N961AT

Service difficulty reports · 199

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 = 'N961AT' 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 DALA2016060904472Angle · crackedCRACKED ANGLES BS 1168 BETWEEN LONGERON 3RTO 2L. ANGLES REPLACED IAW DWG 9911860, REV L AND SRM 51-41-02 AND SRM 51-41-05.Jun 8, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060904471Structure · corrodedCORROSION ON INTERNAL STRUCTURE BETWEEN BS 900 TO 910 BETWEEN LONGERON 25 TO 26L. STRUCTURE REPAIRED IAW SRM 53-02-01, REPAIR 1, 51-40-08, AND 51-10-04 PAR 15-21-37 AND 51-41-02.Jun 8, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060904470Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTER SKIN OF FUEL ACCESS PLATE NR 620FT. CORROSION SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE NR 620 FT WERE REMOVED IAW SRM 57-10-01. COUNTERSINK AND SETTLEMENT AREA WERE MEASURED AND COUNTERSINK MAX DIAMETER IS 0Jun 8, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060804420Floor Panel · damagedDAMAGED PASSENGER CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 546511-14 REV ORG.Jun 7, 2016 · N961AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016060804415Frame · crackedCRACK ON FRAME ANGLE BS 1116, LONGERON 15L AT AFT ACCESSORY COMPARTMENT. THE ANGLE WAS REPLACED IAW DWG 5913595 REV.AP AND SRM 51-41-05, 51-41-02.Jun 7, 2016 · N961AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016060704395Cusp Web · crackedCRACKED RT CUSP WEB AT X -44 TO X -54 BETWEEN BS 218 AND 237 AT CABIN FLOOR STRUCTURE. REPAIR ON CUSP WEB IAW SRM 53-00-55, FIG 219, REP 4.Jun 6, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060704393Channel · crackedCRACKS ON CHANNEL OF FLOOR PANEL NR 222 X. CHANNEL WAS REPAIRED IAW SRM 53-20-50, FIG 201. HFEC INSPECTION WAS PERFORMED, NO CRACKS WERE FOUND AFTER STOP DRILL IAW NDT SPM 06-10-001.Jun 6, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060604390Door · wornMAINTENANCE DISCOVERED THAT THE AFT CABIN BULKHEAD EMERGENCY ESCAPE DOOR WAS WORN AND DAMAGED ON THE LOWER INBD SIDE. THE DAMAGE AREA WAS REPAIRED IAW SRM 52-10-02. REPAIR 15 AND 16.Jun 5, 2016 · N961AT · Boeing 717200 · DoorsSDR DALA2016060504383Cusp Web · damagedCORROSION ON RT CUPS WEB, UPPER AND LOWER SURFACE, X 54 TO X 60, BS 436 TO 465, 503 TO 522, 522 TO 579. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 203, 51-41-02, AND 51-41-05 FROM BS Y=436 TO Y=465 AREA WAS REINSPECTED AND NO CORROSION WAS FOUND. RII CJun 4, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060504382Floor Panel · damagedDAMAGED PASSENGER CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 546511-14, REV. ORIGINAL.Jun 4, 2016 · N961AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016060404381Skin · crackedCRACKED EXTERNAL SKIN AROUND OF HOLD OPEN LOCK HOUSING AT MAIN L1 DOOR. EXTERNAL SKIN WAS REPAIRED IAW SRM 52-10-01, REP 4, FIG 201. LENGTH CRACK = 0.270", RII COMPLETED.Jun 3, 2016 · N961AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016060404378Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB BS 952. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 205, RII COMPLETED BY INSPECTION.Jun 3, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060304371Floor Panel · damagedDAMAGED PASSENGER CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 546511-14.Jun 2, 2016 · N961AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016060304321Skin · wornWEAR ON EXTERNAL SKIN APPROXIMATELY STATION 170, LOWER EDGE AT MAIN ENTRANCE DOOR. EXTERNAL SKIN, LOWER EDGE, WAS REPAIRED IAW SRM 52-10-01, FIG 201, REP 2 HFEC INSPECTION WAS PERFORMED AND NO CRACKS WERE FOUND. PERFORM INSPECT DECAL CONDITION EVERY "C" CHECJun 2, 2016 · N961AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016060304320Attach Angle · crackedCRACK ON ANGLE TO ATTACH LT AFT ENGINE PYLON SUPPORT BULKHEAD, BS Y=1022 BETWEEN LONGERONS 6 TO 7L ALSO LONGERONS 16 TO 17L. ANGLES WERE REPLACED IAW SRM 51-41-02, 51-41-05, AND 51-10-14, PAR. 21 AND 15.Jun 2, 2016 · N961AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2016060304319Pan · crackedCRACK ON INNER PAN APPROXIMATELY BS 200, AFT EDGE, BETWEEN UPPER EDGE AND BEAM 1 AT MAIN ENTRANCE DOOR. INNER PAN WAS REPAIRED IAW SRM 52-10-02, REP 2, FIG 201. LENGTH OF CRACKS: 1.800", 2.400".Jun 2, 2016 · N961AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016060304318Beam · crackedCRACK ON BEAM NR 1, FWD EDGE AT MAIN ENTRANCE DOOR. BEAM NR 1 WAS REPAIRED IAW SRM 52-10-02, FIG 201, REPAIR 7. LENGTH OF CRACK = 0.800".Jun 2, 2016 · N961AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016060304316Cusp Web · corrodedCRACK ON LT CUSP WEB BETWEEN X 50 TO X 54, BS 674 - 680. CUSP WEB REPAIRED IAW SRM 53-00-55, FIG 226.Jun 2, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060204315Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB BS 940. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 215.Jun 1, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060204314Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB BETWEEN X-54/60, BS 794 TO 813, CARD 111, ZONE 200. RT CUSP WEB WAS REPAIRED BETWEEN BS 794-813 IAW SRM 53-00-55, FIG 216.Jun 1, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060104236Seat Track · crackedCRACKED BEAM BELOW SEAT TRACK X=-54 AT BS 737, PAX CAB, SM, ZONE 140, CARD 6, WB, CARD 6, ZONE 140. BEAM WAS REPLACED IAW SRM 51-41-02, 51-41-05. LONG CRACK: 2.000".May 31, 2016 · N961AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016060104235Cusp Web · corrodedEXCESSIVE CORROSION ON LT CUSP WEB BETWEEN X=54/60 AND BS 995, CARD 110, ZONE 200. LT CUSP WEB BETWEEN X=54/60, BS Y=995 WAS REPAIRED IAW SRM 53-00-55, FIG 215.May 31, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016053104213Frame · crackedCRACK ON FRAME BS 674 - 689, AND BS 715, LONGERON 25RT AT UNDERWING BARREL KEEL BEAMS. FRAME REPAIRED IAW SRM 53-00-00, FIG 201.May 30, 2016 · N961AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016053004203Skin · wornWORN EXTERNAL SKIN AT EDGE BETWEEN BEAMS 1 AND 3 AT AFT CARGO COMPARTMENT DOOR. EXTERNAL SKIN WAS REPAIRED IAW SRM 52-00-01, REPAIR 8, FIG 204.May 29, 2016 · N961AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016053004202Pan · crackedCRACK ON FWD PAN BS 370 BETWEEN BEAMS 2 AND 3 AT FWD CARGO COMPARTMENT DOOR. PAN WAS REPAIRED IAW SRM 52-30-02, FIG.201, 51-41-02, 51-41-04, 51-41-01, 51-10-04 PAR 15.May 29, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016052904201Intercostal · crackedCRACKED INTERCOSTAL X=0, BS 636 TO 617 AT CEILING AREA OF FWD CARGO COMPARTMENT. INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00, FIG 201.May 28, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016052904200Frame · crackedCRACKED FRAME BS 689, LONGERON 26L AT KEEL BEAM AREA. THE FRAME WAS REPARED IAW SRM 53-00-00, REPAIR 1, FIG 201.May 28, 2016 · N961AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016052904199Frame · crackedCRACK ON FRAME BS 674, LONGERON 25L AT UNDER WING BARREL KEEL BEAMS. THE FRAME WAS REPAIRED IAW SRM 53-00-00, REPAIR 1, FIG 201.May 28, 2016 · N961AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016052904197Beam · crackedCRACK ON NR 1 BEAM, FWD EDGE AT MAIN ENTRANCE L1 DOOR. NR 1 BEAM WAS REPAIRED IAW SRM 51-41-02, 51-41-01, SRM 52-10-02, FIG 202, SHEET 8, 51-20-09, 51-41-03, AND 51-10-04, PAR 15.May 28, 2016 · N961AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016052904196Doubler · corrodedCORROSION ON DOUBLER ATTACH INNER FUSELAGE SKIN AND CUSP WEB BETWEEN X=54 TO X=60 BS 579 TO 598, RT SIDE. CORROSION WAS REMOVED, AREA WAS MEASURED. ORIGINAL THICKNESS: 0.080" REMAINING THICKNESS: 0.041" THEREFORE ITS OUT OF LIMITS AND DOUBLER WAS REPLACED IMay 28, 2016 · N961AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016052804194Skin · gougedGOUGES ON EXTERNAL SKIN BETWEEN BS 408-420 BETWEEN BEAM 2 AND LOWER EDGE AT FWD CARGO COMPARTMENT DOOR. SKIN WAS REPAIRED IAW SRM 52-00-01, FIG 202.May 27, 2016 · N961AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016052704193Cusp Web · corrodedCORROSION ON CUSP WEB BS 245 TO 249, RT SIDE IN REF CARD 59, ZONE 200. CARD 95, ZONE 200. DUE TO EXCESSIVE CORROSION ON CUSP WEB BS 244 TO BS 249 RT SIDE IN REF CARD 59, ZONE 200 AREA WAS REPAIRED IAW SRM 53-00-55, FIG 215, REPAIR 4, SRM 53-20-51, FIG 1 ITEM May 26, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016052704192Cusp Web · corrodedAWR EXCESSIVE CORROSION ON RT CUSP WEB BETWEEN BS 408 AND BS 427 IN REF CARD 59, ZONE 200. CARD 96, ZONE 200. DUE TO EXCESSIVE CORROSION ON CUSP WEB BS 408 AND STA 427 IN REF CARD 59, ZONE 200 AREA WAS REPAIRED IAW SRM 53-00-55, FIG 203, REPAIR 4, DWG 9930538May 26, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016052604182Doubler · damagedPREVIOUS REPAIR DOUBLER WORN AND BENT, INNER PAN AND OUTER PAN BS 954 BETWEEN BEAM 1 AND 2 AT AFT CARGO COMPARTMENT DOOR. REPAIR DOUBLER WAS FABRICATE AND REPLACED IAW SRM 52-30-02, REPAIR 4, FIG 201.May 25, 2016 · N961AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016052604180Cusp Web · crackedCRACKED RT CUPS WEB BETWEEN X=54 TO X=60, BS 368 TO 375. CUSP WEB WAS REPAIRED IAW SRM 53-00-05, FIG 214 AND 51-41-05, 51-41-02, 51-10-04 AND 51-40-08 TRIMOUT WAS ACCOMPLISHED.May 25, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016052604179Floor Support · corrodedCORROSION ON FLOOR SUPPORT X=44 BETWEEN BS 1022 TO 1060 AT LT PAX CABIN. FLOOR SUPPORT WAS REPLACED IAW DWG: 9981474, REV: L.May 25, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016103107958Seat Track · corrodedCORROSION ON SEAT TRACK X 44 AT BS 609. THE SEAT TRACK WAS REPAIRED IAW SRM 51-10-04 AND 53-20-52 FIG.201.May 23, 2016 · N961AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015020501011Frame · crackedOVERWING FRAME CRACKED AT STA 715 RT, CONDITION 3. FRAME REPLACED IAW AMDS WC 5310-01436-03B.Feb 4, 2015 · N961AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2015020300847Cusp Web · crackedRIGHT CUSP WEB CRACKED AT STA 674 BETWEEN INBD AND OTBD SEAT TRACKS. REPLACED CUSP WEB, MEMBRANE, IAW DWG 9910151 AND ER/A 532674-14.Feb 3, 2015 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015011000196Cusp Web · crackedFORWARD CARGO BAY BS 655 RBL 54 CUSP WEB CRACKED. INSTALLED A REPAIR IAW SRM 53-00-55 REPAIR 4.Jan 9, 2015 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2015011000195Cusp Web · crackedFORWARD CARGO BAY BS 655, LBL 54 CUSP WEB CRACKED. INSTALLED A REPAIR IAW SRM 53-00-55, REPAIR 4.Jan 9, 2015 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2014090304890Diode · failedR1 OVERWING DOOR EMERGENCY EXIT MARKER FOUND INOPERATIVE DURING SERVICE CHECK. FOUND L2-788, LIGHT ASSY DISCONNECTED. CONNECTED THE LIGHT AND FOUND DIODE ASSY, R7-188, BAD. REPLACED THE DIODE ALONG WITH THE BATTERY AND POWER SUPPLY, CHECKED NORMAL.Sep 1, 2014 · N961AT · Boeing 717200 · Emergency LightingSDR DALA14036519520Pin · dislodgedPILOT REPORTED THE AMBER CAUTION MESSAGE ILLUMINATED INDICATING THE TAILCONE WAS NOT SECURE. MAINTENANCE FOUND THE INTERNAL TAILCONE RELEASE HANDLE PIN DISLODGED FROM THE RETAINER CLIPS. THE LOCK CABLE WAS REINSERTED AND THE BALL END NOW MAKES PROPER CONTACTJun 18, 2014 · N961AT · Boeing 717200 · Aerodynamic FairingsSDR SWAA2014052028165Light · inoperativeTAIL COMPARTMENT AFT EMERGENCY EXIT LIGHT BULB INOPERATIVE. R & R LAMP IAW AMM.May 16, 2014 · N961AT · Boeing 717200 · Emergency LightingSDR SWAA2014051928149Sign · crackedR1 DOOR EMERGENCY EXIT SIGN CRACKED. R & R SIGN IAW AMM.May 16, 2014 · N961AT · Boeing 717200 · Emergency LightingSDR SWAA2014051928148Light · inoperativeR1 DOOR EMERGENCY EXIT SIGN LOWER BULB INOPERATIVE. R & R BULB IAW AMM.May 16, 2014 · N961AT · Boeing 717200 · Emergency LightingSDR SWAA2014051427960Fitting · missingTAIL CONE EVACUATION SLIDE COVER MISSING AFT RETAINER CLIP. INSTALLED CLIP IAW AMM.May 9, 2014 · N961AT · Boeing 717200 · Emergency EquipmentSDR DALA1608489520Skin · gougedSKIN GOUGED AT BS 229-237 BETWEEN LONGERON 6L AND 7L. REPAIRED, SKIN IAW SRM 53-03-01-2R-1, FIGURE 211, SHEET 3.Apr 13, 2014 · N961AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR SWAA2014042227294Former · crackedFORMER CRACKED AT BS 237, LONGERON 18L. R & R FORMER IAW DWG.Apr 12, 2014 · N961AT · Boeing 717200 · Fuselage Main, FrameSDR DALA1608479520Skin · dentedDENT ON LT FUSELAGE AT BS 237 AND 5" ABOVE LONGERON 18. REPAIRED SKIN IAW SRM 53-00-01-2R-6.S062052.Apr 10, 2014 · N961AT · Boeing 717200 · Fuselage Main, Plate/Skin
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