# Service difficulty reports: N122NJ, cancelled Jun 3, 2004

A list on [N122NJ, cancelled Jun 3, 2004](https://openairdocs.org/deregistered/N122NJ-2004-06-03.md).

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

- [SDR P2EA2002M047](https://openairdocs.org/sdr/P2EA2002M047.md): Lens · missing · Jul 1, 2002 · N122NJ · Boeing 737230 · Emergency Lighting
  > 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.md): Light · Mar 24, 2002 · N122NJ · Boeing 737230 · Emergency Lighting
  > 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 closing action for P2EA2002M018. Reference VAM 037, dated 03/24/02
- [SDR P2EA2002M016](https://openairdocs.org/sdr/P2EA2002M016.md): Hinge Fitting · vibrates · Mar 4, 2002 · N122NJ · Boeing 737230 · Horizontal Stabilizer Structure
  > 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 VIBRATION NOTED TO THIS DATE.
- [SDR P2EA2002M011](https://openairdocs.org/sdr/P2EA2002M011.md): Structure · vibration · Mar 1, 2002 · N122NJ · Boeing 737230 · Fuselage Main, Structure
  > DURING FLIGHT A FLIGHT ATTENDANT REPORTED VIBRATION AT THE AFT GALLEY FLOOR. VIBRATION STOPPED AND THEN STARTED AGAIN DURING FLIGHT. ALL SYSTEMS INDICATED NORMAL AND AIRCRAFT CONTINUED TO SCHEDULED DESTINATION AND LANDED WITH NO INCIDENT. AIRCRAFT WAS INSPEC
- [SDR P2EA2001V0030](https://openairdocs.org/sdr/P2EA2001V0030.md): Flap · delaminated · Nov 21, 2001 · N122NJ · Boeing 737230 · Trailing Edge Flaps
  > 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 Delamination From WBL 73.00 to 89 & From WBL 156.15 to 145.15 IAW COOPESA EO No. COO-CMP-3-57-613-01, Dated No
- [SDR P2EA2001V0029](https://openairdocs.org/sdr/P2EA2001V0029.md): Flap · delaminated · Nov 21, 2001 · N122NJ · Boeing 737230 · Trailing Edge Flaps
  > 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 COOPESA EO No. COO-CMP-3-57-610-01, Dated Nov 06, 2001 Approved on FAA 8110-3 Form By DERT710167SW.
- [SDR P2EA2001V0028](https://openairdocs.org/sdr/P2EA2001V0028.md): Flap · worn · Nov 21, 2001 · N122NJ · Boeing 737230 · Trailing Edge Flaps
  > 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 EO No. COO-CMP-3-57-608-01, Dated Nov 06, 2001 Approved on FAA 8110-3 Form By DERT-710167SW.Note: See
- [SDR P2EA2001V0027](https://openairdocs.org/sdr/P2EA2001V0027.md): Flap · delaminated · Nov 21, 2001 · N122NJ · Boeing 737230 · Trailing Edge Flaps
  > 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 180.75 to 165.875 & From Wbl 155.75 to 143 IAW COOPESA EO No.COO-CMP-3-57-612-01 Dated Nov 06, 2001, Ap
- [SDR P2EA2001V0025](https://openairdocs.org/sdr/P2EA2001V0025.md): Door · delaminated · Nov 20, 2001 · N122NJ · Boeing 737230 · Landing Gear Doors
  > 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 BS262.5, IAW COOPESA EO No.COO-CMP-3-52-614-01, Dated Nov 07, 2001 & Documented on FAA 8110-3 Form Approv
- [SDR P2EA2001V0026](https://openairdocs.org/sdr/P2EA2001V0026.md): Flap · delaminated · Nov 20, 2001 · N122NJ · Boeing 737230 · Trailing Edge Flaps
  > 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.COO-CMP-3-57-611-01 Dated Nov 06,2001 & Documented on FAA 8110-3 Form Approved by DERT-710167SW.Not
- [SDR P2EA2001V0024](https://openairdocs.org/sdr/P2EA2001V0024.md): Attach Angle · cracked · Nov 14, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Bulkhead
  > During "C" Check Inspection.-Control Cabin, Fwd Pressure Bulkhead BS178, R-H Side Chord Cracked Between WL 207 & 210.-Preventive Modification accomplished at Fwd Pressure Bulkhead BS178, R-H Chord, Between WL184 & 230 due to Crack IAW Boeing S/B 737-53A1173, R
- [SDR P2EA2001V0023](https://openairdocs.org/sdr/P2EA2001V0023.md): Skin · dented · Nov 14, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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, Between Str 19 & 24 R-H, IAW SRM 53-30-3, Fig 17.Note: See COOPESA Work Order No.O10863 1-8, VAM100 No
- [SDR P2EA2001V0022](https://openairdocs.org/sdr/P2EA2001V0022.md): Skin · cracked · Nov 14, 2001 · N122NJ · Boeing 737230 · Fuselage, Door Hinge
  > 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 Lower Hinge Cut out, From BS945to BS956, Between Str 13 & 16 L-H, IAW SRM 53-30-3, Fig 34.Note: See
- [SDR P2EA2001V0021](https://openairdocs.org/sdr/P2EA2001V0021.md): Skin · dented · Nov 13, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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, Between Str 25 & 28 R-H, Due to Dent, IAW Boeing Telex COO-SJO-01-00893H & COOPESA E.O. No.COO-3-53-607
- [SDR P2EA2001V0020](https://openairdocs.org/sdr/P2EA2001V0020.md): Skin · dented · Nov 13, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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, Between Str 24 & 25 L-H, Due to Dent IAW SRM 53-30-3 Fig 5.Note: See COOPESA Work Order No.O10863 1-17,
- [SDR P2EA2001V0019](https://openairdocs.org/sdr/P2EA2001V0019.md): Stringer · cracked · Nov 12, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Longeron/Stringer
  > 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, Fig 1Note: See COOPESA Work Order No. O10863 1-70, VAM100 No. 227 & 122SDA099.
- [SDR P2EA2001V0018](https://openairdocs.org/sdr/P2EA2001V0018.md): Skin · dented · Nov 12, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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, Between Str17 & 18 L-H,IAW SRM53-30-3 Fig17Note: See COOPESA Work Order No. O10863 1-9, VAM100 No.046 &
- [SDR P2EA2001V0017](https://openairdocs.org/sdr/P2EA2001V0017.md): Skin Panel · cracked · Nov 12, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Keel
  > 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 BS 661.75 to BS 726.75, Between LBL 6.30 to RBL 6.30 due to Cracks IAW Boeing S/B 737-53-1104, Secti
- [SDR P2EA2001V0016](https://openairdocs.org/sdr/P2EA2001V0016.md): Fairing · worn · Nov 12, 2001 · N122NJ · Boeing 737230 · Nacelle/Pylon, Plate/Skin
  > 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 Repaired due to Wear, IAW COOPESA E.O. No. EO-100-3-54-609-01, Dated Nov 06, 2001 Documented on FAA811
- [SDR P2EA2001V0015](https://openairdocs.org/sdr/P2EA2001V0015.md): Skin · dented · Nov 12, 2001 · N122NJ · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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, Between Str 20 & 27 R-H due to Dent, IAW COOPESA E.O. No.EO-100-3-53-604-01, Dated Nov 05, 2001 Docum
- [SDR P2EA2001V0014](https://openairdocs.org/sdr/P2EA2001V0014.md): Fairing · worn · Nov 12, 2001 · N122NJ · Boeing 737230 · Nacelle/Pylon, Plate/Skin
  > 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. EO-COO-3-54-609-01, Dated Nov 06, 2001, Documented on FAA 8110-3 form approved by DERT710167SW.Note:
- [SDR P2EA2001V0013](https://openairdocs.org/sdr/P2EA2001V0013.md): Skin · dented · Nov 12, 2001 · N122NJ · Boeing 737230 · Vertical Stabilizer, Plate/Skin
  > 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.md): Door Frame · cracked · Nov 12, 2001 · N122NJ · Boeing 737230 · Passenger/Crew Doors
  > 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.md): Coupler · failed · Sep 16, 2001 · N122NJ · Boeing 737230 · Autopilot System
  > 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.md): Tube · damaged · Jun 10, 2001 · N122NJ · Boeing 737230 · Wing Structure
  > 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 HOLD OPEN RODS AND ATTACH BRACKETS IAW BOEING MM 30-22-0, 57-30-00. (M)
- [SDR P2EA01055](https://openairdocs.org/sdr/P2EA01055.md): Flap · malfunctioned · May 12, 2001 · N122NJ · Boeing 737230 · Trailing Edge Flap Control System
  > 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 27-51-01. SYSTEM CHECKED NORMAL ON GROUND. SUBSEQUENTLY, ON APPROACH TO MDW FROM MCI, FLAPS WOULD
- [SDR P2EA01002](https://openairdocs.org/sdr/P2EA01002.md): Warning System · malfunctioned · Jan 19, 2001 · N122NJ · Boeing 737230 · Landing Gear Position and Warning
  > 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 AROUND, CYCLED GEAR 2ND TIME ALL INDICATIONS NORMAL. TESTED GEAR LIGHTS AND HORN IAW BOEING MM 32-
- [SDR P2EA00462](https://openairdocs.org/sdr/P2EA00462.md): Indicator · malfunctioned · Dec 10, 2000 · N122NJ · Boeing 737230 · Instrument Panel
  > 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/HR. AIRCRAFT RETURNED TO MCI WITH NO INCIDENT. REPLACED FUEL FLOW INDICATOR IAW MM 31, OPERATIONA
- [SDR P2EA00241](https://openairdocs.org/sdr/P2EA00241.md): Fitting · corroded · Aug 22, 2000 · N122NJ · Boeing 737230 · Vertical Stabilizer, Attach Fittings
  > 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 RT OUTBOARD AFT LUG, AFT FACE, RT OUTBOARD FORWARD LUG, FORWARD FACE, RT INBOARD AFT LUG, AFT FACE
- [SDR P2EA00244](https://openairdocs.org/sdr/P2EA00244.md): Fitting · misdrilled · Aug 17, 2000 · N122NJ · Boeing 737230 · Fuselage Main, Attach Fittings
  > 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.md): Frame · cracked · Aug 8, 2000 · N122NJ · Boeing 737230 · Fuselage Main, Frame
  > 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.md): Seat Track · corroded · Aug 8, 2000 · N122NJ · Boeing 737230 · Fuselage, Seat/Cargo Attach Fittings
  > 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. (M)
- [SDR P2EA00242](https://openairdocs.org/sdr/P2EA00242.md): Frame · cracked · Aug 7, 2000 · N122NJ · Boeing 737230 · Fuselage Structure (General)
  > 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.md): Skin · delaminated · Aug 4, 2000 · N122NJ · Boeing 737230 · Leading Edge Devices
  > 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 PAGE 45. (M)
- [SDR P2EA00235](https://openairdocs.org/sdr/P2EA00235.md): Frame · cracked · Aug 4, 2000 · N122NJ · Boeing 737230 · Fuselage Main, Frame
  > 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 53-10-4 FIG 10. (M)
- [SDR P2EA00016](https://openairdocs.org/sdr/P2EA00016.md): Pcu · vibrated · Jan 25, 2000 · N122NJ · Boeing 737230 · Rudder Control System
  > FLT 705 - MCI - VIBRATION NOTED DURING ENGINE SHUTDOWN. MAINTENANCE TROUBLESHOT VIBRATION TO B SYSTEM HYDRAULICS, FOUND RUDDER PCU VIBRATING WHEN DEFLECTED FROM CENTER. REMOVED AND REPLACED RUDDER PCU IAW MM 27-21-91. (M)
- [SDR P2EA99239](https://openairdocs.org/sdr/P2EA99239.md): Insulation · out of position · Sep 6, 1999 · N122NJ · Boeing 737230 · Cargo Compartments
  > MCI - THE FOLLOWING WAS REPORTED DURING CREW PRE-DEPARTURE WALK-AROUND. ODOR COMING FROM AIR CONDITIONING DUCTING. FOUND APU BLEED DUCT INSULATION BLANKET, IN AFT CARGO PIT BEHIND FORWARD WALL, SECURED WITH CARGO PIT TAPE. TAPE WAS BURNED AND BRITTLE. PROP

## 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 = 'N122NJ' AND deregistration_id = 'N122NJ-2004-06-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N122NJ-2004-06-03/reports

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