N965UW

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 27,449 hrs · 20,220 cycles

AIRCRAFT WAS GROUNDED: FIRST OFFICERS FIXED WINDSHIELD HAS THREE SMALL CRACKS ALONG THE UPPER EDGE, NEAR THE INNER CORNER IN THE INNER PILES. REPLACED WINDSHIELD PER AMM 56-11-00.

Part: FUEL LINE — LEAKING (APU) · airframe 26,682 hrs · 19,550 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AIRCRAFT WITH APU ON HAS EXHAUST SMELL ON TAKEOFF, APU HAS STRONG RAW FUEL SMELL BOTH FA'S COMPLAIN OF STRONG ODOR OF FUEL ON TAKEOFF SMELLS GO AWAY WHEN APU BLEED IS OFF. MAINTENANCE ISOLATED SOURCE TO APU FUEL FEED LINE LEAK. REPLACED APU FUEL FEED LINE IAW AMM 28-22-08. LEAK CHECK, AND REQUIRED FOLLOW-UP PROCEDURES FOR PNEUMATIC AND ECS SYSTEMS ALL SATISFACTORY.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 26,118 hrs · 19,006 cycles

AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO BOS ON ACCOUNT OF AFT DOOR OPEN INDICATION. AN EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED AMM CHECK IAW AMM TASK 52-72-00-810-804A. OPS CHECK OK.

Part: FUSE — FAILED (MLG) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND EMERGENCY PARKING BRAKE HYD FUSES 2EA FAILED (EMER BRK FAULT) DOSEN'T COME INTO VIEW. REMOVED AND REPLACED EMERGENCY PARKING BRAKE FUSES AND PERFORMED OPS CHECK, OPS GOOD IAW AMM 32-44-07. (SEE SDR # AALA201905289035)

Part: FUSE — FAILED (MLG) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND EMERGENCY PARKING BRAKE HYD FUSES 2EA FAILED (EMER BRK FAULT) DOSEN'T COME INTO VIEW. REMOVED AND REPLACED EMERGENCY PARKING BRAKE FUSES AND PERFORMED OPS CHECK, OPS GOOD IAW AMM 32-44-07. (SEE SDR # AALA201905289004)

Part: SMOKE DETECTOR — CRACKED (LAVATORY) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS FWD LAV SMOKE DETETOR IS CRACKED. FWD LAV SMOKE DETECTOR REPLACED IAW AMM TASK 26-14-01-000-801-A & 26-14-01-400-801-A, SEALANT APPLIED IAW SUBTASK 010-003-A OF ABOVE TASK, OPS CHECK GOOD.

Part: RIB — CRACKED (RT WING) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE VISIT: (DC-001) RT WING L/E RIB #17 IS CRACKED (6" CRACK). REMOVED AND REPLACED RT WING L/E RIB #17 IAW DWG #191-03201-423.

Part: RIB — CRACKED (LT WING) · airframe 25,834 hrs · 18,753 cycles

(DC-005) LT WING L/E RIB #17 IS CRACKED, (6" CRACK). REMOVED AND REPLACED LT WINGL/E RIB #17 IAW DWG #191-03201-423.

Part: DAMPENER — CORRODED (PAX DOOR) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS FORWARD PASSENGER DOOR DAMPER CORRODED. REMOVED AND REPLACED FORWARD PASSENGER DOOR DAMPER IAW AMM 52-11-27.

Part: DAMPENER — CORRODED (SERVICE DOOR) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS AFT CABIN SERVICE DOOR DAMPER CORRODED MARKED RJ-074. REMOVED AND REPLACED AFT CABIN SERVICE DOOR DAMPER IAW AMM 52-42-27. ADJUSTMENT CHECK GOOD.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 25,835 hrs · 18,753 cycles

AIRCRAFT IN BASE VISIT: MAIN CABIN FLOOR PANEL #226BRF DELAMINATE. REMOVED & REINSTALLED MAIN CABIN FLOOR PANEL #226BRF IAW AMM 53-01-0 AND 170-46573-405FF.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE VISIT: MAIN CABIN RT LATERAL SEAT TRACK SCALLOP HAS CORROSION BETWEEN FR 28/29, L=1.4" W=0.95" D=0.032" CORRODED. REMOVED AND REPLACED MAIN CABIN RT LATERAL SEAT TRACK FROM FR 23 TO FR 35 IAW DWG NO 170-67030-465 AND SRM'S 51-40-02/-03, 51-41-01 & 51-43-01.

Part: BEAM — CORRODED (FUSELAGE) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT SERVICE DOOR CUT OUT LOWER BEAM. REPLACED BEAM PER SRM 53-23-11AD.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT MAIN CABIN LEFT HAND OUTBOARD PANEL SUPPORT BETWEEN FR89 AND FR 90 AT Y=-890. REPLACED SUPPORT PER SRM 51-75-16.

Part: FLASHLIGHT — LOW (CABIN) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE MAINTEANCE: MAIN CABIN FLASH LIGHT BATTERY WAS LOW AT AFT LEFT HAND FLIGHT ATTENDANT STATION. REPLACED MAIN CABIN FLASH LIGHT PER AMM 25-42-02.

Part: BEAM — CORRODED (FUSELAGE) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE VISIT: AFT CABIN AT AFT SERVICE DOOR LOWER BEAM HAS CORROSION SEVERAL AREAS CORROSION (1) 3.5"X.95"X.030" (2) 2.2" X.9"X.042" (3) 3.4"X1.6"X.050". REMOVED CORROSION FROM AFT CABIN AT AFT SERVICE DOOR LWR BEAM (1) 3.5"X.95"X.030" (2) 2.2"X.9"X.042" (3) 3.4"X1.6"X.050" IS OUT OF LIMITS IAW SRM 53-23-11AD 54, REMOVED & REPLACED BEAM IAW DWG 170-655-40-431.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN RIGHT LATERAL SEAT TRACK SUPPORT SHEAR WEB CRACKED BETWEEN FR 19 AND FR 20. REPLACED SHEAR WEB PER SRM 51-40-08.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE VISIT: AFT MAIN CABIN AT AFT SERVICE DOOR, LOWER FRAME FOUND 3EA. AREA OF CORROSION (JG02), CORROSION L=1.1 X W=.550 X D=.024. REMOVED AND REPLACED SUPPORT-SEAL REST FROM AFT MAIN CABIN AT AFT SERVICE DOOR, LOWER P/N: 170-87556-502 BATCH#0003482846 IAW SRM 51-41-01; DWG#170-86640-833.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE VISIT: AFT MAIN CABIN CORROSION ON LT O/B PANEL SUPPORT BETWEEN FR89 AND FR 90 Y=-890, CORROSION L=8" W=2.5" D=0.026". REMOVED CORROSION L=8" W=2.5" D=.026" FROM LT O/B PANEL SUPPORT IN AFT M/C BIN FR 89-90 Y=-890 FOUND TO BE OUT LIMITS IAW SRM 51-75-16, REMOVED, REPLACED & RESTORED FINISH, REFER TO IND. SIGN OFF ENTRIES FOR WORK PERFORMED (REF DWG 170-65660).

Part: STOP FITTING — WORN (FUSELAGE) · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD PASSENGER DOOR FRAME STOP FITTING NR 1 PAD IS WORN. REPLACED DOOR STOP PAD PER AMM 53-10-21.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,834 hrs · 18,753 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SUPPORT AT FR 84 AND -Y1145. REPLACED FLOOR SUPPORT PER DRAWING 170-66-000-465.

Part: BOTTLE — ACTIVATION ERROR (L2 DOOR ASSIST) · airframe 25,403 hrs · 18,404 cycles

L2 DOOR ASSIST BOTTLE HAD AN UNWANTED ACTIVATION. MAINTENANCE REPLACED DOOR ASSIST BOTTLE IAW AMM 52-12-51.

Part: WINDOW — LEAKING (COCKPIT) · airframe 24,282 hrs · 17,487 cycles

CAPTAIN DIRECT VIEW WINDOW LEAKING. REPLACED THE LEFT DIRECT VIEW WINDOW IAW AMM 56-12-00. OPS CHECKED OK.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 23,400 hrs · 16,816 cycles

RIGHT SIDE EXIT EMERGENCY LIGHT COVER NOT CLEAR. MAINTENANCE REPLACED RIGHT SIDE AFT EXTERIOR EMERGENCY LIGHT LENS PER AMM 33-50-25 AND PERFORMED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 23,112 hrs · 16,561 cycles

EXIT SIGN FOUND BROKEN. REPLACED THE SIGN.

Part: PANEL — UNSECURE (EMERGENCY LIGHT) · airframe 21,890 hrs · 15,619 cycles

EMERGENCY EXIT PANEL OVER RT DOOR DETACHED. SECURED THE PANEL.

Part: FRAME — CORRODED (FRAME 88) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

CORROSION ON AFT CARGO FRAME 88 BETWEEN STRINGER 27-28R. REPAIRED FRAME IAW EA 264560.

Part: LENS — CRACKED (CABIN) · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN DOOR SURROUND PANEL 226 CREW EXIT LIGHT LENS IS CRACKED. REMOVED AND REPLACED MAIN CABIN DOOR SURROUND PANEL 226 CREW EXIT LIGHT LENS AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-50-15 & 33-50-00-710-801.

Part: LIGHT — CRACKED (CABIN) · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN DOOR SURROUND PANEL 251 HLW EXIT LIGHT LENS COVER IS CRACKED. REMOVED AND REPLACED MAIN CAB DOOR SURROUND PANEL 251 HLW EXIT LIGHT AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER 33-50-15 AND 33-50-00-710-801.

Part: LENS — CRACKED (CABIN) · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN DOOR SURROUND PANEL 252 HRW EXIT LIGHT LENS COVER IS CRACKED. REMOVED AND REPLACED MAIN CAB EXIT LIGHT ASSEMBLY PANEL 252 AT MAIN DOOR SURROUND AND PERFORMED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-50-00-710-801.

Part: FLASHLIGHT — DAMAGED (CABIN) · airframe 20,287 hrs · 14,385 cycles

DAMAGED MAIN CABIN FLASHLIGHT ASSEMBLY AT FORWARD LEFT HAND FLIGHT ATTENDANT SEAT. REPLACED THE FLASHLIGHT IAW AMM 33-51-01.

Part: INTERCOSTAL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

CORROSION ON INTERIOR AFT LOWER FUSELAGE INTERCOSTAL BETWEEN FRAMES 86 AND 87, AND BETWEEN STRINGER 27-28R. REPLACED INTERCOSTAL IAW SRM 51-41-01.

Part: ANGLE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

CORROSION ON INTERIOR AFT LOWER FUSELAGE ANGLE BETWEEN FRAMES 86 AND 87, AND BTWEEN STRINGER 27-28R. REPLACED THE ANGLE IAW SRM 51-41-01.

Part: SHEAR TIE — CORRODED (FRAME 88) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

CORROSION ON AFT CARGO SHEAR TIE AT FRAME 88 BETWEEN STRINGERS 27-28R. REPLACED THE SHEAR TIE IAW SRM 51-41-02, SRM 51-41-03, SRM 51-40-02 AND 51-41-01.

Part: SUPPORT — CRACKED (FRAME 45) · airframe 20,287 hrs · 14,385 cycles

CRACK ON MAIN CABIN FLOOR WEBBING SUPPORT BELOW LT CENTER SEAT TRACK, INBOARD SIDE AT FORWARD END OF WING STUB BOX FRAME 45 AND -Y260. REPAIRED WEB SUPPORT IAW EA 264320.

Part: FLOOR SUPPORT — CRACKED (FRAMES 45-46) · airframe 20,287 hrs · 14,385 cycles

CRACK ON MAIN CABIN FLOOR SUPPORT, AT Y215.9 AND BETWEEN FRAMES 45 TO 46. REPAIRED THE FLOOR SUPPORT IAW EA 264321, E190 SRM 51-23-09, NDTM 51-00-00-916-803-A.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-20) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

CORROSION ON FORWARD MAIN CABIN RIGHT FLOOR SUPPORT AT Y1110 BETWEEN FRAMES 17 AND 18. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, 51-41-02 AND 53-00-00-3 REP 3.

Part: BEAM — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

CORROSION AND ELONGATED HOLE ON FORWARD MAIN CABIN BEAM BETWEEN FRAMES 12 AND 13 AT -Y770. REPLACED BEAM IAW SRM 51-41-01, 51-41-02 AND 51-43-03.

Part: ANGLE — CORRODED (FRAMES 86-87) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

CORROSION ON INTERIOR AFT LOWER FUSELAGE FORWARD ANGLE BETWEEN FRAMES 86 AND 87, AND BETWEEN STRINGERS 27 AND 28R. REPLACED THE ANGLE IAW SRM 51-41-01.

Part: SHEAR TIE — CORRODED (FRAME 87) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

CORROSION ON AFT LOWER FUSELAGE SHEAR TIE AT FRAME 87 BETWEEN STRINGERS 27 - 28R. REPLACED THE SHEAR TIE IAW SRM 51-41-01, 51-41-02, 51-41-03 AND 51-40-02.

Part: INTERCOSTAL — CORRODED (FRAMES 86-87) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

CORROSION ON INTERIOR AFT LOWER FUSELAGE INTERCOSTAL BETWEEN FRAMES 86 AND 87, AND STRINGERS 27-28R. REPLACED INTERCOSTAL IAW SRM 51-41-01, 51-41-02, 51-43-03 AND 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN FLOORBEAM AT Y380 BETWEEN FR 12 AND FR13. REPLACED FLOORBEAM PER SRM 51-41-01 AND 51-43-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN LEFT HAND LONGITUDINAL FLOORBEAM AT -Y260 BETWEEN FR 86 AND FR 88. REPLACED FLOORBEAM PER SRM 51-41-01, SRM 51-42-01, SRM 51-43-01, SRM 53-23-10 AND SRM 51-40-02.

Part: PLATE — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

CORROSION ON AFT MAIN CABIN SILL PLATE AT Y350 AND FRAME 84. REPLACED THE SILL PLATE IAW SRM 53-23-10 AND 51-75-16.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN RIGHT HAND LONGITUDINAL BEAM AT Y260 BETWEEN FR 86 AND FR 88. REPLACED LONGITUDINAL BEAM PER SRM 51-41-01, SRM 51-42-01, SRM 51-43-01, SRM 51-40-02 AND SRM 53-23-10.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT FRAME 16 AND -Y1113. REPLACED FLOOR SUPPORT IAW SRM 51-43-03.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN LEFT HAND FLOOR SHEAR PANEL AT -Y914 BETWEEN FR 87 AND FR88. REPLACED SHEAR PANEL PER SRM 51-42-01, SRM 51-43-01, SRM 51-40-02, AARD 53-00-00-3 REPAIR 3, AND SRM 51-75-16.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR RIGHT HAND SHEAR PANEL BETWEEN FR 87 AND FR 88, BETWEEN Y590 AND Y914. REPLACED SHEAR PANEL PER SRM 51-42-01, SRM 51-43-01, AARD 53-00-00-3, SRM 51-42-02 AND SRM 51-75-16

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON COCKPIT FLOOR STRUCTURE GUSSET AT FR 11. REPLACED GUSSET PER SRM 51-41-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON AFT MAIN CABIN FLOOR SUPPORT AT -Y730 AND FR 86. REPLACED FLOOR SUPPORT PER SRM 51-41-01.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR LEFT HAND UPPER SHEET AT -Y260 BETWEEN FR 85 AND FR 86. REPLACED UPPER SHEET PER SRM 51-43-01, AARD 53-00-00-3, SRM 51-42-02 AND SRM 51-75-16.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN UPPER SHEET BETWEEN FR 85 AND FR 86 AT Y270. REPLACED UPPER SHEET PER AARD 53-00-00-3, E190 SRM 51-10-03, 51-12-01, 51-41-01, 51-45-01, 51-23-04, 51-23-05 AND 51-23-06.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON AFT MAIN CABIN FLOOR PANEL SUPPORT AT FR 86 AND Y712. REPLACED FLOOR PANEL SUPPORT PER SRM 51-41-01.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO DOOR CUTOUT LOWER BEAM AT STRINGER 26R BETWEEN FR 77 AND FR 80. REPLACED LOWER BEAM PER SRM 51-40-00 AND AMM 20-10-01.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON AFT MAIN CABIN FLOOR SUPPORT AT Y712 AND FR 85. REPLACED FLOOR SUPPORT PER SRM 51-41-01.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN LEFT HAND FLOOR PANEL SUPPORT AT FR 90 AND Y812. REPLACED PANEL SUPPORT PER SRM 51-42-01, SRM 51-43-01, SRM 51-41-01 AND AARD 53-00-00-3.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR LEFT HAND GUSSET AT FR 90 AND -Y228. REPLACED GUSSET PER SRM 51-75-16, 51-41-02 AND 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR LEFT HAND GUSSET AT FR 90 AND -Y431. REPLACED GUSSET PER SRM 51-41-02, 51-40-02 AND 51-75-16.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR RIGHT HAND GUSSET AT FR 90 AND Y647. REPLACED GUSSET PER SRM 51-75-16, 51-41-02 AND 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN FLOOR SILL AT Y1000 BETWEEN FR12 AND FR14. REPLACED FLOOR SILL PER ARD 53-00-00-3, SRM 51-41-02 AND 51-43-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,287 hrs · 14,385 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND FORWARD MAIN CABIN SEAT TRACK (2 AREAS) AT Y260 BETWEEN FR 12 AND FR 14. REPLACED SEAT TRACK PER AARD 53-00-00-3, 51-41-01, 51-43-01, 51-23-04, 51-23-05, 51-23-06, 51-40-02 AND 51-40-03.

Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 20,198 hrs · 14,313 cycles

AIRCRAFT WAS GROUNDED: 1L DOOR INDICATION WOULD NOT GO GREEN ON MFD. SHOWED UNKNOWN POSITION. REMOVED DEBRIS FROM GIRT BAR AREA AND ACCOMPLISHED A SATISFACTORY OPS CHECK.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 19,785 hrs · 13,929 cycles

ACFT WAS GROUNDED: DURING PUSHBACK, CAPTAINS SIDE FORWARD NR 1 WINDSHIELD CRACKED. REPLACED CAPTAINS SIDE FORWARD NR 1 WINDSHIELD IAW AMM 56-11-00.

Part: COVER — DIRTY (CABIN) · airframe 17,974 hrs · 14,892 cycles

AIRCRAFT WAS NOT GNDED. FIRST CLASS AREA EMER LIGHTING PATHWAY COVERS DIRTY. REPLACED PHOTO LUMINESCENT INDICATOR LIGHTING STRIP LIGHT IN THE FIRST CLASS IAW AMM 33-50-21.

Part: COVER — BROKEN (EXIT SIGN) · airframe 19,024 hrs · 13,257 cycles

AIRCRAFT WAS NOT GNDED. EXIT SIGN COVER IN THE REAR OF THE ACFT IS BROKEN. REPLACED EXIT SIGN COVER.

Part: LENS — BROKEN (CABIN) · airframe 18,366 hrs · 12,660 cycles

MID CABIN EMER EXIT LIGHT OVERHEAD BROKEN. RE-INSTALLED LENS. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: PIN — DEFECTIVE (EMERGENCY LIGHT) · airframe 15,608 hrs · 10,393 cycles

C3 CHECK LT OVERWING EXIT LIGHT INOPERATIVE. R & R PIN NR 1 AT PLUG P2325 WIRE W201-0404-7-20. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON LT FLOOR SILL BETWEEN FRAME 12 TO 16, Z-490MM, -Y1168MM. REPLACED FLOOR SILL IAW SRM 51-12-01, 51-40-03, 51-41-02 & 51-43-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FRAME 84, Z-490MM, Y268.75MM. REPAIRED SEAT TRACK AT FRAME 84, Z-490MM, Y268.75MM IAW SRM 53-00-10 REPAIR 51.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FRAME 17, Z-490MM, RBL11. REPLACED SEAT TRACK IAW SRM 51-41-01, 51-41-02 & 51-43-03.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON RT FLOOR SILL BETWEEN FRAME 12 TO 14, Z-1490MM & BETWEEN Y-939.8MM - Y1244.6MM. REPLACED RT FLOOR SILL IAW SRM 51-40-03, 51-41-02 & 51-43-02.

Part: SEAL REST — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SEAL REST AT FRAME 24, Z1559MM, Y482.6MM. REPLACED SEAL REST AT FRAME 24, Z1559MM, Y482.6MM IAW SRM 51-10-03, 51-40-02 & 51-42-02.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SHEAR PANEL BETWEEN FRAME 87 TO 88, Z-490MM & BETWEEN Y10.75 TO -Y10.75. REPLACED SHEAR PANEL IAW SRM 53-23-10 & 51-42-01.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON MAIN CABIN FLOOR SPLICE AT FRAME 89, Z-495MM, Y273.05MM. REPLACED MAIN CABIN FLOOR SPLICE IAW SRM 53-23-10, 53-40-03 & 51-43-01.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SUPPORT PANEL AT AFT MAIN CABIN FRAME 87, Z-495MM, Y723.9MM. REPLACED SUPPORT PANEL AT AFT MAIN CABIN FRAME 87, Z-495MM, Y723.9 IAW SRM 51-40-03 & 51-41-01.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON PANEL SHEAR AFT MAIN CABIN BETWEEN FRAME 87 TO 88, Z-490MM & BETWEEN Y40634MM TO Y10414MM. REPLACED PANEL SHEAR AT AFT MAIN CABIN BETWEEN FRAME 87 TO 88, Z-490MM & BETWEEN Y40634MM TO Y10414MM IAW SRM 53-23-10, 51-42-01, 51-40-03 & 51-43-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,607 hrs · 10,393 cycles

C3 CHECK GALVANIC CORROSION ON SEAT TRACK BETWEEN FRAME 12 TO 17, Z-490MM, RBL11. REPLACED SEAT TRACK IAW SRM 51-41-01, 51-41-02 & 51-43-03.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON FLOORBEAM UPPER SHEET BETWEEN FRAME 84 TO 86, Z-490, Y-271.78. REPAIRED FLOORBEAM UPPER SHEET IAW SRM 53-23-10, 51-40-03, 51-43-01 & 51-41-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FRAME 12 TO 20, Z-490MM, -Y275MM. REPLACED SEAT TRACK IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FRAME 84, Z-490MM, -Y268.75MM. REPAIRED SEAT TRACK IAW SRM 51-10-03, 53-23-10 & 53-00-10 REPAIR 51.

Part: REINFORCEMENT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON FLOOR REINFORCEMENT STRUCTURE BETWEEN FRAME 84 - 85, Z-495MM, Y1193.8MM. REPLACED FLOOR REINFORCEMENT STRUCTURE IAW SRM 51-10-03 & 51-40-02.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION AFT CARGO DOOR SEAL REST AT FRAME 77, Z=-1618MM, Y=+384MM. REPLACED AFT CARGO DOOR SEAL REST AT FRAME 77, Z=-1618MM, Y=+384MM IAW SRM 51-10-03 & SRM 53-23-11.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SEAL REST AT FRAME 27, Z1559MM, Y482.6MM. REPLACED SEAL REST AT FRAME 27, Z1559MM, Y482.6MM IAW SRM 53-23-11.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SEAL REST AT FRAME 24, Z1559MM, Y482.6MM. REPLACED SEAL REST AT FRAME 24, Z1559MM, Y482.6MM IAW SRM 53-23-11.

Part: SEAL REST — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,607 hrs · 10,393 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON FWD CARGO DOOR SEAL REST BETWEEN FRAME 24 TO 27, Z-1550MM, Y=533.4MM. REPLACED FWD CARGO DOOR SEAL REST IAW SRM 51-10-03, 51-23-11, 51-41-02, 51-40-02, 51-41-01 & AMM 53-21-29.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 15,521 hrs · 10,317 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: WINDSHIELD — CRACKED (COCKPIT) · airframe 15,354 hrs · 10,186 cycles

A 7 VISIT DELAMINATION & CRACKING ALONG TOP INNER LENGTH OF CAPTAIN'S FIXED WINDSHIELD BETWEEN FRAME 08 TO 09 & STRINGER 02R TO 01R. REPLACED CAPTAIN'S FIXED WINDSHIELD IAW AMM TASK 56-11-00-000-801-A & 56-11-00-400-801-A. WINDSHIELD WIPER OPERATIONS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 15,326 hrs · 10,161 cycles

L1 DOOR ASSIST BOTTLE REQUIRES SERVICE. SERVICED L1 DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 15,326 hrs · 10,161 cycles

L2 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED L2 DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 15,326 hrs · 10,161 cycles

R1 DOOR ASSIST BOTTLE REQUIRES SERVICING. MAINTENANCE SERVICED R1 DOOR ASSIST BOTTLE.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 13,809 hrs · 9,085 cycles

FOUND R1 DOOR HANDLE OUT OF POSITION, HANDLE WAS HALFWAY TOWARD OPEN POSITION. MAINTENANCE REMOVED R1 DOORSLIDE. FOUND GIRT BAR JAMMED BETWEEN DOOR FITTING AND FLOOR PLATE. REINSTALLED SLIDE.

Part: SENSOR — MALFUNCTIONED (RT TAT)

FLIGHT 894, CLT-ATL - THE CREW RECEIVED "TAT 2" FAIL MESSAGE ON APPROACH INTO ATL WITH ELECTRICAL BURNING SMELL. MAINTENANCE IN ATL REPORTED THE CONNECTOR IS BURNT. THE CONNECTOR WAS CAPPED AND STOWED AND THE CIRCUIT BREAKER WAS PULLED. THE AIRCRAFT WAS RELEASED ON MEL. OCTOBER 01 - PHL MAINTENANCE REPLACED THE RIGHT TAT SENSOR PER TASK 34-15-02 AND THE RIGHT UPPER SMART PROBE (AOA) PER TASK 34-13-01. OPERATIONAL CHECK IS GOOD, REMOVED MEL 34-15-03A, CN 2826B01.

Part: SENSOR — MALFUNCTIONED (RT TAT)

FLIGHT 894, CLT-ATL - THE CREW RECEIVED "TAT 2" FAIL MESSAGE ON APPROACH INTO ATL WITH ELECTRICAL BURNING SMELL. MAINTENANCE IN ATL REPORTED THE CONNECTOR IS BURNT. THE CONNECTOR WAS CAPPED AND STOWED AND THE CIRCUIT BREAKER WAS PULLED. THE AIRCRAFT WAS RELEASED ON MEL. OCTOBER 01 - PHL MAINTENANCE REPLACED THE RIGHT TAT SENSOR PER TASK 34-15-02 AND THE RIGHT UPPER SMART PROBE (AOA) PER TASK 34-13-01. OPERATIONAL CHECK IS GOOD, REMOVED MEL 34-15-03A, CN 2826B01.

Part: HANDLE — TORN (ZONE 800)

ORD - FLIGHT DECK DOOR STRAP HANDLE IS TORN. MAINTENANCE REPLACED THE FLIGHT DECK STRAP HANDLE.

Part: SEAT TRACK — DIRTY (COCKPIT)

PHL - THE CAPTAIN'S SEAT WILL NOT LOCK IN PLACE AFTER SLIDING IT LATERALLY. THE SEAT WILL NOT MOVE FORWARD DUE TO THIS PROBLEM. MAINTENANCE CLEANED AND LUBED THE SEAT TRACKS AND RELEASE LEVER.

Part: ENGINE — VIBRATION (NR 2)

FLIGHT 1615, CLT - MCI, PASSING 16,000FT THE NR 2 ENGINE TRIGGERED A HP VIB WARNING LIGHT (REGISTERING 5.0 VIBRATION). AFTER CONSULTING THE CHECKLIST THE CREW RESTORED POWER TO THE ENGINE, SIMILAR RESULTS OCCURRED. THE CREW DECIDED TO RETURN TO CLT. THE ENGINE WAS NOT SHUTDOWN BUT WAS IDLED. THE FLIGHT LANDED UNEVENTFULLY. MX ACTION PENDING