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 DL72S021208Skin · crackedFUSELAGE / SKIN / FS 681-740 / STRG. 4R / SKIN LAP SPLICE : CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 & 740 REVEALED CRACK INDICATIONS. INTERNAL MFEC INSPECTION REVEALED SDR DL72S021207Skin · crackedFUSELAGE / SKIN / FS 481-681 / STRG. 4R / SKIN LAP JOINT : CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP JOINT REVEALED CRACK INDICATIONS BETWEEN FS 481 & 681. INTERNAL MFEC INSPECTION REVEALED SDR DL72S021198Skin · crackedFUSELAGE / SKIN / FS 1070-1090 / STRG. 4R / SKIN LAP JOINT: CRACK REPAIR LFEC INSPECTIONS OF THE STRINGER 4R SKIN LAP JOINT REVEALED A CRACK INDICATION. INTERNAL MFEC INSPECTION DETERMINED A SINGLE SDR DL72S021190Battery Pack · dischargedON LAYOVER CHECK FOUND LEFT OVERWING EMERGENCY LIGHT DIM WHILE PERFORMING EMERGENCY LIGHTS CHECK. REPLACED BATTERY PACK.SDR DL72S021180Smoke Detector · false activationFWD CARGO- FWD SMOKE DETECTOR RED LED LIGHT ON. REPLACED DETECTOR.SDR DL72S021175Battery · dischargedLT SIDE OVERWING EMERGENCY LIGHTS DID NOT ILLUMINATE DURING LAYOVER TEST. REPLACED BATTERY PACK PER M/M. CKS OK.SDR DL72S021172Actuator · leakingAFTER NORMAL LANDING WHILE TAXIING OFF THE RUNWAY, THE CAPT LOST NOSE STEERING. CHECKED A SYSTEM HYD, NO PRESSURE NO FLUID REMOVED AND REPLACED NOSE LOCK ACTUATOR REF MM 32-33-011-4 AND OPS AND LEAK CHECK GOOD.SDR DL72S021164Light · inoperativeSEAT 10DEF EMERGENCY EGRESS LIGHT INOP, RELAMPED.SDR DL72S021146Warning System · malfunctionedON T/O ROLL, SPEED LESS THAN 60KTS, T/O POWER ESTABLISHED 1.94 EPR. THE NR 3 THRUST REV OPERATING LIGHT ILLUMINATED. T/O DISCONTINUED. AFTER CLEARING RUNWAY WITH ENGINE AT IDLE POWER THRUST REV OPERATING LIGHT WENT OUT. T/S THRUST REV OPERATING LIGHT SWITCSDR DL72S021144Frame · crackedTHE INNER CHORD OF THE FS 1303 FRAME WAS FOUND CRACKED AT A HYDRAULIC LINE CLAMP ATTACHMENT LOCATION JUST ABOVE RT VENTRAL STAIRWAY TORQUE BOX STRUCTURE. THE CHORD WAS CUT ABOVE THE DAMAGE AND THE LOWER SECTION OF CHORD REMOVED. A NEW SECTION OF CHORD WAS INSDR DL72S021139Hydraulic Line · chafedTHE HYD SYSTEM B HAD ZERO PRESSURE AND ZERO QUANTITY. FOUND THE B HYD SYSTEM QUANTITY AT .9 ON ARRIVAL, AND FOUND THE NR 2 B HYD PUMP PRESSURE LINE CHAFED, REPLACED THE LINE AND ALSO CHECKED THE CASE DRAIN FILTER WITH NO DEFECTS, LEAK CHECK AND OPS CHECK GOSDR DL72S021133Battery · dischargedAFT OVERHEAD ISLE EMERGENCY LIGHT INOP. REPLACED BATTERY OPS CHECK GOOD.SDR DL72S021111Battery · dischargedRT OVERWING EMERGENCY LIGHTS INOP. REPLACED 5 BATTERY PACKS AND 1 POWER RACK.SDR GAIA02108OPClamp · looseFLT 778 - FWA-BOS - DURING CRUISE, THE NR 1 ENGINE STRUT LIGHT ILLUMINATED. ACCOMPLISHED AOM PROCEDURE AND THE LIGHT EXTINGUISHED. THE AIRCRAFT CONTINUED TO BOS AND LANDED WITHOUT FURTHER OCCURRENCE. FOUND A LOOSE CLAMP AT THE SIXTH STAGE CHECK VALVE IN THESDR DL72S021079Charger · inoperativeOVERWING EMERGENCY EXIT LIGHTS INOP IN EMERGENCY MODE. REMOVED AND REPLACED CHARGER ON RIGHT SIDE, BATTERY ON LEFT SIDE AND EMERGENCY LIGHT ASSEMBLY ON RIGHT OVERWING EXIT.SDR DL72S021072Battery Pack · dischargedAFT EMERGENCY EXIT IDENTIFIER INOP. REPLACED BATTERY PACK.SDR DL72S021051Light · inoperativeDURING L/O CHECK FOUND RIGHT OVERWING EMERGENCY LIGHT INOP RELAMPED. OPS CKS GOOD.SDR DL72S021049Battery · weakR1 OVERHEAD EMERGENCY LIGHT BARELY ILLUMINATES REPLACED BATTERIES OPS CK OKSDR DL72S021034Web · crackedCRACK ON O/B WEB OF #1 SLAT ACT. MOUNT BRACKET REPAIR PER M/M 57-20-021-8SDR DL72S020917Valve · wornAIR RETURN TO CVG FOR HIGH OIL TEMP NUMBER 1 ENG. REPLACED FUEL HEAT VALVE, OP CHECKS NORMAL.SDR DL72S020916Stringer · crackedFUSELAGE / STRINGER / 18A / FS 920-950 : FATIGUE CRACK REPAIR STRINGER 18A WAS FOUND WITH A 4" TYPICAL FATIGUE CRACK AT FS 950. THE STRINGER WAS CUT AT FS 921 AND THE AFT END REMOVED TO ELIMINATESDR COOSDR020218Skin · delaminatedNOSE LANDING GEAR LEFT AFT DOOR DELAMINATED SKIN.SDR COOSDR020217Skin · delaminatedLEFT WING OUTBOARD AILERON TRAILING EDGE DELAMINATED.SDR COOSDR020216Bulkhead · crackedAFT CARGO COMPARTMENT PRESSURE BULKHEAD, CRACKED.SDR COOSDR020221Flap Track · brokenRT WING, INBOARD FLAP, NR 5 MOVABLE FAIRING INBOARD FAIRING TRACK, BROKEN.SDR DL72S020890Skin · crackedDURING LAYOVER, MAINTENANCE FOUND A 1 INCH LONG CRACK IN THE FUSELAGE SKIN BETWEEN TWO FASTENERS AT S-30 BETWEEN FS 990 AND 1009. THE SUBJECT CRACK WAS REMOVED AND AN EXTERNAL DOUBLER INSTALLED. THE REPAIR INCORPORATED AN EXISTING REPAIR INSTALLED PER PREVIOSDR DL72S020866Battery Pack · dischargedLEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY RACK.SDR DL72S020865Battery · dischargedEMERGENCY EXIT LIGHT OVER AFT RT DOOR INOP. REPLACED BATTERY AND RACK. ALSO SECURED GROUND.SDR DL72S020860Skin · crackedTHE LT BOX SKIN OF THE VERTICAL STABILIZER WAS FOUND WITH A CRACK EMANATING FROM A FASTENER COMMON TO THE REAR SPAR LOCATED 1 INCH ABOVE THE FUSELAGE SKIN INTERFACE. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383575-14,SDR DL72S020846Spar · crackedAT F-I LETTER CK FOUND .375 INCH CRACK NR 2 SLAT AT TAI DUCT CUTOUT, INBOARD CORNER. REPAIRED PER M/M 57-54-000-8 FIG 802A.SDR DL72S020845Rib · crackedAT F-1 LETTER CK FOUND DOUBLER CRACKED #4 SLAT INBD ACTUATOR ATTACH NOSE RIB FOUND DOUBLER INCORRECTLY SHIMMED, RESHIMED AND REPLACED DOUBLER PER M/M 57-54-000-8 FIG 804SDR DL72S020844Angle · crackedFOUND ON F1 LETTER CK LOWER COVE SKIN ATTACH ANGLE IS CRACKED AT NUMBER 6 SLAT BELOW ACTUATOR. REPAIRED PER MM 57-54-000-8SDR DL72S020832Angle · crackedFOUND ON E1 LETTER CK. 1 INCH CRACK AT COVE SKIN ATTACH ANGLE NBR 6 SLAT BELOW ACTUATOR ROD REPAIRED PER M/M 57-54-000-8 FIG 805A,SDR DL72S020831Angle · crackedFOUND ON E1 L/C 1.25 INCH CRACK NBR 5 SLAT COVE SKIN ATTACH ANGLE AT INBD END REPAIRED PER M/M57-54-000-8 FIG 805ASDR DL72S020828Skin · crackedFOUND ON E-1 LETTER CK SKIN CRACKED AT BASE OF VERTICAL STAB RT SIDE ABOVE FWD END OF NUMBER 2 ENG CUTOUT AT STR 10. REPAIR PER MM 55-30-000-8.SDR DL72S020819Spar · damagedNR 2 MID FLAP REMOVED FROM AC 533 DURING HMV. AFT SPAR RAIL REPAIRED PER M/M 57-52-0 FIG 802.SDR C7WA200200005Skin · dentedDURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE BS 310 BETWEEN STRINGER 23R AND 24R SKIN WITH DENT OUT OF LIMITS. REPAIRED FUSELAGE SKIN SECTION FROM BS 312.5 TO BS 308 BETWEEN STRINGER 23R AND 24R IAW SRM 53-30-3 FIG 13. (M)SDR C7WA200200004Skin · dentedDURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE BS 40 BETWEEN STRINGER 19R AND 20R SKIN WITH DENT OUT OF LIMITS. INSTALLED REPAIR IAW SRM 53-30-3 FIG 13. (M)SDR C7WA200200027Skin Panel · delaminatedDURING C-CHECK INSPECTION, FOUND LT WING OUTBOARD AILERON TRAILING EDGE PANEL DELAMINATED. REPAIRED LEFT WING OUTBOARD AILERON IAW COOPESA EO COO0CMP-2-57-366-02 WITH DER APPROVAL. (M)SDR C7WA200200026Skin · delaminatedDURING C-CHECK INSPECTION AT , FOUND NLG LEFT AFT DOOR DELAMINATED. REPAIRED DELAMINATION IAW COOPESA EO COO-CMP-2-52-369-02 WITH DER APPROVAL. (M)SDR C7WA200200025Skin · crackedDURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN CRACK AT BS 196.5 WL 217. REPAIRED FUSELAGE SKIN FROM BS 191.5 TO BS 203.0 BETWEEN WL 212.5 AND WL 222.5 LBL 38.0 IAW S/B 727-53-0183 SECTION III PART I PARA C. (M)SDR C7WA200200024Skin · crackedDURING C-CHECK INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 203.8 BETWEEN RIGHT WL 219 AND WL 220. REPAIRED FUSELAGE SKIN FROM BS 191.0 TO BS 209.0 BETWEEN WL 214 AND 224.5 RBL 38.0 IAW S/B 727-53-0183 SECTION III PART I PARA C. (M)SDR C7WA200200022Skin · crackedDURING C-CHECK INSPECTION, FOUND FORWARD ENTRY DOOR OUTER SKIN UPPER HINGE AREA CRACKED. REPAIRED FORWARD ENTRY DOOR SKIN FROM BS 325 TO BS 316 UPPER HINGE CUTOUT IAW SRM 52-00-3 FIG 4. (M)SDR C7WA200200023Skin · corrodedDURING C-CHECK INSPECTION, FOUND EXT FUSELAGE SKIN BULGED AT BS 950F PLUS 10.0 AT STRINGER 4R. REPAIRED FUSELAGE SKIN LEVEL 2 CORROSION FROM BS 950F PLUS 8.00 TO BS 950F PLUS 19.5 BETWEEN STRINGER 3R AND STRINGER 5R IAW SRM 53-30-3 FIG 14 DETAIL IV. (M)SDR C7WA200200021Skin · dentedDURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENT AT BS 360 BETWEEN STRINGER 16L AND 17L. REPAIRED FUSELAGE SKIN FROM BS 360 TO BS 371.50 BETWEEN STRINGER 16L AND STRINGER 21L IAW SRM 53-30-4 FIG 12. (M)SDR C7WA200200020Skin · dentedDURING C-CHECK INSPECTION, FOUND DENT AT BS 421 BETWEEN STRINGER 16R AND 17R. REPAIRED FUSELAGE SKIN FROM BS 416.25 TO BS 428 BETWEEN STRINGER 16R AND STRINGER 18R IAW SRM 53-30-3 FIG 3. (M)SDR C7WA200200019Bulkhead · crackedDURING C-CHECK INSPECTION, FOUND FUSELAGE BS 178 BULKHEAD WITH CRACK BETWEEN LBL 4.00 AND LBL 10.00 BETWEEN WL 232.T AND WL 238.5. REPAIRED CRACKED WEB IAW SRM 53-10-9 FIG 4. (M)SDR C7WA200200018Stringer · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FS STRINGER 26L BETWEEN BS 480 AND BS 720D. REPAIRED FUSELAGE STRINGER 26L FROM BS 480 TO BS 680 IAW SRM 53-10-3 FIG 1. (M)SDR C7WA200200017Stringer · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 25R BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 25R FROM BS 720D PLUS 5.00 TO BS 740 IAW SRM 53-10-3 FIG 3. (M)SDR C7WA200200016Stringer · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 22R BETWEEN BS 720 AND BS 740. REPAIRED FUSELAGE STRINGER 22R BETWEEN BS 720E PLUS 1.50 TO BS 740 IAW SRM 53-10-3 FIG 1. (M)
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