N613FE
Service difficulty reports · 422
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 = 'N613FE' 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 = 'N613FE' 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 FDEA201604171238Web · crackedWHILE ACCOMPLISHING WIC 53.10.05.3 PSE AREA, GVI FOUND MAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX, AT STATION 1305.25 - 1315.42, LONGERON 26R - 27R, CRACKED AS MARKED. MAIN DECK R3 DOOR AFT JAMB LOWER WEB BOX REPAIRED IAW SRM 53-40-15-2R FIGURE 201 REPAIR 3. RSDR FDEA201604171237Web · crackedWHILE ACCOMPLISHING WIC 53.10.05.3 PSE AREA, GVI FOUND MAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX, AT STATION 1305.25 - 1315.42, LONGERON 26L - 27L, CRACKED AS MARKED. MAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX. REPAIRED IAW SRM 53-40-15-2R FIGURE 201 REPAIR 3. SDR FDEA201511243768Line · leakingHYDRAULICS 3 OFF ALERT IN CRUISE, FOLLOWED BY HYD 3 FAIL, APPROX 40 MINUTES LATER. UTILIZED EMERGENCY GEAR EXTENSION METHOD IAW QRH. RESET ALTERNATE RELEASE LANDING GEAR CONTROL LEVER IAW AMM 32-32-00-5. REPLACED NR 3 ENGINE UPPER HYDRAULIC PUMP PRESSURE LISDR FDEA201508232689Probe · faultyACARS WOULD NOT INIT, APPROX 2 MIN AFTER TAKEOFF, THRUST LIMIT MISMATCH MSG ON MCDU. . CHECKED PERFORMED THRUST LIMITS & ENG THRUST ACTUAL STGS, ALL NORMAL. APPROX 12 MIN AFTER TAKEOFF AUTOPILOT DISCONNECT, ATS DISCONNECT & ALL FLIGHT GUIDANCE REMOVED FROM SDR FDEA201504281312Idg · failedRECEIVED LEVEL 1 ALERT GEN 1 OFF. SLIGHT ACRID ODOR, DID CHECKLIST & RETURNED. RAN ENGINE IAW JRH, DISCONNECTED NR 1 GEN IAW MEL 24-21-01. WHILE RUNNING ENG NR 1 THERE WAS NO ODOR IN COCKPIT. WHEN CREW ARRIVED THEY WERE ASKED IF THERE WAS STILL AN ODOR,SDR FDEA201502090497Battery · failedEMERGENCY POWER TEST FAILED 2 TIMES. R & R BOTH BATTERIES & BATTERY CHARGER IAW AMM 24-34-02-4 & 24-34-03-4. PERFORMED EMER POWER TEST & IT PASSED. ACFT OK FOR SERVICE.SDR FDEA201404290882Skin · dentedLEFT WING NR 4 SLAT LE LOWER SURFACE FOUND DENT AT XOS 601. REPAIRED IAW SRM 57-40-01 FIGURE 201 REPAIR 3 REV 55 AND EA 1-5750-T0307828 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 121.SDR FDEA201404210772Longeron Splice · crackedCRACK INDICATION FOUND APPROXIMATELY 1 INCH IN LENGTH DURING X RAY INSPECTION AT CABIN STATION 5-123, LONGERON SPLICE 6L FWD SECTION BETWEEN 1ST AND 2ND FASTENER HOLE. REMOVED AND REPLACED IAW SRM 51-33-01 REV 55 AND DRAWING N5A6774 REV AD. NEW LONGERON SPLISDR FDEA201404210767Frame · dentedSIDEWALL FRAME AT RT STATIONS 5 - 11, LONGERON 12L FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REV 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201404210773Floor Panel · damagedBS 1561 - 1661 FLOOR PANEL 282AF FOUND SPONGY. REMOVED AND REPLACED IAW AMM 53-21-04 REVISION 79. FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005 REVISION K. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201404210769Doubler · crackedLEFT WING FIXED LE BEADED DOUBLER FOUND CRACK AT XOS 765. REPAIRED IAW SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201404210768Doubler · crackedLEFT WING FIXED LE BEADED DOUBLER FOUND CRACKED AT XOS 627. REPAIRED IAW SRM 57-40-02 FIGURE 203 REPAIR 15 REV 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201404200760Frame · dentedDURING REMOVAL OF UPPER SIDEWALL LINER FOR INSPECTION, RT BS 1561 BETWEEN LONGERON 12 & 13R FOUND FRAME DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REV 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 121.SDR FDEA201404170746Wedge · delaminatedLEFT WING OTBD FLAP OTBD TE WEDGE UPPER SURFACE FOUND DELAMINATED AT STATION XOF 749.5 TO XOF 768. REPAIRED IAW SRM 57-50-80 PARA. 4A 1B REPAIR 1 REVISION 55 AND EA 1-5750-T0307626 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 121.SDR FDEA201310052413Switch · dirtyL1 DOOR CHARGE TEST PUSH BUTTON LIGHTS INTERMITTENTLY WHEN PRESSED OR TESTED. CLEANED EVACUATION SLIDE PTT SWITCH IAW SMP. OPS TEST OK IAW AMM 25-61-04-5. ACFT OK FOR SERVICE.SDR FDEA201305050913Lamp · inoperativeRT DOOR ESCAPE SLIDE DID NOT TEST. REPLACED LAMPS FOR SLIDE TEST SWITCH, OPS CHECKED NORMAL.SDR FDEA201211184070Landing Gear · unknownLANDING GEAR DID NOT CYCLE TO GREEN INDICATION. RECYCLED NORMAL GEAR EXTENSION: GREEN. GEAR HANDLE RESISTANCE STIFF, PERFORMED A GENERAL VISUAL INSPECTION OF ALL GEAR DOORS AND ALL LANDING GEAR, ALL FIND NORMAL IAW SMP CLEANED AND INSPECT LANDING GEAR CONTRSDR FDEA201207062493Fitting · corrodedRT WING OTBD FLAP VANE FITTING ECCENTRIC HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER SRM 57-50-02 REPAIR 5 FIGURE 201 REVISION 49 EXISTING SLOT SIZE 0.898" X 0.625" FINAL SLOT SIZE 0.9698" X 0.657" , MAX.ALLOWABLE SIZE 0.940" X 0.670" . SDR FDEA201207062490Door Frame · crackedR3 DOOR BS 1252 FORWARD FRAME LOWER WEB BETWEEN L26 AND L27 CRACKED. REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 49. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201207062492Skin · corrodedAFT ACCESSORY COMPARTMENT FOUND INTERIOR AT BS 2160 AROUND RT SIDE BODY FAIRING CUTOUT WITH CORROSION AT ANCHOR NUT LOCATION. REPAIR CARRIED OUT IAW SRM 53-70-01 REPAIR 3, FIG 201, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 115.SDR FDEA201207062491Skin · crackedFOUND FUSELAGE SKIN RT SIDE AT BS 2140, L36R CRACKED. REPAIR CARRIED OUT IAW SRM 53-70-01, FIG 201 REPAIR 2, REVISION 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201207032457Spar · crackedDURING HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION FOUND CRACK INDICATION AT LEFT NR 4 BANJO FITTING LOWER VERTICAL STAB FORWARD FLANGE OF UPPER REAR SPAR CAP. REPAIRED AS PER SRM 55-30-02 REPAIR 3 FIGURE 201 REVISION 49. REPAIR CLASSIFIED MAJOR AS PER GMMSDR FDEA201207032456Spar · crackedDURING HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION, FOUND CRACK INDICATION AT RT NR 4 BANJO FITTING LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP. REPAIRED AS PER SRM 53-30-02 FIGURE 201 REPAIR 3 REVISION 49 AND EA 1-5530-160973 PART 1. SDR FDEA201207032455Skin · crackedSEVEN FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND STA XORS=713.6. REPAIRED AS PER EA 1-5710-160974 PART 1. REPAIR CLASSIFIED MAJOR SDR FDEA201207032454Skin · crackedELEVEN FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT, BETWEEN STA XORS=683.4 AND STA XORS=713.6. REPAIRED AS PER EA 1-5710-160975 PART 1. REPAIR CLASSIFIESDR FDEA201206302421Gearbox · damagedENGINE NR 1 IDG FEEDER CABLE ADJACENT AREA LT SIDE ACCESSORY GEARBOX FOUND WITH ARCING DAMAGE. ACCOMPLISHED EA 1-7260-161492 PART 1. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 115.SDR FDEA201206302420Feeder Cable · burnedENGINE NR 1 IDG FEEDER CABLE HARNESS FOUND WITH CHAFING AND BURNED. R & R IAW AMM 71-50-04-4-1, REV 72.0, NR1 ENGINE AT 9 O`CLOCK POSITION ELECTRICAL WIRING MOUNTING BRACKET. R & R IAW STANDARD MX PRACTICES. NR 1 ENGINE IDG OPS CHECK CARRIED OUT IAW AMM 24-SDR FDEA201204181469Transducer · damagedNR 3 WHEEL SPEED TRANSDUCER DAMAGED. R & R NR 3 TRANSDUCER AND NR 3 TIRE PRESSURE TRANSMISSION IAW AMM 32-45-03-4-0. OPS CHECKED NR 3 WHEEL TRANSDUCER IAW AMM 32-45-00-5. TIRE PRESSURE CHECKED GOOD IAW MM 32-46-00-5.SDR FDEA201204181467Axle · damagedWHILE CHANGING NR 8 BRAKE FOUND PAINT ON NR 8 AXLE BLISTERED AND COMING OFF. R & R RT MAIN GEAR TRUCK BEAM ASSY IAW MM 32-12-20-4 ON SPECIAL VISIT WO 55507, SEQ 0007.SDR FDEA201107293033Bottle · dischargedWHEN F/O CHECKED THE SLIDE PRESSURE THE L1 DOOR WENT ALL THE WAY TO THE FLOOR. THE EMERGENCY EXIT HANDLE HAD BEEN MOVED WHILE THE DOOR WAS OPEN AND THE PRESSURE IN THE BLOW UP BOTTLE WAS FOUND DEPLETED. RELEASED FOR SERVICE IAW MEL: 52-10-03-03.SDR FDEA201103130950Wire · brokenEMERGENCY LIGHT COMES ON EVEN IF EMERGENCY LIGHT SWITCH IS OFF WHEN ACFT POWER OFF. FOUND LOOSE AND BROKEN OFF OF WIRE PIN "10" IN CONNECTOR PLUG (P1-1756A) REF WDM 33-51-01, PAGE 902. THEN REPAIRED WIRE PIN IAW MM 20-30-05-2. PERFORMED EMER LIGHT TEST ANSDR FDEA201101150179Landing Gear · malfunctionedON TAKEOFF, NOSE GEAR UNSAFE INDICATION. CYCLED GEAR UP/DOWN IAW QRH. UNSAFE REMAINED. NORMAL GEAR FOR LANDING. AT BLOCK IN , FOUND NOSE GEAR PIN STILL INSTALLED. VERBAL CREW SAID NOT OVERSHOOT 230 KNOTS. ALSO CHECKED L/G PINS POUCH & FOUND 3 L/G PINS: 2 MSDR FDEA201101070283Smoke Detector · false activationAT FL320 CARGO FIRE LOWER AFT DISPAYED WITH MASTER WARNING, LEVEL 3 ALERT AND AURAL TONE. DISCHARGED BOTH BOTTLES DURING REMAINDER OF FLIGHT. ON ARRIVAL CHECKED AFT AND CTR CARGO COMPARTMENTS, NO SIGN OF FIRE OR SMOKE. MANUAL CARGO FIRE TEST CARRIED OUT, SDR FDEA201101070282Smoke Detector · inoperativeAT FL320 CARGO FIRE LOWER AFT DISPAYED WITH MASTER WARNING, LEVEL 3 ALERT AND AURAL TONE. DISCHARGED BOTH BOTTLES DURING REMAINDER OF FLIGHT. ON ARRIVAL CHECKED AFT AND CTR CARGO COMPARTMENTS, NO SIGN OF FIRE OR SMOKE. MANUAL CARGO FIRE TEST CARRIED OUT, NSDR FDEA201101070281Smoke Detector · inoperativeAT FL320 CARGO FIRE LOWER AFT DISPAYED WITH MASTER WARNING, LEVEL 3 ALERT AND AURAL TONE. DISCHARGED BOTH BOTTLES DURING REMAINDER OF FLIGHT. ON ARRIVAL CHECKED AFT AND CTR CARGO COMPARTMENTS, NO SIGN OF FIRE OR SMOKE. MANUAL CARGO FIRE TEST CARRIED OUT, NSDR FDEA201101070280Smoke Detector · false activationAT FL320, CARGO FIRE LOWER AFT DISPAYED WITH MASTER WARNING, LEVEL 3 ALERT AND AURAL TONE. DISCHARGED BOTH BOTTLES DURING REMAINDER OF FLIGHT. ON ARRIVAL CHECKED AFT AND CTR CARGO COMPARTMENTS, NO SIGN OF FIRE OR SMOKE. MANUAL CARGO FIRE TEST CARRIED OUT, SDR FDEA201101070071Fire Detector · false activationAT FL320 CARGO FIRE, LOWER AFT DISPAYED WITH MASTER WARNING, LEVEL 3 ALERT AND AURAL TONE. DISCHARGED BOTH BOTTLES DURING REMAINDER OF FLIGHT. ON ARRIVAL CHECKED AFT AND CTR CARGO COMPARTMENTS, NO SIGN OF FIRE OR SMOKE. MANUAL CARGO FIRE TEST CARRIED OUT,SDR FDEA201007272677Skin · crackedDURING HFEC OPEN HOLE INSPECTION 13 EA FASTENER HOLES FOUND CRACK INDICATION AT R/H WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA. XORS= 690 AND STA. XORS= 700. REPAIR CARRIED OUT AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS= 690 AND STA.SDR FDEA201007272676Skin · crackedDURING HFEC OPEN HOLE INSPECTION 09 EA FASTENER HOLES FOUND CRACK INDICATION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA. XORS= 690 AND STA. XORS= 700. REPAIR CARRIED OUT AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STA XORS= 690 AND STA. XORSDR FDEA201007272675Skin · crackedLT WING DROOP L/E UPPER OTBD SKIN CRACKED. REPAIR CARRIED OUT AT LT WING DROOP L/E UPPER OTBD SKIN IAW SRM 57-40-01, FIG 201, REV 43. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 57-40-01, FIG 201, REV 43. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-1SDR FDEA201007252665Longeron · crackedCTR CARGO COMPARTMENT RT TUNNEL AREA - LONGERON L- 29 CRACKED AT STA1673. DAMAGED LONGERON AT CTR CARGO COMPARTMENT RT TUNNEL AREA L-29 STA1673 REMOVED IAW SRM 51-33-01, REV 43. CUTOUT CARRIED OUT IAW SRM 53-00-05, FIG 201 REV 43. NEW LONGERON REWORKED IAW SDR FDEA201007252666Longeron · crackedCTR CARGO COMPARTMENT RT TUNNEL AREA - STA 1673, LONGERON 30R, CRACKED. DAMAGED LONGERON REMOVED AS PER SRM 51-33-01 REVISION 43. CUTOUT CARRIED OUT AS PER SRM 53-00-05 FIGURE 201 REVISION 43. NEW LONGERON REWORKED AS PER DWG AFA7797 REVISION A AND NEW LONGESDR FDEA201007252664Seat Track · gougedMAIN DECK - SEAT TRACK AT STATION 1293 X= 8.5 FOUND GOUGES ON FLANGE AREA. REPAIRED AS PER SRM 53-00-52 FIG. 201 REV. 43. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 110.SDR FDEA201007252663Seat Track · crackedMAIN DECK - SEAT TRACK AT STA 6-70 X= 46 FOUND CRACKED. REMOVED AND FABRICATED NEW SEAT TRACK AND INSTALLED AS PER SRM 51-33-01 REV. 43 AND DWG AGA7082 REV. A. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 110.SDR 08FDEA04214Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING (ARC4009) INBOARD FORWARD BORE MOUNTING HOLE FOUND WITH CORROSION. REFER SNRM NR N01221 RIGHT HAND OUTBOARD FLAP ASSEMBLY REPLACEMENT.SDR 08FDEA04212Support Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FORWARD (ARC4008) OUTBOARD MOUNTING BORE HOLE BETWEEN FLAP AND HINGE FOUND WITH CORROSION. REFER SNRM NR N01221 RIGHT HAND OUTBOARD FLAP ASSEMBLY REPLACEMENT.SDR 08FDEA04205Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR OUTBOARD ATTACHMENT INBOARD FACE FOUND PITTING CORROSION. CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER CMM 57-44-09. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 08FDEA04208Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD BORE HOLE INNER SURFACE FOUND PITTING CORROSION. CORROSION ON OUTBOARD BORE INNER SURFACE AT RT WING OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT REMOVED AND FOUND WITHIN LIMIT AS PER CMM 57-44-09SDR 08FDEA04169Hinge Fitting · scratchedRIGHT WING OUTBOARD FLAP INBOARD HINGE AFT MOUNTING LOWER INBOARD MOUNTING BORE HOLE INNER FACE FOUND WITH SCRATCH MARKS. SCRATCH MARKS AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE AFT MOUNTING LOWER INBOARD MOUNTING BORE HOLE REMOVED AND FOUND WITHIN LIMITSDR 08FDEA04157Hinge Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING (ARC4009) OUTBOARD FORWARD BORE MOUNTING HOLE FOUND WITH CORROSION. RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING (ARC4009) OUTBOARD FORWARD BORE MOUNTING HOLE PITTING CORROSION REMOVED AS PER EO 1-5750-5008 PAR
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