N388AE, cancelled Apr 9, 2008

Service difficulty reports · 19

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 = 'N388AE' AND deregistration_id = 'N388AE-2008-04-09'
  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 SIMA200427203Connector · looseEMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT DOES NOT ILLUMINATE. RESECURED GALLEY CONNECTOR OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200500061)Sep 27, 2004 · N388AE · Saab 340B · Emergency LightingSDR SIMA200415412Skin · dentedDURING AN MBV INSPECTION FRAME 677 WAS FOUND TO BE DENTED JUST ABOVE THE FLOOR ON THE RIGHT SIDE OF THE FUSELAGE. RECONTOURED THE DAMAGED AREA. PERFORMED EDDY CURRENT INSPECTION OF THE REWORKED AREA, NO DEFECTS NOTED. FABRICATED A ANGLED REPAIR DOUBLER. REPMay 26, 2004 · N388AE · Saab 340B · Fuselage Main, Plate/SkinSDR SIMA200415413Skin · dentedABI - AIRCRAFT ARRIVED FOR REPAIR OF HAIL DAMAGE ON THE RIGHT SIDE OF THE VERTICAL STAB AND MBV INSPECTION. CUTOUT TWO DISBOND DENTS. THIRTEEN ABOVE VOR ANTENNA 6.0 AND 9.0 FORWARD OF TRAILING EDGE. FABRICATED TWO FILLERS, FILLER CUT OUT CORES WITH LY/HY 50May 26, 2004 · N388AE · Saab 340B · Vertical Stabilizer, Plate/SkinSDR SIMA200415407Frame · corrodedDURING AN MBV INSPECTION, FRAME 258 WAS FOUND TO HAVE CORROSION BENEATH A PREVIOUS DOUBLER REPAIR. REMOVED THE PREVIOUS DOUBLER, SHIMS, AND FILLER. DOUBLER AND SHIMS INSPECTION AND FOUND TO BE SERVICEABLE. COMPLETELY REMOVED CORROSION BY CUT OUT. PERFORMED May 22, 2004 · N388AE · Saab 340B · Fuselage Main, FrameSDR SIMA200415410Spar · elongatedDURING A MBV INSPECTION OF AIRCRAFT, FOUR RIGHT HORIZONTAL STAB FORWARD UPPE SPAR CAP FASTENERS HOLES AT THE INBOARD END WERE FOUND TO BE ELONGATED. REAMED ALL FOUR HOLES TO .286 OVERSIZE CONDITION AND ACCOMPLISHED COULD WORKING. PERFORMED EDDY CURRENT INSPEMay 22, 2004 · N388AE · Saab 340B · Horizontal Stabilizer, Spar/RibSDR SIMA200415408Frame · corrodedDURING AN MBV INSPECTION, THE UPPER FLANGE OF FRAME 272 WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED THE EMERGENCY BATTERY PACK MOUNTING BRACKET TO ACCESS THE REPAIR AREA. COMLETELY REMOVED THE CORROSION BY CREATING A 2.5 INCH CUTOUT OF THE UPPER FLANMay 20, 2004 · N388AE · Saab 340B · Fuselage Main, FrameSDR SIMA200415409Skin · damagedAIRCRAFT SUSTAINED HAIL DAMATE THAT NECESSITATED THE REPLACEMENT OF THE LEFT HORIZ, STAB UPPER SKIN. REMOVED DAMAGED UPPER SKIN. TRIMMED AND INSTALLED NEW SKIN. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 42, 51-40-21, 22,23, 25, 40, 60, 51-20-50 AND SAAB May 19, 2004 · N388AE · Saab 340B · Horizontal Stabilizer, Plate/SkinSDR SIMA200415406Frame · corrodedABI - DURING AN MBV INSPECTION, THE UPPER FLANGE OF FRAME 225 WAS FOUND TO CORRODED BEYOND SRM LIMITS. COMPLETELY REMOVED THE CORROSION BY CREATING A 3.0 CUTOUT OF THE UPPER FLANGE. FABRICATED A REPAIR ANGLE, SPACER AND FILLER PIECE. REPAIR DONE IAW SAAB REPMay 19, 2004 · N388AE · Saab 340B · Fuselage Main, FrameSDR SIMA200415411Skin · damagedABI - AIRCRAFT SUSTAINED HAL DAMAGE THAT NECESSITATED THE REPLACEMENT OF THE RIGHT HORIZ STAB UPPER SKIN. REMOVED DAMAGED UPPER SKIN. TRIMMED NEW SKIN AND INSTALLED. REPAIR DONE IAW SAAB 340 SRM, 72LKS 3079 REV 43, 51-40-21, 22, 25, 40, 51-20-50, 51-40-60 AMay 19, 2004 · N388AE · Saab 340B · Horizontal Stabilizer, Plate/SkinSDR SIMA200415414Skin · chafedDURING A MBV INSPECTION OF THE RIGHT WING TO NACELLE FILLET AREA THE INBOARD SIDE WAS FOUND TO BE CHAFED. BLENDED CHAFED AREA. PERFORMED AND EDDY CURRENT INSPECTION OF BLENDED AREA. NO CRACKS NOTED. FABRICATED A REPAIR DOUBLER FOR REPAIR. WORK DONE IAW SAMay 19, 2004 · N388AE · Saab 340B · Wing, Plate/SkinSDR SIMA3881161Indicator · failedLOST RIGHT TORQUE INDICATION ON TAKEOFF/ ABORTED TAKEOFF NOTIFICATION WAS VIA TELLISIS FROM FLT CREW- C/A RIA RT TORQUE INDICATOR WITH SERVICEABLE TORQUE INDICATOR. OPS CHECK GOOD IAW MFG AMM.Apr 26, 2002 · N388AE · Saab 340B · Engine BMEP/Torque IndicatingSDR SIMA20130601Light · misinstalledCREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE FLIGHT ATTENDANT JUMPSEAT IS INOPERATIVE. MAINTENANCE FOUND THE LIGHT ASSEMBLY TO BE INSTALLED INCORRECTLY. LIGHT ASSEMBLY WAS REINSTALLED CORRECTLY IAW SAAB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNNov 2, 2001 · N388AE · Saab 340B · Emergency LightingSDR SIMA0554Fire Loop · chafedTUL - FLT 3735 - CREW REPORTED THE RIGHT ENGINE FIRE DETECT FAIL FOLLOWED BY RIGHT ENGINE FIRE INDICATION. CREW SHUT DOWN ENGINE AND SHOT ENGINE FIRE BOTTLES. MAINTENANCE FOUND A FIRE LOOP CHAFED AND NO EVIDENCE OF FIRE. FIRE LOOP WAS REMOVED AND REPLACED, Feb 24, 2001 · N388AE · Saab 340B · Fire DetectionSDR SIMA1682Transducer · inoperativeDFW - FLT 3263 - IN FLIGHT AT 135 KNOTS IN CLIMB, RUDDER LIMITER LIGHT ILLUMINATED. FOLLOWED AOM PROCEDURES, LIGHT CONTINUES TO ILLUMINATE. REMOVED AND REPLACED TRANSDUCER 9CL. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. (M)Jun 16, 2000 · N388AE · Saab 340B · Rudder Control SystemSDR SIMA980501Wheel · brokenDFW - FLT 3804 - NR 1 MAIN WHEEL, ONE-THIRD OF RIN BROKEN OFF, CAUSING THE TIRE TO LOOSE PRESSURE. RAI'D TIRE SHEEL ASSY, RAI'D NR 2 TIRE WHEEL ASSY AS PRECAUTIONARY. PERFORMED VISUAL INSPECTION FOR EXTERIOR DAMAGE TO SKIN, NO DISCREPANCIES NOTED. AIRCRAFT Feb 19, 1998 · N388AE · Saab 340B · Wheel/Ski/FloatSDR SIMA9701602Ballast · failedDFW - FLT 3846 - ELECTRICAL SMOKE SMELL IN CABIN, OVERWING EMERGENCY EXIT AREAS. INSPECTED AND FOUND BALLAST, AT SEATS 9B/C AND 10B/C BURNED. RAI'D BALLAST IAW 33-21-10. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 9, 1997 · N388AE · Saab 340B · Passenger Compartment LightingSDR SIMA9700581Light · failedFLT 3935 - SGF - ON APPROACH TO SGF, THE CREW REPORTED THE LAV LIGHT EMITTED A SMALL AMOUNT OF SMOKE. THE SMOKE DETECTOR DID NOT ILLUMINATE, AND TWO SMALL SCORCH MARKS WERE FOUND ON PANEL. AIRCRAFT LANED WITHOUT INCIDENT. MX INVESTIGATION REVEALED THE LIGHTFeb 27, 1997 · N388AE · Saab 340B · Passenger Compartment LightingSDR SIMA961412Hmu · failedIAH - FLT 3671 - DURING DESCENT FROM 12,000 FEET, A LOUD POP WAS HEARD FROM NR 1 ENGINE FOLLOWED BY A DECREASE IN TEMPERATURE, TORQUE, AND ENGINE SPEED. IGNITION LIGHT CAME ON BUT ENGINE DID NOT RE-LIGHT. THE CREW FOLLOWED THE ENGINE FAILURE CHECK LIST AND LMay 20, 1996 · N388AE · Saab 340B · Fuel Controlling SystemSDR SIMA961361Engine · failedFYV - FLT 3687 - DURING LANDING ROLL-OUT, CAPTAIN REPORTED GETTING LEFT OVERTEMP, CHIP DETECTOR, AND OIL PRESSURE WARNINGS. ENGINE SHUT DOWN. REMOVED AND REPLACED ENGINE. AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES, 288. (X)May 15, 1996 · N388AE · Saab 340B · Engine (Turbine/Turboprop)
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