# N16201: Boeing 737-130, registration cancelled 1998-11-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 16, 1998 - Status when cancelled: Valid registration - Airframe: [Boeing 737-130](https://openairdocs.org/model/boeing-737-130) (registry code 1384435) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 19018 - Type of aircraft: Fixed wing multi engine - Last registry action: November 16, 1998 - Mode S code: A0FB8E - Owner when cancelled: [Rfc 737/23 Inc](https://openairdocs.org/faa-owner/RFC%20737%2F23%20INC) - Location: [Cheyenne, WY](https://openairdocs.org/faa-place/WY/Cheyenne) - Owner type: Corporation - Owner's area on the map: 41.1001° N, 104.9249° W: Placed by OpenAirDocs at the center of ZIP code 82001, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N16201 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16201 - Page: https://openairdocs.org/deregistered/N16201-1998-11-16 From the FAA registry file of October 31, 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 737-130: https://openairdocs.org/model/boeing-737-130.md ## Service difficulty reports (25) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9801218](https://openairdocs.org/sdr/CALA9801218), Jul 8, 1998: ACCESSORY UNIT. INOPERATIVE. THE GEAR HANDLE STOPPED IN THE OFF POSITION WHEN RAISING THE GEAR AFTER TAKEOFF. THE GEAR TRIGGER WAS PULLED AND THE GEAR CAME UP. MAINTENANCE REMOVED AND REPLA - [SDR CALA9601797](https://openairdocs.org/sdr/CALA9601797), Dec 11, 1996: WINDOW FRAME. CORRODED. INSPECTION FOUND FORWARD LOWER CORNER OF NR 4 RT CABIN WINDOW FRAME CORRODED. THE WINDOW FRAME WAS REMOVED AND A NEW FRAME WAS FABRICATED AND INSTALLED IAW SRM - [SDR CALA9601796](https://openairdocs.org/sdr/CALA9601796), Dec 11, 1996: SKIN. CRACKED. INSPECTION FOUND .5 INCH CRACKS IN LT FUSELAGE SKIN AT BS 188 TO 251, WL 207 TO 234. THE AREA WAS REPAIRED IAW SRM 51-30-2, BAC DRAWING NR 65-18420, AND EA 5310 - [SDR CALA9601791](https://openairdocs.org/sdr/CALA9601791), Dec 11, 1996: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED ON UPPER CHORD AT STA 294.5 FROM RBL 20 TO LBL 20. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A NEW FLOORBEAM WAS - [SDR CALA9601790](https://openairdocs.org/sdr/CALA9601790), Dec 11, 1996: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT BS 755, STRINGER 19R. THE CRACKED AREA WAS REMOVED IAW SRM 53-30-3. A DOUBLER WAS FABRICATED AND INSTALLED I - [SDR CALA9601789](https://openairdocs.org/sdr/CALA9601789), Dec 11, 1996: SKIN. CORRODED. INSPECTION FOUND EXTERNAL FUSELAGE SKIN LAP BULGED AND ONE FASTENER SHEARED AT FS 380, STRINGER 26R. THE CORROSION WAS REMOVED IAW SRM 51-10-6. FILLER AND DOUBL - [SDR CALA9601788](https://openairdocs.org/sdr/CALA9601788), Dec 11, 1996: STRINGER. CORRODED. INSPECTION FOUND FUSELAGE STRINGER 24L CORRODED FROM FS 970 TO 1000. THE CORRODED SECTION OF STRINGER WAS REMOVED IAW SRM 51-10-6. STRINGER REPAIR PARTS WERE FA - [SDR CALA9601787](https://openairdocs.org/sdr/CALA9601787), Dec 11, 1996: SKIN. CORRODED. INSPECTION FOUND NLG WHEEL WELL UPPER SKIN CORRODED AFT OF ACCESS, STA 240. THE SKIN WAS REPAIRED IAW ECRA 5310-03378. - [SDR CALA9601846](https://openairdocs.org/sdr/CALA9601846), Dec 9, 1996: BEAR STRAP. CORRODED. INSPECTION FOUND E AND E DOOR CUTOUT BEAR STRAP CORRODED AT FORWARD SIDE OF CUTOUT. STRINGER 29 WAS REMOVED AND CORROSION WAS REMOVED FROM SKIN AND BEAR STRAP I - [SDR CALA9601845](https://openairdocs.org/sdr/CALA9601845), Dec 9, 1996: SKIN. CORRODED. INSPECTION FOUND NOSE WHEEL WELL CUTOUT AFT RT CORNER HAD CORRODED SKIN AND STRESSED FASTENERS. LOWER LOBE SKINS WERE CUT AND REMOVED FROM STA 253 TO 312. THE L - [SDR CALA9601786](https://openairdocs.org/sdr/CALA9601786), Dec 9, 1996: STRINGER. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT STRINGER 7R FASTENER ON RT WING UPPER SURFACE, WBL 200. A REPAIR STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND ECRA - [SDR CALA9601844](https://openairdocs.org/sdr/CALA9601844), Dec 7, 1996: SKIN. CORRODED. INSPECTION FOUND FUSELAGE EXTERIOR SKIN LAP CORRODED AT STA 540, STRINGER 26L. REPAIR FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. - [SDR CALA9601772](https://openairdocs.org/sdr/CALA9601772), Dec 7, 1996: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER T-CAP CORRODED AT STA 328, RBL 10 TO RBL 46. THE UPPER T-CAP WAS REMOVED, A NEW UPPER T-CAP WAS FABRICATED AND INSTALLED IAW SR - [SDR CALA9601771](https://openairdocs.org/sdr/CALA9601771), Dec 7, 1996: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN INTERCOSTAL AT STA 357, STRINGER 16L. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. - [SDR CALA9601769](https://openairdocs.org/sdr/CALA9601769), Dec 6, 1996: WEB. CORRODED. INSPECTION FOUND AFT LAV LT PAN CORRODED AROUND DUMP CHUTE AND CENTER SUBSTRUCTURE CHANNEL CORRODED AT UPPER SURFACE. THE FLOOR WEB AND CENTER CHANNEL WERE REMO - [SDR CALA9601770](https://openairdocs.org/sdr/CALA9601770), Dec 4, 1996: STIFFENER. CORRODED. INSPECTION FOUND STA 285.62 NOSE WHEEL WELL RT VERTICAL STIFFENER CORRODED 3 INCHES FROM LOWER END AND 2 INCHES FROM UPPER END. THE VERTICAL STIFFENER WAS REMOV - [SDR CALA9601842](https://openairdocs.org/sdr/CALA9601842), Nov 25, 1996: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED BETWEEN RIVETS AT BS 964, STRINGER 20L. THE CORRODED AREA OF SKIN WAS CUT OUT, DOUBLERS AND FILLERS WERE FABRICATED AND - [SDR CALA9601843](https://openairdocs.org/sdr/CALA9601843), Nov 16, 1996: SKIN. CRACKED. INSPECTION FOUND A 1.75 INCH CRACK IN FUSELAGE SKIN AT BS 775, STRINGER 19R. THE CRACKED AREA WAS CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM - [SDR CAL960529](https://openairdocs.org/sdr/CAL960529), Apr 25, 1996: SKIN. CRACKED. GSO - REMOVED DAMAGE AREA AND FABRICATED DOUBLER, INSTALLED DOUBLER AT STRINGER 20R - STATION 192 PER SRM 53-30-3. (M) - [SDR CAL960511](https://openairdocs.org/sdr/CAL960511), Apr 21, 1996: SWITCH. INOPERATIVE. FLT NR 234 - EWR - RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT ILLUMINATED, AFTER GEAR LOWERED DURING APPROACH FOR LANDING. CYCLED GEAR, RED AND GREEN LIGHT FLICKE - [SDR CAL951147](https://openairdocs.org/sdr/CAL951147), Dec 13, 1995: SKIN. CORRODED. GSO - INSPECTION FOUND THE FUSELAGE SKIN AND DOUBLERS CORRODED AT AFT LOWER CORNER OF C-1 DOORWAY. THE CORROSION WAS REMOVED. REPAIR DOUBLERS WERE FABRICATED AN - [SDR CAL951145](https://openairdocs.org/sdr/CAL951145), Dec 13, 1995: LIGHT. INOPERATIVE. GSO - INSPECTION FOUND THE LEFT OVERWING INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. THE EMERGENCY EXIT LIGHT ASSEMBLY WAS REMOVED, RECHARGED, AND INSTALLED. (M) - [SDR CAL951144](https://openairdocs.org/sdr/CAL951144), Dec 13, 1995: BATTERY PACK. DISCHARGED. GSO - INSPECTION FOUND THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 23 INOPERATIVE. THE EMERGENCY EXIT LIGHT BATTERY PACK WAS REMOVED AND REPLACED. (M) - [SDR CAL951143](https://openairdocs.org/sdr/CAL951143), Dec 13, 1995: LIGHT. INOPERATIVE. GSO - INSPECTION FOUND THE L-1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. THE L-1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY WAS REMOVED AND REPLACED. (M) - [SDR CAL951142](https://openairdocs.org/sdr/CAL951142), Dec 13, 1995: BATTERY PACK. DISCHARGED. GSO - INSPECTION FOUND BOTH RT WING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (M) ## 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 19950129001939I](https://openairdocs.org/incident/19950129001939I), Jan 29, 1995: Boeing 737130 (N16201), Buffalo, NY. Narrative: on January 29, 1995 on flight from newark, NJ to Buffalo, NY Continental flight 1458, a Boeing 737, N16201, was unable to stabilize pressurization… - [Incident 19941117040539I](https://openairdocs.org/incident/19941117040539I), Nov 17, 1994: Boeing 737130 (N16201), Buffalo, NY. Low oil light on. Shutdown. Landed destination. NR6 bearing oil scavage tube fractured. Ferried to cle for service. ## Other aircraft with N16201 - [Cancelled 1948-04-29](https://openairdocs.org/deregistered/N16201-1948-04-29): Waco ZQC-6, S/N 4398, built 1936. Owner: [Stinson Flying Corporation](https://openairdocs.org/faa-owner/STINSON%20FLYING%20CORPORATION), [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco) --- 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.