# Service difficulty reports: N153FE, cancelled Dec 4, 2006

A list on [N153FE, cancelled Dec 4, 2006](https://openairdocs.org/deregistered/N153FE-2006-12-04.md).

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

- [SDR 97FDEA00379](https://openairdocs.org/sdr/97FDEA00379.md): Light · inoperative · Jul 1, 1997 · N153FE · Boeing 72725 · Emergency Lighting
  > FWD ENTRY DOOR EMERGENCY EXIT LIGHT IS INOP. *S/D* REMOVED AND REPLACED FWD ENTRY DOOR EMERGENCY EXIT LIGHT AND PERFORMED OPERATIONAL TEST IAW FED-EX M/M 33-50-101.
- [SDR 97FDEA00378](https://openairdocs.org/sdr/97FDEA00378.md): Hinge · corroded · Jun 23, 1997 · N153FE · Boeing 72725 · Ailerons
  > NR 0328 033 STA-PAE - R/W O/B AILERON CENTER O/B HINGE FITTING ON AIRCRAFT IS CORRODED (REQUIRES AILERON REMOVAL). REMOVED R/W O/B AILERON. REMOVED AND REPLACED R/W O/B AILERON, O/B HINGE FITTING. REINSTALLED R/W O/B AILERON ALL WORK DONE IAW FED-EX M/M 27
- [SDR 97FDEA00377](https://openairdocs.org/sdr/97FDEA00377.md): Light · inoperative · Jun 23, 1997 · N153FE · Boeing 72725 · Emergency Lighting
  > CONTROL CABIN EMERGENCY EXIT LIGHT IS INOP. *S/D* REMOVED AND REPLACED MOUNTING PLATE FOR EMERGENCY EXIT LIGHT ASSY IN COCKPIT IAW FED-EX WDM 33-51-01. PERFORMED SATISFACTORY TEST IAW FED-EX M/M 33-50-0.
- [SDR 97FDEA00363](https://openairdocs.org/sdr/97FDEA00363.md): Hinge · corroded · Jun 23, 1997 · N153FE · Boeing 72725 · Ailerons
  > STA-PAE: RT WING O/B AILERON CENTER O/B HINGE FITTING ON AIRCRAFT IS CORRODED (REQUIRES AILERON REMOVAL). *S/D* REMOVED RT WING O/B AILERON. REMOVED AND REPLACED RT WING O/B AILERON, O/B HINGE FITTING. REINSTALLED RT WING O/B AILERON. ALL WORK DONE IAW F
- [SDR 97FDEA00351](https://openairdocs.org/sdr/97FDEA00351.md): Skin · cracked · Jun 17, 1997 · N153FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > NR 0745, FASTENER HOLE ON EXTERIOR SKIN HAS CRACK INDICATION BS 220, WL 220, LBL 45. *S/D* REPAIRED FASTENER HOLE ON EXTERIOR SKIN AT BS 220, WL 220, LBL 45 PER FED-EX SRM 53-30-3 AND EO 7-5330-7-2338 PT 1.
- [SDR 97FDEA00348](https://openairdocs.org/sdr/97FDEA00348.md): Frame · cracked · Jun 15, 1997 · N153FE · Boeing 72725 · Fuselage Main, Frame
  > NR 0739 031, BS 1253 FRAME IS CRACKED AT LBL 3 TO LBL 5, WL 368 FRAME LOCATED IN NR 2 ENGINE AIR INLET HOUSING. *S/D* REMOVED DAMAGE, FABRICATED REPAIR PARTS, ALODINED AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS BS 1253, LBL 7 TO RBL 2, WL 368 PER FED-EX
- [SDR 97FDEA00334](https://openairdocs.org/sdr/97FDEA00334.md): Chord · corroded · Jun 8, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR 0287 030 CORROSION ON BS 1176 CHORD RBL 2- RBL 42, WL 208. REMOVED AND REPLACED BS 1176 CHORD WL 208 PER FED-EX SRM 51-10-1.
- [SDR 97FDEA00330](https://openairdocs.org/sdr/97FDEA00330.md): Bulkhead Web · cracked · Jun 7, 1997 · N153FE · Boeing 72725 · Fuselage Main, Bulkhead
  > NR 0759 029, NUMEROUS CRACKS IN 950 BULKHEAD WEB, LBL 60, WL 188 TO 199.
- [SDR 97FDEA00321](https://openairdocs.org/sdr/97FDEA00321.md): Door Frame · corroded · Jun 4, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR 0473 027, CORROSION ON DOOR FRAME DOUBLER AT BS 425.
- [SDR 97FDEA00320](https://openairdocs.org/sdr/97FDEA00320.md): Keel Beam · corroded · Jun 4, 1997 · N153FE · Boeing 72725 · Fuselage Main, Keel
  > NR 0117 028, CORROSION ON LT KEEL BEAM AT BS 1055 TO 1065 ON OUTBOARD FLANGE LBL 7.
- [SDR 97FDEA00319](https://openairdocs.org/sdr/97FDEA00319.md): Tension Strap · corrosion · Jun 2, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR 0716 025, WHILE WORKING NR0476, DISCOVERED CORROSION ON WHEEL WELL FWD BULKHEAD TENSION STRAP LBL 25 TO 70.5, RBL 30 TO 70.5 AROUND FASTENERS. *S/D* REPAIRED WHEEL WELL FWD BULKHEAD TENSION STRAP LBL 25 TO 70-5 AND RBL 30 -TO 70.5 PER EA NR 7-5310-34024
- [SDR 97FDEA00317](https://openairdocs.org/sdr/97FDEA00317.md): Stringer · corroded · May 30, 1997 · N153FE · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > NR 0644 024 CORROSION (C53-111-01(3)) ON STRINGER FITTING ON UPPER AND LOWER O/B FLANGE STR 20 LT, BS 1154-1163. REMOVED AND REPLACED STRINGER FITTING STR 20 LT, BS 1154-1163 IAW FED-EX SRM 51-30-2.
- [SDR 97FDEA00315](https://openairdocs.org/sdr/97FDEA00315.md): Stiffener · corroded · May 29, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR 0470 023, CORROSION (C53-111-01) ON WHEEL WELL VERIFIED STIFFENER BS 320, RBL 14, WL 170. *S/D* REMOVED AND REPLACED VERTICAL STIFFENER AT BS 320, RBL 14, WL 170 IAW FED-EX SRM 51-30-2.
- [SDR 97FDEA00310](https://openairdocs.org/sdr/97FDEA00310.md): Floorbeam · corrosion · May 27, 1997 · N153FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR 0633 022, WHILE WORKING NR 0293, UPON REMOVAL OF LAV WALL HAT CHANNEL FOUND MISDRILLED HOLES AND CORROSION AT BS 344, RBL 53, WL 208 AND CORROSION AT BS 344, RBL 36, WL 208. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLED FLOORBEAM TOP CHORD AT BS 344, RBL
- [SDR 97FDEA00305](https://openairdocs.org/sdr/97FDEA00305.md): Floorbeam · corroded · May 25, 1997 · N153FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR 0388 021, CORROSION ON FLOORBEAM BS 360, LBL 5, WL 208. *S/D* REMOVED CORROSION ON FLOORBEAM BS 360, LBL 5, WL 208. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-8.
- [SDR 97FDEA00306](https://openairdocs.org/sdr/97FDEA00306.md): Former · corroded · May 23, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR 0737 020, WHILE ACCESSING RT KEEL BEAM FOUND LOWER SKIN FORMER CHORD TO BE BADLY CORRODED AT RBL 10, WL 140, BS 950. *S/D* REMOVED AND REPLACED SKIN FORMER CHORD IAW FED-EX SRM 51-30-2, 51-10-6, AND FED-EX M/M 51-20-0.
- [SDR 97FDEA00293](https://openairdocs.org/sdr/97FDEA00293.md): Tank Skin · corrosion · May 18, 1997 · N153FE · Boeing 72725 · Fuel Storage
  > NR 0733 019, WHILE WORKING ON (NR0716) FOUND CORROSION ON LOWER TANK, INTERIOR SKIN STA 868 TO 870, RBL 60-LBL 60, WL 139. *S/D* BLENDED AND REMOVED CORROSION, ON LOWER TANK SKIN. FOUND SKIN IS IN LIMITS PER FED-EX 727 SRM 57-30-1 FIG 4. REWORKED SKIN PER
- [SDR 97FDEA00292](https://openairdocs.org/sdr/97FDEA00292.md): Tank Skin · corrosion · May 18, 1997 · N153FE · Boeing 72725 · Fuel Storage
  > NR 0734 018, WHILE WORKING ON (NR0474) FOUND CORROSION ON UPPER CENTER TANK (INTERIOR SKIN) STA 868 TO 870, RBL 60-LBL 60, WL 178. *S/D* BLENDED AND REMOVED CORROSION ON UPPER TANK SKIN. FOUND SKIN IS IN LIMIT PER FED-EX SRM 727, 57-30-1 FIG 4. REWORKED SK
- [SDR 97FDEA00291](https://openairdocs.org/sdr/97FDEA00291.md): Spar Chord · corrosion · May 18, 1997 · N153FE · Boeing 72725 · Wing Spar
  > CORROSION (C53-132-02,1) ON UPPER REAR SPAR CHORD STA 870, RBL 65, LBL 65, WL 178. *S/D* REMOVED AND REPLACED UPPER SPAR CHORD STA 870, RBL 65, LBL 65, WL 178 PER FED-EX NR 7-5710-34044.
- [SDR 97FDEA00290](https://openairdocs.org/sdr/97FDEA00290.md): Spar Chord · corroded · May 18, 1997 · N153FE · Boeing 72725 · Wing Spar
  > NR 0476 016, CORROSION (SPEC C53-132-02,1) ON STA 870 LOWER REAR SPAR CHORD RBL 25, LBL 25, WL 138. *S/D* REMOVED DAMAGED LOWER REAR SPAR CHORD FROM RBL 70 TO LBL 70, WL 138, BS 870 AND INSTALLED NEW LOWER CHORD PER FED-EX EA 7-5710-34044.
- [SDR 97FDEA00289](https://openairdocs.org/sdr/97FDEA00289.md): Bulkhead Web · corrosion · May 18, 1997 · N153FE · Boeing 72725 · Fuselage Main, Bulkhead
  > NR 0475 015, CORROSION (SPEC C53-132-02,1) ON STA 870 BULKHEAD WEB RBL 65 TO LBL 65, WL 178. *S/D* REMOVED DAMAGED BULKHEAD STA 870, WEB RBL 65 TO LBL 65 AND INSTALLED NEW WEB PER FED-EX EA 7-5710-34044.
- [SDR 97FDEA00284](https://openairdocs.org/sdr/97FDEA00284.md): Keel Beam · corroded · May 17, 1997 · N153FE · Boeing 72725 · Fuselage Main, Keel
  > NR 0116 014, CORROSION ON RT KEEL BEAM AT BS 973, RBL 7, WL 138. *S/D* REMOVED AND REPLACED RT KEEL BEAM AT BS 960, RBL 17, WL 138 IAW SB 727-53-0179.
- [SDR 97FDEA00286](https://openairdocs.org/sdr/97FDEA00286.md): Floorbeam · corroded · May 15, 1997 · N153FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR 0621 013, WHILE WORKING NR 0440 FOUND CORROSION ON FLOORBEAM BS 560, RBL 45, WL 208 UNDER SEAT TRACK. *S/D* REMOVED CORROSION AT BS 560, RBL 45, WL 208 ON FLOORBEAM UNDER SEAT TRACK FOUND TO BE OUT OF LIMITS IAW 727 FED-EX SRM 53-10-02. REPAIRED DAMAGED
- [SDR 97FDEA00280](https://openairdocs.org/sdr/97FDEA00280.md): Chord · corroded · May 14, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR 0471 008, CORROSION (C53-111-01) ON LT MID NOSE CHORD HORIZONTAL FLANGE LOWER SIDE BS 294 TO 350 LBL 15 WILL REQUIRE REMOVAL OF THE FLOOR WEB AND A/C DUCTING TO GAIN ACCESS. *S/D* REMOVED AND REPLACED LT MID NOSE CHORD BS 294 TO 350, WL 169, LBL 15 FED-EX
- [SDR 97FDEA00277](https://openairdocs.org/sdr/97FDEA00277.md): Frame · corroded · May 14, 1997 · N153FE · Boeing 72725 · Fuselage Main, Frame
  > NR 0465 011, FWD CARGO BS 560 TO STR 22L, FRAME CORRODED UNDER SIDEWALL SUPPORT CH. *S/D* MECHANICALLY REMOVED CORROSION BS 560, STR 22L ON AREA OF 1 BY 1.0397. REMOVED.008 FROM.056 MATERIAL. OUT OF LIMITS PER SRM 53-10-4. REPAIRED FRAME IAW FED-EX SRM
- [SDR 97FDEA00279](https://openairdocs.org/sdr/97FDEA00279.md): G-Beam · corroded · May 13, 1997 · N153FE · Boeing 72725 · Fuselage Structure (General)
  > NR 0652 009, WHILE WORKING NR 0506 FOUND CORROSION ON 25 G-BEAM AT BS 266.
- [SDR 97FDEA00278](https://openairdocs.org/sdr/97FDEA00278.md): Floorbeam · corroded · May 13, 1997 · N153FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR 0659 010, CORROSION (C53-111-0, 2) ON LOWER CHORD OF FLOORBEAM BS 600, LBL 18 TO RBL 18, WL 200. *S/D* REPAIRED LOWER CHORD OF FLOORBEAM AT BS 600, LBL 23, RBL 30 IAW FED-EX SRM 53-10-8.
- [SDR 97FDEA00285](https://openairdocs.org/sdr/97FDEA00285.md): Floorbeam · corroded · May 11, 1997 · N153FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR 0390 012, CORROSION (C53-224-02) ON FLOORBEAM BS 620, WL 208, LBL 7 TO LBL 21 AND AROUND NUT PLATE AT LBL 47. *S/D* WHILE REMOVING CORROSION FOUND CRACK IN UPPER CHORD IN EXISTING REPAIR AT LBL 20, STA 620 TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMO
- [SDR 97FDEA00276](https://openairdocs.org/sdr/97FDEA00276.md): Beam · corroded · May 11, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR 0520 005, CORROSION EMANATING FROM UNDER SEAT TRACK ON RBL 24 LONGITUDINAL BEAM BS 760 TO 815, WL 208.1. *S/D* REMOVED AND REPLACED LONGITUDINAL BEAM BS 760 TO 848, RBL 24, WL 208 PER FED-EX SRM 53-10-01.
- [SDR 97FDEA00274](https://openairdocs.org/sdr/97FDEA00274.md): Intercostal · corroded · May 11, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR 0508 007, CORROSION (C53-221-01) ON INTERCOSTAL BETWEEN BS 268 TO 277, LBL 15.
- [SDR 97FDEA00272](https://openairdocs.org/sdr/97FDEA00272.md): Frame · corroded · May 11, 1997 · N153FE · Boeing 72725 · Fuselage Main, Frame
  > NR 0517 004, CORROSION (C53-221-01) ON BS 251.6 FRAME WEB LBL 45, WL 215. *S/D* REPAIRED FRAME WEB AT BS 251.6, LBL 45, WL 215 PER FED-EX SRM 51-40-2 DUE TO CORROSION BEING OUT OF LIMITS PER FED-EX SRM 53-10-1.
- [SDR 97FDEA00271](https://openairdocs.org/sdr/97FDEA00271.md): Intercostal · corroded · May 11, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR 0509 003, CORROSION (C53-221-01) ON INTERCOSTAL BETWEEN BS 259 TO 277, WL 208, LBL 10. *S/D* REMOVED CORROSION ON INTERCOSTAL AT BS 259 TO 277, LBL 10, WL 208. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED, FABRICATED AND REPLACED INTERCOSTA
- [SDR 97FDEA00270](https://openairdocs.org/sdr/97FDEA00270.md): Intercostal · corroded · May 11, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR 0507 002, CORROSION (C53-221-01) ON INTERCOSTAL BETWEEN BS 268 AND 274.
- [SDR 97FDEA00269](https://openairdocs.org/sdr/97FDEA00269.md): Intercostal · corrosion · May 11, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR 0506 001, CORROSION (C53-221-01) ON INTERCOSTAL BETWEEN BS 280 TO 294, RBL 15, WL 208. *S/D* REMOVED AND REPLACED INTERCOSTAL/FLOOR SUPPORT AT BS 277 TO 294, RBL 15, WL 208, DUE TO CORROSION BEING OUT OF LIMITS. WORK PERFORMED IAW FED-EX SRM 53-30-2 AND
- [SDR 97FDEA00322](https://openairdocs.org/sdr/97FDEA00322.md): Beam · corrosion · May 10, 1997 · N153FE · Boeing 72725 · Horizontal Stabilizer Structure
  > NR 0542 026, CORROSION (C55-391-20, 2) RT HORIZONTAL STAB UPPER TIE BEAM HAS AN AREA OF CORROSION 138 FROM INBOARD END LWR FWD SIDE. * S/D* REMOVED AND REPLACED RT HORIZONTAL STAB UPPER TRAILING EDGE BEAM IAW FED-EX SRM 51-30-5.
- [SDR 97FDEA00275](https://openairdocs.org/sdr/97FDEA00275.md): Beam · corroded · May 10, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR 0446 006, CORROSION ON LONGITUDINAL BEAM BS 740 TO 848, LBL 45, WL 208.1. *S/D* REMOVED AND REPLACED LONGITUDINAL BEAM BS 740 TO 848, LBL 45, WL 208.1 IAW FED-EX SRM 51-30-2.

## 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 = 'N153FE' AND deregistration_id = 'N153FE-2006-12-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N153FE-2006-12-04/reports

---
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