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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FOTR2104614939Seat Track · corrodedCABIN SEAT TRACK AT RBL 24.5, FS 690-740 HAS HEAVY CORROSION. REPAIRED ON FASI WO 21046, NR 14939.SDR FOTR15199Skin · crackedNR 5 SLAT OTBD T/E PANEL IS CRACKED AT UPSTOP PAD CUTOUT. REPAIRED ON FASI WO 21046, NR 15199.SDR FOTR2104615158Frame · dentedFWD PIT FRAME BS 700 UPPER FLANGE IS DENTED BETWEEN STR 24R-23R. REPAIRED ON FASI WO 21046, NR 15158.SDR FOTR2104614983Seat Track · corrodedCABIN SEAT TRACK AT RBL 24.5, FS 940 INBD FLANGE HAS HEAVY CORROSION. REPAIRED ON FASI WO 21046, NR 14983.SDR FOTR2104614995Frame · brokenC-1 DOOR, CHUNK MISSING FROM LIGHTENING HOLE ON AFT PORTION OF DOOR, BS 580. REPAIRED ON FASI WO 21046.SDR FOTR2104614700Support Angle · crackedRT WHEEL WELL INBD VERTICAL SUPPORT ANGLE CRACKED BS 870 RBL 8. REPAIRED ON FASI WO 21046, NR 14700.SDR FDEA201105021687Socket · looseEMERGENCY EXIT LIGHTS INOP. FOUND COCKPIT EMERGENCY LIGHT LOOSE IN FIXTURE. RESEATED EMERGENCY LIGHT. OPS CHECK GOOD. FINAL CLOSEDSDR K11A201151172402Stringer · corrodedSTRINGER CORROSION, 10 INCHES.SDR K11A2011052672407Shear Tie · corrodedSHEAR TIE CLIP CORROSION, 6 INCHES, STA 1130 STRINGER 20 TO 21 LEFT.SDR 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 MSDR 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.SDR 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 RESDR K11A2011051172401Pressure Panel · crackedNOSE WHEEL PRESSURE WEB CRACK.SDR 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 103SDR K11A2011052672406Stringer · corrodedSTRINGER CORROSION, STA 950E PLUS 16 INCHES TO = 20 INCHES STRINGER 30, 20 INCH CORROSION.SDR K11A2011052672405Skin · corrodedSKIN CORROSION, STA 720B PLUS 8 INCHES STRINGER 28R, 2 X 3 INCHES.SDR K11A2011052672404Seat Track · corrodedSEAT TRACK CORROSION, 60 INCHES, STA 1010 TO 1070 LBL 46.SDR K11A2011052672403Floorbeam · corrodedFLOORBEAM CORROSION AT STA 1130 LBL 28 AND 43.SDR K11A2011052672402Floorbeam · corrodedFLOORBEAM CORROSION AT STA 1130 LBL 11 AND 18. 2 INCH IN EACH POSITION.SDR K11A2011052672401Frame · corrodedFRAME CORROSION, 3 INCHES AT STA 620 RBL 24.SDR 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 SDR 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.SDR 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.SDR 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.SDR FDEA201104011279Angle · chafedHEADER BEAM, LOWER ANGLE STRAP CHAFED BS 640.SDR 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 4SDR 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.SDR 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.SDR 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.SDR FDEA201103291468Beam · damagedBS 1183 BULKHEAD LBL 20 BEAM AND WEB HAVE CLOSE ON CENTER SPACING BETWEEN FASTENERS. ACCOMPLISHED EA 7-5310-123586.SDR 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 WITHSDR 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 INSDR 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 FSDR 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 FILLERSDR 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 SSDR 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 NOTESDR 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 NOTSDR 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 NOTSDR 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 SDR 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 NRSDR 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 70SDR 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 REPAISDR 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 SDR 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 SDR 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 REPAISDR 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 57-50-3SDR 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 90SDR 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 SDR 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, FABRICATSDR 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 57-50-2
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