# Service difficulty reports: N64339, cancelled Aug 8, 2013

A list on [N64339, cancelled Aug 8, 2013](https://openairdocs.org/deregistered/N64339-2013-08-08.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR TWAA0008901](https://openairdocs.org/sdr/TWAA0008901.md): Battery Pack · inoperative · Jun 6, 2000 · N64339 · Boeing 727231 · Emergency Lighting
  > THE EMERGENCY CEILING AREA LIGHT AT CABIN ROW 3 WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 2-20-00 MCI.
- [SDR TWAA0008205](https://openairdocs.org/sdr/TWAA0008205.md): Actuator · failed · May 22, 2000 · N64339 · Boeing 727231 · Landing Gear Actuator
  > DURING GEAR EXTENSION NOSE GEAR FAILED TO LOCKDOWN. MANUALLY CRANKED NOSE GEAR DOWN. REPLACED NOSE LANDING GEAR DOWNLOCK ACTUATOR. CC03 02-20-00 MCI.
- [SDR TWAA0003106](https://openairdocs.org/sdr/TWAA0003106.md): Skin · delaminated · Feb 17, 2000 · N64339 · Boeing 727231 · Trailing Edge Flaps
  > DURING CHECK-C MAINT, THE LT WING, 24 IN OUT FROM INBD END OF THE INBD TE, THE AFT FLAP WAS DELAMINATED INBD END OF TE. REPLACED FOREFLAP WITH SERVICEABLE UNIT PER MM 27-51 AND M27-27-41 NUMBER 1.
- [SDR TWAA0003105](https://openairdocs.org/sdr/TWAA0003105.md): Skin · damaged · Feb 17, 2000 · N64339 · Boeing 727231 · Leading Edge Devices
  > DURING CHECK-C MAINT, THE LT WING NUMBER 2 FOREFLAP HAD HOLE ON BOTTOM SIDE INBD END. REPLACED FOREFLAP WITH SERVICEABLE UNIT PER MM 27-51, AND M27-27-23.
- [SDR TWAA0003104](https://openairdocs.org/sdr/TWAA0003104.md): Structure · cracked · Feb 16, 2000 · N64339 · Boeing 727231 · Service Doors
  > DURING CHECK-C MAINT, FOUND FWD RT CABIN SERVICE DOOR STRUCTURE WITH CRACK, APPROX 6 INCHES LONG, UNDER AND EMITTING FROM THE FWD LOWER STOP CASTING. REPLACED CRACKED DOOR SECTION PER PRINT NUMBER 65-56150 AND SRM FASTENER SUBSTITUTION 51-30-02.
- [SDR TWAA0002905](https://openairdocs.org/sdr/TWAA0002905.md): Floorbeam · corroded · Feb 14, 2000 · N64339 · Boeing 727231 · Fuselage Main, Floor Beam
  > DURING CHECK-C MAINTENANCE, THE CABIN FLOOR SUPPORT WAS CORRODED AT STA 1110 TO 1130, AT LBL 12 INCHES. MADE NEW FLOOR SUPPORT FROM 7075-T6 PER TWA S/N 56-1850. PRIMED AND INSTALLED PER SRM 51-30-2.
- [SDR TWAA0002904](https://openairdocs.org/sdr/TWAA0002904.md): Bracket · broken · Feb 14, 2000 · N64339 · Boeing 727231 · Wing Miscellaneous Structure
  > DURING CHECK-C MAINT, THE LT WING NUMBER 4 LE SLAT, OTBD STRUCTURAL UP STOP MOUNT BRACKET WAS BROKEN/CRACKED BOTH SIDES. MANUFACTURED NEW BRACKET FROM 7075-T6 PER BOEING PRINT PL-65-17220. PRIMED, PAINTED, AND INSTALLED PER SRM 51-30-2.
- [SDR TWAA0003103](https://openairdocs.org/sdr/TWAA0003103.md): Seat Track · corroded · Feb 13, 2000 · N64339 · Boeing 727231 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINTENANCE, FOUND TOP OF CABIN CHAIR TRACK CORRODED UNDER FLOOR PANELS STA 1030 TO 1070, NUMBER 2 TRACK. REMOVED CORRODED TRACK STA 1030 TO 1070. MADE SECTION OF CHAIR TRACK PER BOEING DRAWING 65-19601 AND INSTALLED TRACK PER SRM 53-10-5.
- [SDR TWAA0002702](https://openairdocs.org/sdr/TWAA0002702.md): Rivet · cracked · Feb 13, 2000 · N64339 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT, FOUND CRACK AT RIVET HEAD ON LT O/B SIDE OF THE NUMBER 2 ENGINE INLET, 17 INCHES UP FROM THE FUSELAGE AND 28 ICHES AFT OF THE INLET L/E. FABRICATED REPAIR PER SRM 54-30-3 AND INSTALLED.
- [SDR TWAA0002803](https://openairdocs.org/sdr/TWAA0002803.md): Skin · corroded · Feb 11, 2000 · N64339 · Boeing 727231 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT, FOUND CORROSION ON SKIN AND SPLICE PLATE AT STA 680, O/B OF STRINGER 28L. REPAIRED PER SRM 53-30-03, PAGE 14E. REMOVED A 4 IN BY 5 IN SECTION OF SKIN AND CORROSION ON STRINGER. CUT TEMPLATE FOR PLUG. SOLD CORROSION/CLEAN UP TO INSPECT
- [SDR TWAA0002606](https://openairdocs.org/sdr/TWAA0002606.md): Stringer · corroded · Feb 9, 2000 · N64339 · Boeing 727231 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT, THERE WAS A BULGE IN THE FUSELAGE SKIN AT STA 660, STRINGER 28L. REPLACED STRINGER FROM STA 657 TO 680 PER SRM 53-10-3, PAGE 3.
- [SDR TWAA0002605](https://openairdocs.org/sdr/TWAA0002605.md): Bulkhead · cracked · Feb 8, 2000 · N64339 · Boeing 727231 · Fuselage Main, Bulkhead
  > DURING CHECK-C MAINT, FOUND A 2 INCH CRACK IN PRESSURE WEB, RT MLG WHEEL WELL AT STA 940, RBL 55. CONFIRMED CRACK WITH HIGH FREQ EDDY CURRENT. INSTALLED REPAIR DOUBLER PER BOEING PRINT 65-89360, AND AD 92-19-11.
- [SDR TWAA0002604](https://openairdocs.org/sdr/TWAA0002604.md): Skin · gouged · Feb 8, 2000 · N64339 · Boeing 727231 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT, FOUND DENT AND GOUGE IN FUSELAGE SKIN AT STA 312, BELOW STRINGER 24R. DENT 1.75 IN BY 2 IN BY 0.046 IN DEEP. NO CRACK FOUND PER PART 6-51-00-03. BLENDED AREA PER SRM 51-10-1. DENT WITHIN LIMITS PER SRM 53-30-1.
- [SDR TWAA0002603](https://openairdocs.org/sdr/TWAA0002603.md): Skin · delaminated · Feb 7, 2000 · N64339 · Boeing 727231 · Trailing Edge Flaps
  > DURING CHECK-C MAINT, THE LEFT WING NUMBER 2 AFT FLAP WAS DELAMINATED TOP SKIN 65 IN FROM O/B END. REMOVED AND REPLACED LEFT I/B TRAILING EDGE AFT FLAP PER MM 27-51-02. SAFTIED AND OP CHECK OK.
- [SDR TWAA0002414](https://openairdocs.org/sdr/TWAA0002414.md): Torque Box · cracked · Feb 7, 2000 · N64339 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT THE RT TORQUE BOX VERTICAL WEB (AFT AIRSTAIRS) REPAIR DOUBLER CRACKED ALONG TOP ROW, STR 1273 TO 1269. REPLACED CRACKED WEB USING 7075T6, 0.032 IN METAL, AND MS20470D5, AND MS20470D6 RIVETS AND SSRM 50-80-211.
- [SDR TWAA0002413](https://openairdocs.org/sdr/TWAA0002413.md): Structure · cracked · Feb 4, 2000 · N64339 · Boeing 727231 · Leading Edge Devices
  > DURING CHECK-C MAINT NUMBER 6 LE SLAT HAD A CRACK AT RIVET UNDER ACTUATOR ATTACH FITTING. FABRICATED A REPAIR PER SRM 57-50-3.
- [SDR TWAA0002412](https://openairdocs.org/sdr/TWAA0002412.md): Torque Box · cracked · Feb 4, 2000 · N64339 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND 1.5 INCH LONG CRACK IN RT TORQUE BOX UPPER BEAM AFT SIDE OF STA 1273, 3 INCHES O/B OF VERT WEB. REPLACED BEAM (P/N 65-17518-6) AND INSTALLED GUSSET 69-67881-1 AND STIFFENER ANGLE 65-17518-15 USING BACB 3088 8 AND BACB 3088 6 HI-LOKS
- [SDR TWAA0000102](https://openairdocs.org/sdr/TWAA0000102.md): Unknown · smoke · Jan 3, 2000 · N64339 · Boeing 727231 · Air Distribution System
  > SMOKE IN THE CABIN WAS REPORTED IN FLIGHT. APPEARED ONLY WHEN ENGINE ANTI-ICE WAS ON. SMOKE HAD NO ODOR. MAINTENANCE RAN ENGINES AND ACCOMPLISHED OTHER CHECKS BUT WAS UNABLE TO DUPLICATE THE PROBLEM. CHECK-C 5-20-99 JFK.
- [SDR TWAA9915503](https://openairdocs.org/sdr/TWAA9915503.md): Line · failed · Nov 12, 1999 · N64339 · Boeing 727231 · Hydraulic System, Main
  > THE NUMBER 1 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON IN FLIGHT AND THE -A- HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. IT WAS NECESSARY TO MANUALLY EXTEND THE LANDING GEAR. THE NUMBER 1 ENGINE PUMP PRESSURE LINE HAD RUBBED THROUGH AT THE PYLON PASS THRO
- [SDR TWAA9811101](https://openairdocs.org/sdr/TWAA9811101.md): Cover · cracked · Jul 12, 1998 · N64339 · Boeing 727231 · Emergency Lighting
  > IN THE AFT CABIN, A FOUR-INCH SECTION OF TH EGRESS LIGHT COVER WAS FOUND BROKEN AND A PIECE MISSING. REPLACED SECTION OF COVER. CHECK-C 5-25-98 JFK.
- [SDR TWAA9802201](https://openairdocs.org/sdr/TWAA9802201.md): Power Pack · inoperative · Feb 11, 1998 · N64339 · Boeing 727231 · Emergency Lighting
  > STL - DURING MAINTENANCE CHECK, THE AFT CABIN EGRESS LIGHTS WERE FOUND INOPERABLE FROM ROW 27 AFT. REMOVED WATER FROM EGRESS LIGHT STRIP AND REPLACED POWER PACK. CHECK-C 5-12-97 MCI. (X)
- [SDR TWAA9801302](https://openairdocs.org/sdr/TWAA9801302.md): Battery Pack · discharged · Jan 24, 1998 · N64339 · Boeing 727231 · Emergency Lighting
  > STL - FLT 325 - L2 DOOR EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE BY MECHANIC. REPLACED ESCAPE LIGHT BATTERY PACK ASSY. (M)
- [SDR TWAA9711709](https://openairdocs.org/sdr/TWAA9711709.md): Rib · cracked · Sep 30, 1997 · N64339 · Boeing 727231 · Wing, Rib/Bulkhead
  > MCI - INSTALLED DOUBLER IN CRACKED RIB CHORD LEFT WING AT STATION 738.5. (M)
- [SDR TWAA9711708](https://openairdocs.org/sdr/TWAA9711708.md): Stringer · cracked · Sep 30, 1997 · N64339 · Boeing 727231 · Fuselage Main, Longeron/Stringer
  > MCI - REPAIRED CRACKED AREA AT STATION 1191 STRINGER 3A LEFT AT AFT END STRINGER T/E CLIP UPPER SIDE OF STRINGER AT LAST RIVIT. (M)
- [SDR TWAA9711707](https://openairdocs.org/sdr/TWAA9711707.md): Door Frame · corroded · Sep 30, 1997 · N64339 · Boeing 727231 · Fuselage Miscellaneous Structure
  > MCI - REMOVED CORROSION AND INSTALLED DOUBLER AT DOOR FRAME WEDGE SPACER BETWEEN INNER FRAME SKIN AND FLOOR SUPPORT BRACKET AT STATION 560 BETWEEN STRINGER 26R AND STRINGER 25R. (M)
- [SDR TWAA9804706](https://openairdocs.org/sdr/TWAA9804706.md): Frame · cracked · May 6, 1997 · N64339 · Boeing 727231 · Fuselage Main, Frame
  > DURING OP17 MAINTENANCE CHECK, FOUND A CRACKED INNER FRAME AT 760 CASTING, LEFT, 6 INCHES INBOARD OF 70.5 WING RIB. REPAIRED PER SERVICE BULLETIN 727-53-0197 AND BOEING DWG 65C36279 AND ARA 11715. (M)
- [SDR TWAA9804705](https://openairdocs.org/sdr/TWAA9804705.md): Rib · cracked · May 6, 1997 · N64339 · Boeing 727231 · Fuselage Main, Frame
  > MCI - DURING OP 17 MAINTENANCE CHECK, EDDY CURRENT SHOWED CRACKS IN FWD UPPER AND LWR FASTENER HOLES IN RIB CHORD UPPER VERTICAL FLANGE, 6 AND 12 O'CLOCK POSITION, FS 760, LBL 70. REPAIRED PER ARA 11715. (M)
- [SDR TWAA9804402](https://openairdocs.org/sdr/TWAA9804402.md): Frame · cracked · May 6, 1997 · N64339 · Boeing 727231 · Fuselage Main, Frame
  > MCI - DURING OP 17 MAINTENANCE CHECK, A CRACKED INNER FRAME 760 CASTING WAS FOUND RT 6 INCH INBOARD OF 70.5 WING RIB. CONFIRMED WITH EDDY CURRENT. REPAIRED PER BOEING DWG NR 65C36279 AND SERVICE BULLETIN 727-53-0197. (M)
- [SDR TWAA9803816](https://openairdocs.org/sdr/TWAA9803816.md): Frame · bent · May 6, 1997 · N64339 · Boeing 727231 · Fuselage Main, Frame
  > MCI - DURING OP 17 MAINTENANCE CHECK, THE FORMER RING AT STATION 1030 STRINGER 25L WAS FOUND BENT. REPAIRED THE FRAME AS PER SSRM 53-60-202 PARA B, SPLICED FRAME REPAIR. (M)
- [SDR TWAA9803806](https://openairdocs.org/sdr/TWAA9803806.md): Casting · cracked · May 6, 1997 · N64339 · Boeing 727231 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 17 MAINTENANCE CHECK, EDDY CURRENT INDICATED A CRACK ON FORWARD HOLES ON CASTING BS 760 RBL 70.5. CRACK RUNNING FROM 12 O'CLOCK TO 6 O'CLOCK IN BOTH HOLES. REPAIRED CRACK AT STATION 760 PREVENTATIVE MODIFICATION PER ARA 11713. (M)
- [SDR TWAA9701101](https://openairdocs.org/sdr/TWAA9701101.md): Accessory Box · failed · Jan 19, 1997 · N64339 · Boeing 727231 · Landing Gear Position and Warning
  > DEN - ON LANDING APPROACH LEFT MAIN LANDING GEAR RED LIGHT REMAINED ILLUMINATED, CYCLED LANDING GEAR WITH SAFE GEAR INDICATION. REMOVED AND REPLACED LANDING GEAR ACCESSORY BOX, MFG P/N 65-60211-59. GEAR LIGHTS CHECKED NORMAL. (M)
- [SDR 96ZZZX1191](https://openairdocs.org/sdr/96ZZZX1191.md): Gusset · cracked · Feb 8, 1996 · N64339 · Boeing 727231 · Fuselage Miscellaneous Structure
  > JFK - DURING CHECK C-4D, FOUND A 1.25 INCH VERTICAL CRACK IN LT SIDE OF FUSELAGE FRAME GUSSET, STA 825.95. REPAIRED PER SB 727-53-0197. AIRCRAFT TT: 53,646 HRS; 35,058 CYCLES.

## 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 = 'N64339' AND deregistration_id = 'N64339-2013-08-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N64339-2013-08-08/reports

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