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 IPXA10M61494Vane · damagedINSPECTION TYPE:2C, LT WING OTBD FLAP VANE OTBD LOWER EDGE HAS WEAR DAMAGE AND MISSING MATERIAL. REMOVED DAMAGE, FILLED AREA AND BONDED REPAIR PLIES IAW STA-SA EA 011-5750-01-A2559 I/R AND EO MD11-5750-38951-A.SDR IPXA10M61495Skin · crackedINSPECTION TYPE:2C, RT WING TELESCOPIC DUCT CUT-OUT CRACKED AT UPPER INBD AND OTBD CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW SRM 57-40-01, REPAIR 10, FIG 201, REV 43.SDR IPXA0M62001Skin · dentedINSPECTION TYPE:4C, DEFERED ITEM D-429361 RT FUS DENT AT STA 1868 AND L3R. REMOVED DAMAGE AT STA 1868 AND L3R. FABRICATED AND INSTALLED REPAIR REF SRM 53-00-01, REPAIR 1, FIG 201, CLASS 1 AND RCD 388368.SDR IPXA10M61224Skin · chafedINSPECTION TYPE:3C, LT ANTI-ICE TELESCOPIC DUCT L/E CUT OUT EXTERNAL DOUBLER CHAFED. REMOVED DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW STA SA EA 011-5730-01-A2545 EO MD11-5730-38820-A.SDR IPXA10M61243Vane · wornINSPECTION TYPE:3C, RT WING OTBD FLAP VANE, OTBD LOWER EDGE HAS AN AREA THAT IS WORN AND MISSING MATERIAL, VIEWED FROM BOTTOM. REMOVED DAMAGED AREA, ACCOMPLISHED WET LAY-UP REPAIR IAW STA SA EA 011-5753-01 I/R AND EO MD115750-38855-A.SDR IPXA10M61108Skin · crackedINSPECTION TYPE:2C, RT WING L/E EXTERIOR SKIN, ANTI-ICE TELESCOPIC DUCT CUT OUT AT APPROX WS XOS 464-470 HAS 2 EA CRACKS IN CORNERS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBER IAW SRM 57-40-01, REPAIR 10, FIG 201.SDR IPXA10M61104Rib · crackedINSPECTION TYPE:2C, RT WING FIXED L/E COMPARTMENT AT APPROX WW XOS 160 PANEL LANDING RIB CRACKED. REMOVED RIB, FABRICATED AND INSTALLED NEW RIB IAW DWG ARB1161.SDR IPXA10M60756Skin · dentedINSPECTION TYPE:1C, DEFERRED ITEM D 421851: L-1 CREW ENTRY DOOR SKIN UPPER EDGE REPAIR. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 52-10-01, REPAIR 3, FIG. 201.SDR IPXA0M60618Longeron Fitting · crackedINSPECTION TYPE:2C, LONGERON 46L SPLICE FITTING CRACKED BETWEEN STA 1522-1542. REMOVED, FABRICATED AND INSTALLED LONGERON SPLICE FITTING.SDR IPXA10M60656Floorbeam · corrodedINSPECTION TYPE:2C, AFT WASTE COMPARTMENT HAS CORROSION ON FLOORBEAM AND CUSP WEB AT INTERSECTION OF FLOORBEAM AT STA 1964 AND CUSP WEB LBL 75. REMOVED CORROSION IN LIMITS ON FLOORBEAM, REMOVED AND FABRICATED, AND INSTALLED WEB CUSP IAW SRM 51-31-01, 51-35-01SDR IPXA10M60018Skin · dentedFUSE SKIN DENTED STA 1964. REPAIRED IAW EO MD11-5330-36005.SDR IPXA10M60437Skin · chippedINSPECTION TYPE:1C, LT WING L/E FIXED COMPARTMENT TELESCOPIC DUCT CUT OUT EXISTING REPAIR (INBD SIDE) FOUND WITH EDGE CHIPPED OFF AS MARKED. REMOVED EXISTING REPAIR FROM LT WING FIXED L/E AT ANTI-ICE DUCT CUT OUT STA XOS464 TO XOS470. FABRICATED AND INSTALLESDR IPXA10M59900Skin · dentedDENT IN FUSELAGE AT AFT EDGE OF CTR CARGO DOOR CUT OUT DAMAGE CUTOUT IS 16.75" X 3.75". REPAIRED IAW EO MD11-5330-37075C.SDR IPXA10M60087Skin · damagedINSPECTION TYPE:2C, CREASE ON EXTERNAL SURFACE OF UPPER FUSELAGE SKIN, APPROX 12:00 POSITION APPROX. FUSELAGE STA 1580. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER, AND INTERNAL FINER DOUBLER IAW SRM 53-00-01, REPAIR 1, FIG 201.SDR IPXA10M60177Support · corrodedINSPECTION TYPE:4C, CORROSION EVIDENT UNDER AND AROUND LOCKBOLT AT FUSELAGE TO FRAME UNION AT LONGERON 27R, APPROX STA 1324. GAINED ACCESS TO AREA. R & R T-ANGLE REF SRM 51-33-01, SRM 51-35-01. RESTORED AREA.SDR IPXA10M60086Intercostal · crackedINSPECTION TYPE:2C INTERCOSTAL STIFFENER IN RT MLG WHEEWELL AFT CUTOUT, OTBD INTERIOR SECTION, 3RD FROM FRONT, IS CRACKED. REMOVED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL IAW SRM 51-35-01. P. 1-3.SDR IPXA10M59971Skin · crackedINSPECTION TYPE:2C, RT SLAT TRACK CUT OUT FOR NR 14 SLAT TRACK CRACKED LOWER OTBD CORNER. REMOVED DAMAGE AT RT NR 14 SLAT TRACK CUT OUT. FABRICATED AND INSTALLED REPAIR REF SRM 57-40-02, FIG 201, REPAIR 7.SDR IPXA10M60150Skin · crackedINSPECTION TYPE:2C, RT TELESCOPIC DUCT CUTOUT UPPER INBD CORNER IS CRACKED. ACCOMPLISHED REPAIR IAW EA 011-5730-01-A2325 I/R AND EO MD11-5730-37918-A.SDR IPXA10M59806Switch · inoperativeR1 DOOR SLIDE REWORK INDICATION SWITCH LIGHT REMOVED WITH UPPER DOOR LINING UNDER DEFERRED IAW MEL 25-61-2 DMP C/W. CONTROL NR M424413 ASSIGNED. R&R BATTERIES AND TESTED IAW MM 25-61-04-4. THIS CLEARS M424413. OPS CHECK GOOD.SDR IPXA10M59548Control Unit · inoperativeAFTER ABOUT 42 MINUTES OF FLIGHT TIME, LEVEL 1 EMERGENCY POWER ON DISPLAYED. TRIED TO RECYCLE EMERGENCY POWER SWITCH NO CHANGE. DUMPED 40,000 LBS FUEL FOR RETURN TO DEPARTURE. EPCU FAULT "ADG BATT CTL RLY/INTFC" INDICATED ON CFDS. CURRENT FAULTS, R & R EPCSDR IPXA10M59658Skin · crackedINSPECTION TYPE:2C, LT WING L/E SKIN AT TELESCOPIC DUCT CUTOUT UPPER INBD CORNER CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW 57-40-01 REPAIR 10, FIG. 201.SDR IPXA10M59693Skin · crackedINSPECTION TYPE:2C, LT WING L/E SKIN AT TELESCOPIC DUCT CUTOUT CRACKED AT UPPER IB CORNER GAINED ACCESS TO AREA, FABRICATED AND INSTALLED REPAIR REF SRM 57-40-01 FIG 201, REPAIR 10, RESTORED AREA.SDR IPXA10M59514Doubler · gougedINSPECTION TYPE:1C, RT WING CUTOUT AT ANTI-ICE DUCT STA XOS 464 AND STA XOS 470 L/E IS GOUGED. REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED NEW REPAIR IAW EA 011-5730-01-A2269, REV IR AND EO MD11 5730-37516-A.SDR IPXA10M59414Stud · brokenINSPECTION TYPE:1C, DURING REMOVAL OF LT OTBD AILERON FOUND OTBD AILERON ACTUATOR LOOSE AT UPPER AND LOWER INBD MOUNTING NUTS ON REAR SPAR FOUND UPPER INBD MOUNT STUD BROKEN AT LT OTBD AILERON ACTUATOR. REMOVED LT OTBD AILERON ACTUATOR REF AMM 27-13-30-4. SDR IPXA10M59511Skin · dentedINSPECTION TYPE:1C, LT INBD FLAP OUTER SKIN HAS A DENT ON OTBD WEDGE REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 011-5750-01-A2270 IR AND EO MD11-5750-37542-A.SDR IPXA10M59105Display · inoperativeDIVERSION - F/O'S MCDU SCREEN WENT BLANK, UNABLE TO RESTORE. DEFERRED D422762 ASSIGNED. SWAPPED NR 2 & NR3 IAW MM 31-65-01-4. NR 2 MCDU OPS CHECK NORMAL. TRANSFER NR 3 MCDU TO MEL 31-65-1-5 AND RTS PASSED.SDR IPXA10M59013Transmitter · inoperativeATB - IFSD - FUEL QTY/USED CHK LEVEL 2 CW QRH SHUTDOWN NR 2 ENG WINDMILL TIME 2 PLUS 15, 11 PSI OIL PRESSURE. PERFORMED SUPPLEMENT FAULT ISOLATION DATA 28-14-00-1. NO DEFECTS FOUND. R & R FUEL FLOW TRANSMITTER ON NR 2 ENG SEE LP 350089/1 & 2 FOR SIGN OFF ANDSDR IPXA10M58939Dimmer · burnedAT 1+20, INTO THE FLIGHT, CREW SMELLED STRONG ELECTRICAL SMELL IN COCKPIT. NOTICED ALL OVERHEAD LIGHTING (BACKLIGHT) WAS OUT AND COULD NOT RECOVER LIGHTING. AFTER 20 MIN SMELL WENT AWAY, NO LIGHTS. FOUND OVERHEAD LIGHTING DIMMER CONTROL U1-130 AT FAULT. RSDR IPXA10M58838Floor Panel · damagedMAIN DECK FLOOR PANEL AT STA 1751 RBL24 DAMAGED (DAMAGE IS ABOUT 36" FWD OF 12/13 SPLIT LINE). REPLACED FLOOR PANEL IAW MD11-5320-27386.SDR IPXA10M58621Duct · separatedWING ANTI ICE DISAGREE ALERT AT ROTATION WITH ENG WING AND TAIL ANTI ICE ON FOR TAKEOFF. ENG NR3 BLEED VALVE WOULD CLOSE AND NR3 PACK FLOW ALERT WOULD ILLUMINATE. FOUND RT WING TELESCOPE DUCT SEPARATED FROM WING DUCT DUE TO MISSING NUT. REPLACED ATTACHING HSDR IPXA10M58633Skin · misrepairedINSPECTION TYPE:4C, REPAIR SURVEY SEQ NR 279-W3-06 PREVIOUS REPAIR DOUBLER NOT IN SRM LT WING NR 4 SLAT APPROX BTWN STA XOS 559-570. REMOVED DOUBLER AND FILLER, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW STASA EA 011-5754-01-A2164 SDR IPXA10M58587Skin · corrodedINSPECTION TYPE:4C, RT FUSELAGE UNDER HORIZONTAL STAB HAS CORROSION AROUND FASTNER HOLES AND SKIN FROM STA 2033 TO 2160 CUTOUT DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53-70-01, REPAIR 3, FIG. 201.SDR IPXA10M58529Skin · crackedINSP TYPE:4C LT WING FIXED L/E TELESCOPIC DUCT CUTOUT CRACKED ON UPPER INBD AND OTBD CORNERS. CUT OUT DAMAGE AREA AND FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 57-40-01, REPAIR 10, FIGURE 201.SDR IPXA10M58530Skin · crackedINSP TYPE:C4, RT WING FIXED L/E TELESCOPING DUCT INBD AFT CUTOUT CRACKED AT CORNER. CUT OUT DAMAGED AREA FABRICATED DOUBLER AND FILLER AND INSTALLED IAW SRM 57-40-01, REPAIR 10, FIGURE 201.SDR IPXA10M58585Skin · gougedINSPECTION TYPE:4C, EXTERNAL FUSELAGE SKIN IS GOUGED FROM RUBBING ON FAIRING NR 154AB APPROX STA 1152. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLERS IAW STA SA EA 011-5330-01-A2167 I/R AND EO MD11-5330-36696-A.SDR IPXA10M58586Skin · misrepairedINSPECTION TYPE:4C, REPAIR SURVEY SEQUENCE NR 279-W3-01, NR 3 SLAT L/E SKIN HAS (I EA) FLUSH REPAIR BTWN STA XOS 419 AND XOS 429. REPAIR DOES NOT CORRELATE TO SRM 57-10-00 VOL I, FIG 35. RADIUS IS .500" TYP. SHOULD BE 1.0" REMOVED DOUBLER, INCREASED TRIM SDR IPXA10M58619Skin · delaminatedINSPECTION TYPE:4C, REPAIR SURVEY SEQUENCE NR 279-52-01 AT RT INBD DETACHABLE ELEVATOR ON LOWER INBD END BETWEEN STA XE 61.56 AND XE 73.56 REPAIR IS DELAMINATED WITH FABRIC EXPOSED. REMOVED PREVIOUS REPAIR AND DAMAGED AREA. BONDED REPAIR PLIES IAW SRM 55-20-8SDR IPXA09M57983Oil System · low pressureNR 2 ENGINE IFSD DUE TO LOW OIL PRESSURE. CREW DECLARED AN EMERGENCY. A/C IS OOS FOR ENGINE CHANGE. R & R NR 2 ENGINE REF TC NO 9130. OPS AND LEAK CHECK OK PER TC 9103SDR WRLA2009195Engine · failedDURING CLIMBOUT, NR 1 ENGINE FAILED CAUSING DAMAGE TO THE LEFT INBOARD AILERON AND LEFT OUTBOARD HORIZONTAL STABILIZER LEADING EDGE. REPLACED NR 1 ENGINE, LEFT INBOARD AILERON, AND LEFT OUTBOARD SECTION OF THE HORIZONTAL STABILIZER LEADING EDGE.SDR IPXA09M56338Engine · vibrationINSPECTION TYPE:N/A LEVEL 1 ENG 1 VIB HI DURING CLIMB FOR 5 MIN. TURB 4.7 ALERT DISAPPEARED AT LEVEL OFF FL360. WITHIN FEW MINUTES AFTER LEVEL OFF, ENG 1 SURGE WITH ENG 1 HI VIB, EGT INCREASED. SMELLED SMOKE/OIL SMELL. SHUT DOWN NR 1 ENG ATB. REMOVED AND RESDR UPS08M53826Engine · overtempAT 2600FT NR 2 ENGINE EGT CLIMBED TO 668 DEGREES FOR 30 SECONDS. VIBRATION FELT IN THE AIRFRAME. PERFORMED ENG OPERATIONAL OVERLIMITS INSPECTION AFTER EGT OVERTEMP IAW AMM 70-00-04-6-2. NO PHYSICAL DAMAGE NOTED. RAN ENGINE AT FLIGHT IDLE, ALL PATAMETERS CHECSDR WRL2008F00005Fitting · corrodedDURING LANDING GEAR REPLACEMENT, MAINT FOUND CORROSION ON CENTER LANDING GEAR LT PILLOW BLOCK AFT UPPER SURFACE OF PILLOW BLOCK AFT BOLT HOLE CORRODED. REWORKED AREA IAW SRM 53-40-00 FIG 16 IAW SERVICE REQUEST ID 1-8801879663.(K)SDR UPS08M52499Oil System · overtempATB - NR 2 ENGINE OIL TEMP WENT TO 175C AFTER TAKEOFF. RAN CHECKLIST WITH NR 2 ENGINE AT IDLE, OIL TEMP WAS 122C (ENG OIL TEMP HI MSG). OIL TEMP WAS IN CAUTION ZONE FOR APPROXIMATELY 3 MINUTES. REFER FIM 79-00-03-02 FIG 105 NO FAULT MSG FOUND. OIL TEMP PEASDR WRLA2008040Hinge Fitting · crackedDURING C-CHECK INSPECTION FOUND LEFT OUTBOARD FLAP CENTER BOX INBOARD AFT HINGE SUPPORT FITTING CRACKED. REMOVED AND REPLACED HINGE WITH NEW PARTS IAW MD11 SRM VOL.II 51-33-01 REV.40SDR WRLA2008032Stiffener · crackedDURING C-CHECK INSPECTION FOUND FLOORBEAM SUPPORT 5 EA STIFFENERS CRACKED STA Y=1841 X=-9.5, X=26, X=30.5, X=38, X=-38. REPLACED STIFFENERS PER MD11 SRM 51-35-01 VOL II REV 40.SDR UPS08M52614Frame · chafedINSP TYPE-C, FWD TAILCONE ACCESS CUT OUT LT FRAME, FOUND CHAFED MARK ON PREVIOUS REPAIR. FWD TAILCONE UPPER FWD DOOR OPENING MECH ASSY REMOVED FOR ACCESS. CHAFE MARK FOUND OUT OF LIMIT & REMOVED IAW SRM 51-31-01 VII R35. FAB NEW FWD TAILCONE FRAME WITH HEATSDR UPS08M52613Skin · crackedINSPECTION TYPE-C, CENTER CARGO DOOR CUTOUT, FOUND PREVIOUS REPAIR DOUBLER AT LOWER AFT EDGE CRACKED AND WITH NON STANDARD FASTENERS AS MARKED. CENTER CARGO DOOR CUTOUT-LOWER AFT SIDE HEATING TUBE REMOVED. PREVIOUS REPAIR DOUBLER REMOVED. SKIN TRIMMED & PROTESDR WRLA2008031Flap · debondedDURING C-CHECK INSPECTION FOUND RIGHT WING INBOARD FLAP DISBONDED. REF EGAT NRC U07003. REPAIRED PER ENGINEERING INSTRUCTION NO.W2008A57B-202 REV.00SDR WRLA2008041Shear Tie · crackedDURING C-CHECK INSPECTION FOUND LT INTERNAL FLAP SUPPORT SHEAR CLIP CRACKED AT STA Y=1521. FABRICATE SHEAR CLIP IAW ENGINEERING INSTRUCTION W2008P53B-226 REV 00. REF EGAT NR U05012.SDR WRLA2008029Seat Track · crackedDURING C-CHECK INSPECTION, MAIN DECK FLOOR PANEL SUPPORT CRACKED STA Y=635 X=8.5 X=27.5. PERFORM MAIN DECK FLOOR SUPPORT SEAT TRACK REPAIR PER MD11 SRM VOL.III 53-70-00 FIG.1 REV.40.
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