N654FE
Service difficulty reports · 237
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 = 'N654FE' 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 = 'N654FE' 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 FDEA201711083200Floor Panel · damagedFWD CARGO FLOOR PANEL 131NG DAMAGED ON EDGES. FABRICATED NEW FLOOR PANEL 131NG ON T17/1306203 IAW SRZ-25-005 CAT "A" MAJOR REPAIR.SDR FDEA201711033141Shear Plate · crackedAFT CABIN FLOOR AREA LT SIDE BETWEEN FR79-FR80 SHEAR PLATE WEB SKIN CRACKED. REMOVED AND REPLACED SHEAR PLATE AFT CABIN LT SIDE BETWEEN FR78 TO FR80 IAW SRM 51-40-21 MAJOR REPAIR.SDR FDEA201709102475Selector · malfunctionedDURING BRAKES CHECK PRIOR TO TAXI, INDICATED BRAKE PRESSURE WOULD NOT GO TO ZERO, BUT RECOVERED TO NORMAL AFTER PARKING BRAKE WAS RELEASED. PRESSURE REACTED NORMALLY AFTER SHUTDOWN. COMPLETED PARKING BRAKE SELECTOR REMOVAL AND REPLACEMENT PER AMM 32-45-12-SDR FDEA201708302415Line · leakingAT CRUISE FL350, RECEIVED A YELLOW SYS HYD ECAM YELLOW SYS LOW QTY, LOW PRESSURE. YELLOW SYS QTY JUST ABOVE THE RED DOT. ACCOMPLISHED ECAM AND QRH PROCEDURES. INSTALLED FLEX LINE IAW AMM 20-23-11, & INSTALLED LACING TAPE OTBD SIDE OF LINE IAW AMM 20-23-14. SDR FDEA201610253688Probe · failedREJECTED TAKEOFF ROLL BECAUSE CAPT AIRSPEED INDICATOR IN PFD INOP. WHEN F/O CALLED 80 KNTS CAPT SIDE STUCK AT 30 KNOTS BUT WAS GETTING TREN ARROW. PERFORMED CAPT'S PITOT SYSTEM TEST, SYSTEM OPS NORMAL. REMOVED NR 1 ADC AND CAPT'S PITOT TUBE AND BLOW OUT PISDR FDEA201610253687Adc · failedREJECTED TAKEOFF ROLL BECAUSE CAPT AIRSPEED INDICATOR IN PFD INOP WHEN F/O CALLED 80 KNTS. CAPT SIDE STUCK AT 30 KNOTS BUT WAS GETTING TREN ARROW. PERFORMED CAPT'S PITOT SYSTEM TEST, SYSTEM OPS NORMAL. REMOVED NR 1 ADC AND CAPT'S PITOT TUBE AND BLOW OUT PITSDR FDEA201506171832Structure · crackedRIGHT WING CTR FLAP INTERNAL STRUCTURE CRACKED AT RIB 18. REPAIRED IAW EA 6-5750-T0318301. MAJOR REPAIR IAW GMM 6-2-100 REV 127.SDR FDEA201506171829Frame · crackedLEFT SIDE FRAME 40, CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION. LOWER HOLE CRACKED. REPAIRED IAW EA 6-5710-T0317493 PT 1. MAJOR REPAIR IAW GMM 6-2-100 REVISION 127.SDR FDEA201506171828Skin · crackedLEFT SIDE FRAME 40, CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION. UPPER HOLE CRACKED. REPAIRED IAW EA 6-5710-T0318571 PT 1. MAJOR REPAIR IAW GMM 6-2-100 REVISION 127.SDR FDEA201506171827Pressure Deck · crackedMAIN DECK CARGO HORIZONTAL PRESSURE DECK WEB CRACKED AT FRAME 47, Y0 - Y450. REPAIRED THE CRACK WEB IAW SRM 53-15-15-201 CONFIG 2 FIG 201. MAJOR REPAIR IAW GMM 6-2-100 REVISION 127.SDR FDEA201501060029Pivot · lack of lubeLANDING GEAR WOULD NOT RETRACT. HEATED GEAR AND GREASED ALL BOGIE PIVOT POINTS ON LEFT GEAR. JACKED ACFT IAW MM 07-11-00-00. RAN NORMAL EXTENSION AND RETRACTION ADJ AND TEST IAW MM 32-31-00-05. LOWERED AND RAISED GEAR SEVERAL TIMES. OPS CHECK GOOD. ACFT OKSDR FDEA201407161817Regulator · faultedDEPARTED WITH NR 2 PRESS REGULATOR DEFERRED INOPERATIVE. AFTER DEPARTURE NR 1 PRESS REGULATOR FAULTED & WOULD NOT RESET. COMPLIED WITH ECAM & QRH, DIVERTED.SDR FDEA201401070049Bearing · contaminatedLANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. JACKED ACFT AND SWUNG GEAR IN BOTH SYSTEMS, WENT UP AND LOCKED OK, PROCEEDED TO LUBE BOTH MLG BOGI BEAMS AND ALL FITTINGS. FOUND WATER IN SEVERAL MAIN BOGIE DURING LUBE. LUBED UNTIL ALL WATER REMOVED. REPEATED GSDR FDEA201307111533Skin · chafedLEFT WING LOWER SURFACE, FOUND PYLON TO WING REINFORCE PLATE, WITH ABRASIONS AT OTBD SIDE. REPAIRED IAW EA 6-5720-T0301089. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201307111532Skin · dentedLEFT FUSELAGE SKIN FOUND ONE DENT AT FR 31 STRINGER 46L. DAMAGED ARE TRIM-OUT. NDI WAS COMPLETED, NO CRACK WAS FOUND. REPAIRED IAW SRM 53-10-12, FIG 208. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201307101517Skin · chafedLT WING INBD FLAP LWR SURFACE FOUND ONE PLACE SCRATCH AT OTBD AREA. IAW SRM 57-50-00, FIG 101, SHEET-5 EXCEEDED ALLOWABLE DAMAGE. TRIMED OUT AND REINFORCE PATCH REPAIR WITH DOUBLER REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201307091512Splice · damagedDURING PFM WORK CARD E6-5310-7-5017 B PT3" FUSE FR47 SPLICE FITTING BETWEEN STR 24 & 26. LT/RT, FOUND 1EA PREVIOUS DRILL MARK NEAR THE HOLE "E" ON 47 SPLICE FITTING LT SIDE. REPAIRED IAW EA 6-5720-T0301089SDR FDEA201307091511Splice · damagedDURING PFM WC E6-5310-7-5017 B PT3" FR 47 SPLICE FITTING BETWEEN STR 24 & 26. FOUND HOLE "N" ENLARGED. REPAIRED IAW EA 6-5310-T0300981.SDR FDEA201307081495Skin · scratchedAFT FUSELAGE LOWER SKIN SCRATCHED AT FR89, S33L ACCOMPLISHED THE WORK EA 6-5330-T0301069. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201306241381Rib · crackedRT WING T/E BOX RIB SKIN HAS CRACK ABOUT .6250" BELOW NR 3 SPOILER INBD EDGE. REPLACED RIB IAW SRM 57-51-11 & 51-72-10. THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100SDR FDEA201306241380Structure · crackedONE CRACK WAS FOUND. THE CRACK, 18MM LENGTH AT ZONE B,J AREA OF RT SIDE NOSE SECTION /FR 12A FITTING. REPLACED IAW EO E6-5340-7-5002 C1 PART7 & PART 8.SDR FDEA201301150097Adc · failedADC FAILURE THEN CAME BACK ON. FD NR 1 & NR 2 FAIL. REMAINED INTERMITTENT. FCP ON & OFF. FREEZING UP. IAW CREW DEBRIEF, RESET OF NR 1 ADC WOULD CLEAR ANOMALY, BUT FAULTS WOULD RETURN. MTP SHOWS ADS 1, FCC 1 & FCC 2 FAULTS ON LAST LEG. ACCOMPLISHED AFS TESSDR FDEA201206302425Flap System · stuckDEPARTING, ECAM ALERT FLAPS STUCK WITH SYSTEM 1 & 2 ON OVERHEAD. CYCLED HANDLE IAW QRH, NO RELIEF. COMPLIED WITH QRH AND RETURN TO DEPARTURE. INSTALLED HARDWARE ON NR 3 LT WING FLAP TRANSMISSION TORQUE TUBE IAW AMM 27-54-15-04 D (2). PERFORMED ADJUSTMENT ASDR FDEA201110044280Transmitter · leakingDURING CRUISE AT FL350 ECAM ANNUCIATED "HYD-GREEN SYS RESEVOIR- LO" FOLLOWED BY GREEN FLUID LOW INDICATION ON OVERHEAD PANEL HYD SCHEMATIC PAGE. FOLLOWED ECAM PROCEDURES , QRH PROCEDURES AND GRAVITY EXTENDED THE LANDING GEAR FOR AN UNEVENTFUL APPROACH AND LANSDR FDEA201109083758Skin Panel · dentedON WALK AROUND, 1 DENT APPROX 2.2" AFT OF FR 65 RT. FOUND OUT OF LIMITS PER SRM 53-10-12. CUT OUT DAMAGED AREA 3.70 L X 3.30 W IAW SRM 53-10-12 FIG 208. FABRICATED REPAIR DOUBLER IAW SRM 53-10-12 FIG 208. INSTALLED DOUBLER IAW SRM 53-10-12 FIG 208, SRI 53SDR FDEA201109013629Skin · damagedRIGHT FUSELAGE HAS 4" CREASE DENT AT FR 38.2-42R WITH FASTENER PULLING AND DISHED, DUE TO PREVIOUSLY MISLOCATION OF CRADLE AT FR. 38.2 VERSES FR 39 - REF EA 6-5310-145629, PG 4 AND EO 6-5310-7-5001, PT 2 COMPLIED WITH EVALUATION OF RT FUSELAGE 4" CREASE DENTSDR FDEA201109013628Skin · damagedLEFT FUSELAGE HAS 4" CREASE DENT AT FR 38.2, STR 42L WITH FASTENER PULLING AND DISHED DUE TO PREVIOUSLY MIS-LOCATION OF CRADLE AT FR 38.2 VERSUS FR 39 - REF EA6-5310- 145629, PG 4 AND EO 6-5310-7-5001, PT2. COMPLIED WITH EVALUATION OF LT FUSELAGE 4" CREASE DSDR FDEA201107252939Shear Tie · buckledFWD CARGO PIT AT AFT BULKHEAD PARTITION FR 38.2 BETWEEN STR 42LT & 43LT SHEAR TIE AT FUSELAGE SKIN HAS BUCKLED. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 51-40-21.SDR FDEA201107252938Shear Tie · buckledFWD CARGO PIT AT AFT BULKHEAD PARTITION FR 38.2 BETWEEN STR 42RT & 43RT SHEAR TIE AT FUSELAGE SKIN HAS BUCKLED. REMOVED AND REINSTALLED SUPPORT ANGLE IAW SRM 51-40-21, REMOVED AND INSTALLED NEW SHEAR TIE ON FR 38.2, STR 42-STR 43, RT SIDE IAW SRM 51-40-21 FABSDR FDEA201107252940Shear Tie · bentFRAME 38.2 BETWEEN STR 43, 44 RT SHEAR TIE HAS SLIGHT BUCKLE, UNABLE TO MEASURE DEFLECTION. REMOVED, FABRICATED AND INSTALLED NEW SHEAR TIE ON FR 38.2 AT STR 43 AND 44RH IAW SRM 51-40-21, PG 7 AND 22, DWG A53777956. NDT CHECKED ROTOPROBE HOLES AND CHECKED FOSDR FDEA201107202845Support · crackedNR1 PYLON UPPER L/E AUX STRUCTURE WEB SUPPORT RT LIGHTNING HOLE HAS 3 EA CRACKS. COMPLIED WITH SB A300-54-6023, REV NR 1 DATED 02/27/02 BY REINFORCEMENT OF THE NR 1 PYLON CANTILEVER WEB BY ADDING A DOUBLER, COMPLIED WITH EA 6-5450-145606.SDR FDEA201107202844Rib · crackedLT WING INBD L/E INSIDE KRUGER FLAP WELL OTBD L/E RIB IS CRACKED APPROX .500 LONG INBD OF NR 1 SLAT TRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW EA 6-5710-145616.SDR FDEA201107202842Frame · gougedMDCC FRAME 28 HAS 2 GOUGES, .100" BETWEEN STR L17 AND L18. FABRICATED AND INSTALLED 1EA REPAIR PLATE AND 1 EA BRIDGE IAW SRM 51-40-21 AND COMPLIED WITH EA6-5310-145643.SDR FDEA201107192812Profile · crackedNR 2 PYLON UPPER L/E AUX STRUCTURE WEB SUPPORT LT LIGHTNING HOLE HAS 3EACH CRACKS. 1IN AND 1.5IN LONG (STA. 537 TO 551) INCORPORATED, SB 300-54-6023 REV NR 1 DATED 02/27/02 BY REINFORCEMENT OF THE NR 2 PYLON CANTILEVER WEB BY ADDING A DOUBLER IAW EA 6-5450-14SDR FDEA201107182781Support · cracked3 INCH LONG CRACK ON WEB SUPPORT AT NR 1 PYLON INSIDE ACCESS 411CL BELOW FEEDER CABLE RIB 8 COMPLIED WITH SB A300-54-6023, REV NR 1 DATED 02-27-02 RE-ENFORCEMENT OF THE NR 1 PYLON CANTILEVER BUY ADDING DOUBLER UNDER THE HORIZ FIRE WALL AND ON THE LONGITUDISDR FDEA201107162765Rib · crackedLT WING INBD L/E INSIDE KRUGER FLAP WELL INBD RIB CRACKED IN JUST OTBD OF ACTUATOR UPPER SURFACE OF LWR ANGLE. R & R SUPPORT ANGLE IAW SRM 51-40-21, PARA 5.SDR FDEA201107152723Seat Track · crackedADAPTER AT FR 54.2, SEAT TRACK 4L AND SEAT TRACK-5L CRACKED 2 " LONG. R & R CLS ADAPTER AT FR 54.2, SEAT TRACK 4L AND 5L, LOCATED AND DRILLED TO MATCH ORIGINAL CONFIGURATION IAW SRM 51-40-44.SDR FDEA201107152722Skin · crackedAFT CARGO DOOR BOTTOM EXTERNAL SKIN IS CRACKED .10 INCH LONG JUST FORWARD OF 2ND HOOK FROM AFT LATCH HOOK. REMOVED DAMAGE ON EXTERNAL BOTTOM SKIN OF AFT CARGO DOOR IAW SRM 51-73-10, PAR F (6), AREA FOUND TO BE OUT OF LIMITS. R & R EXTERNAL BOTTOM SKIN OF ASDR FDEA201107152719Seat Track · corrodedCLS ADAPTOR BETWEEN SEAT TRACK 4L AND 5L, FR 48 HAS CORROSION AT FLOOR PANEL FLANGES / CORNER RADIUS, ABOUT 4 SQUARE INCHES. R & R CLS ADAPTOR IN AT FR 48 BETWEEN SEAT TRACK 4L AND 5L IAW SRM 51-72-10 PG 1-3.SDR FDEA201107152718Seat Track · corrodedFRAME 47 BETWEEN SEAT TRACK 4L AND 5L, CLS ADAPTOR HAS CORROSION AT FLOOR FLANGES/ CORNER RADIUS, ABOUT4 SQUARE INCHES. R & R CLS ADAPTOR FR-47, BETWEEN SEAT TRACK 4L AND 5L IAW SRM 51-72-10, PAGES 1-3.SDR FDEA201107122667Seal · chafedNR 2 ENGINE LT CORE COWL RAIN SEAL HAS CHAFED MARK TOP INNER AFT SIDE 1 IN LONG. R & R RAIN SEAL IAW SRM 51-72-10, PG 1,2 AND 3 DUE TO NO ALLOWABLE LIMITS.SDR FDEA201107092629Stiffener · crackedNR 2 PYLON UPPER L/E ACCESS HOLE 424 AR LANDING AREA METAL SEAT CRACKED .5" LONG. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-21 P 7.SDR FDEA201107092628Support · cracked2 PYLON UPPER L/E WEB SUPPORT RT LIGHTNING HOLE HAS 4EA CRACKS, 2EA 1.5" LONG AND 2EA 1" LONG, STA 537 TO STA 551. COMPLIED WITH SB A300-54-6023 REV 1. COMPLIED WITH EA 6-5450-145606.SDR FDEA201107092627Stiffener · crackedNR 2 PYLON UPPER L/E VERTICAL ANGLE HAS A CRACK 2" LONG AT LT SIDE ACCESS THRU 423AL AND STA 551. COMPLIED WITH SB A300-54-6023.SDR FDEA201107092626Angle · crackedNR 2 PYLON UPPER L/E VERTICAL ANGLE HAS CRACK 1.5" LONG RT SIDE ACCESS THRU 424 AR AT STA 551. COMPLIED WITH SB A300-54-6023 REV NR 1.SDR FDEA201107052590Retainer · damagedCUTOUT AFT FRAME BULB SEAL RETAINER DAMAGED. R & R AFT SEAL RETAINER.SDR FDEA201107052589Support Bracket · crackedLT PYLON HYD LINE SUPPORT ANGLE AT RIB 8 HAS 3 EACH CRACKS 1.5,1.0 AND .500 IN LENGTH. R & R SUPPORT BRACKET IAW SRM 51-40-21, PARA 7.SDR FDEA201107052588Seat Track · corrodedDUMMY TRACK 5L HAS CORROSION ON FLANGE AT FR 40. R & R DUMMY TRACK IAW SRM 51-72-10, PGS 1-3.SDR FDEA201107052587Seat Track · corrodedMAIN CABIN RT SIDE SEAT TRACK 6R FRAME 38.2-40 UPPER FLANGE HAS CORROSION AND 2 EA PLUGS IN SEAT TRACK. R & R SEAT TRACK IAW SRM 51-72-10, PGS 1-3.SDR FDEA201107022557Angle · crackedNR 2 PYLON AFT TOP U ANGLE SUPPORT IS CRACKED 1 IN LONG THROUGH A FASTENER. HOLE R & R ANGLE IAW SRM 51-40-21, PARA 7.
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