N350CJ

Part: SOCKET — SHORTED (WINDOW LIGHT) · airframe 40,716 hrs · 48,668 cycles

WINDOW LIGHTS AT ROWS 6 AND 7 SMELL LIKE BURNING PLASTIC.

Part: LINK — SEPARATED (PROPELLER)

DURING TAKE OFF, THE PROPELLER DID NOT FOLLOW CONDITION LEVER POSITION. THE LINK AT THE PROPELLER CONTROL UNIT WAS FOUND SEPARATED DUE TO A LOCK WASHER THAT FAILED.

Part: ACTUATOR — BINDING (RUDDER) · airframe 40,097 hrs · 47,775 cycles

ON CLIMB GUST LOCK LIGHT CAME ON, AFTER REACHING CRUISE THE CREW BECAME AWARE THAT THERE WAS NO RESPONSE TO THE RUDDER INPUT.

Part: DUCT — BROKEN (ZONE 600) · airframe 38,426 hrs · 45,562 cycles

DURING FLT, RT BLEED AIR LEAK LIGHT ILLUMINATED. CREW COMPLETED QRH 1-6, LIGHT EXTINGUISHED AND FLIGHT CONTINUED. ACFT WAS RETURNED TO HOME BASE USING A FERRY PERMIT. DURING PRELIMINARY INSPECTION FOUND RT BLEED AIR RUBBER DUCT BROKEN. DUCT WAS REPLACED. OPS AND LEAK CHECK PERFORMED FOUND WORKING PROPERLY. ALSO ACFT WAS RELEASED FOR FUNCTIONAL CHECK FLIGHT AND NO ABNORMALITIES FOUND DURING THIS FLIGHT.

Part: ELEMENT — CHAFED (OVERHEAT) · airframe 38,391 hrs · 45,579 cycles

BLEED AIR LEAK CAUTION LIGHT ILLUMINATED DURING FLIGHT, PROCEED TO QRH AND LIGHT REMAINED ILLUMINATED, PROCEEDED WITH ENGINE SHUTDOWN. PRELIMINARY INSPECTION FOUND SENSING ELEMENT CHAFING AGAINST DUCT CLAMP. SENSING ELEMENT REPOSITION AND SECURED, OPS CHECK PERFORMED AND FOUND SYSTEM WORKING PROPERLY.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 36,254 hrs · 42,131 cycles

CREW REPORTED THE CABIN PRESSURE MASTER CAUTION LIGHT ILLUMINATED FOR 2 MINS WITH LOSS OF PRESSURE. THE CREW STARTED THE QRH AND THE LIGHT WENT OUT AND PRESSURE CAME BACK. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. OPS CHECKS GOOD P/N OFF 13053S-1 S/N OFF 115-603, P/N ON 130538-1, S/N ON 77361.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 36,126 hrs · 41,947 cycles

ABORTED TAKEOFF DUE TO CONFIG WARNING. T/O INHIBIT TEST FAILS. WHEN PERFORMING TEST - WHEN P/L ARE AT MAX. THE RT POWER LEVER SPRINGS BACK AFTER TAPING POWER LEVER CAUSING CONFIG WARNING LIGHT, WITH FRICTION LOCK ON WILL HOLD RT PL FORWARD NO CONFIG LIGHT. OPS CHECK GOOD.

Part: FAN — BURNED OUT (RECIRCULATION) · airframe 36,015 hrs · 41,811 cycles

FLIGHT DIVERTED TO ABE DUE TO THE RIGHT RECIRCULATION FAN LIGHT AND LEFT AIR VALVE LIGHT ILLUMINATED DURING FLIGHT FOLLOWED BY THE ODOR OF SMOKE. REMOVED AND REPLACED AVIONICS RECIRCULATION FAN. OPS CHECKED OK, CND THE AIR VALVE.

Part: LIGHT — ILLUMINATED (CABIN) · airframe 35,300 hrs · 40,780 cycles

AIR RETURN DUE TO EMER PWR LIGHT CAME ON IN FLT.

Part: LUG — CORRODED (RUDDER PEDAL) · airframe 35,292 hrs · 40,771 cycles

RUDDER PEDAL CONSOL ASSY LUGS ARE CORRODED. REMOVED AND INSTALLED NEW CONSOL ASSY PN: 7327200-561.

Part: RUDDER PEDAL — CORRODED (COCKPIT) · airframe 35,289 hrs · 40,770 cycles

LT RUDDER PEDAL ASSY P/N 7327200-561 CORRODED. REPLACED ASSY.

Part: STRUCTURE — MISREPAIRED (RT NACELLE) · airframe 35,289 hrs · 40,770 cycles

REPAIR MISC RIVET DEVIATION ON RIGHT I/B NACELLE AT NS 203. COMPLETED REPAIR IAW TD 340-54-09-20.

Part: STRUCTURE — MISREPAIRED (LT NACELLE) · airframe 35,289 hrs · 40,770 cycles

REPAIR MISC RIVET DEVIATION ON LEFT I/B NACELLE. COMPLETED REPAIR IAW TD 340-54-09-19.

Part: FLAP — DAMAGED (RT WING) · airframe 35,289 hrs · 40,770 cycles

RT FLAP BONDED DOUBLER REPAIR. PERFORMED IAW TD340-57-11-03 CONTROL=350-60.

Part: STRUCTURE — MISREPAIRED (RT NACELLE) · airframe 35,289 hrs · 40,770 cycles

REPAIR MISC RIVET DEVIATION ON RIGHT O/B NACELL AT NS 203. COMPLETED REPAIR IAW TD 340-54-09-21.

Part: STRUCTURE — MISREPAIRED (RT NACELLE) · airframe 35,289 hrs · 40,770 cycles

PREVIOUS REPAIR LUG ON RIGHT O/B NACELLE FIG 8 STRAP LUG NOT IN DAMAGE LOG AND NOT DONE IAW SRM 54-10-30-209 OR SB 340-22. COMPLETED REPAIR IAW SAAB STATEMENT 340 SDS 011436 DATED 2007-01-03 AND TD 340-54-11-24. COMPLETED JC 51-00-00S.

Part: STRUCTURE — MISREPAIRED (LT NACELLE) · airframe 35,289 hrs · 40,770 cycles

RIVET MISC RIVET DEVIATION ON LEFT O/B NACELLE AT NS 203. COMPLETED REPAIR IAW TD 340-54-09-18.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 35,289 hrs · 40,770 cycles

DENT IN LOWER FUSELAGE AT STA 212 SL 1527, JUST TO THE LEFT OF NOSE JACK POINT. COMPLETED REPAIR IAW SAAB 340 SRM 53-60-10-202 AND TD 340-53-11-63. COMPLETED JC 51-00-00S.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,289 hrs · 4 cycles

LT FWD SECTION OF I/B SEAT TRACK AT LBL 18.5 FUSELAGE STATION 297 TO 353 HAS HEAVY CORROSION ON CENTER AISLE FLOORBOARD FLANGE. SPLICED IN NEW SECTION 56" LONG FROM STA 297 TO 353 IAW TB 340-53-11-59. COMPLETED JC 51-00-00S.

Part: STRUCTURE — CORRODED (COCKPIT) · airframe 35,289 hrs · 40,770 cycles

LT AND RT COCKPIT FLOORS HAVE DEEP PITTING CORROSION. REFERENCE CONTROL 350-43 & MAL MM409 404548 FOR REPAIRS.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 35,289 hrs · 40,770 cycles

LT FWD COCKPIT BULKHEAD SKIN IS DENTED & CRACKED JUST I/B OF RADOME UPPER LATCH PIN THRU HOLE. REFERENCE SAAB STATEMENT 340SDS023248, TD 340-53-11-62 AND MESABA MM409 # 404644 FOR REPAIR DETAILS.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 35,289 hrs · 40,770 cycles

PREVIOUS REPAIR ON FRAME 258 NOT DONE IAW SRM 53-70-30 AND NOT IN DAMAGE LOG. INSTALLED NEW REPAIR IAW TD340-53-11-08. COMPLETED JC 51-00-00S

Part: SKIN — DENTED (FUSELAGE) · airframe 35,289 hrs · 40,770 cycles

RT ICE SHIELD NR 7 REMOVED FOR SKIN INSPECTION AND FOUND SKIN TO BE DENTED OUT OF LIMITES. INSTALLED REPAIR PATCH IAW TD 340-53-11-06,STA.308 TO 363 SL1615 TO 1618.

Part: FRAME — CORRODED (FUSELAGE) · airframe 35,289 hrs · 40,770 cycles

CORROSION ON FWD FUSELAGE BOTTOM FRAME WEB AT STA 225.0 REF MESABA MM-409 # 404552 TD# 350-53-11-61.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 35,289 hrs · 40,770 cycles

CONTROL NUMBER 350-56 PREVIOUS REPAIR ON LT FUSELAGE AT FUSELAGE STATION 364SL.1618 NOT IN DAMAGE LOG. SECOND RIVET ROW AROUND CUT-OUT MISSING. DRILLED AND INSTALLED EIGHT RIVETS FOR SECOND PERIPHERY ROW AROUND CUT-OUT IAW SAAB SF340 SMR 53-70-10. COMPLETED TD 340-53-11-07 AND JC 51-00-00S.

Part: STRUCTURE — MISREPAIRED (NACELLE) · airframe 35,289 hrs · 40,770 cycles

REPAIRED MISC RIVET DEVIATION ON RT INBOARD NACELLE. REPAIRED IAW TD340-54-09-20 CONTROL=350-4.

Part: STRUCTURE — CORRODED (COCKPIT) · airframe 35,289 hrs · 40,770 cycles

LT FLIGHT DECK FLOOR HAD NUMEROUS AREA'S OF CORROSION. REPAIRED IAW TD340-53-11-27 CONTROL=350-43.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 33,862 hrs · 39,384 cycles

CONFIG WARNING ON TAKEOFF ROLL, LIGHT MINIMAL BRAKING DUE TO RW LENGTH. PERFORMED OPERATIONAL CHECK PER AMM, NO DEFECTS NOTED.

Part: WIRE — DAMAGED (RT EXHAUST) · airframe 33,372 hrs · 38,840 cycles

RIGHT TAIL PIPE HOT CIRCUIT BREAKER POPS OUT DURING CHECK. REPAIRED WIRE AT CONNECTOR 162VP P11, IAW SAAB WM 20-10. PERFORMED INSPECTION CHECK OF RIGHT EXHAUST DUCT OVERTEMP SYSTEM IAW SAAB 340 AMM 26-11, NO DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (NACELLE) · airframe 32,702 hrs · 38,187 cycles

AIRCRAFT REQUIRES MAJOR REPAIR FOR PERMANENT REPAIR OF MISC RIVET DEVIATION ON LT AND RT OUTBOARD NACELLE ALONG WITH LT AND RT INBOARD NACELLE IAW TD'S 340-54-09-18, 340-54-09-19, 340-54-09-20 AND 340-54-09-21.

Part: INDICATOR — UNSERVICEABLE (COCKPIT) · airframe 32,335 hrs · 37,767 cycles

ABORTED TAKEOFF DUE TO LEFT ENGINE TORQUE GAUGE INOP. REMOVED AND REPLACED TORQUE INDICATOR, P/N 10225N01W00.

Part: CONNECTOR — LOOSE (MLG)

LANDING GEAR DOWN UNSAFE (LEFT) FOLLOWED CHECKLIST. NOSE AND RIGHT MAIN LIGHTS ILLUMINATED, NO LEFT MAIN AFTER EMERGENCY RELEASE. REPLACED LIGHT BULBS RESET CB GEAR EXTENDED. INSTALLED GEAR PINS ON ALL GEAR. REMOVED AND REPLACED EXPLOSIVE BOLTS IAW WORKCARD 32-31-09S. TESTED LT AND RT EXPLOSIVE BOLT CIRCUITRY FOUND GOOD AFTER RESETTING CONNECTOR 3GBP1A IAW COLGAN WORKCARD 32-31-08S. PERFORMED GEAR SWINGS IAW AMM 32-30-00. NO DISCREPANCIES NOTED.

Part: SEAL — LEAKING (TAILPIPE SENSOR)

AIR RETURN FOR RT TAILPIPE HOT ON CLIMB-OUT FROM LGA. EMERGENCY DECLARED, LIGHT WENT OUT ON IT'S OWN SHORTLY AFTER. WEATHER ON THE GROUND WAS HEAVY RAIN PRIOR TO DEPARTURE. CW WORKCARD FOR TAILPIPE SENSOR SEALING. ONCE DONE, OPS CHECKED GOOD.

Part: CONNECTOR — SMOKE (CABIN LIGHTS)

FA SAW AND SMELLED SMOKE COMING FROM LIGHT AT 2A, CREW EVACUATED AIRCRAFT USING FORWARD MAIN CABIN DOOR. MX CALLED AND AIRCRAFT TOWED BACK TO GATE. TROUBLESHOT AND FOUND SOCKET FOR SEAT 2A WINDOW LIGHT BURNED, REMOVED BULB FOR SAFETY PURPOSE ITEM DEFERRED IAW MEL 33-20-1-1 CAT C. FOUND SMOKE WAS COMING FROM SEAT 2A BALLAST CONNECTOR DISCONNECTED POWER TO BALLAST FOR SEAT 2A HAD POWER ON AIRCRAFT NO SMOKE NOTICED SEAT 2A LIGHT SYSTEM REMAINS ON MEL.

Part: CONNECTOR — SMOKE (CABIN LIGHT)

FA SMELLED AND SAW SMOKE COMING FROM LIGHTED AREA AT A, PERFORMED PRECAUTIONARY EVACUATION. FOUND SMOKE WAS COMING FROM SEAT 2A BALLAST CONNECTOR, DISCONNECTED POWER TO BALLAST FOR SEAT 2A HAD POWER ON AIRCRAFT NO SMOKE NOTICED AT SEAT 2A, LIGHT SYSTEM REMAINS ON MEL.

Part: EADI — DISTORTED (COCKPIT)

DURING CRUISE; FO'S EADI WENT DISTORTED, LOUD POP HEARD SCREEN CAME BACK FULL THEN ELECTRICAL SMOKE DETECTED.

Part: WIRE HARNESS — UNKNOWN (LT ENGINE) · airframe 27,992 hrs · 33,307 cycles

LT ENGINE TORQUE AND RMP FLUX/AIR RETURN. REPLACED RT ENGINE YELLOW HARNESS. OPS CHECK GOOD.

Part: HANDLE — UNSECURE (EMERGENCY DOOR) · airframe 27,823 hrs · 31,134 cycles

FWD EMERG DOOR HANDLE TO OPEN POSITION IN FLIGHT. RESECURED FWD EMERG DOOR HANDLE SAFTIED, A/C OK FOR SERVICE.

Part: CONTROL HANDLE — MALFUNCTIONED (MLG) · airframe 27,774 hrs · 33,085 cycles

GEAR UNSAFE INDICATION WHEN SELECTED DOWN, NOSE GEAR DOES NOT ILLUMINATE, JIGGLING HANDLE AND ALL 3 COME ON. REPLACED LANDING GEAR CONTROL HANDLE IAW SAAB AMM 32-31-05 FUNCTIONAL CHECK OF EXTENSION AND RETRACTION COMPLIED WITH IAW SAAB 340 32-30-00. NO DEFECT NOTED, PN: D494-12-001, SN ON: 300/05-90, SN OFF: 215/07-88.

Part: WIRE — CHAFED (OVERHEAT SYS) · airframe 27,636 hrs · 32,952 cycles

TAIL PIPE HOT WILL NOT TEST ON LEFT SIDE ALSO NO MASTER WARNING BELL. REPAIRED CHAFED WIRE WG506 IAW WM 20-20, OPS CHECK GOOD IAW SAAB MM 26-12-00, NO DISCREPANCIES NOTED.

Part: HMU — MALFUNCTIONED (ENGINE) · airframe 27,626 hrs · 32,942 cycles

LEFT TORQUE INDICATION FLUCTUATED PLUS/MINUS 3-4 PERCENT DURING CRUISE FLIGHT, AS POWER WAS INCREASED FLUCTUATIONS WERE LONGER. ABOUT 1-2 PERCENT AROUND 40-50 PERCENT TORQUE. NO FLUCTUATIONS ON GROUND OR TAKEOFF WITH CTOT ENGAGED. CLIMB POWER SET AND PROP AT 1270 RPM. CHECKED ALL CONNECTORS LT ENGINE ALL FOUND SECURE CHECKED OIL ADDED 1 QT LT ENGINE SWAPPED TORQUE GAUGES RAN ACFT FOUND NO TORQUE FLUCTUATION DURING RUN UP. GAUGE REMAIN SWAPPED. REPLACED LT HMU IAW GE MM 73-00-00, LEAK CHECK AND OPS TEST GOOD. NO FLUCTUATES NOTED DURING ENGINE RUN, P/N 6068T72P22 S/N ON:11432828, S/N OFF: WYG54843.

Part: CIRCUIT BREAKER — TRIPPED (MLG) · airframe 27,563 hrs · 32,863 cycles

ON APPROACH HAD GEAR UNSAFE INDICATION. CREW NOTICED CB F-7 WAS POPPED. RESET POPPED CB F-7 BREAKER GEAR OPERATED NORMALLY AIRCRAFT LANDED WITHOUT INCIDENT. NO OTHER PROBLEMS FOUND.

Part: WIRE HARNESS — DAMAGED (DECU) · airframe 27,533 hrs · 32,829 cycles

TORQUE ITT NG FUEL FLOW NP FUNCTIONS ON CLIMB-OUT AND CRUISE TORQ FLUCT BETWEEN 4-5 PERCENT, ITT 5C, NG 290, FUEL FLOW 20 PPH, NP, 100 RPM. CLEANED ELECTRICAL CONNECTOR ON LT TORQUE SENSOR AND BLUE WIRE HARNESS CONNECTOR ON DECU. OPS CHECK GOOD. NO FLUCTUATIONS NOTED DURING ENGINE RUN.

Part: CONNECTOR — DIRTY (ENGINE) · airframe 27,409 hrs · 32,689 cycles

NO TORQUE INDICATION ON LT SIDE DURING TAKEOFF ROLL. CLEANED LT ENG YELLOW ENGINE HARNESS CONNECTORS. OPS CHECK GOOD IAW GE MM 74-00-00.

Part: TORQUE SENSOR — DIRTY (LT ENGINE) · airframe 27,307 hrs · 32,585 cycles

NO TQ INDICATION ON LT ENGINE ON TAKEOFF ROLL. CLEANED AND INSPECTED TORQUE SENSOR IAW SAAB AMM 77-13-10-02. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,821 hrs · 32,094 cycles

EMERGENCY LIGHTS OPERATING IMPROPERLY. REPLACED NR 1, 2, 3, 4 AND 5 EMERGENCY LIGHTS POWER SUPPLIES IAW W/C 33-50-02S. OPS CHECK GOOD, POS NR 1-21 LN PN: 60-1321-1, SN ON: 18253, SN OFF: 2012, POS NR 2-20 LN, PN: 60-1321-1, SN ON:21036, SN OFF: 16604, POS NR 3-22 LN, PN: 60-1321-1, SN ON: 18219, SN OFF: 19815, POS NR 4-23 LN, PN: 60-1321-1, SN ON: 21548, SN OFF: 20729, POS NR 5-24 LN, PN: 60-1321-1, SN, ON: 12123, SN OFF: 17622.

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 26,700 hrs · 31,968 cycles

FOUND LANDING GEAR FAILED TO RETRACT. REPLACED LANDING GEAR CONTROL HANDLE IAW MM 32-31-05. OPS CHECK GOOD, PN ON D494-12-001, SN ON 2150788, PN OFF D494-12-002, SN OFF 3030590.

Part: DOWNLOCK SWITCH — DIRTY (MLG) · airframe 26,697 hrs · 31,965 cycles

FOUND DOWN LOCK LIGHT SLOW TO EXTINGUISH DURING RETRACTION. FLIGHT CREW REPORTS 2 NORMAL GEAR EXT/RET CYCLES AFTER INITIAL DISCREPANCY EVALUATED DOWN AND UPLOCK SWITCHES VISUALLY AND CLEANED DEBRIS FROM SWITCH AREA.

Part: UNKNOWN — UNKNOWN · airframe 26,675 hrs · 31,945 cycles

AFTER TAKEOFF THE FLT IDLE STOP LIGHT ILLUMINATED. PERFORMED OPERATIONAL CHECK OF FLIGHT IDLE STOP MECHANISM AS PER SAMM 76-10-60-05. NO FAULTS NOTED, OPS CHECK GOOD AT THIS TIME.

Part: TRANSMITTER — MALFUNCTIONED (AOA) · airframe 25,184 hrs · 30,459 cycles

L STALL FAIL LIGHT CAME ON INFLIGHT. REMOVED AND REPLACED LEFT AOA TRANSMITTER IAW SAAB 340 AMM 27-35-05. PERFORMED FUNCTIONAL TEST IAW COLGAN WORK CARD 27-35-06S. NO FAULTS FOUND PN ON/OFF 861AR S/N ON 00060 S/N OFF 01013.

Part: MANIFOLD — DEFECTIVE (HYDRAULIC SYS) · airframe 24,908 hrs · 30,168 cycles

MAIN ACCUM PRESS DROPS TO 2100 PSI ABOUT EVERY 20 SECONDS AFTER T/O DURING CLIMB OUT. HYD PUMP WORKS PROPERLY, FREQ AT PUMP CYCLES SLOW NEAR CRUISE ALTITUDE. A/C REQUIRES OPS FLIGHT CHECK TO VERIFY MAIN HYD PRESS DROP OFF AFTER GEAR RETRACTION. OPERATIONAL FLT CHECK UNSAT. AC CONTINUES TO LOOSE MAIN ACCUM PRESS RAPIDLY (25 SECONDS) AFTER GEAR RETRACT. HOLDS PRESS AFTER GEAR EXTEND. MX VERIFIED PROPER PRESSURE OF ACCUM AND FLUID LEVEL, NO LEAKS NOTED PINED GEAR DOWN. AIRCRAFT WAS FERRIED FROM IAD TO HEF TROUBLESHOOTING AND MAINTENANCE REMOVED AND REPLACED HYDRAULIC PRESSURE MANIFOLD PN ON/OFF 1M1006-1, SN OFF 387, SN ON 427 IAW 29-10-25 LEAK CHECK GOOD, NO LEAKS NOTED.

Part: DUMP VALVE — FAULTY (HYDRAULIC SYS) · airframe 24,408 hrs · 30,167 cycles

AFTER GEAR RETRACTION MAIN HYDRAULIC PRESSURE WOULD DEPLETE RAPIDLY (WITHIN 5 SECONDS) AND HYDRAULIC PUMP WOULD RUN. THIS OCCURRED FOR 10 MINUTES THEN MAIN HYDRAULIC PRESSURE STABILIZED. A/C REQUIRES OPERATIONAL CHECK FLIGHT TO VERIFY HYD PRESSURE PARAMETERS AFTER GEAR RETRACTION. OPERATIONAL FLIGHT CHECK UNSATISFACTORY, AFTER GEAR RETRACTION AND EXTENSION MAIN RESERVOIR PRESSURE CONTINUES TO DEPLETE RAPIDLY. DURING GEAR EXTENSION PUMP CUT OUT INTERMITTENTLY. R&R MAIN AND EMERGENCY ACCUMULATOR PRESSURE DUMP VALVE IAW 29-10-35 LEAK CHECK GOOD. MAIN RESERVOIR PN ON/OFF 3268 SN OFF 1230, SN ON 046; EMERGENCY RESERVOIR PN ON/OFF 3268, SN OFF 123 SN ON 271.

Part: SWITCH — DIRTY (LT MLG) · airframe 24,455 hrs · 29,677 cycles

UPON LANDING IN BOSTON THE LEFT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE, THE INTRANSIT LIGHT WAS OUT AND THE LEFT MAIN LIGHT CAME ON AFTER THE MISSED APPROACH. CLEANED ALL MICRO SWITCHES ON LEFT GEAR AND CHECKED ALL CANNON PLUGS. ALSO INSPECTED LANDING GEAR AND PERFORMED CHECK FLIGHT FOR LANDING GEAR OPERATION, OPS CHECKED GOOD.

Part: INDICATOR — WARNING LIGHT (ENGINE ITT) · airframe 22,970 hrs · 27,925 cycles

LEFT ITT WENT TO 955 DURING TAKEOFF.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,180 hrs · 25,701 cycles

AFT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY IAW MM 33-50-10, OP CHECKED GOOD.