# Service difficulty reports: N675FE

A list on [N675FE](https://openairdocs.org/aircraft/N675FE.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 5 · 248 reports

- [SDR FDEA202307121743](https://openairdocs.org/sdr/FDEA202307121743.md): Fitting · failed · Jul 12, 2023 · N675FE · Airbus A300* · Fuselage Structure (General)
  > CORROSION FOUND IN THE RIB 5 FITTING. REPAIRED PER AIRBUS REPAIR INSTRUCTIONS R57240425
- [SDR FDEA202210252655](https://openairdocs.org/sdr/FDEA202210252655.md): Spar · cracked · Oct 25, 2022 · N675FE · Airbus A300F4605R · Fuselage Main, Structure
  > CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "C" HOLE FOUND CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE CRACKED FASTENER Ï¿½CÏ¿½
- [SDR FDEA202210242646](https://openairdocs.org/sdr/FDEA202210242646.md): Fitting · cracked · Oct 24, 2022 · N675FE · Airbus A300F4605R · Fuselage Main, Attach Fittings
  > CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER HOLE 165 FOUND CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE CRACKED FASTENER HOLE 165
- [SDR FDEA202210242645](https://openairdocs.org/sdr/FDEA202210242645.md): Seat Track · corroded · Oct 24, 2022 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FR54-FR54.2 Y450 SEAT TRACK FOUND HEAVY CORROSION REPLACED THE MAIN DECK FR54-FR54.2 Y450 CORRODED SEAT TRACK WITH A FABRICATED PART PER DWG: A53813127(ISSUE.C00) AND A300-600F SRM51-40-21. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2
- [SDR FDEA202210222640](https://openairdocs.org/sdr/FDEA202210222640.md): Angle · damaged · Oct 22, 2022 · N675FE · Airbus A300F4605R · Cargo/Baggage Doors
  > COMPLY WITH EA 6-5230-T0369311 B P4, MAIN CARGO DOOR LOWER FWD CORNER CONNECTOR CLIP DAMAGE - REWORK, BY REPLACING THE CONNECTION CLIP REPLACED THE MAIN DECK CARGO DOOR LOWER FWD CORNER CONNECTION CLIP WITH A FABRICATED PART PER DWG: A52371130(ISSUE. F)
- [SDR FDEA202210022443](https://openairdocs.org/sdr/FDEA202210022443.md): Door Frame · cracked · Oct 2, 2022 · N675FE · Airbus A300F4605R · Fuselage Main, Structure
  > RH FWD CREW DOOR - FRAME SEGMENT CRACKED AT FR14C ITEM 40 REPLACED RH FWD CREW DOOR CRACKED FRAME SEGMENT AT FR14C WITH A FABRICATED PART PER A300-600F SRM51-40-21 AND DWG: F52181297 (ISSUE.K), F52181299 (ISSUE.G). TRACKING EA 6-5210-T0370794 P1 RAISED AND
- [SDR FDEA202208181996](https://openairdocs.org/sdr/FDEA202208181996.md): Engine · smoke · Aug 18, 2022 · N675FE · Airbus A300F4605R · Engine (Turbine/Turboprop)
  > AT CRUISE WE NOTICED SOME SORT OF SMOKE IN THE COCKPIT. DECLARED EMERGENCY AND DIVERTED TO PIT. NO SMOKE INDICATOR LIGHTS. EMERGENCY DECLARED. NR 1 ENGINE REMOVED AND REPLACE. COALESCER SOCKS REMOVED AND REPLACED & O2 SERVICED. PERFORMED ENGINE RUNS PER JRH,
- [SDR FDEA202204040829](https://openairdocs.org/sdr/FDEA202204040829.md): Diaphragm · damaged · Apr 4, 2022 · N675FE · Airbus A300F4605R · Passenger/Crew Doors
  > R1 DOOR EMERGENCY CYLINDER-DAMPNER FOUND AT 0 PSI. SERVICED R1 DOOR ASSIST BOTTLE IAW AMM 52-10-14-03-02. NOTICED PRESSURE SLOWLY DEACREASING. AFTER TEN MIN BOTTLE ONLY INDICATING 500PSI. FOUND DIAPHRAM WITH HOLE IN IT, REPLACED DIAPHRAM & O-RINGS LEA
- [SDR FDEA202203160586](https://openairdocs.org/sdr/FDEA202203160586.md): None · none · Mar 16, 2022 · N675FE · Airbus A300* · Detection System
  > DURING DESCENT RECEIVED ENGINE 2 LOOP B FAULT ECAM MESSAGE ACCOMPANIED BY OVERHEAD INDICATION. COMPLIED WITH APPROPRIATE QRH PROCEDURE. RELEASED FOR SERVICE PER MEL: 26-12-XX CATEGORY: C EXP: 26MAR22 "MEL 26-12-XX: ENG 2__LOOP B__ - INOP. FLIGHT CREW M
- [SDR FDEA202202180319](https://openairdocs.org/sdr/FDEA202202180319.md): Slide · failed · Feb 18, 2022 · N675FE · Airbus A300* · Emergency Equipment
  > PDIS 675 25-60 1477 18FEB22 BOS OPEN U WHILE CLOSING THE DOOR, THE DOOR SLIDE DEPLOYED. IT SHOULD BE NOTED THAT THE FO, RAMP, AND MX FOLLOWED PROCEDURES EXACTLY. FURTHERMORE, THE DOOR WAS NOT FULLY CLOSED, NOR WAS THE SLIDE ARMED (IN FACT THE
- [SDR FDEA2020063071374](https://openairdocs.org/sdr/FDEA2020063071374.md): Limiter · malfunctioned · Jun 27, 2020 · N675FE · Airbus A300F4605R · Trailing Edge Flap Control System
  > AFTER TAKEOFF FROM PDX FLAPS SYS 1 AND 2 FAULT. FLAPS STUCK. CONFIGURATION SLATS 15 FLAPS 20 DIVERTED TO KOAK PER GOC REQUEST. RECORDED FAULT (01111) FLAPS JAM. SFCC2 RECORDED FAULT (01110) HIGH SPEED V (01110). SFCC1 AND SFCC 2 BITE TEST PASSED. FOUND
- [SDR FDEA202006101172](https://openairdocs.org/sdr/FDEA202006101172.md): Skin Panel · delaminated · Jun 10, 2020 · N675FE · Airbus A300F4605R · Rudder, Plate/Skin
  > LOWER LT SIDE RUDDER LEADING EDGE PANEL HAS DELAM. REPAIRED RUDDER PANEL IAW EA 6-5540-T0354180 AND SRM 55-41-12 AND 51-77-10.
- [SDR FDEA202006031119](https://openairdocs.org/sdr/FDEA202006031119.md): Skin · gouged · Jun 3, 2020 · N675FE · Airbus A300F4605R · Leading Edge Devices
  > LEFT WING NR 1 SLAT LEADING EDGE UPPER SURFACE HAS GOUGE AND MULTIPLE SCRATCHES ALONG ENTIRE SLAT, FROM END TO END. REPAIRED LEADING EDGE OF LT NR 1 SLAT IAW EA 6-5750-T0354063-P1, SRM 51- 73-10, SRM 51-73-11, SRM 51-21-10, SRM 51-23-10, SRM 51-75-10, AND DWG
- [SDR FDEA202006021114](https://openairdocs.org/sdr/FDEA202006021114.md): Cover · cracked · Jun 2, 2020 · N675FE · Airbus A300* · Nacelle/Pylon Structure
  > #2 ENGINE PYLON INBD SIDE EXTERIOR TRIM IS CRACKED THROUGH AN EXISTING WELD REPAIR AT THE BOTTOM OF THE PYLON APPROX 38" AFT OF THE FIRE BOTTLE ACCESS OPENING REMOVED AND REPLACED EXTERIOR TRIM IAW A300 SRM 51-40-21 AND AIRBUS DWG A54515187, ISSUE E.
- [SDR FDEA2020090862114](https://openairdocs.org/sdr/FDEA2020090862114.md): Trim Panel · cracked · Jun 2, 2020 · N675FE · Airbus A300F4605R · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE PYLON INBOARD SIDE EXTERIOR TRIM IS CRACKED THROUGH AN EXISTING WELD. REPAIR AT THE BOTTOM OF THE PYLON APPROX 38" AFT OF THE FIRE BOTTLE ACCESS OPENING. REMOVED AND REPLACED EXTERIOR TRIM IAW A300 SRM 51-40-21 AND AIRBUS DWG A54515187, ISSUE E.
- [SDR FDEA2020060321114](https://openairdocs.org/sdr/FDEA2020060321114.md): Trim Panel · cracked · Jun 2, 2020 · N675FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 2 ENGINE PYLON INBD SIDE EXTERIOR TRIM IS CRACKED THROUGH AN EXISTING WELD. REPAIR AT THE BOTTOM OF THE PYLON APPROX 38" AFT OF THE FIRE BOTTLE ACCESS OPENING. REMOVED AND REPLACED EXTERIOR TRIM IAW SRM 51-40-21 AND DWG A54515187, ISSUE E.
- [SDR FDEA2020060321110](https://openairdocs.org/sdr/FDEA2020060321110.md): Plate · cracked · Jun 2, 2020 · N675FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 1 PYLON INBD FISH PLATE CRACKED. REMOVED FISH PLATE ON NR 1 PYLON INBD SIDE IAW SRM 51-40-21. LOCATED AND DRILLED NEW FISH PLATE PO 962545.4 AND SHIM PO 972481.1 IAW SRM 51-40-44 AND DWG A54612371 ISSUE B, ASSEMBLED FISH PLATE AND SHIM IAW SRM 51-40-2
- [SDR FDEA2020060111093](https://openairdocs.org/sdr/FDEA2020060111093.md): Seat Track · corroded · May 31, 2020 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK AT -Y953, BETWEEN FR 56 AND FR 57, HAS CORROSION. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-10-16 FIG 201.
- [SDR FDEA2020052981073](https://openairdocs.org/sdr/FDEA2020052981073.md): Seat Track · corroded · May 28, 2020 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN FLOOR SUPPORT STRUCTURE, UPPER SURFACE IS CORRODED AT FRAME 30, LOCATION AT APPROXIMATELY -Y 2425.7. REMOVED DAMAGE IAW SRM 51-73-10 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, WITH A MAX MATERIAL REMOVED OF.024". REPAIRED SEAT TRACK IAW SRM
- [SDR FDEA2020052961055](https://openairdocs.org/sdr/FDEA2020052961055.md): Skin · damaged · May 26, 2020 · N675FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING TASK CARD 53309364 RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 29 AND 30 AND BETWEEN STRINGER 45R AND 46R, PREVIOUS BLENDED OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10
- [SDR FDEA202005261049](https://openairdocs.org/sdr/FDEA202005261049.md): Floor Panel · delaminated · May 26, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN GEAR WELL FLOOR PANEL 147BF IS DELAMINATED. REPAIRED FLOOR PANEL 147BF BY FABRICATION IAW SRZ-25-005 REV: R.
- [SDR FDEA202005261048](https://openairdocs.org/sdr/FDEA202005261048.md): Rib · cracked · May 26, 2020 · N675FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT HAND WING CENTER FLAP SHOWING INDICATION AT RIB 27 AFT CRACKED. REPAIRED LEFT CENTER FLAP RIB 27 IAW SRM 57-50-00 PG 203 AND PG 220 AND EA 6-5750-T0354210-P1.
- [SDR FDEA2020052641041](https://openairdocs.org/sdr/FDEA2020052641041.md): Floorboard · punctured · May 24, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > (PARTS RACK) FLOORBOARD 231GG HAS PUNCTURES. FABRICATED NEW FLOOR PANEL 231GG PER SRZ-25-005 REV R.
- [SDR FDEA202005180979](https://openairdocs.org/sdr/FDEA202005180979.md): Attach Angle · cracked · May 18, 2020 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > ATTACHING ANGLE FOR CUSP WEB JUST AFT OF FRA 79 L/H IS CRACKED REMOVED AND REPLACED ANGLE PER AIRBUS DWG A53981418 ISSUE K
- [SDR FDEA202005180978](https://openairdocs.org/sdr/FDEA202005180978.md): Cusp Web · cracked · May 18, 2020 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > CUSP WEB ON AFT SIDE OF FRA 79 L/H IS CRACKED REMOVED AND REPLACED WEB PER AIRBUS DWG A53981360 ISSUE K
- [SDR FDEA202005180977](https://openairdocs.org/sdr/FDEA202005180977.md): Floorboard · damaged · May 18, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > (PARTS RACK) FLOORBOARD 231FF HAS PUNCTURES REPLACED FLOOR PANEL IAW A300-600 AMM 06-41-53, SRM 53-10-20, SRZ-25-005
- [SDR FDEA202005180976](https://openairdocs.org/sdr/FDEA202005180976.md): Floorboard · damaged · May 18, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > (PARTS RACK) FLOORBOARD 232WG IS PUNCTURED REPLACED FLOOR PANEL IAW A300-600 AMM 06-41-53, SRM 53-10-20, SRZ-25-005
- [SDR FDEA202005180975](https://openairdocs.org/sdr/FDEA202005180975.md): Floorboard · damaged · May 18, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > (PARTS RACK) FLOORBOARD 232SG IS PUNCTURED REPLACED FLOOR PANEL IAW A300-600 AMM 06-41-53, SRM 53-10-20, SRZ-25-005
- [SDR FDEA2020051870965](https://openairdocs.org/sdr/FDEA2020051870965.md): Floorboard · damaged · May 17, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > (PARTS RACK) FLOORBOARD 231YG IS MISSING EDGE FILL FABRICATED NEW FLOOR PANEL PER FEDEX SRZ-25-005 REV R AND PART MARKED NEW PANEL PER FEDEX GMM 07-0-1001
- [SDR FDEA2020051870964](https://openairdocs.org/sdr/FDEA2020051870964.md): Crossbeam · damaged · May 17, 2020 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > CENTER CABIN BELOW FLOOR OVER WING L/H SIDE C44 TRACK SUPPORT GOUGED (STREAMER) REMOVED AND REPLACED CROSSBEAM PER AIRBUS DWG A53812846 ISS. A.
- [SDR FDEA2020051540937](https://openairdocs.org/sdr/FDEA2020051540937.md): Floorboard · damaged · May 14, 2020 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > (PARTS RACK) FLOORBOARD 261PF IS BROKEN ON THE EDGE FABRICATED NEW FLOOR PANEL 261PF IAW FEDEX SRZ 25-005 REV - R, PART MARKED PER FEDEX GMM 07-0-1001
- [SDR FDEA2020042961056](https://openairdocs.org/sdr/FDEA2020042961056.md): Skin · damaged · Apr 26, 2020 · N675FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING TASK CARD 53309364, RE- INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 32 AND 33 AND STRINGER 45R AND 46R, PREVIOUS BLENDED OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12,
- [SDR FDEA2020042961054](https://openairdocs.org/sdr/FDEA2020042961054.md): Skin · damaged · Apr 26, 2020 · N675FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING TASK CARD 53309364, RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS APPROX 7" FWD OF FRAME 35 AND BETWEEN STRINGER 45R AND 46R, PREVIOUS BLENDED OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-
- [SDR FDEA2020042961053](https://openairdocs.org/sdr/FDEA2020042961053.md): Skin · damaged · Apr 26, 2020 · N675FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING TASK CARD 53309364, RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN DAMAGE, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 33 AND 34 AND BETWEEN S45R AND S46R, PREVIOUS BLEND OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12, FIG
- [SDR FDEA202004261052](https://openairdocs.org/sdr/FDEA202004261052.md): Skin · damaged · Apr 26, 2020 · N675FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING TASK CARD 53309364, RE-INSPECTION OF PREVIOUSLY BLENDED EXTERIOR FUSELAGE SKIN, FOUND DAMAGE STILL EXISTS BETWEEN FRAMES 30 AND 31 AND BETWEEN S45R AND S46R, PREVIOUS BLEND OUT AREA. ACCOMPLISHED REPAIR DOUBLER IAW SRM 53-10-12 FIG 208. A
- [SDR FDEA2020060531123](https://openairdocs.org/sdr/FDEA2020060531123.md): Intercostal · cracked · Apr 23, 2020 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > FORWARD CARGO PIT, INTERCOSTAL BETWEEN FRAMES C26-C27, BELOW RT OUTBOARD ROLLER TRACK IS CRACKED ON AFT UPPER CORNER. REMOVED AND REPLACED INTERCOSTAL BETWEEN FRAMES C26-C27, BELOW OUTBOARD ROLLER TRACK IAW SRM 51-40-21 AND DWG 14A53778347.
- [SDR FDEA201802270573](https://openairdocs.org/sdr/FDEA201802270573.md): Power Supply · inoperative · Feb 27, 2018 · N675FE · Airbus A300F4605R · Emergency Equipment
  > PRIOR TO PUSHBACK, RIGHT SLIDE INDICATION WILL NOT SHOW ARMED. TROUBLESHOT IAW ASM 52-73-00. REMOVED AND REPLACED THE AUTONOMOUS POWER SUPPLY IAW MM 52-73-18-04, AND 52-73-00-05-02. OPS CHECKED GOOD.
- [SDR FDEA201708292408](https://openairdocs.org/sdr/FDEA201708292408.md): Floor Panel · broken · Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 251TH FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL 251TH P/N FX-B5327027700200 ON T17/1291751 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.
- [SDR FDEA201708292407](https://openairdocs.org/sdr/FDEA201708292407.md): Floor Panel · broken · Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 252NH FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL 252NH P/N FX-B5327027500300 ON T17/1291764 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.
- [SDR FDEA201708292406](https://openairdocs.org/sdr/FDEA201708292406.md): Floor Panel · broken · Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 241FJ FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL P/N FX- -B5327062003200 ON T17/1291757 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR (241FJ).
- [SDR FDEA201708292405](https://openairdocs.org/sdr/FDEA201708292405.md): Floor Panel · broken · Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 241GJ FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL 241GJ P/N FX-B5327062002000 ON T17/1291773 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.
- [SDR FDEA201708292404](https://openairdocs.org/sdr/FDEA201708292404.md): Floor Panel · broken · Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 241RJ FLOOR PANEL BROKEN. FABRICATED 241RJ FLOOR PANEL P/N FX-B5327062400000 ON T17/1291849 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.
- [SDR FDEA201708292403](https://openairdocs.org/sdr/FDEA201708292403.md): Floor Panel · broken · Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 241TH FLOOR PANEL BROKEN. FABRICATED 241TH FLOOR PANEL P/N FX-B5327060000200 ON T17/1291847 IAW DWG SRZ-25-005 REV M CAT "A" MAJOR REPAIR.
- [SDR FDEA201708292402](https://openairdocs.org/sdr/FDEA201708292402.md): Floor Panel · broken · Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 251BH FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL P/N FX-B5327028700200 ON T17/1291842 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR (251BH).
- [SDR FDEA201708292401](https://openairdocs.org/sdr/FDEA201708292401.md): Floor Panel · broken · Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 252GF FLOOR PANEL BROKEN. FABRICATED 252GF FLOOR PANEL P/N FX-B5327027300000 ON T17/1291843 IAW DWG SRZ-25-005 REV M CAT "A" MAJOR REPAIR.
- [SDR FDEA201708292400](https://openairdocs.org/sdr/FDEA201708292400.md): Floor Panel · broken · Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 242KK FLOOR PANEL BROKEN. FABRICATED FLOOR PANEL 242KK P/N FX-B5327063600000 ON T17/1291838 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.
- [SDR FDEA201708292399](https://openairdocs.org/sdr/FDEA201708292399.md): Floor Panel · broken · Aug 29, 2017 · N675FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 241GF FLOOR PANEL BROKEN. FABRICATED NEW FLOOR PANEL 241GF ON T17/1291767 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR P/N FX-B5327048001600.
- [SDR FDEA201708242353](https://openairdocs.org/sdr/FDEA201708242353.md): Crossbeam · cracked · Aug 24, 2017 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > CROSSBEAM CRACKED IN 2EA PLACES FR41 -Y450 TO -Y953 RT. REMOVED AND REPLACED CROSSBEAM AT FR41 BETWEEN SEAT TRACKS -Y450 TO -Y953 IAW SRM 51-40-21. MAJOR REPAIR.
- [SDR FDEA201708232328](https://openairdocs.org/sdr/FDEA201708232328.md): Seat Track · corroded · Aug 23, 2017 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO SEAT TRACK Y450 FR 55 HAS A BUILDUP OF CORROSIVE MATERIAL. REPLACED SEAT TRACK FROM FR54.2 TO FR57.5 IAW SRM 51-40-21. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-16. MAJOR REPAIR.
- [SDR FDEA201708232326](https://openairdocs.org/sdr/FDEA201708232326.md): Seat Track · cracked · Aug 23, 2017 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > DUMMY SEAT TRACK LT NR 4 AT FR 38.2 TO FR40 FAILED GAP CHECK. REMOVED DUMMY SEAT TRACK CRACKED AT LT NR 4 FR38.2 TO FR40. LOCATED AND DRILLED NEW DUMMY SEAT TRACK AND INSTALLED IAW SRM 51-40-44 AND SRM 51-40-21. MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N675FE/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 = 'N675FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N675FE/reports

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