N959AT

Service difficulty reports · 213

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 = 'N959AT' 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 DALA2016081606037Skin · crackedCRACK ON EXTERNAL FUSELAGE STA 1133 BETWEEN LONGERON 2-3 RT, CARD 14, ZONE 200. REPAIR WAS ACCOMPLISHED IAW ER/A 547895-14 AD REV ORIGINAL. LENGTH CRACK 0.150". REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY. ADDITIONAL ER/A REV WITH AMOC IS REQUIRED Aug 15, 2016 · N959AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016081606036Skin · crackedCRACK ON EXTERNAL FUSELAGE STA 1133 BETWEEN LONGERON 2-3 LT, CARD 13, ZONE 200. REPAIR WAS ACCOMPLISHED IAW ER/A 547895-14, REV ORIGINAL. LENGTH CRACK 0.200". REPAIR APPROVAL IS LIMITED TO 24 MONTHS SERVICE ONLY. ADDITIONAL ER/A REVISION WITH AMOC IS REQUIRAug 15, 2016 · N959AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016081405966Structure · corrodedCORROSION ON PASSENGER ENTRANCE STAIR DOOR. DOOR WAS REPLACED DUE TO EXCESSIVE CORROSION (MORE THAN HALF THICKNESS) IAW SRM 52-00-00 FIG.103.Aug 13, 2016 · N959AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016081405965Cargo Track · corrodedCORROSION ON CARGO TRACK BS 994 - 1002 BETWEEN LONGERONS 27 AND 28R. DUE TO EXCESSIVE CORROSION, THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01.Aug 13, 2016 · N959AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016081205963Access Panel · corrodedCORROSION ON COURTESINKS ACCESS PANEL 620. CORROSION WAS REMOVED IAW SRM 51-10-04 AND FOUND OUT OF LIMITS IAW SRM 57-10-01 AND THE ACCESS PANELWAS REPLACED. .Aug 11, 2016 · N959AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016081105923Structure · crackedCRACKS ON NLG JAMB AT STA Y=45 AND STA X=20 AND X=-20, SM, CARD 1, ZONE 115. REPAIR WAS ACCOMPLISHED IAW ER/A 549227-14, REV ORIGINAL AND ETI-17-16-107, REV ORIGINAL.Aug 10, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017010500101Drag Brace · corrodedRUST ON NLG DRAG BRACE ASSY. (TAPPER PIN LT/RT, END BEARING LT, RT, AND CROSS TUBE). NOSE LANDING GEAR ASSY WAS REPLACED IN REFERENCE WITH IPC 32-00-00-01 AND THE CARD 3221-4001 ZONE 710 JOB #000-0003. RII COMPLETED.Aug 9, 2016 · N959AT · Boeing 717200 · Nose/Tail Landing Gear Strut/AxleSDR DALA2017010500100Thrust Washer · corrodedCORROSION ON THRUST WASHER AT NOSE LANDING GEAR. NOSE LANDING GEAR ASSY WAS REPLACED IAW IPC 32-00-00-01 AND THE CARD 3221-4001, ZONE 710 JOB 000-0003. RII COMPLETED.Aug 9, 2016 · N959AT · Boeing 717200 · Nose/Tail Landing Gear Strut/AxleSDR DALA2016081005905Beam · crackedCRACK ON BEAM NR 7, STA 162.5 AT FWD PASSENGER DOOR STRUCTURE, SM, CARD 15, ZONE 820. CRACK ON BEAM NR 7 WAS REPAIRED IAW SRM 52-10-02, FIG 202. HFEC INSPECTION WAS ACCOMPLISHED NO CRACKS WERE FOUND AFTER STOP DRILL IAW NDT SPM 06-10-01.001. CRACK LONG .750"Aug 9, 2016 · N959AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016080905885Floor Panel · damagedCRACKED CHANNEL ON FLOOR PANEL. FLOOR PANEL REPAIRED PER SRM 53-20-50 FIG. 201.Aug 8, 2016 · N959AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016080905884Cusp Web · corrodedCORROSION ON RT CUSP WEB REPAIR DOUBLER LOWER SKIN BS 446 - 465, X 56 - X 60. REPAIRED PER SRM 53-05-55 FIG. 216, 51-41-02, 51-40-8 PAR. 3, AND 51-10-04 PAR 21-15 AND 37, 51-41-05.Aug 8, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080905883Cusp Web · corrodedCORROSION ON RT CUSP WEB BETWEEN BS 484 - 503. REPAIRED IAW SRM 51-41-02, 53-00-55. FIG.215 AND 51-41-05.Aug 8, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080805823Seat Track · corrodedCORROSION ON LT SEAT TRACK, X=44.5 BETWEEN STA 957-STA 960, ON REF CARD 23, ZONE 200. CUT OUT IN TRACK WAS ACCOMPLISHED IAW SRM 53-20-52, FIG 201, ON STA 957-STA 960, X=44.5 NDT INSPECTION ON AREA NO CRACKS WERE FOUND AROUND CUTOUT, IAW NDT SPM 06-10-01-001, Aug 7, 2016 · N959AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016080805822Fitting · crackedCRACKED RT CLIP FRAME ON CANTED KEELBEAM STA 681 AND 696, CARD 17, ZONE 140. FRAME CLIPS ON STA 681 AND STA 696 WERE REPAIRED IAW SRM 51-70-11, FIG 201.Aug 7, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080805821Fitting · crackedCRACKED LT CLIP FRAME ON CANTED KEELBEAM, STA 681 AND STA 696, CARD 16, ZONE 140. FRAME CLIPS ON STA Y=681 AND Y=696 WERE REPAIRED IAW SRM 51-70-11, FIG 201.Aug 7, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080605820Cusp Web · corrodedEXCESSIVE CORROSION ON LT CUSP MEMBRANE BETWEEN STA 756-775 IN REF CARD 62, ZONE 200. WB, CARD 104, ZONE 200. DUE TO CUSP WEB MEASURE OUT OF LIMITS .028" OF .040", REPAIR WAS ACCOMPLISHED IAW SRM 53-00-55, FIG 215. RII COMPLETED.Aug 5, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016110208145Access Panel · corrodedCORROSION ON ACCESS PANEL 370KR VOR / LOCALIZER ANTENNA PANEL.. UPPER RT VOR / LOCALIZER ANTENNA WAS REPLACED IAW AMM 34-32-03 AND TEST WAS PERFORMED IAW AMM 34-35-01 TEST OK.Aug 4, 2016 · N959AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016110208144Access Panel · corrodedCORROSION ON ACCESS PANEL 370JL VOR / LOCALIZER ANTENNA PANEL. UPPER LT VOR / LOCALIZER ANTENNA PANEL WAS REPLACED IAW AMM 34-32-03 AND TEST WAS PERFORMED IAW AMM 34-35-01. TEST OK.Aug 4, 2016 · N959AT · Boeing 717200 · Visual Omnirange (VOR) SystemSDR DALA2016110208143Access Panel · corrodedCORROSION ON ACCESS PANEL 370DL VOR/LOCALIZER ANTENNA PANEL. LOWER LT VOR/LOCALIZER ANTENNA PANEL WAS REPLACED IAW AMM 34-32-03 AND TEST WAS PERFORMED IAW AMM 34-35-01. TEST OK.Aug 4, 2016 · N959AT · Boeing 717200 · Visual Omnirange (VOR) SystemSDR DALA2016110108052Access Panel · corrodedCORROSION ON ACCESS PANEL 370GR VOR/LOCALIZER ANTENNA PANEL. LOWER RT VOR/LOCALIZER ANTENNA PANEL WAS REPLACED IAW AMM 34-32-03 AND TEST WAS PERFORMED IAW AMM 34-35-01. TEST OK.Aug 4, 2016 · N959AT · Boeing 717200 · Glide Slope SystemSDR DALA2016080505780Pan · crackedCRACKED RT RING PAN FWD LWR BS 794. REPAIRED IAW SRM 56-20-02 TYPE B REPAIR FIG 202.Aug 4, 2016 · N959AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016080405761Cusp Web · corrodedCORROSION ON RT CUSP WEB REPAIR DOUBLER AND ADJACENT AREA BETWEEN STA Y=465 AND STA Y=484 UPPER LOWER SKIN FROM X=56 TO X=60 AT PASSENGER CABIN, CARD 50, ZONE 200. DUE EXCESSIVE DAMAGE, CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 216.Aug 3, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080405760Pan · crackedCRACK FORWARD LOWER RING PAN STA Y=579 RT SIDE AT PASSENGER CABIN STRUCTURE. SM, CARD 3, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH: 0.159" AND NO CRACKS WERE FOUND AFTER REMOVED DAMAGE IAW HFEC INSPECTION.Aug 3, 2016 · N959AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016080405759Pan · crackedCRACKED AFT LOWER RING PAN STA Y=851 LT SIDE AT PASSENGER CABIN STRUCTURE, CARD 4, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH 0.132" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.Aug 3, 2016 · N959AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016080405758Pan · crackedCRACKED AFT UPPER RING PAN STA Y=832, LT SIDE AT PASSENGER CABIN STRUCTURE, CARD 5, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH 0.109" AND NO CRACKS WERE FOUND AFTER REMOVED DAMAGE IAW HFEC INSPECTION.Aug 3, 2016 · N959AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016080405757Pan · crackedCRACKED AFT LOWER RING PAN STA Y=636 LT SIDE AT PASSENGER CABIN STRUCTURE, CARD 6, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH 0.140" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.Aug 3, 2016 · N959AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016080405756Pan · crackedCRACKED AFT LOWER RING PAN, STA Y=617 LT SIDE AT PASSENGER CABIN STRUCTURE. SM, CARD 7, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH: 0.125" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.Aug 3, 2016 · N959AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016080405755Pan · crackedCRACKED AFT LOWER RING PAN STA Y=560 LT SIDE AT PASSENGER CABIN STRUCTURE. SM, CARD 8 ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH=0.158" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.Aug 3, 2016 · N959AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016080305722Fitting · crackedCRACK ON STRAP BETWEEN LONGERON 13/14 RT STA 1022, REAR FACE OF BULKHEAD, CARD 23, ZONE 220. SHEAR CLIP WAS REPLACED IAW SRM 53-20-07, 51-40-02, AND 51-41-05.Aug 2, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080305721Skin · crackedCRACKED EXTERNAL FUSELAGE SKIN BETWEEN LONG 13RT AND 14RT STA Y=1087, CARD 2, ZONE 200. EXTERNAL FUSELAGE SKIN BETWEEN LONG 13 RT AND 14 RT STA Y=1087 WAS REPAIRED IAW ER/A 547894-14, REV ORIGINAL SECTION I. ACCOMPLISH ER/A 547894-14, REV ORIGINAL SECTION IIAug 2, 2016 · N959AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016080305720Skin · crackedCRACKED EXTERNAL FUSELAGE SKIN BETWEEN LONGERON 13RT AND 14RT STA Y=1078 TO Y=1074, CARD 1 ZONE 200. EXTERNAL FUSELAGE SKIN BETWEEN LONG 13 RT AND 14 RT STA Y=1078 TO Y=1074 WAS REPAIRED IAW ER/A 547894-14, REV ORIGINAL SECTION I. ACCOMPLISH ER/A 547894-14 RAug 2, 2016 · N959AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016080105680Access Panel · corrodedCORROSION ON COUNTERSINKS AT FUEL TANK ACCESS 520 MB. CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-23-01-01 AND MUST BE INSTALLED WITH CARD 2040-0010, ZONE 52Jul 31, 2016 · N959AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016080105679Access Panel · corrodedCORROSION ON COUNTERSINKS AT FUEL TANK ACCESS NR 620JB, SM. CORROSION WAS REMOVED, REWORKED AREA WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-23-01-01 AND MUST BE INSTALLED WITH CARD 2040-0012, ZOJul 31, 2016 · N959AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016080105678Access Panel · corrodedCORROSION ON COUNTERSINKS AT FUEL TANK ACCESS 620 CB, SM. CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 57-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-23-01-01 AND MUST BE INSTALLED WITH CARD 2040-0012, ZONJul 31, 2016 · N959AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016080105677Access Panel · corrodedCORROSION ON COUNTERSINKS AT FUEL TANK ACCESS 620DT, SM. CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-22-01 AND MUST BE INSTALLED WITH CARD 2040-0012, ZONE 62Jul 31, 2016 · N959AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016080105676Access Panel · corrodedCORROSION ON COUNTESINKS AT FUEL TANK ACCESS NR 620 GB, SM, CARD 66, ZONE 000, CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED, IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-23-01-01 AND MUST BE INSTALLED WITHJul 31, 2016 · N959AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016080105675Access Panel · corrodedINITIAL CORROSION ON COUNTERSINK AT FUEL TANK ACCESS NR 520, SM, CARD 69, ZONE 000. CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-22-01-01 AND MUST BE INSTALLEDJul 31, 2016 · N959AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016080105673Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT BETWEEN STA 1053-STA 1056 X=-55, W2, SM. CARD 87, ZONE 200. DUE TO EXCESSIVE CORROSION FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02 AND 51-41-05, ORIGINAL THICKNESS 0.080", REMAINING THICKNESS 0.053", THEREFORE IS OUT LIMITS IAW SJul 31, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016073105672Web · corrodedCORROSION UNDER FLOOR SUPPORT BETWEEN STA 190/205 AREA NEXT TO CUSP ANGLE. IN REF CARD 65, ZONE 200, CARD 95, ZONE 200. DUE TO EXCESSIVE CORROSION WEB WAS REPAIRED IAW SRM 51-70-10, FIG 201.Jul 30, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016073105669Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL RT AFT LAVATORY. SM, CARD 30, ZONE 000. FLOOR PANEL RT AFT LAVATORY WAS REPAIRED IAW SRM 51-70-09, REPAIR 3, PARA 6.Jul 30, 2016 · N959AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016073105668Floor Panel · damagedDAMAGE FLOOR PANEL AT LT AFT LAVATORY, N/P 9981474-71, SH-CP-SM, CARD 51, ZONE 000. FLOOR PANEL AT LT AFT LAVATORY WAS REPAIRED IAW SRM 51-70-09 REPAIR 3, PARAGRAPH 6.Jul 30, 2016 · N959AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016073005667Splice · corrodedCORROSION ON RT CUSP LOWER ANGLE SPLICE X=60 BETWEEN STA Y=579 AND Y=598 AT PASSENGER CABIN, SM, CPAX CARD 55, ZONE 200. LOWER ANGLE SPLICE WAS REPLACED IAW SRM 53-20-51, FIG 1 AND 51-41-05.Jul 29, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015113007277Battery Pack · inoperativeDURING SERVICE CHECK. FOUND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AND OPERATION CHECKED NORMALLY.Nov 29, 2015 · N959AT · Boeing 717200 · Emergency LightingSDR DALA2015033102516Frame · crackedDURING SPECIAL VISIT FOR FRAME INSPECTION, FOUND RT FRAME STA Y=674.00 RT CRACKED IN UPPER RADIUS. R & R RT OVERWING FRAME AT STA 674 IAW AMDS 5310-01436-03B.Mar 30, 2015 · N959AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015032902483Frame · crackedDURING FRAME INSPECTION, A CRACK FOUND IN THE RT FRAME. REPAIRED IAW ER/A 530437-14MA.Mar 28, 2015 · N959AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2014122206656Power Supply · inoperativeDURING SERVICE CHECK, FOUND OVER WING AFT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY AT STA 726. FOR OVER WING AFT EMERGENCY LIGHT.Dec 22, 2014 · N959AT · Boeing 717200 · Emergency LightingSDR SWAA2014072830364Lens · crackedFORWARD CTR AISLE OVERHEAD EMER LIGHT CRACKED. R & R LENS IAW AMM.Jul 24, 2014 · N959AT · Boeing 717200 · Emergency LightingSDR SWAA2014072530297Light · inoperativeAFT CABIN EMER LIGHT INOPERATIVE. R & R LIGHT IAW MM.Jul 24, 2014 · N959AT · Boeing 717200 · Emergency LightingSDR SWAA2014072530296Light · inoperativeMID CABIN EMER LIGHT INOPERATIVE. R & R LIGHT IAW MM.Jul 24, 2014 · N959AT · Boeing 717200 · Emergency LightingSDR SWAA2014072530294Light · inoperativeFORWARD CABIN EMER LIGHT INOPERATIVE. R & R LIGHT IAW MM.Jul 24, 2014 · N959AT · Boeing 717200 · Emergency Lighting
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