Boeing 727-228
Service difficulty reports · 1,323
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 = '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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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.SDR 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.SDR 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, HFSDR 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 52-31SDR 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, INSTALLSDR 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.SDR 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.SDR 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.SDR 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. ASDR 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 73SDR 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 IAWSDR DHL99724004Epr Indication · abnormalREJECTED T/O DUE TO ABNORMAL EPR NR 3 ENG INICATION. DEFERRED NR 3 ENG EPR INDICATION.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.SDR 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.SDR DHL99720004Vert Gyro · failedCAPTS ADI ATTITUDE FLAG CAME INTO VIEW DURING A TURN. REPLACED NR 1, OPS CHECK GOOD.SDR 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.SDR DHL99727004Valve · failedNR 3 FUEL TANK CROSSFEED MANIFOLD VALVE INOP ON CLIMBOUT. REPLACED CONNECTOR AND VALVE PER MM 20-61-00 AND 28-22-17.SDR 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 NORMSDR DHL99720003Pump · overheatedON TAKEOFF, NR 2 B-PUMP OVERTEMPED. REMOVED AND REPLACED NR 2 B-PUMP AND CASE DRAIN FILTER PER MM 29-12-11.SDR 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.SDR 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.SDR DHL99727001Adi · failedFIRST OFFICERS ADI FAILED, HAS OFF FLAG AND ADI TUMBLED. RERACKED ADI.SDR 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 SDR 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. SDR 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.SDR 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 22-61-5SDR 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.SDR 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.SDR 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.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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 STASDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR DHL98724004Rt Unit · failedRADAR AT ABILIZATION WAS INOP, NOT PAINTING PROPERLY. REPLACED RADAR R/T.SDR 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.SDR 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.SDR DHL9872082DDoor · crackedAT D CHECK, RT RAM AIR DOOR IS CRACKED AT BOTTOM FLANGE. REPALCED DOOR PER MM 21-56-1, N/R 3666.
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