N656FE
Service difficulty reports · 243
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 = 'N656FE' 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 = 'N656FE' 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 FDEA202607170941Fcu · failedDURING CLIMB OUT PASSING 5000 ATS LEVER TRIPPED OFF AND WE LOST POWER TO THE ENTIRE FCP. NO FLIGHT DIRECTORS, NO FMAS. TRIED RESETTING ATS LEVER AND PITCH TRIM AND YD LEVERS. NO LUCK. AIR TURN BACK. MANUALLY FLOWN AND NO AUTO THROTTLES. AMM: 22-15-12-04SDR FDEA202505030731Crossbeam · crackedMDCC CROSSBEAM AT FR24, Y-450 - Y-953 CRACKED. COMPLIED WITH EA 6-5310-T0383330 P1 TO REPAIR MDCC CRACKED CROSSBEAM AT FR24, Y-450 - Y-953. EA TITLE: FUSELAGE - MAINFRAME - CRACK ON FR24 CROSSBEAM, BETWEEN -Y450 AND -Y953. THIS IS CATEGORY A REPAIR. MAJOR SDR FDEA202504300692Hinge Arm · delaminatedRH WING #4 SPOILER CENTER I/B HINGE ARM LWR SURFACE FOUND DELAMINATION. SIZE: 20MM*13MM, DEPTH: 1.85MM COMPLIED WITH EA 6-5750-T0383238 P1 TO REPAIR RH WING #4 SPOILER CENTER I/B HINGE ARM LWR SURFACE DELAMINATION, EA TITLE: WING - FLIGHT SURFACES - RH #SDR FDEA202504290733Floor Support · corrodedMDCC FLOOR SUPPORT AT FR14-16, -Y1959 CORRODED. FABRICATED THE REPAIR PART PER DWG: A53612213(ISSUE.G00) AND PART MARKED AS FXA5361221321200 PER GMM7-0-1001, REPLACED THE MDCC CORRODED FLOOR SUPPORT AT FR14-16, -Y1959 PER A300-600F SRM51-40-21. THIS IS CATSDR FDEA202504280691Hinge Arm · delaminatedLH WING #5 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: 100MM*15MM, DEPTH: 1.40MM, CENTER I/B HINGE ARM OUTSIDE SURFACE SKIN FOUND DELAMINATION. SIZE: 100MM*20MM, DEPTH: 1.41MM COMPLIED WITH EA: 6-5750-T0383448 P1 TO REPAIRSDR FDEA202504230763Rib · crackedLH CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN STGR2.6 AND STGR2.7 REPAIRED THE LH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB17 BETWEEN STGR2.6 AND STGR2.7 PER A300-600F SRM57-50-00-201 FIG.201 AND COMPLIED WITH EA 6-5750-T0340067 A P2.SDR FDEA202504230656Rib · crackedLH CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB15 BETWEEN STGR2.6 AND STGR2.7, RIB15 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA:6-5750-T0383190 P1 TO REPAIR LH CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB15 BETWEEN STGR2.6 AND STGR2.7, RIB15 BETSDR FDEA202504200764Fitting · not reportedDOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION SDR FDEA202503090340Wire · chafedFOUND CONNECTOR 70WNA TO ASPSU WIRING CAFFED ON SERVERAL WIRES, REF WRI 52-10 7708. AWM: 52-73-01 INSPECTED WIRING AND FOUND ONLY SMALL SPORADIC AREAS OF OUTER INSULATION FLAKING OFF OF THE KAPTON WIRING. NO WIRING DAMAGE NOTED.SDR FDEA202502280307Battery · inoperativeDOOR R1 DOES NOT SHOW SLIDE INDICATION ON ECAM WITH DOOR CLOSED AND ARMED. RELEASED FOR SERVICE PER MEL : 52-30-04 CATEGORY : C EXPIRATION : 09MAR25 "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BESDR FDEA202502150235Ground Wire · damagedDURING EMERGENCY LIGHTS TEST FOUND EXIT LIGHT OVER R 1 DOOR INOP. WHILE TROUBLESHOOTING FOUND GROUND WIRE RECEPTACLE ON BACK OF LIGHT UNIT BROKEN OFF. REMOVED AND REPLACED R1 DOOR EXIT SIGN MODULE. OPS CHECK GOOD. PER SDR REQUIREMENTS THE UNSERVICEABLE.SDR FDEA202501310161Limit Switch · faultedRH (FO SIDE) MAIN ENTRY DOOR SLIDE DOESN T INDICATE SLIDE (ARMED) WITH DOOR SLIDE HANDLE IN ARM POSITION. DURING DEBRIEF WITH INBOUND CREW, THEY STATED THE SLIDE INDICATION WAS NORMAL DURING THEIR FLIGHT. PERFORMED BITE TEST OF AUTONOMOUS STANDBY POWERSDR FDEA202407050946Evas Unit · no testWHILE WORKING EO 6-2560-E0332400 D PT 2, BLOCK 3, DISCOVERED THAT RH EVAS BLOWER BATTERY LIGHTS DO NOT DISPLAY DURING TEST. BLOWER BLOWS BUT NO LIGHTS. RELEASED FOR SERVICE PER MEL : 25-65-04 CATEGORY : D. RT COCKPIT SMOKE VISION SYSTEM (EVAS) - INOP.SDR FDEA202405220719Accumulator · failedON CLIMB OUT GREENS SYSTEM HYDRAULIC ECAM SHOWED LOW QUANTITY. FOLLOWED ECAM PROCEDURES AND QRH. MANUAL GEAR EXTENSION AND SAFELY LANDED AIRCRAFT. TOWED OFF RUNWAY TO PARKING. FOUND GREEN SYSTEM ACCUMULATOR READING APPROXIMATELY 200 PSI. ATTEMPTED TO SERVSDR FDEA202403070250Uplock · failedNOSE GEAR DOOR INDICATED UNSAFE UPON EXTENSION FOR APPROACH AND LANDING. SPEED WAS 180KIAS. ALTITUDE WAS 4000MSL. STATUS/FLAPS WERE 15/15. COMPLIED WITH ECAM AND QRH. ON FINAL THE SECOND TIME, SELECTED FLAPS 20 AND SLOWED TO 160. PASSING 3000 FT THE GEAR SDR FDEA202304060568Smoke Detector · failedAVIONICS SMOKE MASTER WARNING ON SHORT FINAL. NO SMOKE DETECTED IN THE COCKPIT OR THROUGH SNIFFER FAN. SMOKE INDICATION AND WARNING WENT AWAY SHORTLY AFTER CLEARING THE RUNWAY. EMERGENCY DECLARED. R&R SMOKE DETECTORS 11WA MAIN BAY SMOKE DETECTOR, AND 13WASDR FDEA202301190340Fitting · noneDURING PERFORM REPEAT INSPECTION FOR CRACK HOLE AT FR40 CENTER WING JOINT LHS,FOUND MIDDLE HOLE OF CENTER WING JOINT FR40 LHS BOLT HOLE DIAMTER DEVIATION. I.A.W WORK CARD T 6-5710-T0321988 CP3,EA WORK CARD TITLE:WING-BASIC WING STRUCTURE- 2019-21-01-CRACK HSDR FDEA202301180236Web · damagedAIRCRAFT REPAIR ASSESSMENT: EXISTING WEB REPAIR FOUND ON M/D WEB AT FR47, BTW Y0~Y450 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707SDR FDEA202301140235Crossbeam · damagedAGING AIRCRAFT ASSESSMENT: EXISTING CROSSBEAM REPAIR FOUND ON M/D AT FR 66, BTW Y953 ~ Y1456. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE : STRUCTURES-REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.70SDR FDEA202301130121Dummy Rail · wornI.A.W E6-5310-7-3322E PT1 INSPECTION FOUND FR54/FR54.2 RH NO.4 TRACK GAP WAS 1.02MM. (OVER 1MM BUT LESS 2.15MM) I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 P201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202301130120Dummy Rail · wornI.A.W E6-5310-7-3322E PT1 INSPECTION FOUND FR54/FR54.2 RH NO.3 TRACK GAP WAS 1.02MM. (OVER 1MM BUT LESS 2.15MM) I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 P201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202301130119Dummy Rail · wornI.A.W E6-5310-7-3322E PT1 INSPECTION FOUND FR54/FR54.2 LH NO.4 TRACK GAP WAS 1.06MM. (OVER 1MM BUT LESS 2.15MM) I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 P201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202301130118Dummy Rail · wornI.A.W E6-5310-7-3322E PT1 INSPECTION FOUND FR38.2/FR40 LH NO.4 TRACK GAP WAS 1.09MM. (OVER 1MM BUT LESS 2.15MM) I.A.W A300-600 SRM 53-15-16-201 PARA 5A FIG.201 P201-210 PERFORM REPAIR ACCOMPLISHED.SDR FDEA202301120304Spoiler · delaminated1EA DISBOND AREA WAS FOUND AT RH #5 SPOILER TOP SKIN.(1"X 2.25") ACCOMPLISHED THE HOT BOND REPAIR ON RH #5 SPOILER I.A.W A300-600F SRM 57-72-11-201, PARA.12B&D, PAGE.211-213, FIG.205&206 MAJOR REPAIRSDR FDEA202301120303Spoiler · delaminated1EA DISBOND AREA WAS FOUND AT LH #3 SPOILER TOP SKIN.(1.25" X 1.5") ACCOMPLISHED THE HOT BOND REPAIR ON LH #3 SPOILER I.A.W A300-600F SRM 57-72-11-201, PARA.12B&D, PAGE.211-213, FIG.205&206 MAJOR REPAIRSDR FDEA202204180989None · noneMDIS 656 26-20 4661 18APR22 LBB OPEN U DURING PREFLIGHT, FOUND #2 ENGINE AGENT 1 DISCHARGE LIGHT ON. DURING TROUBLESHOOTING FOUND ONE OF THE PINS ON PRESSURE SWITCH CANNON PLUG NOT FULLY SEATED INTO SDR FDEA202109172337Warning Light · false activationCLIMBING THROUGH 17 000 FT JUMPSEATER CALLED TO NOTIFY R1 DOOR LIGHT AND ALARM ON. PASSING 18000 GOT ECAM NOTIFICATION OF R1 NOT CLOSED. RAN QRH. INITIATED RETURN TO MEM. ON DES. AT 14000 FT ECAM NOTIFICATION WENT AWAY. AND JS NOTIFIED R1 LIGHT AND ALSDR FDEA202103180689Feeder Cable · damagedCLIMBING THROUGH 14,000 SMELLED SMOKE AND SAW SMOKE COMING FROM LOWER RIGHT HAND CORNER OF CAP S AFT AFT LATERAL WINDOW. AFT LATERAL WINDOW VERY HOT TO TOUCH. NO FAULT ON OVHD AND NO ECAM. NO APPLICABLE QRH PROCEDURE. TURNED LEFT LAT WINDOW HEAT OFF AND CONSDR FDEA2020080761777Support Beam · crackedFWD CARGO DOOR ACTUATOR SUPPORT BEAM BETWEEN FR22-FR23 FOUND CRACKS AS MARKED. FWD CARGO DOOR ACTUATOR SUPPORT BEAM BETWEEN FR22-FR23 FOUND CRACKS AS MARKED. REPLACED THE CRACKED DOOR ACTUATOR SUPPORT BEAM ON FWD CARGO BETWEEN FR22-FR23 PER A300-600F SRMSDR FDEA2020080761776Support Beam · crackedAFT CARGO DOOR ACTUATOR SUPPORT BEAM BETWEEN FR61-FR62 FOUND CRACKED. REPLACED THE AFT CARGO DOOR ACTUATOR SUPPORT BEAM IAW SRM 51-40-21. THIS REPAIR CATEGORY IS A. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA202007241638Frame · crackedFRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION INSPECTION, RHS UPPER BOLT HOLE WITH CRACK SIGNAL. INSPECTION COMPLIED WITH IAW EA 6-5710-T0355356 P1. MAJOR REPAIR IAW GMM6-2-100.SDR FDEA202007201585Crossbeam · crackedCROSSBEAM ON NLG FR15A WEB FACE AT ATTACHMENT FITTING OF RACK 107VU FOUND CRACKED. CROSSBEAM ON NLG FR15A WEB FACE AT ATTACHMENT FITTING OF RACK 107VU FOUND CRACK. COMPLY WITH EA:6-5310-T0355184 P1. MAJOR REPAIR IAW GMM6-2-100.SDR FDEA2020080541507Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64 , BETWEEN -Y953 AND -Y1456 REPAIRED MAIN DECK CARGO COMPARTMENT FLOOR CROSSBEAM AT FR64 , BETWEEN -Y953 AND -Y1456. PER A300-600F SRM51-10-15 FIG211.THIS REPAIR WAS CATEGORY CATEGOSDR FDEA2020080514506Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSSBEAM CRACKED, AT FRAME 64, BETWEEN -Y1456 AND -Y1959. REPAIRED MAIN DECK CARGO COMPARTMENT FLOOR CROSSBEAM IAW SRM 53-10-15 FIG211. THIS REPAIR WAS CATEGORY A REPAIR, MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA2020080314507Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOORBEAM CRACKED, AT FRAME 64 , BETWEEN -Y953 AND -Y1456. THE FLOORBEAM WAS REPAIRED IAW SRM 51-40-21, & SRM 53-10-15, FIG 211. CATEGORY A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA2020080314506Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOORBEAM CRACKED, AT FRAME 64, BETWEEN -Y1456 AND -Y1959SDR FDEA201907031476Warning System · false activationPDIS 656 27-50 1775 03JUL19 YOW OPEN U LOGPAGES:2691848 ON 6 MILE FINAL SELECTED FLAPS 20 FOR A FLAP 20 LANDING; GOT ECAM FLAP SYS 1 FAULT WITH SINGLE LITE ON OVHD PANEL (FLAP SYS 1 FAULT). FLAPS INDICATED AT FLAP 20, CYCLED FLAPS WITH NO CHSDR FDEA201902076262Smoke Warning · false activationAFTER DEICE WENT TO START # 2 AND GOT A CARGO SMOKE INDICATION. CREW ELECTED TO CALL AIRPORT FIRE DEPARTMENT TO INSPECT FOR SMOKE. FIRE DEPARTMENT ARRIVED AND INSPECTED ALL CARGO COMPARTMENTS ON AIRCRAFT. NO EVIDENCE OF SMOKE OR FIRE PRESENT. WHEN MX ARRIVSDR FDEA201805301342Rudder · noneREWORK OF N/R# N00817 REQUIRED DUE TO INCORRECT REPAIR BEING ACCOMPLISHED ON RUDDER. ACCOMPLISHED REPAIR ON
RUDDER IAW SRM 55-41-12 PARA 22 FIG 221. RSC TRACKING EA 6- 5540-T0340242 PART 1. STABILIZER - RUDDER - DENT
FOUND ON RUDDER LEFT SKIN - SRM COMPOSITESDR FDEA2018052191264Rib · crackedLEFT CENTER FLAP RIB 19 HAD A CRACK AT THE 6TH FASTENER, FWD OF THE REAR SPAR. REMOVED THE CRACK ON THE RIB, FABRRICATED, AND INSTALLED A RIB REPAIR AND DOUBLER IAW SRM 57-50-00, PARA 4A,E. MAJOR REPAIR.SDR FDEA201805191263Rib · crackedLEFT CENTER FLAP RIB 17 WAS CRACKED AT THE 6TH FASTENER, FWD OF THE REAR SPAR. REMOVED AND REPLACED THE RIB IAW SRM 57-50-00, PARA 4A. MAJOR REPAIR.SDR FDEA2018052191262Rib · crackedLEFT CENTER FLAP RIB 11 HAD A CRACK AT THE 6TH FASTENER FWD OF REAR SPAR. REPAIRED THE RIB IAW SRM 57-50-00, FIG 202. MAJOR REPAIR.SDR FDEA2018052191261Seat Track · wornDURING DUMMY SEAT TRACK INSPECTION EO 6-5310-7-3322, FOUND THE SEAT TRACK AT FR 54.1, Y2462 WORN BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-21, AND SRM 53-15-16. MAJOR REPAIR.SDR FDEA2018052191260Rib · crackedLEFT CENTER FLAP RIB 12 HAS A CRACK AT THE 6TH FASTNER FWD OF REAR SPAR. REPAIRED THE RIB IAW SRM 57-50-00, FIG 201.SDR FDEA2018051651240Floor Panel · brokenMDCC FLOOR PANEL 321BH FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA2018051651241Floor Panel · brokenMDCC FLOOR PANEL 232YG FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201805151234Floor Panel · damagedUPPER MAIN CARGO DECK FLOOR PANEL 242UJ WAS FOUND DAMAGED FROM CARGO LOCKS AT NUMEROUS PLACES. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201805151233Floor Panel · brokenMAIN DECK CARGO FLOOR PANEL 252DH FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201805151232Floor Panel · brokenMAIN DECK CARGO FLOOR PANEL 252UH FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.SDR FDEA201805151231Floor Panel · brokenMAIN DECK CARGO FLOOR PANEL 231AH FOUND BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.
Back to N656FE