Pratt & Whitney JT8D-9
Service difficulty reports · 686
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 = 'JT8D9' 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.
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 = 'JT8D9' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201007262760Floorbeam · corrodedFLOORBEAM CORRODED STA 380 RBL 25 T0 45 CUT OUT DAMAGED AREAS DIMS 2" X 9". FABRICATED 2 ANGLES USING 7075-O .090 DIMS 24" X 1.8" AND 17.375" X 1.6" AND FILLER USING 7075T-6 .125 DIMS 2" X 9". HEAT TREATED PARTS TO T6 CONDITION IAW FASI ENG REPORT 2-37153-801SDR K11A2010072672201Stringer · corrodedSTRINGER HAS CORROSION, 12 INCHES.SDR K11A2010072572201Web · corrodedWEB HAS HOLE CORRODED THRU ENTIRE WEB, 6 INCHES.SDR FDEA201007242766Seat Track · corrodedSEAT TRACK CORRODED, STA 1085, BL 0. CORROSION OUT OF LIMITS. REMOVED SEAT TRACK BS 1000 TO BS 1130. FABRICATED NEW SEAT TRACK SECTION USING BAC1520-792-7178-T6511 DIMS 129 3/8", FABRICATED STRAP USING 7075T-6 .250 DIMS 7 1/8" X 2 1/8", FABRICATED 2 ANGLES SDR FDEA201007242767Seat Track · corrodedSEAT TRACK CORRODED, STA 970-1010, RBL 45. CORROSION OUT OF LIMITS. REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792-7178-T6511 DIMS 174 5/8", FABRICATED SPLICE USING BAC1503-100122-7178 DIMS 13", FABRICATED 2 EACH PLATES USING 7075T-6 .25SDR FDEA201007242762Seat Track · corrodedSEAT TRACK CORRODED STA 360-400, RBL 45. REMOVED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK SECTION USING BAC1520-792 7178-T6511 DIMS 136" AND INSTALLED IAW SRM 51-30-2 AND P-F SRM 53-10-2.SDR FDEA201007242763Seat Track · corrodedSEAT TRACK PREVIOUS REPAIR CORRODED STA 360-390, LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178-T6511 DIMS 136" AND INSTALLED IAW SRM 53-10-5SDR FDEA201007232746Skin · chafedSKIN GOUGED STA 720E, STR 19L LAP SEAM. CUT-OUT DAMAGED AREA DIMS 4.7500" X 2.7500". FABRICATED REPAIR DOUBLER USING 2024T- 3 .071 DIMS 12.5" X 9.2500", FABRICATED FILLER USING 2024T-3 .063 DIMS 4.7500" X 2.7500" AND TAPERED SHIMS USING 2024T-3 .071 DIMS 3SDR K11A2010071372201Spar · crackedWING CTR SECTION REAR SPAR WEB, UPPER HAS CRACK IND IN WEB RADIUS, 1 INCH.SDR K11A2010070972204Seat Track · corrodedSEAT TRACK CORROSION 20 INCHES.SDR FDEA201006252320Seat Track · corrodedCORROSION ON SEAT TRACK BS 690-740 LBL25 CORROSION OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178 T6511, DIMS 172", FABRICATED ANGLE SPLICES 2 EA USING BAC1503-100122 7178 T6511 DIMS 13.1250" X 2.3750" EACH ANSDR FDEA201006252322Seat Track · corrodedSEAT TRACK CORRODED BS 690-740 LBL 45. CORROSION OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178 T6511 DIMS 14' 2" AND INSTALLED REPAIR PARTS IAW SRM 53-10-5 AND 51-10-2.SDR FDEA201006192101Shear Tie · misinstalledIMPROPER SPACING OF FASTENERS IN SHEAR TIE AT BS 640 BETWEEN STRINGERS 28L AND 27L. CUT OUT DAMAGED SHEAR TIE IAW SRM 53-10-4 FIG 15. CUT OUT ORIGINAL SKIN AND MCD DOUBLER DIM: 1 1/2" X 1" IAW SRM 53-30-3 FIG 1B. FABRICATED SHEAR TIE FROM 7075 0 .063" DIM: 6" SDR FDEA201006182063Stringer · corrodedCORROSION ON STRINGER 28L AT SPLICE BS 485. CUT OUT DAMAGED SECTION OF STRINGER DIM 24 7/8" LONG IAW SRM 51-10-1. FABRICATED NEW STRINGER HAT SECTION FROM BAC1498-138 7075 T-6 DIM 24 7/8" LONG AND 2EA ANGLES FROM BAC1493-513 7075 T-6 DIM 11 1/2" LONG AND 1EASDR FDEA201006182062Torque Box · crackedAFT AIRSTAIR, LT LOWER TORQUE BOX INNER WEB LIGHTING HOLE IS CRACKED AT BS 1223. CUT OUT DAMAGED AREA DIMS 3/4" X 3/4". FABRICATED REPAIR DOUBLER USING 7075T-6 .032 DIMS 2" X 7" AND INSTALLED IAW SRM 51-30-2, 53-10-2 AND 51-40-2.SDR DALA1012949855Light · inoperativeON FLIGHT CHECK MX FOUND EMERGENCY LIGHTS AT SEAT 6 WERE INOP. MX REPLACED LIGHT ASSY. OPS CHECK OF LIGHTS NOW CHECK GOOD.SDR FDEA201006061844Battery · inoperativeDURING SERVICE CHECK FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. INSTALLED NEW BATTERIES IN EMERGENCY LIGHT ASSY IAW AMM 33-50-001-2. OPS CHECKS GOOD.SDR DALA1012339922Battery Pack · inoperativeDURING LINE CHECK MX FOUND CEILING EMERGENCY SIGNS AT ROW 12 AND 14 INOP. MX REPLACED BATTERY PACKS FOR POWER SUPPLY UNITS AT B5-33 AND B5-25. OPS CHECK OF LIGHTS NOW CHECK GOOD.SDR FDEA201005291707Windshield · crackedR1 WINDOW ARCED AND CRACKED AT FL350 DURING CRUISE. OUTER PANE CRACKED, NO PRESSURIZATION LOSS. R & R R1 WINDSHIELD IAW AMM 56-11-011-4. ALSO MOVED WINDOW WIRING LEAD TO TRANSFORMER TAP TERMINAL 26, IAW AMM 30-41-042-5. OK FOR SERVICE. (CLOSED)SDR FDEA201004131198Rib · crackedNR 3 SLAT 2ND FROM INBD RIB IS CRACKED AT SLAT STA 128. REMOVED CRACKED RIB, FABRICATED NEW RIB USING 7075-O .032 DIMS 18" X 6", HEAT TREATED TO T6 CONDITION IAW ENG REPORT 2-37153-801 REV A, LOCATED, DRILLED AND INSTALLED RIB IAW SRM 51-30-2, 51-20-1, AND 51SDR FDEA201004051058Stringer · damagedUPON REMOVAL OF BS 600 FRAME SUPPORT CLIP, FOUND STR 24 L GOUGED AND PUNCTURED. CUT OUT DAMAGED SECTION OF STRINGER 24L AT BS 600, 17.7500" IN LENGTH IAW SRM, REV 102, 51-10-1 AND 53-10-3 FIG 1. FABRICATED STRINGER FILLER USING BAC1498 -142, 7075-T62, 17.75SDR FDEA201003301031Skin · gougedUPON REMOVAL OF INTERCOSTAL FOUND GOUGE IN FUSELAGE SKIN FWD OF BS 970 BTWN STR 30 AND STR 29R. REMOVED GOUGE AND CORROSION AND FOUND OUT OF LIMITS, REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, CUT OUT DAMAGED AREAS DIMS 2.3750" X 4", 2 3/8" X 5.3125" AND 1" X 3"SDR DALA106299862Longeron Splice · corrodedDURING (H) CHECK FOUND LONGERON SPLICE FITTING CORRODED AT BS 655 L28L. REPAIRED IAW SRM 51-10-4 AND DWG NR 3932849.SDR DALA106309862Skin · chafedDURING (L) CHECK FOUND RT WING L/E NR 1 SLAT OTBD LOWER SURFACE REPAIR DOUBLER CHAFED. REPAIRED IAW SRM 51-30-8, 51-30-8, 51-30-2.SDR FDEA201003240987Web · crackedFWD CARGO CUTOUT, STA 620, BETWEEN STR 24R AND 25R, CRACKED WEB. CUT OUT DAMAGED SECTION OF WEB, FABRICATED NEW FILLER USING 7075T-6 .071 PO 9009353 DIMS 6" X 4", FABRICATED 2 EACH DOUBLERS USING 7075T-6 .080 PO 9008389 DIMS 4" X 4" AND 4" X 3" AND INSTALLED SDR FDEA201003240985Skin · misrepairedPREVIOUS REPAIR LOCATED AT STA 1223 STR 23R REQUIRES EVALUATION IAW EO 7-5100-7-5005 PH. REPAIR HAS BLIND FASTENERS INSTALLED. REMOVED BLIND FASTENERS AND INSTALLED SOLID FASTENERS IAW SRM 53-30-3.SDR FDEA201003241049Shear Tie · corrodedCORROSION ON SHEAR TIE AT STA 720C STR'S 28R AND 27R. CORROSION OUT OF LIMITS, REMOVED SHEAR TIE, FABRICATED NEW SHEAR TIE USING 2024T-3 .040 PO NR 9009253 DIMS 5 INCH BY 2 INCH AND INSTALLED IAW SRM 53-10-1, 53-10-2 AND 51-30-2.SDR FDEA201003240982Stringer · corrodedFWD PIT- CORROSION AROUND DOME NUT IN STRINGER 27R AT BS 705. CORROSION OUT OF LIMITS, REMOVED DAMAGED STRINGER, FABRICATED FILLER USING BAC1498-144 7075T-6 PO 29067266 DIMS 9" X 3", FABRICATED 2 SPLICES USING BAC1498-132 7075T-6 PO 20017112 AND INSTALLEDSDR FDEA201003240986Skin · damagedC-2 DOOR EXTERIOR SKIN HAS ROUTE OUT GREATER THAN .100" AT FWD LOWER CORNER. CUT OUT DAMAGED AREA DIM 3 1/2" X 1 1/2" ON C-2 DOOR FWD LOWER CORNER OF SKIN IAW SRM 51-10-1 AND 52-00-3 FIG 3 FABRICATED REPAIR DOUBLER FROM 2024 T3 .080" PO 9009327 DIM 21 3/8SDR FDEA201003231005Skin · dentedDENTS (2 EA) EXTERIOR FUSELAGE BS 1059 STR 25R.SDR FDEA201003230984Shear Tie · corrodedFWD PIT- CORROSION ON SHEAR TIE AT BS 720B, BETWEEN STRINGERS 28L AND 27L. REMOVED CORROSION ON SHEAR TIE BS 720B BETWEEN STR 28L AND 27L. ORIGINAL THICKNESS .063", MATERIAL LOSS .008" MATERIAL REMAINING .055" FOUND OUT OF LIMITS IAW SRM 51-10-6 AND SRM 53-SDR FDEA201003230983Shear Tie · corrodedFWD PIT- CORROSION ON SHEAR TIE AT BS 720A (FWD SIDE) BETWEEN STRINGERS 28L AND 27L. REMOVED CORROSION ON SHEAR TIE, FWD SIDE BS 720A BETWEEN STRINGERS 28L AND 27L. ORIGINAL THICKNESS .063" MATERIAL LOSS .017" MATERIAL REMAINING .046" FOUND OUT OF LIMITS SDR FDEA201003230981Stringer · corrodedFWD PIT BS 740 STR 27R IS CORRODED AT AFT END. CORROSION OUT OF LIMITS, CUT OUT DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION USING BAC1498-147 7075T-6 PO 20017342 DIMS 8" AND SPLICE USING BAC1498-131 PO 9009232 DIMS 10", FABRICATED SHIMS USING 20SDR FDEA201003220980Stringer · corrodedFWD PIT- STRINGER 26R IS CORRODED AT BS 740. CORROSION OUT OF LIMITS, CUT OUT DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION USING BAC1498-147 7075T-6 PO 20017342 DIMS 8 1/2" AND SPLICE USING BAC1498-131 PO 9009232 DIMS 10 1/4", FABRICATED SHIMS USSDR FDEA201003210970Angle · crackedLT WING T/E FALSE SPAR CHORD ANGLE CRACKED WBL 118. TRIMMED OUT DAMAGE, FABRICATED NEW INBD WEB SECTION USING 7075T-6 .032 PO NR 9009201 DIMS 12 1/8 INCH BY 9 1/2 INCH, FABRICATED NEW LWR CHORD SECTION USING BAC1514-1437 7075T-6 PO NR 2911884, FABRICATED 2 ANSDR FDEA201003200979Angle · corrodedFWD PIT- 740 BULKHEAD LOWER CHORD ANGLE IS CORRODED BETWEEN STRINGERS 28R AND 27R. REMOVED DAMAGED ANGLE SUPPORT IAW SRM 51-30-2, FABRICATED ANGLE SUPPORT USING 7075-O .190 DIMS 10.7" X 12" IAW DWG 69-64841, HEAT TREATED TO T6 CONDITION IAW FASI ENG REPORT 2-SDR FDEA201003201152Skin · damagedFASTENERS WITH IMPROPER SPACING STA 440, STRINGER 19L. CUT OUT DAMAGED AREA, HFEC INSPECTED CUT OUT AND EXISTING HOLES WITH NO DEFECTS NOTED IAW NDTM 51-00-00. FABRICATED REPAIR STRAP USING 2024T-3 .063 PO NR 9009353 DIMS 12 .5" X 4.2500", REPAIR DOUBLER USISDR FDEA201003191191Skin · misrepairedFASTENERS WITH IMPROPER SPACING FWD PIT STA 540, STR 27L CUT OUT DAMAGED AREA THRU SKIN MCD STA 540 STR 27L IAW SRM 53-30-3, FIG 1B FABRICATED STRUCTURAL FILLER, DOUBLER AND TRIPLER IAW SRM 53-30-3 FIG 1B CUT OUT DAMAGED SHEAR TIE IAW SRM 53-10-4, FIG 15 FABRSDR FDEA201003090707Actuator · failedAFTER TAKEOFF, DURING FLAP RETRACTION FROM FLAPS 2, DEG TO FLAPS 0 AMBER LE FLAP LIGHT REMAINED ILLUMINATED. COMPLIED WITH STABILIZER AND IDENTIFIED NR3 SLAT STILL DEPLOYED. EXECUTED RED TABS BUT UNABLE TO ATTAIN CLEAN ACFT CONFIG NR 3 SLAT. REMAINED DEPLOYESDR C8GA201000002Duct · crackedDURING CLIMB OPERATION THE LOWER AFT BODY OVERHEAT ILLUMINATED IN FLIGHT. CREW PERFORMED APPROPRIATE CHECKLIST AND DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THAT THE NR 3 ENGINE ANTI-ICE DUCT WAS CRACKED. REMOVED AND REPAIRED DAMAGSDR FDEA201001130124Shear Tie · corrodedCORRODED SHEAR TIE FWD PIT BS. 680 STR 28L TO 28R. CUT OUT DAMAGED AREA IAW EX SRM 51-10-1 REV 102 FABRICATED REPAIR DOUBLER AND SHEAR TIE IAW SRM 53-10-4 FIG 13 REV 102. FABRICATED RADIUS FILLER IAW SRM 53-10 -4 FIG 13 INSTALLED DOUBLER, SHEAR TIE AND RSDR NWAA085719935Engine · stalledDURING TAKEOFF, ENGINE NR 2 EXPERIENCED MULTIPLE COMPRESSOR STALLS. TAKEOFF ABORTED AT 120 KNOTS. MX PERFORMED POST STALL INSPECTIONS. NTF. ENGINE NR 2 GROUND RUN TO TAKEOFF POWER WITH NO STALL OR SURGE. (K)SDR KNNA200700042Skin · crackedCRACK ON FUSELAGE SKIN AT LWR HINGE CUTOUT DOOR-R2 STA 951. REPAIRED AREA BY CUTTING OUT THE DAMAGE AND INSTALLING A REPAIR IAW SRM 53-30-3 FIG 45 AND ACO-0753104.SDR KNNA200700066Skin · bulgedPREVIOUS REPAIR ON FUSELAGE SKIN AT STA 907 AND STR-25R. REPAIRED BY REMOVING EXISTING REPAIR AND CUTTING OUT THE DAMAGED AREA, THEN FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-30-03 FIG 48 AND SKYKING ACO-0753116SDR KNNA200700067Skin · dentedSEVERAL DENTS IN FUSELAGE SKIN AT STA 410 TO STA 445. REPAIRED AREA BY CUTTING OUT THE DAMAGE AND FABRICATING THEN INSTALLING REPAIR PARTS IAW SRM 53-30-3-FIG 46 AND SKYKING ACO-0753104.SDR GAI2007F00001Connector · dirty(REF NR: GAIA 07-05 OP) DURING CLIMB THE FLIGHT CREW RETRACTED THE FLAPS NORMALLY HOWEVER, AT ZERO DEGREES FLAPS THE AMBER LIGHT REMAINED ILLUMINATED ON THE FRONT PANEL. FE PANEL INDICATED NR 4 SLAT EXTENDED. FOLLOWED OPS PROCEDURE AND CYCLED FLAPS WITH SAMESDR KNNA200700011Frame · misdrilledFOUND MISDRILLED HOLE AT SKIN OF SIDE FRAME, WL 212 LT, STA 179. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF MISDRILLED FASTENER HOLE BS 178 W/L 212.SDR KNNA200700010Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT W/L 234,RBL 9-RBL 10. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 RBL 9-RBL 10 .SDR KNNA200700012Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT STA 178 W/L 213.5, RBL1, W/L 224, LBL-1-RBL1, W/L 227, RBL 1. PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 W/L 213.5, RBL 1,SDR KNNA200700014Frame · crackedFOUND STA 178 RT SIDE FRAME IS CRACKED AT WL 207. PROVIDE INSTRUCTION TO REPAIR CRACK BY INSTALLING A SPLICE OVER THE (RIGHT SIDE) SIDE CHORD AT WL 212.
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