N184US

Part: BOTTLE — LEAKING (ZONE 800) · airframe 76,388 hrs · 29,762 cycles

AIRCRAFT WAS GROUNDED: R1 DOOR WILL NOT FULLY OPEN TO GUST LOCK POSITION. MAINTENANCE FOUND THE R1 DOOR R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW, REPLACED THE R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-01. A SATISFACTORY OPERATIONAL CHECK OF THE R1 DOOR WAS ACCOMPLISHED WITH NO ISSUES NOTED.

Part: LIFE LINE — MISINSTALLED (ZONE 800) · airframe 76,380 hrs · 29,759 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 SLIDE ARM INTERMITTENT. MAINTENANCE FOUND THE MOORING LINE INCORRECTLY INSTALLED ON THE GIRT BAR, REINSTALLED MOORING LINE ON GIRT BAR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-62-44.

Part: SPEAKER — NO TEST (ZONE 200) · airframe 76,380 hrs · 29,759 cycles

AIRCRAFT IN BASE MAINTENANCE: STATION 2 HAS NO ALARM NOISE, THE VISIONAL ALERT WORKS BUT NO AURAL WARNING. MAINTENANCE REPLACED THE LOUDSPEAKER PER AMM 23-73-51 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY EVACUATION SIGNALING SYSTEM PER AMM 23-73-00 WITH NO ISSUES NOTED.

Part: SPEAKER — NO TEST (ZONE 200) · airframe 76,380 hrs · 29,759 cycles

AIRCRAFT IN BASE MAINTENANCE: STATION 3 HAS NO ALARM NOISE, THE VISIONAL ALERT WORKS BUT NO AURAL WARNING. MAINTENANCE REPLACED THE LOUDSPEAKER PER AMM 23-73-51 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY EVACUATION SIGNALING SYSTEM PER AMM 23-73-00 WITH NO ISSUES NOTED.

Part: DIAPHRAGM — LEAKING (ZONE 800) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER DIAPHRAGM PER AMM 52-10-00.

Part: BOSS — LOW PRESSURE (ZONE 800) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWAQRD RIGHT PASSENGER / CREW DOOR 841 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL OVERHANG LOWER SURFACE BETWEEN RIB 7A AND RIB 9. REPAIRED SKIN PANEL PER EA 368796.

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL OVERHANG LOWER SURFACE AT LEVEL RIB 15. REPAIRED SKIN PANEL PER EA 368796.

Part: FITTING — CRACKED (ZONE 100) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK CORNER FITTING OPEN HOLE L6 AT FR 36 AND +Y1292. REPLACED CORNER FITTING PER EA 367961

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL UPPER SURFACE AT RIB 5 AND THE REAR SPAR. REPAIRED SKIN PANEL PER EA 368796.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKD AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 600) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #3 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 600) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #2 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 600) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #1 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.

Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE AT FR 36 AND -Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 367961

Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE AT FR 36 AND +Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 367961

Part: FITTING — CRACKED (ZONE 200) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT AND #7 DOOR STOP FITTING. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE AT FR 16 RIGHT AND #5 DOORSTOP FITTING. REPAIRED FRAME PER EA 367781.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE AT FR 16 LEFT AND #7 DOORSTOP FITTING. REPAIRED FRAME PER EA 367767.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 500) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON #3 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING RIGH HAND CONTINUITY FITTING BETWEEN FR 2 AND FR 3 AT Y0 RIGHT. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING BETWEEN FR 2 AND FR 3 AT Y0 LEFT. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SEAT RAIL BETWEEN FR 64 AND FR 66 AT +Y1292. REPLACED SEAT RAIL PER SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM INBOARD UPPER SECTION CONNECTING SPLICE AT FR 66 AND +Y1292. REPLACED SECTION CONNECTING SPLICE PER SRM 51-72-11.

Part: DOOR SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPLACED SILL PER SRM 51-72-11.

Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23L. REPLACED CORNER SHAPE FITTING PER SRM 51-72-11.

Part: PLATE — LOOSE (ZONE 800) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 843 GRIP PLATE IS LOOSE. MAINTENANCE TIGHTENED GRIP PLATE PER AMM 52-22-22.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION TO PASSENGER CABIN FLOOR SUPPORT BETWEEN FR 12 AND FR 24 AT -Y254. REPLACED FLOOR SUPPORT PER SRM 51-72-11.

Part: FITTING — CRACKED (ZONE 100) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FITTING AT FR 2 AND -Y 330. REPLACED FITTING PER SRM 51-42-11.

Part: SHACKLE — WORN (ZONE 400) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON AFT ATTACH FITTING SHACKLE WORN AT PYLON RIB 10. REPLACED SHACKLE PER AMM 54-51-17.

Part: ATTACH FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON FORWARD ATTACH FITTING (SHACKLE) RIGHT HAND POSITION AT RIB 4. REPLACED PYLON ATTACH FITTING PER AMM 54-51-17-400-001-A

Part: FLOORBEAM — ELONGATED (ZONE 200) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES LOCATED ON FR24 INBOARD SPLICE FLOOR BEAM -Y254 FWD GALLEY AREA (0.222 IN). MAINTENANCE REPLACED SPLICE LOCAED ON FR24 INBOARD FLOOR BEAM -Y254 FWD GALLEY AREA IAW A321 51-42-11-801, SRM 51-72-11-911-001 AND DWG D53110920.

Part: SHACKLE — WORN (ZONE 400) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT PYLON FORWARD INBOARD ATTACH FITTING SHACKLE WORN AT PYLON RIB 4. REPLACED SHACKLE PER AMM 54-51-17.

Part: FLOORBEAM — WORN (ZONE 100) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN FLOOR BEAM OUTBOARD SPLICE HAS WORN / ELONGATED HOLES AT FR 24 AND -Y254. REPLACED SPLICE PER SRM 51-72-11.

Part: BOTTLE — NO TEST (ZONE 800) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: DONT PASS TEST DAMPING FUNCTION ON DOOR DAMPER AND EMERGENCY OPERATION CYLINDER INPASSENGER CREW DOOR 831 AT FWD GALLEY AREA. MAINTENANCE REMOVED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IN PASSENGER CREW DOOR 841 P/N: FE240-004,S/N:3583 AT FWD GALLEY AREA .I.A.W AMM 52-11-14-000-0001-B STEP 3.B,D AND STEP 4.A.

Part: BOTTLE — NO TEST (ZONE 800) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: DONT PASS TEST DAMPING FUNCTION ON DOOR DAMPER AND EMERGENCY OPERATION CYLINDER INPASSENGER CREW DOOR 841 AT FWD GALLEY AREA. MAINTENANCE REMOVED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IN PASSENGER CREW DOOR 841 P/N: FE240-004,S/N:3583 AT FWD GALLEY AREA .I.A.W AMM 52-11-14-000-0001-B STEP 3.B,D AND STEP 4.A.

Part: ATTACH FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON FORWARD ATTACH FITTING (SHACKLE) OUTBOARD ON PYLON INBOARD SIDE. REPLACED PYLON ATTACH FITTING PER AMM 54-51-17-000-001-A AND AMM 54-51-17-400-001-A.

Part: ATTACH FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON FORWARD ATTACH FITTING (SHACKLE) OUTBOARD ON PYLON OUTBOARD SIDE. REPLACED PYLON ATTACH FITTING PER AMM 54-51-17-000-001-A AND AMM 54-51-17-400-001-A.

Part: ATTACH FITTING — CORRODED (ZONE 400) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON FORWARD ATTACH FITTING (SHACKLE) INBOARD ON PYLON OUTBOARD SIDE. REPLACED PYLON ATTACH FITTING PER AMM 54-51-17-000-001-A AND AMM 54-51-17-400-001-A

Part: BEAM — CORRODED (DOOR SILL) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON R2 DOOR SILL BEAM EXISTING REPAIR AT FR 68 AND S23R. REPAIRED THE DOOR SILL BEAM IAW SRM 53-41-14-300-001.

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SECTION-CONNECTING AT FR 68 AND S23L. REPLACED SECTION-CONNECTING PER SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FR 66 AND FR 70 AT+Y765. REPLACED FLOOR SUPPORT PER SRM 51-42-11.

Part: SCREW — DETERIORATED (ZONE 800) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: DETERIORATED, DOOR STOP SCREWS AT POSITION 6 AFT EMERGENCY EXIT DOOR 833 IN PASSENGER CABIN. MAINTENANCE REPLACED DOOR STOP SCREWS AT POSITION 6 AFT EMERGENCY EXIT DOOR 833 IN PASSENGER CABIN I.A.W AMM 52-22-31-000-001-A AND AMM 52-22-31-400-001-A.

Part: SCREW — DETERIORATED (ZONE 800) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: DETERIORATED, DOOR STOP SCREWS AT POSITION 3 AFT EMERGENCY EXIT DOOR 833 IN PASSENGER CABIN. MAINTENANCE REPLACED DOOR STOP SCREWS AT POSITION 3 AFT EMERGENCY EXIT DOOR 833 IN PASSENGER CABIN I.A.W AMM 52-22-31-000-001-A AND AMM 52-22-31-400-001-A.

Part: SCREW — DETERIORATED (ZONE 800) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: DETERIORATED, DOOR STOP SCREW AT POSITION 2 AFT MERGENCY EXIT DOOR 833 IN PASSENGER CABIN. MSINTENANCE REPLACED DOOR STOP SCREW AT POSITION 2 AFT EMERGENCY EXIT DOOR 833 IN PASSENGER CABIN I.A.W AMM 52-22-31-000-001-A AND AMM 52-22-31-400-001-A.

Part: SCREW — DETERIORATED (ZONE 800) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: DETERIORATED, DOOR STOP SCREWS AT POSITION 5 AFT EMERGENCY EXIT DOOR 833 IN PASSENGER CABIN. MAINTENANCE REPLACED DOOR STOP SCREWS AT POSITION 5 AFT EMERGENCY EXIT DOOR 833 IN PASSENGER CABIN I.A.W AMM 52-22-31-000-001-A AND AMM 52-22-31-400-001-A.

Part: FRAME — CRACKED (ZONE 100) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE, CRACKED FRAME SECTION CONNECTION AT FR 66 AND S23L. REPLACED FRAME SECTION CONNECTION PER SRM 51-72-11.

Part: SCREW — DETERIORATED (ZONE 800) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: DETERIORATED, DOOR STOP SCREWS AT POSITION 4 AFT EMERGENCY EXIT DOOR 833 IN PASSENGER CABIN. MAINTENANCE REPLACED DOOR STOP SCREWS AT POSITION 4 AFT EMERGENCY EXIT DOOR 833 IN PASSENGER CABIN I.A.W AMM 52-22-31-000-001-A AND AMM 52-22-31-400-001-A.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FR 68 AND FR 69 AT+Y1162.5. REPLACED FLOOR SUPPORT PER SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FR 68 AND FR 70 AT +Y160.5. REPLACED FLOOR SUPPORT PER SRM 51-72-11.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING 1 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING 1 LH IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 3 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING NO 3 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 5 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING NO 5 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FR 68 AND FR 70 AT -Y160.5. REPLACED FLOOR SUPPORT PER SRM 51-72-11.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 2 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING 2 LH IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE ARM — EXCESS PLAY (ZONE 300 ELEV) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 4 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING 1 LH IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 6 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING NO 6 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 6 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING NO 6 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 1 ON RH HORIZONTAL STABILIZER. MSINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING NO 1 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 3 ON RH HORIZONTAL STABILIZER MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING NO 3 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 2 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING NO 2 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 5 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING NO 5 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ON ELEVATOR HINGE ARM END FITTING NO 4 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING NO 4 ON RH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 500) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON #1 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 500) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON #5 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 500) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON #4 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 600) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #4 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.

Part: SUPPORT FRAME — EXCESS PLAY (ZONE 500) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON #2 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.

Part: HINGE — EXCESS PLAY (ZONE 600) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #5 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.

Part: FORK — NONE (ZONE 100) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FITTING PER EA 367833, THE RIGHT-HAND LATERAL FORK END FITTING BETWEEN FR 23 AND FR 24 AT -Y1293 NEEDS TO BE REPLACED PER THE INSTRUCTIONS OUTLINED IN EA 367833. FORK END FITTING REPLACED PER EA 367833.

Part: FORK — NONE (ZONE 100) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FITTING PER EA 367833, THE LEFT-HAND LATERAL FORK END FITTING BETWEEN FR 23 AND FR 24 AT +Y1293 NEEDS TO BE REPLACED PER THE INSTRUCTIONS OUTLINED IN EA 367833. LATERAL FORK END FITTING REPLACED PER EA 367833.

Part: FITTING — WORN (ZONE 100) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FITTING WORN BETWEEN FR 23 AND FR 24 AT +Y1293. REPLACED LATERAL FITTING PER EA 367833.

Part: FITTING — NONE (ZONE 100) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FITTING PER EA 367833, THE RIGHT-HAND LATERAL FITTING BETWEEN FR 23 AND FR 24 AT -Y1293 NEEDS TO BE REPLACED PER THE INSTRUCTIONS OUTLINED IN EA 367833. LATERAL FITTING REPLACED PER EA 367833.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 76,112 hrs · 29,653 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE AT 0 PSI. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14.

Part: LIFE VEST — MISSING (ZONE 200) · airframe 75,790 hrs · 29,517 cycles

AIRCRAFT WAS NOT GROUNDED: MAINTENANCE FORWARD GALLEY FIRE COMPARTMENT BAG STORAGE CABINET SEAT LIFE VEST MISSING. INSTALLED LIFE VEST AS REQUIRED.

Part: SLIDE — DEFECTIVE (ZONE 800) · airframe 75,615 hrs · 29,448 cycles

AIRCRAFT WAS GROUNDED: 1R DOOR SLIDE ARMING LEVER DIFFICULT TO ARM, LEVER GETS PUSHBACK FROM RUBBER STOP. MAINTENANCE FOUND THE R1 DOOR SLIDE WAS CAUSING THE ISSUE AND REPLACED IT PER TASK CARD 26L00025010. A SATISFACTORY OPERATIONAL CHECK OF THE DOOR ARMING SYSTEM WAS ACCOMPLKISHED WITH NO ISSUES NOTED.

Part: CIRCUIT BOARD — FAULTED (ZONE 200) · airframe 73,287 hrs · 28,402 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INBOUND INTO CLT DUE TO THE FLIGHT CREW REPORTING THAT WHEN SELECTING THE LANDING GEAR DOWN HAD DOWN 3 GREEN BOTH LANDING GEAR INDICATORS AND ECAM BUT HAD UNLOCK ON LANDING GEAR INDICATORS. THE FLIGHT CREW PUT GEAR UP ON GO AROUND AND HAD LEFT MAIN UP, NOSE AND RIGHT MAIN DOWN WITH 3 UNLOCK LIGHTS. ECAM PAGE SHOWED ALL UP. CYCLE GEAR DOWN AND GOT DOWN 3 GREEN BOTH INDICATORS WITH NO UNLOCK LIGHTS. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE ACCOMPLISHED TROUBLE SHOOTING INSTRUCTIONS PER TASK CARD 26C21032002 WITH NO DISCREPANCIES NOTED. AS A PRECAUTION, MAINTENANCE REPLACED LIGHTING TEST AND INTERFACE PANEL BOARD 9LP PER 33-14-33. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: SENSOR — FAULTED (ZONE 700) · airframe 73,245 hrs · 28,383 cycles

AIRCRAFT WAS GROUNDED: THE FLIGHT CREW REPORTED THAT WHILE PUTTING THE LANDING GEAR DOWN FOR LANDING WE RECEIVED THREE GREEN INDICATION WITH A RED UP LOCK INDICATION ON THE RIGHT MAIN. THE FLIGHT CREW WENT AROUND AND UPON PUTTING THE GEAR DOWN AGAIN IT CLEARED. **ORIGINAL REPORT WAS AALA202408213257** MAINTENANCE FOUND FAULT MESSAGES FOR THE RIGHT-WING FLAP ATTACHMENT FAILURE DETECTION SENSOR 40CV. MAINTENANCE REPLACED THE RIGHT-WING INTERCONNECTION STRUT PER AMM 27-51-44 ALONG WITH THE RIGHT-WING FLAP ATTACHMENT FAILURE DETECTION SENSORS 38CV (AALA202408233136) AND 40CV (AALA202408238417) PER AMM 27-51-15. MAINTENANCE ALSO REPLACED THE #2 LANDING GEAR CONTROL INTERFACE UNIT (LGCIU) PER AMM 32-31-71 (AALA202408234319). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: STRUT — FAULTED (ZONE 700) · airframe 73,245 hrs · 28,383 cycles

AIRCRAFT WAS GROUNDED: THE FLIGHT CREW REPORTED THAT WHILE PUTTING THE LANDING GEAR DOWN FOR LANDING WE RECEIVED THREE GREEN INDICATION WITH A RED UP LOCK INDICATION ON THE RIGHT MAIN. THE FLIGHT CREW WENT AROUND AND UPON PUTTING THE GEAR DOWN AGAIN IT CLEARED. **SUPPLEMENTAL REPORT FOR AALA202408213257: MAINTENANCE FOUND FAULT MESSAGES FOR THE RIGHT-WING FLAP ATTACHMENT FAILURE DETECTION SENSOR 40CV. MAINTENANCE REPLACED THE RIGHT-WING INTERCONNECTION STRUT PER AMM 27-51-44 ALONG WITH THE RIGHT-WING FLAP ATTACHMENT FAILURE DETECTION SENSORS 38CV (AALA202408233136) AND 40CV (AALA202408238417) PER AMM 27-51-15. MAINTENANCE ALSO REPLACED THE #2 LANDING GEAR CONTROL INTERFACE UNIT (LGCIU) PER AMM 32-31-71 (AALA202408234319). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED. ** (CLOSED)

Part: SENSOR — FAULTED (ZONE 700) · airframe 73,245 hrs · 28,383 cycles

AIRCRAFT WAS GROUNDED: THE FLIGHT CREW REPORTED THAT WHILE PUTTING THE LANDING GEAR DOWN FOR LANDING WE RECEIVED THREE GREEN INDICATION WITH A RED UP LOCK INDICATION ON THE RIGHT MAIN. THE FLIGHT CREW WENT AROUND AND UPON PUTTING THE GEAR DOWN AGAIN IT CLEARED. **ORIGINAL REPORT WAS AALA202408213257** MAINTENANCE FOUND FAULT MESSAGES FOR THE RIGHT-WING FLAP ATTACHMENT FAILURE DETECTION SENSOR 40CV. MAINTENANCE REPLACED THE RIGHT-WING INTERCONNECTION STRUT PER AMM 27-51-44 ALONG WITH THE RIGHT-WING FLAP ATTACHMENT FAILURE DETECTION SENSORS 38CV (AALA202408233136) AND 40CV (AALA202408238417) PER AMM 27-51-15. MAINTENANCE ALSO REPLACED THE #2 LANDING GEAR CONTROL INTERFACE UNIT (LGCIU) PER AMM 32-31-71 (AALA202408234319). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: LANDING GEAR — FAULTED (ZONE 700) · airframe 73,245 hrs · 28,383 cycles

AIRCRAFT WAS GROUNDED: THE FLIGHT CREW REPORTED THAT WHILE PUTTING THE LANDING GEAR DOWN FOR LANDING WE RECEIVED THREE GREEN INDICATION WITH A RED UP LOCK INDICATION ON THE RIGHT MAIN. THE FLIGHT CREW WENT AROUND AND UPON PUTTING THE GEAR DOWN AGAIN IT CLEARED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED ** (OPEN)

Part: LGCIU — FAULTED (ZONE 700) · airframe 73,245 hrs · 28,383 cycles

AIRCRAFT WAS GROUNDED: THE FLIGHT CREW REPORTED THAT WHILE PUTTING THE LANDING GEAR DOWN FOR LANDING WE RECEIVED THREE GREEN INDICATION WITH A RED UP LOCK INDICATION ON THE RIGHT MAIN. THE FLIGHT CREW WENT AROUND AND UPON PUTTING THE GEAR DOWN AGAIN IT CLEARED. **ORIGINAL REPORT WAS AALA202408213257** MAINTENANCE FOUND FAULT MESSAGES FOR THE RIGHT-WING FLAP ATTACHMENT FAILURE DETECTION SENSOR 40CV. MAINTENANCE REPLACED THE RIGHT-WING INTERCONNECTION STRUT PER AMM 27-51-44 ALONG WITH THE RIGHT-WING FLAP ATTACHMENT FAILURE DETECTION SENSORS 38CV (AALA202408233136) AND 40CV (AALA202408238417) PER AMM 27-51-15. MAINTENANCE ALSO REPLACED THE #2 LANDING GEAR CONTROL INTERFACE UNIT (LGCIU) PER AMM 32-31-71 (AALA202408234319). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: COMPUTER — FATIGUED (ZONE 100) · airframe 73,140 hrs · 28,343 cycles

AIRCRAFT WAS GROUNDED: ON FINAL CONFIGURATION FOR LANDING, FLAPS LOCKED AT NEARLY FLAPS THREE POSITIONS, WITH ACCOMPANYING FLIGHT CONTROL FLAPS ECAM. FLIGHT CREW PERFORMED ECAM ACTIONS AND COMPLETED LANDING. FLAPS DID NOT MOVE AFTER INITIAL MOVE TO POSITION 3. MAINTENANCE REPLACED SLAT FLAP CONTROL COMPUTERS #1 (AALA202408088503) AND #2 (AALA202408086541) PER AMM 27-51-34. A SATISFACTORY OPERATIONAL CHECKL WAS ACCOMPLISHED.

Part: COMPUTER — FAULT MESSAGE (ZONE 100) · airframe 73,140 hrs · 28,343 cycles

AIRCRAFT WAS GROUNDED: ON FINAL CONFIGURATION FOR LANDING, FLAPS LOCKED AT NEARLY FLAPS THREE POSITIONS, WITH ACCOMPANYING FLIGHT CONTROL FLAPS ECAM. FLIGHT CREW PERFORMED ECAM ACTIONS AND COMPLETED LANDING. FLAPS DID NOT MOVE AFTER INITIAL MOVE TO POSITION 3. MAINTENANCE REPLACED SLAT FLAP CONTROL COMPUTERS #1 (AALA202408088503) AND #2 (AALA202408086541) PER AMM 27-51-34. A SATISFACTORY OPERATIONAL CHECKL WAS ACCOMPLISHED.

Part: WATER HEATER — ODOR (LAVATORY) · airframe 72,618 hrs · 28,124 cycles

AIRCRAFT WAS NOT GROUNDED: BURNING PLASTIC SMELL FROM UNDER SINK IN FORWARD LAVATORY. TURNED OFF WATER HEATER BELOW SINK AND SMELL DISSIPATED. PERFORMED JOB CARD 26L00021001. FOUND SOURCE OF ODOR COMING FROM WATER HEATER IN FORWARD LAVATORY. REMOVED AND REPLACED WATER HEATER PER AMM 38-12-16.

Part: SKIN PANEL — CRACKED (ZONE 200 - FUSE) · airframe 72,591 hrs · 28,112 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK FOUND AT THE NOSE FORWARD FUSELAGE LEFT HAND LATERAL FORWARD SKIN PANEL EXTERNAL SURFACE RADIATING FROM FASTENER HOLE BETWEEN FR 13 AND FR 14, BETWEEN AT Z+780 AND Z+950. REPAIRED SKIN PANEL PER EA 355027.

Part: FLOORBEAM — CORRODED (FRM 16) · airframe 72,591 hrs · 28,112 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM AT FR 16 AND +Y765 AT THE LAVATORY MOUNT. REPLACED FLOOR BEAM PER SRM 51-42-11.

Part: SKIN — CRACKED (ZONE 200) · airframe 72,591 hrs · 28,112 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK FOUND AT THE NOSE FORWARD FUSELAGE LEFT HAND LATERAL FORWARD SKIN PANEL EXTERNAL SURFACE RADIATING FROM FASTENER HOLE BETWEEN FR 13 AND FR 14, S10L AND BETWEEN AT Z+780 AND Z+950. REPAIRED SKIN PANEL PER EA 355027. SEE AALA202406117553

Part: SEAT TRACK — CORRODED (FRM 16) · airframe 72,591 hrs · 28,112 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR TRACK AT FR 16 AT FR +Y765 AT THE LAVATORY MOUNT. REPLACED TRACK PER SRM 51-42-11.

Part: FITTING — CRACKED (RT MLG DOOR) · airframe 72,591 hrs · 28,112 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT MAIN LANDING GEAR AFT GEAR DOOR ACTUATOR FITTING AFT LUG CRACKED BETWEEN FR 42 AND FR 43 AT KEEL BEEM RIB W10. REPLACED ACTUATOR FITTING PER EA 354901.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 71,817 hrs · 27,755 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT FLASH LIGHT WILL TEST. REMOVE AND REPLACE FLASHLIGHT AS REQUIRED.

Part: SAFETY VALVE — WARNING MESSAGE (ZONE 100 - FUSE) · airframe 71,500 hrs · 27,609 cycles

AIRCRAFT WAS GROUNDED: AFTER GEAR HANDLE UP AFTER TAKEOFF, FIVE SECOND ECAM: LANDING GEAR NOT UPLOCKED. FLIGHT CREW REPORTED THAT THERE WAS MAYBE ALSO LANDING GEAR DOORS NOT CLOSED MESSAGE. MESSAGE WENT AWAY AND THE FLIGHT CREW COULD NOT RECALL IT BUT IT IS ON CFDS ECAM PAGE. FLIGHT CREW WAS NOT SURE WHICH GEAR INDICATED. MAINTENANCE ACCOMPLISHED TSM 32-31-00-810-808-A AND REPLACED THE FOLLOWING ITEMS: PRIORITY VALVE 1064GM (AALA202401232462), LANDING GEAR SYSTEM ISOLATION SAFETY VALVE 49GA (AALA202401239135) AND RELAY 62GA (AALA202401238893). A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PRIORITY VALVE — WARNING MESSAGE (ZONE 100 - FUSE) · airframe 71,500 hrs · 27,609 cycles

AIRCRAFT WAS GROUNDED: AFTER GEAR HANDLE UP AFTER TAKEOFF, FIVE SECOND ECAM: LANDING GEAR NOT UPLOCKED. FLIGHT CREW REPORTED THAT THERE WAS MAYBE ALSO LANDING GEAR DOORS NOT CLOSED MESSAGE. MESSAGE WENT AWAY AND THE FLIGHT CREW COULD NOT RECALL IT BUT IT IS ON CFDS ECAM PAGE. FLIGHT CREW WAS NOT SURE WHICH GEAR INDICATED. MAINTENANCE ACCOMPLISHED TSM 32-31-00-810-808-A AND REPLACED THE FOLLOWING ITEMS: PRIORITY VALVE 1064GM (AALA202401232462), LANDING GEAR SYSTEM ISOLATION SAFETY VALVE 49GA (AALA202401239135) AND RELAY 62GA (AALA202401238893). A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: RELAY — WARNING MESSAGE (ZONE 100 - FUSE) · airframe 71,500 hrs · 27,609 cycles

AIRCRAFT WAS GROUNDED: AFTER GEAR HANDLE UP AFTER TAKEOFF, FIVE SECOND ECAM: LANDING GEAR NOT UPLOCKED. FLIGHT CREW REPORTED THAT THERE WAS MAYBE ALSO LANDING GEAR DOORS NOT CLOSED MESSAGE. MESSAGE WENT AWAY AND THE FLIGHT CREW COULD NOT RECALL IT BUT IT IS ON CFDS ECAM PAGE. FLIGHT CREW WAS NOT SURE WHICH GEAR INDICATED. MAINTENANCE ACCOMPLISHED TSM 32-31-00-810-808-A AND REPLACED THE FOLLOWING ITEMS: PRIORITY VALVE 1064GM (AALA202401232462), LANDING GEAR SYSTEM ISOLATION SAFETY VALVE 49GA (AALA202401239135) AND RELAY 62GA (AALA202401238893). A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: GENERATOR — FAILED (APU) · airframe 71,380 hrs · 27,559 cycles

AIRCRAFT WAS TAKEN OUT OF SERVICE. APU GENERATOR FAILED EN ROUTE TO CLT IN CRUISE. EXECUTEAPU AUTO SHUTDOWN, EXECUTED AN EMERGENCY LANDING IN CHS. SERVICED APU.**SEE CERS ID 240101840 WHICH I SENT YOU TODAY 1/10/24**

Part: GENERATOR — FAILED (APU) · airframe 71,380 hrs · 27,559 cycles

AIRCRAFT WAS TAKEN OUT OF SERVICE. APU GENERATOR FAILED EN ROUTE TO CLT IN CRUISE, APU AUTO SHUTDOWN. EXECUTED AN EMERGENCY LANDING IN CHS. SERVICED APU. **SUPPLEMENTAL REPORT SUBMITTED TO REMOVE THE UNNECESSARY COMMENT/NOTE**

Part: RESTRICTOR VALVE — DEFECTIVE (MLG) · airframe 71,331 hrs · 27,539 cycles

AIRCRAFT WAS GROUNDED: LANDING GEAR NOT UP LOCKED ECAM MESSAGE ON TAKEOFF FOR NOSE GEAR, CORRECTED ITSELF AFTER APPROXIMATELY 15 SECONDS. MAINTENANCE FOUND NOSE LANDING GEAR DOOR EXTREMELY SLOW TO OPEN AND SOMETIMES WOULD NOT OPEN WITHOUT ASSISTANCE. MAINTENANCE REPLACED RESTRICTOR VALVE 2535GM PER AMM 32-31-57 AND ACCOMPLISHED A SATISFACTORYOPERATIONAL CHECK.

Part: DOOR — STICKING (ZONE 700 - GEARS) · airframe 71,330 hrs · 27,538 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER TAKEOFF PASSING 1,500' AGL, NOSE LANDING GEAR DOOR NOT CLOSED ECAM WITH INDICATION VERIFIED. DOOR SHOWED CLOSE AFTER 10 SEC AND ECAM EXTINGUISHED. MAINTENANCE LUBRICATED THE NOSE LANDING GEAR DOORS PER AMM 12-22-32 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: FILTER — DIRTY (ZONE 900 - LAV/G) · airframe 71,154 hrs · 27,460 cycles

AIRCRAFT WAS NOT GROUNDED: TOD - ECAM LAV FIRE/SMOKE LASTED APPROXIMATLEY 5 SECONDS THEN WENT OUT. FLIGHT ATTENDANTS CONFIRMED - NO SMOKE OR FIRE IN FORWARD LAVATORY. MAINTENANCE WAS UNABLE TO DUPLICATE MALFUNCTION, CLEANED FORWARD LAVATORY A SMOKE DETECTOR FILTER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 26-17-00.

Part: PLATE — LOOSE (ZONE 800 - DOORS) · airframe 70,677 hrs · 27,237 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT RIGHT HAND AFT EMERGENCY EXIT SLIDE ARM HANDLE GRIP PLATE IS LOOSE. SECURED RIGHT HAND AFT EMERGENCY EXIT SLIDE ARM HANDLE GRIP PLATE PER AMM 52-22-22.

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 69,490 hrs · 26,713 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS SLIDE ARM LEVER IS LOOSE DOOR 3R. MAINTENANCE SECURED ARMING LEVER AND AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,124 hrs · 26,521 cycles

AIRCRAFT WAS NOT GROUNDED: 4L DOOR IS CLOSED BUT INDICATING OPEN. **SUPPLEMENTAL REPORT FOR AALA202305122834: MAINTENANCE ACCOMPLISHED TSM 52-13-00 AND FOUND NO DEFECTS WITH THE DOOR INDICATION SYSTEM AND THE INDICATIONS WERE NORMAL. NO DEFECTIVE PARTS WERE INDENTIFIED. ** (CLOSED)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,124 hrs · 26,521 cycles

AIRCRAFT WAS NOT GROUNDED: 4L DOOR IS CLOSED BUT INDICATING OPEN. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: CONTROL UNIT — FAULT MESSAGE (ZONE 100 - FUSE) · airframe 69,001 hrs · 26,471 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING DURING TAXI IN LEFT TURN LOST ANTI SKID AND NOSE WHEEL STEERING, FELT LIKE NOSE WHEEL WENT FULL LEFT AND SKID ON WET TAXIWAY, LOUD VIBRATION CYCLED ANTISKID OFF AND ON. BRAKES AND STEERING RETURNED. POST FLIGHT REPORT SHOWED A FAULT MESSAGE FOR THE BRAKING AND STEERING CONTROL UNIT AND MAINTENANCE REPLACED IT PER AMM 32-42-34. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPISHED.

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 68,702 hrs · 26,325 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3R ARMING LEVER LOOSE. 3R DOOR ARMING LEVER SECURED PER AMM 52-20-00.

Part: HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 68,309 hrs · 26,142 cycles

AIRCRAFT WAS NOT GROUNDED: SLIDE ARM HANDLE ON DOOR 3R LOOSE. MAINTENANCE TIGHTENED HANDLE PER AMM 52-22-22.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 68,207 hrs · 26,099 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY D MESSAGE AND AMBER LIGHTS IN CABIN ILLUMINATED DURING CRUISE. MAINTENANCE ACCOMPLISHED A SATISFACTORY OPERATIONAL TEST OF THE LAVATORY SMOKE DETECTOR PER TASK CARD 26C20026003 WITH NO ISSUES NOTED.

Part: LEVER — LOOSE (R3 DOOR) · airframe 67,873 hrs · 25,943 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 3R DOOR ARM DISARM LEVER LOOSE. MAINTENANCE TIGHTENED LEVER PER AMM 52-22-22.

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 67,711 hrs · 25,876 cycles

AIRCRAFT WAS NOT GROUNDED: 3R DOOR ARMING LEVER LOOSE. MAINTENANCE SECURED ARMING LEVER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-62-00.

Part: ACTUATOR — LEAKING (ZONE 800 - DOORS) · airframe 67,328 hrs · 25,715 cycles

AIRCRAFT WAS GROUNDED: CABIN INTERCOMMUNICATION DATA SYSTEM WARNING LIGHT ON FORWARD FLIGHT ATTENDANT PANEL DURING PRE FLIGHT. REMOVED AND REPLACED R2 DOOR DAMPER AND EMERGENCY OPERATIONAL CYLINDER PER AMM 52-22-14.

Part: NONE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 67,286 hrs · 25,697 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD FLIGHT ATTENDANT PANEL CIDS CAUTION APPEARED AFTER LANDING. MAINTENANCE SERVICED THE RIGHT HAND MID DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: ADIRU — NONE (ZONE 100 - FUSE) · airframe 67,277 hrs · 25,694 cycles

AIRCRAFT WAS GROUNDED: CAT 3 DUAL DISPLAYED IN INOPERATIVE SYSTEM. ATTEMPTED COMPUTER RESET PER QRH WITH NO OTHER FAILURE. WHEN CHANGED FROM AUTOPILOT 2 TO AUTOPILOT 1, AIRCRAFT PITCHED DOWN AND INITIATED UNCOMMANDED DESCENT. STOPPED COMPUTER RESET AS UNSUCCESSFUL. MAINTENANCE REPLACED #1 AIR DATA AND INERTIAL REFERENCE UNIT (ADIRU) AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 34-12-34.

Part: LEVER — LOOSE (ZONE 800 - DOORS) · airframe 67,232 hrs · 25,671 cycles

AIRCRAFT WAS NOT GROUNDED: 3L DOOR ARMING LEVER LOOSE. MAINTENANCE SECURED 3L DOOR ARMING LEVER PER AMM 52-20-00.

Part: CYLINDER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 67,191 hrs · 25,651 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION LIGHT ON FLIGHT ATTENDANT PANEL. CIDS GROUND SCAN FAULTS DOOR BOTTLE MID RIGHT (R2 DOOR) MAINTENANCE SERVICED R2 DOOR DAMPER CYLINDER PER AMM 52-10-00.

Part: NONE — NONE · airframe 66,954 hrs · 25,544 cycles

AIRCRAFT WAS NOT GROUNDED: 4L DOOR SHOWS OPEN WITH DOOR HANDLE CLOSED POSITION. 4L DOOR SHOWS OPEN WITH DOOR HANDLE CLOSED POSITION. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)

Part: DOOR — FAULTY (ZONE 800 - DOORS) · airframe 66,954 hrs · 25,544 cycles

AIRCRAFT WAS NOT GROUNDED: 4L DOOR SHOWS OPEN WITH DOOR HANDLE CLOSED POSITION. 4L DOOR SHOWS OPEN WITH DOOR HANDLE CLOSED POSITION. **SUPPLEMENTAL REPORT FOR AALA202208083139: ACCOMPLISHED OPERATIONS CHECKS DETERMINED TO BE NO FAULT FOUND.** (CLOSED)

Part: BATTERY PACK — NONE (ZONE 200 - FUSE) · airframe 66,887 hrs · 25,519 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNITS FAILED OPERATIONAL CHECK PER TASK CARD 26L000025012. REPLACED BATTERY PACKS AT EMERGENCY POWER SUPPLY UNITS L1 (AALA202207280118), L2 (AALA202207289617) AND L3 (AALA202207287832) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY PACK — NONE (ZONE 200 - FUSE) · airframe 66,887 hrs · 25,519 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNITS FAILED OPERATIONAL CHECK PER TASK CARD 26L000025012. REPLACED BATTERY PACKS AT EMERGENCY POWER SUPPLY UNITS L1 (AALA202207280118), L2 (AALA202207289617) AND L3 (AALA202207287832) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY PACK — NONE (ZONE 200 - FUSE) · airframe 66,887 hrs · 25,519 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNITS FAILED OPERATIONAL CHECK PER TASK CARD 26L000025012. REPLACED BATTERY PACKS AT EMERGENCY POWER SUPPLY UNITS L1 (AALA202207280118), L2 (AALA202207289617) AND L3 (AALA202207287832) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 66,809 hrs · 25,483 cycles

AIRCRAFT WAS GROUNDED: 2R EMERGENCY EXIT DOOR ASSIST BOTTLE PRESSURE LOW FAULT WARNING ON FORWARD FLIGHT ATTENDANT PANEL. SERVICED DOOR ASSIST BOTTLE PER AMM 52-22-00 AND NO FAULT WARNINGS WERE NOTED ON THE FORWARD FLIGHT ATTENDANT PANEL AFTER SERVICING..

Part: NONE — LOW (ZONE 800 - DOORS) · airframe 66,628 hrs · 25,408 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION LIGHT ON FLIGHT ATTENDANTS PANEL. SERVICED RIGHT SIDE MID DOOR ASSIST BOTTLE PER AMM 52-22-00.

Part: NONE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 66,452 hrs · 25,333 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS FAULT ON PANEL. SERVICED RIGHT HAND MID DOOR ASSIST BOTTLE AND OPERATIONAL CHECKED GOOD PER AMM 25-62-46

Part: NONE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 66,177 hrs · 25,215 cycles

AIRCRAFT WAS GROUNDED: AFTER BOTH ENGINE STARTED FORWARD FLIGHT ATTENDANT CIDS PANEL CAUTION LIGHT RETURN TO GATE. SERVICED R2 DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: DAMPER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 66,046 hrs · 25,162 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT PANEL CAUTION LIGHT ON. SERVICED R2 DOOR DAMPER PER AMM 52-10-00 AND CAUTION LIGHT EXTINGUISHED.

Part: HANDLE — LOOSE (ZONE 800 - DOORS) · airframe 65,871 hrs · 25,097 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR 3R ARMING LEVER HANDLE LOOSE. RE-SECURED HANDLE. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK PER AMM 52-22-21.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 65,296 hrs · 24,857 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION DISPLAYED ON FLIGHT ATTENDANT PANEL -MID R DOOR PRESSURE LOW. SERVICED DOOR ASSIST BOTTLE PER TASK CARD 26L80052003.

Part: FLASHLIGHT — NO TEST (ZONE 200 - FUSE) · airframe 65,296 hrs · 24,857 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORT'S FLASHLIGHT AT 4L WILL NOT TEST. RESET FLASHLIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — STICKING (ZONE 800 - DOORS) · airframe 65,039 hrs · 24,737 cycles

AIRCRAFT WAS NOT GROUNDED: 4R SLIDE DIFFICULT TO ARM. CLEANED AND LUBED ACCOMPLISHED AMM 52-10-00 FUCTIONAL TEST GOOD.

Part: ACTUATOR — FAULT MESSAGE (ZONE 800 - DOORS) · airframe 65,035 hrs · 24,733 cycles

AIRCRAFT WAS NOT GROUNDED: CAUTION LIGHT ON CABIN INTERCOMMUNICATION DATA SYSTEM PANEL. SERVICED R2 DOOR ACTUATOR EMERGENCY EXIT.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 64,444 hrs · 24,502 cycles

AIRCRAFT WAS NOT GROUNDED: DURING EMERGENCY POWER SUPPLY UNIT BATTERY SYSTEM TEST, EMERGENCY POWER SUPPLY UNIT BATTERY MID RIGHT MESSAGE. REMOVED AND REPLACED MID RIGHT EMERGENCY POWER SUPPLY UNIT BATTERY.

Part: NONE — NONE · airframe 64,245 hrs · 24,422 cycles

AIRCRAFT WAS GROUNDED: AFTER PUSH BACK, L4 DOOR INDICATES OPEN WITH DOOR CLOSED. RETURNED TO GATE. ACCOMPLISHED TEST OF THE DOOR WARNING SYSTEM PER AMM 57-71-00-710-001-A. L4 DOOR CHECKED GOOD.

Part: FLOOR PANEL — DELAMINATED · airframe 63,778 hrs · 24,237 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 231FF DELAMINATED. REPLACED FLOOR PANEL PER AMM 321 53-00-00.

Part: HANDLE — LACK OF LUBE (L4 DOOR) · airframe 63,129 hrs · 23,961 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR L4 SHOWS OPEN WITH DOOR CLOSED WITH WHITE SLIDE ARMED LIGHT NOT ILLUMINATED. CLEANED AND LUBRICATE L4 DOOR HANDLE.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 62,408 hrs · 23,663 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 2L EMERGENCY EXIT DOOR DAMPER BOTTLE PRESSURE LOW. CHARGED DOOR 2L EMERGENCY EXIT DOOR DAMPER BOTTLE, AS REQUIRED, PER AMM 52-22-00-614-002-A.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 62,408 hrs · 23,663 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 2R EMERGENCY EXIT DOOR DAMPER BOTTLE PRESSURE LOW. CHARGED DOOR 2R EMERGENCY EXIT DOOR DAMPER BOTTLE, AS REQUIRED, PER AMM 52-22-00-614-002-A.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 62,397 hrs · 23,660 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 3R EMERGENCY EXIT DOOR DAMPER BOTTLE PRESSURE LOW. CHARGED DOOR 3R EMERGENCY EXIT DOOR DAMPER BOTTLE, AS REQUIRED.

Part: BOTTLE — LOW PRESSURE (L3 DOOR ASSIST) · airframe 62,397 hrs · 23,660 cycles

AIRCRAFT WAS NOT GROUNDED. DOOR 3L EMERGENCY EXIT DOOR DAMPER BOTTLE PRESSURE LOW. CHARGED DOOR 3L EMERGENCY EXIT DOOR DAMPER BOTTLE, AS REQUIRED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,204 hrs · 23,589 cycles

AIRCRAFT WAS NOT GROUNDED. MULTIPLE EMERGENCY LIGHTS ON SEATS LEFT SIDE OF AIRCRAFT INOPERATIVE AND EXIT SIGN AT L3 DOOR INOPERATIVE. FOUND EMERGENCY POWER SUPPLY UNIT 11WL BAD. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (AALA202010099010) 11WL AND BATTERY, PER AMM 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,204 hrs · 23,589 cycles

AIRCRAFT WAS NOT GROUNDED. MULTIPLE EMERGENCY LIGHTS ON SEATS LEFT SIDE OF AIRCRAFT INOPERATIVE AND EXIT SIGN AT L3 DOOR INOPERATIVE. FOUND EMERGENCY POWER SUPPLY UNIT 11WL BAD. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 11WL AND BATTERY (AALA202010099019), PER AMM 33-51-38.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 62,120 hrs · 23,555 cycles

AIRCRAFT NOT GROUNDED ESCAPE PATH LIGHT LENS COVER MISSING, SEAT 8C. INSTALLED NEW LENS COVER, PER AMM TASK 33-51-400-001. OPERATIONAL CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 62,016 hrs · 23,517 cycles

AIRCRAFT WAS GROUNDED: CIDS LIGHT ON FA FWD PANEL ILLUMINATED. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614 CIDS LIGHT EXTINGUISHED.

Part: DAMPER — LEAKING (R2 DOOR) · airframe 62,016 hrs · 23,517 cycles

AIRCRAFT WAS NOT GROUNDED: DUE TO NUMEROUS SERVICING'S, R2 DOOR DOOR DAMPER AND EMERGENCY OPERATION CYLINDER REQUIRED REPLACEMENT. REPLACED R2 DOOR DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 62,001 hrs · 23,511 cycles

AIRCRAFT NOT GROUNDED - CAUTION LIGHT IN FLIGHT, FORWARD FLIGHT ATTENDANT PANEL; RESET ONCE ON THE GROUND. PERFORMED CIDS (CABIN INTERCOMMUNICATION DATA SYSTEM) TEST, R2 DOOR ASSIST BOTTLE LOW PRESSURE. SERVICED DOOR ASSIST BOTTLE PER AMM 52-22-00, OKAY FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 61,991 hrs · 23,508 cycles

AIRCRAFT WAS NOT GROUNDED: CIDS CAUTION LIGHT ON FLIGHT ATTENDANT PANEL. FOUND R2 DOOR ASSIST BOTTLE PRESSURE OUT OF GREEN BAND RANGE. SERVICED R2 DOOR ASSIST BOTTLE PER AMM 52-22-00.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 61,961 hrs · 23,495 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR ASSIST BOTTLE LOW PRESSURE. SERVICED R2 DOOR ASSIST IAW 52-10-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 61,931 hrs · 23,484 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT COVER AT 8C IS MISSING. REPLACED LENS PER GPM 02.01.2.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 61,839 hrs · 23,452 cycles

AIRCRAFT WAS NOT GROUNDED: COVER PLATE (LENS) OFF SIGN NEAR SEAT 1C. REPLACED LENS. OK FOR CONTINUED SERVICE PER GPM 02.01.2.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 61,694 hrs · 23,397 cycles

AIRCRAFT NOT GROUNDED - R2 FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 25-65-00.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED · airframe 60,951 hrs · 23,083 cycles

AIRCRAFT WAS GROUNDED: ON CLIMBOUT A/THR DISCONNECTED. REENGAGED AUTO THRUST THROUGH A/THR PUSHBUTTON ON FCU. A/THR DISCONNECTED AGAIN. REPEATED REENGAGEMENT. OPERATED NORMAL THERE AFTER. PERFORMED TEST OF ENG AUTO THRUST SYSTEM IAW AMM 22-30-00-710-003-A. AUTO THROTTLE SYSTEM OP TEST GOOD. NO FURTHER FAULTS NOTED.

Part: PITOT TUBE — OBSTRUCTED (CAPTAIN'S) · airframe 60,267 hrs · 22,822 cycles

AIRCRAFT WAS NOT GROUNDED: AT APPROXIMATLEY 875 FEET DURING APPROACH, THE CAPTAIN LOST AIR DATA AND HANDED THE AIRCRAFT OVER TO THE FIRST OFFICER. THE AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE DISCOVERED EVIDENCE OF A BIRD STRIKE AND FEATHERS IN THE CAPTAINS PITOT TUBE. MAINTENANCE REMOVED FEATHERS AND INSPECTED PITOT SYSTEM WITH NO OTHER DEFECTS BEING NOTED.

Part: COMPUTER — FAULTY (ZONE 100) · airframe 60,217 hrs · 22,803 cycles

AIRCRAFT WAS GROUNDED: FLIGHT RETURNED TO CLT ON ACCOUNT OF FLIGHT CONTROL SPOILER FAULT. EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED TSM 27-60-00-810-820-A. REMOVED & REPLACED SPOILER ELEVATOR COMPUTER 3 IAW AMM 27-94-34-400-001A. OPS CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,217 hrs · 22,803 cycles

AIRCRAFT IN BASE VISIT: CRACK INDICATION ON FRAME 16 LH SIDE AT OPEN FASTENER HOLE 8, CRACK DIRECTION IS AT 3 OCLOCK, DEPTH=0.072INCH. AT FWD GALLEY AREA (1EA). PERFORMED REPAIR ON FRAME 16LH ON FASTENER HOLE #8 AT LEVEL DOOR STOP #7 IAW EA #298380.

Part: WARNING LIGHT — BROKEN (EMERGENCY EXIT) · airframe 60,170 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: BROKEN EMERGENCY EXIT DOOR RED WARNING LIGHT CABIN PRESSURE AT E/E DOOR 833 IN PASSENGER CABIN. REPLACED WARNING LIGHT PER AMM 52-73-22-400-003-A.

Part: HINGE — WORN (NLG DOOR) · airframe 60,170 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR RIGHT HAND AFT DOOR AFT HINGE HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE PER CMM 52-82-32.

Part: HINGE — WORN (NLG DOOR) · airframe 60,170 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR RIGHT HAND AFT DOOR FORWARD HINGE HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE PER CMM 52-82-32.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 60,170 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR LEFT AFT DOOR AFT HINGE HAS EXCESSIVE PLAY AND WEAR. REPLACED THE HINGE PER CMM 52-82-32.

Part: HINGE — WORN (NLG DOOR) · airframe 60,170 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: NOSE LANDING GEAR LEFT HAND AFT DOOR FORWARD HINGE HAS EXCESSIVE PLAY AND WEAR. REPLACED HINGE PER CMM 52-82-32.

Part: FLOOR PANEL — ERODED (CABIN) · airframe 60,170 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD WET AREA FLOOR PANEL 221EF ERODED. REPLACED FLOOR PANEL PER AMM 53-12-12-400-001-A.

Part: HINGE ARM — WORN (RT ELEVATOR) · airframe 60,170 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR #6 HINGE ARM BEARING WORN / OUT OF LIMIT ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED #6 HINGE ARM PER AMM 55-16-42-400-001-A.

Part: STOP FITTING — WORN (LT WING SPOILER) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE VISIT: WEAR ON SPOILER 2 (ACTUATOR STOP BOLT) ON LH WING (1 EA). PERFORMED PERMANENT REPAIR LOC ON ACTUATOR STOP BOLT ON SPOILER 2 OF LH WING IAW A321 SRM 57-70-00-300-003 STEP 2A.

Part: STOP FITTING — WORN (LT WING SPOILER) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE VISIT: WEAR ON SPOILER 3 (ACTUATOR STOP BOLT) ON LH WING (1 EA). PERFORMED PERMANENT REPAIR LOC ON ACTUATOR STOP BOLT ON SPOILER 3 OF LH IAW A321 SRM 57-70-00-300-003 STEP 2A.

Part: ATTACH BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #2 UPPER AFT ATTACH BOLT. REPLACED BOLT PER AMM 27-84-63-400-001-A.

Part: ATTACH BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #2 MID FORWARD ATTACH BOLT BETWEEN RIB 3 AND RIB 4. REPLACED ATTACH BOLT PER AMM 27-84-63-400-002-A.

Part: ATTACH BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #2 UPPER FORWARD ATTACH BOLT BETWEEN RIB 3 AND RIB 4. REPLACED ATTACHED BOLT PER AMM 27-84-63-400-002-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 60,170 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOOR PANEL 261PF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: SEAT TRACK — CORRODED (FRAME 20) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK AT FR 20 AND -Y765. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.

Part: HINGE — WORN (VERTICAL STAB) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #2 HAS EXCESSIVE PLAY / WEAR AT RIB 4 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE — WORN (VERTICAL STAB) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE NR 1 HAS EXCESSIVE PLAY / WEAR AT RIB 1 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: SEAT TRACK — CORRODED (FRAME 16) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK AT FR 16 AND +Y765. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAME 16) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK AT FR 16 AND +Y1292. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: HINGE — WORN (VERTICAL STAB) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE. RUDDER HINGE NR 7 HAD EXCESSIVE PLAY AND WEAR AT RIB 11 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE — WORN (RUDDER) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #5 HAS EXCESSIVE PLAY / WEAR AT RIB 7 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOORBEAM AT FR 66 AND +Y1292. REPLACED FLOORBEAM PER SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FRAME 69) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHEAR PLATE AT FR 69 AND S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FRAME 69) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE VISIT: CORROSION SHEAR PLATE STR 23 R AT AFT GALLEY AREA, (CORRODED AREA L= 4.034"W=2.512",0.012"=D). REPLACED SHEAR PLATE LOCATED ON STR23R AT AFT GALLEY AREA IAW A321 SRM 51-572-911-001 AND INSTALLED IAW A321 SRM 51-42-11-801 AND DRAWING D53474180.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT RAIL AT FR 66 AND +Y765. REPLACED SEAT RAIL PER SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FRAME 69) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SHEAR PLATE AT FR 69 AND S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (FRAME 47) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATION ON FLOOR PANEL 251AG. REPLACED FLOOR PANEL 251AG PER SRM 53-02-00-300-011.

Part: INTERCOSTAL — CRACKED (FRAMES 15-16) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND FORWARD DOOR CUT OUT INTERCOSTAL FITTING BETWEEN FR 15 AND FR 16 AT THE NR 7 DOOR STOP AREA. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND FORWARD DOOR CUT OUT INTERCOSTAL FITTING BETWEEN FR 15 AND FR 16 AT DOOR STOP #7. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 251CG DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOOR PANEL 261PF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD WET AREA FLOOR PANEL 222FF DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 261BG AT AFT GALLEY AREA. MAINTENANCE REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION 1.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON AFT WET AREA FLOOR PANEL 262FF. REPLACED FLOOR PANEL PER AMM 53-42-12-400-002-A

Part: FLOOR PANEL — DELAMINATED (FWD WET AREA) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD WET AREA FLOOR PANLE 221EF DELAMINATED FRAMES 16-20, Y254-Y1292. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATION ON FLOOR PANEL 261AG AT AFT GALLEY AREA. MAINTENANCE REPLACED FLOOR PANEL PER SRM 53-02-00-300-011 AND IRM 9701 REVISION 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT WET AREA FLOOR PANEL 262BG DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A.

Part: FLOOR PANEL — CORRODED (FRAME 66) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR PANEL 261LG. REPLACED FLOOR PANEL 261LG PER AMM 53-42-12-400-002-A.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER BETWEEN RIB 7 AND 8 AT 4.5" FROM THE TRAILING EDGE. REPAIRED SKIN PER SRM 55-21-11-300-004.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER BETWEEN RIB 8 AND 9 AT 5.125" FROM THE TRAILING EDGE. REPAIRED SKIN PER SRM 55-21-11-300-004.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR UPPER SUFRACE SKIN HAS INDICATION OF TRAPPED WATER 33 INCHES OUTBOARD OF RIB 5 AND 3.5" INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR UPPER SURFACE SKIN PER SRM 55-21-11-300-004.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE VISIT: CORROSION UPPER SURFACE TOP SKIN AT LEVEL RIB 20 FRONT SPAR ON RH WING, (CORROSION L=1.730Ï¿½ W=0.913Ï¿½ D=0.018Ï¿½). PERFORMED TIME LIMITED REPAIR LOCATED UPPER SURFACE TOP SKIN AT LEVEL RIB 20 FRONT SPAR ON R/H WING IAW EA 298746.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE VISIT: CORROSION UPPER SURFACE TOP SKIN AT LEVEL RIB 19 REAR SPAR ON LH WING. PERFORMED TIME LIMITED REPAIR LOC ON UPPER SURFACE TOP SKIN AT LEVEL RIB 19 REAR SPAR OF LH WING IAW EA 298651.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE VISIT: CORROSION REAR SPAR TRAILING EDGE BTW RIB 7 TO RIB 8 ON RH WING, (CORROSION L= 4.060Ï¿½ W=1.959Ï¿½ D=0.041Ï¿½). PERFORMED TIME LIMITED REPAIR REAR SPAR TRAILING EDGE BTW RIB 7 AND RIB 8 ON RH WING (2EA) IAW EA 298746.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 60,171 hrs · 22,785 cycles

AIRCRAFT IN BASE VISIT: CORROSION REAR SPAR TRAILING EDGE LOC BTW RIB 7 TO RIB 8 OF LH WING. PERFORMED TIME LIMITED REPAIR LOC. ON REAR SPAR TRAILING EDGE RIB 7 AND RIB 9 OF LH WING IAW EA 298651.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 59,656 hrs · 22,597 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR ASSIST BOTTLE PRESSURE LOW AT DOOR 1L. MAINTENANCE SERVICED DOOR ASSIST TO PROPER PRESSURE PER AMM 52-22-00.

Part: LIGHT — INOPERATIVE (ROW 8C) · airframe 58,709 hrs · 22,242 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 8C EMERGENCY SEAT MOUNTED LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT SEAT MOUNTED ASSEMBLY PER AMM 33-51-18 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 58,709 hrs · 22,242 cycles

AIRCRAFT WAS GROUNDED: AFT CARGO FLOOR PANEL 151PF IS SPONGY. REPLACED FLOOR PANEL PER AMM 25-28-00.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 58,709 hrs · 22,242 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR PRESSURE WAS LOW. MAINTENANCE CHARGED DAMPER TO PROPER PRESSURE PER AMM 52-10-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 58,508 hrs · 22,154 cycles

L1 DOOR ASSIST BOTTLE PRESSURE WAS LOW. MAINTENANCE SERVICED THE BOTTLE IAW AMM 52-10-00-614-001A.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 58,508 hrs · 22,154 cycles

MAINTENANCE REPORTED THE L1 DOOR EMERGENCY ASSIST BOTTLE HAD LOW PRESSURE. SERVICED THE DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001A. LEAK CHECKED OKAY.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 57,982 hrs · 21,934 cycles

L1 DOOR ASSIST BOTTLE HAD LOW PRESSURE. SERVICED THE L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,791 hrs · 21,863 cycles

EXIT LIGHT ABOVE THE L3 DOOR WAS INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED OK IAW AMM 33-20-00.

Part: LENS — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,503 hrs · 21,738 cycles

SEAT 25D EXIT LIGHT INOPERATIVE. INSTALLED A REPLACEMENT LENS ON THE EXIT LIGHT. OPS NORMAL.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 57,491 hrs · 21,732 cycles

L1 DOOR DAMPER CYLINDER PRESSURE WAS LOW. SERVICED THE CYLINDER IAW AMM 52-10-00. LEAK CHECKED GOOD, OK FOR SERVICE.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 57,096 hrs · 21,581 cycles

SEAT 8C EMERGENCY LIGHT LENS WAS MISSING. MAINTENANCE REPLACED THE LENS AMM 33-50-00, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: COVER — DETACHED (ASSIST HANDLE) · airframe 56,504 hrs · 21,347 cycles

HANDLE COVER AT THE R1 DOOR CAME OFF. MAINTENANCE REPLACED R1 DOOR ASSIST HANDLE AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SPRING — BROKEN (GIRT BAR) · airframe 56,389 hrs · 21,306 cycles

L1 AFT GIRT BAR LATCH BROKEN. REPLACED SPRING PER AMM 52-11-31. OPS CHECKED NORMAL.

Part: COVER — CRACKED (EXIT SIGN) · airframe 56,389 hrs · 21,306 cycles

L1 DOOR EXIT SIGN COVER CRACKED. REPLACED THE EXIT SIGN COVER.

Part: ACCUMULATOR — LOW PRESSURE (PARKING BRAKE) · airframe 56,389 hrs · 21,306 cycles

NITROGEN CHARGE PRESSURE LOW PARKING/EMERGENCY ACCUMULATOR. SERVICED PARKING ACCUMULATOR PER AMM 12-14-32.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,363 hrs · 21,298 cycles

FLOOR EMERGENCY LIGHT COVER AT ROW 32ABC LT WAS MISSING. INSTALLED A NEW LENS. OK FOR CONTINUED SERVICE IAW GPM 02-01-2.

Part: INDICATION SYS — MALFUNCTIONED (L4 DOOR) · airframe 55,749 hrs · 21,060 cycles

AIRCRAFT WAS NOT GROUNDED. L4 DOOR INDICATES OPEN WHEN CLOSED. PERFORMED AMM TASK 52-13-00-18-803-A, CYCLED L4 DOOR SEVERAL TIMES. FOUND L4 DOOR AND INDICATOR TO BE OPERATING NORMALLY, COULD NOT DUPLICATE.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 55,594 hrs · 21,005 cycles

L1 DOOR ASSIST BOTTLE PRESSURE WAS LOW. SERVICED THE L1 DOOR ASSIST BOTTLE IAW AMM 52-22-00.

Part: LENS — MISSING (READING LIGHT) · airframe 55,354 hrs · 20,920 cycles

L2 DOOR AREA READING LIGHT LENS MISSING. REPLACED THE LENS IAW MM 33-25-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 55,354 hrs · 20,920 cycles

L2 DOOR EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS IAW MM 33-25-00.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 54,996 hrs · 20,779 cycles

AIRCRAFT WAS NOT GROUNDED. AFT FLOOR PANEL 152 DW DELAMINATED. REPLACED FLOOR PANEL PER 25-55-11.

Part: FLOORBOARD — DELAMINATED (AFT CARGO) · airframe 54,987 hrs · 20,775 cycles

DELAMINATED FLOOR BOARD 151MK IN AFT CARGO AREA. REPLACED THE FLOOR BOARD IAW AMM 53-42-15.

Part: BATTERY — WEAK (FLASHLIGHT) · airframe 53,997 hrs · 20,387 cycles

AFT RIGHT EMERGENCY FLASHLIGHT HAS WEAK BATTERY. REPLACED BATTERY IAW AMM.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 53,800 hrs · 20,318 cycles

EMERGENCY POWER SUPPLY UNIT BATTERY FAULT ON CIDS PANEL. REMOVED AND REPLACED EMERGENCY POWER SUPPLY.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 53,774 hrs · 20,306 cycles

LEFT ELEVATOR NR 6 HNGE FITTING WORN. REPLACED LEFT ELEVATOR IAW AMM 27-34-41-400-001-A. AIRCRAFT WAS GROUNDED.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 53,774 hrs · 20,306 cycles

LEFT ELEVATOR HINGE FITTINGS 1- 6 HAVE PLAY. REPLACED LEFT ELEVATOR HINGE FITTINGS 1- 6 IAW AMM 55-16-42. AIRCRAFT WAS GROUNDED.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 53,774 hrs · 20,306 cycles

RIGHT ELEVATOR HINGE FITTINGS 1 THRU 6 HAVE PLAY. REPLACED RIGHT ELEVATOR HINGE FITTINGS 1 THRU 6 PER AMM 55-16-42. AIRCRAFT WAS GROUNDED

Part: BOTTLE — LOW PRESSURE (DOOR) · airframe 53,704 hrs · 20,281 cycles

DOOR DAMPNER LOW PRESSURE. SERVICED THE DOOR DAMPNER IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 53,304 hrs · 20,133 cycles

LENS COVER SEAT 1C (EMERGENCY LIGHT) MISSING. REPLACED LIGHT LENS COVER ON SEAT 1C.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 52,549 hrs · 19,871 cycles

ROW 8 RIGHT EMERGENCY EXIT LIGHT PLASTIC LENS ON SEAT MISSING. REPLACED THE LENS. OK FOR SERVICE.

Part: ELEC CONNECTOR — DIRTY (L4 DOOR) · airframe 52,512 hrs · 19,854 cycles

AFT L4 DOOR DISPLAYED IN ABER WHEN CLOSED. REMOVED THE ELECTRICAL CONNECTOR FROM PROXIMITY SWITCH, CLEANED AND SECURED. OPS CHECKED OK.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 52,156 hrs · 19,721 cycles

EMERGENCY LIGHTS WILL NOT CHECK ON CIDS. REPLACED CABIN POWER SUPPLY UNIT.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 51,900 hrs · 19,615 cycles

LIGHT LENS ON EMERGENCY EXIT LIGHT HAS FALLEN OFF. REPLACED EMERGENCY EXIT LIGHT LENS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 51,722 hrs · 19,547 cycles

EMERGENCY LIGHT LENS MISSING AT SEAT 1C. REPLACED THE LENS.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 51,633 hrs · 19,512 cycles

EMERGENCY EXIT MARKER AT THE R1 DOOR MISSING THE LENS. INSTALLED THE LENS.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 51,615 hrs · 19,506 cycles

PLASTIC COVER FOR EMERGEMERGENCY LIGHT AT THE L1 DOOR IS BROKEN. REPLACED THE LENS.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 51,431 hrs · 19,432 cycles

AIRCRAFT NOT GROUNDED. CABIN EMERGENCY EXIT PATH LIGHT AT ROW 25 INOPERATIVE. FOUND SEAT TO WALL CONNECTOR DISCONNECTED. CONNECTED CONNECTOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — UNSECURE (CABIN) · airframe 51,029 hrs · 19,295 cycles

EMERGENCY EXIT LIGHT UNSECURE. MAINTENANCE SECURED THE EMERGENCY LIGHT AND TRIM AT SEAT 9D AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: COVER — UNSECURE (CABIN) · airframe 51,010 hrs · 19,287 cycles

AIRCRAFT WAS NOT GROUNDED. INFLIGHT REPORTS: EXIT LIGHT COVER 9L CAME OFF. RESECURED EXIT LIGHT COVER PER AMM 33-51-19.

Part: COVER — UNSECURE (CABIN) · airframe 50,700 hrs · 19,161 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT COVER FELL OFF AT 9D. MAINTENANCE INSTALLED NEW EMERGENCY EXIT LIGHT LENS COVER.

Part: DOOR — OBSTRUCTED (L4) · airframe 50,626 hrs · 19,135 cycles

L4 DOOR SHOWS OPEN ON ECAM BUT FLIGHT ATTENDANT FULLY CLOSED DOOR. MAINTENANCE FOUND INSULATION BETWEEN L4 DOOR HANDLE AND PROXIMITY SWITCH , REPOSITIONED INSULATION AND ACCOMPLISHED A SATISFACTORY OPS CHECKED IAW AMM 52-71-00.

Part: SWITCH — BENT (FUEL SYSTEM) · airframe 49,832 hrs · 18,830 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED UNWANTED FUEL IN ACT 2. MAINTENANCE FOUND FUEL PANEL SWITCH GUARD ON 801VU BENT, KEEPING SELECTOR SWITCH BETWEEN OPEN AND CLOSED POSITION. REPLACED PANEL SWITCH PER AMM 2825-55-400-001-A.

Part: APU — OVERSERVICED · airframe 49,613 hrs · 18,742 cycles

AIRCRAFT HAS FOUL ODOR IN MAIN CABIN ON THE GROUND. AIRCRAFT GROUNDED. MAINTENACE FOUND THE APU OIL OVER SERVICED AND REMOVED 1 PINT OF OIL.

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 49,508 hrs · 18,705 cycles

RIGHT SIDE BOX BEAM UPPER FLANGE AFT 2 FASTENER HOLES HAVE CRACKS AT FRAME 43 AND -Y1622. REPAIRED THE BOX BEAM IAW EO 5315Y066.

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 49,508 hrs · 18,705 cycles

LEFT SIDE BOX BEAM UPPER FLANGE CRACKED AT FR 43, +Y1622. REPAIRED THE BOX BEAM IAW EO 5315Y066.

Part: MODULE — LEAKING (APU) · airframe 49,399 hrs · 18,656 cycles

AIRCRAFT WAS GROUNDED, CREW REPORTED A STRONG ODOR TROUGH ACFT CABIN THAT SMELLED LIKE PLASTIC OR CRAYONS DURING THE BOARDING PROCESS WITH APU BLEED AIR ON. THE ACFT WAS DEPLANED AND REMOVED FROM SERVICE. MAINTENANCE FOUND AN OIL LEAK AT THE APU LUBE MODULE AND REPLACED IT IAW AMM 49-91-45. A SATISFACTORY LEAK AND OPS CHECK WAS ACCOMPLISHED ALONG WITH THE DECONTAMINATION TASK CARD 26L00021004 WITH NO ADDITIONAL ODORS NOTED.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 49,214 hrs · 18,581 cycles

AIRCRAFT WAS GNDED. MODERATE AIRFRAME VIBRATION AT 330 KIAS, CLIMBING THROUGH FL 260. RAPID ONSET, GRADUAL REDUCTION AT 300 - 305 KIAS. NOT VISIBLE ON FLIGHT CONTROL PAGE, VIBRATION RATE 60 - 75 HZ. VIBRATION DID NOT CHANGE WITH POWER REDUCTION. REPLACED THE RT ELEVATOR NR 2 HINGE FITTING & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. ALSO SEE RELATED REPORT ON AALA 201605309003.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 49,214 hrs · 18,581 cycles

AIRCRAFT WAS GNDED. MODERATE AIRFRAME VIBRATION AT 30 KIAS, CLIMBING THROUGH FL 260. RAPID ONSET, GRADUAL REDUCTION AT 300 - 305 KIAS. NOT VISIBLE ON FLIGHT CONTROL PAGE, VIBRATION RATE 60 - 75 HZ. VIBRATION DID NOT CHANGE WITH POWER REDUCTION. REPLACED THE LT ELEVATOR NR 1 HINGE FITTING & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. ALSO SEE RELATED REPORT ON AALA 201605319004.

Part: LENS — WRONG PART (CABIN) · airframe 48,793 hrs · 18,392 cycles

AIRCRAFT WAS NOT GNDED. SEAT MOUNTED EMER LIGHT LENS COVERS 8D, REQUIRED TO BE RED IAW JC 26L00005005. REPLACED LENS COVER IAW AMM 33-51-18.

Part: LENS — WRONG PART (CABIN) · airframe 48,793 hrs · 18,392 cycles

AIRCRAFT WAS NOT GNDED. SEAT MOUNTED EMER LIGHT LENS COVER 10C, REQUIRED TO BE RED IAW JC 26L00005005. REPLACED LENS COVER IAW AMM 33-51-18.

Part: PROXIMITY SENSOR — DEFECTIVE (LANDING GEAR) · airframe 48,611 hrs · 18,318 cycles

RETURNED, ACFT WAS GNDED, AFTER TAKEOFF THE FLIGHT CREW WAS UNABLE TO RETRACT THE LG, THE HANDLE WOULD NOT MOVE WHICH WAS FOLLOWED BY AN ECAM SHOCK ABSORBER FAULT. THE FAULT CLEARED ON ITS OWN, CREW RETURNED, BUT DID NOT DECLARE AN EMER. THE ACFT LANDED AT DEN WITH NOT FURTHER INCIDENT. MX ACCOMPLISHED TSM 32-31-00-810-860-A. NO FAULTS FOUND. PERFORMED EXTENSION TEST OF THE NORMAL EXTENSION & RETRACTION OF THE NLG IAW AMM 32-31-00-720-003A. NOO FAULTS FOUND. ACFT WAS RETURNED TO SERVICE. ACCOMPLISHED ADDITIONAL TROUBLESHOOTING & REPLACED PROXIMITY SENSORS G24 & G25 IAW AMM 32-31-73 & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. SAME PART NUMBER FOR BOTH SENSORS WHICH HAS BEEN ADDED TO SECTION 5.

Part: LENS — MISSING (CABIN) · airframe 48,460 hrs · 18,254 cycles

AIRCRAFT WAS NOT GNDED. LENS COVER MISSING EMER LIGHT WALL MOUNTED AT MID-LAVATORY. INSTALLED LENS COVER IAW AMM 33-51-19.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,478 hrs · 17,839 cycles

REAR CABIN EMER FLASHLIGHT NOT OPERATING LT SIDE. REPLACED BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SCHRADER VALVE — LEAKING (L2 DOOR) · airframe 46,380 hrs · 17,383 cycles

FLIGHT ATTENDANT HAS 2 RED LIGHTS ON CAUTION BUTTON ON CIDS PANEL. FOUND SCHRADER VLV LEAKING AT L2 DOOR DAMPER. R & R SCHRADER CHARGING VLV IAW AMM TASK 52-22-00-860-005-A & SERVICED IAW TASK 52-22-00-614-002-A. OPERATIONS CHECKED GOOD.

Part: ACTUATOR — LOW PRESSURE (L2 DOOR) · airframe 46,074 hrs · 17,273 cycles

CAUTION LIGHT ILLUMINATED ON CIDS PANEL. SERVICED THE L2 DOOR ASSIST ACTUATOR.

Part: LENS — MISSING (CABIN) · airframe 45,850 hrs · 17,185 cycles

EMERGENCY PATH LIGHTING MISSING UNDER SEAT LENS AT 1 LT. REPLACED THE EMER LIGHT LENS AT SEAT 1 LT.

Part: BOTTLE — LOW PRESSURE (ENTRY DOOR)

MAIN ENTRY DOOR ASSIST BOTTLE LOW PRESS. SERVICED THE MAIN ENTRY DOOR ASSIST BOTTLE.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 45,058 hrs · 16,853 cycles

CIDS PANEL CAUTION LIGHT ON. FOUND DOOR L2 ASSIST PRESS LOW. SERVICED DOOR L2 ASSIST CYLINDER IAW AMM 52-22-00-614-002.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 44,702 hrs · 16,713 cycles

L1 DOOR ASSIST BOTTLE LOW. SERVICED L1 DOOR ASSIST BOTTLE TO IAW AMM 52-00-614.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 44,682 hrs · 16,705 cycles

CIDSS CAUTION LIGHTS ON FWD. FLIGHT ATTENDANT PANEL ILLUMINATED. DOOR L2 ASSIST BOTTLE LOW, SERVICED DOOR L2 ASSIST BOTTLE IAW AMM 5200-614-050-A.

Part: LENS — MISSING (CABIN) · airframe 43,938 hrs · 16,408 cycles

RON VISIT SEAT ROW 8 LT EMER LIGHT LENS MISSING. REPLACED EMER LIGHT LENS.

Part: LENS — MISSING (CABIN) · airframe 43,898 hrs · 16,394 cycles

ROW 10C EMER LIGHT LENS IS MISSING. INSTALLED EMER LIGHT LENS AT 10C IAW AMM 33-50-00.

Part: DAMPER — LOW PRESSURE (L2 DOOR) · airframe 43,877 hrs · 16,382 cycles

REPORTED THE L2 DOOR DAMPER LOW. SERVICED L2 DOOR DAMPER IAW TASK 52-22-00-614-002.

Part: DAMPER — LOW PRESSURE (L1 DOOR) · airframe 43,877 hrs · 16,382 cycles

REPORTED THE L1 DOOR DAMPER LOW. SERVICED L1 DOOR DAMPER IAW AMM TASK 52-22-00-614-002.

Part: POWER SUPPLY — FAULTED (CABIN) · airframe 43,816 hrs · 16,356 cycles

MID CABIN POWER SUPPLY FAULT ON TEST. R & R POWER SUPPLY IAW AMM 33-51-38. OPERATIONS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,816 hrs · 16,356 cycles

THE MID LT & RT EMER LIGHTS FAILED. R & R MID LT & RT EMER LIGHT BATTERIES IAW AMM 33-51-00. OPERATIONS CHECKED GOOD.

Part: PIN — MISSING (R2 DOOR) · airframe 43,728 hrs · 16,321 cycles

THE R2 DOOR DISARM HANDLE LOOSE & MISSING PIN. REPLACED MISSING PIN & SECURED GRIP PLATE FOR DOOR R2 DISARM HANDLE.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 43,732 hrs · 16,322 cycles

THE L1 DOOR ASSIST & DAMPER ACTUATOR BOTTLE WITH LOW PSI 300. SERVICED L1 DOOR ACTUATOR IAW AMM 52-10-00-614-001.

Part: PIN — MISSING (L2 DOOR) · airframe 43,732 hrs · 16,322 cycles

THE LT L2 DOOR DISARM HANDLE LOOSE & MISSING PIN. INSTALLED PIN AS NEEDED.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 43,657 hrs · 16,290 cycles

CREW RECEIVED A RED CIDS LIGHT ON FWD FLIGHT ATTENDANT PANEL. L2 DOOR ASSIST BOTTLE LOW. SERVICED L2 DOOR ASSIST BOTTLE. OPERATIONS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 43,511 hrs · 16,243 cycles

EMERGENCY AISLE LIGHT LENS IS MISSING AT ROW 22R. INSTALLED EMER LIGHT LENS AT ROW 22R.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 43,511 hrs · 16,243 cycles

L1 DOOR ASSIST BOTTLE PRESS IS LOW. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 42,955 hrs · 16,008 cycles

THE R4 DOOR EMER OPERATION CYLINDER IS 200 PSI LOWER THAN PLACARD. SERVICED R4 DOOR EMER OPERATION CYLINDER IAW AMM 52-10-00-614-001A.

Part: LEVER — LOOSE (R3 DOOR) · airframe 42,650 hrs · 15,880 cycles

CREW REPORTED 3R DOOR ARMING LEVER LOOSE. SECURED DOOR LEVER, OPERATIONS GOOD.

Part: COVER — MISSING (CABIN) · airframe 42,131 hrs · 15,664 cycles

AIRCRAFT ROW 10 LT COVER OVER EMERGENCY FLOOR LIGHT MISSING. REPLACED EMERGENCY FLOOR LIGHT COVER 10 LT.

Part: SLAT — LOCKED (WING) · airframe 42,118 hrs · 15,659 cycles

DURING APPROACH, CREW SELECTED CONF 1, GOT IC SLAT FAULT, SLATS WERE LOCKED UP. DECLARED AN EMERGENCY, ON FOURTH CYCLE, SLATS WENT DOWN & NORMAL THEREAFTER. FLIGHT LANDED SAFELY & TAXIED TO THE GATE. ACCOMPLISHED TSM CK 27-81-00-810-810A, CHECKED GOOD, NO FAULTS FOUND.

Part: UNKNOWN — SMOKE (BLEED AIR SYS) · airframe 42,042 hrs · 15,622 cycles

ON LANDING ROLLOUT, FLIGHT ATTENDANT CALLED & SAID THAT WE HAD SMOKE IN THE CABIN, AFT MOSTLY, & IT WAS GETTING PRETTY THICK. A COMMENT THAT IT MAY BE COMING FROM THE VENTS. NOT MUCH SMOKE IN THE FWD. AVIONICS SAID IMMEDIATE ACTION, QRH CHECKLIST WAS EXECUTED WHICH SEEMED TO CLEAR IT UP FOR THE MOST PART. PROCEEDED TO THE GATE SO WE COULD REMOVE THE PASSENGERS. AS A PRECAUTION, WE HAD THE FIRE DEPARTMENT GO THROUGH THE CABIN & E&E COMPARTMENT WITH THEIR OWN SNIFFER. FOUND NO RESULTS, ACCOMPLISHED JOB CARD 26L00021001 & FOUND THE NR 1 BLEED TO BE THE CAUSE OF CABIN ODOR. PLACED NR 1 BLEED AIR SYS ON MEL 36-11-01A. COMPLIED WITH JOB CARD 26L00021001 AGAIN & RAN PACKS WITH APU & ENGINES ALL NIGHT. NO ODOR NOTICED, CLEARED & REMOVED MEL 36-11-01A.

Part: LEVER — LOOSE (L2 DOOR) · airframe 41,933 hrs · 15,572 cycles

CREW REPORTED 2L DOOR ARMING LEVER LOOSE. CORRECTLY TORQUED HARDWARE ON 2L DOOR ARMING LEVER, OK FOR SERVICE.

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 41,803 hrs · 15,513 cycles

MAINTENANCE REPORTED THE EMERGENCY EXIT DOOR 3R HANDLE LOOSE, HAS EXCESSIVE MOVEMENT. MX TIGHTENED ARM & DISARMED HANDLE, OPERATIONS CHECKED GOOD.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 41,675 hrs · 15,459 cycles

CREW REPORTED THE FLIGHT ATTENDANT FWD PANEL CIDS CAUTION LIGHT ON. FLIGHT RETURNED TO THE GATE. FOUND THE MID LT DOOR PRESS ON CIDS SERVICED 2L DOOR ASSIST BOTTLE IAW AMM 52-22-00-614-002-A.

Part: COVER — BROKEN (CABIN) · airframe 41,576 hrs · 15,422 cycles

CREW REPORTED THE EMERGENCY PATH LIGHT COVER AT SEAT 3C BROKEN. MX REPLACED SEAT 3C EMERGENCY EXIT LIGHT COVER AS REQUIRED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 41,301 hrs · 15,307 cycles

THE FLASHLIGHT AT DOOR 2R NOT BLINKING. REPLACED EMERGENCY FLASHLIGHT BATTERY AT 2R DOOR, OPERATIONS CHECKED OK.

Part: LENS — BROKEN (CABIN) · airframe 41,274 hrs · 15,300 cycles

THE EMERGENCY EXIT 3R PLASTIC LENS COVER BROKEN, DUCT TAPED. REPLACED LIGHT COVER AS NEEDED, CHECKED OK.

Part: LEVER — LOOSE (L3 DOOR) · airframe 41,240 hrs · 15,288 cycles

BOTH 3L & 3R DOOR ARMING LEVERS ARE LOOSE. TIGHTENED BOTH 3L & 3R ARMING LEVERS IAW A321 AMM 52-22-00-820, OPERATIONS CHECKED GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 40,981 hrs · 15,164 cycles

CREW REPORTED A EMERGENCY LIGHT LENS BROKEN. MAINTENANCE REPLACED LENS.

Part: UNKNOWN — ODOR (CABIN) · airframe 40,617 hrs · 15,017 cycles

THRU 10,000 FEET ELECTRIC ODOR IN FORWARD GALLEY. TROBLESHOT CABIN AIR QUALITY, NO ODORS NOTED.

Part: DOOR — CRACKED (TAILCONE) · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CRACK ON TAIL CONE SERVICE DOOR 312AR BETWEEN FRAMES 71 & 72 & BETWEEN S31-32R. REPAIRED TAILCONE SERVICE DOOR IAW SRM 51-42-11 & DWG D52470005.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 40,581 hrs · 14,999 cycles

2S CHECK - LEFT FORWARD EMERGENCY DOOR ASSIST BOTTLE PRESSURE LOW. REPLACED DIAPHRAM PIN & SEALS ON LT FORWARD EMERGENCY DOOR ASSIST BOTTLE & SERVICED TO PROPER PRESSURE IAW AMM 52-10-00-610-001-A.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 40,581 hrs · 14,999 cycles

2S CHECK, DELAMINATION FOUND ON FLOOR PANEL 151GF BETWEEN FRAMES 53 TO 56 & S38L TO 38R. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 40,581 hrs · 14,999 cycles

2S CHECK, DELAMINATION FOUND ON FLOOR PANEL 231YH BETWEEN FRAMES 35.1 TO 35.5 & Y254 TO -Y254. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK - CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 47.2 TO 47.4, -Y1732. REPLACED FLOOR SUPPORT IAW SRM 51-42-11, 51-44-11 & 51-75-12.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 40,581 hrs · 14,999 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 261DF BETWEEN FRAMES 66 TO 68 BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00, PARA 8H., FIG 209.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 68 TO 69, Y1162. REPLACED FLOOR SUPPORT IAW SRM 51-42-11, 53-41-14 & 51-75-12.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 66, Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-42-11, 53-41-14 & 51-75-12.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 40,581 hrs · 14,999 cycles

DELAMINATION ON FLOOR PANEL 261HG BETWEEN FRAMES 64 TO 66 & BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL IAW SRM 53-02-00, PARA 8H., FIG 209.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 67 TO 68, Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-42-11, 53-00-14 & 51-75-12.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 40,581 hrs · 14,999 cycles

DELAMINATION ON FLOOR PANEL 261CG BETWEEN FRAMES 64 TO 66 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00, PARA 8H., FIG 209.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON FLOOR SUPPORT BETWEEN FRAME 47 Y1732. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-00-14, 51-42-11 & 51-75-12.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON L2 DOOR SILL BETWEEN FRAMES 66 TO 68, Y1732. REPLACED SILL IAW SRM 51-74-00, 51-41-14, 51-42-11 & 51-75-12.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 40,581 hrs · 14,999 cycles

DELAMINATION ON FLOOR PANEL 262BG BETWEEN FRAMES 64 TO 66 BETWEEN -Y765 TO -Y1732. REPLACED FLOOR PANEL IAW SRM 53-02-00, PARA 8H., FIG 209.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 40,581 hrs · 14,999 cycles

DELAMINATION ON FLOOR PANEL 221PF BETWEEN FRAMES 12 TO 16 & BETWEEN Y250 TO Y1732. REPLACED FLOOR PANEL IAW SRM 53-02-00, PARA 8H., FIG 209, & 53-12-00, DIA 101.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 40,581 hrs · 14,999 cycles

DELAMINATION ON FLOOR PANEL 221EF BETWEEN FRAMES 16 TO 20 & BETWEEN Y254 TO Y1292. REPLACED FLOOR PANEL IAW SRM 53-02-00, PARA 8H., FIG 209, & 53-12-00, DIA 101.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 68 TO 69, -Y1162. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-41-14, 51-42-11 & 51-75-12.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 67 TO 68, -Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 51-41-14, 51-42-11 & 51-75-12.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 65 TO 66, -Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-41-14, 51-42-11 & 51-75-12.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON L4 DOOR SHAPE SILL AT FRAME 67, Y1470. REPLACED SILL IAW SRM 51-74-00, 53-41-41, 51-44-11 & 51-42-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 67 TO 69, -Y465. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-41-14, 51-42-11 & 51-75-12.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON FLOORBEAM BETWEEN FRAMES 65 TO 67, -Y765. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-41-14, 51-42-11 & 51-75-12.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON R2 DOOR SILL BETWEEN FRAMES 66 TO 68, -Y1732. REPLACED SILL IAW SRM 51-74-00, 51-41-14, 51-44-11, 51-42-11 & 51-75-12.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION FOUND ON FLOOR SUPPORT BETWEEN FRAMES 65 - 66, Y765. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 51-42-11, 53-00-14 & 51-75-12.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION FOUND ON FLOOR SUPPORT BETWEEN FRAMES 66 TO 68, -Y765. REPLACED FLOOR SUPPORT IAW SRM 51-42-11, 51-72-11 & 51-75-12.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON SHEAR PLATE BETWEEN FRAMES 69 TO 70, Y1732. REPLACED SHEAR PLATE IAW SRM 51-73-00, 51-42-11, 51-21-11 & 51-75-12.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON SEAT TRACK BETWEEN FRAMES 16 TO 20, Y1292. REPLACED SEAT TRACK IAW SRM 51-42-11, 53-41-15 & 51-44-11.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 69 - 70, Y765. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-00-14, 51-42-11, 51-75-12.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON FLOOR SUPPORT AT FR20, -Y254. REPLACED FLOOR SUPPORT IAW SRM 51-74-00, 53-11-14, 51-42-11 & 51-75-12.

Part: DUMMY RAIL — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON DUMMY RAIL BETWEEN FR12 TO FR16, -Y81. REPLACED DUMMY RAIL IAW SRM 53-11-14, 51-42-11 & 51-44-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON SEAT TRACK AT FRAME 20, -Y765. REPLACED SEAT TRACK IAW SRM 51-74-00, 51-42-11 & 51-75-12.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON SEAT TRACK BETWEEN FRAMES 16 AND 21, -Y1292. REPLACED SEAT TRACK IAW SRM 51-74-00, 53-11-15 AND 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,581 hrs · 14,999 cycles

2S CHECK, CORROSION ON SEAT TRACK BETWEEN FRAMES 65 AND 67, -Y318. REPLACED SEAT TRACK IAW SRM 51-72-12 AND 51-42-11.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 40,428 hrs · 14,933 cycles

CIDS CAUTION LIGHT ON FWD F/A PANEL. SERVICED THE R2 DOOR ASSIST BOTTLE IAW AMM 52-22-00-860-003.

Part: LENS — MISSING (CABIN) · airframe 40,017 hrs · 14,755 cycles

MISSING LENS ON EMERGENCY LIGHT AT ROW 20C. INSTALLED LENS ON EMERGENCY LIGHT AT ROW 20C IAW AMM 33-51-19.

Part: SLIDING WINDOW — CRACKED (COCKPIT) · airframe 39,982 hrs · 14,738 cycles

CAPTAIN'S SLIDING WINDOW APPEARS TO HAVE SEVERAL CRACKS IN THE TOP LT CORNER PLUS SEVERAL EXTENDING STRAIGHT DOWN. THE SUN LIGHT MADE THEM LOOK CRACKED. R & R LT SLIDING WINDOW IAW AMM 56-12-11.

Part: LENS — MISSING (CABIN) · airframe 39,390 hrs · 14,490 cycles

R4 DOOR EMERGENCY EXIT LENS COVER MISSING. REPLACED R4 DOOR EMERGENCY EXIT LENS COVER.

Part: SKIN — CANNING (FUSELAGE) · airframe 39,070 hrs · 14,349 cycles

RON VISIT - OIL CANNING ON EXTERNAL FUSELAGE SKIN BETWEEN FR3 TO FR4 APPROX 10 INCHES ABOVE, FORWARD & TO THE RIGHT OF FORWARD AVIONICS DOOR 811. REPAIRED FUSELAGE SKIN BETWEEN FR3 TO FR4 IAW A321 SRM 53-00-11 FIG 220.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 37,295 hrs · 13,632 cycles

2L DOOR BOTTLE LOW PRESSURE. SERVICED EMERGENCY OPERATION CYLINDER AT EMERGENCY EXIT DOOR 2L IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002A.

Part: CYLINDER — LOW PRESSURE (DOOR) · airframe 36,385 hrs · 13,278 cycles

FORWARD LEFT DAMPER / EMERGENCY OPERATION CYLINDER LOW PRESSURE. SERVICED FORWARD LEFT DAMPER / EMERGENCY OPERATION CYLINDER IAW AMM 52-10-00-614-001-A.

Part: CYLINDER — LOW PRESSURE (DOOR) · airframe 36,385 hrs · 13,278 cycles

AFT RIGHT DAMPER/EMERGENCY OPERATION CYLINDER LOW PRESSURE. SERVICED AFT RIGHT DAMPER / EMERGENCY OPERATION CYLINDER. OPS CHECKED GOOD.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 35,981 hrs · 13,101 cycles

L-1 DOOR BOTTLE NEEDS SERVICE. MAINTENANCE SERVICED L1 DOOR BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: ACCESS DOOR — MISSING (ZONE 100) · airframe 35,887 hrs · 13,062 cycles

ON WALKAROUND INSPECTION ,AFTER ARRIVAL, FOUND BLUE HYDRAULIC SERVICE DOOR MISSING. INSTALLED NEW UPPER ACCESS DOOR IAW MM 52-42-25-400-001A.

Part: CYLINDER — LOW PRESSURE (R3 DOOR) · airframe 34,506 hrs · 12,544 cycles

CIDS CAUTION LIGHT "ON" CIDS PANEL. FOUND R3 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED BOTTLE IAW AMM 52-10-00-614-001, CIDS OPS CHECKED NORMAL.

Part: LENS — MISSING (CABIN) · airframe 34,496 hrs · 12,542 cycles

THE 4R DOOR COVER OVER EXIT LIGHT IS MISSING. REPLACED LENS COVER ON 4R DOOR (OVER EXIT LIGHT LED).

Part: LEVER — LOOSE (EMERGENCY EXIT) · airframe 34,389 hrs · 12,506 cycles

EMERGENCY EXIT DOOR 3R ARM / DISARM LEVER LOOSE. SECURED LEVER.

Part: LENS — MISSING (EXIT SIGN) · airframe 34,369 hrs · 12,496 cycles

LENS COVER EXIT SIGN MISSING FROM R4 ENTRY DOOR. INSTALLED NEW LENS COVER EXIT SIGN R4 ENTRY DOOR. OPS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 34,345 hrs · 12,480 cycles

AISLE EXIT LIGHT COVER SEAT 8D IS MISSING. MAINTENANCE INSTALLED AISLE EXIT LIGHT COVER AT SEAT ROW 8D.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 34,214 hrs · 12,444 cycles

L-1 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED L-1 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 33,947 hrs · 12,333 cycles

L1 DOOR ASSIST ACCUMULATOR PRESSURE REQUIRES SERVICING. MAINTENANCE SERVICED L1 DOOR ASSIST ACCUMULATOR IAW AIRBUS MAINTENANCE MANUAL 52-10-00-614.

Part: CHILLER — DEFECTIVE (GALLEY) · airframe 33,856 hrs · 12,297 cycles

AFT GALLEY AREA HAD AN ACRID ODOR THAT DID NOT DIMINISH UNTIL THE CHILLER WAS TURNED OFF - CIRCUIT BREAKER WAS PULLED AS PRECAUTION. MAINTENANCE REMOVED AND REPLACED AFT GALLEY CHILLER.

Part: DAMPER — LOW PRESSURE (EMERGENCY EXIT) · airframe 33,257 hrs · 12,085 cycles

EES - PHL-SAN - FORWARD R/H MID (R2) PASSENGER EMERGENCY DOOR DAMPER NEEDS SERVICE. SERVICED FORWARD RT MID (R2) PASSENGER EMERGENCY DOOR DAMPER IAW AMM 52-10-00-03.

Part: DAMPER — LOW PRESSURE (PAX DOOR) · airframe 33,257 hrs · 12,085 cycles

EES - PHL-SAN - AFT RT PASSENGER SERVICE / EMERGENCY DOOR DAMPER NEEDS SERVICE. SERVICED AFT RT PASSENGER SERVICE / EMERGENCY DOOR DAMPER IAW AMM 52-10-00-03.

Part: DAMPER — LOW PRESSURE (EMERGENCY EXIT) · airframe 33,257 hrs · 12,085 cycles

EES - PHL-SAN - AFT LT MID PASSENGER EMERGENCY DOOR DAMPER NEEDS SERVICE (L3). SERVICED AFT LT MID PASSENGER EMERGENCY DOOR DAMPER IAW AMM 52-10-00-03.

Part: DAMPER — LOW PRESSURE (PAX DOOR) · airframe 33,257 hrs · 12,085 cycles

EES - PHL-SAN - AFT LT PASSENGER SERVICE / EMERGENCY DOOR DAMPER NEEDS SERVICE. SERVICED LT AFT PASSENGER SERVICE / EMERGENCY DOOR IAW AMM 52-10-00-03.

Part: ACTUATOR — LOW PRESSURE (EMERGENCY EXIT) · airframe 33,257 hrs · 12,085 cycles

EES - PHL-SAN - FORWARD LT MID PASSENGER EMERGENCY DOOR DAMPER NEEDS SERVICE (L2). SERVICED FORWARD MID LT PASSENGER EMERGENCY DOOR DAMPER (L2) IAW AMM 52-10-00-03.

Part: DAMPER — LOW PRESSURE (EMERGENCY EXIT) · airframe 33,257 hrs · 12,085 cycles

EES - PHL-SAN - RT AFT MID (R3) PASSENGER EMERGENCY DOOR DAMPER NEEDS SERVICE. SERVICED RT AFT MID (R3) PASSENGER EMERGENCY DOOR DAMPER IAW AMM 52-10-00-03.

Part: LENS — MISSING (CABIN) · airframe 33,170 hrs · 12,061 cycles

LAX - EEL - L4 DOOR EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED MISSING LIGHT LENS COVER.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 32,992 hrs · 11,995 cycles

MX - LAX - EES - L-1 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: TRANSMITTER — INACCURATE (OIL SYSTEM) · airframe 32,970 hrs · 11,986 cycles

FLT 1694 - TPA-PHL - EMERGENCY LANDING - NR 2 ENGINE & NR 2 IDG INDICATED A SUSTAINED HIGH OIL TEMPERATURE OF 150 DEGREES FOR A MAXIMUM OF 10 MINUTES. DIVERTED TO JAX. NR 2 OIL QUANTITY READING IS INACCURATE. REMOVED AND REPLACED NR 2 ENGINE OIL QUANTITY TRANSMITTER PER AMM 79-31-15-05. OPERATIONAL CHECK WAS GOOD.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 32,856 hrs · 11,942 cycles

FLT 1463 - CLT-SFO - PASSENGER DOOR L1 AND EMERGENCY DOOR L2 DOOR ASSIST BOTTLES REQUIRE SERVICING. SERVICED L1 DOOR ASSIST BOTTLES PER AMM 52-10-00-614-001 AND AMM 52-22-00-614-002. OPERATIONAL CHECK WAS GOOD.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 32,856 hrs · 11,942 cycles

FLT 1463 - CLT-SFO - PASSENGER DOOR L1 AND EMERGENCY DOOR L2 DOOR ASSIST BOTTLES REQUIRE SERVICING. SERVICED L2 DOOR ASSIST BOTTLES PER AMM 52-10-00-614-001 AND AMM 52-22-00-614-002. OPERATIONAL CHECK WAS GOOD.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 32,638 hrs · 11,874 cycles

FLT 1482 - ATL - EES - L-1 DOOR ASSIST BOTTLE LOW. MAINTENANCE SERVICED L-1 DOOR ASSIST BOTTLE AS REQUIRED.

Part: BEARING — FAILED (ENGINE) · airframe 32,553 hrs · 11,840 cycles

FLT 1446 -AT CRUISE, 5.2 VIBRATION INDICATION ON N2. BEGAN NEARING A THUMPING SOUND WHICH WAS MORE PRONOUNCED IN THE REAR OF THE AIRCRAFT AS CONFIMED BY THE FLIGHT ATTENDANTS. N2 WENT TO 9 AND THE ENGINE BEGAN TO SPOOL DOWN. CREW PERFORMED ENGINE SHUTDOWN PROCEDURES AND DECLARED EMERGENCY, DIVERTED TO OMA. REMOVED AND REPLACED NR 2 ENGINE PER PER JPC 2640071001. VENDOR IDENTIFIED FAILURE OF NR 4 BEARING AS THE ROOT CAUSE.

Part: DIAPHRAGM — DEFECTIVE (L1 DOOR) · airframe 31,800 hrs · 11,550 cycles

FLT 1753 - TPA - EES - FOUND DOOR L1 EMERGENCY ASSIST BOTTLE PRESSURE AT 0 PSI, PERCUSSION MECHANISM NOT ACTUATED. MAINTENANCE REPLACED DOOR L1 PERCUSSION MECHANISM DIAPHRAGM AND SEALS AND SERVICED DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: BOTTLE — LOW PRESSURE (R4 DOOR) · airframe 31,800 hrs · 11,550 cycles

FLT 1753 - TPA - EES - FOUND DOOR R4 EMERGENCY ASSIST BOTTLE LOW. MAINTENANCE SERVICED R4 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,195 hrs · 11,326 cycles

PIT - C11 - EEL - EMERGENCY LIGHT ASSEMBLY ABOVE R-4 DOOR IS BAD. REPLACED EMERGENCY LIGHT ASSEMBLY ABOVE R-4 DOOR IAW A321 AMM 33-51-11.

Part: CABLE — BROKEN (CABIN) · airframe 31,195 hrs · 11,326 cycles

PIT - C11 - EEL - ROW 10L EMERGENCY FLOOR LIGHT IS INOP. BROKEN WIRE AT FLOOR TO CABIN WALL AREA. REPLACED WALL TO SEAT CABLE ASSEMBLY IAW A321 AMM 33-51-19.

Part: BOTTLE — LOW PRESSURE (CABIN DOOR) · airframe 30,489 hrs · 11,042 cycles

FLT 1431 - LAX - EES - CIDS PANEL CAUTION LIGHT LEFT MID CABIN DOOR LOW. MAINTENANCE SERVICED LEFT MID DOOR ASSIST BOTTLE TO PROPER PRESSURE IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002.

Part: ACTUATOR — LOW PRESSURE (L2 DOOR) · airframe 29,724 hrs · 10,773 cycles

FLT 797 - LAX - EES - CIDS CAUTION LIGHT ON. MAINTENANCE SERVICED L2 DOOR ASSIST ACTUATOR IAW AIRBUS MAINTENANCE MANUAL 52-22-00-614-002.

Part: BOTTLE — LOW PRESSURE (EVAC SLIDE) · airframe 29,523 hrs · 10,690 cycles

FLT 1021 - CLT - EES - CIDS PANEL LIGHTS FOR L-2 DOOR. MAINTENANCE SERVICED L-2 DOOR EMERGENCY SLIDE BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-22-00-616-002.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 29,075 hrs · 10,523 cycles

FLT 770 - CLT - EES - CIDS CAUTION LIGHT REMAINS ON. MAINTENANCE FOUND MID LEFT DOOR (L2) BOTTLE PRESSURE LOW. SERVICED DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-10-00-03.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 28,300 hrs · 10,217 cycles

FLT 1496 - CABIN FLASHLIGHT STRAP MISSING. MAINTENANCE REMOVED AND REPLACED CABIN FLASHLIGHT AT FORWARD GALLEY LEFT FLIGHT ATTENDANT JUMPSEAT AND REPLACED STRAP AS REQUIRED.

Part: LENS — MISSING (CABIN) · airframe 28,081 hrs · 10,146 cycles

FLT 1630 - LGA - EEL - EMERGENCY EXIT LIGHT FLOOR LEVEL AT ROW 9 MISSING COVER. MAINTENANCE REPLACED MISSING COVER AT ROW 9.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 27,149 hrs · 9,807 cycles

LOG PAGE 4515062 - FLT 965-SFO - EMERGENCY EGRESS SYSTEM - LT NR 2 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED LT NR 2 DOOR ASSIST BOTTLE.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 27,011 hrs · 9,765 cycles

FLT 1144 - PHL - EMERGENCY EGRESS SYSTEM - CIDS PANEL CAUTION. MAINTENANCE SERVICED L1 AND L2 DOOR ASSIST BOTTLES PER AIRBUS MAINTENANCE MANUAL 52-11-14.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 27,011 hrs · 9,765 cycles

FLT 1144 - PHL - EMERGENCY EGRESS SYSTEM - CIDS PANEL CAUTION. MAINTENANCE SERVICED L1 AND L2 DOOR ASSIST BOTTLES PER AIRBUS MAINTENANCE MANUAL 52-11-14.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 26,612 hrs · 9,640 cycles

FLT 1558 - CLT - EMERGENCY EGRESS SYSTEM - CAUTION LIGHTS ILLUMINATED ON FLIGHT ATTENDANT CIDS PANEL. MAINTENANCE SERVICED L2 DOOR ASSIST CYLINDER PER AIRBUS MAINTENANCE MANUAL 52-10-00-991-029.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 26,557 hrs · 9,622 cycles

FLT 1532 - SEA - EMERGENCY EGRESS SYSTEM - CIDS CAUTION LIGHT ON. MAINTENANCE SERVICED L-2 DOOR ASSIST BOTTLE IAW AIRBUS MAINTENANCE MANUAL 52-22-00.

Part: CYLINDER — LOW PRESSURE (LT DOOR) · airframe 25,589 hrs · 9,295 cycles

FLT 753 - PHL - EMERGENCY EQUIPMENT - PILOT REPORTED CIDS CAUTION LIGHT ON. MAINTENANCE SERVICED MID LEFT DOOR ASSIST BOTTLE AND RESET CIDS SYSTEM.

Part: CHARGER — DEFECTIVE (CABIN) · airframe 24,975 hrs · 9,086 cycles

TPA - EEL - A03 CHECK - NR 8286691, AFT RIGHT EMERGENCY LIGHT BATTERY CHARGER FOUND BAD DURING TEST OF CABIN EMERGENCY LIGHTING. REMOVED, REPLACED AND OPERATIONAL CHECKED AFT RIGHT EMERGENCY LIGHT BATTERY CHARGER IAW A321 AMM 33-51-38.

Part: BEARING — FAILED (NR 2 ENGINE) · airframe 24,737 hrs · 9,007 cycles

FLT 1419 PHL-LAX - EMERGENCY LANDING - CREW REPORTED A COMPRESSOR STALL AT FL310 ON THE NR 2 ENGINE. AIRCRAFT DESCENDED TO 280 AND VIBRATIONS CONTINUED. ENGINE WAS SHUT DOWN DUE TO BLUE ELECTRICAL SYSTEM FAILURE. CREW DECLARED AN EMERGENCY AND DIVERTED TO COS. MX R&R THE NR 2 ENGINE DUE TO FAILED BOROSCOPE. ALSO REPLACED BLUE SYSTEM HYDRAULIC RESERVOIR PRESSURIZATION LINE AND HYDRAULIC LINE FROM PUMP TO ACOUSTIC FILTER DUE TO CHAFING.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 24,569 hrs · 8,940 cycles

LOG PAGE 4310910 FLT NR 788 CLT-TPA EEL EMERGENCY POWER SUPPLY UNIT FAILED AFT MID CABIN RT SIDE. MX R&R THE EPSU. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,971 hrs · 8,440 cycles

FLT 881 CLT - 2R FLASHLIGHT BATTERY WEAK. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT BATTERY AT 2R DOOR. OPERATIONAL CHECK WAS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 20,303 hrs · 20,303 cycles

TOPSIDE OF FLOORBEAM Y1292 HAS CORROSION. INSTALLED FILLER WITH ANGLE SPLICES ON BOTH SIDES PER SRM 53-00-14; CORR TASK JA-220-53500, DEFECT SIZE: 1.5 X 1.5 INCH.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 1 · airframe 20,303 hrs · 20,303 cycles

FR 66 JUST FWD OF RT AFT DOOR IN SILL PLATE UPPER ANGLE AT NUT CLIP HOLE CORRODED. INSTALLED ANGLE (BATHRUB) REPAIR PER SRM 53-41-14; CORR TASK JA-260-53500-14, DEFECT SIZE: 1 X 1 INCH.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 1 · airframe 20,303 hrs · 20,303 cycles

TOPSIDE OF FLOORBEAM HAS CORROSION. REMOVED CORRODED FLOORBEAM & INSTALLED NEW BEAM PER SRM 51-72-11; CORR TASK JA-220-53500; DEFECT SIZE: 1 X 1 INCH.

Part: SKIN — CORRODED (FUSELAGE)

CORRODED RIVET TAILS WERE FOUND IN THE FUSELAGE FORWARD CARGO COMPARTMENT BETWEEN FRAME 26 TO 35.7 STRINGER 38R TO 38L. APPROXIMATELY 217 RIVETS WERE REPLACED. A RESIDUE OF SODIUM CHLORIDE ATTACKED THE RIVETS. NUMEROUS OTHER RIVETS HAD THE PAINT FLAKING OFF THE RIVET TAILS THAT WERE CLEANED AND HAD PRIMER AND PAINT REAPPLIED. AIRCRAFT WAS MFG 31 JANUARY 2002. (K)

Part: BRAKE — MALFUNCTIONED (LANDING GEAR)

EN-ROUTE, THE CREW REPORTED THAT THE BRAKES WERE VERY SPONGY AND THAT THE AIRCRAFT WAS HARD TO STOP. THE FLIGHT PARKED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE BRAKES. NO FAULTS WERE FOUND.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

BDL - FOUND THE EMERGENCY POWER SUPPLY UNIT BATTERY WEAK AT THE R3 DOOR LOCATION. MAINTENANCE REPLACED THE BATTERY FOR THE EMERGENCY POWER SUPPLY UNIT AT THE R3 DOOR LOCATION. (M)

Part: BATTERY — WEAK (EMERGENCY LIGHT)

BDL - FOUND THE EMERGENCY POWER SUPPLY UNIT BATTERY WEAK AT THE L3 DOOR LOCATIONS. MAINTENANCE REPLACED THE BATTERY FOR THE EMERGENCY POEWR SUPPLY UNIT AT THE L3 DOOR LOCATION. (M)