PRIESTER AVIATION, LLC

Operated by Priester Aviation LLC (per NTSB report)

SIGHT AND SMELL OF SMOKE IN THE COCKPIT AND THE CABIN ON CLIMB OUT AT APPROX 3800 FT OUT OF KFFL. CREW DECLARED EMERGENCY AND RETURNED TO KFFL. LANDED WITH NO ISSUES. PASSENGERS OWNER PART 91 FLIGHT.

#4 MAIN WHEEL ASSEMBLY HEAT SHIELDS MISSING. THEY DEPARTED THE AIRCRAFT AND WERE FOUND ON THE APRON BY AIRPORT OPERATIONS.IN PELLSTON REGIONAL AIRPORT (KPLN)

ON ARRIVAL INTO HOU AFTER LEVELING AND THE THRUST LEVERS ADVANCING THE EICAS, AURAL WARNINGS, RH ENGINE FIRE PUSH, AND FIRE BOOTLE SWITCH LIGHTS ALL ILLUMINATED AND GAVE THE INDICATION OF THERE BEING A FIRE ON THE #2 ENGINE. RETARDING THE THRUST LEVERS CAUSED ALL FIRE ANNUNCIATIONS AND LIGHTS TO EXTINGUISH. THE TOTAL TIME FOR THE ALARMS WAS ROUGHLY 5 CONSTANT SECONDS. THE ENGINES SHOWED NO SIGNS OF ANYTHING TO CORROBORATE THE INDICATIONS. THE N1, ITT, N2, FUEL FLOW, OIL PRESSURE AND FAN VIBE INDICATORS WERE ALL INDICATING NORMAL AND SYMMETRICAL. THERE WAS NO CHANGE IN FLIGHT CHARACTERISTICS, FEEL, AUDIO CUES, OR SMOKE INDICATIONS. AN EMERGENCY WAS NOT DECLARED, AS WE WERE CLOSE TO LANDING AND THERE WERE NO INDICATIONS TO SUPPORT ANY EMERGENCY AS ALL NOTIFICATIONS AND WARNINGS HAD CLEARED. ON INITIAL INSPECTION OF THE RH ENGINE, FOUND THE GROUND WIRE TO THE LOWER HARNESS BROKEN OFF AT THE TERMINAL. REPAIRED BROKEN TERMINAL IAW SPM 20-16-20. GROUND RUN AND OPS CHECK GOOD.

CREW REPORTED A SLIGHT NOSE WHEEL SHIMMY ON LANDING - DURING TIRE REMOVAL FOUND A DE-BONDED RUBBER STRIP OF THE TIRE WAS LOOSE INSIDE THE WHEEL WAS TOLD THIS IS USED BY THE TIRE MANUFACTURE TO BALANCE THE TIRE DURING MANUFACTURING.

ENGINE FAILURE ON CLIMB PASSING FL270 THE RIGHT ENGINE FAILED. R CONT IGN WAS SELECTED IN ORDER TO ATTEMPT AN AUTOMATIC RELIGHT. NO RELIGHT. ENGINE WIND MILLING. NO OBVIOUS INDICATION ON WHY THE ENGINE FAILED. RETURNED TO BANGKOK, EXECUTED ENGINE SHUTDOWN IN FLIGHT NON NORMAL CHECKLIST IN ORDER TO PREVENT ANY POSSIBLE FURTHER DAMAGE TO THE ENGINE. SINGLE ENGINE LANDING WAS UNEVENTFUL.

UPON ESTABLISHING A POSITIVE RATE OF CLIMB, THE LANDING GEAR WAS RETRACTED. AT V2 PLUS 10 THE FLAPS WERE RETRACTED. AT WHICH POINT A STAB MISCOMPARE WAS NOTICED. WE REQUESTED A LEVEL OFF AT 8,000 FT. WE SLOWED THE AIRCRAFT TO BELOW 200 KNOTS. WE THEN NOTICED A GEAR UNLOCKED LIGHT ILLUMINATED. ALL THREE GEAR INDICATIONS WERE EXTINGUISHED. FOUND RIGHT HAND NOSE LANDING GEAR UP-LOCK ROLLER BRACKET ASSEMBLY BENT DOWN 1/10 OF INCH. REMOVED AND REPLACED BRACKET P/N 6642652-14 AND PERFORMED SATISFACTORY OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM. THIS BRACKET WAS KEEPING THE NOSE GEAR POSITION SWITCH FROM ACTIVATING THE CORRECT CONFIGURATION OF THE NOSE GEAR. SUSPECT IT WAS BENT DURING TOWING.

CABIN DUCT OVERHEAT INDICATION ILLUMINATED SHORTLY AFTER TAKE OFF FROM KJAX, RETURNED TO JAX FOR MAINTENANCE. FOUND THAT PN 27241287-14 CABIN TEMP CONTROL VALVE HAD FAILED. REPLACED VALVE AND RESUMED OPERATIONS THE FOLLOWING DAY.

CRUISE ALTITUDE FL410 ENG NR 1 COMPUTER LIGHT ILLUMINATED WITH SLIGHT RPM ROLLBACK. FOLLOWED CHECKLIST, RESETTING COMPUTER. 30 SECONDS LATER REPEAT OCCURRENCE. FOLLOWED CHECKLIST AGAIN AND CONTINUED FLIGHT WITH COMPUTER OFF AND IN MANUAL MODE. DECIDED TO LAND IN KPBI RATHER THAN PROCEEDING WITH A KNOWN MECHANICAL ISSUE.

CLIMBING THRU FL340 THE CABIN ALT WARNING ILLUMINATED WITH THE ASSOCIATED HORN. CREW DONNED OXYGEN MASKS & REQUESTED A LEVEL OFF, FOLLOWED BY AN IMMEDIATE DESCENT. EMER WAS DECLARED WITH CTR. CABIN NOTICES WERE TURNED ON & PAX OXYGEN MASKS AUTO DEPLOYED. ALL APPLICABLE CHECKLISTS WERE COMPLETED. ACFT LANDED SAFELY & NO PAXS WERE INJURED. PRESSURIZATION SYS WAS MEL'D IAW MEL 21-30-3. ACFT RETURNED FOR TROUBLESHOOTING OF PROBLEM. NO PAXS WERE ON THE RETURN LEG.

CLEARED DIRECT TO THE INITIAL APPROACH, SAW THE GPS UNIT DIM THEN GO BLACK. IMMEDIATELY AFTER, SMELLED A BURNING ODOR COMING FROM THE COCKPIT. IMMEDIATELY TURNED OFF THE UNIT AND DECLARED AN EMERGENCY WITH APPROACH CONTROL. ONCE POWER WAS REMOVED FROM THE UNIT, THE ODOR SLOWLY DISSIPATED. MADE A NORMAL LANDING AND TAXIED INTO THE RAMP. NO FIRE OCCURRED AFTER REMOVING POWER FROM THE UNIT.

ON INITIAL CLIMB OUT COPILOT RT SIDE WINDOW STARTED LEAKING. FLIGHT CREW STOPPED CLIMB TO DISCUSS OPTIONS. CREW DECIDED TO RETURN & HAVE WINDOW CHECKED. THIS WAS THE FIRST FLIGHT SINCE WINDOW WAS REPLACED. GND PRESSURIZATION WAS PERFORMED ON THE GND TO OPERATIONS CHECK THE WINDOW & IT DID NOT SHOW ANY SIGNS OF LEAKAGE. WHEN WINDOW RETAINER WAS REMOVED FOR INSPECTION, SOME OF THE SEALER DID NOT SET UP CORRECTLY. OLD SEALER WAS CLEANED OUT & WINDOW RESEALED.

AIRCRAFT HAD BAGGAGE SMOKE ANNUNCIATOR LIGHT ILLUMINATE DURING FLIGHT. PER CHECKLIST PROCEDURES CREW DECLARED EMERGENCY & LANDED AT WEST PALM BEACH. UPON LANDING FIRE DEPARTMENT WAS WAITING WITH HEAT DETECTORS TO CHECK FOR HOT SPOTS IN THE BAGGAGE COMPARTMENT. NO SMOKE OR HOT SPOTS DETECTED. VISUAL INSPECTION OF THE BAGGAGE AREA SHOWED NO SIGNS OF SMOKE OR FIRE. TROUBLE SHOT TO BAD SMOKE DETECTOR. REPLACED AFT SMOKE DETECTOR WITH NEW SMOKE DETECTOR.

NLG DID NOT RETRACT WHEN GEAR HANDLE SELECTED UP. EMER & ABNORMAL PROCEDURES CHECKLIST FOLLOWED & GEAR WAS SELECTED DOWN. MLG EXTENDED & GREEN BUT NLG RETRACTED & HAD RED UNLOCKED LIGHT. TOWER VERIFIED MAINS DOWN & NOSE GEAR UP. EMER LG WILL NOT EXTEND PROCEDURE DID NOT BRING THE NLG DOWN, EMER DECLARED & ACFT ROUTED TO MKE. ACFT MADE A NLG UP LANDING WITH NO INJURIES. NLG SPADE DOOR & LT GEAR DOOR REMOVED & VISUAL CONFIRMATION WAS MADE THAT NLG UPLOCK WAS RELEASED. HYD LINES WERE CRACKED ON THE NLG & GEAR EXTENDED & VERIFIED AS LOCKED. INITIAL INVESTIGATION REVELS FLEXIBLE HYD LINES WERE POSSIBLY SWAPPED DURING RECENT IMPLEMENTATION OF SB680-32-06 NLG ISOLATOR PIN REPLACEMENT.

AIRCRAFT DEPARTED, ENROUTE, AT 25 MINUTES INTO FLIGHT AND AT FL450 PIC NOTICED A 1500LB FUEL IMBALANCE WITH THE LT SIDE READING LOW. FUEL QUANTITY ON LT SIDE CONTINUED TO DECREASE ON BOTH THE PRIMARY AND STANDBY INDICATIONS. IT WAS AT THIS TIME THE PIC SUSPECTED A MAJOR FUEL LEAK AND DECLARED AN EMERGENCY. ACFT WAS DIVERTED DUE TO LONG RUNWAY AND GOOD WEATHER. WHEN DESCENDING FROM FL450 TO FL410 FUEL LEVEL INCREASED AND WENT BACK TO EVEN. ACFT LEVELED OFF AT FL400 FOR 10 MINUTES WITH NORMAL, BALANCED FUEL LEVEL INDICATION. THEN FUEL LEVEL DECREASED TO ZERO ON LT SIDE ON PRIMARY AND SECONDARY INDICATOR. ACFT DID NOT DISPLAY "LOW FUEL" WARNING CAS MESSAGE. INDICATION THEN WENT FROM ZERO TO NORMAL AND BACK TO ZERO AGAIN. ACFT THEN MADE A SAFE EMERGENCY LANDING. ON THE GROUND A VISUAL INSPECTION WAS CARRIED OUT TO ENSURE NO EXTERNAL FUEL LEAKAGE HAD OCCURRED. TECHNICAL SUPPORT WAS CONTACTED AND ADVISED OF THE SITUATION AND RECOMMENDED TROUBLESHOOTING PROCEDURES. RECOMMENDED TO RESET ALL CONNECTIONS ON FUEL CONDITIONER AND FUEL INDICATOR JUNCTION BOX. ALL CONNECTORS ON THESE BOXES WERE REMOVED, INSPECTED, CLEANED, AND RESET. A SELF TEST WAS PERFORMED ON THE FUEL INDICATION SYS AND NO DEFECTS NOTED. ACFT DEPARTED AND CONTINUED ON WITH NO OTHER ISSUES. AIRCRAFT THEN CONTINUED ON WITH NO OTHER ISSUES. PROBLEM APPEARS TO BE FROM A LOOSE CONNECTION ON EITHER THE FUEL CONDITIONER OR THE FUEL INDICATOR JUNCTION BOX. NO PARTS WERE CHANGED AND THE ACFT FUEL INDICATION SYSTEM IS OPERATING PROPERLY AT THIS TIME.

REPAIR SURFACE AND INNER GRANULAR CORROSION LOCATED ON FWD WING PLANK IN THE AREA OF THE LT LOWER REBATE AT WING BL19.0 TO B.L.21.0. REF GDAS-BAF W/O SC3925.12.12 FOR FURTHER DETAILS. RECEIVED ENGINEERING DISPOSITION DATED 02/11/2010, W/O SC19577 STATING REPAIR IAW BLUE PRINT SE45803171-1 REV., PLANK RPR-WING,LWR, LT, LBL 20.0, FRONT BEAM,REF: FAA FORM 8100-9 DATED 02/15/2010, AR-E-1018 STRUCTURAL, SUBJECT MAJOR REPAIR , ACCEPTABLE USE OF BLUE PRINT SE40001055 REV. L TOP DWG.

REPAIRED SURFACE AND INNER GRANULAR CORROSION LOCATED FWD WING PLANK IN AREA OF FUEL ACCESS DOOR. REF: GDAS-BAF W/O SC3925 FOR FURTHER DETAILS. RECEIVED ENGINEERING DISPOSITION DATED 02/05/2010, W/O CS197059 STATING REPAIR IAW BLUE PRINT SE45803171-1 REV.-, PLANK RPR-WING,LWR,RT,BL 23-39, FRONT BEAM,REF FAA FORM 8100-9 DATED 02/05/2010, AR-E 1094 STRUCTURAL, SUBJECT MAJOR REPAIR, ACCEPTABLE USE OF BLUE PRINT SE40001055 REV.J TOP DWG.

CREW NOTED NR1 HYD SYS LOSS OF HYD PRESSURE AND QTY AT CRUISE 30 MIN INTO FLIGHT. UNEVENTFUL LANDING. TROUBLESHOOTING FOUND ADEL CLAMP TO HAVE WORN RUBBER WHICH ALLOWED CLAMP TO CHAFE THROUGH HYD PRESSURE LINE FROM ENG DRIVEN HYD PUMP WHERE IT ENTERS THE HYD NR1 MANIFOLD IN THE AFT EQUIP BAY.

THIS IS ACTUALLY A G-36. THE ENGINE LOST POWER ON CLIMBOUT. TROUBLESHOOTING REVEALED THAT THE FUEL DELIVERY LINE 36-920001-13 HAD A HOLE ARCED IN IT FROM AN ELECTRICAL WIRE, P6 PIN 14 WIRE H21A20. THE WIRE BUNDLE HAD BEEN RUBBING AGAINST THE FUEL LINE AND HAD CHAFED THROUGH THE INSULATION ON THE WIRE. THE CENTER CONDUCTOR CONTACTED THE ALUMINUM FUEL LINE AND ARCED A HOLE THROUGH IT. THE HOLE CAUSED THE ENGINE DRIVEN FUEL PUMP TO SUCK AIR. THE PILOT TURNED THE ELECTRIC FUEL BOOST PUMP ON TO ENABLE HIMSELF TO SAFELY LAND BACK AT DEPARTURE. THE FUEL LINE THAT HAD THE HOLE ARCED IN IT RAN FROM THE FUEL SELECTOR TO THE AFT SIDE OF THE FIREWALL, FWD AND ABOVE THE PILOTS RUDDER PEDALS. WE REPLACED THE LINE PN 36-920001-13 AND REPAIRED THE WIRE. WE TIED THE WIRE BUNDLE TO PREVENT THE CHAFING THAT HAD BEEN OCCURRING.

THE AIRCRAFT WAS DISPATCHED ON A 14CFR PART 135 CHARTER FLIGHT WITH 3 PASSENGERS ON BOARD. THE AIRCRAFT TOOK OFF BUT WHEN THE LANDING GEAR WAS RETRACTED, THE NOSE GEAR LOCKED, BUT BOTH MAIN GEAR FREE FELL INTO THE DOWN POSITION. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AND WAS JACKED UP IN HANGAR. DETAILED INSPECTION REVEALED THAT A WIRE HAD PULLED LOOSE FROM THE PLUG CONNECTOR IN THE RT WHEEL WELL. FURTHER INVESTIGATION SHOWED THAT ANOTHER WIRE HAD PULLED FREE FROM THE LT UPLOCK SWITCH. THE WIRES WERE REPINNED AND REINSERTED INTO THE CORRECT LOCATION IN THE UPLOCK SWITCH CONNECTORS. THE LANDING GEAR WAS CYCLED THROUGH SEVERAL TIMES AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE AIRCRAFT WAS REMOVED FROM JACKS AND A TEST FLIGHT WAS FLOWN WITHOUT ANY FURTHER PROBLEMS.

DURING A ROUTINE BLOCK INSPECTION, A VISUAL INSPECTION OF THE WINGS REVEALED MULTIPLE WIRES SHOWING DAMAGE IN THE FLAP WELL AREA, FWD OF THE IB FLAPS. THE CAUSE DAMAGE TO THE WIRE BUNDLES F50B602101A1 AND F50B602102A1 COULD NOT BE DETERMINED. SOME SHOWED SIGNS OF HEAT DAMAGE AND OTHERS SEEMED FRAYED OR CHAFED OR CHEWED. NO SYSTEM MALFUNCTIONS WERE NOTED BY THE FLIGHT CREW PRIOR TO THE NSPECTION. THE AC WAS ON AN INTERNATIONAL FLIGHT PRIOR TO THE INSPECTION. THE WIRES WERE REPLACED IAW THE MFG MM AND STANDARD PRACTICES AND ADDITIONAL SHIELDING WAS APPLIED. INSPECTION OF OTHER AC IN THE FLEET SHOWED NO SIMILAR DAMAGE. RECOMMENDATIONS ARE TO SHIELD WIRE BUNDLES BETTER AND PAY MORE ATTENTION TO FLAP WELL ARE

NR 2 ENGINE DRIVEN HYDRAULIC PUMP FAILED IN FLIGHT. UPON REMOVAL OF FAILED PUMP. INSPECTION FOUND ONE PLUG O-RING HANGING OUT ALLOWING FLUID TO ESCAPE. (WP19200407082)

DURING MAX POWER ASSURANCE RUN, PARKING BRAKE FAILS TO SECURE A/C EPR IS 1.4 AND ABOVE. MLG BRAKES SAME AT POWER SETTING 1.6 AND ABOVE. PERFORMED PARKING T/S+RIG CHECK IAW M/M 32-44-0. OPS CHECK GOOD. PERFORMED HYD BRAKE SYS T/S IAW 32-41-00. FOUND RT MLG BRAKE METERING VALVE OUT OF ADJ. BLEEDING TO RETURN SIDE UNABLE TO ADJ. REMOVED AND REPLACED BRAKE METERING VALVE.

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT AIRSTAIR INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT CONTACT AT AFT AIRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

DFW DURING OVERNIGHT MAINTENANCE AFT AIRSTAIRS EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT AIR STAIRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

DFW DURING OVERNIGHT MAINTENANCE AFT CARGO EXTERNAL EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AFT AIR CARGO EXTERNAL EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.

MIA DURING OVERNIGHT MAINTENANCE AFT STAIRWAY OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

TUL - CORROSION ON LOWER SKIN CENTER SECTION TANK. INSTALLED REPAIR PER SRM 57-30-3 FIG 7 AND FIG 8. (X)

TUL - CORROSION ON UPPER LEFT OUTBOARD TE BEAM AT NR 7 ELEVATOR HINGE AREA. REMOVED CORROSION, INSTALLED DOUBLER PER ESO 11697 DAED 4-25-00. (X)

TUL - DEEP SCRATCH IN SKIN STA 412, STR 24R. INSTALLED REPAIR AT STA 412, STR 24R IAW SRM 53-30-3. (X)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS UNDER EXIT MARKER ADJACENT TO AFT SERVICE DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION.(M)

RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHT AT VENTRAL STAIRS INOPERATIVE. CLEANED AND ADJUSTED ELECTRICAL CONTACTS OF BATTERY/CHARGER TO EMERGENCY EXIT OVERHEAD LIGHT AT VENTRAL STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

LGA - FLT 1886 - DURING LANDING AT LGA COCKPIT EMERGENCY EXIT LIGHTS ILLUMINATED AND REMAINED ILLUMINATED WITH SWITCH TURNED OFF. REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

TUL - FOUND CORROSION ON STRINGER SPLICE AT BS 480. REMOVED CORRODED STRINGER SPLICE AND INSTALLED REPAIR SPLICE PE SRM 53-10-3. (M)

TUL - FOUND CORROSION ON SHEAR TIE STATION 700 BETWEEN STRINGER 27R AND 28R. INSTALLED DOUBLER ON SHEAR TIE STATION 700 BETWEEN STRINGER 27 AND 28R PER SRM 53-10-4 PAGES 58-60. (M)

AIR VALVE STUCK IN OPEN POSITION CAUSING FULL HOT AIR TO CABIN. SMOKE STARTED TO FLOW INTO CABIN AFTER TAKEOFF. AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. MAINTENANCE CLEANED VALVES AND OPS CHECKED OK. BOTH BYPASS VALVES WILL BE REPLACED.

AIR VALVE STUCK IN OPEN POSITION CAUSING FULL HOT AIR TO CABIN. SMOKE STARTED TO FLOW INTO CABIN AFTER TAKEOFF. AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. MAINTENANCE CLEANED VALVES AND OPS CHECKED OK. BOTH BYPASS VALVES WILL BE REPLACED.

ORD - AFTER TAKEOFF, SMOKE AND FUMES FROM BEHIND F/E. PULLED RADIO PRIMARY CIRCUIT BREAKER AND SMOKE AND FUMES WENT AWAY. REF: PREVIOUS WRITE-UP 07. REPLACED PANEL AND INSTALLED RADIO PRIMARY CIRCUIT BREAKER AND VARIABLE CONTROL TRANSFORMER. CHECKED ALL CENTER PANEL LIGHTS FOR ONE HOUR AND CHECKED BEHIND B-18 CIRCUIT BREAKER PANEL. ALL CHECKED NORMAL.

ORD - FLT 1391 - AFTER TAKEOFF, COCKPIT CREW NOTED A LIGHT, BUT DEFINITE ELECTRICAL BURNING SMELL BEHIND FLIGHT ENGINEER'S PANEL. CREW PULLED RADIO PRIMARY CURCUIT BREAKER TO SHUT OFF POWER AND ELIMINATE POSSIBLE FIRE HAZARD. SMELL DISSIPATED, FLIGHT RETURNED ORD AND LANDED WITHOUT INCIDENT. REPLACED VARIABLE CONTROL TRANSFORMER, PANEL, AND INSTRUMENT RADIO PRIMARY CIRCUIT BREAKER. CHECKED ALL CENTER PANEL LIGHTS FOR ONE HOUR AND P-18 CIRCUIT BREAKER PANEL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT MID CABIN WOULD NOT TEST. SECURED WIRING, SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

MIA - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING AT MID CABIN INOPERATIVE. SECURED SEGMENT OF EMERGENCY EXIT FLOOR PATH LIGHTING AT MID CABIN BELOW SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

TUL - NR 5 LEADING EDGE INBOARD ATTACH ANGLE CRACKED LOWER LEG. INSTALLED NEW ACTUATOR MOUNT INBOARD NR 5 SLAT. TST: 43,979 HOURS. CYCLES, 23,050. (X)

TUL - FORWARD ENTRY DOOR UPPER HINGE CUT-OUT CRACKED. VERIFIED WITH HFEC (MARKED) EXTERNAL. ROUTED OUT CRACK AND INSTALLED DOUBLER AND FILLERS IAW SB 727-53-0198, FIG 4. TST: 43,979 HOURS. CYCLES, 23,058. (X)

TUL - CRACK IN OUTBOARD FLANGE RADIUS IN STR 29R, STA 990 TO STA 995. INSTALLED STR 29R REPAIR PER SRM 53-10-3, FIG 1. INSTALLED SKIN REPAIR DOUBLER AND TRIPLER PER SRM 53-30-3, FIG 3A. TST: 43,979 HOURS. CYCLES, 23,058. (X)

TUL - CORROSION ON FUSELAGE SKIN INSIDE AFT CARGO ADJACENT TO OUTBOARD FLANGE OF STR 29R, STA 990 - STA 996. REPAIRED PER SRM 53-10-3, FIG 3 AND SRM 53-30-3, FIG 3A. TST: 43,979 HOURS. CYCLES, 23,058. (X)

TUL - FIXED LEADING EDGE SKIN CRACKED 7 INCHES LONG AFT OF NR 5 SLAT OUTBOARD END. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER SRM 57-30-4, PAGES 11A AND 11B. TST: 43,979 HOURS. CYCLES, 23,058. (X)

DFW - DURING OVERNIGHT MAINTENANCE, FOUND AFT CARGO EMERGENCY LIGHT INOPERATIVE. REPLACED AFT CARGO DOOR HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

TUL - FOUND CORROSION ON FORWARD WING SPAR AND LOWER CHORD ANGLE. CORROSION REMOVED INSTALLED DOUBLERS PER SRM 57-10-6 PG 2A-2C, 6, 7, AND 9. (M)

TUL - FOUND CORROSION VERTICAL BRACKET 11B NR 5 LSAT ACTUATOR BY NR 3 FUEL VALVE. REMOVED AND REPLACED BRACKET WITH NEW SERVICABLE BRACKET. (M)

TUL - FOUND LEFT HORIZONTAL STABILIZER TRAILING EDGE SKIN CORRODED, AT UPPER SKIN ABOVE OUTBOARD ELEVATOR FITTING. REMOVED CORROSION, TREATED AND INSTALLED EXTERNAL DOUBLER PER ESO1 697 DATED 6-21-96. (M)

TUL - FOUND LEFT LEADING EDGE WING RUBBING FUSELAGE 2 SPOTS STATIONS 720D AND 720E, STRINGER 18L AND STRINGER 19. CUT OUT WORN SPOTS (2) ON FUSELAGE. INSTALLED FILLERS AND OUTSIDE DOUBLER OVER Z AREAS. DOUBLERS ARE ONE CONTINUED PIECE CONSTRUCTION.