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 UPS00234448Light · inoperativeINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT OVER FWD ENTRY INOP. REPLACED L-1 EMERGENCY LIGHT ASSY, OPS CK NML TAG 189742 REF MM 33-55-101.Nov 14, 2000 · N911UP · Boeing 72727C · Emergency LightingSDR UPS00234445Battery · dischargedINSPECTION TYPE:C, FWD ENTRY DOOR EMERGENCY EXIT LIGHT BATTERIES WEAK. REPLACED BATTERIES, OPS CKS OK.Nov 12, 2000 · N915UP · Boeing 72727C · Emergency LightingSDR UPS00234444Battery · dischargedINSPECTION TYPE:C, COCKPIT EMERGENCY EXIT LIGHT BATTERIES WEAK. REPLACED BATTERIES, OPS CKS OK.Nov 12, 2000 · N915UP · Boeing 72727C · Emergency LightingSDR UPS00234269Light · inoperativeINSPECTION TYPE:N/A, CREW ENTRY DOOR EMERGENCY EXIT DOOR LIGHTS INOP, BATTERIES CHANGED PREVIOUSLY 3 TIMES. LIGHT ASSY REPLACED.Oct 26, 2000 · N914UP · Boeing 72727C · Emergency LightingSDR UPS00234214Light · inoperativeINSPECTION TYPE:N/A, EXIT LIGHT OVER MAIN ENTRY DOOR COMES ON WHEN POWER IS REMOVED FROM AIRCRAFT. REMOVED AND REPLACED EXIT LIGHT ASSY, CKS OK.Oct 19, 2000 · N914UP · Boeing 72727C · Emergency LightingSDR UPS00234212Light · inoperativeINSPECTION TYPE:N/A, FWD ENTRY DOOR EMERGENCY LIGHT WILL NOT EXTINGUISH AUTOMATICALLY AFTER TEST OR SHUTDOWN. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, TESTS GOOD.Oct 19, 2000 · N910UP · Boeing 72727C · Emergency LightingSDR UPS00234211Light · inoperativeINSPECTION TYPE:N/A, ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED 2 BATTERIES FROM LIGHT ASSY. INSTALLED AND TESTED EMERGENCY LIGHTS PER MM 33-30-01, TESTED GOOD.Oct 17, 2000 · N914UP · Boeing 72727C · Emergency LightingSDR UPS00233920Switch · out of adjINSPECTION TYPE:N/A, CREW DECLARED EMERGENCY DUE TO AFT AIRSTAIR LIGHT ILLUMINATED IN FLIGHT. ADJUSTED AND OPS CK AIRSTAIR SWITCH PER MM 52-70-01 & 52-62-01.Oct 10, 2000 · N910UP · Boeing 72727C · Door Warning SystemSDR UPS00233857Light · inoperativeINSPECTION TYPE:N/A FWD ENTRY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES LIGHTS, OPS CK OK.Oct 6, 2000 · N914UP · Boeing 72727C · Emergency LightingSDR UPS00233838Terminal · brokenINSPECTION TYPE:C, EMERGENCY LIGHT AT ENTRY DOOR, LIGHTS WEAK. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY, FOUND BATTERY TERMINAL BROKEN. LIGHT OPS CKS NORMAL. P/N OFF/ON 10-0067-9, S/N OFF 01, S/N ON UP11337.Oct 5, 2000 · N914UP · Boeing 72727C · Emergency LightingSDR UPS00233798Skin · damagedINSPECTION TYPE:C, LEFT WING LEADING EDGE AT WS 171.5 ABOVE NR 3 LEADING EDGE FLAP DAMAGED. INSTALLED SKIN REPAIR FROM WS 171.5 TO 160.0, DOUBLER MATERIAL USED, 2024-T3, 0.080, 8 X 7 INCHES. ANGLE REPAIR INSTALLED MATERIAL USED 7075-T6, 20 TRACK PART NUMBERSep 16, 2000 · N915UP · Boeing 72727C · Leading Edge DevicesSDR UPS00233797Skin · damagedINSPECTION TYPE:C, LEFT WING LEADING EDGE AT WS 251 ABOVE NR 2 LEADING EDGE FLAP IS DAMAGED. INSTALLED DOUBLER REPAIR, MATERIAL 2024-T3,0. 080, 9 X 7 INCHES, FILLER 2024-T3, 0.080, 3.35 X 3.125 INCHES, HEAT SHIELD MATERIAL USED, 2024-T3 0.016, 9.5 X 10.5 INCHSep 16, 2000 · N915UP · Boeing 72727C · Trailing Edge FlapsSDR UPS00233739Structure · corrodedINSPECTION TYPE:N/A, NR 3 L/E FLAP HAS HOLE DUE TO CORROSION. *S/D* REMOVED AND REPLACED NR 3 L/E FLAP ASSY PER MM 27-81-01. OPS NORMAL. (P/N 65-16225 -1) (S/N BN592) ON, (S/N 373) OFFSep 12, 2000 · N911UP · Boeing 72727C · Leading Edge DevicesSDR UPS00233342Window · crackedINSPECTION TYPE:N/A, CAPTAINS L1 WINDOW CRACKED. *S/D* WINDOW REMOVED AND REPLACED PER 727 MM 56-11-11. WINDOW HEAT SYSTEM TESTED OK PER B727 MM 30-41-01.Jul 12, 2000 · N911UP · Boeing 72727C · Flight Compartment WindowsSDR 00FDEA00437Bracket · separatedDURING A ROUTINE INSP, FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE LIGHT BRACKET WAS FND SEPARATED FROM LIGHT. REPAIRED BRACKET ASSY PER IAW SRM 51-30-2.Jul 6, 2000 · N146FE · Boeing 72727C · Passenger/Crew DoorsSDR 00FDEA00436Splice · corrodedDURING ROUTINE INSP, THE CENTER WING AFT UPPER SPAR SPLICE AT BS 870, RBL 70.5 FND CORRODED BEYOND ALLOWED LIMITS. R&R PER IAW SRM 51-30-2.Jul 6, 2000 · N146FE · Boeing 72727C · Wing, Center BoxSDR 00FDEA00432Spoiler · crackedDURING ROUTINE INSPECTION NR 10 SPOILER SKIN FOUND CRACKED AT CENTER MOUNTING LUG. R&R IAW MM 27-61-001-4. RIGGED & OPS CHECKED SPOILER IAW MM 27-61-001-5.Jul 5, 2000 · N146FE · Boeing 72727C · SpoilersSDR 00FDEA00431Fitting · crackedN 349 DURING ROUTINE INSPECTION, BS 870 RT, TERMINAL FITTING FOUND CRACKED AT FWD UPPER FASTENER HOLE AT S-9 RT. R&R PER IAW FEDEX EA 7-5310-50105.Jul 5, 2000 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 00FDEA00430Spoiler · crackedDURING ROUTINE INSPECTION, NR 11 SPOILER PANEL WAS FOUND CRACKED. R&R IAW SRM 51-40-6. RIGGED & OPS CHECK SPOILER IAW MM 27-61-001-5.Jul 5, 2000 · N146FE · Boeing 72727C · SpoilersSDR 00FDEA00429Skin · corrodedN 165 DURING ROUTINE INSPECTION, FUSELAGE SKIN WAS FOUND BULGED BETWEEN STR 24 LT & 27 LT JUST AFT OF BS 1183. R&R IAW SRM 53-30-3.Jul 5, 2000 · N146FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 00FDEA00428Skin · crackedDURING ROUTINE INSPECTION, FUSELAGE SKIN WAS FOUND CRACKED AT STR 1, BS 430. R&R PER IAW SRM 53-30-3 FIG 4.Jul 5, 2000 · N146FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 00FDEA00427Skin · corrodedDURING ROUTINE INSPECTION, CORROSION FOUND ON EXTERNAL FUSELAGE BETWEEN STR 7 RT TO 10 RT FROM BS 1173 - 1183. R&R SKIN BETWEEN STR 3 RT & 10 RT FROM BS 1080 - 1183 IAW BOEING DRAWING 65-18382 & SRM 51-30-2.Jul 5, 2000 · N146FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 00FDEA00426Slide · tornN 45 DURING ROUTINE INSPECTION, FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE GIRT ASSY FOUND FRAYED & TORN. R&R GIRT ASSY IAW SRM 51-40-9.Jul 5, 2000 · N146FE · Boeing 72727C · Escape SlideSDR UPS00233150Battery · dischargedEMERGENCY LIGHT BATTERY DEAD R&R EMERGENCY LIGHT BATTERIES OPERATION CHECKS NORMALJun 29, 2000 · N909UP · Boeing 72727C · Emergency LightingSDR UPS00232915Web · crackedINSPECTION TYPE:C, WHILE WORKING CUSTOMER CARD 134185, FOUND CRACK IN VERTICAL WEB IN CENTER FUEL CELL BS 825, LBL 27, WL 193 FWD SIDE OF WEB. REMOVED VERTICAL WEB FROM LBL 25 FOR ACCESS, REMOVED DAMAGED AREA 3 X 3, FABRICATED REPAIR DOUBLER FOR WEB. INSTALLJun 21, 2000 · N907UP · Boeing 72727C · Fuel StorageSDR UPS00232917Bulkhead · corrodedINSPECTION TYPE:C, WHILE WORKING CUSTOMER NR 134500 FUSELAGE 88 DISCOVERED MAIN WHEEL WELL RT FWD BULKHEAD CORRODED BS 870 RBL 45 - 54. REMOVED CORROSION 5.5 X 8 AREA RBL 45 TO 54 PER SRM 51-10-6. FABRICATED FILLER AND REPAIR PLATE AND SHIMS AND INSTALLED ALJun 14, 2000 · N907UP · Boeing 72727C · Fuselage Main, BulkheadSDR UPS00232881Flap · malfunctionedINSPECTION TYPE:N/A, OUTBOARD FLAPS VERY SLOW TO RETRACT OUT OF CAE WOULD NOT EXTEND PAST 15 DEGREES AT ROA WITH NORMAL HYD FLAPS OPERATED NORMAL INTO CAE. A/C DID NOT LAND AT ROA, AIR TURNBACK TO CAE. REPAIRS IN PROGRESS AT CAE.Jun 13, 2000 · N908UP · Boeing 72727C · Trailing Edge Flap Control SystemSDR CA000614032Engine · smoke(CAN) DURING CLIMBOUT FROM YOW AN ODOR SUSPECTED TO BE OF ENGINE FLUID ORIGIN WAS DETECTED IN THE PAX CABIN ALONG WITH A SLIGHT HAZE. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED THE SOURCE OF THE PROBLEM WAS Jun 12, 2000 · Boeing 72727C · Engine (Turbine/Turboprop)SDR UPS00233237Skin · corrodedINSPECTION TYPE: C, FOUND CORROSION ON LOWER SIDE OF THE UPPER SKIN AT STA 870, RBL 50. REPAIRED IAW ER 00-662.Jun 9, 2000 · N907UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR CA000713005Wheel · damaged(CAN) MAIN WHEEL ASSEMBLY FOUND DAMAGED FROM A BRAKE DRIVE KEY COMING LOOSE.BRAKE ASSEMBLY DAMAGED BY WHEEL DRIVE KEY COMING LOOSE. MAIN WHEELAND BRAKE ASSEMBLY REPLACED AND CHECKS SERVICEABLE.Jun 2, 2000 · Boeing 72727C · Wheel/Ski/FloatSDR UPS00233236Spar · corrodedINSPECTION TYPE: C, CORROSION ON CENTER WING BS 870 REAR SPAR WEB BL 0 - BL 6, WL 160 REPAIRED IAW ER 00-0662Jun 2, 2000 · N907UP · Boeing 72727C · Wing SparSDR UPS00233235Hinge Fitting · corrodedINSPECTION TYPE: C, NR 6 KRUGER FLAP FIXED CENTER LE HINGE FITTING CORRODED AT LE ATTACH POINT. REPLACED FIXED CENTER LE FITTINGJun 2, 2000 · N907UP · Boeing 72727C · Leading Edge DevicesSDR UPS00233234Strap · corrodedINSPECTION TYPE: C, CORROSION BETWEEN BARE STRAP AND FUSELAGE SKIN AFT UPPER MCD BS 632 WL 300 RBL 22-30 REPAIRED IAW ER 00-0665Jun 2, 2000 · N907UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00232943Skin · corrodedINSPECTION TYPE:C, BULGING SKIN AT BS 360 BETWEEN STR 26 LT TO 27 LT ON EXTERNAL SKIN. ACCOMPLISHED REPAIR PER EO B727-5310-1371 APP 8.5 AND DRAWING NR 69-62161.Jun 2, 2000 · N907UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00232610Trunnion · brokenINSPECTION TYPE:C, RT MLG TRUNNION BROKE WHILE AIRCRAFT WAS PARKED. *S/D* RIGHT MAIN GEAR REMOVED AND REPLACED.May 15, 2000 · N911UP · Boeing 72727C · Main Landing Gear Attach SectionSDR UPS00232542Frame · corrodedINSPECTION TYPE:C, RT AFT OVERWING EXIT HATCH HAS CORROSION AT FWD EDGE FRAME AT LOWER STOP PIN 2 INCHES BELOW DATA PLATE. UPON FURTHER INVESTIGATION FOUND AREA TO BE CRACKED APPROX .5 INCH LONG, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED FRAMay 10, 2000 · N911UP · Boeing 72727C · Emergency ExitsSDR UPS00232580Stringer · corrodedINSPECTION TYPE:C, STR 25R BS 730 CORRODED. FOUND WHILE WORKING CUSTOMER CARD NR 150173 FUSE 46. REMOVED AND REPAIRED STRINGER SECTION IAW SRM 53-10-3.May 7, 2000 · N911UP · Boeing 72727C · Fuselage Main, Longeron/StringerSDR UPS00232521Stringer · corrodedINSPECTION TYPE:C, STRINGER 3L AND THE SHIM CRACKED AND CORRODED AT BS 440. REMOVED CORRODED STRINGER FROM BS 430 - 455, FABRICATED REPAIR AND INSTALLED PER SRM 53-10-3, 51-30-2, 51-30-5.May 3, 2000 · N911UP · Boeing 72727C · Fuselage Main, Longeron/StringerSDR UPS00232425Valve · not openedINSPECTION TYPE:N/A, OXYGEN PRESSURE DROPPED TO APPROX 300 PSI AFTER TAKEOFF. AIR TURNBACK TO SAT FOUND OXYGEN BOTTLE CLOSED. OPENED VALVE AND OPS CHECKED IAW MM 35-12-00, OPS CHECKED GOOD.Apr 25, 2000 · N911UP · Boeing 72727C · Crew Oxygen SystemSDR CA000530030Line · ruptured(CAN) NR 2 MAIN WHEEL BRAKE FOUND ON FIRE FOLLOWING ENGINE SHUT DOWN. HYD BRAKE LINE TO NR 1 BRAKE RUPTURED. LINE AND NR 1 AND 2 BRAKE REPLACED.Apr 18, 2000 · Boeing 72727C · BrakeSDR UPS00232253Frame · corrodedINSPECTION TYPE:C WHILE WORKING CARD B727-5310-1371E, FOUND CORROSION ON FRAME AT BS 425 BL 0 WL 146 AROUND E & E BAY DOOR FWD LATCH FITTING. REMOVED CORROSION ON FRAME AT BS 425 IN A AREA 3 X 3 X .040 DEEP ORIG THICKNESS IS .040, FOUND TO BE OUT OF LIMITS IAApr 6, 2000 · N914UP · Boeing 72727C · Fuselage Main, FrameSDR UPS00232188Bulkhead · corrodedINSPECTION TYPE: C, CORROSION ON TOP EDGE OF STA 870 BULKHEAD AT WL 200, LBL 15 - 25 REMOVED CORROSION PER SRM 51-10-6 AND 53-10-1 2X4 INSTALLED FABRICATED DOUBLER AND STIFFNER L) ON BEADED PRESSURE WEB PER SRM 53-10-2, 53-10-9Mar 31, 2000 · N914UP · Boeing 72727C · Fuselage Main, BulkheadSDR UPS00232189Floorbeam · corrodedINSPECTION TYPE: C, CORROSION ON FWD SIDE OF FLOORBEAM AT CARGO DOOR LATCH FITTING 5.0 I/B FROM NR 3 LATCH AT BS 580, WL 207. REMOVED CORROSION ON FWD SIDE OF FLOORBEAM UPPER FLANGE, LOWER SURFACE PER SRM 51-10-6. REMOVED .029X1.0X2.5 FROM ORIGINAL THICKMar 27, 2000 · N914UP · Boeing 72727C · Fuselage Main, Floor BeamSDR UPS00232080Web · corrodedINSPECTION TYPE : C WHILE WORKING CUSTOMER CARD NR 114598 FOUND CORROSION ON WEB, BS 640, LBL 48, WL 208 FABRICATED REPAIR PART AND INSTALLED PER UPS EO NR 727-53-2234Mar 22, 2000 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00232248Skin · corrodedINSPECTION TYPE:C, BULGING SKIN AFT OF BS 740, BETWEEN STR 9L AND 10L. CUT OUT DAMAGED (BULGED) OUTER SKIN PER ER NR 00-0342 AND REPLACED SKIN SEGMENT PER ER NR 00-0342. SRM 51-10-1, SRM 51-10-7, SRM 51-20-1, SRM 53- 30-03, SRM 51-30-02, SRM 51-30-08, SRM 51Mar 18, 2000 · N914UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00232040Frame · corrodedINSPECTION TYPE:C CORROSION ON FRAME UPPER FLANGE AT BS 380 ABOVE STRINGER 20 LT SIDE. REPAIRED FRAME PER SRM 57-40-3.Mar 17, 2000 · N914UP · Boeing 72727C · Fuselage Main, FrameSDR UPS00231999Skin · crackedINSPECTION TYPE:C CRACK ON SKIN LT BS 251..6 FWD ROW WL 216 (END MARKED) IN ADDITION TO CRACK FOUND ALSO NOTED CRACKS AT BS 243.7, WL216 WL 221 AND WL 225 REFERENCE NRC NR'S 114717, 114718, 114719, 114720. ALL CRACKS MENTIONED ABOVE ARE ADDRESSED WITH THIS REMar 15, 2000 · N914UP · Boeing 72727C · Fuselage Main, Plate/SkinSDR UPS00232247Forging · crackedINSPECTION TYPE:C 740 FORGING HAS A CRACK IN HORIZONTAL FLANGE BETWEEN STR 19L AND 3 BELOW STR 20L. REMOVED LEFT HAND 740 FORGING AND INSTALLED NEW PER EO 727-5310-7477 AND DWG 65C13724; SRM ADDENDUM.Mar 6, 2000 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00232251Stiffener · corrodedINSPECTION TYPE:C, CORROSION (C53-100-01.09-02) ON STIFFENER AT BS 880, WL 199 LBL 3. REMOVED, FABRICATED AND INSTALLED STIFFENER PER SRM 51-30-2 AND 51-30-5.Mar 4, 2000 · N914UP · Boeing 72727C · Fuselage Miscellaneous StructureSDR UPS00232250Fitting · corrodedINSPECTION TYPE:C, CORROSION ON NR 2 SPOILER ACTUATOR FITTING AROUND SPOILER PANEL HINGE BOLTS. REPLACED NR 2 SPOILER ACTUATOR FITTING PER MM 27-61-81 AND MM 27-51-131.Mar 3, 2000 · N914UP · Boeing 72727C · Drag Control Actuator
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