Boeing 727-2S2F

Service difficulty reports · 842

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 = '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 VGCA20250805002Skin Panel · corrodedAFT LOWER FUSELAGE SKIN PANEL CORROSION FROM BS1148-1166 AND S-18L TO S-20L.Aug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR VGCA20250805001Keelbeam · corrodedCENTER FUSELAGE SECTION RH DELTA BEAM LOWER CHORD CORRODED FROM BS720F-755 AND S-27L TO S-27RAug 5, 2025 · N216WE · Boeing 7272S2F · Fuselage Main, KeelSDR VGCA20230323001Gearbox · leaking#2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO LOW OIL PRESSURE. FOUND LOOSE FASTENER ON MAIN ACCESORY GEARBOX CAUSING OIL LOSS.Mar 23, 2023 · N215WE · Boeing 7272S2F · Engine Oil PressureSDR VGCA20230213002Stub Frame · damagedMISSDRILLED HOLES IN VERTICAL FLANGE OF LEFT STUB BEAM LOWER CHORD PART NUMBER 65-86355-3 AT STATION 783.95Feb 13, 2023 · N215WE · Boeing 7272S2F · Fuselage Main, FrameSDR VGCA20230213001Frame · scratchedDAMAGED HOLE / DEEP SCRATCH AT THE LOWEST HOLE OF THE INBOARD CHORD OF THE LH FRAME PART NUMBER 65-16326-139 AT STATION 783.95Feb 13, 2023 · N215WE · Boeing 7272S2F · Fuselage Main, FrameSDR VGCA20211113001None · noneDURING CLIMB WHILE PASSING THROUGH FL250 THE AIRCRAFT EXPERIENCED A RAPID DECOMPRESSON THAT WAS NOT CONTROLLABLE FROM THE FLIGHT DECK. EMERGENCY DECENT WAS INITATED AND AIRCRAFT RETURNED WITHOUT FURTHER INCIDENTNov 13, 2021 · N216WE · Boeing 7272S2F · Cabin Pressure Control SystemSDR VGCA20201028001Proximity Sensor · intermittentDURING APPROACH WITH THE GEAR SELECTED DOWN, LEFT GEAR UNSAFE LIGHT ILLUMINATED WITH NO GREEN LIGHT. NOSE AND RIGHT GEAR INDICATE SAFE. DOORS LIGHT INDICATES NORMAL. MANUAL CRANKING OF THE LEFT GEAR WAS NORMAL AND INDICATED DOWN AND LOCKED WITH THE MECHANICOct 28, 2020 · N215WE · Boeing 7272S2F · Landing Gear Position and WarningSDR VGCA202009098302Floorbeam · corrodedCORROSION ON FLOOR BEAM LOWER FLANGE AT STATION 950D LBL 20.Aug 31, 2020 · N215WE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR VGCA2020090983101Spar · corrodedCORROSION ON WING CENTER SECTION FRONT SPAR LOWER CHORD BETWEEN LBL 3.25 AND RBL 10.25.Aug 31, 2020 · N215WE · Boeing 7272S2F · Wing SparSDR VGCA2020072016001Cabin Pressure · abnormalLOST CABIN PRESSUURIZATION AT FLIGHT LEVEL 30000, CABIN ALTITUDE WARNING HORN SOUNDED AT 10000 FEET CABIN PRESSURE. UNABLE TO CONTROL CABIN PRESSURE WITH OUTFLOW VALVE CLOSED.Jul 16, 2020 · N216WE · Boeing 7272S2F · Cabin Pressure Control SystemSDR VGCA2020041309007Seat Track · gougedSEAT TRACK GOUGED IN MAIN CARGO DEK FLOOR AT BS. 625, RBL 62.5. FOUND BEYOND ALLOWABLE DAMAGE. SEGEMENT OF SEAT TRACK REPLACED IN ACCORDANCE WITH B727 SRMApr 9, 2020 · N216WE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR VGCA2020041309006Pressure Panel · puncturedPRESSURE PAN WEB PUNCHTURED BETWEEN BS. 880 - 890 AND LBL. 48 - 68 AT MAIN CARGO DECK FLOOR. REPLACED WITH PART IN ACCORDANCE WITH B727 SRM.Apr 9, 2020 · N216WE · Boeing 7272S2F · Fuselage Main, StructureSDR VGCA2020041309005Pressure Panel · puncturedPRESSURE PAN WEB PUNCTURED BETWEEN BS. 880 - 890 AND RBL. 48 - 68 AT MAIN CARGO DECK FLOOR. REPLACED WITH NEW PART IN ACCORDANCE WITH B727 SRMApr 9, 2020 · N216WE · Boeing 7272S2F · Fuselage Main, StructureSDR VGCA2020041309004Seat Track · crackedSEAT TRACK FLANGE CRACKED IN MAIN CARGO DECK FLOOR AT BS. 870, LBL, 62.5. FOUND BEYOND ALLOWABLE DAMAGE. SEAT TRACK SEGMENT REPLACED IN ACCORDANCE WITH B727 SRM.Apr 9, 2020 · N216WE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR VGCA2020041309003Seat Track · gougedSEAT TRACK FLANGE GOUGED IN MAIN CARGO DECK FLOOR AT BS. 870, LBL 45.5. FOUND BEYOND ALLOWABLE DAMAGE. SEAT TRACK SEGMENT REPLACED IN ACCORDANCE WITH B727 SRM.Apr 9, 2020 · N216WE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR VGCA2020041309002Panel · dentedHORIZONTAL STABILIZER LH SIDE LEADING EDGE PANEL #9122 REWORKED (BLEND OUT) DENT FOUND BEYOND ALLOWABLE DAMAGE, REPAIRED IN ACCORDANCE WITH B727-200 SRMApr 9, 2020 · N216WE · Boeing 7272S2F · Horizontal Stabilizer, Plate/SkinSDR VGCA2020041309001Web · crackedWEB TANGS CRACKED AT BS. 600 AND BS 620 BETWEEN STR. 3L AND STR. 4L, ABOVE MAIN CARGO DOOR. PART REPLACEMENT REQUIRED.Apr 9, 2020 · N216WE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR VGCA20180108001Locking Plate · corrodedWHILE GAINING ACCESS TO PERFORM AD 2008-22-12F, FOUND THE HORIZONTAL STABILIZER HINGE BEARING RETAINER LOCKING PLATE HAD A BROKEN BOLT. REMOVED THE STABILIZER TO REPLACE THE BROKEN BOLT, DISCOVERED SURFACE CORROSION ON RH ATTACH FITTING.Jan 8, 2018 · N215WE · Boeing 7272S2F · Horizontal Stabilizer StructureSDR 2017FA0000453Engine · detachedDURING THE LANDING ROLL, THE NR 3 ENGINE SEPARATED COMPLETELY FROM THE FUSELAGE, AFTER THRUST REVERSE APPLICATION AND DEPLOYMENT. THE ENGINE FELL TO THE RUNWAY. THE ACFT HAD FLOWN 78 HOURS AND 48 CYCLES BEFORE THIS OCCURRENCE.Sep 26, 2016 · N209FE · Boeing 7272S2F · Engine (Turbine/Turboprop)SDR VGCA20150901001Light · dimCOCKPIT EMER EXIT LIGHTS DIM. REPLACED EMER EXIT LIGHT UNIT.Sep 1, 2015 · N216WE · Boeing 7272S2F · Emergency LightingSDR VGCA20150526001Web · crackedDURING THE UNRELATED ACCOMPLISHMENT OF AD 2014-21-09 PARAGRAPH H DISCOVERED BOTH LT & RT WEB OF ELEVATOR QUADRANT ASSEMBLIES CRACKED. R & R BOTH WEBS.May 26, 2015 · N215WE · Boeing 7272S2F · Elevator Miscellaneous StructureSDR VGCA20150413001A/C Pack · overheatedAIR CONDITIONING PACK OVERHEAT.Apr 13, 2015 · N215WE · Boeing 7272S2F · Cabin Cooling SystemSDR VGCA20140620001Service Panel · departedNUMBER 1 ENG VIBRATION IN FLIGHT, AFTER LANDING PERFORMED WALK AROUND AT WHICH POINT DISCOVERED THE LT HYD ACCESS PANEL MISSING & DENT IN LT INLET COWLING RESULTING IN SUSPECTED FOD DAMAGE.Jun 20, 2014 · N216WE · Boeing 7272S2F · Hydraulic Compartment DoorsSDR VGCA20140609001Skin · dentedFUSELAGE SKIN DENTED BETWEEN STATIONS 344 & 351 LT ABOVE STRINGER 19L.Jun 9, 2014 · N215WE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR VGCA20140605001Skin · damagedSUSPECTED LIGHTNING STRIKE ON RIVET AT STATION 680, STRINGER 3L RESULTING IN FUSELAGE SKIN DAMAGE.Jun 5, 2014 · N215WE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR VGCA20140425001Slat · damagedRIGHT HAND SLAT TE NR 5 DAMAGED.Apr 25, 2014 · N216WE · Boeing 7272S2F · Leading Edge DevicesSDR FDEA201307051482Light · inoperativeON SERVICE CHECK, FOUND L1 DOOR EXIT LIGHT INOPERATIVE. R & R L1 DOOR EMERGENCY LIGHT, REF AMM 33-50-101-2. OPS CHECKED GOOD. ACFT OK TO CONTINUE.Jul 5, 2013 · N204FE · Boeing 7272S2F · Emergency LightingSDR FDEA201305060923Battery Pack · inoperativeFOUND EMERGENCY LIGHT ABOVE MAIN ENTRY DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW MM 33-50-101-2. OPS CHECKED NORMAL. OK FOR SERVICE.May 6, 2013 · N204FE · Boeing 7272S2F · Emergency LightingSDR FDEA201303010488Transmitter · malfunctionedDURING FLAP RETRACTION, SYS A PRESSURE DECREASED TO APROX 1000 PSI FROM FLAPS 5 -2 PRESSURE DECREASED. ENG 1 A PUMP LIGHT ILLUMINATED INT AND WITH FLAP RETRACTION SYS A QTY WAS JUST UNDER 1 GAL, COMPLIED WITH QRH RETURNED IND. INSPECTED ACFT FOR LEAKS, NO Mar 1, 2013 · N204FE · Boeing 7272S2F · Hydraulic Indicating SystemSDR FDEA201212114278Attach Fitting · crackedFOUND A CRACK ABOUT 7MM IN LENGTH AT FLANGE RADIUS OF AFT CARGO COMPARTMENT DOOR ACTUATOR ATTACH FITTING. REPLACED THE ATTACH FITTING IAW SRM 51-40-21.Dec 11, 2012 · N210FE · Boeing 7272S2F · Fuselage Main, Attach FittingsSDR FDEA201212114315Slide · dislodgedDURING CLOSING FORWARD ENTRY DOOR, ESCAPE SLIDE DROPPED OUT FROM BOTTOM OF RETAINING CASE. REINSTALLED ENTRY DOOR SLIDE IAW AMM 25-60-015-2. CHECKS GOOD FOR SECURITY.Dec 11, 2012 · N213FE · Boeing 7272S2F · Escape SlideSDR FDEA201212054249Module · malfunctionedCLIMBING THROUGH 4000' MSL LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, RAN QRH LIGHT DID NOT EXTINGUISH, RTB. LIGHT DID NOT EXTINGUISH UNTIL IN CHOCKS, SHUTTING DOWN ALL ENGINES. R & R OVERHEAT PROTECTION MODULE IAW SMP, PERFORMED TEST IAW MM REF. 26-14-000-Dec 5, 2012 · N213FE · Boeing 7272S2F · Overheat DetectionSDR FDEA201211073901Battery Pack · inoperativeEMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR DOES NOT ILLUMINATE DURING BATTERY AND STANDBY POWER CHECK. R & R BATTERIES IN EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR IAW AMM 33-50-101-2, OPS CHECKED GOOD.Nov 7, 2012 · N204FE · Boeing 7272S2F · Emergency LightingSDR FDEA201209293509Blades · damagedDURING CRUISE FLIGHT, NR 2 ENGINE THROTTLE LEVER BEGAN VIBRATING WITH ASSOCIATED MILD ACFT VIBRATION FELT. RAN QRH AND REDUCED NR 2 THROTTLE TO IDLE. SHORTLY AFTER REACHING, NR 2 ENGINE EXCELLERATED TO 92 PERCENT N2 AND REMAINED THERE WITH THROTTLE LEVER ASep 29, 2012 · N203FE · Boeing 7272S2F · Turbine SectionSDR FDEA201209293512Hinge · damagedLOUD SQUEL COMING FROM AREA UPPER FRONT SIDE OF COCKPIT NEXT TO S/O PANEL. CLOSING CARGO OUTFLOW VALVE HAS NO EFFECT. STARTED DURING CLIMB AROUND 250. WENT AWAY AT LEVEL OFF AT 350 THEN IMMEDIATELY CAME BACK. CONTINUED TO 370. ALL PRESSURIZATION INDICATISep 29, 2012 · N204FE · Boeing 7272S2F · Passenger/Crew DoorsSDR FDEA201208183072Battery Pack · failedL1 DOOR EMERGENCY EXIT LIGHTS LT SIDE, LIGHT INOPERATIVE. BATTERY PACK ONLY READS 1.3VDC, REMOVED AND REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY LIGHTS. OPS CHECKED NORMAL IAW MM 33-50-051-2.Aug 18, 2012 · N204FE · Boeing 7272S2F · Emergency LightingSDR FDEA201208042837Guide · out of adjustON BLOCK-IN, CAPTAIN OPENED SLIDING WINDOW TO TALK TO GROUND CREW. UNABLE TO CLOSE. TROUBLESHOT DOWN TO FWD AND AFT GLIDES. ADJUSTED AND TESTED L2 CAPT'S SLIDING WINDOW IAW MM56-12-011-5. OPS NORMAL.Aug 4, 2012 · N211FE · Boeing 7272S2F · Flight Compartment WindowsSDR FDEA201207282730Pin · out of adjustON PREFLIGHT, CAPTAIN`S SLIDING WINDOW WILL NOT CLOSE. ADJUSTED GUIDE PIN IAW MM 56-12-011-5. OPS CHECKED NORMAL.Jul 28, 2012 · N211FE · Boeing 7272S2F · Flight Compartment WindowsSDR FDEA201207282729Bottle · dischargedLEFT "BOTTLE DISCHARGED" LIGHT ILLUMINATED ON OVERHEAD PANEL. R & R LT ENGINE FIRE EXTINGUISHER BOTTLE IAW MM 26-21-001-4 AND PERFORMED INSPECTION CHECK IAW MM26-21-001-6. OPS NORMAL.Jul 28, 2012 · N204FE · Boeing 7272S2F · Extinguishing SystemSDR FDEA201206142233Attach Fitting · wornOPEN RT ATTACH FITTING FOR L1 DOOR THAT HOLD ESCAPE SLIDE HAS ONE OF THE FITTINGS WORN. OTHER SIDE SNAPS IN WORN FITTING. HOLDS ROD IN WITH NO RESTRAINT. REMOVED AND STOWED SLIDE IAW MM 25-60-015-2, PART 2A, 2B. REPLACED GIRT BAR RETAINING CLIPS ON COVER Jun 14, 2012 · N211FE · Boeing 7272S2F · Emergency EquipmentSDR FDEA201206142244Position Switch · failedRETRACTING FLAPS FROM 5 TO 2 DEGREES, AMBER L/E FLAPS LIGHT STAYED ON. S/O POSITION TEST SELECTOR SHOWED NR 2 KREGER FLAP OUT. COMPLIED WITH QRH. NO HELP. RETURNED TO DEPARTURE. R & R FLAP POSITION SWITCH IAW AMM 27-82-0001-4. OPS CHECKED GOOD.Jun 14, 2012 · N211FE · Boeing 7272S2F · Leading Edge Slat Control SystemSDR FDEA201206062104Door · out of adjustON LANDING, FWD ENTRY DOOR LIGHT ILLUMINATED ON S/O PANEL VISUAL INSPECTION, DURING SHUTDOWN VERIFIED FWD ENTRY DOOR WAS SLIGHTLY AJAR. ADJUSTED UPPER LINK ARM AND ALIGNED TORQUE TUBES REF 52-11-001-5. START WITH C. STEP (8). ADJUSTED IAW STEP 3. FORWARDJun 6, 2012 · N204FE · Boeing 7272S2F · Passenger/Crew DoorsSDR FDEA201206022057Warning Light · false activationON LANDING, FWD ENTRY DOOR LIGHT ON S/O PANEL ILLUMINATED. VISUAL INSPECTION DURING SHUTDOWN, CHECKLIST VERIFIED FWD ENTRY DOOR WAS SLIGHTLY AJAR. OPS CHECK OF FWD ENTRY DOOR WARNING SWITCH CHECKED GOOD REF AMM CH 52-70-001-5.Jun 2, 2012 · N204FE · Boeing 7272S2F · Door Warning SystemSDR FDEA201206012042Slide · dislodgedEVACUATION SLIDE FELL OUT OF ITS CONTAINER. STOWED L1 DOOR ESCAPE SLIDE IAW AMM 25-60-015-2.Jun 1, 2012 · N211FE · Boeing 7272S2F · Escape SlideSDR FDEA201205312036Slide · dislodgedEVACUATION SLIDE FELL OUT OF ITS CONTAINER. STOWED L1 DOOR ESCAPE SLIDE PER AMM 25-60-015-2.May 31, 2012 · N211FE · Boeing 7272S2F · Escape SlideSDR FDEA201205302014Door · out of adjustDURING CLIMB, PASSING 2000 AGL. FWD ENTRY ANNUNCIATOR LIGHT ON, SO PANEL ANNUNCIATED. RAN QRH. INSPECTED DOOR HANDLE AND LIGHT EXTINGUISHED. PRESSURIZATION OK THROUGHOUT. CONTINUED IAW QRH. FOUND LT ENTRY DOOR NOT LATCHING IN DETENT. ADJUSTED DOOR TO COMay 30, 2012 · N204FE · Boeing 7272S2F · Passenger/Crew DoorsSDR FDEA201205231937Door · out of adjustFWD ENTRY DOOR HANDLE MOVED SLIGHTLY TOWARD OPEN DURING LANDING AND FWD ENTRY DOOR LIGHT ILLUMINATED. ADJUSTED FWD ENTRY DOOR FOR SOFT UNLATCHING AND OPS CHECKED FWD ENTRY DOOR OK IAW MM 52-11-001-5.May 23, 2012 · N204FE · Boeing 7272S2F · Passenger/Crew DoorsSDR VGCA20120521006Keelbeam · corrodedCORROSION ON LWR INBD FLANGE OF STR 28R AND 28L FWD OF DELTA KEEL AT STA 740.May 21, 2012 · N215WE · Boeing 7272S2F · Fuselage Main, KeelSDR VGCA20120521005Floorbeam · corrodedCORROSION ON FWD CARGO PIT FLOOR SUPPORT STA 537 RBL8 AND RBL13.May 21, 2012 · N215WE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR VGCA20120521004Keel · corrodedCORROSION ON KEEL LT SIDE BESIDE STA 740.May 21, 2012 · N215WE · Boeing 7272S2F · Fuselage Main, Keel
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