# N10236: Boeing 737-222, registration cancelled 1999-06-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 15, 1999 - Status when cancelled: Valid registration - Airframe: [Boeing 737-222](https://openairdocs.org/model/boeing-737-222) (registry code 1384473) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 19937 - Type of aircraft: Fixed wing multi engine - Certificate issued: January 13, 1999 - Last registry action: January 20, 1999 - Mode S code: A00F02 - Owner when cancelled: [Rfc 737 23 Inc](https://openairdocs.org/faa-owner/RFC%20737%2023%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/N10236 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=10236 - Page: https://openairdocs.org/deregistered/N10236-1999-06-15 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 737-222: https://openairdocs.org/model/boeing-737-222.md ## Service difficulty reports (36) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9801537](https://openairdocs.org/sdr/CALA9801537), Aug 26, 1998: SOLENOID. INOPERATIVE. THE LANDING GEAR HANDLE WOULD NOT MOVE PAST OFF POSITION TO UP UNLESS OVERRIDE TRIGGER WAS PULLED AFTER TAKEOFF. MAINTENANCE FOUND THE LANDING GEAR CONTROL LEVE - [SDR CALA9800690](https://openairdocs.org/sdr/CALA9800690), Apr 23, 1998: LINE. LEAKING. THE B SYSTEM HYDRAULIC QUANTITY DECREASED TO 1.8 GALLONS IN FLIGHT AND WAS ACCOMPANIED BY ILLUMINATION OF THE B SYSTEM LOW QUANTITY LIGHT. THE ABNORMAL CHECKLIS - [SDR CALA9800390](https://openairdocs.org/sdr/CALA9800390), Mar 5, 1998: SIGN. SHORTED. THE CREW REPORTED SMOKE APPEARED MOMENTARILY IN CABIN AT PUSH TIME. MAINTENANCE FOUND THE NO SMOKING FASTEN SEAT BELT SYSTEM INOPERATIVE WITH THE ROW 6 ABC OVER - [SDR CALA9701651](https://openairdocs.org/sdr/CALA9701651), Nov 19, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, LBL 1.5 AND LBL 9. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03623. - [SDR CALA9701650](https://openairdocs.org/sdr/CALA9701650), Nov 19, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER CAP CORRODED AT STA 312, RT OUTBOARD END. THE CORRODED SECTION WAS REMOVED IAW SRM 51-30-2, REPAIR FILLER AND ANGLES WERE FABRI - [SDR CALA9701649](https://openairdocs.org/sdr/CALA9701649), Nov 19, 1997: WEB. CORRODED. INSPECTION FOUND WEB CORRODED AT BS 330 TO 340, RT CUSP. THE CORROSION WAS REMOVED IAW SRM 51-10-6, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40- - [SDR CALA9701648](https://openairdocs.org/sdr/CALA9701648), Nov 19, 1997: ANGLE. CORRODED. INSPECTION FOUND CORROSION IN ANGLE AT BS 797, S26L. THE CORRODED AREA WAS CUT OUT IAW SRM 53-10-3, FIGURE NR 1, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IA - [SDR CALA9701647](https://openairdocs.org/sdr/CALA9701647), Nov 19, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER T-CAP CORRODED AT STA 344 FROM LBL 24 TO RBL 24. THE CORRODED FLOORBEAM CAP WAS REMOVED, A REPLACEMENT CAP AND SPLICES WERE FAB - [SDR CALA9701646](https://openairdocs.org/sdr/CALA9701646), Nov 19, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 328 TO 344, LBL 10. THE FLOOR SUPPORT WAS REMOVED IAW SRM 53-10-2. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW - [SDR CALA9701645](https://openairdocs.org/sdr/CALA9701645), Nov 19, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 294.5 TO 312, RBL 10. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10- - [SDR CALA9701644](https://openairdocs.org/sdr/CALA9701644), Nov 19, 1997: FRAME. CORRODED. INSPECTION FOUND CABIN FLOOR FRAME CORRODED AT STA 987 FROM BL 55L TO BL 55R. THE CORRODED UPPER CAP WAS REMOVED IAW SRM 51-30-2. A NEW UPPER CAP WAS FABRICATED - [SDR CALA9701643](https://openairdocs.org/sdr/CALA9701643), Nov 19, 1997: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM UPPER CAP AND WEB CORRODED INSIDE E AND E COMPARTMENT AT BS 328. THE CORRODED SECTION OF BEAM CAP WAS REMOVED AND A NEW SECTION AND S - [SDR CALA9701642](https://openairdocs.org/sdr/CALA9701642), Nov 19, 1997: SUPPORT. CORRODED. INSPECTION FOUND FLOOR SUPPORT UPPER PLATE CORRODED AT STA 328 TO 344, RBL 10. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW - [SDR CALA9701376](https://openairdocs.org/sdr/CALA9701376), Sep 17, 1997: HYD LINE. CRACKED. THE AIRCRAFT LOST A-HYDRAULIC SYSTEM WHILE EN ROUTE. THE HYDRAULIC LOSS CHECKLIST WAS COMPLETED AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOU - [SDR CALA9601488](https://openairdocs.org/sdr/CALA9601488), Oct 12, 1996: STRINGER. CRACKED. RIGHT A/C BAY OUTBOARD SIDE APPROX 1.5 LONG CRACK EXTENDING UNDER STIFFENER AT FUSELAGE STATION. REMOVED STIFFENER, STOP DRILLED CRACK, AND INSTALLED PER SRM 51 - [SDR CALA9601487](https://openairdocs.org/sdr/CALA9601487), Oct 12, 1996: SKIN. CORRODED. AFT FUSELAGE STATION 877 TO 857 AT STATION 24R LAP JOINT SWOLLEN BETWEEN FASTENER HEADS. REMOVED FASTENERS AT LAP JOINT AND CORROSION PER SRM 51-10-2 AND 51-10- - [SDR CALA9601486](https://openairdocs.org/sdr/CALA9601486), Oct 12, 1996: BATTERY PACK. DISCHARGED. L2 DOOR MOUNTED ESCAPE SLIDE LIGHT INOP. REPLACED BATTERY PACK PER MM 33-51-63. - [SDR CALA9601485](https://openairdocs.org/sdr/CALA9601485), Oct 3, 1996: SKIN. BULGED. EXTERIOR SKIN ON LEFT SIDE NOSE WHEEL WELL EDGE HAS BULGES AND RIVETS PULLING THROUGH FROM STATION 235.8 TO 251.8. CUT OUT DAMAGED AREA, FABRICATED FILLER AND D - [SDR CALA9601484](https://openairdocs.org/sdr/CALA9601484), Oct 3, 1996: SKIN. OIL CAN. FUSELAGE SKIN OIL CAN AT BS 390L AND STR 17L. TRIMMED OUT DAMAGED AREA PER SRM 53-30-3, FABRICATED DOUBLER PER SRM 53-30-3 AND 51-10-2, INSTALLED DOUBLER PER SR - [SDR CALA9601483](https://openairdocs.org/sdr/CALA9601483), Oct 3, 1996: BLKHD WEB. CRACKED. FORWARD FACE OF FORWARD PRESSURE BULKHEAD STATION 178 CRACKED ON LEFT SIDE ABOVE WL 208 APPROX 8. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER, IN - [SDR CALA9601482](https://openairdocs.org/sdr/CALA9601482), Oct 3, 1996: BULKHEAD. CRACKED. FORWARD FACE OF FORWARD PRESSURE BULKHEAD STATION 178 CRACKED ON RIGHT SIDE ABOVE WL STA 208, APPROX 8. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILL - [SDR CALA9601481](https://openairdocs.org/sdr/CALA9601481), Oct 3, 1996: SKIN. CRACKED. FUSELAGE SKIN CRACKED IN 2 PLACES ON LEFT SIDE BETWEEN STA 727A AND 727B AT STRINGER 18 APPROX 3 EACH. CUT OUT DAMAGED AREA, FABRICATED FILLER AND EXTERNAL DOUB - [SDR CAL950970](https://openairdocs.org/sdr/CAL950970), Oct 24, 1995: BATTERY PACK. DISCHARGED. GSO - EXIT LIGHT INOP. REPLACED RIGHT EXTERNAL EMERGENCY EXIT LIGHT BATTERY PACK AND BATTERY. (M) - [SDR CAL950969](https://openairdocs.org/sdr/CAL950969), Oct 24, 1995: BATTERY PACK. DISCHARGED. GSO - AIRCRAFT IN 1/2 D-CHECK, FOUND LEFT EXTERNAL EMERGENCY LIGHT INOP. REPLACED LEFT EXTERNAL EMERGENCY EXIT LIGHT BATTERY PACK AND BATTERY. (M) - [SDR CAL950968](https://openairdocs.org/sdr/CAL950968), Oct 24, 1995: BATTERY PACK. DISCHARGED. GSO - AIRCRAFT IN 1/2 D-CHECK, FOUND BATTERY PACK INOP. REPLACED BATTERY PACK FOR L-1 SLIDE. (M) - [SDR CAL950967](https://openairdocs.org/sdr/CAL950967), Oct 24, 1995: FRAME. CRACKED. GSO - AIRCRAFT IN D-CHECK, FOUND CRACK IN FRAME SEGMENT APPROXIMATLY .75 INCH AT BS 500A BETWEEN S20L, S21L, AND ABOVE S23L, REMOVED AND REPLACED. (M0 - [SDR CAL950966](https://openairdocs.org/sdr/CAL950966), Oct 24, 1995: FRAME. CRACKED. GSO - AIRCRAFT IN 1/2 D-CHECK, FOUND CRACK APPROXIMATELY .75 INCH IN FRAME SEGMENT AT BS 400 BETWEEN S21L AND S22L, REMOVED AND REPLACED. (M) - [SDR CAL950965](https://openairdocs.org/sdr/CAL950965), Oct 24, 1995: FRAME. CRACKED. GSO - AIRCRAFT IN 1/2 D-CHECK, FOUND CRACK IN FRAME SEGMENT APPROXIMATELY .75 INCH AT BS 500A BETWEEN S20R AND S21R, REMOVED AND REPLACED. (M) - [SDR CAL950964](https://openairdocs.org/sdr/CAL950964), Oct 24, 1995: FRAME. CRACKED. GSO - AIRCRAFT IN ONE-HALF D-CHECK. DURING INSPECTION, FOUND CRACK APPROXIMATELY .75 INCH AT BS 420 BETWEEN S21L, S22L, S23L. STOP DRILLED CRACK AND INSTALLED D - [SDR CAL950963](https://openairdocs.org/sdr/CAL950963), Oct 24, 1995: FRAME. CRACKED. GSO - AIRCRAFT IN ONE-HALF D-CHECK DURING INSPECTION, FOUND CRACK FRAME SEGMENT APPROXIMATELY .05 INCH AT BS 480 BETWEEN S20L AND S21L. REMOVED AND REPLACED. (X - [SDR CAL950962](https://openairdocs.org/sdr/CAL950962), Oct 24, 1995: FRAME. CRACKED. GSO - AIRCRAFT IN 1/2 D-CHECK DURING INSPECTION, FOUND CRACK IN FRAME SEGMENT AT BS 460 APPROXIMATELY .75 INCH, BETWEEN S20L AND S21L. REMOVED AND REPAIRED. (X) - [SDR CAL950960](https://openairdocs.org/sdr/CAL950960), Oct 24, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND CRACKS IN FRAME AT BS 500B BETWEEN STR 19L AND STR 20L, AND BETWEEN STR 25L AND STR 27L. THE CRACK AT EACH LOCATION WAS APPROXIMATELY .33 - [SDR CAL950959](https://openairdocs.org/sdr/CAL950959), Oct 24, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND CRACKS IN FRAME AT BS 500 BETWEEN STR 21L AND STR 22L AND STR 22L AND STR 23L. THE CRACK AT EACH LOCATION WAS APPROXIMATELY .75 INCH LONG - [SDR CAL950958](https://openairdocs.org/sdr/CAL950958), Oct 24, 1995: FRAME. CRACKED. GSO - INSPECTION FOUND A CRACK IN FRAME AT BS 420 BETWEEN S22R AND S21R AND BETWEEN S21R AND S20R. THE CRACK AT EACH LOCATION WAS APPROXIMATELY .75 INCH LONG. T - [SDR CAL950956](https://openairdocs.org/sdr/CAL950956), Oct 24, 1995: SKIN. CRACKED. GSO - INSPECTION FOUND A .50 INCH CRACK AT FORWARD LOWER CORNER OF AFT CARGO DOOR CUT-OUT, EXTERNAL SKIN. THE CRACKED AREA WAS REMOVED. A FILLER AND DOUBLER REP - [SDR CAL950527](https://openairdocs.org/sdr/CAL950527), Jun 28, 1995: HYD LINE. WORN. FLT NR 1728 - CLE - THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IND. BOTH THE RED AND GREEN LIGHTS REMAINED ON. WHEN THE GEAR HANDLE WAS PLACED D ## 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 19930601024099I](https://openairdocs.org/incident/19930601024099I), Jun 1, 1993: Boeing 737222 (N10236), Cleveland, OH. Autopilot felt heavy. B hydraulic light on. Returned. Found b system hydraulic flight control module had failed. ## Other aircraft with N10236 - [Cancelled 2023-05-09](https://openairdocs.org/deregistered/N10236-2023-05-09): Cox Alvin G OSPREY II, S/N 289, built 2006. Owner: [Huffman Benjamin J](https://openairdocs.org/faa-owner/HUFFMAN%20BENJAMIN%20J), [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio) --- 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.