Lights · battery pack · not reportedAug 22, 2017
OVERWING EMERGENCY EVACUATION LIGHT BATTERY PACK OPS CHECK. REPLACED OVERWING EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK IAW AMM 33-53-00 PERFORMED SATISFACTORY OPS CHECK.
From FAA Service Difficulty Reports; matched by N-number and serial number.Stabilizers · bearing · nickedAug 18, 2017
LEFT ELEVATOR NR 1 HINGE BEARING NICKED. REMOVED THE HINGE BEARING HOUSING IAW OVERHAUL MANUAL 27-30-1. REMOVED AND REPLACED THE BEARING AND REINSTALLED HINGE HOUSING IAW CMM 27-30-1 AND SOPM 20-10-7.
From FAA Service Difficulty Reports; matched by N-number and serial number.Stabilizers · seal · damagedAug 17, 2017
ON INSTALLATION OF LEFT ELEVATOR TO HORIZONTAL STAB, DAMAGE WAS FOUND ON THE AFT SPAR REAR CAP, XE225. REPAIRED LT HORIZONTAL STAB T/E SPAR SEAL IAW ER/A 398032-14MA.
From FAA Service Difficulty Reports; matched by N-number and serial number.Fuselage · cusp web · crackedAug 16, 2017
ON REMOVAL OF THE RT SIDE FLOOR WEB, A CRACK WAS NOTICED AT FWD CORNER CUT OUT. REPAIRED THE CUSP WEB AT BS 807 IAW SRM 53-05, PAR 144, FIG 131A-21, DWG 9910151, REV BU, REV CH, AND DWG 9930538 REV CE.
From FAA Service Difficulty Reports; matched by N-number and serial number.Electrical power · wire · damagedJun 25, 2017
ACFT DIVERTED, DURING CLIMB OUT, PASSING THROUGH 26K, A STRONG ACRID ODOR BECAME APPARENT IN THE COCKPIT. FLIGHT ATTENDANTS REPORTED SAME ODOR IN CABIN. BEGAN DESCENT DIVERSION. AFTER APPROXIMATELY 1-1.5 MINUTES BOTH OIL TEMP HIGH LIGHTS ILLUMINATED. THROTTLES WERE AT IDLE. PERFORMED QRH…
From FAA Service Difficulty Reports; matched by N-number and serial number.Wings · structure · puncturedJun 7, 2017
DURING A SERVICE CHECK, FOUND A DENT WITH A PUNCTURE ON BACKSIDE OF RT NR 1 SLAT, 45 INCHES FROM INBOARD, 2.25 X 1.87 L X .195 DEEP. REMOVED AND REPLACED THE SLAT IAW AMDS CARD 2700-4224-RH-01.
From FAA Service Difficulty Reports; matched by N-number and serial number.Stabilizers · skin · crackedJan 22, 2017
HORIZONTAL STABILIZER UPPER RT AFT SKIN PANEL CRACKED. DRILLED END CRACK 0.250 DRILLED IAW SR09550028. ENLARGE STOP DRILL IAW SR09550028 STEP 42. HFEC INSP AREA IAW NDTM 06-1001.001 NO DEFECTS NOTED. ALODINED & PRIMED. SEALED AREA REINSTALLED FILLER AND APPLIED 2 LAYERS SPEED TAPE AND SEALED.
From FAA Service Difficulty Reports; matched by N-number and serial number.