N734CK

Part: SENSOR — OUT OF LIMITS (PITCH TRIM) · airframe 55,205 hrs · 37,225 cycles

DURING CLIMB SOON AFTER REACHING 1000 FT CLIMB AGL FEEL DIFF PRESS AND SPEED TRIM FAIL ANNUNCIATOR LIGHTS ILLUMINATED, ELEVATOR CONTROL WAS MARGINALLY HEAVY, AND AUTO PILOT WOULD NOT MAINTAIN PITCH CONTROL. : R&R ELEVATOR FEEL COMPUTER IAW B737 AMM 22-31-37 PARA 2A AND 27-31-37 PARA 3 G (11) AND B737 AMM 27-31-00 PARA 16A THROUGH AND INCLUDING 27-31-00 PARA 16 F (4)(D). R&R ELEVATOR FEEL POSITION SENSOR IAW B737 AMM 22-11-30.

Part: FLAP SYSTEM — FAULTED · airframe 55,180 hrs · 37,201 cycles

PROBLEM DESCRIPTION: TRAILING EDGE FLAP ASYMMETRY LEFT FLAP INDICATE UP & RIGHT FLAP INDICATES L1, SLATS DID NOT EXTEND WHEN FLAP HANDLE WAS MOVED TO #1 DETENT. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: FOUND #3 FLAP TRANSMISSION TORQUE TUBE COUPLING DISENGAGED. INSPECTED TORQUE TUBE IAW B737 AMM 27-51-00. RE-ENGAGED AND SECURED TORQUE TUBE COUPLING IAW B737 AMM 27-57-64, PERFORMED OPS CHECK OF TRAILING EDGE FLAP SYSTEM IAW B737 AMM 27-51-00 OPS CHECK GOOD.

Part: TIE DOWN — CRACKED (BS 727D) · airframe 54,824 hrs · 36,867 cycles

AFT CARGO COMPARTMENT B.S 727D RBL 14 HAS CRACK ON TRACK TIE DOWN LWR LEG.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 54,824 hrs · 36,867 cycles

LH WING IB AFT FLAP IB SECTION HAS DELAMINATION.

Part: TORQUE BOX — CORRODED (BS 1104) · airframe 54,824 hrs · 36,867 cycles

EVIDENCE OF CORROSION ON UPPER WEB AROUND NUTPLATES AT APROX STA 1104 INSIDE LH TORQUE BOX.

Part: TIE DOWN — CORRODED (BS 727D) · corrosion level 2 · airframe 54,824 hrs · 36,867 cycles

AFT CARGO COMPARTMENT AT B.S. 727D RBL 14, EVIDENCE OF CORROSION AT CARGO TIE DOWN.

Part: UNKNOWN — CORRODED (NR 2 NACELLE) · airframe 54,824 hrs · 36,867 cycles

#2 PYLON HAS EVIDENCE OF CORROSION ON TOP SIDE

Part: SKIN — CORRODED (NR 1 NACELLE) · airframe 54,824 hrs · 36,867 cycles

#1 PYLON HAS EVIDENCE OF CORROSION ON TOP SIDE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,418 hrs · 36,491 cycles

DURING FLIGHT LE FLAP TRANSIT LIGHT ILLUMINATED (#5 LE LIGHT)

Part: STRUCTURE — HANDLER ERROR · airframe 54,144 hrs · 36,226 cycles

DURING TAXI AT KCVG THE AIRCRAFT DEPARTED THE PAVED SURFACE. DURING RECOVERY THE AIRCRAFT WAS DAMAGED BY SUPPORT EQUIPMENT. DAMAGE IS LOCATED ON THE AFT FUSELAGE JUST FORWARD OF THE AFT LOWER CARGO DOOR. CORRECTIVE ACTION FOR THE REPAIR WILL BE LOGGED AFTER THE COMPLETION OF THE REPAIRS AS A STRUCTURAL DAMAGE REPORT.

Part: TRANSCEIVER — INOPERATIVE (ZONE 100) · airframe 53,360 hrs · 35,587 cycles

PROBLEM DESCRIPTION: NUMBER 1 VHF COM NOT TRANSMITTING. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: SWAPPED #1 AND #2 VHF COM R/T IAW KCII GMM CHAPTER 1, TRANSFERRED TO DMI # 73400055 IAW KCII B737 MEL 23-3A CAT C DUE 11-19-2021 PLACARDS INSTALLED. REF CLEARING OF DMI #73400055. CLEARED ON LOG PAGE 737-001-5676 R&R VHF R/T IAW B737 AMM 23-21-21 OPS CHECK GOOD IAW B737 AMM 23-21-01 THIS CLEARS DMI 73400055 PLACARDS REMOVED.

Part: DOOR — OUT OF ADJUST (ZONE 100) · airframe 53,275 hrs · 35,514 cycles

UNABLE TO PRESSURIZE IN AUTO OR STANDBY. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: FOUND AFT CARGO DOOR SLIGHTLY OPEN, ADJUSTED AFT CARGO DOOR IAW B737 AMM 53-11-00. CARGO DOOR CHECK GOOD, PERFORMED OPS CHECK AND LEAK CHECK OF PRESSURIZATION SYSTEM IAW B737 AMM 21-31-00, NO DEFECTS NOTED

Part: TRANSPONDER — MALFUNCTIONED (CO PILOT'S) · airframe 52,664 hrs · 34,928 cycles

CO PILOT STATIC INSTRUMENT AS WELL AS TRANSPONDER FAILED ON TAKEOFF. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: PERFORMED OPERATIONS CHECK OF THE NR 2 EFIS SYSTEM, IRU SYSTEM, DADC AND ATC SYSTEM, IAW B737 AMM 34-22-00, 34-28-01, 34-12-01 AND 34-53-02. ALL SYSTEMS OPERATIONS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: INDICATOR — FAILED (FLAP POSITION) · airframe 52,587 hrs · 34,882 cycles

FLAPS FAILED TO EXTEND PAST 15 DEGREES ON LANDING APPROACH. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: R & R TRAILING EDGE FLAP POSITION INDICATOR, IAW B737 AMM 27-58-41. ALL OPERATIONS CHECKS GOOD NO DEFECTS NOTED.

Part: SKIN — CORRODED (BS 986-1006) · corrosion level 2 · airframe 52,308 hrs · 34,675 cycles

DRAIN MAST MATING SKIN SURFACE HAS CORROSION @ #2 & #4 MOUNTING HOLES LOCATED @ STA 986 - 1006 BETWEEN STR 26L & 25L

Part: MEC — FAILED (NR 1 ENGINE) · airframe 52,307 hrs · 34,674 cycles

DURING TAKEOFF, NR 1 ENGINE HIT 965 DEG. FOR 3 SECONDS UNTIL PULLED BACK. ENGINE WAS REMOVED AND SENT FOR A SHOP VISIT DURING SHOP VISIT, R & R THE EGT HARNESS, RERIGGED THE VSV, AND R & R THE MEC, ENGINE WAS REINSTALLED AND PAST ALL TESTS

Part: ENGINE — OVERTEMP (NR 1) · airframe 52,307 hrs · 34,674 cycles

DURING TAKEOFF NR 1 ENGINE HIT 965 DEG. FOR 3 SECONDS UNTIL PULLED BACK. PERFORMED VISUAL INSPECTION OF NR 1 ENGINE INLET AND EXHAUST, NO DEFECTS NOTED AND PERFORMED BORESCOPE INSPECTION OF THE HTP BLADES AND THE 1ST STAGE LPT BLADES IAW AMM 72-00-00, NO DEFECTS NOTED, A/C FOUND TO BE SUITABLE FOR NON-REVENUE FLIGHT TO OSC IAW AMM 72-00-00. FURTHER INSPECTION IN PROGRESS IN KOSC.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 522,138 hrs · 34,492 cycles

DURING A CHECK FOUND R1 & L1 DOOR EMERGENCY LIGHTING INOP

Part: PROXIMITY SWITCH — FAULTY (RT MLG) · airframe 51,784 hrs · 34,152 cycles

ON GEAR RETRACTION RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CORRECTIVE ACTION: R&R RIGHT MAIN GEAR UPLOCK PROXIMITY SWITCH IAW AMM 32-61-21, PERFORMED OPS CHECK AND GEAR SWING IAW AMM 32-61-21

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 51,766 hrs · 34,132 cycles

DURING CLIMB OUT AT 14,000 FT CABIN PRESSURE GOES TO 10,000 FT IN STAND BY AND AUTO MODES

Part: DAMPER — DAMAGED (RT MLG) · airframe 51,719 hrs · 34,094 cycles

UPON LANDING RIGHT HAND MAIN LANDING GEAR TORSION LINK BROKE, CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: R&R THE MAIN LANDING GEAR UPPER AND LOWER TORSION LINK, TORSION LINK PIN, LEFT HAND SHIMMY DAMPER, #3 & #4 MWA, #3 BRAKE LINE, #4 BRAKE LINE AND NUMBER 3 BRAKE. PERFORMED MAIN GEAR DAMPER TEST / INSPECTION, NO DEFECTS NOTED.

Part: CONNECTOR — LOOSE (SMOKE DETECTOR) · airframe 51,291 hrs · 33,658 cycles

ON CLIMB OUT AT 8000 FEET THE CAPT AND FO RED MAIN CARGO SMOKE ANNUNCIATOR LIGHTS ILLUMINATED ON THE BOTTOM FWD INSTRUMENT PANEL AS WELL AS THE NR 5 SMOKE DETECTOR LIGHT ON THE AFT OVERHEAD PANEL. CORRECTIVE ACTION: FOUND LOOSE CONNECTOR ON NR 5 MAIN DECK SMOKE DETECTOR. RE SECURED CONNECTOR, OPS CHECK GOOD IAW AEI MM 26-19-01, NO DEFECTS NOTED.

Part: SHIMMY DAMPENER — MISSING (LT MLG) · airframe 51,190 hrs · 33,556 cycles

UPON LANDING AT KCVG ON RUNWAY 09 AND AT THE TIME OF TOUCHDOWN THE AIRCRAFT SHOOK LEFT TO RIGHT AND PULLED TO THE RIGHT. POST FLIGHT INSPECTION FOUND LEFT MAIN LANDING GEAR SHIMMY DAMPENER MISSING AND TORSION LINK BROKEN AND DAMAGE TO THE HYDRAULIC LINES AND WHEEL ASSY. AIRCRAFT TAXIED UNDER ITS OWN POWER TO ITS PARKING LOCATION. AIRPORT CLOSED RUNWAY UNTIL A FOD CHECK WAS COMPLETED. REPAIR AND CORRECTIVE ACTION IN WORK AT THIS TIME.

Part: TURBINE BLADES — DAMAGED (NR 2 ENGINE) · airframe 50,901 hrs · 33,248 cycles

ON PRE-FLIGHT FOUND DAMAGE TO NR 2 ENGINE TURBINE BLADE. R&R NR 2 ENGINE IAW AMM 71-00-00.

Part: BATTERY PACK — LOW VOLTAGE (CABIN) · airframe 50,889 hrs · 33,234 cycles

EMERGENCY LIGHT FAIL FUNCTIONAL TEST, LT/RT EMERGENCY BATTERY PACKS

Part: SKIN — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 50,889 hrs · 33,234 cycles

#1 PYLON TOP SIDE APPROX NAC STA 240 HAS CORROSION

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,889 hrs · 33,234 cycles

FUSELAGE - FLIGHT CREW COMPARTMENT AT APPROX STA 250 LBL 48" EVIDENCE OF CORROSION (JD-50)

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,889 hrs · 33,234 cycles

EVIDENCE OF CORROSION ON AFT PIT FLOOR STRUCTURE AT STA 727A +10 LBL 15

Part: FLOOR SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,889 hrs · 33,234 cycles

EVIDENCE OF CORROSION ON AFT PIT FLOOR STRUCTURE AT STA 727G RBL 15

Part: SKIN — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 50,889 hrs · 33,234 cycles

NR 1 PYLON TOP SIDE APPROX NAC STA 220 HAS CORROSION, NR 1 PYLON AT W BL 190.00-193.50, NAC 196.84-201.34 (APPROX.) SKIN BLEND DOUBLER