N332CK

Part: CONNECTOR — BROKEN (CABIN PRESSURE) · airframe 75,906 hrs · 46,644 cycles

CABIN ALTITUDE WARNING HORN AND LIGHT CAME ON DURING FLIGHT @ FL 360. LEFT BLEED WAS SHOWING 12 PSI AND RIGHT BLEED WAS SHOWING 38 PSI. REMOVED AND REPLACED CONNECTOR D1208 IAW SWPM 20-61-11. PERFORMED ENGINE RUN IAW AMM 71-00-00. EGT SYSTEM OPS CHECKS GOOD IAW AMM 77-21-00. NO DEFECTS NOTED.

Part: CABIN PRESSURE — FAULTED · airframe 75,906 hrs · 46,644 cycles

CABIN ALTITUDE WARNING HORN AND LIGHT CAME ON DURING FLIGHT @ FL 360. LEFT BLEED WAS SHOWING 12 PSI AND RIGHT BLEED WAS SHOWING 38 PSI.

Part: CONTROLLER — DEFECTIVE (CABIN PRESSURE) · airframe 75,820 hrs · 46,603 cycles

WHILE ON DESCENT LOST CABIN PRESSURE AT 33,000 FEET MADE EMERGENCY DECENT BOTH PACKS OPERATED NORMAL NO PACK TRIP. CORRECTIVE ACTION: REMOVED AND REPLACED CABIN PRESSURE CONTROLLER OPS CHECK GOOD.

Part: CABIN PRESSURE — FAILED

WHILE ON DECENT LOST CABIN PRESSURE AT 33,000 FEET MADE EMERGENCY DECENT BOTH PACKS OPERATIONAL NORMAL NO PACK TRIP.

Part: SENSE LINE — UNSECURE (ADC) · airframe 75,756 hrs · 46,573 cycles

AIRSPEED INDICATOR F/O SIDE ROSE TO 62 KTS AND STOPPED. FAILED 80 KTS CHECK. CORRECTIVE ACTION: RESECURED FIRST OFFICERS AIR DATA COMPUTER Q.D. SENSE LINE IAW B737 AMM 34-12-11. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,751 hrs · 46,568 cycles

DURING CLIMB ENGINE 1 WOULD NOT ACHIEVE COMMAND POWER SETTING AFTER INITIAL THRUST REDUCTION FROM TAKEOFF POWER ENGINE 1N HUNG BELOW 70% WHILE N2 INCREASED TO LIMITS.

Part: NONE — NONE · airframe 74,639 hrs · 45,785 cycles

PROBLEM DESCRIPTION: RIGHT PACK TRIP UNABLE TO CONTROL CABIN PRESSURE UNTIL 10,000 FEET. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: REMOVED DEBRIS FROM AFT PIT DOOR, PERFORMED CABIN PRESSURIZATION CHECK IAW B737 AMM 21-31-00 OPS CHECK GOOD NO DEFECTS NOTED

Part: CONTROLLER — INTERMITTENT (CABIN PRESSURE) · airframe 74,300 hrs · 45,563 cycles

INTERMITTENT CONTROL OF PRESSURIZATION. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: R&R CABIN PRESSURE CONTROL PANEL IAW B737 AMM 21-31-21 OPS CHECK GOOD IAW B737 AMM 21-31-00 NO DEFECTS NOTED

Part: UNKNOWN — VIBRATION · airframe 73,787 hrs · 45,201 cycles

DURING FUNCTIONAL FLIGHT FOR FLAP REMOVAL EXPERIENCED HIGH FREQUENCY BUFFET CLIMBING THROUGH FL 240 @ 280 KIAS, CLEAN WING. INSPECTED AND OPS CHECK TRAILING EDGE FLAPS, LEADING EDGE FLAPS AND KRUEGER FLAPS IAW AMM 27-51-00, 27-81-00 NO DEFECTS NOTED. AIRCRAFT PASSED FUNCTIONAL EVAL FLIGHT ON NEXT FLIGHT AND HAS FLOWN 20 HOURS AND 17 CYCLES SINCE THIS CLEARING ACTION

Part: WINDOW — CRACKED (L5) · airframe 73,463 hrs · 44,994 cycles

L5 WINDOW CRACKED IN FLIGHT. AIRCRAFT RETURNED TO KSAT. R & R L5 WINDOW, IAW AMM 56-11-31.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,325 hrs · 44,925 cycles

SKIN DAMAGED STA 1080 FWD OF APU ACCESS DOOR

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 73,325 hrs · 44,925 cycles

AT STA 291.5 STR 14R R1 DOOR LOWER HINGE CUTOUT HAS CRACK INDICATION

Part: FITTING — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 73,325 hrs · 44,925 cycles

LT HORIZONTAL STAB FWD LOWER FITTING CORRODED

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 73,325 hrs · 44,925 cycles

AT STATION 277-360 STR 20L OUTER "T" CHORD IS CRACKED

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,325 hrs · 44,925 cycles

MAIN DECK FLOOR BEAM STA 312 LBL 12 HAS CORROSION AT INTERSECTION

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,325 hrs · 44,925 cycles

R/H TORQUE BOX STRINGER STA 1088-1156 IS CORRODED

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,325 hrs · 44,925 cycles

R/H TORQUE BOX STRINGER STA 1088-1130 IS CORRODED

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 73,325 hrs · 44,925 cycles

L/H WING @ THE MAIN LANDING GEAR SUPPORT BEAM SUPPORT FITTING REAR SPAR STA 224.14 @ UPPER CHORD CRACKED INDICATION

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,325 hrs · 44,925 cycles

CRACK INDICATION AT STA 500 = 11" STR 14R

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 73,325 hrs · 44,925 cycles

CRACK FOUND ON STIFFNER RBL 6.15 ON THE WING CENTER SECTION REAR SPAR

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 73,325 hrs · 44,925 cycles

CRACK FOUND ON STIFFNER LBL 6.15 ON THE WING CENTER SECTION REAR SPAR

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 73,325 hrs · 44,925 cycles

RIGHT WING AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM IS CRACKED

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 73,325 hrs · 44,925 cycles

LEFT WING AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM IS CRACKED

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,325 hrs · 44,925 cycles

AT STA 636-663 LBL 60MAIN DECK SEAT TRACK HAS AREAS OF CORROSION

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 73,325 hrs · 44,925 cycles

BS 639 RBL 45.5 WL 204 FLLORBEAM WEB CRACKED @ 2 LOWER FASTER HOLES

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 73,325 hrs · 44,925 cycles

CUSP WEB CRACKED FWD OF BS 639 RBL 70

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 73,325 hrs · 44,925 cycles

CUSP WEB CRACKED AFT OF BS 616 LBL 64 & LBL 70

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 73,325 hrs · 44,925 cycles

CUSP WEB CRACKED FWD OF BS 639 LBL 70

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 73,325 hrs · 44,925 cycles

CUSP WEB CRACKED AFT OF BS 616 RBL 64

Part: SPAR — GOUGED (ZONE 300) · airframe 73,325 hrs · 44,925 cycles

R/H I/B AFT UPPER SIDE OF FRONT SPAR CHORD LUG HAS GOUGED AREAS AROUND WASHER

Part: SPAR — GOUGED (HORIZ STAB) · airframe 73,325 hrs · 44,925 cycles

L/H I/B UPPER SIDE OF FRONT SPAR CHORD LUG HAS GUAGED AREAS AROUND WASHER (HORIZONTAL STAB)

Part: FRAME — CRACKED (FUSELAGE) · airframe 73,325 hrs · 44,925 cycles

R/H FRAME @ STA 500B HAS A CRACK IN THE INBD SIDE OF POWER CABLE HOLE BETWEEN S-20 & S-21

Part: SKIN — CRACKED (SERVICE DOOR) · airframe 73,325 hrs · 44,925 cycles

FWD GALLEY SERVICE DOOR FWD UPPER CORNER HAS CRACKS COMING FROM FASTENER HOLE WITH ENDS OF CRACKS MARKED

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 73,325 hrs · 44,925 cycles

LEFT WING UPPER SURFACE WBL 72 APPROX S-19C HAS CORROSION