# Service difficulty reports: N121NJ, cancelled Dec 14, 2007

A list on [N121NJ, cancelled Dec 14, 2007](https://openairdocs.org/deregistered/N121NJ-2007-12-14.md).

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

Page 1 of 2 · 66 reports

- [SDR P2EA2002M009](https://openairdocs.org/sdr/P2EA2002M009.md): Thrust Reverser · cracked · Feb 17, 2002 · N121NJ · Boeing 7372Q8 · Engine Thrust Reverser
  > 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 OPS CHECK NORMAL.
- [SDR P2EA2002M002](https://openairdocs.org/sdr/P2EA2002M002.md): Bushing · worn · Jan 10, 2002 · N121NJ · Boeing 7372Q8 · Trailing Edge Flap Actuator
  > 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 JACKSCREW GEAR BOX END UNIVERSAL JOINT BUSHINGS WORN. OVERHAULED THE NR 7 FLAP JACKSCREW GEAR BOX END UN
- [SDR P2EA2001M0018](https://openairdocs.org/sdr/P2EA2001M0018.md): Light · loose · Dec 23, 2001 · N121NJ · Boeing 7372Q8 · Emergency Lighting
  > 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.md): Pcu · Dec 3, 2001 · N121NJ · Boeing 7372Q8 · Rudder Control System
  > 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 FLUTERING OF RUDDER STOPPED. REMOVED AND REPLACED THE RUDDER PCU I.A.W. BMM 27-21-91 OPS AND LEAK CHECKS GO
- [SDR P2EA2001M0011](https://openairdocs.org/sdr/P2EA2001M0011.md): Psu · unsecure · Nov 23, 2001 · N121NJ · Boeing 7372Q8 · Passenger Compartment Equipment
  > 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.md): Control Panel · defective · Jun 1, 2001 · N121NJ · Boeing 7372Q8 · Fire Detection
  > 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 NOT EXTINGUISH AND BELL WOULD NOT SILENCE. NO OTHER SYSTEM FIRE WARNING LIGHTS WERE ON. AIRCRAFT
- [SDR P2EA01077](https://openairdocs.org/sdr/P2EA01077.md): Cargo Track · broken · May 28, 2001 · N121NJ · Boeing 7372Q8 · Fuselage, Seat/Cargo Attach Fittings
  > 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 53-10-5 FIG 11. (M)
- [SDR P2EA01076](https://openairdocs.org/sdr/P2EA01076.md): Bulkhead · cracked · May 16, 2001 · N121NJ · Boeing 7372Q8 · Fuselage Main, Bulkhead
  > 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 INCHES. REPAIRED FUSELAGE AT BS 178, FORWARD PRESSURE BULKHEAD WEB FROM RBL 1.3 TO RBL 18 BETWEEN WL 21
- [SDR P2EA01075](https://openairdocs.org/sdr/P2EA01075.md): Skin · dented · May 14, 2001 · N121NJ · Boeing 7372Q8 · Trailing Edge Flaps
  > 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 65-46434-140, S/N BN-299 AT UPPER SKIN BETWEEN WBL 86 AND 95 IAW SRM 51-40-20 REPAIR 9, FIG 18. (M)
- [SDR P2EA01079](https://openairdocs.org/sdr/P2EA01079.md): Skin · debonded · May 14, 2001 · N121NJ · Boeing 7372Q8 · Spoilers
  > 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 SRM 51-40-20 FIG 10 REPAIR 1. BONDED LOWER SKIN AROUND ACTUATOR FITTING IAW SRM 51-40-20 FIG 10 REP
- [SDR P2EA01057](https://openairdocs.org/sdr/P2EA01057.md): Skin · delaminated · May 14, 2001 · N121NJ · Boeing 7372Q8 · Spoilers
  > 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.md): Skin · dented · May 14, 2001 · N121NJ · Boeing 7372Q8 · Trailing Edge Flaps
  > 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.md): Skin · dented · May 14, 2001 · N121NJ · Boeing 7372Q8 · Leading Edge Devices
  > 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.md): Skin · dented · May 14, 2001 · N121NJ · Boeing 7372Q8 · Trailing Edge Flaps
  > 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.md): Slat · delaminated · May 14, 2001 · N121NJ · Boeing 7372Q8 · Leading Edge Devices
  > 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.md): Skin · dented · May 14, 2001 · N121NJ · Boeing 7372Q8 · Leading Edge Devices
  > 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 P/N 65-46430-89, S/N BN-295 IAW SRM 51-40-20, REPAIR NR 22 FIG 31. DENTS AT WBL 101.24 AND 115.00
- [SDR P2EA01073](https://openairdocs.org/sdr/P2EA01073.md): Skin · delaminated · May 14, 2001 · N121NJ · Boeing 7372Q8 · Leading Edge Devices
  > 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 LOWER SKIN BETWEEN SLAT STATION 244.53 AND 254 IAW SRM 51-40-20, REPAIR 15, FIG 24. (M)
- [SDR P2EA01074](https://openairdocs.org/sdr/P2EA01074.md): Skin · dented · May 14, 2001 · N121NJ · Boeing 7372Q8 · Trailing Edge Flaps
  > 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 65-46434-139, S/N BN-299 AT UPPER SKIN BETWEEN WBL 80 AND 87 IAW SRM 51-40-20 REPAIR 9 FIG 18. (M)
- [SDR P2EA000234](https://openairdocs.org/sdr/P2EA000234.md): Panel · dented · Aug 6, 2000 · N121NJ · Boeing 7372Q8 · Horizontal Stabilizer Structure
  > 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 LEADING EDGE PANEL PER SRM 55-10-0. (M)
- [SDR P2EA000208](https://openairdocs.org/sdr/P2EA000208.md): Skin · dented · Jun 9, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > 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 DELTA ERA NR 377496-14. (M)
- [SDR P2EA000207](https://openairdocs.org/sdr/P2EA000207.md): Stringer · cracked · Jun 9, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Jun 9, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Jun 9, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Longeron/Stringer
  > 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.md): Attach Fitting · misdrilled · Apr 4, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Attach Fittings
  > 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 BS 328 RBL 50.5 WITH FABRICATED FITTING PER BOEING SRM 51-10-1. WORK ACCOMPLISHED ON NON-ROUTINE
- [SDR P2EA00086](https://openairdocs.org/sdr/P2EA00086.md): Skin · delaminated · Mar 31, 2000 · N121NJ · Boeing 7372Q8 · Leading Edge Devices
  > 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 OUTBOARD FORE FLAP INBOARD END DELAMINATED WITH DOUBLER PER SRM 51-40-6 WORK ACCOMPLISHED ON NON-RO
- [SDR P2EA00090](https://openairdocs.org/sdr/P2EA00090.md): Stringer · cracked · Mar 28, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Longeron/Stringer
  > 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 INCH. REPAIRED STRINGER 18R WITH STRINGER SPLICE PER BOEING SRM 53-10-3 PAGE 10 FIG 1 SHEET 8 WORK
- [SDR P2EA00083](https://openairdocs.org/sdr/P2EA00083.md): Skin · dented · Mar 28, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > 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 DOUBLER OF FUSELAGE SKIN BS 940 STRINGER 18L PER SRM 51-30-3 FIG 6 WORK COMPLETED ON VAM100-0420. (M)
- [SDR P2EA00082](https://openairdocs.org/sdr/P2EA00082.md): Housing · damaged · Mar 27, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Structure
  > 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 28L, WL 208.1 PER SRM 51-10-1, 51-10-3 WORK ACCOMPLISHED ON NON-ROUTINE NR 0404. (M)
- [SDR P2EA00081](https://openairdocs.org/sdr/P2EA00081.md): Angle · cracked · Mar 27, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Miscellaneous Structure
  > 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 14-15L PER SRM 51-10-1, 51-30-2 WORK ACCOMPLISHED ON NON-ROUTINE NR 0344. (M)
- [SDR P2EA00107](https://openairdocs.org/sdr/P2EA00107.md): Skin · cracked · Mar 26, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > 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 CUTOUT BS 328 STRINGER 17R PER BOEING SRM 53-30-3 FIG 26 WORK COMPLETED ON VAM100-0406. (M)
- [SDR P2EA00092](https://openairdocs.org/sdr/P2EA00092.md): Galley Track · corroded · Mar 24, 2000 · N121NJ · Boeing 7372Q8 · Fuselage, Seat/Cargo Attach Fittings
  > 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. REPAIRED SEAT TRACK AT FWD GALLY BS 328 WL 208.1 RBL 42.8 BY SPLICING PER BOEING SRM 53-10-5 FIG
- [SDR P2EA00080](https://openairdocs.org/sdr/P2EA00080.md): Skin · misrepaired · Mar 24, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > 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, STRINGER 18-19L IAW SRM 53-30-3 WORK ACCOMPLISHED ON NON-ROUTINE NR 0331. (M)
- [SDR P2EA00104](https://openairdocs.org/sdr/P2EA00104.md): Skin · delaminated · Mar 23, 2000 · N121NJ · Boeing 7372Q8 · Trailing Edge Flaps
  > 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 INCH. REPAIRED RIGHT INBOARD FORE FLAP IAW BOEING SRM 51-40-6 WORK COMPLETED ON VAM100-0152. (M)
- [SDR P2EA00102](https://openairdocs.org/sdr/P2EA00102.md): Skin · delaminated · Mar 23, 2000 · N121NJ · Boeing 7372Q8 · Leading Edge Devices
  > 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 WITH SERVICEABLE SLAT P/N NR 65-46-422-282 IAW BOEING MM 27-81-12 WORK COMPLETED ON VAM 100-0374.(M)
- [SDR P2EA00074](https://openairdocs.org/sdr/P2EA00074.md): Skin · dented · Mar 20, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > 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. REPAIRED DENT TO FUSELAGE BS 324 STRINGER 20-21R WITH DOUBLER PER SRM 52-00-03 WORK ACCOMPLISHED ON N
- [SDR P2EA00091](https://openairdocs.org/sdr/P2EA00091.md): Skin · cracked · Mar 19, 2000 · N121NJ · Boeing 7372Q8 · Wing, Plate/Skin
  > 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 SKIN AT LE STATION 219 PER BOEING SRM 57-20-2 FIG 1 AND 51-10-1 PARAGRAPH 4 WORK ACCOMPLISHED ON NON-R
- [SDR P2EA00087](https://openairdocs.org/sdr/P2EA00087.md): Frame · cracked · Mar 18, 2000 · N121NJ · Boeing 7372Q8 · Wing Miscellaneous Structure
  > 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 RIGHT INBOARD UPPER CHORD BY REPLACEMENT PER SRM 51-10-1 ADN 52-20-2 WORK ACCOMPLISHED ON NON-ROUTINE
- [SDR P2EA00088](https://openairdocs.org/sdr/P2EA00088.md): Skin · delaminated · Mar 17, 2000 · N121NJ · Boeing 7372Q8 · Trailing Edge Flaps
  > 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 AFT FLAP TRAILING EDGE WBL 247 PER BOEING SRM 51-40-6 PAGE 8 PARA 11 WORK ACCOMPLISHED ON NON-ROUTI
- [SDR P2EA00084](https://openairdocs.org/sdr/P2EA00084.md): Skin · damaged · Mar 17, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > 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 INSTALLED DOUBLER OF FUSELAGE SKIN BS 332 STRINGER 23-24R WL 163 PER SRM 51-30-3 FIG 9 WORK COMPLETE
- [SDR P2EA00089](https://openairdocs.org/sdr/P2EA00089.md): Skin · cracked · Mar 16, 2000 · N121NJ · Boeing 7372Q8 · Leading Edge Devices
  > 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 LEFT WING LEADING EDGE SKIN AT NR 3 SLAT ARM CUTOUT WSS 42 WBL 227 AND WSS 90 WBL 279 PER BOEING SRM
- [SDR P2EA00103](https://openairdocs.org/sdr/P2EA00103.md): Skin · delaminated · Mar 16, 2000 · N121NJ · Boeing 7372Q8 · Spoilers
  > 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 RWBL 114 WL 200 IAW BOEING SRM 51-40-6 WORK COMPLETED ON VAM100-0150. (M)
- [SDR P2EA00101](https://openairdocs.org/sdr/P2EA00101.md): Skin · dented · Mar 16, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > 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 FUSELAGE SKIN BS 368-386 STRINGER 18-19R PER APPROVED SPAR MPP NR VAN-2000-737-53-030 REPAIR AND BO
- [SDR P2EA00098](https://openairdocs.org/sdr/P2EA00098.md): Floorbeam · misdrilled · Mar 16, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Floor Beam
  > 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 FLOORBEAM WEB AT BS 328, WL 208.1 RBL 42.5 WITH WEB SPLICE INCORRECTED PER SRM 51-40-3 FIG 1. WORK A
- [SDR P2EA00097](https://openairdocs.org/sdr/P2EA00097.md): Skin · dented · Mar 16, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > 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 WITH DOUBLER AT BS 1010, STRINGER 11-12L PER SRM 53-30-3 FIG 1 WORK ACCOMPLISHED ON NON-ROUTINE NR 01
- [SDR P2EA00094](https://openairdocs.org/sdr/P2EA00094.md): Door Frame · cracked · Mar 15, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Structure
  > 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 WITH DOUBLER PER SRM 51-40-3 FIG 1 WORK ACCOMPLISHED ON NON-ROUTINE NR 137. (M)
- [SDR P2EA00093](https://openairdocs.org/sdr/P2EA00093.md): Door Frame · cracked · Mar 15, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Miscellaneous Structure
  > 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 WITH DOUBLER PER SRM 51-40-3, FIG 1 WORK ACCOMPLISHED ON NON-ROUTINE NR 137. (M)
- [SDR P2EA00079](https://openairdocs.org/sdr/P2EA00079.md): Skin · cracked · Mar 15, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > 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 52-30-3 PAGE 11-12B. WORK ACCOMPLISHED ON NON-ROUTINE NR 0095. (M)
- [SDR P2EA00076](https://openairdocs.org/sdr/P2EA00076.md): Angle · cracked · Mar 15, 2000 · N121NJ · Boeing 7372Q8 · Passenger/Crew Doors
  > 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 BOEING SRM 51-10-1, 51-30-02 WORK ACCOMPLISHED OF NON-ROUTINE NR 0085. (M)
- [SDR P2EA00075](https://openairdocs.org/sdr/P2EA00075.md): Angle · cracked · Mar 15, 2000 · N121NJ · Boeing 7372Q8 · Passenger/Crew Doors
  > 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.md): Skin · dented · Mar 15, 2000 · N121NJ · Boeing 7372Q8 · Fuselage Main, Plate/Skin
  > 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 945.5 STRINGER 21-22L WITH DOUBLER PER SRM 52-00-03 FIG 1 WORK ACCOMPLISHED ON NON-ROUTINE NR 0119

Next page: https://openairdocs.org/deregistered/N121NJ-2007-12-14/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N121NJ' AND deregistration_id = 'N121NJ-2007-12-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N121NJ-2007-12-14/reports

---
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.