N952UW

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · airframe 26,134 hrs · 21,374 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN FLOOR SHEAR PANEL BETWEEN FR 87 AND FR 88, BETWEEN Y284 AND Y838. REPLACED SHEAR PANEL PER AARD 53-00-00-3 REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 90) · airframe 26,134 hrs · 21,374 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR SUPPORT AT FR 90 AND Y= 635. REPLACED FLOOR SUPPORT PER SRM 51-75-16.

Part: FLOOR SUPPORT — CORRODED (FRAME 89) · airframe 26,134 hrs · 21,374 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN FLOOR SUPPORT AT FR 89 AND Y914. REPLACED FLOOR SUPPORT PER SRM 51-41-02.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · airframe 26,134 hrs · 21,374 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN FLOOR SHEAR PANEL BETWEEN FR 87 FR 88 AND Y=- 939. REPLACED SHEAR PANEL PER AARD 53-00-00-3 REPAIR 3.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · airframe 26,134 hrs · 21,374 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN FLOOR SHEAR PANEL BETWEEN FR 87 AND FR 88 AND BETWEEN Y=-254 TO Y=254. REPLACED SHEAR PANEL PER AARD 53-00-00-3 REPAIR 3.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 25,745 hrs · 20,995 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT FLIGHT ATTANDANT REPORTED BRAKEAWAY FLASH LIGHT INOPERABLE. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER AMM 33-51-00.

Part: LOCK — DIRTY (R1 DOOR SLIDE) · airframe 22,261 hrs · 18,197 cycles

UNABLE TO ARM THE R1 DOOR. REMOVED DEBRIS FROM SLIDE LOCKING PLATES.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 21,284 hrs · 17,465 cycles

OVER DOOR EMERGENCY LIGHT SIGN AT L2 DOOR IS CRACKED. REPLACED OVER DOOR EMEGENCY LIGHT SIGN. AIRCRAFT WAS GROUNDED.

Part: RIB — CRACKED (RT WING) · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT WING LEADING EDGE RIB 17 CRACKED. REPLACED RIB PER SRM 51-41-00, 51-41-02, 51-43-03, 51-43-04 AND DRAWING 190-31005-409.

Part: FITTING — CORRODED (RT WING) · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT WING TIP LOWER AFT FITTING. REPLACED RIGHT WING TIP LOWER AFT FITTING PER SRM 51-43-06 AND DRAWING 190-341-50-021.

Part: SIGN — CRACKED (EMERGENCY LIGHTS) · airframe 21,283 hrs · 17,464 cycles

L2 DOOR LOWER EMERGENCY LIGHT SIGN IS CRACKED. REPLACED L2 DOOR EMERGENCY LIGHT ASSEMBLY. AIRCRAFT WAS GROUNDED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,283 hrs · 17,464 cycles

R2 DOOR LOWER EXIT SIGN HAS ONLY HALF OF THE LIGHTS WORKING. REPLACED R2 LOWER EMERGENCY LIGHT EXIT SIGN. AIRCRAFT WAS GROUNDED.

Part: BUSHING — MIGRATED (LT ELEVATOR) · airframe 21,283 hrs · 17,464 cycles

MIGRATED BUSHING ON THE LEFT ELEVATOR NR 3 FITTING, INBD LUG AT UPPER BORE LOCATION. REPAIRED THE ELEVATOR IAW EA 271821.

Part: SKIN — CRACKED (LT WING) · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LEFT WING LEADING EDGE SKIN AT THE NR 2 SLAT OTBD TRACK CUTOUT. REPAIRED THE SKIN IAW EA 271560.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 21,283 hrs · 17,464 cycles

WING TO FUSELAGE FAIRING 199ML LIGHT LENS COVER IS CRACKED. REPLACED LENS. AIRCRAFT WAS GROUNDED.

Part: ROLLER — FROZEN (OVERWING EXIT) · airframe 21,283 hrs · 17,464 cycles

RIGHT OVERWING ESCAPE HATCH CUTOUT, TWO LATCH ROLLERS ARE FROZEN AT UPPER FRAME. CLEANED, LUBRICATED AND CHECKED LATCH ROLLERS IAW AMM 05-25-00, AMM 52-21-00, AND AMM SDS 52-20-00/1.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 21,283 hrs · 17,464 cycles

CEILING PANEL EXIT LIGHT LENS WAS BROKEN. REPLACED LENS. AIRCRAFT WAS GROUNDED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 21,283 hrs · 17,464 cycles

FORWARD LEFT EMERGENCY LIGHT BATTERY PACK FAILED. REPLACED FORWARD LEFT EMERGENCY LIGHT BATTERY PACK. AIRCRAFT WAS GROUNDED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT FR 84 AND Y=+285. REPAIRED SEAT TRACK PER SRM 53-00-10 REPAIR 51 AND DRAWING 170-65600-443.

Part: WINDOW — CLOUDY (CABIN) · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. PASSENGER WINDOW 1 LEFT IS CLOUDY. REPLACED WINDOW PER AMM 21-31-00 AND ACCOMPLISHED A SATISFACTORY LEAK CHECK.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN LEFT HAND SHEAR PANEL BETWEEN FR 87 AND FR 88, BETWEEN -Y450 AND -Y960. REPLACED SHEAR PANEL PER AARD 53-00-00-3, SRM 51-42-01, 51-42-02, AND 51-43-03.

Part: SUPPORT — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

CORROSION ON MAIN CABIN AFT LAVATORY SUPPORT AT LBL 36 BETWEEN FRAMES 87 AND 88. REPLACED THE LAVATORY SUPPORT IAW SRM 51-43-03, AND DRAWING 170-65660-445.

Part: FLOOR SUPPORT — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

CORROSION ON FORWARD MAIN CABIN LEFT AFT FLOOR SUPPORT AT -Y1156 BETWEEN FRAMES 19 AND 20. REPAIRED THE FLOOR SUPPORT IAW 53-10-00-2, REPAIR 2.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN FLOOR PANEL SUPPORT ANGLE AT Y915 AND FR 12. REPLACED SUPPORT ANGLE PER DRAWING 170-00810-419 AND SRM 51-41-01.

Part: PLATE — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

CORROSION AND SCRATCH ON AFT MAIN CABIN REINFORCEMENT PLATE AT FRAME 84 BETWEEN Y315 AND Y1040. REPLACED REINFORCEMENT PLATE IAW DRAWING 190-65140-801.

Part: BEAM — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

CORROSION ON RIGHT FORWARD MAIN CABIN BEAM AT Y381 BETWEEN FR 12 AND FR 13. REPLACED THE BEAM IAW DRAWING 190-05555-802, SRM 51-41-01, AND SRM 51-43-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN RIGHT HAND FLOOR TRACK BETWEEN FR 12 AND FR 18 AT Y276. REPLACED FLOOR TRACK PER AARD 53-00-00-3 REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

CORROSION ON AFT MAIN CABIN RIGHT HAND FLOOR PANEL SUPPORT AT Y450 BETWEEN FR 88 AND FR 90. REPLACED FLOOR PANEL SUPPORT PER DRAWING 170-66000-439 REV A, SRM 51-43-03 AND 51-41-01.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON AFT MAIN CABIN PANEL SUPPORT AT FR 85 AND Y720. REPLACED SUPPORT PER SRM 51-41-01, DRAWING 170-65660-445.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON AFT MAIN CABIN PANEL SUPPORT AT FR 86 AND Y720. REPLACED SUPPORT PER E190 SRM 51-41-01, DRAWING 170-65660-445.

Part: DOUBLER — CORRODED (FRAMES 13-16) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

CORROSION ON FORWARD MAIN CABIN LEFT FORWARD FLOOR DOUBLER BETWEEN FRAMES 13 AND 16, -Y304 AND -Y914. REPLACED FLOOR DOUBLER IAW SRM 51-40-02,M AND DRAWING 170-00822-503.

Part: SPLICE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

CORROSION ON THE LEFT AFT MAIN CABIN FLOOR SPLICE AT -Y1020 BETWEEN FRAMES 87 AND 88. REPLACED THE FLOOR SPLICE IAW DRAWING 170-66000-445.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

CORROSION ON FORWARD MAIN CABIN RIGHT FORWARD FLOOR SUPPORT BETWEEN FRAMES 12 AND 14. REPLACED THE FLOOR SUPPORT IAW DWG 53-00-00-3.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN LEFT HAND AFT FLOOR DOUBLER BETWEEN FR 19 AND FR 20, AND BETWEEN -Y304 AND -Y850. REPLACED DOUBLER PER DRAWING 170-00822-503.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN LEFT HAND PANEL SUPPORT AT FR 90 AND -Y810. REPLACED SUPPORT PER DRAWING 170-66000-439 REV A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOORBEAM BETWEEN FR 17 AND FR 18 AT Y=+308. REPLACED FLOORBEAM PER DRAWING 170-00822-503.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

CORROSION ON FORWARD MAIN CABIN, LEFT FORWARD FLOOR SUPPORT BETWEEN FRAMES 12 AND 13. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-503.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

CORROSION ON RIGHT HAND AFT MAIN CABIN FLOOR GUSSET AT FR 90 AND Y580. REPLACED GUSSET PER DRAWING 170-60001-823.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN RIGHT HAND AFT FLOOR SILL BETWEEN FR 17 AND FR 20, AND BETWEEN Y1060 AND Y1257. REPLACED SILL PER AARD 53-00-00-3 REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,283 hrs · 17,464 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FLOOR SUPPORT AT FR 19 AND Y=-1140. REPLACED FLOOR SUPPORT PER SRM 51-43-03 AND DRAWING 170-29712-805.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 20,123 hrs · 16,639 cycles

DURING ACCOMPLISHMENT OF A-1 CHECK, FOUND FIRST OFFICER'S FIXED WINDSHIELD WITH MULTIPLE CRACKS ALONG THE UPPER EDGE INBOARD AREA. REPLACED FIXED WINDSHIELD IAW AMM 56-11-00.

Part: SLIDE — DEFECTIVE (L2 DOOR) · airframe 20,024 hrs · 16,548 cycles

WHILE OPENING THE L2 DOOR, THE SLIDE WAS DISLODGED FROM THE BUSTLE. (SLIDE DID NOT DEPLOY) MAINTENANCE NOTED THE SLIDE LACING WAS UNWRAPPED AND REPLACED THE SLIDE PER AMM 25-65-01/400. AIRCRAFT WAS GROUNDED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,017 hrs · 16,540 cycles

RIGHT AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY IAW AMM 33-50-25.

Part: ACM — FAILED (LEFT) · airframe 19,664 hrs · 16,290 cycles

SMOKE ODOR DURING APPROACH, FOLLOWED BY LOUD NOISE ON THE LEFT SIDE OF AIRCRAFT, FOLLOWED BY PACK 1 FAIL ON SHORT FINAL AND HOT AIR COMING THRU COCKPIT VENT. AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND THAT THE AIR CYCLE MACHINE HAD THREE BROKEN BLADES AND REPLACED IAW AMM 21-51-05.

Part: WINDOW SHADE — OUT OF ADJUST (CABIN) · airframe 18,752 hrs · 15,493 cycles

AIRCRAFT WAS NOT GNDED. RT OVERWING EXIT WINDOW SHADE WILL NOT OPEN. MX ADJUSTED WINDOW SHADE IAW AMM 25-23-15.

Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 18,396 hrs · 15,175 cycles

AIRCRAFT WAS NOT GNDED. AFT LT SLIDE GAUGE IN RED. REQUIRES REPLACEMENT IAW JC 43C20025001. REPLACED AFT LT SLIDE IAW TASK CARD 43L00025001.

Part: DOOR — FAULTED (OVERWING EXIT) · airframe 18,316 hrs · 15,104 cycles

RETURNED, ACFT WAS NOT GNDED. CLIMBING THROUGH 1500" FLIGHT CREW RECEIVED EICAS MSG, DOOR EMER LT OPEN. FLIGHT CREW DECLARED AN EMER & RETURNED, WHERE THE ACFT LANDED WITHOUT FURTHER INCIDENT. MSG EXTINGUISHED AFTER LANDING. VENT FLAP FOUND PARTIALLY OPEN UPON ARRIVAL AT GATE. REMOVED OVERWING HATCH. INSPECTED S327, WARNING SWITCH & DOOR HANDLE MECH IAW AMM 52-70-00. RE-INSTALLED DOOR. PRESSURIZED ACFT TO 5 PSI. NO DEFECT NOTED IAW AMM 21-30-00. ACFT OK FOR SERVICE.

Part: SLIDE — UNSERVICEABLE (L2 DOOR)

DURING INSTALL OF L2 SLIDE, SLIDE UNRAVELED. REMOVED & INSTALLED SERVICEABLE EMER EVACUATION SLIDE ASSEMBLY AT L2 AFT PAX DOOR IAW AMM 25-65-01-000-81-A & AMM 25-65-01-400-801-A & CARD 43C81252001 STEP 12.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,095 hrs · 14,030 cycles

COCKPIT FLOOR ANGLE SUPPORT IS CRACKED AT FRAME 12 & BL 0. FABRICATED & INSTALLED NEW ANGLE IAW SRM 51-41-01.

Part: SKIN — CRACKED (LT WING) · airframe 17,095 hrs · 14,030 cycles

C3 CHECK, LT WING TE LOWER SURFACE EXTERNAL SKIN HAS A CRACK ON BOTH SIDES OF THE FASTENER HOLE, 1.25" OTBD OF WING RIB 10. REPAIRED WING SKIN IAW EA 252235.

Part: SLIDING WINDOW — DETERIORATED (COCKPIT) · airframe 17,095 hrs · 14,030 cycles

C3 CHECK, LT SIDE PILOTS SLIDING WINDOW, CANNOT SEE OUT, VISION NOT CLEAR. REPLACED LT SIDE PILOTS SLIDING WINDOW IAW AMM 56-12-00.

Part: SIGN — CRACKED (CABIN) · airframe 17,095 hrs · 14,030 cycles

C3 CHECK, THE R1 DOOR LOWER EMER LIGHT SIGN IS CRACKED. REPLACED R1 DOOR EMER EXIT SIGN. OPERATIONAL CHECKED GOOD IAW AMM 33-50-00 & 33-50-15.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,095 hrs · 14,030 cycles

C3 CHECK, THE L1 DOOR LOWER LAVATORY EMER LIGHT SIGN LENS IS CRACKED. REPLACED THE L1 DOOR LOWER LAVATORY EMER LIGHT SIG. OPERATIONAL CHECKED GOOD IAW AMM 33-50-00 & 33-50-15.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,095 hrs · 14,030 cycles

C3 CHECK, AT THE R1 DOOR THE TOP EMER LIGHT SIGN LENS IS CRACKED. REPLACED THE R1 DOOR THE TOP EMER LIGHT SIGN LENS. OPERATIONAL CHECKED GOOD IAW AMM 3350-00 & 33-50-15.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,095 hrs · 14,030 cycles

3C CHECK, MAIN CABIN RT AFT FLASHLIGHT BATTERY IS LOW. REPLACED FLASHLIGHT BATTERY IAW AMM 33-51-00.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,095 hrs · 14,030 cycles

3C CHECK, AT THE R1 DOOR THE BOTTOM EMER LIGHT SIGN LENS IS CRACKED. REPLACED THE R1 DOOR THE BOTTOM EMER LIGHT SIGN LENS. OPERATIONAL CHECKED IAW AMM 33-51-00 & 33-50-15.

Part: LENS — CRACKED (EXIT SIGN) · airframe 17,095 hrs · 14,030 cycles

C3 CHECK, THE L1 DOOR TOP EMER LIGHT SIGN LENS IS CRACKED. REPLACED THE L1 DOOR TOP EMER LIGHT SIGN. OPERATIONAL CHECKED GOOD IAW AMM 33-50-00 & 33-50-15.

Part: LENS — CRACKED (EXTERIOR) · airframe 17,095 hrs · 14,030 cycles

C3 CHECK, FAIRING 198NR EMER LIGHT LENS CRACKED. REPLACED FAIRING 198NR EMER LIGHT. OPERATIONAL CHECKED GOOD IAW AMM 33-50-25.

Part: SIGN — DETERIORATED (CABIN) · airframe 17,095 hrs · 14,030 cycles

C3 CHECK, THE LT OVERWING LOWER EMER LIGHT EXIT SIGN IS DETERIORATED. REPLACED THE LT OVERWING LOWER EMER LIGHT EXIT SIGN IS DETERIORATED. OPERATIONAL CHECKED GOOD IAW AMM 33-50-00 & 33-50-15.

Part: GLOWSTRIP — DAMAGED (CABIN)

MAIN CABIN LT & RT PHOTO LUMINESCENT STRIPS HAVE MORE THAN 10% DAMAGED. R & R LT & RT PHOTO LUMINESCENT STRIPS AT MAIN CABIN IAW AMM 33-50-21.

Part: SETSCREW — BROKEN (SERVICE DOOR)

FORWARD SERVICE DOOR, FWD SIDE BOLT IS BROKEN & REQUIRES A NUT. R & R FWD SERVICE DOOR GIRT BAR FWD SET SCREW & LOCKNUT IAW 52-41-00 TW ID 15-083 DD 12 18 2015. GIRT BAR ADJUSTMENT CHECKED GOOD.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,095 hrs · 14,030 cycles

C3 CHECK, AFT MAIN CABIN FLOOR STRUCTURE GUSSET AT FRAME 90 & Y 584.2 IS CORRODED. R & R GUSSET IAW SRM 51-41-02.

Part: BEARING — FROZEN (SERVICE DOOR) · airframe 17,095 hrs · 14,030 cycles

C3 CHECK, FROZEN ROLLER BEARINGS, 2 AT FWD SERVICE DOOR EXTERNAL HANDLE BOX MECHANISM. REMOVED, CLEANED & REINSTALLED 2 EACH ROLLER BEARINGS AT FWD SERVICE DOOR EXTERNAL HANDLE BOX MECHANISM IAW CMM 52-41-22. OPERATIONAL CHECKED GOOD.

Part: BEARING — FROZEN (PAX DOOR) · airframe 170,995 hrs · 14,030 cycles

C3, FROZEN ROLLER BEARING ON AT AFT PAX DOOR EXTERNAL HANDLE BOX MECHANISM. REMOVED, CLEANED & REINSTALLED ROLLER BEARING AT AFT PAX DOOR EXTERNAL HANDLE BOX MECHANISM IAW CMM 52-12-22. OPERATION CHECKED GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,095 hrs · 14,030 cycles

C3 CHECK, COCKPIT FLOOR ANGLE SUPPORT IS CRACKED AT FRAME 12 & LBL37. FABRICATED & INSTALLED ANGLE SUPPORT IAW SRM 51-41-01.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 16,641 hrs · 13,695 cycles

FORWARD FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE. INSTALLED NEW BATTERY. OPERATIONAL CHECK IS GOOD.

Part: SEAL — LACK OF LUBE (L1 DOOR) · airframe 16,348 hrs · 13,507 cycles

FLIGHT ATTENDANT REPORTED THAT MAIN CABIN DOOR 1L VERY DIFFICULT TO CLOSE & AIR LEAKING NOISE INFLIGHT. INSPECTED, CLEANED & LUBED MAIN CABIN 1L DOOR SEAL AS REQUIRED. CHECKED OKAY.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 15,301 hrs · 12,649 cycles

ON DEPARTURE AFTER GEAR RETRACTION ACRID SMELL IN THE COCKPIT & THROUGHOUT ENTIRE CABIN. R & R NR 2 ACM & HEAT EXCHANGER DUE TO BLADE DAMAGE FROM THE ACM. R & R RECIRCULATION FILTERS.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 14,921 hrs · 12,255 cycles

THE RT PYLON LOWER LINK OTBD FITTING SHEAR PIN LOCKNUT LOOSE & THE BUSHING MIGRATED. RE-TORQUED THE LOCKNUT & APPLIED THE APPROPRIATE SAFETIES.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 14,921 hrs · 12,255 cycles

RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE LT PYLON INBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFTIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.

Part: CONNECTOR — BROKEN (RT WING) · airframe 14,861 hrs · 12,187 cycles

BLEED 2 LEAK EICAS MSG, FOLLOWED QRH PROCEDURES. EICAS MSG EXTINGUISHED. BLEED 2 LEAK EICAS ILLUMINATED AGAIN. ACCOMPLISHED QRH PROCEDURE, DEPRESSURIZED ACFT. FOUND LOOP 5 BEHIND RT WING TO BODY FAIRING CONNECTOR J1059 BROKEN. REPLACED CONNECTOR.

Part: SLIDE — UNSERVICEABLE (L2 DOOR)

L2 DOOR SLIDE NEEDS CHANGED DUE TO PIN ENGAGEMENT. REPLACED L2 DOOR SLIDE, OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,199 hrs · 10,986 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT POWER UNIT.

Part: MODULE — FAULTY (BRAKE SYSTEM) · airframe 10,933 hrs · 9,224 cycles

ON LANDING ROLLOUT ABOUT 90 KNOTS EICAS MESSAGE FOR ABOUT 2 SECONDS RT/LT BRAKE FAIL - NO BRAKES AND THEN EICAS MESSAGE WENT AWAY AND NORMAL BRAKES. REMOVED AND REPLACED MAIN AUTO BRAKE MODULE.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON BOX BEAM PANEL BETWEEN FR87 TO FR88, Z-490 & BETWEEN Y273 TO Y893. REPLACED BOX BEAM PANEL IAW TYPICAL REPAIR TR 190-5300-11-0563.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON BOX BEAM AT FR87, Z-490, Y273. REPLACED BOX BEAM IAW TYPICAL REPAIR TR 190-5300-11-0563.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON BOX BEAM PLATE BETWEEN FR87 TO FR88, Z-490, -Y273. REPLACED BOX BEAM PLATE BETWEEN FR87 TO FR88, Z-490, -Y273 IAW TYPICAL REPAIR TR190-5300-11-0563.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR TRACK BEAM BETWEEN FR12 & FR20+8 INCHES, Z-490, Y273. REPLACED FLOOR TRACK BEAM BETWEEN FR12 & FR20+8 INCHES, Z-490, Y273 IAW TYPICAL REPAIR TR 190-5300-11-0563A & SRM PART 2, 51-41-00.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 GALVANIC CORROSION ON SPICE PLATE AT FR90, Z-490, Y625. REPLACED SPICE PLATE AT FR90, Z-490, Y625 IAW DRAWING 170-60001-825 & EMBRAER SRM 51-40-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR85 TO FR86, Z-490, Y273. REPLACED FLOORBEAM BETWEEN FR85 TO FR86, Z-490, Y273 IAW EMBRAER SRM 51-41-01 & TYPICAL REPAIR TR190-5300-11-0563A.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 GALVANIC CORROSION ON SPICE PLATE AT FR90, Z-490, Y507. REPLACED SPICE PLATE AT FR90, Z-490, Y507 IAW DRAWING 170-60001-825 & EMBRAER SRM 51-40-04.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON BOX BEAM PLATE AT FR87, Z-490, Y273. REPLACED BOX BEAM PLATE AT FR87, Z-490, Y273 IAW TYPICAL REPAIR TR190-5300-11-0563.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON SPICE PLATE BETWEEN FR87 TO FR88, Z-490. REPLACED SPICE PLATE BETWEEN FR87 TO FR88, Z-490 IAW DRAWING 170-6600-439.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR87 TO FR88, Z-490, Y273. REPLACED FLOORBEAM BETWEEN FR87 TO FR88, Z-490, Y273 IAW EMBRAER SRM 53-23-10 & DRAWING 170-65660-439.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON BOX BEAM AT FR87, Z-490 & BETWEEN Y273 TO Y625. REPLACED BOX BEAM IAW TYPICAL REPAIR TR 190-5300-11-0563.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR86 TO FR87, Z-490, -Y273. REPLACED FLOORBEAM BETWEEN FR86 TO FR87, Z-490, -Y273 IAW EMBRAER SRM 51-43-01 & DRAWING 170-65660-439.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FORWARD ENTRANCE FLOOR DOUBLER BETWEEN FR13 TO FR16, Z-490 & BETWEEN Y315 TO Y925. REPLACED FORWARD ENTRANCE FLOOR DOUBLER IAW EMBRAER SRM 51-41-00 & TYPICAL REPAIR TR 190-5300-11-0563A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM UPPER SHEET BETWEEN FR85 TO FR86, Z-490, -Y273. REPLACED FLOORBEAM UPPER SHEET BETWEEN FR85 TO FR86, Z-490, -Y273 IAW EMBRAER SRM 51-41-01 & 51-43-01.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 GALVANIC CORROSION ON BOX BEAM AT FR87, Z-490 & BETWEEN Y273 TO Y625. REPLACED BOX BEAM IAW TYPICAL REPAIR TR 190-5300-11-0563A.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON BOX BEAM PANEL BETWEEN FR87 TO FR88, Z-490 & BETWEEN Y273 TO Y893. REPLACED BOX BEAM PANEL IAW TYPICAL REPAIR TR 190-5300-11-0563.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - EXFOLIATION CORROSION ON GUSSET PLATE AT FR90, -Y273. REPLACED GUSSET PLATE AT FR90, -Y273 IAW E190 SRM 51-41-02, SRM 51-40-04.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SILL PLATE BETWEEN FR12 TO FR16 & BETWEEN Y1090 TO Y1280. REPLACED SILL PLATE BETWEEN FR12 TO FR16 & BETWEEN Y1090 TO Y1280 IAW TYPICAL REPAIR TR190-5300-11-0563 & EMBRAER SRM 51-41-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - EXFOLIATION CORROSION ON FLOORBEAM AT FR17, S17R, -Z490. REPLACED FLOORBEAM AT FR17, S17R, -Z490 IAW E190 SRM 51-41-00, PART 2.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,756 hrs · 9,063 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FORWARD ENTRANCE SILL PLATE BETWEEN FR12 TO FR14 & BETWEEN -Y980 TO -Y1280. REPLACED SILL PLATE BETWEEN FR12 TO FR14 & BETWEEN -Y980 TO -Y1280 IAW TYPICAL REPAIR TR190-5300-11-0563 & EMBRAER SRM 51-43-02.

Part: MODULE — INOPERATIVE (CABIN)

EMERGENCY LIGHT BATTERY FAULT. MAINTENANCE REMOVED & REPLACED GENERIC I/O MODULE MAU 2 SLOT 9/10. I/O MODULE CHECKS GOOD.

Part: POWER UNIT — INOPERATIVE (CABIN)

EMERGENCY LIGHT BATTERY FAULT. MAINTENANCE RESEATED CONNECTOR PLUG P1711, REMOVED & REPLACED A/C POWER UNITS EMERGENCY LIGHTING FWD, MID &AFT RIGHT SIDE OF A/C. POWER UNITS CHECK GOOD.

Part: POWER UNIT — INOPERATIVE (CABIN)

EMERGENCY LIGHT BATTERY FAULT. MAINTENANCE RESEATED CONNECTOR PLUG P1711, REMOVED & REPLACED A/C POWER UNITS EMERGENCY LIGHTING FWD, MID &AFT RIGHT SIDE OF A/C. POWER UNITS CHECK GOOD.

Part: CONNECTOR — NOT SEATED (CABIN)

EMERGENCY LIGHT BATTERY FAULT. MAINTENANCE RESEATED CONNECTOR PLUG P1711, REMOVED & REPLACED A/C POWER UNITS EMERGENCY LIGHTING FWD, MID & AFT RIGHT SIDE OF A/C. POWER UNITS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,369 hrs · 8,726 cycles

EMERGENCY LIGHT BATTERY FAULT MESSAGE ON EICAS. MAINTENANCE CHARGED BATTERY POWER UNITS. OPERATIONAL CHECK IS GOOD.

Part: CABLE — LACK OF LUBE (R2 DOOR) · airframe 10,109 hrs · 8,459 cycles

THE 2R DOOR HANDLE HARD TO ARM. MAINTENANCE LUBRICATED DOOR ARMING CABLE OPERATIONAL CHECK IS GOOD.

Part: CABLE — BROKEN (GIRT BAR) · airframe 9,964 hrs · 8,315 cycles

FOUND ARMING CABLE BROKEN ON R2 DOOR. MAINTENANCE REMOVED & REPLACED R2 DOOR EVACUATION SLIDE MECHANISM. OPS CHECKED OKAY.

Part: BOTTLE — LOW PRESSURE (SERVICE DOOR) · airframe 8,709 hrs · 7,305 cycles

BOS - AFT SERVICE DOOR REQUIRES SERVICING. MAINTENANCE SERVICED THE AFT SERVICE DOOR PER AMM 52-45-51-03.

Part: SENSE LINE — CONTAMINATED (BLEED AIR SYS) · airframe 8,356 hrs · 7,003 cycles

FLIGHT 703, PHL-PIT - BLEED 2 OVERPRESS CAUTION EICAS ON CLIMBOUT. QRH PROCEDURE FOLLOWED. BLEED 2 OVERPRESS REMOVED ANNUNCIATED UNTIL NR 2 THRUST LEVER TO IDLE IAW QRH. NOTE: ON ECS SYNOPTIC PAGE. NR 2 BLEED INDICATED 120 PSI BEFORE BLEED SELECTED OFF. MAINTENANCE - PER FIM PROCEDURE 36-14-00-810-809A, REMOVED WATER CONTAMINATION FROM PRESSURE SENSE LINE, AND REMOVED AND REPLACED BLEED PRESSURE SENSOR PER AMM 36-14-02 UPS CHECK GOOD AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (CABIN)

BOS - OVERWING EMERGENCY LIGHTS MID CEILING PANEL INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY NICAD BATTERY.

Part: SLIDE — MALFUNCTIONED (R2 DOOR) · airframe 5,786 hrs · 4,721 cycles

PIT - C1 - EES - JOB CARD 43T20025001 - DURING R-2 DOOR EMERGENCY EVACUATION SLIDE TEST, SLIDE HUNG UP BETWEEN DOOR & AIRCRAFT AFTER DOOR WAS FULLY OPENED MANUALLY & EMERGENCY LIGHTS FAILED TO ILLUMINATE. REPLACED SLIDE AT R-2 DOOR.

Part: PLUNGER — DIRTY (R2 DOOR) · airframe 5,786 hrs · 4,721 cycles

PIT - C1 - EES - JOB CARD # 43T20025001 - DURING R-2 DOOR EMERGENCY EVACUATION SLIDE TEST, PNEUMATIC ASSEMBLY DID NOT FULLY OPEN DOOR WITH 2200 PSI. REMOVED CLEANED & REINSTALLED PNEUMATIC ASSEMBLY PLUNGER & SPRING ASSEMBLY.

Part: ACCUMULATOR — LOW PRESSURE (R1 DOOR)

ATL - THE R1 DOOR EMERGENCY ACCUMULATOR PRESSURE IS LOW. MAINTENANCE SERVICED THE R1 EMERGENCY ACCUMULATOR.