Boeing 727-233

Service difficulty reports · 3,034

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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 = '727233'
  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 05FDEA01925Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 950C, STR 8R. REPLACED CRACKED STRINGER CLIP PER SRM 51-30-2.Jul 13, 2005 · N218FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 05FDEA01921Stringer Clip · crackedFUSELAGE UPPER LOBE STRINGER CLIP CRACKED BS 680 STR-5L. REMOVED FABRICATED AND INSTALLED STRINGER CLIP AT BS 680 STR 5L IAW SRM 51-20-1, 51- 30-02, 51-10-02.Jul 13, 2005 · N218FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR PCSA708051Module · malfunctionedON DEPARTURE, CREW REPORTED STALL WARNING STICK SHAKER CAME ON AT ROTATION. CREW DUMPED FUEL, RETURNED AND LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUBLESHOT STALL WARNING SYSTEM. OPERATIONAL CHECK NORMAL IAW B-727 MM CH 34-18-01, UNABLE TO DUPLICATJul 8, 2005 · N395AJ · Boeing 727233 · Stall Warning SystemSDR 05FDEA01708Skin · damagedFUSELAGE EXTERNAL SKIN OF AFT AIRSTAIR, SECTION 48, AREA FROM LE TO 27 INCH AFT OF LE, LBL 21 TO RBL 21, HAS GRAVEL DAMAGE.Jun 27, 2005 · N263FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA01665Skin · corrodedAFT CARGO CORROSION ON FUSELAGE SKIN STA 1010, STR 29L. OUT OF LIMITS AREA CUT OUT, INSTALLED SRM REPAIR TO THE SKIN AT STA. 1010, STR 29L, REF SRM 53-30-3 PAGE 14E-14O FIG 3AJun 23, 2005 · N263FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA01664Floorbeam · corrodedCORROSION ON FLOORBEAM LBL 10, BS 560. REPAIRED PER SRM 53-10-8.Jun 23, 2005 · N264FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 05FDEA01666Seat Track · corrodedSEAT TRACK LBL 24 HAS CORROSION FROM STA 344-480. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.Jun 23, 2005 · N272FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01649Intercostal · crackedINTERCOSTAL CRACKED STA 358, STR 16 LT. REPAIRED INTERCOSTAL PER SRM 51-40-2.Jun 22, 2005 · N264FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 05FDEA01648Skin · gougedFUSELAGE EXTERNAL SKIN GOUGED AT AFT AIRSTAIR CUTOUT, BS 1230, LBL 20. REPAIRED SKIN AT AFT AIR STAIR CUTOUT BS 1230, LBL 20 PER SRM 53-30-3.Jun 22, 2005 · N263FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR PCSA6210501Oil System · leakingDURING CRUISE NR 3 ENGINE OIL TEMP WAS BETWEEN 125 & 130 DEG FOR 15 MINUTES. PERFORMED ALT PROCEDURES, RETARDED THROTTLE, DIDN'T HELP. SHUTDOWN NR 3 ENGINE, ENGINE WINDMILLED FOR 45 MIN. OIL PRESSURE STAYED ABOVE 25 PSI. DIVERTED & LANDED AT SJU. MX INSPEJun 21, 2005 · N395AJ · Boeing 727233 · Turbine Engine Oil SystemSDR PCSA06080501Connector · dirtyFLIGHT 8113 TTPP/SVMC - AFTER DEPARTURE FROM TTPP, CREW REPORTED UNABLE TO RETRACT OUTBOARD FLAPS FROM 5 DEGREES. RETURNED AIRCRAFT TO TTPP USING THE SPLIT FLAP ALTERNATE PROCEDURE IAW AMERIJET 727 AIRCRAFT OPS MANUAL CHAPTER 5 PAGE 53 AND 54. AIRCRAFT LANDEJun 6, 2005 · N495AJ · Boeing 727233 · Flight Control System WiringSDR 05FDEA01398Skin · deformedWHILE WORKING NOSE AREA DOUBLER FOUND SKIN DEFORMED ALONG LT SIDE. REPLACED DOUBLER PER FED-EX EA 7-5330-86293.May 21, 2005 · N264FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR PCSA0519051Connector · looseFLIGHT 846 DURING CLIMB FROM KIN CREW REPORTED LEADING EDGE AMBER LIGHT CAME ON, CYCLED FLAPS TO 5 DEGREES AND BACK TO 0 DEGREES. LIGHT REMAINED ON, CONFIRMED WITH FLT ENGINEER FLAP SLAT ANNUNCIATOR PANEL. FOLLOWED INOPERATIVE L/E FLAP/SLATS ALTERNATE PROCEDMay 19, 2005 · N495AJ · Boeing 727233 · Leading Edge Slat Position Indicating SystemSDR PCSA0518051Cover · leakingDURING CLIMB CREW REPORTED LOSS OF HYDRAULIC (A) SYSTEM. AIRCRAFT WAS DIVERTED AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND FEEL COMPUTER FILTER COVER LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED FEEL COMPUTER FILTER CAP AND O-RING IAW MM CH 20-10May 18, 2005 · N395AJ · Boeing 727233 · Hydraulic Reservoir, MainSDR 05FDEA01371Skin Panel · gougedCOMPLY WITH EA 7-5330-55484 FUSELAGE, PLATES AND SKIN GOUGE REPAIR AT BS 950E, STR 19R. COMPLIED WITH EA 7-5330-55484 FUSELAGE, PLATES AND SKIN GOUGE REPAIR AT BS 950E, STR 19R. THIS IS A MAJOR REPAIR.May 18, 2005 · N254FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA01360Fairing · crackedLT WING LOWER T/E FLAP TRACK SKATE FAIRING BEHIND MLG STRUT IS CRACKED. REMOVED AND REPLACED SKATE FAIRING IAW SRM 51-30-2.May 17, 2005 · N254FE · Boeing 727233 · Trailing Edge FlapsSDR 05FDEA01359Floorbeam · damagedFLOORBEAM LBL 7-RBL 40 UPPER CHORD REQUIRES MAJOR REPAIR. REMOVED AND REPLACED UPPER T-CHORD IAW SRZ 53-034E REPAIR NR 7.May 17, 2005 · N254FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 05FDEA01358Insulation · damagedEQUIPMENT AND FURNISHINGS INSULATION BLANKETS. PARTIAL REPLACEMENT STA 360-1183, MAIN CABIN COMPARTMENT. COMPLIED WITH EA 7-2580-81692.May 17, 2005 · N254FE · Boeing 727233 · Cargo CompartmentsSDR 05FDEA01349Tire · defectiveRTO DUE TO VIBRATION ON T/O ROLL. MINOR VIBRATION AT 60 KTS INCREASING IN INTENSIVE TO MODERATE VIBRATION AS SPEED INCREASED RTO AT 110 KTS. RTO AT 0815Z WITH 49 MIN COOL TIME. AFTER DEBRIEF WITH FLIGHT CREW IT WAS DETERMINED THAT VIBRATION WAS WORSE WHEN YMay 17, 2005 · N220FE · Boeing 727233 · TireSDR 05FDEA01289Retainer · corrodedLT NOSE GEAR AFT DOOR SEAL RETAINER CORRODED. REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-30-2.May 15, 2005 · N254FE · Boeing 727233 · Landing Gear DoorsSDR 05FDEA01288Insulation · damagedCOMPLY WITH EA 7-2580-81691 "EQUIPMENT AND FURNISHINGS. INSULATION BLANKETS, PARTIAL REPLACEMENT, STA 178-294, LOWER SECTION 41 INCH.May 15, 2005 · N254FE · Boeing 727233 · Accessory CompartmentSDR 05FDEA01259Doubler · corrodedFUSELAGE STA 740 BULKHEAD SUPPORT DOUBLER CORROSION. COMPLIED WITH EA 7-5310-55482 FUSELAGE STA 740 BULKHEAD SUPPORT DOUBLER CORROSION AT MAE. THIS IS A MAJOR REPAIR.May 12, 2005 · N254FE · Boeing 727233 · Fuselage Main, BulkheadSDR PCSA5030501Cdu · shortedFLIGHT 711 MIA TO MEX, DURING CRUISE LOWER CARGO FIRE LIGHT AND BELL CAME ON INDICATING A AFT FIRE. FUEL WAS DUMPED, AIRCRAFT DIVERTED TO MID AND LANDED WITH NO FURTHER INCIDENT. UPON INSPECTION OF THE AFT CARGO COMPARTMENT ON THE GROUND NO FIRE WAS OBSERVEDMay 3, 2005 · N495AJ · Boeing 727233 · Fire DetectionSDR 05FDEA01160Skin · dentedBS 720 15 TO 20, CREASED DENT BETWEEN STRINGER 18L-19L. REPAIRED SKIN AT BS 720 PLUS 15 TO PLUS 20, STR 18L - 19L PER SRM 53-30-3.Apr 28, 2005 · N264FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA01170Shear Tie · corrodedCORROSION ON SHEAR TIE LOWER SURFACE AT SKIN BS 1130 BETWEEN STR 29L AND STR 30. REPLACED SHEAR TIE PER SRM 53-10-1.Apr 28, 2005 · N264FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 05FDEA01168Skin · tornFORWARD ENTRY DOOR LOWER HINGE ARM AND SNUBBER CUTOUT SKIN IS TORN. REPAIRED FORWARD ENTRY DOOR LOWER HINGE ARM CUTOUT PER SRM 51-40-2.Apr 28, 2005 · N264FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA01159Bracket · corrodedCORROSION C-53-100-01 AT LEFT MAIN WHEEL WELL, BS 919 WL 189 LBL 65 UPPER SURFACE. WORK TO BE ACCOMPLISHED ON CUSTOMER ID N00428.Apr 28, 2005 · N264FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 05FDEA01169Frame · corrodedCORROSION ON FRAME BS 700 LBL 13 WL 148. REPAIRED BS 700 FRAME, LBL 13, WL 148 PER SRM 53-10-4.Apr 28, 2005 · N264FE · Boeing 727233 · Fuselage Main, FrameSDR 05FDEA01158Structure · corrodedCORROSION AT LEFT MAIN WHEEL WELL, BS 928-932 WL 189 LBL 65 UPPER SURFACE. REPLACED STRINGER 18A PER SRM 51-40-3.Apr 28, 2005 · N264FE · Boeing 727233 · Fuselage Main, StructureSDR 05FDEA01144Roller · damagedDURING LANDING ROLLOUT, AFT AIRSTAIR EXTENDED. REMOVED AND REPLACED AFT RT SIDE ROLLER BECAUSE ROLLER DOES NOT TURN. REPLACED MAIN BEARING AS PER 727-200 M/M 52-62-001-1, T/S DOOR OPS CKED OK. OK FOR FLT.Apr 27, 2005 · N257FE · Boeing 727233 · Entrance StairsSDR 05FDEA01102Seat Track · damagedSEAT TRACK STA 244 TO 480 RBL 45, HAS EXISTING BLEND REPAIRS AND AN EXISTING SPLICE REPAIR AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED SEAT TRACK IAW SRM 51-30-2. FAB'D SEAT TRACK ON TRAVELER NR T5/510065. LOCATED AND DRILLED IAW SRM 53-10-5 FIG 3. Apr 22, 2005 · N254FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01060Seat Track · damagedSEAT TRACK, STA 344 - 480 HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002, LBL 45. REMOVED SEAT TRACK STA 344 - 480 LBL 45 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK PER TRAVELER NR T5/510063, BATCH NR 888841, PO NR MST0017183. LOCATEApr 21, 2005 · N254FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01059Seat Track · damagedSEAT TRACK, STA 344, LBL 24 HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED SEAT TRACK STA 344 - 480 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK PER TRAVELER NRT5/510064, BATCH NR 888841, P.O. NR MST0017183. LOCATED AND DRILLEDApr 21, 2005 · N254FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01058Strap · chafedMAIN DECK CARGO, AT STA 1030 AND 1050 STR 6L, LINER FRAME ASSY HAS CHAFED INTO THE FRAME STRAP'S AND HARDWARE. GOUGE OUT OF LIMITS IAW BOEING SRM 53-10-1. REMOVED AND REPLACED STRAP IAW BOEING SRM 51-30-2.Apr 21, 2005 · N254FE · Boeing 727233 · Fuselage Main, FrameSDR CA050426003Valve · fouled(CAN) AFTER DEPARTING, THE CREW OBSERVED AN INDICATION OF ANTI-ICE SELECT FAILURE ON NR1 ENGINE. THE CREW RETURNED TO DEPARTURE, WHERE MAINTENANCE FOUND INTERNAL PARTS FROM THE THERMOSTATIC VALVE FOR THE NR1 LT NOSE COWL ANTI-ICE HAD FOULED THE ANTI-ICE VALVE.Apr 20, 2005 · Boeing 727233 · Antenna/Radome Anti-Ice/De-Ice SystemSDR 05FDEA00847Skin · crackedCRACKED EXTERNAL SKIN FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED CRACK PER FED-EX EA 7-5330-86273.Apr 5, 2005 · N272FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA00832Skin · dentedDENT IN EXTERNAL FUSELAGE SKIN AT BS 1345 BY LEFT AFT CORNER OF AIRSTAIR CUT OUT. REPAIRED DENT PER SRM 54-30-3.Apr 4, 2005 · N272FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA00779Housing · gougedNR 3 LOWER CARGO DOOR, HANDLE HOUSING GOUGED BY HANDLE STUD. REMOVED AND REPLACED #3 LWR CARGO DOOR HANDLE PER SRM 51-30-02.Apr 1, 2005 · N272FE · Boeing 727233 · Cargo/Baggage DoorsSDR 05FDEA00735Shear Web · corrodedCORROSION IN SHEAR WEB BS 1166 LBL 29-33 WL 208.Mar 31, 2005 · N272FE · Boeing 727233 · Fuselage Main, StructureSDR 05FDEA00736Support · corrodedLWR FUSELAGE, BS 740 R A/C BAY RBL 10, CORROSION EMANATING FROM LWR CHORD AND BULKHEAD. REPAIRED BS470 LOWER CHORD PER FED-EX EA 7-5310-86268.Mar 31, 2005 · N272FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 05FDEA00691Skin · gougedEXTERNAL FUSELAGE SKIN GOUGED AT NR 3 CARGO DOOR CUTOUT, BS 1096 AT STR 24R. REPAIRED GOUGE PER FED-EX EA. 7-5330-86272.Mar 29, 2005 · N272FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 05FDEA00629Seat Track · corrodedSEAT TRACK, STA. 344 - 480, LBL 24 HAS CORROSION AND EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2 - MAT ID BAC 1520-792 IAW SRM 51-10-2 FIG 7. NEW EXTRUSION SCALLOPED ON TRAV NR T5/501341. Mar 22, 2005 · N271FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA00520Adc · malfunctionedREJECTED TAKEOFF. REMOVED AND REPLACED AIR DATA COMPUTER IAW MM 34-12-011-4. GRD CK OK. A/C DOWN GRADED TO NOT CAT II. A/P NR 1 CK CAT II A/P NR 2 CK CAT II PREMATURE REMOVAL/INSTALLATION OFF MFG HG480B13.Mar 15, 2005 · N275FE · Boeing 727233 · Air Data ComputerSDR 05FDEA00519Adc · malfunctionedREJECTED TO AT 80 KTS. RAN RTO CHECKLIST. NO AIRSPEED ON CAPT'S AIRSPEED INDICATOR. REMOVED AND REPLACED AIR DATA COMPUTER IAW MM 34-12-011-4. A/C DOWN GRADED TO NOT CAT II. A/P NR 1 CK CAT II A/P NR 2 CK CAT II. R/I FROM FACT PREMATURE REMOVAL/INSTALLMar 15, 2005 · N275FE · Boeing 727233 · Air Data ComputerSDR 05FDEA00318Module · failedWHEN GEAR HANDLE IS UP, RIGHT GEAR SAFE GREEN LIGHT WILL NOT TEST. REPLACED BULBS CYCLED CBS. SWAPPED RIGHT GEAR AND LEFT GEAR LIGHTS IN LEFT POSITION, RIGHT LIGHT WORKED IN RIGHT POSITION, LEFT LIGHT DID NOT WORK. CK'D CONTINUITY THROUGH WARN LIGHT PUSH TOFeb 26, 2005 · N222FE · Boeing 727233 · Landing Gear Position and WarningSDR 05FDEA00280Skin Panel · corrodedOVERWING BOX, TANK TOP, HAS CORROSION AT BODY STATION 840 RIGHT BUTT LINE 12.0. REPAIRED OVERWING BOX FUEL TANK, STATION 840 AT RIGHT BUTT LINE 12.0 IAW FEDEX EA 7-5730-83992, WINGS-UPPER SKIN PANEL, CENTER TANK CORROSION-REPAIR.Feb 12, 2005 · N258FE · Boeing 727233 · Wing, Plate/SkinSDR CA050203005Cylinder · intermittent(CAN) NLG FAILED TO EXTEND ON APPROACH, THEN RE-CYCLED AND EXTENDED NORMALLY. NOSE GEAR JACKED, NOSE GEAR TRUNION GREASED AND GEAR RETRACTED AND EXTENDED 4 TIMES WITH NO FAULTS. AC WAS DISPATCHED WITH NO FURTHER FAULTS. QA GROUNDED THE AC DUE TO 2 OTHER EVENFeb 2, 2005 · Boeing 727233 · Nose/Tail Landing GearSDR CA050119003Switch · intermittent(CAN) ON APPROACH, LANDING GEAR CYCLED DOWN FOR LANDING. THE NOSE LANDING GEAR RED INDICATOR STAYED ILLUMINATED AND NO GREEN INDICATION WAS SEEN. GEAR WAS RE-CYCLED AND THE GEAR WAS EXTENDED WITH PROPER INDICATION. MAINTENANCE LUBED THE NOSE GEAR AND JACKED THJan 19, 2005 · Boeing 727233 · Landing Gear Position and WarningSDR CA050105013Actuator · separated(CAN) ON APPROACH, THE CREW OBSERVED 'A' (HYDRAULIC) SYSTEM DEPLETION. SYSTEM DESELECTED, NORMAL LANDING CARRIED OUT. THE NOSE LANDING GEAR DOWN LOCK ACTUATOR SEPARATED FROM THE AIRFRAME MOUNT AND HAD DAMAGED THE HYDRAULIC LINES.Dec 29, 2004 · Boeing 727233 · Landing Gear ActuatorSDR CA041216008Transmitter · sticking(CAN) DURING INITIAL CLIMBOUT, FLAPS CYCLED FROM 5 DEG. TO 2 DEG. CREW NOTICED THAT LT OUTBOARD FLAPS WERE INDICATING 5 DEG. & RT OUTBOARD FLAPS WERE INDICATING 3 DEG. CAUSING AN ASSYMETRY SPLIT. CREW HAD TO DUMP FUEL TO LAND WITHIN LANDING WEIGHT. CREW ACCOMPDec 15, 2004 · Boeing 727233 · Trailing Flap Position Indicating System
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