N915AT

Service difficulty reports · 197

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 = 'N915AT' 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 DALA2016061004499Frame · crackedCRACKED FRAME BS 696, LONG 26 RT AND FRAME BS 715, LONGERON 27R AT UNDERWING BARREL KEELBEAM INTERNAL STRUCTURE. SM, CARD 16, ZONE 140. FRAMES WERE REPAIRED IAW SRM 51-70-11, REPAIR 1, SRM 51-41-02, SRM 51-10-04 PAR 15 AND 21. RII COMPLETED.Jun 9, 2016 · N915AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016060904483Frame · crackedCRACKED FRAME BS 696, LONG 26LT AND FRAME 715, LONG 27 LT AT UNDERWING BARREL KEEL BEAM INTERNAL STRUCTURE. FRAMES WERE REPAIRED IAW SRM 51-70-11 REPAIR 1, FIG 201, SRM 51-41-02, SRM 51-10-04 PAR 15-21, 37, 51-41-05.Jun 8, 2016 · N915AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016060904482Floor Panel · damagedDAMAGE AND MISSING FERRULES ON FLOOR PANELS NR 222AVF AND 223CF AT CABIN PAX. FLOOR PANEL NR 222AVF WAS REPLACED FERRUL IAW ER/A 546544-14 REV. ORIGINAL. FLOOR PANEL NR 223CF WAS FABRICATED IAW ER/A 546544-14 REV ORIGINAL.Jun 8, 2016 · N915AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016060904479Skin · corrodedCORROSION ON CENTER WING UPPER SKIN, JUST FWD OF SLANT PANEL AND BS X= 40.5, CARD 3, ZONE 140). FUEL LINE WAS REMOVED AND INSTALLED IAW AMM 20-10-03 917-81 FASTENERS WERE REMOVED AND INSTALLED IAW SRM 51-41-05 CORROSION WAS REMOVED IAW SRM 57-10-01 AND (UT) WAJun 8, 2016 · N915AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016060904478Door Frame · crackedCRACKED NLG DOOR JAMB BS Y=46 X=18 LT Z=-33 AT NLG W/W. NLG DOOR JAMB WAS REPAIRED IAW SRM 53-10-14, FIG 201.Jun 8, 2016 · N915AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016060904477Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620LB AT RT WING. CORROSION ON COUNTERSINK AT ACCESS PLATE 620LB WAS REMOVED AND MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.536, 0.550, AND 0.545 AND WAS REPLACED WITH CONDITION IJun 8, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060904476Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520LB AT LT WING. CORROSION AT COUNTERSINK OF FUEL ACCESS DOOR 520LB WAS REMOVED, MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES .579, .538, .543 IAW SRM 57-10-01, ACCESS PLATE WAS REPLAJun 8, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060904475Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520GB AT LT WING. CORROSION AT COUNTERSINK OF FUEL ACCESS DOOR 520GB WAS REMOVED, MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES .560, .553 AND .558 IAW 57-10-01 ACCESS PLATE WAS REPLACJun 8, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060904474Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520DB AT LT WING. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 520DB WAS REMOVED AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.552, 0.538, 0.563 IAW SRM 57-10-01 AND ACCESS PLJun 8, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060904473Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520CB AT LT WING. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 520CB WAS REMOVED AND MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.538 AND 0.540 ACCESS PLATE WAS REPLACED IAW SRM 57-1Jun 8, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060804419Web · corrodedCORROSION ON DIAPHRAGM FROM BS 195 TO 200 AND BETWEEN X -52 TO X -58. DIAPHRAGM WAS REPAIRED IAW SRM 51-70-10, FIG 201.Jun 7, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060804418Floor Panel · brokenBROKEN CORE ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 546544-14, REV ORIGINAL.Jun 7, 2016 · N915AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016060804417Stiffener · crackedCRACK ON STIFFENERS OF PASSENGER CABIN FLOOR PANELS 222AFF, 222ALF, 222AJF. SM, CARD 57 ZONE 000. STIFFENERS OF PASSENGER CABIN FLOOR PANELS 222AFF, 222ALF, AND 222AJF WERE REPAIRED IAW SRM 53-20-50, REPAIR 5, FIG 201 AND 202. CRACK L=0.235", CRACK L=0.324",Jun 7, 2016 · N915AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016060804416Cusp Web · crackedCRACKS RT CUSP WEB BETWEEN BS 218 TO 237 X 44. CUSP WEB WAS REPLACED IAW SRM 51-41-01, 51-41-02, 51-41-05, AND DWG 9930538, REV CC.Jun 7, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060704396Floor Support · crackedCRACK ON FLOOR SUPPORT BS 636, X 0. CRACK WAS STOPP DRILLED IAW SRM 53-00-00, FIG 1. REPAIR PART WAS FABRICATED IAW SRM 53-00-00 FIG 201. REPAIR INSTALLED IAW SRM 51-40-02.Jun 6, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060704394Fitting · crackedCRACKED FITTING AT BS 737, X 43 AND Z -11. FITTING WAS REPLACED IAW SRM 51-41-05, 51-41-02, 51-40-08, AND 51-10-04 PAR 15 AND 21.Jun 6, 2016 · N915AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2016060704392Skin · damagedDAMAGE ON LT SIDE OF RUDDER SKIN PANEL, LOWER SECTION. SM, CARD 5, ZONE 370. DAMAGED AREA WAS REPAIRED IAW SRM 51-70-13 R1.Jun 6, 2016 · N915AT · Boeing 717200 · Rudder, Plate/SkinSDR DALA2016060604389Cusp Web · crackedCRACKED LT CUSP WEB BS 813 AND 825. CUSP WEB WAS REPLACED IAW SRM 53-00-55, FIG 226.Jun 5, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060604388Cusp Web · crackedCRACKED LT CUSP WEB BS 674-676, X 44 TO 46. CUSP WEB WAS REPLACED IAW SRM 53-00-55, FIG 223,Jun 5, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060604387Stiffener · crackedCRACKED STIFFENER ON AFT PRESSURE BULKHEAD BETWEEN LONGERONS 7RT AND 8 RT AT PASSENGER CABIN. STIFFENER WAS REPLACED IAW SRM 51-41-05 DWG 9915558, REV BA CRACK L= 0.750".Jun 5, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060604385Floorbeam · crackedCRACKED FLOORBEAM BS 737 AND X -50. FLOORBEAM WAS REPLACED IAW 51-41-02 AND 51-41-05.Jun 5, 2016 · N915AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2016060504384Frame · crackedCRACKED FRAME BS 1037 AT INTERSECTION WITH LONG 17RT. RT AFT LAV AREA. FRAME ON STA Y=1037, RT WAS REPAIRED IAW SRM 53-20-07, FIG 201.Jun 4, 2016 · N915AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016060404380Longeron · corrodedCORROSION ON LONGERON TERMINAL 24 RT, BETWEEN BS 927 TO 946 AT AFT CARGO COMPARTMENT. LONGERON END WAS REPLACED IAW DWG 5911494, REV CZ AND SRM 51-41-05, PAR 8, UT, WAS ACCOMPLISHED ORIGINAL THICKNESS 0.050" REMAINING THICKNESS 0.025 THEREFORE IT IS OUT OF LJun 3, 2016 · N915AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016060404379Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND ELONGATED HOLE OF COUNTERSINK OF FUEL ACCESS DOOR 141AR. CARD 44, ZONE 000. CORROSION SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS PLATE 141AR WERE REMOVED AND MEASURED, AND FOUND OUT OF LIMITS WITH 5 HOLES 0.700", 0.662", 0Jun 3, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060204313Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620DT AT RT WING. CORROSION AT COUNTERSINK OF FUEL ACCESS PLATE 620DT WAS REMOVED AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES .680 IN, 0.680 IN AND 0.665 IN, IAW SRM 57-10-01Jun 1, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060204312Access Panel · corrodedCORROSION AND COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620AT AT RT WING. CORROSION AT COUNTERSINK OF FUEL ACCESS PLATE 620 AT WAS REMOVED AND COUNTERSINK WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.661 IN, 0.665 IN, 0.666 IN, IAW AJun 1, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060204311Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520DT AT LT WING. CORROSION AT FUEL ACCESS PLATE 520DT ON COUNTERSINK WAS REMOVED, MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES DIAMETER MAX 0.619IN, 0.672IN AND 0.694 IN IAW SRM 57-1Jun 1, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060104241Cusp Web · corrodedCORROSION ON RT CUSP WEB BS 503 TO 522. CUSP WEB WAS REMOVED, AND FOUND OUT OF LIMITS. CUSP WEB WAS REPAIRED IAW SRM 51-41-02, SRM 51-10-04 PAR 15, 21, 26, AND 37, SRM 53-00-55.May 31, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060104240Pan · crackedCRACKED RT UPPER/FWD CORNER ON RING PAN BETWEEN BS 636 TO 655. RING PAN WAS REPAIRED IAW SRM 50-20-02. REPAIR 1, FIG 202, TYPE B.May 31, 2016 · N915AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016060104239Pan · crackedCRACKED RT UPPER/FWD CORNER ON RING PAN BETWEEN BS 696 TO 715. RING PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 203, TYPE C.May 31, 2016 · N915AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016060104238Pan · crackedCRACKED RT UPPER, AFT CORNER ON RING PAN BETWEEN BS 832 TO 851. RING PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202, TYPE B.May 31, 2016 · N915AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016060104237Pan · crackedCRACK ON FWD/LOWER CORNER AT LT RING PAN BETWEEN BS 832 TO 851 IN CPAX, SM, ZONE: 201 CARD: 3. DAMAGE ARE WAS TRIMED OUT IAW SRM 56-20-02, FIG 202. REPAIR PARTS WERE FABRICATED IAW SRM 50-20-02, FIG 202, REPAIR PARTS WERE INSTALLED IAW SRM 51-40-02 AND 51-40-May 31, 2016 · N915AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016053104212Pan · crackedCRACK ON AFT/UPPER CORNER BETWEEN BS 851 TO 870 AT LT RING PAN. PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.May 30, 2016 · N915AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016053104211Cusp Web · crackedCRACKED LT CUSP WEB BETWEEN BS 587 TO 589, X=45. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 221.May 30, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016053104210Pan · crackedCRACK ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 636 TO BS 655 IN CPAX, SM, ZONE: 201 CARD: 10. ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 636 TO 655 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.May 30, 2016 · N915AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016053104209Pan · crackedCRACK ON FWD, UPPER CORNER AT LT RING PAN BETWEEN BS 756 TO 775. ON FWD/UPPER CORNER AT LT RING PAN BETWEEN BS 756 TO 775 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.May 30, 2016 · N915AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016053104207Pan · crackedCRACK ON AFT, UPPER CORNER AT LT RING PAN BETWEEN BS 813 TO 832. ON AFT, UPPER CORNER AT LT RING PAN BETWEEN BS 813 TO 832 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202, CRACK LENGTH, L= 0.235".May 30, 2016 · N915AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016053104206Pan · crackedCRACK ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 908 TO 927. ON FWD / LOWER CORNER AT LT RING PAN BETWEEN BS 908 TO 927 WAS REPAIRED IAW SRM 50-20-02, REPAIR 1, FIG 202, CRACK LENGTH 0.198".May 30, 2016 · N915AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016053104205Pan · crackedCRACK ON FWD/LOWER CORNER AT LT RING PAN BETWEEN BS 617 TO 636. THE PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR, FIG 202.May 30, 2016 · N915AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016052904198Cusp Web · crackedCRACKED CUSP WEB BETWEEN X=54 AND X=60 BETWEEN BS 851 AND 870. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 216.May 28, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015031602167Power Supply · inoperativeDURING SERVICE CHECK, FOUND CATWALK AND AFT CABIN DOOR LIGHTED SIGN FOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY IAW AMM 33-51.Mar 14, 2015 · N915AT · Boeing 717200 · Emergency LightingSDR DALA2015021301237Frame · crackedDURING SPECIAL VISIT, FOUND MAIN FRAME BS 674 RT CRACKED, HFEC VERIFIED. REPAIRED IAW ER/A 530437-14MA AND AMDS WC 5310-01436-03B.Feb 13, 2015 · N915AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015021301236Cusp Web · crackedDURING SPECIAL VISIT, FOUND RT CUSP WEB CRACKED AT BS 655 OVERWING FRAME CUTOUT. INSTALLED NEW WEB IAW ER/A 532911-14.Feb 12, 2015 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015021401235Cusp Web · crackedRIGHT CUSP WEB CRACKED AT BS 655 OVERWING FRAME CUTOUT. REPAIR DOUBLER INSTALLED IAW SRM FIG 201, 53-00-00.Feb 10, 2015 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR SWAA2014072330218Light · inoperativeR1 DOOR EMER LIGHT LAMP INOPERATIVE. R & R LAMP IAW AMM.Jul 18, 2014 · N915AT · Boeing 717200 · Emergency LightingSDR SWAA2014072130173Light · inoperativeTAIL CONE CATWALK FWD EMER LIGHT BULB INOPERATIVE. RELAMPED BULB IAW AMM.Jul 18, 2014 · N915AT · Boeing 717200 · Emergency LightingSDR SWAA2014072130172Light · inoperativeRIGHT AFT OVERWING EXIT EMER LIGHT BULB INOPERATIVE. RELAMPED IAW AMM.Jul 18, 2014 · N915AT · Boeing 717200 · Emergency LightingSDR SWAA2014071429911Skin · crackedRIGHT FUSELAGE AFT EDGE OF CARGO DOOR CUT OUT SKIN CRACKED AT BS 994. REPAIRED SKIN IAW SRM.Jul 11, 2014 · N915AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR SWAA2014071429920Battery · failedFORWARD OVERWING DOOR EMER EXIT LIGHTS FAILED OPERATIONS CHECK. REMOVED BATTERY IAW AMM.Jul 9, 2014 · N915AT · Boeing 717200 · Emergency LightingSDR SWAA2014071429919Pan · crackedAFT LOWER FUSELAGE, CONDITIONED AIR GND CONNECTION CUT OUT PAN CRACKED AT UPPER AFT RADIUS. R & R PAN IAW AMM & DWG.Jul 1, 2014 · N915AT · Boeing 717200 · Fuselage Miscellaneous Structure
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