Boeing 727-25

Service difficulty reports · 827

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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 = '72725'
  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.

SDR DHL9670824CSkin · corrodedAT C-CHECK, MATERIAL LOSS NOTED AT BS 360 BETWEEN STR R 19 AND STR R 23 FWD SIDE OF BS 360. REMOVED DAMAGED SECTION STA 338 TO 360, STR 19 TO STR 24, 22 INCHES BY 42 INCHES. ACCOMPLISHED SKIN SPLICE IAW AVITAS EO 96 PMSI 129RO-2.Sep 6, 1996 · N708DH · Boeing 72725 · Fuselage Main, Plate/SkinSDR DHL9670820CFloorbeam · corrodedAT C-CHECK, FWD CARGO COMPT STA 600 CABIN FLOORBEAM HEAVILY CORRODED LBL 12 TO 16. INSTALLED REPAIR PER SRM 53-10-8, 2 ANGLES 40 INCHES, STRAP 2 INCHES BY 36 INCHES AND T-ANGLE 29 INCHES.Sep 6, 1996 · N708DH · Boeing 72725 · Fuselage Main, Floor BeamSDR DHL9670815CRib · crackedAT C-CHECK, CRACKS FOUND AT WING STA 738.5 RIB AT LWR STR 6 AND UPPER STR 14. STOPPED DRILLED CRACKS, INSTALLED REPAIR AT STR 14 PER SRM 57-10-5, 10 INCHES LONG. INSTALLED REPAIR AT STR 6 PER SRM 57-10-5, 10 INCHES LONG.Sep 6, 1996 · N708DH · Boeing 72725 · Wing, Rib/BulkheadSDR DHL9670810CRib · crackedAT C-CHECK, WING RIB AT STA 601.5 HAS CRACKS AT LOWER STR 6, 8 AND TOP STRINGER 11. REMOVED AND REPLACED WING RIB AT STA 601.5 PER S/B 57-127.Sep 6, 1996 · N708DH · Boeing 72725 · Wing, Rib/BulkheadSDR DHL9670809CRib · crackedAT C-CHECK, INSPECTION REVEALED WING RIB AT WS 656.5 HAS CRACK AT LOWER STR 6, 8 AND TOP STR 9 AND 13. REMOVED AND REPLACED RIB PER S/B 57-127.Sep 6, 1996 · N708DH · Boeing 72725 · Wing, Rib/BulkheadSDR DHL9670803CRib · crackedAT C-CHECK, RIGHT WING RIB CRACKED AT WS 546.5 STR 7 AND STR 8. STOP DRILLED CRACKS, INSTALLED RIB REPAIR PER S/B 57-0127, 3.125 INCHES BY 17 INCHES.Sep 6, 1996 · N708DH · Boeing 72725 · Wing, Rib/BulkheadSDR 96FDEA01442Floorbeam · corrodedNR 0446 AND 005, CORROSION (C53-111-01, -2) ON LOWER CHORD OF FLOORBEAM AT BS 600 LBL 15 WL 200. *S/D* REMOVED AND REPLACED FLOORBEAM LOWER CHORD STA 600 LBL TO RBL 25 WL 200 PER FEDEX SRM 53-10-8 FIG 2.Sep 6, 1996 · N510FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA01438Floorbeam · corrodedNR 0285 AND 004, CORROSION (C53-224-02) ON 344 FLOORBEAM RBL 18 TO LBL 65 WL 208, OUT OF LIMITS. *S/D* REMOVED CORROSION ON BS 344 FLOORBEAM RBL 18 TO LBL 65 WL 208. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM UPPER CHORD RBL 70 TO LBL 70 IASep 6, 1996 · N510FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA01437Floor Beam · corrosionNR 0292 AND 003, CORROSION (C53-224-01, -3) AROUND NUTPLATE HOLES ON BS 1030 UPPER CHORD RBL 21 TO LBL 21 WL 208. *S/D* REPAIRED OUT OF LIMITS UPPER CHORD IAW FEDEX SRM 53-10-8.Sep 6, 1996 · N510FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA01436Skin · delaminatedNR 0196 AND 002, LT WING I/B FORE FLAP HAS A LARGE CREASED DENT MID SPAN UPPER SURFACE WBL 203.0. *S/D* LT WING I/B FORE FLAP REPAIRED PER FDEA SRM 51-40-6.Sep 6, 1996 · N510FE · Boeing 72725 · Trailing Edge FlapsSDR DHL9670831CFrame · misdrilledAT C-CHECK, MISDRILLED HOLES INTO RADIUS OF LEFT FRAME I/B FLANGE AT BS 760.5 ABOVE FLOOR LINE. INSTALLED REPAIR PER S/B 53-197Sep 5, 1996 · N708DH · Boeing 72725 · Fuselage Main, FrameSDR DHL9670830CFrame · drilledAT C-CHECK, FOUND MISDRILLED HOLES INTO RADIUS ON FRAME I/B FLANGE AT BS 848 RIGHT SIDE 4 INCHES ABOVE FLOOR LINE. INSTALLED REPAIR KIT 65C36282-2 PER S/B 53-197.Sep 5, 1996 · N708DH · Boeing 72725 · Fuselage Main, FrameSDR DHL9670829CSkin · crackedAT C-CHECK, FUSELAGE EXTERIOR SKIN CRACKED AROUND FASTENER AT BS 211.9 RIGHT SIDE APPROX WL 210. CUT OUT DAMAGED AREA, FABRICATED DOUBLER REPAIR PER SRM 53-30-3 18 INCHES BY 15 INCHES.Sep 5, 1996 · N708DH · Boeing 72725 · Fuselage Main, Plate/SkinSDR DHL9670822CFitting · crackedAT C-CHECK, BS 950 FITTING ON LEFT SIDE HAS A 11 INCH CRACK AROUND BOSS FOR UPPER SEGMENT AFT BEARING. REMOVED AND REPLACED FITTING PER S/B 53-196 AND S/B 53-126.Sep 5, 1996 · N708DH · Boeing 72725 · Fuselage Miscellaneous StructureSDR DHL9670804CFrame · crackedAT C-CHECK, CABIN FRAME AT STA 620 CRACKED AND DAMAGED AT PREVIOUS REPAIR RT SIDE FWD OF MID GALLEY DOOR JUST ABOVE FLOOR LEVEL. CUT OUT DAMAGED AREA OF FRAME, INSTALLED REPAIR DOUBLER STA 620 PER SRM 53-10-4, 13 INCHES BY 8 INCHES.Sep 5, 1996 · N708DH · Boeing 72725 · Fuselage Main, FrameSDR DHL9670801CDoor Frame · crackedAT C-CHECK, GALLEY DOOR CUTOUT AT FS 635 DAMAGED AND CRACKED JUST ABOVE FLOOR LEVEL. INSTALLED FRAME REPAIR PER SRM 53-10-4. REPAIR SIZE 8 INCHES BY 6 INCHES BY 2 INCHES.Sep 5, 1996 · N708DH · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA01433Wedge · delaminationNR 0175 AND 001, RT WING O/B MID FLAP T/E WEDGE DELAMINATED MARKED. *S/D* REMOVED AND REPLACED DAMAGED SKIN ON RT WING O/B MID FLAP T/E WEDGE IAW FDEA SRM 51-40-6.Sep 5, 1996 · N510FE · Boeing 72725 · Trailing Edge FlapsSDR DHL9670823CRib · crackedAT C-CHECK, RIB CRACKED AT WS 738.5, 2 CRACKS IN LOWER FLANGE AT STR 6 AND BETWEEN STR 6 AND 8 AND UPPER RIB AT STR 12. REMOVED AND REPLACED RIB PER 57-127.Sep 4, 1996 · N708DH · Boeing 72725 · Wing, Rib/BulkheadSDR DHL9670819CRib · crackedAT C-CHECK, INSPECTION OF RIGHT WING SHOWS CRACKS AT STR 11 AND 15 UPPER AND 8 AND 9 LOWER, STA 629.0. REMOVED AND REPLACED RIB PER S/B 57-127.Sep 4, 1996 · N708DH · Boeing 72725 · Wing, Rib/BulkheadSDR DHL9670808CRib · crackedAT C-CHECK, INSPECTION REVEALED CRACKS AT RIB UPPER FLANGE AT STR 13 AND 14 AND LOWER FLANGE AT STR 8 WS 686.5. INSTALLED REPAIRS PER S/B 57-0127, UPPER REPAIR 15 INCHES BY 3.5 INCHES, LOWER DOUBLER 8 INCHES BY 3.5 INCHES.Sep 4, 1996 · N708DH · Boeing 72725 · Wing, Rib/BulkheadSDR DHL9670805CRib · crackedAT C-CHECK, WING RIB CRACKED AT LOWER FLANGE AT STA 601.5, STR 7. STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR AT LOWER FLANGE PER SRM 57-10-5, 15 INCHES BY 5 INCHES.Sep 4, 1996 · N708DH · Boeing 72725 · Wing, Rib/BulkheadSDR DHL9670802CSeat Track · corrodedAT C-CHECK, FWD BAGGAGE COMPT HAS SEAT TRACK CORROSION AT STA 615. REPLACED FWD BAGGAGE SEAT TRACK FROM STA 580 TO 700, PER SRM 51-10-1.Sep 4, 1996 · N708DH · Boeing 72725 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9670812CBulkhead Channel · corrodedAT C-CHECK, FWD NOSE COMPT STA 227 BULKHEAD VERTICAL CHANNEL HAS CORROSION STARTING FROM BILGE CENTER LINE. REMOVED AND REPLACED VERTICAL CHANNEL PER SRM 51-10-1.Sep 3, 1996 · N708DH · Boeing 72725 · Fuselage Main, BulkheadSDR 96FDEA01425Frame · corrodedNR 0514 AND 013, CORROSION (C53-221-01) ON FRAME BS 235 LBL 45 WL 217.Sep 3, 1996 · N509FE · Boeing 72725 · Fuselage Main, FrameSDR 96FDEA01424Chord · corrosionNR 0394 AND 012, CORROSION (C53-224-01, -2) ON BS 1176.9 CHORD AT RBL 1 TO 6 AND LBL 10 TO 4 OUT OF LIMITS WL 208. *S/D* CORROSION FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED DAMAGED CHORD AS PER SERVICE BULLETIN NR 727-53-0184 METHOD 3 AND DROWING 65C335Sep 3, 1996 · N509FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR DHL9670821CWeb · corrodedAT C-CHECK, NOSE WHEEL WELL HAS EXFOLIATION CORROSION AT BS 298 BL 0 TO RBL 6, HORIZONTAL WEB OF DOG HOUSE. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 53-10-9, 11 INCHES BY 15 INCHES.Sep 2, 1996 · N708DH · Boeing 72725 · Fuselage Miscellaneous StructureSDR DHL9670818CAngle · crackedAT C-CHECK, NR 7 SLAT ACTUATOR, INBD TRUNNION VERT ANGLE AT FWD SPAR, STAINLESS DOUBLER HAS CRACK BEYOND STOP DRILL. FABRICATED ANGLE 1 INCH BY 35 INCHES PER S/B 57-0130, FABRICATED DOUBLER PER S/B, 8 INCHES BY 3.5 INCHES AND INSTALLED PER SRM 51-30-2 AND S/Sep 2, 1996 · N708DH · Boeing 72725 · Leading Edge Slat ActuatorSDR DHL9670806CSupport Beam · crackedAT C-CHECK, LEFT CORNER OF NLG SUPPORT BEAM IS CRACKED OUTSIDE OF REPAIR AND PAST STOP DRILL. ACCOMPLISHED REPAIR PER S/B 53-108 AND DRAWING 65C15312. REPAIR 9 INCHES BY 10 INCHES.Sep 2, 1996 · N708DH · Boeing 72725 · Fuselage Miscellaneous StructureSDR DHL9670827CMount · crackedAT C-CHECK, NR 2 LEADING EDGE FLAP ACTUATOR MOUNT CRACKED ON INBD SIDE TOP AND BOTTOM. REMOVED AND REPLACED ACTUATOR MOUNT PER SRM 51-10-1.Sep 1, 1996 · N708DH · Boeing 72725 · Leading Edge Slat ActuatorSDR DHL9670807CSkin · dentedAT C-CHECK, FUSELAGE SKIN DENTED AT STA 228 AT STR 26 RT. CUT OUT DAMAGED AREA, INSTALLED PER SRM 53-30-3. FILLER 3 INCHES BY 2 INCHES, 10 INCHES BY 10 INCHES AND DOUBLER 10 INCHES BY 10 INCHES .Sep 1, 1996 · N708DH · Boeing 72725 · Fuselage Main, Plate/SkinSDR DHL9670834CTrunnion · crackedAT C-CHECK, INSTALLED PERMANENT REPAIR OF NOSE GEAR LT TRUNNION AFT SIDE. REMOVED AND REPLACED TRUNNION PER S/B 53-119.Aug 31, 1996 · N708DH · Boeing 72725 · Nose/Tail Landing Gear Attach SectionSDR DHL9670826CRib · crackedAT C-CHECK, LEFT WING RIB UPPER CHORD AT BL 70.5, SHOWED CRACK INDICATIONS IN VERTICAL FLANGE DURING HFEC INSPECTON. TRIMMED AREAS PER BOEING INSTRUCTIONS. HFEC TRIMMED EDGES AND FASTENER HOLES COMMON TO REPAIR AREA. INSTALLED REPAIR PER S/B 57-112 AND BOEIAug 31, 1996 · N708DH · Boeing 72725 · Wing, Rib/BulkheadSDR DHL9670825CSkin · damagedAT C-CHECK, EFFECT PERMANANT REPAIR ON LT OUTBOARD AILERON TRAILING EDGE. INSTALLED BONDING REPAIR PER SRM 51-40-6 AND REPLACED SKIN LOWER SURFACE, SIZE 43.5 INCHES BY 7 INCHES. CHECK BALANCE PER SRM 51-80-4.Aug 31, 1996 · N708DH · Boeing 72725 · AileronsSDR 96FDEA01421Stick Shaker · failed testCONTINUOUS STICK SHAKER AT TAKEOFF. STANDARD POWER TAKEOFF 36C, ADVANCED THROTTLES TO MOMENTARY FIREWALL POWER. PULLED AC NR 1 STALL WARNING CIRCUIT BREAKER, SHAKER STOPPED. ATTEMPTED 1 RESET OF CIRCUIT BREAKER, STILL HAD SHAKER. PULLED CIRCUIT BREAKER ANDAug 30, 1996 · N136FE · Boeing 72725 · Airspeed/Mach IndicatorSDR DHL9670811CSkin · dentedAT C-CHECK, FUSELAGE SKIN DENTED AT BS 1130 BETWEEN S-8 AND S-17 LT. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 53-30-3, 9 INCHES BY 12 INCHES.Aug 29, 1996 · N708DH · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA01491Clip · brokenNR 0219 AND 010, STRINGER CLIP AT BS 640 STRINGER 19 RT IS BROKEN. REMOVED DAMAGED STR CLIP AND INSTALLED NEW STR CLIP BS 640 STR 19 RT.Aug 29, 1996 · N509FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA01417Skin · delaminationNR 0520 AND 011, RT WING I/B AFT FLAP O/B AFT CORNER HAS APPROX 60 SQ INCHES OF DELAMINATION. *S/D* RT WING I/B AFT FLAP O/B AFT CORNER REPAIRED IAW FED EX SRM 51-40-6.Aug 29, 1996 · N509FE · Boeing 72725 · Trailing Edge FlapsSDR 96FDEA01416Clip · brokenNR 0219 AND 010. STRINGER CLIP AT BS 640, STRINGER 19 RT IS BROKEN. REMOVED DAMAGED STR CLIP AND INSTALLED NEW STR CLIP, BS 640, STR 19 RT HAND.Aug 29, 1996 · N509FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA01409Flap · corrodedNR 0441 AND 006, CORROSION AT NR 1 K-FLAP.Aug 27, 1996 · N509FE · Boeing 72725 · Leading Edge DevicesSDR 96FDEA01408Chord · corrodedNR 0544 AND 005, CORROSION BETWEEN UPPER 870 VERTICAL FLANGE OF CHORD AND 870 WEB LBL 12 TO 20. *S/D* REMOVED CORROSION ON VERTICAL FLANGE OF 870 CHORD FOUND TO BE WITHIN LIMITS PER FED EX SRM 57-10-1. REPAIRED 870 WEB PER FED EX SRM 57-10-6 FIG 1.Aug 27, 1996 · N509FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 96FDEA01407Stringer · crackedNR 0451 AND 004, WHILE WORKING NR 0219 FOUND STRINGER 19 RT AT BS 640 TO BE CRACKED.Aug 27, 1996 · N509FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 96FDEA01406Frame · damageNR 0357 AND 003, DAMAGE FRAME AT BS 580 RBL 18 WL 156.Aug 27, 1996 · N509FE · Boeing 72725 · Fuselage Main, FrameSDR 96FDEA01399Floor Beam · corrodedNR0456, CORROSION (C53-224-01) ON FLOOR BEAM STR 560 RBL 21 WL 208 GLAND NUTPLATE HOLE. *S/D* REMOVED CORROSION ON UPPER CORD, FABRICATED REPAIR ANGLES AND FILLER. INSTALLED REPAIR PER FEDEX SRM-53-10-8 FIG 8 AND 53-10-1 FIG 4.Aug 23, 1996 · N509FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 96FDEA01398Bonding Jumper · corrodedNR0349, CORROSION AT NR 2 K-FLAP I/B LOWER BONDING JUMPER ATTACH POINTS. *S/D* REMOVED AND REPLACED NR 2 K-FLAP PER FEDEX MM 27-81-1.Aug 23, 1996 · N509FE · Boeing 72725 · Leading Edge DevicesSDR 96FDEA01343Line · leakingNR 2 ENGINE WOULD NOT RUN HIGHER THAN EPR 1.02, N1 63.0, EGT 260 DEGREES, N2 74.0, AND FUEL FLOW 2950 POUNDS PER HOUR. POSSIBLE FUEL LEAK. ENGINE SHUT DOWN AS A PRECAUTION. FOUND LEAK ON SECONDARY MANIFOLD TUBE. REMOVED AND REPLACED PACKING FOR SECONDARYAug 10, 1996 · N502FE · Boeing 72725 · Engine Fuel DistributionSDR EISA96103Retract Mech · out of adjustNOSE GEAR DOORS VIBRATE AND FWD PANEL 'DOOR LIGHT' ON F/E PANEL NOSE GEAR DOOR LIGHTS COME ON. 305KIAS RECYCLED GEAR, SAME PROBLEM 330KIAS. RIGGED NLG DOORS PER MM 32-22-12 AND MM 32-22-1, OPS CHECK NORMAL. (M)Jul 26, 1996 · N290NE · Boeing 72725 · Landing Gear Door Retract SectionSDR CA960802001Control · plate shorted(CAN) A/P SYSTEM CONTROL BOX HAD BACK PLATE LIGHTING SHORT.Jul 24, 1996 · Boeing 72725 · Autopilot SystemSDR 96FDEA01182Te Wedge · delaminatedNR0707, 050, LEFT WING I/B MID FLAP T/E WEDGE HAS SEVERAL AREAS OF DELAMINATION. *S/D* REPAIRED DAMAGED SKIN TO LEFT WING I/B MID FLAP IAW FEDEX SRM 51-40-6.Jun 27, 1996 · N506FE · Boeing 72725 · Trailing Edge FlapsSDR 96FDEA01168Skin · chafedNR 0512 AND 049. SKIN CHAFED AT LAP, STR 19L, BS 693. ****S/D**** REPAIRED SKIN CHAFED AT LAP STR 19L, BS 693 - BS 730, IAW FEDEX EA 7-5330-29190.Jun 25, 1996 · N506FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 96FDEA01167Frame · corrodedNR 0543 AND 048. CORROSION ON FRAME AND FAIL-SAFE, BS 312, LBL 49, WL 180. ******S/D***** (MFG PART NUMBER 65-16314-71.) REMOVED AND REPLACED FRAME AND FAIL-SAFE, BS 312, LBL 49, WL 180, IAW FEDEX SRM 53-10-8, SRM 53-10-1.Jun 25, 1996 · N506FE · Boeing 72725 · Fuselage Main, Frame
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