N732DH, cancelled Feb 21, 2013
Service difficulty reports · 18
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 = 'N732DH' AND deregistration_id = 'N732DH-2013-02-21' 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 = 'N732DH' AND deregistration_id = 'N732DH-2013-02-21' 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 SIMA201101802Sign · brokenDURING MAINTENANCE BASE VISIT FOUND THE CABIN OVERHEAD LINER EMERGENCY EXIT SIGN BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CABIN OVERHEAD EMERGENCY EXIT SIGN IAW EMB 135 AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WSDR SIMA200702302Unknown · leakingNR 2 SHUTDOWN DUE TO A LOUD POP FOLLOWED BY ENGINE OIL QUANTITY DROPPING TO 3 QUARTS, ITT IN AMBER RANGE EXCEEDING 930 DEGREES, AIRSPEED 280 KNOTS, FLIGHT LEVEL 350. MULTIPLE EICAS MESSAGES, PUNGENT WHITE SMOKE ENTERED CABIN, DISSIPATED AFTER SHUTDOWN OF NR 2SDR SIMA200427904Floor Support · corrodedCENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. CUT OUT A SECTION OF THE OMEGA BEAM TO REMOVE DAMAGE. FABRICATED A REPAIR ANGLE, FILLER AND SHIMS. REPAIR DOEN IAW EMB 145SRM (SRM EMB 145/1142 REV 27) CHAPTER 53-22-10, FIG 203. (SW21200500268)SDR SIMA200427905Floor Support · corrodedCORROSION WAS FOUND ON A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20. REMOVED RPREVIOUS REPAIR. FABRICATED A DOUBLER ANGLE, FILLER, REINFORCEMENT PLATE AND 2 SHIMS. REPAIR DONE IAW EMB 145 SRM (SRM 145/1142, CHAPTER 53, REV 27) 53-21-10 ITEM 2 FIGURE 2SDR SIMA200426901Stringer · chafedABI - DURING AN IMBV INSPECTION, STRINGER 19R WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3093A DATEDSDR SIMA200426906Sill · corrodedABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED DAMAGED SILL AND INSTALLED NEW SILL IAW EMB REPAIR STATEMENT IC 2003/145-0818 DATED MARCH 6, 2003, AND AMERICAN EAGEL ENGINEERING TECHNICAL NOTICE EB 53-009. (M)SDR SIMA200426905Floor Support · corrodedDURING AN IMBV INSPECTION, THE FORWARD GALLEY FLOOR DIGITAL WAS FOUND CORRODED. CUT OUT A DAMAGED SECTION FROM EXISTING DIGITAL AND CLEANED AREA. FABRICATED TWO REPAIR DOUBLERS AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 53-21-10 ANDSDR SIMA200426904Beam · corrodedDURING AN IMBV INSPECTION THE GALLEY CENTER BEAM WAS FOUND CORRODED. CUTOUT A SECTION OF THE DAMGAED AREA. FABRICATED A U SHAPE DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 27, CHAPTER 53-21-10 PARA 5 FIG 204 SHEET 2. (M)SDR SIMA200217322Frame · bentAPU COWLING INTERIOR FORWARD FRAME IS BENT ABOVE THE TOP LEFT MOUNT HOLE, RECONTOURED FORWARD FRAME, PERFORMED NDT, NO DEFECTS. DONE IAW SRM AND MFG GST.SDR SIMA200217316Skin · gougedTHREE GOUGES BETWEEN FRAMES 15-16, BETWEEN STRINGERS 16L AND 17L. (SUP) BLENDED GOUGES, PERFORMED NDT WITH NO DEFECTS. GOUGES ACCEPTED AS IS IAW MFG GST.SDR SIMA200217317Skin · gougedGOUGE IN FUSELAGE SKIN BETWEEN FRAMES 71 AND 72 AND STRINGERS 16R AND 17R. BLENDED GOUGE, PERFORMED NDT WITH NO DEFECTS. GOUGE ACCEPTED AS IS IAW MFG GST.SDR SIMA200217318Skin · gougedGOUGE ON FORWARD EDGE OF MAIN DOOR SKIN. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. GOUGED ACCEPTED AS IS IAW MFG GST.SDR SIMA200217319Structure · gougedGOUGE BETWEEN JUNCTION 1 AND FRAME 14, ALONG STRINGER 15L. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST.SDR SIMA200217320Structure · gougedGOUGE BETWEEN FRAMES 16-17 BETWEEN STRINGERS 16L AND 17L. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST.SDR SIMA200217321Skin · gougedLEFT NR 1 LEADING EDGE GOUGED 11 INCH INBOARD OF LANDING LIGHT LENS COVER. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST.SDR SIMA200208712Fire Warning · false activationRDU - FLT 4549 - ON CLIMB-OUT, CREW HAD CARGO COMPARTMENT SMOKE WARNING AND DISCHARGED FIRE BOTTLES. DECLARED EMERGENCY AND RETURNED TO RDU. NO FIRE NOTICED. REPLACED CARGO FIRE BOTTLES. PERFORMED SYSTEMS OPS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICESDR SIMA20011079Smoke · detectedLGA - FLT 4521 - DURING INITIAL POWER UP ON AIRCRAFT WITH BATTERY AND AVIONICS SWITCHES ON, SMOKE WAS OBSERVED POURING OUT OF THE CENTER CONSOLE. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. PERFORMED APU START AND RAN ELECTRICAL SYSTEM AND FOUND NO EVIDENCESDR SIMA200102901Structure · leakingLGA - FLT 4559 - DURING CLIMB, CREW REPORTED A PRESSURIZATION LEAK IN THE FORWARD NOSE GEAR AREA. CABIN PRESSURE STARTED TO CLIMB TO 6 PSI AT 5000 FEET. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK IAW EMB MM 21-31-00 WAS GOOD AND AIRCRAFT
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