N815EA, cancelled May 19, 2023

Service difficulty reports · 70

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N815EA' AND deregistration_id = 'N815EA-2023-05-19'
  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 C8GA2012011800002Window · crackedDURING CRUISE OPERATION THE R1 WINDOW BEGAN ARCING AND GLOWING RED. WHILE DESCENDING, THERE WAS A LOUD BANG AND NOTED THAT THE WINDOW HAD CRACKED. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED WITHOUT INCIDENT. R & R THE R1 WINDOW AND WINDOW HEAT CONTROLLERJan 18, 2012 · N815EA · Boeing 727225 · Flight Compartment WindowsSDR FOTR2101904252Skin · damagedLIGHTNING STRIKE REPAIR AT FUSELAGE SKIN STATION 720B+13 BETWEEN STRINGER 17-18 LT. REMOVED BLIND FASTENER AT FUSELAGE SKIN STATION 720B+13 BETWEEN STR. 17-18 LT IAW SRM 51-30-2. HFEC AREA IAW NDTM 51-00-00 FIGURE 23 PART 6 WITH NO DEFECTS NOTED. INSTALLED FFeb 25, 2011 · N815EA · Boeing 727225 · Fuselage Main, Plate/SkinSDR FOTR2101904448Skin · dentedEVALUATE EXISTING DENT AT FUSELAGE SKIN STATION 364 BETWEEN STRINGER 23-24 RT. REMOVED PREVIOUS REPAIR FROM BS364 STR. 23-24 RT IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER FROM 2024T3 .071 PO 90010841 DIM. 8.5" X 11" AND FABRICATED NEW STRUCTURAL FILLERFeb 25, 2011 · N815EA · Boeing 727225 · Fuselage Main, Plate/SkinSDR FOTR2101904238Skin · damagedEVALUATE EXISTING LIGHTNING STRIKE REPAIR AT FUSELAGE SKIN STATION 506 BETWEEN STRINGER 24-25 LT. REMOVED BLIND FASTENER AT FUSELAGE SKIN STATION 506 IAW SRM 51-30-2. HFEC AREA IAW NDTM 51-00-00 FIGURE 23 PART 6 WITH NO DEFECTS NOTED. INSTALLED FASTENER IAW SFeb 25, 2011 · N815EA · Boeing 727225 · Fuselage Main, Plate/SkinSDR FOTR2101904027Skin · damagedEVALUATE EXISTING LIGHTNING STRIKE REPAIR AT FUSELAGE SKIN STATION 296 BETWEEN STRINGER 26-25 LT. REMOVED BLIND FASTENER AT FUSELAGE SKIN STATION 296 BETWEEN STRINGER 26-25 LT IAW SRM 51-30-2. HFEC AREA IAW NDTM 51-00-00 FIGURE 23 PART 6 WITH NO DEFECTS NOTEFeb 25, 2011 · N815EA · Boeing 727225 · Fuselage Structure (General)SDR FOTR2101904249Skin · damagedEVALUATE EXISTING LIGHTNING STRIKE REPAIR AT FUSELAGE SKIN STATION 720A BETWEEN STRINGER 18-19 LT. REMOVED BLIND FASTENER AT FUSELAGE SKIN STATION 720A BETWEEN STRINGER 18-19 LT IAW SRM 51-30-2. HFEC AREA IAW NDTM 51-00-00 FIGURE 23 PART 6 WITH NO DEFECTS NOTFeb 25, 2011 · N815EA · Boeing 727225 · Fuselage Main, Plate/SkinSDR FOTR2101904250Skin · damagedEVALUATE EXISTING LIGHTNING STRIKE REPAIR @ FUSELAGE SKIN STA. 720B+3 AND 702B+4 BETWEEN STR. 18-19 L/H.... REMOVED BLIND FASTENER @ FUSELAGE SKIN STA 720B+3 AND 720B+4 IAW B727 SRM 51-30-2. HFEC AREA IAW N727 NDTM 51-00-00 PART 6 FIGURE 23 WITH NO DEFECTS NOTFeb 25, 2011 · N815EA · Boeing 727225 · Fuselage Main, Plate/SkinSDR FOTR2101904396Seat Track · corrodedSTA 865, LBL 24 AND LBL 45, SEAT TRACK FLANGE CORRODED. REMOVED SEAT TRACK FLANGE AT STA 865, LBL24 AND LBL45 IAW SRM 51-30-2. FABRICATED 2 EA NEW PARTS FROM BAC1520-1466 7178T6511, EXTRUSION PO NR 20126164 DIM 20" X 3.5" IAW SRM 53-10-2 FIG 7 AND INSTALLED Feb 21, 2011 · N815EA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR2101903914Skin · bentPREVIOUS REPAIR ON RT WING INBD FLAP, INBD END BENT, WBL 70. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR PART FROM 2024T3 .063 DIM 2.5" X 2" PO 90010689 IAW SRM 57-50-4 AND 57-50-2. INSTALLED REPAIR PART IAW SRM 51-30-2 AND 57-50-4. FASI NRFeb 21, 2011 · N815EA · Boeing 727225 · Trailing Edge FlapsSDR FOTR2101904393Frame · dentedAFT CARGO COMPARTMENT, FRAME DENTED BETWEEN 25R-26R, BS 1010. CUTOUT DAMAGED AREA DIM. 1" X 1.25" IAW SRM 51-40-3, FIG 1. FABRICATED REPAIR FRAME FROM 7075-0 .063 PO 90010872, DIM 18" X 3.75" IAW SRM 51-40-3, FIG 1 AND 53-10-2 FIG 5. HEAT TREATED PART TO 70Feb 21, 2011 · N815EA · Boeing 727225 · Fuselage Main, FrameSDR FOTR2101904392Frame · dentedAFT CARGO COMPARTMENT, FRAME DENTED BETWEEN STRINGER 25L-26L BS 1090 CUTOUT DAMAGED AREA 1" X 1.25" IAW SRM 51-40-3, FIG 1. FABRICATED REPAIR FRAME FROM 7075-0 .063 PO 90010872, DIM 17.75" X 3.75" IAW SRM 51-40-3, FIG 1 AND 53-10-2, FIG 5. HEAT TREATED REPAIFeb 21, 2011 · N815EA · Boeing 727225 · Fuselage Main, FrameSDR FOTR2101903974Cover · crackedLT WING L/E NR 2 SLAT TRACK COVER CRACKED. (OTBD TRACK) STOP DRILLED CRACK ON NR 2 SLAT IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 7075T6 .080" PO 9007282 DIM. 6.2" X 7.1" IAW SRM 57-50-3. INSTALLED DOUBLER IAW SRM 57-50-3, FIG 1 AND 51-30-2. FASI NR Feb 21, 2011 · N815EA · Boeing 727225 · Leading Edge DevicesSDR FOTR2101904218Frame · gougedFRAME AT STA 660 BETWEEN STR 6R AND STR 7R IS GOUGED. REMOVED DAMAGED AREA OF FRAME IAW SRM 51-10-1, DIM 1.5" X 1.5". FABRICATED 2 EA CHANNELS 12" X 3" FROM 7075-0 .063 IAW SRM 53-10-4. HEAT TREATED CHANNELS TO 7075T6 IAW FAS ENG REPORT NR 237153-801A AND Feb 21, 2011 · N815EA · Boeing 727225 · Fuselage Main, FrameSDR FOTR2101904217Frame · gougedFRAME AT STA 640 STR 6R IS GOUGED AND DENTED. REMOVED DAMAGED AREA OF FRAME 1.5" X 1.5" IAW SRM 51-10-1. FABRICATED CHANNEL 2 EA 12" X 3" FROM 7075-0 .063 PO 90010872 IAW SRM 53-10-4. HEAT TREATED TO 7075T6 IAW FAS ENG REPORT NR 237153-801A. INSTALLED REPAIFeb 21, 2011 · N815EA · Boeing 727225 · Fuselage Main, FrameSDR FOTR2101903892Skin · chafedLWR T/E INTERIOR LIP OF NR 8 SLAT CHAFED ALONG LENGTH OF SLAT. BLENDED CHAFED AREA ORIG MAT .070 WITH .039 REMAINING AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-1 AND 57-50-1 FIG 2. FABRICATED DOUBLER FROM 2024T3 .080 DIM. 6" X 4" PO 90010831 IAW SRM 57-50-3Feb 21, 2011 · N815EA · Boeing 727225 · Leading Edge DevicesSDR FOTR2101904400Skin · debondedLT WING T/E NR 6 SPOILER UPPER SKIN IS DISBONDED. REMOVED DAMAGE APPROX 13" X 5.5" AND CLEANED AND PREPPED AREA IAW SRM 51-40-20, PG 12-14 PARA 7.FABRICATED REPAIR FILLER, DIM 13" X 5.5" FROM 7075T6 .025 PO 9009504 AND DOUBLER 16" X 7" FROM 7075T6 .025 PO 90Feb 21, 2011 · N815EA · Boeing 727225 · SpoilersSDR FOTR2101904371Stringer · dentedFWD PIT LT SIDE STR 25L HAS A DENT AT BS 508. CUTOUT DAMAGED STRINGER DIM. 2.1" LONG. FABRICATED HAT CHANNEL FROM BAC1498-140 7075T6 PO 2101970 DIM 2.1" LONG. FABRICATED "U" CHANNEL FROM BAC1493-412 7075T6, PO 290435 DIM. 10.7" LONG. FABRICATED 2 EA ANGLES Feb 21, 2011 · N815EA · Boeing 727225 · Fuselage Main, Longeron/StringerSDR FOTR2101904166Seat Track · corrodedCABIN SEAT TRACK AT BS 480-720B, LBL 24.5 HAS HEAVY CORROSION IN SEVERAL AREAS OVER ENTIRE LENGTH. REMOVED CORROSION ON SEAT TRACK LBL 24, BS 480-720B AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-1, 53-10-1, FIG 3. REMOVED SEAT TRACK IAW SRM 51-30-2, FABRICATFeb 21, 2011 · N815EA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR2101904399Skin · debondedLT WING NR 1 SPOILER UPPER SKIN IS DEBONDED. REMOVED DAMAGE, CLEANED AND PREPPED AREA IAW SRM 51-40-20, PARA 7,11 AND 14. FABRICATED FILLER DIM 24" X 7" .025 AND DOUBLER 25.5" X 9" .025 FROM 7075T6 PO 9009504 IAW SRM 51-40-20, PARA 8,10,11,14 AND SRM 57-50-2Feb 21, 2011 · N815EA · Boeing 727225 · SpoilersSDR FOTR2101904398Skin · debondedRT WING T/E NR 10 SPOILER UPPER SKIN IS DEBONDED. REMOVED DAMAGE, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20, PARA 7, 11, 14, 15, AND 18. FABRICATED REPAIR FILLER 13.5" X 3.5" AND DOUBLER 15" X 5" FROM 7075T6 .025 PO 90010605 IAW SRM 51-40-20, PARA 8.Feb 21, 2011 · N815EA · Boeing 727225 · SpoilersSDR C8GA2010000073Indicator · malfunctionedON TAKEOFF ROLL, THE NR1 EPR INDICATION PEGGED. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE BLOCKS. HIGH ENERGY INSP WAS PERFORMED. R & R THE NR1 EPR INDICATOR, OPS CHECK GOOD. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.Nov 10, 2010 · N815EA · Boeing 727225 · Engine Pressure Ratio (EPR)SDR C8GA20090075Pump · faultyFLT 720 FROM TOL TO ATL, DURING CLIMB-OUT THE NR 2 ENGINE FUEL FLOW BECAME ERRATIC, THE N1 AND N2 STARTED WINDING DOWN FOLLOWED BY COMPRESSOR STALL. THE NR 2 ENGINE WAS SHUT DOWN, EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO TOL WHERE IT LANDED WITHOUT IMay 13, 2009 · N815EA · Boeing 727225 · Engine Fuel PumpSDR C8GA20070003Blades · damagedFLT 1723 FROM BOS TO TOL, DURING CLIMB-OUT, NR 2 ENGINE BEGAN TO VIBRATE AND WAS CONFIRMED WITH THE THROTTLE. ENGINE BEGAN TO COMPRESSOR STALL, ENGINE WAS SHUTDOWN AND AIRCRAFT LANDED WITHOUT INCIDENT IN TOL. POST FLIGHT INSPECTION REVEALED FOD DAMAGE TO THEFeb 16, 2007 · N815EA · Boeing 727225 · Turbine Engine Compressor SectionSDR C8GA20060020Rod · brokenFLT 713 FROM BOS TO ROC, AFTER TAKEOFF AND CLIMBING, THE RIGHT MAIN GEAR DOOR LIGHT REMAINED ON. CYCLED THE GEAR AND THE LIGHT REMAINED ILLUMINATED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT IN BOS. ON POST FLIGHT INSP NOTED THAT THNov 22, 2006 · N815EA · Boeing 727225 · Landing Gear Retraction/Extension SystemSDR C8GA20060006Quick Disconnect · looseFLT 1719 FROM MCO TO ATL, DURING TAKEOFF ROLL, FOR’S AIRSPEED INDICATOR BEGAN TO LAG. AFTER TAKEOFF WHILE CLIMBING, GEAR RETRACTED AND FLAPS RETRACTING FOR’S AIRSPEED INDICATOR WENT TO ZERO. AIRCRAFT RETURNED TO MCO WITHOUT INCIDENT. ON POST FLIGHT FOUND FOMar 28, 2006 · N815EA · Boeing 727225 · Airspeed/Mach IndicatorSDR C8GA20060004Oil Cooler · failedFLT 1707 FROM PHX TO MEM. DURING CLIMBOUT NR 2 ENGINE OIL TEMP BEGAN RISING. INITATED ENGINE SHUT DOWN AS PRECAUTIONARY. EMERGENCY WAS DECLARED, AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. FOUND NR 2 ENGINE OIL COOLER BAD. REMOVED AND REPLACED OMar 2, 2006 · N815EA · Boeing 727225 · Engine Oil CoolerSDR 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 2002F00589Flap · dentedAT C-CHECK, FOUND DENT OUT OF LIMITS ON RIGHT WING INBOARD AFT FLAP. (M)Apr 12, 2002 · N815EA · Boeing 727225 · Trailing Edge FlapsSDR 2002F00588Frame · crackedAT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME, UPPER CHORD, CRACKED AT STATION 580 RBL 3. (M)Apr 3, 2002 · N815EA · Boeing 727225 · Fuselage Main, FrameSDR 2002F00586Floorbeam · crackedAT C-CHECK, FOUND FORWARD CABIN FLOORBEAM CRACKED IN RADIUS 1.5 INCHES LONG AT STATION 326 RBL 24. (M)Apr 2, 2002 · N815EA · Boeing 727225 · Fuselage Main, Floor BeamSDR 2002F00497Floor Support · crackedAT C-CHECK, FOUND AFT PIT FLOOR SUPPORT CRACKED AT STATION 950F LBL 4. (M)Apr 2, 2002 · N815EA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 2002F00496Frame · corrodedAT C-CHECK, FOUND CORROSION ON FRAME AT FORWARD ACCESS COMPARTMENT AFT OF DOOR AT STATION 227. (M)Mar 28, 2002 · N815EA · Boeing 727225 · Fuselage Main, FrameSDR 2002F00495Frame · crackedAT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME CRACKED AT STATION 560 RBL 3. (M)Mar 28, 2002 · N815EA · Boeing 727225 · Fuselage Main, FrameSDR 2002F00494Shear Tie · corrodedAT C-CHECK, FOUND SHEAR TIE CORRODED AT COMPARTMENT FRAME STATION 720A LBL 10. (M)Mar 28, 2002 · N815EA · Boeing 727225 · Fuselage Main, StructureSDR 2002F00477Web · tornAT C-CHECK, FOUND AFT CARGO DOOR CLOSE OUT WEB TORN AT STATION 620 ABOVE STRINGER 26R. (M)Mar 28, 2002 · N815EA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 2002F00476Angle · crackedAT C-CHECK, FOUND L-ANGLE CRACKED BELOW FORWARD CARGO DOOR CUTOUT, FORWARD WEB AT STATION 560 BETWEEN STRINGER 23 AND 24R. (M)Mar 28, 2002 · N815EA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 2002F00463Frame · crackedAT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME UPPER CHORD CRACKED AT STATION 600 RBL 3. (M)Mar 28, 2002 · N815EA · Boeing 727225 · Fuselage Main, FrameSDR 2002F00462Panel · corrodedAT C-CHECK, FOUND CORROSION IN AFT PIT AT RIGHT TRANSITION PANEL TOP SIDE FROM STATION 950A TO 1066. (M)Mar 28, 2002 · N815EA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 2002F00461Seat Track · gougedAT C-CHECK, FOUND SEAT TRACK GOUGED AT STATION 848 TO 870 RB 44. (M)Mar 28, 2002 · N815EA · Boeing 727224 · Fuselage, Seat/Cargo Attach FittingsSDR 2002F00460Bulkhead · crackedAT C-CHECK, FOUND THREE CRACKS AT FORWARD PIT AFT BULKHEAD CENTER PANEL. (M)Mar 28, 2002 · N815EA · Boeing 727225 · Fuselage Main, BulkheadSDR 2002F00475Floor Support · corrodedAT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STATION 644 RBL 9. (M)Mar 25, 2002 · N815EA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 2002F00474Bracket · damagedAT C-CHECK, FOUND NR 3 SPOILER INBOARD ATTACH BRACKET WITH TWO ELONGATED HOLES AT STATION 507 AND 515. (M)Mar 23, 2002 · N815EA · Boeing 727225 · SpoilersSDR 2002F00457Support · corrodedAT C-CHECK, FOUND CORROSION ON FORWARD CARGO SUPPORT AT STATION 644. (M)Mar 22, 2002 · N815EA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 2002F00455Seat Track · wornAT C-CHECK, FOUND SEAT TRACK WORN OUT OF LIMITS AT STATION 852-868. (M)Mar 22, 2002 · N815EA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 2002F00454Support · corrodedAT C-CHECK, FOUND FORWARD CARGO SUPPORT CORROSION AT STATION 536. (M)Mar 21, 2002 · N815EA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 2002F00453Frame · crackedAT C-CHECK, FOUND CRACK SIX INCHES LONG AT LOWER LEFT Z-FRAME IN FORWARD CARGO PIT STATION 480 LBL 32. (M)Mar 20, 2002 · N815EA · Boeing 727225 · Fuselage Main, FrameSDR 2002F00452Panel · corrodedAT C-CHECK, FOUND CORROSION AND CRACK IN THE FORWARD PIT AT THE RIGHT TRANSITION PANEL TOP SIDE FROM STATION 480-560. (M)Mar 20, 2002 · N815EA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 2002F00451Skin · chafedAT C-CHECK, FOUND L-1 DOOR INTERIOR SKIN CHAFED BETWEEN THE CENTER STOPS ON THE AFT EDGE. (M)Mar 19, 2002 · N815EA · Boeing 727225 · Passenger/Crew DoorsSDR 2002F00450Web · corrodedAT C-CHECK, FOUND AFT PIT SHEAR FLOOR WEB CORRODED AT STATION 1183 RBL 18. (M)Mar 18, 2002 · N815EA · Boeing 727225 · Fuselage Floor PanelSDR 2002F00456Seat Track · wornAT C-CHECK, FOUND SEAT TRACK WORN OUT OF LIMITS AT STATION 700D TO STATION 720E LBL 44. (M)Feb 22, 2002 · N815EA · Boeing 727225 · Fuselage, Seat/Cargo Attach Fittings
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