N653DL, cancelled Aug 21, 2018
Service difficulty reports · 43
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 = 'N653DL' AND deregistration_id = 'N653DL-2018-08-21' 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 = 'N653DL' AND deregistration_id = 'N653DL-2018-08-21' 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 DL757101266Wire Harness · damagedDURING LAYOVER CHECK, MX FOUND THE EMERGENCY PATH LIGHT AT ROW 38DEF INOPERATIVE. MX REPLACED THE LIGHT HARNESS. OPS CHECK WAS GOOD.SDR DL757100509Wire · unsecureSEVERAL CABIN EPATH LIGHTS INOP AT ROWS 4, 19, 26 AND 34. RESECURED WIRES AT AFFECTED SEATS. CHECKS OK.SDR DL757091464Fitting · damagedONE (1) EA HOLE IS ELONGATED ON LT WING O/B SIDELOAD FITTING. C/W ERA 476269-14 REV O.SDR DL757091466Bulkhead · gougedFOUND GOUGE ON SURFACE NR 1 PYLON BULKHEAD. C/W ERA 472263-14 REV O.SDR DL757091465Skin · damagedFOUND TWO (2) EA HOLES TO BE .500 AT RT STA 116.05. C/W ERA 476265-14 REV O.SDR DL757091463Structure · damagedAFTER REMOVAL OF LT SIDE NR 2 PYLON, FOUND 1 EA HOLE TO BE .500 AT LT STA 116.05. C/W ERA 476264-14 REV O.SDR DL757091467Bulkhead · chafedNR 1 PYLON BULKHEAD CHAFED. C/W ERA 476263 REV O.SDR DL757061027Light · inoperativeON APP GEAR SELECTED DOWN LEFT GEAR GREEN LIGHT DID NOT ILLUMINATE CHECKED LIGHT TEST BULB WAS OK AFTER GA. QRH PROCEDURE FOLLOWED AFTER RECYCLE OF GEAR LIGHT REILLUMINATED LND NML. NO ASSOCIATED EICAS ON CONFIG WARN NOTED. DEBRIEFED CREW FOUND LT GEAR GREESDR DU4R2006294Support · corrodedLOWER WING TO BODY FAIRING STRUCTURE CORRODED RT BS 880. REMOVED CORRODED T-ANGLE, FABRICATED AND INSTALLED REPAIR T-ANGLE 36.800" FROM BAC1505-101029 IAW B757 SRM 51-40-02, 51-20-01, AMM 51-00-00-01 AND DPS 900-2 NR 5.SDR DU4R2006290Frame · dentedAFT PIT STA 1320 S-25R - S-26R FRAME DENTED. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED FRAME REPAIR 26 X 5 INCHES FROM 7075-T6. 071 IAW B757 SRM 51-70-11 FIG 1 AND 51-40-02.SDR DU4R2006287Frame · bentFRAME AS STA 1440 , S-26L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 10.5 X 2.5 INCHES FROM 7075-T6 .063 AND CLIP P/N 3.30 X 1.75 INCHES FROM BAC1518-769 IAW B757 SRM 51-70-11, 51-20-01 AND 51-40-02.SDR DU4R2006292Floor Panel · corrodedCORROSION ON FWD PIT FLOOR PANEL LT NR 5 BS 750 - 845. REMOVED CORROSION IAW B757 SRM 51-10-02 FOUND L00 PERCENT MATERIAL LOSS IAW B757 SRM 53-00-53. FABRICATED AND INSTALLED REPAIR FLOOR PANEL 94 X 18 INCHES FROM 2024-T3 .020 IAW B757 SRM 53-30-53 AND 51-20SDR DU4R2006282Frame · bentFRAME AS STA 1300, S-26L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 11.40 X 2.50 INCHES FROM 7075-T6 .071 IAW B757 SRM 51-70-11 AND 51-20-1.SDR DU4R2006286Frame · bentFRAME AS STA 1240, S-26R IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 10.4 X 2.5 INCHES FROM 7075-T6 .080 IAW B757 SRM 51-70-11, 51-20-01 AND 51-40-02.SDR DU4R2006285Frame · bentFRAME AS STA 1480, S-26L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 10 X 2.4 INCHES FROM 7075-T6 .063 IAW B757 SRM 51-70-11, 51-20-01 AND 51-40-02.SDR DU4R2006284Frame · bentFRAME AS STA 1320, S-26R IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 13 X 4 FROM 7075-T6 .071 AND CLIP P/N 140N2063-56 IAW B757 SRM 51-70-11 AND 51-40-02.SDR DU4R2006283Frame · bentFRAME AS STA 1340, S-26R IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 13 X 4 INCHES FROM 7075-T6 .071 AND CLIP IAW B757 SRM 51-70-11 AND 51-40-02.SDR DU4R2006278Skin · dentedC-2 DOOR INTERNAL SKIN HAS 2EA DENTS (WITH CREASE MARKS) AT STA 1400. MEASURED DENTS A=.400", Y= .029 A/Y RATIO 13. FABRICATED AND INSTALLED INTERNAL FLUSH REPAIR 3.8 DIAMETER FROM 2024-T3 .063 IAW B757 SRM 52-30-01 FIG 201.SDR DU4R2006279Skin · crackedC-2 DOOR INTERNAL SKIN LWR AFT CORNER HAS CRACK STA 1440. CUT OUT EDGE CRACK ON C-2 DOOR EXTERNAL SKIN AT LOWER AFT CORNER STA 1140. FOUND WITHIN LIMITS IAW B757 SRM 52-30-01 DETAIL IV. HFEC PER NTM PT6 51-00-19, NO CRACK INDICATION. TREATED IAW B757 SRM 5SDR DUR42006293Floor Panel · corrodedFWD CARGO COMPT PIT FLOOR PANEL RT NR 5 CORRODED AT BS 750 - 845. REMOVED CORROSION IAW B757 SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-53. FABRICATED AND INSTALLED REPAIR FLOOR PANEL 94 X 18 INCHES FROM 2024-T3 .020 IAW B757 SRM 51-40-05 ANSDR DU4R2006289Seat Track · gougedMAIN CABIN SEAT TRACK FROM STA 760 TO STA 880 LBL 45 INNER SURFACE HAS MULTIPLE GOUGES. REMOVED GOUGED SECTIONOF SEAT TRACK. CUT, DRILLED UP AND INSTALLED NEW SEAT TRACK SECTION 10 X 1.5 INCH FROM BAC1520-792 IAW B757 SRM 51-20-01, 51-40-2, 51-40-05, 51-40-0SDR DU4R2006281Frame · bentFRAME AS STA 1400, S-25L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 22.5 X 3.75 INCHES FROM 7075-T6 .063, AND 2EA CLIPS P/N 140N2063-56 IAW B757 SRM 51-70-11 FIG 1, 51-20-2, 51-40-02.SDR DU4R2006280Frame · bentFRAME AS STA 1420, S-26L IS BENT. CUT OUT BENT PORTION. FABRICATED AND INSTALLED FRAME SECTION REPAIR 11.625 X 3.75 INCHES FROM 7075-T6 .063, FILLER AND CLIP P/N 140N2063-56 IAW B757 SRM 51-70-11 FIG 1, 51-20-2, 51-40-02.SDR DU4R2006291Floor Support · dentedFWD CARGO FLOOR SUPPORT HAS DENTS BETWEEN STA 580 & 600 AT LBL 2. CUT OUT DENTED SECTION. FABRICATED AND INSTALLED REPAIR 40.80 INCHES AND 2 EA SPLICES 10.00 X 1.10 X .75 AND 10.0 X 1.10 X .65 FROM BAC1517-2226 IAW B757 SRM 53-00-53, 51-70-11, 51-70-12, 51-2SDR DU4R2006288Skin · dentedDENT LEFT SIDE FUSELAGE SKIN 7 FEET FWD OF L-2 DOOR. CUT OUT DENTED PORTION. FABRICATED AND INSTALLED REPAIR DOUBLER 9.5 X 9.5 INCHES FROM 2024-T3 .020 CLAD AND ID TAG IAW B757 SRM 53-00-01, 51-20-01, 51-40-02 AND 51-40-08 AND PROCESS STANDARD 900-5-1, NR 4.SDR DL757040719Odor · detectedDURING FLIGHT TO DAY, BURNING PLASTIC SMELL IN MID GALLEY, THIS PER FLT ATTENDANT REPORT. CALLED CONTRACT MTC TO INVESTIGATE. CONTRACT MTC TURNED ON ALL MID GALLEY OVENS AND COFFEEMAKERS AND LIGHT. COULD NOT FIND ANY EVIDENCE OF A BURNING PLASTIC SMELL FROMSDR DL757030966Control Panel · overheatedSMOKE OBSERVED DURING FINAL APPROACH, AFTER NOSE GEAR LANDING LIGHT, TAXI LIGHT AND TURNOFF LIGHT WERE ILLUM. SMOKE OBSERVED AT LWR PORTION OF O/H PNL JUST BELOW LIGHT SWITCH. FOUND WIRE CONNECTORS AT TURNOFF LIGHT SWITCHES S1 AND S2 OVERHEATED. CHECKED ANDSDR DL757030182Eec · unserviceableLT ENGINE PRIMARY CONTROL STATUS MSG, LT ENGINE FAILED. REPLACED NR 1 ENGINE EEC. PERFORMED WINDMILL INSPECTION ON ENGINE. NO DEFECTS NOTED.SDR DL757010477Slat Track · damagedLE FLAP ASSY ON FLAP RETRACTION - DECLARED EMERGENCY AND LANDED WITH NO INCIDENT. MTC IN WORK - FOUND NR 2 LE SLAT TRACK BROKEN LOOSE ON ARRIVAL.SDR DL757001074Skin · lightning strikeTHE FUSELAGE CROWN SKIN SUFFERED A LIGHTNING BURN AT FS 590 AND STRINGER 1, ADJACENT TO THE ANTI-COLLISION LIGHT INSTALLATION. THE SKIN DAMAGE WAS REMOVED WITH A 1.25 DIA CUTOUT. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER SIZED TO REPASDR DL757001073Skin · lightning strikeTHE FUSELAGE CROWN SKIN BETWEEN FS 680 & 700 AND STRINGERS 1 AND 2L SUFFERED TWO LIGHTNING BURNS. THE TWO LOCATIONS WERE REMOVED WITH 1 INCH DIAMETER CUTOUTS IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 37SDR DL757001054Skin · lightning strikeTHE FUSELAGE SKIN WAS FOUND WITH LIGHTNING STRIKE DAMAGE BETWEEN FS 460 AND 500 NEAR STRINGER 2R. THE DAMAGE WAS REMOVED WITH THREE SMALL 1 INCH CUTOUTS IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 377418-SDR DL757972504Skin · crackedDURING INSPECTION OF A PREVIOUSLY ACCOMPLISHED REPAIR ON THE NR 1 ENGINE NACELLE STRUT SKIN AN ADDITIONAL CRACK WAS FOUND EMANATING FROM THE CUTOUT. REPAIRED PER ERA 331028-14.SDR DL757972503Sill · corrodedCORROSION WAS FOUND ON THE C1 DOOR LWR SILL OUTBD CHORD. REPAIRED PER ERA 331050-14.SDR DL757962731Bushing · wornDURING ACCOMPLISHMENT OF INSPECTION PER OPN 8201, OUTBOARD MIDSPAR FITTING BUSHING ON THE NR 2 ENGINE WAS FOUND TO HAVE MIGRATED .150 AND WAS LOOSE. THIS ER/A AUTHORIZES REPLACEMENT OF THE BUSHING PER BACO S/B 757-54-0026. DIA OF OUTBOARD LUG PRIOR TO REWORKSDR DL757954798Skin · crackedPYLON SKIN CRACKED NR 2 PYLON O/B SIDE AT FWD ACCESS HOLE, 1 PLACE. REMOVED FASTENERS/CRACK PER SRM 54-51-01 AND INSTALLED DOUBLER PER SRM 54-51-01.SDR DL757954797Skin · crackedPYLON SKIN CRACKED NR 2 PYLON I/B SIDE AT FWD ACCESS HOLE, 2 PLACES. DRILLED OUT ALL FASTENERS, CUT OUT DAMAGED AREA, DRILLED AND INSTALLED REPAIR PER 54-50-01 PG 207.SDR DL757953931Latching Mech · out of rigCLIMBING THROUGH 2500 FT, CENTER ENTRY DOOR LIGHT ILLUMINATED. DOOR HANDLE WAS HELD CLOSED BY FLIGHT ATTENDANT TO PREVENT IT MOVING TO OPEN POSITION. INSPECTED 2 RT DOOR, FOUND UNLATCHING FORCE BELOW MINIMUMS. ADJUSTED PER MM 52-11-00 DOOR LATCHING FORCE WISDR DL757952622Radome · delaminatedRADOME WAS ROUTED TO SHOP FOR DELAMINATION, DUE TO LIGHTNING STRIKE. REPAIRED PER SRM 53-10-72.SDR DL757951938Skin · delaminatedDURING SHOP INSP, THE T/E WEDGE WAS FOUND TO BE DELAMINATED. REPLACED T/E WEDGE PER SRM 57-43-02 FIG 202.SDR DL757951905Te Skin · crackedFOUND DURING LETTER CHECK, I/B FLAP BOTTOM T/E CRACKED O/B OF AFT TRUNNION FAIRING, LT WING. REPAIRED PER SRM 51-70-07 AND PAINTED.SDR DL757951904Radome · dentedDURING LETTER CHECK, FOUND RADOME WITH DAMAGED AREA AT RBL 34.5, WL 190, A 1 BY 7 DENT ON RT SIDE. REPAIRED DAMAGED AREA OF RADOME AS PER SRM 53-10-72 AND PAINTED.SDR DL757951849Skin · delaminatedUPPER OUTBOARD SECTION OF TRAILING EDGE WEDGE DELAMINATED. LOWER SKIN OF TRAILING EDGE WEDGE PUNCTURED. REPLACED TRAILING EDGE WEDGE AS PER SRM 57-43-02. FOUND AND REPAIRED DURING SHOP INSPECTION.
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