Boeing 727-2J0
Service difficulty reports · 220
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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 = '7272J0' 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 = '7272J0' 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 GAIA00621Skin · crackedDISCREPANCY: DURING ROUTINE INSPECTION AT FLIGHTSTAR AIRCRAFT SERVICES REPAIR STATION IN JAX IT WAS DISCOVERED THAT THERE WAS A CRACK AT THE SKIN LAP JOINT, LOWER FASTENER ROW AT FASTENERS AT BS1004, STRINGER S4R. THIS WAS FOUND AS A RESULT OF HFEC INSPECTION.SDR GAIA00620Skin · crackedDISCREPANCY: DURING ROUTINE INSPECTION AT FLIGHTSTAR AIRCRAFT SERVICES REPAIR STATION IN JAX IT WAS DISCOVERED THAT THERE WAS A CRACK AT THE SKIN LAP JOINT, LOWER FASTENER ROW AT FASTENERS AT BS 528, 543, 568, 609, 611, 630, 631, 632, 633, 645, 647, 649, AND 6SDR GAIA00619Skin · crackedDISCREPANCY: DURING ROUTINE INSPECTION AT FLIGHTSTAR AIRCRAFT SERVICES REPAIR STATION IN JAX IT WAS DISCOVERED THAT THERE WAS A CRACK AT THE FORWARD ENTRY DOOR LOWER HINGE CUT OUT ON THE EXTERIOR SKIN ONLY. REF N/R 1252.. CORRECTIVE ACTION: FABRICATED DOUBLERSDR GAIA00524Door · malfunctionedFLT 1729 - DEN-FWA - AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT GO PAST OFF, GEAR AND DOORS LIGHTS WERE ALL ILLUMINATED. CYCLED THE GEAR THREE TIMES AND THERE WAS NO CHARGE. THE AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. JACKED AIRCSDR RIVA0000026Skin · dentedPSM, THE NR 3 ENG NACELLE NOSE COWL IS DENTED BEYOND LIMITS AT NAC STA 63.5 AT THE 5 O''CLOCK POS. REPAIRED THE AREA BY INSTALL OF A FLUSH TYPE REPAIR. REMOVED THE DAMAGED AREA IAW SRM 54-30-3 FIG 2. FABRICATED THE FILLER, DOUBLER AND SHIMS IAW SRM 54-30-3 SDR 00392H.P. Bleed Valve · leakingDISCREPANCY: DURING CRUISE THE #3 STRUT OVERHEAD LIGHT ILLUMINATED. THE CREW COMPLIED WITH THE APPROPRIATE CHECKLISTS, AND LIGHT WENT OUT WHEN #3 ENGINE WAS RETURNED TO IDLE POSITION. A/C CONTINUED TO HSV AND LANDED WITHOUT FURTHER DIFFICULTIES. CORRECTIVE ACTSDR GAIA00391Clamp · looseFLT 1759 - IAH-MEM - DURING CRUISE, THE NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. THE CREW COMPLIED WITH THE APPROPRIATE CHECKLISTS, AND LIGHT WENT OUT WHEN NR 3 ENGINE WAS RETURNED TO THE IDLE POSITION. THE AIRCRAFT CONTINUED TO MEM AND LANDED WITHOUT ANY FURTSDR GAIA00389Skin · lightning strikeFLT 714 - TOL-STL - DURING CRUISE, THE AIRCRAFT ENCOUNTERED A LIGHTNING STRIKE. THE AIRCRAFT CONTINUED TO STL AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. THE LIGHTNING STRIKE INSPECTION REVEALED FOUR EACH RIVETS/SKIN DAMAGED ON THE RIGHT SIDE OF AIRCRAFT DUSDR GAIA00390B-Nut · looseFLT 1760 - FWA-IAH - DURING CRUISE, THE NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. THE CREW COMPLIED WITH THE APPROPRIATE CHECKLISTS, AND CONTINUED TO IAH AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. FOUND B-NUT LOOSE ON 13TH STAGE MODULATION VALVE. RESECURED LSDR RIVA0000013Regulator · activatedAFTER DEPARTURE FROM SFB, CREW FOUND OXYGEN WAS DEPLETED. AIRCRAFT RETURNED TO SFB WITHOUT INCIDENT. THE FLIGHT ENGINEERS REGULATOR SWITCH WAS FOUND TO BE IN THE ON POSITION. RETURNED THE FLIGHT ENGINEERS REGULTOR SWITCH TO THE OFF POSITION AND SERVICED THESDR RIVA0000012Starter · damagedWHILE EN ROUTE TO PIT, NUMBER 3 ENGINE START VALVE LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AS PER SUPPLEMENTARY PROCEDURES. THE AIRCRAFT CONTINUED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE STARTER TO BE DAMAGED. THE STARTER AND START VALVE WERSDR RIVA0000011Rib · crackedNR 5 SLAT LEADING EDGE RIBS (2 EACH) CRACKED AT SLAT STATION 61 AND 63. REPAIRED IAW BOEING SRM 57-50-3, FIGURE 9. FABRICATED AND INSTALLED DOUBLERS (2 EACH) FROM .032 CRES A1S1,321 ANNEALED CONDITION. DOUBLER AT SLAT STATION 63 INSTALLED WITH SHIM AND RADISDR RIVA0000010Seat Track · damagedTWO OBLONG (ELONGATED) HOLES IN SEAT TRACK, LOCATION BS 390 LBL 38.SDR RIVA0000009Fitting · corrodedDURING REPLACEMENT OF L1 DOOR PLATE GUIDE ASSEMBLY AND ARM ASSEMBLY, THE UPPER FUSELAGE SUPPORT FITTING FOR THE UPPER DOOR HINGE (BODY STATION 310, WATER LINE 260) WAS FOUND TO BE CORRODED. REPAIR BY REPLACEMENT OF UPGRADED PART (PART NUMBER 50-9327-5) IN ACCSDR GAIA0092Bulb · failedDURING ROUTINE MAINTENANCE AT CLT, IT WAS DISCOVERED THAT ONE EACH LAMP FOR THE EMERGENCY EXIT LIGHT AT THE L-1 DOOR HAD BURNED OUT. REMOVED AND REPLACED ONE EACH LAMP AT THE L-1 DOOR. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR RIVA0000007Angle · crackedNR 4 SLAT REAR LOWER ANGLE, WS 191 TO WS 198, CRACKED 7 INCHES ALONG PREVIOUS REPAIR. INSTALLED REPAIR DOCUMENTED IN BOEING SRM 51-40-3, FIG 1. REMOVED ANGLE IAW BSRM 51-30-2. FABRICATED REPAIR ANGLE USING .050 INCH 2024 T-3 ALUMINUM. FABRICATED REPAIR ANGSDR RIVA0000006Rib · crackedNR 4 SLAT, OTBD RIB WS 198 CRACKED, 1 INCH LONG. INSTALLED REPAIR DOCUMENTED IN BOEING SRM 51-40-3. CUT OUT DAMAGED AREA OF RIB. FABRICATED DOUBLER USING .050 INCH 2024 T-3 ALUMINUM. FABRICATED ANGLE USING .063 INCH 2024 T-3 ALUMINUM. APPLIED PROTECTIVE TSDR RIVA0000005Skin · gougedRIGHT OTBD T/E FOREFLAP HAD GOUGE IN L/E AT WS 550. INSTALLED REPAIR DOCUMENTED IN BOEING SRM 57-50-4, FIG 1. REMOVED DAMAGED AREA. FABRICATED DOUBLER FROM .050 INCH 2024 T-3 ALUMINUM. APPLIED PROTECTIVE TREATMENT IAW BSRM 51-10-2. INSTALLED DOUBLER. RESDR RIVA0000004Skin · dentedDENT IN LOWER SKIN OF LT OTBD AILERON AT WBL 540.2 INCHES BEHIND FRONT SPAR. INSTALLED FLUSH PATCH REPAIR DOCUMENTED IN THE BOEING SRM 57-50-5. REMOVED DAMAGED SECTION OF SKIN. FABRICATED DOUBLER AND FILLER FROM .020 INCH 7075 T-6 ALUM. APPLIED PROTECTIVE SDR RIVA0000003Rib · crackedDAMAGE TO RT WING OTBD AFT FLAP, OTBD CONTROL ROD ATTACH BRACKET AND L/E RIB AT WBL 464. REPAIRED RIB AND BRACKET BY REPLACEMENT. USED REPAIR DOCUMENTED IN BOEING SRM 57-50-4 FOR L/E SECTION REMOVED TO GAIN ACCESS. REMOVED L/E SKIN SECTION, FABRICATED DOUBLSDR RIVA0000002Rib · crackedNR 5 LEADING EDGE SLAT INBOARD RIB, AT ACUATOR ATTACHMENT WS 234 IS CRACKED. REPAIRED IAW BOEING SRM 57-50-3, FIGURE 9. FABRICATED DOUBLER FROM .050 INCH 2024-T3 ALUMINUM. APPLIED PROTECTIVE TREATMENT TO ALL PARTS AS REQUIRED. INSTALLED DOUBLER. REBALANCESDR GAIA0088Battery · dischargedDURING ROUTINE MAINTENANCE AT HNL, IT WAS DISCOVERED THAT THE EMERGENCY EXIT LIGHTS WOULD NOT RETAIN A CHARGE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERIES. OPERATIONAL CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA0039Door Frame · crackedDURING A B CHECK LEVEL INSPECTION AT DFW, IT WAS DISCOVERED THAT THE AFT BAGGAGE DOOR LOWER FORWARD FRAME AT BS 950E WAS CRACKED. REPAIRED CRACK IAW BOEING SERVICE BULLETIN 727-53A0199. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA99211ADuct · rupturedDURING CLIMB-OUT FROM TOL, HAD A NR 1 ENGINE FIRE WARNING. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO TOL. THE AIRCRAFT LANED WITHOUT FURTHER PROBLEMS. FOUND THE 8TH STAGE BLEED AIR SUPPLY DUCT RUPTURED. ALSO, FOUND A PIECE OF THE DUCT STUCK IN THE SDR 99ZZZX3447Wire · strippedDURING DAILY CHECK, SECTION OF EMERGENCY PATH LIGHTING WAS FOUND INOPERATIVE RESULTING IN A 30-MINUTE DELAY. A STRIPPED WIRE WAS FOUND IN THE EMERGENCY PATH LIGHTING. THE WIRE WAS REPAIRED AND THE OPERATIONAL CHECK WAS GOOD.SDR 99ZZZX3265Wire · failedDURING DAILY CHECK, SECTION OF EMERGENCY PATH LIGHTING WAS FOUND INOPERATIVE RESULTING IN A 30-MINUTE DELAY. A STRIPPED WIRE WAS FOUND IN THE EMERGENCY PATH LIGHTING. THE WIRE WAS REPAIRED AND THE OPERATIONAL CHECK WAS GOOD. (X)SDR 99ZZZX3266Battery · dischargedSJU - DELAY RESULTING FROM EMERGENCY TRACK LIGHTING AFT OF ROW 5 VERY DIM. CHARGED EMERGENCY TRACK LIGHTING BATTERY. OPERATIONAL CHECK GOOD. (X)SDR 99ZZZX2502Ring · crackedPRIOR TO B-CHECK, ENGINE RUN, MECHANIC NOTICED SMALL PIECE OF METAL MISSING FROM NR 1 ENGINE NOSE COWL ASSEMBLY MOUNT RING AT LOWER MOUNT BOLT. UPON FURTHER INSPECTION, MOUNT RING WAS FOUND CRACKED OUT AROUND 10 OF 23 MOUNT BOLTS. REMOVED NOSE COWL ASSY. ISDR GAIA9974O-Ring · deterioratedDURING BOS-TOL - FLT 715 - DURING DESCENT AT FL280, THE FLIGHT CREW NOTICED THAT THE NR 1 ENGINE WOULD ONLY PRODUCE PARTIAL POWER. THE FLIGHT CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN ON THE NR 1 ENGINE AND DECLARED AN EMERGENCY. THE AIRCRAFT CONTINUED SDR GAIA9973Connector · dirtyFLT 504 - DURING CLIMB-OUT FROM TOL, THE NR 5 SLAT INDICATE AS NOT RETRACED WHILE ALL OTHER TRAILING AND LEADING EDGE DEVICES WERE RETRACTED. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO TOL. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. CLEANED NR 5 SSDR GAIA9972Oil Tube · brokenFLT 504 - TOL - DURING CLIMB-OUT, HAD OIL PRESSURE ON NR 1 ENGINE DROP TO 5-10 PSI. PRECAUTIONARY SHUT DOWN NR 1 ENGINE. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO TOL. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. FOUND NR 1 BEARING PRESSURE TUBE BSDR GAIA9997Pitot Tube · cloggedAFTER TAKEOFF FROM AUS TO STL, FLIGHT 721, HAD THE CO-PILOTS AIRSPEED INDICATOR DECREASE 40 TO 50 KNOTS FROM THE CAPTAINS AIRSPEED INDICATOR. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO AUS. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. FOUND AN OBSTRSDR 99ZZZX3446Egt Indicator · failedAPPROXIMATELY TEN MINUTES AFTER TAKEOFF FROM EWR, NR 3 EGT GAUGE QUIT WORKING. AIRCRAFT RETURNED TO EWR. REMOVED AND REPLACED NR 3 EGT INDICATOR. OPERATIONAL CHECK SATISFACTORY.SDR GAIA9960APin · missingMCO - FLT 1726 - AFTER TAKEOFF, RETRACTED GEAR AND GEAR DOOR LIGHT REMAINED ON. RECYCLED GEAR AND LIGHT REMAINED ON. PROCEEDED TO MEM AND LANDING WAS SMOOTH. BRAKING WAS STARTED AT 80 KIS, RUMBLE WAS NOTICED IN THE AIRCRAFT. UNABLE TO STEER AIRCRAFT. AIRCSDR GAIA9956Battery · dischargedDURING ROUTINE MAINTENANCE WALK AROUND IN TOL, FOUND COCKPIT 'EMERGENCY EXIT' LIGHT BATTERY DEAD. REMOVED AND REPLACED COCKPIT 'EMERGENCY EXIT' LIGHT. OPERATIONAL CHECK GOOD. NO ADDITIONAL PROBLEMS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR GAIA9934Light · inoperativeON POSTFLIGHT, FOUND THE FORWARD COCKPIT EMEGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE FORWARD COCKPIT EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA98130Pump · leakingCAPTAIN REPORTED AIRCRAFT LOST 'B' SYSTEM HYDRAULIC QUANTITY 10 MINUTES FROM LANDING AT OAK. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. FOUND NR 1 HYDRAULIC PUMP LEAKING. REPLACED NR 1 HYD PUMP. (M)SDR 98ZZZX2710B Nut · looseAIRCRAFT DIVERTED INTO KFLL DUE LOSS OF A-SYSTEM HYDRAULIC FLUID: FOUND B-NUT NR 1 ENGINE MAIN HYD LINE LOOSE. TIGHTENED B-NUT. CHECKED CASE DRAIN FITTINGS. PRESSURE CHECKED SYSTEM. RELEASED AIRCRAFT.SDR 98ZZZX2546B-Nut · looseAIRCRAFT DIVERTED INTO KFLL. DUE LOSS OF A-SYSTEM HYDRAULIC FLUID, FOUND B-NUT NR 1 ENGINE MAIN HYDRAULIC LINE LOOSE. TIGHTENED B-NUT, CHECKED CASE DRAIN FITTINGS. PRESSURE CHECKED SYSTEM. RELEASE AIRCRAFT.SDR GAIA9819Stud · looseON DEPARTURE OUT OF TOL, RAPIDLY LOST OIL QTY NR 3 ENGINE DURING CLIMB-OUT, TEMPS AND PRESSURES OK. SHUT DOWN ENGINE AT 1.5 GALLONS REMAINING. ON POST FLIGHT FOUND STUD PULLED FROM OIL FILTER HOUSING. REPAIRED LOOSE STUD AND REMOVED AND REPLACED OIL FILTER SDR B4MR97031Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND LFT WING, O/B MID FLAP, L/E LWR SURFACE, CORROSION ON TWO AREAS. (REFERENCE: O/B ATTACHED FAIRING FWD AREA). REPAIRED IAW ENGINEERING SKETCH NR AIA/E/2587, APPROVED BY FAA FORM 8110-3 DATED 7-21-97 PN=7075-T6 0.125IN. SDR B4MR97030Angle · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND LEFT MLG WW, AFT BULKHEAD LWR CENTER AREA, CORROSION ON T-ANGLE. REMOVED CORROSION ON T-ANGLE, FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. REMOVED DAMAGED AREA, REPAIRED T-ANGLE IAW B727 SRM 51-40-4, 51-30-2 AND MSDR B4MR97029Structure · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND LT WING L/E AREA, NR 2 L/E FLAP STA 212 HAS SUPPORT ANGLE WEB CORRODED AND CORROSION AROUND ANCHOR NUTS. FOUND CORROSION TO BE OUT OF LIMITS IAW B727 SRM 57-20-1. REMOVED AND REPLACED ACCESS WEBBING PANEL, TOP COVESDR B4MR97028Floorbeam · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND STA 328 FLOORBEAM AT LBL 3 HAS CORROSION. REPAIRED FLOORBEAM IAW B727 SRM 53-10-8 FIG 3. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 110399.SDR B4MR97027Seat Track · wornDURING ROUTINE CPCP CHECK INSPECTION, FOUND FE SEAT TRACK IS WORN. REPLACED FE SEAT TRACK IAW B727 BOEING MM CHAPTER 25-10-81. CORROSION TASK CARD NUMBER C53-221-01. NON-ROUTINE TASK CARD NUMBER 110442.SDR B4MR97026Skin · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND TOP RT ELEVATOR ES92 AREA HAS SURFACE CORROSION OUT OF LIMITS. REPAIRED AND REPLACED A PIECE OF TOP SKIN IAW B727 SRM 55-20-3 FIG 2 PN=2024-T3 .032. CORROSION TASK CARD NUMBER C55-300-10. NON-ROUTINE TASK CARD NUMSDR B4MR97025Skin · corrosionDURING ROUTINE CPCP CHECK INSPECTION, FOUND FORWARD PIT FS 686 S26R TO 25R HAS SURFACE CORROSION ON INTERNAL SKIN. CORROSION OUT OF LIMITS IAW B727 SRM 53-30-1. REPAIRED IAW SRM 53-30-3 FIG 5 PN=2024-T3. CORROSION TASK CARD NUMBER C53-113-01. NON-ROUTINE TSDR B4MR97024Skin · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND RT MLG W/W OUTBD, ABOVE MLG BEAM, BETWEEN STA 930 AND 940 PRESSURE DECK SKIN AND FASTENERS HAVE CORROSION. REPAIRED AREA (CORROSION OUT OF LIMITS IAW B727 SRM 53-10-1) IAW SRM 53-10-9 FIG 4 PN=2024-T3. CORROSION TASDR B4MR97023Support · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND COCKPIT AREA, CO-PILOT SEAT BASE SUPPORT NEEDING ANTI CORROSION TREATMENT ON BOTH AFT ATTACH POINTS. REMOVED AND REPLACED CO-PILOT SEAT BASE SUPPORT IAW BOEING B727 MM CHAPTER 25-10-42. NEW BASE SUPPORT REQUIRED DUSDR B4MR97022Keel Beam · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND KEEL BEAM RT W/W UNDER APU ANGLE CORRODED TOP AND BOTTOM. OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER SRM 51-40-4 PN=7075-T6 OR 2X2X.150. CORROSION TASK CARD NUMBER C53-132-01. NON-ROUTINE TASK CARD NUMBER 108224
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