Boeing 727-224
Service difficulty reports · 2,252
Newest first. General aviation reporting is voluntary.
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 = '727224' 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 aircraft_model_key = '727224' 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 MZZA79051Jack Cone · corrodedKUL - CORROSION ON FLANGES AND INSIDE BORES OF NOSE LANDING GEAR TOW LUG FORGING. REMOVED SLEEVES AND CORROSION IN BORES, FABRICATED AND INSTALLED SLEEVES, REMOVED FLANGE CORROSION AND FABRICATED AND INSTALLED SHIMES. REINSTALLED TOWING ASSY AND JACK CONE IASDR CALA9700352Hyd Hose · leakingTHE AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO PTY WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC FLEX HOSE IN TAIL SECTION OF AIRCRAFT LEAKING. THE HYDRAULIC FLEX LINE WAS REMOVED AND RSDR CALA9700421Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 1070 TO 1140, RBL 66. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-10-6.SDR CALA9700420Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 1050, RBL 26 TO 66. THE CORRODED AREA WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-40-5, 51-10-2, AND 51-30-2.SDR CALA9700419Floor Pan · corrodedINSPECTION FOUND LEFT AFT LAV FLOOR PAN CORRODED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-6.SDR MZZA97066Tab · delaminationKUL - L.P. 826718. RIGHT ELEVATOR TAB HAS SKIN SEPARATED AT ALL THREE BULLNOSE CUT OUTS. REPAIRED SEPARATION PER SRM 51-20-04. (X)SDR MZZA97050Tab · delaminatedKUL - LP NR 826716. LEFT ELEVATOR OUTBOARD TAB BULL NOSE CUT OUT SKIN IS SEPARATED. REPAIRED SEPARATION PER SRM 51-20-04. (X)SDR MZZA97049Tab · delaminatedKUL - LP NR 826735. RIGHT ELEVATOR TAB T/E SECTION IS DELAMINATED. ELEVATOR T AB REMOVED, REPAIRED AND REINSTALLED PER SRM 51-40-06 PLUS MM 27-30-11. WEIGHT AND BALANCE REQUIRES CUT OUT PER SRM 51-80-9. (X)SDR MZZA97067Stringer · corrodedKUL - L/P 826603. C2 CARGO DOOR THRESHOLD BOTTOM SECTION HAS CORROSION. CUT OUT DAMAGE IAW 51-40-2. FABRICATED PARTS IAW EC/RA NR 5310-0354. INSTALLED PARTS. (X)SDR MZZA97044Foreflap · delaminatedKUL - LP NR 826613. ULTRASONIC BOND INSPECTION CUT OUT AND FOUND DELAMINATION ON LEFT TRAILING EDGE FOREFLAP (OTBD) AT TWO AREAS APPROXIMATELY 23 INCHES AND 6 INCHES LONG. REFER TO NDT REPORT NR FAA 1024. ITEM REMOVED AND SENT TO WORK SHOP. REPAIRED IAW SRSDR MZZA97065Cowl · crackedKUL - LP NR 836562. NEED TO REPAIR NOSE COWL ABOUT 6 O'CLOCK POSITION. FOUND TEAR PORTION .50 INCH WIDE, 2 EACH ENGINE NR 1. NOSE COWL REPAIRED PER ECRA 7110-01204. FOR DIP SEE LOG PAGE NR 7927625. (X)SDR GAIA9710AWire · looseFLT 2829 - CLT-TOL - AFTER DEPARTURE FROM CLT, CARGO SMOKE DETECTOR WARNING LIGHT ILLUMINATED. FLIGHT CREW NOTIFIED ATC, AIRCRAFT DIVERTED AND MADE AN UNEVENTFUL LANDING. AFTER INVESTIGATION MX CREW FOUND LOOSE CRIMP ON GROUNDING WIRE ON NR 6 DETECTOR AND RESDR MZZA97057Bearing · seizedKUL - RIGHT MLG EMERGENCY EXTENSION UPLOCK CRANK LINK ROLLER BEARING FROZEN. REMOVED AND REPLACED UPLOCK CRANK LINK ROLLER BEARING IAW B727 MM 32-32-51. OPS CHECK GOOD. (M)SDR MZZA97048Idler Link · wornKUL - LP NR 867787. RIGHT ELEVATOR TAB HAS EXCESSIVE PLAY AS MEASURED AT TRAILING EDGE. REPLACED ELEVATOR TAB IDLER LINK AND BUSHINGS IAW MM 27-30-61. OPS CHECK GOOD. (X)SDR GAIA9710Smoke Light · illuminatedFLT 2829 - CLT-TOL - AFTER DEPARTURE FROM CLT CARGO SMOKE DETECTOR WARNING LIGHT ILLUMINATED, FLIGHT CREW NOTIFIED ATC. AIRCRAFT DIVERTED AND MADE AN UNEVENTFUL LANDING. (M)SDR CALA9700344Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 300, RBL 12 TO RBL 40. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.SDR CALA9700340Floor Support · brokenINSPECTION FOUND FLOOR SUPPORT BROKEN AT STA 758, BL ZERO. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9700339Floor Support · corrodedINSPECTION FOUND INBOARD END OF CABIN FLOOR SUPPORT CORRODED AT STA 342. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-1, 51-10-2, AND 51-40-4.SDR CALA9700338Bulkhead · corrodedINSPECTION FOUND BULKHEAD AND SKIN CORRODED IN FORWARD CARGO BILGE AREA AT STA 560, STRINGER 28R. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A SKIN REPAIR WAS INSTALLED IAW SRM 53-30-3.SDR CALA9700337Floor Panel · corrodedINSPECTION FOUND CABIN FLOOR PANEL CORRODED AT B.S. 1144, RBL 40. A REPAIR WAS PERFORMED IAW SRM 51-40-2 AND 51-10-2.SDR CALA9700427Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN UPPER RIB CAP OF RT WING LEADING EDGE FS 340. THE ANGLE WAS REMOVED, A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-2.SDR CALA9700424Skin · corrodedINSPECTION FOUND LOWER FUSELAGE SKIN CORRODED AT STA 580. THE CORRODED SECTION OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-30-3.SDR CALA9700411Splice · corrodedINSPECTION FOUND STRINGER 27 SPLICE CORRODED AT STA 660 IN FORWARD CARGO BILGE AREA. THE SPLICE WAS REMOVED AND THE CORROSION ON SKIN WAS REMOVED. A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-6, AND 51-10-1.SDR CALA9700410Stringer · corrodedINSPECTION FOUND STRINGER 27L IN FORWARD BILGE AREA CORRODED AT STA 560. THE STRINGER WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-2.SDR CALA9700309Battery Pack · dischargedINSPECTION FOUND AFT ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED.SDR GAIA9705Smoke Light · illuminatedCARGO SMOKE LIGHT ILLUMINATED DURING FLIGHT, VERIFIED ON SMOKE OR FIRE AS PER EMERGENCY CHECK LIST. OPS CHECK NORMAL ON GROUND. (M)SDR CALA9700426Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN LT WING ANGLE AT OUTBOARD SIDE OF LEADING EDGE NOSE RIB, SLAT STA 0. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-40-3.SDR CALA9700425Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 344, RBL 15. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR CALA9700233Power Supply · inoperativeINSPECTION FOUND RT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. BOTH RT OVERWING CHARGING PACKS WERE REPLACED.SDR MZZA97031Fuel Contl Unit · failedGUM - FLT 915 - DURING CLIMB-OUT, NR 2 ENGINE WAS SHOWING ERRATIC INDICATION WHILE PASSING THROUGH 1000 FEET, EPR PLUS/MINUS .05, N1 PLUS 10 PERCENT, EGT PLUS/MINUS 50 DEGREES CELSIUS, N2 PLUS/MINUS 10 PERCENT, FUEL FLOW PLUS/MINUS 500 LBS. CREW AIR RETURN TOSDR CALA9700198Accessory Unit · inoperativeTHE LANDING GEAR OVERRIDE TRIGGER HAD TO BE USED TO RETRACT GEAR AFTER TAKEOFF. TROUBLESHOOTING PER MM 32-31-11, FOUND NO FAULTS. THE LANDING GEAR ACCESSORY UNIT WAS REPLACED AS A PRECAUTIONARY MEASURE, OPERATIONAL CHECKS WERE GOOD.SDR GAIA9701Warning Light · illuminatedFLT NR 1829 - RDU-TOL - AFTER TAKEOFF FROM RDU, NLG RETRACTED BUT RED UNSAFE LIGHT REMAINED ON. RECYCLED GEAR 3 TIMES LIGHT EXTINGUISHED, BUT CAME BACK ON IN CLIMB. RETURNED TO RDU AND MADE NORMAL UNEVENTFUL LANDING. AIRCRAFT SPECIAL FERRIED GEAR DOWN TO CLSDR GAIA9708Rib · crackedFOUDN ON SV1 CARD 8265, RIGHT WING RIB WS 738.5 CRACKED. REMOVED AND REPLACED RIB RIGHT WS 738.5 PER SB 727 57-0127. (M)SDR GAIA9707Rib · crackedFOUND ON SV1 CARD 8266, LEFT WING RIB WS 738.5 CRACKED. REMOVED AND REPLACED RIB LEFT WS 738.5 PER SB 727 57-0127. (M)SDR GAIA9706Frame · crackedFOUND ON SV1, RIGHT SIDE STATION 930 STRINGER 14, HAS CRACK IN BELL FRAME. REMOVED DAMAGE AND REPAIRED PER SB 727 53-0162. (M)SDR MZZA96226Angle · corrodedTNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, BULGE WAS FOUND ON TAIL SKID COMPARTMENT CUTOUT AT REAR POSITION. THE CORRODED ANGLE WAS REMOVED REPAIRED PER B727 SRM 51-40-3 FIG 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 840803 9SEQ NR 01151). (M)SDR MZZA96225Web · corrodedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON TAIL SKIN COMPARTMENT RT SIDE OF WEB AT AFT LOWER POSITION. THE CORRODED WEB WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-2 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITESDR MZZA96216Sign Cover · brokenTNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, BROKEN 'EXIT' SIGN COVER WAS FOUND ON LEFT AFT EMERGENCY EXIT DOOR. THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-105 PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFACTORYSDR MZZA96215Sign Cover · brokenTNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, BROKEN 'EXIT' SIGN COVERS WERE FOUND ON PASSENGER CABIN COMPARTMENT AT THE FOLLOWING POSITIONS; SIDE OF R1 GALLEY DOOR, SIDE OF R2 GALLEY DOOR, SIDE OF RT FORWARD EMERGENCY EXIT DOOR. THE DAMAGED 'EXIT' SIGNSDR MZZA96214Skin · dentedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DENT WAS FOUND ON FUSELAGE SKIN AT BS 1140 BETWEEN STRINGER 20L AND STRINGER 21L AND THE DENT DEPTH BEYOND THE SPECIFIED LIMIT. THE DAMAGED SKIN WAS REPAIRED PER B727 SRM 53-30-3 FIGURE 1. REF, HANGAR SDR MZZA96224Skin · delaminatedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RT WING OUTBOARD T/E FORE FLAP L/E UPPER SKIN AT WBL 417. THE DAMAGED SKIN 2.2 INCH BY 3.2 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTISDR MZZA96223Skin · tornTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, RT WING OUTBOARD AILERON T/E HONEYCOMB LOWER SKIN WAS FOUND TO BE TORN AT AFT EDGE. THE DAMAGED SKIN .375 INCH BY 1 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTISDR MZZA96220Skin · delaminatedTNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, DELAMINATION WAS FOUND ON LT WING INBOARD T/E AFT FLAP T/E UPPER SKIN AT WBL 77. THE DAMAGED SKIN 2.2 INBY BY 7.8 INCH SIZE WAS TRIMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ISDR MZZA96219Skin · delaminatedTNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, DELAMINATION WAS FOUND ON LT WING INBOARD T/E AFT FLAP T/E UPPER SKIN AT WBL 100. THE DAMAGED SKIN 1.75 INCH BY 8.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE RESDR MZZA96213Web · oil canningTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON LOWER VENTRAL STAIRWALL TORQUE BOX AT THE FOLLOWING AREAS, RT SIDE BETWEEN BS 1283 AND BS 1303, LEFT SIDE BETWEEN BS 1243 AND BS 1283, LT SIDE AT BS 1225. THE DAMAGED WEB WERE RSDR MZZA96212Web · crackedTNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, .5 INCH LONG CRACK WAS FOUND ON LEFT SIDE LOWER VENTRAL STAIRWALL TORQUE BOX WEB AT BS 1220 LIGHTENING HOLE CUTOUT. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2 FIGURE 1. REF, HANGAR NON ROUSDR MZZA96211Web · crackedTNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, .5 INCH LONG CRACK WAS FOUND ON LT SIDE LOWER VENTRAL STAIRWALL TORQUE BOX WEB AT BS 1225 LIGHTENING HOLE CUTOUT. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2 FIGURE 1. REF, HANGAR NON ROUTISDR MZZA96210Web · crackedTNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, ONE INCH LONG CRACK WAS FOUND ON LT SIDE LOWER VENTRAL STAIRWALL TORQUE BOX WEB AT BS 1213 LIGHTENING HOLE CUTOUT. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2 FIGURE 1. REF, HANGAR NON ROUTISDR MZZA96209Angle · corrodedTNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, INTERGRANNULAR CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT STRINGER 27R END TIE ANGLE AT BS 740. THE DAMAGED TIE ANGLE WAS REMOVED AND REPLACED WITH NEW TIE ANGLE PER B727 SRM 51-30-2. REF, HANGAR NON SDR MZZA96208Stringer · corrodedTNN - DURING S-CHECK INSPECTION ON A/C AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT, STRINGER 27R BETWEEN BS 720F PLUS 15 AND BS 740. THE CORRODED STRINGER FROM BS 720F PLUS 12 TO BS 740 WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-
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