Boeing 727-225
Service difficulty reports · 4,226
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 = '727225' 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 = '727225' 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 08FDEA02574Seat Track · corrodedCABIN SEAT TRACK AT STA 910 - STA 914, LBL 31, WL 208 IS CORRODED REMOVED SEAT TRACK, VERIFIY MATERIAL ID AS BAC1520-792 7178T651 ATAG NR A20604, P/O 1039090. FABRICATED SEAT TRACK, ALODINED, PRIMED AND INSTALLED IAW:BAC1520-792 REV B AND IPB 53-42-00 AND SRMSDR 08FDEA02572Channel · crackedNLG W/W AFT BULKHEAD STA 351.2, CRACK ON DOWN LOCK ACTUATOR MOUNT U-CHANNEL. COMING OUT OF UPPER LEFT FASTENER HOLE. REMOVED DOWN LOCK ACTUATOR MOUNT U-CHANNEL, DRILLED UP NEW CHANNEL P/N 69-19122-2, AND INSTALLED. REF DWG 69-18194 AND SRM 51-30-02 PG 1-10 SDR 08FDEA02571Channel · crackedDOT 7 AFT PIT, FLOOR SUPPORT ATTACH ANGLE MISDRILLED AND CRACKED ON LOWER SURFACE AS MARKED, LOCATED AT STA 1070 5 INCH, LBL 18 INCH. REPLACED ATTACH ANGLE REF SRM 51-30-02 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02570Crease Beam · crackedFUSELAGE CREASE BEAM WEB CRACKED, STR17L, BS-640-660 FABRICATED NEW CREASE BEAM WEB PER SAMPLE AND BOEING DWG NR 65-58536. TRANSFERED NEW FASTENER HOLES REF, SRM 51-30-2, PG 1-10. TREATED AND PRIMED WEB, REF: SRM 51-10-2, PG 1-2. WEB BE INSTALLED ON NR N007SDR 08FDEA02569Panel · crackedPANEL RACK: FWD ENTRY DOOR LINER, SLIDE PACK PANEL CRACKED AT CUT OUTS. REMOVED AND REPLACED DOOR LINER SLIDE PAN REF SRM 51-30-02 PG 13-14. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02568Support Angle · crackedRT WING LWR FIXED T/E PANEL BELOW NR 14 SPOILER ACTUATOR. FLAP TRACK SUPPORT ANGLE CRACKED. REMOVED AND MANUFACTURED NEW O/B ANGLE FOR NR 8 FLAP TRACK SUPPORT BRACKET REF BOEING DRAWING 69-22894-9 AND SRM 51-20-1. INSTALLED NEW MANUFACTURED ANGLE ON BRACKETSDR 08FDEA02567Hinge · corrodedNLG STRUT WELL CUT OUT LT AFT DR SEAL RETAINER IS CORRODED BS 282-334, LBL 17, WL 150 (MRK). REMOVED OLD SEAL RETAINER, REF:SRM 51-30-02. INSTALLED NEW SEAL RETAINER, REF: SRM 51-30-02, P-1. THIS IS CLASSIFIED AS A MINOR REPAIR. THREE HINGE BRACKETS REMOVSDR 08FDEA02552Frame · chafedDOT 5, AFT PIT, STA 1148, FRAME WORN FROM HYDRAULIC LINES CHAFING, LOCATED BETWEEN STR 21L TO STR 22L. REPAIRED FRAME AT STA 1148 BETWEEN STR 21L TO STR22L. REF SRM 51-40-3 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR. INSTALLED DOUBLER ON FRAME AT STA 11SDR 08FDEA02551Angle · crackedRT MLG STA 940 UPPER BEAM ANGLE CRACKED IN RADIUS. FABRICATED NEW ANGLE. REF BOEING DWG 69-65045. MATCH DRILLED REF DWG 69-65045. INSTALLED ANGLE. REF SRM 51-30-2. THIS IS CLASSFIED A MINOR REPAIR.SDR 08FDEA02512Bulkhead · corrodedNOSE WHEEL WELL AFT WALL (STA 351) SURFACE UNDER DOWN LOCK ACTUATOR MOUNT IS CORRODED. REMOVED CORROSION, NDT, MATERIAL THICKNESS, ORIG. "T" = .072" MAT REMAINING =.065". .007' MAT LOSS. WITHIN LIMITS REF FED EX EA NR 7-5310-113999, TREATED AND PRIMED, AND SDR 08FDEA02479Skin · delaminatedTAIL CONE: VERTICAL STAB PNL 9703 HAS NUMEROUS PUNCTURES AND DELAM. REPAIRED PANEL NR 9703. REF SRM 51-40-9 PAR 3, 4 PAGES 2A-6. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02482Stringer Clip · crackedMID CABIN AT STA 804 STRINGER 7R STRINGER CLIP CRACKED. REMOVED STRINGER CLIP STA 804 STR 7R. REF 727 SRM 51-30-2 P1. MATCH DRILLED NEW STRINGER CLIP P/N 65-4531342 A 18793 P/O 1038874. REF 727 SRM 51-30-2 P1. INSTALLED NEW STRINGER CLIP STA 804 STR 7R RESDR 08FDEA02470Panel · delaminatedTAIL DOCK VERTICAL STAB LT TOP PNL 9706 HAS DELAM ON PNL RADIUS IN CTR OF PNL. REPAIRED PANEL NR 9706 REF SRM 51-40-9 PAR 3, 4. "THIS IS CLASSIFIED AS A MINOR REPAIR."SDR 08FDEA02468Stringer Clip · corrodedSTRINGER CLIP ON STR 9L AT FS 720B HAS CORROSION ON SIDES REMOVED STRINGER CLIP REF SRM 51-30-02. DRILLED UP NEW CLIP. INSTALLED NEW CLIP REF SRM 51-30-02, THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA02465Hinge · crackedGROUND POWER ACCESS PANEL. TOP HINGE BRACKET CRACKED REMOVED DAMAGED PART PER REF SRM 51-30-02 PG 1-3, FABRICATED NEW PART PER REF DWG NR 66-16849-7. TREATED AND PRIMED NEW PART PER REF SRM 51-10-02. INSTALLED NEW PART PER REF SRM 51-30-02 PG 1-3. THIS IS SDR 08FDEA02464Hinge · crackedGROUND POWER ACCESS PANEL. TOP HINGE BRACKET CRACKED REMOVED DAMAGED PART PER REF SRM 51-30-02 PG 1-3, FABRICATED NEW PART PER REF DWG NR 66-16849-7, TREATED AND PRIMED NEW PART PER REF SRM 51-10-02. INSTALLED NEW PART PER REF SRM 51-30-02 PG 1-3. THIS IS CSDR 08FDEA02462Strap · corrodedFWD CARGO COMPARTMENT RT STRIP AT STA 620 - 660, CORRODED ON BACK SIDE AND CRACKED FABRICATED NEW STRIP USING .063" 2024 T-3, A93206 REF BAC DWG 65-67255 1498-288 SRM 51-20-1 FIG 7. TREATED AND PRIMED REF 51-10-2 PART MARKED REF FED EX GMM 7-0-1001. THIS IS SDR 08FDEA02454Panel · crackedRT LOWER SIDE T/E PANEL FOWARD OF I/B AILERON HAS CRACK IN O/B EDGE SUPPORT ANGLE 1 3/4 INCH FORWARD FROM AFT EDGE. REMOVED DAMAGED PART PER REF SRM 51-30-2 PG 1-3. FABRICATED NEW PART PER DWG 65-19281-107. TREATED AND PRIMED NEW PART PER REF SRM 51-10-02. SDR 08FDEA02453Stringer Clip · crackedSTRINGER CLIP CRACKED BS 950C, STRINGER 5L REPLACED STRINGER CLIP REF SRM 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA02450Rib · crackedNLG LEFT FWD LEFT DOOR, CRACK IN AFT SIDE FRAME AT O/B STOP FITTING LOWER 2 FASTENERS FOR INNER SUPPORT. REPAIRED NLG DOOR REF SRM 51-40-3 PG 1-6. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02449Rib · crackedNLG RIGHT FWD DOOR, CRACK IN AFT SIDE FRAME AT O/B STOP FITTING LOWER 2 FASTENERS FOR INNER STRUCTURE. REMOVED AND REPLACED DOOR FOR ACCESS, REPAIRED DOOR REF MM 32-22-001-4 AND SRM 51-40-3 FIG 1. ADJUSTED AND OPS CHECK OF DOOR ACCOMPLISHED ON W/C 71C130-0SDR CA080624003Indicator · malfunctioned(CAN) ON TAKE-OFF/CLIMB OUT, THE NR 3 ENGINE EGT WAS 60 DEGREES HIGHER THAN ENGINES 1 AND 2. THROUGH 1000 FEET AGL THE NR 3 OIL TEMP WENT INTO THE RED BAND. A REDUCTION IN POWER FOR QUITE THRUST BROUGHT THE OIL TEMP BACK TO THE YELLOW BAND. A RESUMPTION IN POWSDR 08FDEA02430Floorbeam · damagedPASS CABIN AT STA 760 CARGO FLOOR SUPPORT NUT PLATE IS MIS-DRILLED AT RBL 4, WL 208. REMOVED FLOOR SUPPORT CHANNEL, LOCATED, DRILLED, AND INSTALLED NEW FLOOR SUPPORT P/N 65-25589-6, A18848, PO NR 1038952 REF SRM 51-30-5 PG 6, 51-30-2 PG 4.SDR 08FDEA02429Stringer Clip · crackedSTRINGER CLIP CRACKED, BS 950 E, STRINGER 6L. REPLACED STRINGER CLIP REF SRM 51-30-2 PG 1-7. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA02428Spar · corrodedPANEL JUST AFT OF RT WING AFT SPAR LOWER CHORD IS CORRODED FABRICATED NEW PANEL FROM JUST AFT OF RT WING SPAR LOWER CHORD REF. BOEING DWG 65-26797-3, TREATED AND PRIMED AND PAINTED REF SRM 51-10-2 PG 1-7, MM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAISDR 08FDEA02426Stringer Clip · corrodedSTRINGER CLIP ON STR 8L, AT FS HAS AREAS OF SURFACE CORROSION REMOVED AND REPLACED STR CLIP, STA 720B, STR 8L REF SRM 51-30-2 PGS 8-9 AND 32.SDR 08FDEA02424Stringer Clip · corrodedFWD LWR PIT BILGE, CORROSION ON INBD SIDE OF STR CLIP AT FWD SIDE OF FRAME AT STA 480 STR 26R. REMOVED AND REPLACED STR CLIP AT FWD LWR, PIT BILGE STA 480, STR 26R, FWD SIDE REF SRM 51-30-02 PG 1-5. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02423Stringer Clip · crackedSTRINGER CLIP CRACKED AT LOWER O/B RADIUS STR 5R STA 760 REPLACED STRINGER CLIP TO STR 5, STA 760 REF SRM 51-30-2 PG 10. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA02419Tab · delaminatedRT HORIZONTAL STAB ELEVATOR TRIM TAB IS DISBONDED ON LE UPPER SURFACE 29 INCHES OUT FROM INBD EDGE AT NR 3 HINGE. REMOVED AND INSTALLED NEW SERVICABLE TAB REF MM 27-30-011-2, OPERATIONAL AND FUNCTIONAL CHECK ACP ON W/C 73C022-00 THIS IS CLASSIFIED AS A MINOR SDR 08FDEA02418Stringer Clip · crackedSTRINGER CLIP CRACKED, BS 950D, STRINGER 6L. REPLACED STRINGER CLIP AT BS 950D STRINGER 6L REF SRM 51-30-2 PG 1-11. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA02417Skin · gougedDURING INSPECTION OF NR 2 ENG INLET, RAN JLG INTO FUSELAGE AT STATION 1030 STRINGER 1R TO 3R, LIGHT SCRATCH AND GOUGE REMOVED DAMAGE PER REF SRM 53-30-3 FIG 3. NDT DAMAGE REMOVAL AND MATERIAL LOSS. PER REF 727 NDT MAN PART 6, 51-00-00 FIG 23. TOOL IDM-0065.SDR 08FDEA02415Frame · damagedFIGURE "8" HOLE ON STA 760 FRAME I/B OF STR 5L. FABRICATED REPAIR PART (CHANNEL) FOR FRAME STA 760, STRINGER 5L, REF SRM 51-40-03. HEAT TREATED, TRACKING NR 208-06-060, TREATED AND PRIMED AND INSTALLED REF SRM 51-10-2 PG 1-7, 51-30-2 PG 2, 51-40-03 FIG 1, THSDR 08FDEA02414Skin · damagedDRILL START NEXT TO RIVET, UNDER PANEL 9702, VERTICAL STABILIZER UPPER SKIN, DEPTH OUT OF LIMITS. FOUND WHILE ACCOMPLISHING N/R N00752, FOUND DAMAGE TO BE OUT OF LIMITS. VERIFIED REPAIR MATERIAL TO 2024-T-3 .080". FABRICATED REPAIR DOUBLER AND INSTALLED DOUSDR 08FDEA02411Stringer · damagedSTRINGER 6L, MIS-DRILLED HOLE, BS 950D, UPPER WEB. REMOVED DAMAGE SECTION OF STRG 6L, BS 950D 10. FABRICATED REPAIR PARTS REF SRM 53-10-3 PG 5-9. TREATED AND PRIMED REPAIR PARTS REF SOPM 20-43-03 PG 3. INSTALLED REPAIR PARTS REF SRM 53-10-02 PG 1-8 AND SRMSDR 08FDEA02409Frame · crackedFWD LAV BS 312 FRAME CRACKED FROM O/B WEB FASTENER TO O/B RADIUS JUST BELOW S-13 R. FABRICATED 3 REPAIR PARTS FOR FWD LAV BS 312 FRAME, REF SRM 53-10-4 FIG 1, HEAT TREATED, TRACKING NR 2008-06-068, 2008-06-064, AND 2008-06-065, TREATED AND PRIMED AND INSTALLESDR 08FDEA02407Frame · damagedFUSELAGE FORMER FRAME DOUBLE DRILLED ON VERT FLANGE WITH LESS THEN 1/4 D DISTANCE BETWEEN HOLES AT FS 760 BETWEEN STR 3R AND 4R REPAIR DOUBLE DRILLED HOLE ON FRAME STA 760 BETWEEN STR 3R AND 4R REF SRM 53-10-4 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA02406Panel · crackedPANEL RACK, UPPER APU PANEL CUTOUT FASTENER HOLE CRACKED/GOUGE FABRICATED NEW PANEL FROM 2024 T-3 .040", APPLIED ALODINE, PRIMER AND PAINT REF DWG 65-58541, SRM 51-10-02 PG 7 AND MM 51-20-151-7 PG 1/2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02405Fairing · crackedNR 4 FLAP TRACK MID FAIRING, CRACK ON INNER SIDE OF MLG FLYING DOOR FWD HINGE CUT OUT ON FAIRING. FABRICATED NEW DOUBLER, REF 727 51-20-1 PG 4, MATERIAL VERIFIED AS 7075-76 .050" REF BAC DWG 65-21795. REPLACEMENT MATERIAL VERIFIED AS 7075-76 .050" BY A-TAG NSDR 08FDEA02300Cabin Pressure · malfunctionedFL270 AND .80 MACH, UPON COMP OF THROTTLE ALIGN CK AND RECYCLING OF NR 1 AND NR 2 ENG BLEED S CABIN PRESS BEGAN TO CLIMB AT 500-1000' FPM. COULD NOT STOP CLIMB AND APPROACHING 10K CAB PRESS WE WERE FORCED TO DESCEND TO 10K' AND DIVERT INTO DSM. IAW QRH ATTEMSDR 08FDEA02285Stringer Clip · crackedSTRINGER CLIP CRACKED, BS 950D, STRINGER 5L REMOVED CRACKED STRINGER CLIP FROM BS 950D, STRINGER 5L, AND INSTALLED A NEW STRINGER CLIP AT SAME LOCATION, REF SRM 51-30-02 P 1-32. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA02284Stringer Clip · corrodedCABIN, BS 720B AT 7L STRINGER CLIP HAS CORROSION REMOVED CLIP REF SRM 51-30-02 DRILLED UP NEW CLIP. INSTALLED NEW CLIP REF 51-30-02 PG 1-17, THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA02283Stringer Clip · crackedCABIN, BS 520 S 3R CLIP CRACKED (STR CLIP) REMOVED CLIP REF SRM 51-30-02, DRILLED UP NEW CLIP. INSTALLED CLIP REF SRM 51-30-2 PG 1-17. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA02282Skin · crackedAFT CARGO DOOR LOWER FWD SKIN CRACKED CRACK ON EDGE OF SKIN (OUT OF LIMITS). REMOVED DAMAGED SKIN INSTALLED FILLER AND DOUBLER REPAIR REF SRM 52-00-3 PG 7-13, REPAIR CLASSIFIED AS A MAJOR.SDR C8G2008F00013Indicator · faultyDURING TAKEOFF ROLL THE NR 2 ENGINE EGT INDICATOR WENT TO ZERO INDICATION. THE TAKEOFF WAS ABORTED, WHERE THE AC RETURNED TO BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED NR 2 ENGINE EGT INDICATOR AT FAULT. THE NR 2 ENGINE EGT INDICATOR WAS REMOVED SDR C8GA200800AIndicator · malfunctionedFLT 738 FRO TOL TO SLW. DURING TAKEOFF ROLL THE NR 2 ENG EGT INDICATOR WENT TO ZERO INDICATION. THE TAKEOFF WAS ABORTED. THE ACFT RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED NR 2 ENGINE EGT INDICATOR AT FAULT. THE NR 2 ENG EGTSDR C8G2008F00002Indicator · inoperativeDURING TAKEOFF ROLL, THE NR 2 EGT INDICATOR WENT TO ZERO INDICATION. THE TAKEOFF WAS ABORTED AND THE AC RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THE NR 2 ENGINE EGT INDICATOR WAS AT FAULT. THE NR 2 EGT INDICATOR WAS REMOVED AND REPSDR DHLA200800056Wheel · vibrationRTO DUE TO HEAVY VIBRATION THAT SEEMED TO EMANATE FROM NOSE WHEEL NOTE RTO AT 80 KIAS FULL REVERSE & MODERATE BREAKING USED. REMOVED AND REPLACED BOTH NOSE WHEELS PER MM 32-45-11. FIT 520. AIRCRAFT WAS GROUNDED. (A)SDR DHLA200800055Wheel · noisyRTO DUE TO HEAVY VIBRATION THAT SEEMED TO EMANATE FROM NOSE WHEEL NOTE RTO AT 80 KIAS FULL REVERSE AND MODERATE BREAKING USED. REMOVED AND REPLACED BOTH NOSE WHEELS PER MM 32-45-11. FIT 520 AIRCRAFT WAS GROUNDED. (A)SDR 08FDEA01799Transceiver · failed(AIR-TURN-BACK), WX RADAR PAINTS INTERMITTENT FALSE RETURNS ONE SIDE THEN THE OTHER, STABILIZED OR UNSTABILIZED. WHEN UNSTABILIZED, RADAR PAINTS A SINGLE SPOKE AT THE 11 -12 O'CLOCK POSITION. GOING BACK TO STABILIZED, IT PAINTS A DOUBLE SPOKE. VERIFIED OLD SDR DHL200874301Mount Bracket · crackedMAIN CARGO DOOR AT FORWARD HOOK ACTUATOR UPPER MOUNT BRACKET HAS CRACK AT AFT INBOARD CORNER RADIUS TO BOLT HOLE. NEW PART FABRICATED USING DRAWING 52-523 FOR ONE TIME USE. MATERIAL USED 2024-T3 .090" PO NR 6193. INSTALLED NEW FABRICATED IAW BOEING SRM 51-
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