# Service difficulty reports: N881AA, cancelled Aug 3, 2009

A list on [N881AA, cancelled Aug 3, 2009](https://openairdocs.org/deregistered/N881AA-2009-08-03.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 AALA20011956](https://openairdocs.org/sdr/AALA20011956.md): Light · inoperative · Oct 23, 2001 · N881AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT ROW 6 THROUGH 8 INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT SPLICE AT ROW 6 THROUGH 8. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20011319](https://openairdocs.org/sdr/AALA20011319.md): Web · cracked · Jun 13, 2001 · N881AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - FOUND SMALL CRACK AT RIVET IN TOP OF VERTICAL WEB STATION 1280. CRACK WAS STOPPED DRILLED AND DOUBLER INSTALLED PER SRM 51-40-2 FIG 1. (M)
- [SDR AALA20011269](https://openairdocs.org/sdr/AALA20011269.md): Spar · corroded · Jun 9, 2001 · N881AA · Boeing 727223 · Standard Practices/Structures
  > TUL - FOUND CORROSION ON FRONT SPAR AT NR 2 SLAT ACTUATOR CUT OUT LOWER SIDE. FABRICATED STRAP.040-17-7 PH STAINLESS STEEL. INSTALLED 6 EACH FASTENERS EITHER SIDE OF BLEND AREA WET. INSTALLED PER ESO 11697 DATED 6/07/2001. (M)
- [SDR AALA20011270](https://openairdocs.org/sdr/AALA20011270.md): Elevator · cracked · Jun 8, 2001 · N881AA · Boeing 727223 · Empennage Structure
  > TUL - FOUND CRACK IN LOWER SKIN OF LEFT ELEVATOR. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM 55-20-3 PAGE 7. (M)
- [SDR AALA20010599](https://openairdocs.org/sdr/AALA20010599.md): Wire · broken · Mar 23, 2001 · N881AA · Boeing 727223 · Light System Wiring
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 20 BROKEN. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA20000935](https://openairdocs.org/sdr/AALA20000935.md): Skin · corroded · Jun 2, 2000 · N881AA · Boeing 727223 · Wing, Plate/Skin
  > TUL - FOUND HEAVY CORROSION ON LOWER AFT SKIN ABOVE RIGHT PRIMARY HEAT EXCHANGER AT BS 850 RBL 30. INSTALLED LOWER WING SKIN REPAIR IAW ESO 91697 DATED 6/2/00 AND SRM 51-30-3. (M)
- [SDR AALA20000934](https://openairdocs.org/sdr/AALA20000934.md): Skin · cracked · Jun 2, 2000 · N881AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND FUSELAGE SKIN CRACKED AT THE AFT LOWER HOLE FOR THE WIRE BUNDLE INBOARD OF THE 13TH STAGE MODULATING VALVE. STOP DRILLED CRACK AND INSTALLED DOBLER PER ESO 11697 6-2-00. (M)
- [SDR AALA20000621](https://openairdocs.org/sdr/AALA20000621.md): Light · inoperative · Apr 11, 2000 · N881AA · Boeing 727223 · Emergency Lighting
  > ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROW 26-27 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA2000535](https://openairdocs.org/sdr/AALA2000535.md): Lens · damaged · Mar 21, 2000 · N881AA · Boeing 727223 · Emergency Lighting
  > TUL - FOUND AISLE LIGHTING IN POOR CONDITION, LENS DAMAGED. REPLACED DAMAGED SECTIONS IAW MM 33-50-01. (M)
- [SDR AALA2000534](https://openairdocs.org/sdr/AALA2000534.md): Light · inoperative · Mar 21, 2000 · N881AA · Boeing 727223 · Emergency Lighting
  > TUL - FOUND LIGHT FAILED TO ILLUMINATE WHEN EMERGENCY EXIT LIGHT SWITCH TURNED ON. REPLACED LIGHT ASSY WITH SERVICEABLE UNIT IAW MM 33-50-01. (M)
- [SDR AALA2000536](https://openairdocs.org/sdr/AALA2000536.md): Light · inoperative · Mar 20, 2000 · N881AA · Boeing 727223 · Emergency Lighting
  > TUL - FOUND OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE AT FS 1340. REMOVED AND REPLACED LIGHT ASSY AND PERFORMED OPS CHECK IAW 33-50-01. (M)
- [SDR AALA20000092](https://openairdocs.org/sdr/AALA20000092.md): Light · inoperative · Jan 15, 2000 · N881AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT OVERHEAD LIGHT AT AFT AIRSTAIR INOPERATIVE. REPLACED EMERGENCY EXIT OVERHEAD LIGHT AT AFT AIRSTAIR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
- [SDR AALA991510](https://openairdocs.org/sdr/AALA991510.md): Wire · broken · Oct 6, 1999 · N881AA · Boeing 727223 · Light System Wiring
  > ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT ROW 18 DEF THROUGH 20 DEF INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA991443](https://openairdocs.org/sdr/AALA991443.md): Wire · broken · Sep 21, 1999 · N881AA · Boeing 727223 · Light System Wiring
  > MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN EMERGENCY EXIT ROWS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA991141](https://openairdocs.org/sdr/AALA991141.md): Spar · corroded · Aug 2, 1999 · N881AA · Boeing 727223 · Horizontal Stabilizer, Spar/Rib
  > TUL - LEFT HORIZONTAL STAB REAR SPAR UPPER CHORD CORRODED FORWARD OF NR 1 BALANCE PANEL STATION 33-34. BLENDED CORROSION PER ESO 11697, PAGES 1 AND 2, DATED 8-2-00. TREATED, PRIMED, SEALED AND PAINTED AREA. (M)
- [SDR AALA991142](https://openairdocs.org/sdr/AALA991142.md): Stiffener · corroded · Jul 29, 1999 · N881AA · Boeing 727223 · Fuselage Miscellaneous Structure
  > TUL - STATION 920 STIFFENER AT INBOARD W/W WALL CORRODED AT NUTPLATE LOWER FORWARD CORNER OF APU AIR INTLET SCREEN. REMOVED CORROSION. INSTALLED REPAIR DOUBLER PER SRM 51-40-3. (M)
- [SDR AALA990985](https://openairdocs.org/sdr/AALA990985.md): Light · inoperative · Jul 3, 1999 · N881AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT MIDDLE OF COACH INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA990984](https://openairdocs.org/sdr/AALA990984.md): Connector · broken · Jul 3, 1999 · N881AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA990775](https://openairdocs.org/sdr/AALA990775.md): Wire · broken · May 27, 1999 · N881AA · Boeing 727223 · Light System Wiring
  > MIA - DURING OVERNIGHT MAINTENANCE, MID-CABIN EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRE FOR MID-CABIN EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA990705](https://openairdocs.org/sdr/AALA990705.md): Light · inoperative · May 13, 1999 · N881AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING MAINTENANCE CHECK, AFT AIR STAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIR STAIRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA990547](https://openairdocs.org/sdr/AALA990547.md): Wire · broken · Apr 20, 1999 · N881AA · Boeing 727223 · Light System Wiring
  > ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. SPLICED EMERGENCY EXIT FLOOR PATH LIGHTING BROKEN WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA990048](https://openairdocs.org/sdr/AALA990048.md): Light · inoperative · Jan 11, 1999 · N881AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, AFT AIR STAIR EMERGENCY EXIT INOPERATIVE. REPLACED AFT AIR STAIRS EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA981565](https://openairdocs.org/sdr/AALA981565.md): Skin · corroded · Aug 19, 1998 · N881AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON SKIN UNDER INTERCOSTAL AT LBL 8. INSTALLED DOUBLER REPAIR PER SRM 53-30-3. (M)
- [SDR AALA981564](https://openairdocs.org/sdr/AALA981564.md): Spar · corroded · Aug 18, 1998 · N881AA · Boeing 727223 · Wing Spar
  > TUL - FRONT SPAR LOWER CHORD CORRODED BELOW NR 1 KRUGER FLAP ACTUATOR FS 300 TO 305. INSTALLED REPAIR PER AARD 57-30-00-2 PAGE 1-3. (M)
- [SDR AALA981563](https://openairdocs.org/sdr/AALA981563.md): Stringer · cracked · Aug 18, 1998 · N881AA · Boeing 727223 · Wing, Longeron/Stringer
  > TUL - FOUND CRACK IN STRINGER NR 8 AT RIB ATTACHMENT TOP OF RIB. INSTALLED STRINGER REPAIR PER SB 727-57A159. (M)
- [SDR AALA981562](https://openairdocs.org/sdr/AALA981562.md): Skin · corroded · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - FOUND CORROSION ON FUSELAGE SKIN UNDER INTERCOSTAL AT STRINGER 28R, STATION 580 - STATION 600. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3. (M)
- [SDR AALA981561](https://openairdocs.org/sdr/AALA981561.md): Skin · corroded · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - BELLY SKIN CORROSION UNDER STR 27R, STA 1075 - STA 1086. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3. TST: 53,245 HOURS. CYCLES: 32,117. (X)
- [SDR AALA981560](https://openairdocs.org/sdr/AALA981560.md): Skin · corroded · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > TUL - SKIN UNDER INTERCOSTAL CORRODED JUST OUTBOARD OF FORWARD CARGO. INSTALLED REPAIR PER SRM 53-30-3 FIG 3. TST: 53,245 HOURS. CYCLES: 32,117. (X)
- [SDR AALA981559](https://openairdocs.org/sdr/AALA981559.md): Stringer · corroded · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - STR 27R OUTBOARD LEG CORRODED TOP EDGE STA 663. REPAIRED PER SRM 53-10-3 FIG 2. TST: 53,245 HOURS. CYCLES: 32,117. (X)
- [SDR AALA981558](https://openairdocs.org/sdr/AALA981558.md): Stringer · cracked · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - STR 15R CRACKED AT END TO FIRST FASTENER AT FS 720B. REPAIRED PER SRM 53-20-3 FIG 5. TST: 53,245 HOURS. CYCLES: 32,117. (X)
- [SDR AALA981557](https://openairdocs.org/sdr/AALA981557.md): Stringer · cracked · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - STR 15L CRACKED AT END TO FIRST FASTENER FORWARD 4 INCHES OF FS 720C. REPAIRED PER SRM 53-10-3 FIG 5. TST: 53,245 HOURS. CYCLES: 32,117. (X)
- [SDR AALA981556](https://openairdocs.org/sdr/AALA981556.md): Stringer · corroded · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - STR 27R CORRODED AT OUTBOARD END STA 1076. INSTALLED STRINGER REPAIR AT STA 1076 PER SRM 53-10-3 FIG 1. TST: 53,245 HOURS. CYCLES: 32,117. (X)
- [SDR AALA981555](https://openairdocs.org/sdr/AALA981555.md): Stringer · corroded · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - STR 27R CORRODED STA 720F + 4 INCHES TO STA 740. INSTALLED STRINGER SPLICE PER SRM 53-10-3 PG HB FIG 1. TST: 53,245 HOURS. CYCLES: 32,117. (X)
- [SDR AALA981554](https://openairdocs.org/sdr/AALA981554.md): Stringer · corroded · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - CORROSION ON STR 28R OUTBOARD SIDE STA 595. INSTALLED STRINGER SPLICE SECTION REPAIR PER SRM 53-10-3 FIG 1. TST: 53,245 HOURS. CYCLES: 32,117. (X)
- [SDR AALA981553](https://openairdocs.org/sdr/AALA981553.md): Stringer · corroded · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - STR 27R OUTBOARD LEG CORRODED AT STA 680. REMOVED STRINGER SECTION, SPLICED NEW SECTION PER SRM 53-10-3 FIG 1. TST: 53,245 HOURS. CYCLES: 32,117. (X)
- [SDR AALA981552](https://openairdocs.org/sdr/AALA981552.md): Floorbeam · corroded · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Floor Beam
  > TUL - CORROSION AT FLOORBEAM AT STA 344 FROM LBL 24 TO RBL 24. INSTALLED FLOORBEAM REPAIR PER ESO 11697 AT STA 344. ESO DATED 7-28-98. TST: 53,245 HOURS. CYCLES: 32,117. (X)
- [SDR AALA981551](https://openairdocs.org/sdr/AALA981551.md): Frame · cracked · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - BELL FRAME CRACKED STA 380 BETWEEN STR'S 7-8, RT SIDE. REPAIRED FRAME PER SRM 53-10-4 FIG 2. TST: 53,245 HOURS. CYCLES: 32,117. (X)
- [SDR AALA981550](https://openairdocs.org/sdr/AALA981550.md): Frame · dented · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - BELT FRAME STA 580 UPPER LIP DENTED BETWEEN STR 24L AND STR 23L (DISTORTED WEB). REPAIRED PER SRM 53-10-4 FIG 1. TST: 53,245 HOURS. CYCLES: 32,117. (X)
- [SDR AALA981549](https://openairdocs.org/sdr/AALA981549.md): Frame · cracked · Aug 18, 1998 · N881AA · Boeing 727223 · Fuselage Main, Frame
  > TUL - BELT FRAME CRACKED 1 INCH LONG FROM RIVET TO STRINGER. CUT OUT RADIUS, STA 1180, STR 26R. INSTALLED REPAIR PER SRM 51-40-2 FIG 1 USING 7075T6 MATERIAL,.063 INCH THICKNESS WITH 2 ROWS FASTENERS,.1875 INCH HI-LOCKS, AROUND DAMAGE,.75 INCH SPACE BETWEE
- [SDR AALA981445](https://openairdocs.org/sdr/AALA981445.md): Stringer · cracked · Jul 28, 1998 · N881AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > TUL - FOUND STATION 344 STRINGER 5 RT BACKSIDE OF STRINGER CRACKED TWO PLACES UPPER AND LOWER. CUTOUT DAMAGED AREA. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 3 THROUGH 4B. (M)
- [SDR AALA980714](https://openairdocs.org/sdr/AALA980714.md): Light · inoperative · Apr 7, 1998 · N881AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN AFT COACH INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LGHT STRIP IN AFT COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA980711](https://openairdocs.org/sdr/AALA980711.md): Light · inoperative · Apr 7, 1998 · N881AA · Boeing 727223 · Emergency Lighting
  > DFW - DURING OVERNIGHT MAINTENANCE, AFT SECTION OF COACH EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN AFT COACH SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
- [SDR AALA972247](https://openairdocs.org/sdr/AALA972247.md): Pin · not removed · Nov 25, 1997 · N881AA · Boeing 727223 · Landing Gear Retraction/Extension System
  > DTW - FLT 1765 - AFTER TAKEOFF FROM DTW, NOSE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REMOVED NOSE GEAR PIN THAT WAS STILL INSTALLED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
- [SDR AALA970408](https://openairdocs.org/sdr/AALA970408.md): Flap Track · oversized hole · Feb 26, 1997 · N881AA · Boeing 727223 · Trailing Edge Flaps
  > AFW - FLAP TRACK NR 4 BOLT HOLE REAMED TO.689. BUSHINGS CAP PLATED WITHOUT NICKLE STRIKE. REQUEST ENGINEERING APPROVAL. REPAIRED PER MRB 727-0028. (M)
- [SDR AALA970406](https://openairdocs.org/sdr/AALA970406.md): Stringer · corroded · Feb 26, 1997 · N881AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > AFW - FOUND STRINGER 29R AT APPROX STATION 1018 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED PER MRB 727-0027. (M)
- [SDR AALA970414](https://openairdocs.org/sdr/AALA970414.md): Stringer · corroded · Feb 25, 1997 · N881AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > AFW - FOUND CORROSION IN STRINGER FORWARD CARGO STRINGER 27R. INSTALLED STRINGER SPLICE PER SRM 53-10-3. (M)
- [SDR AALA970412](https://openairdocs.org/sdr/AALA970412.md): Stringer · corroded · Feb 25, 1997 · N881AA · Boeing 727223 · Fuselage Main, Longeron/Stringer
  > AFW - FOUND CORROSION ON STRINGER. INSTALLED REPAIR PER SRM 53-10-3. (M)
- [SDR AALA970410](https://openairdocs.org/sdr/AALA970410.md): Skin · corroded · Feb 25, 1997 · N881AA · Boeing 727223 · Fuselage Main, Plate/Skin
  > AFW - FOUND BULGE IN SKIN AT FUSELAGE. INSTALLED DOUBLER PER SRM 53-30-3. (M)
- [SDR AALA961375](https://openairdocs.org/sdr/AALA961375.md): Fan · defective · Sep 19, 1996 · N881AA · Boeing 727223 · Air Distribution Fan
  > DFW - FLT 942 - EN ROUTE MAI/DFW DURING CRUISE, SLIGHT SULPHUR ODOR NOTED FROM GASPER. ACCOMPLISHED ABNORMAL PROCEDURE. WHEN BUS TIE BREAKERS TO GASPER TRIPPED, ODOR DISSIPATED. AIRCRAFT PROCEEDED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED GASPER FAN. S
- [SDR AALA961004](https://openairdocs.org/sdr/AALA961004.md): Seat Track · corroded · Jul 2, 1996 · N881AA · Boeing 727223 · Fuselage, Seat/Cargo Attach Fittings
  > TUL - FOUND CORROSION ON SEAT TRACK STATION 1110 TO 1130 LEFT OUTBOARD. REPLACED SEAT TRACK, LEFT OUTBOARD STATION 1110 TO 1130. (M)

Next page: https://openairdocs.org/deregistered/N881AA-2009-08-03/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 = 'N881AA' AND deregistration_id = 'N881AA-2009-08-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N881AA-2009-08-03/reports

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