Boeing 747-243B
Service difficulty reports · 506
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 = '747243B' 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 = '747243B' 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 UIEA200600295Skin · corrodedCORROSION FOUND BETWEEN UPPER WING SKIN REAR SPAR AREA AND FLYING PANEL AT STATION 406. REPAIR CARRIED OUT IAW XEO 57-112106 AND SRM 57-30-01 FIG 1.SDR UIEA200600294Skin · corrodedCORROSION FOUND ON RT WING REAR EDGE BETWEEN REAR SPAR UPPER SKIN AND FWD EDGE OF FLYING PANEL. PANELS AT STA 456 AND 586. LEVEL 1 CORROSION. REPAIR CARRIED OUT PER XEO 57-112206 AND SRM 57-30-01 FIG 1.SDR UIEA200600279Warning Light · malfunctionedAFTER PUTTING GEAR DOWN, WE HAD A GREEN GEAR LIGHT MOMENTARILY ON FOLLOWED BY A MOMENTARILY RED LIGHT, ALL GEAR LIGHTS WENT OUT. ENGINEER PANEL LIGHTS FOR GEAR CHECKED NORMAL. RESET C/B C613 PANEL. CARRIED OUT OPERATIONAL CHECK OF LANDING GEAR INDICATION LIGHTSDR UIEA200600288Line · leakingUPON ARRIVAL, MAINTENANCE NOTICED A STRONG ODOR OF FUEL THROUGH OUT THE AIRCRAFT. INSPECTED THE FUEL TANKS FUEL LINES, ALL ENGINE FUEL LINES MAIN DECK AND LOWER CARGO AREAS NO TROUBLE FOUND. CHECKED APU AREA AND FOUND FUEL LEAKING AT APU FUEL TUBE FITTINGS FRSDR UIEA200600272Drive Unit · unserviceableON TAKEOFF ROLL AT APPROX 95 KNOTS AMBER L/E FLAP DISAGREEMENT LIGHT AND AMBER CAUTION L/E FLAP LIGHT. TAKE OFF WARNING HORN SOUNDED. REJECTED T/O. REMOVED AND REPLACED L1,L4 R2 AND R3 L/E FLAP DRIVE UNITS IAW AMM 27-81-03. DRIVE UNITS SERVICED IAW AMM 12-30-SDR UIEA200600270Rib · crackedRT WING SUPPORT RIB FOR FLYING PANEL, IB OF NR 7 SPOILER AT WBL253.0 HAS A CRACK. ACCOMPLISHED PERMANENT REPAIR IAW SRM 51-40-02 FIG. 1.SDR UIEA200600266Skin · delaminatedRT INBOARD MID FLAP, BOTTOM SIDE SKIN AT WBL 195.750 HAS 1.250 BY 5.0 INCH AREA OF DELAMINATION. ACCOMPLISHED PREPREG LAYUP 250 DEGREES CURE PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 2 AND 51-40-12.SDR UIEA200600265Panel · crackedLT WING TOP T/E PANEL AT WBL 235.65 HAS A 1.750 INCH CRACK 17.0 INCHES FROM FORWARD EDGE OF PANEL. ACCOMPLISHED PREPREG LAYUP 250 DEGREES CURE PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG. 2 AND SRM 51-40-12.SDR UIEA200600264Panel · delaminatedRT WING TOP L/E PANEL AT ILES 559.72 HAS AREA OF 4.0 BY 7.0 INCH OF DELAMINATION. ACCOMPLISHED PREPREG LAYUP 250 DEGREES F CURE PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 2 AND 747 SRM 51-40-12.SDR UIEA200600255Relief Valve · failedNR 1 ENGINE FIRE INDICATION, FL330 2135Z, NACELLE TEMP INDICATIONS ON "B" LOOP OVER 5.0. "B" LOOP WAS DEFERRRED. FHB SECTION 3 PROCEDURES ACCOMPLISHED. FOUND OVERPRESSURE RELIEF VALVE LEAKING EXCESSIVELY AT 40-PSI. REPLACED VALVE PER AMM 36-11-00 ADJ TEST.SDR UIEA200600253Control Valve · failedBLOCK TURN BACK, DUE TO SMOKE IN COCKPIT APPEARS TO BE BLEED AIR SMOKE. NR 3 PACK VALVE CLOSED ACM OUTLET TEMP 85 DEGREES C, NO TRIP. SUSPECT SMOKE CAME FROM CONTAMINATED AIR DUCT AND DUE TO ACM NR 3 ABOVE 85 DEGREES C. PERFORMED OPS TEST, AIR CONDITIONING SDR UIEA200600225Valve · inoperativeDURING CRUISE, COULD NOT CLOSE NR 1 PYLON VALVE WITH ASSOCIATED SWITCH, VLV CLOSED. ON ENG SHUT DOWN (DIV). DURING CRUISE, COULD NOT CLOSE NR 3 PYLON VALVE WITH ASSOCIATED SWITCH, VLV CLOSED. ON ENG SHUT DOWN (DIV). DURING CRUISE, COULD NOT CLOSE NR 4 PYLOSDR UIEA200600215Check Valve · rupturedAFTER V1, NR 1 ENGINE LOOP FAULT FORWARD AND LIGHT ILLUMINATED, B-LOOP AT ENGINE PANEL AT 9.0 A-LOOP AT 6.5, VISUAL INSPECTION, LOWER BLOW DOOR OPEN. CHAPTER 5 DUCT SEPARATION INSPECTION REQUIRED ON NR 1 ENGINE. FOUND 8TH STAGE CHECK VALVE RUPTURED, REMOVED SDR UIEA200600204Controller · defectiveR1-OVERHEAT CAME ON, WOULD NOT RESET. HAD ELECTRICAL ODOR AND C/B OPENED. REMOVED AND REPLACED R1 WINDOW HEAT CONTROLLER, R1 WINDOW OPS NORMAL PER MM 30-41-00.SDR UIEA200600178Tire · separatedAIR TURN BACK DUE TO TIRE SEPARATION AFTER TO. UPON ARRIVAL MAINTENANCE FOUND ALL 4EA WHEELS ON LT BODY GEAR SEPARATED. ADDITIONAL DAMAGE FOUND TO LT BODY GEAR TRUCK ASSY, FLAP DRIVE TUBES, LOWER FUSELAGE, NR 2 VHF ANTENNA, HYDRAULIC LINES WHEEL WELL AND BODY SDR UIEA200600176Panel · crackedDURING REGULAR INSPECTION, RT WING OB MID FLAP COVER PANEL DISCOVERED CRACKED ON UNDERSIDE APPROX 4 INCH ADJACENT TO SUPPORT ARMS AT STA 862/866. REPAIRED IAW SRM 51-40-14 AND EO 4757A300.SDR UIEA200600177Panel · crackedDURING REGULAR INSPECTION, LT WING OB MID FLAP COVE PANEL DISCOVERED CRACKED ON UNDERSIDE APPROX 22 IN ADJACENT TO SUPPORT ARMS LOCATED AT STA 1100/1122. REPAIRED IAW SRM 51-40-12 AND EO 4757A301.SDR UIEA200600174Valve · damagedABORTED TAKEOFF, POOR ACCELERATION. A/C PULLING LEFT AFTER A/C STOPPED ON RUNWAY, ALL BRAKES LOCKED UP AND WOULD NOT RELEASE FOR APPROX 20 SECONDS. LEFT WING AND BODY,LEFT FRONT AND LEFT REAR IN RED SCALE 8+, PULLED VOICE RECORDER C/B. REMOVED AND REPLACED SDR UIEA200600160Unknown · malfunctionedUPON THROTTLE ADVANCE AND BRAKE RELEASE, AIRCRAFT VEERED SHARPLY TO THE RIGHT. FULL LEFT RUDDER WAS APPLIED ACFT CONT, TO VEER RT. TAKEOFF ABORTED. OPS CHECKED BRAKES, AS PER MM 32-41-15 OPS CK NORMAL. OPS CHECKED BODY GEARS STEERING AS PER MM 32-53-00. OSDR UIEA200600144Bearing · migratedPYLON NR 4 DIAGONAL BRACE LOWER SPAR FITTING BEARING MIGRATED. BEARING WAS REMOVED AND REPLACED WITH NEXT AVAILABLE OVERSIZED BEARING P/N KSC273624B-090 AS PER SRM 54-41-03 AND MM 54-10-03.SDR UIEA200600120Pdu · failedAIR TURNBACK, NR 3 LEADING EDGE FLAP LEFT WING WOULDN'T RETRACT ELECTRICALLY. PNEUMATICS WAS DISCONNECTED FOR PREVIOUS WRITE UP PAGE 597439. DUMPED 26.5 KILO OF FUEL. REMOVED AND REPLACED THE LEFT HAND NR 3 L/E PDU IAW MM 27-81-03.SDR UIEA200600087Inu · inoperativeON CLIMB, BOTH ATT LIGHTS (WARNING) ILLUMINATED WITH CAPTS ADI FROZEN, W/ATT FLAG IN VIEW, ACCOMPLISHED CK LIST PROCEDURES. SWITCHING TO ALT, NO HELP. NR 1 INS FAILED WITH WARNING LIGHT AND BLACK SCREEN. NR 3 INS DISPLAYED A WARNING LIGHT WITH ERRONEOUS G/SSDR UIEA200600076Air Data Module · inoperativeCAPT'S MACH METER YELLOW FLAG IN VIEW AFTER TAKE OFF. REMOVED AND REPLACED NR 1 CADC IAW AMM 34-12-01. OPS CHECKED OKAY. RII PERFORMED.SDR UIEA200600079Access Panel · crackedNR 2 PYLON FWD ACCESS CUT OUT FOUND CRACKED AT TOP FWD AND AFT BOTTOM AREA BETWEEN NAC STA 211.42 TO NAC STA 222.50, (LHS) (ACCESS PANEL #462AL). INTERIM REPAIRED AS PER BOEING MSG 1-168393318-4. PERFORM REPEAT DV. INSP OF SUBJECT REPAIRED AREA AT EVERY C-CHSDR UIEA200600078Support Fitting · corrodedCORROSION FOUND ON NR 4 BEARING SUPPORT FITTING, P/N 65B08410-5 BY SIAGE W/SHOP DURING LT INBD TE MID FLAP SHOP VISIT. POS 002, P/N 65B02025-35, S/N 000388. BEARING SUPPORT FITTING P/N 65B08410-5 REPAIR CARRIED OUT IAW BOEING REPAIR NR 1-168327827 BY W/SHOP. SDR UIEA200600077Bushing · corrodedCORROSION FOUND IN BUSHING BORES OF INBD FLAP TRACK ASSY NR 4 BY SIAGE WORKSHOP DURING REPAIR (SHOP VISIT) P/N 65B17064-13, S/N 0039. REPAIR CARRIED OUT IAW BOEING REPAIR NR 1-171550575 BY W/SHOP. REFER TO SWJC NR MS 130382145 AND SWJC NR E-W3LG000130382145 SDR UIEA200600075Skin · crackedNR 1 PYLON FOUND INTERIOR SKIN CRACKED AT RT SIDE BETWEEN NAC STA 248 TO NAC STA 259, BELOW RHS PRE-COOLER ACCESS CUT OUT LOWER HORIZONTAL STIFFENER. A/F INSP CARRIED OUT AS REQUIRED A/F. S/M REPAIR CARRIED OUT AS PER BOEING MESSAGE NR1-168393257-11, -16,-18SDR UIEA200600073Pylon · wrinkledNR 2 PYLON FOUND WITH WRINKLE SKIN ON RHS FWD OF PYLON VALVE MANUAL CRANK AREA. WRINKLE SKIN INSPECTION CARRIED OUT IAW BOE MSG NUMBER: 1-167645228-9, FOUND SATISFACTORY. REPEAT DETAIL VISUAL INSP EVERY C-CHK, NOT TO EXCCED 18 MONTHS.SDR UIEA200600068Skin · crackedNR 16 KRUEGER FLAT DEFECTS, P/N 65B39200-10, S/N 000296. STIFFENER CRACKS AT RTS EDGE. ALL "P" SEAL AND MOLDING SEAL WORN. MICA STRIPE CRACK. 1 LOCATION DELAMINATED AS MARKED. EXTERNAL PAINT WORK DETERIORATED. REPAIRED CARRIED OUT AS PER SWJC, MSG 63/02/SDR UIEA200600067Structure · crackedNR 15 KRUEGER FLAP DEFECTS, P/N 65B39250-2, S/N 000292, ALL "P" SEAL AND MOLDING SEAL WORN. OUTBD ARM PIVOT BEARING MIGRATED. STIFFENER CRACK AT EX-REPAIR AREA. BULL NOSE CRACK AT MID SECTION. REPAIR CARRIED OUT AS PER SWSC MSO 66/02/06, CS/020/03/06, TPAFSDR UIEA200600064Repair · unknownFOUND FUSELAGE SKIN, SECTION 46 NON-STANDARD REPAIR INSTALLED AT AFT UPPER EDGE OF MED 4R CUT OUT, BETWEEN STR 17R & 19R. C/OUT HFEC ON TRIM LINE AND EXISTING FASTENER HOLES WITH DOUBLER REMOVED, NIL FINDING. C/OUT HFEC ON FUSELAGE SKIN WITH DOUBLER AREA, NISDR UIEA200600063Bulkhead · crackedFOUND 01 OFF CRACK AT STA 400 WHEEL WELL BULKHEAD PAN ASSY LOWER RT CORNER CUT OUT RBL.15.0. CARRIED OUT EDDY CURRENT INSP, AS PER MTM PT-6 51-00-00 FIG 16 AND 23, NIL CRACK INDICATION AT THIS LINE AND FASTENER HOLES. PAN ASSY REMOVED, FOUND CRACK ON BULKHEASDR UIEA200600062Attach Fitting · crackedUPPER DECK FLOORBEAM TO FRAME CONNECTOR AT STA 340 LHS FOUND 1 OFF HOLE CRACK 3MM LONG ON FRAME WEB. CRACKED FRAME WEB REPAIRED IAW, BOEING MSG NR 1-167357676-7 DATED 10 MARCH 06. FABRICATED DOUBLER MATERIAL 2024-T3 0.080", 2 OFF FILLERS MATERIAL 2024-T3 0.0SDR UIEA200600074Seal · crackedNR 11 KRUEGER FOUND WITH FOLLOWING DEFECTS, UPPER STIFFENER FOUND CRACKED AT INBD SIDE. BULLNOSE MICA STRIP MISSING. OUTBD CURVE SEAL EDGE ON FLAP FOUND CRACKED. TORN SEAL AT TOP, AND BOTH SIDES, PN=65B39200-9, SN=000302. REPAIRED CARRIED OUT AS PER SWJC: SDR UIEA200600072Bearing · wornNR 12 KRUEGER FOUND WITH FOLLOWING: 5 OUTBD HINGE BEARING FOUND WORN. SEAL FOUND TORN AT TOP AND BOTH SIDES. REPAIRED CARRIED OUT AS PER SWJC:MSG 61/02/06.SDR UIEA200600059Frame · crackedFUSELAGE FRAME BS 480 RT FOUND WITH 1 CRACKS AT STRINGER 11 CUT OUT. CRACKED FRAME REPAIRED IAW BOEING MSG NR 1-166738303-4, DATED 03 MARCH 06. FABRICATED 2 OFF DOUBLERS MATERIAL 2024-T3 0.063" & 0.063". FABRICATED 1 OFF CUP MATERIAL 2024-T42 0.050".SDR UIEA200600058Frame · crackedFUSELAGE FRAME BS 480 LT FOUND WITH 1 CRACKS AT STRINGER 12 CUT OUT. CRACKED FRAME REPAIRED IAW BOEING MSG NR 1-166738303-4 DATED 03 MARCH 06. FABRICATED 2 OFF DOUBLERS MATERIAL 2024-T3 0.063" & 0.032" RESPECTIVELY. FABRICATED 1 OFF CUP MATERIAL 2024-T42 0.SDR UIEA200600057Frame · crackedFUSELAGE FRAME BS 500 RT FOUND WITH 2 CRACKS AT STINGER 11 CUT OUT AND 1 CRACK AT STRINGER 10A. CRACKED FRAME REPAIRED IAW BOEING MSG NR 1-1667383034 DATE 06 MARCH 06. FABRICATED 3 OFF DOUBLERS MATERIAL 2024-T3, 0.063", 0.032", 0.063" RESPECTIVELY. FABRICATSDR UIEA200600056Frame · crackedFUSELAGE FRAME BS 500 LT FOUND WITH 1 CRACKS AT STRINGER 11 CUT OUT. CRACKED FRAME REPAIRED IAW BOEING MSG NR 1-166738303-4, DATED 06 MARCH 06. FABRICATED 2 OFF DOUBLERS MATERIAL 2024-T3 0.63" & 0.032" RESPECTIVELY. FABRICATED 1 OFF CUP MATERIAL 2024-T42 0.SDR UIEA200600055Frame · crackedFUSELAGE FRAME BS 520 RT FOUND WITH 2 CRACKS AT STRINGER 11 CUT OUT. CRACKED FRAME REPAIRED IAW BOEING MSG NR 1-166738303-4. DATE 06 MARCH 2006. FABRICATED 03 OFF DOUBLERS MATERIAL 2024-T3.(0.063",0.032",0.063" RESPECTIVELY). FAB 1 OFF CUP MATERIAL 2024-T3 SDR UIEA200600060Beam · crackedLT WING FIXED LEADING EDGE NOSE BEAM CAP LOWER SKIN FOUND CRACKED AROUND FASTENERS AT ILES 630. LHW FIXED LEADING EDGE SKIN AT ILES 630. CRACKED REPAIRED AS PER BOEING MSG 1-166123104-2,FAA FORM 8100-9 DATED 24 MARCH 2006.SDR UIEA200600071Panel · crackedLWR RUDDER SENT TO W/SHOP FOR THE FOLLOWING REPAIRS, LOWER CLOSURE PANEL BONDED STIFFENER FOUND BADLY WORN AT SEVERAL LOCATION. LOWER MOST FWD RIB FOUND CRACKED. LOWEST HINGE BEARING COVER MISSING PART NR 65B05501-1 S/N NSN. REPAIRED RUDDER INSTALLED IAW AMSDR UIEA200600050Skin · crackedLT WING LEADING EDGE FIXED BULLNOSE, FOUND CRACKED AT BOTTOM CUT-OUT, AT NR 12 KRUEGER INBD LINKAGE MOUNTING AREA. ILES 445 LOWER BEAM. LHW LOWER BEAM CRACK REPAIRED AS PER BOEING MSG. 1-168482122-2 AND FAA 8100-9 DATED 20 MARCH 2006.SDR UIEA20060052Mount · crackedRHW NR 15 KRUEGER FLAP TOP MOUNTING POINT (O/B) CUT OUT AT LEADING EDGE CAP, FOUND WITH HEARLINE CRACK PROPAGATING FROM FASTENER HOLE (LWR BEAM), ILES 514. RHW LOWER BEAM CRACK REPAIRED AS PER BOEING MSG 1-168482122-2, AND FAA 8100-9 DATED 20 MARCH 2006.SDR UIEA200600053Access Panel · crackedNR 1 PYLON ACCESS PANEL CUT-OUT FOUND CRACKED AT LOWER AFT SIDE FWD OF NAC STA 291.5 (ACCESS PANEL 453AL). ACCESS PANEL 453AL CUT-OUT CRACK REPAIRED AS PER BOEING MSG, NR 1-167526498-2 AND FAA FORM 8100-9, DATED 15 MARCH 2006 TO CONDUCT DETAIL VISUAL INSPECTISDR UIEA200600054Access Panel · crackedNR 1 PYLON ACCESS PANEL CUT-OUT FOUND CRACKED AT LOWER AFT SIDE FWD OF NAC STA 248 (ACCESS PANEL 452DL). ACCESS PANEL 452DL CUT-OUT CRACK REPAIRED AS PER BOEING MSG, NR 1-167526498-2 AND FAA FORM 8100-9, DATED 15 MARCH 2006 TO CONDUCT DETAIL VISUAL INSPECTIONSDR UIEA20060053Access Panel · crackedNR 1 PYLON ACCESS PANEL CUT-OUT FOUND CRACKED AT LOWER AFT SIDE FWD OF NAC STA 291.5. (ACCESS PANEL 453AL). ACCESS PANEL 453AL CUT-OUT CRACK REPAIRED AS PER BOEING MSG, NR 1-167526498-2 AND FAA FORM 8100-9 DATED 15 MARCH 2006, TO CONDUCT DETAIL VISUAL INSPECTSDR UIEA200600045Clamp · brokenFIRE WARNING AT 70KTS. A/C RETURNED TO BLOCKS. ON POST FLIGHT INSPECTION FOUND NR 3 BOTTOM DOOR OPEN, & INBOARD PYLON DOOR OPEN. FOUND HP VALVE LOWER CLAMP OFF POSITION, ADJUSTED DUCTS AND REPLACED LOWER CLAMP AS PER MM 36-11-05. LEAK CHECK OK.SDR UIEA200600019Seat Track · brokenMAIN DECK CARGO COMPT, SEAT TRACK IS MISSING TWO TABS BY THE MAIN CARGO DOOR BS 1800. REPLACED SEAT TRACK PER SRM 53-10-05 AND EO4753A686.SDR UIEA200600016Panel · crackedNR 6 SPOILER HAS A SMALL CRACK AT OUTBOARD SIDE OF ACTUATOR HINGE FITTING ,1ST ROW, FWD HI-LOK, FROM DOUBLER EDGE TO HI-LOK. REMOVED AND REPLACED NR 6 SPOILER PANEL ASSY AS PER 747 MM 27-62-01.
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