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 DL72S960480Wire Harness · burnedA/C LOST N-1 INDICATION, FUEL HEAT LIGHT AND START VALVE LIGHT 'ON'. F/F STUCK ON 4800 PPH, ENGINE SHUTDOWN. FOUND WIRE HARNESS MELTED IN FWD PYLON SPLICED IN NEW ENG WIRING AT PLUGS D374J, D356J, D350J, D386P AND D362J, PERFORMED CK OUT PER PFHB AND CKS GOOJan 1, 1996 · N408DA · Boeing 727232 · Engine Indicating System WiringSDR DL72S960005Battery · dischargedRIGHT OVERWING CENTER EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY PACK AND CHECKS OK.Jan 1, 1996 · N403DA · Boeing 727232 · Emergency LightingSDR DL72S960004Battery · dischargedRIGHT OVERWING EMERGENCY LIGHT EXIT SIGNS INOP. REPLACED BATTERY PACK AND CHECKS OK.Jan 1, 1996 · N403DA · Boeing 727232 · Emergency LightingSDR DL72L960001Pbe · popped indicatorFIRST CLASS COAT CLOSET PBE UNSERVICEABLE, INDICATOR POPPED. REPLACED PBE.Jan 1, 1996 · N501DA · Boeing 727232 · Portable Oxygen SystemSDR DL72S954811Power Supply · inoperativeRT AFT OVER DOOR EMERGENCY LIGHT OUT. REPLACED M1093 RACK AND OPERATIONAL CHECKS GOOD.Dec 31, 1995 · N495DA · Boeing 727232 · Emergency LightingSDR 96ZZZX1395Doubler · crackedBRACKET CRACKED IN FORWARD CARGO BETWEEN STR 26R AND STR 27R AT STA 546. STOP DRILLED CRACK, FABBED DOUBLER AND INSTALLED PER SRM 51-20-2.Dec 29, 1995 · N18786 · Boeing 727232 · Fuselage Miscellaneous StructureSDR 96ZZZX1394Doubler · corrodedAFT RT LAV, APPROXIMATELY 6 INCHES DIAMETER AREA OF BULGING ON SUB-FLOOR AROUND PLUMBING LINES. REMOVED CORROSION, FABBED AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2.Dec 29, 1995 · N18786 · Boeing 727232 · Fuselage Miscellaneous StructureSDR 96ZZZM303Angle · crackedMAIN CABIN CRACK IN FLOOR BOARD ATTACH ANGLE AT STATION 1130 RBL 64. ALSO, SMALL AREA OF LEVEL 1 CORROSION 6 INCHES FARTHER AFT FROM CRACK. REMOVED CORROSION, MATERIAL LOSS WITHIN ACCEPTABLE LIMITS PER SRM 51-10-6, 51-10-3 AND FABRICATED ANGLE DOUBLERS, ALODDec 29, 1995 · N18786 · Boeing 727232 · Fuselage Miscellaneous StructureSDR 96ZZZM284Channel · corrodedLEVEL 2 SURFACE CORROSION WIDE SPREAD ON R-1 DOOR THRESHOLD Z-CHANNEL FROM STATION 380-420 RBL 53. REMOVED AND REPLACED 2 CHANNEL PER LIMITS PER SRM 51-40-2. (M)Dec 29, 1995 · N18786 · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S960024Skin · crackedA SKIN CRACK, 1.75 INCH BY 2 INCH WAS DISCOVERED BETWEEN STRINGER 27R AND 28R, FS 481. THE PREVIOUS REPAIR ON THIS SECTION MEASURED 5.5 INCH BY 13 INCH. THE REPAIRS WERE INCORPORATED INTO ONE REPAIR AFTER REMOVAL OF PREVIOUS REPAIR. THIS ER/A SUPERCEDES ER/Dec 28, 1995 · N407DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S954794Angle · crackedFOUND DURING A-1 LETTER CHECK, NR 6 L/E FLAP ACTUATOR I/B ATTACH ANGLE CRACKED. REPAIRED PER M/M 57-20-21 PAR 12.Dec 28, 1995 · N497DA · Boeing 727232 · Wing Miscellaneous StructureSDR DL72S954793Skin · crackedFOUND DURING A-1 LETTER CHECK, NR 8 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.Dec 28, 1995 · N497DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954792Skin · crackedFOUND DURING A-1 LETTER CHECK, NR 7 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED O/B END. REPAIRED PER M/M 57-54-0 PAR 5A.Dec 28, 1995 · N497DA · Boeing 727232 · Leading Edge DevicesSDR DL72K954796Battery Pack · dischargedEMERGENCY LIGHTING INOP OVER L-2 DOOR. ITEM FOUND DURING MTC LAYOVER. REPLACED BATT PACK AND ALL OPS NORMAL.Dec 28, 1995 · N417DA · Boeing 727232 · Emergency LightingSDR DL72S954780Angle · crackedFOUND ON B1 LETTER CK, ANGLE CRACKED STA 910 LT SIDE. REPAIRED PER MM 53-11-0.Dec 27, 1995 · N483DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S954779Inlet Skin · crackedFOUND ON B1 LETTER CK, 1 INCH CRACK IN THE NR 2 ENGINE INLET HOUSING AT LOWER AFT CORNER OF PANEL 9516. REPAIRED PER MM 54-30-0.Dec 27, 1995 · N483DA · Boeing 727232 · Engine Cowling SystemSDR DL72S954778Web · crackedFOUND ON B1 LETTER CK, LOWER LT TORQUE BOX WEB CRACKED TWO PLACES, 1 INCH AT FORWARD CENTER LIGHTNING HOLE STA 1223 AND .25 INCH CRACK AT THE NEXT LIGHTNING HOLE AFT AND BELOW THE FORWARD CENTER LIGHTNING HOLE. REPAIRED PER MM 53-11-0.Dec 27, 1995 · N483DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR 96ZZZX1396Floor Beam · corrodedSTA 380.0 FLOOR BEAM UPPER CORD HAS LEVEL 2 CORROSION ACROSS IT FROM RBL 13 TO RBL 60. REMOVED AREA OUT OF LIMITS AND REPAIRED PER SRM 53-10-8, FIGURE 3.Dec 27, 1995 · N18786 · Boeing 727232 · Fuselage Main, Floor BeamSDR DL72S954771Skin · crackedFOUND ON C2 LETTER CHECK, MAIN ENTRY DOOR OUTER SKIN CRACKED .75 INCH LOWER AFT CORNER. REPAIRED PER MM 52-11-01.Dec 26, 1995 · N529DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S954761Tube · wornPIREP LOSS OF ALL HYD B-QUANTITY IN-FLIGHT. FOUND HYD LINE IN LEFT BODY FAIRING AREA LEAKING. REF IPC 29-14-0-6, ITEM 155, AND ITEM 160. HOLE IN LINE DUE TO CHAFING.Dec 23, 1995 · N408DA · Boeing 727232 · Hydraulic System, MainSDR DL72K961612Transverse Beam · crackedTHERE IS A 1.5 INCH CRACK IN THE AFT GUSSET AND FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1263. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS REPLACEMENT DOES NOT TERMINDec 23, 1995 · N417DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR CAL951174Battery · inoperativeFLT NR 293 - EWR - THE OVERHEAD EMEGENCY EXIT LIGHT AT AFT GALLEY WOULD NOT ILLUMINATE. THE EMERGENCY EXIT LIGHT BATTERY WAS REPLACED AND OPERATION OF THE LIGHT WAS RESTORED. (M)Dec 23, 1995 · N45793 · Boeing 727232 · Emergency LightingSDR DL72S960026Stringer · crackedTHE VENT STRINGER 13 ON THE LT WING WAS FOUND WITH A CRACK IN THE STRINGER TO RIB ATTACH TAB AT WING STATION 656.5. DUE TO THE EXTENT OF THE CRACK, THE STOP DRILL REPAIR CALLED OUT IN EO 4-60350-3AD COULD NOT BE ACCOMPLISHED. THE DAMAGED TAB WAS REMOVED AND Dec 22, 1995 · N496DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S960025Skin · crackedTHE FUSELAGE SKIN AT THE RT AFT SERVICE DOOR CUTOUT, LOWER AFT CORNER WAS CUT OUT TO REMOVE DAMAGE AROUND EXISTING NUTPLATE HOLE. THE RESULTANT CUT OUT IS APPROX 2.3 UP/DOWN AND 2.1 FWD/AFT. THE CUT OUT IS THROUGH THE SKIN AND BONDED DOUBLER ONLY. INSTALLEDDec 22, 1995 · N496DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S960020Frames · crackedTHE LT FS 784 OVERWING EXIT FRAME WAS FOUND WITH A CRACK 1.1 INCH LONG. IT BEGAN AT A FASTENER HOLE ON THE INBD FLANGE AT WL 215 AND RAN HORIZONTALLY FWD AND THROUGH THE BEND RADIUS JUST INTO THE WEB. THIS CRACK IS OUTSIDE THE TYPICAL CRACK AREA AS DEFINED IDec 21, 1995 · N496DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S954750Solenoid · failedIRR - ON TAKEOFF, GEAR HANDLE WOULD NOT RAISE PAST THE OFF POSITION. PUT GEAR HANDLE BACK DOWN. DIVERTED TO DEN DUE TO GEAR HANDLE. CORRECTIVE ACTION - REPLACED LANDING GEAR HANDLE LATCH LEVER SOLENOID PER DELTA M/M 32-31-16. CYCLED GEAR SEVERAL TIMES, ALLDec 21, 1995 · N405DA · Boeing 727232 · Landing Gear SelectorSDR 96ZZZX1393Seat Track · corrodedSEAT TRACK, RBL 13, STA 340 - STA 380, HAS LEVEL 2 CORROSION AT SEVERAL AREAS ALONG FLANGES AND FLOOR BEAM ATTACH POINTS. REMOVED DAMAGED SEAT TRACK, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION PER SRM 51-10-1 AND SRM 51-30-2.Dec 21, 1995 · N18786 · Boeing 727232 · Fuselage, Seat/Cargo Attach FittingsSDR DL72S960393Rib Tab · crackedDURING INSPECTION, STRINGER 8R OF THE VERTICAL STAB. HAS A CRACK ON THE FIN STA. 157.2 RIB ATTACHMENT TAB. THE SUBJECT CRACK RUNS FROM FASTENER HOLE TO EDGE OF TAB. A REPAIR ANGLE WAS INSTALLED IN ACCORDANCE WITH B727 S/B 55-0075.Dec 20, 1995 · N493DA · Boeing 727232 · Vertical Stabilizer, Spar/RibSDR DL72S960021Skin · corrosionTHE FUSELAGE SKIN AT STA 500 STR 28R WAS DAMAGED BY CORROSION AND A 13.5 INCH BY 3.5 INCH SECTION WAS CUTOUT. A SKIN REPAIR WAS ACCOMPLISHED PER B727 SRM 53-30-3 FIG 3, EXCEPT THE DOUBLER WAS EXTENDED FORWARD TO STA 480 BUTT JOINT. REPAIRS ACCOMPLISHED PER DDec 20, 1995 · N531DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S954791Stringer · crackedFORWARD LOWER FUSELAGE BS-480 STRINGER 28R SKIN BULGING AND CRACKED. REPAIRED PER DL ERA 302938-14.Dec 20, 1995 · N407DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S954747Battery Pack · dischargedEMERGENCY LIGHT OUT LOWER RT OVERWING FAIRING. REPLACED EMERGENCY LIGHT BATTERY PACK. CKS NORMAL.Dec 19, 1995 · N407DA · Boeing 727232 · Emergency LightingSDR DL72S954733Pbe · defectivePBE, LOCATED IN FIRST CLASS COAT CLOSET, HAS UNSERVICEABLE INDICATOR PROTRUDING PAST CONTAINER. REPLACED PBE.Dec 19, 1995 · N541DA · Boeing 727232 · Portable Oxygen SystemSDR DL72L954738Pack Valve · malfunctionedA/C WOULD NOT MAINTAIN PRESSURIZATION WITH SINGLE PACK. OPS CARGO HEAT VALVE CLOSED. REPLACED RT FWD PACK VALVE. REPLACED EQUIPMENT COOLING. SHUT OFF VALVE. PRESSURIZED A/C. CKS NORMAL.Dec 19, 1995 · N509DA · Boeing 727232 · Cabin Cooling SystemSDR DL72S954728Stringer · crackedFOUND DURING E-2 LETTER CHECK, VERTICAL STAB STRINGERS CRACKED, STR 8 RIGHT STA 133.8 AND STR 9 RIGHT STA 133.8. REPAIRED PER M/M 53-30-0 PAR 3.Dec 18, 1995 · N521DA · Boeing 727232 · Vertical StabilizerSDR DL72S954727Angle · crackedFOUND DURING E-2 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED UNDER TAI DUCT. REPAIRED PER M/M 57-54-0.Dec 18, 1995 · N521DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954716Eel · brokenEMERGENCY EXIT LIGHT AT GALLEY SERVICE DOOR IS BROKEN (LEFT). REPLACED LIGHT ASSY, OPS CHECKS NORMAL.Dec 16, 1995 · N477DA · Boeing 727232 · Emergency LightingSDR DL72S954715Eel Power Supply · inoperativeAFT SECTION OF EMERGENCY ESCAPE PATH LIGHT INOP. REPLACED BATTERY POWER SUPPLY, OPS CHECKS NORMAL. S/N ON 0483.Dec 16, 1995 · N477DA · Boeing 727232 · Emergency LightingSDR DL72S954709Cooling Valve · failedDURING CLIMB AND LEVEL AT FL 240, WERE UNABLE TO MAINTAIN, CABIN SLOWEST RATE OF ASSENT WAS 700 FPM. DESCENDED AND RETURNED TO JFK. FOUND EQUIPMENT COOLING VALVE STUCK OPEN. REPLACED VALVE. RETURNED TO SERVICE.Dec 15, 1995 · N407DA · Boeing 727232 · Cabin Cooling SystemSDR DL72S954726Web · fatigueMTC REPORTS, DAMAGE TO THE REAR SPAR WEB OF THE CENTER SECTION FUEL TANK. THE DAMAGE IS LOCATED APPROXIMATELY BETWEEN LBL 17.2 AND LBL 25.5. DAMAGE REMOVAL RESULTED IN A 3 I/B - O/B BY 1 UP/DOWN CUTOUT. THE WEB IS MANUFACTURED FROM 0.375 2024-T351 MACHINED Dec 13, 1995 · N403DA · Boeing 727232 · Wing SparSDR DL72S954696Gearbox · failedNR 2 ENG FAILED ON TAKEOFF. AFTER RETURNING TO YVR, CNTR MAINT FOUND THE NR 2 ENGINE GEARBOX HAD COME APART. REPLACED ENGINE AND ROUTED TO SHOP.Dec 13, 1995 · N532DA · Boeing 727232 · Turbine Engine Accessory DriveSDR DL72L961620Skin · corrosionTHE SKIN AND STRINGER AT FS 480 TO 520 AND STR 26R WERE FOUND CORRODED. THE SKIN CORROSION REQUIRED A 3.25 BY 2.75 CUTOUT IN THE UPPER AND LOWER SKINS OF THE STR 26R LAP JOINT. THE STRINGER CORROSION REQUIRED A CUTOUT IN THE STRINGER FROM THE EXISTING FACTORDec 13, 1995 · N504DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR 95FDEA01898Frame · misdrilledWHEN WORKING 7-5310-7-3367A1 PT 4, FOUND PILOT HOLE ON EDGE OF 3RD ABOVE THE FLOOR BS 783.95 RT WL 208. PILOT HOLES ARE IN FRAME ONLY. REPAIRED DAMAGED FRAME IAW FEDEX EA 7-5310-26784.Dec 13, 1995 · N498FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01897Frame · misdrilledWHEN WORKING 7-5310-7-3367 REV A1 PART 1, FOUND PILOT HOLES ON EDGE OF 3RD AND 4TH EXISTING FASTENER HOLES ABOVE THE FLOOR AT BS 760 LT WL 208. PILOT HOLES ARE IN FRAME ONLY. REPAIRED DAMAGED FRAME IAW FEDEX 7-5310-26784.Dec 13, 1995 · N498FE · Boeing 727232 · Fuselage Main, FrameSDR 95FDEA01896Frame · misdrilledWHILE WORKING EO 7-5310-7-3367A1 PT9, FOUND FIVE EXISTING HOLES IN 783 FRAME WHEN DRILLED IN NEW REPAIR WOULD FALL OUT IN RADIUS OF REPAIR ON 783 FRAME RT WL 200 TO 201, 207 AND 214 TO 216. INSTALLED FASTENERS IAW FEDEX EA 7-5310-26784.Dec 13, 1995 · N498FE · Boeing 727232 · Fuselage Main, FrameSDR DL72S960022Frame · oversized holesDURING ACCOMPLISHMENT OF EO4-61904-3AD, SEVERAL HOLES IN THE INB'D FRAME FLANGE AT FS 760.95 LT AND RT WERE OVERSIZED BEYOND LIMITS. THE OVERSIZED HOLES WERE REWORKED AND OVERSIZED FASTENERS WERE INSTALLED PER BACO TWX DAL-ATL-95-1340RR DTD 11 DEC 95, DL ERA Dec 12, 1995 · N496DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S954731Rib · crackedFOUND ON CV2 CHECK TRANSFERRRED FROM N/R 33 ITEM NR 2, .4375 INCH CRACK AT NR 6 SLAT NOSE RIB INBD SIDE OF ACTUATOR. REPAIRED PER M/M 57-54-0 AND ID PER PS 900-5-1 NR 4.Dec 12, 1995 · N531DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954706Angle · crackedFOUND ON CV2 CHECK, TWO CRACKS IN NR 7 SLAT COVE PANEL ATTACH ANGLE BELOW TAI DUCT. REPAIR: REPAIRED PER M/M 57-54-0, PAR 5A.Dec 12, 1995 · N531DA · Boeing 727232 · Leading Edge DevicesSDR DL72S954705Angle · crackedFOUND ON CV2 CHECK 1.) 1.25 INCH CRACK AT NR 7 SLAT COVE PANEL ATTACH ANGLE JUST INBOARD OF INBOARD TRACK. 2.) SCREWS/BOLTS LOOSE AT NR 7 SLAT INBOARD TRACK FAIRING. REPAIR: 1.) REPAIRED PER M/M 57-54-0 PAR 2. 2.) REPAIRED AS SECURED FASTENERS.Dec 12, 1995 · N531DA · Boeing 727232 · Leading Edge DevicesSDR DL72L954688Web · crackedFOUND ON E2 LETTER CK, .2187 INCH CRACK IN 48 SECT TORQUE BOX WEB LIGHTENING HOLE RT FWD SIDE. REPAIRED PER MM 53-11-0.Dec 12, 1995 · N504DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR 95FDEA01892Gusset · crackedGUSSET AT FRAME BS 825.95 IS CRACKED, RBL 65, WL 198. REPAIR ACCOMPLISHED IAW FEDEX EO 7-5310-7-3367A1, PART 6.Dec 12, 1995 · N498FE · Boeing 727232 · Fuselage Miscellaneous Structure
Back to Boeing 727-232