Boeing 727-25C

Service difficulty reports · 2,007

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 = '72725C'
  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 UPS01236934Pressure Panel · crackedINSPECTION TYPE:C NLG WW, BEHIND NOSE LANDING GEAR RT SIDE WALL SHOWS CRACK BETWEEN RIVETS. CUT OUT DAMAGE SECTION AS PER B727 SRM 51-40-2. ACCOMPLISHED NDT AROUND CUT OUT AREAS, NO CRACK AS PER 727 NDT PART 6 53-00-00. INSTALLED REPAIR DOUBLER AS PER B727 SRAug 28, 2001 · N949UP · Boeing 72725C · Fuselage Main, BulkheadSDR UPS01236970Doubler · corrodedINSPECTION TYPE:C CORROSION AFT CARGO DOOR CUT OUT INNER DOUBLER STRAP BETWEEN BS1030 AND BS1130 AND BETWEEN STR 17R AND 20R. REMOVED INNER DOUBLER STRAP BETWEEN BS1030 AND BS1130 STR17 AND STR 20 IAW SRM B727-51-30-02. FABRICATED INNER DOUBLER STRAP IAW Aug 27, 2001 · N949UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS01236939Doubler · corrodedINSPECTION TYPE:C AFT CARGO CUT OUT UPER SILL INTERNAL DOUBLER, HAS CORROSION FROM BS 1080. REMOVED CORROSION, FOUNF OUT OF LIMITS AT STA 1040-1080 AS PER B727- SRM 51-10-6 CUT OUT DAMAGE AREA AS PER 53-10-01 UPPER SILL INTERNAL DOUBLER BS 1080 AS PER TELEAug 24, 2001 · N949UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS01236940Skin · corrodedINSPECTION TYPE:C FUSELAGE SKIN BULGING AROUND FASTENERS ABOVE UPPER AFT CORNER OF AFT CARGO DOOR BS 1080 TO BS 1130 STR 17R TO STR 20R. REMOVED AND REPLACED FUSELAGE SKIN FROM BS 1080 TO BS 1185 FORM STR 17R TO STR 20R AS PER BOEING DRAWING # 6518385 ANDAug 21, 2001 · N949UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS01236612Web · crackedINSPECTION TYPE:C NLG WHEEL WELL R/H SIDEWALL AREA HSA CRACK APPROX BS 240 BELOW ACCESS PANEL 3122. REMOVED FASTENERS AT R/H SIDE BS 240 CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-02. PERFORMANCE NDT INSP AS PER B727 NDT 51-00-00 FIG 4. FOUND NO CRACK. INAug 2, 2001 · N947UP · Boeing 72725C · Fuselage Main, StructureSDR UPS01236611Web · crackedINSPECTION TYPE:C NLG WHEEL WELL L/H SIDE WEB AREA HAS CRACK APPROX BS 250 BELOW ACCESS PANEL 3122 REMOVED FASTENERS ON NLG WHEEL WELL L/H SIDE WEB AREA APPROX BS250 BELOW ACCESS PANEL 3122 AS PER B727 SRM 51-30-2. CUT OUT DAMAGE AREA AS PER B727 SRM 51-4Aug 2, 2001 · N947UP · Boeing 72725C · Fuselage Main, StructureSDR UPS01236610Web · crackedINSPECTION TYPE:C NLG WHEEL EWLL. L/H SIDE WALL AREA HAS CRACK APPROX. BS244 BELOW ACCESS PANEL 3122. REMOVED FASTENERS ON NLG L/H WHEEL WELL L/H SIDE WEB AREA APPROX BS 244 BELOW ACCESS PANEL 3122 AS PER SRM 51-30-02. CUT OUT DAMAGE AREA AS PER B727 SRMAug 2, 2001 · N947UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS01236613Web · crackedINSPECTION TYPE:C MAIN CABIN LEFT AFT LAV, BS 1180 OUTBOARD FLOOR WEB CRACK. REMOVED AND REPLACED FLOOR WEB (DITCHING PANEL) AT BS 1180 LBL 55 REF B727 SRM 51-10-01 AND 51-30-02 MATERIAL USED 2024 T3/.020" ALUMINUM.Jul 31, 2001 · N947UP · Boeing 72725C · Fuselage Main, StructureSDR 01FDEA00607Switch · inoperativeDUR TEST FLT AT 12000 CLIMB MC DOOR LIGHT CAME ON. ADJUSTED MC DOOR WARN MICROSWITCHES, AND OPS CK GOOD PER IAW FEDEX MM 52-70-000-5.Jul 26, 2001 · N116FE · Boeing 72725C · Door Warning SystemSDR 01FDEA00578Fitting · crackedDURING ROUTINE INSP FOUND SUPPORT FITTING FOR NR 6 LEADING EDGE SLAT UP STOP CRACKED. *S/D* REMOVED AND REPLACED FITTINGS PER IAW SRM 51-20-1.Jul 18, 2001 · N116FE · Boeing 72725C · Wing Miscellaneous StructureSDR 01FDEA00576Fitting · corrodedDURING ROUTINE INSP FOUND SUPPORT FITTING FOR NLG DOOR ACTUATOR ROD CORRODED. *S/D* REMOVED AND REPLACED FITTING PER IAW SRM 51-30-2.Jul 18, 2001 · N116FE · Boeing 72725C · Landing Gear Door ActuatorSDR 01FDEA00577Fitting · crackedDURING ROUTINE INSP FOUND SUPPORT FITTING NR 2 KRUEGER FLAP ACTUATOR SUPPORT FITTING AT FRONT SPAR CRACKED. *S/D* REMOVED AND REPLACED PER IAW SRM 57-20-1.Jul 18, 2001 · N116FE · Boeing 72725C · Leading Edge Slat ActuatorSDR UPS01236254Computer · faultyINSPECTION TYPE:N/A, WHEN THROTTLES RETARDED AT 4000 FT ON APPROACH, WHEEL WELL FIRE LIGHT CAME ON. WENT OUT AS SOON AS GEAR DOWN. INSPECTED WHEEL WELL FIRE LOOP, FOUND AREA OF CONTACT ON AIRFRAME REPOSITION FIRE LOOP. CHANGED FIRE AND OVERHEAT COMPUTER AS Jul 9, 2001 · N951UP · Boeing 72725C · Fire DetectionSDR 01FDEA00524Skin · crackedDURING INSP HFEC IND CRACK FUSELAGE SKIN RT AT BS 252 BELOW CO-PILOTS NR 3 WINDOW. *S/D* REMOVED AND REPLACED PER IAW EA 7-5330-57300.Jul 6, 2001 · N116FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS01236098Fire Loop · contaminatedINSPECTION TYPE:N/A WHEEL WELL FIRE LIGHT AND BELL CAME ON ON APPROACH AT APPROX 3000 FT MSL WHEN GEAR EXTENDED, LIGHT EXTINGUISHED. NO APPARENT DAMAGE OR PROBLEMS ON LANDING. INSPECTED ALL WHEEL WELL FIRE LOOPS FOR GROUNDS. FOUND CONTAMINATION IN THE NOSE Jun 14, 2001 · N931UP · Boeing 72725C · Fire DetectionSDR UPS01236032Warning Light · false indicationINSPECTION TYPE:N/A WHEEL WELL FIRE LIGHT ILLUMINATED AFTER TAKEOFF. LIGHT WENT OUT AFTER GEAR EXTENTSION. A/C FLOWN TO SDF WITH LANDING GEAR DOWN AT 250 KTS. 2ND PAGE/ REF ITEM 1 PREVIOUS LOG PAGE WHEEL WELL FIRE WARN LIGHT ON AFTER GEAR RETRACTION. NO DEJun 11, 2001 · N951UP · Boeing 72725C · Fire DetectionSDR 01FDEA00396Link · vibrationUPON LANDING WITH SPOILER and REVERSERS ABOUT 90 KTS. NOSE GEAR START VIBRATING. *S/d* Removed and replaced NLG TORSION LINKS PER IAW MM 32-21-051-4, LT & RT NLG WHEELS PER IAW MM 32-45-011-4. OPS CHECK GOOD.Jun 6, 2001 · N116FE · Boeing 72725C · Landing Gear Retraction/Extension SystemSDR UPS01236105Stringer · corrodedINSPECTION TYPE:C STRINGER TERMINAL FITTING CORRODED AT BS 1183 STR 18L REMOVED CORRODED STRINGER BS 1183, STR18L. PER SRM 51-30-2, FABRICATED STRINGER TERMINAL FITTING PER BOEING DRAWING 65-242276 AND B727 SRM 51-10-2 TREATED AND PRIMED. INSTALLED STRINGEMay 31, 2001 · N950UP · Boeing 72725C · Fuselage Main, StructureSDR UPS01236102Skin · crackedINSPECTION TYPE:C NOSE WHEEL WELL R/H SIDE WALL SHOW CRACK AT BS 294 WL165 CRACK ABOUT 10" LONG LOOKING GROM INSIDE REMOVED VERTICAL ANGLE FOR ACCESS REPAIR PER B727 SRM 51-30-2 CUT OUT DAMAGE AREA PER B727 SRM 51-40-2 APP.4 SIDE CUT OUT 6"X1" PERFORMED May 29, 2001 · N950UP · Boeing 72725C · Fuselage Structure (General)SDR 01FDEA00391Stringer · crackedAT BS 400 STR 1, 2R & 3L ARE CRACKED AT FASTENER COMMON TO STR AND FRAME. REMOVED AND REPLACED STRINGERS PER IAW FEDEX EA 7-5310-57956.May 29, 2001 · N118FE · Boeing 72725C · Fuselage Main, Longeron/StringerSDR UPS01236104Keelbeam · crackedINSPECTION TYPE:C KEEL BEAM BS 900 APPROX APU COMPARTMENT ACCESS PANEL SHOWS A HOLE AND CRACKED AREA. CUT DAMAGED AREA AT KEEL BEAM ACCESS PANEL BS 900 APU COMPARTMENT AS PER B727 SRM 51-10-1, INSTALLED DOUBLER ON KEEL BEAM ACCESS PANEL AS PER B727 SRM 51-40-May 27, 2001 · N950UP · Boeing 72725C · Fuselage Main, KeelSDR UPS01236103Spar · crackedINSPECTION TYPE:C, LEFT WING REAR SPAR UPPER CHORD AT WING STATION APPROX CRACK INDICATION IS ABOUT 2 INCHES LONG OUTBOARD OF NR 1 FUEL SOV. REMOVE CRACK AT REAR SPAR UPPER CHORD AT WS 190 AND INSTALL FILLER AND DOUBLER REPAIR AS PER BOEING DRAWING 65C196447,May 27, 2001 · N950UP · Boeing 72725C · Wing SparSDR UPS01236100Bulkhead · crackedINSPECTION TYPE:C CRACKS AT BULKHEAD STA 294.5 RBL 12, NOSE LANDING GEAR WHEEL WELL, INSPECTED. INSPECTED NLG WHEEL WELL BULKHEAD AND VERIFY CRACK AS PER B727 NAT MANUAL PART 6 51-00-00 FIG 4. REMOVED VERTICAL ANGLE TO ACCESS REPAIR AND CUT OUT CRACK AREAMay 27, 2001 · N950UP · Boeing 72725C · Fuselage Main, StructureSDR UPS01236101Skin · corrodedINSPECTION TYPE:C, INDICATION OF MATERIAL LOSS GREATER THAN 10 8/0 IN THE SKIN AT CIRCUMFERENTIAL JOINT BS 441 BETWEEN S 17R AND S 20R FORWARD PANEL. CUT DAMAGED AREA ON STA 441 BETWEEN STA 17R AND STA 20R PER DRAWING 69-62161. INSTALLED DOUBLER REPAIR IN CMay 26, 2001 · N950UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS01235893Door Seal · tornINSPECTION TYPE:N/A PILOT REPORT-AT 5000 FT LOST CABIN PRESSURIZATION REPAIRED MAIN ENTRY DOOR SEALMay 15, 2001 · N931UP · Boeing 72725C · Passenger/Crew DoorsSDR UPS01235831Attach Angle · crackedINSPECTION TYPE:N/A WING TO BODY ATTACH ANGLE CRACKED REMOVED L BRACKET 6196. REMOVED SLIDING FAIRING STRICKER BRACKET TO FOM 61964 FABRICATED AND REINSTALLED BRACKET PER 51-1-0 OF SRMMay 8, 2001 · N949UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS01235981Beam · crackedINSPECTION TYPE:N/A VERTICAL BEAM AT BS 1183 CRACKED LBL 26.83 WL 260 APPROX 2 INCH LONG FROM LIGHTENING HOLE. REPAIRED CRACK BY STOP DRILLING. HFEC AREA INSTALLED REPAIR PER B727.Apr 29, 2001 · N948UP · Boeing 72725C · Fuselage Main, StructureSDR UPS01235838Pressure Panel · crackedINSPECTION TYPE:C NLG WHEEL WELL LT SIDEWALL SHOW CRACK RUNNING BETWEEN FASTENERS AT 243.7 TO LOWER CHORD. REMOVED LT SIDE WALL AND FASTENERS AT BS 243.7 IAW SRM 51-30-2. CUT OUT CRACK SECTION PER SRM 51-40-2 FIG 1. APPROX SIZE 7 X 1 INCH, INSTALLED DOUBLERApr 29, 2001 · N948UP · Boeing 72725C · Fuselage Main, StructureSDR UPS01235837Pressure Panel · crackedINSPECTION TYPE:C NLG WHEEL WELL LT SIDEWALL SHOW CRACK RUNNING BETWEEN FASTENERS AT BS 277.5 TO LOWER CHORD. REMOVED NOSE WHEEL WELL ACCESS PANEL LT AFT TO GAIN ACCESS AND REMOVED FASTENERS LT SIDE AT 277.5 S PER B727 SRM 51-30-2. CUT OUT CRACK SECTION AS PApr 29, 2001 · N948UP · Boeing 72725C · Fuselage Main, StructureSDR UPS01235982Drag Brace · crackedINSPECTION TYPE:N/A DRAG BRACE SUPPORT BEAM IS CRACKED AT LT AFT CORNER CONFIRMED BY HFEC. STOP DRILLED CRACK PER SRM HFEC INSPECTED AREA FOUND NO CRACKS BEYOND AREA. FOUND CRACK TO BE BEYOND REPAIRABLE LIMITS PER UPS EO B727 -5310-0943. REMOVED AND REPLACEApr 28, 2001 · N948UP · Boeing 72725C · Landing Gear Retraction/Extension SystemSDR UPS01235980Bulkhead · crackedINSPECTION TYPE:C PRESSURE BULKHEAD CRACKED RBL 18 AT HAND PUMP LOWER OUTBOARD MOUNT BRACKET. CUT OUT CRACKED AREA AT BS 1183 RBL 18 AS PER SRM 51-10-1. NDI NO CRACK FOUND, INSTALLED DOUBLER PER B727 SRM 53-10-9.Apr 28, 2001 · N948UP · Boeing 72725C · Fuselage Main, BulkheadSDR CA010508011Skin · delaminated(CAN) DURING ROUTING C CHECK INSPECTION , FOUND EVIDENCE OF DELAMINATION AT UPPER CHORD, 8 INCHES LONG, 6 1/2 INCHES FORWARD OF AFT MOUNT FITTING. WINGLET REMOVED AND RETURNED TO WINGLET SYSTEM FOR EVALUATION AND POSSIBLE RECTIFICATION. WINGLET SYSTEMS PROVIDEApr 20, 2001 · Boeing 72725C · Wing, Plate/SkinSDR UPS01235587Door · will not testINSPECTION TYPE:N/A FWD FLIGHT ATTENDANT O2 DOOR WOULD NOT DEPLOY. PERFORMED E.O.727-3520-14476-A OPS CK FWD FLT ATTENDANTS O2 MASK DOOR DROP CK. OPS CKS GOODApr 13, 2001 · N947UP · Boeing 72725C · Crew Oxygen SystemSDR 01FDEA00274Fitting · corrodedDURING ROUTINE INSP STRINGER 18L END FITTING AT BS 1183 FOUND CORRODED. *S/D* REMOVED AND REPLACED STR T-FITTING PER IAW BAC 727 SRM 51-30-2.Apr 12, 2001 · N124FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 01FDEA00275Fitting · corrodedDURING ROUTINE INSP, STR 18R END FITTING AT BS 1183 FOUND CORRODED. *S/D* REMOVED AND REPLACED STR T-FITTING PER IAW BAC 727 SRM 51-30-2.Apr 12, 2001 · N124FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 01FDEA00272Fitting · crackedDURING ROUTINE INSP, RT MAIN GEAR DOOR TO WING FAIRING ROLLER FITTING FOUND CRACKED. ** S/D ** R&R FITTING PER IAW BAC 727 SRM 51-30-2.Apr 12, 2001 · N124FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 01FDEA00258Skin · crackedDURING ROUTINE INSP, RT WING UPPER SKIN LEAD EDGE FOUND CRACKED AT WS 46, 8 INCHES FWD OF THE FWD WING SPAR.** S/D ** FAB & REPAIR PER IAW BAC 727 SRM 57-30-4 & SRM 51-30-2.Apr 6, 2001 · N124FE · Boeing 72725C · Wing, Plate/SkinSDR 01FDEA00266Spar · corrodedDURING ROUTINE INSP, FWD FACE OF THE BS 870 BULKHEAD BL 0 UP 9 INCHES FROM OPEN FOR HOT AIR DUCT IN KEELBEAM FOUND CORRODED. *S/D* REPAIRED REAR SPAR WEB PER IAW FEDEX EA 7-5710-57223.Apr 6, 2001 · N124FE · Boeing 72725C · Wing SparSDR 01FDEA00265Seat Track · corrodedDURING ROUTINE INSP, NR 2 SEAT TRACK FOUND CORRODED BS 610. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5.Apr 6, 2001 · N124FE · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR 01FDEA00264Seat Track · corrodedDURING ROUTINE INSP, NR 3 SEAT TRACK FOUND CORRODED FROM BS 640-740. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5.Apr 6, 2001 · N124FE · Boeing 72725C · Fuselage, Seat/Cargo Attach FittingsSDR 01FDEA00263Plate · crackedDURING ROUTINE INSP, RT ELEVATOR REAR SPAR NR 4 SHEAR PLATE FOUND CRACKED. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-2, 51-30-2.Apr 6, 2001 · N124FE · Boeing 72725C · Elevator StructureSDR UPS01235763Skin · crackedINSPECTION TYPE: C, FUSELAGE NOSE SECTION RT SIDE BS 203.8 WL 219.5 STR.15R SKIN CRACKED AROUND FASTENERS (2EA) NDT INSP. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR AT R/H SIDE BS 203.8 WL 219.5 STR.15R AS PER B727 SRM 53-30-3 FIG.3 MATERIAL USED 2024Apr 4, 2001 · N951UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS01235762Skin · crackedINSPECTION TYPE:C FUSELAGE NOSE SECTION LT SIDE BS 235.8 WL 220 STR 15L SKIN CRACKED AROUND FASTENER. NDT INSP. CUT-OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR AT LT SIDE BS 235.8 WL 220 STR 15L AS PER B727 SRM 53-30-3 FIG.3 MATERIAL USED 2024-T3 .063 9.5 XApr 4, 2001 · N951UP · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS01235761Structure · crackedINSPECTION TYPE:C AFT AIRSTAIRS HAS 5 INCH CRACK. REPAIRED BY E.O. B72752102687, NEEDS PERMANENT REPAIR. CUT-OUT CRACKED AREA OF SKIN 1.25 X 4 AND INSTALL FLUSH DOUBLER REPAIR 3 X 7 TO LT TOP CORNER I/A/W B727 SRM 52-10-2 FIG.4 REMOVED AND REPLACED O/B VERTIApr 4, 2001 · N951UP · Boeing 72725C · Entrance StairsSDR UPS01235481Smoke Detector · inoperativeMAIN CABIN SMOKE DETECTOR FAILED TO TEST. RELAMPED AND DISPATCHED AIRCRAFTApr 1, 2001 · N946UP · Boeing 72725C · Smoke DetectionSDR 01FDEA00247Skin · crackedDURING INSP FUSELAGE SKIN AT BS 249, WL 245 WAS FOUND CRACKED AT FASTENER HOLE BENEATH THE PILOTS NR 3 WINDOW. *S/D* REPAIRED SKIN PER IAW FEDEX EA 7-5330-57216.Mar 31, 2001 · N124FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR 01FDEA00244Spar · corrodedDURING ROUTINE INSP, THE AFT FACE OF THE CENTER WING TANK FOUND CORRODED 9 INCHES UP FROM BOTTOM OF THE TANK AT RBL 9. *S/D* REPAIRED REAR SPAR PER IAW FEDEX EA 7-5710-57223.Mar 31, 2001 · N124FE · Boeing 72725C · Wing SparSDR 01FDEA00246Spar · corrodedDURING ROUTINE INSP, THE CTR FUEL TANK AFT WEB FOUND CORRODED ON THE AFT FACE FROM LBL 15 TO LBL 18, 6-8 IN UP FROM BOTTOM OF TANK. *S/D* REPAIRED REAR SPAR WEB PER IAW FEDEX EA 7-5710-57223.Mar 31, 2001 · N124FE · Boeing 72725C · Wing SparSDR 01FDEA00245Stiffener · corrodedDURING ROUTINE INSP THE VERTICAL STIFFENER AT LBL 14 ON THE AFT SIDE OF THE CTR WING TANK FOUND CORRODED 2 IN FROM TOP OF THE STIFFENER.Mar 31, 2001 · N124FE · Boeing 72725C · Wing, Center BoxSDR UPS01235463Windshield · failedFIRST OFFICERS WINDSHIELD SHATTERED. OLD WINDOW REMOVED NEW WINDOW PARTIALLY INSTALLED / R&R R1 WINDOW PER M/M 56-11-1 WINDOW HEAT OPS CHECK GOODMar 28, 2001 · N933UP · Boeing 72725C · Flight Compartment Windows
Back to Boeing 727-25C