Boeing 727-233
Service difficulty reports · 3,034
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 = '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 98FDEA00064Frame · dentedNR 0508 FWD CARGO, BELT FRAME AT BS 600L DENTED JUST ABOVE STR 23L. REMOVED DAMAGED AREA OF FRAME AND REPAIRED WITH TYPICAL FORMED SECTION REPAIR PER SRM 51-40-3 PG 1, FIG 1.SDR 98FDEA00060Frame · dentedNR 0507 LOWER FWD CARGO COMPARTMENT BS 520 FUSE FRAME DENTED AT STRINGER 22L TO STR 24L. REMOVED DAMAGED SECTION OF FUSE FRAME. INSTALLED REPAIR DOUBLER PER AARD SRM 53-10-07-3 PG (ES0 11697).SDR 98FDEA00053Floorbeam · corrodedNR 0682, WORK CARD NR 72C237-02, BS 1070, RBL 60 TO LBL 24, LOWER FWD FLANGE CORRODED OF FLOORBEAM. CUT OUT CORROSION DAMAGE. INSTALLED FLOORBEAM REPAIR DOUBLER PER SRM 53-10-8.SDR 98FDEA00051Frame · dentedFWD CARGO STATION 500 AT STRINGER 23 LT HAS DENTED FRAME. NR 0330 LOWER FWD CARGO LT SIDE BS 500 LT BELLFRAME DENTED AT STR 24 LT. REMOVED DAMAGED AREA OF BELT FRAME STRINGER 23 TO 25 LT USING .25 DRILL FOR CORNER RADIUS. FABRICATED REPAIR FROM SHOP MANUFACSDR 98FDEA00050Frame · dentedFWD CARGO BS 700 FRAME DENTED BETWEEN STRINGER 23 LT TO STR 25 LT. REMOVED DAMAGED AREA OF BELLFRAME 10 LONG USING .25 DRILL AT ENDS TO MAINTAIN .25 RADIUS. FABRICATED FROM PANEL (P/N EY74) 7075-T6 X .063 THICK AND INSTALLED DOUBLER PER SRM 53-10-07-5 (AARD)SDR 98FDEA00046Connector · corroded98-0030 - AFTER TAKEOFF GEAR UP: RED NOSE GEAR LIGHT REILLUMINATED AFTER HANDLE PLACED TO OFF. RED TABS, NO HELP. RED LIGHT COMES ON AFTER DELAY, NOT IMMEDIATELY WHEN PLACING HANDLE TO OFF. REMOVED AND REPLACED NOSE GEAR LOCK SWITCH S96 AND NOSE LANDING GESDR 98FDEA00052Frame · dentedFORWARD CARGO AT BS 680 LT FRAME DENTED BETWEEN STRINGER 22 LT AND 25 LT. REMOVED 13 DAMAGED SECTION USING .25 RADII ON RELIEF AREAS. FABRICATED AND INSTALLED DOUBLER OF .063 THICK 7075-T6 MATERIAL (P/N 563886) 24 LONG AND INSTALLED REPAIR IAW SRM 53-10-04 PSDR 98FDEA00045Control Module · malfunctioned98-0029 NOSEGEAR UNSAFE, LANDING GEAR HANDLE UP DOOR LIGHTS OUT. REPLACED LANDING GEAR ACCESSORY CONTROL MODULE PER MAINTENANCE MANUAL 32-09-121 PAGE 401 TEST PER 32-09-122 PARAGRAPH 6A, PAGE 505.SDR 98FDEA00043Connector · corrodedNOSE GEAR UNSAFE LIGHT (RED) WITH LANDING GEAR HANDLE UP. ALL DOOR LIGHTS OUT. (CYCLED GEAR AND PROBLEM REMAINS, RED NOSE GEAR LIGHT ON) NOTE: NORMAL GEAR DOWN, NORMAL HYDRAULICS. AFTER 45 MINUTES, GREEN NOSE GEAR LIGHT ALSO ILLUMINATED AT THE SAME TIME, BSDR 98FDEA00021B-Loop · inoperativeNR 2 ENGINE FIRE DETECTION LIGHT ILLUMINATED IN FLIGHT ACCOMPLISHED RED TAB PROCEDURES AND LIGHT REMAINED ON. GOOD FIRE PROTECTION VERIFIED THROUGH RED TABS AND MINIMUM EQUIPMENT LIST (WARNING, FIRE WARNING TEST GOOD). IDENTIFY B-LOOP INOPERATIVE NR 2 ENGINESDR 98FDEA00014Air Data Comp · failed98-0011 - ON CLIMB-OUT (APPROX 2000FT) CAPTAIN LOST AIRSPEED, ALTIMETER, GPWS. SUSPECTED NR 1 AIR DATA COMPUTER FAILURE. ALL CIRCUIT BREAKERS CHECK, NONE TRIPPED. RED TABS COMPLIED WITH. REMOVED AND REPLACED NR 1 AIR DATA COMPUTER. PERFORMED LOW LEVEL LEASDR 98FDEA00013Air Data Comp · failed98-0010 - NR 1 AIR DATA COMPUTER CIRCUIT BREAKER TRIPPED ON CLIMB-OUT, EFFECTING CAPTAIN'S AIRSPEED, ALTIMETER, GPWS. RESET CIRCUIT BREAKER TRIPPED AGAIN. REMOVED AND REPLACED NR 1 AIR DATA COMPUTER. SYSTEM OPERATIONAL AND LEAK CHECKS GOOD.SDR 98FDEA00008Air Data Comp · failedAIR DATA COMPUTER NR 1 CIRCUIT BREAKER POPPED ON TAKEOFF ROLL, CONTINUED TO TROUBLESHOOT PROBLEM IN AIR. CIRCUIT BREAKER WOULD NOT RESET. RETURNED TO SDF FOR MAINTENANCE TO WORK. REMOVED AND REPLACED AIR DATA COMPUTER PER MAINTENANCE MANUAL 34-12-0 PAGES 8 SDR 98FDEA00003Fire Loop · wornCREW VERBALLY REPORTED, ENGINE NR 3 FIRE LOOP-B, WITH FAULT LIGHT ON AND BELL/FIRE LIGHTS INTERMITTENTLY ACTUATING DURING FLIGHT. TROUBLESHOT B-LOOP AND FOUND ON ENG NR 3 FIREWALL FIRE DETECTION ELEMENT FORWARD CONNECTOR (D1498) CERAMIC INSULATOR WORN, CAUSINSDR AALA980013Wire · brokenIAH - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT FLOOR LIGHTS IN CABIN NOT OPERATING PROPERLY. REPAIRED BROKEN EMERGENCY EXIT FLOOR LIGHT WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)SDR 97FDEA00901Bulb · failedON CLIMBOUT, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. CHECK LIST WAS RUN. SOURCE OF OVERHEAT APPEARED TO BE NR 2 ENGINE INLET AND COWL ANTI-ICE SYSTEM. CHECKED ALL FIRE LOOPS, FOUND NO PROBLEMS. CLOSED UP AFT AIRSTAIRS, RAN BOTH PACKS TO HEAT UP AIR SDR CA971216068Pump · leaking(CAN) LOW PRESSURE INDICATION ON "B" HYDRAULIC SYSTEM. SYSTEM ISOLATED. AIRCRAFT LANDED. "O" RING, "B" PUMP PRESSURE ADAPTER REPLACED.SDR 97FDEA00833Position Ind · malfunctionedDURING FLAP RETRACTION AT 2 DEGREE ON CLIMBOUT, THE NR 4 RIGHT INBD FLAP DID NOT RETRACT. THE POSITION TEST SELECTOR INDICATED THE SAME. THE LEADING EDGE FLAPS POSITION IND LIGHTS WERE AMBER. PROCEEDED WITH RED TAB CHECK LIST AND MADE A NORMAL LANDING. REMSDR CA971113070Spacer Casing · failed(CAN) THE AIRCRAFT SUFFERED A COMPLETE LOSS OF POWER ON NR NR3 ENGINE DURING CLIMB-OUT. INVESTIGATION FOUND COMPRESSOR DAMAGE CAUSED BY THE INGESTION OF FAILED SECTIONS OF A SPACER CASING BETWEEN THE INLET GUIDE VANE CASE AND THE FIRST STAGE COMPRESSOR.SDR CA971113069Airspeed Indictr · failed(CAN) NR 2 AIR SPEED INDICATOR NOT OPERATING ON TAKEOFF. REPLACED.SDR CA971113074Pump · sheared shaft(CAN) NR 1 HYDRAULIC SYSTEM WOULD NOT PRESSURIZE AFTER START-UP. SHAFT SHEARED. REPLACED. PART TC: 1,831.SDR CA971028001Indicator · error(CAN) AIR SPEED INDICATOR (ASI) INDICATED 20 KNOTS VARIANCE FROM THE NR1 POSITION ASI, REPLACED.SDR 97FDEA00749Frame · dentedNR 0572, LWR AFT CARGO, DENT IN FRAME 1010 ABOVE STR 25R, CUT OUT DAMAGE. INSTALLED REPAIR PER SRM 53-10-4.SDR 97FDEA00740Chord · crackedCRACK IN FWD LWR FLANGE OF 2ND CHORD FWD OF RT WING REAR SPAR, INSIDE FUEL CELL AT WS 686.5. INSTALLED DOUBLER PER BOEING SB NR 727-57A159.SDR 97FDEA00739Chord · mismanufacturedRT WING, WS 686.5, AFT SIDE OF 2ND CHORD, FWD OF REAR SPAR HAS AREA WHERE TOO MUCH MATERIAL (TAK). REMOVED NEXT TO DOUBLE FLUSH RIVET. BLENDED OUT AREA PER SRM 51-10-1 PG 2 AND PER SB 727 57A159. ALODINED AND PRIMED PER M/M 51-20-1. INSTALLED REPAIR PER EASDR CA971113073Fuel Contrl Unit · malfunction(CAN) COMMENCING TAKEOFF ROLL, NR 2 ENGINE DECELERATED TO IDLE AND HAD NO THRUST LEVER RESPONSE. THE TAKEOFF WAS REJECTED AND THE AIRCRAFT RETURNED TO BLOCKS. MAINTENANCE FOUND NO FAULT. THE FUEL CONTROL UNIT AND THE ENGINE DRIVEN FUEL PUMP WERE REPLACED, ASSDR 97FDEA00750Seat Track · corrodedNR 0643 GEN NR 72C237-02 BS 1015, LBL 25 SEAT TRACK HAS CORROSION BETWEEN LUGS AND ON TOP OF LUGS. REMOVED AND REPLACED OLD SEAT TRACK WITH NEW ONE PER SRM 51-10-1.SDR 97FDEA00707Fuel Pump · malfunctionAFTER T/O, THE NR 1 CSD RISE TEMP WAS PEGGED OFF SCALE HIGH. THEN NOTICED NR 1 CSD LO PRESS LIGHT FLICK EVERY 5-15 SEC. NR 1 GEN OUTPUT NORM BUSSES WERE IN PARALLEL OPER. THEN NR 1 ENG ROLL BK AND BEGAN TO SURGE. DISCONNECTED NR 1 CSD JUST AS WE BEGAN TO RSDR 97FDEA00700Skin · damagedNR 1 CARGO DOOR CUTOUT BS 600 FUSELAGE SKIN, DOUBLER AND TRIPLER DAMAGED AT LWR CUTOUT. *S/D* INSTALLED DOUBLERS AND FILLER IN CARGO DOOR CUTOUT PER EA 75-330-29236 DATED 10-03-97.SDR 97FDEA00681Line · failedHYDRAULIC LOSS SYSTEM-A UPON GEAR RETRACTION. PRESSURE 0 ENGINE LOW PRESSURE LIGHT INITIALLY ILLUMINATED, ONLY PRESSURE WAS 3000. HYDRAULIC QUANTITY WENT FROM 0 TO 1.2, ENGINE 1 PUMP LOW PRESSURE LIGHT EXTINGUISHED FOR 10 SEC THEN HYDRAULIC QUANTITY WENT TO SDR 97FDEA00679Seal · failedON INITIAL CLIMBOUT NR 3 OIL LOW PRESSURE LIGHT ILLUMINATED. OIL PRESSURE READ 30 PSI AND DECREASING, OIL QUANTITY READ 0, OIL TEMPERATURE PEGGED HOT. SHUT DOWN ENGINE PER RED TAB PROCEDURES. WINDMILLED ENGINE FOR 13 MINUTES. OIL TEMPERATURE GREATER THAN 1SDR 97FDEA00671Light · looseNOSE GEAR GREEN LIGHT WAS INTERMITTENT. FOUND LOOSE LIGHT ASSEMBLY. TIGHTENED SOCKET AND RELAMPED, OK FOR SERVICE.SDR 97FDEA00652Sensing Element · malfunction97-0178 4 MINUTES 30 SECONDS AFTER SWITCHING BLEEDS AT FLIGHT LEVEL 180 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. BLEED SWITCHED BACK (NR 1 BACK ON, NR 2 OFF) AND LIGHT WENT OUT AFTER 4 MINUTES.RAN ALL 3 ENGINE PER JET RUN HANDBOOK AND COULD NOT DUPLICATE PRSDR 97FDEA00646Duct · leakedWITHIN 5 MINUTES OF SWITCHING OVER TO NR 2 ENGINE BLEED FOR NR 1 PACK LOWER AFT BODY OVERHEAT LIGHT CAME ON. LIGHT EXTINGUISHED WITHIN 30 SECONDS OF PLACING NR 2 BLEED SWITCH BACK OFF. RAN NR 1 AND NR 2 ENGINES TO POWER. COULD NOT DUPLICATE PROBLEM. LEAK CSDR 97FDEA00599Clamp · failedON CLIMBOUT, APPROXIMATELY 5 MINUTES AFTER CLOSING NR 1 BLEED AND OPENING NR 2 BLEED AT 18,000 FT LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. INITIATED CHECKLIST. AFTER SWITCHING TO NR 1 BLEED, LIGHT EXTINGUISHED. NOTED L-PACK AT 145 DEG C. PARTIALLY OPENEDSDR 97FDEA00596Overheat Light · wrong bulbLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED 5 MINUTES AFTER SWITCHING LEFT AIR CONDITIONING PACK FROM NR 1 TO NR 2 ENGINE. CHECKLIST COMPLIED WITH LIGHT WENT OUT AFTER CLOSING NR 1 START LEVER. RAN ALL 3 ENGINES WITH ALL BLEEDS OPEN AND BOTH PACKS ON COULD NOTSDR 97FDEA00595Duct · leakingLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED APPROX 5 MINS AFTER SWAPPING BLEEDS FROM NR 1 TO NR 2 ON THE ALTIMETERS CHECKLIST. RAN THE LOWER AFT BODY OVERHEAT LIGHT CHECKLIST AND THE LIGHT EXTINGUISHED AFTER SWAPPING BLEEDS BACK TO NR 1. CONTINUED FLIGHT WITH SDR 97FDEA00548Bellframe · dentedNR 0747, NR 0798 71C209-02 - FWD CARGO BS 500, STR 19-25 RT: 11 DENTS ON TOP SIDE OF BELLFRAME. INSTALLED DOUBLERS BS 500 RT PER SRM 51-40-3.SDR 97FDEA00549Bellframe · bentNR 0544 71C70902 - LOWER AFT CARGO COMP, FS 970 BELLFRAME INNER FLANGE BENT OUTWARD BETWEEN STR 25 AND 26 LEFT. REMOVED DAMAGED DOUBLER PER SRM 51-40-3. INSTALLED DOUBLER PER SRM 51-40-30.SDR 97FDEA00533Overheat Light · illuminatedSHORTLY AFTER SWITCHING BLEEDS FOR THE RIGHT PACK FROM THE NR 3 ENGINE TO THE NR 2 ENGINE DURING CLIMB ABOVE FLIGHT LEVEL 180 THE LOWER AFT BODY OVERHEAT WARN LIGHT ILLUM. WE PERFORMED THE STEPS AS PER THE EMERGENCY CK LIST PROC FOR THE LWR AFT BODY OVERHEAT.SDR 97FDEA00531Circuit Breaker · trippedON TAKEOFF ROLL, CAPTAINS AIR SPEED AND ALTIMETER FAILED. AFTER AIRCRAFT WAS LOADED IN RAIN SHOWERS. NR 1 AIR DATA COMPUTER CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER AND RAN OPERATIONAL CHECK PER MAINTENANCE MANUAL 34-12-0 PAGE 509, OPERATIONAL CHECK GOSDR CA970820018Fire Wire · faulty(CAN) ON TAKEOFF ROLL CREW OBSERVED A FIRE INDICATION ON NR1 ENGINE. BOTH BOTTLES FIRED, AIRCRAFT RETURNED TO BLOCKS. NO EVIDENCE OF FIRE DETECTED. BOTTLES REPLACED. PYLON FIRE WIRE REPLACED AS PRECAUTION.SDR 97FDEA00550Bellframe · dentedNR 0504 71C205-02 FWD CARGO BS 680, STR 21-25 RT, 2 DENTS IN TOP LEG OF BELLFRAME. CUT OUT DAMAGED AREA OF BELLFRAME PER SRM 53-10-4. INSTALLED REPAIR PER SRM 51-40-3.SDR 97FDEA00547Bellframe · dentedNR 0741 71C209-02 - FWD CARGO BS 560, STR 22-25 LT 8 DENTS IN TOP SURFACE OF BELLFRAME. CUT OUT DAMAGED SECTION OF BELLFRAME PER SRM 53-10-4. INSTALLED BELLFRAME REPAIR PER SRM 53-40-4.SDR 97FDEA00545Frame · corrodedNR 0310 71C709-02 - LOWER AFT CARGO COMPT NR 2 CARGO DOOR CUTOUT AFT LOWER CORNER SEVERE CORROSION AFFECTING 1.5 BY 1 AREA OF AFT DOOR FRAME AT FS 990 BETWEEN STRINGER 26 AND 27 RT. REMOVED CORROSION PER SRM 51-10-6. TREATED AND PRIMED AREA. INSTALLED ANGLESDR 97FDEA00510Doubler · crackedNR 0727 W/C 72C235-02 - STR 15L CRACKED AT END STA 720B + 5. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-3 FIG 5.SDR 97FDEA00509Doubler · damagedNR 0732 72C235-02 - STR 15L CHANNEL GOUGED AT STA 680 BLENDED OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-3 PAGE 5 FIG 3.SDR 97FDEA00508Stringer · corrodedNR 0114, NR0280 71C209-02 - CORROSION STR 27 RT, BS 684-687 CORRODED, BLENDED BEYOND LIMITS FOR REMOVAL. REMOVED CORRODED SECTION, SPLICED IN NEW STRINGER SECTION PE153-10-3 SRM.SDR 97FDEA00557Bellframe · dentedNR 0741 71C209-02 - FWD CARGO BS 560, STR 22-25 LEFT, 8 DENTS IN TOP SURFACE OF BELLFRAME. INSTALL BELLFRAME REPAIR PER SRM 51-40-3.SDR 97FDEA00556Bellframe · dentedNR 0328 71C209-02 - FWD CARGO BS 700, STR 22-25 LEFT, 7 DENTS IN UPPER LEG OF BELLFRAME. INSTALLED REPAIR PER SRM 51-40-3.
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