N66734, cancelled Aug 11, 2008
Service difficulty reports · 48
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N66734' AND deregistration_id = 'N66734-2008-08-11' 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 n_number = 'N66734' AND deregistration_id = 'N66734-2008-08-11' 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 CALA9801534Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN L-ANGLE OF LT WING J-BEAM ABOVE NR 7 SPOILER ACTUATOR. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-1, PAGE 4 AND 51-30-2.SDR CALA9801533Chord · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LOWER FORWARD CHORD OF LT WING BELOW NR 7 SPOILER ACTUATOR. THE CRACKED SECTION WAS CUT OUT, A REPAIR WAS INSTALLED IAW ECRA 5720-01675.SDR CALA9801532Fitting · corrodedINSPECTION FOUND NOSE GEAR LT TRUNNION FITTING AND CAP CORRODED IN AREAS OF BUSHING RECESS. THE FACES AND BORE OF LT NLG TRUNNION AND CAP ASSEMBLY WERE MACHINED IAW SRM 53-40-1 AND ECRA 5340-01323.SDR CALA9801531Fitting · corrodedINSPECTION FOUND NOSE GEAR RT TRUNNION FITTING AND CAP CORRODED. THE STIFFENERS AND FITTING WERE REMOVED AND THE AREA WAS REPAIRED IAW SRM 51-10-2 AND 51-10-6.SDR CALA9801530Chord · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RT WING TRAILING EDGE LOWER CHORD AT NR 8 SPOILER ACTUATOR CASTING. THE CRACKED SECTION OF CHORD WAS REMOVED IAW SRM 51-30-2. A REPAIR WAS INSTALLED IAW SRM 51-10-1 AND ECRA 5720-01675.SDR CALA9801519Bracket · crackedINSPECTION FOUND A 0.4 INCH CRACK IN RT WING LEADING EDGE FLAP NR 6 ACTUATOR MOUNT BRACKET. THE MOUNT BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-1.SDR CALA9801518Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN J-BEAM APPROXIMATELY 1.5 INCHES ABOVE NR 7 SPOILER ACTUATOR AT CUTOUT ABOVE INBOARD END OF AFT FALSE SPAR. PANELS AND A FITTING WERE REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5740-02914 AND SRM 51-10-2, AND 51-10-6. THE SDR CALA9801446Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING TRAILING EDGE UPPER ATTACH ANGLE ABOVE NR 6 GEARBOX FOR FLAP. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-10-6.SDR CALA9801445Panel · crackedINSPECTION FOUND THREE CRACKS IN LT HORIZONTAL STABILIZER BALANCE PANEL NR 9116. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. TWO EACH DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 55-20-3.SDR CALA9801414Skin · crackedINSPECTION FOUND A .15625 AND .09375 CRACK IN LT WING NR 4 SLAT LOWER TRAILING EDGE SKIN AT RADIUS OUTBOARD OF INBOARD TRACK, 36.5 INCHES FROM INBOARD END. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3, 51-10-2, AND 51-40SDR CALA9801413Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN INBOARD BRACKET WHERE LT WING NR 1 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CALA9801412Bracket · crackedINSPECTION FOUND A .75 INCH CRACK IN INBOARD BRACKET WHERE LT WING NR 2 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED IAW SRM 51-30-2. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-2.SDR CALA9801411Bracket · crackedINSPECTION FOUND A 1 CRACK IN RT NR 5 LEADING EDGE FLAP ACTUATOR MOUNT BRACKET AT UPPER OUTBOARD LEADING EDGE. THE MOUNT BRACKET WAS REMOVED IAW SRM 51-30-2. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9801392Angle · crackedINSPECTION FOUND 2.5 INCH CRACK AT CURVED ANGLE AT OUTBOARD SIDE OF LT WING FIXED LEADING EDGE RIB SLAT STA 0. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-40-3.SDR CALA9700803Stringer · crackedINSPECTION FOUND A 3 INCH CRACK IN RT WING STRINGER 17 AT STA 330.5. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-4.SDR CALA9700807Frame · corrodedINSPECTION FOUND LOWER CHORD OF FRAME CORRODED AROUND NUT PLATE ATTACH HOLES AT STA 1130 FROM RBL 0 TO RBL 42. A REPAIR WAS FABRICATED AND INSTALLED IAW BOEING DRAWING 26256-1254.SDR CALA9700806Frame · corrodedINSPECTION FOUND LOWER CHORD OF FRAME CORRODED AROUND NUT PLATE ATTACH HOLES AT STA 1110 FROM RBL 0 TO RBL 42. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9700805Skin · corrodedINSPECTION FOUND FUSELAGE SKIN LAP JOINT CORRODED BETWEEN STA 720E AND 740 AT STRINGER 26R. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02521 AND SRM 51-30-8.SDR CALA9700804Slat · crackedINSPECTION FOUND A .25 INCH CRACK IN RT WING SLAT NR 6 OUTBOARD HOOK AREA. REPAIRED IAW SRM 57-30-4.SDR CALA9700802Flap · crackedINSPECTION FOUND A 1.125 INCH CRACK ABOVE NR 1 FLAP TRACK AREA IN LT WING OUTBOARD FOREFLAP LEADING EDGE. A DOUBLER WAS INSTALLED IAW SRM 57-50-4.SDR CALA9700801Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN LT WING LEADING EDGE SKIN AT NR 3 SLAT OUTBOARD HOOK CUTOUT. REPAIRED IAW SRM 57-30-4, PAGE 24 FIGURE 26.SDR CALA9700799Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING GEAR DOOR AFT HINGE SKIN. A DOUBLER WAS INSTALLED IAW SRM 52-00-3.SDR CALA9700798Bulkhead · crackedINSPECTION FOUND A 1.75 INCH CRACK IN RT MLG WELL BULKHEAD AT STA 870, BELOW APU LOAD CONTROL VALVE. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5310-01544.SDR CALA9700800Angle · crackedINSPECTION FOUND TWO 2 CRACKS IN LT WING RIB TO UPPER SKIN ATTACH ANGLE AT SLAT STA 0 INSIDE LEADING EDGE AREA. THE ANGLE WAS REPLACED IAW SRM 51-10-1.SDR CAL960513Flap Fairing · dentedFLT NR 663 - EWR - RIGHT OUTBOARD FLAP TRACK FAIRING (AFT SECTION) HAS DENT. REMOVED AND REINSTALLED FAIRING. OPS CHECK GOOD. (M)SDR CAL960494Pneumatic Duct · rupturedIAH - FLT 1876 - THE NR 1 ENGINE FIRE BELL AND LIGHT ACTIVATED AFTER TAKEOFF FROM IAH. THE ENGINE WAS RUN IN IDLE AND THE NR 1 BLEED WAS TURNED OFF. THE FIRE WARNING CEASED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUSDR CAL951018Fasteners · looseIAH - FLT 0495 - A LIQUID VAPOR TRAIL WAS REPORTED COMING FROM BETWEEN RT OUTBOARD AILERON AND NR 7 JACKSCREW FAIRING WHILE IN-FLIGHT. FUEL WAS DUMPED TO 21,000 POUNDS AND THE TRAIL OF VAPOR CEASED. THE AIRCRAFT WAS RETURNED TO IAH. MAINTENANCE FOUND SEVERASDR CAL950784Lock Actuator · inoperativeEWR - FLT 0434 - THE NLG FAILED TO EXTEND ON APPROACH TO EWR, THE GEAR WAS CYCLED DURING A 'GO AROUND' AND THE NOSE GEAR EXTENDED NORMALLY. THE NLG LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-11. AN EXTENSION/RETRACTION TEST WAS PERFORMED IAW MM 32-3SDR CAL950372Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN NR 3 SLAT RIB INBOARD OF TRACK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-6 AND 57-50-3. (M)SDR CAL950371Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN NR 7 SLAT RIB AT OUTBOARD SIDE ON OUTBOARD TRACK. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-3 AND 57-50-3. (M)SDR CAL950370Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN NR 4 SLAT OUTBOARD SECOND RIB. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-50-3. (M)SDR CAL950369Skin · crackedGSO - INSPECTION FOUND A .125 INCH CRACK IN THE NR 2 LEADING EDGE FLAP INNER SKIN UNDER ACTUATOR. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EC 5720-01064 AND SRM 51-30-2. (M)SDR CAL950368Te Panel · crackedGSO - INSPECTION FOUND THE LEFT WING UPPER SURFACE TRAILING EDGE PANEL AT OUTBOARD END OF OUTBOARD FLAP WITH A 1 INCH CRACK IN DOUBLER ATTACHED TO INBOARD SIDE. THE CRACKED DOUBLER WAS REMOVED. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-1 AND 5SDR CAL950367Support · corrodedGSO - INSPECTION FOUND CORROSION ON LOWER SIDE OF FLOOR SUPPORT IN FORWARD PIT AT STATION 620. THE CORRODED AREA WS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2. (M)SDR CAL950366Intercostal · crackedGSO - INSPECTION FOUND THE LT MAIN LANDING GEAR BAY INTERCOSTAL AT BS 890 CRACKED AND CORRODED. THE CRACK WAS .75 INCH LONG. THE DAMAGED AREA OF INTERCOSTAL WAS CUT OUT. REPAIR FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-3. (SDR CAL950365Stringer · crackedGSO - INSPECTION FOUND, CRACKS AND CORROSION IN STRINGER 20R AT STA 500 TO 520. THE CRACKS WERE .125 INCH TO .25 INCH IN LENGTH. THE DAMAGED SECTION OF STRINGER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. (Z)SDR CAL950363Angle · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FLOOR PANEL SUPPORT ANGLE AT BS 760, BL 0 - BL 24R. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-40-3, AND 51-30-2. (W)SDR CAL9503624Angle · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT ANGLE AT BS 760, BL 0 - BL 24L. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-40-4, AND 51-30-2. (W)SDR CAL950362Pressure Web · corrodedGSO - INSPECTION FOUND CORROSION ON PRESSURE WEB IN RT LAVATORY. THE CORROSION WAS REMOVED. DOUBLERS AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-40-2. (W)SDR CAL950361Web · crackedGSO - INSPECTION FOUND A .25 INCH CRACK IN WEB AT STRINGER 16L, STATION 308.9 INSIDE CONTROL CABIN AT MAIN ENTRY DOOR FRAME. THE CRACKED WEB WAS REPLACED IAW SRM 51-30-2 AND 51-10-1. (W)SDR CAL950360Support · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT FLANGE AT BS 990. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 53-10-2. (W)SDR CAL950359Support · crackedGSO - INSPECTION FOUND FLOOR SUPPORT IN FORWARD PIT AT STATION 720 ABOVE STRINGER 26L CRACKED IN TWO PLACES. THE CRACKS WERE .75 INCH LONG. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, AND 53-10-5. (W)SDR CAL950358Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK ON LOWER SIDE OF LEFT WING INTERNAL RIB AT WS 738.5, ABOVE S-8. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-10-5. (W)SDR CAL950357Chord · corrodedGSO - INSPECTION FOUND REINFORCEMENT CHORD AT STATION 1183 CORRODED. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-30-2. (W)SDR CAL950356Support · corrodedGSO - INSPECTION FOUND FLOOR SUPPORT CORRODED ON BOTTOM SIDE AT FORWARD PIT STATION 720. THE CORROSION WAS REMOVED AND A REPAIR WEB WAS INSTALLED IAW SRM 51-30-2. (W)SDR CAL950355Skin · crackedGSO - INSPECTION FOUND A .125 INCH CRACK IN SKIN AT LAP SPLICE 26L, BS 513. THE CRACKED AREA WAS CUT OUT. REPAIRED DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 53-30-3. (W)SDR CAL950011Oil Press Tube · brokenGSO - FLT 0383 - THE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO WHILE EN ROUTE FROM EWR TO RSW. THE OIL PRESSURE DECREASED TO THE YELLOW ARC. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR SDR CAL95002Eel Relay · inoperativeIAH - FLT 1076 - CABIN EMERGENCY AISLE PATH LIGHTING WOULD NOT COME ON AUTOMATICALLY WHEN SWITCHED TO STANDBY POWER DURING A PREFLIGHT CHECK. THE EMERGENCY POWER LIGHT RELAY WAS REMOVED AND REPLACED AND OPERATION OF THE AISLE PATH LIGHTING WAS RESTORED. (X)
Back to N66734, cancelled Aug 11, 2008