# Service difficulty reports: N724FD

A list on [N724FD](https://openairdocs.org/aircraft/N724FD.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 · 218 reports

- [SDR FDEA202605010531](https://openairdocs.org/sdr/FDEA202605010531.md): Bottle · discharged · May 1, 2026 · N724FD · Airbus A300B4622R · Passenger/Crew Doors
  > WHILE WORKING WRIS 25-60-2704 AND 52-10-2698. MECHANICS OPENED THE L1 DOOR AND THE EMERGENCY DOOR ASSIST BOTTLE DISCHARGED WITH THE HANDLE IN THE DISARMED POSTION AND THE SAFETY PIN INSTALLED. SERVICED L1 FWD DOOR DAMPER AND EMERGENCY OPERATION CYLINDER
- [SDR FDEA202604250502](https://openairdocs.org/sdr/FDEA202604250502.md): Girt Bar · out of adjust · Apr 25, 2026 · N724FD · Airbus A300B4622R · Emergency Equipment
  > DOOR 1L WOULD NOT DISARM AFTER THE FLIGHT. RELEASED FOR SERVICE IAW MEL 52-11-01-05. CREW ENTRY DOOR L1 INOP. MEL 52-11-01-05. FOUND L1 DOOR GIRT BAR MISALIGNED AND RE ADJUSTED GIRT BAR IN REF TO 25-61-22-04-01.COMPLETED INSTALL OF L1 DOOR SLIDE/RAFT
- [SDR FDEA202603250373](https://openairdocs.org/sdr/FDEA202603250373.md): Packing · leaking · Mar 25, 2026 · N724FD · Airbus A300B4622R · Hydraulic System, Main
  > AT CRUISE GOT GREEN HYD LOW QTY. BOTH ECAM AND OVERHEAD GAGE SHOWED ALL FLUID LOST. USED MANUAL GEAR EXTENSION. AFTER LANDING, GREEN HYD QTY BACK INTO GREEN RANGE, BUT BELOW TOP HAT. EMERGENCY DECLARED AFTER BREIF WITH FLIGHT CREW, WHEN ECAM MESSAGE APPE
- [SDR FDEA202506231027](https://openairdocs.org/sdr/FDEA202506231027.md): Power Supply · failed · Jun 23, 2025 · N724FD · Airbus A300B4622R · Door Warning System
  > WHILE WORKING WRI 05-25/1837, ASPSU TEST SHOWED BATTERY 1 FAULT. AMM: 52-73-18-04 REMOVED AND REPLACED ASPSU EMERGENCY POWER SUPPLY BATTERY 1( AERO DESIGN, INC., PN: AD-3214-31, SN: 246253). OPS CHECK GOOD. OK FOR SERVICE.
- [SDR FDEA202501240123](https://openairdocs.org/sdr/FDEA202501240123.md): Failsafe · cracked · Jan 24, 2025 · N724FD · Airbus A300B4622R · Fuselage Main, Structure
  > HFEC INSPECTION OF REWORKED AREA ON LH #1 DOOR FAIL SAFE RING FWD LWR CORNER FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5312-82930 C P3. TITLE: FUSELAGE NOSE SECTION - EXFOLIATION CORROSION AT FAIL SAFE RING ON DOOR #1 LHS. REPAIRED THE LH #1 DOOR FAIL SAFE RI
- [SDR FDEA202412301852](https://openairdocs.org/sdr/FDEA202412301852.md): Skin · contaminated · Dec 30, 2024 · N724FD · Airbus A300B4622R · Elevator, Plate/Skin
  > LEFT ELEVATOR TOP SKIN FOUND WATER INGRESS BETWEEN ER2 AND ER3. REPAIRED THE DAMAGED AREA OF LH ELEVATOR TOP SKIN BETWEEN ER2 AND ER3 PER A300-600 SRM55-21-12-201 PARA.5.J & SRM51-77-12-201. TRACKING EA 6-5520-T0381697 P1 RAISED AND ACCOMPLISHED. TITLE: ST
- [SDR FDEA202412181813](https://openairdocs.org/sdr/FDEA202412181813.md): Frame Splice · cracked · Dec 18, 2024 · N724FD · Airbus A300B4622R · Fuselage Main, Frame
  > FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STGR24LH & STGR26LH FASTENER HOLE H FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5310-T0313717 B P3. TITLE: FUSELAGE - MAINFRAME - FASTENER HOLES CRACKED C/T FRAME 47 SPLICE FITTING BETWEEN STR 24 & 26 (EO 6-5310-7-5017 P
- [SDR FDEA202412131797](https://openairdocs.org/sdr/FDEA202412131797.md): Frame · cracked · Dec 13, 2024 · N724FD · Airbus A300B4622R · Fuselage Main, Frame
  > CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "G" HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA: 6-5710-T0381607 P1. TITLE: WINGS - BASIC WING STRUCTURE - LH WING FR47 REAR SPAR HOLE G CRACK REPAIR
- [SDR FDEA202412041773](https://openairdocs.org/sdr/FDEA202412041773.md): Spoiler · delaminated · Dec 4, 2024 · N724FD · Airbus A300B4622R · Spoilers
  > RH WING #4 SPOILER CENTER I/B & O/B HINGE ARM LWR SURFACES AND CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: (1)32MM*15MM, DEPTH: 2.4MM (2)43MM*16MM, DEPTH: 2.3MM (3)45MM*15MM, DEPTH: 1.0MM COMPLIED WITH EA: 6-5750-T0351531 A P2. TITLE: WI
- [SDR FDEA202412041772](https://openairdocs.org/sdr/FDEA202412041772.md): Spoiler · delaminated · Dec 4, 2024 · N724FD · Airbus A300B4622R · Spoilers
  > RH WING #3 SPOILER CENTER I/B & O/B HINGE ARM LWR SURFACES AND CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: (1)65MM*27MM, DEPTH: 2.5MM (2)50MM*20MM, DEPTH: 2.5MM (3)30MM*25MM, DEPTH: 1.3MM COMPLIED WITH EA: 6-5750-T0351530 A P2. TITLE: WI
- [SDR FDEA202412011758](https://openairdocs.org/sdr/FDEA202412011758.md): Web · cracked · Dec 1, 2024 · N724FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FR47, Y953-Y1456 UNDERFLOOR WEB CRACKED REPAIRED THE MAIN DECK FR47, Y953-Y1456 UNDERFLOOR CRACKED WEB PER SRM53-15-15-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER SRI53-15-15-2-001-00. INSPECTION THRESHOLD FR
- [SDR FDEA202412011757](https://openairdocs.org/sdr/FDEA202412011757.md): Pressure Deck · corroded · Dec 1, 2024 · N724FD · Airbus A300B4622R · Fuselage Main, Structure
  > BAY AFT OF FWD CARGO COMPT. - HORIZONTAL PRESSURE DECK UPR SURFACE BETWEEN FR39 AND FR40 RH SIDE O/B OF -Y2354 FOUND CORROSION COMPLIED WITH EA: 6-5310-T0381667 P1. TITLE: FUSELAGE - MAINFRAME- EXFOLIATED CORROSION ON HORIZONTAL PRESSURE FLOOR PANEL BETWE
- [SDR FDEA202412011756](https://openairdocs.org/sdr/FDEA202412011756.md): Pressure Deck · corroded · Dec 1, 2024 · N724FD · Airbus A300B4622R · Fuselage Main, Structure
  > BAY AFT OF FWD CARGO COMPT. - HORIZONTAL PRESSURE DECK UPR SURFACE BETWEEN FR39 AND FR40 LH SIDE O/B OF Y2354 FOUND CORROSION COMPLIED WITH EA: 6-5310-T0381667 P1. TITLE: FUSELAGE - MAINFRAME- EXFOLIATED CORROSION ON HORIZONTAL PRESSURE FLOOR PANEL BETWEE
- [SDR FDEA202410061430](https://openairdocs.org/sdr/FDEA202410061430.md): Battery · no test · Oct 6, 2024 · N724FD · Airbus A300B4622R · Emergency Lighting
  > DURING SERVICE CHECK EMERGENCY LIGHTS TEST FAILED R/I 06OCT24 09:00 MEM REASON CODE: PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-31 POS: 3 SRL: 243581 ON MPN: AD-3214-31 CPN: 3310373 SRL: 243726
- [SDR FDEA202212152917](https://openairdocs.org/sdr/FDEA202212152917.md): Flap System · faulted · Dec 15, 2022 · N724FD · Airbus A300B4622R · Trailing Edge Flap Control System
  > WHEN SELECTING FLAPS 20 RECEIVED A FLAPS SYSTEM 2 FAULT. DISCONTINUED APPROACH, REVIEWED QRH AND RETURNED FOR LANDING, SELECTED FLAPS 40 NO FURTHER ISSUES. SFCC-2 SHOWED ALL FLAP FAULT BALLS. RESET SAME AND BITE CHECK PASSED. RAN NR 1 ENG IAW JRH AND RAN
- [SDR FDEA202211042730](https://openairdocs.org/sdr/FDEA202211042730.md): Fire Loop · faulted · Nov 4, 2022 · N724FD · Airbus A300B4622R · Detection System
  > ON DEPARTURE PASSING THRU 12000 FT, ENG 2 LOOP A FAULT WENT ON & OFF. PACK 2 FAULT CAME ON & WENT OFF, MAIN CARGO SMOKE ILLUMINATED FOR 15 SECS WENT OFF, CAME BACK ON FOR 15 SECS & WENT OFF, CAME BACK ON FOR APPROX 1 MIN. COMPLIED WITH ECAM, DECLARED AN EM
- [SDR FDEA202207131793](https://openairdocs.org/sdr/FDEA202207131793.md): Flap · inoperative · Jul 13, 2022 · N724FD · Airbus A300* · Trailing Edge Flap Actuator
  > PDIS 724 27-80 8940 13JUL22 NRT FACT U UPON SLAT EXTENSION FOR LANDING, RECEIVED FLT CTL, KRUGER NOT EXTENDED ECAM MESSAGE. MEL 15JUL22 06:51 NRT RELEASED FOR SERVICE PER MEL
- [SDR FDEA202206201615](https://openairdocs.org/sdr/FDEA202206201615.md): None · none · Jun 20, 2022 · N724FD · Airbus A300* · Fuselage Structure (General)
  > THE LOWER FUSELAGE SKIN WAS FOUND CHAFFING AT FR66 STR 51-52R LOWER AREA WITH MARK. CUT OUT THE DAMAGE AND INSTALLED THE FILLER AND REPAIR DOUBLER, THIS IS CAT.B REPAIR. I.A.W A300-600 SRM 53-10-12-201 PARA.6 PAGE.357-360 FIG.225 (SHEET.3), SRI:53-10-12-
- [SDR FDEA202206181632](https://openairdocs.org/sdr/FDEA202206181632.md): Floor Panel · dented · Jun 18, 2022 · N724FD · Airbus A300* · Fuselage Structure (General)
  > AT THE TIME OF AGING AIRCRAFT INSPRCEION,FOUND FLOOR PANEL 162HF HAS SEVERAL IMPACT DAMAGES IN THE BULK COMPARTMENT. MEASURED THE SEVERAL DAMAGES WITHIN REPAIRABLE LIMITS AND FILLED WITH FILLER I.A.W A300-600 S.R.M 53-10-20-201 PARA.10A, PAGE. 212-213,
- [SDR FDEA202206141635](https://openairdocs.org/sdr/FDEA202206141635.md): Floor Panel · dented · Jun 14, 2022 · N724FD · Airbus A300* · Fuselage Structure (General)
  > AT THE TIME OF AGING AIRCRAFT INSPRCEION,FOUND FLOOR PANEL 161GF HAS SEVERAL IMPACT DAMAGES IN THE BULK COMPARTMENT. MEASURED THE SEVERAL DAMAGES WITHIN REPAIRABLE LIMITS AND FILLED WITH ADHESIVE I.A.W A300-600 S.R.M 53-10-20-201 PARA.10A, PAGE.212-213,
- [SDR FDEA202206091480](https://openairdocs.org/sdr/FDEA202206091480.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR LWR SKIN LOCATED AT ER10-725MM FRONT SPAR 70MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON LH ELEVATOR (PN:A55276055000-95, SN:CG-1059), REF TO EA:6-5520-9214
- [SDR FDEA202206091471](https://openairdocs.org/sdr/FDEA202206091471.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR UPR SKIN LOCATED AT ER 6 T/E -220MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON LH ELEVATOR (PN:A55276055000-95, SN:CG-1059), REF TO EA:6-5520-92148C P2, TITL
- [SDR FDEA202206091426](https://openairdocs.org/sdr/FDEA202206091426.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR UPR SKIN LOCATED AT ER 2 450MM, T/E -115MM POSITION. FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON LH ELEVATOR (PN:A55276055000-95, SN:CG-1059), REF TO EA:6-5520-92148C P
- [SDR FDEA202206091502](https://openairdocs.org/sdr/FDEA202206091502.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR UPR SKIN LOCATED AT ER 5-410MM FRONT SPAR 390MM POSITION ACCOMPLISHED THE CATE.B COMPOSITE REPAIR WITH REPAIR PLIES AND EPOXY RESIN, SEE JPF FOR DETAIL INFORMATION I.A.W A300-60
- [SDR FDEA202206091500](https://openairdocs.org/sdr/FDEA202206091500.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR LWR SKIN LOCATED AT ER 6 80MM T/E-235MM POSITION ACCOMPLISHED THE CATE.B COMPOSITE REPAIR WITH REPAIR PLIES AND EPOXY RESIN, SEE JPF FOR DETAIL INFORMATION I.A.W A300-600 SRM 55-
- [SDR FDEA202206091498](https://openairdocs.org/sdr/FDEA202206091498.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR LWR SKIN LOCATED AT ER 7 100MM T/E-200MM POSITION ACCOMPLISHED THE CATE.B COMPOSITE REPAIR WITH REPAIR PLIES AND EPOXY RESIN, SEE JPF FOR DETAIL INFORMATION I.A.W A300-600 SRM 55
- [SDR FDEA202206091497](https://openairdocs.org/sdr/FDEA202206091497.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON R/H ELEVATOR UPR SKIN LOCATED AT ER16-190MM T/E-190MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON RH ELEVATOR (PN:A5527605600096, SN:CG1079), REFER TO EA NO:6-5520-92149B
- [SDR FDEA202206091482](https://openairdocs.org/sdr/FDEA202206091482.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR LWR SKIN LOCATED AT ER 16 330MM FRONT SPAR 140MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON LH ELEVATOR (PN:A55276055000-95, SN:CG-1059), REF TO EA:6-5520-921
- [SDR FDEA202206091481](https://openairdocs.org/sdr/FDEA202206091481.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR LWR SKIN LOCATED AT ER10 450MM T/E-115MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON LH ELEVATOR (PN:A55276055000-95, SN:CG-1059), REF TO EA:6-5520-92148C P2,
- [SDR FDEA202206091478](https://openairdocs.org/sdr/FDEA202206091478.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR LWR SKIN LOCATED AT ER 7 230MM FRONT SPAR 85MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON LH ELEVATOR (PN:A55276055000-95, SN:CG-1059), REF TO EA:6-5520-92148
- [SDR FDEA202206091477](https://openairdocs.org/sdr/FDEA202206091477.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR LWR SKIN LOCATED AT ER 5-270MM T/E-190MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON LH ELEVATOR (PN:A55276055000-95, SN:CG-1059), REF TO EA:6-5520-92148C P2,
- [SDR FDEA202206091476](https://openairdocs.org/sdr/FDEA202206091476.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR LWR SKIN LOCATED AT ER 2 270MM T/E-350MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON LH ELEVATOR (PN:A55276055000-95, SN:CG-1059), REF TO EA:6-5520-92148C P2,
- [SDR FDEA202206091475](https://openairdocs.org/sdr/FDEA202206091475.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR LWR SKIN LOCATED AT ER 2 290MM T/E-170MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON LH ELEVATOR (PN:A55276055000-95, SN:CG-1059), REF TO EA:6-5520-92148C P2,
- [SDR FDEA202206091474](https://openairdocs.org/sdr/FDEA202206091474.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR LWR SKIN LOCATED AT ER 5-480MM FRONT SPAR 420MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON LH ELEVATOR (PN:A55276055000-95, SN:CG-1059), REF TO EA:6-5520-921
- [SDR FDEA202206091473](https://openairdocs.org/sdr/FDEA202206091473.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR LWR SKIN LOCATED AT ER 5-430MM FRONT SPAR 120MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON LH ELEVATOR (PN:A55276055000-95, SN:CG-1059), REF TO EA:6-5520-921
- [SDR FDEA202206091472](https://openairdocs.org/sdr/FDEA202206091472.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR UPR SKIN LOCATED AT ER13 300MM T/E -390MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON LH ELEVATOR (PN:A55276055000-95, SN:CG-1059), REF TO EA:6-5520-92148C P
- [SDR FDEA202206091470](https://openairdocs.org/sdr/FDEA202206091470.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON L/H ELEVATOR UPR SKIN LOCATED AT ER 5 15MM T/E -240MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON LH ELEVATOR (PN:A55276055000-95, SN:CG-1059), REF TO EA:6-5520-92148C P2,
- [SDR FDEA202206091469](https://openairdocs.org/sdr/FDEA202206091469.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON R/H ELEVATOR LWR SKIN LOCATED AT ER 5 230MM FRONT SPAR 260MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON RH ELEVATOR (PN:A5527605600096, SN:CG1079), REFER TO EA NO:6-5520-
- [SDR FDEA202206091468](https://openairdocs.org/sdr/FDEA202206091468.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON R/H ELEVATOR LWR SKIN LOCATED AT ER 6 150MM FRONT SPAR 270MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON RH ELEVATOR (PN:A5527605600096, SN:CG1079), REFER TO EA NO:6-5520-
- [SDR FDEA202206091467](https://openairdocs.org/sdr/FDEA202206091467.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON R/H ELEVATOR LWR SKIN LOCATED AT ER 7 355MM FRONT SPAR 230MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON RH ELEVATOR (PN:A5527605600096, SN:CG1079), REFER TO EA NO:6-5520-
- [SDR FDEA202206091466](https://openairdocs.org/sdr/FDEA202206091466.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON R/H ELEVATOR LWR SKIN LOCATED AT ER10 290MM FRONT SPAR 390MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON RH ELEVATOR (PN:A5527605600096, SN:CG1079), REFER TO EA NO:6-5520-
- [SDR FDEA202206091465](https://openairdocs.org/sdr/FDEA202206091465.md): Elevator · unknown · Jun 9, 2022 · N724FD · Airbus A300* · Elevator Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING COMPOSITE REPAIR FOUND ON R/H ELEVATOR UPR SKIN LOCATED AT ER16-190MM T/E-190MM POSITION FOUND EXISTING REPAIR WITHOUT APPROVED DOCUMENTATION ON RH ELEVATOR (PN:A5527605600096, SN:CG1079), REFER TO EA NO:6-5520-92149B
- [SDR FDEA202206071644](https://openairdocs.org/sdr/FDEA202206071644.md): Floor Panel · damaged · Jun 7, 2022 · N724FD · Airbus A300* · Fuselage Structure (General)
  > AFT CARGO COMPT #152KF FLOOR PANEL WAS FOUND INSERTS DAMAGED. REPAIRED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005.
- [SDR FDEA202206061515](https://openairdocs.org/sdr/FDEA202206061515.md): None · unknown · Jun 6, 2022 · N724FD · Airbus A300* · Fuselage Structure (General)
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING STRINGER REPAIR FOUND ON FWD CARGO COMPARTMENT BTW FR30~31,STGR36L POSITION COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310.RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTING REPAIR D
- [SDR FDEA202206041642](https://openairdocs.org/sdr/FDEA202206041642.md): Floor Panel · damaged · Jun 4, 2022 · N724FD · Airbus A300* · Fuselage Structure (General)
  > THE #241PH FLOOR PANEL WAS FOUND 2EA INSERT DAMAGED REPLACED THE DAMAGED INSERT WITH NEW ONE I.A.W FEDEX DRAWING NO:SRZ-25-005.
- [SDR FDEA202206041641](https://openairdocs.org/sdr/FDEA202206041641.md): Floor Panel · damaged · Jun 4, 2022 · N724FD · Airbus A300* · Fuselage Structure (General)
  > THE #242SF FLOOR PANEL WAS FOUND 3EA INSERT DAMAGED REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005.
- [SDR FDEA202206041637](https://openairdocs.org/sdr/FDEA202206041637.md): Floor Panel · damaged · Jun 4, 2022 · N724FD · Airbus A300* · Fuselage Structure (General)
  > THE #242NH FLOOR PANEL WAS FOUND 2EA INSERT DAMAGED REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005.
- [SDR FDEA202206041636](https://openairdocs.org/sdr/FDEA202206041636.md): Floor Panel · damaged · Jun 4, 2022 · N724FD · Airbus A300* · Fuselage Structure (General)
  > THE #242TG FLOOR PANEL WAS FOUND 2EA INSERT DAMAGED REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005.
- [SDR FDEA202206041519](https://openairdocs.org/sdr/FDEA202206041519.md): Fitting · damaged · Jun 4, 2022 · N724FD · Airbus A300* · Horizontal Stabilizer Structure
  > RH THS SPAR BOX INTERNAL FOUND I'B-FWD HOIST POINT FITTING DAMAGE AT RIB 5 AREA. REPLACED THE HOIST POINT FITTING WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001, PAGE.2
- [SDR FDEA202206041514](https://openairdocs.org/sdr/FDEA202206041514.md): Fitting · damaged · Jun 4, 2022 · N724FD · Airbus A300* · Horizontal Stabilizer Structure
  > LH THS SPAR BOX INTERNAL FOUND O'B-AFT HOIST POINT FITTING CORROSION AT RIB 14 AREA. REPLACED THE HOIST POINT FITTING WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001, PAGE.2

Next page: https://openairdocs.org/aircraft/N724FD/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 = 'N724FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N724FD/reports

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