N2817W, cancelled Aug 19, 2013
Service difficulty reports · 44
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 = 'N2817W' AND deregistration_id = 'N2817W-2013-08-19' 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 = 'N2817W' AND deregistration_id = 'N2817W-2013-08-19' 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 DL72W002099Brake Assy · malfunctionedAIR TURNBACK - AFTER TAKEOFF, STAB TRIM LOCKED AND WOULD NOT TRIM NOSE UP. OCCURRED IN BOTH ELECTRIC MODES (AUTO-PILOT AND MAIN) AND MANUAL. ACTIVATION OF STAB BRAKE RELEASE RELEASED THE STAB. THIS OCCURRED APPROX 12 TIMES AS ACFT RETURNED TO LAND, NORMAL SDR DL72W001842Fitting · looseDURING REPETITIVE INSPECTIONS, THE I/B SLAT TRACKS ON THE NR 3 AND NR 4 SLATS WERE FOUND TO HAVE LOOSE BOLTS IN THE DOWNSTOP FITTINGS. THE CONDITION IS TYPICAL OF BAC S/B 727-57-0171. BOTH SLAT TRACKS FOR THE NR 3 AND NR 4 SLATS WERE MODIFIED PER THE SSDR DL72W000785Light · inoperativeEMERGENCY LIGHT ABOVE THE L1 DOOR FLICKERS IN FLT. REPLACED LIGHT ASSY.SDR DL72W991810Bulkhead Beam · crackedFUSELAGE BULKHEAD FS 1183, RBL 26.83, VERTICAL BEAM, CRACK REPAIR. THE RBL 26.83 VERTICAL BEAM ON THE FS 1183 BULKHEAD WAS FOUND WITH A TYPICAL CRACK. THE BEAM WAS REPAIRED PER BOEING S/B 727-53-0182, REV 1 AND DOCUMENTED PER ER/A 367994-14AD.SDR DL72W990863Skin · crackedA 2.5 INCH CRACK IN RT ELEVATOR LOWER SKIN AFT OF NR 4 BALANCE BOARD. REPAIRED PER SRM 55-20-3.SDR DL72W990862Frame · crackedFOUND AT B-2 LETTER CHECK, .5 INCH CRACK ON LT AFT ENTRY DOOR FRAME. REPAIRED PER SRM 53-10-9.SDR DL72W990861Frame · crackedFOUND AT B-2 LETTER CHECK, .5 INCH CRACK ON RT AFT ENTRY DOOR FRAME. REPAIRED PER SRM 53-10-9.SDR DL72W990756Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 5 CRACKS IN TWO CONSECUTIVE FRAME BAYS. THE SKIN LAP WAS CUT OUT ALONG THE ENTISDR DL72W990755Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 41 CRACKS ALONG THE PANEL. THE LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRSDR DL72W990753Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 9 CRACKS IN THE PANEL. THE SKIN LAP WAS CUT OUT ALONG THE LENGTH OF THE PANEL ANSDR DL72W990530Coalescer · dirtySTRONG BURNING SMELL IN CABIN NEAR OVERWING EXITS WHEN MAIN SUPPLY TEMP EXCEEDS 80 DEGREES F. ISOLATED PACKS WITH APU AND ALL ENG BLEED SOURCES. RAN SUPPLY TEMP TO 130 DEGREES F WITH EVERY COMBINATION POSSIBLE. NO SMELLS OF ANY KIND. REPLACED BOTH WATER SESDR DL72W990517Air Distribution · odorSTRONG BURNING SMELL IN MID CABIN NEAR OVERWING EXITS. CKD APU FOR SIGNS OF OIL LEAKS, NONE FOUND. CHECKED OPR OF PACKS AND PACK FANS, NORMAL. RAN PACKS NO ABNORMAL ODORS NOTED IN CABIN.SDR DL72W981884Skin · damageDURING REPLACEMENT OF BELLY SKIN, A FASTENER HOLE SUSTAINED TOOLING DAMAGE NEAR THE C-1 DOOR CUTOUT. REPAIR PER ERA 332149-14.SDR DL72W981984Skin · crackedCRACK IN COVE SKIN 31 INCHES FROM I/B END OF FLAP. DAMAGE REPAIRED PER MM 57-52-0 FIG 809.SDR DL72W981983Spar · crackedAFT SPAR RAIL CRACKED TWO PLACES 35 INCHES FROM I/B END OF FLAP. DAMAGE WAS REPAIRED PER MM 57-52-0 FIG 802.SDR DL72W981964Spar · crackedAFT SPAR RAIL CRACKED 2 PLACES, 21 INCHES FROM I/B END OF FLAP. REPAIRED PER MM 57-52-0 FIG 802.SDR DL72W981858Rib · crackedDURING SHOP VISIT, THE I/B AFT CLOSEOUT RIB WAS FOUND CRACKED. THE RIB WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 808.SDR DL72W981887Heat Shield · crackedCRACKS IN HEAT SHIELD, NR 6 LE SLAT, ONE IS JUST OUTBOARD OF ACTUATOR ATTACH RIB, THE OTHER IS JUST OUTBOARD OF OUTBOARD TRACK. MANUFACTURED AND INSTALLED DOUBLERS ON HEAT SHIELD SKIN PER MM 57-54-0 FIG 803A. MANUFACTURED AND INSTALLED DOUBLER ON HEAT SHIELDSDR DL72W981166Shim · migratedDURING ROUTINE INSPECTIONS PER SI 4-58662-12AD, LAMINATED SHIMS WERE FOUND MIGRATED GREATER THAN THE .25 LIMIT ALLOWED PER BAC S/B 727-57-0178 AND AD 90-07-05. THE SHIMS WERE REPLACED PER THE REQUIREMENTS OF THE S/B AND THE AD. THE INSPECTIONS PER SI 4-58662SDR DL72W980638Light · inoperativeON LAYOVER 2 CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY LIGHT INOP. RELAMPED, NO HELP. REPLACED BATTERIES, NO HELP. REPLACED LIGHT ASSEMBLY AND INSTALLED NEW BATTERIES, OPERATIONAL CHECKS NORMAL.SDR DL72W972221Fuel Control · failedENGINE NUMBER ONE FAILURE IMMEDIATELY AFTER T/O. FLAMEOUT/ LOSS OF THRUST REPORT FILLED OUT. REMOVED AND REPLACED NR ONE ENGINE FUEL BOOST PUMP AND FUEL CONTROL. RAN AND TRIMMED ENGINE PER PRHB.SDR DL72W972117Bulkhead Web · crackedDURING INPSECTION OF STA 1183 BULKHEAD PER SPECIAL INSPECTION 4-69150-12, A CRACK WAS DISCOVERED JUST BELOW A STIFFENER AT LBL 30, WL 188 IN THE WEB. THE CRACK MEASURED 2.5 INCHES. THE WEB MATERIAL IS .050 2024-T3 CLAD. THE -12 SPECIAL INSPECTION CALLS FOR SDR DL72W971823Bracket · crackedNR 6 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED I/B SIDE AT MOUNT BOLT HOLES. REPAIRED PER MM 57-20-21.SDR DL72W971822Stiffener · crackedFOUND DURING A-1 LETTER CHECK, 1.5 INCH CRACK L/E SPAR STIFFENER AT NR 2 SLAT I/B TRACK ROLLER BOX I/B SIDE. REPAIRED PER M/M 57-20-21.SDR DL72W970354Fitting · crackedFOUND A 1 INCH CRACK IN RT ELEVATOR HINGE SUPPORT CASTING 4TH HINGE FROM O/B END. REPAIRED PER M/M 55-10-31.SDR DL72W962768Stringer · crackedFOUND DURING MV2, JUST INSIDE ACCESS 9504 ON RT SIDE 2ND FROM TOP STRINGER, CRACK AT RIB ATTACH BOLT. FABRICATED AND DRILLED REPAIR PARTS PER M/M 55-30-0 PG. 803. INSTALLED REPAIR PER M/M 55-30-0.SDR DL72W970038Blkhd Stiffener · crackedA CRACK WAS FOUND IN THE VERTICAL STIFFENER AT LBL 36.83 ON THE FWD SIDE OF THE BS 1183 BULKHEAD. THE CRACK WAS APPROX 1.75 LONG AT WL 237. THE STIFFENER WAS REPAIRED PER BOEING S/B 727-53-0192.SDR DL72W962740Skin · bentL-1 DOOR EXT SKIN UPPER AFT CORNER BENT. STRAIGHTENED METAL, DYE-CHECKED FOR CRACKS PER PS 400-6-3. REPAIRED PER M/M 52-10-01 FIGURE 804, PG 806.SDR DL72W962243Battery Pack · dischargedFWD OVERWING EXIT LIGHT ON RIGHT SIDE OF FUSELAGE INOP. REPLACED BATTERY PACK, OVERWING EXIT LIGHT CHECKED GOOD.SDR DL72W970183Rib · crackedDURING INITIAL INSPECTION, RIB NR 4 AND RIB NR 5 WERE FOUND CRACKED. THEY WERE REPAIRED PER SRM 57-50-3.SDR DL72W961250Fuel Pump · failedNUMBER 1 ENGINE SHUTDOWN 30 SECONDS AFTER LIFT OFF. FOUND SHAFT SHEARED ON FUEL PUMP. REPLACED PUMP AND CONTROL.SDR DL72W960212Cooling Valve · failedDISPATCHED WITH ONE PACK, MIX VLV INOP. ACFT WOULD NOT HOLD THE CABIN WITH CARGO HEAT OUTFLOW CLOSED AND OUTFLOW VLV FULL CLOSED. REPLACED EQUIP COOLING VLV IN E/E COMP, PRESS ACFT TO 3 PSI AND OPERATION CKS OK.SDR DL72W960023Skin · dentedTHE FUSELAGE SKIN WAS OIL CANNED BETWEEN FS 660 TO 680 STR 23R AND STR 26R. THE DAMAGED AREA OF THE SKIN WAS TRIMMED OUT FROM FS 680 BUTT JOINT FORWARD FOR 19.75 AND FROM THE SKIN LAP JOINT AT STR 26R UP 25.75. A REPAIR DOUBLER WAS INSTALLED PER 8110-3 12-28SDR DL72W954776Beaded Doubler · crackedDURING C/V, FOUND RT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BEADED DOUBLER LOWER PANEL CRACKED. REPAIRED PER SRM 55-20-3 FIG 3.SDR DL72W961618Skin · corrosionTHE SKIN AT FS 680 CL AND FS 690 STR 26R WAS FOUND TO HAVE CORROSION DAMAGE. THE DAMAGE CUTOUT AT STA 680 CL IS APPROXIMATELY 2 BY 3, LOCAL SKIN THICKNESS IS 0.050. THE DAMAGE CUTOUT AT FS 690 IS APPROXIMATELY 2 BY 2, WITH A LOCAL SKIN THICKNESS OF 0.050. TSDR DL72W961619Skin · corrosionTHE SUBJECT FUSELAGE SKIN WAS FOUND WITH CORROSION DAMAGE AT STR 26L LAP JOINT, FS 500, 520 TO 540 AND 560 TO 570. AT FS 500, THE DAMAGE CUTOUT IS APPROXIMATELY 8 BY 2 IN THE LOWER SKIN. AT FS 520 TO 540, THE DAMAGE CUTOUT IS APPROXIMATELY 7.75 BY 2 IN THE USDR DL72W954720Seat Track · corrodedSEAT TRACK AT G-3 GALLEY INBOARD AFT MOUNT IS CORRODED. REPAIR PER M/M 53-20-11, PAGE 805.SDR DL72W954490Window · crackedR2 WINDOW OUTER PANE CRACKED PASSING THROUGH 23,000 ON CLIMBOUT. REPLACED R2 WINDOW AND HEAT CONTROLLER.SDR DL72W954367Battery · out of positionOVERHEAD EMERGENCY LIGHT AT ROW 29 INOP. FOUND BATTERY CASE OUT OF POSITION. REPLACED BATTERY AS PRECATIONARY, OPN NORMAL.SDR DL72W954096Battery Pack · dischargedLT AFT OVERWING EMERGENCY LIGHT INOP. FOUND DEFECTIVE BATTERY PACK, REPLACED PACK, OPERATION NORMAL.SDR DL72W954095Bulb · failedRT AFT OVERWING EMERGENCY LIGHT INOP. RELAMPED, OPERATION NORMAL.SDR DL72W952363Slat · crackedFOUND DURING E-1 LETTER CHECK - .25 INCH CRACK AT NR 7 SLAT O/B STOP PAD BELOW COVE PNL. REPAIRED PER MM 57-54-0.SDR DL72W952362Rib · crackedFOUND DURING E-1 LETTER CHECK - .1875 INCH CRACK BOTTOM OF NOSE RIB JUST LEFT OF SLAT ACTUATOR ROD END ON NR 4 SLAT. ONE INCH CRACK ON NR 4 SLAT I/B TRACK LOWER FAIRING RADIUS. BOTH REPAIRED PER MM 57-54-0.SDR DL72W952361Slat · crackedFOUND DURING E-1 LETTER CHECK - .50 INCH CRACK AT I/B STOP PAD ON NR 2 SLAT. REPAIRED PER MM 57-54-0.
Back to N2817W, cancelled Aug 19, 2013