N16151
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
AFT SIDE OF AFT EMERGENCY EXIT LOCATOR INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY EXIT LOCATOR LIGHT. OPS CHECK FAILED. REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER #4. OPS CHECK SAT.
ENGINE 1 SHUTDOWN INFLIGHT DURING CRUISE. REMOVED PMA AND LWR IGNITER FOR BORESCOPE AND INSTALLED. REMOVED PMA AND LWR IGNITER FOR BORESCOPE AND INSTALLED. REMOVED AND REPLACED ENGINE 1. PERFORMED HIGH POWER RUN. OPS/LEAK CHECK SAT. NO DEFECTS NOTED AT THIS TIME.
RH AFT RIB IN MLG BAY IS CRACKED. REMOVED AND REPLACED RH AFT RIB IN MLG BAY.
RH FLOORBEAM CAP CORRODED AT MOUNT HOLES FOR LAV. REMOVED RH FLOORBEAM CAP FOR REPLACE, LOCATED, AND DRILLED AND INSSTALLED
RH FLOORBEAM CAP CORRODED UNDER BULKHEAD AT LAV. REMOVED CORRODED FLOORBEAM CAP, LOCATED AND DRILLED AND INSTALLED
RH FLOORBEAM AT F.S 23 CORRODED. REMOVED AND REPLACED WITH NEW REPAIR DOUBLER ON RH FLOORBEAM AT F.S. 23
LH FLOORSILL F.S. 18 - F.S 18A CORRODED. REMOVED CORRODED LH FLOORSILL @ F.S. 18 - F.S. 18A LOCATED AND DRILLED AND INSTALLED NEW SILL.
CORROSION ON FLOORSILL AT SERVICE DOOR. REMOVED AND REPLACED FLOORSILL AT SERVICE DOOR.
FLOOR SILL AT MOUNT BOLT AT F.S. 22 CORRODED. REMOVED AND REPLACED CAP ON FLOORSILL AT FS22
CENTER FLOORBEAM CAP CORRODED AROUND MOUNT HOLES AT LAV. REMOVED CORRODED FLOORBEAM CAP, LOCATED AND DRILLED NEW
OB FLOORSILL UNDER LAV CORRODED. REMOVED AND REPLACED OB FLOORSILL.
LH FWD FLOORSILL IN CARGO DAMAGED. REMOVED AND REPLACED LH SILL AT LH FLOOR SILL IN CARGO.
LH SHEAR CLIP AT REAR CABIN BULKHEAD BETWEEN STRINGER 6L AND 7L IS CRACKED. REMOVED AND REPLACED LH SHEAR CLIP AT REAR CABIN BULKHEAD BETWEEN STRINGER 6L AND 7L.
RH SHEAR CLIP AT REAR CABIN BULKHEAD BETWEEN STRINGER 6R AND 7R IS CRACKED. REMOVED AND REPLACED RH SHEAR CLIP AT REAR CABIN BULKHEAD BETWEEN STR 6R-7R.
LH AFT RIB IN MLG BAY HAS MULTIPLE CRACKS. REMOVED AND REPLACED LH AFT RIB IN MLG BAY.
FLOORSILL OB CORRODED FRM 46-49. REMOVED CORRODED SILL AND LOCATED AND DRILLED AND INSTALLED NEW SILL.
LH WTF FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH AFT EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT
LH ABOVE THE WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH ABOVE THE WING EMERGENCY LIGHT. OPS CHECK SAT
COCKPIT EMERGENCY LIGHT OUT. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT BULB. OPS CHECK GOOD.
LH ESCAPE HATCH EXIT IDENTIFIER SIGN INOPERATIVE. REMOVED AND REPLACED LH ESCAPE HATCH EXIT IDENTIFIER SIGN. OPS CHECK FAILED. RESTORED TO ORIGINAL CONFIGURATION. REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER #5. OPS CHECK SAT
FLAP LOW SPEED AT ACCELERATION ALTITUDE FOLLOWED BY FLAP FAIL SHORTLY AFTER. REMOVED AND REPLACED FECU. OPS CHECK SAT.
NOT ABLE TO OPEN THE MAIN CABIN DOOR FROM INSIDE THE PLANE. REPOSITIONED MAIN CABIN DOOR HANDLE. OPS CHECK GOOD
LEFT SIDE ESCAPE HATCH EXIT IDENTIFIER INOPERATIVE. LIGHT FUNCTIONED AFTER RUNNING APU AND PERFORMING FUNCTIONAL TEST. OPS CHECK SAT.
FOUND LH LOWER HATCH DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LOWER HATCH DOOR EMERGENCY LIGHT. OPS CHECK SAT
MCD EMERGENCY LIGHT INOPERATIVE. REMOVED MCD EMERGENCY LIGHT HOUSING. FOUND BAD GROUND. CLEANED GROUND WIRE RING TERMINAL. REINSTALLED MCD EMERGENCY LIGHT. OPS CHECK SAT
COVER FRAME 68 SHEAR CLIP REPAIR INVESTIGATION. AT FRAME 68 SHEAR CLIP REPAIR REMOVED AT FR 68, SHEAR CLIP REPAIRED.
AFTER NDT INSPECTION, RH FUSE SKIN FOUND CRACKED AT FR 75 BTW STR 2R-3R. RH FUSE SKIN AT FR 75 BTW STR 2R-3R CRACK REMOVED. RH FUSE SKIN AT FR 75 BTW STR 2R-3R REPAIRED
CENTER FUSE I, UNDER FLOOR SKIN CORRODED BTW FRAME 17-19 AND STR 21R-21L. CENTER FUSE I, UNDER FLOOR SKIN BTW FRAME 17-18 AND STR 21R-21L BLENDED FOR INVESTIGATION. AFTER INVESTIGATION, CORROSION ON LOWER SKIN BTW FR 17-19 AND BTW STR 21L-21R FOUND OUT OF LIMITS. DURING THE INSTALLATON OF THE REPAIR DOUBLER, THE SKIN STARTED TO DO AN OIL-CANNING EFFECT AFT OF THE CUTOUT. SKIN REPAIRED IN CF BW FR17-19 AND STR 21L-21R PERFORMED. CORROSION LEVEL 1
INSPECT FOR AND TREAT AS NEEDED ANY CORROSION UNDER THE REAR FUSELAGE II NAMEPLATES. ON LOWER REAR FUSE II LH OUTB RIB, BTW FR 79-80 RIB DAMAGED. SPLICE REPAIR ON LOWER REAR FUSE II LH OUTB RIB, BTW FR 79-80 REPAIRED. AT FR 78 NAMEPLATES REMOVED FOR INVESTIGATION AND SKIN FOUND CORRODED OUT OF LIMIT. CORROSION ON SKIN REPAIRED WITH DOUBLER AND NAMEPLATES RE-INSTALLED. CORROSION LEVEL 1
CENTER FUSE IV, UNDER FLOOR, SHEAR CLIP FRAME 60 BTW STR 18R-20R CORRODED. CENTER FUSE IV, UNDERFLOOR, SHEAR CLIP FRAME 60 BTW 18R-20R OUT OF LIMITS. CENTER FUSE IV, POST FR60 REMOVED FOR ACCESS AND SHEAR CLIP FR 60 STR 18R-20R REMOVED FOR REPLACEMENT. CENTER FUSE IV, UNDERFLOOR, SHEAR CLIP FR60 BTW STR 18R-20R REPLACED WITH MADE REPAIR PART, LOCALLY FABRICATED AND MASTER PART AND INSTALLED WITH RIVETS. POST AT FR60 REINSTALLED
AFTER NDT INSPECTION, CRACK FOUND IN LH PYLON YOKE BLIND FASTENER HOLE. HOLE REPAIRED WITH BUSHING AND ALTERNATE MATERIAL
BAGGAGE DOOR SCRATCHED ABOVE FLAPPER DOOR. ON BAGGAGE DOOR ABOVE FLAPPER AREA STRIPPED FOR INVESTIGATION, SCRATCH WITH DENT OUT OF LIMITS. PERFORMED CUT-OUT ON BAGGAGE DOOR. FABRICATED, LOCATED, AND DRILLED REPAIR DOUBLER AND REPAIR FILLER. INSTALLED REPAIR PARTS ON BAGGAGE DOOR ABOVE FLAPPER DOOR. BAGGAGE DOOR SCRATCHES AND DENT REPAIRED.
CF2, RH SIDE, FR25 AT FLOOR LEVEL BEHIND SILL, FRAME FOUND CRACKED. FRAME SPLICED.
CENTER FUSE IV, UNDER FLOOR, LH GUSSET BTW FRAME 59-61 CORRODED. OMEGA BEAM BLENDED OUT OF LIMITS BTW FR 60-61. CENTER FUSE IV BTW FR 60-61, LH OMEGA BEAM REPAIRED AND GUSSET REPLACED. NO CORROSION FOUND.
VENTRAL FUEL TANK, FWD SECTION BRACKET CORRODED. WEB REPAIRED. CORROSION LEVEL 1.
CENTER FUSE IV, UNDER FLOOR, RH OMEGA BEAM BTW FR 59-61 CORRODED. RH OMEGA BEAM BTW FR 60-61 IN CENTER FUSE IV UNDERFLOOR, CORROSION UNDER NUT PLATE CUT. RH OMEGA BEAM BTW FR60-61 IN CENTER FUSE IV REPAIRED WITH DOUBLER. NO CORROSION FOUND.
CENTER FUSE IV, UNDER FLOOR, CENTER OMEGA BEAM BTW FRAME 59-61 CORRODED. CENTER OMEGA BEAM BTW FR 60-61 IN CENTER FUSE IV UNDERFLOOR, CORROSION UNDER NUT PLATE CUT. CENTER OMEGA BEAM BTW FR60-61 IN CENTER FUSE IV REPAIRED WITH DOUBLER. NO CORROSION FOUND.
3 EMERGENCY LIGHTS INOPERATIVE AT ROW 18. REMOVED AND REPLACED #3 EMERGENCY BATTERY. OPS CHECK GOOD.
LOWER EMERGENCY LIGHT AT SEAT 18A INOPERATIVE. R&R EXIT ID SIGN. OPS CHECK SAT.
BLEED 1 LEAK MESSAGE ON EICAS. (CREW REPORTED AT FL220 MESSAGE APPEARED AND HE DECLARED AN EMERGENCY, THE THEN WENT THROUGH THE CHECKLIST AND WHEN BLEED WAS DESELECTED THE MESSAGE WENT OUT SO HE ADVISED TOWER HE RESOLVED THE ISSUE AND DIDNâT NEED PRIORITY LANDING BUT REPORTED AN EMERGENCY WAS STILL DECLARED). R&R AIR BLEED SYSTEM DUCT LINE O-RINGS @ POSITIONS 15, 23 AND 29. PERFORMED AIR BLEED SYSTEM DUCT LEAKAGE TEST. OPS CHECK SAT. LEAK CHECK SAT.
LT EMERGENCY EXIT ROW LOWER EXIT ID SIGN INOPERATIVE. INSPECTED LT EMERGENCY EXIT IDENTIFIER SIGN AT THE EMERGENCY EXIT ROW AND RE-CONNECTED HARNESS FOR THE PROPER CONNECTION. OPERATIONS CHECK COMPLETED, NO FAULTS FOUND.
EMERGENCY FLOOR LIGHT PATH, FRONT END OF EACH SIDE STRIP RED BLOCKS ARE MISSING OR WORN. ALSO, MISSING 4 END CAPS AT POSITION 9A, 9CD, 22CD AND FWD RIGHT JUST AFT GALLEY. MULTIPLE LOCATION TRACK IS LOOSE FROM FLOOR. INSTALLED EMERGENCY FLOOR LIGHTING PATH FRONT END STRIPS OF MISSING RED BLOCKS. INSTALLED 4 END CAPS AT LOCATIONS 9A, 9CD, 22CD AND FWD RIGHT END AFT GALLEY.
BLEED LEAK IN FLT--- T/S MSG PER FIM TASK 36-20-00. FOUND FAN AIR VALVE CLAMP LOOSE. SAME RETORQUED. PERFORMED OPS CHECK WITH NO FAULTS NOTED.
BLEED #1 LEAK IN ICE CONDITIONS. PERFORMED OPS CHECK OF ANTI-ICE SYSTEMS. OPS CHECK GOOD.
BRACKET BROKE INSIDE 1ST LT FUEL UNDERWING ACCESS OPENING ON 1ST RIB. R&R BRACKET INSIDE 1ST LT FUEL UNDERWING ACCESS OPENING ON THE FIRST RIB.
AFT CARGO FRAME 67 O/B SIDE OF LT OMEGA BEAM FLOOR SUPPORT BRACKET IS CRACKED. REMOVED & REPLACED BRACKET.
LT OMEGA BEAM UPPER DIGITAL AT FRAME 16 CRACKED. REPAIRED LT OMEGA BEAM UPPER DIGITAL.
AFT CARGO FRAME 65 RT SIDEWALL LINER SUPPORT HAS CORROSION AT STR 15R. R&R AFT CARGO FRAME 65 RT SIDEWALL LINER SUPPORT.
SIGNS OF CORROSION ON CARGO FLOOR GUSSET BETWEEN FR 65-68 - REMOVED GUSSET. MATCH DRILLED AND COUNTERSUNK NEW GUSSET. INSTALLED GUSSET BETWEEN FR 65-68.
RT WING T/E O/B FLAP SHROUD I/B SUPPORT STANDOFF IS CRACKED. REMOVED & REPLACED STANDOFF SUPPORT AT RT WING T/E O/B FLAP UPPER SHROUD.
LT WING T/E O/B FLAP SHROUD I/B SUPPORT STANDOFF IS CRACKED. REMOVED & REPLACED STANDOFF SUPPORT AT LT WING T/E O/B FLAP UPPER SHROUD.
CARGO DOOR Z ANGLE FWD AND AFT DOUBLERS ARE CORRODED. REMOVED & REPLACED FWD DOUBLER. AFT DOUBLER SHOES NO CORROSION DAMAGE AND IS SERVICEABLE AS IS.
SERVICE DOOR LOWER THRESHOLD HAS CORROSION ON UPPER SURFACE FROM FR 20 THRU 22. BLEND OUT THE DAMAGED AREA AND REMOVED ALL OF THE CORROSION. REQUIRES TO BE NDI. PERFORMED HF EC INSPECTION OF BLENDED AREAS. NO DEFECTS NOTED. GOOD TO CONTINUE WITH REPAIR. REPAIRED THE DAMAGED AREA.
CARGO DOOR CUT OUT HAS CORROSION AT FR 65 BELOW STR 16. REMOVED UPPER OPENING 'X' ANGLE, FWD (FR 65) SHEAR TIE, AND FWD CARGO DOOT TRACK. DE-RIVETED WEB ASSEMBLY FWD OF FRAME 65 TO ALLOW MOVEMENT FOR CUTTING FRAME 65. REMOVED ACCUPLEX BRACKETS / HDW. PICKED UP AND TRANSFERED HOLES ONTO NEW FR 65 SHEAR CLIP, SPLICED FR 65 AND PICKED UP HOLES ON NEW FR 65 PIECE. FABRICATED DOUBLERS FOR FR 65 SPLICE LOCATION. DRILLED, ALODINED & PRIMED. FABRICATED SHIM FOR USE BEHIND DOUBLER TO ALLOW PROPER RIG OF REPAIR COMPONENTS. BEGAN INSTALLATION OF REPAIR COMPONENTS. INSTALLED UPPER OPENING 'Z' ANGLE & RELATED BRACKETS. INSTALLED REPAIR. FILLET / EDGE SEAL STILL REQUIRES & 5 CHERRY RIVETS AT FRAME 62/UPPER 'Z' ANGLE INTERFACE. REMOVED FWD BAGGAGE DOOR MICROSWITCH TO FOM. APPLIED FILLET EDGE SEALANT & INSTALLED 5 CHERRY RIVET ON 'Z' ANGLE. INSTALLED BAGGAGE DOOR MICROSWITCH, OPS CHECK GOOD.
CENTER OMEGA BEAM CENTER SPLICE IS CRACKED AT FR 20 TO 22. REMOVED ANGLE AT CENTER OMEGA BEAM SPLICE FR 20 TO 22. INSTALLED ANGLE AT CENTER OMEGA BEAM SPLICE FR 20 TO 22.
SHEAR CLIP CRACKED PAX CABIN LH SIDE AT FRAME 26 STR 15L. R&R CRACKED SHEAR CLIP AT FR 26 STR 15L.
RT FLOOR SILL AFT OF FRAME 23 CORRODED. BLEND OUT THE DAMAGED AREA AND REMOVED AL OF THE CORROSION STILL REQUIRES TO BE NDI. PERFORMED HF EC INSPECTION OF BLENDED AREA NO DEFECTS NOTED. GOOD TO CONTINUE WITH REPAIR. REPAIRED THE DAMAGED AREA.
RT STEP-UP AT FRAME 23 HAS CORROSION. REMOVED RT STEP-UP AT FRAME 23. INSTALLED RT STEP-UP AT FRAME 23.
RT WALL SEAT TRACKS BETWEEN FRAMES 41 & 50 HAVE CORROSION. R&R CORRODED WALL SEAT TRACKS BETWEEN FRAMES 41 & 50.
LT FLOOR SILL BETWEEN FRAMES 46 & 51 HAVE CORROSION. REMOVED THE 2 LT FLOOR SILLS FROM FRAME 46-FR52 & REPLACED THE AFT ONE & FWD ONE TO FR46 NEEDS DRILLED & INSTALLED YET. INSTALLED THE FWD LT SILL AT FR46.
STOP SIGN ON RT OMEGA BEAM AT FRAME 22 HAS CORROSION. REMOVED & REPLACED STOP SIGN ON RT OMEGA BEAM AT FRAME 22.
LT FLOOR SEAT TRACKS BETWEEN FRAMES 39 & 42 HAVE LIGHT CORROSION. R&R CORRODED LT FLOOR SEAT TRACKS BETWEEN FRAMES 39 & 42.
RAMP SUPPORT ANGLE CRACKED ON LT OMEGA BEAM AT FRAME 19. REMOVED & REPLACED RAMP SUPPORT ANGLE ON LT OMEGA BEAM AT FR 19.
CRACK AT LT FRAME 46 LOWER FRAME END FITTING BELOW LT FLOOR SILL. R&R THE CRACKED FITTING AT FR 46 BELOW FLOOR SILL.
CARGO COMPARTMENT RT FLOOR SILL AT FRAME 67 CRACKED. R&R RT FLOOR SILL AT FR 67.
LT OMEGA BEAM UPPER DIGITAL AT FRAME 50 HAS CORROSION. REMOVED SEAT TRACKS AND OMEGA BEAM UPPER DIGITAL. INSTALLED OMEGA BEAM UPPER DIGITAL, SEAT TRACKS STILL NEEDS TO BE INSTALLED. INSTALLED THE SEAT TRACKS.
RT FLOOR SILL AT FRAME 46 & 48 HAVE CORROSION. REMOVED THE RT FLOOR SILL AT FR 46 AND THE ONE AT FR 48. INSTALLED RT FLOOR SILLS AT FR 46 & FR 48.
CARGO COMPARTMENT SHEAR CLIP CRACKED AT FRAME 65 STR 17L. R&R SHEAR CLIP AT FR 65 STR 17L.
LT OMEGA BEAM UPPER DIGITAL HAS CORROSION FWD OF FRAME 19. CUTOUT DAMAGE ON LT OMEGA BEAM UPPER DIGITAL, FWD OF FRAME 19. REQUIRES NDI. PERFORMED HF EC INSPECTION OF CUTOUT EDGES. NO DEFECTS NOTED. GOOD TO CONTINUE WITH REPAIR. FABRICATED DOUBLER AND FILLER AND INSTALLED ON LT OMEGA BEAM UPPER DIGITAL FWD OF FR 19. FINISHED INSTALLATION OF FILLER AND DOUBLER ON LT OMEGA BEAM UPPER DIGITAL AT FWD OF FRAME 19. RESTORED SURFACE PROTECTION.
LT SILL CORRODED BETWEEN FR 19 & 21. R&R LT SILL BETWEEN FR 19 & 21.
CENTER OMEGA BEAM UPPER DIGITAL HAS CORROSION BETWEEN FRAME 20 & 23. REMOVED CENTER OMEGA BEAM UPPER DIGITAL BETWEEN FRAME 20 AND 23. LOCATED AND DRILLED NEW OMEGA BEAM. STARTED INSTALLATION OF NEW OMEGA BEAM DIGITAL BETWEEN FRAME 23 AND 23. FINISHED INSTALLING OMEGA BEAM UPPER DIGITAL.
AFT CARGO DOOR AFT TORSION BAR LOWER SUPPORT BRACKET IS CRACKED ON BACKSIDE. R&R CARGO DOOR TORSION BAR LOWER SUPPORT BRACKET.
CARGO DOOR CUP HOLDER SUPPORT AT FR 68 IS CRACKED ON LOWER SIDE. R&R CARGO DOOR CUP HOLDER SUPPORT BRACKET AT FR 68.
AFT CARGO FRAME 67 ABOVE CARGO DOOR SHEAR CLIP IS CRACKED BETWEEN STR 5 & 6L. REMOVED & REPLACED SHEAR CLIP.
AFT CARGO FRAME 73 RT SIDE SHEAR CLIP IS CRACKED BETWEEN STR 9 & 10R. R&R AFT CARGO FR 73 RT SIDE SHEAR CLIP BETWEEN STR 9 & 10R.
AFT CARGO FRAME 68 ABOVE CARGO DOOR SHEAR CLIP IS CRACKED BETWEEN STR 6 & 7 LT. R&R SHEER CLIP AT FR 68 ABOVE CARGO DOOR.
AFT CARGO FRAME 73 LT SHEAR CLIP IS CRACKED BETWEEN STR 9 & 10 LT. R&R AFT CARGO FR 73 SHEAR CLIP BETWEEN STR 9&10 LT.
LT AFT WHEEL WELL WEB IS CRACKED IN 2 PLACES. REMOVED LH AFT WHEEL WELL WEB & LOWER ANGLE. INSTALLED NEW LOWER REAR ANGLE. INSTALLED NEW LH AFT WHEEL WELL WEB.
CARGO DOOR LOWER FRAME ANGLE SUPPORT HAS CORROSION AROUND NUTPLATE HOLES. REMOVED AND INSTALLED CARGO DOOR LOWER FRAME ANGLE SUPPORT. FURTHER WORK INCLUDES INSTALLING NUTPLATES. INSTALLED NUTPLATES ON CARGO DOOR LOWER FRAME ANGLE SUPPORT.
LT WING L/E UPPER SURFACE AT FRAME 41 BELLY FAIRING 'L' ANGLE ON TOP OF WING IS CRACKED. REMOVED DAMAGED AREA OF SUPPORT ANGLE. REMOVED FUEL PNL 155NZ. REPAIRED LT WING UPPER SURFACE AT FRAME 41 'L' ANGLE. NUTPLATE FOR FWD FAIRING STILL REQUIRES INSTALL. INSTALLED NUTPLATE ON LT 'L' ANGLE. INSTALLED FUEL PANEL 155NZ.
AFT CARGO DOOR CUT OUT FWD LATERAL 'L' SHAPE ANGLE AT FRAME 65 HAS CORROSION ON LOWER FWD CORNER. REMOVED & REPLACED SHEAR TIE.
CARGO DOOR CUT OUT FWD LOWER CORNER AT FRAME 65 CLOSE OUT PANEL HAS CORROSION. REMOVED DAMAGE COMPONENTS / FRAMES. LOCATED & DRILLED NEW CLOSE OUT PANEL. INSTALLED NEW CLOSE OUT PANEL AT FRAME 65.
AFT CARGO AT FR 65 SIDEWALL LINER SUPPORT FRAME HAS CORROSION & GOUGES AROUND NUTPLATE HOLES BETWEEN STR 2 THRU 14 LT. REMOVED RIVETS SECURING FRAME TO THE AIRCRAFT, TO ALLOW CUT OUT OF AFFECTED AREA. DEVELOPED RIVET PATTERN AND FABRICATED REPAIR PARTS. COMPLETED REPAIR ON FR 65.
AFT CARGO FRAME 62 LT SIDE SHEAR CLIP IS CRACKED BETWEEN STR 7 & 8 L. REMOVED SHEAR CLIP. INSTALLED AFT CARGO FRAME 62 LT SHEAR CLIP.
RT AFT WHEEL WELL WEB IS CRACKED IN 4 PLACES. REMOVED CRACKED LOWER ANGLE ON RT AFT WHEEL WELL WEB. INSTALLED NEW LOWER ANGLE. NUTPLATES STILL NEED INSTALLED. INSTALLED NUTPLATES ON RT AFT WHEEL WELL WEB. OUTBOARD RIB ON WHEEL WELL WEB NEEDS INSTALLED. INSTALLED OUTBOARD RIB ON RT AFT WHEEL WELL WEB.
RT AFT FUSELAGE EXTERIOR SKIN AT FR 78 AT STR 4R HAS CRACK AROUND 2 EA RIVETS. REMOVED 2 EA RIVETS. UPSIZED HOLE TO .193 AND COUNTERSUNK. PERFORMED HF EC INSPECTION OF REWORKED AREAS. NO DEFECTS NOTED. GOOD TO CONTINUE WITH REPAIR. INSTALLED 2 EA RIVETS.
COCKPIT FR 10 RT SIDE IS CRACKED AT UPPER END BELOW DV SLIDING WINDOW. R&R COCKPIT FR 10 RT SIDE.
CARGO DOOR LOWER THRESHOLD 'Z' ANGLE HAS CORROSION. REMOVED DAMAGED 'Z' ANGLE. PICKED-UP AND TRANSFEREDHOLE ON TO NEW CARGO DOOR LOWER 'Z' ANGLE. INSTALLED LOWER 'Z' ANGLE. TRIM & EDGE SEAL LEFT REMAINING. APPLIED EDGE SEAL & TRIMMED CARGO DOOR LOWER THRESHOLD.
COCKPIT FRAME 10 LT SIDE IS CRACKED AT UPPER END BELOW DV SLIDING WINDOW. R&R COCKPIT FR 10 LT SIDE.
NLG UPLOCK SUPPORT BRACKET IS CRACKED. R & R NLG UPPER SUPPORT BRACKET.
RAD/ALT FAIL IN FLIGHT. DEFERRED RAD ALT NR 1. R&R RA ANTENNAS. OPS CHECK GOOD.
PACK 1 OFF DURING FLIGHT NO OTHER ASOCIATED EICAS MESSAGES, PACK 2 ALREADY ON DEFERRAL. RESEALED EXHAUST DUCT FROM HEAT EXCHANGER. OPS CHECK GOOD.
PASSENGER NOTICED FUEL LEAKING FROM THE LEFT WING DURING FLIGHT. FIRST OFFICER VERIFIED FUEL LEAKING FROM THE LEFT WING. CAPTAIN REPORTED LOST 50 LBS FROM THE LEFT WING WITHIN 10 MINUTES. INSPECTED THE LEFT WING FOR LEAKS, FOUND TO BE TYPE 1 RUNNING LEAK, SEALED THE LT FUEL TANK, .LEAK CHECKED GOOD.
LEFT WINDSHIELD WIPER FLOPPING AND MOVING LATERALLY DURING CLIMB AND LEVEL FLIGHT. FOUND WIPER OVERHEAD CONTROL PANEL ASSY CONNECTOR OUT OF PLACE AND SECURED IT. OPS CHECKED GOOD.
AHRS 1 FAIL IN FLIGHT. R&R NR 1 AHRS COMPUTER, OPS CHECK GOOD.
LEFT OVERWING EMERGENCY SIGN WAS INOPERATIVE. FOUND THE LT OVERWING EMERGENCY SIGN CONNECTOR WAS LOOSE. CONNECTED, OPS CHECKED GOOD.
LT UPPER EMERGENCY DOOR EXIT LIGHT INOP. R&R NR 3 EMERGENCY LIGHT BATTERY, OPS CHECK GOOD.
NR 1 ENGINE OIL PRESSURE RAPIDLY FLUCTUATED TO ABOUT 163 PSI ABOVE 27000. PRESSURE BECAME NORMAL AGAIN BELOW 27000. R & R THE NR 1 PRESSURE TRANSDUCER, OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED.
EMERGENCY EXIT LIGHT IN PSU PANEL AT 18CD LIGHT 22 IS INOPERATIVE. R & R EMERGENCY LIGHT BULB AT 18CD. OPS CHECK GOOD.
HYD SYSTEM 2 FAIL IN FLIGHT. R & R NR 2 HYD PUMP ENG PRESSURE LINE. OPS AND LEAK CHECK GOOD.
BLEED 2 LEAK. R & R BLEED SEALS. LEAK AND OPS CHECK GOOD.
LEFT EMERGENCY EXIT DOOR MARKER NR 23 IS INOPERATIVE. UPON INSPECTION, FOUND ELECTRICAL CONNECTORS TO BE DISCONNECTED. CONNECTED THE CONNECTORS. OPS CHECKED GOOD.
CEILING EMERGENCY EXIT SIGN AT ROW 18, AFT SIDE, LIGHT 18B IS INOPERATIVE. RE-CONNECTED THE PIN CONTACT FOR CEILING EMERGENCY EXIT SIGN AT ROW 18, AFT SIDE, LIGHT 18B. OPS CHECK GOOD.
PASSENGER REPORTED THERE WAS SOMETHING STREAMING FROM WING DURING CRUISE, RETURNED TO BLOCK. MAINTENANCE PERFORMED GVI OF WING FOR LEAKS, NO DEFECTS NOTED.
PILOT REPORTED A STRONG BURNING ODOR NEAR SEAT 1A WHEN THE ACFT WAS POWERED UP. MX R & R THE CABIN LIGHTING CONTROL MODULE ASSY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
DURING MX INSPECTION THE LT SIDE OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MX R & R LAMP, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
THE CREW REPORTED CABIN SMOKE. MAINTENANCE INSPECTED AND REPLACED THE SIDE WALL LIGHT FIXTURE BRACKET AT SEAT 10A. OPS CHECKED WERE GOOD.
LOWER TCAS ANTENNA BASE CORRODED. R & R LOWER TCAS ANTENNA IAW AMM 34-43-03.
FLOOR SUPPORT AT Y0.0 X 8154.0 IS CORRODED. BLENDED CORROSION ON FLOOR SUPPORT. ALLOWABLE MATERIAL LOSS IS LESS THAN 30 PERCENT. MATERIAL LOSS WAS .008". FOUND TO BE WITHIN LIMITS IAW SRM 53-22-10.
FLOOR SUPPORT AT Y0.0 AND X 6723.0 IS CORRODED. BLENDED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-21-10.
LEFT SILL AT STGR 15L AND X16783.5 IS CORRODED. BLENDED LT SILL AT STGR 15L AND X16783.5 IAW SRM 53-23-10. FOUND TO BE WITH-IN ALLOWABLE LIMITS IAW SRM 53-23-10.
RIGHT FLOOR SUPPORT JUST AFT OF SERVICE DOOR AT S15R X-6723.0 IS CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-02.
RIGHT STRINGER 15 BETWEEN BS 11016.4 AND 11388.8 IS CORRODED. BLENDED CORROSION ON RT STRINGER. ALLOWABLE MATERIAL LOSS IS 30 PERCENT MATERIAL LOSS WAS .008". FOUND TO BE WITHIN LIMITS IAW SRM 53-22-10.
FLOOR SUPPORT AT Y0.0 AND X14513.6 IS CORRODED. R & R CENTER FLOORBEAM GUSSET BETWEEN FRAMES 39-46 IAW SRM 51-40-02.
AFT AVIONICS DOOR, FORWARD PIN FUSELAGE BRACKET IS GOUGED. BLENDED GOUGE WITH .010 MATERIAL LOSS IAW EMB ETD2014-145-024302 AND EXPRESSJET EC5330-02878, REV ORIG, DATED 24 MAR 2014. NDT PERFORMED BY KB INSPECTION SERVICES, CRS# K9QR554B ON 24 MAR 2014. AVMAX WORK ORDER 80210; WORK CARD 2269. DMI CREATED TO ACCOMPLISH TASK 53-31-00-220-838-A00 AT INTERVAL OF 4,520 FC. NEXT INSP DUE AT 21,156FC.
AFT FUSELAGE AFT AVIONICS DOOR HAS GOUGES AT HANDLE CUTOUT EDGE. BLENDED OUT 3 GOUGES AT HANDLE CUTOUT EDGE WITH DIMENSION OF 1.1" LONG BY .075" WIDE IAW ETD2014-145-022223 AND EC5230-01323, REV, ORIG, DATED 19 MAR 2014. NDT PERFORMED ON 18 MAR 2014. THIS REPAIR HAS RECURRING INSPECTION AND A DMI CREATED FOR ACCOMPLISHMENT OF TASK 52-44-00-220-801-AOO AT AN INTERVAL OF 10,000 FC.
CREW REPORTED A POSSIBLE FUEL LEAK FROM THE RT WING. ACFT RETURNED TO DEPARTURE WITHOUT INCIDENT. MAINTENANCE R & R FLAPPER VALVE AT RIB 19 ON THE RT WING, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
DURING SCHEDULED MX INSPECTION THE AFT CEILING EMERGENCY LIGHT ABOVE ROW 12 WAS FOUND INOPERATIVE. MX R & R THE CEILING EMERGENCY LIGHT LAMP WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
THE CREW REPORTED A BLEED OVERTEMP IN CLIMB. THE ACFT RETURNED TO DEPLARTURE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NR 1 PRECOOLER. OPS CHECKED GOOD.
IAH - FLIGHT 4348 THE CREW REPORTED A SMOKE SMELL IN THE CABIN. MAINTENANCE COMPLIED WITH FIM TASK 72-00-00-810-814 WITH NO DEFECTS OR SMELL NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
IAH - DURING MAINTENANCE INSPECTION THE CEILING PANEL OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
EWR FLT 2162 THE CREW REPORTED THE ISIS FAILED IN FLIGHT. SCREEN WENT BLANK. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ISIS CONTROL UNIT AND OPERATIONAL CHECKS WERE GOOD.
FLIGHT 2685 - FLIGHT CREW REPORTED LANDING GEAR AIR/GROUND SYSTEM FAIL ON ROTATION DURING T/O. EWR MX REMOVED AND REPLACED LGEU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
IAH - FLIGHT 2122, THE CREW REPORTED THAT THE THRUST RATING SETTINGS WOULD NOT RESPOND CORRECTLY. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE POWERPLANT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
TYS - RT MLG HOLLOW PIN FWD BEARING HOUSING IS SCRATCHED/GOUGED ACROSS WIDTH AT THE 4 O'CLOCK AND 8 O'CLOCK POSITION. REMOVED AND REPLACED RT FWD SIDE BRACE FITTING IAW EC5750-01418.
TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RT FLOOR SILL CORRODED AT FR.60. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 145XR SRM 51-40-02, 06;5120-03. ALODINED IAW EMB 135/145 CPM 51-21-04. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RT FLOOR SILL CORRODED FROM FR 48 TO FR 52. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 145XR SRM 51-40-02;09, 51-20-03 AND CPM 51-21-07. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
TYS - AFT SERVICE DOOR SILL CORRODED AT FWD END. REMOVED AND REPLACED AFT SERVICE DOOR SILL.
FLIGHT 2245 - FLIGHT CREW REPORTED TAT NR 1 HEAT INOP INDICATION ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. MX R & R NR 1 TAT PROBE AND PERFORMED OPS CHECK SUCCESSFUL. ACFT APPROVED TO RETURN TO SERVICE.
FLIGHT 3070 - EWR - DURING PREFLIGHT, FLIGHT CREW FOUND EMERGENCY LIGHT STRIP BROKEN. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
FLIGHT 2355 - EWR - DURING PREFLIGHT CHECK, FLIGHT CREW REPORTED RED MARKING MISSING ON THE EMERGENCY FLOOR STRIP. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT FLOOR STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
FWD EMERGENCY LIGHT INOPERATIVE. AND REPLACED NR 1 & NR 2 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04. OPS CHECK GOOD. NOTE: AC HAS BEEN IN C-CHECK SINCE 8/26. (K)
AC IS CURRENTLY IN C-CHECK AND THE RT AILERON SHROUD BONDING STRAPS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE BONDING STRAP PLATE IAW EC 575001315. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (K)
AC IS CURRENTLY IN C-CHECK AND THE LT AILERON SHROUD BONDING STRAPS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE BONDING STRAP PLATE IAW EC 5750-01315. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (K)
ACFT WAS EN ROUTE TO EWR FROM LIT WHEN THE DV WINDOW SEAL STARTED SQUALLING. CREW DIVERTED THE FLIGHT TO TYS WHERE MAINTENANCE REPOSITIONED THE DV WINDOW SEAL ON THE CAPTAINâS SIDE. LEAK CHECK GOOD AND SIGNED OFF TO SERVICE. (S)
FLIGHT 2358 - EWR - FLIGHT CREW REPORTED STRONG FUEL ODOR IN THE ACFT. EWR MX REMOVED AND REPLACED APU SECONDARY FUEL MANIFOLD ASSEMBLY IAW ENGINE MANUAL 49-31-06 AND PERFORMED OPERATIONAL AND LEAK CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. (A)
RIC - DURING ROUTINE INSPECTION, RIC MX FOUND BOTTOM EXIT SIGN AT SEAT 12C INOPERATIVE. MX REMOVED AND REPLACED SIGN AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
CLE FLIGHT 2034 - THE CREW REPORTED A HIGH STAGE VALVE 2 FAIL MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE HIGH STAGE BLEED VALVE AND SWITCH. OPERATIONAL CHECKS WERE GOOD.
IAH - FLIGHT 2533, THE CREW REPORTED THAT THE APU CAUSES FUEL SMELL IN THE CABIN AND COCKPIT. MAINTENANCE PLACED THE APU ON MEL 49-00-00 CAT-C CTL NR 134748, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. IN BNA, MAINTENANCE TIGHTENED LOOSE FUEL LINE AT APU FUEL CONTROL IAW VCMM HAM SUN 49-32-01 MM. OPS CHECK AND LEAK CHECK GOOD.
IAH - FLIGHT 2680, THE CREW REPORTED THAT AFTER STARTING THE APU ON THE GROUND, AND OPENING APU BLEED AIR, THERE WAS A STRONG ODOR OF JET FUEL IN THE CABIN. THE AIRCRAFT CONTINUED TO THE GATE WHERE MAINTENANCE OPERATIONALLY CHECKED THE APU WITH NO DEFECTS, OR ODORS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
DURING ROUTINE MAINTENANCE THE RIGHT FORWARD EMERGENCY LIGHT WOULD NOT ILLUMINATE. THE NR 2 EMERGENCY BATTERY LIGHT POWER SUPPLY WAS REPLACED. OPERATIONAL CHECKS WERE GOOD.
FLT 2887, DURING SCHEDULED MAINTENANCE THE RT OVERWING EMERGENCY EXIT LIGHT DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY POWER SUPPLY, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY.
MCI - DURING MAINTENANCE INSPECTION, THE FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
CLE FLIGHT 2034 - THE CREW REPORTED THE EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING TESTING. MAINTENANCE INSPECTED AND RESECURED THE CONNECTOR ON THE EMERGENCY EXIT SIGN. OPERATIONAL CHECKS WERE GOOD.
IAH - THE CREW REPORTED A LAV SMOKE DETECTOR INDICATION IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A LOOSE CONNECTOR ON THE SMOKE DETECTOR PANEL. MAINTENANCE RESECURED THE CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.