Boeing 747-428
Service difficulty reports · 496
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 = '747428' 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 = '747428' 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 U2RA201811180001Panel · delaminatedRIGHT WING LEADING EDGE PANEL FOUND DELAMINATED. REMOVED AND REPLACED RIGHT WING LEADING EDGE PANEL IAW SRM 51-40-02.SDR U2RA201811120001Adc · faultyRIGHT TRANSPONDER ALTITUDE REPORTING IN ERROR, AS REPORTED BY AIR TRAFFIC CONTROL. TROUBLESHOOTING REVEALED THE ERROR WAS CAUSED BY THE BY THE LEFT DIGITAL AIR DATA COMPUTER. THE LEFT DIGITAL AIR DATA COMPUTER WAS FOUND TO BE READING 250 FOOT HIGH. THE LEFT DSDR U2RA201811090002Stringer · crackedNUMBER 7 VARIABLE CAMBER FLAP ATTACHMENT STRINGER HAS 1 EACH CRACK. REPLACED VARIABLE CAMBER FLAP ASSEMBLY PER AIRCRAFT MAINTENANCE MANUAL 27-81-02.SDR U2RA201811090001Stringer · crackedNUMBER 20 VARIABLE CAMBER FLAP ATTACHMENT STRINGER HAS 1 EACH CRACK. REPLACED CRACKED STRINGER PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-02.SDR U2RA201810240001Rib · crackedRIGHT HAND LEADING EDGE SUPPORT RIB FOUND CRACKED 0.70 INCHES AT ILES 330. REPLACED RIB PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-05.SDR U2RA201809280002Rib · crackedRIGHT HAND WING LANDING GEAR INBOARD WHEEL WELL DOOR, FORWARD EDGE FOUND 1 EACH 1.2 INCH CRACK. REPAIRED PER DRAWING 52-18298-1 REVISION NEW, DATED OCTOBER 08, 2018.SDR U2RA201809280001Stiffener · crackedLEFT HAND WING INTERIOR OF PANEL 511CTA, INBOARD CORNER VERTICAL STIFFENER HAS 1.5 INCH CRACK. REPLACED VERTICAL STIFFENER PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-05.SDR U2RA201809270006Skin · deformedRIGHT HAND WING LEADING EDGE SKIN OUTBOARD OF LANDING LIGHT HAS TILTED FASTENERS. REPAIRED PER STRUCTURAL REPAIR MANUAL 57-41-01-2R-5.SDR U2RA201809270005Filler · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL, ON THE RIGHT HAND ENTRY DOOR NUMBER 5 AFT UPPER CORNER CUTOUT, 3 EACH 0.10 INCH CRACKS WERE DISCOVERED ON FILLER. ACCOMPLISHED SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL PART 5 - PREVSDR U2RA201809270004Strap · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL, ON THE RIGHT HAND ENTRY DOOR NUMBER 5 AFT UPPER CORNER CUTOUT, 2 EACH 0.125 INCH CRACKS WERE DISCOVERED. ACCOMPLISHED SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL PART 5 - PREVENTIVE MOSDR U2RA201809270003Strap · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL, ON THE LEFT HAND ENTRY DOOR NUMBER 5 AFT UPPER CORNER CUTOUT, 1 EACH 0.125 INCH CRACK WAS DISCOVERED. ACCOMPLISHED SERVICE BULLETIN 747-53A2839 REVISION ORIGINAL PART 5 - PREVENTIVE MODIFSDR U2RA201809270002Web · crackedRIGHT HAND LEADING EDGE SUPPORT WEB LOWER FLANGE FOUND CRACKED 0.50 INCHES AT WING LEADING EDGE STATION 330.0. REPLACED WEB PER STRUCTURAL REPAIR MANUAL 51-40-02.SDR U2RA201809270001Doubler · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2651 REVISION 1 STATION 2403.6 TO STATION 2524.4, UPPER LOBE DOUBLER AT THE FUSELAGE VERTICAL STABILIZER ATTACH FITTINGS INSPECTION, A 2 INCH CRACK WAS DISCOVERED ON THE RIGHT HAND SIDE, FROM STATION 2519 TO 252SDR U2RA201809260001Frame · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2416 REVISION 3. FUSELAGE CENTER SECTION BODY STATION 1265 FRAME INSPECTION, REPAIR, AND MODIFICATION, FLOOR INTERCOSTAL. FRAME INNER CHORD ON RIGHT SIDE WAS FOUND CRACKED. ACCOMPLISHED MODIFICATION PER SERVICE SDR U2RA201809250009Skin Panel · corrodedRIGHT HAND WING TRAILING EDGE OUTBOARD FORE FLAP HAS 2 EACH AREAS OF CORROSION ON LOWER SKIN PANEL. CORROSION CLEANUP OUTSIDE OF STRUCTURAL REPAIR MANUAL LIMITS. REPLACED RIGHT HAND WING TRAILING EDGE OUTBOARD FORE FLAP PER AIRCRAFT MAINTENANCE MANUAL 27-51-0SDR U2RA201809250008Attach Bracket · crackedRIGHT HAND WING TRAILING EDGE CAVITY PANEL SUPPORT BEAM AFT END ATTACH BRACKET CRACKED. REPLACED BRACKET PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-02.SDR U2RA201809250007Stringer · crackedNUMBER 7 VARIABLE CAMBER FLAP LOWER CENTER STRINGER CRACKED. REPLACED CRACKED STRINGER PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-02.SDR U2RA201809250006Stringer · crackedNUMBER 20 VARIABLE CAMBER FLAP LOWER CENTER STRINGER CRACKED. REPLACED CRACKED STRINGER PER STRUCTURAL REPAIR MANUAL 51-10-02 AND 51-40-02.SDR U2RA201809250005Skin · damagedRIGHT HAND BODY LANDING GEAR INBOARD STRUT DOOR INTERIOR SKIN FOUND TO HAVE RIVETS LOOSE AND HOLES ENLARGED. REPAIRED PER DRAWING 52-18315-1.SDR U2RA201809250004Skin · wornLEFT HAND BODY LANDING GEAR INBOARD STRUT DOOR INTERIOR SKIN FOUND TO HAVE RIVETS LOOSE AND HOLES ENLARGED. REPAIRED PER DRAWING 52-18303-1.SDR U2RA201809250003Skin · damagedRIGHT HAND WING LEADING EDGE SKIN RIVETS LOOSE AND HOLES ELONGATED AT ILES 693.5. REPAIRED PER FLIGHT VEHICLES CONSULTING DRAWING NUMBER 57-18290-1 DATED 10/05/2018.SDR U2RA201809250002Power Supply · inoperativeEMERGENCY LIGHTS L1853, L1854, AND L5735 ARE INOPERATIVE (MAIN DECK LEFT DOOR). REPLACED EMERGENCY LIGHT BATTERY PACK ASSEMBLY PER AIRCRAFT MAINTENANCE MANUAL 33-51-04. LIGHTS OPERATE NORMAL.SDR U2RA201809250001Power Supply · inoperativeUPPER DECK RIGHT HAND DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY SUPPLY ASSEMBLY PER AIRCRAFT MAINTENANCE MANUAL 31-31-04. LIGHT OPERATES NORMAL.SDR U2RA201809240002Reservoir · low pressureRIGHT HAND UPPER DECK DOOR SLIDE RESERVOIR HAS LOW PRESSURE. RESERVOIR REPLACED PER AIRCRAFT MAINTENANCE MANUAL 25-68-02.SDR U2RA201809110001Sign · damagedUPPER DECK EMERGENCY EXIT SIGN DAMAGED. REPLACED EMERGENCY EXIT SIGN ASSEMBLY PER AIRCRAFT MAINTENANCE MANUAL 33-51-00.SDR U2RA201807220001Frame · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2494 REVISION 2 FOUND FRAME AFT INNER CHORD AT STATION 2230 RT R5 DOOR CRACKED. ACCOMPLISHED FRAME INNER CHORD CRACK REPAIR IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 53-60-07 REPAIR 7.SDR U2RA201807260002Door Frame · crackedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 747-53A2494 REVISION 2 FOUND FRAME AFT INNER CHORD AT STATION 2231 LEFT HAND R5 DOOR CRACKED. ACCOMPLISHED FRAME INNER CHORD CRACK REPAIR IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 53-60-07 REPAIR 7.SDR U2RA201807230001Support Frame · crackedLEFT SIDE AIRCONDITIONING BAY, AFT UPPER BODY FAIRING SUPPORT FRAME IS CRACKED AT THE ANGLE. REPAIRED FAIRING SUPPORT FRAME IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 53-00-71-2R-1 AND 51-70-11.SDR U2RA201807260001Support Rib · crackedLEFT WING TRAILING EDGE SUPPORT RIB WEB AT WBL 255.692 INBOARD OF THE NR 6 SPOILER IS CRACKED. REMOVED CRACKED WEB, FABRICATED NEW LAMINATED WEB IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 57-51-02-01-1 IDENTIFICATION AND INSTALLED NEW WEB IN ACCORDANCE WITH SDR U2RA201803250001Hose · leakingDURING DECENT TO APPROACH, THE NR 1 HYDRAULIC SYSTEM FAILED DUE TO FLUID LEAK. FOUND THE NR 1 HYDRAULIC SYSTEM AIR DRIVEN DEMAND HYDRAULIC PUMP PRESSURE HOSE LEAKING. REMOVED AND REPLACED THE HYDRUALIC PRESSURE HOSE IIAW MM 29-11-17, 29-11-23, AND 20-1SDR U2RA201802140001Seat Track · damagedDAMAGED SEAT TRACK BS 1915 - 1918, RBL 25.75, WL 118. ACCOMPLISHED INTERIM REPAIR EO 53-18042.SDR U2RA201711270001Closeout Panel · missingDURING LEVEL FLIGHT, DETECTED A SUDDEN MEDIUM FREQUENCY VIBRATION. AIRSPEED WAS REDUCED AND VIBRATION STOPPED. FOUND THE NUMBER 11 KRUEGER FLAP OUTBOARD SEAL PANEL UNDER LEFT WING AT APPROXIMATELY WS 614 TO 642 LEADING EDGE AREA TO BE MISSING. PERFORMED AIRSDR U2RA201710100001Actuator · inoperativeDURING FLIGHT, RECEIVED EICAS MASSEAGE FOR DOOR U/D FLT LOCK MESSAGE REMAINED UNTIL LANDING. TROUBLESHOT ECIAS MESSAGE, FOUND RIGHT UPPERDECK DOOR FLIGHT LOCK ACTUATOR INOPERATIVE.SDR U2RA201709160001Battery Pack · no testLEFT UPPER DECK EMERGENCY EXIT DOOR, EMERGENCY DEPLOY BATTERY DOES NOT TEST. REMOVED AND REPLACED THE BATTERY IAW AIRCRAFT MAINTENANCE MANUAL 52-23-14.SDR U2RA201707130001Battery Pack · dischargedEMERGENCY EXIT LIGHT ABOVE RIGHT UPPER DECK EMERGENCY EXIT DOOR, L1 AND R1 MAIN DECK DOORS WON'T ILLUMINATE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-04. PERFORMED SATISFACTORY OPERATIONAL CHECK.SDR U2RA201706240001Sleeve · damagedNUMBER 3 ENGINE INBOARD THRUST REVERSER SLEEVE DAMAGED, WITH HONEYCOMB EXPOSED AT THE 9 O'CLOCK POSITION. - INTERIM REPAIR OF NUMBER 3 ENGINE INBOARD THRUST REVERSER TRANSLATING SLEEVE ACCOMPLISHED IN ACCORDANCE WITH FLIGHT VEHICLES CONSULTING, INC. DRAWING NUSDR U2RA201706090004Web · crackedDURING ACCOMPLISHMENT A D CHECK INSPECTION, FOUND RIGHT WING TRAILING EDGE SUPPORT RIB WEB CRACKED AT INBOARD SIDE OF THE NR 7 GROUND SPOILER. - REMOVED AND REPLACED RIGHT WING TRAILING EDGE SUPPORT RIB WEB IAW SRM 51-40-02.SDR U2RA201705130002Power Supply · no testLEFT UPPER DECK DOOR EMERGENCY POWER SYSTEM WILL NOT TEST. REPLACED THE LT POWER SUPPLY IAW AMM 33-51-04. OPS CHECKED GOOD.SDR U2RA201705130001Power Supply · no testRIGHT UPPER DECK DOOR, EMERGENCY POWER SYSTEM WILL NOT TEST. REPLACED THE RT POWER SUPPLY IAW AMM 33-51-04. OPS CHECKED GOOD.SDR U2RA201706090009Structure · crackedDURING ACCOMPLISHMENT D CHECK INSPECTION FOUND LEFT HORIZONTAL STABILIZER LOWER CHORD CRACKED AT APPROXIMATE HTSA BUTT LINE 421 OUTBOARD END. REPAIRED LEFT HORIZONTAL STABILIZER LOWER CHORD IN ACCORDANCE WITH SRM 51-70-12.SDR U2RA201705200007Rib · crackedDURING "D" CHECK INSPECTION FOUND LEFT HAND HORIZONTAL STABILIZER TIP FAIRING RIB P/N 65B03521-17 CRACKED. REPAIRED LEFT HAND HORIZONTAL STABILIZER FAIRING RIB IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 55-10-30 AND 51-70-11.SDR U2RA201705200006Rib · crackedDURING "D" CHECK INSPECTION FOUND LEFT HAND HORIZONTAL STABILIZER TIP FAIRING RIB P/N 65B03521-019 CRACKED. REPAIRED LEFT HAND HORIZONTAL STABILIZER FAIRING RIB IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 55-10-30 AND 51-70-11.SDR U2RA201705200005Rib · crackedDURING "D" CHECK INSPECTION FOUND LEFT HAND HORIZONTAL STABILIZER TIP FAIRING RIB P/N 65B03521-013 CRACKED. REPAIRED LEFT HAND HORIZONTAL STABILIZER FAIRING RIB IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 55-10-30 AND 51-70-11.SDR U2RA201705200004Rib · crackedDURING "D" CHECK INSPECTION FOUND LEFT HAND HORIZONTAL STABILIZER TIP FAIRING RIB P/N 65B03521-9 CRACKED. REPAIRED LEFT HAND HORIZONTAL STABILIZER FAIRING RIB IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 55-10-30 AND 51-70-11.SDR U2RA201705200003Rib · crackedDURING "D" CHECK INSPECTION FOUND LEFT HAND HORIZONTAL STABILIZER TIP FAIRING RIB CRACKED. - REPAIRED LEFT HAND HORIZONTAL STABILIZER FAIRING RIB IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 55-10-30 AND 51-70-11.SDR U2RA201706090007Rib · crackedDURING ACCOMPLISHMENT D CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER TIP RIB CRACKED. REPAIRED THE RIB IAW SRM 51-70-11.SDR U2RA201704080001Sleeve · damagedDAMAGE FOUND ON THE NR 4 ENGINE THRUST REVERSER OUTBOARD SLEEVE. ACCOMPLISHED A TIME LIMITED REPAIR IAW DRAWING 54-17042-1.SDR U2RA2017060800001Web · gougedDURING ACCOMPLISHMENT OF D CHECK INSPECTION FOUND RIGHT HAND OUTBOARD ELEVATOR INBOARD WEB GOUGED. REMOVED AND REPLACED RIGHT HAND OUTBOARD ELEVATOR INBOARD WED IN ACCORDANCE WITH SRM 51-40-02.SDR U2RA201706080001Hinge Fitting · wornDURING ACCOMPLISHMENT OF D CHECK INSPECTION FOUND RIGHT HAND OUTBOARD ELEVATOR NR 3 HINGE BEARING LOOSE IN FITTING. REMOVED AND REPLACED RIGHT HAND OUTBOARD ELEVATOR NR 3 HINGE FITTING AND BEARING IN ACCORDANCE WITH AMM 27-31-03.SDR U2RA201706130001Fitting · wornDURING A D CHECK INSPECTION, FOUND THE NR 4 ENGINE OUTBOARD THRUST REVERSER WILL NOT LATCH DUE TO OUTBOARD THRUST REVERSER FORWARD END HANGING TO LOW. REPLACED HINGE FITTING BEARING AND REPAIRED THRUST REVERSER CENTER HINGE FITTING IAW EO MAS-J217-N919CA-007.
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