N741FD

Service difficulty reports · 198

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 = 'N741FD' 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 FDEA201706051565Fitting · crackedSPAR & BOTTOM PANEL NDT INSPECTION OF HOLE F FOUND TO HAVE A CRACK SIGNAL. REPAIRED IAW EA6-5710-T0332723 P1. MAJOR REPAIR IAW GMM 6-2-100.Jun 5, 2017 · N741FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201705291542Fitting · crackedNDT INSPECTION OF THE BOTTOM PANEL FITTING FAILED WITH A CRACK SIGNAL RT SIDE, COMPLIED WITH EA6-5710-T0332723, P1. MAJOR REPAIR IAW GMM 6-2-100.May 29, 2017 · N741FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201705291543Fitting · crackedRT WING FR47 REAR SPAR AREA HOLE 155 NDT INSPECTION FOUND CRACK (D1=11.5MM, D2=8MM, DIRECTION:12 O'CLOCK, LOOK FROM UP TO LOWER) COMPLIED WITH EA6-5710-T0332723 P1 EA TITLE: WINGS-BASIC WING STRUCTURE- EO:6-5710-7-3305 E1 PT1-4-CRACK HOLES AT FR47_SB57-6113 R0May 29, 2017 · N741FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201705291541Fitting · crackedFUSE-CTR WING BOX-INSP OF REAR SPAR & BOTTOM PANEL-NDT INSPECTION OF HOLE "S" WITH CRACK SIGNAL (LT SIDE) COMPLIED WITH EA6-5710-T0332723 P1 EA TITLE:WINGS-BASIC WING STRUCTURE- EO:6-5710-7-3305 E1 PT1-4-CRACK HOLES AT FR47_SB57-6113 R0 EMBODIMENT REPAIRED THMay 29, 2017 · N741FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201705271527Fitting · crackedBOTTOM PANEL FITTING FAILED NDT INSPECTION OF HOLE F, A CRACK SIGNAL ON THE RT SIDE. COMPLIED WITH EA6-5710-T0332723, P1. MAJOR REPAIR IAW GMM 6-2-100.May 27, 2017 · N741FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201704161204Floorbeam · corrodedBULK CARGO BAY FLOORBEAM UPPER SURFACE CORRODED, FRAME 69 BETWEEN Y535 AND Y-432. REPLACED THE FLOORBEAM IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Apr 16, 2017 · N741FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA201704131161Skin · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB CRACKED. REPAIRED IAW EA:6-5750-T0332530 P1. MAJOR REPAIR IAW GMM 6-2-100.Apr 13, 2017 · N741FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201704131160Skin · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGE NDT SDI FOUND FLAP RIB 18, BTW STRINGER 2.1AND REAR SPAR, UPPER FLANGE CRACKED. REPAIRED IAW EA 6-5750-T0332530 P1. MAJOR REPAIR IAW GMM 6-2-100.Apr 13, 2017 · N741FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201704121136Floor Support · corrodedMAIN DECK FLOOR SUPPORT CORRODED, BETWEEN FRAMES 11 AND 13A, Y770. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Apr 12, 2017 · N741FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201704111225Structure · crackedRT WING ROOT STRUCTURE FR40 RT LOWER JUNCTION HOLE FOUND CRACK SIGNAL. PERFORMED A FITTING CUTOUT AND LARGE FITTING REPAIR IAW EA 6-5710-T0332507 P1. MAJOR REPAIR IAW GMM 6-2-100.Apr 11, 2017 · N741FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA201703311025Skin · crackedLOWER FUSELAGE SKIN CRACKED ON FWD CARGO DOOR CUTOUT FWD EDGE FRAME 20A, STRINGER 28R. COMPLIED WITH EA 6-5330-T0332337 P1, REPAIRED. MAJOR REPAIR IAW GMM 6-2-100Mar 31, 2017 · N741FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201603281091Sensor · malfunctionedADC FAULT 1 DURING CLIMB OUT. ADDITIONAL DISCREPANCY 22-20 7947. PITCH TRIM 2 FAULT DURING CLIMB OUT. STAB JAM ALERT. PERFORMED BITE TEST OF MTP, FAULTED AOA SENSOR 3. R & R AOA SENSOR 3 IAW AMM 22-27-39-4. PERFORMED WIRING CHECK BETWEEN AOA SENSOR 3 & DMar 28, 2016 · N741FD · Airbus A300B4622R · Stall Warning SystemSDR FDEA201601300399Control Unit · inoperativeN THE BLOCKS WE GOT AFT CARGO SMOKE DETECTION. REMOVED MAIN CARGO & RE-TESTED MAIN DECK CARGO SMOKE DETECTION, MAIN AFT SMOKE DETECTION TESTED NORMAL. SUSPECT CONDENSATION EMITTING FROM THE AMJ & AYY CANS. ORDERING SMOKE DETECTOR CONTROL UNIT. CREW STATED Jan 30, 2016 · N741FD · Airbus A300B4622R · Smoke DetectionSDR FDEA201511023438Slide · malfunctionedUPON CLOSING DOORS FOR DEPARTURE FROM GATE, THE R1 DOOR WHEN CLOSED DID NOT INDICATE 2 GREEN. WHILE TRYING TO TEST DOOR, R1 WAS INADVERTENTLY OPENED & AFTER BEING ARMED, SLIDE PARTIALLY DEPLOYED. INSTALLED LIFE RAFT IAW MM CHP 25-61-24-04-01 AS REQUIRED. ANov 2, 2015 · N741FD · Airbus A300B4622R · Escape SlideSDR FDEA201510223311Static Port · damagedDURING INSPECTION OF THE RT SIDE STATIC PORTS, FOUND FIRST OFFICERS, AFT PORT, WITH APPARENT LIGHTNING STRIKE DAMAGE. NO DAMAGE LIMITS AVAILABLE IN AMM OR SRM FOR THE PORT ITSELF. REMOVED FIRST OFFICERS STATIC PROBE 36DA IAW MM 34-11-16-04. LINES CAPPED, EOct 22, 2015 · N741FD · Airbus A300B4622R · Pitot/Static SystemSDR FDEA201509092824Sensor · inoperativeDURING TAKEOFF AT 70 KIAS, RECEIVED ECAM WARNING FOR TRIM NOT IN TAKEOFF RANGE. ABORTED TAKEOFF, CHECKED TRIM SETTINGS, ALL GOOD. ATTEMPTED TAKEOFF ON POWER APPLICATION, RECEIVED INTERMITTENT TRIM WARNINGS WITH POWER SET AT 1.10 EPR. RETURNED TO GATE. R Sep 9, 2015 · N741FD · Airbus A300B4622R · Stabilizer Position IndicatingSDR FDEA201411173713Splice · crackedFUSE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 & 26 LT FASTENER HOLE I WITH CRACK SIGNAL. COMPLIED WITH EO 6-5310-7-5017 P5 TO REMOVE THE CRACK. TITLE:FUSELAGE-MAIN FRAME- AD2004-20-14. INSPECTION-HOLES IN FUSELAGE. FRAME 47 SPLICE FITTING BEWTEEN STR24 & Nov 17, 2014 · N741FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201411173714Floor Support · corrodedBULK CARGO COMPARTMENT FRAME 63 - 64 Y-140 LONGITUDINAL FLOOR SUPPORT CORRODED. REPLACED THE NEW FLOOR SUPPORT PER A300-600 SRM51-40-21Nov 17, 2014 · N741FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201411113627Floor Support · corrodedMAIN DECK FWD COURIER AREA FRAMES 11 - 14, Y953 FLOOR SUPPORT CORRODED. REPAIRED IAW SRM 53-12-15 FIG 207.Nov 11, 2014 · N741FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201405070959Fitting · corrodedRIGHT RIB 5 FWD LUG HAS CORROSION IN BORE. COMPLIED WITH EA 6-5710-T0307942 P2 WING BASIC WING STRUCTURE LT & RT 5 FWD LUG CORROSION ON THE RT RIB 5 FITTING.May 7, 2014 · N741FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA201405070958Fitting · corrodedLEFT RIB 5 FWD LUG HAS CORROSION IN BORE. COMPLIED WITH EA 6-5710-T0307942 P-1, WINGS & BASIC WING STRUCTURE, LT & RT RIB 5 FWD LUG CORROSION FOR THE LT RIB 5 FITTING.May 7, 2014 · N741FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA201304300890Computer · failedFLAP RETRACTED PASSING 205KTS ECAM VMO WARNING O'SPD 205 KTS. ECAM CANCELED WARNING AND SLOWED TO 200 KTS. AFT T/O ECAM WRNG T/O CONF WRNG TOO LOW FLAPS ONLY MOMENTARYILY. PDIS 741 27-01 5155 AFT LANDING ECAM WARNING FWS AMBER FAULT MONITOR SYSTEM. AFTER TApr 30, 2013 · N741FD · Airbus A300B4622R · Trailing Edge Flap Control SystemSDR FDEA201210303777Servo Valve · failedON ROTATION, RECEIVED ECAM ANTI-SKID FAULT WITH THE BREAK FAIL ILLUMINATED. SELECTED BRAKE ANTI-SKID SWITCH TO ALTERNATE ON IAW ECAM AND BREAK FAIL LIGHT EXTINGUISHED. NR 4 BRAKE SHOWED ANTI-SKID RELEASE BARS ON ECAM. REPLACED NR 4 BRAKE NORM SERVO-VALVE (Oct 30, 2012 · N741FD · Airbus A300B4622R · Brake Anti-Skid SectionSDR FDEA201208263176Roller Track · corrodedFWD CARGO BAY ROLLER TRACK LWR SURFACE CORRODED. REMOVE THE ROLLER TRACK IAW AMM25-52-21-04. CUT OUT THE DAMAGE PORTION IAW SRM 53-10-15/201. MAKE THE REPAIR DOUBLER IAW SRM 53-10-15/201. FABRICATE THE ROLLER TRACK REPAIR PART AND THE L-SECTION REPAIR PARTAug 26, 2012 · N741FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201208263169Floorbeam · corrodedCARGO BAY FR 69 FLOORBEAM CORRODED. BLEND OUT THE CORROSION IAW SRM 51-74-10 AND APPLY ALODINE IAW SRM 51-21-10. MEASURE THE REMAINING THICKNESS IAW NTM51-10-04, THE REMAINING THICKNESS IS 0.075 INCHES. ORIGINAL THICKNESS IS 0.098", FOUND OUT OF LIMITS IAWAug 26, 2012 · N741FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA201208243150Window Frame · chafedCOCKPIT LT SLIDING WINDOW FRAME FWD SECTION EDGE CHAFED COMPLY WITH EA:6-5610-149055.Aug 24, 2012 · N741FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201208233136Stringer · corrodedAFT CARGO BAY FR 54-FR 54.1, S56L STRINGER CORRODED. REMOVE THE RELATED FASTENERS IAW SRM 51-40-21. BLEND OUT THE CORROSION IAW SRM 51-74-10 & APPLY ALODINE IAW SRM 51-21-10. MEASURE THE REMAINING THICKNESS IAW NTM 51-10-04 & CHECK FOR CRACK IAW NTM51-10-08Aug 23, 2012 · N741FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA201208233133Structure · damagedRT WING TIP L/E FOUND ONE LIGHTNING STRIKE, COMPLIED WITH EA 6-5730-149056.Aug 23, 2012 · N741FD · Airbus A300B4622R · Wing Main, Frame StructureSDR FDEA201208173046Skin · damagedFUSELAGE CROWN SKIN FOUND LIGHTNING STRIKE UNDER VHF ANTENNA BETWEEN FR 20-21. REPAIRED EA 6-5330-149057.Aug 17, 2012 · N741FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201208072869Crossbeam · corrodedMAIN DECK FR50 -Y1959 TO -Y2462 CROSSBEAM CORRODED. REMOVED ADAPTOR PER SRM 51-40-21. FABRICATED REPAIR PARTS PER DWG:Y53829705. INSTALLED REPAIR ADAPTOR CROSSBEAM PER SRM 51-40-21 4. RESTORED FINISH PER SRM 51-75-10.Aug 7, 2012 · N741FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA201208072870Floor Support · corrodedMAIN DECK FR11-14 Y1456 FLOOR SUPPORT CORRODED. REPAIRED IAW EA 6-5310-162732.Aug 7, 2012 · N741FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201204241572Sensor · malfunctionedNR 2 ENGINE SHUTDOWN IN FLIGHT, DUE TO HIGH OIL TEMPERATURE AT 180 DEGREES. OIL DELTA T WAS 0 DEGREE CENTIGRADE 31 MIN WINDMILLING. DFDR DATA CONFIRMED THE NR 2 ENGINE OIL TEMPERATURE INDICATION SYS WAS ERRATIC BEFORE ENGINE SHUTDOWN. R & R NR 2 ENGINE TApr 24, 2012 · N741FD · Airbus A300B4622R · Engine Temperature Indicating SystemSDR FDEA201112085211Coalescer Bag · odorNR 2 PACK FLOW BECAME UNSTABLE IN CRUISE, LOW FLOW ADVISORY, INLET TEMPS VARYING WILDLY. NR 1 PACK LOW FLOW INDICATION AFTER SEVEAL HOURS OF NORMAL USE. FAINTLY ODD PACK ODOR ACOMPANIED PACK ADVISORY INLET TEMPS NR 1-20C, NR 2-60C. NR 1 PACK VALVE DISAGRDec 8, 2011 · N741FD · Airbus A300B4622R · Humidity Control SystemSDR FDEA201108313592Bulb · failedAFTER LEVEL OFF, GOT ECAM ADVISORY (NO OTHER ALERTS OR WARNINGS) OF NR2 ENG OIL TEMP ABOVE 177 DEG C SHUTDOWN NR 2 ENG ACCORDING TO QRH PROCEDURES DIVERTED. REMOVED AND REPLACED NEW OIL TEMP BULB PER MM 79-32-11-04-0. LEAK CHECKED AND SAFTEY WIRED AFTER CHECAug 31, 2011 · N741FD · Airbus A300B4622R · Engine Oil Indicating SystemSDR FDEA201101120128Computer · faultedPITCH FEEL NR 2 FAULTED TURNED IT OFF FOR APPROX (1) MINUTE RESET AND FAULT WENT AWAY. (2) MINUTES LATER IT FAULTED AGAIN IAW ECAM/QRH TURNED IT OFF AND COMPLIED W/QRH. FOUND FAULT LIGHT ON NR 2 COMPUTER FLC R & R IAW MM 27-23-26-4.Jan 12, 2011 · N741FD · Airbus A300B4622R · Stabilizer Control SystemSDR FDEA201011234474Smoke Detector · failedAVIONICS SMOKE INDICATION PASSING 13000'. CHECKED AVIONICS COMPARTMENT SMOKE DETECTION USING MM-26-15-00-05 OPS NORMAL. AS A PRECAUTION R&R COCKPIT AND AVIONICS SMOKE DETECTORS. USING MM-26-15-12-04. ALSO OPS NORMAL. ACFT OK FOR SERVICE.Nov 23, 2010 · N741FD · Airbus A300B4622R · Fire DetectionSDR FDEA201008203058Skin · corrodedLT WING BOTTOM SKIN LOWER SURFACE HAS CORROSION BETWEEN THE CTR SPAR AND THE REAR SPAR IN NUMEROUS SPOPTS JUST INBD OF THE NR1 PYLON. RIB 7-8. REMOVED SEAL, AFT LOWER FAIRING SECTION, AFT PYLON SECTION AND 3 EA. ATTACH BRACKETS PER SRM 51-40-21, PARA'S 5Aug 20, 2010 · N741FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA201008102910Skin · crackedRT WING LOWER SKIN PANEL FASTENER HOLE CRACKED. COMPLIED WITH EA 6-5710-136685.Aug 10, 2010 · N741FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA201008042809Fairing · delaminatedRIGHT WING FLAP TRACK FAIRING 633 BB INTERIOR IS DELAMINATED. REPAIRED RT FLAP FAIRING 633 BB BY REMOVING DELAMINATED AREA, FABRICATING AND BONDING NEW CORE PLUG; APPLYING AND CURING FIBERGLASS REPAIR OVERLAYS IAW EA 36-5750-136688 AND SRM 57-20-35.Aug 4, 2010 · N741FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201008032788Fitting · crackedRT WING JACK PAD FITTING IS CRACKED. REMOVED FITTING SRM 51-40-21, PARA 5, PG 7. MACHINED NEW JACK PAD IAW DWG A57240935, ISSUE "C". DIMENSION CHECK ON JACK PAD WITHIN LIMITS. FINAL HOLE SIZES WILL BE REAMED TO SIZE PRIOR TO INSTALLATION ON ACFT IAW DWG A5Aug 3, 2010 · N741FD · Airbus A300B4622R · Wing, Attach FittingsSDR FDEA201008022785Support · crackedNR 2 PYLON RT FWD L/E NACELLE FAIRING STRUCTURE IS CRACKED AT A FASTENER. R & R CRACKED A5461221600040 SUPPORT WITH A NEW A5461221600040 SUPPORT, PO 688444.2 IAW SRM 51-40-21, PG 7.Aug 2, 2010 · N741FD · Airbus A300B4622R · Nacelle/Pylon, Main FrameSDR FDEA201008022784Support · crackedNR1 PYLON LT FWD L/E NACELLE FAIRING STRUCTURE IS CRACKED AT A FASTENER. R & R CRACKED A5461221600040 SUPPORT WITH A NEW A5461221600040 SUPPORT, PO 688444.2 IAW SRM 51-40-21, PG 7.Aug 2, 2010 · N741FD · Airbus A300B4622R · Nacelle/Pylon, Main FrameSDR FDEA201007262691Skin · crackedRIGHT WING LEADING EDGE SKIN AT THE NR 3 SCREW JACK CUTOUT UPPER INBD CORNER. VERIFIED CRACK BY HFEC IAW NTM PT6 51-10-08, CRACK FOUND. REMOVED DAMAGED SKIN SECTION IAW SRM 57-44-12, FIG 203. MATERIAL ID FOR A REPAIR PARTS 0.063 7075-T6, PO 678296.3 PER A30Jul 26, 2010 · N741FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA201007152535Attach Bracket · crackedMAIN CABIN UNDER FLOOR WEB ATTACH BRACKET CRACKED. FR.48,RBL70. REMOVED CRACKED WEB ATTACH BRACKET IAW SRM 51-40-21. DRILLED TO FIT, NEW WEB BRACKET IAW SRM 51-72-10, PG 2. INSTALLED NEW WEB ATACH BRACKET IAW SRM 51-72-10 PG 2 AND SRM51-40-21.Jul 15, 2010 · N741FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA201007132496Seat Track · damagedMAIN CABIN FLOOR TRACK SCALLOP BROKEN BS X3018,FR 42- FR 43,LBL Y1456. REMOVED SEAT TRACK SECTION AT FR.40 TO FR.45 LBLY1456 IAW SRM 51-40-21, MAT ID FOR NEW SECTION OF SEAT TRACK A53274005 PO 699729.2 IAW SRM 53-15-16 FIG.4 AND 53-10-16 FIG. 203. FABRICATEDJul 13, 2010 · N741FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201007092456Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 251 NG CORNER IS CRACKED FROM FRAME 57.1 - FRAME 58; LBL 58. FABRICATED NEW MAIN CARGO FLOORBOARD 251 NG IAW DWG SRZ 25-005, REV "H".Jul 9, 2010 · N741FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201007092455Floorboard · damagedMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR241 RJ IS BROKEN. FABRICATED NEW MAIN CARGO FLOORBOARD 241 RJ IAW DWG SRZ 25-005, REV "H".Jul 9, 2010 · N741FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201007092454Floorboard · damagedMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 242 RJ IS BROKEN. FABRICATED NEW FLOORBOARD 242 RJ IAW DWG SRZ 25-005, REV "H".Jul 9, 2010 · N741FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201007092453Floorboard · damagedMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 242 JV IS BROKEN. FABRICATED NEW FLOORBOARD 242 VJ IAW DWG SRZ 25-005, REV "H".Jul 9, 2010 · N741FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201007092452Floorboard · brokenMAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 242 ZH IS BROKEN. FABRICATED NEW FLOORBOARD 242 ZH IAW DWG SRZ 25-005, REV "H".Jul 9, 2010 · N741FD · Airbus A300B4622R · Fuselage Floor Panel
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