Boeing 727-228

Service difficulty reports · 1,323

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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 = '727228'
  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 DHL9972712CAngle · crackedAT C CHECK, LT WING COVE PANEL SUPPORT ROD ATTACH ANGLES CRACKED STA 568 OUTBD NR 2 SPOILER ACT. REPLACED LT WING COVE PANEL SUPPORT BRKT AT STA 568 O/B OF NR 2 SPOILER ACT PER B727 SRM 51-30-2 N/R 1464.Aug 19, 1999 · N727DH · Boeing 727228 · Wing Miscellaneous StructureSDR DHL9972704CBracket · crackedAT C CHECK, LT WING COVE PANEL SUPPORT ROD I/B OF NR 2 SPOILER ACT LOWER END SUPPORT BRACKET CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW B727 SRM 51-30-2 N/R 1465.Aug 19, 1999 · N727DH · Boeing 727228 · Wing Miscellaneous StructureSDR DHL9972711CBracked · crackedAT C CHECK, LT WING COVE PANEL SUPPORT ROD ATTACH BRACKET CRACKED I/B NR 3 SPOILER ACT. REPLACED SUPPORT ROD ATTACH BRACKET AT LT COVE I/B AT NR 3 SPOILER ACT PER B727 SRM 51-30-2 N/R 1469.Aug 18, 1999 · N727DH · Boeing 727228 · Wing Miscellaneous StructureSDR DHL9972737CSkin · crackedAT C CHECK, LT WING UPPER SURFACE NR 4 SPOILER PANEL NR 2 AND NR 4 HINGE CUTOUTS CRACKED. VERIFIED CRACK INDICATIONS USING HFEC INSP PER NDT MANUAL PART 6-51-00-00 FIG 4, STOP DRILLED CRACK PER SRM 57-30-4 AT NR 4 SPOILER PANEL NR 2 AND NR 4 HINGE CUTOUTS, HFAug 17, 1999 · N727DH · Boeing 727228 · SpoilersSDR DHL9972726CBracket · crackedAT C CHECK, FWD CARGO COMPARTMENT DOOR SNUBBER FWD END SUPPORT BRACKET IS CRACKED. REMOVED FWD CARGO DOOR FOR ACCESS IAW B727 MM 52-31-0. REMOVED AND REPLACED SNUBBER FWD END SUPPORT BRACKET, INSTALLED FWD CARGO DOOR PER MM 52-31-0, OPS CHECK OK PER MM 52-31Aug 17, 1999 · N727DH · Boeing 727228 · Cargo/Baggage DoorsSDR DHL9972722CPanel · delamiantedAT C CHECK, LT WING LOWER SURFACE COVE PANEL AFT OF ACCESS PANEL 8405 WITH AREAS DELAMINATED. REMOVED PANEL AT LT WING AFT OF PANEL 8405 AS PER B727 SRM 51-30-2, INSTALLED BONDING REPAIR PER SRM 51-40-6 FIG 1 SIZE 11 X 72 USING ADHESIVE FILM AF163-2K, INSTALLAug 17, 1999 · N727DH · Boeing 727228 · Wing, Plate/SkinSDR DHL9972705CBracket · crackedAT C CHECK, LT WING REAR SPAR CAVITY AREA WS 544.00 COVE PANEL LOWER SUPPORT BRACKET CRACKED. REMOVED AND REPLACED I/B AND O/B BRACKETS AT LT WING REAR SPAR WS 544.00 PER SRM 51-30-2 N/R 1421.Aug 17, 1999 · N727DH · Boeing 727228 · Wing Miscellaneous StructureSDR DHL9972703CSupport · crackedAT C CHECK, LT WING REAR SPAR CAVITY AREA WS 567.0 COVE PANEL LOWER SUPPORT CRACKET CRACKED. REPLACED COVE PANEL SUPPPORT BRKT AT WS 567.0 PER B727 SRM 51-30-2 N/R 1422.Aug 17, 1999 · N727DH · Boeing 727228 · Wing Miscellaneous StructureSDR DHL9972702CSupport · crackedAT C CHECK, LT WING REAR SPAR CAVITY AREA WS 499.0 COVE PANEL LOWER SUPPORT BRACKET CRACKED. REPLACED LT WING COVE PANEL SUPPORT BRACKET AT WS 499 PER B727 SRM 51-30-2 N/R 1423.Aug 17, 1999 · N727DH · Boeing 727228 · Wing Miscellaneous StructureSDR DHL9972731CSkin · crackedAT C CHECK, LEFT FLYING DOOR IS CRACKED ON EXTERIOR AT FWD END WHERE DOOOR ANGLES MEET. CUT OUT DAMAGED AREA AT LEFT FLYING DOOR FWD END PER SRM 51-40-3, INSTALLED REPAIR ON EXTERIOR SKIN AT FWD END WHERE DOOR ANGLES MEET USING 2024T3 .050 PER SRM 51-30-2. AAug 16, 1999 · N727DH · Boeing 727228 · Landing Gear DoorsSDR DHL9972730CSkin · holeAT C CHECK, LEFT FLYING DOOR HAS A HOLE IN THE INNER SKIN 10 AFT OF THE FWD EDGE. APPROX SIZE OF HOLE IS .5 X .0625. INSTALLED REPAIR AT LEFT FLYING DOOR IN THE INNER SKIN USING 2024T3 .050 18 X 14 PER SRM 51-30-2. ALODINED AND PRIMED IAW SRM 51-10-2 N/R 73Aug 16, 1999 · N727DH · Boeing 727228 · Landing Gear DoorsSDR DHL99720006Egt Indication · exceeded limitsAFTER TAKEOFF ROTATION, NR 1 EGT WAS GOING TO EXCEED TAKEOFF LIMITS NR 1 THRUST LEVER WAS REDUCED IN ORDER TO MAINTAIN A MAX CONTINUOUS EGT LIMIT OF NR 1 ENGINE. EPR AT THIS POINT WAS 1.70. GROUND RAN NR 1 ENG TO TAKEOFF EPR ALL INDICATIONS WITHIN LIMITS IAWAug 12, 1999 · N720DH · Boeing 727228 · Engine EGT/TIT Indicating SystemSDR DHL99724004Epr Indication · abnormalREJECTED T/O DUE TO ABNORMAL EPR NR 3 ENG INICATION. DEFERRED NR 3 ENG EPR INDICATION.Aug 10, 1999 · N724DH · Boeing 727228 · Engine Pressure Ratio (EPR)SDR DHL99720005Altimeter · failedF/O'S ALTIMETER STUCK FOR 800 FT DURING CLIMB AT FL 30.0. REPLACED F/O'S ALTIMETER, SYSTEM OPS CHECKED GOOD IAW MM 34-12-01.Aug 3, 1999 · N720DH · Boeing 727228 · Altimeter, Barometric/EncoderSDR DHL99727005Mechanism · out of adjustON CLIMBOUT AT 28,000 FT 320 KTS VIBRATION ONSET, SLOWED TO 295 VIBRATION STOPPED. DID NOT VIBRATE IN CRUISE. INSPECTED IAW MM 05-51-181. FOUND RT I/B TRAILING EDGE FLAP ECCENTRICS HAVE EXCESSIVE CLEARENCE. ADJUSTED PER MM 27-51-1.Jul 20, 1999 · N727DH · Boeing 727228 · Trailing Edge Flap Control SystemSDR DHL99720004Vert Gyro · failedCAPTS ADI ATTITUDE FLAG CAME INTO VIEW DURING A TURN. REPLACED NR 1, OPS CHECK GOOD.Jul 20, 1999 · N720DH · Boeing 727228 · Attitude Gyro and Indicating SystemSDR DHL99726001Dg Syst · failedNR 1 COMPASS FLAG, HEADING FLAG IN HSI AND COMPASS FLAG IN NR 2 RMI IN VIEW. REPLACED NR 1 DG. OPS CHECK GOOD PER MM 34-21-71.Jul 13, 1999 · N726DH · Boeing 727228 · Directional Gyro and Indicating SystemSDR DHL99727004Valve · failedNR 3 FUEL TANK CROSSFEED MANIFOLD VALVE INOP ON CLIMBOUT. REPLACED CONNECTOR AND VALVE PER MM 20-61-00 AND 28-22-17.Jun 17, 1999 · N727DH · Boeing 727228 · Fuel Transfer ValveSDR DHL99721004Indicator · malfunctionedAT FL 310, THE NR 1 OIL TEMP NEEDLE INCREASED TO 130 CELSIUS. FOLLOWING A REDUCTION IN THRUST TO 1.5 EPR THE TEMP DROPPED BELOW 120. HOWEVER, THE NEEDLE CONTINUED TO FLUCTUATE AND GIVE ERRATIC READINGS. TEMP REMAINED BELOW 120. ALL OTHER INDICATIONS NORMJun 8, 1999 · N721DH · Boeing 727228 · Engine Oil TemperatureSDR DHL99720003Pump · overheatedON TAKEOFF, NR 2 B-PUMP OVERTEMPED. REMOVED AND REPLACED NR 2 B-PUMP AND CASE DRAIN FILTER PER MM 29-12-11.Jun 8, 1999 · N720DH · Boeing 727228 · Hydraulic Pump, AuxiliarySDR DHL99727003Seal · dirtyAIRCRAFT FAILED TO PRESSURIZE. TROUBLESHOOT SYSTEM, FOUND DEBRIS IN LOWER CARGO DOOR SEAL. REMOVED DEBRIS AND AIRCRAFT PRESSURIZED NORMAL PER MM 21-50-0.May 18, 1999 · N727DH · Boeing 727228 · Cargo/Baggage DoorsSDR DHL99727002Panel · brokenAIRFRAME VIBRATION AT 285 KTS ABOVE 300 KTS VIBRATION IS SEVERE. FOUND THREE FLAP COVE PANELS BROKEN, ONE AT STA 543 AND TWO AT STA 521. REPLACED PER MM 57-30-0.Apr 26, 1999 · N727DH · Boeing 727228 · Wing, Plate/SkinSDR DHL99727001Adi · failedFIRST OFFICERS ADI FAILED, HAS OFF FLAG AND ADI TUMBLED. RERACKED ADI.Apr 8, 1999 · N727DH · Boeing 727228 · Integrated Flight SystemSDR DHL99720002Controller · inoperativeDURING CLIMBOUT, GEN NR 1 CARRIED ALL ELECTRICAL LOAD AT 50 KW. NR 1 CSD IN TEMP 120 DEGREES. NR 2 AND 3 GEN CARRIED NO LOAD. NR 2 AND 3 CSD IN TEMP 80 DEGREES C. ALL THREE GEN VOLTS AND FREQS NORMAL. FIVE MINUTES AFTER DEPARTURE THE LOADS EQUALLED OUT AND Apr 5, 1999 · N720DH · Boeing 727228 · AC RegulatorSDR DHL99720001Accessory Unit · failedDEPARTING JFK RIGHT GEAR WARNING LIGHT ILLUMINATED WITH GEAR IN UP POSITION. GEAR RECYCLED. WHEN GEAR WAS PLACED UP, LEFT MAIN & RT MAIN RED WARNING AND SECOND OFFICER LEFT MAIN & RT MAIN GEAR DOOR LIGHTS ILLUMINATED. PLACED GEAR DOWN, ALL LIGHTS NORMAL. Feb 21, 1999 · N720DH · Boeing 727228 · Landing Gear Position and WarningSDR DHL99721003Servo · malfunctionedAUTO-PILOT AND STAB CRUISE TRIM WILL NOT TRIM NOSE UP. REMOVED AND REPLACED AUTO PILOT STAB TRIM SERVO PER MM 22-11-211, OPS CHECK GOOD.Feb 5, 1999 · N721DH · Boeing 727228 · Autopilot Trim ServoSDR DHL99721002Controls · malfunctionedWHEN AILERON INPUT IS APPLIED A NULL AREA OF 10 DEGREES LEFT AND RIGHT IS DETECTED WITH NO ROLL RESPONSE. AILERON TRIM SET 1 UNIT RT, RUDDER 0. INSPECTED AILERON MOVEMENT, NO DEFECT NOTED AND CHECK LOST MOTION DEVICE, FOUND TO BE WITHIN LIMITS PER MM 22-61-5Jan 30, 1999 · N721DH · Boeing 727228 · Aileron Control SystemSDR DHL99724002Valve · crackedDURING GEAR RETRACTION EXPERIENCED COMPLETE HYDRAULIC FLUID LOSS OF A SYSTEM. FOUND LEFT MAIN GEAR LOCK OPERATION SEQUENCE VALVE CRACKED. REMOVED AND REPLACED VALVE PER MM 32-32-31, OPS CHECK GOOD.Jan 27, 1999 · N724DH · Boeing 727228 · Landing Gear Retraction/Extension SystemSDR DHL99721001Switch · failedNR 6 L/E KRUEGER FLAP FAILED TO RETRACT AFTER TAKEOFF. COMPLETED ABNORMAL PROCEDURES, RETURNED TO SJU FOR LANDING. REMOVED ANF, REPLACED SWITCH ON NR 6 KRUEGER FLAP.Jan 27, 1999 · N721DH · Boeing 727228 · Leading Edge Slat Control SystemSDR DHL99724003Engine · failedNR 3 ENGINE OIL BYPASS LIGHT ILLUMINATED, OIL TEMP WENT TO 150. PERFORMED ENGINE SHUTDOWN. REMOVED AND REPLACED ENGINE PER MM 71-01-14.Jan 7, 1999 · N724DH · Boeing 727228 · Engine (Turbine/Turboprop)SDR DHL99724001Compressor · stalledNUMBER 3 ENGINE HAS SEVERE COMPRESSOR STALL AFTER TAKEOFF. ENGINE SHUT DOWN AND DIVERTED TO TAKEOFF ALTERNATE AT MCI. REMOVED AND REPLACED ENGINE.Jan 2, 1999 · N724DH · Boeing 727228 · Turbine Engine Compressor SectionSDR DHL98727004Switch · failedNR 4 LEADING EDGE FLAP AMBER LIGHT ON BOTH FWD PANEL AND AFT PANEL WITH FLAPS UP ACCELERATING TO 300 KTS. REMOVED AND REPLACED FLAP SWITCH.Dec 22, 1998 · N727DH · Boeing 727228 · Leading Edge Slat Position Indicating SystemSDR DHL9872061DFlap · damagedAT D CHECK, LEFT I/B MID FLAP DAMAGED AT I/B AFT END. INSTALLED F/G OVERLAY PER SRM 51-40-8, 5 BY 8 N/R 1084.Nov 27, 1998 · N720DH · Boeing 727228 · Trailing Edge FlapsSDR DHL9872088DSkin · crackedAT D CHECK, FWD ENTRY DOOR HAS SEVERAL BROKEN RIVETS AND SKIN CRACK AT FASTENER HOLE. CUT OUT CRACKED SECTION, HFEC, INSTALLED REPAIR DOUBLER PER SRM 52-00-3, 9 BY 6, N/R 3691.Nov 24, 1998 · N720DH · Boeing 727228 · Passenger/Crew DoorsSDR DHL9872003DFrame · crackedAT D CHECK, CRACKED FRAME STA 990 AT STR 26L, CRACK TERMINATED AT FASTENER HOL, VERIFIED BY HFEC. INSTALLED DOUBLER REPAIR PER SRM 53-10-4, 2 FT BY 7, N/R 3558.Nov 21, 1998 · N720DH · Boeing 727228 · Fuselage Main, FrameSDR DHL9872094DFrame · crackedAT D CHECK, RT WHEEL WELL FUSELAGE FRAME CRACKED JUST BELOW PRESSURE DECK BS 930. REMOVED AND REPLACED CORRODED L ANGLE. FABRICATED NEW FRAME PER BOEING DRAWING 65-16336. INSTALLED REPAIR AT PREVIOUS REPAIR PER BOEING DRAWING. INSTALLED FRAME REPAIR AT STANov 20, 1998 · N720DH · Boeing 727228 · Fuselage Main, FrameSDR DHL9872060DSpar · wornAT D CHECK, NR 4 SLAT WHERE NR 12 RIB FROM O/B END ATTACHED TO SPAR WEB HOLES ARE LARGE AND ELONGATED. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 57-30-3, 7 BY 4, N/R 1958.Nov 19, 1998 · N720DH · Boeing 727228 · Wing SparSDR DHL9872057DFitting · corrodedAT D CHECK, RIGHT WING ATTACH FITTING AT STA 950 RBL 56 STR 18 A IS CORRODED. REMOVED AND REPLACED FITTING PER SRM 51-30-2, N/R 7696.Nov 19, 1998 · N720DH · Boeing 727228 · Fuselage, Wing Attach FittingsSDR DHL9872018DAngle · damagedAT D CHECK, NR 1 ENGINE LOWER COWLING O/B SECTION AFT OF 2ND 'U' BOLT CUT OUT ANGLE DAMAGED. REPLACED DAMAGED ANGLE PER SRM 51-40-3, 25 BY 4, N/R 6780.Nov 18, 1998 · N720DH · Boeing 727228 · Engine Cowling SystemSDR DHL9872093DFrame · crackedAT D CHECK, RIGHT WHEEL WELL AFT OF UPLOCK FITTING BS 915 CRACKED FRAME 12 BELOW PRESSURE FLOOR. STOP DRILLED, HFEC, INSTALLED ANGLE PER SRM 57-40-3, 4 BY 8, N/R 2916.Nov 17, 1998 · N720DH · Boeing 727228 · Wing SparSDR DHL9872087DClip · corrodedAT D CHECK, AFT CARGO COMP STA 970 STR 27L AND TIE CLIP CORRODED. REMOVED DAMAGED STRINGER, INSTALLED DOUBLER REPAIR PER SRM 53-10-3 28, N/R 3678.Nov 17, 1998 · N720DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL9872086DAngle · crackedAT D CHECK, ANGLE CRACKED AT BS 720F STRINGER 28R TO 28L APPROX EXTERIOR SKIN A/C BAY. REMOVED AND REPLACED ANGLE PER SRM 51-40-3, 1 FT BY 1 BY 20, N/R 3676.Nov 17, 1998 · N720DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL9872085DIntercostal · corrodedAT D CHECK, CORROSION ON INTERCOSTAL BETWEEN STA 950 A TO STA 950B, STR 28 LT AFT CARGO COMPT. INSTALLED ANGLE REPAIR PER SRM 51-40-2, 6 BY 4, N/R 3673.Nov 16, 1998 · N720DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL9872059DRib · crackedAT D CHECK, LEFT WING NR 4 L/E SLAT RIB MARKED NR 11 CRACKED. REPLACED RIB PER SRM 57-50-2, N/R 1979.Nov 16, 1998 · N720DH · Boeing 727228 · Leading Edge DevicesSDR DHL9872041DSkin · corrodedAT D CHECK, NR 2 ENGINE LT STUB SURFACED SKIN HAS CRACKS AND BULGING AROUND FASTENERS APPROX BS 1360 STR 8L. REMOVED AND INSTALLED NEW SKIN PER SRM 53-30-3, 2 FT BY 2 FT, N/R 4611.Nov 14, 1998 · N720DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL9872019DSeat Track · crackedAT D CHECK, SEAT TRACK CRACKED AT STA 950 RBL 24 INBD LEG. CUT OUT DAMAGE AND INSTALLED REPAIR FROM STA 910 TO 950 PER SRM 53-10-5, N/R 5864.Nov 14, 1998 · N720DH · Boeing 727228 · Fuselage, Seat/Cargo Attach FittingsSDR DHL98724004Rt Unit · failedRADAR AT ABILIZATION WAS INOP, NOT PAINTING PROPERLY. REPLACED RADAR R/T.Nov 13, 1998 · N724DH · Boeing 727228 · Weather Radar SystemSDR DHL9872084DFrame · corrodedAT D CHECK, REAR CARGO FRAME CORRODED AT STA 950C AT STR 26R. INSTALLED REPAIR PER SRM 53-10-4, 8 BY 5, N/R 3667.Nov 13, 1998 · N720DH · Boeing 727228 · Fuselage Main, FrameSDR DHL9872083DFloorbeam · corrodedAT D CHECK, FLOORBEAM CORRODED TOP AND BOTTOM SIDES OF UPPER FLANGE FS 1070 RBL 65. CUT OUT DAMGAGED AREA. INSTALLED REPAIR PER SRM 53-10-8, 2 BY 30, N/R 3668.Nov 13, 1998 · N720DH · Boeing 727228 · Fuselage Main, Floor BeamSDR DHL9872082DDoor · crackedAT D CHECK, RT RAM AIR DOOR IS CRACKED AT BOTTOM FLANGE. REPALCED DOOR PER MM 21-56-1, N/R 3666.Nov 13, 1998 · N720DH · Boeing 727228 · Air Conditioning Doors
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