Boeing 727-214

Service difficulty reports · 296

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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 aircraft_model_key = '727214'
  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 GAIA00625Loop · out of positionDISCREPANCY: DURING CRUISE, THE #3 ENGINE STRUT OVERHEAD LIGHT ILLUMINATED. EXECUTED PROCEDURES IAW KHA AOM VOLUME 1. THE AIRCRAFT CONTINUED TO TOL AND MADE AN UNEVENTFUL LANDING.CORRECTIVE ACTION: MAINTENANCE OPENED THE #3 ENGINE LOWER STRUT PANELS AND INSPECSep 27, 2000 · N750US · Boeing 727214 · Overheat DetectionSDR GAIA00508Control Cable · brokenFLT 504 - TOL-DAL - DURING TAKEOFF, THE CREW EXPERIENCED ASYMMETRICAL FLAP SPLIT ON THE OUTBOARD FLAPS, RT AT 5 DEGREES, LEFT AT FLAPS 15 DEGREES. TEH CREW DECLARED AN EMERGENCY AND RETURNED TO TOL. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE TROUBAug 29, 2000 · N750US · Boeing 727214 · Trailing Edge Flap Control SystemSDR GAIA00441Detector · out of positionFLT 2731 - LRD-BRO - LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED ON DESCENT INTO BRO. FOLLOWED AOM LOER AFT BODY OVERHEAT PROCEDURES. THE AIRCRAFT MADE AN UNEVENTFUL LANDING IN BRO. REPOSITIONED AFT BODY HEAT WARNING STRIP. OPERATIONALLY CHECKS GOOD. AIRCRAFJul 24, 2000 · N750US · Boeing 727214 · Overheat DetectionSDR GAIA00437Module · malfunctionedFLT 2708 - MEM-SLC - DURING CLIMB-OUT, THE LOWER BODY AFT OVER HEAT LIGHT WAS ILLUMINATED. THE AIRCRAFT CONTINUED TO SLC AND MADE A NORMAL ROUTINE LANDING. MAINTENANCE REPLACED THE FIRE AND OVERHEAT DETECTION UNIT. CARRIED OUT ENGINE RUN ON BOTH NR 1 AND NRJul 20, 2000 · N750US · Boeing 727214 · Overheat DetectionSDR 00381Flange · drilled throughDISCREPANCY: DURING ROUTINE "C" MAINTENANCE CHECK THE MAIN CARGO DOOR REINFORCEMENT BRACKET DRILLED INTO AT THE INBOARD FLANGE AT BODY STATION 672.0 STRINGER 7 LEFT. CORRECTIVE ACTION: REMOVED AND REPLACED REINFORCEMENT BRACKET IN ACCORDANCE WITH FAA ADVISOR CJun 30, 2000 · N751US · Boeing 727214 · Fuselage Main, StructureSDR GAIA00375Seat Track · corrodedDURING ROUTINE C-CHECK MAINTENANCE, FOUND ON SEAT TRACK FUSELAGE BS 370 LEFT BODY LINE 45. REPAIRED IAW B727 SRM 53-10-5 AND REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 30, 2000 · N751US · Boeing 727214 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA00376Seat Track · corrodedDURING ROUTINE C-CHECK, FOUND CORROSION ON SEAT TRACK FUSELAGE BS 370 LEFT BODY LINE 25. REPAIRED IAW B727 SRM 53-10-5 AND REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 30, 2000 · N751US · Boeing 727214 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA00377Web · corrodedDURING ROUTINE C-CHECK, FOUND THE NR 2 LOWER CARGO DOOR FORWARD FRAME WEB BS 950E RIGHT BL 30 HAS CRACK INDICATION AT FASTENER HOLE. REPAIRED IAW B727 SB 53A0199 PART II, FORWARD CORNER. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 30, 2000 · N751US · Boeing 727214 · Fuselage Miscellaneous StructureSDR GAIA00378Flange · crackedDURNIG ROUTINE C-CHECK, FOUND THE NR 4 SLAT ACTUATOR INBOARD ATTACHMENT FLANGE WAS CRACKED BETWEEN TWO MOUNTING BOLTS. REMOVED AND REPLACED ACTUATOR FLANGE AND LOCATED HOLES IN NEW FLANGE. INSTALLED AND REPAIRED IAW B727 SRM 51-30-5 AND 51-30-2. OPERATIONALJun 30, 2000 · N751US · Boeing 727214 · Leading Edge DevicesSDR GAIA00379Bushing · wornDURING ROUTINE C-CHECK, FOUND THE RIGHT WING, MAIN LANDING GEAR ATTACH FITTING, BUSHING HOLES WORN AND GOUGED. REPLACED BUSHING IAW B727 SB 57-153 REV 4. KIT NR 65C25353-19. BLENDED GOUGES IAW REO S00239. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 30, 2000 · N751US · Boeing 727214 · Wing, Landing Gear Attach FittingsSDR GAIA00380Angle · crackedDURING ROUTINE C-CHECK, FOUND A CRACK IN THE FORWARD UPPER HOLE IN THE UPPER VERTICAL FLANGE OF THE WING TO BODY RIB FITTING UPPER CHORD AT RIGHT BS 760.95. COMPLIED WITH BOEING 727 SB 727-57-0112 REV 5. INSTALLED SUPPORT ANGLE IAW BOEING 727 SB 57-0112 AND Jun 30, 2000 · N751US · Boeing 727214 · Wing Miscellaneous StructureSDR GAIA00372Attach Fitting · crackedDURING ROUTINE C-CHECK, MAINTENANCE FOUND THE LEFT AILERON TAB, OUTBOARD ATTACH HINGE CRACKED. INSTALLED ATTACH HINGE IAW BOEING 727 SRM 57-50-11. DOCUMENTED ON TIMCO NON ROUTINE 23300 W/O 101026. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 30, 2000 · N751US · Boeing 727214 · AileronsSDR GAIA00373Seat Track · corrodedDURING ROUTINE C-CHECK MAINTENANCE FOUND CORROSION ON SEAT TRACK FUSELAGE BS 580 LEFT BODY LINE 25 WATER LINE 208. REPAIRED IAW B727 SRM 53-10-5 AND REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 30, 2000 · N751US · Boeing 727214 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA00374Stringer Clip · damagedDURING ROUTINE C-CHECK MAINTENANCE, FOUND STRINGER CLIP DAMAGED AT BS 680 STRINGER 9 LEFT. REMOVED DAMAGE ON CLIP IAW B727 SRM 53-10-1. REMOVED BRACKET AND CLEANED DAMAGE. FOUND WITH IN LIMITS IAW B727 SRM 53-10-1 AND SRM 53-10-6. INSTALLED IAW BOEING SRM 5Jun 30, 2000 · N751US · Boeing 727214 · Fuselage Miscellaneous StructureSDR GAIA00279Boot · tornLRD/BRO - FLT 2731 - DURING CRUISE, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. FOUND SEVERAL LOOSE CLAMPS, ALSO TORN BOOT ON LEFT INLET DUCT. REMOVED AND REPLACED DUCT. TIGHTENED CLAMPS. OPERATIONAL CHECK PERFORMED OKAY. AIRCRAFT WAS RETURNED TO SERVICE. May 16, 2000 · N750US · Boeing 727214 · Air Intake Anti/De-Ice SystemSDR GAIA00259Warning Light · illuminatedDURING FLT 731, LRD-IAH - RED LEFT GEAR WARNING LIGHT ILLUMINATED. RECYCLED, LIGHT REMAINED ILLUMINATED. TEN MINUTES LATER LIGHT EXTINGUISHED. INSPECTED PROX SWITCH, WIRING AND CANNON PLUG. NO FAULTS FOUND, PER MM 32-61-0. OPERATIONAL CHECK GOOD. AIRCRAFApr 27, 2000 · N750US · Boeing 727214 · Landing Gear Position and WarningSDR 20000727AP004Valve · inoperativeFLT 503 - KDAY-KOKC - IN FLIGHT, COPILOT RMI (CAPTAINS HIS COMPASS NR 1) SYNCRONIZATION INFLIGHT 12 DEGREES OFF FROM COMPASS NR 2 AND MAGNETIC COMPASS. RETURNED KDAY WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED NR 1 FLUX VALVE IAW B727 MM 34-21-12. OPERATApr 19, 2000 · N227JL · Boeing 727214 · Attitude and Direction Data SystemSDR GAIA00181Stringer · crackedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND STRINGER CRACKED 4 INCHES AFT OF BS 720B.L REPAIRED AIW SRM 53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, Longeron/StringerSDR GAIA00182Frame · damagedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 540 FUSELAGE FRAME DAMAGED AT AND BELOW STRINGER 16R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, FrameSDR GAIA00183Seat Track · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CORROSION ON SEAT TRACK END AT RBL 24, FS 480. REPAIRED IAW SRM 53-10-5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA00184Seat Track · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CORROSION ON SEAT TRACK STATION 345, RBL 25. REPAIRED IAW SRM 53-10-5. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage, Seat/Cargo Attach FittingsSDR GAIA00185Frame · damagedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 520 FUSELAGE FRAME INBOARD FLANGE DAMAGED AT AND BELOW STRINGER 16R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, FrameSDR GAIA00186Shear Tie · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND SHEAR TIE CORRODED AT BS 640, RBL 13. REPAIRED IAW SRM 51-20-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, StructureSDR GAIA00187Stringer Clip · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CORROSION ON STRINGER SPLICE ON STRINGER 28R, BS 680. REPAIRED IAW SRM 53-10-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Miscellaneous StructureSDR GAIA00188Stringer Clip · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CORROSION ON STRINGER SPLICE ON STRINGER 28L, BS 680. REPAIRED IAW SRM 53-10-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Miscellaneous StructureSDR GAIA00189Stringer Clip · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CORROSION ON STRINGER SPLICE ON STRINGER 27L, BS 680. REPAIRED IAW SRM 53-10-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Miscellaneous StructureSDR GAIA00190Door Frame · crackedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND EXIT DOOR FRAME CRACKED AFT OF LATCH FITTING ON AIRCRAFT STATION 440R. REPAIRED IAW SRM 51-40-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, StructureSDR GAIA00191Frame · dentedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 440 FUSELAGE FRAME INBOARD FLANGE DENTED AT STRINGER 16R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, FrameSDR GAIA00192Frame · dentedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 660 FUSELAGE FRAME INBOARD FLANGE DENTED BELOW STRINGER 16R. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, FrameSDR GAIA00193Frame · misdrilledDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 950C FUSELAGE FRAME INBOARD FLANGE HAS DOUBLE DRILLED HOLE BELOW STRINGER 16L. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, FrameSDR GAIA00194Frame · crackedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 540 RBL 60, WL 212 INNER FRAME DOUBLER CRACKED. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, FrameSDR GAIA00195Keelbeam · crackedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CRACK IN KEEL BEAM LEFT LOWER CHORD. VERTICAL FLANGE FROM STATION 870 TO FIRST HI-LOCK HOLE. REPAIRED IAW SB 727-53-0208. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, KeelSDR GAIA00196Floorbeam · misdrilledDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND FLOORBEAM UPPER CHORD HAS NUMEROUS HOLES DRILLED AT BS 460, LBL 45. REPAIRED IAW SRM 53-10-8. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, Floor BeamSDR GAIA00197Frame · dentedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CIRCUMFERENTIAL FRAME DENTED BS 1166, LBL 63, WL 212. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, FrameSDR GAIA00198Angle · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND CORROSION ON LOWER L-ANGLE HORIZONTAL FLANGE AT STATION 880 WHEEL WELL WEB RBL 69, WL 189. REPAIRED IAW SRM 51-20-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Miscellaneous StructureSDR GAIA00199Angle · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND J-ANGLE CORRODED BS 1090 INBOARD SIDE AT STRINGER 29R. REPAIRED IAW SRM 51-20-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Miscellaneous StructureSDR GAIA00200Angle · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND J-ANGLE CORRODED BS 1090 TO 1100 OUTBOARD SIDE STRINGER 29R. REPAIRED IAW SRM 51-20-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Miscellaneous StructureSDR GAIA00201Stringer · corrodedDURING LIGHT CHECK AT TIMCO/OSC, FOUND CORROSION ON STRINGER 29R BS 1090. REPAIRED IAW SRM 53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, Longeron/StringerSDR GAIA00202Stringer · corrodedDURING LIGHT C-CHECK AT TIMC/OSC, FOUND STRINGER 30 HAS CORROSION JUST FORWARD OF FRAME 1166 IN BELLY OF AFT CARGO COMPARTMENT. REPAIRED IAW SRM 53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, Longeron/StringerSDR GAIA00203Skin · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND SKIN PILLOWED BELOW AFT WASTE SERVICE PANEL. REPAIRED IAW SRM 51-20-1 AND TIMCO REO S00124. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, Plate/SkinSDR GAIA00204Skin · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND SKIN BULGING AFT LAV SERVICE AREA LOWER AFT CORNER BS 1178. REPAIRED IAW SRM 51-20-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, Plate/SkinSDR GAIA00205Shear Tie · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND SHEAR TIE CORRODED BS 1166 ON RIGHT OF STRINGER 30. REPAIRED IAW SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, StructureSDR GAIA00206Stringer · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND STRINGER 22L SPLICE CORRODED. REPAIRED IAW SRM 51-30-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, Longeron/StringerSDR GAIA00207Frame · corrodedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND T-CHORD CORRODED LEFT SIDE OF NOSE LANDING GEAR WHEEL WELL STATION 335 AT STRINGER 25L. REPAIRED IAW TIMCO REO S00138. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, FrameSDR GAIA00176Frame · damagedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 804.5 FUSELAGE FRAME INBOARD FLANGE DAMAGED AT STRINGER 16L. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, FrameSDR GAIA00177Stringer · crackedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND STRINGER 15L CRACKED FOUR INCHES FORWARD OF BS 720C. REPAIRED IAW SRM 53-10-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, Longeron/StringerSDR GAIA00178Frame · misdrilledDURING LIGHT C-CHECK, AT TIMCO/OSC, FOUND MISDRILLED HOLE ON CIRCUMFERENTIAL FRAME BS 1148, LBL 64, WL 212. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, FrameSDR GAIA00179Skin · dentedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND DENT IN FUSELAGE SKIN AT BS 287 BELOW STRINGER 22L. REPAIRED IAW SRM 53-30-3. THE AIRCARFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, Plate/SkinSDR GAIA00180Frame · damagedDURING LIGHT C-CHECK AT TIMCO/OSC, FOUND BS 720 FUSELAGE FRAME DAMAGED AT STRINGER 16L. REPAIRED IAW SRM 51-40-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, FrameSDR GAIA00172Frame · damagedDURING LIGHT C-CHECK AT TIMCO/OSC, THE FOLLOWING DISCREPANCY WAS FOUND, BS 360 FUSELAGE FRAME INBOARD FLANGE DAMAGED AT S-16L. REPAIRED IAW SRM 51-40-3 FIG 1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 10, 2000 · N750US · Boeing 727214 · Fuselage Main, Frame
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