N963UW

Part: UNKNOWN — ODOR (CABIN) · airframe 23,950 hrs · 17,455 cycles

AIRCRAFT WAS GROUNDED: DURING TAKEOFF ODOR DETECTED THROUGHOUT AIRCRAFT, SMELLED LIKE HEATER BEING USED FOR THE FIRST TIME OF SEASON. FLIGHT ATTENDANT REPORTED FEELING ILL FROM ODOR. NO CUSTOMERS REPORTED ILL EFFECTS. ODOR BEGAN TO DISSIPATE WITHIN 5 MINUTES. CLEARED UP DURING REMAINDER OF CLIMB, SLIGHT ODOR DETECTED AT BEGINNING OF DESCENT CLOSED X BLEED AND TURNED OFF NR 1 PACK AND IT SEEMED TO DISSIPATE, BUT SMELLED HOT. MAINTENANCE ACCOMPLISHED INITIAL TROUBLESHOOTING PER JOB CARD 43L00021001 AND BLEED AIR-BLASTER PROCEDURE PER JOB CARD 43L00036002. NO ODOR NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,811 hrs · 17,342 cycles

AIRCRAFT WAS NOT GROUNDED. PHOTOLUMINESCENT INDICATOR STRIP LIGHTS WERE INOPERABLE IN THE FIRST CLASS AREA. MAINTENANCE REPLACED LIGHTS PER AMM 33-50-21 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: RELEASE MECH — BROKEN (COCKPIT DOOR) · airframe 23,745 hrs · 17,287 cycles

EMERGENCY RELEASE PIN ON THE UPPER INTERIOR SIDE OF THE COCKPIT DOOR WAS BROKEN. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE RELEASE CHORD AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 22,702 hrs · 16,440 cycles

RIGHT AFT DOOR EMERGENCY EXIT LIGHT LENS CRACKED. MAINTENANCE REPLACED THE LENS IAW AMM 33-50-00, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: SMOKE DETECTOR — FALSE INDICATION (FWD LAVATORY) · airframe 21,379 hrs · 15,365 cycles

LAVATORY SMOKE WARNING APPEARED FOR 5-6 SECONDS. INSPECTED FORWARD DETECTORS WITH NO FAULTS FOUND.

Part: OIL SYSTEM — OVERSERVICED (LT ENGINE) · airframe 21,027 hrs · 15,055 cycles

AIRCRAFT WAS GROUNDED. IMMEDIATELY AFTER TAKEOFF STRONG ELECTRICAL BURNING SMELL WITH NO VISIBLE SMOKE. FLIGHT RETURNED TO FIELD AND DECLARED AN EMERGENCY. LEFT HAND ENGINE OIL OVERSERVICED. DRAINED OIL TO PROPER LEVEL.

Part: LINK — WORN (ENGINE) · airframe 21,020 hrs · 15,050 cycles

FORWARD MOUNT LINKS WORN. REPLACED THE MOUNT LINKS IAW MM 71-00-20-450-804.

Part: MODULE — FAILED (AVIONICS) · airframe 20,440 hrs · 14,598 cycles

DURING APPROACH, CREW REPORTED A FAILURE OF THE MODULAR AVIONICS UNIT 3A. DECLARED EMERGENCY, PERMANENT LOSS OF FMS 2 A/P CHANNEL 2 GPS 2. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED PROCESSOR MODULE IAW AMM TASK 31-41-04-000-801A. ACCOMPLISHED NAVIGATIONAL DATA BASE LOAD IAW JOB CARD 43T22034001.

Part: MODULE — FAILED (AVIONICS) · airframe 20,440 hrs · 14,598 cycles

DURING APPROACH, FLIGHT CREW REPORTED A FAILURE OF THE MODULAR AVIONICS UNIT 3A. DECLARED EMERGENCY AT 24,000, PERMANENT LOSS OF FMS 2 A/P CHANNEL 2 GPS 2. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED PROCESSOR MODULE PER AMM TASK 31-41-04-000-801A. ACCOMPLISHED NAVIGATIONAL DATA BASE LOAD PER JOB CARD 43T22034001.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 19,550 hrs · 13,898 cycles

AIRCRAFT WAS GROUNDED: CAPTAIN`S WINDSHIELD CRACKED. REPLACED CAPTAIN`S WINDSHIELD IAW AMM 56-11-00-000-801-A AND 56-11-00-400-801-A.

Part: ROLLER — SEIZED (OVERWING EXIT) · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT OVERWING EXIT DOOR CUTOUT, UPPER ROLLERS, 2EA ARE FROZEN. CLEANED & EXERCISED 2EA ROLLERS AT LT OVERWING EXIT AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 12-21-01.

Part: ROLLER — FROZEN (OVERWING EXIT) · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: RT OVERWING EXIT DOOR CUTOUT, UPPER ROLLERS, 2 EA ARE FROZEN. CLEANED & EXERCISED RT OVERWING EXIT DOOR ROLLERS AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 12-22-01.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE, R2 DOOR SURROUND EMERGENCY LIGHT IS HALF INOPERATIVE. REPLACED EMERGENCY EXIT IDENTIFIER SIGN AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-50-15-400-801-A.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN WING BOX FLOOR SUPPORT HAS CRACK AT FRAME 45 AND LBL 10. REPAIRED FLOOR SUPPORT IAW EA 262892.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN WING BOX FLOOR SUPPORT HAS CRACK AT FRAME 45 AND RBL 10. REPAIRED FLOOR SUPPORT IAW EA 262896.

Part: HINGE FITTING — EXCESS PLAY (LT WING) · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT AILERON NR 3 HINGE FITTING FAILED BACKLASH CHECK. REPLACED HINGE FITTING IAW AMM 57-61-00-000-801.

Part: HINGE FITTING — EXCESS PLAY (LT WING) · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT AILERON NR 2 HINGE FITTING FAILED BACKLASH CHECK. REPLACED HINGE FITTING IAW AMM 57-61-00-000-801.

Part: HINGE FITTING — EXCESS PLAY (LT WING) · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: LT AILERON NR 1 HINGE FITTING FAILED BACKLASH CHECK. REPLACED HINGE FITTING IAW AMM 57-61-00-000-801.

Part: HINGE FITTING — EXCESS PLAY (LT WING) · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT AILERON NR 4 HINGE FITTING FAILED BACKLASH CHECK. REPLACED HINGE FITTING IAW AMM 57-61-00-000-801.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

ACFT IN BASE MAINTENANCE: CORROSION ON SKIN BETWEEN FRAME 73 AND FRAME 74 AT STR 29 LT. REPAIRED SKIN IAW EA 262904.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STR SPLICE BETWEEN FRAME 73 AND FRAME 74 AT STR 29 LT. REPLACED STR SPLICE IAW DWG 190-17825-803 AND SRM 51-43-03.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER SPLICE BETWEEN FRAME 73 AND FRAME 74 AT STR 29 LT. REPLACED STRINGER SPLICE IAW DWG 1700-17825-803 AND SRM 51-43-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT MAIN CABIN LT SEAT TRACK AT FRAME 84 AND FRAME-Y305. REPAIRED SEAT TRACK IAW SRM 53-00-10, REPAIR 51, FIG 205.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: VERTICAL STABILZER T/E RIB NR 9 CRACKED ON RT ATTACH POINT SEVERAL PLACES. REPLACED RIB IAW DWG 170-63200-451 AND E190 SRM 51-41-01.

Part: LENS — CRACKED (EXTERIOR LIGHT) · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: LT LOWER EMERGENCY LIGHT LENS CRACKED ON AFT WING TO FUSELAGE FAIRING. REPLACED EMERGENCY LIGHT LENS IAW AMM 33-50-25.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON FORWARD MAIN CABIN RT FLOOR TRACK BETWEEN FRAME 12 AND FRAME 18 AT +Y276. REPLACED FLOOR TRACK IAW E190 AARD 53-00-00-3, REPAIR 3, SRM 51-40-02, 51-41-01 AND 51-41-02.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

CORROSION ON AFT MAIN CABIN LEFT HAND SHEAR PLATE BETWEEN FRAMES 87 & 88 AND BETWEEN -Y304 & -Y1041. REPLACED SHEAR PLATE IAW AARD 53-00-00-3 REPAIR 3 & SRM 51-42-03 & 51-40-02.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON GALLEY SUPPORT FITTING BETWEEN FRAME 87 AND FRAME 88 AT +Y584. REPLACED GALLEY SUPPORT FITTING IAW SRM 51-43-03,51-40-02 & DWG: 170-65660-447.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON AFT MAIN CABIN RT SHEAR PANEL BETWEEN FRAME 87 & FRAME 88 AT +Y1041. REPLACED SHEAR PANEL IAW SRM 51-42-01,51-40-02,51-42-02 & E190 AARD 53-00-00-3, REPAIR 3.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON GALLEY SUPPORT FITTING BETWEEN FRAME 87 AND FRAME 88 AT +Y889. REPLACED GALLEY SUPPORT FITTING IAW SRM 51-10-03, 51-43-03 AND DWG 170-65660-447.

Part: SUPPORT FITTING — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

CORROSION ON GALLEY SUPPORT FITTING BETWEEN FRAMES 87 & 88 AT -Y914. REPLACED GALLEY SUPPORT FITTING IAW DRAWING 170-65660-447.

Part: GUSSET — CHAFED (SERVICE DOOR) · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD SERVICE DOOR GUSSET PLATE IS CHAFED AT DOOR BEAM NR 3. REPLACED GUSSET PLATE DWG 170-68200-411 AND SRM 51-40-02,51-41-01 & 51-42-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES 86-89) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

CORROSION ON AFT MAIN CABIN RIGHT FLOOR SUPPORT BETWEEN FRAMES 85 & 86 AT +Y260. REPLACED FLOOR SUPPORT IAW SRM 51-41-01, 51-43-01,51-40-02, 51-42-01, 51-43-03 AND E190 AARD 53-00-00-3 REPAIR 3.

Part: DOUBLER — CORRODED (FRAME 16) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

CORROSION ON FORWARD MAIN CABIN LEFT FORWARD FLOOR DOUBLER AT FRAME 16 AND -Y330. REPLACED THE DOUBLER IAW SRM 51-41-02, 51-40-02 AND 53-00-00-3 REPAIR 3.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHEAR PLATE BETWEEN FRAME 87 AND FRAME 88, BETWEEN Y=-222 AND Y=+222. REPLACED SHEAR PLATE IAW AARD 53-00-00-3, REPAIR 3 AND SRM 51-43-03.

Part: FLOOR SUPPORT — CORRODED (FRAMES 89-90) · corrosion level 2 · airframe 19,516 hrs · 13,782 cycles

CORROSION ON AFT MAIN CABIN RIGHT FLOOR SUPPORT BETWEEN FRAMES 89 & 90 BETWEEN +Y946 AND +Y997. REPLACED FLOOR SUPPORT IAW SRM 51-43-03, 51-42-01, 51-40-02, 51-43-03, 51-41-02 AND 53-00-00-3 REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

CORROSION ON AFT MAIN CABIN LEFT INBOARD FLOOR SUPPORT AT FRAME 84 AND -Y330. REPLACED THE FLOOR SUPPORT IAW SRM 51-43-01, 51-43-03 AND 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

CORROSION ON FORWARD MAIN CABIN RIGHT FLOOR SUPPORT BETWEEN FRAMES 17 AND 18 AT +Y330. REPLACED THE FLOOR SUPPORT IAW SRM 51-43-03, 51-41-02, 51-40-02, 51-43-02, 51-43-01 AND DRAWING 170-00822-503.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD MAIN CABIN LT FORWARD FLOOR SILL AT FRAME 16 AND Y= -1145. REPLACED FLOOR SILL IAW SRM 51-41-02, 51-43-04, 51-40-02, 51-40-06 AND AARD 53-10-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 86) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

CORROSION AND A CRACK ON FLOOR SUPPORT LOCATED AT FRAME 86 AND -Y717. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-66000-455 & SRM'S 51-40-02 & 51-43-01.

Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

CORROSION ON AFT MAIN CABIN CENTER SPLICE AT FRAME 90 AND Y 0. REPLACED SPLICE IAW DRAWING 170-65660-447, SRM 51-40-02& 51-43-03.

Part: UPPER SHEET — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

CORROSION ON AFT MAIN CABIN RIGHT HAND UPPER SHEET BETWEEN FRAMES 85 - 86, +Y260. REMOVED AND REPLACED UPPER SHEET IAW SRM 51-41-01 & 51-43-03 AND AARD 53-00-00-3 REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

CORROSION ON AFT MAIN CABIN LEFT OUTBOARD PANEL SUPPORT AT FRAME 84 AND BETWEEN -Y939 AND -Y1016. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-66000-455, SRMS 51-40-02, AND 51-43-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

CORROSION ON FORWARD MAIN CABIN RIGHT FORWARD FLOOR SUPPORT BETWEEN FRAMES 12 AND 14, BETWEEN +Y920 AND +Y1244. REPLACED THE FLOOR SUPPORT IAW AARD 53-00-00-3 REPAIR 3 FIG 1 SHT 3, SRM 51-40-02, 51-41-02, AND 51-43-04.

Part: FLOOR SUPPORT — CORRODED (FRAMES 88-90) · corrosion level 2 · airframe 19,516 hrs · 13,782 cycles

CORROSION ON AFT MAIN CABIN LEFT FLOOR SUPPORT BETWEEN FRAMES 88 - 90, BETWEEN -Y946 AND -Y997. REPLACED THE FLOOR SUPPORT IAW 53-00-00-3 REPAIR 3, SRM 51-40-02, 51-41-02 & 51-41-01.

Part: UPPER SHEET — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 19,516 hrs · 13,783 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT MAIN CABIN ON LEFT HAND UPPER SHEET BETWEEN FR 85 & FR 86 AT -Y260. REPLACED UPPER SHEET PER AARD 53-00-00-3 REPAIR 3 AND SRM'S 51-43-03, 51-41-02.

Part: GUSSET — CHAFED (SERVICE DOOR) · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MANITNENACE, AFT SERVICE DOOR, UPPER FORWARD FRAME GUSSET HAS CHAFE DAMAGE. REPLACED GUSSET PLATE IAW SRM 51-43-03 AND DWG 170-69500-417.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

CORROSION ON AFT MAIN CABIN RIGHT OUTBOARD UPPER GUESSET AT FRAME 90 BETWEEN +Y457 AND +Y698. REPLACED THE GUESSET IAW SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,516 hrs · 13,872 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON FORWARD MAIN CABIN LT AFT FLOOR SUPPORT AT FRAME 19 AND -Y1092. REPLACED FLOOR SUPPORT IAW DWG 170-29712-802, SRM 51-43-01 AND SRM 51-23-04.

Part: LIGHT — DIRTY (CABIN) · airframe 19,263 hrs · 13,657 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY PATH MARKINGS IN FLOOR IN VICINITY OF SEAT 1D SOILED. CAN NOT BE SEEN IN DARK. CLEANED EMERGENCY PATH STRIP AT SEAT 1D.

Part: LINKAGE — LACK OF LUBE (L2 DOOR) · airframe 19,263 hrs · 13,657 cycles

AIRCRAFT WAS NOT GROUNDED: 2L DOOR WHEN ARMING DOOR AND CLOSING VENT FLAPS BOTH LEVERS DO NOT TRAVEL THE SAME DISTANCE LEAVING A GAP BETWEEN LEAVER THAT CAUSED INJURY TO F/A HAND. CLEANED AND LUBED LINKAGE FOR 2L DOOR ARMING MECHANISM AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 52-12-00.

Part: OUTLET — SPARKS (COCKPIT) · airframe 19,165 hrs · 13,551 cycles

AIRCRAFT WAS NOT GROUNDED: SPARKS CAME FROM F/O PC OUTLET CONTROL WHEN TURNED ON. REPLACED F/O PC OUTLET AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 24-54-01.

Part: LIGHT — BROKEN (CABIN) · airframe 18,790 hrs · 13,250 cycles

AIRCRAFT IN BASE MX. MAIN CABIN L1 DOOR FLIGHT ATTENDANT EMER LIGHT BEZEL BROKEN. REPLACED LIGHT BEZEL & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-15.

Part: SLIDE — UNSERVICEABLE (ZONE 800) · airframe 18,508 hrs · 13,039 cycles

AIRCRAFT WAS NOT GNDED. WHILE ACCOMPLISHING A SCHEDULED SLIDE CHANGE, MX DISCOVERED THE FOLLOWING ON THE REPLACEMENT SLIDE. THE ATTACHMENT POINT FOR THE BUSSEL AD A NUTPLATE WITH DAMAGE TO THE RUBBER & PREVENTED INSTALLATION OF THE BUSSEL ATTACHMENT HARDWARE. THE SLIDE RETURNED TO STOCK & A SERVICEABLE SLIDE WAS INSTALLED IN ITS PLACE.

Part: LENS — DETACHED (CABIN) · airframe 18,398 hrs · 12,928 cycles

AIRCRAFT WAS NOT GNDED. OVERWING EMER LIGHT COVER FALLS OUT OF COVER. REPLACED LENS COVER & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-00.

Part: FITTING — DIRTY (GIRT BAR) · airframe 70,210 hrs · 26,901 cycles

AIRCRAFT WAS GNDED. L1 DOOR WILL NOT DISARM. FOUND EXCESSIVE DIRT ON GIRT BAR FITTINGS, REMOVED DIRT. OPERATED DOOR IAW FIM 52-11-00-810-806A & 52-11-00-810-808A. ARMED & DISARMED & OPERATED DOOR SEVERAL TIMES FROM BOTH INSIDE & OUTSIDE, COULD NOT DUPLICATE.

Part: GLOWSTRIP — DETACHED (CABIN) · airframe 18,126 hrs · 12,692 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT GLOW STRIP NEAR FWD GALLEY NEEDS TO BE ATTACHED. SECURED EMER LIGHT GLOW STRIP & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — FAULTY (R2 DOOR) · airframe 17,342 hrs · 11,860 cycles

R2 DOOR DOES NOT ARM OR DISARM PROPERLY. R & R AFT RT SERVICE DOOR SLIDE IAW JC 43L00052001.

Part: CABLE — DEFECTIVE (R2 DOOR) · airframe 17,342 hrs · 11,860 cycles

R2 DOOR DOES NOT ARM OR DISARM PROPERLY. IAW EA 252921, SB 190-52-0042 & AMM 52-42-40 R & R THE ARM DISARM CABLE ON THE AFT RT SERVICE DOOR. OPERATIONS CHECKED GOOD.

Part: SEAT — DEFECTIVE (COCKPIT) · airframe 16,365 hrs · 11,033 cycles

FIRST OFFICER SEAT LATERAL SLIDE WILL NOT LOCK. REPLACED FIRST OFFICER SEAT.

Part: MODULE — FAULTY (MLG STEERING) · airframe 16,323 hrs · 10,989 cycles

AT GEAR EXTENSION STEER FAIL CAUTION ON EICAS ILLUMINATED. STEERING DID NOT WORK AFTER LANDING. R & R THE STEERING CONTROL MODULE.

Part: SCREW — LOOSE (COCKPIT DOOR) · airframe 15,224 hrs · 10,033 cycles

COCKPIT DOOR DID NOT REMAIN LOCKED DURING TAKEOFF. FOUND SCREWS LOOSE ON DOOR STOP ANGLE BELOW COCKPIT DOOR LOCK. TIGHTENED SCREWS DOOR CHECKED GOOD.

Part: INSULATION — OUT OF POSITION (ZONE 100) · airframe 14,981 hrs · 9,803 cycles

EN-ROUTE PRESSURIZATION AUTO FAIL. RESET ACCOMPLISHED & DID NOT RESET 1ST TIME FAILED AGAIN & DID NOT RESET. PRESSURIZATION MAN FAIL WHILE ACCOMPLISHING MAN PRESSURIZATION PROCEDURE. FOUND INSULATION BLANKET OBSTRUCTING CPCS OUT FLOW VLV. REMOVED BLANKET & PERFORMED SATISFACTORY FUNCTION TEST OF THE PRESSURIZATION CONTROL SYS.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 14,962 hrs · 9,793 cycles

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.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 14,962 hrs · 9,793 cycles

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.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 14,962 hrs · 9,793 cycles

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.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 14,962 hrs · 9,793 cycles

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.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR SUPPORT UPPER SHEET BETWEEN FRAME 84 TO 85, Z-490MM, -Y203.2. REPLACED CABIN FLOOR SUPPORT UPPER SHEET BETWEEN FRAME 84 TO 85, Z-490MM, -Y203.2 SRM 53-23-10, FIG 55.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SEAL REST BETWEEN FRAME 77 TO 80, Z-1550MM, Y325MM. REPLACED SEAL REST BETWEEN FRAME 77 TO 80, Z-1550MM, Y325MM IAW SRM 51-10-03, 53-23-11, 53-41-01 & AMM 53-23-29.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SHEAR PANEL BETWEEN FRAME 88 TO 87, Z-490 & BETWEEN Y279.4 TO Y1143. REPLACED SHEAR PANEL BETWEEN FRAME 88 TO 87, Z-490 & BETWEEN Y279.4 TO Y1143 IAW SRM 51-40-02, 51-43-01 & 51-42-01.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 EXFOLIATION CORROSION ON PANEL SUPPORT AT FRAME 89, Z-490 & -Y330.2. REPLACED PANEL SUPPORT AT FRAME 89, Z-490 & -Y330.2 IAW SRM 51-41-01, 51-42-01 & 51-43-01.

Part: DOOR — CORRODED (CARGO BAY) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON FWD CARGO BAY DOOR AT FRAME 24, Z-1550MM, Y600MM. REPLACED FWD CARGO BAY DOOR AT FRAME 24, Z-1550MM, Y600MM SRM 51-10-03.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR DOUBLER AT FRAME 20, Z-490, -Y735. REPLACED FLOOR DOUBLER AT FRAME 20, Z-490, -Y735 IAW E190 51-40-02, 51-41-02 & 51-40-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR TRACK BETWEEN FRAME 18 TO 19, Z-490, -Y279.39. REPLACED FLOOR TRACK BETWEEN FRAME 18 TO 19, Z-490, -Y279.39 IAW SRM 53-10-10, 51-43-04, 51-43-03 & 51-41-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK 13.5 INCHES AFT OF FRAME 75, Y-490MM, Y275MM. REPLACED SEAT TRACK 13.5 INCHES AFT OF FRAME 75, Y-490MM, Y275MM IAW SRM 53-23-10, 51-43-03 & 51-43-04.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SEAL REST BETWEEN FRAME 24 TO 27, Z-1550MM, Y600MM. REPLACED SEAL REST BETWEEN FRAME 24 TO 27, Z-1550MM, Y600MM IAW SRM 51-10-03, 51-41-01, 51-40-02 & 51-41-01.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR STRUCTURE SPLICE AT FRAME 88, Z-490MM, -Y275MM. REPAIRED CABIN FLOOR STRUCTURE SPLICE AT FRAME 88, Z-490MM, -Y275MM IAW EA 507502 & SRM 51-10-03.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SHEAR PANEL AT FRAME 87, Z-490 & BETWEEN -Y304.8 TO -Y762. REPLACED SHEAR PANEL AT FRAME 87, Z-490 & BETWEEN -Y304.8 TO -Y762 IAW SRM 51-43-03, 51-43-03 & 51-40-02.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR STRUCTURE SPLICE AT FRAME 90, Z-490MM, Y=0. REPLACED CABIN FLOOR STRUCTURE SPLICE AT FRAME 90, Z-490MM, Y=0 IAW 51-21-01, 51-75-16 & 51-43-01, PAR 5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FRAME 84, Z-490MM, Y250. REPLACED SEAT TRACK AT FRAME 84, Z-490MM, Y250 SRM 53-23-10, 51-43-03 & 51-43-04.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 EXFOLIATION CORROSION ON SHEAR CLIP AT FRAME 82 BETWEEN STRINGER 27R TO 28R, -Y1559MM. REPLACED SHEAR CLIP AT FRAME 82 BETWEEN STRINGER 27R TO 28R, -Y1559MM IAW SRM 51-75-16, 53-23-04, 51-41-01 & 51-41-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON ANTENNA DOUBLER BETWEEN FRAME 21 TO 22 & BETWEEN STRINGER 27R TO 28R. REPAIRED ANTENNA DOUBLER BETWEEN FRAME 21 TO 22 & BETWEEN STRINGER 27R TO 28R SRM 53-10-01, 51-40-02 & 51-41-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON BAG DOUBLER BETWEEN FRAME 26 TO 27, Z=-1559, Y600MM. REPLACED BAG DOUBLER BETWEEN FRAME 26 TO 27, Z=-1559, Y600MM IAW SRM 51-43-02, 51-41-02 & 51-40-02.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,962 hrs · 9,793 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON BAG DOOR SEAL REST AT FRAME 27, Z-1550MM, Y600MM. REPLACED BAG DOOR SEAL REST AT FRAME 27, Z-1550MM, Y600MM IAW SRM 51-10-03, P 2 & 53-21-11, PG 2.

Part: SENSOR — FAULTY (LE SLAT) · airframe 14,767 hrs · 9,624 cycles

SLAT SLOW SPEED, CHANGED TO AMBER, SLAT FAIL ON EICAS. THE CREW HAD TO PERFORM A NO FLAP LANDING. THE FLIGHT LANDED WITHOUT INCIDENT & TAXIED TO THE GATE. R & R THE RT INBD SKEW SENSOR.

Part: PNEUMATIC SYSTEM — FAULTY (PAX DOOR) · airframe 14,624 hrs · 9,506 cycles

ONE FWD DOOR PNEUMATIC ASSEMBLY KEEPS BLOWING DIAPHRAGM WHEN TRYING TO SERVICE ASSIST BOTTLE. R & R FWD LT PAX DOOR PNEUMATIC ASSEMBLY. LEAK CHECK IS GOOD,

Part: LENS — MISSING (EXIT SIGN) · airframe 14,329 hrs · 9,256 cycles

OVERWING EMERGENCY EXIT SIGN LENS MISSING. INSTALLED OVERWING EMERGENCY EXIT SIGN LENS AS REQUIRED, OPERATIONS CHECKED NORMAL.

Part: BOTTLE — LOW PRESSURE (SERVICE DOOR) · airframe 14,089 hrs · 9,078 cycles

RIGHT AFT SERVICE DOOR PNEUMATIC ASSIST BOTTLE ASSEMBLY REQUIRES SERVICING. SERVICED THE PNEUMATIC ASSIST BOTTLE ASSEMBLY.

Part: BOTTLE — LOW PRESSURE (PAX DOOR) · airframe 13,750 hrs · 8,849 cycles

AFT LEFT DOOR PNEUMATIC ASSEMBLY LOW. MX SERVICED AFT LT DOOR PNEUMATIC ASSEMBLY.

Part: BOTTLE — LOW PRESSURE (PAX DOOR ASSIST) · airframe 12,579 hrs · 7,952 cycles

RT AFT PAX DOOR ASSIST BOTTLE HAS LOW PRESSURE. SERVICED BOTTLE.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYSTEM)

FLT 1118, CLT-PWM - THE CAPTAIN USED EMERGENCY AUTHORITY TO DESCEND TO FL200 AND BELOW OVER BOS DUE TO WING ANTI-ICE FAIL MESSAGE. THE DESCENT WAS NECESSARY TO EXIT ICING CONDITIONS ABOVE FL200. THE FLIGHT CONTINUED TO PWN AND LANDED WITHOUT INCIDENT. MAINTENANCE OPERATED THE SYSTEM, ALL OPERATIONAL CHECKS WERE SATISFACTORY, AC IS OK FOR SERVICE.

Part: PIN — STUCK (GIRT BAR)

FLIGHT 1846 - CLT-PHL - THE FRONT LEFT DOOR WON'T DISARM. PASSENGERS USED AIRSTAIRS TO DEPLANE. MAINTENANCE FOUND THE BUSTLE LANYARD PIN JAMMED UNDER THE GIRT BAR PREVENTING THE SLIDE TO DISARM. THE LANYARD AND PIN WERE FREED AND DISARMED THE DOOR SUCCESSFULLY. SEVERAL OPERATIONAL CHECKS WERE PERFORMED AND VERIFIED POSITIVE ENGAGEMENT OF THE LANYARD PIN IN HOUSING.

Part: LANYARD — JAMMED (L1 DOOR)

DTW - THE FORWARD LEFT ENTRY DOOR ARMING LEVER IS JAMMED IN THE ARMED POSITION. MAINTENANCE REMOVED THE L1 DOOR SLIDE TO FACILITATE REMOVAL OF THE LEFT LANYARD PIN THAT WAS JAMMED UNDER THE GIRT BAR. PERFORMED SEVERAL OPERATIONAL CHECKS OF THE GIRT BAR ENGAGING AND DISENGAGING WITH NO FAULTS.

Part: LANYARD — JAMMED (L1 DOOR)

DTW - THE FORWARD LEFT ENTRY DOOR ARMING LEVER IS JAMMED IN THE ARMED POSITION. MAINTENANCE REMOVED THE L1 DOOR SLIDE TO FACILITATE REMOVAL OF THE LEFT LANYARD PIN THAT WAS JAMMED UNDER THE GIRT BAR. PERFORMED SEVERAL OPERATIONAL CHECKS OF THE GIRT BAR ENGAGING AND DISENGAGING WITH NO FAULTS.

Part: OIL SYSTEM — LOW (APU)

FLIGHT 9225, IAH-PHL - A MAINTENANCE FERRY FLIGHT WITH AN INOPERATIVE GENERATOR RECEIVED APU LOW OIL PRESSURE AMBER ALERT ON EICAS. AFTER CONSULTING THE QRH IT WAS DECIDED TO RETURN TO IAH. UPON LANDING THE APU FAIL LIGHT ILLUMINATED AND THE APU AUTO SHUTDOWN. MAINTENANCE FOUND THE APU OIL QUANTITY LOW AND SERVICED APU AS REQUIRED.

Part: CABLE — OUT OF ADJUST (COCKPIT)

CLT - THE CAPTAIN'S SEAT BACK UNABLE TO REMAIN ERECT OR PROPERLY ADJUST WITHIN FULL RANGE OF MOTION. MAINTENANCE ADJUSTED THE SEAT CABLE.