Boeing 747-281F

Service difficulty reports · 52

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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 aircraft_model_key = '747281F'
  ORDER BY difficulty_date DESC"

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SDR Q2SA20120930197Battery Pack · dischargedEMERGENCY FLOOR LIGHTING IN UPPER DECK INOP. REMOVED AND REPLACED BATTERY PACK CARTRIDGE IAW 3-51-04. SYS OPS CHECK NORMAL.Sep 30, 2012 · N783SA · Boeing 747281F · Emergency LightingSDR Q2SA201209301Battery Pack · defectiveEMERGENCY LIGHT IN THE COCKPIT INTERMITTENT. REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSY IAW 33-51-07. SYSTEM OPS CHECK NORMAL.Sep 30, 2012 · N783SA · Boeing 747281F · Emergency LightingSDR Q2SA2012091178305Generator · failedWHILE EN ROUTE FROM MIA TO ANC EXPERIENCED A NR 1 AND NR 3 GENERATOR FAILURE. THEREAFTER DISPATCH WAS NOTIFIED BY THE CREW, THE AIRCRAFT HAD LOST A THIRD GENERATOR. SHORTLY AFTER THAT THEY LOST THE FOURTH AND FINAL AIRCRAFT GENERATOR JUST BEFORE LANDING. THSep 11, 2012 · N783SA · Boeing 747281F · AC Generator-AlternatorSDR Q2SA2012072875813Skin · failedDURING POST-FLIGHT, FOUND A HOLE AND CRACK DAMGE AT SECTION 48 LH SIDE BETWEEN STATION 2638 AND 2658 AND S-11L AND S-13L. STRINGER (P/N 65B 02976-1) CHORD (P/N 65B02515-113) AND ANGLE (P/N 65B02712-139) ASSEMBLIES WERE FOUND TO BE DAMAGED BEYOND ALLOWABLE LIMIJul 28, 2012 · N758SA · Boeing 747281F · Fuselage Main, Plate/SkinSDR TX9Y20111214011Cargo Track · crackedFORWARD CARGO TRACK FORWARD RIGHT CORNER WAS FOUND CRACKED. REPAIRED AS PER SRM 53-10-05 FIG 5 REV 120.Dec 11, 2011 · N758SA · Boeing 747281F · Fuselage, Seat/Cargo Attach FittingsSDR TX9Y20111208008Structure · corrodedLT WING T/E INBOARD MID FLAP T/E LOWER CHORD WAS FOUND CORROSION. THREE CORROSION AREAS WERE FOUND ON LEFT T/E INBOARD MID FLAP (P/N:65B02025-35) T/E LOWER CHORD (P/N:65B02098-1) HORIZONTAL FLANGE LOWER SURFACE. THE REPAIR WAS CARRIED OUT PER BOEING MESSAGE Dec 7, 2011 · N758SA · Boeing 747281F · Trailing Edge FlapsSDR TX9Y20111208009Mount · corrodedNR 4 ENG AFTER UPPER ENG MOUNT UPPER SURFACE WAS FOUND RUSTED HEAVILY. NR 4 ENGINE AFTER ENGINE MOUNT WAS REPLACED AS PER AMM 71-21-03 REV 86.Dec 7, 2011 · N758SA · Boeing 747281F · Engine Mount SectionSDR TX9Y20111208010Skin · crackedDURING REMOVING TWO ADDITIONAL DOUBLERS, THREE HOLE CRACK ON THE LEFT DOUBLER FUSELAGE SKIN AND TWO HOLE CRACK ON THE RIGHT DOUBLER FUSELAGE SKIN WERE FOUND. FOR EXISTING REPAIR DOUBLERS WHICH COMMON TO NOSE WHEEL WELL AFTER CORNER SKIN BETWEEN STA 400 TO STADec 7, 2011 · N758SA · Boeing 747281F · Fuselage Main, Plate/SkinSDR TX9Y20111207007Longeron · crackedDURING INSPECTION OF NR 3 ENGINE RT SIDE COWL, ONE CRACK AND ONE DEEP CHAFING DAMAGE WERE FOUND AT LOWER LONGERON (P/N:65B94280-199). THE REPAIR WAS PERFORMED AS PER BOEING MESSAGE NUMBER TEC-SOF-11-0102.Dec 5, 2011 · N758SA · Boeing 747281F · Engine Cowling SystemSDR TX9Y20111206004Skin · dentedFUSELAGE SKIN (STA2200-STA2400,STR27-STR28) WAS FOUND ONE ORIGINAL REPAIR RIVET AND DENT. FUSELAGE SKIN DOUBLER WAS REPAIRED AS PER SRM 53-30-03 FIG 4 REV 120.Dec 4, 2011 · N758SA · Boeing 747281F · Fuselage Main, Plate/SkinSDR TX9Y20111205003Failsafe · corrodedDURING DATUM AIRCRAFT INPUT,A CORROSION (SIZE ABOUT:3.3"*0.8") WAS FOUND ON BULK CARGO FRAME LOWER LOBE FAIL SAFE CHORD (P/N:65B04347-149,STA2200) HORIZONTAL FLANGE AT STR 40R. THE REPAIR WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0099. THE REPAIR WADec 3, 2011 · N758SA · Boeing 747281F · Fuselage Main, FrameSDR TX9Y20111202001Skin · dentedBULK CARGO DOOR SKIN FORWARD LOWER CORNER WAS FOUND A DENT. THE SKIN SMOOTHED OUT WAS FOUND OUT LIMITS. BULK CARGO DOOR SKIN DENT AREA WAS REPAIRED AS PER SRM 52-00-03 FIG 9 REV 120.Dec 1, 2011 · N758SA · Boeing 747281F · Cargo/Baggage DoorsSDR TX9Y20111202002Doubler · crackedNR 9 SPOILER HINGE DOUBLER AND NR 11 SPOILER HINGE DOUBLER WERE FOUND CRACKED. NR 9 SPOILER AND NR 11 SPOILER WERE REPLACED AS PER AMM 27-61-02 REV 86.Dec 1, 2011 · N758SA · Boeing 747281F · SpoilersSDR TX9Y20111121010Access Panel · damagedMAIN DECK MEC BAY ACCESS PANEL ASSY (P/N:65B11970-35) LOWER SURFACE WAS FOUND DENTS AND PUNCTURE HOLE, AND AT THE ACCESS PANEL (P/N:65B16167-14) CORNERS WAS FOUND CHIPPED OFF. THE REPAIR WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0097 AND SRM 51-40-20Nov 18, 2011 · N783SA · Boeing 747281F · Fuselage Miscellaneous StructureSDR TX9Y20111116009Tension Tie · crackedUPPER DECK TENSION TIE STA 860 RT FAIL SAFE CHORD WAS FOUND CRACK. UPPER DECK TENSION TIE STA 860 RT FAIL SAFE CHORD WAS REPAIRED PER SRM 51-40-03 FIG 2 REV 120. THE REPAIR IS APPROVED FOR 24 MONTHS.Nov 14, 2011 · N783SA · Boeing 747281F · Fuselage Miscellaneous StructureSDR TX9Y20111115008Tension Tie · crackedUPPER DECK STA 800 LT & RT FWD CHANNEL OF TENSION TIE WAS FOUND CRACK. UPPER DECK STA 840 LT FWD CHANNEL OF TENSION TIE WAS FOUND CRACK. UPPER DECK STA 860 RT TENSION TIE WAS FOUND CRACK. UPPER DECK TENSION TIES (STA 800 LT & RT, STA 840 LT AND STA 860 RT) Nov 14, 2011 · N783SA · Boeing 747281F · Fuselage Miscellaneous StructureSDR TX9Y20111114007Structure · damagedONE ELONGATED HOLE WAS FOUND COMMON TO RT INBOARD FIXED TRAILING EDGE BEAM UPPER CHORD (P/N:65B11614) AT APPROX WBL 235.20. THE REPAIR WAS CARRIED OUT PER BOEING MESSAGE NUMBER TEC-SOF-11-0077 AND SRM 51-10-02. DETAILS OF THE REPAIR ARE RECORDED IN EN EA-57-Nov 11, 2011 · N783SA · Boeing 747281F · Wing Miscellaneous StructureSDR TX9Y20111111006Doubler · corrodedWATER SERVICE PORT EXTERIOR DOUBLER WAS FOUND CORROSION (BS 980-BS 1000, STR 44R-STR 46R). THE CORROSION WAS REMOVED AS PER SRM 51-10-01 REV 120. THE CORROSION WAS BLENDED OUT, NOT WITHIN SRM 53-30-01 REV 120 LIMITS. THE NEW WATER SERVICE PORT EXTERIOR DOUBLENov 8, 2011 · N783SA · Boeing 747281F · Fuselage Main, Plate/SkinSDR TX9Y20111111005Shear Tie · crackedWING CENTER SECTION FRONT SPAR LOCATION RBBL 33.89 SHEAR TIE (P/N:69B14267-9) WAS FOUND CRACK. A NEW SHEAR TIE WAS FABRICATED AS PER DRAWING 69B14267-9. THE REWORK OF TWO TAPER HOLES WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0096 AND SRM 51-30-05. DENov 8, 2011 · N783SA · Boeing 747281F · Wing SparSDR TX9Y20111111004Panel · damagedONE ELONGATED HOLE WAS FOUND COMMON TO DOOR PANEL (P/N:65B90719-86) OF NR 1 PYLON INBOARD TRAILING EDGE FAIRING DOOR ASSY (P/N:65B90717) AT APPROX STA 297.5. THE REPAIR WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0078 AND SRM 51-10-01. DETAILS OF THE Nov 8, 2011 · N783SA · Boeing 747281F · Nacelle/Pylon Miscellaneous StructureSDR TX9Y20111108003Flap Track · corrodedFLAP TRACK NR 4 FORWARD END CLEVIS INBOARD LUG SURFACE FOUND CORROSION INDICATION ON INBOARD LUG INBOARD SURFACE. THE REPAIR WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0092 AND SB 747-57-2307 REVISION 2. THE DEVIATION WAS APPROVED UNDER ODA-300064-NMNov 5, 2011 · N783SA · Boeing 747281F · Trailing Edge FlapsSDR TX9Y20111104002Structure · crackedCRACK INDICATIONS FOUND ON NR 2 PYLON STRUT STRUCTURE. REPAIRED PER MN TEC-SOF-11-0088, SRM 51-10-01 AND SRM 51-40-02.Nov 1, 2011 · N783SA · Boeing 747281F · Nacelle/Pylon, Main FrameSDR TX9Y20111104001Splice Plate · crackedA FASTENER HOLE WAS FOUND CRACKED AT HORIZONTAL STABILIZER CENTER SECTION LT SIDE LOWER SPLICE PLATE. REPLACED PER MN TEC-SOF-11-0082 AND SRM 51-30-05.Nov 1, 2011 · N783SA · Boeing 747281F · Horizontal Stabilizer StructureSDR Q2SA783004Duct · crackedNR 3 ENG FIRE WARNING LIGHT ILLUM WHILE ADVANCING POWER TO 88% RPM. BOTH NR 3 ENG NACELLE IND WERE AT 10 UNITS. EGT WAS RISING THRU 800 DEG CELCIUS WHILE OTHER ENG WERE AT APPROX 700 DEG CELSIUS. AIRSPEED WAS 200 KTS, 3500 FT MSL, LEVEL, FLAPS 5 CONFIG. ENSep 2, 2011 · N783SA · Boeing 747281F · Pneumatic Distribution SystemSDR Q2SA758012Engine · failedFLIGHT MAS6145, WHILE PREPARING FOR TAKEOFF, EXPERIENCED AN UNCONTAINED ENGINE FAILURE.Sep 24, 2010 · N758SA · Boeing 747281F · Engine (Turbine/Turboprop)SDR Q2SA795002AActuator · missingACFT 795 DEPARTED AS FLT SOO113, BOTH TAXI & TAKEOFF OPS WERE NORMAL. MLG HANDLE SELECTED TO "UP" POSITION AFTER LIFTOFF. BOTH RED "DOOR OPEN" & "RED "GEAR" LIGHTS REMAINED ILLUMINATED. FO CONTINUED FLYING & CLIMBED ON COURSE. CAPTAIN & FE COMPLETED QRH PROCEDAug 24, 2010 · N758SA · Boeing 747281F · Landing Gear ActuatorSDR Q2SA758011Engine · leakingDURING THE TAKEOFF ROLL IN OMDB NR 1 EGT GAUGE BRIEFLY WENT TO 0, THEN RETURNED TO NORMAL. DURING THE CLIMB TO FL 300 IT WAS NOTICED, NR 1 EGT WAS RUNNING SIGNIFICANTLY HOTTER (APPROXIMATELY 80 DEG C) THAN THE OTHERS. AT THE TOP OF CLIMB, THE NR 1 EGT KEPT CJul 22, 2010 · N758SA · Boeing 747281F · Turbine Engine Oil SystemSDR VGQY2010051800005Mount · corrodedDRWS NR 0020, NR 3 ENGINE AFT. UPPER MOUNT FOUND RUST. REMOVED AND REPROTECTED PER OHM CMM 71-20-02. MATERIAL REMOVED = 0.008", FOUND WITHIN LIMITS PER OHM CMM 71-20-02.May 18, 2010 · N820SA · Boeing 747281F · Engine Mount SectionSDR 2010FA0000346Hinge Fitting · crackedHORIZ STABILIZER LT 2 PLACES 0.9 INCH AND 0.8 INCH & RT 2 PLACES 1.1 INCH AND 0.85 INCH, HINGE FITTING CRACKED.Apr 15, 2010 · N758SA · Boeing 747281F · Horizontal Stabilizer, Attach FittingsSDR 2010FA0000345Stiffener · crackedPYLON NR 2 INBD NR 3 STIFFENER CRACK 0.67 INCH BETWEEN NAC STA 248 AND NAC STA 259 ON THE RT SIDE.Apr 15, 2010 · N758SA · Boeing 747281F · Nacelle/Pylon Miscellaneous StructureSDR 2010FA0000344Skin · corrodedFWD CARGO LOWER FUSELAGE SKIN AT STA 1000 WAS CORRODED LEVEL 2.Apr 15, 2010 · N758SA · Boeing 747281F · Fuselage Main, Plate/SkinSDR 2010FA0000343Doubler · crackedMAIN ENTRY DOOR NR 1 UPPER OUTER SKIN DOUBLER CRACK, 0.35 INCH AT UPPER HINGE DOOR.Apr 15, 2010 · N758SA · Boeing 747281F · Passenger/Crew DoorsSDR 2010FA0000342Stiffener · crackedPYLON NR 1, INBD NR 3, STIFFENER CRACK.Apr 15, 2010 · N758SA · Boeing 747281F · Nacelle/Pylon, Main FrameSDR VGQY2010041300005Skin · damagedCOMPLIED WITH EN 1040-10, PERMANENT REPAIR FOR SKIN DAMAGE AT STA 520 T0 STA 700 BETWEEN S-39R TO S-42R.Apr 13, 2010 · N783SA · Boeing 747281F · Fuselage Main, Plate/SkinSDR VGQY2010041400006Skin · damagedREQUEST PERMANENT REPAIR ON BELLY SKIN AT STA 520 - 540 STR 38R - 42R IAW SRM 783-007. COMPLIED WITH EN 1040-10, PERMANENT REPAIR FOR SKIN DAMAGE AT STA 520 T0 STA 700 BETWEEN S-39R TO S-42R.Apr 13, 2010 · N783SA · Boeing 747281F · Fuselage Main, Plate/SkinSDR VGQY2010041400005Skin · damagedREQUEST PERMANENT REPAIR ON BELLY SKIN AT STA 670-700 S37-42R IAW REP 783-024 PAGE 1 OF 4. REF: RAP 783-007. COMPLIED WITH EN 1040-10, PERMANENT REPAIR FOR SKIN DAMAGE AT STA 520 T0 STA 700 BETWEEN S-39R TO S-42R.Apr 13, 2010 · N783SA · Boeing 747281F · Fuselage Main, Plate/SkinSDR VGQY2010041400004Mount · corrodedNR 4 ENG PYLON, LOWER AFT MOUNT FOUND WITH SURFACE CORROSION. REMOVED AND REPLACED NR 4 ENGINE AFT LOWER ENGINE MOUNT AS PER AMM 71-21-04 REV 84.Apr 13, 2010 · N783SA · Boeing 747281F · Engine Mount SectionSDR VGQY2010041400003Mount · corrodedNR 4 ENG PYLON, UPPER AFT MOUNT FOUND WITH SURFACE CORROSION. REMOVED AND REPLACED NR 4 ENGINE AFT UPPER ENGINE MOUNT AS PER AMM 71-21-04 REV 84.Apr 13, 2010 · N783SA · Boeing 747281F · Engine Mount SectionSDR VGQY2010041300002Structure · corrodedSTA 1920 FRAME BULB TEE 65B04333-89 VERTICAL FLANGE IS FOUND CRACKED AND CHIPPED OFF AT RBL 6.30. COMPLIED WITH EN 1044-10, REPAIR FOR CRACKED 65B0433-89 BULB TEE VERTICAL FLANGE AT STA 1920 FRAME RBL 6.30.Apr 13, 2010 · N783SA · Boeing 747281F · Fuselage Main, StructureSDR Q2SA758010Doubler · crackedMAIN ENTRY DOOR NR 1 UPPER OUTER SKIN DOUBLER CRACK AT UPPER HINGE DOOR.Apr 12, 2010 · N758SA · Boeing 747281F · Passenger/Crew DoorsSDR Q2SA758009Stiffener · crackedPYLON NR 1 INBOARD NR 3 STIFFENER CRACK.Apr 12, 2010 · N758SA · Boeing 747281F · Nacelle/Pylon Miscellaneous StructureSDR VGQY2010041300001Stiffener · corrodedRIGHT HORIZONTAL STABILIZER REAR SPAR AT ELEVATOR STATION 206.8 STIFFENER LOWER END FOUND CORRODED. COMPLIED WITH EN 1048-10, ALTERNATIVE FABRICATION FOR HORIZONTAL STAB REAR SPAR ATTACHED ANGLE 65B03779-12.Apr 12, 2010 · N783SA · Boeing 747281F · Horizontal Stabilizer Miscellaneous StructureSDR Q2SA758008A/C Pack · vibrationDEPARTURE FROM VAKK TO VMCC: AFTER TAKEOFF NR 1 AIR CONDITIONING PACK STARTED SEVERE RUMBLING NOISE AND EMITTED AN ODOR. AIRCRAFT QUICK HANDBOOK PROCEDURE ACCOMPLISHED. REMOVED AND REPLACED ACM AND DUCT ASSEMBLY. OPERATIONAL AND LEAK CHECK ACCOMPLISHED ANDNov 13, 2009 · N758SA · Boeing 747281F · Cabin Cooling SystemSDR Q2SA783003Hydraulic Line · rupturedAFTER TAKING OFF FROM KDOV, NR 1 HYDRAULIC SYSTEM QUANTITY DECREASED RAPIDLY, CREW RAN ABNORMAL CHECKLIST IN ACCORDANCE WITH B-747-200/300 QUICK REFERENCE HANDBOOK. CONTINUED FLIGHT AND LANDED SAFELY AT KJFK. AFTER LANDING MAINTENANCE CREW FOUND A RUPTURED HOct 31, 2009 · N783SA · Boeing 747281F · Hydraulic System, MainSDR Q2SA758007Fuel Filter · failedON TAKEOFF CLIMBOUT OF KJFK, ENGINE NR 1 AND ENGINE NR 4 FUEL FILTER BYPASS INDICATION LIGHTS CAME ON AND STAYED ON, CREW ELECTED TO TERMINATE FLIGHT, DUMPED 156,000 LBS OF FUEL, RETURNED TO KJFK AND LANDED SAFELY. AFTER LANDING MAINTENANCE CREW IN KJFK REPLAOct 24, 2009 · N758SA · Boeing 747281F · Engine Fuel DistributionSDR Q2SA758006Slide · unwanted deployPRIOR TO DEPARTURE FROM KJFK, LEFT UPPER DECK EMERGENCY EXIT SLIDE INADVERTENTLY DEPLOYED. REMOVED SLIDE IN ACCORDANCE WITH AMM 25-68-02. TRANSFERRED TO DEFERRED MAINTENANCE ITEM NR 18844 PER MEL 25-11, CAT. C. PLACARD INSTALLED.Apr 20, 2009 · N758SA · Boeing 747281F · Escape SlideSDR Q2SA758005Pms · inactiveCLIMB-OUT OF EBLG, PERFORMANCE MANAGEMENT SYSTEM (PMS) LIGHT ILLUMINATED IN FLIGHT AND AUTOPILOTS "A" AND "B" WOULD NOT FOLLOW FLIGHT MANAGEMENT SYSTEM (FMS) COMMAND. AIR TURN BACK TO EBLG. NO FUEL DUMPED. OPERATIONALLY CHECKED IN ACCORDANCE WITH DELCO OPERMar 17, 2009 · N758SA · Boeing 747281F · Flight Management Computing Hardware SystemSDR Q2SA758004Thrust Reverser · deployedON CLIMB-OUT FROM ADDIS ABABA, ETHIOPIA (HAAB), AIRCRAFT PERFORMED AN AIR TURN BACK DUE TO INDICATION OF NR 4 ENGINE THRUST REVERSER TRYING TO DEPLOY IN FLIGHT. CREW WAS ALERTED BY THRUST REVERSER VALVE LIGHT AND TRANSIT LIGHT ILLUMINATING. CREW RETURNED TO Dec 21, 2008 · N758SA · Boeing 747281F · Engine Thrust ReverserSDR Q2SA783002Pitot Line · brokenON DEPARTURE FROM KJFK, CAPTAIN'S POSITION LOST ALL PRIMARY INSTRUMENTS (AIRSPEED, ALTITUDE, IVSI INDICATORS). AIR TURN BACK TO KFJK, NO FUEL DUMP PERFORMED. CADC REPLACED AND BROKEN PITOT LINE FOUND BEHIND CAPTAIN'S ALTIMETER.Dec 15, 2008 · N783SA · Boeing 747281F · Pitot/Static SystemSDR Q2SA758003Engine · damagedDURING TAKEOFF AFTER V1 FROM HAAB, BIRD INGESTION INTO NR 3 ENGINE. AIR TURNBACK TO HAAB. FUEL DUMP OF 50,000 LBS. INSPECTION AFTER LANDING CONFIRMED DAMAGE TO NR 3 ENGINE FAN BLADES, AS WELL AS EVIDENCE OF BIRD STRIKE ON NR 2 ENGINE. NR 1, 3, 4, 6, 11, 13Oct 9, 2008 · N758SA · Boeing 747281F · Engine (Turbine/Turboprop)
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