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 20000502AP004Seat Track · gougedFOUND CABIN SEAT TRACK WORN, GOUGED AND CORRODED STATION 950B TO STATION 990, LBL 24. REPLACED SEAT TRACK PER SRM 53-10-5 FIG 2. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 20000502AP003Stringer · crackedFOUND STRINGER CRACKED IN COMPARTMENT ABOVE FIN STATION 133.8, STRINGER IS FIFTH UP FROM BOTTOM OF COMPARTMENT. INSTALLED REPAIR PER SRM 55-30-1 FIG 1. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Vertical Stabilizer, Spar/RibSDR 20000502AP002Skin · crackedFOUND NR 2 S DUCT ANTI-ICE INNER SKIN CRACKED AT LOWER CORNER. LOCATED IN FORTH COMPARTMENT DOWN FROM V STABILIZER ACCESS PLATE. STOP DRILLED DRILLED CRACK AND INSTALLED REPAIR PER SRM 51-40-2 PAGE 6. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Elevator, Plate/SkinSDR 20000502AP001Rib · crackedFOUND 1 INCH CRACK IN RIB ADJACENT TO CENTER FOREFLAP TRACK GUIDE, LEFT INBOARD MIDFLAP. REMOVED AND REPLACED FLAP ASSY WITH SERVICEABLE UNIT. (M)Oct 27, 1999 · N887MA · Boeing 727225 · Wing, Rib/BulkheadSDR EISA99228Floorbeam · corrodedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON LOWER SURFACE OF MAIN CABIN FLOORBEAM AT BS 950C LBL 25. REMOVED CORROSION AND MATERIAL LOSS OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED AREA. FABRICATED REPAIR ANGLES AND FILLER PER SRM 53-10Oct 27, 1999 · N353PA · Boeing 727225 · Fuselage Main, Floor BeamSDR EISA99227Stringer · corrodedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED CORROSION ON STR 24L AT BS 950. REMOVED CORROSION AND MATERIAL LOSS OF LIMITS PER SRM 53-10-1. FABRICATED AND INSTALLED STRINGER REPAIR PER SRM 53-10-3 AND SRM 51-30-2. TT: 65,345:17 HOURS. TC: 43,81Oct 27, 1999 · N353PA · Boeing 727225 · Fuselage Main, Longeron/StringerSDR EISA99212Mechanism · out of adjustL-1 DOOR WARNING LIGHT ILLUMINATED ON CLIMB-OUT, DOOR NOT IN CLOSED POSITION. AIRCRAFT WOULD NOT PRESSURIZE. RIGGED L-1 DOOR OPERATION CHECK, PRESSURE CHECK GOOD. (M)Oct 27, 1999 · N352PA · Boeing 727225 · Passenger/Crew DoorsSDR USAA109906Smoke Detector · failedFLT 6141 - BOS-LGA - FOUND ON L/S, AFT LAV SMOKE DETECTOR TEST WILL NOT SHUT OFF. REPLACED AFT LAV SMOKE DETECTOR. (M)Oct 24, 1999 · N918TS · Boeing 727225 · Smoke DetectionSDR EISA99244Floorbeam · corrodedROUTINE C-CHECK INSPECTION CARD REVEALED CORROSION ON MAIN CABIN FLOORBEAM T-CAP AT BS 400 RBL 10. REMOVED CORROSION PER SRM 51-10-6, FABRICATED AND INSTALLED REPAIR PER SRM'S 51-10-8 AND 51-30-2. TT: 65,345:17 HOURS. TC: 43,816. (X)Oct 21, 1999 · N353PA · Boeing 727225 · Fuselage Main, Floor BeamSDR EISA99231Angle · corrodedACCOMPLISHMENT OF ROUTINE C-CHECK INSPECTION WORK CARD REVEALED CORROSION ON FLOORBEAM ANGLE IN AFT BAGGAGE COMPARTMENT AT FS 1148, LBL 8 TO RBL 8. REMOVED CORROSION IAW SRM 51-10-6 OUT OF LIMITS. REMOVED DAMAGED ANGLE AND FABRICATED NEW ANGLE IAW SRM 53-10-Oct 21, 1999 · N353PA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 99ZZZX4356Skin · misrepairedPREVIOUS DOUBLER REPAIR AT FORWARD RIGHT JACK PAD AREA, STR 19R TO STR 24R STA 333 TO STA 360 DO NOT HAVE PROVISIONS FOR JACK PAD (HOLES). FOUND DURING SCHEDULED C-MAINTENANCE CHECK.Oct 21, 1999 · N887MA · Boeing 727225 · Fuselage Main, Plate/SkinSDR EISA99229Floorbeam · corrodedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD FOUND CORROSION ON FLOORBEAM UPPER T-CAP AT BS 480, BL ZERO AND RBL 120. REMOVED CORROSION PER SRM 51-10-6, MATERIAL LOSS OUT OF LIMITS PER SRM 53-10-1, CUT OUT DAMAGED AREA PER SRM 53-10-8. FABRICATED AND INSTALLEOct 19, 1999 · N353PA · Boeing 727225 · Fuselage Main, Floor BeamSDR EISA99238Floorbeam · corrodedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD FOUND CORROSION ON FLOORBEAM T-CAP AT FS 1050 LBL 20 MAIN CABIN FLOOR STRUCTURE. REMOVED CORROSION AND MATERIAL LOSS OUT OF LIMITS. SRM 53-10-1, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 AND SRM 51-30-2. TT:Oct 18, 1999 · N353PA · Boeing 727225 · Fuselage Main, Floor BeamSDR EISA99239Seat Track · corrodedDURING THE ACCOMPLISHMENT OF A ROUTINE C-CHECK WORK CARD, FOUND CORROSION ON MAIN CABIN SEAT TRACK AT BS 848 TO BS 990 RBL 20. CORROSION REMOVED PER SRM 51-10-6 AND MATERIAL LOSS OUT OF LIMITS. FABRICATED NEW SECTION OF TRACK PER SAMPLE. REPLACED TRACK SECTOct 13, 1999 · N353PA · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 99FDEA00421Switch · lack of lubeCONFIGURED AC WITH GEAR AND 15 DEG FLAPS DURING APPROACH. GEAR EXTENSION NORMAL, BUT DOOR LIGHT AND LEFT GEAR DOOR LIGHT REMAINED ILLUMINATED. LUBED DOOR WARNING SWITCH, GEAR DOOR WARNING SYS CK GOOD PER MM 32-62-011.Oct 13, 1999 · N463FE · Boeing 727225 · Landing Gear Position and WarningSDR 99FDEA00420Switch · dirtyON T/O LANDING GEAR RED DOOR LIGHT AND AMBER NOSE GEAR LIGHT REMAIN ON WITH GEAR UP. COMPLIED WITH RED TABS AND LIGHT REMAIN ON. CLEANED DOOR AND GEAR SWITCHES, CHECKED FOR ADJUSTMENT AND ALL INDICATIONS NORMAL.Oct 11, 1999 · N467FE · Boeing 727225 · Landing Gear Position and WarningSDR EISA99177Fire Warning · failedFIRE BELL DOES NOT SOUND IN EITHER ENGINE FIRE OR APU FIRE TEST. REMOVED AND REPLACED FIRE AND OVERHEAT ACCESSORY PANEL. NO HELP. REMOVED AND REPLACED AURAL WARNING BOX FIRE TEST IAW MM 26-14-11. (M)Oct 8, 1999 · N352PA · Boeing 727225 · Fire DetectionSDR DHL9974219CFairing · dentedAT C-CHECK, DENT AT WING TO FUSELAGE FAIRING AT APPROX STA 720E ATR 26RT. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 6.5 BY 2.5, N/R 5461.Oct 7, 1999 · N742DH · Boeing 727225 · Aerodynamic FairingsSDR 99ZZZX4131Intercostal · crackedDURING CONFORMITY INSPECTION, AN INTERCOSTAL WAS FOUND CRACKED AT STA 360, S16L.Oct 7, 1999 · N8840E · Boeing 727225 · Fuselage Miscellaneous StructureSDR SCNA99124Light · inopDURING A LINE MAINTENANCE CHECK, THE FLOOR EMERGENCY TRACK LIGHTING AT ROW 28 WAS FOUND INOPERATIVE. REPAIRED WIRING AT TRACK AT ROW 28. OPERATIONALLY CHECKS GOOD.Oct 5, 1999 · N283SC · Boeing 727225 · Emergency LightingSDR DHL9974218CBracket · crackedAT C-CHECK, NR 4 TRAILING EDGE FLAP INBD BEARING BRACKET TO BULL NOSE CRACKED. REMOVED AND REPLACED NR 4 LE FLAP PER MM 27-81-4. N/R 2366.Oct 5, 1999 · N742DH · Boeing 727225 · Leading Edge DevicesSDR SCNA99125Light · inopDURING A LINE MAINTENANCE CHECKTHE CENTER SECTION FLOOR EMERGENCY TRACK WAS FOUND INOPERATIVE. REMOVED AND REPLACED ROW 20 EMERGENCY PATHWAY LIGHT SOCKET. OPERATIONALLY CHECKS GOOD.Oct 4, 1999 · N282SC · Boeing 727225 · Emergency LightingSDR DHL9974223CCowl · misrepairedAT C-CHECK, NR 1 ENGINE NOSE COWL HAS IMPROPER REPAIR TO SKIN EDGE AT FRAME APPROX NAC STA99. REMOVED OLD REPAIR. INSTALLED DOUBLER PER SRM 51-40-2, 4 BY 7.5, N/R 6680.Oct 4, 1999 · N742DH · Boeing 727225 · Engine Cowling SystemSDR DHL9974222CCowl · puncturedAT C CHECK, NR 1 NOSE COWL HAS SMALL PUNCTURES IN SKIN AT FRAME APPROX NAC STA 92. CUT OUT DAMAGED AREA. INSTALLED DOUBLER 4 BY 8 PER SRM 54-30-3. N/R 6679.Oct 4, 1999 · N742DH · Boeing 727225 · Engine Cowling SystemSDR USAA109902Smoke Detector · failedRIGHT AFT LAV SMOKE DETECTOR WON'T TEST. REPLACED SMOKE DETECTOR, CHECKS OK PER MM 26-10-0. (M)Oct 2, 1999 · N922TS · Boeing 727225 · Smoke DetectionSDR DHL9974210CBracket · crackedAT C-CHECK, 4 FLAP TRACK FWD FIXED FAIRING BRACKET CRACKED AT FWD OUTBD CORNER. REPLACED FIXED FAIRING BRACKET PER SRM 51-40-2, 14 BY 14, N/R 7307.Sep 30, 1999 · N742DH · Boeing 727225 · Trailing Edge FlapsSDR 99ZZZX3947Angle · crackedLOWER TRAILING EDGE PANEL BELOW NR 8 SPOILER ACTUATOR (FALSE SPAR) LOWER CHORD ANGLE CRACKED. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED POSSIBLE CAUSE AS WING FLEXING LOADS.Sep 29, 1999 · N887MA · Boeing 727225 · Wing Miscellaneous StructureSDR 99ZZZX3946Beam · crackedRIGHT WING TRAILING EDGE J-BEAM CRACKED (.3750 INCH) ABOVE NR 8 SPOILER ACTUATOR. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DESIGN FLAW OR WING FLEXING LOADS.Sep 29, 1999 · N887MA · Boeing 727225 · Wing Miscellaneous StructureSDR 99ZZZX3945Floorbeam · corrodedCABIN FLOORBEAM STA 344 RBL 24 TO WALL HAS CORROSION. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER STATED POSSIBLE CAUSE AS LIQUID SPILLS OR DISSIMILAR METAL.Sep 29, 1999 · N887MA · Boeing 727225 · Fuselage Miscellaneous StructureSDR 99ZZZX3944Floorbeam · corrodedCABIN FLOORBEAM AT STA 1130 RBL 36 HAS CORROSION AROUND SCREW HOLES. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER STATED POSSIBLE CAUSE AS LIQUID SPILLS OR DISSIMILAR METAL.Sep 29, 1999 · N887MA · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL9974209CMixer · crackedAT C-CHECK, NR 2 ENGINE EXHAUST MIXER HAS BRACKET BROKEN AT 6 O'CLOCK. WELDED CRACKED PER MM 72-55-02, N/R 6672.Sep 28, 1999 · N742DH · Boeing 727225 · Engine Noise SuppressorSDR DHL9974226CRub Block · corrodedAT C-CHECK, RT STABILIZER RUB BLOCK TRACK HAS CORROSION BULGE. REMOVED RACK. INSTALLED NEW TRACK PER SRM 51-30-2, N/R 4298.Sep 27, 1999 · N742DH · Boeing 727225 · Horizontal Stabilizer StructureSDR DHL9974208CRub Block · cororodedAT C CHECK, LEFT STABILIZER RUB BLOCK TRACK HAS CORROSION BULGE. REMOVED AND INSTALLED NEW TRACK PER SRM 51-30-2, N/R 4297.Sep 27, 1999 · N742DH · Boeing 727225 · Horizontal Stabilizer StructureSDR DHL9974207CBracket · crackedAT C-CHECK, LT WING OUTBD FLAP COVE PANEL OUTBD ROD SUPPORT BRACKET CRACKED BELOW NR 2 FLIGHT SPOILER. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-30-2, N/R 1074.Sep 27, 1999 · N742DH · Boeing 727225 · Trailing Edge FlapsSDR DHL9974217CCowl · crackedAT C CHECK, NR 3 ENG NOSE COWL AFT WEB CRACKED OUT. INSTALLED WEB REPAIR PER SRM 51-40-2, 27 BY 6, N/R 6671.Sep 26, 1999 · N742DH · Boeing 727225 · Engine Cowling SystemSDR DHL9974216CCowl · crackedAT C CHECK, NR 1 ENGINE UPPER COWL PANEL REPAIR DOUBLER AT FWD INBD CORNER IS CRACKED. REPLACED DOUBLER AT CORNER PER SRM 54-30-3, 14 BY 6, N/R 6668.Sep 26, 1999 · N742DH · Boeing 727225 · Engine Cowling SystemSDR DHL9974224CFairing · crackedAT C-CHECK, RT WING INBD FLAP INBD TRACK AFT FAIRING CRACKED AT 2 LOCATIONS. REMOVED DOUBLER AT UPPER END AND REPLACED PER SRM 51-30-2, 4 BY 8. WELDED OTHER CRACK, N/R 2333.Sep 25, 1999 · N742DH · Boeing 727225 · Trailing Edge FlapsSDR DHL9974221CAngle · crackedAT C-CHECK, AFT AIRSTAIR RT LOWER TORQUE BOX UNDER STAIR ACTUATOR FITTING, HAS CRACK IN ANGLE ALONG STA 1273 INBD SIDE. REMOVED ANGLE SUPPORT AND INSTALLED NEW SUPPORT PER S/B 53-0129, N/R 4260.Sep 25, 1999 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR DHL9974215CAngle · crackedAT C CHECK, RT WING COVE PANEL SUPPORT ROD INBD ATTACH ANGLE CRACKED UNDER INBD END OF NR 13 SPOILER PANEL. REMOVED AND REPLACED ANGLE PER SRM 51-30-2, N/R 2324.Sep 25, 1999 · N742DH · Boeing 727225 · SpoilersSDR DHL9974213CCowl · crackedAT C-CHECK, NR 1 ENGINE NOSE COWL AFT EDGE OF COWL SKIN IS BENT AND PULLED LOOSE FROM RIVET HEAD AND SKIN FLUSH REPAIR NOT FITTED PROPERLY. REMOVED FLUSH REPAIR, CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 51-30-2 11.5 BY 5, N/R 6641.Sep 25, 1999 · N742DH · Boeing 727225 · Engine Cowling SystemSDR DHL9974211CFrame · damagedAT C CHECK, NR 3 ENGINE LOWER COWL, HORIZONTAL FRAME DAMAGED INBD SIDE 27 AFT FOF FWD EDGE. REMOVED AND REPLACED DAMAGED FRAME PER SRM 1-10-2, N/R 6634.Sep 25, 1999 · N742DH · Boeing 727225 · Engine Cowling SystemSDR DHL9974225CSkin · chaffedAT C-CHECK, CHAFFED MARK ON LE OF RT INBD FOREFLAP AT NR 5 FLAP TRACK. REMOVED OLD REPAIR, INSTALLED FLUSH REPAIR PER SRM 57-50-4, 20.25 BY 9.5, N/R 2318.Sep 24, 1999 · N742DH · Boeing 727225 · Trailing Edge FlapsSDR DHL9974220CAngle · crackedAT C CHECK, LEFT WING L/E CAVITY AT WS 130 RIB ATTACH ANGLE IS CRACKED BEYOND OLD DOUBLER. STOP DRILLED BOTH ENDS OF CRACK ON ANGLE, BEYOND LIMITS. REMOVED AND REPLACED ANGLE PER SRM 51-30-2. N/R 1033.Sep 24, 1999 · N742DH · Boeing 727225 · Wing Miscellaneous StructureSDR DHL9974214CCowl · crackedAT C CHECK, NR 3 ENGINE INLET COWL OUTER SKIN CRACKED AT FASTENER AT 1 O'CLOCK APPROX 6 AFT OF LEADING EDGE. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 54-30-3, 10 BY 2, N/R 6624.Sep 24, 1999 · N742DH · Boeing 727225 · Engine Cowling SystemSDR DHL9974212CSeat Track · wornAT C CHECK, NR 4 SEAT TRACK WORN AT STA 530 . CUT OUT DAMAGED SECTION, INSTALLED NEW SECTION, PER SRM 53-10-5, 20 LONG, N/R 3048.Sep 24, 1999 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9974206CSkin · crackedAT C-CHECK, LT FIXED LEADING EDGE CUT OUT FOR NR 3 SLAT OUTBD TRACK IS CRACKED. CUT OUT DAMAGED AREA. INSTALLED FLUSH REPAIR PER SRM 57-30-4 2 BY 2, N/R 1029.Sep 24, 1999 · N742DH · Boeing 727225 · Wing, Plate/SkinSDR DHL9974204CCowl · damagedAT C CHECK, NR 4 ENGINE INLET COWL OUTER SKIN DAMAGED ALONG TRAILING EDGE AT 4 O' CLOCK. CUT OUT DAMAGED AREA. INSTALLED DOUBLER REPAIR PER SRM 54-30-3, 8.25 BY 4.75, N/R 6625.Sep 24, 1999 · N742DH · Boeing 727225 · Engine Cowling SystemSDR DL72S992166Spar · crackedDURING ACCOMPLISHMENT OF PREVENTATIVE MODIFICATION OF MIDFLAP REAR SPAR ATTACH HOLES PER EO 4-58705-3AD, A FATIGUE CRACK WAS FOUND IN ONE OF THE MOD HOLES IN THE REAR SPAR CHORD. THE HOLE WAS REAMED UP FROM .1875 DIA TO .25 INCH DIA TO REMOVE CRACK INDISep 23, 1999 · N8873Z · Boeing 727225 · Trailing Edge FlapsSDR DHL9974205CAngle · damagedAT C CHECK, RIGHT WING L/E SLAT CRACKED JUST BELOW FWD END OF ANTI-ICE DUCT. CUT OUT DAMAGED SECTION OF ATTACH ANGLE. INSTALLED FORMED SECTION REPAIR PER SRM 51-40-3. 18 BY 1 BY 1, N/R 2271.Sep 23, 1999 · N742DH · Boeing 727225 · Leading Edge DevicesSDR DL72S992088Bracket · crackedTHREE INCH CRACK IN NR 8 SLAT ACTUATOR I/B SUPPORT BRACKET. REPAIRED PER MM 51-20-21.Sep 17, 1999 · N8889Z · Boeing 727225 · Leading Edge Slat Actuator
Back to Boeing 727-225