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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA202011122831Angle · crackedRT WING, RIB 8 INSPECTION OF CENTER SPAR SEALING ANGLE VERTICAL WEB ADJACENT TO PYLON REAR ATTACH FITTING, FASTENER HOLE 58 FOUND CRACK. COMPLIED WITH EA: 6-5710-106289 C P4. TITLE: WINGS-BASIC WING STRUCTURE-SB A300-57-6033 ELONGATED HOLES & CRACK AT RIB 8 SDR FDEA202011122830Floorbeam · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE CROSSBEAM CORRODED AT FR 60 BETWEEN Y805 AND -Y805. REPAIRED THE AFT CARGO COMPARTMENT FLOOR SUPPORT CROSSBEAM AT FR 60 BETWEEN Y805 AND -Y805, PER A300-600 SRM 53-10-15-201 PARAGRAPH 9. THIS IS CATEGORY A REPAIRSDR FDEA202011122829Crossbeam · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE-CROSSBEAM CORRODED, AT FR 59, BETWEEN Y805 AND -Y805. REPAIRED THE AFT CARGO COMPARTMENT FLOOR SUPPORT CROSSBEAM AT FR 59, BETWEEN Y805 AND -Y805, PER A300-600 SRM53-10-15-201 PARAGRAPH 9. THIS IS CATEGORY A REPASDR FDEA202011122828Pressure Deck · damagedHORIZONTAL PRESSURE DECK UPPER SURFACE BETWEEN FR 39 AND FR 40, -Y1959 AND -Y2462 FOUND 1 EA PUNCTURE. COMPLIED WITH EA: 6-5310-T0357997 P1. TITLE: FUSELAGE-MAINFRAME-PUNCTURE ON PRESSURE FLOOR PANEL BETWEEN FR 39 AND FR 40 AT Y-2354-REPAIR. REPAIRED THE HOSDR FDEA202011122833Skin · crackedRT WING-RIB 15 RIB 16, WING UPPER SKIN CRACKED APPROXIMATELY 3.0 INCH IN LENGTH (NEAR REAR SPAR). REPAIRED THE RT WING RIB 15-RIB 16 UPPER SKIN NEAR REAR SPAR CRACK, PER A300-600 SRM 57-20-12-201 PARA 4B. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMSDR FDEA202011082797Hinge Arm · delaminatedLT WING NR 4 SPOILER CENTER INBOARD HINGE ARM LOWER SURFACE AND CENTER OUTBOARD HINGE ARM OUTBOARD SURFACE FOUND DELAMINATION. SIZE: 50MM * 30MM DEPTH: 2.66MM, 20MM * 10MM DEPTH: 1.63MM. COMPLIED WITH EA: 6-5750-T0357699 P1. EA TITLE: WING-FLIGHT SURFACES-LSDR FDEA202011082796Hinge Arm · delaminatedRT WING NR 3 SPOILER CENTER INBOARD HINGE ARM OUTBOARD ZONE FOUND DELAMINATION. AREA: 20MM*10MM DEPTH: 1.42MM COMPLIED WITH EA: 6-5750-T0357731 P1. EA TITLE: WING-FLIGHT SURFACES-RT NR 3 SPOILER ENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE RT SDR FDEA202011052776Stiffener · crackedCENTER WING BOX FRONT SPAR VERTICAL STIFFENER AT Y1456 LOWER END CRACKED COMPLIED WITH EA: 6-5710-T0358000 P1. EA TITLE: WINGS-BASIC WING STRUCTURE- CWB FRONT SPAR VERTICAL STIFFENER CRACK AT FR 40, Y1456 LT SIDE-REPAIR. REPAIRED THE CENTER WING BOX FRONT SSDR FDEA202011052778Stiffener · crackedCENTER WING BOX FRONT SPAR VERTICAL STIFFENER AT Y450 LOWER END CRACKED. REPAIRED THE CENTER WING BOX FRONT SPAR VERTICAL STIFFENER AT Y450 LOWER END CRACK, PER A300-600 SRM57-10-21 FIG 201. THIS IS CATEGORY A REPAIR. MAJOR REPAIR, IAW FEDEX GMM6-2-100.SDR FDEA202011052777Stiffener · crackedCENTER WING BOX FRONT SPAR VERTICAL STIFFENER AT Y953 LOWER END CRACKED. REPAIRED THE CENTER WING BOX FRONT SPAR VERTICAL STIFFENER AT Y953 LOWER END CRACK, PER A300-600 SRM57-10-21 FIG 201. THIS IS CATEGORY A REPAIR. MAJOR REPAIR, IAW FEDEX GMM6-2-100.SDR FDEA202011052780Stiffener · crackedCENTER WING BOX FRONT SPAR VERTICAL STIFFENER AT -Y953 LOWER END CRACKED.SDR FDEA202011052779Stiffener · crackedCENTER WING BOX FRONT SPAR VERTICAL STIFFENER AT Y0 LOWER END CRACKED.SDR FDEA202011012740Stringer · corrodedAFT CARGO STRINGER 46RH FOUND CORROSION BETWEEN FR60 AND FR64 COMPLIED WITH EA: 6-5310-147615 A P2. TITLE: FUSELAGE - MAINFRAME - PREVIOUS REPAIR ON STRINGER 46RH, BETWEEN FR63 AND 63A. REPAIRED THE AFT CARGO STRINGER 46RH BETWEEN FR60 AND FR64 CORROSION. SDR FDEA202011012739Web · crackedMAIN DECK FR47 Y953~Y1456 UNDERFLOOR WEB CRACKED REPAIRED THE MAIN DECK FR47 Y953~Y1456 UNDERFLOOR CRACKED WEB PER A300-600 SRM53- 15-15 FIG201 SHEET 2 , THIS IS CATEGORY B REPAIR AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600 SRI 53-15-15-2-0SDR FDEA202011012738Web · crackedMAIN DECK FR47 Y0~Y450 UNDERFLOOR WEB CRACKED FABRICATED THE REPAIR PART PER DWG: A53832100 AND PART MARKED AS FXA5383210020800 PER GMM7-0-1001. REPLACED THE MAIN DECK FR47 Y0~Y450 UNDERFLOOR CRACKED WEB PER A300-600 SRM51-40-21. THIS IS CATEGORY A REPASDR FDEA202010162535Pitot Head · failedPDIS 728 34-14 5508 16OCT20 VCV OPEN U. REJECTED TAKE-OFF FOR AIRSPEED DISCREPANCY BETWEEN F/O AND CAPT SIDE. REPLACED F/O'S PITOT PROBE, REF MM 34-11-15-04. AMT RVSM M54RV01 EXP 15JUL21-A/C REMAINS RVSM CAPABLE. SDR INFO: MPN OFF=0851HV, S/N OFF=320060, MSDR FDEA201910282763Wire Harness · damagedMDIS 728 21-26 4813 26OCT19 MEM OPEN U WHILE PREFORMING "FLIGHT COMPARTMENT AND ELECTRONICS RACKS AIR DISTRIBUTION - ADJUSTMENT/TEST" AMM 21-21-00-05, CBS: EXTRACT FAN HI SPD, HI SPD, STBY PITOT SUPPLY, FAN SUPPLY LO SPD, 105 XP BUS BAR, HYD SDR FDEA2019082312000Indicator · inaccurateLEVEL AT FL 340, BOTH CA & FO STBY AIRSPEED INDICATORS INDICATED 125 KTS. BOTH CA & FO PRIMARY A/S IND. ON EFIS INDICATED 275 KTS. TAS 470 KTS. TAT -12. VMC CONDITIONS. APPROX 40 MINUTES LATER, WITH NO CHANGE IN CONDITIONS, BOTH STBY A/S IND. RETURNED TO SDR FDEA201906181353Floor Panel · damagedMAIN CABIN FLOOR PANEL 231TG IS BROKEN @ PREVIOUS REPAIR. FABRICATED NEW FLOOR PANEL PER FEDEX SRZ 25-005 REV P.SDR FDEA2019062081352Floor Panel · damagedMAIN CABIN FLOOR PANEL 232CF HAS A BROKEN CORNER, FOUND BEFORE REMOVAL FABRICATED NEW FLOOR PANEL PER FEDEX SRZ 25-005 REV P.SDR FDEA2019062081351Floor Panel · damagedMAIN CABIN FLOOR PANEL 232LG HAS MISSING EDGE FILLER AND IS DELAMMED IN THE CORNER OR THE BOARD. FABRICATED NEW FLOOR PANEL PER FEDEX SRZ 25-005 REV P.SDR FDEA2019062081350Floor Panel · damagedMAIN CABIN FLOOR PANEL 232GG HAS MULTIPLE PUNCTURES FABRICATED NEW FLOOR PANEL PER FEDEX SRZ 25-005 REV P.SDR FDEA2019062081349Floor Panel · damagedMAIN CABIN FLOOR PANEL 231LG HAS A CRACKED SKIN ON BOTTOM OF PANEL AND IS PUNCTURED. FABRICATED NEW FLOOR PANEL PER FEDEX SRZ 25-005 REV P.SDR FDEA2019062081348Floor Panel · damagedMAIN CABIN FLOOR PANEL 231WG HAS A CRACKED SKIN ON BOTTOM OF PANEL FABRICATED NEW FLOOR PANEL PER FEDEX SRZ 25-005 REV P.SDR FDEA2019062081347Floor Panel · damagedMAIN CABIN FLOOR PANEL 221PF HAS MULTIPLE PUNCTURES IN SKIN FABRICATED NEW FLOOR PANEL PER FEDEX SRZ 25-005 REV P.SDR FDEA2019062081345Floor Panel · damagedMAIN CABIN FLOOR PANEL 221GF HAS CRACKED SKIN @ PREVIOUS REPAIR FABRICATED NEW FLOOR PANEL PER FEDEX DWG SRZ 25-005 REV P.SDR FDEA201804211089Fmu · malfunctionedDURING DESCENT THROUGH FL 250, THE NR 2 ENGINE INDICATIONS ROLLED BACK AND ECAM INDICATED THE NR 2 ENGINE FAILED. NOTHING WAS NOTED AS THE CAUSE FOR THIS, GOOD OIL QUANTITY, AND GOOD FUEL INDICATIONS. AFTER GOING TO CONTINUOUS IGNITION RELIGHT, THE ENGINE SDR FDEA201712293470Skin · corrodedAVIONICS COMPARTMENT LEFT SIDE BELOW FLOOR PANEL 121LF BETWEEN FRAMES 11 AND 11A, STRINGER 49, SKIN PANEL IS CORREDED. COMPLIED WITH E 6-5330-T0337315 STEPS 1-5 DOUBLER REPAIR. MAJOR REPAIR.SDR FDEA201712293469Skin · wornLEFT WING MID FLAP UPPER AFT SURFACE HAS TWO WEAR MARKS. ACCOMPLISHED EA 6-5750-T0337587. MAJOR REPAIR.SDR FDEA201712293465Skin · wornLEFT WING OTBD FLAP UPPER SURFACE WORN. ACCOMPLISHED EA 6-5750-T0337393. MAJOR REPAIRSDR FDEA201712273458Rib · crackedLEFT WING CENTER FLAP INTERNAL RIB 26 CRACKED. REPAIRED THE RIB IAW SRM 57-50-00, FIG 201. MAJOR REPAIR.SDR FDEA201712273457Rib · crackedLEFT WING CENTER FLAP INTERNAL RIB 15 CRACKED. REPAIRED THE RIB IAW SRM 57-50-00, FIG 201. MAJOR REPAIR.SDR FDEA201712273456Rib · crackedLEFT WING CENTER FLAP INTERNAL RIB 13 CRACKED. REPAIRED THE RIB IAW SRM 57-50-00, FIG 201. MAJOR REPAIR.SDR FDEA201712273455Rib · crackedLEFT WING CENTER FLAP INTERNAL RIB 11 CRACKED AT TOP SKIN ATTACH, 6 FASTENERS FWD OF REAR SPAR. REPAIRED THE RIB FLANGE IAW SRM 57-50-00, FIG 203, MAJOR REPAIRSDR FDEA201712183410Crossbeam · corrodedAT STATION 69, STRINGER 51 RT BLK SIDE CROSSBEAM CORRODED. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 51-40-21. MAJOR REPAIR.SDR FDEA201712123365Floor Panel · damagedMAIN CABIN FLOOR PANEL 242FJ BROKEN. FABRICATED NEW FLOOR PANEL 242FJ ON T17/1311146. MAJOR REPAIR.SDR FDEA201712123375Floor Panel · brokenMAIN CABIN FLOOR PANEL 251WH BROKEN. FABRICATED NEW FLOOR PANEL 251WH ON VTMAE TRAVELER # T17/ 1311074 IAW SRZ 25-005. MAJOR REPAIRSDR FDEA201712123374Floor Panel · brokenMAIN CABIN FLOOR PANEL 241MJ BROKEN. FABRICATED NEW FLOOR PANEL 241MJ ON VTMAE TRAVELER # T17/1311189 IAW SRZ 25-005. MAJOR REPAIRSDR FDEA201712123373Floor Panel · brokenMAIN CABIN FLOOR PANEL 241DF BROKEN. FABRICATED NEW FLOOR PANEL 241DF ON VTMAE TRAVELER # T17/ 1311183 IAW SRZ 25-005. MAJOR REPAIRSDR FDEA201712123372Floor Panel · brokenMAIN CABIN FLOOR PANEL 262AH BROKEN. FABRICATED NEW FLOOR PANEL 262AH ON VTMAE TRAVELER # T17/ 1311147 IAW SRZ 25-005. MAJOR REPAIRSDR FDEA201712123370Floor Panel · brokenMAIN CABIN FLOOR PANEL 252BH BROKEN. FABRICATED NEW FLOOR PANEL 252BH ON VTMAE TRAVELER # T17/1311075 IAW SRZ 25-005. MAJOR REPAIRSDR FDEA201712123369Floor Panel · brokenMAIN CABIN FLOOR PANEL 251WG BROKEN. FABRICATED NEW FLOOR PANEL 251WG ON VTMAE TRAVELER # T17/1311150 IAW SRZ 25-005. MAJOR REPAIRSDR FDEA201712123368Floor Panel · brokenMAIN CABIN FLOOR PANEL 252AH BROKEN. FABRICATED NEW FLOOR PANEL 252AH ON VTMAE TRAVELER # T17/ 1311185 IAW SRZ 25-005. MAJOR REPAIRSDR FDEA201712123367Floor Panel · brokenMAIN CABIN FLOOR PANEL 241TJ BROKEN. FABRICATED NEW FLOOR PANEL 241TJ ON VTMAE TRAVELER # T17/ 1311076 IAW SRZ 25-005. MAJOR REPAIRSDR FDEA201712123364Floor Panel · brokenMAIN CABIN FLOOR PANEL 242YJ BROKEN. FABRICATED NEW FLOOR PANEL 242YJ ON VTMAE TRAVELER # T17/1311078 IAW SRZ 25-005. MAJOR REPAIRSDR FDEA201712123363Floor Panel · brokenMAIN CABIN FLOOR PANEL 242SH BROKEN. FABRICATED NEW FLOOR PANEL 242SH ON VTMAE TRAVELER # T17/1811149 IAW SRZ 25-005. MAJOR REPAIRSDR FDEA201712123362Floor Panel · brokenMAIN CABIN FLOOR PANEL 242BF BROKEN. FABRICATED NEW FLOOR PANEL 242BF ON VTMAE TRAVELER # T17/1311232 IAW SRZ 25-005. MAJOR REPAIRSDR FDEA201708182268Hydraulic System · lowBLUE SYSTEM HYDRAULIC WARNING LOW QUANTITY DISPLAYED DURING TAKE OFF ROLL AT 60 KTS. REJECTED THE TAKE OFF. ECAM LIGHT EXTINGUISHED WHEN THROTTLES RETARDED. DRAINED, SERVICED AND BLED THE BLUE HYD SYS AND SYS ACCUMULATOR IAW AMM 12-12-29, 12-14-29, 29-14-SDR FDEA201707191991Battery Pack · no testR1 ECAM SLIDE INDICATION IS INOPERATIVE. PERFORMED THE EMERGENCY ESCAPE SLIDE RELEASE WARNING ADJUSTMENT AND TEST. BATTERY CAPACITY TEST FROM THE BUILT-IN TEST PANEL. BATTERY CAPACITY TEST FAILED. REPLACED BOTH THE NR 1 AND 2 ASPSU BATTERIES IAW AMM 52-73-SDR FDEA201612024308Linkage · brokenNOSE GEAR DOOR FAULT LIGHT DURING GEAR EXTENSION. FAULT WENT AWAY AFTER CLEARING THE RUNWAY. FOUND THE RIGHT NLG SMALL DOOR HAS BROKEN LINKAGE AND A BROKEN AFT HINGE. INSTALLED RIGHT NOSE GEAR AFT DOOR. AND ROTATING ROD IAW AMM 32-22-13-04. JACKED NOSE G
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