# Service difficulty reports: N134FE, cancelled Oct 15, 2002

A list on [N134FE, cancelled Oct 15, 2002](https://openairdocs.org/deregistered/N134FE-2002-10-15.md).

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

- [SDR 00FDEA00007](https://openairdocs.org/sdr/00FDEA00007.md): Warning Light · illuminated · Jan 5, 2000 · N134FE · Boeing 72725C · Hydraulic Pump (Electric/Engine), Main
  > 00-7 - AFTER T/O, NR 1 HYD SYS A PUMP LIGHT FLICKERED. HYD SYS 'A' QUANTITY WENT TO ZERO. REMOVED AND REPLACED BOTH CASE DRAIN FILTERS NO METAL FOUND PER 727-100 MM 29-11-041-2. REMOVED AND REPLACED 'A' SYS RETURN FILTER PER 727-100 MM 29-11-102-2. OPS AND
- [SDR 97FDEA00826](https://openairdocs.org/sdr/97FDEA00826.md): Keel Beam · corroded · Nov 11, 1997 · N134FE · Boeing 72725C · Fuselage Main, Keel
  > WHILE WORKING NR 0091 FOUND CORROSION AT KEEL BEAM VERTICAL FLANGE BS 874, RBL 6.5, WL 142. *S/D* REPAIRED KEEL BEAM VERTICAL FLANGE BS 874, RBL 6.5, WL 142 IAW FED-EX EA 7-5310-36872.
- [SDR 97FDEA00825](https://openairdocs.org/sdr/97FDEA00825.md): Keel Beam · corroded · Nov 11, 1997 · N134FE · Boeing 72725C · Fuselage Main, Keel
  > CORROSION ON KEEL BEAM STR 29 LT, BS 1066, WL 148. *S/D* REPAIRED KEEL BEAM STR 29 LT, BS 1060 TO 1080, WL 148 PER FED-EX EA 7-5310-36873.
- [SDR 97FDEA00796](https://openairdocs.org/sdr/97FDEA00796.md): Fitting · cracked · Oct 31, 1997 · N134FE · Boeing 72725C · Cargo/Baggage Doors
  > AFT CARGO DOOR BOTTOM FWD STOP PIN FITTING IS CRACKED ON THE LOWER FLANGES. *S/D* REMOVED AND INSTALLED NEW AFT CARGO DOOR BOTTOM FORWARD STOP FITTING. ALL WORK DONE IAW FED SRM 51-30-2, 51-30-5 AND FED M/M 51-20-151.
- [SDR 97FDEA00723](https://openairdocs.org/sdr/97FDEA00723.md): Intercostal · cracked · Oct 10, 1997 · N134FE · Boeing 72725C · Cargo/Baggage Doors
  > AFT CARGO DOOR FWD HINGE ARM MOUNT INTERCOSTAL IS CRACKED AT MOUNT UPPER ATTACH BOLT. *S/D* REMOVED FWD HINGE ARM AND INTERCOSTAL. DRILLED REPLACEMENT INTERCOSTAL AND INSTALLED ALL FASTENERS PER FED-EX SRM'S 51-30-2 AND 51-10-1.
- [SDR 97FDEA00715](https://openairdocs.org/sdr/97FDEA00715.md): Beam · cracked · Oct 7, 1997 · N134FE · Boeing 72725C · Cargo/Baggage Doors
  > AFT CARGO DOOR NR 5 TRANSVERSE BEAM HAS TWO CRACKS IN OUTBD RADIUS; ONE APPROX.5 LONG THE OTHER APPROX 1.5 LONG. *S/D* REMOVED AND INSTALLED NEW AFT CARGO DOOR NR 5 TRANSVERSE BEAM WORK DONE IAW FED-EX SRM 51-30-2 AND 51-30-5.
- [SDR 97FDEA00714](https://openairdocs.org/sdr/97FDEA00714.md): Floorbeam · corroded · Oct 7, 1997 · N134FE · Boeing 72725C · Fuselage Main, Floor Beam
  > CORROSION (C53-224-08) ON FLOORBEAM UNDER NUT PLATE BS 1150, LBL 58, WL 208. *S/D* FABRICATED AND INSTALLED REPAIR PARTS FOR FLOORBEAM AT BS 1130, LBL 60, WL 208 PER FED 5710-36882.
- [SDR 97FDEA00713](https://openairdocs.org/sdr/97FDEA00713.md): Skin · corroded · Oct 7, 1997 · N134FE · Boeing 72725C · Fuselage Main, Plate/Skin
  > DURING ROUTINE LFEC INSP, NOTED AREA OF GREATER THAN 10 PERCENT MATERIAL LOSS IN FWD SKIN BS 441 CIRCUMFERENTIAL BUTT SPLICE, BETWEEN STR 3R AND 4R (MARKED IN RED). *S/D* REPLACED SKIN AND REPAIRED LAP TEAR STRAP AND MODIFIED BUT JOINT REPAIR BS 360 TO 480,
- [SDR 97FDEA00706](https://openairdocs.org/sdr/97FDEA00706.md): Bulkhead Web · cracked · Oct 6, 1997 · N134FE · Boeing 72725C · Fuselage Main, Bulkhead
  > EVIDENCE OF A CRACK AT FASTENER FWD SIDE OF BS 178 PRESSURE BULKHEAD WL 236, RBL 10. *S/D* REPAIRED DAMAGED PRESSURE BULKHEAD BS 178, WL 236, RBL 10 PER FED-EX SRM 53-10-9.
- [SDR 97FDEA00705](https://openairdocs.org/sdr/97FDEA00705.md): Shear Tie · cracked · Oct 3, 1997 · N134FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > CRACKED SHEAR TIE AT BS 990 I/B SIDE OF LT KEEL BEAM WL 138. *S/D* REMOVED DAMAGE, FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED PER FED-EX SRM 51-30-02, 53-10-04 AND 51-20-01.
- [SDR 96FDEA01605](https://openairdocs.org/sdr/96FDEA01605.md): Indication · malfunctioned · Oct 24, 1996 · N134FE · Boeing 72725C · Landing Gear Position and Warning
  > ON INITIAL LANDING GEAR EXTENSION, NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. RAN CHECK LIST AFTER GO AROUND ON SECOND EXTENSION INDICATED DOWN AND LOCKED. NOSE GEAR DOOR LIGHT WAS ILLUMINATED FOR AN EXCESSIVELY LONG TIME DURING EXTENSION. INSPECTED NOSE
- [SDR 96FDEA01474](https://openairdocs.org/sdr/96FDEA01474.md): Connector · dirty · Sep 13, 1996 · N134FE · Boeing 72725 · Leading Edge Slat Actuator
  > ON FLAP RETRACTION FROM 2 DEGREES TO 0 DEGREES THE AMBER LEADING EDGE FLAP LIGHT REMAINED ON. SECOND OFFICER'S AUXILIARY PANEL POSITION INDICATOR SHOWED THAT THE NR 7 LEADING EDGE DEVICE WAS INTRANSIT. COMPLETED CHECKLIST FOR LEADING EDGE DEVICE FAILURE ON F
- [SDR 95FDEA00852](https://openairdocs.org/sdr/95FDEA00852.md): Casting · cracked · Jun 21, 1995 · N134FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > LIGHT CORROSION ON HEAVY CARGO DOOR CASTING STA 620 ON UNDERSIDE OF LEG, AFT SIDE OF 620 INCLUDING CORRODED GOUGE. HFEC'D AREA, APPROXIMATELY A 1.50 INCH CRACK, RUNS INTO RADIUS MARKED ENDS. INSTALLED DOUBLER REPAIR PER ESO 11782. INSTALLED DOUBLER PER FED
- [SDR 95FDEA00855](https://openairdocs.org/sdr/95FDEA00855.md): Floorbeam · corroded · Jun 20, 1995 · N134FE · Boeing 72725C · Fuselage Main, Floor Beam
  > FS 344 LBL 6-14 CORROSION ON TOP LEG OF FLOORBEAM. INSTALLED FLOORBEAM CAP PER 53-10-8.
- [SDR 95FDEA00858](https://openairdocs.org/sdr/95FDEA00858.md): Fitting · cracked · Jun 8, 1995 · N134FE · Boeing 72725C · Cargo/Baggage Doors
  > MAIN CARGO DOOR AFT CAM SUPPORT FITTING CRACKED. REPLACED FITTING WITH 65-26680-5 IN PLACE OF ORIGINAL - 3 FITTINGS OBSOLETE PER EA NR 7-5230-25056.
- [SDR 95FDEA00857](https://openairdocs.org/sdr/95FDEA00857.md): Fitting · cracked · Jun 8, 1995 · N134FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > RIGHT STA 870 CRACK ABOVE STR 10 EXTENDING UNDER SPLICE PLATE - AFT SIDE OF 870 FORGING. REPAIRED BS 870 TERMINAL FITTING AS PER BOEING SB 727-53-0.
- [SDR 95FDEA00856](https://openairdocs.org/sdr/95FDEA00856.md): Floor Beam · corroded · Jun 7, 1995 · N134FE · Boeing 72725C · Fuselage Main, Floor Beam
  > CORROSION ON TOP OF LEG ON FLOORBEAM (TOP LEG) STA 480 RBL 18-20. BLENDED OUT CORROSION ON TOP LEG OF FLOORBEAM, BLENDED OUT AREA 2.0 INCHES X.75 INCH WIDE, AT A DEPTH OF.045 INCH EXCEEDING SRM LIMITS. INSTALLED STRAP REPAIR PER ESO 11782 DATED 6-13-95 EA
- [SDR 95FDEA00854](https://openairdocs.org/sdr/95FDEA00854.md): Spar Web · corroded · Jun 7, 1995 · N134FE · Boeing 72725C · Wing Spar
  > CENTER WING BOX AFT SPAR WEB SKIN AT UPPER CHORD HAS FOUR EACH FASTENERS WITH POPPED HEADS AND ONE READY TO POP, TOTAL FIVE. WEB SKIN IS BULGED AT APPROX RBL 50. REMOVED RIVETS AND CUT OUT TOP PORTION OF WEB OUT TO REMOVE CORROSION ON UPPER SPAR. INSTALLED
- [SDR 95FDEA00853](https://openairdocs.org/sdr/95FDEA00853.md): Floor Beam · corroded · Jun 7, 1995 · N134FE · Boeing 72725C · Fuselage Main, Floor Beam
  > FS 360 RBL 19-20. CORROSION ON FLOORBEAM AROUND FLOORBOARD ATTACH SCREW HOLE. REPAIRED PER AA ESO 11782 FEDEX EA NR 7-5310-25029.
- [SDR 95FDEA00851](https://openairdocs.org/sdr/95FDEA00851.md): Floor Beam · corroded · Jun 7, 1995 · N134FE · Boeing 72725C · Fuselage Main, Floor Beam
  > CORROSION ON TOP OF FLOORBEAM AROUND FLOORBOARD ATTACH SCREW HOLE, BS 360 RBL 20-22. BLENDED OUT CORROSION ON TOP LEG OF FLOORBEAM. BLEND OUT AREA IS 2.0 INCHES X 1.0 INCH X.075 INCH DEEP, PER SRM 51-10-6 GUIDELINES. INSTALLED REPAIR STRAP PER ESO 11782 DA
- [SDR 95FDEA00850](https://openairdocs.org/sdr/95FDEA00850.md): Fitting · cracked · Jun 6, 1995 · N134FE · Boeing 72725C · Cargo/Baggage Doors
  > UPPER LOBE CARGO DOOR: CARGO DOOR AFT CAM SUPPORT FITTING CRACKED BETWEEN 2ND AND 3RD RIVET IN WEB AT INBD ROW OF FASTENERS. REMOVED AND REPLACED CASTING PER ESO 11782 FEDEX EA NR 7-5230-25056.

## 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 = 'N134FE' AND deregistration_id = 'N134FE-2002-10-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N134FE-2002-10-15/reports

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