N574FE
Service difficulty reports · 611
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 = 'N574FE' 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 = 'N574FE' 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 FDEA201901080047Transmitter · faultyPDIS 574 79-32 8368 08JAN19 LAX OPEN U LOGPAGES:3074658 ON CLIMBOUT PASSING FL 300, NOTICED NR 3 ENG OIL PRESSURE LOW, IN YELLOW, 22 PSI. NR 1 PSI WAS 55, NR 2 WS 54. TALKED TO MOCC & GOCC & DECIDEDTO RETURN TO LAX. RAN NR 1 AND NR 3 ENGINES AT DIFFERENT POWERSDR FDEA2018100532773Piston · leakingUPON ARRIVAL FOUND L GEAR NR 6 BRAKE AREA ON FIRE, FOUND EVIDENCE OF HYD LEAK FROM NR 6 BRAKE PISTON. ALL TIRES PRESSURE ARE NORMAL, BRAKES TEMP ARE NORMAL ALSO. REMOVED AND REPLACED NR 6 BRAKE AS PER AMM 32-43-20-4 AND TESTED NORMAL PER AMM 32-46-00-5, NO LEASDR FDEA201803210748Seal · damagedLEVEL 2 WING ANTI ICE DISAGREE DURING CLIMB OUT AT 3,000 FT MSL. RETURNED TO DEPARTURE, INSTALLED A NEW ANTI-ICE DUCT SEALS AT SLATS 3 - 4 AND 5 - 6 IAW MM 30-11-03-2. RT WING DECAY CHECKED GOOD MM 36-00-01-5. WING ANTI-ICE CHECKED GOOD IAW MM 30-11-00-5.SDR FDEA201710233025Hinge Bracket · wornLEFT FWD WING SIDE INBD FLAP FWD OTBD HINGE PIVOT BORE WORN. FOUND THE INDB & OTBD FACE OUT OF LIMITS IAW CMM 57-44-07. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-87635F, P2, STEP 1F (1) AND STEP 1F (3). THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMMSDR FDEA201710193007Hinge · wornUPPER CARGO DOOR, FWD HINGE LOBES ON AIRCRAFT, FOUND INSIDE DIAMETER WORN, EXCEEDED MAXIMUM PERMITTED LIMITS. FOUND THE NR 1 HOLE EXCEED LIMITS IAW SRM 52-30-16-1A. REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5310-T0335958, PART 1, STEP 2 AND 5,SDR FDEA201710193006Frame · crackedLEFT MLG DOOR CENTER UPPER FRAME FOUND TWO CRACKS. REPAIRED IAW EA 1-5280-T0336029 P1, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201710172970Bracket · wornLEFT WING TELESCOPIC DUCT DOOR CUTOUT INBD AND OUTBD BRACKET WORN XOS 464-470. REMOVED IAW SRM 51-31-01-0G AND FABRICATED A NEW CAP IAW DWG ARB1284, REV AC. INSTALLED THE NEW CAPS IAW SRM 51-35-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710142959Skin · chafedRIGHT WING DROOP LEADING EDGE, INBD EDGE, CHAFED AT XDLE 309. REPAIRED IAW SRM 57-40-01-2R, FIG 202, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710142952Skin · crackedDURING HFEC INSPECTION ON LEFT WING FIXED LEADING EDGE SLAT TRACK CUTOUT, AFT INBOARD CORNER CRACKED, 1/8 INCH IN LENGTH AT XOS 655. REPAIRED THE SKIN IAW SRM 57-40-02-2R, FIGURE 201, REPAIR 7. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710142951Skin · chafedLEFT NR 3 SLAT LOWER AFT SKIN EDGE INBD AND OTBD OF TELESCOPIC DUCT CUTOUT DOOR FOUND CHAFING MARKS. REPAIRED.SDR FDEA201710142940Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 643 - 648 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710142939Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 610 - 615 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710142938Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 625 - 627 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710122915Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT XOS 729 - 734 FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM6-2-100.SDR FDEA201710122914Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT XOS 692 - 698 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710122913Cargo Track · gougedMAIN DECK CARGO TRACK CROWN DAMAGED AT BS 1269, LBL 47.5. THE CARGO TRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 201, ALLOWABLE DAMAGE 1. THE CARGO TRACK WAS REPLACED FROM BS 6-100 TO 1170 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR SDR FDEA201710122911Frame · crackedLEFT WING LEADING EDGE CAVITY FRAME FOUND CRACKED AT XOS 801. THE FRAME WAS REMOVED IAW SRM 51-31-01-0G. FABRICATED A NEW FRAME IAW DRAWING ARB2922, REV B. INSTALLED THE NEW FRAME AIW SRM 51-35-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710122910Rib · crackedLEFT WING LEADING EDGE RIB DOUBLER AT XOS 789, FOUND CRACKED. THE DOUBLER WAS REMOVED IAW SRM 51-31-01-0G, FABRICATED A NEW DOUBLER IAW DRAWING ARB3954, REV K. INSTALLED THE DOUBLER IAW SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710122909Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT XOS 629 - 633 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710122908Seat Track · gougedMAIN DECK CARGO TRACK CROWN DAMAGED AT BS 1289, RBL 47.5. FOUND OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPLACED FROM BS 1248 TO 1331 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GSDR FDEA201709152566Roller · bindingDURING GEAR RETRACTION WE GOT A RIGHT MAIN UNSAFE GEAR UP INDICATION. RAN QRH PROCEDURE AND OBTAINED A GOOD GEAR UP INDICATION. DURING TROUBLESHOOTING FOUND RIGHT MAIN GEAR DOOR FELL OPEN WITH NO HYDRAULIC PRESSURE AND DOOR HANDLE IN THE UP POSITION. INSPECTSDR FDEA201708102175Cable · brokenRIGHT WING OUTBOARD NR 8 SLAT HAS A BROKEN DRIVE CABLE. REPLACED THE SLAT CABLES 84E & 84F IAW AMM 20-20-06-2. PERFORMED TENSION ADJUSTMENT OF THE DRIVE CABLE.SDR FDEA201701240244Clamp · out of positionAFTER TAKE OFF WITH AIR MANUAL AND ICING ANTICIPATED, ENGINE & WING ANTI-ICE WAS ON & ARMED. WHEN THE WING ANTI-ICE VALVE ATTEMPTED TO OPEN LEVEL 2 WING ANTI-ICE DISAGREE ILLUMINATED. NO LONGER IN ICING CONDITIONS, DESELECTED WING ANTI-ICE AND ALERT EXTINGSDR FDEA201610223678Bracket · chafedWHILE INSTALLING THE RT WING NR 4 L/E SLAT, FOUND THE SLAT DRIVE CABLE HAS A BROKEN BRACKET HOLDING THE PULLEY. JUST I/B OF DRIVE SLAT TRACK. , INSTALLED A NEW RT NR 4 SLAT RETRACT PULLEY AND BRACKET. TORQUED BOLTS TO BRACKET AND PULLEY IAW AMM 20-50-02-2. SDR FDEA201605291778Relay · malfunctionedINFLIGHT AT FL 320 DEU'S 4 - 6 & MCDU 2 WENT BLANK & IMMEDIATELY GOT LEVEL 1 BUSS RT EMERGENCY AC OFF ALERT. ALSO OFF LIGHT RT EMERGENCY AC ON OVERHEAD & ELECTRICAL DISPLAY, MANY ASSOCIATED ALERTS, SELECT FADEC ALTERNATE, SINGLE LAND, ATC TRANSPONDER 2 FAIL, SDR FDEA201605261740Arming Lever · brokenLOCKING LATCH FOR L1 DOOR, DISARM LEVER BROKEN OFF. R & R THE L1 DOOR ARMING LEVER. OPERATIONS CHECKED NORMAL IAW AMM 52-11-02-4. ACFT OK TO CONTINUE.SDR FDEA201605141580Probe · malfunctionedAPPROXIMATELY 2 HRS INTO FLIGHT FUEL TOTAL & ALL 3 MAIN TANKS SHOWED FLUCTUATION OF 5000 LBS. QRH FUEL QTY ABNORMAL INDICATION COMPLIED WITH. RELEASED FOR SERVICE IAW MEL 28-01-01-02 CATEGORY AN EXPIRATION 16 MAY 16. TANK NR 2 FUEL TANK SYNOPTIC QTY DISPLAYSDR FDEA201512073931Skin · chafedRIGHT WING FIXED LEADING EDGE SKIN LOWER EDGE FOUND CHAFFED JUST OUTBOARD OF DROOP LEADING EDGE. REPAIRED IAW EA 1-5730-T0321987 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201512023850Longeron · corrodedCENTER CARGO COMPARTMENT BILGE AREA LONGERON 51L , STATION 1601, FOUND WITH CORROSION. REPAIRED IAW EA 1-5310-T0322006A PT 1. WORK INSTRUCTION REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100. REFER TO WRI 53103463 FOR WORK DETAILS.SDR FDEA201512023849Skin · crackedLEFT WING, NR 14 LE SLAT TRACK LOWER CUT OUT SKIN, FOUND CRACK AT STATION XOS 891. CRACKED AREA TRIM OUT & CARRIED OUT REPAIR IAW SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201512023848Longeron Splice · crackedMAIN DECK CARGO LT LONGERON 15L, AT STATION 5-0, FOUND LONGERON END SPLICE CRACKED. REMOVED IAW SRM 51-33-01-0G. LONGERON SPLICE FABRICATED BY MACHINING IAW DWG AEA7654 REV C & INSTALLED IAW SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201512013835Longeron · corrodedCENTER CARGO COMPARTMENT BILGE AREA AT STATION 1701, LONGERON 48R, FOUND CORROSION. REPAIRED IAW EA 1-5310-T0321985 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 53103462 FOR WORK DETAILS.SDR FDEA201512013834Doubler · crackedLEFT WING, FIXED LE BEADED DOUBLER AT XOS 646, FOUND CRACK DURING OTBD SLAT DRIVE CABLE INSPECTION. CARRIED OUT DOUBLER REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201512013833Doubler · crackedLEFT WING, FIXED LE BEADED DOUBLER AT XOS 613, FOUND CRACK DURING OTBD SLAT DRIVE CABLE INSPECTION. CARRIED OUT INNER SKIN DOUBLER REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201511293816Skin · damagedTO CARRY OUT PERMANENT REPAIR ON LT WING LEADING SKIN AT NR 8 SLAT TRACK CUT OUT AT STATION XOS 547.588 IAW EA 1-5730-T0309161 PART 3 WORK INSTRUCTIONS. REPAIRED IAW EA 1-5730-T0309161A PT 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TO WRI 57303453SDR FDEA201511293824Web · crackedMAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX AT BS 1305.25 - 1315.42, LONGERON 26 - 27L, FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201511293823Web · crackedMAIN DECK L3 DOOR FWD JAMB LOWER WEB BOX AT BS 1250.75 - 1256.75, LONGERON 26L - 27L, FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED IAW GMM 6-2-100.SDR FDEA201511293822Web · crackedMAIN DECK R3 DOOR FWD JAMB LOWER WEB BOX AT BS 1250.75 - 1256.75, LONGERON 26 - 27R, FOUND CRACKED. REPAIRED IAW SRM 53-40-15-2R FIG 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201511293821Seat Track · crackedMAIN DECK FLOOR SEAT TRACK AT STATION 695, X= -27.5, FOUND CRACKED AS MARKED. SECTIONAL REPAIR CARRIED OUT ON SEAT TRACK AT MAIN DECK FLOOR STATION 685 - 745, X= -27.5 AREA IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201511293820Seat Track · crackedMAIN DECK FLOOR SEAT TRACK AT STATION 695, X= 8.5, FOUND CRACKED AS MARKED. SECTIONAL REPAIR CARRIED OUT ON SEAT TRACK AT MAIN DECK FLOOR STATION 685 - 745, X=8.5 AREA IAW SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201511293819Frame · damagedMAIN DECK, LT FRAME AT BS 1681, LONGERON 12L, FOUND REPAIR DOUBLER DAMAGED. REPAIRED IAW SRM 53-00-07-2R FIG 201 REPAIR 2. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201511293818Skin · wornRIGHT WING INBD AILERON, LOWER LE SKIN FOUND WORN AT APPROX STATION XIA 524.456. REMOVED IAW SRM 51-31-01-0G. NEW SKIN FABRICATED IAW DWG ARC 1250 REV D. NEW FABRICATED SKIN INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REFER TSDR FDEA201511293817Strap · crackedRIGHT WING TE LOWER CHORD STRAP SILL FOUND CRACK AT WING STATION XORS 402. REMOVED IAW SRM 51-31-01-0G. NEW STRAP SILL FABRICATED BY MACHINING IAW DWG ARC7008 REV C. NEW FABRICATED STRAP SILL INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMSDR FDEA201511073511Wire · damagedANTI-SKID FAIL ON APPROACH. REPLACED WIRE HARNESS (AES9301-501), REF SWP 20-10-10.SDR FDEA201509112844Unknown · malfunctionedWE HAD A RAPID DEPRESSURIZATION. PAIR HEARD THUMP, BUMP ON RT SIDE OF ACFT FLIGHT 370 1000Z ACFT STOPPED AT TAXIWAY FOR GVI EXTERIOR & NO DAMAGE FOUND. ACFT ON BLOCK IAW AMM 21-00-00-5. PERFORMED FUSELAGE PRESS DECAY TEST & PRESSURIZED CABIN PRESS TO 8 PSI SDR FDEA201508162566Cap · looseNUMBER 1 ENG OIL PRESS DISPLAYED AN AMBER BOX, 15 MIN AFTER DEPARTURE, CLIMB POWER FL335 TO FL350. AT CRUISE, PRESS WENT INTO GREEN. AMBER BOX APPEARED AGAIN WITH A LOSS OF 3 QTS OIL, 20 INTO FLIGHT. PRECAUTIONARY SHUTDOWN INFLIGHT, WIND MILLED FROM 1422Z SDR FDEA201505041379Charger · failedDURING PREFLIGHT CHECK FOUND, EMERGENCY POWER TEST FAIL. R & R BATTERY CHARGER IAW MM 24-34-03-4. PERFORMED OPERATIONS TEST OF THE BATTERY CHARGER IAW MM 24-34-03-5. TESTED OK. CHECKED EMER POWER TESTED GOOD.SDR FDEA201406231526Skin · crackedDURING FCD ON LT WING FOUND POSSIBLE CRACK ON NR 8 SLAT TRACK. PERFORMED HFEC INSPECTION IAW NTSPM 06-10-01001. VERIFIED CRACK, COMPLIED WITH EASDR FDEA201406231525Access Panel · crackedRT WING FUEL PANEL DOOR INBD POSSIBLE CRACK. PERFORMED HFEC INSPECTION ON SUSPECTED CRACK IAW NDTSPM 06-10-01. CRACK RUNS PAST RIVET, FUELING DOOR REMOVED & ADJUSTED PANEL INBD TO FACILITATE REPAIR. REMOVED FASTENERS TO BE INCLUDED IN REPAIR. CUT OUT DASDR FDEA201405241153Engine · making metalWHILE LEVEL AT FL370, RECEIVE A LEVEL 2, NR 3 ENGINE OIL FILTER ALERT. COMPLIED WITH QRH DIRECTIVE & SHUTDOWN NR 3 ENGINE. ALL OTHER ENGINE INDICATIONS WERE NORMAL. REMOVED MAIN CHIP DETECTOR & FOUND LARGE QTY OF LARGE METAL PARTICLES. REMOVED OIL FILTER
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