Boeing 747-124
Service difficulty reports · 1,113
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 = '747124' 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 = '747124' 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 P5CA9701443Skin · delaminatedRT INBOARD ELEVATOR OUTBOARD END OF LOWER SURFACE DELAMINATED. REPAIRED PER BOEING SRM 51-40-15.SDR P5CA9701442Skin · delaminatedLT INBOARD ELEVATOR TRAILING EDGE DELAMINATED 24 INCHES INBOARD. REPAIRED PER BOEING SRM 51-40-15.SDR P5CA9701441Skin · delaminatedRT INBOARD ELEVATOR LOWER SURFACE DELAMINATED 30 INCHES IN FROM INBOARD END. REPAIRED PER BOEING SRM 51-40-15.SDR P5CA9701440Skin · damagedLT INBOARD TRAILING EDGE MIDFLAP INBD CORNER HAS SEVERAL SMALL HOLES. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9701438Panel Door · delaminatedNR 3 PYLON 473 CL PANEL DOOR DELAMINATED. REPAIRED PER BOEING SRM 51-40-06.SDR P5CA9701439Skin · damagedBS 1940 S48 TO S47 R SKIN CREASED. FILLER AND DOUBLER INSTALLED PER BOEING SRM 53-30-03.SDR P5CA9701374Skin · crackedGROUND DAMAGE FOUND ON BOTTOM OF FUSELAGE AREA BELOW REAR CARGO DOOR BS 1980 BETWEEN S46R TO S50L, DEEPEST GOUGE APPROXIMATELY .025 AT S49R WHERE CRACK IN SKIN DETECTED BY HFEC CHECK. REPAIRED CRACK PER BOEING SRM 53-30-03 FIGURE 1 BLENDED GOUGES PER 51-10-01SDR P5CA9701295Bull Nose · missingON POST FLIGHT, FOUND NR 6 LEADING EDGE FLAP BULL NOSE MISSING. AIRCRAFT DISPATCHED PER CDL 27-81-3. BULL NOSE TO BE REPLACED.SDR P5CA9701187Fuel Control · failedDURING CRUISE FLIGHT, NR 2 ENGINE STALLED. ALL INDICATIONS SHOWED THRUST LOSS. ATTEMPTED RESTART, ENGINE DID RELIGHT BUT DID NOT STABILIZE. ACCOMPLISHED ENGINE SHUT DOWN PROCEDURE. POSITIVE OIL PRESSURE AT ALL TIMES. FCU CYCLED 1 MIN EACH 30 MIN. REMOVEDSDR P5CA9701096Spar Chord · crackedFRONT SPAR LOWER CHORD CRACKS AT FSSO 1440 AND 1425 RHS. REPAIRED PERMANENTLY BY REPLACING CRACKED CHORD SECTIONS WITH NEW CHORD SECTIONS AND SPLICE STRAPS AT FSSO 1395 RHS PER RS NR 57-21-33404.SDR P5CA9701095Spar Chord · crackedFRONT SPAR LOWER CHORD CRACKS AT FSSO 1446 LHS. REPAIRED PERMANENTLY BY REPLACING CRACKED CHORD SECTION WITH NEW CHORD SECTION AND SPLICE STRAP AT FSSO 1425 LHS AS PER RS NR R-57-21-33403.SDR P5CA9701064Stringer · corrodedLEVEL 2, STRINGER 44 HEAVILY CORRODED AT STA 1860, STA 1900 AND STA 1920. ALSO, CORROSION AREA HAD BEEN CRACKED THROUGH THE STRINGER. CORROSION REMOVED, 2 STRINGER SECTIONS ARE TO BE SPLICED IN AT BS 1850 AND BS 1910, USING HALF CHANNEL SPLICE AND STRAP AT ESDR P5CA9701063Tension Tie · crackedCRACK IN MAIN DECK TENSION TIE FORWARD CHANNEL AT STA 900, LHS. TRIMMED OUT CRACK AND THE TRIM LINE WAS HFEC INSPECTED TO ENSURE NO OTHER DISCREPANCIES EXIST. ACTION CARRIED OUT PER RS NR R-53-15-33394.SDR P5CA9701062Skin · corrodedLEVEL 2, CORROSION AT BS 1720 AFTER EDGE OF MED NR 4 CUTOUT, AT TWO LOCATIONS, S-18R AND S-19R AND AT S-22R. TRIMMED OUT DAMAGED SKIN AND INSTALLED FILLER AND EXTERNAL DOUBLERS PER RS NR R53-11-33400, R-53-11-33399.SDR P5CA9701070Stringer · corrodedLEVEL 2, AFT CARGO STR 48R FOUND CORRODED AT BS 1880 TO 1890. REPAIRED STRINGER AT BS 1870 TO BS 1890 PER BOEING SRM 53-10-03.SDR P5CA9701068Bulkhead Web · corrodedLEVEL 2, LT WLG W/W CANTED BULHEAD WEB BULGED UP AT BS 1245, LBL 10. TRIMMED WEB BONDSKIN AREA 4 BY 6 AND DOUBLER REPAIRED PER BOEING SRM 51-40-02.SDR P5CA9701066Seat Track · corrodedLEVEL 2, U/D SEAT TRACK FOUND DAMAGE AT BS 520 TO BS 550 LBL 65. REPLACED SEAT TRACK AT BS 530 EXISTING SPLICE TO BS 560 PER BOEING SRM 53-10-05.SDR TWRA97133Battery Pack · dischargedDURING DAILY SERVICE, FOUND LEFT OVERWING EVAC LIGHT INOP (3RD LIGHT). REMOVED AND REPLACED BATTERY PACK. OPS CHECK OK PER MM 33-51-00. (M)SDR P5CA9701090Support · corrodedLEVEL 2, FX KEEL BEAM BOX LWR ACCESS PANEL SUPPORT BEAM FOUND CORRODED ON BS 1468 LBL 14 TO RBL 14. REPLACED SUPPORT BEAM PER BOEING SRM 51-10-01, (P/N 65B14058-1).SDR P5CA9701082Seat Track · corrodedLEVEL 2, U/D BS 530 TO BS 550 LBL 65 SEAT TRACK CORRODED ON FLANGE AREA. REPLACED SEAT TRACK AT BS 530 EXISTING SPLICE TO BS 560 PER BOEING SRM 53-10-05.SDR P5CA9701100Lower Gate · corrodedLEVEL 2, L4 DOOR LOWER GATE SEVERE CORROSION FOUND. REMOVED CORROSION PER BOEING SRM 51-10-01 AND REPROTECTED PER BOEING SRM 51-10-02. TOUCH UP PAINT PER MM 51-24-11.SDR P5CA9701099Upper Gate · crackedCRACKED REVEALED AT L3 DOOR UPPER GATE (2 EA). REINSTALLED RIVETS PER BOEING SRM 51-30-02, REMOVED AND REPLACED L3 DOOR UPPER GATE PER MM 52-11-07.SDR P5CA9701098Panel · cracked2 CRACKS REVEALED ON LOWER SURFACE ACTUATOR ATTACH FITTING O/B AREA. REPLACED NR 7 SPOILER PANEL PER MM 27-62-01.SDR P5CA9701097Panel · crackedA .5 INCH CRACK REVEALED ON ACTUATOR ATTACH HINGE FITTING I/B FILLET AREA. REPLACED NR 9 SPOILER PANEL PER MM 27-61-02.SDR P5CA9701091Strut · chafedRT WING LANDING GEAR SHOCK STRUT INNER CYLINDER O/B BRAKE EQUALIZING ROD ATTACH LUG DEEP CHAFE MARK. REF BOEING TELEX PAO-HKG-97-0008RE, 0011RE LOCAL BLENDING C/O, NDT INSPECTED SHOT PEENING AND STYLUS CADIUM PLATED. THE CYLINDER AND BRAKE ROD REQ OVERHAUL WSDR P5CA9701089Skin · corrodedLEVEL 2, RHW LOWER SKIN AT WS 966 TO WS 976 AT REAR SPAR EXTENSION CORROSION FOUND EXCEEDS BOEING SRM 57-30-01 AFTER BLENDING. REF BOEING TELEX PAO-HKG-97-0015TE FOR REPAIR.SDR P5CA9701088Spar · crackedLHW FRONT SPAR LOWER CHORD CRACK FOUND 9 INCHES LONG AT OLES 1440, REF BOEING PAO-HKG-97-0021RE FOR REPAIR.SDR P5CA9701087Spar · crackedRHW FRONT SPAR LWR CHORD CRACK FOUND 2 INCH LONG AT OLES 1430, REF BOEING PAO-HKG-97-0021RE FOR REPAIR.SDR P5CA9701086Tension Tie · crackedCABIN, TENSION TIE AT BS 900 LT SIDE CRACKED .125 INCH LONG, REF BOEING TELEX PAO-HKG-97-0010RE REPAIR SCHEME.SDR P5CA9701085Skin · corrodedLEVEL 2, CABIN R4 DOOR AFT CUTOUT SKIN CORRODED SPOTS AT 2 LOCATIONS, REF BOEING TELEX PAO-HKG-97-0005RE AND 0006RE FOR REPAIR.SDR P5CA9701084Brace · delaminatedNR 3 PYLON DIAGONAL BRACE AFT SECTION DEEP CHAFE MARK FOUND EXCEED SRM 54-40-01, REF BOEING TELEX PAO-HKG-97-0009RE FOR REPAIR.SDR P5CA9701083Angle · delaminatedNR 4 PYLON FWD ENG MOUNT BHD CHAFE MARK FOUND ON I/B RADIUS ANGLE LWR SECTION. ORIGINAL THICKNESS 0.059 REMAIN 0.046 REF BOEING TELEX PAO - HKG- 97 - 0014RE FOR REPAIR.SDR P5CA9701076Stringer · crackedM/D BS 1346 S10L STRINGER END AREA FOUND CRACKED .75 INCH LONG. REPAIRED STRINGER BETWEEN BS 1330 TO BS 1350 PER BOEING SRM 53-10-03.SDR P5CA9701075Channel · crackedM/D TENSION TIE AT BS 800 LT SIDE FOUND CHANNEL CRACKED .0625. REPAIRED TENSION TIE PER SB 747-53-2371.SDR P5CA9701073Floorbeam · corrodedLEVEL 2, U/D BS 480 RBL 42 RBL 65 FLOORBEAM FOUND CORRODED. REPAIRED FLOORBEAM AT RBL 36 TO RBL 56 PER BOEING SRM 53-10-07. ALSO BLENDED OUT AND REPROTECTED AT RBL 56 TO RBL 65 PER BOEING SRM 51-10-01.SDR P5CA9701072Fitting · crackedLHW NR 5 SPOILER ACTUATOR MOUNT FTG FOUND CRACKED AT I/B LWR SECTION LENGTH 1.5 INCHES LONG. REPLACED FITTING (P/N 65B08099-) PER DWG 65B08099.SDR P5CA9701069Tie Down Track · corrodedLEVEL 2, M/D TIE DOWN TRACK AT BS 1100 RBL 75 FOUND CRACK 4 INCHES LONG. REPLACED TIE DOWN TRACK BETWEEN BS 1090 TO BS 1210 PER BOEING SRM 53-10-05.SDR P5CA9701067Skin · wornSKIN LAP BS 520 TO BS 526 S12L EXISTING COUNTERSUNK HOLES OVERSIZED. REPAIRED SKIN LAP AT BS 520 TO BS 526 PER BOEING SRM 53-30-03.SDR P5CA9701065Trunnion · crackedNOSE LANDING GEAR LT TRUNNION FTG CRACKED ABOUT 2 INCHES LONG REVEALED AT AFT ATTACH FLANGE. REPLACED TRUNNION FTG (P/N 65B10081-7) PER DWG 65B10081.SDR P5CA9700678Skin · corrodedLEVEL 1 CORROSION, M/D SKIN LAP FAYING EDGE BS 741 TO 1000, STR R12. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02 AND MM 51-24-11.SDR P5CA9701093Skin · misdrilledU/D SKIN LAP JOINT BETWEEN BS 880 TO BS 860 FOUND MANY FASTENER HOLES FOUND INSUFFICIENT EDGE MARGIN AT S12L TOP ROW. REPAIRED SKIN LAP BETWEEN BS 880 TO BS 960 PER BOEING SRM 53-30-03.SDR P5CA9701079Skin · crackedBS 820 TO 840 S12L SKIN LAP JOINT TOP ROW FASTENER HOLES FOUND (2 EA) CRACKED. REPAIRED SKIN LAP JOINT AT BS 820 TO BS 840 SILL PER BOEING SRM 53-30-03.SDR P5CA9700836Bracket · brokenM/D BS 840 BARRIER NET LT MOST O/B VERT SUPPORT TOP ATT BRACKET BROKEN. REPLACED PER BOEING SRM 51-10-07.SDR P5CA9701014Air Inlet · crackedNR 2 AIR COND RAM AIR INLET AFT DOOR FOUND CRACKED AFTER HINGE REMOVED. REPLACED AIR INLET AFT DOOR ASSY PER MM 21-62-02.SDR P5CA9700840Floor Panel · spongyU/D BS 520 TO 600 MOST LT O/B FLOOR PNL FOUND SPONGY. REPLACED/REINSTALLED SVC TAG NR 2042412.SDR P5CA9700839Rivets · shearedNR 4 PYLON TORQUE B/HEAD STIFFENER RIVETS FOUND SHEARED. REPLACED AND DETAILED INSP AT SURROUNDING STRUCTURE CARRIED OUT NIL FURTHER DAMAGE FOUND, REF NR 867322.SDR P5CA9700838Floor Panel · spongyU/D FLOOR PNL FOUND SPONGY BET BS 520 TO 580 LBL 40 TO 65 IPC 53-21-17-01. REPLACED/REINSTALLED SVC TAG NT 2042488.SDR P5CA9700837Rib · crackedRT WING L/E CAVITY AT STA 852.45 SUPPORT RIB AFT END UPPER POSITION CRACKED. REPAIRED PER BOEING SRM 57-20-03.SDR P5CA9700577Blkhd Stiffener · sheared rivitsEIGHTEEN RIVETS SHEARED ON NR 4 PYLON AFT BULKHEAD STIFFENER AT NACELLE STATION 268.4 NACELLE WATER LINE 153.6. NEW RIVETS INSTALLED AND DETAILED INSPECTION WAS PERFORMED AT AFT BULKHEAD SUPPORTING STRUCTURE. NO OTHER DAMAGE FOUND. NOTE: PYLON MODIFICATIONSDR P5CA9701168Skin · tornLHW - I/B FORE FLAP O/B SURFACE PANEL UPPER AREA FOUND SKIN PORTION TORN OUT. REPAIRED, SKIN HOT BOND PER BOEING SRM 51-40-06.
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