# Service difficulty reports: N155FE, cancelled Oct 15, 2002

A list on [N155FE, cancelled Oct 15, 2002](https://openairdocs.org/deregistered/N155FE-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.

Page 1 of 2 · 62 reports

- [SDR 01FDEA00931](https://openairdocs.org/sdr/01FDEA00931.md): Hydraulic System · leaking · Oct 26, 2001 · N155FE · Boeing 72725 · Hydraulic System, Main
  > A-SYS QUANTITY DECREASING. SERVICED A-HYD SYS, NO LEAKS NOTED. OK FOR SERVICE.
- [SDR 00FDEA00125](https://openairdocs.org/sdr/00FDEA00125.md): Hinge · cracked · Feb 29, 2000 · N155FE · Boeing 72725 · Wing, Control Surface Attach Fittings
  > LEFT WING OTBD ATTACH FITTING (HINGE HALF) FOR THE INBD AILERON IS CRACKED. REMOVED AND REPLACED PER IAW SRM 51 -30-2.
- [SDR 99FDEA00056](https://openairdocs.org/sdr/99FDEA00056.md): Switch · inoperative · Feb 10, 1999 · N155FE · Boeing 72725 · Landing Gear Retraction/Extension System
  > NO NOSE GEAR IND IN DIM POS WHEN SEL GEAR DOWN. REMOVED AND REPLACED S96 NOSE LANDING GEAR LOCK SWITCH REF THE FX72ING GEAR LOCK PINS.
- [SDR 98FDEA00615](https://openairdocs.org/sdr/98FDEA00615.md): Line · failed · Oct 2, 1998 · N155FE · Boeing 72725 · Hydraulic System, Main
  > 98-241 COMPLETE LOSS OF SYS A IN FLT PRESS AND QUAN ZERO UNTIL GEAR CRANK DOWN. PER CONVERSATION WITH CREW 0 QUAN. LOW PRESS LIGHTS CAME ON. CREW SHUT OFF PUMP WITH 1000 PSI SHOW ON GAGE. REMOVED AND REPLACED PRESS LINE, NR 1 AND 2 ENG CASE DRAIN FILTER M
- [SDR 97FDEA00641](https://openairdocs.org/sdr/97FDEA00641.md): Light · defective · Sep 9, 1997 · N155FE · Boeing 72725 · Emergency Lighting
  > FWD ENTRY EMERGENCY EXIT LIGHT ILLUMINATED WITH SWITCH POSITION IN OFF AND PWR IS REMOVED FROM A/C. *S/D* REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PER FED-EX M/M 33-50-101.
- [SDR 97FDEA00628](https://openairdocs.org/sdr/97FDEA00628.md): Flap · delaminated · Sep 3, 1997 · N155FE · Boeing 72725 · Trailing Edge Flaps
  > RT WING O/B MIDFLAP HAS TWO AREAS OF DELAMINATION ON UPPER SURFACE OF T/E WEDGE. * S/D* REMOVED AREAS OF DELAMINATION FROM RT WING O/B MIDFLAP AND REPAIRED IAW FED-EX SRM 51-40-06.
- [SDR 97FDEA00620](https://openairdocs.org/sdr/97FDEA00620.md): Flap · delaminated · Sep 2, 1997 · N155FE · Boeing 72725 · Trailing Edge Flaps
  > RT WING INBD FOREFLAP DELAMINATED 96 FROM INBD END. *S/D* REMOVED 8 BY 8 AREA OF DELAMINATION. REPAIRED PER FED-EX SRM 51-40-06.
- [SDR 97FDEA00602](https://openairdocs.org/sdr/97FDEA00602.md): Skin · corroded · Sep 2, 1997 · N155FE · Boeing 72725 · Wing, Plate/Skin
  > CORROSION (C53-224-05) ON UPPER FUEL CELL SKIN BS 850 TO 865, LBL 46 TO 67, WL 190. CORROSION APPEARS TO RUN UNDER 850 STUB BEAM AND 70.5 AND CHORD. * S/D* REMOVED CORROSION FOUND TO BE WITHIN LIMITS. FLAP PEENED AREA. ALODINED AND PRIMED AREA.
- [SDR 96FDEA01518](https://openairdocs.org/sdr/96FDEA01518.md): Switch · inoperative · Sep 21, 1996 · N155FE · Boeing 72725 · Landing Gear Position and Warning
  > WHEN PUTTING GEAR DOWN, NOSE GEAR DOOR LIGHT INOPERATIVE. REMOVED AND REPLACED NOSE LANDING GEAR LOCK SWITCH IN ACCORDANCE WITH MAINTENANCE MANUAL 32-61-21 PAGE 404, TESTED GOOD PER 32-61-21 PAGE 502.
- [SDR 96FDEA01517](https://openairdocs.org/sdr/96FDEA01517.md): Switch · inoperative · Sep 20, 1996 · N155FE · Boeing 72725 · Landing Gear Position and Warning
  > DURING APPROACH, GREEN NOSE GEAR LIGHT EXTINGUISHED AFTER THREE GREEN GEAR INDICATIONS WERE OBTAINED, NO RED UNSAFE LIGHTS CAME ON. GEAR WAS RECYCLED, SAFE INDICATOR WAS OBTAINED AND VISUALLY CHECKED. REMOVED AND REPLACED NG DOWN AND LOCK POSITION SWITCH, CH
- [SDR 95FDEA00455](https://openairdocs.org/sdr/95FDEA00455.md): Seat Track · corroded · Apr 26, 1995 · N155FE · Boeing 72725 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION (72C235-02) ON SEAT TRACK BS 496 RBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 480 TO 510 RBL 25 WL 208 PER FEDEX SRM 53-10-05 AND 53-10-01.
- [SDR 95FDEA00498](https://openairdocs.org/sdr/95FDEA00498.md): Frame · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Frame
  > FRAME IS CRACKED AT BS 804 WL 209 LBL 67 TO 71.REMOVED AND REPLACED FRAME SECTION AT BS 804 LBL 67 TO 71 WL 199 TO 31.
- [SDR 95FDEA00497](https://openairdocs.org/sdr/95FDEA00497.md): Terminal Fitting · corroded · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > SUSPECT INDICATIONS FOUND AT BS 870 L/T TERMINAL FITTING DURING UT INSP, REQUIRES REMOVAL OF FWD AND AFT SPLICE PLATES TO VERIFY INDICATIONS WITH HFEC. REPAIRED BS 870 TERMINAL FITTING LT IAW FEDEX EA 7-5310-24490 AND 7-5310-24491.
- [SDR 95FDEA00496](https://openairdocs.org/sdr/95FDEA00496.md): Doubler · crack · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > R/T NR 2 WINDOW HAS A CRACK IN THE UPPER QUADRANT OF THE UPPER AFT RADIUS IN THE DOUBLER, CRACK IS NOT CONTAINED. REPAIRED CRACK IN UPPER AFT RADIUS OF R/T NR 2 WINDOW UPPER QUADRANT PER FEDEX EO 7-5330-7-3354 PT 5.
- [SDR 95FDEA00495](https://openairdocs.org/sdr/95FDEA00495.md): Skin · damaged · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > UPON REMOVAL OF RADOME, FOUND DAMAGE TO SKIN AT BS 177 WL 242 RBL 10 TO LBL 9. REMOVED AND REPLACED SKIN AT BS 177 WL 242 RBL 10 TO LBL 9.
- [SDR 95FDEA00494](https://openairdocs.org/sdr/95FDEA00494.md): Frame · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Frame
  > CRACK INDICATION IN THE FIRST AND SECOND FASTENER HOLES BELOW THE FLOOR IN THE R/T FRAME AT BS 848.5. REPAIRED R/T FRAME AT BS 848.5 IAW FEDEX EA 7-5310-24522.
- [SDR 95FDEA00493](https://openairdocs.org/sdr/95FDEA00493.md): Frame · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Frame
  > CRACK INDICATION IN FIRST HOLE ABOVE FLOOR L/T FRAME BS 760. REPAIRED FRAME AT BS 760 L/T IAW FEDEX EA 7-5310-24533.
- [SDR 95FDEA00492](https://openairdocs.org/sdr/95FDEA00492.md): Frame · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Frame
  > CRACK INDICATION IN SECOND HOLE BELOW FLOOR L/T FRAME AT BS 825. REPAIRED FRAME AT BS 825 L/T IAW FEDEX EA 7-5310-24522.
- [SDR 95FDEA00491](https://openairdocs.org/sdr/95FDEA00491.md): Gusset · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > FRAME GUSSET CRACKED ON INBOARD ROW OF FASTENERS FROM BOTTOM OF GUSSET TO FIRST FASTENER IN ROW STA 825.95, RBL 66.5 WL 197. REMOVED CRACKED FRAME GUSSET AT BS 825 R/T AND INSTALLED NEW GUSSET IAW FEDEX EA 7-5310-24522.
- [SDR 95FDEA00490](https://openairdocs.org/sdr/95FDEA00490.md): Skin · gouged · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > BS 350 BETWEEN STR 22 TO 23R THERE IS A DEEP GOUGE ON EXTERIOR SKIN. REPAIRED GOUGE ON EXTERIOR SKIN IAW FEDEX SRM 53-30-3 FIG 1 LOC BS 350 STR 22 TO 23R.
- [SDR 95FDEA00489](https://openairdocs.org/sdr/95FDEA00489.md): Clip · damaged · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > MECHANICAL DAMAGE ON STR CLIP AT BS 828 STR 7R. REMOVED AND REPLACED STR CLIP AT BS 828 STR 7R ALL WORK DONE IAW FEDEX DRAWING 65-163282.
- [SDR 95FDEA00488](https://openairdocs.org/sdr/95FDEA00488.md): Frame · gouged · Apr 25, 1995 · N155FE · Boeing 72725 · Cargo/Baggage Doors
  > MAIN CARGO DOOR AFT FRAME LOWER SECTION IS GOUGED ON INNER RADIUS APPROXIMATELY 75 PERCENT OF MATERIAL THICKNESS, BS 620 LBL 60 WL 218. REPAIRED DAMAGE OF MAIN CARGO DOOR AFT FRAME LOWER SECTION ON INNER RADIUS AT BS 620, LBL 60 WL 218 IAW EA 7-5230-24523.
- [SDR 95FDEA00487](https://openairdocs.org/sdr/95FDEA00487.md): Frame · damaged · Apr 25, 1995 · N155FE · Boeing 72725 · Vertical Stabilizer
  > L/T VERTICAL FIN FRAME AT LBL 11 FIN STA 267 WL 420 UNDER PANEL 9601 HAS A FASTENER THAT HAS PULLED THROUGH. REPAIRED AREA ON L/T VERTICAL FIN FRAME AT LBL 11 FINE STA 267 WL 420 IAW EA 7-5510-24465.
- [SDR 95FDEA00486](https://openairdocs.org/sdr/95FDEA00486.md): Stiffener · corroded · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > CORROSION ON HORZ STIFFENER HORIZ FLANGE AT BS 294.5 TO 15 INCHES LBL 10 TO RBL 10 WL 182. REMOVED AND REPLACED HORIZONTAL STIFFENER AT BS 294.5 LBL 10 TO RBL 10 WL 183.
- [SDR 95FDEA00485](https://openairdocs.org/sdr/95FDEA00485.md): Skin · gouged · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > BS 360 STR 246 THERE IS A GOUGE ON EXTERIOR SKIN. FOUND GOUGE TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. REPAIRED DAMAGED AREA AT BS 360 STR 246 IAW FEDEX EO 7-5330-7-23196 PART 5 AND DRAWING 69-62161.
- [SDR 95FDEA00484](https://openairdocs.org/sdr/95FDEA00484.md): Chord · corroded · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > BS 259 WL 172 LBL 27 CHORD CORRODED. REMOVED CORROSION ON CHORD, OUT OF LIMITS PER FEDEX SRM 53-10-1. DRILLED ALODINED PRIMED AND INSTALLED REPAIR STRAP PER FEDEX EA 7-5310-24483.
- [SDR 95FDEA00483](https://openairdocs.org/sdr/95FDEA00483.md): Chord · corroded · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > CORROSION (72C235-02) ON FLOORBEAM AT BS 620 LBL 31 AND LBL 42 WL 208 AND RBL 10-13. REMOVED AND REPLACED FLOORBEAM UPPER CHORD AT BS 620 RBL 35 TO LT OUTBOARD END. FABRICATED CHORD AND REPLACED AS PER FEDEX SRM 53-10-8.
- [SDR 95FDEA00482](https://openairdocs.org/sdr/95FDEA00482.md): Floorbeam · corrosion · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION (72C235-02) UNDER FLANGE OF FLOORBEAM BS 480 LBL 27, 43 AND RBL 48 WL 208. REMOVED CORROSION, DETERMINED TO BE OUT OF LIMITS. REPAIRED AFFECTED AREAS PER EA 7-5310-24479.
- [SDR 95FDEA00481](https://openairdocs.org/sdr/95FDEA00481.md): Floorbeam · corroded · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION (72C235-02) ON 312 FLOORBEAM WL 208 LBL 3, 23 AND 48. CORROSION FOUND BEYOND LIMITS. REPLACED FLOORBEAM BS 312 WL 208 RBL 4.5 TO LBL 55 PER EA 7-5310-24463.
- [SDR 95FDEA00480](https://openairdocs.org/sdr/95FDEA00480.md): Floorbeam · corroded · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION AROUND FLOORBOARD FASTENER HOLES ON UNDERSIDE OF THE FLOORBEAM AT STA 1110 RBL 9 TO RBL 44. FOUND CORROSION BEYOND LIMITS. REPAIRED 1110 FLOORBEAM PER EA 7-53-10-24462.
- [SDR 95FDEA00479](https://openairdocs.org/sdr/95FDEA00479.md): Stringer · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > CRACKED STR 6L AT BS 990 WL 288. REPAIRED STR 6L AT BS 990 WL 288 PER FEDEX SRM 53-10-3.
- [SDR 95FDEA00478](https://openairdocs.org/sdr/95FDEA00478.md): Track · corroded · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BS 559 LBL 45 WL 208 AND BS 620 TO 628. ALSO, BS 641 AND 601. REPLACED SECTION OF SEAT TRACK FROM BS 550 TO 650 LBL 45 WL 208 IAW FEDEX SRM 53-10-5.
- [SDR 95FDEA00477](https://openairdocs.org/sdr/95FDEA00477.md): Floorbeam · corrosion · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION IN THE FWD CARGO BAY THERE IS CORROSION ON LOWER FLANAGE OF FLOORBEAM AT NUTPLATE LOCATION BS 660 RBL 14 WL 200. BLENDED AND REMOVED CORROSION ON FLOORBEAM, ORIGINAL THICKNESS OF MATERIAL 133 REMOVED.027 5 BY 1 AREA, FLOORBEAM, OUT OF LIMITS PER FE
- [SDR 95FDEA00476](https://openairdocs.org/sdr/95FDEA00476.md): Skin · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > CORROSION AND GOUGE ON SKIN BS 1183 TO 1342 STR 20 TO 27L. REMOVED CORROSION FROM SKIN AND INSTALLED DOUBLER OVER AREA WHERE SKIN WAS REMOVED DUE TO GOUGE. IAW FEDEX SRM 53-30-3.
- [SDR 95FDEA00475](https://openairdocs.org/sdr/95FDEA00475.md): Web · corroded · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > CORROSION UNDER WEB 254 TO 259 RBL 48 WL 224. REMOVED CORRODED DOUBLER STA 254 TO 259 RBL 48 WL 224, FABRICATED NEW DOULBER, ALODINED, PRIMED, INSTALLED.
- [SDR 95FDEA00474](https://openairdocs.org/sdr/95FDEA00474.md): Seat Track · corroded · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSIN ON SEAT TRACK BS 48 RBL 45 WL 208. ALSO, AT BS 578 RBL 45 SHEARED FASTENER AT 480 RBL 45. REMOVED AND REPLACED SEAT TRACK AT RBL 45, WL 208 BS 480 TO 580 IAW FEDEX SRM 53-10-5. ALSO, REPLACED SHEARED FASTENER AT RBL 45, BS 480 REINSTALL AND REMOVED
- [SDR 95FDEA00473](https://openairdocs.org/sdr/95FDEA00473.md): Stiffener · corroded · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > BS 254 WL 173, RBL 25 HORIZONTAL STIFFENER IS CORRODED. BLENDED OUT AND REMOVED CORROSION, CUT AND TRIMMED OFF FLANGE. FABRICATED A NEW REPAIR PART, ALODINED, PRIMED, PAINTED PART, INSTALLED PART WET WITH SEALANT. ALL WORK ACCOMPLISHED IAW FEDEX (EA 7-5310-
- [SDR 95FDEA00472](https://openairdocs.org/sdr/95FDEA00472.md): Hinge · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Ailerons
  > RT WING O/B AILERON, OTBD CENTER HINGE FITTING CRACKED. REMOVED CRACKED FITTING, INSTALLED NEW FITTING.
- [SDR 95FDEA00471](https://openairdocs.org/sdr/95FDEA00471.md): Skin · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > BS 251.6 STR 22R, POSSIBLE CRACK IN SKIN AT FASTENER. REPAIRED CRACK IN SKIN PER FEDEX SRM 53-30-3 BS 251.6 STR 22R.
- [SDR 95FDEA00470](https://openairdocs.org/sdr/95FDEA00470.md): Frame · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Frame
  > CRACKED FRAME AT BS 1090 LBL 22 UNDER FLOOR TO SIDEWALL SUPPORT WL 150. REPAIRED CRACKED FRAME PER FEDEX SRM 51-40-3.
- [SDR 95FDEA00469](https://openairdocs.org/sdr/95FDEA00469.md): Blkhd Web · carcked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Bulkhead
  > CRACK IN 950 BULKHEAD RBL 22 WL 183. REPAIRED CRACK IN 950 BULKHEAD RBL 22 WL 183 PER FEDEX SRM 53-10-9.
- [SDR 95FDEA00468](https://openairdocs.org/sdr/95FDEA00468.md): Blkhd Web · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Bulkhead
  > CRACK IN 950 BULKHEAD RBL 22 WL 166. REPAIRED CRACK IN 950 BULKHEAD RBL 22 WL 166 PER FEDEX SRM 53-10-9.
- [SDR 95FDEA00467](https://openairdocs.org/sdr/95FDEA00467.md): Skin · dented · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > BS 460-520 BETWEEN STR 20R TO 21R THERE IS A DENT IN SKIN THAT OIL CANS. CUT OUT DAMAGED AREA FABRICATED REPAIR DOUBLER ALODINE AND PRIMERED, INSTALLED WET WITH SEALANT, INSTALLED FASTENERS IAW FEDEX SRM 53-30-3.
- [SDR 95FDEA00466](https://openairdocs.org/sdr/95FDEA00466.md): Floorbeam · corroded · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION (72C235-02) ON FLOORBEAM AT BS 680 RBL 10 WL 208. REMOVED AND REPLACED TOP CHORD ON FLOORBEAM AT BS 680 LBL 10 TO RB 15, WL 208 PER FEDEX SRM 53-10-8.
- [SDR 95FDEA00465](https://openairdocs.org/sdr/95FDEA00465.md): Skin · lightning strike · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > BS 294.5 BETWEEN STR 24L AND 25L, THERE IS A LIGHTNING STRIKE. BLENDED AREA BS 294.5 BETWEEN STR 24L TO 25L AND FABRICATED DOUBLER, INSTALLED PER FEDEX SRM 53-30-3.
- [SDR 95FDEA00464](https://openairdocs.org/sdr/95FDEA00464.md): Failsafe Chord · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > CRACKED FAILSAFE CHORD BS 1110 STR 24L. REPAIRED CRACKED FAILSAFE CHORD AT BS 1110 STR 24L AS PER FEDEX SRM 51-40-4.
- [SDR 95FDEA00463](https://openairdocs.org/sdr/95FDEA00463.md): Bulkhead · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Bulkhead
  > CRACK IN 950 BULKHEAD LBL 41, WL 182. REPAIRED CRACK IN 950 BULKHEAD AT LBL 41 WL 182 IAW FEDEX 727 SRM 53-10-9.
- [SDR 95FDEA00462](https://openairdocs.org/sdr/95FDEA00462.md): Frame · damaged · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Frame
  > DAMAGED FRAME AT WL 300, STA 1110, STR 2L PLUS 2 INCHES. REMOVED DAMAGED AREA FROM FRAME AT WL 300 STA 1110 STR 2L, FABRICATED AND INSTALLED DOUBLER PER FEDEX SRM 53-10-4 PG 2.
- [SDR 95FDEA00461](https://openairdocs.org/sdr/95FDEA00461.md): Shear Tie · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > CORROSION ON SHEAR TIE BS 1148, LBL 22, WL 153. REMOVE AND REPLACED SHEAR TIE AT BS 1148, LBL 22, WL 153 AS PER FEDEX SRM 53-10-4.
- [SDR 95FDEA00460](https://openairdocs.org/sdr/95FDEA00460.md): Stringer · cracked · Apr 25, 1995 · N155FE · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > CRACKED STR 22L, BS 1030. CUT OUT DAMAGED AREA FABRICATED REPAIR PARTS, INSTALLED REPAIR PARTS NET WITH SEAL AND INSTALLED FASTENERS, ALL WORK DONE IN ACCORDANCE WITH FEDEX SRM 53-10-3 AT BS 1030 STR 22L. MFG P/N M377459, BAC1498132, M424422.

Next page: https://openairdocs.org/deregistered/N155FE-2002-10-15/reports.md?page=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 = 'N155FE' AND deregistration_id = 'N155FE-2002-10-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N155FE-2002-10-15/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.