N947AT

Service difficulty reports · 231

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 = 'N947AT' 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 DALA2019090805215Web · crackedCRACK ON INTERNAL STRUCTURE OF L1 DOOR. NRC 0066: WEB ON INTERNAL STRUCTURE OF L1 DOOR WAS REPAIRED PER SRM 52-00-00-2R REPAIR 2 FIG 201. (LP #1260373)Sep 7, 2019 · N947AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2019090805214Beam · crackedCRACKED LT NOSE LANDING GEAR JAMB BEAM AROUND STA Y=52 (FYT). NRC 00607: CRACKED LT NOSE LANDING GEAR JAMB BEAM AROUND STA Y=52 WAS REPAIRED PER ETI-17-19-158 REV. 1 AND ER/A 581111-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-581111 ADDED FOSep 7, 2019 · N947AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019090805213Skin · corrodedCORROSION IN ACCESSES #620DT, 620FT, 620DB, AND 620EB ON AREA SETTLEMENT AND COUNTERSINK AT FUEL TANK (AD). NRC 00551: CORROSION LEVEL 2, CORROSION IS OUT OF LIMITS. FUEL ACCESS PLATE #620EB WAS REPLACED. FUEL ACCESS PLATE WAS INSTALLED UNDER NR 2040-0012, JOBSep 7, 2019 · N947AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019090705212Floor Panel · damagedPUNCTURES, MISSING INSERTS, AND DELAMINATION ON FLOOR PANEL #211ANF (CPIL). NRC 00702: PUNCTURES AND DELAMINATION ON FLOOR PANEL #211ANF WERE REPAIRED PER SRM 51-70-09-2R-6 PAR. A TO H. NEW INSERTS WERE INSTALLED PER AMM 20-60-11. (LP #1259314)Sep 7, 2019 · N947AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2019090705211Cusp Web · crackedCRACK ON LT CUSP MEMBRANE STA 536 BTW X=44.5 AND X=54.5 AT PAX CABIN. (CPAX). NRC 00395: LT CUSP MEMBRANE STA 536 BTW X=44.5 AND X=54.5 WAS REPLACED PER 53-00-55-2R-4 FIG 226. (LP #1259207)Sep 6, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019090705210Frame · crackedCRACK FRAME BTW STA 1037 AND L=13 RT (FUS). NRC 00618: FRAME BTW STA 1037 AND L=13 RT WAS REPAIRED PER ER/A 581116-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND ETI-17-19-160 REV 1. ASSOCIATED ER/A 00-581116 ADDED FOR AC 9507. (LP #1258837)Sep 6, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019090705209Frame · crackedCRACK FRAME BTW STA 1037 AND L=14 ALSO L=17 LT (FUS). NRC 00617: FRAME BTW STA 1037 AND L=14 ALSO L=17 LT WAS REPAIRED PER ER/A 581057-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND ETI-17-19-159 REV.1. ASSOCIATED ER/A 00-581057 ADDED FOR AC 9507. (LP #125855Sep 6, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019090505163Beam · crackedCRACKED RT NOSE LANDING GEAR JAMB BEAM AROUND STA Y=47 (FYT). NRC 00456: RT NOSE LANDING GEAR JAMB BEAM AROUND STA Y=47 WAS REPAIRED PER SRM 53-10-14-2R-2 FIG.201. (LP #1256460)Sep 5, 2019 · N947AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019090305119Housing · corrodedCORROSION ON BEARING HOUSING OF RUDDER TORQUE TUBE AFT FUSELAGE AREA (A&P). NRC 00586: CORROSION LEVEL 2, BEARING HOUSING OF RUDDER TORQUE TUBE AFT FUSELAGE AREA WAS REPLACED PER AMM 27-21-01 AND SRM 51-41-02-0G. (LP #1252777)Sep 2, 2019 · N947AT · Boeing 717200 · Rudder Miscellaneous StructureSDR DALA2019090105118Door Frame · corrodedCORRROSION AT LWR, FWD DOOR JAMB. NRC 00170: CORROSION LEVEL 2, LOWER FWD DOOR JAMB WAS REPAIRED PER SRM 53-20-05-2R FIGURE 201. (LP #1250148)Aug 31, 2019 · N947AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019090105117Cusp Web · corrodedCORROSION ON LT CUSP WEB MEMBRANE IS OUT OF LIMITS FROM STA Y=980 TO Y=983 AND BTW X=60 TO X=54 (CPAX). NRC 00664: CORROSION LEVEL 2, CUSP WEB MEMBRANE LT FROM STA Y=980 TO Y=983 AND BTW X=60 TO X=54 WAS REPAIRED PER SRM 53-00-55-2R-4 FIG. 215. (LP #1249804)Aug 31, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019083105116Not Reported · crackedCRACK AT L=4 LT STA Y=1022 (CPAX). NRC 00532: L=4 LT STA Y=1022 WAS REPAIRED PER SRM 53-00-05-2R-2- FIG. 201. (LP #1248630)Aug 30, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019082905054Longeron · crackedCRACK AT LONGERON 5 LT, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.Aug 29, 2019 · N947AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019082805007Gusset · crackedCRACK GUSSET AT L=7 RH STA Y=1022 (CPAX). NRC 00537: GUSSET AT L=7 RH STA Y=1022 WERE REPAIRED PER ER/A 580881-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND ETI-17-19-154 REV. ORIGINAL. ASSOCIATED ER/A 14-580881 ADDED FOR AC 9507. (LP #1243761)Aug 27, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019082805006Skin · crackedCRACK AT FUSELAGE SKIN STA Y=1095 BTW L=13/14 LH (FUS). NRC 00039: FUSELAGE SKIN STA Y=1095 BTW L=13/14 LH WAS REPAIRED PER ER/A 580773-14 REV. ORIGINAL (PERMANENT REPAIR) AND ETI-17-19-155 REV. 1. WILL BE MONITORED BY LOG PAGE #1241544 PER ER/A NO 580773-14 RAug 27, 2019 · N947AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019082805005Former · crackedCRACK ON KEEL BEAM FORMER LH SIDE STA Y=696 AND X=30 (CPAX). NRC 00590: KEEL BEAM FORMER LH SIDE STA Y=696 AND X=30 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1 FIG 201. (LP #1243383)Aug 27, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019082805004Longeron · crackedCRACK AT L=6 LH STA Y=1022 (CPAX). NRC 00534: LONGERON 6 LH STA Y=1022 WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #1243376)Aug 27, 2019 · N947AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019082805003Access Panel · corrodedCORROSION IN ACCESSES #520CT AND 620CT ON AREA SETTLEMENT AND COUNTERSINK AT FUEL TANK (AI) (AD). NRC 00549: CORROSION LEVEL 2, FUEL ACCESS PLATE #520CT AND 620CT WERE REPLACED PER AMDS 2040-0012, 2040-0010, AND VERIFIED PER B717-200 IPC 57-22- 01-01. (LP #124Aug 27, 2019 · N947AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019082704976Former · crackedCRACK ON KEEL BEAM FORMER RH SIDE STA Y=715 AND X=-37. NRC 00595: CRACK ON KEEL BEAM FORMER RH SIDE STA Y=715 AND X=-37 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1 FIG. 201. (LP #1242493)Aug 27, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019082704974Keelbeam · crackedCRACK ON KEEL BEAM FORMER RH SIDE STA Y=679 AND X=-43 (FUS). NRC 00649: CRACK ON KEEL BEAM FORMER RH SIDE STA Y=679 AND X=-43 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1 FIG. 201. (LP #1241655)Aug 26, 2019 · N947AT · Boeing 717200 · Fuselage Main, KeelSDR DALA2019082704973Former · crackedCRACK ON KEEL BEAM FORMER RH SIDE STA Y=696 AND X=-30 (FUS). NRC 00591: CRACK ON KEEL BEAM FORMER RH SIDE STA Y=696 AND X=-30 CRACK ON KEEL BEAM FORMER RH SIDE STA Y=696 AND X=-30 WAS REPAIRED PER B717-200 SRM 51-70-11-2R-1 FIG. 201. (LP #1241629)Aug 26, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019082604960Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA X=07 FROM Y=160 TO Y=200 AT FWD WET AREA IN REF NRC 00587 (W1). NRC 00680: CORROSION LEVEL 2, FLOOR SUPPORT STA X=07 FROM Y=160 TO Y=200 AT FWD WET AREA (W1) WAS REPLACED PER B717- 200 SRM 53-10-51-0I-2 AND 51-41-01-0G. (LP #1240Aug 26, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019082604959Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA X=-05 FROM Y=200 TO Y=160 AT FWD WET AREA IN REF NRC 00588 (W1). NRC 00679: CORROSION LEVEL 2, FLOOR SUPPORT STA X=-05 FROM Y=200 TO Y=160 WAS REPLACED PER B717-200 SRM 53-10-51-0I -2 AND SRM 51-41-01-0G.Aug 26, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019082604958Keelbeam · crackedCRACK ON KEEL BEAM FORMER LH SIDE STA Y=679 AND X=43 (FUS). NRC 00648: CRACK ON KEEL BEAM FORMER LH SIDE STA Y=679 AND X=43 WAS REPAIRED PER B717-200 SRM 51-70-11 FIG 201 REP 1. (LP #1240605)Aug 25, 2019 · N947AT · Boeing 717200 · Fuselage Main, KeelSDR DALA2019082604957Keelbeam · crackedCRACK ON KEEL BEAM FORMER LH SIDE STA Y=715 AND X=37 (FUS). NRC 00594: CRACK ON KEEL BEAM FORMER LH SIDE STA Y=715 AND X=37 WAS REPAIRED PER B717-200 SRM 51-70-11 FIG 201 REP 1. (LP #1240592)Aug 25, 2019 · N947AT · Boeing 717200 · Fuselage Main, KeelSDR DALA2019082654955Skin · dentedSEVERAL DENTS ON LOWER AREA FWD FLAP MOVABLE VANE LEFT WING (AI). NRC 00247: LH WING FWD FLAP MOVABLE VANE WAS REPAIRED PER B 717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PARAGRAPH 4 FIGURE 202.Aug 24, 2019 · N947AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2019082644953Longeron · crackedCRACK AT LONGERON 4R, BS 1022, THE LONGERON WAS REPAIR IAW SRM 53-00-05-2R-2, FIG 201.Aug 24, 2019 · N947AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019082304923Cusp Web · crackedCRACK ON RH CUSP MEMBRANE STA 620 BTW X=- 44.5 AND X=-54.5 AT PAX CABIN. (CPAX). NRC 00396: RH CUSP MEMBRANE STA 620 BTW X=-44.5 AND X=-54.5 WERE REPAIRED PER B717-200 SRM 53-00-55-2R- 4 FIG. 215. (LP #1236084)Aug 23, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019082304922Cusp Web · crackedCRACK ON RH CUSP MEMBRANE STA 536 BTW X=- 44.5 AND X=-54.5 AT PAX CABIN. RH CUSP MEMBRANE STA 536 BTW X=-44.5 AND X=-54.5 WERE REPAIRED PER B717-200 SRM 53-00-55-2R- 4- FIG.219.Aug 22, 2019 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019082104885Frame · crackedCRACK AT LH RING PAN FWR LOWER SECTION BTW STA Y=889. LH RING PAN FWR LOWER SECTION BTW STA Y=889 WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1 FIG. 202.Aug 21, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019082104884Frame · crackedCRACK AT LH RING PAN FWD LOWER SECTION BTW Y=636. LH RING PAN FWD LOWER SECTION BTW Y=636 WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1- FIG. 202.Aug 21, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019082104883Frame · crackedCRACK AT RH RING PAN AT STA Y=870. RH RING PAN AT STA Y=870 WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1- FIG. 202.Aug 21, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019082104882Frame · crackedCRACK AT LH RING PAN FWD LOWER SECTION BTW Y=794. LH RING PAN FWD LOWER SECTION BTW Y=794/ 813 WAS REPAIRED PER B-717-200 SRM 56-20-02-2R-1 FIG. 202.Aug 20, 2019 · N947AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019081904853Hinge · crackedCRACK CUTOUT ON AFT HINGE AT RH/LH FIXED NLG DOOR (FUS). NRC 00136: CRACK CUTOUT ON AFT HINGE AT RH/LH FIXED NLG DOOR WAS REPAIRED PER B717-200 SRM 53-10-01-2R PROCEDURE 11 FIG. 201. (LP #1229158)Aug 18, 2019 · N947AT · Boeing 717200 · Fuselage, Door HingeSDR DALA2019070204004Light · disconnectedTHE CABIN CEILING EMERGENCY LIGHTS AT ROW 1 & 24 ARE INOPERATIVE. ONE LIGHT AT EACH LOCATION IS INOPERATIVE, LIGHTS ARE NOT ADJACENT. EACH WAS RELAMPED, BUT DID NOT CORRECT THE PROBLEM. THE LIGHTS WERE PLACED ON MEL 33-51-01A AND PLACARDS INSTALLED. MAINTENACEJun 21, 2019 · N947AT · Boeing 717200 · Emergency LightingSDR DALA2019012600572Lens · missingTHE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT 29B. MAINTENANCE INSTALLED THE LENS COVER. CHECK IS GOOD. (LP #0918194)Jan 25, 2019 · N947AT · Boeing 717200 · Emergency LightingSDR DALA2018032301851Skin · damagedSKIN AROUND LAV VENT ON BELLY BULDGED. FOUND AREA CORRODED AND SKIN CRACKED. REPAIRED IAW ER/A 566366-14, REV O.Mar 22, 2018 · N947AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018123197450Skin · corrodedTHE RIGHT HAND FUSELAGE SKIN AT VACUUM WASTE TANK VENT STA 1022-1037 / L28R-29R HAS CORROSION. ER/A 566366-14 ISSUED AND IS CURRENT. SECTION II IS LIMITED TO 12 MONTHS AFTER SECTION I, PENDING DAMAGE TOLERANCE ANALYSIS. ASSOCIATED ER/A 95-566366 ADDED FOR AC 9Mar 20, 2018 · N947AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017112908379Light · fodTHE CAPTAIN REPORTED A FIRE IN THE CABIN AT THE L1 DOOR AND TAXIED THE AIRCRAFT BACK TO THE GATE. THE FLIGHT ATTENDANT USED THE FIRE EXTINGUISHER ON A BURNING NAPKIN IN THE OVERHEAD LIGHT FIXTURE. THE NAPKIN REMAINS WERE REMOVED BY THE FLIGHT ATTENDANT. MAINNov 26, 2017 · N947AT · Boeing 717200 · Passenger Compartment LightingSDR DALA2019091005259Spar · crackedER/A 561912-14AD SECTION I ISSUED FOR CRACK REPAIR ON VERTICAL STABILIZER FRONT SPAR RT CHORD AND WEB. AD 2016-09-05 AFFECTED. ASSOCIATED ER/A 00-561912 ADDED FOR AC 9507. ASSOCIATED AA 5530-01048 ADDED FOR AC 9507. REF NEW LP 1262502FOR DTA, THIS LP TERMINATESep 26, 2017 · N947AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017092707108Spar Cap · crackedVERTICAL STABILIZER LEADING EDGE SPAR CAP WEB CRACKED. REPAIRED REF ER/A 561912-14AD, REV ORIGINAL.Sep 26, 2017 · N947AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017092707107Spar · crackedVERTICAL STAB, FOUND RIGHT SPAR CRACKED AT ZFS=52.267 REPAIRED IAW ER/A 561912-14AD REV ORIGINAL.Sep 26, 2017 · N947AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017092707106Spar Cap · damagedVERTICAL STABILIZER RIGHT FRONT SPAR CAP FORWARD FLANGE HAS CRACK INDICATIONS IN FIVE HOLES BELOW THE LEADING EDGE SKIN SPLICE ZFS=52.267. REPAIRED ER/A 561912-14AD, REV ORIGINAL.Sep 26, 2017 · N947AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017092707105Structure · damagedVERTICAL STAB LEFT AND RIGHT SIDE ZFS 52.267 UPPER TWO ROWS FASTENERS 85 LOOSE AND ELONGATED HOLES. COMPLIED WITH PRI 560974-14AD REV. 0, REV. 1, AND REV. 2. REPAIRED REF ER/A 560974-14AD REV ORIG. COMPLIED WITH ER/A 560974-14AD REV A.Sep 26, 2017 · N947AT · Boeing 717200 · Vertical StabilizerSDR DALA2017092207031Attach Fitting · corrodedCORROSION ON GALLEY FLOOR AT GALLEY SERVICE DOOR AFT GIRT BAR LATCH ATTACH FITTING. . REPLACED THE GIRT BAR ATTACH FITTING IAW SRM 51-00-07.Sep 21, 2017 · N947AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2017092207030Fitting · corrodedCORROSION ON GALLEY FLOOR AT GALLEY SERVICE DOOR FWD. GIRT BAR LATCH ATTACH FITTING. REMOVED AND REPLACED THE GIRT BAR ATTACH FITTING IAW SRM 51-00-07.Sep 21, 2017 · N947AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2017092207029Floor Support · corrodedCORROSION 0N GALLEY FLOOR SUPPORT ANGLE LBL 52 BETWEEN STA. 168 AND 193. M. NR 000-0001:5300-0116/029 00165 REMOVED CORROSION REF B717 SRM 53-00-00-1A. INSTALLED NEW GALLEY FLOOR SUPPORT. (LP #0222753)Sep 21, 2017 · N947AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017092207028Attach Angle · corrodedCORROSION ON GALLEY FLOOD ATTACH ANGLE LBL 44 BETWEEN BS 172 AND 199. REMOVED CORROSION IAW STM 53-00-00-1A. INSTALLED A NEW GALLEY FLOOR ATTACH ANGLE.Sep 21, 2017 · N947AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2017080806055Cable Assy · disconnectedFOUND CABLE BALL ASSEMBLY DISCONNECTED FROM SLIDE HANDLE LATCH ASSEMBLY ON TAILCONE SLIDE. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYSTEM AND COULD HAVE AN ADVERSE EFFECT ON THE EVACUATION ROUTE IF IT PREVENTED PROPER DEPLOYMENT OF THE TAILCONE. THAug 5, 2017 · N947AT · Boeing 717200 · Escape SlideSDR DALA2017052104055Battery · dischargedEMERGENCY EXIT SIGN IN CEILING FORWARD OF 1ST CLASS IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN B5-259 POWER PACK REF AMM 33-51. OPERATIONAL CHECK IS GOOD.May 21, 2017 · N947AT · Boeing 717200 · Emergency Lighting
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