N957AT

Service difficulty reports · 187

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 = 'N957AT' 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 DALA2023062905213Unknown · unknownCORROSION ON CUSP WEB BTW STA Y=218/220 AND BTW STA X=-44/-54 AT PAX CABIN (W1). SUMMARY OF NRC 00377: CORROSION LEVEL 2. CUSP WEB BTW STA Y=218/220 WAS REPLACED B717-200 SRM 51-41-02 PAR 4 AND 51 -41-05-0G. (LP #2839683)Jun 28, 2023 · N957AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023062905212Unknown · unknownCORROSION ON FLOOR SUPPORT STA Y=370 BTW STRG 29R AND STRG 29L AT FWD CARGO COMPARMENT. SUMMARY OF NRC 00190: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=370 BTW STRG 29R AND STRG 29L AT FWD CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2839189)Jun 28, 2023 · N957AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023062805185Unknown · unknownCRACK FOUND ON CUSP WEB AFTER REMOVAL ANGLE ON FLOOR STRUCTURE RH SIDE BTW STA 636 AND STA 655 PAX CABIN. SUMMARY OF NRC 00607: CUSP WEB RH SIDE BTW STA 636 AND STA 655 PAX CABIN WAS REPAIRED PER B-717-200 SRM 53-00-55-2R4. (LP #2836798)Jun 27, 2023 · N957AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023062805184Unknown · unknownCRACK ON FRAME STA Y=1037 OVER SRT 17 RH AT CPAX. SUMMARY OF NRC 00424: FRAME STA Y=1037 OVER SRT 17 RH AT CPAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 4. (LP #2836625)Jun 27, 2023 · N957AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023062805183Unknown · unknownCRACK WAS FOUND ON FWD PAN OF AFT CARGO DOOR. (PTAS). SUMMARY OF NRC 00599: FWD PAN AT AFT CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 8 REPAIR 8. (LP #2836314)Jun 26, 2023 · N957AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2023062805177Unknown · unknownCORROSION ON CUSP WEB Y=313, Y=389, Y=636, AND X=-50 (APROX) AT PASSENGER CABIN. SUMMARY OF NRC 00515; CUSP WEB Y=313, Y=389, Y=636, AND X =-50 AT PASSENGER CABIN WERE REPAIRED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2833071)Jun 25, 2023 · N957AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023062305082Unknown · unknownDRILL HOLES, ADITTIONAL FOUND ON CUSP WEB AFTER REMOVAL ANGLE ON FLOOR STRUCTURE LH SIDE BTW STA 294 AND STA 313 PAX CABIN. SUMMARY OF NRC 00608: CUSP WEB LH SIDE BTW STA 294 AND STA 313 WAS REPAIRED PER B-717-200 SRM 53-00-55-2R PAR 4. (LP #2829937)Jun 22, 2023 · N957AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023062305081Unknown · unknownCORROSION ON DIAPHRAGM STA Y=217 AND X=-41 APROX AT PAX CABIN (W1). SUMMARY OF NRC 00428: CORROSION LEVEL 2. (WEB) DIAPHRAGM STA Y=217 AND X=-41 APROX AT PAX CABIN WAS FABRICATED PER DWG 9936535 AND INSTALL IS ACCOMPLISHED UNDER NRC 00413 AND B717-200 SRM 51-4Jun 22, 2023 · N957AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2023062005003Unknown · unknownTOOL MARKS ON CUSP WEB STA Y=255 AND LBL=46 APROX AT PAX CABIN (W1). SUMMARY OF NRC 00430: CUSP WEB STA Y=255 AND LBL=46 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG.219. (LP #2825205)Jun 20, 2023 · N957AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2023061904970Unknown · unknownPUNTURES (2 EA) ON WEB STA Y=211 APROX AND BTW STA X= 44/54 AT PAX CABIN (W1). SUMMARY OF NRC 00383: WEB STA Y=211 AND BTW STA X=44/54 WAS REPAIRED PER B-717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #2821676)Jun 17, 2023 · N957AT · Boeing 717200 · Fuselage Structure (General)SDR DALA2023061604901Unknown · unknownCORROSION ON FLOOR FITTING STA Y=217 AND RBL=11 AT PAX CABIN (W1). SUMMARY OF NRC 00396: CORROSION LEVEL 2. FLOOR FITTING WAS REPLACED PER B-717-200 SRM 51-41-05-0G. (LP #2818599)Jun 15, 2023 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2023061604899Unknown · unknownCRACK ON INSIDE JAMB STA Y=160 ON TOP OF PASSENGER ENTRANCE DOOR L1. SUMMARY OF NRC 00143: CRACKED INSIDE JAMB ON TOP OF PASSENGER ENTRANCE DOOR L1 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-01-0G. (LP #2818186)Jun 15, 2023 · N957AT · Boeing 717200 · Fuselage Structure (General)SDR DALA2023061304792Unknown · unknownCRACK ON DOOR BEAM #1 STA Y=162 AT PASSENGER ENTRANCE DOOR L1. SUMMARY OF NRC 00140: DOOR BEAM #1 STA Y=162 AT PASSENGER ENTRANCE DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 7. (LP #2809935)Jun 10, 2023 · N957AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019072904460Battery Pack · dischargedEMERGENCY LIGHTS #L2-873, L2-845, L2-846, L2-848, AND L2-847 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE B5-260 BATTERY PACK AND CHARGER PER AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. (LP #4621054)Jul 29, 2019 · N957AT · Boeing 717200 · Emergency LightingSDR DALA2019062103704Power Supply · inoperativeTHE AFT BULKHEAD DOOR EXIT MARKER SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY B5-260 PER B717 AMM 33-50. THE AFT BULKHEAD DOOR EXIT SIGN NOW OPERATES NORMALLY. (LP #5359820)Jun 21, 2019 · N957AT · Boeing 717200 · Emergency LightingSDR DALA2018051503324Skin · damagedTHE LT AND RT VERTICAL STABILIZER EDGE STRUCTURE SPLICE BAND, HAD DEFORMED HOLES ON THE THIRD ROW OF FASTENERS. REAMED AND INSTALLED BUSHINGS IAW DRAWING SG95550001, REV B. INSTALLED AN EXTERNAL DOUBLER IAW DRAWING SG95550001, REV B.May 14, 2018 · N957AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA201805143267Longeron · crackedAFT ACCY EMPENNAGE LONGERON 2R, BS 1132 FOUND CRACKED ON THE AFT SIDE. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-05, REPAIR 2.May 8, 2018 · N957AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018050903266Longeron · crackedAFT ACCESSORY EMPENNAGE LONGERON 2L, BS 1132 WAS FOUND CRACKED ON THE AFT SIDE. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-05, REPAIR 2.May 8, 2018 · N957AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018010800148Lens · unsecureEMERGENCY EXIT COVER DIFFUSER LENS MISSING FROM CEILING EXIT LIGHT AT ROW 1. MAINTENANCE LOCATED THE EMERGENCY EXIT COVER AND SECURED IAW AMM 33-51. OK FOR SERVICE.Jan 7, 2018 · N957AT · Boeing 717200 · Emergency LightingSDR DALA2017071305388Cover · unsecureEMERGENCY EXIT LIGHT COVER UNSECURE AT ROW 1. INSTALLED THE LIGHT COVER.Jul 12, 2017 · N957AT · Boeing 717200 · Emergency LightingSDR DALA2016081505970Socket · shortedMAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN FOR BOTH THE LEFT AND RIGHT OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE FOUND THAT THE SOCKET FOR THE LIGHT ASSEMBLY WAS SHORTED AND REPLACED IT. A SATISFACTORY FUNCTIONAL CHECK WAS PERFORMED FOLLOWING REPLACEAug 13, 2016 · N957AT · Boeing 717200 · Emergency LightingSDR DALA2016052604181Cusp Web · corrodedAT BS 446 RT CUSP WEB CORRODED ON BOTTOM SIDE. REMOVED CUSP WEB, RT WEB OUT OF LIMITS MATERIAL IS 100 PERCENT IN SEVERAL LOCATIONS, REMOVED CUSP TEE AT BS 446-484, CUSP TEE IS OUT OF LIMITS 100 PERCENT MATERIAL LOSS AT SEVERAL LOCATIONS, FABRICATED REPAIR PIEMay 25, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016052604184Pin · unsecureL1 DOOR SLIDE LOWER INFLATION CABLE PIN FOUND UNSECURED. INSTALLED PASSENGER ENTRY DOOR SLIDE.May 24, 2016 · N957AT · Boeing 717200 · Escape SlideSDR DALA2016103107957Web · corrodedVERTICAL WEB AFT OF L1 DOOR FRAME IS CORRODED ABOVE FLOOR BS 190. COMPLIED WITH ERA 54677-14 REV ORIGINAL.May 23, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016052404176Cusp Web · crackedCUSP WEB CRACKED AT APPROXIMATELY BS 670 RT. R & R RT CUSP WEB AT BS 670 IAW DWG 9910151, REV CH.May 23, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016052404177Intercostal · corrodedLOWER FUSELAGE, AFT CARGO BILGE, BETWEEN BS 1028-1037-L30, CORROSION. REMOVED INTERCOSTAL REINSTALLED INTERCOSTAL IAW SRM 51-40-2. REMOVED STR, FABRICATED NEW STR 717, SRM 52-20-05. INSTALLED STR IAW 717 SRM 51-40-2.May 20, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016052104174Skin · crackedBS 1022 ABOVE LONGERON 14R EXTERNAL SKIN CRACKED, HFEC VERIFIED. REPAIRED THE SKIN IAW ERA NR 545671-14.May 20, 2016 · N957AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016052404178Stiffener · crackedAFT ACCY RT SIDE FRAMES 1178.225 & 1200 HAVE 2 EA SUPPORT STIFFENERS CRACKED. CAN BE SEEN INSIDE RT VENT BOX. R & R CRACKED STIFFENERS IAW SRM 51-41-02, SECTION 4.May 19, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016052004040Shear Tie · crackedBS 1022, BELOW LONGERON 14R FOUND SHEAR TIE CRACKED DURING INSPECTION WITH ORN 66647-200-0049. REPLACED SHEAR TIE IAW SRM 51-41-05, PARA 2.May 17, 2016 · N957AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016052004037Former · crackedLOWER FUSELAGE, LT FILLET, BS 674-L27L, CRACKED STR IN BOX. MARKED ON OUTSIDE. REPAIRED FORMER BS 674, L27L IAW ER/A 545672-14, REV 0. ASSOCIATED ER/A 54-567214 ADDED FOR AC 9516.May 17, 2016 · N957AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016051803990Cusp Web · crackedCUSP WEB CRACKED AT BS 813. REPAIRED THE CUSP WEB IAW SRM 53-00-55, REPAIR 4, FIG 216.May 17, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016051803988Skin · crackedSTA 1037 ABOVE LONGERON 14R EXTERNAL SKIN CRACKED, HFEC VERIFIED. CUTOUT CRACKED SKIN AND INSTALLED REPAIR IAW PRI 545670-14, REV 3 AND ER/A 545670-14.May 17, 2016 · N957AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051803987Skin · crackedBS 1037, ABOVE LONGERON 14L EXTERNAL SKIN CRACKED, HFEC VERIFIED. CUTOUT CRACKED SKIN AND INSTALLED REPAIR IAW PRI 545670-14, REV 3 AND ER/A 545670-14.May 17, 2016 · N957AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016052104173Structure · crackedLOWER FUSELAGE, RT FILLET, BS 696 STRINGER 27R, CRACKED STRINGER END. REPAIRED DAMAGED FORMER AT BS 696-L27R IAW ERA 545672-14.May 13, 2016 · N957AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016052004041Cusp Web · corrodedLEFT CUSP WEB CORRODED AT BS 446 - 927. BLENDED CORRODED AREAS FOUND TO BE WITHIN LIMITS IAW SRM 53-00-55, FIG 101.May 12, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016051303918Cusp Web · crackedCUSP WEB CRACKED AT BS 813 RIGHT. REPAIRED CUSP WEB AT FS 813 BY REMOVING DAMAGE AND INSTALLING A DOUBLER IAW SRM 53-00-55, REPAIR 4, FIG 216.May 12, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016051303917Seat Track · corrodedF/O'S AFT OTBD SEAT TRACK IS CORRODED IN SEVERAL PLACES. REPLACED F/O AFT SEAT TRACK IAW SRM 51-41-01, PARA 2 DUE TO PART BEING CORRODED OUT OF LIMITS.May 12, 2016 · N957AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016051303915Skin · crackedSKIN CRACKED AT APPROXIMATELY FS 1095 AND APPROX 6" ABOVE RT PYLON-M. REPAIRED SKIN CRACK AT FS 1095 IAW ER/A 54669-14. SRM 51-40-05, PG 1 IDENTIFY REPAIRED IAW ER/A 54669-14. ASSOCIATED ER/A 54-566914 ADDED FOR AC 9516.May 12, 2016 · N957AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051203891Intercostal · crackedINTERCOSTAL CRACKED IN FWD CARGO CEILING AT BL 0, BS 636. REPAIRED DAMAGED INTERCOSTAL AT BS 636, BL-0 IAW SRM 53-00-00, REPAIR 1.May 11, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016051103851Cusp Web · corrodedAT BS 370 RT CORRODED CUSP WEB. CORROSION CUT-OUT AND REPAIRED IAW SRM 53-00-55, REPAIR 4, FIG 216 & 223. CORROSION AT FASTENER HOLE REMOVED, BLEND OUT, & WITHIN ALLOWABLE LIMITS, REMOVED .001 ALLOWED REMOVING .002 IAW SRM 53-00-55. ALLOWABLE DAMAGE 1, PARA May 10, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016051303916Skin · gougedVERTICAL STABILIZER SKIN RT GOUGED UNDER PANEL 360AT. REPLACED NEW VERTICAL STABILIZER SKIN RT IAW DWG 5936143 AND 51-41-02, PARA 4 AND 51-41-05, PARA 2.May 9, 2016 · N957AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2016051003834Seat Track · corrodedLOWER FUSELAGE, AFT CARGO, RT SEAT TRACK FOR BS 995-1021, FASTENER HOLES CORRODED. FABRICATED NEW AFT CARGO RT SEAT TRACK F/S 995-1021 IAW SRM 51-40-08, TABLE 1. NEW SEAT TRACK TO BE INSTALLED ON NR 66647-0100-077, PARTIAL 4.May 9, 2016 · N957AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016051103850Cusp Web · corrodedCUSB WEB AT BS 585 RT CORRODED. REPLACED LOWER CUSP TEE SPLICE CORRODED OUT OF LIMITS 50 PERCENT. REPLACED UPPER CUSP TEE SPLICE AND DAMAGED CUSP WEB AT BS 575 TO 595 IAW SRM 53-00-00, FIG 103, SRM 51-41-05, SRM 51-41-02.May 8, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016051003833Floor Support · damagedMULTIPLE DISCREPANCIES NOTED ON THE FORE TO AFT FLOORBEAMS BS 1022-1053. REPLACED FORE TO AFT FLOORBEAMS BS 1022-1053 RT AND LT BL 445 IAW SRM 51-41-05, PG 17, PARA 8, ER/A 545674-14. COMPLIED WITH ASSOCIATED ER/A 54-567414 ADDED FOR AC 9516.May 8, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016050603710Attach Angle · crackedPYLON BULKHEAD BS 1022 AFT ATTACH ANGLE CRACKED AROUND 2 FASTENERS LONGERON 7L. REPAIRED ATTACH ANGLE AT 1022 L7L IAW SRM 51-70-11, REPAIR 1, FIG 201.May 5, 2016 · N957AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2016050603709Attach Angle · crackedPYLON BULKHEAD BS 1022 AFT ATTACH ANGLE CRACKED AROUND 2 FASTENERS, LONGERON 7R. REPAIRED ATTACH ANGLE AT 1022 L7R IAW SRM 51-70-11, REPAIR 1, FIG 201.May 5, 2016 · N957AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2016050503661Bracket · crackedINTERCOSTAL BRACKETS ARE CRACKED, VERIFIED WITH HFEC ON THE FWD SIDE OF FRAME AT BS 237. JUST OTBD OF LONGERON 28L ABD OTBD OF LONG .28R LOCATED UNDER CARGO TIE-DOWN TRACKS. REMOVED CRACKED INTERCOSTAL BRACKETS AT BS 237, STR 28R AND 28L. FABRICATED ANGLES 9May 4, 2016 · N957AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2015121507611Sign · inoperativeDURING THE TURN-AROUND CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE AFT OVERWING HATCHES ON BOTH SIDES WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Dec 14, 2015 · N957AT · Boeing 717200 · Emergency LightingSDR DALA2015100906013Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THE MID-CABIN EMERGENCY LIGHTING WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND OPS CHECKED GOOD.Oct 9, 2015 · N957AT · Boeing 717200 · Emergency LightingSDR DALA2015030101769Frame · crackedDURING AD MANDATED INSPECTION, FOUND LT OVERWING FRAME AT STATION 696 CRACKED BELOW L18. REPLACED IAW DWG SR95530013, REV A, SRM 51-40-2 AND 51-40-05.Feb 28, 2015 · N957AT · Boeing 717200 · Fuselage Main, Frame
Back to N957AT