Boeing 727-225

Service difficulty reports · 4,226

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 = '727225'
  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 DHL2001742528Web · corrodedDURING C-CHECK, AFT CABIN HAS CORROSION AT LWR WEB AT STA 1177 AND RBL 17. ROUTED OUT CORROSION AT LWR WEB AT STA 1172 AND RBL 17 AS PER B-727 SRM 51-40-2. INSTALLED DOUBLER REPAIR IAW B-727 SRM 51-40-2 FIGURE 1.Oct 10, 2001 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2001742521Web · corrodedAT C-CHECK, AFT CABIN HAS CORROSION AT LWR WEB STA 1177 & RBL 17.Oct 10, 2001 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2001742517Support · crackedAT C-CHECK, AFT BAG BIN, SIDE WALL TO FLOOR, SUB FLOOR ABOVE 55R 27L IS CRACKED AT STA 1148, MARKED.Oct 10, 2001 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2001742543Seat Track · brokenAT C-CHECK, MAIN CABIN SEAT TRACK AT LBL 48 SHOW BROKEN LUGS AT BS 670, 710, BS 730. REMOVED CABIN SEAT TRACK LBL 48 FROM BS 620 TO BS 740 AS PER B-727 SRM 51-30-2. INSTALLED NEW SEAT TRACK FROM BS 620 TO 740 AS PER B-727 SRM 53-10-5 FIGURE 7.Oct 9, 2001 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2001742540Skin · corrodedAT C-CHECK, LWR FUSE HAS BULGING SKIN AT BS 1050 & STR R28. CUT OUT DAMAGED STR 35. REMOVED PREVIOUS DOUBLER REPAIR AT STR 28R AND STA 1050. REMOVED CORROSION ON INNER SKIN AT STA 1050, STR 28R, FOUND TO BE OUT OF LIMITS. CUT OUT CORRODED AREA AT LWR SKIN Oct 9, 2001 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2001742531Skin · bulgedAT C-CHECK, LOWER FUSELAGE HAS BULGING SKIN AT BS 1050 & STRINGER R28.Oct 9, 2001 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2001742522Skin · corrodedDURING C-CHECK, LOWER FUSELAGE HAS BULGING SKIN AT BS 1050 AND STRINGER R28. CUT OUT DAMAGED STRINGER 35 IAW B-727 SRM 53-10-3. REMOVED CORROSION ON INNER SKIN AT STATION 1050, STRINGER 28R, FOUND TO BE OUT OF LIMITS AS PER B-727 SRM 51-10-6. CUT OUT CORROOct 9, 2001 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2001742520Skin · bulgedAT C-CHECK, LOWER FUSELAGE HAS BULGING SKIN AT BS 1050 AND STRINGER L28.Oct 9, 2001 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2001742542Seat Track · brokenAT C-CHECK, SEAT TRACK HAS BROKEN LUGS AT BS 720C LBL 48. REMOVED AND REPLACED SEAT TRACK FROM BS 620 TO BS 740 LBL 48 AS PER B-727 SRM 51-30-2 AND 53-10-5 FIGURE 7.Oct 8, 2001 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2001742516Skin · corrodedAT C-CHECK, NR 2 ENG, FWD LT COWL FWD LOWER CORNER, SKIN EDGE AND INTERIOR ANGLE DOUBLER IS CORRODED.Oct 8, 2001 · N742DH · Boeing 727225 · Engine Cowling SystemSDR DHL2001742515Doubler · damagedAT C-CHECK, LT WING ROOT T/E (FALSE SPAR) LWR PANEL ABOVE GEAR, OLD REPAIR IS COMING OFF AT TOP SIDE.Oct 5, 2001 · N742DH · Boeing 727225 · Wing, Plate/SkinSDR DHL2001742511Floor Panel · corrodedAT C-CHECK- FWD LAV FLOOR PANEL IS CORRODED, MARKED.Oct 5, 2001 · N742DH · Boeing 727225 · Fuselage Floor PanelSDR DHL2001742510Skin · erodedAT C-CHECK, VERTICAL STAB L/E PANEL NR 9502 AT LOWER SECTION HF ANTENNA IS ERODED.Oct 5, 2001 · N742DH · Boeing 727225 · Vertical Stabilizer, Plate/SkinSDR DHL2001742505Plate · crackedAT C CHECK- AFT CABIN HAS SHEAR WEB PLATE HAS CRACK AROUND BOLT, AND BOLT IMPROPERLY INSTALLED BS 1176 RBL 30. REMOVED FASTENER AND CUT OUT DAMAGE AREA FOR CRACK AT AFT CABIN STA 1187 RBL 30 CUT OUT SIZE .75 AND .5 INCH AS PER B727 SRM 51-40-2. REMOVED AND ROct 4, 2001 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2001742506Web · corrodedAT C-CHECK, AFT CABIN HAS SHEAR WEB PLATE WITH CORROSION IN TWO PLACES BS 1166 & RBL 15. CUT OUT CORNER AREA OF SHEAR WEB AT BS 1148 & 1166 RBL 15 INCHES. INSTALLED DOUBLER REPAIR AT BS 1148 AND 1166 AS PER B727 SRM 51-40-2 FIG 1.Oct 4, 2001 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2001742530Plate · crackedDURING C-CHECK, AFT CABIN HAS SHEAR VIEW PLATE HAS CRACK AROUND BOLT, AND BOLT IMPROPERLY INSTALLED BS 1176 RBL 30. REMOVED FASTENER AND CUT OUT DAMAGE AREA FOR CRACK AT AFT CABIN STA 1176 RBL 30. REMOVED AND REPLACED DOUBLER AT CABIN BS 1176 RBL 30.Oct 4, 2001 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2001742529Web · corrodedDURING C-CHECK, AFT CABIN HAS SHEAR WEB PLATE WITH CORROSION IN TWO PLACES BS 1166 AND 1148 RBL 15. CUT OUT CORRODED AREA OF SHEAR WEB AT BS 1148 AND 1166 RBL 15. INSTALLED DOUBLER REPAIR AT BS 1148 AND 1166 AS PER B-727 SRM 51-40-2 FIGURE 1.Oct 4, 2001 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2001742514Skin · damagedAT C-CHECK, RT ELEVATOR TOP SURFACE I/B (CLOSE TO TAB I/B AREA) SHOW A 2 X 4 INCHES. TEMPORARY REPAIR.Oct 4, 2001 · N742DH · Boeing 727225 · Elevator, Plate/SkinSDR DHL2001742513Spar · crackedAT C-CHECK, CRACK IN FULSE SPAR WEB NR 4 FLAP TRACK, MKD.Oct 4, 2001 · N742DH · Boeing 727225 · Wing SparSDR DHL2001742512Skin · damagedAT C-CHECK, RIGHT WING INBOARD FLAP AFT LOWER SKIN HAS PITTED AREA IN TWO PLACES INBOARD AND MID SECTION OF FLAP.Oct 4, 2001 · N742DH · Boeing 727225 · Trailing Edge FlapsSDR DHL2001742509Skin · damagedAT C-CHECK, TAIL CONE UPPER SIDE RT AFT AREA. SKIN HAS THREE SMALL HOLES. (RED MARKED)Oct 4, 2001 · N742DH · Boeing 727225 · Aerodynamic FairingsSDR DHL2001742508Spar · corrodedAT C-CHECK- RT WING REAR AUX SPAR AT WS 294. FOUND CORROSION TO FWD/UPPER ANGLE.Oct 4, 2001 · N742DH · Boeing 727225 · Wing SparSDR DHL2001742507Spar · corrodedAT C-CHECK, LIGHT CORROSION OF FWD SIDE OF FULSE SPAR ABOVE O/B FLAP POSITION TRANSMITTER MKD.Oct 4, 2001 · N742DH · Boeing 727225 · Wing SparSDR DHL2001742545Attach Fitting · crackedAT C-CHECK, LT WING L/E NR 4 SLAT ACTUATOR FRONT SPAR ATTACH I/B FITTING CRACKED 2 PLACES. REMOVED AND INSTALLED NEW I/B FITTING AT LT WING NR 4 SLAT ACTUATOR SUPPORT.Oct 3, 2001 · N742DH · Boeing 727225 · Leading Edge Slat ActuatorSDR DHL2001742525Angle · crackedAT C-CHECK, FUSELAGE LEFT WING T/E AREA, UPPER FIXED PANEL TOP OF I/B FLAP O/B JACKSCREW HAS SUPPORT ANGLE CRACKED ALONG RIVET.Oct 3, 2001 · N742DH · Boeing 727225 · Wing, Plate/SkinSDR DHL2001742504Angle · crackedAT C-CHECK, RT WING L/E INTERIOR AT WS 130, FOUND CRACK DAMAGE TO UPPER ANGLE BETWEEN UPPER SKIN AND STA 130 RIB. REMOVED UPPER ANGLE AT RT WING L/E INTERIOR AT WS 130 BETWEEN UPPER SKIN AND STA 130 RIB IAW B727 SRM 51-30-2. INSTALLED UPPER ANGLE AT RT WING Oct 3, 2001 · N742DH · Boeing 727225 · Wing Miscellaneous StructureSDR DHL2001742503Channel · crackedAT C-CHECK, LEFT WING T/E AREA, UPPER FIXED PANEL TOP OF I/B FLAP O/B JACKSREW HAS SUPPORT ANGLE CRACKED ALONG RIVET. REMOVED AND REPLACED U-CHANEL SUPPORT ON LEFT WING T/E FIXED PANEL TOP OF I/B FLAP O/B JACKSCREW, IAW B727-SRM 51-10-1.Oct 3, 2001 · N742DH · Boeing 727225 · Wing Miscellaneous StructureSDR DHL2001742526Floorbeam · crackedDURING C-CHECK, CABIN FLOORBEAM HAS CRACKED WEB BS 825.95 LEFT O/B LBL 60, CRACK STARTS FROM ABOVE GUSSET FASTENER HOLE. REMOVED WEB AT BS 825.95 LBL 60 AS PER B-727 SRM 51-30-2. FABRICATE NEW WEB AS PER B-727 SRM 53-10-2 FIGURE 7. INSTALLED WEB AS PER B-727 Oct 3, 2001 · N742DH · Boeing 727225 · Fuselage Main, Floor BeamSDR DHL2001742500Bracket · crackedAT C-CHECK, LT MLG DEBOOST CYLS ATTACH BRACKET CRACKED AT CENTER OF BACK PANEL. REMOVED LT MLG DEBOOST CYLS ATTACH BRACKET AS PER B727 MM 32-41-21 FOR S/M ACCESS. FABRICATED NEW BRACKET SUPPORT PANEL FOR LML GEAR DEBOOST CYLS AS PER B727 SRM 53-10-2 FIG 5. IOct 3, 2001 · N742DH · Boeing 727225 · Main Landing Gear Attach SectionSDR DHL2001742502Attach Angle · crackedAT C-CHECK, RT FWD FUSE FAIRING ATTACH ANGLE CRACKED STA 720 RBL 6. STOP DRILLED CRACK AT RT FWD FUS FAIRING ATTACH ANGLE STA 720 RBL 6 AS PER B727 SRM 51-10-1. ACCOMPLISHED NDT INSPECTED AROUND STOP HOLE, NO CRACK NOTED. INSTALLED DOUBLER REPAIR AT RT FWD Oct 2, 2001 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL2001742501Skin · crackedAT C-CHECK-FUSELAGE, AFT AIRSTAIRS, LT SIDE AT TOP CUTOUT AREA FOR AIRSTAIRS FUSELAGE SKIN HAS CRACK AT CORNER OF CUTOUT BS 1222. ROUTED OUT CRACK AREA OF FUSELAGE AFT 1222 AS PER B727 SRM 51-10-01. PERFORMED HFEC IAW B727 NDT MANUAL 51-00-00, PART 6 FIG 4. Oct 2, 2001 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR DHL2001742541Angle · crackedAT C-CHECK, LEFT WING HAS A CRACK AT LEFT EDGE FRONT SPAR VERTICAL ANGLE LOWER END AT WBL 92.8 MARKED. CUT OFF LOWER SECTION OF ANGLE AT WBL 92.8 LEFT WING L/E AS PER B-727 SRM 51-40-4 FIGURE 2. FABRICATE NEW ANGLE AS PER B-727 SRM 51-40-4. ALODINED AND PRIOct 1, 2001 · N742DH · Boeing 727225 · Wing Miscellaneous StructureSDR DHL2001742544Angle · crackedAT C-CHECK, LT WING HAS A CRACK AT LEADING EDGE FRONT VERTICAL ANGLE LOWER END AT WBL 92.8.Oct 1, 2001 · N742DH · Boeing 727225 · Wing Miscellaneous StructureSDR DHL2001742013Duct · dislodgedNR 3 ENG GROUND FAULT LIGHT ILLUMINATED. FOUND GENERATOR COOLING DUCT DISLODGED AND RESTING ON FIRE LOOP. RESECURED COOLING DUCT, CLEANED AND RE SEATED FIRE LOOP C/P. OPS NORMAL IAW MM CH 26-11-0.Sep 24, 2001 · N742DH · Boeing 727225 · Engine Cooling SystemSDR MYW2001F00000Tube · damagedAFTER TAKEOFF AT APPROXIMATELY 1500 FT. THE NR 1 ENGINE FIRE WARNING (BOTTLE AND BELL) ACTIVATED. AOM EMERGENCY PROCEDURES PER 2-C-2 COMPLIED WITH. DUMPED APPROXIMATELY 12000 POUNDS OF FUEL PER AOM PROCEDURE 2-A-B-1. RETURNED TO AIRPORT. PREPARED FOR 2 ENGISep 24, 2001 · N803MA · Boeing 727225 · Engine (Turbine/Turboprop)SDR 2001F00588Fire Loop · failedWHEEL WELL FIRE WARNING LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. COMPLIED WITH EMERGENCY CHECKLIST AND EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO DAYTON AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE FIRE DETECTOR BOX AND BOTH MAIN WHEEL WELL FIRE Sep 21, 2001 · N8878Z · Boeing 727225 · Fire DetectionSDR 2001F00587Detector · faultyWHEEL WELL FIRE WARNING LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. COMPLIED WITH EMERGENCY CHECKLIST AND EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO DAYTON AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE FIRE DETECTOR BOX AND BOTH MAIN WHEEL WELL FIRE Sep 21, 2001 · N8878Z · Boeing 727225 · Fire DetectionSDR EISA20010122Light · defectiveEMERGENCY EXIT LIGHT AT L1 DOOR VERY DIM. REMOVED AND REPLACED EXIT LIGHT IAW MM 33, OPS CHECKS NORMAL.Sep 17, 2001 · N354PA · Boeing 727225 · Emergency LightingSDR 01FDEA00843Switch · failedAFT T/O GEAR WAS RETRACT NORMAL WHEN HANDLE IN OFF POS. REMOVED AND REPLACED RIGHT AND LEFT NOSE LAND GEAR DOOR SWITCH PER MM 32-33-00-5.Sep 14, 2001 · N469FE · Boeing 727225 · Landing Gear Position and WarningSDR GAIA01308OPLight · inoperativeDURING MAINTENANCE AT TOL, IT WAS DISCOVERED THAT THE L1 DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 8, 2001 · N936PG · Boeing 727225 · Emergency LightingSDR GAIA01307OPContactor · dirtyDURING MAINTENANCE AT TOL, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. INSPECTION FOUND THE EMERGENCY EXIT LIGHT CONNECTIONS DIRTY. THE CONNECTORS WERE CLEANED AND THE LIGHT WAS REINSTALLED. THE SYSTEM OPERATIONALLY CHECKED GOODSep 8, 2001 · N936PG · Boeing 727225 · Emergency LightingSDR DHL2001748001EngineDuring drop in-to keep from exceeding E.G.T. had to reduce thrust, on #1 engine during take-off. Unable to maintain take-off thrust.1) Checked #1 engine E.G.T. indicator and total resistance, all checked good I.A.W. B-727 M.M. 77-21-00.2) Checked #1 E.P.R. , nSep 3, 2001 · N748DH · Boeing 727225 · Engine Temperature Indicating SystemSDR 2001748001EngineDuring drop in-to keep from exceeding E.G.T. had to reduce thrust, on #1 engine during take-off. Unable to maintain take-off thrust.1) Checked #1 engine E.G.T. indicator and total resistance, all checked good I.A.W. B-727 M.M. 77-21-00.2) Checked #1 E.P.R. , nSep 3, 2001 · N748DH · Boeing 727225 · Engine Temperature Indicating SystemSDR 01FDEA00794Warning Light · illuminatedUSING NR 2 ENG RT BLEED TO PROVIDE AIR TO RT PACK, LWR AFT BODY OVERHEAD LIGHT ILLUM. RED TABS FOLLOWED.Aug 31, 2001 · N466FE · Boeing 727225 · Overheat DetectionSDR DHL2001748005Engine · malfunctionedDURING TEST FLIGHT DISCREPANCY----------- NR 1 ENGINE GROUND FAULT INDICATOR ILLUMINATED.Aug 30, 2001 · N748DH · Boeing 727225 · Smoke DetectionSDR DHL2001743012Indicator · malfunctioned1) REJECTED T/O DUE TO 30KT DISCREPENCY BETWEEN CAPTAIN & F/O AIRSPEED INDICATOR. REJECTED WHEN: F/O AIRSPEED INDICATED 110KTS,CAPTAINS INDICATED 80KTS. 2) FOUND INSECT IN CAPTAINS AIRSPEED PITOT TUBE. REMOVED BUG AND PERFORMED PITOT STATIC TEST PER MMAug 30, 2001 · N743DH · Boeing 727225 · Airspeed/Mach IndicatorSDR GAIA01302OPConnector · dirtyDURING MAINTENANCE AT TOL, IT WAS DISCOVERED THAT THE COCKPIT EMERGENCY EXIT LIGHT WAS INOPERATIVE. INSPECTION FOUND THE EMERGENCY EXIT LIGHT CONNECTIONS DIRTY THE CONNECTORS WERE CLEANED AND THE LIGHT WAS REINSTALLED. THE SYSTEM OPERATIONALLY CHECKED GOOD.Aug 28, 2001 · N936PG · Boeing 727225 · Emergency LightingSDR DHL2001748004Fuel Cell · leakingDURING "DROP IN INSPECTION" DISCREPANCY---------- SUSPECT FUEL LEAK IN THE AREA OF THE RIGHT WING REAR SPAR JUST OUTBD. OF THE RIGHT MAIN GEAR.Aug 27, 2001 · N748DH · Boeing 727225 · Fuel StorageSDR DHL2001748003Annunciator · false activationON TEST FLIGHT DISCREPANCY------- WINDSHEAR ANNUNCIATION INTERMITTENT OPERATION ROUTINE FAIL IN FLIGHT.Aug 26, 2001 · N748DH · Boeing 727225 · Instrument PanelSDR DHL2001748002Switch · malfunctionedDURING TEST FLIGHT (DISCREPANCY)-------- MACH OVERSPEED ACTUATED AT .84 MACH AT 278 KNOTS AT 37000.1) ONT/S FOUND 300 FEET PER MINUTE LEAK ON AUX STATIC SYS, OUT OF LIMITS PER B-727 M.M. 34-11-00.2)FOUND CRACKED TEE-FITTING ON AUX STATIC LINE AT E AND E COMPARAug 26, 2001 · N748DH · Boeing 727225 · Instrument Panel
Back to Boeing 727-225