# Service difficulty reports: N511FE, cancelled Aug 22, 2013

A list on [N511FE, cancelled Aug 22, 2013](https://openairdocs.org/deregistered/N511FE-2013-08-22.md).

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

- [SDR 99FDEA00245](https://openairdocs.org/sdr/99FDEA00245.md): Web · corroded · Jun 25, 1999 · N511FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > WHILE WORKING NR 0795 FOUND CORROSION NOSE WHEEL WELL HORIZONTAL WEB AND BONDED DOUBLERS AT BS 294 TO BS 309, RBL 13 TO LBL 13, WL 181.
- [SDR 99FDEA00221](https://openairdocs.org/sdr/99FDEA00221.md): Chord · corroded · Jun 15, 1999 · N511FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > CORROSION (C53-224-03) PREVIOUS BLEND ON RT MID NOSE, BS 304-314, RBL 20, WL 170.
- [SDR 99FDEA00220](https://openairdocs.org/sdr/99FDEA00220.md): Floorbeam · corroded · Jun 15, 1999 · N511FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR 639 - WHILE WORK NR 284 FOUND CORROSION ON FLOORBEAM, BS 560, RBL 10-12, WL 208. REPAIRED FLOORBEAM IAW FEDEX SRM 53-10-8 AND 51-30-2.
- [SDR 99FDEA00219](https://openairdocs.org/sdr/99FDEA00219.md): Web · gouged · Jun 15, 1999 · N511FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > FOUND CORROSION (C53-224-03) AND GOUGE ON VERTICAL WEB NEAR RT TRUNNION BOLT HOLE BS 309, RBL 14, WL 169.
- [SDR 99FDEA00218](https://openairdocs.org/sdr/99FDEA00218.md): Frame · cracked · Jun 15, 1999 · N511FE · Boeing 72725 · Fuselage Main, Frame
  > CRACK INDICATION AT BS 970 FRAME, BOTTOM HOLE OF FRAME TO STRINGER 9L.
- [SDR 99FDEA00216](https://openairdocs.org/sdr/99FDEA00216.md): Chord · corroded · Jun 11, 1999 · N511FE · Boeing 72725 · Wing Miscellaneous Structure
  > NR 799 WHILE WORKING NR 246 FOUND WING CTR SECTION LWR CHORD AT BS 870, RBL 16 TO RBL 55 TO BE CORRODED.
- [SDR 99FDEA00215](https://openairdocs.org/sdr/99FDEA00215.md): Web · corroded · Jun 11, 1999 · N511FE · Boeing 72725 · Wing Miscellaneous Structure
  > NR 634 WHILE WORKING NR 246 FOUND BS 870 WING CTR SECTION AFT VERTICAL WEB TO BE CORRODED BEYOND LIMITS.
- [SDR 99FDEA00214](https://openairdocs.org/sdr/99FDEA00214.md): Chord · corroded · Jun 11, 1999 · N511FE · Boeing 72725 · Wing Miscellaneous Structure
  > NR 246 CORROSION (C53-132-02(1)) BETWEEN BS 870 UPPER CHORD AND 870 WEB AT LBL 41.
- [SDR 96FDEA01615](https://openairdocs.org/sdr/96FDEA01615.md): Bulkhead · cracked · Oct 26, 1996 · N511FE · Boeing 72725 · Fuselage Main, Bulkhead
  > NR 0509 024, CRACK ON THE AFT SIDE OF THE 870 BULKHEAD AT RBL 9.5 AND WL 157.
- [SDR 96FDEA01614](https://openairdocs.org/sdr/96FDEA01614.md): Bulkhead · cracked · Oct 25, 1996 · N511FE · Boeing 72725 · Fuselage Main, Bulkhead
  > NR 0507 023, POSSIBLE CRACK ON AFT SIDE OF BS 950 BULKHEAD AT LBL 4 WL 176 AND AT LBL 11, WL 181 TO 184.
- [SDR 96FDEA01583](https://openairdocs.org/sdr/96FDEA01583.md): Floorbeam · corroded · Oct 15, 1996 · N511FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR 0437 AND 022, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY AT BS 1148 LBL 11 TO 23 WL 199 ON FLOORBEAM AT NUTPLATE HOLES. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM AT BS 1148 LBL 11 TO 23 WL 199 IAW FEDEX EA 7-5310-31191.
- [SDR 96FDEA01582](https://openairdocs.org/sdr/96FDEA01582.md): Floorbeam · corroded · Oct 14, 1996 · N511FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR 0609 AND 021, CORROSION (C53-224-01, -3) ON STA 1110 RBL 23 WL 208 UNDER TOP FLANGE OF FLOORBEAM. *S/D* FOUND CORROSION TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR IAW FEDEX EA 7-5310-31193.
- [SDR 96FDEA01577](https://openairdocs.org/sdr/96FDEA01577.md): S-Duct Skin · corroded · Oct 14, 1996 · N511FE · Boeing 72725 · Nacelle/Pylon Structure
  > NR0496 AND 019, CORROSION (C54-451-02) ON INTERIOR SKIN OF S-DUCT AT BS 1201 AT CENTER LINE, MIDDLE OF S-DUCT. *S/D* REMOVED DAMAGED SKIN OF INTERIOR OF S-DUCT AT BS 1201. INSTALLED REPAIR DOUBLER IAW FEDEX 727 SRM 54-10-03.
- [SDR 96FDEA01571](https://openairdocs.org/sdr/96FDEA01571.md): Skin · creased · Oct 8, 1996 · N511FE · Boeing 72725 · Fuselage Main, Plate/Skin
  > NR0145 AND 018, CREASE ON SKIN AT BS 254 STR 20 TO 21R. *S/D* REMOVED DAMAGE FROM SKIN AT BS 254 BETWEEN STR 20 TO 21R, FABRICATED AND INSTALLED REPAIR PER FEDEX SRM 53-30-03.
- [SDR 96FDEA01567](https://openairdocs.org/sdr/96FDEA01567.md): Stiffener · cracked · Oct 8, 1996 · N511FE · Boeing 72725 · Wing Miscellaneous Structure
  > NR0510 AND 017, TOP OF THE VERTICAL STIFFENER IS CRACKED IN THE WING CENTER SECTION AT BS 740 RBL 45. *S/D* REMOVED AND REPLACED VERTICAL STIFFENER IN THE WING CENTER SECTION AT BS 740 RBL 45 IAW FEDEX SRM 51-30-2.
- [SDR 96FDEA01566](https://openairdocs.org/sdr/96FDEA01566.md): Floor Beam · corroded · Oct 7, 1996 · N511FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR0438 AND 016, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY AT BS 1130 LBL 11 TO 13 WL 199 ON FLOORBEAM AT NUTPLATE HOLES. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMGE, FABRICATED REPAIR FILLERS AND ANGLES, INSTALLED IAW FEDEX EA 7-5310-311
- [SDR 96FDEA01563](https://openairdocs.org/sdr/96FDEA01563.md): Floor Beam · corrosion · Oct 4, 1996 · N511FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR0594 AND 015, CORROSION (C53-224-01, -3) AT BS 1110 RBL 43 WL 207 EMITTING FROM UNDER SIDE OF TOP FLANGE OF FLOOR BEAM AT FASTENER HOLE. *S/D* REPAIRED CORROSION DAMAGE ON FLOOR BEAM AT BS 1110 RBL 43 WL 207 PER FEDEX SRM 53-10-8 FIG 8.
- [SDR 96FDEA01557](https://openairdocs.org/sdr/96FDEA01557.md): Floorbeam · corroded · Sep 30, 1996 · N511FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR0440 AND 012, CORROSION (C53-111-01,-3) IN AFT CARGO BAY AT BS1050 LBL TO RBL 20 WL 199 ON FLOOR BEAM AT NUTPLATE HOLES. *S/D* REMOVED CORRODED SECTION OF BS 1050 FLOORBEAM FROM LBL TO RBL 25 LOWER FLANGE. REPAIRED LOWER FLANGE PER FEDEX SRM 53-10-8 FIG 3
- [SDR 96FDEA01553](https://openairdocs.org/sdr/96FDEA01553.md): Bonding Jumper · corroded · Sep 30, 1996 · N511FE · Boeing 72725 · Leading Edge Devices
  > NR0589 AND 010, WHILE WORKING NR0218 FOUND NR 2 K-FLAP I/B BULLNOSE BONDING JUMPER UPPER ATTACH POINT CORRODED. *S/D* REPAIRED PER FEDEX SRM 57-50-3.
- [SDR 96FDEA01552](https://openairdocs.org/sdr/96FDEA01552.md): Floorbeam · corrosion · Sep 28, 1996 · N511FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR0434 AND 009, CORROSION (C53-224-01, -1, -100) AT STA 620 RBL 3 WL 208 ON FRAME FILLER. *S/D* REPAIRED FLOORBEAM AT BS 620 WL 208 RBL 35 TO LBL 24 IAW FEDEX SRM 53-10-8 FIG 3.
- [SDR 96FDEA01551](https://openairdocs.org/sdr/96FDEA01551.md): Skin · delamination · Sep 28, 1996 · N511FE · Boeing 72725 · Trailing Edge Flaps
  > NR0579 AND 008, WHILE WORKING NR0576 FOUND THREE AREAS OF DELAMINATION ON LOWER SURFACE. *S/D* REPAIRED DAMAGED SKIN TO RIGHT I/B FORE FLAP LOWER SURFACE PER FEDEX SRM 51-40-6.
- [SDR 96FDEA01556](https://openairdocs.org/sdr/96FDEA01556.md): Frame · corroded · Sep 27, 1996 · N511FE · Boeing 72725 · Fuselage Main, Frame
  > NR0541 AND 011, FOUND CORROSION (C53-221-01) ON FRAME WEB AND TWO STIFFENERS AFT SIDE OF BS 251.6 RBL 51 WL 215 TO 221. *S/D* REMOVED CORRODED WEB AND STIFFENERS AT BS 251.6 RBL 51 WL 215 TO 221. FABRICATED AND INSTALLED WEB AND STIFFENERS IAW FEDEX SRM 51
- [SDR 96FDEA01584](https://openairdocs.org/sdr/96FDEA01584.md): Skin · cracked · Sep 25, 1996 · N511FE · Boeing 72725 · Ailerons
  > NR 0580 AND 020, CRACK IN L/W O/B AILERON I/B AFT TRAILING EDGE CHORD. *S/D* STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER FEDEX SRM 51-40-3.
- [SDR 96FDEA01535](https://openairdocs.org/sdr/96FDEA01535.md): Skin · delaminated · Sep 25, 1996 · N511FE · Boeing 72725 · Trailing Edge Flaps
  > NR0576 AND 007, RT WING I/B FORE FLAP IS DELAMINATED AT I/B END UPPER SURFACE. *S/D* REPAIRED DAMAGED AREA TO RT WING I/B FORE FLAP PER SRM 51-40-6.
- [SDR 96FDEA01534](https://openairdocs.org/sdr/96FDEA01534.md): Act Mount · cracked · Sep 25, 1996 · N511FE · Boeing 72725 · Leading Edge Slat Actuator
  > NR 0219 AND 006. NR 3 SLAT ACTUATOR ROD END MOUNT I/B AND O/B RIBS ARE CRACKED. ***S/D***** REMOVED AND REPLACED NR 3 SLAT ACTUATOR ROD AND MOUNT I/B AND O/B RIBS ON SLAT.
- [SDR 96FDEA01519](https://openairdocs.org/sdr/96FDEA01519.md): Door Frame · cracked · Sep 21, 1996 · N511FE · Boeing 72725 · Passenger/Crew Doors
  > NR0055, 004, AFT ENTRY DOOR LT SIDE FRAME IS CRACKED AT 41 INCHES FROM BOTTOM OF DOOR.
- [SDR 96FDEA01587](https://openairdocs.org/sdr/96FDEA01587.md): Floorbeam · corroded · Sep 20, 1996 · N511FE · Boeing 72725 · Fuselage Main, Floor Beam
  > CORROSION (C53-111-01, -3) IN AFT CARGO BAY AT BS 1050 LBL 20 TO RBL 20 WL 199 ON FLOORBEAM AT NUTPLATES HOLES. REMOVED CORRODED SECTION OF BS 1050 FLOORBEAM FROM LBL 25 TO RBL 25 WL 199 LOWER FLANGE. REPAIRED LOWER FLANGE PER FEDEX SRM 53-10-8 FIG 3 EA NR 7
- [SDR 96FDEA01562](https://openairdocs.org/sdr/96FDEA01562.md): Floorbeam · corroded · Sep 20, 1996 · N511FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR0435 AND 014, CORROSION (C53-224-01, -3, C53-224-04) STR 9L STA 1130 RBL 25 TO 45 WL 208 UPPER FLANGE. *S/D* FOUND CORROSION TO BE OUT OF LIMITS. REPAIRED FLOORBEAM UPPER FLANGE BS 1130, RBL 25 TO 45 WL 208 IAW FEDEX EA 7-5310-31186.
- [SDR 96FDEA01561](https://openairdocs.org/sdr/96FDEA01561.md): Floorbeam · corroded · Sep 20, 1996 · N511FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR0439 AND 013, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY AT BS 1110 LBL 16 TO 30 WL 199 ON FLOORBEAM AT NUTPLATE HOLES. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. REMOVED CORRODED SECTION AND REPAIRED LOWER FLANGE IAW FEDEX EA 7-5310-31192.
- [SDR 96FDEA01512](https://openairdocs.org/sdr/96FDEA01512.md): Doorway Frame · corroded · Sep 20, 1996 · N511FE · Boeing 72725 · Fuselage Miscellaneous Structure
  > NR0324 AND 003, CORROSION (C53-111-01, -3) IN THE AFT CARGO BAY ON THE FWD SIDE OF THE AFT CARGO DOOR FRAME BS 1110 STR 19R. *S/D* REMOVED DAMAGED AREA ON FRAME AT BS 1110 STR 19R. INSTALLED REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED 2 REPAIR SPLIC
- [SDR 96FDEA01511](https://openairdocs.org/sdr/96FDEA01511.md): Bonding Jumper · corroded · Sep 20, 1996 · N511FE · Boeing 72725 · Leading Edge Devices
  > NR 0214 AND 002. NR 1 K-FLAP TO BULLNOSE INBOARD BONDING JUMPER UPPER AND LOWER ATTACH POINTS ARE CORRODED. REMOVED CORRODED AREAS, BLENDED, AND TREATED UPPER ATTACH POINT. REMOVED DAMAGED AREA ON NR 1 K-FLAP TO BULLNOSE INBOARD BONDING JUMPER AND REPAIRED
- [SDR 96FDEA01513](https://openairdocs.org/sdr/96FDEA01513.md): Floorbeam · corroded · Sep 18, 1996 · N511FE · Boeing 72725 · Fuselage Main, Floor Beam
  > NR0250 AND 001, CORROSION (C53-111-01-2) ON FLOORBEAM LOWER FLANGE AROUND NUTPLATE HOLE AT BS 520 WL 200 RBL 4. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLES AND REPAIR FILLER PER FEDEX SRM 53-10-8 ON

## 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 = 'N511FE' AND deregistration_id = 'N511FE-2013-08-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N511FE-2013-08-22/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.