N68079

HEYING PDQ-2 Minor injury Part 91 — operator not named in the NTSB record

ATA 3416

Part: ADC — INOPERATIVE (COCKPIT) · airframe 63,667 hrs · 21,301 cycles

DURING CLIMB OUT, PASSING 12,000 FT, RECEIVED AN ALT DISAGREE AMBER EICAS. ALSO, INTERMITTENT IAS DISAGREE. RAN QRH AND LEVELED AT FL260. CAPTAIN`S ALTIMETER AT 14,000 FT AND F/O'S SHOWED 13,750 FT. CAPTAIN`S ALTIMETER AT FL 240, F/O'S INDICATED FL 237. AT FL 260 ON CAPTAIN`S ALTIMETER, F/O'S INDICATED 25,640 FT. REMOVED AND REPLACED THE RIGHT AIR DATA COMPUTER IAW MM 34-12-01-4. ALL TESTS PASSED, AND OPS CHECKED GOOD. OK TO CONTINUE.

ATA 2750

Part: ELECTRONIC UNIT — FAILED (SLATS) · airframe 63,489 hrs · 21,162 cycles

LE SLAT ASSEMBLY ON UPPER EICAS IN FLIGHT. THIS WAS PRECEDED BY THE FLAP INDICATOR NEEDLE RAPIDLY CYCLING BETWEEN UP AND THE MID RANGE POSITION BETWEEN UP AND 1. WHEN MOVED THE FLAP HANDLE FROM UP TO 1, THE LE SLAT ASSYM CAME ON UPPER EICAS WITH MASTER CAUTION. SLATS WERE LOCKED OUT FOR LANDING. BITE CHECKED PROXIMITY ELETRONIC UNIT, MCDP AND FLAP/SLAT ELECTRONICS UNITS, NO FAULTS LOGGED LAST FLIGHT LEG. INSPECTED LEADING EDGE SLAT POS SENSORS FOR OBVIOUS DEFECTS, NONE FOUND. ACCOMPLISHED BITE CHECKS OF THE PSEU AND FSEU PER MM 32-09-04-4, 27-51-01-4 ALL TESTED NORMALLY WITH NO FAULTS. SUSPECT FSEU AT FAULT, REPLACED SAME REF MM 27-51-01-4, AND OPS CHECKED NORMAL PER MM 27-51-01-4, 27-51-45-2-0. CYCLED FLAPS SEVERAL TIMES WITH NO ABNORMAL INDICATION AND NORMAL OPERATION.

ATA 2730

Part: COMPUTER — MALFUNCTIONED (ELEVATOR FEEL) · airframe 61,920 hrs · 20,411 cycles

DURING CLIMB OUT, ELEVATOR FLUTTER FROM 260 KTS UP TO 300 KTS. NO CHANGE WITH AUTO PILOT ON OR OFF. R & R THE ELEVATOR FEEL COMPUTER.

ATA 7830

Part: RELAY — INOPERATIVE (THRUST REVERSER) · airframe 61,383 hrs · 20,115 cycles

DURING PUSHBACK, REV ISLN, LIGHT ON THROTTLE QUADRANT ILLUMINATED. ADVISED MX THEY SAID IT WOULD EXTINGUISH AFTER TAKEOFF. AFTER TAKEOFF, REV ISLN, REMAINED ILLUMINATED. FOR SAFETY DID AN AIR TURN BACK. R & R K2157. OPENED CB AIR & GND SYS 1 & REV ISLN LIGHT WENT OUT. OPERATIONS CHECKED NORMAL.

ATA 5753

Part: SKIN — DENTED (TE FLAP) · airframe 61,090 hrs · 19,963 cycles

LEFT WING INBD AFT FLAP, DENTED ON LOWER SURFACE, 50 INCHES FROM INBD END. REPAIRED BY HOT BONDING NEW CONE & DOUBLER ON IAW SRM 57-53-01-2R FIG 201 AND SRM 51-70-10-2R PARAGRAPH 20

ATA 2761

Part: ACTUATOR — LEAKING (SPOILERS) · airframe 605 hrs · 19,708 cycles

DURING CLIMB OUT GOT AN EICAS RT HYD QTY, FOLLOWED SEVERAL MINUTES LATER BY RT HYD PRIME PUMP EICAS. BOTH SYS PRESS & QTY WENT ZERO. DEBRIEFED ENG DRIVEN HYD PUMP WAS NOT SHUT DOWN UNTIL AFTER ZERO PRESS WAS INDICATED. CASE DRAIN FILTER NEEDS TO BE REMOVED & INSPECTED FOR POSSIBLE CONTAMINATION. RT OUTBOARD INBOARD SPOILER ACTUATOR REMOVED AND REPLACED DUE TO LEAKING AT ROD END SEAL IAW AMM 27-61-02-4. LEAK & OPS CHECKED GOOD. OPS AND LEAK CHECKED RIGHT HYDRAULIC SYSTEM. SYSTEM OPS AND LEAK CHECKED GOOD. FLUID QUANTITY LEVEL MAINTAINED AT 100% IAW AMM 29-11-00-6.

ATA 5270

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 600 hrs · 19,517 cycles

AT FL 370 HAD MAIN CARGO DOOR LIGHT, WENT OUT AROUND 16,000 FT. TROUBLESHOT IAW FIM 52-71 FIGURE 104B. PERFORMED FAULT HISTORY IAW FIM 32-09 & FOUND NO FAULTS LOGGED. PERFORMED PSEU BITE TEST & BITE TEST PASSED. PERFORMED RESISTANCE CHECK OF PROXIMITY SENSOR & SENSORS READ WITHIN LIMITS. PERFORMED PSEU TARGET TEST & ALL TARGET TESTS PASSED. INSPECTED GAP CLEARANCE, DOOR CLOSED SENSOR, DOOR LATCHED SENSOR & DOOR LOCKED SENSOR. FOUND SENSOR MISALIGNED WITH TARGET. ADJUSTED IAW MM 52-71-09-2. RETESTED PROXIMITY SENSORS & TARGETS AFTER ADJUSTMENT & ALL TESTS PASSED. MAIN CARGO DOOR INDICATION SYS CHECKED GOOD. CHECKED DOOR WARNING SYS IAW MM 52-71-00-5. ALL CHECKS PASSED OK.

ATA 2121

Part: FAN — FAILED (EQUIPMENT) · airframe 598 hrs · 19,450 cycles

COCKPIT HAS A ELEC BURNING ODOR. FWD EQUIP COOLING SUPPLY FAN INOPERATIVE. FOUND FWD EQ SUP FAN 1, STATUS MESSAGE AS WELL. FAN ALSO OPERATING VERY LOUD. R & R SUPPLY 1 FWD RACK EXHAUST FAN IAW MM 21-58-06-4.