# Service difficulty reports: N406DA, cancelled Feb 16, 2001

A list on [N406DA, cancelled Feb 16, 2001](https://openairdocs.org/deregistered/N406DA-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 · 60 reports

- [SDR DL72S002085](https://openairdocs.org/sdr/DL72S002085.md): Battery Pack · inoperative · Oct 22, 2000 · N406DA · Boeing 727232 · Emergency Lighting
  > FOUND THE BATTERY PACK INOP AT THE AFT CARGO DOOR EMERGENCY LIGHTS. CHANGED BATTERY PACK, EMERGENCY LIGHTS ARE OK.
- [SDR DL72S001796](https://openairdocs.org/sdr/DL72S001796.md): Transmitter · inoperative · Sep 17, 2000 · N406DA · Boeing 727232 · Trailing Flap Position Indicating System
  > OUTBOARD FLAP INDICATIONS SPLIT AT 15 DEG CAUSING A LOCKOUT. ALT FLAP EXTEND USED. INDICATORS BOUNCE BETWEEN SPLIT AND EQUAL SETTINGS. NO ROLL TENDENCIES WERE FELT WHEN FLAPS WERE EXTENDED. REPLACED LEFT OUTBOARD FLAP TRANSMITTER PER M/M. FLAP IND AND OPE
- [SDR DL72S001765](https://openairdocs.org/sdr/DL72S001765.md): Angle · cracked · Sep 11, 2000 · N406DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON C1 LETTER CK, 1.25 INCH CRACK IN THE RT FS 870 KEEL BEAM I/B ATTACH ANGLE. STOP DRILLED CRACK PER B727 DRD 53-10-9D FIG 806D.
- [SDR DL72S001710](https://openairdocs.org/sdr/DL72S001710.md): Bracket · broken · Sep 6, 2000 · N406DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > 2L GIRT BAR ATTACH FITTING TO FLOOR SPRING BROKEN, BAR WILL NOT ENGAGE. REPLACED BROKEN BRACKET.
- [SDR DL72S001706](https://openairdocs.org/sdr/DL72S001706.md): Battery · discharged · Sep 5, 2000 · N406DA · Boeing 727232 · Emergency Equipment
  > AFT I/B EMERGENCY FLASHLIGHT BATTERY DEAD. REPLACED BATTERY.
- [SDR DL72S001566](https://openairdocs.org/sdr/DL72S001566.md): Battery · leaking · Aug 15, 2000 · N406DA · Boeing 727232 · Emergency Lighting
  > L1 OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY DUE TO WEAK BATTERIES LEAKING INTO LIGHT ASSY.
- [SDR DL72S001039](https://openairdocs.org/sdr/DL72S001039.md): Light · inoperative · May 26, 2000 · N406DA · Boeing 727232 · Emergency Lighting
  > AFT AIRSTAIRS EMERGENCY LIGHT FAILED TO TEST. REPLACED LIGHT ASSY.
- [SDR DL72S000571](https://openairdocs.org/sdr/DL72S000571.md): Battery · inoperative · Mar 24, 2000 · N406DA · Boeing 727232 · Emergency Lighting
  > LEFT AFT OVERWING EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. LIGHT OPN CKS GOOD.
- [SDR DL72S000273](https://openairdocs.org/sdr/DL72S000273.md): Bulkhead · cracked · Feb 7, 2000 · N406DA · Boeing 727232 · Fuselage Main, Bulkhead
  > FS 870 WEB CRACKED RT MLG W/W AT APU LOAD CONTROL VALVE. CUT OUT 1.5 INCH AT 6:00 POS. INSTALLED TIME LIMITED REPAIR PER SRM 53-10-9D FIG 806D.
- [SDR DL72S000272](https://openairdocs.org/sdr/DL72S000272.md): Angle · cracked · Feb 7, 2000 · N406DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A 2 INCH CRACK IN TORQUE BOX SHELF ANGLE FWD SIDE OF STA 1263. REPLACED ANGLE PER SRM 53-10-10D FIGURE 803D.
- [SDR DL72S992251](https://openairdocs.org/sdr/DL72S992251.md): Battery · discharged · Oct 10, 1999 · N406DA · Boeing 727232 · Emergency Lighting
  > AFT AIRSTAIR EMERGENCY LIGHTS INOP. REPLACED BATTERY'S, OPS NOW OK.
- [SDR DL72S992130](https://openairdocs.org/sdr/DL72S992130.md): Battery · discharged · Sep 23, 1999 · N406DA · Boeing 727232 · Emergency Lighting
  > AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP ON L/O CHECK. REPLACED BATTERYS (P/N 334101877), OPER NOW NORMAL.
- [SDR DL72S991960](https://openairdocs.org/sdr/DL72S991960.md): Battery Pack · discharged · Sep 3, 1999 · N406DA · Boeing 727232 · Emergency Lighting
  > RT AFT 2 OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS M957 AND M956, OPS CHKS GOOD.
- [SDR DL72S991935](https://openairdocs.org/sdr/DL72S991935.md): Insulation · split · Aug 2, 1999 · N406DA · Boeing 727232 · Electrical Power System Wiring
  > ON HUSH-KIT MOD FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISC WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL-24-0
- [SDR DL72S991487](https://openairdocs.org/sdr/DL72S991487.md): Web · cracked · Jul 1, 1999 · N406DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > TPA LTR CHK B1,.375 INCH CRACK TORQUE BOX VERT WEB STA 1226. REPAIRED PER MM 53-11-0.
- [SDR DL72S991485](https://openairdocs.org/sdr/DL72S991485.md): Frame · cracked · Jul 1, 1999 · N406DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND AT B-1 LTR CK, AFT ENTRY DOOR FRAME CUTOUT CRACKED LT SIDE 10 INCHES FROM TOP OF CUTOUT. REPAIRED PER SRM 53-10-9.
- [SDR DL72S990747](https://openairdocs.org/sdr/DL72S990747.md): Skin · cracked · Apr 1, 1999 · N406DA · 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 PANEL. INTERNAL HFEC INSPECTION CONFIRMED 11 CRACKS ALONG THE PANEL. THE SKIN LAP WAS CUT OUT OVER THE LENGTH OF THE PANEL
- [SDR DL72S990746](https://openairdocs.org/sdr/DL72S990746.md): Skin · cracked · Apr 1, 1999 · N406DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 25 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP WAS CUT OUT ALONG THE PANEL LENGTH AND R
- [SDR DL72S982437](https://openairdocs.org/sdr/DL72S982437.md): Skin · damaged · Nov 25, 1998 · N406DA · Boeing 727232 · Horizontal Stabilizer, Plate/Skin
  > LWR SKIN OF THE LT HORIZONTAL STAB HAS A PRE-EXISTING EXTERNAL T/L REPAIR. NEED PERMANENT REPAIR INSTRUCTIONS. REPAIRED PER ERA 332447-14.
- [SDR DL72S982282](https://openairdocs.org/sdr/DL72S982282.md): Rib · cracked · Nov 6, 1998 · N406DA · Boeing 727232 · Wing, Rib/Bulkhead
  > DURING SHOP INSPECTION, A REPAIR DOUBLER AT THE I/B AFT RIB WAS FOUND TO BE CRACKED. THE DOUBLER WAS REMOVED AND THE RIB WAS REPAIRED PER MM 57-52-0 FIG 808.
- [SDR DL72S982567](https://openairdocs.org/sdr/DL72S982567.md): Spar · cracked · Nov 5, 1998 · N406DA · Boeing 727232 · Trailing Edge Flaps
  > NR 2 MID FLAP, CRACK AFT SPAR RAIL 33 FROM I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 615732.
- [SDR DL72S982301](https://openairdocs.org/sdr/DL72S982301.md): Flap Track · corroded · Nov 5, 1998 · N406DA · Boeing 727232 · Trailing Edge Flaps
  > INBOARD FLAP INBOARD TRACK TYP CORROSION AT FWD LUG AND MLG BEAM ATTACH HOLES: AD 90-07-05. INSTALL OVERSIZED BUSHINGS IN FWD LUG HOLES, OVERSIZE MLG BEAM ATTACH HOLES AND PROCEED WITH SPLICE PLATE REPAIR PER BAC SB 727-57-0178.
- [SDR DL72S982404](https://openairdocs.org/sdr/DL72S982404.md): Angle · cracked · Nov 4, 1998 · N406DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 19 INCHES FROM I/B END. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.
- [SDR DL72S982369](https://openairdocs.org/sdr/DL72S982369.md): Skin · cracked · Nov 3, 1998 · N406DA · Boeing 727232 · Elevator, Plate/Skin
  > SKIN CRACKED APPROX 1.5 ON LWR SURFACE OF RT ELEV FWD AND I/B OF TAB CONTROL ROD. DYE CHECKED AND STOP DRILLED CRACKS, FABRICATED REPAIR PART PER SRM 55-20-3 FIG 5. OK TO INSTALL. INSTALLED DOUBLER, FASTENERS AND DOUBLE WEIGH 63G PER SRM 55-20-3 FIG 5.
- [SDR DL72S982363](https://openairdocs.org/sdr/DL72S982363.md): Angle · damaged · Nov 3, 1998 · N406DA · Boeing 727232 · Leading Edge Devices
  > NR 4 SLAT, ANGLE CRACKED IN CORNER. DYE CHECKED PER PS 900-6-3. NO CRACK FOUND. BURNISHED AREA, TREATED AND PAINTED PER PS 900-2 NR 5.
- [SDR DL72S982440](https://openairdocs.org/sdr/DL72S982440.md): Skin · corroded · Oct 25, 1998 · N406DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A SKIN BULGE AND TWO CRACKED FASTENER HOLES WERE DISCOVERED AT BS 681, 8 INCHES ABOVE STRINGER 14R. UPON FURTHER INSPECTION CORROSION WAS FOUND ON THE I/B SIDE OF THE WINDOW BELT SKIN PANEL. REPAIRED PER ERA 332473-14.
- [SDR DL72S982439](https://openairdocs.org/sdr/DL72S982439.md): Frame · damaged · Oct 25, 1998 · N406DA · Boeing 727232 · Fuselage Main, Frame
  > LOWER LOBE FRAMES IN THE AFT B/B AT BS 1030 WERE FOUND DENTED BETWEEN S26R AND 27R. MISDRILLED HOLES WERE DONE DURING ACCOMPLISHMENT OF SRM REPAIR. REPAIRED PER ERA 332463-14AD.
- [SDR DL72S982438](https://openairdocs.org/sdr/DL72S982438.md): Shear Tie · damaged · Oct 25, 1998 · N406DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > SHEAR TIES AT BS 580 AND 620, S14R WERE DAMAGED DUE TO REWORK OF THE SKIN LAP JOINT. REPAIRED PER ERA 332452-14.
- [SDR DL72S980928](https://openairdocs.org/sdr/DL72S980928.md): Battery Pack · discharged · Apr 30, 1998 · N406DA · Boeing 727232 · Emergency Lighting
  > ON INSP, FOUND AFT EMERGENCY EXIT SIGN NO TEST. REPLACED BATTERY PACK.
- [SDR DL72S980623](https://openairdocs.org/sdr/DL72S980623.md): Angle · cracked · Mar 20, 1998 · N406DA · Boeing 727232 · Leading Edge Slat Actuator
  > NR 7 SLAT ACT O/B ATTACH ANGLE CRACKED AT UPPER LOBE. REPAIRED PER MM 57-42-0.
- [SDR DL72S980622](https://openairdocs.org/sdr/DL72S980622.md): Web · cracked · Mar 20, 1998 · N406DA · Boeing 727232 · Leading Edge Devices
  > NR 8 SLAT ACT I/B AND O/B ATTACH ANGLE CRACKED AT WEB. REPAIRED PER MM 57-20-21.
- [SDR DL72S980621](https://openairdocs.org/sdr/DL72S980621.md): Angle · cracked · Mar 20, 1998 · N406DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON A1 LETTER CK, NR 8 SLAT LOWER ATTACH ANGLE CRACKED AT THE INBD STOP PAD. REPAIRED PER MM 57-54-0.
- [SDR DL72S980620](https://openairdocs.org/sdr/DL72S980620.md): Stiffener · cracked · Mar 20, 1998 · N406DA · Boeing 727232 · Wing Miscellaneous Structure
  > FOUND ON A1 LETTER CK, 1 INCH CRACK IN LOWER END OF L/E SPAR STIFFENER NR 2 SLAT O/B TRACK, INBD STIFFENER. REPAIRED PER MM 57-20-21.
- [SDR DL72S972567](https://openairdocs.org/sdr/DL72S972567.md): Roller · binding · Dec 8, 1997 · N406DA · Boeing 727232 · Passenger/Crew Doors
  > AFTER TAKEOFF, THE LEFT FORWARD ENTRY DOOR DID NOT SEAL PROPERLY. DAYLIGHT COULD BE SEEN THROUGH THE DOOR SEAL. FOUND DOOR NOT CLOSED PROPERLY. INSPECTED DOOR, FOUND CAMPLATE ROLLER BINDING. REPLACED ROLLER, FOUND UPPER DOOR GUIDE HINGE GUIDE ARM OUT OF AD
- [SDR DL72S972081](https://openairdocs.org/sdr/DL72S972081.md): Fuel Control · failed · Oct 17, 1997 · N406DA · Boeing 727232 · Fuel Control/Turbine Engines
  > APPROX 40 MINS INTO FLIGHT AT FL330 THE NR 1 ENG INVOLUNTARILY WENT TO FULL POWER. THE THROTTLE DID NOT MOVE. PHYSICAL MOVEMENT OF THE THROTTLE PRODUCED NO ENGINE RESPONSE. PARAMETERS AT SHUTDOWN AS FOLLOWS OIL PRESSURE POSITIVE 45 EPR 2.4 N1-102 EGT-600C
- [SDR DL72S970340](https://openairdocs.org/sdr/DL72S970340.md): Spar · cracked · Feb 12, 1997 · N406DA · Boeing 727232 · Trailing Edge Flaps
  > DURING THE CURRENT SHOP VISIT AND INSPECTION PER SI 4-58705-12AD, THE UPPER CHORD WAS FOUND COMPLETELY FRACTURED. THE SPAR WEB WAS NOT DAMAGED. HOWEVER, THE FRACTURE OF THE UPPER CHORD APPARENTLY CAUSED A CRACK IN THE SKIN BETWEEN TWO FASTENER HOLES. MAINTE
- [SDR DL72S970201](https://openairdocs.org/sdr/DL72S970201.md): Compressor Case · damaged · Feb 1, 1997 · N406DA · Boeing 727232 · Turbine Engine Compressor Section
  > ON TAKEOFF AT 1,000 FEET, NR 1 ENGINE FIRE LIGHT ILLUMINATED AND FIRE BELL OCCURRED. ALL ENGINE INDICATIONS ON TAKEOFF AND FIRE LIGHT WERE NORMAL AND APPROX EQUAL. ALL EMERGENCY CHECK LISTS COMPLETED AND RETURNED TO LAND, ENGINE WAS THEN SHUT DOWN ON FINAL.
- [SDR DL72S970179](https://openairdocs.org/sdr/DL72S970179.md): Fitting · cracked · Jan 3, 1997 · N406DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > THE LT INBOARD STR 3A TENSION TIE FITTING WAS FOUND CRACKED. THE TENSION TIE BOLT HAS BEEN REPLACED IN ACCORDANCE WITH S/B 727-53-0178 WHICH IS REQUIRED BY A.D. 90-06-09. THE FITTING WAS REPLACED PER S/B 727-53-0095.
- [SDR DL72S970043](https://openairdocs.org/sdr/DL72S970043.md): Angle · worn · Dec 24, 1996 · N406DA · Boeing 727232 · Nacelle/Pylon Structure
  > FOUND THE LWR LIP OF FWD COWL SUPPORT ANGLE WORN AT THE NR 2 ENG FIREWALL. THE DAMAGE WAS REMOVED AND A NEW FRAME DRILLED AND INSTALLED PER SRM 53-11-0, PG 801.
- [SDR DL72S962101](https://openairdocs.org/sdr/DL72S962101.md): Battery Pack · discharged · Sep 11, 1996 · N406DA · Boeing 727232 · Emergency Lighting
  > RT AFT SLIDE EMERG LITE INOP C/A RPLD BATT PACK AT RACK M957 OPS CHKS GOOD
- [SDR DL72S961986](https://openairdocs.org/sdr/DL72S961986.md): Light · inoperative · Aug 27, 1996 · N406DA · Boeing 727232 · Emergency Lighting
  > ON LAYOVER, FOUND LEFT FWD ENTRY DOOR EMERGENCY LIGHT NOT TESTING. REPLACED LIGHT ASSEMBLY (P/N 334701743) AND BATTERIES. LIGHT NOW TESTS OK.
- [SDR DL72S961414](https://openairdocs.org/sdr/DL72S961414.md): Torque Box · cracked · May 21, 1996 · N406DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > THERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF THE AD 94-07-08 WHICH REQUIRES INSPECTION PER SB 53-0129. THIS ERA WILL REPLACE THE DAMAGED PART IN ACCORD
- [SDR DL72S961293](https://openairdocs.org/sdr/DL72S961293.md): Transverse Beam · cracked · May 21, 1996 · N406DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > CRACK IN ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA IS SUBJECT OF AD 94-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ERA WILL REPLACE THE DAMAGED PART IN ACCORDANCE WITH THE S/B.
- [SDR DL72S961224](https://openairdocs.org/sdr/DL72S961224.md): Skin · cracked · May 20, 1996 · N406DA · Boeing 727232 · Elevator, Plate/Skin
  > A.5 INCH CRACK FROM FASTENER RT ELEVATOR LOWER SKIN JUST INBD OF 3RD FROM OUTBD HINGE. REPAIRED PER SRM 55-20-3.
- [SDR DL72S961223](https://openairdocs.org/sdr/DL72S961223.md): Skin · cracked · May 20, 1996 · N406DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A.5 INCH CRACK IN FUSELAGE SKIN AT LWR INBD CORNER OF R-4 WINDOW CUTOUT. REPAIRED PER SRM 53-30-3.
- [SDR DL72S961222](https://openairdocs.org/sdr/DL72S961222.md): Tq Box Web · cracked · May 20, 1996 · N406DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > TORQUE BOX VERTICAL WEB CRACKED 1 INCH AT FASTENER, UPPER ROW OF RIVETS STA 1233 LT LOWER TORQUE BOX. REPAIRED PER M/M 53-11-0 FIG 819.
- [SDR DL72S961221](https://openairdocs.org/sdr/DL72S961221.md): Door Frame · cracked · May 20, 1996 · N406DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > 1 INCH CRACK AT RT AFT SERVICE DOOR FWD FRAME ON FUSE, EXTENDING FROM UPPER STOP PAD CASTING. REPAIRED PER MM 53-13-0.
- [SDR DL72S960643](https://openairdocs.org/sdr/DL72S960643.md): Bulb · failed · Mar 23, 1996 · N406DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY TRACK LIGHTING UNDER SEAT 31D IS OUT. RELAMPED BULB, CKS NORMAL.
- [SDR DL72S960175](https://openairdocs.org/sdr/DL72S960175.md): Rib · cracked · Nov 21, 1995 · N406DA · Boeing 727232 · Leading Edge Devices
  > DURING INSPECTION, NR 8 LE SLAT WAS FOUND WITH INTERNAL RIB NR 3 AND NR 2 CRACKED. REPAIRED PER MM 57-54-0.
- [SDR DL72S954060](https://openairdocs.org/sdr/DL72S954060.md): Angle · cracked · Oct 19, 1995 · N406DA · Boeing 727232 · Leading Edge Devices
  > NR 6 L/E SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT O/B END. REPAIRED PER SRM 57-54-0. FOUND AT LETTER CHECK.

Next page: https://openairdocs.org/deregistered/N406DA-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 = 'N406DA' AND deregistration_id = 'N406DA-2001-02-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N406DA-2001-02-16/reports

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