N933AT

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 = 'N933AT' 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 DALA2022050503142Channel · corrodedCORROSION ON FRAME CHANNEL STA Y=180 STR=30 AT E/E COMPARTMENT. SUMMARY OF NRC 00113: CORROSION LEVEL 2, FRAME CHANNEL STA Y=180 STR=30 AT E/E COMPARTMENT, WAS REPAIRED PER B717-200 SRM 53-20-07-2R, REPAIR 3. (LP #2223147)May 4, 2022 · N933AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2022050503141Door Track · corrodedCORROSION ON LOWER DOOR JAMB PAN AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00019: CORROSION LEVEL 2, LOWER DOOR JAMB PAN AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-15-2R REPAIR 7. (LP #2222868)May 4, 2022 · N933AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2022050503140Skin · crackedCRACK ON FUSELAGE SKIN STA Y=1155 BTW LONGERON 28L TO 29L. SUMMARY OF NRC 00225: FUSELAGE SKIN STA Y=1155 BTW LONGERON 28L TO 29L WAS REPAIRED PER B717-200 SRM 53-00-00-2R. (LP #2222777)May 4, 2022 · N933AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2022050403118Longeron · corrodedCORROSION ON LONGERON 30 BTW STA Y:908 TO Y:956 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00117: CORROSION LEVEL 2, SECTION LONGERON 30 BTW STA 898 TO 964 WAS REPLACED PER B717 SRM 51-41-02-0G. (LP #2220258)May 2, 2022 · N933AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2022050403117Longeron · corrodedCORROSION ON LONGERON 29L BTW STA Y:907 TO 964 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00112: CORROSION LEVEL 2, SECTION LONGERON 29L BTW STA 898 TO 964 WAS REPLACED PER B717 SRM 51-41-02-0G. (LP #2220090)May 2, 2022 · N933AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2022050403119Spar · wornDISCOVERED WEAR ON THE PREVIOUS REPAIR AT THE RIGHT WING FIXED LEADING EDGE STA XIS 117. SUMMARY OF NRC 00055: WING FIXED LEADING EDGE STA XIS 117 WAS REPAIRED PER ER/A 599011-14 REV. ORIGINAL, SECTION I. PERMANENT REPAIR AND PER PRI 599011-14 REV 0. ASSOCIATEMay 1, 2022 · N933AT · Boeing 717200 · Wing SparSDR DALA2022050403116Doubler · wornFOUND WEAR ON THE FIXED LEADING EDGE REPAIR DOUBLER STA XOS 329 TO 335 AT LH WING (LW). SUMMARY OF NRC 00033: FIXED LEADING EDGE REPAIR DOUBLER STA XOS 329 TO 335 AT LH WING WAS REPLACED PER ER/A 551840-14 REV. ORIGINAL SECTION I. PERMANENT REPAIR. (LP #221844May 1, 2022 · N933AT · Boeing 717200 · Wing SparSDR DALA2022042903017None · noneAFTER REMOVAL OF FLOOR PANEL 221AF, SEVERAL PLACES OF CORROSION WERE FOUND ON THE FLOOR SUPPORT BTW STA 157 AND 170 IN THE PASSENGER CABIN. SUMMARY OF NRC 00053: CORROSION LEVEL 2, FLOOR SUPPORT WAS REPLACED PER B717 SRM SRM 51-41-05-0G. (LP #2214987)Apr 28, 2022 · N933AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2019122007451Structure · damagedRHS VERTICAL STAB LEADING EDGE THREE FASTENER HOLES BELOW ZF 52 SPLICE SHOW CRACK INDICATION. CRACK IS NOT IN SKIN. ALL DAMAGED COMPLETE ON PRI 583922-14AD REV 2. INSTALLED VERTICAL LEADING EDGE PER B717 AMM 55-32-01 400-802. LEAK TEST OF RUDDER LIMITER GOODDec 19, 2019 · N933AT · Boeing 717200 · Vertical StabilizerSDR DALA2019031301670Battery · dischargedON THE SERVICE CHECK, THE AFT CABIN OVERHEAD EMERGENCY LIGHT B5-260 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY ONLY ON POWER SUPPLY B5-260 PER AMM 33-51-03. OPERATIONAL CHECK WAS NORMAL. OK FOR SERVICE. (LP #5838604)Mar 12, 2019 · N933AT · Boeing 717200 · Emergency LightingSDR DALA2018122007296Frame · crackedLEFT OVER WING FRAME AT STA Y=696.00 IS CRACKED. CRACK IS CONDITION 3, EQUAL OR GREATER THAN 0.125. REPLACED FRAME REF 5310-01436-03A.Dec 19, 2018 · N933AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018121807289Cam · out of positionTHE TAIL CONE RELEASE CAM WAS FOUND TO BE CLOCKED INCORRECTLY. MAINTENANCE RE-CLOCKED THE TAIL CONE RELEASE CAM REF AMM 53-52-03.Dec 14, 2018 · N933AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2017040302635Battery Pack · inoperativeFWD UPPER EMERGENCY EXIT LIGHT IS INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD. ACFT OK FOR SERVICE.Apr 3, 2017 · N933AT · Boeing 717200 · Emergency LightingSDR DALA2017010400048Skin · crackedFUSELAGE STA 1134 ON LT SIDE OF VERTICAL HAS SKIN CRACKED AROUND RIVET REQUEST VERIFICATION WITH HFEC MARKED. REPLACED DAMAGED AREA IAW ER/A 551837-14AD REV O.Jan 3, 2017 · N933AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017010400047Fastener · looseLT VERTICAL STAB L/E SKIN BELOW ZFS 52.267 HAS 10 LOOSE SCREWS IN UPPER ROW BELOW SPLICE AND 2 LOOSE FASTENERS IN LWR ROW BELOW SPLICE REF AA WORK CARD 5530-01048-01 STEP 3. REPAIRED DAMAGED AREA IAW ER/A 551841-14AD REV O.Jan 3, 2017 · N933AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2017010400080Longeron · corrodedALC LONGERON 30 HAS CORROSION IN MULTIPLE AREAS FROM FUSELAGE FRAME STA 986 TO STA 1037. REPAIRED L30 FROM STA 899-1053 IAW SRM 53-20-05 REP 1.Dec 31, 2016 · N933AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017010200003Rivet · leakingRIGHT WING UPPER SURFACE, LE WING XRS 115.500. RIVET SEEPING FUEL. REPAIRED IAW ER/A PR551844-14, SRM 51-40-02.Dec 31, 2016 · N933AT · Boeing 717200 · Wing Main, Frame StructureSDR DALA2017010100002Door Frame · corrodedDOOR FRAME LOWER HALF INCLUDING PAN AND SEAL SPLICES HAS MULTIPLE AREAS OF CORROSION. BLEND AND CHECK LIMITS. REPLACED THE DOOR FRAME IAW SRM 51-41-02.Dec 30, 2016 · N933AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017010100001Skin · crackedLEFT WING, LWR SURFACE, LE, XOS 332.558 CRACKED. REPAIR IAW SRM 57-40-01 REPAIR 7. FABRICATED AND INSTALLED INTERNAL/EXTERNAL DOUBLERS WITH FILLERS IAW ER/A 551840-14 REV ORIGINAL.Dec 30, 2016 · N933AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017010400079Seat Track · corrodedRT CARGO SEAT TRACK IS CORRODED JUST FWD OF DOOR JAMB FWD LOWER CORNER. BLENDED CORROSION ON LWR RT CARGO SEAT TRACK AFTER EVALUATION OF BLEND FLANGE THICKNESS FOUND TO BE .040 ALLOWABLE MINIMUM FLANGE THICKNESS IS .060 THIS IS OUT OF LIMITS PER SRM 53-20-52 ADec 29, 2016 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017010400042Shear Tie · corrodedCORROSION ON FORWARD SIDE OF ALC FRAME AND SHEAR TIES AT STA 1022.091 BETWEEN LONGERONS 29L AND 29R (MARKED IN RED). BLENDED CORROSION ON SHEAR TIE AT STA 1022 L29L -L29R. NOMINAL THICKNESS .050 REMAINING THICKNESS .038 REPAIRED SHEAR TIE IAW SRM 53-20-06 REPADec 29, 2016 · N933AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2017010300012Structure · crackedLEFT WING, LE NR 5 SLAT, OTBD L SURFACE CRACKED. REPAIRED IAW SRM 51-41-02 AND 51-41-08.Dec 29, 2016 · N933AT · Boeing 717200 · Leading Edge DevicesSDR DALA2017010400081Seat Track · corrodedCORROSION ON THE RIGHT CENTER SEAT TRACK (RBL44.5), FROM STA 197 TO STA 256. REPLACED RIGHT CENTER SEAT TRACK AT RBL 44.5 FROM STA 197-256 IAW AMM 53-22-01-400-800 SEE PARTIAL WS PG 1 AND 2. MATERIAL ID IAW SRM 53-20-52 LOCATED AND DRILLED NEW SEAT TRACK SECTIDec 28, 2016 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017010400044Cusp Web · crackedUPPER FUSELAGE, CABIN RT CUSP WEB STA 458-503 BL54 5R CORROSION MARKED "CORROSION". REPLACED CUSP WEB RT STA 389-503 IAW SRM 51-41-02, 51-41-05. WORK COMPLETED ON OUTSIDE REPAIR NON-ROUTINE CARD 74117-0200-0257.Dec 28, 2016 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017010300007Seat Track · corrodedCORROSION ON THE RIGHT INBD SEAT TRACK RBL 22, BS 197 TO 256. REPLACED THE SEAT TRACK IAW SRM 53-20-52 REPAIR 5.Dec 28, 2016 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017010300006Seat Track · damagedRT OTBD SEAT TRACK, BS 756 - 813 RBL 56 GOUGED AND CORRODED. REPLACED THE SEAT TRACK IAW SRM 53-20-52 (FIG 201) REPAIR 5.Dec 28, 2016 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017010500082Cusp Web · corrodedUPPER FUSELAGE, CABIN RT CUSP WEB STA 389-427 BL54.5R CORROSION MARKED "CORROSION". BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS ORG 0.020 REMAINING 0.007" REPLACED CUSP WEB WITH NEW CUSP WEB. NEW CUSP WEB IAW DWG #9430538475 AND 51-41-02, 51-41-05.Dec 27, 2016 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017010400043Former · corrodedCORROSION ON FORMER STA 954 L29L-L30. BLENDED CORROSION ON FORMER AT STA 954 IAW SRM 53-00-00 FIG 103 .037 REMAINING OF .063 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103 (6784). REPAIRED OUT OF LIMITS AREA IAW SRM 53-00-06 REPAIR 2.Dec 27, 2016 · N933AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017010300009Seat Track · corrodedRBL 56 OTBD SEAT TRACK BS 927 - 986, FOUND SEVERAL SPOTS OF CORROSION. BLENDED AREAS OF CORROSION IAW SRM 53-00-00 FIG 103 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52 FIG 101. REPAIRED IAW SRM 53-20-52 REPAIR 1.Dec 27, 2016 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017010300008Seat Track · corrodedRBL 56 OTBD SEAT TRACK BS 870 - 898 FOUND SEVERAL SPOTS OF CORROSION. REPLACED THE SEAT TRACK IAW SRM 53-20-52 (FIG 201) REPAIR 5.Dec 27, 2016 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017010400045Cusp Web · crackedRT CUSP WEB CRACK AT STA 318 RBL 44. REPAIRED CRACKED RT CUSP WEB AT STA 318 RBL 44 IAW SRM 53-00-55 FIG 221 .032.Dec 26, 2016 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017010300011Cusp Web · crackedRIGHT CUSP WEB CRACKED AT RBL 54.5, BS 503. REPAIRED THE CUSP WEB IAW SRM 53-00-55 REPAIR 4.Dec 23, 2016 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017010300005Seat Track · corrodedCORROSION ON THE LEFT INBD SEAT TRACK LBL 22, BS 465 - 503. CUT OUT DAMAGE AND INSTALLED 3 LUG REPAIR IAW SRM 53-20-52 REPAIR 1 FIG 201.Dec 23, 2016 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016122410064Frame · corrodedFRAME BS 313 HAS CORROSION AROUND FASTENERS AT ATTACH POINT FOR STR 30. BLENDED CORROSION ON FRAME AT STA 313 STR 30 AND FOUND TO BE OUT OF LIMITS ORG 0.050" REMAINING .039" WITHOUT TOOL TAG 6785 REPAIRED FRAME STA 313 STR 30 IAW B717 SRM 53-00-00 FIG 103 AND Dec 22, 2016 · N933AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016122410063Cusp Web · corrodedSURFACE CORROSION ON RIGHT SIDE CUSP WEB AT BS 562, 582, 598-617. REPAIRED CUSP WEB IAW SRM 53-00-55 2R-4.Dec 22, 2016 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016122410062Cusp Web · corrodedSURFACE CORROSION ON RT CUSP WEB AT BS 598-617. REPAIRED THE CUSP WEB IAW SRM 53-00-55 2R-4.Dec 22, 2016 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016122310055Seat Track · corrodedLEFT OTBD SEAT TRACK LBL 56, BS 726-826 HAS CORROSION, AND SCRATCHES. REPAIRED IAW SRM 53-20-52-2R-1.Dec 21, 2016 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016122310054Seat Track · corrodedLEFT OTBD SEAT TRACK LBL 56, BS 608-703 HAS CORROSION. BLENDED CORROSION . REPAIRED IAW SRM 53-20-52 REPAIR 1.Dec 21, 2016 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016122310053Seat Track · damagedLEFT OUTBD SEAT TRACK LBL 56 BS 488-581 HAS CORROSION, AND NICKS. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-20-52. REPAIRED IAW SRM 53-20-52 REPAIR 1.Dec 21, 2016 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016122210024Seat Track · corrodedLEFT OTBD SEAT TRACK LBL 56 BS 1010-1022 CORRODED. BLENDED THE CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-20-52 REPAIR 1.Dec 21, 2016 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016122210023Seat Track · corrodedLEFT OTBD SEAT TRACK LBL 56 BS 488 CORRODED OUT OF LIMITS. REPAIRED THE SEAT TRACK IAW SRM 53-20-52-2R-1.Dec 21, 2016 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016122210022Support Bracket · crackedUPPER CABIN SEAT TRACK SUPPORT BRACKET AT BS 715 LBL 44 IS CRACKED. REMOVED THE SEAT TRACK SUPPORT BRACKET AND INSTALLED A NEW BRACKET IAW SRM 51-41-05.Dec 21, 2016 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016122210021Structure · corrodedFOUND AFTER REMOVAL OF FLOOR SUPPORT AT BS 172 TO 178 SUBFLOOR CORRODED. TRIMMED CORRODED SUBFLOOR IAW SRM 51-70-10 REPAIR 1, FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 51-70-10 REPAIR 1, AND SRM 53-10-51, INSTALLED THE REPAIR IAW SRM 51-70-10 REPAIR 1.Dec 21, 2016 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016122210020Floor Support · corrodedFLOOR SUPPORT HAS CORROSION ON UNDERSIDE. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-05 PG 17 STEP 8 AND SRM 51-41-02 PG 3 PAR F. ORIGINAL .Dec 21, 2016 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016122210019Skin · damagedRUDDER LOWER LEFT SIDE EXTERNAL SKIN IS BENT AT EDGE. REPAIRED IAW SRM 51-70-13 FIG 202Dec 21, 2016 · N933AT · Boeing 717200 · Rudder, Plate/SkinSDR DALA2016122210018Support Bracket · crackedUPPER CABIN SEAT TRACK SUPPORT BRACKET AT BS 737 RBL 44 IS CRACKED. REPLACED THE SUPPORT BRACKET IAW SRM 51-41-05.Dec 21, 2016 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016122210017Seat Track · corrodedUPPER CABIN LEFT INBD SEAT TRACK LBL 22 BS 465 CORRODED OUT OF LIMITS. CUT OUT DAMAGE AND INSTALLED A REPAIR IAW SRM 53-20-52 REPAIR 1.Dec 21, 2016 · N933AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016122610066Floor Support · corrodedMAIN ENTRANCE DOOR THRESHOLD FLOOR SUPPORT BS 160 - 200, LBL 62 CORRODED. BLENDED AND FOUND TO BE OUT OF LIMITS. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, 51-41-05, 51-41-08, AND DRAWING 52929169.Dec 20, 2016 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016122109991Cusp Web · crackedRT CUSP WEB AT STA 679 IS CRACKED. MARKED IN RED. REPAIRED CRACK CUSP WEB AT STA 679 RT IAW 53-00-55 REPAIR NR 4.Dec 20, 2016 · N933AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016122610067Floor Panel · corrodedFORWARD CARGO FLOOR PANEL CORRODED. BLENDED THE FLOOR PANEL IAW SRM 53-00-00 SHEET 1. FOUND TO BE OUT OF LIMITS. FABRICATED A NEW FLOOR PANEL IAW AMM 25-58-01-350-801 C1 AND C2.Dec 19, 2016 · N933AT · Boeing 717200 · Fuselage Floor Panel
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