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 CALA9701702Control Tab · disbondedINSPECTION FOUND RT ELEVATOR CONTROL TAB TRAILING EDGE DISBONDING. THE TAB WAS REMOVED AND A SERVICEABLE TAB WAS INSTALLED IAW SRM 51-40-10.SDR CALA9701701Stringer · crackedINSPECTION FOUND A .75 INCH CRACK IN AFT TANG AT AFT VENT BOX STRINGER INSIDE RT WING TANK ACCESS CUTOUT 7616, WS 629. THE AREA WAS REPAIRED IAW EA 5762-01050.SDR CALA9701700Rib · crackedINSPECTION FOUND A 2 INCH CRACK IN RIB AT FIRST LOWER STRINGER FROM FRONT SPAR, WS 738.50 AT ACCESS CUTOUT 7701, RT WING. THE RIB WAS REPAIRED IAW SRM 57-10-5, FIGURE 2, 51-30-2 AND 51-10-2.SDR DL72S972582Fitting · corrosionRT FT WING ATTACH FITTING HAS CORROSION AT SEVERAL LOCATIONS INSIDE BORE. REMOVED CORROSION IAW SRM 53-40-1 PG 18. TREATED AND PAINTED PER PS 900-3-6.SDR DL72S972581Stringer · crackedSTRINGER CRACKED WS 686.5 STRINGER NR 10 IS CRACKED AT FASTENER HOLE. REPAIRED PER MM 57-13-0.SDR CALA9701693Clip · corrodedINSPECTION FOUND CORROSION ON CLIP RT SIDE UNDER CABIN FLOOR EIGHT INCHES FORWARD OF FS 1183, STRINGER 18R. FASTENERS AND PARTS WERE REMOVED, A DOUBLER ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CALA9701692Rib · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT WING RIB. THE CRACK WAS LOCATED AT LOWER FLANGE WHERE IT MOUNTS TO SECOND FROM FORWARD END HEAVY STRINGER, WS 656.50, ACCESS CUTOUT 7217. THE RIB WAS REPAIRED IAW SRM 57-10-5, FIGURE 1.SDR CALA9701691Control Tab · disbondedINSPECTION FOUND LT ELEVATOR CONTROL TAB OUTBOARD TRAILING EDGE CORNER SEPARATING. THE ELEVATOR TAB WAS REMOVED AND A SERVICEABLE TAB WAS INSTALLED IAW MM 27-30.SDR CALA9701690Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT RT AFT OVERWING EXIT CUTOUT. THE SKIN WAS REPAIRED IAW SRM 53-30-3, FIGURE 16. THE EXIT HATCH WAS TESTED IAW MM 52-21-0.SDR CALA9701689Floorbeam · crackedINSPECTION FOUND A .5 INCH CRACK OUT OF FORWARD FASTENER HOLE TO EDGE IN FLOORBEAM AT BS 940, LBL 59. A REPAIR WAS PERFORMED IAW JA5310-0185301001 AND REPAIR DOCUMENT M AND E NR 07-5310-1-0143.SDR CALA9701688Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN UPPER INBOARD AREA OF ANGLE AT RT AFT STAIR TORQUE BOX, STA 1263R. THE CRACKED ANGLE WAS REMOVED IAW SRM 51-30-2. THE WEB WAS REMOVED IAW SRM 51-30-2. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2. THE WEB WAS INSSDR CALA9701687Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED WITH A BROKEN RIVET AT STA 680, STRINGER 26R. THE CORROSION WAS REMOVED AND THE CORRODED AREA WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-40-5.SDR CALA9701686Skin · corrodedINSPECTION FOUND LEFT CENTER FUSELAGE SKIN CORRODED WITH A BROKEN RIVET AT STA 720A, STRINGER 26L. THE CORRODED AREA WAS CUT OUT AND THE CORROSION WAS CLEANED IAW SRM 51-10-6. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 53-30-3, AND 51-30-2.SDR CALA9701685Skin · crackedINSPECTION FOUND TWO EACH .125 INCH CRACKS IN NLG WHEEL WELL TOP CENTER PANEL AT BL 0, JUST FORWARD OF STA 294.5. THE CRACKS WERE STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2.SDR CALA9701679Light · inoperativeINSPECTION FOUND AFT AIRSTAIR OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT ASSEMBLY WAS REMOVED AND REPLACED.SDR DL72S972757Skin · puncturedTHE COVE SKIN WAS FOUND WITH A HOLE 26 FROM IB END DURING SHOP VISIT. THE DAMAGE WAS REMOVED AND A DOUBLER INSTALLED PER 727 MM 57-52-00.SDR DL72S972756Angle · crackedTHE AFT LOWER CHORD ANGLE WAS FOUND CRACKED DURING SHOP VISIT. THE CHORD WAS REPAIRED PER 727 MM 57-52-00 BY REMOVING DAMAGE AND REPLACING AND INSTALLING A DOUBLER.SDR DL72S972755Angle · crackedTHE LOWER AFT CHORD ANGLE WAS FOUND CRACKED 18 FROM IB END DURING A SHOP VISIT. THE CHORD WAS REPAIRED PER 727 MM 57-52-00 BY REMOVING DAMAGE AND INSTALLING A DOUBLER.SDR DL72S972626Rib · crackedNR 6 SLAT RIB CRACKED LOWER SURFACE. REMOVED RIVETS FORM RIB, BEGAN FABRICATION OF REPAIR DOUBLERS PER M/M 57-40-0 FIG 814. DRILLED AFT DOUBLER, STOP DRILLED PER SRM 57-54-0. ROUTED OUT DAMAGE PER SRM. INSTALLED REPAIR PER SRM.SDR DL72S972625Rib · crackedNR 7 SLAT RIB CRACKED JUST OUTBD OF ACTUATOR ROD END AREA. FABRICATED REPAIR PER MM 57-54-0 FIG 814. INSTALLED REPAIR PER MM 57-54-0 FIG 814.SDR DL72S972624Rib · crackedNR 6 SLAT RIB CRACKED ON INBD END. MADE DOUBLER IAW MM. DRILLED UP AND TREATED AND PAINTED. INSTALLED DOUBLER PER M/M 57-54-0 FIG 814. INSTALLED SEAL.SDR DL72S972623Stop · wornNR 4 SLAT INBD STOP WORN, 2ND WEB FROM INBD END CRACKED OUT UNDER N/P. FABRICATED REPAIR PER MM 57-54-0 FIG 814. OK TO TREAT AND PAINT. TREATED AND PAINTED PER PS 900-2 NR 5. INSTALLED REPAIR PER MM 57-54-0 FIG 814. WEAR WITHIN LIMITS PER MM 27-87-0 FIG 5SDR DL72S972580Stringer · crackedLT WING STR TO RIB HFEC INSPECTION SHOWS STRINGER TO RIB ATTCH FLANGE MARKED 'C' AT WS 629.0 HAS CRACK INDICATIONS -MARKED- THAT EXTENDS FROM HOLE TO EDGE OF FLANGE. CUTOUT ACCESS HOLE ON VENT BOX PER MM 57-13-10. DRILLED REPAIR PARTS PER MM 57-13-10 FIG 804SDR DL72S972579Fitting · corrosionCORROSION ON RT FRONT SPAR WING TO BODY FWD FITTING. REMOVED CORROSION AT PER SRM 51-10-6. TREATED AND PAINTED PER PS 900-3-6.SDR DL72S972578Fitting · corrosionCORROSION ON LEFT AFT SPAR WING TO BODY FITTING (AFT END). REMOVED CORROSION IAW SRM 53-40-1 PG 18. TREATED AND PAINTED PER PS 900-3-6.SDR DL72S972460Light · inoperativeL1 DOOR EXIT SIGN EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY.SDR DL72S972459Battery Charger · inoperativeE-PATH LIGHT INOP ROWS 12 TO 19. REPLACED BATTERY CHARGER.SDR DL72L972468Battery · dischargedCABIN EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK.SDR DL72K972461Battery · dischargedL1 DOOR OVERHEAD EMERGENCY EXIT SIGN WILL NOT ILLUM. REPLACED BATT'S IN LIGHT ASSY, CKS NML.SDR DL72S972452Battery Pack · dischargedF/C OVRHD EMERGENCY LIGHTS INOP. REPLACED BATTERIES.SDR DL72S972438Cable · out of adjAFT AIRSTAIRS OPENED IN FLIGHT. FOUND OVERCENTER BUNGEE WEAK. REPLACED T/S AFT AIRSTAIRS. REPLACED UPLOCK SW, CHECKED AND ADJ CABLE RIGGING PER M/M 52-62-01, SYS OPS CKS NORMAL. INSPECTED AFT AIRSTAIR UPLOCK LINKAGE, NO SHEARED BOLTS OR OBVIOUS DAMAGE.SDR DL72K972444Skin · crackedA 1 INCH CRACK VERT STAB SKIN BELOW ROUND ACCESS PANEL 9523. REPAIRED PER MM 54-30-0 PG 803.SDR DL72K972443Skin · crackedA 1 INCH CRACK AT VERT STAB SKIN BELOW ROUND ACCESS PANEL 9524. REPAIRED PER MM 54-30-0 PG 803.SDR DL72K972442Web · crackedA .25 INCH CRACK PAST ROUTE OUT AT RT VERT TORQUE BOX WEB STA 1283. REPAIRED PER MM 53-11-0.SDR DL72K972441Web · crackedA 1.375 INCH CRACK UPPER LT TORQUE BOX WEB LIGHTENING HOLE STA 1293. REPAIRED PER MM 53-11-0 PG 828.SDR DL72S972622Skin · crackedSKIN CRACKED AT INSPECTION PANEL 9524. ROUTED OUT CRACK AND MANUFACTURED DOUBLER PER M/M 54-30-0. INSTALLED DOUBLER PER SRM 54-30-0, FIG 803.SDR DL72S972577Rib · crackedCRACK - STRINGER TO RIB WS 629, S-9 AFT HOLE, RT WING. REPAIRED PER MM 57-13-00.SDR DL72S972576Rib · crackedCRACK - STRINGER TO RIB WS 629, S-13 AFT HOLE, RT WING. REPAIRED PER MM 57-13-00.SDR DL72S972575Rib · crackedRT WING WS 629 S-AA CRACKED AT STR TO RIB CONNECTION REF OP8602 RC 882. REPAIRED PER MM 57-13-00.SDR DL72S972574Light Box · corrodedLIGHT BOX CORRODED AROUND EDGES STA 720B AND 720C BETWEEN STRINGERS 16R TO 14R. REMOVED LIGHT BOX. REMOVED CORROSION PER SRM 51-10-6 NOT WITHIN ALLOWABLE LIMITS PER SRM 53-30-1 FIG 7. COMPLETED DRILLING DOUBLER PER SRM 53-30-3 FIG 22. INSTALLED DOUBLER PERSDR DL72S972573Stringer · corrodedLIGHT BOX CORRODED STRINGER 152, BETWEEN STA 720B AND 720C. REMOVED LIGHT BOX FOR ACCESS, REMOVED CORROSION PER 51-10-6 NOT WITHIN ALLOWABLE LIMITS PER SRM 53-30-1 FIG 7. COMPLETED FABRICATING REPAIR DOUBLER PER SRM 53-30-3 FIG 22 T AND P PER PS 900-2 NR 5. SDR DL72S972572Stringer · crackedHFEC INSP SHOWED CRACK INDICATION AT WS 656.5 FWD VENT HOLE. CUT ACCESS HOLE IN VENT BOX PER M/M 57-13-00. REPAIRED CRACK PER MM 57-13-0 FIG 80.SDR DL72S972474Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT THE S-26L LAP SPLICE AT STA 575. THE SKIN DAMAGE IS ADJACENT TO A PREVIOUSLY INSTALLED INTERNAL REPAIR. THE NEW DAMAGE WAS REPAIRED WITH AN OVERLAPPING DOUBLER PER ER/A 363252-14, REV A.SDR DL72S972466Skin · crackedFUSELAGE/ F-N WINDOW POST : REPAIR FOR SKIN CRACK. A .75 INCH CRACK WAS FOUND IN THE SKIN AT THE UPPER AFT CORNER OF THE R5 WINDOW AT THE F-N WINDOW POST. THE CRACK WAS ABOVE AN EXISTING WINDOW POST MOD STRAP. THE CRACK WAS STOP DRILLED AND REPAIRED WITH SDR DL72S972433Battery · dischargedAT LAYOVER, FOUND L2 DOOR EMERGENCY EXIT POWER PACK INOP. REPLACED BATTERIES.SDR DL72S972424Frame · corrodedFUSELAGE FRAME AT STA 560 WAS FOUND WITH CORROSION AT S26R. A 3 INCH SECTION OF A LEG WAS REMOVED. REPAIRED PER ERA 331039-14.SDR DL72K972437Coupling · crackedB-SYSTEM HYDRAULIC QUANTITY LOST IN FLIGHT. FOUND THE QUICK DISCONNECT MALE END COUPLING CRACKED, THE ONE THAT GOES TO THE NR 2 B-PUMP. REPLACED COUPLING AND REPLACED NR 2 B-PUMP. RAN A LEAK CHECK AND FOUND NO FURTHER PROBLEM. REPLACED B-PUMP AS PRECAUTIONSDR DL72K972436Web · crackedRT VENTRAL STAIR WEB LIGHTENING HOLES : NR 1, .25 INCH CRACK UPPER HOLE FWD OF STA 1243. NR 2, .75 INCH AND .25 INCH CRACKS IN UPPER HOLE AFT OF STA 1243. NR 3, (2 EA) .25 INCH CRACKS LOWER HOLE AFT OF STA 1243. FOUND DURING B-2 LETTER CHECK TPA. INSTALLESDR DL72K972435Web · crackedA .75 INCH CRACK LT VENTRAL STAIR WEB UPPER JUST AFT STA 1243. FOUND DURING B-2 LETTER CHECK TPA. INSTALLED DOUBLER PER M/M 53-11-0 NR 16.SDR DL72K972434Chord · crackedA 2 INCH CRACK BEYOND PREVIOUS STOP DRILL AT CHORD BS 1342 LT SIDE ABOVE NR 2 ENG INLET. STOP DRILLED PER M/M 53-11-0 F 807.
Back to Boeing 727-232