# Service difficulty reports: N707AA, cancelled Jan 6, 2005

A list on [N707AA, cancelled Jan 6, 2005](https://openairdocs.org/deregistered/N707AA-2005-01-06.md).

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

- [SDR 2002F00058](https://openairdocs.org/sdr/2002F00058.md): Pitot Line · contaminated · Nov 4, 2001 · N707AA · Boeing 727223 · Pitot/Static System
  > ON REPOSITION FLIGHT DUE TO IMPENDING HURRICANE ON TAKEOFF ROLL. NO CAPTAINS AIR SPEED INDICATION FLUSHED SYSTEM PER MM 34-11-0 PAGE 209 AND PERFORMED OPS CHECK PER MM 34-11-0. OPS CHECK OK. (M)
- [SDR 2002F00057](https://openairdocs.org/sdr/2002F00057.md): Pitot Line · contaminated · Nov 4, 2001 · N707AA · Boeing 727223 · Pitot/Static System
  > ON REPOSITION FLIGHT DUE TO IMPENDING HURRICANE ON TAKEOFF ROLL. NO CAPTAINS AIR SPEED INDICATION FLUSHED SYSTEM PER MM 34-11-0 PAGE 209 AND PERFORMED OPS CHECK PER MM 34-11-0. OPS CHECK OK. (M)
- [SDR AALA20011199](https://openairdocs.org/sdr/AALA20011199.md): Floorbeam · corroded · Jun 6, 2001 · N707AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - FOUND CORROSION ON UNDERSIDE OF FLOORBEAM AT DOOR SILL AREA FRAME 62 INBOARD OF ROLLOUT DEVICE. CORROSION IS HALF WAY THROUGH FLOORBEAM. INSTALLED FABRICATED SECTION OF FLOORBEAM AT DOOR SILL AREA STATION 4097 (FRAME 62) PER SRM 51-72-10. (M)
- [SDR AALA20011121](https://openairdocs.org/sdr/AALA20011121.md): Charger · inoperative · May 22, 2001 · N707AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY CHARGER SYSTEM FOR LEFT OVERWING EMERGENCY EXIT LIGHT. (M)
- [SDR AALA20002160](https://openairdocs.org/sdr/AALA20002160.md): Wire · damaged · Dec 29, 2000 · N707AA · Boeing 727223 · Light System Wiring
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHT AT SEAT 6D THROUGH 15D INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR LIGHT WIRE AT SEAT 5 AND 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001957](https://openairdocs.org/sdr/AALA20001957.md): Connector · disconnected · Nov 17, 2000 · N707AA · Boeing 727223 · Emergency Lighting
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT FROM ROW 6D TO 15D INOPERATIVE. RE-SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001959](https://openairdocs.org/sdr/AALA20001959.md): Connector · disconnected · Nov 17, 2000 · N707AA · Boeing 727223 · Emergency Lighting
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT BETWEEN 6D AND 15D INOPERATIVE. RE-SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20001286](https://openairdocs.org/sdr/AALA20001286.md): Light · inoperative · Aug 6, 2000 · N707AA · Boeing 727223 · Emergency Lighting
  > MIA DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT OVER FORWARD GALLEY DOOR INOPERATIVE. REPLACED LIGHT SYSTEM GROUND CHECK NORMAL OPERATION.
- [SDR AALA20000392](https://openairdocs.org/sdr/AALA20000392.md): Wire · broken · Mar 3, 2000 · N707AA · Boeing 727223 · Light System Wiring
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVERWING EXIT INOPERATIVE. REPAIRED BROKEN WIRE IN OVERWING LIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA20000034](https://openairdocs.org/sdr/AALA20000034.md): Connector · loose · Jan 6, 2000 · N707AA · Boeing 727223 · Emergency Lighting
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 14-18 INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT ROW 14-18. SYSTEM GRUOND CHECK NORMAL OPERATION. (M)
- [SDR AALA991075](https://openairdocs.org/sdr/AALA991075.md): Wire · broken · Jul 22, 1999 · N707AA · Boeing 727223 · Light System Wiring
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGNCY EXIT FLOOR PATH LIGHTING FROM ROWS 25 TO 28 DEF INOPERATIVE. REPAIRED WIRE TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA990885](https://openairdocs.org/sdr/AALA990885.md): Floor · corroded · Jun 16, 1999 · N707AA · Boeing 727223 · Fuselage Floor Panel
  > TUL - EXFOLIATED CORROSION ON FLOOR PAN EXTRUDING UNDER AND CAUSING BULGING TO FLOOR STRAP ON FORWARD SIDE OF STATION 1183 BULKHEAD, AT LOWER RIGHT CORNER OF VAULT DOOR FRAME, RBL 14 - RBL 24. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-2 AND FLOOR PAN ON
- [SDR AALA990884](https://openairdocs.org/sdr/AALA990884.md): Skin · cracked · Jun 15, 1999 · N707AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - HFEC INDICATES CRACK IN FUSE SKIN AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER BSB 727-53-0198 PAGE 32, FIG 4 DETAIL IV. (M)
- [SDR AALA990886](https://openairdocs.org/sdr/AALA990886.md): Floorbeam · corroded · Jun 9, 1999 · N707AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - CABIN FLOORBEAM CORRODED TOP SIDE RBL 52-62. REMOVED CORROSION AND INSTALLED REPAIRED DOUBLER PER AARD 53-10-07-2. (M)
- [SDR AALA981194](https://openairdocs.org/sdr/AALA981194.md): Spar Cap · corroded · Jun 18, 1998 · N707AA · Boeing 727223 · Horizontal Stabilizer, Spar/Rib
  > TUL - RIGHT HORIZONTAL STABILIZER T/E SPAR CAP HAS CORROSION UNDER DOUBLER, BETWEEN NR 6 AND NR 7 ELEVATOR HINGES. TREATED, PRIMED, AND PAINTED AREA, INSTALLED FILLER AND DOUBLER IAW SRM 55-10-6 AND ESO 11-6-97, DATED 6-3-98. TST: 46,450. CYCLES: 24,085.
- [SDR AALA980902](https://openairdocs.org/sdr/AALA980902.md): Connector · disconnected · May 6, 1998 · N707AA · Boeing 727223 · Emergency Lighting
  > MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. RESECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA980450](https://openairdocs.org/sdr/AALA980450.md): Clip · out of adjust · Mar 8, 1998 · N707AA · Boeing 727223 · Emergency Lighting
  > RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN VENTRAL STAIR INOPERATIVE. ADJUSTED CLIPS ON EMERGENCY EXIT CHARGER FOR VENTRAL STAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA980253](https://openairdocs.org/sdr/AALA980253.md): Wire · broken · Feb 6, 1998 · N707AA · Boeing 727223 · Light System Wiring
  > MIA - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTING AT PASSENGER SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BROKEN WIRE AT EMERGENCY FLOOR LIGHT PASSENGER SEAT ROWS 9 TO 15. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA971444](https://openairdocs.org/sdr/AALA971444.md): Fuel Cap · departed a/c · Aug 11, 1997 · N707AA · Boeing 727223 · Fuel Storage
  > JFK - FLT 803 - AFTER TAKEOFF LGA DURING CLIMB-OUT, NR 1 FUEL QTY BEGAN DECREASING AT AN ABNORMAL RATE. ACCOMPLISHED ABNORMAL PROCEDURE FOR DECREASING FUEL QTY AND AIRCRAFT DIVERTED TO JFK, LANDING WITHOUT INCIDENT. REPLACED LEFT OVERWING FUEL CAP WHICH HAD
- [SDR AALA971250](https://openairdocs.org/sdr/AALA971250.md): Stringer · corroded · Jul 11, 1997 · N707AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION STR 27L OUTBOARD SIDE AND INSIDE CHANNEL STA 676 - STA 680. REMOVED CORRODED SECTION OF STRINGER AND SPLICED IN NEW SECTION PER SRM 53-10-3, FIG 1. TST: 44,187 HOURS. CYCLES: 22,987. (X)
- [SDR AALA970888](https://openairdocs.org/sdr/AALA970888.md): Connector · broken · May 9, 1997 · N707AA · Boeing 727223 · Emergency Lighting
  > MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN AFT SECTION OF MAIN CABIN FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR IN AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA961636](https://openairdocs.org/sdr/AALA961636.md): Wire · broken · Nov 12, 1996 · N707AA · Boeing 727223 · Light System Wiring
  > IAH - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR LIGHTS AT FIRST CLASS DIVIDER INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR LIGHT WIRE AT FIRST CLASS DIVIDER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA961051](https://openairdocs.org/sdr/AALA961051.md): Shear Tie · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - CORROSION ON SHEAR TIE, STA 720 FROM STR 28L - STR 28R. REPLACED WITH NEW SHEAR TIE. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961050](https://openairdocs.org/sdr/AALA961050.md): Frame · gouged · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Main, Frame
  > TL - HOLE AND GOUGE IN RADIUS OF BELT FRAME. REPAIRED FRAME PER SRM 53-10-4, FIGURE 2. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961049](https://openairdocs.org/sdr/AALA961049.md): Frame · misdrilled · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - HOLE DRILLED IN RADIUS OF FRAME. REPAIRED FRAME PER SRM 53-10-4, FIGURE 2. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961048](https://openairdocs.org/sdr/AALA961048.md): Frame · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - CORROSION ON LOWER BELL FRAME, STA 720. INSTALLED REPAIR ON BELL FRAME PER SRM 53-10-4. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961044](https://openairdocs.org/sdr/AALA961044.md): Skin · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - CORROSION ON BELLY SKIN. INSTALLED DOUBLER PER SRM 53-30-3, PAGES 12-14A. REMOVED CORROSION. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961043](https://openairdocs.org/sdr/AALA961043.md): Shear Tie · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > REMOVED SHEAR TIE, REPLACED WITH NEW SHEAR TIE, STA 700, 28LT-28RT PER 53-10-3. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961042](https://openairdocs.org/sdr/AALA961042.md): Strap · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - CORROSION ON STRAP. REMOVED CORROSION, INSTALLED NEW STRAP FRAME 610-620 PER SRM 53-10-3. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961041](https://openairdocs.org/sdr/AALA961041.md): Stringer · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON STA 27R. REMOVED STA 27R, STA 680 - STA 710. INSTALLED NEW SECTION OF STRINGER PER 53-10-3. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961040](https://openairdocs.org/sdr/AALA961040.md): Stringer · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON STR 28L, OUTBOARD SIDE. REMOVED CORROSION STA 28L STA 480 - STA 488. REPAIRED STR 28L, STA 484 PER SRM 53-10-3. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961039](https://openairdocs.org/sdr/AALA961039.md): Stringer · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND CORROSION ON STRINGER 27R. REPAIRED STRINGER PER SRM 53-10-3 PG 3-4. REMOVED CORROSION PER SRM 51-10-6. (M)
- [SDR AALA961038](https://openairdocs.org/sdr/AALA961038.md): Skin · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON SKIN STATION 480 TO 500, STATION 28 LEFT. INSTALLED REPAIR PER SRM 53-30-3, STATION 480 TO 500, STRINGER 28 LEFT. (M)
- [SDR AALA961037](https://openairdocs.org/sdr/AALA961037.md): Stringer · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - HEAVY CORROSION ON STR 29R FROM STA 950E TO STA 1000. REMOVED AND REPLACED STR 29R, STA 950-STA 1000 IAW SRM 53-10-3, AND INSTALLED DOUBLER AND TRIPLER IAW SRM 53-30-3, FIGURE 3, AND ESO 11697, DATED 6-10-96. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961036](https://openairdocs.org/sdr/AALA961036.md): Stringer · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON STR 28R, STA 680 TO STA 720 PLUS 3 INCHES. REMOVED AND INSTALLED NEW STRINGER PER SRM 51-10-1, PAGE 4. ALODINED, PRIMED AND PAINTED PER MM 51-20-0. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961035](https://openairdocs.org/sdr/AALA961035.md): Web · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > FIVE PLACES OF CORROSION ON RIGHT AFT LAVATORY FLOOR WEB, EACH BEING APPROXIMATELY 2 INCHES BY 6 INCHES IN A 20 SQUARE INCH AREA WITH 2 PLACES PASSED LIMITS. REMOVED CORROSION SECTION, REPLACED WITH SHIMMED DOUBLER PER SRM 51-40-2. ALODINED, PRIMED AND PAINT
- [SDR AALA961034](https://openairdocs.org/sdr/AALA961034.md): Stringer · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON STR 28L, STA 704. INSTALLATED NEW SECTION OF STR 28L, STA 680 TO STA 720. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961033](https://openairdocs.org/sdr/AALA961033.md): Stiffener · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Wing Miscellaneous Structure
  > TUL - LEFT WING FORWARD SPAR, CORROSION ON VERTICAL STIFFENER, FSS 245. REPLACED VERTICAL STIFFENER PER SRM 51-10-4, PAGE 4. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961032](https://openairdocs.org/sdr/AALA961032.md): Stiffener · corroded · Jul 11, 1996 · N707AA · Boeing 727223 · Wing Miscellaneous Structure
  > TUL - LEFT WING FORWARD SPAR, CORROSION ON VERTICAL STIFFENER FSS 255. REPLACED STIFFENER PER SRM 51-10-4. TST: 41,665 HOURS. CYCLES: 21,768. (X)
- [SDR AALA961031](https://openairdocs.org/sdr/AALA961031.md): Frame · double drilled · Jul 11, 1996 · N707AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - DOUBLE HOLE DRILLED IN BELT FRAME. REPAIRED FRAME PER SRM 53-10-4, FIGURE 2. TST: 41,665 HOURS. CYCLES: 21,768. (X)

## 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 = 'N707AA' AND deregistration_id = 'N707AA-2005-01-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N707AA-2005-01-06/reports

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