N52616
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
19 reports on file, 2004-02-22 – 2009-09-05.
Part: SKIN — CRACKED (FUSELAGE)
DURING SCHEDULED INSPECTION, FOUND EXTERIOR SKIN AT LOWER FWD CORNER OF AFT CARGO COMPT DOOR FRAME HAS CRACK INDICATION AND SIGNS OF GALLING FROM SCUFF PLATE
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,281 hrs · 21,721 cycles
EMERGENCY LIGHT BURNED OUT OVER RIGHT REAR SERVICE DOOR. CHARGED BATTERY PACK OPS. CHECKED GOOD.
Part: SKIN — DENTED (BS 927-947)
DURING SCHEDULED INSP, FOUND DENT ON FUSELAGE BELLY SKIN BETWEEN FRAMES AT BS 927-947, S25-27R. REVISION SEE ITEM (G)
Earlier reports · 2004–2007 · 16 reports
2007
Part: STRINGER — CRACKED (BS 360 S16L) · airframe 36,796 hrs · 19,438 cycles
INSPECTION FOUND STRINGER 16L CHANNEL CRACKED AT FASTENER HOLE COMMON TO WEB AND CLIP AT STA 360. MULTIPLE CRACKS WERE FOUND IN THE SAME LOCATION, REPAIRED IAW ECRA 5311-01378.
Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 36,796 hrs · 19,438 cycles
INSPECTION FOUND LIGHT SURFACE CORROSION AROUND FASTENER HOLES ALONG FLOORBEAM AT STA 986.5, LBL 55 TO RBL 55.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 36,796 hrs · 19,438 cycles
INSPECTION FOUND A .5 INCH CRACK IN RT HORIZONTAL STABILIZER SKIN FROM STAB STA 97-126. A PERMANENT REPAIR WAS PERFORMED BY INSTALLING A DOUBLER IAW ECRA 5510-01724, REV A.
Part: INTERCOSTAL — CRACKED (BS 348.2-360) · airframe 36,796 hrs · 19,438 cycles
INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL BETWEEN BS 348.2 AND BS 360.0, S16L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 53-10-04, REPAIR 2, FIGURE 201.
Part: DOOR FRAME — CRACKED (BS 440-460) · airframe 36,796 hrs · 19,438 cycles
INSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO DOOR AFT FRAME AT LOWER DOOR STOP AREA, STA 440-460, S14R TO S27R. THE AFT FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02.
Part: FRAME — CRACKED (BS 400 S8-9R) · airframe 36,796 hrs · 19,438 cycles
INSPECTION FOUND A 0.2 INCH CRACK IN FRAME AT STA 400 BETWEEN STRINGERS 8R AND 9R. THE CRACKED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5310-04672.
Part: SKIN — CRACKED (BS 219.8-227.8) · airframe 36,796 hrs · 19,438 cycles
INSPECTION FOUND A .75 INCH CRACK IN EXTERIOR FUSELAGE SKIN AT CAPTAIN'S WINDSHIELD O/B CORNER, STA 219.8-227.8, S9L. THE SKIN WAS REPAIRED IAW SRM 53-10-01, FIGURE 201, REPAIR 10.
Part: FRAME — CRACKED (BS 520 S8-9R) · airframe 36,796 hrs · 19,438 cycles
INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 520 BETWEEN STRINGERS 8R AND 9R. THE CRACKED AREA WAS CUT OUT AND REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04672.
Part: FRAME — CRACKED (BS 380 S8-9R) · airframe 36,796 hrs · 19,438 cycles
INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 380 BETWEEN STRINGERS 8R AND 9R. THE CRACKED AREA WAS CUT OUT AND REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04672.
Part: FRAME — CRACKED (BS 400 S8-9L) · airframe 36,796 hrs · 19,438 cycles
INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 400 BETWEEN STRINGERS 8L AND 9L. REPAIR ANGLES WERE INSTALLED IAW ECRA 5310-04672.
Part: FRAME — CRACKED (BS 440 S8-9L) · airframe 36,796 hrs · 19,438 cycles
INSPECTION FOUND A .25 INCH CRACK IN FRAME AT STA 440 BETWEEN STRINGERS 8L AND 9L. THE CRACKED AREA WAS CUT OUT AND REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04672.
2006
Part: WINDOW — CRACKED (COCKPIT) · airframe 33,977 hrs · 17,968 cycles
F/O FWD WINDOW CRACKED AFTER TAKEOFF. REPLACED WINDOW IAW AMM 56-11-11.
Part: BATTERY PACK — INOPERATIVE (ROWS 21-24) · airframe 32,700 hrs · 17,301 cycles
THE SEAT EMERGENCY LIGHTS AT ROWS 21-24 WERE FOUND INOPERATIVE. THE RT AFT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-51.
2005
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,624 hrs · 16,236 cycles
INSPECTION FOUND THE LAST FOUR ROWS OF EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK IN THE AFT GALLEY OVERHEAD WAS REMOVED AND REPLACED.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,617 hrs · 16,232 cycles
INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STA 947.5, LBL 15 TO RBL 15. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-51, PAGE 212-215.
2004
Part: SKIN — CRACKED (HORIZ STAB) · airframe 27,728 hrs · 14,755 cycles
INSPECTION FOUND TWO 1 INCH CRACKS IN RT LOWER HORIZONTAL STABILIZER SKIN AT REAR SPAR STA 100 AND 129. A REPAIR WAS INSTALLED IAW ECRA 5510-01724.