N727FD

Service difficulty reports · 185

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 = 'N727FD' 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 FDEA202006191291Floor Panel · crackedMAIN CARGO FLOOR PANEL 241VH HAS CRACK. FABRICATED FLOOR PANEL 241VH ON VT MAE TRAVELER TD/000321 IAW DWG SRZ-25-005 REV R. CLASSIFIED AS CAT "A" MAJOR REPAIR. INSTALLED FLOOR PANEL 241VH ON 240-FL-FIT CARD 000079.Jun 19, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA202006191290Floor Panel · crackedMAIN CARGO FLOOR PANEL 241SH HAS CRACK. FABRICATED FLOOR PANEL 241SH ON VT MAE TRAVELER TD/000316 IAW SRZ-25-005 REV R. CLASSIFED AS CAT "A" MAJOR REPAIR. FLOOR PANEL 241SH INSTALLED ON 240-FL-FIT CARD 000079.Jun 19, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA202006191289Floor Panel · crackedMAIN CARGO FLOOR PANEL 241ZH HAS CRACK. FABRICATED FLOOR PANEL 241HZ ON TD/000320 IAW SRZ-25-005 REV R. CLASSIFED AS CAT "A" MAJOR REPAIR. FLOOR PANEL 241ZH INSTALLED ON 240-FL-FIT CARD 000079.Jun 19, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA202006191286Floor Panel · crackedMAIN CARGO FLOOR PANEL 241EF HAS CRACK. FABRICATED FLOOR PANEL ON VTMAE TRAVELER # TD/000315 IAW SRZ 25-005 REV "R". CLASSIFIED AS CAT "A" REPAIR. FLOOR PANEL 241EF INSTALLED ON 240-FL-FIT CARD # 000079. MAJOR REPAIRJun 19, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA202006161258Floor Panel · crackedMAIN CARGO FLOOR PANEL 242LK WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005 REV R. CLASSIFIED AS A CATAGORY A REPAIR. THE FLOOR PANEL WAS INSTALLED. MAJOR REPAIR.Jun 16, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA202006161256Floor Panel · crackedMAIN CARGO FLOOR PANEL 241AK WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005 REV R. CLASSIFIED AS A CATATORY A REPAIR. THE FLOOR PANEL WAS INSTALLED. MAJOR REPAIR.Jun 16, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA202006161255Floor Panel · crackedMAIN CARGO FLOOR PANEL 242JF WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005 REV R. CLASSIFIED AS A CATAGORY A REPAIR. FLOOR PANEL INATALLED. MAJOR REPAIR.Jun 16, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA202006161257Floor Panel · crackedMAIN CARGO FLOOR PANEL 242QJ WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005 REV R. CLASSIFIED AS CATAGORY A REPAIR. THE FLOOR PANEL WAS INSTALLED. MAJOR REPAIR.Jun 16, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA202006161254Floor Panel · crackedMAIN CARGO FLOOR PANEL 242FJ WAS CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ 25-005 REV "R". CLASSIFIED AS A CATAGORY A REPAIR. THE FLOOR PANEL WAS INSTALLED. MAJOR REPAIR.Jun 16, 2020 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2020061651242Seat Track · damagedMCD SEAT TRACK AT STA -Y1959 FR 29-30 HAS ELONGATED FASTENER HOLE. CUT OUT DAMAGE IAW SRM 51-73-10, FABRICATED ANGLE AND FILLER IAW SRM 53-10-16 FIG 201, TREATED AND PRIMED IAW SRM 51-21-10, TOP COATED IAW SRM 51-75-10, INSTALLED ANGLE AND FILLER IAW SRM 51-4Jun 15, 2020 · N727FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020010650022Switch · faultyPRIOR TO ENGINE START BEACON WAS TURNED ON. ELECTRICAL SMOKE SMELL WAS NOTICED AND BREAKER FOR UPPER BEACON POPPED. SMELL DISIPATED AFTER BREAKER POPPED. INSPECTED AREA INSIDE BREAKER PANEL FOR SIGNS OF DEBRIS OR BURNT WIRING, NONE FOUND. PLACED UPPER BEACJan 5, 2020 · N727FD · Airbus A300B4622R · Exterior LightingSDR FDEA2018080311876Brake · crackedDURING NR 1 TIRE CHANGE, FOUND SEVERAL CRACKED ROTOR DRIVE SEGMENTS CRACKED ON NR 1 BRAKE. REMOVED AND REPLACED THE NR 1 BRAKE, REF AMM 32-42-27-04. OPS AND LEAK CKS GOOD, OK FOR SERVICE.Aug 1, 2018 · N727FD · Airbus A300F4622R · BrakeSDR FDEA201801130082Smoke Detector · contaminatedAFTER EXTENSIVE DE-ICE AND NORMAL TAKEOFF, IN CLIMB-OUT FROM MEM, RECEIVED REPETITIVE AVIONICS SMOKE ECAM. COMPLIED WITH ECAM/QRH PROCEDURES. USING SNIFFER FAN DID NOT DETECT AND SMOKE/ODORS. RETURNED TO LAND MEM. FOUND MOISTURE IN COCKPIT DUCT SMOKE DET(13Jan 13, 2018 · N727FD · Airbus A300B4622R · Smoke DetectionSDR FDEA201711093210Rib · crackedRT WING L/E RIB O/B OF KRUEGER FLAP ACTUATOR CRACKED. REMOVED RIB FROM RT WING O/B OF KRUEGER FLAP IAW SRM 51-40-21. FABRICATE RIB ON T17/1306581 INSTALLED RIB ON RT WING O/B KRUEGER FLAP IAW SRM 51-40-21. MAJOR REPAIR.Nov 9, 2017 · N727FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA201711063171Seat Track · damagedMDC SEAT TRACK SCALLOPS DAMAGED BETWEEN FR60 AND FR61, Y1456. SEAT TRACK AT Y1456 FR60 - FR61 REPAIRED IAW SRM 53-10-16 FIG 208. MAJOR REPAIRNov 6, 2017 · N727FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201711063170Support Frame · corrodedRT WING KRUGER FLAP SUPPORT FRAME LOWER SIDE HAS CORROSION AND CRACKS. REMOVED AND REPLACED SUPPORT FRAME FITTING AT RT WING KRUGER FLAP IAW SRM 51-40-21. MAJOR REPAIR.Nov 6, 2017 · N727FD · Airbus A300B4622R · Wing, Attach FittingsSDR FDEA201711033163Floor Panel · damagedPANEL 132RF FLOOR PANEL IS DAMAGED. REPAIRED FLOOR PANEL 132RF (CRACK 3.0" LONG) IAW SRM 53-10-20. MAJOR REPAIR.Nov 3, 2017 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201711023130Rib · crackedLEFT CENTER FLAP INTERNAL RIB NR 3 IS CRACKED AT TOP OF THE SKIN ATTACHMENT. REPAIRED THE RIB IAW SRM 57-50-00, STEP 4A, FIG 201. MAJOR REPAIR.Nov 2, 2017 · N727FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201710283096Floor Panel · brokenMDCC 252DK FLOOR PANEL BROKEN FABRICATED NEW FLOOR PANEL 252DK ON T17/1302769 DATED 10/17/17 IAW SRZ-25-005, MAJOR REPAIR.Oct 28, 2017 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201710283095Floor Panel · damagedMDC 241LK FLOOR PANEL BROKEN FABRICATED NEW FLOOR PANEL 241LK ON T17/1302767 DATED 10/17/17 IAW SRZ-25-005, MAJOR REPAIR.Oct 28, 2017 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201710283094Floor Panel · damagedMDCC 242RJ FLOOR PANEL BROKEN FABRICATED NEW FLOOR PANEL 242RJ ON T17/1302766 DATED 10/17/17 IAW SRZ-25-005, MAJOR REPAIR.Oct 28, 2017 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201710283093Floor Panel · damagedMDCC 241SF FLOOR PANEL BROKEN FABRICATED NEW FLOOR PANEL 241SF ON T17/1302765 DATED 10/17/17 IAW SRZ-25-005, MAJOR REPAIR.Oct 28, 2017 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201710283092Floor Panel · damagedMDCC 241PF FLOOR PANEL BROKEN FABRICATED NEW FLOOR PANEL 241PF ON T17/1302763 DATED 10/17/17 IAW SRZ-25-005, MAJOR REPAIR.Oct 28, 2017 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201710283091Floor Panel · damagedMDCC 241JF FLOOR PANEL BROKEN FABRICATED NEW FLOOR PANEL 241JF ON T17/1302770 DATED 10/17/17 IAW SRZ-25-005, MAJOR REPAIR.Oct 28, 2017 · N727FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201710203018Shear Plate · crackedMAIN DECK CARGO LT SIDEWALL SHEAR PLATE, FRAMES 80 - 81 FOUND CRACKED. REMOVED THE SHEAR PLATE IAW SRM 51-40-21, AND INSTALLED A NEW SHEAR PLATE IAW SRM 51-40-21. APPLIED TOP COAT IAW SRM 51-23-10. MAJOR REPAIR.Oct 20, 2017 · N727FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201702050479Bustle · misinstalledL1 DOOR WILL NOT DISARM. FOUND SLIDE BUSSEL WHERE GIRT BAR PASSES THRU SLIDE UPSIDE DOWN.Feb 5, 2017 · N727FD · Airbus A300B4622R · Passenger/Crew DoorsSDR FDEA201702040428Cable · failedON PRE-FLGHT FOUND RT NLG STEERING CABLE FRAYED. ONE OF THE 3 STRANDS IS BROKEN. REMOVED AND REPLACED THE NOSE GEAR STEERING CONTROL CABLE IAW AMM 32-51-00-04. PERFORMED FUNCTIONAL TEST OF STEERING HYDRAULIC SYSTEM IAW AMM 32-51-00-05. ALL TESTS WERE SATIFeb 4, 2017 · N727FD · Airbus A300B4622R · Landing Gear Steering SystemSDR FDEA201606031798Switching Unit · failedAFTER TAKEOFF & RETRACTING THE GEAR, THE GEAR DOORS DID NOT CLOSE, AMBER INDICATION ON BOTH PANELS, ALL THREE LIGHTS, LOUD NOISE & VIBRATION NOTED. RAN QRH & RETURNED. TROUBLE SHOT IAW FIM 32-30-00 FIG 104. R & R LG SELECTOR LEVER SWITCH UNIT IAW MM 32-31-1Jun 3, 2016 · N727FD · Airbus A300B4622R · Landing Gear SelectorSDR FDEA201511093539Battery · dischargedDURING PREFLIGHT CHECK, FOUND THE EMER LIGHTS TEST IN COURIER AREA INOPERATIVE. RELEASED FOR SERVICE IAW MEL 33-51-05-02 CATEGORY C, EXPIRATION 16 NOV 15. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY BATTERY IAW MM: 33-51-14-04-09. PERFORMED EMER LIGHNov 9, 2015 · N727FD · Airbus A300B4622R · Emergency LightingSDR FDEA201507232344Skin · damagedLEFT INBD FLAP MID LE UPPER SURFACE DAMAGED. COMPLIED WITH EA 6-5750-T0318847 A P 1. THE REPAIR WAS CATEGORY A. THIS REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 23, 2015 · N727FD · Airbus A300F4622R · Trailing Edge FlapsSDR FDEA201507092176Skin · damagedLEFT INBD FLAP, OTBD LE UPPER SURFACE DAMAGED. REPAIRED IAW EA 6-5750-T0318751 P 1. MAJOR REPAIR IAW GMM 6-2-100.Jul 9, 2015 · N727FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201507072160Floor Support · corrodedMDCC FRAME 12 - 14, Y953 FLOOR SUPPORT CORRODED. IAW SRM 51-74-10 . REMOVED THE CORROSION & DAMAGE WAS OUT OF LIMITS IAW SRM 53-12-15. CUT OUT THE DAMAGED AREA OF THE TEE SECTION & DEBURR THE EDGES IAW SRM 53-12-15-201 FIG 207. MANUFACTURE THE REPAIR FLOOR Jul 7, 2015 · N727FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201402120304Tire · failedAFTER LANDING FOUND NR 3 MAIN TIRE BLOWN OUT, DAMAGE NOTED TO BRAKE FAN ASSEMBLY & BRAKE TEMP WIRING. R & R MLG WHEEL ASSY IAW MM 12-37-32-00-02Feb 12, 2014 · N727FD · Airbus A300B4622R · Fuselage, Door HingeSDR FDEA201307221633Window Frame · chafedCAPTAIN`S SLIDING WINDOW FRAME SHOWS EVIDENCE OF CHAFING AND FRETTING DAMAGE FROM AN ADJACENT SOLID RIVET TAIL WHEN IN THE CLOSED POSITION. SLIDING WINDOW REPLACED IAW AMM 56-12-11-P401.Jul 22, 2013 · N727FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201307211612Skin · damagedFUSELAGE SKIN BURNED BETWEEN FRAMES 34 TO 35 S45R. REPAIRED DAMAGE. INSTALLED REPAIR ON SKIN IAW SRM 53-10-12. REPAIR IS CLASSIFIED AS MAJOR.Jul 21, 2013 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201307211611Skin · burnedNUMEROUS BURNS ON LOWER FUSELAGE SKIN. REPAIRED IAW EA 6-5313-167480 AND RDAS 70579402/003/2013.Jul 21, 2013 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201307211608Skin · burnedBURNS ON FUSELAGE SKIN AND FASTENERS BETWEEN FRAMES 21-23, S46-49R. REPAIRED IAW RDAS 70579402/003/2013 AND EA 6-5313-167480. REPAIR CLASSIFIED AS MAJOR.Jul 21, 2013 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201307211607Skin · corrodedBURNS AND CORROSION FOUND ON SKIN AND FASTENERS BETWEEN FRAMES 25-26 AND S46-51R. REPAIRED IAW RDAS 70579402/003/2013 AND EA 6-5313-167480. REPAIR CLASSIFIED AS MAJOR.Jul 21, 2013 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201307211606Skin · contaminatedSUSPECT WATER INGRESS ON LOWER SKIN OF THE LEFT ELEVATOR. INVESTIGATION CARRIED OUT IAW EA 6-5521-167459 AND EO 6-5520-7-5000, P3. LT ELEVATOR REPLACED.Jul 21, 2013 · N727FD · Airbus A300B4622R · Elevator, Plate/SkinSDR FDEA201307211610Skin · crackedLT PYLON INBD SKIN AT LOWER EDGE AT APPROX RIB 18 HAS CRACKED PANEL ATTACHING LUG. LT PYLON INBD SKIN AT LOWER EDGE AT APPROX RIB 18 X1 ATTACHMENT LUG REPAIRED IAW DWG 41R54610328, SRM 51-40-02 AND EA 6-5451-167479.Jul 21, 2013 · N727FD · Airbus A300B4622R · Nacelle/Pylon, Plate/SkinSDR FDEA201307211609Skin · crackedLEFT PYLON OTBD SKIN AT LOWER EDGE AT APPROX RIB 18 HAS 2 CRACKED PANEL ATTACHING LUGS. LEFT PYLON OTBD PYLON SKIN AT LOWER EDGE AT APPROX RIB 18 X2 ATTACHMENT LUGS. REPAIRED IAW DWG 41R54610393, SRM 51-40-02 AND EA 6-5451-167479.Jul 21, 2013 · N727FD · Airbus A300B4622R · Nacelle/Pylon, Plate/SkinSDR FDEA201307201605Window Frame · chafedF/O SLIDING WINDOW FRAME SHOWS EVIDENCE OF CHAFING/FRETTING DAMAGE FROM AN ADJACENT SOLID RIVET TAIL WHEN IN THE CLOSED POSITION. DAMAGED AREA BLENDED, ASSESSED AND NDT INSPECTED IAW CMM 56-12-11 AND NTM 51-10- 08 WITHIN LIMITS AND EA 6-5300-167476 ,PAGES 1Jul 20, 2013 · N727FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201307201604Skin · damagedFR 13 CIRCUMFERENTIAL JOINT NDT HOLE DAMAGE INDICATION LOCATED AT X 5 FASTENERS (MARKED IN BLACK INK) ABOVE STR 25RH X 5 FASTENERS LOCATED ON FR 13, STR 25RH. CLEANED, DE-BURRED AND HFEC INSPECTION C/OUT. NO FAULT INDICATIONS APPARENT. FASTENERS REPLACED WJul 20, 2013 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201307201603Skin · damagedFR 13, CIRCUMFERENTIAL JOINT NDT HOLE DAMAGE INDICATION LOCATED AT X 1 ABOVE STR 25LH. X 1 FASTENER LOCATED ON FR 13, STR 25LH HOLE CLEANED, DEBURRED AND HFEC ROTARY INSPECTION C/OUT. NO FAULT INDICATION APPARENT. FASTENER REPLACED WHILE ACCOMPLISHING EJul 20, 2013 · N727FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201307191597Rib · corrodedRIGHT WING RIB 5 FWD LUG CORROSION EVIDENT WITHIN BORE AND ON FWD AND AFT FACES RT WING RIB 5 FWD LUG CORROSION REMOVED, NDT INSPECTED AND REPAIRED IAW EA 6-5710-167468 AND REPAIR SCHEME R572-40425, ISS B, APP 3 JPF PAGES X3 ITEMS 1-8. MLG REINSTALLED. REPAIRJul 19, 2013 · N727FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA201307191596Rib · corrodedLEFT WING RIB 5 FWD LUG CORROSION EVIDENT WITHIN BORE AND ON AFT FACE LT WING RIB 5 FWD LUG CORROSION REMOVED, NDT INSPECTED AND REPAIRED IAW EA 6-5710-167467 AND REPAIR SCHEME R572-40425 ISS B APP 3 JPF PAGES X3 ITEMS 1-8. MLG REINSTALLED REPAIR CLASSED AS CAJul 19, 2013 · N727FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA201210013528Selector Valve · malfunctionedLANDING GEAR DID NOT RETRACT EITHER SYS 1 OR 2 ON FIRST TRY LOUD BANG WITH GEAR DOORS UNLOCKED INDICATION CYCLED DOWN AND UP AGAIN SYS 1 STILL UNSAFE NO LOUD BANG. DOOR INDICATE UNLOCKED MAIN GEAR DOWN GREEN CYCLED DOWN ALL INDICATED 1 GREEN APPEARED MAIN GEAOct 1, 2012 · N727FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR FDEA201209293513Landing Gear · malfunctionedLANDING GEAR WOULD NOT RETRACT, SYSTEM 2 CYCLE GEAR SAME RESULT. SWITCH TO SYSTEM 1, NO CHANGE AT FIRST, AFTER 2 OR 3 CYCLE ATTEMPS, GEAR RETRACTED. PERFORMED TROUBLESHOOTING IAW WIRING SHCEMATIC 32-31-00. SUSPECT SELECTOR VALVE MLG CONTROL OR SWITCH UNITSep 29, 2012 · N727FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR FDEA201209033213Frame · crackedCRACK INDICATION ON FR40 RT WING ROOT REPAIR CARRIED OUT IAW EA6-5315-162966 AND SB A300-57-6052.Sep 3, 2012 · N727FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201104121460Skin · corrodedSURFACE CORROSION AROUND WING FUEL LEVEL INDICATOR 1A-1 ON LT WING LOWER SURFACE. REPAIR CARRIED OUT IAW EA6-5730-150102. AREA BLENDED AND SHOT PEENED, NDT CARRIED OUT IAW NTM 57-20-10 WITH NO CORROSION EVIDENT.Apr 12, 2011 · N727FD · Airbus A300B4622R · Wing, Plate/Skin
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