N971AT

Service difficulty reports · 229

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 = 'N971AT' 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 DALA2021110406787None · noneREF NRC 503: CRACK FOUND ON APU EXHAUST DUCT MATING FLANGE. MARKED. NRC 503: COMPLIED WITH PRI 594460-14 REV 3 AND ERA 594460- 14 REV ORG (PRI AND ERA MATCH). (LP #1977938)Oct 9, 2021 · N971AT · Boeing 717200 · APU Exhaust SystemSDR DALA2021100506082None · noneCORROSION AFT CARGO STR30 STA870-990. (MKD). SUMMARY SEE NRC 056-0008:5331-2001/002 00294: REPAIRED PER B717 SRM 53-20-05-2R PROCEDURE 1. (LP #1971678)Oct 4, 2021 · N971AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2021100506081None · noneCORROSION AFT CARGO STR29L STA870-960. (MKD). SUMMARY SEE NRC 056-0008:5331-2001/001 00293: REPAIRED PER B717 SRM 53-20-05-2R PROCEDURE 1. (LP #1971674)Oct 4, 2021 · N971AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2021100506079None · noneSHEAR TIE @ STA 974 IS CORRODED BETWEEN STR 29L AND STR 30. LSUMMARY SEE NRC 056-0008:5331-2001/009 00449: REPLACED PER DWG #9958215 AND B-717 SRM 51-40-02. (LP #1968275)Oct 1, 2021 · N971AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2021100506078None · noneSHEAR TIE @ STA 954 IS CORRODED BETWEEN STR29L AND STR30. SUMMARY SEE NRC 056-0008:5331-2001/010 00450: REPLACED PER DWG #9958214 AND B717 SRM 51-40-02. (LP #1968271)Oct 1, 2021 · N971AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2021110506808None · noneAFT CARGO DOOR CUTOUT: SKIN CRACKED AND BENT LOCATED DIRECTLY FWD OF THE STOP FITTING SECOND FROM THE BOTTOM AFT SIDE. MARKED. COMPLIED WITH B717 SRM 53-20-15-2R PROCEDURE 10 OPTION 2. (LP #1967266)Sep 30, 2021 · N971AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2021100506075Doubler · corrodedSEVERE CORROSION FOUND ON L-DOUBLER UNDER FRAME 1053. SUMMARY SEE NRC 055-0022:5310-2014/007 00470: REPLACED PER DWG# 9915561. (LP #1967265)Sep 30, 2021 · N971AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2021100105940None · noneCORROSION FWD / LWR / CTR. (MKD). SUMMARY SEE NRC 055-0022:5310-2014/001 00292: REPLACED TRIANGLE DOUBLER PER DWG #5910130. BLENDED AND CHECKED LIMITS ON P-DOME SKIN PER B717 SRM 53-20-08-2R. (LP #1964541)Sep 28, 2021 · N971AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2021062903513Regulator · faultedSHIP 9533 - THE FLIGHT CREW RECEIVED A "TAIL MANIFOLD FAIL" TWICE ON DESCENT IN TO AVL AND DIVERTED TO CLT. AN EMERGENCY WAS DECLARED. CORRECTIVE ACTION: MAINTENANCE REPLACED THE TAIL PRESSURE REGULATING AND SHUTOFF VALVE AND RE-SECURED PNEUMATIC SENSE LINE ONJun 28, 2021 · N971AT · Boeing 717200 · Pneumatic Indicating SystemSDR DALA2020121404062Lens · damagedTHE EMERGENCY EXIT COVER DIFFUSER LENS IS DAMAGED OR MISSING. MAINTENANCE REPLACED THE LIGHT ASSEMBLY L2-791 FIRST CLASS MIDDLE AISLE, REF SWPM CH 20 AND B717 WDM 33-51-12. OPERATIONAL CHECK WAS GOOD.Dec 14, 2020 · N971AT · Boeing 717200 · Emergency LightingSDR DALA2020120703988Battery Pack · inoperativeTHE EMERGENCY OVERHEAD LIGHT AND EXIT SIGN ABOVE THE FLIGHT ATTENDANT SEAT AT THE L1 DOOR WAS NOTED BY THE FLIGHT ATTENDANT TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-235, PER B717 AMM 33-56. OPERATIONAL CHECK WAS GOOD.Dec 5, 2020 · N971AT · Boeing 717200 · Emergency LightingSDR DALA2020061202464Light · inoperativeTHE LT OVERWING EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE LT OVERWING EMERGENCY LIGHT IAW AMM 33-51. OPERATIONAL CHECK WAS GOOD.Jun 12, 2020 · N971AT · Boeing 717200 · Emergency LightingSDR DALA2019022541194Frame · crackedL/H OVERWING FRAME AT STA 696 CRACKED REF 5310-01436-04A STEP #10. NRC 034-0001:5310-01436-04A/001 00021: REPLACED FRAME PER ROUTINE CARD 5310-01436-03A. (LP #0957078)Feb 23, 2019 · N971AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019022531188Door Sill · damagedDURING BUY BACK OF BLEND REPAIR FOUND LOW SPOT ON AFT CARGO COMPTARTMENT DOOR SILL AFT OF DOOR DOWN STOP FITTING. MKD. NRC 001-0307:5231-2002/006 00178: REPLACED DOOR JAMB REF B717 SRM 53-20-15-2R PROCED 7. (LP #0955479)Feb 22, 2019 · N971AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018111656644Retainer · brokenWHILE WORKING WORK CARD, THE TAILCONE ESCAPE SLIDE SAFETY PIN INSPECTION REVIELED THAT THE TAIL CONE SLIDE COVER CLIP RETAINER WAS BROKEN. A NEW TAILCONE ESCAPE SLIDE COVER CLIP RETAINER WAS INSTALLED PER ZODIAC AEROSPACE CMM 25-66-20. (LP #4860405)Nov 14, 2018 · N971AT · Boeing 717200 · Escape SlideSDR DALA2017122708919Power Supply · inoperativeON SERVICE CHECK, MAINTENACE FOUND FOUR EMERGENCY EXIT LIGHTS, IN THE TAIL COMPARTMENT PASSAGE WAY TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY (B5-260) IAW AMM 33-51. OPS CHECK WAS NORMAL.Dec 24, 2017 · N971AT · Boeing 717200 · Emergency LightingSDR DALA2017070205124Lens · missingSTANDBY DIFFUSER LENS IS MISSING AT ROW 27. INSTALLED SERVICEABLE LENS COVER ON EMERGENCY LIGHT AT ROW 27, OPS CK NORMAL.Jul 1, 2017 · N971AT · Boeing 717200 · Emergency LightingSDR DALA2017040402712Skin · crackedSKIN CRACK ON THE TOP OF THE FUSELAGE AT BS 1133 TO THE LEFT OF THE VERTICAL STAB. REPAIRED THE SKIN IAW ERA 555586-14AD REV 0.Mar 31, 2017 · N971AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017040402711Skin · crackedSKIN CRACK ON THE TOP OF THE FUSELAGE AT BS 1133 ON THE RIGHT SIDE OF THE VERTICAL STAB. REPAIRED THE SKIN IAW ERA 555587-14AD, REV O.Mar 31, 2017 · N971AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017040402714Pan · corrodedFWD CARGO DOOR FRAME CORRODED IN SEVERAL PLACES. REPAIRED CARGO FRAME PAN IAW SRM 53-20-15-2R.Mar 29, 2017 · N971AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017040402713Skin · corrodedLARGE AREA OF BLOW OUT CORROSION BS 737 TO SLANT PANEL LBL 4. REPAIRED THE AREA IAW ERA 555592-14 REV 0.Mar 29, 2017 · N971AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017032902555Skin · crackedSKIN CRACKED ON THE TOP OF THE FUSELAGE AT BS 1152 ON THE LEFT OF THE VERTICAL STAB. REPAIRED THE SKIN CRACK IAW ER/A 555585-14, AND PRI 555585-14, REV 0 AND 1.Mar 27, 2017 · N971AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017032902554Frame · corrodedCORROSION FRAME BS 946 BETWEEN LONGERONS 29 - 30R. REPAIRED IAW SRM 53-00-06-2R-2, AND 51-32-01.Mar 24, 2017 · N971AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017032702412Seat Track · damagedSEAT TRACK BS 200 - 256, RBL 44.5, GOUGED AND CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 53-20-52-1A-1, FIG 201, SRM 51-40-02-0G, 51-40-04, 51-41-08-0G, AND 51-41-05-0G.Mar 24, 2017 · N971AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017032502405Angle · corrodedR1 DOOR FRAME LOWER TRIANGLE POCKETS HAVE CORROSION. REPLACED RIGHT CUSP ANGLE FROM BS 158 TO 229 IAW SRM 53-00-55, REPAIR 3, SRM 51-41-02, & SRM 51-41-05.Mar 24, 2017 · N971AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017032902558Vane · delaminatedRIGHT FORWARD MOVEABLE VANE HAS DELAMINATION ON THE UPPER SKIN. REPAIRED THE VANE IAW SRM 57-53-01-2R-1, AND SRM 51-70-02-0G. RESTORED FINISH IAW AMM 51-10-00 370-805.Mar 23, 2017 · N971AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2017032902556Skin · delaminatedRIGHT FORWARD MOVEABLE VANE HAS DELAMINATION ON THE UPPER SKIN. REMOVED FWD VANE, REPAIRED THE DELAMINATED AREA WITH A DOUBLER IAW SRM 57-53-01-2R-1, PARA 4B-4C, AND SRM 51-70-07-0G. INSTALLED THE VANE IAW AMM 27-50-03 400-801.Mar 23, 2017 · N971AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2017032802514Skin · crackedSTA 1022 ABOVE LONGERON 14L FUSELAGE SKIN CRACKED AT FORMER LWR FWD FASTENER (EXTERNAL). HFEC VERIFIED IAW NDT SPM 06-10-01-.001 ETHF PROCEDURE 1, CUT OUT REGION OF EXTERNAL SKIN AND INTERNAL DOUBLER AND INSTALLED REPAIR AT FS 1022 ABOVE LONGERON 14L IAW ER/AMar 23, 2017 · N971AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017032702413Attach Angle · chafedATTACH FLANGE UNDER PANEL 370AL CHAFED. THE ATTACH ANGLE WAS FOUND TO BE CRACKED, REPLACED THE ATTACH FLANGE IAW DWG 5910242, AND SRM 51-41-02.Mar 22, 2017 · N971AT · Boeing 717200 · Vertical StabilizerSDR DALA2017032302373Former · crackedLT CANTED KEEL FORMERS ARE CRACKED O/B ENDS STA 674, 696, 715. REPAIRED LT CANTED KEEL FORMERS IAW ER/A 545683-14MA REV 0.Mar 22, 2017 · N971AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017032202327Splice · corrodedCORROSION ON RT SIDE CUSP WEB AT FUSELAGE SKIN SPLICE BETWEEN FRAME STA 579-598 BELOW FLOOR. FOUND CORROSION TO BE ON CUSP ANGLE SPLICE ONLY. REPLACE CUSP ANGLE SPLICE IAW DWG 9910151 AND SRM 51-40-02.Mar 21, 2017 · N971AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017032202285Seat Track · damagedLEFT CENTER SEAT TRACK BS 756 - 856, LBL 44.5 HAS SCRATCHES, AND CORROSION. BLENDED THE SEAT TRACK. REPAIRED IAW 53-20-52 REP 5.Mar 21, 2017 · N971AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017032202284Skin · crackedBS 1087 ABOVE LONGERON 14L FUSELAGE SKIN CRACKED. HFEC VERIFIED IAW NDT SPM 06-10-01.001 ETHF PROCEDURE 1. REPAIRED IAW ERA 555590-14 REV 0.Mar 21, 2017 · N971AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017032202279Cusp Web · crackedFOUND CRACKED CUSP WEB AT BS 814, LBL45. REMOVED THE DAMAGED SECTION OF THE CUSP WEB AND INSTALLED A REPAIR DOUBLER IAW SRM 53-00-55, REPAIR 4, FIG 221.Mar 21, 2017 · N971AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017032202328Cusp Web · corrodedCUSP MEMBRANE AT RT STA 180 CORRODED. BLENDED CORROSION OUT OF LIMITS IAW SRM 53-00-55 FIG 101 ORIGINAL THICKNESS .020, .020 REMOVED. REPAIRED CUSP MEMBRANE IAW ER/A 551819-14MA2.Mar 20, 2017 · N971AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017032002191Seat Track · corrodedUPPER FUSELAGE, RIGHT INBD SEAT TRACK, STA 200 TO STA 256 BL22R, GOUGED AND CORRODED METAL. CORROSION AT STA 235 RBL 22 EXCEEDED 50% OF ORIGINAL THICKNESS, FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52 1A-1, 51-30-07-0G. INSTALLED NEW SECTION OF SEAT TRACK RBL 22Mar 19, 2017 · N971AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017032202282Seat Track · corrodedRIGHT INBD SEAT TRACK, RBL 22, BS 429 IS CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-20-52-2R.Mar 17, 2017 · N971AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017032202281Seat Track · corrodedRIGHT INBD SEAT TRACK, RBL 22, BS 358 - 456 HAS AREAS OF LIGHT CORROSION AND MISSING PAINT. BLENDED THE SEAT TRACK. FOUND TO BE OUT OF LIMITS. REPAIRED SEAT TRACK BS 400-403 IAW SRM 53-20-52-2R.Mar 17, 2017 · N971AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017031702114Cusp Web · damagedCRACK AND CORROSION AT THE UNDERSIDE OF THE CUSP WEB AT BS 612, RBL 56. REPAIRED THE CUSP WEB IAW SRM 53-00-55 2R-4.Mar 15, 2017 · N971AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017032202283Pan · crackedFLC DOOR FWD SIDE AT LOCKING LATCH BRACKET LOOSE AND DOOR PAN CRACKED. REPAIRED THE PAN IAW SRM 52-30-02-2R PROCEDURE 4, FABRICATED A REPAIR DOUBLER IAW SRM 51-22-01, PAGES 2 - 5. TIGHTENED LATCH BRACKET IAW SRM 51-41-01, FIG 1.Mar 13, 2017 · N971AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017031702115Pan · crackedFLC DOOR AFT SIDE AT LOCKING LATCH BRACKET LOOSE AND CRACKED DOOR PAN. REPAIRED THE DOOR PAN IAW SRM 52-30-02-2R PROCEDURE 4.Mar 10, 2017 · N971AT · Boeing 717200 · DoorsSDR DALA2017011700352Terminal · looseDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN THE COCKPIT WAS INOPERATIVE. MAINTENANCE FOUND THAT THE BATTERY CONNECTION WAS LOOSE. THE BATTERY CONNECTOR WAS SECURED AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Jan 15, 2017 · N971AT · Boeing 717200 · Light System WiringSDR DALA2016090606386Battery Pack · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT ROW 20 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Sep 4, 2016 · N971AT · Boeing 717200 · Emergency LightingSDR DALA2016060304372Lanyard · disconnectedF/A DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE AT DOOR 1L HAD A DISCONNECTED LANYARD. THE LANYARD WAS NOT CONNECTED BETWEEN THE GIRT-BAR AND THE SLIDE RELEASE. THIS WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14 CFR PARTJun 2, 2016 · N971AT · Boeing 717200 · Escape SlideSDR DALA2016032302230Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT ROWS 1-5 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Mar 21, 2016 · N971AT · Boeing 717200 · Emergency LightingSDR DALA2015121707646Lanyard · unsecureMAINTENANCE DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE LANYARD AT THE 1L DOOR WAS NOT SECURED. THE LANYARD WAS NOT CONNECTED BETWEEN THE GIRT-BAR AND THE SLIDE RELEASE. THIS WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14Dec 16, 2015 · N971AT · Boeing 717200 · Escape SlideSDR DALA2015110106689Fire Detector · false activationRETURNED TO DEPARTURE DUE TO LT ENGINE FIRE WARNING. CREW ACCOMPLISHED QRH PROCEDURES. BOTH FIRE BOTTLES WERE UTILIZED AND FIRE WARNING REMAINED WITH ENGINE SHUTDOWN. MAINTENANCE REPORTED FIRE INDICATION ILLUMINATED AFTER ACFT ARRIVED AT THE GATE. DISCONNENov 2, 2015 · N971AT · Boeing 717200 · Fire DetectionSDR DALA2015081104905Door Frame · crackedDURING LT OVERWING FRAME 715 INSPECTION, HFEC CONFIRMED CRACK .125" DEEP. REPAIRED IAW AMDS WC 5310-01436-03A.Aug 10, 2015 · N971AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2015080904904Cusp Web · damagedDURING OVERWING FRAME INSPECTION, FOUND CUSP WEB FROM BS 674 - 715 LT SIDE DAMAGED. REPAIRED IAW ER/A 533035-14MA AND SRM 51-02, PAGE 1.Aug 8, 2015 · N971AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015080704846Cusp Web · crackedCUSP WEB UNDER SEAT TRACK SPLICE AT STA 591, LBL 55 IS CRACKED. REPAIRED IAW DWG 9910151-115.Aug 7, 2015 · N971AT · Boeing 717200 · Fuselage Miscellaneous Structure
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