Boeing 727-2S2F
Service difficulty reports · 842
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 = '7272S2F' 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 = '7272S2F' 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 FDEA200907022466Angle · crackedNR 2 SLAT LOWER AFT ANGLE IS CRACKED BELOW TEE DUCT REMOVED INNER PANELS IAW SRM 51-30-2. CUT OUT DAMAGED AREA OF ANGLE IAW SRM 51-40-4 FIG 1 FABRICATED ANGLE SECTION IAW SRM 57-50-2 AND 51-40-4, ALODINED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PSDR FDEA200906262444Skin · crackedNR 3 SLAT CRACKED T/E AT OTBD HOOK AFT ATTACH FASTENERS. HFEC VERIFIED THAT CRACK ENDS AT FASTENER HOLE IAW NDTM 51-00-00. FABRICATED DOUBLER AND INSTALLED IAW SRM 57-50-3 AND 51-30-8.SDR FDEA200906262320Spar · crackedCRACK ANGLE LT WING FALSE SPAR AT NR 7 SPOILER ATTACH FITTING. CUT ANGLE AT LT WING FALSE SPAR IAW FX DWG SR 27-57-038 REV C. FABRICATED 2 ANGLES. HEAT TREATED ANGLES FROM 'O' TO T6 IAW FAS ENG REPORT NR 2-37153-801 REV A, FABRICATED DOUBLER, WEB, LOWER ANGSDR FDEA200906252332Floorbeam · corrodedFORWARD ENTRY WAY - FLOORBEAM CORRODED AT BS 344 RBL 10 TO LBL 45. REMOVED FLOORBEAM, FABRICATED NEW FLOORBEAM AND INSTALLED IAW DWG SR27-53-007 AND SRM 53-10-2, 51-30-5 AND 51-30-2.SDR FDEA200906222462Skin · bulgedSKIN BULGE FUSELAGE STATION 219 STRINGER 24L. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2.SDR FDEA200906222334Skin · crackedLT MLG WING DOOR IS CRACKED AT AFT HINGE POINT. REMOVED DAMAGED AREA, FABRICATED REPAIR AND INSTALLED IAW DRAWING 65C27128 AND SRM 51-30-2.SDR FDEA200906222330Unknown · misrepairedPREVIOUS REPAIR STA 380 STR 29L HAS FASTENERS WITH IMPROPER EDGE MARGIN. REMOVED PREVIOUS REPAIR, HFEC INSPECTED HOLES WITH NO DEFECTS NOTED, FABRICATED NEW DOUBLER AND INSTALLED IAW EA 7-5330-126836.SDR FDEA200906222221Fire Detector · failedDURING CLIMBOUT AT APX 19000 FT, 1 BELL TONE FOR APX 1 SECOND. CHECKED ALL FIRE DETECTION SYS AND LOOPS (A B) AND APPEARED TO OPERATE NORMALLY. APX 2 MINS LATER HAD INTERMITTENT FIRE WARNING FOR NR 1 ENG, THEN WARNING STOPPED. RUN CHECKLIST FOR ENG FIRE AND SDR FDEA200906222203Skin · dentedOIL CANNING SKIN AT STA 180 STR 26L. CUT OUT DAMAGED AREAS, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-30-3, 53-30-2, 51-10-2 AND 51-30-2.SDR FDEA200906202333Rib · crackedNR 4 SLAT HAS 2 CRACKED RIBS ON EITHER SIDE OF THE ACTUATOR FWD MOUNT. REMOVED L/E SLAT ACCESS PANEL IAW SRM 51-30-2. REMOVED DAMAGED RIBS AT NR4 SLAT 2 EACH IAW SRM 51-30-2. LOCATED AND DRILLED NEW RIBS IAW SRM 51-30-5 RIB PN 65-17276-9 AND 65-17276-11. SDR FDEA200906202331Window Frame · corrodedCORROSION ON WINDOW FRAME RT FUSELAGE STA 650. REMOVED CORROSION FROM WINDOW FRAME AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 51-10-6, 56-20-1, 56-20-3 AND 51-30-2.SDR FDEA200906192181Warning Bell · false activationAT LEVEL OFF 330 CREW HEARD DING OF FIRE BELL. INSPECTED COCKPIT FOR LIGHTS, NONE ILLUMINATED. DID ENG FIRE TEST WITH NORMAL RESULTS. RIGHT AFTER FIRE TEST, NR 1 ENG FIRE LIGHT ILLUMINATED WITH CONSTANT BELL. RAN RED TAB PROCEDURE, FIRE LIGHT WENT OUT WITHSDR FDEA200906182160Unknown · unknownAT LEVEL OFF 330 CREW HEARD DING OF FIRE BELL. INSPECTED COCKPIT FOR LIGHTS, NONE ILLUMINATED. DID ENG FIRE TEST WITH NORMAL RESULTS. RIGHT AFTER FIRE TEST NR 1 ENG FIRE LIGHT ILLUMINATED WITH CONSTANT BELL. RAN RED TAB PROCEDURE, FIRE LIGHT WENT OUT WITH SDR FDEA200902270766Warning Light · false activationTAILSKID LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW REPORTED THAT AFTER CYCLING GEAR THE SYSTEM WORKED NORMALLY AND ON APPROACH, SYSTEM FUNCTIONED NORMAL. INSPECTED SWITCH AT TAILSKID. NO DEFECTS FOUND. SUSPECT ICE IN BILLINGS CAUSED SWITCH TO STICK. SDR FDEA200902250718Engine · failedNR 3 ENG FIRE WARNING INDICATION. SHUT DOWN ENG IAW QRH. INDICATION PERSISTED. BLEW BOTH FIRE BOTTLES. INDICATION PERSISTED INTERMITTENTLY THROUGHOUT LANDING AND TAXI-IN. NR 3 ENG WINDMILLED FOR 6 MINS. UNABLE TO DETERMINE IF OIL PRESS WAS GREATER THAN 1SDR FDEA200902070480Indicator · burnedAT FLIGHT LEVEL 390 SMELLED FUMES IN COCKPIT. DECLARED AN EMERGENCY AND LANDED AT DEN AIRPORT. MED BRAKE WAS USED AND EMERGENCY EGRESS CONDUCTED. FSFO CHECKLIST EXECUTED. ISOLATED BURNED ODOR TO FLT ENGINEERS PANEL AND FOUND NR 3 ENGINE OIL QUANTITY IND ISDR FDEA200901200268Indicator · failedF/O AIRSPEED INDICATOR FAILED: NEEDLE STOPPED AT 200 KTS AND OFF FLAG, RESTORED THEN SECOND FAILURE AT 250 KTS AND OFF FLAG. REMOVED AND REPLACED NR 2 AIRSPEED INDICATOR. SYS CKS NORMAL. NO LEAKS NOTED IAW 727 M/M 34-12-000-5. PREMATURE REMOVAL/INSTALLATIOSDR FDEA200901100122Floor Support · corrodedMCD FLOOR SUPPORT UPPER SURFACE SKIN CORRODED BETWEEN BS 304 AND BS 344 LBL 30. REPAIRED FLOORBEAM AT STA 304 LBL 30 IAW SRM 53-10-8 FIG 9 AND REPLACED 2 FLOOR SUPPORTS IAW SRM 51-30-2 MAJOR REPAIR RII RDR SDR.SDR FDEA200901100121Support Beam · crackedNR 4 FLAP TRACK AFT MOUNT VISUALLY CRACKED IN 2 PLACES AT WING TRAILING EDGE REPAIRED LT WING SPOILER SUPPORT BEAM LWR CHORD IAW EA 7-5710-124053 BY SPLICING THE LOWER CHORD MAJOR REPAIR RDR AND SDR RII.SDR FDEA200901020003Skin · damagedDEEP WEAR MARKS IN FUSE SKIN BETWEEN STA 970 AND 990 AT BODY FAIRING LWR CONTACT AREA STR 24L. REMOVED AND REPLACED DAMAGE SKIN AREA APPROX BY 6 INCHES X 3 INCHES WITH REPAIR DOUBLER AND FILLER IAW SRM 53-30-3, FIG.3, CLASSIFIED AS MAJOR REPAIR.SDR FDEA200812075103Seat Track · corrodedAT RBL 24 STA 1148 FLOORBEAM UPPER FLANGE CORRODED. DUE TO FLOOR SUPPORT REPAIR 1'4 INCH HOLE IN SEAT TRACK WILL NOT HAVE EDGE DISTANCE IF DRILLED IN SAME LOCATION AS ORIGINAL. SEE SNRM N00516 FOR FLOOR REPAIR DUE TO "T" CAP REPLACEMENT, A 1/4 INCH HOLE REQUSDR FDEA200812065098Skin · misrepairedFOUND RT STAB UPPER EXTERNAL REPAIR LOCATED AT APPROX SS 180, 6 INCHES FWD OF AFT EDGE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FOUND REPAIR DOES NOT COMPLY WITH CURRENTS SRM REPAISDR FDEA200812065097Skin · misrepairedFOUND RT STAB UPPER SURFACE EXTERNAL REPAIR LOCATED AT APPROX SS 145 8 INCHES FWD OF AFT EDGE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA FOUND REPAIR DOES NOT COMPLY WITH CURRENT SRM RESDR FDEA200812055094Skin · misrepairedFOUND FLUSH SKIN REPAIR LOCATED AT APPROX BS 308 BETWEEN STR S-10L AND S-11L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED FLUSH REPAIR, NDT'D ALL COMMON FASTENER HOLES AND EDGE SDR FDEA200812045076Channel · corrodedOTBD HAT CHANNEL HAS CORROSION AROUND NUT PLATE HOLES. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED, LOCATED AND DRILLED HOLES, TREATED, PRIMED AND INSTALLED NEW HAT CHANNEL, REFERENCE DWG NR 65-19606/ITEM NR 19, CLASSIFIED AS A MAJOR REPAIR.SDR FDEA200812045083Floor Support · damagedREWORK OF SNRM N00933, FLOOR SUPORT AT FS 1148 RBL 45 WAS MISSDRILLED FABRICATED NEW FLOOR SUPPORT REF DRAWING B27-53-015B. INSTALLED REF SRM 51-30-2 THIS IS CLASSIFED AS A MAJOR REPAIRSDR FDEA200812045080Angle · corrodedAFT PIT BULKHEAD UPPER ANGLE CORRODED CENTERLINE TO RBL 1166. REMOVED AND REPLACED UPPER CHORD ANGLE AT STA 1166 IN LWR AFT CARGO PIT REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR FDEA200812045079Floor Support · corrodedMAIN DECK FLOOR STRUCTURE, BL 0 BEAM, RT ATTACH ANGLE IS CORRODED AT LWR EDGE AT 1169 TO 1172, RBL 1 WL 205. REMOVED, FABRICATED NEW ANGLE REF DRAWING 69-34832 AND INSTALLED REF SRM 51-30-2. THIS IS CLASSIFED AS A MINOR REPAIRSDR FDEA200812045078Seat Track · corrodedAT RBL 45 STA 1148 FLOORBEAM UPPER FLANGE CORRODED DUE TO REPAIR ON SNRM NR N00516 1/4 INCH HOLE IN SEAT TRACK WILL NOT HAVE EDGE DISTANCE IF DRILLED IN SAME LOCATION AS ORIGINAL. DUE TO TEE CAP REPLACMENT A 1/4 INCH HOLE REQUIRED IN SEAT TRACK WOULD HAVE BEESDR FDEA200812045077Floor Support · corrodedFLOOR SUPPORT AT FS 1130 TO FS 1148, RBL 62, WL 206, HAS CORROSION AROUND SEVERAL NUT PLATES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED, LOCATED AND DRILLED HOLES, TRIMMED, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT. REF BOEING DWR 69SDR FDEA200812045085Support · corrodedMAIN DECK BULKHEAD SUPPORT CORRODED AT AFT BULKHEAD FITTING STA 1183 LBL 18, WL 208. REMOVED CORROSION, OUT OF LIMITS .018 MATERIAL REMOVED, ORIGINAL MATERIAL .063, .045 REMAINING. INSTALLED DOUBLER AND SPLICED FLOOR SUPPORT REF SRM 51-40-3 PG 1, DWR 65-3177SDR FDEA200812045081Floorbeam · corrodedMAIN DECK FLOOR BS 1176.5 CHORD HAS CORROSION ON UPPER FWD FLANGE AND INSIDE FASTENER HOLES FROM RBL 1 TO 24. REPLACED CHORD REF SRM 51-30-02, THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR FDEA200812035065Floorbeam · corrodedMAIN DECK FLOORBEAM LWR FLANGE IS CORRODED BS 1166, RBL 10-42, WL 200. REMOVED CORROSION FROM LOWER CHORD, ORIGINAL TEE .125 REMAINING .110. REMOVED .015 OUT OF LIMITS, REMOVED DAMAGED AREA, FABRICATED REPAIR PIECES, ALODINED, PRIMED AND INSTALLED REPAIR PIESDR FDEA200812035064Pan · crackedBS 1166 RBL 45-60 DITCHING PAN HAS 3 CRACKS REPLACED DITCH PAN REF DWR 65-29548 AND SRM 51-30-2 PG 4. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR FDEA200812025038Angle · crackedCRACKED LOWER ANGLE FALSE SPAR AT SPOILER NR 8 RT WING. REMOVED SPAR DOUBLER & INBD WEB SECTION IAW SRM 51-30-2. FABBED NEW DOUBLER IAW SRM 51-30-2 & DWG NR SR 27-57-038 REV C. FABBED NEW INBD WEB SECTION IAW DWG NR SR 27-57-038 REV C & SRM 51-30-2. FABBEDSDR FDEA200812025037Actuator · brokenAFT AIRSTAIR LIGHT ILLUMINATED IN-FLIGHT CLIMBING THROUGH 4,500 FEET. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B. AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP." REPLACED WARN RT HAND UPLOCK ROLLER FITTING PER SMP, FOUND SWITCH S395 ROLLER ACTUATOR BROKEN ASDR FDEA200811264991Keelbeam · corrodedLOWER AFT CARGO AREA CORROSION AT STA 950E - 950C ON LEFT KEELBEAM. INSTALLED REPAIR STRAP REF EA 7-5310-118316. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR FDEA200811264989Keelbeam · corrodedAFT PIT KEELBEAM IS CORRODED BS 950F - 970, STR 29R, WL 139. INSTALLED REPAIR STRAP REF EA 7-5310-118316 P 1-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR FDEA200811264992Keelbeam · corrodedLOWER AFT CARGO BAY LT KEELBEAM BS 950E 6 OTBD FLANGE IS CORRODED. INSTALLED REPAIR STRAP REF EA 7-5310-118316. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR FDEA200811264990Keelbeam · corrodedAFT PIT BILGE KEELBEAM IS CORRODED BS 950E-950F, S29R, WL 139. REPAIR STRAP INSTALLED REF EA 7-5310-118316 PG 1-2. ORIGINAL MATERIAL THICKNESS .150, MATERIAL REMOVED .029, .121 REMAINING. OUT OF LIMITS, REF EA 7-5310-118316. THIS IS CLASSIFIED AS A MAJORSDR FDEA200811264978Beam · corrodedCABIN FLOORBEAM, UPPER CAP LOWER SURFACE, CORRODED AROUND NUTPLATE, STA 950 RBL 5 BLENDED AREA TO REMOVE CORROSION, ORIGINAL MAT .150, LOSS .035 REMAINING .115 AND FOUND TO BE OUT OF LIMITS REF SRM 53-10-1. OBTAINED EA 7-5310-123812. FOUND MORE CORROSION DURSDR 08FDEA04959Shear Tie · corrodedFOUND AFT PIT FRAME SHEAR TIE REPAIR LOCATED AT APPROX BS 950D STR S-29L TO S-28L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING APPROVED DATA. ACCOMPLISHED REPAIR AT BS 950D STR 29L TO S28L FRAME SHEAR TIESDR 08FDEA04953Frame · corrodedC-2 PIT FLOOR FRAME SHEAR TIE AT FS 970, RBL9 TO RBL15, WL 139 HAS CORROSION ON AFT TO BOTTOM SIDE. INSTALLED NEW SHEARTIE REF SRM 53-10-4. THIS IS CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA04950Frame · misrepairedFOUND AFT PIT FRAME REPAIR LOCATED AT APPROX BS 1050 STR S-27L TO 26L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EVALUATION DETERMINED INSUFFICIENT FASTENERS. REMOVED REPAIR SRM 51-30-SDR 08FDEA04945Intercostal · corrodedLOWER AFT CARGO AREA- CORROSION ON WEB RBL 18 STA 950F 4 WL 148 BLENDED OUT CORROSION REMOVED .025 FROM ORIGINAL .040, REMAINING THICKNESS .015. FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED INTERCOSTAL WEB STA 950F- 970 RBL 18 WL 148 AND FABRICATED REPLACESDR 08FDEA04944Shear Tie · corrodedAFT PIT BILGE BODY FRAME SHEAR TIE IS CORRODED BS 970, STR 29L OB, WL 139. REMOVED FLOOR SUPPORT ANGLE AT FRAME 970 LBL 9 REF SRM 51-30-2 PG 1-9. REMOVED CORROSION ON SHEAR TIE REF SRM 53-10-1, ORIG THICK .073, REMAINING .011, OUT OF LIMITS. REMOVED DAMAGEDSDR FDEA200811194920Skin · chafedLOWER RIGHT EXTERIOR FUSELAGE SKIN IS CHAFED AT AFT CARGO PIT DOOR CUTOUT FWD LWR CORNER STA 950E, STR 26-R REPAIRED FWD LOWER CORNER OF FUSELAGE SKIN AT AFT CAGO DOOR CUT OUT REF EA 7- 5330-123818. BLENDED FOUND OUT OF LIMITS. ORIGINAL .080" , REMAININGSDR FDEA200811194922Seat Track · corrodedSEAT TRACK CORRODED, MAIN DECK AT RBL 24 BS 1148 TO 1176 FABRICATED SEAT TRACK, LOCATED AND DRILLED HOLES, TREATED AND PRIMED NEW SEAT TRACK EXTENSION REF SNRM N00801 SRM 51-30-5, SRM 51-10-2 AND MM 51-20-151-07. CLASSIFIED AS A MAJOR REPAIR.SDR 08FDEA04931Floorbeam · corrodedMAIN DECK 1130 FLOORBEAM UPPER TEE CAP HAS A DOUBLE DRILLED 1/4 INCH RBL 57.5 INCH.SDR 08FDEA04930Seat Track · corrodedMAIN CABIN FLOOR, CORROSION ON SEAT TRACK FROM STA 567-639 LBL 46 REMOVED CORROSION FROM SEAT TRACK ORIGINAL MATERIAL THICKNESS TEE .094 AFTER BLENDING .010 MATERIAL. REMOVED REMAINING .084 AND IS OUT OF LIMITS REF SRM 53-10-1. REMOVED SEAT TRACK REF SRM 51-
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