N16887, cancelled May 22, 2003

Service difficulty reports · 36

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 = 'N16887' AND deregistration_id = 'N16887-2003-05-22'
  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 CALA0100538Battery · dischargedINSPECTION FOUND AFT CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD.Jun 12, 2001 · N16887 · Doug DC982 · Emergency EquipmentSDR CALA0001374Battery Pack · inoperativeINSPECTION FOUND AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-53-00.Sep 3, 2000 · N16887 · Doug DC982 · Emergency LightingSDR CALA0001293Angle · corrodedINSPECTION FOUND L-ANGLE CORRODED UNDER EXISTING DOUBLER AT CANTED BULKHEAD STA 1463, L16R. A NEW ANGLE SECTION WAS INSTALLED IAW SRM 53-03, FIGURE 27.Aug 21, 2000 · N16887 · Doug DC982 · Fuselage Miscellaneous StructureSDR ALA0001292Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT NUT PLATE MOUNT AREA, STA 1338 BELOW LT AFT LAV. A SPLICE SECTION WAS INSTALLED IAW SRM 51-30-0 AND 51-10-3.Aug 21, 2000 · N16887 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0001274Attach Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT STA 1486, L3R. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 53-05, FIGURE 23.Aug 18, 2000 · N16887 · Doug DC982 · Fuselage Main, Attach FittingsSDR CALA0001271Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 237 BETWEEN LONGERON 17L AND 18L. THE SKIN SECTION WAS REPLACED IAW ECRA 5330-02445.Aug 16, 2000 · N16887 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001270Web · crackedINSPECTION FOUND A 2 INCH CRACK IN WEB AT CANTED BULKHEAD STA 1463, LONGERON 17R. THE CRACKED SECTION OF WEB WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4, SHEET 3.Aug 16, 2000 · N16887 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001269Pan · chafedINSPECTION FOUND MAIN BAGGAGE BIN DOOR PAN CHAFED AT FORWARD EDGE OF NR 1 STOP PAD. REPAIRED IAW ECRA 5230-01540.Aug 16, 2000 · N16887 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001268Pan · crackedINSPECTION FOUND A .25 INCH CRACK IN MAIN BAGGAGE BIN DOOR PAN UNDER NR 4 STOP PAD BRACKET AT AFT EDGE OF DOOR. REPAIRED IAW SRM 52-05, FIGURE 26A AND 50.Aug 16, 2000 · N16887 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001267Floorbeam · wornINSPECTION FOUND CABIN FLOORBEAM WORN AT RT CENTER OF FORWARD CARGO BEAM, STA 389. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-05, FIGURE 86.Aug 15, 2000 · N16887 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0001265Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AFT OF THE L-1 DOOR AND APPROXIMATELY 8 INCHES ABOVE FORWARD LAV SERVICE PANEL AT STA 226, LONGERON 17L-18L. INSPECTION FOUND THE DENT TO BE IN CONDITION (1) PER SRM 53-04, PAGE 218, TABLE C. THE DENT WAS BLENDED OUT ANDAug 14, 2000 · N16887 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001264Fitting · corrodedINSPECTION FOUND LT SIDEWALL LOWER ATTACH FITTING CORRODED AT STA 200. A NEW FITTING WAS INSTALLED IAW SRM 51-30.Aug 14, 2000 · N16887 · Doug DC982 · Fuselage Main, Attach FittingsSDR CALA0001245Angle · corrodedINSPECTION FOUND MAIN BAGGAGE BIN DOOR JAMB Z-ANGLE CORRODED AT I/B SIDE AROUND HI-SHEARS. THE CORROSION ON DOOR FRAME Z-ANGLE WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63.Aug 8, 2000 · N16887 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001244Web · corrodedINSPECTION FOUND LT CUSP MEMBRANE CORRODED AT STA 200 JUST AFT OF MCD CUTOUT AT LOWER SIDE. THE CUSP MEMBRANE WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND ECRA 5310-03778.Aug 8, 2000 · N16887 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001232Seat Track · corrodedINSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT STA 236. THE CORRODED SECTION OF SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F.Aug 4, 2000 · N16887 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9901511Battery Pack · dischargedINSPECTION FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS ABOVE BOTH LEFT AND RIGHT DOORS INOPERATIVE DURING EMERGENCY LIGHT TEST. THE POWER SUPPLY BATTERY PACK WAS REMOVED AND REPLACED. OPERATION CHECKED GOOD IAW MM 33-53-00, PAGE 407.Nov 18, 1999 · N16887 · Doug DC982 · Emergency LightingSDR CALA9900214Strut · reqd serviceTHE LANDING GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED SAFELY. MAINTENANCE FOUND THE NLG STRUT FLAT. A COMPLETE STRUT SERVICE WAS PERFORMED IAW MM 32-21-02. THE NOSE GEAR WAS CYCLED AND LANDING GEAR Mar 5, 1999 · N16887 · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR CALA9801212Pins · wornTHE FORCE REQUIRED TO RELEASE TAILCONE USING EXTERIOR HANDLE WAS BELOW LIMITS. WORN ALIGNMENT PINS AND RECEPTACLES WERE REPLACED AND LATCHES WERE ADJUSTED IAW MM 53-50-00.Jul 6, 1998 · N16887 · Doug DC982 · Aerodynamic FairingsSDR CALA9801211Web · corrodedINSPECTION FOUND WEB CORRODED AT STA 1212 AFT OF DOOR INBOARD OF LONGERON 27R. A REPAIR WAS INSTALLED IAW ECRA 5310-03742.Jul 2, 1998 · N16887 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9801186Skin · crackedINSPECTION FOUND A .25 INCH CRACK IN MAIN CABIN DOOR SKIN WITH DEEP WEAR MARKS ON HOLD OPEN HOOK PAN ON DOOR. A REPAIR DOUBLER WAS INSTALLED AND THE PAN WAS REPLACED IAW SRM 52-05.Jun 30, 1998 · N16887 · Doug DC982 · Passenger/Crew DoorsSDR CALA9801185Spacer · corrodedINSPECTION FOUND CORROSION ON AFT BAGGAGE BIN Z-ANGLE REPAIR SPACER AT STA 1155 TO 1212. THE REPAIR SPACER WAS REMOVED AND REPLACED IAW SRM 51-30-5.Jun 29, 1998 · N16887 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9801184Intercostal · crackedINSPECTION FOUND A .5 INCH CRACK AT EXTERNAL HANDLE RECESS CUP OF MAIN CABIN DOOR INTERCOSTAL. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2.Jun 29, 1998 · N16887 · Doug DC982 · Passenger/Crew DoorsSDR CALA9801182Beam · crackedINSPECTION FOUND A .25 INCH CRACK IN RADIUS OF MAIN CABIN DOOR NR 1 HORIZONTAL BEAM FORWARD END. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31.Jun 26, 1998 · N16887 · Doug DC982 · Passenger/Crew DoorsSDR CALA9801176Beam · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD END OF FORWARD GALLEY SERVICE DOOR NR 4 BEAM. THE NR 4 BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2.Jun 26, 1998 · N16887 · Doug DC982 · Galley DoorsSDR CALA9601340Fuel Control · leakingA STRONG FUEL SMELL WAS NOTICED IN THE COCKPIT AND CABIN WHILE DESCENDING INTO CLE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FUEL LEAKING FROM APU FUEL CONTROL DRAIN. THE APU FUEL CONTROL UNIT WAS REMOVED AND REPLACED PER MM 49-01-1. THE APUSep 29, 1996 · N16887 · Doug DC982 · APU Engine Fuel and ControlSDR CALA9601102Clips · out of adjustTHE FORCE REQUIRED TO PULL INTERIOR AND EXTERIOR TAILCONE RELEASE HANDLES OUT OF CLIPS WAS EXCESSIVE. THE CLIPS WERE ADJUSTED IAW MM 53-53-00.Jul 25, 1996 · N16887 · Doug DC982 · Aerodynamic FairingsSDR CALA9601094Hat Section · corrodedINSPECTION FOUND HAT SECTION CORRODED AROUND NUTPLATE HOLE BETWEEN PANEL J AND H AT FORWARD ENTRY. THE HAT SECTION WAS REMOVED AND A NEW HAT SECTION WAS INSTALLED IAW SRM 51-30-1.Jul 17, 1996 · N16887 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9601097Sub Floor · corrodedINSPECTION FOUND BOTTOM OF SUB-FLOOR CORRODED OUTBOARD OF LEFT OUTBOARD SEAT TRACK AT STA 1136-1274. THE SUB-FLOOR WAS REPLACED IAW SRM 51-30-02.Jul 12, 1996 · N16887 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9601099Channel · crackedINSPECTION FOUND Z-CHANNEL CRACKED AT STA 69. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, PAGE 9 AND SRM 51-30-5.Jul 11, 1996 · N16887 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9601095Intercostal · crackedINSPECTION FOUND FIVE 1 INCH CRACKS IN INTERCOSTAL IN AFT BAGGAGE BIN AT STA 1309. THE CRACKS WERE STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2.Jul 11, 1996 · N16887 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9601096Intercostal · crackedINSPECTION FOUND A 10 INCH CRACK IN FORWARD BAGGAGE BIN INTERCOSTAL AT VHF ANTENNA MOUNT BETWEEN STA 465 AND STA 484. THE INTERCOSTAL WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2.Jul 10, 1996 · N16887 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9601101Latches · out of adjustTHE FORCE REQUIRED TO DROP TAILCONE USING THE INTERIOR RELEASE HANDLE AND AFT ENTRANCE DOOR RELEASE HANDLE WAS EXCESSIVE. THE TAILCONE LATCHES WERE ADJUSTED IAW MM 53-53-00.Jul 9, 1996 · N16887 · Doug DC982 · Aerodynamic FairingsSDR CALA9601100Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED FORWARD OF PITOT TUBES. THE DENTED SECTION OF SKIN WAS REPLACED IAW SRM 51-30-2 AND SRM 51-30-5.Jul 8, 1996 · N16887 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9601098Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED BETWEEN LONGERON 21R AND 22R AT STA 165. THE DENT WAS COLD-FORMED AND DYE CHECKED WITH NO CRACKS FOUND. AN INTERNAL DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, PAGE 218.Jul 8, 1996 · N16887 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9600770Hyd Line · leakingTHE RIGHT HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO WHILE EN ROUTE. EMERGENCY GEAR EXTENSION WAS USED PRIOR TO LANDING. THE LT MLG DOOR WAS DAMAGED UPON LANDING AT EWR. MAINTENANCE FOUND THE HYDRAULIC LINE FOR NOSE GEAR UP LEAKING AND THE LINE Jun 8, 1996 · N16887 · Doug DC982 · Hydraulic System, MainSDR CAL960542Oil Tank Vent · cloggedFLT NR 279 - EWR - PRIOR TO PUSH BACK CABIN BEGAN TO FILL WITH SMOKE. DURING T/S FOUND OIL LEAKED ON COALESCER BAGS DUE TO APU OIL TANK BEING OVERSERVICED. REMOVED AND REPLACED COALESCER BAGS CLEANED APU OIL TANK VENT HOLE, DRAINED 2 QTS OF OIL. TANK NOW REApr 27, 1996 · N16887 · Doug DC982 · APU Oil System
Back to N16887, cancelled May 22, 2003