N893AT

Service difficulty reports · 171

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 = 'N893AT' 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.

SDR DALA2016030201570Web · corrodedAFT PIT FORWARD DOOR CUTOUT THRESHOLD WEB CORRODED IN SEVERAL LOCATIONS BETWEEN STATIONS 947 AND 954. LONGERONS 26-25R MARKED. BLENDED OUT CORROSION ORIGINAL .040" REMAINING .028", LOSS .012". FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, PG 105. FABRICATED Mar 1, 2016 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102807820Angle · corrodedRIGHT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 20 INCHES OUTBOARD OF INBOARD WHEEL WELL. REMOVED CORROSION. ROTO PEENED AND RESTORED FINISH IAW PIR ER/A 540747-14 REV O AND ER/A 540747-14 ORIGINAL.Feb 29, 2016 · N893AT · Boeing 717200 · Wing, Rib/BulkheadSDR DALA2016102807819Angle · corrodedLEFT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 19 INCHES OUTBOARD OF INBOARD WHEEL WELL BULKHEAD. REMOVED CORROSION. ROTO PEENED AND RESTORED FINISH IAW ER/A 540747-14 ORIG. AND PRI ER/A 540747-14 REV O.Feb 29, 2016 · N893AT · Boeing 717200 · Wing, Rib/BulkheadSDR DALA2016102807818Angle · corrodedLEFT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 30 INCHES OUTBOARD OF INBOARD WHEEL WELL BULHEAD. REMOVED CORROSION. ROTO PEENED AND RESTORED FINISH IAW PRI ER/A 540747-14 REV 0 AND ER/A 540747 ORIGINAL.Feb 29, 2016 · N893AT · Boeing 717200 · Wing, Rib/BulkheadSDR DALA2016030101538Strap · corrodedAFT CARGO STRAP AT BS 892, LONGERON 30 IS CORRODED NEAR FASTENER ON UPPER SURFACE. BLENDED OUT CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, PG 105. FABRICATED NEW SPLICE ON WO 033609-1600-0006 INSTALLED IAW DWG 5919707.Feb 29, 2016 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102807817Bulkhead · corrodedAFT CARGO BAY BILGE AREA BS 813 BETWEEN LONGERON 28 AND 29R BULKHEAD HAS CORROSION. REPAIRED IAW ER/A 540745-14 REV O.Feb 28, 2016 · N893AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2016022901488Frame · crackedAFT CARGO DOOR INTERNAL STRUCTURE AFT FRAME CRACKED ABOVE CENTER STOP FITTING. STOP DRILLED CRACKS, REMOVED FASTENERS, REMOVED FILLER FROM PAN. VERIFIED MATERIAL FOR REPAIR DOUBLER ATAG 27991, CUT, FIT, LOCATED NEW DOUBLER & SHIMS IAW SRM 52-30-02 REPAIR 6. Feb 28, 2016 · N893AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016022901487Frame · crackedAFT CARGO DOOR INTERNAL STRUCTURE UPPER FWD CORNER FRAME CRACKED AT UPPER STOP FITTING. REMOVED DOOR SEAL, STOP DRILLED CRACKS, REMOVED FASTENER IN REPAIR AREA, REMOVED FILLER FROM PAN, VERIFIED MATERIAL FOR REPAIR DOUBLER ATAG A63804, CUT, TRIMED AND LOCATEDFeb 28, 2016 · N893AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016022901485Floor Panel · damagedFLOOR PANEL 222SF DAMAGED. FABRICATED NEW HAT CHANNEL IAW DWG NR 9952521, REV BB ID:1, FRAME 1 OF 1. TREATED & PRIMED NEW HAT CHANNEL IAW SRM 51-10-04, STEP 15 & 21. REPLACED NEW HAT CHANNEL TO FLOORBOARD IAW DWG 9952521, REV BB, ID: 1, FRAME 1 OF 1.Feb 28, 2016 · N893AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016102807816Angle · corrodedLEFT WHEEL WELL FORWARD BULKHEAD UPPER ANGLE IS CORRODED 19 INCHES OUTBOARD OF INBOARD WHEEL WELL BULKHEAD. REMOVED CORROSION, ROTOR PEENED AND RESTORED FINISH IAW ER/A 540747-14 ORIGINAL AND PRI ER/A540747-14 REV 0.Feb 26, 2016 · N893AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2016022701484Hinge Fitting · crackedAFT CARGO COMPARTMENT DOOR JAMB UPPER SILL FWD HINGE FITTING LOWER FWD AND AFT ATTACH CLIPS CRACKED. REMOVED OLD, FABRICATED NEW, TREAT, PRIMED, APPLIED TOP COAT, APPLIED CIC. INSTALLED NEW AFT CARGO COMPARTMENT DOOR JAMB UPPER SILL FWD HINGE FITTING LOWER FFeb 26, 2016 · N893AT · Boeing 717200 · Fuselage, Door HingeSDR DALA2016022701482Cusp Web · corrodedLEFT CUSP WEB BETWEEN BS 465-484 HAS 3 AREAS OF CORROSION. LEFT CUSP WEB, FS 465-484 HAS 3 AREAS OF CORROSION. REMOVED CORROSION MECHANICALLY. ORIGINAL "T" .020, LOSS OF .004, .016 REMAINING. FOUND TO BE OUT OF LIMITS. ACCESSED AREA TO BE REPAIRED. DRILLEDFeb 26, 2016 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016022701481Cusp Web · corrodedLEFT CUSP WEB BETWEEN BS 446-465 HAS 2 AREAS OF CORROSION. LEFT CUSP WEB, FS 446-FS 465, 2 AREAS CORROSION. REMOVED CORROSION MECHANICALLY. ORIGINAL "T" .020, LOSS OF .005, .015 REMAINING. FOUND TO BE OUT OF LIMITS. ACCESSED AREA TO BE REPAIRED. DRILLED &Feb 26, 2016 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016022601443Floorboard · damagedPASSENGER FLOORBOARD 222AFF CRACK IN MIDDLE OF PANEL VERFIED MATERIAL FOR NEW HAT CHANNEL A TAG A53914 FABRICATED NEW HAT CHANNEL IAW DWG 9952521, REV BB ID1 FRAME 1 OF 1. TREATED AND PRIMED NEW HAT CHANNEL IAW SRM 51-10-04, STEP 21 AND STEP 25 INSTALLED NEW Feb 25, 2016 · N893AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016022301313Seat Track · corrodedPASSENGER CABIN INBD SEAT TRACK CORRODED AT BS 522, RBL 22". REMOVED CORROSION ON PASSENGER CABIN INBD SEAT TRACK BS 522, RBL 22", CHECK MATERIAL ORIG "T" .115, LOSS OF .033, REMAINING MATERIAL OF .082 FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52, FIG 101, NEW SFeb 22, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016022301312Seat Track · corrodedPASSENGER CABIN INBD SEAT TRACK CORRODED AT BS 488, RBL 22". REMOVED CORROSION OF CABIN SEAT TRACK AT BS 488, RBL 22 IAW SRM 53-20-52, PG 103, FIG 101 AND 51-10-04; FOUND TO BE WITH OUT LIMITS IAW SRM 53-20-52, FIG 101. REPLACEMENT OF SEAT TRACK REF WORK CAFeb 22, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016022301311Seat Track · corrodedPASSENGER CABIN INBD SEAT TRACK CORRODED AT BS 551, RBL 22". REPLACED PASSENGER CABIN INBD SEAT TRACK FROM BS 470 TO 580, RBL 22". TREATED AND PRIMED, TOPCOATED SEAT TRACK IAW SRM 51-10-04, PG 20,29, AND 49 AND INSTALLATION OF SEAT TRACK REF SRM 53-20-52 REPFeb 22, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016022301309Floor Panel · corrodedPASSENGER CABIN FLOOR PANEL 221ER HAS AREAS OF CORROSION ON FWD END OF PANEL. REMOVED CORROSION FROM FLOOR PANEL 221ER. PANEL WAS OUT OF LIMITS. NEW PANEL WAS LOCATED AND DRILLED TO FIT ACFT IAW DWG 9957828, REV AB ID:1 FRAME 2 OF 3, PANEL WAS TREATED & PRIMFeb 22, 2016 · N893AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016022301308Seat Track · not reportedREPLACE MAIN CABIN SEAT TRACK BS 200-588, RBL 44.5. REPLACED SEAT TRACK BS 200-588, RBL 44.5 IAW DWG 5930547.Feb 22, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016022201272Strap · crackedFORWARD CARGO COMPARTMENT DOOR JAMB LOWER SILL 4.5" SPLICE STRAP CORRODED 5" FWD OF LOWER FWD STOP FITTING. REMOVED CORROSION IN SPECIFIED AREA FOUND BLENDED LIMITS TO BE BEYOND ACCPTABLE LIMITS ORGINAL MATERIAL .080 REF SRM 53-20-15, FIG 1, MATERIAL LOSS OF Feb 21, 2016 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016022201271Door Frame · corrodedFORWARD CARGO COMPARTMENT DOOR JAMP LOWER SILL 4.5" SPLICE STRAP CORRODED 5" AFT STOP FITTING. REMOVED CORROSION IN SPECIFIED AREA FOUND BLENDED LIMITS TO BE BEYOND ACCEPTABLE LIMITS, ORGINAL MATERIAL .080, REF SRM 53-20-15, FIG 1. MATERIAL LOSS OF .040 USFeb 21, 2016 · N893AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016102707783Seat Track · corrodedPASSENGER CABIN CENTER SEAT TRACK CORRODED BS 295 RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED.Feb 20, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016102707782Seat Track · corrodedPASSENGER CABIN CENTER SEAT TRACK CORRODED BS 400 RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED.Feb 20, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016102707781Seat Track · corrodedPASSENGER CABIN CENTER SEAT TRACK CORRODED BS 522 RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED.Feb 20, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016102707780Seat Track · corrodedPASSENGER CABIN CENTER SEAT TRACK CORRODED BS 551 RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED.Feb 20, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016102707779Seat Track · corrodedPASSENGER CABIN CTR SEAT TRACK CORRODED BS 345 RBL 43. REMOVED AND REPLACED THE SEAT TRACK.Feb 20, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016102707778Seat Track · corrodedPASSENGER CABIN CTR SEAT TRACK CORRODED BS 432 RBL 43. REMOVED AND REPLACED.Feb 20, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016102707777Seat Track · corrodedPASSENGER CABIN CTR SEAT TRACK CORRODED BS 323 RBL 43. REMOVED AND REPLACED.Feb 20, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016102707776Seat Track · corrodedPASSENGER CABIN CTR SEAT TRACK CORRODED BS 488 RBL 43. REMOVED AND REPLACED.Feb 20, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016102707775Seat Track · corrodedPASSENGER CABIN CENTER SEAT TRACK CORRODED BS 460 RBL 43. REMOVED AND REPLACED.Feb 20, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016022201274Seat Track · corrodedPASSENGER CABIN INBD SEAT TRACK CORRODED AT BS 608, RBL 22". REMOVED CORROSION, VERIFIED LIMITS, MAX MATERIAL LOSS -.020, MATERIAL LOSS .022, SEAT TRACK AT BS 608, RBL 22 OUT OF LIMITS. REMOVED SEAT TRACK SECTION 588-645, RBL 22, RECEIVED AND VERIFIED MATERIFeb 20, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016022201275Attach Bracket · crackedRT WING FIXED L/E WING ROOT INBD SIDE WING TO BODY FAIRING MOUNT STRUCTURE ATTACH BRACKET CRACKED. REPLACED RT WING ROOT FIXED L/E WING TO BODY FAIRING MOUNT ATTACH BRACKET IAW SRM 51-42-02, PG 1-11 AND DWG 5919110 SH5.Feb 19, 2016 · N893AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2016021901247Floor Support · corrodedPASSENGER CABIN FLOOR SUPPORT CORRODED AT BS 180-188 LBL 55. REMOVED OUT OF LIMITS FLOOR SUPPORT FABRCATED NEW SUPPORT AND INSTALLED AT CABIN FLOOR BS 154 TO 192 LBL -55 IAW SRM 51-40-02, 51-30-07, 51-40-08, 51-10-04.Feb 18, 2016 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016021801162Seat Track · corrodedDURING LT SEAT TRACK INSPECTION, FOUND LT CENTER SEAT TRACK CORRODED TOP AND BOTTOM AT BS 276. REMOVED CORROSION ON SEAT TRACK AT BS 276, LBL 44.5. REPAIRED USING SEAT TRACK PLUG REPAIR IAW SRM 53-20-52. FIG 4, 201. AREA HAS BEEN TREATED, PRIMED, TOP COATEDFeb 17, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016021801161Seat Track · corrodedPASSENGER CABIN INBD SEAT TRACK CORRODED AT BS 280, RBL 22. REMOVED CORROSION FROM SEAT TRACK AT BS 280, RBL 22" IAW SRM 53-20-52, PG 103, FIG 101 AND 51-10-04 USING A 10X MAG LENS. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52, ALLOWABLE DAMAGE, FIG 101. REPAIRFeb 17, 2016 · N893AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016022001266Floor Support · corrodedAFT CARGO BAY BILGE AREA BETWEEN BS 954 AND BS 946, LONGERON 29R AND 30 FLOOR SUPPORT IS CORRODED TOP SURFACE WHERE CONECTS TO THE BILGE SKIN. BLENDED FLOOR SUPPORT AND CHECKED LIMITS IAW SRM 53-00-00. DAMAGE WAS 100 PERCENT MATERIAL LOSS. LOCATED AND DRILLFeb 15, 2016 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102707772Cusp Web · corrodedCUSP WEB IS CORRODED BS 598 - 617, LBL 59. BLENDED CORROSION IAW SRM 51-10-04 AND SRM 53-00-55. ONE AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55. CUT OUT DAMAGE AND FABRICATED REPAIR IAW SRM 53-00-55 REPAIR 4. INSTALLED REPAIR DOUBLERS AND FILLERS IAW SRM 5Feb 13, 2016 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102707771Shim · corrodedAFT CARGO BAY THRESHOLD LT AND RT SHIMS FOR STRAP THAT GOES ON TOP OF DOOR THRESHOLD WEB BETWEEN BS 994 - 986, LONGERON 28 AND 29R CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00 PAGE 105. FABRICATED NEW SHIM IAW DWG 5910158 REV DW. RESTFeb 13, 2016 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015061303787Frame · crackedDURING SCHEDULED INSPECTION, FOUND FRAME BS 715 CRACKED EXCEEDING 1.0. REPLACED THE FRAME IAW AMDS CARD 5310-01436-03A.Jun 12, 2015 · N893AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015061303786Frame · crackedDURING SCHEDULED INSPECTION, FOUND LT OVERWING FRAME BS 696 CRACKED EXCEEDING .25. REPLACED THE FRAME IAW AMDS CARD 5310-01436-03A AND COMPLETED REQUIRED INSPECTIONS.Jun 12, 2015 · N893AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015060803627Cusp Web · crackedDURING INSPECTION, FOUND CUSP WEB CRACKED AT BS 660. INSTALLED A REPAIR IAW 53-00-55.Jun 5, 2015 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015032602424Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT ALL OF THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT P5-119 FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Mar 26, 2015 · N893AT · Boeing 717200 · Emergency LightingSDR DALA2015022301552Battery Pack · inoperativeDURING LINE CHECK IN SAV, NOTED FWD RT + LT OVERWING UPPER EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-51.Feb 20, 2015 · N893AT · Boeing 717200 · Emergency LightingSDR DALA2015020200846Stiffener · crackedBS 737, LBL 54 VERTICAL STIFFENER CRACKED. REPLACED IAW SRM 51-41-02, 51-10-04, 51-40-08 & 51-41-02.Feb 1, 2015 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015020200845Stiffener · crackedBS 737, RBL 54 VERTICAL STIFFENER CRACKED. REPLACED STIFFENER IAW SRM 51-41-02, 51-40-08 & 51-10-04.Feb 1, 2015 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2014030325690Light · looseR1 DOOR EMERGENCY EXIT SIGN BULB LOOSE. SECURED BULB IAW MM.Feb 28, 2014 · N893AT · Boeing 717200 · Emergency LightingSDR SWAA2014030325689Light · looseL1 DOOR EMERGENCY EXIT SIGN BULB LOOSE. SECURED BULB IAW MM.Feb 28, 2014 · N893AT · Boeing 717200 · Emergency LightingSDR SWAA2014022125399Doubler · corrodedFLOOR WEB DOUBLER CORRODED AT BS 200, LBL 12. REPAIRED DOUBLER IAW SRM.Feb 17, 2014 · N893AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2014013024705Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 222ADF DELAMINATED. REPAIRED PANEL 22ADF IAW AMM & SRM.Jan 25, 2014 · N893AT · Boeing 717200 · Fuselage Floor PanelSDR SWAA2014021925328Tab · delaminatedLT ELEVATOR GEARED TAB DELAMINATED AT OTBD HINGE. REPAIRED TAB IAW SRM.Jan 17, 2014 · N893AT · Boeing 717200 · Elevator, Tab Structure
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