# Service difficulty reports: N543DA, cancelled Jul 20, 2010

A list on [N543DA, cancelled Jul 20, 2010](https://openairdocs.org/deregistered/N543DA-2010-07-20.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 · 80 reports

- [SDR DL72S020607](https://openairdocs.org/sdr/DL72S020607.md): Compressor · damaged · May 29, 2002 · N543DA · Boeing 727232 · Turbine Engine Compressor Section
  > NR 3 ENG WOULD NOT ACCELERATE ON ADDING T/O POWER. ABORTED T/O AT ABOUT 30 KTS. BORESCOPE INSPECTED 3 ENG 6 AND 7 STG COMP. FOUND 7 STG COMP BLD DAMAGE BEYOND M/M LIMITS. FULL LENGTH OF BLD. ALL BBLDS DAMAGED (361774). REPLACED 3 ENG PER CARD DECK 4T203
- [SDR DL72S020344](https://openairdocs.org/sdr/DL72S020344.md): Outflow Valve · malfunctioned · Mar 20, 2002 · N543DA · Boeing 727232 · Pressure Regulator/Outflow Valve
  > DURING CLIMBOUT FROM ATL, CABIN ALT CONT TO CLIMB AT 400 FT / MIN TO APPROX 9800 FT. A DESCENT WAS INITIATED AT 27000 FT TO AN ALTITUDE OF 16000 FT WHERE PRESSURIZATION COULD BE MAINTAINED. CARGO VALVE INDICATOR CLOSED THE ENTIRE FLIGHT. CHANGES TO BLEED SO
- [SDR DL72S020213](https://openairdocs.org/sdr/DL72S020213.md): Frame · cracked · Feb 20, 2002 · N543DA · Boeing 727232 · Fuselage Structure (General)
  > FOUND ON F-2 LETTER CK 3/4 IN CRACK MLG UPLOCK FRAME SUPPORTSTRUCTURE AT STA 913 RIGHT W/W. REPAIRED PER MM 53-11-000-8.
- [SDR DL72S011790](https://openairdocs.org/sdr/DL72S011790.md): Door Frame · cracked · Nov 11, 2001 · N543DA · Boeing 727232 · Fuselage Main, Structure
  > THE FWD FRAME OF THE C1 DOOR OPENING AT FS 560 WAS FOUND WITH TWO WEB CRACKS AT EXISTING FASTENER LOCATIONS BELOW THE UPPER DOOR SILL. THE CRACKS ARE TYPICAL OF BAC S/B 727-53-0219 AND AD 99-23-13. THE CRACKS WERE CUT OUT OF THE WEB AND REPAIRED WITH A TITAN
- [SDR DL72S011722](https://openairdocs.org/sdr/DL72S011722.md): Slat · cracked · Oct 16, 2001 · N543DA · Boeing 727232 · Wing Miscellaneous Structure
  > MULTIPLE RIBS CRACKED,REPAIRED PER AMM 57-54-000-8 FIG 814
- [SDR DL72S011236](https://openairdocs.org/sdr/DL72S011236.md): Angle · cracked · Jul 25, 2001 · N543DA · Boeing 727232 · Wing Structure
  > COVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT #3 SLAT __REPAIRED PER MM 57-54-000-8
- [SDR DL72S011235](https://openairdocs.org/sdr/DL72S011235.md): Angle · cracked · Jul 25, 2001 · N543DA · Boeing 727232 · Wing Structure
  > COVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT #2 SLAT __REPAIRED PER MM 57-54-000-8
- [SDR DL72S011234](https://openairdocs.org/sdr/DL72S011234.md): Bracket · cracked · Jul 25, 2001 · N543DA · Boeing 727232 · Wing Structure
  > 3 INCH CRACK AT #1 SLAT ACT. ATTACH I/B AND O/B BRACKET __REPAIRED PER M/M 57-20-021-8
- [SDR DL72S011232](https://openairdocs.org/sdr/DL72S011232.md): Stiffener · cracked · Jul 25, 2001 · N543DA · Boeing 727232 · Wing Miscellaneous Structure
  > FOUND ON F-1 CK 1 INCH CRACK L/E WING VERTICAL SPAR STIFFENER O/B SIDE OF NUMBER 6 SLAT O/B TRACK.
- [SDR DL72S011231](https://openairdocs.org/sdr/DL72S011231.md): Angle · cracked · Jul 25, 2001 · N543DA · Boeing 727232 · Wing Structure
  > FOUND ON F1 LETTER CK NUMBER 8 SLAT ACTUATOR INBD ATTACH ANGLE CRACKED. REPAIRED PER MM 57-20-021-8.
- [SDR DL72S010876](https://openairdocs.org/sdr/DL72S010876.md): Indicator · faulty · May 31, 2001 · N543DA · Boeing 727232 · Trailing Flap Position Indicating System
  > AFTER TAKEOFF RETRACTING FLAPS TO 5 DEGS INBD FLAPS REMAINED AT 15 DEGS. INBOARD FLAPS REMAINED AT 15 DEGS AFTER POM PROCEDURES. PILOT DECLARED EMERGENCY. REPLACED INBD FLAP POSITION IND AND INBD FLAP ASSY LOCK OUTRELAY R-187.
- [SDR DL72S010210](https://openairdocs.org/sdr/DL72S010210.md): Battery · inoperative · Feb 6, 2001 · N543DA · Boeing 727232 · Emergency Lighting
  > L2 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, CHECKS GOOD.
- [SDR DL72S010177](https://openairdocs.org/sdr/DL72S010177.md): Engine · missing · Jan 31, 2001 · N543DA · Boeing 727232 · Engine (Turbine/Turboprop)
  > NR 3 OIL QTY DECREASE TO ZERO. DURING CRUISE FOLLOWED BY FLUCUATING OIL PRESS, SHUT DOWN NR 3 ENGINE PER POM. COMPLETED ENGINE FLAME OUT / LOSS OF THRUST SHUTDOWN FORM. ENGINE SHUTDOWN TIME 30 MIN / OIL PRESS WINDMILL 25 PSI / OIL QTY 0. FOUND 3 STUDS ON G
- [SDR DL72S000998](https://openairdocs.org/sdr/DL72S000998.md): Frame · cracked · May 19, 2000 · N543DA · Boeing 727232 · Fuselage Main, Frame
  > A.5 INCH CRACK WAS FOUND IN THE WEB OF THE C1 DOOR OPENING AFT FRAME (FS 620) JUST BELOW THE NR 6 DOOR STOP. THE CRACK WAS COMMON TO A FASTENER HOLE ATTACHING THE WEB TO THE OUTER FRAME CHORD. THE WEB WAS LOCALLY TRIMMED AWAY TO REMOVE THE CRACK AND REPAIR
- [SDR DL72S000938](https://openairdocs.org/sdr/DL72S000938.md): Skin · corroded · May 10, 2000 · N543DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 560 OVER STRINGER 28L. THE CORROSION WAS REMOVED WITH A 14 X 1.5 CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 377271-14.
- [SDR DL72S000637](https://openairdocs.org/sdr/DL72S000637.md): Line · chafed · Apr 4, 2000 · N543DA · Boeing 727232 · Hydraulic System, Main
  > A SYSTEM FAILURE. FOUND LINE TO NR 2 LEAKING. REPLACED WITH TEMP/APPROVED LINE. LEAK AND OPS CKS GOOD. HYD FLUID AT 3 GAL.
- [SDR DL72S000520](https://openairdocs.org/sdr/DL72S000520.md): Battery · discharged · Mar 16, 2000 · N543DA · Boeing 727232 · Emergency Lighting
  > AFT CABIN DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS NOW OK.
- [SDR DL72S000519](https://openairdocs.org/sdr/DL72S000519.md): Battery · discharged · Mar 16, 2000 · N543DA · Boeing 727232 · Emergency Lighting
  > MID CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY, OPS NOW OK.
- [SDR DL72S000249](https://openairdocs.org/sdr/DL72S000249.md): Door · failed · Feb 2, 2000 · N543DA · Boeing 727232 · Cabin Cooling System
  > RIGHT PACK TRIP FOLLOWED BY SMOKE IN CABIN. FOUND RT COOLING DOOR NOT OPENING WHEN PACK SELECTED. REPLACED RT COOLING DOOR ACTUATOR RELAY.
- [SDR DL72S992390](https://openairdocs.org/sdr/DL72S992390.md): Battery · discharged · Oct 28, 1999 · N543DA · Boeing 727232 · Emergency Lighting
  > AFT AIRSTAIR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, OPS CK OK.
- [SDR DL72S992266](https://openairdocs.org/sdr/DL72S992266.md): Web · cracked · Oct 12, 1999 · N543DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON D2 LETTER CK,.25 INCH CRACK LEFT VERTICAL TORQUE BOX WEB LIGHTENING HOLE STA 1323.. ALSO, RT VERTICAL TORQUE BOX WEB AT LIGHTENING HOLE AT STA 1233 CRACKED.25 INCH. REPAIRED PER MM 53-11-0.
- [SDR DL72S991635](https://openairdocs.org/sdr/DL72S991635.md): Flap · broke · Jul 20, 1999 · N543DA · Boeing 727232 · Trailing Edge Flaps
  > ON APPROACH, RIGHT O/B TRAILING EDGE FOREFLAP BROKE IN HALF. DID NOT LEAVE AIRCRAFT. DID GO-AROUND. A/C LANDED WITHOUT INCIDENT.
- [SDR DL72S990531](https://openairdocs.org/sdr/DL72S990531.md): Web · cracked · Mar 12, 1999 · N543DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > RT SIDE TORQUE BOX WEB HAS.125 INCH CRACK PROTRUDING PAST. ROUTE OUT REPAIR AT STA 1283 LOWER HOLE M/M 53-11-0 PG 832.
- [SDR DL72S990248](https://openairdocs.org/sdr/DL72S990248.md): Gearbox · leaking · Feb 5, 1999 · N543DA · Boeing 727232 · Turbine Engine Accessory Drive
  > ON APPROACH INTO CVG PASSING THROUGH APPROX 9000 AGL, NR 2 LOW OIL PRESS LIGHT ILLUMINATED. OIL QTY WAS AND NOW OBSERVED TO DECREASE, OIL TEMP NORMAL, INCREASED ABOVE 105 DEG C. ENGINE SHUT DOWN PER POM PROCEDURES. FOUND NR 2 ENG GEARBOX LEAKING AT 6 O'CLOC
- [SDR DL72S981650](https://openairdocs.org/sdr/DL72S981650.md): Bulkhead Web · cracked · Aug 8, 1998 · N543DA · Boeing 727232 · Fuselage Main, Bulkhead
  > THE FS 1183 BULKHEAD WEB WAS FOUND WITH A 1 INCH CRACK AT RBL 25 AND WL 169. THE CRACK WAS REPAIRED WITH A TITANIUM REPAIR DOUBLER ON A TEMPORARY BASIS WITH REPETITIVE INSPECTIONS. THE PERMANENT REPAIR WILL ACCOMPLISH A WEB MODIFICATION PER BAC S/B 727-53-02
- [SDR DL72S980397](https://openairdocs.org/sdr/DL72S980397.md): Skin · corroded · Feb 13, 1998 · N543DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A 24 X 17.5 AREA OF SKIN WAS TRIMMED AWAY BETWEEN FS 480 AND FS 500, AND BETWEEN STRINGERS 27L AND 27R. THE SKIN CUTOUT WAS REPAIRED WITH A DOUBLER AND TRIPLER INSTALLED PERER/A 364006-14, REV A.
- [SDR DL72S980320](https://openairdocs.org/sdr/DL72S980320.md): Floorbeam · corrosion · Feb 3, 1998 · N543DA · Boeing 727232 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM STA 1030 AT BOLT HOLES AT BL 0, LBL 9 AND RBL 10.5. CORROSION WITHIN LIMITS AT BL 0 AND RBL 10.5. CORROSION OUT OF LIMIT AT STA LB 9 PER SRM 53-10-1. INSTALLED REPAIR PER M/M 53-20-11.
- [SDR DL72S980319](https://openairdocs.org/sdr/DL72S980319.md): Floorbeam · cracked · Feb 3, 1998 · N543DA · Boeing 727232 · Fuselage Main, Floor Beam
  > .75 INCH CRACK ON FLOORBEAM STA 344 AT LBL 30 AT FLOOR PANEL FASTENER HOLE. DRILLED UP REPLACEMENT SECTION PER SRM 53-10-8.
- [SDR DL72S971858](https://openairdocs.org/sdr/DL72S971858.md): Bulb · failed · Sep 23, 1997 · N543DA · Boeing 727232 · Emergency Lighting
  > ONE WHITE EMERGENCY PATH LIGHT INOP. REPLACED BULB.
- [SDR DL72S961759](https://openairdocs.org/sdr/DL72S961759.md): Pack Fan · inoperative · Jul 23, 1996 · N543DA · Boeing 727232 · Cabin Cooling System
  > REJECTED TAKEOFF AT DFW 18L DUE TO RT PACK TRIPPING OFF AND FILLING THE CABIN WITH SMOKE. REPLACED RIGHT PACK FAN. OPS CHECK NORMAL.
- [SDR DL72S960806](https://openairdocs.org/sdr/DL72S960806.md): Skin · cracked · Apr 8, 1996 · N543DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON A2 LETTER CHECK, 1 INCH VISIBLE CRACK ON NR 7 SLAT COVE SKIN SUPPORT ANGLE. REPAIRED PER MM 57-54-0.
- [SDR DL72S960805](https://openairdocs.org/sdr/DL72S960805.md): Skin · cracked · Apr 8, 1996 · N543DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND ON A2 LETTER CHECK, L1 DOOR UPPER AND LOWER HINGE CUTOUTS CRACKED, UPPER.5 INCH LOWER.875 INCH. REPAIRED PER MM 53-30-0.
- [SDR DL72S960370](https://openairdocs.org/sdr/DL72S960370.md): Hprsov · malfunctioned · Feb 18, 1996 · N543DA · Boeing 727232 · Cabin Cooling System
  > ON DECENT AT ABOUT 9K, STRONG DUSTY ELEC SMELL IN AFT ENTRY AREA. THE WING AND ENGINE HEAT OFF. DEACTIVATED GALLEY POWER AND LAV FLUSH MOTORS AS PRECAUTION. INSPECTED AND OPERATED SYSTEMS, UNABLE TO DUPLICATE. SUBSEQUENT OCCURENCE ISOLATED PROBLEM TO HIGH
- [SDR DL72S960369](https://openairdocs.org/sdr/DL72S960369.md): Air Distr · odor · Feb 18, 1996 · N543DA · Boeing 727232 · Air Distribution System
  > DURING FINAL APPROACH, FLT ATTN NOTICED BURNING SMELL LIKE FIREWORKS, AROUND LT AFT LAV AREA. MTC POWERED A/C, TURNED ON ALL GALLEY AND LAV EQUIPMENT AND WAS UNABLE TO REPRODUCE ANY NOTICEABLE SMELL.
- [SDR DL72S960200](https://openairdocs.org/sdr/DL72S960200.md): Baffle · cracked · Dec 9, 1995 · N543DA · Boeing 727232 · Leading Edge Devices
  > DURING ROUTINE SHOP INSPECTION, A CRACK WAS FOUND IN THE ANTI-ICE BAFFLE BETWEEN THE 11TH AND 12TH RIB FROM THE I/B END. BAFFLE WAS REPAIRED AS PER MM 57-57-0 FIG 8103A FOR NR 2 L/E SLAT.
- [SDR DL72S953614](https://openairdocs.org/sdr/DL72S953614.md): Angle · cracked · Sep 5, 1995 · N543DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON A-1 LETTER CHECK,.25 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER MM 57-54-0.
- [SDR DL72S951679](https://openairdocs.org/sdr/DL72S951679.md): Nose Cowl · cracked · Mar 22, 1995 · N543DA · Boeing 727232 · Engine Cowling System
  > OUTER FRAME AND BULKHEAD DAMAGED UNDER TEMP. REPAIR AT 3 O'CLOCK POSITION. DAMAGE WAS REPAIRED PER B-727 SRM 54-10-3 FIG 3 FOR NR 3 ENGINE NOSE COWL, DURING SHOP INSPECTION.
- [SDR DL72S950946](https://openairdocs.org/sdr/DL72S950946.md): Skin · dented · Feb 25, 1995 · N543DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT, FOUND THE NR 1 MIDFLAP LEADING EDGE SKIN DENTED I/B OF F/F TRACK CUTOUT 98 INCHES FROM I/B END. CUT OUT DAMAGE AND INSTALLED DOUBLER PER MM 57-50-0 FIG 803 PG 808.
- [SDR DL72S951319](https://openairdocs.org/sdr/DL72S951319.md): Nose Cowl · damaged · Feb 22, 1995 · N543DA · Boeing 727232 · Engine Cowling System
  > DURING SHOP INSPECTION, FOUND AFT BULKHEAD TORN AND BENT AT STATION 99.25, OF NOSE COWL. REPAIRED DAMAGE PER SRM 54-10-3 FIG NR 3.
- [SDR DL72S950660](https://openairdocs.org/sdr/DL72S950660.md): Te Panel · delaminated · Feb 17, 1995 · N543DA · Boeing 727232 · Spoilers
  > DURING SHOP INSPECTION, FOUND RIGHT WING SPOILER PANEL TRAILING EDGE DELAMINATED. REPAIRED PER SRM 57-50-6.
- [SDR DL72S950644](https://openairdocs.org/sdr/DL72S950644.md): Panel · delaminated · Feb 16, 1995 · N543DA · Boeing 727232 · Spoilers
  > DURING HMV, FOUND NR 12 SPOILER PANEL DELAMINATED AT THE TRAILING EDGE, REPAIRED PER B-727 SRM 51-40-6.
- [SDR DL72S950718](https://openairdocs.org/sdr/DL72S950718.md): Support Bracket · cracked · Feb 15, 1995 · N543DA · Boeing 727232 · Leading Edge Devices
  > AT HMV, FOUND NR 5 KRGR FLAP ACT SUPPORT BRACKET CRACKED AT LWR OB LEG. FABRICATED AND INSTALLED NEW DOUBLER PER M/M 57-20-21.
- [SDR DL72S950648](https://openairdocs.org/sdr/DL72S950648.md): Bracket · cracked · Feb 15, 1995 · N543DA · Boeing 727232 · Leading Edge Slat Control System
  > AT HMV, NR 6 LEADING EDGE FLAP ACTUATOR SUPPORT BRACKETS WERE FOUND CRACKED. REPAIRED THE BRACKETS PER MAINTENANCE MANUAL 57-20-21.
- [SDR DL72S954267](https://openairdocs.org/sdr/DL72S954267.md): Flap Track · corrosion · Feb 14, 1995 · N543DA · Boeing 727232 · Wing, Landing Gear Attach Fittings
  > THE LEFT SIDE INBOARD TRACK FOR THE INBOARD FLAP WAS FOUND WITH CORROSION IN THE RADIUS BLOCK FASTENER HOLE, FORWARD OF THE AFT TRACK TO MAIN LANDING GEAR BEAM ATTACH HOLE, ON BOTH THE INBOARD AND OUTBOARD SIDES OF THE TRACK. THE HOLES WERE BOTH OVERSIZED TO
- [SDR DL72S951435](https://openairdocs.org/sdr/DL72S951435.md): Rear Spar · cracked · Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge Flaps
  > AT SHOP INSP, NR 3 MID FLAP WAS FOUND WITH BOTTOM REAR SPAR CRACKED AT 40 INCHES FROM I/B END. REPAIRED PER MM 57-52-0 PG 807.
- [SDR DL72S951434](https://openairdocs.org/sdr/DL72S951434.md): Spar · cracked · Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge Flaps
  > BOTTOM REAR SPAR CHORD CRACKED 54 INCHES FROM I/B END OF NR 3 MID FLAP. REPLACED CHORD PER MM 57-52-0. FOUND DURING SHOP INSPECTION.
- [SDR DL72S951433](https://openairdocs.org/sdr/DL72S951433.md): Angle · cracked · Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge Flaps
  > CHORD ANGLE REPAIR CRACKED AT I/B PUSH ROD CUTOUT NR 3 MID FLAP. REPLACED CHORD PER MM 57-52-0.
- [SDR DL72S951432](https://openairdocs.org/sdr/DL72S951432.md): Angle · cracked · Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge Flaps
  > AT SHOP INSPECTION, NR 3 MID FLAP WAS FOUND WITH CHORD ANGLE CRACKED AT I/B AFT FLAP TRACK CUTOUT. REPLACED CHORD PER SRM 57-52-0.
- [SDR DL72S951431](https://openairdocs.org/sdr/DL72S951431.md): Fitting · worn · Feb 14, 1995 · N543DA · Boeing 727232 · Trailing Edge Flaps
  > AT SHOP INSPECTION, NR 3 MID FLAP CARRIAGE SUPPORT FITTING INBOARD THRUST BEARING RETAINER BOLT HOLES ARE CORRODED. REAMED HOLE TO.312 TO REMOVE CORROSION HFEC, TREATED AND BUSH PER SRM 57-50-4.
- [SDR DL72S950708](https://openairdocs.org/sdr/DL72S950708.md): Skin · delaminated · Feb 14, 1995 · N543DA · Boeing 727232 · Spoilers
  > AT HMV, FOUND NR 14 SPOILER DELAMINATED. REPAIRED PER SRM 57-50-6.

Next page: https://openairdocs.org/deregistered/N543DA-2010-07-20/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 = 'N543DA' AND deregistration_id = 'N543DA-2010-07-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N543DA-2010-07-20/reports

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