Pratt & Whitney PW4462

Service difficulty reports · 778

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 = 'PW4462'
  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.

SDR WRLA20090926245Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CENTER CARGO , L=2, STA 5-123 , L50R. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1133 REV 00. INSTALLED NEW LONGERONSep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/StringerSDR WRLA20090926248Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CENTER CARGO , L=1, STA 5-123 , L34L. REMOVED DAMAGE LONGERON SPLICE IAW SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1130 REV 00. INSTALL NEW LONGERON SPLICE Sep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/StringerSDR WRLA20090926249Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CENTER CARGO , L=2, STA 5-123 , L38L. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1131 REV 00. INSTALL NEW LONGERON SSep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/StringerSDR WRLA20090926250Longeron Splice · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LONGERON SPLICE FTG , CENTER CARGO , L=3, STA 5-123 , L51L. REMOVED DAMAGE LONGERON SPLICE IAW MD-11 SRM 51-33-01 REV 41. FABRICATE NEW LONGERON SPLICE IAW EI NR W2009P53B-1132 REV00. INSTALL NEW LONGERON SPSep 26, 2009 · N271WA · Doug MD11 · Fuselage Main, Longeron/StringerSDR WRLA20090926216Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1870, X=-75.25. REPAIR THE SEAT TRACK IAW SRM 53-00-52 REPAIR REV 41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926218Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 6-30, X=8.5. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR REV41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926223Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1239-1250, X=-107.25. REPAIRED THE SEAT TRACK IAW SRM 53-00-52 RPR 1 REV41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926229Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 909-929, X=107.25. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR REV41. APPLY PROTECTION COATING IAW MD-11 SRM 52-21-01 REV41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926230Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 532-559, X=73. REPAIRED THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR1 REV41. APPLY PROTECTION COATING MD-11 SRM 51-21-01 REV41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926234Beam · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LT WING FIXED INNER T/E LOWER BEAM, STA XW200,L=14 . JOB COMPLETED IAW EI NR W2009A57B-1122 REV00 AND REV01.Sep 26, 2009 · N271WA · Doug MD11 · Wing Main, Frame StructureSDR WRLA20090926222Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1121-1127, X=-75.25. REPAIR THE SEAT TRACK IAW SRM 53-00-52 RPR REV 41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV 41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926224Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK AT STA 1249, X=107.25. REPAIR THE SEAT TRACK IAW MD-11 SRM 53-00-52 RPR REV 41. APPLY PROTECTION COATING IAW MD-11 SRM 51-21-01 REV 41.Sep 26, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090926246Skin · delaminatedDURING 2C CHECK, EGAT MECHANIC FOUND DISBOND ON THE RIGHT WING INBOARD FLAP VANE LOWER SKIN DISBOND 12 *19 AT XIFH210. REMOVED RIGHT WING INBOARD FLAP VANE (J/C ATTACHING SHEET NR 088958 ITEM 01). REPAIRED THE DISBOND DAMAGE AREA IAW EGAT EI NR W2009A57B-113Sep 26, 2009 · N271WA · Doug MD11 · Trailing Edge FlapsSDR WRLA20090926247Skin · delaminatedDURING 2C CHECK, EGAT MECHANIC FOUND DISBOND ON THE LEFT WING INBOARD FLAP VANE LOWER SKIN DISBOND (7 *17 ) AT XIFH 192. CUT OUT DENT SKIN SANDED AROUND THE AREA AND CLEAN BONDED FIBERGLASS FABRIC USE WET LAY-UP AT 200 OF CURE FOR 220 MINS WITH VACUUM PRESSURSep 26, 2009 · N271WA · Doug MD11 · Trailing Edge FlapsSDR WRLA20090919208Seat Track · corrodedDURING 2C CHECK, EGAT MECHANIC FOUND CORROSION ON M/D SEAT TRACK BETWEEN STA 1351 AND STA 1361, X=107.25. REPAIR THE SEAT TRACK IAW SRM 53-00-52 RPR 1 REV 41. APPLY PROTECTION COATING IAW SRM 51-21-01 REV41.Sep 19, 2009 · N271WA · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA20090918205Skin · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK WITH FASTENER HOLE WORN OUT ON INBD/OUTBD SKIN (P/N: AUB7562-5 AND AUB7652-6) OF NR 3 PYLON FWD FAIRING. PERFORM EI W2009A54B-1109, REV 00 TO REPAIR THE DAMAGED AREA.Sep 18, 2009 · N271WA · Doug MD11 · Nacelle/Pylon, Plate/SkinSDR FDEA200909173312Shear Tie · corrodedAFT CARGO COMPARTMENT - STA 1953 FROM LONGERON 50 LT TO LONGERON 49 RT FRAME SHEAR CLIP FOUND CORROSION. REPAIRED IAW SRM 51-31-01 REV 41.Sep 17, 2009 · N522FE · Doug MD11F · Fuselage Internal Mounting StructureSDR WRLA20090917204Fitting · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON NLG TRUNNION SUPPORT FITTING, Y=582, X=24. CRACK LENGTH MEASURED 1 INCH. REPAIR THE NLG TRUNNION SUPPORT FITTING IAW MD-11 SRM 53-10-14 FIGURE 202, REPAIR 2, REV 41.Sep 17, 2009 · N271WA · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR WRLA20090917201Doubler · crackedCRACK - DURING 2C CHECK, EGAT MECHANIC FOUND THE STIFFENER DOUBLER AT THE CENTER GEAR W/W WEB Y:1382, X:+31.50 HAS CRACKED FROM THE FASTENER AREA (LEFT STIFFENER). ACCORDING TO EI W2009A53B-1114 REV 00 TO FABRICATE REPAIR PARTS. REINSTALL FASTENERS PER MD-11Sep 17, 2009 · N271WA · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA20090917202Doubler · crackedCRACK - DURING 2C CHECK, EGAT MECHANIC FOUND THE STIFFENER DOUBLER AT THE CENTER GEAR W/W WEB Y:1381, X:-31.50 HAS CRACKED FROM THE FASTENER AREA (RIGHT STIFFENER). ACCORDING TO EI W2009A53B-1115 REV 00 TO FABRICATE REPAIR PARTS. RE-INSTALLED FASTENERS PER MSep 17, 2009 · N271WA · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA20090917203Skin Panel · crackedDURING 2C CHECK, EGAT MECHANIC FOUND SKIN BULGE ON RT NOSE FUSELAGE UPPER, STA 275, X=-10. INSTALLED SKIN REPAIR IAW EI W2009A53B-1120 REV 00.Sep 17, 2009 · N271WA · Doug MD11 · Fuselage Main, Plate/SkinSDR WRLA20090916199Rib · crackedDURING 2C CHECK, EGAT MECHANIC FOUND THE STOP RIB AT THE L/E (XOVH 537) OF RIGHT OUTBOARD T/E FLAP CRACK. ACCOMPLISH E.I NO:W2009A57B-1092, REV 00 AND E.I NR :W2009A57B-1207 REV 00.Sep 16, 2009 · N271WA · Doug MD11 · Trailing Edge FlapsSDR WRLA20090916200Rib · crackedDURING 2C CHECK, EGAT MECHANIC FOUND THE STOP RIB AT THE L/E (XOVH 537) OF LEFT OUTBOARD T/E FLAP CRACK. ACCOMPLISH EI NR:W2009A57B-1093, REV 00 AND EI NR:W2009A57B-1205.Sep 16, 2009 · N271WA · Doug MD11 · Trailing Edge FlapsSDR FDEA200909063263Skin · corrodedLT WING UPPER SKIN AT STA, XORS 130 TO XORS 197 FOUND CORROSIONS. REPAIR IAW EA 1-5710-132213 TITLE: "WINGS-LT WING UPPER SKIN SURFACE CORROSION - REPAIR"Sep 6, 2009 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200909043258Skin · corrodedLEFT STA 1229 XCW= 97 TO XCW= 107 CTR WING UPPER PANEL FOUND CORROSION. REPAIRED IAW EA 1-5710-133850. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 107.Sep 4, 2009 · N521FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200908253085Hinge Bracket · corrodedRT WING - WING SIDE OTBD FLAP OTBD HINGE LWR MOUNT OTBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-132208 (MAJOR REPAIR).Aug 25, 2009 · N580FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200908243080Cargo Track · crackedCRACKED LOWER FLANGE OF FLOOR TRACK AT LT STA 755, X=27.5 IN MAIN DECK CARGO. REPAIRED AS PER SRM53-00-52 FIG201 REPAIR1 REV41 (MAJOR REPAIR).Aug 24, 2009 · N580FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200908233072Longeron Splice · crackedAFT CABIN RT SIDE AT APPROX STA 5-123, LONGERON 12 RT FOUND LONGERON SPLICE CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01, REVISION 41. NEW LONGERON SPLICE MACHINE IAW DWG A5A7112, REVISION D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 107.Aug 23, 2009 · N525FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR WRLA20090819198Pump · leakingDURING CLIMBOUT, NR 3 ENGINE LT EDP INDICATED OVERTEMP. ONE HOUR AFTER DEPARTURE, NR 3 ENGINE RT EDP INDICATED OVERTEMP. ONE HOUR FIFTEEN MINUTES AFTER DEPARTURE NR 3 HYDRAULIC SYSTEM INDICATED 0 HYDRAULIC FLUID QUANTITY. DIVERTED TO LEJ (EDDP) FOR MAINTENAAug 19, 2009 · N274WA · Doug MD11F · Hydraulic Pump (Electric/Engine), MainSDR WRLA20090814255Skin · damagedTHE RT DETACHABLE ELEVATOR WAS DAMAGED DUE TO CONTACT WITH GROUND EQUIPMENT. THE UPPER AND LOWER SKINS WERE DAMAGED ON THE TRAILING EDGE. THE INBD CORNER WAS CRACKED AND WAS REMOVED THROUGH ALL PLIES. IN ADDITION, THE INNERMOST PLY OF THE OUTER SKIN IS DAMAAug 14, 2009 · N271WA · Doug MD11 · Elevator, Plate/SkinSDR WRLA20090810196Skin · damagedDAMAGE TO THE FUSELAGE SKIN AT THE FORWARD LOWER CORNER OF THE UPPER CARGO DOOR CUTOUT. REPAIRED IN ACCORDANCE WITH WOA ERA 09-53-103.Aug 10, 2009 · N275WA · Doug MD11F · Fuselage Main, Plate/SkinSDR WRLA2009189Engine · vibrationNR 1 ENGINE HI VIBRATION/LOW RPM IN INITIAL CLIMB OUT. HIGH EGT 917C. DURING SHUTDOWN ENGINE FIRE AGENT DISCHARGED.Jul 13, 2009 · N277WA · Doug MD11 · Engine (Turbine/Turboprop)SDR WRLA2009119Seat Track · corrodedDURING "C" CHECK INSPECTION FOUND MAIN DECK CARGO CABIN SEAT TRACK CORROSION AND WEAR ON STA 1847-1884 AND X=47.5. CUT OUT SEAT TRACK FROM Y= 1831 TO 1887 AT X= 47.5 AND REPAIRED SEAT TRACK IAW MD-11 SRM 53-70-00 VOL 1 REV 40 FIG 1. JOB COMPLETED AND CONDITIMay 12, 2009 · N276WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2009120Seat Track · corrodedDURING "C" CHECK INSPECTION IN TPE, FOUND CORROSION ON MAIN DECK SEAT TRACK FLOOR PANEL SUPPORT AREA AT STA 976 AND X=8.5. CUT OUT SEAT TRACK FROM Y= 919 TO 985 AT X= 8.5 AND REPAIRED SEAT TRACK IAW SRM 53-70-00 VOL 1 REV 40 FIG 1. JOB COMPLETED AND CONDITIOMay 12, 2009 · N276WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2009121Seat Track · corrodedDURING "C" CHECK INSPECTION IN TPE FOUND MAIN DECK SEAT TRACK CRACK ON STA 1832 AND X=8.5. CUT OUT SEAT TRACK FROM Y= 1731 TO 1832 AT X= 8.5 AND REPAIRED SEAT TRACK IAW SRM 53-70-00 VOL 1 REV 40 FIG 1. JOB COMPLETED AND CONDITION CHECK NORMAL.May 12, 2009 · N276WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2009122Seat Track · corrodedDURING "C" CHECK INSPECTION IN TPE, FOUND MAIN DECK CABIN SEAT TRACK CORROSION AND WEAR ON STA 1776-1811 AND X=-8.5. CUT OUT SEAT TRACK FROM Y= 1731 TO 1811 AT X= -8.5 AND REPAIRED SEAT TRACK IAW SRM 53-70-00 VOL 1 REV 40 FIG 1. JOB COMPLETED AND CONDITION May 12, 2009 · N276WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2009123Seat Track · corrodedDURING "C" CHECK INSPECTION FOUND MAIN DECK CABIN SEAT TRACK CORROSION AND WEAR ON STA 1787 - 1682 AND X=8.5. CUT OUT SEAT TRACK FROM Y= 1682 TO 1707 AT X= 8.5 AND REPAIRED SEAT TRACK IAW SRM 53-70-00 VOL 1 REV 40 FIG 1. JOB COMPLETED AND CONDITION CHECK NORMay 12, 2009 · N276WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200903291096Engine · power lossENG NR 3 FLAMED OUT IN FLIGHT. FL 320. LOUD BANG & SHUDDER WITH HIGH EGT INDICATION. DUMPED 59K LBS OF FUEL. LOUD COMPRESSOR STALL SOUND AND LOOKS LIKE EGT WENT TO 680 DEG C. ENGINE APPEARED TO ROLL BACK. HE CONSIDERED A RESTART BUT HIGH EGT PROMPTED SHUTDOWMar 29, 2009 · N529FE · Doug MD11F · Engine (Turbine/Turboprop)SDR FDEA200903251036Pump · failedNR 3 ENG FLAME OUT DURING DESCENT, 280KTS/13000. PERFORMED LEVEL 3 ENG RPM LOW CHECKLIST, FOLLOWED BY ENG RESTART IN FLIGHT CHECKLIST, GOOD RESTART 10000/270 KTS. CKD ALL DEU AND FADEC NO FAULT SHOWN, INSP INLET & EXHUAST, CORE AREA NO DEFECT NOTED, R & R Mar 25, 2009 · N528FE · Doug MD11F · Engine Fuel PumpSDR WRLA2009011Rib · crackedDURING A04 CHK, LT WING INBOARD SLAT FILLET CHAFING AT WING FUSELAGE FAIRING. SLAT I/B RIB CRACKED & FAIRING RIB CRACKED. REMOVED AND REPLACED NR 1 SLAT.Jan 18, 2009 · N274 · Doug MD11F · Leading Edge DevicesSDR FDEA200901150208Unknown · vibrationAFTER TAKEOFF PASSING 13000 FT IN CLIMB PWR NR 1 ENG STARTED VIBRATING. AT LEVEL OFF PULLED NR 1 THROTTLE TO IDLE AND WHEN PASSING BELOW 80 PERCENT N1 VIBRATION WENT DOWN SIGNIFICANTLY AND AT IDLE NO VIBRATION NOTED. KEPT THROTTLE BELOW 80 PERCENT TO REMAINDJan 15, 2009 · N621FE · Doug MD11F · Engine (Turbine/Turboprop)SDR WRLA2009007Mount · corrodedNR 3 ENG MOUNT ISOLATOR, INSIDE FAN CASE, HAS RED POWDERY SUBSTANCE DRIPPING OUT ONTO COMPRESSOR, A-07 CHECK. REMOVED NR 3 ENG FWD MOUNT ISOLATOR IAW MM 71-00-39 PW ENG MANUAL. INSP, OK TO INSTALL. 01-09-09 REPLACED MOUNT WITH SERVICEABLE MOUNT IAW ENG MANUAJan 9, 2009 · N276WA · Doug MD11 · Engine (Turbine/Turboprop)SDR WRLA2009001Engine · defectiveIN CRUISE RECEIVED A LVL 2 ENG 2 OIL FILTER ALERT. NOTICED INCREASING EVM COMP INDICATION AND RECIEVED A LVL 1 ENG 2 VIB HI ALERT. LATER MODERATE A/C VIB NOTICED, EVM COMP OF 5.0, A LVL 2 SEL FADEC ALT ALERT AND A DROP IN N1 OF NR 2 ENG COMPLETED IFSD PROCEDURJan 1, 2009 · N272WA · Doug MD11 · Engine (Turbine/Turboprop)SDR WRLA2008073Skin · corrodedDURING INSPECTION FOUND FUSELAGE SKIN AND REINFORCING DOUBLER CORRODED AT AFT LAV EXHAUST PORT STA 1959 BETWEEN LONGERONS LS9R AND L40R. CORRECTIVE ACTION: REF. DELTA ERA 47026114 REMOVED DAMAGED AREA, PERFORMED HF EDDY CURRENT INSPECTION AS REQUIRED, FABRICAAug 26, 2008 · N272WA · Doug MD11 · Fuselage Main, Plate/SkinSDR WRLA2008071Doubler · crackedCENTER MLG WW RT BULKHEAD CUTOUT DOUBLER CRACKED AT RT FWD CORNER.Aug 22, 2008 · N277WA · Doug MD11 · Fuselage Main, BulkheadSDR WRLA2008070Doubler · crackedDURING INSPECTION FOUND CRACK ON CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD LT & RT AROUND LATERAL CONTROL MIXER. CORRECTIVE ACTION: INSTALLED ANGLE REF ROD SKETCH 91-09-09-002.Aug 22, 2008 · N279WA · Doug MD11F · Fuselage Miscellaneous StructureSDR WRLA2008068ADoubler · crackedDURING A CHECK INSPECTION SR TECHNICS, CRACKS FOUND ON CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD LT SIDE AROUND LATERAL CONTROL MIXER DOUBLERS. REPAIRED PER WORLD AIRWAYS ENGINEERING REPAIR AUTHORIZTION DOCUMENT 08-53-73. (S)Aug 20, 2008 · N274WA · Doug MD11F · Fuselage Main, StructureSDR WRLA2008069ADoubler · crackedDURING INSPECTION FOUND CRACK ON CLG WHEEL WELL LT AND RT DOUBLER AT Y=1381, X=31.5 AND -31.5. REPAIRED CRACK AREA IAW EI W2008A53B-761 REV.00. JOB COMPLETED AND CONDITION CHECK NORMAL. (S)Aug 20, 2008 · N275WA · Doug MD11F · Fuselage Main, StructureSDR WRLA2008066Seat Track · crackedDURING "C" CHECK INSPECTION IN TPE FOUND CRACK IN THE MAIN DECK SEAT TRACK AT Y=760, X=47.5. (S)Aug 5, 2008 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2008067Seat Track · crackedDURING INSPECTION FOUND MAIN DECK CARGO SEAT TRACK CRACK AT Y=760, X=47.6. REPAIRED CRACK SET TRACK IAW MD-11SRM VOL 1 53-70-00 REV 40. JOB COMPLETED AND CONDITION CHECK NORMAL. (S)Aug 5, 2008 · N275WA · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
Back to Pratt & Whitney PW4462