Boeing 727-173C

Service difficulty reports · 436

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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 = '727173C'
  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 UPS04243186Intercostal · crackedINSPECTION TYPE: C, INTERCOSTAL CRACKED ON TOILET COMPARTMENT FLOOR BS 294.5-312. INTERCOSTAL REMOVED IAW SRM 51-30-02 AND DAMAGE REMOVED IAW SRM 51-40-03. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT6 FIG 4, NO DEFECTS FOUND. INSTALLED REPAIR AND INTERCOSTALSep 7, 2004 · N938UP · Boeing 727173C · Fuselage Miscellaneous StructureSDR UPS04243207Yoke · corrodedINSPECTION TYPE: C, ON REMOVAL OF LT MLG SWING LINK, YOKE OVER SWING LINK FOUND TO HAVE PITTING CORROSION. REPLACED YOKE ASSY IAW MM 32-32-00.Sep 6, 2004 · N938UP · Boeing 727173C · Main Landing Gear Attach SectionSDR UPS04243180Bushing · corrodedINSPECTION TYPE:C, ENGINE NR 1 FWD MOUNT FITTING, REPAIR BUSHINGS IN BOTH O/B HOLES HAVE MIGRATED. REPAIRED IAW UPS EO B727-5440-11592-A.Sep 6, 2004 · N938UP · Boeing 727173C · Engine Mount SectionSDR UPS04243242Lap Joint · corrodedINSPECTION TYPE: C, RIVETS PULLED BETWEEN BS 810-830 STR 4L, CORROSION AT LAP JOINT OUT OF LIMITS IAW SRM 53-30-1. CORRODED SKIN TRIMMED OUT. REPAIR PARTS FABRICATED AND INSTALLED IAW SRM 53-30-1.Sep 5, 2004 · N938UP · Boeing 727173C · Fuselage Main, Plate/SkinSDR UPS04243240Angle · crackedINSPECTION TYPE:C, NR 2 SPOILER ACTUATOR SUPPORT CASTING ANGLE CRACKED AT LOWER INBOARD ATTACH POINT. REPLACED ANGLE IAW SRM 51-30-02. REINSTALLED NR 2 SPOILER ACTUATOR IAW 27-61-81.Sep 3, 2004 · N938UP · Boeing 727173C · SpoilersSDR UPS04243181Panel · delaminatedINSPECTION TYPE: C, LEFT WING UPPER SURFACE T/E PANEL FWD OD MLG BEAM HAS DELAMINATION ON AFT END, ALSO HAS UPPER SURFACE DENTS. REPAIRED AND INSTALLED PANEL AS PER DRAWING 65-21655 IAW SRM 51-30-02.Sep 2, 2004 · N938UP · Boeing 727173C · Wing, Plate/SkinSDR UPS04243241Tab · delaminatedINSPECTION TYPE: C, RIGHT OUTBOARD AILERON TAB DELAMINATED AT OUTBOARD UPPER TRAILING EDGE. AILERON TAB REPLACED IAW MM 27-10-19.Sep 1, 2004 · N938UP · Boeing 727173C · Aileron TabsSDR UPS04243239Spoiler · crackedINSPECTION TYPE: C, NR 14 SPOILER PANEL HAS EVIDENCE OF DELAM AT LOWER I/B CORNER. NR 14 SPOILER PANEL REPLACED IAW MM 27-61-01.Sep 1, 2004 · N938UP · Boeing 727173C · SpoilersSDR UPS04243222Angle · crackedINSPECTION TYPE: C, SUSPECT CRACK ON INTERNAL STRUCTURE OF AFT LOWER CARGO DOOR. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT6 FIG 4, CRACK CONFIRMED ENDS MARKED. REPLACED ANGLE IAW EO B727-5230-0032.Sep 1, 2004 · N938UP · Boeing 727173C · Cargo/Baggage DoorsSDR UPS04243196Bulkhead · crackedINSPECTION TYPE:C, BULGING CORROSION AND CRACKED SKIN FOUND ON BS 870 BULKHEAD RBL 43 APPROX HALF WAY DOWN ON BULKHEAD. DERIVETED REPAIR STRAP ON BULKHEAD IAW SRM 51-30-02. REPAIR FOUND OUT OF LIMITS. DAMAGED SECTION CUT OUT IAW SRM 53-10-09. HFEC CARRIED Aug 31, 2004 · N938UP · Boeing 727173C · Fuselage Main, BulkheadSDR UPS04243174Skin · crackedINSPECTION TYPE:C, RIGHT WING DOOR LOWER SKIN HAS TWO SUSPECT CRACKS IN SKIN AT FWD END MID WAY ON DOOR. WING DOOR REPLACED ON NRC 733172.Aug 31, 2004 · N938UP · Boeing 727173C · Landing Gear DoorsSDR UPS04243244Fitting · crackedINSPECTION TYPE:C, SUSPECT CRACK ON LEFT 950 O/B LUG AFT SIDE. FITTING REPLACED IAW SRM 51-30-02 AND AAAE EO 2004-083-001R1 (727-53- 20161).Aug 29, 2004 · N938UP · Boeing 727173C · Fuselage Main, Attach FittingsSDR UPS04243236Door · crackedINSPECTION TYPE:C, SUSPECT CRACK AT ATTACH LUG OF TAIL SKID DOOR AND STRUT. HFEC CARRIED OUT IAW NDT MANUAL 51-00-00. RESULT - CRACK CONFIRMED. INSTALLED NEW TAIL SKID DOOR IAW MM 32-71-61. TAIL SKID TESTED SATISFACTORY IAW MM 32-71-01.Aug 29, 2004 · N938UP · Boeing 727173C · DoorsSDR UPS04243185Angle · corrodedINSPECTION TYPE:C, ANGLE BRACKET ON LOWER FWD BS 880 CORRODED RT MLG WW. INSTALLED NEW BRACKET IAW SRM 51-30-02.Aug 29, 2004 · N938UP · Boeing 727173C · Fuselage Miscellaneous StructureSDR UPS04242701Carriage · wornATB FL 330 IN CLIMB EXPERIENCED MODERATE VIBRATION. FOUND LEFT OUTBOARD TRAILING FLAP, INBOARD TRACK AFT ROLLER CLEARANCE OUT OF TOLERANCE. REPLACED ROLLER.Jul 9, 2004 · N938UP · Boeing 727173C · Trailing Edge FlapsSDR UPS04242666Carriage · wornAIRFRAME HAS A VIBRATION - ATB. TE FLAP CARRIER HAS EXCESS PLAY.Jul 9, 2004 · N938UP · Boeing 727173C · Trailing Edge FlapsSDR XNOA1178Line · leakingLOSS "A" SYSTEM PRESSURE & QUANTITY. INSTALLED TEMP FLEX LINE IAW B727 MM 20-10-12 & ENA GMM CHAPTER 5, PRESSURE LEAK CK GOOD. TRANSFERRED TO CARRY-OVER ITEM 1388 PLACARD INSTALLED.(STATUS:ORIG/OPEN) R & R TEMP FLEX HOSE FROM NOSE L/G ACTUATOR IAW B727 MM 20-Feb 25, 2004 · N704A · Boeing 727173C · Hydraulic System, MainSDR UPS03241144Battery · inoperativeEMERGENCY EXIT LIGHT OVERHEAD FORWARD ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED BATTERIES FORWARD ENTRY EMERGENCY EXIT LIGHT ASSY. CHECKS NORMAL.Aug 26, 2003 · N938UP · Boeing 727173C · Emergency LightingSDR UPS03240412Bracket · crackedINSPECTION TYPE: C, INTERCOSTAL MOUNT BRACKET BS 1060 CRACKED. FABRICATED NEW BRACKET IAW SRM 51-20-1, REPROTECTED BRACKET IAW SRM 51-10-2, MOUNT BRACKET INSTALLED IAW SRM 51-30-02.Mar 29, 2003 · N938UP · Boeing 727173C · Fuselage Miscellaneous StructureSDR UPS03240411Bracket · crackedINSPECTION TYPE: C, INTERCOSTAL IN AFT FREIGHT HOLD CRACKED BS 1040 BS 1060 (SUPPORTS DOOR HOLD-PEN BRACKET). FABRICATED INTERCOSTAL BRACKET IAW SRM 51-20-1, REPROTECTED BRACKET IAW SRM 51-20-2. INTERCOSTAL INSTALLED IAW SRM 51-30-02.Mar 28, 2003 · N938UP · Boeing 727173C · Fuselage Miscellaneous StructureSDR UPS03240422Skin · corrodedINSPECTION TYPE:C EVIDENCE OF CORROSION AT CIRCUMFERENTIAL JOINT 480 BETWEEN STRINGER 10R AND 14R. REPAIRED IAW UPS REPAIR FILE 727-53-20106.Mar 23, 2003 · N938UP · Boeing 727173C · Fuselage Main, Plate/SkinSDR UPS03240416Skin · corrodedINSPECTION TYPE: C, EVIDENCE OF CORROSION AT CIRCUMFERENTIAL JOINT BS 480 RT BETWEEN ST R10 AND 14 RT. LFEC C/W MATERIAL LOSS INDICATIONS MARKED. PAINT STRIPPED AND FASTENERS REMOVED IAW SRM 51-30-2. DAMAGED AREA CUT OUT, CUTOUT HFEC AND NDF, HOLES HFEC ANMar 23, 2003 · N938UP · Boeing 727173C · Fuselage Main, Plate/SkinSDR 03FDEA00179Switch · failedRED RT GEAR DOOR LIGHT ILLUMINATED ON LANDING GEAR RETRACTION. CREW CYCLED GEAR IAW QRH, LIGHT REMAINED ILLUMINATED FOR DURATION OF FLIGHT. REMOVED AND REPLACED RT MLG DOOR WARNING SWITCH IAW M/M 32-62-011-4 OPERATIONAL CHECK NORMAL.Feb 26, 2003 · N199FE · Boeing 727173C · Landing Gear Position and WarningSDR XNOA01107Engine · stalledON ROTATION NR 2 ENGINE COMPRESSOR STALLED 3 TIMES. REDUCED POWER, ENGINE STABILIZED. FURTHER ADVANCEMENT OF NR 2 THROTTLE SHOWED ALL PARAMETERS NORMAL. PERFORMED VISUAL INSPECTION AND GROUND OPERATIONAL RUN. ALL ENGINE PARAMETERS WITHIN LIMITS. NO DEFECTFeb 25, 2003 · N704A · Boeing 727173C · Turbine Engine Compressor SectionSDR XNOA01087Carbon Seal · leakingNR 2 ENGINE OIL QUANTITY DECREASED IN FLT. REPLACED WORN CARBON SEAL IN ACCESSORY GEARBOX AT FUEL PUMP DRIVE. LEAK & OPS CHECKS GOOD IAW MM 73-11-1.Nov 12, 2002 · N704A · Boeing 727173C · Turbine Engine Oil SystemSDR UPS02238691Light · not seatedINSPECTION TYPE:N/A COCKPIT EMERGENCY LIGHT ILLUMINATED IN ARMED POSITION. RESEAT COCKPIT EMERGENCY EXIT LIGHT, OPS CHECK GOOD.Jun 24, 2002 · N938UP · Boeing 727173C · Emergency LightingSDR UPS03240417Gusset · crackedINSPECTION TYPE: C, SUSPECT CRACK AT 1263 UPPER BEAM AT INNER RADIUS OF FLANGE ADJACENT TO THIRD FASTENER VERT, FROM I/B END, RT TORQUE BOX (GUSSET). HFEC C/W CRACK CONFIRMED AND ENDS MARKED. GUSSET AND ANCILLARY STRUT URE DISPLACED IAW SRM 5130-02. NEW GUMar 26, 2002 · N938UP · Boeing 727173C · Fuselage Main, StructureSDR 02FDEA00182Indicator · faultyA/C W/N PRESSURIZE, APPEARED LEFT PACK NOT SUPPLYING AIR TO A/C. RAN ENGS, PERFORMED AIR COND AND PRESSURIZATION OPS TEST PER JET RUN HDBK CHAPTER 7 & 5A. PRESSURIZED IN AUTO AND MANUAL MODE. BOTH TEST CHECK NORM BOTH PACKS MAINTAIN AIR.Mar 5, 2002 · N199FE · Boeing 727173C · Cabin Pressure IndicatorSDR 01FDEA00909Warning System · malfunctionedLEADING EDGE NR 6 FAILED DURING FLAP RETRACTION. OPERATED FLAPS & SLATS, ALL IND NORMAL PER MM 27-81-000-0.Oct 23, 2001 · N199FE · Boeing 727173C · Leading Edge Slat Position Indicating SystemSDR UPS01237068Skin · crackedINSPECTION TYPE:C NWW PRESS CEILING IS CRACKED AT BS 285, BETWEEN RBL 3 AND RBL 6, CON FIRMED BY NDT. CUT OUT CRACK AT NWW PRESS CEILING RBL 3 APPROX 4"X1" AND AT LBL 6 APPROX 5"X1" IAW B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR AT NWW PRESS CEILING BS 28Sep 21, 2001 · N938UP · Boeing 727173C · Fuselage Main, Plate/SkinSDR UPS01237067Pressure Panel · crackedINSPECTION TYPE:C NWW PRESSURE CEILING IS CRACKED BETWEEN BS 270 - 273 RBL 14, CONFIRMED BY NDT. CUT OUT CRACK APPROX 4 X 1 INCH AT NWW PRESS CEILING BS 270 - 273 RBL 14 IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR ON NWW PRESS CEILING IAW B727 SRM 51-40-2Sep 21, 2001 · N938UP · Boeing 727173C · Fuselage Main, BulkheadSDR UPS01237066Skin · crackedINSPECTION TYPE:C NWW R/H PRESSURE WEB IS CRACKED EXTENDING FROM REPAIR DOUBLER AT BS 277, APPROX 8" FROM BOTOM OF WW, CONFIRMED BY NDT. REMOVED OLD DOUBLER REPAIR IAW B727 SRM 51-40-2. CUT OUT CRACK AT N WW RH PRESSURE WEB BS 277 IAW B727 SRM 51-40-2. ISep 21, 2001 · N938UP · Boeing 727173C · Fuselage Main, Plate/SkinSDR UPS01237065Skin · crackedINSPECTION TYPE:C NWW R/H PRESSURE WEB IS CRACKED BETWEEN BS 260-265, JUST BELOW PANEL #3125, CONFIRMED BY NDT. CUT OUT CRACK AREA AT NWW R/H PERSURE WEB BS 260-365 AS PER B727 SRM 51-40-2 APPROX 2"X1". INSTALLED DOUBLER REPIAR AS PER B727 SRM 51-4 0-2.Sep 21, 2001 · N938UP · Boeing 727173C · Fuselage Main, Plate/SkinSDR UPS01237064Skin · crackedINSPECTION TYPE:C NOSE W/W PRESSURE CEILING IS CRACKED AT BL-0. BETWEEN BS 290-288, CONFIRMED BY NDT. CUT OUT CRACK AT NWW PRESSURE CEILING AT BL-0 STA 303 APPROX 3"X1" IAW B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR ON NWW PRESSURE CEILING IAW B727 SRM 5Sep 21, 2001 · N938UP · Boeing 727173C · Fuselage Main, Plate/SkinSDR UPS01237076Skin · corrodedINSPECTION TYPE:C LEFT NOSE SECTION EXTERIOR FUSELAGE SKIN SHOWS BULGE STR 25L AND BS 300. CUT OUT DAMAGED AREA AT EXTERIOR FUSELAGE SKIN L/H STR 25L BS 300, APROX 10"X3" IAW B727 53-30-3 FIG 3. REMOVED CORROSION ON SKIN STA 310 STR 25L, MATERIAL LOST .00Sep 19, 2001 · N938UP · Boeing 727173C · Fuselage Main, Plate/SkinSDR UPS01237075Splice Plate · crackedINSPECTION TYPE:C RIGHT MAIN W/W CENTER SPLICE PLATE CRACKED AT STR 18A RT. STA 935 STOP DRILLED END OF CRACK IAW B727 SRM 51-10-1. INSTALLED REPAIR IAW EO B727-5330-3815A ON FUSELAGE SKIN BS 935 STR 18A R/H SIDE.Sep 19, 2001 · N938UP · Boeing 727173C · Wing, Attach FittingsSDR UPS01237072Splice Plate · crackedINSPECTION TYPE:C LEFT MAIN WHEEL WELL CENTER SPLICE PLATE, CRACK AT STR 18 ALT BS935 STOP DRILED END OF CRACK IAW B727 SRM 51-10-10, INSTALLED REPAIR STR 18 ALT SIDE FUSELAGE SKIN IAW B727 EO B727-5330-3815A.Sep 19, 2001 · N938UP · Boeing 727173C · Wing, Attach FittingsSDR UPS01237073Beam · crackedINSPECTION TYPE:C NUMBER 3 FUEL TANK CRACK ON L/G SUPPORT BEAM AT WS 304. REPLACED BUSHING RT LANDING GEAR O/B END OF BEAM IAW SB 727-57-167. REMOVED AND REPLACED FWD AND AFT FITTINGS AT WS 304 LEFT GEAR SUPPORT BEAM AS PER B727 SRM 51-10-2. PERFORMED HFEC Sep 15, 2001 · N938UP · Boeing 727173C · Wing, Landing Gear Attach FittingsSDR UPS01235892Outflow Valve · obstructedINSPECTION TYPE:N/A DIVERSION-UNABLE TO PRESSURIZE AIRCRAFT. CLEARED DEBRIS FROM OUTFLOW VALVE.May 15, 2001 · N938UP · Boeing 727173C · Pressure Regulator/Outflow ValveSDR UPS01235615Connector · looseINSPECTION TYPE:N/A ATB-OUTBD FLAPS WOULD NOT MOVE ON INITIAL EXTENSION AT MCI. SECURED CONNECTORPLUG IN RT W/W, OPS CHECK GOODApr 17, 2001 · N938UP · Boeing 727173C · Trailing Edge Flap Control SystemSDR UPS01235272Gyro · failedINSPECTION TYPE:N/A (BTB) DURING TAKEOFF INITIAL ACCELERATION F/O''S EADI BLANKED. REPLACED NR 2 VERT GYRO PER BMM 34-22-21. NOTE: THIS SAME NR 2 VG WAS REPLACED ON INB FLT FOR A 5 DEGREE ROLL. THE S/N REMOVED FROM BTB IS 81144914, THE PIREP DEBRIEF, INDICAMar 13, 2001 · N938UP · Boeing 727173C · Attitude Gyro and Indicating SystemSDR UPS00234227Light · inoperativeINSPECTION TYPE:N/A, COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY.Oct 24, 2000 · N938UP · Boeing 727173C · Emergency LightingSDR UPS00233428Relay · failedINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS IN ARMED POSITION AND CIRCUIT BREAKER POWER FAIL RELAY POPPED, WILL NOT RESET. REMOVED AND REPLACED R70 CHARGER CONTROL RELAY.Jul 28, 2000 · N938UP · Boeing 727173C · Emergency LightingSDR UPS00232595Angle · crackedINSPECTION TYPE:C+SI, LWR FWD CARGO HOLD DOOR CRACK ON SUPPORT ANGLE UNDER BALANCE SPRING SUPPORT BRACKET. ANGLE FABRICATED AND INSTALLED IAW DRAWING NR 65-18620.May 2, 2000 · N938UP · Boeing 727173C · Cargo/Baggage DoorsSDR UPS00232596Support Fitting · corrodedINSPECTION TYPE:C+SI, NR 5 FLAP TRACK FWD SUPPORT FITTING CORRODED. NR 5 FLAP TRACK FWD SUPPORT FITTING REPLACED IAW MM 20-80-01 & DRAWING NR 65-21651.Apr 28, 2000 · N938UP · Boeing 727173C · Trailing Edge Flap Control SystemSDR UPS00232628Beam · corrodedINSPECTION TYPE:C+SI, CORROSION FOUND ON LWR RT BEAM OF DELTA BEAM AT BODY FAIRING SUPPORT LUG. CORROSION REMOVED FROM SUPPORT LUG AND FOUND TO BE OUT OF LIMITS. LUG REMOVED FROM BEAM. ALL CORROSION REMOVED FROM AFFECTED AREA IAW SRM 51-10-6. HFEC INSPECTIApr 27, 2000 · N938UP · Boeing 727173C · Fuselage Miscellaneous StructureSDR UPS00232624Stringer · crackedINSPECTION TYPE:C+SI, SUSPECT CRACK ON STRINGER AT ATTACHMENT POINT TO FRAME AT BS 720 STR 21L IN LWR FWD CARGO HOLD. HFEC INSPECTION CARRIED IAW B727 NDTM PT6 51-00-00 FIG 4. CRACK CONFIRMED. CRACK CONTAINED IAW SRM 51-10-2. HFEC INSPECTION CARRIED OUT IAApr 27, 2000 · N938UP · Boeing 727173C · Fuselage Main, Longeron/StringerSDR UPS00232621Stringer · crackedINSPECTION TYPE:C+SI, CRACK ON STRINGER AT BS 440 AT STR 22L FWD OF CARGO HOLD FWD WALL. REPAIR CARRIED OUT IAW SRM 53-10-3 FIG 2. HFEC INSP CARRIED OUT IAW B727 NDT MANUAL PART 6, 51-00-00 FIG 4. NO DEFECT FOUND POST DAMAGE REMOVAL.Apr 27, 2000 · N938UP · Boeing 727173C · Fuselage Main, StructureSDR UPS00232598Angle · crackedINSPECTION TYPE:C+SI, SUSPECT CRACK ON ANGLE BETWEEN FRAME AND FLOOR AT LWR FWD CARGO DOOR FWD HINGE CUTOUT AT BS 535 STR 17. REPLACEMENT ANGLE FABRICATED AND INSTALLED IAW DRAWING NR 65-16352.Apr 27, 2000 · N938UP · Boeing 727173C · Fuselage Miscellaneous StructureSDR UPS00232597Support Fitting · corrodedINSPECTION TYPE:C+SI, NR 4 FLAP TRACK FWD SUPPPORT FITTING CORRODED. NR 4 FLAP TRACK FWD SUPPORT FITTING REPLACED IAW MM 20-80-01 & DRAWING 65-21651.Apr 27, 2000 · N938UP · Boeing 727173C · Trailing Edge Flap Control System
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