# Service difficulty reports: N2812W, cancelled Mar 21, 2013

A list on [N2812W, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N2812W-2013-03-21.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 · 59 reports

- [SDR DL72W002521](https://openairdocs.org/sdr/DL72W002521.md): Light · inoperative · Dec 16, 2000 · N2812W · Boeing 727247 · Lighting System
  > FWD OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY
- [SDR DL72W002026](https://openairdocs.org/sdr/DL72W002026.md): Bulkhead · cracked · Oct 14, 2000 · N2812W · Boeing 727247 · Fuselage Main, Bulkhead
  > THE LT SIDEWALL BULKHEAD WEB OF THE NLG WHEEL WELL WAS FOUND WITH A 2 INCH LONG AND 4 INCH LONG CRACK NEAR FS 290 AND WL 169. THE CRACKS ARE TYPICAL OF BAC S/B 727-53-0145. THE CRACKS WERE REPAIRED WITH AN ALUMINUM REPAIR DOUBLER. REINFORCEMENT STRAPS WER
- [SDR DL72W002002](https://openairdocs.org/sdr/DL72W002002.md): Stringer · cracked · Oct 13, 2000 · N2812W · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > ONE INCH CRACK STG 18A HORIZONTAL FLANGE 9 INCHES FWD OF AFT END. REPAIR PER MM 53-12-0.
- [SDR DL72W002001](https://openairdocs.org/sdr/DL72W002001.md): Stringer · cracked · Oct 13, 2000 · N2812W · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > FROM E-1 LTR CK N/R 87, APPROX 1 INCH CRACK IN STG 18A HORIZ FLANGE 9 INCHES FWD OF AFT EDGE. REPAIRED PER M/M 53-12-0 LEVEL 1 REPAIR.
- [SDR DL72W000974](https://openairdocs.org/sdr/DL72W000974.md): Skin · cracked · May 15, 2000 · N2812W · Boeing 727247 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 480 & 680 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC INSPECTION CONFIRMED MULTIPLE CRACKS IN MULTIPLE FRAME BAYS. THE LOWER AND UPPER SKIN PANELS WERE CUT TO R
- [SDR DL72W000843](https://openairdocs.org/sdr/DL72W000843.md): Coalescer Bag · dirty · Apr 29, 2000 · N2812W · Boeing 727247 · Humidity Control System
  > DESCENT TO 21000 FT, MAIN DUCT TEMP ROSE TO 120 DEGREES. GOT TEMP BACK TO 80 DEGREES. F/A NOTIFIED CREW SMOKE IN CABIN. BY THE TIME ACFT WAS ON THE GROUND SMOKE HAD DISSIPATED. REPLACED COALESCER BAGS, RAN ENGINES. UNABLE TO DUPLICATE.
- [SDR DL72W000581](https://openairdocs.org/sdr/DL72W000581.md): Frame · cracked · Mar 24, 2000 · N2812W · Boeing 727247 · Fuselage Main, Frame
  > THE INNER CHORD OF THE C2 DOOR CUTOUT AFT FRAME AT FS 990 WAS FOUND WITH A.75 INCH CRACK IN THE HORIZONTAL FLANGE BETWEEN STRINGER 26R & 27R. THE CRACK WAS NEAR AN EXISTING CHORD REPAIR. THE EXISTING REPAIR WAS REMOVED AND A 4 INCH LONG SECTION OF HORIZONT
- [SDR DL72W992627](https://openairdocs.org/sdr/DL72W992627.md): Coalescer · contaminated · Nov 30, 1999 · N2812W · Boeing 727247 · Humidity Control System
  > SMOKE ENTERED CABIN AFTER START, PACKS WERE ON BUT NOT OVERHEATED. PNEUMATIC SOURCE WAS APU ON ENGINE NR 1. REPLACED APU FLOW-MULTIPLIER AND COALESCER BAGS. SERVICED APU TO PROPER LEVEL, OP CKS GOOD.
- [SDR DL72W992604](https://openairdocs.org/sdr/DL72W992604.md): Engine · malfunctioned · Nov 23, 1999 · N2812W · Boeing 727247 · Engine (Turbine/Turboprop)
  > DURING T/O, NR 1 THROTTLE HAD TO BE ADVANCED BEYOND NORMAL POS TO ATTAIN T/O EPR, EGT AND N2 WERE IN CAUTION RANGE FOR NR 1 ENG & N1 WAS LOWER THAN NR 2 & NR 3 ENG. DUCT PRESS ON LT SIDE WAS 30 PSI ON RT 68 PSI. AFT F/A HEARD WHAT SOUNDED LIKE A BACKFIRE ON
- [SDR DL72W992109](https://openairdocs.org/sdr/DL72W992109.md): Fan · failed · Sep 20, 1999 · N2812W · Boeing 727247 · Air Distribution Fan
  > RT PACK PEGGED AC AMP METER, SMOKE IN COCKPIT AND CABIN. REPLACED RT PACK FAN.
- [SDR DL72W992014](https://openairdocs.org/sdr/DL72W992014.md): Angle · corroded · Sep 9, 1999 · N2812W · Boeing 727247 · Nacelle/Pylon Structure
  > DURING HUSH-KIT MOD, FOUND NR 2 AFT MOUNT SUPPORT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED OLD ANGLE WITH ONE OF NEW MFG.
- [SDR DL72W992355](https://openairdocs.org/sdr/DL72W992355.md): Insulation · damaged · Aug 31, 1999 · N2812W · Boeing 727247 · Electrical Power System Wiring
  > ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL (P/N 012210733) PER BOEING SERVICE LETTER 727-SL
- [SDR DL72W982611](https://openairdocs.org/sdr/DL72W982611.md): Skin · corroded · Dec 21, 1998 · N2812W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, FS 660-681 STRINGER 26R, REPAIR FOR CORROSION AT SKIN LAP. THE UPPER SKIN AT THE STRINGER 26R SKIN LAP SPLICE WAS FOUND WITH CORROSION BETWEEN FS 660-665. THE SKIN WAS CUTOUT OVER A 4 BY 4 AREA TO REMOVE THE CORROSION. THE CUTOUT WAS ADJACENT
- [SDR DL72W982250](https://openairdocs.org/sdr/DL72W982250.md): Battery · discharged · Nov 1, 1998 · N2812W · Boeing 727247 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK INOP. REPLACED BATTERY PACK.
- [SDR DL72W981557](https://openairdocs.org/sdr/DL72W981557.md): Skin · corroded · Jul 23, 1998 · N2812W · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 540-560 L 0, REPAIR FOR SKIN CORROSION CUTOUTS, TWO AREAS OF CORROSION WERE FOUND IN THE FUSELAGE BELLY SKIN AT APPROX BL 0 BETWEEN FS 540 AND 560. THE CORROSION WAS CUT OUT OF THE SKIN WITH A 7.5 BY 2.12 CUTOUT AND A 2.25 BY 2 CUTOUT. TH
- [SDR DL72W981550](https://openairdocs.org/sdr/DL72W981550.md): Skin · cracked · Jul 23, 1998 · N2812W · Boeing 727247 · Service Doors
  > FOUND ON MV1 CHECK, 1 CRACK THRU RIVET IN R2 DOOR SKIN LWR FWD CORNER JUST ABOVE GATE HINGE. FABRICATED DOUBLER PER ERA 365315-14 AND INSTALLED DOUBLER.
- [SDR DL72W981525](https://openairdocs.org/sdr/DL72W981525.md): Former · cracked · Jul 1, 1998 · N2812W · Boeing 727247 · Fuselage Miscellaneous Structure
  > CORROSION TASK C53-113-01, CORROSION CRACK AFT SIDE OF FORMER 1070 JUST OUTBD OF STR 28 LT. REPAIRED PER SRM 53-10-4 FIG 27.
- [SDR DL72W981371](https://openairdocs.org/sdr/DL72W981371.md): Floor Beam · corroded · Jul 1, 1998 · N2812W · Boeing 727247 · Fuselage Main, Floor Beam
  > SEVERAL SMALL AREAS OF CORROSION AND BARE METAL AT FLOORBEAM STA 344 AND RBL12 TO LBL 60. REPAIRED PER SRM 53-10-8 FIG 11.
- [SDR DL72W981526](https://openairdocs.org/sdr/DL72W981526.md): Frame · cracked · Jun 30, 1998 · N2812W · Boeing 727247 · Service Doors
  > R-1 DOOR AFT FRAME CRACKED.5 VISIBLE, JUST ABOVE AFT LOWER STOP CASTING. REPAIRED PER M/M 52-12-0 FIG 804.
- [SDR DL72W981233](https://openairdocs.org/sdr/DL72W981233.md): Stiffener · cracked · Jun 9, 1998 · N2812W · Boeing 727247 · Wing Miscellaneous Structure
  > OUTBOARD L/E SPAR STIFFENER CRACKED NR 6 SLAT I/B TRACK O/B SIDE. REPLACED SPAR STIFFENER PER M/M 57-20-21.
- [SDR DL72W981232](https://openairdocs.org/sdr/DL72W981232.md): Bracket · cracked · Jun 9, 1998 · N2812W · Boeing 727247 · Leading Edge Devices
  > A 1.75 INCH CRACK O/B AFT MOUNT BRACKET NR 1 SLAT ACT. ALSO INBD BRACKET CRACKED 2 INCHES. REPAIRED PER MM 57-21-21.
- [SDR DL72W981231](https://openairdocs.org/sdr/DL72W981231.md): Fitting · cracked · Jun 9, 1998 · N2812W · Boeing 727247 · Leading Edge Slat Actuator
  > NR 4 SPOILER O/B ACT SUPPORT FITTING CRACKED. REPAIRED PER MM 57-42-0.
- [SDR DL72W980325](https://openairdocs.org/sdr/DL72W980325.md): Skin · corroded · Feb 6, 1998 · N2812W · Boeing 727247 · Fuselage Main, Plate/Skin
  > A 1 X 1 CUTOUT WAS MADE IN THE FUSELAGE SKIN AT FS 580 JUST ABOVE STRINGER 27L. THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 363961-14, REV A.
- [SDR DL72W972276](https://openairdocs.org/sdr/DL72W972276.md): Stringer · cracked · Nov 6, 1997 · N2812W · Boeing 727247 · Vertical Stabilizer
  > FOUND ON B-2 LETTER CK, CRACK AT BOLT HOLE OF VERTICAL STAB STRINGER S-9 AT STAB STA 133.80 RT SIDE. REPAIRED PER MM 55-30-0.
- [SDR DL72W972159](https://openairdocs.org/sdr/DL72W972159.md): Battery Pack · discharged · Oct 25, 1997 · N2812W · Boeing 727247 · Emergency Lighting
  > FWD AND MID OVERWING EMERG LIGHTS INOP. FOUND BATT PACK FOR FWD EMERG LIGHT INOP. REPLACED BATT PACK. OPS CK OK. FOUND PWR SUPPLY FOR MID EMERG LIGHT INOP. REPLACED PWR SUPPLY AND BATT PACK. OPS CK OK.
- [SDR DL72W971086](https://openairdocs.org/sdr/DL72W971086.md): Wire · cut · Jun 5, 1997 · N2812W · Boeing 727247 · Light System Wiring
  > AFT LEFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. FOUND GROUND WIRE CUT IN TWO PLACES. ONE AND ONE HALF INCH WAS REMOVED AT BOTH LOCATIONS WHERE WIRE PASS OVER SEAT TRACK. REPAIRED WIRE, CKS OK.
- [SDR DL72W970296](https://openairdocs.org/sdr/DL72W970296.md): Start Valve · failed · Feb 10, 1997 · N2812W · Boeing 727247 · Engine Start Valves/Controls
  > DURING CLIMBOUT, NR 1 ENG START VLV LIGHT ILLUMINATED. REPLACED START VLV AND PRESS SW.
- [SDR DL72W962103](https://openairdocs.org/sdr/DL72W962103.md): Gasper Fan · failed · Sep 12, 1996 · N2812W · Boeing 727247 · Air Distribution Fan
  > STRONG BURNING SMELL IN COCKPIT REPLACED GASPER FAN. OPERATIONAL CHECKS GOOD.
- [SDR DL72W954031](https://openairdocs.org/sdr/DL72W954031.md): Spar · cracked · Sep 26, 1995 · N2812W · Boeing 727247 · Trailing Edge Flaps
  > DURING HMV SHOP INSP, FOUND THE AFT LOWER SPAR CHORD CRACKED 56 INCHES FROM I/B END. REPAIRED PER M/M 57-52-0, FOR NR 2 MIDFLAP.
- [SDR DL72W953461](https://openairdocs.org/sdr/DL72W953461.md): Skin · corroded · Aug 14, 1995 · N2812W · Boeing 727247 · Fuselage Main, Plate/Skin
  > DURING OVERHAUL INSPECTION, THE LOWER FUSELAGE SKIN PANEL BETWEEN BS 259.50 AND BS 312 AT STRINGER 20R HAD TO BE TRIMMED TO REMOVE CORROSION DAMAGE TO THE SKIN BELOW THE FWD LAV SERVICE DOOR. REPAIRED IN ACCORDANCE WITH FAA/DER FORM 8110-3, DATED 08-14-95, AN
- [SDR DL72W953420](https://openairdocs.org/sdr/DL72W953420.md): Skin · damaged · Aug 9, 1995 · N2812W · Boeing 727247 · Fuselage Main, Plate/Skin
  > AT HMV, DURING ACCOMPLISHMENT OF PERMANENT REPAIRS TO FUSELAGE SKIN PER DL ERA 256356-14AD. TO FACILITATE MAINTENANCE, AN ADDITIONAL AREA OF SKIN WAS REPLACED AT FS 680 AND 720A +15, PER DL ERA 302240-14.
- [SDR DL72W953362](https://openairdocs.org/sdr/DL72W953362.md): Seat Track · corroded · Aug 4, 1995 · N2812W · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HMV, FOUND SEAT TRACK CORRODED AT RBL 28 FROM STA 1110 TO 1130. REPLACED SEAT TRACK PER 53-20-11.
- [SDR DL72W953422](https://openairdocs.org/sdr/DL72W953422.md): Skin · dented · Jul 31, 1995 · N2812W · Boeing 727247 · Fuselage Main, Plate/Skin
  > A DENT WAS FOUND IN THE UPPER FORWARD CORNER OF AN EXISTING REPAIR AT FS 335 AND STRINGER 24R (REF ER/A 215945-14). THE SECTION WAS TRIMMED OUT AND A DOUBLER WAS INSTALLED PER DL ERA 302205-14.
- [SDR DL72W953263](https://openairdocs.org/sdr/DL72W953263.md): Stringer · cracked · Jul 28, 1995 · N2812W · Boeing 727247 · Wing, Longeron/Stringer
  > OUTBOARD SIDE OF WING STR CRACKED AT FS 686.5 IN NR 1 FUEL TANK LT WING. INSTALLED REPAIR PER MM 57-13-0 PG 808.
- [SDR DL72W953268](https://openairdocs.org/sdr/DL72W953268.md): Stringer · cracked · Jul 27, 1995 · N2812W · Boeing 727247 · Wing, Longeron/Stringer
  > RT WING STR. TO RIB CRACKED AT BOLT HOLE AT WS 629. REPAIRED PER MM 57-13-0. FOUND AT HMV.
- [SDR DL72W953273](https://openairdocs.org/sdr/DL72W953273.md): Floor Beam · corroded · Jul 26, 1995 · N2812W · Boeing 727247 · Fuselage Main, Floor Beam
  > DURING HMV, FOUND CORROSION ON FLOOR BEAM STA 344 RBL 50. REPAIRED PER SRM 53-10-8.
- [SDR DL72W953366](https://openairdocs.org/sdr/DL72W953366.md): Skin · cracked · Jul 25, 1995 · N2812W · Boeing 727247 · Galley Doors
  > DURING HMV, FOUND R-2 DOOR SKIN CRACKED AT THE LOWER FWD CORNER. REPAIRED PER M/M 52-14-0 NR 7.
- [SDR DL72W953363](https://openairdocs.org/sdr/DL72W953363.md): Frame · cracked · Jul 24, 1995 · N2812W · Boeing 727247 · Fuselage Main, Frame
  > DURING HMV, FOUND FRAME AT STA 930 LEFT CRACKED 6 INCHES ABOVE STR 14L. REPAIRED PER SRM 53-10-4 FIG 25.
- [SDR DL72W953320](https://openairdocs.org/sdr/DL72W953320.md): Le Skin · cracked · Jul 24, 1995 · N2812W · Boeing 727247 · Leading Edge Devices
  > CORNER MISSING L/E OF O/B END, NR 3 L/E KRUGER FLAP. REPAIRED PER M/M 57-53-0 FIG 803, DURING SHOP VISIT.
- [SDR DL72W953282](https://openairdocs.org/sdr/DL72W953282.md): Rib · cracked · Jul 24, 1995 · N2812W · Boeing 727247 · Leading Edge Devices
  > NR 6 SLAT NR 7 RIB CRACKED. REPAIRED PER MM 57-54-0 PG 814, FOUND AT HMV.
- [SDR DL72W953281](https://openairdocs.org/sdr/DL72W953281.md): Rib · cracked · Jul 24, 1995 · N2812W · Boeing 727247 · Leading Edge Devices
  > NR 6 SLAT NR 1 RIB CRACKED. REPAIRED PER MM 57-54-0 PG 814, FOUND AT HMV.
- [SDR DL72W953267](https://openairdocs.org/sdr/DL72W953267.md): Stringer · cracked · Jul 24, 1995 · N2812W · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > STR 15R CRACKED AT STA 720B AND 720C. REPAIRED PER SRM 55-10-3.
- [SDR DL72W953261](https://openairdocs.org/sdr/DL72W953261.md): Stringer · cracked · Jul 24, 1995 · N2812W · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > CRACK IN STRINGER JUST FWD OF LT WING ILLUM. LT BETWEEN 720B AND 720C. INSTALLED REPAIR PER SRM 53-10-3. FOUND AT HMV.
- [SDR DL72W953202](https://openairdocs.org/sdr/DL72W953202.md): Stringer · cracked · Jul 24, 1995 · N2812W · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > STRINGER CRACKED, STRINGER 15L BETWEEN STA 720B AND 720C, AFT SIDE OF LIGHT ASSEMBLY. REPAIRED PER SRM 53-10-3, FOUND AT HMV.
- [SDR DL72W953370](https://openairdocs.org/sdr/DL72W953370.md): Skin · damaged · Jul 23, 1995 · N2812W · Boeing 727247 · Fuselage Main, Plate/Skin
  > DURING HMV, FOUND TEMP REPAIR INSTALLED AT FS 1223 STR 27L. REPAIRED PER MM 53-30-0 PAGE 804.
- [SDR DL72W953369](https://openairdocs.org/sdr/DL72W953369.md): Skin · damaged · Jul 23, 1995 · N2812W · Boeing 727247 · Fuselage Main, Plate/Skin
  > DURING HMV, FOUND TEMP REPAIR INSTALLED AT FS 1223 ALONG STR 27R. REPAIRED PER MM 53-30-0 PAGE 804.
- [SDR DL72W953368](https://openairdocs.org/sdr/DL72W953368.md): Skin · damaged · Jul 23, 1995 · N2812W · Boeing 727247 · Fuselage Main, Plate/Skin
  > DURING HMV, FOUND TEMP REPAIR INSTALLED AT FS 1223 RBL 12. REPAIRED PER MM 53-30-0 PAGE 804.
- [SDR DL72W953367](https://openairdocs.org/sdr/DL72W953367.md): Skin · damaged · Jul 23, 1995 · N2812W · Boeing 727247 · Nacelle/Pylon, Plate/Skin
  > DURING HMV, FOUND TEMP REPAIRED INSTALLED RIGHT SIDE AFT AND ABOVE PANEL 9516. REPAIRED PER MM 53-30-0 PAGE 801 AND 802.
- [SDR DL72W953365](https://openairdocs.org/sdr/DL72W953365.md): Support Ring · worn · Jul 23, 1995 · N2812W · Boeing 727247 · Engine Cowling System
  > DURING HMV, FOUND NR 2 ENG COWL SUPPORT RING WORN. REPAIRED PER M/M 53-11-0 PAGE 801.
- [SDR DL72W953364](https://openairdocs.org/sdr/DL72W953364.md): Web · cracked · Jul 23, 1995 · N2812W · Boeing 727247 · Fuselage Miscellaneous Structure
  > DURING HMV, FOUND WEB CRACKED AT STA 1278 IN 48 SECTION, LOWER INSP HOLE. REPAIRED PER MM53-11-0 PAGE 832.

Next page: https://openairdocs.org/deregistered/N2812W-2013-03-21/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 = 'N2812W' AND deregistration_id = 'N2812W-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N2812W-2013-03-21/reports

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