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.

SDR WRLA2008027Nose Cowl · debondedDURING C-CHECK INSPECTION NR 3 ENGINE NOSE COWL INNER BARREL COMPOSITE DISBONDED. REF EGAT NR U02006. REPAIRED NR 3 ENGINE INLET COWL DISBONDED AREA IAW ERA 087123.Mar 11, 2008 · N380WA · Doug MD11F · Engine Cowling SystemSDR WRLA2008028Intercostal · crackedDURING C-CHECK INSPECTION CRACK FOUND LT WHEEL WELL UNDER WING BARREL KEEL STRUCTURE INTERCOSTAL. REF EGAT NR U05001. REPLADCED LT WHEELWELL UNDERWING BARREL KEEL STRUCTURE INTERCOSTAL PER MD11 SRM 51-35-01 VOL.II REV.40.Mar 11, 2008 · N380WA · Doug MD11F · Fuselage Miscellaneous StructureSDR WRLA2007135Solenoid · malfunctionedGEC 8282 EGNX/KJFK 12/15/2007 - INTENSE ODOR TOP OF CLIMB. DISCOVERED ODOR COMING FROM COCKPIT DOOR ELECTRIC LATCHING MECHANISM. BREAKER PULLED ODOR CEASED. REMOVED AND REPLACED DOOR ELECTRIC STRIKER ASSY PER MM 52-51-04.Dec 17, 2007 · N279WA · Doug MD11F · Fixed Inner DoorsSDR WRLA2007130Skin · debondedDURING C-CHECK INSPECTION FOUND LEFT OUTBOARD FLAP TRAILING EDGE OUTBOARD EDGE SKIN DISBOND 33 X 4.5 INCHES. REPAIRED DAMAGE AS PER EGAT EI NO.W2007A57B-710 REV.1 REF EGAT NRC U07001.Dec 1, 2007 · N803DE · Doug MD11 · Trailing Edge FlapsSDR WRLA2007132Trunnion · crackedDURING C-CHECK INSPECTION FOUND NOSE LANDING GEAR LEFT HAND TRUNNION FITTING CRACKED. REPAIRED LT NOSE LANDING GEAR FITTING PER MD11 SRM VOL.1 53-40-00 REV.40 REF EGAT NRC U05005.Dec 1, 2007 · N803DE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR WRLA2007131Door Frame · damagedDURING C-CHECK INSPECTION FOUND CENTER CARGO DOOR JAMB LOWER AFT EDGE DAMAGED. REPAIRED DAMAGE PER MD11 SRM 53-50-00 FIG.17 VIEW B REF WOA ERA 7-53-62.Dec 1, 2007 · N803DE · Doug MD11 · Fuselage Main, StructureSDR WRLA2007116Seat Track · damagedMAIN DECK CARGO SEAT TRACK DAMAGED STA Y=635 X=27.50. REPLACED SEAT TRACK REF SRM 53-70-00 FIG1 REV 40.Oct 28, 2007 · N380WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2007117Cargo Track · damagedMAIN DECK CARGO SEAT TRACK DAMAGED STA Y=635 X=47.50. REPLACED SEAT TRACK REF SRM 53-70-00 FIG 1 REV 40.Oct 28, 2007 · N380WA · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2007102Skin · crackedDURING 4C + 12A CHECK FOUND RIGHT WING FIXED L/E SKIN CRACK AT CORNERS OF CUTOUT L=0.3 INCH, AT STA XOS 464 L=0.5 INCH STA XOS 470. 10-25-07 REPAIRED THE RT WING FIXED LEADING EDGE SKIN CRACK AT CORNERS OF CUTOUT AT STA XOS=464,470 PER MD11 SRM VOL.I 57-Oct 5, 2007 · N273WA · Doug MD11 · Wing, Plate/SkinSDR WRLA2007103Ballast · failedEDDP/OKBK ROW 10 & 11 SEATS A, B & C OVERHEAD CEILING LIGHT ABOVE & BEHIND LUGGAGE BIN WAS HOT WITH BURNING PLASTIC ODOR LIGHT WAS DISCONNECTED. 10-18-07 R & R BALLAST.Oct 5, 2007 · N804DE · Doug MD11 · Passenger Compartment LightingSDR WRLA2007081Engine · overtempKBGR/EINN, IN CRUISE FLIGHT EXPERIENCED MODERATE VIBRATION FOLLOWED BY LEVEL 2 ALERT SELECT FADEC ALT NR 3. RETARDED THROTTLE HALF WAY & SELECTED NR 3 FADEC TO ALT. EGT CONTINUED TO RISE. IN FLIGHT ENGINE SHUT DOWN CHECKLIST WAS ACCOMPLISHED. EMERGENCY DECAug 9, 2007 · N803DE · Doug MD11 · Engine (Turbine/Turboprop)SDR WRLA2007080Structure · crackedDURING 1C+12A CHECK, EGAT MAINT FOUND CRACK ON LT WING ANTI-ICING TELESCOPING DUCT DOOR CUTOUT AT STA XOS=464 & XOS=470. CRACK REPAIRED PER MD-11 SRM VOL 1 57-10-00 FIG 43 REV 39 & EI 2006P20A-124 REV 00. (REPAIR DOUBLER)Aug 4, 2007 · N801DE · Doug MD11 · Wing Miscellaneous StructureSDR ASMF200707019Relay · cloggedAIRCRAFT RETURNED TO PLATFORM, AC CROSS TIE AND APU RT BUSS LIGHTS TURNED ON. BCU WAS REPLACED IAW MM 24-20-00 AND AC CROSS TIE LIGHT TURNED OFF, BUT RT BUSS LIGHT CONTINUED ON. RT BUSS LIGHT WAS DEFERRED BY MEL 24-1-1 AND AIRCRAFT WAS DISPATCHED. AFTER, AIRJul 29, 2007 · N838AM · Doug MD83 · Electrical Power SystemSDR UPS07M50341Handle · inoperativeLANDING GEAR HANDLE WILL NOT MOVE TO UP POSITION. PERFORMED CHECKLIST, GEAR WOULD NOT RETRACT. FOUND RT TRUCK BEAM ACT PRESS RELIEF VALVE AND ONE WAY RESTRICTOR FAILED. BOTH REPLACED IAW AMM 32-37-01 AND 04. ALSO REPLACED TWO-WAY RESTRICTOR AND TRIM ACTUATOJul 28, 2007 · N277UP · Doug MD11F · Landing Gear SelectorSDR WRLA2007079Oven · malfunctionedKBWI/LIMC FWD GALLEY OVENS MADE POPPING SOUND FOLLOWED BY ELECTRICAL SMELL WHILE COOKING. REMOVED POWER FROM OVENS BY PULLING C/B'S. RAN BOTH OVENS FOR ONE HOUR, BOTH OPERATED AS NORMAL IAW MM 25-31-50.Jul 9, 2007 · N801DE · Doug MD11 · Buffet/GalleysSDR WRLA2007077Fan · noisyFLIGHT 8400 FORWARD CHILLER FAN NOISY - POSSIBLE SOURCE OF ELECTRICAL BURNING ODOR . NR 2 RADAR UNIT (FWD E/E) VERY HOT, POSSIBLE SOURCE OF ELECTRICAL BURNING ODOR. CHECKED CHILLER FOR CHAFED WIRES OR DAMAGE, NONE FOUND. NO ELECTRICAL BURNING ODOR, BUT CHILJun 11, 2007 · N801DE · Doug MD11 · Buffet/GalleysSDR WRLA2007069Fan · failedFLIGHT 8011 KBAD/PHIK 05/25/07 - DURING CRUISE FLT350 ELECTRICAL FUMES REPORTED BY CABIN CREW IN A ZONE. COMPLIED WITH VOL 1 PROCEDURES. FUMES DISSIPATED WHEN CAB BUSS SWITCH SELECTED OFF. PAX REPORTED HIGH PITCHED NOISE FROM LEFT REAR WALL OF -A ZONE- UNKNMay 25, 2007 · N801DE · Doug MD11 · Air Distribution FanSDR WRLA2007054Unknown · smokeLAD/IAH AIR TURNBACK DUE TO FLIGHT CABIN CREW REPORTED ELECTRICAL SMOKE AFT OF L2 DOOR LT SIDE ROW 15AV CABINET, F/A'S ISOLATED ELECTRICAL AND ALL SMOKE DISSIPATED. RAN CHECKLIST AND RETURNED TO FNLU. AFTER DOING A SEARCH OF THE SUSPECTED AREA OF CABIN FROM Apr 5, 2007 · N803DE · Doug MD11 · Air Distribution SystemSDR WRLA2007037Stiffener · crackedDURING 3C + 12A CHECK, EGAT MECHANIC FOUND RIGHT WHEEL WELL DOOR OUTBOARD JAMB ASSY STIFFENER CRACK L =.06" AT STA Y = 1474. REF DRAWING ANS7203. REMOVED THE CRACKED STIFFENER AND INSTALLED NEW PARTS PER MD-11 SRM 51-35-01 VOL II REV 38. CONDITION CHECK NORFeb 15, 2007 · N380WA · Doug MD11 · Fuselage Miscellaneous StructureSDR WRLA2007036Blades · damagedJFK/BRU AIR TURNBACK DUE TO ENGINE VIBRATION HIGH ALERT ON NR 2 ENGINE AT 700 FT ON TAKEOFF NR 2 ENGINE COMPRESSOR READS 5.8 VIBRATION AND SOUND PRESENT. WHEN THROTTLE RETARDED VIBRATION CEASED. DUMPED FUEL AND RETURNED BACK FOR LANDING AT JFK. NR 2 ENGINE Feb 15, 2007 · N279 · Doug MD11F · Turbine Engine Compressor SectionSDR WRLA2007035Torque Box · crackedDURING 3C + 12A CHECK, EGAT MECHANIC FOUND ENG 2 LT TORQUE BOX LOWER SIDE CASCADE FWD RING CAP OUTER CRACK APPROX 1". REF CMM 78-32-35 PAGE 1021 ITEM 505.Feb 10, 2007 · N380WA · Doug MD11 · Engine (Turbine/Turboprop)SDR WRLA2007034Torque Box · crackedDURING 3C + 12A CHECK, EGAT MECHANIC FOUND ENG 2 RT TORQUE BOX LOWER SIDE CASCADE FWD RING CAP OUTER CRACK APPROX 1" AND DOOR AND CRACK ABOUT 1.5". REF CMM 78-32-35 PAGE 1007 ITEM 121 AND PAGE 1021 ITEM 505. PER ENGINEERING INSTRUCTION NO:W2007A78B-110 REV:00Feb 10, 2007 · N380WA · Doug MD11 · Engine (Turbine/Turboprop)SDR WRLA2007033Skin Panel · crackedFOUND NR 1 PYLON PRECOOLER TORQUE BOX SKIN PANEL GOUGE. PERFORM NR 1 PYLON PRECOOLER TORQUE BOX SIDE SKIN PANEL GOUGE AREA DOUBLER INSTALL REPAIR PER MD-11 SRM VOL 1, 54-00-01 FIG 3 REV:38.Feb 10, 2007 · N380WA · Doug MD11 · Nacelle/Pylon, Plate/SkinSDR WRLA2007032Skin · delaminatedDURING 3C + 12A CHECK, EGAT MECHANIC FOUND RIGHT OUTBOARD FLAP UPPER SURFACE TRAILING EDGE WEDGE IS DELAMINATED. REMOVE RT WING OUTBD FLAP WEDGE. PERFORM THE ENGINEERING INSTRUCTION NO.W2007A57B-095 REV.00, PAGE 1 OF 3 ITEM 1~7, PAGE 2 OF 3 ITEM 8~10. INSTAFeb 9, 2007 · N380WA · Doug MD11 · Trailing Edge FlapsSDR WRLA2007031Skin · debondedDURING 3C + 12A CHECK, EGAT MECHANIC FOUND LEFT WING OUTBOARD FLAP WEDGE INBOARD SIDE DISBOND ABOUT 4 INCHES. CHECK THE DAMAGE AREA AND CLEANUP. BONDED FIBERGLASS FABRIC USE WET LAYUP AT TEMP 160 DEGREE F, 90 MINS VACUUM;22 INCH/HG CURE PER MD11F SRM VOL 57-Feb 9, 2007 · N380WA · Doug MD11 · Trailing Edge FlapsSDR WRLA2007030Support · crackedDURING 3C + 12A CHECK, EGAT MECHANIC FOUND CRACK AT RIGHT W/W NR 3 HYD SYSTEM REGULATOR SUPPORT CRACK 2.5 INCHES. PERFORM RT WW NR 3 HYD SYSTEM REGULATOR INTERCOSTAL SUPPORT CRACK REPAIRED PER ENGINEERING INSTRUCTION NR W2007A53-094 REV:00 & EI NR W2006 P20A-Feb 8, 2007 · N380WA · Doug MD11 · Fuselage Main, Attach FittingsSDR WRLA2007029Structure · crackedDURING 3C & 12A CHECK, EGAT MECHANIC FOUND CRACK AT NR 3 AIR CONDITION COMPARTMENT DOOR UPPER SIDE CRACK 3". PERFORM NR 3 AIR CONDITION DOOR SKIN CRACK AREA REPAIR PER MD-11 SRM VOL 1 52-10-00 FIG.1 REV:38. CONDITION CHECK NORMAL AND JOB COMPLETED.Feb 8, 2007 · N380WA · Doug MD11 · Air Conditioning DoorsSDR WRLA2007039Panel · wornDURING 3C + 12A CHECK, EGAT MECHANIC FOUND WORN AT RIGHT WING INBOARD AILERON OUTBOARD FIXED PNL FWD ROW FASTENER HOLES STA XORS + 433 TO 480, REAR SPAR. PERFORM RIGHT WING INBOARD AILERON OUTBOARD FIXED PANEL REPAIRED PER ENGINEERING INSTRUCTION W2007A57B-09Feb 8, 2007 · N380WA · Doug MD11 · AileronsSDR WRLA2007038Bracket · crackedDURING 3C+12A CHECK, EGAT MECHANIC FOUND TAIL SECTION STA 2033-2122 TAIL FUEL SYSTEM HAVE BRACKET CRACK AND CLAMP CRACK. REPLACED TAIL FUEL SYSTEM BRACKET AND CLAMP PER AMM 20-05-02 900-801 REV 57.Feb 8, 2007 · N380WA · Doug MD11 · Aircraft Fuel Distribution SystemSDR WRLA2007027Rib · crackedDURING 3C & 12A CHECK, EGAT MECHANIC FOUND CRACK AT RT WING FIXED LE SLAT INTERNAL NO. 16 RIB APPROX 05". REMOVED RT WING NR 16 RIB, REPAIRED AREA, WIRE, CLAMP, PULLEY, TRACK AND CABLE PER T/C. REPLACED WITH NEW RIB AT RT WING NR 16 RIB PER MD-11 SRM 51-33-01 Feb 7, 2007 · N380WA · Doug MD11 · Wing, Rib/BulkheadSDR WRLA2007028Rib · crackedDURING 3C &12A CHECK, EGAT MECHANIC FOUND CRACK AT L/H WING FIXED L/E SLAT INTERNAL NO. 16 RIB APPROX 05". REMOVED LT WING NR 16 RIB & REPAIRED AREA, WIRE, CLAMP, PULLEY, TRACK AND CABLE PER NR 0028049, ITEM 1&2. REPLACED WITH NEW RIB AT LT WING NR 16 RIB PERFeb 7, 2007 · N380WA · Doug MD11 · Wing, Rib/BulkheadSDR DL76L070047Wire · chafedDURING BRAKE RELEASE WHILE PUSHING THROTTLES FORWARD AT APPROX 1.3 EPR, THE RIGHT ENG OIL PRESSURE LIGHT ILLUMINATED AND PRESSURE GAUGE READ AT APPROX 213PSI. IMMEDIATE ABORT PERFORMED. AT IDLE RIGHT ENG OIL PRESS IS NORMAL APPROX 106 PSI. R ENG OIL PRESS EJan 19, 2007 · N173DN · Boeing 767332 · Turbine Engine System WiringSDR WRLA2007001Longeron · corrodedDURING 2C+12A+150M CHECK, EGAT MAINT FOUND CORROSION AT STA 630 - STA 670 LONGERON R51. CUT AND FABRICATE REPAIR THE DAMAGED AREA PER MD-11F SRM 53-10-00 REV 38 FIG 1 & 2. CONDITION CHECK NORMAL.Jan 4, 2007 · N276WA · Doug MD11F · Fuselage Main, Longeron/StringerSDR WRLA2006105Skin Panel · dentedREF WOA ERA 06-05-013R1 (LT SIDE OF FUSELAGE DAMAGED AT FS 765 TO FS 791 STR 38L-39L.) EXA 06-15-013R1 TO INSTALL PERMANENT REPAIR (SECTION 3 OF ERA). REMOVED TEMPORARY REPAIR AND INSTALLED PERMANENT REPAIR IAW SRM.Nov 6, 2006 · N277WA · Doug MD11 · Fuselage Main, Plate/SkinSDR WRLA2006102Fan · inoperativeATL/LEJ DIVERSION TO BGR DUE TO VISIBLE FUMES AND SMOKE ODOR IN MID CABIN. CHECKED SIDEWALL LIGHTS & OVERHEAD LIGHTING, CHECKED PAX ENTERTAINMENT SYSTEM SEB, ODU'S NO FAULTS FOUND. CHECKED LAV FLUSH WATER HEATERS, ALL OK. FOUND ALL 3 PHASES C/B'S ON NR 3 RENov 4, 2006 · N801DE · Doug MD11 · Air Distribution FanSDR WRLA2006104Seat Track · corrodedDURING 4C+12A+150M CHECK IN TPE, FOUND CORROSION AT M/D CABIN SEAT TRACK STA 891 LT SIDE NR 2 SEAT TRACK. REPAIRED THE DAMAGED AREA FOR SEAT TRACK AT STA891 LT NR 2 SEAT TRACK PER MD-11 SRM 53-70-00 VOL.1 REV38 FIG 1. JOB COMPLETED AND CONDITION CHECK NORMAL.Nov 4, 2006 · N804DE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2006103Seat Track · corrodedDURING 4C+12A+150M CHECK IN TPE, FOUND CORROSION AT MID CABIN SEAT TRACK STA 891 LT SIDE NR 1 SEAT TRACK. REPAIRED THE DAMAGED AREA FOR SEAT TRACK AT STA 891 LT NR 1 SEAT TRACK PER MD-11 SRM 53-70-00 VOL 1 REV 38 FIG 1. JOB COMPLETED AND CONDITION CHECK NORMANov 3, 2006 · N804DE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS06M48250Indicator · malfunctionedINSPECTION TYPE: N/A EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST IND. SYS DOOR 1L LIGHT DOES NOT GO OFF. LIGHT ON DIM IN FLIGHT. PRESS-TO-TEST NORMAL ON GROUND. ON T/S FOUND LIGHT HOLDER INCORRECTLY SEATED. RESEATED LAMP HOLDER AND PERFORMED ADJ/TEST IAW Oct 14, 2006 · N275UP · Doug MD11F · Escape SlideSDR 06FDEA03190Case · chafedENG NR 1 FAN CASE AT AFT 1:00 POS FOUND WITH CHAFE MARK AT 8 PLACES (P/N 51G478). CHAFE MARK MEASURED AND FOUND 3 AREAS OUT OF LIMIT PER AMM 72-33-06-6. REFER TO E.A.1-7233-103553. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.Sep 5, 2006 · N521FE · Doug MD11 · Turbine Engine Compressor SectionSDR UPS06M47819Indication Sys · malfunctionedINSPECTION TYPE: N/A CABIN DOOR FWD L INDICATION STAYS ON AFTER DOOR IS CLOSED SECURED SLIDE COVER TO DOOR. OPS CKD DOOR. ALL INDICATIONS NORMALAug 28, 2006 · N273UP · Doug MD11F · Door Warning SystemSDR WRLA2006006Fan Blade · damagedDURING CLIMB, FLIGHT CREW NOTED FAN VIBRATION REACHED 3.2. AIRCRAFT RETURNED TO SNN (EINN). UPON ARRIVAL NR 2 ENGINE WAS INSPECTED. FAN INSPECTION FOUND MULTIPLE FAN BLADES AND EXIT GUIDE VANES DAMAGED DUE TO SUSPECTED FOREIGN OBJECT DAMAGE. R/R NR 2 ENG FAFeb 28, 2006 · N803 · Doug MD11F · Engine (Turbine/Turboprop)SDR 05FDEA04029Repair · noneSNRM N1460: FORWARD CARGO - STA 1079 LONGERON 27R FOUND WITH EXISTING REPAIR. REPAIR PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH MD11 SERVICE BULLETIN 53-042 R02. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. THIS IS NOT A REPORTABLE ISSUE. NO DEFECT OR MALFUNNov 30, 2005 · N524FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 05FDEA04030Repair · unknownSNRM N1608: REFERENCE TO EO 1-5100-7-5001 PT1 - FORWARD CARGO - STA 775 TO 795 LONGERON 27R FOUND WITH EXISTING REPAIR. FOUND REPAIR PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH MD11 SERVICE BULLETIN 53-042 R02. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. THNov 30, 2005 · N524FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 05FDEA04031Repair · unknownSNRM N1609: REFERENCE TO E1-5100-7-5001 PT1 - FORWARD CARGO - STA 839 TO 859 LONGERON 27R FOUND WITH EXISTING REPAIR. REPAIR PREVIOUSLY ACCOMPLISHED IN ACCORDANCE WITH MD11 SERVICE BULLETIN 53-042 R02. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. NARI, NO M ORNov 30, 2005 · N524FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 05FDEA04032Seat Track · corrodedSTA 859 LBL 8 SEAT TRACK FOUND CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-00.Nov 30, 2005 · N524FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA04028Skin · dentedSNRM N2641: CABIN - R4 DOOR EXTERIOR SKIN UPPER EDGE FOUND WITH DENT. CARRIED OUT REPAIR AS PER SRM 52-10-00.Nov 29, 2005 · N524FE · Doug MD11 · Service DoorsSDR 05FDEA04027Seat Track · corrodedFS 5-0 TO 1501 LBL 21 FOUND SEAT TRACK WITH CORROSION. REMOVED AS PER SRM 51-21-01. FOUND EXCEEDED LIMIT AS PER SRM 53-70-00. REMOVED AT EXISTING SPLICE AND TRIMMED AS PER SRM 53-70-00. NEW SEAT TRACK REWORKED AND INSTALLED AS PER SRM 53-70-00 VOLUME I. RENov 29, 2005 · N524FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR WRLA2005147Wire · damagedTPE/ANC AFTER 5HRS FLIGHT CAC FAN 2 C/B POPPED. AFTER LANDING AND ENGINE SHUTDOWN IN ANC CAC FAN 1 C/B POPPED. AFTER 7HRS 20MIN LEVEL 1 ALERT "AC TIE 1 OFF" APPEARED. CORRETIVE ACTION: UPON INITIAL INSPECTION FOUND AC BUS TIE RELAY OVERHEATED THE BUNDLE AND CANov 23, 2005 · N380 · Doug MD11F · Electrical Power System WiringSDR WRLA2005145Slide · deployedL1 DOOR SLIDE WAS INADVERTANTLY DEPLOYED; SLIDE DID NOT INFLATE BECAUSE THE BOARDING STAND WAS IN PLACE AND PREVENTED IT FROM DROPPING FAR ENOUGH TO ACTIVATE. REPACKED AND REPLACED SLIDE ON L1 DOOR PER AIRCRAFT MAINTENANCE MANUAL PRACTICES.Nov 2, 2005 · N381 · Doug MD11F · Escape SlideSDR UPS05M45539Bulb · burned outR1 DOOR EMERGENCY EXIT SIGN, HALF OF THE BULBS ARE BURNED OUT. RELAMPED, OPS CKS NORMAL IAW MM CH 33-50-00.Oct 2, 2005 · N279UP · Doug MD11F · Emergency Lighting
Back to Pratt & Whitney PW4460