Boeing 727-233
Service difficulty reports · 3,034
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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 = '727233' 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 = '727233' 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 06FDEA2002Spacer · looseRIGHT ELEVATOR, NR 1 ELEVATOR RUB BLOCK SPACER IS LOOSE IN LOWER TRAILING EDGE BEAM. REPAIRED R/H ELEVATOR NR 1 RUB BLOCK SPACER IN T/E BEAM IAW FED-EX EA 7-5510-100547.SDR 06FDEA1980Shear Tie · corrodedFOUND BS 1148 BETWEEN STRS 30 AND 29 RT SHEAR TIE IS CORRODED. REMOVED SHEAR TIE BS 1148 STR 29 & 30 R/H PER SRM 51-30-2. BLENDED CORROSION 3 X 3 .030. ORIG THICKNESS .063. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SHEAR TIE USING 7075T6 .063 LOT #500810 SDR 06FDEA1943Frame · crackedFOUND CORROSION AT STA 1176 RBL 2 WL 208 FRAME IS CORRODED AND CRACKED. REMOVED AND REPLACED FRAME IAW SRM 51-30-2 AT BS 1176, LBL 68 - RBL 68.SDR PCSA051106SUPPump · failedFLIGHT 843 DEPARTED MIA AND DURING THE CLIMB THE CREW REPORTED NR 1 ENGINE LOW OIL PRESSURE LIGHT CAME ON DURING FLIGHT FOLLOWED BY F/E'S OIL PRESSURE GAUGE DROPPED TO 5 TO 10 PSI, SHUT DOWN NR 1 ENGINE PER AMJ CHECKLIST, DUMPED FUEL AND RETURNED TO MIA. THE SDR PCSA05110601Engine · failedFLIGHT 843 DEPARTED MIA AND DURING THE CLIMB THE CREW REPORTED NR 1 ENGINE LOW OIL PRESSURE LIGHT CAME ON DURING FLIGHT FOLLOWED BY F/E'S OIL PRESSURE GAUGE DROPPED TO 5 TO 10 PSI, SHUT DOWN NR 1 ENGINE PER AMJ CHECKLIST. DUMPED FUEL AND RETURNED TO MIA. THESDR 06FDEA1801Structure · ground damageLEFT SIDE OF FUSELAGE JUST FWD OF WING L/E WAS STRUCK BY VENDORS CREW, ENTRY STAIRS CAUSING MAJOR DAMAGE. REPAIRED FUSELAGE SKIN DAMAGE AS PER E.A. 7-5330-100531 AND SRM 53-30-3 FIG.12.REF N/R 9SDR 06FDEA1786None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT LT ELEVATOR INBOARD UPPER SURFACE WAS ACCOMPLISHED IAW SRM 55-20-3 FIG 1 PAGE 1, BASED ON AN EXTERNAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBER, GENERAL WORKMANSSDR 06FDEA1784Repair · misinstalledFOUND EXISTING REPAIR INSTALLED AT STA 270 STR 17L IS NOT CONFORMED TO FAA APPROVED REPAIR DATA. REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER IAW SRM 53-30-3, FIG 3A. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND SRM 53-30-3 FIG 3A. REPAIR IS CLASSIFSDR 06FDEA1783Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED AT STA 280 STR 22R IS NOT CONFORMED TO FAA APPROVED REPAIR DATA. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR DOUBLER IAW SRM 53-30-2 FIG 4. INSTALLED REPAIR DOUBLER IAW SRM 53-30-2 AND SRM 53-30-3. REPAIR IS CLASSIFIED ASDR 06FDEA1754Smoke Detector · malfunctionedPASSING FL 240 NR 1 MAIN CARGO SMOKE LIGHT ILLUMINATE WITH ASSOCIATED AURAL WARNING. EMERGENCY DESCENT, PASSING 12,000 FT CABIN ALTITUDE THE LIGHT EXTINGUISHED. NEVER ANY INDICATION OF SMOKE OR FUMES. MEM BLEW OUT SENSE LINES AND REMOVED AND REPLACED DETECTSDR 06FDEA1753Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED AT STA 765 STR 8R IS NOT CONFORMED TO FAA APPROVED DATA, REMOVED EXISTING REPAIR AND REINSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 AND SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6- 2-100.SDR 06FDEA1745Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED ON NR 7 LEADING EDGE SLAT IS NOT COMPLIED WITH FAA APPROVED DATA. REMOVED EXISTING REPAIR AND REINSTALLED REPAIR DOUBLER IAW SRM 57-50-3, FIG 1. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.SDR 06FDEA1728Engine · seizedAFTER T/O AT 1,000' WITH STD POWER, NR 3 ENGINE SEIZED AT QUIET OIL QUANTITY DROPPED TO ZERO. CONDUCTED EPR REDUCTION. QRH ENGINE FIRE/SEVERE DAMAGE CHECKLIST. RETURNED TO FIELD. CRASH CREW REPORTED OIL LEAKING FROM ENGINE. PERFORMED ENGINE SEIZURE INSP PSDR 06FDEA1722None · nonePREVIOUSLY REPAIR INSTALLED AT STA 710, STR 21L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 2 PAGE 9. BASED ON AN EXTERNAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS.SDR 06FDEA1721None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT LT FWD ENTRY DOOR HINGE CUTOUTS WAS ACCOMPLISHED IAW EA 7-5330-28325, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP SDR 06FDEA1705None · noneFOUND REPAIR LOCATED ON AFT CARGO DOOR REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR DETERMINED TO BE IAW SRM 52-00-3 FIG 3 BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLSDR CA060427004Shutoff Valve · malfunctioned(CAN) CLIMBING THROUGH FL20 THE F/E ADVISED OF PRESSURIZATION PROBLEMS. AFTER REDUCING TO 10,000 FT. CABIN INDICATED 10,000 WITH 3 PSI DIFF.WHEN THRUST REDUCED THE DIFF WAS 0. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE REPLACED THE PRESSURIZATIONSDR 06FDEA1420Fitting · looseNR 1 ENGINE FAILED TO MAKE STANDARD EPR ON TAKEOFF ROLL TARGET EPR 2.08, MADE ONLY 1.8 WITH THRUST LEVER AT FORWARD STOP. ENGINE WAS VERY SLOW TO ACCELERATE. NO OTHER PARAMETERS EXCEEDED. RUNWAY 27, WEATHER: 190/4KTS, 1ONM VIS, TEMP19*C, DEW POINT 11*C, 30.SDR 06FDEA1317Pressure Switch · malfunctionedAT FL350, AND FUEL TEMPERATURE 5, NR 2 FUEL ICING LIGHT ILLUMINATED. PERFORMED RELEVANT EMERG CK-LIST. DECLARED EMERGENCY. RELEASED FOR SERVICE PER MEL/CDL: 73-04 CATEGORY: C "MEL 73-04. TWO FUEL FILTER DIFFERENTIAL PRESSURE WARNING SYSTEM INOP. REMOVED ASDR 06FDEA1278Repair · misinstalledIMPROPER REPAIR INSTALLED STA 430 - 436 STR 21R - 22R. REMOVED, FABRICATED, ALODINED, PRIMED AND INSTALLED FUSELAGE FLUSH REPAIR IAW FX SRM 53-30-3 FIG 2, 51-30-2 AND 51-10-2.SDR PCSA033006Engine · damagedFLIGHT 848 AFTER PUSHBACK FROM PAP, THE CREW REPORTED WHEN POWER WAS ADDED THE NUMBER ONE ENGINE EXPERIENCED A VIBRATION. THE AIRCRAFT RETURNED TO THE GATE WITHOUT ANY FURTHER INCIDENT. FURTHER INSPECTION OF THE NUMBER ONE ENGINE INLET FOUND THE C-1 BLADES HSDR PCSA03020601Actuator · stuckON CLIMB, NUMBER 1 SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO KMIA AND LANDED WITH NO INCIDENT. MAINTENANCE FOUND NUMBER 1 SLAT ACTUATOR FAILED IN THE EXTENDED POSITION. SLAT ACTUATOR REMOVED AND REPLACED PER B727 MM 27-81-32, OPS AND LEAK CHECK OK. NO DESDR 06FDEA0888Repair · noneFOUND 3 REPAIRS LOCATED ON NR 3 CARGO DOOR OUTER SKIN, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIRS WERE ACCOMPLISHED USING FAA APPROVED DATA. REPAIRS FOUND TO BE IAW SRM 52-00-3 FIG 3. REPAIRS CLASSIFIED AS MAJOR.SDR 06FDEA0887Repair · noneFOUND REPAIR LOCATED ON RIGHT WING L/E ABOVE THE NR 4 KRUGER FLAP REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR FOUND TO IAW SRM 57-30-4 FIG 2. REPAIR CLASSIFIED AS MAJOR IAW FEDSDR 06FDEA0883Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 400 STR 17L-18L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBER, GENERAL WORKMSDR 06FDEA0882Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 188 STR 21R WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG 5, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKSDR 06FDEA0881Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1030 STR 18L-19L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBER, GENERAL WORKSDR 06FDEA0880Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 720E STR 19L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3, FIG 4 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSSDR 06FDEA0879Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050 STR 27R-28R WAS DETERMINED TO BE ACCOMPLISHED PER SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENERAL WORKSDR 06FDEA0870Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 540 STR 27R WAS ACCOMPLISHED PER FEDEX EA 7-5330-85285, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR ISSDR PCSA02230601Wheel · vibrationAT T/O, A SEVERE VIBRATION DURING T/O ROLL. CREW ABORTED T/O AT 100 KNOTS AND COMPLIED WITH AFM PROCEDURES. THE AIRCRAFT RETURNED TO THE BLOCK WITHOUT ANY FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED A CLOSE VISUAL INSPECTION OF THE MAIN TIRES, NO DEFECTS NOTSDR PCSA02090603Thermal Switch · intermittentCREW PREPARED FOR TAKEOFF, CREW REPORTED NR 1 ENGINE BLEED TRIPPED WHEN TAKEOFF POWER SET. AIRCRAFT RETURNED TO BLOCK WITHOUT INCIDENT. MX TROUBLESHOT & ACCOMPLISHED OPERATIONAL CHECKS OF THE BLEED SYSTEM AND COULD NOT DUPLICATE THE PROBLEM, THE AMERIJET FLISDR PCSA02090602Modulating Valve · malfunctionedFLIGHT 839 DURING PREPARATION FOR TAKEOFF, THE CREW REPORTED THE NUMBER 1 ENGINE BLEED TRIPPED WHEN TAKEOFF POWER WAS SET, 95 PSI DUCT PRESSURE INDICATED. THE AIRCRAFT RETURNED TO THE BLOCK WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUBLESHOT AND REPLACED TSDR PCSA02090601Flap · malfunctionedFLIGHT 839 DEPARTED MIA AND DURING THE CLIMB THE CREW REPORTED THE INBOARD FLAPS WERE STUCK AT 5 DEGREES, THE AIRCRAFT RETURNED BACK AND LANDED AT MIA WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMED A GENERAL VISUAL INSPECTION OF THE INBOARD FLAP SYSTEM IAW BSDR 06FDEA0186Engine · failedDURING A MAX POWER T/O AT 70-80 KNOTS THERE WAS A LOUD BANG AND AIRCRAFT PULLED LEFT. PERFORMED REJECTED. NR 1 EPR - 2.18 AT FAILURE. REPLACED NR 1 ENG PER WORK CARDS 70T0001-01 AND 70T030 1-01. ALL TEST NORMAL. RELEASED FOR SERVICE. COMPLIED WITH EO 7-SDR PCSA1110601Line · leakingDURING CLIMB, CREW REPORTED "A" SYSTEM HYD QTY IND DROPPED, CREW SUSPECTED AN "A" SYSTEM HYD FLUID LEAK. A/C RETURNED BACK TO MIA AND LANDED W/O ANY FURTHER INCIDENT. MX TROUBLESHOT "A" SYSTEM HYD LEAK, A LEAKING HYD LINE FOUND AT "B" NUT CONNECTION TO "A" SYSDR PCSA12300501Control Panel · unsecureCLIMBED TO CRUISE, CREW REPORTED NR 3 GEN BREAKER LIGHT CAME ON & WOULD NOT HOLD POWER, NR 2 GEN BREAKER & FIELD LIGHTS CAME ON, NO FAULT NOTED, RESET NR 2 GEN & 20 MIN LATER FAULT RETURNED NO LIGHTS. DID NOT RESET NR 2 BREAKER. DIVERTED ACFT, & LANDED WITHOUTSDR 05FDEA04421Transmitter · failedNUMBER 3 ENG EPR GAUGE FAILED TO REACH TAKEOFF EPR. UPON BLOCK IN NUMBER 3 EPR WAS SPINNING. RELEASED FOR SERVICE PER MEL/CDL: 77-01-01 CAT 'C' EXP: 31DEC05. NR 3 ENGINE EPR INDICATOR, INOP. REMOVED AND REPLACED NR 3 EPR TRANSMITTER PER 727-200 M/M 77-1SDR 05FDEA04423Skin · gougedA GOUGE FOUND AT BS 950E, STR 19R DURING PRIMARY INSPECTION, REPAIR ACCOMPLISHED WITH EA 7-5330-92374 ISSUED BY FEDEX ENGINEERING, REPAIR IS CLASSIFIED AS MAJOR PER EA 7-5330-92374.SDR 05FDEA04376Repair · undamagedFOUND PREVIOUSLY INSTALLED REPAIR ON UPPER SURFACE OF LT ELEVATOR WAS ACCOMPLISHED IAW ENGINEERING REPAIR NR 16-0193, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERALSDR 05FDEA04375Repair · undamagedFOUND PREVIOUSLY INSTALLED REINFORCEMENT DOUBLER AT STA 344 BETWEEN STR 4L AND 5L WAS ACCOMPLISHED IAW RIGID BARRIER MODIFICATION DOCUMENT EA 7-5340-7-5002, PAGE 1 AND VENTURA AEROSPACE DWG 2942, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SSDR 05FDEA04374Repair · undamagedFOUND PREVIOUSLY INSTALLED REPAIR AT STA 720D, STR 19R WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 6, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENERS SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPAIRSDR 05FDEA04373Repair · undamagedFOUND PREVIOUSLY INSTALLED REPAIR AT AFT LOWER CORNER OF FWD GALLEY DOOR CUT OUT WAS ACCOMPLISHED IAW SB 727-53-0188, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERALSDR 05FDEA04372Repair · undamagedFOUND PREVIOUSLY INSTALLED REPAIR AT STA 680, STR 28 WAS ACCOMPLISHED IAW SRM 51-40-3, FIG 1 PAGE 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, REPSDR 05FDEA04371Repair · noneFOUND PREVIOUSLY INSTALLED REPAIR AT LT ENTRY DOOR STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345 PT.2, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP, RSDR 05FDEA04370None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 660, STR 28R TO 28L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 2, PAGE 9, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSDR 05FDEA04361Indication Sys · out of rigLIGHT ILLUMINATED, PASSING 16K MSL (MCD A LIGHT WAS OUT AND TESTED GOOD). DESCENDED TO 10K MSL. LIGHT EXTINGUISHED AT 12K MSL, BULB TESTED GOOD. RELEASED FOR SERVICE PER MEL/CDL: 52-15-01 CATEGORY: C EXP: 26DEC05 "MEL 52-15-01: MCD WARN LIGHT SYS B INOP. SDR PCSA12150501Outflow Valve · stuckFLIGHT 731 AFTER DEPARTURE, DURING CLIMB THRU 6000 FT. CREW REPORTED CABIN PRESSURIZATION STARTED CLIMBING AT AN EXCESSIVE RATE AND COULD NOT MAINTAIN CABIN PRESSURIZATION. THE CREW REPORTED THE OUTFLOW VALVE WAS FULLY CLOSED, IT APPEARED THAT THE RT PACK WAS SDR 05FDEA04343Repair · unknownFOUND PREVIOUSLY REPAIR ON LT INBOARD FORE FLAP LEADING EDGE WAS ACCOMPLISHED IAS SRM 57-50-4, FIG 1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS SDR 05FDEA04342Repair · unknownFOUND PREVIOUS REPAIR ON LT OUTBOARD FOREFLAP LEADING EDGE WAS ACCOMPLISHED IAW SRM 57-50-4, FIG 1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENERS NUMBER AND SPACING AND GENERAL WORKMANSHIP, REPAIR
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