Boeing 727-232
Service difficulty reports · 6,539
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 = '727232' 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 = '727232' 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 DL72S960251Rib · crackedDURING SHOP INSPECTION FOR LEADING EDGE SLAT NR 6, RIBS NR 5 AND NR 13 FOUND TO BE CRACKED. REPAIRED RIBS PER M/M 57-54-0 FIG 805.SDR DL72S954596Rib · crackedDURING SHOP INSPECITON, NR 4 L/E SLAT WAS FOUND WITH CRACKED RIB AT I/B SIDE OF ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0 FIG 805.SDR DL72S954558Skin · bentLOWER SKIN BENT AND A PIECE MISSING AT THE ACTUATOR RIBS LOCATION. INSTALLED DOUBLER PER M/M 57-54-0, FIG. 815, DURING SHOP VISIT, FOR NR 4 L/E SLAT.SDR DL72S954549Rib · crackedDURING SHOP INSPECTION, NR 6 L/E RIB WAS FOUND WITH L/E SUPPORT RIBS NRS 3, 4, 7, 8, 10 AND 12 CRACKED. REPAIRED PER MM 57-54-0.SDR DL72S954547Hyd Module · leakingON CLIMB-OUT, ELEV FEEL DIFFERENTIAL PRESS LIGHT BEGAN TO FLICKER, HYDRAULIC PRESSURE AND QUANTITY GOOD ON ALL SYSTEMS, ABOUT 5 MINUTES LATER, THE HYDRAULIC SYSTEM-A OVERHEAT LIGHT ILLUMINATED. TURNED NR 1 PUMP BACK ON, WAS GOOD FOR ABOUT 2 MINUTES, AND LIGHTSDR DL72K961587Angle · crackedTHERE IS A 2.5 CRACK IN THE ANGLE OF BOTH THE FWD AND AFT TRANSVERSE BEAMS OF THE RT TORQUE BOX AT FS 1273. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE TSDR 95FDEA01827Floor Beam · corrodedCORROSION AROUND FASTENER HOLES ON BS 950F, FLOOR UPPER CHORD, RBL 10-RBL 21, WL 208. REPAIRED BS 950F FLOOR BEAM AT RBL 10, WL 208 IAW FEDEX EA 7-5310-26291. C/A ADDITION.SDR 95FDEA01826Web · corrodedWHILE WORKING NR0676, FOUND CORROSION ON AFT SIDE OF WEB STA 219.8 WL 214 TO 222 LBL 44.SDR 95FDEA01825Floorbeam · corrodedCORROSION AROUND FASTENER HOLES ON TOP CHORD OF FLOORBEAM AT BS 720A RBL 21 LBL 10, 16 AND 21 WL 208.SDR 95FDEA01822Str Clip · crackedCRACKED STR CLIP AT BS 600 STR 4R. REMOVED AND REPLACED CRACKED STR CLIP AT BS 600 4R IAW FEDEX SRM 53-10-4.SDR 95FDEA01821Floorbeam · corrodedCORROSION AROUND FASTENER HOLE ON TOP CHORD OF FLOORBEAM AT BS 540 LBL 10.5 WL 208. REMOVED CORROSION AROUND FASTENER HOLE ON TOP CHORD OF FLOORBEAM AT BS 540 LBL 10.5 WL 208. DAMAGE WAS FOUND TO BE BEYOND LIMITS PER FEDEX SRM 53-10-1. REPAIRED DAMAGED AREASDR 95FDEA01817Frame · double drilledDOUBLE HOLE IN FRAME WEB BS 1010, WL 295, LBL 33. REMOVED DAMAGED AREA, INSTALLED REPAIR IAW FEDEX SRM 53-10-4. C/A ADDITION.SDR 95FDEA01799Stringer · corrodedCORROSION (C53-111-01-, 3), ON STR 20L AT BS 1042 TO 1048. REMOVED CORROSION ON STR 20L AT BS 1042 TO 1048. FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED STR 20L PER FEDEX SRM 53-10-3.SDR DL72S954659Inlet Skin · damagedNR 2 ENGINE INLET EXT SKIN RIGHT SIDE TEMPORARY REPAIR DOUBLER AT LWR AFT CUTOUT FOR PANEL 9516. MANUFACTURED NEW DOUBLER PER M/M 54-30-0. INSTALLED REPAIR PER M/M 54-30-0.SDR DL72S954622Stringer · damagedFROM ATL/HMV - STR 29L HAS TOOLING DAMAGE AT STA 1000. CORRECTION: FORMED REPAIR DOUBLER AND BEGAN DRILLING DOUBLER. ROUTED OUT DAMAGE, FABRICATED FILLER PER M/M 53-12-0, FIG. 806. OK TO INSTALL REPAIR. INSTALLED DOUBLER PER M/M 53-12-0.SDR DL72S954536Eel · inoperativeAFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY.SDR DL72S954499Rib · crackedDURING ROUTINE SHOP INSPECTION A CRACK WAS FOUND IN THE 16TH RIB AND A DOUBLER WAS INSTALLED USING MM 57-54-0 FOR NR 6 L/E SLAT.SDR DL72K954537Hyd Module · crackedFOUND DURING A-2 LETTER CHECK - CHECK VALVE BROKEN/BLOWN AT BASE OF A-SYSTEM PRESSURE MODULE. REPLACED A-SYSTEM MODULE, P/N 294001002.SDR 95FDEA01833Skin · dentedDENT IN SKIN AT BS 230 BETWEEN STR 24-25L. MEASURED DEPTH OF DENT AT .7 INCH BY .035 INCH FOUND TO BE OUT OF LIMITS. REPAIRED DENT PER FEDEX SRM 53-30-3, FIG 13, PG 74-74D. DENT FOUND OUT OF LIMITS PER FEDEX SRM 53-30-1.SDR 95FDEA01832Frame · dentedDENT IN TOP OF FRAME AT BS 500, LBL 32, WL 158. REPAIRED FRAME AS PER FEDEX SRM 51-40-3 AND 53-10-2 AT BS 500, LBL 32, WL 158.SDR 95FDEA01820Floorbeam · corrodedCORROSION (C53-224-01), ON FLOORBEAM UPPER CHORD AT BS 950D LBL 20 RBL 20 WL 208.1. REPLACED UPPER CHORD FROM BS 950D FLOORBEAM RBL 20 LBL 15 WL 208.1, WORK DONE IAW FEDEX SRM 53-10-8 FIG 3.SDR 95FDEA01819Beam · corrodedCORROSION AT BS 750 BEAM UPPER CHORD FROM LBL 27 RBL 27 WL 208.1.SDR 95FDEA01818Failsafe · corrodedCORROSION ON FAILSAFE AT BS 1030, LBL 65, WL 189. REPAIRED FAILSAFE AT BS 1030, LBL 65, WL 189 IAW FEDEX SRM 51-40-4.SDR DL72S960582Rib · crackedLOWER AFT CORNER OF NR 2 RIB FROM OUTBOARD END CRACKED. REPAIRD PER MM 57 54 0, FIG 814, DURING SHOP INSPECTION FOR NR 5 L/E SLAT.SDR 95FDEA01824Shear Tie · corrodedCORROSION (C53-224-04) ON SHEAR TIE BS 1010, STR 7L. REMOVED CORROSION FROM SHEAR TIE FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-1. FABRICATED AND INSTALLED NEW SHEAR TIE AT BS 1010, STR 7L.SDR DL72S954698Angle · damagedUPON HMV, FOUND NR 2 ENG PYLON CIRCUMFERENTIAL ANGLE FOR MOUNTING SURFACE OF FWD COWL HAS TEMPORARY REPAIR INSTALLED. FABRICATED AND INSTALLED NEW ANGLE PER MM 53-11-0.SDR DL72S954483Duct · rupturedFLT DIVERTED INTO DCA AT FL 350, CABIN ALT 5,600 FT, AFTER ABOUT 10 MIN OF LITE VIBRATION OF UNKNOWN ORIGIN, CABIN CLIMBED AT 500 FT/MIN AND UNABLE TO CONTROL IN ANY MODE OF PRESS. ACCOMPLISHED LOSS OF PRESS AND EMERGENCY DESCENT CK LIST AT 10,000 FT, CABIN CSDR DL72S954482Ballast · failedLOG ITEM 2, ELECTRICAL SMELL IN MID CABIN POPPED LT AFT CABIN CEILNG LIGHT C/B. FOUND BALLAST AT STA 910 INTERNALLY SHORTED CAUSING BURNT ELECTRICAL SMELL IN CABIN. REPLACED BALLAST, OPERATION NORMAL.SDR DL72S954658Inlet Skin · damagedTIME LIMITED REPAIR INSTALLED AT NR 2 ENGINE INLET DUCT HOUSING RT SKIN AT LOWER AFT CORNER OF ACCESS PLATE 9516 CUTOUT REF NR 86 PER M/M 54-30-0 PG 802. REPAIRED PER M/M 54-30-0 REF NR 861.SDR DL72S954476Angle · crackedFOUND DURING B-1 LETTER CHECK, NR 5 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED .25 INCH AT O/B END. REPAIRED PER M/M 57-54-0 PAR 5A.SDR DL72S954475Actuator Mount · crackedFOUND DURING B-1 LETTER CHECK, NR 7 L/E SLAT ACTUATOR MOUNT FITTING CRACKED 1 INCH AT LWR I/B MOUNT BOLT. REPAIRED PER M/M 57-42-0 PAR 5.SDR DL72S954473Spar Stiffener · crackedFOUND ON B1 LETTER CK, LE SPAR STIFFENER CRACKED OUTBD TRACK NUMBER 3 SLAT INBD ANGLE. REPAIRED PER MM 57-20-21.SDR DL72S960175Rib · crackedDURING INSPECTION, NR 8 LE SLAT WAS FOUND WITH INTERNAL RIB NR 3 AND NR 2 CRACKED. REPAIRED PER MM 57-54-0.SDR DL72S954469Act Fitting · crackedFOUND DURING E-1 LETTER CHECK, NR 2 SLAT ACTUATOR O/B ATTACH FITTING BROKEN AT I/B ATTACH BOLT AREA. REPAIRED PER ERA 302790-14 CODE 4-57-45.SDR DL72S954467Angle · crackedA .25 INCH CRACK AT COVE SKIN ANGLE FOR NR 2 SLAT AT ANTI-ICE DUCT. FOUND DURING E-1 LTR CK TPAMM AND REPAIRED PER 57-54-0.SDR DL72S954466Web · crackedLWR LT TORQUE BOX VERT WEB CRACKED .375 INCH AT LWR FWD LIGHTENING HOLE NEXT TO EXISTING DOUBLER. FOUND DURING E-1 LTR CK TPAMM AND REPAIRED PER M/M 53-11-0.SDR DL72S954465Act Fitting · crackedNR 2 SLAT ACTUATOR O/B ATTACH FITTING BROKEN AT UPPER ATTACH BOLT AREA. FOUND DURING E-1 LTR CK TPAMM AND REPAIRED PER 57-42-0 AND ERA 302790-14.SDR 95FDEA1801Chord · corrodedCORROSION AT BS 430 BEAM LOWER CHORD LBL 46 LBL 52 WL 801.SDR 95FDEA1800Stringer · corrodedCORROSION (C53-224-01), ON STRINGER NR 5 RT AT BS 600 TO 740.SDR 95FDEA1799Stringer · corrodedCORROSION (C53-111-01-3), ON STRINGER AT BS 1042 TO 1048.SDR 95FDEA1798Stringer · corrodedCORROSION (C53-224-04), ON STRINGER AT BS 1133 AND 1139 STR 6 RT.SDR 95FDEA1797Floorbeam · corrodedCORROSION (C53-111-01-3), ON BOTTOM CHORD OF FLOORBEAM AT BS 1070 WL 200 RBL 51 LBL 42 AT NUTPLATE HOLES.SDR 95FDEA1796Gusset · crackedGUSSET AT FRAME BS 825.95 IS CRACKED RBL 65, WL 198.SDR 95FDEA01770Stringer · corrodedCORROSION (C53-224-04), ON STR 7R BS 1126. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-1. REPAIRED STRINGER IAW FEDEX SRM 53-10-3 AND EA 7-5310-26724.SDR 95FDEA01769Floor Beam · corrodedCORROSION (C53-111-01(3)) ON BOTTOM CHORD OF FLOOR BEAM BS 1130, LBL 43-RBL 51, WL 200 AT NUTPLATE HOLES. REMOVED CORROSION ON BOTTOM CHORD OF FLOOR BEAM BS 1130, LBL 43-RBL 51. CORROSION FOUND TO BE OUT OF LIMITS AS PER FEDEX SRM 53-10-1. REPAIRED BOTTOM CSDR 95FDEA01768Floorbeam · corrodedCORROSION (C53-111-01, 2), ON BOTTOM CHORD OF FLOORBEAM BS 1148 LBL 21 RBL 12 WL 200 AT NUTPLATE HOLES. REPAIRED BOTTOM CHORD OF FLOORBEAM BS 1148 LBL 21 RBL 12 WL 200 AT NUTPLATE HOLES PER FEDEX SRM 53-10-1 AND 53-10-8 THAT WAS OUT OF LIMITS.SDR DL72S954637Stiffener · crackedFOUND ON CV2 CHECK, 1 INCH CRACK IN LOWER END OF SPAR STIFFENER ON INBOARD SIDE NR 6 SLAT OUTBOARD TRACK. REPAIR: REPAIRED PER M/M 57-20-21, PG 813.SDR DL72S954624Skin · crackedFOUND ON CV2 CHECK, PREVIOUSLY STOP-DRILLED CRACK IN SKIN, LT FORWARD AIRSTAIR CUT-OUT. REPAIR: REPAIRED PER M/M 53-30-0.SDR DL72S954623Skin · crackedFOUND ON CV2 CHECK, 1 CRACK IN SKIN OF NR 5 L/E FLAP AT OUTBOARD LOWER LIP HINGE CUTOUT. REPAIR: REPAIRED PER M/M 57-53-0.SDR DL72S954616Skin · wornFOUND ON CV2 CHECK WEAR MARK FROM CONTACT ON UPPER SKIN OF LT HORIZONTAL STABILIZER INBOARD OF ELEVATOR ACTUATOR ACCESS PANEL AND ABOVE BALANCE BOARD BAY NR 1.
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