N21144
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
AT EMERGENCY EXIT ROW LH EXIT IDENTIFIER SIGN, LH AND RH EXIT MARKING SIGN AND OVERHEAD EXIT LOCATOR LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY #3. OPS CHECK SAT.
#2 EMERGENCY BATTERY INOPERATIVE. REMOVED AND REPLACED #2 EMERGENCY BATTERY. OPS CHECK GOOD.
L-SHAPE FRAME 65, DAMAGE FROM IMPACT. SPLICE REPAIR ON LH REAR FUSE I FRAME 65 SHEAR CLIP BTW STR 14L-15L
LH FR 65 BTW STR 14-15 FOUND CORRODED. CORROSION LEVEL 1. SPLICE AND FRAME SECTION FABRICATED. SPLICE REPAIRED ON LH REAR FUSE I FRAME 65 BTW STR 14L-15L
SHEAR CLIP FOUND CRACKED AT FR66 BTW STR 7L-9L. SHEAR CLIP FABRICATED WITH ALTERNATE MATERIAL. SHEAR CLIP INSTALLED.
SHEAR CLIP FOUND CRACKED ON FR 72 BTW STR 8R-10R. SHEAR CLIP FABRICATED WITH ALTERNATE MATERIAL. SHEAR CLIP INSTALLED.
RH OMEGA BEAM AT FR 22 CORROSION FOUND AROUND ANCHOR NUT HOLE. REPAIR DOUBLER ON CENTER FUSE I RH OMEGA BEAM, ON UPPER SURFACE AT FR 22
CENTER FUSE IV, FRAME 53 CRACKED AT STR 7R. SPLICE REPAIR ON CENTER FUSE IV FRAME 53 AT STR 7R. SPLICE FABRICATED.
IN REAR FUSELAGE COMPARTMENT AT BULKHEAD 80 ON RH SIDE BTW STR 6 AND 7 FOUND 1 BUSHING DAMAGED ON SKIN SIDE. BUSHING REPLACED
LH WING #1 LEADING EDGE, DENT FOUND 36" FROM INBD EDGE. REPAIR DOUBLER ON LH WING LEADING EDGE #1 BTW RIB YS=723-YS=991 REPAIRED
CF4 RH OMEGA BEAM X2 ANCHOR NUT LOCATION FOUND CRACKED, BTW FR 59-61. CF4 RH OMEGA BEAM FR 59-61 X2 CUTOUT PERFORMED. CF4 RH OMEGA BEAM BTW FR 59-61 REPAIR PEROFRMED.
SERVICE DOOR LOWER BEAM FOUND CORRODED BTW FR 20-22. REPAIR DOUBLER ON CENTER FUSE I SERVICE DOOR LOWER SILL ON CENTER SECTION
LH OMEGA BEAM FOUND CRACKED AT FR21. LH OMEGA BEAM AT FR21 REPAIRED.
CF3 MIDDLE OMEGA BEAM, RH ANGLE FOUND CORRODED. CF3 MIDDLE OMEGA BEAM, RH ANGLE BLENDED OUT OF LIMITS. CF3 MIDDLE OMEGA BEAM RH ANGLE REMOVED AND REPAIR COMPLETED
EXTERNAL REAR FUSE I, CRACK FOUND FRAME 75 BTW STR 2L-3L. REPAIR DOUBLER ON LH REAR FUSE I SKIN, AT FR 75 AT STR 2L
CF4 LH GUSSET BTW FR 59-61 FOUND CORRODED. CF4 LH GUSSET BTW FR 59-61 BLENDED OUT OF LIMIT AND REMOVED FOR REPLACEMENT. CF4 LH GUSSET BTW FR 59-61 REPLACED.
EXTERNAL FWD FUSE, DENT FOUND 3 INCH AFT FRAME 1A AND 3 INCHES BELOW STR 15R. DENT ON SKIN 3 INCH AFT OF FR 1A AND 3 INCH BELOW STR 15R REPAIRED WITH DOUBLER. ALSO NOTICED 7 PREVIOUS REPAIRS FOUND ON SKIN BTW FR 1A-2 BTW STR 13R-17R. 2 REPAIRS FOUND WITH ELONGATED HOLES AND 5 REPAIRS FOUND WITH KNIFE EDGE HOLES. SKIN REPAIRED WITH 6 RIVET PLUGS AND 1 BUSHING.
CF4 MIDDLE GUSSET BTW FR 59-61 FOUND CORRODED. CF4 MIDDLE GUSSET, BTW FR 59-61 REMOVED. LATE ENTRY, CF4 MIDDLE GUSSET BTW FR 59-61 BLENDED OUT OF LIMIT. CF4 MIDDLE GUSSET BTW FR 59-61 REPLACED
CF4 RH GUSSET BTW FR 59-61 FOUND CORRODED. CF4 RH GUSSET BTW FR 59-61 BLENDED OUT OF LIMIT. CF4 RH GUSSET BTW FR 59-61 REMOVED AND INSTALLED
EXTERNAL RF II, CRACK FOUND FRAME 77 BTW STR 8L-9L. BUSHING REPAIR ON LH REAR FUSE II SKIN, AT FR 77 BTW STR 8L-9L
EXTERNAL RF II, CRACK FOUND FRAME 78 BTW STR 5L-6L. BUSHING REPAIR ON LH REAR FUSE II SKIN, AT FR 78 BTW STR 5L-6L
EXTERNAL REAR FUSE 1, CRACK (X2) FOUND FRAME 77 BTW STR 9R-8R AND BTW STR 5R-7R. 2 BUSHING REPAIRS ON RH REAR FUSE II SKIN, AT FR77 BTW STR 6R-7R AND STR 8R-9R
CF4 MIDDLE OMEGA BEAM X2 ANCHOR NUT LOCATION FOUND CRACKED, BTW FR 59-61. CF4 MIDDLE OMEGA BEAM BTW FR 59-61 X2 CUT OUT PERFORMED. CF4 MIDDLE OMEGA BEAM BTW FR 59-61 REPAIR PERFORMED
IN REAR FUSELAGE COMPARTMENT, AT BULKHEAD 80, RH SHEAR CLIP CRACKED BETWEEN STRINGERS 5 AND STRINGERS 7. IN REAR FUSELAGE COMPARTMENT AT BULKHEAD 80. RH SHEAR CLIP REMOVED FOR REPLACEMENT BTW STR 5-7. IN REAR FUSELAGE COMPARTMENT AT BULKHEAD 80, RH BTW STR 5-7 SHEAR CLIP REPLACED
CF4 LH OMEGA BEAM BTW FR 59-61, ANCHOR NUT LOCATION FOUND CRACKED. CF4 LH OMEGA BEAM BTW FR 59-61, CUTOUT PERFORMED. CF4 LH OMEGA BEAM BTW FR 59-61 REPAIR PERFORMED
NLG UPLOCK TOP AFT CROSSBEAM CRACKED. NLG UPLOCK TOP AFT CROSSBEAM REMOVED AND REPLACED.
CF4 TOILET CUP CORRODED. CF4, TOILET CUP BLENDED OUT OF LIMIT. TOILET HINGED REMOVED AND FOUND CRACKED. TOILET CUP REMOVED AND REPLACED. TOILET HINGE REPLACED AND REINSTALLED
CF4 LH AT FR 60 SHEAR CLIP FOUND CRACKED BTW STR 15L-16L. CF4 LH AT FR60 BTW STR 15L-16L, SHEAR CLIP REMOVED AND REPLACED WITH LOCALLY FABRICATED PART
CF3 UNDERFLOOR AT FR46 LH ANGLE FOUND CRACKED. CF3 UNDERFLOOR AT FR46 LH ANGLE REMOVED AND REPLACED
NLG FWD CROSSBEAM FOUND CRACKED. NLG FWD CROSSBEAM REMOVED AND REPLACED.
CF3 RH OMEGA BEAM OUTBD ANGLE FOUND CRACKED. REMOVED RH OMEGA BEAM OUTBD ANGLE FOR REPLACEMENT. NEW ANGLES INSTALLED ON RH OMEGA BEAM OUTBD SIDE
LH INTERCOSTAL ON NLG UPLOCK ASSEMBLY FOUND CRACKED. LH INTERCOSTAL ON NLG UPLOCK ASSEMBLY REPLACED
REAR FUSE 1, FRAME 71, SHEAR CLIP FOUND CRACKED BTW STR 18L-17L. REAR FUSE I, FRAME 71, SHEAR CLIP REPLACED.
EXTERNAL RF II CRACK FOUND FRAME 79 BTW STR 4R-3R AND BTW STR 4R-5R. REPAIR DOUBLER ON RH REAR FUSE II SKIN, AT FR79 BTW STR 3R-5R.
RH OMEGA BEAM TOP DOUBLER FOUND CORRODED AT FR 22. RH OMEGA BEAM TOP DOUBLER AT FR22 BLENDED OUT OF LIMITS. RH OMEGA BEAM TOP DOUBLER AT FR22 REMOVED AND REPLACED
CF1, LH OMEGA BEAM FOUND CORRODED AT FR20. CF1, LH OMEGA BEAM AT FR20 BLENDED OUT OF LIMITS. CF1, LH OMEGA BEAM CUT OUT PERFORMED. CF1, LH OMEGA BEAM REPAIRED
REAR FUSE I, FRAME 73, SHEAR CLIP BTW STR 16L-17L FOUND CORRODED. REAR FUSE I, FRAME 73, SHEAR CLIP BTW STR 16L-17L REPLACED WITH NEW PART.
REAR FUSE I, FRAME 65, SHEAR CLIP FOUND CRACKED BTW STR 19L-18L. RF1, FR65, SHEAR CLIP BTW STR 19L-18L REMOVED AND REPLACED
CENTER FUSE IV, RH SILL BTW FRAME 53-59 FOUND CORRODED. CENTER FUSE IV, RH SILL BTW FRAME 53-59 CORROSION BLENDED AND FOUND OF OF LIMIT. CENTER FUSE IV RH SILL BTW FRAME 53-59 REMOVED AND REPLACED
CF3 RH GUSSET #5 BTW FR 46-52 FOUND CORRODED. CF3 RH GUSSET #5 BTW FR 46-52 BLENDED OUT OF LIMITS. CF3 RH GUSSET #5 BTW FR 46-52 REPLACED
REAR FUSE I, FRAME 72, SHEAR CLIP BTW STR 18L-17L FOUND CRACKED. REAR FUSE I, FRAME 72 SHEAR CLIP BTW STR 18L-17L REPLACED
CF2 LH SILL #2 FOUND CORRODED BTW FR 23-29. CF2 LH SILL #2 BTW FR 23-29 BLENDED OUT OF LIMITS. CF2 LH SILL #2 BTW FR 23-29 REMOVED AND REPLACED
REAR FUSE I, FRAME 72 SHEAR CLIP BTW STR 16L-17L FOUND CRACKED. ON REAR FUSE I, FR 72 SHEAR CLIP BTW STR 16L-17L REMOVED AND REPLACED
CF3, LH SILL #4 BTW FR 35-41 FOUND CORRODED. CF3 LH SILL #4 BTW FR35-41 CORROSION BLENDED AND FOUND OUT OF LIMITS, CF3 LH SILL #4 BTW FR 35-41 REMOVED AND REPLACED
BIRD STRIKE ON FWD FUSELAGE OF MAIN BATTERY COMPARTMENT DOOR LOWER CORNER COMPLY WITH PERMANENT REPAIR. REPAIR DOUBLER ON LH FWD FUSE I SKIN, BTW FR 3-4 AND BTW STR 15L-17L
SHEAR CLIP FOUND CRACKED ON FR 73 BTW STR 9R-11R. ON FR73 BTW STR 9R-11R SHEAR CLIP REMOVED AND REPLACED
CF2 RH AT FR26, SHEAR CLIP FOUND CRACKED BTW STR 15-16. RH AT FR26 BTW STR 15-16, SHEAR CLIP REMOVED AND REPLACED
ALL 3 CARGO DOOR SUPPORT BRACKETS FOUND CRACKED BTW FR 67-68 AND STR 4R-5R. DOOR SUPPORT BRACKET BTW FR 67-68 AND STR 4R REPLACED. DOOR SUPPORT BRACKET BTW FR 67-68 BTW STR 4R-5R REMOVED AND REPLACED. DOOR SUPPORT BRACKET BTW FR 67-68 STR 5R REPLACED.
CENTER FUSE IV, CENTER GUSSET BTW FRAME 53-59 FOUND CORRODED. CF4, CENTER GUSSET BTW FR 53-59 BLENDED OUT OF LIMIT. CF 4 CENTER GUSSET BTW FR 53-59 REMOVED AND REPLACED.
CF2 RH AT FR25, SHEAR CLIP FOUND CRACKED BTW STR 15-16. RH AT FR25 SHEAR CLIP BTW STR 15-16 REMOVED AND REPLACED
CF2 RH AT FR27, SHEAR CLIP BTW STR 15-16 FOUND CRACKED. RH AT FR27 BTW STR 15-16, SHEAR CLIP REMOVED AND REPLACED
ALLY FLOOR SUPPORT ON CENTER OMEGA BEAM FOUND CRACKED AT FR20 UNDER CROSSBEAM. ALLY FLOOR SUPPORT ON CENTER OMEGA BEAM AT FR 20 REMOVED AND REPLACED
CENTER FUSE I, BTW FRAME 15-16 AND BTW 9R-7R, SUPPORT ASSEMBLY FOUND CRACKED. CENTER FUSE I BTW FRAME 15-16 AND BTW STR 9R-7R SUPPORT ASSEMBLY REMOVED AND REPLACED
LH AFT WW RIB FOUND CRACKED. LH AFT WW RIB REMOVED AND REPLACED
RH AFT WW RIB FOUND CRACKED. RH AFT WW RIB REMOVED AND REPLACED
EXTERNAL REAR FUSE 1, CRACK FOUND FRAME 75 BTW STR 2R-3R. REPAIR DOUBLER ON RH REAR FUSE I SKIN, AT FR 75 AT STR 2R
CENTER FUSE I, FRAME 15, SHEAR CLIP CRACKED BTW STR 15R-16R. CENTER FUSE I, FRAME 15 SHEAR CLIP CRACKED. REMOVED AND REPLACED.
CF2 LH AT FR25, SHEAR CLIP FOUND CRACKED BTW STR 15-16. CF2, LH SHEAR CLIP AT FR25 BTW STR 15-16 REPLACED
CF2 RH AT FR 24, SHEAR CLIP FOUND CRACKED BTW STR 15-16. RH SHEAR CLIP AT FR24 BTW STR 15-16 REPLACED
SHEAR CLIP FOUND CRACKED AT FR67 BTW STR 6R-7R. SHEAR CLIP AT FR67 BTW STR 6R-7R REPLACED
RH OMEGA BEAM TOP DOUBLER FOUND CORRODED AT FR20. RH OMEGA BEAM TOP DOUBLER AT FR20 REMOVED AND REPLACED. RH OMEGA BEAM TOP DOUBLER AT FR20 REPLACED
RH SILL FWD OR SERVICE DOOR CORRODED BTW FR 19A-20. RH SILL FWD BTW FR 19A-20 IS OUT OF LIMIT. RH SILL FWD BTW FR 19 AND 20 REMOVED AND INSTALLED
SHEAR CLIP FOUND CRACKED ON FR68 BTW STR 6L-9L. ON FR68 BTW STR 6L-9L SHEAR CLIP REMOVED AND REPLACED
SHEAR CLIP FOUND CRACKED ON FR 73 BTW 9L-11L. ON FR73 BTW STR 9L-11L SHEAR CLIP REMOVED AND REPLACED
SHEAR CLIP FOUND CRACKED AT FR66 BTW STR 6R-7R. AT FR66 BTW 6R-7R SHEAR CLIP REMOVED AND REPLACED
LG LEVER WOULD NOT GO UP AFTER TAKEOFF. SERVICED NLG. PERFORMED DVI OF ALL 3 LG PROX SWITCHES. JIGGLED CONNECTIONS BEFORE GEAR SWINGS. REMOVED AND REPLACED LGEU. OPS CHECK SAT. VERIFIED RH MLG WAS PROPERLY SERVICED. PERFORMED GEAR SWINGS WITH BREAKOUT BOX. AIRCRAFT RELEASED FOR OCF. OCF SATISFACTORY.
LANDING GEAR WOULD NOT COME UP AFTER TO, LG A/GND FAIL ON EICAS. CONNECTED BREAKOUT BOX AND PERFORMED MULTIPLE GEAR SWINGS. FOUND RH LANDING GEAR TRAILING ARM PROX SWITCH INOPERATIVE. REMOVED AND REPLACED LANDING GEAR TRAILING ARM PROX SWITCH. OPS CHECK SAT. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER. PERFORMED GEAR SWINGS WITH NO FAULTS FOUND. OPS CHECK SAT. CHECKED PROXIMITY SENSOR GAPS AND ALL WERE WITHIN LIMITS. ALL CANNON PLUGS WERE SECURE. NO DEFECTS NOTED. INSPECTED ALL 3 GEARS AND ENSURED THAT SERVICING IS CORRECT. NO DEFECTS NOTED. VERIFIED CANNON PLUG PINS ON PROX SWITCHES TO CHECK FOR BENT PINS. NO DEFECTS NOTED. ENSURED ALL CANNON PLUGS WERE ON CORRECT AND TIGHT.
AFTER RUNNING QRH FOR I/A FAIL SMOKE IN COCKPIT. PERFORMED OPS CHECK OF DISTRIBUTION SYSTEM AND PACKS. NO DEFECTS OR SMOKE NOTED.
EMERGENCY LIGHTS OVER EXIT ROW 18 WILL NOT ILLUMINATE DURING TEST. RESET SYSTEM, GROUND FUNCTIONAL CHECK GOOD.
MCD WILL NOT OPEN FROM OUTSIDE. OPEN MAIN CABIN DOOR FROM OUTSIDE, OPS CHECK GOOD.
EMERGENCY LIGHT BATTERIES DEAD. REMOVED AND REPLACED #2, #3 AND #4 EMERGENCY LIGHT BATTERIES. OPS CHECK SAT. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM. OPS CHECK SAT.
AILERON STIFF / BINDING SENSATION IN FLIGHT. AUDIBLE GRINDING WHEN ROLLING. R/R R/H I/B AILERON CABLE PULLEY AT FRAME 15. PERFORMED AILERON CONTROL CABLES ADJUSTMENT/TENSION, OPS CHECK SAT
RAPID DECOMPRESSION OCCURRED AT 32,000 FT. INITIATED EMERGENCY DECENT. PERFORMED GVI FUSELAGE COCKPIT EMERGENCY EXITS, MCD VENT PANEL, SERVICE DOOR VENT PANEL AS WELL AS CARGO DOOR VENT PANEL. INSPECTED AFT AVIONICS COMPARTMENT DOOR AND FWD ACCESS HATCH. NO OBVIOUS DEFECTS PRESENT. PERFORMED GVI OF THE GROUND AIR START AND AIR CONDITION VALVE GVI OF BOTH PACKS DUCTS AND COUPLINGS. GVI OF BOTH OUTFLOW VALVES. REMOVED HARDWARE FROM TWO OF FWD AC DRAIN VALVES. PERFORMED PRESSURIZATION ADJUSTMENT AND TEST OF THE AIRCRAFT IN MANUAL MODE AND AUTO MODE. PERFORMED TEST FOR CABIN LEAKAGE. OPS AND LEAK CHECKED GOOD. NO FURTHER DEFECTS NOTED
MAIN CABIN - CORROSION - AT LH IB SIDE OF THE FLOOR SUPPORT RT LH FR 35-FR38. REMOVED AND REPLACED LH IB FLOOR STRUCTURE AT FR35-FR38
CORROSION ON CENTER FUSELAGE I SERVICE DOOR SILL SCUFF PLATE SUPPORT BEAM FR 20-21 AND Y = +30". EVALUATED CORROSION ON CENTER FUSELAGE I SERVICE DOOR SILL SCUFF PLATE SUPPORT BETWEEN FR 20-21 AND Y = +30" AND FOUND 100% MATERIAL LOSS. REMOVED AND REPLACED SERVICE DOOR SILL SCUFF PLATE SUPPORT
MAIN CABIN - INTERNAL - FASTENERS HAVE CORROSION ON SHEAR TIE - AT FWD SIDE OF LH FR 51 BETWEEN STGR 18 AND STGR 19. REMOVED AND REPLACED SHEAR CLIP AT FRAME 51 LH BETWEEN STRINGER 18 AND STRINGER 19.
NLG - INTERNAL - UPLOCK SUPPORT STRUCTURE - FWD CROSSBEAM CRACKED. REMOVED AND REPLACED NLG - INTERNAL - UPLOCK SUPPORT STRUCTURE - FWD CROSSBEAM
CENTER FUSELAGE I REINFORCEMENT PLATE IS CRACKED BETWEEN FR14 AND FR 15 AND Y = .32". REMOVED AND REPLACED REINFORCEMENT PLATE AT CENTER FUSELAGE BETWEEN FR 14 AND FR 15 AND Y = .32"
FLOOR BEAM HAS CORROSION AT SCREW HOLES FOR FLOOR PANEL 261DF. REMOVED AND REPLACED GUSSET AT FR59-FR61
CORROSION IN CARGO COMPARTMENT DOOR CUTOUT AFT LOWER SILL HAS 3 SPOTS AT FR65-FR68. REMOVED AND REPLACED COMPARTMENT DOOR LOWER SILL.
MAIN CABIN - INTERNAL - LH OMEGA BEAM LOCATED BETWEEN FR 15 - FR 23 CRACKED AT AFT END OF LOWER IB FLANGE. REPAIRED MAIN CABIN - INTERNAL - LH IB OMEGA BEAM LOCATED BETWEEN FR15-FR23
MAIN CABIN - INTERNAL - CENTER FLR SUPPORT BEAM - IB (LWR) FLANGE HAS CORROSION AT RH FR50. REMOVED AND REPLACED MAIN CABIN INTERNAL CENTER FLR SUPPORT BEAM AT RH FR50
2 FASTENERS REQUIRE REMOVAL AND INSTALLATION ON LH AND RH PYLON YOKES UPPER FLANGE. REMOVED EXISTING FASTENERS FROM BOTH #1 AND #2 PYLON SPAR II YOKE. REWORK TO BOTH #1 AND #2 PYLON SPAR II YOKE RIVET HOLES BY INSTALLING BUSHLOC BUSHINGS
MAIN CABIN - INTERNAL - CORROSION AT LH IB FLOOR SUPPORT BEAM AT FR23 - FR29. REMOVED AND REPLACED MAIN CABIN LH OMEGA BEAM FROM FR23-FR29
MAIN CABIN - INTERNAL - CORROSION - AT RH IB SIDE OF THE CENTER FLOOR SUPPORT BEAM - RH FR35-FR39. REMOVED AND REPLACED MAIN CABIN CENTER OMEGA BEAM FROM FR35-FR39
MAIN CABIN - INTERNAL - CORROSION - AT CENTER FLR STRUCTURE IB SIDE HAS CORROSION FR39-FR44. REMOVED AND REPLACED MAIN CABIN OMEGA BEAM, CENTER FLR STRUCTURE IB SIDE FR39-FR44
CORROSION ON ANGLE AT CARGO DOOR CUTOUT STA X22010.2 FWD FRAME LOWER BETWEEN STRG 16L AND STRG 17L COMMON TO FUSELAGE SKIN. REPAIRED CARGO DOOR CUTOUT STA X22010.2 FWD FRAME LOWER ANGLE SEGMENT SHEAR CLIP AT FRAME 65 BETWEEN S15L AND S18L
MAIN CABIN - INTERNAL - CORROSION - AT RH IB SIDE OF IB FLR SUPPORT BEAM BETWEEN FR 23-FR29. REMOVED AND REPLACED OMEGA BEAM ASSY IN MAIN CABIN INTERNAL RH IB SIDE FR23 - FR29
MAIN CABIN - INTERNAL - CORROSION AT RH IB SIDE OF IB FLOOR SUPPORT BEAM AT FR31 - FR35. REMOVED AND REPLACED OMEGA BEAM ASSY MAIN CABIN - INTERNAL - CORROSION AT RH IB SIDE AT FR31 - FR35
MAIN CABIN - CORROSION - AT LH IB FLOOR STRUCTURE - IB SIDE HAS CORROSION FROM FR 39 - FR 44. EVALUATED CORROSION ON LH IB FLR STRUCTURE IB SIDE FROM FR39-FR44, FOUND TO HAVE 100% MATERIAL LOSS. REMOVED AND REPLACED OMEGA BEAM
COCKPIT UPPER FRAME 10 CRACKED. REMOVED AND REPLACED COCKPIT UPPER FRAME 10 OVERHEAD PANEL.
AISLE SIDE FRAMES CRACKED ON SEAT 3A, 7A, 8A, 10A, 19A, AND 21A. RR SEATS 3A, 7A, 8A, 10A, 19A, AND 21A.
DENT ON LOWER REAR FUSE 2, BETWEEN FR 77-80 AND BETWEEN STR 21L-21R. REPAIRED DENT ON LOWER FUS-2 BETWEEN FR 77-80 & BETWEEN STR 21L-21R.
REPAIR DOUBLER ON LT CENTER FUSE 1, BETWEEN FR 19-20 AND BETWEEN STR 11L-12L. DOUBLER REPAIR ON LT CENTER FUS-1, BETWEEN FR 19-20 AND BETWEEN STR 11L-12L REWORKED.
APU FIRE INDICATION AND SMELL OF SMOKE IN CABIN AND COCKPIT---INSP APU AREA. NO SIGNS OF FIRE OR FUEL LEAKS. PERFORMEDAPU START UP. ISNP AGAIN NO DEFECTS NOTED. ADDITIONAL MX-- PERFORMED OPS CHECKS OF PACKS WITH AND WITHOUT ENG RUNNING, NO SIGNS OF SMOKE IN CABIN OR COCKPIT.
BREAK INBD INOP ON EICAS. PERFORMED FULL BLEED OF THE NORMAL BRAKE AND EMERGENCY PARKING BRAKE SYSTEMS. OPS CHECK GOOD AT THIS TIME.
MAIN DOOR EMERGENCY LIGHT LOCATED ON BOTTOM OF THE PLUG DOOR HINGE, IS INOP. R/R LIGHT BULB ON MAIN DOOR EXTERNAL EMERGENCY LIGHT ASSY.OPS CHECK GOOD.
RETURNED FROM FLIGHT. COCKPIT TEMP REACHED 37 DEGREES CELSIUS. FOUND COCKPIT DISTRIBUTION DUCT DISCONNECTED AT THREE POINTS. INSTALLED BLANKET COVERS AND RECONNECTED DUCTS. OPS CHECK GOOD.
ABORTED TAKEOFF FOR PACK 2 OVERHEAT WITH NOTICEABLE SMELL. AUTHORIZED PER MAINTENANCE CONTROL TO PERFORM MIP 1.76. NO FURTHER ACTION REQUIRED.
INBOARD BRAKE INOP EICAS ON APPROACH. R&R I/B BRAKE CONTROL VALVE, CARRIED OUT OPS CHECK AND LEAK CHECK. FOUND GOOD.
WING ANTI ICE FAIL MESSAGE ON EICAS IN ICING CONDITIONS. R/R E1 HIGH STAGE VALVE. OPS CHECK GOOD.
BLEED 1 LOW TEMP IN ICING CONDITONS. THRUST SETTING AT 88 PERCENT. MESSAGE WENT AWAY OUT IF ICING. R/R NR 1 LOW TEMP THERMOSTAT. OPS CHECK GOOD.
BRK INBD INOP. INSPECTED BRAKES AND WIRING FOR DEFECTS, NONE FOUND. R&R BRAKE CONTROL UNIT. PERFORMED ADJUSTMENT TEST OF BRAKE SYSTEM. SYSTEM OPS NORMAL.
BRAKES ON LEFT SIDE FULLY RELEASING WHILE HOLDING PRESSURE. R2 NR 1 BRAKE AND BLED LT BRAKES. PERFORMED TAXI CHECK AND FOUND NO FAULTS. OPS CHECK GOOD. MORE INFORMATION PROVIDED WHEN AVAILABLE.
APU SHUNT GND BURNT THROUGH SHEAR TIE. REAR FUSELAGE IIâ FRAME 80 APU SHUNTâ BURN DAMAGE - PERMANENT REPAIR. COMPLIED ON ETD2018-145-092121. DETAILS FOR THIS REPAIR HAVE BEEN EMAILED TO [email protected], WITH SUBJECT 21144 SDR RAIA201808280001.
MAIN PAX DOOR DIFFICULT TO OPEN. SERVICED MAIN DOOR MECHANISM AND OPS CHECK GOOD.
FUEL VENTING OUT OF RIGHT WING. R2 FUEL FLAPPER VALVE.
PAX DOOR SWING ARM EMERGENCY LIGHT (#1) LENS IS CRACKED. R & R PAX DOOR SWING ARM EMERGENCY LIGHT (#1) LENS. OPS CHECK GOOD.
MAIN CABIN DOOR DIFFICULT TO OPEN. LUBED MAIN DOOR ACTUATING AND LOCKING MECHANISM, OPS CHECK GOOD.
NR 1 ENGINE FIRE DETECTOR FAILED. R & R FIRE DETECTOR LOOP.
PRESSURIZATION IN AUTO MODE SPIKES UPON TURNING ON. R & R VACUUM PUMP VACUUM LINES. PERFORMED OPS CHECK OF PRESSURIZATION SYSTEM, OPS CHECK GOOD
BLEED 1 AND 2 OVERTEMP DURING CRUISE. R & R FAN AIR VALVE, OPS CHECKED GOOD.
PASSENGER DOOR FLOOD LIGHT HAS A CRACKED LENS. R & R THE LENS, OPS CHECKED GOOD.
PAX DOOR SWING ARM EMERGENCY LIGHT (1)LENS CRACKED. R & R PAX DOOR SWING ARM EMERGENCY LIGHT (1)ASSEMBLY, OPS CHECK GOOD.
HYDRAULIC SYSTEM 1 LOW QUANTITY AFTER GEAR RETRACTION LOSS OF PRESSURE ON LANDING SMOKE FROM NR 1 ENG REPORTED ON LANDING. SERVICED NR 1 HYD SYSTEM. R&R NR 1 EDP HYD LINE DUE TO HOLE IN LINE. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.
PAX DOOR EMERGENCY LIGHT IS INOPERATIVE. RESEATED THE LIGHT, OPS CHECKED GOOD.
CEILING CENTER CABIN EMERGENCY LIGHT FLICKERING. R&R CEILING CENTER CABIN EMERGENCY LIGHT OPS CHECK GOOD
SMOKE IN COCKPIT ON GROUND AFTER PUSHBACK, BOTH ENGINES RUNNING. MAINTENANCE PERFORMED FIM TASK 21-20-00 FOR UNKOWN SOURCE OF SMOKE AND ABNORMAL ODOR IN COCKPIT. PERFORMED ENGINE RUNS, INSPECTED ALL COMPONENTS, NO SMOKE OR ELECTRICAL ODOR WAS NOTICED, ACFT RELEASE FOR SERVICE.
NR 2 EMERGENCY BATTERY SUPPLY LOW VOLTAGE. R & R NR 2 BATTERY POWER SUPPLY, EMEGENCY. OPS CHECK GOOD.
COCKPIT CEILING EMERGENCY LIGHT INOPERATIVE. R & R COCKPIT CEILING EMERGENCY LIGHT. OPS CHECKED NORMAL.
BIRD STRIKE WAS DISCOVERED NEAR FRAME 8 AT STR 13L. MAINTENANCE CUTOUT THE DAMAGE AND PERFORMED A DOUBLER REPAIR, LEAK CHECKS WERE PERFORMED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
DURING INSPECTION, THE EMERGENCY EXIT LIGHT ON THE GALLEY SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 2 DC/AC INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
THE CREW REPORTED AN E2 FAILURE IN FLIGHT AND THAT THEY OBSERVED THE ITT REACH ABOVE 1000 ITT. THE ACFT RETURNED, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE NR 2 ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
DURING 3A CHECK, RT EMERGENCY OVERWING LIGHT INOPERATIVE. R & R RT OVERWING EMERGENCY LIGHT. OPS CHECK GOOD.
DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EXIT ROW CEILING LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE RESET THE ELECTRICAL SYSTEM ON THE ACFT, OPERATIONALLY TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01723. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
DURING C-CHECK, RT GROUND SPOILER UPPER ACTUATOR ATTACHMENT FITTING OTBD HAT BUSHING MIGRATED. MX R & R RT GROUND SPOILER UPPER ACTUATOR ATTACHMENT FITTING BRACKET IAW EC5740-01288, ORIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
DURING C-CHECK, LT SPEED BRAKE ACTUATOR FITTING HAT BUSHING MIGRATED. MX R & R LT SPEED BRAKE ACTUATOR FITTING HAT BUSHING IAW EC5740-01152, REV C. AND AMM 27-62-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
DURING C-CHECK, RUDDER ONE UPPER ATTACHMENT BRACKET HAS PLAY. MX R & R RUDDER UPPER HINGE FITTING ATTACHMENT BRACKET IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
DURING C-CHECK, RT GROUND SPOILER CENTER ATTACHMENT FITTING HAS MIGRATED HAT BUSHING. MX R & R RT GROUND SPOILER CENTER ATTACHMENT FITTING IAW EC5740-01288, REV ORIG AND EC5740-01152, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
DURING C-CHECK, RT GROUND SPOILER ACTUATOR HAS MIGRATED HAT BUSHING AT UPPER ATTACHMENT LUG. MX R & R RT GROUND SPOILER CENTER HINGE BRACKET IAW EC5740-01288 ORIG. ACFT APPROVED FOR RETURN TO SERVICE.
DURING C-CHECK, RT FRAME 10 CRACKED AT DV WINDOW. MX R & R RT FRAME 10 AT DV WINDOW IAW SRM 51-40-02 AND IAW CPM 31-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
DURING C-CHECK, RT SPOILER ACTUATOR UPPER OTBD HAT BUSHING MIGRATED. MX R & R RT GROUND SPOILER CENTER HINGE BRACKET IAW EC5740-01288 ORIG. ACFT RETURNED TO SERVICE.
DURING C-CHECK, LT SPEED BRAKE CENTER HINGE OTBD HAT BUSHING MIGRATED. MX R & R LT SPEED BRAKE CENTER HINGE OTBD HAT BUSHING IAW EC5740-01152, REV C AND AMM 27-62-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
DURING C-CHECK, RT GROUND SPOILER UPPER ACTUATOR ATTACHMENT FITTING INBD HAT BUSHING MIGRATED. MX R & R RT GROUND SPOILER CENTER HINGE BRACKET IAW EC5740-01288 ORIG. ACFT RETURNED TO SERVICE.
BURNING ODOR REPORTED IN CABIN. MX INSPECTED CABIN AND FOUND SIDEWALL LIGHT BALLAST AT 14A TO BE THE CAUSE. MX R & R BALLAST, OPS CHECKED SUCCESSFUL AND NO FURTHER BURNING ODORS. ACFT WAS APPROVED FOR RETURN TO SERVICE.
THE FORWARD FUSELAGE RT UPPER NOSE SKIN WAS DAMAGED BY BIRD IMPACT. R & R SKIN PANEL AND PERFORMED A TEST FLIGHT TO CONFIRM THE ACCURACY OF THE PITOT SYS. OPS CHECKED GOOD AND ACFT WAS RELEASED FOR SERVICE. FRAME 3 DAMAGED FROM BIRD STRIKE BETWEEN STRINGER 6R AND 9R. RECOUNTOURED FRAME, FABRICATED AND INSTALLED DOUBLERS.
RIC - DURING ROUTINE MAINTENANCE, MX FOUND LT OVERWING EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE RESET THE EMERGENCY LIGHTS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
CLE FLT 3013 THE CREW REPORTED A "ENG 1 REV DISAGREE" ON THE EICAS IN FLIGHT. ALSO REPORTED A SPOILER FAIL MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED RELAYS KO479 AND K1202. OPERATIONAL CHECKS WERE GOOD.
SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED AT FR 23. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-21-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV - DURING C-CHECK WORKING RIVETS ON RT FUSELAGE SKIN BETWEEN FR 77-79. REPAIRED SKIN IAW EC5330-02104. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV - DURING C-CHECK WORKING RIVETS ON LT FUSELAGE SKIN BETWEEN FR 77-79. REPAIRED SKIN IAW EC5330-02104. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV - DURING C-CHECK LT OMEGA BEAM CORRODED AT FR 38. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV - DURING C-CHECK LT PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT BRACKET IAW EC5750-01177. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV - DURING C-CHECK RT PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT BRACKET IAW EC5750-01177. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 24-25. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
FLIGHT 2829 - EWR - DURING CLIMBING, FLIGHT CREW REPORTED TAT 2 HEAT INOP INDICATION ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED TAT 2 PROBE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
FLIGHT 2075 - EWR - FLIGHT CREW REPORTED AIR/GRND FAIL MESSAGE ON EICAS WHEN LANDING GEAR EXTENDED. EWR MX CLEANED AND RE-SECURED RT MLG PROX SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
THE RT FORWARD FUSELAGE WAS STRUCK BY A BIRD JUST AFT OF FRAME 5. THE DAMAGE WAS CONTAINED BETWEEN FRMS 5 & 6, STR 11R & 13R. THE SKIN DEFLECTED INWARD OVER THE INTERSECTION OF 4 SKINS. FRM 6 WAS BUCKLED AT THE DAMAGED AREA BETWEEN STR 11 & 12. THE SKIN SPLICE STRAPS WERE ALSO DEFLECTED INWARD. MX CUT AND REMOVED DAMAGED SECTION OF FRM 6 BETWEEN STR 9 & 15R. CUT AND REMOVED DAMAGED SKIN SPLICE STRAPS BETWEEN STR 9 & 13R. RE-CONTOURED THE DENTED SKIN, PERFORMED NDT TO ASSURE THERE ARE NO CRACKS. SPLICED IN NEW SECTIONS OF STRAP AND A NEW SECTION OF FRM. REPAIRED IAW EC5330-01890. ACFT RELEASED AND RETURNED TO SERVICE.
IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT ON THE AFT GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE INVERTER, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
SHV - DURING C-CHECK THE INTERNAL SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 17 AND 19 AND STRINGERS 21L AND 21R. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145XR SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
E2 OIL IMP BYP ON EICAS ABOUT 10 MINUTES LATER HEARD NOISE, FELT VIBRATION AND MOVEMENT. NR 2 ENG ITT INDICATOR WENT DASHES, N1 WAS FLUCTUATING GREATLY THEN WENT TO APPROX 35% OIL QUANTITY INDICATION 5 QTS COMMANDED AN ENGINE SHUT DOWN AND DIVERTED TO TUS. MAINTENANCE REMOVED AND REPLACED NR 2 ENG. REF TASK CARD 6271001. OPS AND LEAK CHECK GOOD. AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. [07-27-07] ENGINE CONDITION REPORT RECEIVED AND DOCUMENTS NR 4 BEARING CAGE FRACTURE AS PART THAT ULTIMATELY FAILED AND CAUSED NR 2 ENGINE UNCOMMANDED SHUTDOWN.
IAH - FLIGHT 3034, THE CREW REPORTED A STRONG ODOR LIKE SOMETHING BURNING DURING THE LAST TEN MINUTES OF THE FLIGHT WHEN THE APU BLEED WAS SELECTED, AND THE ODOR EVENTUALLY WENT AWAY. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE PACKS AND APU WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
CREW REPORTED RUMBLING AND BURNING SMELL WHEN PACK NR 2 IS SELECTED IN BOTH MAIN AND AUTO MODE. MAINTENANCE FOUND BOTH AIR CONDITIONING DUCTS OFF AND MELTED, REMOVED AND REPLACED BOTH A/C DUCTS, REMOVED AND REPLACED OVER TEMPERATURE SWITCH AS A PRECAUTION IAW EMB 145 XR MM 21-20-04 AND 21-51-08, OPS CHECKED SYSTEM GOOD.
TUL - FLIGHT 2723, DURING CRUISE AT FLIGHT LEVEL 350, THE CREW REPORTED A NUMBER ONE ENGINE FAILURE. THE AIRCRAFT DIVERTED TO TUL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
CREW REPORTED, EMERGENCY LIGHTS CAME ON WHEN SIDE WALL CEILING LIGHTS ARE TURNED ON. MAINTENANCE FOUND GROUND STUD GS8008DC TO BE CORRODED. REBONDED STUD IAW EMB145 33-50-50. AFTER REPAIR FOUND NR 3 BATTERY PACK FOR EMERGENCY LIGHTS POSITION THREE WAS DISCHARGED. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK POSITION NR 3. OPS CHECKED EMERGENCY LIGHTING SYSTEM GOOD IAW EMB145 33-50-04. AIRCRAFT RETURNED TO SERVICE.
EMERGENCY LIGHTS STAYED ON IN ARM POSITION. DOWNPOWERED ACFT & RESELECTED ARMING SWITCH, EMERGENCY LIGHTS OPS CHECKED GOOD. AFTER ARRIVING, EMERGENCY LIGHTS ARE ON WHEN SWITCH IS IN THE ARM POSITION, WHEN F/A TURNS CABIN LIGHTS OFF EMERGENCY LIGHTS GO OFF. MX REMOVED & REPLACED ALL FOUR BATTERY PACKS, ACFT OPS CHECKED GOOD. ON PREFLIGHT, EMERGENCY LIGHTS COME ON WHEN SIDEWALL & CEILING LIGHTS ARE TURNED ON, EMERGENCY LIGHTS ARMED POSITION. MX REMOVED & REPLACED CONTROL MODULE ASSEMBLY WHICH DID NOT CURE PROBLEM. TROUBLESHOT DOWN TO FAULTY CANNON PLUG P8906, MEGAHOMED CANNON PLUG P8906, NO FAULTS FOUND. CLEANED METAL CHIPS OUT OF PLUG P8906, OPS CHECKED EMERGENCY LIGHTS GOOD. ACFT RETURNED TO SERVICE.
SDF - DURING 2A CHECK FOUND PAX DOOR PHOTOLUMINESCENT LIGHT STRIP COVER CRACKED. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP COVER. AIRCRAFT APPROVED AND RETURNED TO SERVICE.
CREW REPORTED, EMERGENCY LIGHTS ILLUMINATE WHEN SIDE LIGHTS SELECTED ON FLIGHT ATTENDANTS CONTROL PANEL. MAINTENANCE REMOVED AND REPLACED FLIGHT ATTENDANTS CONTROL PANEL IAW EMB145 MM 33-26-01 AND RESECURED PIN 10 ON CONNECTOR P8905 IAW EMB 145XR AMM 20-21-00, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
FLIGHT 2658, IAH TO PIT, AIRCRAFT DIVERTED INTO TYS FOR A FUEL IMBALANCE. WING TANK NR 1 FUEL QTY INDICATION WAS MEL'ED IN IAH PRIOR TO FLIGHT DEPARTURE, UPON LANDING IN TYS, MAINTENANCE CHECKED THE FUEL QTY. WITH UNDER WING STICKS AND FOUND THE SPLIT TO BE WITHIN TOLERANCE. THE FLIGHT CONTINUED ON, LATER THAT NIGHT MECHANICS CLEARED THE MEL IN EWR BY CLEANING THE NR 1 DAU CONNECTOR. THE AIRCRAFT WAS RELEASED TO SERVICE.