Boeing 727-22C

Service difficulty reports · 2,328

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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 = '72722C'
  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 UPS01235790Casting · corrodedINSPECTION TYPE:C, NR 7 SPOILER SUPPORT CASTING IS CORRODED BEYOND LIMITS. NR 7 SPOILER CASTING REMOVED & REPLACED IAW DRW 65-16216 & IAW SRM 51- 10-2Apr 20, 2001 · N930UP · Boeing 72722C · SpoilersSDR UPS01235775Skin · crackedINSPECTION TYPE: C, ON HFEC INSPECTION CRACKS FOUND ON FUSELAGE SKIN AT BS 235.8 BETWEEN SL 223 & 225 LT. SKIN REPAIR CARRIED OUT IAW SRM 530 FIG 3Apr 20, 2001 · N930UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR DHL2001705530Support Fitting · crackedAT C-CHECK - LEFT MAIN BEAM WHEEL WELL SUPPORT FITTING BS 930 SHOW'S CRACK AT L-18L, AS MKD LOWER FWD SIDE. CRACK VERIFY BY NDT AS PER 51-000 FIG 1 RUNNING BETWEEN FASTENERS 1 & 2 FROM BOTTOM. LEFT MAIN GEAR WHEEL WELL SUPPORT FITTING BS 930 CRACK HAS BEEN PApr 19, 2001 · N705DH · Boeing 72722C · Fuselage, Landing Gear Attach FittingsSDR DHL2001705518Panel · damagedC-CHECK- LT WING FIXED LEADING EDGE. CORNER OF L/E PANEL IS BROKEN OFF. LOCATED DIRECTLY BELOW GHE I/B WING ROOT LANDING LIGHT ASSY. INSTALLED DOUBLER & FILLER.Apr 19, 2001 · N705DH · Boeing 72722C · Wing, Plate/SkinSDR DHL2001705502Floor Panel · corrodedAT C-CHECK, FWD LAVATORY FWD FLOOR PANEL AT FS 303 HAS SEVERAL SPOTS OF CORROSION. REMOVED FWD LAV FLOOR PANEL AT STA 303 FOR REPLACEMENT AS PER B727 SRM 51-30-2. MADE NEW FLOOR PANEL MATERIAL USED 2024 T3 (.040) PO 83110438 LOT 220081 MATERIAL SIZE 30 X 12.Apr 19, 2001 · N705DH · Boeing 72722C · Fuselage Floor PanelSDR DHL2001705525Angle · corrodedC-CHECK, FWD LAVATORY HAS CORROSION UNDER CENTER ANGLE AT FS 340 RBL 40.REMOVED DAMAGED SECTION AND INSTALLED REPAIR.Apr 19, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous StructureSDR DHL2001705522Floor Support · crackedC-CHECK- CORROSION & CRACKED FLOOR SUPPORT AFT BAGGAGE COMPART LBL22 STA 1012-1027. REMOVED AND REPLACED FLOOR SUPPORT RUNNER FROM STA 960 TO STA 1027 LBL22 IAW B727 SRM 51-30-2.Apr 19, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous StructureSDR DHL2001705520Floor Support · corrodedC-CHECK- CORROSION, FLOOR SUPPORT AFT BAGGAGE COMPART STA 1160 STR 26 WL 156 LBL 24 UNDER SIDE. REMOVED AND INSTALLED NEW FLOOR SUPPORT AT AFT CARGO COMPT BS 1160 FROM STR 26L TO 26R AS PER B727SRM 51-40-2 AND 51-30-2.Apr 19, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS01235780Web · corrodedINSPECTION TYPE: C, SURFACE CORROSION FOUND ON LOWER SURFACE OF HORIZONTAL WEB S18A RT, BETWEEN BS 880 & 950. ALL REPAIRS CARRIED OUT IAW SRM 51-10-6, 51-10-1, 51-10-2, 51-30-2 & SMRO EO 2001-013-001 UPS ENGINEERING FILE NO 727-53-20015Apr 19, 2001 · N930UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR DHL2001705508Retainer · crackedAT C-CHECK, FUSELAGE BS 870 REAR UPPER CHORD CENTER TANK RBL 46 TO OUT. HEAVY CORROSION AND PRESSURE SEAL RETAINER IS ALSO CRACKED. FOUND SEAL RETAINER ATTACH ANGLE TO BE CORRODED BS 870 RBL46 AND CRACKED. REMOVED ATTACH ANGLE FROM RBL 40 TO RBL 63 APPROX, Apr 18, 2001 · N705DH · Boeing 72722C · Fuel StorageSDR DHL2001705506Doubler · damagedAT C-CHECK, NR 3 ENG, LWR COWL INTERNAL SURFACE, RIGHT AFTER 2ND U-BOLT, STRINGER PREVIOUS DOUBLER REPAIR SHOWS BIG HOLE (8 O''CLOCK POS APPROX). REMOVED DAMAGED EXISTING DOUBLER IAW B727 SRM 51-30-2. FABRICATED DOUBLER 8 X 12 2024-0 .050 LOT 471153 PO 83196Apr 18, 2001 · N705DH · Boeing 72722C · Engine Cowling SystemSDR DHL2001705504Seat Track · damagedAT C-CHECK, SEAT TRACK NR 6 SHOWS PREVIOUS HEAVY BLEND-OUT REWORK AT BS 680 - BS 695 RBL 45. REMOVED AND REPLACED SECTION OF SEAT TRACK FROM STA 680 TO STA 695 RBL 45 AS PER B727 SRM 51-10-2.Apr 18, 2001 · N705DH · Boeing 72722C · Fuselage, Seat/Cargo Attach FittingsSDR UPS01235808Stringer · corrodedINSPECTION TYPE:C CORROSION FOUND ON S18A LT AT BS 890 TO 940 HORIZ. FLANGE AT BODY F AIRING SUPPORT. REPAIR CARRIED OUT IAW SRM 51-30-2 51-30-6 & SMRO EO 2001-013-002 UPS ENGINEERING FILE NO 727-53-20016Apr 18, 2001 · N930UP · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS01235807Stringer · corrodedINSPECTION TYPE: C, CORROSION FOUND AT BS 870 LT ON S18A LWR AFT ATTACH BOLT LOCATION. REPAIR CARRIED OUT IAW SRM 51-10-6 & SHANNON MRO EO 2001-013-002 UPS ENGINEERING FILE NO 727-53-20016Apr 18, 2001 · N930UP · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS01235777Housing · corrodedINSPECTION TYPE: C, CORROSION ON OPERATING HANDLE HOUSING ON AFT RT EMERGENCY EXIT. OPERATING HOUSING REPLACED IAW SRM 51-30-2 & PER DRW 50-7978Apr 18, 2001 · N930UP · Boeing 72722C · Emergency ExitsSDR DHL2001705514Antenna · delaminatedAT C-CHECK- NR 2 ATC ANTENNA DELAMINATED AND GASKET DETERIORATED. REMOVED NR 2 ATC ANTENNA AND ROUTED TO STOCK IAW B727 MM 34-43-41. INSTALLED NR 2 ATC ANTENNA AS PER B727 MM 34-43-41. OPS CHECK NR 2 ATC SYSTEM PER B727 MM 34-43-0. OPS CHECK GOOD.Apr 17, 2001 · N705DH · Boeing 72722C · ATC Transponder SystemSDR DHL2001705507Spoiler · delaminatedC-CHECK, NR 9 SPOILER IS DELAMINATED AT FWD UPPER RT CORNER. REMOVED AND REPLACED NR 9 SPOILER PANEL PER B727 MM 27-62-1 P 401. ADJUST AND TEST. ACCOMPLISH OPERATIONAL CHECK OF NR 9 SPOILER IAW B727 CH 27-62-0 MM, OPS CHECK OK.Apr 17, 2001 · N705DH · Boeing 72722C · SpoilersSDR DHL2001705503Angle · crackedAT C-CHECK, NR 2 ENG LT AFT COWL HAS LOWER FWD COENER WITH CRACK ANGLE. REMOVED AND REPLACED NR 2 LT AFT CORNER ANGLE. MATERIAL USED 2024T3 .050 MATERIAL SIZE 12 X 2.5 PO 83112359 LOT 35803 AS PER B727 SRM 51-30-202. TREATED AND PRIMED AREA AS PER B727 SRMApr 17, 2001 · N705DH · Boeing 72722C · Engine Cowling SystemSDR DHL2001705501Attach Angle · crackedAT C-CHECK, MAIN CARGO DOOR CUTOUT, UPPER AFT CORNER AREA, GILL LINER ATTACH ANGLE SHOWS CRACK DAMAGE. REMOVED CRACKED GIL LINER ATTACH ANGLE AT MAIN CARGO DOOR CUTOUT AFT CORNER AREA AS PER B727 SRM 51-30-2. REMOVED AND REPLACED GILL LINER ATTACH ANGLE ON CApr 17, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous StructureSDR DHL2001705529Rib · crackedC-CHECK- C/W DHL J/C MPRGAA1A57005 INSP. REPLACE WING OUTBOARD RIB WS 686.5. PERFORMED HFEC INSP OF RT WING RIB STA 686.5 RIB TO STRINGER ATTACH POINTS. CRACK FOUND AT UPPER STRINGER FLANGE AT STR 12. INSTALLED REPAIR.Apr 17, 2001 · N705DH · Boeing 72722C · Wing, Rib/BulkheadSDR DHL2001705537Rib · crackedC-CHECK C/W DHL J/C MPRGAA1AS7005 INSP, REPLACE WING OUTBOARD RIB WS 738.5 RTPERFORMED HFEC INSP. OF RT. WING RIB STA 738.5 RIB, CRACK FOUND AT LOWER RIB STR 8. INSTALLED RIB REPAIR.Apr 17, 2001 · N705DH · Boeing 72722C · Wing, Rib/BulkheadSDR DHL2001705528Rib · crackedC-CHECK C/W DHL J/C MPRGAA1A57005INSP, REPLACE WING OUTBOARD RIB WS 656.5. PERFORMED HFEC INSP OF RT WING RIB STA 656.5, RIB TO STRINGER ATTACH POINTS CRACK FOUND AT UPPER STRINGER FLANGE AT STRINGERS 13,12. INSTALLED REPAIRS.Apr 17, 2001 · N705DH · Boeing 72722C · Wing, Rib/BulkheadSDR DHL2001705534Beam · crackedON C-CHECK, FWD SIDE BS 1183 VERTICAL BEAM LBL 26.83 WL 268 HAS A VISUAL CRACK TOP SIDE OF THE LIGHTENING HOLE (MARKED) REP MPRGAA1A53001 S/B 727-53AO173. AD 85-20-03. REMOVED FASTENERS ON VERTICAL BEAM STA 1183 BULKHEAD BL 2683, REMOVED STIFFENER TEES AT WL 2Apr 17, 2001 · N705DH · Boeing 72722C · Fuselage Main, StructureSDR DHL2001705527Rib · crackedAT C CHECK C/W DHL J/C MPRGAA1A57005 INSP, REPLACE WING OUTBOARD RIB WS 546.5 RT. HFEC INDICATED RIB IS CRACKED.Apr 17, 2001 · N705DH · Boeing 72722C · Wing, Rib/BulkheadSDR DHL2001705526Skin · dentedC-CHECK- LOWER FWD CARGO DOOR EXT SKIN HAS MANY DENTS. REPAIRED CARGO DOOR SKIN.Apr 17, 2001 · N705DH · Boeing 72722C · Cargo/Baggage DoorsSDR DHL2001705519Attach Angle · damagedC-CHECK- MAIN CARGO DOOR CUT-OUT AT BS 510 GILLLINER ATTACHING ANGLE DAMAGED. REMOVED & REPLACED GILL LINER ATTACH ANGLE.Apr 17, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous StructureSDR DHL2001705516Angle · crackedAT C-CHECK-T/E LWR PANEL SUPPORT ANGLE IS CRACKED AT STA 545. REPLACED T/E LWR PANEL SUPPORT ANGLE AT R/W STA 545 PER B727 SRM 51-30-2.Apr 16, 2001 · N705DH · Boeing 72722C · Wing Miscellaneous StructureSDR DHL2001705505Angle · bentAT C-CHECK, NR 1 ENG, LWR COWL O/B FWD AREA , INT ANGLE WORN AND BENT. REFERENCE: FWD OF 2ND U-BOLT, UPPER OF OIL SERVICE DOOR. REMOVED AND REPLACED INTERNAL ANGLE ON 1 ENG, LWR COWL O/B FWD OF 2ND U-BOLT ABOVE OIL SERVICE DOOR PER B727 SRM 51-30-2. MAT USEApr 16, 2001 · N705DH · Boeing 72722C · Engine Cowling SystemSDR DHL2001705521Angle · corrodedC-CHECK LT RAM AIR DUCT SUPPORT STRUCTURE HAS CORROSION BULGE BS 660 AT LT RAM AIR DOOR INBD HINGE. REMOVED AND REPLACED RAM AIR DUCT SUPPORT ANGLE AS PER B727 SRM 51-30-2.Apr 16, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous StructureSDR DHL2001705541Pressure Panel · crackedAT C-CHECK, NOSE GEAR WHEEL WELL RT SIDEWALL PANEL IS CRACKED BS 285.6 WL 158 CRACK RUNNING ALONG FASTENERS ROWS, 2 PLACES. ACCOMPLISHED HFEC INSP OF NOSE WHEEL WELL RT SIDEWALL PANEL. VERIFIED AND MARKED ENDS OF CRACKS. CUTOUT DAMAGE SECTION. NO FURTHER CApr 15, 2001 · N705DH · Boeing 72722C · Fuselage Main, BulkheadSDR DHL2001705513Pressure Panel · crackedAT C-CHECK, NOSE GEAR WHEEL WELL RT SIDEWALL PANEL IS CRACKED BS 285.6 WL 158. CRACK RUNNING ALONG FAST ROWS-2 PLACES.- MRD 2. REMOVED FASTENERS AND PAINT AT NWW. RT SIDEWALL BS 285 WL 158 TO VERIFY CRACK ENDS AS PER B727 SRM 51-30-2. ACCOMPLISHED HFEC INSPApr 15, 2001 · N705DH · Boeing 72722C · Fuselage Main, BulkheadSDR DHL2001705512Pressure Panel · crackedAT C-CHECK- NOSE GEAR WHEEL WELL RT SIDEWALL PANEL IS CRACKED BS 285.6 WL 158. CRACK RUNNING ALONG FAST ROWS-2 PLACES. FABRICATED EXTERNAL DOUBLER REPAIR AT NOSE WW RT SIDEWALL FROM BS 250 TO 294.5 AS PER B727 S/B 53-0065- MAT USED 2024 T3 .050 38 X 34 INCH LApr 15, 2001 · N705DH · Boeing 72722C · Fuselage Main, StructureSDR DHL2001705510Pressure Panel · crackedC-CHECK- NLG WW RT SIDEWALL PANEL IS CRACKED BS 285.6 WL 158. CRACK RUNNING ALONG FASTENER ROWS-2 PLACES. INSTALLED DOUBLER REPAIR AT NLG WW RT SIDE FABRICATED EXTERNAL DOUBLER REPAIR AT NOSE WW RT SIDEWALL FROM BS 250 TO 294.5 AS PER B727 S/B 53-0065- MAT USEApr 15, 2001 · N705DH · Boeing 72722C · Fuselage Main, StructureSDR DHL2001705543Pressure Panel · crackedC-CHECK- NLG WW RT SIDEWALL PANEL CRACKED BS 263.5 FASTNENER ROW UPPER OF AFT ACCESS DOOR. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR.Apr 15, 2001 · N705DH · Boeing 72722C · Fuselage Main, StructureSDR DHL2001705524Pressure Panel · crackedC-CHECK- NLG WW TOP CEILLING PANEL IS CRACKED AROUND FASTENER ROW AT BS285.5 RBL 3. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR & FILLERApr 15, 2001 · N705DH · Boeing 72722C · Fuselage Main, StructureSDR DHL2001705523Cover · crackedC-CHECK NLG WW LT SIDEWALL LWR CHORD COVER SHOW CRACK AROUND FAST HEAD 2 EA. REMOVED AND REPLACED SIDEWALL LWR CHORD COVER AT NLG WW LT SIDE AS PER B727SRM 51-30-2.Apr 15, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous StructureSDR 20010514SG007Hydraulic Line · brokenLOST ''A'' SYSTEM HYDRAULICS IN FLIGHT. RAN APPROPRIATE CHECK LIST. EMERGENCY DECLARED. REMOVED AND REPLACED BROKE HYDRAULIC LINE ON NR 2 SPOILER ACTUATOR. (M)Mar 31, 2001 · N421EX · Boeing 72722C · Hydraulic System, MainSDR UPS01235445Girt Bar · inoperativeINSPECTION TYPE: PREFLT, ESCAPE SLIDE GIRT BAR STOW HOOKS DO NOT HOLD BAR IN PLACE WHEN SLIDE IS DISENGAGED. REMOVED MAIN ENTRY DOOR SLIDE COVER FOR REPAIR. INSTALLED MAIN ENTRY DOOR EVACUATION SLIDE AND COVER IAW B727 MM 25-60-03.Mar 21, 2001 · N929UP · Boeing 72722C · Escape SlideSDR UPS01235325Slide · out of positionINSPECTION TYPE IN ESCAPE SLIDE FELL OUT. RE-PACKED EMERGENCY ESCAPE SLIDE.Mar 21, 2001 · N929UP · Boeing 72722C · Escape SlideSDR UPS01235229Stringer · corrodedINSPECTION TYPE:C+SI, DURING REPAIR TO CORRODED STRINGER 24R AT BS 463 FASTENER HOLE SIZES AT ENDS OF FRAME TO SKIN WERE FOUND TO BE EXCESSIVE BS 460 BETWEEN S2 4R AND S25R. CARRIED OUT REPAIR IAW SRM 53-10-4.Mar 5, 2001 · N941UP · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS01235184Seat · defectiveINSPECTION TYPE:N/A, CAPT''S SEAT W/N LOCK INTO POSITION. CLEANED AND LUBED HORIZONTAL MECHANISM ON CAPT''S SEAT O/C IAW M/M 25-10-42. SEAT CHECKS OK.Mar 3, 2001 · N942UP · Boeing 72722C · Flight Compartment EquipmentSDR UPS01235253Bulkhead · chafedINSPECTION TYPE:C+SI, OPERATING HANDLE FOR AIRSTAIRS PUMP HAS CHAFED AFT PRESSURE BULKHEAD. REPAIRED IAW SMRO EO 2001-006-019.Feb 23, 2001 · N941UP · Boeing 72722C · Fuselage Main, BulkheadSDR UPS01235214Splice · crackedINSPECTION TYPE:C+SI, SPLICE FITTING AT BS 1040 (REAR CARGO COMPT) CORRODED AND CRACKED. REPLACED FITTING IAW SRM 51-30-2.Feb 23, 2001 · N941UP · Boeing 72722C · Fuselage Miscellaneous StructureSDR DHL2001705002Connector · dirtyON GEAR EXTENSION, RECEIVED NO GREEN-LIGHT ON NOSE GEAR INDICATION ON FWD CENTER PANEL. AFTER LANDING AND DURING ROLLOUT LIGHT INDICATION ILLUMINATED AS NORMAL. CLEANED CONNECTOR ON NOSE DOWNLOCK SWITCH. COMPLIED WITH NOSE GEAR LOCK TEST PER B727 MM CH 32-6Feb 23, 2001 · N705DH · Boeing 72722C · Landing Gear Position and WarningSDR UPS01235255Fastener · corrodedINSPECTION TYPE:C+SI, BOLTS FOUND CORRODED AT BS 360 BETWEEN STR 24-26L AND 24-26R. HOLES REWORKED IAW SMRO EO 2001-006-020.Feb 22, 2001 · N941UP · Boeing 72722C · Fuselage Main, FrameSDR UPS01235230Pressure Panel · crackedINSPECTION TYPE:C+SI, NOSE WHEEL WALKWAY AREA PRESSURE PANEL CRACKED AT UPPER SIDE BS 309 LBL 4. CARRIED OUT REPAIR IAW SRM 51-20-1.Feb 22, 2001 · N941UP · Boeing 72722C · Fuselage Main, StructureSDR CA010307012Tube · cracked(CAN) AIRCRAFT ARRIVED WITH NOSE LANDING GEAR FLAT. ATTEMPTS TO RESERVICE OLEO FAILED DUE TO RAPID LEAKING. UPON INVESTIGATION IT WAS FOUND THAT THE INNER PISTON TUBE ASSEMBLY WAS CRACKED AT ITS LOWER FLANGE ALLOWING FLUID AND NITROGEN TO ESCAPE. TUBE ASSEMBLYFeb 21, 2001 · Boeing 72722C · Nose/Tail Landing Gear Strut/AxleSDR UPS01235244Stringer · corrodedINSPECTION TYPE:C+SI, CORROSION ON STRINGER 25R BS 463. REPLACED STRINGER IAW SRM 53-10-3.Feb 21, 2001 · N941UP · Boeing 72722C · Fuselage Main, Longeron/StringerSDR UPS01235235Panel · corrodedINSPECTION TYPE:C+SI, NR 5 BALANCE BAY HINGE LT ELEVATOR HAS SLIGHT SURFACE CORROSION. BALANCE PANEL REPLACED IAW MM 27-30-21.Feb 20, 2001 · N941UP · Boeing 72722C · Elevator, Plate/SkinSDR UPS01235273Attach Fitting · crackedINSPECTION TYPE:C+SI, RT WING - CRACK AT NR 7 FLAP TRACK ATTACH AREA O/B FASTENER ROW, THIRD HOLE FROM FRONT. REPAIR CARRIED OUT IAW SRM 51-30-5 & SMRO WO 2001-006-013 UPS ENGINEERING FILE NR B727-5730-14010-A.Feb 19, 2001 · N941UP · Boeing 72722C · Wing, Control Surface Attach Fittings
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