# Service difficulty reports: N416DA, cancelled Jul 11, 2013

A list on [N416DA, cancelled Jul 11, 2013](https://openairdocs.org/deregistered/N416DA-2013-07-11.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 · 56 reports

- [SDR DL72S001143](https://openairdocs.org/sdr/DL72S001143.md): Skin · cracked · Jun 13, 2000 · N416DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON S26L FROM BS 480 TO 680, CRACK INDICATIONS WERE FOUND IN TWO FRAME BAYS. HFEC INSPECTION OF THE ENTIRE LAP JOINT VERIFIED TWO CRACKS IN THE LWR ROW OF THE LWR SKIN BETWEEN BS 540 AND 560 AT FASTENERS
- [SDR DL72S000780](https://openairdocs.org/sdr/DL72S000780.md): Connector · corroded · Apr 21, 2000 · N416DA · Boeing 727232 · Trailing Edge Flap Control System
  > DURING FLAP RETRACTION AT THE 15 DEG POSITION THE I/B FLAPS INDICATED ASYMMETRY. POM PROCEDURE C/W. RETURNED TO CVG. LANDING WEIGHT 151,000 LBS. SMOOTH LANDING. FOUND RIGHT /B CANNON PLUG AT TRANSMITTER CORRODED. REPLACED SAME. NO HELP. ISOLATED PROBLEM
- [SDR DL72S000670](https://openairdocs.org/sdr/DL72S000670.md): Fitting · cracked · Apr 7, 2000 · N416DA · Boeing 727232 · Empennage Structure
  > LEFT I/B TENSION TIE FITTING CRACKED IN 48 SEC. REPLACED FITTING PER BAC DRAWING 65-17509 REV M. NRC 63 TPA F-2 LTR CHECK.
- [SDR DL72S000550](https://openairdocs.org/sdr/DL72S000550.md): Valve · leaking · Mar 20, 2000 · N416DA · Boeing 727232 · Rudder Control System
  > SYSTEM A HYD LOSS IN FLT. DIVERTED TO ELP. FOUND LWR RUDDER PCU YAW DAMPER ENGAGE SOLENOID VALVE LEAKING. REPLACED SOLENOID VALVE AND HYDRAULIC CASE DRAIN AND PRESS FILTERS.
- [SDR DL72S992574](https://openairdocs.org/sdr/DL72S992574.md): Beam · cracked · Nov 20, 1999 · N416DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > THE RBL 17.8 VERTICAL DOOR BEAM ON THE FS 1183 BULKHEAD WAS FOUND WITH A SMALL CRACK IN A FASTENER HOLE COMMON TO AN EXISTING REPAIR. THE CRACK WAS REMOVED BY OVERSIZING THE.0625 INCH FASTENER HOLE TO.296 DIA WITH AN ADDITIONAL.0625 OVERSIZE. THE CRACK WA
- [SDR DL72S992211](https://openairdocs.org/sdr/DL72S992211.md): Spar Web · cracked · Oct 3, 1999 · N416DA · Boeing 727232 · Wing Spar
  > CENTER WING, REAR SPAR, WEB LBL 17, CRACK REPAIR. THE CENTER WING REAR SPAR WEB WAS FOUND WITH A.5 TYPICAL CRACK NEAR THE UPPER SPAR CAP. THE CRACK IS TYPICAL OF BAC S/B 727-57A0182. THE CRACK WAS ROUTED OUT OF THE WEB AND REPAIRED WITH AN ALUMINUM DOUBLER
- [SDR DL72S992012](https://openairdocs.org/sdr/DL72S992012.md): Stiffener · cracked · Sep 10, 1999 · N416DA · Boeing 727232 · Wing Miscellaneous Structure
  > 2 INCH VISIBLE CRACK IN VERT SPAR STIFFENER I/B SIDE OF O/B TRACK NR 3 L/E SLAT. REPAIRED PER MM 57-20-21 P 813.
- [SDR DL72S992011](https://openairdocs.org/sdr/DL72S992011.md): Stiffener · cracked · Sep 10, 1999 · N416DA · Boeing 727232 · Leading Edge Devices
  > L/E SPAR STIFFENER CRACKED AT NR 7 SLAT I/B TRACK O/B SIDE OF TRACK. REPAIR PER MM 57-20-21.
- [SDR DL72S992010](https://openairdocs.org/sdr/DL72S992010.md): Skin · cracked · Sep 10, 1999 · N416DA · Boeing 727232 · Nacelle/Pylon Structure
  > .5 INCH CRACK ON DUCT HOUSING SKIN AT PANEL 9524 RT SIDE. REPAIR PER MM 54-30-0.
- [SDR DL72S992009](https://openairdocs.org/sdr/DL72S992009.md): Web · cracked · Sep 10, 1999 · N416DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > .25 INCH CRACK ON LEFT VERT TORQUE BOX WEB LWR LIGHTING HOLE STA 1290. ROUTE OUT CRACK PER MM 53-11-0.
- [SDR DL72S992008](https://openairdocs.org/sdr/DL72S992008.md): Stringer · cracked · Sep 10, 1999 · N416DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND ON F1 LETTER CK, 1 INCH CRACK IN STRINGER 18A AT STA 940 IN THE UPPER AND LOWER RADIUS RT. REPAIRED PER MM 53-12-0.
- [SDR DL72S991845](https://openairdocs.org/sdr/DL72S991845.md): Light · broken · Aug 17, 1999 · N416DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT 10D BROKEN. REPLACED BULBS AND LIGHT COVER ASSY.
- [SDR DL72S991555](https://openairdocs.org/sdr/DL72S991555.md): Light · inoperative · Jul 10, 1999 · N416DA · Boeing 727232 · Emergency Lighting
  > R1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY AND BATTERIES, OPS NOW OK.
- [SDR DL72S991554](https://openairdocs.org/sdr/DL72S991554.md): Battery · discharged · Jul 10, 1999 · N416DA · Boeing 727232 · Emergency Lighting
  > AFT AIRSTAIR EMERG EXIT LIGHT INOP. REPLACED BATTERIES, OPS NOW OK.
- [SDR DL72S990903](https://openairdocs.org/sdr/DL72S990903.md): Skin · cracked · Apr 24, 1999 · N416DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 481-681 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 6 CRACKS IN TWO ADJ
- [SDR DL72S990902](https://openairdocs.org/sdr/DL72S990902.md): Skin · cracked · Apr 24, 1999 · N416DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 440-460 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRA
- [SDR DL72S990268](https://openairdocs.org/sdr/DL72S990268.md): Rib · cracked · Feb 9, 1999 · N416DA · Boeing 727232 · Vertical Stabilizer
  > VERTICAL FIN RIB CHORD CRACKED 1.25 INCH FIN STA 133.800, AT STR 8 ATTACH BOLT RT SIDE. REPAIR PER M/M 55-30-0 FIG 802.
- [SDR DL72S990267](https://openairdocs.org/sdr/DL72S990267.md): Clip · cracked · Feb 9, 1999 · N416DA · Boeing 727232 · Vertical Stabilizer
  > 1 IN CRACK IN LT VERT FIN SKIN TO RIB ATTACH CLIP, STA 180.600 ABOVE STR 10. REPAIR PER M/M 55-30-0 FIG 803.
- [SDR DL72S990266](https://openairdocs.org/sdr/DL72S990266.md): Panel · cracked · Feb 9, 1999 · N416DA · Boeing 727232 · Elevator Structure
  > 2 INCH CRACK NR 2 BALANCE BOARD CLOSE OUT PANEL, RT ELEVATOR. REPAIR PER SRM 55-20-3.
- [SDR DL72S981854](https://openairdocs.org/sdr/DL72S981854.md): Battery Pack · discharged · Sep 7, 1998 · N416DA · Boeing 727232 · Emergency Lighting
  > DURING L/O, FOUND OVERWING EMERGENCY EXIT LIGHTS NOT ILLUM AT LT WING STA 804. REPLACED BATTERY PACK, OP CKS NORMAL.
- [SDR DL72S981805](https://openairdocs.org/sdr/DL72S981805.md): Fan · failed · Aug 31, 1998 · N416DA · Boeing 727232 · Air Distribution Fan
  > SMOKE AND FUMES IN COCKPIT AND CABIN, RAN CK LIST AND COULD NOT FIND SOURCE. ALSO, ELECTRICAL BURNT PLASTIC SMELL. INSPECTED COALESCER BAGS, CKS GOOD. INSPECTED E & E AREA, CKS GOOD. INSPECTED GALLEY AREA, CKS GOOD. FOUND SMELL COMING FROM GASPER FAN, RAN
- [SDR DL72S981574](https://openairdocs.org/sdr/DL72S981574.md): Line · failed · Jul 29, 1998 · N416DA · Boeing 727232 · Hydraulic System, Main
  > 20 MIN AFTER TAKEOFF FROM ABQ, HAD TOTAL LOSS OF A SYSTEM HYDRAULICS. C/W POM PROCEDURES. DIVERTED TO DFW. REPLACED BROKEN LINE TO A SYSTEM HYDRAULIC MODULE. REPLACED NR 1 ENGINE DRIVEN HYD PUMP. PRESSURE AND LEAK CHECK OK.
- [SDR DL72S981415](https://openairdocs.org/sdr/DL72S981415.md): Skin · cracked · Jul 6, 1998 · N416DA · Boeing 727232 · Passenger/Crew Doors
  > FOUND ON E1 LETTER CK,.25 INCH CRACK IN L1 DOOR SKIN AT LOWER HINGE CUTOUT. REPAIRED PER MM 52-11-0.
- [SDR DL72S981387](https://openairdocs.org/sdr/DL72S981387.md): Stringer · cracked · Jul 2, 1998 · N416DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > SEVERAL FASTENER HOLES AT S18A AT FS 940 ON THE LT SIDE WERE FOUND CRACKED. CRACKS WERE IN THE STRINGER ONLY AND DID NOT EXTEND TO THE UNDERLYING STRUCTURE. REPAIRED PER ERA 331854-14.
- [SDR DL72S981386](https://openairdocs.org/sdr/DL72S981386.md): Skin · corroded · Jul 2, 1998 · N416DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > CORROSION DAMAGE FOUND IN THE LWR SKIN AT APPROX FS720C+10 AT S26R. REPAIRED PER ERA 331866-14.
- [SDR DL72S981385](https://openairdocs.org/sdr/DL72S981385.md): Frame · cracked · Jul 2, 1998 · N416DA · Boeing 727232 · Fuselage Main, Frame
  > WHILE PERFORMING THE REPAIR/MOD PER EO 4-61904-3AD. MAINTENANCE FOUND THE 2ND FASTENER BELOW THE FLOOR LINE TO BE AT A DIAMETER OF 0.375. REPAIRED PER ERA 331852-14AD.
- [SDR DL72S981395](https://openairdocs.org/sdr/DL72S981395.md): Skin · corroded · Jul 1, 1998 · N416DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND AT STA 1009 AND STR 28L ON THE INTERNAL SKIN BUTT SPLICE STRAP IN AN AREA PREVIOUSLY REPAIRED. THE PREVIOUS REPAIRS WERE REMOVED, AND RE-REPAIRED. REPAIRED PER ERA 237701-14.
- [SDR DL72S981521](https://openairdocs.org/sdr/DL72S981521.md): Doubler · damaged · Jun 19, 1998 · N416DA · Boeing 727232 · Trailing Edge Flaps
  > REPAIR DOUBLER IS CRACKED AT LWR AFT SPAR 21 AND 35 FROM I/B END. THIS DAMAGE WAS REPAIRED PER M/M 57-52-0, FIG 802. THIS DAMAGED WAS RECORDED ON N/R 007474 AND 007475.
- [SDR DL72S981522](https://openairdocs.org/sdr/DL72S981522.md): Skin · damaged · Jun 18, 1998 · N416DA · Boeing 727232 · Trailing Edge Flaps
  > COVE SKIN IS CRACKED 32 FROM I/B END. THIS DAMAGED WAS RECORRED ON SHOP N/R 007470 AND REPAIRED PER M/M 57-52-0 FIG 809.
- [SDR DL72S981321](https://openairdocs.org/sdr/DL72S981321.md): Angle · cracked · Jun 18, 1998 · N416DA · Boeing 727232 · Vertical Stabilizer
  > ANGLE CRACKED INSIDE OF VERT STAB 4TH BAY DOWN FROM OPENING STR 5 ON RT SIDE CRACK IS ON VERT LEG. REMOVED FASTENERS, DRILLED OP REPAIR PARTS PER MM 55-30-0 PG 802. INSTALLED DOUBLER PER MM 55-30-0 PG 802.
- [SDR DL72S981320](https://openairdocs.org/sdr/DL72S981320.md): Stringer · cracked · Jun 15, 1998 · N416DA · Boeing 727232 · Vertical Stabilizer
  > STRINGER CRACKED INSIDE VERTICAL STAB 4TH BAY UP FROM ACCESS 9504 STR 8R. STOP DRILLED CRACK, DYE CHECKED PER PS900-6-3, NR 1 FABRICATED REPAIR PER M/M 53-30-0 FIG 803. INSTALLED DOUBLER PER MM 53-30-0 FIG 803.
- [SDR DL72S981305](https://openairdocs.org/sdr/DL72S981305.md): Skin · damaged · Jun 15, 1998 · N416DA · Boeing 727232 · Horizontal Stabilizer, Plate/Skin
  > OUTER SKIN DAMAGED AT FASTENER HOLE ON PANEL 9115. REPAIRED PER SRM 55-30-3 FIG 3.
- [SDR DL72S981304](https://openairdocs.org/sdr/DL72S981304.md): Web · cracked · Jun 15, 1998 · N416DA · Boeing 727232 · Vertical Stabilizer
  > VERT WEB CRACKED INSIDE STABILIZER ABOVE S-DUCT STA 1303. REPAIRED PER SRM 53-10-4 FIG 17, LT AND RT SIDE.
- [SDR DL72S981269](https://openairdocs.org/sdr/DL72S981269.md): Skin · separated · Jun 15, 1998 · N416DA · Boeing 727232 · Elevator, Plate/Skin
  > RT ELEVATOR I/B T/E SKIN, SEPARATED. DRILLED REPAIR FASTENER HOLES PER M/M 55-20-0 PG 801. INSTALLED REPAIR FASTENER PER M/M 55-20-0 PG 801.
- [SDR DL72S980838](https://openairdocs.org/sdr/DL72S980838.md): Battery Pack · discharge · Apr 18, 1998 · N416DA · Boeing 727232 · Emergency Lighting
  > EMERG LIGHT IN THE COCKPIT IS INOP. REPLACED BATTERY PACK ASSY AND THE BATTERIES CK OK.
- [SDR DL72S980401](https://openairdocs.org/sdr/DL72S980401.md): Battery Pack · discharged · Feb 17, 1998 · N416DA · Boeing 727232 · Emergency Lighting
  > L1, R1, L2 AND R2 DOORS EMERGENCY LIGHTS INOP. REPLACED BATT PACKS.
- [SDR DL72S980382](https://openairdocs.org/sdr/DL72S980382.md): Battery · discharged · Feb 10, 1998 · N416DA · Boeing 727232 · Emergency Lighting
  > ON S/C, FOUND AFT SECTION OF EMERGENCY ESCAPE LIGHTS INOP. REPLACED BATTER, OPS NORMAL.
- [SDR DL72S972485](https://openairdocs.org/sdr/DL72S972485.md): Skin · cracked · Nov 26, 1997 · N416DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > A.1875 INCH CRACK IN SKIN RT LOWER FWD CORNER OF VERTICAL STAB SADDLE PLATE CUTOUT (PANEL 9501). INSTALLED DOUBLER PER M/M54-30-0 FIG 802.
- [SDR DL72S972091](https://openairdocs.org/sdr/DL72S972091.md): Battery Pack · discharged · Oct 18, 1997 · N416DA · Boeing 727232 · Emergency Lighting
  > ON S/C, FOUND LT AND RT FWD DOOR EXTEROIR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, OPS NORMAL.
- [SDR DL72S971784](https://openairdocs.org/sdr/DL72S971784.md): Light · inoperative · Sep 11, 1997 · N416DA · Boeing 727232 · Emergency Lighting
  > COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY.
- [SDR DL72S971650](https://openairdocs.org/sdr/DL72S971650.md): Batteries · discharged · Aug 23, 1997 · N416DA · Boeing 727232 · Emergency Lighting
  > EMERG LIGHTS ABOVE AFT AIRSTAIRS INOP. REPLACED BATTERIES.
- [SDR DL72S970244](https://openairdocs.org/sdr/DL72S970244.md): Battery Pack · discharged · Feb 8, 1997 · N416DA · Boeing 727232 · Emergency Lighting
  > ELECTRICAL COMPARTMENT EMERGENCY LIGHT INOP. REPLACED BATT, PACK.
- [SDR DL72S962139](https://openairdocs.org/sdr/DL72S962139.md): Acm · contaminated · Sep 19, 1996 · N416DA · Boeing 727232 · Cabin Cooling System
  > SMOKE IN CABIN DURING CRUISE FLT. INSPECTED CABIN NR 1 AND 2 ENGINES AND LEFT AND RIGHT PACKS. FOUND WATER IN RIGHT ACM OIL. REPLACED RIGHT ACM AND COALESCER, OPS CK NORMAL.
- [SDR DL72S961371](https://openairdocs.org/sdr/DL72S961371.md): Floor Beam · corroded · May 29, 1996 · N416DA · Boeing 727232 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON FLOOR BEAM, STA 1030 UPPER FLANGE FASTENER HOLES AT LBL 0 AND LBL 9. REPAIRED PER M/M 53-20-11 PG 811B.
- [SDR DL72S961370](https://openairdocs.org/sdr/DL72S961370.md): Floor Beam · corroded · May 29, 1996 · N416DA · Boeing 727232 · Fuselage Main, Floor Beam
  > FOUND CORROSION 0N TOP OF FLOOR BEAM AT STA 1070, RBL 44 TO RBL 58. REPAIRED PER M/M 53-20-11 FIG 804A.
- [SDR DL72S960732](https://openairdocs.org/sdr/DL72S960732.md): Seal · torn · Apr 1, 1996 · N416DA · Boeing 727232 · Cargo/Baggage Doors
  > AT FLIGHT LEVEL 290 LOUD RUMBLE FOLLOWED BY RAPID RISE IN CABIN ALT. BOTH OUTFLOW VALVES CLOSED AND FLT LEVEL 220, CABIN STILL CLIMBING SLOWLY. DESCENDED TO 10,000 FT TO MAINTAIN PRESS. FOUND FWD CARGO DOOR SEAL DAMAGE AND OUT OF RETAINER. REPLACED DOOR SE
- [SDR DL72S960502](https://openairdocs.org/sdr/DL72S960502.md): Web · cracked · Mar 1, 1996 · N416DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON C1 LETTER CK, TORQUE BOX WEB CRACKED.50 INCH AT STA 1235, LT, AND.1250 INCH AT STA 1263 RT. REPAIRED PER MM 53-11-0.
- [SDR DL72S960501](https://openairdocs.org/sdr/DL72S960501.md): Angle · cracked · Mar 1, 1996 · N416DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON C1 LETTER CK, FOUND 1.25 INCH CRACK AT NR 7 SLAT I/B TRACK BOX INBD ANGLE. REPAIRED PER MM 57-20-21.
- [SDR DL72S954383](https://openairdocs.org/sdr/DL72S954383.md): Winshield · delaminated · Nov 14, 1995 · N416DA · Boeing 727232 · Flight Compartment Windows
  > CAPT WINDSCREEN DELAMINATED, RETARDS VISION. REPLACED WINDSCREEN.
- [SDR DL72S953190](https://openairdocs.org/sdr/DL72S953190.md): Skin · cracked · Jul 25, 1995 · N416DA · Boeing 727232 · Wing, Plate/Skin
  > 2.25 INCH CRACK IN WING L/E SKIN AT WS 463.0 AFT OF NR 5 SLAT ABOVE REFUELING PANEL. FOUND AT B2 LTR CK. REPAIRED PER MM 57-20-21.

Next page: https://openairdocs.org/deregistered/N416DA-2013-07-11/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 = 'N416DA' AND deregistration_id = 'N416DA-2013-07-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N416DA-2013-07-11/reports

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