Boeing 727-27C

Service difficulty reports · 1,078

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 = '72727C'
  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 UPS96205742Carriage · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON NR 1 CARRIAGE INSIDE SPINDAL BOLT. REMOVED AND REPLACED NR 1 FLAP CARRIAGE ON NRC 438048.Mar 16, 1996 · N907UP · Boeing 72727C · Trailing Edge FlapsSDR UPS96205741Carriage · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON NR 8 CARRIAGE INSIDE SPINDAL BOLT. REMOVED AND REPLACED NR 8 FLAP CARRIAGE ON NRC 437965.Mar 16, 1996 · N907UP · Boeing 72727C · Trailing Edge FlapsSDR UPS96205740Bonding Jumper · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED NR 2 K-FLAP OUTBOARD BULLNOSE BONDING JUMPER UPPER HAS PITTING ON OUTBOARD SIDE OF RIB. REMOVED DAMAGED AREA FAB REPAIR PARTS AND INSTALLED IAW SRM 57-50-3.Mar 16, 1996 · N907UP · Boeing 72727C · Leading Edge DevicesSDR UPS96205739Tab Assy · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED LT WING, INBOARD AILERON TAB SIDE HINGE FITTINGS ARE CORRODED. REPLACED TAB ASSY.Mar 16, 1996 · N907UP · Boeing 72727C · Aileron TabsSDR UPS96205734Frame · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON FRAME AT STA 312, RBL 43, WL 170. REMOVED DAMAGED SECTION OF FRAME AND FAB REPAIR PARTS AND INSTALLED. ALL WORK IAW SRM 51-10-2, 51-40-2, 53-10-1, 51-10-6, 51-30-2, AND MM 51-20-151.Mar 16, 1996 · N907UP · Boeing 72727C · Fuselage Main, FrameSDR UPS96205732Intercostal · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON INTERCOSTAL AT BS 215, RBL 26, WL 176. REMOVED CORROSION AT BS 215, RBL 26, WL 176 PER SRM 51-20-4, 53-10-1, AND 51-30-5.Mar 16, 1996 · N907UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS96205743Clip · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STRINGER CLIP BS 734, STR 6 RT. REMOVED AND REPLACED STR TIE PER SRM 51-30-2, AND MM 53-11-00.Mar 15, 1996 · N907UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS96205738Fitting · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED LT WING, INBOARD AILERON CENTER HINGE FITTING IS CORRODED, AILERON SIDE. REPLACED FITTING IAW SRM 51-30-2, AND OHM 57-50-1.Mar 15, 1996 · N907UP · Boeing 72727C · AileronsSDR UPS96205737Fitting · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED LT WING, INBOARD AILERON CENTER HINGE FITTING IS CORRODED, WING SIDE. REPLACED FITTING IAW MM 27-10-1.Mar 15, 1996 · N907UP · Boeing 72727C · Wing, Control Surface Attach FittingsSDR UPS96205736Intercostal · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON INTERCOSTAL STA 740-760, RBL 65, WL 208, AROUND FASTENER HOLES. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-30-2.Mar 15, 1996 · N907UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS96205733Fork Assy · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED FORK ASSY CORRODED BEYOND REPAIR. REMOVED AND REPLACED FORK ASSY IAW OHM 20-50-01 AND SRM 51-20-4.Mar 15, 1996 · N907UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS96205731Web · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CRACK ON NLG W/W WEB AT BS 292, RBL 23, WL 191. REMOVED AND REPLACED WEB IAW UPS SRM 51-40-02, 51-10-2, 51-30-2, AND 51-20-4.Mar 15, 1996 · N907UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS96206024Angle · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT SKIN SUPPORT ANGLE IS CRACKED AT FS 1345 AND FIN STA 22.5. REMOVED DAMAGED SECTION IAW SRM 51-40-3, FAB AND INSTALLED REPAIR IAW SRM 51-40-3.Mar 14, 1996 · N948UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS96205715Sill · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON MOP SILL AT STA 304-309, RBL 58, WL 208. REMOVED CORROSION IAW 53-10-1. CORROSION EXTENDED TO STA 335, STA 320, AND STA 334 OUT OF LIMITS. REPAIRED MOP SILL PER SRM 51-40-3 AT STA 320, 334.Mar 14, 1996 · N907UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS96205716Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STR 9R FROM BS 680 - BS 700. REPAIRED STRINGER IAW 53-10-1 AND 53-10-3.Mar 12, 1996 · N907UP · Boeing 72727C · Fuselage Main, Longeron/StringerSDR UPS96205714Tie · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON STR 22R AT BS 363 TO BS 380 RBL 50, WL 165. REMOVED CORROSION IAW SRM 53-10-1. REPLACED STRINGER FRAME TIE IAW 51-30-2.Mar 12, 1996 · N907UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS96205691Frame · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION ON LOWER END OF FRAME AT BS 212 LBL 16 WL 168. REMOVED CORROSION, FABRICATED NEW WEB AND INSTALLED PER SRM 51-30-2.Mar 11, 1996 · N907UP · Boeing 72727C · Fuselage Main, FrameSDR CA960315011Engine · failure(CAN) BOROSCOPE EXAMINATION OF ENGINE WAS INCONCLUSIVE BUT APPARENT DAMAGE SUGGESTS A COMBUSTION CAN FAILURE OF SOME DESCRIPTION MAY HAVE INDUCED THE NOZZLE AND T1 DAMAGE OR THE POSSIBILITY OF T1 BLADE FAILURE AS THE SECOND OPTION. AN ENGINE CORE STRIP REPORT Mar 11, 1996 · Boeing 72727C · Engine (Turbine/Turboprop)SDR UPS96205695Skin · delaminatedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED RT WING O/B AILERON TAB I/B AND SKIN IS DELAMINATED UPPER SURFACE. REPAIRED RIGHT WING OUTBOARD AILERON TAB IAW SRM 51-40-6 AND 51-80-6.Mar 10, 1996 · N907UP · Boeing 72727C · Aileron TabsSDR UPS96205692Stringer · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED STR AT STA 993 CRACKED. STOP DRILLED AND SPLICED IN REPAIR IAW MM 51-20-31 SRM 53-10-3, 51-30-2, AND 51-20-4.Mar 10, 1996 · N907UP · Boeing 72727C · Fuselage Main, Longeron/StringerSDR UPS96205693Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED NR 6 SLAT HAS CRACK ON FIRST RIB I/B FROM O/B END. REMOVED AND REPLACED RIB IAW SRM 57-50-3.Mar 9, 1996 · N907UP · Boeing 72727C · Leading Edge DevicesSDR UPS96206023Channel · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1342 RT CHANNEL WL 247 RBL 18 IS CORRODED AFT SIDE OF 1342 FRAME. REMOVED AND REPLACED CHANNEL IAW BAC DWG 65-93155 B727-5530-4601 AND SRM 51-30-2.Mar 8, 1996 · N948UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS96206022Channel · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1342 LT CHANNEL WL 247 LBL 18 IS CORRODED AFT SIDE OF 1342 FRAME. REMOVED AND REPLACED CHANNEL IAW BAC DWG 65-93155 B727-5530-4601 AND SRM 51-30-2.Mar 8, 1996 · N948UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS96206021Frame · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT FRAME CHORD AT STA 1342 RBL 20 WL 238 IS CORRODED. REPLACED LT I/B CHORD PER SRM 51-10-1.Mar 8, 1996 · N948UP · Boeing 72727C · Fuselage Main, FrameSDR UPS96206020Frame · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT FRAME CHORD AT STA 1342 RBL 20 WL 238 IS CORRODED. REPLACED RT I/B CHORD PER SRM 51-10-1.Mar 8, 1996 · N948UP · Boeing 72727C · Fuselage Main, FrameSDR UPS96205843Floor Support · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING CORROSION ON FLOOR SUPPORT STA 328-344, RBL 41, WL 208 OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-1, 51-30-2.Mar 5, 1996 · N907UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS96205694Bushing · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION LEFT FRONT BOTTLE PIN BUSHING, ON FWD FACE. REMOVED AND REPLACED BUSHING IAW MM 57-41-11 AND 57-10-7.Mar 5, 1996 · N907UP · Boeing 72727C · Wing, Fuselage Attach FittingsSDR UPS96205834Beam · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED FORWARD CARGO DOOR NR 5 TRANSVERSE BEAM CRACKED IN OUTBOARD RADIUS AT NR 1 AND NR 2 SKIN VERTICAL STIFFENERS. REMOVED INNER SKIN, REMOVED NR 5 TRANSVERSE BEAM, FABRICATED NEW TRANSVERSE BEAM, AND INSTALLED IN DOOR. Mar 3, 1996 · N907UP · Boeing 72727C · Cargo/Baggage DoorsSDR CA960311023Engine · vibration(CAN) ON TAKEOFF, THE CREW CARRIED OUT A PRECAUTIONARY ENGINE SHUT DOWN DUE TO VIBRATION.Mar 2, 1996 · Boeing 72727C · Engine (Turbine/Turboprop)SDR UPS96205797Transverse Beam · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED FWD CARGO DOOR TRANSVERSE BEAM AND O/B L-ANGLE ARE CRACKED IN O/B RADIUS AT OUTER SKIN VERT STIFFENERS. REMOVED AND REPLACED TRANVERSE BEAM IAW SRM 51-10-1, 51-10-2, 51-30-5, 51-30-2, 51-20-4 AND MM 51-20-151.Feb 23, 1996 · N907UP · Boeing 72727C · Cargo/Baggage DoorsSDR UPS96205796Gate · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION AND CRACKING MID GALLEY DOOR UPPER GATE UPPER EDGE. REMOVED AND REPLACED UPPER GATE IAW UPS OHM 52-46-01.Feb 23, 1996 · N907UP · Boeing 72727C · Galley DoorsSDR UPS96205795Gate · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED CORROSION AND CRACKING MID GALLEY DOOR LOWER GATE LOWER FWD CORNER. REMOVED AND REPLACED LOWER GATE IAW UPS OHM 52-46-01.Feb 23, 1996 · N907UP · Boeing 72727C · Galley DoorsSDR UPS205349Light · inoperativeMAINTENANCE REPORTED, FWD COCKPIT EMERGENCY EXIT LIGHT INOP. RESET EMERGENCY EXIT LIGHT, BATT RECHARGED AND OPS CHECK OF LIGHT GOOD, NO DEFECTS SEEN.Jan 31, 1996 · N914UP · Boeing 72727C · Emergency LightingSDR UPS205348Battery · dischargedMAINTENANCE REPORTED, EMERGENCY EXIT LIGHT ASSY AT MAIN ENTRY AND CABIN ENTRANCE WEAK AND WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD.Jan 30, 1996 · N910UP · Boeing 72727C · Emergency LightingSDR UPS97221812Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT INOP AT CREW ENTRY DOOR AND EMERGENCY LIGHT INOP AT COCKPIT DOOR. REMOVED AND REPLACED BATTERY PACKS.Jan 14, 1996 · N908UP · Boeing 72727C · Emergency LightingSDR 95FDEA01912Actuator · malfunctionedWHEN RETRACTING FLAPS TO A 2 DEGREE POSITION AFTER TAKEOFF, NR 5 LED REMAINED EXTENDED, FLAPS POSITIONED TO 5 DEGREES NORMAL LED EXTENSION, FLAPS TO 2 DEGREE POSITION REMAINED EXTENDED. REMOVED AND REPLACED NR 5 L/E FLAP ACTUATOR. OPS AND LEAK CHECKS NORMAL Dec 21, 1995 · N145FE · Boeing 72727C · Leading Edge Slat ActuatorSDR UPS205165Battery · dischargedMAINTENANCE REPORTED, CREW ENTRY DOOR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED CREW ENTRY EMERGENCY EXIT LIGHT BATTERIES AND LIGHT OPERATES NORMALLY.Dec 16, 1995 · N907UP · Boeing 72727C · Emergency LightingSDR UPS205127Door Frame · crackedWHILE ON GROUND, MAINTENANCE FOUND FWD CARGO DOOR FUSELAGE FRAME, FWD SIDE, 4TH STOP UP, DOUBLER CRACKED BEYOND STOP DRILL LIMITS.Dec 2, 1995 · N908UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS205102Retract Mech · lack of lubeSDF - ON APPROACH, NOSE GEAR DID NOT ILLUMINATE DOWN AND LOCKED. RECYCLED GEAR AND NOSE GEAR DID INDICATE DOWN AND LOCKED ON SECOND ATTEMPT. HANDLE HARDER TO MOVE THAN NORMAL. CHECKED OVER CENTER LINK AND LIBED LINKAGES, OPERATED GEAR SEVERAL TIMES AND CHECNov 17, 1995 · N909UP · Boeing 72727C · Landing Gear Retraction/Extension SystemSDR UPS205101Retract Mech · lack of lubeSDF - CREW REPORTED ON APPROACH, NOSE GEAR DID NOT ILLUMINATE DOWN AND LOCKED. RECYCLED GEAR AND NOSE GEAR DID INDICATE DOWN AND LOCKED ON SECOND ATTEMPT. MAINTENANCE CHECKED OVER CENTER LINK AND LUBED LINKAGES, OPERATED GEAR SEVERAL TIMES AND CHECKED TIME PNov 17, 1995 · N909UP · Boeing 72727C · Landing Gear Retraction/Extension SystemSDR UPS205011Connector · shortedCREW REPORTED ON TAKEOFF, WHEN LDG GEAR WAS RETRACTED, RED WARNING LIGHTS ILLUMINATED. RECYCLED AND DOOR WARNING LIGHT WORKED NORMAL. AMBER F/E LIGHTS OPS NORMAL. RED WARNING LIGHTS REMAINED ILLUMINATED UNTIL LANDING, WHEN GEAR WAS SELECTED DOWN, THEN THEY Nov 11, 1995 · N908UP · Boeing 72727C · Landing Gear Position and WarningSDR UPS204818Skin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL UPPER SKIN BS 775 TO 785 RBL 64. CUT OUT CORRODED SECTION OF FUEL CELL SKIN AND REPAIRED PER EO B727-5730-7507-A.Oct 17, 1995 · N909UP · Boeing 72727C · Wing, Plate/SkinSDR UPS204817Skin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL UPPER SKIN BS 770 TO 800, LBL 64. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 57-30-1. CUT OUT CORRODED SKIN AND REPAIRED PER EO B727-5730-7506-A.Oct 17, 1995 · N909UP · Boeing 72727C · Wing, Plate/SkinSDR UPS204816Skin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND UPON REMOVAL OF RBL 45 LONGITUDINAL BEAM, FUEL CELL UPPER SKIN TO BE CORRODED AT BS 865 TO 870, RBL 45 WL 178. BLENDED OUT CORROSION AND REPAIRED DOUBLER PER EO B727-5730-7514-A.Oct 17, 1995 · N909UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS204815Frame · corrodedWHILE IN FOR C-CHECK, MAINTENANCE FOUND DISCOVERED CORROSION ON BS 760 FRAME WEB FWD SIDE LBL 70 WL 203. REMOVED CORROSION AND REPAIRED AREA PER EO B727-53-1691.Oct 17, 1995 · N909UP · Boeing 72727C · Fuselage Main, FrameSDR UPS204814Stringer · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND DURING PRESSURE LEAK OF FUEL VENT FOUND FORWARD VENT STRINGER WEB CRACKED AT LBL 26, STA 760 1 INCH LONG. REPAIRED PER UPS EO 727-57-1658.Oct 17, 1995 · N909UP · Boeing 72727C · Fuselage Main, Longeron/StringerSDR UPS204813Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND HFEC INSPECTION REVEALED CRACK INDICATIONS AT FASTNERS BS 264 AND 265, STRINGER 9 RT ON EXTERIOR SKIN. ACCESS THE DAMAGED AREA, CUTOUT AREA OF SKIN AND FABRICATED REPAIR PARTS. INSTALLED REPAIR PART AND REINSTALLED ITOct 17, 1995 · N909UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS204812Doubled · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND MID GALLEY DOOR CUTOUT DOUBLER IS CRACKED AT BS 639.0 WL 274.25. STOP DRILLED CRACK, INSTALLED DOUBLER IAW EO B727-5330-2685.Oct 17, 1995 · N909UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS204811Skin · corrosionWHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER RUDDER SKIN ACCESS PANEL 9510. REMOVED CORROSION BY REMOVING BONDED SKIN, FABRICATED REPAIR PARTS AND FINAL INSTALLATION PER SRM 55-20-3.Oct 17, 1995 · N909UP · Boeing 72727C · Rudder, Plate/SkinSDR UPS204785Floor Beam · corrodedWHILE IN FOR D-CHECK, MAINTENANCE FOUND CENTER OF STA 344 FLOOR BEAM CORRODED AROUND FASTENER HOLES WHILE WORKING CARD 376276. REMOVED CORRODED PORTION OF FLOOR BEAM THAT WAS PREVIOUSLY REPLACED. FABRICATED REPLACEMENT BEAM PER SRM 53-10-2 AND 53-10-1. INSTOct 10, 1995 · N909UP · Boeing 72727C · Fuselage Main, Floor Beam
Back to Boeing 727-27C