# Service difficulty reports: N720FD, cancelled Jun 28, 2024

A list on [N720FD, cancelled Jun 28, 2024](https://openairdocs.org/deregistered/N720FD-2024-06-28.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 2 · 51 reports

- [SDR FDEA201412244177](https://openairdocs.org/sdr/FDEA201412244177.md): Power Supply · inoperative · Dec 24, 2014 · N720FD · Airbus A300B4622 · Door Warning System
  > L1 & R1 DOOR ESCAPE SLIDE RELEASE WARNING LIGHTS INOPERATIVE. BUZZERS OPS NORMAL. R & R AUTONOMOUS STANDBY POWER SUPPLY UNIT IAW AMM 52-73-18-04. OPS CHECKED GOOD. PTT BUTTONS ILLUMINATE RED WARNING LIGHTS ON BOTH L1 & R1 DOORS.
- [SDR FDEA201412194178](https://openairdocs.org/sdr/FDEA201412194178.md): Power Supply · inoperative · Dec 19, 2014 · N720FD · Airbus A300B4622 · Door Warning System
  > AFTER BLOCK IN, R1 DOOR SLIDE ARMED NOT ON ECAM. FIRST OFFICER SAID DOOR WAS ARMED, RECYCLED ARM HANDLE, STILL NO CHANGE, NO "SLIDE" ILLUMINATED. R & R R1 DOOR LIMIT SWITCH IAW AMM 52-71-11-04-01. OPS CHECK SHOWED DOOR CLOSED ON ECAM BUT DID NOT SHOW THAT
- [SDR FDEA201211184069](https://openairdocs.org/sdr/FDEA201211184069.md): Frame · damaged · Nov 18, 2012 · N720FD · Airbus A300B4622 · Fuselage Main, Frame
  > MAIN DEC CARGO FR 28 S8-20 LT FRAME DAMAGED, BLEND OUT THE DAMAGE IAW SRM 51-73-10, COMPLIED WITH EA 6-5310-163149.
- [SDR FDEA201211154022](https://openairdocs.org/sdr/FDEA201211154022.md): Skin · delaminated · Nov 15, 2012 · N720FD · Airbus A300B4622 · Wing, Plate/Skin
  > RIGHT WING OTBD FIXED L/E OTBD TRAILING SECTION DELAMINATED. REMOVED THE ORIGINAL T/E DOUBLER IAW SRM 51-40-21 MADE THE REPAIR INSERT & DOUBLER IAW SRM 57-51-12/201 FIG 215. INSTALLED THE INSERT & DOUBLER IAW SRM 57-51-12/201, FIG 215.
- [SDR FDEA201211144014](https://openairdocs.org/sdr/FDEA201211144014.md): Skin · damaged · Nov 14, 2012 · N720FD · Airbus A300B4622 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN FR38, S35-36R FOUND ONE LIGHTNING STRIKE. REMOVED DAMAGE IAW SRM 51-73-10. EXCEED LIMITS IAW SRM 53-10-12/101, DIAGRAM 112, REPAIRED IAW SRM 53-10-12/201 FIG 225.
- [SDR FDEA201211144007](https://openairdocs.org/sdr/FDEA201211144007.md): Skin · delaminated · Nov 14, 2012 · N720FD · Airbus A300B4622 · Wing, Plate/Skin
  > RT WING OTBD FIXED T/E UPPER SURFACE DELAMINATED. REMOVED THE DAMAGE T/E SKIN IAW SRM 51-40-21 MADE THE REPAIR INSERT & DOUBLER IAW SRM 57-51-12/201, FIG215 WET INSTALLED THE INSERT & DOUBLER IAW SRM 57-51-12/201, FIG 215 SEALED THE EDGE WITH SEALANT IAW SRM
- [SDR FDEA201211133986](https://openairdocs.org/sdr/FDEA201211133986.md): Skin · delaminated · Nov 13, 2012 · N720FD · Airbus A300B4622 · Wing, Plate/Skin
  > SKIN DOUBLER AT RT WING TIP UPPER SKIN UNDERNEATH STATIC DISCHARGE DELAMINATION FOUND AROUND THE ORIGINAL DOUBLER AT RT WING TIP UPPER SKIN. UNDERNEATH STATIC DISCHARGE, REPAIRED IAW SRM 57-51-12/201, FIG 215 AND CLASSFIED AS MAJOR IAW GMM6-2-100.
- [SDR FDEA201211013798](https://openairdocs.org/sdr/FDEA201211013798.md): Floor Support · corroded · Nov 1, 2012 · N720FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED AND DELAMINATED BETWEEN FR11 TO FR13A. REPLACED FLOOR SUPPORT PER SRM51-40-21.
- [SDR FDEA201210243735](https://openairdocs.org/sdr/FDEA201210243735.md): Spar · cracked · Oct 24, 2012 · N720FD · Airbus A300B4622 · Wing, Center Box
  > ONE CRACK WAS FOUND AT FASTENER HOLE "F" OF LT CENTER WING BOX OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REPAIRED PER EA 6-5710-163148.
- [SDR FDEA201210243734](https://openairdocs.org/sdr/FDEA201210243734.md): Spar · cracked · Oct 24, 2012 · N720FD · Airbus A300B4622 · Wing, Center Box
  > ONE CRACK WAS FOUND AT FASTENER HOLE "F" OF RT CENTER WING BOX OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REPAIRED PER EA 6-5710-163148.
- [SDR FDEA201210243733](https://openairdocs.org/sdr/FDEA201210243733.md): Spar · cracked · Oct 24, 2012 · N720FD · Airbus A300B4622 · Wing, Center Box
  > ONE CRACK WAS FOUND AT FASTENER HOLE "C" OF RT CENTER WING BOX OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REPAIRED PER EA 6-5710-163148.
- [SDR FDEA201210243732](https://openairdocs.org/sdr/FDEA201210243732.md): Frame · cracked · Oct 24, 2012 · N720FD · Airbus A300B4622 · Fuselage Main, Frame
  > FOUND A CRACK 6MM IN LENGTH AT RT SIDE FRAME 40 LOWER OTBD RADIUS AREA. COMPLIED WITH EA 6-5710-163147.
- [SDR FDEA201210243731](https://openairdocs.org/sdr/FDEA201210243731.md): Frame · cracked · Oct 24, 2012 · N720FD · Airbus A300B4622 · Wing Spar
  > FOUND A CRACK 8MM IN LENGTH AT LT SIDE FRAME 40 LOWER OTBD RADIUS AREA. REPAIRED PER EA 6-5710-163147
- [SDR FDEA201210243730](https://openairdocs.org/sdr/FDEA201210243730.md): Rib · cracked · Oct 24, 2012 · N720FD · Airbus A300B4622 · Wing, Rib/Bulkhead
  > ONE CRACK ABOUT 10MM IN LENGTH WAS FOUND IN THE AREA OF HOLE 47 OF MLG RIB 5, RT SIDE. COMPLIED WITH EA 6-5710-163-146
- [SDR FDEA201210053559](https://openairdocs.org/sdr/FDEA201210053559.md): Limiter · failed · Oct 5, 2012 · N720FD · Airbus A300F4622R · Leading Edge Slat Control System
  > FAULT ON INITIAL SLAT EXTENSION SLATS STUCK AT 00 FOLLOWED QRH ECAM. TRIED FLAP/SLAT LEVER EXTEND TWO TIMES SAME AS SLAT ONLY STUCK 0. PERFORMED SFCC BITE, CHECKED NR 1 SFCC FAULT CODE 00110 & NR 2 SFCC SLAT JAM LATCHED. PERFORMED FLAP/SLAT OPS CHECKED NORMA
- [SDR FDEA201208102939](https://openairdocs.org/sdr/FDEA201208102939.md): Computer · faulted · Aug 10, 2012 · N720FD · Airbus A300B4622 · Trailing Edge Flap Control System
  > FLAPS STUCK AT 20 DEG ON TAKEOFF. WOULD NOT MOVE AND RECYCLE WAS NO HELP. LEFT FLAPS DOWN AFTER LANDING AT 20 DEG. NR 1 SFCC FAULTED HIGH SPEED P SWITCH AND NR 2 SFCC FAULTED FLAP JAM. R & R SCREWJACK IAW AMM 27-54-21-04, 27-54-22-04, & 27-54-24-04. CA
- [SDR FDEA201208102937](https://openairdocs.org/sdr/FDEA201208102937.md): Flap System · malfunctioned · Aug 10, 2012 · N720FD · Airbus A300F4622R · Trailing Edge Flap Control System
  > FLAPS WOULD NOT RETRACT AFTER TAKE OFF. FLAPS STUCK AT 20 DEGREES. RECYCLE, NO HELP. RETRACTED NORMAL AFTER LANDING. AFTER BLOCK IN, NOTED FLAPS WERE FULLY RETRACTED. INTERROGATED MTP, NO FAULTS. INSPECTED BOTH NR 1 & NR 2 SFCC'S. BOTH SFCC'S REGISTERED A
- [SDR FDEA201203170993](https://openairdocs.org/sdr/FDEA201203170993.md): Flap System · malfunctioned · Mar 17, 2012 · N720FD · Airbus A300B4622 · Trailing Edge Flap Control System
  > AFTER TAKE OFF, FLAPS WOULD NOT RETRACT FROM 20 DEG COMPLIED QRH. RETURNED TO LAND IAW INSTRUCTION CARRIED OUT LUBRICATION ON LT FLAP TRACK AND JACKSCREW DRIVE UNITS. SERVICED LT FLAP TRACK TORQUE LIMITER, TEE GEAR BOX, DOWN DRIVE GEAR BOX, BEVEL GEAR AND
- [SDR FDEA201201220300](https://openairdocs.org/sdr/FDEA201201220300.md): Rib · cracked · Jan 22, 2012 · N720FD · Airbus A300F4622R · Wing, Landing Gear Attach Fittings
  > A CRACK WAS FOUND IN THE AREA OF HOLE 47 OF LT SIDE MLG RIB NR 5 AT THE SPOT FACE, THE CRACK LENGTH WAS 33 MM. REPAIRED THE HOLE 47 OF LH MLG RIB 5 IAW EA 6-5750-149032 PART1.
- [SDR FDEA201107082618](https://openairdocs.org/sdr/FDEA201107082618.md): Unknown · smoke · Jul 8, 2011 · N720FD · Airbus A300B4622 · Wing Structure
  > ON TAKEOFF, TOWER REPORTED "EXCESSIVE SMOKE TRAILING FROM LT WING." DID AN ATB, NO INDICATION OF SMOKE ON ACFT AND NO ECAM WARNINGS. MX NOTED NO LEAKS FROM LT WING OR ENGINE. CREW STATED NO ABNORMAL HYD QTY OR OIL QTY DECREASE DURING TAKEOFF. NO ABNORMA
- [SDR FDEA201103040852](https://openairdocs.org/sdr/FDEA201103040852.md): Lug · corroded · Mar 4, 2011 · N720FD · Airbus A300B4622 · Wing, Landing Gear Attach Fittings
  > LT MLG RIB 5 AFT PINTLE FWD LUG BUSHING CAME OUT OF FITTING WHILE REMOVING LT MLG REAR PIN. REMOVED LEVEL 1 CORROSION. COMPLIED WITH EA 6-5710-145574 LT MLG RIB 5 AFT PINTLE FWD LUG.
- [SDR FDEA201103040850](https://openairdocs.org/sdr/FDEA201103040850.md): Bushing · failed · Mar 4, 2011 · N720FD · Airbus A300B4622 · Wing, Landing Gear Attach Fittings
  > RT MLG FIB 5 AFT PINTLE FWD BUSHING CAME OUT OF FITTING WHILE REMOVING LT MLG REAR PIN REMOVED LEVEL 1 CORROSION. COMPLIED WITH EA 6-5710-145574 RT MLG AFT PINTLE FWD LUG.
- [SDR FDEA201010053949](https://openairdocs.org/sdr/FDEA201010053949.md): Smoke Detector · malfunctioned · Oct 5, 2010 · N720FD · Airbus A300F4622R · Smoke Detection
  > LOWER FWD CARGO COMPT SMOKE ALERT. BOTH BOTTLES HAVE BEEN DISCHARGED. R&R'D BOTH FORWARD LOWER CARGO BAY SMOKE DETECTORS. AS PER A300-600 AMM 26-16-11-04, PERFORMED OPS TEST NORMALLY. OK FOR SERVICE. RAN UP ENGINES FOR 15 MINS, PACKS ON, AND COULD NOT FIN
- [SDR FDEA201007242656](https://openairdocs.org/sdr/FDEA201007242656.md): Stiffener · corroded · Jul 24, 2010 · N720FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > AVIONICS COMPARTMENT FUSELAGE STRUCTURE BELOW WASTE WATER CONNECTION BOX AT FRAME 12 STR 44L HAS CORROSION ON INTERNAL DOUBLE REMOVED LEVEL 1 CORROSION. REPLACED INTERNAL DOUBLE/STIFFENER AT WASTE WATER CONNECTION BOX IAW EA NR 6-5310-135232, DATED 7/23/10
- [SDR FDEA201007102472](https://openairdocs.org/sdr/FDEA201007102472.md): Web · cracked · Jul 10, 2010 · N720FD · Airbus A300F4622R · Cargo/Baggage Doors
  > AFT CARGO DOOR INNER SURFACE WEB, FWD OF HINGE FITTING HAS A 2" CRACK. FABRICATED WEB PLATE REPAIR IAW SRM 51-71-30 PG 201-204 INSTALLED WEB PLATE REPAIR IAW SRM 51-71-30, PG 201-204.
- [SDR FDEA201007102471](https://openairdocs.org/sdr/FDEA201007102471.md): Skin · damaged · Jul 10, 2010 · N720FD · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > RT FWD FUSELAGE EXTERNAL SKIN AT FRAME 20 COMMON TO FWD EDGE OF DOOR CUT-OUT 2 EA AREAS OF IMPACT DAMAGE. AREA 1=.500" X.250" X.316" AREA 2= 8.500" X.250" X.365" BETWEEN RT STR 36 AND 40 REMOVED DAMAGED FRAME SECTION IAW REPAIR DWG SR 30-53-001. INSTAL
- [SDR FDEA201007102470](https://openairdocs.org/sdr/FDEA201007102470.md): Seat Track · cracked · Jul 10, 2010 · N720FD · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK FRAME 50, SEAT TRACK 4 LT SUPPORT TANG CRACKED 10 IN BELOW FLOOR LEVEL. REMOVED CRACKED LINK AND REPLACED WITH NEW PART LINK AT FR 50, SEAT TRACK 4 LT IAW SRM 51-40-21.
- [SDR FDEA201007102469](https://openairdocs.org/sdr/FDEA201007102469.md): Seat Track · cracked · Jul 10, 2010 · N720FD · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK FRAME 48, SEAT TRACK 4 RT SUPPORT TANG CRACKED 10 IN BELOW FLOOR LEVEL. REMOVED CRACKED LINK AND REPLACED WITH NEW PART LINK AT FRAME 48, SEAT TRACK 4 RT IAW SRM 51-40-21.
- [SDR FDEA201007102468](https://openairdocs.org/sdr/FDEA201007102468.md): Seat Track · cracked · Jul 10, 2010 · N720FD · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK FRAME 48 SEAT TRACK 4 LT SUPPORT TANG CRACKED 10 IN BELOW FLOOR LEVEL REMOVED CRACKED LINK AND REPLACED WITH NEW PART LINK AT FRAME 48, SEAT TRACK 4 LT IAW SRM 51-40-21.
- [SDR FDEA201007102467](https://openairdocs.org/sdr/FDEA201007102467.md): Seat Track · cracked · Jul 10, 2010 · N720FD · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK FRAME 49 SEAT TRACK 4 LT SUPPORT TANG CRACKED 10 IN BELOW FLOOR LEVEL REMOVED CRACKED LINK AND REPLACED WITH NEW PART AT FR 49, SEAT TRACK 4 LT IAW SRM 51-40-21.
- [SDR FDEA200809053733](https://openairdocs.org/sdr/FDEA200809053733.md): Smoke Detector · failed · Sep 5, 2008 · N720FD · Airbus A300B4622 · Smoke Detection
  > "AVIONICS SMOKE" WARNING ILLUMINATED AT 9000 FT ON CLIMB-OUT. ACCOMPLISHED ALL QRH PROCEDURES. INSPECTED AVIONICS COMPARTMENT, MIN EQUIP BAY AND COCKPIT FOR EVIDENCE OF SMOKE OR FIRE. NO DISCREPANCIES FOUND. AVIONICS SMOKE DET WARNING, DISPLAYS AND ALERT L
- [SDR 08FDEA03733](https://openairdocs.org/sdr/08FDEA03733.md): Smoke Detector · failed · Sep 5, 2008 · N720FD · Airbus A300B4622 · Smoke Detection
  > "AVIONICS SMOKE" WARNING ILLUMINATED AT 9000' ON CLIMB-OUT. ACCOMPLISHED ALL QRH PROCEDURES. INSPECTED AVIONICS COMPARTMENT, MIN EQUIP BAY AND COCKPIT FOR EVIDENCE OF SMOKE OR FIRE. NO DISCREPANCIES FOUND. AVIONICS SMOKE DET WARNING, DISPLAYS AND ALERT LI
- [SDR 08FDEA01753](https://openairdocs.org/sdr/08FDEA01753.md): Skin · damaged · May 5, 2008 · N720FD · Airbus A300B4622R · Leading Edge Devices
  > UPON SLAT/ K-FLAP EXTENSION, THE RT/K-FLAP PANEL CONTACTED THE UPPER CLOSE-OUT PANEL RESULTING IN DEFORMATION OF PANEL EDGES AND ATTACH LINK. REPLACED K-FLAP SKIN IAW SRM 51-40-21, REPLACED K-FLAP VANE ASSY IAW AMM 27-87-12-4. REPLACED WING WEB/FORMER IAW SR
- [SDR 08FDEA01148](https://openairdocs.org/sdr/08FDEA01148.md): Floor Support · corroded · Mar 26, 2008 · N720FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPT FR 69 FLOOR SUPPORT CORRODED LBL20 AND TIE DOWN FITTING MISSING. REMOVED DAMAGED FLOOR CROSS BEAM IAW SRM 51-40-21. RECEIVED NEW FLOOR CROSS BEAM P/N NR A59374322230 BATCH NR 0001436243. LOCATED AND DRILLED IAW SRM 51-40-44. INSTALLED AND
- [SDR 08FDEA01147](https://openairdocs.org/sdr/08FDEA01147.md): Shear Plate · cracked · Mar 26, 2008 · N720FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > MCD FR79-80 STRING 26L ATTACH WEB CRACKED REMOVED SHEAR PLATE IAW SRM 51-40-21. FABBED SHEAR PLATE IAW MAE TRAVLER T8/731840. LOCATED AND DRILLED IAW SRM 51-40-44, ALODINED IAW SRM 51-20-10. PRIMED IAW SRM 51-20-10. INSTALLED SHEAR PLATE IAW SRM 51-40-21.
- [SDR 08FDEA01130](https://openairdocs.org/sdr/08FDEA01130.md): Floorbeam · corroded · Mar 24, 2008 · N720FD · Airbus A300B4622 · Fuselage Main, Floor Beam
  > AFT CARGO FR 67 FLOOR PANEL HAS SEVERAL SPOTS OF CORROSION LBL 60 TO RBL 60, CROSS BEAM. REMOVED CROSS BEAM IAW SRM 51-73-10 LOCATED AND DRILLED NEW CROSS BEAM IAW SRM 51-40-44. INSTALLED CROSS BEAM IAW SRM 51-40-21.
- [SDR 08FDEA01129](https://openairdocs.org/sdr/08FDEA01129.md): Floor Support · corroded · Mar 24, 2008 · N720FD · Airbus A300B4622 · Fuselage Miscellaneous Structure
  > MAIN CARGO COMPARTMENT FLOOR SUPPORT BETWEEN FR 14 AND FR 16 RBL 40 HAS CORROSION IN SEVERAL PLACES ON LOWER SURFACE AROUND FASTENER HOLES REMOVED FLOOR SUPPORT BEAM IAW SRM 51-40-21. FABRICATED NEW FLOOR SUPPORT BEAM IAW SRM 53-12-15 AND SPLICES, LOCATED AND
- [SDR 08FDEA01016](https://openairdocs.org/sdr/08FDEA01016.md): Seat Track · corroded · Mar 18, 2008 · N720FD · Airbus A300B4622 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK ZONE 221, FORWARD CABIN SEAT TRACK 37.5 LBL HAS STRUCTURAL DAMAGE (HEAVY CORROSION EXFOLIATED) BETWEEN FR 15A THRU FR 19. REMOVED SEAT TRACK IAW SRM 51-40-21, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-44. INSTALLED NEW SEAT TRACK IAW SRM 5
- [SDR 08FDEA00902](https://openairdocs.org/sdr/08FDEA00902.md): Seat Track · corroded · Mar 12, 2008 · N720FD · Airbus A300B4622 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK ZONE 221.FORWARD CABIN SEAT TRACK LBL 18 (Y450) BETWEEN FR 14 THRU FR19 HAS STRUCTURAL DAMAGES (HEAVY CORROSION, EXFOLIATION). REMOVED SEAT TRACK IAW SRM 51-40-21 LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-44. INSTALLED SEAT TRACK IAW SRM 5
- [SDR 08FDEA00345](https://openairdocs.org/sdr/08FDEA00345.md): Rib · cracked · Feb 3, 2008 · N720FD · Airbus A300B4622 · Wing, Rib/Bulkhead
  > RIB NR 25 FOUND TO BE CRACKED. REPLACE DAMAGED RIB.
- [SDR 06FDEA03634](https://openairdocs.org/sdr/06FDEA03634.md): Module · malfunctioned · Oct 13, 2006 · N720FD · Airbus A300F4622R · Pitot/Static System
  > F/O'S PFD AIRSPEED LAGGED CAPT. PFD AND BOTH STBY AIRSPEED GAUGES BY 40 KTS, THEN STOPPED INCREASING AT 200 KIAS, LATER CAPT PFD AIRSPEED READ 300 KIAS, F/O' PFD AIRSPEED READ 200. FACT 13OCT06 06:02 ORD R REPLACED F/O ADC AND CHECK PER MM 34-11-34-4
- [SDR 06FDEA03633](https://openairdocs.org/sdr/06FDEA03633.md): Indicator · malfunctioned · Oct 13, 2006 · N720FD · Airbus A300B4622 · Airspeed/Mach Indicator
  > ON T/O ROLL F/O'S AIRSPEED INDICATION ON THE PFD DID NOT BREAK UNTIL THE THE CAPTAINS AIRSPEED REACHED 70KTS. (30 KT DIFFERENCE) IN WORK.
- [SDR 06FDEA03631](https://openairdocs.org/sdr/06FDEA03631.md): Module · malfunctioned · Oct 13, 2006 · N720FD · Airbus A300F4622R · Pitot/Static System
  > PDIS 720 34-11 0002739 13OCT06 ORD CLOSE R 1ST RTO OF 2 F/O'S PFD AIRSPEED LAGGED CAPT. PFD AND BOTH STBY AIRSPEED GAUGES BY 40 KTS, THEN STOPPED INCREASING AT 200 KIAS, LATER CAPT. PFD AIRSPEED READ 300 KIAS, F/O' PFD AIRSPEED READ 200. OFF MFG 404
- [SDR 06FDEA2593](https://openairdocs.org/sdr/06FDEA2593.md): Tee Fitting · leaking · Jul 16, 2006 · N720FD · Airbus A300B4622 · Hydraulic System, Main
  > GREEN SYSTEM OIL QUANTITY (LOST AUTOPILOT NR 1 SPOILERS ETC) CHECKED ECAM, HYDRO SYSTEM ALMOST ZERO, PRESSURE GONE, AFTER MANUALLY LOWERING GEAR, QUANITTY CAME UP SOME. FOUND T-FITTING LEAKING ON STAB JUST O/B OFF PITCH ACT, ON LT SIDE. REMOVED T-FITTING AN
- [SDR 05FDEA04314](https://openairdocs.org/sdr/05FDEA04314.md): Frame · cracked · Dec 14, 2005 · N720FD · Airbus A300B4622R · Engine Thrust Reverser
  > EXHAUST THRUST REVERSER TORQUE BOX FWD FRAME CRACKS. COMPLIED WITH EA 6-7830-923658 EXHAUST THRUST REVERSER TORQUE BOX FWD FRAME CRACKS PART 1.
- [SDR 05FDEA03933](https://openairdocs.org/sdr/05FDEA03933.md): Repair · unknown · Nov 21, 2005 · N720FD · Airbus A300B4622R · Engine Thrust Reverser
  > THRUST REVERSER-UPPER TORQUE BOX CAP GOUGE REPAIR. COMPLIED WITH EA 6-7830-92361 THRUST REVERSER UPPER TORQUE BOX GOUGE REPAIR.
- [SDR 05FDEA03902](https://openairdocs.org/sdr/05FDEA03902.md): Access Door · gouged · Nov 19, 2005 · N720FD · Airbus A300B4622R · Engine Thrust Reverser
  > COMPLY WITH EA 6-7830-92360, THRUST REVERSER NR 1 INBD T/R ACCESS DOOR GOUGE REPAIR. COMPLIED WITH EA 6-7830-92360.
- [SDR 05FDEA03899](https://openairdocs.org/sdr/05FDEA03899.md): Fitting · damaged · Nov 18, 2005 · N720FD · Airbus A300B4622R · Fuselage Main, Attach Fittings
  > COMPLY WITH EA 6-5310-92351, FUSELAGE SB 53-6111, DISCREPANT BASE FITTING HOLES AT FS 45 RT. COMPLIED WITH EA 6-5310-92351B.
- [SDR 05FDEA03847](https://openairdocs.org/sdr/05FDEA03847.md): Frame · misdrilled · Nov 16, 2005 · N720FD · Airbus A300B4622R · Fuselage Main, Frame
  > COMPLY WITH EA 6-5310-92355 FUSELAGE MAIN FRAME EXISTING SHORT PITCH HOLES FR 42, STR 36 RT AND 36 LT. COMLIED WITH EA 6-5310-92355 FUSELAGE MAIN FRAME EXISTING SHORT PITCH HOLES FR 42, STR 36 RT AND 36 LT.
- [SDR 05FDEA03590](https://openairdocs.org/sdr/05FDEA03590.md): Panel · cracked · Oct 30, 2005 · N720FD · Airbus A300B4622R · Wing, Plate/Skin
  > RT WING BOTTOM PNL 675 DB CUT-OUT HAS CRACK.

Next page: https://openairdocs.org/deregistered/N720FD-2024-06-28/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 = 'N720FD' AND deregistration_id = 'N720FD-2024-06-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N720FD-2024-06-28/reports

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