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 CALA9900157Midflap · bentINSPECTION FOUND LT WING IB MIDFLAP BENT AT AFT IB AREA. THE BENT AREA WAS CUT OUT AND A HOT BOND REPAIR WAS INSTALLED IAW SRM 57-50-2, PAGE 5.SDR CALA9900137Wire · shortedINSPECTION FOUND EMERGENCY PATH SEAT MOUNTED LIGHTS INOPERATIVE FROM ROW 5 TO 15. CAPPED SHORTED WIRES AND OPERATION CHECKED NORMAL IAW MM 33-51-00, PAGE 112.SDR GAIA9912Switch · dirtyAFTER DEPARTING TOL, CARGO DOOR ANNUNCIATOR FLICKERED. AIRCRAFT RETURNED TO TOL AND MADE AN UNEVENTFUL LANDING. CLEANED DIRT AND DEBRIS FROM (FORWARD BELLY) CARGO DOOR SEAL AND SWITCH. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICESDR GAIA9907Line · looseDURING SCHEDULED FLIGHT BETWEEN ELP AND HUF, THE NR 2 ENGINE OIL QUANTITY WENT OT ZERO IN FLIGHT. LOW OIL PRESSURE LIGHT ILLUMINATED, AND OIL TEMPERATURE BEGAN TO CLIMB. THE ENGINE WAS SHUTDOWN IN FLIGHT. EMERGENCY LANDING WAS DECLARED INTO MCI, AND LANDED SDR CALA9900016Clip · crackedKEEL BEAM RIGHT WHEEL WELL ATTACH CLIP CRACKED. REPLACED VERTICAL STIFFENER RT INBOARD CORNER AS PER ORIGINAL PER SRM 51-30-2.SDR MZZA98263Valve · malfunctionedFLT 956 - TKK - AFTER TAKEOFF FROM TKK WHEN MLG WAS RAISED, ALL LIGHTS WENT OUT INDICATING THE GEAR UP AND LOCKED. SHORTLY AFTER THE RIGHT MLG RED LIGHT CAME ON INDICATING NOT UP AND LOCKED. UPON VISUAL INSPECTION, RIGHT GEAR WAS NOTED TO BE ALL THE WAY DOWNSDR MZZA98289Flap Track · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON NR 4 FLAP TRACK MOUNTING PAD 'A' AROUND THE BOLT HOLE. THE DAMAGED NR 4 FLAP TRACK P/N 65-19270-10 WAS REMOVED AND REPLACED PER B727 MM 27-51-31. (M)SDR CALA9802116Batteries · dischargedTHE R-1 DOOR INTERIOR OVERHEAD LIGHT WOULD NOT TEST. THE BATTERIES WERE REPLACED IAW MM 33-50-101 AND OPERATION CHECKED GOOD.SDR MZZA98291Angle · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1.125 INCH LONG CRACK WAS FOUND ON RT WING T/E INBOARD MID FLAP LOWER CLOSURE ANGLE AT WBL 124. THE CLOSURE ANGLE CRACK AREA (1.125 INCH LONG) WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-4. (M)SDR MZZA98287Bracket · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 4 INCHES LONG CRACK WAS FOUND ON FUSELAGE S-16L REINFORCEMENT BRACKET AT BS 297. THE DAMAGED REINFORCEMENT BRACKET WAS REMOVED AND REPLACED WITH NEW BRACKET. (M)SDR MZZA98286Skin · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON RIGHT FUSELAGE SKIN AT WING SCANNING LIGHT CUT OUT. THE CORRODED SKIN WAS CLEANUP AND REPAIRED PER B727 SRM 53-30-3 FIGURE 22. (M)SDR MZZA98290Skin · delaminatedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD MID FLAP UPPER SKIN AT WBL 226. THE DAMAGED SKIN 7 INCH BY 2 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M)SDR MZZA98268Stringer · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FORWARD CARGO COMPACTMENT STRINGER S-27R AT BS 740. THE CORRODED STRINGER 5 INCH LONG WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-3 FIGURE 1. (M)SDR MZZA98285Support · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON AFT GALLEY FLOOR SUPPORT (HAT CHANNEL) AT BS 1033, RBL 55. THE CORRODED FLOOR SUPPORT (HAT CHANNEL) WAS REMOVED AND REPLACED WITH NEW FLOOR SUPPORT HAT CHANNEL MADE FROM BAC 15SDR MZZA98284Seat Track · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK AT RBL 24.75 BETWEEN BS 1030 AND BS 1070. THE CORRODED SEAT TRACK FROM BS 1030 TO BS 1090 WAS TRIMMED OUT AND INSTALLED REPLACEMENT TRACK PER B72SDR MZZA98283Seat Track · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TG CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK AT BS 1075, RBL 55. THE CORRODED SEAT TRACK FLANGE WAS CLEANED UP AND REPAIRED PER B727 SRM 53-10-5 FIGURE 9. (M)SDR MZZA98282Support · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR PANEL SUPPORT 'T' ANGLE AT RBL 12 BETWEEN BS 405 AND BS 415. THE CORRODED FLOOR SUPPORT 'T' ANGLE WAS REMOVED AND REPLACED WITH NEW SUPPORT 'T' ANGLE MADESDR MZZA98281Seat Track · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION AS FOUND ON PASSENGER CABIN SEAT TRAC AT RBL 22.09 BETWEEN BS 396 AND BS 412. THE CORRODED SEAT TRACK FROM BS 380 TO BS 420 WAS TRIMMED OUT AND INSTALLED REPLACEMENT TRACK PER B727 SRM 53-1SDR MZZA98280Support · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR PANEL SUPPORT 'T' ANGLE AT BS 414 BETWEEN RBL 12 AND RBL 21. THE CORRODED FLOOR PANEL SUPPORT 'T' ANGLE WAS REMOVED AND REPLACED WITH NEW SUPPORT 'T' ANGLSDR MZZA98279Support · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR PANEL SUPPORT 'T' ANGLE AT BS 414 RBL 40. THE CORRODED FLOOR PANEL SUPPORT 'T' ANGLE WAS REMOVED AND REPLACED WITH NEW SUPPORT 'T' ANGLE MADE FROM BAC1506SDR MZZA98278Support · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER FLOOR PANEL SUPPORT 'T' ANGLE AT BS 417, RBL 47. THE CORRODED FLOOR PANEL SUPPORT 'T' ANGLE WAS REMOVED AND REPLACED WITH NEW SUPPORT 'T' ANGLE MADE FROM BAC1506-43. SDR MZZA98277Seat Track · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK AT RBL 42.8 BETWEEN BS 380 AND BS 420. THE CORRODED SEAT TRACK FROM BS 380 TO BS 420 WAS TRIMMED OUT AND INSTALLED REPLACEMENT TRACK PER B727 SRM 53-SDR MZZA98276Bulkhead Web · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON BS 1183 BULKHEAD FLOOR SHEAR WEB AT RBL 15. THE CORRODED WEB WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-2. (M)SDR MZZA98275Support · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON RIGHT AFT LAVATORY PARTITION LOWER SUPPORT HAT CHANNEL AT BS 1138 BETWEEN RBL 27 AND RBL 52. THE CORRODED PARTITION LOWER SUPPORT HAT CHANNEL WAS REMOVED AND REPLACED WITH NEW SDR MZZA98274Seat Track · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON PASSENGER SEAT TRACK AT RBL 45.5 BETWEEN BS 1117 AND BS 1138. THE CORRODED SEAT TRACK FROM BS 1110, AND BS 1138 WAS TRIMMED OUT AND INSTALLED REPLACEMENT TRACK PER B727 SRM 53-10-SDR MZZA98272Fitting · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASI, LG CORROSION WAS FOUND ON BS 1183 BULKHEAD S-17R FORWARD END FITTING. THE CORRODED FORWARD END FITTING, P/N 65-24276-50 WAS REMOVED AND REPLACED WITH NEW END FITTING. (M)SDR MZZA98271Support · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR PANEL SUPPORT 'T' ANGLE AT BS 1138, LBL 14. THE CORRODED FLOOR PANEL SUPPORT 'T' ANGLE FLANGE 2 INCH LONG WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-SDR MZZA98270Intercostal · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON BS 1176.9 REINFORCEMENT CHORD BETWEEN LBL40 AND LBL48. THE CORRODED REINFORCEMENT CHORD WAS CLEAN UP AND REPAIRED PER EC/RA 5310-01555 DATED 9-5-90. (M)SDR MZZA98269Support · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON LEFT AFT LAVATORY PARTITION LOWER SUPPORT HAT CHANNEL AT BS 1138, LBL 24. THE CORRODED LAVATORY PARTITION LOWER SUPPORT HAT CHANNEL WAS REMOVED AND REPLACED WITH NEW HAT CHANNESDR CALA9802082Bearing · wornTHE NOSE GEAR DOORS OPEN LIGHT ON BOTH THE FORWARD AND SECOND OFFICER'S PANELS WERE ILLUMINATED AFTER GEAR RETRACTION DEPARTING BWI. THE WARNING LIGHTS WERE ACCOMPANIED BY RUMBLING AIR NOISE. THE GEAR WAS CYCLED WITH NO CHANGE. THE AIRCRAFT WAS DIVERTED TO SDR MZZA98267Skin · corrodedTNN - DUIRNG D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON WING CENTER SECTION LOWER SKIN LOWER SURFACE BETWEEN S-4C AND S-5C AND BETWEEN RBBL 27 AND RBBL 30. THE CORRODED AREA WAS CLEAN UP AND REPAIRED PER B727 SRM 57-30-3 FIGURE 10. SDR MZZA98266Bulkhead Plate · corrodedTNN - DUIRNG D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TG CORROSION WAS FOUND ON BS 740 BULKHEAD LOWER WIRING ACCESS HOLE REINFORCEMENT PLATE. THE CORRODED WIRING ACCESS HOLE REINFORCEMENT PLATE P/N 69-64841-1 WAS REMOVED AND REPLACED WITH NEW REINFORCEMENTSDR MZZA98294Spar · corrodedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON RIGHT WING T/E INBOARD MID FLAP REAR SPAR LOWER CHORD HORIZONTAL FORWARD FLANGE AT WBL 2105. THE CORRODED REAR SPAR LOWER CHORD HORIZONTAL FORWARD FLANGE WAS CLEAN UP AND REPAISDR MZZA98292Angle · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 2 INCH LONG CRACK WAS FOUND ON RT WING T/E INBOARD MID FLAP LOWER CLOSURE ANGLE AT WBL 204. THE CLOSURE ANGLE CRACK AREA (2 INCH LONG) WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-4. (M)SDR MZZA98265Stringer · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1.1 INCH LONG CRACK WAS FOND ON LEFT FUSELAGE STRINGER S-18A VERTICAL FLANGE AT BS 948. THE DAMAGED STRINGER S-18A AFT BS 920 WAS TRIMMED OUT AND SPLICE REPAIRED WITH NEW SECTION OF S-18A PER EC/PA 5310SDR MZZA98293Bearing · frozenTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, RT MLG DOOR MANUAL RELEASE CRANK ROLLER WAS FOUND FROZEN. THE DAMAGED BEARING P/N BACB10B131 WAS REMOVED AND REPLACED PER B727 MM 20-10-7 AND OPERATION CHECK FOUND SATISFACTORY. (M)SDR GAIA98123Frame · corrodedLEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. CABIN FRAME HAS CORROSION AT BS 1160, STRINGER 25L. REMOVED CORROSION AND DAMAGE. FABRICATED REPAIR ANGLE IAW B727 SRM 53-10-4, FIG 12. INSTALLED REPAIR IAW B727 SRM 53-10-04 FIG 12. (M)SDR GAIA98122Angle · corrodedLEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. OUTER SIDE OF FLOORBEAM WEB, AFT ATTACH ANGLE IS CORRODED, BS 870, RBL 45. REMOVED CORROSION AND REPAIRED TEE ANGLE AT BS 870, RBL 45. REMOVED CORROSION AND REPAIRED TEE ANGLE AT BS 870, ISDR GAIA98121Floorbeam · corrodedLEVEL 2 CORROSIO NFOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FLOORBEAM HAS SURFACE CORROSION, TOP FLANGE, AT BS 1070 RBL 48 AND 53. REMOVED CORROSION FROM UPPER SURFACE OF FLOORBEAM IAW B727 SRM 53-10-01. FABRICATED REPAIR PARTS IAW BAC 7SDR GAIA98120Floorbeam · corrodedLEVEL 2 CORROSION FOUND DURNIG A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FLOORBEAM TOP SURFACE HAS CORROSION AT BS 1070, RBL 53. REMOVED CORROSION FROM UPPER SURFACE OF FLOORBEAM IAW B727 SRM 53-10-01. INSTALLED REPAIR PARTS IAW B727 SRM 51-30-02 ANDSDR GAIA98119Angle · corrodedLEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FLOOR CHORD ANGLE HAS SURFACE CORROSION AT BS 1177, RBL 54 TO RBL 66. REMOVED CORRODED ANGLE IAW B727 SRM 51-30-2. REPLACED ANGLE IAW B727 SRM 51-10-1 AND 51-30-2. (M)SDR GAIA98118Frame · corrodedLEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FUSELAGE CIRCUMFERENTIAL FRAME HAS SURFACE CORROSION AT BS 1148, STRINGER 16R TO 12R. CLEANED CORROSION AND FOUND, OUT OF LIMITS. FABRICATED REPAIR PART IAW B727 51-40-03, FIG 1SDR GAIA98117Floorbeam · corrodedLEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FLOOR CHORD AND UPPER ANGLE HAS SURFACE CORROSION AT BS 1176.9, LBL 61 - LBL 66. REMOVED CORRSOSION AND REPAIRED DAMAGED CHORD IAW AMERICAN INTERNATIONAL AIRWAYS EDR. ENGINEERINSDR GAIA98116Floorbeam · corrodedLEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN, MAIN CABIN FLOORBEAM HAS SURFACE CORROSION ON TOP FLANGE, BS 1110, RBL 43. REMOVED CORROSION IAW B727 SRM. FABRICATED REPAIR PARTS IAW B727 SRM. FABRICATED REPAIRPARTS IAW B727 SRM 53-10-8SDR MZZA98288Angle · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACK WAS FOUND ON NR 3 SPOILER ACTUATOR SUPPORT ANGLE. THE CRACK SUPPORT ANGLE P/N 65-24608-17 WAS REMOVED AND REPLACED NEW ONE. (M)SDR GAIA98110Connector · looseDURING APPROACH FROM KYIP TO KHUF, WHEN GEAR WAS SELECTED DOWN, THE LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED ON FIRST AND SECOND ATTEMPTS. IT INDICATED DOWN AND LOCKED ON THE THIRD ATTEMPT. AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND A LOOSE COSDR GAIA9898Fitting · damagedDURING ROUTINE HEAVY CHECK, INSPECTION FOUND TWO PILOT HOLES ELONGATED, LOCATED AT RT MLG WHEEL WELL AREA. THE HOLES WHERE REPAIRED USING FLIGHT VEHICLES INC REPAIR SKETCH NUMBER 57-98515-2. THE AIRCRAFT WAS THEN RETURN TO SERVICE (M)SDR GAIA9897Floorbeam · crackedDURING ROUTINE HEAVY CHECK, INSPECTION FOUND A CRACK IN THE FLOORBEAM LOCATED AT BS 740 RBL 35 UPPER CHORD. THE CRACK WAS REPAIRED USING FLIGHT VEHICLES INC REPAIR SKETCH NUMBER 53-98522-2. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)SDR GAIA9896Floorbeam · crackedDURING ROUTINE HEAVY CHECK, INSPECTION FOUND A CRACK IN THE FLOORBEAM LOCATED AT BS 870 LBL 24.75. DURING REPAIR USING SRM REFERENCES MAINTENANCE MISSED DRILLED A HOLE IN WHICH REPAIR WAS OUTSIDE THE SCOPE OF THE SRM REPAIR. THE MISSED DRILLED HOLE WAS REPAISDR GAIA9895Stringer · damagedDURING HEAVY C-CHECK INSPECTION, REVEALED TWO HOLES ELONGATED AT FS 360 STRINGER 19 LEFT. THE HOLES WHERE REAMED TO CORRECT THE OBLONG CONDITION. THE DAMAGE WAS REPAIRED IAW BOEING TELEX AOC-OKO-98-0087RR. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)
Back to Boeing 727-224