N889MA
Service difficulty reports not matched to an aircraft · 48
They name N889MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N889MA' AND registry_match IS NULL 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 = 'N889MA' AND registry_match IS NULL 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 2003F00136Battery Pack · dischargedDURING P/T FOUND DOOR 2 AISLE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK, LIGHTS OPS CHECKS GOOD IAW AMM 33-50-00. (M)SDR 2003F00105Light · inoperativeDURING P/T FOUND FORWARD MOST E-PATH LIGHT STRIP OUT. REMOVED AND REPLACED E-PATH LIGHT STRIP, OPS CHECK NORMAL. (M)SDR 2002F01021Battery · dischargedDURING PREFLIGHT, FOUND CENTER EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY FOR EXTERIOR OVERWING EXIT LIGHT. OPERATIONAL CHECKED OK IAW 33-50-22. AIRCRAFT RETURNED TO SERVICE. (M)SDR 2002F00226Valve · defectiveFOUND AIRCRAFT COULD NOT PRESSURIZE ON ASCENT, RIGHT PACK VALVE INTERMITTENT. A/C DESCENDED TO 10,000 FT. PERFORMED AOM PROCEDURES A/C LANDED. REPLACED PACK VALVE, OPS CHECK NORMAL ON GROUND. AIRCRAFT RETURN TO SERVICE. (M)SDR 2001F00455Light · inoperativeDURING PREFLIGHT, TRANSIT EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 28 CEILING INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AT ROW 28. OPS CHECK OK IAW B727 33-50-1. AIRCRAFT RETURNED TO SERVICE. (M)SDR 2001F00096Shutoff Valve · leakingWHILE ON SINGLE PACK OPERATION AND AT FL250 CABIN PRESS KEPT CLIMBING. FOLLOWED AOM PROCEDURE AND DESCENDED. WHILE DESCENDING CABIN CONTINUED TO CLIMB TO FL160 WITH THRUST LEVERS UP, PASS MASKS DROPPED AT 13,000 FEET. FOUND CLAMPS TO HEAT EXCHANGER VERY LOOSDR 20010125SG017Fuel Control · malfunctionedON TAKEOFF ROLL, ENGINE NR 3 DID NOT PRODUCE RATED TAKEOFF THRUST. CAPTAIN ABORTED TAKEOFF AT 80 KNOTS. A/C WEIGHT 180.8. REMOVED AND REPLACED FUEL CONTROL UNIT IAW 73-21-1. OPERATIONAL CHECKED NR 3 ENGINE IAW 71-00-00. (M)SDR 20010124SG004Fuel Control · malfunctionedON TAKEOFF ROLL, ENGINE NR 3 DID NOT PRODUCE RATED TAKEOFF THRUST. CAPTAIN ABORTED TAKEOFF AT 80 KNOTS. A/C WEIGHT 180.8. REMOVED AND REPLACED FUEL CONTROL UNIT IAW 73-21-1. OPS CHECKED NR 3 ENGINE IAW 71-00-00. OPS NORMAL. (M)SDR 20010406SG005Control Cable · out of adjIN CRUISE FLIGHT, NOSE GEAR DOOR LIGHTS COMES ''ON'' AT 310 KNOTS COMES BACK ''OFF'' AT 293 KNOTS. INSPECTED NOSE GEAR WW DOORS AND FOUND CABLES TO BE OUT OF TOLERANCE. ADJUSTED CABLES IAW 32-22-1. OPERATION CHECK GOOD. PERFORMED RETRACTION, SYSTEM OPS CHESDR 20000511AP029Beam · crackedFOUND J BEAM HAS TWO .375 INCH CRACKS AT LEFT WING TRAILING EDGE AREA ABOVE NR 7 SPOILER ACTUATOR AREAS. REMOVED WALKING BEAM PANEL AND SMALL SKIN PANEL IAW 51-30-2 PAGE 2. REMOVED J BEAM IAW 51-30-2 PAGE 1. INSTALLED J BEAM IAW 51-30-2 PAGE 4. INSTALLED RSDR 20000511AP028Beam · crackedFOUND J BEAM HAS .375 INCH CRACK AT RIGHT WING ABOVE NR 8 SPOILER ACTUATOR AREA. REMOVED RIGHT WING TOP SKIN AND WALKING BEAM PANEL IAW 51-30-2 PAGE 2. REMOVED J BEAM AT RIGHT WING ABOVE NR 8 SPOILER. INSTALLED NEW J BEAM IAW 51-30-2 PAGE 1. INSTALLED REMOSDR 20000511AP027Retainer · crackedSEAL RETAINER CRACKED ABOVE RIGHT ELEPHANT EAR FAIRING ON AFT SEGMENT. REMOVED SEAL RETAINER, DRILLED HOLES IN NEW RETAINER IAW 51-30-2 PAGE 5. INSTALLED RETAINER IAW 51-30-2 PAGE 5. (M)SDR 20000511AP026Web · crackedVERTICAL FIN LEADING EDGE PANEL 9602 INNER CURVED WEB HAS 1 INCH CRACK AT CORNER. STOP DRILLED CRACK IAW 51-10-1 PAGE 613. FABRICATED DOUBLER IAW 51-40-2 PAGE 2, 3, 6. TREATED AND PRIMED IAW 51-10-2 PAGE 1. INSTALLED DOUBLER AND WEB IAW 51-30-2 PAGE 1. (MSDR 20000511AP025Web · tornVERTICAL LEADING EDGE CENTER SECTION INTERIOR WEB IS DAMGED AT THREE CORNERS. CUT OUT DAMAGED AREAS IAWS 51-40-2 PAGES 2/3. HFEC SHOWS NO CRACKS IAW 51-00-00 PAR 6. TREATED AND PRIMED IAW 51-10-2 PAGE 1. INSTALLED REPAIR IAW 51-40-2. (M)SDR 20000511AP024Bracket · crackedFOUND NR 7 SPOILER OUTBOARD HINGE SUPPORT CRACKED. REMOVED CRACKED HINGE SUPPORT BRACKET. DRILLED NEW SUPPORT BRACKET IAW 51-10-1 PAGE 14. INSTALLED NEW HINGE SUPPORT BRACKET IAW 51-10-1 PAGE 1. (M)SDR 20000511AP023Floorbeam · corrodedTOP OF FLOORBEAM BS 1110 BL 0 - LBL 12 AND BL 0 - RBL 12. REMOVED CORROSION IAW 51-10-6 PAGE 2. AREA OUT OF LIMITS. CUT OUT DAMAGED AREA IAW 53-10-8 FIG 8. FABRICATED ANGLE AND FILLER REPAIR IAW 53-10-8 FIG 8 SHEET 4-5. ACCOMPLISHED HFEC AROUND EDGES OF CSDR 20000511AP022Flap Track · corrodedRIGHT OUTBOARD MID FLAP INBOARD TRAILING EDGE FLAP TRACK CORRODED. REMOVED RETAINER CHANNEL IAW 51-30-2 PAGE 3. FABRICATED RETAINER IAW 51-10-1 PAGE 1. TREATED AND PRIMED IAW 51-10-2 PAGE 4. INSTALLED NEW RETAINER CHANNEL IAW 51-30-3 PAGE 2. (M)SDR 20000511AP021Floor Support · corrodedFOUND FLOOR SUPPORT BS 1110 TO 1130 LBL 12 CORRODED. REMOVED FLOOR SUPPORT IAW 51-30-2 PAGE 1. FABRICATED SUPPORT IAW 51-10-1 PAGE 2. TREATED AND PRIMED IAW 51-10-2. INSTALLED FLOOR SUPPORT IAW 51-30-2 PAGE 1. (M)SDR 20000511AP020Floorbeam · groovedFOUND FLOORBEAM BS 1110 LBL 45 HAS 2.5 INCH GROOVE CENTER OF TOP FLANGE. REMOVED WEB, SIDE WALLS AND SEAT TRACK. CUT OUT DAMAGED AREA IAW 53-10-2 FIG 3. ACCOMPLISHED HFEC INSPECTION AROUND EDGES OF CUTOUT IAW 51-00-00. NO CRACKS NOTED. FABRICATED FLOORBEASDR 20000511AP019Support Bracket · bentSUPPORT FOR CONDUIT CRACKED AND BENT BS 1110 TO 1130 LBL 33. REMOVED DAMAGED U CHANNEL SUPPORT AND ANGLE BRACKET IAW 51-30-2 PAGE 1/2. FABRICATED NEW U CHANNEL IAW 51-40-3 PAGE 3. TREATED, PRIMED AND PAINTED IAW 51-10-2 PAGE 2. INSTALLED U CHANNEL SUPPORT SDR 20000511AP018Angle · crackedCABIN FLOOR SUPPORT INTERCOSTAL TOP ANGLE CRACKED AT SCREWHEAD BL 0 BETWEEN BS 950A AND 950B. REMOVED ANGLE IAW 51-30-2 PAGE 2. FABRICATED NEW ANGLE IAW 51-40-2 PAGE 3. TREATED AND PRIMED IAW 51-10-2. INSTALLED ANGLE IAW 51-30-2 PAGE 12. (M)SDR 20000511AP017Retainer · corrodedFOUND SEAL RETAINER CHANNEL CORRODED, LOCATED AT TRAILING EDGE OF RIGHT OUTBOARD MID FLAP. REMOVED RETAINER CHANNEL IAW 51-30-2 PAGE 3. FABRICATED NEW RETAINER CHANNEL IAW 51-10-1 PAGE 1. TREATED AND PRIMED IAW 51-10-2 PAGE 4. INSTALLED NEW RETAINER CHANNESDR 20000511AP016Skin · crackedVERTICAL STABILIZER LOWER LEADING EDGE FAIRING NR 9501 HAS .5 INCH CRACK IN SKIN AND CHAFED AROUND END. CUT OUT DAMAGED AREA IAW 51-40-2 FIG 1. FABRICATED DOUBLER IAW 51-40-2 FIG 1. INSTALLED REPAIR IAW 51-30-2 PAGE 2. (M)SDR 20000511AP015Angle · damagedCABIN FLOOR PANEL SUPPORT RIB BETWEEN STATION 720F AND 740 BL 0 TORN. REMOVED ANGLE SUPPORT BETWEEN STATION 720F TO 740 AT BL 0 IAW 51-30-2 PAGE 1. FABRICATED ANGLE SUPPORT IAW 53-10-4 PAGE 2. TREATED, PRIMED AND INSTALLED IAW 51-10-2 AND 51-30-2 PAGE 1. (SDR 20000511AP014Fairing · crackedFOUND .75 INCH CRACK AT TOP OF RIGHT INBOARD FLAP AFT TEARDROP FAIRING. REMOVED AND REPLACED RIGHT INBOARD FLAP AFT TEARDROP FAIRING. (M)SDR 20000511AP013Fairing · crackedFOUND 1.5 INCH CRACK AT AFT MOUNT HOLE OF LEFT INBOARD FLAP INBOARD TEARDROP FAIRING. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD TEARDROP FAIRING. (M)SDR 20000511AP011Seat Track · corrodedFOUND CABIN SEAT TRACK STATION 360 TO 440 RBL 48 HAS CORROSION. REMOVED CORROSION IAW 51-10-6 PAGE 12 FOUND OUT OF LIMITS IAW 51-10-1 PAGE 15. FABRICATED NEW SEAT TRACK IAW 53-10-5 PAGE 21. TREATED, PRIMED AND INSTALLED SEAT TRACK IAW 53-10-5 PAGE 21. (M)SDR 20000511AP010Seat Track · corrodedFOUND CABIN TRACK STATION 360 TO 420 RBL 24 HAS CORROSION. REMOVED CORROSION IAW 51-10-6 PAGE 2 FOUND OUT OF LIMITS. FABRICATES SEAT TRACK IAW 51-10-1. TREATED AND PRIMED IAW 51-10-2 PAGE 1. INSTALLED TRACK IAW 51-30-2. (M)SDR 20000511AP009Seat Track · corrodedCABIN FLOORBEAM STATION 320 LBL 46 HAS CORROSION AT ANCHOR NOT. REMOVED CORROSION IAW 51-10-6 PAGE 12. ACCOMPLISHED UT THICKNESS CHECK FOUND OUT OF LIMITS. CUT OUT DAMAGED AREA IAW 53-10-8 PAGE 49. FABRICATED ANGLES AND SPLICE, INSTALLED, TREATED IAW 53-10SDR 20000511AP008Seat Track · corrodedFOUND CABIN SEAT TRACK LBL 44 STATION 1110 TO 1070 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW 51-10-6 PAGE 6. REMVOED SEAT TRACK IAW 51-30-2 PAGE 5. FABRICATED SEAT TRACK IAW 53-10-5 PAGE 4. TREATED AND PRIMED IAW 51-10-2 PAGE 6. INSTALLED TSDR 20000511AP007Seat Track · corrodedFOUND CABIN SEAT TRACK STATION 1070 LBL 50 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW 51-30-2 PAGE 2. REMOVED HAT CHANNEL STATION 1070 LBL 50 IAW 51-30-2 PAGE 2. FABRICATED HAT CHANNEL IAW 51-10-1 PAGE 2. TREATED INSTALLED HAT CHANNEL IAW 51-1SDR 20000511AP006Strap · crackedFOUND .03125 INCH CRACK AT RIGHT WING FIXED LEADING EDGE AT AFT INBOARD END OF CUTOUT WHERE NR 5 SLAT INBOARD HOOK GOES INTO. REMOVED FASTENERS IAW 51-30-2 PAGE 1-2. STOP DRILLED CRACK IAW 51-10-1 PAGE 6. HFEC INSPECTION CONFIRMED CRACK CONTAINED IAW 51-00-SDR 20000511AP005Hinge · crackedFOUND .3125 INCH CRACK AT CUT OUT ON TOP OF LEFT WING FOR NR 4 SPOILER 2ND FROM OUTBOARD HINGE. STOP DRILLED CRACK IAW 51-10-1 PAGE 6B. HFEC INSPECTION CONFIRMED CRACK CONFINED IAW 51-30-2 PAGE 1. FABRICATED DOUBLER REPAIR IAW 57-30-4 FIG 10.8 PAGE 3. TREASDR 20000511AP004Seat Track · corrodedCABIN SEAT TRACK STATION 344 TO 400 LBL 44 HAS CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW 53-10-1 FIG 3. FABRICATED SEAT TRACK IAW 51-30-5 PAGE 1. TREATED INSTALLED IAW 51-10-2 PAGE 1 AND 51-30-2. (M)SDR 20000511AP003Seat Track · crackedCABIN SEAT TRACK STATION 344-400 LBL 24 HAS CORROSION. REMOVED CORROSION AND FOUND SEAT TRACK OUT OF LIMITS IAW 51-10-6 PAGE 12. FABRICATED NEW SEAT TRACK STATION 344-400 LBL 24 IAW 53-10-5 PAGE 4. TREATED AND PRIMED IAW 51-10-2 PAGE 2-4. INSTALLED SEAT TRSDR 20000511AP002Angle · crackedFLAP FAIRING SUPPORT ANGLE HAS 1.125 INCH CRACK AT INBOARD SIDE OF LEFT WING NR 3 FLAP TRACK BELOW AFT FALSE SPAR AREA. REMOVED FAIRING, ACCOMPLISHED HFEC INSPECTION CONFIRMED ENDS OF CRACK IAW 51-00-00 PAGE 6. STOP DRILLED CRACK IAW 51-10-1 PAGE 6B. HFEC ISDR 20000511AP001Angle · crackedANGLE HAS .25 INCH CRACK AT BOTTOM OF LEFT WING UPPER TRAILING EDGE PANEL, 5 FT FORWARD OF LEFT INBOARD AILERON INBOARD LEADING EDGE. REMOVED ANGLE AND FABICATED NEW ANGLE IAW 51-10-1 PAGE 2. INSTALLED ANGLE IAW 51-10-2 PAGE 1. (M)SDR 20000510AP007Skin · crackedFOUND .4374 INCH CRACK THROUGH FASTENER HOLE AT RIGHT OUTBOARD FOREFLAP LEADING EDGE ABOVE NR 7 FLAP TRACK AREA. STOP DRILLED CRACK IAW SRM 51-10-1 PAGE 1. FABRICATED COUPLER REPAIR IAW 57-50-4 PAGE 17. HFEC INSPECTION OF CUTOUT CONFIRMED NO CRACKS. FABRICSDR 20000510AP006Rib · crackedFOUND .75 INCH CRACK AT RIGHT WING OUTBOARD MIDFLAP INBOARD MOST RIB AT LOWER AFT END. REMOVED JACKSCREW FAIRING. FABRICATED SINGLE REPAIR IAW 57-50-2 PAGE 5. HFEC CONFIRMED CRACK IS CONTAINED BY STOP HOLE IAW 51-00-00 PAGE 6. INSTALLED ANGLE REPAIR IAW 57SDR 20000510AP005Skin · crackedFOUND .5 INCH CRACK AT FASTENER HOLE AND TWO RIVETS CRACKED LOWER LEADING EDGE SKIN OF LEFT WING NR 3 SLAT BELOW UPSTOP PAD AREA. ACCOMPLISHED HFEC INSPECTION AND MARKED END OF CRACK IAW 51-00-00 PART 6. STOPPED DRILLED END OF CRACK IAW 51-10-1 PAGE 3. HFEC SDR 20000510AP004Web · crackedFOUND 1.75 INCH CRACK AT LEFT WING OUTBOARD MID FLAP INBOARD MOST RIB AT LOWER AFT END. STOP DRILLED CRACK IAW SRM 51-10-1. FABRICATED WEB REPAIR IAW 51-40-2 PAGE 5. HFEC INSPECTION CONFIRMED CRACK WAS CONTAINED. FABRICATED WEB REPAIR IAW 51-40-2 PAGE 5. SDR 99ZZZX2824Track · corrodedLOG PAGE 25775. DURING INSPECTION OF AREA DUE TO REMOVAL OF FLAP FOR GROUND DAMAGE, FOUND SHIMS MIGRATED ON PAD A. REMOVED TRACK TO REPLACE. REMOVED AND REPLACED SHIMS AND NR 4 FLAP TRACK IAW BOEING SB 727-57-0178 REV 5. (X)SDR 99ZZZM381Lamp · disconnectedON PREFLIGHT TRANSIT, FOUND EPL TRACK LIGHTS BETWEEN ROW 17-18C INOPERATIVE. RECONNECTED EPL LIGHTS IAW 33-50-0. OPS CHECKED OK. (M)SDR 98ZZZM878Battery Pack · dischargedDURING PREFLIGHT, FOUND EXTERIOR EMERGENCY LIGHT, MOST AFT ON LEFT FAIRING INOPERATIVE. REPLACED BATTERY PACK IAW MM 33-50-22. OPS CHECK OK. (M)SDR 98ZZZX3400Light · inoperativeON PRE-FLIGHT TRANSIT, FOUND EPL LIGHT INOPERATIVE FROM ROWS 1-4; ALSO, L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. TROUBLESHOT SYSTEM. FOUND POWER CABLE ASSEMBLY SHORTED. REPLACED CABLE, OPS CHECK GOOD IAW 33-50-01.SDR MYWA970032Bulb · failedRIGHT AFT EMERGENCY EXIT SIGN - AFT BULB OUT. RELAMPED. OPS CHECK GOOD PER B727 MM 33-50-1. (X)SDR MYWA970008Turbine · failedON DESCENT WITH POWER APPROX 50 PERCENT, A MODERATE VIBRATION WAS FELT. WITH THRUST LEVER AT IDLE NO VIBRATION NOTE, HOWEVER, ON ACCELERATION VIBRATION INCREASED WITH LEVER MOVEMENT. REMOVED AND REPLACED NR 3 ENGINE S/N 700279. ON INSPECTION OF ENGINE FOUNDSDR 96ZZZX3977Actuator · failedLOG REPORT: GL521 AT MIA - RETURN FROM FLIGHT. AFTER TAKEOFF WHILE RETRACTING THE FLAPS FROM THE 5-DEGREE TO THE 2-DEGREE POSITIONS, THE LE FLAP AMBER INTRANSIT LIGHT ILLUMINATED ON THE FORWARD AND FE'S PANELS FOR THE NR 8 POSITION. REPLACED NR 8 SLAT ACTUA
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