# Service difficulty reports: N533DA, cancelled Mar 30, 2005

A list on [N533DA, cancelled Mar 30, 2005](https://openairdocs.org/deregistered/N533DA-2005-03-30.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 · 55 reports

- [SDR DL72S030300](https://openairdocs.org/sdr/DL72S030300.md): Control Valve · leaking · Mar 29, 2003 · N533DA · Boeing 727232 · Landing Gear Retraction/Extension System
  > SHORTLY AFTER T/O SYS-A HYD LOW PRESS LIGHT ILLUM. FOUND LANDING GEAR CONTROL VALVE LEAKING AT FITTING. REPLACED FITTING AND O-RING.
- [SDR DL72S021457](https://openairdocs.org/sdr/DL72S021457.md): Actuator · leaking · Dec 21, 2002 · N533DA · Boeing 727232 · Hydraulic System, Main
  > ON APPROACH AFTER FLAPS 15 COMPLETE LOSS OF A SYSTEM QUANTITY AND PRESSURE. EMERGENCY PROCEDURES CHECKLIST FOLLOWED WITH MANUAL LANDING GEAR EXTENSION. A SYSTEM HYDRAULIC PUMPS WERE DEACTIVATED WITHIN 2 MINUTES CA_FOUND NBR 4 KREUG
- [SDR DL72S021378](https://openairdocs.org/sdr/DL72S021378.md): Handle · broken · Nov 25, 2002 · N533DA · Boeing 727232 · Passenger/Crew Doors
  > L2 DOOR UPPER CRANK BROKE WHILE CLOSING DOOR, ROD ALSO DAMAGED SHEET METAL ON DOOR. REPLACED DOOR.
- [SDR DL72S021144](https://openairdocs.org/sdr/DL72S021144.md): Frame · cracked · Sep 26, 2002 · N533DA · Boeing 727232 · Fuselage Main, Frame
  > THE INNER CHORD OF THE FS 1303 FRAME WAS FOUND CRACKED AT A HYDRAULIC LINE CLAMP ATTACHMENT LOCATION JUST ABOVE RT VENTRAL STAIRWAY TORQUE BOX STRUCTURE. THE CHORD WAS CUT ABOVE THE DAMAGE AND THE LOWER SECTION OF CHORD REMOVED. A NEW SECTION OF CHORD WAS IN
- [SDR DL72S020819](https://openairdocs.org/sdr/DL72S020819.md): Spar · damaged · Jul 16, 2002 · N533DA · Boeing 727232 · Trailing Edge Flaps
  > NR 2 MID FLAP REMOVED FROM AC 533 DURING HMV. AFT SPAR RAIL REPAIRED PER M/M 57-52-0 FIG 802.
- [SDR DL72S020231](https://openairdocs.org/sdr/DL72S020231.md): Skin · cracked · Feb 22, 2002 · N533DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > A.9375 INCH CRACK WAS FOUND FROM FASTENER HOLE AT THE STRINGER 7L SKIN SPLICE TO THE EDGE OF THE SKIN. THE CRACK WAS VERIFIED TO BE CONTAINED IN THE FASTENER HOLE THROUGH HFEC INSPECTION. THE CRACKED AREA WAS REPAIRED WITH AN EXTERNAL TITANIUM DOUBLER.
- [SDR DL72S020216](https://openairdocs.org/sdr/DL72S020216.md): Spar · cracked · Feb 21, 2002 · N533DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON A2 LETTER CHECK, NR 7 SLAT FWD SPAR AND RIB CRACKED AT ACTUATOR ROD END. REPAIRED PER MM 57-54-000-8.
- [SDR DL72S020136](https://openairdocs.org/sdr/DL72S020136.md): Light · inoperative · Feb 4, 2002 · N533DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY EXIT SIGN AT L1 DOOR INOP. REPLACED LIGHTS ASSY AND BATTERIES, CHECKS OK.
- [SDR DL72S011822](https://openairdocs.org/sdr/DL72S011822.md): Light · inoperative · Nov 17, 2001 · N533DA · Boeing 727232 · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY.
- [SDR DL72S011264](https://openairdocs.org/sdr/DL72S011264.md): Frame · cracked · Jul 30, 2001 · N533DA · Boeing 727232 · Fuselage Main, Structure
  > A 2" CRACK WAS FOUND AT THE FS 416 AFT FRAME OF THE R1 DOOR CUTOUT. THE CRACK WAS CUT OUT AND A REPAIR ANGLE INSTALLED.THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72S011237](https://openairdocs.org/sdr/DL72S011237.md): Frame · cracked · Jul 26, 2001 · N533DA · Boeing 727232 · Fuselage Main, Frame
  > THE UPPER FAIL-SAFE CHORD OF THE FS 720B FRAME WAS FOUND CRACKED INBOARD OF STR 26L. THE DAMAGE WAS FOUND DURING INSP AT HMV.
- [SDR DL72S011227](https://openairdocs.org/sdr/DL72S011227.md): Flap Track · corroded · Jul 25, 2001 · N533DA · Boeing 727232 · Trailing Edge Flaps
  > INBOARD FLAP, NR 4 TRACK WAS FOUND WITH CORROSION AND WEAR AT THE MLG AND SPOILER BEAM ATTACH PADS, FWD ATTACH LUGS, MLG DOOR HINGE FITTING ATTACH HOLES, TOGGLE DETENT HOLE, AND CLIP ASSY AND SPACER BAR ATTACH HOLES.
- [SDR DL72S011226](https://openairdocs.org/sdr/DL72S011226.md): Web · corroded · Jul 25, 2001 · N533DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND ON THE C2 DOOR SILL WEB AT FS 970. THE DAMAGE WAS FOUND DURING AN INSPECTION AT HMV.
- [SDR DL72S011241](https://openairdocs.org/sdr/DL72S011241.md): Stringer · cracked · Jul 23, 2001 · N533DA · Boeing 727232 · Wing, Longeron/Stringer
  > AT HMV FOUND STRINGER CRACKED UPPER STRINGER 10 AT LT WS 629-00.
- [SDR DL72S011195](https://openairdocs.org/sdr/DL72S011195.md): Frame · cracked · Jul 19, 2001 · N533DA · Boeing 727232 · Fuselage Main, Frame
  > THE RT FS 784 FRAME HAS A SMALL CRACK EMANATING FROM THE FIRST HOLE ABOVE THE FLOOR LINE IN THE INNER CHORD.
- [SDR DL72S011145](https://openairdocs.org/sdr/DL72S011145.md): Skin · cracked · Jul 11, 2001 · N533DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING HMV CRACKS WERE FOUND IN THE STRINGER 4L LAP JOINT BETWEEN FS 970 AND FS 990. THE CRACKS WERE REPAIRED PER B727 SRM 53-30-3, FIG 5.
- [SDR DL72S011135](https://openairdocs.org/sdr/DL72S011135.md): Frame · cracked · Jul 9, 2001 · N533DA · Boeing 727232 · Fuselage Main, Frame
  > A CRACK WAS FOUND IN THE LOWER HOLE OF THE FS 783.95 FRAME TYPICAL TO THAT NOTED IN SB 727-53-0197. THE CRACK WAS CUT OUT AND REPAIRED WITH A 65C36280-24 KIT PER THE S/B. THE DAMAGE WAS FOUND DURING THE AD MANDATED INSPECTION.
- [SDR DL72S011134](https://openairdocs.org/sdr/DL72S011134.md): Flap Track · corroded · Jul 9, 2001 · N533DA · Boeing 727232 · Trailing Edge Flaps
  > INBOARD FLAP, NR 4 INBOARD TRACK FOUND WITH CORROSION AND WEAR AT MLG AND SPOILER BEAM ATTACH PADS, AND FWD LUG AND MLG DOOR HINGE FITTING HOLES. REPAIR PER ER/A 402041-14AD.
- [SDR DL72S011123](https://openairdocs.org/sdr/DL72S011123.md): Doubler · cracked · Jul 6, 2001 · N533DA · Boeing 727232 · Trailing Edge Flaps
  > AFT CHORD ANGLE, LOWER SPAR RAIL, REPAIR DOUBLER CRACKED 37 INCHES FROM I/B END. REPAIRED ON SHOP ORDER A64256, N/R CARD 018778.
- [SDR DL72S011117](https://openairdocs.org/sdr/DL72S011117.md): Skin · cracked · Jul 6, 2001 · N533DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING LFEC INSPECTIONS PER AD 99-04-22, A CRACK WAS FOUND IN THE STR 4L LAP JOINT AT BETWEEN FS 440 AND 460. THE CRACK WAS CUT OUT AND REPAIRED PER B727 SRM 53-30-3, FIGURE 5. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL72S011219](https://openairdocs.org/sdr/DL72S011219.md): Rib · cracked · Jul 4, 2001 · N533DA · Boeing 727232 · Leading Edge Devices
  > AT HMV FOUND RIB CRACKED #3 O/B RIB OF O/B SLAT TRACK(#6 SLAT) CORR: TRIMED OUT DAMAGE FABD REPAIR DOUBLER PER MM 57-54-000-8,REMOVED SLAT TRACK,OK INSTL REPAIR,INSTLD #3 OB RIBDOUBLER PER MM 57-54,INSTL
- [SDR DL72S010392](https://openairdocs.org/sdr/DL72S010392.md): Battery Pack · discharged · Mar 10, 2001 · N533DA · Boeing 727232 · Emergency Lighting
  > ON L/O FOUND FWD ESCAPE PATH FLOOR LIGHTS ROWS 20 TO 26 INOPERATIVE. SECURED CONNECTON AT SEAT 20D AND REPLACED BATTERY M9027 PACK- OPS NML NOW.
- [SDR DL72S011218](https://openairdocs.org/sdr/DL72S011218.md): Angle · cracked · Feb 4, 2001 · N533DA · Boeing 727232 · Leading Edge Devices
  > AT HMV FOUND ANGLE CRACKED UNDER I/B UP STOP NR 6 SLAT.
- [SDR DL72S002489](https://openairdocs.org/sdr/DL72S002489.md): Beam · cracked · Dec 21, 2000 · N533DA · Boeing 727232 · Fuselage Main, Structure
  > FUSELAGE / VENTRAL STAIRWAY OPENING / RT TORQUE BOX / FS 1263: CRACKED BEAM AND GUSSET INSPECTIONS OF THE RT VENTRAL STAIRWAY TORQUE BOX STRUCTURE REVEALED A.5" CRACK IN THE UPPER HORIZONTAL BEAM AND A 1.5 INCH CRACK IN THE GUSSET CHANNEL AT FS 1263. THE
- [SDR DL72S002485](https://openairdocs.org/sdr/DL72S002485.md): Skin · cracked · Dec 20, 2000 · N533DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > FOUND ON F2 LETTER CK 1 INCH AND 3/8 IN CRACK IN VERTICAL STAB SKIN BELOW L/H SIDE OF ACCESS PANEL 9501. REPAIRED PER SRM 55-30-3.
- [SDR DL72S001641](https://openairdocs.org/sdr/DL72S001641.md): Windshield · cracked · Aug 24, 2000 · N533DA · Boeing 727232 · Flight Compartment Windows
  > INBOUND ITEM RT WINDSHIELD DAMAGED. CREW REPORTED ENCOUNTERING HAIL. RADOME DAMAGED AS WELL. REPLACED AFFECTED PARTS.
- [SDR DL72S992261](https://openairdocs.org/sdr/DL72S992261.md): Angle · cracked · Oct 11, 1999 · N533DA · Boeing 727232 · Spoilers
  > NR 14 SPOILER ACT O/B MOUNT CASTING CRACKED {ATTACH ANGLE}. REPLACED ANGLE PER M/M 57-42-0..
- [SDR DL72S991222](https://openairdocs.org/sdr/DL72S991222.md): Skin · cracked · May 29, 1999 · N533DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 AND 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 12 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP WAS CUT OUT AND REPAIRED WI
- [SDR DL72S990899](https://openairdocs.org/sdr/DL72S990899.md): Skin · corroded · Apr 24, 1999 · N533DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 1010-1080 STRG 26L-26R, CORROSION REPAIR. THE FUSEALAGE SKIN WAS FOUND CORRODED BETWEEN FS 1046 AND 1055 BELOW STRINGER 27. THERE WERE SEVERAL OTHER SKIN PANEL. REPAIR DOUBLERS IN THE AREA. TO ELIMINATE THE DAMAGE AND EXISTING REPAIRS, THE
- [SDR DL72S990898](https://openairdocs.org/sdr/DL72S990898.md): Frame · corroded · Apr 24, 1999 · N533DA · Boeing 727232 · Fuselage Main, Frame
  > FUSELAGE C3 DOOR CUTOUT AFT FRAME FS 1142 STRINGER 28R:CORROSION REPAIR. THE SKIN ATTACH FLANGE OF THE AFT FRAME OF THE C3 DOOR CUTOUT WAS FOUND CORRODED AT STRINGER 28R. THE CORRODED FLANGE WAS TRIMMED AWAY AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE PE
- [SDR DL72S990897](https://openairdocs.org/sdr/DL72S990897.md): Skin · corroded · Apr 24, 1999 · N533DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 560-580, STRG 28L, SKIN CORROSION REPAIR. AN AREA OF CORROSION WAS FOUND IN THE FUSELAGE SKIN NEAR STRINGER 28L BETWEEN FS 559 AND 564. THE CORROSION WAS CUTOUT WITH A 7 BY 1.85 CUTOUT. THERE WAS AN EXISTING REPAIR DOUBLER ADJACENT TO T
- [SDR DL72S990910](https://openairdocs.org/sdr/DL72S990910.md): Skin · corroded · Apr 23, 1999 · N533DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 950F-970, STRINGER 28L, CORROSION CUTOUT REPAIR. THE FUSELAGE SKIN WAS FOUND CORRODED AT STRINGER 28L BETWEEN FS 950F AND FS 970. THE CORROSION WAS REMOVED WITH A 26 BY 3 CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITHAN EXTERNAL ALUMINUM
- [SDR DL72S990671](https://openairdocs.org/sdr/DL72S990671.md): Wire · failed · Mar 27, 1999 · N533DA · Boeing 727232 · Electrical Power System Wiring
  > LT GENERATOR ON LANDING, LOUD SOUND OF GENERATOR FAILING. ELECTRICAL SMELL IN COCKPIT. DIFF FAULT LIGHT ON ANN PANEL. MTC FOUND BURNT WIRES GOING TO DISTRIBUTION 1 SECT X C/B C829. REPAIRED WIRING PER M/M.
- [SDR DL72S990628](https://openairdocs.org/sdr/DL72S990628.md): Rib · cracked · Mar 23, 1999 · N533DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON E1 LETTER CK, NR 5 SLAT ACT I/B ATTACH RIB CRACKED. REPAIRED PER MM 57-54-0.
- [SDR DL72S980160](https://openairdocs.org/sdr/DL72S980160.md): Web · cracked · Jan 19, 1998 · N533DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON D1 LETTER CK,.5 INCH CRACK AT LT TORQUE BOX VERICAL WEB LIGHTENING HOLE STA 1263. REPAIRED PER MM 53-11-0.
- [SDR DL72S980159](https://openairdocs.org/sdr/DL72S980159.md): Web · cracked · Jan 19, 1998 · N533DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON D1 LETTER CK,.25 INCH CRACK RT TORQUE BOX VERTICAL WEB LIGHTENING HOLE STA 1303. ROUTED OUT DAMAGED AREA PER MM 53-11-0.
- [SDR DL72S972352](https://openairdocs.org/sdr/DL72S972352.md): Skin · deformed · Nov 12, 1997 · N533DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE SKIN WAS FOUND WITH AN OIL CANNED SKIN CONDITION OVER FIVE STRINGER BAYS BETWEEN STA 660 TO 680 AND STRINGERS 20R TO 25R. A NEW SECTION OF SKIN WAS SPLICED IN PER ER/A 363183-14.
- [SDR DL72S972367](https://openairdocs.org/sdr/DL72S972367.md): Light · inoperative · Nov 9, 1997 · N533DA · Boeing 727232 · Emergency Lighting
  > OVHD EMERGENCY LIGHT INOP AT SEAT 14. REPLACED LIGHT ASSY EMERGENCY LIGHT, OPERATES NORMALLY PER MM.
- [SDR DL72S971697](https://openairdocs.org/sdr/DL72S971697.md): O-Ring · failed · Aug 29, 1997 · N533DA · Boeing 727232 · Turbine Engine Accessory Drive
  > IN CRUISE, NR 2 ENG OIL QTY DECREASED TO ZERO, OIL PRESS FLUCT AT 40 PSI, ALL OTHER IND NORM. OIL PRESS LIGHT ILLUMINATED AT IDLE, SHUT ENG DOWN. REPLACED O-RING ON FUEL PUMP DRIVE SHAFT.
- [SDR DL72S971470](https://openairdocs.org/sdr/DL72S971470.md): Battery · discharged · Jul 27, 1997 · N533DA · Boeing 727232 · Emergency Lighting
  > EMERG LIGHT O/H ROW 13 DID NOT TEST. REPLACED BATTERY, CKS OK.
- [SDR DL72S962655](https://openairdocs.org/sdr/DL72S962655.md): Tire · failed · Dec 5, 1996 · N533DA · Boeing 727232 · Tire
  > NR 4 BLEW ON T/O. REPLACED NR 3, 4 MAIN WHEEL ASSY. A/C FERRIED TO DFW ACCT OF DAMAGE TO RT INBD MID FLAP AND RT MAIN GEAR WING DOOR.
- [SDR DL72S961184](https://openairdocs.org/sdr/DL72S961184.md): Light · inoperative · May 16, 1996 · N533DA · Boeing 727232 · Emergency Lighting
  > L2 DOOR EXTERIOR EMERGENCY SLIDE ILLUMINATION LIGHT INOP. CLEANED LIGHT SOCKET CENTER CONTACT, REBULBED AND OPN NOW NORMAL.
- [SDR DL72S960851](https://openairdocs.org/sdr/DL72S960851.md): Web · cracked · Apr 12, 1996 · N533DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > LOWER LT TORQUE BOX VERTICAL WEB CRACKED BEYOND ROUTED OUT REPAIR, UPPER LIGHTENING HOLE STA 1228. REPAIRED PER M/M 53-11-0 PG 828.
- [SDR DL72S960850](https://openairdocs.org/sdr/DL72S960850.md): Web · cracked · Apr 12, 1996 · N533DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A.375 INCH CRACK IN LT LOWER TORQUE BOX VERTICAL WEB UPPER FWD END STA 1213. REPAIRED PER M/M 53-11-0.
- [SDR DL72S960849](https://openairdocs.org/sdr/DL72S960849.md): Stringer · cracked · Apr 12, 1996 · N533DA · Boeing 727232 · Vertical Stabilizer
  > A.75 INCH CRACK IN VERT STAB STR 7 AT 3RD BULKHEAD ABOVE OPENING TO CRAWLWAY. REPAIRED PER M/M 55-30-0.
- [SDR DL72S960848](https://openairdocs.org/sdr/DL72S960848.md): Skin · cracked · Apr 12, 1996 · N533DA · Boeing 727232 · Nacelle/Pylon Structure
  > A 1 INCH CRACK IN NR 2 ENG INLET OUTER SKIN LT SIDE 8 O'CLOCK POSITION APPROX 36 INCHES AFT OF L/E. INSTALLED DOUBLER PER SRM 55-30-0.
- [SDR DL72S954482](https://openairdocs.org/sdr/DL72S954482.md): Ballast · failed · Nov 23, 1995 · N533DA · Boeing 727232 · Passenger Compartment Lighting
  > LOG ITEM 2, ELECTRICAL SMELL IN MID CABIN POPPED LT AFT CABIN CEILNG LIGHT C/B. FOUND BALLAST AT STA 910 INTERNALLY SHORTED CAUSING BURNT ELECTRICAL SMELL IN CABIN. REPLACED BALLAST, OPERATION NORMAL.
- [SDR DL72S954355](https://openairdocs.org/sdr/DL72S954355.md): Duct · cracked · Nov 12, 1995 · N533DA · Boeing 727232 · Humidity Control System
  > UNABLE TO MAINTAIN PRESSURIZATION DURING CRUISE. FOUND LEFT WATER SEPARATOR FWD CLAMP SEPARATED AND WATER SEPARATOR TO MIZ VALVE DUCT CRACKED IN SEVERAL PLACES. REPLACED DUCT AND SEPARATOR, OPERATION NORMAL.
- [SDR DL72S953913](https://openairdocs.org/sdr/DL72S953913.md): Skin · worn · Sep 10, 1995 · N533DA · Boeing 727232 · Ailerons
  > DURING SHOP INSPECTION, L/W AILERON WAS FOUND WITH AREAS OF WEAR DAMAGE TO SKIN. ACCOMPLISHED REPAIRS PER SRM 51-50-5 AND SRM 51-40-3.
- [SDR DL72S952660](https://openairdocs.org/sdr/DL72S952660.md): Skin · damaged · Jun 2, 1995 · N533DA · Boeing 727232 · Trailing Edge Flaps
  > NR 2 AFT FLAP REPLACED TEMP. REPAIR 50 FROM INBD END LOWER SKIN PER SRM 57-50-4, FIG. 10 AND ERA 27109-14. FOUND DURING SHOP INSPECTION.

Next page: https://openairdocs.org/deregistered/N533DA-2005-03-30/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 = 'N533DA' AND deregistration_id = 'N533DA-2005-03-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N533DA-2005-03-30/reports

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