Boeing 727-247

Service difficulty reports · 2,669

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 = '727247'
  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 DL72E992066Angle · repairedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 34 FROM IB END. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A SPLICE DOUBLER AND NEW SECTION OF ANGLE.Apr 28, 1999 · N830WA · Boeing 727247 · Trailing Edge FlapsSDR DL72E992065Angle · misrepairedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 56 FROM IB END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A SPLICE DOUBLER AND A NEW SECTION OF ANGLE.Apr 28, 1999 · N830WA · Boeing 727247 · Trailing Edge FlapsSDR DL72E992041Angle · repairedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 19 FROM THE IB END OF THE FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALL A DOUBER AND SECTION OF ANGLE.Apr 28, 1999 · N830WA · Boeing 727247 · Trailing Edge FlapsSDR DL72E992040Angle · repairedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 33 FROM IB END OF THE FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER AND SECTION OF ANGLE.Apr 28, 1999 · N830WA · Boeing 727247 · Leading Edge DevicesSDR DL72E992039Angle · crackedDURING SHOP INSPECTION, THE LOWER AFT CLOSEOUT ANGLE WAS FOUND CRACKED 55 FROM IB END OF THE FLAP. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0, FIG 802.Apr 28, 1999 · N830WA · Boeing 727247 · Trailing Edge FlapsSDR DL72E990992Rib · crackedLT STR TO RIB ATTACH FLANGE CRACKED INSIDE VERTICAL FIN AT RIB STA 179 STR 8L. FABRICATED REPAIR PER M/M 55-30-0 FIG 803. OK TO INSTALL. REPAIRED PER M/M 55-30-0 RIG 803.Apr 28, 1999 · N830WA · Boeing 727247 · Vertical Stabilizer, Spar/RibSDR DL72E990934Bushing · looseNR 4 FLAPTRACK FWD MOUNT PORKCHOP FITTING BUSHING LOOSE. REMOVED FITTING, BUSHING REMOVED. CORROSION FOUND, REWORKED ON N/R 642.Apr 28, 1999 · N830WA · Boeing 727247 · Trailing Edge FlapsSDR DL72W990923Skin · crackedFUSELAGE SKIN FS 360-380 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETApr 27, 1999 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990922Skin · crackedFUSELAGE SKIN FS 481-681, STRINGER 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC 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 INSPECTION CONFIRMED 20 CRACKS. THE EApr 26, 1999 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990907Skin · crackedFUSELAGE CK REPAIR, LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 21 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP WAS CUTOUT ANApr 25, 1999 · N2821W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990893Power Supply · inopAFT ZONE OF EMERGENCY LIGHTS AFT OF SEAT 26 INOP. DURING SVC CK TEST, REPLACED POWER SUPPLY.Apr 25, 1999 · N295WA · Boeing 727247 · Emergency LightingSDR DL72W990906Skin · crackedFUSELAGE SKIN FS 481-681,STRINGER 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC 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 INSPECTION CONFIRMED 13 CRACKS ALONG THApr 24, 1999 · N2821W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990901Skin · crackedFUSELAGE SKIN FS 440-460 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION OF THE ENTIRE PANEL CONFApr 24, 1999 · N2821W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990884Angle · crackedTORQUE BOX HORIZONTAL Z ANGLE CRACKED AT STA 1273. TORQUE BOX HORIZONTAL ANGLE FWD SIDE OF Z ANGLE CRACKED AT STA 1273. REPLACED PARTS PER SRM 53-10-10.Apr 23, 1999 · N296WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990878Bracket · crackedREF NRC 84 C-2 LETTER CHECK, NR 8 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED. INSTALLED DOUBLER PER M/M 57-20-22.Apr 22, 1999 · N2814W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W990877Bracket · crackedREF NRC 83 C-2 LETTER CHECK, NR 7 SLAT ACT INBD MOUNT BRACKET CRACKED. INSTALLED DOUBLER PER M/M 57-42-0.Apr 22, 1999 · N2814W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72E990874Oil Screen · leakingNR 3 ENG OIL ZERO, SHUT DOWN ENG. FOUND MAIN OIL SCREEN LEAKING. REPLACED MAIN OIL SCREEN AND O-RING SEAL PER MM 71-00 PG 212L AND 212M. NO LEAKS ON ENG RUN.Apr 22, 1999 · N283WA · Boeing 727247 · Turbine Engine Oil SystemSDR 99FDEA00157Skin · corrodedSKIN BULGING AT BS 1115 BETWEEN STR 26L AND 27L. *S/D* REMOVED AND REPLACED SKIN BULGE PER IAW FEDEX EA 7-5330-45222.Apr 21, 1999 · N234FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR 99FDEA00156Floorbeam · corrodedFOUND FLOORBEAM TO BE CORRODED AT BS 1090, RBL 45, WL 208. *S/D* REMOVED AND REPLACED UPPER FLANGE OF FLOORBEAM PER FEDEX EA 7-5310-45246.Apr 21, 1999 · N234FE · Boeing 727247 · Fuselage Main, Floor BeamSDR DL72W990863Skin · crackedA 2.5 INCH CRACK IN RT ELEVATOR LOWER SKIN AFT OF NR 4 BALANCE BOARD. REPAIRED PER SRM 55-20-3.Apr 19, 1999 · N2817W · Boeing 727247 · Elevator, Plate/SkinSDR DL72W990862Frame · crackedFOUND AT B-2 LETTER CHECK, .5 INCH CRACK ON LT AFT ENTRY DOOR FRAME. REPAIRED PER SRM 53-10-9.Apr 19, 1999 · N2817W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990861Frame · crackedFOUND AT B-2 LETTER CHECK, .5 INCH CRACK ON RT AFT ENTRY DOOR FRAME. REPAIRED PER SRM 53-10-9.Apr 19, 1999 · N2817W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990859Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PAApr 19, 1999 · N2816W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990858Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PAApr 19, 1999 · N2816W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990857Skin · 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 PANEL. INTERNAL HFEC INSPECTION CONFIRMED 24 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND Apr 19, 1999 · N2816W · Boeing 727247 · Fuselage Main, Plate/SkinSDR 99FDEA00150Frame · corrodedNR 790 - CORROSION (C53-111-01(3)) ON FRAME AT BS 1070, STR 27R. REPAIRED FRAME AT BS 1070, STR 27R, IAW FEDEX SRM 51-40-3 FIG 1.Apr 16, 1999 · N234FE · Boeing 727247 · Fuselage Main, FrameSDR 99FDEA00149Floorbeam · corrodedNR 794 - CORROSION (C53-111-01(3)) ON FLOORBEAM LWR CHORD AT BS 1070, WL 200, LBL 40 - RBL 48. REMOVED AND REPLACED BS 1070 FLOORBEAM IAW FEDEX EA 7-5310-45262A.Apr 16, 1999 · N234FE · Boeing 727247 · Fuselage Main, Floor BeamSDR 99FDEA00148Stringer · corrodedWHILE WORKING NR 802, FOUND CORROSION ON STRINGER 28R, BS 950E+1.Apr 16, 1999 · N234FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W990825Skin · crackedWHILE ACCOMPLISHING HFEC INSPECTIONS PER SI 4-74176-12AD, REV F, CRACK INDICATIONS WERE NOTED BETWEEN BS 520 AND 681 AT S4R. ADDITIONALLY, GROUND DAMAGE WAS INDUCED TO THE AREA WHILE ACCOMPLISHING THE STANDARD REPAIR. REPAIRED PER ERA 332946-14AD, REV F.Apr 13, 1999 · N2820W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990824Skin · crackedWHILE ACCOMPLISHING HFEC INSP PER SI 4-74176-12AD, REV F, A CRACK INDICATION WAS FOUND BETWEEN BS 681 AND BS 700; AT S4R. REPAIRED PER ERA 332945-14AD, REV A.Apr 13, 1999 · N2820W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E990800Wire · failedA/C ESCAPE PATH LIGHTING FOUND INOP IN SEVERAL LOCATIONS. REPAIRED AND REPLACED GROUND WIRING AT THE FWD BATTERY PACK MULTI SPLICE AREA. ALL CK'S OK.Apr 12, 1999 · N282WA · Boeing 727247 · Light System WiringSDR 99FDEA00140Beam · crackedLT FWD ENTRY DOOR GATE BEAM CRACKED AT LOWER FORWARD STOP FITTING. ** S/D ** STOP DRILLED LT FWD ENTRY DOOR GATE BEAM AT LWR FWD STOP FITTING AND INSTALLED DOUBLER IAW FEDEX SR 27-52-015 STEP 1 THRU 10.Apr 12, 1999 · N234FE · Boeing 727247 · Passenger/Crew DoorsSDR DL72W990787Fuel Pump · malfunctionedENGINE NR 1 FLAME OUT ON TAKEOFF ROLL. REPLACING NR 1 ENGINE FUEL AND FUEL PUMP IN PROGRESS.Apr 11, 1999 · N291WA · Boeing 727247 · Engine Fuel PumpSDR DL72E990783Battery · dischargedLT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATT M955. OPS CHKS GOOD.Apr 10, 1999 · N283WA · Boeing 727247 · Emergency LightingSDR DL72W990754Skin · corrodedON HUSH-KIT MOD OPN 57118, LOWER SKIN LAP JOINT INSPECTION FOUND CORROSION ON FUSELAGE SKIN BETWEEN BONDED METAL SKIN LAYERS AT STATION 259.5R TO 360R. REPLACED SKIN SECTION WITH A/C SKIN SECTION FROM MANUFACTURER.Apr 7, 1999 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR 99FDEA00137Splice · corrodedUPON REMOVAL OF STR ON NR 303 FOUND CORROSION ON STR SPLICE STR 26L, BS 480. *S/D* REMOVED AND REPLACED STR SPLICE PER IAW FEDEX SRM 51-30-2.Apr 7, 1999 · N234FE · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990756Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 5 CRACKS IN TWO CONSECUTIVE FRAME BAYS. THE SKIN LAP WAS CUT OUT ALONG THE ENTIApr 6, 1999 · N2817W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990755Skin · 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 INSPECTION CONFIRMED 41 CRACKS ALONG THE PANEL. THE LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGTH AND REPAIRApr 6, 1999 · N2817W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990753Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 9 CRACKS IN THE PANEL. THE SKIN LAP WAS CUT OUT ALONG THE LENGTH OF THE PANEL ANApr 6, 1999 · N2817W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990752Skin · corrodedTHE FUSELAGE SKIN PANEL BETWEEN FS 259.5 AND 360 AND BETWEEN STRINGER 19R AND 24R WAS FOUND WITH SEVERAL AREAS OF CORROSION. THE PANEL WAS REMOVED AND A NEW BOEING SKIN PANEL INSTALLED PER ER/A 366991-14.Apr 6, 1999 · N2815W · Boeing 727247 · Fuselage Main, Plate/SkinSDR 99FDEA00135Stringer · corrodedCORROSION (C53-111-01,2) ON STRINGER 26L, BS 494. *S/D* REMOVED AND REPLACED STR 26L, BS 482-496 IAW FEDEX SRM 53-10-3 FIG 1.Apr 5, 1999 · N234FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR 99FDEA00134Stringer · corrodedCORROSION (C53-111-01, 3) ON STR 25R AT BS 1176. *S/D* REMOVED AND REPLACED 25R FROM BS 1158 TO 1183 IAW FEDEX SRM 53-10-3 FIG 1.Apr 5, 1999 · N234FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR 99FDEA00133Beam · corrodedCORROSION (C53-221-01) ON FWD EDGE OF 25 G-BEAM BS 264, LBL 4 TO LBL 7, WL 208. *S/D* REMOVED AND REPLACED 25 G-BEAM, BS 264, LBL 8 TO RBL 21, WL 208 IAW FEDEX EA NR 7-5310-45212.Apr 5, 1999 · N234FE · Boeing 727247 · Fuselage Main, Plate/SkinSDR 99FDEA00132Stringer · corrodedCORROSION (C53-111-01, 3) ON STR 27R AT BS 990. *S/D* REMOVED AND REPLACED STR 27R PER FEDEX EA 7-5310-45210A.Apr 5, 1999 · N234FE · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72E990733Battery Pack · dischargedEMERGENCY EXIT LIGHT SIGN OVER RT OVERWING EXIT INOP ON TEST. REPLACED RACK AND BATTERY PACK, OPN CKS OK.Apr 3, 1999 · N831WA · Boeing 727247 · Emergency LightingSDR DL72E990723Battery · dischargedCENTER LT OVERWING EMERG LIGHT INOP. REPLACED BATTERY AT M954, OPS CHKS GOOD.Apr 1, 1999 · N2829W · Boeing 727247 · Emergency LightingSDR DL72W990710Web · crackedA TYPICAL CRACK WAS FOUND IN THE INBOARD VERTICAL WEB OF THE RT AFT ENTRY DOOR TORQUE BOX AT FS 1271. THE CRACK WAS REPAIRED PER BAC S/B 727-53-0129 AND DOCUMENTED PER ER/A 367089-14AD.Mar 31, 1999 · N2819W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990694Rib · crackedUPPER CHORD ANGLE OF LT WING RIB AT WS 171.5 WAS FOUND WITH TWO CRACKS. THE CRACKS ARE LOCATED AT S16 AND S17. REPAIRED PER ERA 332958-14, REV A.Mar 30, 1999 · N2820W · Boeing 727247 · Wing, Rib/BulkheadSDR DL72W990693Frame · wornBS 1148 FRAME WAS FOUND WORN ON THE I/B HORIZ FLANGE RADIUS AT S22L. THE WEAR WAS CAUSED BY CONTACT WITH A HYD LINE. REPAIRED PER ERA 332949-14, REV A.Mar 30, 1999 · N2820W · Boeing 727247 · Fuselage Main, FrameSDR DL72W990691Skin · dentedA GOUGE WAS FOUND IN THE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT BS 990. THE DAMAGE IS LOCATED ABOVE S24R. THE SKIN, DOUBLER AND TRIPLER WERE DAMAGE, BUT NOT THE BEAR STRAP. REPAIRED PER ERA 332963-14, REV A.Mar 30, 1999 · N2820W · Boeing 727247 · Fuselage Main, Plate/Skin
Back to Boeing 727-247