# N462AT: 1982 Boeing 737-297, registration cancelled 2006-06-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 13, 2006 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 737-297](https://openairdocs.org/model/boeing-737-297) (registry code 1384480) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 22631 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: July 19, 1982 - Certificate issued: April 10, 2000 - Last registry action: April 18, 2006 - Mode S code: A5A11B - Owner when cancelled: [Greenwich Industrial Services LLC](https://openairdocs.org/faa-owner/GREENWICH%20INDUSTRIAL%20SERVICES%20LLC) - Location: [Branford, CT](https://openairdocs.org/faa-place/CT/Branford) - Owner type: Corporation - Owner's area on the map: 41.2800° N, 72.7859° W: Placed by OpenAirDocs at the center of ZIP code 06405, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N462AT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=462AT - Page: https://openairdocs.org/deregistered/N462AT-2006-06-13 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 737-297: https://openairdocs.org/model/boeing-737-297.md ## Service difficulty reports (39) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AT9900634](https://openairdocs.org/sdr/AT9900634), Sep 3, 1999: OIL LINE. BROKEN. NR 2 ENGINE OIL PSI AND QUANTITY WENT TO ZERO, SHUT DOWN ENGINE IN-FLIGHTAND DIVERTED TO JAN. LANDED AIRCRAFT WITHIN THIRTY MINUTES OF INCIDENT. FOUND BROKEN OI - [SDR AT9900601R1](https://openairdocs.org/sdr/AT9900601R1), Aug 18, 1999: TIRE. BLOWN. NR 3 TIRE FAILURE CAUSED DAMAGE TO AIRCRAFT WHICH RESULTED IN ALL HYDRAULIC FLUID LOSS. REMOVED AND REPLACED NR 3 AND NR 4 TIRE AND BRAKE, NR 1 AND NR 2 ENGINE - [SDR AT9900601](https://openairdocs.org/sdr/AT9900601), Aug 18, 1999: TIRE. FAILED. NR 3 TIRE FAILURE CAUSED DAMAGE TO AIRCRAFT WHICH RESULTED IN ALL HYDRAULIC FLUID LOSS. REMOVED AND REPLACED NR 3 TIRE AND A REVISION NR AT9900601R1 WILL FOLLOW - [SDR AT9900575](https://openairdocs.org/sdr/AT9900575), Aug 13, 1999: FITTING. DAMAGED. AT ALTITUDE NR 1 ENGINE OIL QUANTITY WENT TO ZERO AND OIL PRESSURE DROPPED INTO THE AMBER BAND. SHUT DOWN THE ENGINE AND RETURNED. OIL PRESSURE REMAINED AT 35 P - [SDR ATT9900539](https://openairdocs.org/sdr/ATT9900539), Jul 28, 1999: PUMP. LEAKING. NR 1 ENGINE LOST ALL OIL QUANTITY. ENGINE WAS SHUT DOWN ON SHORT FINAL WITH OIL PRESSURE GOING TOWARDS ZERO. OIL TEMPERATURE OK. INSPECTION FOUND OIL PUDDLING A - [SDR AT9900493](https://openairdocs.org/sdr/AT9900493), Jul 13, 1999: FUSE. FAILED. DURING LAYOVER, FOUND AN EMERGENCY PATH LIGHTING SEGMENT OUT. REPLACED BATTERY CHARGER FOR BLOWN FUSE (F2), OPS CHECK NORMAL IAW MM 33-51-00. - [SDR AT9900492](https://openairdocs.org/sdr/AT9900492), Jul 9, 1999: BATTERY CHARGER. DEFECTIVE. EMERGENCY EVACUATION LIGHTS INOPERATIVE IN FORWARD SECTION OF AIRCRAFT. REMOVED AND REPLACED FORWARD BATTERY PACK CHARGER IAW MM 33-51-51. - [SDR VJ9800364](https://openairdocs.org/sdr/VJ9800364), Aug 7, 1998: INTERCOASTAL. CORRODED. FUSELAGE INTERIOR BETWEEN BS 312 AND 294.5, INTERCOSTAL AT RBL 24 IS CORRODED ON TOP. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-10-1 AND 51-10-6. REMOVED INTER - [SDR VJ9800363](https://openairdocs.org/sdr/VJ9800363), Aug 7, 1998: FLOORBEAM. CORRODED. FUSELAGE INTERIOR, FLOORBEAM AT BS 294.5 IS CORRODED ON TOP AT RBL 12. REMOVED CORROSION .024 TO .041 MATERIAL LOSS OUT OF LIMITS. GAUGE NR A-0358 IAW SRM 51-10 - [SDR VJ9800360](https://openairdocs.org/sdr/VJ9800360), Aug 7, 1998: ANGLE. CORRODED. AFT CARGO STRINGER 27R AT STA 962 AT FASTENER HOLE CORRODED. MAT LOSS IN THE BASE OF STRINGER AT STA 951-967 (27R) OUT OF LIMITS IAW SRM 53-10-1. CUT OUT CORROD - [SDR VJ9800367](https://openairdocs.org/sdr/VJ9800367), Aug 6, 1998: SKIN. CORRODED. CORROSION ON SIDE MOUNT AREA FOR EYE BROW WINDOW NR 5. REMOVED CORROSION OUT OF LIMITS, FABRICATED REPAIR DOUBLER FROM 2024 T-3 .063 ABD STRAP REPAIR FROM 7075 - [SDR VJ9800356](https://openairdocs.org/sdr/VJ9800356), Aug 6, 1998: FLOORBEAM. CORRODED. EXFOLIATED CORROSION ON BS 328 FLOORBEAM CAP UNDER TAPERED SHIN RBL 54. REMOVED CORROSION IAW SRM 51-10-6. MATERIAL LOSS TO BE OUT OF LIMITS. REMOVED T CHORD ST - [SDR VJ9800359](https://openairdocs.org/sdr/VJ9800359), Aug 5, 1998: ANGLE. CORRODED. L-1 DOOR FWD GIRT BAR ATTACH BRACKET BLOCK CORRODED ON BS 312 FLOORBEAM. REMOVED CORRODED ATTACH BRACKET IAW SRM 51-30-1. FOUND TO BE OUT OF LIMITS IAW SRM 53-1 - [SDR VJ9800358](https://openairdocs.org/sdr/VJ9800358), Aug 4, 1998: ANGLE. CORRODED. FILLER STRIPS ON TOP SIDE OF CUSP ANGLE AT L-1 DOOR THRESHOLD CORRODED BS 312-344. REMOVED CORROSION ON THRESHOLD, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01 AN - [SDR VJ9800357](https://openairdocs.org/sdr/VJ9800357), Aug 4, 1998: ANGLE. CORRODED. EXFOLIATED CORROSION AROUND NUT PLATE ON UNDERSIDE OF CUSP ANGLE AT L-1 DOOR THRESHOLD, BS 326. REMOVED SUPPORT ANGLE AND REMOVED CORROSION, LOSS FOUND TO BE OU - [SDR VJ9800350](https://openairdocs.org/sdr/VJ9800350), Aug 4, 1998: ANGLE. CORRODED. L-1 DOOR SILL LOWER SUPPORT ANGLE BETWEEN STA 328-312 HAS 100 PERCENT MATERIAL LOSS. REMOVED SUPPORT ANGLE AND CLEANED CORROSION, MATERIAL LOSS 100 PERCENT OUT - [SDR VJ9800351](https://openairdocs.org/sdr/VJ9800351), Aug 2, 1998: ANGLE. CORRODED. AFT ALV AT STA 296 BUTT LINE LBL35 ON REMOVAL OF SUPPORT ANGLE, LOWER SUPPORT U CHANNEL HAS CORROSION BEYOND LIMITS. REMOVED LOWER CHANNEL SUPPORT IAW B 737 SRM - [SDR VJ9800361](https://openairdocs.org/sdr/VJ9800361), Aug 1, 1998: ANGLE. CORRODED. AFT TOILET FLOOR SUPPORT AT BL 12 L BS 1016 IS CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-30-1. REMOVED CORROSION IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS. FA - [SDR VJ9800365](https://openairdocs.org/sdr/VJ9800365), Jul 31, 1998: STRINGER. CORRODED. AFT CARGO STRINGER 27L FROM APPROX 986-1010 HAS NUMBEROUS SURFACE CORROSION ON THE CHANNEL AND ON LT SIDE AND ON THE BELLY SKIN. REMOVED CORROSION OUT OF LIMITS - [SDR VJ9800355](https://openairdocs.org/sdr/VJ9800355), Jul 31, 1998: ANGLE. CORRODED. CORROSION FOUND ON FWD LAV AFT WALL ATTACH ANGLE BS 300 LB 35. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED ATTACH ANGLE IAW SRM 51-30-2 - [SDR VJ9800353](https://openairdocs.org/sdr/VJ9800353), Jul 31, 1998: FLOORBEAM. CORRODED. AFT CARGO AREA AROUND STA 1006-1016 UNDER LT AFT LAV CORROSION BETWEEN THE FLOORBEAMS AND FLOOR BOARDS. REMOVED CORRODED AREA STA 1006-1016 WITHIN LIMITS. REMOV - [SDR VJ9800354](https://openairdocs.org/sdr/VJ9800354), Jul 30, 1998: ANGLE. CORRODED. AFT TOILET FWD WALL TIE DOWN ANGLE IS CORRODED. REMOVED CORROSION OUT OF LIMTS, MAT LOSS .045 IAW SRM 53-10-1. REMOVED BRACKET TO FABRICATE NEW ANGLE IAW SRM 51 - [SDR VJ9800352](https://openairdocs.org/sdr/VJ9800352), Jul 29, 1998: ANGLE. CORRODED. UPON REMOVAL OF FWD AFT LAV AFT WALL ATTACH ANGLE, AT BS 300, LOWER HAT SUPPORT HAS IG CORROSION. REMOVED HAT SUPPORT FOUND CORROSION BEYOND LIMTS IAW SRM 53-10 - [SDR VJ9800362](https://openairdocs.org/sdr/VJ9800362), Jul 28, 1998: SUPPORT. CORRODED. AFT TOILET UNDER FLOOR SUPPORT AT BL0 BS 1016 IS CORRODED. REMOVED CORROSION IAW SRM 51-10-2. FLOOR SUPPORT FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 AND 51-10- - [SDR VJ9800366](https://openairdocs.org/sdr/VJ9800366), Jul 27, 1998: PANEL. CORRODED. FWD CARGO PTI, STA 492.4 TO 520 RT SIDE TRANSITION PANEL HAS CORROSION OVER TOP OF STRINGER 26 RT. REMOVED CORROSION OUT OF LIMITS. FABRICATED TRANSITIONS PANEL - [SDR VJ9800041](https://openairdocs.org/sdr/VJ9800041), Mar 12, 1998: BATTERY. DISCHARGED. BOTH EMERGENCY EXIT LIGHTS AT AFT ENTRY SERVICE DOOR INOP. REPLACED BATTERY PACK. - [SDR ZZDA3324697](https://openairdocs.org/sdr/ZZDA3324697), Oct 28, 1997: LAMP. FAILED. DURING A LAYOVER CHECK, MAINTENANCE FOUND BOTH AFT EXTERIOR EMERGENCY LIGHTS INOPERABLE. RELAMPED BOTH EXTERIOR EMERGENCY LIGHTS. OPS CHECKED GOOD. (X) - [SDR 97ZZZM1053](https://openairdocs.org/sdr/97ZZZM1053), Aug 29, 1997: POWER SUPPLY. INOPERATIVE. POST FLT INSPECTION, RIGHT FUSELAGE FWD EMERGENCY EXTERIOR LIGHT ASSY CORRODED. REPAIRED BARE WIRE AND REPLACED BATTERY PACK IN FWD CARGO PIT. REPLACED REFLECTO - [SDR 97ZZZM1054](https://openairdocs.org/sdr/97ZZZM1054), Jul 23, 1997: WIRE. BROKEN. DURING POST FLIGHT, FOUND ROW 19 EMERGENCY EXIT FLOOR LIGHT INOP. REPAIRED BROKEN WIRE AT ROW 19 EMERGENCY LIGHT SOCKET. - [SDR 97ZZZM928](https://openairdocs.org/sdr/97ZZZM928), Jul 19, 1997: LIGHT. INOPERATIVE. DURNIG A LAYOVER SERVICE, TWO E-PATH FLOOR LIGHTS WERE NOTICED INOP. THE TWO E-PATH FLOOR LIGHTS WERE REPLACED. THE SYSTEM WAS TESTED NORMAL. (M) - [SDR ZZDA5311197](https://openairdocs.org/sdr/ZZDA5311197), May 28, 1997: STRINGER. DAMAGED. DURING C-CHECK, FOUND REPAIR AT STR 2L AND STR 3L AT STA 578 TO STA 597 NEEDS REPLACEMENT. FABRICATED DOUBLER FROM 2024 T3 .080 INCH, 10.5 INCHES BY 8 INCHES IA - [SDR ZZDA5711397](https://openairdocs.org/sdr/ZZDA5711397), May 27, 1997: SKIN. CORRODED. DURING C-CHECK, FOUND CORROSION AROUND SCREW HOLES IN LEFT MAIN GEAR SUPPORT STRUCTURE. REMOVED CORROSION AROUND SCREW HOLES AND OVERSIZED 14 EACH HOLES TO .25 - [SDR ZZDA5311497](https://openairdocs.org/sdr/ZZDA5311497), May 27, 1997: SKIN. CRACKED. DURING C-CHECK, FOUND STR 19R AT BS 312.3 LOWER ROW OF FASTENERS OF SKIN LAP SHOW CRACK INDICATIONS. FABRICATED FILLER AND DOUBLER FROM 2024 T3 .080 INCH, 2 INC - [SDR ZZDA5311297](https://openairdocs.org/sdr/ZZDA5311297), May 27, 1997: FLOOR BEAM. CORRODED. DURING C-CHECK, FOUND CORROSION ON FLOOR BEAM AT FASTENER HOLE AT STA 986.5. FABRICATED DOUBLER FROM 7075 T6 .071 INCH, 11 INCHES BY 2.5 INCHES. FABRICATED DOUB - [SDR ZZDA5310997](https://openairdocs.org/sdr/ZZDA5310997), May 27, 1997: SEAT TRACK. CORRODED. DURING C-CHECK, FOUND EXFOLIATION CORROSION IN INBOARD SEAT TRACK AT STA 344. FABRICATED NEW SEAT TRACK FROM BAC 1520-792 13.75 INCHES BY 3.5 INCHES IAW B737 SR - [SDR ZZDA5310897](https://openairdocs.org/sdr/ZZDA5310897), May 27, 1997: SEAT TRACK. CORRODED. DURING C-CHECK, FOUND CORROSION IN RIGHT OUTBOARD SEAT TRACK AT STA 344. FABRICATED NEW FLOOR TRACK SECTION FROM BAC 1520-792 34 INCHES BY 3.25 INCHES IAW B737 - [SDR 96ZZZM1418](https://openairdocs.org/sdr/96ZZZM1418), Jul 12, 1996: WHEEL ASSY. FAILED. AFTER LANDING, DURING TAXI TO GATE, THE NR 4 MLG WHEEL ASSY FAILED CAUSING THE NR 4 HUB CAP TO IMPACT THE NR 2 ENG INBOARD COWLING DAMAGING THE FORWARD AND AFT - [SDR 95ZZZM315](https://openairdocs.org/sdr/95ZZZM315), Jul 28, 1995: HARNESS. FAILED. ON APPROACH TO CVG THE CREW OF FLIGHT 700 OBSERVED THE NR 1 FUEL QUANTITY SYSTEM GIVING AN ERRATIC INDICATION. THE CAPTAIN DECLARED AN EMERGENCY. LANDED WITHOUT - [SDR 95ZZZM1](https://openairdocs.org/sdr/95ZZZM1), Apr 19, 1995: SKIN. DELAMINATED. ON 4-18-95, THE PILOT IN COMMAND OF A/C FOUND NR 6 LE SLAT DELAMINATED DURING PREFLIGHT AT CVG. MAINTENANCE CONTROL CONTACTED AN EMERGENCY MAINTENANCE CREW TO E ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19990818022499I](https://openairdocs.org/incident/19990818022499I), Aug 18, 1999: Boeing 737297 (N462AT), Dallas-Ft Worth, TX. (-5)Airtran airways flight 866, 18AUG1999, james s. sargent-captain, blown tire and hydraulic loss on takeoff. At 130 knots the aircraft had the feeling like… --- 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.