N671FE

Service difficulty reports · 189

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 = 'N671FE' 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 FDEA201002220489Seat Track · damagedMAIN DECK CARGO COMPARTMENT SEA TRACK 4 RT,FR 29 HAS 4 EA BROKEN SCALLOPS. REMOVED DAMAGED SECTION OF SEAT TRACK 4RT AND INSTALLED SEAT TRACK SPLICE REPAIR AT TRACK 4RT BETWEEN FR 26 AND 30 IAW FREIGHTER SRM 53-10-16, PG 201.Feb 22, 2010 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002190477Floorbeam · bentMDCC FLOORBEAM AT FR 65 BETWEEN SEATTRACKS 3L AND 4L IS BENT/ DISTORTED APPROX 18 " IN LONG X .08 DEFLECTION. REPAIRED FLOORBEAM AT FR 65 BETWEEN 3L AND 4L USING SPLICING METHOD IAW SRM 53-10-15, CONFIG 2, PG 27, FIG 3, SHEET 2 COMPLIED WITH REQUIRED OPS TEST Feb 19, 2010 · N671FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201002170443Floorbeam · damagedFLOORBEAM AT FR 64 BETWEEN SEAT TRACKS 3L AND 4L IS BENT/DISTORTED APPROX 18 IN LENGTH X .05 IN DEFLECTION. REPAIRED FR 64 CROSSBEAM USING SPLICING METHOD IAW FREIGHTER SRM 53-10-15, FIG 207, SHT 41.Feb 17, 2010 · N671FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201002070351Seat Track · crackedSEATRACK 4-R HAS 2EA AREAS OF CORROSION BETWEEN FR 39-44 UPON INSP FOUND SEAT TRACK 4R NR FR 39 TO FR 44 CRACKED BY A LENGTH 5IN". REMOVED DAMAGED DUMMY TRACK & INSTALLED NEW DUMMY TRACK IAW SRM 51-72-10. TOPCOATED FASTENERS IAW SRM 51-75-10.Feb 7, 2010 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002070350Floorbeam · crackedCROSSBEAM AT FR 31 FWD SIDE 1 IN BELOW FLOOR AND LBL 67 IN CRACKED .5 IN LENGTH. ROUTED OUT CRACK ON CROSSBEAM AT FR 31 FWD 1 IN. BELOW FLOOR LBL 67 IN FABBED DOUBLER AND INSTALLED IAW SRM 53-10-15 FIG 212 SHEET 1.Feb 7, 2010 · N671FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201002060349Seat Track · wornFUSELAGE INT DUMMY SEAT TRACK RT 2R AT FRAME 38.2 ATTACHMENT GAP IS .020 IN. EXCEEDS LIMITS IAW EO 6-5310-7-3322 PT1. REMOVED DUMMY SEAT TRACK RT 2R FRAME 38.2 IAW SRM 53-15-16. FABBED 1 EA INSERT BUSHING AND BONDED INSERT IN DUMMY SEAT TRACK IAW SRM 53-15-1Feb 6, 2010 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002060348Seat Track · wornFUSELAGE INT DUMMY SEAT TRACK RT 3R AT FRAME 38.2 ATTACHMENT GAP IS .019 INCH. EXCEEDS LIMITS IAW EO E6-5310-7-3322 PT 1. REMOVED DUMMY SEAT TRACK RT 3R AT FRAME 38.2. FABBED 1 EA INSERT BUSHING AND BONDED INSERT IN DUMMY SEAT TRACK IAW SRM 53-15-16. REINFeb 6, 2010 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002060347Seat Track · wornFUSELAGE INT, DUMMY SEAT TRACK LT NR 2 AT FRAME 38.2, ATTACHMENT GAP IS .017 IN. EXCEEDS LIMITS IAW EO 6-5310-7-3322 PT1. REMOVED DUMMY SEAT TRACK LT NR 2 AT FRAME 38.2 AND REPAIRED IAW SRM 53-15-16. FABBED BUSHING INSERT AND BONDING INSERT IN TRACK IAW SRM Feb 6, 2010 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002060346Seat Track · corrodedMDCC SEAT TRACK 3R HAS A 1 SQ INCH AREA OF CORROSION BETWEEN FRAMES 38.1 AND 38.2. REMOVED LEVEL 1 CORROSION. FOUND OUT OF LIMITS. R & R SEAT TRACK 3R BETWEEN FRAMES 38.1 AND 38.2 IAW SRM 53-10-16. SEAT TRACK FABRICATED FROM EXTRUSION PN 60-22457/7075T7651Feb 6, 2010 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002060345Adapter · corrodedMDCC CLS ADAPTER UPR SURFACE BETWEEN SCALLOPS CORRODED LOCATED FRAME 24 RBL, 63 INCHES TO RBL 65 INCHES. REMOVED LEVEL 1 CORROSION. FOUND OUT OF LIMITS. R & R MDCC CLS ADAPTER FRAME 24 RBL 63 INCHES IAW SRM 51-72-10.Feb 6, 2010 · N671FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201002060344Seat Track · crackedDUMMY TRACK 4R BETWEEN FRAMES 54.1 AND 54.2 IS CRACKED AT THE SCALLOPS APPROX 6 INCHES. R & R DUMMY TRACK 4R BETWEEN FRAMES 54.1 AND 54.2 IAW SRM 53-15-16.Feb 6, 2010 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002060343Adapter · gougedMDCC CLS ADAPTER BETWEEN SEAT TRACKS 4L AND 5L WORN .37 SQ INCHES FRAME 30. REMOVED AND REPLACED CLS ADAPTER BETWEEN SEAT TRACKS 4L AND 5L FRAME 30 IAW SRM 51-72-10.Feb 6, 2010 · N671FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201002060342Adapter · corrodedCLS ADAPTER UPR SURFACE CORRODED AT SCALLOPS LOCATED FRAME 22 RBL 63 INCH TO 65 INCH. REMOVED LEVEL 1 CORROSION. FOUND OUT OF LIMITS. R & R CLS ADAPTER IAW SRM 51-72-10.Feb 6, 2010 · N671FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201002060341Seat Track · corrodedMDCC SEAT TRACK 3R BETWEEN FRAMES 54 TO 54.1 HAS A 1 SQ INCH AREA OF CORROSION ON TRACK AND SCALLOPS. R & R SEAT TRACK 3R BETWEEN 54 AND 54.1 IAW SRM 51-72-10.Feb 6, 2010 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201002060340Seat Track · corrodedMDCC SEAT TRACK 4L BETWEEN FRAMES 38 AND 40 HAS 4 EA AREAS OF CORROSION. DEFECT MEASURES 4 SQ INCHES. REMOVED LEVEL 1 CORROSION FOUND TRACK OUT OF LIMITS. R & R DUMMY SEAT TRACK BETWEEN FRAMES 38 AND 40 IAW SRM 51-72-10.Feb 6, 2010 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200812125135Restrictor Valve · dirtyON APPROACH, LOWERED LANDING GEAR, LT MAIN GEAR SHOWED UNSAFE IN BOTH SYS 1 AND SYS 2 AND NR 3 GEAR SYS. ON GO AROUND, GEAR CAME DOWN. CREW AND STATED LIGHTS WENT SAFE AFTER GO AROUND, RAISED GEAR AND TRIED AGAIN. RECEIVED UNSAFE LIGHTS AGAIN FOR LT MLG. Dec 12, 2008 · N671FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 08FDEA01786Outflow Valve · damagedCLIMBING THROUGH FL 320 RECEIVED CABIN PRESS ADVISORY. ATTEMPTED TO SLOW CABIN ALTITUDE BUT OBSERVED FWD OUTFLOW VALVE OPEN HALFWAY. ATTEMPTED CYCLING BETWEEN REG 1 AND 2 TO TRY AND GET PRESS SYSTEM TO RESPOND. SLOWED A/C CLIMB AND RECEIVED CABIN ALTITUDE May 7, 2008 · N671FE · Airbus A300F4605R · Pressure Regulator/Outflow ValveSDR 07FDEA05074Unknown · unknownIMMEDIATELY AFTER SELECTING TOGA ON THE RUNWAY GOT A CHIME AND ECAM MESSAGE. INITIATED AN ABORT THEN SAW AN ECAM MESSAGE INDICATING FMS DISAGREE. TAXIED CLEAR AND RELOADED THE RUNWAY IN THE FMS. ON THE SECOND TAKEOFF ATTEMPT THE TOGA LEVERS WOULD NOT ENGAGDec 17, 2007 · N671FE · Airbus A300F4605R · Central WarningSDR 07FDEA05039Seat Track · corrodedMCC SEAT TRACK SECTION 3R HAS CORROSION AT FR'S 57.1, 57.3 AND 57.5 REMOVED CORROSION IAW A300 SRM 51-74-10. ALODINED AND PRIMED IAW A300 SRM 51-75-10. AREA WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK IAW A300 SRM 53-10-16. REPAIRED AND INSTADec 12, 2007 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA05038Seat Track · corrodedMCC SEAT TRACK 2R HAS CORROSION AT FR75, 77, AND 78. INSTALLED SECTION OF SEAT TRACK AND 2 EA SPLICE AT 2 RT FR 75-77- AND 78 IAW A300 SRM 53-10-16.Dec 12, 2007 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04952Floorbeam · crackedFWD CARGO COMPT FR 29 BETWEEN SEAT TRACKS 3R-2R APPROX 3/4 INCH CRACK IN FLOORBEAM REPAIRED CROSSBEAM AT FR 29 BETWEEN SEAT TRACK RT 2-3 IAW A300-600 FSRM 53-10-15.Nov 27, 2007 · N671FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 07FDEA04951Crossbeam · crackedFWD CARGO COMPT MAIN CABIN CROSSBEAM C-27 BETWEEN RT SEAT TRACK 2-3 CRACKED ON VERTICAL STIFFENER UPPER CONTOUR APPROX 1/4 IN LONG. REPAIRED CROSSBEAM C-27 BETWEEN RT SEAT TRACK 2-3 IAW A300-600 FSRM 53-10-15.Nov 27, 2007 · N671FE · Airbus A300F4605R · Fuselage Main, StructureSDR 07FDEA04950Seat Track · corrodedMCC FR 72 SEAT TRACK 3R HAS CORROSION I PLACE. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN FR 71 TO FR 73 IAW A300-600 SRM 53-10-16 AND 51-40-21.Nov 27, 2007 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04949Seat Track · corrodedMCC SEAT TRACK SECTION 2L HAS CORROSION AT FRAMES 77 AND 78. REMOVED AND INSTALLED SEAT TRACK IAW A300-600 SRM 53-1-16 AND 51-40-21.Nov 27, 2007 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04948Seat Track · corrodedMCC SEAT TRACK SECTION 3 R HAS CORROSION AT FRAMES FR 64.5 , 65.5 , AND 66. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 53-10-16. INSTALLED NEW SEAT TRACK, SECTION AND REPAIR SPLICES IAW A300-600 SRM 53-10-16 FROM FR 64 TO FR 68.Nov 27, 2007 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04864Seat Track · corrodedMAIN CABIN LT NR 3 SEAT TRACK HAS 3 EACH AREAS OF CORROSION INSIDE/TOP OF SCALOPE HOLES WITH APPROX MEASUREMENTS FR 43=3-SQ IN, BETWEEN FR 44-45 =3 SQ IN ,FR 45- 46= 1 SQ IN. REMOVED AND REPLACED SEAT TRACK PER A300-600 SRM 51-40-21 AS FOUND BEYOND LIMIT PENov 19, 2007 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04842Seat Track · corrodedMAIN CABIN LT NR 5 SEAT TRACK HAS 3 AREAS OF CORROSION INSIDE/TOP SCALOPE HOLES WITH APPROXIMATE MEASUREMENTS AS FOLLOWS; BETWEEN FR 44 -45 = 4 SQ IN, AFT OF FR 42 =4 SQ IN FR 41 = 3.5 SQ IN. REMOVED SEAT TRACK L5 FR 40 TO FR 45, AND REINSTALLED NEW PART PER Nov 18, 2007 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04841Seat Track · corrodedMAIN CABIN LT SEAT TRACK NR 2 HAS THREE AREAS OF CORROSION INSIDE SCALOPE HOLES ON FOLLOWING; FR 42 = 2 IN LONG, FR 43 AFT 3 SQ IN, FR44- 45 2.5 SQ IN. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10, DUE BEYOND LIMITS.Nov 18, 2007 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02434Adc · failedDIVERTED TO IAD, CLIMBING THRU 16,000', GOT APPROX 25 KT DIFFERENCE IN AIR SPEED IND. SECONDARY GEAR IND INOP. ENG N-1 MODE FAULT. BLOWING OUT NR 2 SYS, REMOVED AND REPLACED ADC NR 2 PER MM 34-11-34-4. REMOVED AND REPLACED PROX BOX PER MM 32-31-71-4. ACN Jul 11, 2007 · N671FE · Airbus A300F4605R · Airspeed/Mach IndicatorSDR 07FDEA00231Flow Valve · malfunctionedACFT DIVERTED INTO LBB WITH CREW LP SUPPLY READING 0 PSI AND NO AIR FLOW TO ANY POSS ON FLT DECK. TROUBLE SHOT PROBLEM TO CREW LP FLOW VALVE. SWAPED FLOW VALVE FROM COURIER POSS TO CREW POSS. CREW LP SYSTEM NOW OPERATIONAL. NO LEAKS NOTED AT THIS TIME. WILJan 31, 2007 · N671FE · Airbus A300F4605R · Crew Oxygen SystemSDR 06FDEA1260Coupling · leakingON T/O ROLL, WHEN N1 WAS 80 - 90%, GOT GEN 1 FAULT ALERT. ABORTED T/O AT 70KTS. RESET GEN 1 AND ATTEMPTS A SECOND T/O WITH THE SAME RESULT. ABORTS AGAIN AT 70KTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 24-11-01 CATEGORY: B EXPIRATION: 31MAR06 "MEL 24-11-Mar 28, 2006 · N671FE · Airbus A300F4605R · Alternator-Generator DriveSDR 06FDEA0812Hydraulic Line · chafedPDIS 671 29-11 0007374 22FEB06 OAK OPEN R LOGPAGES: 01086620 ECAM ALERT AT FL320 GREEN HYD SYS QNT LOW ALERT. MANUAL GEAR EXTENSION ACCOMPLISHED. FLUID DRIPPING FROM NR1 ENG RESEARCHING. FOUND 2 HYDR LINES LEAKING THAT HAD BEEN CHAFED THROUGH AT A CLAMP INFeb 23, 2006 · N671FE · Airbus A300* · Hydraulic System, MainSDR 05FDEA04211Windshield · crackedRT WINDSHIELD CRACKED. REMOVED AND REPLACED RT WINDSHIELD PANEL PER A300 AMM 56-11-11-4. NEEDS SEALANT CURE CHECK, WINDSHIELD WIPER INSTALLED AND OPS CHECK.Dec 9, 2005 · N671FE · Airbus A300B4605R · Flight Compartment WindowsSDR 05FDEA04200Windshield · crackedRT WINDSHIELD CRACKED. CREW NOTICED A SMALL CRACK DURING CLIMB, DID NOT HEAR OR FEEL ANYTHING HIT WINDOW. NOTICED WINDOW ARCHING, WINDOW HEAT WAS TURNED OFF, THEN THE WINDSHIELD SPIDER WEBBED. REMOVED AND REPLACED RT WINDSHIELD PANEL PER A300 AMM 56-11-11-4Dec 9, 2005 · N671FE · Airbus A300F4605R · Flight Compartment WindowsSDR 05FDEA02418Skin · dentedLT I/B T/E FLAP, LWR SURFACE SKIN DENTED/GOUGED BEHIND NR 2 LT FLAP JACK SCREW. MEASURED DEPTH OF DENT AT .162 OUT OF LIMITS IAW SRM 57-50-00 FIG 101. INSTALLED REPAIR IAW SRM 57-52-12. REVIEW OF REPAIR REVEALS IT AS UNSAT DUE TO UNAPPLICABLE SRM SCHEME. SAug 11, 2005 · N671FE · Airbus A300F4605R · Trailing Edge FlapsSDR 05FDEA02327Fairing · delaminatedNR 1 PYLON AFT FAIRING 473EL DELAMINATED.Aug 8, 2005 · N671FE · Airbus A300B4605R · Nacelle/Pylon Miscellaneous StructureSDR 05FDEA02326Support Bracket · crackedNR 1 ENG HYDRAULIC CASE DRAIN LINES SUPPORT BRACKET CRACKED ACCESS THRU 473CL PNL.Aug 8, 2005 · N671FE · Airbus A300* · Nacelle/Pylon Miscellaneous StructureSDR 05FDEA02246Floor Panel · damagedMDC FLOOR PNL 232FF IS DAMAGED.Aug 4, 2005 · N671FE · Airbus A300B4605R · Fuselage Floor PanelSDR 05FDEA02245Floor Panel · damagedMDC FLOOR PNL 231FG DAMAGE.Aug 4, 2005 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR 05FDEA02244Floor Panel · damagedMDC FLOOR PNL 232TG DAMAGED.Aug 4, 2005 · N671FE · Airbus A300B4605R · Fuselage Floor PanelSDR 05FDEA02243Bearing · damagedMCD FLOOR PNL 232FG HAS BALL BEARING DAMAGE.Aug 4, 2005 · N671FE · Airbus A300B4605R · Cargo CompartmentsSDR 05FDEA02242Floor Panel · puncturedMDC FLOOR PNL 251YG HAS SEVERAL PUNCTURES ON LWR SURFACE AND 1 ON UPPER SURFACE.Aug 4, 2005 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR 05FDEA02241Floor Panel · damagedMDC FLOOR PNL 231FF DAMAGED.Aug 4, 2005 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR 05FDEA02240Floor Panel · crackedMAIN CARGO COMPT FLOOR PNL 262ZF IS CRACKED AT ATTACH POINT.Aug 4, 2005 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR 05FDEA02239Floor Panel · crackedMAIN CARGO COMPT FLOOR PANEL 242EK IS CRACKED AT SEAT TRACK ATTACH POINT.Aug 4, 2005 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR 05FDEA02228Service difficultyNR 1 ENG FAN CASE HAS 2 PREVIOUSLY STOP DRILLED CRACKS ON FWD DOLLY MOUNTS AT APPROX 8 O'CLOCK. FPI IAW NTM 51-91-00 CRACK IS CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 SPM. STOP DRILL ACCEPTABLE PER EA 6-7223-82106 AND PER AAug 3, 2005 · N671FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR 05FDEA02227Service difficultyNR 1 ENG FAN CASE HAS 2 PREVIOUSLY STOP DRILLED CRACK ON AFT DOLLY MOUNT AT APPROX 8 O'CLOCK POSITION. FPI IAW NTM 51-91-00 CRACK CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 OF SPM. STOP DRILLS ACCEPTABLE PER EA 6-7223-82106-NAug 3, 2005 · N671FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR 05FDEA02226Powerplant · crackedW/O 29493, NR N00177, ENGINE NR 1 AT FORWARD INBOARD LOWER HOIST POINT, THE FLANGE IS CRACKED AT IT'S BASE. FPI IAWM NTM 51-91-00 CRACK IS CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 PER GESPM STOP DRILL ACCEPTABLE PER EAAug 3, 2005 · N671FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR 05FDEA02212Skin · damagedLEFT WING I/B FLAP BOTTOM SKIN HAS CREASE AT MID SECTION REPAIRED DAMAGED SECTION OF LEFT I/B TRAILING EDGE FLAP LOWER SURFACE SKIN AND 2 EA STRINGERS IAW SRM 57-50-00 FIG 206. PREPPED AND PAINTED IAW MM 51-75-10-8.Aug 2, 2005 · N671FE · Airbus A300B4605R · Trailing Edge FlapsSDR 05FDEA02169Web · crackedAFT MAIN DECK REAR CARGO COMPT FR 79 WITH STR 26 WEB IS CRACKED.Aug 2, 2005 · N671FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
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