Boeing 727-227
Service difficulty reports · 5,082
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 = '727227' 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 = '727227' 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 C8GA20090212Skin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LOWER FORWARD CORNER OF MAIN CARGO DOOR INNER SKIN IS GOUGED AND CRACKED. REMOVED INNER SKIN , FABRICATED NEW SKIN. INSTALLED SKIN, NO OTHER DEFECTS WERE NOTED AIRCRAFT WAS RETURNED TO SESDR C8GA20090211Skin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LOWER FORWARD CORNER OF MAIN CARGO DOOR INNER SKIN IS GOUGED AND CRACKED. REMOVED INNER SKIN , FABRICATED NEW SKIN. INSTALLED SKIN, NO OTHER DEFECTS WERE NOTED AIRCRAFT WAS RETURNED TO SESDR C8GA200902010Strap · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE STRUCTURAL PLATE ON OUTSIDE SKIN STRINGER 17L AT B.S. 846 HAS EXFOLIATION CORROSION. CORROSION WAS REMOVED, HFEC PERFORMED AND NEW DOUBLER WAS FABRICATED FROM 7075 T6 .063. NO OTHER DEFECTSSDR C8GA200902009Stringer · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE WING CENTER SECTION RBL 70.5 STRINGER 17R IS CORRODED BETWEEN B.S. 740-760. REMOVED CORROSION, FABRICATED INTERNAL ANGLE FROM 7075 T6 .063" DIM 16.125 X 2.750", EXTERNAL DOUBLER FROM 7075 TSDR C8GA20090208Floorbeam · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE AFT PIT FLOORBEAM IS CORRODED AT B.S. 950F LBL 70. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED SECTION. FABRICATED UPPER CHORD, 2 EA SUPPORT ANGLES, 2 EA STRAPS.SDR C8GA20090207Floorbeam · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE AFT PIT FLOORBEAM IS CORRODED AT B.S. 950D LBL 60 - LBL 70. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED SECTION DIM 16.5". FABRICATED UPPER CHORD, 2 EA SUPPORT ANGLES, & 2 EA STRAPSDR C8GA200902006Floorbeam · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE CABIN FLOORBEAM AT EXISTING REPAIR IS CORRODED BETWEEN LBL 18 - LBL 50 AT B.S 950C. REMOVED OLD REPAIR AND FABRICATED NEW FROM BAC 1490-2888, ANGLES, AND FILLER. INSTALLED REPAIR, NO OTHERSDR C8GA200902005Floorbeam · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE CABIN FLOORBEAM UPPER FLANGE IS CORRODED BETWEEN RBL 45- RBL 70 AT B.S 950F. CORROSION WAS OUT OF LIMITS REMOVED DAMAGED FLOORBEAM UPPER CHORD. FABRICATED REPAIR PARTS P/N BAC 1505-100617,SDR C8GA20090204Floorbeam · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE CABIN FLOORBEAM UPPER FLANGE IS CORRODED BETWEEN RBL 45- RBL 70 AT B.S 970. CORROSION WAS OUT OF LIMITS REMOVED DAMAGED FLOORBEAM . FABRICATED REPAIR PARTS P/N BAC 1505-100617, BAC 1490-27SDR C8GA20090203Floorbeam · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE CABIN FLOORBEAM UPPER FLANGE IS CORRODED ON LOWER SURFACE AT B.S 950D RBL 21. CORROSION WAS OUT OF LIMITS REMOVED DAMAGED FLOORBEAM P/N BAC 1505-100617, FABRICATED REPAIR ANGLE BAC 1490-26SDR C8GA20090202Floorbeam · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE CABIN FLOOR BEAM UPPER FLANGE IS CORRODED ON LOWER SURFACE AT B.S 950D RBL 4. CORROSION WAS OUT OF LIMITS REMOVED AND REPLACED DAMAGED CHORD, SUPPORT ANGLE BAC1490-2785, SUPPORT ANGLE BAC SDR C8GA20090200Strap · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE AFT PIT FLOORBEAM BS 950 BETWEEN RBL 60 AND RBL 70 IS CORRODED. REMOVED CORROSION, INSTALLED NEW STRAP PN 65-16338-276 BETWEEN BS 840-950A. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA20090199Floorbeam · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT FLOOR BEAM UPPER FLANGE IN AFT PIT AT RBL 39, BS 1130 IS CORRODED. PREVIOUS REPAIR WAS REMOVED TO ALLOW FOR CORROSION CLEAN UP, CORROSION WAS REMOVED. FABRICATED FILLER FROM 7075 T6 1 EA .160 INCH X 1.25 ISDR C8GA20090198Panel · misrepairedWHILE IN HEAVY MX, PERFORMING INSP, IT WAS NOTED THAT THE RT ELEVATOR UPPER SKIN EXISTING REPAIR IS NON SRM COMPLIANT. REMOVED AND REPLACED UPPER SKIN PANEL PN 65-25637-74. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA20090197Skin · damagedWHILE IN HEAVY MX, PERFORMING INSP, IT WAS NOTED THAT THE RT ELEVATOR UPPER INBD SKIN PANEL IS DAMAGED. REMOVED DAMAGED AREA DIM 1.5 INCHES X 2.5 INCHES. FABRICATED FILLER FROM 2024 T3 .063 INCH DIM 1.5 INCH X 2.5 INCH AND DOUBLER FROM 2024-T3 DIM 4.5 INCHESSDR C8GA20090196Stringer · corrodedWHILE IN HEAVY MX, PERFORMING INSP, IT WAS NOTED THAT STR 26R BS 735 IS CORRODED. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF STR, FABRICATED FILLER FROM BAC 1498-146 DIM 2.625 INCHES, FABRICATED REPAIR SPLICE FROM BAC 1498-131 DIM 12.375 SDR C8GA20090194Door Frame · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE C2 DOOR CUTOUT FWD FRAME BS 950E, INNER CHORD UPPER FLANGE IS CORRODED ON LOWER SURFACE AT NUT PLATE BETWEEN STR 27R-26R. CUT-OUT DAMAGED AREA AT 950E. FABRICATED 2 ANGLES, HEAT TREATED TO T6, FABRICATSDR C8GA20090193Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STRINGER 27L IS CORRODED AT BS 400-420. REMOVED DAMAGED SECTION OF STR DIM 21.25 INCHES X .625 INCH, FABRICATED NEW STR FROM BAC 1493-578, 7075 T6. FABRICATED 2 REPAIR SPLICES FROM 7075 T6 .063 INCHES DIM. SDR C8GA20090192Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT STR 18L END FITTING IS CORRODED AT STA 1177-1183. CORRODED FITTING WAS REMOVED, FABRICATED NEW FITTING FROM 2024-T3511 DIM. 3.56 INCHES X 5.85 INCHES AND INSTALLED FITTING. NO OTHER DEFECTS WERE NOTED. ACSDR C8GA2009133Rod · brokenFLT 712. LANDING IN SAN ACFT DEVELOPED A VIOLENT UNCONTROLLABLE NOSE WHEEL SHIMMY. ACFT SLOWED TO DISCOVER A LOSS OF NLG STEERING. POST FLT INSPECTION PERFORMED, NOTED THE TORSION LINK PIN WAS NOT INSTALLED IN THE LINKS & THE NLG LIGHT CONDUIT WRAPPED AROUND SDR C8GA20090191Web · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE WEB AT BS 950F-970 RBL 4 IS CORRODED. REMOVED DAMAGED WEB, FABRICATED NEW FROM 7075 T6 .040 INCH DIM 19.875 INCHES X 9.750 INCHES. INSTALLED WEB, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVISDR C8GA20090190Shear Tie · corrodedWHILE IN HEAVY MX, PERFORMING INSP, IT WAS NOTED THAT SHEAR TIE IS CORRODED AT BS 950E BETWEEN STR 29R-30. REMOVED DAMAGED SHEAR TIE AND FABRICATED NEW FROM 7075 T6 DIM. 4 INCHES X 5 INCHES, .071 INCH, INSTALLED SHEAR TIE, NO OTHER DEFECTS WERE NOTED. ACFT WSDR C8GA20090189Shear Tie · corrodedWHILE IN HEAVY MX, PERFORMING INSP, IT WAS NOTED THAT SHEAR TIE IS CORRODED AT BS 950F BETWEEN STR 30-29R. REMOVED CORROSION, PERFORMED UT INSP AND FABRICATED DOUBLER FROM 7075 T6 DIM 4 INCHES X 5 INCHES, .071 INCH. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOSDR C8GA20090188Intercostal · crackedWHILE IN HEAVY MX, PERFORMING INSP, IT WAS NOTED THAT INTERCOSTAL AT BS 950-950A IS CRACKED BETWEEN STR 20L-21L. REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW FROM 7075-0 DIM 14 INCHES X 16 INCHES, .080 INCH HEAT TREATED TO T6. INSTALLED REPAIR, NO OTHER DEFESDR C8GA20090187Intercostal · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT INTERCOSTAL AT BS 950E +6 IS CORRODED ON THE FWD SIDE BETWEEN STR 30-27R. REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW FROM 7075-0 DIM. 27 INCHES X 8 INCHES .040 INCH HEAT TREATED TO T6. INSTALLED REPAIR, NOSDR C8GA20090186Shear Tie · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT LOW FLANGE FWD SIDE AT STR 30-28R AT BS 970 IS CORRODED. REMOVED DAMAGED AREA, FABRICATED NEW SHEAR TIE FROM 7075 T6 DIM 2 INCHES X 6.5 INCHES .071 INCH, INSTALLED FABRICATED SHEAR TIE. NO OTHER DEFECTS WERSDR C8GA20090185Angle · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STR 28L ATTACH ANGLE AT BS 950 IS CORRODED. INSTALLED NEW ATTACH ANGLE PN 69-14473-1. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR FDEA200906272329Control Valve · leakingUNABLE TO CONTROL PRESSURIZATION WITH ANY MODE (AUTO, STANDBY, OR MANUAL). DESCENDED TO 11,000. PERFOMED OPS CHECK OF CABIN PRESS CONTROL SYSTEM PER MM 21-31-000-1 ALL MODES OP CHECK NORMAL. VERIFIED CABIN OUTFLOW VALVE IS CLOSED WHEN COMMANDED CLOSED. WISDR FDEA200906182154Oil System · low pressureLOW OIL PRESSURE LIGHT ILLUMINATED, OIL PRESSURE ON S/O'S PANEL INDICATED YELLOW ARC, PREFORMED ENG FAIL/SHUTDOWN CHECKLIST. DURING CHECKLIST OIL QUANITY DROPPED RAPIDLY TO ZERO. OIL PRESSURE IN YELLOW ARE FOR APPROX 130 MIN. DURING DECENT PERFORMED ENG WINSDR FDEA200905061556Relay · failedFL240, GLARESHIELD FIRE LIGHT CAME ON FOR LESS THAN 1 SEC. NO OTHER FIRE INDICATIONS. AT 1135 AND 1140Z FIRE LIGHT AGAIN BLINKED ON AND OFF WITH FIRE BELL FOR LESS THAN 1 SEC AT 1141Z FIRE LIGHT, BELL, AND APU LIGHT ALL CAME ON AND STAYED ON. PULLED APU FIRSDR FDEA200903120910Line · leakingLOST SYS "A" HYDRAULICS WHEN MOVING FLAPS FROM 2 DEG TO 5 DEG. HYD SYS "A" PUMP LIGHTS DID NOT ILLUMINATE. KEPT POSITIVE PRESSURE. FOUND 5/8 INCH LINE TO A SYS PRESSURE MODULE LEAKING. IPC REF 29-15-00-01G ITEM 280 LINE FROM NR 1 ENG "A" PUMP TO MODULE. SDR FDEA200903110898Control Valve · failedAIRCRAFT WOULD NOT PRESSURIZE PROPERLY. TWO MIN AFTER LEVEL OFF AT FL320 CABIN PRESSURE CLIMBED THROUGH 10 K MSL. CREW EXECUTED CABIN ALT WARNING/RAPID DEPRESSURIZATION AND EMERGENCY DESCENT CHECKLIST. AIRCRAFT FAILED TO HOLD PRESSURE (CABIN ALT CLIMBING )SDR DHLA7812009510Shear Tie · corrodedLOWER FUSELAGE FWD CARGO COMPT FRAME SHEAR TIE WITH CORROSION AT BS 600 BETWEEN S27L AN S28L NOTED WHEN PERFORMING REPAIR. REPAIRED FRAME SHEAR TIE IAW B727-200 SRM 53-10-4 FIG 11.SDR DHLA7812009512Shear Tie · corrodedLOWER FUSELAGE FWD CARGO COMPT AT BS 600 BETWEEN 227L AN 28L FRAME SHEAR TIE WITH CORRODED. REPAIRED FRAME SHEAR TIE SECTION IAW SRM 53-10-4 FIG 11. REPLACED INTERCOSTAL IAW SRM 51-10-1 PARA 7A.SDR DHLA7812009511Shear Tie · corrodedLOWER FUSELAGE FWD CARGO COMPT AT BS 582 BETWEEN S27L AND S28L INTERCOSTAL WITH CORR. REPAIRED FRAME SHEAR TIE SECTION IAW 7272 200 SRM 53-10-4 FIG 11. REPLACED INTERCOSTAL ANGLE IAW B727SRM 51-10-1 PARA 7A.SDR DHLA7812009516Intercostal · corrodedLOWER FUSELAGE FWD CARGO COMPT AT BS 600 LBL 9 SHEAR TIE AND INTERCOSTAL WITH CORROSION. REPAIRED FRAME SHEAR TIE SECTION AT BS 600 BETWEEN S27L AND S28L IAW SRM 53-10-4 FIG 11. REPLACED INTERCOSTAL ANGLE FROM BS 580 TO BS 600 BETWEEN S27L AN S28L IAW SRM 51SDR FDEA200902270763Bulkhead · crackedNOSE LANDING BULKHEAD STA NR 351.2 HAS 3 CRACKS MIGRATING FROM 1 FASTENER HOLE ATTACHING THE NOSE GEAR LOCK ACTUATOR FITTING TO BULKHEAD. TRIMMED CRACKS, INSTALLED REPAIR DOUBLER FABRICATED FROM 7075 T6 0.100.BATCH NR 1338161.SDR FDEA200902250717Actuator · malfunctionedAFTER PLACING LANDING GEAR LEVER IN DOWN POSITION NOSE GEAR RED LIGHT REMAINED ON AND GREEN NOSE GEAR LIGHT DID NOT COME ON. DID A MANUAL GEAR EXTENSION AND GOT PROPER DOWN AND LOCKED INDICATION. FOUND NLG LOCK HYD ACTUATOR FITTING CRACKED. REMOVED AND REPLSDR DHLA7812009505Strap · crackedLOWER FUSELAGE E/E COMPARTMRNT AT BS 328 BL0 WL 200 STABILIZER STRAP CRACKED. REPAIRED STABILIZER STRAP FROM BS 294.5 TO BS 360 BL0 WL 200 IAW B727 SRM 51-10-1 PAR 7A.SDR DHLA7812009515Stringer · corrodedLOWER FUSELAGE AFT CARGO COMPT STRINGER FROM BS 1166 TO BS 1183 S22L WITH CORROSION. REPAIRED FUSELAGE S22L SECTION BETWEEN BS 1149 AND BS 1183 IAW SRM 53-10-3 FIG 1 DETAIL I.SDR DHLA7812009513Floorbeam · corrodedLOWER FUSELAGE AFT CARGO COMPT BS 1090 LBL 19.5 FLOORBEAM LOWER CHORD WITH CORROSION. REPAIRED FUSELAGE FLOORBEAM FWD FLANGE SECTION AT BS 1090 IAW SRM 53-10-8 FIG 8.SDR DHLA7812009506Floorbeam · corrodedLOWER FUSELAGE AFT CARGO COMPARTMENT BS 950E LBL 43 FLOORBEAM LOWER CHORD WITH CORROSION. REPAIRED AFT CARGO COMPARTMENT FLOORBEAM LOWER CHORD BS 950E BETWEEN LBL 35.5 AND LBL 50.5 IAW SRM 53-10-8 FIG.8.SDR DHLA7812009503Strap · crackedLOWER FUSELAGE AFT CARGO COMPARTMENT BS 950E RBL 24 STABILIZER STRAP WITH CRACK. REPAIRED STABILIZER STRAP IAW B727-200 SRM 51-40-3 FIG 1 AT RBL 24 BETWEEN BS 950C + 4.25 INCH AND BS 950E + 12.5 INCH.SDR DHLA7812009517Stringer · corrodedLOWER FUSELAGE E/E STRINGER AT BS 438 S26R WITH CORROSION. REPAIRED S26R BS 424 TO BS 456 IAW SRM 53-10-3 FIG 1 DETAIL I.SDR DHLA7812009501Frame · crackedUPPER FUSELAGE FWD LAVATORY SECTION BS 312 AT STR 13R FRAME WITH CRACK. REPAIRED FUSELAGE FRAME SECTION AT BS 312 BETWEEN STR, 11R AND STR 14R DUE TO CRACK IAW B727 SRM 53-10-4 FIG 1.SDR DHLA2009781500Web · corrodedUPPER FUSELAGE CARGO CABIN AT BS 1172 WL 208 LBL 68 INCH WEB WITH CORROSION. REPAIRED WEB DUE TO CORROSION FROM BS 1168 TO BS 1176,WL 208 LBL 66 INCH TO 70 INCH IAW B727-200 SRM 51-40-2 FIG 1. NOTE PERMANENT MAJOR REPAIR.SDR DHLA7812009504Frame · dentedLOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 500 BETWEEN S22 AND S24R FRAME WITH DENTS. REPAIRED FRAME AT FWD CARGO COMPT STA 500 BETWEEN S20R TO S25R IAW 727SRM 51-40-3 FIG 1. RIVETS AND LOCK FASTENERS INSTALLED IAW B727 SRM 51-30-2 PARA 4 4B AND PARA 7D.SDR DHLA7812009513ASupport Fitting · crackedLT WING FRONT SPAR SECTION NR 3 SLAT ACT CAVITY INBD SUPPORT FITTING CRACKED AT LOWER SECTION. REPLACED SUPPORT FITTING IAW B727-200 SRM 51-10-1 PARA 7A.SDR FDEA200902050463Muffler · fodNO EQUIP COOLING LIGHT ILLUMINATED AT FL180 ON CLIMB-OUT. QRH COMPLIED WITH EQUIP COOLING CIRCUIT BREAKERS PULLED FOR 15 SECONDS & RESET. LIGHT WENT OUT & REMAINED OUT FOR ABOUT 2 MINS THEN RE-ILLUMINATED. CB PULL IAW QRH. LIGHT EXTINGUISHED DURING APPROACSDR FDEA200902040462Blower · failedEQUIPMENT COOLING LIGHT ILLUMINATED INFLIGHT, APPROX ABOVE 18K FEET. RAN CHECKLIST. COMPLIED WITH PROCEDURE TO PULL APPROPRIATE CIRCUIT BREAKERS. REPEAT WRITEUP, LIGHT WENT OUT ON SHORT FINAL. REMOVED AND REPLACED COOLING BLOWER IAW MM 21-58-011-4, OPS CHE
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