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 CALA9801526Floorbeam · corrodedINSPECTION FOUND AFT PIT FLOORBEAM CRACKED AT BS 950E ABOVE STRINGER 29L. THE CRACKED SECTION OF FLOORBEAM WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 51-40-4, 51-30-2, 51-10-2, AND MM 51-20-0.SDR CALA9801525Angle · corrodedINSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT DOGHOUSE, STA 294.5. THE FLOOR SUPPORT ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2.SDR CALA9801517Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 410 TO 430, RBL 24. THE SEAT TRACK WAS REPLACED IAW SRM 53-10-5, FIGURE 7.SDR CALA9801516Angle · crackedINSPECTION FOUND LT WING FORWARD RIB ATTACH ANGLE CRACKED AT WS 92.8. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 57-20-2, 51-10-2, AND 51-30-2.SDR CALA9801515Angle · crackedINSPECTION FOUND TWO .625 INCH CRACKS IN RT WING TRAILING EDGE SUPPORT ANGLE UNDER NR 13 SPOILER OUTBOARD END AT SUPPORT ROD LOWER ATTACH POINT. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-10-2 AND 51-30-2.SDR CALA9801514Angle · crackedINSPECTION FOUND RT UPPER WING TO BODY FAIRING SUPPORT STRUCTURE CRACKED ON LOWER ANGLE AND WEB AT FS 950. THE CRACK WAS 2 INCHES LONG. THE ANGLE WAS REMOVED AND THE CRACK WAS STOP DRILLED. A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-10-2, 51-00-0 FSDR CALA9801513Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 312 BELOW SRTINGER 13R. THE CRACKED SECTION OF FRAME WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 53-10-4, FIGURE 4 AND 51-30-2.SDR CALA9801512Skin · crackedINSPECTION FOUND L-1 DOOR INNER SKIN CRACKED JUST AFT OF WINDOW OPENING. THE CRACKED AREA WAS CUT OUT. A REPAIR WAS INSTALLED IAW SRM 51-40-2 FIGURE 1, 51-30-2, 52-10-1 FIGURE 1, 51-30-6, 51-30-8, AND 51-40-2 FIGURE 1.SDR CALA9801511Web · crackedINSPECTION FOUND A 3 AND 4 INCH CRACK IN LT CABIN ATTACH WEB AT STA 740, LBL 45. THE CRACKS WERE STOP DRILLED, A DOUBLER WAS INSTALLED IAW SRM 51-10-1, 51-40-2, 53-10-2, AND 51-30-2.SDR CALA9801510Angle · corrodedINSPECTION FOUND LT AFT LAV FLOOR LEVEL ANGLE CORRODED AT FS 1180. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-20-4.SDR DL72S982062Skin · cracked.5 INCH LONG CRACK IN COVE SKIN -31 FROM I/B END OF FLAP, REPAIRED ON SHOP ORDER 553647 PER MM5 7-52-0 FIG 809.SDR DL72S982061Spar · crackedCRACK AFT SPAR RAIL 19 FROM I/B END OF FLAP. REPAIRED ON SHOP ORDER 553647 PER MM 57-52-0 FIG 802.SDR DL72S981764Battery Pack · dischargedON L/O, AFT OVERWING ESCAPE LIGHT INOP. REPLACED BATTERY PACK.SDR DL72S981754Strap · out of positionYELLOW BARRIER STRAP CAUGHT HALF WAY OUT L2 DOOR, UNABLE TO RETRACT IN FLIGHT. AIR TURNBACK. REMOVED YELLOW SAFETY STRAP FROM DOOR JAMB.SDR DL72L981750Skin · corrodedTHE FUSELAGE SKIN AT FS 990 AND STRINGER 28R WAS FOUND CUTOUT TO REMOVE CORROSION OVER A 2 X 3 AREA. THE CUTOUT WAS ADJACENT TO AN EXISTING REPAIR INSTALLED TO REPAIR ANOTHER SKIN CORROSION CUTOUT. THE EXISTING REPAIR WAS REMOVED AND A NEW EXTERNAL ALUMINUM SDR DL72L981749Skin · corrodedTHE FUSELAGE SKIN AT FS 1055 AND STRINGER 29L WAS FOUND WITH CORROSION RESULTING IN A 2 X 3 CUTOUT TO REMOVE THE DAMAGE. THE CUTOUT WAS ADJACENT TO TWO OTHER EXISTING SKIN REPAIRS. ONE OF THE EXISTING REPAIRS WAS REMOVED AND REPLACED WITH A NEW EXTERNAL ALUMSDR DL72L981748Skin · corrodedTHE SKIN WAS FOUND CORRODED BETWEEN FS 480 AND 500 AT STRINGER 28R. THE CORROSION WAS CUTOUT RESULTING IN A 16.75 LONG X 3.25 WIDE CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER, INSTALLED PER PROCEDURES OUTLINED IN B727 SRM 53-30-3, FIG 3SDR DL72S981903Stringer · crackedSTRINGER CRACKED VERTICAL STAB INTERIOR, STRINGER CRACKED AT FIN STA 180.6 STA 9L. CRACK RUNS FROM HOLE TO EDGE OF PART. NO STOP DRILL REQUIRED. FABRICATED REPAIR PER M/M 55-30-0 FIG 803. IK INSTALL. BEGAN INSTALL OF REPAIR PER M/M 55-30-0 FIG 803. FINISSDR DL72S981902Stringer · crackedSTRINGER CRACKED. VERTICAL STAB INTERIOR, STRINGER CRACKED AT FIN STA 157.2 STR 8L. CRACK RAN FROM CTR OF HOLE TO EDGE OF STRINGER. FABRICATED REPAIR ANGLE PER MM 55-30-0 FIG 803 OK TO INSTALL REPAIR. INSTALLED REPAIR PER M/M 55-30-0 FIG 803.SDR DL72S981809Cowl · wornFOUND AT HMV, STA 1352 FWD COWLING RING WORN THROUGH AT 6 O'CLOCK POSITION. ROUTED OUT DAMAGE MANFCT BDLER PER MM 53-11-0 PG 801 AND INSTALLED PER SRM 53-11-0 PG 801.SDR DL72S981742Bypass Light · illuminatedNR 3 ENG FILTER BYPASS LIGHT ILLUM. ENG WAS SHUTDOWN. ENG WINDMILLED FOR REST OF FLT. REMOVED AND INSPECTED NR 3 OIL FILTER, NO MATERIAL IN FILTER. CHIP DETECTOR ALSO CLEAN. FWD OIL BYPASS SYS TO MCO AND PLAC PER 79-00-02. WINDMILLING OK PER MM 71-00 PG SDR DL72S981737Battery Pack · dischargedAFT OVERHEAD EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK, OPS CK GOOD.SDR DL72S981730Chord · crackedDURING ACCOMPLISHMENT OF 4-58560-3AD, A CRACK WAS FOUND IN THE VERT FLANGE OF THE WING TO FUSELAGE UPPER ATTACH CHORD. CRACK PROPAGATES FROM THE EDGE OF THE CHORD ABOVE THE TWO FWD MOST FASTENER HOLES AND TRAVELS DOWN. REPAIRED PER ERA 332062-14AD.SDR DL72S981724Rib · crackedUPPER CHORD OF THE LT WING RIB AT WS 171.5 WAS FOUND W/CRACKS. THE CRACKS WERE LOCATED EMANATING FROM FASTENER HOLES ON THE HORIZ FLANGE OF THE CHORD ANGLE UNDER WING STRINGERS 17 AND 20. REPAIRED PER ERA 332081-14.SDR DL72L981760Spar · crackedTHE REAR SPAR OF THE RT ELEVATOR WAS FOUND WITH A .1875 INCH TYPICAL CRACK AT CENTER HINGE BRACKET SHEAR PLATE. THE CRACK WAS STOP DRILLED PER THE REQUIREMENTS OF AD 96-06-05 AND S/B 727-55-0089. THE REPAIR WAS DOCUMENTED PER ER/A 365499-14AD WHICH ESTABLISHSDR CALA9801500Skin · crackedINSPECTION FOUND TWO 2.5 INCH CRACKS AT RIVET HEADS FORWARD OF OUTBOARD SEQUENCE CARRIAGE ATTACH POINT OF RT INBOARD FOREFLAP. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30.SDR DL72L981718Stringer · corrodedSTRINGER 29R FS 995 CORRODED BEYOND LIMITS. REPAIRED PER SRM 53-10-11 FIG 3.SDR DL72L981717Web · crackedFOUND ON F-1 LETTER CHECK NRC NR 61, TWO 1 INCH CRACKS, LOWER TORQUE BOX LT WEB UPPER EDGE ABOVE LIGHTENING HOLE STA 1223. INSTALLED DOUBLER PER M/M 53-11-0 PG 832.SDR CALA9801495Stiffener · crackedINSPECTION FOUND STIFFENER CRACKED AT LT WING TRAILING EDGE FALSE SPAR WHERE FLAP TRACK NR 3 IS LOCATED. THE STIFFENER WAS REMOVED IAW SRM 51-30-2. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2, AND 51-30-2.SDR CALA9801494Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 950A-950B, LBL 46. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-5, FIGURE 1, 51-10-2, AND MM 51-20-11.SDR CALA9801493Seat Track · corrodedINSPECTION FOUND RT OUTBOARD SEAT TRACK CORRODED AT STA 990-1030. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 53-10-5, 51-10-2, AND MM 51-20-11.SDR CALA9801492Seat Track · corrodedINSPECTION FOUND RT OUTBOARD SEAT TRACK CORRODED AT STA 950-950A. THE SEAT TRACK WAS REMOVED. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, FIGURE 1 AND 7, 51-30-2, 51-10-2, AND MM 51-20-0.SDR CALA9801491Support · corrodedINSPECTION FOUND R-1 DOOR FORWARD SUPPORT CORRODED. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 52-10-1 AND MM 51-20-11.SDR CALA9801490Seat Track · corrodedINSPECTION FOUND LT SEAT TRACK CORRODED AT STA 1050-1060. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, FIGURE 1.SDR DL72S981705Chord · crackedUPPER CHORD ANGLE OF THE RT WING AT WS 171.5 WAS FOUND WITH TWO CRACKS. THE CRACKS WERE LOCATED AT FASTENER HOLES ON THE HORIZ FLANGE OF THE CHORD ANGLE UNDER STRINGERS 16 AND 19. ALSO, THE S18 TAB WAS CRACKED. REPAIRED PER ERA 332040-14.SDR CALA9801485Bracket · corrodedINSPECTION FOUND CORROSION ON TWO L-ANGLE BRACKETS AT AFT SIDE OF STA 251.8, UP SIX INCHES AND TWELVE INCHES FROM FLOOR LEFT SIDE OF COCKPIT. TWO NEW L-ANGLE BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND MM 51-20-11.SDR CALA9801484Angle · corrodedINSPECTION FOUND FLOOR ATTACH ANGLE IN FORWARD CARGO PIT CORRODED AT STA 560, RBL 20. THE CORRODED AREA WAS CUT OUT, AN ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, FIGURE 1.SDR DL72S981733Skin · corrodedAN AREA OF CORROSION WAS FOUND IN THE BELLY SKIN AT FS 680 AND STR 28R. THE CORROSION WAS REMOVED WITH A SKIN CUTOUT. THE CUTOUT WAS NEAR TWO PREVIOUS REPAIRS WHICH WERE REMOVED AND ONE LARGER ALUMINUM EXTERNAL SKIN DOUBLER WAS INSTALLED PER THE GUIDELINES OFSDR DL72S981702Oven · smokingFWD GALLEY OVENS EMITTED BURNING PLASTIC SMELL AND VISABLE SMOKE AFTER TURNING ON. FOUND PLASTIC SHIPPING LABEL ON SIDE OF FOOD CARRIER. REMOVED AND REPLACED CARRIER.SDR CALA9801481Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 1136, RBL 25. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, 51-30-5, 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9801480Frame · corrodedINSPECTION FOUND WEB CORRODED AT FLIGHT DECK FS 219.8, RT FRAME, DIRECTLY BELOW R-2 SLIDING WINDOW. THE WEB WAS REMOVED IAW SRM 51-30-2. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-30-2, 51-10-2, AND MM 51-20-11.SDR CALA9801479Splice · corrodedINSPECTION FOUND BUTT SPLICE CORRODED, DENTED, AND GOUGED AT NR 3 RT CARGO AREA. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-2.SDR CALA9801478Web · crackedINSPECTION FOUND A 1.5 INCH CRACK AT AFT LIGHTENING HOLE OF C-1 CARGO DOOR WEB. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, PAGE 6B, 51-40-2, 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9801474Angle · corrodedINSPECTION FOUND FUSELAGE FRAME ANGLE CORRODED AT STA 360 BETWEEN STRINGER 17R AND 20R. THE ANGLE WAS REMOVED IAW SRM 51-30-2. THE CORROSION WAS REMOVED IAW SRM 51-10-6. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.SDR CALA9801473Sill · corrodedINSPECTION FOUND R-2 DOOR LOWER SILL CORRODED AT BS 1065. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-3. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-11.SDR DL72K981694Battery · dischargedON L/O, FOUND AISLE EMERGENCY LIGHT OUT AT ROW 9. REPLACED BATTERY.SDR CALA9801462Intercostal · crackedINSPECTION FOUND THREE CRACKS IN UPPER FLANGE OF INTERCOSTAL BETWEEN FS 720 AND 720A. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-11.SDR CALA9801461Angle · crackedINSPECTION FOUND TWO ATTACH ANGLES CRACKED UNDER OUTBOARD END OF NR 12 SPOILER AT SUPPORT ROD LOWER ATTACH POINT OF RT WING TRAILING EDGE. THE ATTACH ANGLES WERE REMOVED. TWO NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM SDR CALA9801460Angle · crackedINSPECTION FOUND A CRACK ON THE INBOARD SIDE OF L/E CAVITY BULKHEAD LOWER ANGLE APPROXIMATELY TWENTY INCHES AFT OF KRUEGER FLAP HINGE LINE AT LT WING LEADING EDGE STA 130. THE ANGLE WAS REMOVED AND A NEW REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40SDR CALA9801459Seat Track · corrodedINSPECTION FOUND FORWARD END OF LT INBOARD SEAT TRACK CORRODED AT STA 344 TO 384. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, 51-10-2, 51-30-2, AND MM 51-20-0.
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