# Service difficulty reports: N124NJ, cancelled Nov 12, 2004

A list on [N124NJ, cancelled Nov 12, 2004](https://openairdocs.org/deregistered/N124NJ-2004-11-12.md).

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

- [SDR P2EA2002MO38](https://openairdocs.org/sdr/P2EA2002MO38.md): Indicator · failed · May 23, 2002 · N124NJ · Boeing 737230 · Trailing Flap Position Indicating System
  > 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 ALL POSITION SETTINGS.
- [SDR P2EA2002M005](https://openairdocs.org/sdr/P2EA2002M005.md): Fitting · loose · Feb 8, 2002 · N124NJ · Boeing 737230 · Elevator Tab Control System
  > 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 THE LEFT HAND ELEVATOR TAB CONTROL ROD FITTING LOOSE. RETORQUED THE LEFT HAND ELEVATOR TAB CONTROL
- [SDR P2EA2001V0008](https://openairdocs.org/sdr/P2EA2001V0008.md): Shroud · cracked · Oct 22, 2001 · N124NJ · Boeing 737230 · APU Cowling/Containment
  > 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.md): Crossbeam · cracked · Oct 19, 2001 · N124NJ · Boeing 737230 · Cargo/Baggage Doors
  > 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 IAW SB 737-52A1100 REV 4, SECTION III FIG 4 AND 6.
- [SDR P2EA2001V0004](https://openairdocs.org/sdr/P2EA2001V0004.md): Keelbeam · cracked · Oct 19, 2001 · N124NJ · Boeing 737230 · Fuselage Main, Keel
  > 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+9.75 AND BS 727A+7.25 DUE TO CRACK IAW COOPESA E.O NR COO-3-53-585-01. DOCUMENTED ON FAA FORM 8110-3
- [SDR P2EA2001V0003](https://openairdocs.org/sdr/P2EA2001V0003.md): Skin · dented · Oct 19, 2001 · N124NJ · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 BETWEEN STR 21R AND STR 23R IAW SRM 53-30-3 FIG 28.
- [SDR P2EA2001V0001](https://openairdocs.org/sdr/P2EA2001V0001.md): Skin · dented · Oct 19, 2001 · N124NJ · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 STR 16L IAW SRM 53-30-3 FIG 6.
- [SDR P2EA2001V0011](https://openairdocs.org/sdr/P2EA2001V0011.md): Skin · worn · Oct 18, 2001 · N124NJ · Boeing 737230 · Trailing Edge Flaps
  > 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 51-40-20 REPAIR 21 FIG 30.
- [SDR P2EA2001V0005](https://openairdocs.org/sdr/P2EA2001V0005.md): Skin · dented · Oct 18, 2001 · N124NJ · Boeing 737230 · Cargo/Baggage Doors
  > 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.md): Skin · canning · Oct 18, 2001 · N124NJ · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 BETWEEN STR 16R AND STR 25R IAW COOPESA EO COO-3-53-581-01, DOCUMENT ON FAA 810-3 APPROVED BY FAA DE
- [SDR P2EA2001V0010](https://openairdocs.org/sdr/P2EA2001V0010.md): Skin · dented · Oct 18, 2001 · N124NJ · Boeing 737230 · Wing, Plate/Skin
  > 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.md): Skin · dented · Oct 18, 2001 · N124NJ · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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-3-53-580-01 APPROVED BY DER.
- [SDR P2EA2001M0008](https://openairdocs.org/sdr/P2EA2001M0008.md): Skin · Oct 16, 2001 · N124NJ · Boeing 737230 · Fuselage Structure (General)
  > 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.md): Gyro · failed · Sep 15, 2001 · N124NJ · Boeing 737230 · Attitude Gyro and Indicating System
  > 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 NORMAL IAW MM 22-11-01. (M)
- [SDR P2EA01184](https://openairdocs.org/sdr/P2EA01184.md): Autopilot Sys · malfunctioned · Sep 9, 2001 · N124NJ · Boeing 737230 · Autopilot System
  > 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.md): Flap · malfunctioned · Aug 28, 2001 · N124NJ · Boeing 737230 · Trailing Edge Flap Control System
  > 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 HANDLE A COUPLE OF MORE TIMES AND FLAPS FINALLY EXTENDED TO 25 AND THEN 30. AFTER LANDING, FLAPS RETRAC
- [SDR P2EA01160](https://openairdocs.org/sdr/P2EA01160.md): Autopilot Sys · malfunctioned · Aug 15, 2001 · N124NJ · Boeing 737230 · Autopilot System
  > 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 MAINTENANCE CONTROL. (M)
- [SDR P2EA01137](https://openairdocs.org/sdr/P2EA01137.md): Valve · failed · Jul 22, 2001 · N124NJ · Boeing 737230 · Cabin Pressure Control System
  > 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 WITH NOTICEABLE PRESSURE CHANGE IN OUR EARS. IN DESCENT TO 12,000 FEET WITH POWER AT IDLE SHOWED 4
- [SDR P2EA01133](https://openairdocs.org/sdr/P2EA01133.md): Warning Light · illuminated · Jul 20, 2001 · N124NJ · Boeing 737230 · Door Warning System
  > 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. INSPECTED THE AIRCRAFT L2 DOOR, OPEN AND CLOSED DOOR NORMALLY. NO DEFECTS FOUND. (M)
- [SDR P2EA01050](https://openairdocs.org/sdr/P2EA01050.md): Proximity Switch · out of adj · May 7, 2001 · N124NJ · Boeing 737230 · Leading Edge Slat Position Indicating System
  > 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 TO MCI. DID NOT DECLARE EMERGENCY IN MCI. OVERNIGHT MAINTENANCE AT MCI ADJUSTED NR 1 SLAT PROXIM
- [SDR P2EA2001V0009](https://openairdocs.org/sdr/P2EA2001V0009.md): Skin · dented · Mar 10, 2001 · N124NJ · Boeing 737230 · Cargo/Baggage Doors
  > 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 PERMANENT REPAIR PER SRM 52-00-3 FIG 5 AT AFT CARGO DOOR EXTERNAL SKIN FROM BS 796 TO BS 800.5 BETW
- [SDR P2EA00465](https://openairdocs.org/sdr/P2EA00465.md): Indicator · malfunctioned · Dec 19, 2000 · N124NJ · Boeing 737230 · Trailing Flap Position Indicating System
  > UPON LANDING, FLAPS WOULD NOT EXTEND OR RETRACT PER CONVENTIONAL METHODS. ALTERNATE FLAPS USED AND AIRCRAFT LANDED WITHOUT INCIDENT.RESET FLAP INDICATOR. FLAP SYSTEM INSPECTED AND OPERATIONAL CHECK PERFORMED. NO DEFECTS NOTED.
- [SDR P2EA00464](https://openairdocs.org/sdr/P2EA00464.md): Indicator · malfunctioned · Dec 18, 2000 · N124NJ · Boeing 737230 · Hydraulic Quantity Indicator
  > DURING FLIGHT HYDRAULIC PRESSURE WENT TO ZERO. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO INCIDENT. RESERVOIR CHECKED UPON LANDING, NO DEFECTS NOTED. HYDRAULIC SYSTEM CHECKED FOR LEAKS AND ALL FLIGHT CONTROLS WERE CYCLED TO REMOVE AIR. HYDRAULIC SYSTEM O
- [SDR P2EA00398](https://openairdocs.org/sdr/P2EA00398.md): Warning System · malfunctioned · Nov 20, 2000 · N124NJ · Boeing 737230 · Trailing Flap Position Indicating System
  > 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. AIRCRAFT RETURNED TO GATE WITH NO INCIDENT. PERFORMED TAKEOFF SYSTEM CHECK IAW JOB CARD J2-A2. COULD N
- [SDR P2EA00325](https://openairdocs.org/sdr/P2EA00325.md): Control Handle · faulty · Nov 6, 2000 · N124NJ · Boeing 737230 · Landing Gear Selector
  > 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 RELAY PER MM 32-61-61. CLEANED ADDITIONAL PLUGS. D5082 AND D2618. SYSTEM OPERATED NORMAL PER MM 32
- [SDR P2EA00323](https://openairdocs.org/sdr/P2EA00323.md): Handle · lack of lube · Oct 31, 2000 · N124NJ · Boeing 737230 · Landing Gear Selector
  > 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 WAS EXTENDED BY EMERGENCY PROCEDURES AND MCI - FLT 230 - AN EMERGENCY WAS DECLARED. AIRCRAFT LANDE
- [SDR P2EA00301](https://openairdocs.org/sdr/P2EA00301.md): Circuit Board · failed · Oct 22, 2000 · N124NJ · Boeing 737230 · Landing Gear Position and Warning
  > AFTER TAKE OFF AND DURING GEAR RETRACTION EXPERIENCED AN INTERMITTENT LANDING GEAR WARNING HORN ALONG WITH AN OVERHEAD MASTER CAUTION ANNUNICATOR LIGHT. ELECTRICAL ODOR EVIDENT ON SHUTDOWN AT GATE. A/C RETURNED TO GATE WITH NO INCIDENT. ADJUSTED GAP ON PROXI
- [SDR P2EA00251](https://openairdocs.org/sdr/P2EA00251.md): Fitting · cracked · Sep 12, 2000 · N124NJ · Boeing 737230 · Trailing Edge Flap Actuator
  > 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.md): Bulkhead · cracked · Sep 11, 2000 · N124NJ · Boeing 737230 · Fuselage Main, Bulkhead
  > 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 737-53A1173, SECTION III PART XI STEP H. (M)
- [SDR P2EA00249](https://openairdocs.org/sdr/P2EA00249.md): Beam · cracked · Sep 11, 2000 · N124NJ · Boeing 737230 · Fuselage Main, Bulkhead
  > 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 AND WL 193 IAW SRM 53-10-11 FIG 8. (M)
- [SDR P2EA00199](https://openairdocs.org/sdr/P2EA00199.md): Fan · seized · Jun 6, 2000 · N124NJ · Boeing 737230 · Air Distribution Fan
  > 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 MEL 21-30 CONTROL ITEM NR M124377 CONTROL CABIN AIR FLOW FAN INOPERATIVE. REMOVED AND REPLACED C
- [SDR P2EA00110](https://openairdocs.org/sdr/P2EA00110.md): Engine · vibration · Apr 7, 2000 · N124NJ · Boeing 737230 · Engine (Turbine/Turboprop)
  > 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 OPERATIONAL CHECKS OK. (X)
- [SDR P2EA00069](https://openairdocs.org/sdr/P2EA00069.md): Skin · cracked · Mar 19, 2000 · N124NJ · Boeing 737230 · Fuselage Main, Plate/Skin
  > 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 DRAWING NR 005301 AND 005302, FAA FORM 8110-3. (M)

## 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 = 'N124NJ' AND deregistration_id = 'N124NJ-2004-11-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N124NJ-2004-11-12/reports

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