# N14241: Boeing 737-2CO, registration cancelled 1999-06-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 15, 1999
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-2CO](https://openairdocs.org/model/boeing-737-2co) (registry code 1384488)
- Serial number: 20070
- Type of aircraft: Fixed wing multi engine
- Certificate issued: May 11, 1999
- Last registry action: May 12, 1999
- Mode S code: A0AD1C
- Owner when cancelled: [Rfc 737/23 Inc](https://openairdocs.org/faa-owner/RFC%20737%2F23%20INC)
- Location: [Aurora, CO](https://openairdocs.org/faa-place/CO/Aurora)
- Owner type: Corporation
- Owner's area on the map: 39.6636° N, 104.8378° W: Placed by OpenAirDocs at the center of ZIP code 80014, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N14241
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14241
- Page: https://openairdocs.org/deregistered/N14241-1999-06-15

From the FAA registry file of November 5, 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 737-2CO: https://openairdocs.org/model/boeing-737-2co.md

## Service difficulty reports (44)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR CALA9801914](https://openairdocs.org/sdr/CALA9801914), Oct 7, 1998: LINE. CHAFED. THE 'A' HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE TO EWR. THE GEAR AND FLAPS WERE LOWERED MANUALLY AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE F
- [SDR CALA9801626](https://openairdocs.org/sdr/CALA9801626), Sep 4, 1998: SKIN. CORRODED. INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 435 TO 440, STRINGER 24R. A DOUBLER WAS INSTALLED IAW SRM 53-30-3.
- [SDR CALA9801617](https://openairdocs.org/sdr/CALA9801617), Sep 1, 1998: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE KEEL BEAM LOWER SKIN AT STA 727, RBL 5. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-03, FIGURE 40.
- [SDR CALA9800902](https://openairdocs.org/sdr/CALA9800902), May 24, 1998: WEB. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN LT WHEEL WELL SHEAR WEB AT STA 727. A REPAIR WAS INSTALLED IAW DRAWING 65C29228.
- [SDR CALA9701214](https://openairdocs.org/sdr/CALA9701214), Jul 25, 1997: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT HORIZONTAL STABILIZER SKIN BETWEEN STA 111.1 AND 126.6. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01369.
- [SDR CALA9701218](https://openairdocs.org/sdr/CALA9701218), Jul 16, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED FROM FRAME TO FRAME AT STA 986.5. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-9.
- [SDR CALA9701215](https://openairdocs.org/sdr/CALA9701215), Jul 14, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 967 TO 986, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-3 AND 51-10-2.
- [SDR CALA9701217](https://openairdocs.org/sdr/CALA9701217), Jul 13, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 312, RBL 56. THE CORRODED AREA WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 
- [SDR CALA9701216](https://openairdocs.org/sdr/CALA9701216), Jul 9, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 947.5 TO 995. THE CORRODED SECTION WAS REMOVED, A REPAIR T-SECTION AND FILLER WERE FABRICATED AND INSTALLED IAW S
- [SDR CALA9700076](https://openairdocs.org/sdr/CALA9700076), Jan 26, 1997: HYD LINE. CHAFED. THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO SHORTLY AFTER TAKEOFF. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE NR 2 A-SYSTEM LOW PRESSURE LIGHT. C
- [SDR CALA9601643](https://openairdocs.org/sdr/CALA9601643), Nov 14, 1996: FUEL PUMP. FAILED. THE NR 1 ENGINE FLAMED OUT WHILE CRUISING AT FL 250 EN ROUTE. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGI
- [SDR CALA9601317](https://openairdocs.org/sdr/CALA9601317), Sep 15, 1996: SKIN. CRACKED. THE AIRCRAFT SKIN WAS CRACKED AT C1 DOOR DURING CARGO LOADING. THE CRACK WAS LOCATED AT STA 472.4 BETWEEN STRINGER 20R AND 21R AND MEASURED 1.5 INCH LONG. A REP
- [SDR CALA9601105](https://openairdocs.org/sdr/CALA9601105), Jul 25, 1996: SKIN. BULGED. INSPECTION FOUND FUSELAGE SKIN BULGED AT STA 259, STRINGER 24L. THE BULGED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53
- [SDR CALA9601104](https://openairdocs.org/sdr/CALA9601104), Jul 25, 1996: FLOOR BEAM. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM LOWER T-CHORD AT STA 675, BBL ZERO AND A 2 INCH CRACK WAS ALSO FOUND IN CHORD AT STA 685, BBL ZERO. A REPAIR AT STA
- [SDR CALA9601103](https://openairdocs.org/sdr/CALA9601103), Jul 25, 1996: WEB. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN PRESSURE WEB AT STA 675, BL ZERO TO LBL 1.5. THE CRACKED WEB AREA WAS REMOVED AND A NEW SECTION OF WEB WAS INSTALLED IAW EC
- [SDR CALA9601106](https://openairdocs.org/sdr/CALA9601106), Jul 17, 1996: BATTERY PACK. DISCHARGED. INSPECTION FOUND THE R-2 DOOR SLIDE LIGHT INOPERATIVE. THE BATTERY PACK WAS REPLACED AND THE LANYARD SWITCH WAS CLEANED. THE LIGHT TESTED GOOD IAW MM 33-51-0.
- [SDR CAL960382](https://openairdocs.org/sdr/CAL960382), Mar 21, 1996: HYD LINE. CHAFED. FLT NR 1598 - GSO - THE AIRCRAFT LOST 'A' SYSTEM HYDRAULIC QUANTITY AFTER TAKEOFF FROM GSO. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. M
- [SDR CAL951017](https://openairdocs.org/sdr/CAL951017), Nov 3, 1995: ACCESSORY UNIT. INOPERATIVE. ORF - FLT 1215 - WHEN LANDING GEAR WAS EXTENDED ON APPROACH TO ORF, THE NOSE GEAR INITIALLY INDICATED GREEN, THEN THE RED LIGHT ILLUMINATED AND THE GREEN LIGHT 
- [SDR CAL950996](https://openairdocs.org/sdr/CAL950996), Oct 30, 1995: AIR DATA COMP. INOPERATIVE. CLE - FLT 1255 - WHILE CRUISING AT FL 220 EN ROUTE FROM BDL TO CLE AND WITH AUTOPILOT ENGAGED IN 'B' MODE, THE AIRCRAFT MADE AN ABRUPT BANK TO THE RIGHT. THE AU
- [SDR CAL950583](https://openairdocs.org/sdr/CAL950583), Jun 30, 1995: SKIN. CRACKED. GSO - INSPECTION FOUND A .25 INCH CRACK IN SKIN AT FASTENER STA 727A, S10R. THE CRACKED AREA OF SKIN WAS CUT OUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED 
- [SDR CAL950582](https://openairdocs.org/sdr/CAL950582), Jun 30, 1995: TEAR STRAP. CRACKED. GSO - INSPECTION FOUND A .50 INCH CRACK IN TEAR STRAP AT FASTENER HOLE BELOW STR 14, LT STA 727A. A TEAR STRAP WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X)
- [SDR CAL950581](https://openairdocs.org/sdr/CAL950581), Jun 30, 1995: STRINGER. CRACKED. GSO - INSPECTION FOUND .25 INCH CRACKS AT THREE FASTENERS ON BOTTOM ROW OF STR 14R AT STA 727A. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM
- [SDR CAL950580](https://openairdocs.org/sdr/CAL950580), Jun 30, 1995: DOUBLER. CRACKED. GSO - INSPECTION FOUND A .25 INCH CRACK AT UPPER FORWARD FASTENER ON DOUBLER REPAIR AT BS 727A, S17L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 25,
- [SDR CAL950579](https://openairdocs.org/sdr/CAL950579), Jun 30, 1995: WEB. CRACKED. GSO - INSPECTION FOUND A .75 INCH CRACK IN CUSP MEMBRANE BETWEEN STATION 616 AND 639L. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-0. (M)
- [SDR CAL950578](https://openairdocs.org/sdr/CAL950578), Jun 30, 1995: STRINGER TIES. CRACKED. GSO - INSPECTION FOUND A .25 INCH CRACK IN EACH OF TWO STRINGER TIES AT STRINGERS 4L AND 4R, STATION 702. THE STRINGER TIES WERE REMOVED AND REPLACED IAW SRM 51
- [SDR CAL950577](https://openairdocs.org/sdr/CAL950577), Jun 30, 1995: WEB. CRACKED. GSO - INSPECTION FOUND A .5 INCH CRACK IN CUSP MEMBRANE BETWEEN STATION 638 AND 663L. A WEB WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-0. (M)
- [SDR CAL950576](https://openairdocs.org/sdr/CAL950576), Jun 30, 1995: STRINGER TIES. CRACKED. GSO - INSPECTION FOUND A .25 INCH CRACK IN EACH OF THE STRINGER TIES AT STRINGERS 5R, 2L, 3L, AND 4L, STATION 685. THE STRINGER TIES WERE REMOVED AND REPLACED I
- [SDR CAL950575](https://openairdocs.org/sdr/CAL950575), Jun 30, 1995: STRINGER TIES. CRACKED. GSO - INSPECTION FOUND STRINGER TIES CRACKED AT STATION 767 STRINGERS 4L AND 5L. THE CRACKS WERE .25 INCH LONG. THE STRINGER TIES WERE REMOVED AND REPLACED IAW 
- [SDR CAL950573](https://openairdocs.org/sdr/CAL950573), Jun 30, 1995: WEB. CRACKED. GSO - INSPECTION FOUND A 2 INCH CRACK IN WEB AT BS 947 FORWARD OF R-2 DOOR. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2
- [SDR CAL950572](https://openairdocs.org/sdr/CAL950572), Jun 30, 1995: TEAR STRAP. CRACKED. GSO - INSPECTION FOUND A .5 INCH CRACK IN TEAR STRAP AT FASTENER HOLE RT STATION 752 BELOW STRINGER 14. A NEW TEAR STRAP WAS FABRICATED AND INSTALLED IAW SRM 53
- [SDR CAL950571](https://openairdocs.org/sdr/CAL950571), Jun 30, 1995: ANGLE. CRACKED. GSO - INSPECTION FOUND A .75 INCH CRACK IN RT OUTBOARD STIFFENER ANGLE AT STATION 291 TO 294. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30
- [SDR CAL950570](https://openairdocs.org/sdr/CAL950570), Jun 30, 1995: STRINGER TIES. CRACKED. GSO - INSPECTION FOUND STRINGER TIES AT STATION 597 STRINGERS 5R, 4R, AND 4L CRACKED. THE CRACKS WERE .25 INCH LONG. THE STRINGER TIES WERE REMOVED AND REPLACED
- [SDR CAL950569](https://openairdocs.org/sdr/CAL950569), Jun 30, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A .75 INCH CRACK THROUGH INBOARD CHORD AND WEB OF STATION 639 FRAME AT STRINGER 16R. A NEW CHORD AND WEB WERE INSTALLED PER BOEING DRAWIN
- [SDR CAL950568](https://openairdocs.org/sdr/CAL950568), Jun 30, 1995: SKIN. CRACKED. GSO - INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN ON RIGHT SIDE AT STATION 727 BELOW S18. REPAIR DOUBLERS WERE INSTALLED IAW DRAWING 65C28086 AND SERVICE
- [SDR CAL950565](https://openairdocs.org/sdr/CAL950565), Jun 30, 1995: SKIN. CRACKED. GSO - INSPECTION FOUND A .5 INCH CRACK IN LEFT FORWARD ENTRY DOOR LOWER FRAME SKIN. THE SKIN WAS REPAIRED IAW ECRA 5330-02294 AND BAC DRAWING 65C27257. (M)
- [SDR CAL950564](https://openairdocs.org/sdr/CAL950564), Jun 30, 1995: RIB. CRACKED. GSO - INSPECTION FOUND A .75 INCH CRACK IN INBOARD SIDE NR 5 RIB FROM THE FRONT OF THE LEFT HORIZONTAL STABILIZER. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FAB
- [SDR CAL950562](https://openairdocs.org/sdr/CAL950562), Jun 30, 1995: INTERCOSTAL. CORRODED. GSO - INSPECTION FOUND CORROSION ON INTERCOSTAL FLANGE AT STATION 847-867 BELOW STRINGER 24. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 
- [SDR CAL950561](https://openairdocs.org/sdr/CAL950561), Jun 30, 1995: FLOOR SUPPORT. CORRODED. GSO - INSPECTION FOUND A .75 INCH CRACK IN CABIN FLOOR SUPPORT AND ANGLE AT BS 540, BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5. (M)
- [SDR CAL950560](https://openairdocs.org/sdr/CAL950560), Jun 30, 1995: SUPPORT. CORRODED. GSO - INSPECTION FOUND CORROSION ON FLOOR SUPPORT PANEL ABOVE S25L BETWEEN BS 887 AND BS 907. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 5
- [SDR CAL950559](https://openairdocs.org/sdr/CAL950559), Jun 30, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT BS 400 BETWEEN S20L AND S21L. A NEW FRAME AND FASTENERS WERE FABRICATED AND INSTALLED IAW BOEING DRAWING 65C2
- [SDR CAL950558](https://openairdocs.org/sdr/CAL950558), Jun 30, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT BS 420 BETWEEN S20L AND S21L AND A .5 INCH CRACK IN FRAME AT BS 420 S22L. REPAIR WAS INSTALLED IAW BOEING DRA
- [SDR CAL950557](https://openairdocs.org/sdr/CAL950557), Jun 30, 1995: STRINGER. CORRODED. GSO - INSPECTION FOUND STRINGER 22R CORRODED AT BS 355. A REPAIR WAS INSTALLED IAW SRM 53-10-3 AND 51-30-2. (M)
- [SDR CAL950556](https://openairdocs.org/sdr/CAL950556), Jun 30, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME AT BS 500. A NEW FRAME AND FASTENERS WERE INSTALLED IAW B737 DRAWING 65C25113-A AND SRM 51-30-2. (M)
- [SDR CAL950555](https://openairdocs.org/sdr/CAL950555), Jun 30, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND THE FRAME AT BS 460 CRACKED BETWEEN S22L AND S21L AND BETWEEN S21L AND S20L. BOTH CRACKS WERE .5 INCH LONG. A NEW FRAME AND SPLICE WERE I

## FAA accident and incident reports (3)

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 19950201002699I](https://openairdocs.org/incident/19950201002699I), Feb 1, 1995: Boeing 737275 (N14241), Buffalo, NY, Minor damage. Narrative: on February 1,1995, at 0735 EST, a Boeing 737, N14241, operated by Continental airlines inc., during landing at Buffalo international airport,…
- [Incident 19930729030379I](https://openairdocs.org/incident/19930729030379I), Jul 29, 1993: Boeing 737200 (N14241), Baltimore, MD. NR2 engine secured due to loss of oil quanity on climb. Returned. Found facture in NR2 accessory gear box housing.
- [Incident 19910808040199I](https://openairdocs.org/incident/19910808040199I), Aug 8, 1991: Boeing 737200 (N14241), Detroit, MI, Minor damage. Disposable diaper caught in lavatory dump valve. Fluid leaked,forming ice. Ice broke loose damaging stabilizer.

## Other aircraft with N14241

- [Cancelled 1937-08-03](https://openairdocs.org/deregistered/N14241-1937-08-03): Northrop DELTA 1D, S/N 38. Owner: [Vimalert Co Ltd Inc](https://openairdocs.org/faa-owner/VIMALERT%20CO%20LTD%20INC), [Jersey City, NJ](https://openairdocs.org/faa-place/NJ/Jersey%20City)

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