# Service difficulty reports: N682FE

A list on [N682FE](https://openairdocs.org/aircraft/N682FE.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 6 · 299 reports

- [SDR FDEA202602040128](https://openairdocs.org/sdr/FDEA202602040128.md): Valve · faulted · Feb 4, 2026 · N682FE · Airbus A300F4605R · Landing Gear Retraction/Extension System
  > WHILE PERFORMING OPS CHECK OF ELCTROHYDRAULIC VALVE 3GA REPLACEMENT WRI 5-25/4268. THE NOSE GEAR RETRACTED.
- [SDR FDEA202601310109](https://openairdocs.org/sdr/FDEA202601310109.md): Battery Pack · no test · Jan 31, 2026 · N682FE · Airbus A300F4605R · Emergency Lighting
  > EMERGENCY LIGHT TEST SWITCH DOES NOT TEST. ENTRY AREA, RED EMER LT SWITCH DOES NOT ILLUMINATE EMERGENCY LIGHTS, SWITCH DOES ILLUMINATE RED. REMOVED & REPLACED THE EMERGENCY POWER SUPPLY BATTERY, OP TESTED GOOD.
- [SDR FDEA202412241850](https://openairdocs.org/sdr/FDEA202412241850.md): Wire · detached · Dec 24, 2024 · N682FE · Airbus A300F4605R · Door System Wiring
  > EMERGENCY ACCESS SWITCH AND MOMENTARY DOOR BELL BUTTON INOP. DURING T/S FOUND WIRE JMPR-22 BROKEN AT EMERGENCY ENTRY SWITCH TERM 1. RETERMINATED WIRE JMPR-22 AND 9005-20 AT EMERGENCY ENTRY SWITCH TERM 1. OPS CHK REQ'D. ACCOMPLISHED OPS TEST OF COCKPIT D
- [SDR FDEA202404070447](https://openairdocs.org/sdr/FDEA202404070447.md): Frame · cracked · Apr 7, 2024 · N682FE · Airbus A300F4605R · Wing Main, Frame Structure
  > WINGS - BASIC WING STRUCTRUE - INSPECTION OF FR40 LOWER OUTBOARD RADIUS, LH SIDE, OUND CRACK AT AREA A STARTED FROM THE HOLE A LWR EDGE COMPILED WITH EO 6-5710-E0333575 D P5. REPAIRED THE CRACKED AREA A ON LH SIDE FR40 FWD FITTING LOWER OUTBOARD RADIUS. TH
- [SDR FDEA202404010429](https://openairdocs.org/sdr/FDEA202404010429.md): Web · cracked · Apr 1, 2024 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FR47 BETWEEN -Y953 AND -Y1456 UNDERFLOOR WEB CRACKED. REPAIRED THE MAIN DECK FR47 BETWEEN -Y953 AND -Y1456 UNDERFLOOR CRACKED WEB PER A300-600F SRM53-15-15-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A30
- [SDR FDEA202404010428](https://openairdocs.org/sdr/FDEA202404010428.md): Web · cracked · Apr 1, 2024 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FR47 BETWEEN Y953 AND Y1456 UNDERFLOOR WEB CRACKED. REPAIRED THE MAIN DECK FR47 BETWEEN Y953 AND Y1456 UNDERFLOOR CRACKED WEB PER A300-600F SRM53-15-15-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-60
- [SDR FDEA202404010427](https://openairdocs.org/sdr/FDEA202404010427.md): Web · cracked · Apr 1, 2024 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FR47 BETWEEN Y0 AND -Y450 UNDERFLOOR WEB CRACKED. REPAIRED THE MAIN DECK FR47 BETWEEN Y0 AND -Y450 UNDERFLOOR CRACKED WEB PER A300- 600F SRM53-15-15-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F
- [SDR FDEA202404010426](https://openairdocs.org/sdr/FDEA202404010426.md): Web · cracked · Apr 1, 2024 · N682FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FR47 BETWEEN Y0 AND Y450 UNDERFLOOR WEB CRACKED. REPAIRED THE MAIN DECK FR47 BETWEEN Y0 AND Y450 UNDERFLOOR CRACKED WEB PER A300- 600F SRM53-15-15-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI
- [SDR FDEA202404010425](https://openairdocs.org/sdr/FDEA202404010425.md): Crossbeam · cracked · Apr 1, 2024 · N682FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR61, BETWEEN -Y1456 AND -Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR61 BETWEEN -Y1456 AND -Y1959 PER A300-600F SRM53-10-15-201 PARA.14. THIS IS
- [SDR FDEA202403050248](https://openairdocs.org/sdr/FDEA202403050248.md): Lug · corroded · Mar 5, 2024 · N682FE · Airbus A300F4605R · Wing, Landing Gear Attach Fittings
  > L/H MLG RIB 5 FWD LUG SHOWS SIGNS OF CORROSION IN GREASE GROOVE. REPAIRED IAW AIRBUS REPAIR INSTRUCTIONS R57240425. SEE FINAL EA 6-5710-T0378283. TITLE: WINGS - LH MAIN LANDING GEAR FITTING - REPAIR OF RIB 5 AFT PINTLE FWD LUG BORE CORROSIION IAW AIRBUS R
- [SDR FDEA202403050247](https://openairdocs.org/sdr/FDEA202403050247.md): Lug · corroded · Mar 5, 2024 · N682FE · Airbus A300F4605R · Wing, Landing Gear Attach Fittings
  > R/H MLG RIB 5 FWD LUG SHOWS SIGNS OF CORROSION IN GREASE GROOVE REPAIRED R/H MLG RIB 5 FWD LUG PER AIRBUS R57240425 SEE JPF PAGES 1-2, ITEMS 1-16 FOR WORK COMPLETED, EA # 6-5710-T0378296 P1 TITLE: WINGS - RH MAIN LANDING GEAR FITTING - REPAIR OF RIB 5 AFTY
- [SDR FDEA202312211950](https://openairdocs.org/sdr/FDEA202312211950.md): Engine · leaking · Dec 21, 2023 · N682FE · Airbus A300* · Engine Oil Indicating System
  > ENG 1 OIL LO PRESS. PRESSURE INDICATED NORMAL ON ENG PAGE AND GAUGE. HOWEVER, WE NOTICED OIL QUANTITY DECREASING. DECREASING APPROX 2 QUARTS PER 10 MINUTES. AFTER LANDING BACK AT KMEM WE HAD 5 QUARTS REMAINING. 8 QUARTS AFTER ENG SHUTDOWN. ADDED 12 QTS OI
- [SDR FDEA202312200245](https://openairdocs.org/sdr/FDEA202312200245.md): Fitting · corroded · Dec 20, 2023 · N682FE · Airbus A300F4605R · Fuselage, Landing Gear Attach Fittings
  > LHRIB 5 FITTING HAS CORROSION REPAIRED PER AIRBUS REPAIR DRAWING R57240425
- [SDR FDEA202312200244](https://openairdocs.org/sdr/FDEA202312200244.md): Fitting · corroded · Dec 20, 2023 · N682FE · Airbus A300F4605R · Fuselage Main, Structure
  > RH RIB 5 FITTING HAS CORROSION. REPAIR PER AIRBUS REPAIR DRAWING R57240425
- [SDR FDEA202312161943](https://openairdocs.org/sdr/FDEA202312161943.md): Unknown · unknown · Dec 16, 2023 · N682FE · Airbus A300* · Escape Slide
  > R1 SLIDE INDICATION NOT SHOWING ON ECAM WHEN DOOR IS CLOSED AND ARMED, ALL OTHER DOOR CLOSED AND LOCKED INDICATIONS ARE FINE. PERFORMED T/S FOUND NO R1" SLIDE" INDICATION ON ECAM. PERFORMED TEST OF AUTOMOMOUS STBY PWR UNIT AND R1 "SLIDE" INDICATION RETUR
- [SDR FDEA202304110624](https://openairdocs.org/sdr/FDEA202304110624.md): Idg · failed · Apr 11, 2023 · N682FE · Airbus A300F4605R · AC Generator-Alternator
  > ON DESCENT LOST GEN 2. GEN DID NOT RESET. REMOVED AND REPLACED #2 ENGINE IDG OPS CHECK GOOD AT THIS TIME REF A 300 AMM 24-11-11-04-01.
- [SDR FDEA202211072737](https://openairdocs.org/sdr/FDEA202211072737.md): Meter · no test · Nov 7, 2022 · N682FE · Airbus A300F4605R · Passenger Oxygen System
  > #4 COURIOUR O2 MASK FLOW METER BLINKER DOES NOT OPERATE DURING TEST. REPLACED #4 COURIER OXYGEN MASK STOWAGE BOX.
- [SDR FDEA202201060018](https://openairdocs.org/sdr/FDEA202201060018.md): Transmitter · faulted · Jan 6, 2022 · N682FE · Airbus A300F4605R · Hydraulic System, Main
  > ON TAKE OFF ROLL @ 60 KNOTS RECIEVED ECAM ALERT FOR YELLOW SYSTEM LOW PRESSURE. REJECT THE TAKE OFF AND RETURN TO GATE (NOTE: CREW REPORTED SYSTEM PRESSURE RETURN TO NORMAL DURING TAXI IN) REMOVED AND REPLACED YELLOW SYSTEM HYD QTY TRANSMITTER. REF AM
- [SDR FDEA202112233123](https://openairdocs.org/sdr/FDEA202112233123.md): Pressure Switch · failed · Dec 23, 2021 · N682FE · Airbus A300* · Hydraulic System, Main
  > PDIS 682 29-10 0412 23DEC21 MEM FACT U SHORTLY AFTER TAKEOFF, CLIMBING THRU 5000 FEET, ECAM DISPLAYED HYD LOW PRESSURE YELLOW SYSTEM. ECAM AND QRH WERE FOLLOWED AND AN UNEVENTFUL LANDING WAS MADE BACK TO RWY 18C KMEM. A300-600 AMM 29-24-00
- [SDR FDEA202112220148](https://openairdocs.org/sdr/FDEA202112220148.md): Power Supply · inoperative · Dec 22, 2021 · N682FE · Airbus A300* · Emergency Lighting
  > MDIS 682 33-50 0405 22DEC21 GSP FACT U EMERGENCY EXIT LIGHT POWER SUPPLY BATTERY IS DEAD. R/I 22DEC21 01:03 GSP U REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-31 POS: 3 SRL: 278291
- [SDR FDEA202112190147](https://openairdocs.org/sdr/FDEA202112190147.md): Power Supply · inoperative · Dec 19, 2021 · N682FE · Airbus A300* · Emergency Lighting
  > MDIS 682 33-50 0400 19DEC21 MEM FACT U EMERGENCY LIGHTS NOT WORKING. R/I 19DEC21 20:26 MEM U REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-30 POS: 3 SRL: 120148 TAG NBR: 28H905
- [SDR FDEA202110082521](https://openairdocs.org/sdr/FDEA202110082521.md): Web · cracked · Oct 8, 2021 · N682FE · Airbus A300* · Nacelle/Pylon Structure
  > NO.2 ENG EXTERAL PYLON BOX (R/H) HAVE CRACK ON THE RIB8 REPLACED THE DAMAGED WEB WITH NEW ONE BY FASTENERS I.A.W. A300-600F SRM 51-72-10- 001, P. 2 AND 51-40-21-001, PARA. 6, P. 7B-23.
- [SDR FDEA202110082520](https://openairdocs.org/sdr/FDEA202110082520.md): Web · cracked · Oct 8, 2021 · N682FE · Airbus A300* · Nacelle/Pylon Structure
  > NO.1 PYLON BOX OUTSIDE SKIN HAS CRACKS ON THE RIB 8 BOTH SIDE. CRACKED RIB 8 WEB REPLACED NEW PART. INSTALLED WITH RIVETS AND FASTENERS I.A.W A300-600F SRM 51-72-10-001, PAGE 2 AND SRM 51-40-21-001,PARA 6 PAGE 7B -PAGE 23
- [SDR FDEA202110042505](https://openairdocs.org/sdr/FDEA202110042505.md): Stiffener · cracked · Oct 4, 2021 · N682FE · Airbus A300F4605R · Nacelle/Pylon Structure
  > RH PYLON FORWARD FAIRING STIFFENER CRACKED AT THE RIB JO0 FWD AREA REINFORCED REPAIR DOUBLER & ANGLE WORK INSTRUCTION I.A.W. A300-600F SRM 54-54-11- 201- 2, PARA. 5A, PAGE 201-207, FIG. 201.
- [SDR FDEA202110022531](https://openairdocs.org/sdr/FDEA202110022531.md): Floor Panel · damaged · Oct 2, 2021 · N682FE · Airbus A300* · Fuselage Floor Panel
  > THE #232HG FLOOR PANEL OF MDC WAS FOUND DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.
- [SDR FDEA202110022530](https://openairdocs.org/sdr/FDEA202110022530.md): Floor Panel · damaged · Oct 2, 2021 · N682FE · Airbus A300* · Fuselage Floor Panel
  > THE 241BK PANEL OF MDC WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.
- [SDR FDEA202110022527](https://openairdocs.org/sdr/FDEA202110022527.md): Floor Panel · damaged · Oct 2, 2021 · N682FE · Airbus A300* · Fuselage Floor Panel
  > THE #252UH FLOOR PANEL OF MDC WAS FOUND EDGE DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.
- [SDR FDEA202110012549](https://openairdocs.org/sdr/FDEA202110012549.md): Seat Track · unknown · Oct 1, 2021 · N682FE · Airbus A300* · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR36 TO FR37,-Y450 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 53-10
- [SDR FDEA202110012548](https://openairdocs.org/sdr/FDEA202110012548.md): Seat Track · unknown · Oct 1, 2021 · N682FE · Airbus A300* · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR30 TO FR31,-Y1456 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 53-1
- [SDR FDEA202110012547](https://openairdocs.org/sdr/FDEA202110012547.md): Seat Track · unknown · Oct 1, 2021 · N682FE · Airbus A300* · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR29 TO FR30,-Y953 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 53-10
- [SDR FDEA202110012532](https://openairdocs.org/sdr/FDEA202110012532.md): Floor Panel · damaged · Oct 1, 2021 · N682FE · Airbus A300* · Fuselage Floor Panel
  > THE 251RH FLOOR PANEL OF MDC WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.
- [SDR FDEA202110012529](https://openairdocs.org/sdr/FDEA202110012529.md): Floor Panel · damaged · Oct 1, 2021 · N682FE · Airbus A300* · Fuselage Floor Panel
  > THE 251XG FLOOR PANEL OF MDC WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.
- [SDR FDEA202110012528](https://openairdocs.org/sdr/FDEA202110012528.md): Floor Panel · damaged · Oct 1, 2021 · N682FE · Airbus A300* · Fuselage Floor Panel
  > THE 231FH FLOOR PANEL OF MDC WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.
- [SDR FDEA202110012506](https://openairdocs.org/sdr/FDEA202110012506.md): Access Door · cracked · Oct 1, 2021 · N682FE · Airbus A300F4605R · Service Doors
  > AFTER PAINT REMOVAL FOUND EQUIPMENT COMPARTMENT ACCESS DOOR 1 EA CRACK AT AFT UPPER LATCH CUTOUT AREA. CUT OUT THE DAMAGED AREA. FABRICATED THE REPAIR DOUBLER AND INSTALLED THEM WITH RIVETS I.A.W. A300-600F SRM 52-41-12-201, PARA. 5, FIG. 201, P. 202-205
- [SDR FDEA202109272553](https://openairdocs.org/sdr/FDEA202109272553.md): Skin · unknown · Sep 27, 2021 · N682FE · Airbus A300* · Wing, Plate/Skin
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON LH WING LWR L/E PANEL 513AB CUTOUT FWD O/B POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F
- [SDR FDEA202109272552](https://openairdocs.org/sdr/FDEA202109272552.md): Skin · unknown · Sep 27, 2021 · N682FE · Airbus A300* · Wing, Plate/Skin
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON R/H WING LWR L/E PANEL 613AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM
- [SDR FDEA202109272551](https://openairdocs.org/sdr/FDEA202109272551.md): Skin · unknown · Sep 27, 2021 · N682FE · Airbus A300* · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON FUSELAGE SKIN BTW FR101 TO FR103 AND STR-2L TO STR-5L POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DAT
- [SDR FDEA202109272550](https://openairdocs.org/sdr/FDEA202109272550.md): None · unknown · Sep 27, 2021 · N682FE · Airbus A300* · Standard Practices/Structures
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON RUDDER TRAILING EDGE APEX AREA LOCATED BTW T/E SCREW LINE NO.20 AND NO.21 FASTENER COUNTED FROM LOWER SIDE. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETER
- [SDR FDEA202109252467](https://openairdocs.org/sdr/FDEA202109252467.md): Stiffener · bent · Sep 25, 2021 · N682FE · Airbus A300F4605R · Fuselage Main, Structure
  > AGING AIRCRAFT RECORDS REVIEW:AT THE TIME OF RECORDS REVIEW THE FOLLOWING WAS IDENTIFIED ON W/O 67250,SNRM N00580, PRIMARY STRUCTURE REMOVED AND REPLACED, PRIMARY STRUCTURE LOCALLY FABRICATED, SEE JPF ITEM 5, AND TRAVELER T16/1235154, SNRM BLOCK 16 NOT I
- [SDR FDEA202109242488](https://openairdocs.org/sdr/FDEA202109242488.md): Rib · cracked · Sep 24, 2021 · N682FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB 26AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364452 P1, TITLE: WING-FLIGHT SURFACES-LH CENTER FLAP, CRACK IN UPPER FLANGE OF RIB26 AT STRINGERS 2.8-ALI 575306-0
- [SDR FDEA202109212526](https://openairdocs.org/sdr/FDEA202109212526.md): Floor Panel · damaged · Sep 21, 2021 · N682FE · Airbus A300* · Fuselage Floor Panel
  > FWD CARGO COMPT #131KG FLOOR PANEL WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B FIG. 203 SHEET 1, P. 209-211.
- [SDR FDEA202109212525](https://openairdocs.org/sdr/FDEA202109212525.md): Floor Panel · damaged · Sep 21, 2021 · N682FE · Airbus A300* · Fuselage Floor Panel
  > FWD CARGO COMPT #131LG FLOOR PANEL WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B FIG. 203 SHEET 1, P. 209-211.
- [SDR FDEA202109212524](https://openairdocs.org/sdr/FDEA202109212524.md): Floor Panel · damaged · Sep 21, 2021 · N682FE · Airbus A300* · Fuselage Floor Panel
  > FWD CARGO COMPT #131QG FLOOR PANEL WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203 SHEET 1, P. 209-211.
- [SDR FDEA202109182358](https://openairdocs.org/sdr/FDEA202109182358.md): Floor Panel · damaged · Sep 18, 2021 · N682FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #147CF KEEL BEAM FLOOR WAS FOUND SOFTEN AND CAUSE BY HYD FLUID CONTAMINATION FABRICATED FLOOR PANEL #147CF I.A.W FEDEX DWG SRZ-25-005 REV.R
- [SDR FDEA202106081471](https://openairdocs.org/sdr/FDEA202106081471.md): Isolation Valve · leaking · Jun 8, 2021 · N682FE · Airbus A300F4605R · Hydraulic System, Main
  > PDIS 682 29-10 9603 08JUN21 JFK OPEN U AT FL 240 RECEIVED ECAM WARNING FOR YELLOW HYD SYSTEM LO PRESSURE. AFTER ANALYZING WE FOUND LOSS OF ALL YELLOW HYDRAULIC FLUID. RAN QRH, DECLARED EMERGENCY AND LANDED. AMM: 27-14-21-04 REMOVED AND REPLA
- [SDR FDEA2019121323235](https://openairdocs.org/sdr/FDEA2019121323235.md): Manifold · cracked · Dec 12, 2019 · N682FE · Airbus A300F4605R · Hydraulic System, Main
  > ABOUT 15-20 MINS AFTER LEVEL OFF AT 350FL WE NOTICED THAT THE GREEN HYD LEVEL WAS LOW. 10 MINS LATER WE GOT A GREEN LOW FLUID LEVEL ON THE ECAM. FOLLOWED PROCEDURES AND SECURED THE GREEN SYSTEM. DURING THE REST OF THE FLIGHT WE RECIEVED MANY GREEN LOW LEVEL
- [SDR FDEA2019032760731](https://openairdocs.org/sdr/FDEA2019032760731.md): Floor Panel · damaged · Mar 26, 2019 · N682FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 252VF HAS DAMAGE. FABRICATED NEW FLOOR PANEL 252VF ON VT MAE TRAVELER T19/1403082 IAW DWG SRZ-25- 005. CAT "A" MAJOR REPAIR
- [SDR FDEA2019032760729](https://openairdocs.org/sdr/FDEA2019032760729.md): Floor Panel · damaged · Mar 26, 2019 · N682FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 252GF HAS DAMAGE. FABRICATED NEW FLOOR PANEL 252GF ON VT MAE TRAVELER T19/1403192 IAW DWG SRZ-25- 005. CAT "A" MAJOR REPAIR
- [SDR FDEA201903260733](https://openairdocs.org/sdr/FDEA201903260733.md): Floor Panel · damaged · Mar 26, 2019 · N682FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231QG IS BROKEN FABRACATED NEW FLOOR PANEL 231QG ON T19/1403671 IAW DWG SRZ-25-005 CAT "A" MAJOR REPAIR.
- [SDR FDEA201903260732](https://openairdocs.org/sdr/FDEA201903260732.md): Floor Panel · damaged · Mar 26, 2019 · N682FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 261XF AFT INBD INSERT PULLED THROUGH PANEL. FABRICATED NEW FLOOR PANEL 261XF ON T19/1403254 IAW DWG SRZ-25-005 MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N682FE/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 = 'N682FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N682FE/reports

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