# Service difficulty reports: N461AT, cancelled Sep 15, 2000 A list on [N461AT, cancelled Sep 15, 2000](https://openairdocs.org/deregistered/N461AT-2000-09-15.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AT9900095](https://openairdocs.org/sdr/AT9900095.md): Bulb · failed · Feb 6, 1999 · N461AT · Boeing 7372E1 · Emergency Lighting > DURING SCHEDULED MAINTENANCE FOUND EXTERIOR EMERGENCY LIGHT AT L-2 DOOR AND AFT SERVICE DOOR INOPERATIVE. RELAMPED BOTH EMERGENCY LIGHT AND OPS CHECKED THE SYSTEM IAW MM 33-00. - [SDR VJ9800286](https://openairdocs.org/sdr/VJ9800286.md): Battery Pack · discharged · Aug 24, 1998 · N461AT · Boeing 7372E1 · Emergency Lighting > FORWARD LT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK; OPS CHECKED GOOD. - [SDR VJ9800205](https://openairdocs.org/sdr/VJ9800205.md): Skin · cracked · Jun 1, 1998 · N461AT · Boeing 7372E1 · Fuselage Main, Plate/Skin > DURING C-CHECK, FOUND DOOR FRAME WEB SKIN CRACKED AT AFT CARGO FWD LANDING AT FS 784 RS 23 ABOVE LOWER STOP PAD. - [SDR VJ9800204](https://openairdocs.org/sdr/VJ9800204.md): Support · corroded · Jun 1, 1998 · N461AT · Boeing 7372E1 · Fuselage Miscellaneous Structure > DURING C-CHECK, FOUND FLOORBOARD SUPPORT HAS I/G CORROSION AT FS 294 TO 306 LBL 12. - [SDR VJ9800203](https://openairdocs.org/sdr/VJ9800203.md): Angle · corroded · May 18, 1998 · N461AT · Boeing 7372E1 · Fuselage Miscellaneous Structure > DURING C-CHECK, FOUND MAIN CABIN FS 277 RBL 12 FLOOR SUPORT ANGLE HAS HEAVY SURFACE CORROSION. REMOVED CORROSION AND INSTALLED L-ANGLE REPAIR IAW 737 SRM 51-20-2. - [SDR VJ9800150](https://openairdocs.org/sdr/VJ9800150.md): Light · inoperative · May 8, 1998 · N461AT · Boeing 7372E1 · Emergency Lighting > FWD EMERGENCY PATH LIGHTING INOP. FERRIED AC TO MCO, THEN ONTO DHN FOR C CHECK WHERE IT WILL BE FIXED. - [SDR VJ09800053](https://openairdocs.org/sdr/VJ09800053.md): Deflector · inoperative · Mar 22, 1998 · N461AT · Boeing 7372E1 · Emergency Lighting > DURING LAYOVER CHECK, FOUND L-1 DOOR EMERGENCY EXIT ESCAPE SLIDE LIGHT INOP. REPLACED LIGHT DEFLECTOR ASSY. (M) - [SDR VJ9800023](https://openairdocs.org/sdr/VJ9800023.md): Connector · dirty · Feb 20, 1998 · N461AT · Boeing 737268 · Emergency Lighting > AFT SECTION OF EMERGENCY PATH LIGHTING INOPERATIVE. CLEANED AND DRIED CONNECTIONS, OPS CHECKED NORMAL. - [SDR ZZDA3324797](https://openairdocs.org/sdr/ZZDA3324797.md): Light · inoperative · Oct 29, 1997 · N461AT · Boeing 7372E1 · Emergency Lighting > DURING A ROUTINE LAY-OVER CHECK, THE FLIGHT DECK EMERGENCY LIGHT WAS FOUND INOPERABLE. AT STA GSO, DEFERRED THE LIGHT PACK MEL 33-17 M-1398 (OK FOR DAYLIGHT OPS ONLY). AT MCO, REPLACED FLIGHT DECK EMERGENCY LIGHT PACK AND CLEARED THE MEL. (X) - [SDR ZZDA3318597](https://openairdocs.org/sdr/ZZDA3318597.md): Light · dirty · Sep 23, 1997 · N461AT · Boeing 7372E1 · Emergency Lighting > DURING LAYOVER CHECK, FOUND MAINTENANCE ENTRY FLOOR PATH LIGHTING INOPERABLE LAST 10 ROWS AND R2 DOOR LOWER EXIT LIGHT FOUND INOPERABLE. MAINTENANCE TROUBLESHOT E-PATH LIGHT BY INSPECTING BATTERY PACKS, FOUND NO FAULTS. FOUND MOISTURE IN FLOOR TRACK LIGHTING - [SDR 97ZZZM926](https://openairdocs.org/sdr/97ZZZM926.md): Wire · broken · Jul 17, 1997 · N461AT · Boeing 7372E1 · Light System Wiring > DURING A LAY OVER CHECK, A TEST WAS DONE TO THE FLOOR PATH LIGHT SYSTEM AND A SECTION OF LIGHTS WAS NOT WORKING. A BROKEN WIRE WAS FOUND UNDER THE FLOOR CARPETING. THE WIRE WAS REPAIRED PER STANDARD WIRING PRACTICES IAW MANUAL 20-30-12. THE WIRES WERE SECURE - [SDR 97ZZZM665](https://openairdocs.org/sdr/97ZZZM665.md): Pcu · cracked · May 19, 1997 · N461AT · Boeing 7372E1 · Aileron Control System > FLT 741 - MCO - LOST HYDRAULIC 'A' SYSTEM PRESSURE AFTER LANDING AND EXITING THE RUNWAY. QTY WENT TO ZERO. REPLACED 'A' SYSTEM AILERON PCU (PCU HOUSING FOUND TO BE CRACKED). REPLACED 'A' SYSTEM MAIN HYDRAULIC FILTER. NO EVIDENCE OF METAL CONTAMINATION WAS - [SDR 97ZZZM668](https://openairdocs.org/sdr/97ZZZM668.md): Lighting · inoperative · May 7, 1997 · N461AT · Boeing 7372E1 · Emergency Lighting > DURING A TRANSIT CHECK, THE EMERGENCY PATH LIGHTING SYSTEM WAS INOP. ALL OVERHEAD AND DOOR EMERGENCY LIGHTS OPS CHECK NORMAL. REMOVED MOISTURE FROM THE EMERGENCY PATH LIGHTING TRACK. EMERGENCY PATH LIGHTING SYSTEM OPERATIONAL CHECK GOOD IAW B737 MM 33-51-11 - [SDR 97ZZZM669](https://openairdocs.org/sdr/97ZZZM669.md): Battery Pack · discharged · May 6, 1997 · N461AT · Boeing 7372E1 · Emergency Lighting > WHILE PERFORMING A LAY OVER CHECK, EMERGENCY PATH LIGHTING IN THE AFT AISLE WAS INOP. REMOVED AND REPLACED AFT EMERGENCY LIGHTS BATTERY PACK IAW MM 33-51-01. OPERATION CHECK GOOD. (M) - [SDR 97ZZZM666](https://openairdocs.org/sdr/97ZZZM666.md): Fire Loop · crimped · Apr 30, 1997 · N461AT · Boeing 7372E1 · Fire Detection > FLT 581 - MDT-MCO - DIVERTED TO GSO DUE TO LOG ITEM 'APU FIRE WARNING AND BELL INTERMITTENT IN FLIGHT'. APU WAS NOT RUNNING APU FIRE HANDLE PULLED. INSPECTED APU AND FOUND NUMEROUS CRIMPS IN LOWER APU FIRE DETECTION LOOP (FWD). REMOVED AND REPLACED THE APU - [SDR 97ZZZM644](https://openairdocs.org/sdr/97ZZZM644.md): Floorbeam · corroded · Feb 13, 1997 · N461AT · Boeing 7372E1 · Fuselage Main, Floor Beam > 31J - THE FOLLOWING WAS FOUND, AFT CARGO FLOORBEAM STATION 1007 HAS CORROSION RBL 24 TO LBL 40. REMOVED CORRODED AREA, FABRICATED TWO 'L' ANGLES, DIM 31 INCH BY 2 INCH BY 1 INCH AND 27.5 INCH BY 2 INCH BY 1 INCH. FABRICATED T-CAP, 27.6 INCH BY 2 INCH BY 2.8 - [SDR 97ZZZM643](https://openairdocs.org/sdr/97ZZZM643.md): Support · corroded · Feb 13, 1997 · N461AT · Boeing 7372E1 · Fuselage Miscellaneous Structure > 31J - THE FOLLOWING WAS FOUND, AFT CARGO FLOOR SUPPORT STATION 1007 TO 987 LBL 4 TO LBL 24 HAS CORROSION (OUT OF LIMITS). REMOVED FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT, DIMENSIONS 26.5 INBH 1.25 INCH BY 2.1 INCH, AND INSTALLED NEW FLOOR SUPPORT ALL IAW - [SDR 97ZZZM642](https://openairdocs.org/sdr/97ZZZM642.md): Angle · corroded · Feb 13, 1997 · N461AT · Boeing 7372E1 · Fuselage Miscellaneous Structure > 31J - THE FOLLOWING WAS FOUND, MAIN CABIN STATION 990 LBL 10 FLOOR SUPPORT CORRODED BEYOND LIMITS. FABRICATED NEW FLOOR SUPPORT STRAP, DIMENSIONS 14 INCH BY 3 INCH AND 10 INCH BY 3 INCH, AND INSTALLED STRAPS ALL IAW B737 SRM 51-20-1 AND 51-30-2. N/R NR 17N1- - [SDR 97ZZZM637](https://openairdocs.org/sdr/97ZZZM637.md): Angle · corroded · Feb 13, 1997 · N461AT · Boeing 7372E1 · Fuselage Miscellaneous Structure > 31J - THE FOLLOWING WAS FOUND, MAIN CABIN STATION 989.0 LBL 10 FLOOR SUPPORT ANGLE CORRODED BEYOND LIMITS. REMOVED CORRODED ANGLE, FABRICATED NEW ANGLE. DIMENSIONS 8 INCH BY 1 INCH BY 1.25 INCH, AND INSTALLED ALL IAW B737 SRM 51-30-2, 51-40-4, AND 51-10-2. - [SDR 97ZZZM586](https://openairdocs.org/sdr/97ZZZM586.md): Floorbeam · corroded · Feb 12, 1997 · N461AT · Boeing 7372E1 · Fuselage Main, Floor Beam > DURING A SCHEDULED INSPECTION AT AERO CORP, THE FOLLOWING WAS FOUND; CABIN FLOORBEAM AT STATION 360 LBL 24 - RBL 24 TOP OF FLOORBEAM AROUND FASTENER HOLES HAVE EXFOLIATION AND CORROSION. FABRICATED (2) 'L' ANGLES FROM 7075 T6 26 INCH BY.75 INCH BY 1,.9375 I - [SDR 97ZZZM585](https://openairdocs.org/sdr/97ZZZM585.md): Angle · corroded · Feb 12, 1997 · N461AT · Boeing 7372E1 · Fuselage Miscellaneous Structure > DURING A SCHEDULED INSPECTION AT AERO CORP, THE FOLLOWING WAS FOUND; FLOOR SUPPORT AND LT FORWARD LAVATORY BULKHEAD SUPPORT CHANNEL STATION 294.5-277 LBL 15, FLOOR SUPPORT SHIM CORRODED AND BULKHEAD CHANNEL 100 PERCENT MATERIAL LOOSE. SHIM FOUND TO BE IN THE - [SDR 97ZZZM625](https://openairdocs.org/sdr/97ZZZM625.md): Angle · corroded · Feb 9, 1997 · N461AT · Boeing 7372E1 · Fuselage Miscellaneous Structure > AFT CARGO FLOOR ATTACH ANGLE NR 6 CORROSION THROUGH OUT. CUT OUT CORRODED SECTION OF ANGLE AND FABRICATED REPAIR ANGLE FROM 7075 T-6 511 L-ANGLE EXTRUSION.080 INCH BY 1 INCH BY 1 INCH BY 9 INCH. DRILLED, DEBURRED, COUNTERSUNK IAW B737 SRM 51-10-05, 51-10-7, - [SDR 97ZZZM636](https://openairdocs.org/sdr/97ZZZM636.md): Seat Track · misdrilled · Feb 4, 1997 · N461AT · Boeing 7372E1 · Fuselage, Seat/Cargo Attach Fittings > 31J - THE FOLLOWING WAS FOUND, CABIN SEAT TRACK LEFT OUTBOARD HAS HOLES.5 INCH DRILLED IN TOP THROUGH OUT. REMOVED AND REPLACED SEAT TRACK FROM STATION 520-540 IAW SRM 51-30-2. REMOVED AND REPLACED SEAT TRACK FROM STATION 727-727B IAW SRM 51-30-2. FABRICAT - [SDR 97ZZZM635](https://openairdocs.org/sdr/97ZZZM635.md): Seat Track · misdrilled · Feb 4, 1997 · N461AT · Boeing 7372E1 · Fuselage, Seat/Cargo Attach Fittings > 31J - THE FOLLOWING WAS FOUND, CABIN SEAT TRACK LEFT OUTBOARD HAS HOLES.5 INCH DRILLED IN TOP THROUGH OUT. REMOVED AND REPLACED SEAT TRACK FROM STATION 520-540 IAW SRM 51-30-2. REMOVED AND REPLACED SEAT TRACK FROM STATION 727-727B IAW SRM 51-30-2. FABRICAT - [SDR 97ZZZM630](https://openairdocs.org/sdr/97ZZZM630.md): Seat Track · corroded · Feb 4, 1997 · N461AT · Boeing 7372E1 · Fuselage, Seat/Cargo Attach Fittings > 31J - THE FOLLOWING WAS FOUND, CABIN SEAT TRACK RIGHT OUTBOARD HAS HOLES DRILLED IN TOP THROUGH OUT. REMOVED SEAT TRACK FROM STATION 420-480 520. FABRICATED NEW SEAT TRACK FROM BAC 1520-792 AND INSTALLED IAW SRM 53-10-5. REMOVED AND FABRICATED NEW SEAT TRAC - [SDR 97ZZZM629](https://openairdocs.org/sdr/97ZZZM629.md): Seat Track · misdrilled · Feb 4, 1997 · N461AT · Boeing 7372E1 · Fuselage, Seat/Cargo Attach Fittings > 31J - THE FOLLOWING WAS FOUND, CABIN SEAT TRACK T/H INBOARD HAS HOLES DRILLED IN TOP THROUGH OUT. FABRICATED NEW SEAT TRACK FROM BAC 1520-792 100 INCHES LONG. INSTALLED NEW SEAT TRACK IAW SRM 51-10-2. REMOVED SEAT TRACK FROM STATION 520-540 AND INSTALLED NE - [SDR 97ZZZM628](https://openairdocs.org/sdr/97ZZZM628.md): Seat Track · misdrilled · Feb 4, 1997 · N461AT · Boeing 7372E1 · Fuselage, Seat/Cargo Attach Fittings > 31J - THE FOLLOWING WAS FOUND, CABIN SEAT TRACK T/H INBOARD HAS HOLES DRILLED IN TOP THROUGH OUT. FABRICATED NEW SEAT TRACK FROM BAC 1520-792 100 INCHES LONG. INSTALLED NEW SEAT TRACK IAW SRM 51-10-2. REMOVED SEAT TRACK FROM STATION 520-540 AND INSTALLED NE - [SDR 97ZZZM627](https://openairdocs.org/sdr/97ZZZM627.md): Seat Tracks · misdrilled · Feb 4, 1997 · N461AT · Boeing 7372E1 · Fuselage, Seat/Cargo Attach Fittings > 31J - DURING A SCHEDULED INSPECTION, THE FOLLOWING WAS FOUND, CABIN SEAT TRACK LEFT INBOARD HAS HOLES DRILLED IN TOP THROUGH OUT, REMOVED AND INSTALLED SEAT TRACK AT STATIONS 480-520, 727-727B, 520-540 IAW SRM 51-10-3. REMOVED, FABRICATED AND INSTALLED SEAT - [SDR 97ZZZM626](https://openairdocs.org/sdr/97ZZZM626.md): Seat Tracks · damaged · Feb 4, 1997 · N461AT · Boeing 7372E1 · Fuselage, Seat/Cargo Attach Fittings > 31J - DURING A SCHEDULED INSPECTION, THE FOLLOWING WAS FOUND, CABIN SEAT TRACK LEFT INBOARD HAS HOLES DRILLED IN TOP THROUGH OUT, REMOVED AND INSTALLED SEAT TRACK AT STATIONS 480-520, 727-727B, 520-540 IAW SRM 51-10-3. REMOVED, FABRICATED AND INSTALLED SEAT - [SDR 97ZZZM641](https://openairdocs.org/sdr/97ZZZM641.md): Floorbeam · corroded · Feb 3, 1997 · N461AT · Boeing 7372E1 · Fuselage Main, Floor Beam > 31J - THE FOLLOWING WAS FOUND, CABIN FLOORBEAM STATION 328 BL '0' 60 HAS CORROSION. FABRICATED NEW FLOORBEAM FROM BAC 1505-100246 15.5 BY 2 INCH IAW SRM 51-101. FABRICATED T-CAP FROM 7075 T6511 2.25 INCH BY 3 INCH BY 60 INCH AND 1.25 INCH BY 2.25 INCH BY 60 - [SDR 97ZZZM640](https://openairdocs.org/sdr/97ZZZM640.md): Support · corroded · Feb 3, 1997 · N461AT · Boeing 7372E1 · Fuselage Miscellaneous Structure > 31J - THE FOLLOWING WAS FOUND, CABIN FLOOR SUPPORT STATION 328-344 LBL 12 HAS CORROSION. FABRICATED FLOOR SUPPORT FROM 7075 T6511.095 15.5 INCH BY 1.75 INCH BY.1.5 INCH. FABRICATED SHIM FROM 7075 T6.050 15.5 INCH BY 1.75 INCH BY IAW SRM 53-10-4. INSTALLE - [SDR 97ZZZM639](https://openairdocs.org/sdr/97ZZZM639.md): Support · corroded · Feb 3, 1997 · N461AT · Boeing 7372E1 · Fuselage Miscellaneous Structure > 31J - THE FOLLOWING WAS FOUND, CABIN FLOOR SUPPORT STATION 312-328 LBL 12 HAS CORROSION. FABRICATED FLOOR SUPPORT FROM 7075-6511.090 BAC 1505-100246 1.875 BY 15.5. FABRICATED SHIM FROM 7075 T6.090 1.75 INCH BY 13 INCH IAW SRM 51-10-1. INSTALLED FLOOR SUPPO - [SDR 97ZZZM634](https://openairdocs.org/sdr/97ZZZM634.md): Floorbeam · corroded · Feb 3, 1997 · N461AT · Boeing 7372E1 · Fuselage Main, Floor Beam > 31J - THE FOLLOWING WAS FOUND, CABIN FLOORBEAM HAS CORROSION STATION 295 RBL 60 TO UNDER FORWARD LAVATORY. FABRICATED T-CAP SECTION FRM AND 10136-2401 79.5 INCH BY 2.5 INCH BY 1.25 INCH. FABRICATED FOUR ANGLES 7075 T6.063 1 INCH BY 1 INCH 14 INCH TWO AND 1 - [SDR 97ZZZM633](https://openairdocs.org/sdr/97ZZZM633.md): Floor Support · corroded · Feb 3, 1997 · N461AT · Boeing 7372E1 · Fuselage Miscellaneous Structure > 31J - THE FOLLOWING WAS FOUND, CABIN FLOOR SUPPORT STATION 344-360 RBL 12 HAS CORROSION. FABRICATED FLOOR SUPPORT FORM BAC 1506-43 7076 T6.063 15.5 INCH BY 1 INCH. INSTALLED IAW SRM 51-40-1, N/R NR 71093/0704. - [SDR 97ZZZM632](https://openairdocs.org/sdr/97ZZZM632.md): Floorbeam · corroded · Feb 3, 1997 · N461AT · Boeing 7372E1 · Fuselage Main, Floor Beam > 31J - THE FOLLOWING WAS FOUND, CABIN FLOORBEAM HAS CORROSION STATION 344 RBL 16 - LBL 60. FABRICATED T-CAP FROM 60-893 83 INCH BY 1 INCH BY 1.25 INCH. FABRICATED FOUR ANGLES FROM BAC 1490-2865 TWO 11 INCH BY 1.5 INCH BY 1 INCH AND TWO 7.25 INCH BY 1 INCH BY - [SDR 97ZZZM631](https://openairdocs.org/sdr/97ZZZM631.md): Floorbeam · corroded · Feb 3, 1997 · N461AT · Boeing 7372E1 · Fuselage Main, Floor Beam > 31J - THE FOLLOWING WAS FOUND, CABIN FLOORBEAM AND PAN HAS CORROSION. FABRICATED FILLER AND SHIM FROM 7075 T6.071 8.5 INCH BY 1 INCH (SHIM) 7075 T6.125 3.5 INCH BY 1 INCH IAW EO 97-470. INSTALLED REPAIRS IAW EO 97-470, N/R NR 71123/0734. - [SDR 97ZZZM638](https://openairdocs.org/sdr/97ZZZM638.md): Floorbeam · corroded · Feb 1, 1997 · N461AT · Boeing 7372E1 · Fuselage Main, Floor Beam > 31J - THE FOLLOWING WAS FOUND, MAIN CABIN, STATION 986 LBL 0-12 FLOORBEAM CORRODED. FABRICATED NEW T-ANGLE. FABRICATED TWO STRAPS FROM 7075 T6.063 10.75 INCH BY 1 INCH AND 9.2 INCH BY 1 INCH. FABRICATED TWO STRAPS FROM 7075 T6.071 13.5 INCH BY 1 INCH. FA - [SDR 97ZZZM589](https://openairdocs.org/sdr/97ZZZM589.md): Frame · corroded · Jan 29, 1997 · N461AT · Boeing 7372E1 · Fuselage Main, Frame > DURING A SCHEDULED INSPECTION AT AERO CORP, THE FOLLOWING WAS FOUND; AFT CARGO FRAME STATION 887 AND 22L - 19L HAS CORROSION. FABRICATED DOUBLER FROM 7075-0.063 21.25 INCH BY 1.5 INCH BY 1 INCH. INSTALLED REPAIR IAW SRM 51-40-3 AND 51-10-2. - [SDR 97ZZZM588](https://openairdocs.org/sdr/97ZZZM588.md): Angle · corroded · Jan 29, 1997 · N461AT · Boeing 7372E1 · Fuselage Miscellaneous Structure > DURING AN SCHEDULED INSPECTION AT AERO CORP, THE FOLLOWING WAS FOUND; IN THE FORWARD LOWER CARGO PIT AT BS 460 BL 22 RIGHT, THERE IS AN AREA OF CORROSION UNDER THE TRANSITION PANEL. FORMED ANGLE FROM 7075-0.063 14.875 INCH BY 1 INCH BY 1.25 INCH. DEBURRED A - [SDR 97ZZZM587](https://openairdocs.org/sdr/97ZZZM587.md): Angle · corroded · Jan 29, 1997 · N461AT · Boeing 7372E1 · Fuselage Miscellaneous Structure > DURING AN SCHEDULED INSPECTION AT AERO CORP, THE FOLLOWING WAS FOUND; IN THE FORWARD LOWER CARGO PIT AT BS 480 BL 22 RIGHT, THERE IS AN AREA OF CORROSION UNDER THE TRANSITION PANEL. FORMED ANGLE FROM 7075-0.063 23 INCH BY 2.75 INCH BY 1.25 INCH. INSTALLED I - [SDR 96ZZZX4179](https://openairdocs.org/sdr/96ZZZX4179.md): Bracket · worn · Jul 22, 1996 · N461AT · Boeing 7372E1 · Elevator Tab Control System > TYS/MCO - FLT 621 - FLIGHT CREW REPORTED NR 2 ENGINE VIBRATION DURING FLIGHT. TROUBLESHOT ENGINE AND FOUND NO DISCREPANCIES. DURING TEST FLIGHT, MAINTENANCE FOUND THAT VIBRATION ORIGINATED AT AFT FUSELAGE. INSPECTION REVEALED THAT LEFT ELEVATOR TRIM TAB HAD ## 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 = 'N461AT' AND deregistration_id = 'N461AT-2000-09-15' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N461AT-2000-09-15/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.