# Service difficulty reports: N401DA, cancelled Aug 15, 2013

A list on [N401DA, cancelled Aug 15, 2013](https://openairdocs.org/deregistered/N401DA-2013-08-15.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 · 76 reports

- [SDR DL72S001142](https://openairdocs.org/sdr/DL72S001142.md): Valve · inoperative · Jun 13, 2000 · N401DA · Boeing 727232 · Fuel Dump System
  > LDFT TANK 2 DUMP VALVE WON''T OPEN. LIGHT STAYS ON WHEN TRYING TO OPEN.
- [SDR DL72S000993](https://openairdocs.org/sdr/DL72S000993.md): Battery Pack · will not test · May 20, 2000 · N401DA · Boeing 727232 · Emergency Lighting
  > BATTERY PACK FOR EMERGENCY LIGHTS AT THE C-2 CARGO DOOR (M-957) WOULD NOT TEST. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK GOOD.
- [SDR DL72S000806](https://openairdocs.org/sdr/DL72S000806.md): Stiffener · cracked · Apr 25, 2000 · N401DA · Boeing 727232 · Leading Edge Devices
  > A 1 INCH CRACK IN SPAR STIFFENER I/B SIDE OF NR 6 SLAT I/B TRACK. REPLACED STIFFENER PER M/M 57-20-21. TPA D-1 LETTER CHECK.
- [SDR DL72S000805](https://openairdocs.org/sdr/DL72S000805.md): Angle · cracked · Apr 25, 2000 · N401DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A 1.5 INCH CRACK IN BS 870 LT MLG WW I/B ATTACH ANGLE. REPAIRED PER SRM 53-10-9D.
- [SDR DL72S000278](https://openairdocs.org/sdr/DL72S000278.md): Acm · leaking · Feb 9, 2000 · N401DA · Boeing 727232 · Cabin Cooling System
  > PASSENGER CABIN FILLED WITH LIGHT SMOKE AND RIGHT AFT LAV SMOKE ALARM WENT OFF. SHORTLY THEREAFTER RIGHT PACK TRIP OFF LIGHT ILLUM. SMOKE CLEARED AFTER RUNNING SMOKE ILLIMINATION CHECK. FOUND OIL LEAKING FROM RT ACM. REPLACED SAME.
- [SDR DL72S992444](https://openairdocs.org/sdr/DL72S992444.md): Valve · failed · Nov 5, 1999 · N401DA · Boeing 727232 · Cabin Cooling System
  > AFTER NR 3 ENG START AND RT PACK SELECTED ON, LOUD BANG WAS HEARD IN COCKPIT/CABIN. RT DUCT PRESS NEEDLE WENT TO ZERO AND AFT FLT ATTENDANTS REPORTED FUEL SMELL. INSPECTED DUCTS AT NR 3 ENG/PYLON/AFT AIRSTAIR FOR DAMAGE/LEAKAGE, CK GOOD. CHECKED DUCTS AT RT
- [SDR DL72S992413](https://openairdocs.org/sdr/DL72S992413.md): Actuator · failed · Oct 31, 1999 · N401DA · Boeing 727232 · Leading Edge Slat Actuator
  > NUMBER THREE LEADING EDGE FLAP INDICATION AND UNCOMMANDED ROLL. REPLACED NUMBER THREE LEADING EDGE FLAP ACTUATOR.
- [SDR DL72S991663](https://openairdocs.org/sdr/DL72S991663.md): Light · damaged · Jul 23, 1999 · N401DA · Boeing 727232 · Emergency Lighting
  > ONE EMERGENCY LIGHT AT 20 DEF INOP. REPLACED SEAT ASSY AT ROW 20 DEF. OPS CHECK GOOD. MCO AND PLACARD REMOVED.
- [SDR DL72S990407](https://openairdocs.org/sdr/DL72S990407.md): Stiffener · cracked · Feb 26, 1999 · N401DA · Boeing 727232 · Wing Miscellaneous Structure
  > TPA - LTR CHK C-1 02/26/99, WING LE SPAR STIFFENER CRACKED AT I/B SIDE NR 2 SLAT I/B TRACK BOX. REPLACED STIFFENER PER MM 57-20-21.
- [SDR DL72S990406](https://openairdocs.org/sdr/DL72S990406.md): Bracket · cracked · Feb 26, 1999 · N401DA · Boeing 727232 · Leading Edge Slat Actuator
  > NR 8 SLAT ACT I/B MOUNT BRACKET CRACKED AT WEB. REPAIRED PER M/M 57-20-21.
- [SDR DL72S990405](https://openairdocs.org/sdr/DL72S990405.md): Skin · cracked · Feb 26, 1999 · N401DA · Boeing 727232 · Leading Edge Devices
  > NR 7 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0.
- [SDR DL72S990367](https://openairdocs.org/sdr/DL72S990367.md): Skin · cracked · Feb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 460 INDICATED A SINGLE CRACK. INTERNAL HFEC INSPECTION CONFIRMED ONE CRACK ONLY AT FS 444. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND REPAIRED PER THE B727 SRM 53-30-3, FIG 5. TEN FASTE
- [SDR DL72S990366](https://openairdocs.org/sdr/DL72S990366.md): Skin · cracked · Feb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL OF THE STRINGER 4R LAP SPLICE BETWEEN FS 360 AND 481. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL LENGTH. THE LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PANEL LEN
- [SDR DL72S990365](https://openairdocs.org/sdr/DL72S990365.md): Skin · cracked · Feb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN AT THE STRINGER 4R LAP SPLICE BETWEEN FS 681 AND 740. INTERNAL HFEC INSPECTION VERIFIED 27 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG THE ENTIRE PANEL LENGTH AND R
- [SDR DL72S990364](https://openairdocs.org/sdr/DL72S990364.md): Skin · cracked · Feb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 4R LAP SPLICE BETWEEN FS 481 AND 680. INTERNAL HFEC INSPECTION CONFIRMED 31 CRACKS ALONG THE PANEL LENGTH. THE LAP SPLICE WAS CUTOUT ALONG THE PANEL LENGTH AND REPAIR
- [SDR DL72S990362](https://openairdocs.org/sdr/DL72S990362.md): Skin · cracked · Feb 23, 1999 · N401DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN OF THE STRINGER 26L LAP SPLICE BETWEEN FS 480 AND 681. INTERNAL HFEC INSPECTION CONFIRMED A TOTAL OF 6 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE
- [SDR DL72S990017](https://openairdocs.org/sdr/DL72S990017.md): Power Supply · inop · Jan 4, 1999 · N401DA · Boeing 727232 · Emergency Lighting
  > FUSE BLOWN, EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY.
- [SDR DL72S982162](https://openairdocs.org/sdr/DL72S982162.md): Battery · discharged · Oct 18, 1998 · N401DA · Boeing 727232 · Emergency Lighting
  > RT FWD ENTRY DOOR OVERHEAD EMEGENCY LIGHT WILL NOT TEST. REPLACED BATTERIES AND RACK NOW CKS NORMAL.
- [SDR DL72S982033](https://openairdocs.org/sdr/DL72S982033.md): Track · corrosion · Oct 2, 1998 · N401DA · Boeing 727232 · Trailing Edge Flaps
  > INBD FLAP INBD TRACK TYP CORROSION AT MLG BEAM ATTACH HOLES AND FWD LUG: AD 90-07-05: TYPICAL CORROSION WAS FOUND TO THE MLG BEAM ATTACH HOLES (WITHIN THE AD AREA) AND AT THE FWD ATTACH LUG. OVERSIZED CORRODED HOLES AND MACHINED LUG FACES.
- [SDR DL72S982114](https://openairdocs.org/sdr/DL72S982114.md): Track · corroded · Sep 28, 1998 · N401DA · Boeing 727232 · Trailing Edge Flaps
  > BUSH FWD ATTACH LUG AND REPAIR MLG BEAM ATTACH HOLES PER SB 727-57-0178, EXCEPT INCREASE HOLE DIA TO.847.
- [SDR DL72S982113](https://openairdocs.org/sdr/DL72S982113.md): Track · corroded · Sep 28, 1998 · N401DA · Boeing 727232 · Trailing Edge Flaps
  > TYPICAL CORROSION FOUND IN MLG BEAM ATTACH HOLES. REPAIRED SIMILAR TO SB 727-57-0178 EXCEPT TO OS HOLES,.838 MAX DIAMETER TO REMOVE ALL CORROSION.
- [SDR DL72S981772](https://openairdocs.org/sdr/DL72S981772.md): Switch · failed · Aug 27, 1998 · N401DA · Boeing 727232 · Leading Edge Slat Position Indicating System
  > AMBER LEADING EDGE FLAP LIGHT WOULD NOT EXTINGUISH WHEN FLAPS WERE MOVED FROM 5 TO 2 DEGREES. REPLACED RETRACT SWITCH ON NR 1 SLAT ACTUATOR.
- [SDR DL72S981546](https://openairdocs.org/sdr/DL72S981546.md): Skin · cracked · Jul 24, 1998 · N401DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND AT B-2 LETTER CK,.5 INCH CRACK, FUSELAGE SKIN AT L-4 WINDOW SCREW LOWER INBD CORNER. REPAIRED PER SRM 53-30-3.
- [SDR DL72S981478](https://openairdocs.org/sdr/DL72S981478.md): Battery Pack · discharged · Jul 15, 1998 · N401DA · Boeing 727232 · Emergency Lighting
  > LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT ASSY AND CHANGED BATTERY PACK PER M/M. OP CHECK GOOD BATTERY PACK REMOVED 7997. BATTERY PACK INSTALLED, C6495 P/N 334102486.
- [SDR DL72S981373](https://openairdocs.org/sdr/DL72S981373.md): Rack · inoperative · Jun 30, 1998 · N401DA · Boeing 727232 · Emergency Lighting
  > RT SIDE EMER LIGHT OVERWING EXIT LIGHTS INOP. REPLACED LIGHT RACK.
- [SDR DL72S981202](https://openairdocs.org/sdr/DL72S981202.md): Rack · inoperative · Jun 6, 1998 · N401DA · Boeing 727232 · Emergency Lighting
  > OVERWING EXIT EMERG LIGHTS FAILED TO ILLUMINATE. REPLACED RACK.
- [SDR DL72S980974](https://openairdocs.org/sdr/DL72S980974.md): Battery Pack · discharged · May 7, 1998 · N401DA · Boeing 727232 · Emergency Lighting
  > AFT GALLEY OVERHEAD EXIT SIGN INOP. REPLACED POWER PACK.
- [SDR DL72S980132](https://openairdocs.org/sdr/DL72S980132.md): Battery Pack · discharged · Jan 17, 1998 · N401DA · Boeing 727232 · Emergency Lighting
  > AFT EXIT AISLE OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, SYSTEM OPERATIONAL CHECK NORMAL.
- [SDR DL72S972661](https://openairdocs.org/sdr/DL72S972661.md): Skin · cracked · Dec 15, 1997 · N401DA · Boeing 727232 · Nacelle/Pylon, Plate/Skin
  > SKIN, CRACKED THE FWD SECTION OF S DUCT FWD SKIN LIP AT THE 12:00 O'CLOCK POSITION. REMOVED DAMAGED SECTION OF SKIN PER SRM. FABRICATED REPAIR PARTS PER SRM 54-10-3 FIG 13. TREATED AND PAINTED PER SRM 54-10-3. OK TO INSTALL REPAIR PER SRM 54-10-3. INSTALL
- [SDR DL72S972742](https://openairdocs.org/sdr/DL72S972742.md): Rib · cracked · Dec 10, 1997 · N401DA · Boeing 727232 · Trailing Edge Flaps
  > THE I/B AFT CLOSEOUT RIB WAS FOUND CRACKED DURING SHOP VISIT. THE RIB WAS REPAIRED BY INSTALLING A DOUBLER PER 727 M/M 57-52-0.
- [SDR DL72S972627](https://openairdocs.org/sdr/DL72S972627.md): Beam · cracked · Dec 4, 1997 · N401DA · Boeing 727232 · Wing Miscellaneous Structure
  > RT WING SPOILER SUPPORT BEAM CRACKED IN O/B BOLT HOLE FOR NR 5 FLAP TRACK. REMOVED DAMAGED SECTION OF SPOILER BEAM PER M/M 57-55-0 FIG 805. REMOVED SUPPORT BETWEEN SPOILERS 7 AND 8. FABRICATED EXTRUDED CHORD IAW M/M 57-55-0 PG 810. DRILLED CHORD, DOUBLER T
- [SDR DL72S972582](https://openairdocs.org/sdr/DL72S972582.md): Fitting · corrosion · Nov 25, 1997 · N401DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > RT FT WING ATTACH FITTING HAS CORROSION AT SEVERAL LOCATIONS INSIDE BORE. REMOVED CORROSION IAW SRM 53-40-1 PG 18. TREATED AND PAINTED PER PS 900-3-6.
- [SDR DL72S972581](https://openairdocs.org/sdr/DL72S972581.md): Stringer · cracked · Nov 25, 1997 · N401DA · Boeing 727232 · Wing, Longeron/Stringer
  > STRINGER CRACKED WS 686.5 STRINGER NR 10 IS CRACKED AT FASTENER HOLE. REPAIRED PER MM 57-13-0.
- [SDR DL72S972757](https://openairdocs.org/sdr/DL72S972757.md): Skin · punctured · Nov 24, 1997 · N401DA · Boeing 727232 · Trailing Edge Flaps
  > THE COVE SKIN WAS FOUND WITH A HOLE 26 FROM IB END DURING SHOP VISIT. THE DAMAGE WAS REMOVED AND A DOUBLER INSTALLED PER 727 MM 57-52-00.
- [SDR DL72S972756](https://openairdocs.org/sdr/DL72S972756.md): Angle · cracked · Nov 24, 1997 · N401DA · Boeing 727232 · Trailing Edge Flaps
  > THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED DURING SHOP VISIT. THE CHORD WAS REPAIRED PER 727 MM 57-52-00 BY REMOVING DAMAGE AND REPLACING AND INSTALLING A DOUBLER.
- [SDR DL72S972755](https://openairdocs.org/sdr/DL72S972755.md): Angle · cracked · Nov 24, 1997 · N401DA · Boeing 727232 · Trailing Edge Flaps
  > THE LOWER AFT CHORD ANGLE WAS FOUND CRACKED 18 FROM IB END DURING A SHOP VISIT. THE CHORD WAS REPAIRED PER 727 MM 57-52-00 BY REMOVING DAMAGE AND INSTALLING A DOUBLER.
- [SDR DL72S972626](https://openairdocs.org/sdr/DL72S972626.md): Rib · cracked · Nov 24, 1997 · N401DA · Boeing 727232 · Leading Edge Devices
  > NR 6 SLAT RIB CRACKED LOWER SURFACE. REMOVED RIVETS FORM RIB, BEGAN FABRICATION OF REPAIR DOUBLERS PER M/M 57-40-0 FIG 814. DRILLED AFT DOUBLER, STOP DRILLED PER SRM 57-54-0. ROUTED OUT DAMAGE PER SRM. INSTALLED REPAIR PER SRM.
- [SDR DL72S972625](https://openairdocs.org/sdr/DL72S972625.md): Rib · cracked · Nov 24, 1997 · N401DA · Boeing 727232 · Leading Edge Devices
  > NR 7 SLAT RIB CRACKED JUST OUTBD OF ACTUATOR ROD END AREA. FABRICATED REPAIR PER MM 57-54-0 FIG 814. INSTALLED REPAIR PER MM 57-54-0 FIG 814.
- [SDR DL72S972624](https://openairdocs.org/sdr/DL72S972624.md): Rib · cracked · Nov 24, 1997 · N401DA · Boeing 727232 · Leading Edge Devices
  > NR 6 SLAT RIB CRACKED ON INBD END. MADE DOUBLER IAW MM. DRILLED UP AND TREATED AND PAINTED. INSTALLED DOUBLER PER M/M 57-54-0 FIG 814. INSTALLED SEAL.
- [SDR DL72S972623](https://openairdocs.org/sdr/DL72S972623.md): Stop · worn · Nov 24, 1997 · N401DA · Boeing 727232 · Leading Edge Devices
  > NR 4 SLAT INBD STOP WORN, 2ND WEB FROM INBD END CRACKED OUT UNDER N/P. FABRICATED REPAIR PER MM 57-54-0 FIG 814. OK TO TREAT AND PAINT. TREATED AND PAINTED PER PS 900-2 NR 5. INSTALLED REPAIR PER MM 57-54-0 FIG 814. WEAR WITHIN LIMITS PER MM 27-87-0 FIG 5
- [SDR DL72S972580](https://openairdocs.org/sdr/DL72S972580.md): Stringer · cracked · Nov 24, 1997 · N401DA · Boeing 727232 · Wing, Longeron/Stringer
  > LT WING STR TO RIB HFEC INSPECTION SHOWS STRINGER TO RIB ATTCH FLANGE MARKED 'C' AT WS 629.0 HAS CRACK INDICATIONS -MARKED- THAT EXTENDS FROM HOLE TO EDGE OF FLANGE. CUTOUT ACCESS HOLE ON VENT BOX PER MM 57-13-10. DRILLED REPAIR PARTS PER MM 57-13-10 FIG 804
- [SDR DL72S972579](https://openairdocs.org/sdr/DL72S972579.md): Fitting · corrosion · Nov 24, 1997 · N401DA · Boeing 727232 · Wing, Fuselage Attach Fittings
  > CORROSION ON RT FRONT SPAR WING TO BODY FWD FITTING. REMOVED CORROSION AT PER SRM 51-10-6. TREATED AND PAINTED PER PS 900-3-6.
- [SDR DL72S972578](https://openairdocs.org/sdr/DL72S972578.md): Fitting · corrosion · Nov 24, 1997 · N401DA · Boeing 727232 · Wing, Fuselage Attach Fittings
  > CORROSION ON LEFT AFT SPAR WING TO BODY FITTING (AFT END). REMOVED CORROSION IAW SRM 53-40-1 PG 18. TREATED AND PAINTED PER PS 900-3-6.
- [SDR DL72S972622](https://openairdocs.org/sdr/DL72S972622.md): Skin · cracked · Nov 21, 1997 · N401DA · Boeing 727232 · Nacelle/Pylon, Plate/Skin
  > SKIN CRACKED AT INSPECTION PANEL 9524. ROUTED OUT CRACK AND MANUFACTURED DOUBLER PER M/M 54-30-0. INSTALLED DOUBLER PER SRM 54-30-0, FIG 803.
- [SDR DL72S972577](https://openairdocs.org/sdr/DL72S972577.md): Rib · cracked · Nov 21, 1997 · N401DA · Boeing 727232 · Wing, Rib/Bulkhead
  > CRACK - STRINGER TO RIB WS 629, S-9 AFT HOLE, RT WING. REPAIRED PER MM 57-13-00.
- [SDR DL72S972576](https://openairdocs.org/sdr/DL72S972576.md): Rib · cracked · Nov 21, 1997 · N401DA · Boeing 727232 · Wing, Rib/Bulkhead
  > CRACK - STRINGER TO RIB WS 629, S-13 AFT HOLE, RT WING. REPAIRED PER MM 57-13-00.
- [SDR DL72S972575](https://openairdocs.org/sdr/DL72S972575.md): Rib · cracked · Nov 21, 1997 · N401DA · Boeing 727232 · Wing, Rib/Bulkhead
  > RT WING WS 629 S-AA CRACKED AT STR TO RIB CONNECTION REF OP8602 RC 882. REPAIRED PER MM 57-13-00.
- [SDR DL72S972574](https://openairdocs.org/sdr/DL72S972574.md): Light Box · corroded · Nov 21, 1997 · N401DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > LIGHT BOX CORRODED AROUND EDGES STA 720B AND 720C BETWEEN STRINGERS 16R TO 14R. REMOVED LIGHT BOX. REMOVED CORROSION PER SRM 51-10-6 NOT WITHIN ALLOWABLE LIMITS PER SRM 53-30-1 FIG 7. COMPLETED DRILLING DOUBLER PER SRM 53-30-3 FIG 22. INSTALLED DOUBLER PER
- [SDR DL72S972573](https://openairdocs.org/sdr/DL72S972573.md): Stringer · corroded · Nov 21, 1997 · N401DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > LIGHT BOX CORRODED STRINGER 152, BETWEEN STA 720B AND 720C. REMOVED LIGHT BOX FOR ACCESS, REMOVED CORROSION PER 51-10-6 NOT WITHIN ALLOWABLE LIMITS PER SRM 53-30-1 FIG 7. COMPLETED FABRICATING REPAIR DOUBLER PER SRM 53-30-3 FIG 22 T AND P PER PS 900-2 NR 5.
- [SDR DL72S972572](https://openairdocs.org/sdr/DL72S972572.md): Stringer · cracked · Nov 21, 1997 · N401DA · Boeing 727232 · Wing, Longeron/Stringer
  > HFEC INSP SHOWED CRACK INDICATION AT WS 656.5 FWD VENT HOLE. CUT ACCESS HOLE IN VENT BOX PER M/M 57-13-00. REPAIRED CRACK PER MM 57-13-0 FIG 80.

Next page: https://openairdocs.org/deregistered/N401DA-2013-08-15/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 = 'N401DA' AND deregistration_id = 'N401DA-2013-08-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N401DA-2013-08-15/reports

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