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 07FDEA01502Connector · damagedNR 1 ENG FIRE DETECTION A LOOP INOP. MEL 03APR07 00:03 YOW ACN RELEASED FOR SERVICE PER MEL/CDL: 26-06-B. REMOVABLE ON P6 AREA, APU START PANEL, L/E ANNUNC. PANEL, GEN. FAULT ANNUNC. PANEL. REMOVED RELAY R730, DEPINNED PIN 9 FROM D5220J, DEPINNED PINS 6SDR 07FDEA01483Control Valve · failedS/O REPERTED HEARING A SLIGHT POP PASSING 2000FT AFTER RIGHT PACK WAS TURNED ON.NORMAL INDICATION RIGHT PACK MATCHED LEFT PACK TEMP BUT AIR MIX VALVE STAYED COLD ON RIGHT PACK.CABIN STARTED A HIGHER THAN NORMAL CLIMB 71500 FT/MIN IN MAN PRESSURIZATION WITSDR 07FDEA01062Frame · damagedMAIN DECK BODY, FRAME WEB AND SHEAR TIE HAVE 2 EA SHORT PITCH (0.25 INCH) MISDRILLED FASTENER HOLES BS 640, STR 5R. REMOVED DAMAGE FROM WEB, FABRICATED AND INSTALLED REPAIR AND NEW SHEAR TIE. TREATED AND PRIMED REPAIR PARTS REF EA 7-5310-107003.SDR 07FDEA00130Engine · failedNR 2 ENGINE FAILED DURING CLIMB-OUT AT APPROX 1500 FT ABOVE GROUND. NOTED HIGH EGT (AROUND 780 C), EPR 0, N1 AND N2 WINDMILLING. OIL QTY 3 GALS ENGINE FAILED WITH A LOUD BANG AND SPARKS REPORTED TRAILING AIRCRAFT BY TOWER. VISUAL INSPECTION OF ENGINE REVEASDR 06FDEA04305Beam · crackedNR 3 CARGO DOOR, LWR BEAM CRACKED FWD END. REPAIRED IAW EA 7-5230-106835 PT1 REF WRI 52-30/8690.SDR 06FDEA03941Depressor · damagedAFT NR 2 CARGO DOOR LWR FWD CORNER SEAL DEPRESSOR DAMAGED. REMOVED AND REPLACED AFT NO. 2 CARGO DOOR LWR FWD SEAL DEPRESSOR IAW SRM 51- 30-5.SDR 06FDEA03819Flap Track · corrodedNR 2 FLAP TRACK, AFT MOUNT HOLE IS CORRODED. REMOVED AND REPLACED NR 2 FLAP TRACK IAW FED EX W/C 27X5706-03.SDR 06FDEA03818Skin · corrodedCORROSION ON WING LOWER SKIN SURFACE, AT NR 2 AFT FLAP TRACK MOUNT. REMOVED CORROSION ON WING LWR SURFACE AT NR 2 FLAP TRACK MOUNT AND REPAIRED IAW FED EX EA 7-5710-100598.SDR 06FDEA03817Skin · gougedWHILE WORKING CUSTOMER CARD NR N00224, FOUND OUT OF LIMITS GOUGE IN EXTERIOR SKIN BS 538 1.5 INCH BELOW STR 25 RT. REMOVED DAMAGE IN EXTERNAL SKIN BS 538 BELOW STR 25R AND REPAIRED IAW SRM 53-30-3 FIG 1.SDR 06FDEA03798Indicator · inoperativeLT MAIN GEAR INDICATOR NOT WORKING. INSTALLED NEW LIGHT ASSEMBLY PER SMP, P/N 10-61803-49. LIGHT OPERATION CHECKS GOOD.SDR 06FDEA03797Fire Warning · activatedDURING CLIMBOUT PASSING 5000 FEET MSL,AFTER SETTING CLIMB POWER NR 2 ENGINE FIRE LIGHT AND FIRE BELL CAME ON. BELL WAS SILENCED. NR 2 ENGINE SHUTDOWN WITH START LEVER, LIGHT WENT OUT AFTER PULLING NR 2 ENG FIRE HANDLE. FIRE BOTTLES WERE NOT DISCHARGED. REMSDR 06FDEA03794Frame · damagedFWD CARGO COMPARTMENT, DAMAGE TO STA 560 FRAME BETWEEN STR 22L AND 25L. REPAIRED FRAME IAW SRM 51-40-3.SDR 06FDEA03791Frame · damagedL/H INTERIOR FUSELAGE, FRAME REPAIR STA. 930 STRINGER 5L, REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF THE REPAIR IS IN ACCORDANCE WITH FAA APPROVED DATA. REPAIRED FRAME AT BS 930, STR 5L PER SRM 51-40-3.SDR 06FDEA03620Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER TEE CORRODED TOP SIDE BS 620 LBL 10. REMOVED DAMAGED UPPER TEE IAW B 727 SRM 53-10-8 FIG. 3. FABRICATED AND INSTALLED REPAIR PARTS IAW B 727 SRM 53-10-8 FIG. 3.SDR 06FDEA03599Skin · chafedINTERIOR CABIN, MCD CUTOUT RESTRAINT WEB SKIN IS CHAFED AT BS 639, WL 295, LBL 24. EVALUATED CHAFED AREA ON MCD CUTOUT RESTRAINT WEB SKIN BS 639, WL 295. REMOVED DAMAGED AREA AND FABRICATED REPAIR PARTS FOR WEB AND ALODINE, PRIMED AND INSTALLED AT BS 639 WLSDR 06FDEA03597Skin · chafedINTERIOR CABIN, MCD CUTOUT RESTRAINT WEB SKIN IS CHAFED AT BS 636, WL 289. EVALUATED CHAFFED AREA ON MCD RESTRAINT WEB SKIN AT BS 636 WL 289 FOUND WEB SKIN TO BE OUT OF LIMITS. REMOVED DAMAGED AREA AND FABRICATED REPAIR PARTS AND ALODINED, PRIMED AND INSTALSDR 06FDEA03391Stringer Clip · crackedUPPER LOBE INTERIOR - STRINGER CLIP CRACKED STA 950F - STR 3L. COMING REPLACED CRACKED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA03390Stringer Clip · crackedUPPER LOBE INTERIOR - STRINGER CLIP CRACKED STA 950B - STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA03389Stringer Clip · crackedFWD CARGO BAY STRINGER CLIP CRACKED STA 560 STR 23L REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA03388Stringer Clip · crackedUPPER LOBE INTERIOR - STRINGER CLIP CRACKED STA 950C - S9R. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA03387Stringer · dentedFWD CARGO BAY DENT IN STRINGER STA 517 STR 23R. REPRAIRED DENTED STRINGER IAW SRM 53-10-3 FIG 2.SDR 06FDEA03386Skin · unknownEXISTING EXTERNAL DOUBLER REPAIR APPROX. 5.5" X 5.5" ON LT NR 2 DOOR LOWER SURFACE. (DOT 23) REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED PER FAA APPROVED DATA. REPARIED L-2 IAW FAA APPROVED DATA SRM 52-00-3.SDR 06FDEA03382Shear Web · misdrilledWHILE WORKING N00648 FOUND NUMEROUS DOUBLE HOLES IN SHEAR WEB BS 1130-1176, RBL 25-45, WL 208. REMOVED, FABRICATED AND INSTALLED SHEAR WEB IAW SRM 51-30-02.SDR 06FDEA03381Window · damagedUPON REMOVAL OF F/O'S NR 1 WINDOW, FOUND UPPER O/B FASTENER HOLE TO BE ELONGATED. FOUND HOLE AT UPPER O/B CORNER OF F/O'S NR 1 WINDOW TO BE OUT OF LIMITS. REPAIRED AREA AS PER FED-EX EA 7-5330-100586. MAJOR REPAIR.SDR 06FDEA03380Skin · misrepairedEXISTING EXTERNAL DOUBLER REPAIR ON PNEMUATIC GROUND SERVICE CONNECTION AFT LT CUT OUT. (DOT 16) REPAIR REQUIRES EVALUATION FOR MAJOR.MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. UPON INVESTIGATION FOUND REPAIR NOT TO BSDR 06FDEA03257Floorbeam · corrodedCORROSION AFT CARGO BAY FLOORBEAM LWR SECTION BS 1070, RBL 41-51, WL 201 REMOVED CORROSION FROM LWR CHORD BS 1070 RBL 41-51. FOUND BLENDED AREAS TO BE WITHIN LIMITS PER SRM 53-10-1, 51-10-2.SDR 06FDEA03136Skin · damagedN01183 EXISTING EXTERNAL DOUBLER REPAIR APPROX 5 INCH X 10 INCH AT STA. 1155, BETWEEN RT STRINGER 29-30 (DOT NR 22) REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPLACED EXISTING EXTERNALSDR 06FDEA03135Frame · dentedAFT CARGO BAY FRAME DENTED AT BS 1070 BETWEEN STR 26L AND 27L UPPER SURFACE. CUT OUT DAMAGE ON FRAME AT BS 1070 BETWEEN STR 26L & 27L LOWER SURFACE AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3.SDR 06FDEA03130Indicator · inoperativeRTO FOR INOP NR 2 EPR GAUGE MAX SPEED WAS 70 KTS. EPR INDICATION WAS GOOD ON HIGH POWER RUNUP.SDR 06FDEA03131Indicator · inoperativeDURING RUNUP FOR T/O WITH INOP EPR GAUGE NEITHER N1 OR EPR WOULD GET APLC CALCULATED PARAMETERS. REJECTED T/O CALCULATED NR 2 ENG. EPR WAS 2.18 ACHIEVED ONLY 2.03 EPR. CALCULATED N1 WAS 100.6 ONLY ACHIEVED 97.0 N1. ENGINE NOT MAKING ENOUGH POWER.SDR 06FDEA3000Skin · chafedTHE RT HORIZONTAL NR 5 BALANCE BAY UPPER SKIN PANEL IS CHAFED AT THE TE OF THE STIFFENER OB END. REMOVED AND REPLACED SKIN PANEL PER FED EX EA 7-5510-100575.SDR 06FDEA2997Floorbeam · gougedFUSELAGE INTERIOR FLOOR STRUCTURE, BS 328 LBL 45 WL 208, FLOORBEAM GOUGED. REPAIRED DAMAGED FLOOR BEAM PER FED EX EA 7-5310-100573.SDR 06FDEA2996Support Fitting · gougedGOUGES IN MAIN CARGO DOOR FORWARD ACTUATOR SUPPORT FITTING JUST BELOW UPPER ATTACH POINT OF AFT REACTION LINK. REPAIRED DAMAGED ACTUATOR SUPPORT FITTING PER FEDEX EA 7-5230-100572.SDR C8GA20060011Generator · malfunctionedFLT 717 FROM STL TO TOL. ON TAKEOFF ROLL, NR 2 GENERATOR TRIPPED OFF LINE AND UNDER VOLTAGE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS. PLACED NR 2 GENERATOR/CSD ON MEL 24-1. AIRCRAFT RETURNED TO SERVICE. ON 8/17/06, COULD NOT DUPLICATE DISCREPANCY. SDR 06FDEA2989Floorbeam · gougedN01216 FUSELAGE INTERIOR FLOOR STRUCTURE BS 1110 RBL 2 TO 22 WL 208 FLOORBEAM UPPER SURFACE GOUGED. REPARIED FLOOR BEAM PER FED EX EA 7-5310-100571.SDR 06FDEA2990Plate · misdrilledN01369 FUSELAGE INTERIOR FLOOR STRUCTURE BS 720D LBL 21 TOP SURFACE OF FLOORBEAM NUT PLATE HOLES MISDRILLED. REPARIED MISS DRILLED HOLES PER FED EX EA 7-5310-100570.SDR 06FDEA2968Motor · failedAFTER TAKEOFF WITH GEAR UP DURING FLAP RETRACTION, HYD SYSTEM-A BEGAN DECREASING TOWARD ZERO. RAN CHECK LIST AND LEAK DIDN'T STOP. INSTALLED NEW OUTBD FLAP HYD PUMP PER M/M 27-51-062-4. REPLACED NR 1 AND NR 2 ENG CASE DRAIN FILTERS PER M/M 29-11-041-2, NO CSDR 06FDEA2964Support Beam · crackedRIGHT WING - UPPER I/B MOST FIXED T/E PANEL/HUD LINE SUPPORT BEAM (RUNNING ALONG THE FWD SIDE OF THE MLG BEAM) CRACKED AT I/B END LOWER CHORD, APROX 26 INCHES I/B OF FWD MLG TRUNNION BEARING. REPAIRED RT WING UPPER I/B MOST FIXED T/E PANEL HYD LINE SUPPORT BESDR 06FDEA2962Bushing · galledN01113, NR 2 FLAP TRACK, BUSHING GALLED IN IB BOLT HOLE AT FWD ATTACH POINT IN REAR SPAR. REPAIRED BUSHING NR2 FLAP TRACK IB BOLT HOLE AT FWD ATTACH POINT IN REAR SPAR IAW EA 7-5710-100565.SDR 06FDEA2918Floorbeam · corrodedCORROSION (C53-224-01(2) BS 950 FLOORBEAM UPPER TEE EMANATING FROM UNDER NUTPLATES RBL10 AND 27 WL 208. REPARIED CORROSION ON BS 950 FLOORBEAM RBL 10 AND 27 WL 208 PER FED EX EA 7-5310- 100568.SDR 06FDEA2920Skin · dentedEXTERIOR SKIN HAS DENT JUST BELOW FWD ENTRY DOOR UPR HINGE CUTOUT. REPAIRED DENT IN EXTERIOR SKIN JUST BELOW FWD ENTRY DOOR UPPER HINGE CUTOUT IAW EA NR 7-5330-100564.SDR 06FDEA2921Door · dentedN00870 DENT ON FWD ENTRY DOOR ON IB WEB LIGHTNING HOLE AT BS 335 STR 14L ** SD ** COMING. REPAIRED DENT ON FWD ENTRY DOOR ON IB WEB LIGHTING HOLE AT BS 335, STER 14L IAW, SRM 51-40-2.SDR 06FDEA2922Door · dentedDENT ON FWD ENTRY DOOR ON IB WEB AFT EDGE AT 346 STR 13L. REPAIRED DENT ON FWD ENTRY DOOR ON IB WEB AFT EDGE AT 346 STR 13L IAW SRM 51-40-2.SDR 06FDEA2925Stringer Clip · corrodedWHILE ACCOMPLISHING NR N01259, FOUND SURFACE CORROSION ON STRINGER CLIP, AT BS 720A, STR 2R. REMOVED AND REPLACED STRINGER CLIP AT BS 720A STR 2R IAW SRM 51-30-2.SDR 06FDEA2926Stringer Clip · corrodedWHILE ACCOMPLISHING NR N01259, FOUND SURFACE CORROSION ON STRINGER CLIP, AT BS 720A, STR 3R. REMOVED AND REPLACED STRINGER CLIP AT BS 720A STR 3R IAW SRM 51-30-2.SDR 06FDEA2927Stringer Clip · corrodedWHILE ACCOMPLISHING NR N01259 FOUND SURFACE CORROSION ON STRINGER CLIP AT BS 720A, STR 4R. REMOVED AND REPLACED STRINGER CLIP AT BS 720A STR 4R IAW SRM 51-30-2.SDR 06FDEA2928Stringer Clip · corrodedN01429 WHILE ACCOMPLISHING NR N01259, FOUND SURFACE CORROSION ON STINGER CLIP, AT BS 720A, STR 1. REMOVED AND REPLACED STRINGER CLIP AT BS 720A STR 1 IAW SRM 51-30-2 AND 51-30-5.SDR 06FDEA2924Compressor · stalledAS WE APPLIED T/O POWER (STD POWERS) HEARD A LOUD BANG (COMPRESSOR STALL) AND REJECTED T/O BEFORE T/O POWER WAS SET. MAX SPEED 20KTS WIND 12KT X-WIND. SAT CONFIRMED NR 2 ENGINE COMPRESSOR STALL. C/W AMM 71-00-000-6 3.B. CENTER ENG COMPRESSOR STALL INSPESDR 06FDEA2923Pressure Switch · corrodedIN LEVEL FLIGHT AT 16,000 W/ 6000 NR OF FUEL IN NR 2 TANK THE RT AFT FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED. NO CB'S WERE OUT. TROUBLESHOT SYSTEM CHECKED WIRING TO PRESSURE SW. WIRING CKS OK. READ PRESSURE SW WITH PUMP ON AND OFF. SW STAYS CLOSED.SDR 06FDEA2911Floorbeam · damagedEXISTING FLOORBEAM REPAIR AT STA 344 ON MAIN CARGO DECK LBL 40 TO RBL 15. REPAIR REQURIES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED UPPER FLOORBEAM CHORD IAW SRM 53-10-1, 53-30-2
Back to Boeing 727-200