N206FE

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,924 hrs · 16,495 cycles

FWD CARGO COMP'T FLOOR SUPPORT IS CRACKED AT STA 700 RBL 13. REMOVED AND REPLACED FLOOR SUPPORT SECTION IAW SRM 51-40-4.

Part: RIB — CRACKED (RT WING) · airframe 28,924 hrs · 16,495 cycles

RIGHT WING L/E UPPER SUPPORT RIB IS CRACKED AT WS 349. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-10-1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,924 hrs · 16,495 cycles

FWD CARGO COMPT FLOOR SUPPORT IS CRACKED AT STA 700 RBL 13. REMOVED AND REPLACED FLOOR SUPPORT SECTION IAW SRM 51-40-4.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,924 hrs · 16,495 cycles

LOWER FUSELAGE EXTERIOR SURFACE, SKIN CRACKED AT STATION 1010 AT APPROX STR 29R WITH CORROSION. CUT OUT DAMAGED SECTION OF SKIN IAW SRM 53-30-3 FIG 3A, FABRICATED AND INSTALLED (1) EA DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3A AT MAE.

Part: RIB — CRACKED (RT WING) · airframe 28,924 hrs · 16,495 cycles

RIGHT WING L/E UPPER SUPPORT RIB IS CRACKED AT WS 349. REMOVED AND REPLACED CRACKED RIB IAW SRM 51-10-1.

Part: SKIN — GOUGED (L/E SLAT) · airframe 28,924 hrs · 16,495 cycles

COMPLY WITH EA 7-5750-77346; WINGS, LEADING EDGE NR 6 SLAT TRAILING EDGE REPAIR, SLAT STA 167.9. COMPLIED WITH EA 7-5750-77346; REPAIRED NR 6 SLAT TRAILING EDGE.

Part: STRUCTURE — GOUGED (L/E SLAT) · airframe 28,924 hrs · 16,495 cycles

COMPLY WITH EA 7-5750-77346; WINGS - LEADING EDGE NR 6 SLAT TRAILING EDGE REPAIR, SLAT STA 167.9. COMPLIED WITH EA 7-5750-77346; REPAIRED NR 6 SLAT TRAILING EDGE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,924 hrs · 16,495 cycles

MAIN CARGO COMPT SEAT TRACK HAS CORROSION, GOUGED SCALLOPS AND DRILL STARTS AT FS 1050-1140 LBL 45. REMOVED AND REPLACED SEAT TRACK STA 1050-1140 LBL 45 IAW SRM 53-10-5 AND 51-30-2.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 28,924 hrs · 16,495 cycles

MAIN CARGO COMPT CARGO TRACK HAS CORROSION, GOUGED SCALLOPS AND DRILL STARTS AT FS 1050-1140 LBL 45. REMOVED AND REPLACED CARGO TRACK STA 1050-1140 LBL 45 IAW SRM 53-10-5 AND 51-30-2.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 28,924 hrs · 16,495 cycles

COMPLY WITH EA 7-5310-77345 FUSELAGE MAINFRAME BL 0 SEAT TRACK SPLICE CORRODED. COMPLIED WITH EA 7-5310-77345 FUSELAGE MAINFRAME BL 0 SEAT TRACK SPLICE.

Part: CARGO TRACK — GOUGED (CARGO BAY) · airframe 28,924 hrs · 16,495 cycles

MAIN CARGO COMPT CARGO TRACK HAS GOUGED SCALLOPS AT FS 755 - 765 LBL 63. REMOVED AND REPLACED CARGO TRACK SECTION AT FS 755 - 765 LBL 63, IAW SRM 51-30-2 AT MAE.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 28,924 hrs · 16,495 cycles

MAIN CARGO COMPT. SEAT TRACK HAS GOUGED SCALLOPS AT FS 755 - 765, LBL 63. REMOVED AND REPLACED SEAT TRACK SECTION AT F/S 755-765, LBL 63, IAW SRM 51-30-2.

Part: SUPPORT — CRACKED (NR 2 NACELLE) · airframe 28,924 hrs · 16,495 cycles

NR 2 RIGHT AFT COWL ENGINE DRAIN LINE SUPPORT CRACKED. FABRICATED DRAIN LINE SUPPORT FROM 2024-T3 .032C BATCH 715298 AND INSTALLED IAW SRM 51-30-2 AT MAE.

Part: FRAME — DAMAGED (NLG SUPPORT) · airframe 28,924 hrs · 16,495 cycles

COMPLY WITH EA 7-5310-77343; FUSELAGE MAIN FRAME MISDRILLED HOLE REPAIR BS 336.0, RBL 6.5 WL 153. COMPLIED WITH EA 7-5310-77343 FUSELAGE MAIN FRAME MISDRILLED HOLE REPAIR BS 336.0 RBL 6.5 WL 153 AT MAE.

Part: BRACKET — CHAFED (NR 2 NACELLE) · airframe 28,924 hrs · 16,495 cycles

NR 2 ENG RIGHT AFT COWL OVERBOARD DRAIN SUPPORT BRACKET & RIVET CHAFED. FABRICATED NEW SUPPORT BRACKET USING 2024-T3 .050C BATCH 742514 AND INSTALLED IAW SRM 51-30-2 AT MAE.

Part: STRIP — TORN (PYLON) · airframe 28,924 hrs · 16,495 cycles

PANEL 5531 CHAFE STRIP IS TORN. REMOVED AND REPLACED STRIP IAW SRM 51-30-2 AT MAE. FABBED FROM 301-25 .012SS BATCH 000705488.

Part: PITOT TUBE — OBSTRUCTED (PITOT STATIC) · airframe 28,201 hrs · 16,116 cycles

F/O AIRSPEED INDCATOR INOP ON T/O UPON ARRIVAL CHECKED FOR OBTRUCTIONS IN BOTH CAPTS & F/O'S PITOT TUBES NO BLOCKAGE NOTED. R&R F/O'S AIRSPEED INDICATOR.OPS CHECKS GOOD PER B727-200_M.M. CHAPT.34-12-000-5.

Part: LATCH — STUCK (COCKPIT) · airframe 27,944 hrs · 15,974 cycles

AFTER T/O FROM KGEG F2 F/O COULD NOT RAISE THE LANDING GEAR LEVER BEYOND THE OFF POSITION. FOLLOWED RED TABS LANDING GEAR LEVER LATCH FAILED TO RELEASE. CHECKLIST, CHECK 2F RESET P6- 3 LANDING GEAR 2 LEVER LATCH 2 FLIGHT CB. LANDING GEAR THEN RETRACTED.

Part: INDICATOR — ERRATIC (COCKPIT) · airframe 27,030 hrs · 15,500 cycles

ON TAKEOFF ROLL, JUST PRIOR TO V1, ALL 3 FUEL FLOW INDICATIONS BECAME ERRATIC. AFTER TAKEOFF ALL 3 FUEL FLOW INDICATORS WERE READING APPROX CORRECT BUT FLUCTUATIONS +/- 2000 LBS. AFTER 10 MINUTES ALL THREE FUEL FLOW GAUGES BECAME COMPLETELY ERRATIC AND UNUSABLE. CHECKED 28VDC AND 115VDC TO FUEL FLOW POWER SUPPLY CONNECTOR D100 AT PINS 2 AND 7 AND GROUNDS AT PINS 1 AND 6 WHILE SHAKING OUT WIRING. CHECK WIRING FOR SHORTS TO GROUND AND CONTINUITY FROM POWER SUPPLY TO F/ F INDICATORS WHILE SHAKING OUT WIRING. REMOVED AND REPLACED FUEL FLOW POWER SUPPLY IAW MM. TAXIED AIRCRAFT AND RAN ALL THREE ENGINES TO HIGH POWER IAW JRH. ALL FUEL FLOW INDICATIONS CHECKED NORMAL. AIRCRAFT OK FOR SERVICE.

Part: GASPER FAN — MALFUNCTIONED (CABIN) · airframe 26,762 hrs · 15,343 cycles

GASPER FAN CB POPPED. MILD ELECTRICAL SMOKE IN FLT STATION. REPLACED GASPER FAN PER M/M 21-23-011-4. SYSTEM OPS CHECK OK.

Part: UPLOCK SWITCH — FAULTY (NLG)

NOSE GEAR RED LIGHT ILLUM WITH GEAR HANDLE IN UP POS. REMOVED AND REPLACED NOSE GEAR LOCK SW PER MM 32-61-071-4. CLEANED GEAR HANDLE CONTACT PRECAUTIONARY.

Part: ACTUATOR — FAILED (L/E FLAP)

ON DEPARTURE RETRACTING FLAPS ON RIGHT WOULD NOT RETRACT. REMOVED AND REPLACED NR 6 KRUEGER FLAP ACTUATOR PER MM 27-81-022-4.

Part: SWITCH — DIRTY (LANDING GEAR)

ON LANDING GEAR EXT THE LANDING GEAR DOOR LIGHT ON FWD PANEL IND 3 GRN AND 4 RED LIGHT. REMOVED DUST AND DEBRIS FROM LANDING GEAR CNTRL LEVER POS IND SWITCH, CYCLE SEV TIMES. CK NORM GOOD PER MM 332-61-12 PG 401-403. OK FOR SERVICE. INSTALLED AND REMOVED LANDING GEAR PINS.

Part: INDICATION — MALFUNCTIONED (LE FLAPS)

REPEAT WRITEUP FLAPS RETRACT WITH LEAD EDGE FLAP LIGHT OUT THE LEAD EDGE FLAP AMBER LIGHT ILLUM. OPER FLAPS AND SLATS IN ALL POS. VISUAL INSP, THE MOVEMENT OF FLAPS AND SLATS, IT OPER NORM. CAN'T DUP ON GROUND, PERFORMED T/O WARN CK ALL SWITCHES OPER NORM. A/C OK TO CONT.

Part: DETECTION UNIT — MALFUNCTIONED (E/E COMP)

LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED IN CRUISE FLIGHT. (NO ANTI-ICE ON AT ALL). NR 2 ENGINE LEFT BLEED ON NR 3 BLEED ON, LEFT AND RIGHT PACKS ON. FOLLOWED RED TABS PROCEDURES. LIGHT WENT OUT AFTER NR 1 ENGINE BLEED TURNED OFF FOR SEVERAL MINUTES. RAN ALL ENGINES ON GATE. NO DEFECT NOTED. REMOVED AND REPLACED OVERHEAT DETECTION UNIT, (PRECAUTIONARY).

Part: DOUBLER — MALFUNCTION (BS 720)

NR 0384, 71C301-02, SKIN GOUGED AT LWR FUSELAGE STA 720F FWD OF GROUND AIR INLET. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3.

Part: RETRACT MECH — DAMAGED (NLG)

UPON LDG AT 147K AND ROLLOUT TO 110K AT WHICH POINT A NOTICEABLE SHIMMY BEGAN AND GOT WORSE. A/C DIRECTION MAINTAINED WITH DIFFERENTIAL BRAKES AND REVERSE. NOSE WHEEL STEERING WAS COMPLETELY INEFFECTIVE. EMERGENCY EQUIPMENT REPORTED TO FLIGHT DECK, AND THAT NO TIRES WERE BLOWN. ****S/D**** INSP NOSE WHEEL STRUT AND DOORS. REPLACED GROUND SHIFT ROD AND TORQUE LINK PIN. BURNISHED OUT DAMAGE ON LOWER LINK AND REPAINTED. REMOVED AND REPLACED BOTH NOSE WHEEL TIRES PER MM 32-45-11 PG 402 AND MM-15-31, PG 202. A/C OKAY FOR SERVICE.

Part: FIRE DETECTORS — MALFUNCTIONED (NR 2 ENGINE)

ENG FIRE WARNING LIGHT ILLUMINATES WHEN POWER WAS REDUCED ON ENG NR 2. OPS AT IDLE AND LIGHT REMAINS OUT. LEAK CHECKED ENG AND FOUND NO BLEED AIR LEAKS. REMOVED AND REPLACED ENG AND FIREWALL FIRE DETECTION ELEMENTS. RAN ENG FOR 5 MINUTES AT POWER, PLUS TAXI TO AND FROM RUNUP AREA. NR 2 FIRE WARNING OPS CHECK GOOD.

Part: FIRE WARNING — ACTIVATED (NR 2 ENGINE)

NR 2 ENGINE HAD FIRE WARNING IN FLT. LIGHT WENT OUT WHEN THRUST LEVER RETARDED TO IDLE. LIGHT CAME ON AT TOP OF DESCENT AT 35,000 FT. SUSPECT BLEED AIR LEAK, FIRE LOOPS CHECKED GOOD. RAN NR 2 ENGINE, CHECKED FOR AIR LEAKS, CHECKED FIRE WARNING SYSTEM. FOUND NO AIR LEAKS AND SYSTEM CHECKS OK PER MM 26-11-00.

Part: FIRE WIRE CONN — DIRTY (NR 3 ENGINE)

IMMEDIATELY AFTER DISCONNECTING NR 3 CSD, FIRE BELL AND WARNING LIGHTS ON PILOTS PANEL AND NR 3 FIRE HANDLE ILLUMINATED MOMENTARILY BOTH SYS-A AND LOOPS WERE TESTED, TEST WAS GOOD. FIRE BELL WOULD INTERMITTENLY COME ON. FOUND LOOSE CLAMP ON LOWER PART OF NR 3 ENG, CLEANED OILY CONNECTORS AND TIGHTENED CLAMP, OPS CK GOOD.

Part: OVERHEAT WIRE — BARE (NR 2 ENGINE)

DIA - NR 2 FIRE WARNING IND ON MOMENTARILY ON APPROACH INTO DEN, LESS THAN 2 SECOND BELL AND LIGHT. SYS CHECKS OK. OPENED COWL AND INSPECTED ALL DUCTS AND ENGINE. FOR LOOSE CONNECTIONS OR BREAKS, CHECKED OK. FOUND EXPOSED WIRE ON OVER HEAT WIRE ADJACENT TO GENERATOR FEEDER CABLES. INSTALLED HEAT SHRINK AND CLEANED CONNECTOR. FOUND AFT CONNECTORS OILY, CLEANED, CHECKED PER JET RUN HANDBOOK 5-17, OK FOR SERVICE.

Part: FIRE WIRE — LOOSE (LT/RT MLG WW)

FIRE WARNING BELL SOUNDED INTERMITTENTLY AND FIRE WARNING LIGHTS ON THE DASH AND WHEEL WELL LIGHT FLICKERED. NO LIGHTS IN THE HANDLES ON THE OVERHEAD PANEL. BELL SILENCED ITSELF AND LIGHTS WENT OUT. RESECURED L AND R LOOP CONNECTIONS IN WHEEL WELLS AND OPS CHECK GOOD.

Part: FIRE CONTL UNIT — MALFUNCTIONED (NR 2 ENGINE)

NR 2 ENG FIRE WARNING WOULD INTERMITTENTLY COME ON IN FLT AND DURING TAXI IN. FIRE TEST SYSTEMS CHECKED AND TESTED GOOD. REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT PER MM 26-11-01 AND OPS CHECK NORMAL. REMOVED AND REPLACED FIRE AND OVERHEAT DETECTOR, PRECAUTIONARY DUE TO HISTROY.

Part: HEAT VALVE — FAILED (NR 2 ENGINE)

GDL - NR 2 FUEL HEAT VALVE STUCK OPEN. FOLLOWED PROCEDURE, SHUT NR 2 ENG DOWN. REMOVED AND REPLACED FUEL HEAT ANTI-ICE VALVE, PER MM 73-14-11 PG 401, OPS CHECKED GOOD, OK FOR SERVICE. A/C DIVERTED TO GDL DUE PRECAUTIONARY NR 2 ENG SHUTDOWN.

Part: OIL TEMP BULB — FAILED (NR 2 ENG)

NR 2 ENG OIL TEMP IND 150 AFTER TAKEOFF WE REDUCED PWR TO 1.43 75 PERCENT N1, 350 EGT 82 N2. AFTER 15 MIN ENG OIL TEMP 140. ENG SHUTDOWN WAS ACCOMPLISHED IAW. CHECKLIST. AFTER PWR REDUCTION CSD TEMP DECREASED FROM 118 TO 80 DEG CELSIUS. REMOVED AND REPLACED NR 2 ENG OIL TEMP BULB AS PER MM 79-34-21. RAN NR 2 ENG AS PER JRH OPS CK GOOD. ALSO, SERVICED NR 2 CSD AND NR 2 ENG OIL.