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 07FDEA01024Floorbeam · corrodedFOUND CABIN FLOORBEAM UPPER SURFACE HAS CORROSION, FS 580, RBL 24.75, TO RBL 45.5. REWORKED IAW FEDEX EA 7-5310-102028.SDR 07FDEA01022Skin · crackedLT HORIZONTAL STAB, ELEVATOR LWR SURFACE SKIN HAS CRACKS COMING OUT OF FWD AND AFT EDGES OF FASTENER HOLES, 38.5" OB OF INBD EDGE AND 13.5" FWD OF AFT EDGE. REPAIRED BONDED SKIN REF SRM 51-40-20 PG 59, 60, COOK TICKET ATTACHED TO N00129. PRIMED/PAINTED EXTERSDR 07FDEA01012Retainer · crackedRIGHT AFT EMERGENCY EXIT HATCH AFT LOWER SECTION HAS CRACKED SEAL RETAINER. REMOVED RETAINER REF SRM 51-20-2. FABRICATED NEW SEAL RETAINER REF BAC DWG 50-07978-53. INSTALLED NEW SEAL REF SRM 51-20-2 PG 4.SDR 07FDEA01004Skin · misrepairedREPAIR AT STA 298-307, STR 21R TO 23R DOES NOT COMPLY WITH FAA APPROVE DATA. REMOVED REPAIR, FAB`D NEW REPAIR DOUBLER IAW SRM 53-30-3, FIG 3, TABLE 1, MAT 2024-T3, .063C, AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3, FIG 3.SDR 07FDEA01002Skin · damagedFOUND REPAIR AT LT WING FIXED LE AT IB END OF NR 3 SLAT. REPAIR REQUIRES EVALUATION FOR MAJOR/MMINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FOUND EXISTING REPAIR DAMAGED. REMOVED DAMAGED REPAIR FILLER, FABRICATED NEW FILLER ANSDR 07FDEA00991Crease Beam · damagedCABIN LT CREASE BEAM INNER CHORD HAS 5 EA PLUGGED HOLES WL 208, BS 740 - 760. REMOVED SUPPORT ANGLE, AND INSTALLED NEW SUPPORT ANGLE, REFERENCE SRM 51-30-02. CLASSIFIED AS MAJOR REPAIR.SDR 07FDEA00983Intercostal · corrodedFOUND INTERCOSTAL CORRODED FS 348 TO 360, AT STR 12L. REMOVED CORRODED, CHECKED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1, FIG 1, SHEET 2. FAB`D NEW FILLER AND DOUBLER FROM 7075-T6, .040C BATCH 1120917, AND 7075-T6, .050C BATCH 761741 IAW SRM 51-40-2, FISDR 07FDEA00982Intercostal · corrodedINTERCOSTAL CORRODED FS 348 TO 360 AT STR 9L. REMOVED CORROSION, CHECKED LIMITS, IAW SRM 53-104-1, FIG 1, SHEET 2. FAB`D NEW FILLER AND DOUBLER FROM 7075-T6, .040C BATCH 1107917 AND 7075-T6, .050C BATCH 76174. IAW SRM 51-40-2, FIG 1. INSTALLED FILLER AND DOSDR 07FDEA00981Skin · corrodedAFT CARGO FWD OF STA 1166, FROM LBL 6 TO RBL 2, HAS CORROSION ON SKIN. REMOVED CORROSION IAW SRM 51-10-6, UT INSP PER NTM 51-00-00, PT4, MAT THICKNESS BEFORE .125 AFTER REWORK .118, FOUND TO BE WITH IN LIMITS IAW SRM 53-10-1, FIG 1, DETAIL I. TREATED AND PRISDR 07FDEA00977Angle · crackedMAIN CABIN UPPER LOBE STA 1100, "LEFT AND 1" RIGHT OF STR 1, HAS 2EA RIVETS WITH CRACKS AROUND RIVETS. REPAIRED DAMAGED AREA IAW SRM 53-30-3, FIG 3, AND SB 727-53A0204. REPAIRED DAMAGED SKATE ANGLE IAW SRM 51-40-9. PREPPED AND PAINTED AREA IAW AMM 51-20-151-SDR C1HA200778001Line · looseON CLIMB-OUT FROM DEN, NR 3 EPR STARTED SURGING UP AND DOWN 10 TO 15 PERCENT, SHUT OFF RT PACK, SURGING STOPPED. MADE PRECAUTIONARY LANDING BACK IN DEN CONFIRMED FAULT FOUND 10 SENSE LINES LOOSE ON RT FLOW CONTROL VALVE. TIGHTENED PER STD PRACTICES REF MM 36SDR 07FDEA00913Skin · misrepairedFOUND EXTERNAL FUSELAGE REPAIR AT APPROX STA 1110-1130, AT S-20L DID NOT CONFORM TO SRM 53-30-3 FIG 5. REMOVED EXISTING REPAIR, EXTENDED FILLER AT LAP AND INSTALLED DOUBLER REF SRM 53-30-3 FIG 5.SDR 07FDEA00916Floorbeam · crackedFLIGHT DECK FLOOR SUPPORT CHANNEL IS CRACKED ON TOP OF CHANNEL LOCATED AT BS 285, LBL 6.5. INSTALLED NEW SUPPORT CHANNEL PER SRM 51-30-2 PG 2. CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA00912Bracket · crackedNLG W/W CEILING THRU LT ACCESS PNL LT SUPPORT HAS CRACKS ON BOTH ENDS FS 259.50. REMOVED SEAT TRACK FOR ACCESS IAW SRM 51-30-2. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-30-2. REINSTALLED SEAT TRACK IAW SRM 51-30-2.SDR 07FDEA00911Skin · corrodedRIGHT WING LOWER SURFACE HAS CORROSION AT NR 6 FLAP TRACK MID ATTACH POINT. ACCOMPLISHED REPAIR OF ATTACH POINT, REF EA 7-5730-107001, WRI 57309127.SDR 07FDEA00880Stringer Clip · damagedMAIN CABIN FS 640, STR 3R STRINGER CLIP IS DAMAGED. FABRICATED STRINGER CLIP, TREATED, PRIMED AND INSTALLED CLIP REF SRM 51-10-2 PG 3, SRM 51-30-2 PG 3, AND DWG 65-15935-16. CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA00870Beam · corrodedAC BAY LBL 13 BEAM LOWER CHORD HAS CORROSION AROUND GROUND STUDS AND CLAMP SCREW BS 745-765, WL 140 ACCOMPLISHED REPAIR AT A/C BAY LBL 13 BEAM LOWER CHORD BS 745-765 REF SRM 51-40-3 PG 1-6. CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA00868Skin · misrepairedFOUND FLUSH REPAIR AT APPROX FUSELAGE STATION 1110-1130 BETWEEN STR 13L-14L DID NOT CONFORM TO EA NR 7-5330-107007. REMOVED EXISTING INTERNAL PLUG DOUBLER PER EA NR 7-5330-107007. FABRICATED .090" INTERNAL DOUBLER TO COMFORM TO EA TREATED AND PRIMED, AND INSSDR C1HA200775001Clamp · looseEN ROUTE HAD LOWER AFT BODY HEAT LIGHT ILLUMINATE. RAN COM.2.36.5- AFTER SHUTTING OFF LEFT NR 1 BLEED VALVE, LIGHT EXTINGUISHED. AFTER SHUTTING OFF ENGINE NR 1 BLEED VALVE FOLLOWED BY LT A/C PACK, RT PACK WOULD NOT HOLD PRESSURIZATION, HAD TO DESCENT TO 1100SDR 07FDEA00848Skin · misrepairedEXTERNAL DOUBLER LOCATED AT STA 1087- 1096, STR 22R - 23R, DOES NOT COMPLY WITH FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR DOUBLER AND FILLER FROM MAT 2024-T3, .071. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER AND FSDR 07FDEA00847Skin · corrodedAFT BAG BIN FUSE SKIN CORRODED ADJACENT TO STR 29L BETWEEN FS 950D TO 950E. CUT OUT DAMAGE, FABRICATED REPAIR PLATE AND FILLER FROM MAT 2024-T3. TREATED AND PRIMED IAW SRM 51-10-2 AND INSTALLED REPAIR IAW SRM 53-30-3, FIG 3. MAJOR REPAIR.SDR 07FDEA00840Skin · misrepairedFOUND EXTERNAL REPAIR APPROX BETWEEN STA 720C AND 720D, BETWEEN STR 7R-8R, TO BE INSTALLED WITH BLIND FASTENERS, AND DOUBLER ENDS ON STRUCTURE. REMOVED AND REPLACED DOUBLER BETWEEN STA 720C AND 720D. SEALED AND PAINTED. REF SRM 53-30-3 FIG 1.SDR 07FDEA00833Bulkhead · corrodedFOUND FWD CARGO STA 720D LWR BULKHEAD BEAM HAS CORROSION AT LBL25. REMOVED AND REPLACED ANGLE IAW SRM 51-30-2.SDR 07FDEA00832Skin · crackedCABIN FWD RT GALLEY DOOR EXT UPPER HINGE CUT OUT DOOR SKIN HAS A CRACK. STOPPED DRILLED CRACK IAW SRM IAW SRM 52-00-3 FIG 3. FABRICATED REPAIR DOUBLER FROM 2024 T-3 .080C. INSTALLED REPAIR IAW SRM 52-00-3 FIG 3. REPAIR CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA00831Support Bracket · crackedNR 2 FLAP TRACK AFT SUPPORT BRACKET IS CRACKED OTBD AFT END. REMOVED AND REPLACED BRACKET IAW SRM 51-30-2.SDR 07FDEA00801Structure · crackedFOUND LMLG WING DOOR LWR AFT EDGE ANGLE IS CRACKED. REPAIRED LMLG WING DOOR LWR AFT EDGE ANGLE REF SRM 51-40-3 FIGURE 1.SDR 07FDEA00777Skin · unknownTHE MAIN CARGO DOOR HAS 4 EXTERNAL DOUBLERS ON ITS INTERNAL SKIN ALONG THE TOP EDGE AT STATIONS 520, 540, 560, AND 580. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00776Frame · unknownFOUND AFT PIT FRAME REPAIR, STA 970, ABOVE S23L TO S24L. COMPLY WITH ATTACHMENT "B" OF EO 7- 5100-7-5005 PT2. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00775Frame · unknownFOUND AFT PIT FRAME REPAIR STA 950, ABOVE S24L TO S25L. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00774Stringer · unknownAFT PIT, FUSE STRINGER REPAIR STA 1130- 1166,S29. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00773Stringer · unknownAFT PIT, FUSE STRINGER REPAIR, STA 1070- 1090,S20R. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00772Stringer · unknownAFT PIT FUSE STRINGER REPAIR, STA 1050- 1070,S20R. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00771Torque Box · unknownEXTERNAL DOUBLER SECTION 48, RT LOWER TORQUE BOX, ATA 1227.5,RBL 20, WL 190. COMPLY WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00766Torque Box · unknownFOUND EXTERNAL DOUBLER, SECTION 48, RT LOWER TORQUE BOX STA 1237, RBL 20, WL 189. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2, MAJOR REPAIR.SDR 07FDEA00760Torque Box · unknownFOUND EXTERNAL DOUBLER, SECTION 48, RT LOWER TORQUE BOX STA 1238, RBL20, WL 183. COMPLIED WITH ATTACHMENT "B" OF EO 7-5100-7-5005 PT2.SDR 07FDEA00752Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK OTBD FLANGE IS CORRODED AT BS 950 ,10 TO 950A 8, LBL 25, WL 208. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS REF SRM 53-10-1 FIG 3. REPAIRED SEAT TRACK REF SRM 53-10-5 FIG 7. CLASSIFIED AS A MAJOR REPAIR.SDR 07FDEA00721Seat Track · corrodedFOUND MAIN DECK FLOOR SUPPORT SEAT TRACK OUTBD FLANGE IS CORRODED AT BS 1080 - 1090, RBL 1, WL 208. REMOVED DAMAGED/CORRODED OUT OF LIMIT SEAT TRACK FROM STA 1010 TO STA 1130, BL0 AND INSTALLED NEW SEAT TRACK REF SRM 53-10-2 FIGURE 7A SHEET 16 PAGE 16 AND SRMSDR 07FDEA00688Skin · dentedLOWER FUSELAGE AT BS 1148 TO 1170 BETWEEN STR 19R AND 20R, SKIN IS CREASED. REMOVED DAMAGE AND MANUFACTURED REPAIR PARTS REF SRM 53-30-3, PG 5. TREAT AND PRIMED REPAIR PARTS AND REPAIR AREA ON A/C SKIN REF SRM 51-10-2 PG 7. INSTALLED FASTENERS REF SRM 51-30-SDR 07FDEA00687Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION SPOTS FS 620-720F LBL 45, REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.SDR 07FDEA00686Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION SPOTS FS 620 - 700 RBL 24. REMOVED AND REPLACED SEAT TRACK FS 620 - 700 RBL 24 IAW SRM 51-30-2.SDR 07FDEA00685Seat Track · corrodedFOUND MAIN DECK SEAT TRACK STA 740-850 RBL-45 HAS AREA OF BARE METAL AND CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2.SDR 07FDEA00684Floor Skin · corrodedE/E COMPT RT O/B FLOOR PNL WEB HAS CORROSION FS - 435, REMOVED AND REPLACED DAMAGED WEB AT STA 435 IAW SRM 51-30-2. NEW WEB MADE ON TRAVELER T7/665341.SDR 07FDEA00683Fitting · damagedMAIN CABIN FS 340 STR 8L DOOR STOP FITTING FOR FWD ENTRY HAS A MISDRILLED HOLE. REMOVED OLD FITTING, DRILLED AND INSTALLED NEW STOP FITTING REF SRM 51-30-02 PG 4, MM 52-11-011-8 PG 1, POLY PAINTED FITTING REF MM 51-20-103-7, PG 1.SDR 07FDEA00682Angle · crackedFOUND LT FWD EMERGENCY EXIT UPPER FWD SEAL RETAINER ANGLE IS CRACKED AT FASTENER HOLE. REMOVED LT FWD EMERGENCY EXIT UPPER FWD SEAL RETAINER ANGLE AND INSTALLED NEW RETAINER ANGLE PER SRM 51-30-02 PG 2. REMOVED LINER AND REINSTALLED LINER PER SRM 51-30-02 PGSDR 07FDEA00681Stringer Clip · crackedFOUND MAIN DECK BODY FRAME STRINGER CLIP IS CRACKED AT BS 950D, STR 9L. REMOVED DAMAGED CLIP REF SRM 51-30-2. INSTALLED NEW CLIP REF SRM 51-30-2.SDR 07FDEA00680Seat Track · corrodedFOUND MAIN DECK FS 500 AND FS 525, LBL 26 SEAT TRACK CORRODED, DUE TO BEING PREVIOUSLY BLENDED AND NO PROTECTIVE FINISH APPLIED. REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK FROM BAC 1520-792, 7178T6511. INSTALLED NEW SEAT TRACK FROM BS 480-680 10 AT LBL SDR 07FDEA00678Frame · crackedFRAME 277 IS CRACKED IN THE RADIUS OF CUT OUT FOR STRINGER 16R DISPLACED WIRING FOR ACCESS. VERIFIED CRACK, REMOVED FASTENERS AND DAMAGE, VERIFIED DAMAGE REMOVED AND MATERIAL LOSS. FABRICATED, TREATED AND INSTALLED DOUBLER, FILLER AND CLIP REF SRM 51-40-2 SDR 07FDEA00660Stringer Clip · crackedFOUND MAIN DECK BODY FRAME STR CLIP IS CRACKED AT BS 970, STR 9L REMOVED AND REPLACED CRACKED STRINGER ATTACH CLIP AT STRINGER 9L, BS 970 PER SRM 51-30-02 PG 8.SDR 07FDEA00659Door · corrodedFOUND NLG LEFT FORWARD DOOR, INBOARD INNER CHORD IS CORRODED THRU AT AFT END REPLACED LEFT FWD NLG DOOR. REF MM 32-22-001-4, PG 1. DOOR ADJUSTMENT AND TEST ACCOMPLISHED ON ROUTINE CARD 71C130-00 SEQ# 98.SDR 07FDEA00653Skin · misrepairedFOUND REPAIR AT LT WING INBD FOREFLAP LE SKIN 21" FROM IB END (EXTERNAL REPAIR). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR, FOUND NOT TO CONFORM TO SRM 57-50-4 FIG 1. RE
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