N664FE
Service difficulty reports · 307
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 = 'N664FE' 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 = 'N664FE' 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 FDEA202205071281Floor Panel · damagedTHE #242JG FLOOR PANEL WAS FOUND INSERT DAMAGED WITH MARK REPLACED THE DAMAGED INSERTS WITH NEW INSERTS I.A.W A300-600F SRM 51-72-10-001, P.2 AND FEDEX DRAWING NO: SRZ-25-005.SDR FDEA202205071214Floor Panel · damagedTHE #241UF FLOOR PANEL WAS FOUND INSERT DAMAGED WITH MARK REPLACED THE DAMAGED INSERT WITH NEW INSERT I.A.W A300-600F SRM 51-72-10-001, P.2 AND FEDEX DRAWING NO: SRZ-25-005.SDR FDEA202205071341Hinge Arm · crackedVERTICAL STABILIZER TO RUDDER NO.4 HINGE ARM FOUND UPPER PART CRACK AND 1EA RIVET HEAD SHEAR AT RIB 10,LH AREA. REPLACED THE UPPER HINGE ARM WITH NEW ONE I.A.W EA NO:6-5530-T0368481 P1, SEQ NO:001036, TITLE:STABILIERS-VERTICAL STABILIZER RUDDER HINGE ARM #SDR FDEA202205071299None · crackedVERTICAL STABILIZER TO RUDDER NO.4 HINGE ARM FOUND LOWER PART LH JOINT BRACKET BROKEN AT RIB 10 AREA. REPLACED THE BRACKET WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, P.2SDR FDEA202205071200Floor Support · corrodedN00240 THE COURIER AREA FOUND FLOOR SUPPORT GOT CORROSION LOCATION AT FR14 -3.5" AND Y730. REMOVED DAMAGED FLOOR SUPPORT AND REPLACED WITH NEW ONE. I.A.W. A300-600F SRM 51- 72-10-001, PAGE.1-2 & 51-40-21-001 PARA.6 PAGE. 7B-23.SDR FDEA202205021280Floor Panel · damagedTHE FLOOR PANEL #132NG WAS FOUND INSER DAMAGED REPLACED THE DAMAGED INSERTS WITH NEW INSERTS I.A.W A300-600F SRM 51-72-10-001, P.2 AND FEDEX DRAWING NO: SRZ-25-005.SDR FDEA202205021387Stiffener · corrodedWASTE WATER SERVICE PANEL CUTOUT FWD LOWER CORNER SKIN AREA CORROSION AT FR12 POSITION. REPLACED THE STIFFENER WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE.2SDR FDEA202203150519Power Supply · failedMDIS 664 33-50 4218 17JAN22 LAX FACT U ON 'A' CHECK FOUND THE OPS CHECK OF THE EMERGENCY POWER SUPPLY FAILING. R/I 17JAN22 16:56 LAX U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 3214-41 POS: ONL SRLSDR FDEA202203140500None · failedPDIS 664 22-10 4554 10MAR22 IND FACT U AFTER TAKEOFF, NOTICED CAPTAINS PFD SHOWED RED ZIPPER LIMIT AT 270 KTS AS IF THE GEAR WAS DOWN. BOTH GEAR INDICATOR SYSTEMS SHOWED ALL GEAR UP AND DOORS CLOSED. AT 10,000 FEET WE SWITCHED CAPT SIDE TO ADSDR FDEA202012263213Fan · failedON RUNWAY WHILE RUNNING UP ENGINES TO 40% FOR TAKEOFF, BLOWER FAULT LIGHT ILLUMINATED. REJECTED TAKEOFF AND APPLIED PDM. MEL 21-23-01-01-A 'VENT BLOWER FAN INOPERABLE'. RELEASED FOR SERVICE, PER MEL: 21-XX-XX-XX CAT: C "MEL 21-XX-XX-XX: VENT BLOWER FAN-INOPSDR FDEA202003120555Actuator · failedPDIS 664 32-20 2538 12MAR20 GRR OPEN U LOGPAGES:2927851 ON TAKEOFF RECEIVED L/G DOOR NOT CLOSED ECAM/CAUTION. NOSE GEAR. COMPLIED WITH ECAM/QRH. NO WIND NOISE FROM HANGING GEAR DOORS. NO INCREASED FUEL BURN NOTED. ALL LDG GEAR INDICATED UP & SDR FDEA2019121323231Skin · damagedPOSSIBLE TRAPPED WATER FOUND USING THERMOGRAPHIC INSPECTION 4" FORWARD OF TRAILING EDGE IN AREA 2. MARKED. LEFT SIDE ELEVATOR. REMOVED AND REPLACED L/H ELEVATOR IAW A300-600 AMM 27-31-24-04, FUNCTION CHECK OF ELEVATOR MECHANICAL CONTROL AND PITCH UNCOUPLSDR FDEA2019121323226Skin · gougedEXTERIOR FUSELAGE AT THE LOWER FWD EDGE OF THE AFT CARGO DOOR CUTOUT HAS A CLUSTER OF GOUGES SPANNING APPROX 15" (VIEWED WITH THE CARGO DOOR OPEN) REPAIRED AFT CARGO DOOR CUTOUT IAW A300-600 SRM 53-17-12 FIG 201SDR FDEA2019121313223Floorboard · damagedFLOORBOARD PANEL 252XG REQUIRES FABRICATION FAB NEW PANEL AND APPLIED TOPCOAT IAW FEDEX SRZ 25-005 REV R AND A300-600 AMM 51- 75-10, AND PART MARKED FLOOR PANEL PER FEDEX GMM 07-0-1000, 7.B. (2) AND (6)SDR FDEA2019121313222Skin · chafedR/H WING INBD FLAP LWR L/E SURFACE HAS 2EA GOUGES AT THE INBD HINGE WHERE THE AERODYNAMIC COVER PANEL MAKES CONTACT (INBD AND OTBD OF THE LUG FITTINGS) REPAIRED R/H WING INBD LWR L/E SURFACE AT THE INBD HINGE WHERE THE AERODYNAMIC COVER PANEL MAKES CONTACTSDR FDEA2019120653185Bracket · chafed#2 PYLON IB BRACKET AT RIB 20 IS CHAFED THROUGH MATERIAL ACCOMPLISHED REPAIR AT #2 PYLON INBOARD AFT UPPER SPAR WEB IAW FEDEX EA: 6-5450- T0350874 T0350874-P1. TITLED: NACELLES/PYLON - WING PYLON/STRUT - NO. 2 PYLON INBOARD AFT UPPER SPAR WEB.SDR FDEA201912043176Actuator · damagedHORIZONTAL STAB JACK SCREW HAS DAMAGED THREADS AT LOWER END COMPLIED WITH EA # 6-2740-T0350478, FLIGHT CONTROL-H.STAB / SPEED TRIM - THS JACKSCREW, LOWER THREADS, GOUGE * THIS EA DEVIATES FROM EO 6-2740-7-5001.SDR FDEA2019120433167Structure · crackedRH PYLON TOP AFT SECTION I/B METAL STRIP CRACKED REPLACED STRIP P/N A5451532700103 ON R/H PYLON TOP AFT SECTION I/B SIDE IAW A300-600 SRM 51-40-21 AND AIRBUS DWG A54515326 ISSUE ESDR FDEA201912013158Stringer · corrodedFWD PIT BETWEEN FR 38.2 AND FR 39 STR 43R CORRODED REPAIRED STRINGER 43R BETWEEN FR38.2 AND FR39 IAW A300-600 SRM 53-10-14 FIG 208SDR FDEA201911273123Attach Angle · corrodedL/H WHEEL WELL, PRESSURE DECK ATTACH ANGLE @ FR47 LBL80 IS EXFOLIATED REMOVED AND REPLACED PRESSURE DECK ATTACH ANGLE IAW AIRBUS DWG A57130516, ISSUE C, AIRBUS DWG A57111104, ISSUE M AND A300-600 SRM 51-49-00.SDR FDEA201911263119Skin · gouged#1 ENG O/B CORECOWL AFT UPPER CHAFE STRIP GOUGED REMOVED AND REPLACED ATTACH BRACKET AND WEARSTRIP PER ROHR SRM 54-04-01, AND EA# 6-7110-T0351046 P1. TITLED: POWER PLANT - WING ENG COWL - #1 ENG OUTBD CORE COWL, WEAR PLATE SUPPORT, CHAFED.SDR FDEA2019112613021Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 152RF DAMAGED FAB NEW AFT CARGO FLOOR PANEL 152RF IAW A300-600 SRZ 25-005 REV R, RESTORED FINISH SRM 51-75- 10, PART MARKED GMM 07 10, PART MARKED GMM 07-0-1000SDR FDEA2019112213025Hinge · crackedRH PYLON TOP O/B METAL SEAL I/B T/R HINGE PANEL CRACKED REMOVED, REPAIRED, AND REINSTALLED #2 PYLON O/B EXTRUSION EDGING IAW AIRBUS DWG A54612094, ISSUE D AND A300-600 SRM 54-56-10, CONFIG-1, FIGURE 201. FEDEX EA: 6-5450-T0350729 P1. NACELLES/PYLONS - PYSDR FDEA2019112213023Skate Angle · cracked#1 PYLON BELLOW PANEL#411DL T/R SUPPORT SKATE ANGLE CRACK. REMOVED, REPAIRED, AND REINSTALLED #1 PYLON SUPPORT SKATE ANLGE EDGING IAW A300-600 DWG# A54612094 ISSUE D. FEDEX EA# 6-5450-T0350728 P1. NACELLES/PYLONS - PYLON FILLETS/ FAIRINGS PYLON FILLETSSDR FDEA2019112213020Floor Panel · damagedAFT CARGO COMPARTMENT L/H FLOOR PANEL 151TF DAMAGED FAB NEW AFT CARGO L/H FLOOR PANEL 151TF IAW A300-600 SRZ 25-005 REV R, RESTORED FINISH SRM 51- 75 75-10, PART MARK GMM 07-0-1000SDR FDEA2019112213019Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 152QF DAMAGED FAB NEW AFT CARGO FLOOR PANEL 152QF IAW A300-600 SRZ 25-005 REV R, RESTORED FINISH SRM 51-75- 10, PART MARKED GMM 07-0-1000SDR FDEA2019112203016Floorbeam · crackedMAIN CABIN FLOORBOARD CROSSBEAM LOCATED AT FRAME 44 BETWEEN SEAT TRACKS 3R AND 4R HAS A CRACK AND ELONGATED FASTENER HOLES (PARTS RACK) FABRICATED NEW CROSSBEAM PER FEDEX EA 6-5310-T0350590 & AIRBUS DWG A53812970 ISSUE A, 6-5310-T0350590-P1 FUSELAGE - MAINSDR FDEA2019112203015Seat Track · wornMAIN CABIN SEAT TRACK 3R (-Y953) HAS WORN SCALLOPS LOCATED AT FRAME 44 REMOVED AND REPLACED SEAT TRACK 3R PER A300-600 DWG: A538-13684, ISSUE E, AND, A300-600 SRM 51-40-21.SDR FDEA2019112203014Seat Track · crackedINBOARD SPLICE ANGLE CRACKED ON SEAT TRACK -Y953 (3R) BETWEEN FRAMES 44 - 45 FABRICATED NEW SPLICE ANGLE AND REMOVED & REPLACED W/ NEW SPLICE ANGLE PER A300-600 DWG: A538-13684, ISSUE E, AND, A300-600 SRM 51-40-21SDR FDEA201911192996Blowout Panel · gouged#1 ENGINE, INBOARD THRUST REVERSER, HINGE LATCH PANEL, UPPER FACE GOUGED 2 SPOTS REMOVED AND REPLACED BLOW OUT DOOR ASSY IAW MRAS CMM 78-32-00, FIG 703. EXHAUST SYSTEM - THRUST REVERSER GEN - #1 ENGINE I/B T/R HINGE LATCH PANEL - FASTENER. FASTENER.SDR FDEA2019111982986Floorboard · delaminatedMAIN CABIN FLOORBOARD 222RF IS DELAMED FABRICATED NEW FLOORBOARD 222 RF IAW FEDEX DWG SRZ-25-005 REV.R AND PART MARKED IAW GMM 07-0-1000 7.B (2) AND (6)SDR FDEA2019111982985Floorboard · damagedMAIN CABIN FLOORBOARD 232 TG IS DAMAGED FABRICATED NEW FLOOR PANEL 232 TG IAW FEDEX DWG SRZ-25-005 REV. R AND PART MARKED IAW FEDEX GMM 07-0-1000 7.B.(2) AND (6)SDR FDEA2019111982984Floorboard · damagedMAIN CABIN FLOORBOARD 232YG IS DAMAGED FABRICATED NEW FLOORBOARD 232 YG IAW FEDEX DWG SRZ-25-005 REV.R AND PART MARKED IAW GMM 07-0-1000 7.B. (2) AND (6)SDR FDEA2019111982983Floorboard · damagedMAIN CABIN FLOORBOARD 231 YG IS DAMAGED FABRICATED NEW FLOORBOARD 231 YG IAW FEDWX DWG SRZ-25-005 REV. R AND PART MARKED IAW GMM 07-0-1000 7.B. (2) AND (6)SDR FDEA2019111982982Floorboard · damagedMAIN CABIN FLOORBOARD 242QJ IS DAMAGED FABRICATED NEW FLOOR PANEL 242 QJ IAW FEDEX DWG SRZ-25-005 REV.R. AND GMM 07-0- 1000 7.B. (2) AND (6)SDR FDEA2019111982981Floorboard · damagedMAIN CABIN FLOORBOARD 241TH IS DAMAGED FABRICATED NEW FLOOR PANEL 241 TH IAW FEDEX DWG SRZ-25-005 REV.R AND GMM 07-0- 1000 7.B. (2) AND (6)SDR FDEA2019111982980Floorboard · crackedMAIN CABIN FLOORBOARD 241RG IS CRACKED FABRICATED NEW FLOOR PANEL 241 RG IAW FEDEX DWG SRZ-25-005 REV. R AND GMM 07-0- 1000 7.B. (2) AND (6)SDR FDEA2019111982979Floorbeam · corrodedAFT CARGO COMPARTMENT @ FRAME 63 FRAME CORRODED UNDER FASTENER REPAIRED T-CAP IAW A300-600 SRM 53-10-15 FIG 208SDR FDEA2019111542958Floorboard · damagedMAIN CABIN FLOORBOARD 241AJ IS DAMAGED FABRICATED NEW FLOORBOARD 241AJ IAW FEDEX DWG SRZ-25-005 REV.R AND PART MARKED IAW GMM 07-0-1000 7.B. (2) & (6)SDR FDEA2019111542957Floorboard · damagedMAIN CABIN FLOORBOARD 252YG IS DAMAGED FABRICATED NEW FLOORBOARD 252YG IAW FEDEX DWG SRZ-25-005 REV.R AND PART MARKED IAW GMM 07-0-1000 7.B. (2) & (6)SDR FDEA2019111542956Floorboard · crackedMAIN CABIN FLOORBOARD 251GF IS CRACKED FABRICATED NEW FLOORBOARD 251GF IAW FEDEX DWG SRZ-25-005 REV.R AND PART MARKED IAW GMM 07-0-1000 7.B.(2) & (6)SDR FDEA2019111532947Floorboard · damagedMAIN CABIN FLOORBOARD 241QJ IS DAMAGED FABRICATED NEW FLOOR PANEL IAW FEDEX DWG SRZ-25-005 REV.R AND GMM 07-0-1000 7.B. (2) & (6)SDR FDEA2019111532946Floorboard · damagedMAIN CABIN FLOORBOARD 242UJ IS DAMAGED FABRICATED NEW FLOOR PANEL IAW FEDEX DWG SRZ-25-005 REV. R AND GMM 07-0-1000 7.B. (2) AND (6)SDR FDEA2019111532945Floorboard · damagedMAIN CABIN FLOORBOARD 252UH IS DAMAGED FABRICATED NEW FLOOR PANEL 252UH IAW FEDEX DWG SRZ-25-005 REV. R AND GMM 07-0- 1000 7.B. (2) AND (6)SDR FDEA2019111522933Floorboard · delaminatedFLOORBOARD 261AH IS DELAMED FABRICATED NEW FLOORBOARD 261AH IAW FEDEX DWG SRZ-25-005 REV. R AND PART MARKED IAW GMM 07-0-1000 7.B. (2) & (6)SDR FDEA2019111522932Floorboard · damagedMAIN CABIN FLOORBOARD 242BF IS DAMAGED FABRICATED NEW FLOORBOARD 242BF IAW FEDEX DWG SRZ-25-005 REV. R AND PART MARKED IAW GMM 07-0-1000 7.B. (2) & (6)SDR FDEA2019111522931Floorboard · crackedMAIN CABIN FLOORBOARD 241NJ IS CRACKED FABRICATED NEW FLOORBOARD 241NJ IAW FEDEX DWG SRZ-25-005 REV. R AND PARTMARKED IAW GMM 07-0-1000 7.B. (2) & (6)SDR FDEA2019111522930Floorboard · crackedMAIN CABIN FLOORBOARD 251RG IS CRACKED FABRICATED NEW FLOORBOARD 251RG IAW FEDEX DWG SRZ-25-005 REV. R AND PART MARKED IAW GMM 07-0-1000 7.B. (2) & (6)SDR FDEA2019111522929Floorboard · damagedMAIN CABIN FLOORBOARD 242ZJ IS DAMAGED FABRICATED NEW FLOORBOARD 242ZJ IAW FEDEX DWG SRZ-25-005 REV. R AND PART MARKED IAW GMM 07-0-1000 7.B. (2) & (6)SDR FDEA2019111522928Floorboard · damagedMAIN CABIN FLOORBOARD 242EK IS DAMAGED FABRICATED NEW FLOORBOARD 242EK IAW FEDEX DWG. SRZ-25-005 REV. R AND PART MARKED IAW GMM 07-0-1000 7.B. (2) & (6)
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