N223USBoeing 737-201
This N-number isn't registered right now. Below is its last known registration, canceled Feb 12, 2004.
Safety record in brief:No NTSB accidents or incidents since 198221 ADs may apply50 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Belina Export INC
- Owner type
- Non Citizen Corporation
- City, state
- Miami, FL
- Certificate issued
- Feb 11, 2004
- Canceled
- Feb 12, 2004
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Boeing
- Model
- 737-201
- Serial number
- 21665
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 100
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A1EDF9
Engine
- Type
- Turbo-fan
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2004Belina Export INCMiami, FL
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (21)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2019-14-02 | Hydraulic power | Aug 27, 2019 | Airframe (737-201) |
| 2002-20-07 R1 | Boeing Model 737 Series Airplanes | Nov 12, 2002 | Airframe (737-201) |
| 2002-20-07 | Boeing Model 737 Series Airplanes | Nov 12, 2002 | Airframe (737-201) |
| 2001-11-11 | Boeing Model 737, 747, and 777 Series Airplanes | Jul 16, 2001 | Airframe (737-201)Serial numbers per Boeing Service Bulletins 737-25-1371 Rev 2, 737-25-1407, 747-25-3196 Rev 1, 777-25-0111 Rev 1 |
| 2001-10-14 | Boeing Model 737, 747, 757, 767, and 777 Series Airplanes | Jun 8, 2001 | Airframe (737-201)Serial numbers per Boeing Special Attention Service Bulletins 737-35-1076, 737-35-1077, 747-35-2111, 757-35-0021, 757-35-0022, 767-35-0043, 767-35-0044, 777-35-0008, all dated March 1, 2001. Only with: Equipped with chemical oxygen generators. |
Show all 21 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2001-08-24 | Boeing Model 737 Series Airplanes | May 10, 2001 | Airframe (737-201) |
| 2000-22-02 R1 | Boeing Model 737 Series Airplanes | Nov 13, 2000 | Airframe (737-201) |
| 2000-22-02 | Boeing Model 737 Series Airplanes | Nov 13, 2000 | Airframe (737-201) |
| 2000-15-16 | Boeing Model 737, 757, 767, and 777 Series Airplanes | Sep 12, 2000 | Airframe (737-201)Certain serial numbers: 737 1–2984; 757 1–798; 767 1–682; 777 1–083. Only with: Ranges are line numbers; equipped with Puritan-Bennett passenger and flight attendant oxygen masks as listed in Boeing Service Bulletins 737-35-1049, 757-35-0014, 767-35-0033, or 777-35-0005. |
| 99-11-05 | Boeing Model 737 Series Airplanes | Jun 28, 1999 | Airframe (737-201) |
| 99-22-16 | Boeing Model 737 Series Airplanes | Dec 7, 1999 | Airframe (737-201)Serial numbers per Boeing Service Bulletin 737-52-1128, dated April 22, 1999, or Boeing Service Bulletin 737-52-1137, dated May 13, 1999 |
| 98-13-12 R1 | Boeing Model 737, 747, 757, 767, and 777 Series Airplanes | Dec 28, 1998 | Airframe (737-201)Serial numbers per Boeing Alert Service Bulletins 737-27A1212, 747-27A2368 Revision 2, 757-27A0128, 767-27A0156, 777-27A0029 Revision 1 |
| 98-22-10 | Boeing Model 737 Series Airplanes | Nov 12, 1998 | Airframe (737-201)Serial numbers per Boeing Service Bulletin 737-53A1108, Revision 5, dated October 26, 1989 |
| 98-18-20 | Boeing Model 727 and Model 737 Series Airplanes Equipped with J.C. Carter Company Fuel… | Oct 21, 1998 | Airframe (737-201)Only with: Equipped with J.C. Carter Company fuel valve actuators P/N 40574-2 (Kearfott Models 3715-7 and -8) or 40574-5 (Kearfott Model 3715-9). |
| 98-13-12 | Boeing Model 737, 747, 757, 767, and 777 Series Airplanes | Jul 6, 1998 | Airframe (737-201)Serial numbers per Boeing Alert Service Bulletins 737-27A1212, 747-27A2368, 757-27A0128, 767-27A0156, and 777-27A0029, dated March 26, 1998 |
| 98-03-10 | Boeing Model 737, 747, 757, and 767 Series Airplanes | Feb 19, 1998 | Airframe (737-201)Certain serial numbers: 737 1–2836; 747 1–1104; 757 1–731; 767 1–642. Only with: Equipped with non-powered IPECO pilots' seats; ranges are line position numbers. |
| 97-22-07 | Boeing Model 737 Series Airplanes | Nov 12, 1997 | Airframe (737-201)Certain serial numbers: 737 292–2565. Only with: Limited to airplanes with line numbers 292 through 2565 inclusive. |
| 97-18-06 | Boeing Model 737 Series Airplanes | Nov 12, 1997 | Airframe (737-201) |
| 97-05-10 | Boeing Model 737 Series Airplanes | Mar 19, 1997 | Airframe (737-201)Only with: Having a main rudder power control unit (PCU) identified in Boeing Service Letter 737-SL-27-112-B, dated February 6, 1997. |
| 97-04-01 | Boeing Model 737 Series Airplanes | Mar 21, 1997 | Airframe (737-201)Serial numbers per Boeing Service Bulletin 737-27-1155, dated October 26, 1989, as revised by Notices of Status Change 737-27-1155NSC1, NSC2, and NSC3 |
| 95-23-10 | Boeing Model 737 Series Airplanes | Dec 13, 1995 | Airframe (737-201) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (50)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Fuselage · angle · corrodedJun 19, 2006
FOUND ANGLE CORRODED STA 727E TO 767. REPLACED TRANSITION ANGLE IAW SRM 51-10-02 LEVEL 1 C53-202-01, DEFECT SIZE: .5" BY .750".
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor support · corrodedMay 30, 2006
FOUND LBL 33, BETWEEN BS 324-345 CORRODED. FABRICATED AND INSTALLED REPLACEMENT PART PER SRM 53-00-51, 51-40-05, 51-40-02, DEFECT SIZE: .3"L BY 1.0" W BY .015"D.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedFeb 24, 2006
STA 807 BETWEEN S8L AND 9L AT OVERHEAD BIN LOWER ATTACH POINT CRACKED. FABRICATED REPAIR PARTS AND INSTALLED IAW TR 53-10-20C, DEFECT SIZE: 1 INCH.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · floor support · corrodedFeb 22, 2006
MAIN DECK, STA 337-365, RBL 60, WL 208 AT 1R DOOR; TASK C53-222-03 CORROSION. FAB'D NEW FLOOR SUPPORT CHANNEL PER SRM 51-40-02, 53-00-51, 51-20-01, 51-21-10, 52-11-25, DEFECT SIZE: 6"L X 2"W X .024"D & 7"L X 2.5"W X .040"D.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · intercostal · crackedJan 30, 2006
FOUND INTERCOSTAL CRACKED, BS 660 S-14L. REMOVED DAMAGE AND ISNTALLED REPAIR PARTS IAW EO 5304R143, DEFECT SIZE: 1".
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · corrodedJan 23, 2006
LEFT Z-ANGLE BETWEEN 312 TO STA 344 CORROSION. REPLACED WITH IDENTICAL PART, NEW Z-ANGLE IAW SRM 51-40-02, DEFECT SIZE: .5 X 2 INCH.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · seat track · corrodedNov 22, 2003
CLT - FOUND SEAT TRACK CORRODED .125 SQUARE INCH AREA, FRAME 63 RBL 17.75. DAMAGED TRACK REMOVED AND REPLACED WITH NEW SECTION PER SRM 51-74-00 AND 51-72-11. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedOct 24, 2000
CLT - FOUND SKIN CRACKED 1.5 INCH, FUSELAGE SKIN STATION 942 JUST ABOVE STRINGER 22L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Air conditioning and pressurization · controller · failedJun 5, 2000
MKE - FLT 891 - ON CLIMB-OUT, THE PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED. CAPT TOOK OVER FOR THE FIRST OFFICER, WHO WAS FLYING THE A/C, AND THE FIRST OFFICER WENT THROUGH THE QUICK REFERENCE HANDBOOK PROCEDURES. SWITCHED TO STANDBY SYSTEM AND CABIN WENT TO 10,000 FT WITH WARNING HORN SOUNDING.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · crackedFeb 28, 2000
CLT - FOUND 1.5 INCH CRACK ATTACH ANGLE, BS 664, STRINGER 18A, ATTACH ANGLE IT W/W. FABRICATED ATTACH ANGLE PER EO 5393G256 AND SRM 51-40-03. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 50 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026