Boeing 727-277

Service difficulty reports · 627

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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 = '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.

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-Aug 30, 1999 · N245FE · Boeing 727277 · Horizontal Stabilizer StructureSDR CA991209031Wheel · damaged(CAN) RIGHT NOSE WHEEL INNER RIM DAMAGED AROUND ENTIRE CIRCUMFERENCE. WHEEL REPLACED.Jul 24, 1999 · Boeing 727277 · Wheel/Ski/FloatSDR 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.May 23, 1999 · Boeing 727277 · Fire DetectionSDR CA990614062Actuator · slow(CAN) FLAPS SLOW TO RETRACT FROM 5 TO 2 DEGREES. FLAP UP CABLE TENSION LOW.May 21, 1999 · Boeing 727277 · Trailing Edge Flap ActuatorSDR EISA99128Excitor · inoperativeNR 3 ENGINE WOULD NOT LIGHT OFF. REMOVED AND REPLACED NR 3 ENGINE IGNITION EXCITOR. (M)May 20, 1999 · N275WC · Boeing 727277 · ExciterSDR CA990614065Audio Unit · failed(CAN) RADIO NAV FAILURES, IDENT STRENGTHS LOW FOR CAPT, FO AND SO. REPLACED AUDIO ACCESSORY UNIT.Mar 20, 1999 · Boeing 727277 · Audio Integrating SystemSDR 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 POSMar 12, 1999 · Boeing 727277 · Leading Edge Slat Control SystemSDR 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)Feb 25, 1999 · N627DH · Boeing 727277 · Fuselage Main, Plate/SkinSDR 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)Feb 24, 1999 · N627DH · Boeing 727277 · Drag Control SystemSDR 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 B7Feb 23, 1999 · N627DH · Boeing 727277 · Fuselage Miscellaneous StructureSDR 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 B7Feb 23, 1999 · N627DH · Boeing 727277 · Fuselage Miscellaneous StructureSDR 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 B7Feb 23, 1999 · N627DH · Boeing 727277 · Fuselage Miscellaneous StructureSDR 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 B72Feb 23, 1999 · N627DH · Boeing 727277 · Fuselage Miscellaneous StructureSDR 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 B72Feb 23, 1999 · N627DH · Boeing 727277 · Fuselage Miscellaneous StructureSDR CA990308017Actuator · leaking(CAN) LEFT MAIN GEAR ACTUATOR LEAKING, REPLACED.Feb 15, 1999 · Boeing 727277 · Landing Gear ActuatorSDR CA990203005Switch · stuck(CAN) NR 2 ENGINE START VALVE LIGHT ILLUMINATED IN-FLIGHT. START VALVE REPLACED, LIGHT STILL ON. PRESSURE SWITCH REPLACED, CHECKED SERVICEABLE.Jan 23, 1999 · Boeing 727277 · Engine Start Valves/ControlsSDR 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/B727/152Jan 8, 1999 · Boeing 727277 · Wing, Center BoxSDR 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/Dec 31, 1998 · N246FE · Boeing 727277 · Leading Edge Slat ActuatorSDR 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.Dec 19, 1998 · Boeing 727277 · Fuselage Main, FrameSDR 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 MONITDec 17, 1998 · N626DH · Boeing 727277 · AC Generator-AlternatorSDR 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)Dec 9, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR 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)Dec 9, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR 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)Dec 9, 1998 · N275WC · Boeing 727277 · Electrical/Electronic Compartment DoorsSDR 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)Dec 9, 1998 · N275WC · Boeing 727277 · Leading Edge DevicesSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR 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.Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Miscellaneous StructureSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Leading Edge DevicesSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Leading Edge DevicesSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Leading Edge DevicesSDR 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 BADec 8, 1998 · N275WC · Boeing 727277 · Elevator, Plate/SkinSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, BulkheadSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, Floor BeamSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Fuselage Main, FrameSDR 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)Dec 8, 1998 · N275WC · Boeing 727277 · Trailing Edge FlapsSDR 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.Dec 4, 1998 · N244FE · Boeing 727277 · Trailing Edge Flap Control SystemSDR 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.Oct 11, 1998 · N626DH · Boeing 727277 · Fuselage Main, Plate/SkinSDR 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 Oct 9, 1998 · N243FE · Boeing 727277 · Rudder Control System
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