N728FD

Service difficulty reports · 266

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N728FD' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201607012221Controller · malfunctionedDURING CRUISE AT FL 300, THE NR 1 BLEED FAULTED. THE NR 2 BLEED ALREADY MEL'D. FOLLOW THE QRH PROCEDURES AND DIVERTED. PERFORMED BITE CHECK OF NR 1 PNUEMATIC CONTROLLER. DISPLAYED C CONTROLLER FAULT IAW TSM 41HA CONTROLLER AT FAULT. REPLACED NR 1 PNUEMATIJul 1, 2016 · N728FD · Airbus A300B4622R · Pneumatic Distribution SystemSDR FDEA201509092825Master Cylinder · leakingDURING LANDING, LT BRAKES GRABBED HARD & CAUSED A CONTROL ISSUE. TEMPS CLIMBED TO ABOVE 400 DEGREES ON LT & RT REMAINED APPROX 60 DEGREES, NO NOTICEABLE STEERING ISSUES DURING TAXI. LT BRAKE HAD MORE TRAVEL BEFORE GRABBING THAN RT. NOTED LT GEAR BRAKE TEMPSep 9, 2015 · N728FD · Airbus A300B4622R · Master Cylinder/Brake ValveSDR FDEA201508152549Skin · crackedRIGHT WING SPOILER 4, LOW SURFACE SHOWS EVIDENCE OF A CRACK. REPAIRED THE RT WING NR 4 SPOILER LOWER SURFACE DAMAGE. MAJOR REPAIR IAW GMM 6-2-100.Aug 15, 2015 · N728FD · Airbus A300B4622R · SpoilersSDR FDEA201508052469Seat Track · corrodedFRAME 17, Y450, SEAT TRACK ONE BOLT HOLE WITH SLIGHT CORROSION. REPLACED THE SEAT TRACK IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Aug 5, 2015 · N728FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201508032451Panel · crackedRIGHT WING, FUSELAGE CENTER WING BOX, INSPECTION OF REAR SPAR & BOTTOM PANEL HOLE Y FOUND A CRACK. REPAIRED IAW EA 6-5710-T0319444 P 1. MAJOR REPAIR IAW GMM 6-2-100.Aug 3, 2015 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201508012446Web · crackedON THE CENTER OF LEFT MID FLAP, RIB 17 - RIB 19 FOUND WEB CRACKED. REPAIRED IAW EA 6-5750-T0319244 P 1. MAJOR REPAIR IAW MM 6-2-100.Aug 1, 2015 · N728FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201507292428Fitting · damagedPERFORM TERMINATING ACTION OF EA 6-5710-102692 PT 2. BUSHING REPAIR TO LT SIDE FRAME 47 INTERNAL CORNER ANGLE FITTING FASTENER HOLE Q NR 2. THE REPAIR CATEGORY TBD, REPAIR LIFE LIMITATION IS 6 MONTHS. MAJOR REPAIR IAW GMM 6-2-100.Jul 29, 2015 · N728FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA201507292431Support · corrodedMAIN DECK FRAME 47, -Y953 TO -Y1456, UNDERFLOOR, ONE SUPPORT WEB CRACKED. REPAIRED IAW SRM 53-15-15 FIG 201 SHT 2. MAJOR REPAIR IAW GMM 6-2-100.Jul 29, 2015 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201507292430Support · corrodedMAIN DECK FRAME 47, Y0 - -Y450 UNDERFLOOR, ONE SUPPORT WEB CRACKED. REPAIRED IAW SRM 53-15-15 FIG 201 SHT 2. MAJOR REPAIR IAW GMM 6-2-100.Jul 29, 2015 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201507292429Support · crackedMAIN DECK FRAME 47, Y0 - Y450 UNDERFLOOR, ONE SUPPORT WEB CRACKED. REPLACED THE CRACKED WEB IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Jul 29, 2015 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201507282419Floor Support · corrodedAFT CARGO, FRAME 58, -Y750 - Y750, FLOOR SUPPORT WITH INNER GRANULAR CORROSION. REPAIRED THE CROSSBEAM IAW SRM 53-10-15 FIG 208 SHT 2. MAJOR REPAIR IAW GMM 6-2-100.Jul 28, 2015 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201507282410Frame · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL, TENSION BOLT JUNCTION INSPECTION. RIGHT SIDE LOWER BOLT HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0319314 P 1. REPAIRED THE RT SIDE LOWER BOLT HOLE OF FRAME 40 TO CTR WING JOINT. MAJOR REPAIR IAW GMJul 28, 2015 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201507282409Frame · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL, TENSION BOLT JUNCTION INSPECTION. RIGHT SIDE MIDDLE BOLT HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0319314 P 1. REPAIRED THE RT SIDE MIDDLE BOLT HOLE OF FRAME 40 TO CTR WING JOINT. MAJOR REPAIR IAW Jul 28, 2015 · N728FD · Airbus A300F4622R · Fuselage Main, FrameSDR FDEA201507282408Frame · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL, TENSION BOLT JUNCTION INSPECTION. RIGHT SIDE UPPER BOLT HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0319314 P1. REPAIRED THE RT SIDE UPPER BOLT HOLE OF FRAME 40 TO CTR WING JOINT. MAJOR REPAIR IAW GMMJul 28, 2015 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201507282407Frame · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL, TENSION BOLT JUNCTION INSPECTION. LEFT SIDE LOWER BOLT HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0319314 P 1. REPAIRED THE LT SIDE LOWER BOLT HOLE OF FRAME 40 TO CTR WING JOINT. MAJOR REPAIR IAW GMMJul 28, 2015 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201507282406Frame · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL, TENSION BOLT JUNCTION INSPECTION. LEFT SIDE MIDDLE BOLT HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0319314 P 1. REPAIRED THE LT SIDE MIDDLE BOLT HOLE OF FRAME 40 TO CTR WING JOINT. MAJOR REPAIR IAW GJul 28, 2015 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201507282405Frame · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL, TENSION BOLT JUNCTION INSPECTION. LEFT SIDE UPPER BOLT HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0319314 P 1. REPAIRED THE LT SIDE UPPER BOLT HOLE OF FRAME 40 TO CTR WING JOINT. MAJOR REPAIR IAW GMMJul 28, 2015 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201310102470Rvdt · failedREJECTED TAKEOFF DUE TO NR 1 ENGINE THRUST REVERSER UNLOCK INDICATION ON ECAM. NR 1 ENGINE GAUGE READING NOT RESPONSIVE. REMOVED AND REPLACED RVDT ON NR 1 ENGINE.Oct 10, 2013 · N728FD · Airbus A300B4622R · Engine Thrust ReverserSDR FDEA201307091516Attach Fitting · corrodedRT WING, RIB 5, MLG ATTACH FITTING CORRODED IN FWD PINTLE PIN LUG. R & R RT WING RIB 5 MLG ATTACH FITTING IAW EA 6-5710T0300313 PT2. UNDER CAS WO 581 AND WO M-304804.Jul 9, 2013 · N728FD · Airbus A300B4622R · Wing, Landing Gear Attach FittingsSDR FDEA201307091515Attach Fitting · corrodedLEFT WING RIB 5 MLG ATTACH FITTING HAS CORROSION IN FWD PINTLE PIN LUG. R & R LT WING RIB MLG ATTACH FITTING IAW EA 6-5710T0300313, PT1 UNDER CAS WO 581 AND WO M-304804.Jul 9, 2013 · N728FD · Airbus A300B4622R · Wing, Landing Gear Attach FittingsSDR FDEA201304290884Bushing · dislodgedLEFT FR 13 CIRCUMFERENTIAL JOINT SKIN HAS ONE HOLE REQUIRES BUSHING. PREVIOUS REPAIR BUSHING CAME OUT WITH FASTENER WHILE PREPARING AREA FOR A SPECIAL DETAIL INSPECTON. FABRICATED REPLACEMENT BUSHING IAW IAW SRM 51-40-51. INSTALLED REPAIR BUSHING IAW SRM 53Apr 29, 2013 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201304050731Adapter · crackedMAIN DECK CABIN AT FR 54.2 BETWEEN SEAT TRACK 2R AND 3R HAS A CLEVIS ADAPTER SCALLOP CRACKED. REMOVED CLEVIS ADAPTER, FABRICATED DRILLED AND REPROTECTED REPAIR ADAPTER IAW SRM 51-72-10 AND SRM 51-75-10. INSTALLED CLEVIS ADAPTER IAW SRM 51-72-10. REMOVED ANApr 5, 2013 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201303300691Floorboard · crackedMAIN DECK CARGO FLOORBOARD 241TH IS CRACKED ACCROSS ITS WIDTH. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Mar 30, 2013 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201303240654Link · crackedMAIN DECK CARGO FR 48 LOWER STRUCTURE THRUST PLATE TAB CRACKED. R & R ONE THRUST PLATE LINK IAW SRM 51-72-10.Mar 24, 2013 · N728FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201303210635Floor Panel · corrodedFWD CARGO FLOOR PANEL 131QF BACK SIDE HAS APPROX 60 SQUARE INCHES OF CORROSION EXTENDING UNDER METAL FOIL COVERING. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG. SRZ-25-005 REV J.Mar 21, 2013 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201303210634Floor Panel · inoperativeFWD CARGO FLOOR PANEL 131YF HAS BROKE OUT FILLER AT FASTENER HOLE AND SIX PUNCTURES ON BACK SIDE. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005 REV J.Mar 21, 2013 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201303200627Floor Panel · damagedFWD CARGO FLOOR PANEL 132QF INNER SURFACE HAS SIX PUNCTURES. FABRICATED REPLACEMENT PANEL 132QF IAW DWG SR2 25-005, REV J.Mar 20, 2013 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201303200632Floorboard · delaminatedAFT CARGO FLOORBOARD 161AF SKIN DELAMINATED BY 3 FT X .5 FT ON 1 CORNER AND 10 X 2" ON OPPOSITE CORNER. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-011, REV E, DWG SRZ 25-005, REV J.Mar 20, 2013 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201303200631Floorboard · damagedON REMOVAL OF FLOORBOARD 242FK TO ACCESS MAINTENANCE REPAIR PER N/R 00300. FOUND FLOORBOARD LOWER SKIN TORN BY 1 1/2 X 1 1/2 INCH. FABRICATED REPLACEMENT FLOORBOARDIAW DWG SRZ 25-005 REV JMar 20, 2013 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201303200630Floor Panel · damagedAFT CARGO FLOOR PANEL 162HF HAS A CRACK HOLE PUNCH MEASURES 1.2500" AND 1 HOLE PUNCH IMPACT 1 INCH AND EDGE SKIN TORN BY 4 INCH AND SEVERAL SMALL HOLE PUNCHES FABRICATED. REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-011, REV E AND SRZ 25-005, REV J.Mar 20, 2013 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201303200629Floor Panel · damagedAFT CARGO FLOOR PANEL 161 GF HAS A CUT OF 2", IMPACT CUT 2.5", SKIN CUT .7500. IMPACT DENT MEASURES 2 X 2" IN UPPER SKIN SURFACE. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J AND SRZ 25-011, REV E.Mar 20, 2013 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201303200628Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241WH IS CRACKED ACCROSS ITS WIDTH. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J.Mar 20, 2013 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201303190614Floorboard · damagedFLOORBOARD 24GK , INBD FWD CORNER IS BROKEN OFF. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.Mar 19, 2013 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201303190613Floorboard · crackedFLOORBOARD 242VH IS CRACKED ALL THE WAY ACCROSS. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.Mar 19, 2013 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201303190612Floorboard · damagedFLOORBOARD 241RJ IS BROKEN IN TWO. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005 REV J.Mar 19, 2013 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201303190611Floorboard · crackedMAIN DECK CARGO FLOORBOARD 242ZJ HAS APPROX A 10 INCH CRACK. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Mar 19, 2013 · N728FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201109264125Drag Strut · failedDURING ROUTINE NORMAL GEAR EXTENTION AND RETRACTION POST REINSTALLATION OF MLG ACTUATORS. THE NLG TELESCOPIC DRAG STRUT WITH THE PIN INSTALLED, BEGAN TO RETRACT AND SHEARED THE PIN AND THE DOWN LOCK VALVE. R & R NLG TELESCOPIC STRUT IAW AMM 32-31-24-04. PSep 26, 2011 · N728FD · Airbus A300B4622R · Nose/Tail Landing Gear Strut/AxleSDR FDEA201103171057Transmitter · malfunctionedFLIGHT, ECAM "HYD LO QTY-GREEN" ALERT TURNED OFF GREEN PUMPS, QTY WAS RED DOT 1.3 GALLONS. WITH GREEN PUMPS OFF QTY REMAINED 1.3 TILL AFTER LANDING. HYD PUMPS NEVER WERE OPERATED DRY, HYD PUMPS ALLWAYS HAD OPERATING PRESS TILL SHUTOFF, THEN ALLWAYS HAD CMar 17, 2011 · N728FD · Airbus A300B4622R · Hydraulic Indicating SystemSDR FDEA201103150974Rib · crackedLT WING INBD T/E FLAP HORIZ UPPER FLANGE OF RIB 25A FOUND CRACKED RIB AT LT WING INBD T/E FLAP HORIZ UPPER FLANGE OF RIB 25A R & R IAW SRM 51-40-21, REV 74. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Mar 15, 2011 · N728FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201103050862Frame · crackedREFER TO FEDEX E.O. 6-5310-7-5017A PART 4, EOCN A4: HFEC INSPECTION CARRIED OUT AND FOUND FASTENER HOLE "K" WITH CRACKED INDICATION AT FRAME 47RH, BETWEEN STR 24 AND STR 25 INNER CHORD. ONE (1) EACH FASTENER HOLE (HOLE K) AT RIGHT HAND FRAME 47 INNER CHORDMar 5, 2011 · N728FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201102220690Angle · wornFWD CARGO DOOR AT UPPER HINGE CUT OUT AREA FOUND NR 9 HINGE FROM FWD WITH WORN HINGE STOP FITTING. WORN ANGLE STOP FITTING AT FORWARD CARGO DOOR UPPER HINGE CUT-OUT AREA NR 9 REPLACED PER EA 6-5340-147605. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Feb 22, 2011 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201102210642Mount · corrodedFWD NR 2 ENGINE MOUNT MATING SURFACE FOUND WITH CORROSION. CORROSION REMOVED AT NR 2 ENGINE FORWARD MOUNT MATING SURFACE AND FOUND WITHIN LIMITS AS PER CMM 71-20-04 REPAIR 5 FIGURE 504 REV 54. MATERIAL ORIGINAL THICKNESS= 0.765", MATERIAL REMOVED= 0.003", Feb 21, 2011 · N728FD · Airbus A300B4622R · Engine Mount SectionSDR FDEA201102210641Mount · corrodedAFT ENGINE MOUNT MATING SURFACE FOUND WITH CORROSION. CORROSION REMOVED AND CLEANED-UP PER CMM 71-20-05 REPAIR 3 TABLE 601 REV 50 AND FOUND WITHIN LIMITS AS PER CMM 71-20-05 FIGURE 501 REV 50. ORIGINAL MATERIAL THICKNESS= 0.125", MATERIAL REMOVED= 0.002"Feb 21, 2011 · N728FD · Airbus A300B4622R · Engine Mount SectionSDR FDEA201102210640Mount · corrodedNR 2 ENGINE PYLON - FWD ENGINE MOUNT BOLT HOLE FOUND WITH SPOT FACE CORRODED. COROSSION REMOVED AS PER SRM 51-74-10 REV 74 AND FOUND WITHIN LIMITS AS PER SRM 54-51- 81 FIGURE 104 REV 74. ORIGINAL MATERIAL THICKNESS: 0.078" , MATERIAL REMOVED: 0.017", MATERIFeb 21, 2011 · N728FD · Airbus A300B4622R · Engine Mount SectionSDR FDEA201102200639Spar · damagedSPAR REF EO 6-5710-7-3305 PART 2, STEP 15 HOLE (I) DIAMETER OF HOLE EXCEEDED EO REQUIREMENT LIMIT. HOLE (I) DIAMETER = 0.572" (MAXIMUM DIAMETER ALLOWED = 0.531"). EO 6-5710-7-3305 PART 2, STEP 15 HOLE (I) DIAMETER REPAIR HAS EXISTING REPAIR RECORD AND PREVIFeb 20, 2011 · N728FD · Airbus A300B4622R · Wing SparSDR FDEA201102180628Skin · crackedLT WING FIXED T/E PANEL UPPER SURFACE AT APPROX STA 1270, FOUND CRACKED. REPAIRED AS PER SRM 57-51-12 FIGURE 210 REV 74. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 111.Feb 18, 2011 · N728FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA201102180627Skin · dentedLOWER FUSELAGE SKIN FOUND WITH DENT BETWEEN STATION FR 67 AND FR68, BULK CARGO DOOR CUT OUT LOWER SKIN AREA. MEASURED DENT = 0.034", WIDTH = 0.610", LENGTH = 1.190". REPAIR ACCOMPLISHED PER E.A.6-5330-147612. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVFeb 18, 2011 · N728FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201102180626Panel · crackedHORIZONTAL STABILIZER - RT INBD L/E PANEL NR 341AB FOUND WITH 0.75 INCH CRACK ON MOST INBD FRAME (RIB) EDGE. REPAIR ACCOMPLISHED AS PER E.A. 6-5510-142456. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 111.Feb 18, 2011 · N728FD · Airbus A300B4622R · Horizontal Stabilizer, Plate/SkinSDR FDEA201102180625Support · damagedAFT FUSELAGE COMPARTMENT - SUPPORT FRAME ON FRAME 86, STRINGER 36 FOUND DAMAGED. DAMAGED SUPPORT FRAME REMOVED AND NEW SUPPORT FRAME INSTALLED PER SRM 51-40-21 REV 74. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 111.Feb 18, 2011 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201102180624Support · damagedAFT FUSELAGE COMPARTMENT - SUPPORT FRAME ON FRAME 86, STRINGER 33 FOUND DAMAGED. DAMAGED SUPPORT FRAME REMOVED AND REPLACED WITH NEW SUPPORT FRAME PER SRM 51-40-21 REV 74. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 111.Feb 18, 2011 · N728FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
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