Boeing 747-228F
Service difficulty reports · 199
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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 = '747228F' 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 = '747228F' 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 754001Fire Loop · inoperativeDURING CLIMB-OUT, APU FIRE BELL AND LIGHTS ACTIVATED. APU FIRE CHECKLIST PERFORMED BUT DID NOT STOP BELL RINGING OR LIGHTS FLASHING. SELECTED FIRE WARNING SYSTEM "A" AND CONDITION CLEARED. INSPECTED APU COMPARTMENT AND FOUND NO EVIDENCE OF FIRE. FOUND APU SDR UIEA200700451Access Panel · delaminatedAIR CONDITION ACCESS PANEL 192ER EXTERNAL SURFACE IS DELAMINATED. REPAIRED AS PER SRM 51-40-17 AND BOEING MESSAGE 1-638498164-2.SDR UIEA200700446Fitting · corrodedBS 230 RBL 1 BILGE AREA BEAM WEB SUPPORT FITTING CORRODED. REPLACED FITTING AS PER SRM 51-10-01 AND BOEING MESSAGE 1-637033946-3.SDR UIEA200700444Bulkhead · crackedRIGHT SIDE NOSE WHEEL WELL BULKHEAD WEB CRACKED AT STATION 260, WL 182 RBL 38. WEB REPAIRED AS PER BOEING MESSAGE 1-636527780-4.SDR UIEA200700447Skin · corrodedNR 8 SPOILER AREA OF UPPER SKIN AND REAR SPAR HAS AREA OF CORROSION. REPAIRED AS PER BOEING MESSAGE 1--638467931-2.SDR UIEA200700450Brace · looseNR 1 PYLON DIAGONAL BRACE UNDERWING FITTING TENSION FASTENER HEAD SHEARED. REMOVED AND INSTALLED FASTENER AS PER 51-30-02.SDR UIEA200700449Spar Cap · corrodedRIGHT WING FRONT SPAR LOWER CHORD AREA BETWEEN FSSO 1322 AND 1340 CORRODED. CORROSION REMOVED AS PER SRM 51-10-01 AND BOEING MESSAGE 1-638497220-2.SDR UIEA200700448Spar Cap · corrodedRIGHT WING FRONT SPAR LOWER CHORD AREA FSSO 1356 CORRODED. CORROSION REMOVED AS PER SRM 51-10-01 AND BOEING MESSAGE 1-638497220-2.SDR UIEA200700443Brace · chafedNR 4 STRUT DIAGONAL BRACE FORWARD END CHAFED. CHAFING AREA DAMAGE BLENDED AS PER BOEING MESSAGE 1-636565614-4.SDR UIEA200700445Fairing · delaminatedFUSELAGE FAIRING 193C AREA OF DELAMINATION. DELAMINATED AREA REPAIRED AS PER SRM 51-40-12SDR 753003Yaw Damper · faultyHAD SEVERAL HARD RUDDER KICKS. FOUND THAT SHUTTING DOWN LOWER YAW DAMPER PROBLEM WENT AWAY. DEFERRED ITEM IN ACCORDANCE WITH DDPG PROCEDURES 22-3. REMOVED AND REPLACED LOWER YAW DAMPER COMPUTER IN ACCORDANCE WITH AMM 22-16-02. OPERATIONAL CHECK GOOD. DEFERRSDR UIEA200700324Skin · delaminatedLT WING UPPER SURFACE TRAILING EDGE FIXED PANEL AT STATION 1224 HAS AN AREA OF 2.0 INCH LONG BY 15.0 INCH WIDE AREA OF DELAMINATION. PERMANENT REPAIR OF AREA WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 2, SHEETS 4 & 5.SDR 753002Inu · failedTAKEOFF REJECTED AT 120 KNOTS AT RKSI, DUE TO NR 1 INS FAIL WARNING AND CAPTAIN'S ATTITUDE INSTRUMENT FAIL WARNING. REMOVED AND REPLACED NR 1 INU IN ACCORDANCE WITH AMM 34-41-03. OPERATIONAL CHECK NORMAL ON GROUND. ACCOMPLISHED HIGH ENERGY STOP/HEAT DAMAGE SDR UIEA200700248Skin · dentedLOWER FUSELAGE, RT SIDE AT STA 660 HAS A DENT BETWEEN S43 AND S44 RT CAUSED BY ACCIDENT DURING STORM. ACCOMPLISHED PERMANENT REPAIR OF EXTERIOR SKIN AS PER 747-200 SRM 53-30-03 FIG 17, ALSO, PERMANENT REPAIR OF BROKEN SHEAR TIE AT BS 660 S43R-S44R WAS REPAIRESDR UIEA200700247Skin · unknownRADOME SKIN HAS A 2.0 INCH BY 4.0 INCH PREVIOUS REPAIR FILLER ERODED AT 11 O'CLOCK POSITION. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 53-50-03 PAGE 23, PAR 15. ALSO REFERENCE ATLAS AIR XEO 53-061507-1.SDR 751003Fitting · shearedLOUD THUMP HEARD WHEN MOVING FLAPS FROM 10 TO 20 DEGREES. INSPECTED AIRCRAFT AND FOUND RT INBD TRAILING EDGE FORE-FLAP FITTING SHEARED AND OTHER COMPONENTS IN THE AREA DAMAGED. REMOVED AND REPLACED FORE-FLAP, 2 EACH RIBS, RT INBD AILERON AND PERFORMED A FLAPSDR UIEA200700144Skin · crackedFUSELAGE SKIN HAS A CRACK APPROX 400", AT BS 789 S46R AND RIVET PULLING THROUGH. REPAIRED ACCOMPLISHED AS PER XEO NR 53-032207.SDR 752006Regulator Valve · leakingNR 1 ENGINE MAXIMUM TAKEOFF POWER. PILOT'S PANEL ENGINE LOOP FAULT LIGHT ILLUMINATED INTERMITTENTLY FOLLOWED BY INTERMITTENT FIRE WARNING. NACELLE TEMPERATURE FLUCTUATED 5 TO FULL SCALE. SET CLIMB POWER. NACELLE TEMPERATURE A & B SETTLED TO 2.0. TAKEOFF POSDR 752005Circuit Card · malfunctionedMAXIMUM POWER TAKEOFF OUT OF PANC, N1 SET AT 105.8 PERCENT. AFTER TAKEOFF PASSING THRU 1000 FEET, NR 1 ENGINE NACELLE FAULT LIGHT ILLUMINATED INTERMITTENTLY ACCOMPANIED BY FIRE WARNING. BELL ALSO RANG INTERMITTENTLY. NACELLE INDICATORS A & B WERE FLUCTUATINSDR UIEA200700132Oil Filter · unserviceableNR 2 OIL FILTER BY PASS LIGHT ILLUMINATED DURING DESCENT, LIGHT REMAINED AT IDLE THRUST, SHUT DOWN NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE OIL FILTER AS PER MM 79-21-04. PERFORMED ENGINE RUN NO LEAK NOTED.SDR 753001Clamp · brokenDURING THE CLIMB-OUT OF PANC, NR 4 ENGINE FIRE WARNING AND HIGH NACELLE TEMPERATURE. ENGINE SHUTDOWN, DUMPED 61,000 LBS FUEL. NO FIRE EXTINGUISHER ACTIVATED. RETURNED TO PANC. FOUND BROKEN CLAMP AT 14TH STAGE BLEED AIR DUCT AND HIGH STAGE VALVE.SDR UIEA200700002Seat Track · brokenMAIN CARGO COMPARTMENT SEAT TRACK AT STATION 1960 RT, RBL 11 HAS 1 EACH BROKEN CROWN LUG. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM STATION 1946 TO 1969 RT AS PER 747 SRM 53-10-05 FIG 14.SDR UIEA200600291Circuit Card · failedRED GEAR LIGHT CAME ON AFTER RETRACTION WITH AURAL WARNING ON IN UP POSITION, GEAR UNSAFE CHECK ACCOMPLISHED PER FHB PROCEDURES AND RETURNED FOR LANDING. T/S FOUND A-9 CARD IN ALT CONTROL BOX FAILED. REMOVED AND REPLACED CARD PER AMM 32-61-00.SDR UIEA200600282Skin · crackedMAIN ENTRY DOOR L-1, LOWER, FORWARD HINGE CUT-OUT HAS A CRACK AT PREVIOUS REPAIR DOUBLER. PERMANENT EXTERNAL DOUBLER REPAIR WAS ACCOMPLISHED IAW SB 747-52-2144 REV 2 AND REFERENCE EO NR 4752A111.SDR Q2SA752004Wire Harness · shortedNR 3 ENGINE NACELLE A & B LOOP ON TAKEOFF HAD FLICKERING ENGINE FIRE INDICATION WITH FLICKERING FAULT LIGHT ON FLIGHT ENGINEER PANEL AT APPROXIMATELY 91 PERCENT N1. NACELLE TEMPERATURE INDICATION FLUCTUATED ABOVE 2.5 TO 7.0. A & B LOOP FLUCTUATED.SDR 751002Tube · blownNR1 ENGINE FIRE WARNING ILLUMINATED ON TAKEOFF. SHUTDOWN NR 1 ENGINE. DUMPED 160,000 LBS OF FUEL AND RETURNED TO DEPARTING AIRPORT (ZSPD).SDR UIEA200600197Skin · delaminatedRT AFT IB FLAP UPPER AND LOWER SIDES OF SKIN HAVE AN AREA OF DELAMINATION. UPPER SIDE IS AT WBL 278.750 AND DAMAGE AREA IS 1.5 INCHES. LOWER SIDE IS AT WBL 272.00 AND DAMAGE IS 2.0 INCHES. ACCOMPLISHED PREPREG 250 DEGREES F. PERMANENT REPAIR OF BOTH AREAS IAWSDR Q2SA751001Clamp · looseON CLIMBOUT FROM ZGGG, NR 3 ENGINE FIRE WARNING LIGHT AND BELL ILLUMINATED. FOLLOWED QRH PROCEDURES IAW EAC 107-47. ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO ZGGG FOR REPAIRS. FOUND LOOSE CLAMP ON HIGH STAGE VALVE. TIGHTENED CLAMP AND LEAK CHECKED GOOD.SDR UIEA200600181Skin · crackedPYLON NR 4 ACCESS SKIN CUTOUT AT NAC STA. 273.09, PANEL 483AL, HAS A 0.750 INCH LONG CRACK AT UPPER FORWARD CORNER. ACCOMPLISHED SKIN PERMANENT REPAIR IAW SRM 54-31-03 FIG. 6.ALSO, REFERENCE EO 4754A231.SDR UIEA200600179Brace · chafedNR 1 PYLON DIAGONAL BRACE HAS A CHAFED AREA ON OB SIDE ZONE 3A. ACCOMPLISHED BLENDOUT REPAIR AND FOUND WITHIN LIMITS IAW SRM 54-41-01 FIG. 3. PERFORMED FPI OF REWORKED AREA, NO DEFECTS FOUND IAW ASTM 1417-05. SHOT PEENED REWORKED AREA IAW SOPM 20-10-03. TREASDR UIEA200600182Skin · delaminatedLT WING UPPER SURFACE LEADING EDGE PANEL AT OLES STA. 1336.0 AND 1495.0 HAS 2 EACH SMALL AREAS OF DELAMINATION. AREAS ARE BOTH 2.0 INCH BY 2.0 INCH. ACCOMPLISHED PREPREG 250 DEGREE PERMANENT HOT BOND REPAIR SRM 51-40-12 AND SRM 51-40-09 FIG. 18. ALSO, REFERENSDR UIEA200600180Skin · crackedPYLON NR 4 ACCESS SKIN CUTOUT AT NAC STA 281.34, PANEL 483AL, HAS A 1.0 INCH LONG CRACK AT LOWER AFT CORNER. ACCOMPLISHED SKIN AND INNER DOUBLER PERMANENT REPAIR SRM 54-31-03 FIG. 6.ALSO, REFERENCE EO 4754A231.SDR UIEA200600183Stiffener · crackedNOSE WHEEL WELL, LT SIDEWALL STIFFENER BETWEEN FUSELAGE STATION 320 LT AND 340 LT, WL 180, WAS FOUND WITH CRACK DURING HFEC INSPECTION. REMOVED AND REPLACED STIFFENER WITH A NEW STIFFENER EXTRUSION P/N BAC1517-1558 IAW SRM 51-40-04 FIG. 2 AND SRM 51-30-02.SDR UIEA200600156Flap · activatedAFTER CLIMB-OUT AND FLAP RETRACTION FROM 5*-1*, FLAPS STAYED IN FLAPS 5* POSITION, ACCOMPLISHED ALT FLAP OPERATION SECT III FLAPS MOVED TO APPROX 3*, THEN STOPPED NO OTHER MOVEMENT WAS POSSIBLE INITIAL CK FOR OPEN C/B'S AND FURTHER INVESTIGATED PROBLEM. NO SPSDR 752003Relief Valve · leakingNR 1 ENGINE FIRE LIGHT ILLUMINATED AT 17,000 FEET. PERFORMED QRH CHECKLIST, WITH THRUST LEVER CLOSED AND START LEVER CUTOFF, ENGINE FIRE LIGHT WENT OUT AND NACELLE TEMPERATURE DROPPED. ENGINE HYDRAULIC PUMP WAS NOT PUT INTO SUPPLY OFF. FIRE HANDLE WAS NOT PSDR 752001Duct · leakingNR 3 ENGINE FIRE LOOP FAULT LIGHT ILLUMINATED WITH ASSOCIATED AURAL FIRE WARNING HORN. ENGINE SHUTDOWN AND DISCHARGED FIRE EXTINGUISHER BOTTLE. DUMPED 150,000 LBS OF FUEL AND RETURNED TO DEPARTING AIRPORT (RKSI).SDR 752002Relief Valve · leakingNR 3 ENGINE NACELLE TEMPERATURE ROSE INTO THE YELLOW BAND AT CLIMB POWER OF 103% N1. RETARDED THRUST LEVER TO 65% N1 AND TEMPERATURE DROPPED INTO NORMAL RANGE.SDR UIEA200600142Steering Sys · malfunctionedRTO AT 30 KTS AIRCRAFT DRIFTED LEFT WITH NO EFFECTIVE CONTROL, W/NOSE WHEEL STEERING. NOSE WHEEL STEERING APPEARS TO BE INOP. TRANSF TO DMI M06-076 PER MEL 32-18 CAT 'C'.PLACARD. VERIFIED OPS RUDDER PEDAL NORMAL. VERIFIED OPS TILLER STEERING NORMAL.SDR UIEA200700249Panel · crackedLT HORIZONTAL STABILIZER, LOWER T/E ACCESS PANEL 334 GBL HAS 2 EACH CRACKS ON INBOARD SIDE OF PANEL. CRACKS ARE 2.0 INCH IN LENGTH. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 51-40-09 FIG 13, 747-200 SRM 51-40-12. ALSO REFERENCE ATLAS AIR XEO 55-06150SDR UIEA200600122Apu · malfunctionedAPU FIRE BOTTLE WAS DISCHARGED DUE TO HEAVY BLACK SMOKE COMING FROM INLET, TAILPIPE, AND COWLING OF APU. APU INOP DUE TO FIRE BOTTLE PREVIOUSLY DISCHARGED. FIRE BOTTLE TRANSFERRED TO DI PG 88002 CAT C, PER MEL 26-8 M06-056. INSPECTED APU PER MM 49-11-00 PG6SDR UIEA200600119Compressor · stalledON TAKEOFF OUT OF DOV NR 2 ENGINE STALLED ABOUT 5 TIMES WITH REDUCTIONS IN N1, EGT AND N2. NO PARAMETERS WERE EXCEEDED. FLIGHT CONTINUED TO JFK WITHOUT SHUTDOWN. PERFORMED BOROSCOPE OF HPC. 1, 2, 3, 4 AND 7TH STAGES. DEFECTS NOTED, ENGINE TO BE REPLACED. SDR UIEA200600115Skin · dentedFOUND DENTS AT BS 660 BETWEEN S-46L AND S-45R. REPAIR ACCOMPLISHED AS PER BOEING MESSAGE 1-17408378 AND FAA FORM 8100-9.SDR UIEA200600114Skin · crackedNR 1 PYLON RIGHT SIDE SKIN ASSEMBLY WAS FOUND CRACKED IN THE AREA COVERED BY TITANIUM DOUBLERS. INTERIM REPAIR FOR THE NR 1 PYLON 65B94100 SKIN ASSEMBLY, WAS ACCOMPLISHED AS PER BOEING MESSAGE 1-178658112 AND FAA FORM 8100-9.SDR UIEA200600113Skin · crackedDURING A C-CHECK, CRACK DAMAGE WAS FOUND IN THE 65B94052 SKIN ASSEMBLY NR 3 STIFFENER AND PRE-COOLER EXHAUST CUT OUT EDGE ADJACENT TO N.S. 248 NR 2 PYLON. INTERIM REPAIR AS AN AMOC TO AD 95-13-07, ON THE RIGHT SIDE OF THE STRUT STRUCTURAL ASSEMBLIES OF THE NRSDR UIEA200600111Skin · crackedTHE CRACKS WERE FOUND IN THE SUBJECT STRUT CAP SKIN ASSEMBLY AND ADJACENT BULKHEAD STRAP AT STA-286 BULKHEAD INSTALLATION CROWN AREA AT B-L. 0-0. THE AFT EDGE OF CAP SKIN ASSEMBLY. THE BULKHEAD STRAP IN AREA COMMON TO CAP SKIN. INTERIM REPAIR OF THE 65B9405SDR UIEA200600110Skin · crackedCRACK DAMAGE WAS FOUND IN THE 65B94052 SKIN ASSEMBLY NR 3 STIFFENER, AND PRE-COOLER EXHAUST CUT OUT ADJACENT TO THE AFT CORNER AT N.S.248, ON THE RIGHT SIDE OF THE STRUT STRUCTURAL ASSEMBLIES FOR NR 3 AND NR 4 PYLONS. INTERIM REPAIR FOR THE NR 3 AND NR 4 STRUSDR UIEA200600106Bulkhead · crackedBS 2598 BULKHEAD AFT OUTER CHORD ATTACH FASTENER CRACKS AT STR 12L,LBL 50-55, WL 310-315. REPAIR ACCOMPLISHED AS PER BOEING MESSAGE 1-17563784 AND FAA FORM 8100-9.SDR UIEA200600105Skin · corrodedCORROSION IN THE INTERNAL BEAR STRAP AT THE RT AFT CORNER OF THE FORWARD LAVATORY SERVICE DOOR CUT-OUT, BS 560, STR 46R. REPAIR ACCOMPLISHED AS PER BOEING MESSAGE NR 1-177290023 ANF FAA FORM 8100-9.SDR UIEA200600108Floorbeam · corrodedREPORTED CORROSION ADJACENT TO AN EXISTING REPAIR ANGLE AT THE MAIN DECK FLOORBEAM UPPER T-CHORD HORIZONTAL FLANGE AT STA 620. REPAIR ACCOMPLISHED AS PER BOEING MESSAGE 1-178210650 AND FAA FORM 8100-9.SDR UIEA200600103Floorbeam · corrodedREPORTED CORROSION ON THE MAIN DECK FLOORBEAM UPPER T-CHORD HORIZONTAL FLANGE AT STA 500 BETWEEN APPROXIMATELY LBL 50.0 AND LBL 60.0. THE UPPER CHORD WAS REPLACED WITH SPLICES AT LBL 21.37.5 AND LBL 78.5, SIMILAR TO 747 SRM 53-10-07 FIG 12. REPAIR ACCOMPLISH
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