# Service difficulty reports: N404DA, cancelled Feb 16, 2001

A list on [N404DA, cancelled Feb 16, 2001](https://openairdocs.org/deregistered/N404DA-2001-02-16.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 · 52 reports

- [SDR DL72S002300](https://openairdocs.org/sdr/DL72S002300.md): Flashlight · unserviceable · Nov 26, 2000 · N404DA · Boeing 727232 · Emergency Equipment
  > F/A LOWER FWD FLASHLIGHT NOT FLASHING. REPLACED FLASHLIGHT
- [SDR DL72S001259](https://openairdocs.org/sdr/DL72S001259.md): Switch · failed · Jul 4, 2000 · N404DA · Boeing 727232 · Heating System
  > AUTO PACK TRIP ARMED, LIGHT DID NOT ILLUMINATE ON T/O ROLL. REJECTED TAKEOFF AT 90 KTS AND 169,960 LBS. REPLACED AUTO PACK TRIP SWITCHES ON ENG 1, 2 & 3. OP CHECKS GOOD.
- [SDR DL72S000916](https://openairdocs.org/sdr/DL72S000916.md): Fcu · malfunctioned · May 7, 2000 · N404DA · Boeing 727232 · Fuel Control/Turbine Engines
  > ON CLIMBOUT, NR 2 ENG ALL INDICATORS FLUX AND EGT AT 580 DEG. REPLACED FUEL CONTROL.
- [SDR DL72S992609](https://openairdocs.org/sdr/DL72S992609.md): Power Pack · leaking · Nov 27, 1999 · N404DA · Boeing 727232 · Elevator Control System
  > SYS A QTY RAPIDLY DECREASED ON GEAR RETRACTION. FOUND RT ELEV POWER PACK LEAKING. REPLACED RT ELEV POWER PACK.
- [SDR DL72S992402](https://openairdocs.org/sdr/DL72S992402.md): Battery · discharged · Oct 29, 1999 · N404DA · Boeing 727232 · Emergency Lighting
  > ROW 2 OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATT PACK, OPS CK OK.
- [SDR DL72S991626](https://openairdocs.org/sdr/DL72S991626.md): Angle · cracked · Jul 19, 1999 · N404DA · Boeing 727232 · Wing Miscellaneous Structure
  > NR 5 SLAT LOWER COVE ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0 FIG 812.
- [SDR DL72S991421](https://openairdocs.org/sdr/DL72S991421.md): Bulb · failed · Jun 23, 1999 · N404DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY EXIT LIGHT AT THE LEFT SERVICE DOOR INOP. EMERGENCY EXIT LIGHT AT FWD GALLEY NEEDS RELAMPING. RELAMPED LIGHTS.
- [SDR DL72S991280](https://openairdocs.org/sdr/DL72S991280.md): Light · inoperative · Jun 7, 1999 · N404DA · Boeing 727232 · Emergency Lighting
  > LT OVERWING EXTERIOR EMERGENCY LIGHT INOP.
- [SDR DL72S991274](https://openairdocs.org/sdr/DL72S991274.md): Light · missing · Jun 7, 1999 · N404DA · Boeing 727232 · Emergency Lighting
  > ON L/O, FOUND SEAT 20D EMERGENCY LIGHT MISSING. REPLACED LIGHT ASSY, OPS CKS GOOD.
- [SDR DL72S990572](https://openairdocs.org/sdr/DL72S990572.md): Skin · cracked · Mar 13, 1999 · N404DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 15 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENGT
- [SDR DL72S990561](https://openairdocs.org/sdr/DL72S990561.md): Skin · cracked · Mar 13, 1999 · N404DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 21 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE LENGT
- [SDR DL72S990545](https://openairdocs.org/sdr/DL72S990545.md): Skin · cracked · Mar 13, 1999 · N404DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 86 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL
- [SDR DL72S990569](https://openairdocs.org/sdr/DL72S990569.md): Skin · cracked · Mar 12, 1999 · N404DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A CRACK BETWEEN FS 520 AND 540. THE CRACK WAS ROUTED OUT AND REPAIRED PER B727 SRM 53
- [SDR DL72S990567](https://openairdocs.org/sdr/DL72S990567.md): Skin · cracked · Mar 11, 1999 · N404DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED A CRACK IN LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION OF THE ENTIRE PANEL CONFIRMED A SINGLE CRACK BETWEEN FS 560 AND 580. THE CRACK WAS ROUTED OUT AND
- [SDR DL72S990544](https://openairdocs.org/sdr/DL72S990544.md): Skin · cracked · Mar 11, 1999 · N404DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE PANEL LENG
- [SDR DL72S982549](https://openairdocs.org/sdr/DL72S982549.md): Rib · cracked · Dec 11, 1998 · N404DA · Boeing 727232 · Leading Edge Devices
  > LTR CHK B-1 12-11-98, NR 5 L/E SLAT I/B ACTUATOR NOSE RIB CRACKED. REPAIRED PER MM 57-54-0.
- [SDR DL72S982548](https://openairdocs.org/sdr/DL72S982548.md): Web · cracked · Dec 11, 1998 · N404DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > RIGHT I/B VERT TORQUE BOX WEB HAS.5 INCH CRACK AT LWR LIGHTENING HOLE STA 1239 RT. REPAIRED PER M/M 53-11-0 PG 832 TO 833.
- [SDR DL72S982547](https://openairdocs.org/sdr/DL72S982547.md): Frame · cracked · Dec 11, 1998 · N404DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND AT B-1 LETTER CHECK, AFT ENTRYWAY RT FRAME HAS.5 INCH VISIBLE CRACK AT FWD SIDE APPROX 6 INCHES BELOW UPPER STOP PAD. REPAIRED PER SRM 53-10-9.
- [SDR DL72S981350](https://openairdocs.org/sdr/DL72S981350.md): Battery Pack · discharged · Jun 27, 1998 · N404DA · Boeing 727232 · Emergency Lighting
  > RT FWD OVERWING EMER EXIT LIGHT INOP. REPLACED BATT RACK, OPS OK.
- [SDR DL72S981064](https://openairdocs.org/sdr/DL72S981064.md): Skin · corroded · May 18, 1998 · N404DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF 4-69078-3AD AN EXISTING REPAIR WAS FOUND TO BE CORRODED. REPAIRED PER ERA 331732-14.
- [SDR DL72S981063](https://openairdocs.org/sdr/DL72S981063.md): Skin · cracked · May 18, 1998 · N404DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A 1.5 INCH CRACK WAS FOUND IN THE UPPER HINGE CUTOUT DOUBLER OF THE R1 DOOR. REPAIRED PER ERA 331703-14.
- [SDR DL72S981062](https://openairdocs.org/sdr/DL72S981062.md): Fitting · worn · May 18, 1998 · N404DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > SIX FASTENER HOLES WERE FOUND WORN OUT OF ROUND. THE HOLES ARE AT FS 1183 TORQUE BOX AREA AND ARE COMMON TO THE AFT INBD AND OUTBD TENSION TIE FITTINGS. REPAIRED PER ERA 331729-14.
- [SDR DL72S981061](https://openairdocs.org/sdr/DL72S981061.md): Frame · cracked · May 18, 1998 · N404DA · Boeing 727232 · Fuselage Main, Frame
  > CRACKS FOUND IN THE INBD FLANGES OF BOTH LT AND RT OVER WING EXIT FRAMES AT FS 783.95. REPAIRED PER ERA 331706-14AD.
- [SDR DL72S980924](https://openairdocs.org/sdr/DL72S980924.md): Cowl · worn · Apr 22, 1998 · N404DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > LT FWD ENG COWL SUPPORT RING LIP WORN AT AFT FWD COWL SUPPORT MATING SURFACE, AFT LT EMPENNAGE 6-11 O'CLOCK. REMOVED DAMAGED AREA, WITHIN LIMITS PER SRM 53-10-1 FIG 1 SECTION AT 6:00 AND 7:00 OUT OF LIMITS. FABRICATED REPAIR PER M/M 53-11-0 PG 801 SECTION 7:
- [SDR DL72S980994](https://openairdocs.org/sdr/DL72S980994.md): Skin · cracked · Apr 21, 1998 · N404DA · Boeing 727232 · Nacelle/Pylon, Plate/Skin
  > C/W ERA 300554-14 CODE 4-54-31 PERM REPAIR, NACELLES/THINNER SKIN, NR 2 ENG FS 1151.68. TIME LIMITED. REMOVED DAMAGED SKIN, FABD REPAIR PER SRM 54-10-3 FIG 13. DYE CKD AND FOUND TO BE REMOVED PER PS 900-6-3 NR 1 REF N/R 398.
- [SDR DL72S980967](https://openairdocs.org/sdr/DL72S980967.md): Angle · cracked · Apr 21, 1998 · N404DA · Boeing 727232 · Wing Miscellaneous Structure
  > ANGLE CRACKED IN WING LEADING EDGE, INBD END NR 3 KRUEGER FLAP. DYE CKD TO CONFIRM CRACK. STOP DRILLED, FABD DOUBLER PER SRM 51-40-3, C/W MM 57-20-21 FIG 807.
- [SDR DL72S980966](https://openairdocs.org/sdr/DL72S980966.md): Bracket · cracked · Apr 21, 1998 · N404DA · Boeing 727232 · Leading Edge Slat Actuator
  > AT HMV, FOUND RW ACTUATOR BRACKET CRACKED NR 6 KRUEGER FLAP ACTUATOR BRACKET LOWER O/B FWD CORNER. REMOVED ACT AND BEAM PER MM 57-20-21, STOP DRILLED CRACK, INSTALLED PER MM 57-20-21.
- [SDR DL72S980961](https://openairdocs.org/sdr/DL72S980961.md): Frame · bent · Apr 21, 1998 · N404DA · Boeing 727232 · Fuselage Main, Frame
  > FOUND AT HMV, FRAME BENT STA 950E BETWEEN STR 26L-27L. STARTED REPAIR PER SRM 53-10-4, COMPLETED REPAIR PER SRM 53-10-4.
- [SDR DL72S980959](https://openairdocs.org/sdr/DL72S980959.md): Bracket · cracked · Apr 21, 1998 · N404DA · Boeing 727232 · Leading Edge Devices
  > ACTUATOR ATTACH BRACKET CRACKED FWD LOWER INBD CORNER OF NR 5 KRUEGER FLAP. REPAIRED PER M/M 57-20-21 FIG 807.
- [SDR DL72S972269](https://openairdocs.org/sdr/DL72S972269.md): Battery Pack · discharged · Nov 5, 1997 · N404DA · Boeing 727232 · Emergency Lighting
  > OVERHEAD AISLE EMERGENCY LIGHT AT ROW 3 INOP- REPLD BATTERY RACK AND BATTERY PACK
- [SDR DL72S972268](https://openairdocs.org/sdr/DL72S972268.md): Battery Pack · discharged · Nov 5, 1997 · N404DA · Boeing 727232 · Emergency Lighting
  > OVERHEAD AISLE EMERGENCY LIGHT AT AFT LAVS INOP- REPLD BATTERY RACK AND BATTERY PACK.
- [SDR DL72S972267](https://openairdocs.org/sdr/DL72S972267.md): Switch · inoperative · Nov 5, 1997 · N404DA · Boeing 727232 · Emergency Lighting
  > AFT CARGO DOOR EMER LITE INTERMITTENTLY CYCLING ON AND OFF- REPLD BATT SW RACK- OPS CK NML
- [SDR DL72S971953](https://openairdocs.org/sdr/DL72S971953.md): Rear Spar Web · cracked · Sep 26, 1997 · N404DA · Boeing 727232 · Wing Spar
  > THE WING CENTER SECTION REAR SPAR WEB IS CRACKED AT LBL 20.5. THE CRACK IS APPROX 2.5 LONG IN A CHEMMILL RADIUS JUST BELOW THE SPAR UPPER CHORD. AN ACCESS HOLE WILL BE CUT OUT AS REQUIRED TO GAIN ACCESS TO THE REAR SPAR WEB IN THE WING SECTION. THE CUTOUT I
- [SDR DL72S971674](https://openairdocs.org/sdr/DL72S971674.md): Bracket · cracked · Aug 27, 1997 · N404DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND DURING A-1 LETTER CHECK, 2.5 INCH CRACK NR 1 L/E SLAT ACTUATOR O/B ATTACH BRACKET. REPAIRED PER M/M 57-20-21.
- [SDR DL72S971673](https://openairdocs.org/sdr/DL72S971673.md): Stiffener · cracked · Aug 27, 1997 · N404DA · Boeing 727232 · Wing Miscellaneous Structure
  > FOUND DURING A-1 LETTER CHECK, FOUND 1.5 INCH CRACK AT WING L/E VERTICAL STIFFENER NR 6 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21.
- [SDR DL72S970144](https://openairdocs.org/sdr/DL72S970144.md): Stringer · cracked · Jan 24, 1997 · N404DA · Boeing 727232 · Vertical Stabilizer
  > A 1 INCH VISIBLE CRACK IN VERT STAB S-8L, 1 INCH VISIBLE CRACK IN VERT STAB S-9L, 1 INCH VISIBLE CRACK IN VERT STAB S-7L. REPAIRED PER M/M 55-30-0.
- [SDR DL72S970143](https://openairdocs.org/sdr/DL72S970143.md): Vert Stab Web · cracked · Jan 24, 1997 · N404DA · Boeing 727232 · Vertical Stabilizer
  > A 1.5 INCH CRACK IN VERT STAB WEB STA 1303 ACROSS TOP OF NR 2 ENG S-DUCT LOWER RT CORNER. REPAIRED PER M/M 53-11-0.
- [SDR DL72S970142](https://openairdocs.org/sdr/DL72S970142.md): Bulkhead Web · cracked · Jan 24, 1997 · N404DA · Boeing 727232 · Fuselage Main, Bulkhead
  > FOUND DURING F-2 LETTER CHECK, 1.5 INCH CRACK BS 1303 BULKHEAD WEB AT LWR RT CORNER.
- [SDR DL72S970141](https://openairdocs.org/sdr/DL72S970141.md): Stringer · cracked · Jan 24, 1997 · N404DA · Boeing 727232 · Vertical Stabilizer
  > FOUND DURING F-2 LETTER CHECK, VERTICAL STAB STR 7 LEFT STA 133.8 CRACKED 1 INCH, STR 8 LEFT STA 157.2 CRACKED 1 INCH AND STR 9 LEFT STA 133.8 CRACKED 1 INCH. REPAIRED PER M/M 55-30-0.
- [SDR DL72S970002](https://openairdocs.org/sdr/DL72S970002.md): Light · inoperative · Jan 1, 1997 · N404DA · Boeing 727232 · Emergency Lighting
  > R1 DOOR EMERGENCY LIGHT OVRHEAD WILL NOT TEST. REPLACED LIGHT ASSY, CHECKS GOOD.
- [SDR DL72S962741](https://openairdocs.org/sdr/DL72S962741.md): Spar · damaged · Oct 3, 1996 · N404DA · Boeing 727232 · Trailing Edge Flaps
  > FOUND DAMAGE ON RT FLAP. REPLACED AFT SPAR SECTION 0 TO 54 FROM I/B END OF FLAP PER M/M 57-52-0, TASK BN BO.
- [SDR DL72S961528](https://openairdocs.org/sdr/DL72S961528.md): Rib · cracked · Jun 25, 1996 · N404DA · Boeing 727232 · Leading Edge Devices
  > FOUND A.5 INCH CRACK IN RADIUS OF NOSE RIB INBD SIDE OF INBD TRACK, NR 6 SLAT. REPAIRED PER MM 57-54-0.
- [SDR DL72S960982](https://openairdocs.org/sdr/DL72S960982.md): Battery Pack · discharged · Apr 25, 1996 · N404DA · Boeing 727232 · Emergency Lighting
  > ON LAYOVER, FOUND LT FORWARD OVERWING EMERGENCY LICHTS INOPERATIVE. REPLACED M654 EMERGENCY LIGHT BATTERY PACK.
- [SDR DL72S960981](https://openairdocs.org/sdr/DL72S960981.md): Battery Pack · discharged · Apr 25, 1996 · N404DA · Boeing 727232 · Emergency Lighting
  > AFT EXIT DOOR EMERGENCY LIGHT INOP. REPLACED M1089 EMERENCY BATTERY PACK.
- [SDR DL72S960432](https://openairdocs.org/sdr/DL72S960432.md): Beam · cracked · Dec 1, 1995 · N404DA · Boeing 727232 · Electrical/Electronic Compartment Doors
  > DURING INSPECTION, FOUND A 2 INCH CRACK IN THE E/E COMPARTMENT DOOR AFT TRANSVERSE BEAM AFT LOWER ATTACH ANGLE. THE CRACK IS LOCATED IN THE RADIUS OF THE L-ANGLE AND RUNS BETWEEN 2 EXISTING ADJACENT FASTENERS. AN EXISTING REPAIR IS INSTALLED ON THE FWD FACE
- [SDR DL72S954582](https://openairdocs.org/sdr/DL72S954582.md): Tie Angle · cracked · Nov 30, 1995 · N404DA · Boeing 727232 · Vertical Stabilizer
  > FOUND DURING E-2 LETTER CHECK, VERTICAL STAB STRINGER TIE ANGLES CRACKED AT STA 157.200 2ND BAY FROM TOP LT SIDE. TWO ANGLES CRACKED AT 4TH BAY FROM TOP STA 133.800. REPAIRED PER M/M 53-30-0 PAR 3.
- [SDR DL72S953989](https://openairdocs.org/sdr/DL72S953989.md): Eel Battery Pack · discharged · Oct 12, 1995 · N404DA · Boeing 727232 · Emergency Lighting
  > LEFT CENTER OVERWING EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AT M954, OPERATION NORMAL.
- [SDR DL72S952044](https://openairdocs.org/sdr/DL72S952044.md): Web · cracked · May 11, 1995 · N404DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING E-1 LETTER CHECK, 1 INCH CRACK AT STA 1223 ABOVE LIGHTENING HOLE IN TORQUE BOX WEB LT. REPAIRED PER SRM 53-11-0.
- [SDR DL72S952043](https://openairdocs.org/sdr/DL72S952043.md): Rib · cracked · May 11, 1995 · N404DA · Boeing 727232 · Leading Edge Devices
  > FOUND DURING E-1 LETTER CHECK, NBR 7 L/E SLAT NOSE RIB HAS.25 INCH CRK AT FWD SIDE RT SIDE OF ACTUATOR ATTACH POINT. REPAIRED PER MM 57-54-0 PG 803.
- [SDR DL72S952042](https://openairdocs.org/sdr/DL72S952042.md): Web · cracked · May 11, 1995 · N404DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING E-1 LETTER CHECK,.375 INCH CRK 48 SEC TORQUE BOX WEB STA 1303 RT AT LIGHTENING HOLE. REPAIRED PER SRM 53-11-0.

Next page: https://openairdocs.org/deregistered/N404DA-2001-02-16/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 = 'N404DA' AND deregistration_id = 'N404DA-2001-02-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N404DA-2001-02-16/reports

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