# Service difficulty reports: N670FE

A list on [N670FE](https://openairdocs.org/aircraft/N670FE.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 · 205 reports

- [SDR FDEA202610041482](https://openairdocs.org/sdr/FDEA202610041482.md): Structure · cracked · Oct 4, 2026 · N670FE · Airbus A300F4605R · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR UPPER EDGE AT PT1 BTWN FR 22 & 25, FOUND CRACK SIGNAL AT 2 EA FASTENER HOLES. COMPLIED WITH EA 6-5230-T0388992 P1 REPAIR MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR22 AND FR25 2EA CRACK HOLES. EA TITLE: DOORS - CARGO DOOR/HYD SYS -
- [SDR FDEA202609281443](https://openairdocs.org/sdr/FDEA202609281443.md): Fitting · damaged · Sep 28, 2026 · N670FE · Airbus A300F4605R · Cargo/Baggage Doors
  > COMPLY WITH EO 6-5230-E0378588 C P5. DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. COMPLIED WITH EO 6-5230-E0378588 C P5. TITLE: DOORS - CARGO DOO
- [SDR FDEA202609221405](https://openairdocs.org/sdr/FDEA202609221405.md): Stiffener · corroded · Sep 22, 2026 · N670FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > TOILET SERVICE ACCESS PANEL FWD LOWER CUTOUT CORRODED. REPLACED THE CORRODED STIFFENER AT TOILET SERVICE ACCESS PANEL FWD LOWER CUTOUT PER A300-600F SRM51-40-21 & DWG.A53612375(ISSUE.K). THIS IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202609221403](https://openairdocs.org/sdr/FDEA202609221403.md): Rib · cracked · Sep 22, 2026 · N670FE · Airbus A300F4605R · Trailing Edge Flaps
  > RIGHT WING CENTER FLAP RIB UPR FLANGE FOUND CRACK AT RIB15 BETWEEN STRINGERS 2.6, 2.7, & 2.8. CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100 I.A.W EA T6-5750-T0378801 P1, SEQ 1119, LT CENTER FLAP WITH OVERSIZED HOLE ON UPPER SKIN AT RIB 11. REPAIRED IAW GMM6-2
- [SDR FDEA202609221402](https://openairdocs.org/sdr/FDEA202609221402.md): Rib · cracked · Sep 22, 2026 · N670FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT WING CENTER FLAP RIB UPPER FLANGE FOUND CRACKED AT RIB 26 BETWEEN STGR2.6 AND STGR2.7. COMPLIED WITH EA 6-5750-T0388894 P1 REPAIR LT WING CENTER FLAP UPR FLANGE CRACK. THIS IS CAT A REPAIR. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202609211390](https://openairdocs.org/sdr/FDEA202609211390.md): Stringer Splice · cracked · Sep 21, 2026 · N670FE · Airbus A300F4605R · Fuselage Main, Longeron/Stringer
  > MDCC FR 47, S-18L STRINGER SPLICE CRACKED. REPLACED THE STRINGER SPLICE AT MDCC FR47, S-18L PER A300-600F SRM51-40-21 & DWG.A53833157(ISSUE:F00). THIS IS CAT A REPAIR. MAJOR REPAIR IAW GMM6-2-100.
- [SDR FDEA202605090573](https://openairdocs.org/sdr/FDEA202605090573.md): Door · faulted · May 9, 2026 · N670FE · Airbus A300F4605R · Door Warning System
  > PRIOR TO BLOCK OUT, R1 DOOR WILL NOT SHOW ARMED ON ECAM. MCO RELEASED FOR SERVICE PER MEL: 52-30-04 TROUBLESHOOTING IS REQUIRED PRIOR TO INSTALLING PART(S).
- [SDR FDEA202602250280](https://openairdocs.org/sdr/FDEA202602250280.md): Unknown · odor · Feb 25, 2026 · N670FE · Airbus A300F4605R · Air Distribution System
  > AT 1706Z, IN CRUISE FL350,.8 MACH, STRONG FUMES LIKE BURNING SULPHUR FROM FIREWORKS ENTERED THE COCKPIT. DONNED OXYGEN MASKS, DECLARED EMERGENCY, AND MADE LANDING. BOTH COCKPIT MASKS AND WALK AROUND BOTTLE WERE USED. INSPECTED BOTH ENGS NR 1 BEARING MANIF
- [SDR FDEA202602150209](https://openairdocs.org/sdr/FDEA202602150209.md): Safety Wire · wrong part · Feb 15, 2026 · N670FE · Airbus A300F4605R · Escape Slide
  > WHILE PERFORMING F.E.A. 6-2560-F0386375 REV NO. A PS P1, FOUND EJECTOR BAG RELEASE CABLE SAFETY WIRE INCORRECT. L1 DOOR SLIDE AMM: 25-61-20-05-01 REMOVED AND INSTALLED NEW SAFETY WIRE MS20995CY16 CAD-PLATED COPPER WIRE ON EJECTOR BAG RELEASE CABLE. A
- [SDR FDEA202602150208](https://openairdocs.org/sdr/FDEA202602150208.md): Safety Wire · wrong part · Feb 15, 2026 · N670FE · Airbus A300F4605R · Escape Slide
  > WHILE PERFORMING F.E.A. 6-2560-F0386375 REV NO. A PS P1, FOUND PACKBOARD RELEASE CABLE SAFETY WIRE INCORRECT. L1 DOOR SLIDE AMM: 25-61-20-05-01 REMOVED AND REPLACED PACKBOARD RELEASE CABLE SAFETY WIRE WITH MS20995C15 STAINLESS STEEL WIRE. A/C OK FOR
- [SDR FDEA202510021876](https://openairdocs.org/sdr/FDEA202510021876.md): Light · faulted · Oct 2, 2025 · N670FE · Airbus A300F4605R · Emergency Lighting
  > L1 DOOR EMERG. EXIT FWD DOWN SPOT LIGHT WILL NOT ILLUMINATE. AMM: 33-51-13-04 SERVICED L1 EMERG DOOR EXIT LIGHT. OK FOR SERVICE.
- [SDR FDEA202510021875](https://openairdocs.org/sdr/FDEA202510021875.md): Light · malfunctioned · Oct 2, 2025 · N670FE · Airbus A300F4605R · Emergency Lighting
  > R1 DOOR EMERG. EXIT FWD DOWN SPOT LIGHT WILL NOT ILLUMINATE. SERVICED R1 DOOR EMERGANCY LIGHT. OK FOR SERVICE
- [SDR FDEA202405120653](https://openairdocs.org/sdr/FDEA202405120653.md): Skin · delaminated · May 12, 2024 · N670FE · Airbus A300F4605R · Spoilers
  > LH WING #4 SPOILER CENTER O/B HINGE ARM LWR SKIN FOUND DELAMINATION. SIZE: 17MM*9MM. DEPTH: 2.00MM COMPLIED WITH EA 6-5750-T0379097 P1, ACCOMPLISHED THE MODIFICATION OF SB A300-57-6082 R03 ON THE LH WING #4 SPOILER AND ALLOWED TO LEAVE THE DELAMINATION AS
- [SDR FDEA202405120652](https://openairdocs.org/sdr/FDEA202405120652.md): Floorbeam · cracked · May 12, 2024 · N670FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN DECK CARGO COMPARTMENT FR67 CROSSBEAM BETWEEN Y1456 AND Y1959 FOUND A CRACK. REPAIRED THE CRACKED CROSSBEAM AT MAIN DECK CARGO COMPARTMENT FR67 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 PARA.14 FIGURE.211. THIS IS CATEGORY A REPAIR. MAJO
- [SDR FDEA202405120651](https://openairdocs.org/sdr/FDEA202405120651.md): Floorbeam · cracked · May 12, 2024 · N670FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN DECK CARGO COMPARTMENT CROSSBEAM FR30 BETWEEN Y1456 AND Y1959 FOUND A CRACK REPAIRED THE MAIN DECK CARGO COMPARTMENT CRACKED CROSSBEAM FR30 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 PARA.15 FIGURE 212 AND EA 6-5310-T0379137 P1. TITLE: FU
- [SDR FDEA202405070608](https://openairdocs.org/sdr/FDEA202405070608.md): None · none · May 7, 2024 · N670FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR30 CROSSBEAM BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR30 CROSSBEAM BETWEEN -Y450 AND -Y953 WAS EVALUATED AND REPAIRED IT PER EA: 6-5321-
- [SDR FDEA202405070607](https://openairdocs.org/sdr/FDEA202405070607.md): None · none · May 7, 2024 · N670FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR29 CROSSBEAM BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR29 CROSSBEAM BETWEEN -Y450 AND -Y953 WAS EVALUATED AND REPAIRED IT PER EA: 6-5321-
- [SDR FDEA202405070606](https://openairdocs.org/sdr/FDEA202405070606.md): None · none · May 7, 2024 · N670FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR28 CROSSBEAM BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR28 CROSSBEAM BETWEEN -Y450 AND -Y953 WAS EVALUATED AND REPAIRED IT PER EA: 6-5321-
- [SDR FDEA202405070605](https://openairdocs.org/sdr/FDEA202405070605.md): None · none · May 7, 2024 · N670FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR75-FR76 SEAT TRACK AT -Y450 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR75-FR76 SEAT TRACK AT -Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-1
- [SDR FDEA202405070604](https://openairdocs.org/sdr/FDEA202405070604.md): None · none · May 7, 2024 · N670FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR31 CROSSBEAM BETWEEN Y1456 AND Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT FR31 CROSSBEAM BETWEEN Y1456 AND Y1959 WAS EVALUATED AND FOUND IN CONFORMITY WITH A
- [SDR FDEA202405060602](https://openairdocs.org/sdr/FDEA202405060602.md): None · none · May 6, 2024 · N670FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON AFT CARGO FR63 FLOOR BEAM BETWEEN Y805 AND Y1470 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON AFT CARGO FR63 FLOOR BEAM BETWEEN Y805 AND Y1470 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-10-15-201, FIG208.
- [SDR FDEA202405050581](https://openairdocs.org/sdr/FDEA202405050581.md): Web · cracked · May 5, 2024 · N670FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO UNDER FLOOR WEB FR47 -Y953~-Y1456 FOUND 1EA CRACK REPAIRED THE MAIN DECK CARGO UNDER FLOOR CRACKED WEB FR47 -Y953 ~ -Y1456 PER A300- 600F SRM53-15-15-201 FIG.201. THIS IS A CAT B REPAIR. THE INSPECTION THRESHOLD WAS 24000FC AFTER REPAIR EMB
- [SDR FDEA202405050580](https://openairdocs.org/sdr/FDEA202405050580.md): None · none · May 5, 2024 · N670FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB12 - RIB13 BETWEEN S2.2 AND S2.4 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RH WING CENTER FLAP LOWER SKIN RIB12-RIB13 BETWEEN S2.2 & 2.4 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH SRM 5
- [SDR FDEA202405050579](https://openairdocs.org/sdr/FDEA202405050579.md): Static Wick · corroded · May 5, 2024 · N670FE · Airbus A300* · Pitot/Static System
  > RH WING OUTER FLAP OUTBOARD AREA 1EA STATIC DISCHARGER BASE CORRODED COMPLIED WITH EA 6-5750-T0379031 P1 REPAIRED THE RH WING O/B FLAP OUTER T/E CORRODED UPPER SKIN. TITLE: WINGS - FLIGHT SURFACES - RH O/B FLAP, OUTER TRAILING EDGE, UPPER SKIN CORROSION UN
- [SDR FDEA202405050578](https://openairdocs.org/sdr/FDEA202405050578.md): None · none · May 5, 2024 · N670FE · Airbus A300* · Standard Practices/Structures
  > EXISTING REPAIR ON FUSELAGE FRAME FR20A S37R-S42R REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE FRAME FR20A S37R-S42R WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-13-13-201 FIG.201. COMPLIED WITH EA 6-5310-54559 B P2
- [SDR FDEA202203230653](https://openairdocs.org/sdr/FDEA202203230653.md): Line · leaking · Mar 23, 2022 · N670FE · Airbus A300F4605R · Hydraulic System, Main
  > ECAM DISPLAYED HYD RSVR LO LEVEL GREEN SYS. CONFIRMED GREEN HYD QTY WAS AT THE RED DOT, COMPLIED WITH ECAM & SHUTOFF ENGINE DRIVEN PUMPS. COMPLETED ALL THE QRH PROCEDURES INCLUDING GRAVITY GEAR EXTENSION. AFTER ACFT FULLY CONFIGURED FOR LANDING. GREE
- [SDR FDEA202201280153](https://openairdocs.org/sdr/FDEA202201280153.md): Gusset · cracked · Jan 28, 2022 · N670FE · Airbus A300* · Fuselage Main, Structure
  > FIRST OFFICER'S WINDOW FRAME 4RH GUSSET FOUND CRACK SIGNAL AT HOLE #10 REPLACED THE CRACKED FIRST OFFICER'S WINDOW FRAME 4RH GUSSET PER EA: 6-5310- T0354786 A P2. TITLE: FUSELAGE - MAINFRAME - FIRST OFFICER'S WINDOW FRAME 4RH GUSSET, CRACK INDICATION AT HOL
- [SDR FDEA202201260132](https://openairdocs.org/sdr/FDEA202201260132.md): Skin · dented · Jan 26, 2022 · N670FE · Airbus A300* · Fuselage Main, Plate/Skin
  > LWR FUSELAGE SKIN FR33 STGR41-42LH FOUND DENT REPAIRED THE DEFORMED LWR FUSELAGE SKIN AT FR33 STGR41-42LH PER A300-600F SRM53-10-12 FIG210. THIS IS CATEGORY B REPAIR. IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI 53-10-12-2-004-00. FIRST INSP
- [SDR FDEA202201190082](https://openairdocs.org/sdr/FDEA202201190082.md): Spoiler · delaminated · Jan 19, 2022 · N670FE · Airbus A300* · Wing, Control Surfaces
  > LH WING #5 SPOILER CENTER I/B & O/B HINGE ARM LWR SURFACE FOUND DELAMINATION. SIZE: (1) 20MM*20MM, DEPTH: 1.9MM (2) 40MM*20MM, DEPTH: 2.2MM COMPLIED WITH EA: 6-5750-T0366401 P1. TITLE: WING - FLIGHT SURFACES - LH 5# SPOILER CENTER HINGE ARMS LOWER SURFAC
- [SDR FDEA202201110039](https://openairdocs.org/sdr/FDEA202201110039.md): Crossbeam · cracked · Jan 11, 2022 · N670FE · Airbus A300* · Fuselage Main, Structure
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN -Y953 AND -Y1456 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR64 BETWEEN -Y953 AND -Y1456 PER A300-600F SRM53-10-15 FIGURE 211. THIS IS C
- [SDR FDEA202201080024](https://openairdocs.org/sdr/FDEA202201080024.md): Crossbeam · cracked · Jan 8, 2022 · N670FE · Airbus A300* · Fuselage Main, Structure
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN -Y1456 AND -Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959 PER A300-600F SRM53-10-15 FIGURE 211. THIS IS
- [SDR FDEA202105111182](https://openairdocs.org/sdr/FDEA202105111182.md): Damper · failed · May 11, 2021 · N670FE · Airbus A300F4605R · Landing Gear Retraction/Extension System
  > ON T/O COULD NOT RETRACT LANDING GEAR IN SYSTEM 1 OR 2. COMPLIED WITH ALL ECAM AND QRH PROCEDURES.. R&R LH PITCH DAMPER REF A300 MM 32-11-15-04. JACKED A/C AND SWUNG GEAR SEVERAL TIMES IN EACH SYSTEM, GEAR SWING AND IND. CHECKS GOOD. BITE CHECKED P
- [SDR FDEA201907261715](https://openairdocs.org/sdr/FDEA201907261715.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL 152WF AFT PIT IS DAMAGED. FLOOR PANEL FABRICATED ON MAE TRAVELER T19/1429934 IAW DWG SRZ-25-005. MAJOR REPAIR
- [SDR FDEA201907261726](https://openairdocs.org/sdr/FDEA201907261726.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 242RJ BROKEN. FABRICATED FLOOR PANEL 242RJ ON TRAVELER T19/1431751 IAW SRZ-25-005. MAJOR REPAIR
- [SDR FDEA201907261724](https://openairdocs.org/sdr/FDEA201907261724.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN HAS A DAMAGED FLOOR BOARD PANEL 231WG. FABRICATED FLOOR PANEL 231WG ON TRAVELER T19/1430541 IAW SRZ-25-005 MAJOR REPAIR
- [SDR FDEA201907261718](https://openairdocs.org/sdr/FDEA201907261718.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL 161AF BULK CARGO IS DAMAGED. FLOOR PANEL FABRICATED ON MAE TRAVELER T19/1430127 IAW DWG SRZ-25-005. MAJOR REPAIR
- [SDR FDEA201907261711](https://openairdocs.org/sdr/FDEA201907261711.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL 151PF AFT PIT IS DAMAGED. FLOOR PANEL FABRICATED ON MAE TRAVELER T19/1430110 IAW DWG SRZ-25-005 MAJOR REPAIR
- [SDR FDEA201907261725](https://openairdocs.org/sdr/FDEA201907261725.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL 251VH INSERT RIPPED OUT OF FWD LT CORNER. FABRICATED FLOOR PANEL 251VH ON T19/1430557 IAW DWG SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201907261723](https://openairdocs.org/sdr/FDEA201907261723.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN HAS A DAMAGED FLOOR PANEL 262MF. RECEIVED FABRICATED FLOOR BOARD 262MF ON T19/1430553 IAW DWG SRZ-25-005 MAJOR REPAIR.
- [SDR FDEA201907261722](https://openairdocs.org/sdr/FDEA201907261722.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN HAS A DAMAGED FLOOR BOARD PANEL 261ZF. RECEIVED FABRICATED FLOOR BOARD ON T19/1430438 IAW DWG SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201907261721](https://openairdocs.org/sdr/FDEA201907261721.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN HAS A DAMAGED FLOOR BOARD PANEL 242JF. RECEIVED FABRICATED FLOOR BOARD 242JF ON T19/1430523 IAW DWG SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201907261720](https://openairdocs.org/sdr/FDEA201907261720.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN HAS A DAMAGED FLOOR BOARD PANEL 231UG. FABRICATED FLOOR PANEL ON T19/1430547 IAW DWG SRZ-25-005 MAJOR REPAIR.
- [SDR FDEA201907261719](https://openairdocs.org/sdr/FDEA201907261719.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL 161GF BULK CARGO IS DAMAGED. FLOOR PANEL FARICATED ON T19/1430131 IAW DWG SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201907261717](https://openairdocs.org/sdr/FDEA201907261717.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL 152PF AFT PIT IS DAMAGED. FLOOR PANEL FABRICATED ON T19/1430083 IAW DWG SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201907261714](https://openairdocs.org/sdr/FDEA201907261714.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL 152TF AFT PIT IS DAMAGED. FLOOR PANEL FABRICATED ON T19/1430105 IAW SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201907261713](https://openairdocs.org/sdr/FDEA201907261713.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL 152QF AFT PIT IS DAMAGED. FLOOR PANEL FABRICATED ON T19/1430087 IAW DWG SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201907261712](https://openairdocs.org/sdr/FDEA201907261712.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL 151XF AFT PIT IS DAMAGED. FLOOR PANEL FABRICATED ON T19/1430121 IAW DWG SRZ-25-005. MAJOR REPAIR.
- [SDR FDEA201907261710](https://openairdocs.org/sdr/FDEA201907261710.md): Floor Panel · damaged · Jul 26, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL 151MF AFT PIT IS DAMAGED. FLOOR PANEL FABRICATED ON T19/1430112 IAW DWG SRZ-25-005 MAJOR REPAIR.
- [SDR FDEA201907251700](https://openairdocs.org/sdr/FDEA201907251700.md): Floor Panel · damaged · Jul 25, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN HAS A DAMAGED FLOOR BOARD PANEL 251SH. RECEIVED FABRICATED FLOOR BOARD 251SH ON T19/1430534 IAW DWG SRZ-25- 005. MAJOR REPAIR.
- [SDR FDEA201907251699](https://openairdocs.org/sdr/FDEA201907251699.md): Floor Panel · damaged · Jul 25, 2019 · N670FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN HAS A DAMAGED FLOOR BOARD PANEL 241AJ. RECEIVED FABRICATED FLOOR BOARD 241AJ ON T19/1430333 IAW DWG SRZ-25-005. MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N670FE/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 = 'N670FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N670FE/reports

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