# N14233: Boeing 737-217, registration cancelled 1999-06-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 24, 1999
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-217](https://openairdocs.org/model/boeing-737-217) (registry code 1384464)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 19887
- Type of aircraft: Fixed wing multi engine
- Certificate issued: March 31, 1999
- Last registry action: March 31, 1999
- Mode S code: A0ACFB
- 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/N14233
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=14233
- Page: https://openairdocs.org/deregistered/N14233-1999-06-24

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 737-217: https://openairdocs.org/model/boeing-737-217.md

## Service difficulty reports (52, newest 50)

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

- [SDR CALA9801858](https://openairdocs.org/sdr/CALA9801858), Sep 25, 1998: LINE. LEAKING. THE NR 1 ENGINE THROTTLE WAS TWO KNOBS AHEAD OF NR 2 WITH CLIMB POWER SET OUT OF MSP. THE SPLIT INCREASED TO ABOUT 3 KNOBS DIFFERENCE AS CLIMB PROGRESSED. FUEL 
- [SDR CALA9800039](https://openairdocs.org/sdr/CALA9800039), Jan 14, 1998: CONTROL CABLE. OUT OF ADJ. THE LANDING GEAR HANDLE COULD NOT BE MOVED BEYOND THE OFF POSITION AFTER TAKEOFF. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO BOS WH
- [SDR CALA9800017](https://openairdocs.org/sdr/CALA9800017), Jan 12, 1998: SOLENOID. INOPERATIVE. THE LANDING GEAR HANDLE WOULD NOT GO PAST THE OFF DETENT AFTER TAKEOFF. THE OVERRIDE DID NOT WORK EITHER. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHO
- [SDR CALA9701377](https://openairdocs.org/sdr/CALA9701377), Sep 20, 1997: HYD LINE. CHAFED. THE A-HYDRAULIC SYSTEM BEGAN TO LEAK SLOWLY WHILE EN ROUTE. THE HYDRAULIC PUMPS WERE TURNED OFF BEFORE LOW PRESSURE LIGHTS ILLUMINATED. THE AIRCRAFT WAS DIVERTE
- [SDR CALA9700160](https://openairdocs.org/sdr/CALA9700160), Feb 6, 1997: SKIN. CRACKED. INSPECTION FOUND A 4.5 INCH CRACK IN RT WING LEADING EDGE SKIN AT WS 190. THE CRACKED AREA WAS REMOVED, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-30
- [SDR CALA9700176](https://openairdocs.org/sdr/CALA9700176), Feb 5, 1997: ANGLE. CRACKED. INSPECTION FOUND A 2.5 INCH CRACK IN RIB LOWER CHORD ANGLE AT S3 IN FUEL ACCESS PANEL 7202 AT LT WING FUEL TANK, WBL 135.5. THE CRACKED AREA WAS REMOVED, A REPA
- [SDR CALA9700175](https://openairdocs.org/sdr/CALA9700175), Feb 5, 1997: ANGLE. CRACKED. INSPECTION FOUND STA 540 WING TO BODY FRAME CRACKED LOWER AREA LBL 31, T-ANGLE WAS CRACKED INTO TWO PIECES. THE CRACKED SECTION WAS REMOVED, ANGLES AND T-CHORD 
- [SDR CALA9700172](https://openairdocs.org/sdr/CALA9700172), Feb 5, 1997: WEB. CRACKED. INSPECTION FOUND THREE EACH CRACKS AT RIVETS OF WEB UNDER NR 3 SEAT TRACK AT BS 715. THE CRACKS WERE APPROXIMATELY 2 INCHES LONG. THE CRACKED AREAS WERE REMOVED
- [SDR CALA9700171](https://openairdocs.org/sdr/CALA9700171), Feb 5, 1997: BULKHEAD WEB. PUNCTURED. INSPECTION FOUND A .25 INCH DIAMETER PUNCTURE IN AFT PRESSURE BULKHEAD WEB AT 8:30 POSITION, TWO FEET FROM CENTER. THE DAMAGED AREA WAS REMOVED, A DOUBLER AND F
- [SDR CALA9700170](https://openairdocs.org/sdr/CALA9700170), Feb 5, 1997: SKIN. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN SKIN PANEL AT LEADING EDGE STA 213 OF LT WING LOWER SURFACE. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-0 AND 51-
- [SDR CALA9700169](https://openairdocs.org/sdr/CALA9700169), Feb 5, 1997: STRINGER. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN STRINGER AT STA 907. THE CRACKED SECTION OF STRINGER WAS REMOVED IAW SRM 53-10-3, STRINGER SPLICES WERE FABRICATED AND INSTAL
- [SDR CALA9700168](https://openairdocs.org/sdr/CALA9700168), Feb 5, 1997: STRINGER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF STRINGER 6L AT STA 787. THE CRACKED SECTION OF STRINGER WAS REMOVED, A STRINGER REPAIR WAS FABRICATED AND INSTALLE
- [SDR CALA9700167](https://openairdocs.org/sdr/CALA9700167), Feb 5, 1997: FITTING. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT BOTTOM AFT FACE OF VERTICAL STABILIZER LT AFT OUTBOARD FITTING TO LUG. THE CRACKED FITTING WAS REMOVED, A NEW FITTING WAS DRI
- [SDR CALA9700166](https://openairdocs.org/sdr/CALA9700166), Feb 5, 1997: SUPPORT. BROKEN. INSPECTION FOUND FORWARD CARGO PIT FLOOR SUPPORT BROKEN AT STA 490 ABOVE STRINGER 28L. THE BROKEN SECTION WAS REMOVED IAW SRM 53-10-1 AND 51-30-2, A NEW SECTION
- [SDR CALA9700159](https://openairdocs.org/sdr/CALA9700159), Feb 4, 1997: FRAME. CORRODED. INSPECTION FOUND STA 250 RT VERTICAL STIFFENER, STA 277 RT FRAME WEB, STA 270 RT SHEAR TIE ANGLE CHORD IN RT NOSE WHEEL WELL CORRODED. A VERTICAL BEAM, FRAME WE
- [SDR CALA9700158](https://openairdocs.org/sdr/CALA9700158), Feb 4, 1997: FRAME. CORRODED. INSPECTION FOUND STA 270 LT FRAME, STA 277 LT CAP ANGLE, FRAME WEB, STIFFENER CHANNELS AT STA 270 AND 277, AND BEAR STRAP AT STA 277 LT CORRODED. FRAME ANGLES, 
- [SDR CALA9700157](https://openairdocs.org/sdr/CALA9700157), Feb 4, 1997: BULKHEAD. CRACKED. INSPECTION FOUND A 8.25 INCH CRACK AT RBL 7.5 AND A 5.25 INCH CRACK AT LBL 6.12 IN BULKHEAD, STA 294.5. THE CRACKED AREAS WERE CUT OUT, DOUBLERS AND FILLERS WER
- [SDR CALA9700146](https://openairdocs.org/sdr/CALA9700146), Feb 3, 1997: FRAME. CRACKED. INSPECTION FOUND FRAME CRACKED AND BENT AT STA 987, BL ZERO - RBL 10. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-30-2.
- [SDR CALA9700145](https://openairdocs.org/sdr/CALA9700145), Feb 3, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED BETWEEN SEAT TRACKS 2-13 AT STA 360. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-9.
- [SDR CALA9700144](https://openairdocs.org/sdr/CALA9700144), Feb 3, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 744, RBL 15 TO LBL 15. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED. A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED
- [SDR CALA9700143](https://openairdocs.org/sdr/CALA9700143), Feb 3, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 980. THE UPPER FLANGE WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 51-30-2.
- [SDR CALA9700142](https://openairdocs.org/sdr/CALA9700142), Feb 3, 1997: SUPPORT. CRACKED. INSPECTION FOUND TWO 8 INCH CRACKS IN FORWARD CARGO PIT FLOOR SUPPORT AT STA 460, RBL 14. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 
- [SDR CALA9700141](https://openairdocs.org/sdr/CALA9700141), Feb 3, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT STA 328, RBL 24 TO RBL 50. THE UPPER CHORD OF BEAM WAS REMOVED. REPAIRS WERE FABRICATED AND INSTALLED IAW
- [SDR CALA9700138](https://openairdocs.org/sdr/CALA9700138), Feb 3, 1997: SKIN. GOUGED. INSPECTION FOUND AFT CARGO DOOR CUTOUT FORWARD LOWER CORNER SKIN GOUGED. THE GOUGED SKIN WAS CUT OUT, REPAIR FILLERS AND DOUBLER WERE FABRICATED AND INSTALLED I
- [SDR CALA9700137](https://openairdocs.org/sdr/CALA9700137), Feb 3, 1997: ANGLE. CORRODED. INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 947 TO 970, ON RT SIDE. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED, A REPAIR SECTION AND SPLICES WER
- [SDR CALA9700136](https://openairdocs.org/sdr/CALA9700136), Feb 3, 1997: FLOORBEAM. CRACKED. INSPECTION FOUND A 2 INCH CRACK ON UPPER FLANGE OF FLOORBEAM AT BS 667, BL 0. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5710-01779.
- [SDR CALA9700135](https://openairdocs.org/sdr/CALA9700135), Feb 3, 1997: FLOORBEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LOWER RADIUS OF FLOORBEAM AT STA 685, BL 0. A 1 INCH CRACK WAS FOUND IN TRANSVERSE BEAM AT STA 675, BL 0. THE FLOORBEAM WAS R
- [SDR CALA9700134](https://openairdocs.org/sdr/CALA9700134), Jan 30, 1997: BULKHEAD. CRACKED. INSPECTION FOUND AN 8 INCH CRACK IN BULKHEAD AT STA 178, RBL 29 AND A 10 INCH CRACK WAS FOUND IN BULKHEAD AT STA 178, LBL 29. THE CRACKED AREAS WERE CUT OUT, FI
- [SDR CALA9700133](https://openairdocs.org/sdr/CALA9700133), Jan 30, 1997: STRINGER. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN STRINGER AT RT WING FS 465 LEADING EDGE SLAT WELL. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTALLED
- [SDR CAL960447](https://openairdocs.org/sdr/CAL960447), Apr 5, 1996: FLOORBEAM. CRACKED. GSO - INSPECTION FOUND A .50 INCH CRACK AND CORROSION ON COCKPIT AFT FLOORBEAM AT STA 459. THE CORRODED AREAS WERE REMOVED. NEW ANGLES WERE FABRICATED AND INSTA
- [SDR CAL960449](https://openairdocs.org/sdr/CAL960449), Mar 30, 1996: FRAME. CRACKED. GSO - INSPECTION FOUND A 3 INCH CRACK IN LOWER FORWARD FRAME OF C-1 DOOR. THE FRAME SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)
- [SDR CAL960448](https://openairdocs.org/sdr/CAL960448), Mar 28, 1996: SKIN. CORRODED. GSO - INSPECTION FOUND THE NR 2 ENGINE FORWARD OUTBOARD COWL OUTER SKIN CORRODED AROUND ENGINE RADIUS WARNING PLACARD. THE CORRODED SECTION OF SKIN WAS CUT OUT.
- [SDR CALA950524](https://openairdocs.org/sdr/CALA950524), Jun 25, 1995: LINE. CHAFED. DFW - FLT 1648 - LOSS OF A-SYSTEM HYD QUANTITY. REQUIRED BRAKE REPLACEMENT TO REMOVE FROM RUNWAY DUE TO OVERTEMP ON LANDING. FOUND LINE ON NR 2 ENGINE DRIVEN PU
- [SDR CAL950484](https://openairdocs.org/sdr/CAL950484), Jun 13, 1995: CARGO DOOR. CRACKED. CLE - FLT 1639 - MAINTENANCE FOUND TWO CRACKS IN THE FORWARD CARGO DOOR AT THE SEAL RETAINER WHILE UNDERGOING A DECAY CHECK FOR PRESSURIZATION PROBLEMS. THE CRA
- [SDR CAL950339](https://openairdocs.org/sdr/CAL950339), Apr 28, 1995: FAN BLADE. BENT. FLT NR 1464 - IAH - ON MAINTENANCE WALKAROUND, FOUND NR 2 ENGINE FAN BLADE BENT OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE ENGINE C1 DISK FAN ASSY. CHANGE COM
- [SDR CAL950273](https://openairdocs.org/sdr/CAL950273), Apr 15, 1995: HYD MODULE. FAILED. GSO - FLT 1735 - THE A-HYDRAULIC SYSTEM PRESSURE DROPPED TO ZERO DURING CLIMB OUT OF GSO. CHECK LIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED
- [SDR CAL950111](https://openairdocs.org/sdr/CAL950111), Feb 1, 1995: SKIN. CRACKED. GSO - INSPECTION FOUND SKIN CRACKED AT SEVERAL FASTENER HOLES ON RT SIDE OF FUSELAGE BETWEEN BS 188 AND BS 251.6. ALL CRACKS WERE APPROXIMATELY 1 INCH LONG. THE
- [SDR CAL950110](https://openairdocs.org/sdr/CAL950110), Feb 1, 1995: SKIN. CRACKED. GSO - INSPECTION FOUND SKIN CRACKED AT SEVERAL FASTENER HOLES BETWEEN BS 188 AND BS 251.6 ON THE LT SIDE OF FUSELAGE. ALL CRACKS WERE APPROXIMTELY .25 INCH LONG
- [SDR CAL950109](https://openairdocs.org/sdr/CAL950109), Feb 1, 1995: SKIN. CORRODED. GSO - INSPECTION FOUND CORROSION ON RT EXTERNAL SKIN AND DOUBLER AT STA 727 BETWEEN STR 17R AND STR 18R. THE CORROSION WAS REMOVED AND A DOUBLER IN INSTALLED IA
- [SDR CAL950108](https://openairdocs.org/sdr/CAL950108), Feb 1, 1995: SKIN. CRACKED. GSO - INSPECTION FOUND A .50 INCH CRACK IN THE LT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN AT STA 66. THE CRACK WAS STOP DRILLED AND REPAIR DOUBLERS WERE 
- [SDR CAL950107](https://openairdocs.org/sdr/CAL950107), Feb 1, 1995: INTERCOSTAL. CRACKED. GSO - INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL BEHIND AFT FORMER IN E AND E BAY. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INST
- [SDR CAL950106](https://openairdocs.org/sdr/CAL950106), Feb 1, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A 1 INCH CRACK IN BELT FRAME AT BS 500 BETWEEN STR 21L AND STR 20L. THE CRACKED BELT FRAME WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM
- [SDR CAL950100](https://openairdocs.org/sdr/CAL950100), Feb 1, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A .50 INCH CRACK IN BELT FRAME AT BS 480 BETWEEN STR 21L AND STR 20L. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-30
- [SDR CAL950099](https://openairdocs.org/sdr/CAL950099), Feb 1, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A 1 INCH CRACK IN BELT FRAME AT BS 500A BETWEEN STR 21L AND STR 20L. THE CRACKED FRAME WAS CUT OUT IAW BOEING DRAWING 65C225113 AND A REP
- [SDR CAL950098](https://openairdocs.org/sdr/CAL950098), Feb 1, 1995: BELT FRAME. CRACKED. GSO - INSPECTION FOUND A 2 INCH CRACK IN BELT FRAME AT BS 420, STR 22L. THE CRACK WAS REPAIRED IAW BOEING DRAWING 65C25113. (X)
- [SDR CAL950097](https://openairdocs.org/sdr/CAL950097), Feb 1, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A .50 INCH CRACK IN STA 578 MAIN CABIN FRAME AT STR 16 - STR 17L. THE FRAME WAS REPAIRED IAW SRM 51-40-3 AND SRM 51-30-2. (X)
- [SDR CAL950096](https://openairdocs.org/sdr/CAL950096), Feb 1, 1995: STRINGER. CRACKED. GSO - INSPECTION FOUND A 1 INCH CRACK IN STR 5R AT STA 685. THE CRACK WAS STOP DRILLED AND A REPAIR CHANNEL WAS INSTALLED IAW SRM 53-10-3. (X)
- [SDR CAL950095](https://openairdocs.org/sdr/CAL950095), Feb 1, 1995: CHORD. CRACKED. GSO - INSPECTION FOUND A .50 INCH CRACK IN RT STA 727 OUTBOARD CHORD AT STR 18A. THE CRACKED CHORD WAS REMOVED AND A NEW CHORD WAS FABRICATED AND INSTALLED IAW 
- [SDR CAL950094](https://openairdocs.org/sdr/CAL950094), Feb 1, 1995: FLOOR PANEL. CORRODED. GSO - INSPECTION FOUND THE NR 6 FLOOR PANEL SUPPORT CORRODED AT STA 312. THE PANEL SUPPORT WAS REPAIRED IAW SRM 51-30-2. (X)
- [SDR CAL950093](https://openairdocs.org/sdr/CAL950093), Feb 1, 1995: FLOORBEAM. CRACKED. GSO - INSPECTION FOUND A 1 INCH CRACK IN STA 639 LT SIDE FLOORBEAM WEB CABLE CUTOUT. THE FLOORBEAM WEB WAS REPAIRED IAW BOEING DRAWING 65C25211. (X)

All 52: https://openairdocs.org/deregistered/N14233-1999-06-24/reports.md

## 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 19980813038079I](https://openairdocs.org/incident/19980813038079I), Aug 13, 1998: Boeing 737217 (N14233), Buffalo, NY. (-5)On Thursday, August 13, 1998, at approximately 2131 local, a Continental express B-737, N14233, flight 1160, enroute from toronto, experienced an…

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