N9026C

Part: WIRE — BROKEN (ZONE 200) · airframe 29,746 hrs · 13,965 cycles

AIRCRAFT WAS NOT GROUNDED, 23C SEAT MOUNTED EMERGENCY PATH LIGHTING INOPERATIVE. FOUND BROKEN AND EXPOSED WIRE BY THE LOWER SIDEWALL PANEL. MAINTENANCE REPAIRED WIRE BETWEEN SEATS 22C AND 23C IAW ESPM 20-43-11.

Part: WIRE — BROKEN (ZONE 200) · airframe 29,746 hrs · 13,965 cycles

AIRCRAFT WAS NOT GROUNDED: 22C SEAT MOUNTED EMERGENCY PATH LIGHTING INOP. MAINTENANCE REPAIRED WIRE BETWEEN SEAT 22C AND 23C IAW ESPM 20-43-11 .

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 29,201 hrs · 13,663 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK ESPU SYS TEST FAILED. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY IAW AMM 33-51-38.

Part: CONNECTOR — DISCONNECTED (ZONE 200) · airframe 28,209 hrs · 13,131 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 21C EMERGENCY LIGHT INOP. FOUND WALL CONNECTOR OFF, RECONNECTED CONNECTOR, SEAT 21C EMERGENCY LIGHT OPS NORMAL REF AMM 33-50-00.

Part: CONNECTOR — DISCONNECTED (ZONE 200) · airframe 28,209 hrs · 13,131 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 20 C EMERGENCY LIGHT INOP. MAINTENANCE FOUND WALL CONNECTOR OFF, RECONNECTED CONNCTOR, SEAT 20C EMERGENCY LIGHT OPS NORMAL, REF AMM 33-50-00.

Part: CONTAINMENT BAG — MISSING (ZONE 200) · airframe 28,188 hrs · 13,121 cycles

AIRCRAFT WAS NOT GROUNDED: FIRE CONTAINMENT BAG MISSING FWD CABIN. MAINTENANCE INSTALLED FIRE BAG.

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 27,902 hrs · 12,973 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD MEGAPHONE INOP. MAINTENANCE REPLACED FORWARD MEGAPHONE IAW AMM TASK 25-65-51-920-001-A.

Part: LUG — WORN (ZONE 500) · airframe 27,792 hrs · 12,919 cycles

AIRCRAFT IN BASE MAINTENANCE: WEAR DAMAGE AT L/H MLG RIB 5 FWD LUG AFT BUSHING. MAINTENANCE AVOOMPLISHED TIME LIMITED REPAIR ON L/H WING MLG RIB 5 FWD LUG IAW EA360762.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 27,745 hrs · 12,898 cycles

AIRCRAFT WAS NOT GROUNDED: DURING SLIDE CHANGE EPSU BATTERY FAILED TEST. MAINTENANCE REPLACED EPSU BAT PER AMM 33-51-38.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 25,101 hrs · 11,519 cycles

AIRCRAFT WAS NOT GROUNDED: MIA-CLT DIVERTED TO MCO ACCOUNT OF MAINTENANCE, POSSIBLE FUEL LEAK ON CLIMB ABOUT FL280, FUEL F USED FOB DISAGREE FUEL LEAK PROC APPLY. FLIGHT DECLARED EMERGENCY AND WAS NOT OVERWEIGHT FOR LANDING. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO GATE UNDER OWN POWER. FOUND NO FAULTS AT THIS TIME. ALL FUEL INDICATORS AND LEVELS NORMAL.

Part: LIFE VEST — OPEN (ZONE 200 - FUSE) · airframe 23,894 hrs · 10,861 cycles

AIRCRAFT WAS NOT GROUNDED: CAPTAINS LIFE VEST POUCH HAS BEEN OPENED. MAINTENANCE REPLACED LIFE VEST PER AMM 25-62-00.

Part: LANYARD — OUT OF POSITION (ZONE 800 - DOORS) · airframe 23,542 hrs · 10,682 cycles

AIRCRAFT WAS NOT GROUNDED: ON WALK AROUND DISCOVERED APROXIMATE 6 INCH GREEN ROPE WITH A LOOP ON THE END OUTSIDE THE AIRCRAFT AT 2L DOOR. MAINTENANCE INSTALLED L2 DOOR SLIDE LANYARD PER AMM 25-62-44.

Part: WEB — OUT OF POSITION (ZONE 800 - DOORS) · airframe 23,543 hrs · 10,682 cycles

AIRCRAFT WAS NOT GROUNDED: GROUND PERSONEL NOTIFIED FLIGHT CREW THAT A STRAP WAS HANGING OUT OF THE LEFT AFT DOOR AFTER CATERING DEPARTED. IT APPEARS TO BE DETACHED FROM THE SLIDE. MAINTENANCE RESECURED THE GIRT BAR WEBBING PER AMM 25-62-44

Part: SLIDING WINDOW — OUT OF ADJUST (ZONE 200 - FUSE) · airframe 23,401 hrs · 10,601 cycles

AIRCRAFT WAS GROUNDED: FIRST OFFICERS SLIDING WINDOW DIFFICULT TO OPEN. MAINTENANCE ADJUSTED SLIDING WINDOW LATCHES PER AMM 56-12-11. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: WIRE HARNESS — DEFECTIVE (EMERGENCY LIGHTS) · airframe 22,394 hrs · 10,096 cycles

AIRCRAFT WAS NOT GROUNDED: ESCAPE PATH SEAT MOUNTED LIGHT AT SEAT ROWS 11 AND 12 INOPERATIVE. MAINTENANCE REPLACED ESCAPE PATH LIGHT HARNESS AT SEAT ROW 11 AND 12 PER AMM 33-51-18. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: HINGE PIN — CORRODED (ZONE 700 - GEARS) · airframe 21,634 hrs · 9,749 cycles

AIRCRAFT WAS GROUNDED: DURING INSPECTION OF NOSE LANDING GEAR TORQUE LINK ASSEMBLY, FOUND CENTER HINGE PIN WITH CORROSION ON THREADS. MAINTENANCE REPLACED CENTER HINGE PIN PER AMM 32-21-27.

Part: POWER SUPPLY — NONE (ZONE 200 - FUSE) · airframe 21,311 hrs · 9,571 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PERIODIC SERVICE CHECK EMERGENCY LIGHTS EMERGENCY POWER SUPPLY UNIT TEST FOUND BATTERY/ EMERGENCY POWER SUPPLY UNIT 13WL AFT LEFT CLASS 1 MESSAGE. REPLACED EMERGENCY POWER SUPPLY UNIT 13WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 21,114 hrs · 9,478 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT INOPERATIVE AT ROW 11 A,B AND C. REPLACED POWER SUPPLY UNIT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-21-38

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 18,292 hrs · 8,256 cycles

AIRCRAFT WAS NOT GROUNDED: ROWS 11, 20, 21, 24 AND 25 EMERGENCY LIGHTS OUT. REMOVED AND REPLACED NUMBER 2 EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 18,065 hrs · 8,161 cycles

AIRCRAFT WAS GROUNDED: WHEN PERFORMING EMERGENCY LIGHT TEST PER PS CHECK- CIDS 1 EPSU SYST TEST BAT/EPSU (11WL) EMER L FAULT IS DISPLAYED. REPLACED EMERGENCY POWER SUPPLY INIT 11WL(AALA202108278020) AND BATTERY PACK (AALA202108271828) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 18,065 hrs · 8,161 cycles

AIRCRAFT WAS GROUNDED: WHEN PERFORMING EMERGENCY LIGHT TEST PER PS CHECK- CIDS 1 EPSU SYST TEST BAT/EPSU (11WL) EMER L FAULT IS DISPLAYED. REPLACED EMERGENCY POWER SUPPLY INIT 11WL(AALA202108278020) AND BATTERY PACK(AALA202108271828) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: FILLER — DEBONDED (LT WING TE FLAP) · airframe 17,822 hrs · 8,053 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING OUTBOARD TRAILING EDGE FLAP , TRAILING EDGE FILLER CRACKED AND DISBONDED 109 INCHES FROM THE INBOARD EDGE. REPAIRED FLAP PER EA 329040A.

Part: FUEL FILTER — CLOGGED (NR 1 ENGINE) · airframe 16,993 hrs · 7,716 cycles

AIRCRAFT WAS GROUNDED: AIRCRAFT RETURNED TO DFW DUE TO A #1 ENGINE FUEL FILTER CLOG MESSAGE. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED #1 ENGINE FUEL FILTER (AALA202104139006) PER TASK CARD 26C40073001 AND FUEL FILTER DIFFERENTIAL PRESSURE SWITCH (AALA202104139007) PER AMM 73-34-15-400-041-A. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLSIHED.

Part: SWITCH — FAULTED (FUEL FILTER) · airframe 16,993 hrs · 7,716 cycles

AIRCRAFT WAS GROUNDED: AIRCRAFT RETURNED TO DFW DUE TO A #1 ENGINE FUEL FILTER CLOG MESSAGE. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED #1 ENGINE FUEL FILTER (AALA202104139006) PER TASK CARD 26C40073001 AND FUEL FILTER DIFFERENTIAL PRESSURE SWITCH (AALA202104139007) PER AMM 73-34-15-400-041-A. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLSIHED.

Part: DAMPER — FAILED (PAX DOOR DAMPER) · airframe 15,934 hrs · 7,264 cycles

AIRCRAFT IN BASE MAINTENANCE. PASSENGER CREW DOOR 831 AT FORWARD GALLERY AREA DAMPING FUNCTION DOESN`T PASS OPERATIONAL TEST. REPLACED DOOR DAMPER AT CREW DOOR 831, IAW AMM 52-11-14-400-001-B.

Part: SLIDE — DEFORMED (GALLEY DOOR) · airframe 15,934 hrs · 7,264 cycles

AIRCRAFT IN BASE MAINTENANCE. DEFORMATION SLIDE RAFT PASSENGER CREW DOOR 841 AT FORWARD GALLEY AREA. REPLACED SLIDE RAFT PASSENGER CREW DOOR 841 AT FORWARD GALLEY AREA.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 15,934 hrs · 7,264 cycles

AIRCRAFT IN BASE MAINTENANCE. FOUND EXCESSIVE PLAY BEARING HINGE ARM 4 ELEVATOR ON RIGHT HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NR 4 ON RIGHT HORIZONTAL STABILIZER, IAW AMM 55-16-42-400-001-A STEP 4B AND AMM 55-16-42-000-001-A.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 15,934 hrs · 7,264 cycles

AIRCRAFT IN BASE MAINTENANCE. FOUND EXCESSIVE PLAY BEARING HINGE ARM 3 ELEVATOR ON RT HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NR 3 ON RT HORIZONTAL STABILIZER, IAW AMM 55-16-42-000-001-A AND 55-16-42-400-001-A STEP 4A AND 5A.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 15,934 hrs · 7,264 cycles

AIRCRAFT IN BASE MAINTENANCE. FOUND EXCESSIVE PLAY BEARING HINGE ARM 1 ELEVATOR ON RT HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NR 1 ON RT HORIZONTAL STABILIZER, IAW AMM 55-16-42-000-001-A AND 55-16-42-400-001-A STEP 4A AND 5A.

Part: HINGE ARM — EXCESS PLAY (RT ELEVATOR) · airframe 15,934 hrs · 7,264 cycles

AIRCRAFT IN BASE MAINTENANCE. FOUND EXCESSIVE PLAY BEARING HINGE ARM 2 ELEVATOR ON RT HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING NR 2 ON RT HORIZONTAL STABILIZER, IAW AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 15,934 hrs · 7,264 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY IN RT ELEVATOR HINGE ARM NR 6 FITTING. REPLACED HINGE FITTING WITH NEW, IAW AMM 55-16-42-400-001-A.

Part: LIFE RAFT — DEFORMED (GALLEY) · airframe 15,934 hrs · 7,264 cycles

AIRCRAFT IN BASE MAINTENANCE. FOUND DEFORMATION OF SLIDE RAFT AT PASSENGER/CREW DOOR IN FORWARD GALLEY AREA. REPLACED SLIDE RAFT.

Part: HINGE FITTING — EXCESS PLAY (RT ELEVATOR) · airframe 15,934 hrs · 7,264 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY IN RT ELEVATOR HINGE ARM NR 5 FITTING. REPLACED HINGE FITTING WITH NEW, IAW AMM 55-16-42-400-001-A.

Part: SHEAR PLATE — CRACKED (FRAMES 69-70) · airframe 15,758 hrs · 7,163 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK IN SHEAR PLATE BETWEEN FR 69 AND FR 70 AT STR 23L, MEASURING L=1.000 IN. REPLACED SHEAR PLATE WITH MODIFIED PART, IAW A319 SRM 51-72-11-911-001 AND 51-42-11-801 AND DRAWING D53475180.

Part: FITTING — CORRODED (FRAME 67) · corrosion level 2 · airframe 15,934 hrs · 7,264 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT LEFT HAND PASSENGER/CREW DOOR CUT OUT LOWER SILL CENTER FITTING AT FR 67 AND S23L. REPLACED CENTER FITTING, PER SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FRAMES 69-70) · airframe 15,934 hrs · 7,264 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN SHEAR PLATE BETWEEN FR 69 AND FR 70 AT STR 23R, MEASURING L=0.634 IN. REPLACED SHEAR PLATE WITH NEW, IAW SRM A319 51-42-11-801 AND 51-72-11-911-001 AND DRAWING D53474180.

Part: SLIDE — WARNING LIGHT · airframe 15,855 hrs · 7,218 cycles

AIRCRAFT WAS GROUNDED: CABIN INTERCOMMUNICATION DATA SYSTEM 1 TEST SHOW 13WL L AFT SLIDE/LIGHT. REMOVED AND REPLACED L4 DOOR SLIDE RAFT.

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 14,788 hrs · 6,689 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD GALLEY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED GALLEY FLASHLIGHT PER AMM 25-65-00.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 14,545 hrs · 6,578 cycles

AIRCRAFT WAS GROUNDED: AT CRUISE 370 ECAM MESSAGE FUEL F USED / FOB DISAGREE WENT TO FUEL LEAK PRO C. DETERMINED FUEL LEAK UNLIKELY, PROBLEM WITH FUEL INDICATION. PRECAUTINARY LANDING AT IAH, EMERGENCY DECLARED. 0 LEFT MAIN TANK WAS LOWEST INDICATION.

Part: BATTERY — DISCHARGED (CABIN) · airframe 13,533 hrs · 6,098 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT BATTERY (10WL) FAILED PS BITE CHECK. MAINTENANCE LIGHT BATTERY PER MM 33-51-38.

Part: BATTERY — FAILED (CABIN) · airframe 13,533 hrs · 6,098 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT BATTERY (11WL) FAILED PS BITE CHECK. MAINTENANCE LIGHT BATTERY PER MM 33-51-38.

Part: HINGE FITTING — WORN (RUDDER) · airframe 12,342 hrs · 5,549 cycles

AIRCRAFT WAS GROUNDED: RUDDER NR 7 HINGE FITTING BEARING WORN. REPLACED HINGE FITTING PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 12,342 hrs · 5,549 cycles

AIRCRAFT WAS GROUNDED: RIGHT HAND ELEVATOR NR 4 HINGE FITTING BEARING IS CORRODED AND WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RUDDER) · airframe 12,342 hrs · 5,549 cycles

AIRCRAFT WAS GROUNDED: RUDDER NR 4 HINGE FITTING BEARING WORN. REPLACED HINGE FITTING PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 12,342 hrs · 5,549 cycles

AIRCRAFT WAS GROUNDED: RUDDER NR 1 HINGE FITTING BEARING WORN. REPLACED HINGE FITTING PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 12,342 hrs · 5,549 cycles

AIRCRAFT WAS GROUNDED: RUDDER NR 2 HINGE FITTING BEARING WORN. REPLACED HINGE FITTING PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 12,342 hrs · 5,549 cycles

AIRCRAFT WAS GROUNDED: RUDDER NR 3 HINGE FITTING BEARING WORN. REPLACED HINGE FITTING PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 12,342 hrs · 5,549 cycles

AIRCRAFT WAS GROUNDED: RUDDER NR 5 HINGE FITTING BEARING WORN. REPLACED HINGE FITTING PER AMM 55-36-41.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 12,342 hrs · 5,549 cycles

AIRCRAFT WAS GROUNDED: LEFT HAND ELEVATOR NR 4 HINGE FITTING BEARING IS CORRODED AND WORN. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 10,743 hrs · 4,829 cycles

R2 DOOR AFT LOWER EMERGENCY EXIT SIGN WAS BROKEN. REPLACED THE SIGN IAW AMM 33-51-13.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 10,743 hrs · 4,829 cycles

R1 DOOR FORWARD LOWER EMERGENCY EXIT SIGN WAS BROKEN. REPLACED THE SIGN IAW AMM 33-51-13.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 10,719 hrs · 4,811 cycles

EMERGENCY LIGHT POWER SUPPLY SYSTEM TEST, CIDS 1 FAILED FOR THE BATTERY ON EMERGENCY POWER SUPPLY UNIT 12WL. MAINTENANCE REPLACED THE BATTERY IAW AMM 33-51-38 AND 33-51-38-000-002-A.

Part: BOTTLE — LOW PRESSURE (DOOR) · airframe 10,122 hrs · 4,541 cycles

FORWARD RIGHT ENTRY DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. SERVICED ENTRY DOOR DAMPER AND EMERGENCY OPERATION CYLINDER TO CORRECT PRESSURE IAWAMM 52-10-00.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 6,163 hrs · 2,812 cycles

EMERGENCY POWER SUPPLY UNIT 12WL FAILS SYSTEM TEST. REPLACED EMERGENCY POWER SUPPLY UNIT 12WL IAW AMM 33-51-38 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: UNKNOWN — VIBRATION · airframe 5,504 hrs · 2,502 cycles

AFTER TAKEOFF, A LOUD RUMBLING NOISE AND VIBRATION OCCURRED. PASSENGERS FELT VIBRATION IN MIDDLE OF AIRCRAFT AND REPORTED WATER DRIPPING FROM AIR CONDITIONING OUTLETS. ACCOMPLISHED TSM 05-50-00-810-801 AND 53-35-00-810. EMERGENCY DECLARED.AIRCRAFT WAS GROUNDED. RETURNED TO DEPARTURE UNEVENTFUL LANDING. INSPECTED WING TO BODY FAIRING SEALS, LEFT/RIGHT PACK BAYS, RECIRCULATION FANS, FLAPS/FAIRINGS LEFT/RIGHT WING, BOTH WHEEL WELLS, ALL COMPONENTS CHECKED OK. OPERATIONAL CHECKED GOOD.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 5,485 hrs · 2,493 cycles

EMERGENCY POWER SUPPLY UNIT FAILED CIDS TEST AT 10WL. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 10WL BATTERY IAW AMM 33-51-38. OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 5,251 hrs · 2,392 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT AT 11WL FAILED CIDS TEST. REMOVED AND REPLACED POWER SUPPLY BATTERY IAW AMM 33-51-38. SYSYTEM CHECKED NORMAL.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 4,069 hrs · 1,865 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY POWER SUPPLY UNIT 10WL FAILED DURING TEST. R & R POWER SUPPLY IAW AMM 31-51-00. OPS CHECK NORMAL.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 408 hrs · 193 cycles

AIR INTERRUPT, RETURNED, EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, BEGAN FEELING CABIN PRESS FLUCTUATIONS ACCOMPANIED BY LOUD SQUEAL FROM RT AFT OF ACFT THAT INCREASED WITH ALTITUDE. R & R OUTFLOW VLV ASSEMBLY IAW AMM 21-31-51. ACCOMPLISHED OPERATIONAL TEST IAW AMM 21-31-00. SYS CHECKED NORMAL.

Part: TARGET — OUT OF ADJUST (CARGO DOOR) · airframe 152 hrs · 71 cycles

AIR INTERRUPT, RETURNED, AN EMER NOT DECLARED. LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB AFT CARGO DOOR OPEN LIGHT ILLUMINATED. VERIFIED AFT CARGO DOOR CLOSED & LOCKED. ACCOMPLISHED TSM 52-32-00 & FOUND SENSOR 32WV TARGET GAP OUT OF LIMITS. ADJUSTED TARGET GAP IAW AMM 52-71-00. SYS CHECKED NORMAL.