# N412CE: 1971 Boeing 737-205, registration cancelled 2013-07-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 29, 2013
- Status when cancelled: Sale reported, canceled
- Airframe: [Boeing 737-205](https://openairdocs.org/model/boeing-737-205) (registry code 1384456)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 20412
- Year built: 1971
- Type of aircraft: Fixed wing multi engine
- Last registry action: April 14, 2005
- Mode S code: A4DBC5
- Location: [Weston, FL](https://openairdocs.org/faa-place/FL/Weston)
- Owner type: Individual
- Owner's area on the map: 26.1105° N, 80.3740° W: Placed by OpenAirDocs at the center of ZIP code 33326, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N412CE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=412CE
- Page: https://openairdocs.org/deregistered/N412CE-2013-07-29

From the FAA registry file of October 29, 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 737-205: https://openairdocs.org/model/boeing-737-205.md

## Service difficulty reports (92, newest 50)

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

- [SDR P2EA00225](https://openairdocs.org/sdr/P2EA00225), Jul 10, 2000: FLOORBEAM. CRACKED. SJO - DURING C-CHECK, LEFT AIR CONDITIONING BAY, WING CENTER SECTIN RBL 40.875 BETWEEN BS 573 AND BS 576 LOWER BEAM WEB WITH A CRACK, 2.5 INCHES LONG BY .001 IN
- [SDR P2EA00224](https://openairdocs.org/sdr/P2EA00224), Jul 10, 2000: FLOORBEAM. CORRODED. SJO - DURING C-CHECK, RIGHT AIR CONDITIONING BAY, WING CENTER SECTION RBL 40.875 BETWEEN BS 571 AND BS 584 LOWER BEAM WEB WITH A CRACK 2 INCHES LONG BY .002 INC
- [SDR P2EA00223](https://openairdocs.org/sdr/P2EA00223), Jul 10, 2000: FRAME. CRACKED. SJO - DURING C-CHECK, FUSELAGE FRAME CRACKED AT BS 794, BETWEEN STRINGER 18RT AND STRINGER 27 RT, DEFECT SIZE 3 INCHES LONG BY .001 INCH WIDE. REPAIRED FUSELAGE
- [SDR P2EA00220](https://openairdocs.org/sdr/P2EA00220), Jul 10, 2000: FAIRING. DELAMINATED. SJO - DURING C-CHECK, ADF ANTENNA DELAMINATED ON LEFT WING TO BODY FAIRING, DEFECT SIZE 40 INCHES BY 29.750 INCHES. REPAIRED LEFT WING TO BODY SENSE ANTENNA PER
- [SDR P2EA00200](https://openairdocs.org/sdr/P2EA00200), Jun 11, 2000: MODULE. FAILED. FLT 305 - MCI - AIR RETURN, EMERGENCY DECLARED, LANDING UNEVENTFUL. ON CLIMB-OUT, STICK SHAKER WENT OUT AT 210 KNOTS ON FLAP RETRACTION, GOT WORSE, RETURNED TO 
- [SDR P2EA00116](https://openairdocs.org/sdr/P2EA00116), Apr 25, 2000: ACTUATOR. MALFUNCTIONED. MYR - FLT 406 - ON APPRAOCH TO MYR, RECEIVED UNCOMMANDED AFT STABAILIZER TRIM. PUT TRIM CUT OUT SWITCH TO OFF, BUT TRIM DID NOT STOP. GRABBED TRIM WHEEL AND TRI
- [SDR P2EA99307](https://openairdocs.org/sdr/P2EA99307), Oct 24, 1999: ACM. FAILED. MCI - FLT 584 - AFTER SHUT DOWN OF NR 1 ENGINE A BURNING ODOR WAS NOTICE FOLLOWED, A FEW SECONDS LATER, BY SMOKE IN THE COCKPIT AND FORWARD CABIN. REMOVED AND R
- [SDR P2EA99227](https://openairdocs.org/sdr/P2EA99227), Aug 28, 1999: MECHANISM. OUT OF ADJUST. PIT - FLT 422 - NO EMERGENCY DECLARED, LANDING NORMAL. STRONG VIBRATION NOTED IN MID CABIN WHEN FLAPS EXTENDED FOR LANDING. ADJUSTED LEFT TRAILING EDGE AFT FLAP
- [SDR P2EA99209](https://openairdocs.org/sdr/P2EA99209), May 25, 1999: STRINGER. CRACKED. SJO - DURING C-CHECK, STRINGER 17L WAS CRACKED FROM BS 727 TO BS 796. REPAIRED PER EO COO-3-53-334-99 DATED 5/28/99. (M)
- [SDR P2EA99200](https://openairdocs.org/sdr/P2EA99200), May 21, 1999: ANGLES. CRACKED. SJO - DURING C-CHECK, THE LOWER FUSELAGE, EXTERNAL SKIN DRAG ANGLES AT BS 560, STRINGER 24L WAS FOUND CRACKED. REPAIRED PER, SB 737-53-1031 SECTION III PART III
- [SDR P2EA99202](https://openairdocs.org/sdr/P2EA99202), May 20, 1999: DOOR. CRACKED. SJO - DURING C-CHECK, THE LEFT RAM AIR DOOR WAS FOUND CRACKED. REPAIRED PER EO COO-3-52-316-99. (M)
- [SDR P2EA99190](https://openairdocs.org/sdr/P2EA99190), May 17, 1999: BEAM. CRACKED. SJO - DURNG C-CHECK, THE FORWARD SERVICE DOOR (R1) INTERNAL BEAM NR 7 AFT SECTION IS CRACKED. REPAIRED PER SRM 51-10-03 FIGURE 1. (M)
- [SDR P2EA99192](https://openairdocs.org/sdr/P2EA99192), May 12, 1999: SKIN. DELAMINATED. SJO - DURING C-CHECK, THE NR 8 SPOILER WAS FOUND DELAMINATED. REPAIRED PER COOPESA EO NR COO-CMP-3-57-299-99 DATED MAY 18, 1999. (M)
- [SDR P2EA99191](https://openairdocs.org/sdr/P2EA99191), May 12, 1999: SKIN. DELAMINATION. SJO - DURING C-CHECK, THE NR 2 SPOILER, WAS FOUND DELAMINATED. REPAIRED PER COOPESA EO NR COO-CMP-3-57-300-99, DATED MAY 18, 1999. (M)
- [SDR P2EA99203](https://openairdocs.org/sdr/P2EA99203), May 10, 1999: CHORD. CRACKED. SJO - DURING C-CHECK, A CHORD WAS FOUND CRACKED AT BS 727, STRINGER 18A, LEFT OUTBOARD SIDE. REPAIRED PER SB 737-53-1088. (M)
- [SDR P2EA99207](https://openairdocs.org/sdr/P2EA99207), May 8, 1999: FRAME. CRACKED. SJO - DURING C-CHECK, R1 DOOR FORWARD FRAME LOWER REINFORCEMENT WAS CRACKED. REPAIRED PER SRM 51-10-01. (M)
- [SDR P2EA99206](https://openairdocs.org/sdr/P2EA99206), May 8, 1999: HINGE. CRACKED. SJO - DURING C-CHECK, LEFT WING NR 1 SPOILER CENTER FITTING WAS CRACKED. FABRICATED FITTING PER EO COO-3-57-301-99. REMOVED AND REPLACED FITTING PER SRM 51-10-0
- [SDR P2EA99205](https://openairdocs.org/sdr/P2EA99205), May 8, 1999: BEAM. CRACKED. SJO - DURING C-CHECK, R1 DOOR BEAM NR 6 BETWEEN AFT FRAME AND AFT INTERCOSTAL WAS CRACKED. REPAIRED PER SRM 51-40-03 FIG 1. (M)
- [SDR P2EA99204](https://openairdocs.org/sdr/P2EA99204), May 8, 1999: FRAME. CRACKED. SJO - DURING C-CHECK, R1 DOOR, AFT FRAME LOWER END WAS CRACKED. REMOVED AND REPLACED FRAME PER SRM 51-10-01. (M)
- [SDR P2EA99201](https://openairdocs.org/sdr/P2EA99201), May 8, 1999: FRAME. CRACKED. SJO - DURING C-CHECK, R1 DOOR WAS FOUND CRACKED AT FORWARD FRAME LOWER SECTION. REMOVED AND REPLACED FRAME PER SRM 51-10-01. (M)
- [SDR P2EA99196](https://openairdocs.org/sdr/P2EA99196), May 8, 1999: BEAM. CRACKED. SJO - DURING C-CHECK, R1 DOOR, AFT FRAME, LOWER BEAM REINFORCEMENT WAS CRACKED. REPAIRED PER SRM 51-10-01 PAGE 5 AND 51-30-02. (M)
- [SDR P2EA99194](https://openairdocs.org/sdr/P2EA99194), May 8, 1999: SKIN. DAMAGED. SJO - DURNIG C-CHECK, THE LOWER AFT CORNER OF THE FORWARD CARGO COMPARTMENT DOOR CUT OUT WAS FOUND WITH MISSING MATERIAL. REPAIRED DOOR CUT OUT SKIN AND BEARSTR
- [SDR P2EA99189](https://openairdocs.org/sdr/P2EA99189), May 8, 1999: SKIN. CRACKED. SJO - DURING C-CHECK, A CRACK WAS FOUND AT THE EXTERNAL FUSELAGE NR 3 WINDOW CUTOUT. REPAIRED PER S/B 737-53-1115 DATED JAN 2, 1988, SECTION II FIG 3. (M)
- [SDR P2EA99187](https://openairdocs.org/sdr/P2EA99187), May 8, 1999: SKIN. CRACKED. SJO - DURING C-CHECK, A CRACK WAS FOUND ON THE R1 DOOR, EXTERNAL SKIN, NEAR THE LOWER HINGE, LENGTH .5 INCH. REPAIRED PER SRM 52-00-3 FIG 6. (M)
- [SDR P2EA99198](https://openairdocs.org/sdr/P2EA99198), May 7, 1999: BEAM. CRACKED. SJO - DURING C-CHECK, LEFT WHEEL WELL SHEAR BEAM BS 668, LBL 65, WL 194 WAS FOUND CRACKED. REPAIRED PER BOEING S/B 737-53-1066 REV 3 DATED 02/25/93, SECTION III
- [SDR P2EA99197](https://openairdocs.org/sdr/P2EA99197), May 7, 1999: STRINGER. CRACKED. SJO - DURING C-CHECK, SKIN AT BS 727 'A' BETWEEN STRINGER 14R AND 16R WAS FOUND CRACKED IN TWO PLACES. REPAIRED PER EO COO-SJO-99-0628RR DATED 05/20/99. (M)
- [SDR P2EA99193](https://openairdocs.org/sdr/P2EA99193), May 7, 1999: SKIN. CORRODED. SJO - DURING C-CHECK, THE FORWARD LAVATORY SERVICE PANEL CUT OUT SKIN WAS FOUND CORRODED. THE EXTERNAL FUSELAGE SERVICE PANEL DOUBLER WAS REPLACED PER SRM 51-10
- [SDR P2EA99188](https://openairdocs.org/sdr/P2EA99188), May 7, 1999: RIB. CRACKED. SJO - DURNG C-CHECK, WHILE INSPECTING THE LEFT WING TO BODY RIB CHORD AT BS 665, BBL 70.85, A CRACK WAS NOTED ON THE HORIZONTAL FLANGE. LENGTH 2 INCH. THAT CRAC
- [SDR P2EA99183](https://openairdocs.org/sdr/P2EA99183), May 2, 1999: SWITCH. FAILED. ATL - FLT 301 - NR 1 ENGINE START LIGHT ILLUMINATED ON TAKEOFF. REJECTED TAKEOFF. LIGHT WENT OUT WHEN ENGINES CAME TO IDLE. REPLACED NR 1 ENGINE START VALVE AND
- [SDR P2EA99208](https://openairdocs.org/sdr/P2EA99208), Apr 14, 1999: SKIN. CRACKED. SJO - DURING C-CHECK, LEFT EXTERNAL SKIN WAS CRACKED THREE PLACES FROM BS 727 TO 727 'A' AND STRINGER 14L TO 17L REPAIRED PER EO COO-3-53-314-99 DATED 5/22/99. 
- [SDR P2EA99132](https://openairdocs.org/sdr/P2EA99132), Apr 11, 1999: VALVE. LACK OF LUBE. PIT - FLT 707 - AS POWER WAS APPLIED FOR TAKEOFF, NR 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED. INDICATION WAS ACCOMPANIED BY A POPPING SOUND. CLEANED AND LUB
- [SDR P2EA99003](https://openairdocs.org/sdr/P2EA99003), Jan 13, 1999: SKIN. DAMAGED. MDW - FLT 374 - AIRCRAFT SKIN DAMAGED BY BAGGAGE TUG (CART) AT STATION 380 RT, WL 185. REPAIRED PER SRM 53-30-3, FIG 1. (M)
- [SDR P2EA98175](https://openairdocs.org/sdr/P2EA98175), Sep 29, 1998: DOOR WARNING. MALFUNCTIONED. MCI - FLT 301 - AIR RETURN, NO EMERGENCY DECLARED, LANDING UNEVENTFUL. AFT CARGO DOOR LIGHT CAME ON AFTER TAKEOFF, AIRCRAFT WAS NOT PRESSURIZING. RETURNED TO MC
- [SDR P2EA98156](https://openairdocs.org/sdr/P2EA98156), Aug 11, 1998: DOOR. CRACKED. MCI - RIGHT NLG DOOR LOWER FORWARD CORNER HAS DAMAGE. INSPECT RIGHT NLG DOOR FORWARD HINGE FITTING FOR CRACKS. REPLACED RIGHT NLG DOOR AND PERFORMED GEAR SWING 
- [SDR P2EA98105](https://openairdocs.org/sdr/P2EA98105), May 8, 1998: UPLOCK SENSOR. OUT OF ADJUST. MCI - FLT 917 - LEFT GEAR RED LIGHT ILLUMINATED. GEAR HANDLE PLACED DOWN, RED LIGHT OUT, GREEN LIGHT ON. ADJUSTED UPLOCK SENSOR PER MM 32-61-21 AND PERFORMED GE
- [SDR P2EA98102](https://openairdocs.org/sdr/P2EA98102), May 4, 1998: WIRE. DAMAGED. FLT 119 - ATL - NO EMERGENCY DECLARED, LANDING NORMAL. LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATES INTERMITTENTLY, IN UP AND OFF POSITIONS. FOUND BLUE WIRE TO UPLOC
- [SDR P2EA98096](https://openairdocs.org/sdr/P2EA98096), Apr 7, 1998: SKIN. CRACKED. SJO - EXTERIOR FUSELAGE SKIN CRACKED AT BS 830, STRINGER 14RT. REPAIRED FUSELAGE SKIN SECTION FROM BS 827 TO BS 847, BETWEEN STRINGER 11RT AND STRINGER 14 RT, P
- [SDR P2EA98070](https://openairdocs.org/sdr/P2EA98070), Apr 4, 1998: CHORD. CRACKED. SJO - Q-CHECK, RIGHT WING INBOARD TRAILING EDGE MID FLAP 'T' CHORD CRACKED AT WBL 87.73. REPAIRED MID FLAP TRAILING EDGE PER SRM 51-10-1 FIG PAGE 5. RIVETS REPL
- [SDR P2EA98076](https://openairdocs.org/sdr/P2EA98076), Apr 3, 1998: FRAME. CORRODED. SJO - Q-CHECK, WINDOW FRAME (24LT) WITH PROVISIONAL REPAIR AND CORRODED BEYOND LIMITS, BS 747. REPLACED WINDOW FRAME BETWEEN BS 747 AND BS 767 PER SRM 51-10-1 P
- [SDR P2EA98082](https://openairdocs.org/sdr/P2EA98082), Apr 1, 1998: SKIN. CRACKED. SJO - Q-CHECK, EXTERIOR FUSELAGE SKIN CRACKED AT BS 765 BETWEEN STRINGER 13 LT AND 14 LT. REPAIRED FUSELAGE SKIN SECTION FROM BS 727B PLUS 15 TO BS 767 BETWEEN 
- [SDR P2EA98075](https://openairdocs.org/sdr/P2EA98075), Apr 1, 1998: CHORD. CORRODED. Q-CHECK, NOSE LANDING GEAR WHEEL WELL TORQUE BOX RIGHT LOWER 'T' CHORD CORRODED BEYOND LIMITS AT BS 227.8. REPLACED T-CHORD BETWEEN BS 227.8 AND BS 294.5, WL 15
- [SDR P2EA98074](https://openairdocs.org/sdr/P2EA98074), Apr 1, 1998: CHORD. CORRODED. SJO - Q-CHECK, NOSE LANDING GEAR WHEEL WELL TORQUE BOX LOWER LEFT 'T' CHORD CORRODED BEYOND LIMITS AT BS 229.8. FABRICATED 'T' CHORD PER SRM 51-20-1, 51-10-1, 5
- [SDR P2EA98063](https://openairdocs.org/sdr/P2EA98063), Mar 31, 1998: FRAME. CRACKED. SJO - Q-CHECK, FORWARD CARGO DOOR FRAME CRACKED FROM BEAM NR 4 TO BEAM NR 5, INNER SKIN CRACKED BETWEEN BEAM NR 5 AND THE LOWER FRAME. FABRICATED AND REPAIRED N
- [SDR P2EA98095](https://openairdocs.org/sdr/P2EA98095), Mar 30, 1998: FLOORBEAM. CORRODED. Q-CHECK ITEM, FLOORBEAM CORRODED BEYOND LIMITS BETWEEN BS 967.5 AND 986.6, RBL 20 WL 208.1. REPAIRED FLOORBEAM BETWEEN BS 967.5 AND BS 986.6 RBL 20 PER BOEING F
- [SDR P2EA98069](https://openairdocs.org/sdr/P2EA98069), Mar 27, 1998: FITTING. CRACKED. SJO - Q-CHECK, FORWARD GALLEY DOOR (R1) FITTING CRACKED BS 290, STRINGER 8RH. REPLACED FITTING REPLACED PER SRM 51-10-1 FIG PAGE 6. RIVETS REPLACED PER SRM 51-3
- [SDR P2EA980667](https://openairdocs.org/sdr/P2EA980667), Mar 27, 1998: FITTING. CRACKED. SJO - Q-CHECK, FORWARD GALLEY DOOR, LOWER HINGE SUPPORT FITTING CRACKED AT BS 290, STRINGER 14RT. REPLACED FITTING PER SRM 51-10-1, PAGE 6. RIVETS REPLACED PER 
- [SDR P2EA98066](https://openairdocs.org/sdr/P2EA98066), Mar 27, 1998: SKIN. CRACKED. SJO - Q-CHECK, EXTERIOR FUSELAGE SKIN CRACKED BETWEEN BS 500 PLUS 9 INCHES TO BS 500A PLUS 2 INCHEC, STRINGER 12 RT AND STRINGER 14 RT. REPAIRED FUSELAGE SKIN S
- [SDR P2EA98065](https://openairdocs.org/sdr/P2EA98065), Mar 27, 1998: SKIN. CRACKED. SJO - Q-CHECK, EXTERIOR FUSELAGE SECTION CRACKED AT TWO POSITIONS BETWEEN BS 458 AND BS 491, STRINGER 10 RT TO STRINGER 14 RT. REPAIRED FUSELAGE SKIN SECTION PE
- [SDR P2EA98060](https://openairdocs.org/sdr/P2EA98060), Mar 26, 1998: FITTING. CRACKED. SJO - Q-CHECK, AFT GALLEY DOOR LOWER HINGE SUPPORT FITTING CRACKED, BS 954, STRINGER 14 RT. REPLACED HINGE SUPPORT FITTING PER SRM 51-10-1 PAGE 5. RIVETS REPLAC
- [SDR P2EA98071](https://openairdocs.org/sdr/P2EA98071), Mar 25, 1998: SKIN. CORRODED. SJO - Q-CHECK, UPPER FUSELAGE SKIN CORRODED BEYOND LIMITS AT BS 1104, STRINGER 5 LT AND STRINGER 6LT. REPAIRED FUSELAGE SKIN SECTION FROM BS 1098 TO BS 1111, BE

All 92: https://openairdocs.org/deregistered/N412CE-2013-07-29/reports.md

## FAA accident and incident reports (5)

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 20000610021789I](https://openairdocs.org/incident/20000610021789I), Jun 10, 2000: Boeing 737205 (N412CE), Kansas City, MO, Minor damage. (-23) During the climbout, stick shaker went off at 210 knots. On flap retraction, shaker continued with airspeed in limits. Aircraft returned to Kansas City…
- [Incident 20000422019569I](https://openairdocs.org/incident/20000422019569I), Apr 22, 2000: Boeing 737205 (N412CE), Kansas City, MO. (-23)On April 22, 2000, vanguard airlines, fligth 307, was enroute from mci to den. During climbout from mci the pilot reported that at 21,500 feet, cabin PSI…
- [Incident 19991013031069I](https://openairdocs.org/incident/19991013031069I), Oct 13, 1999: Boeing 737205 (N412CE), Buffalo, NY. (-23) On Wednesday, October 13, 1999, at 0738 local, a Boeing 737, N412CE, flight 938, operated by vanguard airlines, departed from Buffalo niagara…
- [Incident 19990725023749I](https://openairdocs.org/incident/19990725023749I), Jul 25, 1999: Boeing 737205 (N412CE), Kansas City, MO, Minor damage. (-23) On July 25, 1999, vanguard airlines, flight 301, a Boeing 737, was enroute from mci to den, when the landing gear would not go up on take off. No…
- [Incident 19990331018479I](https://openairdocs.org/incident/19990331018479I), Mar 31, 1999: Boeing 737205 (N412CE), Kansas City, MO. (-5) Pilot reported "loud noise occurred just upon lift off. Noise sounded like a loud bang around the nose wheel area. All cockpit indications normal."…

---
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.