Boeing 727-82C
Service difficulty reports · 164
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 = '72782C' 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 = '72782C' 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 DHL200070906CRib · crackedLEFT WING NR 1 L/E STAT 4TH INTERNAL RIB FROM O/B END CRACKED AT LOWER AFT SIDE. REMOVED 4TH RIB FROM O/B END OF NR 1 L/E SLAT TO BE REPAIRED PER SRM 51-30-2. INSTALLED REPAIR PER SRM 51-30-2. INSTALLED RIB AND DOUBLER PER SRM 51-30-2.SDR DHL200070904CSkin · damagedLEFT WING, PREVIOUS REPAIR DOUBLER CRACKED WBL 273.3 AT RIB O/B SIDE UPPER AFT. REMOVED AND REPLACED REPAIR AT LT WING UPPER SIDE WBL 273.3 PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-10-6.SDR DHL200070952DFitting · crackedLEFT WING NR 1 L/E FLAP CENTER HINGE FITTING ON L/E CRACKED AROUND SUPPORT ROD. REMOVED CENTER HINGE FITTING PER SRM 51-30-2. INSTALLED NEW HINGE FITTING PER SRM 57-50-2.SDR DHL200070925CPanel · damagedVERT STABILIZER, L/E FIN PANEL NR 9501, SEVERAL FASTENER HOLES ARE OVERSIZED. INSTALLED DOUBLER PER SRM 51-10-2. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200070962DFitting · crackedRT WING FRONT SPAR TERMINAL FITTING CRACKED IN BOTTLE PIN HOLE (APPROX 3 IN CRACK) VERIFIED BY HFEC. REMOVED LEADING EDGE PER SRM 51-30-2. REMOVED WIRING AS PER M/M 27-82-00. REMOVED FUEL LINE S PER M/M 28-22-0. PLACED A/C IN JIG POSITION PER SRM 51-50-1 ASDR DHL200070959DFitting · damagedLEFT WING FWD TERMINAL PIN BORE DAMAGED. REMOVED PNEUMATIC DUCTS AND HYD LINES FOR ACCESS PER M/M 20-10-15. REMOVED L/E PER SRM 51-30-2. PERFORMED HFEC PER NDT MAN 6-51-00-00. NO CRACK NOTED. FLAP PEEN AREA PER DHL-00-00015F. INSTALLED BUSHINGS AND PIN PSDR DHL200070960DFitting · damagedRT WING FRONT SPAR TERMINAL FITTING CRACKED IN BOTTLE PIN HOLE (APPROX 3 IN CRACK) VERIFIED BY HFEC. REMOVED LEADING EDGE PER SRM 51-30-2. REMOVED WIRING AS PER M/M 27-82-00. REMOVED FUEL LINE S PER M/M 28-22-0. PLACED A/C IN JIG POSITION PER SRM 51-50-1 ASDR DHL200070954DFairing · gougedLT FUSELAGE BODY FAIRING FOR THE NR 4 JACKSCREW AND ELEPHANT EAR FAIRING IS GOUGED IN 2 PLACES 16 INCHES FROM THE END. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8. SANDED AND PAINTED PER SRM 51-20-2.SDR DHL200070953DFairing · gougedLT FUSELAGE BODY FAIRING FOR THE NR 4 JACKSCREW AND ELEPHANT EAR FAIRING IS GOUGED IN 2 PLACES 16 INCHES FROM THE END. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8. SANDED AND PAINTED PER SRM 51-20-2.SDR DHL200070924CSkin · gougedLEFT MAIN LANDING GEAR FLYING DOOR HAS GOUGE AT LOWER SKIN ON TOP OF REPAIR. REMOVED OLD REPAIR PER SRM 51-30-2. CLEANED, TREATED AND PRIMED AREA PER SRM 51-10-2. FABRICATED REPAIR DOUBLER PER SRM 51-40-2. HEAT TREATED DOUBLER PER SRM 51-10-3. TREATED ANDSDR DHL200070921CSkin · crackedNR 3 ENG COWLING O/B SIDE AFT SECTION CLOSE TO HORIZONTAL LATCH SKIN IS CRACKED. INSTALLED DOUBLER REPAIR ON AFFECTED AREA PER SRM 51-40-2.SDR DHL200070920CSupport Bracket · corrodedRT WING AT NR 6 SPOILER CENTER FITTING SUPPORT SHOWS CORROSION AND WORKING FASTENERS AT THE BOTTOM. REMOVED AND REPLACED BRACKET PER SRM 51-30-2. TREATED AND PRIMED AREA PER SRM 51-10-3.SDR DHL200070918CChannel · bent9-G NET LT SIDEWALL FITTING MARKED NR 4 HAS STR U-CHANNEL BENT. REMOVED U-CHANNEL PER SRM 51-30-2. FABRICATED NEW U-CHANNEL, TREATED AND PRIMED PER SRM 51-10-2. INSTALLED NEW U-CHANNEL PER SRM 51-30-2.SDR DHL200070917CSkin · corrodedNR 1 LOWER COWLING CLOSE TO FIRE ACCESS, SKIN IS CORRODED ON PREVIOUS REPAIR. REMOVED OLD REPAIR PER SRM 51-30-2. CUT OUT DAMAGED SECTION OF SKIN (18 X 5.5 INCH)PER SRM 54-10-3. INSTALLED DOUBLER REPAIR PER SRM 54-10-3 FIG 5. ALL REPAIR PARTS WERE TREATED SDR DHL200070916CPanel · delaminatedRIGHT WING T/E LOWER PANEL LOCATED DWN NR 9 SPOILER SHOWS DELAMINATION AREA AT O/B END. REMOVED PANEL FOR COMPOSIT REPAIR PER SRM 51-30-2. INSTALLED COMPOSIT REPAIR PER SRM 51-40-6. REINSTALLED PANEL PER SRM 51-30-2.SDR DHL200070915CPanel · delaminatedRIGHT WING LWR ACCESS PANEL NR 8506, SHOWS A DELAMINATED AREA. REMOVED ACCESS PANEL FOR COMPOSIT REPAIR PER SRM 51-30-2. INSTALLED COMPOSIT REPAIR PER SRM 51-40-6. INSTALLED REPAIRED PANEL PER SRM 51-30-2.SDR DHL200070914CSkin · delaminatedRIGHT WING T/E LOWER PANEL O/B OF I/B AILERON SHOWS DELAMINATION AREA AT I/B END. REMOVED PANEL FOR COMPOSIT REPAIR PER SRM 51-30-2. INSTALLED COMPOSIT REPAIR PER SRM 51-40-6. INSTALLED REPAIRED PANEL PER SRM 51-30-2.SDR DHL200070903CAngle · damagedLOWER FUESLAGE A/C ACCESS BAY PANEL 3310L, HORIZONTAL ANGLE DAMAGED AT SMALL ACCESS HINGE ATTACH AREA. REMOVED AND REPLACED ANGLE AT LOWER FUESLAGE A/C ACCESS BAY PANEL 3310L PER SRM 53-50-1. ALODINED AND PRIMED PER SRM 51-10-2.SDR DHL200070902CStructure · crackedCRACKED METAL STRIP FWD LWR CORNER OF MAIN CARGO DOOR STA 480 WL 215L. REMOVED AND REPLACED METAL STRIP AT FWD LWR CORNER OF MAIN CARGO DOOR AT STA 480 WL 215L PER SRM 51-30-2. TREATED AND PRIMED AREA PER SRM 51-10-2.SDR DHL200070957DFairing · crackedLT FUSELAGE BODY FAIRING FOR THE NR 4 JACK SCREW AND ELEPHANT EAR FAIRING IS CRACKED AND FASTENERS ARE MISSING OR COMING LOOSE AT FWD END, LOCATED JUST AFT OF BS 950. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8. SANDED AND PAINTED PER SRM 51-20-0.SDR DHL20007094Structure · corrodedGALLEY DOOR HAS CORROSION JUST BELOW UPPER HINGE SUPPORT FITTING. REMOVED SURFACE CORROSION AT GALLEY DOOR HINGE SUPPORT PER SRM 51-10-6. FOUND CRACK AT THE FITTING LOWER SUPPORT BRACKET. REMOVED INNER SKIN AT RT GALLEY DOOR AND LOWER WEBS PER SRM 51-30-2. SDR DHL200070947DStructure · corrodedGALLEY DOOR HAS CORROSION JUST BELOW UPPER HINGE SUPPORT FITTING. REMOVED SURFACE CORROSION AT GALLEY DOOR HINGE SUPPORT PER SRM 51-10-6. FOUND CRACK AT THE FITTING LOWER SUPPORT BRACKET. REMOVED INNER SKIN AT RT GALLEY DOOR AND LOWER WEBS PER SRM 51-30-2. SDR DHL200070940DStructure · corrodedGALLEY DOOR HAS CORROSION JUST BELOW UPPER HINGE SUPPORT FITTING. REMOVED SURFACE CORROSION AT GALLEY DOOR HINGE SUPPORT PER SRM 51-10-6. FOUND CRACK AT THE FITTING LOWER SUPPORT BRACKET. REMOVED INNER SKIN AT RT GALLEY DOOR AND LOWER WEBS PER SRM 51-30-2. SDR DHL200070939DStructure · corrodedGALLEY DOOR HAS CORROSION JUST BELOW UPPER HINGE SUPPORT FITTING. REMOVED SURFACE CORROSION AT GALLEY DOOR HINGE SUPPORT PER SRM 51-10-6. FOUND CRACK AT THE FITTING LOWER SUPPORT BRACKET. REMOVED INNER SKIN AT RT GALLEY DOOR AND LOWER WEBS PER SRM 51-30-2. SDR DHL20007093Structure · corrodedGALLEY DOOR HAS CORROSION JUST BELOW UPPER HINGE SUPPORT FITTING. REMOVED SURFACE CORROSION AT GALLEY DOOR HINGE SUPPORT PER SRM 51-10-6. FOUND CRACK AT THE FITTING LOWER SUPPORT BRACKET. REMOVED INNER SKIN AT RT GALLEY DOOR AND LOWER WEBS PER SRM 51-30-2. SDR DHL200070938Structure · corrodedGALLEY DOOR HAS CORROSION JUST BELOW UPPER HINGE SUPPORT FITTING. REMOVED SURFACE CORROSION AT GALLEY DOOR HINGE SUPPORT PER SRM 51-10-6. FOUND CRACK AT THE FITTING LOWER SUPPORT BRACKET. REMOVED INNER SKIN AT RT GALLEY DOOR AND LOWER WEBS PER SRM 51-30-2. SDR DHL200070938DStructure · corrodedGALLEY DOOR HAS CORROSION JUST BELOW UPPER HINGE SUPPORT FITTING. REMOVED SURFACE CORROSION AT GALLEY DOOR HINGE SUPPORT PER SRM 51-10-6. FOUND CRACK AT THE FITTING LOWER SUPPORT BRACKET. REMOVED INNER SKIN AT RT GALLEY DOOR AND LOWER WEBS PER SRM 51-30-2. SDR DHL200070937DFitting · corrodedRT W/W FUSELAGE FITTING 950 HAS CORROSION BELOW PRESS FLOOR AND BULKHEAD 950. REMOVED PULLY BRACKET AND ANGLE FOR ACCESS OF CORROSION PER SRM 51-30-2. REMOVED FASTENERS AT STA 950 SUB FLOOR WEB TO REMOVE CORROSION ON 950 WHALE BONE FITTING PER SRM 51-30-2. SDR DHL200070909CSkin · crackedRT WING NR 5 L/E SLAT O/B GUIDE SEAL AREA, WING SKIN IS CRACKED. CLEANED AREA FOR NDT INSP PER NDT M/M 51-00-00. COMFIRMED 2 CRACKS PER NDT M/M 51-00-00. REMOVED GUIDE SEAL FOR ACCESS PER SRM 51-30-2. REMOVED ANTI ICE DUCT FOR ACCESS PER SRM 51-30-2. STOPSDR 2000709001CSkin · crackedNR 2 L/E FLAP INNER ANTI-ICE SKIN IS CRACKED AT ATTACH RIVET LOCATED AT THE THIRD BAY FROM THE O/B END. REMOVED INNER ANTI-ICE SKIN AT NR 2 L/E FLAP AS PER SRM 51-30-2. REPAIRED ANTI-ICE SKIN AT NR 2 L/E FLAP AS PER SRM 57-30-1. TREATED WITH ALODINE AND PRISDR DHL200070956DAngle · crackedLT WING LEADING EDGE CAVITY VERTICAL SUPPORT ANGLES FOR THE NR 3 SLAT I/B TRACK SUPPORT RIBS ARE CRACKED. LOCATED AT FRONT SPAR. REMOVED FUEL LINE TO GAIN ACCSES PER M/M 28-22-131. REMOVED HYD LINES FOR ACCSESS PER M/M 29-00. REMOVED VERT SUPPORTS PER SRM SDR DHL200070955DSkin · delaminatedSPOILER NR 6 HAS DELAMINATION AT I/B ATTACH FITTING LWR SURFACE. INSTALLED REPAIR TO I/B ATTACH FITTING PER SRM 51-40-5. SANDED AND PAINTED PER SRM 51-20-2.SDR DHL200070951DSkin · damagedRT WING UPPER SURFACE PANEL SKIN BULGE FWD OF I/B CORNER OF I/B AILERON. PERFORMED COMPOSITE REPAIR PER SRM 51-40-6. SANDED AND PAINTED AREA PER SRM 51-20-0.SDR DHL200070927CRib · crackedAFT STAIR AREA APPROX BS 1283 LT SECTION NR 2 AIR INTAKE DUCT HAS RIB CRACKED AT BOTH SIDES JUST AT ATTACHING POINT OF CSD AIR DUCT. REMOVED FASTENERS AND CUT OUT DAMAGED AREA PER SRM 54-10-3. INSTALLED RIB REPAIR AT CENTER ENGINE AIR INTAKE DUCT PER SRM 54-SDR DHL200070922CWeb · crackedLEFT WING WEB CRACKED AT UPPER I/B AFT SIDE WBL 273.3. STOP DRILLED CRACK PER SRM 51-10-1. INSPECTED WITH HFEC PER NDT M/M 6-51-000, CONFIRMED NO CRACK PAST STOP DRILL. INSTALLED DOUBLER REPAIR PER SRM 51-40-2. TREATED AND PRIMED AREA PER SRM 51-10-2.SDR DHL200070910CPanel · corrodedUPPER FUSELAGE TOILET FLOOR PANEL IS DAMAGED AND HAS CORROSION. REMOVED FLOOR PANEL PER SRM 51-30-2. FABRICATED NEW FLOOR PANEL PER SRM 53-10-1. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED NEW SUB FLOOR PER SRM 51-30-2.SDR DHL20070950DStructure · crackedRT WING TO FUSELAGE FILLET AREA STR 18 A CRACKED AT FS 948. VERIFIED CRACK WITH HFEC INSP. REMOVED FASTENERS PER SRM 51-30-2. FABRICATED REPAIR PER DRWNG DHL-MIA 00-00022H. STOP DRILLED END OF CRACK PER SRM 51-10-1. APPLIED PRIMER PER SRM 51-10-2. INSTALSDR 20000428AP011Fire Loop · out of positionFLT 610 MSP-SEA - NR 3 GROUND FAULT FIRE LIGHT ILLUMINATED IN FLIGHT. REPOSITIONED NR 3 ENGINE FIRE LOOP. (M)SDR 20000405AP003Fire Loop · out of positionFLT 719 - PHX-IND - NR 3 GROUND FAULT DETECTOR LIGHT ILLUMINATED IN FLIGHT. REPOSITIONED FIRE LOOP. (M)SDR 20000405AP002Fire Loop · out of positionFLT 615 - PIT-PHL - NR 3 GROUND FAULT LIGHT ON. DEFERRED IN PIT, CLEARED IN PHL. REPOSITIONED FIRE LOOP. (M)SDR 2000ZZZM199Fire Loop · misroutedFLT 711 - EWR-IND - FIRE DETECTION B-LOOP LIGH TON NR 3 ENGINE. REROUTED NR 3 ENGINE GROUND LOOP. (M)SDR 2000ZZZM201Fire Loop · out of adjustFLT 713 - GSO-CLT - NR 2 ENGINE FIRE DETECTOR LOOP LIGHT ILLUMINATED ON ENGINEERS PANEL. DEFERRED IN CLT, CLEARED IN EWR. FOUND SENSOR TOUCHING BRACKET ADJUSTED SENSOR AND LIGHT WENT OUT. (M)SDR DHL2000709001Warning Light · illuminatedON APPROACH, NOSE GEAR FAILED TO LOCK DOWN ( RED LIGHT ILLUMINATED). RECYCLED GEAR TWICE, EACH ATTEMPT RED UNLOCKED LIGHT ILLUMINATED. UNABLE TO VISUALLY VERIFY GEAR DOWN/LOCKED. SELECTED FLAPS 30, GOT GEAR WARNING HORN. RETRACTED GEAR AND EXTENDED WITH A HSDR 2000ZZZM184Fire Loop · out of positionFLT 607 - IND-DEN - ENGINE NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATES SPORADICALLY IN FLIGHT. REPOSITIONED FIRE LOOP NR 3 ENGINE. (M)SDR 99ZZZM735Clamp · looseFLT 707 - DEN-IND - LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT OF DEN WITH WING AND ENGINE ANTI-ICE ON. FOUND LOOSE CLAMP ON OVERHEAT LOOP, RESECURED CLAMP, ALL OPERATIONS NORMAL. (M)SDR DHL99709003Engine · failedNR 3 OIL TEMP ABOVE 157C APPROX 5 MINUTES UNTIL ENGINE SHUT DOWN WAS ACCOMPLISHED. AFTER SHUT DOWN, OIL TEMP SLOWLY CAME DOWN. 20 MIN AFTER SHUTDOWN, TEMP WAS 65C AS OIL COOLED PRESSURE INCREASED WIND MILLED FOR APPROX 10 MIN WITH LOW OIL PRESSURE LIT ON ANSDR 99ZZZM769Fire Loop · groundedFLT 648 - DFW-OMA - NR 1 FIRE DETECTION LIGHT ON INTERMITTENTLY. REPOSITIONED FIRE LOOP AWAY FROM A TUBE. (M)SDR DHL99709002Structure · bird strikeON TAKEOFF AT 100 AGL, HAD MULTIPLE BIRD STRIKES. COMPLIED WITH BIRD STRIKE INSPECT, NO DEFECT NOTED.SDR DHL99709001Gland Nut · leakingDURING GEAR RETRACTION, NOSE GEAR DOOR LIGHT WOULD NOT EXTINGUISH. ON EXTENSION, ALL INDICATIONS WERE NORMAL. ABNORMAL INDICATIONS ON FWD AND F/E PANEL. FOUND GLAND NUT LEAKING. REPLACED SAME. CYCLED GEAR SEVERAL TIMES. SYS CKS NORMAL.SDR DHL98709001Temp Bulb · failedEN ROUTE, NR 2 ENGINE OIL TEMP INDICATION 140 DEGREE CELSIUS AT CRUISE THRUST. REDUCED TO IDLE FOR APPROX 12 MIN, TEMPERATURE CONTINOUSLY INDICATED 140C, PEAK TEMP 155C. ABNORMAL PROC AND ENGINE SHUT DOWN. REMOVED AND REPLACED TEMP BULB, OIL AND FILTER.
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