# Service difficulty reports: Boeing 727-22

A list on [Boeing 727-22](https://openairdocs.org/model/boeing-727-22.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 26 · 1,282 reports

- [SDR 07FDEA00427](https://openairdocs.org/sdr/07FDEA00427.md): Computer · malfunctioned · Feb 8, 2007 · N191FE · Boeing 72722 · Stall Warning System
  > CAPT STICK SHAKER ACTIVATED ON ROTATION. SHAKER SPEED WAS ABNORMALLY SLOW, ABOUT 1/3 NORMAL RATE DURING TEST. SHAKER CONTINUED FOR APPROX 3 MINUTES AND SLOWED GRADUALLY UNTIL IT STOPPED. AIRCRAFT FLEW NORMALLY. REMOVED AND REPLACED NR 1 STALL WARNING COMPU
- [SDR 06FDEA04137](https://openairdocs.org/sdr/06FDEA04137.md): Shutoff Valve · failed · Nov 29, 2006 · N151FE · Boeing 72722 · Cabin Cooling System
  > LOST PRESSURIZATION AT FL 260. COMPLIED WITH QRH, A/C DID NOT PRESSURIZE AUTO OR MANUAL. TROUBLESHOT TO LT PAC S/O VALVE INOP. PWR TO VALVE. REMOVED AND REPLACED LT PAC S/O VALVE PER SMP. LT PAC OPS NORMAL. PRESSURIZED A/C PER JRH TO 1 PSI DIFF OK FOR SE
- [SDR 06FDEA1959](https://openairdocs.org/sdr/06FDEA1959.md): Repair · unknown · May 18, 2006 · N270FE · Boeing 72722 · Wing Main, Frame Structure
  > FOUND PREVIOUSLY REPAIR ON LT INBD MID FLAP LOWER SURFACE INBD OF INBD CARRIAGE FAIRING IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR AND REINSTALLED REPAIR PARTS IAW EA 7-5710-92428. REPAIR IS CLASSIFED AS MAJOR PER FEDEX GMM 6-2-100.
- [SDR 06FDEA1958](https://openairdocs.org/sdr/06FDEA1958.md): Skin · corroded · May 17, 2006 · N192FE · Boeing 72722 · Horizontal Stabilizer, Plate/Skin
  > LOWER SKIN OF LEFT HORIZONTAL STAB HAS NUMEROUS AREAS OF CORROSION FROM STAB TIP TO I/B END, FWD SRAP TO AFT SPAR. REPAIRED PER FED EX EA 7-5510-102242.
- [SDR 06FDEA1941](https://openairdocs.org/sdr/06FDEA1941.md): Beam · chafed · May 17, 2006 · N192FE · Boeing 72722 · Elevator Structure
  > WHILE GETTING AND OK TO CLOSE, FOUND RT ELEVATOR RUB BLOCK SPACER LOOSE AND CHAFING INTO LOWER TRAILING EDGE BEAM AT ELEV STA 118.13. REPAIRED RT HORIZ STAB LOWER TRAILING EDGE BEAM AT ELEV STA 118.13 IAW FED EX EA 7- 5510-100932.
- [SDR 06FDEA1928](https://openairdocs.org/sdr/06FDEA1928.md): Door Frame · corroded · May 15, 2006 · N192FE · Boeing 72722 · Fuselage Main, Structure
  > LEFT AFT EMERGENCY EXIT SEAL FRAME CORRODED. FOUND CORROSION ON SEAL FRAME TO BE OUT OF LIMITS. REMOVED AND REPLACED LT AFT EMERGENCY EXIT HATCH PER MM 52-21-000-5.
- [SDR 06FDEA1911](https://openairdocs.org/sdr/06FDEA1911.md): Attach Fitting · corroded · May 12, 2006 · N192FE · Boeing 72722 · Trailing Edge Flaps
  > NR 2 FLAP TRACK FWD ATTACH FITTING IS CORRODED. REMOVED, REPAIRED AND REINSTALLED NR 2 FLAP TRACK FWD ATTACH FITTING IAW OHM 20-50-01 ANS FED EX EA 7-5710-96623.
- [SDR 06FDEA1799](https://openairdocs.org/sdr/06FDEA1799.md): Skin · corroded · May 11, 2006 · N192FE · Boeing 72722 · Horizontal Stabilizer, Plate/Skin
  > FOUND LOWER SKIN OF RIGHT HORIZONTAL STAB HAS NUMEROUS AREAS OF CORROSION FROM STAB TIP TO IB END, FWD SPAR TO AFT SPAR. REPAIRED PER FED EX EA 7-5510-102242.
- [SDR 06FDEA1724](https://openairdocs.org/sdr/06FDEA1724.md): Fitting · cracked · May 5, 2006 · N192FE · Boeing 72722 · Fuselage Main, Attach Fittings
  > WHILE INSPECTING BS 870 RT TERMINAL FITTING PER FED EX EO 7-5310-7-3663 03 PART 4 FOUND CRACK INDICATION IN ROW 3 HOLE NR 5. REPAIRED DAMAGED HOLE BS 870 TERMINAL FITTING ROW 3, HOLE NR 5 PER FED EX EA 7-5310-99513.
- [SDR 06FDEA1697](https://openairdocs.org/sdr/06FDEA1697.md): Flap Track · damaged · May 3, 2006 · N192FE · Boeing 72722 · Trailing Edge Flaps
  > NR 6 FLAP TRACK AFT ATTACH FITTING DAMAGED OB BARREL NUT HOLE. REMOVED AND REPLACED NR 6 FLAP TRACK AFT O/B ATTACH FITTING PER SRM 51-30-02 AND SRM 51-20-01.
- [SDR 06FDEA1655](https://openairdocs.org/sdr/06FDEA1655.md): Floorbeam · corroded · May 1, 2006 · N192FE · Boeing 72722 · Fuselage Main, Floor Beam
  > FOUND 1110 FLOORBEAM CORRODED ON LOWER FLANGE LBL 30 TO RBL 30. REMOVED AND REINSTALLED AFT CARGO BAY CEILING PANELS BS 1110 TO BS 1170 AND REMOVED AND REINSTALLED FLOORBOARDS BS 1030 TO BS 1100 RBL 0 TO RBL 45 FOR ACCESS IAW SRM 51-30-2. FOUND CORROSION
- [SDR 06FDEA1659](https://openairdocs.org/sdr/06FDEA1659.md): Attach Fitting · damaged · May 1, 2006 · N185FE · Boeing 72722 · Wing, Landing Gear Attach Fittings
  > FORWARD TRUNNION ATTACH FTG OVERSIZE HOLE REWORK. COMPLIED WITH EA 7-5710-7-92417 WINGS MAIN FRAME MLG TRUNNION ATT FITTING OVERSIZE HOLE REWORK RII:573074.
- [SDR 06FDEA1658](https://openairdocs.org/sdr/06FDEA1658.md): None · none · May 1, 2006 · N185FE · Boeing 72722 · Standard Practices/Structures
  > TRUNNION ATTACH FITTING MODIFICATION. COMPLIED WITH EO 7-5710-7-2314D PT5 WINGS MLG TRUNNION ATTACH FITTING.
- [SDR 06FDEA1578](https://openairdocs.org/sdr/06FDEA1578.md): Shear Tie · cracked · Apr 24, 2006 · N192FE · Boeing 72722 · Fuselage Internal Mounting Structure
  > FOUND CRACK IN OEM SHEAR TIE AT BS 520 ABOVE STR 22L. REPAIRED OEM SHEAR TIE AT BS 520 ABOVE STR 22L IAW SRM 53-10-04.
- [SDR 06FDEA1455](https://openairdocs.org/sdr/06FDEA1455.md): Web · gouged · Apr 14, 2006 · N192FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > FOUND FUSELAGE BS 480 TO 640, STR 3L, CARGO DOOR SURROUND WEB GOUGED IN NUMEROUS AREAS. ALL WORK ACCOMPLISHED IAW FEDEX EA 7-5330-99510.
- [SDR 06FDEA1422](https://openairdocs.org/sdr/06FDEA1422.md): Web · corroded · Apr 12, 2006 · N192FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON FLOOR WEB, BS 1130 TO 1176 RBL 49 TO 63, WL 208. REPAIRED FLOOR WEB AT BS 1130 TO 1176 RBL 49 TO 63, WL 208 IAW SRM 51-40-02.
- [SDR 06FDEA1363](https://openairdocs.org/sdr/06FDEA1363.md): Keelbeam · corroded · Apr 10, 2006 · N192FE · Boeing 72722 · Fuselage Main, Floor Beam
  > STA 1030 - 1050 STR 29R HAS CORROSION ON STR FLANGE.
- [SDR 06FDEA1362](https://openairdocs.org/sdr/06FDEA1362.md): Keelbeam · corroded · Apr 10, 2006 · N192FE · Boeing 72722 · Fuselage Main, Keel
  > FOUND STA 1034 STR 29L, CORROSION ON STR FLANGE AT RIVET TAIL.
- [SDR 06FDEA1361](https://openairdocs.org/sdr/06FDEA1361.md): Web · tool damage · Apr 10, 2006 · N192FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > FOUND DRILL START BEHIND VERTICAL STIFFENER ON FWD SIDE OF 870 WEB.
- [SDR 06FDEA1337](https://openairdocs.org/sdr/06FDEA1337.md): Web · corroded · Apr 7, 2006 · N192FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON FLOOR WEB, BS 1155, RBL 41, WL 208. REPAIRED PER SRM 51-40-02.
- [SDR 06FDEA1336](https://openairdocs.org/sdr/06FDEA1336.md): Skin · dented · Apr 7, 2006 · N192FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN DENT BS 693, 5" BELOW STR 26R. REPAIRED PER SRM 53-30-3.
- [SDR 06FDEA1334](https://openairdocs.org/sdr/06FDEA1334.md): Skin · corroded · Apr 7, 2006 · N192FE · Boeing 72722 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STABILIZER CORROSION REMOVAL DAMAGE IS OUT OF LIMITS AT RT STAB STA 120,.5 INCHES AFT OF THE LE SPAR AND FWD EDGE OF THE SKIN NECESSITATING A REPAIR FROM FEDEX NR N00382 (TAIL 5008). REPAIRED RT HORIZ STAB AT RT STAB STA 120,.5" AFT OF THE L
- [SDR 06FDEA1333](https://openairdocs.org/sdr/06FDEA1333.md): Skin · corroded · Apr 7, 2006 · N192FE · Boeing 72722 · Horizontal Stabilizer, Plate/Skin
  > FOUND RT HORIZONTAL STABILIZER CORROSION REMOVAL DAMAGE IS OUT OF LIMITS AT RT STAB STA 116.5, 9.5 INCHES AFT OF THE LE SPAR AND FWD EDGE OF THE SKIN NECESSITATING A REPAIR FROM FEDEX NR N00382 (TAIL 5008). REPAIRED PER SRM 55-10-3.
- [SDR 06FDEA1332](https://openairdocs.org/sdr/06FDEA1332.md): Skin · chafed · Apr 7, 2006 · N192FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > UPON REMOVAL OF FAIRING 3509 FOR ACCESS FOUND EXTERNAL FUSELAGE SKIN CHAFED AT FAIRING CONTACT LINE, BS 1110-1130 BETWEEN STR 25 AND 26 LEFT. REPAIRED PER SRM 53-30-3.
- [SDR 06FDEA1321](https://openairdocs.org/sdr/06FDEA1321.md): Stringer · corroded · Apr 6, 2006 · N192FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > FOUND STA 970 - 1030, CORROSION IN STR 30 AT RIVET TAILS. REPAIRED STR 30 PER SRM 53-10-3.
- [SDR 06FDEA1313](https://openairdocs.org/sdr/06FDEA1313.md): Flap Track · corroded · Apr 5, 2006 · N192FE · Boeing 72722 · Trailing Edge Flaps
  > NR 6 FLAP TRACK IS CORRODED AT SAFETY BOLT HOLE. REPLACED NR 6 FLAP TRACK IAW TASK CARD 27X5708-03.
- [SDR 06FDEA1279](https://openairdocs.org/sdr/06FDEA1279.md): Frame · corroded · Apr 3, 2006 · N192FE · Boeing 72722 · Fuselage Main, Frame
  > FOUND STA 1070 BETWEEN STR 28L AND 29L, CORROSION ON FRAME OUTBOARD FLANGE. REPAIRED FRAME BS 1070 STR 28L TO 29L IAW SRM 53-10-4.
- [SDR 06FDEA1300](https://openairdocs.org/sdr/06FDEA1300.md): Flap Track · corroded · Apr 3, 2006 · N192FE · Boeing 72722 · Trailing Edge Flaps
  > NR 8 FLAP TRACK FWD LUG IS CORRODED. REPLACED NR 8 FLAP TRACK IAW TASK CARD 27X5710-03.
- [SDR 06FDEA1299](https://openairdocs.org/sdr/06FDEA1299.md): Skin · damaged · Apr 3, 2006 · N192FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND STA 342, 4" BELOW STR 21L SKIN HAS SHARP PROTRUSION, FROM APPARENT INTERNAL IMPACT. REPAIRED DAMAGE AT STA 342 4" BELOW STR 21L IAW SRM 53-30-3 FIG 13A.
- [SDR 06FDEA1281](https://openairdocs.org/sdr/06FDEA1281.md): Flap Track · corroded · Apr 3, 2006 · N192FE · Boeing 72722 · Trailing Edge Flaps
  > NR 7 FLAP TRACK CORRODED AT FWD END. REPLACED NR 7 FLAP TRACK IAW TASK CARD 27X5709-03.
- [SDR 06FDEA1280](https://openairdocs.org/sdr/06FDEA1280.md): Web · corroded · Apr 3, 2006 · N192FE · Boeing 72722 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON FLOOR WEB, BS 1146 TO 1173, LBL 7 TO 14, WL 208. REPLACED FLOOR WEB, BS 1146-1173 WL 208 PER SRM 51-30-2, 51-10-2, 51-20-4.
- [SDR 06FDEA1247](https://openairdocs.org/sdr/06FDEA1247.md): Skin · dented · Mar 27, 2006 · N192FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND DENT IN SKIN, BS 1084, 1" ABOVE STR 2L TO 4" ABOVE STR 4L. ALL WORK ACCOMPLISHED IAW FED EX EA 7-5330-99514 FOUND TO BE A MAJOR REPAIR
- [SDR 06FDEA0844](https://openairdocs.org/sdr/06FDEA0844.md): Skin · damaged · Feb 26, 2006 · N191FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > DENT WITH ASSOCIATED GOUGE IN FUSELAGE SKIN, BS 590, BETWEEN STR 17 AND 18 RT. FOUND TO BE OUT OF SERVICE LIMITS, REPAIRED IAW SRM 53-30-3 FIG 13A.
- [SDR 06FDEA0806](https://openairdocs.org/sdr/06FDEA0806.md): Shear Tie · damaged · Feb 22, 2006 · N191FE · Boeing 72722 · Fuselage Internal Mounting Structure
  > WHILE REMOVING SKIN FOR ACCESS ON STR 27L REPAIR; FOUND SHEAR TIE AT BS 1143 STR 27L DAMAGED. REPAIRED SHEAR TIE PER SRM 53-10-4 FIG 15.
- [SDR 06FDEA0537](https://openairdocs.org/sdr/06FDEA0537.md): Spar · tool damage · Feb 3, 2006 · N191FE · Boeing 72722 · Wing Spar
  > RT WING FRONT SPAR LOWER CHORD PLATE HAS A MISSED DRILLED HOLE LOCATED DIRECTLY BELOW THE NR 4 K-FLAP ACTUATOR. REPAIRED MISSDRILLED HOLE IAW FED EX EA 7-5710-96565.
- [SDR 06FDEA0131](https://openairdocs.org/sdr/06FDEA0131.md): Stringer · damaged · Jan 9, 2006 · N191FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT HOLE IN STR 23 LT B/S 965. REPAIRED AFT CARGO COMPARTMENT STR 23L AT BS 965, HOLE IN TOP OF STR IAW SRM 53-10-3.
- [SDR 06FDEA0060](https://openairdocs.org/sdr/06FDEA0060.md): Floorbeam · corroded · Jan 6, 2006 · N191FE · Boeing 72722 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON FLOORBEAM UPPER FLANGE AROUND NUTPLATES AT BS 1130, LBL 10 TO RBL 29, WL 208. REPAIRED FLOORBEAM UPPER FLANGE BS1130, RBL 10, WL 208 IAW SRM 53-10-8.
- [SDR 06FDEA0015](https://openairdocs.org/sdr/06FDEA0015.md): Stringer · cracked · Jan 3, 2006 · N191FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > FOUND STR 26R CRACKED AT FASTENER HOLE O/B FLANGE BS 430. REPAIRED CRACKED FASTENER IAW SRM 53-10-03.
- [SDR 06FDEA0013](https://openairdocs.org/sdr/06FDEA0013.md): Skin · chafed · Jan 3, 2006 · N191FE · Boeing 72722 · Nacelle/Pylon, Plate/Skin
  > FOUND SECTION SKIN IS CHAFED ABOVE RT LWR RAIN GUTTER, BS 1351. REPAIRED SKIN CHAFE OVER RT LWR RAIN GUTTER, BS 1351 PER SRM 54-30-3.
- [SDR 05FDEA04395](https://openairdocs.org/sdr/05FDEA04395.md): Structure · corroded · Dec 21, 2005 · N191FE · Boeing 72722 · Fuselage Main, Structure
  > BS 297 CORROSION ON LT LOWER NOSE CHORD.
- [SDR 05FDEA04351](https://openairdocs.org/sdr/05FDEA04351.md): Door · obstructed · Dec 16, 2005 · N189FE · Boeing 72722 · Cargo/Baggage Doors
  > ON DEPARTURE, FORWARD CARGO DOOR LIGHT ILLUMINATED, COULD NOT PRESSURIZE AIRCRAFT, RETURNED TO MEM. FOUND DOOR LATCH HANDLE STOWED, DOOR CL0SED BUT NOT LOCKED OVER CENTER. ALSO, FOUND BUNGEE STUCK IN DOOR LATCH MECHANISM ON FWD SIDE OF DOOR. OPENED DOOR, PU
- [SDR 05FDEA04265](https://openairdocs.org/sdr/05FDEA04265.md): Accessory Unit · failed · Dec 12, 2005 · N188FE · Boeing 72722 · Landing Gear Position and Warning
  > DURING TEST FLIGHT, HAD NO LEFT MAIN GEAR INDICATION. PERFORMED GOOD RING OUT PER FED EX WDM 32-64-02, 32-64-01. REPLACED LANDING GEAR ACCESSORY UNIT AND PERFORMED GOOD FUNCTIONAL TEST PER FED EX MM 20-10-017-2, 32-09-111-5.
- [SDR 05FDEA03859](https://openairdocs.org/sdr/05FDEA03859.md): Rib · mislocated · Nov 17, 2005 · N188FE · Boeing 72722 · Elevator Structure
  > WHILE WORKING CARD N01365, FOUND RT NR 5 ELEVATOR HINGE RIB MISLOCATED. REMOVED AND REPLACED RT NR 5 ELEVATOR HINGE RIB PER EA 7-5510-91413.
- [SDR 05FDEA03835](https://openairdocs.org/sdr/05FDEA03835.md): Rib · damaged · Nov 16, 2005 · N188FE · Boeing 72722 · Horizontal Stabilizer, Spar/Rib
  > DURING INSPECTION OF THE LT HORIZ STAB ELEVATOR RIB AT ELEV STA 136.5, FOUND TO HAVE EXISTING REPAIRS ON THE LOWER IB AND OB FLANGES OF THE RIB AT THE TRAILING EDGE BEAM. RIB REQUIRES REPLACEMENT PER FEDEX EO 7-5510-7-5001 PT 1. REPAIRED PER S.B. 727-55A00
- [SDR 05FDEA03801](https://openairdocs.org/sdr/05FDEA03801.md): Repair · unknown · Nov 14, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > REPAIR AT BS 480 STR 26L TO 27L REQUIRES ENGINEERING DISPOSITION PER EO 7- 5100-7-5000 P3. COMPLIED WITH FED-EX EA 7-5330-95353. FOUND TO BE MAJOR REPAIR
- [SDR 05FDEA03615](https://openairdocs.org/sdr/05FDEA03615.md): Stringer · unknown · Nov 3, 2005 · N188FE · Boeing 72722 · Fuselage Main, Longeron/Stringer
  > STR 25R REQUIRES ENGINEERING DISPOSITION PER EO 7-5100-7-5000 PT1. COMPLIED WITH E.A. 7-5330-91409
- [SDR 05FDEA03614](https://openairdocs.org/sdr/05FDEA03614.md): Frame · damaged · Nov 3, 2005 · N188FE · Boeing 72722 · Fuselage Main, Frame
  > FUSELAGE, MAIN FRAME FORWARD CARGO DOOR FORWARD FRAME REPLACEMENT AD'S 90-06-09 AND 98-11-03 R1 (LOG BOOK ENTRY REQUIRED). REPAIRED PER E.A. 7-5310-93709
- [SDR 05FDEA03560](https://openairdocs.org/sdr/05FDEA03560.md): Floorbeam · corroded · Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Floor Beam
  > FOUND CORROSION (C53-224-01) ON MAIN CARGO DECK FLOORBEAM UPPER AND LOWER FLANGE AT BS 1130 BETWEEN RBL 25 AND RBL 45, WL 208. REPAIRED MAIN DECK FLOORBEAM UPPER FLANGE AT BS 1130, RBL 45, WL 208 REF SRM 53-10- 8 FIG 10.
- [SDR 05FDEA03559](https://openairdocs.org/sdr/05FDEA03559.md): Skin · damaged · Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 10L. REPAIRED PER E.O. 7-5330-7-2319 PT 5
- [SDR 05FDEA03558](https://openairdocs.org/sdr/05FDEA03558.md): Skin · damaged · Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/Skin
  > FOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 10R. REPAIRED PER E.O. 7-5330-7-2319 PT 5

Next page: https://openairdocs.org/model/boeing-727-22/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 aircraft_model_key = '72722'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-22/reports

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