# Service difficulty reports: N413DA, cancelled Oct 13, 2000 A list on [N413DA, cancelled Oct 13, 2000](https://openairdocs.org/deregistered/N413DA-2000-10-13.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DL72K001172](https://openairdocs.org/sdr/DL72K001172.md): Engine · flamed out · Jun 16, 2000 · N413DA · Boeing 727232 · Engine (Turbine/Turboprop) > 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 PARAME - [SDR DL72K000299](https://openairdocs.org/sdr/DL72K000299.md): Battery · discharged · Feb 12, 2000 · N413DA · Boeing 727232 · Emergency Lighting > AFT AIRSTAIR EMERGENCY LIGHT FOUND INOP. REPLACED BATTERIES DUE LOW VOLTAGE, CHECKS NORMAL. - [SDR DL72K992529](https://openairdocs.org/sdr/DL72K992529.md): Skin · punctured · Nov 15, 1999 · N413DA · Boeing 727232 · Fuselage Main, Plate/Skin > 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 S - [SDR DL72K991526](https://openairdocs.org/sdr/DL72K991526.md): Fuel Pump · failed · Jul 7, 1999 · N413DA · Boeing 727232 · Engine Fuel Pump > 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. - [SDR DL72K982156](https://openairdocs.org/sdr/DL72K982156.md): Skin · cracked · Oct 16, 1998 · N413DA · Boeing 727232 · Fuselage Main, Plate/Skin > A.5 INCH CRACK FUSELAGE SKIN AT L-4 WINDOW I/B FWD ATTACH SCREW. REPAIRED PER SRM 53-30-3. - [SDR DL72K982155](https://openairdocs.org/sdr/DL72K982155.md): Web · cracked · Oct 16, 1998 · N413DA · Boeing 727232 · Fuselage Miscellaneous Structure > RT TORQUE BOX VERT WEB CRACKED AT LIGHTENING HOLES STA 1290 AND 1235 RT. REPAIRED PER MM 53-11-0 PG 832. - [SDR DL72K980085](https://openairdocs.org/sdr/DL72K980085.md): Sign · inoperative · Jan 12, 1998 · N413DA · Boeing 727232 · Emergency Lighting > R1 OVERHEAD EMERGENCY EXIT SIGN WILL NOT ILLUM WHEN SELECTED. REPLACED R1 OVERHEAD EMERGENCY EXIT LIGHT ASSY, CKS NML. - [SDR DL72K971800](https://openairdocs.org/sdr/DL72K971800.md): Power Supply · inoperative · Sep 14, 1997 · N413DA · Boeing 727232 · Emergency Lighting > AFT EMERGENCY EXIT PATH LIGHTS INOP. CHANGED PWR SUPPLY, OPS NORMAL. - [SDR DL72K970520](https://openairdocs.org/sdr/DL72K970520.md): Pack · failed · Mar 20, 1997 · N413DA · Boeing 727232 · Cabin Cooling System > RT PACK TRIPS OFF REPEATEDLY, SMOKES IN CABIN. FLIGHT CREW PLACARD DISP NR 72. - [SDR DL72K962069](https://openairdocs.org/sdr/DL72K962069.md): Doubler · damaged · May 13, 1996 · N413DA · Boeing 727232 · Galley Doors > INSTALLED REPAIR DOUBLER PER SRM 52-00-3 SKIN WAS DAMAGED AT THE UPPER FWD CORNER. - [SDR DL72K961123](https://openairdocs.org/sdr/DL72K961123.md): Angle · cracked · May 10, 1996 · N413DA · Boeing 727232 · Leading Edge Devices > NR 3 SLAT INBD STOP PAD ANGLE CRACKED. REPAIRED PER M/M 57-54-0 FIG 812. - [SDR DL72K961121](https://openairdocs.org/sdr/DL72K961121.md): Angle · cracked · May 10, 1996 · N413DA · Boeing 727232 · Leading Edge Devices > SKIN ANGLE CRACKED PAST PREVIOUS ROUT OUT BELOW NR 7 SLAT TAI DUCT. REPAIRED PER M/M 57-54-0 PG 807A. - [SDR DL72K960128](https://openairdocs.org/sdr/DL72K960128.md): Skin · corrosion · Jan 5, 1996 · N413DA · Boeing 727232 · Fuselage Main, Plate/Skin > 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. - [SDR DL72K960014](https://openairdocs.org/sdr/DL72K960014.md): Floorbeam · corroded · Jan 3, 1996 · N413DA · Boeing 727232 · Fuselage Main, Floor Beam > 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. - [SDR DL72K960013](https://openairdocs.org/sdr/DL72K960013.md): Floor Channel · corroded · Jan 3, 1996 · N413DA · Boeing 727232 · Fuselage Miscellaneous Structure > 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. - [SDR DL72K950826](https://openairdocs.org/sdr/DL72K950826.md): Angle · cracked · Feb 24, 1995 · N413DA · Boeing 727232 · Fuselage Miscellaneous Structure > DURING A-2 LETTER CHECK, FOUND ANGLE DAMAGED AT FWD LWR NR 2 ENG CUTOUT. REPAIRED PER MM 53-11-0 PG 801. - [SDR DL72K950824](https://openairdocs.org/sdr/DL72K950824.md): Skin · cracked · Feb 24, 1995 · N413DA · Boeing 727232 · Fuselage Main, Plate/Skin > 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. - [SDR DL72K950823](https://openairdocs.org/sdr/DL72K950823.md): Web · cracked · Feb 24, 1995 · N413DA · Boeing 727232 · Fuselage Miscellaneous Structure > 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. - [SDR DL72K950820](https://openairdocs.org/sdr/DL72K950820.md): Eel Bulb · failed · Feb 22, 1995 · N413DA · Boeing 727232 · Emergency Lighting > DURIING PREFLIGHT FOUND SEVERAL LIGHTS OUT IN FLOOR ESCAPE PATH TRACK LIGHTS, RELAMPED, OPERATION NORMAL. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N413DA' AND deregistration_id = 'N413DA-2000-10-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N413DA-2000-10-13/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.