N85323
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
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
NR 1 ENGINE PYLON INBOARD AND OTBD UPPER LINK FITTINGS ARE CHAFED & GOUGED. REPAIRED PER ETD.
NR 2 ENGINE PYLON INBOARD AND OUTBOARD UPPER LINK FITTINGS ARE CHAFED & GOUGED. REPAIRED PER ETD.
FLOOR PANEL 231ALF HAS DAMAGED HONEYCOMB CORE. REPAIRED PER ETD.
LEFT WHEEL WELL FR52 LH RIB REPLACEMENT SB E175-57-4654 DEVIATION. REPLACED,
FLOOR SUPPORT AT RBL11 BETWEEN FR 12 TO FR 18 IS CORRODED OUT OF LIMITS IN MULTIPLE SPOTS. REPLACED
RIGHT WING, FIXED LEADING EDGE OVER PYLON, PREVIOUS REPAIR HAS CHAFE MARKS OUT OF LIMITS. REPAIRED.
LEFT WING, FIXED LEADING EDGE OVER PYLON, PREVIOUS REPAIR HAS CHAFE MARKS OUT OF LIMITS. REPAIRED.
FLOOR PANEL SUPPORT/SILL AT FR84 BETWEEN RBL36-48 IS CORRODED. OUT OF LIMITS. REPLACED
EXISTING REPAIR DOUBLER ON RBL11, BETWEEN FR 87-89 IS CORRODED, OUT OF LIMTS. REPLACED
FLOOR SILL/DOUBLER BETWEEN FR12-FR14 AND BETWEEN RBL32-RBL48 IS CORRODED OUT OF LIMITS. REPLACED
PREVIOUS REPAIR DOUBLER ON RBL 11, AT FR 84 IS CORRODED OUT OF LIMTS. REPLACED
PYLON PANEL 429ML HAS MULTIPLE CHAFES ON INSIDE OF PANEL. REPAIRED.
FWD CARGO DOOR, BOTH FWD AND AFT VENT FLAP CAMS ARE CHAFED, OUT OF LIMITS. REPAIRED
AFT CARGO DOOR, BOTH FWD AND AFT VENT FLAP CAMS ARE CHAFED, OUT OF LIMITS. REPAIRED
AFT CARGO DOOR, BOTH FWD AND AFT VENT FLAP CAMS ARE CHAFED, OUT OF LIMITS. REPAIRED.
PYLON PANEL 419NR HAS MULTIPLE CHAFES ON INSIDE OF PANEL. REPAIRED.
HORIZONTAL STAB TIP CAP, 335AL, RIB CRACKED. REPAIRED
NR 1 ENGINE HIGH OIL TEMP INDICATION IN CLIMB, EMER DECLARED WITH INFLIGHT SHUTDOWN - RTF. REPLACED ENGINE 1 W5 HARNESS AND OIL TEMPERATURE SENSOR. GROUND RUNS PASSED
LH SIDE BETWEEN UPPER SKIN AND WING UPPER SKIN - GAP CHECK FAILED AT WING TIP
LH WING SPAR 1 CRACKED AT WINGTIP ATTACH LOCATION
RH DIRECT VISION WINDOW, LOWER AFT TRACK GOUGED
RH WING SPAR 1 CRACKED AT WINGTIP ATTACH LOCATION
AFT CARGO DOOR SILL AREA, LIGHTNING HOLE COVER / FLOOR SUPPORT HAS CHAFE DAMAGE.
RH WING TIP AFT SPAR O/B UPPER ATTACH HOLE, BUSHING HOLE DAMAGED
IN CABIN BETWEEN FR89 - FR90 STRINGER 21R CORRODED. REPAIRED
FWD CARGO DOOR AREA BEHIND PROTECTOR PLATE HAS MULTIPLE SCREW HOLES CORRODED.
WING CENTER BOX, SPAR 2 IN RH CENTER FUEL TANK, BLANGE (STRINGER IS GOUGED.
RH WING TRAILING AFT SIDE OF WING SPAR 2 FITTING FOR AILERON QUADRANT ASSY CRACKED, LOCATED IN RH MLG WHEEL WELL.
RH WING TRAILING AFT SIDE OF WING SPAR 2 FITTING FOR AILERON QUADRANT ASSY CRACKED, LOCATED IN RH MLG WHEEL WELL.
EVIDENCE OF CORROSION FOUND ON #3 FWD FLAP TRACK MOUNT O/B SIDE
LH SHEAR PANEL BETWEEN FR87-FR88 CORRODED ON FWD SIDE. REPLACED.
FWD CARGO DOOR FWD LOWER SEAL DEPRESSOR CORRODED IN MULTIPLE PLACES. REPLACED.
RH MOP SILL AT RBL36 SITTING ON TOP OF CROSSBEAM AT FR84 IS CORRODED. REPLACED.
FLOORBOARD SUPPORT AT FR86 AND RBL16 BROKEN. REPLACED.
RH WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS. REPAIRED
ANGLE CLIP ON THE FWD SIDE OF FLOOR BEAM 12 AT BL 0 IS CRACKED. REPLACED.
FLOOR GUSSET AT FR90 BL0 CORRODED. REPLACED.
351GL HAS DENT ON FWD SIDE OF PANEL
AFT CARGO DOOR CUTOUT SEAL DEPRESSOR LOWER FWD EDGE CORRODED. REPLACED.
CENTER SHEAR PANEL BETWEEN FR87-FR88 CORRODED ON FWD SIDE. REPLACED.
LH WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS. REPAIRED
EXISTING DOUBLER CAP REPAIR ON LONG BEAM AT LBL10 BETWEEN FR87 - FR88 CORRODED. REPLACED.
FASTENERS AND BEAM CORRODED AT FR87 - FR88 RBL10. REPAIRED
EXISTING HORSESHOE REPAIR AT FR84 AT RH SEAT TRACK CORRODED. REPLACED
RH MOP SILL AT RBL36 SITTING ON TOP OF CROSSBEAM AT FR84 CORRODED. REPLACED
ROW 1/2 A FLOOR PHOTO ILLUM STRIP INOP/CORRECTIVE ACTION: R&R STRIP
FLOOR WEB ON TOP OF FR14 CORRODED BETWEEN RBL35 THRU RBL45
AFT RH MOP SILL FR88-FR90 CORRODED
PANEL SUPPORT ON THE FWD SIDE OF FR87 AT RBL24 CORRODED
GALLEY SUPPORT BETWEEN FR87 AND FR88 AT RBL24 CORRODED
FLOOR WEB ON TOP OF FR87 CORRODED BETWEEN RBL12 THRU RBL40
FLOOR BEAM AT RBL11 CORRODED BETWEEN FR85 THRU FR86
FLOOR BEAM AT RBL11 CORRODED BETWEEN FR86 THRU FR87
FLOOR BEAM AT LBL11 CORRODED BETWEEN FR85 THRU FR86
FLOOR BEAM AT RBL11 CORRODED AT FR13
FLOOR BEAM AT LBL11 CORRODED BETWEEN FR18 THRU FR20
WING SPAR 2 LOWER ANGLE LOCATED FWD OF LH WHEEL WELL FWD SIDE OF BULKHEAD CRACKED
ANGLE CLIP ON THE FWD SIDE OF FLOOR BEAM 12 UNDER LH SIDE COUNSIL IS CRACKED
CA FLASHLIGHT NOT CHARGING- PLACED ON MEL
FD OVERHEAD EMER LIGHT INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY.
RH WINGTIP #1 SPAR IS CRACKED AND REQUIRES REPLACEMENT
LH WINGTIP #1 SPAR CRACKED AND REQUIRES REPLACEMENT
FLOOR CROSSBEAM AT FR17 AT RBL12 HAS AREA OF CORROSION
FLOOR CROSSBEAM AT FR17 AT LBL11 HAS AREAS OF CORROSION
L/H SEAT TRACK AT FR 17 RBL 12 FWD LUG CORRODED OUT OF LIMITS. REPAIRED SEAT TRACK IAW EMB 175 SRM 53-00-10.
R/H O/B FLOOR SUPPORT FR88-FR90 CORRODED OUT OF LIMITS. REMOVED AND REPLACED PART.
FLOOR BEAM AT FR85 RBL 11 CORRODED OUT OF LIMITS. REPAIRED FLOOR BEAM IAW EMBRAER ETD 2021-170-008756.
FLOOR SUPPORT SPLICE PLATE AT FR90 RBL 25 CORRODED OUT OF LIMITS. REMOVED AND REPLACED PART.
L/H WHEEL WELL FWD FRAME 52 IS CRACKED. REPAIRED CRACK IAW EMB 175 SRM 53-22-04 FIG 22.
FLOOR SUPPORT WEB FR87-88 RBL 11 TO RBL41 CORRODED OUT OF LIMITS. REMOVED AND REPLACED PART.
FLOOR BEAM FR 12-14 RBL 11 CORRODED OUT OF LIMITS. REPAIRED FLOOR BEAM IAW EMB 175 SRM 53-10-10 REPAIR 01.
FLOOR SUPPORT WEB FR87-88 RBL 11-LBL11 CORRODED OUT OF LIMITS. REMOVED AND REPLACED PART.
R/H FLOOR BEAM SUPPORT WEB BETWEEN FR12-FR14 CORRODED OUT OF LIMITS. REMOVED AND REPLACED WEB.
FLOOR BEAM AT FR 87 LBL 11 IS CORRODED AT AND AROUND RIVET. FOUND TO BE OUT OF LIMITS. REPAIRED BEAM IAW EMB 175 SRM 53-23-10.
R/H H-STAB HAS CRACKED RIB AS SEEN FROM 3RD INSPECTION HOLE FROM O/B END OF FWD SPAR. REPAIR WAS ACCOMPLISHED BY PERFORMING EMBRAER SERVICE BULLETIN 170-55-0014.
FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. OPEN
CA'S FLASHLIGHT INOP PLACED ON MEL
FWD FA FLASHLIGHT NOT CHARGING. REPLACED FLASHLIGHT BATTERIES, OPS NORMAL.
FWD F/A FLASHLIGHT INOP. R&R BATTERY.
AFT F/A FLASHLIGHT INOP. REPLACED BATTERY.
FWD FA FLASHLIGHT INOP. REPLACED FLASHLIGHT BATTERY.
RT AFT FUSELAGE SKIN - THROUGH DAMAGE HOLE; TWO DENTS. REPAIRED FUSELAGE SKIN IAW ETD2019-170-056775.
RT AFT FUSELAGE SKIN - THROUGH DAMAGE HOLE; TWO DENTS. PERFORMED PERMANENT REPAIR IAW ETD 2019-170-059335.
FWD FA FLASHLIGHT INOP. MX REPLACED THE BATTERY.
FWD FA FLASHLIGHT INOP. PLACED ON MEL.
PHOTOLUMIN STRIP AT FWD FA CLOSET INOP.
FWD FA FLASHLIGHT INOPERATIVE.
AFT FA FLASHLIGHT INOPERATIVE.
FWD FA FLASHLIGHT INOP. PLACED ON MEL.
FIRST OFFICER`S FLASHLIGHT INOPERATIVE. REPLACED BATTERY.
FWD SERVICE DOOR EXIT SIGN INOPERATIVE.
FWD F/A FLASHLIGHT INOP. PLACED ON MEL.
FWD FA FLASHLIGHT INOP. PLACED ON MEL.
AFT FA FLASHLIGHT INOP. REPLACED BATTERY.
FWD FA FLASHLIGHT INOPERATIVE.
FWD F/A FLASHLIGHT NOT BLINKING.
F/O EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY.
FWD F/A FLASHLIGHT INOPERATIVE. PLACED ON MEL.
L2 DOOR PNEUMATIC PRESSURE ASSY FOUND 850 PSI BELOW SERVICEABLE LIMITS IAW MM 52-00-00.
R2 DOOR PNEUMATIC PRESSURE ASSY FOUND 850 PSI BELOW SERVICEABLE LIMITS IAW MM 52-00-00.
L-1 DOOR PNEUMATIC PRESSURE ASSY FOUND 850PSI, BELOW MINIMUM LIMITS 2250 PSI SERVICEABLE LIMITS, IAW AMM 52-00-00. MO55 CREATED FOR GVI AFTER 24HRS/ 2X NR'S CREATED FOR SERVICING AND GVI FROM 24 HRS AFTER SERVICING
L1 DOOR PNEUMATIC PRESSURE ASSY FOUND 850 PSI BELOW SERVICEABLE LIMITS IAW MM 52-00-00.
R1 DOOR PNEUMATIC PRESSURE ASSY FOUND 850 PSI BELOW SERVICEABLE LIMITS IAW MM 52-00-00 MO55, CREATED FOR GVI AFTER 24 HRS. 2X NRS CREATED FOR SERVICING AND GVI FROM 24 HRS AFTER SERVICING, SUBMITTING SUPPLEMENTAL INFORMATION FOR CLOSING C/A FOR PREVIOUSLY SUBMITTED SDR.
FWD F/A FLASHLIGHT WOULD NOT CHARGE. R & R BATTERY.
FWD F/A FLASHLIGHT INOPERATIVE.
GALLEY FLASHLIGHT INOPERATIVE.
AFT F/A FLASHLIGHT NOT BLINKING. R & R BATTERY.