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 DHL2006749003Structure · crackedFUSELAGE STR 23L CRACKED AT STA 698. CUT OUT DAMAGE STRINGER DIM 13 INCHES IAW B727 SRM 53-10-3 FIG 1. FABBED STRINGER SECTION FROM P/N BAC1498-142 7075 -T62 PO 4002741 DIM 13 INCHES AND 2EA SPLICES FROM BAC 1498-132 PO 610190 DIM 12 INCHES EA IAW B727 SRM 5SDR DHL2006749002Skin · puncturedFOUND FUSELAGE SKIN IS PUNCTURED AT APPROX STA 700 AND STR 23L. OPENED SIDE WALL LOWER SECTION IAW B727 SRM 25-52-00. REMOVED EXISTING REPAIR IAW B727 SRM 51-30-2. CUT OUT DAMAGE AREA OF SKIN DIM 2 1/8" BY 2 IAW B727 SRM 53-30-3 FIG 3. FABBED DOUBLER USINGSDR DHL2006749001Skin · damagedFOUND FUSELAGE DAMAGE BS 700 AND STR 23. REF ITEM 6M THIS LG PG. INTERIM REPAIR PERFORMED EO AA91-1. INSTALLED INTERIM REPAIR IAW ED AA99-1. TRANSFERRED TO DMI 24642 IAW GMM 3.5 CAT I, PLACARD INST ID NR 34940.SDR 06FDEA0996Skin · damagedBS 430-480 SHIM BELOW S4L SKIN LAP HAS SEVERAL HOLES WITH LESS THAN 2D OR NO EDGE MARGIN. COMPLIED WITH FED EX EA 7-5330-98585.SDR 06FDEA0997Floorbeam · maint errorDOUBLE HOLE BS 400 RBL 12.5 WL 208. *S/D* REMOVED DAMAGED AREA ON FLOORBEAM UPPER CHORD 8.5 INCHES LONG BY 1 INCH WIDE. FABRICATED & INSTALLED REPAIR IAW SRM 51-30-2, 53-10-8.SDR 06FDEA0995Duct · crackedNR 2 ENGINE S-DUCT INNER SKIN HAS A SMALL CRACK AT THE 3 O'CLOCK POSITION WHERE THE S-DUCT MEETS THE INLET. REPAIRED NR 2 ENGINE "S" DUCT INNER SKIN AT 3 O'CLOCK POSITION IAW FED EX EA 7-7160- 96621.SDR 06FDEA0994Connector · damagedFIRE INDICATION ON NR 1 ENGINE, SHUTDOWN IN FLIGHT. BOTH BOTTLES DISCHARGED. LIGHT EXTINGUISHED WHEN PWR REDUCED, CAME BACK ON WHEN PWR APPLIED. REPLACED AFT A-LOOP DETECTOR CONNECTOR IAW 727-200 WDM 26-11-01 AND OP CHECKED IAW 727-200 MM 26-11-002-5, WITH SDR 06FDEA0993Unknown · crackedBS 638 STR 27 HAS A CRACK. REMOVED, REPAIRED DAMAGED STR. 27L BS 630-650 PER SRM 51-30-2, 53-10-3, 53-10-2, AND FED EX MM 51-20-021-7, 51-20-151-7.SDR 06FDEA0990Warning Horn · false activationMAIN CARGO SMOKE POSITION 3 ILLUMINATED INTERMITTANTLY ACCOMPANIED BY FIRE BELL AT 35,000 FT CONTINUED FOR APPROX 5 MIN AND QUIT JUST PRIOR TO LANDING. PTT GOT A FLASHING POSITION 3 AND STEADY ALL OTHERS. PERFORMED CARGO SMOKE DETECTOR TEST WITH NO FAULTS. SDR 06FDEA0988Skin · chafedRIGHT FUSELAGE IS CHAFED AT LANDING FACE FOR WING TO BODY FAIRING, FWD OF LANDING LIGHT. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FUSELAGE SKIN REPAIR FROM STA 720D TO 720E BETWEEN STRINGERS 18R TO 20R ALL IAW FX B727-200 SRM 53-30-3 FIG 14,SDR 06FDEA0986Beam · crackedCRACK AT LEFT SPOILER BEAM, I/B END. *S/D* REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED SAME IAW FED EX EA 7-5710- 96597.SDR 06FDEA0984Warning System · activatedON TAKEOFF ROLL LED INDICATIONS WENT AMBER THEN BACK TO GREEN, AT 45-60 KTS WENT AMBER. TAKEOFF REJECTED.SDR 06FDEA0975Fitting · corrodedWHILE WORKING WORK INSTRUCTION CARD 71C716-00 FOUND 2 FASTENER HOLES TO HAVE CORROSION AND TO BE OVERSIZED AT BS 1183 STR 27L AND 27R. *S/D* COMPLIED WITH FED EX EA 7-5310-96599.SDR 06FDEA0973Compressor · stalledDEPARTING 23R IND USING STD PWER, EXPERIENCED COMPRESSOR STALLS ON NR 2 ENGINE. REJECTED TAKEOFF AT 50KTS AND EXITED RWY. ENGINE GAUGES WERE NORMAL EXCEPT NR 2 EPR, WHICH BARELY CLIMBED WHEN POWER WAS APPLIED. LEARN FROM THE MISTAKES OF OTHERS. REMOVED ANDSDR 06FDEA0977Repair · unknownEXISTING REPAIR STA 720-745 STR 21L-22L IS IAW EXISTING FAA DATA. REPLACE EXISTING REPAIR PER SRM. FABRICATED AND INSTALLED NEW DOUBLER AND FILLER FROM 2024- T3 .063 BATCH 1022264 IAW SRM 53-30-3 FIG 2, 4 & 51-30-2, TREATED, PRIMED AND PAINTED IAW SRM 51-10SDR 06FDEA0959Web · crackedWHILE WORKING RUDDER TRIM ACTUATOR REPLACEMENT, FOUND VERTICAL FIN WEB CRACKED UNDER WASHER HOLDING THE PRESSURE SEAL FOR THE RTB CABLE AT FIN STA 87. *S/D* REPAIRED PER FEDEX EA 7-5330-96598.SDR 06FDEA0960Doubler · unknownREPLACE FWD AND AFT UPPER MCD CUTOUT DOUBLERS. FABRICATED, ALODINED AND PRIMERED UPPER MCD CUTOUT DOUBLER PER FED EX SRM 53- 30-2, 51-30-5.SDR 06FDEA0957Skin · corrodedAFT PIT STA 1050 RBL 10 SKIN IS CORRODED. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FUSELAGE SKIN REPAIR AT STA 1050 FROM RBL10 TO RBL 12 ALL IAW FX B727 SRM 53-30-3 FIG 3, 51-10-6, 51-30-2 AND 51-10-2.SDR 06FDEA0956Stringer · crackedSTRINGER AT FS 360 - 420 S18R IS CRACKED. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED STRINGER REPAIR AT STA 360 - 420 ON S18R ALL IAW FX B727 SRM 53-10-3 FIG 2 AND 51-10-2.SDR 06FDEA0955Stringer · corrodedSTA 950A TO 950B STRINGER 29 LEFT HAS CORROSION. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR AT STA 950A TO 950B ON STRINGER 29L ALL IAW FX SRZ SR27-53-023A FIG 7 AND B727 SRM 51-30-2, 51-10-2.SDR 06FDEA0939Web · corrodedCORROSION ON WEB BS 720E 4 RBL 66 WL 208. REMOVED AND REPLACED WEB AT BS 720E 4 RBL 66 WL 208 IAW SRM 51-30-2.SDR 06FDEA0938Crease Beam · misdrilledWHILE WORKING ON ATTACHING L-ANGLE FOUND CREASE BEAM WEB AT BS 720F 16, WL 208, LBL 64 WITH MISDRILLED HOLE. *S/D* REMOVED AND REPLACED CREASE BEAM WEB AT BS 720F TO 740, LBL 64, WL 208 IAW SRM 51-30-02.SDR 06FDEA0937Crease Beam · misdrilledWHILE WORKING ON ATTACHING L-ANGLE FOUND CREASE BEAM WEB AT BS 720F, WL 208, LBL 64 WITH MISDRILLED HOLE. *S/D* REMOVED AND REPLACED CREASE BEAM WEB AT BS 720E TO 720F, LBL 64, WL 208 IAW SRM 51-30-2.SDR 06FDEA0936Crease Beam · misdrilledWHILE WORKING ON ATTACHING L-ANGLE FOUND CREASE BEAM WEB AT BS 720E, WL 208, LBL 64 WITH MISSED DRILLED HOLE. *S/D* REMOVED AND REPLACED CREASE BEAM WEB BS 720D TO 720E, LBL 64, WL 208 IAW SRM 51-30-2.SDR 06FDEA0930Repair · misinstalledEXTERNAL UPPER FUSELAGE LEFT SIDE STA 393 WL 272 CIRCULAR DENT APPROX 1 X 1 INCH. REPAIR REQUIRES EVALUATION FOR MAJOR MINER DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. CIRCULAR DENT APPROX 1 X 1 INCH STA 393 WL 272 WAS NOT IAW SDR 06FDEA0933Frame · misdrilledBS 609 LBL 22 2EA FASTENER HOLES IN STUB FRAME HAVE LESS THAT 4D SPACING. FWD HOLE HAS LESS THAT 2D EDGE MARGIN. HOLE SIZES .312, SPACING .818, EDGE MARGIN .510. *S/D* COMPLIED WITH FED EX EA 7-5310-98576.SDR 06FDEA0932Sill · corrodedWEB AT FWD CARGO DOOR SILL BS 600, BELOW FLOOR SUPPORT HAS CORROSION. *S/D* REMOVED AND REPLACED WEB AT FWD CARGO DOOR SILL BS 600 BELOW FLOOR SUPPORT IAW SRM 51-30-2, 51-20-1.SDR 06FDEA0931Repair · misinstalledEXTERNAL DOUBLER REPAIR APPROX 7 X 6 INCH STA 1223 AFT OF PNEUMATIC SERVICE PANEL. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. *S/D* EVALUATED REPAIR DOUBLER AND FOUND TO BE NOT ACCORDSDR 06FDEA0929Stringer · tool damageREWORK REQUIRED DUE TO DRILL STARTS IN WEB OF STR AT STR CLIP INSTALLED AT BS 1090 STR 1. REPAIRED PER FED EX EA 7-5310-96616.SDR 06FDEA0928Stringer Clip · damagedSTRINGER CLIP AT BS 1090 AT STR 1 IS MISSING ALL FASTENERS COMMON TO FRAME. INSTALLED FASTENERS IN STR CLIP PER SRM 51-30-2.SDR 06FDEA0916Floorbeam · damagedFLOORBEAM BS 950A, HAS MECHANICAL DAMAGE AT WL 207, LBL 1 (AFT SIDE OF VERTICAL FLANGE). REPAIRED BS 950A FLOORBEAM, WL 207, LBL 1 PER FED EX EA 7-5310-98584.SDR 06FDEA0918Support Fitting · corrodedNLG LEFT UPPER HALF TRUNNION RACE SUPPORT FITTING HAS CORROSION AND GOUGED IN BORE. *S/D* LEFT NLG UPPER HALF TRUNNION RACE SUPPORT FITTING RE-WORKED ON OSS WORK ORDER 26594 IAW SRM 53-40-01.SDR 06FDEA0917Support Fitting · corrodedRIGHT NLG TRUNNION SUPPORT ASSY, UPPER AND LOWER FITTING BEARING RACE BORES HAVE CORROSION. *S/D* CORROSION RIGHT NLG UPPER AND LOWER TRUNNION FITTING BEARING RACES RE-WORKED ON OSS WORK ORDER 26594 IAW SRM 53-40-01.SDR 06FDEA0915Skin · gougedEXTERNAL LWR LOBE SKIN BS 460 TO 560 BETWEEN STR 23R & 25R, SKIN HAS NUMEROUS GOUGES. *S/D* ACCOMPLISHED FED EX EA 7-5330-98569.SDR 06FDEA0922Skin · misinstalledN01379 BS 451 STR 4L SKIN LAP HAS HOLES WITH LESS THAN 2D EDGE MARGIN AND LESS THAN 4D FASTENER SPACING. ** SD ** COMINGSDR 06FDEA0914Repair · misinstalledLOWER FWD CARGO COMP FLOOR FRAME REPAIR FUSELAGE STA 580 RBL 3. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. *S/D* EVALUATED FRAME REPAIR AT STR 580, RBL 3. REPAIR FOUND NOT IN ACCORDASDR 06FDEA0890Repair · noneREPAIR DOUBLER AT STA 370, STRINGER STR 18-L , REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR DOUBLER AT STA 370 STR 18-L WAS INSTALLED USING FAA APPROVED DATA. DOUBLER WAS REMOVED SDR 06FDEA0878Repair · noneFOUND REPAIR AT STA 990 STR 27R, REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 7-5310-27778. REPAIR CLASSIFIED AS MAJOR.SDR 06FDEA0877Repair · noneFOUND REPAIR LOCATED AT STA 700 STR 28L REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 7-5310-02879.SDR 06FDEA0876Repair · noneFOUND REPAIR LOCATED AT STA 1130 STR 5L, REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 7-5330-56270.SDR 06FDEA0875Repair · noneFOUND REPAIR LOCATED AT STA 630 STR 27L REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION, AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 5330-B27- 20619. REPAIR CLASSIFIED AS SDR 06FDEA0873Repair · noneFOUND REPAIR LOCATED AT STA 400 STR 15L REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 7-5330-70501. REPAIR IS CLASSIFIED AS MAJOR.SDR 06FDEA0872Repair · noneFOUND REPAIR LOCATED AT STA 380 STR 15L REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR ACCOMPLISHED USING FAA APPROVED DATA ON FEDEX EA 7-5330-70501. REPAIR IS CLASSIFIED AS MAJOR.SDR 06FDEA0871Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED ON UPPER RUDDER TRAILING EDGE WAS ACCOMPLISHED IAW SRM 51-40-9, FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, RESDR 06FDEA0863Frame · corrodedFRAME AT STA 950C 4 INCHES RT OF CENTER LINE IS CORRODED. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FRAME REPAIR AT STA 950C LBL 4 TO RBL 4 ALL IAW FX B727 SRM 53-10-4 FIG12,51-30-2,53-10-1, 53-10-2 AND 51-10-2.SDR 06FDEA0861Floorbeam · corrodedAFT PIT FLOORBEAM LOWER CHORD SEVERAL AREAS CORRODED BS 1070 AT LBL 26. REMOVED DAMAGE, FABRICATED, HEAT TREATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR TO STA BS 1070 BETWEEN RBL 54 AND LBL 26 ALL IAW FX SRZ SR27-53-034E REPAIR NR 8, B727 SRM'S 51-SDR 06FDEA0865Floorbeam · corrodedFWD PIT MAIN CABIN FLOORBEAM LOWER SIDE HAS CORROSION AROUND NUT PLATES STA 720 BETWEEN LBL 50 AND RBL 50. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR STA 720 FROM LBL 50 TO RBL 50 ALL IAW FX SRM DRAWING SR27-53-034.SDR 06FDEA0864Stringer · corrodedFWD PIT BS 700 AT STRINGER 28L CORROSION ON STRINGER AND WEB. CORRECTIVE ACTION: REMOVED DAMAGE,LOCATED, DRILLED AND INSTALLED NEW STRINGER AT STA 700 TO 720 AND S28L ALL IAW FX B727 SRM'S 53-10-3 FIG1,51-30-2 AND 53-10-1.SDR 06FDEA0862Skin · corrodedFUS SKIN AT FWD PIT STA 700-720A BETWEEN STRINGER 27L AND 28L IS CORRODED. REMOVED DAMAGE, FABRICATED, ALODINED , PRIMED AND INSTALLED FUS SKIN REPAIR STA 700-720A FROM STRINGER 27L TO 28L ALL IAW SRM'S 53-30-1 FIG1,53-30-3 FIG3,51-30-2 AND 51-10-2. SNRM N0SDR 06FDEA0860Skin · lightning strikeNOSE AREA FUSELAGE EXTERNAL SKIN HAS SEVERAL LIGHTNING STRIKES BETWEEN BS178 AND 203.8 BETWEEN STRINGERS 24 TO 26 LT. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED. FUS SKIN REPAIR STA 178 TO 203 BETWEEN STRINGERS 26LAND 24L ALL IAW FX B727 SRM'
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