# N221US: Boeing 737-2H5, registration cancelled 2000-06-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 14, 2000 - Status when cancelled: Valid registration - Airframe: [Boeing 737-2H5](https://openairdocs.org/model/boeing-737-2h5) (registry code 138448E) - Serial number: 20454 - Type of aircraft: Fixed wing multi engine - Certificate issued: January 14, 1999 - Last registry action: January 14, 1999 - Mode S code: A1E68B - Owner when cancelled: [State Street Bank & Trust Co Trustee](https://openairdocs.org/faa-owner/STATE%20STREET%20BANK%20%26%20TRUST%20CO%20TRUSTEE) - Location: [Hartford, CT](https://openairdocs.org/faa-place/CT/Hartford) - Owner type: Corporation - Owner's area on the map: 41.7651° N, 72.6708° W: Placed by OpenAirDocs at the center of ZIP code 06103, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N221US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=221US - Page: https://openairdocs.org/deregistered/N221US-2000-06-14 From the FAA registry file of October 28, 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 737-2H5: https://openairdocs.org/model/boeing-737-2h5.md ## Service difficulty reports (63, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 98ZZZM494](https://openairdocs.org/sdr/98ZZZM494), May 27, 1998: POWER SUPPLY. INOPERATIVE. FORWARD LEFT (PAX) AND RT SERVICE DOOR EXIT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED FORWARD EMERGENCY LIGHTS POWER SUPPLY PACK, S/N ON 1715, S/N OFF 15002, - [SDR 98ZZZM401](https://openairdocs.org/sdr/98ZZZM401), Feb 26, 1998: SPLICE. BROKEN. ON OVERNIGHT CHECK, FOUND ROW 2 EMERGENCY LIGHT INOP. FOUND BUTT SPLICE BROKEN. REINSTALLED NEW SPLICE, OPS CHECK OK. (M) - [SDR 98ZZZM80](https://openairdocs.org/sdr/98ZZZM80), Dec 12, 1997: LIGHT. INOPERATIVE. FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP, FOUND ON RON MAINTENANCE CHECK. REPLACED LIGHT ASSY, OPS CHECK GOOD. (M) - [SDR 97ZZZM426](https://openairdocs.org/sdr/97ZZZM426), Mar 2, 1997: SKIN. CRACKED. FOUND 5 CRACKS AT FASTENERS STATION 373, 374, 375, 377, STRINGER 15L. REPAIRED PER SRM 53-30-3. (M) - [SDR 97ZZZM425](https://openairdocs.org/sdr/97ZZZM425), Mar 2, 1997: SKIN. CRACKED. FOUND .125 INCH CRACK AT FASTENER HOLE. REPAIRED PER SRM 53-30-1. - [SDR 97ZZZM424](https://openairdocs.org/sdr/97ZZZM424), Mar 2, 1997: SKIN. CRACKED. FOUND TWO .25 INCH LONG CRACKS. REPAIRED PER SRM 53-30-3 FIG 1. - [SDR 97ZZZM423](https://openairdocs.org/sdr/97ZZZM423), Mar 2, 1997: SKIN. CRACKED. FOUND TWO CRACKS AT FASTENER HOLES. REPAIRED PER SRM 53-30-3. - [SDR 97ZZZM422](https://openairdocs.org/sdr/97ZZZM422), Mar 2, 1997: FRAME. CRACKED. FOUND ONE INCH CRACK IN FRAME. REPAIRED PER SRM 51-40-2. - [SDR 97ZZZM421](https://openairdocs.org/sdr/97ZZZM421), Mar 2, 1997: FRAME. CRACKED. LEFT OUTBOARD CHORD ANGLE CRACKED STATION 1156 WL 274, .75 INCH CRACK. REPAIRED PER EO 5391G569. - [SDR 97ZZZM420](https://openairdocs.org/sdr/97ZZZM420), Mar 2, 1997: STRINGER. CRACKED. ONE INCH CRACK IN STRINGER. REPAIRED PER SRM 53-10-3. - [SDR 97ZZZM419](https://openairdocs.org/sdr/97ZZZM419), Mar 2, 1997: SKIN. DISBOND. SKIN DISBONDED AT LOWER CORNERS OF EMERGENCY EXIT APERTURE, REPAIRED PER EA 42068. - [SDR 97ZZZM418](https://openairdocs.org/sdr/97ZZZM418), Mar 2, 1997: SKIN. CRACKED. 3 INCH BY 5 INCH DELAMINATED AREA AND CRACKS AT SIX FASTENER HOLES. REPAIRED PER EA 42062. (M) - [SDR 97ZZZM417](https://openairdocs.org/sdr/97ZZZM417), Mar 2, 1997: BULKHEAD FITTING. CRACKED. BULKHEAD FITTING CRACKED 3 INCHES. TIME LIMITED REPAIR INSTALLED PER EA 42071 AND DWG 65C 29229. (M) - [SDR 96ZZZX1484](https://openairdocs.org/sdr/96ZZZX1484), Mar 1, 1996: SKIN. CRACKED. GSO - .1250 INCH CRACK AT RIVET HOLE FOUND. INSTALLED DOUBLER SRM 53-30-3, FIGURE 6. - [SDR 96ZZZX1483](https://openairdocs.org/sdr/96ZZZX1483), Mar 1, 1996: SKIN. CRACKED. GSO - FIVE .25 INCH CRACKS AT RIVET HOLES FOUND. INSTALLED REPAIR PER E.A. 40951. - [SDR 96ZZZX1482](https://openairdocs.org/sdr/96ZZZX1482), Mar 1, 1996: SKIN. CRACKED. GSO - 3 CRACKS FORWARD UPPER CORNER, FORWARD SERVICE DOORWAY. INSTALLED DOUBLER PER E.A. 40950. - [SDR E9WA](https://openairdocs.org/sdr/E9WA), Feb 16, 1996: SKIN. DAMAGED. CLT - INSPECTION VISUALLY FOUND MISSING TRAILING EDGE HONEYCOMB CORE MATERIAL LOCATED AT THE VERTICAL STAB AT RUDDER STATION 218 RIGHT TRAILING EDGE PANEL. COMP - [SDR 96ZZZM798](https://openairdocs.org/sdr/96ZZZM798), Feb 16, 1996: SKIN. DAMAGED. CLT - INSPECTION FOUND 2 PREVIOUSLY INSTALLED DOUBLERS WITH BLIND FASTENERS LOCATED AT FUSELGE SKIN, FS 727A AT STRINGER 15R AND 16R. INSTALLED EXTERNAL DOUBLER - [SDR 96ZZZM744](https://openairdocs.org/sdr/96ZZZM744), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND MEASURING 12 INCHES BY 2.5 INCHES LOCATED FUSELAGE SKIN AT STATION 927-947 AND STRINGER 14L. INST - [SDR 96ZZZM743](https://openairdocs.org/sdr/96ZZZM743), Feb 16, 1996: SKIN. CRACKED. CLT - INSPECTION VISUALLY FOUND A CRACK THROUGH RIVET .1875 INCH UP AND .125 INCH DOWN LOCATED AT FUSELAGE SKIN AT STATION 251 AND STRINGER 11L. INSTALLED DOUBL - [SDR 96ZZZM742](https://openairdocs.org/sdr/96ZZZM742), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC, FOUND DISBONDED SKIN AND DOUBLER MEASURING 9 INCHES BY 5 INCHES LOCATED AT THE FUSELAGE SKIN AT STATION 288, STRINGER 14L AND ST - [SDR 96ZZZM741](https://openairdocs.org/sdr/96ZZZM741), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC, FOUND DISBONDED SKIN AND DOUBLER AT THE FUSELAGE SKIN MEASURING 5 INCHES BY 18 INCHES LOCATED AT STATION 920 TO 927 AND STRINGER - [SDR 96ZZZM740](https://openairdocs.org/sdr/96ZZZM740), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 3 INCHES BY 4 INCHES AT STATION 967 ABOVE STRINGER 5L. INSTALL - [SDR 96ZZZM739](https://openairdocs.org/sdr/96ZZZM739), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 5 INCHES BY 4 INCHES AT STATION 356, STRINGER 15L AND 16L. INS - [SDR 96ZZZM738](https://openairdocs.org/sdr/96ZZZM738), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 14 INCHES BY 2.5 INCHES AT STATION 902 TO 914 AND STRINGER 13R - [SDR 96ZZZM737](https://openairdocs.org/sdr/96ZZZM737), Feb 16, 1996: SKIN. CRACKED. CLT - INSPECTION VISUALLY FOUND AND VERIFIED WITH HFEC A 1.25 INCH CRACK LOCATED AT FUSELAGE SKIN FS 1137 AND STRINGER 12L. INSTALLED DOUBLER AS PER BOEING SRM - [SDR 96ZZZM736](https://openairdocs.org/sdr/96ZZZM736), Feb 16, 1996: SUPPORT BEAM. CORROSION. CLT - INSPECTION VISUALLY FOUND LEVEL I CORROSION AT THE FUSELAGE FLOOR SUPPORT BEAM LOCATED AT LBL 2 TO LBL 6 AND STATION 1014. FABRICATED REPLACEMENT H-CHANNE - [SDR 96ZZZM735](https://openairdocs.org/sdr/96ZZZM735), Feb 16, 1996: SKIN. GOUGED. CLT - INSPECTION VISUALLY FOUND A 1.5 INCH GOUGE .019 DEEP AT FUSELAGE SKIN LOCATED AT FS 360 1 INCH ABOVE STRINGER 18L. INSTALLED DOUBLER AS PER BOEING SRM 53- - [SDR 96ZZZM734](https://openairdocs.org/sdr/96ZZZM734), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC FOUND DISBONDED SKIN AND DOUBLER AT THE FUSELAGE SKIN LOCATED AT STATION 927 TO 947 AND STRINGER 21R TO STRINGER 20R. REMOVED AND - [SDR 96ZZZM733](https://openairdocs.org/sdr/96ZZZM733), Feb 16, 1996: SKIN. CORROSION. CLT - INSPECTION VISUALLY FOUND A LEVEL I CORRODED PRODUCTION STRINGER SPLICE 6 INCHES AT THE FUSELAGE SKIN LOCATED AT STATION 908 AND STRINGER 20R. REPLACED AN - [SDR 96ZZZM732](https://openairdocs.org/sdr/96ZZZM732), Feb 16, 1996: SKIN. DISBONDED. CLT - INSPECTION VISUALLY FOUND 6 INCH DISBONDED FUSELAGE SKIN LOCATED AT STATION 954 BETWEEN STRINGER 24 AND STRINGER 23R. REPLACED SKIN AS PER USAIR EA NR 580 - [SDR 96ZZZM731](https://openairdocs.org/sdr/96ZZZM731), Feb 16, 1996: ANGLE. CRACKED. CLT - INSPECTION VISUALLY FOUND A 1.5 INCH CRACK LOCATED AT THE FUSELAGE RADIUS OF ANGLE AT FS 1085 AND STRINGER 2L. INSTALLED AND MANUFACTURED ANGLE AS PER BOE - [SDR 96ZZZM730](https://openairdocs.org/sdr/96ZZZM730), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC, FOUND TWO 6 INCHES BY 6 INCHES AND 8 INCHES BY 2 INCHES AREAS OF SKIN AND DOUBLER DISBOND LOCATED AT THE FUSELAGE SKIN BETWEEN S - [SDR 96ZZZM729](https://openairdocs.org/sdr/96ZZZM729), Feb 16, 1996: SKIN. DISBONDED. CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND LOCATED AT STATION 927 TO 947, STRINGER 9L AND STRINGER 10L. INSTALLED FIELD DOUBLERS AS - [SDR 96ZZZM728](https://openairdocs.org/sdr/96ZZZM728), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC, FOUND TWO AREAS OF DISBOND, 14 INCHES BY 8 INCHES AND 4 INCHES BY 8 INCHES LOCATED AT THE FUSELAGE SKIN AT STATION 312-344 AND S - [SDR 96ZZZM727](https://openairdocs.org/sdr/96ZZZM727), Feb 16, 1996: SKIN. DISBONDED. CLT - INSPECTION BY ULTRASONIC FOUND FUSELAGE SKIN AND DOUBLER DISBOND LOCATED AT STATION 635, STRINGER 8R AND STRINGER 9R. INSTALLED FIELD RIVETS AS PER BOEING - [SDR 96ZZZM726](https://openairdocs.org/sdr/96ZZZM726), Feb 16, 1996: SKIN. DISBONDED. CLT - INSPECTION BY ULTRASONIC FOUND FUSELAGE SKIN AND DOUBLER DISBOND 7 INCH BY 2 INCH LOCATED AT STATION 986.5 TO 1016, STRINGER 9R TO STRINGER 10R. INSTALLED - [SDR 96ZZZM725](https://openairdocs.org/sdr/96ZZZM725), Feb 16, 1996: CHORD. CRACKED. CLT - INSPECTION FOUND BY ULTRASONIC AND EDDY CURRENT A CRACK APPROXIMATELY 1 INCH LOCATED AT THE FUSELAGE CHORD, RHS BS 727, OUTBOARD CHORD AT STRINGER 18A. CH - [SDR 96ZZZM724](https://openairdocs.org/sdr/96ZZZM724), Feb 16, 1996: VERTICAL FIN. DENTED. CLT - INSPECTION VISUALLY FOUND A DENT LOCATED AT VERTICAL STABILIZER MEASURING 1 INCH BY 2.5 INCH AT FIN STATION 209.90, RIGHT INSPAR. CUT OUT DAMAGE, INSTALLE - [SDR 96ZZZM723](https://openairdocs.org/sdr/96ZZZM723), Feb 16, 1996: CHORD. CRACKED. CLT - INSPECTION FOUND BY ULTRASONIC AND EDDY CURRENT, A CRACK APPROXIMATELY 1 INCH, LOCATED AT THE FUSELAGE CHORD, RHS BS 727, OUTBOARD AT STRINGER 18A. CHORD - [SDR 96ZZZM722](https://openairdocs.org/sdr/96ZZZM722), Feb 16, 1996: ANGLE. CRACKED. CLT - INSPECTION VISUALLY FOUND A 1.5 INCH CRACK LOCATED AT THE FUSELAGE RADIUS OF ANGLE AT FS 1085 AND STRINGER 2L. INSTALLED AND MANUFACTURED ANGLE AS PER BOE - [SDR 96ZZZM721](https://openairdocs.org/sdr/96ZZZM721), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC, FOUND TWO 6 INCH BY 6 INCH AND 8 INCH BY 2 INCH AREAS OF SKIN AND DOUBLER DISBOND LOCATED AT THE FUSELAGE SKIN BETWEEN STATION 2 - [SDR 96ZZZM720](https://openairdocs.org/sdr/96ZZZM720), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND LOCATED AT STATION 927 TO 947, STRINGER 9L AND STRINGER 10L. INSTALLED FIELD DOUBLERS AS - [SDR 96ZZZM719](https://openairdocs.org/sdr/96ZZZM719), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC, FOUND TWO AREAS OF DISBOND, 14 INCHES BY 8 INCHES AND 4 INCHES BY 8 INCHES LOCATED AT THE FUSELAGE SKIN AT STATION 312-344 AND S - [SDR 96ZZZM718](https://openairdocs.org/sdr/96ZZZM718), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC FOUND FUSELAGE SKIN AND DOUBLER DISBOND LOCATED AT STATION 635, STRINGER 8R AND STRINGER 9R. INSTALLED FIELD RIVETS AS PER BOEING - [SDR 96ZZZM717](https://openairdocs.org/sdr/96ZZZM717), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND 7 INCHES BY 2 INCHES LOCATED AT STATION 986.5 TO 1016, STRINGER 9R TO STRINGER 10R. INST - [SDR 96ZZZM716](https://openairdocs.org/sdr/96ZZZM716), Feb 16, 1996: SKIN. DISBOND. CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND, 13 INCHES BY 13 INCHES LOCATED AT STATION 986.5 TO 1016 AND STRINGER 12R TO STRINGER 13 - [SDR 96ZZZM715](https://openairdocs.org/sdr/96ZZZM715), Feb 16, 1996: SKIN. DISBONDED. CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND MEASURING 12 INCHES BY 2.5 INCHES LOCATED FUSELAGE SKIN AT STATION 927-947 AND STRINGER 14L. INST - [SDR 96ZZZM714](https://openairdocs.org/sdr/96ZZZM714), Feb 16, 1996: SKIN. CRACKED. CLT - INSPECTION VISUALLY FOUND A CRACK THROUGH RIVET .1875 INCH UP AND .125 INCH DOWN LOCATED AT FUSELAGE SKIN AT STATION 251 AND STRINGER 11L. INSTALLED DOUBL - [SDR 96ZZZM713](https://openairdocs.org/sdr/96ZZZM713), Feb 16, 1996: SKIN. DISBONDED. CLT - INSPECTION BY ULTRASONIC FOUND DISBONDED SKIN AND DOUBLER MEASURING 9 INCHES BY 5 INCHES LOCATED AT THE FUSELAGE SKIN AT STATION 288, STRINGER 14L AND STR All 63: https://openairdocs.org/deregistered/N221US-2000-06-14/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA96IA061](https://openairdocs.org/ntsb/DCA96IA061), Jun 10, 1996: Boeing B-737-201 (N221US), Richmond, VA, incident, no damage. Probable cause: The yaw/roll upset of the airplane resulting from the movement of the rudder surface to its blowdown limit. The rudder surface most likely deflected in a direction opposite to that commanded by the… ## FAA accident and incident reports (2) 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 19960514018549I](https://openairdocs.org/incident/19960514018549I), May 14, 1996: Boeing 7372H5 (N221US), Trenton, NJ. Narrative: on 05/14/96 flight 411 took off from Trenton-Mercer County Airport (ttn) en route to bos. After levelling at 10,000 ft. and within 12-15 minutes the… - [Incident 19930914038059I](https://openairdocs.org/incident/19930914038059I), Sep 14, 1993: Boeing 7372H5 (N221US), Syracuse, NY. NR1 engine overheat light on. Diverted to Syracuse. Found 13th stage duct clamp broken. Replaced clamp. ## Other aircraft with N221US - [Registered now](https://openairdocs.org/aircraft/N221US): Costruzioni Aeronautiche Tecna P2010 TDI, S/N 212/US, built 2023 --- 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.