# Service difficulty reports: N2815W, cancelled Aug 27, 2012

A list on [N2815W, cancelled Aug 27, 2012](https://openairdocs.org/deregistered/N2815W-2012-08-27.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 DL72W010853](https://openairdocs.org/sdr/DL72W010853.md): Controller · faulty · May 27, 2001 · N2815W · Boeing 727247 · Cabin Pressure Controller
  > A/C WILL NOT HOLD PRESSURIZATION AT FL240 WITH 1 PACK. DESCENDED TO FL150 TO MAINTAIN CABIN. REPLACED PRESSURE CONTROLLER AND E/E OVERBOARD VALVE.
- [SDR DL72W010637](https://openairdocs.org/sdr/DL72W010637.md): Skin · cracked · Apr 17, 2001 · N2815W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, FS 360-480 AT STR 4R SKIN LAP SPLICE CRACK REPAIR LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 480 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONFIRMED 5 CRACKS ALONG THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. AN
- [SDR DL72W010572](https://openairdocs.org/sdr/DL72W010572.md): Controller · malfunctioned · Apr 7, 2001 · N2815W · Boeing 727247 · Air Conditioning System
  > CLIMBING THROUGH 17,000 FT.IN AUTO MODE AIRCRAFT CABIN ALT. PRESSURE CLIMBED THROUGH 10,000FT RAPIDLY. FOLLOWED LOSS OF PRESSURIZATION, CHECKLISTS AND WAS ABLE TO REGAIN CABIN CONTROL AFTER CYCLING LEFT PACK. STBY.MODE WORKED FINE AFTER THAT.
- [SDR DL72W001521](https://openairdocs.org/sdr/DL72W001521.md): Battery · discharged · Aug 10, 2000 · N2815W · Boeing 727247 · Emergency Equipment
  > EMERGENCY FLASHLIGHT AT AFT F/A SEAT LIGHT NOT BLINKING. REPLACED BATTERY, OPS NORMAL.
- [SDR DL72W001141](https://openairdocs.org/sdr/DL72W001141.md): Skin · cracked · Jun 13, 2000 · N2815W · Boeing 727247 · Fuselage Main, Plate/Skin
  > WHILE ACCOMPLISHING LFEC INSP PER 4-74176-12AD ON S4L LAP JOINT, CRACK INDICATION WAS NOTED BETWEEN BS 440 AND 460. INTERNAL HFEC INSPECTION OF ENTIRE PANEL PER SI A SINGLE CRACK WAS VERIFIED BETWEEN BS 440 AND 460 (FASTENER NR 10). DAMAGE WAS REPAIRED PER E
- [SDR DL72W000983](https://openairdocs.org/sdr/DL72W000983.md): Actuator · inoperative · May 19, 2000 · N2815W · Boeing 727247 · Landing Gear Actuator
  > RT MAIN GEAR FAILED TO EXTEND DURING NORMAL EXTENSION. CHECK LIST PROCEDURES WERE USED AND RT GEAR WAS EXTENDED AND LEFT IN THE EXTENDED POSITION FOR THE REMAINDER OF THE FLT. REPLACED RT GEAR SEQUENCE VLV PER MM 32-32-21, NO HELP. STILL NEEDS MANUAL EXTENS
- [SDR DL72W000199](https://openairdocs.org/sdr/DL72W000199.md): Skin · cracked · Jan 26, 2000 · N2815W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE UPPER FUSELAGE SKIN WAS FOUND WITH CRACK INDICATIONS AT THE UPPER ROW OF FASTENERS IN THE STRINGER 26R SKIN LAP SPLICE AT FS 662. ALL CRACK DAMAGE WAS REMOVED WITH A 4.25 X 2.75 CUTOUT. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER B727
- [SDR DL72W992594](https://openairdocs.org/sdr/DL72W992594.md): Skin · dented · Oct 8, 1999 · N2815W · Boeing 727247 · Trailing Edge Flaps
  > INBOARD L/E DENTED AND WORN. REPAIRED ON SHOP ORDER 927514 PER M/M 57-52-0 FIG 803 {FLAP SHOP}.
- [SDR DL72W991428](https://openairdocs.org/sdr/DL72W991428.md): Stiffener · cracked · Jun 24, 1999 · N2815W · Boeing 727247 · Wing Spar
  > TPA LTR CHK B-1, O/B SPAR STIFFENER CRACKED AT NR 3 SLAT I/B TRACK. REPLACED STIFFENER PER M/M 57-20-21.
- [SDR DL72W991427](https://openairdocs.org/sdr/DL72W991427.md): Frame · cracked · Jun 24, 1999 · N2815W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND AT B-1 LTR CK, AFT CABIN ENTRY DOOR FRAME CUTOUT CRACKED LT SIDE 10 INCHES FROM TOP OF CUTOUT. REPAIRED PER SRM 53-10-9.
- [SDR DL72W990923](https://openairdocs.org/sdr/DL72W990923.md): Skin · cracked · Apr 27, 1999 · N2815W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 360-380 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BET
- [SDR DL72W990922](https://openairdocs.org/sdr/DL72W990922.md): Skin · cracked · Apr 26, 1999 · N2815W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 481-681, STRINGER 4R, SKIN LAP SPLICE, CRACK REPAIR. 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. INTERNAL HFEC INSPECTION CONFIRMED 20 CRACKS. THE E
- [SDR DL72W990754](https://openairdocs.org/sdr/DL72W990754.md): Skin · corroded · Apr 7, 1999 · N2815W · Boeing 727247 · Fuselage Main, Plate/Skin
  > ON HUSH-KIT MOD OPN 57118, LOWER SKIN LAP JOINT INSPECTION FOUND CORROSION ON FUSELAGE SKIN BETWEEN BONDED METAL SKIN LAYERS AT STATION 259.5R TO 360R. REPLACED SKIN SECTION WITH A/C SKIN SECTION FROM MANUFACTURER.
- [SDR DL72W990752](https://openairdocs.org/sdr/DL72W990752.md): Skin · corroded · Apr 6, 1999 · N2815W · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN PANEL BETWEEN FS 259.5 AND 360 AND BETWEEN STRINGER 19R AND 24R WAS FOUND WITH SEVERAL AREAS OF CORROSION. THE PANEL WAS REMOVED AND A NEW BOEING SKIN PANEL INSTALLED PER ER/A 366991-14.
- [SDR DL72W990498](https://openairdocs.org/sdr/DL72W990498.md): Angle · corroded · Mar 10, 1999 · N2815W · Boeing 727247 · Engine Mount Section
  > ON HUSH-KIT MOD FOUND RT NR 2 ENG AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG LIMITS. REPLACED CHORD ANGLE WITH PART OF NEW MFG.
- [SDR DL72W990496](https://openairdocs.org/sdr/DL72W990496.md): Angle · corroded · Mar 9, 1999 · N2815W · Boeing 727247 · Engine Mount Section
  > ON HUSH-KIT MOD FOUND LT NR 2 ENGINE AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG LIMITS. REMOVED CHORD ANGLE AND REPLACED WITH NEW MFG PART.
- [SDR DL72W990585](https://openairdocs.org/sdr/DL72W990585.md): Insulation · cracked · Mar 4, 1999 · N2815W · Boeing 727247 · Electrical Power System Wiring
  > DURING HUSH-KIT MOD FOUND INSULATION CRACKED ON GEN FEEDER CABLES IN PYLON ON NR 3 ENGINE. SPLICED IN NEW CABLE (P/N 0122107330) FROM SPLICES IN 48 SECTION TO FIREWALL DISCONNECT.
- [SDR DL72W990321](https://openairdocs.org/sdr/DL72W990321.md): Light · inop · Feb 17, 1999 · N2815W · Boeing 727247 · Flight Compartment Lighting
  > F/O MAP LIGHT SMOKED AND FUMED. REPLACED LIGHT ASSY.
- [SDR DL72W990307](https://openairdocs.org/sdr/DL72W990307.md): Clacker · failed · Feb 16, 1999 · N2815W · Boeing 727247 · Central Warning
  > ATB - ELECT SMELL FROM RT SIDE OF COCKPIT. REPLACED OVERSPEED CLACKER.
- [SDR DL72W982652](https://openairdocs.org/sdr/DL72W982652.md): Bolt · missing · Dec 29, 1998 · N2815W · Boeing 727247 · Leading Edge Slat Actuator
  > ON APPROACH, LEADING EDGE FLAP NR 3 UNSAFE HAD AMBER LIGHT, ON GO-AROUND FLAPS WENT GREEN. SAFE INDICATION ON LANDING. AFTER LANDING FLAPS TO 25 DEGREES, FLAP INDICATION WENT TO AMBER. FOUND ACTUATOR DISCONNECTED FROM FLAP, BOLT MISSING. DAMAGE TO FLAP CO
- [SDR DL72W982347](https://openairdocs.org/sdr/DL72W982347.md): Angle · cracked · Oct 22, 1998 · N2815W · Boeing 727247 · Trailing Edge Flaps
  > DURING SHOP INSP, THE LOWER AFT CHORD ANGLE WAS FOUND CRACKED 33 AND 36.5 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.
- [SDR DL72W981761](https://openairdocs.org/sdr/DL72W981761.md): Shim · migrated · Aug 22, 1998 · N2815W · Boeing 727247 · Trailing Edge Flaps
  > THE I/B TRACK OF THE LT WING I/B FLAP WAS FOUND WITH THE LAMINATED SHIM MIGRATED.25 AS TYPICAL OF S/B 727-57-0178 AND AD 90-07-05. THE SHIM WAS REPLACED PER THE REQUIREMENTS OF THE S/B AND DOCUMENTED PER ER/A 365509-14AD.
- [SDR DL72W981738](https://openairdocs.org/sdr/DL72W981738.md): Battery · discharged · Aug 19, 1998 · N2815W · Boeing 727247 · Emergency Lighting
  > OVERWING EMERGENCY EXIT LIGHTS FLASHING. REPLACED RACK AND BATTERY, OPS CHECK GOOD.
- [SDR DL72W981663](https://openairdocs.org/sdr/DL72W981663.md): Battery Pack · discharged · Aug 12, 1998 · N2815W · Boeing 727247 · Emergency Lighting
  > R-1 DOOR EMERG LIGHT INOP. REPLACED BATT PACK, OPS NOW OK.
- [SDR DL72W980584](https://openairdocs.org/sdr/DL72W980584.md): Strap · cracked · Mar 11, 1998 · N2815W · Boeing 727247 · Fuselage Miscellaneous Structure
  > THE R1 DOOR CUTOUT REINFORCING DOUBLER (BEAR STRAP) WAS FOUND WITH A TYPICAL CRACK IN UPPER HINGE CUTOUT. THE SKIN WAS CUT TO ACCESS THE CRACK AND THE BEAR STRAP WAS CUT TO REMOVE THE CRACK. THE CUTOUTS WERE REPAIRED WITH A DOUBLER AND TRIPLER PER THE GUIDLI
- [SDR DL72W980556](https://openairdocs.org/sdr/DL72W980556.md): Aux Spar · chafed · Mar 11, 1998 · N2815W · Boeing 727247 · Wing Miscellaneous Structure
  > MLG AUX SPAR CHAFED AT INBD FWD END LT SIDE. REPAIRED PER MM 57-43-0 P 801.
- [SDR DL72W980555](https://openairdocs.org/sdr/DL72W980555.md): Web · cracked · Mar 11, 1998 · N2815W · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND ON A1 LETTER CK.25 IN CRACK AT LIGHTENING HOLE VERTICAL WEB STA 1233R IN 48 SECTION. ROUTED OUT DAMAGED AREA PER MM 53-11-0.
- [SDR DL72W972475](https://openairdocs.org/sdr/DL72W972475.md): Frame · cracked · Nov 24, 1997 · N2815W · Boeing 727247 · Fuselage Miscellaneous Structure
  > NR 2 CARGO DOOR FWD FRAME HAS A 1.5 INCH CRACK AT LWR DOOR STOP FITTING. INSTALLED DOUBLER PER SRM 53-10-4.
- [SDR DL72W970775](https://openairdocs.org/sdr/DL72W970775.md): Battery · discharged · Apr 26, 1997 · N2815W · Boeing 727247 · Emergency Lighting
  > RT OVERWING EXTERIOR EMERG LIGHT INOP. REPLACED BATTERY, CKS NORMAL.
- [SDR DL72W970268](https://openairdocs.org/sdr/DL72W970268.md): Power Supply · inoperative · Feb 12, 1997 · N2815W · Boeing 727247 · Emergency Lighting
  > ON L/O CK, FOUND RT OVERWING EXIT SIGNS WOULD NOT ILLUMINATE WITH EMER LTS ON. REPLACED POWER SUPPLY AND BATTERY, OPS CKS OK.
- [SDR DL72W970265](https://openairdocs.org/sdr/DL72W970265.md): Power Supply · inoperative · Feb 12, 1997 · N2815W · Boeing 727247 · Emergency Lighting
  > ON L/O CK, FOUND RT OVERWING EXIT SIGNS WOULD NOT ILLUMINATE WITH EMERGENCY LIGHTS ON. REPLACED POWER SUPPLY AND BATT, OPN CKS OK.
- [SDR DL72W970216](https://openairdocs.org/sdr/DL72W970216.md): Skin · corrosion · Jan 27, 1997 · N2815W · Boeing 727247 · Fuselage Main, Plate/Skin
  > CORROSION WAS FOUND ON THE FUSELAGE LOWER SKIN BETWEEN AT 681 AND 720 JUST I/B OF STR 26R IN THE VICINITY OF AN EXISTING REPAIR. THE EXISTING DOUBLER WAS REMOVED AND A SINGLE REPAIR COVERED BOTH AREAS. THIS REPAIR IS APPROVED BY FAA/DER FORM 8110-3, DER DESI
- [SDR DL72W970190](https://openairdocs.org/sdr/DL72W970190.md): Skin · gouged · Jan 16, 1997 · N2815W · Boeing 727247 · Fuselage Main, Plate/Skin
  > DURING THE INSTALLATION OF THE UPPER HINGE REPAIR/MODIFICATION PER 727-53-0198, A GOUGE WAS FOUND IN THE LOWER FUSELAGE SKIN JUST AFT OF THE REPAIR AREA. DAMAGE REMOVAL RESULTED IN A 1 INCH BY 2 INCH CUT-OUT IN THE SKIN. DUE TO THE CLOSE PROXIMITY OF THIS DA
- [SDR DL72W970102](https://openairdocs.org/sdr/DL72W970102.md): Skin · cracked · Jan 16, 1997 · N2815W · Boeing 727247 · Fuselage Main, Plate/Skin
  > AT MIDVISIT, THE SKIN AT GROUND PNEUMATIC DUCT ACCESS DOOR WAS FOUND CRACKED AT THE AFT I/B CUTOUT CORNER. A DOUBLER WAS FABRICATED AND DRILLED AND INSTALLED PER MM 53-30-0 FIG 802.
- [SDR DL72W970191](https://openairdocs.org/sdr/DL72W970191.md): Skin · cracked · Jan 15, 1997 · N2815W · Boeing 727247 · Fuselage Main, Plate/Skin
  > TWO CRACKS IN THE SKIN AND DOOR SURROUND STRUCTURE WERE FOUND IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE FIRST CRACK MEASURES APPROXIMATELY 2.25 INCHES AND PENETRATES THE EXTERNAL SKIN AND BONDED DOUBLER. THE SECOND CRACK MEASURES APPROXIMATELY 2.25
- [SDR DL72W970180](https://openairdocs.org/sdr/DL72W970180.md): Angle · corrosion · Jan 14, 1997 · N2815W · Boeing 727247 · Fuselage Miscellaneous Structure
  > CORROSION ON MOUNT ANGLES AROUND PERIPHERY OF LOWER FUSELAGE FAIRING OPENING AFT OF LOWER ROTATING BEACON. BEGAN REMOVING T-ANGLES FROM STA 820-920. FABRICATED NEW REPLACEMENT PARTS FOR RT BEAM PER SRM 53-30-1. COMPLETED INST OF RT ANGLE. FABRICATED LT BE
- [SDR DL72W970130](https://openairdocs.org/sdr/DL72W970130.md): Bulkhead · cracked · Jan 14, 1997 · N2815W · Boeing 727247 · Fuselage Main, Bulkhead
  > AT MIDVISIT THE BULKHEAD WEB WAS FOUND CRACKED AT BOTH LOWER O/B CORNERS AT FS 1303. THIS WAS REPAIRED PER SRM 53-10-4.
- [SDR DL72W970115](https://openairdocs.org/sdr/DL72W970115.md): Door Frame · cracked · Jan 14, 1997 · N2815W · Boeing 727247 · Passenger/Crew Doors
  > FOUND R-2 DOOR FRAME CRACKED AT UPPER HINGE CUTOUT. FABRICATED DOUBLER PER SRM 52-40-2 FIG 4. ROUTED OUT DAMAGE PER SRM 52-40-2 FIG 4, INSTALLED DOUBLER PER SRM 52-40-2 FIG 4.
- [SDR DL72W970034](https://openairdocs.org/sdr/DL72W970034.md): Stiffener · cracked · Jan 8, 1997 · N2815W · Boeing 727247 · Leading Edge Devices
  > L/E VERTICAL SPAR STIFFENER CRACKED AT NR 3 SLAT O/B TRACK I/B STIFFENER. REPLACED STIFFENER PER MM 57-20-21.
- [SDR DL72W961557](https://openairdocs.org/sdr/DL72W961557.md): Tr Unit · burnt · Jun 29, 1996 · N2815W · Boeing 727247 · DC Rectifier/Converter
  > VISIBLE SMOKE EXHAUSTING FROM E/E COMP WITH ESS TR C/B POPPED, SMELLS ELECTRICAL. FOUND AND REMOVED ESS T/R AND REPLACED NR 3 TR, OPS OK.
- [SDR DL72W961352](https://openairdocs.org/sdr/DL72W961352.md): Skin · corrosion · May 29, 1996 · N2815W · Boeing 727247 · Fuselage Main, Plate/Skin
  > MTC REPORTS CORROSION ON THE FUSELAGE SKIN AT STA 540 AT STR 27R. CUT-OUT RESULTED IN 5.5 INCHES FWD/AFT BY 3.3 INCHES CIRCUM. AN EXISTING REPAIR INBD OF NEW DAMAGE REPAIRS A CUTOUT MEASURING.15 INCH FWD/AFT BY 2.5 INCHES CIRCUM. SKIN IS MACHINED FROM.125
- [SDR DL72W961310](https://openairdocs.org/sdr/DL72W961310.md): Frame · cracked · May 28, 1996 · N2815W · Boeing 727247 · Passenger/Crew Doors
  > L-2 DOOR FRAME UPPER HINGE CUTOUT CRACKED. REPAIRED PER SRM 52-40-2.
- [SDR DL72W961309](https://openairdocs.org/sdr/DL72W961309.md): Skin · cracked · May 28, 1996 · N2815W · Boeing 727247 · Vertical Stabilizer, Plate/Skin
  > TWO,.75 INCH CRACKS IN VERTICAL STAB SKIN FWD OF SADDLE PANEL RT SIDE ABOVE PANEL 9516. REPAIRED PER M/M 54-30-0.
- [SDR DL72W961308](https://openairdocs.org/sdr/DL72W961308.md): Doubler · cracked · May 28, 1996 · N2815W · Boeing 727247 · Elevator Structure
  > REPAIR DOUBLER CRACKED RT ELEV 3RD FROM O/B HINGE RIB. REPAIRED PER M/M 55-10-31.
- [SDR DL72W961270](https://openairdocs.org/sdr/DL72W961270.md): Light · inoperative · May 23, 1996 · N2815W · Boeing 727247 · Emergency Lighting
  > ON T/S INSP, FOUND COCKPIT OVER DOOR EMERGENCY EXIT/FLASHLIGHT DID NOT OPERATE IN THE ON POSITION DURING TEST. REPLACED ASSEMBLY 334701743.
- [SDR DL72W954737](https://openairdocs.org/sdr/DL72W954737.md): Bulb · failed · Dec 19, 1995 · N2815W · Boeing 727247 · Fire Detection
  > ENGINE FIRE TEST CAUSES NR 1 ENG A/B FIRE DETECTION CIRCUIT BREAKER TO TRIP. REPLACED ENG FIRE TEST PANEL. REPLACED FIRE DET MOD. NO HELP. REPLACED FAULT BULB IN FIRE HANDLE. SYSTEM NOW CKS NORMAL.
- [SDR DL72W954576](https://openairdocs.org/sdr/DL72W954576.md): Skin · cracked · Nov 29, 1995 · N2815W · Boeing 727247 · Leading Edge Devices
  > DURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH FLOATING SKIN CRACKED AT FASTENERS BETWEEN RIBS NR 8 AND 9, 13 AND 14. REPAIRED PER MM 57-54-0.
- [SDR DL72W954611](https://openairdocs.org/sdr/DL72W954611.md): Rib · cracked · Nov 21, 1995 · N2815W · Boeing 727247 · Leading Edge Devices
  > DURING ROUTINE SHOP INSPECTION, RIB NR 13 FROM THE O/B END WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER THE B-727 MM 57-54-0 PG 806 AND 807, FOR NR 1 L/E SLAT.
- [SDR DL72W954680](https://openairdocs.org/sdr/DL72W954680.md): Skin · cracked · Nov 20, 1995 · N2815W · Boeing 727247 · Leading Edge Devices
  > UPON INITIAL INSPECTION, CRACK FOUND IN NR 5 SLAT SKIN UNDER AIR FENCE. REPAIRED PER M/M 57-54-0.
- [SDR DL72W954580](https://openairdocs.org/sdr/DL72W954580.md): Rib · cracked · Nov 20, 1995 · N2815W · Boeing 727247 · Leading Edge Devices
  > NR 1 SLAT RIB MARKED 15 CRACKED. REPAIRED PER MM 57-54-0 PG 819.

Next page: https://openairdocs.org/deregistered/N2815W-2012-08-27/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 = 'N2815W' AND deregistration_id = 'N2815W-2012-08-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N2815W-2012-08-27/reports

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