# Service difficulty reports: N468DA, cancelled Apr 18, 2000

A list on [N468DA, cancelled Apr 18, 2000](https://openairdocs.org/deregistered/N468DA-2000-04-18.md).

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

- [SDR DL72S982339](https://openairdocs.org/sdr/DL72S982339.md): Battery Pack · discharged · Nov 12, 1998 · N468DA · Boeing 727232 · Emergency Lighting
  > RIGHT AFT OVERWING EXIT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72S981339](https://openairdocs.org/sdr/DL72S981339.md): Skin · cracked · Jun 25, 1998 · N468DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND ON F2 LETTER CK, CRACK IN SKIN I/B AFT CORNER OF GROUND AIR CONNECTION PANEL. REPAIRED PER MM 53-30-0.
- [SDR DL72S980795](https://openairdocs.org/sdr/DL72S980795.md): Rack · inoperative · Apr 12, 1998 · N468DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHT OVER AFT LEFT DOOR INOP. REPLACED RACK, OPN GOOD.
- [SDR DL72S980323](https://openairdocs.org/sdr/DL72S980323.md): Clamp · broken · Feb 6, 1998 · N468DA · Boeing 727232 · Pneumatic Distribution System
  > AT CRUISE, GOT NR 1 ENG FIRE WARNING. SHUTDOWN ENGINE. REPLACED CLAMP ON 13TH STG DUCT AND REPAIRED BURNED WIRES.
- [SDR DL72S980236](https://openairdocs.org/sdr/DL72S980236.md): Battery Pack · discharged · Jan 28, 1998 · N468DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHTS AT L-1, L-2, R-2 ABOVE DOOR INOP. REPLACED EMERGENCY BATTERIES PACK AT L-1, L-2, R-2. EMERGENCY LIGHTS CHECK GOOD.
- [SDR DL72S972699](https://openairdocs.org/sdr/DL72S972699.md): Skin · corroded · Dec 19, 1997 · N468DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CORRODED AT THE STRINGER 26L LAPSPLICE BETWEEN FS 575 AND 613. THE CORRODED AREA WAS CUTOUT AND A REPAIR DOUBLER INSTALLED. AREAS FWD AND AFT OF THE CUTOUT WERE INSPECTED TO ENSURE NO FURTHER CORROSION WAS PRESENT. THE REPAIR
- [SDR DL72S972438](https://openairdocs.org/sdr/DL72S972438.md): Cable · out of adj · Nov 22, 1997 · N468DA · Boeing 727232 · Entrance Stairs
  > AFT AIRSTAIRS OPENED IN FLIGHT. FOUND OVERCENTER BUNGEE WEAK. REPLACED T/S AFT AIRSTAIRS. REPLACED UPLOCK SW, CHECKED AND ADJ CABLE RIGGING PER M/M 52-62-01, SYS OPS CKS NORMAL. INSPECTED AFT AIRSTAIR UPLOCK LINKAGE, NO SHEARED BOLTS OR OBVIOUS DAMAGE.
- [SDR DL72S972474](https://openairdocs.org/sdr/DL72S972474.md): Skin · corroded · Nov 21, 1997 · N468DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CORRODED AT THE S-26L LAP SPLICE AT STA 575. THE SKIN DAMAGE IS ADJACENT TO A PREVIOUSLY INSTALLED INTERNAL REPAIR. THE NEW DAMAGE WAS REPAIRED WITH AN OVERLAPPING DOUBLER PER ER/A 363252-14, REV A.
- [SDR DL72S972466](https://openairdocs.org/sdr/DL72S972466.md): Skin · cracked · Nov 21, 1997 · N468DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE/ F-N WINDOW POST: REPAIR FOR SKIN CRACK. A.75 INCH CRACK WAS FOUND IN THE SKIN AT THE UPPER AFT CORNER OF THE R5 WINDOW AT THE F-N WINDOW POST. THE CRACK WAS ABOVE AN EXISTING WINDOW POST MOD STRAP. THE CRACK WAS STOP DRILLED AND REPAIRED WITH
- [SDR DL72S972381](https://openairdocs.org/sdr/DL72S972381.md): Battery · discharged · Nov 16, 1997 · N468DA · Boeing 727232 · Emergency Lighting
  > FWD AND AFT EMERGENCY PATH LIGHTS INOP. REPLACED FWD AND AFT BATTERY PACKS, OK.
- [SDR DL72S972274](https://openairdocs.org/sdr/DL72S972274.md): Air Distribution · odor · Nov 6, 1997 · N468DA · Boeing 727232 · Air Distribution System
  > ELECTRICAL FUMES AND HEAT AT SEAT 17F. FOUND AFT CABIN ZONE TRIM VALVE OPEN SUPPLYING DUCT HOT AIR IN THE AREA OF 17F. RESET CABIN TEMP TRIM ALL A/C SYSTEMS CKS NML. NO ELECTRICAL ODORS IN CABIN, ALL INSPECTIONS OK.
- [SDR DL72S971711](https://openairdocs.org/sdr/DL72S971711.md): Actuator · leaking · Aug 31, 1997 · N468DA · Boeing 727232 · Leading Edge Slat Actuator
  > SYS-A HYD PRESSURE AND QUANTITY WENT TO ZERO DURING CLIMBOUT. REPLACED NR 3 L/E SLAT.
- [SDR DL72S971444](https://openairdocs.org/sdr/DL72S971444.md): Blkhd Stiffener · cracked · Jul 10, 1997 · N468DA · Boeing 727232 · Fuselage Main, Bulkhead
  > A CRACK WAS FOUND IN THE VERTICAL STIFFENER AT RBL 36.83 ON THE FORWARD SIDE OF THE BS 1183 BULKHEAD. THE CRACK IS APPROX.5 INCH LONG AND IS LOCATED AT APPROX WL 249 IN THE INB'D RADIUS OF THE AFT CHORD. THIS AREA IS ADDRESSED IN EO 4-59821-3, WHICH INCORPO
- [SDR DL72S971421](https://openairdocs.org/sdr/DL72S971421.md): Skin · worn · Jul 7, 1997 · N468DA · Boeing 727232 · Leading Edge Devices
  > NR 4 L/E SLAT INNER SKIN WORN AND GOUGED I/B OF ACTUATOR. REPAIRED PER B-727 M/M57-54-0, FIG 801.
- [SDR DL72S970832](https://openairdocs.org/sdr/DL72S970832.md): Beam · cracked · Apr 30, 1997 · N468DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND CRACKS IN THE RT TORQUE BOX UPPER FORWARD TRANSVERSE BEAMS AT FS 1263 AND 1273. THIS AREA SUBJECT TO AD 94-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. REPLACED PARTS IN ACCORDANCE WITH THE S/B.
- [SDR DL72S970801](https://openairdocs.org/sdr/DL72S970801.md): Skin · cracked · Apr 29, 1997 · N468DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > FOUND TWO CRACKS AT RT SIDE OF VERTICAL STABILIZER SKIN APPROX STA 1203. REPAIRED PER MM 54-30-0.
- [SDR DL72S970493](https://openairdocs.org/sdr/DL72S970493.md): Light · missing · Mar 16, 1997 · N468DA · Boeing 727232 · Emergency Lighting
  > FOUND EMERGENCY TRACK LIGHT MISSING AT 30 DEF. REPAIRED: REPLACED LIGHT ASSY- OPN CKS GOOD.
- [SDR DL72S961160](https://openairdocs.org/sdr/DL72S961160.md): Shim · out of position · May 13, 1996 · N468DA · Boeing 727232 · Trailing Edge Flaps
  > DURING INSPECTIONS PER SI 4-58663-12AD, THE LAMINATED SHIMS INSTALLED ON THE RIGHT AND LEFT WING INBOARD TRAILING EDGE FLAP INBOARD TRACKS WERE FOUND TO HAVE MIGRATED GREATER THAN THE 0.25 LIMIT SPECIFIED IN THE INSPECTION. IN COMPLIANCE WITH AD 90-07-05, THE
- [SDR DL72S960465](https://openairdocs.org/sdr/DL72S960465.md): Skin · corroded · Feb 29, 1996 · N468DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND CORRODED ALONG THE S-26L LAP JOINT AT STA 700. REMOVAL OF THE CORROSION RESULTED IN A 3 INCH WIDE BY 10 INCH LONG CUT OUT IN THE OVERLAPPING SKIN ONLY. A PREVIOUS REPAIR DOUBLER IS LOCATED WITHIN 2 INCHES OF THI
- [SDR DL72S960464](https://openairdocs.org/sdr/DL72S960464.md): Skin · cracked · Feb 29, 1996 · N468DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, THE SKIN AT STA 312 AND S-22R WAS FOUND TO HAVE TWO CRACKS EMANATING FROM FASTENERS. ALSO, A PREVIOUS REPAIR WAS INSTALLED JUST BELOW THE TWO CRACKS. IN ACCORDANCE WITH B727 SRM 53-30-3 FIG 3, BOTH DAMAGE LOCATIONS WERE INCORPORATED UNDER
- [SDR DL72S960456](https://openairdocs.org/sdr/DL72S960456.md): Skin · cracked · Feb 28, 1996 · N468DA · Boeing 727232 · Passenger/Crew Doors
  > MAIN ENTRY DOOR OUTER SKIN CRACKED.25 INCH AT RIVET TOP AFT CORNER. FOUND AT D-2 LTR CHECK. REPAIRED PER MM 52-11-01 FIG 804.
- [SDR DL72S954536](https://openairdocs.org/sdr/DL72S954536.md): Eel · inoperative · Nov 27, 1995 · N468DA · Boeing 727232 · Emergency Lighting
  > AFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY.
- [SDR DL72S953427](https://openairdocs.org/sdr/DL72S953427.md): Eel Lamp · inop · Aug 18, 1995 · N468DA · Boeing 727232 · Emergency Lighting
  > FOUND ON L/O EMERGENCY LIGHT PATH, LIGHT OUT AND LENS MISSING R2 DOOR. REPLACED LAMP HOLDER, BULB AND LENS. OPS CK GOOD.
- [SDR DL72S953243](https://openairdocs.org/sdr/DL72S953243.md): Web · crack · Jul 31, 1995 · N468DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A 2.5 AND 1 INCH CRACK BELOW LOAD CONTROL VALVE CUTOUT, BS 870 WEB RT WW. FOUND AT D-1 LTR CK. REPAIRED PER SRM 53-10-9.
- [SDR DL72S952910](https://openairdocs.org/sdr/DL72S952910.md): Skin · damaged · Jun 19, 1995 · N468DA · Boeing 727232 · Ailerons
  > DURING A SHOP INSPECTION, THE SKIN ON THE LOWER INBD SECTION WAS FOUND TO HAVE SEVERAL DENTS AND ELONGATED HOLES, IN WHICH RIVETS WERE PULLING THROUGH. A SKIN SPLICE REPAIR WAS INSTALLED PER THE M/M 57-51-0 FOR THE LEFT OUTBOARD AILERON.
- [SDR DL72S952852](https://openairdocs.org/sdr/DL72S952852.md): Skin · damaged · Jun 19, 1995 · N468DA · Boeing 727232 · Ailerons
  > DURING A SHOP INSPECTION, THE LOWER OUTBOARD SKIN WAS FOUND TO HAVE SEVERAL FASTENERS PULLING THROUGH THE SKIN. A REPAIR WAS INSTALLED PER THE M/M 57-51-0, FOR LEFT OUTBOARD AILERON.
- [SDR DL72S960394](https://openairdocs.org/sdr/DL72S960394.md): Web · cracked · Mar 16, 1995 · N468DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL CRACKED BETWEEN STA 294.5 AND 285.5 APPROXIMATELY AT WL 170. THE CRACK IS APPROXIMATELY 1.75 INCH IN LENGTH. IN ACCORDANCE WITH S/B 727-53-145, THE WEB WAS TRIMMED OUT AND A REPAIR DOUBLER A
- [SDR DL72S951147](https://openairdocs.org/sdr/DL72S951147.md): Door · cracked · Mar 14, 1995 · N468DA · Boeing 727232 · Service Doors
  > FOUND DURING CV-2 L/O CHK,.5 INCH CRACK IN FWD SVC DOOR FWD UPPER CORNER. REPAIRED PER MM 52-12-0 PG 808.
- [SDR DL72S951094](https://openairdocs.org/sdr/DL72S951094.md): Skin · corroded · Mar 10, 1995 · N468DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND ON CV2 CHECK, CORROSION ON SKIN O/B SIDE STR 28L UNDER INNER COSTAL AFT OF STA 480. REPAIRED PER SRM 53-30-3 FIG 1.
- [SDR DL72S951055](https://openairdocs.org/sdr/DL72S951055.md): Skin · cracked · Mar 7, 1995 · N468DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND ON CV2 CHECK, SKIN DAMAGED AT STR 27L BETWEEN 720A AND 720B. REPAIRED PER SRM 53-30-3 FIG 3.
- [SDR DL72S951098](https://openairdocs.org/sdr/DL72S951098.md): Skin · corroded · Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND ON CV2 CHECK, CORROSION LEFT SIDE OF STRINGER SPLICE STR 28L STA 480. REPAIRED SKIN PER SRM 53-30-3 FIG 3. REPLACED FACTORY SPLICE WITH SAME.
- [SDR DL72S951097](https://openairdocs.org/sdr/DL72S951097.md): Z Angle · corroded · Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON CV2 CHECK, CORROSION FOUND ON 'Z' ANGLE ABOVE STR 27R JUST FWD OF STA 620. REPAIRED PER ERA 301345-14 CODE 4-53-21-04.
- [SDR DL72S951096](https://openairdocs.org/sdr/DL72S951096.md): Floor Support · corroded · Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON CV2 CHECK, FLOOR SUPPORT 'Z' CHANNEL CORRODED AT FASTNER HOLES ABOVE STR 27R STA 620-640. REPAIRED PER ERA 301345-14 CODE 4-53-21-04.
- [SDR DL72S951095](https://openairdocs.org/sdr/DL72S951095.md): Stringer · corroded · Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND ON CV2 CHECK, STR 27L AT STA 720D TO FWD OF STA 720C, WITH CORROSION DAMAGE, REPAIRED PER ERA 30133744.
- [SDR DL72S950978](https://openairdocs.org/sdr/DL72S950978.md): Stringer · corroded · Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND ON CV2 CK, CORROSION BOTTOM SIDE OF O/B LEG UNDER NUTPLATE STR 28R FWD OF STA 540. REPAIRED PER SRM 53-10-3 FIG 2.
- [SDR DL72S950977](https://openairdocs.org/sdr/DL72S950977.md): Seat Track · corroded · Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND ON CV2 CK, CORROSION AT GALLEY SUPPORT TRACK BS 1070 PLUS 6. REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7.
- [SDR DL72S950976](https://openairdocs.org/sdr/DL72S950976.md): Seat Track · corroded · Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND ON CV2 CK, CORROSION AT LEFT O/B SEAT TRACK BS 1010. REPLACED SEAT TRACK SECTION PER SRM 53-10-5 FIG 7.
- [SDR DL72S950975](https://openairdocs.org/sdr/DL72S950975.md): Seat Track · corroded · Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND ON CV2 CK, CORROSION AT SEAT TRACK FROM STA 344 TO STA 440BL 24R. REPLACED TRACK SECTION BS 344 TO 400 PER SRM 53-10-5 FIG 7.
- [SDR DL72S950974](https://openairdocs.org/sdr/DL72S950974.md): Seat Track · corroded · Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND ON CV2 CK, CORROSION AT TOP AND UNDERSIDE OF SEAT TRACK AT CLIPNUT HOLES BETWEEN STA 380 AND STA 400 RBL 44. REPLACED SEAT TRACK SECTION FROM 344 TO 400 AT VRBL 64 PER SRM 53-10-5 FIG 7.
- [SDR DL72S950973](https://openairdocs.org/sdr/DL72S950973.md): Angle · corroded · Feb 28, 1995 · N468DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON CV2 CK, CORROSION ON FLOOR SUPPORT ANGLE STA 1067 LBL 27 TO 45. REPLACED FLOOR ANGLE.
- [SDR DL72S951089](https://openairdocs.org/sdr/DL72S951089.md): Angle · cracked · Feb 27, 1995 · N468DA · Boeing 727232 · Fuselage, Landing Gear Attach Fittings
  > FOUND DURING CV-2 L/O CHK,.25 INCH CRACK AT STA 913 SUPPORT ANGLE ABOVE H BRACKET RT SIDE. LANDING GEAR UPLOCK ATTACH STRUCTURE. REPAIRED PER MM 53-11-0 PG 834.
- [SDR DL72S951088](https://openairdocs.org/sdr/DL72S951088.md): Bracket · cracked · Feb 27, 1995 · N468DA · Boeing 727232 · Fuselage, Landing Gear Attach Fittings
  > FOUND DURING CV-2/ LO CHECK,.25 INCH VISIBLE CRACK AT STA 910 ANGLE ABOVE H BRACKET. RIGHT L/G UPLOCK ATTACH STRUCTURE. REPAIRED PER MM 53-11-0 PG 834.
- [SDR DL72S951054](https://openairdocs.org/sdr/DL72S951054.md): Spar Stifner · cracked · Feb 27, 1995 · N468DA · Boeing 727232 · Wing Spar
  > FOUND ON CV 2 CHECK 1 INCH CRACK IN LEADING EDGE SPAR STIFFENER AT NR 7 SLAT O/B TRACK O/B ANGLE. REPAIRED AND REPLACED STIFFNER PER M/M 57-20-21 PG 813.
- [SDR DL72S950991](https://openairdocs.org/sdr/DL72S950991.md): Angle · cracked · Feb 27, 1995 · N468DA · Boeing 727232 · Trailing Edge Flaps
  > FOUND ON CV2 CHECK.25 INCH CRACK NR 6 FLAP ACTUATOR ATTACH ANGLE LOWER OUTBOARD SIDE REPAIR. REPAIRED PER MM 57-20-21 PG 811.
- [SDR DL72S950990](https://openairdocs.org/sdr/DL72S950990.md): Skin · cracked · Feb 27, 1995 · N468DA · Boeing 727232 · Nacelle/Pylon, Plate/Skin
  > FOUND ON CV2 CHECK.25 INCH CRACKS IN SKIN AT FASTNER HOLES (4 PLACES) RT SIDE ABOVE FWD VERTICAL SPAR AND FWD OF PANEL 95012) FASTNERS LOOSE FWD OF PANEL 9501 REPAIR-1) REPAIR PER MM 54-30-0 PG801/FIG801 2).
- [SDR DL72S950972](https://openairdocs.org/sdr/DL72S950972.md): Skin · scraped · Feb 27, 1995 · N468DA · Boeing 727232 · Passenger/Crew Doors
  > FOUND ON CV2 CK, PER OMI PERMANENT REPAIR OF L-1 DOOR AFT END LWR RT CORNER SCRAPE. INSTALLED DOUBLER PER ERA 301277-14 CODE 4-53-31-20.
- [SDR DL72S950033](https://openairdocs.org/sdr/DL72S950033.md): Angle · cracked · Jan 3, 1995 · N468DA · Boeing 727232 · Elevator, Spar/Rib
  > DURING LETTER CHECK, THE LEFT ELEVATOR INTERNAL SUPPORT ANGLE INSIDE ACCESS PANEL 9307 WAS FOUND CRACKED. REPAIRED PER SRM 55-21-4 FIG 1.

## 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 = 'N468DA' AND deregistration_id = 'N468DA-2000-04-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N468DA-2000-04-18/reports

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