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 05FDEA01925Stringer Clip · crackedFUSELAGE UPPER LOBE, STRINGER CLIP IS CRACKED, BS 950C, STR 8R. REPLACED CRACKED STRINGER CLIP PER SRM 51-30-2.SDR 05FDEA01921Stringer Clip · crackedFUSELAGE UPPER LOBE STRINGER CLIP CRACKED BS 680 STR-5L. REMOVED FABRICATED AND INSTALLED STRINGER CLIP AT BS 680 STR 5L IAW SRM 51-20-1, 51- 30-02, 51-10-02.SDR PCSA708051Module · malfunctionedON DEPARTURE, CREW REPORTED STALL WARNING STICK SHAKER CAME ON AT ROTATION. CREW DUMPED FUEL, RETURNED AND LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUBLESHOT STALL WARNING SYSTEM. OPERATIONAL CHECK NORMAL IAW B-727 MM CH 34-18-01, UNABLE TO DUPLICATSDR 05FDEA01708Skin · damagedFUSELAGE EXTERNAL SKIN OF AFT AIRSTAIR, SECTION 48, AREA FROM LE TO 27 INCH AFT OF LE, LBL 21 TO RBL 21, HAS GRAVEL DAMAGE.SDR 05FDEA01665Skin · corrodedAFT CARGO CORROSION ON FUSELAGE SKIN STA 1010, STR 29L. OUT OF LIMITS AREA CUT OUT, INSTALLED SRM REPAIR TO THE SKIN AT STA. 1010, STR 29L, REF SRM 53-30-3 PAGE 14E-14O FIG 3ASDR 05FDEA01664Floorbeam · corrodedCORROSION ON FLOORBEAM LBL 10, BS 560. REPAIRED PER SRM 53-10-8.SDR 05FDEA01666Seat Track · corrodedSEAT TRACK LBL 24 HAS CORROSION FROM STA 344-480. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.SDR 05FDEA01649Intercostal · crackedINTERCOSTAL CRACKED STA 358, STR 16 LT. REPAIRED INTERCOSTAL PER SRM 51-40-2.SDR 05FDEA01648Skin · gougedFUSELAGE EXTERNAL SKIN GOUGED AT AFT AIRSTAIR CUTOUT, BS 1230, LBL 20. REPAIRED SKIN AT AFT AIR STAIR CUTOUT BS 1230, LBL 20 PER SRM 53-30-3.SDR PCSA6210501Oil System · leakingDURING CRUISE NR 3 ENGINE OIL TEMP WAS BETWEEN 125 & 130 DEG FOR 15 MINUTES. PERFORMED ALT PROCEDURES, RETARDED THROTTLE, DIDN'T HELP. SHUTDOWN NR 3 ENGINE, ENGINE WINDMILLED FOR 45 MIN. OIL PRESSURE STAYED ABOVE 25 PSI. DIVERTED & LANDED AT SJU. MX INSPESDR PCSA06080501Connector · dirtyFLIGHT 8113 TTPP/SVMC - AFTER DEPARTURE FROM TTPP, CREW REPORTED UNABLE TO RETRACT OUTBOARD FLAPS FROM 5 DEGREES. RETURNED AIRCRAFT TO TTPP USING THE SPLIT FLAP ALTERNATE PROCEDURE IAW AMERIJET 727 AIRCRAFT OPS MANUAL CHAPTER 5 PAGE 53 AND 54. AIRCRAFT LANDESDR 05FDEA01398Skin · deformedWHILE WORKING NOSE AREA DOUBLER FOUND SKIN DEFORMED ALONG LT SIDE. REPLACED DOUBLER PER FED-EX EA 7-5330-86293.SDR PCSA0519051Connector · looseFLIGHT 846 DURING CLIMB FROM KIN CREW REPORTED LEADING EDGE AMBER LIGHT CAME ON, CYCLED FLAPS TO 5 DEGREES AND BACK TO 0 DEGREES. LIGHT REMAINED ON, CONFIRMED WITH FLT ENGINEER FLAP SLAT ANNUNCIATOR PANEL. FOLLOWED INOPERATIVE L/E FLAP/SLATS ALTERNATE PROCEDSDR PCSA0518051Cover · leakingDURING CLIMB CREW REPORTED LOSS OF HYDRAULIC (A) SYSTEM. AIRCRAFT WAS DIVERTED AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND FEEL COMPUTER FILTER COVER LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED FEEL COMPUTER FILTER CAP AND O-RING IAW MM CH 20-10SDR 05FDEA01371Skin Panel · gougedCOMPLY WITH EA 7-5330-55484 FUSELAGE, PLATES AND SKIN GOUGE REPAIR AT BS 950E, STR 19R. COMPLIED WITH EA 7-5330-55484 FUSELAGE, PLATES AND SKIN GOUGE REPAIR AT BS 950E, STR 19R. THIS IS A MAJOR REPAIR.SDR 05FDEA01360Fairing · crackedLT WING LOWER T/E FLAP TRACK SKATE FAIRING BEHIND MLG STRUT IS CRACKED. REMOVED AND REPLACED SKATE FAIRING IAW SRM 51-30-2.SDR 05FDEA01359Floorbeam · damagedFLOORBEAM LBL 7-RBL 40 UPPER CHORD REQUIRES MAJOR REPAIR. REMOVED AND REPLACED UPPER T-CHORD IAW SRZ 53-034E REPAIR NR 7.SDR 05FDEA01358Insulation · damagedEQUIPMENT AND FURNISHINGS INSULATION BLANKETS. PARTIAL REPLACEMENT STA 360-1183, MAIN CABIN COMPARTMENT. COMPLIED WITH EA 7-2580-81692.SDR 05FDEA01349Tire · defectiveRTO DUE TO VIBRATION ON T/O ROLL. MINOR VIBRATION AT 60 KTS INCREASING IN INTENSIVE TO MODERATE VIBRATION AS SPEED INCREASED RTO AT 110 KTS. RTO AT 0815Z WITH 49 MIN COOL TIME. AFTER DEBRIEF WITH FLIGHT CREW IT WAS DETERMINED THAT VIBRATION WAS WORSE WHEN YSDR 05FDEA01289Retainer · corrodedLT NOSE GEAR AFT DOOR SEAL RETAINER CORRODED. REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-30-2.SDR 05FDEA01288Insulation · damagedCOMPLY WITH EA 7-2580-81691 "EQUIPMENT AND FURNISHINGS. INSULATION BLANKETS, PARTIAL REPLACEMENT, STA 178-294, LOWER SECTION 41 INCH.SDR 05FDEA01259Doubler · corrodedFUSELAGE STA 740 BULKHEAD SUPPORT DOUBLER CORROSION. COMPLIED WITH EA 7-5310-55482 FUSELAGE STA 740 BULKHEAD SUPPORT DOUBLER CORROSION AT MAE. THIS IS A MAJOR REPAIR.SDR PCSA5030501Cdu · shortedFLIGHT 711 MIA TO MEX, DURING CRUISE LOWER CARGO FIRE LIGHT AND BELL CAME ON INDICATING A AFT FIRE. FUEL WAS DUMPED, AIRCRAFT DIVERTED TO MID AND LANDED WITH NO FURTHER INCIDENT. UPON INSPECTION OF THE AFT CARGO COMPARTMENT ON THE GROUND NO FIRE WAS OBSERVEDSDR 05FDEA01160Skin · dentedBS 720 15 TO 20, CREASED DENT BETWEEN STRINGER 18L-19L. REPAIRED SKIN AT BS 720 PLUS 15 TO PLUS 20, STR 18L - 19L PER SRM 53-30-3.SDR 05FDEA01170Shear Tie · corrodedCORROSION ON SHEAR TIE LOWER SURFACE AT SKIN BS 1130 BETWEEN STR 29L AND STR 30. REPLACED SHEAR TIE PER SRM 53-10-1.SDR 05FDEA01168Skin · tornFORWARD ENTRY DOOR LOWER HINGE ARM AND SNUBBER CUTOUT SKIN IS TORN. REPAIRED FORWARD ENTRY DOOR LOWER HINGE ARM CUTOUT PER SRM 51-40-2.SDR 05FDEA01159Bracket · corrodedCORROSION C-53-100-01 AT LEFT MAIN WHEEL WELL, BS 919 WL 189 LBL 65 UPPER SURFACE. WORK TO BE ACCOMPLISHED ON CUSTOMER ID N00428.SDR 05FDEA01169Frame · corrodedCORROSION ON FRAME BS 700 LBL 13 WL 148. REPAIRED BS 700 FRAME, LBL 13, WL 148 PER SRM 53-10-4.SDR 05FDEA01158Structure · corrodedCORROSION AT LEFT MAIN WHEEL WELL, BS 928-932 WL 189 LBL 65 UPPER SURFACE. REPLACED STRINGER 18A PER SRM 51-40-3.SDR 05FDEA01144Roller · damagedDURING LANDING ROLLOUT, AFT AIRSTAIR EXTENDED. REMOVED AND REPLACED AFT RT SIDE ROLLER BECAUSE ROLLER DOES NOT TURN. REPLACED MAIN BEARING AS PER 727-200 M/M 52-62-001-1, T/S DOOR OPS CKED OK. OK FOR FLT.SDR 05FDEA01102Seat Track · damagedSEAT TRACK STA 244 TO 480 RBL 45, HAS EXISTING BLEND REPAIRS AND AN EXISTING SPLICE REPAIR AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED SEAT TRACK IAW SRM 51-30-2. FAB'D SEAT TRACK ON TRAVELER NR T5/510065. LOCATED AND DRILLED IAW SRM 53-10-5 FIG 3. SDR 05FDEA01060Seat Track · damagedSEAT TRACK, STA 344 - 480 HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002, LBL 45. REMOVED SEAT TRACK STA 344 - 480 LBL 45 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK PER TRAVELER NR T5/510063, BATCH NR 888841, PO NR MST0017183. LOCATESDR 05FDEA01059Seat Track · damagedSEAT TRACK, STA 344, LBL 24 HAS EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED SEAT TRACK STA 344 - 480 IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK PER TRAVELER NRT5/510064, BATCH NR 888841, P.O. NR MST0017183. LOCATED AND DRILLEDSDR 05FDEA01058Strap · chafedMAIN DECK CARGO, AT STA 1030 AND 1050 STR 6L, LINER FRAME ASSY HAS CHAFED INTO THE FRAME STRAP'S AND HARDWARE. GOUGE OUT OF LIMITS IAW BOEING SRM 53-10-1. REMOVED AND REPLACED STRAP IAW BOEING SRM 51-30-2.SDR CA050426003Valve · fouled(CAN) AFTER DEPARTING, THE CREW OBSERVED AN INDICATION OF ANTI-ICE SELECT FAILURE ON NR1 ENGINE. THE CREW RETURNED TO DEPARTURE, WHERE MAINTENANCE FOUND INTERNAL PARTS FROM THE THERMOSTATIC VALVE FOR THE NR1 LT NOSE COWL ANTI-ICE HAD FOULED THE ANTI-ICE VALVE.SDR 05FDEA00847Skin · crackedCRACKED EXTERNAL SKIN FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED CRACK PER FED-EX EA 7-5330-86273.SDR 05FDEA00832Skin · dentedDENT IN EXTERNAL FUSELAGE SKIN AT BS 1345 BY LEFT AFT CORNER OF AIRSTAIR CUT OUT. REPAIRED DENT PER SRM 54-30-3.SDR 05FDEA00779Housing · gougedNR 3 LOWER CARGO DOOR, HANDLE HOUSING GOUGED BY HANDLE STUD. REMOVED AND REPLACED #3 LWR CARGO DOOR HANDLE PER SRM 51-30-02.SDR 05FDEA00735Shear Web · corrodedCORROSION IN SHEAR WEB BS 1166 LBL 29-33 WL 208.SDR 05FDEA00736Support · corrodedLWR FUSELAGE, BS 740 R A/C BAY RBL 10, CORROSION EMANATING FROM LWR CHORD AND BULKHEAD. REPAIRED BS470 LOWER CHORD PER FED-EX EA 7-5310-86268.SDR 05FDEA00691Skin · gougedEXTERNAL FUSELAGE SKIN GOUGED AT NR 3 CARGO DOOR CUTOUT, BS 1096 AT STR 24R. REPAIRED GOUGE PER FED-EX EA. 7-5330-86272.SDR 05FDEA00629Seat Track · corrodedSEAT TRACK, STA. 344 - 480, LBL 24 HAS CORROSION AND EXISTING BLEND REPAIRS AND REQUIRES REPLACEMENT PER 7-5340-7-5002. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2 - MAT ID BAC 1520-792 IAW SRM 51-10-2 FIG 7. NEW EXTRUSION SCALLOPED ON TRAV NR T5/501341. SDR 05FDEA00520Adc · malfunctionedREJECTED TAKEOFF. REMOVED AND REPLACED AIR DATA COMPUTER IAW MM 34-12-011-4. GRD CK OK. A/C DOWN GRADED TO NOT CAT II. A/P NR 1 CK CAT II A/P NR 2 CK CAT II PREMATURE REMOVAL/INSTALLATION OFF MFG HG480B13.SDR 05FDEA00519Adc · malfunctionedREJECTED TO AT 80 KTS. RAN RTO CHECKLIST. NO AIRSPEED ON CAPT'S AIRSPEED INDICATOR. REMOVED AND REPLACED AIR DATA COMPUTER IAW MM 34-12-011-4. A/C DOWN GRADED TO NOT CAT II. A/P NR 1 CK CAT II A/P NR 2 CK CAT II. R/I FROM FACT PREMATURE REMOVAL/INSTALLSDR 05FDEA00318Module · failedWHEN GEAR HANDLE IS UP, RIGHT GEAR SAFE GREEN LIGHT WILL NOT TEST. REPLACED BULBS CYCLED CBS. SWAPPED RIGHT GEAR AND LEFT GEAR LIGHTS IN LEFT POSITION, RIGHT LIGHT WORKED IN RIGHT POSITION, LEFT LIGHT DID NOT WORK. CK'D CONTINUITY THROUGH WARN LIGHT PUSH TOSDR 05FDEA00280Skin Panel · corrodedOVERWING BOX, TANK TOP, HAS CORROSION AT BODY STATION 840 RIGHT BUTT LINE 12.0. REPAIRED OVERWING BOX FUEL TANK, STATION 840 AT RIGHT BUTT LINE 12.0 IAW FEDEX EA 7-5730-83992, WINGS-UPPER SKIN PANEL, CENTER TANK CORROSION-REPAIR.SDR CA050203005Cylinder · intermittent(CAN) NLG FAILED TO EXTEND ON APPROACH, THEN RE-CYCLED AND EXTENDED NORMALLY. NOSE GEAR JACKED, NOSE GEAR TRUNION GREASED AND GEAR RETRACTED AND EXTENDED 4 TIMES WITH NO FAULTS. AC WAS DISPATCHED WITH NO FURTHER FAULTS. QA GROUNDED THE AC DUE TO 2 OTHER EVENSDR CA050119003Switch · intermittent(CAN) ON APPROACH, LANDING GEAR CYCLED DOWN FOR LANDING. THE NOSE LANDING GEAR RED INDICATOR STAYED ILLUMINATED AND NO GREEN INDICATION WAS SEEN. GEAR WAS RE-CYCLED AND THE GEAR WAS EXTENDED WITH PROPER INDICATION. MAINTENANCE LUBED THE NOSE GEAR AND JACKED THSDR CA050105013Actuator · separated(CAN) ON APPROACH, THE CREW OBSERVED 'A' (HYDRAULIC) SYSTEM DEPLETION. SYSTEM DESELECTED, NORMAL LANDING CARRIED OUT. THE NOSE LANDING GEAR DOWN LOCK ACTUATOR SEPARATED FROM THE AIRFRAME MOUNT AND HAD DAMAGED THE HYDRAULIC LINES.SDR CA041216008Transmitter · sticking(CAN) DURING INITIAL CLIMBOUT, FLAPS CYCLED FROM 5 DEG. TO 2 DEG. CREW NOTICED THAT LT OUTBOARD FLAPS WERE INDICATING 5 DEG. & RT OUTBOARD FLAPS WERE INDICATING 3 DEG. CAUSING AN ASSYMETRY SPLIT. CREW HAD TO DUMP FUEL TO LAND WITHIN LANDING WEIGHT. CREW ACCOMP
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