Boeing 747-122

Service difficulty reports · 2,143

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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 = '747122'
  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.

SDR P5CA9701471Support · corrodedLEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1400 - BS 1414 LBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.Jul 31, 1997 · N853FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9701470Support · corrodedLEVEL 1 CORROSION, FUSELAGE BS 1480 LBL 60 - RBL 60 BODY FAIRING SUPPORT RIB FOUND CORRODED. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW 51-10-02.Jul 31, 1997 · N853FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9701469Support · corrodedLEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORROSION ON BS 1470 - LBL 15 - RBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.Jul 31, 1997 · N853FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9701468Support · corrodedLEVEL 1 CORROSION, FUSELAGE KEEL BEAM BOX LOWER ACCESS PANEL SUPPORT FOUND CORRODED ON BS 1468- LBL 15 - RBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.Jul 31, 1997 · N853FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9701386Duct · leakingIN CRUISE FL 290 LEFT WING OVERHEAT LIGHT ILLUMINATED, COMPLIED WITH WING OVERHEAT PROCEDURE ISOLATED LEFT WING AND NR 1 AND NR 2 ENGINES WITH PYLON VALVES LIGHT WENT OUT. RETURNED THRUST TO NORMAL, LIGHT STAYED OUT. FOUND PNEUMATIC LEAK 1 FOOT INBOARD OF NRJul 31, 1997 · N852FT · Boeing 747122 · Pneumatic Distribution SystemSDR P5CA9701524Skin · crackedA .25 INCH CRACK ON SKIN BS 2606 BETWEEN S 51R AND S 49R. REPAIRED PER BOEING SRM 53-30-03.Jul 30, 1997 · N853FT · Boeing 747122 · Fuselage Main, Plate/SkinSDR P5CA9701518Support Beam · crackedCRACK LEFT WING SPOILER SUPPORT BEAM WEB LOWER CHORD AT OUTBOARD OF NR 6 SPOILER AREA. REPAIRED PER BOEING SRM 51-40-04.Jul 30, 1997 · N853FT · Boeing 747122 · Wing Miscellaneous StructureSDR P5CA9701517Bulkhead Fitting · crackedCRACK BS 1241 BULKHEAD AFT HOLE AT PASSENGER DECK FITTING, CRACK .0625 RUNNING DOWNWARD. REAMED HOLE TO 0.875 AS PER SB 53-2283, HOLE CHECKED CRACK FREE.Jul 30, 1997 · N853FT · Boeing 747122 · Fuselage Main, BulkheadSDR P5CA9701467Skin · corrodedLEVEL 1 CORROSION, LHW LWR SKIN INTERIOR SURFACE IN FRONT OF FRONT SPAR CHORD FOUND CORROSION AT WING LEADING EDGE CAVITY APPROX TO OLES 1415. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.Jul 30, 1997 · N853FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA9701466Sill · corrodedLEVEL 1 CORROSION, AFT CARGO BS 1808-1812 STR 42R DOOR SILL WEB OUTBD FACE FOUND CORRODED. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.Jul 30, 1997 · N853FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9701379Actuator Beam · brokenRIGHT WING GEAR DOOR REMAINED OPEN AFTER LANDING. FOUND BROKEN RIGHT WING LANDING GEAR DOOR ACTUATOR BEAM. REPLACED ACTUATOR BEAM PER BOEING M/M 32-32-28. CHECKED DOOR RIG PER M/M 32-12-04.Jul 30, 1997 · N854FT · Boeing 747122 · Landing Gear Door ActuatorSDR P5CA9701378Overheat Switch · out of positionLEFT WING LEADING EDGE OVERHEAT LIGHT FLICKERED INTERMITTENTLY, WING BLEED ISOLATED, LIGHT CONTINUED TO FLICKER. FOUND S-898 LEADING EDGE OVERHEAT SWITCH TOUCHING STRUCTURE CORRECTED SWITCH POSITION TO NORMAL TESTED PER M/M 26-18-00. ALSO, CHECKED FOR PNEUMAJul 30, 1997 · N852FT · Boeing 747122 · Overheat DetectionSDR P5CA9701465Skin · corrodedLEVEL CORROSION, LHW UPPER SKIN CORROSION IN FRONT OF MID SPAR (NR 12 LEADING EDGE FLAP). CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.Jul 29, 1997 · N853FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA9701464Skin · corrodedLEVEL 1 CORROSION, RHW UPPER TRAILING EDGE PANEL FORWARD EDGE ATTACH TO WING SKIN AREA FOUND CORROSION AT NR 8 SPOILER AREA. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.Jul 29, 1997 · N853FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA9701463Skin · corrodedLEVEL 1 CORROSION, LHW UPPER SKIN TRAILING EDGE FOUND CORROSION AT REAR SPAR CHORD TO SKIN ATTACH FASTENERS AREA IN FRONT OF NR 3 SPOILER OUTBD CORNER. CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.Jul 29, 1997 · N853FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA9701462Skin · corrodedLEVEL 1 CORROSION, LHW UPPER SKIN FOUND SURFACE CORROSION AT REAR SPAR CHORD TO UPPER SKIN ATTACH FASTENERS AREA (APPROX AT WBL 163). CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.Jul 29, 1997 · N853FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA9701461Skin · corrodedLEVEL 1 CORROSION, LHW UPPER SKIN FOUND SURFACE CORROSION IN FRONT OF NR 3 SPOILER (MID SPAR ATTACH FASTENERS). CORROSION REMOVED PER BOEING SRM 51-10-01 AND TREATED IAW SRM 51-10-02.Jul 29, 1997 · N853FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA9701372Fitting · corrodedLEVEL 1 CORROSION, RIGHT ATTACH FITTING TO KEEL BEAM LOWER SURFACE BS 980.8 AT FASTENERS. REMOVED CORROSION PER SRM 51-10-01 FOUND WITHIN LIMITS PER SRM 51-10-02 AND 51-30-02.Jul 26, 1997 · N851FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9701371T Chord · corrodedLEVEL 2 CORROSION, PANEL SUPPORT BS 965 LBL 48. REPLACED T-CHORD PER BOEING SRM 51-30-02.Jul 26, 1997 · N851FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9701370Support · corrodedLEVEL 2 CORROSION PANEL SUPPORT LOWER FUSELAGE FORWARD OF WATER SERVICE PANEL. REPAIRED PER SRM 51-40-04 AND 51-10-01.Jul 26, 1997 · N851FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9701369Panel · delaminatedDELAMINATED PANEL NR 344NB RIGHT HORIZONTAL STABILIZER LOWER SURFACE. REPAIRED PER BOEING SRM 51-40-06.Jul 26, 1997 · N851FT · Boeing 747122 · Horizontal Stabilizer, Plate/SkinSDR P5CA9701368Skin · delaminatedDELAMINATED PANEL NR 334NB LEFT HORIZONTAL STABILIZER LOWER SURFACE. REPAIRED PER BOEING SRM 51-40-06 AND 55-10-12.Jul 26, 1997 · N851FT · Boeing 747122 · Horizontal Stabilizer, Plate/SkinSDR P5CA9701367Skin · delaminatedDELAMINATED PANEL NR 334MB LEFT HORIZONTAL STABILIZER LOWER SURFACE. REPAIRED PER BOEING SRM 51-40-05.Jul 26, 1997 · N851FT · Boeing 747122 · Horizontal Stabilizer, Plate/SkinSDR P5CA9701375Panel · crackedCRACK ON INBOARD END OF LEFT WING INBOARD FLAP COVER PANEL. REPAIRED PER BOEING SRM 51-40-09 AND 51-24-11.Jul 25, 1997 · N851FT · Boeing 747122 · Trailing Edge FlapsSDR P5CA9701310Fitting · corrodedLEVEL 1 CORROSION, LWR SURFACE STA 968 RT FORWARD FITTING KEEL BEAM IN CENTER OF FITTING AT FASTENERS. REMOVED CORROSION, FOUND TO BE WITHIN LIMITS IAW BOEING SRM 53-10-01 FIG. 1 ORIG. MAT .260 NOW .224 TREATED AND PRIMED IAW BOEING SRM 51-10-06.Jul 24, 1997 · N851FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9701309Panel · corrodedLEVEL 1 CORROSION, LWR FUSELAGE NR 1 HEAT EXCHANGER PANEL AROUND FASTENERS. REPAIRED AREA PER BOEING SRM 51-40-11 PRIMED AND PAINTED PER BOEING SRM 51-24-11.Jul 24, 1997 · N851FT · Boeing 747122 · Fuselage Main, Plate/SkinSDR P5CA9701308Skin · corrodedLEVEL 2 CORROSION, LWR FUSELAGE BETWEEN NR 1 AND NR 3 ACM DOORS, PANEL. REMOVED CORROSION FROM LWR FUSELAGE BETWEEN NR 1 AND NR 3 ACM DOORS IAW BOEING SRM 51-10-01 AND TREATED AND PRIMED AREA PER BOEING SRM 51-10-02.Jul 24, 1997 · N851FT · Boeing 747122 · Fuselage Main, Plate/SkinSDR P5CA9701306Panel · corrodedLEVEL 2, CORROSION LWR SURFACE STA 980, LBL 40 BODY PANEL SUPPORT. REPAIRED DAMAGED AREA FAB. REPAIR PARTS AND INSTALLED IAW BOEING SRM 51-40-04.Jul 24, 1997 · N851FT · Boeing 747122 · Fuselage Main, Plate/SkinSDR P5CA9701305Fill Valve · corrodedLEVEL 1 CORROSION, LWR SURFACE STA 970 WATER SERVICE STATION WATER TANK FILL VALVE HANDLE AT MOUNT. CORROSION REMOVED FOUND TO BE WITHIN LIMITS IAW BOEING SRM 53-10-01 FIG 1, REG MAT .130 NOW .111 TREATED AND PRIMED PER SRM 51-10-06.Jul 24, 1997 · N851FT · Boeing 747122 · Potable Water SystemSDR P5CA9701359Skin · corrodedLEVEL 1 CORROSION, LWR SURFACE STA 980 LEFT FORWARD ATTACH FITTING TO KEEL BEAM HAS CORROSION AROUND FASTENERS. REMOVED CORROSION IAW BOEING SRM 53-30-01 FOUND TO BE WITHIN LIMITS IAW SRM 53-10-01 FIG 1 ORIG MAT .560 NOW .543 TREATED AND PRIMED IAW SRM 53-10Jul 23, 1997 · N851FT · Boeing 747122 · Fuselage Main, Plate/SkinSDR P5CA9701307Radome · delaminatedNOSE RADOME HAS SEVERAL AREAS OF EXPOSED COMPOSITE AND DELAMINATION. CLEANED, SANDED AND POTTED DAMAGED AREA IAW BOEING SRM 53-50-03 AND PREP AND PAINTED SPOTS ON NOSE RADOME IAW 51-24-11.Jul 23, 1997 · N851FT · Boeing 747122 · Aerodynamic FairingsSDR P5CA9701304Fitting · corrodedLEVEL 1 - CORROSION, LWR SURFACE STA 980 LEFT FORWARD ATTACH FITTING TO KEEL BEAM AROUND FASTENERS. CORROSION REMOVED PER BOEING SRM 53-30-01 WITHIN LIMITS IAW SRM 53-10-01 FIG 1 ORIG MAT .560 NOW .543 TREATED AND PRIMED IAW SRM 53-10-06.Jul 23, 1997 · N851FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9701303Overhead Panel · corrodedLEVEL 1 - CORRODED CENTER ELECTRICAL COMPARTMENT FORWARD OVERHEAD PANEL AROUND FASTENERS AT AFT END. CORROSION REMOVED AROUND FASTENERS AT CENTER ELECTRICAL COMPARTMENT FORWARD OVERHEAD PANEL FOUND TO BE WITHIN LIMITS IAW BOEING SRM 51-10-01. TREATED AND PRIJul 21, 1997 · N851FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9701539Fitting · crackedNR 1 PYLON UNDERWING DIAGONAL BRACE FITTING CRACKED AT OUTBOARD SIDE AFT RADIUS POSITION. FITTING REPLACED PER SB 57-2288.Jul 19, 1997 · N853FT · Boeing 747122 · Wing, Nacelle/Pylon Attach FittingsSDR P5CA9701346Frame · corrodedLEVEL 2 CORROSION, NR 1 PYLON CORROSION ON THE BOTTOM END OF RIGHT FRAME AT NAC STA 162 WL 140.5 SB 54A2159 FINDING. REPAIRED FRAME IAW BOEING SRM 54-10-03 FIG 1.Jul 17, 1997 · N854FT · Boeing 747122 · Nacelle/Pylon, Frame/Spar/RibSDR P5CA9701301Altimeter · stickingON DESCENT, FIRST OFFICER'S ALTIMETER STICKING FOR APPROXIMATELY 500 FT. REMOVED AND REPLACED ALTIMETER PER BOEING M/M 34-13-04 AND OPERATIONAL CHECKED PER M/M 34-17-04.Jul 17, 1997 · N850FT · Boeing 747122 · Altimeter, Barometric/EncoderSDR P5CA9701354Bulkhead Chord · crackedCRACK FOUND ON NR 1 PYLON AFT BULKHEAD, INBD VERTICAL CHORD INBD ROW NR 4 FASTENER HOLE, .125 INCH LONG CRACK. REPLACED CHORD IAW SRM 51-10-01 AND SB 747-54A2159 NON ROUTINE CARD S/N 6006.Jul 16, 1997 · N854FT · Boeing 747122 · Nacelle/Pylon, Bulkhead/FirewallSDR P5CA9701345Skin · crackedNR 3 PYLON SKIN IS CRACKED ON INBD SIDE UNDER SKIN DOUBLER AT NAC ST 180 NAC WL 140.2-142.2, REPAIRED IAW SB 54-2034. NON ROUTINE CARD S/N 6144.Jul 16, 1997 · N854FT · Boeing 747122 · Nacelle/Pylon, Plate/SkinSDR P5CA9701342Spar Cap · corrodedLEVEL 1 CORROSION, WING FRONT SPAR UPPER CAP HAS LIGHT SURFACE CORROSION AT NAC ST 305 RWBL 472-473. REMOVED CORROSION IAW BOEING SRM 51-10-01 NON ROUTINE CARD S/N 7059.Jul 16, 1997 · N854FT · Boeing 747122 · Wing SparSDR P5CA9701328Skin · crackedNR 1 PYLON OUTBD SKIN CRACKED UNDER DOUBLER AT NAC ST 180 NAC WL 140.2. STOP HOLE DRILLED IAW BOEING SRM 51-10-01 SKIN REPAIRED IAW SB 54-2034 FIG 5.Jul 16, 1997 · N854FT · Boeing 747122 · Nacelle/Pylon, Plate/SkinSDR P5CA9701358Longeron · corrodedLEVEL 2 CORROSION, LONGERON BS 1300-1325. REPAIRED PER HAECO RS 53-41-33455. NON ROUTINE CARD S/N 6543.Jul 14, 1997 · N854FT · Boeing 747122 · Fuselage Main, Longeron/StringerSDR P5CA9701357Skin · corrodedLEVEL 2 CORROSION, SKIN BS 2484 STR 20L-23L. REPAIRED PER HAECO RS 53-21-33454. NON ROUTINE CARD S/N 6404.Jul 14, 1997 · N854FT · Boeing 747122 · Fuselage Main, Plate/SkinSDR P5CA9701356Shear Tie · corrodedLEVEL 2 CORROSION, SHEAR TIE CORRODED AT BS 520 STR 40R-41R. REPAIRED PER HAECO RS 53-11-33436. NON ROUTINE CARD S/N 5844.Jul 14, 1997 · N854FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR P5CA9701355Actuator Beam · elongatedFASTENER HOLE ELONGATED AT BS 580 AND 660. REPAIRED PER HAECO RS 53-21-33435.Jul 14, 1997 · N854FT · Boeing 747122 · Fuselage Miscellaneous StructureSDR 97UAL900582Beam · crackedFATIGUE CRACK FOUND ON FOWARD LOWER CORNER OF DOOR FOUR RIGHT. CRACKING IS SIMILAR TO THAT REFERENCED IN SERVICE BULLETIN 747-52-2168. THERE WAS NO COLLISION OR CORROSION DAMAGE. HOWEVER, AN OLD SHEETMETAL REPAIR ON THE BEAM MAY HAVE CREATED A STRESS CONCENJul 14, 1997 · N4723U · Boeing 747122 · Passenger/Crew DoorsSDR P5CA9701343Skin · corrodedLEVEL 1 CORROSION, NR 3 PYLON AREA LOWER WING SKIN EXTENSION HAS FRETTING TYPE CORROSION AT RWBL 450-456 NAC ST 301.4-306. REMOVED CORROSION IAW SRM 51-10-01 AND REPROTECTED IAW SRM 51-10-02, MM 51-24-11 BLEND OUT IS WITHIN SRM 57-30-01 LIMITS. NON ROUTINE CJul 12, 1997 · N854FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA9701341Skin · corrodedLEVEL 1 CORROSION ON UNDERWING SKIN AT OUTBD MIDSPAR FITTING RWBL 840. REMOVED CORROSION AND REPROTECTED IAW BOEING SRM 51-10-02. BLEND OUT WITHIN BOEING SRM 57-30-01 LIMITS NON ROUTINE CARD S/N 7004.Jul 12, 1997 · N854FT · Boeing 747122 · Wing, Plate/SkinSDR P5CA9701340Bulkhead Tee · corrodedLEVEL 1 CORROSION, NR 2 PYLON TORQUE BULKHEAD 'T' CHORDS HAVE LIGHT SURFACE CORROSION AT NAC ST 301 WL 296-288. REMOVED CORROSION IAW BOEING SRM 51-10-01 AND IS WITHIN SRM LIMITS SRM 54-10-01.Jul 11, 1997 · N854FT · Boeing 747122 · Nacelle/Pylon, Bulkhead/FirewallSDR P5CA9701363Frame · crackedNR 3 PYLON INBD FRAME AT NAC STA 162 WL 146 HAS DEEP CHAFE MARK. REPLACED FRAME PER BOEING SRM 51-10-01.Jul 9, 1997 · N854FT · Boeing 747122 · Nacelle/Pylon, Frame/Spar/RibSDR P5CA9701361Frame · crackedNR 3 PYLON INBD FRAME AT NAC STA 192 WL 153 IS CRACKED AND DEEP CHAFING ADJACENT TO LANYARD CLIP. REPLACED FRAME PER BOEING SRM 51-10-01.Jul 9, 1997 · N854FT · Boeing 747122 · Nacelle/Pylon, Frame/Spar/Rib
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