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.

SDR DL72S990562Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 360 AND 380. THE CRACKS WERE ROUTED OUT AND REPAIRED PER B727 SRM Mar 11, 1999 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990544Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGMar 11, 1999 · N404DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990541Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 36 CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE LENGTH OF THE PANEL AND REPAIRED WMar 11, 1999 · N499DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990540Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC CONFIRMED 69 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUTOUT ALONG THE ENTIRE LENGTH OF THE PAMar 11, 1999 · N499DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K990555Cowling · wornWORN, NO 2 ENG COWLING LANDING - FROM 1 O'CLOCK TO 11 O'CLOCK POSITION. REMOVED DAMAGED SECTION OF CHORD, FORMED AND DRILLED REPAIR ANGLES FOR SPLICE. DRILLED NEW SECTION OF CHORD OK TO INSTALL. INSTALLED LT SPLICE. COMPLETED INSTALLATION OF RING AND RT SPMar 11, 1999 · N491DA · Boeing 727232 · Engine Cowling SystemSDR DL72K990512Actuator · leakingON WALKAROUND INSPECTION, FOUND NR 14 SPOILER ACTUATOR LEAKING.Mar 11, 1999 · N410DA · Boeing 727232 · Drag Control ActuatorSDR DL72S990560Skin · crackedLFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. HFEC INTERNAL INSPECTION CONFIREMD SEVERAL CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE LENGTH OF THE PAMar 10, 1999 · N403DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990522Skin · crackedWHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12 ON THE S4R LAP JOINT CRACK INDICATIONS WERE FOUND BETWEEN BS 681 AND BS 740. HFEC INSPECTION CONFIRMED 8 CRACK INDICAITONS IN THE LOWER FASTENER ROW OF THE LAP JOINT, IN THE LWR SKIN. REPAIRED PER ERA 33Mar 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990521Skin · crackedWHILE ACCOMPLISHING LFEC INSP PER SI 4-74176-12, ON THE S4R LAP JOINT CRACK INDICATIONS WERE FOUND BETWEEN BS 481 AND 680. HFEC CONFIRMED 15 CRACK INDICATIONS IN THE LWR FASTENER ROW OF THE LAP JOINT IN THE LWR SKIN. REPAIRED PER ERA 332838-14AD, REV A.Mar 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990520Frame · dentedTWO DENTED AREAS WERE FOUND ON THE I/B CHORD OF THE BS 950C FRAME BETWEEN S24L AND 27L. REPAIRED PER ERA 332897-14, REV A.Mar 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S990510Angle · crackedREPAIR ANGLE CRACKED NR 7 SLAT STOP PAD I/B SIDE. REPAIRED PER MM 57-54-0 PG 816.Mar 10, 1999 · N419DA · Boeing 727232 · Leading Edge DevicesSDR DL72S990509Skin · crackedA .25 INCH CRACK FUSELAGE SKIN AT FASTENER JUST AFT OF L-3 COCKPIT WINDOW. REPAIRED PER SRM 53-30-3 FIG 8.Mar 10, 1999 · N419DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990508Bracket · crackedFOUND ON F1 LETTER CK, CRACK IN NR 1 SLAT ACTUATOR SUPPORT BRACKET WEB I/B SIDE. REPAIRED PER MM 57-20-21.Mar 10, 1999 · N419DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S990507Stiffener · crackedFOUND ON F1 LETTER CK, L/E SPAR STIFFENER CRACKED AT LOWER END NR 3 SLAT O/B TRACK I/B SIDE. REPAIRED PER MM 57-20-21.Mar 10, 1999 · N419DA · Boeing 727232 · Leading Edge DevicesSDR DL72S990505Skin · crackedA .5 INCH CRACK IN RT ELEVATOR LOWER SKIN AT FWD SPAR AREA. REPAIRED PER SRM 55-20-3 FIG 4.Mar 10, 1999 · N419DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S990501Frame · crackedFOUND ON F1 LETTER CK, AFT ENTRY DOOR FRAME CRACKED RT SIDE 10 INCHES BELOW THE TOP OF THE DOOR CUTOUT. REPAIRED PER SRM 53-10-9.Mar 10, 1999 · N419DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990490Skin · crackedWHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON S4R LAP JOINT, 2 CRACK INDICATIONS WERE FOUND BETWEEN BS 360 AND 481. HFEC INSP VERIFIED CRACK INDICATIONS. REPAIRED PER ERA 332834-14AD, REV A.Mar 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990489Skin · misdrilledFUSELAGE SKIN WAS MISDRILLED AT S11R AT BS 1233. REPAIRED PER ERA 332842-14, REV A.Mar 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990488Fitting · corrodedCORROSION FOUND IN THE RT MLG SUPPORT BEAM O/B BORE AND IN THE FWD AND AFT FITTINGS. REWORKED PER ERA 332851-14.Mar 10, 1999 · N411DA · Boeing 727232 · Wing, Landing Gear Attach FittingsSDR DL72S990487Fitting · corrodedCORROSION WAS FOUND IN THE BORE OF THE RT WING AFT TERMINAL FITTING. REPAIRED PER ERA 366788-14, REV A.Mar 10, 1999 · N411DA · Boeing 727232 · Wing, Fuselage Attach FittingsSDR DL72S990486Frame · corrodedBS 600 FRAME BELOW THE CARGO FLOOR AT STR 28R WAS FOUND CORRODED. THE UPPER FRAME OF THE LOWER LOBE CTR FRAME SECTION AND SOME EXISTING REPAIRS WERE ALSO FOUND CORRODED. REPAIRED PER ERA 332893-14, REV A.Mar 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S990549Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 REVEALED A CRACK BETWEEN FS 660 AND 681 IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTION OF THE ENTIRE PANEL CONFIRMED THE SINGLE CRACK. THE CRACK WAS ROUTED OUT OMar 9, 1999 · N403DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990548Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTION OF THE ENTIRE SKIN PANEL CONFIRMED ONE CRACK BETWEEN FS 400 AND 420. THE CRACK AREA WAS ROUTED OUTMar 9, 1999 · N403DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990485Skin · wornTHE UPPER SKIN OF THE S19R LAP SPLICE WAS FOUND TORN AT BS 720E-5 DUE TO MISALIGNMENT OF THE WING TO BODY FAIRING UPON INSTALLATION. REPAIRED PER ERA 332901-14AD, REV A.Mar 9, 1999 · N531DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K990590Web · crackedWEB CRACKED VERTICAL STAB INTERIOR - WEB AT STA 1303 IS CRACKED AT BOTH RT AND LT LOWER CORNERS, MARKED. STOP DRILLED CRACKS AND DYE PENETRATE INSP RT AND LT SIDE PER SRM 53-10-4 FIG 17. FABRICATED REPAIR DOUBLERS AND TAPERED SHIM PER SRM 53-10-4 FIG 17. TRMar 9, 1999 · N491DA · Boeing 727232 · Vertical StabilizerSDR DL72K990484Skin · crackedWHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON S4R, CRACK INDICATIONS WERE FOUND BETWEEN BS 481 AND 680. CONDUCTING HFEC INSP CONFIRMED 29 CRACK INDICATIONS IN THE LWR FASTENER ROW OF THE LAP JOINT. REPAIRED PER ERA 332875-14AD, REV A.Mar 9, 1999 · N481DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K990483Skin · crackedWHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON S4R CRACK INDICATIONS WERE FOUND BETWEEN BS 481 AND 680. GAINING INTERNAL ACCESS AND CONDUCTING HFEC INSP CONFIRMED 29 CRACK INDICATIONS IN THE LWR FASTENER ROW OF THE LAP JOINT. REPAIRED PER ERA 33Mar 9, 1999 · N481DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990547Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. HFEC INTERNAL INSPECTION CONFIRMED TWO CRACKS BETWEEN FS 440 AND 460. THE CRACKS WERE ROUTED OUT OF THE SKIN LAP AND Mar 8, 1999 · N497DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990479Mount · crackedFOUND ON E1 LETTER CK, 1 INCH VISIBLE CRACK NR 1 SLAT ACTUATOR O/B MOUNT WEB ABOVE TRUNNION FITTING. REPAIRED PER MM 57-20-21.Mar 8, 1999 · N534DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S990478Frame · crackedFOUND AT E-1 LETTER CK, AFT ENTRY DOOR FRAME CUTOUT HAS .5 INCH VISIBLE CRACK LT SIDE. REPAIRED PER SRM 53-10-9.Mar 8, 1999 · N534DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K990480Battery Pack · dischargedAFT OVERHEAD EMERGENCY EXIT SIGN WOULD NOT ILLUM WHEN TESTED. REPLACED BATTERY CARTRIDGE AND RACK ASSY CKS NORMAL.Mar 8, 1999 · N415DA · Boeing 727232 · Emergency LightingSDR DL72S990492Skin · crackedLFEC INSPECTION REVEALED CRACK INDICATIONS IN THE LOWER ROW OF FASTENERS OF THE LOWER SKIN AT THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 680. INTERNAL HFEC INSPECTION CONFIRMED 54 CRACK INDICATIONS ALONG THE LENGTH OF THE PANEL. THE LAP SPLICE WMar 7, 1999 · N497DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990491Skin · crackedLFEC INSPECTION REVEALED CRACK INDICATIONS IN THE LOWER ROW OF FASTENERS OF THE LOWER SKIN PANE AT THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION CONFIRMED 38 CRACKS ALONG THE LENGTH OF THE PANEL. THE SKIN LAP WAS CUTOUT ALOMar 7, 1999 · N497DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L990494Skin · crackedLFEC INSPECTION REVEALED A CRACK INDICATION NEAR THE LOWER FASTENER ROW OF THE LOWER SKIN AT THE STRINGER 4R SKIN LAP SPLICE NEAR FS 442. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE AT FS 442. THE CRACK WAS REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTEDMar 7, 1999 · N511DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L990493Skin · crackedLFEC INSPECTION INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4R SKIN LAP SPLICE NEAR FS 405. HFEC INTERNAL INSPECTION OF THE SKIN LAP CONFIRMED A CRACK AT FS 405. THE CRACK WAS REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENMar 7, 1999 · N511DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72L990497Skin · crackedTHE VERTICAL STABILIZER SKIN WAS FOUND CRACKED AT FIN STA 42 AT STRINGER 1R BETWEEN RIB 3A AND 4. THE CRACK WAS LOCATED BELOW AN EXISTING REPAIR. THE EXISTING REPAIR WAS REMOVED AND BOTH DAMAGE LOCATIONS INCORPORATED INTO ONE REPAIR PER B727 SRM 55-30-3, FIGMar 6, 1999 · N506DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72S990467Battery · dischargedFLASHLIGHT HAD NO CHARGE. REPLACED BATTERY, OPS CK GOOD.Mar 5, 1999 · N544DA · Boeing 727232 · Emergency LightingSDR DL72S990465Battery Pack · dischargedOVERWING RT SIDE EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND OPS CK GOOD.Mar 5, 1999 · N544DA · Boeing 727232 · Emergency LightingSDR DL72L990469Skin · crackedFOUND DURING F-2 LETTER CHECK, .5 INCH CRACK LT ELEVATOR LOWER SKIN FROM RIVET FWD I/B SIDE OF TAB ROD CUTOUT. REPAIRED PER SRM 55-20-3 FIG 4.Mar 5, 1999 · N506DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S990457Angle · crackedFOUND ON C2 LETTER CK, RT KEEL BEAM SUPPORT ANGLE CRACKED AT STA 870. REPLACED ANGLE PER SRM 53-10-9.Mar 4, 1999 · N544DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990460Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED SEVERAL CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP WAS CUT OUT AND REPAIRED WITHMar 3, 1999 · N402DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990459Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION CONFIRMED 35 CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL LENGTH AND REPAMar 3, 1999 · N402DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990449Web · crackedFOUND ON E2 LETTER CK, LT VERTICAL TORQUE BOX WEB CRACKED AT RIVET ALONG UPPER EDGE AT STA 1266. REPAIRED PER MM 53-11-0.Mar 3, 1999 · N420DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S990441Fitting · wornWEAR WAS FOUND ON BOTH ATTACH LUGS FOR THE HORIZ STAB JACK SCREW MECHANISM. WEAR WAS ON BOTH I/B AND O/B FACES OF EACH LUG. REWORKED PER ERA 332860-14, REV A.Mar 3, 1999 · N411DA · Boeing 727232 · Horizontal Stabilizer StructureSDR DL72S990431Pump · damagedAFTER T/O ON INIT CLMB, BOTH HYD SYS B PUMPS LOW PRESS LIGHTS ILLUM. HYD QTY IN A SYS DROPPED TO 2.5 GALS, B QTY APPEARED NORMAL. PRESS THEN DROPPED TO NEAR ZERO, TURNED PUMPS OFF IAW POM 1 TO 2 MINS AFTER ILLUMINATION. FOUND O-RING ON NR 1 B SYS HYD PUMP CMar 2, 1999 · N522DA · Boeing 727232 · Hydraulic Pump (Electric/Engine), MainSDR DL72L990433Light · inopR1 OVER DOOR EMER LIGHT INOP. REPLACED LIGHT, CKS GOOD.Mar 2, 1999 · N511DA · Boeing 727232 · Emergency LightingSDR DL72S990430Battery Pack · dischargedEXTERIOR EMERGENCY LIGHT R/S BETWEEN OVERWING EMERGENCY EXITS INOP. REPLACED BATTERY PACK, OPS CHECK GOOD.Mar 1, 1999 · N477DA · Boeing 727232 · Emergency LightingSDR DL72S990425Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 & 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 94 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRFeb 28, 1999 · N400DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990424Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 48 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP WAS CUT OUT OF THE PANEL AND REPAFeb 28, 1999 · N400DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990423Skin · crackedLFEC INSPECTION OF THE STRINGER 4R LAP SPLICE INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTION CONFIRMED 3 CRACKS BETWEEN FS 360 AND 380. THE CRACKED AREA OF SKIN LAP WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUFeb 28, 1999 · N400DA · Boeing 727232 · Fuselage Main, Plate/Skin
Back to Boeing 727-232