N677FE
Service difficulty reports · 275
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 = 'N677FE' 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 = 'N677FE' 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 FDEA202609171360Gfi · failedAUTO FUEL FEED FAULTED. USED QRH PROCEDURES TO RESET SYS. NR 2 PUMP FAULTED & WOULD NOT RESET. NR 1 INNER TANK PUMP DEFERRED, LEAVING NO OPERATING PUMP IN RT TANK & APPROX 25,000 POUNDS IN RT TANK UNUSABLE. DECLARED EMERGENCY & TRIED TO ESTABLISH A WAY TO BURNSDR FDEA202504180734Fork · wornRUDDER #2 HINGE ARM BEARING PLAY. REPLACED THE HINGE ARM FORK END ASSY WITH NEW. I.A.W A300-600F SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6~7, PAGE.7B~50. THE REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100. AT RUDDER #2 HINGE ARM.SDR FDEA202504180699Web · bentTHE WEB DEFORM NEAR FR86 S-L33. REPLACED THE DAMAGE STRAP AND WEB WITH NEW PARTS ON FR86, S-33L. I.A.W A300-600F SRM 51-40-21-001, PARA.6, PAGE.7B~PAGE.23 AND 51-72-10-001, PAGE.2. THIS REPAIR IS CLISSIFIED AS MINOR PER GMM 6-2-100.SDR FDEA202504180695Web · bentTHE WEB DEFORM NEAR FR86 S-R33 REPLACED THE WEB AND STRAP WITH NEW PARTS AT FR86~87, STGR33R I.A.W A300-600F SRM 51- 72-10-001, PAGE.2 & 51-40-21-001, PARA.6~7, PAGE.7B~50. THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR FDEA202504180660Floorbeam · corrodedMAIN DECK FLOOR FOUND FLOOR BEAM CORROSION AT FR12A PLUS 16" Y740 REPLACED THE DAMAGE SUPPORT BY NEW ONE WITH RIVETS I.A.W. A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA .6, PAGE,7B~PAGE,23.THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT MAISDR FDEA202504180639Skin · damagedFOUND TWO BURN MARK NEAR RUDDER TOP SIDE TE AND PNL 326AT. PERFORM REPAIR OF APEX STRIP BY NEW STRIP SECTION AND CONNECTION PLATES WITH RIVETS AT NEAR RUDDER TOP SIDE TE AND PNL 326AT AREA I.A.W A300-600F SRM 55-41-12-201, PARA.13, PAGE.237~PAGE.239, FIG.2SDR FDEA202504170722Fitting · damagedREPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER EO NO:E6- 5230-E0378588 B P5 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR23, LONGN1~LONGN3. I.A.W FEDEX EO NO: E6-5230-E0378588 B P5, SEQ NO:963, TITLE: DOORSDR FDEA202504160712Rib · wornRH WING #5 SPOILER O/B JACK RIB UPPER BORE GOT ABRASION ACCOMPLISHED THE REPAIR WITH BUSH, REINFORCING PLATE AND PACKING PLATE AT RH WING #5 SPOILER O/B JACK RIB UPPER BORE ABX184.625 I.A.W EA NO:T6-5740-T0383103 P1, SEQ NO:1060, TITLE:WING-ATTACH FITTINGSSDR FDEA202504150667Seat Track · gougedMAIN DECK FLOOR SEAT TRACK CROWN GOUGE AT FR66 PLUS 11" Y1456 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR66~FR68, Y1456. I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203~208. THIS REPAIR CLASSIFIED AS MAJOR CAT.A PSDR FDEA202504150662Seat Track · gougedMAIN DECK FLOOR SEAT TRACK CROWN GOUGE AT FR66 PLUS 11" Y-450 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR65~FR68, Y-450. I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203~208. THIS REPAIR CLASSIFIED AS MAJOR CAT.A PSDR FDEA202504150625Seat Track · wornMAIN DECK FLOOR SEAT TRACK CROWN GOUGE AT FR57.3 PLUS 2" Y1456 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK AT FR56~FR59, Y1456, I.A.W A300-600F SRM 53-10-16-201 PARA.4 FIG 201,PAGE 203~208 . THIS REPAIR CLASSIFIED AS MAJOR CAT.ASDR FDEA202504140661Seat Track · gougedMAIN DECK FLOOR SEAT TRACK CROWN GOUGE AT FR57.1 PLUS 3" Y-1959 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR57~57.2, Y-1959. I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203~208. THIS REPAIR CLASSIFIED AS MAJOR CAT.SDR FDEA202504140626Seat Track · wornMAIN DECK FLOOR SEAT TRACK CROWN GOUGE AT FR60 PLUS 9" Y953 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK AT FR58~FR61, Y953, I.A.W A300-600F SRM 53-10-16-201 PARA.4 FIG 201,PAGE 203~208 . THIS REPAIR CLASSIFIED AS MAJOR CAT.A PERSDR FDEA202504130637Shear Web · damagedMAIN DECK FLOOR SHEAR WEB BROKEN AT FR77 Y-1897 REMOVED DAMAGED SHEAR WEB AND INSTALLED NEW SHEAR WEB. I.A.W A300-600F SRM 51-72- 10-001, PAGE2 AND 51-40-21-001, PARA6 PAGE 7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT MAIN DECK FLOOR FR77, Y-18SDR FDEA202504120747Crossbeam · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING REPAIR FOUND ON MDCC CROSSBEAM AT FR31, -Y450~-Y953 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, SDR FDEA202504120746Crossbeam · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING REPAIR FOUND ON MDCC CROSSBEAM AT FR29, -Y450~-Y953 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707SDR FDEA202504120742Crossbeam · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING REPAIR FOUND ON MDCC CROSSBEAM AT FR30, - Y450~-Y953 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707SDR FDEA202504120658Floor Support · crackedMAIN DECK FLOOR SUPPORT CRACK APPROX 3/4" AT FR38.1 PLUS 16" Y2602 REPLACED THE SUPPORT WITH NEW PART AND FASTENERS AT MAIN DECK FR38.1 PLUS 16", Y2602. I.A.W A300-600F SRM 51-40-21-001, PARA.7, PAGE.24~50 AND 51-72-10-001, PAGE.2. THE REPAIR CLASSIFIED ASSDR FDEA202504120653Skin · corrodedAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH O/B FLAP UPR SKIN AT RIB27,T/E-2" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR SDR FDEA202504120643Skin · dentedAIRCRAFT REPAIR ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON LH O/B FLAP L/E NOSE BTW RIB14~RIB18 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 1SDR FDEA202504110705Plate · crackedFWD CGO COMP'T LH SIDE PLATE CRACK BETWEEN FR21~FR22 S-43L POSITION. REPLACED THE CRACK PLATE WITH NEW PART AT FWD CARGO COMP'T LH SIDE BETWEEN FR21 TO FR22 , S-43L IAW A300-600F SRM 51-40-21-001 , PARA.6 , PAGE7B~PAGE23. THIS REPAIR IS CLASSIFIED AS MINORSDR FDEA202504110655Skin · damaged2EA WATER TRAPPED AREA (65MMX35MM)(75MMX40MM) WERE FOUND AT LH ELEVATOR TOP SKIN PANEL T/E FASTENER NO.10 AND NO.37. *COUNTING FASTENER FROM I/B TO O/B*. ACCOMPLISHED THE COMPOSITE REPAIR AT LH ELEVATOR TOP SKIN PANEL T/E FASTENER NO.10 AND NO.37 I.A.W A30SDR FDEA202504100618Skin · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER13 PLUS 29.5", T/E-24" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIRSDR FDEA202504100617Skin · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER13 PLUS 28", T/E-18" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMSDR FDEA202504100614Skin · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER2 PLUS 14.5", T/E-12.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUISDR FDEA202504100613Skin · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER2 PLUS 9", T/E-11" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENSDR FDEA202504100612Skin · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR UPR SKIN AT ER2 PLUS 26.5", T/E-29" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIRESDR FDEA202504100611Skin · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR UPR SKIN AT ER2 PLUS 12", T/E-47.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIRESDR FDEA202504100610Skin · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR UPR SKIN AT ER2 PLUS 15", T/E-21" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMESDR FDEA202504090735Attach Fitting · cracked1EA CRACK WAS FOUND AT FWD CARGO DOOR ACTUATOR ATTACH FITTING. ACCOMPLISHED THE REPLACEMENT OF FRAME HEAD AND PERFORMED TRIM OUT ON INNER SKINS AND ANGLE PROFILE AT FWD CARGO DOOR FR22A, BEAM1~3. I.A.W FEDEX EA NO:T6-5230- T0383047 P1, SEQ NO:1070, TITLE:DOSDR FDEA202504080723Fitting · crackedTHE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING WAS FOUND CRACK AT FRAME 24 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR24, LONGN1~LONGN3. I.A.W FEDEX EO NO: E6-5230-E0378588 B P5, SEQ NO:963, TITLE: DOORS - CARGO DOOR/HYD SSDR FDEA202403190315Warning Light · false indicationL1 AND R1 DOOR CABIN AND MAIN CARGO PRESSURE LIGHTS ARE ILLUMINATED ON THE GROUND WITH 0 PSID AND CABIN AT FIELD ELEVATION. RESET GROUND POWER, LIGHTS CLEARED, NO WARNINGS. CABIN PRESSURE CONTROL AND MONITORING ADJUSTMENT/TEST CARRIED OUT IAW 21-31-00-05 WSDR FDEA202401190192Gcu · failedDURING DECENT AC BUS 1 FAILURE. COMPLIED WITH ECAM AND QRH. EMERGENCY DECLARED. REMOVED AND REPLACED NR 1 GCU PER 24-22-12-04. OPS CHECK STILL REQUIRED.PERFORMED #1 IDG SERVICING PER 12-13-24 AMM: 24-22-12-04. PERFORMED ENGINE RUN PER A300 JRH AND OPSDR FDEA202303070384Spoiler · delaminatedLH WING 4# SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE & CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATED (1) (S:10MM*15MM D:1.52MM) (2) (S:10MM*15MM D:1.52MM) REPAIRED LH WING 4# SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE DELAMINATION & CENSDR FDEA202303070383Spoiler · delaminatedRH WING #3 SPOILER I/B CENTER HINGE ARM O/B FOUND DELAMINATION. SIZE: 10MM*18MM , DEPTH: 1.59MM. REPAIRED THE RH WING #3 SPOILER I/B CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION PER FEDEX EA: 6-5750-T0373206 P1 & SB A300-57-6082 R03 FIGURE 2 SHEET 2 & 4 SDR FDEA202303050378Seat Track · corrodedMDCC SEAT TRACK -Y953 CORRODED AT FR54.2 - FR54.3. REPAIRED THE MDCC CORRODED SEAT TRACK -Y953 AT FR54.2 - FR54.3 PER A300-600F SRM53-10- 16-201 FIGURE 201. THIS REPAIR IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.SDR FDEA202303030362Crossbeam · crackedMDCC CROSS BEAM FOUND CRACKED AT FR64 Y1456 - Y1959 REPAIRED THE MDCC CRACKED CROSSBEAM AT FR64 Y1456~Y1959 PER A300-600F SRM51-40-21 & SRM53-10-15-201 PARA.14. THIS REPAIR IS CAT A REPAIR.MAJOR REPAIR IAW FEDEX GMM6-2-100.SDR FDEA202303030361Crossbeam · crackedMDCC CROSS BEAM FOUND CRACKED AT FR32 -Y450 ~ -Y953 REPAIRED THE MDCC CRACKED CROSS BEAM AT FR32 -Y450 ~ -Y953 PER A300-600F SRM53-10-15- 201 PARA.15 & FEDEX EA: 6-5310-T0373225 P1. EA TITLE: FUSELAGE - MAINFRAME - CRACK AT STIFFENER OF FR32 CROSSBEAM BETWESDR FDEA202303030360Crossbeam · crackedMDCC CROSS BEAM FOUND CRACKED AT FR38.2 Y1456 - Y1959 REPAIRED THE MDCC CRACKED CROSS BEAM AT FR38.2 Y1456 ~ Y1959 PER A300-600F SRM53-10- 15-201 PARA. 15 & FEDEX EA: 6-5310-T0373226 P1. EA TITLE: FUSELAGE - MAINFRAME - CRACK AT STIFFENER OF FR38.2 CROSSBEASDR FDEA202301070047Smoke Detector · false activationAT FL370 GOT AFT BULK CARGO SMOKE INDICATION ON ECAM. COMPLIED WITH ECAM AND QRH. AFTER INITIAL INDICATION GOT ANOTHER MASTER WARNING AND ECAM INDICATION APPROXIMATELY 7-8 MINUTES LATER. REMOVED AND REPLACED (9WH, 10WH, 11WH, 44 WH) SMOKE DETECTORS IAW ASDR FDEA202212162926Smoke Detector · false indicationAT CRUISE 33,000, RECEIVED A SMOKE INDICATION FOR THE AFT BULK BAY. FOLLOWED ECAM & QRH. DISCHARGED AGENT 1. INDICATION WENT AWAY AFTER. PERFORMED LOWER CARGO SMOKE DET ADJ/TEST IAW AMM. ALL INDICATIONS NORMAL. PERFORMED GVI OF LOWER AFT CARGO & BULK BAY FOSDR FDEA202211142783Mount · corroded#1 ENG PYLON SIDE OF FWD ENG MOUNT HAS PITTING ON LOWER SURFACE. ORIG SUB DATE: 11/14/2022SDR FDEA202211142782Mount · damaged#1 ENG, FWD MOUNT, AFT OUTBOARD HOLE HAS CORROSION ON THE TOP COUNTERBORE. COMPLIED WITH E.A.#: 6-5451-T0371499 (P1) PYLON STRUCTURE - TAIL PYLON/STRUT - #1 ENGINE FWD MOUNT AFT TENSION BOLT HOLES WITH CORROSION AND NICKS ON BOTTOM SURFACE OF MOUNT COMMSDR FDEA202211142781Mount · corroded#1 ENG, FWD MOUNT, AFT INBD HOLE HAS CORROSION ON TOP COUNTERBORE. 0003684179 : CODY BACKUS CRB - 12-NOV-2022 20:49 COMPLIED WITH E.A.#: 6-5451-T0371499 (P1) PYLON STRUCTURE - TAIL PYLON/STRUT - #1 ENGINE FWD MOUNT AFT TENSION BOLT HOLES WITH CORROSION ANSDR FDEA202211142780Mount · corroded#1 ENGINE PYLON FWD MOUNT AFT OUTBOARD BOLT HOLE PITTED 0000265104 : ARMSTRONG, BERNARD L - 03-NOV-2022 01:25 REPAIRED #1 ENGINE PYLON FWD MOUNT AFT OUTBOARD BOLT HOLE PER AIRBUS SRM 54-51-81. 0003655255 : LEGGETT, JACOB A - 12-NOV-2022 21:37 COMPLIED WITH SDR FDEA202211142779Mount · corroded#1 ENGINE PYLON FWD MOUNT AFT INBOARD BOLT HOLE PITTED. REPAIRED #1 ENGINE PYLON FWD MOUNT AFT INBOARD BOLT HOLE PER AIRBUS SRM 54-51-81. COMPLIED WITH E.A. # 6-5451-T0371499 (P2) TITLE: PYLON STRUCTURE-TAIL PYLON/STRUT-#1 ENGINE FWD MOUNT AFT TENSION BOLSDR FDEA202107281880Autothrottle Sys · malfunctionedON TAKEOFF (NON-PROFILE, AUTOTHROTTLES OFF PER MEL) THROTTLES SPLIT ONE KNOB LENGTH AFTER GEAR RETRACTION. TAKE OFF POWER WAS SET AT 101.5 N1 ON BOTH ENGINES. HOWEVER, SOMETIME AFTER ROTATION, THE NUMBER 2 ENGINE INCREASED TO 108.5 N1 DESPITE AUTOTHROTTLES SDR FDEA202107271881Autothrottle Sys · malfunctionedAFTER GEAR RETRACTION, AUTO THROTTLE SYSTEM COMMANDED #1 ENGINE TO REDUCE POWER BY 3-5% OF SELECTED FLX TRP VALUE. THE #1 THROTTLE WAS SPLIT BY A KNOB WIDTH FROM THE #2 THROTTLE. TRP FLX VALUE REMAIN UNCHANGED FROM BEING SET ON THE GROUND.ONCE THE THROTTLES SDR FDEA202105051135Adc · failedIN CRUISE THE FO S ALTIMETER IS 300 FEET OFF CAPTAIN S ALTIMETER AND 200 FEET OFF THE STANDBY ALTIMETER . PERFORMED PITOT/STATIC ADJ/TEST PER A300 AMM 34-10-00-5. FOUND F/O ALT READING SPLIT FROM CAPTIANS AND STANDBY. R/R'D #2 ADC PER A300 AMM 34-11-34-04. SDR FDEA202102040291Reservoir · failedON APPROACH INTO KMEM RECEIVED ECAM ALERT GREEN HYD RSVR LO LEVEL ALERT. CONFIRMED LOW QUANTITY ON HYDRAULIC GAUGE AND ON ECAM SYSTEM DISPLAY. COMPLIED WITH ECAM AND QRH PROCEDURES, DECLARED EMERGENCY, LANDED SAFELY ON RUNWAY 36C. NO NOTICEABLE HYDRAULI
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