N304FE
Service difficulty reports · 283
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 = 'N304FE' 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 = 'N304FE' 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 FDEA2020072381633Seat Track · wornMAIN CARGO DECK AT APPROX BS 750 & LBL 75.25 SEVERAL SEAT TRACK WORN (MARKED) REMOVED AND REPLACED DAMAGED SEAT TRACK REF. SRM 53-70-00 FIGURE 1 VOLUME 1, SRM 51-41-01 VOLUME 2, DWG SR10-53-010 MAJOR REPAIRSDR FDEA2020072381621Seat Track · wornMAIN CARGO DECK AT APPROX STA 1633 & RBL 47, THE SEAT TRACK WAS WORN. INSTALLED A SPLICE SEAT TRACK REPAIR IAW SRM 53-42-01, FIG 4.SDR FDEA2020072371598Spar Cap · crackedR/H HORZ STAB SPAR CAP UPPER AFT BARREL NUT HOLE HAS A .100 IN. CRACK BELOW EXISTING BLEND OUT INSIDE BARREL NUT HOLE. WORK WITH WORK CARD 55X1203ALI-P6. 0000828605 : BATANGAN JR, ROLAND R - 21-JUL-2020 01:53 ACCOMPLISKED BLEND OUT OF CRACK IN R/H AFT BARRESDR FDEA2020012320195Electronic Unit · failedPDIS 304 32-30 6924 22JAN20 MEM OPEN U LOGPAGES:3213484 DURING A BRAKE OVERHEAT ISSUE, THE AIRCRAFT WAS SLOWED BELOW GEAR EXTENDED SPEED, FLOWN TO A LOWER ALTITUDE (FL330). GEAR DROPPED, TEMP COOLED. SUSPECT BAD INDICATION. RAISED GEAR AND RISDR FDEA2019111982988Skin · crackedMDIS 304 55-40 6800 18NOV19 IND OPEN U OPENED WRI TO FILE AN SDR FOR WRI 5540/6798 WHICH WAS WRITTEN FOR TEMP REPAIR ON LWR AFT RUDDER. REF. HANGAR WO # 75844 N/R N00012. COMPLIED WITH EA 8-5540-T0350913A PART 1, THIS IS A MAJOR REPAIR.SDR FDEA2019111972978Skin · crackedMDIS 304 55-40 6797 18NOV19 IND OPEN U COMPLY WITH EA 8-5540-T0350907 PART 1 TO INSTALL A TEMPORARY REPAIR DOUBLER ON THE LWR AFT RUDDER COMPLIED WITH EA 8-5540-T0350907 PART 1, THIS IS A MAJOR REPAIR.SDR FDEA2019080871807Wire · arcedDURING TROUBLESHOOTING REF N/R 8, FOUND WIRE BUNDLE ARCHING, FRAYED AND BURNED (9EA WIRES) LOCATED IN THE FWD E&E COMPARTMENT, LOWER R/H SIDE NEXT TO AFT EQUIPMENT PANEL. DURING INSPECTION OF WIRE HARNESS IDENTIFIED 18 INDIVIDUAL WIRES THAT WERE DAMAGED.SDR FDEA201907081499B-Nut · loosePDIS 304 29-02 6389 08JUL19 PDX FACT U LOGPAGES:2466655 DURING CRUISE FLIGHT, WE GOT A LEVEL ONE ALERT HYD 3 ELEV OFF WITH 4.4 QUANTITY IN HYDRAULIC SYSTEM #3. QUANTITY CONTINUED TO SLOWY DECREASE TO 3.0. DURING APPROACH CONFIQURATION, QUANTIY DROPPSDR FDEA2019060311200Bushing · corrodedRH NLG SIDE LOAD (TRUNNION) FITTING BORE CORRODED ORIGINALLY WRI 32-30-6295 WAS CLASSIFIED AS MINOR. DUE TO EXTENT OF CORROSION AND REPAIR EXCEEDING MD11 SRM DAMAGE ALLOWANCE, THIS REPAIR IS NOW A MAJOR REPAIR. INSTALLED 2(EA.) REPAIR BUSHINGS IN RH NLG TSDR FDEA201905030990Reservoir · low pressureMDIS 304 52-20 6276 02MAY19 MEM FACT U L1 DOOR EMERGENCY DOOR ASSIST AIR RESERVOIR NEEDS TO BE SERVICED. SERVICED L1 DOOR EMERGENCY DOOR ASSIST AIR RESERVOIR REF. AMM 52-10-01.SDR FDEA201903180669Floorbeam · crackedMDIS 304 53-10 6241 17MAR19 MEM OPEN U WHILE REMOVING THE UPPER SECTION OF DAMAGED LT CLG SUPPORT FITTING A CRACK IN THE FLOORBEAM FOUND OF APPROX. 1.5" SHGN 17MAR19 05:46 MEM U FLOORBEAM PART NUMBER IS AEA0031-507. COMPLIED WITH REPAIR OF 1501 FLOOR BSDR FDEA201903150648Bulkhead · damagedMDIS 304 53-40 6239 15MAR19 MEM OPEN U CTR LANDING GEAR FITTING AND BULKHEAD DAMAGED ON UNSAFE GEAR RECYCLE PROCEDURE REF WRI #32-30/6200 FACT 01MAY19 20:27 MEM REPAIR OF STA1521 BULKHEAD DUE TO CENTER LANDING GEAR, CYLINDER SUPPORT BEAM FAILURE. WSDR FDEA201903100580Unknown · malfunctionedAFTER GEAR RETRACTION ON T/O, HAD UNSAFE CENTER GEAR INDICATION SLOWED ACFT TO RECYCLE GEAR, AC LOUD BANG VIBRATION EXTENDED GEAR HAD INDICATION OF #3 HYD SYSTEM FAIL REF WRI 05-25-6221 AND 05-25-6218 FOR LT MLG ASSY REMOVAL AND INSTALLATION AS WELL AS LEFT SISDR FDEA201804060894Frame · crackedUPPER MAIN CABIN COMP LT SIDE WALL FRAME CRACKED AT STA 1741 AT LONGERON 13L. REMOVED AND REPLACED SECTION OF FRAME PER SRM 53-30-00 FIG 5 VOL 1.SDR FDEA201803260783Skin · crackedLOWER FUSELAGE SKIN AT BS 1501 BETWEEN LONGERONS 50 - 51R HAD A 2 INCH CRACK PROPAGATING THROUGH TWO FASTENERS HOLES. REPAIRED IAW EA 8-5330-T0339089.SDR FDEA201803150698Beam · chafedAFT CARGO BAY, AFT LAVATORY VENT PRESSURE REGULATING VALVE, BS 1907 LEFT SIDE OF VALVE WAS WORN INTO THE LEFT SIDEWALL VERTICAL BEAM. REMOVED THE DAMAGED AND INSTALLED A REPAIR IAW SRM 53-00-01, FIG 9, SHT 8, VOL 1.SDR FDEA201802210736Beam · crackedLT I/B WING T/E BEAM ASSY UPPER CAP ARC0292 IS CRACKED AT STA XW146. MRKD FWD OF I/B FLAP ABOVE ARC0295 POST ASSY REF ASSY DWG ARC0291. REPAIRED BEAM PER SRM 57-00-01 FIG11 SH 8 PG40 VOL 1 AND DWG ARC0291. MAJOR REPAIRSDR FDEA201802200443Intercostal · crackedNR 2 PACK DOOR CENTER VERTICAL INTERCOSTAL HAS A 4 IN CRACKED. REMOVED AND REPLACED INTERCOSTAL P/N ACA 3820-15 PER DWG ACA 3820.SDR FDEA201802170566Tee Fitting · crackedRIGHT WING ATTACH TEE BS 1159 AT FRONT SPAR, REPAIR ANGLE CRACKED. REPAIR SRM 57-20-00, FIG 5. REMOVED AND REPLACED DAMAGED REPAIR ANGLE IAW SRM 57-20-00, FIG 6, V1.SDR FDEA201802200354Door Sill · corrodedAFT CARGO COMP DOOR SILL FWD LWR CORNER CORRODED. BLENDED AND REMOVED CORROSION SRM 51-21-01 VOL 2.SDR FDEA201802101561Skin Panel · corrodedMAIN DECK APPROX STA 1370 RBL 102 SMALL AREA OF VISIBLE CORROSION DISCOVERED. REPAIRED REF EA 8-5730-T0338774 P1-P5 WING PLATES & SKINS - CTR WING - UPPER AFT SKIN PANEL AT REA SPAR - CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201802120353Door Sill · corrodedAFT CARGO DOOR SILL, AFT LOWER CORNER CORRODED. REMOVED AND REPLACED THE DOOR SILL IAW DWG NGA 6084.SDR FDEA201802090429Door Sill · corrodedAFT CARGO COMPARTMENT DOOR SILL FWD LOWER CORNER CORRODED. BLENDED AND REMOVED CORROSION IAW 51-21-01 V2.SDR FDEA201802080445Seat Track · corrodedMAIN DECK LOADING SYSTEM AT BS 1970, LBL 75 SEAT TRACK HAS CORROSION. REMOVED & REPLACED THE SEAT TRACK IAW DWG AGA3810, SRM 51-31-01, VOL2, AND SRM 51-25-01, VOL 2, FIG 3, PG 5.SDR FDEA201802080324Skin · crackedFUSELAGE SKIN BS 535 AT UPPER AFT CORNER OF THE NR 3 PACK DOOR CUT OUT, HAS A .600 INCH CRACK PROPAGATING THROUGH FASTENER HOLE. REPAIRED IAW SRM 53-50-00, FIG 3A.SDR FDEA201802080323Web · crackedLT NLG WHEEL WELL WEB HAS A 5.5 IN CRACK FWD OF AN EXISTING REPAIR 12 IN AFT OF BULKHEAD.SDR FDEA201802080322Web · crackedRT NLG WHEEL WELL WEB HAS A 4.0 IN CRACK. 15 IN AFT OF FWD BULKHEAD. REPAIRED PER SRM 53-30-00 FIG 6.SDR FDEA201802071596Doubler · chafedLT WING LEADING EDGE BETWEEN SLAT TRACK 6 AND 7, SMALLER DOUBLER WORN. REPLACED DOUBLER AT LT WING LE BETWEEN SLAT TRACK 6 AND 7 REF SRM 57-10-00 VOL I FIG 40. PAINTED REF SRM 51-21-02 VOL II PGS 1-11 "MAJOR REPAIR"SDR FDEA201802071595Doubler · wornLT WING LEADING EDGE BETWEEN SLAT TRACK 6 AND 7, DOUBLER IS WORN THROUGH IN MIDDLE. REPLACED DOUBLER AT LT WING LE BETWEEN SLAT TRACK 6 AND 7 REF SRM 57-10-00 VOL FIG 40. PAINTED REF SRM 51-21-02 VOL II PGS 1-11 "MAJOR REPAIR".SDR FDEA201802070570Frame · crackedLEFT WING LEADING EDGE SKIN HAS A .500 INCH. THE CRACK AT THE UPPER INBD CORNER OF THE SLAT ANTI-ICE DUCT CUT OUT. REPAIRED IAW SRM 57-10-00, FIG 104, VOL 1.SDR FDEA201802060457Skin · corrodedLEFT WING UPPER SURFACE, XORS 917, AT AFT SPAR HAS CORROSION. BLENDED THE CORROSION IAW SRM 57-10-00, VOL I, FIG 59, TO WITHIN LIMITS.SDR FDEA201802060456Skin · corrodedLEFT WING UPPER SURFACE, XORS 670, STRINGER 9, HAS CORROSION. BLENDED THE CORROSION IAW SRM 57-10-00, VOL I, FIG 59, TO WITHIN LIMITS.SDR FDEA201802060455Skin · corrodedLEFT WING UPPER SURFACE, XORS 433, AT REAR SPAR, HAS CORROSION. BLENDED THE CORROSION IAW SRM 57-10-00, VOL I, FIG 59, TO WITHIN LIMITS.SDR FDEA201802060454Skin · corrodedLEFT WING UPPER SURFACE, XORS 433, STRINGER 10, CORRODED. BLENDED THE CORROSION IAW SRM 57-10-00, VOL I, FIG 59, TO WITHIN LIMITS.SDR FDEA201802060453Skin · corrodedLEFT WING UPPER SURFACE, XORS 415, STRINGER 4, HAS CORROSION. BLENDED THE CORROSION IAW SRM 57-10-00, VOL I, FIG 59, TO WITHIN LIMITS.SDR FDEA201802060452Skin · corrodedLEFT WING UPPER SURFACE, XORS 372, AT REAR SPAR HAS CORROSION. BLENDED THE CORROSION IAW SRM 57-10-00, VOL I, FIG 59, TO WITHIN LIMITS.SDR FDEA201802060451Skin · corrodedLEFT WING UPPER SURFACE, XORS 382, AT REAR SPAR HAS CORROSION. BLENDED THE CORROSION IAW SRM 57-10-00, VOL I, FIG 59, FOUND WITHIN LIMITS.SDR FDEA201802060450Skin · corrodedLEFT WING UPPER SURFACE, XORS 317, STRINGER 10, HAS CORROSION. BLENDED THE CORROSION IAW SRM 57-10-00, VOL I, FIG 59. FOUND WITHIN LIMITS.SDR FDEA201802060449Skin · corrodedLEFT WING UPPER SURFACE, XORS 317, STRINGER 5, HAS CORROSION. BLENDED OUT THE CORROSION IAW SRM 57-10-00, VOL I, FIG 59. FOUND WITHIN LIMITS.SDR FDEA201802060448Skin · corrodedLEFT WING UPPER SURFACE, XORS 274, STRINGER 13 HAS CORROSION. BLENDED CORROSION IAW SRM 57-10-00, VOL I, FIG 59, FOUND WITHIN LIMITS.SDR FDEA201802060447Skin · corrodedLEFT WING UPPER SURFACE, XORS 299 BETWEEN STRINGERS 12 - 13L HAS CORROSION. BLENDED CORROSION IAW SRM 57-10-00, VOL I, FIG 59. WITHIN LIMITS.SDR FDEA201802060446Skin · corrodedLT WING UPPER SURFACE XORS 321, STRINGER 10L HAS CORROSION. BLENDED THE CORROSION IAW SRM 57-10-00, VOL I, FIG 59, WITHIN LIMITS.SDR FDEA201706081593Solenoid · faultedAFTER DISARMING THE L1 DOOR, THE DOOR COULD NOT BE OPENED WITH ELECTRIC POWER SWITCH. ON BLOCK, ATTEMPTED TO OPEN L1 DOOR. DOOR SOLENOID WOULD CLICK BUT WOULD NOT ACTUATE USING EITHER SWITCH. TAPPED ON DOOR SOLENOID AND DOOR STARTED WORKING. SUSPECT FAULTYSDR FDEA201706071591Solenoid · wornAFTER DISARMING L1 DOOR, THE DOOR COULD NOT BE OPENED WITH ELECTRIC POWER SWITCH. REMOVED AND REPLACED THE SOLENOID IAW AMM 52-11-13-2. OPERATED THE DOOR 12 TIMES, NO PROBLEMS NOTED IAW AMM 52-11-00-6, PARA B , 15SDR FDEA201705121400Connector · looseL1 DOOR WILL NOT RAISE ELECTRICALLY. RELAY CLICKS ONLY. WHILE TRYING TO OPEN L1 DOOR NOTED LOCKING SOLENOID NOT MOVING FULL TRAVEL, COULD ACTUATE SOLENOID LINK ARM BY HAND AND DOOR WOULD OPEN NORMALLY, FOUND WIRE CONNECTOR LOOSE. TIGHTENED THE CONNECTOR, SDR FDEA201703251064Rib · gougedRIB P/N ARB2927-9 IS GOUGED IN SEVERAL AREAS BY FASTENER HOLES. REPLACED RIB REF SRM 51-35-01 AND EA 8-5710-T0332275 PART 1.SDR FDEA201612074349Warning System · activatedAFTER PUSHBACK WITH ALL THREE ENGINES RUNNING WE COMPLETED ALL APPROPRIATE CHECKLISTS FOR MULTIPLE MEL'S. THE NR 3 AIR SYSTEM SHOWS AN AMBER BOXED PRESSURE WITH A LVL 2 ALERT "AIR SYS 3 PRES LO" BLD 3 OFF / 1-3 ISOL VLV ON / PACK 3 OFF.SDR FDEA201610213675Spoiler · lack of lubeDURING DESCENT, EXTENDED SPEED BRAKE TO 1/3, AIRPLANE ROLLED 1 DEGREE RIGHT. AT 2/3 DETENT AIRPLANE ROLLED AIRPLANE ROLLED 7 DEGREES RIGHT. FULL SPEED BRAKE ROLLED 14 DEGREES RIGHT. LUBRICATED THE SPOILERS IAW AMM 12-21-04-3, AND AMM 27-60-00-2. SPOILERS SDR FDEA201606212100Msc · failedDURING PREFLIGHT RECEIVED A CARGO FIRE LOWER FWD 1 ALERT. FORWARD CARGO WAS CLOSED. COMPLIED WITH QRH. INSTALLED AGENT 1 LOWER CARGO COMPARTMENT FIRE EXTINGUISHER CONTAINER'S FWD AND AFT DISCHARGE HEADS AND DISCHARGE CARTRIDGES IN REF TO AMM 26-22-01-4. R&SDR FDEA201606152015Hydraulic Line · looseHYD "3" LEAK DURING CRUISE WITH LEVEL 1, HYD 3, QTY LO, ALERT. LEAK CONTINUED INTO, HYD 3 FAIL, ALERT. NEVER BELOW 2.4 GALS ON NR 3. NO OVERHEAT OR OTHER ALERTS. USED MAIN GEAR ALTERNATE EXTENSION. THE ALTERNATE GEAR EXTENTION PART OF THIS WRI HAS BEEN MOV
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