Boeing 727-23

Service difficulty reports · 375

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 = '72723'
  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 DHL200071703DSkin · dentedAT D-CK, RIGHT WING LEADING EDGE OUTBOARD OF NR 8 SLAT HAS TORN METAL AND DENTED AREA WS 780. STRAIGHTENED OUT DAMAGED AREA PER SRM 51-40-1, BLENDED OUT SMALL DAMAGED AREA PER SRM 57-20-1 FIG 4, MATERIAL LOSS, .003. PERFORMED HFEC INSPECTION OF BLENDED AREA Jan 5, 2000 · N717DH · Boeing 72723 · Leading Edge DevicesSDR DHL200071701DShear Tie · crackedAT D CK, FWD BAGGAGE COMP BS 620 CIRCUMFERENTIAL CLIP TO FUSELAGE SKIN IS CRACKED JUST I/B OF STR 2L. REMOVED DOUBLER REPAIR AT BS 620. FABRICATED DOUBLER REPAIR FOR CIRCUMFERENTIAL CLIP PER SRM 53-10-4, FIG 13, MATERIAL USED 7075-0 .063, 6 BY 4, TREATED ANDJan 5, 2000 · N717DH · Boeing 72723 · Fuselage Miscellaneous StructureSDR DHL200071738DStringer · corrodedAT D CK, AFT CARGO COMPT STR 24L CORRODED AT FASTENER HOLES BTWN FRAMES STA 1148 AND 1166. CUTOUT DAMAGED AREA PER B727 SRM 53-10-3. REPLACED 13 SECTION PER B727 SRM 53-10-3 AND 51-30-2. REF: N/R 3483.Jan 4, 2000 · N717DH · Boeing 72723 · Fuselage Miscellaneous StructureSDR 99ZZZX4082O-Ring · wornIN-FLIGHT, SHUT DOWN OF NR 3 ENGINE DUE TO LOW OIL PRESSURE/QUANTITY INDICATION. AIRCRAFT RETURNED TO KATL. MAINTENANCE REPLACED O-RING ON OIL LINE BANJO FITTING FORWARD OF STARTER.Jul 30, 1999 · N992AJ · Boeing 72723 · Engine Oil Distribution (Airframe Furnished)SDR DHL99717002Switch · failedCARGO DOOR UNLOCK LIGHT ILLUMINATED ON CLIMBOUT FOLLOWED BY LOSS OF PRESSURIZATION. DUMPED FUEL WAS INITIATED. REPLACED LIGHT SOCKET AND SEQUENCE SWITCH.Mar 5, 1999 · N717DH · Boeing 72723 · Cargo/Baggage DoorsSDR DHL99717001Wire · brokenON DESCENT WITH THRUST LEVER TO IDLE, RED NOSE GEAR LIGHT DID NOT ILLUMINATE WITH GEAR HANDLE DOWN. ON GEAR EXT RED LIGHT DID NOT CYCLE GREEN LIGHT DID NOT ILLUMNATE. TOWER ADVISED L/G APPEARED NORMAL. ACCOMPLISHED NORMAL LANDING WITH GPWS AND HORN C/B PULLJan 30, 1999 · N717DH · Boeing 72723 · Landing Gear System WiringSDR DL72L990013Frame · crackedA .25 INCH VISIBLE CRACK LOWER FWD CORNER NR 5 FLAP ACT MOUNT BOX I/B FRAME. REPAIRED PER MM 57-20-21.Jan 4, 1999 · N510DA · Boeing 72723 · Leading Edge DevicesSDR DHL98717004Valve · dirtySMOKE IN COCKPIT AFTER TAKEOFF. FOUND NR 1 ENGINE PRECOOLER CHECK VALVE STUCK OPEN. CLEANED VALVED AND RAN ENGINE, OPS CHECK GOOD.Dec 26, 1998 · N717DH · Boeing 72723 · Pneumatic Distribution SystemSDR DHL98717003P & D Valve · failedAFTER TAKEOFF FROM MIA AT CLIMB, THRUST SETTING THE CREW NOTICED A VIBRATION AND NR 1 ENGINE EPR WAS FLUCTUATING BETWEEN 1.75 AND 1.5 FUEL FLOW AND N2 FLUCTUATING. WHEN THRUST REDUCED THE VIBRATION WAS MINIMAL. FLIGHT RETURNED TO MIA. REMOVED AND REPLACED Nov 17, 1998 · N717DH · Boeing 72723 · Fuel Controlling SystemSDR DHL98717002Valve · failedON CLIMBOUT, NR 1 ENG FUEL HEAT VALVE LIGHT CAME ON. OIL TEMP ROSE TO 140 DEGREES CELSIUS. RETARDED THROTTLE AND HEAT ROSE TO 145 DEGREES. INCREASED THROTTLE TO 80 PERCENT N2 AND TEMP DECREASED TO 140 DEGREES AFTER 15 MIN. SHUT DOWN ENGINE PER AOM. OIL TESep 19, 1998 · N717DH · Boeing 72723 · Fuel HeaterSDR 98ZZZM502Longeron · wornDURING C-CHECK INSPECTION DISCOVERED WEAR MARKS ON THE LEFT AND RIGHT KEEL BEAM LONGERONS AT THE MAIN LANDING GEAR DOOR HINGES, STATION 947 LEFT AND STATION 910 RIGHT. REPAIRED BY BLENDING AWAY THE DAMAGED AREAS, FLAP PEENED, ALODINED, PRIMED AND CORROSION PRJun 1, 1998 · N930FT · Boeing 72723 · Fuselage Main, Longeron/StringerSDR 98ZZZM501Skin · crackedDURING C-CHECK INSPECTION DISCOVERED A CRACK IN THE FIXED LEADING EDGE SKIN AT RIGHT WING LEADING EDGE STATION 155. REPAIRED BY TRIMMING OUT THE CRACK, HFEC NDT INSPECTING, FABRICATING AND INSTALLING A REPAIR DOUBLER AND FILLER WITH BLUEPRINT TYPE FASTENERS. Jun 1, 1998 · N930FT · Boeing 72723 · Wing, Plate/SkinSDR 98ZZZM500Bulkhead Fitting · corrodedDURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE RIGHT BULKHEAD TERMINAL FITTING AT STATION 870. REPAIRED BY BLENDING AWAY THE CORROSION, HFEC NDT INSPECTING, FLAP PEENING BLENDED AREA, ALODINING AND DOUBLE PRIMING BARE ALUMINUM AREAS. REPAIRED IAW EVIJun 1, 1998 · N930FT · Boeing 72723 · Fuselage Main, BulkheadSDR 98ZZZX1445Fitting · corrodedAIRCRAFT UNDERGOING A C-CHECK INSPECTION. THE RT WING TERMINAL FITTING STA 870 WAS FOUND CORRODED BEYOND SRM LIMITATIONS.Mar 31, 1998 · N992AJ · Boeing 72723 · Fuselage Miscellaneous StructureSDR 98ZZZX1444Fitting · corrodedAIRCRAFT UNDERGOING A C-CHECK INSPECTION. THE RT WING TERMINAL FITTING STA 870 WAS FOUND CORRODED BEYOND SRM LIMITATIONS.Mar 31, 1998 · N992AJ · Boeing 72723 · Fuselage Miscellaneous StructureSDR DHL98717001Machanism · lack of lubeAFTER DEP, CARGO DOOR 'UNLOCKED' LIGHT ILLUMINATED, LOST PRESSURIZATION. LIGHT WENT OUT, REGAINED PRESSURIZATION. LIGHT ILLUMINATED AGAIN AND LOST PRESSURIZATION. LIGHT WENT OUT, PRESSURIZATION NEVER RETURNED TO NORMAL. INSPECTED CARGO DOOR, CYCLED DOOR SEFeb 5, 1998 · N717DH · Boeing 72723 · Cargo/Baggage DoorsSDR DHL9871783CCowl · crackedAT C CHECK, NR 1 ENGINE UPPER COWLING NR 1 I/B FRAME SECTION CRACKED. REPLACED FRAME SECTION PER SRM 51-40-3, 15 BY 6, N/R 6135.Jan 9, 1998 · N717DH · Boeing 72723 · Engine Cowling SystemSDR DHL9871707CSkin · delaminatedAT C CHECK, O/B MID FLAP T/E END DELAMINATED. INSTALLED REPAIR PER SRM 51-40-8. REPAIR 17 BY 4 N/R 2169.Jan 8, 1998 · N717DH · Boeing 72723 · Trailing Edge FlapsSDR DHL9871747CRib · crackedAT C CHECK, LEFT WING INTERIOR, LOWER FLANGE OF WING RIB CRACKED AT STRINGER 8 ATTACH FASTENER, WS 546.5. INSTALLED RIB REPAIR PER SRM 57-10-5, 9 BY 3.75, N/R 1236.Jan 5, 1998 · N717DH · Boeing 72723 · Wing, Rib/BulkheadSDR DHL9871738CFloor Panel · delaminatedAT C CHECK, RT SIDE STA 720 NR 6 FLOOR PANEL IS DELAMINATED. REPLACED PANEL PER SRM 51-30-2, 27 BY 16.5, N/R 5131.Jan 5, 1998 · N717DH · Boeing 72723 · Fuselage Floor PanelSDR DHL9871737CRib · crackedAT C CHECK, LOWER FLANGE OF WING RIB CRACKED AT STR 6 ATTACH FASTENER WS 629. INSTALLED DOUBLER REPAIR AT LOWER RIB FLANGE PER SRM 57-10-5, 9.75 BY 3.75, N/R 1237.Jan 5, 1998 · N717DH · Boeing 72723 · Wing, Rib/BulkheadSDR DHL9871736CRib · crackedAT C CHECK, LEFT WING INTERIOR, LOWER FLANGE OF WING RIB CRACKED AT STR 8 WS 686.5. INSTALLED RIB REPAIR PER SRM 57-10-5, 9.75 BY 3.75, N/R 1238.Jan 5, 1998 · N717DH · Boeing 72723 · Wing, Rib/BulkheadSDR DHL9871735CRib · crackedAT C CHECK, UPPER FLANGE OF WING RIB CRACKED AT STR 13 ATTACH FASTENER, WS 686.5. INSTALLED RIB REPAIR PER SRM 57-10-5, 9.75 BY 3.75, N/R 1239.Jan 5, 1998 · N717DH · Boeing 72723 · Wing, Rib/BulkheadSDR DHL9871709CRib · crackedAT C CHECK, RT WING RIB STA 601.5 CRACKED AT LOWER FLANGE AT STR 6. STOP DRILLED END OF CRACK, ACCOMPLISHED NDT, AND INSTALLED DOUBLER REPAIR PER SRM 57-10-5, 9.75 BY 3.75, N/R 2167.Jan 4, 1998 · N717DH · Boeing 72723 · Wing, Rib/BulkheadSDR DHL9871708CStringer · crackedAT C CHECK, RT WING UPPER AFT STR CRACKED AT WS 656.5. HFEC, INSTALLED REPAIRED ANGLES PER S/B 57A159, ANGLES 10.6 AND 4.3, N/R 2166.Jan 4, 1998 · N717DH · Boeing 72723 · Wing, Longeron/StringerSDR DHL9871756CTail Cone · delaminatedAT C CHECK, TAILCONE DELAMINATED. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8, N/R 4023.Jan 3, 1998 · N717DH · Boeing 72723 · Aerodynamic FairingsSDR DHL9877181CCowl · wornAT C CHECK, NR 1 ENGINE TOP COWLING BLOWOUT PANEL INNER TOP DOUBLER CHAFFED THROUGH. REPLACED DOUBLER PER SRM 54-10-3, 1.5 BY 12, N/R 6125.Jan 2, 1998 · N717DH · Boeing 72723 · Engine Cowling SystemSDR DHL9871787CFitting · crackedAT C CHECK, LOWER AFT CARGO COMPT DOOR CUTOUT, LOWER FORWARD STOP FITTING CRACKED. REPLACED FITTING PER SRM 51-30-2, N/R 3191.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage, Door HingeSDR DHL9871782CCowl · chafedAT C CHECK, NR 1 ENGINE TOP COWL INNER STRUCTURE NR 7 RIB FROM FRONT TO BACK CHAFFED THROUGH. INSTALLED DOUBLER PER SRM 54-10-3, 8 BY 1.25 BY .75, FILLER 1 BY .75, N/R 6126.Jan 2, 1998 · N717DH · Boeing 72723 · Engine Cowling SystemSDR DHL9871780CCowl · tornAT C CHECK, NR 1 ENGINE TOP COWLING OUTBD 3RD LATCH CUTOUT METAL TORN. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 54-10-3 DOUBLER 3 BY 2.5', FILLER 1 BY 5, N/R 6121.Jan 2, 1998 · N717DH · Boeing 72723 · Engine Cowling SystemSDR DHL9871779CCowl · crackedAT C CHECK, NR 1 ENGINE BOTTOM COWLING NR 4 LATCH CUTOUT AREA DOUBLER CRACKED. REPLACED DOUBLER PER SRM 51-40-3, 8 BY 7, N/R 6117.Jan 2, 1998 · N717DH · Boeing 72723 · Engine Cowling SystemSDR DHL9871778CCowl · chafedAT C CHECK, NR 1 ENGINE BOTTOM 5TH RIB FROM FRONT 7 O'CLOCK POSITION CHAFFED THROUGH. REMOVED AND REPLACED DOUBLER PER SRM 54-10-3, 8 BY 3, N/R 6116.Jan 2, 1998 · N717DH · Boeing 72723 · Engine Cowling SystemSDR DHL9871777CCowl · dentedAT C CHECK, NR 1 ENGINE BOTTOM COWLING EXTERIOR SKIN DENTED. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER PER SRM 54-10-3 9 BY 7, FILLER 5 BY 2, N/R 6112.Jan 2, 1998 · N717DH · Boeing 72723 · Engine Cowling SystemSDR DHL9871776CCowl · crackedAT C CHECK, NR 1 ENGINE NOSE COWL HAS SEVERAL CRACKS IN EXTERIOR SKIN. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 54-30-3. DOUBLER, 12 BY 2.5, FILLER 3.75 BY 2.75, N/R 6109.Jan 2, 1998 · N717DH · Boeing 72723 · Engine Cowling SystemSDR DHL9871775CCowl · crackedAT C CHECK, NR 1 ENGINE FIXED COWL 3RD HINGE FROM FRONT FLANGE WORN. STOP DRILL CRACK, INSTALLED REPAIR PER SRM 51-40-3, 4 BY 4, N/R 6095.Jan 2, 1998 · N717DH · Boeing 72723 · Engine Cowling SystemSDR DHL9871770CAngle · crackedAT C CHECK, L ANGLE AT FLOOR LEVEL AT RBL 64 CRACKED AT STA 585. REMOVED AND REPLACED ANGLE PER SRM 51-40-4 FROM STA 490 TO 590, N/R 5152.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage Miscellaneous StructureSDR DHL9871769CAngle · bentAT C CHECK, L ANGLE AT FLOOR LEVEL RBL 64 BENT STA 558. REMOVED AND REPLACED ANGLE PER SRM 51-40-4, 80 LONG, N/R 5150.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage Miscellaneous StructureSDR DHL9871768CAngle · crackedAT C CHECK, L ANGLE AT FLOOR LEVEL RBL 64, STA 544 CRACKED. REMOVED AND REPLACED ANGLE PER SRM 51-40-4, 80 INCHES LONG, N/R 5148.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage Miscellaneous StructureSDR DHL9871767CAngle · crackedAT C CHECK, L ANGLE CRACKED AT FLOOR LEVEL AT RBL 664, STA 524 CRACKED. REMOVED AND REPLACED ANGLE PER SRM 51-40-4, 80 LONG, N/R 5143.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage Miscellaneous StructureSDR DHL9871766CAngle · crackedAT C CHECK, L ANGLE AT FLOOR LEVEL AT RBL 64 CRACKED AT STA 504. REMOVED AND REPLACED ANGLE PER SRM 51-40-4, 80 LONG, N/R 5143.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage Miscellaneous StructureSDR DHL9871720CCowling · chafedAT C CHECK, NR 1 ENGINE TOP COWLING OVERHEAD AFT CATCH INNER DOUBLER CHAFFED THROUGH. REPLACED INNER DOUBLER PER SRM 54-10-3, 8 BY 6, N/R 6124.Jan 2, 1998 · N717DH · Boeing 72723 · Engine Cowling SystemSDR DHL9871719CAngle · crackedAT C CHECK, ANGLE CRACKED BENEATH SEAL RETAINER ABOVE AFT OF RT MLG DOOR AFT I/B HINGE. REMOVED AND REPLACED ANGLE SUPPORT PER SRM 51-10-1, 12 BY 4, N/R 7010.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage Miscellaneous StructureSDR DHL9871718CFlange · dentedAT C CHECK, STA 580 I/B FLANGE DENTED BELOW S-16R WEB. REMOVED PREVIOUS REPAIR, INSTALLED DOUBLER PER SRM 51-40-3, 15 BY 4.5, N/R 5151.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage Miscellaneous StructureSDR DHL9871717CFlange · dentedAT C CHECK, STA 540 I/B FLANGE DENTED BELOW S-16 R. REMOVED AND REPLACED DOUBLER REPAIR PER SRM 51-40-3, 12.75 BY 4.5, FILLER 12.75 BY 4, N/R 5147.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage Miscellaneous StructureSDR DHL9871716CRib · crackedAT C-CHECK, STA 520 CIR RIB I/B FLANGE CRACKED BELOW S-16 R WEB TIE CLIP. CUT OUT DAMAGED AREA , INSTALLED DOUBLER REPAIR PER SRM 51-40-3 16 BY 5.25, FILLER 16 BY 4.25, N/R 5146.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage Main, BulkheadSDR DHL9871715CRib · crackedAT C CHECK, STA 500 CIR RIB CRACKED BELOW STR 16R WEB AT INBD FACE. CUTOUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 51-10-2 16 BY 5.25, N/R 5144.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage Main, BulkheadSDR DHL9871714CSeat Track · damagedAT C CHECK, SEAT TRACK NR 2 AND FLOORBEAM DAMAGED AT BS 620 LEFT SIDE. CUT OUT DAMAGED SECTION FROM BS 620 TO 640, CUTOUT DAMAGED UPPER CHORD BEAM 11 STA 620 LBL 39. INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8, 28. INSTALLED NEW SECTION OF SEAT TRACK PER SRMJan 2, 1998 · N717DH · Boeing 72723 · Fuselage, Seat/Cargo Attach FittingsSDR DHL9871713CFitting · crackedAT C CHECK, LOWER AFT CARGO COMPT DOOR CUTOUT , 2ND STOP FITTING FROM AFT BOTTOM CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-10-1, N/R 3198.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage, Door HingeSDR DHL9871712CAngle · bentAT C CHECK, L ANGLE AT STA 605, AT RBL 64 BENT AT FWD END OF AIR DUCT. REPLACED ANGLE FROM 605 TO 620 PER SRM 51-10-1, N/R 3188.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage Miscellaneous StructureSDR DHL9871711CAngle · crackedAT C CHECK, L ANGLE AT FLOOR LEVEL RBL 64 CRACKED AND MISSING PIECE FROM STA 618. REPLACED ANGLE FROM 605 TO 620 PER SRM 51-10-1, N/R 3189.Jan 2, 1998 · N717DH · Boeing 72723 · Fuselage Miscellaneous Structure
Back to Boeing 727-23