# N122NJ: 1981 Boeing 737-230, registration cancelled 2004-06-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 3, 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: 22120
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 21, 1999
- Certificate issued: March 27, 2003
- Last registry action: March 27, 2003
- Mode S code: A05C55
- 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/N122NJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=122NJ
- Page: https://openairdocs.org/deregistered/N122NJ-2004-06-03

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 (37)

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

- [SDR P2EA2002M047](https://openairdocs.org/sdr/P2EA2002M047), Jul 1, 2002: LENS. MISSING. ROW 4 EMERGENCY TRACK LIGHTING MISSING LENS. REMOVED AND REPLACED LENS IAW MM 33-53-0. OPERATIONAL CHECK NORMAL.
- [SDR P2EA2002M018](https://openairdocs.org/sdr/P2EA2002M018), Mar 24, 2002: LIGHT. During operational check at scheduled inspection the R/H AFT Emergency Light was found defective. Removed and replaced Light assembly IAW MM 33-51-81. This is c
- [SDR P2EA2002M016](https://openairdocs.org/sdr/P2EA2002M016), Mar 4, 2002: HINGE FITTING. VIBRATES. INTERMITTENT VIBRATION OBSERVED AROUND THE AFT GALLEY FLOOR AREA. REMOVED AND REPLACED THE NR 4 HINGE FITTING ON THE LT HORIZONTAL STAB IAW MM 27-31-13. NO VIBR
- [SDR P2EA2002M011](https://openairdocs.org/sdr/P2EA2002M011), Mar 1, 2002: STRUCTURE. VIBRATION. DURING FLIGHT A FLIGHT ATTENDANT REPORTED VIBRATION AT THE AFT GALLEY FLOOR. VIBRATION STOPPED AND THEN STARTED AGAIN DURING FLIGHT. ALL SYSTEMS INDICATED NORMA
- [SDR P2EA2001V0030](https://openairdocs.org/sdr/P2EA2001V0030), Nov 21, 2001: FLAP. DELAMINATED. During "C" Inspection.-L-H Wing Imb Fore Flap upper Surface WBL 150.4 Delaminated.-Repaired L-H Wing Imb Fore Flap P/N 65-46430-89, S/N BN-430 Due to Delaminati
- [SDR P2EA2001V0029](https://openairdocs.org/sdr/P2EA2001V0029), Nov 21, 2001: FLAP. DELAMINATED. During "C" Check Inspection.-L-H Wing Outb Flap Imb Hinge Flap, T/E Section Delaminated.-Repaired L-H Outb Flipper Flap, P/N 65-71930-91 Due to Delamination IAW
- [SDR P2EA2001V0028](https://openairdocs.org/sdr/P2EA2001V0028), Nov 21, 2001: FLAP. WORN. During "C" Check Inspection.-R-H Wing Imb Fore Flap Skin Worn at Imb Side.-Repaired R-H Imb Fore Flap, P/N 65-46430-90, S/N BN436 Due to Worn Skin IAW COOPESA E
- [SDR P2EA2001V0027](https://openairdocs.org/sdr/P2EA2001V0027), Nov 21, 2001: FLAP. DELAMINATED. During "C" Check Inspection.-R-H Wing Imb Aft Flap Delaminated & Dented.-Repaired R-H Wing Imb Flap P/N 65-46434-140, S/N BN442 Due to Delamination From Wbl 180
- [SDR P2EA2001V0025](https://openairdocs.org/sdr/P2EA2001V0025), Nov 20, 2001: DOOR. DELAMINATED. During "C" Check Inspection.-R-H NLG Door, P/N 65-50520-504, S/N BNW330 Found With Delamination.-Repaired R-H NLG Door Due to Delamination From BS294.5 to BS262
- [SDR P2EA2001V0026](https://openairdocs.org/sdr/P2EA2001V0026), Nov 20, 2001: FLAP. DELAMINATED. During "c" Check Inspection.-L-H Imb Mid Flap, P/N 65-79953 T/E With Delamination.-Repair T/E of Imb Mid Flap P/N 65-79953 Due to Delamination IAW COOPESA EO No
- [SDR P2EA2001V0024](https://openairdocs.org/sdr/P2EA2001V0024), Nov 14, 2001: ATTACH ANGLE. CRACKED. During "C" Check Inspection.-Control Cabin, Fwd Pressure Bulkhead BS178, R-H Side Chord Cracked Between WL 207 & 210.-Preventive Modification accomplished at Fw
- [SDR P2EA2001V0023](https://openairdocs.org/sdr/P2EA2001V0023), Nov 14, 2001: SKIN. DENTED. During "C" Check Inspection.-Fuselage at BS325, Between Str 20 & 21 R-H, Skin With Dent Out of Limits.-Fuselage Skin Section Repaired, From BS320 to BS350.5, Be
- [SDR P2EA2001V0022](https://openairdocs.org/sdr/P2EA2001V0022), Nov 14, 2001: SKIN. CRACKED. During "C" Check Inspection.-L2 Door Area, Fuselage Lower Hinge Cut out, Lower Section, Skin With Sharp Edges & Crack.-Repaired Fuselage Skin Section at L2 door
- [SDR P2EA2001V0021](https://openairdocs.org/sdr/P2EA2001V0021), Nov 13, 2001: SKIN. DENTED. During "C" Check Inspection.-Fuselage at BS499, Between Str 26 & 27 R-H, Skin With Dent Out of Limits.-Fuselage Skin Section Repaired From BS492 to BS504.5, Bet
- [SDR P2EA2001V0020](https://openairdocs.org/sdr/P2EA2001V0020), Nov 13, 2001: SKIN. DENTED. During "C" Check Inspection.-Fuselage at BS984, Between Str 24 & 25 L-H, Skin With Dent Out of Limits.-Fuselage Skin Section Repaired From BS982 to BS986.5, Bet
- [SDR P2EA2001V0019](https://openairdocs.org/sdr/P2EA2001V0019), Nov 12, 2001: STRINGER. CRACKED. During "C" Check Inspection.-Fuselage, BS1080, Str 22 R-H With Crack.-Fuselage Stringer Section Repaired at Str 22 R-H, From BS1050 to BS1088, IAW SRM 53-10-3, 
- [SDR P2EA2001V0018](https://openairdocs.org/sdr/P2EA2001V0018), Nov 12, 2001: SKIN. DENTED. During "C" Check Inspection.-Fuselage, at BS390, Between Str 17 & 18 L-H, Skin With Dent Out of Limits.-Repaired Fuselage Skin Section From BS387 to BS396, Betw
- [SDR P2EA2001V0017](https://openairdocs.org/sdr/P2EA2001V0017), Nov 12, 2001: SKIN PANEL. CRACKED. During "C" Check Inspection.-Fuselage, Keel Beam Panel Cracked at BS 698 and With Loose Rivets at BS726, Str27 L-H.-Replaced Fuselage Keel Beam Skin Panel from 
- [SDR P2EA2001V0016](https://openairdocs.org/sdr/P2EA2001V0016), Nov 12, 2001: FAIRING. WORN. During "C" Check Inspection.-Engine No.1, Nacelle Fairing, Imb Aft Section, Outter Skin With Wear.-Engine No.1, Nacelle Fairing, Imb Aft Section, Outter Skin Re
- [SDR P2EA2001V0015](https://openairdocs.org/sdr/P2EA2001V0015), Nov 12, 2001: SKIN. DENTED. During "c" Check Inspection:-Fuselage, BS1086, Between Str 25 & 26 R-H Skin With Dent Out of Limits.-Repaired Fuselage Skin Section From BS1069.5 to BS1090.5, B
- [SDR P2EA2001V0014](https://openairdocs.org/sdr/P2EA2001V0014), Nov 12, 2001: FAIRING. WORN. During "C" Check Inspection:-No.2 Engine Pylon, Aft Fairing Worn at Imb Side.-No. 2 Pylon Imboard Fairing Outer Skin Repaired due to Wear, IAW COOPESA E.O. No. 
- [SDR P2EA2001V0013](https://openairdocs.org/sdr/P2EA2001V0013), Nov 12, 2001: SKIN. DENTED. C CHECK, VERTICAL FIN WITH DENTS BETWEEN FIN STA 191.5 - 180.3. REPAIRED SKIN IAW SRM 55-30-6 FIG 2.
- [SDR P2EA2001V0012](https://openairdocs.org/sdr/P2EA2001V0012), Nov 12, 2001: DOOR FRAME. CRACKED. DURING C CHECK INSPECTION, L1 DOOR FWD AND AFT LOWER CORNER AND LOWER PAN WITH A CRACK. REPAIRED DOOR FRAME IAW SRM 51-40-3 FIG 1.
- [SDR P2EA01190](https://openairdocs.org/sdr/P2EA01190), Sep 16, 2001: COUPLER. FAILED. FLT 552 - MDW - YAW DAMPER INOPERATIVE. REMOVED AND REPLACED YAW DAMPER COUPLER OPERATIONAL CHECK NORMAL IAW MM 22-12-0. (M)
- [SDR P2EA01092](https://openairdocs.org/sdr/P2EA01092), Jun 10, 2001: TUBE. DAMAGED. MCI - FLT 906 - DURING WALK AROUND, FOUND THAT THE AIRCRAFT REFUELING DOOR HAD BEEN LEFT OPEN ON ITS FLIGHT FROM MSY. DAMAGE WAS CAUSED TO AN ANTI-ICE DUCT, TWO
- [SDR P2EA01055](https://openairdocs.org/sdr/P2EA01055), May 12, 2001: FLAP. MALFUNCTIONED. MCI - FLT 356, 354, 2259 - WHILE ON APPROACH INTO MCI FROM BUF, FLAPS WOULD NOT EXTEND BEYOND 25 DEGREES. MAINTENANCE PERFORMED OPERATIONAL CHECK PER BOEING MM 
- [SDR P2EA01002](https://openairdocs.org/sdr/P2EA01002), Jan 19, 2001: WARNING SYSTEM. MALFUNCTIONED. MCI - FLT 101 - DURING APPROACH WITH LANDING GEAR HANDLE DOWN, GEAR INDICATION OF 3 GREEN, 3 RED LIGHTS ON AND WARNIGN HORN SOUNDING. ABORTED APPROACH AND WENT 
- [SDR P2EA00462](https://openairdocs.org/sdr/P2EA00462), Dec 10, 2000: INDICATOR. MALFUNCTIONED. MCI - FLT 625 - IN-FLIGHT AND WITH NR 2 FUEL QUANTITY INDICATOR ON DEFERRAL, THE NR 2 FUEL FLOW INDICATOR READ 1800/HR WHILE NR 1 FUEL FLOW INDICATOR READS 2700
- [SDR P2EA00241](https://openairdocs.org/sdr/P2EA00241), Aug 22, 2000: FITTING. CORRODED. DURING C-CHECK INSPECTION, (SB 737-55-1028) OF THE FIN ATTACHMENT FITTINGS, CORROSION WAS FOUNDON FIVE OF EIGHT ATTACHMENT LUGS. THE CORROSION WAS FOUND ON THE 
- [SDR P2EA00244](https://openairdocs.org/sdr/P2EA00244), Aug 17, 2000: FITTING. MISDRILLED. DURING C-CHECK, LOWER HOLE IN FITTING AT BS 695 BORED SLIGHTLY OFFSET. ENLARGED HOLE TO .9375 DIA AND INSTALLED BUSHING IAW MPP B737-VAG-00-53-010. (M)
- [SDR P2EA00239](https://openairdocs.org/sdr/P2EA00239), Aug 8, 2000: FRAME. CRACKED. DURING C-CHECK, VERTICAL CHORD CRACKED .375 INCHES IN LENGTH AT BS 178, LBL 5.7 INCH AND WL 181.57. REPAIRED IAW SB 737-53A-1173 PARA B2 PAGE 70. (M)
- [SDR P2EA00236](https://openairdocs.org/sdr/P2EA00236), Aug 8, 2000: SEAT TRACK. CORRODED. DURING C-CHECK, FOUND CORROSION (LEVEL 2) ON SEAT TRACK FROM BS 340 TO 360, LBL 45 AND WL 208. FABRICATED SEAT TRACK IAW SRM 51-20-1 AND INSTALLED IAW MM 25-52.
- [SDR P2EA00242](https://openairdocs.org/sdr/P2EA00242), Aug 7, 2000: FRAME. CRACKED. DURING C-CHECK, LEFT CHORD CRACKED 1.25 INCH AT BS 178 WL 207 AND LBL 23. REPAIRED CRACK IAW SB 737-53A-1173, FIG 61. (M)
- [SDR P2EA00245](https://openairdocs.org/sdr/P2EA00245), Aug 4, 2000: SKIN. DELAMINATED. DURING C-CHECK, RIGHT OUTBOARD FORE FLAP UPPER SKIN IS DELAMINATED (16 INCHES) AND DENTED. REPAIRED FORE FLAP IAW SRM 51-40-6 PAGE 8 PARA 11 AND SRM 51-40-6 PAG
- [SDR P2EA00235](https://openairdocs.org/sdr/P2EA00235), Aug 4, 2000: FRAME. CRACKED. DURING C-CHECK, FRAME LOWER LOBE CRACKED LENGTH 4 INCH, AT BS 312 BETWEEN STRINGER 24L AND 25L. REPAIRED FRAME AT BS 312 BETWEEN STRINGER 24L AND 25L IAW SRM 53
- [SDR P2EA00016](https://openairdocs.org/sdr/P2EA00016), Jan 25, 2000: PCU. VIBRATED. FLT 705 - MCI - VIBRATION NOTED DURING ENGINE SHUTDOWN. MAINTENANCE TROUBLESHOT VIBRATION TO B SYSTEM HYDRAULICS, FOUND RUDDER PCU VIBRATING WHEN DEFLECTED FROM
- [SDR P2EA99239](https://openairdocs.org/sdr/P2EA99239), Sep 6, 1999: INSULATION. OUT OF POSITION. MCI - THE FOLLOWING WAS REPORTED DURING CREW PRE-DEPARTURE WALK-AROUND. ODOR COMING FROM AIR CONDITIONING DUCTING. FOUND APU BLEED DUCT INSULATION BLANKET, IN A

## FAA accident and incident reports (4)

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 20020726027129I](https://openairdocs.org/incident/20020726027129I), Jul 26, 2002: Boeing 737230 (N122NJ), Kansas City, MO. (-23) On July 26, 2002, vanguard airlines, flt. 842 reported to ATC of a foul smell in the cabin due to a birdstrike and declared an emergency. The a/c landed…
- [Incident 20020301008319I](https://openairdocs.org/incident/20020301008319I), Mar 1, 2002: Boeing 737230 (N122NJ), Kansas City, MO. (-23) Vanguard flight 400 reported shaking in the aircraft. Returned to mci to check out problem and landed without incident at 1630Z. Flight attendant…
- [Incident 20001210021379I](https://openairdocs.org/incident/20001210021379I), Dec 10, 2000: Boeing 737230 (N122NJ), Kansas City, MO. (-23)On December 10, 2000, at approx. 2130 CDT, vanguard airlines flight VGD625, a Boeing 737, N122NJ, left Kansas City International Airport, Kansas City, MO.…
- [Incident 19990920027469I](https://openairdocs.org/incident/19990920027469I), Sep 20, 1999: Boeing 737230 (N122NJ), Kansas City, MO. (-23) After takeoff numerous annunciators and master caution lights illuminated. Aircraft returned to mci and landed without incident, no emergency was…

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