Boeing 727-108C

Service difficulty reports · 255

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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 UPS204555Fitting · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON UPPER FWD SIDE OF NR 2 K-FLAP OUTBOARD MOUNTING LUG WHILE WORKING NR 360298 (WINGS 203). REMOVED AND REPLACED NR 2 K-FLAP OUTBOARD MOUNTING FITTING PER SRM 51-30-2 AND MM 27-81-01.Sep 28, 1995 · N936UP · Boeing 727108C · Leading Edge DevicesSDR UPS204554Web · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 4 SLAT RIB CRACKED AT SLAT STA 7.25. REMOVED AND REPLACED NR 4 SLAT RIB AT SLAT STA 7.25 IAW SRM 51-10-1, 51-30-2.Sep 28, 1995 · N936UP · Boeing 727108C · Leading Edge DevicesSDR UPS204553Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 3 SLAT, RIB JUST I/B OF TAI T-DUCT, CRACKED AT FWD CORNER. REMOVED AND REPLACED NR 3 SLAT RIB JUST I/B OF TAI T-DUCT IAW SRM 51-10-1, 51-30-2.Sep 28, 1995 · N936UP · Boeing 727108C · Leading Edge DevicesSDR UPS204552Frame · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND FRAME CRACKED AT STRINGER TO FRAME ATTACH POINT BS 804 STRINGER 14 RT. REPAIRED FRAME PER SRM 51-40-3.Sep 28, 1995 · N936UP · Boeing 727108C · Fuselage Main, FrameSDR UPS204551Stringer · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-0.1-08-01) ON STR 6L STA 660-680. REPAIRED IAW SRM 53-10-3, 51-10-2, 51-10-3.Sep 28, 1995 · N936UP · Boeing 727108C · Fuselage Main, Longeron/StringerSDR UPS204550Clip · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-111-01.00-01) BS 400 STR 19L ON STRINGER CLIP. REPLACED CLIP IAW SRM 51-10-6, 51-30-2 SRM 51-20-4.Sep 28, 1995 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS204549Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB ON NR 5 SLAT 23 INCHES FROM O/B END (4TH RIB FROM O/B END, MARKED). REMOVED AND REPLACED 4TH RIB FROM O/B END OF NR 5 SLAT IAW SRM 51-30-2, 51-30-5.Sep 28, 1995 · N936UP · Boeing 727108C · Leading Edge DevicesSDR UPS204548Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND LOWER LT HORIZONTAL STAB RIB CHORD HAS A CRACK AT STA STA 8.00 (MARKED AT FRONT SPAR WEB). REMOVED AND REPLACED RIB CHORD AT LT STAB STA 8.00 PER SRM 51-10-1 AND SRM 51-30-2.Sep 28, 1995 · N936UP · Boeing 727108C · Horizontal Stabilizer, Spar/RibSDR UPS204547Trim Tab · delaminatedWHILE IN FOR SI CHECK, MAINTENANCE FOUND RT WING I/B AILERON TAB IS DELAMINATED AT T/E (MARKED). REPLACED RT WING AILERON TAB IAW SRM 51-80.Sep 28, 1995 · N936UP · Boeing 727108C · Aileron TabsSDR UPS204546Floor Beam · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-01) ON FLOOR BEAM STA 344 LBL 60-RBL 60 WL 208. MECHANICALLY REMOVED CORROSION IAW SRM 51-10-6. REPAIRED FLOOR BEAM IAW SRM5 1-30-2, 51-10-2, 53-10-8.Sep 28, 1995 · N936UP · Boeing 727108C · Fuselage Main, Floor BeamSDR UPS204545Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.00-03) ON STRINGER 1 STA 1110-1130. CORROSION MECHANICALLY REMOVED IAW SRM 51-10-6. REPAIRED STR 1 STA 1110-1130 IAW SRM 53-10-3.Sep 28, 1995 · N936UP · Boeing 727108C · Fuselage Main, Longeron/StringerSDR UPS204544Skin · corrosionWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.06-03) ON INTERIOR SKIN STA 1070-1090 STR 10-14 RT FROM UNDER WINDOW CASTING AND REPAIR DOUBLERS. REPLACED WINDOW FRAME PER SRM 51-10-1, 51-10-2, 51-10-6, 51-30-2, 53-10-4 AND 51-20-4.Sep 28, 1995 · N936UP · Boeing 727108C · Fuselage Main, Plate/SkinSDR UPS204543Chord · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION BS 1110, WL 199 BL 0 ON THE STABILIZATION STRAP (CHORD) AROUND THE NUT PLATES. REMOVED CORROSION PER SRM 53-10-1. REMOVED DAMAGED SECTION, FABRICATED REPLACEMENT CHORD AND INSTALLED PER SRM 51-30-2 AND SRM 5Sep 28, 1995 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS204507Rib Chord · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HAND HORIZONTAL STABILIZER, INBOARD UPPER CLOSURE WEB CHORD FROM APPROXIMATELY 11.5 TO 24.75 AFT OF HORIZONTAL STABILIZER FRONT SPAR. MAINTENANCE REMOVED, FABRICATED AND REPLACED THE CHORD IAW SRSep 22, 1995 · N936UP · Boeing 727108C · Horizontal Stabilizer, Spar/RibSDR UPS204506Doubler · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE DOUBLER AT STATION 307.5 TO STA 316, LBL 12.5 WL 181 TO 169. MAINTENANCE REMOVED TRIPLER AND REMOVED CORROSION ON TRIPLER. CORROSION FOUND BEYOND LIMITS, FABRICATED NEW DOUBLER AND TRIPLER, FINAL INSTASep 22, 1995 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS204505Frame · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE FASTENER HOLES, COMMON TO FRAME AT STATION 360 LBL 48 WL 165, BS 360 LBL 45 WL 165, BS 360 LBL 35 WL 158 AND BS 360 RBL 21 WL 151. MAINTENANCE REPAIRED PER UPS EO 727-53-1667.Sep 22, 1995 · N936UP · Boeing 727108C · Fuselage Main, FrameSDR UPS204504Fitting · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE TRACK ATTACH POINT, LEFT WING NR 3 FLAP TRACK INBOARD AFT ATTACH FITTING AT SPOILER SUPPORT BEAM. MAINTENANCE REMOVED THE CRACKED ATTACH FITTING, INSTALLED A NEW ATTACH FITTING PER SRM 51-30-2, MM 27-51-Sep 22, 1995 · N936UP · Boeing 727108C · Wing, Control Surface Attach FittingsSDR UPS204503Rib · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE HORIZONTAL STABILIZER RIGHT HAND INBOARD CLOSURE WEB, INSIDE ACCESS HOLE 9223 AREA, FWD WEB UPPER END WHERE THE WEB ATTACHING BRACKET IS MOUNTED AND EXTENDING 16 INCHES FWD. MAINTENANCE REMOVED, FABRICSep 22, 1995 · N936UP · Boeing 727108C · Horizontal Stabilizer, Spar/RibSDR UPS204502Lower Frame · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER SEAL OF THE LEFT HAND AFT OVERWING EXIT HATCH. MAINTENANCE REMOVED THE LOWER AFT FRAME AND SEAL FORMERS, INSTALLED NEW FRAME AND SEAL FORMER. INSTALLATION IAW SRM 51-30-2, 53-30-01, AND 52-20-1.Sep 22, 1995 · N936UP · Boeing 727108C · Emergency ExitsSDR UPS204501Intercostal · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE INTERCOSTAL AT STA 277 TO 294 WL 208. MAINTENANCE REPLACED THE DAMAGED AREA IAW SRM 51-30-2, 51-10-2, 51-10-6 AND 51-20-6.Sep 22, 1995 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS204489Stringers · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION IN VARIOUS SPOTS ON STRINGER 5, 6, 7, 8 AT STATION 277 - 294, LBL 29 - 47 AND WL 268 - 287. MAINTENANCE REPLACED STRINGERS 7 AND 8L ON UPS EO 5310-1259F, STRINGERS 5 AND 6L WERE REMOVED AND REPLACED IAW SRM.Sep 20, 1995 · N936UP · Boeing 727108C · Fuselage Main, Longeron/StringerSDR UPS204487Beam · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT HORIZONTAL TRAILING EDGE BEAM EXTERIOR SURFACE AT STAB STATION 225.54 AND 182.5. MAINTENANCE CUTOUT THE DAMAGED SECTION AND SPLICED IN NEW SECTION IAW SRM 55-10-6.Sep 20, 1995 · N936UP · Boeing 727108C · Horizontal Stabilizer StructureSDR UPS204486Floor Beam · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE FLOOR BEAM AROUND THE NUTPLATE HOLE FORWARD LOWER SIDE OF THE UPPER CHORD ON THE FLOOR BEAM AT STATION 500, LBL 55 - 57 AND WL 208. MAINTENANCE REPAIRED THE FLOOR BEAM IAW SRM 53-10-8.Sep 20, 1995 · N936UP · Boeing 727108C · Fuselage Main, Floor BeamSDR UPS204485Stringer · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN STRINGER 16 AT STATION 294.5, LBL 59 AND WL 217. MAINTENANCE REMOVED AND REPLACED PART OF THE STRINGER IAW UPS EO B727-5310-1259F.Sep 20, 1995 · N936UP · Boeing 727108C · Fuselage Main, Longeron/StringerSDR UPS204484Splice · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE TOP OF FRAME AT STATION 380 AND STRINGER 26R - 25R. MAINTENANCE REPLACED THE FRAME SPLICE IAW SRM 53-10-1, 53-10- 2 AND 51-10-6.Sep 20, 1995 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS204483Spar Web · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT WING FRONT SPAR CENTER TANK ACCESS DOOR CUTOUT ON THE OUTER SURFACE. MAINTENANCE REMOVED THE DAMAGED AREA, REPAIRED AND INSTALLED PER SRM 57-30-3 AND UPS EO 727-57-1630.Sep 20, 1995 · N936UP · Boeing 727108C · Wing SparSDR UPS204481Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE RIB OF THE NR 6 SLAT ATTACH ROD END ATTACH POINT. MAINTENANCE REMOVED THE CRACKED RIB AND REPLACED WITH A NEW RIB IAW SRM 51-30-2, 51-30-8 AND 51-30-5.Sep 20, 1995 · N936UP · Boeing 727108C · Leading Edge DevicesSDR UPS204480Stiffener · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE LEFT HORIZONTAL STABILIZER WEB STIFFENER AT STAB STATION 73 ON THE UPPER SIDE OF THE STIFFENER. MAINTENANCE REMOVED THE CRACKED STIFFENER AND REPLACED WITH NEW IAW SRM 57-30-2.Sep 20, 1995 · N936UP · Boeing 727108C · Horizontal Stabilizer StructureSDR UPS204479Stiffener · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE LEFT HORIZONTAL STABILIZER WEB STIFFENER AT STAB STATION 64 ON THE UPPER SIDE OF STIFFENER. MAINTENANCE REMOVED THE CRACKED STIFFENER AND REPLACED WITH NEW PER SRM 57-30-2.Sep 20, 1995 · N936UP · Boeing 727108C · Horizontal Stabilizer StructureSDR UPS204478Stiffener · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK ON THE LEFT HORIZONTAL STABLIZER WEB STIFFENER AT STATION 54 ON THE UPPER SIDE OF THE STIFFENER. MAINTENANCE REMOVED THE CRACKED STIFFENER AND REPLACED WITH NEW IAW SRM 57-30-2.Sep 20, 1995 · N936UP · Boeing 727108C · Horizontal Stabilizer StructureSDR UPS204477Stiffener · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HORIZONTAL STABILIZER AFT INTERSPAR WEB INBOARD ATTACHING BRACKET INSIDE ACCESS PANEL AREA 9206. MAINTENANCE FABRICATED NEW STIFFENER AND INSTALLED IAW SRM 51-30-2 AND 55-10-1.Sep 20, 1995 · N936UP · Boeing 727108C · Horizontal Stabilizer StructureSDR UPS204476Stiffener · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE HORIZONTAL STABILIZER RIGHT INBOARD CLOSURE WEB INSIDE ACCESS PANEL 9205 AREA AT UPPER END OF WEB WHERE AFT INTERSPAR WEB ATTACHING BRACKET IS MOUNTED. MAINTENANCE FABRICATED NEW STIFFENER AND INSTALLESep 20, 1995 · N936UP · Boeing 727108C · Horizontal Stabilizer StructureSDR UPS204475Skin · delaminatedWHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON UPPER SURFACE RUB STRIP OF THE RIGHT WING INBOARD FORE FLAP. MAINTENANCE REPAIRED THE DAMAGED AREA IAW SRM 51-40-6.Sep 20, 1995 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS204474Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 5L AND STATION 1130 - 1180. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED PER SRM 53-10-3, 53-10-2, 51-30-3, 51-10-2 AND 51-10-6.Sep 20, 1995 · N936UP · Boeing 727108C · Fuselage Main, Longeron/StringerSDR UPS204473Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 4R AT STATION 1110 - 1180. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED AND INSTALLED IAW SRM 53-10-1, 53-10-2, 51-10-6, 53-10-3, 51-30-2.Sep 20, 1995 · N936UP · Boeing 727108C · Fuselage Main, Longeron/StringerSDR UPS204472Stringer · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7L STATION 1110 - 1176. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2.Sep 20, 1995 · N936UP · Boeing 727108C · Fuselage Main, Longeron/StringerSDR UPS204471Chord · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER NOSE CHORD AT STATION 324, 340, 346, RBL 14.5 AND WL 166. MAINTENANCE REPLACED THE CHORD IAW SRM 51-10-2, 51-10-6, 51-30-2, 53-10-1 AND 51-20-4.Sep 20, 1995 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS204470Chord · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER NOSE CHORD AT STATION 334 AND 335 AND LBL 14.5. MAINTENANCE REPLACED THE CHORD IAW SRM 51-10-2, 51-10-6, 51-30-2. 53-10-1 AND MM 51-20-4.Sep 20, 1995 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS204469Intercostal · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND THE NUT PLATES AT STATION 803, RBL 6 AND WL 148. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED NEW INTERCOSTAL AND INSTALLED IAW SRM 53-10-1, 51-10-6 AND 51-30-2.Sep 20, 1995 · N936UP · Boeing 727108C · Fuselage Miscellaneous StructureSDR UPS204451Spar Chord · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE LEFT HAND HORIZONTAL STABILIZER LOWER AFT SPAR CHORD AT STAB STATION 170. MAINTENANCE STOP DRILLED THE CRACK, NDT VERIFIED CONTAINMENT, FABRICATED REPAIR ANGLE DOUBLER.Sep 18, 1995 · N936UP · Boeing 727108C · Horizontal Stabilizer, Spar/RibSDR UPS204450Blkhd Support · corrodedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD CARGO BAY AT THE HORIZONTAL ANGLE OF THE 680 BULKHEAD SUPPORT, LBL 13 RBL 17 AND WL 198. MAINTENANCE REPLACED THE SUPPORT IAW SRM 51-20-1, 51-30-5 AND 51-30-2.Sep 18, 1995 · N936UP · Boeing 727108C · Fuselage Main, BulkheadSDR UPS204449Te Wedge · delaminatedWHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE LEFT WING OUTBOARD MIDFLAP TRAILING EDGE WEDGE. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED GLASS REPAIR AND INSTALLED IAW SRM 51-40-6.Sep 18, 1995 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS204448Skin · delaminatedWHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE LEFT WING OUTBOARD AFT FLAP UPPER SURFACE CENTER. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED FIBERGLASS REPAIR AND INSTALLED PER SRM 51-40-6.Sep 18, 1995 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS204447Te Wedge · delaminatedWHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE INBOARD END UPPER SURFACE OF THE TRAILING EDGE WEDGE, ON THE LEFT WING INBOARD MIDFLAP. MAINTENANCE REMOVED THE DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED THE REPAIR PER SRM 51-40-6.Sep 18, 1995 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS204446Skin · delaminatedWHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE OF THE RIGHT WING INBOARD AFT FLAP. MAINTENANCE REMOVED THE DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED REPAIR PER SRM 51-40-6.Sep 18, 1995 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS204445Skin · delaminatedWHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION AND MULTIPLE DENTS ALONG THE LOWER SURFACE OF THE RIGHT WING INBOARD AFT FLAP. MAINTENANCE REMOVED THE DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED REPAIRS PER SRM 51-40-6.Sep 18, 1995 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS204444Doubler · delaminatedWHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION AT THE SEAM DOUBLER ON THE RIGHT WING INBOARD FOREFLAP LOWER SURFACE. MAINTENANCE REMOVED THE DAMAGED AREAS, APPLIED FIBERGLASS AND COMPLETED THE REPAIR PER SRM 51-51-11, 51-40-6.Sep 18, 1995 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS204443Te Wedge · delaminatedWHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE RIGHT WING INBOARD MIDFLAP TRAILING EDGE WEDGE, AT THE UPPER SURFACE NR 3 AFT FLAP CARRIAGE AND LOWER SURFACE AT THE NR 4. MAINTENANCE REPLACED THE TRAILING EDGE WEDGE.Sep 18, 1995 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS204442Te Skin · delaminatedWHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE RIGHT WING INBOARD MIDFLAP UPPER AND LOWER TRAILING EDGE SURFACES, AT NR 1 AFT FLAP CARRIAGES. MAINTENANCE REPLACED THE TRAILING EDGE WEB.Sep 18, 1995 · N936UP · Boeing 727108C · Trailing Edge FlapsSDR UPS204441Skin · delaminatedWHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION IN THE RIGHT WING INBOARD FOREFLAP ALONG THE LEADING EDGE INBOARD END LOWER SURFACE. MAINTENANCE REMOVED THE DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED REPAIR PER MM 51-20-151, 51-40-6.Sep 18, 1995 · N936UP · Boeing 727108C · Trailing Edge Flaps
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