Pratt & Whitney PW4460
Service difficulty reports · 472
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 = 'PW4460' 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 = 'PW4460' 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 WRNA201301310002Eec · failedDURING TAKEOFF ROLL, CREW RECEIVED A LEVEL 2 ALERT ON THE EAD WITH A MASTER CAUTION LIGHT FOR ENGINE N1, RPM HIGH. DISCONTINUED TAKEOFF. MAXIMUM N1 RPM RECORDED WAS 111.6. NO FURTHER INCIDENT. FOLLOWED PROCEDURES IN FIM 77-11-06, INSPECTED ENGINE. NO FAULTSDR WRNA201301270017Engine · failedDURING TAKEOFF ROLL, CREW DISCOVERED THE ACFT SUFFERED AN AUDIBLE ENGINE STALL AND FAILURE. CREW ABORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. MX DISCOVERED METAL IN THE EXHAUST OF THE ENGINE, WITH LOTS OF METAL ON RUNWAY AS WELL. REMOVED SDR WRNA201312270016Cable · brokenDURING APPROACH, CREW EXPERIENCED A SLAT DISAGREE INDICATION. TOOK APPROPRIATE PECAUTIONS AN LANDED WITHOUT INCIDENT. AFTER VISUAL INSPECTION BY MAINTENANCE, PROBLEM WAS FOUND TO BE BROKEN SLAT CABLES. REPLACED SLAT CABLES, PERFORMED ADJUSTMENT AND RIGGED.SDR FDEA201312122967Meter · failedFUEL QTY, FUEL USED CHECK DISPLAYED AT APPROX 22437. ESTIMATED FUEL USED WAS 5K LBS ABOVE FUEL BURNED. IAW FUEL QTY 1 USED CHECKLIST ISOLATED THEN SHUT DOWN ENG NR 1. NO FURTHER LEAK. CONTINUED IAW CHECK LIST ISOLATED TANK TO ENG, LEAK CONTINUED. THEN IASDR WRLA20131118603Spinner · failedSPINNER CAME APART AND DAMAGED 15 C-1 FAN BLADES AND ENGINE INLET COWL. FOUND FOD TO NR 3 ENG. BLADES, SPINNER & ENG. INLET COWL. REPLACED ENG. INLET COWL, SPINNER AND ALL 38 FAN BLADES, REF AMM 22-31-02. HIGH POWER ENGINE RUN C/W REF. AMM 71-00-00. ALL OPSSDR IPXA3M79821Compressor · stalledNR 3 ENGINE COMPRESSOR STALL ON TAKEOFF AT GEAR RETRACTION, ENGINE TEMP HIGH (745 DEGREES C), EXPERIENCED YAW AND VIBRATION UNTIL THROTTLE PULLED TO IDLE, DUMPED FUEL TO LAND. AIR TURN BACK. R & R NR 3 ENGINE IAW T/C 9102. TESTED ALL PROCEDURES IN T/C 9102.SDR WRNA201308070011Oil System · overheatedON DEPARTURE, "OIL TEMP HIGH" ANNUNCIATION WITH OIL TEMP ON THE NR 1 ENGINE AT 166 DEGREE C. REDUCED POWER ON NR 1 IAW THE QRH. IDLE POWER WAS REQUIRED TO KEEP THE TEMPERATURE FROM EXCEEDING LIMIT. MAXIMUM OIL TEMPERATURE ACHIEVED 168 DEGREE C. WITH IDLE PSDR IPXA3M78849Landing Gear · inoperativeCENTER GEAR FAILED TO EXTEND MANUALLY. OPENSDR IPXA13M78849Landing Gear · unknownCENTER GEAR FAILED TO EXTEND MANUALLY. PERFORMED OPS TEST LANDING GEAR ALTERNATE RELEASE SYS IAW MM 32-32-00-710-803. ALL TESTS PASS OK FOR SVC.SDR IPXA13M78483Access Panel · missingLEFT OTBD ELEVATOR MISSING ACCESS PANEL AT BOTTOM OTBD. INSTALLED HINGE COVER IN REF TO CMM 55-21-02.SDR FDEA201305020898Fmu · faulted"FADEC ALT" MANUAL THROTTLES AT T/O NR 2 WOULD NOT ACHIEVE "MAX POWER" AT FADEC BAR, BOTH EPR & N1 NOTED BELOW NR 1 & 3 ENG. FADEC MODE IN NORMAL AND ALT. ALL ENGINE PARAMETERS WITHIN SPECIFIED LIMITS OUTLINED IN JRH. PERFORMED MAX POWER ASSURANCE RUN. NOTSDR WRNA201300009Carbon Seal · brokenNR 1 ENGINE OIL QTY LOW, TEMP AND PRESSURE NORMAL. DURING CLIMBOUT FROM MIA TO LIM. PILOTS NOTICED NR 1 ENGINE HAD LOSS OIL QUANTITY WITH TEMP AND PRESSURE NORMAL. CREW FOLLOWED SHUTDOWN PROCEDURES FOR NR 1 ENGINE, DUMPED 27000KGS FUEL, AND RETURNED TO MIA SDR WRNA201300008Housing · damagedDURING FLIGHT FROM IQQ TO MIA PILOTS NOTICED NR 1 ENGINE HAD LOSS OF OIL PRESSURE AND OIL QUANTITY. CREW FOLLOWED SHUTDOWN PROCEDURES FOR NR 1 ENGINE. ON SHUTDOWN CREW NOTED: OIL QTY: 1 QT, OIL TEMP: 156 DEG, OIL PRESSURE: 168. CREW RETURNED TO IQQ WITHOUT SDR FDEA201304080744Engine · failedON DOWN WIND DTW 4000, 190 KTS HEARD BANG AND FELT VIBRATIONS NR 3 RPM LO ALERT DISPLAYED" N1 18 PERCENT, EGT 540 N2 :45 PERCENT COMPLIED WITH ENG RPM LO CHECKLIST AND SHUTDOWN ENGINE. R & R NR 3 ENGINE. EA 1-7100-167353 COMPLIED WITH. OPS CHECKED GOOD.SDR WRNA201300007Gcu · malfunctionedDURING CRUISE FROM LTX TO MIA, CREW ENCOUNTERED A NR 3 GENERATOR OFF LIGHT AND LOSS OF POWER TO BUS NR 3 AND RIGHT EMERGENCY BUS. CREW DEPLOYED THE ADG AND REGAINED POWER TO BOTH BUSES. CREW DIVERTED INTO BOG DUE TO REMAINING FUEL ON BOARD WITH NO FURTHER INSDR WRNA201300006Seal · leakingDURING FLIGHT FROM CCS TO SCL PILOTS NOTICED NR 1 ENGINE HAD LOSS OF OIL PRESSURE AND OIL QUANTITY. CREW FOLLOWED SHUTDOWN PROCEDURES FOR NR 1 ENGINE. ON SHUTDOWN CREW NOTED THE FOLLOWING: OIL QTY: 1 QT., OIL TEMP: 156 DEG., OIL PRESSURE: 168. CREW RETURNESDR WRLA20130225580Cargo Track · crackedDAMAGE AT SEAT TRACK IN MAIN CARGO COMPARTMENT STA 630 RBL 8. SEAT TRACK REPLACED ACC SRM 53-00-52 REV 51.SDR WRLA20130225581Cargo Track · crackedDAMAGE AT SEAT TRACK IN MAIN CARGO COMPARTMENT STA 630 LBL 8. SEAT TRACK REPLACED ACC SRM 53-00-52 REV 51.SDR IPXA13M76807Scavenge Pump · leakingNR2 ENGINE LOST OIL PRESSURE AND OIL QUANTITY. CREW SHUTDOWN THE ENGINE AND DECLARED EMERGENCY. OIL LEAK TRACED TO OIL SCAV PUMP, ENGINE CHANGED DUE WINDMILLING WITH "0" OIL PRESSURE IAW TC 9103.SDR IPXA3M76771Engine · leakingEMERGENCY DECLARED -CREW EXPERIENCED LOSS OF OIL PRESSURE ON NR 3 ENGINE. PERFORMED A PRECAUTIONARY SHUTDOWN, DIVERTED. LANDED SAFELY WITHOUT INCIDENT. R & R NR 3 ENG IAW TC 9101. OPS CHECKED GOOD.SDR IPXA13M76674Line · crackedFL360, OBSERVED LEVEL 1 HYD 3 1 ELEV OFF 3-2 NRMP INOP. NR 3 HYD QTY LOW, EMERGENCY DECLARED. R & R LINE ASSY IAW MM 20 50 01 & 32 43 20 . NO LEAKS NOTED AT THIS TIME. OPS CHECKED GOOD.SDR IPXA2M76316B-Nut · looseDIVERSION - NR 1 ENGINE OIL QUANTITY DECREASED AT APPROX 1 QT IAW 30 MINUTES FOUND LOOSE B-NUT ON OIL PRESSURE TRANSMITTER. RETORQUED AND LEAK CHECKED OK.SDR WRNA201200014Engine · bird ingestionAFTER TAKEOFF FROM SUMU, HAD HIGH VIBRATION NR 3 ENGINE. DUMPED FUEL TO MAX LANDING WEIGHT AND RETURNED TO FIELD FOR A SAFE LANDING. AFTER LANDING ENGINE NR 3 WAS SHUT DOWN AS PRECAUTION. ON POST FLIGHT INSPECTION, FOUND 6 DAMAGED FAN BLADES WITH EVIDENCE OSDR IPXA12M75337Fitting · corrodedINSPECTION TYPE:3C, RCB FLOOR FITTING NR 10 RT SIDE CORRODED. AFTER REMOVAL FOUND PART CRACKED. FABRICATED REPLACEMENT FITTING IAW DWG WSP0750 AND SP11250221.SDR IPXA12M75166Light · inoperativeRIGHT SIDE DOOR ESCAPE SLIDE PRESSURE TEST LIGHT DOES NOT ILLUMINATE WHEN PUSHED. OPEN.SDR IPXA2M75166Switch · inoperativeRT SIDE DOOR ESCAPE SLIDE PRESSURE TEST LIGHT DOES NOT ILLUMINATE WHEN PUSHED. R & R PRESSURE TO TEST SWITCH IAW MM 25-61-04. OPS CKS OK. THIS CLEARS M487705. PLACARD REMOVED.SDR IPXA2M75290Fitting · crackedINSPECTION TYPE: 3C, RT LOWER WINGLET FWD MOUNT FITTING CRACKED. REPLACED BOTH ATTACH FITTINGS ON RT LWR WINGLET WITH KIT SB11570063-5, APPX E. (MAJOR)SDR IPXA12M75336Doubler · crackedINSPECTION TYPE:3C, LT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XOS 667. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 661-667 IAW EO MD11-5730-42916-D & SRM 57-40-02, REPAIR 9, FIG 203. (MAJOR)SDR FDEA201209023206Battery · unknownBATTERY DISCHARGE ILLUMINATED SEVERAL TIMES STAYED ON FOR APPROX 2 MIN LAST DURATION THEN EXTINGUISHED. EPCU FAULT REVIEW SHOWED "COOLING VALVE 3/ INTFC", BATTERY CHARGER FAULT DISPLAY SHOWED "CHARGER FAIL, BATT FAIL, BUSS OK". TROUBLE SHOT IAW MM 24-30-0SDR IPXA2M75277Seat Track · corrodedINSPECTION TYPE: 3C, SEAT TRACK CORRODED AT COURIER SEAT AFT CENTER ATTACH POINT. REPLACED CORRODED SEACTION OF SEAT TRACK ALONG RBL 17 BETWEEN BS 439 - 516 IAW DWG WSP0826 AND SRM 51-31-01. MINOR.SDR IPXA2M75278Seat Track · corrodedINSPECTION TYPE:3C SEAT TRACK CORRODED AT COURIER SEAT RT AFT ATTACH POINT. REPLACED CORRODED SEACTION OF SEAT TRACK ALONG RBL 36 BETWEEN STA 439-516 IAW DWG WSP0826 AND SRM 51-31-01. MINOR.SDR IPXA12M75175Web · crackedINSPECTION TYPE: 4C, R3 DOOR AFT JAMB LOWER WEB LIGHTNING HOLE CRACKED. REPAIRED R3 DOOR AFT JAMB LOWER WEB LIGHTNING HOLE REF SRM 53-40-15, REPAIR 3, FIG 201.SDR IPXA2M75196Longeron Splice · crackedINSPECTION TYPE:4C, SPLICE FITTING CRACKED ON FWD END AT L34R AND BS 1531/5-123. REPLACED SPLICE FITTING AT STA 1531/5-123 AND L34R REF SRM 51-33- 01, PG 30 AND 45.SDR IPXA2M75284Skin · crackedINSPECTION TYPE:4C, RT WING FIXED L/E SKIN IS CRACKED AT NR 13 SLAT TRACK CUT-OUT. REPAIRED RT WING FIXED L/E SLAT NR 13 SLAT TRACK CUT OUT REF SRM 57- 40-02, REPAIR 7, FIG 201.SDR IPXA2M75297Skin · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E SKIN IS CRACKED AT INBD FWD CORNER OF PANEL 619CB. REPAIRED RT WING FIXED L/E SKIN AT INBD FWD CORNER OF PANEL 619CB REF SRM 57-40-02, REPAIR 7, FIG 201.SDR IPXA2M75311Former · crackedINSPECTION TYPE:4C, LT WING FIXED L/E FORMER CRACKED AT AFT END XOR 377. REMOVED, FABRICATED AND INSTALLED LT WING FIXED L/E FORMER IAW DWG ARB1162, SRM 51-35-01, SRM 51-33-01.SDR IPXA12M75316Former · crackedINSPECTION TYPE:4C, LT WING FIXED L/E SUPPORT FORMER CRACKED BETWEEN FASTENERS AT APPX STA XOR 917. REMOVED, FABRICATED AND INSTALLED SUPPORT FORMER AT LT WING FIXED L/E AT STA XOR 917 REF SRM 51-31-01 PG 1 AND SRM 51-35-01.SDR IPXA12M75322Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT STA XOS636. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER AT XOS636 REF MD11-5730-42916-D.SDR IPXA12M75323Doubler · crackedINSPECTION TYPE: 4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AROUND FASTENERS AT STA XOS 667. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER REF EO MD11-5730-42916-D.SDR IPXA12M75377Longeron · corrodedINSPECTION TYPE: 4C, LONGERON 52, EXFOLIATED BETWEEN STA 1129/6-73 AND 1129/6-90 ON LT, RT AND BOTTOM SIDES OF FLANGES. REPAIRED LONGERON 52 BETWEEN STA 1129/6-73 AND STA 1129/6-90 BY FABRICATION AND PART REPLACEMENT REF DWG A6A7027, SRM 51-33-01, PAGE 1 AND SDR IPXA12M75382Floor Panel · puncturedINSPECTION TYPE: 4C, MAIN DECK FLOOR PANEL DENTED AND PUNCTURED. R & R FLOOR PANEL REF AMM 53-21-09-400-801.SDR IPXA2M75441Fitting · damagedINSPECTION TYPE: 4C, FOUND LOOSE FASTENERS ON NR 4 BANJO FITTING TO PYLON CARRY THRU CAP. REPAIRED VERTICAL STAB AFT SPAR RT NR 4 BANJO FITTING FASTENER HOLES COMMON TO THE NR 2 PYLON CARRY THRU CAP ATTACHMENT REF EO MD11-5530-46641-A APPX C AND E.SDR IPXA2M75079Lamp · inoperativeONE EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-12-15.SDR IPXA12M74943Structure · delaminatedRT OTBD ELEVATOR T/E HAS DAMAGE. REPAIRED IAW EO MD11-5520-47952-B.SDR FDEA201208193079Battery · failedNR 2 EMERGENCY BATTERY TEST FAILED. R & R NR 2 EMERGENCY BATTERY REF AMM 33-51-01-4. OPS TESTED GOOD.SDR IPXA12M74945Wire · damagedEMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRING IAW WDM 33-52 AT L2-484, CHECKED GOOD.SDR IPXA2M75066Longeron Splice · crackedINSPECTION TYPE:4C, LONGERON 2L SPLICE FITTING CRACKED AT BS 1129. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE FITTING AT BS 1129 L2L IAW DWG ADA8413 & SRM 51-33-01.SDR IPXA2M75206Fairing · crackedINSPECTION TYPE: 4C, NR 3 PYLON LOWER AFT FAIRING FOUND WITH A CRACK PROPAGATING FROM PREVIOUS STOP-DRILL REPAIR NEAR YPN297. REPAIRED NR 3 PYLON LOWER AFT FAIRING IAW EA 011-5450-01-A4215 REV IR AND UPS EO MD11-5450-48454-A.SDR IPXA12M75092Seat Track · crackedINSPECTION TYPE: 4C, SEAT TRACK LOWER FLANGE CRACKED AT BS 1421, LBL 9. REPAIRED SEAT TRACK IAW SRM 53-00-52, REPAIR 1, FIG 201.SDR IPXA2M75146Skin · corrodedINSPECTION TYPE: 4C, CENTER WING UPPER EXTERIOR SKIN CORRODED IN MAIN CABIN SUBFLOOR ABOVE STRINGER 15 AT LBL 114 F/STA 1227 (XCW103-109). REPAIRED CORROSION ON CENTER WING UPPER SKIN ABOVE S15 BETWEEN XCW103-109 IAW STA SA EA 011-5730-01-A4214, REV IR & EO M
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