# Service difficulty reports: N8875Z, cancelled Apr 1, 2003

A list on [N8875Z, cancelled Apr 1, 2003](https://openairdocs.org/deregistered/N8875Z-2003-04-01.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 · 87 reports

- [SDR DL72S030148](https://openairdocs.org/sdr/DL72S030148.md): Skin · cracked · Feb 10, 2003 · N8875Z · Boeing 727225A · Fuselage Main, Plate/Skin
  > TWO EXISTING SMALL REPAIR DOUBLERS WERE INSTALLED ON THE AIRCRAFT AT THE UPPER FWD CORNER OF THE L1 DOOR CUTOUT. ONE REPAIR WAS FOR A SMALL CRACK IN THE SKIN AT THE EDGE OF THE DOOR AND THE OTHER FOR A BLENDOUT OF A LIGHTNING STRIKE. BOTH REPAIR WERE TEMPORA
- [SDR DL72S030031](https://openairdocs.org/sdr/DL72S030031.md): Wire · out of position · Jan 6, 2003 · N8875Z · Boeing 727225A · Navigation System Wiring
  > ESSENTIAL POWER AND ALL FWD PANEL LIGHTS ON WITH A/P WAILER GOING OFF THEN LIGHTS WENT TO FULL ON. CREW THEN SMELLED A BURNING ELECTRICAL SMELL. WINDSHEAR C/BS POPPED. FOUND WIRES TO CAPTS AMBER W/S CAUTION LIGHT TERMINALS 2 AND 4 SWAPPED. REPAIRED WIRING
- [SDR DL72S021433](https://openairdocs.org/sdr/DL72S021433.md): Module · malfunctioned · Dec 11, 2002 · N8875Z · Boeing 727225A · Wind Shear Detection System
  > AFTER LEVEL OFF AT 330 ALL BUT 3 OR 4 LIGHTS ON FWD INST PANEL CAME ON. COULD NOT ISOLATE PROBLEM. LIGHTS WENT OUT AFTER 10 MIN AND COCKPIT WAS FILLED WITH STRONG BURNING ELECTRICAL SMELL. WENT TO 02. LANDED ASAP. FOUND WINDSHEAR DC C/B OUT. DURING WINDS
- [SDR DL72S021405](https://openairdocs.org/sdr/DL72S021405.md): Battery Pack · discharged · Dec 3, 2002 · N8875Z · Boeing 727225A · Emergency Lighting
  > LT OVERWING EMERGENCY LIGHT AT FWD MOST POSITION IS INOP. REPLACED BATTERY PACK OPERATES NORMAL.
- [SDR DL72S020624](https://openairdocs.org/sdr/DL72S020624.md): Panel · missing · Jun 4, 2002 · N8875Z · Boeing 727225A · Vertical Stabilizer, Plate/Skin
  > TOP CAP ON VERTICAL STABILIZER MISSING. REPLACED PANEL.
- [SDR DL72S020384](https://openairdocs.org/sdr/DL72S020384.md): Bottle · inoperative · Mar 30, 2002 · N8875Z · Boeing 727225A · Fire Bottle, Fixed
  > NR 1 CARGO FIRE BOTTLE SQUIBS DO NOT TEST. REPLACED NR 1 CARGO FIRE BOTTLE, TEST OK.
- [SDR DL72S020374](https://openairdocs.org/sdr/DL72S020374.md): Stiffener · cracked · Mar 26, 2002 · N8875Z · Boeing 727225A · Wing Miscellaneous Structure
  > OUTBOARD SPAR STIFFENER CRACKED NR 4 SLAT INBOARD TRACK. REPLACED SPAR STIFFENER.
- [SDR DL72S020373](https://openairdocs.org/sdr/DL72S020373.md): Skin · cracked · Mar 26, 2002 · N8875Z · Boeing 727225A · Elevator Structure
  > 2 INCH CRACK R/H ELEVATOR LWR SKIN FWD OF TAB O/B BALANCE WEIGHT REPAIRED PER SRM 55-20-3D
- [SDR DL72S020226](https://openairdocs.org/sdr/DL72S020226.md): Light · inoperative · Feb 24, 2002 · N8875Z · Boeing 727225A · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT IN CEILING, SEAT 25 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY.
- [SDR DL72S020116](https://openairdocs.org/sdr/DL72S020116.md): Battery · discharged · Jan 31, 2002 · N8875Z · Boeing 727225A · Emergency Lighting
  > EMERGENCY LIGHTS ABOVE SEAT 3B WOULD NOT COME ON. REPLACED BATTERY.
- [SDR DL72S020115](https://openairdocs.org/sdr/DL72S020115.md): Battery Pack · discharged · Jan 31, 2002 · N8875Z · Boeing 727225A · Emergency Lighting
  > EMERGENCY LIGHT ABOVE SEAT 3B WOULD NOT COME ON. REPLACED BATTERY AND BATTERY RACK.
- [SDR DL72S011778](https://openairdocs.org/sdr/DL72S011778.md): Attach Fitting · corroded · Nov 6, 2001 · N8875Z · Boeing 727225A · Fuselage, Landing Gear Attach Fittings
  > THE AFT LOWER LUG OF THE FS 940 MLG SUPPORT BEAM ATTACH LINK WAS FOUND WITH CORROSION ON THE FWD FACE OF THE LUG. THE CORROSION WAS REMOVED BY SPOTFACING THE LUG FACE AND SHIMMING THE GAP CREATED. THE WORK WAS ACCOMPLISHED PER ER/A 382016-14, REV A.
- [SDR DL72S011743](https://openairdocs.org/sdr/DL72S011743.md): Beam · corroded · Oct 31, 2001 · N8875Z · Boeing 727225A · Wing, Landing Gear Attach Fittings
  > THE RT MLG BEAM WAS FOUND WITH CORROSION IN THE 2ND LUG LOCATION FROM THE INBOARD END OF THE BEAM. THE CORROSION WAS REMOVED BY OVERSIZING THE HOLE BORE AND MACHINING A.035 INCH SPOTFACE ON THE FWD FACE OF THE LUG. THE BORE WAS RESTORED WITH AN OVERSIZE BU
- [SDR DL72S011702](https://openairdocs.org/sdr/DL72S011702.md): Rib · cracked · Oct 19, 2001 · N8875Z · Boeing 727225A · Wing, Rib/Bulkhead
  > INSPECTION OF THE RBL 70.5 UPPER RIB CHORD AT FS 760.95 ON THE RT WING PER BAC S/B 727-57-0112 AND AD 94-07-08 REVEALED CRACK INDICATIONS IN TWO FASTENER HOLES. THE HOLES WERE OVERSIZED AND BUSHED TO REMOVE THE CRACKS. THE AREA WAS REPAIRED WITH A REPAIR ANG
- [SDR DL72S011701](https://openairdocs.org/sdr/DL72S011701.md): Sill · corroded · Oct 19, 2001 · N8875Z · Boeing 727225A · Fuselage Miscellaneous Structure
  > THE OUTER CHORD OF THE C2 DOOR CUTOUT LOWER SILL STRINGER BEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION ON THE OUTER FLANGE. THE CORROSION WAS REMOVED WITH SEVERAL LOCAL BLENDS AND TRIM OUTS IN THE FLANGE ALONG WITH SEVERAL OVERSIZED FASTENER HOLES. THE CHO
- [SDR DL72S011678](https://openairdocs.org/sdr/DL72S011678.md): Floorbeam · corroded · Oct 2, 2001 · N8875Z · Boeing 727225A · Fuselage Main, Floor Beam
  > FOUND DURING CORROSION MID VISIT INSP MV4. CORROSION ON UPPER SURFACE OF FLOORBEAM STA 344 OUTBOARD OF INBOARD SEAT TRACK. SPLICED IN NEW T-CAP SECTION PER SRM 53-10-8D FIG 802D FROM RBL 10 TO TERMINATION OF FLOORBEAM AT RBL 60.
- [SDR DL72S011351](https://openairdocs.org/sdr/DL72S011351.md): Skin · cracked · Aug 16, 2001 · N8875Z · Boeing 727225A · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / L1 DOOR CUTOUT / FWD EDGE / STRG. 7L: CRACK REPAIR A SMALL CRACK WAS FOUND IN THE SKIN AT THE FWD EDGE OF THE L1 DOOR CUTOUT AT STRINGER 7L BELOW THE UPPER FWD CORNER. THE CRACK WAS REMOVE
- [SDR DL72S011139](https://openairdocs.org/sdr/DL72S011139.md): Actuator · defective · Jul 9, 2001 · N8875Z · Boeing 727225A · Leading Edge Slat Actuator
  > ON FLAP RETRACTION AFTER T/O AMBER L/E FLAP LIGHT ON FWD PANEL REMAINED ILLUMINATED. NR 1 SLAT LIGHT ON S/O PANEL REMAINED ILLUMINATED. FLAPS 5 AND LOWER SHOWED NORMAL IND. REPLACED NR 1 SLAT ACTUATOR. FLAP/SLAT INDICATION OPS, CHECKS OK.
- [SDR DL72S011034](https://openairdocs.org/sdr/DL72S011034.md): Light · inoperative · Jun 22, 2001 · N8875Z · Boeing 727225A · Emergency Lighting
  > FWD GALLEY EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY.
- [SDR DL72S010450](https://openairdocs.org/sdr/DL72S010450.md): Battery · unserviceable · Mar 18, 2001 · N8875Z · Boeing 727225A · Emergency Lighting
  > AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WILL NOT TEST. REPLACED BATTERIES NOW CKS NML
- [SDR DL72S011907](https://openairdocs.org/sdr/DL72S011907.md): Slat · damaged · Jan 30, 2001 · N8875Z · Boeing 727225A · Leading Edge Devices
  > NR 3 SLAT, B727 REPAIRED PER M/M 57-54-000-8 FIG. 814 AND 804, S/N: BN29, P/N: 65-16222-91
- [SDR DL72S010101](https://openairdocs.org/sdr/DL72S010101.md): Skin · cracked · Jan 19, 2001 · N8875Z · Boeing 727225A · Leading Edge Devices
  > A.5 INCH CRACK AT NR 6 SLAT I/B TRACK CUTOUT. REPAIRED PER MM 57-20-021-8.
- [SDR DL72S010100](https://openairdocs.org/sdr/DL72S010100.md): Stiffener · cracked · Jan 19, 2001 · N8875Z · Boeing 727225A · Leading Edge Devices
  > FWD SPAR STIFFENERS CRACKED AT I/B AND O/B SIDES OF NR 7 L/E SLAT I/B TRACK. BOTH REPAIRED PER MM 57-20-021-8.
- [SDR DL72S010099](https://openairdocs.org/sdr/DL72S010099.md): Stiffener · cracked · Jan 19, 2001 · N8875Z · Boeing 727225A · Leading Edge Devices
  > FWD SPAR STIFFENERS CRACKED AT I/B AND O/B SIDES OF NR 6 L/E SLAT I/B TRACK. BOTH REPAIRED PER MM 57-20-021-8.
- [SDR DL72S001447](https://openairdocs.org/sdr/DL72S001447.md): Indicator · inoperative · Aug 1, 2000 · N8875Z · Boeing 727225A · Altimeter, Barometric/Encoder
  > DURING TAXI-OUT, BOTH CAPTS ALTIMETERS DISPLAYED OFF FLAGS. REPLACED LT ALTIMETER.
- [SDR DL72S001200](https://openairdocs.org/sdr/DL72S001200.md): Battery Pack · inoperative · Jun 24, 2000 · N8875Z · Boeing 727225 · Emergency Lighting
  > AFT STAIR EMERG LIGHT INOPERATIVE. REPLACED BATTERY PACK, OP CKS GOOD.
- [SDR DL72S001162](https://openairdocs.org/sdr/DL72S001162.md): Skin · cracked · Jun 15, 2000 · N8875Z · Boeing 727225A · Fuselage Main, Plate/Skin
  > THE LOWER HINGE CUTOUT OF THE FWD PASSENGER DOOR SURROUND SKIN WAS FOUND WITH A.5 TYPICAL CRACK. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER ER/A 377566-14, REV A. THE CRACK IS TYPICAL OF BAC S/B 727-53-0198.
- [SDR DL72S001122](https://openairdocs.org/sdr/DL72S001122.md): Power Supply · inoperative · Jun 9, 2000 · N8875Z · Boeing 727225A · Emergency Lighting
  > CABIN MID SECTION EMER ESCAPE PATH LIGHTS INOP. FOUND ON SERVICE CHECK. REPLACED FORWARD POWER SUPPLY.
- [SDR DL72S000865](https://openairdocs.org/sdr/DL72S000865.md): Light · inoperative · May 1, 2000 · N8875Z · Boeing 727225A · Emergency Lighting
  > DURING SERVICE CHECK AD 8, FOUND EMERGENCY EXIT SIGN ABOVE L-1 DOOR INOP DURING TEST. REPLACED LIGHT ASSY AND BATTERIES, OPS NORMAL.
- [SDR DL72S992497](https://openairdocs.org/sdr/DL72S992497.md): Web · cracked · Nov 11, 1999 · N8875Z · Boeing 727225 · Fuselage Miscellaneous Structure
  > VERT WEB OF LT LOWER TORQUE BOX IN 48 SECTION CRACKED AT STA 1235 AT UPPER RIVET ROW.25 INCH. INSTALLED DOUBLER PER M/M 53-11-0- NR 19, A-1 LETTER CHECK.
- [SDR DL72S991041](https://openairdocs.org/sdr/DL72S991041.md): Engine · failed · May 11, 1999 · N8875Z · Boeing 727225A · Engine (Turbine/Turboprop)
  > NR 3 ENGINE BLEED TRIP IN FLIGHT. AIRCRAFT RETURNED TO DFW. REPLACED NR 3 ENGINE 13 STAGE PRESSURE REGULATOR. TIGHTENED 2 LINES, LEAK CHECKS GOOD.
- [SDR DL72S991038](https://openairdocs.org/sdr/DL72S991038.md): Epr Indicator · fluctuates · May 11, 1999 · N8875Z · Boeing 727225A · Engine Pressure Ratio (EPR)
  > REJECTED TAKEOFF AT DFW DUE TO NR 1 ENGINE EGT FLUCUATION SPEED 70 KTS. TIGHTENED TWO JUNCTIONS AND REPLACED INDICATOR, RAN ENGINE.
- [SDR DL72S990895](https://openairdocs.org/sdr/DL72S990895.md): Beam · corroded · Apr 23, 1999 · N8875Z · Boeing 727225A · Spoilers
  > AD 90-07-05 AND 90-06-09, NR 4 INB'D FLAP TRACK, TYP CORROSION AT MLG BEAM AND SPOILER BEAM ATTACH PADS. DURING OVERHAUL OF FLAP TRACK, CORROSION WAS FOUND AT THE MLG BEAM AND SPOILER BEAM ATTACH PADS AND BOLT HOLES. THE PADS WERE MACHINED AND THE HOLES OVER
- [SDR DL72S991020](https://openairdocs.org/sdr/DL72S991020.md): Skin · worn · Apr 16, 1999 · N8875Z · Boeing 727225 · Trailing Edge Flaps
  > LOWER L/E SKIN WORN APPROX 3 INCH LONG AREA O/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 803.
- [SDR DL72S990823](https://openairdocs.org/sdr/DL72S990823.md): Stringer · cracked · Apr 13, 1999 · N8875Z · Boeing 727225 · Wing, Longeron/Stringer
  > TWO CRACKS WERE FOUND; ONE IN S9L AND THE OTHER IN S10L ON THE LT WING AT WS 656.5. BOTH CRACKS ARE LOCATED ON THE LWR HORIZ LEG OF THE ZEE STRINGERS. REPAIRED PER ERA 333023-14AD.
- [SDR DL72S990821](https://openairdocs.org/sdr/DL72S990821.md): Stringer · cracked · Apr 13, 1999 · N8875Z · Boeing 727225 · Vertical Stabilizer
  > VERTICAL STAB S7 WAS FOUND CRACKED AT STA 157.2 DURING INSP PER SI 4-59253-12AD. REPAIRED PER ERA 333025-14A.D
- [SDR DL72S990820](https://openairdocs.org/sdr/DL72S990820.md): Skin · cracked · Apr 13, 1999 · N8875Z · Boeing 727225 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING HFEC INSPECTIONS PER SI 4-47176-12AD, REV F, A CRACK INDICATION WAS FOUND AT TWO FASTENER LOCATIONS BETWEEN BS 560 AND BS 580 AT S26L. REPAIRED PER ERA 332999-14AD.
- [SDR DL72S991051](https://openairdocs.org/sdr/DL72S991051.md): Skin · cracked · Apr 9, 1999 · N8875Z · Boeing 727225A · Trailing Edge Flaps
  > DURING SHOP INSPECTION THE COVE SKIN WAS FOUND CRACKED 32 INCHES FROM THE I/B END OF MIDFLAP. THE COVE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 809.
- [SDR DL72S990773](https://openairdocs.org/sdr/DL72S990773.md): Spar · misrepaired · Apr 9, 1999 · N8875Z · Boeing 727225 · Trailing Edge Flaps
  > NR 2 MIDFLAP/UPPER SPAR CHORD, WBL 124 ALT FASTENER INSTALL DURING ACCOMPLISHMENT OF EO 4-58705-3AD (REF SB 727-57-160). MAINTENANCE UNABLE TO INSTALL REQUIRED HI-LOCK COLLAR ON SPAR-TO-SKIN ATTACH HOLE DUE TO INTERFERENCE WITH SPAR RADIUS. AUTHORIZED USE OF
- [SDR DL72S991033](https://openairdocs.org/sdr/DL72S991033.md): Spar · cracked · Apr 1, 1999 · N8875Z · Boeing 727225A · Trailing Edge Flaps
  > AFT SPAR RAIL CRACKED, 62 INCHES FROM I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 802.
- [SDR DL72S991032](https://openairdocs.org/sdr/DL72S991032.md): Spar · damaged · Apr 1, 1999 · N8875Z · Boeing 727225A · Trailing Edge Flaps
  > TEMPORARY REPAIR AFT SPAR RAIL, 47 INCHES FROM I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 802.
- [SDR DL72S991031](https://openairdocs.org/sdr/DL72S991031.md): Spar · damaged · Apr 1, 1999 · N8875Z · Boeing 727225A · Trailing Edge Flaps
  > TWO CRACKS AT AFT SPAR RAIL, 34 INCHES FROM I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 802.
- [SDR DL72S990793](https://openairdocs.org/sdr/DL72S990793.md): S Duct · cracked · Mar 31, 1999 · N8875Z · Boeing 727225 · Nacelle/Pylon Structure
  > FLANGE CRACKED AND DENTED SEVERAL PLACES, FWD FLANGE ON UPPER S DUCT SECT. BEGAN REMOVAL OF FASTENERS ON UPPER S DUCT FLANGES. COMPLETED REMOVAL OF FASTENERS. BEGAN FABRICATIONS REPAIR PIECES. COMPLETED FABRICATING REPAIR PIECES PER SRM 54-10-3 FIG 13. DY
- [SDR DL72S981780](https://openairdocs.org/sdr/DL72S981780.md): Valve · cracked · Aug 28, 1998 · N8875Z · Boeing 727225 · Landing Gear Retraction/Extension System
  > AIR RETURN, HYD FAILURE RT MAIN GEAR UPLOCK SEQUENCING VLV. HOUSING CRACKED. REPLACED VALVE.
- [SDR DL72S981558](https://openairdocs.org/sdr/DL72S981558.md): Frame · corroded · Jul 24, 1998 · N8875Z · Boeing 727225 · Fuselage Miscellaneous Structure
  > FUSELAGE C1 DOOR CUTOUT AFT (STA 620) DOOR JAMB FRAME INNER CHORD S-25R, SPLICE REPAIR. THE INNER CHORD OF THE C1 DOOR CUTOUT AFT JAMB FRAME AT FS 620 WAS FOUND BADLY CORRODED BELOW S-25R. THE INNER CHORD WAS CUT NEAR S-25R AND A NEW LOWER SECTION INSTALLED.
- [SDR DL72S981516](https://openairdocs.org/sdr/DL72S981516.md): Web · part · Jul 21, 1998 · N8875Z · Boeing 727225 · Fuselage Miscellaneous Structure
  > VERTICLE WEB CRACKED STA 1224 LBL 24 ABOVE EXISTING REPAIR. REPAIRED PER M/M 53-11-0 PG 832.
- [SDR DL72S981515](https://openairdocs.org/sdr/DL72S981515.md): Web · cracked · Jul 21, 1998 · N8875Z · Boeing 727225 · Fuselage Miscellaneous Structure
  > VERTICLE WEB CRACKED APPROX.25 INCH LONG AT LIGHTNING HOLE STA 1240. REPAIRED PER M/M 53-11-0 PG 832.
- [SDR DL72S981514](https://openairdocs.org/sdr/DL72S981514.md): Web · cracked · Jul 21, 1998 · N8875Z · Boeing 727225 · Fuselage Miscellaneous Structure
  > VERTICLE WEB DAMAGED AT LIGHTNING HOLE RT SIDE STA 1263- 2. VERTICLE WEB DAMAGED AT LIGHTNING HOLE RT SIDE STA 1228. REPAIRED PER M/M 53-11-0 PG 828.
- [SDR DL72S981155](https://openairdocs.org/sdr/DL72S981155.md): Connector · dirty · May 31, 1998 · N8875Z · Boeing 727225 · Aircraft Fuel Distribution System
  > ON DEPARTURE, COULD NOT CROSSFEED NR 1 ENG OFF OF FUEL TANKS NR 2 OR NR 3. REMOVED LOCKWIRE FROM VALVE. CLEANED CANNON PLUG AND MOTOR PLUG. OPN OF VALVE NML. REMOVED MCO AND PLACARD.
- [SDR DL72S972655](https://openairdocs.org/sdr/DL72S972655.md): Batteries · discharged · Dec 16, 1997 · N8875Z · Boeing 727225 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR IS INOP. REPLACED LIGHT ASSY AND BATTERIES. OPS NORMAL.

Next page: https://openairdocs.org/deregistered/N8875Z-2003-04-01/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 = 'N8875Z' AND deregistration_id = 'N8875Z-2003-04-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8875Z-2003-04-01/reports

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