Boeing 727-27C

Service difficulty reports · 1,078

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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 = '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 UPS97222445Seat Track · corrodedINSPECTION TYPE-SI, CORROSION ON SEAT TRACK BS 364 LBL 65 WL 208. SEAT TRACK SECTION REMOVED AND REPLACED WITH NEW SECTION IAW SRM 51-30-2, 51-30-5, 51-30-8.Mar 15, 1997 · N909UP · Boeing 72727C · Fuselage, Seat/Cargo Attach FittingsSDR UPS97222306Control Valve · leakingAPPROX 5 MIN AFTER T/O, BOTH A-SYS LOW HYD PRESS LIGHTS ILLUMINATED AND THE A-SYS QTY DROPPED TO ZERO. A-SYS PRESS REMAINED AT APPROX 2000 PSI, BUT OSCILATED FROM 1500-2400 PSI AFTER CK LIST COMPLETE A-SYS QTY ROSE TO 1.7. ALL CK LIST COMPLIED WITH AND AIRCRMar 11, 1997 · N939UP · Boeing 72727C · Trailing Edge Flap Control SystemSDR UPS97222271Skin · corrodedINSPECTION TYPE-SI, CORROSION ON SKIN 620-630 LBL 38 WL 291-307. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-30-1 REPAIRED IAW EWO 97-2045 UPS ENG FILE NR 727-53-1865 AND NON ROUTINE 497979.Mar 9, 1997 · N910UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS97222270Strap · crackedINSPECTION TYPE-SI, LFEC INSP OF BEAR STRAP, AT BS 620, EXHIBIT CRACK INDICATIONS AT 6 FASTENERS (MARKED) BETWEEN STR 14L AND 15 L. REQUIRE FASTENER REMOVAL TO FACILITATE INVESTIGATION INSP. REPAIRED PER EWO 97-2055 UPS ENG FILE NR727-53-1863.Mar 9, 1997 · N910UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222273Doubler · corrodedINSPECTION TYPE-SI, CORROSION ON LOWER SKIN SURFACE AT NR 2 FLAP TRACK AFT ATTACH POINT. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 57-30-01, REPAIRED PER EWO 97-2044 UPS ENG FILE NR 727-57-1796.Mar 8, 1997 · N910UP · Boeing 72727C · Trailing Edge FlapsSDR UPS97222272Skin · corrodedINSPECTION TYPE-SI, WHILE WORKING CUST CARD 497867, FOUND CORROSION ON TOP OF SKIN ON FUEL TANK, STA 850-870 WL 191 LBL 50-65 MARKED. FOUND CORROSION TO BE OUT OF LIMITS, REPAIRED IAW EWO 97-2059 UPS ENG FILE NR727-57-1797.Mar 8, 1997 · N910UP · Boeing 72727C · Wing, Plate/SkinSDR 97FDEA00139Retract Mech · lack of lubeON GEAR EXTENSION, RED NOSE GEAR LIGHT DID NOT ILLUMINATE NORM. GRN LIGHT CAME ON OK, IT THEN FLICKERED AND THE WARN HORN STARTED TO SOUND INTERMITTENTLY. GRN LIGHT THEN WENT OUT AND WOULD NOT TEST, THEN TESTED OK. THROTTLE RESTARTED AND UNSAFE INDICATION WMar 5, 1997 · N146FE · Boeing 72727C · Landing Gear Retraction/Extension SystemSDR UPS97222179Stringer · corrodedINSPECTION TYPE-SI, CORROSION ON STR 4 BS 310 TO 340 AND INTERCOSTAL ATTACH TO STRINGER. REMOVED CORROSION IAW SRM 51-10-6, REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED STR 4L AND INTERCOSTAL FROM STA 310 TO 340 IAW SRM 53-10-3, 53-10-4, 51-20-1, 51Feb 27, 1997 · N910UP · Boeing 72727C · Fuselage Main, Longeron/StringerSDR UPS97222178Chord · corrodedINSPECTION TYPE-C, CORROSION BS 740 UPPER CHORD SHOWS SIGNS OF CORROSION AT RBL 45 TO RBL 52 AND LBL 47 WL 200. CORROSION REMOVED REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPLACED UPPER CHORD FROM 32.75 TO 70.5 IAW TRAMCO EWO 97-2043 (UPS FILE B727-57-17Feb 27, 1997 · N910UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222216Bearing Support · crackedINSPECTION TYPE:SI, NOTED CRACK INDICATION ON RT MLG FWD TRUNNION BEARING SUPPORT. REMOVED AND REPLACED RT MLG FWD TRUNNION BEARING SUPPORT IAW M/M 32-11-51.Feb 26, 1997 · N910UP · Boeing 72727C · Main Landing Gear Attach SectionSDR UPS97222274Spar Chord · corrodedINSPECTION TYPE-SI, WHILE WORKING CUST CARD 497867, FOUND LOWER CHORD BS 870, TO BE CORRODED. REMOVED CORRODED LOWER SPAR CHORD AT BS 870, INSTALLED A NEW SPAR CHORD IAW SRM 57-10-1, EWO 97-2050 UPS ENG FILE NR 727-57-1788.Feb 25, 1997 · N910UP · Boeing 72727C · Wing SparSDR UPS97222177Spar Chord · corrodedINSPECTION TYPE-C, WHILE WORKING CUST CARD 497867 FOUND LOWER CHORD BS 870 TO BE CORRODED. REMOVED CORRODED LOWER SPAR CHORD AT BS 870 AND INSTALLED A NEW SPAR CHORD IAW SRM 57-10-1 AND EWO 97-2050.Feb 25, 1997 · N910UP · Boeing 72727C · Wing SparSDR UPS97222138Stiffener · corrodedINSPECTION TYPE-SI, CORROSION ON VERTICAL STIFFENER BS 259.5 WL 162 RBL 24. REMOVED CORROSION REWORK DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED VERTICAL STIFFENER AT BS 259.5 RBL 24 WL 162 IAW SRM 51-40-4.Feb 24, 1997 · N910UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222137Beam · crackedINSPECTION TYPE-SI, WHILE WORKING NRC 497868 FOUND RBL 45 LONGITUDINAL BEAM LOWER CHORD CRACKED IN RADIUS STA 745 WL 204. REPLACED LONG BEAM LOWER CHORD AT RBL 45 STA 745 IAW SRM 51-10-1, 51-10-2, 51-30-2 AND BOEING DRAWING 65-34144.Feb 24, 1997 · N910UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222148Seat Track · corrodedINSPECTION TYPE-C, CORROSION ON CARGO SEAT TRACK, STA 538 RBL 12. CORROSION REMOVAL OUT OF LIMITS. REMOVED SEAT TRACK FROM BS 480 TO 540, FABRICATED NEW SECTION OF SEAT TRACK, INSTALLED PER SRM 51-10-06, 53-10-05.Feb 23, 1997 · N908UP · Boeing 72727C · Fuselage, Seat/Cargo Attach FittingsSDR UPS97222147Seat Track · crackedINSPECTION TYPE-C, WHILE WORKING CARD 509145 FUSEL 43 FOUND CARGO FLOOR TRACK CRACKED BETWEEN BS 558 AND BS 564 RBL 12. REMOVED CRACKED SECTION OF SEAT TRACK, FABRICATED REPLACEMENT PART, INSTALLED PER SRM 53-10-5, 51-10-6.Feb 23, 1997 · N908UP · Boeing 72727C · Fuselage, Seat/Cargo Attach FittingsSDR UPS97222146Floorbeam · corrodedINSPECTION TYPE-C, CORROSION ON FLOORBEAM TOP CHORD FORWARD SIDE STA 328, WL 208 RBL 39. CORROSION REMOVAL OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER SRM 53-10-1, 53-10-8, 51-20-4 MM 51-20-131.Feb 23, 1997 · N908UP · Boeing 72727C · Fuselage Main, Floor BeamSDR UPS97222145Splice · crackedINSPECTION TYPE-C, WHILE WORKING CUST CARD 509379 FUSEL 71 FOUND FRAME BELOW CARGO TRACK TO BE CRACKED BS 540 RBL 15. REMOVED DAMAGED FRAME, FABRICATION, INSTALLATION ALL WORK DONE PER SRM 51-40-3.Feb 23, 1997 · N908UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222144Skin · corrodedINSPECTION TYPE-C, CORROSION ON INNER SKIN BS 1080 BETWEEN STR 5L AND STR 6L ON AFT SKIN. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER EO B727-5330-1177K.Feb 22, 1997 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS97222143Skin · corrodedINSPECTION TYPE-C, CORROSION ON INNER SKIN BS 1080 BETWEEN STR 1 TO 4 LEFT OF STR 2L. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER EO B727-5330-1177K.Feb 22, 1997 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS97222142Beam · crackedINSPECTION TYPE-C, POSSIBLE CRACK ON BEAM AT LIGHTENING HOLE BS 1183 LBL 26.83 WL 259.5. STOP DRILLED CRACK, HFEC CONFIRMED CONTAINMENT, REPAIRED IAW B727-5310-1116-D.Feb 21, 1997 · N908UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222103Skin · corrodedINSPECTION SI-CHECK, NR 6 K-FLAP INNER SURFACE IS CORRODED UNDER FASTENER ON RIB 6 FROM OUTBOARD END. CORROSION REMOVED, REWORK OUT OF LIMITS IAW SRM 57-50-1. REMOVED AND REPLACED NR 6 K-FLAP IAW MM 27-81-01.Feb 20, 1997 · N910UP · Boeing 72727C · Leading Edge DevicesSDR UPS97222102Lugs · corrodedINSPECTION SI-CHECK, NR 2 K-FLAP HAS CORROSION ON OUTBOARD LUG OUTBOARD SIDE AROUND BOLTS. CORROSION FOUND TO BE OUT OF LIMITS IAW UPS EO B727-5750-5542. REMOVED AND REPLACED NR 2 K-FLAP IAW MM 27-81-01.Feb 20, 1997 · N910UP · Boeing 72727C · Leading Edge DevicesSDR UPS97222174Rib · crackedINSPECTION TYPE-C, RIB AT LEFT WING BL 620 IS CRACKED. STOP DRILLED CRACK, VERIFIED CONTAINMENT, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-10-2, 51-40-2.Feb 19, 1997 · N908UP · Boeing 72727C · Wing, Rib/BulkheadSDR UPS97222140Fitting · corrodedINSPECTION TYPE-SI, CORROSION IN WELL OF BARRIER NET CASTING BS 360 TO 380 LBL 5 WL 205. MECHANICALLY REMOVED CORROSION IAW SRM 51-10-6, REWORK IS OUT OF LIMITS IAW SRM 53-10-1, REWORKED IAW TRAMCO EWO 97-2060 UPS EO FILE NR 727-53-1857 R1.Feb 19, 1997 · N910UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS97222162Skin · corrodedINSPECTION TYPE-C, NR 1 SPOILER IS DISBONDED AND CORRODED. REMOVED DAMAGED PANEL AND REPLACED WITH SERVICEABLE PANEL IAW MM 27-61-01.Feb 18, 1997 · N908UP · Boeing 72727C · SpoilersSDR UPS97222161Skin · delaminatedINSPECTION TYPE-C, NR 6 SPOILER HAS 8 BY 18 AREA OF DELAMINATION UPPER SURFACE I/B FWD CORNER. REMOVED DAMAGED AREA REPAIRED IAW SRM 57-60-6.Feb 18, 1997 · N908UP · Boeing 72727C · SpoilersSDR UPS97222160Hinge · corrodedINSPECTION TYPE-C, WHILE WORKING CUST ID 509318 FOUND CORROSION ON THE NR 6 SPOILER CENTER HINGE. REMOVED CORRODED FITTING AND REPLACED WITH NEW PART IAW SRM 51-30-5 MM 27-62-81 SRM 51-30-2 MM 27-50-00.Feb 18, 1997 · N908UP · Boeing 72727C · SpoilersSDR UPS97222175Beam · crackedINSPECTION TYPE-C, FWD ENTRY DOOR NR 1 LOWER LONGITUDINAL BEAM CRACKED IN OUTBOARD RADIUS ALONG AFT END. STOP DRILLED CRACK, VERIFIED CONTAINMENT, FABRICATED REPAIR PARTS, INSTALLED IAW SRM 51-40-3, 51-30-2.Feb 17, 1997 · N908UP · Boeing 72727C · Passenger/Crew DoorsSDR UPS97222163Skin · corrodedINSPECTION TYPE-C, CORROSION SKIN AT OXYGEN SERVICING PANEL BULGING. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-30-3, 51-20-15, 53-10-3, 51-10-1, 51-40-3.Feb 17, 1997 · N908UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS97222267Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION STA 950 FLOORBEAM ON TOP AND BOTTOM OF UPPER CHORD AROUND NUTPLATE HOLES LBL 60 TO RBL 60. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER SRM 53-10-6, 51-20-151, 53 10-5, 51-30-2 AND EWO 97-2056 UPS ENG FILE NFeb 7, 1997 · N910UP · Boeing 72727C · Fuselage Main, Floor BeamSDR UPS97222068Corner Fitting · corrodedINSPECTION TYPE-SI, UPON REMOVAL OF PRESSURE SEAL FOUND MAIN CARGO DOOR FWD UPPER SEAL RETAINER CORNER CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED FITTING, LOCATED, DRILLED NEW PART, INSTALLED ALL WORK DONE PER SRM 51-30-1, 51-30-Feb 7, 1997 · N910UP · Boeing 72727C · Cargo/Baggage DoorsSDR UPS97222067Corner Fitting · corrodedINSPECTION TYPE-SI, UPON REMOVAL OF PRESSURE SEAL FOUND MAIN CARGO DOOR AFT UPPER SEAL RETAINER CORNER CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED CORNER, LOCATED, DRILLED NEW PART, INSTALLED. ALL WORK DONE PER SRM 51-30-2, 51-30-Feb 7, 1997 · N910UP · Boeing 72727C · Cargo/Baggage DoorsSDR UPS97221899Cargo Track · corrodedINSPECTION TYPE: C. CORROSION ON CARGO FLOOR SEAT TRACK BS 1051 RBL 15.5 BOTTOM SIDE OF FLANGE. REMOVED DAMAGED SECTION AND INSTALLED REPAIR SECTION IAW SRM 53-10-5.Feb 3, 1997 · N939UP · Boeing 72727C · Fuselage, Seat/Cargo Attach FittingsSDR UPS97221910Seat Track · corrodedINSPECTION TYPE: SI. CORROSION IN CENTER OF SEAT TRACK STA 1030-1050 LBL 25. REMOVED CORROSION IN CENTER OF SEAT TRACK STA 1039-1044 LBL 25 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPAIRED SEAT TRACK STA 1000-1060 LBL 25 PER SRM 53-10-5, 51-30-2.Feb 2, 1997 · N910UP · Boeing 72727C · Fuselage, Seat/Cargo Attach FittingsSDR UPS97221908Stringer · corrodedINSPECTION TYPE: SI. CORROSION ON STR 4L STA 970-990 STA 1110-1130 STA 1150-1170. AREAS MARKED CORROSION STA 1110-1130 STA 1150-1170 WITHIN LIMITS, STA 970-990 OUT OF LIMITS PER SRM 51-10-1, REPAIRED PER SRM 53-10-3 MM 51-20-21, 51-20-31.Feb 1, 1997 · N910UP · Boeing 72727C · Fuselage Main, Longeron/StringerSDR UPS97221906Frame · crackedINSPECTION TYPE: SI. CRACKED ON FRAME AT STA 277 LBL 52 WL 219 AND WL 235. REPAIRED FRAME AT STA 277 LBL 52 WL 219 AND 235 IAW SRM 51-40-2.Jan 31, 1997 · N910UP · Boeing 72727C · Fuselage Main, FrameSDR UPS97221904Frame · crackedINSPECTION TYPE: SI. CRACKED FRAME STA 620 STR 22R I/B FLANGE AT NUTPLATE HOLE WL 170 RBL 50. REPAIRED FRAME AT STA 620 STR 22R IAW SRM 51-40-3.Jan 31, 1997 · N910UP · Boeing 72727C · Fuselage Main, FrameSDR UPS97221902Skin · delaminationINSPECTION TYPE: C. LT WING AFT I/B FLAP HAS A 4 INCH BY 4 INCH AREA OF DELAMINATION 9 INCHES FROM O/B END AND 9 INCHES FROM TRAILING EDGE OUTER SURFACE. REPAIRED LT WING I/B AFT FLAP IAW SRM 51-40-6.Jan 31, 1997 · N939UP · Boeing 72727C · Trailing Edge FlapsSDR UPS97221901Skin · delaminatedINSPECTION TYPE: C. RT WING I/B AFT FLAP HAS 2 AREAS OF DELAMINATION 18 INCHES FROM I/B END, 13 INCHES FROM T/E UPPER SURFACE. REPAIRED RT WING I/B AFT FLAP IAW SRM 51-40-6.Jan 31, 1997 · N939UP · Boeing 72727C · Trailing Edge FlapsSDR CA970217004Screwjack · req lube(CAN) WHILE CONDUCTING PREFLIGHT CHECKS CREW REPORTED THE STAB TRIM VERY HEAVY WHEN SELECTED TO MANUAL. SCREWJACK CLEANED AND LUBRICATED.Jan 31, 1997 · Boeing 72727C · Elevator Tab Control SystemSDR UPS97221903Hinge Assy · corrodedINSPECTION TYPE: SI. CORROSION ON LT O/B AILERON CENTER I/B HINGE FITTING (WING SIDE). REMOVED AND REPLACED LT O/B AILERON HINGE FITTING (CENTER I/B) IAW SRM 51-30-2, 51-30-5.Jan 30, 1997 · N910UP · Boeing 72727C · AileronsSDR UPS97221880Skin · delaminatedINSPECTION TYPE: SI. NR 9 SPOILER INBOARD UPPER SURFACE CORNER IS DELAMINATED. DELAMINATION BEING REPAIRED ON NON-ROUTINE CARD NUMBER 498268. WORK ON THAT CARD PERFORMED IAW SRM 51-40-6.Jan 29, 1997 · N910UP · Boeing 72727C · SpoilersSDR UPS97221879Skin · delaminatedINSPECTION TYPE: SI. NR 13 SPOILER PANEL IS DELAMINATED AROUND THE CENTER HINGE FITTING LOWER SURFACE. NR 13 SPOILER TO BE REPLACED ON NRC 498267. WORK PERFORMED IAW MM 27-61-01.Jan 29, 1997 · N910UP · Boeing 72727C · SpoilersSDR UPS97221878Flap Track · corrodedINSPECTION TYPE: SI. CORROSION ON R/W NR 8 FLAP TRACK PITTED AT AFT MAIN AND FAILSAFE BOLT HOLES. FLAP TRACK RECEIVED, BEING INSTALLED ON TC C57-581-04-4 WORK TO BE PERFORMED IAW MM 27-51-31.Jan 29, 1997 · N910UP · Boeing 72727C · Trailing Edge FlapsSDR UPS97221876Skin · delaminatedINSPECTION TYPE: SI. NR 13 SPOILER IS DELAMINATED ON THE UPPER SURFACE AROUND CENTER HINGE FITTING. SPOILER NR 13 BEING REPLACED ON NON-ROUTINE CARD NUMBER 498267. WORK TO BE PERFORMED IAW MM 27-61-01.Jan 29, 1997 · N910UP · Boeing 72727C · SpoilersSDR UPS97222275Bulkhead Web · corrodedINSPECTION TYPE-SI, WHILE WORKING NRC 497869, FOUND CORROSION ON FWD SIDE OF 870 WEB WL 186 LBL 60-65 AT INSPECTION PANEL ACCESS (WHEEL WELL WEB). FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-1, 53-10-9, 51-20-4 AND 51-30-1.Jan 28, 1997 · N910UP · Boeing 72727C · Fuselage Main, BulkheadSDR UPS97222106Spar · corrodedINSPECTION SI-CHECK, BS 870 REAR SPAR SPAN WISE CORRODED. FABRICATED AND INSTALLED REPAIR SPAN WISE IAW SRM 51-10-1, 51-30-2, 51-30-5.Jan 28, 1997 · N910UP · Boeing 72727C · Wing SparSDR UPS97221873Stringer · corrodedINSPECTION TYPE: C. WHILE WORKING 950 SIDE FITTING FOUND STRINGER 9 TO BE CORRODED AT BS 960 RT SIDE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, IAW SRM 51-10-6, 53-10-11, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-3.Jan 26, 1997 · N939UP · Boeing 72727C · Fuselage Main, Longeron/StringerSDR UPS97221850Batteries · dischargedINSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT INOP AT MAIN ENTRY DOOR. REPLACED BATTERIES, OPS CHECKS OK.Jan 25, 1997 · N908UP · Boeing 72727C · Emergency Lighting
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