# N124NJ: Boeing 737-230, registration cancelled 2004-11-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 12, 2004
- Exported to: Chile
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-230](https://openairdocs.org/model/boeing-737-230) (registry code 1384401)
- Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 22122
- Year built: 0
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 19, 1999
- Certificate issued: March 27, 2003
- Last registry action: March 27, 2003
- Mode S code: A063C3
- Owner when cancelled: [Finova Capital Corp](https://openairdocs.org/faa-owner/FINOVA%20CAPITAL%20CORP)
- Location: [Scottsdale, AZ](https://openairdocs.org/faa-place/AZ/Scottsdale)
- Owner type: Corporation
- Owner's area on the map: 33.4945° N, 111.9207° W: Placed by OpenAirDocs at the center of ZIP code 85251, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N124NJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=124NJ
- Page: https://openairdocs.org/deregistered/N124NJ-2004-11-12

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 737-230: https://openairdocs.org/model/boeing-737-230.md

## Service difficulty reports (33)

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

- [SDR P2EA2002MO38](https://openairdocs.org/sdr/P2EA2002MO38), May 23, 2002: INDICATOR. FAILED. T/E FLAPS WOULD NOT EXTEND FROM FULL UP POSITION UPON DEPARTURE FROM GATE. REMOVED AND REPLACED THE FLAP POSITION INDICATOR PER MM 27-58-41, OPS CHECK GOOD AT A
- [SDR P2EA2002M005](https://openairdocs.org/sdr/P2EA2002M005), Feb 8, 2002: FITTING. LOOSE. AIRCRAFT VIBRATES AT 280 KIAS OR .73 MACH AND GREATER VIBRATION FELT ON COCKPIT FLOOR, CABIN FLOOR TO AFT GALLEY. INSPECTED ELEVATOR AND ELEVATOR TAB AND FOUND 
- [SDR P2EA2001V0008](https://openairdocs.org/sdr/P2EA2001V0008), Oct 22, 2001: SHROUD. CRACKED. DURING C-CHECK FOUND APU SHROUD (COWL) LEFT AFT SIDE CRACKED. APU LOWER SHROUD SKIN REPAIRED IAW COOPESA EO COO-3-49-587-01, DOCUMENTED ON FAA FORM 8110-3.
- [SDR P2EA2001V0007](https://openairdocs.org/sdr/P2EA2001V0007), Oct 19, 2001: CROSSBEAM. CRACKED. DURING C CHECK WAS FOUND THE FWD CARGO DOOR, FWD LOWER CORNER CROSS BEAM CRACKED. FWD CARGO DOOR CROSS BEAM FWD T CHORD AND PERFORMED PREVENTIVE MODIFICATION IA
- [SDR P2EA2001V0004](https://openairdocs.org/sdr/P2EA2001V0004), Oct 19, 2001: KEELBEAM. CRACKED. DURING C CHECK FOUND THE AFT CARGO COMPARTMENT STR 27R AT BS 727+16 KEEL BEAM CHORD WITH CRACK. FUSELAGE KELL BEAM SECTION REPAIRED AT STR 27R, BETWEEN BS 727+9
- [SDR P2EA2001V0003](https://openairdocs.org/sdr/P2EA2001V0003), Oct 19, 2001: SKIN. DENTED. DURING C CHECK FOUND THE EXTERNAL FUSELAGE SKIN AT BS 909.25 BETWEEN STR 21R AND 22R WITH DENT OUT LIMITS. FUSELAGE SKIN SECTION REPAIRED FROM BS 907 TO BS 912 
- [SDR P2EA2001V0001](https://openairdocs.org/sdr/P2EA2001V0001), Oct 19, 2001: SKIN. DENTED. DURING C CHECK: EXTERNAL FUSELAGE AT BS 1042 BETWEEN STR 14L AND 15L SKIN WITH DENT. FUSELAGE SKIN SECTION REPAIRED FROM BS 1039 TO BS 1048 BETWEEN STR 13L TO S
- [SDR P2EA2001V0011](https://openairdocs.org/sdr/P2EA2001V0011), Oct 18, 2001: SKIN. WORN. DURING C-CHECK, FOUND THE LEFT WING T/E FORE FLAP P/N 65-46430-89, S/N BN 436 UPPER SKIN WORN. LT WING I/B FORE FLAP REPAIRED FROM WBL 74.5 TO WBL 79.5 IAW SRM 
- [SDR P2EA2001V0005](https://openairdocs.org/sdr/P2EA2001V0005), Oct 18, 2001: SKIN. DENTED. DURING C CHECK: FWD CARGO DOOR EXTERNAL SKIN WITH SEVERAL DENTS OUT LIMITS. FWD CARGO DOOR SKIN REPLACED IAW SRM 52-30-2 FIG 3.
- [SDR P2EA2001V0002](https://openairdocs.org/sdr/P2EA2001V0002), Oct 18, 2001: SKIN. CANNING. DURING C CHECK WAS FOUND THE EXTERNAL FUSELAGE SKIN AT BS 1078 BETWEEN STR 23R AND STR 24R WITH OIL CAN. FUSELAGE SKIN SECTION REPAIRED FROM BS 1054 TO BS 1088 
- [SDR P2EA2001V0010](https://openairdocs.org/sdr/P2EA2001V0010), Oct 18, 2001: SKIN. DENTED. DURING C-CHECK RIGHT WING L/E SECTION FSS 338 OUTER SKIN WITH DENT. RIGHT WING L/E SECTION BETWEEN FSS 333.8 AND FSS 345.8 DUE TO DENT IAW SRM 57-30-4 FIG 5.
- [SDR P2EA2001V0006](https://openairdocs.org/sdr/P2EA2001V0006), Oct 18, 2001: SKIN. DENTED. DURING C CHECK EXTERNAL FUSELAGE BS 374 STR 20R SKIN WITH DENT OUT LIMITS. SKIN SECTION REPAIRED FROM BS 367 TO 381.5 BTW STR 19R AND STR 21R IAW COOPESA EO COO
- [SDR P2EA2001M0008](https://openairdocs.org/sdr/P2EA2001M0008), Oct 16, 2001: SKIN. During Inspection found Crack in fuselage skin at BS 847 and STR. 25R approx. 1.00" in length.See Vanguard Aircraft log page #92242
- [SDR P2EA01192](https://openairdocs.org/sdr/P2EA01192), Sep 15, 2001: GYRO. FAILED. FLT 313 - MCI - WITH `A` AUTO PILOT ENGAGED, YOKE JERKS/PUMPS 3 OR 4 TIMES ABRUPTLY IN DESCENT. REMOVED AND REPLACED NR 1 VERTICAL GYRO AND OPERATIONAL CHECK NO
- [SDR P2EA01184](https://openairdocs.org/sdr/P2EA01184), Sep 9, 2001: AUTOPILOT SYS. MALFUNCTIONED. A CHANNEL AUTO PILOT STARTED TO SHAKE IN THE DESCENT. PERFORMED ADJUSTMENT AND TEST PER MM 22-11-01, NO DEFECTS NOTED. (M)
- [SDR P2EA01171](https://openairdocs.org/sdr/P2EA01171), Aug 28, 2001: FLAP. MALFUNCTIONED. FLT 451-MCI- ON APPROACH INTO MCI WHEN FLAPS SELECTED TO 1, FLAPS DID NOT EXTEND. RECYCLED AND FLAPS EXTENDED UP TO 15, BUT WOULD NOT GO TO 25. RECYCLED THE HAN
- [SDR P2EA01160](https://openairdocs.org/sdr/P2EA01160), Aug 15, 2001: AUTOPILOT SYS. MALFUNCTIONED. FLT 350 - MCI - AUTO PILOT A CHANNEL WOULD NOT STAY ENGAGED DURING CLIMB-OUT OR CRUISE. DEFERRED AUTO PILOT A CHANNEL IAW MEL 22-1, CI NR M124864 PER MAINTENANC
- [SDR P2EA01137](https://openairdocs.org/sdr/P2EA01137), Jul 22, 2001: VALVE. FAILED. FLT 940 - MCI - ON DESCENT TO 12,000 FEET POWER AT IDLE, CABIN NI 700 FEET DESCENT. WHEN ADVANCING POWER AT 12,000 TO 1.3 EPR CABIN SHOWED DESCENT OF 2000 FEET 
- [SDR P2EA01133](https://openairdocs.org/sdr/P2EA01133), Jul 20, 2001: WARNING LIGHT. ILLUMINATED. FLT 554 - MCI - AFTER PUSH BACK FROM GATE AND AFTER APPLICATION OF AIRCRAFT POWER, THE AFT SERVICE DOOR UNSAFE LIGHT ILLUMINATED. RETURNED TO THE GATE. INSPECTE
- [SDR P2EA01050](https://openairdocs.org/sdr/P2EA01050), May 7, 2001: PROXIMITY SWITCH. OUT OF ADJ. FLT 350 - MCI-MDW EN ROUTE CALL, 'INTRANSIT' LEADING EDGE SLAT. WOULD HAVE TO MAKE FLAPS 15 LANDING AND WOULD BE UNABLE TO LAND IN MDW. DECISION MADE TO RETURN 
- [SDR P2EA2001V0009](https://openairdocs.org/sdr/P2EA2001V0009), Mar 10, 2001: SKIN. DENTED. ON LEADING EDGE OF AFT CARGO DOOR SKIN APPROXIMATELY 18 INCHES FROM LOWER EDGE WITH BOEING TEMPORARY REPAIR PER VAG-MCI-01-0002H DUE DENT OUT LIMITS. INSTALLED 
- [SDR P2EA00465](https://openairdocs.org/sdr/P2EA00465), Dec 19, 2000: INDICATOR. MALFUNCTIONED. UPON LANDING, FLAPS WOULD NOT EXTEND OR RETRACT PER CONVENTIONAL METHODS. ALTERNATE FLAPS USED AND AIRCRAFT LANDED WITHOUT INCIDENT.RESET FLAP INDICATOR. FLAP S
- [SDR P2EA00464](https://openairdocs.org/sdr/P2EA00464), Dec 18, 2000: INDICATOR. MALFUNCTIONED. DURING FLIGHT HYDRAULIC PRESSURE WENT TO ZERO. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO INCIDENT. RESERVOIR CHECKED UPON LANDING, NO DEFECTS NOTED. HYDRAULI
- [SDR P2EA00398](https://openairdocs.org/sdr/P2EA00398), Nov 20, 2000: WARNING SYSTEM. MALFUNCTIONED. DEN - FLT 206 - ON TAKEOFF ROLL, AS RT ENGINE EPR INCREASED PAST 1.30 RECEIVED TAKEOFF CONFIGURATION WARNING HORN. RECYCLED FLAPS UP, HORN STILL PRESENT. AIRCRA
- [SDR P2EA00325](https://openairdocs.org/sdr/P2EA00325), Nov 6, 2000: CONTROL HANDLE. FAULTY. MCI - FLT 101 - ON ENGINE SHUT DOWN, ALL THREE RED LANDING GEAR LIGHTS ILLUMINATED. REPLACED LANDING GEAR CONTROL LEVER ASSY PER MM 32-31-11. REPLACED R273 RELA
- [SDR P2EA00323](https://openairdocs.org/sdr/P2EA00323), Oct 31, 2000: HANDLE. LACK OF LUBE. MCI - FLT 230 - ON APPROACH WHEN LANDING GEAR WAS EXTENDED, THREE GREEN LIGHTS APPEARED INITIALLY. ON 2-MILE FINAL, THREE RED LIGHTS ILLUMINATED. LANDING GEAR W
- [SDR P2EA00301](https://openairdocs.org/sdr/P2EA00301), Oct 22, 2000: CIRCUIT BOARD. FAILED. AFTER TAKE OFF AND DURING GEAR RETRACTION EXPERIENCED AN INTERMITTENT LANDING GEAR WARNING HORN ALONG WITH AN OVERHEAD MASTER CAUTION ANNUNICATOR LIGHT. ELECTRI
- [SDR P2EA00251](https://openairdocs.org/sdr/P2EA00251), Sep 12, 2000: FITTING. CRACKED. SJO - DURING C-CHECK, LEFT WING INBOARD FLAP BOOM FORWARD ATTACH FITTING CRACKED. REPAIRED BY MODIFICATION IAW SB 737-27-1110 SECTION III FIGURES 2, 3 AND 4. (M
- [SDR P2EA00250](https://openairdocs.org/sdr/P2EA00250), Sep 11, 2000: BULKHEAD. CRACKED. SJO - DURING C-CHECK, LEFT SIDE CHORD AT BS 178 CRACKED .5 INCHES, WL 207 AND WL 190. REMOVED SIDE CHORD AND REPLACED CHORD WITH UPGRADED PART IAW SB 737-53A117
- [SDR P2EA00249](https://openairdocs.org/sdr/P2EA00249), Sep 11, 2000: BEAM. CRACKED. SJO - DURING C-CHECK, VERTICAL BEAM CHORD CRACKED 1 INCH AT BS 178, WL 184 AND LBL 5.7. REPAIRED VERTICAL BEAM FORWARD CHORD AT BS 178 LBL 5.7 BETWEEN WL 177 AN
- [SDR P2EA00199](https://openairdocs.org/sdr/P2EA00199), Jun 6, 2000: FAN. SEIZED. DEN - FLT 301 - AFTER LANDING, LIGHT SMOKE AND FUMES WERE NOTED IN COCKPIT. DEFERRED CONTROL CABIN AIR FLOW FAN PER MEL 21-30 CONTROL ITEM NR M124377. REFERENCE
- [SDR P2EA00110](https://openairdocs.org/sdr/P2EA00110), Apr 7, 2000: ENGINE. VIBRATION. MCI - UNUSUAL VIBRATION NOTED FROM NR 1 ENGINE AT IDLE TO 55 PERCENT N-1 AFTER PUSHBACK. REPLACED NR 1 ENGINE PER VANGUARD TASK CARD J271-00-01-C. LEAK AND OPER
- [SDR P2EA00069](https://openairdocs.org/sdr/P2EA00069), Mar 19, 2000: SKIN. CRACKED. MDW - FUSELAGE DAMAGED AT BS 794 BETWEEN S21R AND S22R BY BELT LOADER DURING THROUGH FLIGHT SERVICE. REPAIRED FUSELAGE SKIN AT BS 794, S21R AND S22R PER FEC DRA

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