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 U2RA201702260001Fire Detector · false activationFWD CARGO FIRE INDICATION DURING LANDING DECELERATION, EICAS MESSAGE AND FIRE BELL, SITUATION RESET ITSELF AND STOPPED AFTER RUNWAY EXIT. CHECKED FORWARD CARGO FOR SIGNS OF FIRE OR SMOKE, NONE FOUND. PERFORMED FIRE AND SMOKE DETECTION GROUND TEST IAW AMM SDR U2RA201705200001Ballscrew · brinelledDURING INSPECTION REQUIRED BY AD 2006-10-02 FOUND HORIZONTAL STABILIZER BALLSCREW TO HAVE INDICATIONS OF BRENELLING IN THE NEUTRAL ZONE AREA OF THE BALLSCREW THREADS. REMOVED AND REPLACED HORIZONTAL STABILIZER BALLSCREW IN ACCORDANCE WITH AIRCRAFT MAINTENANCE SDR U2RA201706090005Scuff Plate · crackedDURING ACCOMPLISHMENT D CHECK INSPECTION, FOUND BULK CARGO DOOR SCUFF PLATE CRACKED. PERFORMED WELD REPAIR OF BULK CARGO DOOR SCUFF PLATE IN ACCORDANCE WITH ENGINEERING INSTRUCTIONS MAS-J217-N919CA-002-1 AND SRM 53-00-15-2R-15 REPAIR 5.SDR U2RA201705120002Skin Panel · looseRIGHT HAND HORIZONTAL STABILIZER LOWER SURFACE AT STATION 440 JUST AFT OF LEADING EDGE HAS REPAIR WITH AREA OF PEELING PAINT AND POSSIBLE LOOSE FASTENERS. REMOVED AND REPLACED PREVIOUS REPAIR IN ACCORDANCE WITH SRM 55-10-01-2R-6. APPLIED PAINT TOP COAT.SDR U2RA201702150001Strap · crackedTENSION TIE STRAPS AT BS 1140 LEFT HAVE TWO CRACKS. REMOVED AND REPLACED THE TENSION TIE STRAPS IAW SRM 51-40-02 PAGES 4-7 AND SB 747-53A2507 REVISION 2.SDR U2RA201705110002Doubler · crackedDURING "D' CHECK INSPECTION FOUND EXTERNAL FUSELAGE SKIN REPAIR DOUBLER BETWEEN BODY STATION 720-741 AND STRINGERS 46 LEFT AND 47 LEFT WITH CRACK. - REMOVED AND REPLACED EXTERNAL FUSELAGE SKIN DOUBLER AT BODY STATION 720-741 BETWEEN STRINGERS 46 LEFT AND 47 LESDR U2RA201706140001Channel · crackedDURING ACCOMPLISHMENT D CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER UPPER AND LOWER FLANGE CRACKED AT PANEL OPENING FOR ACCESS PANEL 336QBL AT LEFT HAND HORIZONTAL STABILIZER TIP OTBD AFT CORNER. REMOVED AND REPLACED THE CHANNEL IAW DRAWING 65B03710 ASDR U2RA201705110001Strap · corrodedDURING "D' CHECK INSPECTION FOUND RIGHT WING LEADING EDGE AT 640 ILES UPPER CHORD STRAP WITH CORROSION. REMOVED AND REPLACED RIGHT WING UPPER CHORD STRAP AT 640 ILES IN ACCORDANCE WITH DRAWING NUMBER 65B14548 AND SRM 51-40-02.SDR U2RA201701310004Frame · crackedPREVIOUS TENSION TIE ATTACH LOCATION AT BS 1160 FRAME WEB HAS TWO PREVIOUS FASTENER HOLES CRACKED. ACCOMPLISHED OVERSIZE HOLE REPAIR IAW SERVICE BULLETIN 747-53A2507 REVISION 2.SDR U2RA201701310003Tension Tie · crackedTENSION TIE AT BS 1200 FRAME CRACKED. ACCOMPLISHED OVERSIZE HOLE REPAIR IAW SERVICE BULLETIN 747-53A2507 REVISION 2.SDR U2RA201701310002Tension Tie · crackedTENSION TIE AT BS 1160 RIGHT SIDE, FOUND CRACKED. REPAIRED IAW SERVICE BULLETIN 747-53A2507 REVISION 2.SDR U2RA201701310001Tension Tie · crackedTENSION TIE AT BS 1120 CRACKED. PERFORMED OVER SIZE HOLE REPAIR IAW SERVICE BULLETIN 747-53A2507 REVISION 2.SDR U2RA201701300003Pin · wornMAIN DECK SIDE CARGO DOOR MID FRAME AFT LATCH WORN. REMOVED AND REPLACED THE LATCH PIN IAW AMM 52-32-24.SDR U2RA201701300002Pin · wornMAIN DECK SIDE CARGO DOOR MID FRAME FORWARD LATCH PIN WORN. REMOVED AND REPLACED MAIN DECK SIDE CARGO DOOR LATCH PIN IAW AMM 52-32-24.SDR U2RA201701300001Pin · wornMAIN DECK SIDE CARGO DOOR FORWARD LATCH PIN WORN. REMOVED AND REPLACED THE LATCH PIN IAW SERVICE BULLETIN 747-52A2294 REVISION 4.SDR U2RA201701290001Angle · crackedNR 4 NACELLE FIREWALL LOWER SURFACE CRACKED IN THE FAIRING SUPPORT ANGLE. REMOVED AND REPLACED NR 4 NACELLE IAW SRM 51-40-02.SDR U2RA201706150001Frame · crackedDURING ACCOMPLISHMENT OF AD 2016-05-12, AND SERVICE BULLETIN 747-53A2507 REV 2, FOUND BS 1200 LEFT FRAME TO HAVE 9 EACH FASTENER HOLES TO HAVE CRACK INDICATIONS AND 3 FASTENER HOLES ON THE TENSION TIE CHANNEL WITH CRACK INDICATIONS. ACCOMPLISHED OVERSIZE FASTSDR U2RA201706130003Skin · chafedDURING A D CHECK INSPECTION, FOUND THE NR 4 ENGINE OTBD CORE COWL WITH WEAR GROOVE AT PRE-COOLER EXHAUST DUCT OPENING. REPAIRED IAW EO MAS-J217-N919CA-004.SDR U2RA201706110001Longeron · damagedDURING ACCOMPLISHMENT D CHECK INSPECTION FOUND NUMBER 4 ENGINE INBOARD CORE COWL RIVET PULLED THROUGH LOWER EDGE. REMOVED AND REPLACED LOWER AFT SECTION AND DAMAGED FASTENERS IN ACCORDANCE WITH ENGINEERING DISPOSITION EO MAS-J217-N919CA-008 REV IR AND SRM 51-4SDR U2RA201705120001Fitting · looseDURING ACCOMPLISHMENT OF INSPECTION REQUIRED BY AIRWORTHINESS DIRECTIVE, 2012-07-07 AND SERVICE BULLETIN 747-53A2835 REVISION 1, FOUND AFT CARGO DOOR NR 1 LATCH FITTING PIN LOOSE IN THE FITTING. ACCOMPLISHED REPAIR OF THE AFT CARGO DOOR ATTACH FITTING IN ACCORSDR U2RA201701280002Frame · crackedBS 1200 FRAME AT TENSION TIE ATTACH, FOUND TO HAVE 9 FASTNER HOLES WITH CRACK INDICATIONS AND THE TENSION TIE CHANNEL WAS FOUND TO HAVE 3 FASTENER HOLES WITH CRACK INDICATIONS. - PERFOMED OVERSIZE HOLE REPAIR AT ALL CRACKED FASTENER HOLE LOCATIONS IN ACCORDANCSDR U2RA201701280001Frame · crackedBS 1200 LEFT FRAME TENSION TIE ATTACH POINT CRACKED. PERFOMED OVERSIZE HOLE REPAIR OF CRACKED FASTENER HOLES IAW SERVICE BULLETIN 747-53A2507 REVISION 2.SDR U2RA201706130002Duct · chafedDURING A D CHECK INSPECTION, FOUND THE NR 2 ENGINE INBOARD CORE COWL WITH WEAR GROOVE AT PRE-COOLER EXHAUST DUCT OPENING. REPAIRED CORE COWL PRE-COOLER EXHAUST DUCT IAW EO MAS-J217-N919CA-004.SDR U2RA201706090006Stiffener · crackedDURING ACCOMPLISHMENT D CHECK INSPECTION, FOUND RIGHT WING TRAILING EDGE VERTICAL STIFFENER CRACKED ON UPPER END AT OUTBOARD SIDE OF #8 SPOILER. REMOVED AND REPLACED RIGHT WING TRAILING EDGE VERTICAL STIFFENER IAW SRM 51-40-01.SDR U2RA201705210003Support Rib · chafedDURING "D" CHECK INSPECTION FOUND, NUMBER 4 ENGINE OUTBOARD THRUST REVERSER, FIRE SUPPORT RIB WITH WEAR DAMAGE. REPAIRED RIB BY INSTALLING REPAIR DOUBLER IN ACCORDANCE WITH COMPONENT MAINTENANCE MANUAL 78-32-02.SDR U2RA201705210002Flap · delaminatedDURING "D" CHECK INSPECTION FOUND, RIGHT HAND, INBOARD, AFT FLAP, FORWARD FACE HAS AREA WITH 3 EACH DENTS WITH DELAMINATION. REPAIRED DENTED AND DELAMINATED AREAS OF RIGHT HAND INBOARD AFT FLAP, FORWARD FACE IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTERSDR U2RA201705210001Flap · puncturedDURING "D" CHECK INSPECTION FOUND, RIGHT HAND INBOARD MID FLAP, FORWARD LOWER FACE OF AFT WEDGE WITH 3 EACH PUNCTURES. REPAIRED DAMAGED AREAS OF RIGHT HAND INBOARD MID FLAP, FORWARD LOWER FACE OF WEDGE IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL CHAPTER 57-53SDR U2RA201702220001Skin Panel · dentedDURING "D' CHECK INSPECTION FOUND SCRAPE AND DENT IN FUSELAGE BELLY SKIN AT BODY STATION 820 LEFT OF BUT LINE 2 INCHES BETWEEN STRINGERS 46 LEFT AND 47 RIGHT. REPAIRED DAMAGED FUSELAGE SKIN BY INSTALLING EXTERNAL DOUBLER IN ACCORDANCE WITH SRM 53-00-01 REPAIRSDR U2RA201701250002Bearing · corrodedNR 3 PYLON OUTBOARD DUAL SIDE BRACE UPPER BEARING RACE CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE BEARING IAW SERVICE BULLETIN 747-54A2218.SDR U2RA201701250001Fitting · crackedRIGHT WING TRAILING EDGE SUPPORT ROD ATTACH FITTING CRACKED AT OUTBAORD SIDE OF THE NR 8 GROUND SPOILER. REMOVED AND REPLACED FITTING IAW SRM 51-40-02SDR U2RA201701240001Battery Pack · depletedRIGHT UPPER DECK DOOR FAILS BATTERY CHECK AND PRESSURE CARTRIDGE TEST DC VOLTS LOW. REMOVED AND REPLACED BATTERY POWER PACK IAW AMM 52-23-14.SDR U2RA201705210004Flap · chafedDURING "D" CHECK INSPECTION FOUND, LEFT HAND OUTBOARD FORE FLAP WITH DAMAGE ON OUTBOARD LEADING EDGE. REPAIRED LEFT HAND OUTBOARD FORE FLAP LEADING EDGE IAW STRUCTURAL REPAIR MANUAL CHAPTER 57-53-01 REPAIR 1 AND 51-70-07.SDR U2RA201706090008Duct · damagedDURING ACCOMPLISHMENT D CHECK INSPECTION FOUND APU COOLING AIR DUCT WITH 3/4 INCH HOLE. REPAIRED APU COOLING AIR DUCT IN ACCORDANCE WITH ENGINEERING INSTRUCTIONS EO MASJ217-N919CA-006 AND AMM 21-51-12.SDR U2RA201705240001Link · corrodedDURING "D" CHECK INSPECTION FOUND, RIGHT WING LEADING EDGE CAVITY RIB SUPPORT LINK CORRODED AT AFT END, WING STATION OLES 1522. REMOVED AND REPLACED RIB SUPPORT LINK IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 51-40-02 AND AIRCRAFT MAINTENANCE MANUAL 20-51-01SDR U2RA201611280001Nose Cowl · chafedINLET COWL, COWL TO STRUT MATING FLANGE SURFACE AT 12 O'CLOCK POSITION WORN. ACCOMPLISHED INTERIM REPAIR IAW EO 5410ERO2253.SDR U2RA201610020001Battery Pack · dischargedUPPER DECK, AISLE, STAIRWAY, AND COCKPIT EMERGENCY LIGHTS DO NOT OPERATE DURING TEST. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-04. OPS TEST SATISFACTORY.SDR U2RA201606100001Winglet · damagedLEFT WINGLET TIP FOUND WITH ONE EACH LIGHTNING STRIKE. ACCOMPLISHED REPAIR OF LT WING WINGLET TE WEDGE CASTING IAW ENGINEERING REPAIR ORDER 5730ERO2161.SDR U2RA201606060001Support Frame · crackedRT WING TO BODY FAIRING 192K SUPPORT FRAME CRACKED. R & R SUPPORT FRAME IAW SRM 51-40-02.SDR U2RA201606030002Frame · crackedRT BODY STATION 1265 FRAME INNER CHORD FOUND WITH 1 CRACK MEASURING 0.030". ACCOMPLISHED REPAIR MODIFICATION OF BODY STATION 1265 CHORD IAW SB 747-53A2416.SDR U2RA201606040001Bracket · crackedRIGHT WING T/E SPAR CAVITY NR 8 SPOILER ACTUATOR INBD LOWER AREA HAS ONE CRACKED BRACKET. R & R BRACKET IAW SRM 51-40-02.SDR U2RA201606030003Skin · dentedAFT CARGO DOOR FORWARD LOWER SKIN EDGE FOUND WITH DENT. REPAIRED AFT CARGO DOOR SKIN BY INSTALLATION OF EXTERNAL DOUBLER IAW SRM 52-30-01, REPAIR 2, FIGURE 201.SDR U2RA201606150003Support Angle · crackedAFT LOWER CARGO COMPARTMENT AT BS 1625 RT OF BUTTLINE 25 POWER DRIVE UNIT SUPPORT ANGLE CRACKED. R & R SUPPORT ANGLE IAW SRM 51-40-02.SDR U2RA201606150002Support Angle · crackedAFT LOWER CARGO COMPARTMENT AT BS 1534 LT OF BUTT LINE 25 POWER DRIVE UNIT SUPPORT ANGLE CRACKED. R & R SUPPORT ANGLE IAW SRM 51-40-02.SDR U2RA201606020002Skin · damagedFOUND FUSELAGE SKIN AT STA 720-740 BETWEEN STR 25L AND 26L WITH BLEND OUT IN CLOSE PROXIMITY TO PREVIOUS EXTERNAL SKIN REPAIR. ACCOMPLISHED EXTERNAL SKIN DOUBLER REPAIR IAW SRM 53-00-01, REPAIR 15, FIGURE 201.SDR U2RA201606020001Skin · dentedFOUND DENT AND BLEND OUT IN CLOSE PROXIMITY ON SKIN NEAR BODY STA 560 BETWEEN STR 35R AND 36R. REPAIR WAS ACCOMPLISHED IAW EB-53-2543 IN REF TO SERVICE REQUEST 3-3617438202. THE REPAIR METHOD HAS BEEN APPROVED.SDR U2RA201606030001Scupper · crackedLEFT STA 1480, AFT BODY SCUPPER CRACKED. R & R SCUPPER IAW SRM 51-40-02.SDR U2RA201606150001Support Angle · crackedFORWARD LOWER CARGO COMPARTMENT AT BS 935 LEFT OF BUTT LINE 25 POWER DRIVE UNIT SUPPORT ANGLE CRACKED. R & R SUPPORT ANGLE IAW SRM 51-40-02.SDR U2RA201606010001Support Frame · crackedLOWER FUSELAGE RT FIXED PANEL 192K SUPPORT FRAME FOUND WITH CRACK. R & R SUPPORT FRAME IAW SRM 51-40-02.SDR U2RA201604090001Light · inoperativeEMERGENCY LIGHT INOPERATIVE FORWARD OF GULL WING DOORS. R & R EMERGENCY LIGHT FORWARD OF GULL WING DOOR IAW AMM 33-51-07.SDR U2RA201604060001Trunnion · corrodedNOSE LANDING GEAR LT AND RT TRUNNION END CAPS HAVE CORROSION. REPAIRED LT AND RT NLG TRUNNIONS BY MACHINE BORING IAW SRM 53-10-90-2R-1.
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