Boeing 727-30C
Service difficulty reports · 931
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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 = '72730C' 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 = '72730C' 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 DHL9970348CBulkhead · damagedAT C CHECK, REPLACED TEMP REPAIR WITH PERMANENT REPAIR BS 870 BULKHEAD WEB. REF: AVITAS ENG LETTER 98 PMS 1.213D-1. REMOVED TEMPORARY REPAIR AT BS 870. REMOVED OLD PRIMER AND PRC AROUND DAMAGED AREA. PERFORMED HFEC INSP OF STOP DRILL AT BS 870 AND WEB IAW NSDR DHL9970347CSkin · damagedAT C CHECK, LT INBD HORIZONTAL STABILIZER LEADING EDGE DAMAGED. REMOVED LEADING EDGE FOR APPROX STA 20 LE TO LE STA 147.32 PER SRM 51-30-2. REMOVED RIBS TO AID IN MAINTAINING CONTOUR OF LEADING EDGE IAW SRM 51-30-2. CUT OUT DAMAGED AREA AT LT LEADING I/B HOSDR DHL9970344CAngle · crackedC-CK, LT WING BS 930 LBL 64 VERT ANG CRACKED. R & R FITTING AT LT STA 930 LBL 64, ALOD & PRIM. INSTALL SPLICES STA 920 STR 15/16 RT. INSTALL REPAIR STR 14 & SUB FLOOR WEBS STA 930-940 & 920-930. REPLACED FLOOR PANEL, INSTALL LT W/W EMERG GEAR EXTEN AND FASSDR DHL9970328CBolts · crackedAT C CHECK, 2 EA SLAT ROLLER BOLTS CRACKED AT LUBE HOLE AND 6 EA SLAT ROLLER BOLTS WORN. REPLACED PER MM 27-81-11, N/R 2074.SDR UPS99230341Skin · corrodedINSPECTION TYPE:C, UPPER FUSELAGE EXTERIOR SKIN IS BULGED AT STR 4 RT TO STR 5 RT BS 480. REMOVED AND REPLACED SKIN FROM BS 440 TO BS 520 FROM STR 10 LT TO 4 RT AND INSTALLED SKIN REPAIR FROM BS 440 TO BS 540 AND FROM STR 4 RT TO STR 5 RT AS PER AVITAS REPAIRSDR UPS99230339Skin · corrodedINSPECTION TYPE:C, UPPER FUSELAGE EXTERIOR SKIN AT SKIN LAP STR 4 RT BS 620 IS BULGED. REMOVED AND REPLACED UPPER FUSELAGE EXTERNAL SKIN FROM BS 520 TO BS 740 FROM STR 6 LT TO 4 RT AS PER AVITAS REPAIR ORDER 99 AVNM 048RO-1, PREVIOSLY ACCOMPLISHED WITH N/R 98SDR UPS99230336Skin · dentedINSPECTION TYPE:C, MAIN CARGO DOOR EXTERIOR SKIN IS DENTED 6 INCHES BELOW THE DOOR HINGE BS 548. REWORKED MAIN CARGO DOOR EXTERIOR SKIN BS 548 AS PER SRM 51-40-1, DENT OUT OF LIMITS. CUT OUT SKIN DAMAGED AREA AS PER B727 SRM 52-00-3, INSTALLED DOUBLER PER B7SDR UPS99230335Skin · corrodedINSPECTION TYPE:C, UPPER FUSELAGE EXTERIOR REPAIR DOUBLER IS BULGED AT STR 5 RT BS 477. REMOVED AND REPLACED UPPER FUSELAGE EXTERIOR SKIN FROM BS 440 TO BS 520 FROM STR 10 LT TO 4 RT AND INSTALLED SKIN REPAIR FROM BS 440 TO BS 540 FROM STR 4 RT TO 5 RT AS PERSDR UPS99230332Skin · corrodedINSPECTION TYPE:C, UPPER FUSELAGE EXTERIOR SKIN IS BULGED FROM STR 1 TO STR 4 RT BS 620. REMOVED AND REPLACED UPPER FUSELAGE EXTERIOR SKIN FROM BS 520 TO BS 740 FROM STR 6 LT TO 4 RT AS PER AVITAS REPAIR ORDER 99 AVHM 048RO- 1. PREVIOUSLY ACCOMPLISHED WITH NSDR DHL9970329CSkin · crackedAT C CHECK, RT WING FIXED LEADING EDGE CUT OUT FOR THE NR 5 SLAT INBD TRACK IS CRACKED. REMOVED SEALS TO GAIN ACCESS TO BACKSIDE OF LEAD EDGE OF WING PER SRM 57-30-4, MADE EXTERNAL DOUBLER PICKED UP EXISTING HOLES 2 EA NEW HLOES ONTO NEW DOUBLER PER SRM 57-30SDR DHL9970330CHinge · crackedAT C CHECK, LW NR 7 SPOILER PANEL CENTER HINGE CASTING OUTBOARD LEG CRACKED AT AFT HOLE. CUT OUT CRACK FROM HINGE CASTING 2 LONG PER SRM 51-10-1, DYE PENETRANT INSPECTED CUTOUT PER MIL 68-66B. NO CRACK NOTED, INSTALLED FILLER AND REINFORCING STRAP AT LEFT WISDR DHL9970317CTail Cone · delaminatedAT C CHECK, TAIL CONE HAS DELAMINATION AT LEFT TOP AREA. REMOVED VERTICAL STABILIZER TAILCONE PER SRM 51-30-2. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8 FIG 1, USED RESIN 50-A AND CLOTH STYLE 720 10 INCH BY 6 INCH, PRIMED ALL REAS PER SRM 51-10-2.SDR DHL9970345CDoor · corrodedAT C CHECK, GALLEY DOOR UPPER FLAP HINGE HAS CORROSION. REMOVED GALLEY DOOR UPPPER FLAP PER MM 20-10-1. INSTALLED GALLEY DOOR UPPER FLAP (GATE ASSY) PER MM 52-12-0. REMOVED AND REPLACED PIN STOP ON GALLEY DOOR UPPER FLAP PER 52-12-0. SEALED OUTSIDE OF DOORSDR DHL9970332CBulkhead Panel · crushedAT C CHECK, RT BS 1183 BULKHEAD PANEL IS CRUSHED AT LOWER END. REPLACED RT STA 1183 BLKHD PANEL PER 53-20-11 MATERIAL USED P/N AE4155-81162, APPROXIMATELY 7X4N/R 5118.SDR DHL9970331CMount · crackedAT C CHECK, ENGINE NR 1 GEARBOX FWD MOUNT CRACKED. REMOVED G/B PER MM-72-00, INSTALLED O/H G/B PER MM-72-0. INSTALLED FUEL LINE FROM FUEL OIL COOLER PER MM 28-40-3, LEAK CHECK, NO LEAK FOUND. OPS CHECKED ENGINE RUN AND TRIM, N/R 6179.SDR DHL9970325CLongeron · crackedAT C CHECK, NR 1 LOWER COWL OUTBOARD LONGERON IS CRACKED UNDER RUB PLATE BY NR 3 LATCH V-BOLT CUTOUT. ALSO, SKIN IS BENT AND CRACKED AROUND CUTOUT. REWORKED SKIN AT NR 1 ENG LOWER COWL NR 3 LATCH U-BOLT CUT OUT PER SRM 51-10-1. NO SIGNIFICANT MATERIAL LOSSSDR DHL9970320CSkin · corrodedAT CHECK, RT WING UPPER SURFACE SKIN BULGES ALONG ROW OF FASTENERS JUST FWD OF THE NR 8 SPOILER PANEL. REMOVED PANEL FOR REAIR, CLEANED MATING SURFACE ON WING, NO CORROSION NOTED, TREATED AND PRIMED AREA PER SRM 51-10-2. INSTALLED BONDED REPAIR AT R/WING UPPSDR DHL9970319CBracket · crackedAT C CHECK, FWD CARGO DOOR UPLOCK SUPPORT BRACKET IS CRACKED. REMOVED FWD CARGO DOOR UP LOCK SUPPORT BRACKET PER SRM 51-30-2. REPLACED FWD CARGO DOOR UPLOCK SUPPORT BRACKET PER SRM 51-30-2 AND 51-40-2, MATERIAL USED 2024T3 .040 6 BY 3, ALODINED AND PRIMED PESDR DHL9970318CStructure · crackedAT C CHECK, FWD ENTRY DOOR INTERIOR FWD UPPER CORNER IS CRACKED. REMOVED INTERIOR FWD ENTRY DOOR PER SRM 51-30-2, FABRICATED NEW LINER SUPPORT FWD CORNER PER SRM 52-10-1 FIG 1 USED .050 2024-0 HEAT TREATED TO 2024T3 PER 99PMSI 247 PG-01. ALODINED AND PRIMED PSDR DHL9970316CFairing · delaminatedAT C CHECK, V STABILIZER HAS FAIRING DELAMINATED ON BOTH SIDES BELOW TAIL CONE. INSTALLED BONDING REPAIR AT VERTICAL STABILIZER FAIRINGS BELOW TAIL CONE PER SRM 51-20-3 FIG 1, MATERIAL USED EPOCAST 1652 A/B, N/R 4127.SDR DHL9970314CCowl · chaffAT C CHECK, NR 1 TOP COWL OUTBOARD LONGERON HAS DEEP CHAFED SPOTS AT 46 AND 54 INCHES FROM AFT EDGE. REPLACED COLGERON SECTION PER SRM 51-40-2 AND 54-10-2 ON NR 1 TOP COWL, USED 2024T3 .050 20 BY 4, TREATED AND PRIMED AREA PER SRM 51-10-2, N/R 6206.SDR DHL9970313CSkin · chafedAT C CHECK, ENGINE NR 2 FWD RT COWL LOWER FWD INSIDE CORNER DOUBLER CHAFFED THROUGH. REMOVED FASTENER AND DAMAGED DOUBLER PER SRM 51-30-2, CLEANED AND PRIMED ARE PER SRM 51-10-2. REPLACED DOUBLER PER SRM 51-30-2 USED .040 14 BY 5 2024-0 HEAT TREATED TO 2024TSDR DHL9970310CDepressor · damagedAT C CHECK, SEAL DEPRESSOR AT MCD AFT OF NR 6 LATCH HAS A SQUARE .25 OF MATERIAL MISSING REQUIRES REPAIR. SMOOTHED DAMAGED SECTION PER SRM 51-40-1. ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED L ANGLE REPAIR PER SRM 51-40-3 FIG 1 USING .063 2024-0 HEAT TSDR DHL9970308CPanel · crackedAT C CHECK, V STAB ACCESS PANEL NR 9774 HAS REPAIRS CRACKING UP L/S. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8 FIG 1 USING RESIN 1304, 6 INCH BY 4 INCH, N/R 4128.SDR DHL9970305CFairing · corrodedAT C CHECK, LEFT WING NR 1 MOVABLE FAIRING SKIN CORRODED AT FWD I/B SIDE AT FAIRING ATTACH POINT. REMOVED PAINT FROM SKIN CORRODED AREA PER MM 51-20-0, CUT 6 INCH BY 5 INCH SECTION OF SKIN AWAY AND INSTALLED REPAIR SKIN AND SPLICE PLATE PER SRM 53-50-1 FIG 1 SDR DHL9970340CCarriage · looseLS NR 4 FLAP CARRIAGE HAS THRUST NUT LOOSE, IT HAS EXCESS CLEARANCE BETWEEN SHIMS AND FLAP FITTING. REMOVED LEFT INBOARD FLAP ASSY PER MM 27-51-3. FOUND LEFT INBOARD THRUST BEARING CASTING OUT OF LIMITS PER MM 27-51-3. REMOVED CARRIAGES FROM OLD FLAP AND TRSDR DHL9970339CAngle · crackedAT C-CHECK, LEFT WING LEADING EDGE CAVITY AREA FSS 115.0 VERTICAL ANGLE CRACKED LOSER SECTION. CUTOUT DAMAGED SECTION 3 BY 2 PER SRM 51-40-3. FABRICATED NEW VERTICAL ANGLE PER SRM 51-40-3 FIGURE 1, MATERIAL USED 7075-0 .071 3 BY 8, .375 INCH, HEAT TREATED 7SDR DHL9970327CSkin · damagedAT C CHECK, LW TOP SKIN PANEL HAS FIBERGLASS REPAIR NOT FINISHED BETWEEN WING AND FUSELAGE. REMOVED LW TOP SKIN PANEL LOCATED BETWEEN WING AND FUSELAGE PER SRM 51-30-2. INSTALLED BONDED REPAIR AT LW TOP PANEL PER SRM 51-40-6 FIG 1 MAT USED 2024 T3 .020 , 202SDR DHL9970326CStiffener · crackedAT C CHECK, LW VERT STIFFENER IS CRACKED AT LOWER END AT FALSE SPAR BELOW NR 5 SPOILER O/B SIDE. STOP DRILLED 1 CRACK PER SRM 57-50-6. REMOVED APPROX 6 OF FASTENERS PER SRM 57-50-6, MADE NEW L ANGLE DOUBLER PER SRM 57-50-6. PICKED UP EXISTING FASTENER HOLESDR DHL9970323CBolt · shearedAT C CHECK, LT WING NR 3 LE SLAT ACTUATOR TIE DOWN BOLT IB LOWER BOLT SHEARED. REPLACE THE IB LOWER BOLT ON NR 3 LE SLAT ACTUATOR PER MM 20-80-1, N/R 1199.SDR DHL9970322CSkin · corrodedAT C CHECK, RT WING INBOARD FORE FLAP HAS SURFACE CORROSION ON LOWER SKIN APPROXIMATELY 12 FROM OUTBD END. REMOVED CORROSION AT RT WING PER SRM 51-10-6, OUT OF LIMITS PER SRM 57-50-1 FIG 3 DETAIL 3. INSTALLED FG OVERLAY REPAIR PER SRM 51-40-8 FIG 1 ON RT WINSDR DHL9970321CSkin · delaminatedAT C CHECK, RT WING UPPER SURFACE SKIN BULGES ALONG PANEL 10 FORWARD OF NR 9 AND NR 10 SPOILER PANEL. REMOVED FASTENERS AT RT WING PANEL PER SRM 51-30-2. FOUND DELAMINATED SKIN IN UPPER PANEL, CLEANED MATING SURFACE ON AIRCRAFT TRATED AND PRIMED. NO CORROSISDR DHL9970315CPlate · crackedAT C CHECK, MAIN CARGO DOOR INTERIOR LOWER PLATE COVER FWD TO AFT SECTION HAS SEVERAL CRACKS AND DENTS ON SURFACE. REMOVED PLATE AT MAIN CARGO DOOR INTERIOR LOWER PLATE COVER REPAIRED PER SRM 51-30-2 AND 51-10-1. ALODINED AND PRIMED PER SRM 51-10-2 USED 2024SDR DHL9970312CLongitudinal · crackedAT C CHECK, E3 ELECTRONIC RACK UPPER RT LONGITUDINAL IS CRACKED 2 PLACES. STOP DRILLED CRACKS PER SRM 51-10-1 2 PLACES. INSTALLED DOUBLER PER SRM 51-40-2 FIG 1 USING 2024T3 .050 6 BY 4 2 EA, ALODINED AND PRIMED PER SRM 51-10-2, N/R 3126.SDR DHL9970309CFloor · crackedAT C CHECK, NOSE W/W PRESS FLOW HAS CRACK AT BS 284.5. REMOVED FLOOR PANEL AT FWD PER SRM 51-30-2. REMOVED 2 EACH OLD DOUBLERS PER SRM 51-30-2. CUT OUT DAMAGED AREA AT BS 284.5 4 BY 1 PER S/B 53-0145, HFEC INSPECTED CUTOUT IAW 51-00-0 FIG 4. NO CRACKS NOTESDR DHL9970307CAngle · crackedAT C CHECK, RT WING TRAILING EDGE COVER PANEL INBOARD SUPPORT ANGLE IS CRACKED AT WS 447.90 JUST INBOARD OF NR 11 SPOILER ACTUATOR. REMOVED AND REPLACED SUPPORT ANGLE AT RT WING AT WS 447.90 PER SRM 51-10-1 PAR 4 AND 51-30-2, N/R 2044.SDR DHL9970302CAngle · crackedAT C CHECK, RT WING TRAILING EDGE COVE PANEL OUTBOARD SUPPORT ANGLE IS CRACKED AT WS 498.08 INBOARD OF THE NR 12 SPOILER ACTUATOR. REPLACED COVER PANEL OUTBRD SUPPORT WS 498.08 PER SRM 51-30-2, 51-10-1 PAR 4 N/R 2045.SDR DHL9970301CCircumferential · crackedAT C CHECK, FWD CARGO COMPT, CRACK AT CIRCUMFERENTIAL STA 640 STRINGER 26L. REMOVED OLD REPAIR, STOP DRILLED CRACK, HFEC. INSTALLED REPAIR PARTS PER SRM 53-10-4, 12 BY 6, N/R 3121.SDR DHL9970338CBulkhead · crackedAT C-CHECK, CRACK AT 1183 BULKHEAD SKIN AFT CARGO COMPT WL 172 RBL 8. REMOVED FASTENERS AND STOP DRILL CRACK AT 1183 BLKD WL 172 RBL 8. PERFORMED HFEC INSPECTION PER NDT MANUAL PART 6 51-00-00 FIG 4. NO CRACK IND PAST STOP DRILLS, CUT OUT DAMAGED AREA PER SSDR DHL9970311CReceptacle · crackedAT C CHECK, BARRIER NET ATTACH RECEPTACLE AT BS 364 BETWEEN STRINGERS 5L AND 6L UPPER MOUNT BRACKET MISSING ATTACH RIVET AND CRACKED. REMOVED BRACKET SUPPORT PER SRM 51-30-2. REPLACED BRACKET SUPPORT PER SRM 51-30-2 USED 7075T0 .071 AND 2024T3 .050, ALODINEDSDR DHL9970304CTab · delaminatedAT C CHECK, L/W OUTBOARD AILERON TAB, HAS ON TOP LEADING EDGE A METAL LIFTING UP AT I/B SIDE. REPLACED LEADING EDGE METAL COVER OF L/W O/B AILERON AT LEADING EDGE INBOARD SIDE OF TAB PER SRM 57-50-2 FIG 8 AND 51-30-2 USING .020 2024-T3 1.5 BY 7, ALODINED PRIMSDR DHL9970306CTip · crackedAT C CHECK, LEFT WING TIP AFT O/B EDGE AREA CRACKED IN TWO PLACES. REMOVED LEFT WING TIP OUTBOARD EDGE FOR REPAIR IAW SRM 51-30-2. STOP DRILLED CRACK AT TWO PLACES IAW SRM 51-10-1, PERFORMED HFEC IAW NDT PART 68-00-00 FIG 4. NO CRACKS NOTED BEYOND STOP DRILSDR DHL9970346CLink · corrodedAT C CHECK, L/W NR 5 SPOILER ACTUATOR GRAY LINK HAS CORROSION INSIDE WING CAVITY. REMOVED LW NR 5 SPOILER ACTUATOR GREY LINK PER MM 57-55-00. REPLACE ACTUATOR LINK PER MM 27-61-81, OPS CHECKED GOOD IAW 27-61-0 N/R 1153.SDR DHL9970324CAttachment · crackedAT C CHECK, LT WING I/B AILERON BALANCE PANEL AFT HINGE ATTACHMENT CRACKED. REMOVED AND REPLACED LT WING I/B AILERON BALANCE PANEL AFT HINGE ATTACHMENTPER MM 27-10-21, N/R 1107.SDR DHL9970303CFairing · crackedAT C CHECK, LEFT WING NR 1 MOVABLE FAIRING GOUGED AT PREVIOUS REPAIR INNER SECTION. REMOVED PAINT FROM REPAIR AREA, REPLACED PREVIOUS REPAIR (5 BY 12) PER SRM 57-20-2 AND SRM 51-40-2, ALODINED AND REPRIMED PER SRM 51-10-2, N/R 1103.SDR DHL99701001Motor · leakingHAD A SYSTEM HYDRAULIC FAILURE. FOUND OUTBD FLAP POWER UNIT HYDRAULIC MOTOR LEAKING. REMOVED AND REPLACED PER MM 27-51-62 LEAK CHECK GOOD SERVICED SYSTEM.SDR DHL9970203CFrame · crackedC CHECK, NR 1 ENGINE UPPER COWLING NR 14 FRAME HS EVIDENCE OF HEAVY CHAFING UNDER IMPROPER STRAP REPAIR AT 1/B FLANGE, AT O/B AFT CORNER OF COWL. REMOVED REPAIR, INSTALLED REPAIR PER SRM 54-10-3, 6 BY 3 N/R 6095.SDR DHL9970244CSeat Track · crackedC CHECK, LWR AFT CARGO COMPARTMENT RT SEAT TRACK CRACK AT BOTH FWD AFT ENDS. REPLACED DAMAGE SECTION OF SEAT TRACK FROM STA 950 TO STA 1030; INSTALLED REPAIR AT STA 1030 AS PER B7272 SRM 53-10-5 FIG 8 MAT USED BAC1520-843 80 LOT NR 148462-1 PO NR 8314055; REPSDR DHL9970214CSkin · crackedC-CHECK, CRACK INDICATION AT FASTENER ONE INCH RIGHT OF (BLO) STA 480. CUT-OUT DAMAGED AREA OF SKIN AT FWD SIDE STA 480 PRODUCTION BREAK BETWEEN BLO AND STR 28R 4.0 BY 2.0 IAW B727 S/B 727-53-0084 DRAWING NO69-62161 SHEET 2. ALODINED AND PRIMED AREA IAW B727SDR DHL9970211CSkin · corrodedC CHECK, PLUS 10 PERCENT MATERIAL LOSS AT STA 259 CIRCUIT BUTT SEAM APPRX S-9L LOCTION. INSTALLED DOUBLER REPAIR AT BS 259 STR 9L PER B727 S/B 727-53-0084 ALODINED AND PRIMED ALL PARTS AND AREA PER B727 SRM 51-10-2 MAT USED. FILLER .050 2024T3 21 BY 4 APPROX
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