# Service difficulty reports: N411DA, cancelled Feb 16, 2001

A list on [N411DA, cancelled Feb 16, 2001](https://openairdocs.org/deregistered/N411DA-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 · 97 reports

- [SDR DL72S002208](https://openairdocs.org/sdr/DL72S002208.md): Light · inoperative · Nov 10, 2000 · N411DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHT OVER L2 DOOR INOP. REPLACED LIGHT ASSY AND BATTERIES, OPS NML.
- [SDR DL72S002149](https://openairdocs.org/sdr/DL72S002149.md): Actuator · leaking · Nov 2, 2000 · N411DA · Boeing 727232 · Leading Edge Slat Actuator
  > ON SLAT EXTENSION NR 6 SLAT NO INTRANSIT OR EXTEND LIGHT. CYCLED SLATS AND LOST A SYS HYD QTY. REPLACED NR 6 SLAT ACTUATOR FOR LEAKING.
- [SDR DL72S002129](https://openairdocs.org/sdr/DL72S002129.md): Battery Pack · discharged · Oct 28, 2000 · N411DA · Boeing 727232 · Emergency Lighting
  > ON SERVICE CK, EMERGENCY LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72S001967](https://openairdocs.org/sdr/DL72S001967.md): Light · inoperative · Oct 10, 2000 · N411DA · Boeing 727232 · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT WILL NOT ILLUM. REPLACED SAME.
- [SDR DL72S000947](https://openairdocs.org/sdr/DL72S000947.md): Keelbeam · cracked · May 12, 2000 · N411DA · Boeing 727232 · Fuselage Main, Keel
  > FOUND ON C1 LETTER CK, LOWER I/B FWD VERTICAL KEEL BEAM ANGLE CRACKED RT WHEEL WELL STA 870. REPAIRED PER MM 53-10-9D.
- [SDR DL72S000946](https://openairdocs.org/sdr/DL72S000946.md): Attach Angle · cracked · May 12, 2000 · N411DA · Boeing 727232 · Wing Miscellaneous Structure
  > FOUND ON C1 LETTER CK, 1 INCH CRACK NR 11 SPOILER ACTUATOR I/B ATTACH ANGLE. REPAIRED PER MM 57-42-0.
- [SDR DL72S992591](https://openairdocs.org/sdr/DL72S992591.md): Battery Pack · discharged · Nov 23, 1999 · N411DA · Boeing 727232 · Emergency Lighting
  > DURING L/O CHECK, FOUND SVL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTS AND PACKS, ALL CHECK OK.
- [SDR DL72S991891](https://openairdocs.org/sdr/DL72S991891.md): Wire · broken · Aug 23, 1999 · N411DA · Boeing 727232 · Light System Wiring
  > CEILING EMERGENCY EXIT LIGHT NEAR OVERWING EXIT IS INOP. REPAIRED A BROKEN WIRE AT THE LIGHT ASSY CONNECTOR.
- [SDR DL72S991307](https://openairdocs.org/sdr/DL72S991307.md): Skin · cracked · Jun 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING LFEC INSPECTION PER SI 4-74176-12AD, NUMEROUS CRACK INDICATIONS WERE FOUND IN THE VARIOUS FRAME BAYS EXTENDING FROM BS 360-480 ALONG S4R. THERE WAS A PREVIOUS REPAIR PER ERA 332834-14AD, REV B WHICH WILL BE REMOVED AND INCORPORATED INTO THIS REPAIR. R
- [SDR DL72S991287](https://openairdocs.org/sdr/DL72S991287.md): Skin · cracked · Jun 8, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED 14 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP FOR THE PANEL WAS CUTOUT AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 367553-14
- [SDR DL72S990616](https://openairdocs.org/sdr/DL72S990616.md): Flap Track · corroded · Mar 15, 1999 · N411DA · Boeing 727232 · Trailing Edge Flaps
  > DURING OUTSIDE REPAIR, OVERHAUL PER CMM AND MOD PER SB 727-57-0178, TYPICAL CORROSION WAS FOUND TO THE FWD ATTACH LUGS AND THE MLG BEAM AND SPOILER BEAM ATTACH PADS AND HOLES. AUTHORIZED BUSHING REPAIR FOR FWD ATTACH LUG AND OVERSIZED SPOILER BEAM ATTACH H
- [SDR DL72S990615](https://openairdocs.org/sdr/DL72S990615.md): Flap Track · corroded · Mar 15, 1999 · N411DA · Boeing 727232 · Trailing Edge Flaps
  > DURING OUTSIDE REPAIR OF COMPONENT AND OVERHAUL PER CMM AND MOD PER SB 727-57-0178, TYPICAL CORROSION WAS FOUND ON THE MLG BEAM AND SPOILER BEAM ATTACH PAD AND HOLES. AUTHORIZED OVERSIZED FASTENERS, BUSHING REPAIR AND LEAVING THE OVERSIZED MLG BEAM ATTACH HOL
- [SDR DL72S990522](https://openairdocs.org/sdr/DL72S990522.md): Skin · cracked · Mar 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12 ON THE S4R LAP JOINT CRACK INDICATIONS WERE FOUND BETWEEN BS 681 AND BS 740. HFEC INSPECTION CONFIRMED 8 CRACK INDICAITONS IN THE LOWER FASTENER ROW OF THE LAP JOINT, IN THE LWR SKIN. REPAIRED PER ERA 33
- [SDR DL72S990521](https://openairdocs.org/sdr/DL72S990521.md): Skin · cracked · Mar 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING LFEC INSP PER SI 4-74176-12, ON THE S4R LAP JOINT CRACK INDICATIONS WERE FOUND BETWEEN BS 481 AND 680. HFEC CONFIRMED 15 CRACK INDICATIONS IN THE LWR FASTENER ROW OF THE LAP JOINT IN THE LWR SKIN. REPAIRED PER ERA 332838-14AD, REV A.
- [SDR DL72S990520](https://openairdocs.org/sdr/DL72S990520.md): Frame · dented · Mar 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, Frame
  > TWO DENTED AREAS WERE FOUND ON THE I/B CHORD OF THE BS 950C FRAME BETWEEN S24L AND 27L. REPAIRED PER ERA 332897-14, REV A.
- [SDR DL72S990490](https://openairdocs.org/sdr/DL72S990490.md): Skin · cracked · Mar 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING LFEC INSPECTIONS PER SI 4-74176-12AD ON S4R LAP JOINT, 2 CRACK INDICATIONS WERE FOUND BETWEEN BS 360 AND 481. HFEC INSP VERIFIED CRACK INDICATIONS. REPAIRED PER ERA 332834-14AD, REV A.
- [SDR DL72S990489](https://openairdocs.org/sdr/DL72S990489.md): Skin · misdrilled · Mar 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS MISDRILLED AT S11R AT BS 1233. REPAIRED PER ERA 332842-14, REV A.
- [SDR DL72S990488](https://openairdocs.org/sdr/DL72S990488.md): Fitting · corroded · Mar 10, 1999 · N411DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > CORROSION FOUND IN THE RT MLG SUPPORT BEAM O/B BORE AND IN THE FWD AND AFT FITTINGS. REWORKED PER ERA 332851-14.
- [SDR DL72S990487](https://openairdocs.org/sdr/DL72S990487.md): Fitting · corroded · Mar 10, 1999 · N411DA · Boeing 727232 · Wing, Fuselage Attach Fittings
  > CORROSION WAS FOUND IN THE BORE OF THE RT WING AFT TERMINAL FITTING. REPAIRED PER ERA 366788-14, REV A.
- [SDR DL72S990486](https://openairdocs.org/sdr/DL72S990486.md): Frame · corroded · Mar 10, 1999 · N411DA · Boeing 727232 · Fuselage Main, Frame
  > BS 600 FRAME BELOW THE CARGO FLOOR AT STR 28R WAS FOUND CORRODED. THE UPPER FRAME OF THE LOWER LOBE CTR FRAME SECTION AND SOME EXISTING REPAIRS WERE ALSO FOUND CORRODED. REPAIRED PER ERA 332893-14, REV A.
- [SDR DL72S990441](https://openairdocs.org/sdr/DL72S990441.md): Fitting · worn · Mar 3, 1999 · N411DA · Boeing 727232 · Horizontal Stabilizer Structure
  > WEAR WAS FOUND ON BOTH ATTACH LUGS FOR THE HORIZ STAB JACK SCREW MECHANISM. WEAR WAS ON BOTH I/B AND O/B FACES OF EACH LUG. REWORKED PER ERA 332860-14, REV A.
- [SDR DL72S990385](https://openairdocs.org/sdr/DL72S990385.md): Skin · torn · Feb 24, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > GOUGE IN SKIN AT THE AFT EDGE OF THE C-2 DOOR CUTOUT AT FS 990. DAMAGED AREA LOCATED AT 2-24R. SKIN, DOUBLER, TRIPLER AND BEAR STRAP ARE ALL DAMAGED. ACTION TAKEN, ERA 332858-14.
- [SDR DL72S990361](https://openairdocs.org/sdr/DL72S990361.md): Frame · dented · Feb 24, 1999 · N411DA · Boeing 727232 · Fuselage Main, Frame
  > FRAME DENTED AFT CARGO COMPT LT FRAME DENTED AT STA 950B ABOVE STR 26L. REMOVED DAMAGED PER SRM 53-10-4 FIG 27. DYE PENETRANT CHECKED PER PS 900-6-3, NO CRACKS NOTED. DRILLED NEW DUCT PER SRM 53-10-4 FIG 27. REMOVED WEB FROM STA 950A TO 950B AT STR 25L. I
- [SDR DL72S990360](https://openairdocs.org/sdr/DL72S990360.md): Frame · dented · Feb 24, 1999 · N411DA · Boeing 727232 · Fuselage Main, Frame
  > FRAME DENTED LT FS 1070, STR 26L. REMOVED DAMAGED AREA, DYE CHECKED PER PS 900-6-3 NR 1. NO FURTHER DAMAGE FOUND. FABRICATED DOUBLER, INSTALLED DOUBLER PER SRM 53-10-4 FIG 27.
- [SDR DL72S990461](https://openairdocs.org/sdr/DL72S990461.md): Fitting · corroded · Feb 23, 1999 · N411DA · Boeing 727232 · Fuselage, Wing Attach Fittings
  > AT HMV2, FOUND CORROSION IN BORES AND MATING SEAM OF AFT RT WING AND FUS REMINAL FITTINGS. BLENDED CORROSION, CHECKED, REWORKED PER ERA 366788-14, INSTALLED BUSHNG.
- [SDR DL72S990398](https://openairdocs.org/sdr/DL72S990398.md): Frame · cracked · Feb 23, 1999 · N411DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > OVERWING EXIT FRAME STA 761 RT, 784 LT AND 784 RT FOUND CRACKED IN I/B FLANGE. ACTION TAKEN, ERA 361976-14AD.
- [SDR DL72S990397](https://openairdocs.org/sdr/DL72S990397.md): Skin · damaged · Feb 23, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE AT AN EXISTING FASTENER IN THE SKIN BETWEEN S-7R AND S-8R AT STA 277. ACTION TAKEN, ERA 255827-14.
- [SDR DL72S990751](https://openairdocs.org/sdr/DL72S990751.md): Skin · worn · Feb 17, 1999 · N411DA · Boeing 727232 · Trailing Edge Flaps
  > LOWER L/E SKIN WORN O/B END OF FLAP APPROX 6 INCHES LONG. REPAIRED PER MM 57-52-0 FIG 803.
- [SDR DL72S991362](https://openairdocs.org/sdr/DL72S991362.md): Spar · damaged · Feb 16, 1999 · N411DA · Boeing 727232 · Trailing Edge Flaps
  > AFT SPAR RAIL DAMAGED AT 2ND FROM I/B AFT FLAP TRACK CUT OUT. REPAIRED PER M/M 57-52-0 FIG 802.
- [SDR DL72S990477](https://openairdocs.org/sdr/DL72S990477.md): Skin · cracked · Feb 15, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > AT HMV2, FOUND SKIN CRACKED - EMPENNAGE EXIT, LOC AT FWD RT CORNER OF AFT AIRSTAIRS CUTOUT. FABRICATED DOUBLER PER MM 53-30-00 PG 803. STOP DRILLED CRACK, INSTALLED DOUBLER.
- [SDR DL72S990450](https://openairdocs.org/sdr/DL72S990450.md): Frame · dented · Feb 15, 1999 · N411DA · Boeing 727232 · Fuselage Main, Frame
  > FRAME DENTED AFT CARGO COMPT LT FRAME DENTED AT STA 950C SEVERAL PLACES FROM STR 27L TO 25L. REMOVED DAMAGE PER SRM 53-10-4 FIG 27, FABRICATED DOUBLER PER SRM 53-10-4 FIG 27. REMOVED FACTORY SPLICE. INSTALLED REPAIR PER SRM 53-10-4 FIG 27 REV NR 1170.
- [SDR DL72S990416](https://openairdocs.org/sdr/DL72S990416.md): Frame · dented · Feb 15, 1999 · N411DA · Boeing 727232 · Fuselage Main, Frame
  > FRAME DENTED AFT CARGO COMPT RT FRAME DENTED AT STA 950C SEVERAL PLACES FROM STR 25R TO STR 26R. CUT OUT DAMAGE PER SRM 53-10-4 FIG 27. DYE PENETRANT INSPECTED CUTOUT PER PS 900-6-3 NO 1 AND FOUND OK. DRILLED DOUBLER AND FILLER PER SRM 53-10-4 FIG 27 AND TR
- [SDR DL72S990379](https://openairdocs.org/sdr/DL72S990379.md): Skin · cracked · Feb 15, 1999 · N411DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > SKIN CRACKED EMPENNAGE EXT LOC AT AFT I/B CORNER OF ACCESS PNL 3903 CUTOUT. FABRICATED DOUBLER PER M/M 53-30-0 PG 803. STOP DRILLED CRACK, INSTALLED DOUBLER PER MM 53-30-0 PG 803, IDENTIFIED PER PS 900-5-1 NR 4.
- [SDR DL72S990462](https://openairdocs.org/sdr/DL72S990462.md): Skin · cracked · Jan 16, 1999 · N411DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED IN TWO PLACES AT THE I/B AFT FLAP DRIVE ROD CUTOUT. THE CRACK WAS REMOVED AND A DOUBLER INSTALLED PER 727 MM 57-52-0 FIG 809.
- [SDR DL72S982455](https://openairdocs.org/sdr/DL72S982455.md): Retract Mech · lack of lube · Nov 29, 1998 · N411DA · Boeing 727232 · Trailing Edge Flap Control System
  > OUTBOARD FLAPS WOULD NOT EXTEND PAST 15 TO 20 DEGS. DIVERTED TO JFK. PERFORMED OPS CHECK, COULD NOT DUPLICATE. DUE PREVIOUS ITEMS, SERVICED TRANS AND JACKSCREW GEARBOXES LUBED TRACKS AND JACKSCREW BALLNUTS ON OUTBOARD FLAPS.
- [SDR DL72S982220](https://openairdocs.org/sdr/DL72S982220.md): Wire · shorted · Oct 28, 1998 · N411DA · Boeing 727232 · Light System Wiring
  > FOUND ON MAINT PREFLIGHT ROWS 12-19 EMERGENCY TRACK LIGHTINGINOP REPLACED BLOWN FUSE ON FWD POWER SUPPLY AFTER REPAIRINGBARE WIRES UNDER SEAT ROW 12 DEF LIGHT OPN NORMAL REPLACED FWD BATTERY PRECAUTIONARY.
- [SDR DL72S982157](https://openairdocs.org/sdr/DL72S982157.md): Battery · discharged · Oct 16, 1998 · N411DA · Boeing 727232 · Emergency Lighting
  > SEAT ROW 25 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY, OPS NOW OK.
- [SDR DL72S982010](https://openairdocs.org/sdr/DL72S982010.md): Angle · cracked · Aug 10, 1998 · N411DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 19 AND 23 INCHES FROM I/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.
- [SDR DL72S982009](https://openairdocs.org/sdr/DL72S982009.md): Angle · cracked · Aug 10, 1998 · N411DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 37 INCHES FROM I/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.
- [SDR DL72S982008](https://openairdocs.org/sdr/DL72S982008.md): Angle · cracked · Aug 10, 1998 · N411DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 35 INCHES FROM THE I/B END. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 802.
- [SDR DL72S982007](https://openairdocs.org/sdr/DL72S982007.md): Angle · cracked · Aug 10, 1998 · N411DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 44 INCHES FROM O/B END. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.
- [SDR DL72S981085](https://openairdocs.org/sdr/DL72S981085.md): Rib · cracked · May 19, 1998 · N411DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON A-1 LETTER CHECK, NR 6 SLAT NOSE RIB CRACKED I/B SIDE OF ACTUATOR.75 INCH. REPAIRED PER M/M 57-54-0.
- [SDR DL72S981084](https://openairdocs.org/sdr/DL72S981084.md): Fitting · cracked · May 19, 1998 · N411DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > TAIL SECTION TIE BOLT FITTING CRACKED LT I/B FITTING, CRACKED JUST O/B OF BOLT HEAD. REPLACED FITTING PER BOEING DWG 65-17509 REV M.
- [SDR DL72S981083](https://openairdocs.org/sdr/DL72S981083.md): Stiffener · cracked · May 19, 1998 · N411DA · Boeing 727232 · Wing Miscellaneous Structure
  > NR 3 SLAT O/B TRACK I/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21 P 813.
- [SDR DL72S981082](https://openairdocs.org/sdr/DL72S981082.md): Bracket · cracked · May 19, 1998 · N411DA · Boeing 727232 · Wing Miscellaneous Structure
  > NR 1 SLAT ACT O/B ATTACH BRACKET CRACKED AT I/B WEB. REPAIRED PER MM 57-20-21 P 812.
- [SDR DL72S981081](https://openairdocs.org/sdr/DL72S981081.md): Skin · crcaked · May 19, 1998 · N411DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND AT A-1 LETTER CHECK, 1.125 INCH CRACK AT FUSELAGE SKIN AT MAIN ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED PER 53-30-3.
- [SDR DL72S972383](https://openairdocs.org/sdr/DL72S972383.md): Battery · discharged · Nov 16, 1997 · N411DA · Boeing 727232 · Emergency Lighting
  > ON PREFLIGHT, COCKPIT EMERGRNCY LIGHT DID NOT ILLUM IN STBY PWR. REPLACED BATTS, OPS NOW OK.
- [SDR DL72S972160](https://openairdocs.org/sdr/DL72S972160.md): Skin · cracked · Oct 25, 1997 · N411DA · Boeing 727232 · Elevator, Plate/Skin
  > .5 INCH CRACK IN LOWER SKIN OF LT ELEVATOR 5 INCHES FROM I/B EDGE. REPAIRED PER SRM 55-20-3.
- [SDR DL72S972157](https://openairdocs.org/sdr/DL72S972157.md): Stringer · cracked · Oct 25, 1997 · N411DA · Boeing 727232 · Vertical Stabilizer
  > VERT FIN STR 9L IS CRACKED AT FIN STA 133.800. REPAIR PER MM 55-30-0.
- [SDR DL72S972156](https://openairdocs.org/sdr/DL72S972156.md): Stringer · cracked · Oct 25, 1997 · N411DA · Boeing 727232 · Vertical Stabilizer
  > VERT FIN STR 9L CRACKED AT FIN STA 157.200. REPAIR PER MM 55-30-0.

Next page: https://openairdocs.org/deregistered/N411DA-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 = 'N411DA' AND deregistration_id = 'N411DA-2001-02-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N411DA-2001-02-16/reports

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