Boeing 727-25C

Service difficulty reports · 2,007

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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 = '72725C'
  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 97FDEA00434Spar Chord · corrodedNR 0145 002 CORROSION (C53-132-02-1/2) ON 870 UPPER CENTER WING SPAR CHORD, VERTICAL FLANGE, RBL 16 TO RBL 24. REPLACED BS 870 UPPER CHORD PER BCE DRAWING 65C2153. REPAIRED CORROSION ON UPPER SKIN OF CENTER FUEL TANK BS 870 TO BS 843, RBL 70.5 TO RBL 37 PER Jun 30, 1997 · N128FE · Boeing 72725C · Wing SparSDR 97FDEA00433Angle · corrodedEXFOLIATION CORROSION ON BS 879 FORGING SPLICE ANGLE AT STRINGER 9 LT FORWARD SIDE. *S/D* REMOVED .020 CORROSION IN A 2 BY 2 AREA FROM BS 870 FORGING SPLICE ANGLE AT STR 9 LT. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED FORGING SPLICE AJun 26, 1997 · N128FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS97223218Light · inoperativeINSPECTION TYPE:N/A, EMERG EXIT LIGHT IN MID GALLEY AFT LIGHT INOP. REMOVED AND REPLACED GALLEY AREA EMERG LIGHT OPS CHECK GOOD. THIS CLEARS DEFERRAL D131757.May 30, 1997 · N951UP · Boeing 72725C · Emergency LightingSDR UPS97223188Battery Pack · dischargedINSPECTION TYPE:SP, FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-00 AND DWG 727-33A006.May 29, 1997 · N949UP · Boeing 72725C · Emergency LightingSDR UPS97223187Light · inoperativeINSPECTION TYPE:SP, COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-00 AND DWG 727-33A-006.May 29, 1997 · N949UP · Boeing 72725C · Emergency LightingSDR UPS97222895Lght · inoperativeINSPECTION TYPE-N/A, AFT LOWER EXIT LIGHT INOP AT ROW NR 13 LT SIDE. REPLACED BATTERY PACK AND OPS CKD NORMAL.May 9, 1997 · N950UP · Boeing 72725C · Emergency LightingSDR UPS97222567Battery · dischargedINSPECTION TYPE P/F, EMERGENCY LIGHTS DID NOT COME ON WHEN TESTED AT COCKPIT DOOR. REPLACED BATTERIES ON EMERGENCY BAT PACK LIGHT (S/N 39810).Apr 11, 1997 · N933UP · Boeing 72725C · Emergency LightingSDR UPS97222430Light · inoperativeRIGHT FWD OVERWING EMER EXIT LIGHT INOP. SYS OPERATES NORMALLY THIS CLEARS M1277128. PLACARD REMOVED.Mar 26, 1997 · N946UP · Boeing 72725C · Emergency LightingSDR UPS97222431Light · inoperativeINSPECTION TYPE-N/A, EMERG LIGHT ASSY 6 AT ROW 11 HAS 1 LIGHT INOP (AFT BULB). RESEATED BATTERY PACK AND LIGHT BULB LT PACK, OPS CK GOOD.Mar 25, 1997 · N946UP · Boeing 72725C · Emergency LightingSDR UPS97222409Oxy Masks · deployedINSPECTION TYPE-N/A, ALL PAX O2 MASKS DEPLOYED REPACKED ALL O2 MASKS AS REQUIRED IAW 35-20-00 DUE TO INADVERTANT DEPLOYMENT, NO OTHER DEFECTS NOTED.Mar 23, 1997 · N947UP · Boeing 72725C · Passenger Oxygen SystemSDR UPS97222374Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY LIGHT SYSTEM FAILED TEST, BATTERY PACKS DISCHARGED. REPLACED BATTERY PACKS AS DIRECTED BY UPS ENGINEERING AND ESTEL SYS REFERENCE TASK CARD 1300. FOLLOWING PART NUMBERS CHANGED: 96-2-1015 (25 EA), 96-2-1033 (4 EA), 96-2-1019 (2Mar 13, 1997 · N946UP · Boeing 72725C · Emergency LightingSDR UPS97222378Battery Pack · dischargedINSPECTION TYPE-IN, EMERGENCY LIGHT SYSTEM FAILED TEST, BATTERY PACKS DISCHARGED. REPLACED BATTERY PACKS AS DIRECTED BY UPS A/C ENGINEERING. REMOVED AND REPLACED BATTERY PACKS AS DIRECTED BY UPS A/C ENGINEERING AND ESTEL SYSTEMS. REF TC 1300 25 EA 96-2-1015Mar 11, 1997 · N946UP · Boeing 72725C · Emergency LightingSDR UPS97222323Light · inoperativeINSPECTION TYPE: MOD COCKPIT EMERGENCY. ENTRANCE LIGHT INOP. REPLACED ALL 3 CONTROL MODULES EMERGENCY LIGHTS. OPS CHECKED GOOD IAW PEMC DRAWING 015-00357.Mar 9, 1997 · N947UP · Boeing 72725C · Emergency LightingSDR UPS97222304Pack · malfunctionedAT DEPARTURE, HEARD A LOUD BOOM. ALL COCKPIT INDICATIONS NORMAL. OPENED COCKPIT DOOR, FOUND CARGO COMPARTMENT FULL OF SMOKE. DI NUMBER 125957. INSPECTED PACK SYSTEM FOR OPERATION AND OIL LEAKS, NONE FOUND. OPERATED LT PACK IAW MM21-00-00, NO FAULTS OR EVIMar 8, 1997 · N932UP · Boeing 72725C · Cabin Cooling SystemSDR UPS97222180Light · inoperativeROW 6 EMER LIGHT BROKEN. REMOVED AND REPLACED THE ROW 6 EMERGENCY FLOOR PROXIMITY LIGHT PER M/M 33-50-71. SYSTEM OPS CHECKS NORMAL PER M/M 33-50-71.Mar 2, 1997 · N946UP · Boeing 72725C · Emergency LightingSDR 97FDEA00132Door Light · illuminatedRIGHT MAIN LANDING GEAR DOOR LIGHT ILLUMINATED, RED DOOR AND ON DOORS PANEL, GEAR UP OR DOWN. RECYCLED GEAR BUT DID NOT CORRECT. RIGHT MAIN LANDING GEAR LIGHT NOT ILLUMINATED ON GROUND IN ROC. LEFT MAIN LANDING GEAR DOOR LIGHT ON AND RIGHT MAIN LANDING GEARFeb 28, 1997 · N116FE · Boeing 72725C · Landing Gear Position and WarningSDR UPS97222201Accessory Unit · malfunctionedON GEAR EXTENSION, THE NOSE GEAR DOWN AND LOCKED GREEN LIGHT DID NOT ILLUMINATE. RECYCLED GEAR AND CHECKED LIGHTS AND C/B'S. THE PROBLEM STILL EXISTS. ACCOMPLISHED PROCEDURES AND CONFIRMED NOSE WHEEL RED STRIPES WERE ALIGNED AND LANDED. DID NOTICE ACRID SMFeb 26, 1997 · N948UP · Boeing 72725C · Landing Gear Position and WarningSDR UPS97222264Angle · corrodedINSPECTION TYPE-D, LT FLOOR SUPPORT ANGLE TO AFT BLKD IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED REPLACEMENT ANGLE AND INSTALLED IAW SRM 53-7-1 AND SRM 51-1-20.Feb 19, 1997 · N948UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS97222077Wire · chafedINSPECTION TYPE-N/A, CLIMB POWER 250 KTS ENG NR 2 OVERHEAT LT ON INFLIGHT 10,000 FT. ALL OTHER INDICATIONS NORMAL, ENGINE NR 2 SHUTDOWN PER CHECKLIST PROCEDURES. RETURNED AND LANDED MEM. UNEVENTFUL PREVIOUS FLIGHT BUT DIFFERENT CREW, SAME PROBLEM. PERFORMEFeb 14, 1997 · N937UP · Boeing 72725C · Overheat DetectionSDR UPS97222053Wire · chafedINSPECTION TYPE-N/A, CLIMB POWER 250 KTS ENG 2 OVERHEAT LIGHT ON INFLIGHT 10,000 FT. ALL OTHER INDICATIONS NORMAL, ENG 2 SHUTDOWN PER CHECKLIST PROCEDURES. PERFORMED ENG OVERHEAT WARNING T/S PER MM 75-41-00, NO DEFECTS NOTED. FOUND WIRE W9281-E9201-20 CHAFIFeb 14, 1997 · N937UP · Boeing 72725C · Engine Indicating System WiringSDR UPS97221855Light · inoperativeINSPECTION TYPE: P/D. ON PREDEPARTURE CK FOUND ENTRY DOOR EMERGENCY EXIT LIGHT NOT WORKING FROM ARM SWITCH, BUT WORKS FROM SWITCH ON LIGHT ASSY ITSELF. REMOVED AND REPLACED ENTRY DOOR EMER EXIT LIGHT ASSY IAW MM 33-50-00 EMER EXIT LIGHTS. OPS CK NORMAL. Jan 28, 1997 · N937UP · Boeing 72725C · Emergency LightingSDR UPS97222398Floorbeam · corrodedINSPECTION TYPE-MOD, STA 560 RBL 55, I/G CORROSION ON TOP OF FLOORBEAM. REPAIRED IAW SRM 53-10-8.Jan 17, 1997 · N949UP · Boeing 72725C · Fuselage Main, Floor BeamSDR 97FDEA00050Door Mechanism · not latchedAIRCRAFT WOULD NOT HOLD PRESSURE ABOVE 2,000 FT GROUND LEVEL. PRESSURIZATION WOULD RESPOND IN MANUAL BUT ONLY TO 10,000 CABIN PRESSURE. THEN EVEN IN FULL MANUAL INCREASE CABIN WOULD CLIMB AT 1,500 TO 1,800 FT PER MINIMUM RATE OF CLIMB. FORWARD ENTRY DOOR WAJan 17, 1997 · N118FE · Boeing 72725C · Passenger/Crew DoorsSDR UPS97221820Light · inoperativeINSPECTION TYPE-N/A, ONE EMERGENCY EXIT LIGHT DOES NOT WORK. REMOVED AND REPLACED LIGHT ASSY, CKS OK.Jan 14, 1997 · N951UP · Boeing 72725C · Emergency LightingSDR UPS97221811Light · inoperativeINSPECTION TYPE-N/A, WITH THE EMERGENCY LIGHTS SWITCH ON P5 IN THE OFF POSITION AND NO ESSENTIAL POWER, COCKPIT DOOR EMERGENCY LIGHT COMES ON. CAN BE TURNED OFF BY SELECTING LIGHT ASSY SWITCH TO ON AND BACK TO ARM. COCKPIT DOOR EMERGENCY LIGHT ASSY REMOVED AJan 10, 1997 · N951UP · Boeing 72725C · Emergency LightingSDR 97FDEA00017Drage Brace · crackedNOSE GEAR DRAG BRACE SHELF CRACKED LT AFT LOWER CORNER. REMOVED AND REPLACED NLG DRAG BRACE SHELF PER S/B 727-53-108 AND SRM 51-10-1.Dec 23, 1996 · N117FE · Boeing 72725C · Nose/Tail Landing GearSDR 97FDEA00016Pin Casting · crackedRT WING, THE FWD TERMINAL PIN CASTING AT STA 740 IS CRACKED IN INSIDE BORE ON I/B LWR SIDE OF BORE. REMOVED AND REPLACED THE RT WING FWD WING TO FUSE TERMINAL PIN CASTING AT STA 740 IAW EA 7-5710-28934, EA 7-5710-28952, BOEING DWG NR 62C29064, BOEING DEG 65-1Dec 23, 1996 · N117FE · Boeing 72725C · Wing Miscellaneous StructureSDR UPS96221787Downlock Switch · inoperativeUNSAFE NOSE GEAR LIGHT INDICATION ON GEAR EXTENSION. STRIPS WERE ALIGNED IN NOSE WHEELWELL. NOSE GEAR MANUAL EXTENSION PERFORMED. EMERGENCY DECLARED AND NORMAL LANDING FOLLOWED. REMOVED AND REPLACED DOWNLOCK SWITCH PER 727 MM 32-61-21. PERFORMED NOSE GEARDec 21, 1996 · N951UP · Boeing 72725C · Landing Gear Position and WarningSDR UPS96221786Lights · inoperativeINSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT IN COCKPIT INOP. REPLACED BATTERIES, OPS CHKS GOOD.Dec 17, 1996 · N951UP · Boeing 72725C · Emergency LightingSDR 96FDEA01701Spar Web · mis-manufacturedNR 1663 RT WING, FRONT SPAR WEB MILLED BEYOND DRAWING 65C29064 SPECIFICATIONS. FABRICATED NEW SPLICES AND INSTALLED SPICES PER EA 7-5710-28952DATED 12/10/96 AND ACCOMPLISHED REMAINING EA 7-5710-28952 DTD 12/10/96 INSTRUCTIONS.Dec 11, 1996 · N117FE · Boeing 72725C · Wing SparSDR 96FDEA01700Skin · oversized holeNR 1653 STRINGER 9L FASTENER HOLE IN FUSELAGE SKIN IS OVERSIZED AT STA 870 WING TO FUSE TERMINAL PIN CASTING. INSTALLED FREEZE PLUG AND DOUBLER PER EA 7-5330-28947A.Dec 11, 1996 · N117FE · Boeing 72725C · Fuselage Main, Plate/SkinSDR UPS96221747Stiffener · corrodedINSPECTION TYPE-C, CENTER WING FRONT LWR SPAR STIFFENER LBL 42 HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW DWG 65-16281 AND SRM 51-30-2.Nov 22, 1996 · N947UP · Boeing 72725C · Wing Miscellaneous StructureSDR UPS96221746Strut Fitting · corrodedINSPECTION TYPE-C, RT SIDE FUSELAGE TO WING STRUT FITTING, WBL 40 RT FWD LWR SPAR CHORD IS HEAVILY CORRODED. REMOVED, FABRICATED AND INSTALLED STRUT FITTING IAW DWG 65-21799 AND SRM 51-30-2.Nov 22, 1996 · N947UP · Boeing 72725C · Wing Miscellaneous StructureSDR UPS96221696Shear Tie · corrodedINSPECTION TYPE-C, SHEAR TIE AT STA 351.2, STR 22R WAS FOUND TO BE CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION OF SHEAR TIE AT BS 351.2, STR 22R, FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-2 AND 51-40-3.Nov 22, 1996 · N947UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96221748Spar Chord · corrodedINSPECTION TYPE-C, CENTER WING TANK FWD LOWER SPAR CHORD SEVERELY CORRODED FROM LBL 26 TO LBL 40 REF N/R 588971. REMOVED AND REPLACED SPAR CHORD IAW SRM 51-30-2, 51-30-10, 51-30-1.Nov 19, 1996 · N947UP · Boeing 72725C · Wing SparSDR FDEA01673Floorbeam · corrodedCORROSION ON VERTICAL WEB OF BS 640 FLOORBEAM RBL 52 THROUGH RBL 61 AFT SIDE UNDER TOP CHORD. REMOVED CORROSION FROM VERTICAL WEB OF BS 640 FLOORBEAM RBL 52 THROUGH RBL 61. AFT SIDE FABRICATED, REPAIR DOUBLER FOR BS 640 FLOORBEAM VERTICAL WEB 17 RBL 52 TO RBNov 15, 1996 · N117FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 96FDEA01680Floorbeam · corrodedCORROSION ON UPPER FLANG OF FLOORBEAM STA 312 LBL 4. CUT OUT CORROSION ALONG WITH CORROSION AND DAMAGE FROM NR 0708 AND NR 1434 OF INST DOUBLER PER SRM 53-10-8 FIG 7 FROM LBL 29 TO RBL 9.Nov 15, 1996 · N117FE · Boeing 72725C · Fuselage Main, Floor BeamSDR 96FDEA01679Fitting · crackedUPPER LOBE; END FITTING CRACK FWD OF STA 870 STR 2R. REMOVED AND REPLACED STR 2R END FITTING FWD OF STA 870 PER 51-10-1 SRM.Nov 14, 1996 · N117FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA01678Rib · crackedHORZ STAB RT SIDE RIB CRACKED, FWD UPPER CHORD, I/B SIDE STA 17.20. REMOVED AND REPLACED CHORD RIB PER EA 7-5510-20214.Nov 14, 1996 · N117FE · Boeing 72725C · Horizontal Stabilizer, Spar/RibSDR 96FDEA01672Floorbeam · corrodedMAIN CARGO FLOORBEAM STA 640 RBL 45 TO 60 HAS CORROSION AND PREVIOUS REPAIR DOES NOT COVER DAMAGE AREA. REMOVED TOP CHORD OF BS 640 FLOORBEAM FROM RBL 19 TO RT OUTBOARD SKIN, FABRICATED NEW TOP CHORD AND REPAIR ANGLES AND STRAPS PER SRM 53-10-8 FIG 5.Nov 14, 1996 · N117FE · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS96221691Frame · crackedINSPECTION TYPE-C, AFT PIT BS 1050 APPROX RBL 3, THE FRAME APPEARS CRACKED IN THE RADIUS OF THE UPPER FLANGE. CUT OUT DAMAGED AREA AS REQUIRED, FABRICATED PARTS AND INSTALLED IAW SRM 51-40-3.Nov 12, 1996 · N947UP · Boeing 72725C · Fuselage Main, FrameSDR 96FDEA01669Floorbeam · corrosionMAIN CARGO COMPARTMENT STA 580 FLOORBEAM RBL 45 FROM C/L, UPPER CHORD OF BEAM CORRODED AFT SIDE AT FASTENERS ON FLOORBEAM. CORROSION REMOVED, THICKNESS LESS THAN ALLOWABLE LIMITS AFTER REPAIR. INSTALLED STRAP PER AARD 53-10-07-2 FIGURE 1. REPAIR INSTALLED ANov 5, 1996 · N117FE · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS96221541Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION ON STA 344 FLOORBEAM UPPER CHORD LBL 55 TO RBL 45 WL 207. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED UPPER CHORD, FABRICATED NEW UPPER CHORD AND INSTALLED UPPER CHORD. ALL WORK DONE IAW SRM 53-10-1, 51-10-1, 51-30-2,Nov 4, 1996 · N932UP · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS96221545Floorbeam · corrodedINSPECTION TYPE-SI, CORROSION STA 1030 FLOORBEAM LBL 5 TO 61 AND RBL 5 TO 30 FWD AFT FLANGES RBL 48 TO 55 FWD FLANGE WL 208 AT NUTPLATE HOLES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-1, REPAIRED PER EO 96-2563.Nov 3, 1996 · N932UP · Boeing 72725C · Fuselage Main, Floor BeamSDR 96FDEA01676Floorbeam · corrodedUPPER LOBE FLOORBEAM HAS CORROSION STA 400 RBL 27 TO RBL 35. INSTALLED REPAIR STRAP TO FLOORBEAM PER SRM 53-10-8.Nov 3, 1996 · N117FE · Boeing 72725C · Fuselage Main, Floor BeamSDR UPS96221695Chord · crackedINSPECTION TYPE-C, VERTICAL STAB RT LOWER TORQUE BOX CHORD CORRODED AND CRACKED. REMOVED DAMAGED SECTION OF CHORD, FABRICATED AND INSTALLED REPAIR PARTS IAW DHC SK947-123 AND SRM 51-30-2 REF ENGINEERING FLIE NR 727-55-0338.Nov 2, 1996 · N947UP · Boeing 72725C · Vertical StabilizerSDR UPS96221546Expansion Link · corrodedINSPECTION TYPE-SI, EXPANSION LINKS ARE CORRODED AT BS 740 WL 162.5 LBL 36 RBL 12. REMOVED CORRODED LINKS WHICH WERE FOUND TO BE OUT OF LIMITS, INSTALLED NEW EXPANSION LINKS IAW SRM 51-10-1, 51-30-2.Nov 1, 1996 · N932UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA01677Fitting · crackedSTR 4R END FITTING CRACKED AT STATION 870 FWD SIDE. REMOVED AND REPLACED STR END FITTING PER 51-10-01.Nov 1, 1996 · N117FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96221547Stiffener · corrodedINSPECTION TYPE-SI, CORROSION ON STIFFENER BS 219.8 LBL 15 WL 165. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED STIFFENER PER SRM 51-30-2.Oct 31, 1996 · N932UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96221544Stringer · corrodedINSPECTION TYPE-SI, CORROSION ON STRINGER AND SPLICE STR 24R 435 TO 475. REMOVED CORROSION ON STRINGER AND SPLICE, FOUND TO BE OUT OF LIMITS. REMOVED OLD STR 24R BS 435 TO 475, INSTALLED NEW STR AND SPLICE ALL WORK DONE IAW SRM 53-10-2, 53-10-3, 51-30-2, 51-Oct 31, 1996 · N932UP · Boeing 72725C · Fuselage Main, Longeron/Stringer
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