Boeing 727-108C

Service difficulty reports · 255

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 = '727108C'
  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 UPS98227948Panel · corrodedINSPECTION TYPE:C CORROSION ON LT HORIZ STAB LE PANEL NR 9103 INBD END. CUT OUT DAMAGED AREA IAW SRM 55-10-3 (FIG 2). CARRIED OUT REPAIR IAW SRM 55-10-3 (FIG 2).Oct 6, 1998 · N936UP · Boeing 727108C · Horizontal Stabilizer, Plate/SkinSDR UPS98227946Support · crackedINSPECTION TYPE:C SUPPORT CHANNEL FOR NR 5 SPOILER PANEL INB DOWNSTOP CASTING CRACKED. NR 5 SPOILER CHANNEL REPLACED IAW SRM 51-30-02.Oct 6, 1998 · N936UP · Boeing 727108C · SpoilersSDR UPS98227952Skin · corrodedINSPECTION TYPE-C, CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 380 S20R. REPAIR CARRIED OUT IAW SRM 53-30-3.Oct 5, 1998 · N936UP · Boeing 727108C · Fuselage Main, Plate/SkinSDR UPS98227945Skin · corrodedINSPECTION TYPE:C SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 380 S20R. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 1.Oct 5, 1998 · N936UP · Boeing 727108C · Fuselage Main, Plate/SkinSDR UPS98227944Quadrant · crackedINSPECTION TYPE:C NR 1 SPOILER QUADRANT IS CRACKED AT CABLE GUARD. NR 11 SPOILER QUADRANT REPLACED IAW 27-61-81 MM.Jul 10, 1998 · N936UP · Boeing 727108C · Drag Control SystemSDR UPS97224873Control Cable · damagedINSPECTION TYPE-N/A, A/C ROLLS NOTICEABLY TO THE LEFT WHEN SPEED BRAKES EXTENDED 15-20 DEGREES AT 250 KTS. REPLACED SPOILER CABLE WSAZ AND RIGGED PER MM 27-61-31, OPS CKS GOOD.Nov 3, 1997 · N936UP · Boeing 727108C · Drag Control SystemSDR UPS97224896Light · inoperativeINSPECTION TYPE-N/A, REPEAT GRIP, UPON ROTATION EMER EXIT LIGHT FELL FROM SOCKET ABOVE MAIN CABIN ENTRANCE. REFER TO LOG PAGE 966096, ITEM NR 1 WILL NOT REMAIN SECURE IN SOCKET. LIGHT INOP UPON INSP. REPAIR FOR CYCLE IAW EO B727-3350-8620-A.Nov 1, 1997 · N936UP · Boeing 727108C · Emergency LightingSDR UPS97224867Light · not secureINSPECTION TYPE-N/A, UPON ENTERING EMERGENCY EXIT LIGHT ABOVE MAIN ENTRY DOOR FOUND LAYING ON FLOOR. EXIT LIGHT DOES NOT LATCH SECURELY IN BRACKET. REINSTALLED EMERGENCY EXIT LIGHT COVER, OPS CK NORMAL.Oct 31, 1997 · N936UP · Boeing 727108C · Emergency LightingSDR UPS97224718Air Distribution · odorINSPECTION TYPE-N/A, SMELLED ON CLIMBOUT A SMOKE SMELL FROM EYELET ON S/O PANEL RAN A/C SMOKE CHECKLIST AND WENT ON O2 MASKS DURING THE FLIGHT THE SMELL CAME AND WENT SEVERAL TIMES. OPERATED BOTH PACKS WITH NR 1 AND 3 ENGS AND WITH APU RAN GASPER FAN CK'D Oct 16, 1997 · N936UP · Boeing 727108C · Air Distribution SystemSDR UPS97222915Hinge · corrodedINSPECTION TYPE-C, AFTER FURTHER INVESTIGATION FOUND THE FWD AND AFT MAIN CARGO DOOR HINGES CORRODED ON CUSTOMER CARD ID NR 625571. REMOVED CORRODED HINGES, PROCURED NEW HINGES AND INSTALLED IAW SRM 51-10-1, SRM 51-30-2, MM 52-34-01 AND MM 51-20-151.May 6, 1997 · N936UP · Boeing 727108C · Cargo/Baggage DoorsSDR UPS97222809Skin · delaminatedINSPECTION TYPE-C, RIGHT WING INBOARD AFT FLAP TRAILING EDGE IS DELAMINATED 11.5 INCHES INBOARD FROM THE OUTBOARD END. REMOVED DAMAGED AREA, REPAIRED PER SRM 51-40-6.Apr 29, 1997 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS97222808Flap · delaminatedINSPECTION TYPE:C, RIGHT WING INBOARD AFT FLAP TRAILING EDGE IS DELAMINTATED 11.5 INCHES INBOARD FROM THE OUTBOARD END. REPAIRED IAW SRM 51-40-6.Apr 28, 1997 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS97222807Flap · delaminatedINSPECTION TYPE:C, R/W I/B AFT FLAP IS DISBONDED IN 2 PLACES AT THE 38 AND 86 FROM I/B END. REPAIRED AFT FLAP IAW SRM 51-40-6.Apr 28, 1997 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS97222810Stiffener · corrodedINSPECTION TYPE-C, CORROSION (C53-111-03-1B) ON STIFFENER BS 336 RBL 15 WL 181. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED STIFFENER IAW SRM 51-20-1, 51-30-5 AND MM 51-20-151.Apr 26, 1997 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS97222806Skin · gougeINSPECTION TYPE:C, UPPER RUDDER EXTERNAL SKIN PANEL AT LEFT RUDDER STA 242.137 TO 271.323 HAS DEEP GOUGE. REMOVED DAMAGED SKIN PANEL, DRILLED UP NEW PANEL COUNTERSUNK AND INSTALLED NEW SKIN PANEL IAW SRM 51-30-2.Apr 24, 1997 · N936UP · Boeing 727108C · Rudder, Plate/SkinSDR UPS97222805Lug · corrodedINSPECTION TYPE:C, NR 6 K-FLAP O/B ATTACH LUG IS CORRODED AT MOUNT BOLT HOLES ON O/B SIDE. REMOVED AND REPLACED NR 6 K-FLAP IAW MM 27-80-01.Apr 24, 1997 · N936UP · Boeing 727108C · Leading Edge DevicesSDR UPS97222671Upper Beam · corrodedINSPECTION TYPE:C, UPON REMOVAL OF MAIN CARGO DOOR, FOUND UPPER BEAM CORRODED. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED MAIN CARGO DOOR UPPER BEAM, FABRICATED NEW UPPER BEAM AND INSTALLED NEW BEAM PER SRM 51-10-1, 51-10-2, 51-30-2.Apr 20, 1997 · N936UP · Boeing 727108C · Cargo/Baggage DoorsSDR UPS97222670Spoiler · delaminatedINSPECTION TYPE:C, NR 1 SPOILER IS SEVERELY DELAMINATED. REMOVED AND REPLACED NR 1 SPOILER PER MM 27-61-01, 27-61-01 27-61-00.Apr 20, 1997 · N936UP · Boeing 727108C · SpoilersSDR UPS97222673Casting · corrodedINSPECTION TYPE:C, UPON REMOVAL OF MAIN CARGO DOOR, FOUND UPPER AFT PRESS SEAL CORNER CASTING CORRODED. CASTING WAS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORNER CASTING PER SRM 51-20-31, 51-30-2, 51-30-5, 51-10-1.Apr 18, 1997 · N936UP · Boeing 727108C · Cargo/Baggage DoorsSDR UPS97222672Casting · corrodedINSPECTION TYPE:C, UPON REMOVAL OF MAIN CARGO DOOR, FOUND FWD UPPER PRESSURE SEAL CORNER CASTING CORRODED. CASTING WAS CORRODED BEYOND LIMITS. REPLACED CASTING WITH NEW PART IAW SRM 51-10-1, 51-30-5, MM 51-20-31.Apr 18, 1997 · N936UP · Boeing 727108C · Cargo/Baggage DoorsSDR UPS97221885Light · inoperativeLEFT LIGHT BULB OF EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR INOPERABLE. (RELAMPED NO HELP). REMOVED AND REPLACED FORWARD ENTRY DOOR EXIT LIGHT ASSY. OPS CHECKS GOOD.Feb 1, 1997 · N936UP · Boeing 727108C · Emergency LightingSDR UPS96221749Batteries · dischargedINSPECTION TYPE-N/A, COCKPIT AND FOREWARD DOOR EMERGENCY EXIT LIGHTS INOP. INSTALLED NEW BATTERIES IN COCKPIT AND FOREWARD DOOR EMERGENCY EXIT LIGHTS, OPS CHECK GOOD.Dec 13, 1996 · N936UP · Boeing 727108C · Emergency LightingSDR UPS204789Spar · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON VERTICAL FIN REAR SPAR CHORD, RUDDER STA 223-STA 238 WHERE PANEL 9515 MATES LT SIDE. REMOVED AND INSTALLED FABRICATED PARTS. WORK DONE IAW E.O. B727-5530-7482A.Oct 10, 1995 · N936UP · Boeing 727108C · Vertical Stabilizer, Spar/RibSDR UPS204788Spar · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION BETWEEN LT HORIZONTAL STAB UPPER REAR SPAR CHORD AND SKIN AT STAB STA 215. REMOVED REAR SPAR CHORD, INSTALLED NEW SPAR CHORD AND FABRICATED RELATED PARTS, INSTALLATION PER SRM 51-30-02 SRM 51-21-31, 51-31-31, 55-10Oct 9, 1995 · N936UP · Boeing 727108C · Horizontal Stabilizer, Spar/RibSDR UPS204780Fitting · crackedWHILE ON GROUND, MAINTENANCE FOUND LOWER RUDDER CENTER RUDDER HINGE SUPPORT FITTING IS CRACKED AT RUD STA 178 LT SIDE 3RD FASTENER FROM TOP. REMOVED RUDDER, INSTALLED SERVICEABLE RUDDER IAW MM 27-20-01.Oct 9, 1995 · N936UP · Boeing 727108C · Rudder/Tab, Attach FittingsSDR UPS204779Fitting · crackedWHILE ON GROUND, MAINTENANCE FOUND UPPER RUDDER CENTER RUDDER HINGE SUPPORT FITTING IS CRACKED AT RUD STA 212 TO 208. REMOVED UPPER RUDDER, INSTALLED REPLACEMENT RUDDER IAW MM 27-20-01.Oct 9, 1995 · N936UP · Boeing 727108C · Rudder/Tab, Attach FittingsSDR UPS204778Skin · delaminatedWHILE ON GROUND, MAINTENANCE FOUND DAMAGE AROUND FASTENERS AT APPROX STAB STA 32.08 TO 44.00 ON LT HORIZONTAL STAB UPPER SURFACE. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW EO B727-5510-7485-A.Oct 9, 1995 · N936UP · Boeing 727108C · Horizontal Stabilizer, Plate/SkinSDR UPS204777Spar · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON RT SIDE VERT FIN UPPER FLANGE ON FRONT SPAR ENTIRE LENGTH STA 6.372 TO 180.6. CORROSION OUT OF LIMITS, REPAIRED RT SPAR CHORD IAW UPS EO B727-5530-7473-A.Oct 9, 1995 · N936UP · Boeing 727108C · Vertical Stabilizer, Spar/RibSDR UPS204776Spar · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON LT SIDE VERTICAL FIN FRONT SPAR FROM FIN STA 108.8 TO 6.372. CORROSION OUT OF LIMITS, REPAIRED LT SPAR CHORD IAW UPS EO B727-5530-7473-A.Oct 9, 1995 · N936UP · Boeing 727108C · Vertical Stabilizer, Spar/RibSDR UPS204775Floorbeam · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION FWD CARGO BAY IN THE NUTPLATE HOLES, LOWER FLANGE OF THE 600 FLOORBEAM LBL 16 RLB 58 WL 201. REPAIRED BS 600 FLOORBEAM IAW UPS EO B727-5310-7463-A. CORROSION REWORK WAS OUT OF LIMTS IAW SRM 53-10-1.Oct 9, 1995 · N936UP · Boeing 727108C · Fuselage Main, Floor BeamSDR UPS204774Flap · corrodedWHILE ON GROUND, MAINTENANCE REPLACED NR 3 K-FLAP, DUE TO CONDITION AND CORROSION. REMOVED AND REPLACED NR 3 K-FLAP IAW MM 27-81-01.Oct 9, 1995 · N936UP · Boeing 727108C · Leading Edge DevicesSDR UPS204773Pressure Panels · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON PANELS BETWEEN GASKET SEAL ON PRESSURE PANELS 3120 AND 3121. REMOVED AND REPLACED PANELS IAW SRM 51-30-2.Oct 9, 1995 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS204772Spar · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON INDICATIONS ON UPPER REAR SPAR ON LT WING AT WS 571. REMOVED CORROSION IAW 57-10-1, REPAIRED SPAR IAW SRM 57-10-6.Oct 9, 1995 · N936UP · Boeing 727108C · Wing SparSDR UPS204771Shear Tie · corrosionWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON VERTICAL FIN SHEAR TIE FITTING, AT FIN STA 204 LT SIDE FORWARD END OF RIB NR 10 INSIDE TUNNEL, FOUND WHILE WORKING TAIL 227 CI 360676. REMOVED SHEAR TIE FITTING AT FIN STA 204 LT SIDE. REPLACED SHEAR TIE IAW WROct 9, 1995 · N936UP · Boeing 727108C · Vertical StabilizerSDR UPS204770Shear Tie · corrosionWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON BOTH LT AND RT VERTICAL STABILIZER SHEAR TIES, AT FWD END OF RIB NR 9 AT FIN STA 180.6 INSIDE VERTICAL FIN TUNNEL. REMOVED AND REPLACED LT AND RT SHEAR TIES IAW 727 SRM 51-30-2.Oct 9, 1995 · N936UP · Boeing 727108C · Vertical StabilizerSDR UPS204769Shear Tie · corrosionWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON RT VERTICAL STABILIZER SHEAR TIE FITTING, AT FIN STA 204 INSIDE VERTICAL FIN TUNNEL. REMOVED AND REPLACED FITTING ON RT VERTICAL STAB AT FIN STA 204 IAW SRM 51-30-2.Oct 9, 1995 · N936UP · Boeing 727108C · Vertical StabilizerSDR UPS204768Fitting · corrosionWHILE ON GROUND, MAINTENANCE FOUND CORROSION LT WING I/B AILERON TURNAROUND FITTING. REPLACED FITTING IAW SRM 51-30-2.Oct 9, 1995 · N936UP · Boeing 727108C · Wing, Control Surface Attach FittingsSDR UPS204767Fitting · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION LT WING O/B AILERON LOCKOUT FITTING HAS CORROSION PITS IN LOWER SURFACE NEXT TO BELL CRANK. REPLACED FITTING IAW SRM 51-30-2, MM 27-10-131, 27-10-121.Oct 9, 1995 · N936UP · Boeing 727108C · Wing, Control Surface Attach FittingsSDR UPS204766Stiffener · crackedWHILE ON GROUND, MAINTENANCE FOUND VERTICAL STIFFENER AT FSS 480, ON O/B SIDE OF NR 6 SLAT I/B TRACK IS CRACKED. REMOVED AND REPLACED CRACKED STIFFENER IAW SRM 51-30-2 AT FSS 480.Oct 9, 1995 · N936UP · Boeing 727108C · Wing Miscellaneous StructureSDR UPS204765Stiffener · crackedWHILE ON GROUND, MAINTENANCE FOUND VERTICAL STIFFENER AT FSS 475, ON THE I/B SIDE OF NR 6 SLAT I/B TRACK IS CRACKED. REMOVED AND REPLACED STIFFENER AT FSS 475, I/B SIDE NR 6 SLAT I/B TRACK IAW SRM 51-30-2.Oct 9, 1995 · N936UP · Boeing 727108C · Wing Miscellaneous StructureSDR UPS204764Spar · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON RT WING L/E LOWER FRONT SPAR CHORD AT FSS 200. MECHANICALLY REMOVED CORROSION, REWORK OUT OF LIMITS IAW SRM 57-10, FRONT SPAR LOWER CHORD REPAIRED IAW UPS EO 727-57-1642.Oct 9, 1995 · N936UP · Boeing 727108C · Wing SparSDR UPS204763Mid Spar · crackedWHILE ON GROUND, MAINTENANCE FOUND RT VERT FIN MID SPAR UPPER FLANGE HAS BROKEN FASTENER HOLE. REMOVED DAMAGE, FABRICATED, INSTALLED REPAIR ANGLES PER SRM 51-30-2 UPS EO 727-55-0303.Oct 9, 1995 · N936UP · Boeing 727108C · Vertical Stabilizer, Spar/RibSDR UPS204762Rib · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION IN BORE FOR BOTTOM BUSHING AND O/B FACE ON UPPER THRUST RIB LUG FOR LOWER SPLICE BEAM, AT APPROX RUDDER STA 128 TO 765 LT. REMOVED CORROSION AND OVERSIZE BORE, INSTALLED OVERSIZED BUSHING IAW EO 727-55-0302.Oct 9, 1995 · N936UP · Boeing 727108C · Rudder, Spar/RibSDR UPS204761Skin · corrosionWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON SKIN AT BS 272 TO 275, LBL 56 WL 209 TO 213. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. TRIMMED OUT DAMAGE AREA, FABRICATED REPAIR DOUBLER, FINAL REPAIR PER SRM 53-30-1, 53-30-2, 51-10-2, 51-30-2, EO B727-53Oct 9, 1995 · N936UP · Boeing 727108C · Fuselage Main, Plate/SkinSDR UPS204760Floorbeam · corrodedWHILE ON GROUND, MAINTENANCE FOUND CORROSION ON FLOORBEAM STA 328 LBL 33 WL 208 AND MECHANICAL DAMAGE LBL 54 WL 208. REPAIRED IAW SRM 53-10-8 AND B727-53-1686.Oct 9, 1995 · N936UP · Boeing 727108C · Fuselage Main, Floor BeamSDR UPS804758Rib · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON BORE FOR BOTTOM BUSHING AND O/B FACE ON UPPER THRUST RIB LUG FOR LOWER SPLICE BEAM AT APPROX RUDDER STA 128.765 LT. MAINTENANCE REMOVED CORROSION AND OVERSIZE BORE, INSTALLED OVERSIZED BUSHING IAW TRAMCO EOct 5, 1995 · N936UP · Boeing 727108C · Horizontal Stabilizer, Spar/RibSDR UPS804757Floor Beam · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM AT STA 420 RBL 45-65, WL 208 LOWER SIDE OF UPPER CHORD. MAINTENANCE REMOVED THE CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. MAINTENANCE REPAIRED IAW UPS EO B727-5310-7455A.Oct 5, 1995 · N936UP · Boeing 727108C · Fuselage Main, Floor BeamSDR UPS804756Floor Beam · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON BEAM STA 420 LBL 0 TO LBL 24 AND LBL 45 - LBL 65, WL 208 LOWER SIDE OF UPPER CHORD. MAINTENANCE REMOVED CORROSION ON UPPER CHORD OF FLOOR BEAM, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. MAINTENANCE REMOVOct 5, 1995 · N936UP · Boeing 727108C · Fuselage Main, Floor BeamSDR UPS804755Web · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND SUPPORT WEB TO BE CRACKED AT BS 600, LBL 7, WL 300. MAINTENANCE REPAIRED AREA IAW EO B727-53-1683.Oct 5, 1995 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS804754Skin · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON SKIN AT BS 272-275, LBL 56, WL 209-213. MAINTENANCE REMOVED THE CORROSION, WAS FOUND TO BE OUT OF LIMITS, TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER, PERFORMED FINAL REPAIR IAW SRM 53-30-1, 53-30-Oct 5, 1995 · N936UP · Boeing 727108C · Fuselage Main, Plate/Skin
Back to Boeing 727-108C