N413DA
Registered owner: BARTKOWSKI TIMOTHY, WA (owner ≠ operator)
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, 1995-02-22 – 2000-06-16.
Part: ENGINE — FLAMED OUT (NR 1) · airframe 60,956 hrs · 55,604 cycles
APROX 20 SECONDS AFTER TAKEOFF NR 1 ENGINE FLAMED OUT WITH NO OTHER ABNORMAL INDICATIONS OR SOUNDS NOTED BY FLIGHT CREW. REPLACED NR 1 ENGINE DRIVEN FUEL PUMP AND FUEL CONTROL UNIT PER MM. RAN AND ADJUSTED NR 1 ENGINE FUEL CONTROL PER PFHB AND MM, ALL PARAMETERS AND LEAK CK GOOD.
Part: BATTERY — DISCHARGED (AIRSTAIR)
AFT AIRSTAIR EMERGENCY LIGHT FOUND INOP. REPLACED BATTERIES DUE LOW VOLTAGE, CHECKS NORMAL.
Earlier reports · 1995–1999 · 17 reports
1999
Part: SKIN — PUNCTURED (FS 440, S-21R)
FUSELAGE SKIN FS 440-460, STRG 20R-21R, CUTOUT REPAIR. THE FUSELAGE SKIN WAS PUNCTURED BETWEEN FS 440 AND 460 AND BETWEEN STRINGERS 20R AND 21R. THE SKIN SPLICE STRAP AT FS 440 WAS SEVERED. THE SKIN DAMAGE WAS REMOVED WITH A 12 BY 8 CUTOUT AND THE DAMAGED SECTION OF SPLICE STRAP WAS CUT OUT. THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND THE SPLICE STRAP WAS REPAIRED WITH AN INTERNAL TITANIUM STRAP PER ER/A 368750-14.
Part: FUEL PUMP — FAILED (NR 1 ENGINE)
NR 1 ENGINE QUIT RIGHT AFTER ROTATION ON TAKEOFF FLIGHT. ATTENDENT REPORTED A POPPING NOISE NO OTHER ABNORMAL IND, FUEL PUMP SHAFT SHEARED. REPLACED SAME AND CONTROL.
1998
Part: WEB — CRACKED (BS 1290)
RT TORQUE BOX VERT WEB CRACKED AT LIGHTENING HOLES STA 1290 AND 1235 RT. REPAIRED PER MM 53-11-0 PG 832.
Part: SKIN — CRACKED (FUSELAGE)
A .5 INCH CRACK FUSELAGE SKIN AT L-4 WINDOW I/B FWD ATTACH SCREW. REPAIRED PER SRM 53-30-3.
Part: SIGN — INOPERATIVE (R1 DOOR)
R1 OVERHEAD EMERGENCY EXIT SIGN WILL NOT ILLUM WHEN SELECTED. REPLACED R1 OVERHEAD EMERGENCY EXIT LIGHT ASSY, CKS NML.
1997
Part: POWER SUPPLY — INOPERATIVE (CABIN)
AFT EMERGENCY EXIT PATH LIGHTS INOP. CHANGED PWR SUPPLY, OPS NORMAL.
Part: PACK — FAILED (RT PACK)
RT PACK TRIPS OFF REPEATEDLY, SMOKES IN CABIN. FLIGHT CREW PLACARD DISP NR 72.
1996
Part: DOUBLER — DAMAGED (GALLEY DOOR)
INSTALLED REPAIR DOUBLER PER SRM 52-00-3 SKIN WAS DAMAGED AT THE UPPER FWD CORNER.
Part: ANGLE — CRACKED (NR 7 LE FLAP)
SKIN ANGLE CRACKED PAST PREVIOUS ROUT OUT BELOW NR 7 SLAT TAI DUCT. REPAIRED PER M/M 57-54-0 PG 807A.
Part: ANGLE — CRACKED (NR 3 LE FLAP)
NR 3 SLAT INBD STOP PAD ANGLE CRACKED. REPAIRED PER M/M 57-54-0 FIG 812.
Part: SKIN — CORROSION (BS 720)
CORROSION WAS FOUND ON THE RAM AIR ACTUATOR ACCESS DOOR CUTOUT AT THE FWD LT CORNER. THE CORROSION WAS CUTOUT AND REPAIRED WITH AN EXTERNAL AND AN INTERNAL DOUBLER PER FAA/DER FORM 8110-3, DATED 1-5-96.
Part: FLOORBEAM — CORRODED (BS 360)
CORROSION FOUND ON FLOORBEAM UPPER ANGLE STA 360 LBL 20 TO RBL 14. INSTALLED REPAIR DOUBLERS PER M/M 53-20-11 PG 802 TO 803.
Part: FLOOR CHANNEL — CORRODED (BS 1110)
FOUND ON MV 1, CORROSION ON FLOOR SUPPORT CHANNEL FWD SIDE TOP LEG STA 1110, LBL 9 AROUND FLOOR PANEL HOLE. REPAIRED PER M/M 53-20-11.
1995
Part: SKIN — CRACKED (PAX DR CUTOUT)
MAIN ENTRY DOOR LWR HINGE CUTOUT AT FUSELAGE SKIN CRACKED 1.5 INCH. CRACK WAS FOUND DURING A-2 LETTER CHECK. REPAIRED PER MM 53-30-0 PG 821.
Part: WEB — CRACKED (FS 1233)
1 INCH CRACK AT LIGHTNING HOLE CUTOUT FLANGE STA 1233L. CRACK WAS FOUND DURING A-2 LETTER CK. INSTALLED DOUBLER PER MM 53-11-0 PG 828.
Part: ANGLE — CRACKED (NR 2 ENG CUTOUT)
DURING A-2 LETTER CHECK, FOUND ANGLE DAMAGED AT FWD LWR NR 2 ENG CUTOUT. REPAIRED PER MM 53-11-0 PG 801.
Part: EEL BULB — FAILED (CABIN)
DURIING PREFLIGHT FOUND SEVERAL LIGHTS OUT IN FLOOR ESCAPE PATH TRACK LIGHTS, RELAMPED, OPERATION NORMAL.