N8882Z, cancelled Jul 20, 2010

Service difficulty reports · 58

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 = 'N8882Z' AND deregistration_id = 'N8882Z-2010-07-20'
  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 DL72S030304Proximity Sensor · out of adjustON T/O AT APPROX 80 KTS NR 3 REVERSER LIGHT CAME ON. T/O ABORTED. ADJUSTED PROX SWITCH.Mar 31, 2003 · N8882Z · Boeing 727225A · Engine Thrust ReverserSDR DL72S030279Fairing · looseAT FL300 SPEED .78/285KTS THE AIRCRAFT HAD MODERATE TO SEVERE VIBRATION IN AIRCRAFT AND CONTROLS. FOUND INBOARD RT FLAP ELEPHANT EAR AND CANOE LOOSE. REPAIRED SAME.Mar 26, 2003 · N8882Z · Boeing 727225A · Trailing Edge FlapsSDR DL72S021475Rib · crackedVERT. STAB RIB L/H ATTACH ANGLE CRACKED AT FIN STA 133.800 AND STR 9LEFT REPAIR PER M/M 55-30-000-8Dec 26, 2002 · N8882Z · Boeing 727225A · Empennage StructureSDR DL72S020642Warning System · activatedCREW REPORTS NOSE GEAR UNSAFE INDICATION AND VIBRATION ON GEAR RETRACTION. JACKED NOSE AND SWUNG GEAR, ALL OPS NORMAL.Jun 9, 2002 · N8882Z · Boeing 727225A · Landing Gear Position and WarningSDR DL72S020571Skin · crackedTHE UPPER HINGE CUTOUT OF THE L1 DOOR CUTOUT WAS FOUND WITH A .5 INCH CRACK IN THE SKIN AND A CRACK INDICATION AT A FASTENER HOLE IN THE BEAR STRAP. THE CRACKS WERE REMOVED AND REPAIRED WITH DOUBLERS PER ER/A 383169-14, REV B.May 17, 2002 · N8882Z · Boeing 727225A · Fuselage Main, Plate/SkinSDR DL72S020549Stringer · corrodedFOUND ON D1 LETTER CK, CORROSION AT STR 28 RT AT STA 620. REPAIRED PER SRM 53-10-3.May 14, 2002 · N8882Z · Boeing 727225A · Fuselage Main, Longeron/StringerSDR DL72S011714Skin · crackedFUSELAGE / SKIN / FWD GALLEY DOOR CUTOUT / LWR AFT CORNER : CRACK REPAIR THE LOWER AFT CORNER OF THE FWD GALLEY DOOR CUTOUT WAS FOUNDWITH A CRACK EMANATING FROM A FASTENER HOLE. THE CRACK IS TYPICAL OF BAC S/B 7Oct 21, 2001 · N8882Z · Boeing 727225A · Fuselage Main, Plate/SkinSDR DL72S011688Skin · crackedFOUND ON C2 LETTER CK 5/16 IN CRACK FUSELAGE SKIN R-1 DOOR LOWER AFT CUTOUT. REPAIRED PER ERA 381969-14 AND EO 4-58974-3AD.Oct 18, 2001 · N8882Z · Boeing 727225A · Fuselage Structure (General)SDR DL72S011451Charger · inoperativeL-1 WING EMERGENCY EXIT LIGHT INOP, REPLACED CHARGER.Aug 29, 2001 · N8882Z · Boeing 727225A · Emergency LightingSDR DL72S010282Battery Pack · dischargedON L/O CHECK, FOUND R-2 OVERHEAD EMERGENCY EXIT DOOR LIGHT INOP. REPLACED R-2 OVERHEAD EMERGENCY EXIT DOOR BATTERY PACK, OPS NOW NORMAL.Feb 17, 2001 · N8882Z · Boeing 727225A · Emergency LightingSDR DL72S002502Frame · crackedFUSELAGE / OVERWING EXIT / LT / FRAME / FS 783.95 : CRACK REPAIR. INSPECTIONS OF THE LH OVERWING EMERGENCY EXIT OPENING FRAMESREVEALED CRACKING IN THE FS 783.95 FRAME. THE CRACKING IS TYPICAL OF BAC S/B 727-53-0197 AND AD 94-02-04. THE FRAME WAS REPAIREDDec 21, 2000 · N8882Z · Boeing 727225A · Fuselage Main, FrameSDR DL72S002006Start Valve · failedNR 2 ENGINE START VALVE CAME AT CLIMBOUT POWER 1.96 EPR WITH THE AIRCRAFT PASSING 5000 FT MSL. AFTER ENGINE NR 2 WAS RETARDEDTHE START VALVE OPEN LIGHT EXTINGUISHED. NR 2 ENG SHUTDOWN. REPLACED START VALVE AND PRESS SW; CKD CHIP DETECTOR AND STRAINER, CKS OOct 13, 2000 · N8882Z · Boeing 727225A · Engine Start Valves/ControlsSDR DL72S001506Web · crackedA 1.5 INCH CRACK IN VERTICAL TORQUE BOX WEB RT FS 121, 3 INCHES JUST ABOVE THIRD STEP FROM TOP (48 SEC). REPAIRED PER M/M.Aug 9, 2000 · N8882Z · Boeing 727225A · Fuselage Miscellaneous StructureSDR DL72S001463Skin · corrodedTHE FUSELAGE SKIN AND UNDERLYING STRINGER WERE FOUND CORRODED BETWEEN FS 680 & 700 AT STRINGER 27R. THE DAMAGED SECTION OF SKIN AND STRINGER WERE CUTOUT AND REMOVED. A NEW SECTION OF STRINGER WAS SPLICED IN PER THE B727 SRM AND THE SKIN CUTOUT WAS REPAIRED WAug 2, 2000 · N8882Z · Boeing 727225A · Fuselage Main, Plate/SkinSDR DL72S001424Beam · tool damageWHILE ACCOMPLISHING INSPECTIONS OF THE LBL 17.8 VERTICAL BEAM ON THE FS 1183 BULKHEAD PER BAC S/B 727-53-0210 AND AD 99-18-05, AN ELONGATED HOLE WAS FOUND COMMON TO THE WL 273 DOOR STOP INTERCOSTAL. THE HOLE WAS REAMED TO A CLEAN AND ROUND CONDITION, HFEC INSJul 27, 2000 · N8882Z · Boeing 727225A · Fuselage Miscellaneous StructureSDR DL72S001126Valve · inoperativeLEFT PACK WILL NOT HOLD CABIN PRESS ABOVE 10,000 FEET. CARGO HEAT OUTFLOW VALVE CLOSED AND PACK ON PRESSURE IN MANUAL OUTFLOW VALVE FULL CLOSED. DUCT PRESSURE WAS NORMAL. REPLACED RT PACK VALVE.Jun 10, 2000 · N8882Z · Boeing 727225A · Cabin Pressure Control SystemSDR DL72S001015Battery Pack · inoperativeOVERWING EMERG LIGHT INOP. REPLACED BATTERY PACK.May 24, 2000 · N8882Z · Boeing 727225A · Emergency LightingSDR DL72S991844Stringer · crackedVERTICAL STAB INTERIOR, STRINGER CRACKED AT TIE TO RIB LEFT SIDE AT FIN STA 1338. INSTALLED REPAIR PER SRM 55-30-0 FIG 803.Aug 9, 1999 · N8882Z · Boeing 727225 · Vertical StabilizerSDR DL72S991317Angle · crackedMLG W/W STA 913 ANGLE CRACKED AT UPPER RADIUS BLOCK ABOVE UPLOCK. REPAIRED PER DAL M/M 53-11-0 PGS 834-837 AND ERA 367582-14 ALLOWING USE OF DAL M/M REPAIR ON EX - EAL AIRCRAFT.Jun 10, 1999 · N8882Z · Boeing 727225A · Fuselage Miscellaneous StructureSDR DL72S991316Frame · crackedLTR CHECK A2, 1 INCH CRACK AT C-2 DOOR CUTOUT FWD FRAME WEB AT LOWER END. REPAIRED PER SRM 53-10-4.Jun 10, 1999 · N8882Z · Boeing 727225A · Fuselage Miscellaneous StructureSDR DL72S991314Web · crackedFOUND ON A2 LETTER CK. .25 INCH CRACK AT RT TORQUE BOX VERT WEB LOWER LIGHTENING HOLE STA 1243. REPAIRED PER MM 53-11-0.Jun 10, 1999 · N8882Z · Boeing 727225A · Fuselage Miscellaneous StructureSDR DL72S991313Web · crackedFOUND ON A-2 LETTER CK, .5 INCH CRACK AT LT TORQUE BOX VERTICAL WEB AT THE UPPER LIGHTENING HOLE STA 1243. REPAIRED PER MM 53-11-0.Jun 10, 1999 · N8882Z · Boeing 727225A · Fuselage Miscellaneous StructureSDR DL72S991099Sign · inoperativeEMERGENCY EXIT SIGN OVER 2R SERVICE DOOR FLICKERS FROM DIM TO BRIGHT WITH EMERGENCY LIGHT SYSTEM OFF.May 18, 1999 · N8882Z · Boeing 727225 · Emergency LightingSDR DL72S990732Valve · leakingLOSS OF B HYD IN FLT. REPLACED LEAKING CHECK VALVE IN LEFT WHEEL WELL.Apr 3, 1999 · N8882Z · Boeing 727225 · Hydraulic System, MainSDR DL72S990401Wire · crackedON HUSH-KIT MOD FOUND NUMEROUS LONGITUDINAL CRACKS ON INSULATION ON ALL 3 GEN FEED CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN RT 48SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS13-58 DL (P/N 012210733).Feb 26, 1999 · N8882Z · Boeing 727225A · Electrical Power System WiringSDR DL72S990368Skin · damagedINCORPORATION OF SKIN DAMAGE INTO MODIFICATION DOUBLER WHILE ACCOMPLISHING A MODIFICATION TO THE AIRCRAFT. INSTALLED FED-EX HUSHKITS AND EXISTING SKIN REPAIR WAS FOUND TO INTERFER WITH THE INSTALLATION OF A TITANIUM MODIFICATION DOUBLER ON THE SKIN. THE EXISFeb 22, 1999 · N8882Z · Boeing 727225A · Fuselage Main, Plate/SkinSDR DL72S990323Angle · corrodedON HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT CHORD ANGLE CORRODED BEYOUND MFG SPECS. REPLACED CHORD ANGLE WITH NEW MFG RT SIDE.Feb 18, 1999 · N8882Z · Boeing 727225A · Nacelle/Pylon StructureSDR DL72S990322Cord Angle · newON HUSH-KIT MOD, FOUND LT NR 2 ENG MOUNT CHORD ANGLE CORRODED BEYOUND MFG SPECS. REPLACED CHORD ANGLE WITH ANGLE OF NEW MFG.Feb 17, 1999 · N8882Z · Boeing 727225A · Empennage StructureSDR DL72S982629Valve · failedLEFT PACK ON, CAUSED SMOKE IN CABIN. REPLACED FWD PACK VALVE AND MIX VALVE. CK OK.Dec 26, 1998 · N8882Z · Boeing 727225 · Cabin Cooling SystemSDR DL72S982277Web · crackedFOUND ON A1 LETTER CK, .5 INCH CRACK LT LOWER TORQUE BOX VERTICAL WEB STA 1283. REPAIRED PER MM 53-11-0 AND ERA 366033-14.Nov 5, 1998 · N8882Z · Boeing 727225 · Fuselage Miscellaneous StructureSDR DL72S982276Web · crackedFOUND ON A1 LETTER CK, 1 INCH CRACK LT TORQUE BOX VERTICAL WEB FWD OF STA 1223. REPAIRED PER MM 53-11-0 AND ERA 366033-14.Nov 5, 1998 · N8882Z · Boeing 727225 · Fuselage Miscellaneous StructureSDR DL72S982275Rib · crackedFOUND ON A1 LETTER CK, 1 INCH CRACK L/E RIB O/B OF ACTUATOR ON NR 4 SLAT. REPAIRED PER MM 57-54-0 AND ERA 366036-14.Nov 5, 1998 · N8882Z · Boeing 727225 · Leading Edge DevicesSDR DL72S981552Battery Pack · dischargedEXTERIOR EMERGENCY LIGHT INOP RT SIDE 2ND LIGHT AFT OF OVERWING ESCAPE HATCHES. REPLACED BULBS, BATTERY PACK, CLEANED SOCKETS AND CHECKS OK.Jul 24, 1998 · N8882Z · Boeing 727225 · Emergency LightingSDR DL72S981551Light · inoperativeEMERGENCY LIGHT INOP ABOVE AFT AIRSTAIR BOTTOM STEP IN CEILING. RELAMPED AND CLEANED SOCKET, CHECKS OK.Jul 24, 1998 · N8882Z · Boeing 727225 · Emergency LightingSDR DL72S981102Outflow Valve · stuckAFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. ALL MODES TRIED, PULLED AND RESET C/B, NO HELP. REPLACED OUTFLOW VALVE AND PRESSURE CONTROLLER AND CONTROL PANEL.May 22, 1998 · N8882Z · Boeing 727225 · Pressure Regulator/Outflow ValveSDR DL72S980991Battery Pack · dischargedEMERGENCY EXIT LIGHT M1088 FAIL TEST. REPLACED BATTERY PACK, CHECKS OK.May 11, 1998 · N8882Z · Boeing 727225 · Emergency LightingSDR DL72S980850Frame · corrodedINBD CHORD OF THE FS 620 FRAME WAS FOUND CORRODED APPROX 2 INCHES OUTBD OF S26R. CORROSION WAS ON THE INBD CHORD ONLY. REPAIRED PER ERA 331533-14.Apr 20, 1998 · N8882Z · Boeing 727225 · Fuselage Main, FrameSDR DL72S980798Skin · damagedAN EXISTING REPAIR WAS REMOVED FROM THE LOWER SKIN PANEL NEAR THE STRINGER 20R LAP SPLICE. THE UNDERLYING SKIN CUTOUT WAS 3.5 X 4. THE SKIN CUTOUT AND SURROUNDING AREA WAS DYE PENETRANT INSPECTED TO ENSURE NO CRACKS AND AN EXTERNAL ALUMINUM DOUBLER INSTALLEDApr 10, 1998 · N8882Z · Boeing 727225 · Fuselage Main, Plate/SkinSDR DL72S980785Floorbeam · corrodedTHE UPPER CAP OF THE FS 1110 PASSENGER FLOORBEAM WAS FOUND CORRODED. A SECTION OF THE CAP WAS CUT OUT BETWEEN RBL 12 AND LBL 12. THE CAP WAS REPAIRED WITH A FILLER SECTION AND FOUR SPLICE ANGLES PER ER/A 364205-14, REV A.Apr 7, 1998 · N8882Z · Boeing 727225 · Fuselage Main, Floor BeamSDR DL72S980510Skin · wornDURING SHOP VISIT THE LEADING EDGE SKIN WAS FOUND WORN BEYOND LIMITS AT THE I/B END OF FLAP. THE SKIN WAS REPAIRED PER 727 MM 57-52-0, FIG 803 BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER.Feb 18, 1998 · N8882Z · Boeing 727225 · Trailing Edge FlapsSDR DL72S980324Spar · crackedAFT SPAR LWR RAIL GOUGED 57 FROM I/B END N/R 004267. AFT SPAR LWR RAIL, CRACKED FROM I/B END. N/R 004268, BOTH AREAS REPAIRED PER M/M 57-52-0 FIG 802. AFT SPAR BOTTOM FLANGE, 15 TR O/B END 5 ELONGATED HOLES N/R 004292, AFT SPAR LWR RAIL CRACKED 19 FROM I/B Dec 23, 1997 · N8882Z · Boeing 727225 · Wing SparSDR DL72S980156Angle · crackedTHE MIDFLAP WAS FOUND TO HAVE A CRACKED REAR SPAR ANGLE DURING SHOP VISIT. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A DOUBLER.Dec 22, 1997 · N8882Z · Boeing 727225 · Trailing Edge FlapsSDR DL72S980155Angle · crackedTHE MIDFLAP WAS FOUND WITH A CRACKED REAR SPAR ANGLE DURING SHOP VISIT. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A DOUBLER.Dec 22, 1997 · N8882Z · Boeing 727225 · Trailing Edge FlapsSDR DL72S980154Cove Skin · crackedDURING SHOP VISIT/INSPECTION, THE NR 2 MIDFLAP COVESKIN WAS FOUND CRACKED 31 INCHES FROM I/B END AT DRIVE ROD CUTOUT. THE COVESKIN WAS REPAIRED PER 727 MM 57-52-0 BY REMOVING THE CRACK AND INSTALLING A DOUBLER.Dec 22, 1997 · N8882Z · Boeing 727225 · Trailing Edge FlapsSDR DL72S980153Angle · crackedDURING SHOP VISIT/INSPECTION, THE NR 2 MIDFLAP AFT SPAR ANGLE WAS FOUND CRACKED 32 FROM THE I/B END OF FLAP. THE DAMAGE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A DOUBLER.Dec 22, 1997 · N8882Z · Boeing 727225 · Trailing Edge FlapsSDR DL72S980509Rib · crackedDURING SHOP VISIT, THE AFT RIB WAS FOUND CRACKED AT AFT SPAR I/B END OF FLAP. THE RIB WAS REPAIRED PER 727 MM 57-52-0 FIG 808 BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER.Dec 18, 1997 · N8882Z · Boeing 727225 · Trailing Edge FlapsSDR DL72S980400Skin · wornDURING SHOP INSPECTION, THE FLAP WAS FOUND WITH LEADING EDGE SKIN WORN BEYOND ALLOWABLE DAMAGE LIMITS AT O/B END. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGED SKIN AND INSTALLING A FILLER AND DOUBLER PER 727 MM 57-52-0, FIG 803.Dec 18, 1997 · N8882Z · Boeing 727225 · Trailing Edge FlapsSDR DL72S980058Angle · crackedAFT LOWER SPAR CHORD ANGLE IS CRACKED 22 FROM O/B END OF FLAP. REPAIRED PER M/M 57-52-0.Dec 11, 1997 · N8882Z · Boeing 727225 · Trailing Edge FlapsSDR IXKA9700003Battery Pack · dischargedAFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK OK PER MM 33-50-23. (M)Feb 2, 1997 · N8882Z · Boeing 727225 · Emergency LightingSDR IXKA9600075Light · brokenEMERGENCY LIGHT AT L1 DOOR BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND OPS CHECKED OK AS PER MM 33-50-01. (M)Sep 2, 1996 · N8882Z · Boeing 727225 · Emergency Lighting
Back to N8882Z, cancelled Jul 20, 2010