# Service difficulty reports: N103FE, cancelled Jan 31, 2006

A list on [N103FE, cancelled Jan 31, 2006](https://openairdocs.org/deregistered/N103FE-2006-01-31.md).

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

- [SDR 03FDEA01262](https://openairdocs.org/sdr/03FDEA01262.md): Skin · cracked · Jul 30, 2003 · N103FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > CRACK INDICATED AT BS 441 BETWEEN STR 1L AND 2L.
- [SDR 03FDEA01263](https://openairdocs.org/sdr/03FDEA01263.md): Tab · delaminated · Jul 21, 2003 · N103FE · Boeing 727100 · Rudder, Tab Structure
  > LOWER RUDDER TAB 2FH SIDE UPPER END IS DELAMINATED AT AFT END.
- [SDR 03FDEA01264](https://openairdocs.org/sdr/03FDEA01264.md): Tab · delaminated · Jul 21, 2003 · N103FE · Boeing 727100 · Rudder, Tab Structure
  > LOWER RUDDER TAB 2FH SIDE IS DELAMINATED 13 22 ABOVE PUSH ROD ATTACH FITTING.
- [SDR 03FDEA01267](https://openairdocs.org/sdr/03FDEA01267.md): Skin · cracked · Jul 19, 2003 · N103FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > L 2FH NLG 2F SKIN CRACKED AT STA 242 BELOW PANEL CUTOUT.
- [SDR 03FDEA01266](https://openairdocs.org/sdr/03FDEA01266.md): Flange · cracked · Jul 19, 2003 · N103FE · Boeing 727100 · Fuselage Main, Structure
  > E AND E COMPT STA 420 STR 26R CRACKED AT LWR FLANGE AND BENT AT STA 422. REPAIRED CRACKED STRINGER IAW BOEING 727-100 SRM 53-10-3
- [SDR 03FDEA01269](https://openairdocs.org/sdr/03FDEA01269.md): Skin · cracked · Jul 19, 2003 · N103FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > L 2FH NLG 2F SKIN CRACKED AT STA 242 BELOW PANEL CUT OUT.
- [SDR 03FDEA01265](https://openairdocs.org/sdr/03FDEA01265.md): Skin · cracked · Jul 18, 2003 · N103FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > AFT CARGO COMPT DOOR LOWER BEAM 22 FOR INTERIOR SKIN IS CRACKED BEYOND STOP DRILL AT FWD END.
- [SDR 00FDEA00412](https://openairdocs.org/sdr/00FDEA00412.md): Flap · malfunctioned · Jun 27, 2000 · N103FE · Boeing 72722C · Trailing Edge Flap Control System
  > WHILE CONFIGURING FOR LANDING, FLAP HANDLE AT 25 DEGREES, INBD FLAP INDICATOR (FWD ONE) READ 0. DURING GO-AROUND WHEN FLAPS CONFIGURED TO 15, FWD INBD INDICATOR 15 & ALL INDICATORS WORKED NORMAL. RAN FLAPS THRU SEVERAL CYCLES OPS CHECK GOOD PER 27-52-000-0.
- [SDR 99FDEA00359](https://openairdocs.org/sdr/99FDEA00359.md): Control Valve · failed · Sep 1, 1999 · N103FE · Boeing 72722C · Air Distribution System
  > BURNING SMELL IN COCKPIT AREA AND IN BULKHEAD AREA NEXT TO LAVATORY. REPLACED FLOW CONTROL VALVE PER B727 MM 21-58-021-4. NO FURTHER SMELLS DETECTED. A/C OK FOR SERVICE.
- [SDR 97FDEA00649](https://openairdocs.org/sdr/97FDEA00649.md): Computer · failed · Sep 11, 1997 · N103FE · Boeing 72722C · Stall Warning System
  > 97-0177 ON T/O UPON ROTATION, THE STALL WARN STICK SHAKER ACTIVATED. USED FIREWALL PWR ON ALL 3 ENG FOR APPROX 45 SEC. ALL ENG PARAMETERS AT RED LINE (N1,EGT). REDUCED ENG POWER AND CONTINUED AROUND FOR A NORM LANDING WITH THE STALL WARN STICK SHAKER ACTIVA
- [SDR 96FDEA00771](https://openairdocs.org/sdr/96FDEA00771.md): Floor Beam · corroded · Apr 4, 1996 · N103FE · Boeing 72722C · Fuselage Main, Floor Beam
  > UPPER LOBE, CORROSION BEYOND LIMITS IN DEPTH ON TOP SURFACE OF FLOOR BEAM BS 480, RBL 26 TO 35. CUT OUT AREA OF CORROSION AND INSTALLED FLOOR BEAM REPAIR PER SRM 51-10-6, 51-10-8 FIG 6 AND 8, ESO 11782 DATE 3-20-96 AA AND EA 7-5310-28846 DATED 3-20-96 FEDEX.
- [SDR 96FDEA00770](https://openairdocs.org/sdr/96FDEA00770.md): Stringer · cracked · Apr 2, 1996 · N103FE · Boeing 72722C · Fuselage Main, Longeron/Stringer
  > FUSE STR 25R CRACKED AROUND FASTENER STA 365. FABRICATED AND INSTALLED REPAIR SECTION OF STR 25R, STR 365 PER SRM 53-10-3 PAGE 4C AND E.
- [SDR 96FDEA00769](https://openairdocs.org/sdr/96FDEA00769.md): Bulkhead · ripples · Mar 28, 1996 · N103FE · Boeing 72722C · Fuselage Main, Bulkhead
  > FUSE RIPPLES IN 1183 BULKHEAD AT BOTTOM INSIDE TAIL SKID COMP. REPAIRED RT 1183 BULKHEAD AT TAIL SKID AREA PER ESO 11782 DATED 03-18-96 AND EA NR 7-5310-28179 DATED 3-26-96.
- [SDR 96FDEA00713](https://openairdocs.org/sdr/96FDEA00713.md): Bellframe · dent · Mar 26, 1996 · N103FE · Boeing 72722C · Fuselage Main, Frame
  > UPPER LOBE BS 580 STR 6R DENT IN BELLFRAME. REMOVED DAMAGED SECTION OF BELLFRAME, FABRICATED SECTION OF BELLFRAME, INSTALLED BELLFRAME REPAIR PER SRM 53-10-4 FIG 1.
- [SDR 96FDEA00712](https://openairdocs.org/sdr/96FDEA00712.md): Bellframe · cracked · Mar 25, 1996 · N103FE · Boeing 72722C · Fuselage Main, Frame
  > AFT CARGO COMP FS 1090 BELLFRAME CRACKED IN FLANGE AND INTO WEB IN AREA BETWEEN STR 26 AND 27L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-3.
- [SDR 96FDEA00711](https://openairdocs.org/sdr/96FDEA00711.md): Bulkhead · cracked · Mar 20, 1996 · N103FE · Boeing 72722C · Fuselage Main, Bulkhead
  > AFT CARGO COMPARTMENT FS 1183 BULKHEAD IS CRACKED BL 30 RT, 10 ABOVE STR 26L COMING OUT BEHIND HORIZ STIFFENER. CRACKED AREA OF BULKHEAD REMOVED AND FILLER AND DOUBLER INSTALLED PER BOEING SB 727-53-0215.
- [SDR 96FDEA00709](https://openairdocs.org/sdr/96FDEA00709.md): Floor Beam · corrosion · Mar 19, 1996 · N103FE · Boeing 72722C · Fuselage Main, Floor Beam
  > UPPER LOBE SLAT BS 344 FLOOR BEAM HAS CORROSION FROM RBL 2 TO LBL 54. REMOVED CORRODED BEAM CAP OF FLOOR BEAM AND INSTALLED NEW REPAIR PER SRM 53-10-8.
- [SDR 95FDEA00446](https://openairdocs.org/sdr/95FDEA00446.md): Engine · failed · May 2, 1995 · N103FE · Boeing 72722C · Engine (Turbine/Turboprop)
  > DURING FLT HAD NR 1 LOW OIL PRESS/FILTER BYPASS LIGHT WITH 46 PSI OIL PRESS NR 1 ENG SHUTDOWN AS PER RED TABS. LIGHT CAME ON AT START OF DESCENT. MINOR VIBRATION NOTED DURING FLIGHT, BUT ALL INDICATIONS NORMAL UNTIL LIGHT CAME ON. FOUND METAL IN THE OIL SYS
- [SDR 95FDEA00074](https://openairdocs.org/sdr/95FDEA00074.md): Support · corroded · Jan 23, 1995 · N103FE · Boeing 72721C · Fuselage Miscellaneous Structure
  > 2 CORRODED FASTENERS RBL 40, BS 320, WL 208 UNDERSIDE OF BEAM AND CHORD. ALSO, FOUND FLOOR SUPPORT CORRODED. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT PER BOEING DRAWING 65-26173, FEDEX SRM 51-10-02, 51-30-2 AND MM 51-20-21.

## 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 = 'N103FE' AND deregistration_id = 'N103FE-2006-01-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N103FE-2006-01-31/reports

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