Pratt & Whitney JT8D-17

Service difficulty reports · 1,680

Newest first. General aviation reporting is voluntary.

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 engine_model_key = 'JT8D17'
  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 DALA1020569856Battery Pack · inoperativeDURING LINE CHECK MX FOUND FIRST CLASS CEILING EMERGENCY LIGHTS INOP. MX REPLACED BATTERIES IN POWER SUPPLY B5-24 REF WDM 33-51-01. OPERATION OF LIGHTS NOW CHECK GOOD.Aug 26, 2010 · N765NC · Doug DC951 · Emergency LightingSDR DALA1019879884Mount · crackedDURING LINE CHECK, FOUND CRACK IN RT PYLON AFT ENGINE MOUNT SUPPORT FRAME AFT WEB. REPAIRED IAW ERA 484935-14.Aug 22, 2010 · N677MC · Doug DC951 · Engine Mount SectionSDR DALA1019889876Attach Angle · crackedDURING LINE CHECK FOUND CRACK IN LT PYLON FAIRING SUPPORT RIB ATTACH ANGLE. REPAIRED IAW DWG 9915500.Aug 21, 2010 · N785NC · Doug DC951 · Nacelle/Pylon, Attach FittingsSDR DALA1019899876Attach Fitting · crackedDURING LINE CHECK FOUND CRACK IN LT PYLON CLOSURE WEB UPPER CLIP INBD SIDE. REPAIRED IAW SRM 54-20-0.Aug 21, 2010 · N785NC · Doug DC951 · Nacelle/Pylon, Attach FittingsSDR DALA1019909876Attach Angle · crackedDURING LINE CHECK FOUND CRACK IN LT ENGINE PYLON INSP PANEL 8103 ATTACH ANGLE. REPAIRED IAW SRM 54-01.Aug 21, 2010 · N785NC · Doug DC951 · Nacelle/Pylon, Attach FittingsSDR EE4Y1010341Stringer · crackedEMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 8L CRACKED AT STA 157, STA 133 AND STA 22.5.Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/RibSDR EE4Y1010342Stringer · crackedEMPENAGE VERTICAL STABILIZER CAVITY,STR 9L CRACKED AT STA 110.Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/RibSDR EE4Y1010343Stringer · crackedEMPENAGE VERTICAL STABILIZER INTERNAL CAVITY,STR 5L AT STA 22.5 AND STA 157 WITH CRACK.Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/RibSDR EE4Y1010344Stringer · crackedEMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 6L CRACKED AT STA 180.Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/RibSDR EE4Y1010345Stringer · crackedEMPENNAGE VERTICAL STABILIZER INTERNAL CAVITY, STR 8R AT STA 180 CRACKED.Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/RibSDR EE4Y1010346Stringer · cracked(EE4Y) EMPENAGE VERTICAL STABILIZER INTERNAL CAVITY, ST STA 157 STR 7L CRACKED.Aug 17, 2010 · N762AT · Boeing 7272B7 · Vertical Stabilizer, Spar/RibSDR DALA1019549877Skin · crackedDURING LINE INSP, FOUND CRACK IN FUSELAGE SKIN AT BS 1303.604 BELOW LONGERON 15R. REPAIRED IAW SRM 53-01-12 & TRM DC9-A-53-30-01-801-663A.Aug 17, 2010 · N786NC · Doug DC951 · Fuselage Main, Plate/SkinSDR EE4Y1010326Keelbeam · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT FROM BS 950A TO BS 989, KEEL BEAM RT WITH CORROSION.Aug 10, 2010 · N762AT · Boeing 7272B7 · Fuselage Main, KeelSDR CA100811001Connector · wornAFTER DEPARTURE, THE NR 1 ENGINE OIL TEMP DROPPED TO ZERO, THE ACFT RETURNED TO THE POINT OF DEPARTURE AND MX REPINNED THE OIL TEMP CONNECTOR AT THE ENGINE.Aug 9, 2010 · Boeing 737248C · Engine Oil System WiringSDR FDEA201008062871Battery · inoperativeCOCKPIT O/H DOOR EMERGENCY LIGHTS GO DIM AFTER 30 SEC. REPLACED BATTERIES O/H COCKPIT DOOR EMERGENCY LIGHT PACK IAW MM 33-50-101-2-0 . OPS CK'S NORMAL. REPLACED BATTERIES O/H COCKPIT DOOR EMERGENCY LIGHT PACK IAW MM 33-50-101-2-0. OPS CKS NORMAL. (CLOSED)Aug 6, 2010 · N492FE · Boeing 727227 · Emergency LightingSDR CA100715006Circuit Breaker · weakDURING CLIMB-OUT THROUGH FL290 MULTIPLE ELECTRICAL EQUIPMENT FAILURES OCCURRED. ALL GENERATOR & TRANSFORMER RECTIFIER INDICATIONS NORMAL. A TRANSFER BUSS CIRCUIT BREAKER FOUND TRIPPED. AFTER A COOLING PERIOD CREW RESET CIRCUIT BREAKER. ALL SYSTEMS RETURNEDJul 12, 2010 · Boeing 7372X6C · DC Power Distribution SystemSDR CA100712011Ball Joint · leakingNR 3 ENGINE FIRE INDICATION ON CLIMB. INFLIGHT SHUTDOWN CARRIED OUT AND AIRCRAFT RETURNED TO STATION. AIRCRAFT INSPECTED, 8TH AND 13TH STAGE DUCT BALL JOINTS (BETWEEN ENGINE AND PYLON) FOUND LEAKING, REPAIRED AND AIRCRAFT RETURNED TO SERVICE.Jul 8, 2010 · Boeing 727281 · Turbine Engine Compressor SectionSDR DALA1022019859Socket · looseDURING LINE CHECK, MX FOUND THAT OF THE OVERWING EMERGENCY EXIT SIGN AT SEATS 15AB WAS INOPERATIVE. MX FOUND THE LIGHT SOCKET WAS LOOSE, RE-SECURED IT, AND FUNCTIONALLY CHECKED THE SYS.Jul 3, 2010 · N768NC · Doug DC951 · Emergency LightingSDR EE4Y100179Spar · corroded((EE4Y)) LT WING FRONT SPAR LOWER CHORD FLANGE WITH CORROSION AT W STA 460. (WO Y10122, SUB JOB 5, ITEM 1).Jun 1, 2010 · N840AL · Boeing 7372X6C · Wing SparSDR DALA1011469882Battery Pack · inoperativeDURING LINE CHECK, MX FOUND EMERGENCY EXIT LIGHT AT ENTRY DOOR INOP. MX REPLACED BATTERY PACK. OPS CHECK OF LIGHT NOW CHECK GOOD.May 29, 2010 · N670MC · Doug DC951 · Emergency LightingSDR EE4Y100108Stringer · crackedEMPENNAGE TAIL COMPARTMENT FWD CORNER OF THE HORIZ STABILIZER CUTOUT AT THE UPPER HORIZ BEAM STRINGER S-5A RT CRACKED FROM BS 1138 TO BS 1142.May 28, 2010 · N840AL · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR EE4Y100109Stringer · corrodedLWR FUSELAGE AFT CARGO COMPARTMENT AT B STA 767, STR 20L WITH CORROSION.May 28, 2010 · N840AL · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR TSAA1077009Bulkhead · crackedA SCHEDULED INSPECTION REVEALED A CRACK AT THE 1ST RIVET AT BS 1016 AFT PRESSURE BULKHEAD AT THE WEB DOME SECTION ALONG STIFFENER/ STR-17L. TRIMMED DOME WEBS ONE FASTENER ROW BELOW EXISTING REPAIR. REMOVED CIRCUMFERENTIAL TEAR STRAP AND DAMAGED WEB DOME SECTIMay 25, 2010 · N842AL · Boeing 737290C · Fuselage Main, BulkheadSDR DALA1010539857Frame · damagedDURING LINE CHECK FOUND DAMAGE TO FRAME AT BS1190 RT SIDE BELOW AUG VALVE. REPAIRED IAW ERA 482388-14, SRM 51-20-03.May 22, 2010 · N766NC · Doug DC951 · Fuselage Main, FrameSDR DALA1010159859Light · brokenON FLIGHT CHECK MX FOUND L1 DOOR EMERGENCY LIGHT BROKEN AND INOP. MX REPLACED LIGHT AT DOOR L1. OPS CHECK OF LIGHT NOW CHECKS GOOD.May 17, 2010 · N768NC · Doug DC951 · Emergency LightingSDR CA100517002Shear Tie · corroded582 HMV, LEVEL 2 CORROSION IDENTIFIED (IN THE FWD E&E BAY AT STA 360 BETWEEN STR 28 AND 27 ON BOTH THE RT AND LT SIDES OF THE ACFT.) - INVESTIGATION DATA STILL BEING COLLECTED - INITIAL REPORT THAT SHEAR TIES AND RADIUS FILLERS WERE REQUIRED TO BE FABRICATEDMay 14, 2010 · Boeing 737275C · Fuselage Internal Mounting StructureSDR FDEA201005081496Engine · leakingOIL QUANTITY DECREASED AFTER TAKEOFF. WITH .8 GAL INDICATED, BEGAN TO DECREASE IN OIL PRESSURE, AND WENT TO ZERO WITH LO PRESS/ FILT BYPASS LT ON. SHUTDOWN TIME 2040Z, ENGINE 2 WINDMILL AT 18 PERCENT N2 AND 13 PERCENT N1 TILL LANDING AT 2103 Z WITH 0 OIL PREMay 8, 2010 · N215FE · Boeing 7272S2F · Turbine Engine Oil SystemSDR TSAA1053008Stringer · crackedDISCOVERED 1" CRACK DURING SCHEDULED INSP AT BS 492.4, S-22R (AFT SIDE OF FWD CARGO DOOR CUTOUT FWD END OF STRINGER). R & R STRINGER ASSY IAW SRM 53-10-3, FIG 1, APPLIED CORROSION INHIBITOR.Apr 26, 2010 · N841AL · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR DALA107789867Door Frame · corrodedDURING "H" CHECK FOUND LOWER DOOR JAMB PAN CORRODED IN AFT CARGO COMPARTMENT. BS1060-BS116 L29R TO L26R. REPAIRED IAW SRM 53-13-3, 53-05-44.Apr 15, 2010 · N776NC · Doug DC951 · Fuselage Main, StructureSDR DALA107809867Longeron · crackedDURING "H" CHECK FOUND CRACK IN L28R IN E&E COMPARTMENT. REPAIRED IAW SRM 53-02-18, 51-30-2, 51-30-5, 51-10-3.Apr 15, 2010 · N776NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA107819867Longeron · crackedDURING "H" CHECK FOUND CRACK IN L28L IN E&E COMPARTMENT. REPAIRED IAW SRM 53-02-18, 51-30-2, 51-30-5, 51-10-3.Apr 15, 2010 · N776NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA107739867Doubler · chafedDURING H-CHECK, FOUND CHAFED DOUBLER ON AFT ACCESSORY COMPARTMENT RT TOP CORNER CUT OUT. REPAIRED IAW SRM 51-30-05, 51-30-01.Apr 13, 2010 · N776NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA107749867Shear Tie · crackedDURING H-CHECK FOUND SHEAR CLIP CRACKED AT BS 1151 BELOW STRINGER 14L. REPAIRED IAW SRM 51-30-02, 51-30-05.Apr 13, 2010 · N776NC · Doug DC951 · Fuselage Internal Mounting StructureSDR DALA107489859Cusp Web · crackedDURING L-CHECK FOUND CRACK IN LT CUSP WEB AT BS1140. REPAIRED IAW SRM 51-70-4 FIG 2, SRM 51-10-4.Apr 10, 2010 · N768NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA107529859Floorbeam · crackedDURING L-CHECK FOUND CRACK AND SHEARED FASTENERS ON CARGO FLOORBEAM AT BS 1140 LBL54. REPAIRED IAW SRM 51-72-01.Apr 10, 2010 · N768NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA107499867Frame · crackedDURING H-CHECK FOUND CRACK IN CANTED FRAME IN AFT ACCY AT BS 1339 JUST ABOVE LT LOWER TAIL CONE LATCH FRAME. REPAIRED IAW SRM 51-30-2, 51-30-5.Apr 10, 2010 · N768NC · Doug DC951 · Fuselage Main, FrameSDR DALA107559867Floor Panel · crackedDURING H-CHECK FOUND CRACK IN FLOOR PANEL NR 63. REPAIRED IAW SRM 51-10-2, 51-70-4, 53-23-0, 51-10-2, 51-30-9, 51-10-3.Apr 10, 2010 · N768NC · Doug DC951 · Fuselage Floor PanelSDR DALA107569867Cusp Web · crackedDURING H-CHECK FOUND CUSP WEB CRACKED AT BS 1130 RT. REPAIRED IAW SRM 51-10-3, 53-10-16-801-663A AND 51-30-2.Apr 10, 2010 · N768NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA107579867Bulkhead · corrodedDURING H-CHECK FOUND LT BULKHEAD PANEL IN AFT CARGO COMPARTMENT HAD CORROSION ON BOTTOM AROUND FASTENERS. REPAIRED IAW 51-10-3-, 53-01-1, 53-23-0, 51-30-1, 51-10-2, 51-30-2, 51-60-0.Apr 10, 2010 · N768NC · Doug DC951 · Fuselage Main, BulkheadSDR DALA107589856Wire · brokenON FLIGHT CHECK MX FOUND SEAT 26D EMERGENCY PATH LIGHT INOP. REPAIRED BROKEN WIRE IAW AMDS 33-51-04. OPS CHECK OF LIGHT IS NOW GOOD.Apr 9, 2010 · N765NC · Doug DC951 · Light System WiringSDR DALA107509867Attach Fitting · crackedDURING H-CHECK, FOUND CRACK IN FRAME ATTACH CLIP OTBD END IN KEEL AREA AT BS 712 RT. REPAIRED IAW SRM 51-30-5, 51-10-4, 51-10-2, 53-03-12.Apr 9, 2010 · N768NC · Doug DC951 · Fuselage Main, Attach FittingsSDR DALA107519867Floor Panel · corrodedDURING H-CHECK FOUND COCKPIT FLOOR PANEL NR 13 WITH SURFACE CORROSION. REPLACED FLOOR PANEL IAW SRM 53-33-00, 53-01-1, DWG 9952827.Apr 9, 2010 · N768NC · Doug DC951 · Fuselage Floor PanelSDR DALA107539867Floor Panel · crackedDURING H-CHECK FOUND CRACK IN FLOOR PANEL NR49. REPAIRED IAW SRM 51-10-2, 51-30-2, 51-10-4, 51-30-8, 53-70-4 FIGURE 2.Apr 9, 2010 · N768NC · Doug DC951 · Fuselage Floor PanelSDR DALA107659867Skin · crackedDURING H-CHECK FOUND L/E SKIN CRACKED ON RT WING AFT MOVEABLE VANE LOWER SURFACE. REPLACED IAW SRM 27-51-02.Apr 9, 2010 · N768NC · Doug DC951 · Leading Edge DevicesSDR DALA107669859Vane · delaminatedDURING L-CHECK FOUND RT WING INBD FLAP VANE TOP SIDE EXISTING REPAIR IS CHAFED AND DELAMINATED. REPAIRED IAW SRM 27-51-03, 51-70-02, 57-03, 57-50-9, 51-10-3.Apr 9, 2010 · N768NC · Doug DC951 · Trailing Edge FlapsSDR DALA107339859Cusp Web · crackedDURING L-CHECK FOUND LT OTBD CUSP WEB CRACKED AT BS1100. REPAIRED IAW SRM 51-30-1, 25-21-00, 51-30-2, 51-10-2, 51-10-3, 51-13-3 PAGE 613, 51-30-5.Apr 8, 2010 · N768NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA107369851Battery Pack · inoperativeWHILE DOING TRANSIT CHECK MX FOUND RT AFT EMERGENCY DOOR LIGHT INOP. MX R & R RT SIDE BATTERY POWER PACK IAW IAW 33-53-00. OPS CHECK OF LIGHT AND BATTERY PACK CHECKS GOOD.Apr 8, 2010 · N760NC · Doug DC951 · Emergency LightingSDR DALA107289867Frame · crackedDURING H-CHECK FOUND CRACK IN FORMER AT BS 1167 AT L18. REPAIRED IAW SRM 51-10-4, 51-30-02, 51-30-05.Apr 7, 2010 · N776NC · Doug DC951 · Fuselage Main, FrameSDR DALA107299867Shear Tie · crackedDURING H-CHECK FOUND CRACK IN SHEAR TIE CLIP LT OTBD END AT BS 734. REPAIRED IAW SRM 53-03-12, 51-10-4, 51-30-5.Apr 7, 2010 · N776NC · Doug DC951 · Fuselage Internal Mounting StructureSDR DALA107309867Membrane · damagedDURING H-CHECK FOUND MEMBRANE UNDER FLOOR PANEL NR 13 BS 153 HAS HOLE IN IT. REPAIRED IAW SRM 53-01-4, 51-10-2, 51-10-4, 53-20-03-801.Apr 7, 2010 · N776NC · Doug DC951 · Fuselage Miscellaneous Structure
Back to Pratt & Whitney JT8D-17