Boeing 727-200
Service difficulty reports · 2,835
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 = '727200' 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 = '727200' 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 03FDEA02177Floorbeam · corrodedCORROSION FLOORBEAM HAS SEVERAL AREAS OF CORROSION STA 360 LBL 0 TO 10.SDR 03FDEA02172Door Frame · damagedFWD CARGO BAY, LWR DOOR CUTOUT THRESHOLD FRAME TOP FLANGE HAS 4 DAMAGED NUT PLATE HOLES. REPAIRED FLOOR BOARD BS 950F-1030, RBL 45-65, WL 208 BY REPLACING MISSING INSERTS PER FED EX DWG SRZ-25-005 REV E.SDR 03FDEA02180Actuator · malfunctionedNOSE GEAR DID NOT EXTEND ON 1ST TRY. RECYCLED GEAR AND IT CAME DOWN. JACKED NOSE GEAR PER 727-200 MM 07-11-000-2. REMOVED AND REPLACED NOSE GEAR ACTUATOR PER 727-200 MM 32-33-001-4. LUBRICATED ALL GEAR COMPONENTS. REMOVED AND REPLACED LANDING GEAR ACC WARSDR 03FDEA02170Stringer Clip · crackedINTERIOR FUSELAGE STRINGER CLIP IS CRACKED AT STR 4L, BS 783. REMOVED AND REPLACED STRINGER CLIP BS 783, STR 4L IAW SRM 51-30-02SDR 03FDEA02169Skin · bulgedN00325 BULGE IN LOWER FUSELAGE SKIN BETWEEN FASTENERS BS 704 STR 28L LBL 6. CUT OUT STR 28L BETWEEN B/S 700-720. FOUND SPLICE PIECE TO BE OUT OF LIMITS (CORRODED). SKIN WAS NOT AFFECTED BY CORROSION. DRILLED UP NEW STR SPLICE SECTION FROM BAC1498-144SDR 03FDEA02167Stringer · crackedVERTICAL FIN STR 8L AT FIN STA 157 IS CRACKED. REPAIRED CRACK IN STRINGE 8 LT AT FIN STA 157 PER SRM 55-30-4 FIG 1.SDR 03FDEA02165Floorbeam · corrodedN01305 CORROSION ON FLOORBEAM AT BS 480 LBL 45 TO RBL 45 UPPER AND LOWER SURFACE ** SD ** COMINGSDR 03FDEA02164Stringer Clip · crackedSTRINGER CLIP CRACKED, STR 6R, BS 950C. REMOVED AND REPLACED STRINGER CLIP AT BS 950C, STRINGER 6R IAW SRM 51-30-2.SDR 03FDEA02163Stringer Clip · crackedBS 720 STR 6 LT STRINGER CLIP IS CRACKED. REMOVED AND REPLACED STRINGER CLIP BS 720, STR 6L IAW SRM 51-30-02.SDR 03FDEA02162Stringer Clip · crackedSTRINGER CLIP CRACKED, STR 5L, BS 950E. REMOVED AND REPLACED STRINGER CLIP AT BS 950E, STR 5L IAW SRM 51-30-2SDR 03FDEA02161Stringer Clip · crackedSTRINGER CLIP CRACKED, STR 4L, BS 950C. REMOVED & REPLACED STRINGER CLIP AT BS 950C, STR 4L IAW SRM 51-30-2SDR 03FDEA02171Stringer Clip · crackedSTR 4 LT BS 720A STRINGER CLIP IS CRACKED.SDR 03FDEA02168Stringer · crackedVERTICAL FIN STR 8L AT FIN STA 180 IS CRACKED.SDR 03FDEA02166Stringer · crackedVERTICAL FIN STR 8L AT FIN STA 133 IS CRACKED ** SD ** COMINGSDR C8GA20030029Accessory Unit · defectiveDURING CLIMB OUT, A/C EXPERIENCED RUNAWAY STAB TRIM. TRIM SWITCHES WERE POSITIONED TO CUT OFF, THIS DISENGAGED PITCH CTRL PADDLE SWITCH TO AUTOPILOT. AC JERKED NOSE UP, BEGAN EXCESSIVE CLIMB OF RATE AT WHICH TIME AUTOPILOT WAS DISENGAGED. AOM CHECKLIST, MN STSDR 03FDEA02150Skin · gougedLOWER FUSELAGE, BS 1090, 1 INCH ABOVE AND 4 INCHES BELOW STR 24 RT, EXTERNAL SKIN IS DENTED, GOUGED AND POSSIBLY CRACKED. DAMAGE ON SKIN FOUND TO BE OUT OF LIMITS. REPAIRED SKIN IAW FED-EX EA 7-5330-55172.SDR 03FDEA02179Linkage · missingINFLIGHT TOTAL LOSS OF NR 1 ENGINE THROTTLE CONTROL. ENGINE NR 1 ACCELERATED TO 90 PERCENT N1 & N2, SUSPECT ZERO SPEED PROTECTION HAS ENGAGED. ENGINE SHUTDOWN IAW CHECKLIST. FOUND NR 1 ENG THROTTLE CONTROL LINKAGE AFT ROD-END BEARING MISSING. CAPT CONFIRMEDSDR 03FDEA02157Fuel Tank · corrodedFOUND CORROSION ON UPPER SURFACE OF WING CENTER TANK BS 825 RBL 12. REMOVED CORROSION ON UPPER SURFACE OF WING CENTER TANK AT BS 825, RBL 12 PER SRM 51-10-06. FOUND DAMAGE AREA TO BE OUT OF LIMITS PER SRM 53-10-1, FIG 1. REMOVED DAMAGE AND REPAIRED PER SSDR 03FDEA02156Intercostal · corrodedCORROSION ON INTERCOSTAL, BS 312-344, LBL 29, WL 208. REMOVED CORROSION ON INTERCOSTAL STA 312-344, LBL 29, WL 208. REMOVED .001 1X1 INCH FROM .075. IN LIMITS. REMOVED CORROSION ON SHIM STA 328-344, LBL 29, WL 208. REMOVED .013 1 X1 INCH FROM .100.SDR 03FDEA02155Stringer Clip · crackedSTRINGER CLIP CRACKED, STR 6L, BS 950C. REMOVED AND REPLACED STRINGER CLIP AT BS 950C, STR 6L IAW SRM 51-30-2.SDR 03FDEA02154Stringer Clip · crackedBS 720B STR 9 RT STR CLIP IS CRACKED. REMOVED CRACKED STR CLIP AT BS 720B STR 9 RT PER SRM 51-30-2. LOCATED, DRILLED, AND INSTALLED NEW STRINGER PER SRM 51-30-5, 51-30-6 AND 51-30-2.SDR 03FDEA02153Stringer Clip · crackedSTRINGER CLIP CRACKED, STR 4L, BS 950F. REMOVED CRACKED STRINGER CLIP BS 950F, STR 4L PER SRM 51-30-2. FABRICATED, LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED NEW STRINGER CLIP BS 950F, STR 4L PER SRM 51-20-1, 51-10-2, 51-30-2 AND FED EX MM 51-20-1SDR 03FDEA02152Stringer Clip · crackedSTRINGER CLIP CRACKED, STR 6R, BS 950F. REMOVED CRACKED STRINGER CLIP BS 950F, STR 6 RT PER SRM 51-30-2. FABRICATED, LOCATED, ALODINED, PRIMED, DRILLED AND INSTALLED NEW STRINGER CLIP BS 950F, STR. 6 RT PER SRM 51-20-1. NEW CLIP FABRICATED FROM .032 707SDR 03FDEA02151Frame · dentedFWD CARGO STA 520 STR 23L FRAME IS DENTED. REMOVED DAMAGE ON FRAME BS 520, STR 23L. FABRICATED FRAME DOUBLER FOR CUT OUT. ALODINED, PRIMED & INSTALLED IAW SRM 51-40-3 AND EA 7-5310-70600.SDR 03FDEA02149Frame · crackedCRACKED FRAME AT BS 640, RBL 9, WL 155.5. CUT OUT CRACK ON FRAME AT BS 640, RBL 9, WL 155.5. REMOVED 2 X 2 INCHES. FABRICATED REPAIR PARTS FROM 7075-T6 .063 LOT 516678. ALODINED, PRIMED AND INSTALLED IAW SRM 51-30- 2, 53-10-1, 51-40-3.SDR 03FDEA02159Transmitter · malfunctionedDESCENDING THRU FL190, HYDRAULIC SYSTEM -A- QUANTITY INDICATED ZERO (PRESSURE GOOD AT 3000 PSI). COMPLIED WITH QRH. AFTER 15 MINUTES AND BEING LEVEL AT 12,000 FOR OVER 5 MINUTES. HYD SYSTEM -A- QUANTITY SLOWLY BEGAN MOVING TO 6.0 GALLONS AND THEN 5.5 GALLONSDR 03FDEA02158Rib · crackedLT WING AFT SPAR, NR 4 SPOILER ACTUATOR INBOARD SUPPORT RIB IS CRACKED. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-30-2. RECEIVED NEW FABRICATED SUPPORT ANGLE P/N FX65-24608 -7, ON TRAVELER T2/385523. LOCATED & DRILLED NEW PART IAW SRM 51-20-1. INSTALLED NESDR 03FDEA02127Keelbeam · corrodedCORROSION AFT CARGO BAY LEFT KEELBEAM LWR O/B FLANGE BS 1000, STR 29L . FOUND CORRODED KEELBEAM OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED STR 29L KEELBEAM IAW FED EX EA 7-5330-55160.SDR 03FDEA02057Stringer · corrodedCORROSION (C53-113-01), IN STRINGER BS 1010-1030 STR 27 LT. FOUND CORROSION ON STRINGER BS 1010-1030, STR 27LT TO BE OUT OF LIMITS PER SRM 53- 10-1. REPAIRED STRINGER IAW SRM 53-10-3.SDR 03FDEA02056Stringer · corrodedCORROSION ON STRINGER BS 1166 STR 24 RT. REMOVED CORROSION & FOUND OUT OF LIMITS. REPAIRED STRINGER BS 1166, STRINGER 24 RT PER SRM 53-10-3 AND 53-10-1.SDR 03FDEA02051Frame · damagedWHILE WORKING FOUND UPPER FLANGE OF FRAME BS 1070 LBL 18 WL 150 TO BE DOUBLE HOLED. REMOVED DAMAGE ON FRQME QT BW 1070, LBL 18, WL 150 UPPER FLANGE. INSTALLED NEW FABRICATED DOUBLER FOR FRAME AT BS 1070, WL 150, LBL 18 IAW SRM 51-40-3.SDR 03FDEA02050Frame · damagedWHILE WORKING FOUND UPPER FLANGE OF FRAME BS 1090 LBL 18 WL 150 TO BE TRIPLE HOLED. REMOVED DAMAGE ON UPPER FLANGE OF FRAME BS 1090, LBL 18, WL 150. INSTALLED NEW FABRICATED DOUBLER FOR FRAME AT BS 1090, WL 150, LBL 18 IAW SRM 51-40-3.SDR 03FDEA02047Frame · corrodedCORROSION ON FRAME BS 1148 BETWEEN STR 25-26 LT. BLENDED CORROSION FROM FRMAE BS 1148 BETWEEN STR 25-26 LT. REMOVED .040 FROM ORIGINAL THICKNESS OF .065. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGE MATERIAL 1 X 2.5 INCH. FABRICATED AND INSTSDR 03FDEA02046Frame · corrodedCORROSION ON FRAME STA 540 RBL 5 WL 147. FRAME AT BS 540, RBL 5, WL 147 FOUND TO BE OUT OF LIMITS DUE TO CORROSION REMOVAL. REPAIRED FRAME SHEAR TIE PER SRM 53-10-1, 53-10-4 FIG 12.SDR 03FDEA02045Floorbeam · corrodedCORROSION ON BS 312 FLOORBEAM UPPER CHORD, LBL 19.5, WL 208. REMOVED CORROSION ON BS 312 FLOOR BEAM UPPER CHORD AT LBL 19.5 IN AREA OF 1 X 1 X .025 INCH MAX REMOVED. FOUND TO BE OUT OF LIMITS. FABRICATED THE REPAIR PART MADE FROM 7075-T6 0.063, AND SDR 03FDEA02049Floorbeam · corrodedCORROSION FLOORBEAM HAS SEVERAL AREAS OF CORROSION STA 380 RBL 45 TO 56.SDR 03FDEA02048Frame · damagedFRAME AT BS 950D BETWEEN STR 26-27 LT HAS HOLE IN UPPER FLANGE RADIUS.SDR 03FDEA02041Fitting · gougedWINGS BASIC- REWORK OF SLIGHT GOUGE IN L/E SLAT ACTUATOR FITTING. COMPLIED WITH ALL ASPECTS OF EA 7-5740-73855.SDR 03FDEA02037Crease Beam · corrodedCREASE BEAM WEB BS 740 TO BS 730F IS CORRODED. REMOVED CORROSION ON CREASE BEAMM WEB BS 740 TO 720F, LBL 65, WL 208. 1X2 INCH. MAXIMUM MATERIAL WAS .020. ORIGINAL THICKNESS .040. OUT OF LIMITS. CUT OUT DAMAGE. FABRICATED FILLER AND DOUBLER LOT 519SDR 03FDEA02036Frame · corrodedCORROSION ON FRAME SPLICE STA 500 RBL 26.5 WL 156. REMOVED CORROSION FWD CARGO ON FRAME SPLICE AT BS 500, RBL 26.5, WL 156 IN AREA OF 1 X1 X .020 INCH MAX REMOVED. FOUND TO BE OUT OF LIMITS. FABRICATED THE DOUBLER MADE FROM 7075-T6 0.071, AND INSTALSDR 03FDEA02039Frame · crackedCRACKED FRAME AT BS 640, RBL 9, WL 155.5. CUT OUT CRACK ON FRAME AT BS 640, RBL 9, WL 155.5. REMOVED 2X2 INCH. FABRICATED REPAIR PARTS FROM 7075-T6 .063 INCH, LOT 516678. ALODINED, PRIMED AND INSTALLED IAW SRM 51-30- 2, 53-10-1, 51-40-3. (CLOSED)SDR 03FDEA02038Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT BS 540, STR 28L. REMOVED CORROSION ON STRINGER CLIP AT B.S. 54O STR 28L. FOUND OUT OF LIMITS. REPLACED STRINGER CLIP PART 65-45313-6 ALL WORK DONE IAW SRM 51-30-2, SRM 53-10-1, SRM 51-30- 5, SRM 51-30-6.SDR XNOA1167Wire · chafedON TAXI OUT AFT LOWER BODY OVERHEAT ILLUMINATED. REPAIRED CHAFED WIRE AT LOWER BODY HEAT LOOP, STAIRWELL POS, IAW B727MM 26-14-0. OPS CHECK NORMAL.SDR 03FDEA01981Fitting · chafedCOMPLY WITH EA 7-5340-73853 FUSELAGE FITTINGS MAIN CARGO DOOR UPPER JAMB LIFT FITTING GOUGES. COMPLIED WITH EA7-5340-73853 DATED 11/20/03 FUSELAGE FITTINGS MAIN CARGO DOOR UPPER JAMB LIFT FITTING GOUGES.SDR 03FDEA01979Probe · contaminatedDURING T/O, NR 1 ENG INDICATED LOW N1 RPM (APPROX 80 PERCENT) WHEN STD EPR SET. ABORTED T/O AT APPROX 90 KTS, 138400 LBS, 600 FT PA, -3 DEGREES C. RAN ALL APPROPRIATE CHECKLISTS AND AFTER COORDINATION WITH GROUND CONTROL RAN UP NR 1 ENG. DURING RUN-UP NR 1 SDR 03FDEA01980Connector · contaminatedAFTER INITIAL TAKEOFF ON FLAP RETRACTION GOING FROM FLAPS 2 TO FLAPS 0. NR 4 LED SLAT WOULD NOT RETRACT. RETURNED TO PHL, HAD TO GO TO FLAPS 5 TO GET GREEN LIGHT AND NORMAL POSITION. FOUND MOISTURE IN NR 4 LEADING EDGE SLAT ACTUATOR CONNECTOR. CLEANED SAMESDR 03FDEA01973Thermostat · inoperativePASSING THROUGH 7500 FT ANTI ICE DUCT OVERHEAT NR 2 LIGHT ILLUMINATED. TEMP WAS FULL HOT 250 DEG C, THEN EXTINGUISHED SHORTLY AFTER (30 SEC) NR 2 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. DUCT OVERHEAT LIGHT ILLUMINATED ONCE AGAIN AFTER LANDING. REMOVED ANSDR 03FDEA01976Indicator · malfunctionedCAPT`S A/S INDICATOR FAILED AT 80 KNOTS. REJECTED THE T/O. ACCOMPLISHED RTO CHECK LIST ON TAXI BACK, CYCLED THE APP CIRCUIT BREAKER AND IT WORKED NORMALLY. REMOVED AND REPLACED CAPTAIN A/S INDICATOR AS PER 727-200 AMM 34-12-021-4. PERFORMED GROUND TEST AS SDR 03FDEA01958Detection Sys · faultyENGINE FIRE WARNING NR 1 ENGINE DURING CLIMBOUT. LIGHT & HORN INTERMITTENT AT FIRST, THEN BOTH CAME ON STEADY. AFTER EXECUTING QRH PROCEDURES AND DISCHARGING BOTH BOTTLES, FIRE WARNING AND HORN STAYED ON UNTIL SHORT FINAL, THEN WENT OUT FOR GOOD. INSPECTED SDR 03FDEA01959Actuator · failedON PUSHBACK MEM AFTER DISCONNECT WITH A PUMPS ON, L/E FLAPS REMAINED UNSAFE. CYCLED FLAPS 2-5 DEGREES WENT GREEN. CYCLED FLAPS BACK UP, UNSAFE WENT OUT. PASSING 10K UNSAFE L/E FLAPS RE-ILLUMINATED. CYCLED DOWN AND BACK LIGHT WENT OUT. PASSING 19K, UNSAFE
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