N8584Z
Registered owner: BANK OF UTAH TRUSTEE, UT (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.
43 reports on file, 2019-02-22 – 2026-08-20.
Part: FLASHLIGHT — NOT SEATED (ZONE 200) · airframe 26,375 hrs · 13,642 cycles
FWD RT F/A FLASHLIGHT INOPERATIVE RESET FWD RT FLASHLIGHT INTO HOLDER. INSTALLED NEW SEAL, FLASHLIGHT WORKS AND TESTS OK IAW AMM 25-64-00-200-802-NG-01.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 25,962 hrs · 13,429 cycles
EMERGENCY LIGHTS INOP AT THE FOLLOWING LOCATIONS: LH OVERWING; LH FUSELAGE AFT TO THE FLAP; AT THE L2 DOOR AND AT THE MAIN CABIN. REMOVED AND REPLACED LT MID AND AFT EMERGENCY LIGHT BATTERY PACKS AND PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-06.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 25,962 hrs · 13,429 cycles
RIGHT AFT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK M01672 AND PERFORMED SATISFACTORY EMERGENCY LGHTS OPS CHECK IAW AMM 33-51-06.
Earlier reports · 2019–2025 · 40 reports
2025
Part: HANDLE — BROKEN (ZONE 800) · airframe 23,850 hrs · 12,354 cycles
FWD ENTRY DOOR ASSIST HANDLE BROKEN. RESECURED FWD ENTRY DOOR ASSIST HANDLE IAW AMM 52-11-31.
Part: CONTROL MODULE — FAILED (CABIN PRESSURE) · airframe 22,379 hrs · 11,600 cycles
AUTO FAIL LIGHT CAME ON AT FL370. RAN QRH. COULD NOT CONTROL PRESSURIZATION IN MANUAL. REMOVED AND REPLACED PER AMM 21-31-02-401-NG (CABIN PRESSURE CONTROL MODULE - REMOVAL/INSTALLATION - PERMANENT)
Part: FLASHLIGHT — FAILED (ZONE 200) · airframe 21,505 hrs · 11,127 cycles
AFT GALLEY LH INBD EMER FLASHLIGHT DOES NOT TEST. NEW FLASHLIGHT AND BATT NO HELP <[01]. OK TO CONTINUE PER [MEL 25-12-01; EMERGENCY FLASHLIGHT HOLDERS / FLASHLIGHTS - CABIN]. WITH SP 1B AND AUTHORIZATION NUMBER 244852; [02] REINSTALLED AFT GALLEY L/H INBOARD EMER FLASHLIGHT PER S.I.P. OPS TEST NORMAL.
Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 21,153 hrs · 10,947 cycles
FWD F/A FLASHLIGHT INOP<[01] REPLACED FWD EMERGENCY FLASHLIGHT BATTERY PER AMM 25-64-00
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 20,860 hrs · 10,788 cycles
CREW REPORTS L/H FWD OVER WING EXIT LIGHT INOP<[01] PREVIOUSLY MEL?D ON LOG PAGE 2762102
2024
Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 19,730 hrs · 10,170 cycles
R2 DOOR SLIDE DRAGGING<[01] ADJUSTED GIRT IAW B737-800 MT 725-61-06.;[02] ADJUSTED GIRT IAW B737-800 MT 725-61-06.
Part: CONNECTOR — NOT SEATED (ZONE 200) · airframe 19,730 hrs · 10,170 cycles
RH AFT OVERWING EMERGENCY EXIT LIGHT DOES NOT LIGHT<[01] TROUBLESHOT AND FOUND CONNECTOR NOT SEATED. RESEATED CONNECTOR AND EMERGENCY LIGHT OP CHECKS GOOD IAW B737 AMM 33-51-01;[02] TROUBLESHOT AND FOUND CONNECTOR NOT SEATED. RESEATED CONNECTOR AND EMERGENCY LIGHT OP CHECKS GOOD IAW B737 AMM 33-51-01
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 19,730 hrs · 10,170 cycles
EMERGENCY LIGHTS INOP AT L1 AND R1 DOORS.<[01] C/W EMERGENCY LIGHTS INOP AT L1 AND R1 DOORS.;[02] VERIFIED C/W EMERGENCY LIGHTS INOP AT L1 AND R1 DOORS.
Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
CR. DC. L/H VAPOR BARRIER ATTACH ANGLE CRACKED AT LBL8<[01] REPAIRED AREA PER B737-800 SRM 57-10-10-2R-5;[02] REPAIRED AREA PER B737-800 SRM 57-10-10-2R-5;[03] VERIFIED REPAIRED AREA PER B737-800 SRM 57-10-10-2R-5
Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
CR. DC. R/H VAPOR BARRIER ATTACH ANGLE CRACKED AT RBL8<[01] REPAIRED AREA PER B737-800 SRM 57-10-10-2R-5;[02] REPAIRED AREA PER B737-800 SRM 57-10-10-2R-5
Part: SHIELD — CORRODED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
AFT CARGO COMPARTMENT AFT CARGO DOOR CUT OUT AFT SHIELD CORRODED AT STREAMER (UPPER AND LOWER SURFACES)<[01] REMOVED AND REPLACED SHEILD PT#146A8127Y10ATSMOR IAW B737-800 SRM 51-40-02 BAC. DWG. 146A8127 REV.:A;[02] REMOVED AND REPLACED SHEILD PT#146A8127Y10ATSMOR IAW B737-800 SRM 51-40-02 BAC. DWG. 146A8127 REV.:A
Part: SHIELD — CORRODED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
AFT CARGO COMPARTMENT RIGHT SIDE TRANSITIONAL PANEL FROM STA767 TO 807 HAS CORROSION AT MULTIPLE PLACES. DOT#G164.<[01] REMOVED CORROSION ORIGINAL THICKNESS .050 REMOVED .006 REMAINING .044 OUT OF LIMITS IAW B737-800 SRM 53-60-15-1A-1. NEW SHEILD INSTALLATION AND RII INSPECTION STEPS ACCOMPLISHED ON CARD TTG8Q00VDLT4.;[02] VERIFIED INSPECTION STEP ACCOMPLISHED;[03] VERIFIED ALL RII INSPECTION ITEMS AND PART REPLACEMENT STEPS HAVE BEEN ACCOMPLISHED ON TTG8Q00VDLT4
Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
AFT CARGO COMPARTMENT LEFT SIDE FROM STA 727F TO STA 807 TRANSITIONAL PANEL HAS CORROSION AT MULTIPLE PLACES.DOT#G166<[01] REMOVED CORROSION AT STA. 727F TO 747 ORIGINAL THICKNESS .040 REMOVED .003 REMAINING .037; WITHIN LIMITS IAW B737-800 SRM 53-00-53; TOOL#T8224A CAL. DATE 08/JUL./25 ALODINED AND PRIMED AREAS IAW B737-800 SRM 51-20-01; FROM STA. 747 TO 807 ORIGINAL THICKNESS .040 REMOVED .006 REMAINING .034 OUT OF LIMITS IAW B737-800 SRM 53-00-53. REPAIRED L/H TRANSITION PANEL FROM STA 737-STA817 IAW B737-800 SRM 53-00-53-2R-5 REPAIR 5 ALODINE; PRIMED TRANSITION AND REPAIR SPLICES IAW B737-800 SRM 51-20-01. INSTALLED NEW TRANSITION PANEL AND REPAIR SPLICES IAW B737-800 SRM 53-00-53-2R-5 REPAUR 5 AND SRM 51-20-01;[02] VERIFIED ALL RII REQUIRED STEPS HAVE BEEN ACCOMPLISHED. VERIFIED REPAIR OF TRANSITION PANEL IAW FROM STA 737-STA817 IAW B737-800 SRM 53-00-53-2R-5 REPAIR 5
Part: SHIELD — CORRODED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
AFT CARGO COMPARTMENT; CARGO DOOR CUTOUT FORWARD SHIELD CORRODED. UPPER AND LOWER SURFACES.<[01] REMOVED AND REPLACED SHEILD PT. #146A8127U12; IAW BAC. DWG. 146A0081 B737-800 SRM 51-40-02;51-05-02.;[02] CORRECTIVE ACTION CORRECTION: REMOVED AND REPLACED SHEILD PT. #146A8127U12; IAW BAC. DWG. 146A0081; B737-800 SRM 51-40-02 AND 51-40-05.;[03] VERIFIED ALL INSPECTION STEPS HAVE BEEN ACCOMPLISHED. C/W TTG8Q00VDLT4;[04] VERIFIED ALL RII ITEMS HAVE BEEN ACCOMPLISHED. VERIFIED INSTALLATION OF SHIELD IAW PT. #146A8127U12; IAW BAC. DWG. 146A0081 B737-800 SRM 51-40-02;51-05-02.
Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
AFT CARGO COMPARTMENT RIGHT SIDE FROM STA 767 TO STA 727F TRANSITIONAL PANEL HAS CORROSION AT MULTIPLE PLACES. DOT#G165.<[01] REMOVED CORROSION AT STA. 727F TO 727J ORIGINAL THICKNESS .040 REMOVED .003 REMAINING .037 IN LIMITS IAW B737-800 SRM 53-00-53 TOOL#T8224ACAL. DATE 08/JUL./25 ALODINED AND PRIMED AREAS IAW B737-800 SRM 51-20-01 AND REMOVED CORROSION AT STA. 727J TO 767 ORIGINAL THICKNESS .040 REMOVED .018 REMAINING .022 OUT OF LIMITS IAW B737-800 SRM 53-00-53; REPAIRED TRANSTION PANEL FROM STA 727H+10-STA 767 IAW B737-800 SRM 53-00-53-2R REPAIR 5 ALODINED; PRIMED TRANSITION PANEL AND REPIRE SPLICE IAW B737-800 SRM 51-20 01. INSTALLED TRANSTION PANEL AND REPAIR SPLICE IAW B737-800 SRM 53-0053-2R -REPAIR 5;[02] REMOVED CORROSION AT STA. 727F TO 727J ORIGINAL THICKNESS .040 REMOVED .003 REMAINING .037 IN LIMITS IAW B737-800 SRM 53-00-53 TOOL#T8224ACAL. DATE 08/JUL./25 ALODINED AND PRIMED AREAS IAW B737-800 SRM 51-20-01 AND REMOVED CORROSION AT STA. 727J TO 767 ORIGINAL THICKNESS .040 REMOVED .018 REMAINING .022 OUT OF LIMITS IAW B737-800 SRM 53-00-53; REPAIRED TRANSTION PANEL FROM STA 727H+10-STA 767 IAW B737-800 SRM 53-00-53-2R REPAIR 5 ALODINED; PRIMED TRANSITION PANEL AND REPIRE SPLICE IAW B737-800 SRM 51-20 01. INSTALLED TRANSTION PANEL AND REPAIR SPLICE IAW B737-800 SRM 53-0053-2R -REPAIR . VERIFIED ALL STEPS AS SIGNED
Part: NUT PLATE — CORRODED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD SHIELD INBOARD STRAP ANGLE CORRODED AT NUT CLIP LOCATIONS ON STRAP.<[01] CLEANED AREA IAW SOPM 20-30-03; NO MATRL. LOSS NOTED. ALODINED PRIMED AREA IAW B737-800 SRM 51-20-01; REMOVED AND REPLACED NUT PLATES IAW B737800 SRM 51-40-02.;[02] VERIFIED CLEANED AREA IAW SOPM 20-30-03; NO MATRL. LOSS NOTED. ALODINED PRIMED AREA IAW B737-800 SRM 51-20-01; REMOVED AND REPLACED NUT PLATES IAW B737800 SRM 51-40-02
Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
AFT CARGO COMPARTMENT LEFT SIDE FROM STA 727F TO STA 807 TRANSITIONAL PANEL HAS CORROSION AT MULTIPLE PLACES.DOT#G166<[01] REMOVED CORROSION AT STA. 727F TO 747 ORIGINAL THICKNESS .040 REMOVED .003 REMAINING .037; WITHIN LIMITS IAW B737-800 SRM 53-00-53; TOOL#T8224A CAL. DATE 08/JUL./25 ALODINED AND PRIMED AREAS IAW B737-800 SRM 51-20-01; FROM STA. 747 TO 807 ORIGINAL THICKNESS .040 REMOVED .006 REMAINING .034 OUT OF LIMITS IAW B737-800 SRM 53-00-53. REPAIRED L/H TRANSITION PANEL FROM STA 737-STA817 IAW B737-800 SRM 53-00-53-2R-5 REPAIR 5 ALODINE; PRIMED TRANSITION AND REPAIR SPLICES IAW B737-800 SRM 51-20-01. INSTALLED NEW TRANSITION PANEL AND REPAIR SPLICES IAW B737-800 SRM 53-00-53-2R-5 REPAUR 5 AND SRM 51-20-01;[02] VERIFIED ALL RII REQUIRED STEPS HAVE BEEN ACCOMPLISHED. VERIFIED REPAIR OF TRANSITION PANEL IAW FROM STA 737-STA817 IAW B737-800 SRM 53-00-53-2R-5 REPAIR 5
Part: ANGLE — CRACKED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
FWD PIT; ANGLE CRACKED AT BS 500G AT STRINGER S-26L. MARKED<[01] REMOVED AND REPLACED ANGLE IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A7505;[02] REMOVED AND REPLACED ANGLE IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A7505. VERIFIED ALL STEPS COMPLETE.
Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
FWD PIT; TRANSITION PANEL CORRODED ON UPPER SURFACE APPROX. RBL-24 BETWEEN BS 500 AND 500A. MARKED<[01] REMOVED AND REPLACED SIDE PLATE SHIELD IAW B737-800 SRM 52-40-02 AND BOEING DWG 143A0080 AND DWG 143A8126;[02] REMOVED AND REPLACED SIDE PLATE SHIELD IAW B737-800 SRM 52-40-02 AND BOEING DWG 143A0080 AND DWG 143A8126. RII STEPS VERIFIED AND COMPLETED.
Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
FWD PIT; STRINGER CLIP CRACKED AT THE FASTENER HOLE AT BS 500I AT STRINGER S-26R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A1234;[02] VERIFIED ALL INSPECTION STEPS HAVE BEEN ACCOMPLISHED IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A1234;[03] VERIFIED THAT ALL RII ITEMS HAVE BEEN ACCOMPLISHED IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A1234 REV -
Part: CHANNEL — CRACKED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
FWD PIT R/H SIDE; CHANNEL CRACKED AT BS 500H AT STRINGER S-26R. MARKED<[01] REMOVED AND REPLACED CLIP PART NUMBER 143A7502-154 @ FWD PIT R/H SIDE; CHANNEL AT BS 500H AT STRINGER S-26R IAW 7373-800 SRM 51-40-02 AND IAW B737-800 DWG. 14A7505 REV:-;[02] REMOVED AND REPLACED CLIP PART NUMBER 143A7502-154 @ FWD PIT R/H SIDE; CHANNEL AT BS 500H AT STRINGER S-26R IAW 7373-800 SRM 51-40-02 AND IAW B737-800 DWG. 14A7505 REV:- C/W
Part: SEAL — CRACKED (ZONE 300) · airframe 19,730 hrs · 10,170 cycles
L/H HORIZONTAL STAB. L/E; UPPER SLIDING SEAL CRACKED AT THE LOWER FWD AND AFT CORNERS.<[01] REMOVED SLIDE SEAL ASSY. & 2EA CLOSEOUT PANELS IAW B737-800 SRM 51-40-02. RECEIVED NEW SLIDE SEAL PN: 181A8025-1 PO# 1094246.5 IAW B737-800 AIPC 53-31-31-03. LOCATED & DRILLED NEW SLIDE SEAL IAW B737-800 SRM 51-40-05. INSTALLED SLIDE SEAL BRACKETS TO SLIDE SEAL IAW B737-800 AIPC 53-31-31-03 & SRM 51-40-02. INSTALLED SLIDE SEAL ASSY IAW B737-800 AIPC 53-31-31-03 & AMM 53-31-31-400-802. INSTALLED 2EA CLOSE OUT PANELS IAW B737-800 SRM 51-40-02.;[02] REMOVED SLIDE SEAL ASSY. & 2EA CLOSEOUT PANELS IAW B737-800 SRM 51-40-02. RECEIVED NEW SLIDE SEAL PN: 181A8025-1 PO# 1094246.5 IAW B737-800 AIPC 53-31-31-03. LOCATED & DRILLED NEW SLIDE SEAL IAW B737-800 SRM 51-40-05. INSTALLED SLIDE SEAL BRACKETS TO SLIDE SEAL IAW B737-800 AIPC 53-31-31-03 & SRM 51-40-02. INSTALLED SLIDE SEAL ASSY IAW B737-800 AIPC 53-31-31-03 & AMM 53-31-31-400-802. INSTALLED 2EA CLOSE OUT PANELS IAW B737-800 SRM 51-40-02.<BR>REVIEWED CARD AND WORK PROCEDURES FOR FINAL.
Part: SEAL — CRACKED (ZONE 300) · airframe 19,730 hrs · 10,170 cycles
R/H HORIZONTAL STAB. L/E; UPPER SLIDING SEAL CRACKED AT LOWER AFT ATTACHMENT AREA.<[01] REMOVED SLIDE SEAL ASSY & 2 EA CLOSEOUT PANELS IAW B737-800 SRM 51-40-02. RECIEVED NEW SLIDE SEAL PN#181A8025-2 PO#1097993.3 IAW B737-800 AIPC 53--31-31-03. LOCATED AND DRILLED NEW SLIDE SEAL IAW B737-800 SRM 51-40-05. INSTALLED SLIDE SEAL BRACKETS TO SLIDE SEAL IAW B737-800 AIPC 53-31-31-03 & SRM 51-40-02. INSTALLED SLIDE SEAL BRACKETS TO SLIDE SEAL IAW B737-800 AIPC 53-31-31-03 & SRM 51-40-02. INSTALLED 2 EA CLOSEOUT PANELS IAW B737-800 SRM 51-40-02.;[02] REMOVED SLIDE SEAL ASSY & 2 EA CLOSEOUT PANELS IAW B737-800 SRM 51-40-02. RECIEVED NEW SLIDE SEAL PN#181A8025-2 PO#1097993.3 IAW B737-800 AIPC 53--31-31-03. LOCATED AND DRILLED NEW SLIDE SEAL IAW B737-800 SRM 51-40-05. INSTALLED SLIDE SEAL BRACKETS TO SLIDE SEAL IAW B737-800 AIPC 53-31-31-03 & SRM 51-40-02. INSTALLED SLIDE SEAL BRACKETS TO SLIDE SEAL IAW B737-800 AIPC 53-31-31-03 & SRM 51-40-02. INSTALLED 2 EA CLOSEOUT PANELS IAW B737-800 SRM 51-40-02.. REVIEWED CARD AND WORK PROCEDURES
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 19,730 hrs · 10,170 cycles
MAIN CABIN FLOOR PANEL SUPPORT ANGLE IS CRACKED AT STA 540; RBL 2. HAECO DOT K880<[01] REMOVED FLOOR PANEL 231UF TO F.O.M. & FLOOR SUPPORT @ STA 540 RBL 2 IAW B737-800 SRM 51-40-02. RECEIVED NEW PLATE PN:143A5240U12 BN: 481637; & PANEL BREAK PN: 143A5240U34 BN: 476735 IAW B737-800 AIPC 53-42-11-66. LOCATED AND DRILLED BOTH PLATE & PANEL BREAK IAW B737-800 SRM 51-40-05. INSTALLED PLATE TO PANEL BREAK IAW B737-800 SRM 51-40-02. INSTALLED PANEL BREAK ASSY & FLOOR PANEL 231UF IAW B737-800 SRM 51-40-02.;[02] REMOVED FLOOR PANEL 231UF TO F.O.M. & FLOOR SUPPORT @ STA 540 RBL 2 IAW B737-800 SRM 51-40-02. RECEIVED NEW PLATE PN:143A5240U12 BN: 481637; & PANEL BREAK PN: 143A5240U34 BN: 476735 IAW B737-800 AIPC 53-42-11-66. LOCATED AND DRILLED BOTH PLATE & PANEL BREAK IAW B737-800 SRM 51-40-05. INSTALLED PLATE TO PANEL BREAK IAW B737-800 SRM 51-40-02. INSTALLED PANEL BREAK ASSY & FLOOR PANEL 231UF IAW B737-800 SRM 51-40-02.
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 19,730 hrs · 10,170 cycles
MAIN CABIN FLOOR PANEL SUPPORT ANGLE IS CRACKED AT STA 540; LBL 2. HAECO DOT K881<[01] REMOVED FLOOR PANEL SUPPORT IAW 737-800 SRM 51-40-02. RECEIVED NEW FLOOR PANEL SUPPORT PN:143A5240-63 BN: 449124 IAW B737-800 AIPC 53-42-11-66. LOCATED AND DRILLED NEW FLOOR PANEL SUPPORT IAW B737-800 SRM 51-40-05. INSTALLED NEW FLOOR PANEL SUPPORT IAW B737-800 SRM 51-40-02.;[02] REMOVED FLOOR PANEL SUPPORT IAW 737-800 SRM 51-40-02. RECEIVED NEW FLOOR PANEL SUPPORT PN:143A5240-63 BN: 449124 IAW B737-800 AIPC 53-42-11-66. LOCATED AND DRILLED NEW FLOOR PANEL SUPPORT IAW B737-800 SRM 51-40-05. INSTALLED NEW FLOOR PANEL SUPPORT IAW B737-800 SRM 51-40-02.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 19,730 hrs · 10,170 cycles
MAIN CABIN FLOOR PANEL SUPPORT ANGLE IS CRACKED AT STA 540; RBL 2. HAECO DOT K880<[01] REMOVED FLOOR PANEL 231UF TO F.O.M. & FLOOR SUPPORT @ STA 540 RBL 2 IAW B737-800 SRM 51-40-02. RECEIVED NEW PLATE PN:143A5240U12 BN: 481637; & PANEL BREAK PN: 143A5240U34 BN: 476735 IAW B737-800 AIPC 53-42-11-66. LOCATED AND DRILLED BOTH PLATE & PANEL BREAK IAW B737-800 SRM 51-40-05. INSTALLED PLATE TO PANEL BREAK IAW B737-800 SRM 51-40-02. INSTALLED PANEL BREAK ASSY & FLOOR PANEL 231UF IAW B737-800 SRM 51-40-02.;[02] REMOVED FLOOR PANEL 231UF TO F.O.M. & FLOOR SUPPORT @ STA 540 RBL 2 IAW B737-800 SRM 51-40-02. RECEIVED NEW PLATE PN:143A5240U12 BN: 481637; & PANEL BREAK PN: 143A5240U34 BN: 476735 IAW B737-800 AIPC 53-42-11-66. LOCATED AND DRILLED BOTH PLATE & PANEL BREAK IAW B737-800 SRM 51-40-05. INSTALLED PLATE TO PANEL BREAK IAW B737-800 SRM 51-40-02. INSTALLED PANEL BREAK ASSY & FLOOR PANEL 231UF IAW B737-800 SRM 51-40-02.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 19,730 hrs · 10,170 cycles
AFT WET AREA FLOOR INTERCOSTAL STA 947.5 - 967 RBL 52.5 IS CORRODED<[01] REMOVED AND REPLACED INTERCOSTAL PER B737-800 SRM 51-40-02 AND BAC DWG 147A5650;[02] REMOVED AND REPLACED INTERCOSTAL PER B737-800 SRM 51-40-02 AND BAC DWG 147A5650
Part: DOUBLER — CRACKED (ZONE 100) · airframe 19,730 hrs · 10,170 cycles
EGPR DOOR CUT OUT LOWER INTERNAL DOUBLER CRACKED<[01] REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER IAW B737-800 SRM 53-10-15-2R-4 REPAIR 4;[02] REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER IAW B737-800 SRM 53-10-15-2R-4 REPAIR 4;[03] VERIFIED REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER IAW B737-800 SRM 53-10-15-2R-4 REPAIR 4
2023
Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 16,046 hrs · 8,140 cycles
FLOOR BOARD SUPPORT L/H PANEL BRAKE ASSY. CRACKED - LOCATED AT STA 540 (P/N 143A5240-35) (ZONE 125)<[01] REMOVED AND REPLACED LT BRAKE ASSY BRACKET FLOOR BOARD SUPPORT PER SRM 51-40-02.
Part: MEGAPHONE — INOPERATIVE (ZN 200 FUS TOP) · airframe 1 hrs · 7,645 cycles
AFT GALLEY MEGAPHONE NOT TESTING<[01] R AND R AFT MEGAPHONE PER M/M REF. 24-64-00.
2022
Part: FLASHLIGHT — NO TEST (AFT CABIN) · airframe 13,760 hrs · 6,867 cycles
ONE AFT EMERGENCY FLASHLIGHT; AFT GALLEY; CA SIDE WILL NOT TEST. / [01] R/R FLASHLIGHT ASSY AMM 25-64-00
Part: NONE — LOOSE (L1 DOOR) · airframe 13,237 hrs · 6,569 cycles
L1 DOOR SLIDE GURT BAR FLAP HANGING TOO LOW. / [01] SECURED VELCRO FLAP PER MT#725-61-06.
Part: BATTERY PACK — INOPERATIVE (FWD CABIN) · airframe 11,697 hrs · 5,685 cycles
1 FWD FLASHLIGHT INOP / [01] R/R BATT. PACK PER AMM 25-64-00
Part: BATTERY — FAULTY (FWD CABIN) · airframe 11,018 hrs · 5,319 cycles
FORWARD F/A FLASHLIGHT WILL NOT TEST ; / [01] REMOVED AND REPLACED FOWARD F/A FLASHLIGHT AND BATT REF AMM 25-64-00. OPS CHECK GOOD.
Part: FLASHLIGHT — FAULTY (FWD CABIN) · airframe 11,018 hrs · 5,319 cycles
FORWARD F/A FLASHLIGHT WILL NOT TEST ; / [01] REMOVED AND REPLACED FOWARD F/A FLASHLIGHT AND BATT REF AMM 25-64-00. OPS CHECK GOOD.
2021
Part: RETAINER — DIRTY (L1 DOOR GIRT BAR) · airframe 4,294 hrs · 9,106 cycles
FWD ENTRY DOOR SLIDE NOT ARMING CORRECTLY. / INSPECTED AND FOUND GIRT BAR CLIPS DIRTY.CLEANED GIRT BAR CLIPS IAW AMM 25-60-00. CRS #QGTR841X
Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 8,218 hrs · 3,827 cycles
FO SIDE AFT OVERWING EMERGENCY EXIT DOOR WINDOW LIGHT IS INOP. ( CABIN INTERIOR ILLUM BOEING SKY INTERIOR PHOTOLUMINESCENT ) REMOVED AND REPLACED LAMP RT OVERWING EXIT (EMERGENCY) IAW AMM 335104.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,199 hrs · 3,818 cycles
FIRST OFFICER SIDE AFT OVERWING EMERGENCY EXIT DOOR WINDOW LIGHT IS INOP. (CABIN INTERIOR ILLUM BOEING SKY INTERIOR PHOTO LUMINESCENT) RE-LAMPED OVERWING RT SIDE AFT LAMP IAW 3351-04 CL NR 86400.
2019
Part: LENS — BROKEN (CABIN) · airframe 1,472 hrs · 644 cycles
LT AFT OVERWING DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LIGHT ASSEMBLY PER MM.
Part: SIGN — UNSECURE (CABIN) · airframe 1,472 hrs · 644 cycles
RT EMERGENCY EXIT SIGN FELL OFF. SECURED SIGN PER MM.