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 DL72S954052Angle · crackedBULKHEAD ATTACH ANGLE CRACKED AT STR 10 LT SIDE FIN STA 180.600, INSIDE VERT STAB CRAWLWAY. FOUND AT D-2 LTR CK AND REPAIRED PER MM 55-30-0.SDR CAL951008Angle · corrodedINSPECTION FOUND ANGLE CORRODED AT BS 320, LBL 15, WL 179, INSIDE E/E COMPARTMENT AT NOSE WHEEL, LEFT SIDE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M)SDR CAL951002Flange · corrodedINSPECTION FOUND CORROSION AT LOWER FLANGE OF FORWARD CARGO COMPARTMENT, BS 529-740R. THE CORROSION WAS REMOVED, AN L-ANGLE WAS FABRICATED AND INSTALLED IAW AERO CORP ENGINEERING ORDER 95-208, REV IR. (M)SDR CAL950934Actuator Ftg · crackedFLT NR 0219 - EWR - THE 'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO ACCOMPANIED BY ILLUMINATION OF THE LOW PRESSURE LIGHTS DURING CLIMB-OUT OF EWR. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH, FUEL WAS DUMPED, AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDSDR DL72S961609Transverse Beam · crackedTHERE IS A CRACK IN THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1273. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AD 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129.SDR DL72S954045Web · crackedA .5 INCH CRACK AT LT TORQUE BOX WEB LIGHTENING HOLE STA 1243. FOUND DURING E-2 LTR CK TPAMM. REPAIRED PER M/M 53-11-0.SDR DL72S954039Skin · crackedFOUND ON B1 LETTER CK, RT ELEVATOR LWR SKIN CRACKED TWO PLACES, ONE INCH EACH, 12 INCHES FWD OF TAB OUTBD END. REPAIRED PER SRM 55-20-3 FIG 4.SDR CAL951014Stringer · corrodedINSPECTION FOUND FORWARD CARGO COMPARTMENT STRINGER 27R CORRODED AT BS 740. THE CORROSION WAS REMOVED FROM STRINGER AND A STRINGER SPLICE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6. (M)SDR CAL951013Skin · corrodedINSPECTION FOUND LOWER SKIN AND STRINGER CORRODED AFT OF DUCT ATTACH POINT IN FORWARD CARGO COMPARTMENT AT STATION 737, RBL 25. THE CORRODED AREA WAS CUT OUT AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3. (M)SDR CAL951010Support · corrodedINSPECTION FOUND FORWARD CARGO COMPARTMENT LOWER CIRCUMFERENTIAL SUPPORT CORRODED AT BS 740, RBL 5, S28R TIE IN. THE CIRCUMFERENTIAL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-1 AND 51-30-2. (M)SDR DL72S954139Girt Bar Hook · brokenON DEPARTURE, FWD ENTRY DOOR SLIDE GIRT BAR HOOK BROKEN, REPLACED HOOK, OPERATION NORMAL.SDR CAL951012Stringer · corrodedINSPECTION FOUND STRINGER 24R CORRODED AT ATTACH POINT IN FORWARD CARGO COMPARTMENT, BS 738, RBL 40. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW SECTION AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-5. (M)SDR CAL951006Frame · crackedINSPECTION FOUND A 2 INCH CRACK IN CIRCUMFERENTIAL BY INNER FLANGE ABOVE S25L AT BS 970. AN L-ANGLE AND SPLICE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (X)SDR DL72S954146Skin · corrosionCORROSION WAS FOUND ON THE RAM AIR ACTUATOR ACCESS DOOR CUT-OUT AT THE FWD LT CORNER AND LT SIDE OF THE AFT EDGE. THE SKIN IS 0.168 INCH (MEASURED) CLAD 2024-T3 AND IS CHEM MILLED AROUND THE DOOR TO 0.085 INCH (MEASURED). ACCOMPLISHED REPAIRS PER DL ERA 3026SDR CAL951009Former · crackedINSPECTION FOUND A 6 INCH CRACK IN FORMER AT STATION 1345 ABOVE NR 2 ENGINE FIREWALL. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M)SDR CAL951004Skin · corrodedINSPECTION FOUND SKIN CORRODED IN FORWARD CARGO PIT BILGE AT BS 720C TO BS 720D, LBL 20. THE CORROSION WAS REMOVED AND A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-3. (M)SDR DL72S954138Eel Battery Pack · dischargedDURING INSPECTION, RT AFT SERVICE DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK OPERATION NORMAL.SDR DL72S953996Flow Cntl Vlv · failedRIGHT PACK FAILED IN FLIGHT AT FL 250. AIRCRAFT LOST PRESSURIZATION, LT PACK ON MCO. REPLACED AFT FLOW CONTROL VALVE, OPERATION NORMAL.SDR CAL951005Rib · crackedINSPECTION FOUND A 2.8 INCH CRACK IN OUTBOARD SIDE OF RIB AT RIGHT WING STATION 686.5. A U-CHANNEL REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-5. (M)SDR DL72S953990Angle · crackedFOUND DURING F-1 LETTER CHECK, .25 INCH CRACK IN RADIUS FROM UNDER BLOCK STA 910 RT MLG UPLOCK H-BRACKET FWD SUPPORT ANGLE. REPAIRED PER M/M 53-11-0 PG 834 AND 835.SDR DL72S953989Eel Battery Pack · dischargedLEFT CENTER OVERWING EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AT M954, OPERATION NORMAL.SDR DL72S953982Door · crackedA FIVE INCH CRACK WAS FOUND IN THE R-1 DOOR. THE CRACK EXTENDED FROM THE UPPER AFT CORNER DOWN THE AFT FRAME. REPAIR INCLUDED DOOR REPLACEMENT.SDR CAL951011Frame · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FRAME AROUND RADIUS TO TOOL HOLE AT BS 970 BETWEEN S26L AND S27L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-30-3 AND 51-40-2. (M)SDR DL72S954053Angle · corrodedFOUND ON CV2 CHECK, CORROSION ON SKIN SUPPORT ANGLE STA 740 AND RBL 10. REPAIRED PER M/M 53-11-0 PG 858, REPLACED SKIN SUPPORT ANGLE.SDR DL72S953979Angle · crackedFOUND ON CV2 CHECK, COVE SKIN SUPPORT ANGLE CRACKED AT INBD STOP PAD NR 6 SLAT. REPAIRED PER M/M 57-54-0 FIG 816.SDR DL72S953978Angle · crackedFOUND ON CV2 CHECK, COVE SKIN SUPPORT ANGLE CRACKED AT INBD STOP PAD NR 7 SLAT. FASTENERS LOOSE OUTBD SLAT TRACK FAIRING NR 7 SLAT. REPAIRED PER M/M 57-54-0 2. REPLACED FASTENER.SDR DL72S960540Skin · crackedUPON SHOP INSPECTION, FOUND OUTER SKIN AND FRAME CRACKED AT UPPER FORWARD CORNER. REPAIRED SKIN PER SRM 52-00-3, FIG 4 AND REPAIRED FRAME PER MM 52-12-0, FIG 805, FOR R-1 SERVICE DOOR.SDR DL72S953957Floor Beam · corrodedFOUND ON CV2 CHECK, CORROSION ON FLOOR BEAM CORRODED AT STA 400 BETWEEN BL ZERO AND RBL 44. REPAIR: REPAIRED PER MM 53-20-11, FIG 804 A.SDR DL72S953953Frame · misdrilledDURING ACCOMPLISHMENT OF THE MODIFICATION TO THE OVER-WING EXIT FRAME AT STA 761 ON THE LEFT SIDE, THE ADDED FASTENER HOLES THROUGH THE REPAIR ANGLE WEB AND FRAME WERE OVERSIZED TO .25 INCH.SDR CAL951007Web · corrodedINSPECTION FOUND CORROSION IN WEB, AFT FRAME OF AFT CARGO DOOR ABOVE S27R, BS 1114-BS 1148. THE CORROSION WAS REMOVED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (X)SDR DL72S953933Rib · crackedRIB CRACKED-NR 2 SLAT RIB MARKED NR 11 CRACKED AT LOWER ATTACH ANGLE. CORRECTION-FABRICATED REPAIR PER M/M 57-54-0, PG 805.SDR DL72S953927Cove Angle · crackedDURING F-1 LTR CHECK, FOUND NR 8 SLAT COVE ANGLE CRACKED BELOW ANTI-ICE DUCT. REPAIRED PER M/M 57-54-0.SDR CAL951015Attach Fitting · corrodedINSPECTION FOUND CORROSION ON AND UNDER FORWARD CARGO DOOR THRESHOLD FORWARD ATTACH FITTING AT BS 560-566. THE FITTING AND CLIP ASSEMBLY UNDER FORWARD CARGO DOOR THRESHOLD WERE REMOVED AND REPLACED IAW SRM 52-10-1 AND 53-10-1. (M)SDR DL72S954042Rib · crackedATL - HMV, NR 6 SLAT I/B RIB AT INBOARD SLAT TRACK CRACKED IN LWR RADIUS. REMOVED FASTENERS FROM REPAIR AREA, FABRICATED REPAIR PER 57-54-0 FIG 805.SDR CAL951003Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN FRAME AT BS 520 ABOVE STRINGER 24L. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4. (M)SDR DL72S953956Skin · gougedDURING SHOP INSPECTION, NR 1 L/E SLAT WAS FOUND WITH LOWER SKIN GOUGED AT ACTUATOR ATTACH RIBS. REPAIRED PER SRM 57-50-3.SDR DL72S953923Skin · wornUPON HMV, FOUND SKIN WORN ON SECTION OF SKIN UNDER LIFT FENCE NR 4 SLAT. REPAIRED PER MM 57-54-0 PG 817.SDR DL72S953907Eel Battery Pack · dischargedRIGHT CENTER OVERWING EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, OPERATION NORMAL.SDR DL72L961610Transverse Beam · crackedA CRACK IN THE ANGLE ON THE LOWER TORQUE BOX FS 1263 TRANSVERSE BEAM FORWARD RIGHT HAND SIDE. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AD 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS REPLACEMENT DOES NOT TERMINATE THE REPETITIVE INSPECTION SDR DL72L953924Eel Pwr Supply · failedDURING DEPARTURE CHECK, EMERGENCY TRACK LIGHT IN FWD CABIN DO NOT TEST. REPLACED BATTERY PACK M9026, OPERATION NORMAL.SDR DL72S960061Fairing · crackedTHE O/B TRACK FAIRING WAS CRACKED. REPAIRED AS PER MM 57-54-0 FOR NR 3 L/E SLAT.SDR DL72S960036Cove Panel · crackedDURING A SHOP INSPECTION, A CRACK WAS FOUND ON A COVE PANEL LOCATED AT THE I/B UP STOP ATTACH POINT. A REPAIR WAS INSTALLED PER THE M/M 57-54-0, FOR NR 3 L/E SLAT.SDR DL72S960035Rib · crackedDURING A SHOP INSPECTION, A CRACK WAS FOUND ON THE NR 3 RIB AT THE I/B TRACK ATTACH. A REPAIR WAS INSTALLED PER THE M/M 57-54-0 PG 807, FOR NR 3 L/E SLAT.SDR DL72S954043Gate Beam · crackedAT HMV, FWD ENTRY DOOR UPPER GATE BEAM CRACKED AT AFT CORNER STOP LUG. REPLACED UPPER GATE BEAM AND INSTALLED REPAIR PER MM 52-11-01.SDR DL72S953883Window · arcingAT FL 330 HAD BURNING OR SOLVENT TYPE ODOR. THE PROBLEM WAS INTERMITTENT, DECIDED TO DIVERT LAS. FOUND R4 WINDOW ARCING WHEN WINDOW HEAT WAS ON. DEACTIVATED WINDOW HEAT, PLACED ON MCO AND WINDOW WAS REPLACED.SDR DL72L953893Bracket · crackedDURING D-1 LETTER CHECK, FOUND NR 2 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED AT UPPER AND LWR CORNERS, I/B SIDE. REPAIRED PER M/M 57-20-21 PAR 12.SDR DL72S953865Skin · oversized holeUPON INSPECTION, AN OVERSIZED HOLE WAS FOUND IN SKIN OF LEFT O/B AILERON. REPAIRED PER SRM 57-51-0 PG 801.SDR DL72S953856Flap · crackedDURING INSPECTION, FOUND NR 3 KRUEGER FLAP WITH TIME LIMITED REPAIR AT O/B GATE HINGE CUTOUT. REPAIRED PER MM 57-53-0.SDR DL72L953881Angle · crackTHERE IS A .3750 CRACK ON THE RIGHT FORWARD AIRSTAIR TORQUE BOX ANGLE AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-0708, WHICH REQUIRES INSPECTION PER S/B 53-0129.SDR DL72S960030Ribs · crackedDURING INITIAL SHOP INSPECTION, FOUND RIBS NR 16 AND 17 CRACKED AT UPPER FORWARD CORNER. REPAIRED CRACKED AS PER MM 57-54-0.
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