N10791, cancelled Dec 5, 2001

Service difficulty reports · 78

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N10791' AND deregistration_id = 'N10791-2001-12-05'
  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 CALA9901477Light · inopINSPECTION FOUND INTERIOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 22. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.Nov 8, 1999 · N10791 · Boeing 727232 · Emergency LightingSDR CALA9901073Floorbeam · corrodedINSPECTION FOUND MAIN DECK FLOORBEAM IN AFT CARGO COMPARTMENT CORRODED AT STA 1130 FROM BL 0 TO RBL 30. REPAIRED IAW SRM 53-10-8 AND ECRA 5310-03898.Aug 19, 1999 · N10791 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9900621Accessory Unit · inoperativeWHEN GEAR WAS RETRACTED AFTER DEPARTURE A LOUD THUMP WAS HEARD WHEN NOSE GEAR RETRACTED. A LIGHT TEST WAS DONE AND THE NOSE GEAR GREEN LIGHT DID NOT COME ON. PRESS TO TEST AND NEW BULBS HAD NO EFFECT. FLIGHT MANUAL PROCEDURE WAS ACCOMPLISHED. THE LIGHT TESJun 2, 1999 · N10791 · Boeing 727232 · Landing Gear Position and WarningSDR CALA9900024Stator · migratedENGINE NUMBER THREE FAILED ON CLIMB-OUT. CONSTANT VIBRATION, OVER TEMP, ENGINE SHUT DOWN IN FLIGHT. AIRCRAFT RETURNED TO LAS. ENGINE AND DAMAGED COWLING REPLACED AND AIRCRAFT RETURNED TO SERVICE. PRELIMINARY ENGINE INSPECTION REVEALED A FAILURE IN THE HIGH Jan 16, 1999 · N10791 · Boeing 727232 · Turbine Engine Compressor SectionSDR CALA9800812Battery · dischargedMAIN CABIN O/H EMERGENCY LIGHT FLICKERING. RECHARGED BATTERY PACK PER MM 33-50-0.May 7, 1998 · N10791 · Boeing 727232 · Emergency LightingSDR CALA9800747Frame · crackedTOP FLANGE AT FRAME 520 HAS .5 INCH CRACK ABOVE STR 26R. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-6. HEAT TREAT PER BAC 5602.May 3, 1998 · N10791 · Boeing 727232 · Fuselage Main, FrameSDR CALA9800746Oxy Contl Unit · failedFWD OXYGEN PASSENGER DROP FAILED FUNCTIONAL TEST. REPLACED OXYGEN CONTROL UNIT AND PERFORMED PNEUMATIC OXYGEN DROP PER MM 35-21-00.May 3, 1998 · N10791 · Boeing 727232 · Passenger Oxygen SystemSDR CALA9800745Web · crackedVERT STAB INNER COMPARTMENT NR 1 CANTED STATION 1303 HAS CRACK (2.5) AT RT LOWER CORNER. ALSO, CRACK (1) AT RT UPPER CORNER. STOP DRILLED CRACKS, FABRICATED AND INSTALLED DOUBLERS PER SRM 51-40-2.May 3, 1998 · N10791 · Boeing 727232 · Vertical StabilizerSDR CALA9800744Stringer · crackedVERT STAB INNER COMPARTMENT NR 7 STRINGER NR 2 AND NR 3 CRACKED (2) AT ATTACH BOLT. REPAIRED NR 7 RT STRINGER NR 2 AND NR 3 ON VERTICAL STAB PER SRM 55-30-4.May 3, 1998 · N10791 · Boeing 727232 · Vertical StabilizerSDR CALA9800743Jamb · crackedC-1 DOOR JAMB BENT/TORN AT TWO PLACES. REMOVED AND REPLACED DOOR JAMB AS REQUIRED PER SRM 51-10-1.May 3, 1998 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9800742Flange · crackedTOP FLANGE RADIUS FS 700 ABOVE 24 L HAS 1.5 INCH CRACK. STOP DRILLED, FABRICATED DOUBLER AND INSTALLED PER SRM 51-30-2 AND 51-40-3.May 3, 1998 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9800741Wire · brokenLT EXIT LIGHT INOP OVER EXIT IN CABIN. REPAIRED BROKEN WIRE AT EXIT IDENTIFIER, OPS CHECK PER 33-50-00.May 3, 1998 · N10791 · Boeing 727232 · Light System WiringSDR CALA9800740Flange · crackedA 1 INCH CRACK AT FRAME 500 TOP FLANGE RADIUS ABOVE 24 L. FABRICATED NEW DOUBLER AND INSTALLED IN ACCORDANCE WITH SRM 51-40-3. HEAT TREATED PER BAC 5602.May 3, 1998 · N10791 · Boeing 727232 · Fuselage Main, FrameSDR CALA9800739Skin · corrodedFUSELAGE SKIN IN FORWARD BAG BIN FS 695.700 AT RBL HAS SURFACE CORROSION. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-03.May 3, 1998 · N10791 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9800738Wire · brokenESCAPE PATH LIGHTS INOP ROW 24 TO 29. REPAIRED BROKEN WIRE GOING TO SEATS PER MM 33-50-00.May 3, 1998 · N10791 · Boeing 727232 · Light System WiringSDR CALA9800701Support · crackedINSPECTION FOUND A 2.5 CRACK IN VERTICAL STABILIZER STRINGER 4L SUPPORT WEB. THE SUPPORT WEB WAS REMOVED IAW SRM 51-30-2. A NEW SUPPORT WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.Apr 24, 1998 · N10791 · Boeing 727232 · Vertical StabilizerSDR CALA9800700Support · crackedINSPECTION FOUND A 1 CRACK IN VERTICAL STABILIZER SUPPORT WEB AT STRINGER 3L AND STRINGER 3R. THE LT AND RT SUPPORT WEB WAS REMOVED. A NEW SUPPORT WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.Apr 24, 1998 · N10791 · Boeing 727232 · Vertical StabilizerSDR CALA9800699Frame · crackedINSPECTION FOUND A 1 CRACK IN UPPER FLANGE RADIUS OF FRAME 640, RBL 8, FORWARD BAGGAGE BIN. THE CRACKED AREA WAS CUT OUT IAW SRM 51-40-3. A DOUBLER AND FITTING WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1, SHEET A, SRM 51-10-2, AND 51-30-2.Apr 24, 1998 · N10791 · Boeing 727232 · Fuselage Main, FrameSDR CALA9800698Frame · crackedINSPECTION FOUND A .375 INCH CRACK WITH CORROSION IN FRAME 560 TO SKIN ATTACH FLANGE, BBL 0 TO LBL 6. THE CORRODED AREA OF FLANGE WAS CUT OFF IAW SRM 53-10-4. A NEW FLANGE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4.Apr 24, 1998 · N10791 · Boeing 727232 · Fuselage Main, FrameSDR CALA9800697Stringer · corrodedINSPECTION FOUND STRINGER 28L CORRODED AT STA 720D. THE CORRODED AREA OF STRINGER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3.Apr 24, 1998 · N10791 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9800472Hyd Pump · leakingTHE 'A' SYSTEM HYDRAULIC RESERVOIR QUANTITY WENT TO ZERO AND LOW PRESSURE LIGHTS ILLUMINATED WHILE EN ROUTE FROM MSY TO IAH. THE HYDRAULIC QUANTITY LOSS AND HYDRAULIC SYSTEM FAILURE CHECKLISTS WERE COMPLETED. THE LANDING GEAR WAS CRANKED DOWN AND THE FLAPS WMar 17, 1998 · N10791 · Boeing 727232 · Hydraulic Pump (Electric/Engine), MainSDR CALA9701375Beam · crackedINSPECTION FOUND A .365 INCH AND .625 INCH CRACK IN RT WING UPPER TRAILING EDGE AFT OF MLG SUPPORT BEAM AT UPPER INBOARD CORNER OF NR 8 SPOILER ACTUATOR LINKAGE CASTING, WS 232. THE CRACKS WERE ROUTED OUT. REPAIR STRAPS WERE FABRICATED AND INSTALLED IAW ECRAAug 31, 1997 · N10791 · Boeing 727232 · Wing Miscellaneous StructureSDR CALA9701372Doubler · corrodedINSPECTION FOUND CORROSION AND POPPED RIVETS IN REPAIR DOUBLER AT FS 680, STRINGER 28R - 28L. THE EXISTING DOUBLER WAS REMOVED AND THE CORRODED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.Aug 26, 1997 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9701374Skin · puncturedINSPECTION FOUND A .25 INCH DIAMETER HOLE IN SKIN AT UPPER LEADING EDGE OF NR 7 SLAT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-50-3.Aug 25, 1997 · N10791 · Boeing 727232 · Leading Edge DevicesSDR CALA9701371Bracket · crackedINSPECTION FOUND A .5 CRACK IN UPPER AND LOWER RADIUS OF NR 5 KRUGER FLAP ACTUATOR SUPPORT BRACKET. A REPLACEMENT BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.Aug 25, 1997 · N10791 · Boeing 727232 · Leading Edge Slat ActuatorSDR CALA9701369Skin · crackedINSPECTION FOUND A .375 INCH CRACK AT LEFT WING FIXED LEADING EDGE CUTOUT ABOVE NR 3 SLAT INBOARD TRACK. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-30-2, AND 51-40-2.Aug 25, 1997 · N10791 · Boeing 727232 · Wing, Plate/SkinSDR CALA9701373Skin · dentedINSPECTION FOUND TWO DENTS IN RT FUSELAGE SKIN AT STA 380. THE DENTED AREA WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3.Aug 24, 1997 · N10791 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9701370Bracket · crackedINSPECTION FOUND A .75 CRACK IN BRACKET AT INBOARD AND OUTBOARD SIDE WHERE LEFT WING NR 1 L/E FLAP ACTUATOR MOUNTS (I/B LOWER AND O/B UPPER). REPLACEMENT BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-2.Aug 24, 1997 · N10791 · Boeing 727232 · Leading Edge Slat ActuatorSDR CALA9700343Actuator · leakingAIRCRAFT LOST A-HYDRAULIC SYSTEM FLUID AFTER TAKEOFF. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF RUDDER SYSTEM A CAUTION LIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 KREUGER FLAP ACTUATOR LEAKING. THMar 16, 1997 · N10791 · Boeing 727232 · Leading Edge Slat ActuatorSDR CALA9700125Hyd Pump · leakingACFT LOST THE A-HYDRAULIC SYSTEM FLUID QUANTITY ON APPROACH. THE FLUID LOSS WAS ACCOMPANIED BY THE PUMP LIGHT GOING ON AND OFF INTERMITTENTLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING AT PUMP CASEJan 30, 1997 · N10791 · Boeing 727232 · Hydraulic Pump (Electric/Engine), MainSDR CALA9601731Skin · damagedTHE RT INBOARD TRAILING EDGE MID FLAP LOWER SKIN SUSTAINED DAMAGE WHEN THE RT MLG TIRE BLEW. THE MID FLAP WAS REPAIRED IAW ECRA 5750-02565.Nov 19, 1996 · N10791 · Boeing 727232 · Trailing Edge FlapsSDR CALA9601378Gearbox · leakingTHE NR 3 ENGINE LOST OIL QUANTITY AFTER TAKEOFF. THE LOSS OF OIL WAS ACCOMPANIED BY LOSS OF OIL PRESSURE AND ILLUMINATION OF FORWARD PANEL LIGHT. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO SJU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NROct 4, 1996 · N10791 · Boeing 727232 · Turbine Engine Accessory DriveSDR CALA9601303Duct · blownTHE NR 2 ENGINE FAILED AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO SJU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE 13TH STAGE DUCT BLOWN. THE NR 2 ENGINE WILL BE REMOVED AND REPLACED.Sep 11, 1996 · N10791 · Boeing 727232 · Pneumatic Distribution SystemSDR CALA9601146Airstairs · out of adjustTHE AFT AIRSTAIRS FELL DOWN WHILE TAXIING TO GATE AFTER LANDING AT IAH. THE AIRCRAFT WAS STOPPED AND THE STAIRS WERE SECURED. WHEN THE AIRSTAIRS WAS EXAMINED FOR DAMAGE ONLY A SKID MARK WAS FOUND ON THE SKID PLATE. THE AIRSTAIR WAS OPERATED SEVERAL TIMES. Aug 7, 1996 · N10791 · Boeing 727232 · Entrance StairsSDR CALA9600970Actuator · leakingTHE A-SYSTEM HYDRAULIC QUANTITY WAS LOST DURING CLIMBOUT. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 LEADING EDGE FLAP ACTUATOR LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED. IN ADDITIJul 6, 1996 · N10791 · Boeing 727232 · Leading Edge Slat ActuatorSDR CALA9600956Floorbeam · corrodedINSPECTION FOUND THE FLOORBEAM CORRODED AT STA 1130, RBL 34 DURING FLIGHT PHONE INSTALLATION. THE FLOORBEAM WAS REPAIRED IAW SRM 5310-03300.Jun 30, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9600913Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED AT STA 580 BETWEEN STRINGER 27R AND 28R. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 53-10-4, FIG 15 AND MM 51-20-2, 51-20-15.Jun 10, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600901Stringer · corrodedINSPECTION FOUND STRINGER 28R FLANGE CORRODED AT F.S. 685. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3.Jun 5, 1996 · N10791 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9600936Stringer · corrodedINSPECTION FOUND STRINGER 28R CORRODED AT STA 520 T0 540. THE CORRODED STRINGER SECTION WAS REMOVED. A NEW STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2.Jun 2, 1996 · N10791 · Boeing 727232 · Fuselage Main, Longeron/StringerSDR CALA9600938Angle · corrodedINSPECTION FOUND CORROSION ON SKIN ATTACH ANGLE AT STA 580, STRINGER 27L. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, 51-30-2 AND MM 51-20-11.May 29, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600915Support · corrodedINSPECTION FOUND THE FORWARD CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STA 535, S28L TO S29L. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51-40-4, 51-10-2, 53-10-1 AND 51-30-2.May 28, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600919Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED AT STA 265, S25R. A REPAIR WAS PERFORMED IAW SRM 53-10-4, 51-10-2, 51-30-2 AND MM 51-20-21.May 26, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600914Skin · corrodedINSPECTION FOUND SKIN LAP CORRODED AT STA 720D TO 720E, STRINGER 27R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2.May 26, 1996 · N10791 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9600935Angle · corrodedINSPECTION FOUND ATTACH ANGLE CORRODED AT STA 540, S29R. THE ATTACH ANGLE WAS REMOVED. A REPAIR PART WAS FABRICATED IAW SRM 53-10-4, 53-10-1 AND 51-20-4.May 25, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600934Frame · corrodedINSPECTION FOUND STA 540 FRAME ASSEMBLY CORRODED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, PAGE 43.May 25, 1996 · N10791 · Boeing 727232 · Fuselage Main, FrameSDR CALA9600902Angles · corrodedINSPECTION FOUND SKIN ATTACH ANGLES(2) AT BILGE, STA 580, BL ZERO CORRODED. ANGLE DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-0.May 25, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9600900Floor Beam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT B.S. 1130, LBL 25. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-1, 53-10-8, AND MM 51-20-11.May 24, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9600923Floor Beam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 30. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-2, 51-30-4 AND MM 51-20-11.May 23, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor BeamSDR CALA9600912Web · crackedINSPECTION FOUND A FOUR INCH CRACK IN STIFFENER WEB INSIDE VERTICAL FIN ABOVE S-DUCT AT STA 1348. THE CRACK WAS STOPPED DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-30-2 AND MM 51-20-11.May 23, 1996 · N10791 · Boeing 727232 · Vertical StabilizerSDR CALA9600909Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE SKIN FORWARD OF OUTBOARD SLAT CARRIAGE, NR 5 SLAT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 57-30-4, FIG 4 AND 9, MM 51-20-11.May 23, 1996 · N10791 · Boeing 727232 · Wing, Plate/Skin
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