N202KD
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.
20 reports on file, 1995-01-23 – 2000-07-14.
Part: ENGINE — OVERTEMP (RIGHT)
LIT - FLT 3290 - RIGHT ENGINE ON DERIVATIVE POWER. ON TAKEOFF ITT REACHED 932 DEGREES C AT 94 PERCENT TORQUE AT 35 DEGREE CELSIUS. AIRCRAFT IS TO BE RETIRED, ENGINE WILL BE REPLACED PRIOR TO BEING SOLD OR RETURNED TO SAAB. ENGINE WAS REMOVED AND REPLACED IAW SAAB MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. (M)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,972 hrs · 21,731 cycles
DFW - FLT 3304 - FLOOR PROXIMITY EMERGENCY ESCAPE LIGHT INOPERABLE AT 7B, ISSUED MEL 33-15-2. CLOSING ACTION: REMOVED AND REPLACED HOLDER AT 7B IAW 33-50-20. MEL CLEARED AND RESTORED. OPS CHECKED GOOD. (X)
Part: BULB — FAILED (CABIN)
DFW - FLT 3640 - OVERHEAD EMERGENCY LIGHT AT 12 B/C INOPERATIVE. REMOVED AND REPLACED BULB AT 12 B/C. OPS CHECK GOOD. (M)
Earlier reports · 1995–1999 · 17 reports
1999
Part: SMOKE DETECTOR — MALFUNCTIONED (E/E BAY)
DFW - FLT 3252 - AVIONIC SMOKE LIGHT CAME ON FOR ABOUT 10 SECONDS THEN WENT OUT. NO OTHER SIGNS OF SMOKE. REMOVED AND REPLACED AVIONIC SMOKE DETECTOR. OPS CHECK GOOD. (M)
Part: LAMP — FAILED (COCKPIT)
DFW - FLT 3252 - EMERGENCY ARMED LIGHT ON F/A PANEL INOPERATIVE. REMOVED AND REPLACED LAMP ON F/A PANEL. OPS CHECK GOOD. (M)
Part: LONGERON — PUNCTURED (RT NACELLE)
ABI - DURNG MBV INSPECTION, A PUNCTURE DUE TO CHAFING WAS DISCOVERED IN RIGHT NACELLE OUTBOARD LOWER LONGERON AT NS 289.33. BLENDED DAMAGED SURFACE TO VERY FINE SURFACE TEXTURE. PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED REINFORCEMENT ANGLE. APPLIED SURFACE TREATMENT ON THE EDGE OF THE DAMAGE AND THE REINFORCEMENT ANGLE. INSTALLED ANGLE IN NACELLE. WORK DONE IAW SAAB REPAIR STATEMENT 72SDS1354 AND SAAB 340 SRM STANDARD PRACTICES. AIRCRAFT OK FOR SERVICE. (M)
Part: SKIN — CHAFED (FUSELAGE)
ABI - DURING MBV INSPECTION, A CHAF WAS DISCOVERED IN THE REAR LEFT FUSELAGE PANEL AT THE HORIZONTAL STABILIZER LEADING EDGE SEAL. LIGHTLY BLENDED CHAFED AREA TO A FINE SURFACE FINISH. PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED EXTERNAL DOUBLER .025 THICK. APPLIED SURFACE TREATMENT TO BLENDED AREA AND DOUBLER. INSTALLED CHAFING PROTECTION. RESTORED PAINT FINISH. WORK DONE IAW SAAB REPAIR STATEMENT 72SDS1354 AND SAAB 340 SRM STANDARD PRACTICES. AIRCRAFT OK FOR SERVICE. (M)
Part: SKIN — CHAFED (FUSELAGE)
DURING MBV INSPECTION, CHAF WAS DISCOVERED IN THE REAR RIGHT FUSELAGE PANEL AT THE HORIZONTAL STABILIZER LEADING EDGE SEAL. LIGHTLY BLENDED CHAFED AREA TO A FINE SURFACE FINISH. PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED EXTERNAL DOUBLER .025 THICK. APPLIED SURFACE TREATMENT TO BLENDED AREA AND DOUBLER. ATTACHED DOUBLER TO DAMAGED AREA, RESTORED PAINT FINISH. WORK DONE IAW SAAB REPAIR STATEMENT 72SDS1354 AND SAAB 340 SRM STANDARD PRACTICES. AIRCRAFT OK FOR SERVICE. (M)
Part: SKIN — CHAFED (RT NACELLE)
ABI - DURING MBV INSPECTION, CHAFE WAS DISCOVERED IN THE RIGHT NACELLE INBOARD SKIN AT FILLET FAIRING. BLENDED OUT DAMAGE FROM CHAFING TO VERY FINE SURFACE FINISH. PERFORMED EDDY CURRENT INSPECTION OF AREA WITH NO DEFECTS NOTED. FABRICATED DOUBLER .050 THICK AND CONTOUR TO NACELLE PANEL AND CUT TO DIMENSION. APPLIED SURFACE TREATMENT, INSTALLED DOUBLER IN RT NACELLE. RESTORED FINISH PAINT. WORK DONE IAW SAAB REPAIR STATEMENT 72SDS1354 AND SAAB 340 SRM STANDARD PRACTICES. AIRCRAFT OK FOR SERVICE. (M)
Part: SKIN — DENTED (BS 339-363)
ABI - DURING MBV INSPECTION, A DENT WAS DISCOVERED IN THE LEFT FUSELAGE CABIN SKIN JUST AFT OF THE ICE SHIELD BETWEEN STATION 339 AND STATION 363 AND BETWEEN SL 1515 AND SL 1516. STRAIGHTENED DENT OUT TO NORMAL CONTOUR. PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED TWO EXTERNAL DOUBLERS .050 THICK ONE MEASURING 4 INCH BY 11.25 INCH AND THE OTHER MEASURING 5 INCH BY 12.5 INCH. APPLIED SURFACE TREATMENT OF ALODINE AND EPOXY PRIMER TO REPAIR AREAS DOUBLERS AND CUT EDGES. INSTALLED DOUBLERS TO FUSELAGE. APPLIED SURFACE FINISH. WORK DONE IAW SAAB 340 SRM 53-70-10 PAGE 217 FIG 210 AND PAGE 218. AIRCRAFT OK FOR SERVICE. (M)
Part: SEAT TRACK — CORRODED (BS 638-686)
ABI - DURING MBV INSPECTION SEAT TRACK BL 0 TO STATION 638-686 WAS FOUND CORRODED. CUT OUT 47.5 INCH SECTION OF SEAT TRACK DEBURRED, ALODINE, PRIMERED, AND PAINTED EDGES. FABRICATED A 47.5 INCH LONG EXTRUSION OF 4650000-043 SHPAL 7075-T76511. FABRICATED A 15 INCH U-BEAM OF PLAL-7075-T7351 MATERIAL, DEBURRED, ALODINE, AND PAINTED. POSITIONED REPAIR BEAM INSIDE EXISTING TRACK AND INSTALLED IN AIRCRAFT. REPAIR DONE IAW SAAB SRM 53-70-60 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M)
1996
Part: ADI — FAILED (RT COCKPIT)
FLT NR 5751 - MIA - PILOT REPORT, FIRST OFFICERS ADI WENT BLANK AND SMOKE WAS SMELLED IN THE COCKPIT. REMOVED AND REPLACED FIRST OFFICERS ADI. (M)
Part: BEARING — CRACKED (GC 49 GEARCASE)
GEAR CASE WAS RETURNED FOR OIL CONTAMINATION. UNIT WAS DISASSEMBLED AND AN EXAMINATION OF INTERNAL HARDWARE REVEALED A CRACKED INNER RACE ON THE PROPELLER SHAFT FORWARD ROLLER BEARING RACE. LEFT - TSI 4,239.5 HRS. CSI, 4,048.
1995
Part: OVERHEAT SENSOR — MALFUNCTIONED (RT NACELLE)
FLT 4943 - DCA - RIGHT ENGINE TAIL PIPE HOT LIGHT ILLUMINATED AFTER TAKEOFF AT 300 FEET. CREW FOLLOWED EMERGENCY CHECKLIST AND SHUT DOWN RIGHT ENGINE. WARNING PERSISTED. WARNINGS STOPPED AFTER BOTH FIRE BOTTLES WERE DISCHARGED. SYSTEM INSPECTIONS SATISFACTORY. RERACKED WEU. 30 MINUTE ENGINE RUN PERFORMED, OPS CHECKED GOOD. REPLACED 2 FIRE BOTTLES AND SQUIBBS.
Part: CONTROL CABLE — CHAFED (FS 389.0)
DURING ROUTINE C-CHECK INSPECTION, FOUND ELEVATOR PRIMARY FLIGHT CONTROL CABLES CHAFED BY FAIRLEADS AT FS 389.0. CABLE DIAMETER ORIGINALLY IS 0.163 INCH, MEASURED DIAMETER AT CHAFED AREA IS 0.140 INCH. REMOVED AND REPLACED BOTH ELEVATOR PRIMARY FLIGHT CONTROL CABLES.
Part: CONTROL CABLE — CHAFED (FS 389.0)
DURING ROUTINE C-CHECK INSPECTION, FOUND ELEVATOR PRIMARY FLIGHT CONTROL CABLES CHAFED BY FAIRLEADS AT FS 389.0. CABLE DIAMETER ORIGINALLY IS 0.163 INCH, MEASURED DIAMETER AT CHAFED AREA IS 0.140 INCH. REMOVED AND REPLACED BOTH ELEVATOR PRIMARY FLIGHT CONTROL CABLES.
Part: ELEV CONTL CABLE — CHAFED (FS 389.0)
BNA - DURING ROUTINE C-CHECK INSPECTION, FOUND ELEVATOR PRIMARY CABLES CHAFED BY FAIRLEADS AT FS 389.0. CABLE DIAMETER ORIGINALLY WAS 0.163, MEASURED DIAMETER AT CHAFED AREA IS 0.140. REMOVED AND REPLACED BOTH PRIMARY FLIGHT CONTROL CABLES.
Part: ELEV CONTL CABLE — CHAFED (FS 389.0)
BNA - DURING ROUTINE C-CHECK INSPECTION, FOUND ELEVATOR PRIMARY CABLES CHAFED BY FAIRLEADS AT FS 389.0. CABLE DIAMETER ORIGINALLY WAS 0.163, MEASURED DIAMETER AT CHAFED AREA IS 0.140. REMOVED AND REPLACED BOTH PRIMARY FLIGHT CONTROL CABLES.
Part: CABLES — CHAFED (FS 389)
DURING ROUTINE C-CHECK INSPECTION, FOUND ELEVATOR PRIMARY FLIGHT CONTROL CABLES CHAFED BY FAIRLEADS AT FUSELAGE STATION 389.0. CABLE DIAMETER ORIGINALLY IS .163 INCH, MEASURED DIAMETER AT CHAFED AREA IS .140 INCH. REMOVED AND REPLACED BOTH ELEVATOR PRIMARY FLIGHT CONTROL CABLES.
Part: CABLES — CHAFED (FS 389)
DURING ROUTINE C-CHECK INSPECTION, FOUND ELEVATOR PRIMARY FLIGHT CONTROL CABLES CHAFED BY FAIRLEADS AT FUSELAGE STATION 389.0. CABLE DIAMETER ORIGINALLY IS .163 INCH, MEASURED DIAMETER AT CHAFED AREA IS .140 INCH. REMOVED AND REPLACED BOTH ELEVATOR PRIMARY FLIGHT CONTROL CABLES.