Boeing 727-277
Service difficulty reports · 627
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 = '727277' 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 = '727277' 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 99FDEA00357Beam · corrodedBULGE ON LT HORIZONTAL STAB LOWER T/E BEAM I/B END (C55-391-20-1). *S/D* REMOVED AND REPLACED LT HORIZONTAL STAB LWR T/E BEAM IAW FEDEX MM 55-30-021-4, 27-30-005-4, 27-30-01, 27-30-05, 27-30-001-4, 27-30-000-5, 27-30-001-5, FEDEX SRM 51-30-2, 51-30-5, 51-30-SDR CA991209031Wheel · damaged(CAN) RIGHT NOSE WHEEL INNER RIM DAMAGED AROUND ENTIRE CIRCUMFERENCE. WHEEL REPLACED.SDR CA990614066Fire Loop · chafed(CAN) NR 1 ENGINE GROUND FAULT DETECTOR LIGHT ON, NR 1 FIRE PROTECTION LIGHT ON IN-FLIGHT, EXTINGUISHED ON GROUND. FOUND FIRE LOOP CHAFING ON COWLING, REPAIRED.SDR CA990614062Actuator · slow(CAN) FLAPS SLOW TO RETRACT FROM 5 TO 2 DEGREES. FLAP UP CABLE TENSION LOW.SDR EISA99128Excitor · inoperativeNR 3 ENGINE WOULD NOT LIGHT OFF. REMOVED AND REPLACED NR 3 ENGINE IGNITION EXCITOR. (M)SDR CA990614065Audio Unit · failed(CAN) RADIO NAV FAILURES, IDENT STRENGTHS LOW FOR CAPT, FO AND SO. REPLACED AUDIO ACCESSORY UNIT.SDR CA990323012Switch · out of adjust(CAN) WHEN FLAPS SELECTED TO FIVE DEGREES FORWARD FLAP ANNUNCIATOR PANEL ILLUMINATED TO GREEN, NORMAL, THEN INDICATED AMBER AND FLICKERED - GREEN - AMBER WHILE NR 6 LE FLAP INDICATED NEITHER. AFTER SOME TIME ALL INDICATED RETURNED TO NORMAL. NR 6 LE FLAP POSSDR MZZA99052Skin · corrodedTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON RIGHT FUSELAGE SKIN SPLICE PLATE AT BS 848.95 ABOVE STRINGER 18A. THE CORRODED FUSELAGE SKIN SPLICE PLATE WAS REPAIRED PER EC/RA NR 5310-03822 DATED 02 MAR 1999. (M)SDR MZZA9953Pulley · stuckTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, STUCK BEARING WAS FOUND ON LEFT WING SPOILER CONTROL PULLEY BEARING AT INBOARD END OF NR 4 SPOILER. THE DAMAGED SPOILER CONTROL PULLEY P/N BACP30J4, WAS REMOVED AND REPLACED PER B727 MM 27-61-41. (M)SDR MZZA99051Web · canningTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON RIGHT SIDE AFT AIRSTAIR TORQUE BOX VERTICAL WEB BETWEEN BS 1293 AND BS 1313. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STIFFENER ANGLE PER B7SDR MZZA99050Web · canningTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON RIGHT SIDE AFT AIRSTAIR TORQUE BOX VERTICAL WEB BETWEEN BS 1243 AND BS 1253. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STIFFENER ANGLE PER B7SDR MZZA99049Web · canningTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON RIGHT SIDE AFT AIRSTAIR TORQUE BOX VERTICAL WEB BETWEEN BS 1223 AND BS 1233. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STIFFENER ANGLE PER B7SDR MZZA99048Web · canningTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON LEFT SIDE AFT AIRSTAIR TORQUE BOX VERTICAL WEB BETWEEN BS 1303 AND BS 1323. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STIFFENER ANGLE PER B72SDR MZZA99047Web · canningTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON LEFT SIDE AFT AIRSTAIR TORQUE BOX VERTICAL WEB BETWEEN BS 1253 AND BS 1293. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STIFFENER ANGLE PER B72SDR CA990308017Actuator · leaking(CAN) LEFT MAIN GEAR ACTUATOR LEAKING, REPLACED.SDR CA990203005Switch · stuck(CAN) NR 2 ENGINE START VALVE LIGHT ILLUMINATED IN-FLIGHT. START VALVE REPLACED, LIGHT STILL ON. PRESSURE SWITCH REPLACED, CHECKED SERVICEABLE.SDR AU990031Web · cracked(AUS) WING CENTER SECTION REAR SPAR WEB CRACKED IN THE AREA BETWEEN RBL 12 AND RBL 13. THE CRACK WAS LOCATED JUST BELOW THE TANGENT POINT OF THE MACHINED LAND RADIUS OF THE WEB. CRACK LENGTH 19.05 MM (0.750 INCH). FOUND DURING NDT INSPECTION IAW AD/B727/152SDR 98FDEA00771Actuator · malfunctionedWITH FLAPS RETRACT AS A/C ACCEL THRU 270 KIAS, AMBER LEAD EDGE LIGHT ILLUM ON 2ND OFFICER AUXILIARY PNL AND A/C ROLL CONTROL WAS AFFECTED. ANTI ICE WAS ON. BELOW 250 KIAS ALL IND WERE NORM, FLAP EXTENSION AND LAND, ALL APPROPRIATE CK LIST WERE COMPLETE. *S/SDR CA990111029Frame · cracked(CAN) FRAME DAMAGED AT STA 1166 LT SIDE OF A/C 4 INCHES ABOVE FLOOR LEVEL BY CARGO PALLET. BENT BACK AND FLANGE TORN AND 1.5 INCH CRACK IN FRAME. REPAIRED. PART TC: 37,619.SDR MZZA98264Generator · malfunctionedFLT 879 - MNL - IN FLT HAD THE BTB, GENERATOR FIELD RELAY, AND GENERATOR BREAKER LIGHT ILLUMINATED ON NR 2 ENGINE. CREW FOLLOWED PROCEDURE BUT DID NOT DISCONNECT GENERATOR DRIVE. THE NR 2 BUS WAS BROUGHT BACK ON LINE, RETAINED NR 2 CSD AS STANDBY WHILE MONITSDR EISA98316Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND FIVE AREAS OF DELAMINATION ON LEFT OUTBOARD AFT FLAP. REPAIRED AREAS OF DELAMINATION PER SRM 51-40-06, ALUMINUM HONEYCOMB REPAIR. (M)SDR EISA98315Skin · dentedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND DENT ON LOWER SURFACE ON LEFT OUTBOARD AFT FLAP. REPAIRED DENT PER SRM 51-40-6, ALUMINUM HONEYCOMB. (M)SDR EISA98314Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND TWO RIBS AND ONE BRACKET CRACKED IN STRUCTURE OF E/E DOOR. REMOVED DAMAGED RIBS AND BRACKET. FABRICATED AND INSTALLED NEW RIBS AND BRACKET PER SRM 52-40-1 AND 51-30-2. (M)SDR EISA98309Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, NR 8 SLAT WAS FOUND CRACKED AT MOST OUTBOARD RIB. FABRICATED DOUBLER REPAIR PER SRM 57-50-2 AND INSTALLED PER SRM 51-40-3. (M)SDR EISA98319Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD , FOUND TWO AREAS OF DELAMINATION ON RIGH OUTBOARD AFT FLAP TRAILING EDGE. REPAIRED AREAS OF DELAMINATION PER SRM 51-40-05, ALUMINUM HONEYCOMB REPAIR. (M)SDR EISA98318Skin · gougedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND GOUGES ON UPPER SURFACE OF RIGHT OUTBOARD AFT FLAP. REPAIRED THREE GOUGES PER SRM 51-40-6 ALUMINUM HONEYCOMB REPAIR. (M)SDR EISA98317Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND AREA OF DELAMINATION ON OUTBOARD END OF LEFT INBOARD AFT FLAP. REPAIRED AREAS OF DELAMINATION PER SRM 51-40-5, BONDED METAL REPAIR. (M)SDR EISA98313Angle · corrodedDURING ACCOMPLISHMENT OF CPCP WORK CARD C53-224-1 CORROSION WAS FOUND TO EXIST ON FWD LAV BULKHEAD INSTALLATION ANGLE, RBL 16 AND 8 INCHES AFT OF FLT DECK THRESHOLD. REMOVED CORROSION FROM FWD LAV BULKHEAD. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-2.SDR EISA98312Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, NR 2 SLAT WAS DISCOVERED CRACKED AT THIRD RIB FROM INBOARD END. FABRICATED DOUBLER REPAIR PER SRM 57-50-2 AND INSTALLED PER SRM 51-40-2. (M)SDR EISA98311Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, NR 3 SLAT WAS FOUND CRACKED AT 2ND AND 7TH RIBS FROM OUTBOARD END. FABRICATED DOUBLER REPAIRS PER SRM 57-50-2 AND INSTALLED PER SRM 51-40-2. (M)SDR EISA98310Rib · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, NR 5 SLAT WAS FOUND CRACKED AT NR 5 AND NR 9 RIBS FROM INBOARD END. FABRICATED DOUBLER REPAIRS PER SRM 51-50-2 AND INSTALLED PER SRM 57-20-3. (M)SDR EISA98307Skin · crackedDURNG ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, X-RAY INSPECTION OF LEFT ELEVATOR SHOWS CRACK INDICATION OF .25 INCH AS SEEN IN SHOT NR L06, STATION 17.20-53.91). REMOVED LEFT ELEVATOR TAB TO FOM REPAIRED CRACK IN ELEVATOR PER SRM 51-40-3. ACCOMPLISHED BASDR EISA98306Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP CARD NR C53-224-01 REVEALED CORROSION ON UPPER CHORD OF FS 1070 FLOORBEAM RBL 55. REMOVED DAMAGED SECTION OF UPPER CHORD. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M)SDR EISA98302Bulkhead · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND FS 178 BULKHEAD CRACKED, JUST BELOW RADAR ANTENNA. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER B727 SB 53-0213. (M)SDR EISA98301Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD C53-224-01, NINE SMALL AREAS OF DELAMINATION ON RIGHT INBOARD AFT FLAP. REPAIRED ALL AREAS PER SRM 51-40-6. ALUMINUM HONEYCOMB REPAIRS. (M)SDR EISA98300Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP WORK CARD C53-224-01 REVEALED TWO MAIN AREAS OF CORROSION ON UPPER CHORD OF FS 1110 FLOORBEAM. REMOVED DAMAGED AREAS. FABRICATED AND INSTALLED REPAIRS PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M)SDR EISA98299Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP WORK CARD C53-224-01 REVEALED CORROSION ON IN TWO AREAS OF UPPER CHORD OF FLOORBEAM FS 1030. REMOVED DAMAGED AREAS FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M)SDR EISA98297Skin · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND AREA WITH GOUGED AND CRACKED SKIN ON UPPER SURFACE OF RIGHT INBOARD AFT FLAP. REMOVED DAMAGED SKIN. FABRICATED AND INSTALLED NEW SKIN SECTION PER SRM 57-50-4. (M)SDR EISA98293Floorbeam · corrodedDURING C-CHECK ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED FOUR AREAS OF CORROSION ON T-CAP OF FLOORBEAM AT FS 328. REMOVED DAMAGED AREAS AND INSTALLED REPAIRS PER SRM 53-10-8 AND 51-30-2. (M)SDR EISA98292Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED CORROSION ON FLOORBEAM AT FS 400 LBL 45. TRIMMED DAMAGED UPPER CHORD. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 FIGURE 3 AND 51-30-02. (M)SDR EISA98291Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED CORROSION ON UPPER CHORD OF FLOORBEAM AT FS 440 LBL 25. TRIMMED DAMAGED AREA OF UPPER CHORD. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 FIGURE 3 AND 51-30-1. (M)SDR EISA98290Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED THREE AREAS OF CORROSION ON FLOORBEAM AT FS 400. TRIMMED AREAS OF DAMAGED CHORD. FABRICATED AND INSTALLED REPAIRS PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M)SDR EISA98289Floorbeam · corrodedDURING ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED CORROSION ON FLOORBEAM UPPER CHORD AT FS 680. REMOVED DAMAGED AREA OF UPPER CHORD FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M)SDR EISA98288Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND THREE AREAS OF DELAMINATION ON RIGHT INBOARD MID FLAP TRAILING EDGE. REPAIRED AREAS PER SRM 51-40-6 ALUMINUM HONEYCOMB REPAIR. (M)SDR EISA98287Skin · puncturedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND SKIN PUNCTURE ON RIGHT INBOARD MID FLAP TRAILING EDGE LOWER SIDE. REPAIRED SKIN PUNCTURE PER SRM 51-40-6, 51-40-8, AND 51-40-9. (M)SDR EISA98286Frame · crackedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND CRACK IN FRAME AT FS 580 AND STRINGER 7R. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-4. (M)SDR EISA98285Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND TWO AREAS OF DELAMINATION ON LEFT INBOARD MID FLAP. REPAIRED AREAS OF DELAMINATION PER SRM 51-40-6 AND 51-40-8. (M)SDR 98FDEA00724Drive Unit · failedTOTAL LOSS OF A SYS QUANT ON SHORT FINAL. REPLACED CASE DRAIN FILTERS PER MM 29-11-041, I/B FLAP DRIVE UNIT HYD MTR PER MM 27-51-062-4, A SYS HYD PRESS FILTER PER MM 29-11-062-3. ENGINE DRIVEN HYD PUMPS OPER NORM.SDR 98ZZZM931Skin · corrodedTNN - DURNG 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON FUSELAGE SKIN INNER SURFACE AT STRINGER 28L BETWEEN BS 720 AND BS 725. THE CORRODED SKIN 3 INCHES BY 4 INCHES IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-30-3 FIGURE 3.SDR 98FDEA00645Power Unit · leaks98-245 AT FLT LVL 200, ON CLIMB-OUT 'A' SYS QUAN WAS 0.6 GAL GOOD PRESS. ON DESCENT QUANTITY DECREASE TOWARD 0 PRESS ERRATIC. MAN EXTEND GEAR AND FLAP A FLUID SHUTOFF SWITCH CLOSE AT 0835Z. FOUND LEAK LWR RUDDER PWR UNIT AT BASE RUDDER LOAD LIMIT VALVE MT
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