# Service difficulty reports: N544DA, cancelled Nov 8, 2006

A list on [N544DA, cancelled Nov 8, 2006](https://openairdocs.org/deregistered/N544DA-2006-11-08.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 · 67 reports

- [SDR DL72S030141](https://openairdocs.org/sdr/DL72S030141.md): Battery Pack · discharged · Feb 10, 2003 · N544DA · Boeing 727232 · Emergency Lighting
  > RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72S021479](https://openairdocs.org/sdr/DL72S021479.md): Engine · malfunctioned · Dec 29, 2002 · N544DA · Boeing 727232 · Engine (Turbine/Turboprop)
  > NR 3 ENGINE EGT LIMITED IN CLIMB POWER, EGT 590-595 AT 20 TAT CLIMB THRUST (ON T/O USING ALT 40 TAT CLIMB NR 3 EGT 610). AT 20 TAT CLIMB EPR = 1.88 HAD TO PULL NR 3 THROTTLE BACK TO 1.76 EPR TO KEEP EGT AT / BELOW 580. REPLACED NR 3 ENGINE PER 4T203AD.
- [SDR DL72S020370](https://openairdocs.org/sdr/DL72S020370.md): Charger · failed · Mar 25, 2002 · N544DA · Boeing 727232 · Emergency Lighting
  > LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY, OPERATION NORMAL.
- [SDR DL72S020290](https://openairdocs.org/sdr/DL72S020290.md): Charger · failed · Mar 10, 2002 · N544DA · Boeing 727232 · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER.
- [SDR DL72S011797](https://openairdocs.org/sdr/DL72S011797.md): Light · unserviceable · Nov 12, 2001 · N544DA · Boeing 727232 · Emergency Equipment
  > EXIT SIGN ABOVE 1L DOOR DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS TESTED. REPLACED LIGHT ASSY
- [SDR DL72S011191](https://openairdocs.org/sdr/DL72S011191.md): Seal · torn · Jul 18, 2001 · N544DA · Boeing 727232 · Doors
  > ON CLIMBOUT A LOUD SQUEAL DEVELOPED FROM FORWARD LEFT DOOR. NOISE WAS TOO LOUD TO CONTINUE FLIGHT. DECENDED TO 10,000 FTAND CHANGED CABIN TO 2.0 PSID. NOISE STOPPED. CA RPD L1 DOOR SEAL.
- [SDR DL72S011178](https://openairdocs.org/sdr/DL72S011178.md): Web · cracked · Jul 16, 2001 · N544DA · Boeing 727232 · Fuselage Structure (General)
  > FOUND ON E2 LETTER CK R/H INBD VERT TORQUE BOX WEB CRACKED AT UPPER END STA 1214 R/H. REPAIRED PER MM 53-11-000-8.
- [SDR DL72S011177](https://openairdocs.org/sdr/DL72S011177.md): Clip · cracked · Jul 16, 2001 · N544DA · Boeing 727232 · Fuselage Structure (General)
  > FOUND ON E2 LETTER CK SKIN CLIP CRACKED FWD STA 1263 ABOVE STR 12R. REPAIRED PER B727 DAL DRD 53-10-4D FIG 803D.
- [SDR DL72S010591](https://openairdocs.org/sdr/DL72S010591.md): Light · inoperative · Apr 10, 2001 · N544DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHT ON AFT CARGO DOOR INOPERATIVE. REPLACED LIGHT RACK
- [SDR DL72S010580](https://openairdocs.org/sdr/DL72S010580.md): Battery Pack · discharged · Apr 8, 2001 · N544DA · Boeing 727232 · Emergency Lighting
  > LT OVERWING EMERGENCY EXIT LIGHT FLASHING. REMOVED AND REPLACED BATTERY PACK.
- [SDR DL72S010168](https://openairdocs.org/sdr/DL72S010168.md): Light · inoperative · Jan 29, 2001 · N544DA · Boeing 727232 · Emergency Lighting
  > ON L/O FOUND C-2 DOOR EMERGENCY FLOOD LIGHT INOP. REPLACED SAME.
- [SDR DL72S010163](https://openairdocs.org/sdr/DL72S010163.md): Battery · discharged · Jan 29, 2001 · N544DA · Boeing 727232 · Emergency Lighting
  > DURING STBY PWR CK LT SIDE OVERWING EXIT LIGHTS FAILED TO ILLUMINATE. REPLACED BATTERY PACK. ALL CHECKS NORMAL.
- [SDR DL72S002471](https://openairdocs.org/sdr/DL72S002471.md): Stringer · corroded · Dec 15, 2000 · N544DA · Boeing 727232 · Fuselage Main, Keel
  > FUSELAGE / STRINGER / FS 440 / STRG. 27L: SPLICE REPAIR. STRINGER 27L WAS FOUND CORRODED AT FS 440. THE CORRODED SECTION OF STRINGER WAS CUT AWAY TO REMOVE ALL DAMAGED. THE DAMAGED SECTION WAS REPAIRED WITH TWO (2) ALUMINUM REPAIR ANGLES INSTALLED
- [SDR DL72S000968](https://openairdocs.org/sdr/DL72S000968.md): Skin · cracked · May 16, 2000 · N544DA · Boeing 727232 · Leading Edge Devices
  > NR 3 KRUEGER FLAP CRACKED AT O/B LIP HINGE CUTOUT. TPA D-2 LTR CHK. INSTALLED DOUBLER PER M/M 57-53-0, NR 2A.
- [SDR DL72S000923](https://openairdocs.org/sdr/DL72S000923.md): Engine · leaking · May 9, 2000 · N544DA · Boeing 727232 · Engine (Turbine/Turboprop)
  > OIL QUANTITY DECREASED RAPIDLY ON NR 3 ENG. RATE WAS APPROX 1 GAL PER 5 MIN UNTIL REACHING ZERO. ENG CHANGE IN PROGRESS.
- [SDR DL72S000765](https://openairdocs.org/sdr/DL72S000765.md): Flap Track · corroded · Apr 19, 2000 · N544DA · Boeing 727232 · Trailing Edge Flaps
  > TYPICAL CORROSION WAS FOUND ON THE LOWER SURFACE OF THE NR 4 AND NR 5 FLAP TRACKS AND ON THE UPPER SURFACE OF THE MLG AT THE INTERFACE OF THE FLAP TRACK AND THE MLG SUPPORT BEAM. THE CORROSION WAS MACHINED OR SPOTFACED FOR REMOVAL PER THE GUIDANCE OF B
- [SDR DL72S000334](https://openairdocs.org/sdr/DL72S000334.md): Wire · disconnected · Feb 18, 2000 · N544DA · Boeing 727232 · Light System Wiring
  > EMERGENCY EXIT LIGHT OVERRIDE SWITCH AT AFT FLIGHT ATTENDANT STATION INOP. FOUND ONE WIRE DISCONNECTED FROM AFT ATTENDANT EMERGENCY LIGHT SWITCH. RESECURED WIRE TO SWITCH, OPERATION NOW NORMAL.
- [SDR DL72S992243](https://openairdocs.org/sdr/DL72S992243.md): Engine · malfunctioned · Oct 9, 1999 · N544DA · Boeing 727232 · Engine (Turbine/Turboprop)
  > ON CLIMB-OUT, NR 1 ENG OIL FILTER BYPASS LIGHT ILLUMINATED. S/D ENG PER POM. OIL FILTER FOUND CLEAN. REPLACED SAME, ENGINE RUN CHECKS GOOD.
- [SDR DL72S992221](https://openairdocs.org/sdr/DL72S992221.md): Casting · cracked · Oct 5, 1999 · N544DA · Boeing 727232 · Wing Miscellaneous Structure
  > FOUND ON D1 LETTER CK, NR 4 SLAT ACTUATOR I/B MOUNT CASTING CRACKED. REPLACED CASTING.
- [SDR DL72S992220](https://openairdocs.org/sdr/DL72S992220.md): Stiffner · cracked · Oct 5, 1999 · N544DA · Boeing 727232 · Wing Miscellaneous Structure
  > FOUND ON D1 LETTER CK, NR 4 SLAT I/B TRACK I/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21.
- [SDR DL72S992219](https://openairdocs.org/sdr/DL72S992219.md): Rib · cracked · Oct 5, 1999 · N544DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON D1 LETTER CK, NR 1 SLAT L/E NOSE RIB CRACKED 1.5 INCH AT I/B SIDE OF ACTUATOR. REPAIRED PER MM 57-54-0.
- [SDR DL72S991632](https://openairdocs.org/sdr/DL72S991632.md): Skin · crack · Jul 20, 1999 · N544DA · Boeing 727232 · Trailing Edge Flap Actuator
  > LOWER SKIN CUT TO FACILITATE MAINTENANCE. REPAIRED PER M/M 57-54-0 FIG 801.
- [SDR DL72S991631](https://openairdocs.org/sdr/DL72S991631.md): Rib · cracked · Jul 20, 1999 · N544DA · Boeing 727232 · Wing, Rib/Bulkhead
  > RIB CRACKED. REPAIRED RIB PER M/M 57-54-0.
- [SDR DL72S990467](https://openairdocs.org/sdr/DL72S990467.md): Battery · discharged · Mar 5, 1999 · N544DA · Boeing 727232 · Emergency Lighting
  > FLASHLIGHT HAD NO CHARGE. REPLACED BATTERY, OPS CK GOOD.
- [SDR DL72S990465](https://openairdocs.org/sdr/DL72S990465.md): Battery Pack · discharged · Mar 5, 1999 · N544DA · Boeing 727232 · Emergency Lighting
  > OVERWING RT SIDE EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND OPS CK GOOD.
- [SDR DL72S990457](https://openairdocs.org/sdr/DL72S990457.md): Angle · cracked · Mar 4, 1999 · N544DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON C2 LETTER CK, RT KEEL BEAM SUPPORT ANGLE CRACKED AT STA 870. REPLACED ANGLE PER SRM 53-10-9.
- [SDR DL72S982075](https://openairdocs.org/sdr/DL72S982075.md): Bulkhead Beam · cracked · Oct 2, 1998 · N544DA · Boeing 727232 · Fuselage Main, Bulkhead
  > FUSELAGE BULKHEAD FS 1183 LBL 18 VERTICAL BEAM, REPAIR FOR CRACK. A.75 INCH TYPICAL CRACK WAS FOUND IN RADIUS OF THE LBL 18 VERTICAL BEAM LOWER END ON THE FS 1183 BULKHEAD. THE CRACKED BEAM WAS REPAIRED PER BAC S/B 727-53-0202. THE REPAIR WAS DOCUMENTED PE
- [SDR DL72S980659](https://openairdocs.org/sdr/DL72S980659.md): Fuel Control · failed · Mar 25, 1998 · N544DA · Boeing 727232 · Fuel Control/Turbine Engines
  > NR 3 ENG DID NOT RESPOND TO THROTTLE MOVEMENT DURING DESCENT, FLAMEOUT, FUEL FLOW WAS ZERO. EGT AND EPR WERE ZERO AND NOT RESPONDING. N1 AND N2 DISPLAYED WINDMILLING INDICATION, THIS LASTED FOR 2 TO 3 MINUTES. PRIOR TO COMMENCING THE ENG FAILURE FOLLOW UP C
- [SDR DL72S971773](https://openairdocs.org/sdr/DL72S971773.md): Door · cracked · Sep 9, 1997 · N544DA · Boeing 727232 · Cargo/Baggage Doors
  > AT FL 350 CABIN STARTED CLIMBING AT 650 FPM. CARGO HEAT OUTFLOW AND MAIN OUTFLOW VLV'S CLOSED. LT PACK WENT TO FULL CLOSED AND WOULD NOT CHANGE. NO DUCT OVERHEAT OR PACK TRIP OFF LIGHT, ALSO NO PRESS FAILURE LIGHTS. FOUND C-3 CARGO DOOR FWD LWR CORNER CRAC
- [SDR DL72S960814](https://openairdocs.org/sdr/DL72S960814.md): Angle · cracked · Apr 9, 1996 · N544DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON A-1 LETTER CHECK, 1.5 INCH CRACK IN NR 3 L/E SLAT LWR COVE SKIN ANGLE. REPAIRED PER M/M 57-54-0.
- [SDR DL72S960626](https://openairdocs.org/sdr/DL72S960626.md): Bulb · failed · Mar 21, 1996 · N544DA · Boeing 727232 · Emergency Lighting
  > AFT GALLEY DOOR EXIT LIGHT INOP. RELAMPED, OPERATION NORMAL.
- [SDR DL72S954253](https://openairdocs.org/sdr/DL72S954253.md): Chord · cracked · Oct 27, 1995 · N544DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT, A CRACK AND TEMPORARY REPAIR DOUBLER WAS FOUND ON AFT CHORD OF NR 2 MIDFLAP. INSTALLED PERMANENT REPAIR PER MM 57-53-0.
- [SDR DL72S954254](https://openairdocs.org/sdr/DL72S954254.md): Chord · cracked · Oct 19, 1995 · N544DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT, A CRACK WAS DISCOVERED ON AFT CHORD AT I/B DRIVE ROD CUTOUT, OF NR 2 MIDFLAP. REPAIRED PER MM 57-52-0.
- [SDR DL72S953941](https://openairdocs.org/sdr/DL72S953941.md): Le Skin · worn · Sep 26, 1995 · N544DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSP, NR 3 MIDFLAP WAS FOUND WITH I/B L/E SKIN WORN. REPAIRED LEADING EDGE PER MM 57520, BY REMOVING DAMAGED AREA AND INSTALLING A DOUBLER AND FILLER.
- [SDR DL72S953942](https://openairdocs.org/sdr/DL72S953942.md): Skin · worn · Sep 25, 1995 · N544DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSP, NR 4 MIDFLAP L/E SKIN WORN AT O/B END OF FLAP. REPAIRED PER MM 57520 BY REMOVING DAMAGED AREA AND INSTALLING A DOUBLER AND FILLER.
- [SDR DL72S953818](https://openairdocs.org/sdr/DL72S953818.md): Cowling · cracked · Sep 25, 1995 · N544DA · Boeing 727232 · Engine Cowling System
  > DURING A SHOP INSPECTION, THE UPPER FRAME ANGLE WAS FOUND TO BE CRACKED. A REPAIR WAS INSTALLED PER THE S.R.M. 54-10-3. FOR NR 2 ENGINE LEFT FORWARD COWL PANEL.
- [SDR DL72S953879](https://openairdocs.org/sdr/DL72S953879.md): Frame · misdrilled · Sep 22, 1995 · N544DA · Boeing 727232 · Fuselage Main, Frame
  > DURING THE ACCOMPLISHMENT OF DAL EO 4-58560-3AD, IT WAS NOTICED BY MAINTENANCE THAT THE FRAME REINFORCEMENT STRAP ON THE OUTER CHORD OF STA 760.95 FRAM, WAS DOUBLE DRILLED AT THREE LOCATIONS PRIOR TO THIS HEAVY MAINTENANCE VISIT. MAINTENANCE OVERSIZED THE HOL
- [SDR DL72S954036](https://openairdocs.org/sdr/DL72S954036.md): Skin · corroded · Sep 20, 1995 · N544DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > BELLY SKIN, CORROSION AT STA 700 TO 720, O/B OF S-28L AD 91-09-09, 94-05-04. SKIN CORROSION AT STA 700 TO 720, O/B OF S-28L HAS PROMPTED REQUEST FOR AN EXTENSION OF AN EXISTING DOUBLER IN THAT AREA TO COVER THE ADDED DAMAGE REMOVAL, APPROXIMATLY 2 BY 2 INCHES
- [SDR DL72S953779](https://openairdocs.org/sdr/DL72S953779.md): Rib · cracked · Sep 20, 1995 · N544DA · Boeing 727232 · Vertical Stabilizer, Spar/Rib
  > DURING HMV, FOUND ON VERTICAL FIN 4TH RIB DOWN FROM ACCESS HOLE STA 6.372 RIB NR 6 CHORD ANGLE CRACKED AT STR 7 LEFT. REPAIRED PER M/M 55-30-0 PG 802.
- [SDR DL72S953778](https://openairdocs.org/sdr/DL72S953778.md): Rib · cracked · Sep 19, 1995 · N544DA · Boeing 727232 · Leading Edge Devices
  > DURING HMV, FOUND NR 8 SLAT, RIB NR 13 WAS CRACKED IN RADIUS. REPAIRED PER M/M 57-54-0 FIG 805.
- [SDR DL72S953777](https://openairdocs.org/sdr/DL72S953777.md): Rib · cracked · Sep 18, 1995 · N544DA · Boeing 727232 · Leading Edge Devices
  > DURING HMV, FOUND NR 4 SLAT HAS CRACK AT ACTUATOR ATTACH O/B RIB. REPAIRED PER MM 57-54-0 FIG 804.
- [SDR DL72S953776](https://openairdocs.org/sdr/DL72S953776.md): Rib · cracked · Sep 18, 1995 · N544DA · Boeing 727232 · Leading Edge Devices
  > DURING HMV, FOUND NR 3 SLAT HAS CRACK IN LOWER SURFACE OF NR 3 RIB FROM I/B END. REPAIRED PER MM 57-54-0 FIG 805.
- [SDR DL72S953748](https://openairdocs.org/sdr/DL72S953748.md): Angle · cracked · Sep 18, 1995 · N544DA · Boeing 727232 · Leading Edge Devices
  > FOUND DURING HMV - NR 6 SLAT, CRACKED ANGLE BETWEEN DE-ICE TUBE AND FARTHEST ROLLER TRACK. REPAIRED PER M/M 57-54-0, FIG 812.
- [SDR DL72S953730](https://openairdocs.org/sdr/DL72S953730.md): Actuator Mount · cracked · Sep 18, 1995 · N544DA · Boeing 727232 · Leading Edge Devices
  > FOUND AT HMV, NR 4 SLAT MAIN ACTUATOR MOUNT CRACKED AT PREVIOUSLY REPAIRED AREA. REPAIRED PER M/M 57-54-0, FIG 804A.
- [SDR DL72S953729](https://openairdocs.org/sdr/DL72S953729.md): Rib · cracked · Sep 18, 1995 · N544DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON HMV RIB WEB AT TAI, TUBE CRACKED AT NR 6 SLAT INBOARD WEB. REPAIRED RIB PER M/M 57-54-0, FIG 805.
- [SDR DL72S953878](https://openairdocs.org/sdr/DL72S953878.md): Frame · oversized holes · Sep 17, 1995 · N544DA · Boeing 727232 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF EO 4-61904-3AD, SEVERAL HOLES IN THE INBOARD FRAME FLANGE AT FS 760.95, BOTH RT AND LT SIDES WERE OVERSIZED THROUGH THE STRAP, FRAME, AND MODIFICATION ANGLE. ONE HOLE ON THE LEFT HAND SIDE HAS BEEN OVERSIZED TO 0.403 DIA AND REQUIRES
- [SDR DL72S953775](https://openairdocs.org/sdr/DL72S953775.md): Beam · cracked · Sep 15, 1995 · N544DA · Boeing 727232 · Passenger/Crew Doors
  > DURING HMV, FOUND FWD ENTRY DOOR LOWER HORIZONTAL BEAM CRACKED AT AFT CORNER. REPAIRED PER M/M 52-11-01 PG 805.
- [SDR DL72S953695](https://openairdocs.org/sdr/DL72S953695.md): Bracket · cracked · Sep 14, 1995 · N544DA · Boeing 727232 · Leading Edge Devices
  > DURING HMV, FOUND NR 6 KRUEGER FLAP ACTUATOR BRACKET IS CRACKED AT I/B LOWER FWD CORNER. REPAIRED PER M/M 57-20-21.
- [SDR DL72S953774](https://openairdocs.org/sdr/DL72S953774.md): Skin · cracked · Sep 13, 1995 · N544DA · Boeing 727232 · Elevator, Plate/Skin
  > DURING HMV, FOUND LT ELEVATOR SKIN CRACKED APPROX 1.5 INCH CRACK IN UPPER SKIN I/B END NEAR LEADING EDGE. REPAIRED PER SRM 55-20-3.
- [SDR DL72S953880](https://openairdocs.org/sdr/DL72S953880.md): Rib · crack · Sep 12, 1995 · N544DA · Boeing 727232 · Wing, Rib/Bulkhead
  > DURING THE ACCOMPLISHMENT OF EO 4-58560-3AD, A CRACK WAS DETECTED IN A FASTENER HOLE IN THE VERTICAL FLANGE OF THE RIB CHORD AT BS 760.95. REMOVAL OF THE CRACK IN THE RIB CHORD RESULTED IN THE INADVERTENT OVERSIZING OF THE FUSELAGE SKIN AT THIS LOCATION, AS W

Next page: https://openairdocs.org/deregistered/N544DA-2006-11-08/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 = 'N544DA' AND deregistration_id = 'N544DA-2006-11-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N544DA-2006-11-08/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.