N156DL, cancelled Aug 25, 2023
Service difficulty reports · 177
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 = 'N156DL' AND deregistration_id = 'N156DL-2023-08-25' 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 = 'N156DL' AND deregistration_id = 'N156DL-2023-08-25' 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 MK1Y20230503023Unknown · unknownSTA 139 - ATA 180.5, BELOW WINDOWS R1 AND R1: DURING MAINTANACE INSPECTION AT IAI, SHOP FOUND TWO (2) DOCUMENTED REPAIRS AT THE NOTED LOCATION. FWD REPAIR: LIGHTNING STRIKE REPAIR AT STA 139, BELOW WINDOW R1. AFT REPAIR: A DOUBLER REPAIR ON THE EXTERNAL FUS SKSDR MK1Y20230503022Unknown · unknownSTRUT #2, AFT FAIRNG - TRAILING EDGE, RH AND LH, NAC STA 410 TO 413: DURING MAINTENANCE INSPECTION AT IAI FACILITES, SHOP DISCOVERED UNDOCUMENTED DOBULER REPAIR IN STRUT #2, SKIN PANELS, ON BOTH SIDES.SDR MK1Y20230503021Unknown · unknownEXTERNAL FUSELAGE SKIN, STA 661, STR-30R-STR-31R: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE BULGE ON FUSELAGE SKIN LOCATED AT STA 661, 2-INCH BELOW THE STR 30R. INITIAL DIMENSION OF BULGE IS A=0.57”, Y=0.0278” (A/Y=20). BULGE IS OUT OF LIMITS PER SRSDR MK1Y20230503020Unknown · unknownSEC 46 FUSELAGE SKIN, STA 1564.3, 5” ABOVE STR 16L: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE DENT ON FUSELAGE SKIN LOCATED AT STA 1264.3, 5” ABOVE STR 16L. INITIAL DIMENSION OF DENTED AREA A=0.720”, Y=0.032” (A/Y=22). DENT IS OUT OF LIMITS PER SRM SDR MK1Y20230503019Unknown · unknownSECTION 41 – FUSELAGE SKIN – STA 422 BETWEEN STR 31L AND STR 32L: A BULGE OUT OF LIMITS ON THE FUSELAGE SKIN WAS REPAIRED PER SRM 53-00-01 REPAIR 8SDR MK1Y20230503018Unknown · unknownSECTION 43 FUSELAGE SKIN STA 669.3 BETWEEN STR 35L AND STR 36L: AN EXISTING BULGE OUT OF LIMITS ON FUSELAGE SKIN WAS REPAIRED PER SRM 53-00-01 REPAIR 8.SDR MK1Y20230503017Unknown · unknownSEC 43 FUSELAGE SKIN, STA 600.8 BTWN STR 32L-33L: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE DENT ON FUSELAGE SKIN LOCATED AT STA 600.8 BETWEEN STR 32L AND STR 33L. INITIAL DIMENSION OF DENTED AREA A=0.680”, Y=0.027” (A/Y=25). DENT IS OUT OF LIMITS PSDR MK1Y202305173016Unknown · unknownR/H MLG DOOR: MAINTENANCE DISCOVERED A PUNCTURE AT THE INNER SKIN OF R/H MLG DOOR IN A CRITICAL AREA (LESS THAN 10 INCHES FROM THE CENTER HINGE). SHOP REPORTED SEVERAL DAMAGES NEAR THE NOTED PUNCTURE. ALL OTHER DAMAGES WERE REPAIRED PER SRM 52-80 REQUIREMENTS.SDR MK1Y202305173015Unknown · unknownDURING CONVERSION OF S/N 25354, MAINTENANCE WAS REQUIRED TO REPLACE ENGINE #2 INLET COWL. THE REPLACEMENT INLET COWL P/N 224-2101-563, S/N 0634RV860 PROVIDED BY COSTUMER. THE NOTED INLET COWL WAS INSTALLED ON A/C AND POLISHED. MAINTENANCE REPORTED CORROSION/PISDR MK1Y20230503014Unknown · unknownDURING MAINTENANCE INSPECTION SHOP FOUND EXISTING LATCH REPAIR DOUBLER ON THE OUTBD CORE COWL ENG #2 B/T NAC STA 267 TO 274.5 AT 6 O’CLOCK, CENTER LATCH. DURING DISASSEMBLE THE EXISTING DOUBLER, SHOP FOUND TWO (2) ELONGATED HOLES, 1 HOLE IN DIA 0.328” AND THE SDR MK1Y202305173013Unknown · unknownBT STA 1518-1562, STR 38L-37R: DURING DAMAGED SHEAR TIE P/N 140T2102U585 REMOVAL IN ORDER TO INSTALL NEW SHEAR TIE SHOP MISTAKENLY DOUBLE DRILLED THE TEAR STRAP AND SKIN AT 4EA HOLES. THE ORIGINAL HOLE DIA 0.186”. THE HOLES WERE DRILLED UNTIL THE WHOLE DAMAGE SDR MK1Y202305173006Unknown · unknownENG #2, INBD SIDE CORE COWL, S/N 0982, P/N 224M4761-513:
DURING NAINTENANCE INSPECTION SHOP FOUND SEVERAL LOOSE FASTENERS IN THE
EXTERNAL CORE COWL SKIN ON THE INBD SIDE OF ENF #2 BETWEEN NAC STA 303.75 TO
306.75 AT 6 O'CLOCK. AFTER REMOVING THE LOOSE FASTESDR MK1Y20230503001Unknown · unknownCORE COWL, P/N 224-2302-345, S/N 1198: DURING MAINTENANCE INSPECTION AT IAI FACILITIES. AN UNDOCUMENTED DOUBLER REPAIR LOCATED BETWEEN NAC STA 280 AND 288 AT 10 O'CLOCK. SIZE: 7.4"X4.6".
M0566 – A CRACK STRETCHING FROM THE FASTENER TO THE AFT EDGE OF THE EXSDR MK1Y20230503012Unknown · unknownOUTB’D FAN COWL ENG #2 S/N 0424 P/N 224-2202-507. DURING MAINTENANCE CHECK AT IAI FACILITIES, SHOP DISCOVERED THE FOLLOWING FINDINGS: DENT IN THE EXTERNAL FAN COWL SKIN, COMMON TO NAC STA 182.5. 59” AWAY FROM THE BOTTOM EDGE OF THE FAN COWL. THE FIBERS ARE DSDR MK1Y20230503011Unknown · unknownSTA 236.5, LBL 69.25: DURING MAINTENANCE INSPECTION SHOP FOUND FLOOR BEAM AND SHEAR WEB WITH MISSING MATERIAL.SDR MK1Y20230503010Unknown · unknownFUS. SKIN, SEC 48, BT STA 1809.5 – STA 1824, ABOVE STR 22L: DURING MAINTENANCE INSPECTION SHOP FOUND UNDOCUMENTED REPAIR ON THE EXTERNAL FUS SKIN, P/N 148T3181-7. A REVIEW OF THE PREVIOUS OPERATOR’S RECORDS (DAL) WAS PERFORMED AND NO DOCUMENTATION WAS FOUND. TSDR MK1Y20230503009Unknown · unknownSEC 46, STA 1197 – 1197=22, STR 38L -38R: UNDOCUMENTED DOUBLER REPAIR FOUND NEXT TO DOCUMENTED DOUBLER BETWEEN STA 1189 – 1197=14, STR35L – 38L, DOCUMENTED ON ERA 518660-14AD.SDR MK1Y20230503008Unknown · unknownDURING MAINTENANCE INSPECTION, SHOP FOUND A LIGHTNING ST88IKE DAMAGE ON SKIN, AT A BUTT JOINT AT THE NOTED AREA. SHOP PERFORMED 0.4"X1.0" SIZE BLEND OUT ON THE DAMAGED AREA. AFTER NDT INSPECTIONS, IT WAS FOUND THAT THE MINIMUM THICKNESS IS 0.54", AND THE NOMINSDR MK1Y20230503007Unknown · unknownTAILCONE OUTER SKIN BTWN STA 1943.5-1952: DURING CONVERSION AT IAI IN TLV, MTX FOUND SEVERAL DAMAGES AND UNDICUMENTED REPAIRS ON OUTER TAILCONE SKIN. THE FOUNDS WERE: -BLEND OUTS; - WELDING REPAIRS; - LIGHTNING STRIKES; - FASTENER REPAIRS. SOME OF THESE FOUNDISDR MK1Y20230503005Unknown · unknownDURING AIRCRAFT CARGO CONVERSION, A 0.186" DIAMETER INITIAL FASTENER HOLE WAS MISTAKENLY DAMAGED IN THE STA 1065 BULKHEAD WEB AND NO. 6 STIFFENER. THE BULKHEAD STRUCTURE IS CLASSIFIED AS PRIMARY STRUCTURE, A PSE, AND FCBS (NOTE 1) PER REF 767-300 SRM 51-00-04,SDR MK1Y20230503004Unknown · unknownDURING MAINTENANCE INSPECTION AT IAI FACILITIES, SHOP DISCOVERED THE FOLLOVING FINDINGS: M0547 – AN UNDOCUMENTED DOUBLER REPAIR LOCATED BETWEEN NAC STA 286.55 AND 288.95 AT 6 O'CLOCK. SIZE: 5.6"X3.6". M0592 – AN UNDOCUMENTED DOUBLER REPAIR LOCATED (TITANIUSDR MK1Y20230503003Unknown · unknownSTRUT #2, L/H, NAC STA 285.45 TO 289.95, UNDERWING FAIRING: DURING MAINTENANCE INSPECTION AT IAI FACILITIES, SHOP DISCOVERED UNDOCUMENTED DOUBLER REPAIR.SDR MK1Y20230503002Unknown · unknownFUSELAGE SKIN REPAIR, BETWEEN STA 157 AND STA 162, ABOVE STR-21L: DURING MAINTENANCE CHECK, IAI SHOP DISCOVERED AN EXISTING REPAIR IN FUSELAGE SKIN LOCATED AT THE NOTED AREA. THE FLUSH REPAIR IS LOCATED IN THE EXTRA CRITICAL AREA, FWD TO THE PITOT STATIC PROBESDR DALA2020070762549Battery Pack · inoperativeEMERGENCY EXIT LIGHT OVER WING LEFT SIDE IS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.SDR DALA2020070762548Battery Pack · inoperativeEMERGENCY EXIT LIGHT SIGN AT P12 INOPERATIVE. REPLACED BATTERY. SYSTEM OPERATION IS NORMAL.SDR DALA2020051902410Warning System · false activationSHIP 1506 - ATO - ON T/O ROLL, LT YAW DAMP MESSAGE & OVERHEAD LIGHT ILLUMINATED. CORRECTIVE ACTION: INITIALLY APPLIED MEL 22-21-01. DURING RON, PERFORMED SYSTEM BITE & MCDP TESTS 30 & 40. OPERATIONAL CHECK OK. LP 7043212SDR DALA2020040602180Battery Pack · dischargedDURING SERVICE CHECK FOUND BACK CEILING EMERGENCY LIGHTS OUT EXTENDING FROM ROW 35A INTO AFT GALLEY. REPLACED BATTERY PACK. SYSTEM OPERATION IS NORMAL.SDR DALA2020020300825Battery Pack · inoperativeEMERGENCY EXIT SIGN AFT CEILING ARE INOPERATIVE. REPLACED BATTERY M739. SYSTEM OPERATION IS NORMAL.SDR DALA202002030826Battery Pack · inoperativeEMERGENCY LIGHTS AT 34-40AB ON CEILING ARE INOPERATIVE. REPLACED BATTERY AT M739. SYSTEM OPERATION IS NORMAL.SDR DALA2019112506897Charger · inoperativeDURING SERVICE CHECK FOUND AFT 3 LEFT EXTERNAL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM OPERATION IS NORMAL.SDR DALA2019111046511Connector · disconnectedEMERGENCY FLOOR PATH LGITHS ARE INOPERATIVE AT SEAT 39B. RECONNECTED LIGHT ASSEMBLY.SDR DALA2019110106344Battery Pack · inoperativeFOUND EXTERIOR EMERGENCY LIGHT LEFT SIDE L396 AND L645 NOT ILLUMINATING DURING TEST. REPLACED BATTERY PACK ON M738. SYSTEM OPERATION IS NORMAL.SDR DALA2019102196016Skin · cracked#1 PYLON OB SIDE STRUT SKIN HAS 2" CRACK ABOVE 432AL. VERIFIED WITH HFEC SCAN TAG # 6741, CREATE EWO FOR REPAIR. REPAIRED #1 PYLON OB STRUT SKIN IAW ERA 581953-14 REV O. JOB COMPLETE. (LP1321034)SDR DALA2019101765940Skin · crackedNUMBER 1 PYLON PANEL 436CR HAS HOLE ELONGATED , CRACKED ON INNER SKIN AND SPRING SEAL WORN (M) MOORE 350206 09/09/19 (ON REPAIR RACK). REPAIRED PYLON PANEL 436CR I/A/W ERA 581311-14 REV O. (LP1316822)SDR DALA2019101405892Panel · corrodedALC BILGE PNL STA 1153-1175 LBL20-RBL20 CORROSION AT NUMEROUS PLACES. REPAIR BILGE PNAL IAW ERA 581853-14 REV O.SDR DALA2019101105845Skin · bentNO. 2 ENG OUTBD CORE COWL 1ST LATCH HAS BENT SKIN ABOVE LATCH. MARKED. NO. 2 ENG OOUBOARD CORE COWL 1ST LATCH SKIN BENT ABOVE LATCH HAS BEEN REPAIRED PER ER/A 581524-14 REV-0 JOB COMPLETE (LP1309495)SDR DALA2019101115844Skin · corrodedSKIN BENEATH STUB BEAM AT RT FUSELAGE, BS 883.5 WAS CORRODED RBL 90. REPAIRED THE SKIN IAW ERA 581549-14, REV 0.SDR DALA2019101115843Skin · corrodedHORIZONTAL STAB CENTER BOX UPPER SURFACE SKIN CORRODED, STRINGER 3, BL 0. REPAIRED THE UPPER SKIN IAW ERA 581523-14, REV 0.SDR DALA2019100905791Floorbeam · corrodedCORROSION STA 287 FLOOR BEAM RBL 75 (APPROX.) UPPER SURFACE. REMOVED, LOCATED, DRILLED, DEBURD AND INSTALL NEW T-CAP AT STA 287 RBL75, ALODINE, PRIMED AND TOP COAT IAW B767-300 SRM 53-00- 51 FIG 201 REPAIR 1, SRM 51-40-02 AND SRM 51-20-01 JOB COMPLETE. (LP1305SDR DALA2019100405705Shear Tie · corrodedCORROSION FOUND ON THE SHEAR TIE AT BS 1197+110, BETWEEN STRINGERS 35L AND STR 36L. FOUND TO BE OUT OF LIMITS. REPLACED THE SHEAR TIE.SDR DALA2019100405704Shear Tie · corrodedCORROSION FOUND ON THE SHEAR TIE AT BS 1219, STRINGERS 34L-33L. REPLACED THE SHEAR TIE.SDR DALA2019100405703Shear Tie · corrodedCORROSION FOUND ON THE SHEAR TIE AT BS 1219, STRINGERS 35L-34L. REPLACED THE SHEAR TIE.SDR DALA2019100735755Shear Tie · corrodedALC SHEAR TIE AT STA. 1285, BTW STR. 37L AND STR. 38L IS FOUND TO BE OUT OF LIMITS AND REQUIRES REPLACEMENT. REMOVED, FABRICATED, AND INSTALLED NEW SHEAR TIE AT STA 1285 STR 37L TI 38L AS NEEDED I.A.W B767-300 SRM 51-40-02 PARA 4 AND 7 AND BOEING DWG 140T2102.SDR DALA2019100405702Shear Tie · corrodedCORROSION FOUND ON THE SHEAR TIE AT BS 1197+66, STRINGERS 38R-37R. REPLACED THE SHEAR TIE.SDR DALA2019100405701Shear Tie · corrodedCORROSION FOUND ON THE SHEAR TIE AT BS 1263, BETWEEN STRINGERS 38L AND 39L, FOUND OUT OF LIMITS. REPLACED THE SHEAR TIE.SDR DALA2019100405700Shear Tie · corrodedCORROSION FOUND ON THE SHEAR TIE AT BS 1197+88, BETWEEN STRINGERS 36R AND 37R, FOUND OUT OF LIMITS. REPLACED THE SHEAR TIE.SDR DALA2019100405699Shear Tie · corrodedCORROSION FOUND ON THE SHEAR TIE AT BS 1219, BETWEEN STRINGERS 39L AND 39R, FOUND TO BE OUT OF LIMITS. REPLACED THE SHEAR TIE.SDR DALA2019100405698Shear Tie · corrodedCORROSION FOUND ON THE SHEAR TIE AT BS 1197, STRINGERS 38L-39L. REPLACED THE SHEAR TIE.SDR DALA2019100405697Shear Tie · corrodedCORROSION FOUND ON THE SHEAR TIE AT BS 1197+66, STRINGERS 36R-35R CORRODED. REPLACED SHEAR TIE.SDR DALA2019100405696Shear Tie · corrodedCORROSION FOUND ON THE SHEAR TIE AT BS 1197+88 BETWEEN STRINGERS 35R AND 36R, FOUND OUT OF LIMITS. REPLACED THE SHEAR TIE.
Back to N156DL, cancelled Aug 25, 2023