Boeing 747-146
Service difficulty reports · 211
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 = '747146' 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 = '747146' 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 KCSA061502Tension Tie · crackedFUSELAGE TENSION TIE AFT C-CHANNEL IS CRACKED AT RIGHT SIDE OF FRAME CONNECTION AREA, STA 820.SDR KCSA061520Tension Tie · crackedMAIN DECK TENSION TIE HAS .375 INCH CRACK ON AFT C-CHANNEL AT B.S.900, STR-9R.SDR KCSA061515Tension Tie · crackedMAIN DECK TENSION TIE AFT C-CHANNEL HAS A .25 INCH CRACK ABOVE STR 9L.SDR KCSA061514Longeron · corrodedCORROSION ON OVERWING LONGERON I/B CHORD AT BS 1247, WL 172, RBL 116.SDR KCSA061513Tension Tie · crackedMAIN DECK TENSION TIE AFT C-CHANNEL HAS A .25 INCH CRACK AT BS 800, STR 12L.SDR KCSA061512Tension Tie · crackedMAIN DECK TENSION TIE AFT C-CHANNEL HAS .25 INCH CRACK AT BS 920, STR 9R.SDR KCSA061511Frame · crackedFOUR INCH CRACK IN FUSELAGE FRAME WEB AT BS 480, RBL 15, WL 116.SDR KCSA061510Frame · crackedTHREE INCH CRACK IN FUSELAGE FRAME WEB AT BS 480, LBL 34, WL 113.SDR KCSA061501Frame · crackedFUSELAGE FRAME IS DAMAGED AT STA 1700, BETWEEN STR 14R & 15R.SDR KCSA061500Support Bracket · crackedNR 4 PYLON INTERNAL FRAME SUPPORT BRACKET IS CRACKED AT NAC STA 270, OUTBOARD SIDE OF TOP FRAME.SDR KCSA061499Keelbeam · crackedLEFT WING GEAR WHEEL WELL KEEL BEAM WEB IS CRACKED AT STA 1305, WL 95.SDR KCSA061498Frame · crackedFUSELAGE FRAME CRACKED 3 INCHES AT BS 600, STR 6R.SDR KCSA061497Frame · crackedFUSELAGE FRAME CRACKED 5 INCHES AT BS 600, STR 7R.SDR KCSA061495Attach Angle · corrodedCORROSION ON Z-CHANNEL STIFFENER ATTACH ANGLE ON BOTTOM OF THE RT BODY WHEEL WELL PRESSURE DECK AT BS 1438, WL 190, RBL 77.SDR KCSA061496Seat Track · corrodedMAIN DECK SEAT TRACK CORRODED AT BS 1740, LBL 11.SDR KCSA061494Seat Track · corrodedSEAT TRACK CORRODED AT BS 550 TO 630 LBL 70 WL 308.SDR KCSA061493Light · inoperativeUPPER DECK RT EMERGENCY EXIT SLIDE LIGHT INOPERATIVE.SDR KCSA061351Fitting · corrodedR3 DOOR NR 6 FITTING CORRODED AND CRACKED AT STA 1270, WL 250.SDR KCSA061242Sign · inoperativeEMERGENCY EXIT SIGN ABOVE ESCAPE SLIDE INOPERATIVE..SDR 061151Battery Pack · inoperativeUPPER DECK EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK IAW B747 MM 33-51-04.SDR KCSA061150Battery Pack · inoperativeEXTERIOR SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW B747 MM 33-51-04.SDR 061040Battery Pack · inoperativeFOUND UPPER DECK EMERGENCY LIGHT INOP AT BS 540, LT. REMOVED AND REPLACED BATTERY LIGHT PACK IAW B747 MM 33-51-07.SDR 061039Battery Pack · inoperativeFOUND UPPER DECK EMERGENCY LIGHT INOP AT BS 540, RT.SDR 061038Battery Pack · inoperativeMAIN DECK EMERGENCY LIGHT INOP AT B.S.480, LT. REMOVED AND REPLACED BATTERY LIGHT PACK IAW B747 MM 33-51-07.SDR 061037Battery Pack · inoperativeMAIN DECK EMERGENCY LIGHT INOP AT BS400, LT. REMOVED AND REPLACED BATTERY LIGHT PACK IAW B747 MM 33-51-07.SDR 061034Stringer · dentedFOUND FUSELAGE STRINGER DENTED AT STA 170, RT STR 42A. REPAIRED IAW B747 SRM 53-10-03, FIG 3.SDR KCSA06004Smoke · detectedSHORTLY AFTER TAKEOFF, EXPERIENCED THICK SMOKE IN COCKPIT. PERFORMED INSPECTION TROUBLESHOOTING AND ISOLATION PROCEDURES TO ASSOCIATED EQUIPMENT IAW MM AND OTHER APPROVED DATA REFERENCES. COULD NOT DUPLICATE SMOKE CONDITION OR DETERMINE REASONABLE CAUSE FOR THSDR 03022Fire Loop · shortedSHUT DOWN NR 2 ENGINE AT 1640Z DUE TO HIGH NACELLE TEMP 8+ ON THE SCALE INDICATOR LOOP -A-. WINDMILL OIL PRESSURE 23 FOR 2 HOURS 16 MINUTES. NO RESTART ATTEMPTS WERE MADE.SDR KCS2003F00001Blade · damagedON POST FLIGHT INSPECTION, FOUND NR 1, 2, 3, AND 4 ENGINES HAD EVIDENCE OF C-1 BLADE DAMAGE. REMOVED ALL DAMAGED C-1 (N1) BLADES AND INSTALLED MATCHED SET OF C-1 BLADES ON ALL 4 ENGINES IAW MM AND ACCOMPLISHED FOD DAMAGE INSPECTION AND FOUND NO DEFECTS IAW MMSDR 2003F00057Blade · damagedON POST FLIGHT INSPECTION, FOUND NR 1, 2, 3 AND 4 ENGINES HAD EVIDENCE OF C-1 BLADE DAMAGE. REMOVED ALL DAMAGED C-1 (N1) BLADES AND INSTALLED MATCHED SET OF C-1 BLADES ON ALL 4 ENGINES IAW B747 MM 72-32-02/72-31-01 AND ACCOMPLISHED FOD DAMAGE INSPECTION AND FSDR KCS2003F00000Blade · damagedON POST FLIGHT INSPECTION, FOUND NR 1, NR 2, NR 3, AND NR 4 ENGINES HAD EVIDENCE OF C-1 BLADE DAMAGE. REMOVED ALL DAMAGED C-1 (N1) BLADES AND INSTALLED MATCHED SET OF C-1 BLADES ON ALL 4 ENGINES IAW MM AND ACCOMPLISHED FOD DAMAGE INSPECTION AND FOUND NO DEFECSDR K4HA99096Skin · crackedIAB - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP TASK CARDS, FOUND RIGHT WING LEADING EDGE SKIN AT WS 1310 AT THE UPPER EDGE INSIDE OF THE 65B12736-126, ON SKIN PANEL THERE IS A 1 INCH BY 2 INCH AREA OF SEVERE EXFOLIATED CORROSION. THREE CRACSDR K4HA99094Skin · corrosionIAB - DURING ROUTINE ACCOMPLISHMENT OF SCHEDULED C-CHECK AND CPCP CARDS, FOUND THE FLANGE OF THE ACCESS HOLES HAS MODERATE TO SEVERE CORROSION AND DETERIORATION AROUND THE PERIMETER OF THE DOOR MATING SURFACE. AREA OF CORROSION REMOVAL IS BEYOND LIMITS OF SRMSDR CKSA98541Fire Light · illuminatedNR 2 ENGINE 'B' LOOP FIRE DETECTION LIGHT ILLUMINATED, INDICATOR WENT OFF SCALE HIGH AND ERRATIC. INSPECTED LOOPS SYSTEM. OPS CHECK GOOD (TEST) IAW B747 M/M 26-11-00.SDR CKSA98517Fillet · crackedDURING PREFLIGHT, FOUND CRACK 18.5 INCHES LONG IN COMPOSITE PANEL LOCATED IN THE LOWER REAR BODY GEAR/WING TRAILING EDGE FILLET. CRACK IS DIRECTLY BEHIND THE LOWER WATER DRAIN ACCESS HATCH, IN THE LEFT OF THE AIRCRAFT CENTERLINE, BEHIND THE LEFT BODY GEAR, NESDR CKSA98516Engine · malfunctionedDURING ENGINE START, THE NR 1 ENGINE SMOKED. CLEARED AFTER A FEW MOMENTS, ALL INDICATIONS WERE NORMAL. DURING DESCENT AN OILY SMELL CAME THROUGH THE AIR CONDITIONING SYSTEM, WAS ABLE TO STOP THE SMELL BY CLOSING THE NR 1 ENGINE BLEED AIR VALVE. REMOVED AND SDR CKSA98503Wire · damagedRT AFT EMERGENCY EXIT AND FLOOR LIGHTING IS INOP. REPAIRED E PATH LIGHTING AT ZONE D AND E RT SIDE IAW BAC WDM STANDARD PRACTICE. SYSTEM OPS CHECKS NORMAL IAW B747 MM CHAPTER 33 AND 25.SDR CKSA98335Skin · dentedBS 470, SWL 118 LT (LOWER BELLY AREA) HAS A DENT L-2, W-2, D-.350, OUT OF LIMITS. CUT OUT AND REMOVED THE DAMAGED PORTION OF THE SKIN IAW B747 SRM 53-30-03. CHECK MATERIAL FOR FABRICATE SHIM AND DOUBLER 7075T6 .071, 2024T3 .063 IAW SRM 53-30-03. REPAIRED IASDR CKSA98334Frame · tornDURING ROUTINE CPCP INSPECTION, FOUND FRAME WEB TORN AT BS 1820 AND RBL 27 IN AFT CARGO COMPARTMENT FLOOR STRUCTURE. REMOVED DAMAGED AREA IAW SRM 51-10-01. MATERIAL ID 7075-T6 .025 AND 7075-T6 .040. INSTALLED REPAIR IAW SRM 53-10-04 AND 51-30-02. CORROSIONSDR CKSA98333Frame · crunchedDURING ROUTINE CPCP INSPECTION, FOUND CRUNCHED ON THE WEB FRAME OF STA 1820 IN AFT CARGO COMPARTMENT ABOVE STRINGER 51L. REMOVED DAMAGED MATERIAL DENT IAW B747 SRM 51-10-01. MATERIAL ID 7076T6 .025. DOUBLER 7075T6 .040. INSTALLED REPAIR IAW B747 SRM 53-10-SDR CKSA98332Skin · corrodedDURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, CORROSION ON THE SKIN AFT OF STA 2220 BETWEEN STRINGER 46R-47R AND STRINGER 45R-46R IN AFT CARGO COMPARTMENT. REMOVED CORROSION IAW B747 SRM 51-10-01. SKIN IS OUT OF LIMITS IAW B747 SRM 53-10-01. MATERSDR CKSA98331Skin · corrodedDURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, CORROSION ON THE SKIN AFT OF STA 2220 IN AFT CARGO COMPARTMENT BETWEEN S46L AND S45L. REMOVED CORROSION IAW B747 SRM 51-10-01 SKIN IS OUT OF LIMITS IAW B747 SRM 53-10-01. MATERIAL LOOSE BETWEEN S46L ANDSDR CKSA98330Frame · buckledDURING ROUTINE CPCP INSPECTION, FOUND FRAME WEB BUCKLED AT BS 1500 BETWEEN STRINGER 43-47 BOTH LEFT AND RIGHT SIDE IN AFT CARGO COMPARTMENT FLOOR STRUCTURE FWD SECTION. REMOVED DAMAGE IAW B747 SRM 51-40-03 LEFT SIDE. ID MATERIAL IAW B747 SRM 53-10-23 7075-T6SDR CKSA98329Skin · dentedDURING ROUTINE CPCP INSPECTION, FOUND 2.5 INCH DENT IN BS 1580 FRAME WEB SKIN DIRECTLY ABOVE S47R IN AFT CARGO COMPARTMENT FLOOR STRUCTURE FORWARD SECTION. REMOVED DAMAGED MATERIAL AND DENT IAW B747 SRM 51-10-01. MATERIAL ID FILLER 7075-T6 .025 AND DOUBLER 7SDR CKSA98328Skin · tornDURING ROUTINE CPCP INSPECTION, FOUND WEB SKIN TORN IN AFT CARGO COMPARTMENT FLOOR STRUCTURE AT BS 1720 AND RBL 54 ABOVE S44R. REMOVED DAMAGED MATERIAL IAW SRM 51-10-07. MATERIAL ID 2024-T3 .040 IAW SRM 51-40-02. INSTALLED DOUBLER IAW SRM 51-40-02 FIG 1. CSDR CKSA98327Seat Track · brokenDURING ROUTINE CPCP INSPECTION, FOUND IN UPPER DECK CABIN IN FLOOR SUPPORT BETWEEN BS 520 TO BS 540, LBL 40, WL 310 ARE BROKEN. REMOVED DAMAGED SEAT TRACK SECTION IAW B747 SRM 51-30-02. SEAT TRACK WAS FOUND OUT OF LIMITS IAW B747 SRM 51-30-02. MATERIAL ID BSDR CKSA98326Support · crackedDURING ROUTINE CPCP INSPECTION, FOUND FWD CARGO COMPARTMENT STA 570 LBL 24 FLOOR SUPPORT IS CRACKED. REMOVED DAMAGED MATERIAL IAW B747 SRM 51-30-00. ID MATERIAL 2024T3 0.63 IAW B747 SRM 51-10-01. INSTALLED SUPPORT IAW B747 SRM 51-21-01. CORROSION TASK CARDSDR CKSA98325Frame · crackedDURING ROUTINE CPCP INSPECTION, FOUND FWD CARGO COMPARTMENT STA 680, RBL 70, WL118 RIB IS CRACKED. REMOVED DAMAGED RIB IAW SRM 51-30-2. MATERIAL CHECK 2024-T3 .040. INSTALLED NEW RIB IAW SRM 51-30-02. CORROSION TASK CARD NUMBER C53-125-01-1. NON-ROUTINE TSDR CKSA98324Angle · crackedDURING ROUTINE CPCP INSPECTION, FOUND FWD CARGO COMPARTMENT STA 640 LBL 43 FLOOR SUPPORT IS CRACKED. CUT OUT DAMAGED AREA IAW B747 SRM 51-10-01. ID MATERIAL 2024T3 .050. INSTALLED ANGLE AND FILLER IAW B747 SRM 51-30-02. CORROSION TASK CARD NUMBER C53-125-0SDR CKSA98323Skin · corrodedDURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, FWD CARGO COMPARTMENT STA 960, BETWEEN S47R AND S47L SKIN HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01 MATERIAL LOSS 30 PERCENT OUT OF LIMITS IAW B747 SRM 53-30-01. DAMAGED SKIN WAS REMOVED IA
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