N84307
Registered owner: UNITED AIRLINES INC, IL (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
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.
127 reports on file, 2014-10-01 – 2026-08-15.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 25,628 hrs · 15,519 cycles
DURING HEAVY CHECK OF FWD WET AREA, CORRODED SEAT TRACK AT FR 16, TO FR 20 L/H, LBL 12, REMOVED AND REPLACED IAW ERJ 175 SRM 51-41-02, AND SRM 51-43-03, AND SRM 51-43-04. NRC#4502709-1000-0046. REV 45 DATED MAY-28-2021.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 25,628 hrs · 15,519 cycles
DURING HEAVY CHECK OF FWD WET AREA STRUCTURES, CORROSION ON R/H SEAT TRACK FROM FR 12 R/H TO FR 20 R/H, RBL 12, REMOVED AND REPLACED WITH NEW IAW ERJ 175 SRM 51-41-01, SRM 51-43-03, AND SRM 51-43-04. NRC # 4502709-1000-0074, REV 45DATED MAY 28-2021. REV 50 DATED OCT-20-2023.
Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 25,628 hrs · 15,519 cycles
DURING HEAVY CHECK OF FWD WET AREA, CORRODED SILL PLATE BETWEEN FR 12 R/H AND FR 14 R/H, RBL 45 HAS BEEN REPLACED IAW ERJ 175 SRM 51-41-01, AND SRM 51-43-02. NRC# 4502709-1000-0072. REV 45 DATED MAY-28-2021.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 25,628 hrs · 15,519 cycles
DURING HEAVY CHECK OF FWD WET AREA, CABIN FLOOR STRUCTURES, CORRODED SILL PLATE AT FR 16, LBL 48, REMOVED AND REPLACED IAW ERJ 175 SRM 51-41-02 AND SRM 51-43-04. NRC# 4502709-1000-0069. REV 45 DATED MA Y-28-2021
Part: FLOORBEAM — CORRODED (FWD WET AREA) · corrosion level 2 · airframe 25,628 hrs · 15,519 cycles
DURING HEAVY CHECK OF CFIII, AFT WET AREA, CORRODED FLOORBEAM AT FR 86 TO FR 89 LT, RBL 11, HAS BEEN REMOVED AND REPLACED IAW SRM 51-41-01, 51-42-01, AND SRM 51-43-03. NRC# 4502709-1000-0106. REV 45, REV 50.
Part: DOUBLER — CORRODED (ZONE 200) · airframe 25,628 hrs · 15,519 cycles
DURING HEAVY CHECK, INSPECTIONS ON INTERNAL FUSELAGE FWD FLOOR DOUBLER AT FR 16,L/H, LBL 16 REMOVED BY BLENDING, IAW SRM 51-10-03, FOUND TO BE WITH IN LIMITS IAW SRM 53-10-10-AD06. 10 X MAG C/OUT, NO FAULT FOUND, REPROTECTED BLENDED AREA IAW ERJ 175 SRM 51-23-04, SRM 51-23-05, SRM 51-23-06.
Part: SHEAR PANEL — CORRODED (ZONE 20) · corrosion level 2 · airframe 25,628 hrs · 15,519 cycles
DURING HEAVY CHECK, INSPECTIONS OF CFIII, CORRODED SHEAR PANEL SPLICE AT FR 87 L/H TO FR 88 L/H, LBL50, REPLACED WITH NEW, IAW ERJ 175 SRM 51-42-02. NRC# 4502709-10000-0107. REV 45, DATED MAY-28-2021.
Part: GUSSET — CORRODED (ZONE200) · corrosion level 2 · airframe 25,628 hrs · 15,519 cycles
DURING HEAVY CHECK, CFIII, AFT WET AREA, CORRODED GUSSET PLATE AT FR 91, RBL 11 REPLACED WITH NEW IAW ERJ 175 SRM 51-41-02.
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 25,628 hrs · 15,519 cycles
DURING HEAVY CHECK, INSPECTIONS OF CF ILL, CORROSION ON GUSSET PLATE AT FR 90, RIH, RBL 23 REPLACED WITH NEW GUSSET PLATE IAW ERJ 175 SRM 51-41-02. NRC# 4502709-1000-0105, REV 45 DATED MAY-28-2021.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 25,628 hrs · 15,519 cycles
DURING HEAVY CHECK OF FWD WET AREA, CORROSION FOUND ON FLOOR STRUCTURE SILL PLATE BETWEEN FR 16 R/H AND FR 19 R/H, RBL 48, HAS BEEN REMOVED BY BLENING JAW ERJ 175 SRM 51-10-03, MAX MATRL REMOVED .003, FOUND TO BE WITH IN LIMITS IAW SRM 53-10-10, AD06. 10X MAG C/OUT, NO FAULT FOUND. REPROTECTED BLENDED AREA IAW SRM 51-23-04, SRM 51-23-05, SRM 51-23-06. NRC# 4502709-1000-0071 REV 49 DATED APRL-28-2023.
Part: DOUBLER — CORRODED (ZONE 200) · airframe 25,628 hrs · 15,519 cycles
DURING HEAVY CHECK, INSPECTIONS ON INTERNALFUSE FLOOR STRUCTURE, CORROSION FOUND ON DOUBLER AT FR 19 L/H, LBL 24, REMOVED BY BLENDING IAW ERJ 175 SRM 51-10-03, MAX MATERIAL REMOVED .002", FOUND WITH IN LIMITS IAW ERJ 175 SRM 53-10-10, AD06. 10 X MAG C/OUT NO FAULT FOUND. REPROTECTED BLENDED AREA IAW SRM 51-23-04, SRM 51-23-05, SRM 51-23-06. NRC# 4502709-1000-0070. REV 49 DATED APRL-28-2023. CORROSSION LEVEL 1
Earlier reports · 2014–2025 · 116 reports
2025
Part: SUPPORT FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,987 hrs · 14,454 cycles
AFTER REMOVAL OF RH SHEAR WEB, FOUND INBOARD GALLEY SUPPORT CORRODED ON TOP SURFACE DOWN INTO BOLT HOLE. REPLACED.
Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,987 hrs · 14,454 cycles
AFT WET AREA, RH SHEAR PANEL BETWEEN FR87-FR88 IS CORRODED. REPLACED.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,987 hrs · 14,454 cycles
AFT WET AREA, PANEL SUPPORT ON FWD SIDE OF FR87 JUST OUTBOARD OF RBL24 IS CORRODED. REPLACED.
Part: STRAP — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,987 hrs · 14,454 cycles
AFT WET AREA, UPPER STRAP ON BEAM AT RBL10 BETWEEN FR85-FR86 IS CORRODED. REPLACED.
Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,987 hrs · 14,454 cycles
AFTER REMOVING CENTER SHEAR PANEL FOUND OUTBOARD INTERCOSTAL CORRODED. REPLACED.
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,987 hrs · 14,454 cycles
AFT WET AREA, BEAM AT RBL10 BETWEEN FR86 TO FR90 HAS SEVERAL ARES OF CORRODED SPOTS. REPLACED.
Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,987 hrs · 14,454 cycles
AFTER REMOVAL OF R/H SHEAR PANEL FOUND OUTBOARD GALLEY SUPPORT CORRODED. REPLACED.
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,987 hrs · 14,454 cycles
AFT WET AREA, GUSSET AT FR89 RBL10 IS CORRODED. REPLACED.
Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,987 hrs · 14,454 cycles
AFT WET AREA, MIDDLE SHEAR PANEL BETWEEN FR87-FR88 IS CORRODED. REPLACED.
Part: SKIN — DENTED (ZONE 200) · airframe 23,987 hrs · 14,454 cycles
EXTERNAL SKIN HAS A DENT BETWEEN FR19-FR20 AT STR17R-STR18R. REPAIRED PER ETD.
Part: SKIN — SCRATCHED (ZONE 300) · airframe 23,987 hrs · 14,454 cycles
HORIZONTAL STAB L/E PANEL 331AL HAS SCRATCH MARKS. REPAIRED PER ETD.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,987 hrs · 14,454 cycles
AFT WET AREA: AFTER REMOVING RBL10 FLOOR BEAM FOUND DEEP PITTING CORROSION ON FR87 CROSSBEAM. REPAIRED PER ETD.
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 23,987 hrs · 14,454 cycles
GUSSET AT FR90, BL0, IS CORRODED. OUT OF LIMITS. REPLACED
Part: SKIN — CHAFED (ZONE 500) · airframe 23,987 hrs · 14,454 cycles
LEFT WING LEADING EDGE PANEL BETWEEN RIBS 10 AND 11 HAS A PREVIOUS REPAIR THAT IS CHAFED OUT OF LIMITS. REPAIRED
Part: SKIN — CHAFED (ZONE 600) · airframe 23,987 hrs · 14,454 cycles
RIGHT WING LEADING EDGE PANEL BETWEEN RIBS 10 AND 11 IS CHAFED OUT OF LIMITS. REPAIRED
Part: LIGHT — MALFUNCTIONED (ZONE 200) · airframe 22,820 hrs · 13,744 cycles
LUM STRIP AT 1A/2A IS 1/2 BRIGHTNESS
Part: LIGHT — MALFUNCTIONED (ZONE 200) · airframe 22,820 hrs · 13,744 cycles
LUM STRIP AT 1A/2A IS 1/2 BRIGHTNESS
Part: NONE — NONE (NONE) · airframe 22,449 hrs · 13,504 cycles
RETURN TO FIELD DUE TO MEDICAL EMERGENCY DECLARED OVERWEIGHT LANDING. INSPECTION PERFORMED, NO DEFECTS FOUND.
2024
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
AFT CARGO STRINGER 29R CORRODED BETWEEN FR76 AND FR77. REPAIRED
Part: COVER — BENT (PAX DOOR) · airframe 21,532 hrs · 12,855 cycles
FWD PASSENGER DOOR PNL 811DLW FWD SIDE BRACKET BENT AT CENTER SECTION AND DISBONDED FROM MOUNT TABS. REPAIRED
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
AFT CARGO AROUND AFT WASTE DOOR BOX/CUTOUT INTERNAL SIDE CORRODED MULTIPLE PLACES. REPAIRED
Part: SEAL REST — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
AFT CARGO DOOR LOWER SEAL DEPRESSOR LOWER LANDINGS CORRODED IN MULTIPLE PLACES. REPLACED
Part: WASHER — CHAFED (ZONE 400) · airframe 21,532 hrs · 12,855 cycles
I/B ANTI ROTATION WASHER ON I/B SIDE ON #2 PYLON FWD ATTACH LINKS ARE CHAFING LINKS. REPAIRED
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
FRAME CLIP CORRODED AT FR85 BETWEEN STR27R TO STR28R. REPLACED
Part: WASHER — CHAFED (ZONE 400) · airframe 21,532 hrs · 12,855 cycles
I/B ANTI ROTATION WASHER ON O/B SIDE ON #2 PYLON FWD ATTACH LINKS ARE CHAFING LINKS. REPAIRED
Part: SEAL REST — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
FWD CARGO DOOR LOWER SEAL DEPRESSOR LOWER LANDING CORRODED. REPLACED
Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
AFT CARGO AFT OF AFT BULKHEAD INTERNAL SIDE OF POTABLE WATER DRAIN SUPPORT STRUCTURE AND SKIN IS CORRODED. REPLACED INTERCOSTAL
Part: FITTING — CORRODED (ZONE 300) · airframe 21,532 hrs · 12,855 cycles
LH FRAME 100 HORIZONTAL STAB FITTING CHAFED. REPAIRED
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
CORROSION FOUND ON STR28R BETWEEN FR88 - FR89. REPAIRED.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
SHEAR TIE AT FR87 BETWEEN STR27R AND STR28R CORRODED. REPLACED
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
CORROSION FOUND ON STR28R BETWEEN FR88 - FR89. REPAIRED
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
SHEAR TIE AT FR88 BETWEEN STR27R AND STR28R CORRODED. REPLACED
Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
AFT CARGO DOOR SURROUND STRUCTURE LOWER BEAM CORRODED. REPLACED
Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
FLOOR WEB BETWEEN FR87 THRU FR88 AND RBL12 THRU RBL48 CORRODED. REPLACED
Part: GROUND STUD — CORRODED (ZONE 400) · airframe 21,532 hrs · 12,855 cycles
#2 ENGINE IDG GROUNDING BRACKET LOCATED IN THE TRAILING EDGE CAVITY O/B OF THE #2 PYLON CORRODED. REPAIRED
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
FLOOR BEAM FR84 CORRODED BETWEEN RBL12 THRU RBL36. REPAIRED
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
TEXAS DOUBLER ON TOP OF FR90 RBL26 CORRODED. REPLACED.
Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
FLOOR WEB BETWEEN FR12 THRU FR14 AND RBL36 THRU RBL48 CORRODED. REPLACED.
Part: FLOORBEAM — CRACKED (ZONE 200) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
RH FLOOR SILL FR84 RBL32-RBL42 CORRODED. REPLACED.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
FLOOR BEAM FR14 CORRODED BETWEEN RBL22 THRU RBL36. REPAIRED
Part: PANEL — CHAFED (ZONE 400) · airframe 21,532 hrs · 12,855 cycles
LH PYLON PANEL 419UR HAS CHAFING ON INTERIOR SURFACE. REPAIRED
Part: ANGLE — CRACKED (ZONE 200) · airframe 21,532 hrs · 12,855 cycles
ANGLE CLIP ON THE FWD SIDE OF FR12 AT BL0 IS CRACKED. REPLACED.
Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
AFT CARGO, AFT OF AFT BULKHEAD INTERNAL SIDE OF AFT POTABLE WATER DRAIN SUPPORT STRUCTURE AND SKIN HAS LIGHT SURFACE CORROSION IN MULTIPLE PLACES. REPLACED.
Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
FLOOR WEB BETWEEN FR87 THRU FR88 AND RBL12 THRU RBL48 CORRODED. REPLACED
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
FLOOR SUPPORT RBL11 CORRODED BETWEEN FR12 AND FR14. REPAIRED
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
RH FLOOR SILL BETWEEN FR88 THRU FR90 CORRODED. REPLACED.
Part: ANGLE — CRACKED (ZONE 200) · airframe 21,532 hrs · 12,855 cycles
ANGLE CLIP ON THE FWD SIDE OF FR12 UNDER THE LH SIDE CONSOLE CRACKED. REPLACED.
Part: GROUND STUD — CORRODED (ZONE 400) · airframe 21,532 hrs · 12,855 cycles
LH WING IDG GROUNDING BRACKET CORRODE O/B AND AFT OF #1 PYLON. REPAIRED
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
TEXAS DOUBLER ON TOP OF FR90 RBL26 CORRODED. REPLACED.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,532 hrs · 12,855 cycles
FLOOR SUPPORT RBL11 CORRODED BETWEEN FR84 THRU FR86. REPAIRED.
2022
Part: ANGLE — CRACKED (LT MLG WW) · airframe 18,475 hrs · 10,807 cycles
LH WHEEL WELL FWD BULKHEAD TO LWR SPAR ATTACH BRACKET CRACKED
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
FLOOR GUSSETT CORRODED AT FR90 AND RBL9
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
FLOOR BEAM CORRODED BETWEEN FR90 AND FR90A AT RBL9
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
FLOOR GUSSET CORRODED AT FR90 AND RBL9
Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
LH FLOOR SILL CORRODED BETWEEN FR87 AND FR88
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
FLOOR CROSS BEAM CORRODED AT FR90 AND RBL 9 TO RBL 34
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
CORROSION FOUND IN BETWEEN FR19 AND FR20 ON THE AIRCRAFT CENTERLINE IN THE FWD DRY AREA
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
FLOOR BEAM IS CORRODED BETWEEN FR86 AND FR88 AT RBL9
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
FLOOR GUSSET CORRODED AT FR90A AND RBL9
Part: NONE — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
RH FLOOR SILL CORRODED BETWEEN FR8 AND FR90
Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
RH SHEAR PANEL CORRODED BETWEEN FR87 AND FR88
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
FLOOR BEAM CORRODED BETWEEN FR86 AND FR89 AT LBL9
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
FLOOR GUSSET CORRODED AT FR89 AND RBL9
Part: STRAP — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
FLOOR BEAM STRAP BETWEEN FR85 AND FR86 CORRODED
Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
FLOOR GUSSET CORRODED AT FR90 AND RBL24
Part: STRAP — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
FLOOR BEAM STRAP BETWEEN FR85 AND FR86 CORRODED
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
FLOOR BEAM CORRODED BETWEEN FR89 AND FR90 AT RBL 9
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
CORROSION FOUND IN MULTIPLE LOCATIONS AT FR17 ON THE CENTERLINE OF THE AIRCRAFT IN THE FWD DRY AREA
Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
RH FLOOR SILL IS CORRODED BETWEEN FR87 AND FR88
Part: BEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
CORROSION FOUND AT FR19 ON THE AIRCRAFT CENTERLINE IN THE FWD DRY AREA
Part: DOUBLER — CORRODED (ZONE 200) · corrosion level 2 · airframe 18,475 hrs · 10,807 cycles
CORROSION FOUND AT FR14 IN THE FWD DRY AREA ON THE RH SIDE JUST BEFORE GALLEY
Part: RIB — CRACKED (ZONE 300) · airframe 18,475 hrs · 10,807 cycles
RH H-STAB RIB #12 CRACKED
Part: RIB — CRACKED (ZONE 300) · airframe 18,475 hrs · 10,807 cycles
LH H-STAB RIB #11 CRACKED
Part: RIB — CRACKED (ZONE 300) · airframe 18,475 hrs · 10,807 cycles
LH H-STAB RIB#10 CRACKED
Part: RIB — CRACKED (ZONE 300) · airframe 18,475 hrs · 10,807 cycles
RH H-STAB RIB #10 CRACKED
Part: RIB — CRACKED (ZONE 300) · airframe 18,475 hrs · 10,807 cycles
LH H-STAB RIB#12 CRACKED
Part: RIB — CRACKED (ZONE 300) · airframe 18,475 hrs · 10,807 cycles
RH H-STAB RIB #11 CRACKED
2021
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 16,750 hrs · 9,781 cycles
FO'S FLASHLIGHT NOT CHARGING. PLACED ON MEL.
2019
Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 12,724 hrs · 7,409 cycles
CA FLASH LIGHT INOP REPLACED BATTERY
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 12,607 hrs · 7,337 cycles
FLIGHT DECK EMERGENCY LIGHT INOPERATIVE.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,556 hrs · 7,309 cycles
FWD GALLEY FLOORBEAM AT FR14 CORRODED BEYOND LIMITS
Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,556 hrs · 7,309 cycles
FWD GALLEY FLOOR PLATE CORRODED, FOUND CRACKED, 100% MATERIAL LOSS ON AFT O/B CORNER.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,556 hrs · 7,309 cycles
FLOORBEAM AT FRAME 90 AROUND BL 584.2 HAS CORROSION.
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,556 hrs · 7,309 cycles
FLOOR FRAME 87 RBL 18 CORRODED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 12,556 hrs · 7,309 cycles
FLOORBEAM FR 89 CORRODED AT RT FLOOR SILL.
Part: LIGHT — INOPERATIVE (ROW 21) · airframe 12,352 hrs · 7,188 cycles
ROW 21 CEILING LIGHT EMER LIGHT INOP. STILL IN WORK
Part: POWER SUPPLY — INOPERATIVE (COCKPIT) · airframe 12,139 hrs · 7,062 cycles
COCKPIT EMER LIGHTS INOP. REPLACED EMERG LIGHT POWER SUPPLY UNIT.
2018
Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 9,719 hrs · 5,650 cycles
FWD FA FLASHLIGHT INOPERATIVE. REPLACED THE BATTERY.
Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 9,249 hrs · 5,360 cycles
FWD FA FLASHLIGHT WAS INOPERATIVE. REPLACED THE BATTERY.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 9,168 hrs · 5,305 cycles
AFT GALLEY FA FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 9,160 hrs · 5,299 cycles
FWD FA FLASHLIGHT BATTERY DEAD. REPLACED BATTERY.
Part: BRAKE SYS — UNKNOWN (MLG) · airframe 8,784 hrs · 5,062 cycles
LOSS OF BRAKING ON LANDING ROLL OUT. INSPECTED AND OPERATED BRAKE SYSTEM, NO FAULTS NOTED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,549 hrs · 4,941 cycles
R2 DOOR EMER LIGHT INOP.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 8,530 hrs · 4,931 cycles
AFT FA FLASHLIGHT NOT FLASHING. REPLACED BATTERY.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 8,269 hrs · 4,789 cycles
FWD FA FLASHLIGHT INOP. REPLACED FLASHLIGHT ASSY.
Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 8,233 hrs · 4,771 cycles
FWD FA FLASHLIGHT INOPERATIVE.
2017
Part: ENGINE — VIBRATION (NR 2) · airframe 7,541 hrs · 4,360 cycles
EMERGENCY DECLARED AND DIVERTED DUE TO A NR 2 ENGINE N2 VIBRATION 4.0. OPEN
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 7,104 hrs · 4,100 cycles
AFT FA FLASHLIGHT INOPERATIVE. REPLACED THE BATTERY.
Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 7,045 hrs · 4,063 cycles
GUSSET HAS CORROSION, FRAME 90, RBL 584.2, WL 490. REMOVED AND REPLACED GUSSET IAW SRM 51-43-03.
Part: FLOOR SUPPORT — CORRODED (FRAME 87) · corrosion level 2 · airframe 7,045 hrs · 4,063 cycles
GALLEY FLOOR SUPPORT AT FRAME 87, RBL 939.8 HAS CORROSION. REMOVED AND REPLACED GALLEY FLOOR SUPPORT IAW SRM 51-42-03.
Part: FLOOR SUPPORT — CORRODED (FRAME 89) · corrosion level 2 · airframe 7,045 hrs · 4,063 cycles
FLOOR SUPPORT SPLICE HAS CORROSION, STA 24458.0, FRAME 89, RBL 304.8, W/L 490. REMOVED AND REPLACED FLOOR SUPPORT SPLICE IAW SRM 51-43-03.
Part: FLOOR SUPPORT — CORRODED (GALLEY) · corrosion level 2 · airframe 7,045 hrs · 4,063 cycles
GALLEY FLOOR SUPPORT AT FRAME 87, BL 0 HAS CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-03.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 6,959 hrs · 4,015 cycles
FWD FA SEAT EMER EXIT SIGN INOP. REPLACED PWR SUPPLY.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 6,651 hrs · 3,833 cycles
AFT FA FLASHLIGHT INOP. REPLACED BATTERY.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 6,651 hrs · 3,833 cycles
FWD FA FLASHLIGHT INOP. REPLACED BATTERY.
2016
Part: LIGHT — INOPERATIVE (SEAT 1C) · airframe 4,973 hrs · 2,892 cycles
EMERGENCY LIGHT STRIP BELOW SEAT 1C INOPERATIVE. MX SECURED THE STRIP OPS NORMAL
Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 4,190 hrs · 2,407 cycles
FWD F/A FLASHLIGHT LED NOT BLINKING.
Part: FLASHLIGHT — INOPERATIVE (GALLEY) · airframe 3,631 hrs · 2,084 cycles
FORWARD GALLEY FLASHLIGHT INOPERATIVE.
Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 3,316 hrs · 1,924 cycles
AFT F/A FLASHLIGHT INOPERATIVE.
2015
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 2,945 hrs · 1,716 cycles
CAPTAIN FLASHLIGHT INOPERATIVE, REPLACED BATTERY.
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 2,657 hrs · 1,539 cycles
F/O'S FLASHLIGHT INOPERATIVE. REPLACED BATTERIES.
Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 1,896 hrs · 1,095 cycles
L1 DOOR SLIDE PARTIAL DEPLOYED. MAINTENANCE IN WORK.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 1,814 hrs · 1,051 cycles
PAX DOOR EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY PACK.
Part: BOTTLE — DISCHARGED (PAX DOOR) · airframe 935 hrs · 512 cycles
LEFT PAX DOOR PNEUMATIC ASSY PRESURE FOUND BELOW SERVICABLE LIMITS DURING INSPECTION. DOOR SERVICED UP TO SERVICEABLE LIMITS AND MO55 ISSUED M5523287 FOR GVI INSPECTION.
2014
Part: CRADLE — INOPERATIVE (FWD FLASHLIGHT) · airframe 413 hrs · 218 cycles
FWD F/A FLASHLIGHT LED NOT BLINKING.
Part: DIAPHRAGM — RUPTURED (SLIDE BOTTLE) · airframe 70 hrs · 38 cycles
AFTER THE AGENT OPENED THE L1 PAX DOOR THE ARMING HANDLE SLIPPED INTO THE ARMED POSITION. THIS ACTION RUPTURED THE DIAPHRAM ON DOOR ASSIST BOTTLE CAUSING THE BOTTLE TO LOOSE PRESSURE.