# Service difficulty reports: N136FE, cancelled Aug 6, 2012

A list on [N136FE, cancelled Aug 6, 2012](https://openairdocs.org/deregistered/N136FE-2012-08-06.md).

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

- [SDR 05FDEA03795](https://openairdocs.org/sdr/05FDEA03795.md): Light · inoperative · Nov 14, 2005 · N136FE · Boeing 727100 · Door Warning System
  > RTO FOR AFT AIRSTAIR LIGHT IAS 75 KTS. RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 22NOV05 MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP. VERIFIED AFT AIRSTAIR IS CLOSED AND RED LIGHT EXTINGUISHED. COMPLIED WITH TRO HIGH ENE
- [SDR 05FDEA03509](https://openairdocs.org/sdr/05FDEA03509.md): Door · open · Oct 26, 2005 · N136FE · Boeing 72725C · Cargo/Baggage Doors
  > AFTER DEPARTURE, AIRCRAFT WOULD NOT PRESSURIZE. RAN QRH AND NO SUCCESS. APPLIED SYSTEMS KNOWLEDGE AND COULD NOT SOLVE PROBLEM. RETURNED TO MEMPHIS. AFTER BLOCK-IN TO MEMPHIS, AND A VISUAL INSPECTION, FOUND AFT CARGO DOOR OPEN, AND FAIRING DOOR CLOSED. SUS
- [SDR 05FDEA02661](https://openairdocs.org/sdr/05FDEA02661.md): Bracket · cracked · Aug 25, 2005 · N136FE · Boeing 727100 · Wing, Attach Fittings
  > COVE PANEL BRACKET IS BROKEN ON LOWER WING PANEL BELOW NR 3 SPOILER. REMOVED AND REPLACED 3 EA BRACKET P/N 65-21658Y29, 65-21658-27, AND 65-21658Y30, AND 1 EA ROD P/N 69-17911-18 IAW SRM 51-30-2.
- [SDR 03FDEA01982](https://openairdocs.org/sdr/03FDEA01982.md): Battery · discharged · Nov 25, 2003 · N136FE · Boeing 727100 · Emergency Lighting
  > FWD ENTRY AND COCKPIT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES FOR OVERHEAD LIGHT ASSY'S PER FEDEX MM 33-50-101-2. CHECKS GOOD PER FEDEX MM 33-50-101-2.
- [SDR 03FDEA01917](https://openairdocs.org/sdr/03FDEA01917.md): Frame · cracked · Nov 14, 2003 · N136FE · Boeing 727100 · Fuselage Main, Frame
  > FOUND CRACK ON FRAME TOOLING HOLE BS 1050 STR 27L. CUT OUT CRACKED AREA IN FRAME AT BS 1050, STR 27L AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3.
- [SDR 03FDEA01916](https://openairdocs.org/sdr/03FDEA01916.md): Frame · cracked · Nov 14, 2003 · N136FE · Boeing 727100 · Fuselage Main, Frame
  > FOUND FRAME CRACKED AROUND OPEN HOLE BS 1070 STR 27L. CUT OUT CRACKED AREA IN FRAME AT BS 1070, STR 27L AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3 & FED EX EA 7-5310-55117.
- [SDR 03FDEA01912](https://openairdocs.org/sdr/03FDEA01912.md): Web · corroded · Nov 13, 2003 · N136FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT RIGHT WEB AT BS 1130, RBL 61, WL 208. CORROSION ON AFT RIGHT WEB BS 1130, RBL 61, WL 208 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED WEB IAW SRM 51-40-2.
- [SDR 03FDEA01911](https://openairdocs.org/sdr/03FDEA01911.md): Web · corroded · Nov 13, 2003 · N136FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > CORROSION (C53-224-04), SHEAR WEB BS 1166-1173, RBL 53-62, WL 208.
- [SDR 03FDEA01907](https://openairdocs.org/sdr/03FDEA01907.md): Beam · corroded · Nov 12, 2003 · N136FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > CORRODED LONGITUDINAL BEAM BS 846, LBL 44, WL 208.
- [SDR 03FDEA01890](https://openairdocs.org/sdr/03FDEA01890.md): Skin · bulged · Nov 7, 2003 · N136FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN BULGED AT BS 350 BETWEEN STR 25R AND 26R. INVESTIGATED BULGED SKIN BS 350, STR 25R & 26R. FOUND SKIN TO BE CORRODED BETWEEN SHIM AND SHEAR TIE. REMOVED OLD SHIM. FABRICATED NEW SHIM. ALODINED, PRIMED, AND INSTALLED. ALL PER SRM 51-30-2, MM
- [SDR 03FDEA01889](https://openairdocs.org/sdr/03FDEA01889.md): Skin · damaged · Nov 7, 2003 · N136FE · Boeing 727100 · Cargo/Baggage Doors
  > LWR AFT CARGO DOOR SKIN, SKIN DAMAGED ALONG FWD EDGE AT NR 2 STOP FITTING FROM TOP. *S/D* INSPECTED LWR AFT CARGO DOOR SKIN ALONG WD EDGE, DAMAGE WAS 1 X 16 X.25 INCH FOUND TO BE OUT OF LIMITS IAW SRM 52-00-2. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLE
- [SDR 03FDEA01891](https://openairdocs.org/sdr/03FDEA01891.md): Floorbeam · corroded · Nov 7, 2003 · N136FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION ON UPPER CHORD OF FLOORBEAM BS 1130 RBL 61 WL 208. *S/D* REMOVED CORROSION FROM UPPER CHORD BS 1130 FLOORBEAM, RBL 61, WL 208 AND FOUND OUT OF LIMITS. REMOVED CORRODED SECTION OF BEAM. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS. ALL WORK
- [SDR 03FDEA01404](https://openairdocs.org/sdr/03FDEA01404.md): Panel · malfunctioned · Sep 3, 2003 · N136FE · Boeing 727100 · Landing Gear Position and Warning
  > ON INITIAL GEAR EXTENTION, ALL RED GEAR DOOR LIGHTS OPERATED NORMALLY BUT ONLY GREEN MAIN GEAR LIGHTS ILLUMINATED (NO GREEN NOSE GEAR LIGHT). RECYCLED GEAR UP / DOWN, TWO MAIN INDICATED BRIGHT GREEN, NOSE INDICATED VERY DIM GREEN, CYCLED LIGHT TEST SWITCH AND
- [SDR 02FDEA00867](https://openairdocs.org/sdr/02FDEA00867.md): Handle · out of position · Nov 19, 2002 · N136FE · Boeing 727100 · Cargo/Baggage Doors
  > ON DEPARTURE, FWD CARGO DOOR LT ILLUM FOLLOWED RED TABS AND ELECTED TO RETURN TO PIT FOR MX ACTION. PRESSURIZATION NOT NORMAL/NOTED PRESS BUMP DURING CLIMBOUT. UPON INSPECTION OF FORWARD LOWER CARGO DOOR. FOUND HANDLE INSIDE DOOR SLIGHTLY OPPOSITE OF OUTSID
- [SDR 01FDEA00830](https://openairdocs.org/sdr/01FDEA00830.md): Duct · cracked · Sep 11, 2001 · N136FE · Boeing 72725C · Pneumatic Distribution System
  > PASSING 1500 FT ABOVE GROUND LEVEL NR 3 ENG FIRE LIGHT ILLUM WHEN THROTTLE RETARD. REMOVED AND REPLACED 8TH STAGE BLEED DUCT PER MM 36-00-001-2.
- [SDR 00FDEA00807](https://openairdocs.org/sdr/00FDEA00807.md): Connector · failed · Nov 29, 2000 · N136FE · Boeing 72725C · Engine Oil Quantity
  > 00-331 ON DEPARTURE, NR 1 LOW OIL PRESS/FILTER BYPASS LIGHT ILLUMINATED. ** S/D ** ACCOMPLISH WIND MILL INSP DUE TO ENG SHUT DOWN PER MM 72-00-518D. R&R BYPASS SWITCH AS PER 727-100 MM 79-33-002-4. OPS TEST NORMAL.
- [SDR 99FDEA00007](https://openairdocs.org/sdr/99FDEA00007.md): Retract Mech · malfunctioned · Jan 9, 1999 · N136FE · Boeing 72725C · Leading Edge Slat Control System
  > 99-0007 - DURING FLAP RETRACT, NR 6 SLAT DID NOT FULLY RETRACT. UNABLE TO CORRECT WITH RED TAB PROC. INSPECT SLAT, NO DEFECT FOUND. RAN NR 1 ENG WITH HYD PRESS, EXTEND AND RETRACT ALL LEAD EDGE DEVICE WITH NO FAULT OR PROBLEM FND. MOCC NOTIFIED, AC OK FOR
- [SDR 98FDEA00372](https://openairdocs.org/sdr/98FDEA00372.md): Gpws · malfunction · May 29, 1998 · N136FE · Boeing 72725C · Ground Proximity System
  > 98-0141 - GPWS WARNING FOR GEAR AT 500 FT ABOVE GROUND LEVEL (FULL LANDING CONFIGURATION). DURING TROUBLE SHOOTING PROCESS, FOUND TAILSKID CANNON PLUG. INSTALLED GEAR PINS AND CYCLED GEAR AND FLAPS SEVERAL TIMES. ALL INDICATIONS WERE NORMAL. GPWS CHECKED N
- [SDR 96FDEA01421](https://openairdocs.org/sdr/96FDEA01421.md): Stick Shaker · failed test · Aug 30, 1996 · N136FE · Boeing 72725 · Airspeed/Mach Indicator
  > CONTINUOUS STICK SHAKER AT TAKEOFF. STANDARD POWER TAKEOFF 36C, ADVANCED THROTTLES TO MOMENTARY FIREWALL POWER. PULLED AC NR 1 STALL WARNING CIRCUIT BREAKER, SHAKER STOPPED. ATTEMPTED 1 RESET OF CIRCUIT BREAKER, STILL HAD SHAKER. PULLED CIRCUIT BREAKER AND
- [SDR 96FDEA01369](https://openairdocs.org/sdr/96FDEA01369.md): Return Hyd Line · broken · Aug 15, 1996 · N136FE · Boeing 72725C · Drag Control System
  > TOTAL LOSS OF A-SYS HYD AT FLT LEVEL 280. GEAR MANUALLY EXTENDED AND FLAPS WERE EXTENDED THROUGH ALTERNATE FLAP MASTER. REMOVED AND REPLACED SPOILER RETURN LINE RT. FOUND 2 BROKEN BRACKETS AT SPOILER CLOSE OUT PANEL, REMOVED AND REPLACED SAME (P/N 65-21658-
- [SDR 96FDEA01050](https://openairdocs.org/sdr/96FDEA01050.md): Floor Web · corrosion · May 28, 1996 · N136FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > CABIN CORROSION ON FLOOR WEB STA 1178 APPROX 55 INCHES LBL UPPER SURFACE UNDER CHORD ANGLE. CUT OUT DAMAGED FLOOR WEB AREA, FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-40-2.
- [SDR 96FDEA01049](https://openairdocs.org/sdr/96FDEA01049.md): Vert Angle · cracked · May 28, 1996 · N136FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > VERT ANGLE CRACKED AT LIGHTENING HOLE AT BS 1183 RBL 26 TO 9 WL 253. PERFORMED 1183 VERTICAL BEAM MOD PER BOEING SERVICE BULLETIN 727-53-0182 PG 23 SRM 53-10-9.
- [SDR 96FDEA01048](https://openairdocs.org/sdr/96FDEA01048.md): Hinge Casting · broken · May 28, 1996 · N136FE · Boeing 72725C · Ailerons
  > LARGE HINGE ASSEMBLY FOR LEFT HAND O/B AILERON HAS BAR BROKEN OFF. REMOVED HINGE CASTING AND INSTALLED A SERVICEABLE CASTING PER DRAWING NR 65-19260 SHEET 1.
- [SDR 96FDEA01047](https://openairdocs.org/sdr/96FDEA01047.md): Door Frame · cracked · Apr 30, 1996 · N136FE · Boeing 72725C · Fuselage Miscellaneous Structure
  > CRACK IN LWR FWD CORNER OF DOOR FRAME OF FWD LWR CARGO APPROX 1 INCH LONG. STOP DRILLED CRACK AND INSTALLED 7075-6, 0.90 DOUBLER ANGLE PER SRM 53-10-4 PG 39 TO 41.
- [SDR 95FDEA01510](https://openairdocs.org/sdr/95FDEA01510.md): Hyd Line · broken · Oct 7, 1995 · N136FE · Boeing 72725C · Hydraulic System, Main
  > DURING CRUISE FL 290, A/C LOST SYS A-HYD, NO APPARENT REASON. FOUND NR 2 SPOILER PRESS LINE BROKE. REMOVED AND REPLACED PRESS LINE, REMOVED CASE DRAIN FILTERS AND PRESS FILTERS, NO CONTAMINATION FOUND. INSTALLED NEW CASE DRAIN FILTERS PER MM 29-11-41, PRESS

## 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 = 'N136FE' AND deregistration_id = 'N136FE-2012-08-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N136FE-2012-08-06/reports

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