Boeing 727-22C

Service difficulty reports · 2,328

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 = '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 01FDEA00502Fitting · corrodedN 773 DUR ROUTINE INSP, NLG DOOR UPR LINK FITTING BS 227.8 FND CORRODED. R&R FITTING IAW BAC 727 SRM 51-30-2.Jun 26, 2001 · N107FE · Boeing 72722C · Landing Gear Door Retract SectionSDR 01FDEA00453Support · crackedDURING ROUTINE INSP THE NR 1 SEAT TRACK SUPPORT AT BS 860 FOUND CRACKED. *S/D* REMOVED AND REPLACED SUPPORT PER IAW BAC 727 SRM 51-30-2.Jun 18, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS01236190Trunnion · corrodedINSPECTION TYPE:C, RT MLG TRUNNION FITTING HAS CORROSION AND SUSPECT CRACKING AROUND INBD SPECIAL STUD HOLE ON INBD FLANGE. TRUNNION FITTING REPLACED.Jun 16, 2001 · N945UP · Boeing 72722C · Main Landing Gear Attach SectionSDR UPS01236185Bracket · crackedINSPECTION TYPE:C #8 GRND SPOILER INBD END HINGE , CASTING ATTACHED TO MLG BEAM WHICH SUPPORTS THE END HINGE THROUGH A SUPPORT ROD IS CRACKED. REPLACED BRACKET IAW SRM 51-30-02. BRACKET REPLACED WITH ORIGINAL BO LTS.Jun 16, 2001 · N945UP · Boeing 72722C · SpoilersSDR UPS01236178Fitting · crackedINSPECTION TYPE:C TIAL SKID BAY L/H UPPER TIE LINK AFT FITTING, EVIDENCE OF CRACK ON V ERTICAL FLANGE BETWEEN FASTENERS. FITTING REPLACED.Jun 15, 2001 · N945UP · Boeing 72722C · Fuselage Main, StructureSDR UPS01236183Attach Fitting · corrodedINSPECTION TYPE:C, NR 5 FLAP TRACK FWD ATTACH LUG HAS CORROSION ON BORE LANDING GEAR FWD TRUNNION SUPPORT BEARING PIN. ATTACH LUG REPLACED.Jun 14, 2001 · N945UP · Boeing 72722C · Trailing Edge FlapsSDR UPS01236179Bulkhead · crackedINSPECTION TYPE:C, AFT PRESSURE BULKHEAD BS 1183 CRACK OF FWD FLANGE OF BL 17.8 LEFT VERTICAL BEAM AT WL 273 APPROX. REPAIRED/ MODIFIED PER EO B727-5310-11743-B APP C AND E.Jun 14, 2001 · N945UP · Boeing 72722C · Fuselage Main, BulkheadSDR DHL2001705545Plate · corrodedON LINE CHECK- BACK UP PLATE FOR INSPECTION HOLE AT STA 870 RBL 62 HAS CORROSION. REMOVED PRODUCTION DOUBLER AT STA 870 RBL 62 AND ACCESS PANEL. FABRICATED AND INSTALLED NEW PRODUCTION DOUBLER PER B-727 SRM 51-30-2 AND 53-10-1.Jun 14, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS01236182Rib · crackedINSPECTION TYPE:C, NUMBER ONE SLAT HAS CRACK IN RIB O/B OF I/B TRACK. REPAIRED IAW SRM 57-50-3.Jun 13, 2001 · N945UP · Boeing 72722C · Leading Edge DevicesSDR UPS01236181Doubler · crackedINSPECTION TYPE:C, CRACK FOUND IN SKIN DOUBLER AT F+N WINDOW POST RT AT WINDOW CUTOUT, RADIUS AT POINT E THROUGH XRAY INSPECTION. REPAIR CARRIED OUT PER UPS EO B727-5310-0012 APPENDIX D.Jun 13, 2001 · N945UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR UPS01236180Window Post · crackedINSPECTION TYPE:C CRACK FOUND IN F+N WINDOW POST ON SKIN DOUBLER ATL/H WINDOW POST AT WINDOW CUTOUT RADIUS POINT E REPAIRED IAW UPS EO B727-5310-0012Jun 13, 2001 · N945UP · Boeing 72722C · Fuselage Main, StructureSDR UPS01236174Web · crackedINSPECTION TYPE:C ON INSPECTION OF MCD LATCH FITTINGS BY NDT, CRACK FOUND IN FRAME WEB CLEAT AT BS 612.9 DAMAGED AREA TRIMMED OUT AND REPAIRED IAW SRM 51-40-2Jun 13, 2001 · N945UP · Boeing 72722C · Cargo/Baggage DoorsSDR UPS01236171Skin Panel · crackedINSPECTION TYPE:C CRACK IN SKIN BS 1342.4 AT WL246.5R CRACKED REMOVED BY BLENDING MATERIAL. DAMAGED AREA REPAIRED IAW SRM5 3-30-3FIG3A USING 2024T3.050 AND .040.Jun 13, 2001 · N945UP · Boeing 72722C · Fuselage Main, Plate/SkinSDR DHL2001705544Fitting · corrodedON LINE CHECK- BS 870 FITTING TO HORIZ BEAM RT WHEEL WELL SPLICE TEE IS CORRODED AT APPROX W/L 175. REMOVED SPLICE TEE AT BS 870 FITTING TO HORIZ BEAM RT W/W APPROX W/L 175 AS PER B-727 SRM 51-30-2. TRIMMED FITTING HORIZ FLANGES B/S 870 APPROX W/L 175 AS PER Jun 13, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous StructureSDR 01FDEA00414Pressure Panel · crackedDURING ROUTINE INSP LT SIDE WEB IN NOSE WHEEL WELL WAS FOUND CRACKED AT BS 1260. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Main, BulkheadSDR 01FDEA00413Web · crackedDURING ROUTINE INSP, LT SIDE WEB IN AIRSTAIR COMPT FOUND CRACKED AT LIGHTENING HOLE AT BS 1263. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-40-2, 51-30-2.Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 01FDEA00412Fitting · crackedDURING ROUTINE INSP, RT ELEVATOR TAB ROD FITTING FOUND CRACKED. *S/D* REMOVED AND REPLACED RIGHT ELEVATOR TAB PER IAW BAC 727 MM 27-30-011-2.Jun 11, 2001 · N107FE · Boeing 72722C · Elevator Tab Control SystemSDR 01FDEA00401Beam · crackedDURING ROUTINE INSP BS 1183 BULKHEAD VERTICAL BEAM AT LBL 27 FOUND CRACKED AT WL 263. *S/D* REMOVED AND REPLACED PER VERTICAL BEAM PER IAW FEDEX EO 7-5310-7-2346 PART 2.Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Main, BulkheadSDR 01FDEA00411Web · crackedDURING ROUTINE INSP, RT SIDE WEB IN AFT AIRSTAIR AREA FOUND CRACKED AT BS 1283. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 BAC 727 SRM 51-40-2, 51-30-2.Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 01FDEA00410Tie Clip · crackedDURING ROUTINE INSP, STR TIE CLIP AT BS 312, STR 4R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 01FDEA00409Tie Clip · crackedDURING ROUTINE INSP, STR TIE CLIP AT BS 328, STR 14R FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-1, 51-30-2.Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 01FDEA00408Skin · crackedDURING ROUTINE INSP, LT FWD EMERGENCY EXIT HATCH UPPER INNER SKIN FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 52-00-3, 51-30-2.Jun 11, 2001 · N107FE · Boeing 72722C · Emergency ExitsSDR 01FDEA00407Bulkhead · crackedDURING ROUTINE INSP, HFEC IND TWO CRACKS IN BS 1183 BULKHEAD WEB AT WL 283. *S/D* REMOVED AND REPLACED WEB PER IAW FEDEX EO 7-5310-7-5000 PARTS 2 & 4.Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Main, BulkheadSDR 01FDEA00406Bulkhead · crackedDURING ROUTINE INSP, HFEC IND CRACK IN BS 1183 BULKHEAD WEB AT WL 283, RBL 17.8. *S/D* REMOVED AND REPLACED PER IAW FEDEX EO 7-5310-7-5000 PARTS 3 & 5.Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Main, BulkheadSDR 01FDEA00405Fitting · crackedDURING ROUTINE INSP, HFEC IND CRACK IN FASTENER HOLES IN ROW 3, LT BS 870 FITTING AT STR 9L. *S/D* HFEC IND NO CRACKS PER IAW BAC 727 NDT MANUAL PART 6.Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR 01FDEA00404Floorbeam · crackedDURING ROUTINE INSP FLT DECK FLOORBEAM WEB AT BS 299, LBL 6 FOUND CRACKED. *S/D* REMOVED, REPLACED AND FAB WEB PER IAW BAC 727 SRM 51-20-1, SRM 51-30-2.Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Main, Floor BeamSDR 01FDEA00403Rib · crackedDURING ROUTINE INSP LWR RUDDER, LWR THRUST HINGE RIB FOUND CRACKED AT FASTENER COMMON TO FIN REAR SPAR. *S/D* HFEC IND CRACK TERMINATED. REMOVED, REPLACED AND FAB PER IAW FEDEX DRAWING SRM 27-55-005, SRM 51-30-2.Jun 11, 2001 · N107FE · Boeing 72722C · Rudder, Spar/RibSDR 01FDEA00402Support · crackedDURING ROUTINE INSP THE NR 1 SEAT TRACK SUPT AT BS 840 FOUND CRACKED.Jun 11, 2001 · N107FE · Boeing 72722C · Fuselage Miscellaneous StructureSDR DHL2001705003Turbine Wheel · damagedEXCESSIVE VIBRATION AFTER TAKEOFF - DURING CLIMB NR 3 ENG VIBRATED AND LOST POWER. DECLARED EMERGENCY. RETURNED TO ROC. FOUND TURBINE WHEEL DAMAGED. REMOVED AND REPLACED ENGINE. CORRECTIVE ACTION - REMOVED AND REPLACED #3 ENGINE PN JT8D-7B OFF S/N 653870,Jun 2, 2001 · N705DH · Boeing 72722C · Turbine SectionSDR UPS01236010Pressure Panel · crackedINSPECTION TYPE:N/A, RT WHEEL WELL CRACKS. *S/D* REPAIRED PER SRM 51-1-9A.May 26, 2001 · N928UP · Boeing 72722C · Fuselage Main, BulkheadSDR 2001F00129Connector · damagedNR 3 ENGINE FIRE LIGHT CAME ON DURING CLIMB-OUT, PERFORMED ENGINE FIRE IN FLIGHT PROCEDURE. REPAIRED SEVERAL WIRES TO FIRE TEST SWITCH. REMOVED AND REPLACED THE FIRE TEST SWITCH. REPAIRED CONNECTOR AT NR 3 ENGINE FIRE WALL. HIGH POWER ENGINE RUN OPERATIONAMay 19, 2001 · N429EX · Boeing 72722C · Fire DetectionSDR 2001F00130Accessory Unit · faultyDURING CRUISE FLIGHT, NR 3 FIRE LIGHT ILLUMINATED AND BELL SOUNDED, FOLLOWED PROCEDURES. LEFT BOTTLE DISCHARGE LIGHT DID NOT ILLUMINATE. FIRE HANDLE LIGHT DID NOT EXTINGUISH. INSPECTED ENGINE AND FOUND NO FIRE. REMOVED AND REPLACED FIRE DETECTION ACCY UNITMay 18, 2001 · N429EX · Boeing 72722C · Fire DetectionSDR 01FDEA00349Switch · inoperative01-155 ON DEPART WHEN FLAP 2 DEG SEL ON RETRACTION LIGHT ON FWD PNL FLAP/SLAT IND REMAIN AMBER. FND L/E FLAP OVERRIDE TEST SWITCH IN OVERRIDE POS, RETURN TO NORM POSITION, OPS CK GOOD PER 727 MM 27-81-000-6.May 15, 2001 · N112FE · Boeing 72722C · Leading Edge Slat Control SystemSDR DHL2001705538Skin · crackedC-CHECK- LT WING IB L/E EDGE O/B SIDE UPPER SURFACE HAS 2 INCH CRACK. REMOVED DAMAGE AREA AND INSTALLED REPAIR PER B-727 SRM 57-30-4 FIG.6May 7, 2001 · N705DH · Boeing 72722C · Leading Edge DevicesSDR DHL2001705540Bracket · crackedC-CHECK, NR 12 SPOILER ACTUATOR MOUNT BRACKET IS CRACKED, OUTBOARD LWR LUG.REMOVED AND REPLACED NR 12 SPOILER ACTUATOR BRACKET.May 5, 2001 · N705DH · Boeing 72722C · Drag Control ActuatorSDR DHL2001705515Web · crackedC-CHECK WEB CRACKED AT NLG WW RT SIDE AT STA 257 W/L 180 IN BETWEEN PANELS 3123 AND3125 AT 3 EA LOCATION. INSTALLED FILLER & DOUBLER REPAIR AT NLG WW RT SIDE AT STA 257 W/L 180 AS PER B727 S/B 53-00-65.Apr 30, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous StructureSDR CA010529018Nut · cracked(CAN) LT MAIN GEAR OLEO WOULD NOT HOLD AIR CHARGE. OLEO FOUND LOW SEVERAL TIMES AND RECHARGED. UPON INVESTIGATION IT WAS FOUND THAT THE RETAINING NUT FOR THE UPPER OLEO SUPPORT TUBE WAS CRACKED, CAUSING AIR LEAKAGE. FURTHER INVESTIGATION ALSO REVEALED CORROSIOApr 29, 2001 · Boeing 72722C · Main Landing Gear Strut/Axle/TruckSDR DHL2001705531Rib · crackedFOUND WING O/B RIB CRACKED USING HFEC INSP.Apr 23, 2001 · N705DH · Boeing 72722C · Wing, Rib/BulkheadSDR UPS01235805Pressure Panel · corrodedINSPECTION TYPE: C, EVIDENCE OF CORROSION, NOSE WHEEL WELL TORQUE BOX WDF PANHEL BS 294 - 309 . REPAIR CARRIED OUT IAW SRM 53-10-9Apr 23, 2001 · N930UP · Boeing 72722C · Fuselage Main, BulkheadSDR UPS01235802Casting · corrodedINSPECTION TYPE:C, LT O/B AILERON LOCKOUT MECHANISM, MAIN SUPPORT CASTING HAS EVIDENCE OF CORROSION ON NUMEROUS BUSHING AREAS. CASTING REPLACED IAW SRM 51-30-02 & DRAWINGS 65-21776 & 65-21779Apr 23, 2001 · N930UP · Boeing 72722C · Aileron Control SystemSDR DHL2001705509Frame · corrodedAT C-CHECK-NOSE W/W RT SIDE WALL, SIDE FRAME CORRODED AT INNER AREA OF FUSE TUNNEL STA 257 WL 180 AND IN BETWEEN ACCESS PANEL 3123. REMOVED FASTENER AND CUTOUT DAMAGE SECTION WITH CORROSION BEYOND LIMITS AT T-ANGLE WEB SUPPORT AT NOSE W/W RT SIDE WALL BETWEENApr 21, 2001 · N705DH · Boeing 72722C · Fuselage Main, FrameSDR UPS01235792Casting · crackedINSPECTION TYPE:C, LT GEAR OPERATED DOOR SEQUENCE VALVE SUPPORT CASTING CRACKED. CASTING REPLACED IAW MM 32-32-31Apr 21, 2001 · N930UP · Boeing 72722C · Main Landing GearSDR UPS01235658Control Rod · lack of lubeINSPECTION TYPE:IN AILERON STIFF IN LEFT TURNS AILERON SPRING CARTRIDGE FOUND OUT OF RIG. RE-ADJUSTED I.A.W. B727 M .M.27-61-21. SPRING CARTRIDGE OPS CHECKS SERV. CONTROL WHEEL INPUTS (FORCE) THE SAME LEFT AND RIGHT NOTE: MIXER CONTROL ROD AND SPD BRK INPUApr 21, 2001 · N928UP · Boeing 72722C · Aileron Control SystemSDR DHL2001705511Stiffener · corrodedAT C-CHECK- WING CENTER SECTION STA 870 WEB VERTICAL STIFFENER AT BL 0 HAS CORROSION. REMOVED WEB VERTICAL STIFFENER AT WING CENTER SECTION FOR REPLACEMENT AS PER B727 SRM 51-30-2. INSTALLED NEW VERTICAL STIFFENER AT CENTER SECTION BS 870 BL 0 AS PER B727 SRApr 20, 2001 · N705DH · Boeing 72722C · Wing, Center BoxSDR DHL2001705500Channel · corrodedAT C-CHECK, FUSELAGE CORROSION AT HAT CHANNEL ATTACHED TO FLOORBEAM, STA 344 RBL 39. REMOVED HAT CHANNEL FOR REPLACEMENT AS PER SRM 51-30-22. FABRICATED AND INSTALLED NEW HAT CHANNEL AT FWD LAV STA 344 FROM RBL 15 TO RBL 60 AS PER SRM 53-10-2 FIG 3 AND 51-30Apr 20, 2001 · N705DH · Boeing 72722C · Fuselage Miscellaneous StructureSDR UPS01235791Support · corrodedINSPECTION TYPE:C, O/B AILERON LT WING, ALL HINGE SUPPORTS ON REAR SPAR OF AILERON SHOW EVIDENCE OF CORROSION. LT O/B AILERON REMOVED IAW MM 27-10-31, NEW AILERON INSTALLED IAW MM 27-10-31.Apr 20, 2001 · N930UP · Boeing 72722C · AileronsSDR UPS01235812Hinge · corrodedINSPECTION TYPE:C BOTH END HINGES ON NR 7 SPOILER PANEL ARE CORRODED BEYOND LIMITS. REPLACED HINGES IAW SRM 51-30-02Apr 20, 2001 · N930UP · Boeing 72722C · SpoilersSDR UPS01235809Casting · corrodedINSPECTION TYPE: C, EVIDENCE OF CORROSION ON LEFT OUTBOARD AILERON TURNAROUND GEARBOX CASTING. REPLACED GEARBOX CASTING IAW 27-10-131Apr 20, 2001 · N930UP · Boeing 72722C · Aileron Control SystemSDR UPS01235799Support · corrodedINSPECTION TYPE:C, NR 7 SPOILER, I/B END HINGE SUPPORT ATTACHED TO SPOILER SUPPORT BEAM I S CORRODED BEYOND LIMITS. /BEND HINGE REPLACED IAW SRM 51-30-02Apr 20, 2001 · N930UP · Boeing 72722C · SpoilersSDR UPS01235798Rib · corrodedINSPECTION TYPE:C, NR 7 SPOILER, SUPPORT RIB ON I/B SIDE ATACHED TO MLG BEAM IS CORRODED BEYOND LIMITS. REPLACED SUPPORT RIB IAW SRM 51-30-2Apr 20, 2001 · N930UP · Boeing 72722C · Spoilers
Back to Boeing 727-22C