Boeing 727-233
Service difficulty reports · 3,034
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 = '727233' 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 = '727233' 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 01FDEA00358Frame · dentedFRAME DENTED BS 700, LBL 42, WL 160 FOUND TO BE OUT OF LIMITS PER FEDEX EA 7-5310-29267. REMOVED AND REPLACED PER FEDEX SRM 51-40-3. ALODINED AND PRIMED PER FEDEX 51-20-151.SDR 01FDEA00325Splice · corrodedDURING ROUTINE INSP, BS 950 BULKHEAD FOUND CORRODED ON LWR CHORD AT RBL 20. *S/D* REMOVED, REPLACED AND FAB SPLICE ANGLE PER IAW BAC 727 SRM 51-40.SDR 01FDEA00320Accessory Unit · failedATTEMPT TO RAISE GEAR LEVER, WOULD NOT GO BEYOND OFF POS. COMPLIED WITH CKLIST WITH NEGATIVE RESULTS. REPLACED LG ELECTRONIC MODULE PER MM 32-09-21-4. PERFORMED CONTROL HANDLE LOCK SYS TEST PER MM 32-31-011-5. SYS CK OK.SDR 01FDEA00312Splice · crackedDURING ROUTINE INSP THE FAIL-SAFE CHORD SPLICE AT BS 500, STR 21L FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB SPLICE PLATE PER IAW BAC 727 SRM 51-20-1, 51-30-2.SDR 01FDEA00311Splice · crackedDURING ROUTINE INSP THE FAIL-SAFE CHORD SPLICE AT BS 600, STR 21L FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW 727 SRM 51-20-1, 51-30-2.SDR 01FDEA00310Splice · crackedDURING ROUTINE INSP, THE FAIL-SAFE CHORD SPLICE AT BS 520, STR 21L FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.SDR 01FDEA00308Splice · crackedDURING ROUTINE INSP THE FAIL-SAFE CHORD SPLICE AT BS 580, STR 21L FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB SPLICE PLATE PER IAW BAC 727 SRM 51-20-1, 51-30-2.SDR 01FDEA00309Splice · crackedDURING ROUTINE THE FAIL-SAFE CHORD SPLICE AT BS 540, STR 21L FOUND CRACKED. *S/D* REMOVED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.SDR 01FDEA00307Splice · crackedDURING ROUTINE INSP THE FAIL-SAFE CHORD SPLICE AT BS 560, STR 21L FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB SPLICE PLATE PER IAW BAC 727 SRM 51-20-1, 51-30-2.SDR 01FDEA00318Sill · crackedDURING ROUTINE INSP LWR SILL INBOARD RADIUS OF MCD CUTOUT FOUND CRACKED AT BS 500.SDR 01FDEA00317Sill · crackedDURING ROUTINE INSP LWR SILL INBOARD RADIUS OF MCD CUTOUT FOUND CRACKED AT BS 520.SDR 01FDEA00316Sill · crackedDURING ROUTINE INSP LWR SILL INBOARD RADIUS OF THE MCD CUTOUT FOUND CRACKED AT BS 540.SDR 01FDEA00315Sill · crackedDURING ROUTINE INSP LWR SILL INBOARD RADIUS OF MCD CUTOUT FOUND CRACKED AT BS 560.SDR 01FDEA00314Sill · crackedDURING ROUTINE INSP LWR SILL INBOARD RADIUS OF MCD CUTOUT FOUND CRACKED AT BS 580.SDR 01FDEA00313Sill · crackedDURING ROUTINE INSP LWR SILL INBOARD RADIUS OF MCD CUTOUT FOUND CRACKED AT BS 600.SDR CA010507016Filter · blocked(CAN) ON DEPARTURE THE AIRCRAFT EXPERIENCED A COMPRESSOR STALL ON NR 2 ENGINE. THE CREW DECISION WAS MADE TO RETURN TO POINT OF DEPARTURE. MAINTENANCE INVESTIGATION FOUND THE PS3 SENSE LINE FILTER BLOCKED WITH WHAT APPEARED TO BE SHREDDED PAPER FIBRE, ORIGIN USDR 01FDEA00267Seal · failedON PREFLT INSP NOSE GEAR STRUT FULLY COMPRESSED. TAIL STAND OVER PRESSURIZED. ON GEAR RETRACTION THE RED DOORS & AMBER NOSE GEAR LIGHT REMAIN ILLUM. *S/D* REMOVED NOSE INNER CYLINDER, INSTALL SEALS PER 727 200 MM 32-21-001. REMOVED PISTON TUBE ASSY PER 72SDR CA010507017Actuator · fractured(CAN) ON APPROACH TO WHEN FLAP 2 SELECTED THE CREW OBSERVED RAPID DECREASE IN A HYDRAULIC SYSTEM. HYDRAULIC LEAK/LOSS OK. LIST CARRIED OUT. MANUAL GEAR EXTENSION PERFORMED, AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS TOWED FROM THE RUNWAY TO THE HANGAR SDR 01FDEA00297Frame · crackedLWR CARGO COMPT PERF HFEC INSP FOUND 1 CRACK APPROX 1.5 INCH AT BS 600 JUST ABOVE S-20L AT I/B RADIUS SUB FRAME UNDER CARGO DOOR SPOOL FITTING. ** S/D ** R&R & FAB PER FDW DWG 53FX1349. PER SRM 51-10-01 & FDX DFWG 53FX1371.SDR COOSDR010018Skin · corrodedRT WING, LOWER SURFACE AT WS 320, STRINGER 8 SKIN CORRODED.SDR COOSDR010016Floorbeam · corrodedMAIN CARGO CABIN BS 1070, FLOORBEAM UPPER AND LOWER CHORD CORRODED, BETWEEN RBL 61 IN AND LBL 61 IN, WL 208.SDR COOSDR010015Floorbeam · corrodedMAIN CARGO CABIN BS 720D FLOORBEAM UPPER CHORD CORRODED, BETWEEN 45 IN AND LBL 60 IN, WL 208.SDR COOSDR010014Floorbeam · corrodedMAIN CARGO CABIN BS 380 FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 62 IN AND LBL 62 IN, WL 208.SDR COOSDR010013Floorbeam · corrodedMAIN CARGO CABIN BS 950C FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 62 IN AND LBL 62 IN.SDR COOSDR010012Floorbeam · corrodedMAIN CARGO CABIN BS 1130 FLOOR BEAM LOWER CHORD CORRODED, BETWEEN RBL 45 INCHES AND LBL 45 INCHES.SDR COOSDR010011Floorbeam · corrodedMAIN CARGO CABIN BS 1110 FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 61 IN AND LBL 61 INCHES, WL 208.SDR COOSDR010010Floorbeam · corrodedMAIN CARGO CABIN BS 1030 FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 62IN AND LBL 62 IN, WL 208.SDR COOSDR010009Floorbeam · corrodedMAIN CARGO CABIN, BS 950F, FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 62 IN AND LBL 62 IN, WL 208.SDR COOSDR010008Stringer · crackedAFT CARGO COMPARTMENT, STRINGER 30 CRACKED AT BS 950.SDR COOSDR010007Skin · corrodedLOWER FUSELAGE, SKIN CORRODED BETWEEN BS 117B TO BS 1183 BETWEEN STR 25L AND STR 26L.SDR COOSDR010006Floorbeam · corrodedMAIN CARGO CABIN BS 720A FLOOR BEAM UPPER CHORD CORRODED, BETWEEN RBL 60 INCHES AND LBL 60 INCHES, WL 208.SDR COOSDR010005Skin · corrodedSECTION 43-STA720E+11/STA720D+3, S26R AND ST720E+5.25 S26L. INTERNAL FUSELAGE SKIN CORRODED.SDR 01FDEA00248Switch · faultyWHILE LEVEL FLT 330 MAIN CARGO DOOR LIGHT ILLUM ON 2ND OFF PNL. FOLLOW RED TAB HOWEVER, LIGHT REMAIN ON. *S/D* REMOVED AND REPLACED LATCH WARN SWITCH 9034 PER BOEING STANDARD WIRING PRACTICES MANUAL CHPT 20. OPS CK OK PER MM 52-70-001-5.SDR 01FDEA00254Stiffener · corrodedCORROSION ON FWD RT CORNER OF NOSE WHEEL WELL STIFFENER BS 227, WL 165, RBL 20. *S/D* REPAIRED PER FEDEX SRM 51-40-4.SDR 01FDEA00243Beam · corrodedFOUND CORROSION ON I-BEAM AT BS 1182, RBL 25, WL 204. *S/D* OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED AND REPLACED PER FEDEX SRM 51-30-2.SDR 01FDEA00242Floorbeam · corrodedCORROSION ON LWR CHORD OF FLOORBEAM AT BS 1070, RBL 25 AT NUT PLATES. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-10-6, 53-10-8 FIG 2.SDR 01FDEA00241Floorbeam · corrodedCORROSION ON LWR CHORD OF FLOORBEAM BS 1010, LBL 12-15 AROUND NUT PLATE HOLES. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-8 FIG 8.SDR 01FDEA00236Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 328, LBL 30-45, WL 208. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-10-8.SDR 01FDEA00235Spar · chafedVERTICAL STAB MIDSPAR CHORD (STR 7) IS CHAFED, LT SIDE 3 INCHES FROM FRONT OF SLIDE SEAL FRONT TRACK. *S/D* REPAIRED AREA PER FEDEX SR 27-55-008.SDR 01FDEA00233Web · corrodedCORROSION (C53-132-01, -1) BS 850, WL 162, LBL 10. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-10-2, 51-30-2 AND 51-30-5. ALODINED, PRIMED AND PAINTED PER FEDEX PER MM 51-21-152.SDR 01FDEA00226Landing Gear · malfunctionedLANDING GEAR FAILED TO RETRACT. RAN CKLIST, CK CB AND WAS NOT POPPED, ATTEMPT 2ND RETRACT AND WAS SUCCESSFUL. PERF LG HANDLE LOCK SYS ADJUSTMENT AND TEST PER 727-200 MM 32-31-011-5. CK OK. NO BINDING OR STICKING NOTED DURING ACTUATION.SDR 01FDEA00215Frame · damagedNR N 934 DRILL START IN FRAME BS 720E, STR 7LH. ** S/D ** R&R & FAB & ALODINED & PRIMED PER FEDEX SRM 53-10-4 FIG 2.SDR 01FDEA00216Skin · corrodedCORROSION (C53-111-01, 2) ON SKIN UNDER LEVELING COMPOUND BS 684 O/B OF STR 27R. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 53-30-3 FIG 3.SDR 01FDEA00214Skin · damagedA TEMPORARY REPAIR IS INSTALLED ON FUSELAGE AT BS 216, STR 17R. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-30-3 FIG 5.SDR 01FDEA00213Frame · dentedDENT ON THE FRAME BS 1090, STR 26L. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-40-3.SDR 01FDEA00212Frame · dentedFRAME DENTED AT BS 680 BETWEEN STR 23 LT AND 24 LT. *S/D* REMOVED AND REPLACED PER FED-EX SRM 51-40-3 FIG 1.SDR 01FDEA00211Frame · dentedFRAME DENTED AND GOUGED AT BS 520, STR 22 LT - 25 LT. *S/D* REMOVED AND REPLACED PER FED-EX 51-40-3, 51-30-2. ALODINED AND PRIMED ANGLE PER FEDEX MM 51-20-151.SDR 01FDEA00210Frame · dentedBS 600 FRAME DENTED STR 22 LT - 23 LT. *S/D* REMOVED AND REPLACED PER FEDEX SRM 51-40-3.SDR 01FDEA00209Frame · dentedFRAME DENTED AT 500, STR 22 LT, STR 25 LT. *S/D* REMOVED, REPLACED AND FAB PER FEDEX SRM 51-40-3.SDR 01FDEA00217Frame · dentedFRAME 520 DENTED AT RBL 67, WL 212. REMOVED AND REPLACED PER FEDEX SRM 51-40-3.
Back to Boeing 727-233