# Service difficulty reports: N2816W, cancelled Jun 11, 2013

A list on [N2816W, cancelled Jun 11, 2013](https://openairdocs.org/deregistered/N2816W-2013-06-11.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 DL72W010827](https://openairdocs.org/sdr/DL72W010827.md): Actuator · failed · May 23, 2001 · N2816W · Boeing 727247 · Landing Gear Actuator
  > NOSE GEAR FAILED TO EXTEND, ASSOCIATED HYDRAULIC SYSTEM QTY WENT TO ZERO. FOUND NLG LOCK ACTUATOR BLOWN APART. REPLACED SAME.
- [SDR DL72W010810](https://openairdocs.org/sdr/DL72W010810.md): Door · obstructed · May 19, 2001 · N2816W · Boeing 727247 · Door Warning System
  > AFT CARGO DOOR LIGHT ILLUM DURING CLIMBOUT. THERE WAS NO REPORTED PRESSURIZATION PROBLEMS. MTC CLEANED DEBRIS FROM THE DOOR JAMB. NO FURTHER PROBLEMS.
- [SDR DL72W010643](https://openairdocs.org/sdr/DL72W010643.md): Window · worn · Apr 18, 2001 · N2816W · Boeing 727247 · Flight Compartment Windows
  > R-2 WINDOW CAME OPEN ON T/O ROLL. CREW CLOSED WNDOW AND RETURNED TO ABQ. REMOVED AND REPLACED THE R-2 WINDOW
- [SDR DL72W010509](https://openairdocs.org/sdr/DL72W010509.md): Gasper Fan · failed · Mar 28, 2001 · N2816W · Boeing 727247 · Air Distribution Fan
  > PAX REPORTED ELECT SMELL IN CABIN, STRONGEST NEAR ROW 14 OCCURED JUST PRIOR TO LANDING AND DURING TAXI TO GATE.A PAX IN THE VICINITY OF ROW 14 ALSO MENTIONED THE SOUND OF HYD PUMPS GETTING LOUDER JUST PRIOR TO LANDING. FOUND GASPER FAN BAD. REPLACED SAME.
- [SDR DL72W010399](https://openairdocs.org/sdr/DL72W010399.md): Module · failed · Mar 11, 2001 · N2816W · Boeing 727247 · Hydraulic System, Main
  > LOSS OF SYSTEM A FLUID AND PRESSURE SHORTLY AFTER LDG GEAR WAS SELECTED DN. ALL 3 GREEN DN LOCK LGTS ILLUM AND RED DR LGT REMAINED ILLUM. THE L/R GEAR DR AND TAIL SKID AMBER ANNUNCIATORS ON S/O PNL REMAINED ILLUM. FOLLOWED HYD LOSS PRO CEDURES PER POM. UN
- [SDR DL72W010273](https://openairdocs.org/sdr/DL72W010273.md): Frame · cracked · Feb 13, 2001 · N2816W · Boeing 727247 · Fuselage Main, Frame
  > THE INNER CHORD OF THE FS 1303 RT FRAME WAS FOUND WITH A CRACKED FLANGE AT A HYDRAULIC BRACKET ATTACH POINT JUST ABOVE THE AFT VENTRAL STAIRWAY TORQUE BOX. THE CRACKED PORTION OF FLANGE WAS TRIMMED OUT AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE PER E
- [SDR DL72W010271](https://openairdocs.org/sdr/DL72W010271.md): Skin · cracked · Feb 13, 2001 · N2816W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE UPPER AFT CORNER OF THE R5 COCKPIT WINDOW WAS FOUND WITHA.25 INCH LONG CRACK IN THE SKIN. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 380034-14, REV A.
- [SDR DL72W010250](https://openairdocs.org/sdr/DL72W010250.md): Stiffener · cracked · Feb 12, 2001 · N2816W · Boeing 727247 · Leading Edge Devices
  > WING L/E SPAR STIFFENER CRACKED O/B SIDE NR 3 SLAT O/B TRACK. REPAIR PER M/M 57-20-21-8.
- [SDR DL72W010249](https://openairdocs.org/sdr/DL72W010249.md): Stiffener · cracked · Feb 12, 2001 · N2816W · Boeing 727247 · Leading Edge Devices
  > WING L/E SPAR STIFFENER CRACKED I/B SIDE NR 3 SLAT O/B TRACK. REPAIR PER M/M 57-20-021-8.
- [SDR DL72W010248](https://openairdocs.org/sdr/DL72W010248.md): Skin · cracked · Feb 12, 2001 · N2816W · Boeing 727247 · Trailing Edge Flaps
  > A 1 INCH CRACK NR 2 L/E FLAP OUTER SKIN AT LOWER LIP INBD HINGE CUTOUT. REPAIR PER M/M 57-53-000-8.
- [SDR DL72W010231](https://openairdocs.org/sdr/DL72W010231.md): Frame · damaged · Feb 8, 2001 · N2816W · Boeing 727247 · Fuselage Main, Frame
  > THE FS 720D FUSELAGE FRAME WEB WAS DAMAGED BY TOOLING JUST BELOW STRINGER 25R AND THE EXISTING FRAME SPLICE. THE DAMAGE WAS REMOVED WITH A 2 INCH CUTOUT IN THE WEB. THE DAMAGE WAS REPAIRED BY REMOVING THE EXISTING FRAME SPLICE AND FABRIACTING A LAR
- [SDR DL72W002093](https://openairdocs.org/sdr/DL72W002093.md): Engine · leaking · Oct 23, 2000 · N2816W · Boeing 727247 · Turbine Engine Oil System
  > OIL QUANTITY ON NB 3 ENGINE DECREASING AT A RATE OF APPROX 1 QUART EVERY 15 MINUTES. ADDED 18 PINTS OF OIL TO NR 3 ENGINE. FOUND OIL LINE LEAKING. REPLACED BOTH O-RINGS, ITEM 75 AND 40 IPC 79-20-00-20 NR 4, 5 AND 6 BREATHER LINE.
- [SDR DL72W001390](https://openairdocs.org/sdr/DL72W001390.md): Battery · inoperative · Jul 23, 2000 · N2816W · Boeing 727247 · Emergency Lighting
  > AFT RIGHT SERVICE DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, NOW CKS NORMAL.
- [SDR DL72W001341](https://openairdocs.org/sdr/DL72W001341.md): Valve · malfunctioned · Jul 16, 2000 · N2816W · Boeing 727247 · Air Intake Anti/De-Ice System
  > NR 1 ENGINE COWL ANTI-ICE VALVE WON''T INDICATE OPEN IN FLT. GOOD EPR DROP WHEN SWITCHED OPEN. REPLACED NR 1 ENGINE COWL ANTI-ICE VALVE. NO HELP. FOUND BAD GROUND TO PIN B OF VALVE CANNON PLUG. INSTALLED NEW TERMINAL TO GROUND. OPERATION CHECKS GOOD WITH
- [SDR DL72W992659](https://openairdocs.org/sdr/DL72W992659.md): Skin · delaminated · Dec 6, 1999 · N2816W · Boeing 727247 · Spoilers
  > LTR CHK C-1 12/6/99, NR 3 SPOILER DELAMINATED UPPER O/B SIDE. REPAIRED PER SRM 57-50-6.
- [SDR DL72W991030](https://openairdocs.org/sdr/DL72W991030.md): Angle · cracked · May 10, 1999 · N2816W · Boeing 727247 · Leading Edge Devices
  > COVE SKIN ATTACH ANGLE CRACKED BELOW I/B STOP PAD NR 8 SLAT. REPAIRED PER MM 57-54-0 FIG 812.
- [SDR DL72W991029](https://openairdocs.org/sdr/DL72W991029.md): Angle · cracked · May 10, 1999 · N2816W · Boeing 727247 · Spoilers
  > A 1.5 INCH CRACK IN SUPPORT ANGLE FWD OF NR 8 SPOILER. REPAIRED PER MM 57-20-22 FIG 806.
- [SDR DL72W990859](https://openairdocs.org/sdr/DL72W990859.md): Skin · cracked · Apr 19, 1999 · N2816W · Boeing 727247 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PA
- [SDR DL72W990858](https://openairdocs.org/sdr/DL72W990858.md): Skin · cracked · Apr 19, 1999 · N2816W · Boeing 727247 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS IN CONSECUTIVE FRAME BAYS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE PA
- [SDR DL72W990857](https://openairdocs.org/sdr/DL72W990857.md): Skin · cracked · Apr 19, 1999 · N2816W · Boeing 727247 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 24 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP SPLICE WAS CUTOUT AND
- [SDR DL72W990156](https://openairdocs.org/sdr/DL72W990156.md): Sign · missing · Jan 22, 1999 · N2816W · Boeing 727247 · Emergency Lighting
  > RT FWD OVERWING EXIT SIGN MISSING. REPLACED RT FWD OVERWING EXIT SIGN, OP CKS OK.
- [SDR DL72W982373](https://openairdocs.org/sdr/DL72W982373.md): Battery Pack · discharged · Nov 16, 1998 · N2816W · Boeing 727247 · Emergency Lighting
  > RT WING FWD EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY PACK.
- [SDR DL72W982165](https://openairdocs.org/sdr/DL72W982165.md): Web · corroded · Oct 19, 1998 · N2816W · Boeing 727247 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND ON THE UPPER HORIZ PRESSURE WEB DOUBLER OF THE NLG W/W FWD OF BS 315. THE DAMAGE NECESSITATED A NEW SECTION BE SPLICED IN. REPAIRED PER ERA 332271-14.
- [SDR DL72W982138](https://openairdocs.org/sdr/DL72W982138.md): Frame · cracked · Oct 14, 1998 · N2816W · Boeing 727247 · Fuselage Miscellaneous Structure
  > CRACK WAS FOUND IN THE AFT ENTRY DOORWAY LT FRAME AT WL 276.6. THE CRACK WAS 4.5 INCH LENGTH AND TYPICAL OF THAT FOUND IN SB 727-53-0055 REV 9. REPAIRED PER ERA 332362-14AD.
- [SDR DL72W982119](https://openairdocs.org/sdr/DL72W982119.md): Skin · cracked · Oct 12, 1998 · N2816W · Boeing 727247 · Fuselage Main, Plate/Skin
  > A FAILED FASTENER WAS FOUND IN THE UPPER ROW OF THE S26R SKIN LAP JOINT AT BS 684. CRACKS WERE FOUND EMANATING FROM THIS FASTENER HOLE IN THE OUTER SKIN ONLY. THE CRACKS WERE.125 AND.0937 LONG. REPAIRED PER ERA 332342-14.
- [SDR DL72W982118](https://openairdocs.org/sdr/DL72W982118.md): Stringer · corroded · Oct 12, 1998 · N2816W · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > CORROSION WAS FOUND ON THE I/B FLANGE OF S3R AT FS 371 REQUIRING A SECTION OF STRINGER TO BE CUT OUT. REPAIRED PER ERA 332244-14.
- [SDR DL72W982105](https://openairdocs.org/sdr/DL72W982105.md): Angle · cracked · Oct 6, 1998 · N2816W · Boeing 727247 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 33 FROM THE IB END OF FLAP. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0,FIG. 802 BY INSTALLING A DOUBLER AND STOP DRILLING THE CRACK.
- [SDR DL72W982064](https://openairdocs.org/sdr/DL72W982064.md): Stringer · corroded · Oct 6, 1998 · N2816W · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > CORROSION DAMAGE FOUND THAT EXCEEDED ALLOWABLE LIMITS, ON THE S1L, AT BS 375. REPAIRED PER ERA 332246-14.
- [SDR DL72W981971](https://openairdocs.org/sdr/DL72W981971.md): Spar · cracked · Sep 24, 1998 · N2816W · Boeing 727247 · Leading Edge Devices
  > SPAR CRACKED AT ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0.
- [SDR DL72W982217](https://openairdocs.org/sdr/DL72W982217.md): S-Duct · cracked · Sep 14, 1998 · N2816W · Boeing 727247 · Nacelle/Pylon Structure
  > AT HMV FOUND SKIN - BENT/CRACKED INSIDE S-DUCT APPROX 4FT FROM L/E OF INLET AT 12 O-CLOCK POSITION. CORR: MANUFACTURED REPAIR DBLR AND FILLER PER SRM 54-10-3 P.63 INSTLD PER SAME.
- [SDR DL72W982216](https://openairdocs.org/sdr/DL72W982216.md): Stringer · cracked · Sep 11, 1998 · N2816W · Boeing 727247 · Wing, Longeron/Stringer
  > AT HMV, FOUND RT WING OUTER W/UPR STRINGER 2 RIB AT WS 656.5 STRINGER 13 IS CRACKED AT FASTENER HOLE. REPAIR INFO IS REF ON OPN 8602AD ITEM 5. CUT OUT VENT STRINGER, DRILLED UP REPAIR ANGLES RADIUS FILLER COVER ASSY PER M/M 57-13-00. INSTALLED PER SAME.
- [SDR DL72W982213](https://openairdocs.org/sdr/DL72W982213.md): Stringer · cracked · Sep 11, 1998 · N2816W · Boeing 727247 · Wing, Longeron/Stringer
  > ON HMV, RT WING OUTER UPPER STRINGER 2 RIB AT WS 656.5 STR 12 IS CRACKD AT FASTENER HOLE. CUT OUT VENT STRINGER, DRILLED UP REPAIR ANGLES RADUIS FILLERS CVR ASSY PER MM 57-13-00. INSTALLED REPAIR ANGLES.
- [SDR DL72W982210](https://openairdocs.org/sdr/DL72W982210.md): Guide · worn · Sep 10, 1998 · N2816W · Boeing 727247 · Leading Edge Devices
  > AT HMV, FOUND GUIDE ON NR 5 SLAT TRAILING EDGE O/B OF ACTUATOR WORN. WEAR LIMITS OK, REPAIRED PER M/M 27-81-11.
- [SDR DL72W982209](https://openairdocs.org/sdr/DL72W982209.md): Angle · cracked · Sep 10, 1998 · N2816W · Boeing 727247 · Leading Edge Devices
  > AT HMV, FOUND NR 5 SLAT ANGLES - ACTUATOR ATTACH POINT BOTH I/B AND O/B ANGLES CRACKED. STOP DRILLED CRACK PER M/M, FABD REPAIR DOUBLERS, INSTALLED PER MM 57-54-00 FIG 809.
- [SDR DL72W982197](https://openairdocs.org/sdr/DL72W982197.md): Angle · cracked · Sep 10, 1998 · N2816W · Boeing 727247 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED 32 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0 FIG 802, BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER.
- [SDR DL72W981982](https://openairdocs.org/sdr/DL72W981982.md): Rib · cracked · Sep 9, 1998 · N2816W · Boeing 727247 · Trailing Edge Flaps
  > I/B AFT RIB IS CRACKED AT AFT LWR CORNER. REPAIRED PER MM 57-52-0 FIG 808.
- [SDR DL72W981509](https://openairdocs.org/sdr/DL72W981509.md): Skin · cracked · Jul 20, 1998 · N2816W · Boeing 727247 · Aerodynamic Fairings
  > .25 INCH CRACK DORSAL FIN SKIN LEFT SIDE BELOW PANEL 9523. REPAIRED PER M/M 54-30-0 PG 804.
- [SDR DL72W981485](https://openairdocs.org/sdr/DL72W981485.md): Battery Pack · discharged · Jul 16, 1998 · N2816W · Boeing 727247 · Emergency Lighting
  > WORKING L/O, NR 2 FOUND AIRSTAIR UPPER EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER M/M OP CK GOOD.
- [SDR DL72W972589](https://openairdocs.org/sdr/DL72W972589.md): Light Assy · inoperative · Dec 9, 1997 · N2816W · Boeing 727247 · Emergency Lighting
  > RIGHT EMERGENCY OVERWING EXIT LIGHT INOP ON EMERGENCY PWR. OP NORMAL ON AC PWR. REPLACED LIGHT ASSY AT OVERWING EXIT.
- [SDR DL72W972560](https://openairdocs.org/sdr/DL72W972560.md): Bracket · cracked · Dec 6, 1997 · N2816W · Boeing 727247 · Leading Edge Slat Actuator
  > NR 1 SLAT ACTUATOR I/B ATTACH BRACKET CRACKED. OPENED PANELS FOR ACCESS, REMOVED RIB WEB, STOP DRILLED CRACK, DRILLED UP DOUBLER. INSTALLED DOUBLER AND CLOSED UP.
- [SDR DL72W972559](https://openairdocs.org/sdr/DL72W972559.md): Skin · cracked · Dec 6, 1997 · N2816W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FOUND ON A1 LETTER CK,.1562 AND.125 INCH CRACKS IN FUSELAGE SKIN COMING OUT OF RIVET HOLE JUST AFT OF L3 WINDOW LOWER END. REPAIRED PER SRM 53-30-3.
- [SDR DL72W972558](https://openairdocs.org/sdr/DL72W972558.md): Stiffener · cracked · Dec 6, 1997 · N2816W · Boeing 727247 · Wing Miscellaneous Structure
  > A 1.5 INCH CRACK_IN SPAR STIFFENER LOCATED OUTBD SIDE OF NR 6 SLAT INBD TRACK. REPAIRED PER MM 57-20-21.
- [SDR DL72W972557](https://openairdocs.org/sdr/DL72W972557.md): Bracket · cracked · Dec 6, 1997 · N2816W · Boeing 727247 · Leading Edge Slat Actuator
  > FOUND ON A1 LETTER CK, NR 1 SLAT ACTUATOR I/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21.
- [SDR DL72W971990](https://openairdocs.org/sdr/DL72W971990.md): Bulkhead · cracked · Oct 3, 1997 · N2816W · Boeing 727247 · Fuselage Main, Bulkhead
  > A 2 INCH CRACK WAS FOUND IN THE 1183 BULKHEAD AT RBL 8.0 AND WL 180. THIS ER/A WILL GIVE INSTRUCTIONS TO ACCOMPLISH A REPAIR UNTIL THE FULL MODIFICATION REQUIRED BY AIRWORTHINESS DIRECTIVE 90-06-09 IS ACCOMPLISHED. THE REPAIR WILL BE INSTALLED ON THE FWD SID
- [SDR DL72W970919](https://openairdocs.org/sdr/DL72W970919.md): Stringer · cracked · May 13, 1997 · N2816W · Boeing 727247 · Vertical Stabilizer
  > STRINGER 8 CRACKED INSIDE VERT STAB RT SIDE FIN STA 133.800. REPAIRED PER M/M 55-30-0.
- [SDR DL72W962336](https://openairdocs.org/sdr/DL72W962336.md): Frame · cracked · Oct 16, 1996 · N2816W · Boeing 727247 · Service Doors
  > RT AFT SERVICE DOOR FWD FRAME CRACKED.5 INCH AT LOWER I/B CORNER OF UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2 FIG 4.
- [SDR DL72W962333](https://openairdocs.org/sdr/DL72W962333.md): Frame · cracked · Oct 16, 1996 · N2816W · Boeing 727247 · Service Doors
  > RT AFT SERVICE DOOR FWD FRAME CRACKED.5 INCH AT LWR I/B CORNER OF UPPER HINGE CUTOUT. REPAIRED PER SRM 52-40-2 FIG 4.
- [SDR DL72W962332](https://openairdocs.org/sdr/DL72W962332.md): Stiffener · cracked · Oct 16, 1996 · N2816W · Boeing 727247 · Wing Miscellaneous Structure
  > A 1 INCH CRACK IN WING L/E VERTICAL STIFFENER AT NR 5 SLAT I/B TRACK O/B POSITION. REPLACED STIFFENER PER M/M.
- [SDR DL72W960611](https://openairdocs.org/sdr/DL72W960611.md): Skin · cracked · Mar 19, 1996 · N2816W · Boeing 727247 · Vertical Stabilizer, Plate/Skin
  > FOUND DURING E-2 LETTER CHECK - 2 EA,.25 INCH CRACKS EXTENDING FROM RIVET HOLES, RT VERTICAL STAB SKIN, JUST BELOW SADDLE PLATE 9501. REPAIRED PER M/M 54-30-0.
- [SDR DL72W960610](https://openairdocs.org/sdr/DL72W960610.md): Web · cracked · Mar 19, 1996 · N2816W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND DURING E-2 LETTER CHECK -.50 INCH CRACK, LT FWD TORQUE BOX LIGHTENING HOLE. REPAIRED PER M/M 53-11-0.

Next page: https://openairdocs.org/deregistered/N2816W-2013-06-11/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 = 'N2816W' AND deregistration_id = 'N2816W-2013-06-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N2816W-2013-06-11/reports

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