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.
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
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 DALA1022359868Floor Panel · corrodedDURING M-CHECK FOUND CORROSION ON MAIN CABIN FLOOR PANEL NR21 UPPER AND LOWER SURFACES. REPLACED FLOOR PANEL IAW SRM 51-10-4.SDR DALA1022369868Floor Support · corrodedDURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 160 LBL 42. REPAIRED IAW SRM 51-30-07, SRM 51-30-02 & SRM 51-30-05.SDR DALA1022379868Floor Support · corrodedDURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 160 LBL 55. REPAIRED IAW SRM 51-30-02 & SRM 51-30-05.SDR DALA1022389868Intercostal · damagedDURING M-CHECK FOUND INTERCOSTAL AT BS 218-237 BL 0 WITH ELONGATED FASTENER HOLES. REPAIRED IAW SRM 51-10-4, SRM 51-30-2, SRM 51-30-3 & SRM 53-01.SDR TSAA1021016Clamp · dislodgedON DESCENT, AT ABOUT FL 240, THE CREW EXPERIENCED THE ALTITUDE WARNING HORN SOUND. CREW CHECKED THE CABIN ALTITUDE, CANCELLED THE HORN, DONNED OXYGEN MASKS, AND ESTABLISHED COMMUNICATION. CREW DECLARED AN EMERGENCY AND CONTINUED AN EMERGENCY DECENT TO BELOW SDR DALA1022329868Fastener · missingDURING M-CHECK AND CUSP REPAIR FOUND FASTENERS WITH LESS THAT REQUIRED 4 TO 6D PITCH AND MISSING FASTENERS. REPAIRED IAW SRM 51-10-4.SDR DALA1022469886Angle · crackedDURING H-CHECK FOUND CRACK IN BULKHEAD HORIZONTAL SUPPORT ANGLE OTBD CLIP AT BS 1167, L12L. REPAIRED IAW SRM 51-10-2, SRM 51-10-4, SRM 51-30-05.SDR KNNA465091110KMIAWindow · crackedF/O'S SIDE WINDOW CRACKED. F/O'S NR 4 (SHOULD READ AS NR 5) WINDOW BEGAN CRACKING, DECENDED TO 14,000 FT WHILE PERFORMING ABNORMAL PROCEEDURES CHECKLIST BROUGHT CABIN PRESSURE DIFERENTIAL AT OR BELOW 5 PSI ADVISED F/A AND GROUND PERSONNEL, DECLARED EMERGENSDR DALA1022309868Floor Support · corrodedDURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 238-285 BL 0. REPAIRED IAW SRM 51-30-02, SRM 51-30-05 & SRM 51-30-01.SDR DALA1022319868Floor Support · corrodedDURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 237 BL 0. REPAIRED IAW SRM 51-30-02, SRM 51-30-05, SRM 53-13-1 & SRM 51-30-01.SDR DALA1022399868Frame · corrodedDURING M-CHECK, FOUND CORROSION ON FRAME AT BS 1079, FROM S29L TO S29R. REPAIRED IAW SRM 53-03, FIG 2A, SRM 51-10-3 & EA 09A51-37583, PAGE 133.SDR DALA1022409886Floor Support · corrodedDURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 256 -275 LBL 21. REPAIRED IAW SRM 51-20-1, PAGE 109.SDR TSAA1072015Fire Loop · failedNON-ETOPS CARGO FLT 14. CREW NOTED THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED QRH PROCEDURES AND SHUT DOWN THE NR 1 ENGINE. CREW LANDED WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE UPPER OVERHEAT LOOP IN ACCORDANCE WITH MM 26-11-11. OPS CSDR FDEA201009103343Attach Angle · crackedLT WING FALSE SPAR ATTACH ANGLE IS CRACKED WBL 118. REMOVED DOUBLER AND CUT OUT LOWER CHORD IAW DRAWING SR27-57-038 REV C. FABRICATED REPAIR ANGLES, NEW WEB, NEW I/B CHORD SECTION, NEW STRAP, RADIUS FILLERS, AND NEW WEB IAW DRAWING SR 27-57-038 REV C. INSSDR C8GA201000053Access Panel · corrodedDURING HEAVY MX INSP THE LT FUEL TANK ACCESS PLATE (7340) WAS CORRODED. REMOVED AND REPLACED ACCESS PLATE. NO OTHER DEFECTS NOTED, ACFT WAS RETURNED TO SERVICE.SDR FDEA201009093329Keelbeam · crackedRT WW, RT KEEL BEAM IS CRACKED AT BS 875 RBL10 TRIMMED OUT DAMAGED AREA AT LOWER CHORD OF KEEL BEAM STA 875 RBL 6 IAW SRM 51-10-1. FABRICATED DOUBLER FROM PN 15-5PH 0.071" DIM. 8.6250' X 4" AND INSTALLED DOUBLER IAW EA 7-5310-135591.SDR DALA1021779868Floor Support · corrodedDURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 160, BS 200 RBL 44. REPAIRED IAW SRM 51-10-2, SRM 51-10-4 & SRM 51-30-5.SDR DALA1021589868Window Frame · crackedDURING M-CHECK, FOUND CRACK IN UPPER FWD CORNER OF LT CABIN WINDOW FRAME AT BS 775-BS 794. REPAIRED IAW SRM 51-10-4, SRM 53-01 & 51-30-5.SDR DALA1021599868Stringer · crackedDURING M-CHECK, FOUND CRACK IN STRINGER AT BS 294 S17L. REPAIRED IAW SRM 53-02-18.SDR DALA1021609868Stringer · crackedDURING M-CHECK FOUND CRACK IN STRINGER AT BS 313 S17L. REPAIRED IAW SRM 53-02-18.SDR DALA1021619868Window Frame · crackedDURING M-CHECK FOUND CRACK IN LOWER AFT CORNER OF RT CABIN WINDOW FRAME AT BS 734-BS 753. REPAIRED IAW SRM 51-10-4, SRM 53-01 & 51-30-5.SDR DALA1021629868Window Frame · crackedDURING M-CHECK FOUND CRACK IN UPPER FWD CORNER OF LT CABIN WINDOW FRAME AT BS 794-813. REPAIRED IAW SRM 51-10-4, SRM 53-01 & SRM 51-30-5.SDR DALA1021639868Window Frame · crackedDURING M-CHECK FOUND CRACK IN UPPER FWD CORNER OF RT CABIN WINDOW FRAME AT BS 775-794. REPAIRED IAW SRM 51-10-4, SRM 53-01 & SRM 51-30-5.SDR DALA1021349868Intercostal · misinstalledDURING M-CHECK FOUND INTERCOSTAL AT BS 256 TO BS 275 BL0 WITH UPPER ROW OF FASTENERS ELONGATED. REPAIRED IAW SRM 51-30-2, SRM 51-30-5.SDR DALA1021379868Floor Support · crackedDURING M-CHECK FOUND CRACK IN 3 FLOOR SUPPORT FASTENER HOLES AT BS 180 TO BS 190, LBL 58. REPAIRED IAW SRM 51-30-2 & SRM 51-30-5.SDR DALA1021389868Cusp Web · crackedDURING M-CHECK FOUND CRACK IN RT CUSP WEB FASTENER HOLE AT BS 753. REPAIRED IAW SRM 51-10-4 & SRM 51-30-2.SDR DALA1021399868Floor Panel · crackedDURING M-CHECK FOUND TOP SKIN FASTENER HEADS PULLED AND SKIN CRACKED IN FLOOR PANEL NR70. REPAIRED IAW SRM 51-70-4, SRM 51-30-2.SDR DALA1021409868Floor Panel · damagedDURING M-CHECK, FOUND SKIN DAMAGED ON FLOOR PANEL NR 73. REPAIRED IAW SRM 53-23-2, SRM 51-30-2 & SRM 51-20-1.SDR DALA1021419868Floor Support · corrodedDURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 160 TO BS 200 BL 0. REPAIRED IAW SRM 51-10-2, SRM 51-30-2 & SRM 51-30-5.SDR DALA1021439868Frame · gougedDURING M-CHECK FOUND GOUGE IN FRAME, RT SIDE AT BS 1247 BETWEEN S12R & S14R. REPAIRED IAW SRM 53-10-05-801, FIGURE 1.SDR DALA1021449868Floorbeam · corrodedDURING M-CHECK FOUND CORROSION ON FLOORBEAM AT BS 237 LBL 1 TO LBL 20. REPAIRED IAW SRM 51-10-4, SRM 51-30-2.SDR DALA1021429868Floorbeam · crackedDURING M-CHECK FOUND CRACKS IN FLOORBEAM INTERCOSTAL AT BS 465 BL 0. REPAIRED IAW SRM 51-30-5 & SRM 51-30-2.SDR DALA1021499855Power Supply · inoperativeDURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 7-13 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYS.SDR FDEA201009033268Skin · bulgedSKIN BULGE STA 1052, STR 26L, LAP SEAM. CUT OUT LOWER SKIN DIM. 2" X 2" AT STA 1052 STR 26L LAP SEAM. FABRICATED REPAIR FROM 2024T3 0.071" DIM. 9.750" X 9", DOUBLER FROM 2024T3 0.063" DIM. 11" X 5", AND FILLER FROM 2024T3 0.050" DIM. 2" X 2". IAW SRM 53-30-SDR DALA1021359868Window Frame · crackedDURING M-CHECK FOUND CRACK IN RT CABIN WINDOW FRAME UPPER FWD CORNER AT BS 734 TO BS 753. REPAIRED IAW SRM 51-10-4 & A-5—20-02-201-925A-A.SDR DALA1021369868Window Frame · crackedDURING M-CHECK FOUND CRACK IN RT CABIN WINDOW FRAME UPPER FWD CORNER AT BS 794 TO BS 813. REPAIRED IAW SRM 51-10-4 & A-56-20-02-201-925A-A.SDR DALA1021459868Skin · dentedDURING M-CHECK FOUND DENT IN FUSELAGE SKIN AT BS 965 BETWEEN L28R & L29R. REPAIRED IAW SRM 51-30-5 & DWG SG095300001.SDR DALA1021469868Skin · crackedDURING M-CHECK FOUND CRACK IN EXISTING FUSELAGE DOUBLER AT RT SIDE OF AFT NOSE WHEEL WELL DOOR. REPAIRED IAW SRM 53-05-62, PAGE 340-341.SDR FDEA201009033341Skin · corrodedSKIN BULGE STA 1173 AT LAP SEAM STR 20R. COMPLIED WITH EA 7-5330-135593.SDR FDEA201009023272Skin · bulgedSKIN BULGE STA 1045 STR 26R LAP SEAM. REMOVED CORRODED STRINGER SECTION FROM BS 1026 TO 1070, STR 26R IAW SRM 51-30-2. FABRICATED 3 (EA) STRINGER SECTIONS FROM BAC1498-147 7075 T62 DIM 19" AND 4 (EA) SPLICE SECTIONS FROM BAC1498-131 7075 T6 DIM 9" IAW SRM 53SDR DALA1022009859Battery Pack · inoperativeDURING LINE CHECK, MX FOUND THAT BOTH OF THE OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION.SDR FDEA201009023342Skin · crackedRT LOWER AFT FUSELAGE AT BS 1010 STR 28R EXTERIOR SKIN IS CRACKED AND BULGING. CUT OUT DAMAGED AREA IAW SRM 53-30-3 FIG 3A REV 103. FABRICATED REPAIR DOUBLER AND FILLER IAW EA 7-5330-135592. INSTALLED REPAIR DOUBLER AND FILLER IAW EA 7-5330-135592.SDR DALA1021019868Floor Support · corrodedMAIN CABIN BETWEEN FS 160-200, LBL44 FLOOR SUPPORT HAS CORROSION. CPC TASK NR46-53303 REMOVED CORROSION MATERIAL LOSS UP TO .021. ORGINAL MATERIAL .063 FOUND TO BE OUT OF LIMITS IAW SRM 53-01. REMOVED AND FABRICATED NEW PART MAIN CABIN BETWEEN FS 160-200, LBL4SDR DALA1021029868Floor Panel · crackedMAIN CABIN FLOOR PANEL NR50 CRACKED AT 1EA FASTENER HOLE REMOVED DAMAGE AT FASTENER HOLE WITH 2" X 1" CUTOUT. HFEC INSPECTED IAW NDT SRM 06-10-0-001, NO CRACKED NOTED. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-01. REQUIRED INSP COMPLETED.SDR DALA1025989886Angle · crackedDURING H-CHECK FOUND CRACK IN RT PYLON ANGLE AT BS 1151 BETWEEN FUSELAGE AND PYLON. REPAIRED IAW SRM 54-04, FIGURE 10, PAGE 224.SDR DALA1020840868Cusp Web · gougedLT CABIN FLOOR CUSP WEB STA 845 CRACKED AT LIGHTNING HOLE. UPON FURTHER EVALUATION NO CRACKS FOUND AREA FOUND TO BE GOUGED. BLENDED GOUGE .2500" X .7500". FOUND TO BE OUT OF LIMITS. PERFORMED DVI USING 10X MAGNIFIER VERIFIED ALL DAMAGE REMOVED. FABRICATED ANDSDR DALA1020850868Floorbeam · corrodedMAIN CABIN BETWEEN FS 200 LBL 1-20 FLOOR SUPPORT HAS CORROSION CPCP TASK NR46-53303 RII: N REMOVED CORROSION 1" X 1" ORIG. MAT .060 REMOVED .033 REMAINING .027 FOUND TO BE OUT OF LIMITS REMOVED FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-10-03 F3-01 SDR DALA1020820868Floor Panel · crackedMAIN PASSENGER CABIN FLOOR PANEL NR43 TOP SKIN INBD FWD END CRACKED. RII: Y REMOVED FLOOR PANEL NR43 IAW SRM 51-30-1 CUTOUT DAMAGE IAW SRM SRM 51-70 4, HFEC INSPECTED CUTOUT AREA IAW NDT SPM 06-10-01 NO FURTHER DAMAGE NOTED FAB DOUBLER 7075T6 .032 IAW SRM 51SDR DALA1020815522Floor Panel · chafedMAIN PASSENGER CABIN FLOOR, PANEL NR 84, TOP SKIN FWD END 6 EA FASTENER HOLES CHAFED AROUND WASHERS. RII: Y CUTOUT DAMAGED AREA IAW SRM 51-70-04, FIG 1, HFEC INSP IAW NDT SPM 06-10-01, AND NO CRACKS WERE NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 5SDR DALA1020629877Light · missingDURING LINE CHECK MX FOUND EMERGENCY LIGHT AT 6D MISSING. MX INSTALLED NEW LIGHT ASSY AT 6D IAW CMM 25-28-62. OPS CHECK OF LIGHT IS NOW GOOD.
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