Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR HNAA0200049Line · leakingNR 2 ENGINE OIL PRESSURE FLUX AND WARNING LIGHT ILLUMINATED, SHUT DOWN ENGINE QT 45 PSI, FOUND HOT SECTION SOAKED. CLEANED AND SERVICED ENGINE. NR 2 ENGINE LT NACELLE OIL COOLING LINE REMOVED AND REPLACED O-RINGS. RUN-UP AND LEAK CHECK GOOD.SDR HNAA0100052Angle · crackedNR 2 NACELLE HORSE COLLAR WAS FOUND CRACKED IN RADIUS OF FWD UPPER CLOSING ANGLE JUST ABOVE ENGINE HOIST ATTACH BRACKET. REPAIRED PER EO8-54-01-799.SDR HNAA0100026Light · inoperativeEMERGENCY LIGHTS OUT NR 3 & 4, FRONT RED LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY BASE.SDR HNAA0000080Light · inoperativeNUMBER 1 EMERGENCY FLOOR PATH LIGHT INOP. REPLACED LAMEP MODULE.SDR HNAA0000055Angle · crackedDURING AN UNRELATED INSPECTION FOUND THE KEEL STRUCTURE ANGLE AND WEB UNDER L/H CENTER SEAT RAIL AT STA 405.737 CRACKED FROM PREVIOUS IMPACT DAMAGE. PERFORMED MAJOR REPAIR TO STRUCTURE IAW PIEDMONT EO8-53-00-710.SDR HNAA0000047Engine · out of rigNR 1 ENGINE POWER LEVER WOULD NOT ADVANCE PAST 82 PERCENT TORQUE. AIRCRAFT RETURNED TO THE FIELD. RIGGED AND TRIMMED NR 1 ENGINE.SDR HNAA9900018Shroud · crackedNR 1 ENGINE EXHAUST SHROUD HAS 1 INCH CRACK STA 223.4 AT 4 O'CLOCK POSITION, REAR I/B MOUNT BOLT OF FORWARD RADIATION SHIELD IS PULLED THROUGH, REAR O/B ANGLE BRACKET 1.5 INCH CRACK STA XN276.50, OUTLET SHROUD RING 5 CRACKS AT RIVETS STA XN221.25 FROM 4 TO 6 OSDR HNAA9595504Eel Power Supply · inopFLT NR 3040 - FLL TO TPA - DURING PREFLIGHT WALKAROUND, FOUND THE FIRST 2 RED FLOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED THE POWER SUPPLY AT 3352-PS2. (M)SDR HNAA9592503Connector · failedFLT NR 3066 - MCO-TLH - AFTER GEAR EXTENSION, THE NOSE GEAR SHOWED UNSAFE. PERFORMED ALTERNATE GEAR EXTENSION AND LANDED IN TLH WITHOUT INCIDENT. REMOVED AND REPLACED THE CANNON PLUG FOR THE DRAG STAY SENSOR. (M)SDR 95ZZZX6134Autofeather Sw · failedTPA/MIA - FLT 3005 - THE AUTOFEATHER ARM LIGHT FLICKERED AND WENT OUT DURING TAKEOFF. THE AIRCRAFT CONTINUED ON TO MIA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE PROPELLER AUTOFEATHER SWITCH AND THE NR 1 BRAIDED ENGINE HARNESS FROM FIREWALL TO EECSDR 95ZZZX6133Engine Harness · failedTPA/MIA - FLT 3005 - THE AUTOFEATHER ARM LIGHT FLICKERED AND WENT OUT DURING TAKEOFF. THE AIRCRAFT CONTINUED ON TO MIA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE PROPELLER AUTOFEATHER SWITCH AND THE NR 1 BRAIDED ENGINE HARNESS FROM FIREWALL TO EECSDR 95ZZZX6128Tq Control Unit · failedTPA/JAX - FLT 3166 - AFTER TAKEOFF DURING CLIMB, THE AUTOFEATHER ARM LIGHT ILLUMINATED INTERMITTENTLY. THE AIRCRAFT CONTINUED ON TO JAX AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 2 TORQUE SENSOR CONTROL UNIT.SDR 95ZZZM517Switch · failedFLT NR 3031 - TPA-JAX - THE AUTOFEATHER ARM LIGHT FLICKERED ON AND OFF SEVERAL TIMES DURING TAKEOFF. THE AIRCRAFT CONTINUED ON TO JAX AND LANDED WITHOUT INCIDENT. GROUND RUN UP WAS COMPLIED WITH IN JAX AND THE AUTOFEATHER OPERATED NORMALLY. COULD NOT DUPLICSDR 95ZZZX5153Autofeather Sw · dirtyMCO/TLH - FLT 3092 - ON TAKEOFF ROLL, AUTOFEATHER WOULD NOT ARM WHEN POWER LEVERS ADVANCED TO TAKEOFF SETTINGS. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. CLEANED NR 1 AND NR 2 AUTOFEATHER MICROSWITCHES.