N961UW

Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 27,075 hrs · 19,970 cycles

AIRCRAFT WAS NOT GROUNDED: AFT FLIGHT ATTENDANT FLASHLIGHT WAS NOT BLINKING. MAINTENANCE REPLACED FLASHLIGHT BATTERY PER AMM 33-51-00.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 25,340 hrs · 18,427 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY SMOKE ON EICAS, RAN CHECKLIST BUT MESSAGE EXTINGUISHED SHORTLY AFTER ILLUMINATION. ALERT CAME ON THE SECOND TIME LAVATORY DOOR SHUT AND NO SMELL WAS PRESENT, NOTHING IN TRASH. CUSTOMER WAS INTERVIEWED, NO SMOKING HAD TAKEN PLACE. MAINTENANCE RESET SMOKE DETECTION SYSTEM PER FIM TASK 26-14-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: WINDOW — CRAZED (LT OVERWIND EXIT) · airframe 25,175 hrs · 18,302 cycles

LEFT OVERWING ESCAPE HATCH WINDOW HAS INTERNAL CRAZING AND SCRATCHED. REPLACED THE WINDOW IAW AMM 56-20-01.

Part: WINDOW — CRAZED (CABIN) · airframe 25,175 hrs · 18,302 cycles

L1 PAX WINDOW WAS CRAZED. REPLACED THE WINDOW IAW AMM 56-20-00.

Part: STOP FITTING — WORN (R1 DOOR) · airframe 25,175 hrs · 18,302 cycles

R1 DOOR CUT OUT, FORWARD LOWER GUIDE RAMP DOOR STOPS WERE WORN. REPLACED THE DOOR STOPS IAW AMM 53-10-25, AND 52-41-00.

Part: STOP FITTING — WORN (AFT PAX DOOR) · airframe 25,175 hrs · 18,302 cycles

AFT PASSENGER DOOR CUT OUT, AFT UPPER GUIDE RAMP, DOOR STOPS WORN. REPLACED THE DOOR STOPS IAW AMM 53-23-21, AND 52-12-00.

Part: STOP FITTING — WORN (AFT PAX DOOR) · airframe 25,175 hrs · 18,302 cycles

AFT PASSENGER DOOR CUT OUT AFT LOWER GUIDE RAMP DOOR STOPS WERE WORN. REPLACED THE DOOR STOPS IAW AMM 53-23-21, AND 52-12-00.

Part: STOP FITTING — WORN (R1 DOOR) · airframe 25,175 hrs · 18,302 cycles

R1 DOOR CUT OUT, FORWARD UPPER GUIDE RAMP DOOR STOPS WERE WORN. REPLACED THE DOOR STOPS IAW AMM 53-10-25, AND 52-41-00.

Part: SEAL DEPRESSOR — CORRODED (FRAMES 25-26) · airframe 25,175 hrs · 18,302 cycles

CORROSION ON THE AFT CARGO DOOR CUTOUT CENTER LOWER SEAL DEPRESSOR BETWEEN FRAMES 25 AND 26. REPLACED SEAL DEPRESSOR IAW RD 53-00-00-3.

Part: DAMPENER — CORRODED (L2 DOOR) · airframe 18,302 hrs · 25,175 cycles

MAINTENANCE FOUND THE L2 DOOR CUTOUT FWD SIDE, DOOR DAMPNER ASSY, LARGE THREADED AREA CORRODED. REMOVED AND REPLACED THE DAMPER ASSY IAW AMM 52-12-27-000-801-A, AND 52-12-27-400-801-A. ADJUSTMENT CHECKED GOOD.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · airframe 25,175 hrs · 18,302 cycles

CORROSION FOUND ON AFT CABIN WET AREA SHEAR PANEL, FRAMES 87 - 88, +Y584 - +Y914. REPLACED THE SHEAR PANEL IAW RD 53-00-00-3.

Part: WEB — CORRODED (FRAMES 12-13) · airframe 25,175 hrs · 18,302 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON THE FORWARD MAIN CABIN LEFT FLOOR WEB BETWEEN FRAMES 12 - 13, -Y373. REPLACED THE WEB IAW RD 53-10-00-2.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · airframe 25,175 hrs · 18,302 cycles

CORROSION FOUND ON THE AFT CABIN WET AREA FLOOR CENTER SHEAR PANEL BETWEEN FRAMES 87 - 88, -Y380 & +Y380. REPLACED THE SHEAR PANEL IAW RD 53-00-00-3.

Part: FLOOR SUPPORT — CORRODED (FRAME 87) · airframe 25,175 hrs · 18,302 cycles

CORROSION FOUND ON THE AFT CABIN WET AREA FLOOR SUPPORT AT FRAME 87, -Y762. REPLACED THE FLOOR SUPPORT IAW SRM 51-43-01.

Part: WEB — CORRODED (FRAMES 15-16) · airframe 25,175 hrs · 18,302 cycles

CORROSION FOUND ON THE FORWARD CABIN, LEFT UPPER WEB BETWEEN FRAMES 15 AND 16, -Y373. REPLACED THE WEB IAW RD 53-00-00-3.

Part: GUSSET — CORRODED (FRAME 90) · airframe 25,175 hrs · 18,302 cycles

CORROSION FOUND ON THE AFT CABIN FLOOR GUSSET AT FRAME 90, +Y584. REPLACED THE GUSSET IAW RD 51-20-01-1.

Part: FLOOR SUPPORT — CORRODED (FRAME 88) · airframe 25,175 hrs · 18,302 cycles

CORROSION FOUND ON THE AFT CABIN FLOOR SUPPORT AT FRAME 88, +Y914. REPLACED THE FLOOR SUPPORT IAW SRM 51-75-16.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · airframe 25,175 hrs · 18,302 cycles

CORROSION FOUND ON THE FORWARD MAIN CABIN FLOOR SUPPORT BETWEEN FRAMES 17 & 18, +Y323. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · airframe 25,175 hrs · 18,302 cycles

CORROSION FOUND ON THE LEFT AFT CABIN WET AREA FLOOR SHEAR PANEL, FRAMES 87 AND 88, -Y381 AND -Y965. REPLACED THE SHEAR PANEL IAW RD 53-00-00-3.

Part: SEAT TRACK — CORRODED (FRAMES 12-14) · airframe 25,175 hrs · 18,302 cycles

CORROSION ON FORWARD MAIN CABIN RIGHT SEAT TRACK, FRAMES 12 - 14, +Y273. REPLACED THE SEAT TRACK IAW SRM 51-41-01.

Part: WEB — CORRODED (FRAMES 19-20) · airframe 25,175 hrs · 18,302 cycles

CORROSION FOUND ON THE FORWARD MAIN CABIN LEFT FLOOR WEB BETWEEN FRAMES 19 - 20, -Y633. REPLACED THE WEB IAW SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · airframe 25,175 hrs · 18,302 cycles

CORROSION FOUND ON THE FORWARD MAIN CABIN RIGHT FLOOR SUPPORT BETWEEN FRAMES 12 - 13, +Y373. REPLACED THE FLOOR SUPPORT IAW SRM 51-43-01.

Part: SUPPORT — CORRODED (FRAMES 12-14) · airframe 25,175 hrs · 18,302 cycles

CORROSION FOUND ON MAIN CABIN SILL BETWEEN FRAMES 12 AND 14, +Y963. REPLACED THE SILL IAW RD 53-00-00-3, REPAIR 3.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 24,835 hrs · 18,048 cycles

CLIMBING THROUGH 10,000 FEET, AFT LAVATORY SMOKE WARNING APPEARED FOR 5 SECONDS ON EICAS, NO VISUAL OR ODOR OBSERVED FROM LAVATORY. OPS CHECKED OK FOR SERVICE.

Part: WINDSHIELD — LEAKING (COCKPIT) · airframe 24,282 hrs · 17,606 cycles

PRESSURE LEAK SUSPECT ON CAPTAIN`S SLIDING WINDOW LEADING EDGE. THE AIRCRAFT WAS GROUNDED. REPLACED CAPTAIN`S WINDSHIELD AND CAPTAIN`S SLIDING WINDOW. ACCOMPLISHED A SATISFACTORY LEAK CHECK IAW AMM 56-11-00.

Part: SLIDING WINDOW — LEAKING (COCKPIT) · airframe 24,282 hrs · 17,606 cycles

PRESSURE LEAK SUSPECTED ON THE CAPTAIN`S SLIDING WINDOW LEADING EDGE. THE AIRCRAFT WAS GROUNDED. REPLACED THE CAPTAIN`S WINDSHIELD AND CAPTAIN`S SLIDING WINDOW. ACCOMPLISHED A SATISFACTORY LEAK CHECK IAW AMM 56-11-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 23,663 hrs · 17,101 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT FLASHLIGHT INOPERABLE. MAINTENANCE REPLACED AFT RIGHT FLASHLIGHT BATTERY AND PERFORMED SATISFACTORY OPERATIONAL CHECK PER AMM 25-60-00.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 22,864 hrs · 16,462 cycles

AIRCRAFT WAS NOT GROUNDED. LAV SMOKE APPEARED ON EICAS FOR 20 SECONDS THEN DISAPPEARED CHECKED BOTH LAVS AND ALL NORMAL CONDITIONS. NO FAULT NOTED BY MAINTENANCE.

Part: GIRT BAR — MISSING (PAX DOOR) · airframe 22,539 hrs · 16,214 cycles

AIRCRAFT WAS NOT GROUNDED. FORWARD PAX DOOR HARD TO DISARM. REATTACHED FORWARD PASSENGER GIRT BAR.

Part: O-RING — LEAKING (HYD LINE) · airframe 22,083 hrs · 15,833 cycles

EMERGENCY DECLARED. DURING FLIGHT THE CREW OBSERVED HYDRAULIC 3 QUANTITY LOW. FOUND LEAK AT THE NR 3 HYDRAULIC SYSTEM FLOW LIMITER VALVE AT INLET UNION. REMOVED AND REPLACED THE O-RING IAW AMM 29-12-19. AIRCRAFT WAS GROUNDED.

Part: SKIN — CRACKED (LT WING) · airframe 21,972 hrs · 15,746 cycles

WHILE INVESTIGATING A LEFT WING FUEL LEAK, FOUND A CRACK ON THE LEFT WING LOWER SKIN AT STRINGER 27L AND RIB 20. REPAIRED THE LEFT WING LOWER SKIN IAW EA 271742, AND SRM 57-10-01, REPAIR 55P.

Part: FLIGHT DIR — FAULTED (COCKPIT) · airframe 21,105 hrs · 15,096 cycles

AIRCRAFT WAS NOT GROUNDED. REJECTED TAKEOFF AT 60 KIAS DUE TO HIGH WINDS. RECEIVED MULTIPLE MASTER CAUTIONS DUE TO HIGH WINDS DISRUPTING OUR FLIGHT DETECTOR LATERAL & VERTICAL MODES. SAFELY EXITED THE RUNWAY AND RETURNED TO GATE. MAINTENANCE ACCOMPLISHED RESET PER FIM 22-11-00, NO FAULTS NOTED. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK PER JOB CARD 43T22022001 AND INSPECTION PER 05-50-12.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 21,025 hrs · 15,304 cycles

AIRCRAFT WAS GROUNDED. CO-PILOT WINDSCREEN HAS CRACKS AND DELAMINATION AROUND EDGE, SOME CRACKS IN DELAMINATION AREA. REPLACED CO-PILOT WINDSHIELD PER AMM 56-11-00.

Part: INDICATOR — BENT (PAX DOOR) · airframe 19,912 hrs · 14,124 cycles

FORWARD PASSENGER DOOR AFT VISUAL LOCK INDICATOR IS BENT AND MISSING SPRING. REMOVED AND REPLACED FORWARD PASSENGER DOOR AFT VISUAL LOCK INDICATOR AND ITS SPRING IAW AMM 52-11-22-010-002-A AND AMM 52-11-22-410-002-A. ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 52-11-00/1.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 19,908 hrs · 14,122 cycles

DURING OPS CHECK, FOUND FORWARD LEFT LAVATORY EXIT IDENTIFIER SIGN BROKEN. REPLACED THE SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-00-710-801-A, 33-50-15-000-801-A & 33-50-15-400-801-A.

Part: SIGN — CRACKED (EMERGENCY LIGHTS) · airframe 19,908 hrs · 14,122 cycles

RIGHT OVERWING EXIT SIGN CRACKED. REPLACED THE SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-01-710-801.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 19,908 hrs · 14,122 cycles

R/H OVERWING EXIT DOOR SIGN DOES NOT ILLUMINATE. PERFORMED TROUBLESHOOTING AND SECURED PIN 1 AT CONNECTOR P2326 AND SECURED PIN AT DIODE CR0148 IAW SWPM, AMM, WDM AND OPS CHECKED GOOD.

Part: SIGN — CRACKED (EMERGENCY LIGHT) · airframe 19,908 hrs · 14,122 cycles

MAIN CABIN LOWER CEILING PANEL 228ARC EXIT SIGN LENS COVER CRACKED. REPLACED EXIT SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECKED IAW AMM 33-50-19-400-801 AND 33-50-00-710-801.

Part: CONNECTING ROD — CHAFED (PAX DOOR) · airframe 19,908 hrs · 14,122 cycles

AFT PASSENGER DOOR, DOOR CONTROL TO ARMING LEVER CONNECTING ROD HAS CHAFE DAMAGE. REPLACED THE CONNECTING ROD AND ACCOMPLISHED A SATISFACTORY OPS CHECKED IAW AMM 52-12-40-020-002-A AND 52-12-40-420-005-A.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 19,908 hrs · 14,122 cycles

MAIN CABIN AFT SERVICE DOOR SURROUND PANEL 252HRW EXIT SIGN LENS COVER IS CRACKED. REPLACED THE SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-15.

Part: WINDOW — CRAZED (PAX CABIN) · airframe 19,908 hrs · 14,122 cycles

L1 PASSENGER CABIN WINDOW BETWEEN FRAMES 23 AND 24 AND STRINGER 8 - 11L HAS CRAZING. REPLACED THE WINDOW IAW AMM 56-20-00.

Part: ESCAPE ROPE — FRAYED (RT OVERWING) · airframe 19,908 hrs · 14,122 cycles

RIGHT OVERWING ESCAPE LIFE LINE ROPE ASSEMBLY FRAYING NEAR END. REPLACED ESCAPE ROPE ASSEMBLY.

Part: PANEL — CHAFED (RT WING) · airframe 19,908 hrs · 14,122 cycles

RIGHT WING FIXED LEADING EDGE PANEL OUTER SKIN CHAFED JUST ABOVE NR 2 PYLON BETWEEN RIB 7 AND RIB 9A. REPLACED THE PANEL IAW SRM 51-40-02, 51-40-04 & AMM 20-10-07.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN RT FLOOR SILL BETWEEN FRAME 12 AND FRAME 14, BETWEEN +Y920 AND +Y1244. REPLACED SILL IAW AARD 53-00-00-3, REP 3, SRM 51-40-02, SRM 51-43-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RT SEAT TRACK CROWN AT FRAME 84 AND +Y260. REPAIRED SEAT TRACK IAW SRM 53-00-10, REPAIR 51, FIG 205.

Part: DOUBLER — CORRODED (FRAME 84) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

CORROSION ON FLOOR DOUBLER AT FRAME 84 AND +Y330. REPLACED THE FLOOR DOUBLER IAW SRM 51-40-02 & 51-43-04.

Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

CORROSION ON LEFT SEAT TRACK CROWN AT FRAME 84, -Y260. REPAIRED THE SEAT TRACK IAW SRM 53-00-10 REPAIRS 51 FIG 205 SHT 2.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 19,908 hrs · 14,122 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO DOOR CUTOUT LOWER AFT SEAL REST AT FRAME 27 AND STR 26 RT. REPLACED SEAL REST IAW AARD 53-00-00-3, REPAIR 3, FIGURE 2, SHEET 23.

Part: FLOORBEAM — CRACKED (FRAME 12) · airframe 19,908 hrs · 14,122 cycles

COCKPIT FLOORBEAM ANGLE AT FRAME 12 AND Y 0 CRACKED. REPLACED FLOORBEAM ANGLE IAW SRMS 51-41-01 & 51-40-02.

Part: FLOORBEAM — CRACKED (FRAME 12) · airframe 19,908 hrs · 14,122 cycles

COCKPIT FLOORBEAM ANGEL AT FRAME 12 AND -Y939.8 CRACKED. REPLACED FLOORBEAM ANGLE IAW SRM 51-41-01 & 51-40-02.

Part: SHEAR TIE — CORRODED (FRAME 74) · airframe 19,908 hrs · 14,122 cycles

CORROSION ON AFT CARGO BAY SHEAR TIE FRAME 74, STRINGER 29R. REPLACED THE SHEAR TIE IAW SRM 51-41-05 & 51-43-01.

Part: SHEAR TIE — CORRODED (FRAME 74) · airframe 19,908 hrs · 14,122 cycles

CORROSION ON AFT CARGO BAY SHEAR TIE, FRAME 74 AT STRINGER 29L. REPLACED THE SHEAR TIE IAW SRM 51-41-05 & 51-43-01.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION AND ELONGATED HOLES ON FORWARD CABIN RT AFT FLOOR SILL BETWEEN FRAME 17 AND FRAME 18, BETWEEN +Y1060.5 AND +Y1257. REPLACED FLOOR SILL IAW E190 AARD 53-00-00-3, REPAIR 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

CORROSION ON CABIN RT FLOOR TRACK BETWEEN FRAME 12 AND FRAME 20 AT +Y276. REPLACED FLOOR TRACK IAW SRM 51-41-01,02; 51-43-03,04 AND AARD 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LT AFT FLOOR SUPPORT AT FRAME 19 AND -Y1092. REPLACED FLOOR SUPPORT IAW SRM'S 51-40-02 & 51-43-03.

Part: FLOOR SUPPORT — CORRODED (FRAME 17) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

CORROSION ON FORWARD CABIN RIGHT FLOOR SUPPORT AT FRAME 17, +Y711. REPLACED FLOOR SUPPORT IAW SRM 51-40-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LT FLOOR SUPPORT AT FRAME 84 AND -Y1160. REPLACED FLOOR SUPPORT IAW SRM'S 51-41-02 & 51-41-01.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

ACFT IN BASE MAINTENANCE: CORROSION AND ELONGATED HOLES ON AFT CABIN RT FLOOR STRUCTURE DOUBLER AT FRAME 84 AND BETWEEN +Y1016 AND +Y1193. REPLACED DOUBLER IAW SRM 51-43-04 & 51-41-02.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN CENTER SPLICE AT FRAME 90 AND Y0. REPLACED SPLICE IAW SRM 51-43-03.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

ACFT IN BASE MAINTENANCE: CORROSION ON CABIN LT FLOOR SUPPORT AT FRAME 16 AND -Y1143. REPLACED FLOOR SUPPORT IAW SRM 51-43-01, 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN RT FLOOR SUPPORT BETWEEN FRAME 89 ANF FRAME 90, BETWEEN +Y946 AND +Y997. REPLACED FLOOR SUPPORT IAW AARD 53-00-00-3, REPAIR 3 & SRM 51-43-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LT FLOOR TRACK AT FRAME 17 AND -Y276. REPAIRED FLOOR TRACK IAW SRM 53-10-10, REP 51.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

ACFT IN BASE MAINTENANCE: CORROSION CABIN RT OTBD UPPER GUSSET AT FRAME 90 BETWEEN +Y457 AND +Y698. REPLACED GUSSET IAW SRM'S 51-40-02 & 51-23-04.

Part: UPPER SHEET — CORRODED (FRAME 85-86) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

CORROSION ON AFT CABIN LEFT UPPER SHEET BETWEEN FRAMES 85 AND 86, -Y260. REPLACED THE UPPER SHEET IAW SRM 51-43-03.

Part: FLOORBEAM — CORRODED (FRAME 12) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

CORROSION ON FORWARD CABIN RIGHT BEAM AT FRAME 12 AND +Y381. REPLACED THE FLOORBEAM IAW SRM'S 51-40-02, 51-40-03, AND 51-43-01.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

ACFT IN BASE MAINTENANCE: CORROSION ON RT SHEAR PANEL BETWEEN FRAME 87 AND FRAME 88 BETWEEN +Y304 AND +Y1041. REPLACED SHEAR PANEL IAW SRM 51-40-02, 51-40-03, TABLE 2, 51-42-01, 51-43-03.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

CORROSION ON FORWARD CABIN RIGHT FLOOR SUPPORT BETWEEN FRAMES 17 - 18, +Y330. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, 51-43-03, 51-43-04 AND 51-45-00.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LT SHEAR PANEL BETWEEN FRAME 87 AND FRAME 88, BETWEEN -Y304 AND -Y1041. REPLACED SHEAR PANEL IAW SRM 51-40-02, 51-40-03, TABLE 2, 51-42-01, 53-43-03.

Part: SEAL REST — CORRODED (FRAME 24) · airframe 19,908 hrs · 14,122 cycles

CORROSION ON FORWARD CARGO DOOR CUT OUT LOWER FORWARD CORNER SEAL REST AT FRAME 24, STRINGER 25R. REPLACED THE SEAL REST IAW AARD 53-00-00-3 REPAIR 3.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN CENTER SHEAR PANEL BETWEEN FRAME 87 AND FRAME 88, BETWEEN -Y222 AND +Y222. REPLACED SHEAR PANEL IAW SRM 51-40-02, 51-40-03, TABLE 2, 51-42-01, 51-43-03.

Part: SHEAR TIE — CORRODED (FRAME 88) · corrosion level 2 · airframe 19,908 hrs · 14,122 cycles

CORROSION ON SHEAR TIE AT FRAME 88 BETWEEN STRINGER 27 AND 28R. REPLACED THE SHEAR TIE IAW SRM 51-25-16, 51-41-02, 51-40-02, 51-23-04, 51-23-05, 51-23-06 AND CPM 51-25-00.

Part: LIGHT — LOOSE (CABIN) · airframe 19,618 hrs · 13,828 cycles

AIRCRAFT WAS NOT GNDED. EMER FLOOR PATH MARKINGS IN VICINITY OF SEAT 1D LOOSE. SECURED EMER FLOOR PATH MARKING NEAR SEAT 1D AS REQUIRED.

Part: RECEPTACLE — DEFECTIVE (EXTERNAL POWER) · airframe 19,013 hrs · 13,290 cycles

AIRCRAFT WAS GNDED. FIRE REPORTED BY GND PERSONNEL AT GPU RECEPTACLE. REPLACED EXTERNAL AC POWER RECEPTACLE & EXTERNAL POWER MODULE IAW AMM 24-42-03 & 24-42-01. SEE AALA201601279001 FOR ADDITIONAL INFORMATION.

Part: MODULE — DEFECTIVE (GROUND POWER) · airframe 19,013 hrs · 13,290 cycles

AIRCRAFT WAS GNDED. FIRE REPORTED BY GND PERSONNEL AT GPU RECEPTACLE. REPLACED EXTERNAL AC POWER RECEPTACLE & EXTERNAL POWER MODULE IAW AMM 24-42-03 & 24-42-01. SEE AALA201601289004 FOR ADDITIONAL INFORMATION.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 16,561 hrs · 11,185 cycles

AFT FLIGHT ATTENDANT RT SIDE FLASHLIGHT INOPERATIVE. REPLACED AFT FLIGHT ATTENDANT EMER FLASHLIGHT BATTERY. OPERATIONAL CHECK IS OK.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 16,556 hrs · 11,178 cycles

FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT.

Part: MECHANISM — LACK OF LUBE (COCKPIT SEAT) · airframe 15,841 hrs · 10,498 cycles

CAPTAINS SEAT SLIPS OUT OF SELECTED FORE & AFT POSITION. LUBRICATED LOCKING MECHANISMS. CHECKED OK AFTER OPERATING NUMEROUS TIMES. CAPTAINS SEAT OK FOR SERVICE.

Part: SEAT — STICKS (COCKPIT) · airframe 15,842 hrs · 10,498 cycles

CAPTAIN'S SEAT LOCKS STICK & WILL NOT FULLY LOCK IN PLACE, FWD & AFT. R & R CAPTAIN'S SEAT, CHECKED GOOD.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 15,625 hrs · 10,281 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 15,625 hrs · 10,281 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: SHEAR PIN — LOOSE (RT PYLON) · airframe 15,614 hrs · 10,267 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 15,614 hrs · 10,267 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 (RT PYLON) · airframe 15,614 hrs · 10,267 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 (LT PYLON) · airframe 15,614 hrs · 10,267 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: BATTERY — DISCHARGED (CABIN) · airframe 15,556 hrs · 10,214 cycles

AFT LT EMER EXIT IDENTIFIER WILL NOT ILLUMINATE. R & R THE AFT LT EMER NICAD BATTERY.

Part: SHRADER VALVE — LEAKING (PAX DOOR) · airframe 15,460 hrs · 10,132 cycles

C3 CHECK UPON INSTALLATION OF AFT PAX DOOR LINERS NOTICED DOOR ASSIST BOTTLE WAS BELOW 20000 PSI. REPLACED SHRADER VLV AT AFT PAX DOOR PNEUMATIC ASSEMBLY IAW AMM 20-20-13 & AMM 20-20-12 & SERVICED AFT PAX DOOR PNEUMATIC ASSEMBLY IAW AMM 52-12-51. LEAK CHECKED GOOD.

Part: SPRING — MISSING (L1 DOOR) · airframe 15,460 hrs · 10,132 cycles

C3 CHECK FWD PAX DOOR WILL NOT OPEN L1. REPLACED FWD PAX DOOR AFT VISUAL LOCK INDICATOR SPRING, FWD & AFT LOCK INDICATOR BRACKETS IAW AMM 52-11-22. ADJUSTED FWD PAX DOOR VERTICAL ALIGNMENT & THE EXTERNAL STEPS IAW AMM 52-11-00-820-802-A & AMM 52-11-00-820-805A. PERFORMED FWD PAX DOOR EMER EVACUATION SLIDE MECHANISM CHECK IAW AMM 52-11-40, OPERATIONS CHECKED GOOD.

Part: DOOR — OUT OF ALIGNMENT (CABIN) · airframe 15,460 hrs · 10,132 cycles

C3 CHECK FOUND FWD PAX DOOR EMER EVACUATION SLIDE MECHANISM TO DISARM REQUIRED ADJUSTMENT, INCOMING CONDITION. ADJUSTED FWD PAX DOOR VERTICAL ALIGNMENT & THE EXTERNAL STEPS IAW AMM 52-11-00-820-802-A & AMM 52-11-00-820-805A. OPERATIONS CHECKED GOOD IAW AMM 52-11-40.

Part: BEAM — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 15,460 hrs · 10,132 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON FWD SERVICE DOOR GUSSET PLATE BEAM BETWEEN FRAME 15 TO FRAME 16 & BETWEEN STRINGER 15R TO STRINGER 16R, Z=-310MM. REPLACED FWD SERVICE DOOR GUSSET PLATE BEAM BETWEEN FRAME 15 TO FRAME 16 & BETWEEN STRINGER 15R TO STRINGER 16R, Z=-310MM IAW SRM 51-75-16, 51-12-01, 51-10-03 & 51-41-01.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,460 hrs · 10,132 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SHEAR CLIP AT FRAME 83 BETWEEN STRINGER 27R TO STRINGER 28R, Z-1550, Y300. REPLACED SHEAR CLIP AT FRAME 83 BETWEEN STRINGER 27R TO STRINGER 28R, Z-1550, Y300 IAW SRM 51-75-16, 53-23-04, 51-41-01 & 51-41-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,460 hrs · 10,132 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SHEAR CLIP AT FRAME 82 BETWEEN STRINGER 27R TO STRINGER 28R, Y=+300MM. REPLACED SHEAR CLIP AT FRAME 82 BETWEEN STRINGER 27R TO STRINGER 28R, Y=+300MM IAW SRM 51-75-16, 53-23-04 & 51-41-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,460 hrs · 10,132 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON FWD CARGO DOOR CUT OUT LOWER SILL DOUBLER BETWEEN FRAME 24 TO FRAME 25, Z-1559 & BETWEEN -Y262.5 TO -Y350. REPLACED FWD CARGO DOOR CUT OUT LOWER SILL DOUBLER BETWEEN FRAME 24 TO FRAME 25, Z-1559 & BETWEEN -Y262.5 TO -Y350 E190 SRM 51-10-03, 51-41-02, 51-43-01 & 51-43-02.

Part: DOUBLER — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 15,460 hrs · 10,132 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON BAG DOOR DOUBLER BETWEEN FRAME 25 TO FRAME 27, Z=-1559MM & BETWEEN Y=+262MM TO Y=+337.5MM. REPLACED BAG DOOR DOUBLER BETWEEN FRAME 25 TO FRAME 27, Z=-1559MM & BETWEEN Y=+262MM TO Y=+337.5MM IAW SRM 51-10-03, 51-75-16, 51-41-02 & 51-43-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,460 hrs · 10,132 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON FWD FUSELAGE RT FLOOR TRACK BETWEEN FRAME 13 TO FRAME 14, Z= -490MM, Y=+250MM. REPAIRED FWD FUSELAGE RT FLOOR TRACK BETWEEN FRAME 13 TO FRAME 14, Z= -490MM, Y=+250MM IAW SRM 53-10-10 REPAIR 51, 51-75-16 & 51-41-01.

Part: SEAT TRACK — CORRODED (FRAME 18) · corrosion level 2 · airframe 15,460 hrs · 10,132 cycles

DURING C3 CHECK, CORROSION FOUND ON SEAT TRACK AT FRAME 18. REPLACED SEAT TRACK IAW SRM 53-10-10, REPAIR 51, 51-75-16 & 51-10-03.

Part: SEAT TRACK — CORRODED (FRAME 19) · corrosion level 2 · airframe 15,460 hrs · 10,132 cycles

DURING C3 CHECK, CORROSION WAS FOUND ON SEAT TRACK AT FRAME 19. REPLACED SEAT TRACK IAW SRM 53-10-10, REPAIR 51, 51-75-16 & 51-10-03.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,460 hrs · 10,132 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON BEAM SUPPORT, UPPER SHEET, BETWEEN FRAME 86 TO FRAME 87, Z=-490MM, Y=+300MM. REPLACED BEAM SUPPORT, UPPER SHEET, BETWEEN FRAME 86 TO FRAME 87, Z=-490MM, Y=+300MM IAW SRM 51-41-01, 51-43-01 & 51-75-16.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,460 hrs · 10,132 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON REINFORT STRUC BETWEEN FRAME 84 TO FRAME 85, Z=-490MM & BETWEEN Y=+350MM TO Y=+1200MM. REPLACED REINFORT STRUC BETWEEN FRAME 84 TO FRAME 85, Z=-490MM & BETWEEN Y=+350MM TO Y=+1200MM IAW SRM 51-12-00, 51-12-01, 51-10-03 & 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 87) · corrosion level 2 · airframe 15,460 hrs · 10,132 cycles

DURING C3 CHECK, CORROSION FOUND ON FLOOR SUPPORT AT FRAME 87, -Y700. REPLACED FLOOR SUPPORT IAW SRM 51-75-16, 51-41-01 & 51-10-03.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 14,916 hrs · 9,728 cycles

R2 DOOR ASSIST BOTTLE REQUIRES SERVICE. SERVICED R2 DOOR ASSIST BOTTLE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 14,649 hrs · 9,513 cycles

FLIGHT 2099, PHL - DFW, DURING CRUISE AT FL 390 THE CAPTAIN REPORTED VIA ACARS FUMES & DECLARED AN EMERGENCY. FLIGHT LANDED UNEVENTFULLY & TAXIED TO THE GATE. CAPTAIN ADVISED FUMES OF A BURNING PLASTIC SMELL REPORTED IN COCKPIT & CABIN. R & R THE NR 1 ENG.

Part: LOCK — MISALIGNED (L1 DOOR) · airframe 13,631 hrs · 8,724 cycles

UNABLE TO CLOSE L1 DOOR. MX PERFORMED DOOR L1 LOCKING MECHANISM ADJUSTMENT. OPS CHECKED IS OK.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 12,392 hrs · 7,816 cycles

FLIGHT 2133, BOS-LGA - CAPTAINS WINDSCREEN SHATTERED IN FLIGHT. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO BOS. THE FLIGHT LANDED WITHOUT ANY FURTHER ISSUES. MAINTENANCE REPLACED THE CAPTAINS WINDSHIELD. ALSO REMOVED AND RE-INSTALLED THE CAPTAINS WINDSHIELD WIPER TO FACILITATE WINDSHIELD CHANGE.

Part: ACCUMULATOR — UNDERSERVICED (ZONE 800)

ATL - L2 DOOR EMERGENCY ACCUMULATOR PRESSURE IS LOW. MAINTENANCE SERVICED THE L2 DOOR EMERGENCY ACCUMULATOR.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

ORF - FLIGHT ATTENDANTS FLASHLIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN ALL THREE EMERGENCY FLASHLIGHTS.