Boeing 747-2D3B
Service difficulty reports · 182
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 aircraft_model_key = '7472D3B' 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 aircraft_model_key = '7472D3B' 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 UIEA200700093Skin · misrepairedFUSELAGE BS 690 S31L HAS 14" BY 12" EXTERNAL DOUBLER TO LT UPPER STATIC PORT PREVIOUS REPAIRED PER SRM 51-70-00 PG 8E AND F FIG 3 SHEET 6 AND 7. THIS REPAIR IS BEYOND THE LIMIT. REPAIRED ACCOMPLISHED AS PER SRM 53-30-03 FIG 1 AND 51-70-00 FIG 3.SDR UIEA200700090Skin · crackedFUSELAGE SKIN EXTERNAL DOUBLER FOUND CRACKED AT NLG LT FWD CORNER. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-290193820-1 THRU -5 AND FAA FORM 8100-9.SDR UIEA200700086Mount · damagedNR 4 PYLON FWD ENGINE MOUNT FITTING BOTH I/B AND O/B LUG BORE HOLES FOUND OVERSIZED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-290193672-1 THRU -3 AND FAA FORM 8100-9.SDR UIEA200700089Web · corrodedFOUND LT WLG BS 1350 HORIZONTAL WEB UPPER SURFACE FOUND CORROSION. CORROSION REMOVED AND AREA PROTECTED AS PER SRM 51-10-01 AND 51-10-02.SDR UIEA200700085Access Door · damagedNR 3 ENGINE RT FAN T/REV ACCESS DOOR ASSY SKIN DAMAGED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A095 AND FAA FORM 8110-3.SDR UIEA200700087Skin · crackedFUSELAGE SKIN BS 570 EQUIPMENT COOLING OUTLET FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER SB747-53-2386 FIG 5 AND 10.SDR UIEA200700088Fairing · crackedENGINE NR 2 RT T/REV AFT UPPER BEAVER TAIL FAIRING ASSY INNER SKIN FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A094 AND FAA FORM 8110-3.SDR UIEA200700083Skin · corrodedRIGHT WING UPPER SURFACE WS 697, STR28R AT FRONT SPAR FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM 51-10-01 AND 51-10-02.SDR UIEA200700084Skin · corrodedLEFT WING UPPER WING SKIN AT WS320, STR 14L-14L FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM 51-10-01 AND 51-10-02.SDR UIEA200700082Skin · dentedFUSELAGE SKIN DENT FOUND AT BS 1810, S51L-S51R. DENT AREA REWORKED AND PROTECTED AS PER SRM 51-40-01 AND 51-10-02.SDR UIEA200700081Skin · corrodedFOUND RIGHT WING UPPER SURFACE RWS642 AT MID SPAR FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM51-10-01 AND 51-10-02.SDR UIEA200700080Skin · corrodedFOUND LEFT WING UPPER WING SKIN AT WS 1280 FOUND CORROSION. CORROSION REMOVED AND PROTECTED AS PER SRM 51-10-01 AND 51-10-02.SDR UIEA200700075Shear Web · crackedTENSION TIE BS 840-BS 860, LT SLOPING SHEAR WEB FOUND CRACKED AT FWD I/B LOWER CORNER. LEFT SLOPING SHEAR WEB REPLACED AS PER SRM 51-10-01.SDR UIEA200700078Blowout Door · chafedENGINE NR 1 AND NR 2, RT C-DUCT BLOW OUT DOOR ASSEMBLY HAS MISSING MATERIAL AND CHAFE MARKED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A093 AND FAA FORM 8110-3.SDR UIEA200700077Skin · corrodedFOUND CENTER TANK LOWER SKIN LOWER SURFACE FOUND CORROSION JUST ABOVE NR 1 ACM. CORROSION BLEND OUT AND HFEC INSPECTION PERFORMED AS PER BOEING SR ID NR 1-290707077-1 THRU -3 AND FAA FORM 8100-9.SDR UIEA200700076Skin · scratchedFOUND FUSELAGE SKIN SCRATCH FOUND AT BS 2310, S38L-S40L. SCRATCH SLIGHTLY SMOOTHED AND PROTECTED AS PER SRM 51-10-02.SDR UIEA200700074Skin · corrodedLEFT WING LEADING EDGE BULLNOSE FOUND CORROSION OUTBOARD OF LANDING LIGHT. PERMANENT REPAIRED ACCOMPLISHED AS PER BOEING MESSAGE 1-286780848-2 DATED 13 FEB,2007 AND EO NR 4757A281.SDR UIEA200700071Stiffener · crackedFOUND UPPER DECK FLOORBEAM ONE STIFFENER CRACKED AT BS 400 LBL15. UPPER DECK FLOORBEAM STIFFENER REPLACED AS PER SRM 51-10-01.SDR UIEA200700072Intercostal · crackedFOUND UPPER DECK FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 395 RBL 6. U/DECK FLOOR SUPPORT INTERCOSTAL REPLACED AS PER SRM 51-10-01.SDR UIEA200700070Actuator · brokenLOSS OF HYD SYSTEM NR 1, PERFORMED EMERGENCY/ABNORMAL CHECKLIST 3.29 FHB EDP, PUMP PLACED TO SUPPLY OFF AT TIME 2133Z, FLUID QTY TO 0. REMOVED AND REPLACED NOSE DOOR ACTUATOR AS PER AMM 32-34-14.SDR UIEA200600313Support Beam · damagedLT WING LEADING EDGE PANEL BETWEEN ILES 173.6742 AND 330, INNER PANEL SUPPORT BEAM, UPPER CHORD HAS 8 EACH HOLES DRILLED INCORRECTLY. INTERIM REPAIR WAS ACCOMPLISHED PER REFERENCE ATLAS AIR XEO 57-122806 AND 747 SRM 51-40-04, 51-30-02 AND 51-10-02 FAA FORM 81SDR UIEA200600305Relief Valve · faultyDURING CLIMB-OUT, NR 2 ENGINE FIRE WARNING. BOTH ENGINE NACELLE TEMPS ON NR 2 ENGINE READ 8.5. ALL OTHER INDICATIONS NORMAL. ENGINE FIRE HANDLE PULLED. FIRE LIGHT EXTINGUISHED AND NACELLE TEMPS RETURNED TO NORMAL. REPLACED NR 2 PRV PER AMM 36-11-19. REPLSDR UIEA200600277Fire Warning · false activationAPU FIRE WARNING CAME ON IN FLT WITH BELL AND MASTER CAUTION LIGHT ON. APU FIRE HANDLE PULLED AND FIRE BOTTLE IAW FHB 3.26.5. PLACED APU, APU FIRE WARNING ON APU AND APU FIRE BOTTLE ON DMI. APU INSPECTED IAW 49-31-00 PG 601. NO EVIDENCE OF FIRE FOUND. (OPEN).SDR UIEA200600200Warning Horn · false activationRTO TAKEOFF REJECTED AT 110 KTS DUE TO TAKEOFF WARNING HORN. AFTER EXITING RUNWAY A/C CHECKED FOR CONFIGURATION DISCREPANCY. SUSPECT T/O WARNING, ENABLE BY FLAP TAKEOFF WARNING SWITCH, S339 FOUND STICKING, CLEANED SWITCH AND PERFORMED AURAL WARNING LOGIC CIRSDR UIEA200600195Skin · damagedON WALKAROUND, FOUND HOLE IN LEADING EDGE OF RIGHT HORIZONTAL STABILIZER. REPAIR CARRIED OUT AS PER SRM 55-10-03 FIG 1. XEO 55-072806 ALL ORIGINAL SIGNATURES HELD ON XEO 55-072806 ITEM 2. FURTHER INSPECTION REVEALED HOLE IN LEADING EDGE OF RIGHT INBOARD FORESDR UIEA200600189Panel · corrodedL/W-L/E WING PANEL CORRODED TWO SPOTS AREA IS I/B ON MOST I/B L/E NEAR FUSELAGE.SDR UIEA200600191Panel · crackedR/W-O/B MID FLAP COVE PANEL CRACKED AT SUPPORT ARM APPROX 4" CRACK AT 3RD SUPPORT ARM I/B OF NR 8 CANOE.SDR UIEA200600192Panel · crackedR/W-O/B MID FLAP COVE PANEL CRACKED AT SUPPORT ARM APPROX 14". AREA IS BETWEEN NR 7/8 CANOE-MARKED.SDR UIEA200600190Structure · chafedR/W-I/B AFT FLAP-UPPER SURFACE HAS TWO CHAFE MARKS FROM LONG SCREWS IN COVE PANEL ARM. CHAFE AREA ON I/B END-MARKED.SDR UIEA200600175Bolt · shearedNR 3 LT REVERSER, CENTER HINGE FITTING 2 EACH BOLTS FRACTURED. REMOVED AND REPLACED CENTER HINGE FITTING AND BOLTS AS PER 747 SRM 51-30-05 TABLE I PAGE 6 AND SRM 51-30-04 TO NEXT OVERSIZED BOLT P/N BACB30US6K13Y. FASTENER HOLES WERE INSPECTED AS PER NDT MANUSDR UIEA200600170Skin · crackedPYLON NR 2 FORWARD ACCESS PANEL CUTOUT SKIN AND DOUBLER HAS A 1 1/16 INCH CRACK AT LOWER AFT CORNER. ACCOMPLISHED SKIN AND INNER DOUBLER REPAIR AS PER 747 SRM 54-31-03 FIG 6 AND REFERENCE ATLAS AIR XEO NR 54-070806-2.SDR UIEA200600171Brace · chafedPYLON NR 4 DIAGONAL BRACE HAS A CHAFE ON OUTBOARD SIDE CAUSED BY HYDRAULIC COMPARTMENT DOOR ROD FOUND NOT SECURED. ACCOMPLISHED BLEND REPAIR ON BRACE P/N 321U2731-102, S/N MFR 16889 RP 06709322 AS PER 747 SRM 51-41-01 FIG 3 AND REFERENCE ATLAS AIR XEO NO. 54-SDR UIEA200600173Structure · crackedMAIN CARGO DECK DOOR L-4, AT THE ML POSITION HAS A VERY HIGH VOLUME AIR LEAK LIKE A BIG VAC. FOUND 8" CRACK IN FWD LWR CORNER OF 4L MED OUT OF LIMITS PER SRM 52-08-02. REMOVED 4L MED INSP OK TO INSTALL. INSTALLED 4L SERVICEABLE DOOR PER 52-11-01. NEEDS TO BSDR UIEA200600128Valve · malfunctionedAFTER T/O, FIRE INDICATION POINTERS BELL NR 1 ENGINE. COMPLETED ENGINE FIRE, SEVERE DAMAGE OR SEPARATION CHECKLIST. JETTISON APPROX 70,000 KGS, OF FUEL. LANDED UNDER MAX LANDING WEIGHT. PERFORMED PNEUMATIC LEAK CHECK PER MM 71-00-00 PG 510, CHECK OK. PERFSDR UIEA200600094Engine · damagedNR 4 ENGINE COMPRESSOR STALL 33,000. TAT-7, MACH .84, ENGINE SHUT DOWN. HIGH VIBRATION, EGT RISE. NO EXCEEDANCES. AIR TUR BACK. NR 4 ENGINE CHANGED IAW ATLAS AIR ENGINE CHANGES SHEET REV 15 JAN 02.SDR UIEA200600081Skin Panel · corrodedLT WING LE O/B OF O/B LANDING LT AT AREA OF LOOSE RIVETS THERE IS TWO SPOTS OF INNERGRANULAR CORROSION (MARKED). INTERIM REPAIR TO LEADING EDGE LT WING PER SRM 57-30-04 AND XEO57-041306 AND 8110-3. REPEAT INSP EVERY A CK AND PERMANENT REPAIR AT C-CK.SDR UIEA200600007Support · crackedLEFT WING O/B MIDFLAP COVE PANEL CRACKED 18 INCHES LONG AT 3RD SUPPORT ARM I/B OF NR 1 CANOE.SDR UIEA200600010Skin · crackedREFERENCE ENGINEERING ORDER XEO 53-021706, FOUND DENT CRACKED APPROXIMATELY 1 INCH LONG BS 1796 STRINGER 32 RSDR UIEA200600009Support · crackedRIGHT WING OB MID FLAP COVE PANEL CRACKED AT 4TH SUPPORT ARM IB OB #8 CANOE APPROX 18" LONGSDR UIEA200600008Panel · crackedL/W IB MIDFLAP COVE PANEL CRACKED AT PREVIOUS REPAIR- 4TH SUPPORT ARM FROM OB END.SDR UIEA200600004Skin · puncturedLAV SERVICE TRUCK PUT A HOLE IN THE FUSELAGE LEFT HAND LOWER SIDE BETWEEN STRINGERS L39 AND L 40 AT STA 580. NO DAMAGE TO STRINGER. REPAIR ACCOMPLISHED AS PER SRM 53-30-03. REPAIR IS A CAT B REF ATLAS XEO 53-010406.SDR UIEA200500166Switch · defectiveAT APPROX FL 280, AFT CARGO LIGHT ON FE`S PANEL AND CARGO DOOR LIGHT ON PILOTS PANEL BEGAN FLICKERING, SHORTLY IT CAME ON STEADY. DESCENDED AC TO FL250 AND ACCOMPLISHED FHB PROCEDURES FOR DOOR OPEN LIGHT. AT NO TIME EXPERIENCED PRESSURIZATION PROBLEMS PRIOR SDR UIEA200500055Gearbox · seizedDURING CRUISE ENGINE NR 2 FUEL FLOW BEGAN FLUCTUATING FOR 30 SECONDS, THEN THE ENGINE SHUTDOWN WITH THE FOLLOWING INDICATIONS. N1=26.1 PERCENT, EGT 0.0, N2 0.0, OIL PRESSURE 0.0, OIL QUANTITY 3.7 GALLONS, AND FUEL FLOW WAS 1.095. ENGINE WAS WINDMILLING 3 HOUSDR UIEA200500046Drain Mast · damagedA FIRM LANDING ON TOUCH DOWN, ON WALK AROUND, AFTER PARKING, NOTICED NR 3 ENGINE IAW MM. NO FURTHER DAMAGE NOTED. ALSO ALIGNMENT MARKS ON STRUT DOORS ARE ALIGNED AND NO DAMAGE TO CANOES OR TAIL SECTION OF AIRCRAFT FOUND. REPLACEMENT COWLS OR SLEEVES IS NOT SDR UIEA200500022Panel · crackedNR 2 PYLON OUTBOARD SIDE CUTOUT FOR PANEL 463CL HAS A .875 INCH CRACK AT AFT CORNER OF SKIN. CRACK WAS NDT INSPECTED TO VERIFY AREA OF CRACK AS PER B747 NDT MANUAL PART 6 51-00-00 FIG 23. STOP DRILLED CRACK IAW B747 SRM 51-10-01 PAGE 12. HFEC INSPECTED STOPSDR UIEA200500007Sequence Valve · failedNOSE GEAR CYCLED X3 DURING CLIMB-OUT, TO DOORS OPEN AND NOSE GEAR INTRANSIT. ALSO AT THE SAME TIME RT WING DOOR ANNUNCIATOR ON AND GEAR INTRANSIT. ALL CONDITIONS ASSOCIATED WITH AIRCRAFT VIBRATION NOISE VIA AIR STREAM. ALL THREE CYCLES WERE PRECEDED BY RED SDR UIEA200400209Rheostat · burnedHOT SMELL (ELECTRICAL) DETECTED IN CRUSE. C/B PILOT PANEL ENDER FLIGHT DECK LIGHTS WAS PULLED ON P6 PANEL. SMELL STOPPED, SHORTLY AFTER. PANEL BELOW CAPTAIN CUP HOLDER FELT HOT. ON T/S FOUND T77 DIMMER BURNED. REMOVED AND REPLACED DIMMER. OPS CHECK NORMASDR UIEA200400159Support · crackedDURING OVERNIGHT, EXTERNAL IMPACT BY A FOREIGN OBJECT CAUSED BY A TORNADO. AN INSPECTION OF THE AIRCRAFT WAS CARRIED OUT AND IT WAS OBSERVED THAT AT BS 1034 RBL 104, THE UNDERWING FAIRING SUPPORT LOWER CHORD WAS CRACKED AT THE OUTBOARD FLANGE. THE LONGITUDINSDR UIEA200400152Panel · delaminatedFOUND LER LEFT WING PANEL AT ILES 173.6 HAD DELAMINATION HEAT DAMAGE WHILE ON GROUND. THE PANELS WERE REPLACED IAW SRM 51-30-02 AND AMM 51-24-11. (M)SDR UIEA200400140Sequence Valve · failedAFTER TAKEOFF, ON GEAR RETRACTION NOSE LANDING GEAR DOORS KEPT CYCLING, ATTEMPTED RECYCLE NO EFFECT. REMOVED AND REPLACED NOSE GEAR, OPERATED DOOR SEQUENCE VALVE PER MM 32-34-08 PAGE 401-405, OPS AND LEAK CHECK NORMAL. UIEA (M)
Back to Boeing 747-2D3B