Boeing 727-2S2F

Service difficulty reports · 842

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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 = '7272S2F'
  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 96FDEA01032Fire Warning · activatedNR 1 ENG FIRE IND INTERMITTENT BELL AND LIGHT ON CLIMBOUT. RETARDING THROTTLE HAD NO EFFECT ON THE INDICATIONS.May 25, 1996 · N212FE · Boeing 7272S2F · Fire DetectionSDR 96FDEA01025Fire Connector · looseNR 1 ENG FIRE LIGHT INTERMITTENT IND DURING CLIMBOUT. FIRE TEST CHECKED GOOD, NO SECONDARY INDICATIONS. INSPECTED FIRE LOOP AND FOUND LOOSE CONNECTOR, RESEATED SAME AND CHECKED AS PER MM 26-11-01, NO FAULTS NOTED. RAN NR 1 ENG PER JET HANDBOOK, NO FAULTS NOMay 24, 1996 · N212FE · Boeing 7272S2F · Fire DetectionSDR 96FDEA00851Transmitter · leakingDURING CRUISE, A-SYS HYD QTY NOTED LOW, READING LESS THAN HALF GALLON. FOLLOWED EMERGENCY PROCEDURES AND FOLLOWED LOSS OF A-SYSTEM MANUAL GEAR EXTENSION AT IAD. GEAR PINS INSTALLED AND TOWED TO GATE. FOUND SYS-A HYD TRANSMITTER LEAKING INTERNALLY. REPLACEDApr 26, 1996 · N203FE · Boeing 7272S2F · Hydraulic Pressure IndicatorSDR 96FDEA00759Rib · crackedHFEC INSP EXHIBITS CRACKS EMANATING AT 12 AND 6 O'CLOCK FROM THE FWD MOST UPPER HOLE AT THE LT WING RIB CHORD BL 70.5 BS 760. REMOVED CRACK BY STOP DRILLING AND INSTALLED SMALL REPAIR AT STA 760 LBL 70.5 WL 209 TO 208 IAW FEDEX EA 7-5710-28232.Apr 11, 1996 · N217FE · Boeing 7272S2F · Wing, Rib/BulkheadSDR 96FDEA00746Rib · crackedNR 0137, -001, HFEC INSP EXHIBITS A CRACK IN THE FWD MOST UPPER HOLE AT APPROX 12 O'CLOCK AT RT WING RIB CHORD BL 70.5 BS 760. CUT OUT DAMAGE AT 630 JUST BELOW STR 22R AND REPAIRED PER FEDEX SRM 53-30-3 AND EA 7-5710-28223.Apr 5, 1996 · N217FE · Boeing 7272S2F · Wing, Rib/BulkheadSDR 96FDEA00255Retract Mech · malfunctionedNOSE GEAR DOOR WARNING LIGHT ON SECOND OFFICER'S PANEL AND RED DOOR WARNING LIGHT ON FRONT PANEL REMAINED ON AFTER GEAR RETRACTION. THE ABNORMAL PROCEDURE WAS ATTEMPTED. DURING RECYCLE, DOORS OPERATED NORMAL BUT LIGHT REMAINED ON DURING RETRACTION. ALSO, LOFeb 15, 1996 · N211FE · Boeing 7272S2F · Landing Gear Door Retract SectionSDR 96FDEA00184Switch · lack of lubeLT GEAR GREEN LIGHT DID NOT COME ON WHEN LANDING GEAR WAS EXTENDED, RED LIGHT REMAINED ON. AFTER CYCLING GEAR AND MISSED APPROACH, GREEN LIGHT CAME ON AND A/C LANDED. LUBRICATED NOSE LANDING GEAR WITH AEROSHELL NR 5, CLEANED CANNON PLUG AT MICRO SWITCH AND AFeb 5, 1996 · N215FE · Boeing 7272S2F · Landing Gear Position and WarningSDR 96FDEA00025Skin · crackedCRACK IN CORNER OF SKIN BS 1223 LBL 16 WL 148. REPAIRED CRACK IN CORNER OF SKIN AT BS 1223 LBL 16 WL 148 PER FEDEX EA 7-5330-26829.Jan 8, 1996 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 96FDEA00005Skin · crackedCRACK IN CORNER OF SKIN, BS 1223, LBL 16, WL 148. REPAIRED CRACK IN CORNER OF SKIN, BS 1223, LBL 16, WL 148, PER FEDEX EA 7-5330-26829.Jan 2, 1996 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 96FDEA00003Skin · crackedDUE TO SEVERAL DISCREPANCIES CONSISTING OF CRACKS AND WORN FASTENER HOLES, RT ELEVATOR REQUIRED REPLACEMENT. REMOVED AND REPLACED RT ELEVATOR PER FEDEX MM 27-30-0, 27-30-01, 27-30-21, 27-30-05, 27-30-11. FUNCTIONAL TEST PER FEDEX MM 27-30-01 CHECKS GOOD.Jan 2, 1996 · N213FE · Boeing 7272S2F · Elevator, Plate/SkinSDR 96FDEA00001Skin · dentTHE FUSELAGE SKIN IS DENTED AT BS 512 BETWEEN STR 26 TO 27L. REMOVED DENT AND REPAIRED WITH DOUBLER AT BS 512 BETWEEN STR 26 TO 27L IAW FEDEX SRM 53-30-3.Jan 2, 1996 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 96FDEA00002Skin · gougedTHERE IS A GOUGE IN FUSELAGE SKIN EXTERIOR AT BS 527, WL 192 BETWEEN STR 18 - 19L.Dec 28, 1995 · N213FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 95FDEA01901Fire Loop · malfunctionedINTERMITTENT FIRE WARNING NR 1 ENG FOLLOWED BY CONTINUOUS INTERMITTENT WARNING ON SAME. COMPLIED WITH PROCEDURE AND SHUTDOWN NR 1 ENG WARNING, PERSISTED. FIRED NR 1 AND NR 2 BOTTLE INTO NR 1 ENG PER PROCEDURE. WARNING PERSISTED INTERMITTENTLY TILL TOUCHDOWNDec 20, 1995 · N213FE · Boeing 7272S2F · Fire DetectionSDR 95FDEA01895Access Panel · missingUPPER ACCESS PANEL MISSING ON LT NAVIGATION LIGHT. INSTALLED PANEL.Dec 13, 1995 · N201FE · Boeing 7272S2F · Wing, Plate/SkinSDR 95FDEA01865Rib · crackedWHILE WORKING INSP CARD 7-5710-7-2308H PT 1 NOTED CRACK INDICATIONS IN THE FWD UPPER AND LOWER HOLES OF THE 70.5 CHORD BS 760 RT. CRACK INDICATIONS IN THE FWD UPPER ARE IN THE 1 AND 6 O'CLOCK POSITION, LWR FWD HOLE IN 2 O'CLOCK POSITION. TRIMMED OUT CRACKED FDec 6, 1995 · N211FE · Boeing 7272S2F · Wing, Rib/BulkheadSDR 95FDEA01866Fire Detectors · malfunctionedENG FIRE WARNING LIGHT ILLUMINATES WHEN POWER WAS REDUCED ON ENG NR 2. OPS AT IDLE AND LIGHT REMAINS OUT. LEAK CHECKED ENG AND FOUND NO BLEED AIR LEAKS. REMOVED AND REPLACED ENG AND FIREWALL FIRE DETECTION ELEMENTS. RAN ENG FOR 5 MINUTES AT POWER, PLUS TAXDec 2, 1995 · N206FE · Boeing 7272S2F · Fire DetectionSDR 95FDEA01840Chord · crackedNOTED CRACK INDICATIONS LT 70.5 BS 760 WHILE PERFORMING INSPECTION CARD NR 7-5710-7-2308H PT1, CRACK LOCATIONS ARE THE FWD UPPER HOLE AT 11 AND 5 O'CLOCK POSITION L/B LOOKING I/B. CRACK INDICATION ARE IN THE T-CHORD, PLUS CHORD. ACCOMPLISHED CRACK CONTAINMENDec 1, 1995 · N211FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 95FDEA01834Frame · crackedCRACK IN LOWER LOBE FRAME BS 660, RBL 2, WL 154. CUT OUT DAMAGED AREA AT BS 660, BL ZERO - RBL 5, WL 154. FABRICATED REPAIR PARTS OUT OF 7075T6.050 MATERIAL, AND INSTALLED WET WITH SEAL AS PER FEDEX SRM 53-10-2 AND 51-40-3.Nov 27, 1995 · N211FE · Boeing 7272S2F · Fuselage Main, FrameSDR 95FDEA01781Rib Chord · crackedREPAIR WING RIB UPPER CHORDS BS 760.75, RBL AND LBL 70.5, IAW FEDEX EA 7-5710-26265 AND 7-5710-26266. REPAIRED LT RIB UPPER CHORD, BS 760.95 IAW FEDEX EA 7-5710-26266. ALSO, REPAIRED RT RIB UPPER CHORD BS 760.95 IAW FEDEX EA 7-5710-26265.Nov 21, 1995 · N216FE · Boeing 7272S2F · Wing, Rib/BulkheadSDR 95FDEA01790Chord · crackedRIGHT INBOARD MID-FLAP AFT LOWER CHORD CRACKED AT INBOARD AFT FLAP ACTUATOR RUDDER CUT-OUT. REMOVED NR 5 FLAP TRACK AFT FAIRING. REMOVED DAMAGED PORTION OF AFT LOWER CHORD ON RT INBD MID-FLAP AND REPAIRED IAW FEDEX SRM 51-40-4, FIG 1. REINSTALLED NR 5 FLAP Nov 20, 1995 · N216FE · Boeing 7272S2F · Trailing Edge FlapsSDR 95FDEA01794Overheat Wire · bareDIA - NR 2 FIRE WARNING IND ON MOMENTARILY ON APPROACH INTO DEN, LESS THAN 2 SECOND BELL AND LIGHT. SYS CHECKS OK. OPENED COWL AND INSPECTED ALL DUCTS AND ENGINE. FOR LOOSE CONNECTIONS OR BREAKS, CHECKED OK. FOUND EXPOSED WIRE ON OVER HEAT WIRE ADJACENT TONov 18, 1995 · N206FE · Boeing 7272S2F · Overheat DetectionSDR 95FDEA01778Fire Wire Conn · dirtyIMMEDIATELY AFTER DISCONNECTING NR 3 CSD, FIRE BELL AND WARNING LIGHTS ON PILOTS PANEL AND NR 3 FIRE HANDLE ILLUMINATED MOMENTARILY BOTH SYS-A AND LOOPS WERE TESTED, TEST WAS GOOD. FIRE BELL WOULD INTERMITTENLY COME ON. FOUND LOOSE CLAMP ON LOWER PART OF NR Nov 18, 1995 · N206FE · Boeing 7272S2F · Fire DetectionSDR 95FDEA01776Fire Wire · looseFIRE WARNING BELL SOUNDED INTERMITTENTLY AND FIRE WARNING LIGHTS ON THE DASH AND WHEEL WELL LIGHT FLICKERED. NO LIGHTS IN THE HANDLES ON THE OVERHEAD PANEL. BELL SILENCED ITSELF AND LIGHTS WENT OUT. RESECURED L AND R LOOP CONNECTIONS IN WHEEL WELLS AND OPS Nov 17, 1995 · N206FE · Boeing 7272S2F · Fire DetectionSDR 95FDEA01795Fire Contl Unit · malfunctionedNR 2 ENG FIRE WARNING WOULD INTERMITTENTLY COME ON IN FLT AND DURING TAXI IN. FIRE TEST SYSTEMS CHECKED AND TESTED GOOD. REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT PER MM 26-11-01 AND OPS CHECK NORMAL. REMOVED AND REPLACED FIRE AND OVERHEAT DETECTOR, Nov 9, 1995 · N206FE · Boeing 7272S2F · Fire DetectionSDR 95FDEA01673Turbine · failedDURING LOW SPEED TAKEOFF ROLL, ALOUD POP/SHUDDER OF THE AIRCRAFT WAS FELT WITH A SIMULTANEOUS ENGINE FAIL LIGHT ILLUMINATION. A REJECTED TAKEOFF WAS ACCOMPLISHED. AIRCRAFT WAS TAXIED BACK TO RAMP, WITH MAINTENANCE PERSONNEL IN COCKPIT. THE NR 2 ENGINE WAS ANov 1, 1995 · N209FE · Boeing 7272S2F · Engine (Turbine/Turboprop)SDR 95FDEA1571Pitot Tube · blockedFIRST OFFICER'S AIR SPEED FAILED. FOUND PILOT TUBE BLOCKED. REMOVED BLOCKAGE, CHECKED INDICATION WITH BARFIELD TESTER AND OK FOR SERVICE.Oct 20, 1995 · N207FE · Boeing 7272S2F · Pitot/Static SystemSDR 95FDEA01540Turbine · failedABORT ON RUNWAY FOR ENGINE FAILURE ABOUT 80K, #2 ENG MAXIMUM POWER T/O. FOUND NR 2 ENG TURBINE FAILURE. REMOVED NR 2 ENG AS PER WORKCARD 70T0002, INSTALLED NR 2 ENG PER WORKCARD 70T0002. COMPLIED WITH HOOKUPS OPERATIONAL AND LEAK CHECKS PER WORKCARD 70T0002Oct 13, 1995 · N216FE · Boeing 7272S2F · Turbine SectionSDR 95FDEA01203Te Skin · delaminatedDELAM ON TRAILING EDGE OF NR 5 SPOILER. REPAIRED NR 5 SPOILER IAW FEDEX SRM 51-40-6.Aug 28, 1995 · N215FE · Boeing 7272S2F · SpoilersSDR 95FDEA01202Fitting · corrodedCENTER ENGINE REAR SUPPORT FITTING ASSEMBLY IS BADLY CORRODED. REMOVED AND REPLACED CENTER ENGINE REAR SUPPORT FITTING IAW FEDEX SRM 51-30-2, 51-30-4 AND FEDEX MM 71-21-1.Aug 28, 1995 · N215FE · Boeing 7272S2F · Engine Mount SectionSDR 95FDEA01125Floor Beam · double drilledWHILE WORKING NRO0070 FOUND MECHANICAL DAMAGE AND DOUBLE HOLES IN FLOOR BEAM BS 344 RBL 35 - 55 WL 208. REMOVED EXISTING FLOOR BEAM, REPAIRED AND INSTALLED FABRICATED FLOOR BEAM AT BS 344 WL 208 RBL 35 - 55 PER FEDEX SRM 51-10-1, 53-10-2. MFG P/N M446204.Aug 15, 1995 · N203FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 95FDEA01103Floorbeam · double drilledWHILE WORKING NR O0070, FOUND MECHANICAL DAMAGE AND DOUBLE HOLES IN FLOORBEAM BS 344 RBL 35 TO 55 WL 208. REMOVED EXISTING FLOORBEAM, REPAIRED AND INSTALLED FABRICATED FLOORBEAM AT BS 344 WL 208 RBL 35 TO 55 PER FEDEX SRM 51-10-1, 53-10-2.Aug 15, 1995 · N203FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 95FDEA01065Fire Bottle · dischargedGDL - APU LEFT ON THROUGH T/O AND CLIMBOUT, FIRE WARNING LIGHT AND BELL AT APPROX FL 190 TO 200. FIRE HANDLE PULLED, LIGHT WENT OUT IMMEDIATELY AND BOTTLE DISCHARGED. ALL PROCEDURES IN RED TAB'S COMPLIED WITH, FIRE WARNING CIRCUIT TESTEDAND CHECKED GOOD. APAug 2, 1995 · N215FE · Boeing 7272S2F · Fire Bottle, FixedSDR 95FDEA00320Heat Valve · failedGDL - NR 2 FUEL HEAT VALVE STUCK OPEN. FOLLOWED PROCEDURE, SHUT NR 2 ENG DOWN. REMOVED AND REPLACED FUEL HEAT ANTI-ICE VALVE, PER MM 73-14-11 PG 401, OPS CHECKED GOOD, OK FOR SERVICE. A/C DIVERTED TO GDL DUE PRECAUTIONARY NR 2 ENG SHUTDOWN.Mar 21, 1995 · N206FE · Boeing 7272S2F · Fuel HeaterSDR 95FDEA00246Oil Temp Bulb · failedNR 2 ENG OIL TEMP IND 150 AFTER TAKEOFF WE REDUCED PWR TO 1.43 75 PERCENT N1, 350 EGT 82 N2. AFTER 15 MIN ENG OIL TEMP 140. ENG SHUTDOWN WAS ACCOMPLISHED IAW. CHECKLIST. AFTER PWR REDUCTION CSD TEMP DECREASED FROM 118 TO 80 DEG CELSIUS. REMOVED AND REPLACMar 15, 1995 · N206FE · Boeing 7272S2F · Engine Oil TemperatureSDR 95FDEA00134Light · failedSMOKE COMING FROM ENGINEERS FLUORESCENT LIGHT, THIS IS A REPEAT WRITE UP. FOUND FLT ENGINEER'S RT AFT TABLE LIGHT BAD, WITH A BURNT ODOR FROM LIGHT. REMOVED AND REPLACED SAME. OPS CHECKS NORMAL AS PER MM 33-10.Feb 10, 1995 · N201FE · Boeing 7272S2F · Flight Compartment LightingSDR 95FDEA00115Light · smokingSMOKE WAS COMING FROM FLUORESCENT LIGHT AND RIGHT TABLE LIGHT AREA. PULLED C/B FOR F/E TABLE FLUORESCENT LIGHT FIXTURE. NO FURTHER SMOKE, TIGHTENED LOOSE WIRE.Feb 7, 1995 · N201FE · Boeing 7272S2F · Flight Compartment LightingSDR 95FDEA00104Rib · crackedHFECI OF FASTENER HOLES AT BS 760 LBL 70.5 SHOW CORROSION THROUGHOUT ALL SIX HOLES. TOP FWD HOLE IS CRACKED IN RIB CHORD, AND BOTTOM HOLE HAS A CRACK IN THE RIB CHORD. REPAIRED FASTENER HOLES AT BS 760 LBL 70.5 PER FEDEX EA 7-5710-23684.Jan 29, 1995 · N205FE · Boeing 7272S2F · Wing, Rib/BulkheadSDR 95FDEA00103Rib · crackedHFECI OF FASTENER HOLES AT BS 760, RBL 70.5 SHOW CORROSION THROUGHOUT ALL SIX HOLES. TOP FWD HOLE IS CRACKED THREE PLACES IN RIB CHORD, AND BOTTOM FWD HOLE HAS A CRACK IN THE RIB CHORD. REPAIRED FASTENER HOLES AT BS 760, RBL 70.5 PER FEDEX EA 7-5710-2368A.Jan 29, 1995 · N205FE · Boeing 7272S2F · Wing, Rib/BulkheadSDR 95FDEA00094Seat Track · corrodedSEAT TRACK HAS MECHANCIAL DAMAGE ON TOP SURFACE BS 517-523, BL O, WL 209. BLENDED DAMAGE, IT WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK BS 360-550, BL O, WL 208 IAW SRM 53-10-2.Jan 25, 1995 · N205FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00093Seat Track · damagedSEAT TRACK HAS MECHANICAL DAMAGE ON TOP SURFACE OF BS 523 RBL 45 WL 209. REMOVED FABRICATED AND INSTALLED SEAT TRACK IAW SRM 53-10-5.Jan 25, 1995 · N205FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR 95FDEA00082Skin · damagedDENT WITH GOUGE 1 INCH W BY 1.5 INCH L BY .075 INCH D, BS 1284, JUST ABOVE STR 22R FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGE AREA IN ACCORDANCE WITH FEDEX SRM 53-30-3 FIG 1 AT BS 1284 STR 22R.Jan 23, 1995 · N205FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 95FDEA00004Window · crackedR-2 WINDOW FAILED WHILE IN CRUISE AT FL 350 AND CABIN DIFF PRESS OF 8.4 PSI DESCENDED TO FL 240 AND REDUCED CABIN PRESS TO 5.0 PSI. APPEARS TO BE INNER PANE. REMOVED AND REPLACED NR 2 SLIDING WINDOW PER MM 56-12-11.Jan 4, 1995 · N205FE · Boeing 7272S2F · Flight Compartment Windows
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