Pratt & Whitney PW4077
Service difficulty reports · 3,169
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 = 'PW4077' 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 = 'PW4077' 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 CALA2016082395657Battery Pack · inoperativeR2 DOOR EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW MM 33-51-06. OPS CHECKED GOOD.SDR CALA2016082395658Charger · inoperativeNR 3 CABIN DOOR EMERGENCY LIGHT CHARGER INOPERATIVE. REMOVED AND REPLACED THE CHARGER IAW MM 33-51-06, OPS CHECKED GOOD.SDR CALA2016082395659Charger · inoperativeNR 3 CABIN DOOR EMERGENCY LIGHT CHARGER FOUND INOPERATIVE. THE CHARGER WAS REPLACED AND CHECKED NORMAL IAW AMM 33-51-06.SDR CALA2016082395660Skin · chafedNR 1 PYLON PANEL 433CL CUTOUT INNER SKIN CHAFED. AREA SMOOTHED OUT PER SRM 51-10-02. BLEND OUT AREA AT FWD UPPER IS 0.7"X 0.4"WITH 0.114 REMAINING THICKNESS. FWD LWR IS 0.7"X 0.4"WITH .110 REMAINING THICKNESS. AFT UPPER IS 1" X 0.5"WITH 0. 102"REMAINING THISDR CALA2016081895651Unknown · odorCREW REPORTED AN ODOR FROM LAVATORY 101 THAT WAS STRONG AND SMELLED LIKE IODINE. ACCOMPLISHED AN INSPECTION OF MIRROR LIGHTS, WATER HEATER, AND THE FLUSH CONTROL ASSY. NO EVIDENCE OF ELECTRICAL ODOR OR INDICATION OF OVERHEATING. ALSO INSPECTED UNDER THE LAVASDR CALA2016081595647Light · unknownEMERGENCY LIGHTS AT ROWS 16 - 37 FAILED TO ILLUMINATE ALL EMERGENCY LIGHTS TESTED NORMAL ON GROUND.SDR CALA2016080995611Oven · fireOVEN FIRE IN "B" GALLEY. FLAMES IN BACK OF OVEN CONTAINED WITH DOOR CLOSED. R & R OVEN AND CONNECTOR INSPECTION ACCOMPLISHED OK.SDR CALA2016072995600Unknown · odorACRID ELECTRICAL ODOR ON FLIGHT DECK AT GATE. RAN APU 4 HOURS, BOTH PACKS TO FULL COLD AND PACKS TO FULL HOT. FWD GALLEY OVEN AND COFFEEMAKERS ON. NO ABNORMAL ODOR DETECTED.SDR CALA2016072295576Skin · crackedRIGHT FUSELAGE SKIN BS 2260 HAS A CRACK APPROX 1.5 INCHES IN LENGTH. REPAIRED IAW SRM-53-00-01, REPAIR-4, ZONE-B.SDR CALA2016072195568Unknown · odorELECTRICAL ODOR IN AFT CABIN, DECREASED WITH IFE SWITCH OFF. ACCOMPLISHED AMM 05-51-50, NO ELECTRICAL OR ABNORMAL ODOR IN THE CABIN NOTED AT THIS TIMESDR CALA2016071495561Skin · damagedFUSELAGE SKIN ABOVE L1 DOOR DAMAGED. REPAIRED IAW SRM 53-00-01 REPAIR 4.SDR CALA2016070195492Light · shortedBURNING ODOR BETWEEN DOORS 3 AND 4R WHEN WALKING THRU THE CABIN. PERFORMED A WALK THROUGH ENTIRE CABIN, ODOR IS STRONGEST AT 51JH ALONG SIDEWALL AREA ACP CABIN TEST, FOUND OEU 3-3-7 HAD A SHORT CIRCUIT. MESSAGE 23-03485. M23411 LOCATION RIGHT PSU PANEL ROSDR CALA2016061595452Fan · odorF/A REPORT OF AN ELECTRICAL ODOR AT AROUND DOOR 1R AND 1L AND DOOR 2R AND 2L ON DESCENT AROUND 10,000 FT. RAN ALL FORWARD AND MID GALLEY EQUIPMENT. CHECKED ALL CBS AND LIGHTING IN AREA BETWEEN DOORS 1 AND 2 LT AND RT. FOUND WHEN RUNNING FWD UPPER RECIRCULATSDR CALA2016061395448Engine · making metalCREW REPORTED ENGINE 2 BANG ON ROTATION WITH EGT SPIKE OVER 750 DEGREES. ENGINE AUTO SPOOLED BACK TO IDLE CREW RAN QRH AND SHUTDOWN ENGINE USING FUEL LEVER. ACFT CONTINUED TO CLIMB AND THEN RETURNED TO DEPARTURE AFTER DUMPING FUEL. NO SIGNS OF BIRDSTRIKE INSDR CALA2016061395446Fire Loop · shortedLEFT ENGINE FIRE DETECTION SYS LOOP 1 FAILURE. FIRE LOOP 1, LT ENGINE IS SHORTED. ENGINE FIRE DETECTION CARD, LEFT.SDR CALA2016051895365Battery Pack · dischargedL4 DOOR EMER SLIDE LIGHT DIM. REPLACED BATTERY PACK & CHARGER IAW MM 35-51-06.SDR CALA2016051295351Door · dentedECRA 5230-02001 REPAIR ACCOMPLISHED FOR DENT AT AFT LARGE CARGO DOOR, BETWEEN BS 1698 - 1726.45. REPAIR IS PERMANENT PROVIDED INSPECTION ACCOMPLISHED AS REQUIRED. PLANNING CONTACT EG AT 28,500 DOOR TC.SDR CALA2016042895321Skin · gougedGOUGE IN A-C SKIN JUST FWD OF L2 DOOR SILL. REF ESC 160423-2511-1 PARA A & B 1 - 4 & 6. CUT & REMOVED DAMAGE. COMPLIED WITH INSPECTION PORTIONS OF STEP M 1 - 4, & STEPS O, Q, & S OF AVO ESC 160 423-2511-1C. RESTORED DECORATIVE COVER AS REQUIRED. COMPLIEDSDR CALA2016042695302Skin · gougedGOUGE IN A - C SKIN JUST FWD OF L2 DOOR SILL. REF AVO ESC 160423-2511-1 PARA A & B 1-4 & 6 CUT & REMOVED DAMAGE. DO INSPECTION TO SURFACE OF REPAIR AREA & DO INSPECTION TO EXISTING SMC034.SDR CALA2016042295284Roll Pin · broken3L OVERHEAD AISLE EMER LIGHT BRACKET ASSEMBLY ATTACH PIN BROKEN. EMER LIGHT FUNCTION OK. ACCOMPLISHED INTERIM REPAIR TO CROSS AISLE BRACKET. REF IPC 33-51-01-62B FIG 3 ITM 120, ROLL PINS, NEED TWO EACH.SDR CALA2016022495124Skin · corrodedRIGHT WING LOWER SKIN UNDER SURFACE, SEVERAL AREAS WERE FOUND CORRODED, AT WS 573 - 626, STRINGER L14, WS 652 - 705 STRINGER -L14, WS 705 - 758, STRINGER L-14, WS 758 - 810.5, STRINGER -L14, WS 810.5 - 863, STRINGER -L14, WS 863 - 916, STRINGER -L14, WS 916 - SDR CALA2016022495126Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE, FOUND CORROSION AT WS 889.5 - 942, WS 942 - 968.5, WS 995 - 1021.5, WS 1047.5 - 1101, WS 1101 - 1155, WS 1182, WS 1292.5 - 1320 REAR SPAR AREA. LT WING LOWER SKIN EXTERIOR SURFACE CORROSION REMOVED & PROTECTED IAW SRM 51SDR CALA2016022495127Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L8 - L9, WS 1074, STRINGER L10, WS 862 - 916, STRINGER L10, WS 916 - 942, STRINGER L10, WS 995 - 1021, STRINGER L10, WS 1047 - 1101, STRINGER L10, WS 1101 - 1128, STRINGER L10, WS 115 5 - 1182, SDR CALA2016022495128Skin · corrodedLEFT WING LOWER SKIN, EXTERIOR SURFACE FOUND CORROSION, AT STRINGER L14, WS 580 - 599.5, STRINGER L14, WS 626 - 678, STRINGER L14, WS 758 - 810.5, STRINGER L14, WS 810.5 - 863, STRINGER L14, WS 863 - 889.5, STRINGER L14, WS 889.5 - 942, STRINGER L14, WS 942 - SDR CALA2016021695106Autoland Sys · malfunctionedAUTO LAND SYS INOPERATIVE DUE TO FAILURE IN AUTOPILOT FLIGHT DIRECTOR COMPUTERS, MODE CONTROL PANEL, AUTOPILOT BACK DRIVE ACTUATORS OR INTERFACING SYSTEMS. STATUS MSG 2713002 LATCHED CL MODE. ACCOMPLISHED FULL CAT 111 AUTO LAND CHECK. PERFORMED AFDC, MCP, BSDR CALA2016021295102Structure · crackedDENT AT STATION 2105, BETWEEN STRINGER 28R & 29R, HAS CRACK OUT OF SRM LIMITS. REPAIRED IAW SRM 53-00-0 1 REPAIR 6 FIG 202. REPAIR LOCATION STATION 2100 - 2111.SDR CALA2016012895037Skin · corrodedLEFT WING LOWER SKIN, EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, BETWEEN WS 1020 & WS 1050. LT WING LOWER SKIN EXTERIOR SURFACE CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.300, BLEND OUT REMAIN 0.290. HFEC INSDR CALA2016012895038Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE, FOUND CORROSION AT REAR SPAR, WS 1065 - WS 1080 AREA. LT WING LOWER SKIN EXTERIOR SURFACE CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.268, BLEND OUT REMAIN 0.226. HFEC INSPESDR CALA2016012895039Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, WS 1270 & WS 1280 AREA. LT WING LOWER SKIN EXTERIOR SURFACE CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.106, BLEND OUT REMAIN 0.091. HFEC INSPECSDR CALA2016012895040Skin · corrodedRIGHT WING CTR TANK MEASURING STICK 1, SURROUNDING SKIN FOUND CORRODED. REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.557, BLEND OUT AREA REMAIN 0.511. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION CARRIED OUT, NO DEFECTSDR CALA2016012895041Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, WS 1095 - 1105 AREA. REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.256, BLEND OUT REMAIN 0.247. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION CARRIED OUSDR CALA2016012895042Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION, AT STRINGER 14, WS 960 - 1000 AREA. REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.245, BLEND OUT REMAIN 0.200. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION CARRIED SDR CALA2016012895043Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, BETWEEN WS 995 - 1047. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.310 & BLEND OUT REMAIN 0.286. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTSDR CALA2016012895044Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION, AT STRINGER L14, BETWEEN WS 1021 - 1074. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.220, BLEND OUT REMAIN 0.200. HFEC INSPECTION, FLUORESCENT PENETRANT INSSDR CALA2016012895045Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION, AT STRINGER L14, BETWEEN WS 1182 - 1209. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & 51-20-01. SKIN ORIGINAL THICKNESS 0.155, BLEND OUT REMAIN 0.131. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTSDR CALA2016012895046Skin · corrodedRIGHT LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L14, BETWEEN WS 810 - 916. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-0. SKIN ORIGINAL THICKNESS 0.280, BLEND OUT REMAIN 0.241. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION CSDR CALA2016012895047Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT NEAR SPAR, BETWEEN WS 864 - 916. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.350, BLEND OUT REMAIN 0.319. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTIOSDR CALA2016012895048Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L10, BETWEEN WS 863 - 916. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.280, BLEND OUT REMAIN 0.284. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECSDR CALA2016012895049Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L14, BETWEEN WS 942 - 995. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.244, BLEND OUT REMAIN 0.236. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECSDR CALA2016012895050Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L10, BETWEEN WS 1209 - 1264. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.125, BLEND OUT REMAIN 0.089. HFEC INSPECTION, FLUORESCENT PENETRANT INSPSDR CALA2016012895051Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT NEAR SPAR, BETWEEN WS 1047 - 1074. REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.285, BLEND OUT REMAIN 0. 274. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION CARRISDR CALA2016012895052Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L10, BETWEEN WS 1128 - 1155. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.176, BLEND OUT REMAIN 0.172. HFEC INSPECTION, FLUORESCENT PENETRANT INSPSDR CALA2016012895053Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION, AT WS 1128 - 1155 REAR SPAR AREA. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.210, BLEND OUT REMAIN 0.191. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTIONSDR CALA2016012895054Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L11, BETWEEN WS 837 - 889. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.585, BLEND OUT REMAIN 0. 577. HFEC INSPECTION, FLUORESCENT PENETRANT INSPESDR CALA2016012895055Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, BETWEEN WS 1074 - 1101. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & 51-20-01. SKIN ORIGINAL THICKNESS 0.255, BLEND OUT REMAIN 0.246. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION SDR CALA2016012895056Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L10, BETWEEN WS 995 - 1021. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & 51-20-01. SKIN ORIGINAL THICKNESS 0.236, BLEND OUT REMAIN 0.232. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTIOSDR CALA2016012895057Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L14, BETWEEN WS 732 - 810. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.315, BLEND OUT REMAINING 0.305. HFEC INSPECTION, FLUORESCENT PENETRANT INSSDR CALA2016012895058Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, BETWEEN WS 678 - 732. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.377, BLEND OUT REMAIN 0.374. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTISDR CALA2016012595029Engine · oil consumptionDIRTY SOCK ODOR WHEN ACFT REACHED CRUISE, AFTER LEVEL OFF IN FLIGHT DECK & FIRST REAR CABIN, THEN IN FIRST CLASS, HAZE IN FLIGHT DECK WAS INCREASING. SHUT OFF THE UPPER RECIRC FAN & ODOR SEEMED TO INTENSIFY, THE UPPER WAS SELECTED BACK ON THEN THE LOWER WAS SSDR CALA2016012895062Engine · oil consumptionDIRTY SOCK ODOR WHEN ACFT REACHED CRUISE, AFTER LEVEL OFF, IN FLIGHT DECK & FIRST REAR CABIN, THEN IN FIRST CLASS. HAZE IN FLIGHT DECK WAS INCREASING. NR 1 ENG HAS OIL IN THE TAIL PIPE & 9 QTS OF OIL ADDED, HIGH OIL CONSUMPTION. REPLACED NR 1 ENG IAW AMM 71
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