Boeing 727-225

Service difficulty reports · 4,226

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 = '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 FOTR2104614939Seat Track · corrodedCABIN SEAT TRACK AT RBL 24.5, FS 690-740 HAS HEAVY CORROSION. REPAIRED ON FASI WO 21046, NR 14939.May 13, 2011 · N801EA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR15199Skin · crackedNR 5 SLAT OTBD T/E PANEL IS CRACKED AT UPSTOP PAD CUTOUT. REPAIRED ON FASI WO 21046, NR 15199.May 13, 2011 · N801EA · Boeing 727225 · Leading Edge DevicesSDR FOTR2104615158Frame · dentedFWD PIT FRAME BS 700 UPPER FLANGE IS DENTED BETWEEN STR 24R-23R. REPAIRED ON FASI WO 21046, NR 15158.May 12, 2011 · N801EA · Boeing 727225 · Fuselage Main, FrameSDR FOTR2104614983Seat Track · corrodedCABIN SEAT TRACK AT RBL 24.5, FS 940 INBD FLANGE HAS HEAVY CORROSION. REPAIRED ON FASI WO 21046, NR 14983.May 10, 2011 · N801EA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR FOTR2104614995Frame · brokenC-1 DOOR, CHUNK MISSING FROM LIGHTENING HOLE ON AFT PORTION OF DOOR, BS 580. REPAIRED ON FASI WO 21046.May 10, 2011 · N801EA · Boeing 727225 · Cargo/Baggage DoorsSDR FOTR2104614700Support Angle · crackedRT WHEEL WELL INBD VERTICAL SUPPORT ANGLE CRACKED BS 870 RBL 8. REPAIRED ON FASI WO 21046, NR 14700.May 7, 2011 · N801EA · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA201105021687Socket · looseEMERGENCY EXIT LIGHTS INOP. FOUND COCKPIT EMERGENCY LIGHT LOOSE IN FIXTURE. RESEATED EMERGENCY LIGHT. OPS CHECK GOOD. FINAL CLOSEDMay 2, 2011 · N467FE · Boeing 727225 · Emergency LightingSDR K11A201151172402Stringer · corrodedSTRINGER CORROSION, 10 INCHES.Apr 29, 2011 · N724CK · Boeing 727225 · Fuselage Main, Longeron/StringerSDR K11A2011052672407Shear Tie · corrodedSHEAR TIE CLIP CORROSION, 6 INCHES, STA 1130 STRINGER 20 TO 21 LEFT.Apr 28, 2011 · N724CK · Boeing 727225 · Fuselage Internal Mounting StructureSDR FDEA201104271640Line · leakingLOSS OF A SYS PRESSURE AND ALL A SYS HYD FLUID AFTER SUSPECTED LIGHTNING STRIKE. CREW COMPLIED WITH ALL QRH PROCEDURES TO SAFELY RECOVER ACFT. HYD SYS A FLUID SHUTOFF SWITCHES WERE OFF FOR APPROX 50 MINUTES WITH ENGINES 1 AND 2 OPERATING. CREW COMPLETED MApr 27, 2011 · N469FE · Boeing 727225 · Hydraulic System, MainSDR FDEA201104211591Skin · misrepairedMCD EXTERNAL SKIN DOUBLER TO EXTERNAL SKIN STA 560 STR 10L. REMOVED REPAIR AT MCD EXTERNAL SKIN STA 560 STR 10L IAW SRM 51-30-2. FABRICATED DOUBLER AND FILLER, AND INSTALLED FILLER AND DOUBLER REPAIR PER EA 7-5230-136752.Apr 21, 2011 · N468FE · Boeing 727225 · Cargo/Baggage DoorsSDR CA110421011Gearbox · making metal(CAN) ON APR 18, ACFT 728, WHILE FLYING ENROUTE, THE FLIGHT CREW HAD A NR 2 ENGINE LOW PRESSSSURE LIGHT ILLUMINATED, AND OIL QTY DROPPPED TO ZERO. NR 2 ENG WAS SHUTDOWN AND ACFT RETURNED TO DEPARTURE. MAINTENANCE FOUND METAL IN THE MAIN OIL FILTER. GEARBOX REApr 18, 2011 · Boeing 727225 · Accessory GearboxesSDR K11A2011051172401Pressure Panel · crackedNOSE WHEEL PRESSURE WEB CRACK.Apr 15, 2011 · N724CK · Boeing 727225 · Fuselage Main, BulkheadSDR FDEA201104081410Stringer · corrodedAFT CARGO STA 1010, STR 27L CORROSION AROUND RIVET TAIL. REMOVED AND REPLACED PRODUCTION SPLICE STRINGER 27L STA 1010 IAW B727 SRM 51-30-2 REV 103Apr 8, 2011 · N468FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR K11A2011052672406Stringer · corrodedSTRINGER CORROSION, STA 950E PLUS 16 INCHES TO = 20 INCHES STRINGER 30, 20 INCH CORROSION.Apr 7, 2011 · N724CK · Boeing 727225 · Fuselage Main, Longeron/StringerSDR K11A2011052672405Skin · corrodedSKIN CORROSION, STA 720B PLUS 8 INCHES STRINGER 28R, 2 X 3 INCHES.Apr 6, 2011 · N724CK · Boeing 727225 · Fuselage Main, Plate/SkinSDR K11A2011052672404Seat Track · corrodedSEAT TRACK CORROSION, 60 INCHES, STA 1010 TO 1070 LBL 46.Apr 6, 2011 · N724CK · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR K11A2011052672403Floorbeam · corrodedFLOORBEAM CORROSION AT STA 1130 LBL 28 AND 43.Apr 6, 2011 · N724CK · Boeing 727225 · Fuselage Main, Floor BeamSDR K11A2011052672402Floorbeam · corrodedFLOORBEAM CORROSION AT STA 1130 LBL 11 AND 18. 2 INCH IN EACH POSITION.Apr 6, 2011 · N724CK · Boeing 727225 · Fuselage Main, Floor BeamSDR K11A2011052672401Frame · corrodedFRAME CORROSION, 3 INCHES AT STA 620 RBL 24.Apr 6, 2011 · N724CK · Boeing 727225 · Fuselage Main, FrameSDR FDEA201104051319Skin · damagedC-1 DOOR FWD LOWER OUTER SKIN IS OIL CANNED AT BS 560 3" CUT OUT DAMAGED AREA OF SKIN ( DIM 2" X 1 13/16" ) IAW SRM 52-00-3 FIG 3 FABRICATED REPAIR DOUBLER IAW SRM 52-00-3 FIG 3. INSTALLED REPAIR DOUBLER IAW SRM 52-00-3 FIG 3 AND 51-30-2 REV 103 AND EA Apr 5, 2011 · N468FE · Boeing 727225 · Cargo/Baggage DoorsSDR FDEA201104051380Stringer · crackedRT WING STA 686.5 STR 9 IS CRACKED. FABRICATED REPAIR ANGLES AND RADIUS FILLERS. INSTALLED REPAIR PARTS IAW EO 7-5710-7-4322 PT1 AT RT WING STA 686.5 STR 9.Apr 5, 2011 · N468FE · Boeing 727225 · Wing, Longeron/StringerSDR FDEA201104041379Stringer · crackedLT WING, STA 686.5 STR 14 IS CRACKED. CUT ACCESS HOLE IN LT WING STR 14 VENT BOX, FABRICATED REPAIR PARTS, AND INSTALLED REPAIR PARTS IAW EO 7-5710-7-4322 PT1 AT LT WING STA 686.5 STR 14.Apr 4, 2011 · N468FE · Boeing 727225 · Wing, Longeron/StringerSDR FDEA201104041378Stringer · crackedLT WING STA 629.0, STR 8 IS CRACKED. FABRICATED REPAIR ANGLES AND RADIUS FILLERS. INSTALLED REPAIR PARTS IAW EO 7-5710-7-4322 PT1 AT LT WING STA 629.0 STR 8.Apr 4, 2011 · N468FE · Boeing 727225 · Wing, Longeron/StringerSDR FDEA201104011279Angle · chafedHEADER BEAM, LOWER ANGLE STRAP CHAFED BS 640.Apr 1, 2011 · N468FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR FDEA201103301253Skin · gougedLEFT WING, INBD FLAP, FORE FLAP HAS AREA AT MOST OUTBD L/E GOUGED. REMOVED PREVIOUS REPAIR FROM LT INBD FOREFLAP IAW SRM REV 103, 51-30-2. FABRICATED NEW REPAIR IAW SRM 57-50-4, FIG 4 AND 57-50-2, FIG 3 INSTALLED DOUBLER IAW SRM 51-30-2 AND 57-50-4, FIG 4Mar 30, 2011 · N468FE · Boeing 727225 · Trailing Edge FlapsSDR FDEA201103301254Frame · bentAFT CARGO STATION 1050 AT STRINGER 28R, FRAME BENT. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1. INSTALLED DOUBLER IAW SRM 51-30-2 AND 51-40-3 FIG 1.Mar 30, 2011 · N468FE · Boeing 727225 · Fuselage Main, FrameSDR FDEA201103301246Frame · damagedBS 783 FRAME HAS DOUBLE DRILLED HOLE AT FLANGE 3" ABOVE STRINGER 17R. REMOVED DAMAGED HOLE AND INSTALLED FASTENER IAW EO 7-5310-7-3367 PT 4 AND SRM 51-30-2.Mar 30, 2011 · N468FE · Boeing 727225 · Fuselage Main, FrameSDR FDEA201103301247Skin · damagedNR 3 ENGINE NOSE COWL O/B T/E SKIN DAMAGED AT 4:30 POAITION. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER, AND INSTALLED REPAIR PARTS IAW SRM 51-10-1, 51-30-2, 54-30-3 FIG 8.Mar 30, 2011 · N468FE · Boeing 727225 · Nacelle/Pylon, Plate/SkinSDR FDEA201103291468Beam · damagedBS 1183 BULKHEAD LBL 20 BEAM AND WEB HAVE CLOSE ON CENTER SPACING BETWEEN FASTENERS. ACCOMPLISHED EA 7-5310-123586.Mar 29, 2011 · N468FE · Boeing 727225 · Fuselage Main, StructureSDR FDEA201103191082Control Panel · failedAT FL 290 SMELLED STRONG ELECTRICAL ODOR. NO SMOKE NOTED OR CB'S POPPED. DECLARED EMERGENCY AND LANDED. R & R BUSS PROTECTION PANEL CONTROL BOX IAW AMM 20-10-017-2. R & R THE EXTERNAL POWER CONTACT RELAY IAW AMM 24-20-000-5. RAN ALL 3 ENGINES IAW JRH WITHMar 19, 2011 · N463FE · Boeing 727225 · External Power SystemSDR FDEA201103191080Actuator · malfunctionedDURING CLIMBOUT NR 4 LT L/E SLAT DID NOT RETRACT. RAN QRH. RETURNED TO DEPARTURE. JUMPER INSTALLED ON NR 4 SLAT ACTUATOR. DO TO IND OF EXTEND POSITION. MM 27-82-000-1-0, INSTALLED NR 4 L/E SLAT EXTEND SWITCH JUMPER. SYS GROUND CHECKS NORMAL. JUMPER INMar 19, 2011 · N468FE · Boeing 727225 · Leading Edge Slat Control SystemSDR 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 · Spoilers
Back to Boeing 727-225