Boeing 727-51C

Service difficulty reports · 433

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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 = '72751C'
  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 UPS97222384Angle · corrodedINSPECTION TYPE-C, CORROSION FOUND ON BS 740 LOWER FRAME LOWER CHORD ANGLE BETWEEN S23R AND S24R. LOWER CHORD REPAIR CARRIED OUT IAW UPS MAJOR REPAIR AUTHORIZATION FILE NR 727-53-1875.Mar 8, 1997 · N905UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS97222381Fitting · crackedINSPECTION TYPE-C, REPLACE BS 740 FITTING RT DUE TO CRACKED BEYOND LIMITS. BS 740 RT TERMINAL FITTING REPLACED IAW EO B727-5310-7477 USING KIT NR 65C13724-96.Mar 6, 1997 · N905UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS97222382Door Frame · crackedINSPECTION TYPE-C, CRACKS ON MID GALLEY DOOR FRAME AT FWD UPPER CORNER. MID GALLEY DOOR FRAME SECTION REPLACED PER SRM 51-30-2 AND IN CONJUNCTION WITH EO B727-5330-2639 REF NRC 513079.Mar 5, 1997 · N905UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS97222383Skin · corrodedINSPECTION TYPE-C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL DOUBLER BS 364 BETWEEN S6 AND 7 LT. AREA REPAIRED IAW EO B727-5310-1371 APP 8.5.Mar 4, 1997 · N905UP · Boeing 72751C · Fuselage Main, Plate/SkinSDR UPS97222243Battery · dischargedEMERGENCY EXIT LIGHTS ARE INOPERABLE. REPLACED EMERGENCY EXIT LIGHT BATTERIES. OPS CHECKS GOOD.Mar 4, 1997 · N902UP · Boeing 72751C · Emergency LightingSDR 97ZZZM416Wire · chafedWHEEL WELL FIRE WARNING INFLIGHT. REPAIRED CHAFED WIRE ON FORWARD OUTBOARD ELEMENT CONNECTOR IN LEFT WHEEL WELL. (M)Mar 4, 1997 · N416EX · Boeing 72751C · Fire DetectionSDR UPS97222396Skin · corrodedINSPECTION TYPE-C, SUSPECT CORROSION BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER BS 1090 BETWEEN S14R AND S12R. CORRODED / DISBONDED AREA OF INTERNAL DOUBLER REMOVED. CORRODED AREA OF SKIN REMOVED PER SRM 51-10-6. HFEC CARRIED OUT IAW NDT PT6 51-00 -00 FIGMar 3, 1997 · N905UP · Boeing 72751C · Fuselage Main, Plate/SkinSDR UPS97222393Seat Track · crackedINSPECTION TYPE-C, CRACK ON FLANGE OF SEAT TRACK AT BS 760 RBL 45.5. SEAT TRACK REPLACED IAW SRM 51-30-2.Mar 3, 1997 · N905UP · Boeing 72751C · Fuselage, Seat/Cargo Attach FittingsSDR UPS97222392Floorbeam · corrodedINSPECTION TYPE-C, CORROSION ON UNDERSIDE OF FLOORBEAM STN 930 RBL 55.5. HFEC CARRIED OUT IAW NDT PT6 51-00-00 FIG 4, NO DEFECTS INDICATED. REPAIR CARRIED OUT PER UPS MINOR REPAIR AUTHORIZATION FILE NR 727-53- 1870.Mar 2, 1997 · N905UP · Boeing 72751C · Fuselage Main, Floor BeamSDR UPS97222389Bracket · crackedINSPECTION TYPE-C, 9G NET ATTACH FITTING AT S10L TO S9L FOUND TO BE SEPARATED FROM ATTACH CHANNEL PART NR 69-35276-3. ATTACHMENT BRACKET P/N 66-20231-3 REPLACED IAW MM 25-56-201.Mar 2, 1997 · N905UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS97222386Skin · gougeINSPECTION TYPE-C, GOUGE IN FUSELAGE SKIN BS 515 BETWEEN S21R AND S22R. REPAIR CARRIED OUT IAW UPS MINOR REPAIR AUTHORIZATION FILE NR 727-53 -1868.Mar 1, 1997 · N905UP · Boeing 72751C · Fuselage Main, Plate/SkinSDR UPS97222385Beam · crackedINSPECTION TYPE-C, CRACKS FOUND AT BS 1183 LBL 36.83 VERTICAL BEAM BETWEEN WL 233 AND WL 253. TWO CRACKS 1 INCH LONG EITHER SIDE OF VERTICAL BEAM 'T' ANGLE AT WL 238. REPAIR CARRIED OUT IAW EO B727-5311-0631 APP C.Mar 1, 1997 · N905UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS97222380Hinge · corrodedINSPECTION TYPE-C, FWD AND AFT HINGE HALFS OF MAIN CARGO DOOR ARE CORRODED AND OUTSIDE LIMITS. FWD DOOR HINGE REPLACED IAW OHM 52-36-61. AFT HINGE DRESSED OT AND FOUND WITHIN LIMITS PER OHM 52-36-62.Feb 28, 1997 · N905UP · Boeing 72751C · Cargo/Baggage DoorsSDR UPS97222167Fire Contl Box · inoperativeINSPECTION TYPE-NA, DURING DESCENT FROM 250 TO 240 NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED WITH THROTTLE APPROX ONE-THIRD FORWARD. STRUT OVERHEAT CHEKLIST ACCOMPLISHED, LIGHT REMAINED ILLUMINATED AND NR 1 ENG SHUT DOWN. REMOVED AND REPLACED FIRE DETECTOR CFeb 27, 1997 · N903UP · Boeing 72751C · Fire DetectionSDR UPS97222032Coalascer Bag · dirtyON TAKEOFF, NOTICED A STRONG ODOR. RAN AIRCONDITIONING SMOKE CHECKLIST, ODOR DID NOT DECREASE. RETURNED TO IAD. PERFORMED TAKEOFF POWER CK PER MM 71-00-58. NO ODOR NOTICED, CHANGED WATER SEPARATOR BAGS LT/RT PACK. NO OIL FOUND IN DUCTS, OLD BAGS IN GOOD SFeb 13, 1997 · N904UP · Boeing 72751C · Humidity Control SystemSDR UPS96221744Downlock Switch · inoperativeINSPECTION TYPE-N/A, UNSAFE INDICATION RT MAIN GEAR. MANUAL GEAR EXTENSION CHKLIST ACCOMPLISHED, NO SAFE INDICATION. TOWER FLY-BY FOR POSSIBLE STATUS OF GEAR. DECLARED EMERGENCY REQUESTED CRASH CREWS. REMOVED AND REPLACED RT MAIN GEAR DOWNLOCK SWITCH IAW MDec 11, 1996 · N905UP · Boeing 72751C · Landing Gear Position and WarningSDR UPS96221729Bulb · looseINSPECTION TYPE: EMERGENCY EXIT LIGHT OVER DOOR FLICKERING ON AND OFF WHEN CHECKED. FOUND LAMP LOOSE, TIGHTENED. OPS CHK O.K.Dec 4, 1996 · N903UP · Boeing 72751C · Emergency LightingSDR UPS96221316Act Bracket · crackedINSPECTION TYPE-C, RT WING L/E NR 5 K-FLAP ACTUATOR I/B SUPPORT BRACKET IS CRACKED UNDER MOUNT LUG. FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-1, BOEING DRAWING 65-16269, SRM 51-30-2.Sep 26, 1996 · N902UP · Boeing 72751C · Leading Edge Slat ActuatorSDR UPS96221324Web · crackedINSPECTION TYPE-C, RT AFT LOWER TORQUE BOX I/B WEB AT STA 1218 IS CRACKED. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-42.Sep 25, 1996 · N902UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS96221320Rib · crackedINSPECTION TYPE-C, NR 7 SLAT RIB AT THE I/B SIDE OF ACTUATOR IS CRACKED. REMOVED FASTENERS, STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 57-50-2.Sep 25, 1996 · N902UP · Boeing 72751C · Leading Edge DevicesSDR UPS96221317Rib · crackedINSPECTION TYPE-C, NR 4 SLAT INBOARD TRACK, O/B ATTACH RIB IS CRACKED. REPAIRED RIB PER SRM 51-40-3.Sep 25, 1996 · N902UP · Boeing 72751C · Leading Edge DevicesSDR UPS96221321Attach Rib · crackedINSPECTION TYPE-C, RT WING NR 7 SLAT ACTUATOR ROD END ATTACH O/B RIB IS CRACKED. REMOVED FASTENERS, STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 57-50-2, 51-40-3.Sep 23, 1996 · N902UP · Boeing 72751C · Leading Edge Slat ActuatorSDR UPS96221323Bracket · crackedINSPECTION TYPE-C, ATTACH CLIP CRACKED IN RADIUS AT LT W/W FWD UPPER STR 18A TO 870 FITTING. FABRICATED AND INSTALLED CLIP PER BOEING DRAWING 65-22419 AND SRM 51 -30-2.Sep 22, 1996 · N902UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS96221319Act Bracket · crackedINSPECTION TYPE-C RT WING NR 6 K-FLAP ACTUATOR I/B SUPPORT BRACKET IS CRACKED AT LOWER MOUNT LUG. FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-1, 51-30-1, BOEING DRAWING 65-16275.Sep 22, 1996 · N902UP · Boeing 72751C · Leading Edge Slat ActuatorSDR UPS96221318Act Bracket · crackedINSPECTION TYPE-C, RT WING NR 6 K-FLAP ACTUATOR O/B SUPPORT BRACKET IS CRACKED AT LOWER MOUNT LUG. FABRICATED REPLACEMENT BRACKET AND INSTALLED PER SRM 51-10-1, 51-30- 1, BOEING DRAWING 65-16275.Sep 22, 1996 · N902UP · Boeing 72751C · Leading Edge Slat ActuatorSDR UPS96221322Seat Track · corrodedINSPECTION TYPE-C, RT SEAT TRACK HAS LIGHT SURFACE CORROSION FULL LENGTH OF FWD LOWER CARGO. REPLACED SEAT TRACK PER SRM 51-30-2.Sep 21, 1996 · N902UP · Boeing 72751C · Fuselage, Seat/Cargo Attach FittingsSDR CA970326003Track · cracked(CAN) DURING ROUTINE INSPECTION OF AD 90-07-05, SB 727-57-178R5 TO THE LH INBOARD FLAP AND #4 FLAP TRACK A CRACK WAS FOUND THAT EXTENDED AROUND THE ENTIRE BOLT HOLE. INSPECTION AS PER PART ONE OF SB, TRACK DID NOT HAVE THE REPAIR OR THE PREVENTIVE MODIFICATIONSep 13, 1996 · Boeing 72751C · Trailing Edge FlapsSDR UPS96220737Web · crackedINSPECTION TYPE-C, NLG WHEEL WELL LEFT SIDE WEB IS CRACKED AT FS 251.6. REMOVED, FABRICATED AND INSTALLED WEB PER SRM 51-40-2 AND 51-30-2.Jul 27, 1996 · N904UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS96220741Support Channel · crackedINSPECTION TYPE-C, NR 3 SLAT ACTUATOR SUPPORT CHANNEL BETWEEN I/B AND O/B ACTUATOR. REMOVED, FABRICATED AND INSTALLED CHANNEL PER DWG 65-17294 AND SRM 51-30-2.Jul 26, 1996 · N904UP · Boeing 72751C · Leading Edge Slat ActuatorSDR UPS96220740Actuator Ribs · crackedINSPECTION TYPE-C, NR 3 SLAT INBD AND OTBD ACTUATOR ATTACH RIBS ARE CRACKED. REMOVED, FABRICATED AND INSTALLED RIBS PER SRM 57-50-2, 51-30-2 AND BOEING DWG 65-17240.Jul 26, 1996 · N904UP · Boeing 72751C · Leading Edge Slat ActuatorSDR UPS96220739Skin · crackedINSPECTION TYPE-C, MAIN CABIN FS 850 TO 870 BL 0 TO LBL 45 CENTER TANK UPPER PRESSURE SKIN HAS CORROSION. REMOVED AND AREA NOTED WAS SUBMITTED TO ENG FOR REPAIR. FLAP PEENING DAMAGE AREA PER DHC SK 904-400-AND BOEING M/M 20-10-3. ALODINE AND PRIMED STRUCTURJul 26, 1996 · N904UP · Boeing 72751C · Fuselage Main, Plate/SkinSDR UPS96220743Seat Track · crackedINSPECTION TYPE-C, SEAT TRACK AT BS 740 TO 760 LBL 44.5 IS CORRODED AND CRACKED. REMOVED AND REPAIRED TRACK PER SRM 51-30-2.Jul 25, 1996 · N904UP · Boeing 72751C · Fuselage, Seat/Cargo Attach FittingsSDR UPS96220738K-Flap · crackedINSPECTION TYPE-C, NR 1 K-FLAP 6 INCHES O/B OF I/B HINGE, WEB L/E INSIDE HAS A 3 INCH CRACK. REMOVED, FABRICATED REPLACEMENT PART AND INSTALLED IAW 57-10-2 AND 51-30-2.Jul 22, 1996 · N904UP · Boeing 72751C · Leading Edge DevicesSDR UPS96220736Inner Web · crackedINSPECTION TYPE-C, NR 3 SLAT INNER WEB AT ACTUATOR CRACKED ON BOTH SIDES. STOP DRILLED CRACKS PER SRM 51-10-1, FABRICATED AND INSTALLED WEB REPAIR PER SRM 51-40-3 AND 57-50-1.Jul 20, 1996 · N904UP · Boeing 72751C · Leading Edge DevicesSDR UPS96220742Web · crackedINSPECTION TYPE-C, THE RT LWR TORQUE BOX I/B WEB AT STA 1263 TO 1270 HAS 4 CRACKS AT RIVET HOLE AND 3 CRACKS PAST STOOP DRILLS. REPAIRED I/B TORQUE BOX WEB AND INSTALLED THE 65-17510-313 AND 65-175 10-314.Jul 17, 1996 · N904UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS96220617Swtch · defectiveWHEN GEAR LOWERED FOR LANDING, RIGHT MAIN GREEN LIGHT DID NOT ILLUMINATE, WARNING HORN SOUNDED WHEN FLAPS SELECTED TO 30 DEGREES. RECYCLED GEAR PER AMO PROCEDURE. NO CHANGE. ACCOMPLISHED ALTERNATE EXTENSION PROCEDURE, REMOVED AND REPLACED GEAR GREEN LIGHT SJul 16, 1996 · N904UP · Boeing 72751C · Landing Gear Position and WarningSDR UPS96220599Connector · chafedINSPECTION TYPE N/A, ENG 3 STRUT OVERHEAT LIGHT CAME ON JUST PRIOR TO LANDING. EXTINGUISHED AFTER ENGINE WAS SHUT DOWN. ENGINE SHUTDOWN DURING LANDING ROLL. *S/D* REPAIRED CHAFED WIRE AT FIRE WALL. REMOVED AND REPLACED CONNECTOR ON START STRUT, CONNECTOR Jul 10, 1996 · N904UP · Boeing 72751C · Overheat DetectionSDR UPS96220502Attach Angle · crackedINSPECTION TYPE: C. LT WING FROM SPAR VERTICAL STIFFENER/RIB ATTACH ANGLE IS CRACKED AT RT SLAT O/B TRACK I/B ROLLER MOUNTING RIB. REMOVED, FABRICATED, AND INSTALLED NEW STIFFENER IAW DWG 65-16200 AND SRM 51-30-2 AND 57-10-3.Jun 22, 1996 · N903UP · Boeing 72751C · Leading Edge DevicesSDR UPS96220501Floor Beam · corrodedINSPECTION TYPE: C. CORROSION ON FLOOR BEAM UPPER CAP, STA 344, BL ZERO TO LBL 30. REMOVED CORRODED STA 344 FLOOR BEAM UPPERCAP FROM RBL 8 TO LBL 66 AND REPAIRED FLOOR BEAM IAW SRM 53-10-8, FIG 9.Jun 22, 1996 · N903UP · Boeing 72751C · Fuselage Main, Floor BeamSDR UPS96220506Skin · corrodedINSPECTION TYPE: C. CENTER WING SKIN RT AFT CORNER ADJACENT TO STA 870 SEAL DEPRESSOR HAD CORROSION. REPAIRED AREA IAW DHC SK 903-060 AN DSRM 57-00-00.Jun 21, 1996 · N903UP · Boeing 72751C · Wing, Plate/SkinSDR UPS96220497Rod Fitting · corrodedINSPECTION TYPE: C. RT O/B AILERON BUSS ROD FITTING ON AILERON L/E IS CRACKED. INSTALLED REPLACEMENT FITTING IAW SRM 51-30-2.Jun 21, 1996 · N903UP · Boeing 72751C · AileronsSDR UPS96220493Shear Web · corrodedINSPECTION TYPE: C. MAIN CABIN EXFOLIATED CORROSION ON SHEAR WEB STA 1174-1180, RBL 25. CUT OUT DAMAGED AREA AND REPAIRED WEB PER SRM 51-40-2.Jun 20, 1996 · N903UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS96220492Frame · corrodedINSPECTION TYPE: C. FS 351 BETWEEN STR 26R AND 26L FRAME LOWER TEE WAS FOUND TO BE BEYOND LIMITS. AFTER CORROSION REMOVAL ON NR 571011. REMOVED AND REPLACED LOWER TEE FRAME AT STA 351 BETWEEN STR 26R AND 26L PER SRM 57-30-02.Jun 18, 1996 · N903UP · Boeing 72751C · Fuselage Main, FrameSDR UPS96220491Skin · corrodedINSPECTION TYPE: C. RT WING NR 6 K-FLAP IS CORRODED BEYOND ALLOWABLE LIMITS, L/E STA 286.667. REMOVED CORROSION FOUND BEYOND LIMITS. REPAIR IAW 57-50-03.Jun 18, 1996 · N903UP · Boeing 72751C · Leading Edge DevicesSDR UPS96220489Seat Track · corrodedINSPECTION TYPE: C. STA 1130-1136, RBL 62 SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK PER SRM 51-10-01 AND 51-30-02.Jun 18, 1996 · N903UP · Boeing 72751C · Fuselage, Seat/Cargo Attach FittingsSDR UPS96220505Seat Track · corrodedINSPECTION TYPE: C. CORROSION ON SEAT TRACK IN 3 AREAS THAT ARE OUT OF LIMITS AT STR 378, LBL 45.5. REMOVED AND REPLACED SEAT TRACK FROM STA 344-390 IAW SRM 53-10-5 AND 51-30-2.Jun 17, 1996 · N903UP · Boeing 72751C · Fuselage, Seat/Cargo Attach FittingsSDR UPS96220503Seat Track · corrodedINSPECTION TYPE: C. MAIN CABIN SEAT TRACK STA 552, RBL 62 TRACK WAS FOUND BEYOND LIMITS DUE TO CORROSION REMOVAL. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION IAW SRM 53-10-5 FIG 1 AND 51-30-2.Jun 17, 1996 · N903UP · Boeing 72751C · Fuselage, Seat/Cargo Attach FittingsSDR UPS96220504Attach Rib · crackedINSPECTION TYPE: C. NR 4 SLAT O/B ACTUATOR ATTACH RIB CRACKED IN THREE PLACES. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 51-40-2 AND SRM 51-30-2.Jun 14, 1996 · N903UP · Boeing 72751C · Leading Edge DevicesSDR UPS96220500Door Frame Clip · crackedINSPECTION TYPE: C. MCD STA 540, UPPER END AT SBL, THE BELT FRAME TO DOOR FRAME CLIP IS CRACKED. REMOVED, FABRICATED, AND INSTALLED CLIP PER DWG 69-24114 AND 51-30-2.Jun 14, 1996 · N903UP · Boeing 72751C · Fuselage Miscellaneous StructureSDR UPS96220499Door Frame Clip · crackedINSPECTION TYPE: C. MAIN CARGO DOOR AT STA 550 UPPER END STR 3L. FRAME TO DOOR FRAME CLIP IS CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-30-2 AND 51-10-1.Jun 14, 1996 · N903UP · Boeing 72751C · Fuselage Miscellaneous Structure
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