# Service difficulty reports: N8882Z, cancelled Jul 20, 2010

A list on [N8882Z, cancelled Jul 20, 2010](https://openairdocs.org/deregistered/N8882Z-2010-07-20.md).

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

Page 1 of 2 · 58 reports

- [SDR DL72S030304](https://openairdocs.org/sdr/DL72S030304.md): Proximity Sensor · out of adjust · Mar 31, 2003 · N8882Z · Boeing 727225A · Engine Thrust Reverser
  > ON T/O AT APPROX 80 KTS NR 3 REVERSER LIGHT CAME ON. T/O ABORTED. ADJUSTED PROX SWITCH.
- [SDR DL72S030279](https://openairdocs.org/sdr/DL72S030279.md): Fairing · loose · Mar 26, 2003 · N8882Z · Boeing 727225A · Trailing Edge Flaps
  > AT 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.
- [SDR DL72S021475](https://openairdocs.org/sdr/DL72S021475.md): Rib · cracked · Dec 26, 2002 · N8882Z · Boeing 727225A · Empennage Structure
  > VERT. STAB RIB L/H ATTACH ANGLE CRACKED AT FIN STA 133.800 AND STR 9LEFT REPAIR PER M/M 55-30-000-8
- [SDR DL72S020642](https://openairdocs.org/sdr/DL72S020642.md): Warning System · activated · Jun 9, 2002 · N8882Z · Boeing 727225A · Landing Gear Position and Warning
  > CREW REPORTS NOSE GEAR UNSAFE INDICATION AND VIBRATION ON GEAR RETRACTION. JACKED NOSE AND SWUNG GEAR, ALL OPS NORMAL.
- [SDR DL72S020571](https://openairdocs.org/sdr/DL72S020571.md): Skin · cracked · May 17, 2002 · N8882Z · Boeing 727225A · Fuselage Main, Plate/Skin
  > THE 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.
- [SDR DL72S020549](https://openairdocs.org/sdr/DL72S020549.md): Stringer · corroded · May 14, 2002 · N8882Z · Boeing 727225A · Fuselage Main, Longeron/Stringer
  > FOUND ON D1 LETTER CK, CORROSION AT STR 28 RT AT STA 620. REPAIRED PER SRM 53-10-3.
- [SDR DL72S011714](https://openairdocs.org/sdr/DL72S011714.md): Skin · cracked · Oct 21, 2001 · N8882Z · Boeing 727225A · Fuselage Main, Plate/Skin
  > FUSELAGE / 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 7
- [SDR DL72S011688](https://openairdocs.org/sdr/DL72S011688.md): Skin · cracked · Oct 18, 2001 · N8882Z · Boeing 727225A · Fuselage Structure (General)
  > FOUND 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.
- [SDR DL72S011451](https://openairdocs.org/sdr/DL72S011451.md): Charger · inoperative · Aug 29, 2001 · N8882Z · Boeing 727225A · Emergency Lighting
  > L-1 WING EMERGENCY EXIT LIGHT INOP, REPLACED CHARGER.
- [SDR DL72S010282](https://openairdocs.org/sdr/DL72S010282.md): Battery Pack · discharged · Feb 17, 2001 · N8882Z · Boeing 727225A · Emergency Lighting
  > ON L/O CHECK, FOUND R-2 OVERHEAD EMERGENCY EXIT DOOR LIGHT INOP. REPLACED R-2 OVERHEAD EMERGENCY EXIT DOOR BATTERY PACK, OPS NOW NORMAL.
- [SDR DL72S002502](https://openairdocs.org/sdr/DL72S002502.md): Frame · cracked · Dec 21, 2000 · N8882Z · Boeing 727225A · Fuselage Main, Frame
  > FUSELAGE / 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 REPAIRED
- [SDR DL72S002006](https://openairdocs.org/sdr/DL72S002006.md): Start Valve · failed · Oct 13, 2000 · N8882Z · Boeing 727225A · Engine Start Valves/Controls
  > NR 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 O
- [SDR DL72S001506](https://openairdocs.org/sdr/DL72S001506.md): Web · cracked · Aug 9, 2000 · N8882Z · Boeing 727225A · Fuselage Miscellaneous Structure
  > A 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.
- [SDR DL72S001463](https://openairdocs.org/sdr/DL72S001463.md): Skin · corroded · Aug 2, 2000 · N8882Z · Boeing 727225A · Fuselage Main, Plate/Skin
  > THE 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 W
- [SDR DL72S001424](https://openairdocs.org/sdr/DL72S001424.md): Beam · tool damage · Jul 27, 2000 · N8882Z · Boeing 727225A · Fuselage Miscellaneous Structure
  > WHILE 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 INS
- [SDR DL72S001126](https://openairdocs.org/sdr/DL72S001126.md): Valve · inoperative · Jun 10, 2000 · N8882Z · Boeing 727225A · Cabin Pressure Control System
  > LEFT 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.
- [SDR DL72S001015](https://openairdocs.org/sdr/DL72S001015.md): Battery Pack · inoperative · May 24, 2000 · N8882Z · Boeing 727225A · Emergency Lighting
  > OVERWING EMERG LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72S991844](https://openairdocs.org/sdr/DL72S991844.md): Stringer · cracked · Aug 9, 1999 · N8882Z · Boeing 727225 · Vertical Stabilizer
  > VERTICAL STAB INTERIOR, STRINGER CRACKED AT TIE TO RIB LEFT SIDE AT FIN STA 1338. INSTALLED REPAIR PER SRM 55-30-0 FIG 803.
- [SDR DL72S991317](https://openairdocs.org/sdr/DL72S991317.md): Angle · cracked · Jun 10, 1999 · N8882Z · Boeing 727225A · Fuselage Miscellaneous Structure
  > MLG 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.
- [SDR DL72S991316](https://openairdocs.org/sdr/DL72S991316.md): Frame · cracked · Jun 10, 1999 · N8882Z · Boeing 727225A · Fuselage Miscellaneous Structure
  > LTR CHECK A2, 1 INCH CRACK AT C-2 DOOR CUTOUT FWD FRAME WEB AT LOWER END. REPAIRED PER SRM 53-10-4.
- [SDR DL72S991314](https://openairdocs.org/sdr/DL72S991314.md): Web · cracked · Jun 10, 1999 · N8882Z · Boeing 727225A · Fuselage Miscellaneous Structure
  > FOUND ON A2 LETTER CK..25 INCH CRACK AT RT TORQUE BOX VERT WEB LOWER LIGHTENING HOLE STA 1243. REPAIRED PER MM 53-11-0.
- [SDR DL72S991313](https://openairdocs.org/sdr/DL72S991313.md): Web · cracked · Jun 10, 1999 · N8882Z · Boeing 727225A · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR DL72S991099](https://openairdocs.org/sdr/DL72S991099.md): Sign · inoperative · May 18, 1999 · N8882Z · Boeing 727225 · Emergency Lighting
  > EMERGENCY EXIT SIGN OVER 2R SERVICE DOOR FLICKERS FROM DIM TO BRIGHT WITH EMERGENCY LIGHT SYSTEM OFF.
- [SDR DL72S990732](https://openairdocs.org/sdr/DL72S990732.md): Valve · leaking · Apr 3, 1999 · N8882Z · Boeing 727225 · Hydraulic System, Main
  > LOSS OF B HYD IN FLT. REPLACED LEAKING CHECK VALVE IN LEFT WHEEL WELL.
- [SDR DL72S990401](https://openairdocs.org/sdr/DL72S990401.md): Wire · cracked · Feb 26, 1999 · N8882Z · Boeing 727225A · Electrical Power System Wiring
  > ON 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).
- [SDR DL72S990368](https://openairdocs.org/sdr/DL72S990368.md): Skin · damaged · Feb 22, 1999 · N8882Z · Boeing 727225A · Fuselage Main, Plate/Skin
  > INCORPORATION 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 EXIS
- [SDR DL72S990323](https://openairdocs.org/sdr/DL72S990323.md): Angle · corroded · Feb 18, 1999 · N8882Z · Boeing 727225A · Nacelle/Pylon Structure
  > ON HUSH-KIT MOD, FOUND NR 2 ENG AFT MOUNT CHORD ANGLE CORRODED BEYOUND MFG SPECS. REPLACED CHORD ANGLE WITH NEW MFG RT SIDE.
- [SDR DL72S990322](https://openairdocs.org/sdr/DL72S990322.md): Cord Angle · new · Feb 17, 1999 · N8882Z · Boeing 727225A · Empennage Structure
  > ON HUSH-KIT MOD, FOUND LT NR 2 ENG MOUNT CHORD ANGLE CORRODED BEYOUND MFG SPECS. REPLACED CHORD ANGLE WITH ANGLE OF NEW MFG.
- [SDR DL72S982629](https://openairdocs.org/sdr/DL72S982629.md): Valve · failed · Dec 26, 1998 · N8882Z · Boeing 727225 · Cabin Cooling System
  > LEFT PACK ON, CAUSED SMOKE IN CABIN. REPLACED FWD PACK VALVE AND MIX VALVE. CK OK.
- [SDR DL72S982277](https://openairdocs.org/sdr/DL72S982277.md): Web · cracked · Nov 5, 1998 · N8882Z · Boeing 727225 · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR DL72S982276](https://openairdocs.org/sdr/DL72S982276.md): Web · cracked · Nov 5, 1998 · N8882Z · Boeing 727225 · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR DL72S982275](https://openairdocs.org/sdr/DL72S982275.md): Rib · cracked · Nov 5, 1998 · N8882Z · Boeing 727225 · Leading Edge Devices
  > FOUND 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.
- [SDR DL72S981552](https://openairdocs.org/sdr/DL72S981552.md): Battery Pack · discharged · Jul 24, 1998 · N8882Z · Boeing 727225 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT INOP RT SIDE 2ND LIGHT AFT OF OVERWING ESCAPE HATCHES. REPLACED BULBS, BATTERY PACK, CLEANED SOCKETS AND CHECKS OK.
- [SDR DL72S981551](https://openairdocs.org/sdr/DL72S981551.md): Light · inoperative · Jul 24, 1998 · N8882Z · Boeing 727225 · Emergency Lighting
  > EMERGENCY LIGHT INOP ABOVE AFT AIRSTAIR BOTTOM STEP IN CEILING. RELAMPED AND CLEANED SOCKET, CHECKS OK.
- [SDR DL72S981102](https://openairdocs.org/sdr/DL72S981102.md): Outflow Valve · stuck · May 22, 1998 · N8882Z · Boeing 727225 · Pressure Regulator/Outflow Valve
  > AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. ALL MODES TRIED, PULLED AND RESET C/B, NO HELP. REPLACED OUTFLOW VALVE AND PRESSURE CONTROLLER AND CONTROL PANEL.
- [SDR DL72S980991](https://openairdocs.org/sdr/DL72S980991.md): Battery Pack · discharged · May 11, 1998 · N8882Z · Boeing 727225 · Emergency Lighting
  > EMERGENCY EXIT LIGHT M1088 FAIL TEST. REPLACED BATTERY PACK, CHECKS OK.
- [SDR DL72S980850](https://openairdocs.org/sdr/DL72S980850.md): Frame · corroded · Apr 20, 1998 · N8882Z · Boeing 727225 · Fuselage Main, Frame
  > INBD 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.
- [SDR DL72S980798](https://openairdocs.org/sdr/DL72S980798.md): Skin · damaged · Apr 10, 1998 · N8882Z · Boeing 727225 · Fuselage Main, Plate/Skin
  > AN 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 INSTALLED
- [SDR DL72S980785](https://openairdocs.org/sdr/DL72S980785.md): Floorbeam · corroded · Apr 7, 1998 · N8882Z · Boeing 727225 · Fuselage Main, Floor Beam
  > THE 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.
- [SDR DL72S980510](https://openairdocs.org/sdr/DL72S980510.md): Skin · worn · Feb 18, 1998 · N8882Z · Boeing 727225 · Trailing Edge Flaps
  > DURING 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.
- [SDR DL72S980324](https://openairdocs.org/sdr/DL72S980324.md): Spar · cracked · Dec 23, 1997 · N8882Z · Boeing 727225 · Wing Spar
  > AFT 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
- [SDR DL72S980156](https://openairdocs.org/sdr/DL72S980156.md): Angle · cracked · Dec 22, 1997 · N8882Z · Boeing 727225 · Trailing Edge Flaps
  > THE 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.
- [SDR DL72S980155](https://openairdocs.org/sdr/DL72S980155.md): Angle · cracked · Dec 22, 1997 · N8882Z · Boeing 727225 · Trailing Edge Flaps
  > THE 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.
- [SDR DL72S980154](https://openairdocs.org/sdr/DL72S980154.md): Cove Skin · cracked · Dec 22, 1997 · N8882Z · Boeing 727225 · Trailing Edge Flaps
  > DURING 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.
- [SDR DL72S980153](https://openairdocs.org/sdr/DL72S980153.md): Angle · cracked · Dec 22, 1997 · N8882Z · Boeing 727225 · Trailing Edge Flaps
  > DURING 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.
- [SDR DL72S980509](https://openairdocs.org/sdr/DL72S980509.md): Rib · cracked · Dec 18, 1997 · N8882Z · Boeing 727225 · Trailing Edge Flaps
  > DURING 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.
- [SDR DL72S980400](https://openairdocs.org/sdr/DL72S980400.md): Skin · worn · Dec 18, 1997 · N8882Z · Boeing 727225 · Trailing Edge Flaps
  > DURING 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.
- [SDR DL72S980058](https://openairdocs.org/sdr/DL72S980058.md): Angle · cracked · Dec 11, 1997 · N8882Z · Boeing 727225 · Trailing Edge Flaps
  > AFT LOWER SPAR CHORD ANGLE IS CRACKED 22 FROM O/B END OF FLAP. REPAIRED PER M/M 57-52-0.
- [SDR IXKA9700003](https://openairdocs.org/sdr/IXKA9700003.md): Battery Pack · discharged · Feb 2, 1997 · N8882Z · Boeing 727225 · Emergency Lighting
  > AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK OK PER MM 33-50-23. (M)
- [SDR IXKA9600075](https://openairdocs.org/sdr/IXKA9600075.md): Light · broken · Sep 2, 1996 · N8882Z · Boeing 727225 · Emergency Lighting
  > EMERGENCY LIGHT AT L1 DOOR BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND OPS CHECKED OK AS PER MM 33-50-01. (M)

Next page: https://openairdocs.org/deregistered/N8882Z-2010-07-20/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N8882Z-2010-07-20/reports

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