Boeing 727-22C
Service difficulty reports · 2,328
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 = '72722C' 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 = '72722C' 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 96ZZZX1312Skin · damagedDURING D-CHECK, FUSELAGE SKIN AT STR 4L FROM STA 400 TO STA 420 IS DAMAGED. REMOVED FASTENERS PER SRM 51-30-2. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER 2024-T3.050 13 INCH BY 9 INCH PER SRM 53-30-3, FIGURE 14, PRC EDGES PER SRM 51-20-4. TAT: 53,881.4 HRS.SDR 96ZZZX1311Frame · corrosionDURING C-CHECK, CABIN FS 500 FRAME CRACKED JUST ABOVE FLOOR LEVEL, 3.8125 INCHES ABOVE FLOOR LEVEL BETWEEN STR 17R - STR 18R. CUT OUT DAMAGED AREA PER SRM 51-40-3. FABRICATED DOUBLER 7075-T6.063 BY 10.50 INCH BY 4.50 BY 1 INCH PER SRM 51-40-3, AND INSTALLED SDR 96ZZZX1310Vertical Support · crackedDURING D-CHECK, LT WING LEADING EDGE FS 106.8 VERTICAL SUPPORT LOWER END IS CRACKED AT FASTENER ATTACH POINT. FAB NEW ANGLE MATERIAL .050 INCH 2024-T3 LENGTH = 17 INCH BY 2 INCH. INSTALLED PER SRM 51-10-1, PAR 4 AND SRM 51-30-2. TAT: 53,881.4 HRS. TAC: 3SDR 96ZZZX1309Channel · corrosionDURING D-CHECK, CABIN, FLOOR SUPPORT CHANNEL, FS 850-FS 870, RBL 62, HAS CORROSION ON UNDERSIDE OF CHANNEL. REMOVED CORROSION UNDERSIDE OF CHANNEL PER SRM 51-10-6. TREAT AND ALODINE AND PRIMER PER SRM 51-10-2. INSTALLED U-CHANNEL REPAIR 15 INCHES LONG AND MSDR 96ZZZX1308Panels · crackedDURING D-CHECK, CABIN, FWD OF BS 1183 RT, LT OF FLOOR LEVEL FLOTATION PANELS ARE CRACKED. ROUTED OUT CRACK AREAS PER SRM 51-40-2. FABRICATED DOUBLER 2024T3.025, 6 INCH BY 72 INCH, AND INSTALLED PER SRM 51-40-2, AND SRM 51-30-2. SEALED WITH PRC PER SRM 51-20SDR 96ZZZX1307Seat Track · brokenDURING D-CHECK, CABIN, SEAT TRACK BROKEN AT FS 850, RBL 45. CUT OUT BROKEN SECTION OF SEAT TRACK. MADE REPAIR PER SRM 53-10-5, PAGE 4A. DRILLED HOLES, ALODINED AND PRIMED. INSTALLED REPAIR PER SRM 53-10-5, PAGES 4A AND 4B. TAT: 53,881.4 HRS. TAC: 36,38SDR 96ZZZX1306Vertical Support · crackedDURING D-CHECK, STA 920, LT VERTICAL SUPPORT AT STR 15 IS CRACKED AT FASTENER LOCATION. STOP-DRILLED CRACK PER SRM 51-10-01. FABRICATED DOUBLER PER SRM 51-40-3. INSTALLED DOUBLER PER SRM 51-40-21, 5 INCH BY 2 INCH, 2024T3.071. TAT: 53,881.4 HRS. TAC: 36SDR 96ZZZX1305Skin · crackedDURING D-CHECK, NR 10 RIB FROM OUTBOARD END OF SLAT NR 2 LEADING EDGE IS CRACKED AT LOWER FWD CORNER. INSTALLED TYPICAL RIB REPAIR PER SRM 57-50-3. REPLACED FASTENERS PER SRM 51-30-3. TAT: 53,882.4 HRS. TAC: 36,380.SDR 96ZZZX1304Spar · corrodedDURING D-CHECK, WING, CENTER SECTION, INTERNAL REAR SPAR WEB BLR 24 BULGING, POP RIVET HEADS, CORROSION STA 870. CUT OUT DAMAGED WEB PER SRM 57-10-6. INSTALLED NEW STIFFENER PER SRM 51-10-1, PARAGRAPH 4. INSTALLED WEB REPAIR PER SRM 57-10-6. FILLER 3 INCH SDR 96ZZZX1303Skin · gougedDURING C-CHECK, NR 4 RIB FROM INBD END OF STAT NR 2 LEADING EDGE IS GOUGED. TRIMMED OUT DAMAGED AREA PER SRM 51-10-1. TAT: 53,881.4 HRS. TAC: 36,380.SDR 96ZZZX1302Fuel Vent Line · corrodedDURING D-CHECK, FUEL VENT LINE AT WS 629 AND WS 601, CHECK THAT REPAIR IS IN C/W E.O. REPAIR. BLENDED OUT PER SRM 51-40-1. MATERIAL LOOSE .002 INCH. INSTALLED REPAIR PER AVITAS ENGINEERING NR 95PMSI.049RO-0 IN BOTH LOCATIONS. TAT: 53,881.4 HRS. TAC: 36,SDR 96ZZZX1301Vent Line · corrodedDURING D-CHECK, VENT TURBINE AT STA 580 HAS IMPROPER REPAIR. INSTALLED PROPER REPAIR PER AVITAS ENGINEERING NR 95PMSI.049 RO-1. TAT: 53,881.4 HRS. TAC: 36,380.SDR 96ZZZX1300Spar · corrodedDURING D-CHECK, WING, CENTER SECTION, INTERIOR REAR SPAR WEB, BLR 48, BULGING. POP RIVET HEADS. CORROSION STA 870. CUT OUT 2 INCH BY 6 INCH BULGED AREA AND INSTALLED DOUBLER 10 INCH BY 12 INCH, .200 INCH 2024T3 PER SRM 57-10-6. REPLACED STIFFENER PER SRM 5SDR 96ZZZX1299Stringer · crackedDURING D-CHECK, FS 265, STR 9R, HAS SEVEN CRACKED RIVET HOLES. FS 265, STR 10R, HAS BURNISHED SKIN OUT OF LIMITS PER SRM 53-30-01. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED PARTS PER SRM 53-30-3, FILLER MATERIAL .040 INCH, 2024T3, 12 INCH BY 16 INCH DOUSDR 96ZZZX1298Floor Beams · corrosionDURING D-CHECK, LIGHT CORROSION CABIN FLOOR BEAMS, STA 480 AND STA 400, AND SEAT TRACK LIPS. CUT OUT DAMAGED AREA, BS 400, LBL 27, AND REPAIR PER SRM 51-40-4 7075-T6.063, 12 INCH LONG DOUBLER INSTALLED. REMOVED LIGHT CORROSION, BS 400 TO BS 480 PER SRM 51-10SDR 96ZZZX1297Seat Track · corrosionDURING D-CHECK, CORROSION, NR 7 SEAT TRACK, STA 780 TO STA 800. REMOVED CORRODED SEAT TRACK, MADE NEW SEAT TRACK, ALODINED AND PRIMED AND INSTALLED PER SRM 51-10-1. TAT: 53,881.4. TAC: 36,380.SDR 96ZZZX1296Floor Panel · corrodedDURING D-CHECK, CORROSION AND CRACK ON CABIN FLOOR PANEL, STA 1030 TO STA 1110, STR 48 TO STR 60. FABRICATED NEW FLOOR PANEL, STA 1030 - STA 1110, STR 48 TO STR 60 PER SRM 51-10-1 AND SRM 53-20-2. TAT: 53,881.4. TAC: 36,380.SDR 96ZZZX1295Subfloor · corrodedDURING C-CHECK, CORROSION CABIN SUB-FLOOR, STA 1130 TO STA 1136, STR 48 TO STR 58. FOUND CORROSION OUT OF LIMITS, REPAIRED PER SRM 51-40-4, FIGURE 1, MATERIALS USED: ALCLAD 7075-T6.050, 22 INCH BY 2.5 INCH, 7075-T6.90, 18 INCH BY 4 INCH EXTRUSION, 7075-T6.90SDR 96ZZZX1294Subfloor · corrodedDURING D-CHECK, CORROSION ON SUB-FLOOR, STA 1160, BLL 23. CUT 10 INCH BY 7 INCH CORRODED AREA AND INSTALLED 12 INCH BY 10 INCH .063 INCH 7075-T6 DOUBLER PER SRM 51-40-2. TAT: 53,881.4. TAC: 36,380.SDR 96ZZZX1293Cord · corrodedDURING D-CHECK, LOWER RT CORD ANGLE CORRODED ON VERTICAL LEG, STA 312, STR 27R. REMOVED AND REPLACED RT NOSE CORD ANGLE WITH NEW ONE PER SRM 51-10-1, PARAGRAPH 4. TAT: 53,881.4. TAC: 36,380.SDR 96ZZZX1292Spar · corrodedDURING D-CHECK, CORROSION ON AFT UPPER SPAR CAP CENTER WING TANK AT FS 870, LBL 33 TO LBL 48. CUT WEB FROM LBL 33 TO LBL 48, CUT SPAR CAP, 1 INCH BY 4 INCHES. INSTALLED WEB AND ANGLES FOR SPAR REPAIR PER SRM 57-10-6 (WEB REPAIR), 51-40-4 AND AERO NR 95PMSI.0SDR 96ZZZM99999Angle · crackedDURING D-CHECK, LEADING EDGE SUPPORT ANGLE CRACKED AT UPPER AFT CORNER ALONG RADIUS FSS 337. REMOVED AND REPLACED ANGLE PER SRM 51-10-1 15 INCHES BY 2 INCHES 2024-T3 .040.SDR 96ZZZM412Blkhd Skin · corrodedDURING D-CHECK, FOUND ON RT W/W, CORROSION AT BULKHEAD 870 RBL 4 FORWARD OF APU CUT OUT. REMOVED OLD REPAIR, CLEANED AREA AND INSTALLED NEW DOUBLER 2024-T3 .050 2 INCHES BY 4 INCHES AS PER SRM 51-40-2. (M)SDR 96ZZZM411Skin · corrodedDURING D-CHECK, FOUND ON RT W/W, CORROSION ON LOWER SURFACE OF RT W/W PRESSURE DECK AT FS 880 RBL 12 AND 20. REMOVED FLAP CTL VALVE, REMOVED FASTENERS, REMOVED CORROSION, STOP DRILLED CRACK, INSTALLED DOUBLER .080 2024-T3 21 INCHES BY 12 INCHES AND REINSTALLESDR 96ZZZM410Skin · dentedDURING D-CHECK, FOUND ON FUSELAGE EXTERIOR, FUSELAGE SKIN AND EXTERNAL DOUBLER DENTED AT FS 188 APPROXIMATELY AT STRINGER 26R AREA. REMOVED OLD DOUBLER PER SRM 51-30-2. CUT OUT DAMAGE AREA PER SRM 53-30-3. INSTALLED DOUBLER 14.5 INCHES BY 17 INCHES 2024-T3 SDR 96ZZZM409Angle · corrodedDURING D-CHECK, FOUND FUSELAGE EXTERIOR EVIDENCE OF CORROSION AT AFT SIDE OF EXTERNAL DOUBLER AND TWO BLIND FASTENERS AT FS 312 APPROXIATELY BETWEEN STRINGER 26R AND STRINGER 27R. REMOVED DOUBLER, CORROSION FOUND ON NOSE CHORD ANGLE. REPLACED DOUBLER AS PER SDR 96ZZZM408Skin · dentedDURING D-CHECK, FOUND ON FUSELAGE EXTERIOR, FOUR RUSTED FASTENERS AND FUSELAGE SKIN DENTED BETWEEN FS 267 AND FS 282 APPROXIMATELY AT STRINGER 23L. REMOVED DAMAGED AREA PER SRM 53-30-3. FABRICATED DOUBLER 10 INCHES BY 8 INCHES 2024-T3 .063 PER SRM 53-30-3 ANSDR 96ZZZM407Web · crackedDURING D-CHECK, FOUND APPROXIMATELY 3 INCH CRACK IN WEB BETWEEN RIGHT 940 AND 950 FITTINGS AT STRINGER 180 IN R/W/W. REMOVED EXISTING WEB AND TWO ANGLES PER S/B 727-53-140. ALODINED AND PRIMED AREA PER SRM 51-10-2. REPLACED WITH NEW 'T' CHORD PER S/B 727-53SDR 96ZZZM406Cargo Door · crackedDURING D-CHECK, FOUND MCD, BOTTOM OF DOOR INBOARD STRUCTURE JUST BELOW STATION 600, RIB HAS CRACK INDICATION. REMOVED AND REPLACED ALUMINUM SUPPORT BLOCK 7075-T6 .250 5.5 INCH BY 3.5 INCH AS PER SRM 51-10-1 PAR 4 AND 51-30-2.SDR 96ZZZM405Cargo Door · crackedDURING D-CHECK, FOUND MCD, BOTTOM OF DOOR INBOARD STRUCTURE JUST BELOW STATION 500 RIB, HAS CRACK INDICATION. REMOVED RIB AND ALUMINUM BLOCK. FABRICATED NEW ALUMINUM BLOCK 7075-T6 .250 3.5 INCHES BY 5.5 INCHES AND INSTALLED. REPLACED SEAL RETAINER 1 INCH BYSDR 96ZZZM404Skin · dentedDURING D-CHECK, FOUND EXT FUSELAGE, APPROXIMATELY BS 1233 JUST UNDER LAP SEAT 20R, DENTED. FOUND OUT OF LIMITS PER SRM 53-30-1 PAGE 1 PAR B. REMOVE DAMAGED AREA AND FABRICATED FILLER FROM 2024-T3 .050 14.5 INCHES BY 6.5 INCHES AND DOUBLER FROM 2024-T3 .063 1SDR 96ZZZM403Skin · missing fastenerDURING D-CHECK, FOUND EXT FUSELAGE BETWEEN BS 1343-1353 BETWEEN STRINGER 8R-13R MISSING FASTENER, LOOSE FASTENERS, RUST ON WASHERS/FASTENERS, BUCKLED SKIN. FABRICATED AND INSTALLED DOUBLER AS PER SRM 54-30-3 15 INCHES BY 10 INCHES 2024-T3 .063 AND INSTALLED PSDR 96ZZZM402Seat Track · corrodedDURING D-CHECK, FOUND CORROSION ON CABIN FILLER SEAM NR 7 STATION 870 TO STATION 950 SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK FS 870-1070 WIDTH 3.25 INCH, INSTALLED PER SRM 51-10-1 PAR 4 AND SRM 51-30-2.SDR 96ZZZM401Seat Track · corrodedDURING D-CHECK, FOUND CORROSION CABIN SEAT TRACK NR 7 STATION 1030. FABRICATED NEW SEAT TRACK FS 870-1070. INSTALLED TRACK PER SRM 51-10-1 PAR 4 WIDTH 3.25 INCH AND SRM 51-30-2.SDR 96ZZZM400Floor · corrodedDURING D-CHECK, FOUND CORROSION ON CABIN FLOOR STATION 1110 TO 1183 ROW 4. REMOVED CORROSION PER SRM 51-10-6. CUT OUT CORROSION PER SRM 51-10-2. INSTALLED DOUBLER .040 12 INCH BY 5 INCH AND FILLER PER SRM 51-40-1.SDR 96ZZZM399Seat Track · corrodedDURING D-CHECK, FOUND CORROSION NR 1 CABIN SEAT TRACK STATION 700. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK FROM STATION 660-740.SDR 96ZZZM398Seat Track · corrodedDURING D-CHECK, FOUND CORROSION SEAT TRACK NR 1 STATION 950. TWO FASTENERS REMOVED PER SRM 51-30-2. FOUND CORROSION OUT OF LIMITS PER SRM 51-10-6. REPLACEMENT OF SEAT TRACT SECTION 107 AND INSTALLED FASTENERS AS PER SRM 51-10-1 AND 51-30-2.SDR 96ZZZM397Seat Track · corrosionDURING D-CHECK, FOUND CORROSION CABIN SEAT TRACK NR 2 STATION 1131 TO 1135. REMOVED FASTENER PER SRM 51-30-2 AND REMOVED CORROSION PER SRM 51-10-6 MAT LOSS .003. ALODINED AND PRIMED AS PER SRM 51-10-2.SDR 96ZZZM396Support Angle · crackedDURING D-CHECK, FOUND SUPPORT ANGLE CRACKED INSIDE FORWARD CARGO DOOR AT FORWARD EDGE BY THIRD STOP FITTING FROM BOTTOM. REMOVED SUPPORT ANGLE, FABRICATED SUPPORT ANGLE. INSTALLED SUPPORT ANGLE PER SRM 51-10-1 PAGE 4 AND SRM 51-30-2.SDR 96ZZZM395Seat Track · corrodedDURING D-CHECK, FOUND CORROSION CABIN SEAT TRACK NR 7 STATION 1045 TO STATION 1055. FABRICATED NEW SEAT TRACK FS 870-1070. INSTALLED TRACK PER SRM 51-10-1 PAR 4, (WIDTH 3.25 INCH) AND SRM 51-30-2. (M)SDR 96ZZZM394Seat Track · corrosionDURING D-CHECK, FOUND CORROSION CABIN SEAT TRACK NR 7 STATION 1025 TO STATION 1035. FABRICATED NEW SEAT TRACK FS 870-1070. INSTALLED TRACK PER SRM 51-10-1 PAR 4 (WIDTH 3.25 INCH) AND SRM 51-30-2.SDR 96ZZZM393Skin · corrodedDURING D-CHECK, FOUND WING CENTER SECTION LOWER SKIN HAS EXTERIOR CORROSION BULGE/CRACK AT RT EDGE BOLTS BL 70 INCHES R AT 38 INCHES AFT OF FRONT SPAR. REMOVED CORROSION AS PER SRM 51-10-6. ULTRASONIC INSPECTED TO DETERMINE MATERIAL REMOVED. HFEC INSPECTIONSDR 96ZZZM392Floor · corrodedDURING D-CHECK, MANY SPOTS OF HEAVY CORROSION ON SUB FLOOR AROUND RIGHT AFT LAV DRAIN FITTING. CUT OUT CORRODED AREA, CLEANED AREA, ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED DOUBLER 2024-T3 .063 29 INCHES BY 13.5 INCHES AND INSTALLED PER SRM 51-40-2. SDR 96ZZZM391Spar Web · crackedDURING D-CHECK, FOUND VERTICAL WEB ATTACHED TO FRONT SPAR FSS 106.8 CRACKED AT 3 PLACES, SEEN THROUGH ACCESS PANEL 6402. RENIVED FASTENERS PER SRM 51-30-2. STOP DRILLED CRACKS PER SRM 51-10-1. INSTALLED WEB REPAIR PER SRM 51-10-1. INSTALLED WEB REPAIR PER SDR 96ZZZM390Angle · crackedDURING D-CHECK, VERTICAL LEADING EDGE SUPPORT ANGLE, SECOND FROM AFT END IS CRACKED AT LOWER FASTENER FSS 106.8 SEEN THROUGH ACCESS PANEL 6402. REMOVED FASTENERS PER SRM 51-30-2. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED DOUBLER 2024-T3 .050 PER SRM 51SDR 96ZZZM389Angle · crackedDURING D-CHECK, FOUND LOWER SUPPORT ANGLE CRACKED IN TWO PLACES FORWARD OF LOWER SPAR LE SPAR LE STATION 130.7. REMOVED FASTENERS PER SRM 51-30-2. REMOVED DAMAGED AREA AT SUPPORT ANGLE PER SRM 51-40-2. FABRICATED NEW SECTION OF SUPPORT ANGLE 17 INCH BY 1 INSDR 96ZZZM388Skin · crackedDURNG D-CHECK, FOUND AFT CARGO COMPARTMENT DOOR EXTERIOR SKIN 2 EACH SMALL CRACKS AT LOWER AND FORWARD EDGE CORNER. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER 2024-T3 .063 14 INCHES BY 12.5 INCHES AS PER SRM 52-20-2. SEALED EDGE WITH PRC PER SRM 51-20-4.SDR 96ZZZM387Frame · dentedDURING D-CHECK, FOUND FUSELAGE FRAMES DENTED AT INNER ANGLE STATION 520 AND STATION 540 JUST ABOVE STRINGER 6R. CUT OUT DENTED AREA AT STRINGER 520 AND STRINGER 540. FOUND OUT OF LIMITS. REPAIRED AS PER SRM 53-10-4. TWO REPAIRS 12 INCHES BY 3 INCHES 7075-TSDR 96ZZZM386Skin · crackedDURING D-CHECK, FOUND TOP SKIN IS CRACKED AT ONE FASTENER HOLE AT FS 385 STRINGER 4R. CUT OUT DAMAGE AREA PER SRM 53-30-3 FIG 4 AND INSTALLED DOUBLER 9 INCHES BY 8 INCHES 2024-T3 .050 PER SRM 53-30-3 FIG 4.SDR 96ZZZM385Intercostal · corrodedDURING D-CHECK, FOUND FORWARD NOSE COMPARTMENT BETWEEN BS 211.8-219.8 APPROXIMATELY BLL 30, CORROSION AT INTERCOSTAL AND AT FRAME. REMOVED DAMAGED AREA PER SRM 51-30-2. FABRICATED AND INSTALLED NEW PART AS PER SRM 51-40-3.
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