# Service difficulty reports: N505FE, cancelled Oct 15, 2002

A list on [N505FE, cancelled Oct 15, 2002](https://openairdocs.org/deregistered/N505FE-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 96FDEA01058](https://openairdocs.org/sdr/96FDEA01058.md): Skin · corroded · May 31, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > CORROSION (C53-224-04) ON INSIDE OF SKIN EMANATING FROM WINDOW FRAME AT BS 1094, 4 INCHES ABOVE STR 11L. REMOVED CORROSION FROM WINDOW DOUBLER, FOUND TO BE OUT OF LIMITS. REMOVED CORROSION FROM SKIN AND FRAME FOUND TUBE WITHIN LIMITS. REPAIRED WINDOW FRAME
- [SDR 96FDEA01057](https://openairdocs.org/sdr/96FDEA01057.md): Skin · corroded · May 31, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > CORROSION (C53-224-04) ON INSIDE SKIN EMANATING FROM WINDOW FRAME AT BS 1083 TO 1086 STR 11L. REMOVED CORROSION FROM WINDOW DOUBLER FOUND TO BE OUT OF LIMITS. THE SKIN AND FRAME WERE FOUND TO BE IN LIMITS. REPAIRED DOUBLER PER EA 7-5330-28369.
- [SDR 96FDEA1041](https://openairdocs.org/sdr/96FDEA1041.md): Splice Angle · corrosion · May 29, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > WHILE WORKING NR0488, FOUND CORROSION ON SPLICE ANGLE AFT SIDE BS 870 TERMINAL FITTING, STR 9L. REMOVED SPLICE ANGLE ON AFT SIDE OF BS 870 TERMINAL FITTING STR 9L AND REPLACED PER FEDEX SRM 51-10-1.
- [SDR 96FDEA01040](https://openairdocs.org/sdr/96FDEA01040.md): Angle · corrosion · May 29, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > WHILE WORKING ON NR0488, FOUND CORROSION ON SPLICE ANGLE AT BS 870 TERMINAL FITTING STR 9L FWD SIDE. REMOVED SPLICE ANGLE ON FWD SIDE OF 870 TERMINAL FITTING, STR 9L AND REPLACED PER FEDEX SRM 51-10-1.
- [SDR 96FDEA01009](https://openairdocs.org/sdr/96FDEA01009.md): Skin · corroded · May 20, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > WHILE WORKING NR 0351, FOUND CORROSION IN SKIN LAP BETWEEN BONDED DOUBLER AND LOWER SKIN AT BS 1080 - BS 1110, STR 14L. CUT OUT TO REMOVE CORROSION AND REPAIRED SKIN LAP AT BS 1080 - BS 1110, STR 14L PER FEDEX SRM 53-30-3.
- [SDR 96FDEA01008](https://openairdocs.org/sdr/96FDEA01008.md): Stringer · corroded · May 20, 1996 · N505FE · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR 1, BS 414 - BS 420. COMPLETED REPAIR ON STR 1, BS 414 - BS 420, PER FEDEX SRM 53-10-3.
- [SDR 96FDEA00989](https://openairdocs.org/sdr/96FDEA00989.md): Skin · damaged · May 17, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > CORROSION C53-100-01 SKIN AND DOUBLER BULGING BS 334 - BS 352, LBL 21 - LBL 26, WL 145. REMOVED FASTENERS FROM SKIN, FOUND NO CORROSION UNDER SKIN OR DOUBLER. FABRICATED DOUBLER AND INSTALLED, AND INSTALLED ALL FASTENERS IAW SRM 53-30-03.
- [SDR 96FDEA00985](https://openairdocs.org/sdr/96FDEA00985.md): Stringer · corroded · May 16, 1996 · N505FE · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > CORROSION (C53-224-04) ON STR 3L AT BS 950 TO 985. REMOVED CORRODED SECTION OF STR, FABRICATED AND INSTALLED REPAIR AT BS 950 TO 985 STR 3L IAW SRM 53-10-3.
- [SDR 96FDEA00984](https://openairdocs.org/sdr/96FDEA00984.md): Floor Beam · corroded · May 16, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION BS 312 FLOOR BEAM WL 208 LBL 4 TO 19 AND 30. CORROSION ON FLOOR BEAM FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED NEW BEAM AND REPAIR PARTS AND INSTALLED BS 312 LBL 65 TO RBL 8 WL 208 IAW FEDEX SRM 53-10-8.
- [SDR 96FDEA00983](https://openairdocs.org/sdr/96FDEA00983.md): Seat Track · corrosion · May 15, 1996 · N505FE · Boeing 72725 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 45 CORROSION ON SPLICE AT BS 950 PLUS 10 WL 208. REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SEAT TRACK BS 950 PLUS 10 TO 870 RBL 45 PER FEDEX SRM 53-10-5.
- [SDR 96FDEA00970](https://openairdocs.org/sdr/96FDEA00970.md): Skin · delaminated · May 13, 1996 · N505FE · Boeing 72725 · Horizontal Stabilizer, Tab Structure
  > NR0402 AND 022, RT ELEVATOR TAB T/E O/B CORNER IS DELAMINATED. *S/D* REPAIRED RT ELEVATOR TAB IAW FEDEX SRM 51-40-06 AND 51-80-09.
- [SDR 96FDEA00969](https://openairdocs.org/sdr/96FDEA00969.md): Chord · corrosion · May 13, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR0316 AND 024, CORROSION (C53-224-05) ON THE BS 740 LWR CHORD RBL 15 TO 20 ON VERTICAL FLANGE. *S/D* REMOVED LOWER CHORD, CORROSION WAS OUT OF LIMITS, LOCATED NEW LOWER CHORD, DRILLED, FABRICATED SPLICES, TREATED AND INSTALLED ALL PARTS IAW FEDEX EA 7-5710-
- [SDR 96FDEA00967](https://openairdocs.org/sdr/96FDEA00967.md): Support · corroded · May 13, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > CORROSION (C53-100-01) ON TOP AND BOTTOM FLANGES OF FAIRING SUPPORT CHORD BS 351 LBL TO RBL 17 WL 145 AT VARIOUS LOCATIONS. REMOVED FAIRING SUPPORT CHORD BS 351 LBL TO RBL 17 WL 145 AND REPLACED WITH NEW CHORD PER FEDEX SRM 51-30-2.
- [SDR 96FDEA00966](https://openairdocs.org/sdr/96FDEA00966.md): Stringer · cracked · May 13, 1996 · N505FE · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > CRACK IN THE HORIZONTAL FLANGE OF STR 17R AND BS 849. CUT OUT DAMAGED AREA, FABRICATED FILLER, DOUBLER ANGLES, RADIUS FILLERS, DRILLED UP REPAIR PARTS, ALODINED AND PRIMED AND INSTALLED WET WITH SEAL PER FEDEX SRM 51-40-4.
- [SDR 96FDEA00947](https://openairdocs.org/sdr/96FDEA00947.md): Floor Beam · corroded · May 10, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION BS 360 FLOOR BEAM WL 208 RBL 5. CUT OUT DAMAGED PORTION OF FLOOR BEAM AT BS 360 WL 208 RBL 6 TO LBL 10 AND REPAIRED PER FEDEX SRM 53-10-8.
- [SDR 96FDEA00930](https://openairdocs.org/sdr/96FDEA00930.md): Floor Beam · corroded · May 9, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION (C53-224-01, -1) ON UPPER FLANGE OF FLOOR BEAM BS 680 BETWEEN LBL 9 TO 13 LBL 19 TO 2 RBL 10 WL 208. REMOVED CORRODED UPPER FLANGE OF FLOOR BEAM BS 680 LBL 31.5 TO RBL 12 WL 208. FABRICATED, CLEANED, TREATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM
- [SDR 96FDEA00929](https://openairdocs.org/sdr/96FDEA00929.md): Frame · corroded · May 9, 1996 · N505FE · Boeing 72725 · Fuselage Main, Frame
  > CORROSION (C53-111-01, -2) IN FWD CARGO BAY ON FRAME AT BS 680 RBL 62 WL 196. REMOVED CORRODED AREA OF FRAME AT BS 680 RBL 62 WL 196 AND REPAIRED IAW FEDEX SRM 51-40-3.
- [SDR 96FDEA00926](https://openairdocs.org/sdr/96FDEA00926.md): Stringer Tie · damaged · May 8, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > MECHANICAL DAMAGE ON STR EXTENSION ON BOTH SIDES OF THE BS 950 FORGING AT STR 8L. REMOVED AND REPLACED STR EXTENSION ON BOTH SIDES OF THE BS 950 FORGING AT STR 8L.
- [SDR 96FDEA00925](https://openairdocs.org/sdr/96FDEA00925.md): Floor Panel · corrosion · May 8, 1996 · N505FE · Boeing 72725 · Fuselage Floor Panel
  > NR0420 AND 016, CORROSION (C53-221-01) ON FLOOR PANEL UNDER WIRE BUNDLE ON RT SIDE OF CENTER CONSOLE BS 200 TO 288 WL 208 RBL 4 TO 12.
- [SDR 96FDEA01016](https://openairdocs.org/sdr/96FDEA01016.md): Tear Strap · corrosion · May 7, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR0564 -032C, WHILE WORKING NRO498 DISCOVERED CORROSION IN BETWEEN BONDED DOUBLER AND OVERLAPPED SKIN BS 418 TO 464 STR 4R. ACCESSED REPAIR AREA, FOUND BONBED TEAR STRAP CORRODED BEYOND LIMITS. REMOVED FABRICATED AND INSTALLED BONDED TEAR STRAP, REINSTALLED
- [SDR 96FDEA00921](https://openairdocs.org/sdr/96FDEA00921.md): Stringer · cracked · May 7, 1996 · N505FE · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > NR0099 AND 011, STR 20R CRACKED AT EQUIPMENT COOLING DUCT CLAMP AREA AT STA 359.
- [SDR 96FDEA00920](https://openairdocs.org/sdr/96FDEA00920.md): Skin · corroded · May 7, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > NR0496 AND 013, CORROSION BETWEEN SKIN AND BONDED DOUBLER AT BS 360 STR 5 TO 6R.
- [SDR 96FDEA00919](https://openairdocs.org/sdr/96FDEA00919.md): Skin · corroded · May 7, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > NR0498 AND 014, BOND DEGREGATION IN THE FORM OF CORROSION AT BS 441 BETWEEN STR 14 TO 15R, 3.5 BY.3 AREA MARKED. FOUND CORROSION TO BE OUT OF LIMITS. CUT OUT DAMAGE SECTION AT BS 441 RT, FABRICATED REPAIR PARTS AND INSTALLED AND SEALED PER FEDEX EO 753330-
- [SDR 96FDEA00907](https://openairdocs.org/sdr/96FDEA00907.md): Beam · cracked · May 6, 1996 · N505FE · Boeing 72725 · Passenger/Crew Doors
  > FORWARD ENTRY DOOR LOWER GATE BEAM IS CRACKED IN LOWER FORWARD STOP PIN FITTING. REPAIRED FORWARD ENTRY DOOR LOWER GATE BEAM IAW FEDEX EA 7-5210-28328.
- [SDR 96FDEA00906](https://openairdocs.org/sdr/96FDEA00906.md): Skin · damaged · May 6, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN HOLE IN SKIN BS 1178 AT STR 22L. REMOVED DAMAGED SKIN AT BS 1178, STR 22L AND INSTALLED REPAIR DOUBLER AND FILLER. ALL WORK DONE PER FEDEX SRM 53-30-3.
- [SDR 96FDEA00895](https://openairdocs.org/sdr/96FDEA00895.md): Stringer · corroded · May 6, 1996 · N505FE · Boeing 72725 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR 1 BS 414 TO 420. *S/D* COMPLETED REPAIR ON STR 1 BS 414 TO 420 PER FED EX SRM 53-10-3.
- [SDR 96FDEA01089](https://openairdocs.org/sdr/96FDEA01089.md): Web · cracked · May 4, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > WHILE WORKING NR0316, FOUND HOLE TO BE CRACKED UNDER STIFFENER AT BS 740 WEB LBL 55 WL 185. REMOVED BS 740 WEB AND INSTALLED NEW BS 740 WEB PER FEDEX DRAWING 64-18333 AND EA 7-5710-28401.
- [SDR 96FDEA00903](https://openairdocs.org/sdr/96FDEA00903.md): Floor Beam · corrosion · May 4, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR0533 AND 009, CORROSION (C53-224-01, -1) ON UPPER FLANGE FLOOR BEAM PREVIOUS REPAIR BS 620 BETWEEN LBL 22 TO RBL 11 WL 208. *S/D* REMOVED CORRODED UPPER FLANGE FLOORBOARD PREVIOUS REPAIR BS 620 BETWEEN LBL 22 TO RBL 11, WL 208. FABRICATED NEW CHORD AND RE
- [SDR 96FDEA00902](https://openairdocs.org/sdr/96FDEA00902.md): Floor Beam · corroded · May 4, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR0469 AND 008, CORROSION AT BS 344 FLOOR BEAM LBL 40 TO RBL 15 WL 208. ACCOMPLISHED FLOOR BEAM REPAIR AT BS 344 LBL 40 TO RBL 15 WL 208 PER FED EX DRW SR 27-53-007.
- [SDR 96FDEA00897](https://openairdocs.org/sdr/96FDEA00897.md): Act Bracket · cracked · May 3, 1996 · N505FE · Boeing 72725 · Leading Edge Slat Actuator
  > NR 0089 AND NR 002, NR 2 K-FLAP ACTUATOR AFT I/B MOUNT IS CRACKED AT UPPER FWD CORNER. ****S/D ****** COMING. REMOVED AND REPLACED NR 2 K-FLAP ACTUATOR APT I/B MOUNT IAW FEDEX SRM 51-10-1 AND 51-30-2.
- [SDR 96FDEA00896](https://openairdocs.org/sdr/96FDEA00896.md): Floor Beam · corroded · May 3, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR 0514 AND 003, CORROSION C53-224-01(1) ON UPPER FLANGE OF FLOOR BEAM BS 640 BETWEEN RBL 14 - 43, WL 208. *****S/D***** COMING.
- [SDR 96FDEA00894](https://openairdocs.org/sdr/96FDEA00894.md): Skin · damaged · May 3, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > NR0438 AND 005, EXTERNAL SKIN HOLE IN SKIN BS 1178 AT STR 22L. *S/D* REMOVED DAMAGED SKIN AT BS 1178 STR 22L AND INSTALLED REPAIR DOUBLER AND FILLER. ALL WORK DONE PER FEDEX SRM 53-30-3.
- [SDR 96FDEA00893](https://openairdocs.org/sdr/96FDEA00893.md): Floor Beam · corroded · May 3, 1996 · N505FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR0481 AND 006, CORROSION (C53-224-01) ON BS 560 FLOOR BEAM AT LBL 36 TO 7, RBL 8 WL 208. *S/D* REMOVED CORRODED FLOOR BEAM UPPER FLANGE AT LBL 43.5, RBL 13.5 WL 208. FABRICATED REPAIR PARTS, CLEANED AND TREATED, FASTENED INTO PLACE IAW FEDEX SRM 53-10-8.
- [SDR 96FDEA01088](https://openairdocs.org/sdr/96FDEA01088.md): Fitting · cracked · May 1, 1996 · N505FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > ON INSPECTION OF BS 870 TERMINAL FITTING LT ROW, 2 NOTED CRACK INDICATIONS IN 2ND AND 3RD HOLE FROM TOP. REMOVED EXISTING REPAIR, REMOVED EXISTING FASTENERS IN REPAIR AREA, STOP DRILLED CRACK, BLENDED CORROSION, FABRICATED REPAIR PARTS, TREATED MATERIAL, INST
- [SDR 96FDEA01087](https://openairdocs.org/sdr/96FDEA01087.md): Skin · corroded · May 1, 1996 · N505FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > BOND DEGRADATION IN THE FORM OF CORROSION AT BS 441 STR 15 AND 16L,.4 BY 8 AREA MARKED. ALSO, BETWEEN STR 17 AND 18L,.3 BY 2 AREA MARKED. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED CORRODED SECTION OF SKIN AND REPAIRED PER FEDEX EA 7-5330-29115 EA 7-531
- [SDR 96FDEA01086](https://openairdocs.org/sdr/96FDEA01086.md): Frame · cracked · Apr 30, 1996 · N505FE · Boeing 72725 · Fuselage Main, Frame
  > STA 783.95 RBL 65 WL 202 WHILE WORKING CARD 7-5310-7-33678 PT 4, FOUND A CRACK ON INSIDE FRAME WEB, STARTING FROM FASTENER HOLE, BOTTOM AFT SIDE OF FRAME. REMOVED EXISTING FASTENERS FABRICATED REPAIR PARTS DRILLED AND TREATED MATERIAL PLUGGED REQUIRED FASTENE

## 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 = 'N505FE' AND deregistration_id = 'N505FE-2002-10-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N505FE-2002-10-15/reports

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