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.

SDR FDEA201603301121Skin · crackedNEED ALL HOLES INSPECTED WITH NDT COMMON TO CAC RT STATION 1156. PRESS BULKHEAD T CAP AREA, CRACKED T CAP IS REMOVED. ACCOMPLISHED HFEC OF ALL HOLES IAW NDT3PM PART 06. CRACKS FOUND ON SKIN AT LONGERON 37R & 39R. REPAIRED IAW EA 8-5310-T0323753.Mar 30, 2016 · N304FE · Doug MD1030F · Fuselage Main, Plate/SkinSDR FDEA201603170940Doubler · crackedRIGHT WING LE OTB OF SLAT TRACK NR 10, APPROX XORS 570, INTERNAL LE PILLOW DOUBLER HAS CRACKS. REPAIRED DOUBLER AT RT WING LE OTB OF SLAT TRACK NR 10 IAW SRM 57-10-00 FIG 71.Mar 17, 2016 · N304FE · Doug MD1030F · Leading Edge DevicesSDR FDEA201603160936Skin · crackedMAIN CARGO DOOR, AFT JAMB LOWER EDGE CRACKED, APPEARS TO BE THE EXTERNAL SKIN. PREVIOUS REPAIR COMPLIED WITH IAW SEQ 248, EA 8-5330-T0351847 P2. MARKED LIGHTLY BLENDED NOTED SCRATCH & CRACKED AREA, REPAIRED IAW EA 8-5330-T0323830.Mar 16, 2016 · N304FE · Doug MD1030F · Fuselage Main, Plate/SkinSDR FDEA201603160935Seat Track · damagedMAIN CARGO COMPARTMENT, APPROX STATION 735, THIRD LT SEAT TRACK DAMAGED. REPAIRED DAMAGED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1.Mar 16, 2016 · N304FE · Doug MD1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201603160932Web · corrodedRUST & CORROSION UNDER PANEL 487HR & GR, NR 3 ENG OTBD SIDE OF PYLON, AFT OF EXHAUST, TOP EDGE OF PYLON NEAR WING. CORROSION REMOVED IAW SRM 51-21-01 VOL 2 & EA 8-5450-T0323721 PART 1 UPPER WEB REPLACED WITH NEW WEB, PN AUB7366-501.Mar 16, 2016 · N304FE · Doug MD1030F · Nacelle/Pylon Miscellaneous StructureSDR FDEA201603100892Floor Panel · delaminatedMAIN DECK, STATION 1661 - 1741, RBL 38. R & R FLOOR PANEL 282CF.Mar 10, 2016 · N304FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA201603100891Floor Panel · delaminatedMAIN DECK, STATION 1561 - 1661, RBL 38 IS DELAMINATED. R & R FLOOR PANEL 282AF.Mar 10, 2016 · N304FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA201603010747Skin · crackedBS 1156, LOWER FUSELAGE SKIN, LONGERONS 37 - 39R, SHOWS THREE EACH CRACKS, TWO CRACKS AT LONGERON 37R & ONE CRACK AT LONGERON 39R IN SKIN. TRIMMED OUT TWO EACH CRACKS, FABRICATED TWO EACH FILLERS & INSTALLED TWO STRAPS & TWO DOUBLERS WITH FASTENERS AS REQUIMar 1, 2016 · N304FE · Doug MD1030F · Fuselage Main, Plate/SkinSDR FDEA201603010746Tee Fitting · crackedRIGHT BS 1156, PRESS BULKHEAD TEE CAP FWD FLANGE HAS A 1.5 INCH CRACK JUST ABOVE SPLICE PLATE AT LONGERON 37R. THE CRACK PROPAGATED THROUGH THE RADIUS VERTICALLY & EXTENDING BEHIND THE BULKHEAD STIFFENER AT X=88.270. REMOVED FASTENERS, CUT & REMOVED SECTION Mar 1, 2016 · N304FE · Doug MD1030F · Fuselage Main, BulkheadSDR FDEA201602270700Web · crackedNR 3 ENG PYLON, UPPER SPAR WEB, RT SIDE AT F HOLE HAS INDICATION UNDER STIFFENER. OLD WEB WAS R & R BECAUSE OF EXCESSIVE CRACKS FOUND ON THE BOTTOM SIDE OF WEB.Feb 27, 2016 · N304FE · Doug MD1030F · Nacelle/Pylon, Main FrameSDR FDEA201602250688Cargo Track · wornMAIN CARGO COMPARTMENT, APPROX BS 735 THIRD LT CARGO TRACK DAMAGED. REPAIRED THE CARGO TRACK IAW SRM 53-70-00 FIG 1.Feb 25, 2016 · N304FE · Doug MD1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201602230677Floorboard · delaminatedMAIN CABIN, FLOORBOARD AT STATION 1915, RBL 42 HAS DELAMINATION, SHOWING DETERIORATION. R & R FLOORBOARD IAW TO0 SRZ-25-005.Feb 23, 2016 · N304FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA201602200666Doubler · crackedRIGHT WING, LE OTBD OF SLAT 10, APPROX XORS 568, INTERNAL LE FLAT DOUBLER HAS APPROX 7 INCH CRACK, 2 INCHES INBD OF PILLOW CRACK. R & R INTERNAL FLAT DOUBLER IAW DWG ARB 3954.Feb 20, 2016 · N304FE · Doug MD1030F · Wing Miscellaneous StructureSDR FDEA201602200664Seat Track · damagedMAIN DECK, SEAT TRACK DAMAGED AT STATION 1821, RBL 48. R & R SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1A PAGE 7.Feb 20, 2016 · N304FE · Doug MD1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201602200662Floorboard · delaminatedMAIN CARGO, FLOORBOARD AT STATION 1821, RBL 38 HAS DELAMINATION & MISSING INSERTS. FABRICATED NEW FLOORBOARD IAW SRZ-25-005.Feb 20, 2016 · N304FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA201602190639Floorboard · delaminatedMAIN CARGO DOORWAY, FLOORBOARD AT STATION 595, LBL 91 IS DETERIORATED, DELAMINATED & HAS MISSING OR BROKEN INSERTS. FABRICATED A NEW FLOORBOARD IAW SRZ-25-005.Feb 19, 2016 · N304FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA201602180626Seat Track · damagedMAIN DECK, SEAT TRACK DAMAGED, STATION 1521, LBL 48. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1 SHT 2.Feb 18, 2016 · N304FE · Doug MD1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201602180625Floorboard · delaminatedMAIN CARGO FLOORBOARD AT STATION 1741, RBL 38 HAS DELAMINATION & MISSING INSERTS. FABRICATED NEW FLOORBOARD IAW SRZ-25-005.Feb 18, 2016 · N304FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA201602180624Seat Track · damagedMAIN DECK, SEAT TRACK DAMAGED AT STATION 1526, LBL 24. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1A.Feb 18, 2016 · N304FE · Doug MD1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201602180623Seat Track · damagedMAIN DECK, SEAT TRACK DAMAGED, STATION 1511, RBL 48. R & R SECTION OF SEAT TRACK AT STATION 1511 AS REQUIRED.Feb 18, 2016 · N304FE · Doug MD1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201602180622Seat Track · damagedMAIN DECK, SEAT TRACK DAMAGED, STATION 1519, RBL 48. R & R DAMAGED SECTION OF SEAT TRACK AT STATION 1519, RBL 48 & DOCUMENTED ON SNRM 574.Feb 18, 2016 · N304FE · Doug MD1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201602170613Floorboard · delaminatedMAIN CARGO FLOORBOARD AT STATION 1821, RBL 38, PANEL DAMAGED. FABRICATED NEW FLOORBOARD IAW DWG SRZ-25-005.Feb 17, 2016 · N304FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA201602170611Skin · dentedLEFT INBD ELEVATOR, UPPER SURFACE HAS A DENT. REPAIRED DENT LOCATED ON INBD ELEVATOR UPPER SURFACE IAW SRM 55-00-01 VOL 1 FIG 3 SHEET 2.Feb 17, 2016 · N304FE · Doug MD1030F · Elevator, Plate/SkinSDR FDEA201602170610Floorboard · damagedMAIN CARGO FLOORBOARD, STATION 1481, LBL 38, DAMAGED. FABRICATED NEW FLOORBOARD IAW SRM 53-60-00 VOL 1 & DWG SRZ 25-005.Feb 17, 2016 · N304FE · Doug MD1030F · Fuselage Floor PanelSDR FDEA201602110602Seat Track · crackedMAIN DECK FROM STATION 1199 - 1219, RBL 48, SEAT TRACK WORN. REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1 SHT 2.Feb 11, 2016 · N304FE · Doug MD1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201512304103Engine · malfunctioned1:30 INTO A 3:30 FLIGHT, NR 1 OIL QTY READ 0. IAW QRH MONITORED TEMP & PRESS FOR THE NEXT 15 MINS, TEMP REMAINED NORMAL, BUT PRESS DROPPED TO 21 WITH AMBER BOX. IAW QRH SHUT THE ENG DOWN USING ENG SHUT DOWN INFLIGHT. COORDINATED & DIVERTED UNEVENTFULLY. R &Dec 30, 2015 · N304FE · Doug MD1030F · Engine Oil Indicating SystemSDR FDEA201508262700Connector · defectiveINTERMITTENT LEVEL 2, ENG 1 LOOP A, ALERT DURING FLIGHT. ALERT HAPPENED AT ALL FLIGHT LEVELS & WOULD LAST APPROX 15 SECONDS. IAW WMD 26-11-01 R & R MOD BLOCK S3-529 16BA BX. IAW WDM 26-11-01 02 03 & THE HOOKUP CHART R & R CONNECTOR P1-9952.Aug 26, 2015 · N304FE · Doug MD1030F · Fire Protection System WiringSDR FDEA201508262699Connector · defectiveINTERMITTENT LEVEL 2, ENG 3 LOOP AN ALERT DURING FLIGHT. REPEAT WRITE UP. ALERT HAPPENED AT ALL FLIGHT LEVELS & WOULD LAST ABOUT 15 SECONDS, DID NOT ALERT AT THE SAME TIME AS THE NR 1. IAW WMD 26-11-01 R & R MOD BLOCK S3-529 16BA BX. IAW WDM 26-11-01 02 03Aug 26, 2015 · N304FE · Doug MD1030F · Fire Protection System WiringSDR FDEA201508212680Smoke Detector · malfunctionedAFTER CLEARING RUNWAY, WITH ENG 1 & 2 RUNNING, GOT INTERMITTENT CABIN SMOKE INDICATION WITH ONE SENSOR INDICATING ON AIR SYNOPTIC PAGE. SHUTDOWN ENGS & EVACUATED ACFT THRU L1 SLIDE. REMOVED 2R SMOKE DETECTOR & REPLACED IAW AMM 26-15-01-4. TESTED GOOD IAW AAug 21, 2015 · N304FE · Doug MD1030F · Smoke DetectionSDR FDEA201508212679Control Unit · malfunctionedAT FL 350 GOT INTERMITTENT, THEN STEADY NR 3 ENG FIRE INDICATION. ACCOMPLISHED QRH & FIRED BOTTLE. NO VIBRATION NOTED DURING WINDMILLING. R & R FIRE DETECTOR CONTROL UNIT IAW AMM 26-11-01-4.Aug 21, 2015 · N304FE · Doug MD1030F · Fire DetectionSDR FDEA201508212678Fire Loop · out of positionDURING EMERGENCY DESCENT WITH NR 3 ENGINE SHUTDOWN, RECIEVED A LEVEL 1 NR 1 ENGINE FIRE LOOP AN ALERT. REPOSITIONED DISLODGED FAN LOOP & SECURED LOOSE CLAMPS IAW MM 26-11-02-4 & TESTED NORMAL IAW MM 26-11-02 501.Aug 21, 2015 · N304FE · Doug MD1030F · Fire DetectionSDR FDEA201508062491Smoke Warning · false activationAS WE WERE BLOCKING IN, RECEIVED MOMENTARY CABIN SMOKE TWICE, THEN WENT AWAY. REMOVED & INSTALLED SERVICEABLE MISCELLANEOUS SYSTEMS CONTROLLER. OPERATIONAL CHECKED GOOD. PERFORMED LOWER CARGO SMOKE DETECTOR ADJUSTMENT TEST, ALL NORMAL. PERFORMED MAIN CARGOAug 6, 2015 · N304FE · Doug MD1030F · Smoke DetectionSDR FDEA201507232348Unknown · smokeHAD MOMENTARY PAC SOCK SMELL WITH SLIGHT SMOKE & MIST, AFTER ADJUSTING CURRIER SETTING TO 84 FROM 72. NO PROBLEMS AFTER RETURNING TO LOWER TEMP. WHILE RUNNING APU, NOTED HYD FLUID BEING INGESTED INTO THE APU INTAKE, FOUND NR 2 HYD SYS LEAKING AT THE SYS MANJul 23, 2015 · N304FE · Doug MD1030F · Air Distribution SystemSDR FDEA201507182259Unknown · smokeAT CRUISE, EXCESSIVE SMOKE FILLED THE COCKPIT. APPEARED TO COME THROUGH THE A/C VENTILATION SYS. COCKPIT TEMP SETTING HAD RECENTLY BEEN ADJUSTED TO A WARMER SETTING. TEMP CONTROL RETURNED TO COLDEST SETTING. SMOKE DISSIPATED DURING EMERGENCY DESCENT. RANJul 18, 2015 · N304FE · Doug MD1030F · Air Distribution SystemSDR FDEA201503261090Warning System · false activationDURING PREFLIGHT WITH APU START FWD CARGO FLASHING, DISCHARGE LIGHT ILLUMINATED. MX VISUALLY VERIFIED COMPARTMENT WAS CLEAR NO SMOKE. RESET BOTH MSC CB'S CHECKED OPERATION NORMAL. ACFT OK FOR SERVICE.Mar 26, 2015 · N304FE · Doug MD1030F · Smoke DetectionSDR FDEA201408062098Support Fitting · crackedLEFT WING OTBD FLAP INBD HINGE FWD SUPPORT RT FITTING PN ARB2431-509 HAS A CRACK ON FWD END. COMPLIED WITH IN EA T 8-5710-T310392 P1/SEQ 809.Aug 6, 2014 · N304FE · Doug MD1030F · Trailing Edge FlapsSDR FDEA201408062097Support Fitting · crackedLEFT WING OTBD FLAP INBD HINGE FWD SUPPORT LT FITTING PN ARB2431-507 HAS A CRACK ON FWD END. COMPLIED WITH IN EA T 8-5710-T310392 P1/SEQ 809.Aug 6, 2014 · N304FE · Doug MD1030F · Trailing Edge FlapsSDR FDEA201407302006Spar Cap · crackedHORIZONTAL STABILIZER RT AFT UPPER BARREL NUT HOLE HAS A CRACK INDICATION AT THE 6 O'CLOCK POSITION. REMOVED CRACK BY LOCAL BLEND OUT & WITHIN LIMITS IAW WORK CARD F5X1203ALI-P4 FIG 3 TABLE 2. VERIFIED CRACK REMOVAL BY FPI & HFEC INSPECTIONS IAW NDTSPM PART Jul 30, 2014 · N304FE · Doug MD1030F · Horizontal Stabilizer, Spar/RibSDR FDEA201404050663Indicator · inoperativeL1 SLIDE & RAFT WILL NOT TEST. CHANGED BATTERIES, NO HELP. RELEASED FOR SERVICE IAW MEL 25-61-01. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-01, VERIFY & RECORD IN THE AML. EVAC SLIDE SYS PRESS ONCE EACH FLIGHT DAY.Apr 5, 2014 · N304FE · Doug MD1030F · Escape SlideSDR FDEA201310152514Contact · out of positionDURING MX PREFLIGHT, FOUND R1 DOOR EVACUATION SLIDE TEST LIGHT INOPERATIVE. ADJUSTED BATTERY RETAINER CONTACTS IAW AMM-25-61-03-2. LIGHT OPS CHECKED NORMAL IAW AMM-25-61-03-5.Oct 15, 2013 · N304FE · Doug MD1030F · Escape SlideSDR FDEA201306041192Fire Warning · false indicationDURING PRE-START & GROUND LOADING, RECEIVED WORD OF A SUSPECTED APU FIRE. FIRED BOTH BOTTLES. APU RUNNING AT FULL POWER. AFTER AUTO SHUTDOWN BLACK SMOKE SEEN COMING FROM APU TAIL PIPE. PERFORMED INSPECTION OF APU BAY WITH NO DEFECTS NOTED. NO EVIDENCE OF Jun 4, 2013 · N304FE · Doug MD1030F · APU Core EngineSDR FDEA201209193368Uplock Sensor · failedAFTER RAISING GEAR AFTER TAKE OFF, LEVEL 1 BRAKE DIFF TEMP FOLLOWED BY LEVEL 2 BRAKE OVERHEAT. NR 4 WHEEL 935 DEGREE SLOWED TO 240 KNOTS. LOWERED LG NR 4 WHEEL TEMP SHOWED X AFTER 1 MINUTE SHOWED 9 DEGREE. SLOWED TO 220 KNOTS. RAIZED GEAR. HAD UNSAFE INDSep 19, 2012 · N304FE · Doug MD1030F · Landing Gear Position and WarningSDR FDEA201207262686Bolt · corrodedLT MAIN LANDING GEAR TRUCK BEAM PIVOT BOLT PITTED, AND HAS CHROME PLATING THAT IS FLAKING. R & R PIVOT BOLT REF SEQ 741 MAIN GEAR SHOCK STRUT.Jul 26, 2012 · N304FE · Doug MD1030F · Main Landing GearSDR FDEA201202130567Engine · stalledON TAKEOFF ROLL AT APPROX 60 KTS LARGE COMPRESSOR STALL FROM 1 MOTOR WITH YAW AND LARGE VIBRATION. REJECTED TAKE-OFF. NR 1 SHOWED EGT EXCEEDANCE AND N1 WITH (X)- NO ROTATION. SHUTDOWN ENGINE, PULLED FIRE HANDLE. RETURNED TO RAMP. ENGINE REPLACED. DUE TFeb 13, 2012 · N304FE · Doug MD1030F · Engine (Turbine/Turboprop)SDR FDEA201107232912Wire · brokenEVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATING SYS INOPERATIVE. RELEASED FOR SERVICE IAW MEL: 25-61-01. FOUND WHITE WIRE AT BATTERY PACK BROKEN. REPAIRED WHITE WIRE TO BATTERY PACK IAW STANDARD WIRING PRACTICE 20-10-05. REMOVED AND REPLACED BULBSJul 23, 2011 · N304FE · Doug MD1030F · Equipment/Furnishings WiringSDR FDEA201107182779Seal · missingIAW CREW DEBRIEF, CABIN STILL HAS PROBLEM WITH CONTROLLING PRESSURE. FOLLOWING SOME T/S AND WHILE INSTALLING CARGO FWD DOOR SEAL SAW A PIECE OF INSULTION COMING FROM BOTTOM OF THE R3 OVERWING PLUG DOOR. INSPECTED FROM INSIDE OF R3 DOOR FOUND THE LOWER DOOR SEJul 18, 2011 · N304FE · Doug MD1030F · Cargo/Baggage DoorsSDR FDEA201012084621Fire Warning · false activationDURING POWER UP/START OF APU, GOT FLASHING "AGENT DISCH" SW; NO LEVEL 3 CARGO FIRE ALERT, BUT CARGO DOOR (LOWER FWD) WAS CLOSED ALREADY AND COULD NOT BE INSPECTED UNTIL OPEN. PUSHED AGENT DISCHARGE SWITCH FOR LOWER FWD CARGO, BUT ON RETURN TO COCKPIT, HADec 8, 2010 · N304FE · Doug MD1030F · Fire DetectionSDR FDEA201009053299Cylinder · inoperativeCTR LANDING GEAR FAIL TO DEPLOY USING ALTERNATE EXTENSION CABLE. BOTH NORMAL AND CONFIG LANDIG GEAR IN DICATION SHOW CTR LANDING GEAR RED. JACKED AND DOWNJACKED ACFT, DISCONNECTED AND RECONNECTED FWD CENTERLINE GEAR DOORS FROM STRUT, FOUND MAIN GEAR INTERLOSep 5, 2010 · N304FE · Doug MD1030F · Landing Gear Retraction/Extension SystemSDR FDEA201009023246Skin · damagedLEFT WING NR 2 SLAT OUTER SKIN LOWER AFT EDGE HAS A BLENDOUT. FABRICATED REPAIR DOUBLER IAW SRM 57-10-00, FIG 84, VOL 1. ALODINED AND PRIMED IAW IAW SRM 51-21-01, VOL II. INSTALLED DOUBLER IAW SRM 51-35-01, VOL II.Sep 2, 2010 · N304FE · Doug MD1030F · Wing, Control SurfacesSDR FDEA201009013230Frame · damagedMAIN CABIN INTERIOR LINER ATTACH BRACKET HAS A FASTENER THRU THE RADIUS OF FRAME 1159; BETWEEN STRINGER 11R - STRINGER 12R. COMPLIED WITH EA 8-5310-136699.Sep 1, 2010 · N304FE · Doug MD1030F · Fuselage Main, Frame
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