# N121NJ: Boeing 737-2Q8, registration cancelled 2007-12-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 14, 2007
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 737-2Q8](https://openairdocs.org/model/boeing-737-2q8) (registry code 138448K)
- Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051)
- Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 21735
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 14, 1999
- Certificate issued: July 14, 2004
- Last registry action: July 17, 2007
- Mode S code: A0589E
- Owner when cancelled: [Alameda Corporation-Owner Trustee](https://openairdocs.org/faa-owner/ALAMEDA%20CORPORATION-OWNER%20TRUSTEE)
- Location: [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio)
- Owner type: Corporation
- Owner's area on the map: 29.5387° N, 98.4913° W: Placed by OpenAirDocs at the center of ZIP code 78216, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N121NJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=121NJ
- Page: https://openairdocs.org/deregistered/N121NJ-2007-12-14

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 737-2Q8: https://openairdocs.org/model/boeing-737-2q8.md

## Service difficulty reports (66, newest 50)

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

- [SDR P2EA2002M009](https://openairdocs.org/sdr/P2EA2002M009), Feb 17, 2002: THRUST REVERSER. CRACKED. ON WALK-AROUND FOUND THE NR 2 ENGINE THRUST REVERSER WITH CRACK ON THE RIGHT HAND SIDE. REPLACED THE NR 2 ENGINE THRUST REVERSER IAW MM 78-32-10, LEAK CHECK AND
- [SDR P2EA2002M002](https://openairdocs.org/sdr/P2EA2002M002), Jan 10, 2002: BUSHING. WORN. RIGHT HAND TRAILING EDGE FLAP FLUTTERS VISIBLY AT FLAPS 5 ABOVE 200 KTS. OK AT 190 KTS AND AT ALL OTHER FLAP SETTINGS. INSPECTED AND FOUND THE NR 7 FLAP JACKSCR
- [SDR P2EA2001M0018](https://openairdocs.org/sdr/P2EA2001M0018), Dec 23, 2001: LIGHT. LOOSE. DURING TAXI EMERGENCY EXIT LIGHT CENTER OF AIRCRAFT ON RIGHT LOOSE. RESECURED IAW MM 33-20. OPERATIONAL CHECK NORMAL.
- [SDR P2EA2001M0013](https://openairdocs.org/sdr/P2EA2001M0013), Dec 3, 2001: PCU. FLIGHT 350 AT AUS DURING PRE-FLIGHT CHECK THE FLIGHT CREW REPORTED A LATERAL VIBRATION WHEN RUDDER PEDALS WERE BUMPED. CREW SELECTED RUDDER STAND-BY AND FLUTERI
- [SDR P2EA2001M0011](https://openairdocs.org/sdr/P2EA2001M0011), Nov 23, 2001: PSU. UNSECURE. PSU PANEL ABOVE ROW 15 RIGHT FELL DOWN DURING TAXI-OUT. AIRCRAFT RETURNED TO BLOCKS WITH NO INCIDENT. PSU PANEL RESECURED IAW MM 25-23-11.
- [SDR P2EA01087](https://openairdocs.org/sdr/P2EA01087), Jun 1, 2001: CONTROL PANEL. DEFECTIVE. SJO - DURING FERRY FLIGHT OUT OF C-CHECK, MASTER FIRE WARNING LIGHT CAME ON AND FIRE WARNING BELL SOUNDED AFTER APPROX 25 MINUTES OF FLIGHT. WARNING LIGHT WOULD
- [SDR P2EA01077](https://openairdocs.org/sdr/P2EA01077), May 28, 2001: CARGO TRACK. BROKEN. SJO - DURING C-CHECK, FOUND LOWER FUSELAGE, AFT CARGO COMPT BETWEEN BS 790 AND 794 AND BL 19, TRACK BROKEN. TRACK REPAIRED FROM BS 780 TO 808, LBL 19 IAW SRM 53
- [SDR P2EA01076](https://openairdocs.org/sdr/P2EA01076), May 16, 2001: BULKHEAD. CRACKED. SJO - DURING C-CHECK, FOUND FUSELAGE FORWARD PRESSURE BULKHEAD BS 178, WEB WITH CRACK INDICATIONS AT WL 195 LBL 12 INCHES, RBL 15 INCHES, AND WL 218 LBL 12 INCH
- [SDR P2EA01075](https://openairdocs.org/sdr/P2EA01075), May 14, 2001: SKIN. DENTED. SJO - DURING C-CHECK, FOUND RIGHT WING INBOARD AFT FLAP, P/N 65-46434-140, S/N BN-299, UPPER SKIN WITH DENT WBL 87.75. REPAIRED RT INBOARD AFT FLAP, P/N 65-4643
- [SDR P2EA01079](https://openairdocs.org/sdr/P2EA01079), May 14, 2001: SKIN. DEBONDED. SJO - DURING C-CHECK, FOUND RIGHT WING NR 8 GROUND SPOILER, P/N 65-79950-7, S/N BN-03 WITH LOWER SKIN DISBONDED. BONDED LOWER SKIN AROUND ACTUATOR FITTING IAW S
- [SDR P2EA01057](https://openairdocs.org/sdr/P2EA01057), May 14, 2001: SKIN. DELAMINATED. SJO - DURING C-CHECK RIGHT WING NR 8 GROUND SPOILER, P/N 65-79950-7, S/N BN-013 WITH LOWER SKIN DISBONDED. (M)
- [SDR P2EA01058](https://openairdocs.org/sdr/P2EA01058), May 14, 2001: SKIN. DENTED. SJO - DURNG C-CHECK, LEFT WING INBOARD AFT FLAP, P/N 65-46434-139, S/N BN-299, UPPER SURFACE WITH DENT AT WBL 92.5. (M)
- [SDR P2EA01059](https://openairdocs.org/sdr/P2EA01059), May 14, 2001: SKIN. DENTED. SJO - DURING C-CHECK, FOUND LEFT WING INBOARD FORE FLAP, P/N 65-46430-86, S/N BN-295, LOWER SURFACE WITH DENTS AND WORN AT WBL 71.24. (M)
- [SDR P2EA01060](https://openairdocs.org/sdr/P2EA01060), May 14, 2001: SKIN. DENTED. SJO - DURING C-CHECK, FOUND RIGHT WING INBOARD AFT FLAP, P/N 65-46434-140, S/N BN-299, UPPER SKIN WITH DENT WBL 87.75. (M)
- [SDR P2EA01061](https://openairdocs.org/sdr/P2EA01061), May 14, 2001: SLAT. DELAMINATED. SJO - DURING C-CHECK, FOUND RIGHT WING, SLAT NR 5, P/N 65-46422-282, S/N BN-64, OUTBOARD CORNER WITH DELAMINATION. (M)
- [SDR P2EA01072](https://openairdocs.org/sdr/P2EA01072), May 14, 2001: SKIN. DENTED. SJO - DURING C-CHECK, LEFT WING INBOARD FORE FLAP P/N 65-46430-89, S/N BN-295, LOWER SURFACE WITH DENTS AND WORN AT WBL 71.24. REPAIRED UPPER SKIN OF FORE FLAP 
- [SDR P2EA01073](https://openairdocs.org/sdr/P2EA01073), May 14, 2001: SKIN. DELAMINATED. SJO - DURING C-CHECK, RIGHT WING SLAT NR 5, P/N 65-46422-282, S/N BN-64, OUTBOARD CORNER WITH DELAMINATION. REPAIRED SLAT NR 5 PN 65-46422-282, S/N BN-64 AT LOW
- [SDR P2EA01074](https://openairdocs.org/sdr/P2EA01074), May 14, 2001: SKIN. DENTED. SJO - DURING C-CHECK, FOUND LEFT WING INBOARD AFT FLAP P/N 65-46434-139, S/N BN-299, UPPER SURFACE WITH DENT AT WBL 92.5. REPAIRED INBOARD AFT FLAP P/N 65-46434
- [SDR P2EA000234](https://openairdocs.org/sdr/P2EA000234), Aug 6, 2000: PANEL. DENTED. MIC - DURING A WALK AROUND INSPECTION, FOUND BIRD STRIKE ON RIGHT HORIZONTAL STAB, DEFECT SIZE 19 INCHES LONG BY 5.5 INCHES WIDE, 1.75 INCHES DEEP. REPLACED LEA
- [SDR P2EA000208](https://openairdocs.org/sdr/P2EA000208), Jun 9, 2000: SKIN. DENTED. ATL - FUSELAGE SKIN SECTION IS DENTED AND GOUGED BEYOND LIMITS DUE TO GROUND DAMAGE, DEFECT SIZE LENGTH 30 INCHES BY 32 INCHES. REPAIRED STRINGER SECTIN PER DEL
- [SDR P2EA000207](https://openairdocs.org/sdr/P2EA000207), Jun 9, 2000: STRINGER. CRACKED. ATL - FOUND STRINGER 25 LEFT CRACKED AT BS 857 DUE TO GROUND DAMAGE, DEFECT SIZE LENGTH 1.5 INCH. REPAIRED STRINGER SECTION PER SRM 53-10-3 FIG 1. (M)
- [SDR P2EA000206](https://openairdocs.org/sdr/P2EA000206), Jun 9, 2000: STRINGER. CRACKED. ATL - STRINGER 24 LEFT CRACKED AT BS 875 DUE TO GROUND DAMAGE, DEFECT SIZE LENGTH 3.5 INCHES. REPAIRED STRINGER SECTION PER SRM 53-10-3 FIG 1. (M)
- [SDR P2EA000205](https://openairdocs.org/sdr/P2EA000205), Jun 9, 2000: STRINGER. CRACKED. ATL - FOUND STRINGER 23 LEFT CRACKED AT BS 875 DUE TO GROUND DAMAGE, 4.75 INCHES IN LENGTH. REPAIRED STRINGER SECTION PER SRM 53-10-3 FIG 1. (M)
- [SDR P2EA00100](https://openairdocs.org/sdr/P2EA00100), Apr 4, 2000: ATTACH FITTING. MISDRILLED. YXD - DURING C-CHECK, FOUND ATTACH FITTING TO UPPER BEAM BS 328 RBL 50.5 DOUBLER DRILLED, LENGTH .1865 INCH, WIDTH .125 INCH. REPLACED UPPER BEAM ATTACH FITTING
- [SDR P2EA00086](https://openairdocs.org/sdr/P2EA00086), Mar 31, 2000: SKIN. DELAMINATED. YXD - DURING C-CHECK, FOUND THE RIGHT OUTBOARD FORE FLAP INBOARD END BL 334 WITH DELAMINATED, LENGTH 1.5 INCH, WIDTH .500 INCH, DEPTH .089 INCH. REPAIRED RIGHT 
- [SDR P2EA00090](https://openairdocs.org/sdr/P2EA00090), Mar 28, 2000: STRINGER. CRACKED. YXD - DURING REPAIR OF CRACKS TO STRINGER 727 (SEE MRR NR 00066) FOUND STRINGER 18R DAMAGED BY STOP DRILL AT BS 756.9 AND BS 753 DIAMETER .3125 INCH, DEPTH .020
- [SDR P2EA00083](https://openairdocs.org/sdr/P2EA00083), Mar 28, 2000: SKIN. DENTED. YXD - DURING C-CHECK, FOUND DENT OUT OF LIMITS ON FUSELAGE SKIN BS 940 STRINGER 18L, LENGTH 1.25 INCH, WIDTH 1 INCH, DEPTH .050 INCH. REPAIRED AND INSTALLED DOU
- [SDR P2EA00082](https://openairdocs.org/sdr/P2EA00082), Mar 27, 2000: HOUSING. DAMAGED. YXD - DURING C-CHECK, FOUND REPAIR PLATE ON BELLCRANK HOUSING COMPLETELY SEVERED BS 680, BL 28L WL 208.1. REPLACED REPAIR PLATE ON BELL CRANK HOUSING BS 680, BL
- [SDR P2EA00081](https://openairdocs.org/sdr/P2EA00081), Mar 27, 2000: ANGLE. CRACKED. YXD - DURING C-CHECK, FOUND TIE CLIP ANGLE AT BS 360, STRINGER 14-15L WITH CRACK, .5 INCHES LONG. FABRICATED AND REPLACED TIE CLIP ANGLE AT BS 360, STRINGER 14-
- [SDR P2EA00107](https://openairdocs.org/sdr/P2EA00107), Mar 26, 2000: SKIN. CRACKED. YXD - DURING C-CHECK, FOUND FUSELAGE SKIN AT R-1 DOOR CUTOUT CRACKED AT BS 328 STRINGER 17R, LENGTH 2 INCH, WIDTH 1.2 INCH. REPAIRED FUSELAGE SKIN AT R-1 DOOR C
- [SDR P2EA00092](https://openairdocs.org/sdr/P2EA00092), Mar 24, 2000: GALLEY TRACK. CORRODED. YXD - DURING C-CHECK, FOUND FORWARD GALLEY SEAT TRACK CORRODED BEYOND LIMITS AT BS 328, RBL 42.8 WL 208.1, LENGTH 1.1 INCH BY .032 INCH WIDTH BY .100 INCH DEPTH
- [SDR P2EA00080](https://openairdocs.org/sdr/P2EA00080), Mar 24, 2000: SKIN. MISREPAIRED. YXD - DURING C-CHECK, FOUND EXISTING REPAIR AT BS 927, STRINGER 18-19L NOT PER SRM 8.5 INCHES LONG BY 12 INCHES WIDE. REMOVED AND REPLACED DOUBLER AT BS 927, ST
- [SDR P2EA00104](https://openairdocs.org/sdr/P2EA00104), Mar 23, 2000: SKIN. DELAMINATED. YXD - DURING C-CHECK, FOUND RIGHT INBOARD FORE FLAP WITH DELAMINATION AT WL100 38 INCHES FROM INBOARD END LENGTH 1.1 INCH, WIDTH .5 INCHE, WL232 LENGTH .031 INC
- [SDR P2EA00102](https://openairdocs.org/sdr/P2EA00102), Mar 23, 2000: SKIN. DELAMINATED. YXD - DURING C-CHECK, FOUND NR 5 SLAT TRAILING EDGE WITH DELAMINATED AT RWBL 317, LENGTH 4 INCHES, WIDTH 2 INCHES, WL 232, LENGTH 4.5 INCH. REPLACED NR 5 SLAT W
- [SDR P2EA00074](https://openairdocs.org/sdr/P2EA00074), Mar 20, 2000: SKIN. DENTED. YXD - DURNG C-CHECK, FOUND THE FUSELAGE WITH A DENT BEYOND LIMITS (LENGTH 1 INCH, WIDTH .75 INCH, DEPTH .032 INCH) AT BS 324 STRINGER 20-21R PER SRM 53-30-1. RE
- [SDR P2EA00091](https://openairdocs.org/sdr/P2EA00091), Mar 19, 2000: SKIN. CRACKED. YXD - DURING C-CHECK, FOUND LEFT WING INBOARD LEADING EDGE AT LEADING EDGE STATION 219.67 WITH CRACK, LENGTH 2 INCH. REPAIRED LEFT WING INBOARD LEADING EDGE SKI
- [SDR P2EA00087](https://openairdocs.org/sdr/P2EA00087), Mar 18, 2000: FRAME. CRACKED. YXD - DURING C-CHECK, FOUND A CRACK ON RIGHT INBOARD LEADING EDGE UPPER CHORD AT WBL 219.67, LENGTH .4OO INCH, WIDTH .016 INCH. REPAIRED CRACK AT WBL 219.67 RIG
- [SDR P2EA00088](https://openairdocs.org/sdr/P2EA00088), Mar 17, 2000: SKIN. DELAMINATED. YXD - DURING C-CHECK, FOUND LEFT OUTBOARD AFT FLAP TRAILING EDGE WBL 247 WITH DELAMINATION, LENGTH 4 INCH, WIDTH 4 INCH. REPAIRED DELAMINATION ON LEFT OUTBOARD 
- [SDR P2EA00084](https://openairdocs.org/sdr/P2EA00084), Mar 17, 2000: SKIN. DAMAGED. YXD - DURING C-CHECK, FOUND CREASE OUT OF LIMITS ON FUSELAGE SKIN BS 332 STRINGER 23-24R WL 163, LENGTH 2 INCH, WIDTH 1.45 INCH, DEPTH .050 INCH. REPAIRED AND I
- [SDR P2EA00089](https://openairdocs.org/sdr/P2EA00089), Mar 16, 2000: SKIN. CRACKED. YXD - DURING C-CHECK, FOUND LEFT WING LE SKIN NR 3 SLAT ARM CUTOUT AT WSS 42 WBL 227 AND WSS 90 WBL 279 WITH CRACKS, LENGTH .600 INCH AND .450 INCH. REPAIRED LE
- [SDR P2EA00103](https://openairdocs.org/sdr/P2EA00103), Mar 16, 2000: SKIN. DELAMINATED. YXD - DURING C-CHECK, FOUND NR 5 SPOILER UPPER SURFACE WITH DELAMINATED AT RWBL 114 WL 200, LENGTH 3 INCH, WIDTH 6 INCH. REPAIRED NR 5 SPOILER UPPER SURFACE AT 
- [SDR P2EA00101](https://openairdocs.org/sdr/P2EA00101), Mar 16, 2000: SKIN. DENTED. YXD - DURING C-CHECK, FOUND DENT OUT OF LIMITS ON FUSELAGE SKIN BS 368-385 STRINGER 18-19R, LENGTH 1.0 INCH, WIDTH 3.75 INCH. REPAIRED AND INSTALLED DOUBLER ON 
- [SDR P2EA00098](https://openairdocs.org/sdr/P2EA00098), Mar 16, 2000: FLOORBEAM. MISDRILLED. YXD - DURING C-CHECK, UPPER FLOORBEAM WEB AT BS 328 RBL 42.5 WL 208.1 WITH HOLES DOUBLER DRILLED, LENGTH .1855, WIDTH .20 INCH IN FOUR PLACES. REPAIRED UPPER FL
- [SDR P2EA00097](https://openairdocs.org/sdr/P2EA00097), Mar 16, 2000: SKIN. DENTED. YXD - DURING C-CHECK, FOUND FUSELAGE SKIN WITH DENT OUT OF LIMITS AT BS 1010 STRINGER 11-12L, LENGTH 1.80 INCH, WIDTH 1.20 INCH, DEPTH .054 INCH. REPAIR DENT WI
- [SDR P2EA00094](https://openairdocs.org/sdr/P2EA00094), Mar 15, 2000: DOOR FRAME. CRACKED. YXD - DURING C-CHECK, FOUND R-1 DOOR FRAME INTERCOSTAL AT BS 332 STRINGER 11 CRACKED, LENGTH .500 INCH. REPAIRED R-1 DOOR INTERCOSTAL AT BS 332, STRINGER 11 WIT
- [SDR P2EA00093](https://openairdocs.org/sdr/P2EA00093), Mar 15, 2000: DOOR FRAME. CRACKED. YXD - DURING C-CHECK, FOUND R-1 DOOR FRAME INTERCOSTAL AT BS 332 STRINGER 11 CRACKED, LENGTH .500 INCH. REPAIRED R-1 DOOR INTERCOSTAL AT BS 332, STRINGER 11 WIT
- [SDR P2EA00079](https://openairdocs.org/sdr/P2EA00079), Mar 15, 2000: SKIN. CRACKED. YXD - DURING C-CHECK, FOUND A CRACK ON FUSELAGE SKIN 3 INCHES, AT BS 941-945 STRINGER 23-24L. REPAIRED CRACK AT BS 941-945 STRINGER 23L-24L WITH DOUBLER PER SRM
- [SDR P2EA00076](https://openairdocs.org/sdr/P2EA00076), Mar 15, 2000: ANGLE. CRACKED. YXD - DURING C-CHECK, FOUND THE L-1 DOOR UPPER FORWARD ANGLE BS 342 WL 276L WITH A CRACK .75 INCHES LONG. FABRICATED AND REPLACED ANGLE AT BS 314 WL 276L PER BO
- [SDR P2EA00075](https://openairdocs.org/sdr/P2EA00075), Mar 15, 2000: ANGLE. CRACKED. YXD - DURING C-CHECK, FOUND THE L-1 DOOR UPPER AFT ANGLE BS 342 WL 276L PER BOEING SRM 51-10-1 WORK ACCOMPLISHED OF NON-ROUTINE NR 0086. (M)
- [SDR P2EA00073](https://openairdocs.org/sdr/P2EA00073), Mar 15, 2000: SKIN. DENTED. YXD - DURING C-CHECK, FOUND A DENT BEYOND LIMITS (LENGTH 1 INCH, WIDTH 1 INCH, DEPTH .035 INCH) AT BS 945.5 STRINGER 21-22L PER SRM 53-30-1. REPAIRED DENT AT BS

All 66: https://openairdocs.org/deregistered/N121NJ-2007-12-14/reports.md

## FAA accident and incident reports (3)

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 20000123000619I](https://openairdocs.org/incident/20000123000619I), Jan 23, 2000: Boeing 7372Q8 (N121NJ), Kansas City, MO. (-23) On January 23, 2000, vanguard airlines, flight 327, a Boeing 737, was enroute from atl to mci. On decent to mci the aircraft lost "system s" hydraulic…
- [Incident 19990811023679I](https://openairdocs.org/incident/19990811023679I), Aug 11, 1999: Boeing 7372Q8 (N121NJ), Kansas City, MO. (-23) During climb out, gear retracted normal; however, landing gear red intransit lights did not go out. Pilot elected to return to mci and lowered gear. All…
- [Incident 19990808038749I](https://openairdocs.org/incident/19990808038749I), Aug 8, 1999: Boeing 7372Q8 (N121NJ), Chicago, IL, Minor damage. Aircraft struck runway lights and signs on takeoff, damaging them and nose and right main tires on aircraft. Nose taxi light also broken. Takeoff aborted.

## Other aircraft with N121NJ

- [Cancelled 1999-03-18](https://openairdocs.org/deregistered/N121NJ-1999-03-18): Boeing 737-200A, S/N 21735. Owner: [Aerousa Inc](https://openairdocs.org/faa-owner/AEROUSA%20INC), [Danbury, CT](https://openairdocs.org/faa-place/CT/Danbury)

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