Boeing 727-225

Service difficulty reports · 4,226

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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 = '727225'
  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 DHL2003743005Sensor · shortedIN CRUISE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE. LIGHT WENT OUT AFTER RETARDING NR 1 THRUST LEVER. RAN NR 1 ENGINE AND INSPECTED PNEUMATIC DUCTS IN AFT AIRSTAIR WITH PACKS RUNNING, NO LEAKS NOTED. FOUND SENSOR TOUCHING STRMar 19, 2003 · N743DH · Boeing 727225 · Overheat DetectionSDR DHL2003743004Lamp1) APU FIRE WARNING LIGHT IN LEFT-HAND WHEEL WELL WILL NOT ILLUMINATE DURING TEST. 2) RELAMPED APU FIRE WARNING LIGHT LEFT-HAND WHEEL WELL IAW M/M 33-10-51. SYSTEM OPS CHECKED GOOD IAW M/M 26-15-00.Mar 15, 2003 · N743DH · Boeing 727225 · Fire DetectionSDR DHL2003748004Light1) FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE.2) REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECKED NORMAL IAW M/M 33-50-01.Mar 8, 2003 · N748DH · Boeing 727225 · Emergency LightingSDR DHL2003755004Warning Light · false activationRED DOOR LIGHT ON FRONT PANEL, AND NOSE GEAR DOOR LIGHT ON S/O'S ANNUNCIATOR PANEL ILLUMINATED. VERIFIED NOSE DOORS CLOSED AND FAIRED. TRANSFERRED TO MEL 12203 PER MEL 32-1. PLACARDS INSTALLED.Mar 6, 2003 · N755DH · Boeing 727225 · Landing Gear Position and WarningSDR DHL2003755005Valve1) DURING GEAR RETRACTION NOSE GEAR VIBRATED AND SOUNDED LIKE THE NOSE GEAR DOOR WAS NOT CLOSED. NOSE GEAR LIGHT ON S/O'S PANEL AND DOOR LIGHT ON FRONT PANEL WAS ILLUMINATED UNTIL FL 24.0 THEN LIGHTS WENT OUT.2) UPON INSPECTION FOUND NOSE GEAR STRUT FLAT. FOMar 5, 2003 · N755DH · Boeing 727225 · Nose/Tail Landing GearSDR C7WA200200040Pan · crackedL1 DOOR VERY HARD TO CLOSE. DURING INSPECTION OF DOOR FOUND CRACKS IN DOOR PAN AROND UPPER AND LOWER TORQUE TUBES. REMOVED AND REPLACED FORWARD ENTRANCE DOOR. (M)Mar 4, 2003 · N8887Z · Boeing 727225 · Passenger/Crew DoorsSDR 03FDEA00201Frame · dentedDENTED FRAME BS 950E, LBL 31, WL 150. DENT IN FRAME AT B.S. 950E, LBL 31, WL 150 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED FABRICATED U CHANNEL IAW EA 7-5310-69418 AND ER 03-1450 .Mar 4, 2003 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR DHL2003748003Light · inoperativeFORWARD ENTRY EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE DURING STANDBY POWER CHECK. CLEANED AND RE-SECURED EMERGENCY EXIT LIGHT ASSEMBLY IAW B727 M/M 33-50-71. OPS CHECKED SERVICEABLE IAW B727 M/M 33-50-91.Mar 4, 2003 · N748DH · Boeing 727225 · Emergency LightingSDR 03FDEA00192Floorbeam · corrodedCORROSION (C53-224-011) ON TOP OF UPPER LOBE FLOORBEAM AT BS 620, RBL 3, TO RBL 23. CORROSION AT BS 620, WL 208, RBL 3 TO RBL 23 DETERMINED TO BE OUT OF LIMITS IAW B727, SRM 53-10-1 FIG 4. REMOVED UPPER CHORD OF BEAM FROM LBL 32 TO RBL 36.5. FABRICATED REPAMar 3, 2003 · N464FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 03FDEA00198Floor Support · corrodedCORROSION ON FLOOR SUPPORT UNDER NUT PLATE BS 1165 - 1166, RBL 16, WL 155. REMOVED FLOOR SUPPORT BS 1166-1120, RBL 16, WL 155. FABRICATED REPAIR PARTS IAW SRM 53-10-5 AND SR 27-53-039. ALODINED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED IAW SRM 51-30-2.Mar 3, 2003 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 03FDEA00196Stringer Clip · corrodedCORROSION ON STRINGER CLIP, BS 720C STR 26R. REMOVED STRINGER CLIP BS 720C STR 26R, REMOVED CORROSION ON CLIP IN A 1 INCH X 1 INCH AREA. BLENDED 0.020 INCH FROM 0.040 INCH OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED REPLACEMENT STR CLIP FROM 7075 T6 X 0Mar 3, 2003 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 03FDEA00195Shear Tie · corrodedCORROSION ON SHEAR TIE, BS 720 NEXT TO STR 26R. REMOVED CORROSION ON SHEAR TIE, BS 720 BETWEEN STR 26-27 RIGHT, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED, ALODINED AND PRIMED REPAIR PARTS. INSTALLED REPAIR, ALL WORK ACCOMPLISHED IAW SRM 51-10-3,Mar 3, 2003 · N464FE · Boeing 727225 · Fuselage Main, StructureSDR 03FDEA00193Floorbeam · corrodedCORROSION ON 950D FLOORBEAM UPPER FLANGE UPPER AND LOWER SURFACES RBL 25, LBL 25, WL 208. REMOVED CORROSION FROM FLOORBEAM BS 950D, RBL 10.5, FOUND OUT OF LIMITS IAW SRM 53-10-1. CUT OUT DAMAGED SECTION OF UPPER CHORD BS 950D LBL 37-RBL 37. FABRICATED REPAIMar 3, 2003 · N464FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 03FDEA00188Frame · corrodedCORROSION ON REINFORCEMENT FRAME, BS 1176.9, RBL 45 TO RBL 59, WL 208. REMOVED CORROSION ON REINFORCEMENT FRAME, BS 1176.9 RBL 45-59 WL 208. DETERMINED TO BE OUT OF LIMITS IAW 53-10-1. REMOVED AND REPLACED CHORD IAW SRM 51-30-2.Feb 28, 2003 · N464FE · Boeing 727225 · Fuselage Main, StructureSDR 03FDEA00189Skin · dentedLT AFT FUSELAGE SEC 48, SKIN HAS A CREASED DENT AT BS. 1349, WL 196 APPROX 8 O'CLOCK POS. LEFT AFT FUSE, SEC 48, SKIN CREASE DENT AT B.S 1349, WL 196, REMOVED DAMAGE, FOUND TO GO THROUGH BONDED SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER IAW E.A 7-5450Feb 28, 2003 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 03FDEA00183Floorbeam · corrodedCORROSION ON FLOORBEAM REPAIR STRAP BS 1130, RBL 30-RBL 36, WL 200. REMOVED CORROSION ON FLOORBEAM REPAIR STRAP BS 1130, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED STRAP, FABRICATED AND INSTALLED NEW STRAP IAW SRM 51-10-2, 51-10-3, 51-30-2, AND 51-30-5.Feb 26, 2003 · N464FE · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL2003748002Tail Cone1) #1 ENGINE TAIL CONE HAS APPROXIMATELY 1" X 1" HOLE.2) TRANSFERRED TO LOG PAGE 338263, ITEM 15M.3) REF. N/R 21A: #1 ENGINE TAIL CONE HAS APPROXIMATELY 1" X 1" HOLE.4) REMOVED #1 ENGINE TAIL CONE. ITEM PLACED ON DEFERRAL PER DHL MEL/CDL 78-30-4, CONTROL #Feb 26, 2003 · N748DH · Boeing 727225 · Engine Exhaust SystemSDR 03FDEA00184Door · malfunctionedDURING GEAR RETRACTION, THE RT GEAR DOOR LIGHT AND PILOTS GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED. RECYCLED GEAR IAW RED TABS AND LIGHTS EXTINGUISHED. OPERATED RIGHT DOOR FOR MAIN GEAR WITH GROUND RELEASE HANDLE OPERATES NORMAL IAW M/M 32-62-011-5.Feb 26, 2003 · N463FE · Boeing 727225 · Landing Gear Door Retract SectionSDR 03FDEA00182Pressure Panel · gougedGOUGED AREA AT NLW UPPER WEB AT LT PRESSURE PANEL CUT OUT INBOARD SIDE, B.S 242. REMOVED DAMAGE AND REPAIRED IAW SRM 51-40-2. GOUGE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1.Feb 26, 2003 · N464FE · Boeing 727225 · Fuselage Main, BulkheadSDR 03FDEA00181Floorbeam · corrodedCORROSION ON FLOORBEAM LOWER FRAME AROUND NUT PLATE HOLES, B.S.720, LBL 16 TO LBL 21, W.L. 200 AT PREVIOUS REPAIR.Feb 26, 2003 · N464FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 03FDEA00176Shear Tie · crackedWHILE WORKING N00939, FOUND CRACKED SHEAR TIE AT BS 328, STR 26-27 LEFT. REPAIRED SHEAR TIE BS 328, STR. 26-27 LEFT, IAW SRM 53-10-4 FIG. 15.Feb 25, 2003 · N464FE · Boeing 727225 · Fuselage Main, StructureSDR 03FDEA00177Web · corrodedCORROSION ON WEB, STA 1174, RBL 18, WL 208. REMOVED CORROSION AT STA 1174. WEB FOUND OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-1Q0-1, 51-40-2.Feb 25, 2003 · N464FE · Boeing 727225 · Fuselage Main, StructureSDR 03FDEA00174Web · gougedRT WHEEL WELL HAS GOUGE IN WEB. DAMAGE ON RT WHEEL WELL WEB COMMON TO K-BEAM AREA, BS 872, RBL 5.5, WL 150, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER FROM 7075-T6 .040 INCH, LOT NR 472905. ALODINED, PRIMED, PAINTED, AND IFeb 25, 2003 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 03FDEA00175Frame · corrodedCORROSION FORWARD CARGO BAY ON LOWER FRAME AT STA 660, STR 28L TO 28R.Feb 25, 2003 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 03FDEA00169Floorbeam · corrodedCORROSION ON FLOORBEAM REPAIR FILLER B.S. 1070, RBL 42 TO LBL 36. REMOVED CORROSION ON FLOORBEAM REPAIR FILLER BS 1070. FOUND TO BE OUT OF LIMITS. REMOVED FILLER, FABRICATED REPLACEMENT AND INSTALLED IAW SRM 53-10-1, 53-10-8.Feb 24, 2003 · N464FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 03FDEA00168Floorbeam · corrodedCORROSION ON TOP OF UPPER LOBE FLOORBEAM AT BS 344, LBL 3, TO LBL 60. REMOVED CORROSION ON UPPER LOBE OF FLOORBEAM AT 344, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED, TREATED AND INSTALLED REPAIR UPPER LOBE IAW SRM 53-10-8, SR 27-53-007, Feb 24, 2003 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 03FDEA00167Floorbeam · corrodedCORROSION ON FLOORBEAM, UPPER FLANGE AT BS 680 RBL 11, DAMAGED ON REPAIR DOUBLER, NO DAMAGE LIMITS ON REPAIR DOUBLER, REPAIRED FLOORBEAM AT BS 680, WL 208, RBL 11, IAW SRM 53-10-8 FIG 3.Feb 24, 2003 · N464FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 03FDEA00166Skin · dentedSKIN DENT, BS 720B+3, JUST BELOW STR 17R, REWORKED SKIN DENT, BS 720B+3 BELOW STR 17R. A=1.8 Y=.062 A/Y=12.9 AND OIL CANNED. OUT OF LIMITS IAW 53-30-01. REMOVED DAMAGED AREA 2.3 X 2.9. FABRICATED, ALODINED, PRIMED AND PAINTED AND INSTALLED REPAIR DOUBLERFeb 24, 2003 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 03FDEA00156Frame · corrodedWHILE WORKING CARD FOUND LOWER NOSE FRAME LT SIDE TO BE CORRODED AT BS 296 LBL 20. FOUND LOWER NOSE FRAME LT SIDE TO BE OUT OF LIMITS AT BS 296, LBL 70. REMOVED AND REPLACED LT FRAME IAW SRM 51-20-1, 51-30-7, 51-30-5.Feb 21, 2003 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 03FDEA00155Stringer · corrodedCORROSION ON STR 28R, BS 480-484, WL 150, INBOARD SIDE. REMOVED CORROSION FROM STR 28R AT B.S 480+4 INCH, FOUND TO BE OUT OF LIMITS. FABRICATED, ALODINED AND PRIMED REPAIR PARTS, AND INSTALLED IAW SRM 51-10-4, 53-10-1, 53-10-3, 51- 30-2 AND MM 51-20-15Feb 21, 2003 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 03FDEA00153Skin · dentedDENT IN SKIN BS 460-480 BETWEEN 14.15RFeb 21, 2003 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 03FDEA00157Floorbeam · corrodedCORROSION ON FLOORBEAM UPR FLANGE BS 1110, RBL 57 TO LBL 57, WL 208.Feb 21, 2003 · N464FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 03FDEA00158Floorbeam · corrodedCORROSION ON 950F FLOORBEAM UPPER FLANGE UPPER AND LOWER SURFACE FROM LBL 55 TO RBL 55, WL 208.Feb 21, 2003 · N464FE · Boeing 727225 · Fuselage Main, Floor BeamSDR 03FDEA00142Stringer · corrodedCORROSION IN SEVERAL AREAS IN STRINGER 26R FROM BS 620 TO 720A. REMOVED AND REPLACED STRINGER SECTION AT BS 675 - 720+10 IAW SRM 53-10-3.Feb 20, 2003 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 03FDEA00143Skin · corrodedCORROSION ON SKIN AT BS 702, RBL 20, WL 150, BETWEEN STR 26R AND 27R.Feb 20, 2003 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2003748001Battery1) NEITHER THE COCKPIT EMERGENCY EXIT OR THE ENTRYWAY EMERGENCY EXIT LIGHTS WORKED WITH THE SWITCH IN THE ON POSITION.2) REPLACED BATTERIES IN COCKPIT AND ENTRYWAY EXIT LIGHTS. OPS CHECKED GOOD IAW M/M 33-50-0.Feb 20, 2003 · N748DH · Boeing 727225 · Emergency LightingSDR CA030228013Gearbox · failed(CAN) DURING COLD WEATHER, PRE-DEPARTURE CHECK BY MAINTENANCE PERSONNEL, THE STABILIZER TRIM SYSTEM WAS OPERATED. DURING OPERATION A VIBRATION AND NOISE WAS NOTICED. UPON INVESTIGATION IT WAS FOUND THAT THE BRAKE ASSEMBLIES IN THE STABILIZER TRIM GEARBOX WERFeb 19, 2003 · Boeing 727225 · Stabilizer Control SystemSDR DHL2003755003Seal1) DESCENDING THRU 8000' INTO CVG #1 ENGINE LOW OIL PRESSURE LIGHT CAME ON. NOTED OIL QUANTITY AT "0". SHUT DOWN #1 IN FLIGHT.2) FOUND GEAR BOX TO OIL COOLER TUBE LINE LEAKING AT B-NUT. REPLACED RUBBER SEAL, TIGHTENED LINE, AND RAN ENGINE NO LEAKS NOTED IAW Feb 13, 2003 · N755DH · Boeing 727225 · Engine Oil Distribution (Airframe Furnished)SDR DHL2003743003Battery Pack1) MAIN ENTRY DOOR EMERGENCY LIGHTS FOUND HANGING FROM HOLDER AND WILL NOT ILLUMINATE.2) REMOVED AND REPLACED BATTERY PACK, OPS CHECKED NORMAL, MM REF. 33-50-71.Jan 29, 2003 · N743DH · Boeing 727225 · Emergency LightingSDR DHL2003742005Lamp1) POSITION #2 SMOKE DETECTOR WILL NOT TEST.2) REMOVED AND REPLACED TEST LAMP ON SMOKE DETECTOR, OPS CHECKED GOOD IAW BMM 26-17-0.Jan 24, 2003 · N742DH · Boeing 727225 · Smoke DetectionSDR RYN2003F00000Actuator · defectiveDURING CLIMBOUT, NR 7 LEADING EDGE SLAT WOULD NOT RETRACT. EMERGENCY FLAP PROCEDURES FOLLOWED. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT.Jan 23, 2003 · N815EA · Boeing 727225 · Leading Edge Slat ActuatorSDR DHL2003755002Light1) WHEN LANDING GEAR WAS SELECTED DOWN, LEFT MAIN GREEN LIGHT FAILED TO ILLUMINATE. SECONDARY MAIN GREEN LIGHTS WERE ILLUMINATED. CYCLING LIGHTS DIMMER SWITCH GOT ALL GEAR LIGHTS WORKING. 2) REMOVED AND REPLACED KORRY LIGHT ASSEMBLY IAW B727 M/M 33-10-51 (LTJan 23, 2003 · N755DH · Boeing 727225 · Landing Gear Position and WarningSDR DHL2003755001Proximity Sensor · dirtyLT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR SELECTED DOWN (PRIMARY). SECONDARY MAIN GEAR LIGHTS DID ILLUMINATE. CREW PERFORMED THE ABNORMAL PROCEDURE AND MADE NORMAL LANDING. ON FINAL APPROACH LIGHT ILLUMINATED. CLEANED PROXIMITY SENSOR PER M/M Jan 23, 2003 · N755DH · Boeing 727225 · Landing Gear Position and WarningSDR DHL2003742004Lamp1) #2 SMOKE DETECTION TEST LIGHT INOPERATIVE.2) RELAMPED #2 SMOKE DETECTOR IAW M/M 26-17-02, SYSTEM OPS CHECKED GOOD.Jan 22, 2003 · N742DH · Boeing 727225 · Smoke DetectionSDR DHL2003743002Battery Pack · dischargedEMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR INOPERATIVE ON PREFLIGHT. REMOVED AND REPLACED BATTERY PACK. LIGHT OPS CHECKED GOOD PER M/M 33-50-51.Jan 21, 2003 · N743DH · Boeing 727225 · Emergency LightingSDR MYW2003F00001Regulator Valve · inoperativeON DEPARTURE, NR 1 ENGINE SUPPLY PRESSURE (DUCT PRESSURE) REACHED 95 PSI FOLLOWED BY STRUT OVERHEAT AND PACK TRIP. RETURN AIRCRAFT. AIRCRAFT PREPED FOR TWO ENGINE FERR. ACCOMPLISHED TWO ENGINE FERRY TO MIA IAW MM. REMOVED AND REPLACED 13 STAGE MODULATING RJan 18, 2003 · N804MA · Boeing 727225 · Pneumatic Distribution SystemSDR DHL2003742003Fire Loop · out of positionENGINE NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED. TRANSFERRED TO DMI LOG PER DHL MEL 26-9 CAT-C DDD 01-28-2003 DMI 11670. PLACARD INSTALLED. RE; DMI 11670 - NR 3 ENGINE FIRE GROUND FAULT LIGHT ILLUMINATES INTERMITTENTLY. FOUND 3 FIRE LOOP TOUCHINJan 18, 2003 · N742DH · Boeing 727225 · Fire DetectionSDR DHL2003742002Clamp · looseNR 3 FIRE DETECTOR GROUND LIGHT ILLUMINATED. DEFERRED NR 3 ENGINE FIRE DETECTOR GROUND LIGHT IAW MEL 26-9-1. CONTROL 11652. REF DMI 11652, NR 3 FIRE DETECTOR GROUND LIGHT ILLUMINATED. CLEANED CONNECTOR AT ENGINE AREA AND RE-SECURED LOOSE HOLDING CLAMP. PEJan 16, 2003 · N742DH · Boeing 727225 · Fire DetectionSDR DHL2003742001Module · malfunctionedWITH LANDING GEAR HANDLE IN UP POSITION, WARNING HORN SOUNDS CONTINUOUSLY AND ALL THREE RED GEAR UNSAFE LIGHTS ARE ILLUMINATED. RESEATED LANDING GEAR ELECTRONIC MODULE; PERFORMED OPERATIONAL TEST OF LANDING GEAR ELECTRONIC MODULE IAW B-727 M/M 32-09-121, CYCLJan 10, 2003 · N742DH · Boeing 727225 · Landing Gear System WiringSDR DHL2003743001Battery1) LOWER CARGO SMOKE/FIRE DETECTION SYSTEM GREEN LIGHT INOP.2) REMOVED AND REPLACED CCU IAW M/M 26-16-00. NO HELP, TRANSFERRED TO DMI #11515 IAW B-727 MEL 26-19 CAT. "C". PLACARDS INSTALLED.3) REF. DMI #11515 LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM 1Jan 8, 2003 · N743DH · Boeing 727225 · Smoke Detection
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