N617FE
Service difficulty reports · 467
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 = 'N617FE' 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 = 'N617FE' 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 FDEA2020070821302Floor Panel · damagedMAIN DECK CARGO COMPARTMENT AFT LEFT AREA , STATION Y1901 FLOOR PANEL #291GF (SECOND FROM OUTBOARD) FOUND SPONGY. MAIN DECK CARGO COMPARTMENT AFT LEFT AREA, X = 47.5 STATION Y1901. FLOOR PANEL #291GF REMOVED PER AMM 53-21-09-4, FABRICATED PER DRAWING SRSDR FDEA2020070821301Floor Panel · damagedMAIN DECK CARGO COMPARTMENT LEFT SIDE STATION Y535 , OUTBOARD FLOOR PANEL #231EF FOUND WITH SEVERAL PUNCTURES. MAIN DECK CARGO COMPARTMENT LEFT SIDE X = 78 STATION Y535, OUTBOARD FLOOR PANEL #231EF REMOVED PER AMM 53-21-09-4, FABRICATED PER FEDEX DRAWINGSDR FDEA2020070211302Floor Panel · damagedMAIN DECK CARGO COMPARTMENT AFT LEFT AREA, STATION Y1901 FLOOR PANEL 291GF (SECOND FROM OUTBOARD) FOUND SPONGY. MAIN DECK CARGO COMPARTMENT AFT LEFT AREA, STATION Y1901 FLOOR PANEL 291GF REMOVED PER AMM 53-21-09-4, FABRICATED PER DRAWING SRZ-25-005 REVISION RSDR FDEA2020070211301Floor Panel · damagedMAIN DECK CARGO COMPARTMENT LEFT SIDE STATION Y535, OUTBOARD FLOOR PANEL 231EF FOUND WITH SEVERAL PUNCTURES. MAIN DECK CARGO COMPARTMENT LEFT SIDE STATION Y535, OUTBOARD FLOOR PANEL 231EF REMOVED PER AMM 53-21-09-4, FABRICATED PER DRAWING SRZ-25-005 REVISION SDR FDEA2020062311302Floor Panel · damagedMAIN DECK CARGO COMPARTMENT AFT LEFT AREA, STATION Y1901 FLOOR PANEL 291GF (2ND FROM OUTBOARD) FOUND SPONGY.SDR FDEA2020062311301Floor Panel · damagedMAIN DECK CARGO COMPARTMENT LEFT SIDE STATION Y535, OUTBOARD FLOOR PANEL #231EF FOUND WITH SEVERAL PUNCTURES.SDR FDEA202006191281Doubler · corrodedLEFT WING UPPER INBOARD SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER CORRODED NEAR INBOARD EDGE. CORROSION REMOVED AND FOUND EXCEEDED LIMITS. CORROSION REMOVAL 0.100 INCHES MAXIMUN IAW SRM 57-20-01-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED IAW EA 1-5SDR FDEA202006191280Doubler · corrodedRIGHT WING UPPER INBD SURFACE, MAIN LANDING GEAR SUPPORT DOUBLER CORRODED NEAR TWO INBD AFT FASTENERS. CORROSION REMOVED AND FOUND EXCEED LIMITS. CORROSION REMOVAL 0.100 INCHES MAXIMUN IAW SRM 57-20-01-1A, FIGURE 101, ALLOWABLE DAMAGE 1 . REPAIRED IAW EA 1-SDR FDEA202006171260Frame · crackedDURING HFEC INSPECTION, FRAME AT BS 1721, BETWEEN STRINGER 12L AND 13. FOUND CRACKED ON ORIGINAL FRAME APPROXIMATE 1/2 INCH.SDR FDEA2020071031215Former · crackedLEFT WING LEADING EDGE REFUELING PANEL COMPARTMENT CUTOUT EDGE FOUND CRACKED AT OUTBOARD AFT CORNER AREA XOS 643. REMOVED AND FABRICATED A FORMER IAW DRAWING ARB 2917, REVISION L . FABRICATED FORMER INSTALLED IAW SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOSDR FDEA2020070831213Doubler · crackedLEFT HAND WING LEADING EDGE COMPARTMENT FOUND WITH BEAD DOUBLER MINOR CRACKED AT XOS 771 LEFT WING LEADING EDGE COMPARTMENT CRACKED BEADED DOUBLER TRIMMED OUT REPAIR ANGLE AND DOUBLERS FABRICATED AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203 . REPAIR ANGLSDR FDEA2020070831209Doubler · crackedRIGHT HAND WING- LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 639 FOUND CRACK RIGHT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 639 CRACKED AREA TRIMMED OUT . REPAIR ANGLE AND DOUBLERS FABRICATED AS PER SRM 57-40-02-2R FIGURE 203 REPSDR FDEA2020070831208Doubler · crackedLEFT HAND WING- LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 766 FOUND CRACK LEFT WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 766 CRACKED AREA TRIMMED OUT . REPAIR ANGLE AND DOUBLERS FABRICATED AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203SDR FDEA2020070631214Former · crackedRIGHT HAND WING LEADING EDGE PANEL COMPARTMENT CUTOUT EDGE FOUND CRACKED AT OUTBOARD AFT CORNER AREA XOS 643. RIGHT HAND WING LEADING EDGE REFUELING PANEL COMPARTMENT CUTOUT EDGE CRACKED AT OUTBOARD AFT CORNER AREA ( XOS 643 ) REMOVED PER SRM 51-31-01-OG. FASDR FDEA2020070631212Doubler · crackedLEFT HAND WING-LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 609 FOUND CRACK. LEFT WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 609 CRACK AREA TRIMMED OUT AND REPAIR CARRIED OUT PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR PARTS MATERIAL USSDR FDEA2020070631210Doubler · crackedLEFT HAND WING-LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 663 FOUND CRACK. LEFT WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 633 CRACK AREA TRIMMED OUT AND REPAIR CARRIED OUT PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR PARTS MATERIAL USSDR FDEA2020061631215Skin · crackedLEFT HAND WING LEADING EDGE REFUELING PANEL COMPARTMENT CUTOUT EDGE FOUND CRACKED AT OUTBOARD AFT CORNER AREA XOS 643.SDR FDEA2020061631214Skin · crackedRIGHT HAND WING LEADING EDGE PANEL COMPARTMENT CUTOUT EDGE FOUND CRACKED AT OUTBOARD AFT CORNER AREA XOS 643.SDR FDEA2020061631213Doubler · crackedLEFT HAND WING LEADING EDGE COMPARTMENT FOUND WITH BEAD DOUBLER MINOR CRACKED AT XOS 771.SDR FDEA2020061631212Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 609 FOUND CRACK.SDR FDEA2020061631210Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 663 FOUND CRACK.SDR FDEA2020061631209Doubler · crackedRIGHT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 639 FOUND CRACK.SDR FDEA2020061631208Doubler · crackedLEFT HAND WING LEADING EDGE CAVITY BEADED DOUBLER AT STATION XOS 766 FOUND CRACK.SDR FDEA2020070221192Doubler · crackedAGING AIRCRAFT, EXISTING REPAIR AT RIGHT HAND WING LOWER LEADING EDGE, STRINGER DOUBLER REPAIR XOS 906. EXISTING STRINGER DOUBLER REPAIR AT RIGHT HAND WING LOWER LEADING EDGE, XOS 906 REMOVED IN ACCORDANCE WITH SRM 51-31-01-0G AND NEW REPAIR CARRIED OUT IN ACSDR FDEA2020071091163Frame · crackedEMPENNAGE - ACCESS PANEL 364QR FOUND CUT OUT CRACKED UPON PANEL REMOVAL. AT STATION 2164 RIGHT HAND ZID = 75.5 , XID = 9.0 . EMPENNAGE ACCESS PANEL 364QR AT STATION 2164 RIGHT HAND ZID = 75.5 , XID = 9.0 CRACKED SKIN PANEL REMOVED PER SRM 51-31-01-OG . NEWSDR FDEA2020071091162Frame · crackedEMPENNAGE - ACCESS PANEL 363ML FOUND CUT OUT CRACKED UPON PANEL REMOVAL. AT STATION 2164 LEFT HAND , ZID = 72.0 , XID = 9.0 . ACCESS PANEL 363ML AT STATION 2164 LEFT HAND ZID = 72.0 XID = 9.0 CRACK FRAME REMOVED AND REPLACED AS PER EA # 1-5500-T0354594P1.SDR FDEA2020061091163Skin · crackedEMPENNAGE - ACCESS PANEL 364QR FOUND CUT OUT CRACKED UPON PANEL REMOVAL.SDR FDEA2020061091162Skin · crackedEMPENNAGE ACCESS PANEL 363ML FOUND CUT OUT CRACKED UPON PANEL REMOVAL. ACCESS PANEL 363ML AT STATION 2164 LEFT HAND ZID 72.0 CRACK FRAME REMOVED AND REPLACED AS PER EA 1-5500-T0354594 TITLE : STABILIZERS - GENERAL - PYLON CARRY THRU PANEL FRAME AJC 7593-51 ALSDR FDEA2020050410890Trim Motor · cracked2:00 INTO FLT, FLT 370 HYD 3 ELEV OFF ALER. HYD SYS 3 WAS AT 3.9 OVER NEXT FIVE MINUTES DROPPED TO 3.6. DEPRESSURIZED SYS UNTIL LANDING. AFTER LANDING QTY WAS DOWN TO 1.0 FOUND HYDRAULIC FLUID MISTING IN TAIL AREA AROUND HORIZONTAL STABILIZER TRIM MOTORSSDR FDEA2020031290509Compensator · inoperativeAT LEVEL OFF, WHEN COMBINING FUEL USED AND FUEL REMAINING, TOTAL FUEL WAS 7000 # HIGHER THAN OUR INITIAL FUEL AT BLOCK OUT. FUEL QTY NUMBERS ON FUEL SYNOPTIC WERE INTERMITTENTLY AMBER THEN WHITE, BUT FUEL TOTAL WAS ALWAYS GROSSLY INACCURATE, MAXING AT THSDR FDEA2020061622615Skin · corrodedAFT ACCESSORY COMPARTMENT HAS EVIDENCE OF CORROSION ON R/H SIDEWALL. REPAIR IN REF. TO MD11 SRM 53-70-01-2R; FIG. 201.SDR FDEA2019101422615Skin · corrodedAFT ACCESSORY COMPARTMENT HAS EVIDENCE OF CORROSION ON THE RT SIDEWALL. REPAIRED IAW SRM 53-70-01-2R, FIG 201.SDR FDEA2019081521845Electrical Sys · unknownDURING SVC, FOUND EMERGENCY PWR TEST COULD NOT BE COMPLETED. ONLY BATTERY VOLTAGE DROP TO 28V AND GO UP TO 31V WITHOUT BATTERY CHARGING ALERT. EPCU NO FAULT AND RTS TEST PASSED. BAT CHARGER C/B RESET NO HELP AND CYCLED A/C PWR NO HELP. STARTED APU PER JRSDR FDEA2019062421401Check Valve · leakingAPPROX. 1 HOUR INTO FLIGHT LEVEL 1 HYD EIU 3 OFF ALERT. HYD QTY 3.2. HYD QTY CONTINUED TO DECREASE TO 2.5 LEVEL 1 HYD 3 OFF. QTY THEN HELD SEADY AT 2.5. AT SLAT EXNTENSION, QTY IMMEDIATLY DROPPED AND RECIEVED LEVEL 2 HYD FAIL ALERT. QTY WENT TO NEARSDR FDEA201905121038Battery · dischargedPDIS 617 33-50 8018 12MAY19 MEM OPEN U LOGPAGES:3111468 DURING CA CABIN PREFLIGHT, EMER LIGHTS TEST FAILED W/ "EMER LT BAT 1 LOW" FAULT. MEL 12MAY19 20:06 MEM U RELEASED FOR SERVICE PER MEL : 33-50-04 CATEGORY : C EXPIRATION : 22MAY19 "MEL 33-50-04:SDR FDEA201905121037Battery · dischargedDURING CA CABIN PREFLIGHT, EMER LIGHTS TEST FAILED W/ "EMER LT BAT 1 LOW" FAULT. R&R'ED EMERGENCY POWER SUPPLY BAT PER MM 33-51-01-4 AND PERFORMED TEST PER MM 33-51-01-5, TEST PASSED MEL CLOSED.SDR FDEA201902170443Light · malfunctionedEMER LIGHT TEST ARM WOULD NOT TEST. PERFORMED RESET TO EMERGENCY LIGHT CONTROL C/B G13. OPERATIONAL CHECK OKSDR FDEA201812013413Fire Detector · intermittentPDIS 617 26-10 7503 01DEC18 EWR OPEN U LOGPAGES:2733768 "FIRE DET 3 FAIL" BLINKS INTERMITTANTLY. AT TIMES SHGN 02DEC18 19:08 EWR REMOVED AND REPLACED NR 3 ENGINE UPPER TURB R LOOP A (DH4) FIRE DETECTOR AS REQUIRED IN REF TO AMM 26-11-03-4-1 FACT 03DEC18 06:58 SDR FDEA2018081412008Frame · dentedMAIN DECK CARGO BAY FRAME WAS DENTED BS 1761, LONGERON 12L. REPAIRED THE FRAME IAW SRM 53-00-07-2R, FIGURE 201, REPAIR 2. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201808081955Doubler · crackedLEFT WING LEADING EDGE COMPARTMENT LOWER SURFACE, 518GB PANEL CUTOUT, FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA20180821954Doubler · crackedLEFT WING LEADING EDGE COMPARTMENT ALONG XOS 708, AROUND THE NR 5 SLAT AREA, FOUND THE LEADING EDGE PLATING BEADED DOUBLER CRACKED. THE BEADED DOUBLER WAS TRIMMED OUT AND REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MASDR FDEA20180821953Stringer · crackedLEFT WING LEADING EDGE COMPARTMENT ALONG XOS 665, AROUND THE NR 5 SLAT AREA, FOUND LEADING EDGE PLATING STRINGER CRACKED. TRIMMED AND REPAIRED IAW SRM 57-40-03-2R, FIGURE 202, REPAIR 2. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201806061405Tire · leakingLEVEL 1 LOW TIRE PRESSURE ALERT ON NR 5 TIRE CAME ON DURING CLIMB. FOLLOWED BY LEVEL 2 TIRE FAILURE ALERT. C/W QRH AND RETURNED TO KMEM. REPLD NR 5 AND NR 6 WHEEL ASSY REF AMM 32-41-01-4. INSP WHEEL WELL AND LANDING GEAR AREA. NO DAMAGE FOUND. A/C OK FORSDR FDEA2018051871254Flex Line · brokenON BLOCK IN, ADVISED BY GROUND THAT FLAMES WERE COMING FROM LEFT GEAR . TRYING TO CONFIRM, THE FLAMES HAD STOPPED. HIGHEST BRAKE TEMP NOTED ON CONFIG PAGE WAS 6 AT 473. ALL TEMPS ON LEFT TRUCK WERE MID 400S, ALL TEMPS ON RIGHT TRUCK MID 300S. LIGHT TO MEDSDR FDEA201804140994Pitot Line · cloggedAT FL380, WITH THE ENGINE & WING ANTI-ICE ON, RECEIVED AN IAS COMPARITOR LIGHT. A/S STARTED DECAYING TOWARD THE LWR FOOT. STARTED AN IMMEDIATE DESCENT TO FL340. LVL 2 SEL ELEV FEEL MAN. QRH DIRECTED REFERENCE TO FLT INSTEUMENTS > EMERG NON-ALERT PROCEDUSDR FDEA201708062174Skin · crackedCRACK ON FUSELAGE AT THE UPPER AFT CORNER OF NR 1 PACK BAY DOOR. REPAIRED IAW SRM 53-20-15-2R.SDR FDEA201707192002Collar · brokenDURING POSTFLIGHT, FOUND NOSE STRUT LOWER STEERING SUPPORT COLLAR ASSY BROKEN. REMOVAL OF NOSE STRUT LOWER LEG IN PROGRESS AS PER AMM 32-21-01-8 FROM CHAPTER 4 . INSTALLED IAW MM 32-21-01-8 FROM STEP 5.F.11. ALL TEST PASSED INCLUDING NOSE LANDING GESDR FDEA201609273372Vane · corrodedLEFT WING OTBD FLAP VANE HORN FITTING-D, BUSHING BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. REPAIR SLOT BUSHING FABRICATED IAW EA 1-5750-T0328435 PART 1 STEP 1A AND INSTALLED IAW AMM 27-50-32-4.SDR FDEA201609273371Vane · corrodedRIGHT WING OTBD FLAP VANE HORN FITTING-C, BUSHING BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R, FIG 201. A REPAIR SLOT BUSHING WAS FABRICATED IAW EA 1-5750-T0328433 PART 1 STEP 2B AND INSTALLED IAW AMM 27-50-32-4.SDR FDEA201609273370Vane · corrodedRT WING OTBD FLAP VANE HORN FITTING E, BUSHING BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R FIG.201. SLOT BUSHING FABRICATED IAW EA 1-5750-T0328433 PART 1 STEP 2A AND INSTALLED IAW AMM 27-50-32-4.
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