# Service difficulty reports: N322FE, cancelled May 4, 2006

A list on [N322FE, cancelled May 4, 2006](https://openairdocs.org/deregistered/N322FE-2006-05-04.md).

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

- [SDR 2004F00236](https://openairdocs.org/sdr/2004F00236.md): Fuse Link · sheared · Aug 14, 2004 · N322FE · Doug DC1030F · Leading Edge Slat Control System
  > RT OB SLAT RETAINER MECHANISM MECHANICAL FUSE SHEARED. (REFERENCE MM 27-83-08 PAGE 202 FIGURE 201) REFERENCE NON-ROUTINE 39546.
- [SDR 2004F00237](https://openairdocs.org/sdr/2004F00237.md): Sleeve · cracked · Aug 14, 2004 · N322FE · Doug DC1030F · Engine Thrust Reverser
  > NR 3 ENGINE IB THRUST REVERSER EXTRUDED TORQUE RING, AT THE LEADING EDGE OF TRANSLATING SLEEVE, CRACKED AROUND FASTENER HOLE AT 10 O'CLOCK (REVERSER DEPLOYED). REFERENCE NON-ROUTINE 39502.
- [SDR 2004FA0000678](https://openairdocs.org/sdr/2004FA0000678.md): Fuse Pin · sheared · Aug 6, 2004 · N322FE · Doug DC1030F · Leading Edge Slat Actuator
  > RT WING OB SLAT CONTROL MECHANISM HAS ANTI-DROOP FUSE PIN SHEARED. REFERENCE NON-ROUTINE 39501.
- [SDR 2004FA0000679](https://openairdocs.org/sdr/2004FA0000679.md): Attach Fitting · corroded · Aug 6, 2004 · N322FE · Doug DC1030F · Fuselage, Wing Attach Fittings
  > LOWER AFT WING TO CENTER BOX ATTACH SKATE FITTING IS EXFOLIATED, LT WHEEL WELL, FUSELAGE STATION 1366 TO 1381. REFERENCE NON-ROUTINE NR 39431.
- [SDR 01FDEA00218](https://openairdocs.org/sdr/01FDEA00218.md): Pin · defective · Mar 20, 2001 · N322FE · Doug DC1030F · Nose/Tail Landing Gear
  > NOSE GEAR DID NOT RETRACT ON T/O. REMOVED AND REPLACED NOSE GEAR PIN. AC OK TO CONTINUE.
- [SDR 00FDEA00400](https://openairdocs.org/sdr/00FDEA00400.md): Stiffener · corroded · Jun 20, 2000 · N322FE · Doug DC1030F · Fuselage Miscellaneous Structure
  > SNRM 0327 LOWER AUX FUEL TANK AFT BULKHEAD, LT MOST VERTICAL STIFFNER FOUND WITH CORROSION. R&R PER 51-31-01, 21-11-06-2.
- [SDR 00FDEA00399](https://openairdocs.org/sdr/00FDEA00399.md): Support Bracket · cracked · Jun 20, 2000 · N322FE · Doug DC1030F · Wing Miscellaneous Structure
  > SNRM 0338 RT WING PANEL SUPPORT FOR PANEL NR 618GB WAS CRACKED, LOCATED APPROX 4 INCHES OB OF SLAT DRIVE MECH ACCESS PANEL. R&R PER SRM 51-31-01.
- [SDR 00FDEA00403](https://openairdocs.org/sdr/00FDEA00403.md): Skin · cracked · Jun 19, 2000 · N322FE · Doug DC1030F · Trailing Edge Flaps
  > SNRM 0196 LT WING OB FLAP UPPER SKIN SURFACE FOUND CRACKED APPROX 3 5/32 INCHES. R&R PER SRM 51-31-01, 57-10-00, 57-52-02.
- [SDR 00FDEA00402](https://openairdocs.org/sdr/00FDEA00402.md): Skin · cracked · Jun 19, 2000 · N322FE · Doug DC1030F · Trailing Edge Flaps
  > SNRM 0198 LT WING IB FLAP UPPER SKIN FOUND PATCH REPAIR CRACKED APPOX 6 INCHES. R&R PER CMM 57-52-01.
- [SDR 00FDEA00401](https://openairdocs.org/sdr/00FDEA00401.md): Skin · cracked · Jun 19, 2000 · N322FE · Doug DC1030F · Wing, Plate/Skin
  > SNRM 0222 LT WING L/E LOWER ACCESS PANEL CUTOUT NR 526AB FWD SIDE FOUND CRACKED. R&R PER SRM 51-31-01.
- [SDR 00FDEA00398](https://openairdocs.org/sdr/00FDEA00398.md): Channel · corroded · Jun 19, 2000 · N322FE · Doug DC1030F · Fuselage Miscellaneous Structure
  > SNRM 0252 AFT FUSELAGE WATER TANK BAY STA 1996, FUSELAGE FRAME AFT LWR CHANNEL TOP SURFACE CORRODED, LONGERON 50 RT TO LT. R&R CHANNEL & STRAP PER SRM 53-30-00 FIG 8, VOL 1.
- [SDR 98FDEA00413](https://openairdocs.org/sdr/98FDEA00413.md): Fire Bottle · discharged · Jun 20, 1998 · N322FE · Doug DC1030F · Fire Bottle, Fixed
  > ENGINE NR 2, NR 1 BOTTLE LOW PRESSURE LIGHT ILLUMINATING JUST PRIOR TO DEPARTURE. FOUND NR 1 BOTTLE OF APU FIRE EXTINGUISHER SYSTEM HAD DISCHARGED THRU APU PORT (NR 2 ENG FIREX CONTAINER 1). REPLACED NR 2 ENG FIREX CONTAINER 1 PER M/M 26-21-02 AND SQUIB FOR
- [SDR 98FDEA00250](https://openairdocs.org/sdr/98FDEA00250.md): Slider · broken · Apr 5, 1998 · N322FE · Doug DC1030F · Cargo/Baggage Doors
  > SHORT FINAL, LEFT AFT CARGO DOOR LIGHT ON F/E PANEL ILLUM FOLLOWED BY IMMEDIATE PRESSURE DROP IN CABIN. ACFT WAS ALREADY CONFIGURED FOR LANDING, LANDED SUCCESSFULLY, NO FURTHER PROBLEMS. DOOR 4L SWITCH NOT WORKING DUE TO TRACK CAM AND SLIDER BROKEN. REPLACE
- [SDR 96FDEA01489](https://openairdocs.org/sdr/96FDEA01489.md): Hi-Lock Collars · missing · Sep 16, 1996 · N322FE · Doug DC1030F · Vertical Stabilizer
  > SNRM NR 0352, VERTICAL STABILIZER ALL COLLARS MISSING FROM HI-LOCKS BETWEEN AFT H-11 BOLTS THAT ATTACH UPPER VERICAL STABILIZER TO LOWER VERTICAL STABILER. REF LAX C-CH-02, SNRM NR 0352.
- [SDR 96FDEA01490](https://openairdocs.org/sdr/96FDEA01490.md): Tension Strap · cracked · Sep 14, 1996 · N322FE · Doug DC1030F · Wing Miscellaneous Structure
  > SMRM NR 00506, RT WING, O/B FLAP I/B HINGE O/B SIDE TENSION STRAP IS CRACKED AT THE LOWER BOLT HOLE LOWER FLANGE. *S/D* REMOVED AND REPLACED TENSION STRAP BRACKET AS PER SRM 51-00-01 VOL NR I.
- [SDR 96FDEA01435](https://openairdocs.org/sdr/96FDEA01435.md): V-Panel · missing · Sep 4, 1996 · N322FE · Doug DC1030F · Nacelle/Pylon Structure
  > UPON WALK AROUND, FOUND THE V-PANEL ON NR 3 ENGINE PYLON RIPPED AWAY. INSTALLED V-PANEL ON PYLON FARING. ALSO, REPAIRED DAMAGED PYLON FARING HONEYCOMB PANEL OUTBOARD PER DC-10 STRUCTURE REPAIR MANUAL 51-10-00.
- [SDR 95FDEA01428](https://openairdocs.org/sdr/95FDEA01428.md): Duct · failed · Sep 26, 1995 · N322FE · Doug DC1030F · Compressor Bleed Control
  > DURING T/O ROLL, NR 1 ENG N1 IND DROPPED APPROX 10 PERCENT. ADJUSTED THROTTLE TO MATCH N2 AND FUEL FLOW, NO CHANGE NOTED IN N1, EGT IND 910 DEGREES, APPROX 50 DEGREES HIGHER THAN ENG NR 2 AND NR 3. AT APPROX 300 FEET NR 1 FIRE WARNING AND BELL RECEIVED. AC
- [SDR 95FDEA00214](https://openairdocs.org/sdr/95FDEA00214.md): Fire Warning · malfunctioned · Mar 10, 1995 · N322FE · Doug DC1030F · Fire Detection
  > THE APU FIRE LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. IT ALSO ILLUMINATED DURING TAKEOFF OUT OF MEM. FOUND APU FIRE LIGHT ASSY RETAINER PIN MISALIGNED, REMOVED AND REPLACED LIGHT ASSY. OPS CKD GOOD.
- [SDR 95FDEA00005](https://openairdocs.org/sdr/95FDEA00005.md): Duct · failed · Jan 7, 1995 · N322FE · Doug DC1030F · Pneumatic Distribution System
  > ENG FIRE IN NR 2 ENG SHORTLY AFTER ROTATION. OBSERVED EGT REACHED 899 DEG. MEMORY ITEMS ACCOMP, CKLT PROCED COMPLIED WITH, RETURNED TO OAK FOR UNEVENTFUL LANDING (FIRE HANDLE PULLED, BOTTLE NOT DISCHARGED). REPLACED 14TH STAGE LWR CROSSOVER DUCT, LPT COOLIN

## 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 = 'N322FE' AND deregistration_id = 'N322FE-2006-05-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N322FE-2006-05-04/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, except the copies of manufacturers’ service documents, which belong to their rights holders.