THE RIB IAW SRM.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 28,042 hrs · 16,546 cycles
RIGHT HORIZONTAL STABILIZER NR 2 STIFFENER CRACKED AT HSS 92.70, LOWER RADIUS. REPAIRED THE STIFFENER IAW SRM.
Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 28,042 hrs · 16,546 cycles
LEFT MAIN LANDING GEAR WHEEL WELL CENTER WING REAR SPAR VAPOR BARRIER CRACKED 10 INCHES. REPAIRED BARRIER IAW EA.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,953 hrs · 15,917 cycles
RIGHT EXTERIOR EMER OVERWING LIGHT INOPERATIVE. RELAMPED LIGHT IAW SIP.
2015
Part: BATTERY PACK — DISCHARGED (FUSELAGE) · airframe 25,202 hrs · 14,910 cycles
L2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.
Part: SLIDE — UNSECURE (L1 DOOR) · airframe 24,672 hrs · 14,589 cycles
L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.
Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 23,762 hrs · 14,066 cycles
R2 DOOR EMER EVAC SLIDE LOW PRESS. R & R SLIDE IAW MM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 22,889 hrs · 13,555 cycles
EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK AT M1668. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 22,889 hrs · 13,555 cycles
EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK AT M1672. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 22,889 hrs · 13,555 cycles
EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK AT M1673. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 22,889 hrs · 13,555 cycles
EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK AT M1669. R & R BATTERY PACK IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,889 hrs · 13,555 cycles
LEFT OVERHEAD BULLNOSE EMER EXIT LIGHT INOPERATIVE AT ROW 6. R & R LIGHT IAW AMM.
Part: SKIN — CRACKED (LE SLAT) · airframe 22,889 hrs · 13,555 cycles
LEFT WING NR 3 SLAT SKIN CRACKED AT THE ACTUATOR MOUNT LOCATED AT AFT ROW INBD FASTENER. REPAIRED SKIN IAW EA.
Part: BATTERY PACK — FAILED (CABIN) · airframe 22,889 hrs · 13,555 cycles
EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK AT M1670. R & R BATTERY PACK IAW AMM.
2014
Part: COVER — BROKEN (EXIT SIGN) · airframe 21,276 hrs · 12,604 cycles
R1 DOOR EMER EXIT SIGN COVER BROKEN. R & R SIGN ASSEMBLY IAW MM.
Part: SIGN — DAMAGED (CABIN) · airframe 21,276 hrs · 12,604 cycles
BILINGUAL EMER EXIT SIGN ASSEMBLY DAMAGED. R & R SIGN ASSEMBLY IAW MM.
Part: STRAP — CORRODED (CARGO BAY) · airframe 21,276 hrs · 12,604 cycles
AFT CARGO FLOORBOARD STRAP CORRODED AT BS 767+5.5 BETWEEN LBL 20 TO RBL 20. REPAIRED STRAP IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,276 hrs · 12,604 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT REAR SPAR APPROX 3 INCHES OTBD OF STAB STATION 92.70. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,276 hrs · 12,604 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 101.90 APPROX 20 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.
Part: SEAT TRACK — DEFECTIVE (FUSELAGE) · airframe 21,276 hrs · 12,604 cycles
NUMBER 3 SEAT TRACK DEFECTIVE AT RBL 24.75 AFT OTBD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,276 hrs · 12,604 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 147.90 APPROX 25 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,276 hrs · 12,604 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 129.50, APPROX 27 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,276 hrs · 12,604 cycles
RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STAB STATION 147.90, APPROX 10 INCHES FROM REAR SPAR. REPAIRED SKIN IAW SRM.
Part: SEAT TRACK — DEFECTIVE (FUSELAGE) · airframe 21,276 hrs · 12,604 cycles
NUMBER 1 SEAT TRACK DEFECTIVE AT LBL 45.5 AFT OTBD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.
Part: BATTERY PACK — FAILED (CABIN) · airframe 20,696 hrs · 12,259 cycles
LEFT EMERGENCY EXIT LIGHT BATTERY PACK CAPACITY CHECK FAILED BETWEEN ROW 1 TO ROW 4. R & R BATTERY PACK IAW AMM.
Part: COVER — LOOSE (CABIN) · airframe 19,784 hrs · 11,716 cycles
R2 DOOR EEPLS COVER LOOSE. SECURED COVER IAW EA.
2013
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 18,478 hrs · 10,921 cycles
RT HORIZONTAL LOWER IN SPAR SKIN CRACKED AT STAB BS 101.90 9. REPAIRED SKIN IAW SRM.
Part: SLIDE — LOOSE (R1 DOOR) · airframe 18,118 hrs · 10,711 cycles
R1 DOOR SLIDE AFTER GIRT BAR HANDER LOOSE. SECURED SLIDE IAW AMM.
Part: LENS — BROKEN (CABIN) · airframe 16,715 hrs · 9,907 cycles
EXIT ROW RIGHT LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER AMM.
2012
Part: LENS — BROKEN (CABIN) · airframe 14,707 hrs · 8,727 cycles
LEFT EMERGENCY EXIT FLOOR LENS BROKEN AT ROW 12. REMOVED AND REPLACED LENS IAW AMM.
Part: LENS — MISSING (CABIN) · airframe 14,566 hrs · 8,634 cycles
LEFT EEPLS LENS MISSING AT ROW 5. INSTALLED LENS PER MM.
Part: LENS — MISSING (CABIN) · airframe 14,566 hrs · 8,634 cycles
LEFT EEPLS LENS MISSING AT ROW 23. INSTALLED LENS PER MM.
Part: LENS — WORN (CABIN) · airframe 14,338 hrs · 8,500 cycles
FORWARD EEPLS LENS WORN AT ROW 1. REMOVED AND REPLACED LENS PER MM.
Part: LIGHT — CRACKED (CABIN) · airframe 13,883 hrs · 8,220 cycles
EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER AMM.
Part: LIGHT — BROKEN (CABIN) · airframe 13,447 hrs · 7,955 cycles
R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER AMM.
Part: SIGN — BROKEN (CABIN) · airframe 13,240 hrs · 7,836 cycles
R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED 2 DOOR EMERGENCY EXIT SIGN PER M/M.
Part: COVER — CRACKED (CABIN) · airframe 12,812 hrs · 7,583 cycles
LT EGRESS TRACK LIGHTING COVER CRACKED AT ROW 9. REMOVED AND REPLACED COVER IAW M/M.
Part: COVER — CRACKED (CABIN) · airframe 12,812 hrs · 7,583 cycles
LT EGRESS TRACK LIGHTING COVER CRACKED AT ROW 13. REMOVED AND REPLACED COVER IAW M/M.
Part: COVER — CRACKED (CABIN) · airframe 12,734 hrs · 7,537 cycles
LT EEPLS COVER CRACKED AT ROW 10. REMOVED AND REPLACED COVER PER M/M
2011
Part: COVER — CRACKED (CABIN) · airframe 11,588 hrs · 6,877 cycles
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.
Part: COVER — CRACKED (CABIN) · airframe 11,588 hrs · 6,877 cycles
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 4 TO ROW 5. REMOVED AND REPLACED COVER PER MM.
Part: SIGN — BROKEN (CABIN) · airframe 9,314 hrs · 5,574 cycles
AFT EMERGENCY EXIT SIGN MOUNTS BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.
Part: COVER — CRACKED (CABIN) · airframe 9,130 hrs · 5,471 cycles
DURING SCHEDULED HC2 CHECK, FOUND FWD EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 9,130 hrs · 5,471 cycles
DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,776 hrs · 4,712 cycles
DURING SCHEDULED MV3 CHECK, FOUND EEPLS INOP AT ROW 23. REMOVED AND REPLACED EEPLS PER MM.
Part: COVER — BROKEN (CABIN) · airframe 6,805 hrs · 4,114 cycles
L1 DOOR LOWER EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.
Part: LENS — BROKEN (CABIN) · airframe 6,496 hrs · 3,934 cycles
LT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LENS PER MM.
Part: LIGHT — BROKEN (CABIN) · airframe 5,592 hrs · 3,408 cycles
DURING SCHEDULED MV2 CHECK, FOUND EEPLS AT R1 DOOR BROKEN. REMOVED AND REPLACED EEPLS PER MM.
2009
Part: COVER — MISSING (CABIN) · airframe 3,904 hrs · 2,376 cycles
FWD EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.
Part: LIGHT — BROKEN (CABIN) · airframe 1,510 hrs · 929 cycles
DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY LIGHT STRIP BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ASSY PER MM.