Boeing 727-228
Service difficulty reports · 1,323
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 = '727228' 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 = '727228' 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 DHL99720007Switch · brokenCARGO DOOR LIGHT ILLUMINATED CARGO DOOR UNLOCK PASSING THROUGH APPROX 9000 AND 6.5 PSI , THEN WENT OUT AT APPROX 16,000 AND 6.2 PSI. STAYED OUT REMAINDER OF FLIGHT. FOUND AFT AUX LATCH PIN SWITCH BROKEN. REPLACED PER PEMCO MM 52-32-21.SDR DHL99724008Bracket · brokenNR 1 KRUEGER FLAP INTRANSIT LIGHT ON DURING RETRACTION AT FLAPS 5 DEGREE. REMOVED AND REPLACED KRUEGER SWITCH ARM BRACKET PER MM 27-82-1, OPS CHECK OK.SDR DHL9972738CFairing · delamiantedAT C CHECK, LWR LT BODY FAIRING AFT OF HYD ACCESS PANEL 3519 DELAMINATED AT LWR I/B END AND ALONG EDGE. ALSO, MISSING TWO FASTENERS. REMOVED LWR LT BODY FAIRING PER SRM 51-30-2, REPLACED MISSING FASTENERS PER SRM 51-30-2, INSTALLED FG OVERLAY REPAIR AS PER SSDR DHL9972734CWeb · crackedAT C CHECK, HORIZONTAL WEB CRACKED AT STA 380 AND STA 386 UNDER ANTENNA PANEL - MOUNTED. CUT OUT DAMAGED AREA PER 51-10-1 1 X 17 AREA ON STA 380 AND 1 X 10 AREA ON STA 386, PERFORMED HFEC INSP PER 727 NDT MANUAL PART 6-51-00-00 FIG 4. NO CRACK INDICATIONS ATSDR DHL9972732CBulkhead Angle · corrodedAT C CHECK, LWR FWD CARGO COMPARTMENT RT BULKHEAD PANEL LWR ATTACH ANGLE HAS CORROSION AT LWR END. CUT OUT CORRODED AREA PER SRM 51-10-1 17, INSTALLED ANGLE REPAIR AT FWD END USING .063 2024T3 17 X 4 PER SRM 51-40-3. ALODINED AND PRIMED PER SRM 51-10-2 N/R SDR DHL9972719CStringer · corrodedAT C CHECK, STA 950 + 10 STR 29L - CORROSION ON O/B HORIZONTAL LEG. REMOVED CORROSION AT STR 29L -.050 REMOVED IS OUT OF LIMITS PER 727 SRM 53-10-1 AT STA 950. INSTALLED EXTERNAL DOUBLER AND TRIPLER SKIN REINFORCEMENT AREA OF STR 29L + FROM BS 950 TO 950 A PSDR DHL9972750CCircumferential · corrodedAT C CHECK, CORROSION ON CIRCUMFERENTIAL WEBS OF 348.2 AND 360 ON SUPPORT WEB AND ANGLE IN BETWEEN CIR RIBS AT APPROXIMATELY STR 20. REMOVED FASTENERS AND REMOVED CORNER BRACKET SUPPORT AND WEB AT B3 360 PER B727 SRM 51-30-2, REMOVED CORROSION ON CIRCUMFERENTSDR DHL9972745CPlenum · corrodedAT C CHECK, CORROSION IN PLENUM ABOVE AND BETWEEN LT SIDE HEAT EXCHANGERS BS 808 LBL 20. REMOVED CORROSION IN PLENUM ABOVE BTW LT SIDE HEAT EXCHANGERS PER SRM 51-10-6. REMOVED .067 FOUND TO BE OUT OF LIMITS PER SRM 57-30-1 FIG 7. FLAP PEENED ALL AREAS PER BSDR DHL99724006Tire · seperatedNR 3 MAIN TIRE RECAP CAME OFF ON LANDING DAMAGE TO RT INBD FLAP, AND NR 3 ENGINE. REMOVED AND REPLACED WHEEL AND TIRE, RT INBD FLAP ASSY AND C-1 FAN .SDR DHL9972755CFrame · corrodedAT C-CHECK, BS 950 A FRAME IS CORRODED FROM STRINGER 28 LEFT TO STR 30 LEFT. REMOVED FLOOR SUPPORT, CUT OUT CORRODED SHEAR TIES, FROM STR 30 TO 28 LEFT, HFEC, COUNTER SINKS AT FRAME PER SRM. INSTALLED SHEAR TIE REPAIR FROM STRINGER 28 LEFT TO 29 PER SRM 53-SDR DHL9972735CPlenum · corrodedAT C CHECK, CORROSION IN PLENUM ABOVE LT PRIMARY HEAT EXCHANGER. REMOVED CORROSION PER B727 SRM 51-10-6, MATERIAL LOSS .060 FOUND TO BE OUT OF LIMITS PER SRM 57-30-1 FIG 9. FLAP PEENED ALL AREA PER OHM 20-10-3, COLD WORKED ALL FASTENER HOLES PER SRM 51-30-10SDR DHL9972706CStringer · corrodedAT C CHECK, STRINGER TIE CORRODED AT STRINGER 30 BS 950A. REPLACED CORREDED STRINGER TIE PER B727 SRM 51-40-3 USING 2024T3 .050 8X5, ALODINED AND PRIMED REPAIR PARTS PER B727 SRM 51-10-2 N/R 3697.SDR DHL9972742CBulkhead Beam · crackedFOUND CRACK AT STA 1183 VERTICAL I BEAM RBL 36.83 O/B FLANGE WL 235. REMOVED FASTENERS AT BS 1183 AFT BLKHEAD VERTICAL BEAM RBL PER SRM 51-30-2, STOP DRILLED IAW NDT MANUAL 51-00-00 PART 6 FIGURE 4. NO FURTHER CRACK INDICATION NOTED. INSTALLED REPAIR KIT ONSDR DHL9972720CSkin · crackedAT C CHECK, FOUND NR 8 SPOILER PANEL CRACKED I/B SIDE. REMOVED AND REPLACED NR 8 SPOILER PANEL IAW MM 27-61-1, ADJUSTED NR 8 PANEL PER MM 27-61-1, OPS CHECKED OK PER MM 27-61-0 NR 2511.SDR DHL9972715CCowl · wornAT C CHECK, NR 1 ENGINE UPPER COWL O/B EDGE IS WORN THRU BETWEEN NR 2 AND NR 3 COWL LATCHES. REMOVED AND REPLACED ANGLE AT NR 1 ENG UPPER COWL O/B EDGE BETWEEN NR 2 AND NR 3 COWL LATCHES PER B727 SRM 51-30-2 MAT USED .030 2024T3 24.5 X 4, TREATED AND PRIMED USDR DHL9972741CSkin · dentedAT C CHECK, MCD MIDDLE STRIKER PLATES DENTED AT STA 540. FABRICATED NR 2 AND NR 3 STRIKER PLATES AT STA 540 AND STA 600 AS PER SRM 51-40-2 USING 301 .25 HARD SS 15 X 58. TREATED AND PRIMED PER SRM 51-10-2, INSTALLED STRIKER PLATES PER SRM 51-30-2, SEALED EDGSDR DHL9972721CMount · crackedAT C CHECK, LEFT WING NR 5 SPOILER MOUNT CRACKED AFT SIDE ON MIDDLE HINGE I/B SIDE. CUT OUT DAMAGED SECTION I/B FLANGE 1 X 1 APPROX AT LT WS 5 SPOILER MOUNT AS PER AVITAS ENG-REPAIR ORDER 99AVHM .061 RO-1 REV 1R, DYE PENETRANT INSPECTED NR 5 SPOILER MOUNT CUTSDR DHL9972756CFloorbeam · damagedAT C-CHECK, STA 328 FLOORBEAM AT LBL 46 HAS FLOOR PANEL SCREW HOLE REWORKED BEYOND LIMITS. CUT OUT 3 PIECE OF FLOORBEAM, INSTALLED REPAIR PARTS PER SRM 53-10-8, 19 X 2 ANGLE 27 X 2.25 N/R 5810.SDR DHL9972718CCowl · wornAT C CHECK, NR 1 UPPER COWL I/B INT EDGE WORN AFT OF NR 2 U BOLT. REMOVED FASTENERS AT NR 1 ENG UPPER COWL I/B INT AFT OF AT U BOLT PER B727 SRM 51-30-2, REWORKED AREA WITH DAMAGED MATERIAL PER SRM 54-10-1, INSTALLED REPAIR PER B727 SRM 51-30-2 USING STAINLESSDR DHL9972717CCowl · crackedAT C CHECK, NR 3 UPPER COWL NR 1 RIB WORN, CRACKED AND HAS JAGGED EDGE AT I/B UPPER END. REMOVED AND REPLACED CHANNEL AT NR 3 ENG UPPER COWL AT NR 1 RIB AS PER B727 SRM 51-30-2 USING 7075-0 16.25 X 5, TREATED AND PRIMED U CHANNEL PER B727 SRM 51-10-2 NR 6366SDR DHL9972716CCowl · dentedAT C CHECK, NR 1 LWR COWL LWR BELLY SKIN BETWEEN RIBS NR 6 AND NR 8 DENTED AND OIL CANNING. CUT OUT DAMAGE AREA AT NR 1 ENG LWR COWL LWR BELLY SKIN BETWEEN RIBS NR 6 NR 8 PER B727 SRM 54-10-3, FIG 5 11 X 16, CLEANED AREA, TREATED AND PRIMED PER B727 SRM 51-10SDR DHL9972708CCowl · missingAT C CHECK, NR 1 UPPER COWL PREVIOUS REPAIR DOUBLER AFT OF NR 4 LATCH CUTOUT MISSING. REPLACED DOUBLER AT NR 1 ENG UPPER COWL AFT OF NR 4 LATCH PER SRM 51-30-2 USING 2024T3 .032 1X8 N/R 6357.SDR DHL9972753CFrame · crackedAT C-CHECK, LWR AFT CARGO STA 980 O/B OF STR 28 RT FUSE FRAME HAD CORROSION AND CRACKS. REMOVED FASTENERS AT STA 980, CUT FRAME WEB AT 975, NO OTHER WEB CORROSION NOTED. FOUND LWR T ANGLE WEB ATTACH CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AT T ANGLE, ASDR DHL9972751CStringer · corrodedAT C CHECK, LOWER AFT CARGO STA 970 BETWEEN STRINGER 28 RIGHT AND 29 RIGHT LOWER CLIPS ON FRAME HAS CORROSION. CUT OUT DAMAGED AREA FOR REPAIR PER SRM 53-10-4 BETWEEN STR 28 & 29, AT STA 970 7 INCHES LONG, FABRICATE NEW L ANGLE REPAIR AT FRAME ATTACH TO STRINSDR DHL9972746CSeat Track · corrodedAT C CHECK, CORROSION ON NR 5 SEAT TRACK THE LAST O/B TRACK ON THE RT SIDE OF CABIN, NEXT TO THE FWD RIGHT EMERGENCY ESCAPE DOOR (WING) STA 760-850. REMOVED SEAT TRACK CAP FROM STA 760 TO 850 AT NR 5 SEAT TRACK PER SRM 51-30-2. REMOVED NR 5 FLOATING SEAT TRACSDR DHL9972728CStringer · damagedAT C CHECK, LOWER AFT CARGO STA 950F STRINGER 28 RIGHT STRINGER TIE TO FRAME DAMAGED. REMOVED DAMAGED STRINGER TIE AT STA 950F, MADE NEW STRINGER TIE PER SRM 51-40-3, USING 2024T3 .050 6 X 4. ALODINED AND PRIMED PER SRM 57-10-2, INSTALLED STRINGER PER SRM 51SDR DHL9972727CClip · crackedAT C CHECK, LOWER AFT CARGO BETWEEN STA 950 E AND E IAW SRM 51-30-2. REMOVED VERTICAL CLIP AT STR 30 BETWEEN STA 950 E AND E PER SRM 51-30-2, ALODINED AND PRIMED AREA PER SRM 51-10-2, REPLACED CLIP AT STR 30 BETWEEN STA 950 E AND E IAW SRM 51-40-3 USING 7075TSDR DHL9972723CStringer · damagedAT C CHECK, DAMAGED STRINGER TIE ANGLE, STIRNGER 28R STA 1010. REMOVED STRINGER TIE ANGLE AT STRINGER 28R STA 1010 IAW B727 51-30-2, FABRICATED NEW STRINGER TIE ANGLE AT STA 1010 STR 28R PER SRM 51-40-3 USING 2024T3 .040 4 X 7, ALODINED AND PRIMED IAW SRM 51-SDR DHL9972714CStringer · crackedAT C CHECK, LOWER AFT CARGO STA 950D AND STRINGER 28 LEFT STRINGER TIE TO FRAME DAMAGE AND CRACKED. REMOVED STR TIE CLIP AT STA 950D PER SRM 51-30-2, FABRICATED NEW STR TIE CLIP PER SRM 51-40-3 USING 2024T3 .040 4X7, ALODINED AND PRIMED PART IAW B727SRM 51-10SDR DHL9972743CS Duct · crackedAT C CHECK, NR 2 ENGINE S DUCT HOUSING LT OUTER SKIN AT BS 1216 HAD 2 INCH CRACK JUST RIGHT UP OF ACCESS PANEL 9523. REMOVED ACCESS PANEL 9523 TO GAIN ENTRY REMOVED ATTACH RING PER SRM 51-30-2 AND REMOVED PREVIOUS REPAIR. STOP DRILLED CRACK IAW SRM 51-10-1. SDR DHL9972710CAngle · misdrilledAT C CHECK, AFT LOWER CARGO FLOOR SUPPORT ANGLE MISS DRILLED HOLE IN RADIUS. INSTALLED ANGLE REPAIR PER SRM 51-40-3 AND 51-30-2 USING 2024T3 .063 ALODINED AND PRIMED PER B727 SRM 51-10-2 N/R 3658.SDR DHL9972709CSkin · elongated holesAT C CHECK, FASTENER HOLES ELONGATED ON RT SIDE VERTICAL FIN L/E PANEL NR 9601. REPLACED PANEL ON LEFT SIDE VERTICAL FIN L/E USING 2024T3 .040 PER B727 SRM 51-30-2 20 X 15 N/R 4388.SDR DHL9972701CSeat Track · crackedAT C CHECK, RT HORIZONTAL STABILIZER SLIDING SEAL AFT TRACK IS CRACKED UPPER SECTION. REPLACE SLIDING SEAL TRACK LWR SECTION RT AFT IAW B727-SRM 51-30-2 N/R 4386.SDR DHL9972758CFrame · crackedAT C-CHECK, RT MLG FS 910 TOP O/B SIDE UPLOCK FWD SUPPORT FRAME CRACKED. STOP DRILLED CRACKS, HFEC, REPAIRED FRAMES FS 910 AND 913 UPLOCK SUPPORT PER S/B 53-165 N/R 2496.SDR DHL9972757CBracket · crackedAT C-CHECK, NR 1 PYLON FWD IND END VERTICAL BRACKET CRACKED AT UPPER I/B END ACCESS PANEL 5407. REMOVED AND REPLACED BRACKET PER SRM 51-30-2, 9 X 4 N/R 6338.SDR DHL9972754CFloorbeam · corrodedAT C-CHECK, STA 340 FLOORBEAM UPPER CHORD HAS CORROSION BEYOND LIMITS FROM LBL 64 TO LBL 19. REMOVED T ANGLE FROM BS 344 FROM LBL 60 TO RBL 60, INSTALLED NEW T ANGLE PER SRM 53-10-2. INSTALLED NEW HAT CHANNEL FROM BS 320 TO 344 RBL 20 PER SRM 53-10-1, 36 INCSDR DHL9972752CBracket · crackedAT C CHECK, NR 1 ENG PYLON FWD I/B END VERTICAL BRACKET CRACKED AT UPPER I/B END ACCESS PANEL 5407. REMOVED THRUST REV SHUTOFF VALVE. REMOVED 6 BOLTS FROM QUADRANT DISCONNECTED THRUST REV QUADRANT DRUM FOR SM ACCESS PER MM 71-11-21. REMOVED AND REPLACED BRASDR DHL9972749CSupport · crackedAT C CHECK, CRACK ON NR 5 L/E FLAP ACTUATOR SUPPORT BRACKET UPPER I/B SIDE BRACKET IN L/E BAY. ACCOMPLISHED PENETRANT INSPECTION AND VERIFIED A CRACK INDICATION ON NR 5 L/E FLAP ACTUATOR SUPPORT BRACKET UPPER I/B SIDE PER STANDARD OVERHAUL MANUAL 20-20-02. RSDR DHL9972748CFrame · crackedRT MLG WW FS 910 TOP O/B SIDE MLG UPLOCK FWD SUPPORT FRAME CRACKED AS VIEWED THROUGH LIGHTENING HOLE WITH MIRROR 6 BELOW PRESS DECK. REMOVED RT GEAR UPLOCK PER MM 32-32-71, REMOVED FASTENERS RT MLG WW FS 910 TOP O/B SIDE FWD SUPPORT MLG UPLOCK PER SRM 51-30-2SDR DHL9972747CSkin · damagedAT C CHECK, RIGHT LANDING GEAR WING DOOR INTERIOR SKIN HAD TWO SMALL GOUGED SPOTS FWD SIDE. BURNISHED TOP GOUGE ON RT MLG DOOR INTERIOR DOOR SKIN PER SRM 51-10-1. MATERIAL LOSS WAS .003 FOUND TO BE WITHIN LIMITS PER SRM 52-00-2. TREATED AND PRIMED TOP AREA SDR DHL9972740CAngle · crackedAT C CHECK, VERT STAB HAS A T ANGLE CRACKED JUST AFT OF RT LWR ICE SHIELD. REMOVED ANGLE AT VERT STAB JUST AFT RT LWR ICE SHIELD AS PER SRM 51-30-2, INSTALLED NEW T ANGLE AT VERT STA JUST AFT RT LWR ICE SHIELD PER SRM 51-30-2 USING 60-3783 8 LONG. ALODINED ASDR DHL9972739CAngle · corrodedAT C CHECK, ANGLE AT STR 19L LOCATION FROM STA 360 TO 356 HAS CORROSION. REMOVED ATTACH T ANGLE STA 360 - 356 FWD OF STR 19 LT AS PER SRM 51-30-2, FABRICATE REPLACEMENT PART PER DWG 65-18420, USING 60-10005 8 LONG USING 7075T7351 IN PLACE OF 7075T6 IAW 99AVHMSDR DHL9972736CAngle · crackedAT C CHECK, CRACKED ANGLE O/B SIDE OF FUELING STATION WEB UPPER ANGLE. REMOVED FASTENERS AND CUT OUT 2 OF DAMAGED AREA ON ANGLE AT O/B SIDE OF FULING STATION PER SRM 51-30-2 AND 51-40-3. ALODINED AND PRIMED REPAIR PARTS AND MATCHING AREA PER SRM 51-10-2, INSSDR DHL9972733CSupport · crackedAT C CHECK, NR 2 ENG TR CASCADE FWD SUPPORT CRACKED AT 9 O'CLOCK POSITION, LEFT CASCADE. REMOVED NR 2 ENG LEFT CASCADE AS REQUIRED BY B727 MM 78-30-22, WELDED NR 2 ENG TR CASCADE SUPPPORT PER BOEING OHM 78-30-02, PG 410A, SECT E PARA A. INSTALLED LT NR 2 ENGSDR DHL9972729CAngle · crackedAT C CHECK, CRACKED ANGLE RT WING L/E 4 I/B OF L/E STA 1307 CRACKED AT THE LOWER CORNER. REMOVED AND REPLACED ATTACH ANGLE SUPPORT AT RT WING L/E 4 I/B OF STA 1307 PER SRM 57-10-1 FIG 1 AND 51-30-2 USING 2024T3 .050 17 X 1 X 1. ALODINED AND PRIMED PER SRM 51SDR DHL9972725CCowl · crackedAT C CHECK, NR 1 ENG INLET COWL O/B AFT END SKIN DAMAGED AT 9 O'CLOCK. CUT OUT DAMAGED AREA OF OUTER SKIN AT NR 1 INLET PER SRM 54-30-3, CLEANED TREATED AND PRIMED AREA PER B727-SRM 51-10-2, INSTALLED REPAIR PARTS PER SRM 54-30-2,FIG 5. MATERIAL USED DOUBLERSDR DHL9972707CSupport · crackedAT C CHECK, NR 1 ENGINE UPPER T/R CASCADE FWD SUPPORT BRACKETS ARE CRACKED AT 11:00 AND 1:00 POSITIONS. WELDED NR 1 ENGINE UPPER T/R CASCADE FWD SUPPORT BRACKETS AT THE 1:00 POSITION PER BOEING OHM 78-30-02 PG 410A SECTION E PARA A NR 6331.SDR DHL9972744CSeat Track · looseAT C CHECK, SEAT TRACKS LBL 48 MISSING ATTACH FASTENERS AT STA 940. REMOVED FASTENERS AT SEAT TRACK LBL 48 FROM STA 950A TO STA 890 PER SRM 51-30-2. FOUND HOLE TO BE IN WRONG LOCATION. INSTALLED NEW CABIN SEAT TRACK LBL 48 PER SRM 53-10-5 FIG 7. ALODINED ASDR DHL9972724CFairing · crackedAT C CHECK, LT WING NR 4 FLAP TRACK ASSY FIXED FAIRING REAR CUT OUT HAVE TWO AREAS WITH MATERIAL DENTED AND CRACKED. ROUTED OUT CRACK AREA ON NR 4 FLAP TRACK FIXED FAIRING PER SRM 51-10-1 MAINTAINED EDGE DISTANCE FOUND TO BE WITHIN LIMITS, REPLACED DENTED RIBSDR DHL9972713CRib · crackedAT C CHECK, LT WING NR 4 FLAP TRACK ASSY FIXED FAIRING MOST FWD RIB CRACKED. REMOVED AND REPLACED FWD RIB AT LT WING NR 4 FLAP TRACK FIXED FAIRING PER B727 SRM 51-10-1 AND 51-30-2. TREATED AND PRIMED PER SRM 51-10-2 N/R 1453.
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