N803MA

Service difficulty reports not matched to an aircraft · 86

They name N803MA, 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 = 'N803MA' 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.

SDR 2003F00542Hydraulic Line · damagedON TAKEOFF, OUT OF SDF AT GEAR ROTATION LOST SYS 'A' HYD FLUID, SHUT PUMPS OFF ACCOMPLISHED ABNORMAL CHECKLIST. REMOVED AND REPLACED HOSE ASSEMBLY NR 2 ENGINE P/N 10-60563-40, NO METAL FOUND IN CASE DRAIN FILTERS OR SUPPLY FILTERS REPLACED NR 1 AND NR 2 HYDRAJun 27, 2003 · N803MA · Boeing 727225 · Hydraulic System, MainSDR 2003F00383Clamp · looseON CLIMB-OUT FROM MIA, PASSING THROUGH F/ 29 LOWER AFT BODY OVERHEAT LIGHT CAME ON. FOLLOWED AOM AND ISOLATION PROCEDURES. RETURNED TO MIA FOR MAINTENANCE ACTION. T/S PER MM 26-14-0. FOUND LOOSE CLAMP IN AFT CARGO COMPARTMENT SIDEWALL FORWARD CORNER. SECUMay 24, 2003 · N803MA · Boeing 727225 · Pneumatic Distribution SystemSDR 2002F01122Battery Pack · dischargedDURING PREFLIGHT TRANSIT, FOUND LEFT AFT OUTSIDE EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD IAW MM 33-50-01. (M)Nov 13, 2002 · N803MA · Boeing 727225 · Emergency LightingSDR 2002F01022Pump · malfunctionedDURING ASCENT FROM MIA 30 MINUTES INTO FLIGHT NR 2 'B' SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST, NO BREAKERS POPPED. AIRCRAFT RETURNED TO MIAMI. TROUBLESHOT HYDRAULIC SYSTEM. FOUND CURRENT DRAWS FROM RELAY ON PUMP NR 1 Oct 25, 2002 · N803MA · Boeing 727225 · Hydraulic Pump, AuxiliarySDR 2002F00923Battery Pack · dischargedDURING PREFLIGHT TRANSIT, FOUND EMERGENCY PATH LIGHTING INOPERATIVE BETWEEN ROWS 21/30. REMOVED AND REPLACED E PATH BATTERY PACK ON LEFT ROW 27 IAW 33-50-00. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)Sep 19, 2002 · N803MA · Boeing 727225 · Emergency LightingSDR 2002F00890Connector · dirtyAT POWER UP BEFORE TAKEOFF IN KEF, TAKEOFF WARN HORN CAME ON. AIRCRAFT WAS PROPERLY CONFIGURED. EXITED RUNWAY, CYCLED CONTROLS AND RUNUP, NO HELP. RETURN TO GATE. REMOVED CONNECTOR PLUG D4168P FOUND DIRTY. CLEANED CONNECTOR PLUG AND REINSTALLED. OPS CHECJul 10, 2002 · N803MA · Boeing 727225 · Instrument PanelSDR MYW2002F00000Engine · making metalPRIOR TO DESCENT NR 2 ENGINE LOW OIL PRESS/FILTER BYPASS LIGHT ILLUMINATED. ENG NR2 PARAMETERS INDICATION ARE NORMAL OIL PRESS 47 PSI, OIL TEMP 81 DEGREE C, EPR NR 2-165, N1-80.9, EGT-400 DEG. C, N2-85.9, FF-3000PPH, CSD IN TEMP 50 DEG. C, RISE -8 DEG. C. GEMay 13, 2002 · N803MA · Boeing 727225 · Engine (Turbine/Turboprop)SDR 2002F00224Battery Pack · dischargedBATTERY PACK AND BASE ASSEMBLY FAILED ON RIGHT SIDE OVERWING EXIT EMERGENCY LIGHT SYSTEM. REMOVED AND REPLACED BATTERY PACK AND BASE ASSY. OPS CHECK NORMAL ON GROUND IAW MM 33-50-00. AIRCRAFT RETURNED TO SERVICE. (M)Feb 2, 2002 · N803MA · Boeing 727225 · Emergency LightingSDR 2002F00225Switch · damagedON TAKEOFF, WARNING HORN WENT OFF ABORTING TAKEOFF. TROUBLESHOT WARNING SYSTEM TO DAMAGED SWITCH AND CHAFED WIRES. REPLACED SWITCH AND REPAIRED DAMAGED WIRING. OPS CHECK FOUND NORMAL ON GROUND IAW MM. AIRCRAFT RETURNED TO SERVICE. (M)Jan 24, 2002 · N803MA · Boeing 727225 · Central WarningSDR 2002F00016Connector · contaminatedEPL TRACK LIGHTS INOPERATIVE, AFT GALLEY RIGHT SIDE AND L2 DOOR. CLEANED TRAPPED MOISTURE IN TRACK CONNECTORS. OPS TEST NORMAL ON GROUND IAW MM 33-50-02. AIRCRAFT RETURNED TO SERVICE. (M)Dec 20, 2001 · N803MA · Boeing 727225 · Light System WiringSDR 2002F00015Light · inoperativeEPL TRACK LIGHTS INOPERATIVE. REPLACED AFT EPL TRACK LIGHT STRIP, OPS CHECK NORMAL ON GROUND IAW MM 33-50-02. AIRCRAFT RETURNED TO SERVICE. (M)Dec 20, 2001 · N803MA · Boeing 727225 · Emergency LightingSDR 2001F00732Switch · sticksTAKEOFF WARNING HORN CAME ON PRIOR TO BRAKE RELEASE ON RUNWAY. ISSUED MAINTENANCE FERRY PERMIT IN SFB. IN MIA, FOUND UPPER TAKEOFF WARNING SWITCH STICKING. REPLACED UNIT, OPS TEST NORMAL IAW MM 31-26-24. AIRCRAFT RETURNED TO SERVICE. (M)Nov 10, 2001 · N803MA · Boeing 727225 · Central WarningSDR 2001F00727Pitot Tube · obstructedNO AIRSPEED INDICATION ON CAPTAIN AIRSPEED INDICATOR WHEN AT 100 KNOT AS PER F/O INDICATION DURING TAKEOFF RUN. FOUND DEBRIS INSIDE CAPTAIN PITOT PROBE. FLUSHED CAPTAIN PITOT SYSTEM. SYSTEM OPS CHECK NORMAL IAW MM 34-11-00. AIRCRAFT RETURN TO SERVICE. (M)Nov 6, 2001 · N803MA · Boeing 727225 · Pitot/Static SystemSDR 2001F00641Warning System · malfunctionedDURING TAKEOFF ROLL, TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF BELOW 50 KNOTS, CLEARED RUNWAY, DOUBLED CHECKED FLT CONTROLS FOR TAKEOFF CONFIGURATION FOUND NORMAL, VISUAL INSPECTION OUTSIDE AIRCRAFT TO VERIFY FLT CONTROLS CONFIGURATION. PERFORMED TAKEOFFOct 25, 2001 · N803MA · Boeing 727225 · Central WarningSDR MYW2001F00000Tube · damagedAFTER TAKEOFF AT APPROXIMATELY 1500 FT. THE NR 1 ENGINE FIRE WARNING (BOTTLE AND BELL) ACTIVATED. AOM EMERGENCY PROCEDURES PER 2-C-2 COMPLIED WITH. DUMPED APPROXIMATELY 12000 POUNDS OF FUEL PER AOM PROCEDURE 2-A-B-1. RETURNED TO AIRPORT. PREPARED FOR 2 ENGISep 24, 2001 · N803MA · Boeing 727225 · Engine (Turbine/Turboprop)SDR 2001F00154Pulley · bindingAFTER TAKEOFF, DURING FLAP RETRACTION, FLAP AT 2 DEGREE OUTBOARD FLAPS WENT ASYMMETRIC. RETURNED TO MIAMI. TROUBLESHOT SYSTEM. FOUND PULLEY AT NR 7 FLAP CANOE BINDING, CAUSING IMPROPER INDICATION. FREED PULLEY, PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM SEJun 29, 2001 · N803MA · Boeing 727225 · Trailing Edge Flap Control SystemSDR 20010514SG003Charger · inoperativeON PREFLIGHT TRANSIT, FOUND R2 ''EMERGENCY EXIT'' SIGN LIGHT ABOVE DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CHARGER IAW MM 33-50-71. OPS CHECK GOOD. (M)Apr 3, 2001 · N803MA · Boeing 727225 · Emergency LightingSDR 20010406SG007Light · inoperativeON PREFLIGHT TRANSIT, FOUND AFT AREA EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED AFT AREA EMERGENCY EXIT LIGHT IAW MM 33-50-81, OPS CHECK GOOD. (M)Feb 14, 2001 · N803MA · Boeing 727225 · Emergency LightingSDR 20010214SG004Battery Pack · dischargedON PREFLIGHT TRANSIT, FOUND RIGHT MID EXTERNAL OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT MID OVERWING EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-22. OPS CHECK GOOD. (M)Jan 20, 2001 · N803MA · Boeing 727225 · Emergency LightingSDR 20010214SG003Battery Pack · dischargedON PREFLIGHT TRANSIT, FOUND LEFT MID EXTERNAL OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT MID OVERWING EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-22-101. OPS CHECK GOOD. (M)Jan 12, 2001 · N803MA · Boeing 727225 · Emergency LightingSDR 20010214SG005Battery Pack · dischargedON PREFLIGHT TRANSIT, FOUND FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-22. OPS CHECK GOOD. (M)Jan 10, 2001 · N803MA · Boeing 727225 · Emergency LightingSDR 20010119SG003Battery Pack · dischargedDURING PREFLIGHT TRANSIT, FOUND EMERGENCY EXIT LIGHT ABOVE R-2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-71, OPS CHECK GOOD. (M)Nov 16, 2000 · N803MA · Boeing 727225 · Emergency LightingSDR 20010112SG018Battery Pack · dischargedDURING PREFLIGHT TRANSIT, FOUND EMERGENCY EXIT LIGHT ABOVE R-2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-71. OPS CHECK GOOD. (M)Nov 4, 2000 · N803MA · Boeing 727225 · Emergency LightingSDR 20000515AP010Skin · tornFOUND LEFT WING NR 3 LEADING EDGE FLAP TORN AT TRAILING EDGE. BLENDED OUT DAMAGED AREA PER SRM 57-50-3. FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-50-3 PAGE 10 AND 51-10-2 PAGE 1. (M)Sep 10, 1999 · N803MA · Boeing 727225 · Leading Edge DevicesSDR 20000515AP041Light · inoperativeAFT AIRSTAIR UPPER EMERGENCY LIGHT DOES''NT WORK. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW MM 33-50-61 PAGE 403. (M)Sep 8, 1999 · N803MA · Boeing 727225 · Emergency LightingSDR 20000515AP039Ballscrew · corrodedNOSE LANDING GEAR MANUAL EXTENSION JACKSCREW HAS PITTING CORROSION. REMOVED AND REPLACED NLG MANUAL EXTENSION JACKSCREW IAW MM 32-34-1 PAGE 401, OPS CHECK GOOD IAW MM 32-34-0 PAGE 201. (M)Sep 8, 1999 · N803MA · Boeing 727225 · Landing Gear Retraction/Extension SystemSDR 99ZZZX3943Beam · crackedRIGHT WING J-BEAM HAS APPROXIMATELY .3750 INCH CRACK ABOVE NR 8 SPOILER ACTUATOR. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER STATED DESIGN FLAW OR WING FLEX CAUSE OF CRACK.Sep 8, 1999 · N803MA · Boeing 727225 · Wing Miscellaneous StructureSDR 99ZZZX3942Airstair · crackedAFT AIRSTAIRS, AREA AT RIGHT, STA 1263 JUST BELOW ACTUATOR ATTACH FITTING, AREA CRACKED. FOUND DURING C-MAINTENANCE CHECK. OPENING AND CLOSING OF STAIRS CAUSED AREA TO BE UNDER CONSTANT PRESSURE.Sep 8, 1999 · N803MA · Boeing 727225 · Entrance StairsSDR 99ZZZX3941Web · crackedCABIN FLOOR SUPPORT INTERCOSTAL WEB HAS APPROXIMATELY .25 INCH CRACK AT FORWARD END JUST AFT OF BS 400 AT BL ZERO. FOUND DURING C-MAINTENANCE CHECK. SUBMITTER SUGGESTED AREA EXPOSED TO HEAVY LOADS, STRESS.Sep 8, 1999 · N803MA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 99ZZZX3940Frame · corrodedLEFT AFT EXIT HATCH FRAME HAS SIGNS OF CORROSION AT LOWER AFT CORNER. FOUND DURING SCHEDULED C-CHECK. SUBMITTER STATED AREA EXPOSED TO MOISTURE AND OTHER ELEMENTS.Sep 8, 1999 · N803MA · Boeing 727225 · Fuselage Main, FrameSDR 99ZZZX3939Stiffener · crackedONE INCH CRACK AT TOP OF STIFFENER INSIDE RIGHT WING LEADING EDGE AT INBOARD SIDE OF LEADING EDGE RIB WDL 92.0. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED AREA SUBJECTED TO STRESS LOADS AND FLEX.Sep 8, 1999 · N803MA · Boeing 727225 · Wing Miscellaneous StructureSDR 99ZZZX3938Web · crackedLEFT WING LEADING EDGE LBL 92.0 WEB CRACKED 1.5 INCHES DOWN FROM TOP AFT VERTICAL STIFFENER. ACCESS 6302. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED WING FLEX OR STRESS LOADS POSSIBLE CAUSE.Sep 8, 1999 · N803MA · Boeing 727225 · Wing Miscellaneous StructureSDR 99ZZZX3937Floorbeam · corrodedCABIN FLOORBEAM ST STA 1030, LBL 24 THROUGH RBL 25 HAS CORROSION. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER STATED AREA IS EXPOSED TO LIQUID SPILLS.Sep 8, 1999 · N803MA · Boeing 727225 · Fuselage Main, Floor BeamSDR 99ZZZX3936Angle · corrodedCABIN AFT LAVATORY (LEFT SIDE) FLOOR SUPPORT ANGLE AT STA 1150 THROUGH STA 1180 LBL 24 HAS CORROSION. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED LIQUID SPILLS ARE POSSIBLE CAUSE FOR PROBLEM.Sep 8, 1999 · N803MA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 99ZZZX3935Stiffener · crackedONE INCH CRACK AT TOP OF SECOND FROM AFT STIFFENER INSIDE RT WING LE AT INBOARD SIDE OF LEADING EDGE RIB WBL 92.0, ACCESS CUT-OUT 6402. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. AREA EXPOSED TO STRESS LOADS.Sep 8, 1999 · N803MA · Boeing 727225 · Wing Miscellaneous StructureSDR 99ZZZX3934Floorbeam · corrodedCABIN FLOORBEAM STA 400 RBL 12 TO RBL 12LT HAS CORROSION AND DAMAGE HOLE. FOUND DURING SCHEUDLED C-MAINTENANCE CHECK. AREA EXPOSED TO ENVIRONMENTAL CHANGES AS WELL AS LIQUID SPILLS, ETC.Sep 8, 1999 · N803MA · Boeing 727225 · Fuselage Main, Floor BeamSDR 99ZZZX3933Skin · crackedAPPROXIMATELY .6250 INCH CRACK AT LEFT OUTBOARD FOREFLAP LOWER LEADING EDGE ABOVE NR 1 FLAP TRACK. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. AREA EXPOSED TO STRESS LOADS AS WELL AS BENDING LOADS.Sep 8, 1999 · N803MA · Boeing 727225 · Leading Edge DevicesSDR 20000515AP009Skin · crackedFOUND LEFT INBOARD FORE FLAP LEADING EDGE HAS CUT AT CENTER SECTION. STOP DRILLED IAW SRM 57-50-4 HFEC, CRACK CONTAINED AT STOP DRILL PART 6 51-00-00, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-50-4 AND 51-30-2 PAGE 4. (M)Sep 5, 1999 · N803MA · Boeing 727225 · Leading Edge DevicesSDR 20000515AP008Flap Track · corrodedFOUND NR 3 FLAP TRACK AFT ATTACH AREA TOP SURFACE CORRODED. ACCOMPLISHED REPAIR AND INSTALLED FLAP TRACK IAW SB 727-57-0178. (M)Sep 2, 1999 · N803MA · Boeing 727225 · Trailing Edge FlapsSDR 20000515AP015Floorbeam · corrodedFOUND CABIN FLOORBEAM AT STATION 1110 RBL 18 THROUGH LBL 18 HAS CORROSION AT UPPER AND LOWER SURFACE. REMOVED CORROSION AT FLOORBEAM BETWEEN LBL 18 THROUGH RBL 16. REPAIRED FLOORBEAM AT RBL 17 IAW SRM 53-10-8 FIG 3. (M)Sep 2, 1999 · N803MA · Boeing 727225 · Fuselage Main, Floor BeamSDR 20000515AP003Frame · crackedFOUND CRACK IN FORMER AT STATION 930 AND STRINGER 14L. REPAIRED FRAME IAW SB 727-53-0162, REVISION 1. (M)Sep 1, 1999 · N803MA · Boeing 727225 · Fuselage Main, FrameSDR 20000515AP007Bracket · damagedFOUND VERTICAL STABILIZER LEADING EDGE THROUGH PANEL 9502 UPPER RIGHT CORNER BRACKET AND WEB DAMAGED. REMOVED INNER PANEL, CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR IAW SRM 51-10-1 PAGE 4, 51-40-2 PAGE 2, 51-30-1 PAGE 1, 55-10-1 PAGE 6. (M)Aug 31, 1999 · N803MA · Boeing 727225 · Vertical StabilizerSDR 20000515AP040Beam · corrodedRIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE SKIN FROM NR 1 TO NR 3 ELEVATOR ATTACH HINGE AREA HAS SPOTS OF CORROSION. REMOVED TRAILING EDGE BEAM IAW SRM 51-30-2 PAGE 1. INSTALLED TRAILING EDGE BEAM IAW SRM 55-10-6 FIG 1, 51-30-2 PAGE 1. (M)Aug 31, 1999 · N803MA · Boeing 727225 · Horizontal Stabilizer StructureSDR 20000515AP012Seat Track · corrodedFOUND CABIN FLOOR SEAT TRACK SUPPORT BASE HAS CORROSION AT STATION 1020 THROUGH 1130 LBL 25. REMOVED CORROSION, OUT OF LIMITS STATION 990-1130. REMOVED AND REPLACED SEAT TRACK STATION 990-1130 IAW SRM 53-10-30 PATE 20, 51-10-2 PAGE 1. (M)Aug 29, 1999 · N803MA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 20000515AP028Frame · crackedLEFT HORIZONTAL STABILIZER INNER COMPARTMENT NR 5 INBOARD RIB HAS SUPPORT CHORD CRACKED. CUT OUT SKIN TO GAIN ACCESS TO SUPPORT CHORD 3 INCH BY 6 INCH. REMOVED SUPPORT CHORD. FABRICATED AND INSTALLED SUPPORT CHORD. INSTALLED DOUBLER REPAIR TO SKIN CUT OUT Aug 29, 1999 · N803MA · Boeing 727225 · Horizontal Stabilizer, Spar/RibSDR 20000515AP027Angle · crackedFOUND VERTICAL STAB INNER COMPARTMENT RIB NR 9 RIGHT STRINGER NR 9 CRACKED AT ATTACH BOLT. REMOVED CRACKED AREA. NDT AREA FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-4 FIG 1, 55-30-5 FIG 1. (M)Aug 28, 1999 · N803MA · Boeing 727225 · Vertical StabilizerSDR 20000515AP026Angle · crackedFOUND VERTICAL STABILIZER INNER COMPARTMENT NR 8 RIGHT STRINGER NR 8 CRACKED AT ATTACH BOLT. REMOVED CRACKED AREA. NDT AREA FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-4 FIG 1, 55-30-5 FIG 1. (M)Aug 28, 1999 · N803MA · Boeing 727225 · Vertical StabilizerSDR 20000515AP025Angle · crackedFOUND VERTICAL STAB INNER COMPARTMENT NR 6 RIGHT SUPPORT WEB BETWEEN STRINGER NR 8 AND NR 9 CRACKED AT LOWER CORNER. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED ANGLE IAW SRM 51-40-3 PAGE 7. (M)Aug 28, 1999 · N803MA · Boeing 727225 · Vertical StabilizerSDR 20000515AP014Intercostal · corrodedFOUND CABIN FLOOR INTERCOSTAL AT STATION 1110 THROUGH 1130 AT BL 0 HAS CORROSION AT UPPER AND LOWER SURFACE. REMOVED INTERCOSTAL. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-30-2 PAGE 6, 51-20-1 PAGE 4. (M)Aug 26, 1999 · N803MA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 20000515AP013Seat Track · corrodedFOUND CABIN FLOOR SEAT TRACK STATION 1060 RBL 24 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK AT STATION 1060 RBL 24 IAW SRM 53-10-5 PAGE 3, 51-10-2 PAGE 2. (M)Aug 26, 1999 · N803MA · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
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