N957UW
Registered owner: AEROVISION AIRCRAFT SERVICES LLC, MI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| US AIRWAYS INC | Operator | 2011-02-25 – 2011-02-25 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AIRCRAFT WAS GROUNDED: 45 PERCENT YAW TRIM LEFT REQ. TO CENTER YAW INDICATION IN FLIGHT. T/S IAW FIM 27-20-00-810-806-A. FOUND TRIM OF RUDDER TO BE 2.5 DEG. LEFT WITH SURFACE CENTERED ON TAILCONE. C/W RUDDER RIGGING IAW AMM 27-20-00-820-801-A.TO NULL OUT RUDDER TRIM. ALL FLIGHT CONTROL SURFACES CHECK NORMAL IAW AMM 27-20-00.
AIRCRAFT WAS GROUNDED: TO MAINTAIN COORDINATED FLIGHT YAW TRIM REQUIRED BETWEEN 40-50 PERCENT INPUT ON YAW TRIM DURING CLIMB OUT AND CRUISE. FOUND LH IB FLAP NO.1 MECHANISM UPPER ROD BENT AND LH IB TRAILING FLAP OUT OF RIG. REMOVED AND REPLACED LH IB FLAP NO.1 AND NO.2 MECHANISM UPPER AND LOWER RODS IAW AMM 25-51-06 ALL TESTS CHECKED GOOD IAW AMM 27-50-00.
AIRCRAFT WAS GROUNDED: LANDING GEAR AURAL WARNING IN FLIGHT . ACCOMPLISHED QHR TO CLEAR. PERFORMED RADIO ALT TEST IAW TASK # 34-31-00-710-801-A , ALSO PERFORMED TASK 22-11-00-811-997-A , TESTED OK.
AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT BATTERY FAULT EICAS MSG DISPLAYED WHEN LIGHTS TESTED DURING PREFLIGHT 2 OVERHEAD CABIN EMERG LIGHTS DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EMERG LT BATTERY AT PANEL 243 OVERHEAD. OPS CHECK NORMAL.
AIRCRAFT WAS GROUNDED: PILOT REPORTS ELECT SMELL IN COCKPIT THRUOUT A/C CABIN, VERY STRONG IN FIRST CLASS SMELL REPORTED BY FA 1. RETURN TO THE GATE. MAINTENANCE ACCOMPLISHED JOB CARD 43L00021001. FOUND LEFT RECIRCU FAN BAD. REMOVE & REPLACED LEFT RECIRCULATION FAN IAW AMM 21-24-01. REMOVED & REPLCAED RECIRCULATION DUCT IAW AMM 21-24-03. REMOVED & REPLACED RECIRCULATION FILTERS IAW AMM 21-24-02. OPS CHECK GOOD. NO SMELL IN COCKPIT OR CABIN NOTED.
AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS R1 SLIDE PARTIALLY DEPLOYED, ASSIST BOTTLE DEPLETED. REPLACED DIAPHRAGM AND SLIDE ASSEMBLY IAW JOB CARD 43L00025001.
THE PILOT DECLARED AN EMERGENCY DUE TO A FLAPS FAILED EICAS MESSAGE. FLAPS FAILED TO RETRACT PROPERLY FROM 1 TO 0 AFTER TAKE OFF, AND AT EXTENSION FOR LANDING THE FLAPS FAILED AGAIN AND STAYED AT FLAPS 3 WITH FULL FLAPS SELECTED. MAINTNENANCE REMOVED AND REPLACED THE LT FLAP POSITION SENSOR UNIT IAW AMM 27-53-04. OPS CHECKED GOOD, NO FAULTS NOTED.
DURING APPROACH, IN ICING CONDITIONS AT 2500 FEET, THE AIRCRAFT EXPERIENCED VIOLENT ROLL. AP & AT DISCONNECTED AND EICAS MESSAGES WERE DISPLAYED AT FAIL, WIND SHEAR FAIL, STALL PROT FAIL, AND THE AOA LIMIT FAIL. AFTER LANDING, ADS PROBE 3+1 FAIL, DISPLAYED. REPLACED SMART PROBE IAW AMM 34-13-01.
AFT PASSENGER DOOR EMERGENCY SLIDE RELEASE PIN THREAD IS BROKEN OFF. REPLACED AFT PASSENGER DOOR EMERGENCY SLIDE. AIRCRAFT WAS GROUNDED.
AIRCRAFT IS IN BASE, WEAR ON LEFT WING INBOARD FLAP TRACK 2A INBOARD. REPLACED LEFT WING INBOARD FLAP TRACK 2A INBOARD PER AMM 57-54-25.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND COCKPIT FLOOR DOUBLER BETWEEN LBL 0 AND -Y1016, BETWEEN FR 7 AND FR12. REPAIRED COCKPIT FLOOR DOUBLER PER AARD 53-10-10-1 REPAIR 1 AND EA 274427.
AIRCRAFT WAS GROUNDED. AFT SERVICE DOOR EMERGENCY SLIDE, RELEASE PIN THREAD IS BROKEN OFF. REPLACED AFT DOOR EMERGENCY SLIDE.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON COCKPIT FLOOR DOUBLER AT -Y640 BETWEEN FR 19 AND FR 20. REPLACED FLOOR DOUBLER PER AARD 53-00-00-3 REPAIR 3 AND DRAWING 170-00822-413.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERCOSTAL AT FR 87 BETWEEN STRINGER 27R AND 28R. REPLACED INTERCOSTAL PER E190 SRM 51-41-01, 51-42-01, DWG 170-65180-445.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO COMPARTMENT ANGEL FOR DRAIN MAST, AFT OF FR 86, BETWEEN STRINGER 27R AND 28R. REPLACED INTERCOSTAL PER DRAWING 170-65180-445.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO COMPARTMENT ANGLE FOR DRAIN MAST, AFT OF FR 86, BETWEEN STRINGER 27R AND 28R. REPLACED ANGLE PER DRAWING 170-87561-001.
AIRCRAFT IN BASE MAINTENANCE. CRACKED RIGHT WING TRAILING EDGE SKIN AT EDGE PAST FASTENER ON OUTBOARD SIDE OF RIB 10. REPAIRED LOWER SKIN PER SRM 57-10-01 REPAIR 54.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND FORWARD MAIN CABIN FLOORBEAM AT Y320, BETWEEN FR 17 AND FR 18. REPLACED FLOORBEAM PER DRAWINGS 170-00822-505 AND 170-07304-001.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN FLOORBEAM AT Y360, BETWEEN FR 12 AND FR 13. REPLACED FLOORBEAM PER SRM 51-41-01, SRM 51-43-03, AND DRAWING 190-05555-805.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN CROSSBEAM AT Y720 AND FR 14. REPAIRED CROSSBEAM PER SRM53-00-10 REPAIR 53.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN LEFT HAND FLOOR SUPPORT AT -Y1150 AND FR 16. REPLACED FLOOR SUPPORT PER DRAWING 170-00816-415.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN LEFT HAND FLOOR SUPPORT AT -Y770 AND FR 17. REPLACED FLOOR SUPPORT PER DRAWING 170-00822-503.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN LEFT HAND SEAT TRACK AT -Y280 AND FR84. REPAIRED SEAT TRACK PER SRM 53-00-10 REPAIR 51.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT AFT MAIN CABIN FLOOR STRAP SUPPORT AT Y1160, BETWEEN FR 85 AND FR 86. REPLACED FLOOR STRAP SUPPORT PER DRAWING 170-66000-445.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN RIGHT HAND FLOOR SILL AT Y970, BETWEEN FR 12 AND FR 14. REPLACED FLOOR SILL PER 53-00-00-3 REPAIR 3.
AIRCRAFT IN BASE MAINTENANCE. CORRODED FORWARD MAIN CABIN FLOORBEAM AT -Y340 AND Y360, BETWEEN FR12 AND FR13. REPLACED FLOORBEAM PER 53-00-00-3 AND SRM 51-41-02.
AIRCRAFT IN BASE MAINTENANCE. CRACK ON LEFT HAND LOWER REAR SKIN PANEL AROUND FASTENER, NEXT TO DRAIN HOLE, AT SPAR 2 AND RIB 10. REPAIRED SKIN PANEL PER EA 254412.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR PANEL SUPPORT AT -Y1180 AND FR 84. REPLACED FLOOR SUPPORT PER DRAWING 170-66000-445.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN LEFT HAND SEAT TRACK AT -Y280, BETWEEN FR 16 AND FR20. REPLACED SEAT TRACK PER 53-00-00-3 REPAIR 3.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN RIGHT HAND SEAT TRACK AT Y250 AND FR 17. REPLACED SEAT TRACK PER 53-00-00-3 REPAIR 3.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR STRAP SUPPORT AT -Y1180 AND FR 85. REPLACED FLOOR STRAP SUPPORT DRAWING 170-66000-445.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN RIGHT HAND FLOORBEAM FASTENER AT Y280 AND FR 87. REPLACED FLOORBEAM PER AARD 53-00-00-3 REPAIR 3 AND SRM 51-43-03.
CORROSION ON FORWARD MAIN CABIN RIGHT FLOOR SUPPORT AT Y1100, BETWEEN FRAMES 17 AND 18. REPLACED THE FLOOR SUPPORT IAW 53-00-00-3 AND DRAWING 170-00822-413.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN LEFT HAND FLOOR SILL AT -Y1180, BETWEEN FR 12 AND FR 13. REPLACED FLOOR SILL PER 53-00-00-3 REPAIR 3 FIGURE 1 SHEET 11.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN RIGHT HAND REINFORCEMENT STRUCTURE AT FR 84, BETWEEN Y280 AND Y1150. REPLACED FLOOR SUPPORT.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN LEFT HAND FLOOR SUPPORT AT -Y770 AND FR 18. REPLACED FLOOR SUPPORT PER DRAWING 170-00822-413 AND SRM 51-41-01.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR PANEL SUPPORT AT Y920, BETWEEN FR 89 AND FR 90. REPLACED PANEL SUPPORT PER AARD 53-00-00-3 REPAIR 3.
AIRCRAFT IN BASE MAINTENANCE. CORROSION / SCRATCH ON AFT MAIN CABIN RIGHT HAND UPPER SHEET, UNDER SIDE AT Y280 BETWEEN FR 85 AND FR 86. REPLACED UPPER SHEET PER DRAWING 170-65-660-449.
AIRCRAFT WAS NOT GROUNDED. CENTER AISLE FORWARD EXIT LOCATOR LENS COVER MISSING FOR OVERWING EXIT. REPLACED OVERWING EXIT LENS COVER.
LOST HYDRAULIC SYS NR 2 QUANTITY AFTER TAKEOFF. FOUND BROKEN HYDRAULIC LINE AT NR 2 SYS CASE DRAIN FILTER MANIFOLD. REPLACED THE LINE. AIRCRAFT WAS GROUNDED.
LOWER LEFT SIDE CAPTAIN`S WINDSHIELD IS LEAKING WATER FROM BETWEEN THE GLASS AND THE RUBBER SEAL, 15 TO 23 INCHES FROM RIGHT CORNER. REPLACED WINDSHIELD IAW AMM 56-11-00-400-801-A. AIRCRAFT WAS GROUNDED.
AIRCRAFT IN BASE MAINTENANCE, R1 SERVICE DOOR PNEUMATIC BOTTLE NEEDS SERVICING. SERVICED R1 SERVICE DOOR PNEUMATIC BOTTLE PER AMM 52-41-51-614-801.
RETURNED TO DEPARTURE DUE TO THE RIGHT OVERWING EMERGENCY DOOR EXIT INDICATED OPEN ON THE MASTER CAUTION. NO EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. DOORS INDICATE GREEN ON GROUND. MAINTENANCE FOUND RIGHT OVERWING ESCAPE HATCH HANDLE APPROX 10 DEGREE FROM FULL CLOSED POSITION. AT 10 DEGREES LATCH IS MOVED AND MICROSWITCH IS OFF, THIS WAS A GOOD INDICATION. LUBED LATCH HANDLE AND PINS TO ALLOW HANDLE TO MOVE TO 0 DEGREE (FULLY CLOSED) POSITION PER AMM 52-20-00 & AMM 52-21-00.
AIRCRAFT WAS NOT GROUNDED. ENTIRE SECTION OF FIRST PIECE OF PHOTO LUMINESCENT STRIP MISSING SIDE OF ISLE AT 1D. MAINTENANCE REPLACED PHOTO LUMINESCENT STRIP PER 33-50-00.
ACFT WAS GROUNDED, FLIGHT CREW REPORTED RECEIVING A LAV SMOKE EICAS ON TAKEOFF AT 500' AGL, EICAS WENT OUT WITH POWER REDUCTION AND A SMOKE ODOR IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED TC 43L00021001, TROUBLE SHOOT CABIN AIR QUALITY AND TC 43L00036002, PNEUMATIC BLEED AIR BLASTER AND COULD NOT DUPLICATE THE ODOR OR THE LAV SMOKE FAULTS. MAINTENANCE DETERMINED THAT THE ODOR IN THE CABIN WAS DUE TO PRESERVATIVE OIL RESIDUE FROM THE RT ENGINE CHANGE, ACCOMPLISHED PRIOR TO THIS FLIGHT.
AIRCRAFT WAS NOT GNDED. FWD FLIGHT ATTENDANT STATION FLASHLIGHT SECURITY STRAP REQUIRES REPAIR. R & R STRAP. OPERATIONAL CHECKED GOOD.
AIRCRAFT WAS GNDED. AFTER DEPARTURE WHILE CLIMBING, THE NR 1 BLEED SYS FAILED, RESULTING IN A PRESSURIZATION ISSUE AS THE NR 2 BLEED AIR SYS WAS ALREADY ON MEL. DECLARED AN EMER & RETURNED WHERE THE ACFT LANDED SAFELY WITH NO FURTHER INCIDENT. FOUND A BLEED AIR LEAK COMING FROM THE STARTER DUCT IN THE NR 1 PYLON FWD SECTION & REPLACED THE STARTER DUCT IAW AMM 36-11-4 400. NO FAULTS WERE NOTED DURING AN OPERATIONAL CHECK OF THE SYS.
AIRCRAFT WAS NOT GNDED. 1R DOOR WILL NOT ARM. R & R ESCAPE SLIDE. R & R SHEARED FLEX BALL CABLE IAW AMM 52-41-40. OPERATIONS CHECKED OK FOR SERVICE.
AIRCRAFT WAS NOT GNDED. 1R DOOR WILL NOT ARM. R & R ESCAPE SLIDE. R & R SHEARED FLEX BALL CABLE IAW AMM 52-41-40. OPERATIONS CHECKED OK FOR SERVICE.
C3 CHECK, L2 EMER EXIT SIGN HAS LED BURNT OUT. L2 EMER EXIT SIGN HOUSING REPLACED. OPERATIONS CHECKED GOOD IAW AMMS 33-50-17 & 33-50-19.
C3 CHECK, L3 EMER EXIT SIGN HAS LENS DEFECTIVE. L3 EMER EXIT SIGN LENS REPLACED. OPERATIONS CHECKED GOOD IAW AMMS 33-50-17 & 33-50-19.
THE R1 DOOR LOWER EMER EXIT SIGN IDENTIFIER IS CRACKED. R & R R1 DOOR LOWER EMER EXIT SIGN IAW AMM 33-50-15. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.
C3 CHECK, L1 EMER EXIT SIGN HAS LED BURNT OUT. L1 EMER EXIT SIGN HOUSING REPLACED. OPERATIONS CHECKED GOOD IAW AMMS 33-50-17 & 33-50-19.
C3 CHECK, COCKPIT FLOOR CROSSBEAM ATTACH ANGLE CRACKED AT FRAME 12 & LBL 27. REPLACED ANGLE IAW SRM 51-41-02.
C3 CHECK, RT HORIZONTAL STABILIZER AFT SPAR, BETWEEN RIB 5 & 6, INBD ELEVATOR PCU FITTING IS CRACKED AT RADIUS. R & R ELEVATOR PCU FITTING IAW DWG 190-09152-411.
C3 CHECK, LEFT OVERWING CTR EMER PATH LIGHT INOPERATIVE. FOUND LIGHT DISCONNECTED, RECONNECTED LIGHT IAW WDM 33-50-50. PERFORMED OPERATIONAL CHECK IAW AMM 33-50-00. CHECKED GOOD.
C3 CHECK, MAIN CABIN LT & RT PHOTO LUMINESCENT STRIPS ARE DAMAGED, MORE THAN 10%. R & R MAIN CABIN RT PHOTO LUMINESCENT STRIP IAW AMM 33-50-21. SEE ALSO AALA201509309001 FOR LT SIDE.
C3 CHECK, RIGHT AFT WING TO BODY EMER LIGHT LENS IS CRACKED. R & R RT WING TO BODY EMER LIGHT LENS IAW AMM 33-50-25.
CE3 CHECK, THE R2 DOOR UPPER EMER EXIT SIGN IDENTIFIER IS CRACKED. R & R R2 DOOR UPPER EMER EXIT SIGN IAW AMM 33-50-19. OPERATIONAL CHECKED GOOD IAW AMM 33-50-00.
C3 CHECK, MAIN CABIN LT & RT PHOTO LUMINESCENT STRIPS ARE DAMAGED, MORE THAN 10%. R & R MAIN CABIN LT PHOTO LUMINESCENT STRIP IAW AMM 33-50-21. SEE ALSO AALA201509309024 FOR RT SIDE.
C3 CHECK THE R1 DOOR UPPER EMER EXIT SIGN IDENTIFIER IS CRACKED. R & R R1 DOOR UPPER EMER EXIT MARKING SIGN LENS IAW AMM 33-50-17. OPERATIONAL CHECKED GOOD IAW AMM 33-50-00.
C3 CHECK LEFT WING EXIT DOOR, AFT ROLLER IS STUCK. R & R LT OVERWING ESCAPE HATCH UPPER LATCH FITTING ASSEMBLY IAW AMM 52-21-00. ADJUSTMENT CHECKED GOOD.
C3 CHECK, THE L1 DOOR UPPER EMER EXIT SIGN IDENTIFIER IS CRACKED. R & R LENS AT THE EXIT SIGN ABOVE L1 DOOR IAW AMM 33-50-17.
C3 CHECK, THE R2 DOOR LOWER EMER EXIT SIGN IDENTIFIER IS CRACKED. R & R R2 DOOR LOWER EMER EXIT SIGN IDENTIFIER. PERFORMED OPERATIONAL CHECK IAW AMM 33-50-15 & AMM 33-50-00.
C3 CHECK, THE L2 DOOR LOWER EMER EXIT SIGN IDENTIFIER IS CRACKED. R & R L2 DOOR LOWER EMER EXIT SIGN IDENTIFIER. PERFORMED OPERATIONAL CHECK IAW AMM 33-50-00-710-801A & AMM 33-50-15.
C3 CHECK, THE L1 DOOR, LOWER EMER EXIT IDENTIFIER SIGN IS CRACKED. R & R L1 DOOR EMER EXIT IDENTIFIER SIGN IAW AMM 33-50-15. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.
C3 CHECK, LT WING LOWER SURFACE SKIN CRACKED AROUND FASTENER HOLE NEAR DRAIN HOLE, AT SPAR 2 & RIB 10. REPAIRED IAW EA 254412.
C3 CHECK, R2 DOOR PNEUMATIC ASSIST BOTTLE PRESSURES ARE LOW. ACCOMPLISHED CARD 43C82452001.
C3 CHECK, R1 DOOR PNEUMATIC ASSIST BOTTLE PRESSURES ARE LOW. ACCOMPLISHED CARD 43C82152001.
C3 CHECK, AFT PAX DOOR, ESCAPE SLIDE, LOWER RT CORNER ELASTIC STRAP IS BROKEN OFF ACFT. R & R SLIDE IAW CARD 43C81252001.
C3 CHECK, RT OVERWING HATCH CUT OUT, FWD ROLLER IS STUCK. R & R RT OVERWING HATCH CUT OUT, FWD ROLLER IAW AMM 20-10-08-000-801-A.
C3 CHECK, R2 DOOR PNEUMATIC ASSIST ASSEMBLY HAS PLUNGER NOT PROPERLY ALIGNED, RED MARKS DO NOT LINE UP. ACCOMPLISHED CARD 43C82452001.
C3 CHECK, L2 DOOR PNEUMATIC ASSIST BOTTLE PRESS LOW. ACCOMPLISHED CARD 43C81252001.
C3 CHECK, L1 DOOR PNEUMATIC ASSIST BOTTLE PRESSURE LOW. ACCOMPLISHED CARD 43C81152001.
C3 CHECK, CORROSION ON RT SHEAR PANEL, BETWEEN FRAME 87 & 88, Y=+304.8 TO Y=+1041.4. REPLACED IAW SRM 51-42-01 & 51-42-02.
C3 CHECK, CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT LOWER CTR SEAL REST, BETWEEN FRAME 78 - 79 AT STRINGER 26R. REPLACED IAW SRM 53-23-29 & AARD 53-00-00-03 REPAIR 3.
C3 CHECK, VERTICAL STABILIZER REAR SPAR ABOVE NR 3 HINGE FITTING, SUPPORT RIB IS CRACKED. R & R RIB 9 &10 TE PN 170-63629-005, BATCH 0002845448 AT VERTICAL STABILIZER REAR SPAR ABOVE NR 3 HINGE FITTING IAW SRM PART II 51-41-02 PARA 4, PARA 6 & 51-41-01 PARA 4 & PARA 6.
C3 CHECK, CORROSION ON FWD CARGO COMPARTMENT DOOR CUTOUT LOWER CTR SEAL REST, BETWEEN FRAME 25 - 26 AT STRINGER 26R. REPLACED IAW SRM 51-41-01 & AARD 53-00-00-3 REPAIR 3.
C3 CHECK, CORROSION ON CTR SHEAR PANEL, BETWEEN FRAME 87 - 88 & BETWEEN Y=-222.3 - Y=+222.3. REPLACED IAW SRM 53-00-00-3 REPAIR 3.
C3 CHECK, CABIN FLOOR GUSSET AT FRAME 90 & RBL 20 IS CORRODED. FABRICATED & INSTALLED REPLACEMENT GUSSET IAW SRM 51-41-02 & DWG 170-60001-823.
FUMES & HEAVY PETROLEUM SMELL IN COCKPIT & CABIN WHILE DESCENDING BELOW 12,OOO'. FOUND COFFEE RESIDUE COATING THE RT PACK HEAT EXCHANGER & ACM. R & R THE RT PACK HEAT EXCHANGER & ACM. THE RECIRCULATION FILTERS WERE ALSO REPLACED.
FUMES & HEAVY PETROLEUM SMELL IN COCKPIT & CABIN WHILE DESCENDING BELOW 12,OOO'. FOUND COFFEE RESIDUE COATING THE RT PACK HEAT EXCHANGER & ACM. R & R THE RT PACK HEAT EXCHANGER & ACM. THE RECIRCULATION FILTERS WERE ALSO REPLACED.
WHILE CLIMBING OUT THE COCKPIT DOOR OPENED. THE CREW TRIED TO SECURE THE DOOR CLOSED BUT A HINGE WAS BROKEN & LOOSE & THE DOOR WOULD NOT SECURE. THE CREW ADVISED THE TRAVELING FAMS. THE CREW ELECTED TO DIVERT FOR MX. AN EMER WAS DECLARED & THE FLIGHT LANDED & TAXIED TO GATE WITHOUT INCIDENT. R & R THE COCKPIT DOOR HINGES.
RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE LT PYLON OTBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.
RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE LT PYLON INBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.
RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE RT PYLON OTBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.
RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE RT PYLON INBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.
FLIGHT 2187, LGA - DCA. SLAT FAIL EICAS MSG SLATS AT 3 ON APPROACH. THE CREW DECLARED AN EMERGENCY & THE ACFT HAD AN UNEVENTFUL LANDING. R & R THE RT OTBD SLAT SKEW SENSORS.
FLIGHT 2187, LGA - DCA. SLAT FAIL EICAS MSG WITH SLATS AT 3 ON APPROACH. THE CREW DECLARED AN EMERGENCY & THE ACFT HAD AN UNEVENTFUL LANDING. R & R THE RT OTBD SLAT SKEW SENSORS.
FLIGHT CREW RECEIVED BLEED 2 LEAK EICAS MSG ON CLIMB OUT OF PHL AT FL300. CREW DECLARED AN EMERGENCY & PERFORMED A RAPID DESCENT DOWN TO 10,000FT. FLIGHT RETURNED TO PHL & LANDED NORMALLY. R & R THE NR 2 & NR 1 ENG PRE COOLER.
L1 DOOR EMERGENCY OPENING SYS FAILED WHEN PERFORMING FUNCTIONAL CHECK. MX ACCOMPLISHED ADJUSTMENT TEST OF THE CONTROL MECHANISM, CHECKED NORMAL.
PHL, EVACUATION SLIDE FUNCTIONAL TEST DUE ON L1 DOOR, NO LIGHTS ON SLIDE PACK. THIS IS RECORDED AS A SYS FAIL.
AFT LEFT PAX ENTRY DOOR REQUIRES DOOR ASSIST BOTTLE PRESSURE SERVICING . MAINTENANCE SERVICED AFT LEFT PAX ENTRY DOOR.
FWD PAX ENTRY DOOR REQUIRES DOOR ASSIST BOTTLE PRESSURE SERVICED. MAINTENANCE ACCOMPLISHED FORWARD RIGHT PAX ENTRY DOOR ASSIST BOTTLE SERVICE AFTER 24 AND 48 HOURS.
LEFT AFT PASSENGER DOOR EMERGENCY PNEUMATIC ASSY NEEDS SERVICING. MX SERVICED LEFT AFT PASSENGER DOOR EMERGENCY PNEUMATIC ASSY.
C2 CHECK - EMERGENCY POWER SUPPLY NR 5 FAILS TEST. BATTERY FAILED TEST, LIGHT ASSEMBLY INOP AT AFT PASSENGER DOOR. REPLACED EMERGENCY POWER SUPPLY NR 5 IAW EMBRAER E190 AMM 33-50-01.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WASTE PAN BETWEEN FR85 TO FR88, S23L. REPLACED WASTE PAN BETWEEN FR85 TO FR88, S23L IAW EMBRAER E190 SRM 2, 51-40-02.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WASTE BOX DOUBLER BETWEEN FR88 TO FR89, S28R. REPLACED WASTE BOX DOUBLER BETWEEN FR88 TO FR89, S28R IAW E190 SRM 2, 53-42-01.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR19, LBL 11. REPAIRED FLOORBEAM BETWEEN FR16 TO FR19, LBL 11 IAW EA 504962.
C2 CHECK - CORROSION ON SUPPORT RIB AT FR45, -Y26. REPLACED SUPPORT RIB AT FR45, -Y26 IAW EMBRAER E190 SRM 51-10-04.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FORWARD CARGO FLOORBEAM BETWEEN FR26 TO FR27, -Y10. REPLACED FORWARD CARGO FLOORBEAM BETWEEN FR26 TO FR27, -Y10 IAW EMBRAER E190 SRM 2, 51-43-04.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAL PLATE BETWEEN FR24 TO FR25, -Y10. REPLACED SEAL PLATE BETWEEN FR24 TO FR25, -Y10 IAW E190 SRM 2, 51-41-01.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR90, -Y10. REPLACED GUSSET AT FR90, -Y10 IAW E190 SRM 2, 51-41-02.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CROSS BEAM AT FR17 & BETWEEN -Y26 TO -Y28. REPAIRED CROSS BEAM AT FR17 & BETWEEN -Y26 TO -Y28 IAW EA 504965.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR90, -Y22. REPLACED GUSSET AT FR90, -Y22 IAW E190 SRM 2, 51-41-02.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR14 TO FR17, -Y10. REPLACED FLOORBEAM BETWEEN FR14 TO FR17, -Y10 IAW EMBRAER E190 SRM 2, 51-40-02.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SILL PLATE BETWEEN FR12 TO FR14, -Y38. REPLACED SILL PLATE BETWEEN FR12 TO FR14, -Y38 IAW E190 SRM 2, 51-40-02.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CROSSBEAM PANEL SUPPORT AT FR16, -Y29. REPLACED CROSSBEAM PANEL SUPPORT AT FR16, -Y29 IAW E190 SRM 51-41-0.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FORWARD RIGHT SILL BETWEEN FR17 TO FR18 & BETWEEN -Y41 TO -Y48. REPLACED FORWARD RIGHT SILL BETWEEN FR17 TO FR18 & BETWEEN -Y41 TO -Y48 IAW EMBRAER E190 SRM 51-41-02 & 51-43-02.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PANEL BETWEEN FR87 TO FR88 & BETWEEN -Y10 TO Y10. REPLACED SILL PLATE BETWEEN FR12 TO FR14, -Y38 IAW E190 SRM 2, 51-40-02.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR86 TO FR87, -Y10.75. REPLACED FLOORBEAM BETWEEN FR86 TO FR87, -Y10.75 IAW EMBRAER E190 SRM 2, 51-41-01.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PANEL BETWEEN FR87 TO FR88 & BETWEEN -Y12 TO -Y37. REPLACED SHEAR PANEL BETWEEN FR87 TO FR88 & BETWEEN -Y12 TO -Y37 IAW EMBRAER E190 SRM 2, 51-40-02.
C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON UPPER SHEET BETWEEN FR86 TO FR87, Y10.750. REPLACED UPPER SHEET BETWEEN FR86 TO FR87, Y10.750 IAW E190 SRM 2, 51-41-01.
C2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAL PLATE BETWEEN FR24 TO FR27, -Y10. REPLACED SEAL PLATE BETWEEN FR24 TO FR27, -Y10 IAW E190 SRM 51-40-01.
PHL - 1L DOOR WILL NOT CLOSE. REMOVED AND RE-INSTALLED THRESHOLD PLATE AND RESEALED. DOOR CHECKS GOOD.
FLIGHT 183, PHL - DFW - DESCENDING THRU FL 190 CAPTS WINDSHIELD SHATTERED AND STARTED ARCHING, FOLLOWED QRH PROCEDURE. REPLACED L1 WINDSHIELD AND REPLACED CONTROLLLER REF MM 56-11-00. OPERATIONAL AND LEAK CK GOOD.
BOS - EMERGENCY LT BATT FAULT. MAINTENANCE REMOVED AND REPLACED LT EMERGENCY-LIGHT POWER UNIT PER E190 AMM 33-50-01, OPS TEST GOOD.
BOS - UPON ARRIVAL TO AIRCRAFT, MAINT FOUND L-1 DOOR SLIDE PARTIALLY DEPLOYED. MAINTENANCE REPLACED NR 1 DOOR SLIDE ASSY PER AMM 25-65-01, CHECKS GOOD.
FLIGHT 1267, PHL-DFW - BREAK AWAY FLASHLIGHT 2R DOES NOT BLINK. MAINTENANCE REMOVED AND REPLACED 2R FLASHLIGHT. OPERATIONAL CHECK IS SATISFACTORY.
LGA - ROW 1 AC RIGHT FLOOR PATH LIGHTING MISSING. PLACED ON MEL. JUNE 5TH - MAINTENANCE REPLACED MISSING PHOTOLUMINESCENT FLOOR PATH LIGHTING SECTION. THIS CLEARS THE MEL.
BOS - THE AFT LEFT AND RIGHT EMERGENCY LIGHTS ABOVE THE DOOR SLIDES ARE ON. MAINTENANCE ADJUSTED THE AFT LEFT PASSENGER DOOR COURTESY LIGHT MICRO-SWITCH PER 33-26-15. A SUCCESSFUL OPERATIONAL CHECK WAS PERFORMED, THE EMERGENCY LIGHTS CHECK GOOD.
BOS - FLT 1980 EN-ROUTE PHL TO PVD. UPON DESCENT INTO PVD, THE CREW RECEIVED A SLAT FAIL EICAS MESSAGE. AFTER A DISCUSSION WITH MAINTENANCE AND OPERATIONS, IT WAS DECIDED THAT THE FLIGHT SHOULD DIVERT TO A MAINTENANCE BASE. THE CREW DECLARED AN EMERGENCY AND THE FLIGHT DIVERTED TO BOS. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT OUTBOARD SLAT SKEW SENSOR 2/3.
BOS - THE AFT PASSENGER DOOR PNEUMATIC ASSEMBLY DIAPHRAGM PUNCTURED. MAINTENANCE REMOVED AND REPLACED THE PNUEMATIC ASSEMBLY DIAPHRAGM PER AMM 52-11-53.
PIT - C1 - EES - FORWARD SERVICE DOOR SLIDE INFORMATION TAG ON GAGE ILLEGIBLE & BOTTLE PRESSURE READS 0 PSI. REPLACED FORWARD SERVICE DOOR SLIDE IAW JOB CARD 43C82152001.
BOS - THE L1 DOOR ASSIST BOTTLE NEEDS SERVICING. MAINTENANCE SERVICED THE L1 DOOR ASSIST BOTTLE PER AMM 52-11-51-03 A.
BOS - THE R1 DOOR ASSIST BOTTLE REQUIRES SERVICING. MAINTENANCE SERVICED THE R1 DOOR ASSIST BOTTLE PER AMM 52-11-51-03.
PHL - THE CAPTAIN'S SEAT WOULD NOT LOCK IN PLACE. MAINTENANCE REPOSITIONED SEAT ELECTRIC CORD AND LUBED. OPERATIONAL CHECK IS GOOD, AC OKAY FOR SERVICE.
ATL - THE RIGHT SERVICE DOOR ASSIST BOTTLE IS LOW. MAINTENANCE SERVICED THE RIGHT DOOR PNEUMATIC ASSIST BOTTLE.
CLT - THE COCKPIT DOOR CAME OFF THE HINGES WHEN THE DOOR WAS OPENED. MAINTENANCE REMOVED AND REPLACED THE COCKPIT DOOR UPPER HINGE AND PERFORMED ADJUSTMENTS OF THE COCKPIT DOOR.
FLIGHT 1569, BDL-PHL - THE CREW REPORTED AUTO THROTTLE FAIL MESSAGE IN FLIGHT ALONG WITH TAT 2 FAIL, LOSING LEFT NAVIGATION. THE CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. UPON LANDING REPORTED A FAINT ELECTRICAL SMOKE ODOR IN THE COCKPIT AND CABIN. MAINTENANCE REPLACED SPDA DC POWER SUPPLY MODULE. AOA AND TOTAL TEMPERATURE SENSORS WERE ALSO REPLACED.
CLT - FLIGHT ATTENDANT FLASHLIGHT NOT SHOWING THAT IT IS CHARGING. MX R&R THE BATTERY.
THE CREW WAS UNABLE TO RETRACT THE LANDING GEAR UPON TAKEOFF. THE FLIGHT RETUREND TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANIDNG CONTROL LEVER AND THE PROXIMITY SENSOR MODULE. HOWEVER, ON THE FIRST FLIGHT OUT, THE HANDLE TO RETRACT THE GEAR WOULD NOT MOVE PREVENTING THE GEAR FROM RETRACTING. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEEL SENSOR/STEERING SENSOR FEEDBACK ELECTRICAL HARNESS. (K)