N939AT

Service difficulty reports · 175

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 = 'N939AT' 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 DALA2018082305209Longeron Splice · crackedLONGERON 23L AT FWD SPLICE REPAIR WAS CRACKED AT BS 389 - 408. ACCOMPLISHED A PERMANENT REPAIR TO THE LONGERON BETWEEN BS 361 TO 397 IAW SRM 53-00-05, REPAIR 2.Aug 22, 2018 · N939AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018082305208Former · damagedFORMER BS 408 BETWEEN LONGERONS 24L - 25L APPEARS TO BE BENT. REPLACED THE FORMER IAW SRM 51-41-02, AND DRAWING 9911526, REV AZ.Aug 22, 2018 · N939AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018082305207Former · damagedFORMER BS 446, LONGERON 24L - 25L WAS DAMAGED. REPLACED THE FORMER IAW SRM 51-40-02, AND DRAWING 9911526, REV AN, AND REV AZ.Aug 22, 2018 · N939AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018082305206Former · damagedFORMER BS 446 BETWEEN LONGERONS 25L - 26L WAS DAMAGED. REPLACED THE FORMER IAW SRM 51-41-02, DRAWING 9911526, REV AZ, AND REV AN.Aug 22, 2018 · N939AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018081325034Longeron · damagedLONGERON 24L WAS FOUND DAMAGED BETWEEN BS 389 - 490. CUT OUT THE SECTION OF THE LONGERON. FABRICATED REPAIR SPLICES AND CUT A NEW LONGERON. WORK ACCOMPLISHED IAW SRM 53-00-05, REPAIR 2. ACCOMPLISHED HFEC IAW NDT SPM 06-10-01.001, NO CRACKS INDICATED. INAug 11, 2018 · N939AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018081325033Longeron · damagedLONGERON 25L WAS FOUND DAMAGED BETWEEN BS 427 - 490. CUT AND REMOVED THE SECTION OF THE LONGERON . ACCOMPLISHED HFEC IAW NDT SPM 06-10-01. 001, NO CRACKS INDICATED. FABRICATED A REPLACEMENT LONGERON AND SPLICES. INSTALLED THE LONGERON SECTION IAW SRM 53-00-Aug 11, 2018 · N939AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018073104781Release Cable · out of positionAFT INTERNAL TAILCONE RELEASE SYSTEM FAILED THE DROP TEST. IT REQUIRED MORE THAN 35LBS PULL TO ACTIVATE. MAINTENANCE REROUTED THE INTERNAL HANDLE RELEASE CABLE TO THE PROPER ROUTING IAW AMM 53-52-01. TAILCONE RELEASE REPEAT OPERATIONAL CHECK WAS GOOD.Jul 28, 2018 · N939AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2017091906979Lens · missingDURING SVC CHECK FOUND EMERGENCY LIGHT DIFFUSER LENS MISSING AT SEAT 12B. FWD TO NEF 33-51-02. REPLACED MISSING LENS COVER.Sep 17, 2017 · N939AT · Boeing 717200 · Emergency LightingSDR DALA2017083106468Light · malfunctionedTHE FLIGHT CREW FOUND THEY COULD NOT CONTROL THE EMERGENCY PATHWAY LIGHTING IN THE CABIN: IT WOULD FLICKER ON AND OFF ON ITS OWN. MAINTENANCE CALLED IT AN ANOMALY AND DID NOT DO ANY FURTHER TROUBLESHOOTING.Aug 31, 2017 · N939AT · Boeing 717200 · Emergency LightingSDR DALA2017051503893Door Frame · corrodedAFT CARGO BAY HAD CORROSION ON DOOR FRAME PAN. A REPAIR WAS ACCOMPLISHED IAW ETI 17-17-062, REV 3 AND ER/A 558101-14, REV ORIGINAL.May 13, 2017 · N939AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017051403866Repair · damagedELONGATED SEVERAL HOLES ON PREVIOUS REPAIR DOUBLER AT VERTICAL STABILIZER LE SPLICE AT STA ZFS=52.267. REPAIR WAS ACCOMPLISHED PER ETI-17-17-060 REV 3 AND ER/A 535894-14AD REV A.May 13, 2017 · N939AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2017051303865Skin · crackedCRACK ON PRODUCTION DOUBLER UPPER SKIN STA Y=1176 CANT BTW LONG 1 TO 3 RT AFT ACCESSORY COMPARTMENT. REPAIR WAS ACCOMPLISHED PER ETI-17-17-052 REV ORIGINAL AND ER/A 558094-14 REV ORIGINAL.May 12, 2017 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017051203815Skin · crackedCRACKS ON PRODUCTION DOUBLER UPPER SKIN STA Y=1176 CANT BTW LONGS 3L TO 3R AFT ACCESSORY COMPARTMENT. CRACK ON PRODUCTION DOUBLER UPPER SKIN STA Y=1176 CANT BTW LONGS 1 TO 3 LT AFT ACCESSORY WAS REPAIRED PER SRM 53-30-08-2R PROCEDURE 10 REPAIR 10. HFEC INSPECTMay 11, 2017 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017051203814Frame · crackedCRACK ON MAIN FRAME AFT LT STA 1022 LONG 7L. CRACK ON MAIN FRAME AFT LT STA 1022 LONG 7L WAS REPAIRED PER ETI-17-17-052 REV. ORIGINAL AND ER/A 558094-14 REV ORIGINAL.May 11, 2017 · N939AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017051203813Door · wornWEAR ON INNER SURFACE OF LT MLG STRUT DOOR. RT MLG DOOR STRUT WAS REPAIRED IN ACCORDING ETI. 17-17-060 REV ORG AND ER/A 558089-14 REV ORIG.May 11, 2017 · N939AT · Boeing 717200 · Landing Gear DoorsSDR DALA2017051003726Frame · corrodedCORROSION ON FRAME ANGLE BS 974 BETWEEN LONGERONS 24L - 29R IN THE AFT CARGO BAY. THE FRAME ANGLE WAS REPLACED IAW SRM 53-20-07-01-3, AND DWG 9958215, REV AM.May 9, 2017 · N939AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017050903673Door Frame · crackedCRACKED DOOR FRAME BEAM LT SIDE OF NOSE GEAR WHEEL WELL NEAR BS 69.550. REPAIRED IAW ETI-17-17-057, REV 3, AND ER/A 558076-14, REV ORIGINAL.May 8, 2017 · N939AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017050703611Hinge · wornFREE PLAY ON AFT HINGE AT FWD CARGO DOOR. REPAIRED AIW ER/A 558081-14, REV ORIGINAL.May 6, 2017 · N939AT · Boeing 717200 · Fuselage, Door HingeSDR DALA2017050703610Door Frame · crackedCRACK DOOR JAMB BEAM RT SIDE OF NOSE GEAR WHEEL WELL NEAR STA Y=69.550. REPAIR WAS ACCOMPLISHED PER SRM 53-10-14-2R.May 6, 2017 · N939AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017050503577Intercostal · damagedCRACKED AND BENT ON INTERCOSTAL FWD FACE BS 1225, LONGERON 22L AFT ACCESSORY COMPARTMENT. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02, AND 51-10-05, AND DWG 9917701, REV.May 4, 2017 · N939AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017050503576Rub Strip · corrodedCORROSION ON RUBSTRIPS OF FUEL ACCESS PANEL ON THE LT WING. THE RUBSTRIP WAS REPLACED PER B 717-200 SRM 57-10-01 REP 3 PAR 6.May 4, 2017 · N939AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017050503575Skin · crackedFUSELAGE SKIN CRACKED BS 1022, LONGERON 14L. REPAIRED IAW ETI-17-17-050, REV ORIGINAL, AND ER/A 556410-14, REV ORIGINAL.May 4, 2017 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017050503573Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL COUNTERSINK. CORROSION REMOVED PER B717 SRM 57-10-01-2R-2 PAR 5 CONDITION II (2) AND (3).May 4, 2017 · N939AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017050503572Web · damagedELONGATED HOLES ON R1 DOOR WEB AND PAN UPPER/FWD CORNER. REPAIRED IAW ER/A 556413-14, REV ORIGINAL, AND ETI-17-17-051, REV ORIGINAL.May 4, 2017 · N939AT · Boeing 717200 · Service DoorsSDR DALA2017050403545Angle · crackedCRACK ON ANGLE AFT FACE BS 1158 LONGERON 2L IN THE AFT ACCESSORY COMPARTMENT. REPLACED IAW SRM 51-41-05, AND 51-41-02.May 4, 2017 · N939AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017050103482Frame · crackedCRACKED FRAME BS 679, BETWEEN LONGERONS 25 - 28L IN KEEL BEAM AREA. REPAIRED IAW SRM 51-70-11-2R, REPAIR 1.Apr 30, 2017 · N939AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017050103481Floor Panel · brokenBROKEN FLOOR PANEL 221SP. REPAIRED IAW SRM 53-20-50-2R-5.Apr 30, 2017 · N939AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017050103480Frame · crackedCRACKED FRAME BS 679 BETWEEN LONGERON 25 - 28R. THE FRAME WAS REPAIRED IAW SRM 51-70-11-2R.Apr 30, 2017 · N939AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017043003479Frame · crackedCRACKED MAIN FRAME ANGLE BS 1022 BETWEEN LONGERONS 16 AND 17L. THE FRAME ANGLE WAS REPLACED IAW SRM 53-00-06R, 51-41-05, AND DWG 9912243, REV JS.Apr 29, 2017 · N939AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017043003477Channel · crackedCRACKED CHANNEL OF FLOOR PANEL 222AFF. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-20-50-2R-5.Apr 29, 2017 · N939AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017042903475Angle · corrodedCORRODED ANGLE, BELOW THE RT CONSOLE, BETWEEN BS 120 - 148, RBL 54 IN THE COCKPIT. THE ANGLE WAS REPLACED IAW SRM 51-41-02, AND DWG 9936533, REV CM.Apr 28, 2017 · N939AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017042803443Angle · corrodedCORROSION ON RT CUSP ANGLE LOWER SURFACE FROM BS 737 - 756. A NEW CUSP ANGLE WAS REPLACED IAW SRM 51-41-02.Apr 27, 2017 · N939AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017042803442Access Panel · crackedCRACKED FUSELAGE ACCESS PANEL 370AR. THE ACCESS PANEL WAS REPAIRED SRM 55-00-00-2R, REPAIR 1, PROCEDURE 1, AND 51-41-02 HFEC INSPECTION WAS ACCOMPLISHED ON ACCESS PANEL 370 AR, NO CRACKS WERE FOUND AFTER STOP DRILL IAW NDT SPM 06-10-01.001.Apr 27, 2017 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017042703414Pan · crackedCRACKED WINDOW RING PANS ON FOLLOWING LOCATIONS. LWR RT STA 909, UPPER LT STA 850, UPPER LT STA 831. CRACKED WINDOW RING PANS WERE REPAIRED PER SRM 56-20-02-2R.Apr 26, 2017 · N939AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017042603412Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT STA Y=180 BTW X=-9 TO X=-42 FWD WET AREA. DUE TO EXCESSIVE CORROSION ON FLOOR SUPPORT WAS REPLACED PER SRM 51-41-05 AND 51-40-08-0G AND 51-10-04 PAR 15 AND 21.Apr 26, 2017 · N939AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016122610065Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS FOR THE CATWALK WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD. (LP #9077376)Dec 25, 2016 · N939AT · Boeing 717200 · Emergency LightingSDR DALA2016081505971Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR THE AFT COMPARTMENT DOOR WAS INOPERATIVE. MAINTENANCE FOUND THAT THE BATTERY PACK WAS NOT CHARGING AND REPLACED THE CHARGER B5-260. THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (LP #892Aug 13, 2016 · N939AT · Boeing 717200 · Emergency LightingSDR DALA2016062804986Battery Pack · dischargedDURING SERVICE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS IN ROWS 15-19 OF THE CABIN AND THE AFT TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Jun 28, 2016 · N939AT · Boeing 717200 · Emergency LightingSDR DALA2016062404913Skin · damagedFUSELAGE SKIN DAMAGE BETWEEN STA 1095 AND STA 1116, L-21L AND L-23L REF EMPOWER NR 35, RII ENTRY, REF NR 35 REPAIRS MADE IAW ER/A 547473-14, REV A. ASSOCIATED ER/A 14-547473 ADDED FOR AC 9562.Jun 23, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062304865Skin · dentedFUSELAGE DENT ON LT SIDE, STA 1087 AT L-20L. CW ER/A 547473-14, REV A, FINAL ER/A MATCHES ALL PRI REVISIONS.Jun 22, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062304863Skin · damagedDAMAGE TO EMPENNAGE SKIN STA 1178-1144 FROM LONGERON 3R-9R MULTIPLE LOCATIONS. REPAIRED SKIN IAW ER/A 547582-14, REV ORIGINAL ER/A MATCHES ALL PRIS.Jun 22, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062304862Skin Panel · damagedVERTICAL STABILIZER, RT L/E LOWER MAIN SKIN PANELS DENTED AND GOUGED. REPAIRED SKIN IAW ER/A 547396-14, REV ORIGINAL, ER/A MATCHES ALL PRIS.Jun 22, 2016 · N939AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2016062304859Skate Angle · deformedRT SIDE VERTICAL STABILIZER ATTACH SKATE ANGLE IS DEFORMED. REPAIRED IAW ER/A 547541-14, REV ORIGINAL ER/A MATCHES ALL PRIS.Jun 22, 2016 · N939AT · Boeing 717200 · Fuselage, Stabilizer Attach FittingsSDR DALA2016062304858Frame · dentedCANTED FRAME 1189 IS DENTED AT SKIN CUTOUT FOR REPAIR OF DAMAGE AT STR-11R. REPAIRED IAW ER/A 547985-14, REV A, SECTION 2, FRAME DAMAGE PERMANENT REPAIR.Jun 22, 2016 · N939AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016060104310Skin · damagedFUSELAGE SKIN DAMAGED AT APPROXIMATELY BS 1155 L-20L. COMPLETED REPAIR, REF SRM 53-03-01, FIG 204. CLASS 1, REF NR 27 SUMMERY.Jun 1, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062404926Skin · damagedDAMAGE TO VERTICAL STABILIZER RT SKATE ANGLE AND SKIN BETWEEN L2R AND L4R, BETWEEN STA 1103 AND 1145. ACCOMPLISHED HFEC INSPECTION OF CRACK IAW NDT/SPM 06-10-01.001, MARKED THE END OF THE CRACK END AND VERIFIED AFT CRACK EXTENDS INTO CENTER OF A RIVET HOLE OTMay 19, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062404915Skin · puncturedFUSELAGE SKIN PUNCTURED BETWEEN CANTED STA 1103 AND 1131 BETWEEN L6R AND L7R. CUTOUT DAMAGED SKIN. ACCOMPLISHED HFEC INSPECTION OF CUTOUT IAW NDT/SPM 06-10-01.001. NO CRACKS NOTED. INSTALLED DOUBLER IAW INSTRUCTIONS OF ER/A 547090-14, SECTION III. ASSOCIAMay 19, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051904045Skin · gougedLT FUSELAGE GOUGE / DENT 3" X 8" BS 1159, STR 19-20L .0625" DEEP. BLENDED IAW SRM 53-01-01. ACCOMPLISHED HFEC IAW NDT/SPM 06-10-01.001, NO CRACKS NOTED. ACCOMPLISHED INTERNAL GVI, NO DAMAGE NOTED. ACCOMPLISHED UT INSPECTION IAW NDT/SPM 04-00-03. ALODINE AND May 19, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062404927Skin · damagedDENT AND GOUGES IN RT VERTICAL STABILIZER SKIN APPROXIMATELY 12" ABOVE FUSELAGE BETWEEN CS 1103 AND CS 1131. BLEND AREA OF PAINT FOR HFEC. REF SRM 53-01-01. ACCOMPLISHED HFEC INSPECTION OF BLENDED AREA IAW NDT SPM 06-10-01.001. NO CRACKS NOTED. ALODINE ANDMay 18, 2016 · N939AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2016062404925Skin · gougedMULTIPLE GOUGES AND DENTS AT L-3R BETWEEN FS 1095 AND FS 1144. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LOMay 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/Skin
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