# Service difficulty reports: N2820W, cancelled Jul 20, 2010

A list on [N2820W, cancelled Jul 20, 2010](https://openairdocs.org/deregistered/N2820W-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 · 57 reports

- [SDR DL72W011512](https://openairdocs.org/sdr/DL72W011512.md): Panel · missing · Sep 7, 2001 · N2820W · Boeing 727247 · Wing, Plate/Skin
  > PANEL ON TOP OF RT WING TIP NAV LIGHT IS MISSING. REPLACED SAME.
- [SDR DL72W011348](https://openairdocs.org/sdr/DL72W011348.md): Bear Strap · cracked · Aug 17, 2001 · N2820W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE UPPER HINGE CUTOUT OF THE R1 DOOR OPENING WAS FOUND WITH A 2.5 INCH CRACK IN THE BEARSTRAP. THE SKIN WAS CUTOUT TO ACCESS THE BEARSTRAP AND THE CRACK IN THE BEARSTRAP STOP DRILLED. THE AREA WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 38
- [SDR DL72W011133](https://openairdocs.org/sdr/DL72W011133.md): Battery · discharged · Jul 8, 2001 · N2820W · Boeing 727247 · Emergency Lighting
  > 1ST CLASS AISLE EMERGENCY LT INOP - REPLACED BATTERY PACK
- [SDR DL72W010225](https://openairdocs.org/sdr/DL72W010225.md): Indicator · inaccurate · Feb 8, 2001 · N2820W · Boeing 727247 · Trailing Flap Position Indicating System
  > A/C DIVERSION DUE OUTBOARD FLAPS LOCKED OUT. INSPECTED T/E FLAPS. NO DEFECTS NOTED. OPERATED FLAPS. OP CK NML. SWAPPED INDICATORS AS PRECAUTION. FLAP IND AND OPN NML.
- [SDR DL72W010187](https://openairdocs.org/sdr/DL72W010187.md): Transmitter · failed · Feb 1, 2001 · N2820W · Boeing 727247 · Trailing Edge Flap Control System
  > OUTBOARD FLAPS WOULD NOT RETRACT. AIR TURNBACK. INSPECTED FLAP, NO DAMAGE NOTED. RETRACTED FLAPS, NORMAL OPERATED FLAPS AND NO DEFECTS NOTED. FOUND RT O/B FLAP TRANSMITTER CANNON PLUG EXCESSIVELY LOOSE. CLEANED AND RESECURED PLUG. REPLACED RT O/B TRANSMI
- [SDR DL72W010024](https://openairdocs.org/sdr/DL72W010024.md): Skin · cracked · Jan 5, 2001 · N2820W · Boeing 727247 · Elevator Structure
  > A.375 INCH CRACK IN LOWER SKIN OF LT ELEVATOR I/B AND FWD OF TAB CONTROL ROD CUTOUT. REPAIRED PER SRM 55-20-3.
- [SDR DL72W010003](https://openairdocs.org/sdr/DL72W010003.md): Clamp · stretched · Jan 1, 2001 · N2820W · Boeing 727247 · Pneumatic Distribution System
  > AT 60 KTS ON T/O ROLL, LEFT STRUT PNEUMATIC DUCT PRESSURE WENT TO 6 O'CLOCK POSITION. ON CLIMBOUT, NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. NR 1 ENGINE THROTTLE BROUGHT TO IDLE. LIGHT EXTINGUISHED. FOUND WORN DUCT CLAMP ON ENG BLEED SUPPLY DUCT. REPLACED SA
- [SDR DL72W002316](https://openairdocs.org/sdr/DL72W002316.md): Battery · inoperative · Nov 28, 2000 · N2820W · Boeing 727247 · Emergency Lighting
  > LT FWD OVERWING EMERG LIGHTS INOP. CHNGD LT FWD OVERWING _EMERG LIGHT BATT PACK.
- [SDR DL72W001483](https://openairdocs.org/sdr/DL72W001483.md): Line · leaking · Aug 4, 2000 · N2820W · Boeing 727247 · Hydraulic System, Main
  > LOSS OF SYSTEM A FLUID IN FLIGHT WITH A PUMPS RUNNING WITH NO FLUID. FOUND LINE LEAKING AT LEFT MAIN GEAR DOOR ACTUATOR. REPLACED SAME. LEAK CKS GOOD. REPLACED EDP FILTERS PRECAUTIONARY. NO METAL FOUND IN FILTERS. ENGINE PUMPS CK GOOD. SERVICED HYD SYS
- [SDR DL72W001180](https://openairdocs.org/sdr/DL72W001180.md): Fuel Heater · intermittent · Jun 19, 2000 · N2820W · Boeing 727247 · Fuel Heater
  > NR 1 ENG FUEL HEAT VLV INTRANSIT LIGHT ILLUMINATED AFTER TAKEOFF. OIL TEMP IND HIGH. ACCOMPLISHED POM PROCEDURE. LIGHT REMAINED ON AND TEMP HIGH. WHEN FUEL DUMPING WAS STARTED THE LIGHT WENT OUT AND TEMP RETURNED TO NML. REPLACED NR 1 ENG FUEL HEAT VLV, O
- [SDR DL72W001098](https://openairdocs.org/sdr/DL72W001098.md): Stiffener · cracked · Jun 5, 2000 · N2820W · Boeing 727247 · Leading Edge Devices
  > TPA LTR CHK C-1 06/05/00, I/B SPAR STIFFENER CRACKED AT NR 6 SLAT I/B TRACK. REPLACED PER MM 57-20-21
- [SDR DL72W000594](https://openairdocs.org/sdr/DL72W000594.md): Accessory Unit · malfunctioned · Mar 29, 2000 · N2820W · Boeing 727247 · Landing Gear Position and Warning
  > AFTER EXPERIENCING MOD MOUNTAIN WAVE TURBULENCE AT FL330, GOT LEFT GEAR RED AND GREEN LIGHTS WITH GEAR HANDLE IN OFF OR UP POSITION. UPON GEAR DOWN SELECTION RED AND GREEN LIGHTS REMAINED ON. VISUALLY INSPECTED THE GEAR WERE DOWN. LANDED AND PINNED GEAR.
- [SDR DL72W992441](https://openairdocs.org/sdr/DL72W992441.md): Web · cracked · Nov 4, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous Structure
  > REF SHIP 569 TPA LTR CHK B-2 11/04/99,.5 INCH CRACK AT LEFT TORQUE BOX VERT WEB LOWER LIGHTNING HOLE STA 1233. REPAIRED PER MM 53-11-0.
- [SDR DL72W992440](https://openairdocs.org/sdr/DL72W992440.md): Web · cracked · Nov 4, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous Structure
  > REF SHIP 569 TPA LTR CHK B-2 11-04-99,.5 INCH CRACK AT UPPER ROW OF RIVETS LT TORQUE BOX, VERT WEB STA 1305. REPAIRED PER MM 53-11-0.
- [SDR DL72W992438](https://openairdocs.org/sdr/DL72W992438.md): Frame · cracked · Nov 4, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND AT B-2 LETTER CK, AFT ENTRY DOOR LT CUTOUT FRAME CRACKED AT UPPER STOP FITTING STIFFENER. REPAIRED PER SRM 53-10-9.
- [SDR DL72W991199](https://openairdocs.org/sdr/DL72W991199.md): Engine · failed · May 29, 1999 · N2820W · Boeing 727247 · Engine (Turbine/Turboprop)
  > NR 3 ENG POPPED AND SHUDDERED DURING APPLICATION OF T/O PWR, APPROX 1.6 EPR PRIOR TO INDICATION OF AIRSPEED. REPLACED ENGINE.
- [SDR DL72W990825](https://openairdocs.org/sdr/DL72W990825.md): Skin · cracked · Apr 13, 1999 · N2820W · Boeing 727247 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING HFEC INSPECTIONS PER SI 4-74176-12AD, REV F, CRACK INDICATIONS WERE NOTED BETWEEN BS 520 AND 681 AT S4R. ADDITIONALLY, GROUND DAMAGE WAS INDUCED TO THE AREA WHILE ACCOMPLISHING THE STANDARD REPAIR. REPAIRED PER ERA 332946-14AD, REV F.
- [SDR DL72W990824](https://openairdocs.org/sdr/DL72W990824.md): Skin · cracked · Apr 13, 1999 · N2820W · Boeing 727247 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING HFEC INSP PER SI 4-74176-12AD, REV F, A CRACK INDICATION WAS FOUND BETWEEN BS 681 AND BS 700; AT S4R. REPAIRED PER ERA 332945-14AD, REV A.
- [SDR DL72W990694](https://openairdocs.org/sdr/DL72W990694.md): Rib · cracked · Mar 30, 1999 · N2820W · Boeing 727247 · Wing, Rib/Bulkhead
  > UPPER CHORD ANGLE OF LT WING RIB AT WS 171.5 WAS FOUND WITH TWO CRACKS. THE CRACKS ARE LOCATED AT S16 AND S17. REPAIRED PER ERA 332958-14, REV A.
- [SDR DL72W990693](https://openairdocs.org/sdr/DL72W990693.md): Frame · worn · Mar 30, 1999 · N2820W · Boeing 727247 · Fuselage Main, Frame
  > BS 1148 FRAME WAS FOUND WORN ON THE I/B HORIZ FLANGE RADIUS AT S22L. THE WEAR WAS CAUSED BY CONTACT WITH A HYD LINE. REPAIRED PER ERA 332949-14, REV A.
- [SDR DL72W990691](https://openairdocs.org/sdr/DL72W990691.md): Skin · dented · Mar 30, 1999 · N2820W · Boeing 727247 · Fuselage Main, Plate/Skin
  > A GOUGE WAS FOUND IN THE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT BS 990. THE DAMAGE IS LOCATED ABOVE S24R. THE SKIN, DOUBLER AND TRIPLER WERE DAMAGE, BUT NOT THE BEAR STRAP. REPAIRED PER ERA 332963-14, REV A.
- [SDR DL72W990919](https://openairdocs.org/sdr/DL72W990919.md): Spar · cracked · Mar 19, 1999 · N2820W · Boeing 727247 · Trailing Edge Flaps
  > AFT SPAR CRACKED 22 FROM I/B END OF FLAP, THIS DAMAGED WAS REPAIRED PER MM 57-52-0 FIG 802 ON SHOP N/R 011630 LOCATED SHOP ORDER 709228.
- [SDR DL72W990918](https://openairdocs.org/sdr/DL72W990918.md): Spar · damaged · Mar 19, 1999 · N2820W · Boeing 727247 · Trailing Edge Flaps
  > TEMP SPLICE AFT SPAR AT 57 AND 46 FROM I/B END OF FLAP. THIS DAMAGE WAS REPAIRED PER MM 57-52-0 FIG 802 ON SHOP N/R 011626, LISTED ON SHOP ORDER 709228.
- [SDR DL72W990814](https://openairdocs.org/sdr/DL72W990814.md): Angle · cracked · Mar 19, 1999 · N2820W · Boeing 727247 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT SPAR ANGLE WAS FOUND CRACKED 2 PLACES 35 FROM IB END OF FLAP. A NEW SECTION OF SPAR ANGLE WAS DRILLED UP AND INSTALLED PER MM 57-52-01, FIG. 802.
- [SDR DL72W990677](https://openairdocs.org/sdr/DL72W990677.md): Doubler · corroded · Mar 19, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous Structure
  > BONDED DOUBLER - CORRODED FS 72OB AND JUST BELOW STR 4R. REPAIRED PER SRM 53-30-4, METHOD 2, (H). WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).
- [SDR DL72W990769](https://openairdocs.org/sdr/DL72W990769.md): Stringer · cracked · Mar 18, 1999 · N2820W · Boeing 727247 · Vertical Stabilizer
  > STR RT CRACKED INSIDE VERT STA AT B/H STA 133.8 LOC INSIDE VERT STAB. BEGAN FABRICATING REPAIR ANGLE. FABRICATED REPAIR ANGLES PER M/M 55-30-0 PG 803. OK TO INSTALL REPAIR. INSTALLED REPAIR PER M/M 55-30-0 PG 803.
- [SDR DL72W990684](https://openairdocs.org/sdr/DL72W990684.md): Doubler · corroded · Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous Structure
  > BONDED DOUBLER, CORRODED FS 500 STR 3R TO 3L. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).
- [SDR DL72W990683](https://openairdocs.org/sdr/DL72W990683.md): Doubler · corroded · Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous Structure
  > BONDED DOUBLER, CORRODED FS 520 TO 540 FROM STR 4R TO 3L. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2, (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).
- [SDR DL72W990682](https://openairdocs.org/sdr/DL72W990682.md): Doubler · corroded · Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous Structure
  > DOUBLER CORRODED FS 560 TO 580 STR 1-2R. REPAIRED PER SRM 53-30-4, METHOD 2, H. WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).
- [SDR DL72W990681](https://openairdocs.org/sdr/DL72W990681.md): Doubler · corroded · Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous Structure
  > BONDED DOUBLER, CORRODED FS 560 STR 4L TO 3L. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2, (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).
- [SDR DL72W990680](https://openairdocs.org/sdr/DL72W990680.md): Doubler · corroded · Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous Structure
  > BONDED DOUBLER, CORRODED FS 580 FROM STR 4L TO 4R. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).
- [SDR DL72W990679](https://openairdocs.org/sdr/DL72W990679.md): Doubler · corroded · Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous Structure
  > BONDED DOUBLERS, CORRODED FS 600 TO 620 AT STR 4R O/B SIDE OF STR AND SPLICE CORRODED ON I/B SIDE OF STR 22. REPAIRED PER SRM 53-30-4, METHOD 2, (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2, H. OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER
- [SDR DL72W990678](https://openairdocs.org/sdr/DL72W990678.md): Doubler · corroded · Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous Structure
  > BONDED DOUBLER, CORRODED FS 620 FROM STR 1R TO 4L. REPAIRED PER SRM 53-30-4, METHOD 2, (4). WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).
- [SDR DL72W990395](https://openairdocs.org/sdr/DL72W990395.md): Actuator · leaking · Feb 25, 1999 · N2820W · Boeing 727247 · Leading Edge Slat Actuator
  > LOST MAJORITY OF A SYS HYD FLUID WITH SYS A HYD PUMPS OFF. LEAK/LOSS STOPPED AT 1/2 GAL ON INDICATOR. FOUND NR 2 L/E FLAP ACTUATOR LEAKING. REPLACED ACTUATOR, LEAK CHKS NORMAL.
- [SDR DL72W990822](https://openairdocs.org/sdr/DL72W990822.md): Spar · cracked · Jan 22, 1999 · N2820W · Boeing 727247 · Trailing Edge Flaps
  > REAR SPAR CRACKED 19 AND 37 FROM I/B END. REPAIRED PER M/M 57-52-0.
- [SDR DL72W990026](https://openairdocs.org/sdr/DL72W990026.md): Bulkhead Web · cracked · Jan 5, 1999 · N2820W · Boeing 727247 · Fuselage Main, Bulkhead
  > THE FS 1183 BULKHEAD WEB WAS FOUND WITH A CRACK AT WL 169 AND RBL 25. THE CRACK WAS REPAIRED WITH A DOUBLER ON A TIME LIMITED BASIS UNTIL THE FULL BAC S/B 727-53-0215 IS ACCOMPLISHED AT NEXT HMV. THE REPAIR WAS ACCOMPLISHED PER ER/A 366415-14.
- [SDR DL72W982338](https://openairdocs.org/sdr/DL72W982338.md): Battery Pack · discharged · Nov 13, 1998 · N2820W · Boeing 727247 · Emergency Lighting
  > ON S/C, FOUND RT OVERWING EMER LIGHT INOP. FOUND BATT PACK INOP. REPLACED SAME.
- [SDR DL72W981411](https://openairdocs.org/sdr/DL72W981411.md): Actuator · leaking · Jul 5, 1998 · N2820W · Boeing 727247 · Leading Edge Slat Actuator
  > NR 2 SLAT ACTUATOR LEAKING, LOST HYDAULICS ON FINAL. REPLACED ACTUATOR.
- [SDR DL72W981353](https://openairdocs.org/sdr/DL72W981353.md): Battery Pack · discharged · Jun 27, 1998 · N2820W · Boeing 727247 · Emergency Lighting
  > OVERHEAD EMER LIGHT AT ROW 13 INOP. REPLACED BATT PACK, CK OK.
- [SDR DL72W981191](https://openairdocs.org/sdr/DL72W981191.md): Web · cracked · Jun 4, 1998 · N2820W · Boeing 727247 · Fuselage Miscellaneous Structure
  > WEB CRACKED AT FASTENER STA 1239 RT SIDE AFT AIRSTAIR AREA REPAIR PER M/M 53-11-0.
- [SDR DL72W981190](https://openairdocs.org/sdr/DL72W981190.md): Skin · separated · Jun 4, 1998 · N2820W · Boeing 727247 · Elevator, Plate/Skin
  > T/E RT ELEVATOR SEPARATING SEVERAL SMALL AREAS. REPAIR PER M/M 55-20-0.
- [SDR DL72W980387](https://openairdocs.org/sdr/DL72W980387.md): Battery Pack · discharged · Feb 14, 1998 · N2820W · Boeing 727247 · Emergency Lighting
  > ON L/O, CHECK FOUND LT FIXED OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK OF LT FIXED OVERWING EMERGENCY.
- [SDR DL72W990022](https://openairdocs.org/sdr/DL72W990022.md): Skin · cracked · Jan 5, 1998 · N2820W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FOUND ON A2 LETTER CK,.375 INCH CRACK LOWER I/B FASTENER HOLE AT THE L-4 WINDOW CUTOUT. REPAIRED PER SRM 53-30-3.
- [SDR DL72W972585](https://openairdocs.org/sdr/DL72W972585.md): Hyd Line · cracked · Dec 8, 1997 · N2820W · Boeing 727247 · Hydraulic System, Main
  > AT FLT LVL 290 HYD SYS-B QTY WENT TO ZERO. REPLACED HYD LINE AT B-FILTER MODULE.
- [SDR DL72W970599](https://openairdocs.org/sdr/DL72W970599.md): Cowl Flange · worn · Mar 28, 1997 · N2820W · Boeing 727247 · Engine Cowling System
  > FLANGE/RING WORN AT 7 O'CLOCK POS FOR NR 2 ENGINE LT FWD COWL, LOC ON NR 2 LWR FIREWALL. REMOVED DAMAGE SECTION FRM 3 TO 9 O'CLOCK. INSTALLED REPAIR PER MM 53-11-0 PG 827.
- [SDR DL72W970588](https://openairdocs.org/sdr/DL72W970588.md): Web · cracked · Mar 26, 1997 · N2820W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND RT VERTICAL WEB CRACKED, FS 1303 ABOVE S-DUCT INSIDE VERTICAL FIN SAME COND LWR LT SIDE OF WEB. REPAIRED BOTH SIDES PER SRM 53-10-04, FIG 17.
- [SDR DL72W970587](https://openairdocs.org/sdr/DL72W970587.md): Stringer · cracked · Mar 26, 1997 · N2820W · Boeing 727247 · Vertical Stabilizer
  > FOUND VERTICAL FIN LT SIDE, 3RD STR FROM REAR SPAR CRACKED 3RD BAY, ABOVE FIN ACCESS PNL 9504. REPAIRED PER M/M 55-33-00, FIG 803.
- [SDR DL72W970048](https://openairdocs.org/sdr/DL72W970048.md): Battery · discharged · Jan 10, 1997 · N2820W · Boeing 727247 · Emergency Lighting
  > FWD EMERGENCY FLASHLIGHT WON,T BLINK. REPLACED FLASHLIGHT BATTERY AND BULB, OPERATIONAL TEST NML.
- [SDR DL72W961565](https://openairdocs.org/sdr/DL72W961565.md): Generator · failed · Jul 1, 1996 · N2820W · Boeing 727247 · AC Generator-Alternator
  > NR 1 GEN ALREADY ON MCO NR 2 GEN FAILED. NR 2 ENGINE CSD/ GEN CHANGE IN PROGRESS.
- [SDR DL72W961316](https://openairdocs.org/sdr/DL72W961316.md): Rib · cracked · May 29, 1996 · N2820W · Boeing 727247 · Leading Edge Devices
  > RIB NR 21 CRACKED. REPAIRED PER MM 57-54-0.

Next page: https://openairdocs.org/deregistered/N2820W-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 = 'N2820W' AND deregistration_id = 'N2820W-2010-07-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N2820W-2010-07-20/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.