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 95FDEA01858Frame · dentedDENT IN FRAME AT BS 1030 BETWEEN STR 25 AND 26 LBL 30 WL 150. REPAIRED DENT IN FRAME AT BS 1030 BETWEEN STR 25 AND 26 LBL 30 WL 150 PER FEDEX SRM 51-40-3.SDR 95FDEA01856Frame · gougedGOUGE AT FRAME BS 480 BETWEEN STR 14 TO 13R. REPAIRED FRAME AT BS 480 BETWEEN STR 14 TO 13R PER FEDEX 727 SRM 53-10-4.SDR 95FDEA01855Splice · damagedDRILL START ON FRAME SPLICE BS 1130 BETWEEN STR 6 TO 7R. REMOVED FRAME SPLICE AT BS 1130 BETWEEN STR 6 TO 7R AND INSTALLED NEW FRAME SPLICE.SDR 95FDEA01854Frame · dentedDENT IN FRAME BS 660 LBL 34 WL 160. REPAIRED DAMAGED FRAME AT BS 660 LBL 34 WL 160 IAW FEDEX B727 SRM 51-40-3.SDR 95FDEA01853Floorbeam · corrosionCORROSION (C53-224-01, 1) FLOORBEAM STA 400 WL 208.1 LBL 8. FLOORBEAM WAS REPAIRED PER FEDEX B727 SRM 53-10-8 FIG 8 AT STA 400 WL 208.1 LBL 16 TO RBL 9.SDR 95FDEA01852Stringer · gougedGOUGE IN STR 7 LT, BS 965 WL 285 LBL 58. REMOVED DAMAGED STR AND REPAIRED PER SRM 53-10-3.SDR 95FDEA01851Skin · lightning strikeLIGHTNING STRIKE AT BS 680 RBL 5 WL 148. DUE TO BULGE IN SKIN PATCH AT STA 683 RBL 20 WL 150, THE ORIGINAL SKIN PATCH WAS REPLACED AND ALL WORK WAS DONE IAW FEDEX 727 SRM 53-30-3.SDR 95FDEA01849Beam · corrosionCORROSION (C53-224-01), AT BS 950 BEAM TOP CHORD LBL TO RBL 27 WL 208.1. REMOVED CORROSION AND REPAIRED OUT OF LIMIT AREAS PER EA 7-5310-26740 AND FEDEX SRM 53-10-01.SDR 95FDEA01848Frame · damagedMECHANICAL DAMAGE ON FRAME BS 680 RBL 38 WL 162. REPAIRED FRAME AT BS 680 RBL 38 WL 162 IAW FEDEX SRM 51-40-3, DUE TO MECHANICAL DAMAGE PER FEDEX SRM 53-10-1.SDR 95FDEA01847Skin · corrodedCORROSION (C53-111-01), ON INTERIOR OF SKIN AT BS 713 BETWEEN STR 22 TO 23L. REMOVED CORROSION FROM INTERIOR OF SKIN AT BS 713 BETWEEN STR 22 TO 23L. REMOVED .014 FROM ORIGINAL MATERIAL THICKNESS, IN AN AREA OF 1.5 INCH BY 2.5 INCH BY .050 INCH. CORROSION WSDR 95FDEA01846Floorbeam · double drilledUPON REMOVAL OF SEAT TRACK NR0788, FOUND DOUBLE HOLES IN FLOORBEAM BS 580 BL 0 WL 208.5. REPAIRED DOUBLE HOLES IN FLOORBEAM BS 580 BL 0 WL 208.5 IAW FEDEX SRM 53-10-8 FIG 3.SDR 95FDEA01845Skin · dentedWHILE WORKING NR0774, FOUND DENT IN THE FUSELAGE SKIN BS 1304 UNDER STR 17R. REMOVED DAMAGE, FABRICATED DOUBLER, SEALED AND INSTALLED DOUBLER PER FEDEX SRM 53-30-3 FIG 1.SDR 95FDEA01844Frame · corrodedCORROSION (C53-111-01), ON LOWER SIDE OF FLANGE ON BS 680 FRAME BETWEEN STR 23 TO 25L. REPAIRED LOWER SIDE OF FLANGE ON BS 680 FRAME BETWEEN STR 23 TO 25L, DUE TO CORROSION BEING OUT OF LIMITS PER FEDEX SRM 53-10-01.SDR 95FDEA01843Frame · dentedDENT IN FRAME BS 660 RBL 31 TO 36 WL 157. REPAIRED DENT IN FRAME BS 660 RBL 30 TO 43 WL 157 PER FEDEX SRM 51-40-3.SDR DL72S960377Skin · corrodedDURING INSPECTION, MAINTENANCE FOUND THE UPPER SKIN AT THE S-26L LAP JOINT CORRODED BETWEEN STA 700 AND STA 706. DAMAGE REMOVAL RESULTED IN A 3 INCH BY 6 INCH CUT OUT AREA OF THE UPPER SKIN. ALSO, THE 0.020 2024-T3 CLAD BONDED DOUBLER BETWEEN THE UPPER AND LSDR DL72S960392Web · damagedDURING INSPECTION PER S/B 727-53-0129 IN ACCORDANCE WITH AD 94-07-08, THE INBD WEB WAS CUT TO THE BOTTOM EDGE OF THE WEB, THUS SEVERING. ALSO, SEVERAL OBLONG HOLES IN THE WEB WERE FOUND. ACCOMPLISHED REPAIRS PER FORM 8110-3, DATED 12-02-92, BACP TWX DA; -AT;SDR DL72S954604Apu · smokingDEPARTURE TIME WITH APU, EITHER PACK PUTS SMOKE IN CABIN. FOUND APU PUTTING SMOKE IN CABIN DEACTIVATED APU PER MEL.SDR DL72S960432Beam · crackedDURING INSPECTION, FOUND A 2 INCH CRACK IN THE E/E COMPARTMENT DOOR AFT TRANSVERSE BEAM AFT LOWER ATTACH ANGLE. THE CRACK IS LOCATED IN THE RADIUS OF THE L-ANGLE AND RUNS BETWEEN 2 EXISTING ADJACENT FASTENERS. AN EXISTING REPAIR IS INSTALLED ON THE FWD FACE SDR DL72S960380Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THREE LOCATIONS BETWEEN STA 700 AND STA 720, S-27R AND S-28L. DAMAGE WAS MACHINED TO LEAVE A MAXIMUM THICKNESS OF 0.063 IN THE CLAD 2024-T3 SKIN. ALSO, THERE IS AN EXISTING EXTERNAL REPAIR DOUBLER, INSTALLED PER ER/ASDR DL72S960376Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND IN SCATTERED LOCATIONS FROM STA 680 TO 720, BETWEEN S-26L AND 26R. ALSO, THERE WERE THREE EXISTING REPAIR DOUBLERS ON THE LOWER SKIN IN THE SAME AREA. IN ACCORDANCE WITH BAC/O S/B 727-53A203, RV 2, THE EXISTING EXTERNALSDR DL72S954593Rib · crackedUPON INSPECTION, A CRACK WAS FOUND IN RIB NR 9. REPAIRED PER MM 57-54-0 FOR NR 6 L/E SLAT.SDR DL72S954592Rib · crackedUPON INSPECTION, RIB NR 16 WAS FOUND CRACKED. REPAIRED PER MM 57-54-0 FOR NR 6 L/E SLAT.SDR DL72S954591Hook · crackedUPON INSPECTION, A CRACK WAS FOUND IN O/B HOOK. REPAIRED PER SRM 57-50-3 FOR NR 6 L/E SLAT.SDR DL72S954590Rib · crackedUPON INSPECTION, A CRACK WAS FOUND IN A PREVIOUS REPAIR IN RIB NR 10. REPAIRED PER MM 57-54-0 FOR NR 6 L/E SLAT.SDR DL72S954589Rib · crackedUPON INSPECTION, RIB NR 9 ON NR 6 L/E SLAT WAS FOUND CRACKED. REPAIRED PER MM 57-54-0.SDR DL72S954588Rib · crackedUPON INSPECTION, A CRACK WAS FOUND IN RIB NR 18 ON NR 6 L/E SLAT. REPAIRED PER MM 57-54-0.SDR DL72K961588Angle · crackedTHERE IS A 3 INCH CRACK IN THE ANGLE OF THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1273. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THE DAMAGED SDR DL72K954602Cove Skin · crackedFOUND DURING A-2 LETTER CHECK, NR 7 SLAT COVE SKIN ANGLE CRACKED I/B OF TAI DUCT AND UNDER STOP PAD. ALSO, NR 8 COVE SKIN ANGLE CRACKED UNDER TAI DUCT. REPAIRED PER 57-54-0 PG 807 AND 816.SDR 95FDEA01842Fire Warning · activatedNR 2 ENGINE HAD FIRE WARNING IN FLT. LIGHT WENT OUT WHEN THRUST LEVER RETARDED TO IDLE. LIGHT CAME ON AT TOP OF DESCENT AT 35,000 FT. SUSPECT BLEED AIR LEAK, FIRE LOOPS CHECKED GOOD. RAN NR 2 ENGINE, CHECKED FOR AIR LEAKS, CHECKED FIRE WARNING SYSTEM. FOUSDR DL72S954599Angle · crackedDURING SHOP INSPECTION, FOUND NR 4 L/E SLAT WITH LOWER COVE PANEL SUPPORT ANGLE CRACKED AT RIB NR 9. REPAIRED PER MM 57-54-0.SDR DL72S954585Stringer · corrodedDURING INSPECTION, FOUND MISSING AND SHEARED RIVETS AT STRINGER NR 29R AT FS 1176. ALSO, FOUND STRINGER CORRODED. REPAIRED BY REPLACING SECTION OF STRINGER PER SRM 53-10-03 PG 3.SDR DL72S954583Skin · crackedDURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH L/E SKIN CRACKED AT OUTBOARD END. REPAIRED PER SRM 57-30.SDR DL72S954582Tie Angle · crackedFOUND DURING E-2 LETTER CHECK, VERTICAL STAB STRINGER TIE ANGLES CRACKED AT STA 157.200 2ND BAY FROM TOP LT SIDE. TWO ANGLES CRACKED AT 4TH BAY FROM TOP STA 133.800. REPAIRED PER M/M 53-30-0 PAR 3.SDR DL72S954573Rib · wornDURING SHOP INSPECTION, NR 6 L/E SLAT INTERNAL RIB NR 17 WAS FOUND ROUTED BEYOND LIMITS. REPAIRED PER MM 57-54-0.SDR DL72L954595Skin · puncturedDURING GROUND HANDLING, A HOLE WAS PUNCTURED IN THE FUSELAGE SKIN 14 INCHES BY 18 INCHES, BETWEEN FS 420 TO 440 AND S-23R TO S-26R. A PIN IN THE TOWBAR BROKE DURING TOWING AND THE AIRCRAFT STRUCK THE TUG. A TEMPORARY REPAIR WAS INSTALLED AND THE AIRCRAFT WASSDR DL72S960019Skin · crackedTPA MAINTENANCE REPORTED, TWO CRACKS IN THE SKIN AND DOOR SURROUND STRUCTURE IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE FIRST CRACK, APPROXIMATELY 5 INCHES LENGTH, HAS PROPAGATED THROUGH THE EXTERNAL SKIN AND THE BONDED DOUBLER. THE SECOND CRACK 6 INSDR DL72S954807Floorbeam · corrodedAT HMV, CORROSION ON FS 344 FLOORBEAM UPPER CAP LBL 35R BL 25 C53-224-01.05. REPAIRED PER SRM 53-10-8 FIG 10.SDR DL72S954666Bracket · crackedBRACKET CRACKED: NR 1 LE FLAP ACTUATOR INBOARD BRACKET ON FRONT SPAR IS CRACKED IN LOWER FORWARD RADIUS. REMOVED BRACKET. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER MM 57-20-21, PG 811.SDR DL72S954598Rib · crackedDURING SHOP INSPECITON, NR 4 L/E SLAT WAS FOUND WITH CRACKED RIB AT O/B SIDE OF THE O/B SLAT TRACK. REPAIRED PER MM 57-54-0.SDR DL72S954597Rib · crackedDURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH CRACKED RIB ON O/B OF ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0 PG 805.SDR DL72S954567Angle · crackedFOUND .5 INCH CRACK BELOW NR 2 SLAT TAI DUCT, FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0.SDR DL72S954566Angle · crackedFOUND .5 INCH CRACK BELOW NR 3 SLAT TAI DUCT, FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER SRM 57-54-0.SDR DL72S954565Angle · crackedFWD KEEL BEAM ANGLE CRACKED 1 INCH BELOW APU RT SIDE, FOUND DURING A-1 LTR CK TPAMM. TIME LIMITED REPAIR ACCOMPLISHED PER SRM 53-10-9 FIG 13. DAILY INSP REQUIRED AND PERM REPAIR TO BE ACCOMPLISHED WITHIN 100 FLT HOURS.SDR 95FDEA01831Frame · dentedDENT IN FRAME AT BS 520, LBL 32, RBL 46, WL 159 AND 168. REPAIRED DENT IN FRAME AT BS 520, LBL 32, LBL 46, WL 159-168 PER FEDEX SRM 51-40-3.SDR 95FDEA01830Frame · double holeDOUBLE HOLE IN FRAME AT BS 420, STR 4R. REPAIRED DOUBLE HOLE IN FRAME AT BS 420, STR 4R IAW FEDEX SRM 53-10-4.SDR 95FDEA01829Frame · dentedDENT IN FRAME BS 720, LBL 31-37, WL 160. REPAIRED FRAME AT BS 720, LBL 31-37, WL 160 IAW FEDEX SRM 51-40-3.SDR 95FDEA01828Skin · crackedTHE LOWER SURFACE OF THE LT ELEVATOR AT ELEVATOR STA 138, 24 INCHES FORWARD OF T/E HAS A PUNCTURE HOLE THAT IS CRACKED. FABRICATED REPAIR PART AND INSTALLED IT ON THE LOWER SURFACE OF THE LT ELEVATOR AT ELEVATOR STA 138, 24 INCHES FORWARD OF THE T/E IAW FEDEXSDR 95FDEA01823Floor Beam · corrodedCORROSION (C53-224-01(1) FLOOR BEAM STA 328, WL 208.1, LBL 20-LBL 3.SDR 95FDEA01816Frame · dentedDENT IN FRAME AT BS 520, RBL 38-50, WL 172-164. REMOVED DAMAGES AT BS 520, RBL 38-50, WL 172-164. FABRICATED PART, ALODINED, AND PRIMED, AND INSTALLED ON ABOVE AREA, AS PER FEDEX SRM 51-40-3.SDR DL72S960253Rib · crackedDURING SHOP INSPECTION FOR NR 6 LEADING EDGE SLAT, RIBS NR 16 AND NR 18 WERE FOUND TO BE CRACKED. REPAIRED PER MM 57-54-0 FIG 809.
Back to Boeing 727-232