N935AT

Service difficulty reports · 219

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 = 'N935AT' 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 DALA2019042202556Battery Pack · inoperativeEMERGENCY LIGHTS OVER THE AFT OVERWING EXIT IS INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK, B5-230, TO BE BAD. BATTERY PACK B5-230 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5041741)Apr 21, 2019 · N935AT · Boeing 717200 · Emergency LightingSDR DALA2019032701944Battery Pack · dischargedTHE EMERGENCY LIGHTS ARE NOT WORKING AT THE OVERWING EXIT ON ROW 20 AND THE OVERHEAD EXIT ON ROW 20/21. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK B5-230. OPERATIONAL CHECKS ARE GOOD IAW AMM 33-51. OK FOR SERVICE. (LP #5824949)Mar 26, 2019 · N935AT · Boeing 717200 · Emergency LightingSDR DALA2019011200223Frame · crackedSTA Y=696.00 OVERWING FRAME HAS CRACK AT UPPER RADIUS OF THE FRAME TAB GREATER THAN .250 (CONDITION 3) PER STEP 10 OF 5310-01436-04D. REF NRC 49: REPLACED FRAME REF WORK CARD 5310-01436-03B. ASSOCIATED AA 5310-01436 ADDED FOR AC 9564. (LP #0900044)Jan 11, 2019 · N935AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019011200222Frame · crackedSTA 715 LT FRAME CRACKED GREATER THAN 1/4" SEE CONDITION 3 STEP 13, REF NRC 51: REPLACED FRAME REF WORK CARD 5310-01436-03A. (LP #0900033)Jan 11, 2019 · N935AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019011200221Structure · damagedNEW DAMAGE AT PREVIOUS MONITOR PLACARD LH FUSELAGE STA 237 AT CUSP LINE (MKD). NRC 001-0242:5300-2018/010 00016: PRI 574366-14 REV O-2 MATCHES ER/A 574366-14 REV O STEPS 1-8. (LP #0899736)Jan 11, 2019 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019011100220Lanyard · disconnectedTAILCONE DEPLOYMENT SYSTEM LANYARD DISCONNECTED FROM DEPLOYMENT HANDLE ON BOX. NRC 001-0209:2000-1002/014 00195: COMPLIED WITH ON JOB 001-0106:5352-4002. (LANYARD CONNECTED). (LP #0898975)Jan 11, 2019 · N935AT · Boeing 717200 · Emergency EquipmentSDR DALA2019011100219Hinge · out of positionTAILCONE SLIDE BOX COVER HALF HINGES NOT ENGAGED. NRC 001-0209:2000-1002/011 00192: COMPLY WITH ON JOB 001-0106:5352-4002. (ENGAGED HINGES). (LP #0898973)Jan 11, 2019 · N935AT · Boeing 717200 · Escape SlideSDR DALA2018083005391Sign · missingEXIT SIGN MISSING ONE SIDE MID-PLANE. FOUND & RE-SECURED FWD FACING EMERGENCY EXIT SIGN AS REQUIRED.Aug 29, 2018 · N935AT · Boeing 717200 · Emergency LightingSDR DALA2018071104447Skin · corrodedON WALKAROUND FOUND AFT LAV PANEL SKIN CORRODED AND BULGING. REPAIRED ON N/R 1, REF ERA 569907-14.Jul 10, 2018 · N935AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR 2017F00089Skin · delaminatedDURING UNSCHEDULE MAINTENANCE CHECK, THE RT OTBD SPOILER WAS FOUND DELAMINATED.Apr 13, 2017 · N935AT · Boeing 717200 · SpoilersSDR DALA2017012000526Cusp Web · corrodedUPPER CABIN RIGHT CUSP WEB IS CORRODED AT STA 598-620 RBL 59, AT REPAIR BETWEEN STA 655-674 RBL 59, AND IS CRACKED AT STA 674 RBL 47. REPLACED CUSP WEB FROM STA 655 TO 674 IAW SRM 51-41-02, 51-41-03. BLENDED CUSP FROM 598 TO 620 IAW SRM 53-00-00 FIG 103. .019 Jan 19, 2017 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017012000525Longeron · corrodedLONGERON 29R CORRODED STA 927-946. REMOVED .027 WAS REMOVED IAW SRM 53-00-00 FIG 103. LONGERON REPLACED WITH NEW LONGERON IAW SRM 51-41-02 06 ER/A 551819-14MA.Jan 19, 2017 · N935AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017012300588Longeron · corrodedLONGERON 29R CORRODED BS 927 - 946. THE LONGERON WAS BLENDED, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPLACED THE LONGERON IAW SRM 51-41-02-06, AND ER/A 551819-14MA.Jan 18, 2017 · N935AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017012100529Door Frame · crackedR1 SRVC DOOR HAS A CRACKED BEAM INSIDE THE CAVITY AT THE DOOR HOLD OPEN RELEASE HANDLE. REPLACED R1 SERVICE DOOR FRAME INSIDE THE CAVITY AT THE DOOR HOLD OPEN RELEASE HANDLE IAW DRAWING 9911580 AND SRM 51-41-01-OG, 51-41-02 FIG 13, AND 51-41-05 FIG 2.Jan 18, 2017 · N935AT · Boeing 717200 · Service DoorsSDR DALA2017011900476Panel · damagedSEVERAL FASTENERS PULLED THROUGH THE LEFT PYLON FAIRING, LOWER FWD EDGE. REPAIRED THE PANEL IAW 54-00-00 REP 2. FIG 201.Jan 17, 2017 · N935AT · Boeing 717200 · Nacelle/Pylon, Plate/SkinSDR DALA2017011900474Skin · crackedFUSELAGE SKIN CRACKED BS 1022, LONGERON 14L. HFEC VERIFIED IAW NDT SPM ETHF PROCEDURE 1, 06-10-01.001. REPAIRED THE SKIN IAW ER/A 553662-14 REV 0. ASSOCIATED ER/A 00-553662 ADDED FOR AC 9564.Jan 17, 2017 · N935AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017011500332Skin · damagedLEFT VERTICAL STAB L/E AT SPLICE VSS 52.267, UPPER TWO ROWS HAVE 26 LOOSE SCREWS & 22 OVERSIZED HOLES. INSTALLED A REPAIR IAW BSG 95550001 AND W/C 5530-01048-03.Jan 14, 2017 · N935AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2017012600632Longeron · corrodedCORROSION FLC L30 STA 600. L30 STA 600 CORRODED, BLENDED CORROSION AS REQUIRED, IAW B717 SRM 53-00-00 FIG 103. ORIGINAL THICKNESS .170 REMOVED .040. FOUND TO BE OUT OF LIMITS. REPLACED.Jan 13, 2017 · N935AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017011400330Cusp Web · crackedFOUND A CRACK IN THE CUSP WEB BS 655. REPAIRED THE CUSP WEB IAW SRM 53-00-55 REPAIR 4.Jan 13, 2017 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017011900475Cusp Web · corrodedUPPER CABIN RT SIDE CUSP WEB BETWEEN BS 908 - 946 HAS CORROSION ON UPPER AND LOWER SURFACES. REPAIRED THE CUSP WEB IAW SRM 53-00-55 REPAIR 4 FIG 209.Jan 12, 2017 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017011100242Web · damagedFLOOR WEB BELOW PANEL 221EF IS CORRODED WITH A HOLE THROUGH IT. REPAIRED THE WEB IAW ER/A 551819-14MA REV OR.Jan 10, 2017 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017011200252Cusp Web · corrodedRIGHT CUSP WEB IS CORRODED AT BS 366 RBL 59. REPAIRED THE CUSP WEB IAW SRM 53-00-55 REPAIR 4.Jan 9, 2017 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017011000221Cusp Web · corrodedLEFT CUSP WEB BS 655-756 HAS CORROSION WITH CORROSION BETWEEN LBL 44-56. BLENDED AND A CRACK WAS FOUND AT STA 665 LBL 58. DAMAGE WAS REMOVED DOUBLER AND RING. DOUBLER AND FILLER ALODINE & PRIMED PARTS AND INSTALLED IAW SRM 51-10-04, 53-00-55 REPAIR 4 FIG 207.Jan 9, 2017 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017011000220Cusp Web · corrodedLEFT CUSP WEB CORRODED AND HAS HOLE PUNCH THROUGH IT AT BS 370-389. BLENDED AREAS IAW SRM 53-00-00, FOUND TO BE OUT OF LIMITS. ORIGINAL THICKNESS WAS .080 REMOVED .007 REPAIRED IAW 53-00-55. . FABRICATED DOUBLER IAW SRM 53-00-55.Jan 9, 2017 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017011100243Floor Panel · corrodedFWD LOWER CARGO 121MF METAL FLOOR PANEL MOUNT HOLES HAVE SIGNS OF CORROSION. BLENDED THE PANEL IAW SRM 53-00-00. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-50 2R-1.Jan 6, 2017 · N935AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017011100235Cusp Web · corrodedCUSP WEB IS CORRODED AT BS 337 RBL 59. REPAIRED IAW SRM 53-00-55-2R-4.Jan 6, 2017 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017011100234Cusp Web · corrodedCUSP WEB BETWEEN BS 922-933 IS CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS . INSTALLED A REPAIR DOUBLER IAW SRM 53-00-55 REPAIR 4. FIGURE 216.Jan 6, 2017 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017011100233Attach Bracket · crackedFLOORBEAM SUPPORT STRUT ATTACH BRACKET IS CRACKED IN SEVERAL PLACES AT BS 715 LBL 44. REPLACED ATTACH BRACKET IAW SRM 51-41-05 STEP 8.Jan 6, 2017 · N935AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2017011100232Shear Tie · corrodedSHEAR TIE BS 974 BETWEEN STRINGERS 25-26L IS CORRODED. BLENDED IAW SRM 53-00-00 FIG 103 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPAIRED IAW SRM 53-00-06 REPAIR 2.Jan 6, 2017 · N935AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2017011100236Cusp Web · corrodedBS 865 CUSP WEB CORRODED. REPAIRED IAW SRM 53-00-55 REPAIR 4 FIG 213.Jan 4, 2017 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017010500084Cusp Web · corrodedUPPER CABIN RIGHT CUSP WEB IS CORRODED AT STA 825-830 RBL 59. MARKED. BLENDED CORROSION ON CUSP WEB AT STA 825-830 RBL 59. NOMINAL=.020 REMAINING=.014 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55 FIG 101. REPAIRED DAMAGED AREA ON CUSP WEB IAW SRM 53-00-55 REPAIRJan 4, 2017 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017010500083Intercostal · crackedINTERCOSTAL AT STA 636 BL0 CRACKED. REPAIRED CRACKED ANGLE ON INTERCOSTAL STA 636 BL0 IAW SRM 53-00-00 REPAIR 1.Jan 4, 2017 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017010400046Beam · crackedFWD SERVICE DOOR LOWER HORIZONTAL BEAM JUST UNDER LOWER DOOR HINGE CRACKED. REPLACED LOWER HORIZONTAL BEAM ON FWD SERVICE DOOR IAW SRM 51-41-01-0G, 51-41-02 FIG 13, AND 51-41-05 FIG 2.Dec 30, 2016 · N935AT · Boeing 717200 · Service DoorsSDR DALA2015090405411Frame · corrodedFRAME BS 927 HAS CORROSION BETWEEN LONGERON 28L AND 29R ON BOTH SIDES. REPAIRED SRM 53-00-00, FIG 103, AND 51-70-11, FIG 201, REPAIR NR 1.Sep 2, 2015 · N935AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015090205409Door Frame · corrodedAFT CARGO DOOR ENTRY LOWER JAMB HAS CORROSION. REPARIED IAW SRM 53-20-15, REPAIR 7 AND DWG J060288.Sep 2, 2015 · N935AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2015090205410Lanyard · brokenRIGHT FWD DOOR 1 SLIDE PACK: LOWER PARACHUTE PIN LANYARD STRING IS BROKEN. REPLACED EVACUATION SLIDE NR 1 RT SERVICE DOOR IAW AMDS 2561-9005.Sep 1, 2015 · N935AT · Boeing 717200 · Escape SlideSDR DALA2015090105377Door Frame · corrodedFWD CARGO ENTRY LOWER FRAME HAS CORROSION. REPLACED LOWER CARGO DOOR PAN IAW DWG J060228.Aug 31, 2015 · N935AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2015083105278Longeron · corrodedLONGERON 30L HAS SIGNS OF CORROSION BETWEEN FRAME BS 946-1002. REPAIRED IAW ER/A 538313-14.Aug 31, 2015 · N935AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2015083105280Shear Tie · corrodedBS 946 FRAME SHEAR TIE HAS SIGNS OF CORROSION BETWEEN STRINGERS 29R & 29L. INSTALLED SHEAR TIE REPAIR AND REINSTALLED INTERCOSTAL BETWEEN FRAME 946 AND 954, TO THE RT OF L30 IAW SRM 53-00-00, AND SRM 53-00-06, REPAIR NR 2.Aug 30, 2015 · N935AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2015083105279Doubler · corrodedAFT CARGO BILGE, CELL PHONE ANTENNA DOUBLER CORRODED, BS 965-986. REMOVED CORROSION IAW SRM 53-00-00, FIG 103, FABRICATED AND INSTALLED NEW INTERNAL DOUBLER IAW DWG P13110-05105.Aug 30, 2015 · N935AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2015083005277Skin · corrodedFUSELAGE SKIN CORRODED AROUND OPENING OF LAV VACUUM MOTOR EXHAUST PORT. FOUND INTERNAL BRACKET CORRODED BEYOND SRM LIMITS. R & R BRACKET IAW DWG 5936667.Aug 30, 2015 · N935AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2015083005276Frame · corrodedFRAME BS 908 HAS CORROSION BETWEEN LONGERONS 28L-28R. REPAIRED IAW SRM 53-00-06, FIG 201.Aug 28, 2015 · N935AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015082805263Shear Tie · corrodedSHEAR TIE BETWEEN 29 - 30L HAS CORROSION AT BS 1002. REPLACED THE SHEAR TIE IAW SRM 51-40-02.Aug 27, 2015 · N935AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2015082805262Frame · corrodedFRAME BS 1022 HAS CORROSION BETWEEN LONGERON 29L-29R. SPLICED IN A NEW SECTION OF FRAME IAW SRM 53-00-06. REPAIR 2.Aug 27, 2015 · N935AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015082705242Cusp Web · puncturedDURING OVERWING FRAME REPLACEMENT, FOUND CUSP WEB PUNCTURED BETWEEN BS 696 AND BS 715 ON LT SIDE. REPAIRED IAW SRM 53-00-00, FIG 201.Aug 26, 2015 · N935AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015082605235Bulkhead Web · crackedAFT BULKHEAD WEB HAS A 2.5 INCH CRACK NEAR INBD EDGE AT HORIZONTAL STIFFNER. REPAIRED IAW SRM 53-30-08, REPAIR 4.Aug 26, 2015 · N935AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2015082605234Frame · crackedLEFT OVERWING FUSELAGE FRAME AT BS 696 IS CRACKED. REPLACED LT OVERWING FRAME.Aug 25, 2015 · N935AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015081404962Battery Pack · dischargedEMERGENCY LIGHTS IN AFT CAT WALK ARE DIM. REPLACED BATTERY B5-116.Aug 14, 2015 · N935AT · Boeing 717200 · Emergency LightingSDR DALA2015041402759Battery Pack · inoperativeDURING LINE CHECK, NOTED AFT EXIT LIGHTS AT OVERWING DOORS INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-51. LP 6571031.Apr 14, 2015 · N935AT · Boeing 717200 · Emergency LightingSDR DALA2015010500052Pin · pulledDURING SERVICE CHECK, FOUND L1 DOOR SLIDE PIN PULLED. REPLACED L1 DOOR SLIDE IAW WORK CARD 2561-9004.Jan 4, 2015 · N935AT · Boeing 717200 · Escape Slide
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