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 AALA20001188Spar · corrodedTUL - FORWARD LOWER SPAR CORD HAS INTERGRANULAR CORROSION BELOW NR 3 LEADING EDGE FLAP ACTUATOR SUPPORT STRUCTURE. INSTALLED REPAIR PER ESO 11697 DATED 7-7-00. (X)SDR AALA20001187Skin · bulgedTUL - BULGE IN BELLY SKIN STA 708 - STR 27L. INSTALLED REPAIR STA 700 - STA 720 PER ESO 11697 DATED 7-14-00. (X)SDR AALA20001186Stringer · damagedTUL - STR 28L HAS TOOLING DAMAGE 4 INCHES FORWARD STA 950B. CUT OUT DAMAGED AREA, INSTALLED 'U' CHANNEL REPAIR PER SRM 53-10-3 FIG 2 SHEET 3. (X)SDR AALA20001185Frame · gougedTUL - BELT FRAME STA 950C HAS DEEP GOUGE AND SEVERAL DENTS IN FRAME RADIUS BETWEEN STR 25R AND STR 27R. INSTALLED DOUBLER PER SRM 53-10-4. (X)SDR AALA20001197Frame · dentedTUL - DENT IN PREVIOUS REPAIR ON BELT FRAME STA 950F BETWEEN STR 25L AND STR 26L. REPLACED REPAIR SECTION PER SRM 51-40-3. SIZE OF REPAIR 24 INCHES LONG. FASTENER TYPE, SHEAR HILOCKS, FASTENER SIZE .1875 INCH - .25 INCH. NUMBER OF ROWS: 2 ROWS ON SIDE, 1 SDR AALA20001196Frame · dentedCUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-40-3, FIG 1. MATERIAL 7075T6 .050 INCH FASTENERS MS2047006 WITH 5 ROWS PAST DAMAGE USING EXISTING FASTENER HOLES. CUT OUT WAS 1.1 INCH BY 12 INCHES. REPAIR WAS APPROXIMATELY 20 INCHES LONG. (X)SDR 00FDEA00443Warning Light · false indicationNR 1 ENGINE STRUT OVERHEAT LIGHT ILLUM AFT T/O. LIGHT WENT OUT AFT 2 MIN. SYS TEST GOOD. INSPECTED DUCTING AND OVERHEAT LOOP, NO DISCREPANCIES NOTED. TEST GOOD PER MM 26-14-000-5.SDR AALA20001198Frame · crackedTUL - CRACK IN WEB FORWARD CARGO DOOR FRAME AT RIVET HOLE BETWEEN LOWER FORWARD DOOR STOP. INSTALLED DOUBLER PER SRM 51-40-2, FIG 1 WITH MATERIAL 17.7 MT1050 KSI CAD PLATED .050 INCH SIZE 4 INCHES BY 10 INCHES APPROXIMATELY . TYPE FASTENERS BAC30 FPE 8, 10, SDR SCNA00074Bulb · failedDURING FINAL APPROACH WHEN THE LANDING GEAR WAS EXTENDED ONE OF THE GEAR INDICATION LIGHTS FAILED TO ILLUMINATE. THE CREW EXECUTED A GO-AROUND AT MSP. THE CREW CHANGED THE INDICATION BULB, OPERATIONAL CHECKED GOOD, AND LANDED WITHOUT INCIDENT.SDR AALA20001065Light · defectiveTPA DURING OVERNIGHT MAINTENANCE AFT AIR STAIR EMERGENCY LIGHT INOPERATIVE. REPLACED AFT AIR STAIR EMERGENCY LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION.SDR AALA20001085Skin · dentedTUL - FOUND DENT IN FUSELAGE SKIN AFT OF STATION 1342 BULKHEAD APPROX 24 INCHES ABOVE AIRSTAIR CUT OUT. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3, FIGURE NR 1. (M)SDR SCNA00058Light · missingDURING MAINTENANCE LINE CHECK, THE RIGHT FORWARD OVERWING EXIT DOOR WAS FOUND TO BE MISSING THE EMERGENCY EXIT LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY FOR THE RIGHT FORWARD OVERWING DOOR EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKS GOOD.SDR 00FDEA00394Rib · crackedDURING INSPECTION, NR 4 L/E SLAT WAS FOUND CRACKED AT INBOARD ACTUATOR ATTACH RIB. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3 & 51-30-2.SDR 00FDEA00393Rib · crackedDURING INSPECTION, NR 5 L/E SLAT WAS FOUND CRACKED AT INBOARD ACTUATOR ATTACH RIB. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3 & 51-30-2.SDR 00FDEA00392Rib · crackedDURING ROUTINE INSP, NR 5 L/E SLAT WAS FOUND CRACKED AT O/B ACTUATOR ATTACH RIB. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3 & 51-30-2.SDR AALA20001033Switch · inoperativeDFW - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT SIDE FORWARD OVERWING EMERGENCY EXIT LIGHT SWITCH AT SEAT 25D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)SDR AALA20001026Light · inoperativeMIA - FLT 0393 - BEFORE FLIGHT, EMERGENCY EXIT ESCAPE PATH LIGHTS IN CABIN HAD ONE BULB INOPERATIVE. REPLACED LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)SDR SCNA00056Motor · leakingDURING CRUISE FLIGHT THE A-SYSTEM LOST ALL FLUID, THE FLIGHT CREW EXECUTED EMERGENCY CHECK LIST PROCEDURES. PERFORMED MANUAL FLAP AND GEAR EXTENSION AND LANDED. REMOVED AND REPLACED THE FLAP POWER UNIT HYDRAULIC MOTOR IAW B727 MM CH 275162, OPERATIONAL AND LSDR AALA20000947Landing Gear · lack of lubeMCI - FLT 1379 - DURING LANDING MCI, NOSE GEAR LANDING GEAR FAILED TO FULLY EXTEND. RECYCLED GEAR AND GEAR EXTENDED NORMALLY. LANDED MCI WITHOUT INCIDENT. LUBED NOSE LANDING GEAR, SWUNG NOSE GEAR SEVERAL TIMES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR SCNA00050Outflow Valve · failedAFTER TAKEOFF FROM LAS, THE AIRCRAFT WAS UNABLE TO PRESSURIZE. THE FLIGHT CREW DUMPED FUEL AND RETURNED TO POINT OF ORIGIN LAS. THE RIGHT PACK VALVE WAS REMOVED AND REPLACED, PRESSURE AND LEAK CHECK GOOD ON ENGINE RUN.SDR AALA20000905Stringer · crackedTUL - FOUND STRINGER CORRODED AND CRACKED AT STATION 470 TO 474 STRINGER 19R. REMOVED CORROSION ON STRINGER AT STATION 470 TO 474 STRINGER 19R. INSTALLED STRINGER DOUBLER REPAIR PE SRM 53-10-3. (M)SDR AALA20000901Stringer · corrodedTUL - FOUND CORROSION ON STRINGER 28L BETWEEN STATION 680-690. INSTALLED NEW 12 INCH SECTION OF STRINGER IAW SRM 51-10-1 AND REINSTALLED EXISTING STRINGER SPLICES AT STATION 681 AND STATINO 693. (M)SDR AALA20000902Skin · bulgedTUL - FOUND SKIN BULGING AT EDGE OF DOUBLER STATION 680 BETWEEN STRINGER 28L AND 28R. INSTALLED REPAIR DOUBLER AT STATION 671-690 STATION 28 LEFT PER SRM 53-30-3. (M)SDR AALA20000900Frame · crackedTUL - FOUND 480 FRAME CRACKED STRINGER 26R. STOP DRILLED CRACK AND INSTALLED .040 301.5 DOUBLER PER SRM 51-40-2 DOUBLER CAD PLATED (4 INCH BY 6 INCH, 0.040 INCH 301.5 HARD DOUBLER WITH 2 ROWS OF .1875 1ST OVER HI-LOCKS AROUND CRACK). (M)SDR AALA20000904Casting · crackedTUL - FOUND TOP AFT DOOR STOP CASTING CRACKED. REMOVED AND REPLACED CASTING SRM 51-10-1. (M)SDR AALA20000813Light · inoperativeMIA - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY LIGHT BY REAR EXIT DOES NOT ILLUMINATE DURING TEST. REPLACED OVERHEAD EMERGENCY LIGHT BY REAR EXIT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)SDR AALA20000812Connector · defectiveMIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT AT SEATS 27 TO 28 ON RIGHT SIDE INOPERATIVE. REPLACED BAD CONNECTOR AT SEAT 27. SYSTEM GROUND CHECK NORMAL OPERATION. (M)SDR AALA20000903Keelbeam · crackedTUL - FOUND CRACK IN VERTICAL KEELBEAM ANGLE STATION 870 AT APU MOUNT BRACKET ATTACH. INSTALLED STRAP REPAIR PER SRM 53-10-2 FIG 1 PAGE 26. (M)SDR AALA20000802Connector · brokenDFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHTS IN FIRST CLASS AND FORWARD PART OF COACH INOPERATIVE. REPLACED CONNECTOR IN ROW FORWARD OF EMERGENCY OVERWING EXIT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)SDR AALA2000818Frame · crackedTUL - FOUND STATIO 720D BELL FRAME CRACKED AT INBOARD UPPER RADIUS OF CUTOUT FOR STRINGER 26L. STOP DRILLED CRACK INSTALLED TYPICAL WEB REPAIR PER SRM 51-40-2. (M)SDR AALA2000817Frame · crackedTUL - FOUND BELL FRAME CRACKED UPPER FORWARD RADIUS STATION 720D ABOVE STRINGER 26 RT. INSTALLED DOUBLER PER SRM 51-40-3 FROM 7075-T6 .071 INCH USING 3 ROW OF .1875 INCH HI-LOCKS. (M)SDR AALA2000816Skin · corrodedTUL - FOUND SKIN LAP 26R CORRODED ON OUTBOARD SIDE OF STRINGER 26R STATION 720C-D. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AFTER REMOVAL OF CORRODED AREA IAW SRM 53-30-3 FIG 5. (M)SDR AALA2000815Door Frame · corrodedTUL - FOUND LOWER CARGO DOOR FRAME CORRODED AT STATION 950E AFT SIDE OF BELL FRAME. FABRICATED AND INSTALLED FRAME REPAIR AND STRAP PER SRM 51-00-3. (M)SDR 00FDEA00349Skin · crackedDURING ROUTINE INSPECTION, FUSELAGE SKIN FOUND CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT APPROX 0.4 INCH. REMOVED AND REPLACED PER IAW FEDEX EO 7-5330-7-2345.SDR 00FDEA00348Fitting · corrodedDURING ROUTINE INSPECTION, FITTING ON LOWER SIDE OF DOOR JAMB AREA AT BS 620 BETWEEN STR 25R AND 26R. REMOVED AND REPLACED PER IAW SRM 51-30-2.SDR 00FDEA00347Angle · crackedDURING ROUTINE INSPECTION, ANGLE FOUND CRACKED AT BS 560, FROM STR 25R IN DOOR JAMB AREA. REMOVED, FABRICATED AND INSTALLED PER IAW SRM 51-20-1 & SRM 51-30-2.SDR 00FDEA00346Fitting · corrodedDURING ROUTINE INSPECTION, FITTING ON LWR SIDE DOOR JAMB AREA AT BS 620 BETWEEN STR 25R & 26R CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING PER IAW SRM 51-30-2.SDR 00FDEA00344Skin · crackedDURING ROUTINE INSPECTION, EXTERIOR SKIN LEFT SIDE VERTICAL STABILIZER CRACKED AT FIN STA 87, WL 290. REMOVED AND REPLACED PER IAW SRM 51-40-2 & SRM 51-30-2.SDR 00FDEA00343Angle · corrodedDURING ROUTINE INSPECTION, ANGLE ON LWR SIDE OF DOOR JAMB BS 620 CORRODED BEYOND LIMITS FROM STR 27R - 28R. REMOVED AND REPLACED PER IAW SRM 51-40-4.SDR 00FDEA00342Angle · corrodedDURING ROUTINE INSPECTION, FLOOR SUPPORT ANGLE ABOVE STR 29R AT BS 642 CORRODED BEYOND LIMITS. REMOVED AND REPLACED PER IAW SRM 53-10-5 & SRM 51-40-3.SDR 00FDEA00341Skin · gougedDURING ROUTINE INSPECTION, AFT AIRSTAIR EXTERIOR SKIN FOUND GOUGED BEYOND LIMITS AT BS 1300. REMOVED AND REPLACED PER IAW SRM 52-10-2.SDR 00FDEA00340Beltframe · crackedDURING ROUTINE INSPECTION, CRACK IN FWD UPPER FLANGE BELTFRAME BS 1010 BETWEEN STR 26L AND 27L. REMOVED AND REPLACED PER IAW SRM 51-40-3.SDR 00FDEA00339Angle · corrodedDURING ROUTINE INSPECTION, FLOOR SUPPORT ABOVE STR 30 AT BS 1035 CORRODED BEYOND LIMITS. REMOVED AND REPLACED PER IAW SRM 51-40-3.SDR 00FDEA00338Floorboard · crackedDURING ROUTINE INSPECTION, CRACKS FOUND IN FLOOR WEB FWD OF BS 1183 BULKHEAD BL 0 TO LBL 45. REMOVED AND REPLACED WEB PER IAW SRM 51-20-1 AND SRM 51-30-2.SDR 00FDEA00337Floorboard · crackedDURING ROUTINE INSPECTION, CRACKS FOUND IN FLOOR WEB FWD BS 1183 BULKHEAD FROM BL 0 TO RBL 45. REMOVED, FABRICATED AND INSTALLED WEB IAW SRM 51-20-1 & 51-30-2.SDR AALA2000819Stiffener · corrodedTUL - FOUND CORROSION ON VERTICAL STIFFENER AT GROUND WIRES JUST OUTBOARD OF NR 5 LEADING EDGE FLAP ACTUATOR. REMOVED AND REPLACED FRONT SPAR VERT STIFFENER SRM 51-30-2. (M)SDR 00FDEA00336Bulkhead · crackedDURING ROUTINE INSPECTION, CRACK FOUND IN WEB FWD OF BS 1183 BULKHEAD, LBL 50 AT FLOOR LEVEL. REMOVED, FABRICATED AND INSTALLED PER IAW SRM 51-20-1 & SRM 51-30-2.SDR 00FDEA00335Bulkhead · crackedDURING ROUTINE INSPECTION, CRACK FOUND IN WEB AT FWD SIDE OF BS 1183 BULKHEAD, RBL 47 AT FLOOR LEVEL. REMOVED, FABRICATED AND INSTALLED PER IAW SRM 51-40-2 & SRM 51-30-2.SDR 00FDEA00334Bulkhead · crackedDURING ROUTINE INSPECTION, FOUND CRACK IN WEB FWD BS 1183 BULKHEAD, RBL 17 AT FLOOR LEVEL. REMOVED, FABRICATED, AND INSTALLED PER IAW SRM 51-20-1 & SRM 51-30-2.SDR AALA2000785Web · crackedTUL - FOUND STATION 825 RBL 55, WEB CRACKED FROM LIGHTENING HOLE TO FASTENER HOLE, OVERWING FLOORBEAM. REPAIRED WEB PER SRM 51-40-2, INSTALLED DOUBLER. (M)
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