Boeing 727-22

Service difficulty reports · 1,282

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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 = '72722'
  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 DHL9870741CBulkhead · crackedAT C CHECK, AFT BAGGAGE 950 BULKHEAD HAS 8 INCH CRACK AT LBL 22 WL 185. STOP DRILLED CRACK, HFEC. INSTALLED DOUBLER REPAIR PER SRM 53-10-9, 5 BY 12, N/R 3696.Apr 22, 1998 · N707DH · Boeing 72722 · Fuselage Main, BulkheadSDR DHL9870740CBulkhead · crackedAT C-CHECK, AFT BAGGAGE 950 BULKHEAD HAS 7 INCH CRACK AT LBL 58 WL 190 . CUT OUT CRACKED SKIN 10 BY 1.25, HFEC. INSTALLED DOUBLER REPAIR PER SRM 53-10-9. N/R 3697.Apr 22, 1998 · N707DH · Boeing 72722 · Wing, Rib/BulkheadSDR DHL9870733CFitting · crackedAT C-CHECK, FWD CARGO COMPT DOOR CUT OUT FWD FRAME LOWER STOP FITTING CRACKED. REMOVED AND REPLACED STOP FITTING PER SRM 51-10-4. N/R 3635.Apr 22, 1998 · N707DH · Boeing 72722 · Fuselage Miscellaneous StructureSDR DHL9870729CStiffener · crackedAT C-CHECK, RIGHT MLG W/W INBD WALL VERTICAL STIFFENER LOWER AT BS 940 IS CRACKED. REPLACED STIFFENER PER SRM 53-10-1. REPLACED LOWER ATTACH ANGLE PER SRM 53-10-1. N/R 7912.Apr 22, 1998 · N707DH · Boeing 72722 · Fuselage Miscellaneous StructureSDR DHL9870725CSeat Track · corrodedAT C-CHECK, CABIN SEAT TRACK CORRODED AT STA 540 LBL 24. CUT OUT DAMAGED SECTION, INSTALLED NEW TRACK PER SRM 53-10-5. N/R 5586Apr 22, 1998 · N707DH · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9870724CFrame · crackedAT C-CHECK, CABIN HORIZIONTAL SIDEWALL PANEL SUPPORT FRAME IS CRACKED AT GALLEY DOOR FORWARD CUT OUT FRAME ATTACHMENT JUST ABOVE UPPER DOOR HINGE. INSTALLED DOUBLER PER SRM 51-40-2, 6 X 3. N/R 5592Apr 22, 1998 · N707DH · Boeing 72722 · Fuselage Miscellaneous StructureSDR DHL9870706CAngle · crackedAT C-CHECK, NR 5 SLAT THE INBD SLAT TO TRACK ATTACH ANGLES ARE CRACKED. REPLACED ATTACH ANGLES PER SRM 51-40-4, 4.25. N/R 2808Apr 22, 1998 · N707DH · Boeing 72722 · Leading Edge DevicesSDR DHL9870705CPanel · crackedAT C-CHECK, RT WING L/E AT NR 7 SLAT, ACCESS PANEL 8 INBD OF SLAT ACTUATOR HAS SEVERAL CRACKS. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2, 9 X 7. N/R 2842Apr 22, 1998 · N707DH · Boeing 72722 · Wing, Plate/SkinSDR DHL9870704CRib · crackedAT C-CHECK, RT WING RIB WS 546 CRACKED AT TOP FLANGE AT THIRD FROM AFT STRINGER. STOP DRILLED CRACK, HFEC, INSTALLED DOUBLER REPAIR PER SRM 57-10-5, 2 X 1 X 1. N/R 2843Apr 22, 1998 · N707DH · Boeing 72722 · Wing, Rib/BulkheadSDR DHL9870703CRib · crackedAT C-CHECK, RT WING PREV REPAIR DOUBLER CRACKED ON RIB WS 656 LOWER FLANGE AT SECOND FROM AFT STRINGER. REPLACED PREVIOUS DOUBLER PER SRM 57-10-5, 8 X 3.25 X 1 X 1. N/R 2844Apr 22, 1998 · N707DH · Boeing 72722 · Wing, Rib/BulkheadSDR DHL9870743CSkin · corrodedAT C-CHECK, BUTT JOINT BS 259 AFT PANEL INDICATES 10 PERCENT MATERIAL LOSS JUST BELOW STR 14R TO 16R. CUT OUT DAMAGED AREA, INSTALLED SKIN SPLICE PER S/B 53-084 AREA 2 FT BY 2 FT, N/R 3647.Apr 21, 1998 · N707DH · Boeing 72722 · Fuselage Main, Plate/SkinSDR DHL9870734CSkin · crackedAT C CHECK, LOWER SKIN CRACKED AT LAP JOINT BS 384 LOWER FASTENER ROW. REMOVED FASTENERS, OVERSIZED HOLE, ACCOMPLISHED HFEC. INSTALLED FASTENER. N/R 3646.Apr 21, 1998 · N707DH · Boeing 72722 · Fuselage Main, Plate/SkinSDR DHL9870732CFrame · crackedAT C-CHECK, LT WHEEL WELL BS 930 FRAME CRACKED AT UPPER 2 ATTACH FASTENERS, JUST BELOW PRESSURE DECK. HFEC FOR VERIFICATION, STOP DRILLED DECK, HFEC. INSTALLED ASSURANCE CUT, INSTALLED REPAIR PER S/B 53-130 PART 3, N/R 3616.Apr 21, 1998 · N707DH · Boeing 72722 · Fuselage Main, FrameSDR DHL9870731CFitting · crackedAT C-CHECK, NR 7 SPOILER ACTUATOR MOUNT CASTING CRACKED AT UPPER FLANGE AFT END BOTH SIDES. INSTALLED NEW FITTING PER SRM 51-10-1. N/R 1053.Apr 21, 1998 · N707DH · Boeing 72722 · SpoilersSDR DHL9870730CSkin · delaminatedAT C-CHECK, 32 SPOILER PANEL IS DELAMINATED ON TOP SIDE. INSTALLED FIBERGLASS OVERLAY REPAIR UPPER AND LOWER PER SRM 51-40-8. N/R 1041.Apr 21, 1998 · N707DH · Boeing 72722 · SpoilersSDR DHL9870719CFitting · crackedAT D-CHECK, RT AFT EMERGENCY CUTOUT EXIT HAS LOWER CENTER LOCK FITTING CRACKED. REPLACED FITTING PER SRM 51-30-2. N/R 3581Apr 21, 1998 · N707DH · Boeing 72722 · Emergency ExitsSDR DHL9870715CSkin · crackedAT C-CHECK, FWD ENTRY DOOR LOWER BOTTOM FWD EDGE OF DOOR INNER SKIN BENT INWARD AND CRACKED. STOP DRILLED, HFEC AND INSTALLED DOUBLER REPAIR PER SRM 51-40-3, 4 X 5. N/R 3666Apr 21, 1998 · N707DH · Boeing 72722 · Passenger/Crew DoorsSDR DHL9870714CBracket · crackedAT C-CHECK, SUPPORT BRACKET CRACKED AT STRINGER 18A LT FS 945 AS VIEWED FROM TOP OF WING. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-20-2. N/R 3645Apr 21, 1998 · N707DH · Boeing 72722 · Fuselage Miscellaneous StructureSDR DHL9870711CPanel · delaminatedAT C-CHECK, TAIL ACCESS PANEL 9705 SHOWS SIGNS OF DELAMINATION. INSTALLED REPAIR PER SRM 51-40-8, 24 X 15. N/R 4805Apr 21, 1998 · N707DH · Boeing 72722 · Vertical Stabilizer, Plate/SkinSDR DHL9870710CAngle · crackedAT C-CHECK, CRACKED UPPER SKIN SUPPORT ANGLE AT R/W INBD TRAILING EDGE CAVITY, JUST FWD OF INBD AILERON. REPLACED ANGLE PER SRM 51-40-3, 4 X 2.5. N/R 2776Apr 21, 1998 · N707DH · Boeing 72722 · Wing Miscellaneous StructureSDR DHL9870709CFitting · crackedAT C-CHECK, CRACK INDICATION AT R/W INBD T/E FLAP CAVITY NR 10 SPOILER OUTBD HINGE SUPPORT FITTING. REMOVED AND REPLACED FITTING PER SRM 51-30-2. N/R 2778Apr 21, 1998 · N707DH · Boeing 72722 · SpoilersSDR DHL9870708CAngle · crackedAT C-CHECK, RT WING L/E LOWER COVE PANEL SIDE ATTACH ANGLE L/E 130 IS CRACKED AT ATTACH FASTENERS. INSTALLED NEW ANGLE PER SRM 51-40-3, 24 X 12. N/R 2783Apr 21, 1998 · N707DH · Boeing 72722 · Wing Miscellaneous StructureSDR DHL9870707CChannel · crackedAT C-CHECK, R/W OUTBD T/E FLAP WELL T/E LOWER PANEL SUPPORT INBD CHANNEL AT WS 491 CRACKED. REPLACED CRACK PER SRM 51-30-2. N/R 2797Apr 21, 1998 · N707DH · Boeing 72722 · Wing Miscellaneous StructureSDR DHL9870744CSkin · corrodedAT C-CHECK, SKIN BULGE AT BS 390, STR 4 LT. ACCOMPLISHED HFEC, FROM BS 360 TO 440. 10 PERCENT MATERIAL LOSS. CUT OUT DAMAGED AREA 6 BY 3 PER SRM 53-30-3. FABRICATED AND INSTALLED REPAIR PARTS BS 390, STR 14 LEFT PER SRM 53-30-3. N/R 3527.Apr 20, 1998 · N707DH · Boeing 72722 · Fuselage Main, Plate/SkinSDR DHL9870721CHinge · crackedAT C-CHECK, MCD UPPER HINGE CRACKED LUG AT 2ND FROM FWD END. REMOVED AND REPLACED HINGE PER SRM 51-30-2. N/R 3528Apr 20, 1998 · N707DH · Boeing 72722 · Cargo/Baggage DoorsSDR DHL9870720CLinks · chafedAT C-CHECK, NLG WHEEL WELL DOORS ACTUATING MECHANISM ACTUATION ROD, QUADRANT, LINKS ARE CHAFED SEVERELY AT FWD BULKHEAD. REMOVED AND REPLACED MECHANISM AND LINK PER MM 32-21-21. N/R 3577Apr 20, 1998 · N707DH · Boeing 72722 · Landing Gear Door Retract SectionSDR DHL9870718CSkin · crackedAT C-CHECK, CRACKS IN RADUIS AND CORROSION IS PRESENT AT CIRCUMFERENTIAL AT BS 480, OUTBD OF STR 27L AFT IN E AND E COMPT. STOP DRILL CRACK, HFEC, INSTALLED DOUBLER REPAIR PER SRM 51-40-3. 7 X 5'. INSTALLED ANGLE PER SRM 51-40-3, 3 X 2. N/R 3513Apr 20, 1998 · N707DH · Boeing 72722 · Fuselage Main, Plate/SkinSDR DHL9870713CHinge · crackedMAIN CARGO DOOR UPPER HINGE CRACKED LUG AT AFT END. REMOVED AND REPLACED HINGE PER SRM 51-30-2. N/R 3529Apr 20, 1998 · N707DH · Boeing 72722 · Cargo/Baggage DoorsSDR DHL9870702CSkin · crackedAT C-CHECK, NR 3 SLAT INBD TRACK CUTOUT IN WING LEADING EDGE IS CRACKED. STOP DRILL, HFEC, INSTALLED DOUBLER REPAIR PER SRM 51-10-1, 6 X 10. N/R 1016Apr 20, 1998 · N707DH · Boeing 72722 · Wing, Plate/SkinSDR DHL9870701CRib · crackedAT C-CHECK, LEADING EDGE COVE RIB IS CRACKED AT FRONT SPAR STATION 338 ON OUTBD SIDE. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-40-3, 20 X 1.5 X 1.5. N/R 1027Apr 20, 1998 · N707DH · Boeing 72722 · Wing, Rib/BulkheadSDR 98FDEA00231Forging · corrodedWHILE WORKING NR 0441, FOUND CORROSION ON BS 870 FORGING, RBL 57, WL 168. *S/D* REMOVED AND REPLACED RIGHT HAND BS 870 FITTING STR 9 TO WL 156 IAW FED-EX NR 7-5310-38683.Apr 3, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00226Switch · failedMAIN CARGO DOOR LIGHT CAME ON SHORTLY AFTER TAKEOFF. REPLACED LOCK ROD SWITCH AND ADJUSTED PER MAINTENANCE MANUAL 52-70-09, OPERATIONAL CHECKS GOOD.Apr 1, 1998 · N190FE · Boeing 72722 · Door Warning SystemSDR CA980415012Valve · malfunctioned(CAN) DURING ENGINE SPOOL-UP IN PREPARATION TO TAKEOFF, NR 1 ENGINE EXPERIENCED MULTIPLE COMPRESSOR STALLS. AIRCRAFT RETURNED TO THE RAMP. ENGINE INSPECTED FOR DAMAGE AND F.O.D. NO DISCREPANCIES FOUND. FUEL PRESSURIZATION AND DUMP VALVE ADJUSTED. ENGINE Mar 30, 1998 · Boeing 72722 · Fuel Controlling SystemSDR 98FDEA00205Tire · missingRIGHT OUTBOARD ANTI-SKID LIGHT BEGAN TO FLICKER DURING TAKEOFF ROLL, CAME ON SOLID AFTER ROTATION. ROC REPORTED, LOST THE RIGHT MAIN TIRE (OUTBOARD). FOUND NR 4 TIRE MISSING. REMOVED BRAKE TO INSPECT AXLE SLEEVE. REMOVED AND REPLACED AXLE SLEEVE AND INSPECMar 18, 1998 · N193FE · Boeing 72722 · TireSDR 98FDEA00203Splice · crackedNR 0439 014, BS 870 LT UPPER SPLICE PLATE FOR UPPER CHORD HAS 2 CRACKED HOLES AND 1 DAMAGED HOLE AOG ACCESS REQUIRED. REMOVED AND REPLACED BS 870 LT UPPER SPLICE PLATE PER BOEING DRAWING 64-8336.Mar 18, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00181Strap · corrodedCORROSION (C53-132-02-1, 2) ON LOAD TENSION STRAP BS 870, RBL 35 TO 50. *S/D* REPAIRED BS 870 LOAD TENSION STRAP AT RBL 30 TO 60 IAW FED-EX EA 7-5310-37605.Mar 12, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00160Switch · dirty98-0059 ON TAKEOFF, RIGHT MAIN GEAR DOOR LIGHT CAME ON AND WOULD NOT GO OFF. CYCLED GEAR, LIGHT WENT OUT. INSPECTED AND CLEANED RIGHT MAIN GEAR DOOR SWITCH. CYCLED DOOR SEVERAL TIMES. OPERATIONAL CHECK NORMAL.Mar 6, 1998 · N198FE · Boeing 72722 · Landing Gear Position and WarningSDR 98FDEA00092Frame · corrodedNR 0433 012, WHILE WORKING NR0301, FOUND FRAME TO BE CORRODED AT BS 680, RBL 24, WL 155 (STR 26). REMOVED DAMAGE AT BS 680, RBL 24 FROM STR 22-26 RT. FOUND TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-1. REPAIRED DAMAGED FRAME AT BS 680, RBL 24, STR 22-26 RT IAFeb 10, 1998 · N189FE · Boeing 72722 · Fuselage Main, FrameSDR DHL98707001Bulkhead · crackedFOUND SUSPECTED CRACK AT AFT AIRSTAIR DOOR JAMB (1183 BULKHEAD) RIGHT SIDE AT 2ND STOP FROM THE TOP. CRACKED CONFIRMED, STOP DRILLED CRACK, EDDY CURRENT STOP DRILL, INSTALLED DOUBLER REPAIR PER 98PMSI189D-1B ENGINEERING DRAWING.Feb 4, 1998 · N707DH · Boeing 72722 · Fuselage Main, BulkheadSDR 98FDEA00085Heater · inoperativeRIGHT STATIC LIGHT ON PITOT STATIC HEATER MONITOR PANEL ILLUMINATED WITH RIGHT SWITCH ON. FOUND FIRST OFFICER'S RIGHT STATIC PORT NOT HEATING. REPLACED HEATER, OPERATIONAL CHECKED PER MAINTENANCE MANUAL 30-31-0. LEAK CHECKED PER MAINTENANCE MANUAL 34-11-0.Feb 4, 1998 · N167FE · Boeing 72722 · Pitot/Static Anti-Ice SystemSDR 98FDEA00054Stiffener · corrodedCORROSION (C53-224-03-1/2) ON NOSE WHEEL WELL HORIZONTAL STIFFENER BS 303, RBL 8, WL 180. *S/D* REMOVED AND REPLACED HORIZONTAL STIFFENER BS 303, RBL 8, WL 180 IAW FEDEX DRAWING NR 65-18417.00.Jan 26, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00035Tee Fitting · corrodedWHILE WORKING NR0328, FOUND CORROSION ON TEE FITTING AT BS 336, LBL 17, WL 150. *S/D* REMOVED AND REPLACED TEE FITTING AT BS 336, LBL 17, WL 155 IAW FED-EX DRAWING 65-18415.Jan 15, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00031Floorbeam · gougedUPON REMOVAL OF RADIUS FILLER, FOUND DEEP GOUGE AT BS 880, LBL 15, WL 201.5. *S/D* BLENDED OUT GOUGE, CRACK AND CORROSION AT BS 880, LBL 15, WL 201.5 ORIGINAL THICKNESS WAS .1, MATERIAL REMOVED WAS .045. BLENDOUT AREA IS .3 X .2, FOUND TO BE OUT OF LIMITS PJan 15, 1998 · N189FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00028Chord · corrodedWHILE WORKING NR 0329, FOUND FRAME FAIL-SAFE CHORD CORRODED AT BS 312, LBL 19, WL 153. *S/D* FOUND CORROSION DAMAGE ON FAIL-SAFE CHORD AT BS 312, LBL 19, WL 153 TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-1. REMOVED CHORD LBL 19 TO LBL 42. FABRICATED NEW PART AJan 12, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00027Floorbeam · corrodedNR 0429 007, WHILE WORKING NR0408, FOUND CORROSION ON FLOORBEAM BS 344, RBL 17 OUT OF LIMITS AND DOUBLE HOLE DRILLED AT RBL 38, WL 208. REMOVED AND REPLACED BS 344 BEAM UPPER CHORD LBL 17 TO RBL 65 PER FED-EX DRAWING SR 27-53-007.Jan 12, 1998 · N189FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 98FDEA00026Bulkhead Web · corrodedCORROSION (C53-132-02-1, 2) IN NUMEROUS AREAS ON BS 870 BULKHEAD WEB OF CENTER WING SECTION. *S/D* REMOVED AND REPLACED 870 BULKHEAD WEB OF CENTER WING SECTION PER EA 7-5710-38653.Jan 12, 1998 · N189FE · Boeing 72722 · Wing, Rib/BulkheadSDR 98FDEA00025Spar Chord · corrodedCORROSION (C53-132-02-1, 2) ALONG VERTICAL FLANGE OF BS 870 UPPER SPAR CHORD WL 180, RBL 65- LBL 65. *S/D* REMOVED AND REPLACED 870 UPPER SPAR CHORD WL 180, RBL 65 - LBL 65 IAW FED-EX EA 7-5100-37367 AND 7-5710-38653.Jan 12, 1998 · N189FE · Boeing 72722 · Wing SparSDR 98FDEA00018Angle · corrodedNR 0329 004, CORROSION C53-111-03-1/2 ON LT LOWER NOSE CHORD BS 336 TO 350, LBL 17, WL 149. FOUND CORROSION ON LT LOWER NOSE ANGLE BS 336 TO 350, LBL 17, WL 149 TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-01. REMOVED AND REPLACED ANGLE BS 284 TO BS 350, LBL 17,Jan 8, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00017Chord · corrodedNR 0328 003, CORROSION C53-111-03 1/2 ON RT LOWER NOSE CHORD BS 336 TO 350, RBL 17, WL 149. FOUND CORROSION ON RT LOWER NOSE CHORD BS 336 TO BS 350, RBL 17, WL 149 TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-1. REMOVED AND REPLACED CHORD BS 284 TO BS 350 RT, RBJan 8, 1998 · N189FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 98FDEA00015Pneumatic Duct · blownREJECTED TAKEOFF AT 85 KNOTS DUE TO NR 3 ENGINE FIRE WARNING. COMPLETED ENGINE FIRE CHECK LIST AND REJECTED TAKEOFF CHECK LIST. REJECTED TAKEOFF BRAKE COOLING CHART INDICATED 29 MINUTES COOL DOWN IN BLOCKS AT 0339 Z. INSPECTED TIRES AND BRAKES AT 0410Z, OK Jan 8, 1998 · N196FE · Boeing 72722 · Pneumatic Distribution System
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