# N461AT: Boeing 737-2E1, registration cancelled 2000-09-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 15, 2000 - Status when cancelled: Valid registration - Airframe: [Boeing 737-2E1](https://openairdocs.org/model/boeing-737-2e1) (registry code 138448F) - Serial number: 20976 - Type of aircraft: Fixed wing multi engine - Certificate issued: January 25, 1994 - Last registry action: June 2, 1998 - Mode S code: A59D64 - Owner when cancelled: [Polaris Holding Company](https://openairdocs.org/faa-owner/POLARIS%20HOLDING%20COMPANY) - Location: [Stamford, CT](https://openairdocs.org/faa-place/CT/Stamford) - Owner type: Corporation - Owner's area on the map: 41.0534° N, 73.5387° W: Placed by OpenAirDocs: center of Stamford, CT, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N461AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=461AT - Page: https://openairdocs.org/deregistered/N461AT-2000-09-15 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-2E1: https://openairdocs.org/model/boeing-737-2e1.md ## Service difficulty reports (41) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AT9900095](https://openairdocs.org/sdr/AT9900095), Feb 6, 1999: BULB. FAILED. DURING SCHEDULED MAINTENANCE FOUND EXTERIOR EMERGENCY LIGHT AT L-2 DOOR AND AFT SERVICE DOOR INOPERATIVE. RELAMPED BOTH EMERGENCY LIGHT AND OPS CHECKED THE SYST - [SDR VJ9800286](https://openairdocs.org/sdr/VJ9800286), Aug 24, 1998: BATTERY PACK. DISCHARGED. FORWARD LT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK; OPS CHECKED GOOD. - [SDR VJ9800205](https://openairdocs.org/sdr/VJ9800205), Jun 1, 1998: SKIN. CRACKED. 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), Jun 1, 1998: SUPPORT. CORRODED. DURING C-CHECK, FOUND FLOORBOARD SUPPORT HAS I/G CORROSION AT FS 294 TO 306 LBL 12. - [SDR VJ9800203](https://openairdocs.org/sdr/VJ9800203), May 18, 1998: ANGLE. CORRODED. 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- - [SDR VJ9800150](https://openairdocs.org/sdr/VJ9800150), May 8, 1998: LIGHT. INOPERATIVE. 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), Mar 22, 1998: DEFLECTOR. INOPERATIVE. 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), Feb 20, 1998: CONNECTOR. DIRTY. AFT SECTION OF EMERGENCY PATH LIGHTING INOPERATIVE. CLEANED AND DRIED CONNECTIONS, OPS CHECKED NORMAL. - [SDR ZZDA3324797](https://openairdocs.org/sdr/ZZDA3324797), Oct 29, 1997: LIGHT. INOPERATIVE. 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 - [SDR ZZDA3318597](https://openairdocs.org/sdr/ZZDA3318597), Sep 23, 1997: LIGHT. DIRTY. DURING LAYOVER CHECK, FOUND MAINTENANCE ENTRY FLOOR PATH LIGHTING INOPERABLE LAST 10 ROWS AND R2 DOOR LOWER EXIT LIGHT FOUND INOPERABLE. MAINTENANCE TROUBLESHOT - [SDR 97ZZZM926](https://openairdocs.org/sdr/97ZZZM926), Jul 17, 1997: WIRE. BROKEN. 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 CARPETI - [SDR 97ZZZM665](https://openairdocs.org/sdr/97ZZZM665), May 19, 1997: PCU. CRACKED. 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 - [SDR 97ZZZM668](https://openairdocs.org/sdr/97ZZZM668), May 7, 1997: LIGHTING. INOPERATIVE. DURING A TRANSIT CHECK, THE EMERGENCY PATH LIGHTING SYSTEM WAS INOP. ALL OVERHEAD AND DOOR EMERGENCY LIGHTS OPS CHECK NORMAL. REMOVED MOISTURE FROM THE EMERGENC - [SDR 97ZZZM669](https://openairdocs.org/sdr/97ZZZM669), May 6, 1997: BATTERY PACK. DISCHARGED. 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. OP - [SDR 97ZZZM666](https://openairdocs.org/sdr/97ZZZM666), Apr 30, 1997: FIRE LOOP. CRIMPED. 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 AP - [SDR 97ZZZM644](https://openairdocs.org/sdr/97ZZZM644), Feb 13, 1997: FLOORBEAM. CORRODED. 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 - [SDR 97ZZZM643](https://openairdocs.org/sdr/97ZZZM643), Feb 13, 1997: SUPPORT. CORRODED. 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 - [SDR 97ZZZM642](https://openairdocs.org/sdr/97ZZZM642), Feb 13, 1997: ANGLE. CORRODED. 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 I - [SDR 97ZZZM637](https://openairdocs.org/sdr/97ZZZM637), Feb 13, 1997: ANGLE. CORRODED. 31J - THE FOLLOWING WAS FOUND, MAIN CABIN STATION 989.0 LBL 10 FLOOR SUPPORT ANGLE CORRODED BEYOND LIMITS. REMOVED CORRODED ANGLE, FABRICATED NEW ANGLE. DIMENSI - [SDR 97ZZZM586](https://openairdocs.org/sdr/97ZZZM586), Feb 12, 1997: FLOORBEAM. CORRODED. 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 - [SDR 97ZZZM585](https://openairdocs.org/sdr/97ZZZM585), Feb 12, 1997: ANGLE. CORRODED. 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, FL - [SDR 97ZZZM625](https://openairdocs.org/sdr/97ZZZM625), Feb 9, 1997: ANGLE. CORRODED. 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 - [SDR 97ZZZM636](https://openairdocs.org/sdr/97ZZZM636), Feb 4, 1997: SEAT TRACK. MISDRILLED. 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 - [SDR 97ZZZM635](https://openairdocs.org/sdr/97ZZZM635), Feb 4, 1997: SEAT TRACK. MISDRILLED. 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 - [SDR 97ZZZM630](https://openairdocs.org/sdr/97ZZZM630), Feb 4, 1997: SEAT TRACK. CORRODED. 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 - [SDR 97ZZZM629](https://openairdocs.org/sdr/97ZZZM629), Feb 4, 1997: SEAT TRACK. MISDRILLED. 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. I - [SDR 97ZZZM628](https://openairdocs.org/sdr/97ZZZM628), Feb 4, 1997: SEAT TRACK. MISDRILLED. 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. I - [SDR 97ZZZM627](https://openairdocs.org/sdr/97ZZZM627), Feb 4, 1997: SEAT TRACKS. MISDRILLED. 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 TRA - [SDR 97ZZZM626](https://openairdocs.org/sdr/97ZZZM626), Feb 4, 1997: SEAT TRACKS. DAMAGED. 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 TRA - [SDR 97ZZZM641](https://openairdocs.org/sdr/97ZZZM641), Feb 3, 1997: FLOORBEAM. CORRODED. 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. - [SDR 97ZZZM640](https://openairdocs.org/sdr/97ZZZM640), Feb 3, 1997: SUPPORT. CORRODED. 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 - [SDR 97ZZZM639](https://openairdocs.org/sdr/97ZZZM639), Feb 3, 1997: SUPPORT. CORRODED. 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 1 - [SDR 97ZZZM634](https://openairdocs.org/sdr/97ZZZM634), Feb 3, 1997: FLOORBEAM. CORRODED. 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 - [SDR 97ZZZM633](https://openairdocs.org/sdr/97ZZZM633), Feb 3, 1997: FLOOR SUPPORT. CORRODED. 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 I - [SDR 97ZZZM632](https://openairdocs.org/sdr/97ZZZM632), Feb 3, 1997: FLOORBEAM. CORRODED. 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. FABRICATE - [SDR 97ZZZM631](https://openairdocs.org/sdr/97ZZZM631), Feb 3, 1997: FLOORBEAM. CORRODED. 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 IN - [SDR 97ZZZM638](https://openairdocs.org/sdr/97ZZZM638), Feb 1, 1997: FLOORBEAM. CORRODED. 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 B - [SDR 97ZZZM589](https://openairdocs.org/sdr/97ZZZM589), Jan 29, 1997: FRAME. CORRODED. 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 .06 - [SDR 97ZZZM588](https://openairdocs.org/sdr/97ZZZM588), Jan 29, 1997: ANGLE. CORRODED. 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 - [SDR 97ZZZM587](https://openairdocs.org/sdr/97ZZZM587), Jan 29, 1997: ANGLE. CORRODED. 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 - [SDR 96ZZZX4179](https://openairdocs.org/sdr/96ZZZX4179), Jul 22, 1996: BRACKET. WORN. TYS/MCO - FLT 621 - FLIGHT CREW REPORTED NR 2 ENGINE VIBRATION DURING FLIGHT. TROUBLESHOT ENGINE AND FOUND NO DISCREPANCIES. DURING TEST FLIGHT, MAINTENANCE FOU --- 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.