# N16232: Boeing 737-217, registration cancelled 1999-06-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 15, 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: 19886 - Type of aircraft: Fixed wing multi engine - Certificate issued: August 26, 1998 - Last registry action: August 27, 1998 - Mode S code: A0FBF8 - 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/N16232 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16232 - Page: https://openairdocs.org/deregistered/N16232-1999-06-15 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 737-217: https://openairdocs.org/model/boeing-737-217.md ## Service difficulty reports (26) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9701782](https://openairdocs.org/sdr/CALA9701782), Dec 19, 1997: CYLINDER. LEAKING. THE NR 1 ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED AND HYDRAULIC QUANTITY DROPPED TO ZERO ON APPROACH TO EWR. ALL ABNORMAL AND EMERGENCY CHECKLISTS WERE A - [SDR CALA9700978](https://openairdocs.org/sdr/CALA9700978), Jun 28, 1997: LIGHT. INOPERATIVE. INSPECTION FOUND FIRST CLASS EMERGENCY TRACK LIGHT AT L-1 DOOR INOPERATIVE. MAINTENANCE REPLACED SOCKET AND DAMAGED WIRE, OPERATIONAL CHECK WAS GOOD. - [SDR CALA9700584](https://openairdocs.org/sdr/CALA9700584), Apr 19, 1997: TR UNLOCK LIGHT. ILLUMINATED. ONTAKEOFF ROLL, CREW RECEIVED NR 1 THRUST REVERSER UNLOCK LIGHT ILLUMINATE. REJECTED TAKEOFF AT 100 KNOTS. RETURNED TO GATE WHERE MAINTENANCE PERFORMED INSPECTI - [SDR CALA9601628](https://openairdocs.org/sdr/CALA9601628), Nov 14, 1996: SOLENOID. INOPERATIVE. THE GEAR LATCH WOULD NOT RELEASE AFTER TAKEOFF. THE GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. CIRCUIT BREAKERS WERE PULLED AND RESET IAW QRH PROCEDURES, BU - [SDR CALA9601188](https://openairdocs.org/sdr/CALA9601188), Aug 19, 1996: HYD PUMP. LEAKING. THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO FOLLOWED BY LOSS OF PRESSURE ON NR 2 ENGINE WHILE EN ROUTE. AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT - [SDR CALA9600906](https://openairdocs.org/sdr/CALA9600906), Jun 27, 1996: PCU. INOPERATIVE. THE AIRCRAFT HAD AN UNCOMMANDED ROLL TO THE RIGHT ON TAKEOFF. FIFTEEN TO TWENTY DEGREES OF LEFT AILERON WAS REQUIRED TO MAINTAIN LEVEL FLIGHT. ALL OTHER INDICAT - [SDR CALA9600798](https://openairdocs.org/sdr/CALA9600798), May 8, 1996: STRAP. CORRODED. INSPECTION FOUND STRAP AT C-1 DOOR THRESHOLD CORRODED, STA 420 TO 500. A NEW STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. - [SDR CALA9600801](https://openairdocs.org/sdr/CALA9600801), May 6, 1996: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN UPPER SKIN OF RT WING INBOARD AFT FLAP. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLE - [SDR CALA9600811](https://openairdocs.org/sdr/CALA9600811), May 4, 1996: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 294, RBL 40 TO 55. THE CORRODED SECTION OF CHORD WAS CUT OUT, A REPLACEMENT CHORD AND L-ANGLE DOUBLERS WE - [SDR CALA9600810](https://openairdocs.org/sdr/CALA9600810), May 3, 1996: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 328. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS FABRICATED AND INSTALLED IAW SRM 53-10-9 AND MM 51-20. - [SDR CALA9600812](https://openairdocs.org/sdr/CALA9600812), May 1, 1996: FRAME. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN FORWARD CARGO FRAME AT STA 480, S21L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-6. REPAIR PARTS WERE FABRICATED AND INSTALLED - [SDR CALA9600803](https://openairdocs.org/sdr/CALA9600803), May 1, 1996: BRACKET. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN LT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED - [SDR CALA9600802](https://openairdocs.org/sdr/CALA9600802), May 1, 1996: BRACKET. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN RT ANGLE BRACKET AT REAR SPAR OF VERTICAL STABILIZER. THE CRACK WAS STOP DRILLED AND A NEW ANGLE WAS FABRICATED AND INSTALLED - [SDR CALA9600797](https://openairdocs.org/sdr/CALA9600797), May 1, 1996: CHANNEL. CRACKED. THE STRINGER TO FLOOR BEAM ATTACHMENT U-CHANNEL HAD TWO 1 INCH CRACKS AT STA 500A, STRINGER 28R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, FIGURE 7 - [SDR CALA9600796](https://openairdocs.org/sdr/CALA9600796), May 1, 1996: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO PIT INTERCOSTAL AT STA 500, STRINGER 27L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND - [SDR CALA9600795](https://openairdocs.org/sdr/CALA9600795), May 1, 1996: FRAME. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STA 480, BL 0. THE CRACK WAS REMOVED AND A DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-4. - [SDR CALA9600799](https://openairdocs.org/sdr/CALA9600799), Apr 30, 1996: BLKHD STIFFENER. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF VERTICAL STIFFENER AT STA 727 BULKHEAD. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2 AND 51-21. - [SDR CALA9600809](https://openairdocs.org/sdr/CALA9600809), Apr 29, 1996: SKIN. DENTED. INSPECTION FOUND SEVERAL DENTS IN FORWARD CARGO DOOR SKIN. THE DENTED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-00-3, 51-30-2 AND 51-1 - [SDR CALA9600808](https://openairdocs.org/sdr/CALA9600808), Apr 29, 1996: SKIN. CREASED. INSPECTION FOUND A 3 INCH CREASE IN FUSELAGE SKIN AT STA 1120, BL 0. THE CREASED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. - [SDR CALA9600800](https://openairdocs.org/sdr/CALA9600800), Apr 29, 1996: AUX TRACK. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN MID AUXILIARY TRACK OF RT WING ABOVE NR 6 SLAT. A REPAIR WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA9600804](https://openairdocs.org/sdr/CALA9600804), Apr 27, 1996: SLIDE. INOPERATIVE. THE L-1 DOOR EVACUATION SLIDE FAILED DEPLOYMENT TEST. THE COVER LANYARD WOULD NOT RELEASE AND THE SLIDE ONLY PARTIALLY INFLATED. THE SLIDE WAS REMOVED AND REPLA - [SDR CALA9600807](https://openairdocs.org/sdr/CALA9600807), Apr 26, 1996: SIGN. INOPERATIVE. THE SELF ILLUMINATING EXIT SIGN IN AFT CABIN FAILED ILLUMINOSITY CHECK. THE EXIT SIGN WAS REMOVED AND REPLACED. - [SDR CALA9600805](https://openairdocs.org/sdr/CALA9600805), Apr 26, 1996: WIRE. DAMAGED. A SECTION OF FORWARD CABIN EMERGENCY PATH LIGHTS WERE FOUND INOPERATIVE. THE WIRING AT FORWARD TRACK SECTION WAS REPAIRED IAW MM 33-50-0. - [SDR CAL950860](https://openairdocs.org/sdr/CAL950860), Sep 22, 1995: CHORD. CRACKED. GSO - INSPECTION FOUND A 2 INCH CRACK FROM FORWARD HOLE TO AFT HOLE OF RT CHORD AT STA 727, STR 18A. A REPAIR WAS ACCOMPLISHED IAW ECRA 5310-03165 AND EA 5310-0 - [SDR CAL950235](https://openairdocs.org/sdr/CAL950235), Mar 27, 1995: HYD MODULE. INOPERATIVE. MSY - FLT 1275 - THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF WITH THE GEAR HANDLE IN THE UP POSITION. THE GEAR WAS CYCLED AND RED LIGHT EXTIN - [SDR CAL950120](https://openairdocs.org/sdr/CAL950120), Feb 13, 1995: HYD VALVE. LEAKING. BWI - FLT 1555 - THE AIRCRAFT LOST THE 'A' SYSTEM HYDRAULIC QUANTITY SHORTLY AFTER TAKEOFF FROM BWI. THE AIRCRAFT WAS RETURNED TO BWI WHERE IT LANDED WITHOUT IN ## 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 19960825033429I](https://openairdocs.org/incident/19960825033429I), Aug 25, 1996: Boeing 737217 (N16232), Richmond, VA. Narrative: on 08-25-96, at 17:33 local, the Richmond tower received a call from Continental operations on the field. Continental operations reported that the… - [Incident 19940430024219I](https://openairdocs.org/incident/19940430024219I), Apr 30, 1994: Boeing 737217 (N16232), Milwaukee, WI. Smoke in cabin. Diverted. Landed Milwaukee. Maintenance unable to duplicate. ## Other aircraft with N16232 - [Cancelled 1974-08-16](https://openairdocs.org/deregistered/N16232-1974-08-16): Cessna 150L, S/N 15073560. Exported to Canada. Owner: [Pearson Aircraft Inc](https://openairdocs.org/faa-owner/PEARSON%20AIRCRAFT%20INC), [Port Angeles, WA](https://openairdocs.org/faa-place/WA/Port%20Angeles) --- 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.