# Service difficulty reports: N522DA, cancelled Apr 2, 2013

A list on [N522DA, cancelled Apr 2, 2013](https://openairdocs.org/deregistered/N522DA-2013-04-02.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 · 63 reports

- [SDR DL72S020595](https://openairdocs.org/sdr/DL72S020595.md): Ram Air Door · stuck · May 26, 2002 · N522DA · Boeing 727232 · Air Distribution System
  > AT GATE WITH APU POWER,TURNED PACKS ON AND CABIN FILLED WITH SMOKE. FOUND RT PACK RAM AIR SCOOP CK VALVE STUCK OPEN. FREED DOOR, RAN PACKS, RAN ENGINES 1 AND 3. PACK OPERATING, NO FURTHER SMOKE OR FUMES IN CABIN. OK FOR SERVICE.
- [SDR DL72S020588](https://openairdocs.org/sdr/DL72S020588.md): Skin · cracked · May 23, 2002 · N522DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND IN THE BONDED SKIN ASSY AND UNDERLYING BEARSTRAP OF THE LOWER HINGE CUTOUT OF THE L1 DOOR CUTOUT. THE CRACK WAS ROUTED OUT OF THE SKIN AND THE BEARSTRAP. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 383225-14,
- [SDR DL72S020585](https://openairdocs.org/sdr/DL72S020585.md): Skin · corroded · May 23, 2002 · N522DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 1067 / STRG. 28R: CORROSION CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 1067 NEAR STRINGER 28R. THE CORROSION WAS REMOVED WITH A 5.75" X 2" CUTOUT
- [SDR DL72S020584](https://openairdocs.org/sdr/DL72S020584.md): Skin · cracked · May 22, 2002 · N522DA · Boeing 727232 · Vertical Stabilizer
  > FOUND ON E1 LETTER CK 1/2 CRACK VISIBLE VERTICAL STAB AT LWR END SKIN AT AFT SPAR R/H SIDE REPAIRED PER M/M 55-30-000-8 FIG 801
- [SDR DL72S020583](https://openairdocs.org/sdr/DL72S020583.md): Skin · cracked · May 22, 2002 · N522DA · Boeing 727232 · Elevator, Plate/Skin
  > FOUND ON E1 LETTER CK, LT ELEVATOR BONDED BEADED SKIN CRACKED AT STA 100 TO STA 103 FWD OF TAB. REPAIRED PER SRM 55-20-3D FIG 3.
- [SDR DL72S020582](https://openairdocs.org/sdr/DL72S020582.md): Skin · cracked · May 22, 2002 · N522DA · Boeing 727232 · Elevator Structure
  > FOUND ON E1 LETTER CK 2 INCH CRACK L/H ELEVATOR LOWER SKIN FWD OF TAB WRITEN ON CARD 79 REPAIRED PER SRM 55-20-3D FIG 5
- [SDR DL72S020581](https://openairdocs.org/sdr/DL72S020581.md): Angle · cracked · May 22, 2002 · N522DA · Boeing 727232 · Wing Structure
  > FOUND ON E1 LETTER CK LOWER COVE SKIN ATTACH ANGLE IS CRACKED BELOW #2 SLAT TAI DUCT. REPAIRED PER MM 57-54-000-8
- [SDR DL72S020580](https://openairdocs.org/sdr/DL72S020580.md): Web · cracked · May 22, 2002 · N522DA · Boeing 727232 · Wing Structure
  > FOUND ON E1 LETTER CK I/B MOUNT WEB CRACKED #1 SLAT ACTUATOR. REPAIRED PER MM 57-20-21-8.
- [SDR DL72S020338](https://openairdocs.org/sdr/DL72S020338.md): Valve · malfunctioned · Mar 19, 2002 · N522DA · Boeing 727232 · Cabin Cooling System
  > PACKS OVERHEATED ON TAXI OUT. RETURNED TO GATE. HAZE IN CABIN. FOUND RIGHT PACK FREEZING UP, REPLACED 35 DEGREE CONTROLLER AND VALVE.
- [SDR DL72S011682](https://openairdocs.org/sdr/DL72S011682.md): Angle · cracked · Oct 17, 2001 · N522DA · Boeing 727232 · Wing Structure
  > LWR COVE SKIN ANGLE IS CRACKED AT #7 SLAT I/B UPSTOP PAD. SLAT SER # BN324. REPAIRED PER M/M 57-54-000-8
- [SDR DL72S011110](https://openairdocs.org/sdr/DL72S011110.md): Charger · faulty · Jul 4, 2001 · N522DA · Boeing 727232 · Emergency Lighting
  > RIGHT AFT LOWER FUSELAGE EMERGENCY LIGHT INOP. REPLACED CHARGER, CKS OK.
- [SDR DL72S002499](https://openairdocs.org/sdr/DL72S002499.md): Switch · unserviceable · Dec 21, 2000 · N522DA · Boeing 727232 · Leading Edge Slat Control System
  > NR 5 KRUGER FLAP SHOWED AMBER AFTER RETRACTION. CORRECTION: REPLACED NO. 5 KRUGER FLAP POS. SWITCH
- [SDR DL72S002304](https://openairdocs.org/sdr/DL72S002304.md): Skin Panel · damaged · Nov 27, 2000 · N522DA · Boeing 727232 · Elevator, Spar/Rib
  > DURING ACCOMPLISHMENT OF PREVENTIVE MOD. PER E.O. 4-70183-3 THE UPPER AND LOWER SKIN PANELS WERE FOUND WORN FROM REPETITIVE DISASSIMBLY. MANY ATTACHMENT HOLES WERE OVERSIZED. REPAIR PER ER/A 397029-14AD
- [SDR DL72S002288](https://openairdocs.org/sdr/DL72S002288.md): Frame · corroded · Nov 22, 2000 · N522DA · Boeing 727232 · Fuselage Main, Frame
  > FUSELAGE / C3 DOOR CUTOUT SURROUND STRUCTURE / AFT FRAME: CORROSION REPAIR. THE AFT FRAME OF THE C3 DOOR CUTOUT (FS 1142) WAS FOUND WITH CORROSION IN THE SKIN FLANGE BETWEEN STRINGER 28R AND 29R. THE CORRODED FLANGE WAS TRIMMED AWAY. THE DAMAGE WAS REPAIR
- [SDR DL72S002284](https://openairdocs.org/sdr/DL72S002284.md): Frame · cracked · Nov 22, 2000 · N522DA · Boeing 727232 · Fuselage Main, Frame
  > FUSELAGE / C1 DOOR OPENING SURROUND STRUCTURE / AFT FRAME / FS 620: WEB CRACK AND CHORD GOUGE REPAIR NSPECTIONS OF THE AFT DOOR FRAME OF THE C1 DOOR OPENING AT FS 620 REVEALED A.5 INCH CRACK IN THE FRAME WEB JUST BELOW THE #6 DOOR STOP. THE INNER FRAME CHO
- [SDR DL72S002277](https://openairdocs.org/sdr/DL72S002277.md): Skin · worn · Nov 21, 2000 · N522DA · Boeing 727232 · Elevator, Spar/Rib
  > THE HORIZONTAL STABILIZER ELEVATOR SKINS WERE FOUND WITH WORN, WITH ELONGATED FASTENER HOLES. THE FASTENER HOLES ARE COMMON TO THE UPPER AND LOWER SKINS AND THE REAR SPAR. REPAIR PER ER/A 396929-14AD
- [SDR DL72S002282](https://openairdocs.org/sdr/DL72S002282.md): Frame · cracked · Nov 20, 2000 · N522DA · Boeing 727232 · Fuselage Main, Frame
  > FUSELAGE / C1 CARGO DOOR CUTOUT SURROUND STRUCTURE / FWD FRAME / FS 560: WEB CRACK REPAIR THE FWD FRAME OF THE C1 CARGO DOOR CUTOUT (FS 560) WAS FOUNDWITH A CRACK IN THE FRAME WEB. THE CRACK WA REMOVED WITH A.75" DIA HOLE THROUGHT THE WEB. THE FRAME WAS
- [SDR DL72S001650](https://openairdocs.org/sdr/DL72S001650.md): Oxygen Mask · broken · Aug 25, 2000 · N522DA · Boeing 727232 · Crew Oxygen System
  > MICROPHONE JACK FOR O2 MASK IS BROKEN. REPLACED JUMPSEAT O2 MASK ASSY.
- [SDR DL72S001443](https://openairdocs.org/sdr/DL72S001443.md): Casting · cracked · Jul 31, 2000 · N522DA · Boeing 727232 · Spoilers
  > ON C2 LETTER CK, NR 3 SPOILER O/B ATTACH CASTING CRACKED. REPLACED ANGLE PER MM 57-42-0.
- [SDR DL72S001256](https://openairdocs.org/sdr/DL72S001256.md): Battery Pack · discharged · Jul 3, 2000 · N522DA · Boeing 727232 · Emergency Lighting
  > FOUND EMERGENCY EXIT LIGHT ABOVE L-2 DOOR HAS DEAD BATTERY. R & R EMERGENCY EXIT LIGHT ASSY ABOVE L-2 DOOR OPS CK NORMAL.
- [SDR DL72S992817](https://openairdocs.org/sdr/DL72S992817.md): Stiffener · cracked · Dec 22, 1999 · N522DA · Boeing 727232 · Wing Miscellaneous Structure
  > NR 2 SLAT O/B TRACK I/B SPAR STIFFENER CRACKED. REPLACED STIFFENER PER M/M 57-20-21 PG 813.
- [SDR DL72S992816](https://openairdocs.org/sdr/DL72S992816.md): Stringer · cracked · Dec 22, 1999 · N522DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > STR 18A CRACKED AT STA 940 AFT SIDE OF RADIUS BLOCK AT AFT LOWER BOLT. REPAIRED PER M/M 53-12-0 PG 816, LEVEL II TIME LIMITED REPAIR.
- [SDR DL72S991813](https://openairdocs.org/sdr/DL72S991813.md): Battery Pack · discharged · Aug 13, 1999 · N522DA · Boeing 727232 · Emergency Lighting
  > LEFT FWD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS CK OK.
- [SDR DL72S991177](https://openairdocs.org/sdr/DL72S991177.md): Frame · cracked · May 25, 1999 · N522DA · Boeing 727232 · Service Doors
  > A.5 INCH CRACK IN R-1 DOOR FWD FRAME EXTENDING FROM LOWER FWD STOP FITTING. REPAIRED PER MM 52-12-0.
- [SDR DL72S990431](https://openairdocs.org/sdr/DL72S990431.md): Pump · damaged · Mar 2, 1999 · N522DA · Boeing 727232 · Hydraulic Pump (Electric/Engine), Main
  > AFTER T/O ON INIT CLMB, BOTH HYD SYS B PUMPS LOW PRESS LIGHTS ILLUM. HYD QTY IN A SYS DROPPED TO 2.5 GALS, B QTY APPEARED NORMAL. PRESS THEN DROPPED TO NEAR ZERO, TURNED PUMPS OFF IAW POM 1 TO 2 MINS AFTER ILLUMINATION. FOUND O-RING ON NR 1 B SYS HYD PUMP C
- [SDR DL72S982433](https://openairdocs.org/sdr/DL72S982433.md): Battery Pack · discharged · Nov 24, 1998 · N522DA · Boeing 727232 · Emergency Lighting
  > EMERG LIGHT OVERWING FWD POSITION LT WING INOP. REPLACED BATTERY PACK.
- [SDR DL72S982375](https://openairdocs.org/sdr/DL72S982375.md): Light · inop · Nov 16, 1998 · N522DA · Boeing 727232 · Emergency Lighting
  > EMER AREA LIGHT AT WING EXITS IN CABIN INOP. FOUND THAT LAMP AT EXTERIOR WING EXIT SHORTING CIRCUIT. REPLACED LAMP AND BATTERY PACK AND RACK FUSES, OPERATION CHECK GOOD.
- [SDR DL72S980617](https://openairdocs.org/sdr/DL72S980617.md): Frame · corroded · Mar 20, 1998 · N522DA · Boeing 727232 · Fuselage Main, Frame
  > SKIN ATTACH FLANGE AT FS 1166 FRAME WAS CORRODED BETWEEN S28 AND 29 ON THE LT SIDE. REPAIR WILL REQUIRE REACOMMPLISHMENT OF AD92-12-03. REPAIRED PER ERA 331479-14AD.
- [SDR DL72S980616](https://openairdocs.org/sdr/DL72S980616.md): Bulkhead Ftg · damaged · Mar 20, 1998 · N522DA · Boeing 727232 · Fuselage Main, Bulkhead
  > THE BORE OF FS 870 BLKHD LT TERMINAL FITTING WAS O/S TO 4.605 DIAMETER TO REMOVE TOOLING DAMAGE. REWORKED PER ERA 331517-14.
- [SDR DL72S980541](https://openairdocs.org/sdr/DL72S980541.md): Stiffener · cracked · Mar 9, 1998 · N522DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A CRACK WAS FOUND IN THE RBL 36.83 VERT STIFFENER ON THE FWD SIDE FO THE FS 1183 BLKHD. THE CRACK WAS LOCATED AT APPROX WL 238 AND WAS APPROX 2. REPAIRED PER ERA 331448-14AD.
- [SDR DL72S980592](https://openairdocs.org/sdr/DL72S980592.md): Fitting · corroded · Mar 5, 1998 · N522DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > CORROSION ON BORE OF BODY FITTING LT AFT BTL PIN. ALSO, SOME CORROSION ON EDGE OF FITTING BETWEEN WING AND BODY FITTING. REMOVED CORROSION PER 53-40-1 FIG 4. REWORKED NR 1214 BORE, REPAIRED ON NR 1214 AS PER ERA 331517-14.
- [SDR DL72S980667](https://openairdocs.org/sdr/DL72S980667.md): Angle · cracked · Mar 4, 1998 · N522DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE FLAP REAR CHORD ANGLE WAS FOUND CRACKED 32 AND 37 FROM THE IB END. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 802.
- [SDR DL72S980666](https://openairdocs.org/sdr/DL72S980666.md): Angle · cracked · Mar 4, 1998 · N522DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE FLAP WAS FOUND WITH A CRACKED REAR CHORD ANGLE. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A DOUBLER.
- [SDR DL72S980518](https://openairdocs.org/sdr/DL72S980518.md): Web · cracked · Feb 25, 1998 · N522DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSIDE ACCESS 9504 3RD BAY DOWN VERTICAL WEB IS CRACKED ON LT SIDE. FAB REPAIR DOUBLER PER SRM 53-10-4 FIG 17. STOP DRILLED CRACK AND DYE CHECK PER SRM 53-10-4. OK TO INSTALL DOUBLER. INSTALLED DOUBLER.
- [SDR DL72S980517](https://openairdocs.org/sdr/DL72S980517.md): Web · cracked · Feb 25, 1998 · N522DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DUPLICATE ORIGINAL SOILED. INSIDE ACCESS 9504 3RD BAY DOWN VERTICAL WEB IS CRACKED AT 2 LOC ON RT SIDE. REMOVED SECTION OF ANTI-ICE DUCT AND X BRACE FOR ACCESS. FAB REPAIR DOUBLER PER SRM 53-10-4 FIG 17. STOP DRILLED CRACK AND DYE CHECKED PER SRM 53-10-4.
- [SDR DL72S980557](https://openairdocs.org/sdr/DL72S980557.md): Frame · cracked · Feb 24, 1998 · N522DA · Boeing 727232 · Fuselage Main, Frame
  > ITEM: FRAME CRACKED STA 930 ABOVE 14 LT MARKED. REPAIRED PER SRM 53-10-4 FIG 25.
- [SDR DL72S980613](https://openairdocs.org/sdr/DL72S980613.md): Bulkhead Skin · cracked · Feb 23, 1998 · N522DA · Boeing 727232 · Fuselage Main, Bulkhead
  > AT HMV, FOUND APU BLEED AIR CUTOUT FWD BLKHD RT W/W SKIN CRACKED. REPAIRED PER SRM 53-10-9 FIG 5.
- [SDR DL72S980612](https://openairdocs.org/sdr/DL72S980612.md): Frame · cracked · Feb 23, 1998 · N522DA · Boeing 727232 · Fuselage Main, Frame
  > ITEM: AT HMV TEMPORARY REPAIR LMLG UPLOCK FITTING SUPPORT FRAME AFT WEB. REPAIRED PER MM 53-11-0 FIG 814.
- [SDR DL72S980750](https://openairdocs.org/sdr/DL72S980750.md): Angle · damaged · Feb 21, 1998 · N522DA · Boeing 727232 · Trailing Edge Flaps
  > AFT LOWER CHORD ANGLE IS DAMAGED 29 FROM O/B END OF NR 2 MIDFLAP. REPAIRED PER M/M 57-52-0 FIG 802, INSTALLED DOULBER.
- [SDR DL72S971267](https://openairdocs.org/sdr/DL72S971267.md): Hydraulic Line · ruptured · Jun 29, 1997 · N522DA · Boeing 727232 · Hydraulic System, Main
  > SYSTEM A HYDRAULICS TOTAL FAILURE 10 MIN INTO FLIGHT. BY POM ELECTRICALLY OPERATED FLAPS AND CRANKED NOSE GEAR DOWN. MAIN GEAR DOWN BY ALTERNATE METHOD. ALL HAPPENED AT 10,000 FT AND 250 KTS. REPLACED LOWER RUDDER POWER CONTROL UNIT PRESSURE LINE, SERVICED
- [SDR DL72S970491](https://openairdocs.org/sdr/DL72S970491.md): Rudder · deflection · Mar 16, 1997 · N522DA · Boeing 727232 · Rudder Control System
  > ON TAKEOFF ROLL 10 KNOTS BEFORE V1, RUDDER KICKED HARD LEFT TWICE IN RAPID SUCCESSION CAUSING ABRUPT NOSE DEFLECTION. TAKEOFF WAS CONTINUED DUE TO HIGH WEIGHT AND HIGH SPEED.
- [SDR DL72S962690](https://openairdocs.org/sdr/DL72S962690.md): Web · cracked · Dec 13, 1996 · N522DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING F-2 LETTER CHECK, 3 EA.5 INCH CRACKS LWR TORQUE BOX WEB STA 1219 TO 1224 LEFT SIDE. REPAIRED PER M/M 53-11-0.
- [SDR DL72S962689](https://openairdocs.org/sdr/DL72S962689.md): Angle · corroded · Dec 13, 1996 · N522DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING F-2 LETTER CHECK, CORROSION AT FUSELAGE BELLY PANEL 3348L FWD HINGE SUPPORT. REPAIRED PER M/M 53-30-01.
- [SDR DL72S961397](https://openairdocs.org/sdr/DL72S961397.md): Frame · cracked · Jun 3, 1996 · N522DA · Boeing 727232 · Fuselage Main, Frame
  > FOUND CRACKS AT THE LT AND RT FRAMES AT STA 784. REPAIRED BOTH CRACKS PER BAC S/B 727-53-0197, REV 2.
- [SDR DL72S961396](https://openairdocs.org/sdr/DL72S961396.md): Skin · corrosion · Jun 3, 1996 · N522DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND CORROSION SLIGHTLY AFT OF C-3 DOOR OPENING BEAR STRAP. REPAIRED PER ER/A 303676-14.
- [SDR DL72S961358](https://openairdocs.org/sdr/DL72S961358.md): Torque Box · cracked · May 29, 1996 · N522DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > AT MID-VISIT, THE AFT STAIRWELL RT TORQUE BOX WAS FOUND CRACKED AT THE UPPER LIGHTENING HOLE AT STA 1226. REPAIRED PER MM 53-11-0.
- [SDR DL72S961469](https://openairdocs.org/sdr/DL72S961469.md): Blkhd Stiffener · cracked · May 26, 1996 · N522DA · Boeing 727232 · Fuselage Main, Bulkhead
  > CRACKS WERE FOUND EMANATING FROM THE BOTTOM OF THE FLANGE ON THE VERTICAL STIFFENERS LOCATED AT THE BOTH LBL AND RBL 8. REPAIRED PER B727 S/B 727-53-0175, REV 2.
- [SDR DL72S961284](https://openairdocs.org/sdr/DL72S961284.md): Bulkhead · cracked · May 26, 1996 · N522DA · Boeing 727232 · Fuselage Main, Bulkhead
  > CRACKS EMANATING FROM VERTICAL STIFFENERS AT LBL AND RBL 8 ON STA 1183 BULKHEAD. REPAIRED PER EO 4-59275-3AD.
- [SDR DL72S961300](https://openairdocs.org/sdr/DL72S961300.md): Trunnion Ftg · corroded · May 23, 1996 · N522DA · Boeing 727232 · Nose/Tail Landing Gear Attach Section
  > AT MID VISIT, THE NLG TRUNNION FITTING WAS FOUND TO BE CORRODED. REPAIRED PER MM 53-40-0.
- [SDR DL72S961299](https://openairdocs.org/sdr/DL72S961299.md): Trunnion Ftg · corroded · May 23, 1996 · N522DA · Boeing 727232 · Fuselage, Landing Gear Attach Fittings
  > AT MID VISIT, BORE OF NLG FITTING WAS FOUND TO BE PITTED. AREA SPOTFACED, BORED DYE CHECKED, ROTOPEENED AND BUSHING INSTALLED PER M/M 53-40-0.

Next page: https://openairdocs.org/deregistered/N522DA-2013-04-02/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 = 'N522DA' AND deregistration_id = 'N522DA-2013-04-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N522DA-2013-04-02/reports

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