Boeing 727-225
Service difficulty reports · 4,226
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 = '727225' 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 = '727225' 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 DL72P961225Bulkhead Web · crackedTHE BS 1183 BULKHEAD WEB WAS FOUND CRACKED AT RBL 27. THERE IS A .125 VERTICAL CRACK AND A .5 HORIZONTAL CRACK AT WL 170. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF 0.050. THE CRACK LOCATION IS OUTSIDE OF THE INSPECTION AREA SPECSDR DL72P961105Stringer · crackedSTRINGER 18A RT CRACKED AT STA 940 SUPPORT FITTING AFT BOLT. REPAIRED PER MM 53-12-0.SDR DL72P961095Web · crackedA .625 INCH CRACK IN LT LOWER TORQUE BOX VERTICAL WEB AT LOWER LIGHTENING HOLE STA 1237. REPAIRED PER M/M 53-11-0 AND ERA DUE TO EFFECTIVITY.SDR DL72P961094Bracket · crackedAPPROX 2 INCH CRACK IN NR 1 SLAT I/B AND O/B ACTUATOR MOUNT BRACKET'S. REPAIRED PER M/M 57-20-21 AND ERA DUE TO A/C EFFECTIVITY.SDR DL72P961093Bracket · crackedNR 1 L/E FLAP ACTUATOR MOUNT BRACKET CRACKED AT LOWER I/B CORNER. REPAIRED PER M/M 57-20-21 AND ERA DUE TO A/C EFFECTIVITY.SDR DL72P961091Angle · crackedFOUND DURING C-CHECK, .5 INCH CRACK IN NR 1 SLAT SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER M/M 51-54-0 AND ERA DUE TO EFFECTIVITY.SDR DL72P961090Aux Spar · chafedFOUND DURING C-CHECK, LT MLG STRUT DOOR CHAFING AUX SPAR I/B END MARKED, FWD OF NR 4 SCREWJACK. REPAIRED PER M/M 57-43-0 PG 802.SDR DL72P961089Frame · crackedFOUND DURING C-CHECK, AFT RT SVC DOOR FWD FRAME CRACKED AT LWR I/B END OF UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2.SDR 9610392705Battery Pack · dischargedDURING PREFLIGHT, FOUND AFT FLASHLIGHT WOULD NOT TEST. REPLACED BATTERY PACK, CHECKED OK.SDR IXKA960026Wire · damagedMEL CI NR 050001-C FORWARD RED EMERGENCY PATH LIGHT OUT. MX TROUBLESHOT EMERGENCY TRACK LIGHT INOP, DUE TO BAD SPLICE AT PIGTAIL. REPAIRED SPLICE AND EMERGENCY PATH LIGHTS CHECK GOOD. (M)SDR DL72P961059Bulb · failedAFT LT SERVICE DOOR EMERGENCY LIGHT, ONE BULB OUT (LT UPPER). REPLACED EMERGENCY LIGHT ASSY. OPS CHECK GOOD.SDR IXKA960029Lower Gate · damagedFLT 56 - CXL - FORWARD GALLEY SERVICE DOOR (R1) WILL NOT OPEN. FOUND LOWER GATE ASSY ON DOOR DAMAGED. REMOVED AND REPLACED FOWARD GALLEY SERVICE DOOR (R1) LOWER GATE ASSY PER MM 52-10-10. OP CHECK OK. (M)SDR IXKA960025Battery Pack · dischargedFLT 44 - ATL - AFT FLASH LIGHT NO BLINKING. REMOVED AND REPLACED AFT FLASH LIGHT BATTERY PACK. (M)SDR DL72P961613Transverse Beam · crackedTHERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1263. 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 REQUSDR 9609492709Flap Indicator · malfunctionedDURING CLIMB ON RETRACTION, OUTBOARD FLAPS STAYED AT 5 DEGREES WITH THE INBOARD FLAPS WENT TO 2 DEGREES AND STOPPED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED BOTH INBOARD AND OUTBOARD FLAP INDICATORS. PERFORMED FLAP SYSTEM RIG CHECK. SDR SCNA96126Floor Beam · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FLOOR BEAM IN THE AFT PIT AT BS 1110, LBL 12 TO RBL 17, WL 208. REMOVED T-FLANGE, FABRICATED AND INSTALLED NEW T-FLANGE IN ACCORDANCE WITH B727 SRM 53-10-8, FIGURE 3.SDR DL72P961026Skin · cracked1.25 INCH CRACK IN ELEVATOR LOWER SKIN AFT OF NR 2 RT BALANCE BOARD ACCESS PANEL. FOUND DURING C-LETTER CHECK. REPAIRED PER SRM 55-20-3, FIG 4.SDR SCNA96138Formed Section · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON FORMED SECTIONS IN THE GALLEY AREA AT BS 360 TO 380 RBL 65, WL 208. REMOVED FORMED SECTIONS, FABRICATED AND INSTALLED NEW FORMED SECTIONS IN ACCORDANCE WITH B727 SRM 51-30-2 AND 51-20-2.SDR SCNA96137Seat Track · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A SEAT TRACK IN THE GALLEY AREA AT BS 480 RBL 45 WL 208. REMOVED SEAT TRACK, FABRICATED AND INSTALLED A NEW SECTION OF SEAT TRACK IN ACCORDANCE WITH B727 SRM 53-10-5.SDR SCNA96136Seat Track · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A SEAT TRACK AT BS 400, RBL 24.5. REMOVED SEAT TRACK, FABRICATED AND INSTALLED A NEW SEAT TRACK IN ACCORDANCE WITH B727 SRM 53-10-2, 51-30-2 AND MM 51-20-11.SDR SCNA96132Web · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A CABIN WEB LOCATED AT BS 420 TO 428, RBL 65 WL 208. REMOVED CORRODED SECTION OF WEB, FABRICATED AND INSTALLED A NEW WEB IN ACCORDANCE WITH B727 SRM 51-20-2.SDR SCNA96129Seat Track · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON SEVERAL SEAT TRACKS IN THE G-1 GALLEY AT BS 360 TO 380, RBL 24.5, RBL 45 AND RBL 56.5. REMOVED SEAT TRACK FROM BS 340 TO 480, RBL 24.5; BS 340 TO 420, RBL 45 AND BS 340 TO 380, RBL 56.5. FABRICATED AND ISDR IXKA960024Battery Pack · dischargedFOUND LEFT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED POWER PACK AND BATTERY CHARGER ASSY. OPS CHECKS GOOD. (M)SDR 96ZZZM869Battery Charger · inoperativeFOUND LEFT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED POWER PACK AND BATTERY CHARGER ASSY. OPS CHECKS GOOD. REFERENCE IXKA960024.SDR 9609342705T/O Warning · activatedDURING TAKEOFF ROLL, THE AIRCRAFT EXPERIENCED TAKEOFF WARNING INDICATION. TAKEOFF WAS ABORTED WITHOUT INCIDENT AND RETURNED TO THE GATE. SRQ MAINTENANCE PERFORMED FLIGHT CONTROL AND TAKEOFF WARNING CHECK, SYSTEM CHECKED OK.SDR SCNA96135Seat Track · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A LT SEAT TRACK AT BS 1050 TO 1183. REMOVED CORRODED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH B727 SRM 53-10-5 FIGURE 7 AND 51-30-2.SDR SCNA96123Seat Track · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A SEAT TRACK AT BS 1110 TO 1130, RBL 45. REMOVED SEAT TRACK SECTION, FABRICATED AND INSTALLED A NEW SECTION IN ACCORDANCE WITH B727 SRM 53-10-5.SDR SCNA96122Floor Beam · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FLOOR BEAM SUPPORT AT BS 1130. FABRICATED AND INSTALLED A NEW FLOOR BEAM SUPPORT IN ACCORDANCE WITH B727 SRM 53-10-4.SDR SCNA96118Floor Beam · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FLOOR BEAM ON THE LEFT SIDE OF THE CABIN AT BS 1110. REMOVED CORROSION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 53-10-8, FIGURE 3, AND MM 51-20-11.SDR SCNA96108Floor Support · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON FLOOR SUPPORT NEXT TO L2 DOOR, BS 1030. REMOVED CORRODED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW SUPPORT IN ACCORDANCE WITH B727 SRM 51-40-4.SDR SCNA96107Seat Track · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON THE LEFT SIDE CABIN SEAT TRACK, BS 1030 TO 1130. CORROSION WAS WITHIN LIMITS BETWEEN BS 1070 TO 1130. REMOVED, FABRICATED AND INSTALLED A NEW SECTION FROM BS 1010 TO 1070 IN ACCORDANCE WITH B727 SRM 53-1SDR SCNA96128End Cap · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON AN END CAP IN THE AFT PIT, BS 1177, STRINGER 25R. REMOVED CORRODED END CAP FITTING AND INSTALLED A NEW FITTING IN ACCORDANCE WITH B727 SRM 51-30-2 AND MM 53-11-0.SDR SCNA96127Spar · crackedDURING HEAVY MAINTENANCE VISIT, CRACKS WERE FOUND IN SKIN AROUND RIVETS JUST BELOW THE LOWER CHORD OF THE REAR SPAR UNDER NR 2 AND NR 3 SPOILERS. FABRICATED AND INSTALLED A WAFFLE DOUBLER IN ACCORDANCE WIITH B727 SRM 51-40-3, FIGURE 1.SDR SCNA96112Floor Beam · crackedDURING HEAVY MAINTENANCE VISIT, A CRACK WAS FOUND IN THE FLOOR BEAM WEB AT BS 740 BL 0. FABRICATED AND INSTALLED A WEB REPAIR IAW B727 SRM 51-40-2.SDR IXKA960022Battery Pack · dischargedON POST FLIGHT INSPECTION FOUND RIGHT FORWARD OVERWING HATCH EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATIONALLY CHECKS GOOD. (M)SDR IXKA960021Battery Pack · dischargedON POST FLIGHT INSPECTION FOUND RIGHT AFT OVERWING HATCH LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATIONALLY CHECKS GOOD. (M)SDR SCNA96140Angle · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON MAIN CABIN FLOOR STRUCTURE AT BS 312 AND BS 344 LBL 30. REMOVED CORRODED FLOOR ANGLES, FABRICATED AND INSTALLED NEW ANGLES IN ACCORDANCE WITH B727 SRM 51-40-4.SDR SCNA96121Floor Beam · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FLOOR BEAM IN THE AFT CARGO PIT, BS 1030, BL ZERO, WL 208. REMOVED CORROSION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 53-10-8, FIGURE 3.SDR SCNA96120Floor Beam · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON THE UPPER SURFACE OF A FLOOR BEAM AT BS 344, LBL 30 TO RBL 16. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED A REPAIR SECTION IN ACCORDANCE WITH B727 SRM 53-10-8 AND MM 51-20-11.SDR SCNA96139Fitting · crackedDURING HEAVY MAINTENANCE VISIT, A CRACK WAS FOUND EXTENDING FROM A FLANGE RADIUS AT THE BOTTOM OUTBD CORNER OF THE REAR SPAR WING TO BODY FITTING. FABRICATED AND INSTALLED REPAIRS IN ACCORDANCE WITH B727 SRM 51-20-1 AND 51-30-2.SDR SCNA96133Frame · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FRAME IN THE AFT PIT AT BS 1166, BL 0, WL 200. FABRICATED AND INSTALLED A NEW FRAME IN ACCORDANCE WITH B727 SRM 51-30-2 AND 51-40-4 FIGURE 1.SDR SCNA96110Blkhd Stiffener · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STIFFENER, BS 1183 LBL 59 WL 220. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 51-40-4.SDR SCNA96109Blkhd Stiffener · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STIFFENER, BS 1183 RBL 61, WL 220. REMOVED DAMAGE, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH B727 SRM 51-40-4.SDR SCNA96119Frame · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FRAME IN THE AFT PIT AT BS 1110 TO 1130, BL 0, WL 208.1. REMOVED CORROSION, FABRICATED AND INSTALLED AN ANGLE IN ACCORDANCE WITH B727 SRM 51-30-2, 51-20-1 AND MM 51-20-11.SDR SCNA96117Frame · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON A FRAME IN THE AFT PIT BETWEEN BS 1090 AND BS 1110, AT LBL 12, WL 208.1. REMOVED CORROSION, FABRICATED AND INSTALLED A NEW SUPPORT AND STRAP IN ACCORDANCE WITH B727 SRM 53-10-2 AND MM 51-20-11.SDR SCNA96116Angle · crackedDURING HEAVY MAINTENANCE VISIT, A CRACK WAS FOUND EXTENDING FROM A FASTENER LOCATION IN THE LEFT MLG WW LOWER CHORD AT BS 870 LBL 50. REMOVED TWO CRACKED ANGLES, FABRICATED AND INSTALLED NEW ANGLES IN ACCORDANCE WITH B727 SRM 51-30-2 AND 51-40-3 FIGURE 1.SDR SCNA96052Light · failedTHE AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT IN OVERHEAD LIGHT PANEL IS INOP WITH EMERGENCY LIGHTS TURNED ON. REMOVED AND REPLACED AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT IAW MM 33-50-101, LIGHT OPS CHECKED GOOD.SDR IXKA960019Lense · brokenATL - LOG ITEM - 6TH EMERGENCY RED LENSE WOULD NOT STAY DOWN. REPLACED MODULE. (X)SDR SCNA96125Angle · crackedDURING HEAVY MAINTENANCE VISIT, CRACKS WERE FOUND IN TWO SUPPORT ANGLE BRACKETS LOCATED AT THE NR 4 SLAT IN THE LEFT WING. FABRICATED AND INSTALLED TWO REPAIR DOUBLERS IN ACCORDANCE WITH B727 SRM 27-81-11, OPS CHECKED OK.SDR SCNA96124Bulkhead Strap · crackedDURING HEAVY MAINTENANCE VISIT, CRACKS WERE FOUND IN THE FORWARD BULKHEAD STRAP/SKIN BETWEEN THE 2ND, 3RD, 4TH, AND 5TH FASTENERS AT BS 178, BL ZERO, WL 183. FABRICATED A REPAIR DOUBLER AND STRAP IN ACCORDANCE WITH B727 SRM 51-30-2, AND SB 727-23-0065.
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