N684FE

Service difficulty reports · 190

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 = 'N684FE' 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 FDEA201003311042Floorbeam · crackedAFT CARGO FR 64 UPPER FLOORBEAM BETWEEN 4L & 5L IS CRACKED ON AFT SIDE. REMOVED DAMAGE ON AFT CARGO FR 64 UPPER FLOORBEAM BETWEEN 4L & 5L AFT SIDE CHEM MILL, FABRICATED, DRILLED AND INSTALLED REPAIR CHANNEL IAW FREIGHTER SRM 53-10-15 FIG 21. REMOVED AND REINMar 31, 2010 · N684FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201003311041Floorbeam · crackedFWD CARGO FRAME 30 UPPER FLOORBEAM BETWEEN S/T 2R AND 3R IS CRACKED ON FWD SIDE. PERFORMED CROSSBEAM REPAIR AT FWD FACE OF FLOORBEAM FRAME 30 BETWEEN SEAT TRACK 2R AND 3R BY REMOVING DAMAGE, FABRICATING, LOCATING AND DRILLING A FILLER AND REPAIR CHANNEL AND INMar 31, 2010 · N684FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201003301030Floorbeam · crackedAFT CARGO PIT FLOORBEAM FR 58 BETWEEN SEAT TRACK 2&3 RT CRACK, PREVIOUS REPAIR IN AREA WITH 1EA HYLOCK COLLARS MISSING & 1 EA COLLAR BROKEN. R & R CROSSBEAM SECTION AT FR 58. INSTALLED 4 EA REPAIR COUPLING AND 4 EA COUPLING STRAPS IAW SRM 53-10-15 FIG 207.Mar 30, 2010 · N684FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201003281022Skin · bentFWD CARGO DOOR EXTERIOR SKIN AT FWD CORNER HAS 3" AREA OF SKIN BENT INTO WIND DAMAGE CLASSIFIED OUT OF LIMITS IAW SRM 52-30-00. REPAIRED DOOR SKINS IAW SRM 52-31-00, FIG 203 BY INSTALLING DOUBLER AND FILLER TO TOP SKIN.Mar 28, 2010 · N684FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201003250990Floorbeam · crackedFWD CARGO FR 31 UPPER FLOORBEAM BETWEEN 2R AND 3R CRACKED ON FWD SIDE CHEM MILL. ROUTED OUT CRACK, INSTALLED FILLER CHANNEL, APPLIED PROTECTIVE COATING IAW SRM 53-10-15, FIG 212.Mar 25, 2010 · N684FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201003250989Seat Track · wornSEAT TRACK 3L HAS (2 EA) BROKEN SCALLOPS LOCATED 2 IN AFT OF FRAME 59, REMOVED DAMAGED SEAT TRACK. FABRICATED NEW SEAT TRACK AND SPLICE. REPROTECTED ALL PARTS IAW A300 FREIGHTER SRM 53-10-16 FIG 201.Mar 25, 2010 · N684FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903050851Smoke Detector · inoperativeAFTER START GOT ECAM INDICATION FAULT ON MAIN DECK RIGHT AFT CARGO SMOKE DETECTION SYSTEM AND FAULT LIGHT ON OVERHEAD PANEL. CLEARED ITSELF AFTER 2-3 MINUTES. THEN COME ON AGAIN DURING T/O ROLL AT 30-40KIAS. ABORTED T/O. FAULT LIGHT WENT AWAY. RETURNED TOMar 5, 2009 · N684FE · Airbus A300F4605R · Smoke DetectionSDR 08FDEA00819Attach Angle · cracked2ND INBD LEADING EDGE SECTION ON THE RT HORIZONTAL STABILIZER; "UPPER OUTBD ATTACH ANGLE" IS CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-31-01 VOL II PG 1. FORMED NEW ANGEL IAW DWG ALC 07052 REV G. LOCATED; DRILLED & DEBURRED NEW ANGLE IAW SRM 51-31-01 VOL II PMar 10, 2008 · N684FE · Airbus A300F4605R · Horizontal Stabilizer StructureSDR 08FDEA00647Escape Rope · noneF/O ESCAPE ROPE IS STILL IN THE PLASTIC PACKAGING. REMOVED PLASTIC PACKAGING AS REQUIRED. REF FEDEX STANDARD MAINTENANCE PRACTICES.Feb 28, 2008 · N684FE · Airbus A300F4605R · Emergency EquipmentSDR 08FDEA00616Frame · damagedCOCKPIT WINDSHIELD CENTER FRAME EXTERIOR, 2ND BOLT HOLE FROM THE BOTTOM IS ELONGATED. COMPLIED WITH EA NR 6-5310-113036 PART 1.Feb 26, 2008 · N684FE · Airbus A300F4605R · Fuselage Main, FrameSDR 08FDEA00602Skin Panel · crackedNR 1 INBD T/R UPPER FWD SKIN PANEL IS CRACKED. REMOVED DAMAGED SKIN PANEL IAW A300-600 SRM 51-40-21. FABRICATED NEW PANEL IAW A300-600 SRM 51-26-00 AND 51-40-40 AND PER FEDEX GMM N7-0-1001. INSTALLED NEW PANEL IAW A300-600 SRM 51-40-21.Feb 25, 2008 · N684FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA00505Floorboard · crackedMAIN CABIN FLOOR PANEL NR 242EK IS CRACKED. FABRICATED NEW FLOOR PNL NR 242EK IAW FEDEX DWG SRZ 25-005 REV F FOR INSTALLATION, SEE W/C 62C0702. MAJOR REPAIR.Feb 18, 2008 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA00504Floorboard · crackedMAIN CABIN FLOOR PANEL NR 242 RG IS CRACKED. FABRICATED NEW FLOORBOARD PNL NR 242RG IAW FEDEX DWG SRZ 25-005 REV F FOR INSTALLATION SEE W/C 62C0702.Feb 18, 2008 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA00503Floorboard · crackedMAIN CABIN FLOOR PANEL 242 ZJ IS CRACKED. FABRICATED NEW FLOOR BOARD PNL NR 242ZJ IAW FEDEX DWG SRZ 25-005 REV F FOR INSTALLATION SEE W/C 62C0702.Feb 18, 2008 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA00507Fairing · damagedNR 1 PYLON LOWER FAIRING FWD LT ATTACH HOLES ARE ELONGATED. REMOVED SKIN PER SRM 51-40-21 PARA 6 & 7 DUE TO FASTENER HOLES ELONGATED BEYOND LIMITS PER SRM 54-55-51. FABRICATED UPPER LONGERON REPAIR SECTION & SPLICE PER SRM 54-55-51, FIG 207. ALODINED AFeb 18, 2008 · N684FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA00506Floorboard · damagedMAIN CABIN FLOOR PNL 232 YG IS CRUSHED. FABRICATED NEW FLOOR BOARD PNL NR 232 YG IAW FEDEX DWG SRZ 25-005 REV F. FOR INSTALLATION SEE W/C 62C0701.Feb 18, 2008 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA00502Floorboard · crackedMAIN CABIN FLOOR BOARD 242UJ IS CRACKED. FABRICATED NEW FLOOR BOARD PNL NR 242UJ IAW FEDEX DWG SRZ 25-005 REV F. FOR INSTALLATION SEE W/C 62C0702.Feb 18, 2008 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA00501Skin · damagedRT WING LOWER O/B PANEL 590 BB HAS SCRATCHES ON THE SKIN AROUND THE CUTOUT, AND ON THE ANGLES INSIDE THE CUTOUT.Feb 18, 2008 · N684FE · Airbus A300F4605R · Wing, Plate/SkinSDR 08FDEA00441Floor Panel · tornMAIN DECK CARGO COMPARTMENT FLOORBOARD (SR30B5327071400200252) VF IS TORN. FABRICATED NEW FLOORBOARD PANEL NR 252 VF IAW SRZ 25-005 REV F.Feb 14, 2008 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA00436Support Angle · crackedAVIONICS COMPARTMENT STRUCTURE UNDER THE COCKPIT FLOOR, INTERCOSTAL AFT SUPPORT ANGLE CRACKED AT THE BEAM ATTACHMENT; BS 972, LBL 39. REMOVED SUPPORT ANGLE IAW SRM 51-40-10 & 51-23-10. FABBED ANGLE IAW SRM 51-40-44 & TPS 1003 REV A. ALODINED, PRIMED & TOFeb 14, 2008 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA00432Intercostal · crackedAVIONICS COMPARTMENT, INTERCOSTAL UNDER THE FLIGHT DECK FLOOR IS CRACKED ON THE AFT END; LOCATED AT BS 972 (FR 10), LBL 39. REMOVED INTERCOSTAL IAW SRM 51-40-21. FABBED NEW WEB IAW DWG 45-A53611975 ISSUE A, TPS 1003 REV A & SRM 51-40-44. ALODINED, PRFeb 14, 2008 · N684FE · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR 08FDEA00434Floor Panel · tornMAIN DECK CARGO COMPARTMENT FLOOR PANEL 252 GF IS TORN. FABRICATED NEW PANEL 252 GF IAW FEDEX SRZ 25-005 REV F.Feb 14, 2008 · N684FE · Airbus A300B4605R · Fuselage Floor PanelSDR 08FDEA00433Floor Panel · crackedMAIN CARGO COMPARTMENT FLOOR PANEL 262NF IS CRACKED. FABRICATED NEW PANEL 262 NF IAW SRZ 25-005 REV F.Feb 14, 2008 · N684FE · Airbus A300B4605R · Fuselage Floor PanelSDR 08FDEA00431Floor Panel · crackedMAIN CARGO FLOOR PANEL 261AH IS CRACKED ACROSS THE LOWER SURFACE. FABRICATED NEW PANEL 261AH IAW SRZ 25-005 REV F.Feb 14, 2008 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA00430Bushing · corrodedAFT CARGO DOOR NR 1 ECCENTRIC BUSHING SUPPORT INNER BORE IS CORRODED. REMOVED AND REPLACED THE AFT CARGO DOOR NR 1 ECCENTRIC BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND A300-600 AMM 52-32-11-5. T/W TWS 8330A. MINOR REPAIR.Feb 14, 2008 · N684FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR 08FDEA00443Floor Panel · tornMAIN DECK CARGO COMPARTMENT FLOOR BOARD 251 XF IS TORN. FABRICATED NEW PANEL NR 251 XF IAW FEDEX SRZ-005 REV F. MAJOR REPAIR.Feb 14, 2008 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA00421Bushing · corrodedAFT CARGO DOOR ECCENTRIC BUSHING SUPPORT INNER BORE CORRODED. REMOVED AND REPLACED AFT CARGO DOOR NR 2 ECCENTRIC BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND AMM 52-32-11-5. T/W TWS 8330A. MINOR REPAIR.Feb 13, 2008 · N684FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR 08FDEA00420Bushing · corrodedAFT CARGO DOOR NR 4 ECCENTRIC BUSHING SUPPORT INNER BORE IS CORRODED. REMOVED AND REPLACED AFT CARGO DOOR NR 4 ECCENTRIC BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND A300-600AMM 52-32-11-5. T/W, TWS8330A.Feb 13, 2008 · N684FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR 08FDEA00419Bushing · corrodedAFT CARGO DOOR NR 5 ECCENTRIC BUSHING SUPPORT INNER BORE IS CORRECTED. REMOVED AND REPLACED AFT CARGO DOOR NR 5 ECCENTRIC BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND A300-600 AMM 52-32-11-5. T/W TWS8330A.Feb 13, 2008 · N684FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR 08FDEA00416Bushing · corrodedAFT CARGO DOOR NR 6 ECCENTRIC BUSHING SUPPORT INNER BORE IS CORRODED. REMOVED AND REPLACED AFT CARGO DOOR NR 6 ECCENTRIC BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND A300-600 AMM 52-32-11-5. T/W TWS8330A. MINOR REPAIR.Feb 13, 2008 · N684FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR 08FDEA00342Skin · gougedAFT CARGO PIT DOOR CUTOUT, FUSELAGE SKIN GOUGED FWD LOWER CORNER OF CUTOUT FR 59A, STR 40-41R. BLENDED GOUGE IAW SRM 51-73-10. FOUND OUT OF LIMITS IAW SRM 51-40-21. REWORKED AREA IAW SRM 53-17-12-101 C-2 FIG. 104. FOUND TO BE WITHIN LIMITS. ALODINED, PRFeb 1, 2008 · N684FE · Airbus A300B4605R · Fuselage Main, Plate/SkinSDR 08FDEA00309Skin · dentedFOUND FUSELAGE EXT SURFACE SKIN DENTED BETWEEN FR 90 AND FR 91, BL 21L. CHECKED DENT LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-12, PAGE 109. CUT OUT DAMAGE AND FABBED 1 EA REPAIR DOUBLER AND FILLER IAW SRM 53-10-12, FIG 255 SHEET 2, PAGES 357-362. IJan 28, 2008 · N684FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 07FDEA05063Transmitter · failedON CLIMB-OUT, ECAM ADVISORY INDICATED NR 1 ENGINE ZERO OIL PRESSURE CONFIRMED WITH GUAGE WHICH INDICATED ZERO AS WELL. COMPLIED WITH QRH. SHUT NR 1 ENGINE DOWN. LANDED IND. REMOVED AND REPLACED NR 1 ENG. OIL PRESSURE TRANSMITTER IAW AMM 79-33-11-4-05. PEDec 14, 2007 · N684FE · Airbus A300F4605R · Engine Oil Indicating SystemSDR 07FDEA00161Unknown · unknownON POWER UP, NO REV UNLK LIGHTS NOTED ECAM. ENG NR 1 R REV PRESSURIZED. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 04FEB07 "MEL 78-30-01-A: ENGINE. NR 1 THRUST REVERSER, INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POJan 25, 2007 · N684FE · Airbus A300F4605R · Engine Thrust ReverserSDR 04FDEA03484Thrust Reverser · malfunctionedREJECTED TAKEOFF AT 80 KIAS AFTER RECEIVING AMBER ECAM REV 2 PRESS MEL 24DEC04. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) 2 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. R&R DPV Dec 24, 2004 · N684FE · Airbus A300F4605R · Engine Thrust ReverserSDR 04FDEA02261Fan · out of balanceIN ROUTE TO TLC CLIMBING TO 350 - PASSING 330, ENGINE ADV NR 2 N1 VIB 3.2, REDUCED POWER, NO CHANGE. CONTACTED MOCC- TROUBLESHOT ACCESSORIES (HYD & GEN), NO CHANGE. AT FL 250 N1 105.6 VIB WAS 2.9, VIBRATION (AIRFRAME) VIB ON DESCENT. AIRFRAME VIB BETWEEN 8Jul 28, 2004 · N684FE · Airbus A300B4605R · Turbine Engine Compressor SectionSDR 04FDEA02262Fan · out of balanceEN ROUTE TO TLC CLIMBING TO 350 - PASSING 330, ENGINE ADV NR 2 N1 VIB 3.2, REDUCED POWER, NO CHANGE. CONTACTED MOCC- TROUBLESHOT ACCESSORIES (HYD & GEN), NO CHANGE. AT FL 250 N1 105.6 VIB WAS 2.9 VIBRATION (AIRFRAME) VIB ON DESCENT. AIRFRAME VIB BETWEEN 80 Jul 28, 2004 · N684FE · Airbus A300B4605R · Turbine Engine Compressor SectionSDR 03FDEA01333Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 58, 24 INCHES RIGHT OF CENTER, IS CRACKED 3 INCHES DOWN FROM TOP APPROX 1 INCH LONG. REPAIRED IAW FEDEX EA 6-5310-72527.Aug 18, 2003 · N684FE · Airbus A300B4605R · Fuselage Main, Floor BeamSDR 02FDEA00920Connector · looseGOT ECAM WARNING, NR 2 ENGINE THRUST REVERSER PRESSURIZED ON TAKEOFF ROLL, BELOW 80 KNOTS. SECURED CONNECTOR PLUGS AND RAN ENGINES, NO ECAM MESSAGE REPEAT.Dec 4, 2002 · N684FE · Airbus A300F4605R · Engine Thrust ReverserSDR 00FDEA00253Speaker · noisyABORTED T/O DUE TO LOUD SQUEAL NOISE IN COCKPIT OF UNDETERMINED ORIGIN (NOT RADIO). RECONFIGURED AC- WND TO NORMAL UNABLE TO DETERMINE SOURCE OF NOISE. INFO NOTED 2ND T/O ROLL NORMAL. UNABLE TO DUP NOISE.Apr 11, 2000 · N684FE · Airbus A300F4605R · UHF Communications System
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