N650DL
Service difficulty reports · 236
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 = 'N650DL' 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 = 'N650DL' 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 DALA2015102206385Stringer Splice · corrodedAFT PIT BILGE AREA; CORROSION FOUND AT BS 1460, S29L. REMOVED CORROSION AT AFT CARGO BAY BS 1460, S29L SPLICE IAW SRM 51-10-02, SPLICE WITH ORIGINAL THICKNESS OF .100 MATERIAL LOSS .033, MATERIAL REMAINING .067 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03. R SDR DALA2015102206363Stringer Splice · corrodedAFT CARGO BILGE HAS CORROSION FOUND AT BS 1460, S28L. REMOVED CORROSION ON AFT PIT BILGE STR 28L SPLICE BS 1460 IAW SRM 51-10-02 AREA WITH ORIGINAL THICKNESS OF .100 MATERIAL LOSS .028 MATERIAL REMAINING .072 AREA FOUND TO BE WITH OUT OF LIMITS IAW SRM 53-00-SDR DALA2015102106314Cusp Web · corrodedMAIN CABIN LT CUSP WEB SECTION CORRODED BS 1100 LBL 70. REMOVED CORROSION IAW ERA 536297-14, REV O.SDR DALA2015102106313Deck Plate · corrodedMAIN CABIN AFT WET AREA, CORROSION ON FLOOR DECK PLATE, NUMEROUS SPOTS FROM BS 1681-1718, LBL60-RBL60. BIGGEST MEASURED 11" X 3.5", CP53- 252-01. REMOVED MAIN CABIN AFT WET DECK PLATE FROM BS 1680-1720, LBL 60-RBL 60 IAW SRM 51-40-02, FABRICATED NEW DECK PLASDR DALA2015102106312Support Channel · corrodedL-1 DOOR AREA SUPPORT CHANNEL FOR AFT DRAIN HAS SURFACE CORROSION , BS 370, LBL 55. CP53-221-01. R & R L-1 DOOR AREA SUPPORT CHANNEL, BS 370, LBL55, USING PN 161N5170-48, PO 650DL-00146 IAW ENG 141N5170, REV C, CPM 20-40-00, SRM 51-20-01, SRM 51-40-02, AND SRSDR DALA2015102106310Floor Support · damagedMAIN CABIN, FLOOR STRUCTURE INTERCOSTAL IS DAMAGED BETWEEN BS 860-879 BL0. REMOVED MAIN CABIN INTERCOSTAL ANGLE AT BS 860-879 BLO IAW SRM 51-40-02, FABRICATED INTERCOSTAL ANGLE IAW DWG 143N5157, REV: A, PN 7075-O .032, O.O. ST00006259 1" X 18" HEAT TREATED TOSDR DALA2015102106311Support Channel · corrodedR-1 DOOR AREA SUPPORT CHANNEL FOR FWD DRAIN HAS SURFACE CORROSION BS 335, RBL 55 AND BS 345, CP53-222-01. R & R SUPPORT CHANNEL AT R1 DOOR, BS 335, RBL 55 IAW ENGINE DWG 141N5160, REV B, SRM 51-40-02, SRM 51-20-01, SRM 51-40-05, SRM 53-00-15. PN 141N5160U79 SDR DALA2015101906285Floorbeam · corrodedMAIN CABIN WET AREA, CORROSION ON FLOORBEAM, BS 1640, RBL 5 1.5" X 1.5" CP 53-252-01. INSTALLED ID TAG IAW PS 900-5-1, NR 4.SDR DALA2015101906284Frame · corrodedMAIN CABIN AFT SECTION , FRAME AT BS 1640 IS CORRODED AT FLOOR LEVEL, RBL 58, 2.5" X 1.5" CP 53-252-01. INSTALLED REPAIRS PARTS IAW ERA 532900-14AD.SDR DALA2015101906283Frame · corrodedAFT MAIN CABIN AREA, FRAME CORRODED AT BS 1640, LBL 55, JUST FWD OF L-4 DOOR. INSTALLED REPAIRS PART IAW ERA 536296-14AD, REV 1.SDR DALA2015101806279Floor Support · crackedFLOOR SUPPORT CRACK BELLOW MAIN CABIN FLOOR APPROXIMATELY BL0 BETWEEN BS 440 AND BS 460. R & R FLOOR SUPPORT UPPER ANGLE BS 440-460, BL "0" IAW DWG 143N5140, REV C. INSTALLED NEW ANGLE IAW DWG 143N5140, REV C.SDR DALA2015101806278Floor Support · corrodedL-4 DOOR CUTOUT LOWER FLOOR SUPPORT BETWEEN BS 1660 TO 1680 LBL, 50 CORROSION WITH AN AREA OF EXFOLIATION. REMOVED CORROSION ON FLOOR SUPPORT BETWEEN BS 1660 TO 1680 LBL 50 IAW SRM 57-10-02 AREA WITH ORIGINAL THICKNESS .063 MATERIAL LOSS .063 MATERIAL REM "0"SDR DALA2015101806277Floor Support · corrodedL4 DOOR CUT OUT LOWER FLOOR SUPPORT BETWEEN BS 1640 TO 1661 LBL, 50 AREAS WITH HEAVY CORROSION. REMOVED CORROSION ON FLOOR SUPPORT BETWEEN BS 1640 TO 1661, LBL 50 IAW SRM 51-10-02 AREA WITH ORIGINAL THICKNESS .063 MATERIAL LOSS .050 MATERIAL REMAINING .013 FSDR DALA2015101506211Stiffener · corrodedMAIN CABIN AFT DECK PLATE BS 1715, LBL 49 FLOOR SUPPORT STIFFENER CORRODED. REMOVED CORRODED STIFFENER FROM AFT DECK PLATE AT BS 1715, LBL 49, FABRICATED NEW FROM 7075-0.071 PO 00006180, DIM 10.80" X 2.00", HEAT TREATED TO 7075-T6 AND INSTALLED IAW SRM 51-40-SDR DALA2015101506210Stiffener · corrodedMAIN CABIN AFT CHECK PLATE BS 1715, RB 49 FLOOR SUPPORT STIFFENER CORRODED. REMOVED CORRODED STIFFENER FROM AFT DECK PLATE, BS 1715, RBL 49. FABRICATED NEW FROM 70750.071 PO ST-00006180, DIM 10.85" X 2" HEAT TREATED TO 7075T6, AND INSTALLED IAW SRM 51-40-02SDR DALA2015101506208Floorbeam · corrodedMAIN CABIN AFT CHECK PLATE, BS 1715, FLOOR SUPPORT STIFFENER, LBL 33-39 CORRODED. REMOVED CORRODED STIFFENER FROM AFT DECK PLATE BS 1715, LBL 33-39, FABRICATED NEW FROM 7075-0, .071, PO 00006180, DIM 6.0" X 2.00", HEAT TREATED TO 7075-T6 AND INSTALLED IAW SRMSDR DALA2015101506207Floorbeam · corrodedMAIN CABIN AFT DECK PLATE BS 1715, FLOOR SUPPORT, LBL 20-26 CORRODED, STIFFENER, CP 53-252-01. REMOVED CORRODED STIFFENER FROM AFT DECK PLATE BS 1715, LBL 20- 26, FABRICATED NEW FROM 7075-0, .071 PO 00006180, DIM 5" X 2", HEAT TREATED TO 7075-T6 AND INSTALLEDSDR DALA2015101506206Shear Web · corrodedMAIN CABIN AFT SHEAR WEB BS 1720 BETWEEN LBL 60 TO RBL 60 SUPPORT CORRODED AT RBL 56, PARTS RACK, CP 53-252-01. R & R MAIN CABIN AFT SHEAR WEB , BS 1720, LBL 60-RBL 60, IAW ENGINE DWG 146N5300, REV, SRM 51-40-01, SRM 51-40-02, SRM 51-40-04, SRM 51-40-05, ANDSDR DALA2015091505655Support · damagedER/A 471162-14, REV C, LT WING, INBD FLAP, INBD CARRIAGE, AFT ROLLER SUPPORT, ELONGATED HOLES, SECTION II INSPECTIONS.SDR DALA2014063003840Wire · damagedFOUND ASILE EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 19-24. FOUND BAD SPLICE AT ROW 24. REPAIRED IAW SWPM 20-10-30.SDR DALA2014062503778Charger · inoperativeROW 19DEF-23DEF, EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER ASSY IAW AMM 33-51.SDR DALA14019790650Lens · missingEMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. REINSTALLED EMERGENCY EXIT SIGN LENS.SDR DALA14010320650Connector · unsecureEMERGENCY LIGHTS AT ROWS 23 INOPERATIVE. FOUND LOOSE SEAT HARNESS CONNECTION. SEATED & LOCKED, CHECKED GOOD.SDR DALA14010070650Wire · looseFIRST CLASS AND FWD GALLEY EMERGENCY LIGHTS INOPERATIVE. REMOVED POWER SUPPLIES M9101 AND M731 082155 TEMP INST 3 NEW POWER SUPPLIES FOR T/S LIGHTS WORK ONLY FROM L1 TEST SWITCH. COCKPIT SWITCH AND F/A PANEL NOT ACTIVATING ALL LIGHTS. REINSTALLED ALL ORIGISDR DALA14009300650Switch · failedON ARRIVAL, FOUND EMERGENCY EXIT LIGHTS WERE UNCONTROLLABLE. R & R EMERGENCY LIGHT TEST SWITCH ABOVE L1 DOOR. LIGHTS OPERATE NORMALLY AT THIS TIME, AMM 33-51.SDR DALA14008330650Pan · corrodedAFT CARGO BAY, AFT OF AFT BULKHEAD PANEL, EVIDENCE OF LAVATORY DUMP TUBE LEAKING AT CONNECTION TO SERVICE PANEL, BLUE WATER STAINED AND CORROSION ON LAVATORY PAN. CORROSION FOUND TO BE 100 PERCENT MATERIAL LOSS IAW SRM 51-10-02. DOUBLER FABRICATED IAW DWG 14SDR DALA1315020650Engine · failedEMERGENCY DECLARED DUE TO LEFT ENGINE COMPRESSOR STALL AND IN FLIGHT ENGINE SHUTDOWN. MX FOUND METAL IN TAILPIPE. R & R ENGINE.SDR DALA1302220650Skin · damagedDURING WAKE-UP, FOUND A SCRATCH ON THE FUSELAGE AFT OF FORWARD CARGO DOOR. STA 640 STR 23R. REMOVED .010 OF MATERIAL IAW SRM 53-00-01, PG 104, DETAIL 2 WHICH IS WITHIN LIMITS IAW SKIN THICKNESS SRM 53-30-01, PG 4. APPLIED ALODINE AND PAINT. PERFORMED HFEC SDR DALA1234930650Trunnion · corrodedCORROSION WAS FOUND ON THE NOSE LANDING GEAR INBD AND OTBD TRUNNION FITTINGS. BOTH BORES WERE ENLARGED TO A DIA OF 2.813 INCHES FROM AN ORIGINAL SIZE OF 2.762 INCHES. THE INBD TRUNNION FITTING FACE WAS CORRODED REQUIRING REMOVAL WITH SPOTFACE DIA 3.440 INCHESDR DALA1207370650Light · not seatedLINE MAINTENANCE FOUND EMERGENCY EXIT PATH LIGHT INOPERATIVE AT SEATS 19-23 AND EXIT SIGN LIGHT AT R4 WAS INOPERATIVE. LOOSE WIRING AT SPLICE AT SEAT 23 WAS RE-SECURED AND BULB IN EXIT SIGN WAS RESEATED. ALL LIGHTS OPERATING NORMALLY.SDR DALA1514020650Seat · mismanufacturedSEATS, AT ROW 18DE, MISMANUFACTURED ANGLE REPAIRED IAW ERA 496082-14.SDR DALA1107240650Wire · damagedDURING A LAYOVER CHECK, MX FOUND THE FWD CABIN, RED EMERGENCY PATH LIGHT INOPERATIVE. MX REPAIRED THE LIGHT WIRING. OPS CHECK WAS GOOD.SDR DALA1107230650Socket · damagedDURING A LAYOVER CHECK, MX FOUND THE EMERGENCY PATHLIGHT AT SEAT 32D INOPERATIVE. MX REPAIRED THE LIGHT SOCKET. OPS CHECK WAS GOOD.SDR DALA1513910650Tear Strap · debondedFUSELAGE SKIN TEARSTRAP DISBOND, REPAIRED IAW AA 5331-01238.SDR DL757081583Sill · damagedDURING HMV, TWO FASTENER HOLES WERE MISDRILLED IN THE INNER CHORD OF THE LOWER SILL OF THE AFT CARGO DOOR CUTOUT AT STA 1360. THE OVERSIZE HOLES WERE PLUGGED AND A REPAIR ANGLE WAS INSTALLED PER REPAIR INSTRUCTIONS.SDR DL757081582Frame · gougedDURING HMV, TWO GOUGES WERE FOUND IN THE WEB OF THE STA 395 FRAME BETWEEN S11L AND S13L. A NEW FRAME SECTION WAS SPLICED IN BETWEEN S10L AND S11L PER BOEING REPAIR INSTRUCTIONS.SDR DL757081566Panel · inoperativeOXYGEN DOORS AT ROWS 21 DEF, 26 DEF AND 28 ABC DO NOT DROP WHEN FUNCTIONAL CHECK IS PERFORMED. SOLENOIDS DO DISENGAGE. CLEANED AND ADJUSTED DOOR LATCH ACTUATOR ON 21 DEF, 26 DEF AND 28 ABC IAW AMM 35-21-06-404-007. OPS CHECK GOOD IAW AMM 35-21-00-705-0766.SDR DL757081558Panel · stuckROW 2 CD AND ROW 26 ABC OXYGEN PANEL WILL NOT DROP. DOOR LATCH ACTUATORS FOUND STICKING. ACTUATORS EXERCISED. NO DEFECTS NOTED IAW SOPM 20-00-00 PAR 1D.SDR DL757081541Socket · dirtyEXTERNAL EMERGENCY LIGHTS INOP. REMOVED, CLEANED, AND REINSTALLED SOCKETS IAW AMM 33-51-06-962-049. REPLACED LAMPS IAW AMM 33-51-06-962-042. OPS CHECK GOOD IAW AMM 33-51-00-715-075.SDR DL757081485Strut · damagedDURING THE PYLON MOD, THE NR 2 PYLON LT SIDE STRUT WAS FOUND WITH SEVEN OVERSIZE HOLES. SIX OF THE HOLES WERE CLEANED UP FOR OVERSIZE FASTENERS AND ONE HOLE WAS BUSHED TO THE ORIGINAL HOLE SIZE PER BOEING INSTRUCTIONS.SDR DL757081484Carriage · damagedDURING HMV, FOUR ELONGATED BOLT HOLES WERE FOUND IN THE LT WING INBOARD MAIN FLAP INBOARD CARRIAGE ASSEMBLY. THE ELONGATED HOLES WERE REAMED TO ROUND HOLES AND OVERSIZE BOLTS WERE INSTALLED PER BOEING INSTRUCTIONS.SDR DL757081476Bulkhead · chafedDURING HMV AT SAA, THE NR 1 PYLON AFT BULKHEAD LOWER OUTBOARD FLANGE AT NAC STA 203 WAS FOUND CHAFED WHILE ACCOMPLISHING THE PYLON MOD PER SB-757-0034. THE BULKHEAD WAS REPAIRED PER BOEING INSTRUCTIONS.SDR DL757081538Bulkhead · chafedNR 1 PYLON BLKHD (AFT) LWR OUTBD CORNER IS CHAFED. PYLON REPAIRED IAW ERA 471168-14 AD REV 0.SDR DL757081551Frame · corrodedAFT CARGO COMP STA 1560 HAS CORROSION ON FRAME ABOVE L27. BLENDED AREA IAW SRM 53-00-07 PG 103 FIG 101. FOUND OUT OF LIMITS. INSTALLED REPAIR DOUBLER IAW SRM 51-40-07 PG 4 PARA 7.SDR DL757081581Frame · dentedMAIN CABIN FRAME STA 395 LT SIDE FWD CABIN 2 DENTS. BLENDED GOUGES, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 PG 103 DETAIL II. INSTALLED REPAIR PARTS AT FRAME 395 IAW ERA 461183-14 STEP 8.SDR DL757081577Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 365.25 RBL 18 CORRODED. REMOVED DAMAGED FLOOR BEAM IAW SRM 51-40-02 FIG 8 PG 31. REINSTALLED REPAIR PIECE IAW SRM 51-40-05 PG 4 PARA 4.SDR DL757081576Floorbeam · corrodedMAIN CABIN FLOORBEAM CAP 4 INCHES AFT STA 365.25 RBL 54 CORRODED. REPLACED DAMAGED FLOORBEAM CAP AT STA 365.25 TO 395 RBL 54 IAW SRM 51-40-02 FIG 8 PG 31 AND SRM 51-40-02 PG 7 PARA 7D.SDR DL757081557Floorbeam · corrodedMAIN CABIN FLOORBEAM END CAP STA 365.25 RBL 10 CORRODED. REMOVED END CAP IAW SRM 51-40-02 FIG 8 PG 31. INSTALLED REPLACEMENT CAP IAW SRM 51-40-02 PG 4 AND 7.SDR DL757081549Floorbeam · corrodedMAIN CABIN FLOOR CONNECTING CHANNEL 5 INCHES FWD STA 350 LBL 34 CORRODED. REMOVED AND REPLACED DAMAGED SUPPORT IAW SRM 51-40-02 PG 2 PARA 4.SDR DL757081548Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 1640 BL "0" TO RBL 12 UPPER SURFACE OF FLOORBEAM IS CORRODED HEAVILY. REPAIRED IAW SRM 53-00-51, REPAIR 3 FIG 201.
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