# Service difficulty reports: N721FD

A list on [N721FD](https://openairdocs.org/aircraft/N721FD.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 · 231 reports

- [SDR FDEA202609291451](https://openairdocs.org/sdr/FDEA202609291451.md): Drain Line · misinstalled · Sep 29, 2026 · N721FD · Airbus A300B4622R · Hydraulic System, Main
  > DURING THE CLIMB TO FL160 WE NOTICED THE GREEN HYD SYS QITY DECREASING. GREEN HYD SYSTEM CONTINUED TO ZERO ON BOTH ECAM AND OVERHEAD GAUGE. THE BLUE OVER-HEAD HYD SYSTEM QUANTITY INCREASED TO SHOWING OFF SCALE FULL. FOLLOWED ECAM & QRH PROCEDURES INCLUDING
- [SDR FDEA202609091296](https://openairdocs.org/sdr/FDEA202609091296.md): Slide · malfunctioned · Sep 9, 2026 · N721FD · Airbus A300B4622R · Escape Slide
  > AT BLOCK IN L1 DOOR SLIDE WILL NOT DISARM. MEL 09SEP26 18:17 IND RELEASED FOR SERVICE IAW MEL 52-11-01-01, CATEGORY: C EXPIRATION: 19SEP26 MEL 52-11-01-01: CREW ENTRY DOOR ESCAPE SLIDE L1 - INOP. SLIDE REMAINS INSTALLED ON DOOR. MEL: 52-11-01-01 C/
- [SDR FDEA202602040120](https://openairdocs.org/sdr/FDEA202602040120.md): Slide · broken · Feb 4, 2026 · N721FD · Airbus A300B4622R · Escape Slide
  > R1 DOOR SLIDE ASSEMBLY HAS BROKEN BATTERY HARD SHELL. RELEASED FOR SERVICE PER MEL: 52-11-01-01, CATEGORY: C. R1 DOOR ESCAPE SLIDE INOP. SLIDE REMAINS INSTALLED ON DOOR. REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-61-22-04-01. OPS CHECKS GOOD
- [SDR FDEA202602020137](https://openairdocs.org/sdr/FDEA202602020137.md): Slide Raft · inoperative · Feb 2, 2026 · N721FD · Airbus A300B4622R · Escape Slide
  > SMIS 721 25-60 MOD TYPE F MOD NO. 6-2560-F0386261 REV NO. PS P1 EQUIPMENT AND FURNISHINGS - EMERGENCY EVACUATION EQU IPMENT - VERIFICATION OF SAFETY WIRE MATERIAL ON SLIDE PACK BOARD RELEASE CABLE.:CPN 2513882 MPN D30546- 509 L1/R1 DOOR SLIDE. COMPLIED
- [SDR FDEA202511132170](https://openairdocs.org/sdr/FDEA202511132170.md): Door · faulted · Nov 13, 2025 · N721FD · Airbus A300B4622R · Passenger/Crew Doors
  > L1 DOOR WILL NOT DISARM. REVERSED MEL 52-11-01-01. FOUND WITH LOWER COVER REMOVED DOOR DISARMS AND ARMS NORMALLY. REINSTALLED LOWER COVER AND DOOR CONTINUES TO OPERATE NORMALLY. LOWER COVER WAS DAMAGED AND PLACED ON OIL REF WRI 52-10/5586.
- [SDR FDEA202511132169](https://openairdocs.org/sdr/FDEA202511132169.md): Slide · dislodged · Nov 13, 2025 · N721FD · Airbus A300B4622R · Escape Slide
  > LEFT FORWARD ENTRY DOOR WILL NOT DISARM. THE LEVER WILL NOT MOVE ALL THE WAY TO THE DISARM POSITION. MEL: 52-11-01-02 ESCAPE SLIDE CAME LOOSE FROM L1 DOOR, ESCAPE SLIDE REMOVED FROM DOOR, BUT REMAINS ONBOARD IN HAZMAT CONTAINER.
- [SDR FDEA202511132168](https://openairdocs.org/sdr/FDEA202511132168.md): Slide · faulted · Nov 13, 2025 · N721FD · Airbus A300B4622R · Passenger/Crew Doors
  > LEFT FORWARD ENTRY DOOR WILL NOT DISARM. THE LEVER WILL NOT MOVE ALL THE WAY TO THE DISARM POSITION. THIS ITEM WAS ON MEL 52-11-01-01. THE ESCAPE SLIDE HAS COME LOOSE FROM THE STORE, TRANSFERRING WRI 52-10/5579 TO THIS WRI AND PLACING ITEM ON MEL 52-11-
- [SDR FDEA202506060848](https://openairdocs.org/sdr/FDEA202506060848.md): O-Ring · failed · Jun 6, 2025 · N721FD · Airbus A300B4622R · Hydraulic System, Main
  > DURING DESCENT THROUGH FL200 ECAM INDICATED LOSS OF GREEN HYDRAULIC QUANTITY BELOW RED DOT. HYD RESV LOW. COMPLIED WITH ECAM AND QRH. PERFORMED MANUAL GEAR EXTENSION AND LANDED WITH NO FURTHER ISSUES. AFTER THE GEAR WAS EXTENDED GREEN HYDRAULIC SYSTEM R
- [SDR FDEA202502010199](https://openairdocs.org/sdr/FDEA202502010199.md): Rib · cracked · Feb 1, 2025 · N721FD · Airbus A300B4622R · Trailing Edge Flaps
  > RH WING CENTER FLAP PERFORM EA NO.:6-5750-T0381883 P1 STEP 4.A. DVI FOUND RIB 27 FLANGE CRACK BETWEEN STRINGER 2.7 AND REAR SPAR AREA. PERFORMED CUT OUT DAMAGED FLANGES AND INSTALLED REPAIR ANGLES AT RH WING CENTER FLAP RIB27, S-2.7~REAR SPAR AND EXTERNA
- [SDR FDEA202501210207](https://openairdocs.org/sdr/FDEA202501210207.md): Stringer Splice · worn · Jan 21, 2025 · N721FD · Airbus A300B4622R · Fuselage Main, Longeron/Stringer
  > SPLICE HOLE ELONGATION AT FR54 STGR 44RH SIDE. REPLACED THE DAMAGED SPLICE WITH NEW FABRICATED SPLICE AT LOWER FUSELAGE FR54, S- 44R. I.A.W A300-600 SRM 51-72-10-001, PAGE.2& AIRBUS DWG NO:A53812405, REV.C00& FEDEX GMM 07-0-1001. THIS REPAIR IS CLASSIFIED A
- [SDR FDEA202501200239](https://openairdocs.org/sdr/FDEA202501200239.md): Fitting · not reported · Jan 20, 2025 · N721FD · Airbus A300B4622R · Fuselage Structure (General)
  > REPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24 PER EO NO: E6- 5230-E0378588 B P5 REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24, LONGN1~3. I.A.W FEDEX EO NO: E6-5230-E0378588 B P5, SEQ NO:981, TITLE: DOORS-CARGO DOOR/H
- [SDR FDEA202501200238](https://openairdocs.org/sdr/FDEA202501200238.md): Fitting · not reported · Jan 20, 2025 · N721FD · Airbus A300B4622R · Fuselage, Landing Gear Attach Fittings
  > REPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER EO NO: E6- 5230-E0378588 B P5 REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23, LONGN1~3. I.A.W FEDEX EO NO: E6-5230-E0378588 B P5, SEQ NO:981, TITLE: DOORS-CARGO DOOR/H
- [SDR FDEA202501190220](https://openairdocs.org/sdr/FDEA202501190220.md): Rib · gouged · Jan 19, 2025 · N721FD · Airbus A300B4622R · Wing, Rib/Bulkhead
  > THE UPPER BORE GOUGE ON OUTBD JACK RIB OF R6 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT R6 SPOILER OUTBD JACK RIB UPPER BORE I.A.W FEDEX EA NO:T6-5740-T0382066 P1, SEQ NO:1014, TITLE:WINGS-ATTACH FITTINGS-RH WING #6 SPOILER JACK RIB AT STA SP1X31.675 A
- [SDR FDEA202501190219](https://openairdocs.org/sdr/FDEA202501190219.md): Rib · gouged · Jan 19, 2025 · N721FD · Airbus A300B4622R · Wing, Rib/Bulkhead
  > THE UPPER BORE GOUGE ON INBD JACK RIB OF R6 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT R6 SPOILER INBD JACK RIB UPPER BORE I.A.W FEDEX EA NO:T6-5740-T0382066 P1, SEQ NO:1014, TITLE:WINGS-ATTACH FITTINGS-RH WING #6 SPOILER JACK RIB AT STA SP1X31.675 AND
- [SDR FDEA202501190218](https://openairdocs.org/sdr/FDEA202501190218.md): Rib · gouged · Jan 19, 2025 · N721FD · Airbus A300B4622R · Wing, Rib/Bulkhead
  > THE LWR BORE GOUGE ON OUTBD JACK RIB OF R4 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT R4 SPOILER OUTBD JACK RIB LWR BORE I.A.W FEDEX EA NO:T6-5740-T0382065 P1, SEQ NO:1013, TITLE:WING-ATTACH FITTINGS-RH WING #4 SPOILER JACK RIB AT STA ABX112.525-BEAM A
- [SDR FDEA202501170198](https://openairdocs.org/sdr/FDEA202501170198.md): Rib · cracked · Jan 17, 2025 · N721FD · Airbus A300B4622R · Trailing Edge Flaps
  > 1EA CRACK (15MM) WAS FOUND AT R/H WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RH WING CENTER FLAP RIB26, S-2.8~REAR SPAR AND EXTERNAL PLATE AT RIB26~27,S-2.2~REAR SPAR FOR REPAIR
- [SDR FDEA202501170166](https://openairdocs.org/sdr/FDEA202501170166.md): Stringer · deformed · Jan 17, 2025 · N721FD · Airbus A300B4622R · Fuselage Main, Longeron/Stringer
  > TAIL STRUCTURAL FOUND S-36R STRAP DEFORM AT FR86 PLUS 10" AREA. REPLACED THE DAMAGE SECTION-L WITH NEW AT TAIL STRUCTURAL FR 86 PLUS 10" S-36R AREA I.A.W A300-600 SRM 51-72-10-001, PAGE 2. THIS REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.
- [SDR FDEA202501160196](https://openairdocs.org/sdr/FDEA202501160196.md): Seat Track · worn · Jan 16, 2025 · N721FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO COMPARTMENT WAS FOUND SEAT TRACK CROWN WORN AT FR58 PLUS 1", - Y1959 CUT THE DAMAGED SEAT TRACK, FABRICATED THE NEW REPAIR SEAT TRACK AND WET INSTALLED REPAIR PARTS WITH FASTENERS I.A.W A300-600 SRM 53-10-16-201, PARA 10, FIG 208, PAGE 243
- [SDR FDEA202501160188](https://openairdocs.org/sdr/FDEA202501160188.md): Angle · cracked · Jan 16, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > RA COAXIAL CABLE SUPPORT BRACKET CRACK AT FR58~59, STGR 44RH SIDE. REPLACED THE CRACKED RA COAXIAL CABLE SUPPORT BRACKET, AT FR58~59, STGR 44RH SIDE. I.A.W A300-600 SRM 51-72-10-001, PAGE 2. THIS REPAIR IS CLASSIFIED AS MINOR. PER GMM 6-2- 100.
- [SDR FDEA202501160187](https://openairdocs.org/sdr/FDEA202501160187.md): Angle · cracked · Jan 16, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > RA COAXIAL CABLE SUPPORT BRACKET CRACK AT FR64, STGR 50RH~51RH REPLACED THE CRACKED RA COAXIAL CABLE SUPPORT BRACKET, AT FR64, STGR 50RH~51RH. I.A.W A300-600 SRM 51-72-10-001, PAGE 2. THIS REPAIR IS CLASSIFIED AS MINOR, PER GMM 6-2-100
- [SDR FDEA202501160184](https://openairdocs.org/sdr/FDEA202501160184.md): Angle · damaged · Jan 16, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO COMPARTMENT AFT PRESSURE BULKHEAD RH LOWER AREA WAS FOUND 1EA SUPPORT ANGLE BROKEN AS MARKED,FR80/82 REPLACED THE BROKEN SUPPORT ANGLE, AT MAIN DECK CARGO COMPARTMENT AFT PRESSURE BULKHEAD RH LOWER AREA FR80/FR82. I.A.W A300-600 SRM 51-72-1
- [SDR FDEA202501150192](https://openairdocs.org/sdr/FDEA202501150192.md): Skin · damaged · Jan 15, 2025 · N721FD · Airbus A300B4622R · Rudder, Plate/Skin
  > 2EA WATER TRAPPED AREAS WERE FOUND AT LH RUDDER T/E SCREW LINE NO.19(30MM*40MM) FASTENER AND RH RUDDER T/E SCREW LINE NO.39(20MM*80MM) FASTENER. ACCOMPLISHED THE COMPOSITE REPAIR AT LH SKIN SCREW LINE #19 AND RH SKIN SCREW LINE #39 OF RUDDER I.A.W A300-600
- [SDR FDEA202501140195](https://openairdocs.org/sdr/FDEA202501140195.md): Skin · damaged · Jan 14, 2025 · N721FD · Airbus A300B4622R · Elevator, Plate/Skin
  > 1EA WATER TRAPPED AREA(80MM*80MM) WAS FOUND AT RH ELEVATOR LOWER SKIN PANEL T/E FASTENER NO.9. *COUNTING FASTENER FROM I/B TO O/B * ACCOMPLISHED THE COMPOSITE REPAIR AT RH ELEVATOR LOWER SKIN T/E FASTENER #9 I.A.W A300-600 SRM 55-21-12-201, PARA.5B, PAGE.2
- [SDR FDEA202501140194](https://openairdocs.org/sdr/FDEA202501140194.md): Skin · damaged · Jan 14, 2025 · N721FD · Airbus A300B4622R · Elevator, Plate/Skin
  > 2EA WATER TRAPPED AREAS(100MM*130MM,70MM*150MM) WERE FOUND AT LH ELEVATOR LOWER SKIN PANEL T/E FASTENER NO.18 AND NO.24. *COUNTING FASTENER FROM I/B TO O/B * ACCOMPLISHED THE COMPOSITE REPAIRS AT LH ELEVATOR LOWER SKIN T/E FASTENERS #18 AND #24 I.A.W A300
- [SDR FDEA202501130197](https://openairdocs.org/sdr/FDEA202501130197.md): Plate · cracked · Jan 13, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > SIDE PLATE CRACK AT FWD CARGO COMPT FRAME 20 TO 21, Y1420 LH UNDER FLOOR POSITION. REPLACED THE CRACK WALL WITH NEW PART AT FWD CARGO COMPARTMENT BETWEEN FR20 TO FR21, Y1420 I.A.W A300-600 SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B~23. THIS
- [SDR FDEA202501130186](https://openairdocs.org/sdr/FDEA202501130186.md): Profile · cracked · Jan 13, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE WAS FOUND PROFILE-Z CRACK AT FR80/82,Y1447 REPLACED THE DAMAGED PART WITH NEW ONE AND INSTALLED WITH FASTENERS. I.A.W A300-600 SRM 51-72-10-001, PAGE 2 AND SRM 51-40-21-001, PARA 6, PAGE 7B~PAGE23. THIS REPAIR IS CATEGORY A AND CL
- [SDR FDEA202501130185](https://openairdocs.org/sdr/FDEA202501130185.md): Floor Support · cracked · Jan 13, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE WAS FOUND PROFILE-Z CARCK AT FR80/82,-Y1447 REPLACED DAMAGE PROFILE-Z WITH NEW ONE AT MAIN DECK FLOOR STRUCTURE FR80/82, - Y1447. I.A.W A300-600 SRM 51-40-21-001, PARA 6 PAGE 7B - PAGE 23 & 51-72-10-001, PAGE 2. THIS REPAIR IS CLAS
- [SDR FDEA202501130183](https://openairdocs.org/sdr/FDEA202501130183.md): Shear Plate · cracked · Jan 13, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE WAS FOUND PLATE SHEAR CRACK AT FR79 PLUS 4", S-26L REPLACED THE DAMAGE PART WITH NEW ONE AND INSTALLED WITH FASTENERS. I.A.W A300-600 SRM 51-72-10-001, PAGE 2 AND SRM 51-40-21-001, PARA 7, PAGE 24~50. THIS REPAIR IS CATEGORY A AND
- [SDR FDEA202401050039](https://openairdocs.org/sdr/FDEA202401050039.md): Indicator · failed · Jan 5, 2024 · N721FD · Airbus A300* · Fire Detection
  > ENGINE FIRE AND MULTIPLE SYSTEMS WARNINGS AND CAUTIONS AFTER ROTATION IN LIGHT RAIN. ENGINE TEMPERATURE INDICATIONS WERE NORMAL AUTOPILOT AUTOMATION WAS NOT AVAILABLE. EMERGENCY DECLARED. INDICATOR WERE ALL REPLACED AND ALL OPS CHECKS BEING SATISFACTORY.
- [SDR FDEA202312301967](https://openairdocs.org/sdr/FDEA202312301967.md): Control Box · failed · Dec 30, 2023 · N721FD · Airbus A300B4622R · Landing Gear Position and Warning
  > AFTER TAKEOFF, AT GEAR RETRACT, COULDN`T RAISE MLG PAST NEUTRAL IN SYS #1, SWITCHED TO SYS #2, GEAR RETRACTED NORMAL, SEVERAL SYS FAULTED IMMEDIATELY. CABIN PRESSURE REGULATOR #1, BOTH ENGINE PER MODES FAULTED, ATS 1&2 FAULTED, PITCH TRIM #1 FAULTED, ALL PRO
- [SDR FDEA202210132565](https://openairdocs.org/sdr/FDEA202210132565.md): Proximity Sensor · failed · Oct 13, 2022 · N721FD · Airbus A300B4622R · Main Landing Gear
  > AFTER TAKEOFF KMEM 18R. GEAR WOULD NOT RETRACT. HANDLE CAME UP. BUT AFTER DELAY ECAM DISPLAY OF GEAR WOULD NOT RETRACT. FOLLOWED ECAM AND QRH. RETURNED TO KMEM 18C. LANDING UNEVENTFUL REPLACED 64GB PROX SENSOR REF AMM 32-00-00-04. OPS CHECK GOOD. PERF
- [SDR FDEA202206301675](https://openairdocs.org/sdr/FDEA202206301675.md): Floor Panel · damaged · Jun 30, 2022 · N721FD · Airbus A300* · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT #242QH FLOOR PANEL WAS FOUND 2 EA INSERTS DAMAGED. REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005
- [SDR FDEA202206301674](https://openairdocs.org/sdr/FDEA202206301674.md): Floor Panel · damaged · Jun 30, 2022 · N721FD · Airbus A300* · Fuselage Floor Panel
  > AFT CARGO COMPT #151LF FLOOR PANEL WAS FOUND INSERTS DAMAGED. REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005
- [SDR FDEA202206301748](https://openairdocs.org/sdr/FDEA202206301748.md): None · unknown · Jun 30, 2022 · N721FD · Airbus A300* · Nacelle/Pylon Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON #1 PYLON O/B SIDE, AT RIB 8 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 DETER
- [SDR FDEA202206301750](https://openairdocs.org/sdr/FDEA202206301750.md): None · unknown · Jun 30, 2022 · N721FD · Airbus A300* · Fuselage Structure (General)
  > AIRCRAFT REPAIR ASSESSMENT: EXISTING FLOOR BEAM REPAIR FOUND ON AFT CARGO COMPARTMENT AT FR 59, BTW -Y805 ~ -Y1470 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 EX
- [SDR FDEA202206301749](https://openairdocs.org/sdr/FDEA202206301749.md): None · unknown · Jun 30, 2022 · N721FD · Airbus A300* · Nacelle/Pylon Structure
  > AIRCAFT REPAIR ASSESSMENT EXISTING EXTERNAL DOUBLER REPAIR FOUND ON #2 PYLON O/B SIDE, AT RIB 8 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 DETER
- [SDR FDEA202206301747](https://openairdocs.org/sdr/FDEA202206301747.md): None · unknown · Jun 30, 2022 · N721FD · Airbus A300* · Nacelle/Pylon Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON #1 PYLON I/B SIDE, AT RIB8 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 DETERM
- [SDR FDEA202206301746](https://openairdocs.org/sdr/FDEA202206301746.md): Skin · unknown · Jun 30, 2022 · N721FD · Airbus A300* · Fuselage Main, Plate/Skin
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON FUSELAGE SKIN AT FR85,BTW STGR41L-44L. 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 DETE
- [SDR FDEA202206301740](https://openairdocs.org/sdr/FDEA202206301740.md): Skin · unknown · Jun 30, 2022 · N721FD · Airbus A300* · Wing Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND AROUND RH WING LWR SKIN L/E 613AB PANEL AT FWD O/B CUT OUT AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION
- [SDR FDEA202206301739](https://openairdocs.org/sdr/FDEA202206301739.md): Skin · unknown · Jun 30, 2022 · N721FD · Airbus A300* · Wing Structure
  > AIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND AROUND LH WING LWR SKIN L/E 513AB PANEL AT FWD O/B CUT OUT AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION
- [SDR FDEA202206251804](https://openairdocs.org/sdr/FDEA202206251804.md): None · cracked · Jun 25, 2022 · N721FD · Airbus A300* · Fuselage Main, Plate/Skin
  > 1EA CRACK INDICATION WAS FOUND AT RIGHT SIDE FR54 STGR44 FASTENER HOLE. ACCOMPLISHED THE WORK BY REAMING THE HOLE THIS IS CATE.B REPAIR I.A.W EA NO:6-5330- T0369235 P1, SEQ NO:000909, TITLE:FUSELAGE-PLATES & SKINS-RH JUNCTION BETWEEN LATERAL SKIN PANEL AND
- [SDR FDEA202206251701](https://openairdocs.org/sdr/FDEA202206251701.md): Seat Track · corroded · Jun 25, 2022 · N721FD · Airbus A300* · Fuselage Structure (General)
  > MAIN DECK SEAT TRACK FOUND CORROSION NEAR FR 17, Y 450 REMOVED DAMAGE PARTS & NEW TRACK INSTALLED WORK INSTRUCTION IAW A600-600 SRM 51- 40-21-001 PARA.6, PAGE.7B-23 & SRM 51-76-20-201 PARA.4E, PAGE.210~211, FIG.204.
- [SDR FDEA202206241785](https://openairdocs.org/sdr/FDEA202206241785.md): None · none · Jun 24, 2022 · N721FD · Airbus A300* · Fuselage Main, Plate/Skin
  > THE LH LOWER FUSELAGE SKIN WAS FOUND DENT FR67 STGR35 ACCOMPLISHED THE CATE.B DOUBLER REPAIR TO THE LH FUSELAGE SKIN I.A.W A300-600 SRM 53- 10-12-201 PARA.5 PAGE.343-346 FIG.224(SHEET-4) & 53-17-12-001 PAGE.42-43 & SRI:53-10-12-201 IIR:53-10-12-2-004-00 PAR
- [SDR FDEA202206241702](https://openairdocs.org/sdr/FDEA202206241702.md): Seat Track · corroded · Jun 24, 2022 · N721FD · Airbus A300* · Fuselage Structure (General)
  > MAIN DECK SEAT TRACK FOUND CORROSION NEAR FR 15C, Y 950 REPLACED THE SEAT TRACK WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001 PAGE.2 & 51-40-21- 001 PARA.6, PAGE7B-23.
- [SDR FDEA202206241700](https://openairdocs.org/sdr/FDEA202206241700.md): Seat Track · corroded · Jun 24, 2022 · N721FD · Airbus A300* · Fuselage Structure (General)
  > MAIN DECK SEAT TRACK FOUND CORROSION NEAR FR 12A 2", Y 700 REPLACED THE SEAT TRACK WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001 PAGE.2 & 51-40-21- 001 PARA.6, PAGE.7B~23.
- [SDR FDEA202206231909](https://openairdocs.org/sdr/FDEA202206231909.md): Stiffener · corroded · Jun 23, 2022 · N721FD · Airbus A300* · Fuselage Main, Structure
  > WASTE WATER SERIVE PANEL COMP'T LOWER CUTOUT STIFFENER AREA CORROSION AT FR12A POSITION. REPLACED THE SIFFENER WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001, PAGE.2.
- [SDR FDEA202110062474](https://openairdocs.org/sdr/FDEA202110062474.md): Actuator · none · Oct 6, 2021 · N721FD · Airbus A300B4622R · Hydraulic Power System
  > PDIS 721 29-02 1252 06OCT21 MEM OPEN U GREEN SYSTEM HAD HYD LOW PRESSURE. COMPLIED WITH QRH. INFO 06OCT21 04:43 MC1 R LOST GREEN HYD SYSTEM QUANTITY DOWN TO BOTTOM OF YELLOW BAND. FOLLOWED BY LOSS OF SYSTEM PRESSURE. COMPLIED WITH QRH. M
- [SDR FDEA202108122007](https://openairdocs.org/sdr/FDEA202108122007.md): Altimeter · failed · Aug 12, 2021 · N721FD · Airbus A300B4622R · Altimeter, Barometric/Encoder
  > AT FL 360 THE STANDBY ALTIMETER WAS READING 300 FEET HIGHER THAN THE CAPTAIN AND FO ALTIMETERS. AT LOWER ALTITUDES IT RETURNED TO NORMAL. REF GMM 12-7-600. STANDBY ALTIMETER, CREW REPORTED MAIN ALTIMETERS OPS NORMAL. REMOVED AND REPLACED STANDBY ALT
- [SDR FDEA202108071990](https://openairdocs.org/sdr/FDEA202108071990.md): Adc · malfunctioned · Aug 7, 2021 · N721FD · Airbus A300B4622R · Flight Environment Data
  > ON GROUND F/O, CAPT, STBY ALTIMETER W/IN 50 FEET. AT 290 F/O AND CAPT ALTIMETER AGREED. AT 330 F/O READ 32.6 AND STBY READ 330. F/O AIRSPEED WAS 10 TO 15 KTS SLOWER THAN CAPTAIN R/I 07AUG21 01:33 SNA U REASON CODE: PREMATURE REMOVAL/INSTALLATION
- [SDR FDEA202105061140](https://openairdocs.org/sdr/FDEA202105061140.md): Valve · contaminated · May 6, 2021 · N721FD · Airbus A300B4622R · Landing Gear Retraction/Extension System
  > ON APPROACH SELECTED GEAR DOWN. THE LEFT MAIN GEAR AND DOOR WERE SLOW ENOUGH TO CAUSE A GEAR NOT DOWN ECAM, BUT CANCELLED A FEW MOMENTS LATER AS THE CYCLE COMPLETED. NORMAL OPS THEEAFTER. DISCOVERED MATERIAL IN L/H MLG RESTRICTOR VALVE. REMOVED AND REPL

Next page: https://openairdocs.org/aircraft/N721FD/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 = 'N721FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N721FD/reports

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