N937FD
Service difficulty reports · 178
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 = 'N937FD' 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 = 'N937FD' 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 FDEA202003120556Placard · out of positionFLIGHT CREW REPORTED R1 DOOR SLIDE ARM/DISARM INDICATOR PLACARD BEHIND ARMING LEVER IS LOOSE, NOT ATTACHED TO DOOR INTERIOR UPPER PANEL. RE-ATTACHED R-1 DOOR SLIDE AR/ DISARM INDICATOR PLACARD, REF AMM 20-30-01-2 20-30-01-2, THIS CLEARS C/7219856 OK FOSDR FDEA2020030970499Collar · brokenMDIS 937 52-10 9279 07MAR20 MEM OPEN U LOGPAGES:2327590 ON PRE FLIGHT, DISCOVERED BROKEN GUST LOCK BY HUB ON L1 DOOR. L1 DOOR WOULD NOT CLOSE. MEL 07MAR20 09:41 MEM U RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 10SDR FDEA202001300248Lamp · inoperativeDURING POST FLIGHT INSPECTION FOUND R/H EXTERIOR EMERGENCY LIGHT AFT OF R1 DOOR INOP. RELAMPED EXTERIOR RH EMERGECY LIGHT REF AMM 33-51-06-2-1. A/C OK FOR SERVICESDR FDEA201907231672Rvdt · out of adjustAIRCRAFT ROLLS RIGHT AT LIFTOFF. AIRCRAFT ROLLS 1 UNIT LEFT DURING FLIGHT WHEN THE FLIGHT SPOILERS ARE DEPLOYED. TROUBLESHOT PER FRMFIM 27-61 FAULT TREE 804, STEP 1 CLEARANCE CHECKS CHECKED NORMAL. STEP 2 FOUND #7 SPOILER PCA RVDT OUT OF TOLERANCE. ADJUSTSDR FDEA201903090565Guide Arm · out of positionUNABLE TO CLOSE L1 DOOR. FOUND GUIDE ARM CAM FOLLOWER PINS OUT OF TRACK AND BOLTS BACKED OUT OF SUPPORT BRACKET AT SERRATED PLATE. REINSTALLED GUIDE ARM PER AMM 52-11-04-2.SDR FDEA201811143213Warning System · false activationTE FLAP DISAGREE EICAS MSG. CYCLED FLAPS 3 TIMES, NO FAULTS AND ALL INDICATIONS NORMAL PER FIM 27-51 FAULT TREE 803. ALSO REVIEWED TECH TIP 18-0042. OPS CK NORMAL, A/C OK FOR SERVICE.SDR FDEA201809052351Detector · inoperativeWHILE PRE FLIGHTING AIRCRAFT WITH APU RUNNING AND PACKS ON, RECEIVED WHEEL WELL FIRE WARNING. AIRCRAFT WAS EVACUATED AND FIRE TRUCKS CALLED. NO APU AIR DUCT LEAKS NOTED REF WDM 26-17-11, FOUND RIGHT WHEEL WELL DETECTOR ELEM T205 WITH LOW RESISTANCE FROM THE CESDR FDEA201804050857Coupling · leakingABOUT 25 MINUTES INTO FLIGHT, RECEIVED A RT ENGINE OVERHEAT EICAS MESSAGE & RT ENGINE OVERHEAT LIGHT. COMPLIED WITH QRH AND LIGHT WENT OUT AFTER ABOUT 3 MINUTES WITH RIGHT THRUST LEVER AT IDLE. ALL ENGINE INSTRUMENT INDICATIONS WERE NORMAL. LANDED WITH RSDR FDEA201803220754Detector · malfunctionedFL380/.80 MACH RT ENGINE OVERHEAT. RAN QRH REDUCED RT THRUST LEVER TO IDLE OPERATED REMAINDER OF FLIGHT WITH REDUCED THRUST ON R ENGINE (BELOW1.3 EPR). REMOVED AND REPLACED RIGHT ENGINE NACELLE OVERHEAT DETECTORS TS5074 AND TS5073 IAW AMM 26-11-01-4. RAN THESDR FDEA201802130380Fitting · crackedMAIN CABIN BELOW FLOOR, SEEN FROM FWD CARGO BAY. FLOOR BEAM STUB FITTING CRACKED, AFT FLANGE BS 580, LBL 45. COMPLIED WITH EA F-5310-T0338208, P1.SDR FDEA201802200380Fitting · crackedMAIN CABIN BELOW FLOOR SEEN FROM FWD CARGO COMPT FLOORBEAM STUB FITTING CRACKED AFT FLANGE STA 580 LBL.45. COMPLIED WITH EA F-5310-T0338208 P1. FUSELAGE MAINFRAME STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.SDR FDEA201709222676Gust Lock · crackedL1 DOOR GUST LOCK COLLAR BROKEN. R & R THE L1DOOR HOLD OPEN LOCK COLLAR IAW MM 52-11-08-8.SDR FDEA201706201714Power Supply · inoperativeL1 DOOR INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY M731 AND BATTERY PACK IAW AMM 33-51-07-2. OPS CHECKED GOOD. OK FOR SERVICE.SDR FDEA201611083902Pan · gougedL1 DOOR PAN GOUGED AT AFT LWR RADIUS. REMOVED AND REPLACED GOUGED DOOR PAN IAW SRM 51-40-02, AND DRAWING 141N6100.SDR FDEA201607132383Window · failedRIGHT FORWARD WINDOW SHATTERED IN FLIGHT. NO AIR LEAK, NO INNER PANE DEFORMATION, RT WINDOW R1 WAS REMOVED USING AMM 56-11-01-4.
INSTALLED R1 WINDOW AND TORQUED IAW AMM 56-11-01-4. AVIONICS INSTALLING INNER WINDOW TRIM, WIRING AND COMPLETING OPS CHECKS.SDR FDEA201604191258Proximity Switch · failedR1 ENTRY DOOR SLIDE ARMED LIGHT DOES NOT ILLUMINATE WHEN MOVING HANDLE TO ACTIVATE. R & R R1 DOOR FWD GIRT BAR PROXIMITY SWITCH S10216 IAW AMM 25-66-11-2. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVICE.SDR FDEA201604151225Hinge · brokenRAMP WAS DOING TRAINING ON JET & REPORTED L1 DOOR SLIDE COVER CAME LOOSE. ON INSPECTION FOUND TOP FWD HINGE OF COVER IS BROKEN. PLACED COVER ON ORDER. ITEM WILL REQUIRE COMPOSITE REPAIR IAW WRI 25-60 5905. COMPLIED WITH EA F-2560-T0324743 PT 1 SLIDE COVER SDR FDEA201604131196Girt Bar · dirtyRIGHT FWD ENTRY DOOR SLIDE ARM & DISARM LEVER REQUIRES NUMEROUS ATTEMPTS TO ARM DOOR, IN ORDER TO ACTIVATE SLIDE ARM LIGHT. OLD DISCREPANCY 937 25-60 0005899. CLEANED AND LUBED R1 GIRT BAR AND FLOOR FITTINGS PER AMM 25-66-01-4. CHECKED OPERATION OF ARMING ASDR FDEA201508042459Proximity Sensor · obstructedWITH R1 DOOR CLOSED & ARMED SLIDE ARM, LIGHT ABOVE DOOR WILL NOT ILLUMINATE. INSPECTED R1 DOOR GIRT BAR PROX SENSOR & TARGET FOUND DEBRI & SEALANT, GREASE STUCK BETWEEN BOTH THE SENSORS & TARGETS WITH DOOR CLOSED & ARMED. CLEANED BOTH SIDES GIRT BARS & SENSOSDR FDEA201507292437Proximity Sensor · obstructedR1 DOOR IS NOT ARMING WHILE FULLY CLOSED. TROUBLE SHOT IAW FIM 25-66-00 FAULT TREE 802. FOUND BOTH GIRT BAR PROX SENSORS COVERED IN GREASE. CLEANED SENSOR, NO HELP. SUSPECT ONE OF THE PROX SENSORS BAD. OPERATED R1 DOOR, SEVERAL ARMING & DISARM CYCLES. OPSDR FDEA201507232346Proximity Sensor · dirtyR1 DOOR IS NOT ARMING WHILE FULLY CLOSED. CLEANED GIRT BAR PROXIMITY SENSORS.SDR FDEA201501130158Indicator · poppedON FINAL PLACED FLAPS FROM 15 DEGREES TO 20 DEGREES. RECEIVED TE FLAP DISAGREE EICAS. THE FLAP HANDLE WAS IN 20 DEGREE DETENT WITH 17.5 APPROX FLAPS INDICATED ON FLAP INDICATOR. COMPLETED QRH PROCEDURE & LANDED FLAPS 20 VREF 20. TROUBLE SHOT IAW FIM 27-51SDR FDEA201410193301Slide · unsecureUPON OPENING RT FWD ENTRY WITH DOOR DISARMED THE ESCAPE SLIDE FELL OUT OF COMPARTMENT ONTO STAIR SURFACE. R & R R1 DOOR ESCAPE SLIDE IAW MM 25-66-01-4. ALSO SERVICED PAX DOOR EMER POWER RESERVOIR IAW MM 12-15-10-3.SDR FDEA201406121458Coupling · lack of lubeRECEIVED TE DISAGREE DURING APPROACH TO LANDING. CONFIGURATION STOPPED AROUND 17 - 18 DEGREES. TROUBLE SHOT FLAP DISAGREE IAW FIM WITH NO MSG ON EICAS OR FSEU. GREASED TORQUE TUBE COUPLINGS & LIMITERS IAW AMM. PERFORMED OPERATIONS CHECK OF FLAPS IAW AMM WISDR FDEA201311012666Fuel Sys · faultedDURING BLOCKOUT, FUEL ONBOARD WAS EQUAL AT 10,000 LBS, EACH MAIN TANK AND CENTER TANK 300 LBS. CLIMBING OUT AN IMBALANCE APPEARED TO HAVE DEVELOPED AND REACHED 2500LBS. WHERE LT MAIN TANK BEING THE LOWER OF BOTH MAINS. ATTEMPTED TO UTILIZE QRH FUEL BALANCISDR FDEA201308222008Slide · dislodgedAFTER BLOCK-IN , WITH BOTH L1 AND R1 DOORS DISARMED AND L1 DOOR CRACKED, THE L1 DOOR SLIDE FELL OUT ON TO THE CREW STAIRS, BUT DID NOT DEPLOY. MX DISCONNECTED GIRT BAR FROM ACFT, L1 DOOR WAS IN ARMED POSITION AND FULLY OPEN, SLIDE HAD PINS PULLED ON YELLOW COSDR FDEA201308171925Lamp · burned outLEFT FWD ENTRY DOOR SLIDE LIGHT INOPERATIVE. REPLACED LAMPS, OP CHECKED GOOD.SDR FDEA201206152249Warning Light · false activationREJECTED TAKEOFF AT 110 KIAS, DUE TO A RED MASTER WARNING LIGHT. NO EICAS, STATUS, OR ENGINE EXCEEDANCES OBSERVED. COMPLIED WITH QRH BRAKE COOLING CHART AND COORDINATED WITH GOC AND MOCC FOR ANOTHER TAKEOFF. NO ISSUES ON SUBSEQUENT TAKEOFF ATTEMPT. SUSPECT TSDR FDEA201201170210Reservoir · unwanted deployWHEN ACFT BLOCKED IN THE CREW PARTIALLY OPEN LT PASSENGER DOOR. AFTER CREW STAIRS WERE PLACED IN POSITION THE HUB FINISHED OPENING THE DOOR. WHILE THE DOOR WAS BEING OPEN THE DOOR ASSIST BOTTLE BLEW. REMOVED AND REPLACED L1 DOOR EMERGENCY POWER RESERVOSDR FDEA201110074373Light · intermittentON APPROACH, NOSE GEAR DOWN LIGHT DID NOT ILLUMINATE AFTER LOWERING LANDING GEAR. NOSE GEAR LIGHT WOULD NOT TEST, REPLACED LIGHT BULBS STILL NO TEST. PERFORMED GEAR DISAGREE CHECKLIST IN QRH. NOSE GEAR LIGHT STILL INOP. HAD TOWER VISUALLY CHECK NOSE GEAR DOWNSDR FDEA201011044255Blades · damagedON TAKEOFF LT ENG COMPRESSOR STALL. ABORTED TAKEOFF AT 20 KNOTS, PERFORMED VISUAL INSPECTING OF INTAKE & EXHAUST. NO DEFECTS NOTED. THERE WAS A "L ENG SURGE BITE" ON THE MX PAGE. BITE CHECK OF BVCU SHOWED F0 04 F1 & F2 TPU SHOWED. PERFORMED BORESCOPE INSDR FDEA201008153003Module · inoperativeBRAKES ARE VERY TOUCHY. BREAKS GRAB GO FROM NON RESPONSIVE TO OVERLY RESPONSIVE. HOOKED UP BRAKE BLEEDER CART TO CK INDIVIDUAL BRAKE PRESSURES. NR4 BRAKE SHOWED ONLY 1200PSI WHEN BRAKES WERE APPLIED. ALL OTHER BRAKE PRESSURES OK FOR LT & RT GEARS. IAW MSDR FDEA201006302231Panel · corrodedRT OVERWING FILL PORT ADAPTER CUT OUT FOUND WITH LIGHT CORROSION. AFTER CLEANING, RT OVERWING FILL PORT ADAPTER CUT OUT CORROSION REPAIRED IAW EA NR F-5730-135853, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201006302230Frame · gougedCABIN FUSELAGE INTERIOR FRAME WITH EXISTING REPAIR DOUBLER AT BS 1280, BETWEEN STRINGERS S-11L TO S-13L. EVALUATE AND RECTIFY. EXISTING REPAIR EVALUATED IAW ATTACHMENT B OF EO F-5100-7-5001 PT. 1 AND FOUND WITH DEEP GOUGES, R & R REPAIR ON FRAME IAW SRM 53-0SDR FDEA201006302229Floorbeam · corrodedCABIN FUSELAGE INTERIOR FLOORBEAM WITH EXISTING REPAIR DOUBLER AT BS 365, BETWEEN BL 0 TO RBL 65. EVALUATED IAW ATTACHMENT B OF EO F-5100-7-5001 PT 1 AND FOUND WITH CORRODED. R & R IAW STA ENGINEERING EA NR 757-5315-08-E0691 REV A WITH EA NR F-5310-13584SDR FDEA201006302228Skin · damagedNR 2 NACELLE STRUT AFT FAIRING LOWER SEGMENT SKIN JUST AFT OF PP STA 276.93 WITH SEVERAL LOOSE FASTENERS. UPON EVALUATION FOUND HOLES ELONGATED TO REPLACE SKIN. AFT FAIRING LOWER SEGMENT JUST AFT OF PPSTA 276.93, NR 2 ENG NACELLE STRUT, AFT FAIRING SKIN ANDSDR FDEA201006152015Retainer · corrodedFWD CARGO COMPARTMENT, CARGO DOOR SURROUND STRUCTURE LOWER SILL SCUFF PLATE RETAINER PLATE AT STA 560 TO STA 620 FOUND WITH CORROSION. EVALUATE AND RECTIFY. FWD CARGO DOOR SURROUND STRUCTURE LOWER SILL SCUFF PLATE CORRODED. RETAINER PLATE REMOVED FROM STASDR FDEA201006111954Skin · corrodedCABIN: R4 DOOR INTERIOR DOOR SURFACE SKIN HAS CORROSION BELOW PRISMATIC WINDOW. EVALUATE AND RECTIFY. R4 DOOR INTERIOR SKIN BELOW PRISMATIC WINDOW CORROSION REPAIRED EA F-5210-135867, THIS REPAIR IS CLASSIFIED AS MINOR REPAIR IAW GMM 6-2-100 CRITERIA.SDR FDEA201006111953Frame · misinstalledFUSELAGE INTERIOR FRAME WITH EXISTING REPAIR DOUBLER AT RT STA 1460, BETWEEN STRINGERS S-17R TO S-18R, BETWEEN CREASE BEAM AND FRAME. EXISTING REPAIR EVALUATED IAW ATTACHMENT B OF E.O. F-5100-7-5001 PT 1 AND FOUND REPAIR INTERFERED WITH PTF MOD PART INSTALLASDR FDEA201006101920Skin · misrepairedFUSELAGE EXTERIOR SKIN WITH EXISTING REPAIR DOUBLER AT STA 760 TO STA 780, BETWEEN STRINGERS S-15L TO S-17L. EXISTING REPAIR EVALUATED IAW ATTACHMENT "B" OF EO F-5100-7-5001 PT 1 AND FOUND REPAIR CAN NOT MEET THE CURRENT SRM REPAIR. EXISTING REPAIR DOUBLER RSDR FDEA201006101928Access Panel · corrodedRT WING FUEL TANK ACCESS PANEL NR 642BB, CORROSION FOUND IN THE LOWER SURFACE AND ITS SIDE. BLEND AND CHECK LIMITS. RT WING FUEL TANK ACCESS PANEL NR 642BB REPAIRED IAW E.A. NR F-2810-135858-FUEL SYS-TANKS-RT WING LOWER SURFACE FUEL TANK ACCESS COVER CORROSDR FDEA201006101927Access Panel · corrodedRT WING FUEL TANK ACCESS PANEL NR 641MB, CORROSION FOUND IN THE LOWER SURFACE AND ITS SIDE. BLEND AND CHECK LIMIT. RT WING FUEL TANK ACCESS PANEL NR 641MB REPAIRED IAW E.A. NR F-2810-135858. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201006101926Access Panel · corrodedRT WING FUEL TANK ACCESS PANEL NR 641JB, CORROSION FOUND IN THE LOWER SURFACE AND ITS SIDE. BLEND AND CHECK LIMITS. RT WING FUEL TANK ACCESS PANEL NR 641JB REPAIRED IAW E.A. NR F-2810-135858. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201006101925Access Panel · corrodedRT WING FUEL TANK ACCESS PANELS NR 643AB, CORROSION FOUND IN THE LOWER SURFACE AND ITS SIDE. BLEND AND CHECK LIMITS. RT WING FUEL TANK ACCESS PANEL NR 643AB REPAIRED IAW E.A. F-2810-135858. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201006101924Access Panel · corrodedRT WING FUEL TANK ACCESS PANEL NR 641FB, CORROSION FOUND IN THE LOWER SURFACE AND ITS SIDE. BLEND AND CHECK THE LIMITS. RT WING FUEL TANK ACCESS PANEL NR 641FB REPAIRED IAW E.A. NR F-2810-135858. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201006101923Access Panel · corrodedRT WING FUEL TANK ACCESS PANEL NR 641GB, CORROSION FOUND IN THE LOWER SURFACE AND ITS SIDE. BLEND AND CHECK THE LIMITS. RT WING FUEL TANK ACCESS PANEL NR 641GB REPAIRED IAW E.A. F-2810-135858. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.SDR FDEA201006101922Access Panel · corrodedRT WING FUEL TANK ACCESS PANEL NR 642AB, CORROSION FOUND IN LOWER SURFACE OF THE PANEL. BLEND AND CHECK THE LIMIT. RT WING FUEL TANK ACCESS PANEL NR 642AB REPAIRED IAW EA NR F-2810-135858-FUEL SYS-TANKS-RT WING LOWER SURFACE FUEL TANK ACCESS COVER CORROSION SDR FDEA201006101921Access Panel · corrodedRIGHT WING FUEL TANK ACCESS PANEL NR 641LB, CORROSION FOUND IN THE LOWER SURFACE AREA. BLEND AND CHECK LIMIT. RT WING FUEL TANK ACCESS PANEL NO. 641LB REPAIRED IAW EA NR F-2810-135858-FUEL SYS-TANKS-RT WING LOWER SURFACE FUEL TANK ACCESS COVER CORROSION DAMSDR FDEA201006071854Access Panel · corrodedLT WING FUEL TANK ACCESS PANEL NR 541GB, CORROSION FOUND IN THE LOWER SURFACE AND ITS SIDE. CORROSION ON PANEL NR 541GB REPAIRED IAW EA NR F-2810-135857. (LT WING LOWER SURFACE FUEL TANK ACCESS COVER CORROSION DAMAGE REWORK.) REPAIR IS CLASSIFIED AS MAJOR ISDR FDEA201006071853Access Panel · corrodedLT WING FUEL TANK ACCESS PANEL NR 541DB, CORROSION FOUND IN THE AREA BETWEEN MOUNTING HOLE AND SEAL GROOVE LOCATIONS AND ALSO IN THE LOWER SIDE OF THE PANEL. CORROSION REPAIR CARRIED OUT ON PANEL NR 541DB IAW EA F-2810-135857. (LT WING LOWER SURFACE FUEL TANK
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